c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 1999010800159 19990108 00159 WP 1999 1 8 TWAA9900206 1 19990104 A 5320 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE WINDOW BURNED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 DURING OP 15 MAINT CHECK, FOUND STATIC BURN ON WINDOW FRAME NR 24L AND 27L. REPAIRED PER ARA 16076. 2 L 7 2 4F RT A6WE 1999010800164 19990108 00164 SO 1999 1 8 RAAA99E8001 1 19990102 A 3350 8631003 CONTROL MODULE LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 ON PREFLIGHT CREW REPORTED, CABIN EMERGENCY LIGHTS ON CONTINUOUSLY WHEN ARMED. CHANGED AFT EMERGENCY LIGHTS CONTROL MOD ULE DUE FAILED. 2 L 7 4 4T 4A22 1999010800167 19990108 00167 NM 1999 1 8 CALA9900001 1 19990102 A 3244 TIRE BOEING 737 7373T0 1384582 NM RT MLG FAILED A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 17344 23582 A BUMP WAS FELT ON THE RT MLG WITH GEAR HANDLE IN THE UP AND OFF POSITION AFTER TAKEOFF. ALSO, THE RT MLG RED UNSAFE LI GHT WAS ILLUMINATED. THE AIRCRAFT WAS RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE NR 3 MLG TIRE HAD THROWN TREAD ENTANGLED IN GEAR. THE TREAD WAS REMOVED AND THE RT MLG WAS INSPECTED WITH NO DEFECTS NOTED . THE NR 3 AND NR 4 MLG TIRE AND WHEEL ASSEMBLIES WERE REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1999010800169 19990108 00169 WP 1999 1 8 CALA9900003 1 19990102 A 3260 833703 SWITCH DOUG DC9 DC982 3022082 WP LT MLG INOP A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 57837 49582 THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT DID NOT EXTINGUISH. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MLG UPLOCK P ROXIMITY SWITCH IAW MM 32-60-05. ALSO, THE PROXIMITY SWITCH PLUG R5-1152 AND PINS WERE REMOVED AND REPLACED. AN ADJUST MENT/TEST WAS PERFORMED IAW MM 32-60-05, PAGE 201 AND ALL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1999010800172 19990108 00172 SO 1999 1 8 COMA9910003 1 19990103 A 3010 DEICE BOOT EMB 120 EMB120RT SO WING FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 189CA 120189 INBOARD SECTION OF LEADING EDGE DEICE BOOTS FAILED. COULD NOT DUPLICATE DISCREPANCY. INSPECTED DEICE BOOTS AND AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999010800173 19990108 00173 SO 1999 1 8 COMA9910004 1 19990104 A 2910 HYD FLUID EMB 120 EMB120RT SO RIGHT CONTAMINATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 179CA 120179 RIGHT HAND HYDRAULIC RESERVOIR LOW PRESSURE WARNING. REMOVED CONDENSATE WATER FROM RESERVOIR. 2 L 7 2 4T RT A31SO 1999010800174 19990108 00174 EA 1999 1 8 COMA9960005 1 19990104 A 5210 H2912A SPRING CNDAIR CL600 CL6002B19 EA PAX DOOR WORN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 954CA 7100 CABIN DOOR OUTER HANDLE MESSAGE. REPLACED THE OUTER HANDLE LATCH SPRING. 2 L 7 2 4F RT A21EA 1999010800175 19990108 00175 EA 1999 1 8 COMA9960006 1 19990103 A 5710 STRUCTURE CNDAIR CL600 CL6002B19 EA RT WING DAMAGED A COMA K NONE C F.O.D. TX TAXI/GRND HDL 1 SO 01 963CA 7127 DURING TAXI, THE RIGHT HAND WING STRUCT A POWER CART. REPAIRED WING. 2 L 7 2 4F RT A21EA 1999010800176 19990108 00176 EA 1999 1 8 COMA9960007 1 19990104 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 709CA 7238 CABIN DOOR LATCH MESSAGE. COULD NOT DUPLICATE DISCREPANCY. INSPECTED DOOR, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999010800177 19990108 00177 EA 1999 1 8 COMA9960008 1 19990102 A 3010 14463101 PICCOLO TUBE CNDAIR CL600 CL6002B19 EA RT WING CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 938CA 7046 WING ANTI ICE DUCT LEAK WARNING. REPLACED RIGHT HAND WING PICCOLO TUBE. 2 L 7 2 4F RT A21EA 1999010800178 19990108 00178 EA 1999 1 8 COMA9960009 1 19990102 A 3230 SENSOR CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 759CA 7279 LANDING GEAR FAILED TO RETRACT. ADJUSTED NLG PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 1999010800179 19990108 00179 EA 1999 1 8 COMA9960010 1 19990102 A 3230 SWITCH CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 988CA 7204 GEAR DISAGREE MESSAGE, NLG DID NOT RETRACT. ADJUSTED NLG WEIGHT ON WHEELS PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 1999010800180 19990108 00180 NM 1999 1 8 UPS99228317 1 19990104 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, 3 EXIT IDENTIFER LIGHTS OUT AT EMERG EXIT WINDOWS. REMOVED AND REPLACED BATT PACKS AS ABOVE, OPS G OOD. 2 L 7 3 4F A3WE 1999010800209 19990108 00209 EU 1999 1 8 QXEA9802117 1 19990103 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 & 9 INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 480AU 11229 CEILING EXIT SIGN AT ROW 8 AND 9 INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN CIRCUIT BOARD, OPERATIONAL TEST NORMAL . 2 L 7 2 4F RT A20EU 1999010800210 19990108 00210 EU 1999 1 8 QXEA9802118 1 19990102 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 4624 317 11234 THREE CABIN CEILING EVACUATION LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE FORWARD RIGHT PASSENGER COMPARTMENT POWER SUPPLY AND OPERATIONALLY TESTED IT, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1999010800212 19990108 00212 EU 1999 1 8 99FDEA00001 1 19990101 A 2910 O RING AIRBUS 310 A310203 EU NR 1 ENGINE FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 401FE 191 BLUE HYD QTY DROP TO RED DOT AND ECAM WARN ANNUNCIATED. RED TAB PROC FOLLOW PTU TURN ON FOR APPROACH AND LAND. FOUND B LUE SERVO CONTROL FILTER MODULE LEAK ON NR 1 ENG. REMOVED AND REPLACED O-RING ON FILTER BOWL REF MM 29-22-13, LEAK CK G OOD. 2 L 7 2 4F RT A35EU 1999010800213 19990108 00213 NM 1999 1 8 99FDEA00003 1 19990105 A 3260 DOWN LOCK SW BOEING 727 727227 1384078 NM TAIL SKID FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 494FE 21532 TAIL SKID LIGHT ON AFTER TAKEOFF. RECYCLE GEAR, NO SUCCESS. *S/D* REMOVED AND REPLACED DOWN LOCK SWITCH S662 NR MS250 11-1 PER MM 32-71-101. CK ADJUSTMENT OF SWITCH S663 PER MM 32-71-91. CYCLED TAIL SKID, COULD NOT DUP PROBLEM. 2 L 7 3 4F A3WE 1999010800214 19990108 00214 EU 1999 1 8 99FDEA00004 1 19990106 A 2760 RETRACT MECH AIRBUS 310 A310222 3930315 EU NR 1 SPOILER MALFUNCTIONED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 420FE 339 NR 1 SPOILER DEPLOY DURING TAKEOFF ROLL, SPEED 90 KTS. TAKEOFF REJECTED. FOUND NORM OPS TEST OF GROUND SPOILERS AND SP EED BRAKES, CARRIED OUT IAW MM 27-61-00 PG 511, PARA 2 FOUND NORMAL. 2 L 7 2 4F RT A35EU 1999010800215 19990108 00215 EU 1999 1 8 99FDEA00002 1 19990105 A 3230 D224260003 PITCH DAMPER AIRBUS 310 A310203 EU LT MLG LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 415FE 349 AIR TURNBACK, CREW CALLED GEAR AND GEAR WOULD NOT RETRACT. *S/D* REMOVED AND REPLACED LT BOGIE PITCH DAMPER PER MM 32- 11-15. LEAK CK C/W, NO LEAKS NOTED. 2 L 7 2 4F RT A35EU 1999010800216 19990108 00216 WP 1999 1 8 MWEA990001 1 19990104 A 5320 49122611 SPLICE DOUG DC9 DC932 3022066 WP BS 224 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND HEAVY CORROSION AT FORWARD CARGO COMPARTMENT LONGERON SPLICE 28L AT FS 224. MTC REMOVED CORROSION, FABRICATED AND INSTALLED LONGERON SPLICE. 2 L 7 2 4F A6WE 1999010800217 19990108 00217 WP 1999 1 8 MWEA990002 1 19990104 A 5320 2913045501 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 351-362 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CORROSION ON FORWARD CARGO COMPARTMENT INTERCOSTAL LEFT SIDE FROM FUSELAGE 351 TO 362 AT LONGERON 29L. MTC FABRIC ATED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 1999010800218 19990108 00218 WP 1999 1 8 MWEA990003 1 19990104 A 5320 39132911 SPLICE DOUG DC9 DC932 3022066 WP BS 907 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CORROSION ON FORWARD END OF LONGERON SPLICE AT LONGERON 29 LEFT STATION 907. MTC FABRICATED AND INSTALLED NEW SPL ICE SECTION. 2 L 7 2 4F A6WE 1999010800219 19990108 00219 WP 1999 1 8 MWEA990004 1 19990104 A 5350 3920460501 LATCH DOUG DC9 DC932 3022066 WP TAILCONE OUT OF ADJUST A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 MKE - FOUND TAILCONE DEPLOY TENSION LOW. MAINTENANCE LUBRICATED AND ADJUSTED LATCHES. (X) 2 L 7 2 4F A6WE 1999010800221 19990108 00221 WP 1999 1 8 MWEA990006 1 19990104 A 5320 59114073 SKIN DOUG DC9 DC914 3022034 WP SERVICE DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK IN LOWER FORWARD RADIUS OF FORWARD SERVICE DOOR JAMB OUTER SKIN. MTC FABRICATED AND INSTALLED DOUBLER REPAI R. 2 L 7 2 4F A6WE 1999010800224 19990108 00224 NE 1999 1 8 DHL99724001 2 19990102 A 7230 COMPRESSOR BOEING 727 727228 NM PWA JT8 JT8D7 52053 NE NR 3 ENGINE STALLED A DHLA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 01 724DH 19862 657618 NUMBER 3 ENGINE HAS SEVERE COMPRESSOR STALL AFTER TAKEOFF. ENGINE SHUT DOWN AND DIVERTED TO TAKEOFF ALTERNATE AT MCI. R EMOVED AND REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999010800226 19990108 00226 WP 1999 1 8 TWAA9900101 1 19990103 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP EXTERIOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9624T 53594 FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F RT A6WE 1999010800227 19990108 00227 NM 1999 1 8 TWAA9900102 1 19990103 A 3350 58222 BATTERY PACK BOEING 727 727231 1384079 NM ROW 10-17 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 84355 21987 FOUND EMERGENCY EGRESS LIGHTS BETWEEN ROWS 10 AND 17 INOPERATIVE. REPLACED BATTERY PACK. CHECK-C 2-21-98 MCI. 2 L 7 3 4F A3WE 1999010800258 19990108 00258 EA 1999 1 8 COMA9960003 1 19990101 A 2752 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA RT TE FLAP DEFECTIVE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 716CA 7250 FLAPS FAILED DURING APPROACH. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 1999010800261 19990108 00261 NM 1999 1 8 QXEA9802116 1 19990101 A 5210 MECHANISM DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR TO BE STICKING WHEN OPENING FROM INSIDE THE CABIN. MAINTENANCE CLEANE D AND LIGHTLY LUBRICATED THE OVERCENTER CONTROL AND TRACK FOR THE GAS SPRING SLIDER, OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999010800296 19990108 00296 NM 1999 1 8 DL757990001 1 19990101 A 2131 CONTROLLER 211738813 BOEING 757 757232 1384965 NM E & E COMPT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 662DN 115886 24991 AUTO 1 PRESSURIZATION FAILURE AT 31,000 FT. CABIN ALT WARNING CAME ON, DID NOT EXCEED 10,000 FT. REPLACED 1 PRESS CONT ROLLER. BITE FAULTS SELECT PANEL. REPLACED SAME. PRESS A/C, ALL OPS NORMAL. 2 L 7 2 4F RT A2NM 1999010800297 19990108 00297 NM 1999 1 8 DL757990002 1 19990102 A 2622 FIRE EXT 51211 BOEING 757 757232 1384965 NM CABIN REQD SERVICE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 629DL 22919 FIRST CLASS HALON FIRE EXT OUT OF GREEN BAND. REPLACED HALON BOTTLE. 2 L 7 2 4F RT A2NM 1999010800298 19990108 00298 NM 1999 1 8 DLM88990003 1 19990102 A 2611 267201934 SMOKE DETECTOR DOUG MD88 MD88 3023688 NM LAVATORY FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 954DL 49885 AFT LT LAV SMOKE DETECTOR WOULD NOT TEST. REPLACED BATTERY, NO HELP. REPLACED DETECTOR ASSY, OPS CK NORMAL. 2 L 7 2 4F RT A6WE 1999010800299 19990108 00299 NM 1999 1 8 DLM88990004 1 19990103 A 2611 PC1604 BATTERIES DOUG MD88 MD88 3023688 NM LAV SMOKE DET DISCHARGED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 906DE 53415 LEFT AFT LAV SMOKE DETECTOR WENT OFF ON TAKEOFF. PRECAUTIONARY LANDING AT KLGA. INSPECTED A/C OVENS AND VENTILATION SY STEM. ALSO, INSPECTED TAIL CONE AREA, INCLUDING BOTH PACKS. RAN PACKS, NO SMOKE NOTED. REPLACED BATTERIES IN BOTH AFT LAVS SMOKE DETECTORS AS PRECAUTION. 2 L 7 2 4F RT A6WE 1999010800321 19990108 00321 NM 1999 1 8 SWAA990001 1 19990103 A 5313 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 26R AT AFT GALLEY CORRODED. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999010800322 19990108 00322 NM 1999 1 8 SWAA990002 1 19990102 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 626SW 27702 DURING SCHEDULED A2 CHECK, FOUND 2 AFT CABIN EMERGENCY FLASHLIGHTS OUT OF DATE. REPLACED BATTERIES PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010800323 19990108 00323 NM 1999 1 8 SWAA990003 1 19990102 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 626SW 27702 DURING SCHEDULED A2 CHECK, FOUND 2 FWD CABIN EMERGENCY FLASHLIGHTS OUT OF DATE. REPLACED BATTERIES PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010800324 19990108 00324 1999 1 8 SWAA990004 4 19990102 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED SC CHECK, FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLI DE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010800325 19990108 00325 NM 1999 1 8 SWAA990005 1 19990102 A 3350 AD20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED SC CHECK, FOUND CABIN EMERGENCY LIGHTS AFT OF WING INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010800326 19990108 00326 NM 1999 1 8 SWAA990006 1 19990101 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED SC CHECK, AFT ENTRY EMERGENCY LIGHT INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010800327 19990108 00327 NM 1999 1 8 SWAA990007 1 19990101 A 3350 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SC CHECK, FOUND SEVERAL AFT CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1999010800328 19990108 00328 NM 1999 1 8 SWAA990008 1 19990102 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 LT O/B CHORD CRACKED AT WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999010800329 19990108 00329 NM 1999 1 8 SWAA990009 1 19990102 A 2120 AIR DIST BOEING 737 7373H4 1384600 NM CABIN ODOR A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 626SW 27702 F/A REPORTED, STRONG ELECTRICAL SMOKE TYPE ODOR, NO VISIBLE SMOKE VICINITY OF ROWS 18 TO 20. ALSO, CAPT (POSSIBLE AFTER FA CALL BUTTON USE) SAW EVIDENCE OF LIQUID SPILL IN OVERHEAD BIN IN THAT AREA. LOWERED PSU'S AT SEAT ROWS 18 TO 20 LT SIDE, INSPECTED AREAS AND NO DEFECTS FOUND. PERFORMED OPS CKS OF PSU'S, ALL CHECKED OK PER M/M. 2 L 7 2 4F RT A16WE 1999010800330 19990108 00330 NM 1999 1 8 SWAA990010 1 19990102 A 3320 BULB BOEING 737 7372T4 1384492 NM CABIN FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 722WN 22698 SMOKE REPORTED COMING FROM AROUND FORWARD LOWER ENTRY LIGHT RECEPTACLE AND HOLE NEAR RECEPTACLE. INSPECTED AREA AND FOU ND BULB INOP. INSTALLED NEW BULB, OPS CHECK OK. NO SMOKE NOTED. 2 L 7 2 4F A16WE 1999010800331 19990108 00331 NM 1999 1 8 SWAA990011 1 19990101 A 2170 COALESCER BAG BOEING 737 7372H4 138448C NM AC BAY DIRTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 105SW 23249 DURING DESCENT PASSING APPROX 1500 FT, A STRONG SMELL WAS EVIDENT IN THE COCKPIT OF TURBO OIL. SMELL CONTINUED UNTIL SH UTDOWN AT GATE. SERVICED AIR CYCLE MACHINE AND CHANGED WATER SEPARATOR BAG, LEAK CK AND OPS CK GOOD PER M/M. 2 L 7 2 4F A16WE 1999010800332 19990108 00332 NM 1999 1 8 SWAA990012 1 19990103 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM PAX DOORWAY INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PE R BOEING M/M. 2 L 7 2 4F A16WE 1999010800333 19990108 00333 NM 1999 1 8 SWAA990013 1 19990103 A 3350 BULB BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SC CHECK, FOUND FWD SEGMENT WHITE LIGHT OF FLOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F A16WE 1999010800334 19990108 00334 1999 1 8 SWAA990014 2 19990101 A 7200 ENGINE BOEING 737 7373H4 1384600 NM NR 1 BIRD STRIKE A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 620SW 28036 CREW EXPERIENCED A BIRD STRIKE TO NR 1 ENGINE, SLIGHT PARAMETER FLUCTUATION AND SMELL IN CABIN, ENGINE OPERATION WAS NOR MAL. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND EVIDENCE OF CORE INGESTION. NO SHIN GLED BLADES OR DAMAGE NOTED. PERFORMED ENGINE RUN TO T/O POWER PER M/M, ALL OK. ENGINE PLACED ON A 10 CYCLE FLYBACK FO R BORESCOPE INSPECTION. 2 L 7 2 4F RT A16WE 1999010800335 19990108 00335 NM 1999 1 8 SWAA990015 1 19990102 A 2612 D4834PD4574P CONNECTOR BOEING 737 7372H4 138448C NM WHEEL WELL DIRTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 102SW 23108 WHEEL WELL FIRE LIGHT CAME ON DURING CLIMBOUT. LOWERED GEAR, LIGHT WENT OUT. AIRCRAFT RETURNED TO DAL AND MADE AN UNEV ENTFUL LANDING. CLEANED CONNECTOR D4834P AND D4574P, OPS CHECKED GOOD PER M/M. 2 L 7 2 4F A16WE 1999010800384 19990108 00384 1999 1 8 TWAA9900301 4 19990104 A 2565 100504203 SLIDE DOUG DC9 DC982 3022082 WP PAX DOOR LEAKING AIR A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 917TW 49366 THE FORWARD LEFT CABIN DOOR EVACUATION SLIDE WAS FOUND WITH DEPLETED BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHE CK-C 7-15-98 MCI. 2 L 7 2 4F A6WE 1999010800385 19990108 00385 WP 1999 1 8 CALA9900005 1 19990105 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG LOW PRESSURE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 18563 47487 THE LANDING GEAR HANDLE WOULD NOT RAISE PAST UP LATCH CHECK POSITION AND GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRC RAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE NOSE GEAR STRUT WAS SERVICED IAW MM 32-21-2 AND THE GROU ND SHIFT MECHANISM WAS CHECKED IAW MM 32-23-1. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1999010800386 19990108 00386 WP 1999 1 8 CALA9900006 1 19990102 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 THE TAIL CONE RELEASE PULL WAS BELOW LIMITS WHEN USING INTERIOR OR EXTERIOR TAIL CONE HANDLE. THE CABLES, LATCHES AND C LIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1999010800387 19990108 00387 WP 1999 1 8 CALA9900007 1 19990104 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 284 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 6 INCH CRACK IN RT WING LEADING EDGE SKIN AT STA XOS 284. A REPAIR WAS INSTALLED IAW ECRA 5720-01709 . 2 L 7 2 4F A6WE 1999010800388 19990108 00388 WP 1999 1 8 CALA9900008 1 19990106 A 3350 60030431 POWER SUPPLY GRIMES DOUG DC9 DC982 3022082 WP CABIN INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND MID CABIN AND SECOND SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE POWER SUPPLIES FOR EACH LOC ATION WERE REMOVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 1999010800391 19990108 00391 WP 1999 1 8 9900019140 1 19990101 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 DURING LINE CHECK, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999010800392 19990108 00392 WP 1999 1 8 9900029922 1 19990104 A 2751 SRDL12C INDICATOR DOUG DC9 DC932 3022066 WP FLAP POSITION MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 945N 47664 FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES ON LANDING. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCI DENT. MAINTENANCE REPLACED FLAP POSITION INDICATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999010800393 19990108 00393 WP 1999 1 8 9900039918 1 19990101 A 3260 301350101B PSEU DOUG DC9 DC932 3022066 WP LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 940N 4249 4249 47572 LEFT AND RIGHT MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ON AFTER GEAR EXTENSION. FLIGHT CREW DECLARED AN EMERGENCY AND VISUALLY CONFIRMED GEAR TO BE DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PSEU PROCESSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999010800394 19990108 00394 NM 1999 1 8 UPS99228321 1 19990105 A 5220 DOOR BOEING 727 727180C 138406G NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE-N/A, ACCESS DOOR FOR CAPTS OVERHEAD ESCAPE TAPE WILL NOT STAY CLOSED AREA AROUND THE DOOR LOCK IS CRACKE D. INSTALLED SERVICEABLE PANEL LIGHTS, OPS NORMAL, ROPE WAS STOWED. 2 L 7 3 4F A3WE 1999010800395 19990108 00395 NM 1999 1 8 UPS99228322 1 19990105 A 3350 LIGHT BOEING 727 72730C 1384009 NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT AT MAIN PAX DOOR INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999010800396 19990108 00396 NM 1999 1 8 UPS99228323 1 19990105 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-N/A, REAR EXIT EEL INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999010800397 19990108 00397 NM 1999 1 8 UPS99228324 1 19990105 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-N/A, GALLEY EEL INOP. REMOVED AND REPLACED GALLEY EXIT EMERG LIGHT BATT PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999010800398 19990108 00398 NM 1999 1 8 UPS99228325 1 19990105 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-N/A, ROWS 4, 9, 11, 13, 15, 17, 19 EMERG EXIT LIGHTS INOP. REMOVED AND REPLACED BATT PACKS AS ABOVE, OP S CHECK GOOD. 2 L 7 3 4F A3WE 1999010800399 19990108 00399 NM 1999 1 8 UPS99228326 1 19990105 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-N/A, FWD ENTRY EEL INOP TOP AND BOTTOM. REMOVED AND REPLACED EEL BATT PACKS AS ABOVE, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999010800400 19990108 00400 1999 1 8 99FDEA00006 4 19990106 A 2340 JACK AIRBUS 300 A300F4605R 3930327 EU LT COCKPIT LOOSE A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 660FE 759 EXTREME STATIC ON INTERPHONE SYS DURING T/O ROLL. SHUT PHONE SWITCH TO HEAR RADIO. REMOVED CAPTS BOOM MIKE AND HEADSET CONNECTOR PANEL, FOUND RECEIVER JACK LOOSE. TIGHTENED JACK, OPS CK NR 1 VHF PER MM 23-10-00 AND INTERPHONE PER MM 23-4 0-00. 2 L 7 2 4F RT A35EU 1999010800407 19990108 00407 NM 1999 1 8 MWEA99016 1 19990105 A 7830 5938059 NOZZLE DOUG MD88 MD88 3023688 NM RT TR UNIT MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 808ME 48070 THE RIGHT THRUST REVERSER EXHAUST NOZZLE EXTERIOR SURFACE HAS A REPAIR NOT APPLICABLE TO THE MD88. MTC REMOVED AND REPL ACED THRUST REVERSER. 2 L 7 2 4F RT A6WE 1999010800408 19990108 00408 WP 1999 1 8 MWEA99017 1 19990105 A 5320 4912540501 FITTING DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CRACKED FLOORBEAM FITTING AT STATION 965 ABOVE LONGERON 23L ON TOP OF VERTICAL FRAME. MTC FABRICATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999010800409 19990108 00409 NM 1999 1 8 SCNA98157 1 19990102 A 2150 INLET BOEING 727 727225 1384077 NM LT & RT PACK FOD A SCNA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 15 282SC 22558 DURING CLIMBOUT CREW REPORTED UNCONTROLLABLE DUCT TEMPERATURE FOLLOWED BY A PACK OVERHEAT ON BOTH LEFT AND RIGHT PACKS. RETURNED AIRCRAFT TO ORD. FOUND BOTH RAM AIR INLETS BLOCKED WITH PACKED SNOW. REMOVED SNOW AND CHECKED PACK OPERATION AS NORMAL. 2 L 7 3 4F A3WE 1999011500002 19990115 00002 NM 1999 1 15 TWAA9900401 1 19990106 A 3230 69141065 CYLINDER BOEING 727 727231 1384079 NM NLG WORN A TWAA O OTHER J WARNING INDICATION LD LANDING 1 CE 05 54351 21983 ON FIRST GEAR EXTENSION, THE NOSE GEAR DID NOT EXTEND. THE DOORS STAYED CLOSED. RECYCLED THE GEAR AND OPERATION WAS NO RMAL. REPLACED THE NOSE LANDING GEAR TRANSFER CYLINDER. CHECK-C 11-19-98 MCI. 2 L 7 3 4F A3WE 1999011500003 19990115 00003 NM 1999 1 15 AT9900001 1 19990105 A 3397 WIRE BOEING 737 737284 138448R NM ROW 10 DEF DAMAGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 470AT 21501 DURING LAYOVER CHECK, FOUND EMERGENCY PATH LIGHTING AT ROW 10 DEF BROKEN. REPAIRED DAMAGED WIRES PER B737 STANDARD WIRI NG MANUAL 20-10-13. 2 L 7 2 4F A16WE 1999011500007 19990115 00007 NM 1999 1 15 K3HA990001 1 19990104 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN TORN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 EMERGENCY PATH LIGHTING INOP FORWARD AFT SECTION. REPAIRED TORN WIRES AND REPLACED 2 EACH LENS MM REF 33-59-00. OPS CH ECK OK. 2 L 7 3 4F A3WE 1999011500008 19990115 00008 SO 1999 1 15 COMA9910005 1 19990103 A 2440 141CC01AY1 CONTACTOR EMB 120 EMB120RT SO EXTERNAL POWER FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 EXTERNAL POWER CONTACTOR BURNT/OVERHEATED AT TERMINAL ENDS. REPLACED CONTACTOR AND POSITIVE CABLE. 2 L 7 2 4T RT A31SO 1999011500009 19990115 00009 SO 1999 1 15 COMA9910006 1 19990106 A 3010 WARNING EMB 120 EMB120RT SO WING DEICE ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 189CA 120189 WING DEICE FAIL WARNING. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999011500010 19990115 00010 EA 1999 1 15 COMA9960011 1 19990105 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 916CA 13879 7014 CABIN DOOR WARNING. ADJUSTED DOOR LATCH CAM LINKAGE. 2 L 7 2 4F RT A21EA 1999011500011 19990115 00011 EA 1999 1 15 COMA9960012 1 19990105 A 3222 16120NLGQC STRUT CNDAIR CL600 CL6002B19 EA NLG LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 982CA 4231 7168 NLG DID NOT RETRACT WHEN GEAR SELECTED UP. REPLACED THE NLG PISTON TUBE ASSY. 2 L 7 2 4F RT A21EA 1999011500012 19990115 00012 EA 1999 1 15 COMA9960013 1 19990105 A 5610 NP139222 WINDSHIELD CNDAIR CL600 CL6002B19 EA RT COCKPIT SHATTERED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 981CA 4324 7163 CO-PILOTS SIDE WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1999011500013 19990115 00013 EA 1999 1 15 COMA9960014 1 19990106 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 716CA 7250 CABIN DOOR WARNING DURING TAKEOFF. COULD NOT DUPLICATE. NO DEFECTS FOUND WITH DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1999011500014 19990115 00014 EA 1999 1 15 COMA9960015 1 19990103 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 984CA 3870 7171 PILOTS WINDSHIELD SHATTERED.\NREPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1999011500015 19990115 00015 NM 1999 1 15 UPS99228327 1 19990106 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:N/A E/E/L INOP BY CREW ENTRY DOOR R/R FWD E/E/L WITH ROBBED PART FROM A/C 910 OPS CHECK GOOD. S/N ON 2841-8 S/N OFF 6508 2 L 7 3 4F A3WE 1999011500016 19990115 00016 WP 1999 1 15 ABXA9900001 1 19990104 A 2497 WIRE DOUG DC9 DC941 302207N WP E & E COMPT FAILED A ABXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 979AX 47492 DURING TAXI OUT, HEARD POPPING NOISE FROM AC BUS AND OBSERVED ELECTRICAL SMOKE. REPLACED BURNT WIRES AT AC BUS. 2 L 7 2 4F A6WE 1999011500017 19990115 00017 WP 1999 1 15 ABXA9900002 1 19990104 A 3350 014577201 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 901AX 47381 EMERGENCY LIGHTS WOULD NOT TEST OR ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1999011500018 19990115 00018 WP 1999 1 15 ABXA9900003 1 19990104 A 3230 RETRACT MECH DOUG DC8 DC861 3021952 WP LANDING GEAR LACK OF LUBE A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 849AX 45891 ON GEAR RETRACTION, GEAR HANDLE APPEARED TO BE HITTING STOP. RECYCLED HANDLE TWICE. GEAR CAME UP. LUBRICATED LANDING GEAR HANDLE LINKAGE. INSPECTED HANDLE AND CONTROL VALVE. NO DEFECTS NOTED. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999011500019 19990115 00019 WP 1999 1 15 ABXA9900004 1 19990106 A 5610 591297741 TRIM DOUG DC8 DC861 3021952 WP COCKPIT WINDOW BINDING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 CO-PILOT'S CLEARVIEW WINDOW (EMERGENCY EXIT ) WOULD NOT OPEN ALL THE WAY. TRIMMED WINDOW TRIM IAW DC8 MM 25-10-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999011500020 19990115 00020 WP 1999 1 15 ABXA00005 1 19990105 A 3260 7000010101ABX1 SWITCH DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 946AX 47003 LEFT MAIN GEAR SHOWED NO GREEN LIGHTS WHEN GEAR WAS SELECTED DOWN. THE GEAR UNSAFE LIGHT WAS NOT ILLUMINATED. GEAR IND ICATED DOWN AND LOCKED USING ALTERNATE INDICATION SYSTEM. DECLARED EMERGENCY. LANDING WAS UNEVENTFUL. REPLACED LEFT M AIN GEAR DOWN LOCK SWITCH. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999011500021 19990115 00021 WP 1999 1 15 MWEA99018 1 19990104 A 5320 591015837 JAMB DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CORROSION ON AFT CARGO DOOR JAMB FORWARD OUTBOARD WEB. MAINTENANCE FABRICATED AND INSTALLED REPAIR WEB. 2 L 7 2 4F A6WE 1999011500023 19990115 00023 WP 1999 1 15 SCNA99001 1 19990104 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1015 3022118 WP LT OVERWING INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 151SY 3449 48295 DURING A LINE MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCY POWER SUPPLY FAILED TEST. REMOVED AND REPLACED THE LEFT OV ERWING EMERGENCY POWER SUPPLY. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1999011500024 19990115 00024 NM 1999 1 15 DHL99740001 1 19990106 A 5210 PAX DOOR BOEING 727 7272Q9 138448M NM FUSELAGE NOT LATCHED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 740DH 21930 UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. ACCOMPLISHED ABNORMAL PROCEDURES AND RETURNED FOR LANDING. FOUND FWD ENTR Y DOOR NOT FULLY SEATED. INSPECTED DOOR AND SWITCHES. OPERATED DOOR SEVERAL TIMES. DOOR OPERATED NORMAL PER MM 52-11- 01. 2 L 7 3 4F RT A3WE 1999011500025 19990115 00025 NM 1999 1 15 VNAA9901001 1 19990102 A 5240 001A524A0100016 SERVICE DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT FUSELAGE LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 427JS 3039 A GROUND SERVICE DOOR OPEN WARNING MESSAGE ILLUMINATED DURING THE TAKEOFF. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RE TURNED TO THE GATE FOR INSPECTION. MAINTENANCE INSPECTED AND LUBED THE GROUND AIR SERVICE DOOR, IN ACCORDANCE WITH STAN DARD MAINTENANCE PRACTICES. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999011500026 19990115 00026 NM 1999 1 15 VNAA9901002 1 19990105 A 5610 17300009 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT CRACKED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 422JS 36912 3018 THE LEFT SIDE COCKPIT WINDOW CRACKED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY PROB LEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE LEFT SIDE WINDSCREEN, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56 -12-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999011500027 19990115 00027 NM 1999 1 15 TWAA9900501 1 19990107 A 3350 900835A BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54354 21986 THE FLOOR EMERGENCY EXIT LIGHTING AT ROWS 16 TO 18 WERE FLASHING. REPLACED BATTERY PACK. CHECK-C 5-21-98 MCI. 2 L 7 3 4F A3WE 1999011500028 19990115 00028 NM 1999 1 15 HNAA9900001 1 19990106 A 2611 302313 FIRE LOOP DHAV DHC8 DHC8102 2809003 NM BAGG COMPT OUT OF POSITION A HNAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 07 960HA 326 BAGGAGE COMPARTMET SMOKE WARNING LIGHT CAME ON IN FLIGHT INTERMITTENTLY. NO EVIDENCE OF SMOKE. INSPECTED DETECTOR WIRI NG AND FOUND RUB MARKS ON CONNECTOR I-J3. REPOSITIONED WIRING. REPLACED NR 2 SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 1999011500029 19990115 00029 NM 1999 1 15 HNAA9900003 1 19990105 A 5210 503006 VALVE DHAV DHC8 DHC8102 2809003 NM PAX DOOR MALFUNCTIONED A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 981HA 378 UNABLE TO OPEN PASSENGER DOOR FROM INSIDE AIRCRAFT. CYCLED DOOR OPEN/CLOSED. OPERATIONAL CHECKED GOOD. SUSPECT ICE AC CUMULATION IN DOOR SEAL PRESSURE VALVE. FOLLOWUP REPLACEMENT PER SERVICE BULLETIN 8-52-46. 2 H 7 2 4T RT A13NM 1999011500030 19990115 00030 NM 1999 1 15 HNAA9900002 1 19990105 A 3350 BATTERY DHAV DHC8 DHC8201 2809001 NM CABIN DISCHARGED A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 991HA 431 EMERGENCY EXIT SIGNS ABOVE ROW 4 (LT AND RT), EMERGENCY LIGHT OVER AIRSTAIR DOOR, 2 EMERGENCY LIGHTS AT SEAT 1F AND LIGH TS AT ROW 4 INOPERATIVE. REPLACED ALL EMERGENCY LIGHT BATTERIES, P/N 60-1321-1X, SERIAL NUMBERS ORF13, SBY18, ORF077, O RF41, ORF128, SBY43. 2 H 7 2 4T RT A13NM 1999011500032 19990115 00032 WP 1999 1 15 AT9900005 1 19990106 A 2120 AIR DIST DOUG DC9 DC932 3022066 WP CABIN ODOR A ZZDA O OTHER J WARNING INDICATION AP APPROACH 1 SO 15 813AT 47318 DURING FLIGHT, THE AFT LAVATORY SMOKE DETECTOR SOUNDED FLIGHT ATTENDANT REPORTED NO SMOKE, BUT VERIFIED SMOKE ALARMS DID SOUND. AIR CONDITIONING SMOKE PROCEDURES FOLLOWED O2 MASK DON BY CREW, PILOT'S UNABLE TO DETERMINE WHICH PACK WAS CAUS ING SOME SLIGHT SMELL. PER FLIGHT ATTENDANT SMELL AND SMOKE CEASED DURING NON NORMAL CHECK LIST. INSPECTED DUCTING NO DEFECT NOTED, RESIDUAL SMELL WAS FROM APU OIL LEAK PREVIOUSLY DEFFERED. NO SMELL NOTED FOR LAST FLIGHT HOUR AND NO SMEL L NOTED ON GROUND CHECK. OK FOR FLIGHT. 2 L 7 2 4F A6WE 1999011500033 19990115 00033 NM 1999 1 15 AT9900006 1 19990109 A 3350 900835W BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 467AT 22055 FOUND BAD CONNECTION ON BATTERY PACK WHILE TROUBLESHOOTING EMERGENCY LIGHTING AT RIGHT EMERGENCY EXIT OVERHEAD. REMOVED AND REPLACED BATTERY PACK IAW B737 SRM 33-51-31. (X) 2 L 7 2 4F A16WE 1999011500034 19990115 00034 EU 1999 1 15 MALA976283 1 19990105 A 3230 UPLOCK JACK BAC 146 AVRO146RJ85A 1500097 EU LT MLG ICED UP A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 503XJ E2310 LT MLG UP AND LOCKED INDICATION INOP. AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND ICE AROUND UPLOCK JACK. CLEANED AND LUBED LT AND RT UPLOCK JACKS. INSPECTED MAIN GEARS. OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999011500035 19990115 00035 EU 1999 1 15 MALA976284 1 19990107 A 3060 VP3557 DEICE LEADS SAAB SF340 SF340A 7850100 EU LT PROP FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 109XJ 340A109 LT PROP CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. REPLACED ALL FOUR BLADE DEICE LEADS. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999011500036 19990115 00036 EU 1999 1 15 MALA976285 1 19990103 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOP A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 443XJ 443 FA'S EMERGENCY LIGHT ARMED INOP. MAINTENANCE RELAMPED LIGHT. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999011500037 19990115 00037 EU 1999 1 15 MALA976286 1 19990104 A 3150 006WS00 WEU SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 429XJ 429 EMERGENCY LIGHTS UNARMED INDICATOR SAYS ILLUMINATED IN AMED POSITION. MAINTENANCE REPLACED WEU. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999011500042 19990115 00042 NM 1999 1 15 AWXA9900001 1 19990104 A 5330 SKIN BOEING 737 737277 1384570 NM BS 760 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 FOUND CRACK AT STA 760 STR 17 RT. CRACK WAS VERIFIED WITH HFEC. COMPLIED WITH REPAIR PER SRM 53-30-03. INSTALLED DOUB LER OUT OF 2024 T3 .063. 2 L 7 2 4F RT A16WE 1999011500043 19990115 00043 EU 1999 1 15 AWXA9900002 1 19990101 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 618AW 304 DISCREPANCY PILOT REPORT, PLEASE CHECK EMERGENCY EXIT FLOOR LIGHTS. REMOVED AND REPLACED BURNDY BLOCK NR 5 OF 7202VT. F LOOR PROX LIGHTING OPS CK GOOD. 2 L 7 2 4F RT A28NM 1999011500052 19990115 00052 WP 1999 1 15 9900069139 1 19990101 A 5320 DOUBLER DOUG DC9 DC914 3022034 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING M CHECK, FOUND FS 83.5 INNERMOST DOUBLER CRACKED. REPAIRED PER EA 91-159583 AND SB 5300-01041-2, REV.A. 2 L 7 2 4F A6WE 1999011500053 19990115 00053 WP 1999 1 15 9900079139 1 19990101 A 5610 FRAME DOUG DC9 DC914 3022034 WP CTR WINDSHIELD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING PERIODIC CHECK, FOUND CENTER WINDSHIELD FRAME Z CRACKED. REPAIRED PER EA 91-163368. 2 L 7 2 4F A6WE 1999011500054 19990115 00054 WP 1999 1 15 9900041224 1 19990104 A 2133 OUTFLOW VALVE DOUG DC10 DC1030 3023501 WP CABIN MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 01 224NW 46581 DURING DESCENT INTO MSP, LOST CABN PRESSURE AT APPROXIMATELY 36,000 FEET AND MASKS DEPLOYED. CABIN PRESSURE WAS RESTORE D MANUALLY, AT APPROXIMATELY 6,000 FEET, CABIN PRESSURE WAS LOST AGAIN. FLIGHT CONTINUED INTO MSP AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED THE OUTFLOW VALVE GEARBOX AND BUTTERFLY VALVE. MASKS WERE RESET. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999011500055 19990115 00055 WP 1999 1 15 9900059950 1 19990101 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1999011500056 19990115 00056 NM 1999 1 15 UPS99228328 1 19990104 A 5512 652791715 PANEL BOEING 727 727172C 1384058 NM LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:C CORROSION (C53-391-20-00-01) ON LT ELEVATOR BALANCE PNL NR 5 ON WEIGHT ATTACH STOP. REMOVED WEIGHT AT TACH STRIP AND NR 5 BALANCE PNL. REPLACED WITH NEW WEIGHT ATTACH STRIP AND PNL NR 5 IAW SRM 51-30-2 AND SRM 51-30-5, SR M 51-80-5. 2 L 7 3 4F A3WE 1999011500057 19990115 00057 WP 1999 1 15 UPS99828330 1 19990107 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 810UP 46001 EEL INOP. REMOVED AND REPLACED EEL BATTERY PACK, OPS CHK GOOD. 2 L 7 4 4F RT 4A25 1999011500082 19990115 00082 NM 1999 1 15 99FDEA00007 1 19990109 A 2780 RETRACT MECH BOEING 727 72725C 138400H NM NR 6 LE SLAT MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 136FE 19855 99-0007 - DURING FLAP RETRACT, NR 6 SLAT DID NOT FULLY RETRACT. UNABLE TO CORRECT WITH RED TAB PROC. INSPECT SLAT, NO DEFECT FOUND. RAN NR 1 ENG WITH HYD PRESS, EXTEND AND RETRACT ALL LEAD EDGE DEVICE WITH NO FAULT OR PROBLEM FND. MOCC NOTIFIED, AC OK FOR FLT. 2 L 7 3 4F A3WE 1999011500083 19990115 00083 NM 1999 1 15 99FDEA00008 1 19990109 A 2750 MS9391130ZE4C DRIVE MOTOR BOEING 727 727233 138408A NM RT TE FLAP FAILED A FDEA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 279FE 22346 SPLIT FLAP I/B UP, O/B STUCK AT 2 DEG. FOLLOWED AC FLT MAN PROCEDURE, GOT AC CLEAN UP, LOST SYS A QUAN AND PRESS. ALT FLAPS USED, GROUND PROX FLAP INHIBIT CKLIST COMPLETE. WHILE REPLEN A SYS FLUID LOSS OUT OF SHAFT SEAL CAVITY DRAIN ON R T HYD FLAP MOTOR. *S/D* REMOVED AND REPLACED RIGHT FLAP HYD DRIVE MOTOR PER MM 27-51-062-4. FLAP DRIVE MOTOR REQUIRES OPER AND LEAK CK. RAN FLAPS OPER AND LEAK CK OK PER 27-51-062-4. 2 L 7 3 4F RT A3WE 1999011500086 19990115 00086 SO 1999 1 15 SWIA971357 1 19990109 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA O OTHER J WARNING INDICATION LD LANDING 1 NM 07 188SW 120039 FLAP FAULT INBOARD FLAPS. ASYMMETRY FAULT INBOARD PAIR DID NOT RESPOND. REPLACED FLAP CONTROL UNIT WITH SERVICEABLE PA RT. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500087 19990115 00087 NM 1999 1 15 SWAA990016 1 19990104 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 AFT EMERGENCY EXIT FLOOR TRACK LIGHINTING INOPERATIVE(APPROX 10FT). REPAIRED BROKEN WIRE PER M/M. 2 L 7 2 4F RT A16WE 1999011500088 19990115 00088 NM 1999 1 15 SWAA990017 1 19990105 A 3350 BULB BOEING 737 7373H4 1384600 NM ROW 14 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED SC CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT ROW 14, RELAMPED PER M/M. 2 L 7 2 4F RT A16WE 1999011500089 19990115 00089 NM 1999 1 15 SWAA990018 1 19990106 A 3350 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 609SW 27929 FOUND EMERGENCY TRACK LIGHTING INOP AT MID CABIN AREA. RECONNECTED WIRING AND OP CHECKED PER M/M. 2 L 7 2 4F RT A16WE 1999011500090 19990115 00090 NM 1999 1 15 SWAA990019 1 19990106 A 3350 6104781 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SC CHECK, FOUND AFT SECTION OF EMERGENCY TRACK LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK PER M/ M. 2 L 7 2 4F A16WE 1999011500091 19990115 00091 NM 1999 1 15 SWAA990020 1 19990105 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT FASTENER HOLE AND UPPER CHORD, BS 312. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1999011500092 19990115 00092 NM 1999 1 15 SWAA990021 1 19990105 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND NUMEROUS CRACK LOCATIONS IN WEB AT BS 178. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500093 19990115 00093 NM 1999 1 15 SWAA990022 1 19990105 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5. REPLACED T-CHORD PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500094 19990115 00094 NM 1999 1 15 SWAA990023 1 19990105 A 5320 CLIP BOEING 737 7373A4 1384585 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 663, AT S10L AND R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500095 19990115 00095 NM 1999 1 15 SWAA990024 1 19990105 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT FWD FLANGE LOWER SURFACE, BS 1016. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500096 19990115 00096 NM 1999 1 15 SWAA990025 1 19990105 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED NEAR Z ANGLE AT AFT ENTRY DOOR. REPLACED T CHORD PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500097 19990115 00097 NM 1999 1 15 SWAA990026 1 19990105 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED UNDER STRAP AT BS 727D PLUS 6 RBL 8 AND LBL 13. REPAIRED PER SWA RA 1-353-1972. 2 L 7 2 4F RT A16WE 1999011500098 19990115 00098 NM 1999 1 15 SWAA990027 1 19990105 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 745 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 745, BETWEEN S19 AND 20L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500099 19990115 00099 NM 1999 1 15 SWAA990028 1 19990105 A 2120 AIR DIST BOEING 737 7372H4 138448C NM CABIN ODOR A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 089SW 22904 DURING CLIMB-OUT, CREW NOTED A ODOR/SMELL IN CABIN. AIRCRAFT RETURNED TO AMA AND MADE AN UNEVENTFUL LANDING. CHECK ENG INES AND AC PACKS. NO DEFECTS. RAN PACKS, APU AND ENGINES, ODOR CLEARED 2 L 7 2 4F A16WE 1999011500100 19990115 00100 NM 1999 1 15 SWAA990029 1 19990104 A 5314 KEELBEAM BOEING 737 7372H4 138448C NM BS 650 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND CRACK IN LT KEEL BEAM AT BS 650. REPAIRED PER TRAMCO EWO 98-1176. 2 L 7 2 4F A16WE 1999011500101 19990115 00101 NM 1999 1 15 SWAA990030 1 19990104 A 5312 BULKHEAD TEE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/4 CHECK, FOUND BS 178 T CHORD CRACKED AT WL 184, LBL 5.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500102 19990115 00102 EU 1999 1 15 SWAA990031 2 19990106 A 7230 FAN BLABE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE DAMAGED A SWAA A UNSCHED LANDING C F.O.D. CR CRUISE 1 SW 07 672SW 23406 DURING CLIMB-OUT FROM SMF WE HIT A FLOCK OF LARGE BIRDS, ONE OR MORE IMPACTED NR 2 ENGINE. THE ENGINE RAN NORMAL AT IDL E POWER, BUT WE HAD AIRFRAME VIBRATION AND A BURN SMELL FROM THE RIGHT PACK. AIRCRAFT DIVERTED INTO OAK AND MADE AN UNE VENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION PER 5-51-37. FOUND FAN BLADES NR 20 AND NR 21 WITH EXCESSIVE DISTORTI ON. REMOVED AND REPLACED AND REPOSITIONED BLADES AND REMOVED AND REPLACED ENG NOSE COWL PER MM. PERFORMED HIGH POWER R UN OK PER MM. 2 L 7 2 4F 4 F RT A16WE E21EU 1999011500103 19990115 00103 NM 1999 1 15 SWAA990033 1 19990106 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1006 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1006, AT S12L. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500104 19990115 00104 NM 1999 1 15 SWAA990034 1 19990106 A 5330 SKIN BOEING 737 7372H4 138448C NM SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND CRACK IN LOWER HINGE CUTOUT OF AFT SERV DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500105 19990115 00105 NM 1999 1 15 SWAA990035 1 19990106 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 380-520 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FWD CARGO FLOORBEAM CORRODED FROM 380-520, RBL 2 AND LBL 3. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500106 19990115 00106 NM 1999 1 15 SWAA990036 1 19990106 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND STRINGER 19R AT BS 520 CRACKED ON LOWER SIDE. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500107 19990115 00107 NM 1999 1 15 SWAA990037 1 19990106 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1139-1142 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND STRINGER 5L UPPER CHORD CRACKED FROM BS 1139 TO 1142. REPLACED DAMAGED SECTION PER BOEI NG SRM AND BOEING DRAWING 65C35130. 2 L 7 2 4F A16WE 1999011500108 19990115 00108 NM 1999 1 15 SWAA990038 1 19990106 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1154 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND STRINGER 5L LOWER CHORD CRACKED AT BS 1154. REPLACED DAMAGED SECTION PER BOEING SRM AND BOEING DRAWING 65C35130. 2 L 7 2 4F A16WE 1999011500109 19990115 00109 NM 1999 1 15 SWAA990039 1 19990106 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1140 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND STRINGER 5R UPPER AFT CHORD CRACKED AT BS 1140. REPLACED DAMAGED SECTION PER BOEING SRM AND BOEING DRAWING 65C35130. 2 L 7 2 4F A16WE 1999011500110 19990115 00110 NM 1999 1 15 SWAA990040 1 19990106 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND BS 1138 RT DOUBLER STRAP CRACKED AT S12R. REPLACED STRAP PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500111 19990115 00111 NM 1999 1 15 SWAA990041 1 19990106 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1140 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND BS 1140 RT DOUBLER STRAP CRACKED AT S5R. REPLACED STRAP PER BOEING SRM AND BOEING DRAWI NG 65C35130. 2 L 7 2 4F A16WE 1999011500112 19990115 00112 NM 1999 1 15 SWAA990042 1 19990106 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND Z-CHORD BODY CORRODED AT BS 270, LBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500113 19990115 00113 NM 1999 1 15 SWAA990043 1 19990106 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 258 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT 258, 3.5 BELOW S24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500114 19990115 00114 NM 1999 1 15 SWAA990044 1 19990106 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND BS 1138 LT DOUBLER STRAP CRACKED AT 12L. REPLACED STRAP PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500115 19990115 00115 NM 1999 1 15 SWAA990045 1 19990106 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 1155 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND BS 1155 RT LOWER CHORD CRACKED AT 5R. REPLACED CHORD PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500116 19990115 00116 NM 1999 1 15 SWAA990046 1 19990106 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1139 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND S5L LT DOUBLER STRAP CRACKED AT BS 1139. REPLACED STRAP PER BOEING SRM AND BOEING DRAWI NG 65C35130. 2 L 7 2 4F A16WE 1999011500117 19990115 00117 NM 1999 1 15 SWAA990047 1 19990106 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND UPPER SHEAR TIE AT BS 1138 CRACKED AT S5R. REPLACED SHEAR TIE PER BOEING SRM AND BOEING DRAWING 65C35824 2 L 7 2 4F A16WE 1999011500118 19990115 00118 NM 1999 1 15 SWAA990048 1 19990106 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 290 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT 290, AT S20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500119 19990115 00119 NM 1999 1 15 SWAA990049 1 19990106 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 727 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND RT WHEEL WELL WALL BULKHEAD BS 727 GOUGED AT RBL 5, APPROX WL 180, AFT OF FLAP DRIVE MOT OR. REPAIRED PER BOEING SRM AND TRAMCO EWO 98-1188. 2 L 7 2 4F A16WE 1999011500120 19990115 00120 NM 1999 1 15 SWAA990050 1 19990106 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 827 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DENTED BEYOND LIMITS AT BS 827, LBL 28, WL 162. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500121 19990115 00121 1999 1 15 SWAA990051 4 19990105 A 2312 CONNECTOR BOEING 737 7377H4 NM VHF CONTL PANEL LOOSE A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 716SW 27850 EN ROUTE LOST ALL TRANSMIT FUNCTIONS FROM THE CAPT AUDIO PANEL, IE NR 1 AND NR 2 COMM, SERVICE AND FLT INTERPHONE AND O2 MASK. AUDIO ON CAPT AND F/O PANEL WOULD CUT OUT OR FADE OUT. AIRCRAFT DIVERTED TO ABQ AND MADE AN UNEVENTFUL LANDING. SWAPPED VHF CONTROL PANELS CAPT AND F/O. VERIFIED CANNON PLUG CONNECTIONS. OPS CHECK OK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999011500122 19990115 00122 NM 1999 1 15 TWAA9900602 1 19990111 A 3397 WIRE BOEING 767 7673Y0 NM ROW 1-5 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 FOUND EGRESS LIGHT CABIN ROWS 1 THRU 5 INOPERATIVE. FOUND WIRE PULLED OUT OF CONNECTOR. RECONNECTED WIRE. CHECK-C 12- 5-98 LAX. 2 L 7 2 4F RT A1NM 1999011500123 19990115 00123 WP 1999 1 15 TWAA9900603 1 19990110 A 3320 26447 RHEOSTAT DOUG DC9 DC982 3022082 WP CABIN FAILED A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 924TW 49100 THE CABIN SIDEWALL LIGHTS CONTROL CIRCUIT BREAKER POPPED, WITH STRONG ELECTRICAL SMELL. BANDED THE CIRCUIT BREAKER FOR THE LOWER SIDE WALL LIGHTS, AND DEFERRED PER MEL. ON LAYOVER THE LOWER SIDEWALL LIGHTS TRANSFORMER RHEOSTAT WAS REPLACE D. CHECK-C 4-28-98 MCI. 2 L 7 2 4F A6WE 1999011500124 19990115 00124 WP 1999 1 15 TWAA9900604 1 19990107 A 5320 HANGER DOUG DC9 DC983 3022083 WP BS 865 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND LOWER FAIRING T HANGER AT STA 865, 0 IN BL, WAS CRACKED. INSTALLED NEW T HANGER BRACKET (P/N 3936409-505), PER TWA STANDARD PROCEDURES MANUAL 6-70-01. 2 L 7 2 4F RT A6WE 1999011500125 19990115 00125 WP 1999 1 15 TWAA9900605 1 19990104 A 5320 HANGER DOUG DC9 DC983 3022083 WP BS 875 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, THE LOWER FAIRING T HANGER WAS FOUND CRACKED AT 0 IN BL AND STA 875. INSTALLED NEW BRACKET (P /N 3936409-501) PER TWA STANDARD PROCESSES MANUAL 6-70-01. 2 L 7 2 4F RT A6WE 1999011500127 19990115 00127 WP 1999 1 15 AT9900008 1 19990106 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-598 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL. REMOVED LOWER SIDE SKIN FROM FS 229 TO 598 LONGERON 18R THRU 26R FOR REPLACEMENT DUE TO NUMEROUS DENTS AND CORROSION IAW DC9 MM 28-10-7, 30-10-7, SRM 51-10-3, 53-01, 51-30-2 AND AIRTRAN RES 982246. 2 L 7 2 4F A6WE 1999011500129 19990115 00129 WP 1999 1 15 AT9900010 1 19990110 A 3230 3955923503 MECHANISM DOUG DC9 DC932 3022066 WP NLG LACK OF LUBE A ZZDA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 822AT 47274 LANDING GEAR WOULD NOT RETRACT. NOSE GEAR CENTERED BUT STEERABLE. FOUND GROUND SHIFT TO BE FROZEN UP ON NOSE GEAR. DE ICED NOSE GEAR AREA AND LUBED GROUND SHIFT CONTROL IAW DC9 MM 32-10, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999011500130 19990115 00130 NM 1999 1 15 AT9900011 1 19990110 A 3350 07912 BULB BOEING 737 737222 1384473 NM ROW 16 FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 468AT 19074 EMERGENCY PATH LIGHTING INOPERATIVE AT ROW 16. REPLACED LIGHT BULB AND LENS CAP IAW MM 33-50. OPS CHECKED GOOD. (X) 2 L 7 2 4F A16WE 1999011500131 19990115 00131 NM 1999 1 15 AT9900012 1 19990111 A 3350 1000679 LIGHT BOEING 737 7372L9 1384497 NM R2 DOOR INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 R2 EMERGENCY EXIT LIGHT OVER DOOR VERY DIM. REMOVED AND REPLACED R2 EMERGENCY EXIT LIGHT ASSEMBLY PER MM 33-50, OPS CHE CKED GOOD. 2 L 7 2 4F RT A16WE 1999011500132 19990115 00132 NM 1999 1 15 AT9900013 1 19990111 A 3350 1619 BULB BOEING 737 7372L9 1384497 NM FUSELAGE FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 EMERGENCY LIGHT ON RIGHT HAND LOWER AFT WING TO BODY FAIRING IS INOPERATIVE (NEXT TO AFT PIT DOOR). RE-LAMPED RIGHT HAN D AFT LOWER WING TO BODY EMERGENCY LIGHT IAW MM 33-51-21. OPS CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 1999011500133 19990115 00133 NM 1999 1 15 AT9900014 1 19990111 A 3397 WIRE BOEING 737 7372L9 1384497 NM PASSENGER DOOR BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 LOWER L-1 DOOR EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE BEHIND LIGHT. SPLICED WIRE PER STANDARD PRACTICES CHAPTE R 20. OPS CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 1999011500134 19990115 00134 WP 1999 1 15 AT9900015 1 19990109 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND STA 996 FRAME CORRODED UNDER LAVATORY NEXT TO FLOORBEAM ATTACHMENT RIGHT S IDE. FABRICATED AND INSTALLED FLOORBEAM SPLICE REPAIR AND WEB REPAIR AT FS 996 RIGHT HAND BL 10-55 IAW DC9 SRM 51-30, 5 1-10-3, 51-10-4, RES 982191 AND RES 982742, SRM 53-05 FIG 20 A. 2 L 7 2 4F A6WE 1999011500135 19990115 00135 NE 1999 1 15 MALA976287 2 19990104 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A MALA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 GL 15 48XJ 048 ABORTED TAKEOFF DUE RIGHT ENGINE FAILURE. MAINTENANCE REPLACED RIGHT STARTER. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999011500136 19990115 00136 EU 1999 1 15 MALA976288 1 19990104 A 2421 GENERATOR SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 15 420XJ 420 DURING FLIGHT, LEFT GENERATOR OVERTEMP LIGHT FOLLOWED BY LEFT DC GEN CAUTION LIGHT. COMPLIED WITH QRH AND RETURNED TO D TW. 2 L 7 2 4T RT A52EU 1999011500137 19990115 00137 EU 1999 1 15 MALA976289 1 19990105 A 3020 44730501 DEICE MODULE SAAB SF340 340B 7860101 EU RT NACELLE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 457XJ 457 DURING FLIGHT, RIGHT INTAKE HEAT INOP. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RIGHT DEICE MODULE IAW 30-20-15, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999011500138 19990115 00138 EU 1999 1 15 JBXA9900063 1 19990111 A 3620 INDICATION FOKKER F28 F28MK0100 4990807 EU NR 1 BLEED DUCT MALFUNCTIONED A JBXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 103ML 11444 NR 1 BLEED DUCT LEAK ON MFDU. AIRCRAFT AIR RETURNED TO RDU. MAINTENANCE COMPLIED WITH SELF TEST AND LEAK CHECK WITH EN GINES RUNNING. NO FAULTS NOTED AT THIS TIME ALL WORK PERFORMED IAW F-100 MM 36-23-00. 2 L 7 2 4F RT 1999011500139 19990115 00139 SO 1999 1 15 COMA9910007 1 19990107 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 164D 120164 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999011500140 19990115 00140 SO 1999 1 15 COMA9910008 1 19990110 A 5270 12042482001 STRIKER EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 164D 120164 CARGO DOOR WARNING AFTER TAKEOFF. ADJUSTED CARGO DOOR SWITCH STRIKER. 2 L 7 2 4T RT A31SO 1999011500141 19990115 00141 EA 1999 1 15 COMA9960016 1 19990108 A 4950 320207231 CHECK VALVE CNDAIR CL600 CL6002B19 EA APU LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 7169 DURING C-CHECK, FOUND APU AIR SUPPLY CHECK VALVE UPPER PIN EXTREMELY LOOSE. REPLACED VALVE. 2 L 7 2 4F RT A21EA 1999011500142 19990115 00142 EA 1999 1 15 COMA9960017 1 19990108 A 2730 10231007 DAMPENER CNDAIR CL600 CL6002B19 EA LT ELEVATOR LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 2184 7169 DURING C-CHECK, FOUND LEFT INBOARD ELEVATOR FLUTTER DAMPENER TO BE LEAKING. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999011500143 19990115 00143 EA 1999 1 15 COMA9960018 1 19990108 A 2750 601R93106503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 7169 DURING C-CHECK, FOUND RIGHT WING NR 5 FLEXSHAFT UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1999011500144 19990115 00144 EA 1999 1 15 COMA9960019 1 19990107 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO MALFUNCTIONED A COMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 960CA 4874 7117 CARGO SMOKE WARNING. REPLACED CARGO SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 1999011500145 19990115 00145 EA 1999 1 15 COMA9960020 1 19990107 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 710CA 7241 CABIN DOOR WARNING. ADJUSTED CABIN DOOR LATCH CAM MECHANISM. 2 L 7 2 4F RT A21EA 1999011500146 19990115 00146 EA 1999 1 15 COMA9960021 1 19990110 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 938CA 7046 AFT CABIN OVERHEAD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999011500147 19990115 00147 NM 1999 1 15 UPS99428334 1 19990107 A 5712 65B078495 RIB BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE N/A, AFTER REMOVAL OF LT OTBD LEADING EDGE UPPER PANEL, FOUND 7TH L/E RIB FROM OTBD END, UPPER CHORD CRA CKED. REMOVED AND REPLACED RIB IAW SRM 51-30-2, 51-10-6, 51-10-1. 2 L 7 4 4F A20WE 1999011500148 19990115 00148 NM 1999 1 15 UPS99428335 1 19990107 A 5712 65B078515 RIB BOEING 747 747121 1384871 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE-N/A, SIXTH LT WING L/E RIB FROM OTBD END UPPER FLANGE IS CRACKED. REMOVED AND REPLACED L/E RIB IAW SRM 51-30-2, 51-10-6, 51-10-1. 2 L 7 4 4F A20WE 1999011500149 19990115 00149 NM 1999 1 15 UPS99528331 1 19990108 A 3230 RETRACT MECH BOEING 757 75724APF 1384969 NM NLG MALFUNCTIONED A IPXA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 01 468UP 25484 INSPECTION TYPE-N/A, ON DEPARTURE WHEN GEAR HANDLE RAISED TO UP NOSE GEAR GREEN LIGHT REMAINED ON, DOOR LIGHT ON, GEAR D ISAGREE EICAS AND LOUD NOISE LIKE GEAR HANGING. LOWERED GEAR HANDLE TO DOWN AND GOT GOOD INDICATION, RE-RAISED GEAR HAN DLE AND ALL GEAR FAIRED NORMALLY. INSPECTED NOSE GEAR, NO DEFECTS NOTED. 2 L 7 2 4F RT A2NM 1999011500150 19990115 00150 NM 1999 1 15 UPS99528333 1 19990109 A 3260 SENSOR BOEING 757 75724APF 1384969 NM NLG FAILED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 406UP 23728 INSPECTION TYPE-N/A, EICAS MSG NOS A/G DISAGREE IN FLIGHT. REPEAT DISCREPANCY, S10067 FAILS NEAR TARGET TEST WITH NORMA L TARGET GAP VERIFIED. REPLACED FAULTY NOSE GEAR NOT COMPRESSED SENSOR, S10067 PER MM 32-09-08 EXCEPT FOR PERMANENT EL ECTRICAL CONNECTION. 2 L 7 2 4F RT A2NM 1999011500151 19990115 00151 NM 1999 1 15 UPS99628329 1 19990107 A 2751 MODULE BOEING 767 76734AF 1385212 NM TE FLAPS MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 309UP 27740 INSPECTION, A/C WOULD NOT OBTAIN DESIRED SPEED ABOVE 250 KTS ADI INDICATIONS FLAP LIMIT SPD CRZ 310 TAT-26. CLIMBOUT WA S THE SAME, NO EICAS MSG FOR FLAP/SLAT DISAGREE / ASY ASYMMETRY ALT FLAP SELECTOR NORM /OP. COULD NOT DUPLICATE PROBLEM . REMOVED AND REPLACED FLAP/SLAT POSITION MODULE AS PERCAUTIONARY PER MMOC PER M/M 27-51-00. 2 L 7 2 4F RT A1NM 1999011500152 19990115 00152 NM 1999 1 15 QXEA9900014 1 19990107 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTION A QXEA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 09 366PH 604 510 SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. NO EVIDENCE OF SMOKE OR FIRE. MAINTENANCE REPLACED BOTH NR 1 AND NR 2 BAGGAGE SMOKE DETECTORS, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999011500153 19990115 00153 NM 1999 1 15 QXEA9900015 1 19990105 A 5210 85210127051 CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 359PH 514 MAIN CABIN DOOR WILL NOT OPEN. MAINTENANCE REPLACED DOOR SUPPORT CABLE (P/N 85210127-051) AND SUPPORT STRUTS, RIGGED CO UNTERBALANCE AND FUNCTIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999011500154 19990115 00154 EU 1999 1 15 QXEA9900016 1 19990107 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU PAX DOOR INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 498US 11181 EXIT SIGN IN MAIN CABIN OVER COCKPIT DOOR HAS SEVERAL BULBS OUT. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN ASSEMBL Y, OPERATIONAL TEST WAS NORMAL. 2 L 7 2 4F RT A20EU 1999011500155 19990115 00155 NM 1999 1 15 HNAA9900004 1 19990108 A 3350 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM AIRSTAIR DOOR DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 980HA 376 EMERGENCY EXIT LIGHT OVER AIRSTAIR DOOR INOPERATIVE. REPLACED EMERGENCY BATTERY POWER SUPPLY (P/N 61-0478-1X) (S/N PS03 4) AND EMERGENCY LIGHT BATTERY (P/N 60-1321-1X) (S/N SBY128). 2 H 7 2 4T RT A13NM 1999011500156 19990115 00156 NM 1999 1 15 HNAA9900005 1 19990108 A 3010 BOOTS DHAV DHC8 DHC8102 2809003 NM DEICE SYST MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 920HA 084 EN ROUTE MULTIPLE DEICE BOOTS DID NOT INFLATE IN FREEZING CONDITIONS. CHECKED ALL BOOTS WITH SHOP AIR IN MANUAL AND AUT O MODE. REMOVED AND REINSTALLED DRAIN PLUGS WITH NO WATER FOUND OR ANY OTHER DISCREPANCIES. 2 H 7 2 4T RT A13NM 1999011500157 19990115 00157 WP 1999 1 15 99FDEA00009 1 19990109 A 3010 SEAL DOUG DC10 DC1010F 3022111 WP RT WING FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 058FE 46705 NR 3 PNEUMATIC MANIFOLD FAIL LIGHT CAME ON, WING ANTI-ICE WAS USED. FOUND MASSIVE LEAK BETWEEN SLATS R4 AND R5. REPLAC ED PERISEAL ON CONNECTOR SLEEVE. PRESS NR 3 MAN AND RAN NR 3 PACK TO LEAK CK DUCTS, CK NORM. ACCOMPLISHED TEST OF WING ANTI-ICE SYS PER MM 30-11-00-2. 2 L 7 3 4F A22WE 1999011500158 19990115 00158 WP 1999 1 15 MWEA99019 1 19990108 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP PAX DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 500ME 45711 ON PREFLIGHT INSPECTION, THE GALLEY DOOR SLIDE WAS FOUND UNSTOWED. MTC REINSTALLED GALLEY SLIDE. 2 L 7 2 4F A6WE 1999011500159 19990115 00159 WP 1999 1 15 MWEA99020 1 19990107 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 MAIN DOOR SLIDE FELL OFF. MTC RESECURED SLIDE COVER TO DOOR. 2 L 7 2 4F A6WE 1999011500162 19990115 00162 NM 1999 1 15 DLM88990008 1 19990104 A 3610 C17D87 CLAMP C17D87 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE LOOSE A DALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 27 910DL 49541 718247 RT ENGINE NR 2 FAILED PASSING APPROX 5000 FT ON INITIAL CLIMBOUT. THIS APPEARED TO HAPPEN AFTER ENG ANTI-ICE WAS TURNED OFF. ENG RESTARTED NORMALLY AND RAN NORMAL. FOUND STARTER VALVE CLAMP UPSTREAM OF VALVE, OFF THE DUCT. REPLACED CLAM P, RAN ENGINE TO T/O POWER. CHECKED OK. 2 L 7 2 4F 4 F RT A6WE E9NE 1999011500163 19990115 00163 NM 1999 1 15 DL72L990011 1 19990104 A 5753 BRACKET BOEING 727 727232 1384082 NM RT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 FOUND ON D1 LETTER CK, .25 INCH CRACK NR 5 L/E FLAP ACTUATOR OUTBOARD ATTACH BRACKET. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999011500164 19990115 00164 NM 1999 1 15 DL72L990013 1 19990104 A 5754 FRAME BOEING 727 72723 1384004 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 A .25 INCH VISIBLE CRACK LOWER FWD CORNER NR 5 FLAP ACT MOUNT BOX I/B FRAME. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999011500165 19990115 00165 NM 1999 1 15 DL72S990014 1 19990104 A 3350 900542 BATTERY PACK BOEING 727 727225 1384077 NM LT OVERWING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 OVERWING EMERGENCY LIGHTED SIGNS LT OVERWING INOP ON TEST. REPLACED RACK AND BATTERY PACK, OPN CKS OK. 2 L 7 3 4F A3WE 1999011500166 19990115 00166 NM 1999 1 15 DL72L990015 1 19990104 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM ROW 27 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 506DA 21308 ESCAPE PATH LIGHTING INOP ROWS 27 AFT. REPLACED POWER SUPPLY, CKS OK. 2 L 7 3 4F A3WE 1999011500167 19990115 00167 NM 1999 1 15 DL72S990017 1 19990104 A 3350 90052 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 401DA 21145 FUSE BLOWN, EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 1999011500168 19990115 00168 NM 1999 1 15 DL757990018 1 19990104 A 5330 SKIN BOEING 757 757232 1384965 NM BS 520-540 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 666DN 25034 THE FUSELAGE SKIN WAS TORN AND GOUGED AT STRINGER 16L BETWEEN FS 520 TO 540 DUE TO CONTACT WITH A JETWAY. THE DAMAGED S KIN WAS CUTOUT OVER A 24 INCH LONG AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 366403-14. 2 L 7 2 4F RT A2NM 1999011500169 19990115 00169 NM 1999 1 15 DL73E990019 1 19990104 A 5330 655298886 SKIN BOEING 737 737247 138448D NM BS 927 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 378DL 23605 THE FUSELAGE SKIN AT FS 927 AND STRINGER 21L WAS BADLY DENTED. THE SKIN WAS CUT OUT TO REMOVE THE DENT AND AN UNDERLYIN G SECTION OF STRINGER AND TEAR STRAP WERE CUT. THE STRINGER WAS REPAIRED PER THE B727 SRM. THE TEAR STRAP WAS REPAIRED WITH AN INTERNAL ALUMINUM REPAIR DOUBLER AND THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIRS WERE ACCOMPLISHED PER ER/A 366407-14, REV A. 2 L 7 2 4F A16WE 1999011500171 19990115 00171 NM 1999 1 15 DL76L990025 1 19990105 A 5330 SKIN BOEING 767 767332 1382001 NM BS 401 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 189DN 25990 THE FUSELAGE SKIN AND UNDERLYING STRINGER WERE DENTED AND SCRATCHED BY GROUND EQUIPMENT AT FS 401, STRINGER 33R. THE DA MAGED AREA SKIN WAS CUTOUT 16 X 3.5 AREA AND THE DAMAGED SECTION OF STRINGER WAS CUTOUT. THE STRINGER WAS REPAIRED PER THE B767 SRM AND THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 366402-14, REV A. 2 L 7 2 4F RT A1NM 1999011500172 19990115 00172 NM 1999 1 15 DL72W990026 1 19990105 A 5312 BULKHEAD WEB BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 THE FS 1183 BULKHEAD WEB WAS FOUND WITH A CRACK AT WL 169 AND RBL 25. THE CRACK WAS REPAIRED WITH A DOUBLER ON A TIME L IMITED BASIS UNTIL THE FULL BAC S/B 727-53-0215 IS ACCOMPLISHED AT NEXT HMV. THE REPAIR WAS ACCOMPLISHED PER ER/A 36641 5-14. 2 L 7 3 4F A3WE 1999011500173 19990115 00173 NM 1999 1 15 DL72S990027 1 19990106 A 5240 FRAME BOEING 727 727232 1384082 NM R-1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 FOUND ON D2 LETTER CK, .75 INCH CRACK IN R-1 DOOR AFT LOWER FRAME. REPAIRED PER MM 52-12-0. 2 L 7 3 4F A3WE 1999011500174 19990115 00174 NM 1999 1 15 DL72S990028 1 19990106 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 FOUND AT D-2 LETTER CHECK, .5 INCH VISIBLE CRACK AT RT FRAME AFT ENTRYWAY APPROX 6 INCHES BELOW UPPER STOP. REPAIRED PE R SRM 53-10-9. 2 L 7 3 4F A3WE 1999011500175 19990115 00175 NM 1999 1 15 DL72S990029 1 19990106 A 5414 SKIN BOEING 727 727232 1384082 NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 FOUR CRACKS AT FASTENER HOLES FWD OF PNL 9501 RT SIDE. REPAIRED PER MM 54-30-0. 2 L 7 3 4F A3WE 1999011500176 19990115 00176 NM 1999 1 15 DL72S990030 1 19990106 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 VERT FIN STR 9L CRACKED FIN STA 110.400. REPAIRED PER MM 55-30-0. 2 L 7 3 4F A3WE 1999011500177 19990115 00177 NM 1999 1 15 DL72S990031 1 19990106 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 LTR CHK D-2 1/6/99, CRACK IN UPPER O/B RADIUS NR 2 L/E FLAP ACTUATOR MOUNT BRACKET. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999011500178 19990115 00178 NM 1999 1 15 DL72L990034 1 19990107 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 7 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 THE ACTUATOR SUPPORT BRACKET DOUBLERS WERE FOUND CRACKED FOR THE NR 7 SLAT. THE CRACKS ARE TYPICAL OF BAC S/B 727-57- 0 130. THE BRACKETS WERE MODIFIED PER THE INSTRUCTIONS OF THE S/B AND DOCUMENTED PER ER/A 366431-14. 2 L 7 3 4F A3WE 1999011500179 19990115 00179 NM 1999 1 15 DL72W990035 1 19990105 A 5343 TRUNNION BOEING 727 727247 138408F NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND AT MV2 BOLT BORE, CORROSION RT NLG TRUNNION CAP FWD BORE. REAMED HOLE TO 0907 TO REMOVE CORROSION PER MM 53-40-00 TREAT/PAINT. 2 L 7 3 4F A3WE 1999011500180 19990115 00180 NM 1999 1 15 DL72W990036 1 19990105 A 5343 TRUNNION BOEING 727 727247 138408F NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 AT MV2 FOUND BOLT BORE CORRODED LT TRUNNION CAP FWD BORE NLG. REMOVED HOLE TO .892 TO REMOVE CORROSION PER MM 53-40-0, OK TREAT/PAINT HOLE. 2 L 7 3 4F A3WE 1999011500181 19990115 00181 NM 1999 1 15 DL72L990039 1 19990107 A 5754 SKIN BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 NR 7 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999011500182 19990115 00182 NM 1999 1 15 DL76G990040 1 19990107 A 5754 SKIN BOEING 767 7673P6 1385105 NM NR 3 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 153DL 24985 THE UPPER SKIN OF THE NR 3 SLAT T/E WEDGE WAS FOUND WITH A 6 X 13.5 DELAMINATED REPAIR. THE REPAIR WAS REMOVED, ALL DEL AMINATION TO THE SKIN TRIMMED AWAY AND THEN REPAIRED PER B767 SRM 57-43-02. THE REPAIR WAS DOCUMENTED PER ER/A 366 432-14. 2 L 7 2 4F RT A1NM 1999011500183 19990115 00183 NM 1999 1 15 DL76G990041 1 19990106 A 2612 TERMINAL 261701496 BOEING 767 767324 NM NR 1 ENGINE BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 394DL 27394 STATUS MSG LEFT ENGINE FIRE LOOP 1 AND FIRE LOOP 2 AND NO LEFT ENGINE FIRE TEST. FOUND TERMINALS BROKEN AT WIRES W5340- 9001 AND 9002R ON LWR FWD LOOP. INSTALLED TEMPORARY TERMINAL AND MTC FERRIED A/C FOR PERM REPAIR. 2 L 7 2 4F RT A1NM 1999011500185 19990115 00185 NM 1999 1 15 DL72S990044 1 19990108 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 19-26 SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 531DA 21814 FOUND DURING L/O CHECK, EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 19 AND 26 INOP. REPAIRED WIRING. 2 L 7 3 4F A3WE 1999011500186 19990115 00186 NM 1999 1 15 DL72S990047 1 19990108 A 3350 LIGHT RPS1 BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 5973 21431 FOUND DURING NR 7 SERVICE CHECK, EMERGENCY FLOOR TRACK LIGHTS INOP FROM COCKPIT TO 2ND ROW OF TOURIST SEATS. REPLACED B ATTERY PACK, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1999011500187 19990115 00187 NM 1999 1 15 DL72K990050 1 19990109 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM RT OVERWING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 414DA 21256 RT OVERWING CENTER EMERGENCY LIGHT INOP. REPLACED BATTERY ON RACK M956, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999011500188 19990115 00188 NM 1999 1 15 DL72W990051 1 19990107 A 2450 CIRCUIT BREAKER 416000121 BOEING 727 727247 138408F NM GALLEY TRIPPED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 295WA 0052 22532 AFT GALLEY FORWARD COFFEEMAKER HAD MILD ELECTRICAL BURNT SMELL. TURNED OFF GALLEY POWER AND PULLED AFT GALLEY C/B. SME LL DISSIPATED. MTC FOUND COFFEEMAKER INTERNAL C/B POPPED. REPLACED SAME, ALL CHECKS NORMAL. 2 L 7 3 4F A3WE 1999011500189 19990115 00189 NM 1999 1 15 DL76L990054 1 19990110 A 2121 732591F FAN BOEING 767 767332 1382001 NM E & E COMPT FAILED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 194DN 28451 EICAS MSG FWD EQ EXH FAN DISPLAYED, ASSOCIATED CIRCUIT BREAKER POPPED. REPLACED FWD EQ EXH FAN, RESET CIRCUIT BREAKER, OPN NORMAL, MSG DISAPPEARED, REINSTALLED CARGO BIN PANELS. 2 L 7 2 4F RT A1NM 1999011500190 19990115 00190 NM 1999 1 15 DL757990055 1 19990110 A 2612 FIRE LIGHT 346000104 BOEING 757 757232 1384965 NM CENTER CONSOLE CONTAMINATED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 27 630DL 03802F1 22920 AT FLIGHT LEVEL 350 EXPERIENCED MODERATE UNEXPECTED TURBULANCE, BOTTLED WATER SPILLED ON CENTER CONSOLE. DURING DESCENT TO FL 260 AFT CARGO FIRE LIGHT ILLUMINATED. NO OTHER INDICATIONS. HOWEVER, IAW POM NR 1 BOTTLE WAS DISCHARGED AND PAC K SHUT DOWN. LIGHT REMAINED ILLUMINATED. COORDINATED WITH DISPATCH AND MX CONTROL VIA VHF RADIO. AGREED IT WAS A FALS E INDICATION AND FIRE PROTECTION WAS STILL AVAILABLE. LIGHT EXTINGUISHED ABOUT 25 MINUTES LATER. REMOVED AND REPLACED NR 1 FIRE BOTTLE AND COCKPIT BOTTLE DISCHARGE PANEL, OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1999011500191 19990115 00191 NM 1999 1 15 DL72K990057 1 19990110 A 3350 BATTERY PACK 6104789 BOEING 727 727232 1384082 NM PAX DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 481DA 20861 FWD EVACUATION SLIDE LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999011500192 19990115 00192 WP 1999 1 15 SCNA99002 1 19990110 A 3520 WIRE DOUG DC10 DC1015 3022118 WP ROW 6ABC & 7ABC PINCHED A SCNA K NONE N FALSE WARNING CR CRUISE 1 GL 15 151SY 48295 DURING FLIGHT, THE OXYGEN MASKS IN THE FORWARD CABIN EJECTED. TROUBLESHOT PROBLEM TO BE A PINCHED MUX SYSTEM CABLE AT S EAT ROWS 6ABC AND 7ABC. REPLACED THE MUX CABLE AND RESET ALL OXYGEN MASKS THAT DROPPED. PERFORMED OXYGEN DROP TEST PER MM 35-20-00. PASSENGER OXYGEN SYSTEM OPERATIONALLY TEST NORMAL. 2 L 7 3 4F A22WE 1999011500193 19990115 00193 NM 1999 1 15 SCNA99003 1 19990105 A 3350 1102833 LIGHT BOEING 727 7272A1 138407F NM AFT AIRSTAIR INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENACE CHECK,THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY AND BATTERIES, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999011500194 19990115 00194 NM 1999 1 15 SCNA99005 1 19990110 A 3350 1000677 LIGHT BOEING 727 727227 1384078 NM L2 DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A LINE MAINTENANCE CHECK, THE AFT LEFT SERVICE DOOR (L2) OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE IN THE ARM POSITION. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AT THE L2 DOOR, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999011500195 19990115 00195 NM 1999 1 15 SCNA99006 1 19990110 A 2150 39854021 VALVE BOEING 727 7272J4 1384006 NM RT PACK FAILED A SCNA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 290SC 20764 DURING FLIGHT, THE RIGHT PACK WAS FOUND NOT TO PRODUCE ENOUGH AIR TO MAINTAIN FLIGHT AT HIGH ALTITUDE. DIVERTED AIRCRAF T TO MCO. REMOVED AND REPLACED THE RIGHT PACK VALVE PER MM 215571, PACK OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999011500196 19990115 00196 NM 1999 1 15 SCNA99004 1 19990109 A 2741 SWITCH BOEING 727 7272J4 1384006 NM HORIZ STABILIZER FROZEN A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 285SC 21676 DURING TAKEOFF ROLL, THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF. FOUND THE STABILIZER POSITION SWITCH S532 FROZ EN. DEICED THE SWITCH AND CLEANED. PERFORMED A TAKEOFF WARNING SYSTEM CHECK WITH NO FAULTS NOTED. ALL SYSTEMS CHECK N ORMAL AND OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1999011500197 19990115 00197 WP 1999 1 15 DHL99803001 1 19990109 A 5101 STRUCTURE DOUG DC8 DC873F 302199F WP AIRFRAME VIBRATION A DHLA A J UNSCHED LANDING DUMP FUEL E VIBRATION/BUFFET CL CLIMB 1 SO 01 803DH 46123 VIBRATION FELT DURING CLIMB, STARTED AT 190 KTS AND CONTINUED TO INCREASE WITH AIRSPEED UP TO 250 KTS. PERFORMED INSPE CTION OF ALL CONTROL SURFACES AND ACCESS PANELS. ALL AREAS WERE FOUND TO BE OK. ENGINES WERE RAN TO SEVERAL DIFFERENT POWER SETTINGS PER MM 71-00. ALL PARAMETERS NORMAL NO VIBRATION NOTED. 2 L 7 4 4F RT 4A25 1999011500198 19990115 00198 NM 1999 1 15 VNAA9901004 1 19990106 A 5297 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CARGO DOOR BROKEN A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 442JS 3060 THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A CARGO DOOR WARNING MESSAGE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT TOOK PLACE WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AND R EPAIRED A BROKEN SWITCH WIRE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-20-00 AND 52-71-00. OPERATIONAL CHECKS WE RE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999011500606 19990115 00606 NM 1999 1 15 TWAA9900701 1 19990111 A 3350 SOCKET BOEING 767 7673Q8 NM CARGO DOORWAY DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 FOUND EMERGENCY LIGHT INOPERATIVE FWD OF AFT CARGO DOOR ON RT SIDE OF AIRCRAFT. CLEANED BULB AND SOCKET. CHECK-C 12-16 -98 LAX. 2 L 7 2 4F RT A1NM 1999011500607 19990115 00607 NM 1999 1 15 TWAA9900702 1 19990111 A 3397 WIRE BOEING 767 7673Q8 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 FOUND TWO FORWARD EGRESS LIGHTS INOPERATIVE ON RT SIDE OF CABIN. FOUND WIRE DISCONNECTED AND RECONNECTED IT. CHECK-C 1 2-16-98 LAX. 2 L 7 2 4F RT A1NM 1999011500608 19990115 00608 NM 1999 1 15 TWAA9900703 1 19990111 A 3350 SOCKET BOEING 767 7673Q8 NM PAX DOORWAY DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 FOUND LEFT AFT ENTRANCE DOOR FUSELAGE EMERGENCY LIGHT INOPERATIVE. CLEANED BULB AND SOCKET. CHECK-C 12-16-98 LAX. 2 L 7 2 4F RT A1NM 1999011500609 19990115 00609 EU 1999 1 15 MALA976290 1 19990109 A 3230 ACTUATOR BAC 146 AVRO146RJ85A 1500097 EU LT MLG UPLOCK ICED UP A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 505XJ E2313 LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR WAS SELECTED UP. AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND LEFT WH EEL WELL WITH LARGE ICE ACCUMALATION AROUND GEAR DOOR UPLOCK ACTUATOR. REMOVED ICE AND CLEANED CANNON PLUGS, ALL CHECK S GOOD. 2 H 7 4 4F RT A49EU 1999011500610 19990115 00610 1999 1 15 MALA976291 4 19990109 A 3425 AHRS SAAB SF340 SF340A 7850100 EU LT & RT MALFUNCTIONED A MALA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 GL 15 89XJ 089 DUAL AHRS FAILURE IN FLIGHT, DATA WAS 60 DEGREES TO 80 DEGREES OFF. AIRCRAFT RETURNED TO DTW. MAINTENANCE RE-INTIALIZE D BOTH AHRS SYSTEMS. BOTH SYSTEM CHECK GOOD IAW SAAB MM SECTION 34. 2 L 7 2 4T RT A52EU 1999011500611 19990115 00611 EU 1999 1 15 MALA976292 1 19990110 A 3350 LIGHT SAAB SF340 340B 7860101 EU ROW 3 LOOSE A MALA K NONE O OTHER LD LANDING 1 GL 15 233CH 233 EMERGENCY LIGHT PANEL ABOVE SEATS 3 C AND D CAME LOOSE ON TAKEOFF AND LANDING. MAINTENANCE RESECURED PANEL. 2 L 7 2 4T RT A52EU 1999011500612 19990115 00612 EU 1999 1 15 MALA976293 1 19990110 A 3020 CONNECTOR SAAB SF340 340B 7860101 EU LT INTAKE HEAT LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 417XJ 340B417 LEFT ENGINE INTAKE HEAT LIGHT CAME ON IN FLIGHT. AIRCRAFT RETURNED TO DTW. MAINTENANCE SWAPPED TEMP SENSOR ON SHOE BOX T2 INTO T4, T3 INTO T5, REMOVED CANNON PLUG ON LOWER INLET AND FOUND OIL AND MOISTURE. CLEANED AND RESECURED. OPS CH ECK GOOD, RAN ENGINE FOR 15 MINUTES. 2 L 7 2 4T RT A52EU 1999011500613 19990115 00613 EU 1999 1 15 MALA976294 1 19990111 A 3020 939HE POWER RELAY SAAB SF340 340B 7860101 EU LT INTAKE HEAT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 421XJ 421 DURING FLIGHT WITH ENGINE ANTI ICE ON, THE LEFT INTAKE LIGHT COMES ON ABOUT EVERY 30 SECONDS, COMPLETED QRH FOR INTAKE, PROBLE CONTINUED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED LEFT POWER RELAY CONTROL 939HE, COMPLETED OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999011500614 19990115 00614 EU 1999 1 15 MALA976295 1 19990109 A 3350 BATTERY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 15 444XJ 444 ON TAXI OUT FROM GATE, THE EMERGENCY LIGHTS UNARMED ANNUNCITOR LIGHTS STAYED ILLUMINATED. AIRCRAFT RETURNED TO THE GATE . MAINTENANCE RECHARGED EMERGENCY LIGHTS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999011500624 19990115 00624 SO 1999 1 15 COMA9910009 1 19990108 A 3260 922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 258CA 120247 WHEN LANDING GEAR SELECTED UP, ALL RED AND GREEN INDICATIONS ON.\NREPLACED LEFT HAND MLG UPLOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1999011500625 19990115 00625 EA 1999 1 15 COMA9960022 1 19990109 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 958CA 7111 CABIN DOOR WARNING. ADJUSTED CABIN DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1999011500626 19990115 00626 EA 1999 1 15 COMA9960023 1 19990108 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 915CA 9005 7013 FLAPS FAILED AFTER TAKEOFF. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999011500627 19990115 00627 EA 1999 1 15 COMA9960024 1 19990109 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 EA CABIN DIRTY A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 709CA 7238 SMOKE IN CABIN WHEN AIRCRAFT PACKS SELECTED ON AFTER TAKEOFF. SMOKE WAS FROM DEICING FLUID INJESTED INTO AIRCRAFT SYSTE M. REPLACED AIRCRAFT COALESCER BAGS AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999011500628 19990115 00628 EA 1999 1 15 COMA9960025 1 19990110 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 927CA 7031 CABIN DOOR WARNING AFTER TAKEOFF. COULD NOT DUPLICATE. FOUND NO DEFECTS WITH DOOR OPERATION. 2 L 7 2 4F RT A21EA 1999011500629 19990115 00629 EA 1999 1 15 COMA9960026 1 19990108 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 963CA 12145 7127 CARGO SMOKE WARNING DURING TAXI. FALSE WARNING. REPLACED SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 1999011500630 19990115 00630 WP 1999 1 15 UPS99828336 1 19990109 A 5320 FORMER DOUG DC8 DC873F 302199F WP BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE-N/A, AFT ACCESSORY COMPARTMENT, FORMER CRACKED AT STA 1600 BETWEEN L28R AND L29R. REMOVED DAMAGED SECTI ON OF FORMER IAW DC8 SRM 53-2-0. FABRICATED FOR MER REPAIR IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999011500642 19990115 00642 NM 1999 1 15 99UAL900001 1 19990101 A 2751 INDICATOR 1812996 BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE TE FLAPS FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 979UA 2157 21544 TRAILING EDGE FLAPS REMAINED IN TAKEOFF POSITION AFTER TAKEOFF. *S/D* A DETAILED INSPECTION OF FLAP INDICATOR FOUND TH AT THE SYNCRO WAS SLUGGISH. THIS IS CAUSED BY WORN BEARINGS. REPLACED FLAP POSITION INDICATOR PER MM 27-54-05, OPERATI ONAL CHECK IS OK. 2 L 7 2 4F 4 F A16WE E2EA 1999011500643 19990115 00643 NE 1999 1 15 99UAL900002 2 19990102 A 7530 1685MK6 VSV ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 427UA 512 RIGHT ENGINE COMPRESSOR STALL ON TAKEOFF. RETURNED TO FIELD. OVERWEIGHT LANDING. VSV ACTUATOR HAD A DEFECTIVE POSITIO N SENSOR, CAUSING COMPRESSOR STALL. COA IS IN PROCESS TO MODIFY THE LVDT OF THE VSV ACTUATORS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999011500644 19990115 00644 WP 1999 1 15 99UAL900003 1 19990102 A 2170 COALESCER DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN CONTAMINATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1847U 48263 STRONG ODOR, POSSIBLY OF TURBINE OIL AFTER CLIMBOUT AND DESCENT. *S/D* ENG/APU OIL USAGE IS LOW, AND NO HYD FLUID LEA K OR FUEL LEAK WRITE-UPS. COALESCER BAGS REPLACED. OK ON SUBSEQUENT FLIGHTS. 2 L 7 3 4F 4 F A22WE E23EA 1999011500645 19990115 00645 NM 1999 1 15 99UAL900005 1 19990104 A 2750 652661458 TRANSMISSION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT TE FLAP FAILED A UALA A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 WP 29 7264U 21411 AFTER TAKEOFF, RIGHT INBOARD FLAP RETRACTION STUCK BETWEEN 2 AND 5 DEGREES. RETURNED TO ORD. *S/D* FOUND RIGHT INBOAR D MOST JACKSCREW FAILED AT AFT END. REPLACED TRANSMISSION AND JACKSCREW SYSTEM, OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999011500646 19990115 00646 NM 1999 1 15 99UAL900006 1 19990102 A 2130 VALVE AIRESEARCH 39608831 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT FLOW CONTL MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7291U 21569 AFTER TAKEOFF FROM MSP, THE FLIGHT EXPERIENCED A PRESSURIZATION PROBLEM AND CABIN ALTITUDE KEPT CLIMBING EVEN WITH ONLY ONE PACK OPERATING. RETURNED TO MSP DUE TO NOT ENOUGH FUEL ON BOARD TO CONTINUE TO DEN AT 10,000 FEET. *S/D* FOUND TH AT NR 1 PACK DID NOT SEEM TO OPERATE IN FLIGHT. ALSO, LT MAIN ENTRY DOOR SEAL WAS OUT OF ITS RETAINER. SECURED SEAL AN D REPLACE RT FLOW CONTROL MODULATING VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1999011500647 19990115 00647 NM 1999 1 15 99UAL900007 1 19990102 A 2530 805501000 OVEN SELL BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE GALLEY SMOKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 151UA 18285 23736 GALLEY 418 RECON OVEN NR 011 WAS SMOKING. *S/D* THE SHOP REPORT STATES THAT FOREIGN MATERIAL WAS INGESTED AND BLOWN A CROSS THE HEATER ELEMENTS. THE MATERIAL WAS BURNT AND DEPOSITED ON THE TOP BAFFLE ASSEMBLY AND INSIDE THE OVEN CAVITY. THERE WAS NO ELECTRICAL FAILURE. 2 L 7 4 4F 4 F RT A20WE E3NE 1999011500648 19990115 00648 EU 1999 1 15 99UAL900009 1 19990105 A 2910 HYD SYST AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BLUE HYD SYST REQD SERVICE A UALA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 WP 29 414UA 472 DIVERTED TO DEN DUE TO BLUE SYSTEM HYDRAULIC PRESSURE/VOLUME LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 1999011500649 19990115 00649 NM 1999 1 15 99UAL900010 1 19990104 A 2170 8323719600U COALESCER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RIGHT CONTAMINATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7442U 21896 RIGHT PACK MADE A RUMBLING NOISE AND TRIPPED IMMEDIATELY ON THE GROUND IN SLC. CABIN FILLED WITH SMOKE. *S/D* CONTAMI NATED COALESCER BAG. REPLACED COALESCER BAG. 2 L 7 3 4F 4 F A3WE E2EA 1999011500650 19990115 00650 NE 1999 1 15 99UAL900011 2 19990105 A 7321 FUEL CONTROL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE ICED UP A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7447U 21901 700056 ABORTED TAKEOFF AT 100 KNOTS DUE TO NR 1 ENGINE SLOW TO SPOOL UP AND LACK OF DESIRED EGT. *S/D* THE AIRCRAFT WAS MOVED TO A HANGER AND THE NR 1 AND 3 COLD SOAKED ENGINES WERE HEATED TO MELT FROZEN MOISTURE IN THE PS4 TRAP OF THE FUEL CONT ROL. THE NR 2 ENGINE HAD AIRFRAME PROTECTION FROM THE SUBZERO TEMPERATURE AND HIGH WINDS AND HAD PRODUCED FULL POWER. S UBSEQUENTLY ALL THREE ENGINES CHECKED OK AT FULL POWER. 2 L 7 3 4F 4 F A3WE E2EA 1999011500651 19990115 00651 NM 1999 1 15 99UAL900012 1 19990106 A 2150 SWITCH ALLIEDSIGNAL 5486206U1 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT PACK FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 932UA 26658 RIGHT PACK TRIPPED OFF. *S/D* RIGHT PACK TRIPPED OFF DUE TO FAILED 390¡ COMPRESSOR DISCHARGE OVERHEAT SWITCH. REPLACE D 390¡ COMPRESSOR DISCHARGE OVERHEAT SWITCH. OPERATIONAL CHECK IS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999011500652 19990115 00652 NM 1999 1 15 99UAL900013 1 19990106 A 2121 FAN AIRRESEARCH 2075621MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT PACK FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7254U 21401 RIGHT PACK WENT FULL HOT WHEN CLEARING RUNWAY AND CABIN FILLED WITH SMOKE. *S/D* FOUND RT GROUND COOLING FAN INOP. CI RCUIT BREAKER TRIPPED. REPLACED GROUND COOLING FAN. 2 L 7 3 4F 4 F A3WE E2EA 1999011500653 19990115 00653 NM 1999 1 15 99UAL900014 1 19990107 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4060 PW4060 52119 NE 5L DOOR INOP A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 197UA 26901 EMERGENCY AISLE LIGHT INOP AT DR 5L DROP CEILING. 2 L 7 4 4F 4 F RT A20WE E24NE 1999011500654 19990115 00654 NM 1999 1 15 99UAL900015 1 19990107 A 2120 AIR DIST BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 649UA 25286 STRONG BURNING RUBBER SMELL IN FIRST FOUR ROWS OF BUSINESS CLASS. DIVERTED TO PHL. A DETAILED CHECK OF THE AREA WAS AC COMPLISHED AND NO PROBLEMS WERE FOUND. A SEARCH OF THE AMIS DATABASE HAS BEEN ACCOMPLISHED AND NO FAULTS COULD BE ATTRI BUTED TO THIS EVENT. THE AIRCRAFT HAS CONTINUED TO OPERATE WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999011500656 19990115 00656 NM 1999 1 15 99UAL900017 1 19990106 A 3241 CONTROL BOX BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ANTISKID SYST MALFUNCTIONED A UALA O OTHER O OTHER LD LANDING 1 WP 29 7260U 21407 NR 1 AND NR 4 TIRES GROUND DOWN ON LANDING DUE TO LOCKED WHEELS. NR 2 TIRE BLEW AT GATE. *S/D* SUSPECTED ANTISKID FAI LURE. ACCOMPLISHED TEST OF ANTISKID SYSTEM, ALL INDICATIONS NORMAL. REPLACED ALL 4 BRAKES AND 3 TIRES (POSITIONS NR 1, NR 2 AND NR 4). REPAIRED DAMAGE TO UNDERWING PANELS, NR 4 FLAP TRACK FAIRING AND LT MLG STRUT DOOR. PULLED FLIGHT REC ORDER FOR ANALYSIS. SUBSEQUENT MAINTENANCE ACTIONS, ENTERED ITEM TO REPLACE ANTISKID CONTROL BOX (PRECAUTIONARY) AND PE RFORMED CHECK OF ANTISKID TRANSDUCERS AND HUBCAP COUPLINGS FOR DAMAGE. 2 L 7 3 4F 4 F A3WE E2EA 1999011500657 19990115 00657 NM 1999 1 15 99UAL900018 1 19990107 A 3010 65C172813U1 DUCT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 6 LE SLAT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7451U 21905 FOUND NR 6 LEADING EDGE SLAT HEAT TUBE BROKEN AT SWIVEL POINT IN RIGHT WING. *S/D* FOUND BROKEN ANTI ICE DUCT. REPLAC ED DUCT ASSY AND SHAFT ASSY OF NR 6 SLAT TELESCOPING DUCT. 2 L 7 3 4F 4 F A3WE E2EA 1999011500658 19990115 00658 WP 1999 1 15 MWEA99021 1 19990111 A 5320 591015837 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CORROSION ON AFT CARGO DOOR JAMB AFT WEB AREA. MTC FABRICATED AND INSTALLED WEB REPAIR WEB. 2 L 7 2 4F A6WE 1999011500659 19990115 00659 WP 1999 1 15 MWEA99022 1 19990109 A 2560 113317 SLIDE DOUG DC9 DC915 3022036 WP CABIN DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 300ME 45718 SLIDE COVER ON GALLEY DOOR CAME OFF. MTC REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999011500660 19990115 00660 WP 1999 1 15 MWEA99023 1 19990111 A 5530 991183492 ANGLE DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACKED ANGLE BRACKET AT BUSS OF RIGHT VERTICAL STABILIZER AFT SPAR BOX. MTC FABRICATED AND INSTALLED NEW ANGLE C LIP. 2 L 7 2 4F A6WE 1999011500670 19990115 00670 NM 1999 1 15 SWAA990052 1 19990109 A 2150 PACK BOEING 737 7373H4 1384600 NM CABIN SMOKING A SWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 383SW 26589 AIR RETURN DUE TO SMOKE SMELL IN CABIN AND AFT LAV SMOKE DETECTOR SOUNDING. INSPECTED A/C FOR SOURCE OF SMELL. DETERMI NED THAT OILY SMELL WAS COMING FROM THE LT AC PACK. DEFERRED PER MEL 21-1. INSPECTED AFT LAV AREA AND NO EVIDENCE FOUN D. DISCONNECTED DETECTOR AND DEFERRED PER MEL 26-16. 2 L 7 2 4F RT A16WE 1999011500671 19990115 00671 NE 1999 1 15 SWAA990053 2 19990109 A 7321 693733588 FUEL CONTROL BOEING 737 7373T5 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA K NONE X ENGINE FLAMEOUT AP APPROACH 1 SW 07 668SW 23060 INFLIGHT NR 2 ENGINE FAILURE ON APPROACH INTO STL. NO FUEL FLOW INDICATION. NR 2 FUEL SHUTOFF VALVE C/B TRIPPED. COUL D NOT RESET. REMOVED AND REPLACED FUEL CONTROL MODULE AND REPLACED DISCONNECT D5164. OPS CK NORMAL PER M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1999011500672 19990115 00672 NM 1999 1 15 SWAA990054 1 19990107 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACK AT LBL 10 AND RBL 10, WL 234. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500673 19990115 00673 NM 1999 1 15 SWAA990055 1 19990107 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+6, LBL 3 AND 8. REPAIRED PER SWA RA 1-353-1972. 2 L 7 2 4F RT A16WE 1999011500674 19990115 00674 NM 1999 1 15 SWAA990056 1 19990107 A 5312 BULKHEAD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 7.0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500675 19990115 00675 1999 1 15 SWAA990057 4 19990108 A 2565 1061323469 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 DURING PREFLIGHT CHECK, FOUND AFT SERV DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999011500676 19990115 00676 1999 1 15 SWAA990058 4 19990109 A 2565 22D22900131 SLIDE BOEING 737 7372T4 1384492 NM PAX DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING PREFLIGHT CHECK, FOUND AFT ENTRY DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F A16WE 1999011500677 19990115 00677 1999 1 15 SWAA990059 4 19990109 A 2565 21061323427 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED SC CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F A16WE 1999011500678 19990115 00678 NM 1999 1 15 SWAA990060 1 19990110 A 2131 71211997101AB CONTROLLER BOEING 737 7377H4 NM E/E BAY FAILED A SWAA K NONE J WARNING INDICATION DE DESCENT 1 SW 07 713SW 27847 AUTO FAIL LIGHT ON PRESSURIZATION PANEL ILLUMINATED ON DESCENT. ALTERNATE FAILED TO TAKE OVER RIGHT AWAY. REGAINED CON TROL IN MANUAL AND THEN TRIED ALTERNATE AGAIN AND IT WORKED IN ALTERNATE. REMOVED AND REPLACED NR 1 PRESSURE CONTROLLE R PER M/M. GROUND CHECKS GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999011500679 19990115 00679 NM 1999 1 15 SWAA990061 1 19990108 A 3350 LIGHT BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING PREFLIGHT, FOUND ONE EGRESS LIGHT MISSING AFT CABIN AREA. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999011500680 19990115 00680 NM 1999 1 15 SWAA990062 1 19990107 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 700 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 700, AT LBL 60. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500681 19990115 00681 NM 1999 1 15 SWAA990063 1 19990109 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 4.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500682 19990115 00682 NM 1999 1 15 SWAA990064 1 19990109 A 5313 STRINGER BOEING 737 7373A4 1384585 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 360, AT S15L. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500683 19990115 00683 NM 1999 1 15 SWAA990065 1 19990109 A 5313 STRINGER BOEING 737 7373A4 1384585 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 360, AT S11L. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500684 19990115 00684 NM 1999 1 15 SWAA990066 1 19990109 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 940-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 940 TO 947, LBL 17. CUT OUT AND SPLICED IN REPAIR PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1999011500685 19990115 00685 NM 1999 1 15 SWAA990067 1 19990109 A 5320 CHORD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND LT CHORD CRACKED AT BS 178, LBL 29. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500686 19990115 00686 NM 1999 1 15 SWAA990068 1 19990110 A 5314 KEEL BEAM BOEING 737 7373Q8 1384670 NM BS 525 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM LOWER CHORD DAMAGED AT B.S. 525 BY CORROSION. DAMAGE LENGTH APPROX 5 OF I/B SIDE OF 'T' EXTRUSION. MAX DAMAGE DEPTH AFTER CLEANING APPROX 0.070. REPAIRED PER SWA RA 1-353-1974. 2 L 7 2 4F RT A16WE 1999011500687 19990115 00687 NM 1999 1 15 SWAA990069 1 19990110 A 5754 SKIN BOEING 737 7373Q8 1384670 NM NR 3 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C2 CHECK, FOUND NR 3 L/E SLAT LOWER SKIN IS CRACKED 15 O/B OF O/B ACTUATOR STOP PAD 1 LONG. REPAIRED P ER SWA RA 1-357-0616. 2 L 7 2 4F RT A16WE 1999011500688 19990115 00688 NM 1999 1 15 SWAA990070 1 19990108 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, BELOW S15R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500689 19990115 00689 NM 1999 1 15 SWAA990071 1 19990108 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 950 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950 AT S22R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500690 19990115 00690 NM 1999 1 15 SWAA990072 1 19990110 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867 AT S19R, 3 FT FWD OF CARGO DOOR UPPER SIDE, 3.25 LONG. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500691 19990115 00691 NM 1999 1 15 SWAA990073 1 19990111 A 3350 LAMP BOEING 737 7373H4 1384600 NM ROW 18ABC INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED BC2 CHECK, FOUND CABIN EMEGENCY TRACK LIGHTING INOP AT SEAT ROW 18ABC. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999011500692 19990115 00692 NM 1999 1 15 SWAA990074 1 19990110 A 3350 LIGHT BOEING 737 7373H4 1384600 NM ROW 12-18 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED BC2 CHECK, FOUND CABIN EMERGENCY TRACK LIGHTING INOP FROM SEAT ROWS 12 TO 18. REPAIRED LIGHTING PER BO EING M/M. 2 L 7 2 4F RT A16WE 1999011500693 19990115 00693 NM 1999 1 15 SWAA990075 1 19990110 A 3350 SIGN BOEING 737 7373H4 1384600 NM EMER EXIT DOOR LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED BC2 CHECK, FOUND CABIN EMERGENCY EXIT SIGN ABOVE RT EMERGENCY EXIT DOOR PULLED OUT. RESECURED PER BOEI NG M/M. 2 L 7 2 4F RT A16WE 1999011500694 19990115 00694 NM 1999 1 15 SWAA990076 1 19990111 A 3397 WIRE BOEING 737 7373H4 1384600 NM ROW 11-16 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED A2 CHECK, FOUND CABIN EMERGENCY TRACK INOP AT ROWS 11 TO 16. REPAIRED WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999011500724 19990115 00724 NM 1999 1 15 HNAA9900006 1 19990111 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM EMER EXIT DOOR BROKEN A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 928HA 120 FORWARD DOOR EMERGENCY EXIT SIGN, FORWARD AISLE DOWN LIGHT AND ROW 4 RED FLOOR EMERGENCY LIGHT INOPERATIVE. REPAIRED 33 51-PS2 CONNECTOR, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999011500725 19990115 00725 WP 1999 1 15 AT9900016 1 19990108 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 L-1 DOOR SLIDE PACK CAME OFF. RE-INSTALLED L-1 DOOR SLIDE PACK IAW DC9 MM 25-62-0. 2 L 7 2 4F A6WE 1999011500726 19990115 00726 WP 1999 1 15 AT9900017 1 19990110 A 3350 60030431 BATTERY CHARGER DOUG DC9 DC932 3022066 WP CABIN FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 811AT 47285 OVERWING EMERGENCY EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED OVERWING EMERGENCY EXIT BATTERIES AND BATTERY CHA RGER IAW MM 33-50. 2 L 7 2 4F A6WE 1999011500727 19990115 00727 WP 1999 1 15 AT9900018 1 19990111 A 3610 C38037 CLAMP DOUG DC9 DC932 3022066 WP TAIL COMPARTMENT BROKEN A ZZDA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 15 840AT 47523 CLIMBING THROUGH 14,000 FEET MASTER WARNING LIGHT ILLUMINATED WITH TAIL COMPARTMENT TEMPERATURE HI-LIGHT ON, NORMAL PROC EDURES FOLLOWED. REPLACED BROKEN CLAMP AT LEFT HAND HEAT EXCHANGER PRIMARY AIR DUCTING PER MM 36-10. 2 L 7 2 4F A6WE 1999011500728 19990115 00728 WP 1999 1 15 AT9900019 1 19990113 A 3350 AD4002P BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 814AT 47486 WINDOW EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-50. 2 L 7 2 4F A6WE 1999011500729 19990115 00729 WP 1999 1 15 AT9900020 1 19990112 A 5330 5920413 SKIN DOUG DC9 DC932 3022066 WP BS 229-589 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP FL, FUSELAGE SKIN HAS NUMEROUS DENTS FROM FS 229 TO FS 589 RIGHT SIDE. REMOVED AND RE PLACED FUSELAGE SKIN FS 229 TO 589 RIGHT SIDE IAW RES 982130 AND RES 982249. SKIN (P/N 5920-119-5). 2 L 7 2 4F A6WE 1999011500730 19990115 00730 NM 1999 1 15 AT9900021 1 19990109 A 3350 6005401 BATTERY PACK BOEING 737 7372T4 1384492 NM ROW 24 DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 467AT 22055 AFT EMERGENCY LIGHTS SECTION INOPERABLE FROM ROW 24 BACK. RE-SEATED CANNON PLUG ON BATTERY CHARGER RIGHT HAND AT AFT UP PER PACK. OPS CHECKED GOOD PER MM 33-50. (X) 2 L 7 2 4F A16WE 1999011500731 19990115 00731 EA 1999 1 15 JBXA9900064 1 19990112 A 2750 89501009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 578ML 7270 FLAPS FAIL IN FLIGHT, FLAPS AT 4 DEGREES. AIRCRAFT RETURNED TO RDU. MAINTENANCE REMOVED AND REPLACED BPSU RT, ALL WORK PERFORMED IAW CRJ MM 27-51-10, OPS CK GOOD. 2 L 7 2 4F RT A21EA 1999011500732 19990115 00732 NM 1999 1 15 AWXA9900006 1 19990105 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727-760 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN STA 727A AND 760 APPROX ABOVE STRINGER 17 RT FUSEL AGE. TEMP REPAIR PER SRM. REINSPECT AT 3,000 FLIGHT CYCLES AND EVERY 2500 FLIGHT CYCLES THEREAFTER. PERMANENT REPAIR MUST BE C/W WITHIN 10,000 FLIGHT CYCLES PER SRM 53-30-3, FIG 1 PG 2C. 2 L 7 2 4F RT A16WE 1999011500737 19990115 00737 NM 1999 1 15 AWXA9900011 1 19990108 A 3350 033006 POWER SUPPLY BOEING 737 737277 1384570 NM LT UNDERWING INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 LT LOWER FUSELAGE UNDERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LT POWER SUPPLY AND BATTERY PACK, OPS CK GO OD. 2 L 7 2 4F RT A16WE 1999011500738 19990115 00738 NM 1999 1 15 AWXA9900012 1 19990107 A 3350 900835A BATTERY PACK BOEING 737 7372M8 1384483 NM R2 DOORWAY DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 21955 RT EMERGENCY EXIT LIGHT OVER R-2 DOOR INOP. REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT BATTERY PACK, OPS CK GOO D. 2 L 7 2 4F A16WE 1999011500740 19990115 00740 NM 1999 1 15 UPS99428338 1 19990112 A 3510 OXY BOTTLES BOEING 747 747123 1384873 NM COCKPIT FAILED A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 675UP 20390 INSPECTION TYPE-N/A, CREW OXYGEN DROPPED FROM 1200 PSI AT PREFLIGHT TO 500 PSI AT TOP OF CLIMB. REMOVED AND REPLACED LO WER AND UPPER 02 BOTTLES, LEAK CHECKED GOOD. AIR TURNBACK. 2 L 7 4 4F A20WE 1999011500741 19990115 00741 NM 1999 1 15 UPS99428340 1 19990104 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1481 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE-N/A, AFTER REMOVAL OF LT OUTBOARD L/E UPPER PANEL FOUND HEAVY CORROSSION ON WING SKIN UPPER FWD FLANGE A T STA WS 1481. REMOVED CORROSION AT WS 1481 IAW SRM 57-10-01 AND REPAIRED IAW DH SK691-165. 2 L 7 4 4F A20WE 1999011500742 19990115 00742 WP 1999 1 15 UPS99828337 1 19990112 A 3230 RETRACT MECH DOUG DC8 DC871F 302199D WP NLG MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 700UP 45900 INSPECTION TYPE-N/A, NOSE GEAR WOULD NOT RETRACT AFTER T/O. AIR TURNBACK. PER TROUBLESHOOTING PG 101 NOSE GEAR FAILS T O RETRACT, CHECKED CONTROL VALVE, RIGGING AND CABLE TENSION PER MM 32-31-00 PG 204. NO DEFECTS NOTED. GEAR OPERATES NO RMAL. NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999011500743 19990115 00743 EU 1999 1 15 QXEA9900017 1 19990111 A 3397 WIRE GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9 BROKEN A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 494US 11167 CABIN EMERGENCY EVACUATION LIGHTS CAME ON DURING ENGINE START WITH SWITCH IN THE ARM POSITION. MAINTENANCE FOUND THREE BROKEN WIRES AT ROW 9. INSTALLED WIRE SPLICES AND TESTED SYSTEM, OPERATION NORMAL. 2 L 7 2 4F RT A20EU 1999011500744 19990115 00744 WP 1999 1 15 ABXA9900006 1 19990110 A 3260 INDICATION DOUG DC9 DC932 3022066 WP LDG GEAR DOOR MALFUNCTIONED A ABXA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 GL 23 901AX 47381 GEAR DOOR OPEN LIGHT REMAINED ON DURING APPROACH. EXECUTED GO-AROUND, RECYCLED LANDING GEAR AND GEAR DOOR OPEN LIGHT EX TINGUISHED. GEAR DOOR OPEN POSITION INDICATION LIGHT OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1999011500745 19990115 00745 WP 1999 1 15 ABXA9900007 1 19990110 A 3350 60030451 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942AX 47552 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1999011500746 19990115 00746 WP 1999 1 15 ABXA9900008 1 19990112 A 3310 5137501 CHART LIGHT DOUG DC8 DC861 3021952 WP RT COCKPIT SMOKING A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 848AX 46032 DURING CRUISE, FIRST OFFICER'S CHART LIGHT SMOKES WHEN ON. INSPECTED FIRST OFFICER'S CHART LIGHT RHEOSTAT, LIGHT BULBS AND WIRING AND NO DEFECTS NOTED. OPS CHECKED GOOD IAW DC8 MM. 2 L 7 4 4F 4A25 1999011500747 19990115 00747 WP 1999 1 15 MWEA99026 1 19990109 A 5400 591326211 ANGLE DOUG DC9 DC914 3022034 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND CRACKED UPPER ATTACH ANGLE ON LEFT PYLON TRAILING EDGE. MTC FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 1999011500748 19990115 00748 WP 1999 1 15 MWEA99027 1 19990109 A 5320 99578994 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 38 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND CRACKED INTERCOSTAL IN FORWARD ACCESS AT UPPER RIGHT SIDE STATION 38. MTC REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 1999011500749 19990115 00749 NM 1999 1 15 MWEA99028 1 19990108 A 7110 5930640505 SKIN DOUG MD88 MD88 3023688 NM LT COWL PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 FOUND HOLE IN LEFT LOWER AFT COWL. MTC DID A COMPOSITE REPAIR. 2 L 7 2 4F RT A6WE 1999011500750 19990115 00750 NM 1999 1 15 MWEA99029 1 19990111 A 5720 59104721 TIP DOUG MD88 MD88 3023688 NM LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CRACK AND DENT ON LEFT WING TIP. MTC PERFORMED A TEMPORARY DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999011500753 19990115 00753 SO 1999 1 15 SWIA971361 1 19990109 A 5246 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL SERVICE NOT LATCHED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 569SW 120344 RETURNED TO LAS DUE TO SERVICE DOOR LIGHT. FOUND FUEL DOOR NOT LATCHED PROPERLY. FUELER LATCHED DOOR, CHECKS GOOD. ME L 52-70-1. INSPECTED ALL SERVICE DOORS AND LATCHES. ALL FOUND GOOD. SERVICE DOOR LIGHT SYSTEM FOUND TO BE WORKING NOR MAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500754 19990115 00754 SO 1999 1 15 SWIA971362 1 19990109 A 2460 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DC ELECT SYST FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 188SW 120039 FO'S ATTITUDE HEADING INDICATOR FAILED IN FLIGHT. RETURNED TO SLC. REPLACED EMERGENCY BATTERY RELAY BOX. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500755 19990115 00755 SO 1999 1 15 SWIA971363 1 19990109 A 2612 FIRE DETECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE INOP A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 198SW 120227 FIRE DETECTOR INOP RIGHT SIDE WHILE EN ROUTE. RETURNED TO SLC. REPLACED RIGHT ENGINE FIRE DETECTOR, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500756 19990115 00756 SO 1999 1 15 SWIA971364 1 19990109 A 3260 PROX SENSOR EMB 120 EMB120RT SO PWA 118 PW118 NE NLG FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 129AM 120119 DOWNLOCK REL BUTTON REQUIRED FOR GEAR RETRACTION. RETURNED TO PDX. REPLACED NOSE LANDING GEAR SHOCK ABSORBER PROX SENS OR IAW MM 32-01-01. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500757 19990115 00757 EA 1999 1 15 SWIA971365 1 19990109 A 3260 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 407SW 7034 GEAR DISAGREE AND NOSE DOOR DISAGREE RED LIGHTS CAME ON AFTER GEAR HANDLE IS SELECTED UP. GEAR WILL NOT GO UP TO LOCKED POSITION. RETURNED TO SLC. ADJUSTED S23 SENSOR ON NOSE GEAR. GEAR EXTENDS AND RETRACTS NORMALLY, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999011500758 19990115 00758 NM 1999 1 15 VNAA9901005 1 19990108 A 3020 3D355601 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT NACELLE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 430JS 25257 11587 3044 THE AIRCRAFT RETURNED TO THE FIELD FOLLOWING AN INTAKE DEICE FAILURE MESSAGE. MAINTENANCE WAS DISPATCHED FROM PIT TO RE PAIR THE AIRCRAFT. PIT MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND INTAKE EJECTOR FLOW CONTROL VALVE, IN ACCORDAN CE WITH DORNIER MAINTENANCE MANUAL 30-22-03. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVIC E. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999011500759 19990115 00759 NM 1999 1 15 VNAA9901008 1 19990109 A 6120 45C3317B60612 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROPELLER LEAKING A VNAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 429JS 3043 THE LEFT HAND ENGINE OIL TEMPERATURE WAS BELOW EXEPTABLE LIMITS, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. DURING THE TRANSIT TO THE GATE THE OIL TEMPERATURE RETURNED TO ACCEPTABLE LIMITS, BUT THE CREW THEN NOTED OIL ON THE LEFT ENGINE COWLINGS. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND PROPELLER CONTROL UNIT TRANSFER TUBE O RING SEALS, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-31. OPERATIONAL AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999011500790 19990115 00790 NM 1999 1 15 SWAA990077 1 19990111 A 2150 ACM BOEING 737 7373H4 1384600 NM LEFT & RIGHT OVERSERVICED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 383SW 26589 ON CLIMBOUT, NOTICED STRONG OIL SMELL IN CABIN. AIRCRAFT RETURNED TO HOU. REMOVED EXCESSIVE OIL FROM LT AND RT AIR CYC LE MACHINES. REMOVED AND REPLACED BOTH COALESCER BAGS. SYS OPS CHECKED GOOD ON THE GROUND PER MM. 2 L 7 2 4F RT A16WE 1999011500791 19990115 00791 NM 1999 1 15 SWAA990078 1 19990109 A 2150 20405010 ACM BOEING 737 7373H4 1384600 NM LEFT FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 383SW 26589 RETURNED TO DTW DUE TO AFT LAV FIRE WARNING AND STRONG ORDER IN CABIN. INSPECTED OIL QTY IN BOTH AIR CYCLE MACHINES, FO UND TO BE OK. DEFERRED LT PACK FOR TROUBLESHOOTING PER MEL 21-1. INSPECTED ALL DUCTING IN LT AC BAY AND FOUND NO LEAKS . REMOVED AND REPLACED LT AIR CYCLE MACHINE AND LT PACK COALESCER BAG PER M/M. 2 L 7 2 4F RT A16WE 1999011500792 19990115 00792 NM 1999 1 15 SWAA990079 1 19990111 A 3830 LAVATORY BOEING 737 7377H4 NM CABIN REQD SERVICE A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 700GS 27835 AIRCRAFT DIVERTED TO OKC DUE TO LAV SYSTEM GOING INOP. DRAINED AND RESERVICED SYSTEM PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999011500793 19990115 00793 NM 1999 1 15 SWAA990080 1 19990112 A 2530 41610019 COFFEEMAKER BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 391SW 27378 FLIGHT ATTENDANTS REPORTED ACRID, ELECTRICAL TYPE FUMES AFTER TAKEOFF IN AFT GALLEY AREA. AIRCRAFT RETURNED TO PHX. RE MOVED AND REPLACED NR 2 AFT COFFEEMAKER C/B AND BOTH AFT COFFEEMAKERS. RAN ENGS, BOTH PACKS SEVERAL DIFFERENT AFT GALLE Y PWR CONFIGURATIONS. SMELL NO LONGER EXISTS. 2 L 7 2 4F RT A16WE 1999011500794 19990115 00794 NM 1999 1 15 SWAA990082 1 19990112 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 802 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 802, RBL 14. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500795 19990115 00795 NM 1999 1 15 SWAA990083 1 19990112 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND A CRACK IN WEB AT BS 178, RBL 1.0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999011500796 19990115 00796 NM 1999 1 15 SWAA990084 1 19990112 A 5330 SKIN BOEING 737 7373A4 1384585 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND A 1.5 INCH CRACK AT AFT LOWER CORNER OF FWD SERVICE DOOR. REPAIRED PER SWA RA 1-353- 1970. 2 L 7 2 4F RT A16WE 1999011500797 19990115 00797 NM 1999 1 15 SWAA990085 1 19990111 A 3350 LIGHT BOEING 737 7373H4 1384600 NM ROW 12-18 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY EXIT LIGHTING INOP FROM ROWS 12 TO 18. REPOSITIONED LIGHTS. 2 L 7 2 4F RT A16WE 1999011500798 19990115 00798 NM 1999 1 15 SWAA990086 1 19990111 A 3350 SIGN BOEING 737 7373H4 1384600 NM EMER EXIT DOOR DETACHED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY EXIT SIGN ABOVE RT EMERGENCY EXIT DOOR PULLED OUT. RESECURED SIGN LIGHT LEN S PER BOEING MM. 2 L 7 2 4F RT A16WE 1999011500799 19990115 00799 NM 1999 1 15 SWAA990087 1 19990111 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 770 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, AT S18L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500800 19990115 00800 NM 1999 1 15 SWAA990088 1 19990111 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727C-4, ABOVE S4R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999011500801 19990115 00801 NM 1999 1 15 SWAA990089 1 19990111 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 727A + 12 BETWEEN S23-24R. 2 L 7 2 4F A16WE 1999011500802 19990115 00802 NM 1999 1 15 SWAA990090 1 19990112 A 3350 LAMP BOEING 737 7373H4 1384600 NM ROW 18 ABC INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY TRACK LIGHT INOP AT ROW 18ABC. RELAMPED PER BOEING MM. 2 L 7 2 4F RT A16WE 1999011500803 19990115 00803 NM 1999 1 15 SWAA990091 1 19990113 A 3350 LAMP BOEING 737 7373G7 1384595 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED SC CHECK, FOUND SEVERAL FLOOR EMERGENCY EGRESS LIGHTS INOP. REPAIRED LIGHTING SYSTEM PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012000015 19990120 00015 NM 1999 1 20 99FDEA00005 1 19990106 A 3610 322861001 VALVE BOEING 727 72721C 138400M NM NR 1 BLEED SYST FAILED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 144FE 19137 LOWER AFT BODY O/H LIGHT ILLUMINATED. FOLLOWED CK LIST PROCEDURE, CLOSED NR 1 BLEED VALVE AND LEFT PACK. RETARDED NR 1 THROTTLE TO CLIMB POWER. LIGHT REMAINED OUT AND TEST OK, INDICATIVE OF LEAK BETWEEN NR 1 BLEED VALVE AND LEFT PACK VAL VE. REMOVED AND REPLACED PURGE VALVE, OPER CK AND LEAK CK GOOD. REF M/M 36-13-11. NOTE: VALVE HOT AIR WAS LEAK AT HE AT DETECTOR. 2 L 7 3 4F A3WE 1999012200001 19990122 00001 NE 1999 1 22 TWAA9900801 2 19990111 A 7230 810108 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 1 ENG COMP FAILED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 05 950U 49230 1228 ABORTED TAKEOFF WHEN ANOTHER FLIGHT REPORTED SPARKS COMING FROM THE NR 1 ENGINE. METAL WAS FOUND IN THE ENGINE TAIL PIP E. REPLACED ENGINE. CHECK-C 8-24-98 MCI. *S/D* FOUND AN EIGHTH STAGE COMPRESSOR BLADE FRACTURED DUE TO FATIGUE. THE RE WAS SEVERE DOWNSTREAM DAMAGE TO THE N2 COMPRESSOR. 2 L 7 2 4F 4 F A6WE E9NE 1999012200002 19990122 00002 WP 1999 1 22 TWAA9900802 1 19990112 A 2711 CONTROLS DOUG DC9 DC982 3022082 WP AILERO TRIM LACK OF LUBE A TWAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 05 920TW 49369 AILERON TRIM CONTROL FROZE DURING CRUISE AT FL370. AILERON CONTROLS NORMAL DURING FLIGHT. AILERON TRIM OPERATED NORMAL LY AFTER DESCENT THROUGH FL200. INSPECTED AILERON TRIM CONTROL CABLES AND PULLEYS. LUBED ALL CABLES AND PULLEYS WITH LPS1. CHECK-C 6-18-98 STL. 2 L 7 2 4F A6WE 1999012200003 19990122 00003 WP 1999 1 22 TWAA9900803 1 19990112 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 959 BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR PANEL BROKEN AT STA 959, LT SIDE OUTBOARD OF OUTBOARD CHAIR TRACK. INSTALLED WEB REPAIR PER SRM 53-01. 2 L 7 2 4F A6WE 1999012200004 19990122 00004 NM 1999 1 22 CALA9900009 1 19990113 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 FLOOR SUPPORT BEAM HAS SURFACE CORROSION AROUND FASTENER HOLES STA 986.5. INSTALLED NEW FLOORBEAM PER EC/RA 5310-03450. 2 L 7 2 4F RT A16WE 1999012200005 19990122 00005 WP 1999 1 22 CALA9900010 1 19990111 A 3350 TERMINAL DOUG DC9 DC932 3022066 WP EMER EXIT FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 AFT DOOR EMERGENGY EXIT LIGHT INOP. REPAIRED TERMINAL AT LIGHT AND OPS CHECK OK PER MM 33-53-01. 2 L 7 2 4F A6WE 1999012200006 19990122 00006 WP 1999 1 22 CALA9900011 1 19990113 A 5720 ANGLE DOUG DC9 DC932 3022066 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14524 47539 RIB TO LOWER LE ANGLE CRACKED INSIDE RIGHT WING APPROX 8 O/B OF VORTILON. REMOVED CRACKED ANGLE. FABRICATED AND INSTAL LED NEW ANGLE PER SRM 51-30-5, 51-10-0, 51-10-3, AND 51-10-2. 2 L 7 2 4F A6WE 1999012200007 19990122 00007 WP 1999 1 22 CALA9900012 1 19990114 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 332 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 FUSELAGE LOWER SKIN AT APPROX STA 332 AT RT LONGERON 29 AREA HAS ONE POPPED RIVET AND BULGED. FABRICATED, TREATED, PRIM ED, AND INSTALLED NEW FINGER DOUBLER PER SRM 51-00-00. 2 L 7 2 4F A6WE 1999012200008 19990122 00008 WP 1999 1 22 CALA9900013 1 19990114 A 5230 SKIN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 AFT CARGO COMPARTMENT DOOR LOWER EXTERIOR SKIN EDGE BENT. CUT OUT BENT AREA AT AFT CARGO DOOR LOWER EDGE EXTERIOR SKIN AND INSTALLED DOUBLER REPAIR PER SRM 52-01. 2 L 7 2 4F A6WE 1999012200009 19990122 00009 WP 1999 1 22 CALA9900014 1 19990112 A 3350 4T1110B SWITCH DOUG DC9 DC932 3022066 WP COCKPIT OVHD INTERMITTENT A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12539 45792 EMERGENCY FLOOR PATH LIGHTS INTERMITENT FROM COCKPIT SWITCH. REMOVED AND REPLACED COCKPIT SWITCH PER MM 33-00-00. 2 L 7 2 4F A6WE 1999012200010 19990122 00010 WP 1999 1 22 CALA9900015 1 19990112 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18563 47487 FLOOR EMERGENCY EXIT LIGHTS PULLED UP FROM FLOOR. INSTALLED TRACKS AND OPS CHECK OK. 2 L 7 2 4F A6WE 1999012200011 19990122 00011 NM 1999 1 22 CALA9900016 1 19990112 A 5320 CLIP BOEING 727 727224 1384076 NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 KEEL BEAM RIGHT WHEEL WELL ATTACH CLIP CRACKED. REPLACED VERTICAL STIFFENER RT INBOARD CORNER AS PER ORIGINAL PER SRM 5 1-30-2. 2 L 7 3 4F A3WE 1999012200012 19990122 00012 WP 1999 1 22 CALA9900017 1 19990114 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 218 - 229 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 CORROSION AND EXPOSED SEAT TRACK MATERIAL RT CENTER SEAT TRACK BETWEEN STA 218 - 229. REMOVED AND REPLACED SEAT TRACK A T STA 218 THROUGH STA 229 RT CENTER PER SRM 53-05. 2 L 7 2 4F A6WE 1999012200013 19990122 00013 WP 1999 1 22 CALA9900018 1 19990112 A 2120 AIR DIST DOUG DC9 DC982 3022082 WP CABIN SMOKE A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 83872 49120 WHEN USING ENGINE ANTI-ICE DURING TAKEOFF AND LANDING BURNING ODOR AND SMOKE/HAZE IN CABIN AND ODOR IN COCKPIT. SMOKE S TARTED IN AFT CABIN AND WORKED FORWARD. REMOVED AND REPLACE BOTH COALESCER BAGS AND CHECKED PER MM 21-20. RAN BOTH ENG INES TO 1.8 EPR AND ISOLATED APU AND ENGINE AIR. RAN BOTH PACKS AT HIGH HEAT FOR EXTENDED PERIODS. CHECKED 8TH AND 13T H STAGE SADDLE DUCTS FOR OIL. NONE FOUND ALL CHECKS GOOD. 2 L 7 2 4F A6WE 1999012200014 19990122 00014 EU 1999 1 22 9900083253 1 19990111 A 2910 FITTING AIRBUS 320 A320212 EU BLUE HYD SYST LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 353NW 786 DURING DESCENT, RECEIVED HYD 'B' RSVR LOW LVL AND HYD 'B' ELEC PUMP LOW PR MESSAGES. CREW DECLARED AN EMERGENCY AND LAN DED WITHOUT INCIDENT. MAINTENANCE SECURED LEAKING HYDRAULIC LINE FITTING AND SERVICED SYSTEM. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999012200024 19990122 00024 WP 1999 1 22 9900099755 1 19990112 A 5320 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 755NW 47179 DURING PERIODIC CHECK, FOUND ZEE ANGLE (PART NR 5912350-67) CRACKED IN RADIUS. REPAIRED PER EA 97-159630. 2 L 7 2 4F A6WE 1999012200025 19990122 00025 WP 1999 1 22 9900109755 1 19990112 A 5330 SKIN DOUG DC9 DC941 302207N WP BS 1068 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 755NW 47179 DURING PERIODIC CHECK, FOUND SKIN CRACKED AT FS 1068, LONGERON 15L. REPAIRED PER EA 97-159609. 2 L 7 2 4F A6WE 1999012200026 19990122 00026 WP 1999 1 22 9800119755 1 19990112 A 5312 BULKHEAD DOUBLER DOUG DC9 DC941 302207N WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 755NW 47179 DURING PERIODIC CHECK, FOUND DOUBLER (5912350-20) CRACKED AT FS 83.5. REPAIRED PER EA 97-162799. 2 L 7 2 4F A6WE 1999012200027 19990122 00027 WP 1999 1 22 9900129920 1 19990113 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 942N 47459 DURING PERIODIC CHECK, FOUND STRUCTURE FATIGUE AT FS 83.5. REPAIRED PER EA 99-162798. 2 L 7 2 4F A6WE 1999012200053 19990122 00053 NM 1999 1 22 99FDEA00010 1 19990114 A 3260 SWITCH BOEING 727 72725C 138400H NM RT MLG DOOR OUT OF ADJUST A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 124FE 19360 99-0010 - RED DOOR LIGHT ON WHEN GEAR IS OFF. GEAR RECYCLED PER RED TABS. LIGHT WENT OUT AND GEAR LEVER LEFT UP POSITI ON. INSTALL MAIN AND NOSE GEAR PINS 1-14-99. REMOVED ALL 3 GEAR PINS. ADJUST RIGHT MAIN GEAR DR WARNING LIGHT SWITCH PER 727 MM 32-62-11. CHECKS NORMAL. 2 L 7 3 4F A3WE 1999012200054 19990122 00054 WP 1999 1 22 MWEA99030 1 19990112 A 3232 39567851 ACTUATOR DOUG DC9 DC932 3022066 WP NLG DOOR LACK OF LUBE A MWEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 209ME 47730 AFTER TAKEOFF GEAR AND RETRACTION LOTS OF VIBRATION AND IT SEEMS ONE NOSE GEAR DOOR IS NOT CLOSED. FOUND RIGHT NOSE GEA R DOOR OPEN LUBED DOOR LINK ACTUATOR ASSEMBLY. 2 L 7 2 4F A6WE 1999012200055 19990122 00055 NM 1999 1 22 SCNA99007 1 19990112 A 2750 TRANSMISSION BOEING 727 727225 1384077 NM TE FLAPS OUT OF ADJUST A SCNA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 15 283SC 22559 DURING APPROACH, GOT PULL UP AURAL ALERT AT 200 FT AGL. ABORTED APPROACH. INBOARD AND OUTBAORD FLAPS WERE AT 26 DEGREE S PLUS OR MINUS 1 DEGREE. GPWA'S FLAP OVERRIDE WAS SELECTED AND AURAL PULL UP WENT OUT. LANDED UNEVENTFULLY. ADJUSTED INBOARD AND OUTBOARD FLAP TRANSMISSION ASSEMBLIES TO 180 DEGREES OFF STOPS PER MM 275141. RESAFETIED TORQUE TUBES. PE RFORMED GPWS TEST AND SYSTEM OPERATIONALLY CHECKS NORMAL. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999012200056 19990122 00056 NM 1999 1 22 SCNA99008 1 19990112 A 3350 LIGHT BOEING 727 7272A1 138407F NM ROW 3 INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 DURING A LINE MAINTENANCE CHECK, AN EMERGENCY LIGHT WAS FOUND TO BE OUT AT LOCATION SEAT ROW 3 IN THE FLOOR TRACK LIGHTI NG. REPAIRED FLOOR TRACK LIGHT AT SEAT ROW 3. SYSTEM OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999012200057 19990122 00057 WP 1999 1 22 CKSA99001 1 19990105 A 2910 LINE DOUG DC8 DC861 3021952 WP LT MLG DOOR ACT CRACKED A CKSA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 23 817CK 45887 TOTAL LOSS OF HYDRAULIC PRESSURE WITH QUANTITY LOSS ON FLAP EXTENSION. FLIGHT CREW DECLARED EMERGENCY, REQUESTED FIRE T RUCKS TO STAND BY FOR LANDING. AIR BRAKE BOTTLE USED UPON LANDING. FOUND HYDRAULIC PRESSURE DOWN LINE CRACKED AT LEFT GEAR DOOR ACTUATOR. REPLACED HARD LINE, LEAK CHECK OK. SERVICED AND BLED HYDRAULIC SYSTEM. CHECKED ENGINE DRIVEN PUMP S AND CASE DRAIN FILTERS, FOUND OK. CHECKED ENGINE DRIVEN PUMPS FOR OPERATION, FOUND PRESSURE NORMAL. CYCLED ALL HYD P OWERED FLIGHT CONTROLS AND FLAPS, OPERATIONS ALL NORMAL. AUX PUMP, SPOILER PUMP AND RUDDER PUMP ALSO OPERATE NORMALLY. A/C OK FOR SERVICE. 2 L 7 4 4F 4A25 1999012200113 19990122 00113 WP 1999 1 22 TWAA9900901 1 19990114 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9402W 53138 SEVERAL EGRESS LIGHTS WERE INOPERATIVE IN THE FWD CABIN. REPAIRED BROKEN WIRE AT THE END OF THE FIRST CLASS SECTION. C HECK-C 10-25-98 STL. 2 L 7 2 4F RT A6WE 1999012200114 19990122 00114 WP 1999 1 22 TWAA9900902 1 19990112 A 5330 SKIN DOUG DC9 DC915 3022036 WP BS 514 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 490SA 45798 DURING CHECK-C MAINT CHECK, FOUND SIX INCH CRACK IN FUSELAGE SKIN AT STA 514, 12 IN BELOW OVERWING EXIT OPENING ON LEFT SIDE OF AIRCRAFT. REPAIRED CRACK PER ARA 15854 AND ARA 15856. 2 L 7 2 4F A6WE 1999012200115 19990122 00115 WP 1999 1 22 TWAA9901001 1 19990117 A 3350 732 LAMP DOUG DC9 DC983 3022083 WP ROW 9-22-27-28 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9403W 53139 THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 9, 22, 27, AND 28. REPLACED THE LAMP FOR EACH OF THE INOPERATIVE LIGHT S. CHECK-C 11-3-98 MCI. 2 L 7 2 4F RT A6WE 1999012200116 19990122 00116 NM 1999 1 22 TWAA9901002 1 19990117 A 3350 BULB BOEING 757 7572Q8 1384972 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 703TW 27620 FOUND THE LEFT SIDE NUMBER 4 CABIN DOOR SLIDE LIGHT INOPERATIVE ON TEST. REPLACED THE LAMP AND SECURED THE LAMP IN THE SOCKET. CHECK-C 5-9-98 LAX. 2 L 7 2 4F RT A2NM 1999012200117 19990122 00117 NM 1999 1 22 TWAA9901003 1 19990116 A 3350 6104783 BATTERY PACK BOEING 727 727231 1384079 NM PAX DOOR DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54344 21631 FOUND THE OUTSIDE EMERGENCY LIGHT INOPERATIVE AT THE LEFT FORWARD AND RT FORWARD CABIN DOORS. REPLACED THE BATTERY PACK . CHECK-C 2-21-98 JFK. 2 L 7 3 4F A3WE 1999012200118 19990122 00118 WP 1999 1 22 TWAA9901004 1 19990114 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND STRINGER 5L CRACKED ON BOTH SIDES OF FORMER STA 718. INSTALLED NEW STRINGER PIECE AND S PLICED PER SRM 53-02, FIG 18 PG 1. 2 L 7 2 4F A6WE 1999012200119 19990122 00119 WP 1999 1 22 TWAA9901005 1 19990114 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 658 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND LONGERON 7L CRACKED AT STA 658L FORMER TIE. CONFIRMED BY NDT. REMOVED DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-02, PG 48 FIG 18 AND PAGE 51. 2 L 7 2 4F A6WE 1999012200120 19990122 00120 WP 1999 1 22 TWAA9901006 1 19990114 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 658 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 FOUND LONGERON 6L CRACKED AT STA 658L AT FORMER TIE. CONFIRMED BY NTD. REMOVED DAMAGED SECTION AND REPLACED. SPLICED PER SRM 53-02, PG 48 FIG 18 AND PAGE 51. 2 L 7 2 4F A6WE 1999012200121 19990122 00121 WP 1999 1 22 TWAA9901007 1 19990114 A 5311 ANGLE DOUG DC9 DC983 3022083 WP BS 1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 DURING OP 15 MAINT CHECK, FOUND CORROSION ON AFT SIDE OF FORMER SUPPORT ANGLE, STA 1322 LONGERON 28R TO 27L. REMOVED CO RROSION PER STRUCTURAL PROCEDURES MANUAL 6-70-1. CUTOUT AREA BEYOND LIMITS RBL 4 TO LBL 9. REPAIRED PER SRM 53-05, PAG E 6. 2 L 7 2 4F RT A6WE 1999012200123 19990122 00123 NM 1999 1 22 TWAA9901009 1 19990118 A 5754 SKIN BOEING 767 767231 1385131 NM NR 6 LE SLAT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 608TW 22571 NR 6 LE SLAT PANEL TRAILING EDGE AT INBD TOP END HAD REPAIR BLOWN OFF. INSTALLED HOT BOND REPAIR AS REQUIRED PER SRM 51 -70-10, PAGE 26, FIG 10. CHECK-C 10-28-98 LAX. 2 L 7 2 4F RT A1NM 1999012200124 19990122 00124 NM 1999 1 22 HNAA9900007 1 19990113 A 5400 BRACKET DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 PRESSURE MANIFOLD BRACKET IN NR 2 NACELLE CRACKED IN LOWER FORWARD CORNER. REPAIRED IN ACCORDANCE WITH STRUCTURAL REPAI R MANUAL. 2 H 7 2 4T RT A13NM 1999012200125 19990122 00125 NM 1999 1 22 HNAA9900008 1 19990107 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 487 & 202 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 923HA 099 CORROSION AFT SIDE OF FRAME X487 BETWEEN STRINGERS 29S AND 31S AND FRAME AT STATION X202 AND A CRACKED RIVET HOLE ON FRA ME A STATION X222 AT STRINGER 31R. REPAIRED AS NECESSARY. 2 H 7 2 4T RT A13NM 1999012200126 19990122 00126 NM 1999 1 22 HNAA9900009 1 19990110 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM BS 210 CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 923HA 099 FORWARD ANGLE BETWEEN INBOARD SEAT RAILS AT COCKPIT ENTRANCE AT APPROXIMATELY STATION X210 CRACKED. REPLACED BRACKET. 2 H 7 2 4T RT A13NM 1999012200127 19990122 00127 NM 1999 1 22 HNAA9900010 1 19990112 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 488 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 923HA 099 CORROSION ON SEAT RAIL, P/N 85330507-106, ON UPPER LEVEL .012 DEEP AT FRAME STATION X488. REPLACED SEAT RAIL. CORROSIO N ON SEAT RAIL, P/N 85320490-133, BETWEEN STATIONS X242 AND X264 BETWEEN .010 AND .015. REPAIRED AS NECESSARY. CORROSI ON ON SEAT RAIL, P/N 85320490-135, AT FRAME 330 .020 AND .023 DEEP. REPAIRED AS NECESSARY. CORROSION ON SEAT RAIL, P/N 85320701-115, ALONG LENGTH OF RAIL BETWEEN .006 AND .028 DEEP. REPLACED RAIL. CORROSION ON SEAT RAIL, P/N 85320701-11 7, ALONG LENGTH OF RAIL BETWEEN .012 AND .024 DEEP. REPLACED RAIL. 2 H 7 2 4T RT A13NM 1999012200128 19990122 00128 1999 1 22 MALA976296 4 19990112 A 3416 641119001 ALTIMETER SAAB SF340 340B 7860101 EU RT COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 436XJ 436 DURING FLIGHT, THE NR 2 ALTIMETER STICKING FROM 840 FT TO 11000 FT, DURING RETURN TO MSP AND DESCENT, THE ALTIMETER APPE ARS TO FUNCTIONED NORMALLY. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED NR 2 ALTIMETER. SYSTEM CHECKS GOOD IAW SF3 40 MM CHAP 34. 2 L 7 2 4T RT A52EU 1999012200129 19990122 00129 EU 1999 1 22 MALA976297 1 19990111 A 3230 CONTROL LATCH SAAB SF340 SF340A 7850100 EU LANDING GEAR MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 98XJ 098 TAKING OFF FROM GFK, THE GEAR HANDLE DID NOT COME OUT OF DOWN/LOCK POSITION. AS PER QRH, PRESSED DOWN LOCK RELEASE TO R ETRACT GEAR. AIRCRAFT LANDING IN MSP WITHOUT INCIDENT. MAINTENANCE DEFERRED LANDING GEAR CONTROL LATCH PER MEL 32-31-1 (C). OVERRIDE MECHANISM OPERATES NORMALLY, MX NOTICIED AND PLACARD AS REQUIRED. ENTERED INTO DMR. 2 L 7 2 4T RT A52EU 1999012200130 19990122 00130 NM 1999 1 22 K3HA990002 1 19990114 A 2780 CONNECTOR BOEING 727 727225 1384077 NM NR 4 LE FLAP DIRTY A K3HA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 25 8880Z 21453 THE NR 4 LEADING EDGE FLAP WOULD NOT RETRACT ON CLIMB-OUT. RECYCLED SEVERAL TIMES, RETURNED TO EWR. CLEANED CANNON PLU GS AND CHECKED SECURITY AT SWITCH, PERFORMED FLAP OPERATED SEVERAL TIMES, LIGHT OPS CHECKS NORMAL REF MM 27-82-1. 2 L 7 3 4F A3WE 1999012200132 19990122 00132 1999 1 22 LR7A9902 2 19990114 A 7320 6404486 SPEED CONTROL LKHEED 382 382G 526414U SO NR 2 ENGINE FAILED A LR7A E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 403LC 16544 4590 ON TAKEOFF, NR 2 ENGINE WOULD NOT EXCEED 830 DEG TIT, SELECTED NULL AND PULLED IGNITION CONTROL CB ENGINE TIT STAYED AT 830 DEG. TIT, SHUTDOWN ENGINE AT 1226Z. RETURNED TO DEPARTURE AIRPORT. REMOVED AND REPLACED NR 2 SPEEDSENSE CONTROL IA W ALLISON 501 D22 MM CH 73-500 P201 OPS CK NORMAL. 2 H 7 4 4T A1SO 1999012200133 19990122 00133 WP 1999 1 22 IXXA9900001 1 19990115 A 3260 INDICATION DOUG DC8 DC871F 302199D WP NLG MALFUNCTIONED A IXXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 820BX 76742 2555 46065 ON DESCENT INTO TOL, WHEN THE CREW EXTENDED THE LANDING GEAR, THE NOSE GEAR DOWN AND LOCK INDICATION LIGHT FAILED TO ILL UMINATE, ACCOMPANIED BY A LANDING GEAR UNSAFE LIGHT. THE CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATIONS REMA INING THE SAME. MAINTENANCE INSPECTED THE NOSE GEAR AND THE INDICATION SYSTEM WIRING WITH NO DISCREPANCIES NOTED. MAIN TENANCE PERFORMED A SUCCESSFUL GEAR SWING IN ACCORDANCE WITH THE MAINTENANCE MANUAL, ALL INDICATIONS WERE NORMAL, AND TH E AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 1999012200134 19990122 00134 1999 1 22 CALA9900019 4 19990114 A 2565 62772215 SLIDE 62772215 BOEING 777 777224 1385225 NM L2 DOOR FAILED A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 78004 565 565 03889 27580 L2 DOOR SLIDE SEMI DEPLOYED. DOOR OPENED WITH GIRT BAR INSTALLED. SLIDE FELL OUT ONTO JETWAY. DOOR POWER ASSIST BOTTL E DISCHARGED. REMOVED AND REPLACED SLIDE AND ASSIST BOTTLE PER 25-66-01 AND 52-11-22. 2 L 7 2 4F RT T00001SE 1999012200135 19990122 00135 NM 1999 1 22 CALA9900020 1 19990114 A 3213 6573761128 STRUT BOEING 737 7373T0 1384582 NM RT MLG CRACKED A CALA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 09 17356 7880 23942 RIGHT MAIN LANDING GEAR LEAKING FLUID. FOUND 1 CRACK IN MLG CYLINDER. REPLACED MAIN LANDING GEAR. 2 L 7 2 4F RT A16WE 1999012200136 19990122 00136 NM 1999 1 22 CALA9900021 1 19990114 A 3397 WIRE BOEING 727 727232 1384082 NM TAIL COMP SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 EMERGENCY EXIT LIGHT RIGHT HAND CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. FOUND WIRE SHORTED IN AFT LEFT TAIL COMPARTMENT. SECURED WIRES AND PROTECTED PER STANDARD PRACTICES. LIGHTS OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999012200137 19990122 00137 WP 1999 1 22 CALA9900023 1 19990114 A 5320 52932222 SUPPORT DOUG DC9 DC981 3022081 WP BS 148-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 FLOOR SUPPORT HAT SECTION CORRODED STA 148 - 200. FABRICATED AND INSTALLED NEW HAT SECTION PER SRM 51-30-01. 2 L 7 2 4F A6WE 1999012200138 19990122 00138 WP 1999 1 22 CALA990022 1 19990114 A 5350 2818973501 RECEPTICLE DOUG DC9 DC981 3022081 WP TAIL CONE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 TAIL CONE TOP FIVE ALIGNMENT PIN RECEPTICLES WORN. REPLACED TOP FIVE ALIGNMENT PIN RECEPTICLES. 2 L 7 2 4F A6WE 1999012200139 19990122 00139 WP 1999 1 22 9900131158 1 19990111 A 3320 LIGHT DOUG DC10 DC1040 3023508 WP ROW 2 SMOKING A NWAA O OTHER B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC AP APPROACH 1 GL 01 158US 46767 DURING APPROACH INTO BOS, FLIGHT ATTENDANT NOTICED SMOKE FROM CABIN LIGHT ABOVE SEAT 2H AND 2J. NOTIFIED COCKPIT AND SH UT LIGHTS OFF. SMOKE DISSIPATED. CAPTAIN DECLARED A PRECAUTIONARY EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLA CED BALLAST ON LIGHT 2H AND 2J. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999012200148 19990122 00148 WP 1999 1 22 9900149608 1 19990115 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608NW 47423 DURING PERIODIC CHECK, FOUND UPPER CORNER CRACKED AT FS 699, LONGERON 12L TO 26L. REPAIRED PER EA 99-163240. 2 L 7 2 4F A6WE 1999012200149 19990122 00149 WP 1999 1 22 9900159878 1 19990115 A 5400 SPAR DOUG DC9 DC951 3022051 WP RT PYLON WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 787NC 48149 DURING PERIODIC CHECK, RIGHT UPPER AFT PYLON SPAR HOLES 1-22 EXCEED MAXIMUM DIAMETER PER WORK CARD NR 5440-01042. REPAI RED PER EA 99-163231. 2 L 7 2 4F RT A6WE 1999012200154 19990122 00154 SO 1999 1 22 COMA9910010 1 19990108 A 3350 1013073 BULB EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 246CA 120223 FORWARD, RED, EMERGENCY FLOOR LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 1999012200155 19990122 00155 SO 1999 1 22 COMA9910011 1 19990110 A 2750 12042642507 SWITCH EMB 120 EMB120RT SO COCKPIT MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 189CA 19371 120189 FLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR SWITCH. 2 L 7 2 4T RT A31SO 1999012200156 19990122 00156 SO 1999 1 22 COMA9910012 1 19990113 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 FELL OFF A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 164D 120164 EMERGENCY EXIT SIGN AT ROW 5 FELL OFF. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999012200157 19990122 00157 EA 1999 1 22 COMA9960027 1 19990113 A 3222 STRUT CNDAIR CL600 CL6002B19 EA NLG REQD SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 934CA 1 1 7042 NLG DID NOT RETRACT. SERVICED THE NLG STRUT PER M/M INSTRUCTIONS. SYSTEM FUNCTION NORMAL. 2 L 7 2 4F RT A21EA 1999012200158 19990122 00158 EA 1999 1 22 COMA9960028 1 19990110 A 5270 WARNING SYST CNDAIR CL600 CL6002B19 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 710CA 7241 CABIN DOOR LATCH MESSAGE AFTER TAKEOFF. DEFERRED DOOR WORN SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 1999012200159 19990122 00159 EA 1999 1 22 COMA9960029 1 19990109 A 5210 LATCH MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 954CA 7100 CABIN DOOR WARNING MESSAGE. ADJUSTED DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1999012200160 19990122 00160 EA 1999 1 22 COMA9960030 1 19990108 A 3020 300013000002 VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 988CA 2659 7204 RIGHT ENGINE COWL ANTI-ICE MESSAGE. REPLACED ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 1999012200161 19990122 00161 EA 1999 1 22 COMA9960031 1 19990108 A 5270 CONNECTOR CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 7014 CABIN DOOR WARNING MESSAGE. REPAIRED DEFECTIVE WIRING CONNECTOR AT CABIN DOOR. 2 L 7 2 4F RT A21EA 1999012200162 19990122 00162 SO 1999 1 22 COMA9910013 1 19990116 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT LATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 255CA 120238 DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN, CLOSED AND LATCHED DOOR. 2 L 7 2 4T RT A31SO 1999012200163 19990122 00163 SO 1999 1 22 COMA9910014 1 19990117 A 3350 1013073 LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 168CA 120168 EMERGENCY FLOOR LIGHT AT CABIN DOOR IS INOPERABLE. REPALCED LIGHT BULB. 2 L 7 2 4T RT A31SO 1999012200164 19990122 00164 EA 1999 1 22 COMA9960032 1 19990117 A 5270 PS2MB SWITCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 957CA 7109 CABIN DOOR HANDLE WARNING AFTER TAKEOFF. ADJUSTED DOOR HANDLE PROXIMITY SWITCH PS2MB. 2 L 7 2 4F RT A21EA 1999012200165 19990122 00165 EA 1999 1 22 COMA9960033 1 19990116 A 2752 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 719CA 916 7253 FLAPS FAILED AT 17 DEGREES. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 1999012200166 19990122 00166 NE 1999 1 22 COMA9960034 2 19990115 A 7321 8062384 FUEL CONTROL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 943CA 11595 7062 NR 1 ENGINE LAGS NR 2 DURING TAKEOFF. REPLACED THE LEFT ENGINE FUEL CONTROL. 2 L 7 2 4F 4 F RT A21EA E15NE 1999012200167 19990122 00167 EA 1999 1 22 COMA9960035 1 19990117 A 3350 60206 LIGHT CNDAIR CL600 CL6002B19 EA PAX DOOR SMASHED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 MAIN CABIN DOOR EMERGENCY LIGHT IS SMASHED. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A21EA 1999012200168 19990122 00168 NM 1999 1 22 UPS99228341 1 19990115 A 3350 1000679 LIGHT BOEING 727 727185C 138406N NM CABIN MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 EMERGENCY EXIT LIGHT IN COCKPIT DOES NOT COME ON OR IS VERY DIM WHEN EMERGENCY EXIT LIGHT SWITCH SET TO ON. HOWEVER, WH EN SWITCH BEHIND EXIT LIGHT PLASTIC PANEL IS SET TO ON, LIGHT COMES ON BRIGHT. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT ASSY PER MM 33-5 0-01. OPS GOOD. 2 L 7 3 4F A3WE 1999012200169 19990122 00169 NM 1999 1 22 UPS99228356 1 19990114 A 3350 BATTERY BOEING 727 72725C 138400H NM ROW 2ABC DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY EXIT LIGHTS INOP AT SEAT 2ABC. REPLACED EMERGENCY EXIT LIGHT BATTERIES PER 33-50-101, OPS CKECK OK. 2 L 7 3 4F A3WE 1999012200182 19990122 00182 WP 1999 1 22 UPS99828354 1 19990106 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 220-240 MISDRILLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C LONGERON 35R AT FS 220-240 HAS A ROW OF FASTENERS WITH NO OR SHORT ED. REPAIRED LONGERON 35R IAW DH S K 701-833. 2 L 7 4 4F RT 4A25 1999012200184 19990122 00184 NM 1999 1 22 UPS99228359 1 19990106 A 5510 ANGLE BOEING 727 72722C 138400F NM LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C LT STAB TE INBD SUSPECT CRACKS ON WEB SUPPORT ANGLE UPPER AFT END, INBD AND OUTBD OF NR 5 BALANCE BAY. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999012200185 19990122 00185 NM 1999 1 22 UPS99228360 1 19990106 A 7830 06453010059 BRACKET BOEING 727 72722C 138400F NM NR 3 ENGINE TR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C ENGINE NR 3 THRUST REV FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 20-80-01 AND MM 7 8-30-00. 2 L 7 3 4F A3WE 1999012200186 19990122 00186 NM 1999 1 22 UPS99228361 1 19990106 A 7830 064530100 BRACKET BOEING 727 72722C 138400F NM NR 1 ENGINE TR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C ENGINE NR 1 THRUST REV FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 20-80-01 AND MM 7 8-30-00. 2 L 7 3 4F A3WE 1999012200187 19990122 00187 NM 1999 1 22 UPS99228362 1 19990104 A 5330 SKIN BOEING 727 72722C 138400F NM PAX DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C SUSPECT CRACK ON FUSELAGE SKIN AT UPPER FWD CORNER OF FWD ENTRY DOOR. REPAIRED PER EO NR B727-5330-14 60-C. 2 L 7 3 4F A3WE 1999012200188 19990122 00188 NM 1999 1 22 UPS99228363 1 19990106 A 5330 SKIN BOEING 727 72722C 138400F NM BS 400 LIGHTNING STRIKE A IPXA K NONE C F.O.D. IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C LIGHTNING STRIKE ON FUSELAGE SKIN BS 400 BETWEEN S2R AND S3R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1999012200189 19990122 00189 NM 1999 1 22 UPS99228364 1 19990107 A 5754 SKIN BOEING 727 72722C 138400F NM NR 5 LE SLAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C BLEND OUT ON TE OF NR 5 LE SLAT RT WING. DAMAGE REPAIRED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1999012200190 19990122 00190 NM 1999 1 22 UPS99228365 1 19990106 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C DURING INSPECTION OF MAIN CARGO DOOR LATCH, SUPPORT FITTINGS SHEAR TIE FOUND CRACKED ON FRAME AT BS 54 0 AT LATCH SUPPORT FITTING. REPAIR CARRIED OUT IAW SRM 51-40-02, 51-40-03 FIG 1. 2 L 7 3 4F A3WE 1999012200191 19990122 00191 NM 1999 1 22 UPS99228366 1 19990115 A 5753 TRACK BOEING 727 72725C 138400H NM NR 4 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:C (CORROSION C57-581-06.00-03) ON NR 4 FLAP TRACK IN SPOILER BEAM ATTACH HOLES AND AROUND MLG BEAM HOLES . REMOVED OLD FLAP TRACK, INSTALLED NEW FLAP TRACK ON CARD NR 838849, 838505. 2 L 7 3 4F A3WE 1999012200192 19990122 00192 NM 1999 1 22 UPS99228367 1 19990115 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 14 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 LEFT WING EGRESS LIGHTS (EXTERIOR) DO NOT OPERATE. BATTERY PACKS NEED REPLACED 3 TOTAL, P/N 96-2-1015, THEY ARE LOCATED ABOVE ROW 14 RIGHT SIDE OF A/C. REMOVED AND REPLACED LEFT OVERWING EXTERIOR EMERGENCY LIGHT BATTERIES IAW MM 33-50-01. 2 L 7 3 4F A3WE 1999012200193 19990122 00193 NM 1999 1 22 UPS99228369 1 19990115 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY LIGHTS INOP AT LT LAV LOWER LIGHT, AT SEAT 2 C AT BOTTOM OF SEAT, VENTRAL STAIRS AND ALL EXTERIOR LIGHTS OVERW ING. REPLACED NECESSARY BATTERY PACKS FOR EMERGENCY LIGHTING TO ENSURE PROPER OPS PER MM 33-50-01. ALL EMERGENCY LIGHT S EXCEPT THE LEFT OVERWING ARE FUNCTIONAL LEFT WING EGRESS LIGHTS INOP, REFER TO NON ROUTINE. 2 L 7 3 4F A3WE 1999012200194 19990122 00194 NM 1999 1 22 UPS99228370 1 19990114 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY LIGHTS OUT AT CEILING AT ROW 11, LT AFT OVERWING EXIT LIGHT OUT. LOWER EXIT LIGHT OUT IN GALLEY AT SERVICE DO OR. REMOVED AND REPLACED BATTERIES IN ALL SAID LOCATIONS. 2 L 7 3 4F A3WE 1999012200195 19990122 00195 NM 1999 1 22 UPS99528368 1 19990108 A 5347 BAC1520843 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 436UP 25467 INSPECTION TYPE:S-1 CRACKED SEAT TRACK FLANGE AT BS 1010, RBL 16, WL 156. REMOVED CRACKED SEAT TRACK SECTION FROM BS 95 0-BS 1010 RBL 16, WL 156. INSTALLED NEW SEAT TRACK PER SRM 51-10-1. 2 L 7 2 4F RT A2NM 1999012200196 19990122 00196 NM 1999 1 22 UPS99628357 1 19990113 A 3260 SWITCH BOEING 767 76734AF 1385212 NM NLG DOOR MALFUNCTIONED A IPXA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 310UP 27762 ON DESCENT, GOT GEAR DOORS EICAS MSG AND AMBER GEAR DOORS LIGHT. SLOWED TO 250 KNOTS AND LIGHT AND MSG WENT OUT. FOLLO WED CHECKLIST AND RAISED GEAR HANDLE, C/W T/S ERP WAN AND TECH SUPPORT. ALSO, REMOVED AND REPLACED S243 AND S257 NOSE G EAR DOOR SWITCHES, SYS OPS NORMAL. CK'D NOSE GEAR DOORS GAPS AND MISMATCHES WITHIN M/M LIMITS; CHK'D SENSOR GAPS ON S23 4;S253;S256 AND S257 TO BE ATO .120 THOUS. CHK'D LONGITUDNAL SEAL OK FOR SERVICE, CK BULB SEAL GAP AT .200 W/DUCTS. RE MOVED AND REPLACED NOSE GEAR DOOR SWITHCES. OPS CK NORMAL. 2 L 7 2 4F RT A1NM 1999012200199 19990122 00199 WP 1999 1 22 UPS99828373 1 19990103 A 5720 46495961N FITTING DOUG DC8 DC871F 302199D WP WS 410 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 LT WING STA 410 FLAP CANOE INBD SIDE BRACE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0 . 2 L 7 4 4F RT 4A25 1999012200200 19990122 00200 WP 1999 1 22 UPS99828374 1 19990104 A 5320 9755584508 FITTING DOUG DC8 DC871F 302199D WP BS 1278 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 FS 1287 AT LONGERON 21R, THE FLOORBEAM TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200201 19990122 00201 WP 1999 1 22 UPS99828375 1 19990104 A 5320 9755584503 FITTING DOUG DC8 DC871F 302199D WP BS 1324 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 FS 1324 AT LONGERON 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200202 19990122 00202 WP 1999 1 22 UPS99828376 1 19990105 A 5320 47504231N FITTING DOUG DC8 DC871F 302199D WP BS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 FS 902 AT LONGERON 19R, THE INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IA W SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200203 19990122 00203 WP 1999 1 22 UPS99828377 1 19990105 A 5320 47505211N FITTING DOUG DC8 DC871F 302199D WP BS 850 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 LONGERON 1 AT FS 850 LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200204 19990122 00204 WP 1999 1 22 UPS99828378 1 19990105 A 5320 3779659501 FITTING DOUG DC8 DC871F 302199D WP BS 851 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 LONGERON 5L AT FS 851, HAS A CRACKED END FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200205 19990122 00205 WP 1999 1 22 UPS99828379 1 19990105 A 5313 37507571N LONGERON DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 LONGERON 31R AT FS 1050 IS CRACKED. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200206 19990122 00206 WP 1999 1 22 UPS99828380 1 19990106 A 5320 37584952 FITTING DOUG DC8 DC871F 302199D WP BS 1240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 CORROSION ON LONGERON 35R INTERCOSTAL ATTACH FITTING AT FS 1240. REMOVED AND REPLACED FITTING IAW SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200207 19990122 00207 WP 1999 1 22 UPS99828381 1 19990106 A 5720 97532972 ANGLE DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 LT OTBD STUB WING INBD RIB, THE VERTICAL SLOT ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLA CED ANGLE IAW DWG 9753297 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200208 19990122 00208 WP 1999 1 22 UPS99828382 1 19990107 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 RT. WING L/E, LWR SKIN INTERNAL DOUBLER, AT THE L/E OF THE NR 3 PYLON CUTOUT IS CRACKED. STOP DRILLE D CRACK AND REPIARED IAW SRM 57-2-1A FIG 2. 2 L 7 4 4F RT 4A25 1999012200209 19990122 00209 WP 1999 1 22 UPS99828383 1 19990107 A 5720 97532978 ANGLE DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E INBD SIDE OF THE XS 520.168 RIB, THE VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200210 19990122 00210 WP 1999 1 22 UPS99828386 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 466.651 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XS 466.651 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012200211 19990122 00211 WP 1999 1 22 UPS99828387 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XFS 635.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200212 19990122 00212 WP 1999 1 22 UPS99828388 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XFS 628.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200213 19990122 00213 WP 1999 1 22 UPS99828389 1 19990107 A 5720 5769600649 DOUBLER DOUG DC8 DC871F 302199D WP WS 598 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E, LWR T/E DOUBLER AT XFS 598 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPL ACED DOUBLER IAW DWG 5769600 AND SRM 57-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 1999012200214 19990122 00214 WP 1999 1 22 UPS99828390 1 19990107 A 5720 576960037 DOUBLER DOUG DC8 DC871F 302199D WP WS 571 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E, INBD SKIN DOUBLER AT XFS 571 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND RE PLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999012200215 19990122 00215 WP 1999 1 22 UPS99828391 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT 785.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 5 7-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200216 19990122 00216 WP 1999 1 22 UPS99828392 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 741.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT 741.25 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200217 19990122 00217 WP 1999 1 22 UPS99828393 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 741.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XFS 741.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200218 19990122 00218 WP 1999 1 22 UPS99828394 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 722.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XFS 722.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200219 19990122 00219 WP 1999 1 22 UPS99828395 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 716.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XFS 716.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200220 19990122 00220 WP 1999 1 22 UPS99828396 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LT WING L/E RIB AT XFS 860.0 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200221 19990122 00221 WP 1999 1 22 UPS99828397 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LT WING L/E RIB AT XFS 778.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200222 19990122 00222 WP 1999 1 22 UPS99828398 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 722.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LT WING L/E RIB AT XFS 722.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACKED AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200223 19990122 00223 WP 1999 1 22 UPS99828399 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 360.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LT WING L/E RIB AT XFS 360.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200225 19990122 00225 WP 1999 1 22 UPS99828401 1 19990108 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XFS 304.00 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200226 19990122 00226 WP 1999 1 22 UPS99828402 1 19990108 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 442.185 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XS 442.185 IS CRACKED AT THE UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200227 19990122 00227 WP 1999 1 22 UPS99828403 1 19990108 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 454.976 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT XS 454.976 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200228 19990122 00228 WP 1999 1 22 UPS99828404 1 19990110 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 390-450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LONGERON 35L AT FS 390-450 HAS SEVERE CORROSION. REMOVED, FABRICATED, AND REPLACED LONGERON IAW SRM 53-4-1 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200229 19990122 00229 NM 1999 1 22 QXEA9900022 1 19990112 A 2611 PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 367PH 511 PDX- LAVATORY SMOKE DETECTOR ALARM SOUNDED ON CLIMB-OUT. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF FIRE OR SMOKE. REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999012200230 19990122 00230 WP 1999 1 22 99FDEA00011 1 19990113 A 5270 SWITCH DOUG DC10 DC1030F 3023504 WP AC DOOR INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 317FE 46835 AT FL 180 AIR COND DOOR LIGHT CAME ON. A/C REMAIN PRESS, RETURN TO MEM. *S/D* REMOVED AND REPLACED BOTH LEFT SIDE ACC ESS DOOR SWITCH IAW MM 52-70-07. REMOVED AND REPLACED RING TERMINAL, P1-1618 AND RE-TERMINATED WIRES IAW MM CHAPTER 20. AIR COND DOOR LIGHT CK GOOD IAW MM 52-70-07. 2 L 7 3 4F RT A22WE 1999012200231 19990122 00231 NM 1999 1 22 99FDEA00012 1 19990115 A 7930 TRANSMITTER BOEING 727 727227 1384078 NM NR 3 ENGINE MALFUNCTIONED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 481FE 21463 99-0012 - NR 3 ENG LOW OIL PRESS LIGHT ILLUM AFT T/O. ACCOMPLISH ABNORMAL CK LIST WHICH REQUIRE SHUTDOWN. FOUND BLEED AIR DUCT AT STARTER BLOWN. REMOVED AND REPLACED NR 3 OIL PRESSURE TRANSMITTER,SWITCH PER 727 MM 79-32-1,79-33-1. REMOV ED AND REPLACED STARTER SUPPLY DUCT, FUEL HOSE ASSY PER MM 80-11-11, 77-00. 2 L 7 3 4F A3WE 1999012200232 19990122 00232 WP 1999 1 22 99FDEA00013 1 19990114 A 2751 TRANSMITTER DOUG DC10 DC1030F 3023504 WP TE FLAP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 314FE 48312 99-0013 - ON T/O FLAP LIMIT CHANNEL INOP AND SELECT FLAP LIMIT OVERRIDE LIGHT ILL IN READ 10 DEG LT SIDE AND 4 DEG RT SI DE. FOUND LT OTBD FLAP POS TRANSMITTER BAD. REMOVED AND REPLACED SAME PER MM 27-54-03-2. OPS CK GOOD. FOUND DUPLEX A CTUATOR INOP MM 27-56-01-2. 2 L 7 3 4F RT A22WE 1999012200233 19990122 00233 WP 1999 1 22 ABXA9900009 1 19990112 A 3260 H141003 SWITCH DOUG DC8 DC861 3021952 WP RT MLG DEFECTIVE A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 843AX 46017 DURING APPROACH, RIGHT MAIN LANDING GEAR INDICATOR DID NOT ILLUMINATE. EXECUTED GO-AROUND AND RECYCLED GEAR. INDICATIO N WAS NORMAL. REPLACED RIGHT MAIN LANDING GEAR DOWN SWITCH. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999012200234 19990122 00234 WP 1999 1 22 ABXA9900010 1 19990114 A 5270 H2024B SWITCH DOUG DC8 DC861 3021952 WP CARGO DOOR DAMAGED A ABXA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 849AX 45891 AFTER CLIMB-OUT, AFTER TURNING LAST CTC ON, CARGO DOOR WARNING LIGHT ILLUMINATED. DUMPED 20,000 POUNDS OF FUEL AND RETU RNED TO ILN. FOUND LOWER DOOR JAMB SWITCH ARM BENT. REPLACED SWITCH. PRESSURIZED AIRCRAFT. DOOR INDICATION LIGHT, OP S CHECKED GOOD. 2 L 7 4 4F 4A25 1999012200235 19990122 00235 WP 1999 1 22 ABXA9900011 1 19990107 A 5412 59177176 BULKHEAD FITTING DOUG DOUG DC9 DC941 302207N WP BS 1115 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING C-CHECK, FOUND AFT PYLON BULKHEAD ATTACH FITTING CRACKED AT STATION 1115 AND LONGERON 15R. REPLACED FITTING IAW DC9 SRM 51-30-01 AND 51-30-02. 2 L 7 2 4F A6WE 1999012200236 19990122 00236 WP 1999 1 22 ABXA00012 1 19990107 A 5311 5911448523 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 484 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 947AX 47004 DURING C-CHECK, FOUND FRAME AT STATION 484, LONGERON 29 LEFT AND 29 RIGHT. REPLACED SECTION OF FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999012200237 19990122 00237 WP 1999 1 22 ABXA9900013 1 19990107 A 5313 59114277 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 947AX 47004 DURING C-CHECK, FOUND CRACK IN LONGERON 16 RIGHT AT STATION 965. REPLACED SECTION OF LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999012200238 19990122 00238 WP 1999 1 22 ABXA9900014 1 19990107 A 5311 99582387 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 947AX 47004 DURING C-CHECK, FOUND CRACK IN FUSELAGE FRAME AT STATION 980, LONGERON 16 LEFT. REPLACED FRAME SECTION IAW DC9 SRM 53-0 3. 2 L 7 2 4F A6WE 1999012200239 19990122 00239 WP 1999 1 22 ABXA9900015 1 19990113 A 5400 591326241 ANGLE DOUG DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND LEFT PYLON UPPER ATTACH ANGLE CRACKED. REPAIRED ATTACH ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1999012200240 19990122 00240 WP 1999 1 22 ABXA9900016 1 19990115 A 5320 591024175 FITTING DOUG DOUG DC9 DC941 302207N WP BS 1152 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING C-CHECK, FOUND LEFT HEAT EXCHANGER AFT, OUTBOARD MOUNT FITTING CRACKED AT LONGERON 6 LEFT AND STATION 1152. REPL ACED MOUNT FITTING IAW DC9 SRM 51-30-01. 2 L 7 2 4F A6WE 1999012200241 19990122 00241 WP 1999 1 22 ABXA9900017 1 19990115 A 5412 49125402 BULKHEAD FITTING DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING C-CHECK, FOUND PYLON BULKHEAD LOWER FLOOR FITTING CRACKED AT STATION 1041 AND RBL 30. REPAIRED IAW DC9 SRM 54-12 . 2 L 7 2 4F A6WE 1999012200242 19990122 00242 WP 1999 1 22 ABXA9900018 1 19990115 A 5311 5911448519 FRAME DOUG DOUG DC9 DC941 302207N WP BS 484 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING C-CHECK, FOUND FRAME AT STATION 484 CORRODED FROM LONGERON 29 RIGHT TO 29 LEFT. REPAIRED FRAME IAW DC9 SRM 53-03 . 2 L 7 2 4F A6WE 1999012200243 19990122 00243 WP 1999 1 22 ABXA9900019 1 19990115 A 5320 3913575503 INTERCOSTAL DOUG DOUG DC9 DC941 302207N WP BS 541-560 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT STATION 541-560 AND BLO 0.0. REPAIRED INTERCOSTAL IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 1999012200244 19990122 00244 WP 1999 1 22 ABXA9900020 1 19990115 A 5315 99115441 FLOORBEAM DOUG DOUG DC9 DC941 302207N WP BS 541 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING C-CHECK, FOUND FLOORBEAM CORRODED AT STATION 541 AND BLO 0.0. REPAIRED IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 1999012200245 19990122 00245 WP 1999 1 22 MWEA99031 1 19990113 A 3412 034100025 RAT PROBE DOUG DC9 DC932 3022066 WP COCKPIT FAILED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 216ME 47740 RAT PROBE DRAWS ZERO AMPS. MAINTENANCE REMOVED AND REPLACED RAT PROBE. 2 L 7 2 4F A6WE 1999012200246 19990122 00246 NM 1999 1 22 MWEA99032 1 19990113 A 5241 NAS5624R12A CAM DOUG MD88 MD88 3023688 NM GALLEY DOOR WORN A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 808ME 48070 AFT GALLEY DOOR DID NOT PROPERLY CLOSE CAUSING AIR LEAK. MAINTENANCE REMOVED AND REPLACED CAM FOLLOWER ON DOOR. 2 L 7 2 4F RT A6WE 1999012200247 19990122 00247 WP 1999 1 22 MWEA99033 1 19990113 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 500ME 45711 ON PREFLIGHT, INSPECTION FOUND GALLEY DOOR SLIDE UNSTOWED. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1999012200248 19990122 00248 WP 1999 1 22 MWEA99034 1 19990109 A 5330 59134211 SKIN DOUG DC9 DC914 3022034 WP BS 108 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 AIRCRAFT SKIN IS CRACKED AT STATION 108 LONGERON 27R. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999012200249 19990122 00249 WP 1999 1 22 MWEA99035 1 19990114 A 7110 5910306501 COWL DOUG DC9 DC914 3022034 WP LT ENGINE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND CRACK ON LEFT ENGINE UPPER COWL AROUND RIVEL ON PREVIOUS REPAIR. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REP AIR. 2 L 7 2 4F A6WE 1999012200250 19990122 00250 WP 1999 1 22 MWEA99036 1 19990114 A 5230 99576611N INTERCOSTAL DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND CRACKED INTERCOSTAL IN FORWARD CARGO BAY DOOR. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999012200251 19990122 00251 WP 1999 1 22 MWEA99037 1 19990114 A 5311 991184297 FRAME DOUG DC9 DC914 3022034 WP BS 964 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 THE TAILCONE JETTISON HANDLE EXIT SIGN IS CHAFFING HEAVILY INTO THE CANTED FRAME AT STATION 964. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999012200254 19990122 00254 NM 1999 1 22 DL72S990060 1 19990111 A 5312 6516350 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 A CRACK WAS FOUND IN THE LBL 36.83 VERT STIFFENER ON THE FWD SIDE OF THE BS 1183 BLKHD. CRACK IS LOCATED APPROX AT WL 2 38 AND IS APPROX 2 IN LENGTH. REPAIRED PER ERA 332664-14. 2 L 7 3 4F A3WE 1999012200255 19990122 00255 NE 1999 1 22 DL76K990061 2 19990110 A 7200 ENGINE CF680C2B6F BOEING 767 767332 1382001 NM GE CF6 CF680C2B2 30025 NE NR 2 FAILED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 174DZ 704751 29693 704751 COMPRESSOR STALL ON TAKEOFF RETARDED THROTTLE AIR TURN BACK, FOUND METAL IN TAIL PIPE ON INSPECTION. CHANGING NR 2 ENGI NE. 2 L 7 2 4F 4 F RT A1NM E13NE 1999012200256 19990122 00256 NM 1999 1 22 DLM88990064 1 19990111 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 968DL 17183 53161 IMMEDIATELY AFTER TAKEOFF, F/A NOTICED STRONG ODOR IN AFT CABIN, DESCRIBES AS BURNING RUBBER. PERFORMED DUCT BURN OUT. REPLACED COALESCER BAGS. 2 L 7 2 4F RT A6WE 1999012200257 19990122 00257 NM 1999 1 22 DL72S990065 1 19990111 A 5754 SKIN BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 4.5 INCH CRACK IN NR 8 SLAT COVE SKIN ANGLE AT O/B UPSTOP PAD. REPAIR PER MM 57-54-0 PG 816. 2 L 7 3 4F A3WE 1999012200260 19990122 00260 NM 1999 1 22 DL76L990069 1 19990111 A 5400 SPAR WEB BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 PYLON NR 1 ENGINE STRUT AFT UPPER SPAR WEB, STA 222, LBL 4 CRACK REPAIR. THE AFT UPPER SPAR WEB OF THE NR 1 ENGINE PYLO N STRUT WAS FOUND WITH .5 CRACK IN THE AFT, OUTBD CORNER OF THE ECS DUCT CUTOUT AT STA 222 AND LBL 4. THE CRACK WAS ROU TED OUT WITH A SMOOTH RADIUS AND REPAIRED WITH A STEEL REPAIR. DOUBLER PER ER/A 366388-14, REV B. 2 L 7 2 4F RT A1NM 1999012200261 19990122 00261 NM 1999 1 22 DLM88990070 1 19990112 A 2120 AIR DISTRIBUTION DOUG MD88 MD88 3023688 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 909DL 49540 STRONG SMELL REPORTED JUST BEFORE LANDING IN AFT SECT OF CABIN. TURNED ON ALL OVENS AND COFFEE MAKERS IN AFT GALLEY. I NSPECTED LIGHT BALLASTS, NO ABNORMAL ODORS. RAN PACKS ALL CK OK. 2 L 7 2 4F RT A6WE 1999012200262 19990122 00262 WP 1999 1 22 DLL19990075 1 19990112 A 2120 AIR DISTRIBUTION LKHEED 1011 10113853 5265020 WP GALLEY ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 760DH 193Y1194 JUST PRIOR TO LDG, F/AS IN AFT GALLEY SENSED ELECTRICAL SMELL. ALSO, PERSISTED FOR COUPLE MINUTES AFTER LDG, 2ND OFF WE NT BACK AFTER LDG, BUT UNABLE TO CONFIRM. RAN OVENS AND COFFEE MAKERS FOR SEVERAL MINUTES. UNABLE TO DUPLICATE. NO E LECTRICAL SMELL OR SMOKE DETECTED. 2 L 7 3 4F A23WE 1999012200263 19990122 00263 NM 1999 1 22 DL73K990077 1 19990112 A 3397 WIRE BR9279108 BOEING 737 737232 1384475 NM PAX DOOR SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 304DL 23076 LEFT AND RIGHT FWD DOORS EMERGENCY LIGHT EXIT IDENTIFIERS DO NOT ILLUMINATE WHEN TESTED. POWER SUPPLY FUSE BLOWN DUE TO LEFT LIGHT ASSY WIRE SHORTED. REPLACED FUSE IN POWER SUPPLY AND REPLACED LEFT LIGHT ASSY. 2 L 7 2 4F RT A16WE 1999012200264 19990122 00264 NM 1999 1 22 DL72S990080 1 19990113 A 3350 334701744 BATTERY CHARGER 900542 BOEING 727 727232 1384082 NM RT OVERWING EXIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 541DA 10007 22387 ON LAYOVER CHECK, FOUND EMERGENCY EXIT LIGHTS INOP OVER THE RIGHT WING OVER WING EXITS. REPLACED BATTERY CHARGER OPERAT ION NORMAL DPN 334701744 S/N OFF 10007, ON DL52. 2 L 7 3 4F A3WE 1999012200265 19990122 00265 NM 1999 1 22 DL72W990081 1 19990114 A 2751 CONNECTOR BOEING 727 727247 138408F NM TE FLAPS DIRTY A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 290WA 22108 OUTBOARD FLAPS INDICATED ONLY 1 DEG. WHEN FLAPS LEVER WAS AT FIVE. POSITIONED FLAP LEVER BACK UP. FOLLOWED POM PROCEDU RE FOR TRAILING EDGE O/B FLAP MALFUNCTION. BROKE SAFETY WIRES ON GPWS AND ALTERNATE FLAP SWITCH. TRIED O/B FLAP INDICA TOR NO HELP. CLEANED CONNECTOR ON OB FLAP BYPASS VALVE. OPERATION NOW NORMAL. INSPECTED OB FLAP FOR DAMAGE. NONE FOU ND RESAFTIED ALT FLAP AND GPWS SWITCHES. 2 L 7 3 4F A3WE 1999012200346 19990122 00346 NM 1999 1 22 TWAA9901101 1 19990118 A 3350 LIGHT BOEING 767 767231 1385131 NM ROW 18-22 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 610TW 22573 FLOOR EGRESS LIGHTING WAS INOPERATIVE FROM CABIN ROW 18 TO 22. REMOVED MOISTURE FROM TRACK AT SERVICE CENTER CROSSOVER. CHECK-C 12-2-98 LAX. 2 L 7 2 4F RT A1NM 1999012200347 19990122 00347 NM 1999 1 22 TWAA9901102 1 19990118 A 3350 918031TS LIGHT BOEING 727 727231 1384079 NM CABIN INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54340 20845 THE EGRESS LIGHT STRIP WAS INOPERATIVE IN THE FORWARD CABIN LEFT SIDE. REPLACED THE LIGHT STRIP. CHECK-C 9-3-98 MCI. 2 L 7 3 4F A3WE 1999012200348 19990122 00348 NE 1999 1 22 TWAA9901103 2 19990117 A 7314 378200 FUEL PUMP BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE FAILED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 CE 05 54340 20845 1907 ABORTED TAKEOFF WHEN THE NUMBER 3 ENGINE SHUT ITSELF DOWN DURING TAKEOFF ROLL. FOUND THE FUEL PUMP SHAFT SHEARED. REPL ACED THE FUEL CONTROL, (P/N 743602-5) AND THE ENGINE FUEL PUMP. CHECK-C 9-3-98 MCI. 2 L 7 3 4F 4 F A3WE E2EA 1999012200349 19990122 00349 NM 1999 1 22 TWAA9901104 1 19990118 A 3350 6013211 BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54340 20845 THE FORWARD LEFT AND FORWARD RT CABIN DOOR SLIDE LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 9-3 -98 MCI. 2 L 7 3 4F A3WE 1999012200350 19990122 00350 WP 1999 1 22 TWAA9901105 1 19990118 A 3230 RETRACT MECH DOUG DC9 DC983 3022083 WP LANDING GEAR ICED UP A TWAA K NONE O OTHER AP APPROACH 1 CE 05 9303K 49529 THE LANDING GEAR HANDLE WAS DIFFICULT TO MOVE TO THE DOWN POSITION. REQUIRED TWO HANDS AND SOME FORCE. MAINTENANCE PER FORMED NORMAL AND EMERGENCY GEAR EXTENSION AND FOUND NORMAL. CHECKED CABLE RUNS IN ELECTRONIC COMPT AND FOUND NORMAL. P OSSIBLE ICE AFTER HEAVY RAIN AT DEPARTURE STATION. CHECK-C 11-25-98 MCI. 2 L 7 2 4F RT A6WE 1999012200351 19990122 00351 WP 1999 1 22 TWAA9901106 1 19990119 A 3350 58222 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOP A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 931L 47173 THE AFT MOST SECTION OF CABIN FLOOR EGRESS LIGHTS ILLUMINATED IN FLIGHT. CREW TRIED TO RESET BY DISARMING AND REARMING, BUT NO HELP. REPLACED THE POWER SUPPLY. CHECK-C 12-7-98 STL. 2 L 7 2 4F A6WE 1999012200352 19990122 00352 WP 1999 1 22 TWAA9901107 1 19990119 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK AT STA 200 TO 237, RBL 22. REPLACED SEAT TRACK AT PREVIOUS SPL ICE REPAIR WITH (P/N 5910820-3) PER SRM 53-05 FIG F. 2 L 7 2 4F A6WE 1999012200353 19990122 00353 WP 1999 1 22 TWAA9901108 1 19990118 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND STRINGER 4L CRACKED AT STA 200. NEW STRINGER INSTALLED FROM STA 148 TO 229, FACTORY SPL ICE TO END. 2 L 7 2 4F A6WE 1999012200354 19990122 00354 WP 1999 1 22 TWAA9901109 1 19990118 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND STRINGER 2L CRACKED AT STA 200. NEW STRINGER INSTALLED FROM STA 148 TO 229, FACTORY SPL ICE TO END. 2 L 7 2 4F A6WE 1999012200355 19990122 00355 NM 1999 1 22 HNAA9900011 1 19990116 A 3530 MR10042 PBE DHAV DHC8 DHC8102 2809003 NM CABIN UNSERVICEABLE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 930HA 126 PERSONAL BREATHING EQUIPMENT (PBE) IN FLIGHT ATTENDANT'S CLOSET RED INDICATOR PROTRUDING PAST FACE OF CONTAINER. REPLAC ED PBE. 2 H 7 2 4T RT A13NM 1999012200356 19990122 00356 NM 1999 1 22 HNAA9900012 1 19990115 A 5320 INTERCOSTAL DHAV DHC8 DHC8102 2809003 NM FRAME 270 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 828MA 333 INTERCOSTAL AFT OF SILL MEMBER LOCATED AFT OF FRAME X270 IN FUSELAGE RIGHT SIDE HAS HOLE IN FORWARD RADIUS. REPAIRED AS NECESSARY. INTECOSTAL AT STRINGER 23S FRAME X264.1 AND X270.5 CRACKED AT RIVET HOLE JUST FORWARD OF AFT HI-LOK IN LEG A TTACHED TO SEAT RAIL. REPAIRED AS NECESSARY. CLEAT GOUGED THROUGH MATERIAL APPROXIMATELY .200 AT RADIUS ON AFT SIDE OF FRAME X264.1 AND STRINGER 23S. REPAIRED AS NECESSARY. 2 H 7 2 4T RT A13NM 1999012200357 19990122 00357 NM 1999 1 22 HNAA9900013 1 19990115 A 2400 CONDUIT DHAV DHC8 DHC8102 2809003 NM RT WING DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 RIGHT WING WIRE CONDUIT RIPPED OPEN AND BRACKET DAMAGED AT NR 4 FLAP JACKSCREW LOCATION. REPAIRED AS NECESSARY. 2 H 7 2 4T RT A13NM 1999012200358 19990122 00358 NM 1999 1 22 HNAA9900014 1 19990115 A 5752 BRACKET DHAV DHC8 DHC8102 2809003 NM RT AILERON TAB CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 RIGHT HAND AILERON TRIM TAB ATTACH BRACKET CRACKED APPROXIMATELY 1 INCH RADIUS ON AFT SIDE FORWARD. REPLACED BRACKET. 2 H 7 2 4T RT A13NM 1999012200359 19990122 00359 NM 1999 1 22 HNAA9900015 1 19990115 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM RT TE FLAP CHAFED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 RIGHT HAND WING OUTBOARD FLAP INBOARD UPPER SKIN HAS CHAFE, DEPTH IS .009 LENGTH AND WIDTH .3 BY .3 LOCATED 2.5 INCHES F ROM INBOARD EDGE. REPAIRED AS NECESSARY. 2 H 7 2 4T RT A13NM 1999012200360 19990122 00360 NM 1999 1 22 K3HA990003 1 19990116 A 3350 08153000111 LIGHT BOEING 727 727225 1384077 NM CABIN LOOSE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 FLOOR EMERGENCY LIGHTS JUST OUTSIDE COCKPIT DOOR LOOSE. REMOVED AND REPLACED EMERGENCY LIGHTS, TRACK BASE AND COVER. T EST OK, REFERENCE MM 33-50-01. 2 L 7 3 4F A3WE 1999012200361 19990122 00361 NM 1999 1 22 AWXA9900016 1 19990112 A 2120 DUCT BOEING 737 737277 1384570 NM CABIN FAILED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 178AW 22645 PASSING 4500 FT DURING CLIMBOUT, CABIN CREW REPORTED STRONG BURNING FUMES AND A SLIGHT AMOUNT OF SMOKE IN COCKPIT AND CA BIN SIDEWALL VERY HOT TO TOUCH, ROW 6 AIRCRAFT LEFT. ALSO, FLT CREW SMELLED FUMES, EXECUTED AIR TURNBACK. REMOVED ANS REPLACED CABIN TEMP CONTROL REG, AIR COND RELAY UNIT, TEMP SEL, TEMP CTRL, SENSOR, ANTICIPATOR SENSOR, DUCT TEMP LIMIT S ENSOR AND OPS TEST NORMAL, REF LOG 7441246. CABIN WOULD NOT HEAT MIX VALVES AT 1/2 OPEN DUCT TEMP 120-130 DEG, CABIN TE MP 60 DEG. NO AIR COMING FROM OVERHEAD OR FLOOR DUCTS. REMOVED AND REPLACED RT DISTRIBUTION DUCT. 2 L 7 2 4F RT A16WE 1999012200362 19990122 00362 EU 1999 1 22 AWXA9900017 1 19990111 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU L 1 DOOR INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 621AW 053 EXIT LIGHT ABOVE L-1 DOOR INOP. REPLACED EMERGENCY EXIT LIGHT ASSY. 2 L 7 2 4F RT A28NM 1999012200363 19990122 00363 EU 1999 1 22 AWXA9900018 1 19990114 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 55 OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND OPS GOOD. 2 L 7 2 4F RT A28NM 1999012200364 19990122 00364 NM 1999 1 22 RAAA99B2001 1 19990114 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999012200365 19990122 00365 NM 1999 1 22 RAAA99B2002 1 19990115 A 3350 873100112 LIGHT BOEING 727 72722C 138400F NM ROW 22 DAMAGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FLIGHT CREW REPORTED PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT LENS BROKEN AND BULB MISSING. CHANGED LIGHT ASSY DUE DAMAG ED. 2 L 7 3 4F A3WE 1999012200366 19990122 00366 NM 1999 1 22 RAAA99B2003 1 19990115 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999012200367 19990122 00367 SO 1999 1 22 RAAA99E8002 1 19990114 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO COCKPIT FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 COCKPIT PULLDOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 4 4T 4A22 1999012200368 19990122 00368 SO 1999 1 22 RAAA99E9003 1 19990115 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 3 & 13 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROWS 3 AND 13 FLOOR PROXIMITY EGRESS LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 4 4T 4A22 1999012200369 19990122 00369 SO 1999 1 22 RAAA99E9004 1 19990115 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO ROW 2 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 2 PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY DUE FAILED. 2 L 7 4 4T 4A22 1999012200370 19990122 00370 SO 1999 1 22 RAAA99E9005 1 19990115 A 3350 873100212 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 4 4T 4A22 1999012200371 19990122 00371 NE 1999 1 22 9900161232 2 19990110 A 7320 CIT SENSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 232NW 46961 528364 DURING TAKEOFF ROLL, THE NR 3 ENGINE HAD LAGGING N1 INDICATION AND LOW FUEL FLOW INDICATION. THE TAKEOFF WAS ABORTED AT 110 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CHECKED THE COMPRESSOR DISCHARGE LINE FOR LEAKS AND CLEANED THE LINE. ALSO, THE CIT SENSOR WAS CHANGED. AN ENGINE RUN WAS THEN PERFORMED WITH MAXIMUM POWER OBTAINED AND ALL PERF ORMANCE PARAMETERS WITHIN LIMITS. 2 L 7 3 4F 4 F A22WE E23EA 1999012200372 19990122 00372 WP 1999 1 22 9900179928 1 19990112 A 3231 LINK DOUG DC9 DC931 3022065 WP NLG DOOR BINDING A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8921E 45836 DURING APPROACH, THE NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. FLIGHT CREW DECLAR ED AN EMERGENCY AND MANUAL GEAR EXTENSION WAS ACCOMPLISHED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RI GHT NOSE GEAR FORWARD DOOR LINK BINDING. REPLACED LINK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999012200373 19990122 00373 NM 1999 1 22 UPS99228412 1 19990108 A 7120 QF71221073 CROSS STRUT BOEING 727 72722C 138400F NM NR 2 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, ENGINE NR 2 PITTING CORROSION ON TUBE OF CROSS STRUT. REPLACED CROSS STRUT ASSEMBLY IAW MM 71-12-11. 2 L 7 3 4F A3WE 1999012200374 19990122 00374 NM 1999 1 22 UPS99228417 1 19990106 A 5411 65229136 RIB BOEING 727 72722C 138400F NM NR 2 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, SUSPECT CRACK ON CENTER ENGINE AFT MOUNT SUPPORT RIB RIGHT CHORD APP ROX 17 INCHES FROM TOP OF CHORD. RIB CHORD REPLACED IAW DRAWING 65-22913, 65-17553, 65-17551. 2 L 7 3 4F A3WE 1999012200386 19990122 00386 WP 1999 1 22 UPS99828422 1 19990104 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 364 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING UPPER SKIN AT STA 364 AND STR 10 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2- 1 FIG 21A. 2 L 7 4 4F RT 4A25 1999012200387 19990122 00387 WP 1999 1 22 UPS99828423 1 19990109 A 5313 2610338 LONGERON DOUG DC8 DC871F 302199D WP BS 85-95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, LONG 35R FS 85 TO 95 IS CRACKED UNDER THE SPLICE. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 53-2-2 AND 51-1-2OD. 2 L 7 4 4F RT 4A25 1999012200392 19990122 00392 NM 1999 1 22 99FDEA00014 1 19990116 A 3610 CLAMP BOEING 727 72722 1384002 NM BLEED AIR DUCT LOOSED A FDEA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 25 185FE 18871 ENGINE STRUT OVERHEAT LIGHT ILLUM. CK LIST TURN OFF AFFECT WING ANTI-ICE SWITCH CLOSED. ENG STRUT O/H LIGHT WENT OUT. CREW COMMENT, O/H LIGHT WENT OUT WITH ENG PWR DECREASED. FOUND LOOSE CLAMP AT 13TH STAGE CHECK VALVE. TIGHTENED CLAMP . NO O/H AT THIS TIME. 2 L 7 3 4F A3WE 1999012200393 19990122 00393 EU 1999 1 22 99FDEA00015 1 19990116 A 7830 1212828 CABLE AIRBUS 310 A310203 3930313 EU NR 1 ENG TR UNIT TWISTED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 404FE 233 ON T/O ROLL (BELOW 80 KTS) AMBER NR 1 ENG REVERSER UNLOCK LIGHT ILLUM. REJECTED T/O AND RETURNED TO GATE FOR INSPECTION . PERFORMED REJECTION TAKEOFF CHECKLIST. FOUND RT LOWER FLEX CABLE HOUSING TWISTED AND BINDING. REMOVED AND REPLACED FLEX CABLE PER AMM 78-31-12 PG 201-203. T/R OPS CK GOOD ON ENG RUN. 2 L 7 2 4F RT A35EU 1999012200394 19990122 00394 NM 1999 1 22 99FDEA00016 1 19990118 A 5312 65192923 BULKHEAD WEB BOEING 727 72725C 138400H NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 WHILE WORKING NR 500, FOUND AFT BULKHEAD FOR WING CTR SECTION TO BE CORRODED AT RBL 7.5 AND 14.5, WL 150 AND AT BL 0, WL 165, BS 870. *S/D* REMOVED AND REPLACED AFT BULKHEAD FOR WING CTR SECTION BS 870, RBL 70 - LBL 70 PER FEDEX EA 7-5710 -43764. 2 L 7 3 4F A3WE 1999012200395 19990122 00395 NM 1999 1 22 99FDEA00017 1 19990118 A 5711 6595600762 SPAR BOEING 727 72725C 138400H NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 UPON REMOVAL OF CTR WING SECTION AFT BULKHEAD WEB FOUND VERTICAL FLANGE OF LWR 870 SPAR CHORD TO BE CORRODED FROM LBL 60 -RBL 35. 2 L 7 3 4F A3WE 1999012200396 19990122 00396 NM 1999 1 22 99FDEA00018 1 19990118 A 5320 65442341 CHORD BOEING 727 72725C 138400H NM BS 1090 & 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 574 - WHILE WORKING ON NR 395 DISCOVERED CORROSION ON BL0 CHORD AT BS 1090 AND 1110, LBL 2, WL 200. REPLACED BLO CHO RD FROM 1157 TO 1060 PER FED-EX DRAWING 65-44234. 2 L 7 3 4F A3WE 1999012200397 19990122 00397 NM 1999 1 22 99FDEA00019 1 19990118 A 5315 65402732 FLOORBEAM BOEING 727 72725C 138400H NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 575 WHILE WORKING ON NR 395, DISCOVERED CORROSION ON FLOORBEAM LWR CHORD BS 1050, RBL 2, WL 200. REPAIRED FLOORBEAM PER FEDEX EA 7-5310-43772 REV A. 2 L 7 3 4F A3WE 1999012200398 19990122 00398 NM 1999 1 22 99FDEA00020 1 19990118 A 5314 65258101 KEEL BEAM BOEING 727 72725C 138400H NM BS 1121-1180 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 577 - CORROSION ON LEFT KEEL BEAM AT BS 1166. REMOVED AND REPLACED KEEL BEAM FROM BS 1121 TO 1180, LBL 10 PER FED-EX SRM 51-30-2. 2 L 7 3 4F A3WE 1999012200399 19990122 00399 NM 1999 1 22 99UAL900020 1 19990108 A 5220 DOOR AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE EMER EXIT MISINSTALLED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 816UA 871 OVERWING EMERGENCY EXIT DOOR AIR LEAK. SEATS 9BC AND 10ABC NOT TO BE OCCUPIED DURING FLIGHT UNTIL REPAIRS ARE COMPLETE. FOUND DOOR INSTALLED INCORRECTLY WITH SEAL STUCK IN THE GAP BETWEEN THE DOOR AND FUSELAGE. DOOR WAS REINSTALLED CORRE CTLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1999012200400 19990122 00400 NE 1999 1 22 99UAL900021 2 19990110 A 7320 METERING PORT AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE NR 1 ENGINE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 802UA 690 NR 1 ENG LEAKING STREAM OF FUEL WHEN ENG RUNNING. APPEARS TO BE FROM FUEL METERING PORT ON BOTTOM DRAIN FIN. FUEL METE RING UNIT LEAKING FROM DRAIN MAST. NOT A NEW PROBLEM. MRR NOT REQUIRED. COA IN PROCESS TO REDUCE FUEL LEAKS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999012200401 19990122 00401 EU 1999 1 22 99UAL900022 1 19990108 A 8011 STARTER AIRBUS 320 A320232 3930326 EU NR 1 ENGINE SMOKED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 403UA 442 NR 1 ENG STARTER BLEW SPARKS AND SMOKE DURING START AT PUSHBACK. 2 L 7 2 4F RT A28NM 1999012200402 19990122 00402 EU 1999 1 22 99UAL900023 1 19990110 A 3230 RETRACT MECH AIRBUS 320 A320232 3930326 EU NLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 414UA 472 COULD NOT RETRACT NOSE GEAR. ALSO, LGCIU 1 AND 2 SHOWED FAILED. CONNECTED TO UNI. 2 L 7 2 4F RT A28NM 1999012200403 19990122 00403 NE 1999 1 22 99UAL900024 2 19990109 A 7530 7437173 CABLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 609UA 21870 FLYING THROUGH THE TOP OF A CELL FL370, HEAVY PRECIPITATION, ANTI-ICE ON, MODERATE TURBULANCE. NR 2 ENG HAD MULTIPLE CO MPRESSOR STALLS AND LOSS OF POWER FOR APPROX 30-45 SECONDS, THEN RECOVERED. DIVERTED MIA. *S/D* FOUND 3.0 BLEED VALVE FEEDBACK TO ENGINE VANE AND BLEED CONTROL CABLE FORCE WAS HIGH REF MM753205. REPLACED UPPER FEEDBACK CABLE AND CLEANED LOWER FEEDBACK CABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999012200404 19990122 00404 NM 1999 1 22 99UAL900025 1 19990111 A 2782 10617927 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 5 LE SLAT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7287U 21565 UNABLE TO RETRACT NR 5 SLAT, NOTICEABLE YAW. RETURNED TO DTW. *S/D* REPLACED NR 5 LEADING EDGE SLAT ACTUATOR, SYSTEM OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1999012200405 19990122 00405 NM 1999 1 22 99UAL900026 1 19990110 A 2782 10617927 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 5 LE FLAP FAILED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 7461U 21915 ON EXTENSION OF FLAPS NR 5 KRUEGER FLAP DID NOT EXTEND. AMBER LIGHT ON FORWARD PANEL REMAINED ON. SECOND OFFICERS PANE L INDICATED NO EXTENSION. YAW WAS PRESENT IN CONTROLS. MISSED APPROACH WAS ACCOMPLISHED. *S/D* REPLACED LEADING EDGE FLAP ACTUATOR, SYSTEM OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999012200406 19990122 00406 NM 1999 1 22 99UAL900027 1 19990109 A 3260 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7449U 21903 RIGHT GEAR DOOR INDICATION LIGHT ON DURING CLIMBOUT OF MSP. RETURNED TO MSP FOR MAINTENANCE INSPECTION. *S/D* ACCOMPL ISHED TEST OF LANDING GEAR DOOR WARNING SWITCH, TESTS GOOD. ENGINEERING FOLLOWUP - ADDED ITEM TO ACCOMPLISH PRECAUTION ARY REPLACEMENT OF LANDING GEAR WARNING SWITCH AND DOOR ACTUATOR ASSY. 2 L 7 3 4F 4 F A3WE E2EA 1999012200407 19990122 00407 NM 1999 1 22 99UAL900028 1 19990111 A 2160 VALVE ALLIED SIGNA 39811611 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RIGHT FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 989UA 4999 21751 RIGHT MIX VALVE STUCK IN FULL COLD POSITION IN MANUAL AND AUTO SELECTIONS. *S/D* RIGHT HAND MIX VALVE FAILED IN THE FU LL COLD POSITION. REPLACED THE RIGHT HAND MIX VALVE ASSEMBLY, CHECKS GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1999012200408 19990122 00408 NM 1999 1 22 99UAL900029 1 19990110 A 5610 LATCH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT WINDOW MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 611UA 21872 ABORTED TAKEOFF, CAPT'S WINDOW WAS OPENING, OVER 90 KT. *S/D* CHECKED WINDOW LATCH HANDLE OPERATION AND ALL FOUR LATCH CAMS, LATCH STUDS AND LATCH HOOK PER MM. PERFORMED A FULL OPERATIONAL CHECK PER MM, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1999012200409 19990122 00409 NM 1999 1 22 99UAL900030 1 19990113 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY BROKEN A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 171UA 24322 EEL LIGHT BROKEN AT RIGHT-HAND MIDDLE GALLEY AREA. REPLACED EEL LIGHT AT RIGHT-HAND GALLEY AND REPLACED FEEDER WITH COV ER. 2 L 7 4 4F 4 F RT A20WE E24NE 1999012200410 19990122 00410 NM 1999 1 22 99UAL900033 1 19990113 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 2R INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EEL STRIP AT DOOR 2R IS TORN AND THE CONNECTOR IS RIPPED OFF. ALSO, THE COVER IS MISSING. *S/D* REPAIRED AND CHECKS O K. 2 L 7 4 4F 4 F RT A20WE E24NE 1999012200411 19990122 00411 NM 1999 1 22 99UAL900034 1 19990113 A 2497 245905 WIRE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE COCKPIT OUT OF POSITION A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 153UA 20102 ELECTRICAL ODORS (SMOKE) COMES AND GOES. *S/D* WIRE L639-20 WAS FOUND TO BE BINDING ON THE THROTTLE SEAL PLATE. THIS RESULTED IN A SHORT CIRCUIT. THE CONTROL STAND DIMMER UNIT CIRCUIT BREAKER WOULD NOT RESET. THE BURNED WIRE WAS REPLAC ED. ALSO, THE CONTROL STAND LIGHT DIMMER UNIT WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1999012200412 19990122 00412 NM 1999 1 22 99UAL900036 1 19990117 A 2150 CIRCUIT BREAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT PACK FAN TRIPPED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7289U 21567 RETURNED TO GATE AT ORD WITH SMOKE IN CABIN. *S/D* THE RIGHT PACK OVERHEATED DUE TO NO COOLING ON THE GROUND. RESET C IRCUIT BREAKER AND COOLING FAN CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999012200413 19990122 00413 NM 1999 1 22 99UAL900037 1 19990115 A 3397 362624 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 19-26 FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7276U 21423 FLOOR MOUNTED EEL LIGHTS ARE INOPERATIVE FROM ROW 19 TO 26. *S/D* BAD EEL CABLE. REPLACED EEL CABLE AT 23 ABC. 2 L 7 3 4F 4 F A3WE E2EA 1999012200414 19990122 00414 WP 1999 1 22 ABXA9900021 1 19990113 A 7921 15144051 OIL COOLER DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 851AX 4017 3863 45940 669464 NR 3 ENGINE OIL TEMPERATURE WENT TO 150 DEGREES AFTER TAKEOFF. ENGINE WAS SHUTDOWN. REPLACED NR 3 OIL COOLER, TEMPERAT URE BULB AND REGULATOR. OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1999012200415 19990122 00415 WP 1999 1 22 ABXA9900022 1 19990113 A 3230 CONTROL VALVE DOUG DC9 DC932 3022066 WP LANDING GEAR ICED UP A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 939AX 47201 ON APPROACH, LANDING GEAR HANDLE WAS 'FROZEN' IN THE UP POSITION. ACCOMPLISHED DC9 ABNORMAL PROCEDURES. EMERGENCY GEAR EXTENSION, RESULTED IN UNEVENTFUL LANDING. REMOVED ICE FROM LANDING GEAR CONTROL VALVE CABLES, RESET EMERGENCY EXTENSI ON CONTROLS. CYCLED LANDING GEAR CONTROL VALVE, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999012200416 19990122 00416 NM 1999 1 22 SCNA99009 1 19990113 A 3350 37067001 BATTERIES BOEING 727 7272A1 138407F NM ROW 11 DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, AN AISLE EMERGENCY CEILING LIGHT AT ROW 11 WAS FOUND TO BE INOPERATIVE WHEN TESTED. RE MOVED AND REPLACED BATTERIES, SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999012200417 19990122 00417 NM 1999 1 22 SCNA990010 1 19990112 A 3350 LIGHT BOEING 727 7272A1 138407F NM ROW 3 INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 DURING A LINE MAINTENANCE CHECK, AN EMERGENCY FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT SEAT ROW 3. REPAIRED FLO OR TRACK LIGHT AT SEAT ROW 3, OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999012200418 19990122 00418 NM 1999 1 22 SCNA990011 1 19990114 A 3350 900835A BATTERY BOEING 727 7272J4 1384006 NM R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT ABOVE THE R2 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACE D THE BATTERY M1093, SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1999012200419 19990122 00419 NM 1999 1 22 SCNA99012 1 19990117 A 3350 LIGHT BOEING 727 7272J4 1384006 NM ROW 31 DEF INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, AN INOPERATIVE LIGHT WAS FOUND IN THE FLOOR TRACK LIGHTING AT SEAT 31DEF. REPAIRED EME RGENCY LIGHT AT SEAT 31DEF, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999012200420 19990122 00420 NM 1999 1 22 SCNA99013 1 19990113 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, AN OVERHEAD AISLE EMERGENCY LIGHT WAS FOUND TO BE FLASHING. REMOVED AND REPLACED THE B ATTERY PACK M1094, AISLE EMERGENCY LIGHTS OPERATIONALLY CHECK NORMAL. 2 L 7 3 4F A3WE 1999012200531 19990122 00531 SO 1999 1 22 SWIA971366 1 19990108 A 3230 CONTROL BOX EMB 120 EMB120RT SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 289YV 120289 LANDING GEAR HANDLE IN THE UP POSITION, THE LEFT RED LIGHT REMAINED ILLUMINATED. AFTER RECYCLING THE GEAR THE LIGHT REM AINED AND BUFFETING OCCURRED. REPLACED LANDING GEAR CONTROL BOX IAW MM 32-31-01. OPS CHECKS GOOD MM 32-80-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012200532 19990122 00532 NM 1999 1 22 P5CA9900001 1 19990106 A 5247 SKIN BOEING 747 747122 1384872 NM APU DOOR PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RT APU DOOR PUNCTURED BY WORK STAND DURING LIGHT WIND STORM. REPAIRED IAW SRM 52-40-02. 2 L 7 4 4F A20WE 1999012200533 19990122 00533 NM 1999 1 22 P5CA9900002 1 19990110 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2500 PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 CENTER AFT LOWER FUSELAGE APPROX STA 2500 FOUND HOLE. REPAIRED IAW SRM 53-30-03. 2 L 7 4 4F A20WE 1999012200535 19990122 00535 NM 1999 1 22 P5CA9900004 1 19990102 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RIGHT WING FLYING PANEL CRACKED ON LOWER SIDE IN BOX AREA. REMOVED AND REPLACED FLYING PANEL PER MM 57-22-01. 2 L 7 4 4F A20WE 1999012200537 19990122 00537 WP 1999 1 22 RRXA99003 1 19990113 A 3241 420531B CONTROL BOX DOUG DC8 DC871F 302199D WP ANTISKID SYST FAILED A RRXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 15 8079U 45947 MAIN GEAR SPOILER INOPERATIVE, LT ILLUMINATED EN ROUTE. INSPECTED AND TESTED MAIN GEAR GROUND SPOILERS, OPS CHECKS NORM AL. NO DEFECTS NOTED. REMOVED AND REPLACED ANTI SKID CONTROL BOX, OPS NORMAL. 2 L 7 4 4F RT 4A25 1999012200538 19990122 00538 WP 1999 1 22 RRXA99004 1 19990114 A 3230 ROD END DOUG DC8 DC862 3021970 WP RT MLG FAILED A RRXA O OTHER O OTHER AP APPROACH 1 WP 15 990CF 46068 UPON LANDING GEAR EXTENSION THE RIGHT MAIN LANDING GEAR FREE FELL INTO THE DOWN AND LOCKED POSITION. AFTER LANDING THE GEAR WAS PINNED AS A PRECAUTION, TAXIED TO RAMP. ACFT FERRIED TO KMCN FOR REMOVAL AND REPLACEMENT OF RT MLG BOSS PIN IA W DC-8 SB 32-102 PG 1 THRU 13. INSTALLED RT MLG ACTUATOR ROD END AND ADJUSTED PER DC-8 SB 32-131. PERFORMED GEAR RETRA CTION, ALL SYSTEMS CHECKED NORMAL IAW DC-8 MM 32-30-0. 2 L 7 4 4F 4A25 1999012200539 19990122 00539 WP 1999 1 22 RRXA99005 1 19990115 A 3260 H141302 SWITCH DOUG DC8 DC873F 302199F WP RT MLG FAILED A RRXA O OTHER N FALSE WARNING AP APPROACH 1 WP 15 832AL 46063 ON GEAR EXTENSION RIGHT MAIN GEAR LIGHTS WOULD NOT COME ON. SWAPPED BULBS FROM LEFT WITH NO HELP. REMOVED AND REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 1999012200540 19990122 00540 NM 1999 1 22 VNAA9901011 1 19990113 A 5270 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CARGO DOOR DIRTY A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 424JS 3033 THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A CARGO DOOR WARNING MESSAGE. MAINTENANCE INSPECTED AND CLEANED THE DOOR SE NSORS, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-41-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012200541 19990122 00541 NM 1999 1 22 SWAA990094 1 19990114 A 3040 CONTROLLER BOEING 737 7377H4 NM LT/RT WINDSHIELD INOP A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 709SW 27843 FLIGHT DIVERTED TPA DUE TO KNOWN ICING CONDITIONS IN BWI. COCKPIT L1 AND R2 WINDOW HEAT WERE INOP. REPLACED 2 WINDOW H EAT CONTROLLERS AND REPAIRED WIRING AT R2 TERMINAL. 2 L 7 2 4F RT A16WE 1999012200542 19990122 00542 NM 1999 1 22 SWAA990095 1 19990116 A 3397 WIRE BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SC CHECK, FOUND CENTER AISLE OVERHEAD CENTER CABIN EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE IN CANNON PLUG, OPS CKS OK PER M/M. 2 L 7 2 4F A16WE 1999012200543 19990122 00543 NM 1999 1 22 SWAA990096 1 19990114 A 3350 20131A BATTERY BOEING 737 7372H4 138448C NM LT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SC CHECK, FOUND LT OVERWING EXIT LIGHTS AND LT LWR AFT EXIT LT INOP. REMOVED AND REPLACED LT OVERWING BATTERY PACK, PWR SUPPLY AND OPS CKD OK PER MM. 2 L 7 2 4F A16WE 1999012200544 19990122 00544 NM 1999 1 22 SWAA990097 1 19990117 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM RT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SC CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND CHARGER ASSY PER MM, OP'S CHECK NORMAL. 2 L 7 2 4F A16WE 1999012200545 19990122 00545 NM 1999 1 22 SWAA990098 1 19990115 A 3350 6104781 BATTERY BOEING 737 7372T4 1384492 NM ROW 16 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHTS INOP, FLOOR LIGHTS FROM ROW 16 TO AFT, AND AFT ENTRY AND SERV DOO R LOWER EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999012200546 19990122 00546 NM 1999 1 22 SWAA990099 1 19990115 A 3350 LAMP BOEING 737 7373H4 1384600 NM SERVICE DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SC CHECK, FOUND FWD SERV DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999012200547 19990122 00547 NM 1999 1 22 SWAA990100 1 19990115 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602SW 27953 DURING PREFLIGHT CHECK, FOUND CAPT SIDE EMERGENCY EXIT LIGHT RED LENS LOOSE AND EXPOSING WIRES. REPLACED LENS, RESECURE D WIRING AND OP CHECKED PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012200548 19990122 00548 NM 1999 1 22 SWAA990101 1 19990116 A 3350 417A5900 BATTERY CHARGER BOEING 737 7377H4 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED RON CHECK, FOUND MID CABIN FLOOR LIGHTS INOP. REPLACED CHARGER/BATTERY ASSEMBLY PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012200549 19990122 00549 NM 1999 1 22 SWAA990102 1 19990115 A 2400 D00440 CONNECTOR BOEING 737 7373Q8 1384670 NM COCKPIT CHAFED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED RON CHECK, NOTED ELECTRICAL SMELL IN COCKPIT, FOUND CHAFED AND BURNT WIRING AT CONNECTOR D00440. REPAI RED WIRING PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012200550 19990122 00550 NM 1999 1 22 SWAA990103 1 19990114 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 727-747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED SC CHECK, FOUND A 3 INCH CRACK IN FUSELAGE SKIN LOCATED SEC 46 BETWEEN BS 727E AND 747 AT STRINGER 18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999012200551 19990122 00551 NM 1999 1 22 SWAA990104 1 19990114 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178 AT LBL 29, WL 207. REMOVED AND REPLACED CHORD ANGLE PER BOEING SRM. 2 L 7 2 4F A16WE 1999012200552 19990122 00552 NM 1999 1 22 SWAA990105 1 19990114 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, AT S14R. REPAIRED PER TRAMCO EWO 98-1166. 2 L 7 2 4F A16WE 1999012200553 19990122 00553 NM 1999 1 22 SWAA990106 1 19990114 A 5730 SKIN BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT ACT CUTOUT AREA ON WING NOSE CRACKED APPROX .5 INCH. REPAIRED CR ACK PER SWA RA1-257-0621. 2 L 7 2 4F A16WE 1999012200554 19990122 00554 NM 1999 1 22 SWAA990107 1 19990113 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 807 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE DENTED AND CREASED AT BS 807 BELOW CARGO DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999012200555 19990122 00555 1999 1 22 SWAA990108 4 19990113 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED SC CHECK, FOUND L2 DOOR EMERGENCY SLIDE PRESSURE LOW. REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999012200556 19990122 00556 NM 1999 1 22 SWAA990109 1 19990113 A 5210 SKIN BOEING 737 7372T4 1384492 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED SC CHECK, FOUND AFT ENTRY DOOR CRACKED APPROX 5 INCHES AT FWD LOWER CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999012200557 19990122 00557 NM 1999 1 22 SWAA990110 1 19990113 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 732 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, S23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999012200558 19990122 00558 NM 1999 1 22 SWAA990111 1 19990115 A 3350 6104791 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 605SW 27956 DURING SCHEDULED SC CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK AND CHAR GER ASSY FOR RT OVERWING EMERGENCY LIGHT PER M/M. OP'S CHECK NORMAL. (P/N 61-0479-1) OFF, (P/N 61-0478-9) ON, (S/N WN0 020) ON. 2 L 7 2 4F RT A16WE 1999012200559 19990122 00559 NM 1999 1 22 SWAA990112 1 19990115 A 3350 LIGHT BOEING 737 7373H4 1384600 NM ROW 14 ABC LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 605SW 27956 DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS LOOSE AT ROW 14ABC. RESECURED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999012200560 19990122 00560 NM 1999 1 22 SWAA990113 1 19990116 A 3350 D71702001 BATTERY CHARGER BOEING 737 7377H4 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED CHECK, FOUND CABIN MID FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CHARGER/BATTERY UNIT AND OP C HECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999012200561 19990122 00561 NM 1999 1 22 SWAA990114 1 19990118 A 3350 LAMP BOEING 737 7373H4 1384600 NM ROW 7 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY EGRESS LIGHTS OUT AT ROWS 7 AND 15. RELAMPED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999012200562 19990122 00562 NM 1999 1 22 SWAA990115 1 19990119 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED SC CHECK, RT OVERWING EXIT INTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE, LIGHT LOCATED ABOVE DOOR AND L IGHT FORWARD OF DOOR. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER M/M. 2 L 7 2 4F RT A16WE 1999012200563 19990122 00563 NM 1999 1 22 SWAA990116 1 19990119 A 3350 LAMP BOEING 737 7377H4 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED SC CHECK, FOUND BIN EMERGENCY LIGHT INOP AT ROW 13 ABC. RELAMPED PER M/M, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1999012200564 19990122 00564 NM 1999 1 22 SWAA990117 1 19990115 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE DAMAGED AT BS 360, S14R. REMOVED AND REPLACED SPLICE PER BOEING SRM. 2 L 7 2 4F A16WE 1999012200565 19990122 00565 NM 1999 1 22 SWAA990118 1 19990115 A 5754 SKIN BOEING 737 7372H4 138448C NM NR 5 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D-CHECK, FOUND NR 5 SLAT LOWER T/E SKIN LOWER SURFACE CRACKED AT FASTENER LOCATION 39 INCHES FROM I/B E ND. REPAIRED PER TRAMCO EWO 98-1191. 2 L 7 2 4F A16WE 1999012200566 19990122 00566 NM 1999 1 22 SWAA990119 1 19990115 A 5312 BLKHD STIFFENER BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED 1/4D CHECK, ULTRASONIC CRACK INDICATION UNDER STIFFENER WL 218, RBL 10 FWD SIDE OF BLKHD BS 178. REPAI RED PER BOEING SRM. 2 L 7 2 4F A16WE 1999012200567 19990122 00567 NM 1999 1 22 SWAA990120 1 19990115 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SC CHECK, FOUND A 4 INCH CRACK IN FUSELAGE SKIN 27 INCHES FWD OF OUTFLOW VALVE, BETWEEN STRINGERS 27 AN D 26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999012200568 19990122 00568 NM 1999 1 22 SWAA990121 1 19990115 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED UNDER STRAP AT BS 727D + 6, LBL 17. REPAIRED PER SWA RA 1-353-197 9. 2 L 7 2 4F RT A16WE 1999012200569 19990122 00569 1999 1 22 SWAA990122 2 19990117 A 7314 3404021030 FUEL PUMP BOEING 737 7377H4 NM NR 1 ENGINE FAILED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 711HK 27845 ENG NR 1 FAILED ON TAXI-OUT APPROXIMATELY 3 MIN AFTER ROLL BACK ON ENG NR 2. SOURCE OFF LT NR 1 ILLUMINATED MASTER CAUT ION, LOCKED DOWN ENGINE INDIC AND SAW ENG FAIL ON NR 1. NO OTHER UNUSUAL INDICATIONS. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP AND HMU ASSY PER M/M. ENG RUN OP CK GOOD. 2 L 7 2 4F RT A16WE 1999012200570 19990122 00570 NM 1999 1 22 SWAA990092 1 19990113 A 2150 20405011 ACM BOEING 737 737301 1384611 NM AC COMPT FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 659SW 23229 AT FL350, F/A'S REPORTED STRONG FUMES AFT OF ROW 17 IN MAIN CABIN. TURNED OFF RECIRC FAN AND RIGHT PACK AND CLOSED ISOL ATION VALVE. RETURNED TO BWI. FUMES WEAKENED NOTICEABLY. DEFERRED RIGHT PACK MEL. REPLACED BOTH COALESCER BAGS. OPE RATED LEFT PACK WITH ENGINES AND APU, NO ODOR NOTED. REMOVED AND REPLACED ACM AND AIR SEPARATOR, OP CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999012200571 19990122 00571 NM 1999 1 22 SWAA990093 1 19990113 A 3320 BALLAST BOEING 737 7372H4 138448C NM LAVATORY FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 74SW 22674 AFT F/A REPORTED SMOKE AND ELECTRICAL FUMES IN REAR LAV, AFT LAV MIRROR C/B HAD TRIPPED. ALL AFT LAV CB`S WERE PULLED BY FLIGHT CREW. SMOKE AND FUMES SUBSIDED. SMOKE ALARM IN AFT LAV DOES GO OFF. INSPECTED AFT LAV AREA, FOUND AFT LA V MIRROR BALLAST TO BE SOURCE, DEACTIVATED LAV MIRROR LIGHT, OK TO CONTINUE PER MAL 33-2 SP 1, COLLARED AFT LAV C/B, NO EVIDENCE OF FIRE NOTED. DURING OVERNIGHT MAINTENANCE, R&R AFT LAV MIRROR LIGHT BALLAST PER M/M 2 L 7 2 4F A16WE 1999012200711 19990122 00711 EU 1999 1 22 RAIA990102 1 19990103 A 3244 AH52688 TIRE BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 341TE 950 FLT 7347 - STL - BOTH NOSE TIRES FLAT. MAINTENANCE REPLACED BOTH NOSE WHEEL ASSY. (M) 2 L 7 2 4T RT A56EU 1999012200712 19990122 00712 EU 1999 1 22 RAIA990101 1 19990103 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 435AM 889 FLT 7476 - STL - LEFT ENGINE FIRE LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT ENGINE FIRE LOOP. (M) 2 L 7 2 4T RT A56EU 1999012200754 19990122 00754 WP 1999 1 22 TWAA9901201 1 19990112 A 5712 RIB DOUG DC9 DC983 3022083 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND ON RT WING 2 CRACKS ON RIB LOCATED ONE FT O/B OF NR 8 TRACK. STOP DRILLED CRACKS AND IN STALLED DOUBLER PER SRM 57-01, FIG 3 SHEET 3. 2 L 7 2 4F RT A6WE 1999012200755 19990122 00755 WP 1999 1 22 TWAA9901202 1 19990113 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT RBL 22 IN STA 237. REMOVED APPROX 60 INCHES OF SEAT TRACK S TARTING AT STA 200. INSTALLED NEW TRACK AND SPLICE PER SRM 53-05, FIG 4F. 2 L 7 2 4F RT A6WE 1999012200756 19990122 00756 WP 1999 1 22 TWAA9901203 1 19990114 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1206 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1206, LBL 22 IN. REPLACED CORRODED SECTION OF CHAIR TRA CK PER SRM 53-05, PG 10G. 2 L 7 2 4F RT A6WE 1999012200757 19990122 00757 WP 1999 1 22 TWAA9901204 1 19990114 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 484-502 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORROSION AT STA 484 TO 502 ON RT SIDE. REMOVED CORROSION PER SPM 6-80-0 1. REPAIRED PER SRM 53-01, PG 9. 2 L 7 2 4F RT A6WE 1999012200758 19990122 00758 WP 1999 1 22 TWAA9901205 1 19990115 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 598-617 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE WITH CORROSION BETWEEN STA 598 AND 617 AT CABIN SIDEWALL AREA. CUT OUT D AMAGED AREAS AND INSTALLED DOUBLER PER SRM 53-01, FIG 2. 2 L 7 2 4F RT A6WE 1999012200759 19990122 00759 WP 1999 1 22 TWAA9901206 1 19990115 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 1063 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND I/B EDGE OF MEMBRANE CRACKED BENEATH CHAIR TRACK AT STA 1063, LBL 42 IN. REPAIRED MEMBR ANE PER SRM 53-01, PG 9. 2 L 7 2 4F RT A6WE 1999012200760 19990122 00760 WP 1999 1 22 TWAA9901207 1 19990115 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 400-408 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 400 TO 408, LT SIDE. CUT OUT CORRODED SECTION AND INSTAL LED TWO ROW REPAIR DOUBLER PER SRM 53-01, PG 18. 2 L 7 2 4F RT A6WE 1999012200761 19990122 00761 WP 1999 1 22 TWAA9901208 1 19990115 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 465-475 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED STA 465 TO 475 ON LT SIDE. CUT OUT CORRODED SECTION AND INSTALL ED TWO ROW REPAIR DOUBLER PER SRM 53-01, PG 18. 2 L 7 2 4F RT A6WE 1999012200762 19990122 00762 WP 1999 1 22 TWAA9901209 1 19990115 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 1212-1219 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL FOOT CORRODED BETWEEN STA 1212 AND 1219, RBL 4 IN. INSTALLED NEW FOOT PER S RM 6-70-0 PG 3 AND USED FASTENERS PER SPM 6-30-01 PAGE 1 AND 2. 2 L 7 2 4F RT A6WE 1999012200763 19990122 00763 EU 1999 1 22 MALA976298 1 19990113 A 3060 660713245 DEICE TIMER SAAB SF340 340B 7860101 EU RT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 439XJ 439 AFTER TAKEOFF, THE RIGHT PROP LIGHT ILLUMINATED AFTER SELECTING RIGHT PROP SWITCH TO NORM OR MAX, ILLUMINATED 30 SECONDS AFTER SELECTED ON. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE PROP DEICE TIMER, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999012200764 19990122 00764 EU 1999 1 22 MALA976299 1 19990114 A 2750 HP14161005 CONTROL VALVE SAAB SF340 SF340A 7850100 EU TE FLAPS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 41XJ 041 FLAPS CAUTION LIGHT ON CWP ILLUMINATED DURING CRUISE. RESET BREAKER AND LIGHT WENT OUT. WHEN FLAPS SELECTED DURING APP ROACH, CWP LIGHT CAME ON AND BREAKER POPPED, COMPLETED O DEGREE FLAP LANDING. RETURNED TO DTW. MAINTENANCE REPLACED FL AP CONTROL VALVE AND FLAP CONTROLLER. PERFORMED FUNCTION CHECKS OF FLAPS IAW AMM 27-51-00, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999012200765 19990122 00765 EU 1999 1 22 MALA976300 1 19990116 A 2930 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU HYD IND SYST MALFUNCTIONED A MALA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 15 68XJ 068 IN FLIGHT, CREW NOTICED HYDRAULIC QUANTITY AT 0, MAIN ACCUMULATOR PRESSURE AT O AND INBOARD BRAKES AT 0, NO HYDRAULIC CA UTION LIGHT INDICATIONS. RAN QRH, EMERGENCY HANDLE LOWERED GEAR. MAINTENANCE COULD NOT DUPLICATE. INSPECTED WIRING AN D TERMINALS FROM CIRCUIT BREAKER M-3 TO 36VTS, NO FAULTS NOTED. HYDRAULIC INDICATION OPERATES NORMALLY. REPLACED M-3 C IRCUIT BREAKER. 2 L 7 2 4T RT A52EU 1999012200771 19990122 00771 WP 1999 1 22 IXXA9900002 1 19990116 A 3231 DOOR DOUG DC8 DC863F 302198F WP LT MLG NOT FAIRED A IXXA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 784AL 46135 EN ROUTE, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCH WARNING LIGHT ILLUMINATED, DOOR NOT LATCH REMAINED EXTIN GUSHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE JACKED THE AIRCRAFT AND PERFORMED GEAR SWIN G, WHICH REVEALED THE LEFT MAIN CENTER GEAR DOOR NOT FAIRING PROPERLY. MAINTENANCE ADJUSTED THE CENTER GEAR DOOR IN ACC ORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL. A SUCCESSFUL GEAR SWING, RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 1999012200772 19990122 00772 NE 1999 1 22 CALA9900024 2 19990116 A 7230 STATOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE MIGRATED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN E M T VIBRATION/BUFFET OVER TEMP ENGINE CASE PENETRATION CL CLIMB 1 SW 09 10791 20645 687337 ENGINE NUMBER THREE FAILED ON CLIMB-OUT. CONSTANT VIBRATION, OVER TEMP, ENGINE SHUT DOWN IN FLIGHT. AIRCRAFT RETURNED TO LAS. ENGINE AND DAMAGED COWLING REPLACED AND AIRCRAFT RETURNED TO SERVICE. PRELIMINARY ENGINE INSPECTION REVEALED A FAILURE IN THE HIGH PRESSURE COMPRESSOR SECTION AND AN UNCONTAINED CASE PENETRATION IN THE PRBC AREA CAUSING COWL DAMAGE . SDR TO REMAIN OPEN PENDING ENGINEERING INVESTIGATION AND ENGINE TEARDOWN. TEARDOWN FINDINGS REVEALED C12 STATOR MIGR ATION AS THE PRIMARY CAUSE OF ENGINE FAILURE. 2 L 7 3 4F 4 F A3WE E2EA 1999012200773 19990122 00773 EU 1999 1 22 9900183263 1 19990117 A 5240 FE240004 CYLINDER AIRBUS 320 A320212 EU AFT RT DOOR BINDING A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 363NW 923 WHILE PREPARING TO CATER AIRCRAFT, IT WAS REPORTED THAT THE AFT RIGHT CABIN DOOR WOULD NOT FULLY OPEN AND LATCH. MAINTE NANCE REPLACED THE DOOR DAMPER/ASSIST CYLINDER, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999012200774 19990122 00774 WP 1999 1 22 9900199933 1 19990114 A 3233 ACTUATOR DOUG DC9 DC931 3022065 WP NLG FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 1334U 47280 DURING APPROACH, CREW HEARD A LOUD THUD FROM THE NOSE GEAR AREA. FLAP/RUDDER STOP LIGHT ILLUMINATED, HYDRAULIC PRESSURE WAS BETWEEN 800 TO 1000 PSI, AND GEAR DOOR OPEN LIGHT ILLUMINATED. FLIGHT CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR RETRACT CYLINDER, RIGHT AUXILIARY HYDRAULIC PUMP, RIGHT ENG INE DRIVEN PUMP, AND HYDRAULIC FILTERS. ALSO, REPLACED THE RIGHT MAIN GEAR DOOR AND LEFT MAIN GEAR DOOR SKID PADS DUE T O DAMAGE INCURRED ON LANDING. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999012200775 19990122 00775 WP 1999 1 22 9900209997 1 19990116 A 3233 39132445501 ACTUATOR DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8933E 21264 21264 47142 NOSE LANDING GEAR WOULD NOT EXTEND DURING APPROACH. CREW UTILIZED EMERGENCY GEAR EXTENSION LEVER AND AIRCRAFT LANDED WI THOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR ACTUATING CYLINDER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999012200776 19990122 00776 WP 1999 1 22 9900219975 1 19990117 A 2120 AIR DIST DOUG DC9 DC931 3022065 WP CABIN SMOKE A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 9339 47382 DURING INITIAL CLIMB, FLIGHT ATTENDANT REPORTED SMOKE IN REAR OF AIRCRAFT ACCOMPANIED BY LEFT AFT LAVATORY SMOKE DETECTO R SOUNDING. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND RAN BOTH ENGINE S TO TAKEOFF POWER. NO OIL OR SMOKE WAS NOTED. 2 L 7 2 4F A6WE 1999012200777 19990122 00777 NM 1999 1 22 UPS99228429 1 19990111 A 5311 FRAME BOEING 727 72730C 1384009 NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CRACK AT BS 930 LT FRAME. CRACK REPAIRED IAW DRAWING 65-80107 AND EO B727-5310-2611. 2 L 7 3 4F A3WE 1999012200778 19990122 00778 NM 1999 1 22 UPS99228431 1 19990108 A 5720 WEB BOEING 727 72730C 1384009 NM WS 357 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, LT WING NR 4 LE SLAT AND O/B ACTUATOR WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIRED I AW SRM 57-50-3. 2 L 7 3 4F A3WE 1999012200779 19990122 00779 NM 1999 1 22 UPS99228432 1 19990105 A 5755 SKIN BOEING 727 72730C 1384009 NM NR 9 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, NR 9 SPOILER PANEL LOWER SKIN DELAMINATED. REPAIRED IAW SRM 57-50-6 FIG 5. 2 L 7 3 4F A3WE 1999012200780 19990122 00780 NM 1999 1 22 UPS99228433 1 19990106 A 5400 WEB BOEING 727 72730C 1384009 NM BS 1376 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 LT APPROX. NEW WEB FABRICATED AND IN STALLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1999012200781 19990122 00781 NM 1999 1 22 UPS99228434 1 19990106 A 5400 WEB BOEING 727 72730C 1384009 NM BS 1376 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 RT APPROX. NEW WEB FABRICATED AND IN STALLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1999012200782 19990122 00782 NM 1999 1 22 UPS99228435 1 19990107 A 5320 FITTING BOEING 727 72730C 1384009 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 RT FITTING AT AFT O/B FLANGE ABOVE STRINGER 9. REPAIR C ARRIED OUT IAW B727-5310-3057 AND DRAWING 65C35277. 2 L 7 3 4F A3WE 1999012200783 19990122 00783 NM 1999 1 22 UPS99228436 1 19990107 A 5320 FITTING BOEING 727 72730C 1384009 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 LT FITTING AT FWD OUTBOARD FLANGE ABOVE STRINGER 9. REP AIR CARRIED OUT IAW APPENDIX C OF B727-5310-3057 AND DRAWING 65C3 5277. 2 L 7 3 4F A3WE 1999012200784 19990122 00784 NM 1999 1 22 UPS99228437 1 19990119 A 3350 BATTERY BOEING 727 72725C 138400H NM EXTERIOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, DURING SEGMENT CHECK FOUND ALL EMERGENCY LIGHTS ON EXTERIOR OF A/C INOP. REMOVED AND REPLACED 7 BA TTERIES, OPS CKS GOOD. 2 L 7 3 4F A3WE 1999012200785 19990122 00785 NM 1999 1 22 UPS99228438 1 19990119 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, DURING SEGMENT CHECK FOUND MID CABIN LEFT OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATT ERY PACK, OPS CKS NORMAL. 2 L 7 3 4F A3WE 1999012200786 19990122 00786 NM 1999 1 22 UPS99228439 1 19990120 A 5712 6516250 RIB BOEING 727 72725C 138400H NM WS 519 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, LEFT WING RIB UPPER CHORD CRACKED AT WING STA 519. REPAIRED UPPER CHORD PER SRM 51-40-4. 2 L 7 3 4F A3WE 1999012200787 19990122 00787 NM 1999 1 22 UPS99228441 1 19990119 A 5320 MOP SILL BOEING 727 72725C 138400H NM BS 340-308 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-224-06-1B) MAIN DECK ENTRY MOPSILL BS 340 TO 308 WL 208 LBL 72. REMOVED CORRODED MOP SILL, INSTALLED NEW MOPSILL IAW SRM 51-20-1, 51-30-2, 51-30-8. 2 L 7 3 4F A3WE 1999012200788 19990122 00788 NM 1999 1 22 UPS99228442 1 19990119 A 5347 BAC15201430 SEAT TRACK BOEING 727 72725C 138400H NM BS 620-700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-224-01-1B) ON MAIN DECK SEAT TRACK BS 620 TO 700 RBL 65 WL 208 (TOP AND BOTTOM SURFAC ES, LT FLANGE AND IN WELL AT BS 680). REMOVED CORRODED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-3 0-1, 51-30-2. 2 L 7 3 4F A3WE 1999012200789 19990122 00789 NM 1999 1 22 UPS99228443 1 19990118 A 5347 7178T6511 SEAT TRACK BOEING 727 72725C 138400H NM BS 700-740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-224-01-1B) ON SEAT TRACK STA 700 TO 740, RBL 25. REMOVED CORROSION FOUND TO BE OUT O F LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999012200790 19990122 00790 NM 1999 1 22 UPS99228444 1 19990115 A 5713 BAC15104417178 STRINGER BOEING 727 72725C 138400H NM WS 171.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, LT WING UPPER STRINGER 19 IS CRACKED AT WS 171.5 (VENT STRINGER). REPAIRED SECTION OF STRINGER 19 A T WS 171.5 PER SRM 57-10-4. 2 L 7 3 4F A3WE 1999012200791 19990122 00791 NM 1999 1 22 UPS99228445 1 19990115 A 5347 BAC1520843 TIE DOWN TRACK BOEING 727 72725C 138400H NM BS 520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-113-01.00-01) ON CARGO TIE DOWN TRACK, BS 520 LBL 15 FWD CARGO BAY AT NET ATTACH POIN T. EVALUATED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED TIE DOWN TRACK PER SRM 51-30-02, SRM 57-30-05. 2 L 7 3 4F A3WE 1999012200792 19990122 00792 1999 1 22 UPS99428385 4 19990112 A 2565 ATTACH CHORD BOEING 747 747123 1384873 NM DOOR SLIDE MISRIGGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE-N/A, DURING SHOP VISIT FOUND THE ATTACH CHORD TIED TO THE SHORT LOOP. PLACED THE ATTACHED CHORD THROUGH THE SHORT LOOP, ATTACHING THE ATTACH CHORD TO THE CONE AND REINSTALLING PIN PER BF GOODRICH OVERHAUL MANUAL 25-68-03. 2 L 7 4 4F A20WE 1999012200818 19990122 00818 EU 1999 1 22 QXEA9900092 1 19990116 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 BOTH SIDES OF EMERGENCY EXIT SIGN AT ROW 8 ARE INOPERATIVE. MAINTENANCE REPLACED THE CIRCUIT BOARD, OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F RT A20EU 1999012200819 19990122 00819 EU 1999 1 22 QXEA9900093 1 19990119 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 481US 11230 CENTER CABIN EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE CIRCUIT BOARD, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1999012200820 19990122 00820 EU 1999 1 22 QXEA9900094 1 19990119 A 3397 WIRE GRIMES FOKKER F28 F28MK4000 4990810 EU SEAT 1-2-3-4 BROKEN A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 487US 11238 PASSENGER SEAT MOUNTED EMERGENCY EVACUATION LIGHTING ON SEATS 1, 2, 3, 4 STUCK ON. MAINTENANCE REPAIRED BROKEN WIRES UN DER SEAT, OPERATIONAL CHECK IS NORMAL. 2 L 7 2 4F RT A20EU 1999012200821 19990122 00821 EU 1999 1 22 QXEA9900095 1 19990116 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 BOTH AFT EXTERIOR EVACUATION LIGHTS DO NOT ILLUMINATE WHEN SELECTED ON. MAINTENANCE REPLACED THE POWER SUPPLY UNIT FOR THE SPECIFIC LIGHT ASSEMBLIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1999012200822 19990122 00822 NM 1999 1 22 99FDEA00021 1 19990118 A 5311 65185385 FRAME BOEING 727 72725C 138400H NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 500 - CORROSION (C53-132-02(1)) INDICATIONS BETWEEN LWR FLANGE AND WEB OF BS 870 UPPER CHORD LBL 40-50. REMOVED AND REPLACED UPPER SPAR CHORD BS 870, RBL 70 - LBL 70 PER FEDEX EA 7-5710-43764. 2 L 7 3 4F A3WE 1999012200823 19990122 00823 NM 1999 1 22 99FDEA00022 1 19990120 A 2750 MECHANISM BOEING 727 72722C 138400F NM TE FLAPS ICED UP A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 105FE 19194 DURING FLAP RETRACT ON T/O, FLAPS DID NOT MOVE TO SELECT POSITION. INSPECTED FLAPS, NO FAULTS FOUND. SUSPECT PROBLEM D UE TO COLD WEATHER ICING CONDITION. HEAT LT AND RT WHEEL WELLS. CYCLED FLAPS FOUND TO BE WITHIN LIMITS AS PER M/M 27-5 2-12 & 27-52-1. 2 L 7 3 4F A3WE 1999012200824 19990122 00824 WP 1999 1 22 MWEA99038 1 19990115 A 5230 3914025502 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FOUND CRACK ON AFT CARGO DOOR BEAM END FITTING. MTC FABRICATED AND INSTALLED NEW END FITTING. 2 L 7 2 4F A6WE 1999012200825 19990122 00825 WP 1999 1 22 MWEA99039 1 19990118 A 5330 591142379 SKIN DOUG DC9 DC932 3022066 WP BS 890-897 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FUSELAGE SKIN DENTED AT STATION 890 TO 897 BETWEEN LONGERON 24 AND 25 LEFT. MTC FABRICATED AND INSTALLED DOUBLER REPAIR . 2 L 7 2 4F A6WE 1999012400001 19990124 00001 WP 1999 1 24 AT9900002 1 19990105 A 2560 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR DISENGAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 GALLEY DOOR SLIDE FALL OFF DOOR. REINSTALLED GALLEY R-1DOOR SLIDE PER 25-61 STANDARD PRACTICES. 2 L 7 2 4F A6WE 1999012900001 19990129 00001 NM 1999 1 29 TWAA9901301 1 19990120 A 3397 WIRE BOEING 767 7673Y0 NM ROW 5 DISCONNECTED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 TWO FLOOR EGRESS LIGHTS WERE INOPERATIVE AT SEAT ROW 5, RT SIDE OF CABIN. FOUND WIRES DISCONNECTED, AND RECONNECTED SAM E. CHECK-C 12-5-98 LAX. 2 L 7 2 4F RT A1NM 1999012900002 19990129 00002 NM 1999 1 29 TWAA9901302 1 19990120 A 3350 1317 LAMP BOEING 767 7673Y0 NM ROW 3 WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 FOUND INOPERATIVE EMERGENCY LIGHT IN CEILING ABOVE SEAT ROW 3 ON RT SIDE OF CABIN. REPLACED LAMP. CHECK-C 12-5-98 LAX. 2 L 7 2 4F RT A1NM 1999012900003 19990129 00003 WP 1999 1 29 TWAA9901303 1 19990120 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 22 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 940AS 49825 FOUND OVERWING EMERGENCY EXIT SIGNS INOPERATIVE AT ROW 22 ON BOTH LT AND RT SIDES OF CABIN. REPLACED BATTERY PACK. CHE CK-C 6-28-98 MCI. 2 L 7 2 4F A6WE 1999012900004 19990129 00004 WP 1999 1 29 TWAA9901304 1 19990120 A 3350 CM2232 LAMP DOUG DC9 DC982 3022082 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 940AS 49825 FOUND THE EXTERIOR EMERGENCY EXIT SIGNS INOPERATIVE ON LT AND RT SIDES OF AIRCRAFT. RELAMPED BOTH SIGNS. CHECK-C 6-28- 98 MCI. 2 L 7 2 4F A6WE 1999012900005 19990129 00005 WP 1999 1 29 TWAA9901305 1 19990116 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 199 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND HOLE IN MEMBRANE AT STA 199, APPROXIMATELY LBL 16 INCHES. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01, PAGE 18 FIG 4. 2 L 7 2 4F RT A6WE 1999012900006 19990129 00006 WP 1999 1 29 TWAA9901306 1 19990117 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND SIDEWALL FLOOR MEMBRANE WITH CORROSION BETWEEN LONGERON 655 AND 658. CUT OUT CORRODED A REA, INSTALLED 3 INCH BY 16 INCH 2024T3 0.032 DOUBLER, PER SRM 53-01, PG 18 FIG 4. 2 L 7 2 4F RT A6WE 1999012900007 19990129 00007 WP 1999 1 29 TWAA9901307 1 19990117 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 522-541 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 522 TO 541, RT SIDE. REMOVED CORROSION PER STD PROCESSES MANUAL 6-80-1, PARA B PG 1. REPAIRED PER SRM 53-01, PG 18. 2 L 7 2 4F RT A6WE 1999012900008 19990129 00008 WP 1999 1 29 TWAA9901308 1 19990119 A 5720 DOUBLER DOUG DC9 DC915 3022036 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 490SA 45798 DURING CHECK-C MAINT, FOUND ONE INCH CRACK IN LT WING IN UPPER WING FUEL TANK ACCESS PLATE DOUBLER NR 1307. STOP DRILLE D CRACK AND INSTALLED REPAIR PER SRM 57-03 AND SRM 51-60-0. 2 L 7 2 4F A6WE 1999012900009 19990129 00009 WP 1999 1 29 TWAA9901309 1 19990117 A 5210 STRUCTURE DOUG DC9 DC983 3022083 WP PAX DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND IN FWD LT CABIN DOOR WHERE SEAL CONTROL SHAFT PASSES THRU INTERNAL STRUCTURE TO CONNECT WITH SEAL ACTUATING LINK, STRUCTURE HAS CORROSION APPROXIMATELY 17 INCHES FROM LE OF DOOR AND 4 INCHES FROM BOTTOM OF DO OR. INSTALLED NEW SHAFT SUPPORT PER SRM 51-01 PG 01. 2 L 7 2 4F RT A6WE 1999012900010 19990129 00010 EU 1999 1 29 AWXA9900019 1 19990119 A 5347 R53070089202 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 254 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 627AW 66 DURING ROUTINE MAINTENANCE CHECK, FOUND LT AND RT FLOOR TRACK DUMMY RAILS AT STATION Y254, FRAMES FR16 TO FR20 WERE CORR ODED BEYOND SRM LIMITS. DUMMY RAILS REPLACED PER SRM 51-54-00. 2 L 7 2 4F RT A28NM 1999012900011 19990129 00011 EU 1999 1 29 AWXA9900020 1 19990116 A 2611 PAI283000 SMOKE DETECTOR AIRBUS 320 A320231 3930325 EU LAVATORY DAMAGED A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 636AW 29863 098 ECAM SMOKE LAVATORY DET FAULT, SUSPECT LAV (AFT LEFT). A/C RETURNED TO LAS VEGAS. DETECTOR TAMPERED WITH BY PASSENGER. PLACED ON MEL 26-17-01, LOCKED OUT LAV. REMOVED AND REPLACED DETECTOR IN LAV D PER AMM CHAP 26, SYS CKS OK THROUGH CF DS. 2 L 7 2 4F RT A28NM 1999012900012 19990129 00012 NM 1999 1 29 AWXA9900021 1 19990113 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 664 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND TRANSVERSE FLOORBEAM BL 0 CRACKED AT STA 664. REPAIRED TRANSVERSE FLOORBEAM BL 0PER B737-57-1210. CUT OUT DAMAGED WEB, INSTALLED FABRICATED AND SB KIT PARTS PER SB 737-57-1210. 2 L 7 2 4F RT A16WE 1999012900013 19990129 00013 NM 1999 1 29 AWXA9900022 1 19990120 A 2424 948F4582 GCU BOEING 737 7373G7 1384595 NM NR 1 FAILED A AWXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 158AW 26265 23780 ON TAXI OUT, SMOKE BELLOWED FROM THE F/O C/B, THE NR 1 GEN FELL OFF LINE. F/O PULLED THE C/B (GCU-1) WHERE THE SMOKE WA S COMING FROM, THEN SMOKE STOPPED. REMOVED AND REPLACED NR 1 GCU AND NR 1 GENERATOR BREAKER, RAN ENG OPS CK GOOD PER BM M 24-21-41. 2 L 7 2 4F RT A16WE 1999012900014 19990129 00014 NM 1999 1 29 AWXA9900023 1 19990119 A 2840 693733588 SWITCH BOEING 737 7373G7 1384595 NM FUEL PRESSURE MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 151AW 23219 JUST AFTER TAKEOFF, ALL FUEL LOW PRESSURE LIGHTS ILLUMINATED WITH MASTER CAUTION LIGHT. EXECUTED AIR TURNBACK. RAN ENG INES TO TAKEOFF POWER, BITE TEST, AND DRIP STICK PER MM 28-22-00 OK FOR FLIGHT AS PRECAUTION IN PHX. REMOVED AND REPLAC ED FWD AND AFT LOW PRESSURE SWITCHES FOR FUEL TANK NR 2 AND FUEL HEAT MODULE. 2 L 7 2 4F RT A16WE 1999012900015 19990129 00015 WP 1999 1 29 CALA9900025 1 19990119 A 5240 991158221 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 FORWARD SERVICE DOOR HORIZONTAL BEAM HAS 4 CRACKS IN RADIUS WHERE LOWER HINGE ATTACHES. REPLACED HORIZONTAL BEAM PER SR M 51-30-2. 2 L 7 2 4F A6WE 1999012900016 19990129 00016 WP 1999 1 29 CALA9900026 1 19990119 A 5330 59114023 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 SMALL CUTOUT FOR MAIN CABIN DOOR HOLD OPEN HOOK FUSELAGE SKIN PULLED AWAY, 2 X 1 X .125. INSTALLED DOUBLERS PER SRM 53- 04. 2 L 7 2 4F A6WE 1999012900017 19990129 00017 WP 1999 1 29 CALA9900027 1 19990119 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 198 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 FWD WATER DRAIN MAST MOUNT STRUCTURE HAS CORROSION INSIDE E & E COMPARTMENT STA 198 RIGHT OF CENTER. REMOVED AND REPLAC ED INTERCOSTAL, DOUBLER AND DRAIN MAST PER SRM 51-30-2. 2 L 7 2 4F A6WE 1999012900018 19990129 00018 WP 1999 1 29 CALA9900028 1 19990119 A 5347 593056671 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1136 - 1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 CORROSION ON FLOOR BOARD SUPPORT FLANGE LEFT CENTER SEAT TRACK, SEVERAL AREAS STA 1136 TO 1231. REMOVED AND REPLACED SE AT TRACK PER SRM 51-30-0 FROM STA 1032 TO 1245. 2 L 7 2 4F A6WE 1999012900019 19990129 00019 WP 1999 1 29 CALA9900029 1 19990119 A 5330 5924802 SKIN DOUG DC9 DC982 3022082 WP BS 237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 FUSELAGE SKIN AT STA 237 HAS A DEEP DENT. INSTALLED NEW SECTION OF SKIN PER EC/RA 5330-02445. 2 L 7 2 4F A6WE 1999012900020 19990129 00020 WP 1999 1 29 CALA9900030 1 19990119 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1136 - 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 CORROSION ON LEFT INBOARD SEAT TRACK STA 1136 TO 1155. REPAIRED PER SRM 53-05. 2 L 7 2 4F A6WE 1999012900021 19990129 00021 WP 1999 1 29 CALA9900031 1 19990119 A 5330 59354341 SKIN DOUG DC9 DC982 3022082 WP BS 180 - 313 LIGHTNING STRIKE A CALA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 72822 49482 SEVERAL SMALL LIGHTNING STRIKES, LONG 24 TO 26 LT STA 218 TO 313. BLENDED OUT LIGHTNING STRIKE DAMAGE OR PLUGGED AS NEC ESSARY PER SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1999012900022 19990129 00022 WP 1999 1 29 CALA9900032 1 19990120 A 5240 991158221N BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 FORWARD SERVICE DOOR NUMBER 4 BEAM CRACKED AT AFT SIDE RADIUS 3/4. INSTALLED NEW BEAM PER SRM 51-30. 2 L 7 2 4F A6WE 1999012900023 19990129 00023 WP 1999 1 29 CALA9900033 1 19990120 A 5330 59354341 SKIN DOUG DC9 DC982 3022082 WP BS 294 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 DENT AT STA 294 LEFT BETWEEN LONG 22 AND 23. COLD FORMED DENT BACK TO CONTOUR. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04. 2 L 7 2 4F A6WE 1999012900024 19990129 00024 WP 1999 1 29 CALA9900034 1 19990120 A 5743 BEAM DOUG DC10 DC1030 3023501 WP LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13086 46917 LEFT MAIN LANDING GEAR SUPPORT BEAM RETRACT CYLINDER SUPPORT FRAME ATTACHMENT BOLT HOLES CORRODED. HOLES REWORKED AND B USHED PER EC/RA 5743-01012. 2 L 7 3 4F A22WE 1999012900025 19990129 00025 WP 1999 1 29 CALA9900035 1 19990120 A 5743 BEAM DOUG DC10 DC1030 3023501 WP RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13086 46917 RIGHT MAIN LANDING GEAR SUPPORT FRAME ATTACHMENT BOLT HOLES CORRODED. HOLES REWORKED AND BUSHED PER EC/RA 5473-01012. 2 L 7 3 4F A22WE 1999012900026 19990129 00026 WP 1999 1 29 CALA9900036 1 19990120 A 5320 FRAME DOUG DC9 DC932 3022066 WP AIRSTAIR DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 AIRSTAIR DOOR CUTOUT LEFT SUPPORT FRAME CRACKED .75 BELOW AIRSTAIR OPEN/CLOSE FORWARD BRACKET ATTACH LEG, APPROX FS 1090 . CUT DAMAGED AREA, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER PER SRM 53-01. 2 L 7 2 4F A6WE 1999012900027 19990129 00027 WP 1999 1 29 CALA9900037 1 19990120 A 5712 99193315 RIB DOUG DC9 DC932 3022066 WP WS 545 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14524 47539 RIB CRACKED THROUGH FASTENER HOLE INSIDE LEFT WING L/E XRS545 (.5) 12 INCES OUTSIDE OF NR 5 SLAT CENTER TRACK. REMOVED AND INSTALLED NEW RIB PER SRM 51-30-2. 2 L 7 2 4F A6WE 1999012900028 19990129 00028 WP 1999 1 29 CALA9900038 1 19990121 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 HEAVY CORROSION ON LOWER FORWARD FLANGE AND FWD FACE OF BELT FRAME AT STA 1322 L28 TO R28. REPAIRED PER SRM 53-03. 2 L 7 2 4F A6WE 1999012900029 19990129 00029 NE 1999 1 29 COMA9910015 2 19990118 A 7532 VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE MALFUNCTIONED A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 244CA 120217 AIR CONDITIONING SYSTEM EMITS SMOKE. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RIGHT HAND ENGINE P2.5/3 SWITCHING VALVE FOR TROUBLESHOOTING. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012900030 19990129 00030 SO 1999 1 29 COMA9910016 1 19990120 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 256CA 3848 120245 EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4T RT A31SO 1999012900031 19990129 00031 EA 1999 1 29 COMA9960036 1 19990118 A 2760 CONTROL CNDAIR CL600 CL6002B19 EA SPOILER OUT OF POSITION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK W INADEQUATE Q C TO TAKEOFF 1 SO 01 920CA 7022 CON FIG SPOILERS WARNING DURING TAKEOFF. FOUND SPOILER CONTROL NOT STOWED. OPERATIONAL CHECK OF SYSTEM NORMAL. 2 L 7 2 4F RT A21EA 1999012900032 19990129 00032 NM 1999 1 29 UPS99228446 1 19990107 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, FWD CARGO HOLD ON INSPECTION OF CARGO DOOR LATCH SUPPORT FITTINGS SHEAR TIE ON FRAME AT BS 520 FOUND CRACKED. REPAIRED IAW SRM 51-40-02, 51-40-03, FIG 1. 2 L 7 3 4F A3WE 1999012900033 19990129 00033 NM 1999 1 29 UPS99228447 1 19990108 A 7830 SKIN BOEING 727 72722C 138400F NM NR 1 ENG TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, ENGINE NR 1 THRUST REVERSER LOWER DOOR INNER SKIN CRACKED (2 LOCATIONS). CRACKS STOP DRILLED IAW SRM 78-30-01. 2 L 7 3 4F A3WE 1999012900034 19990129 00034 NM 1999 1 29 UPS99228448 1 19990111 A 5311 FRAME BOEING 727 72722C 138400F NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, CRACK AT BS 930 LT FRAME CRACK. REPAIRED IAW DRAWING 65-80107 AND EO B727-5310-2611. 2 L 7 3 4F A3WE 1999012900035 19990129 00035 NM 1999 1 29 UPS99228449 1 19990108 A 5754 WEB BOEING 727 72722C 138400F NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, LT WING NR 4 LE SLAT AND ACTUATOR WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIRED IAW S RM 57-50-3. 2 L 7 3 4F A3WE 1999012900036 19990129 00036 NM 1999 1 29 UPS99228450 1 19990105 A 5755 SKIN BOEING 727 72722C 138400F NM NR 9 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, NR 9 SPOILER PANEL LOWER SKIN DELAMINATED. REPAIRED IAW SRM 57-50-6 FIG 5. 2 L 7 3 4F A3WE 1999012900037 19990129 00037 NM 1999 1 29 UPS99228451 1 19990106 A 5400 WEB BOEING 727 72722C 138400F NM BS 1376 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE SUSPECT CRACK ON WEB AT BS 1376 LT APPROX. NEW WEB FABRICATED AND IN STALLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1999012900038 19990129 00038 NM 1999 1 29 UPS99228452 1 19990106 A 5400 WEB BOEING 727 72722C 138400F NM BS 1376 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, CENTER ENGINE SUPPORT STRUCTURE, SUSPECT CRACK ON WEB AT BS 1376 RT APPROX. NEW WEB FABRICATED AND I NSTALLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1999012900039 19990129 00039 NM 1999 1 29 UPS99228453 1 19990107 A 5320 FITTING BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 RT FITTING AT AFT OUTBOARD FLANGE ABOVE STRINGER 9. REP AIR CARRRIED OUT IAW B727-5310-3057 AND DRAWING 65C35277. 2 L 7 3 4F A3WE 1999012900040 19990129 00040 NM 1999 1 29 UPS99228454 1 19990107 A 5320 FITTING BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE-C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 LT FITTING AT FWD OUTBOARD FLANGE ABOVE STRINGER 9. REP AIR CARREID OUT IAW APPENDIX C OF B727-5310-3057 AND DRAWING 65C35277. 2 L 7 3 4F A3WE 1999012900041 19990129 00041 NM 1999 1 29 QXEA9900096 1 19990120 A 5210 85210263101 GAS SPRING DHAV DHC8 DHC8102 2809003 NM CABIN DOOR MALFUNCTION A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 829PH 304 MAIN CABIN DOOR HARD TO OPEN AND CLOSE. MAINTENANCE REPLACED THE MAIN CABIN DOOR GAS SPRINGS, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999012900042 19990129 00042 NM 1999 1 29 QXEA9900097 1 19990118 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 356PH 1895 16 502 EMERGENCY LIGHT AT ROW 3 INOP. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 3, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999012900043 19990129 00043 NM 1999 1 29 QXEA9900098 1 19990119 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 823PH 11410 110 CREW EMERGENCY ESCAPE LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY ESCAPE LIGHT, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999012900044 19990129 00044 NM 1999 1 29 QXEA9900099 1 19990118 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 825PH 15593 213 COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE. MAINTENANCE REPLACED THE OVERHEAD LIGHT, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999012900045 19990129 00045 NM 1999 1 29 99FDEA00023 1 19990121 A 2130 SEAL BOEING 727 727227 1384078 NM CABIN PRESSURE LEAKING A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 478FE 21395 99-0017 - A/C WOULD NOT PRESSURIZE, NO LIGHTS ON PRESSURIZATION PANEL, LOUD NOISE IN BACK (SEAL). PRESSURIZED A/C PER J ET RUN HANDBK 7-41 THROUGH 7-49 WITH APU ON GROUND PASSED TEST. 2 L 7 3 4F A3WE 1999012900046 19990129 00046 NM 1999 1 29 VNAA9901012 1 19990111 A 5240 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE SERVICE DOOR FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 328LS 3025 THE AIRCRAFT RETURNED TO THE FIELD DUE TO THE COMMUNICATION DOOR FAILING TO SEAL. MAINTENANCE INSPECTED AND RE-SEALED T HE COMMUNICATION DOOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 51-22-00. OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900047 19990129 00047 NM 1999 1 29 VNAA9901014 1 19990114 A 7603 001A761A1021002 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 424JS 3033 THE LEFT HAND POWER LEVER FAILED TO ADVANCE ABOVE FLIGHT IDLE WHEN SELECTED DURING THE TAKEOFF ROLL. THE TAKEOFF WAS AB ORTED AND THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND LUBED THE LEFT HAND POWER LEVER RELEA SE TRIGGERS, OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900048 19990129 00048 NM 1999 1 29 VNAA9901015 1 19990116 A 3234 7178011 CONTROL HANDLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LANDING GEAR FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 328LS 90915 3025 DURING THE APPROACH, THE RIGHT HAND MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. AN EMERGENCY WAS DECLARED AND T HE AIRCRAFT LANDED SAFELY IN PIT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL HANDLE, IN ACCORDANCE WIT H DORNIER MANTENANCE MANUAL 32-31-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900049 19990129 00049 NM 1999 1 29 VNAA9901017 1 19990118 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 432JS 78905 2136 3045 DURING THE PREFLIGHT INSPECTION, EMERGENCY LIGHTS AT ROWS THREE AND SIX WERE NOTED TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL C HECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900050 19990129 00050 NM 1999 1 29 VNAA9901019 1 19990120 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 4-6 DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 328JS 74319 661 3030 THE EMERGENCY LIGHTS AT ROWS FOUR THROUGH SIX WERE NOTED TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERA TIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900068 19990129 00068 EU 1999 1 29 99ZZZX418 1 19990106 A 3260 INDICATOR STBROS SD3 SD330 8100602 EU COCKPIT INOPERABLE A DATA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 13 2629P SH3079 THE RIGHT GEAR DOWN INDICATION LIGHT WAS INOPERABLE SO THE CAPTAIN DECLARED AN EMERGENCY INTO SDF AND LANDED WITHOUT INC IDENCE. THE RIGHT GEAR DOWN INDICATION LIGHT WAS MEL'ED AND THE AIRCRAFT WAS FLOWN TO BKW. THE MECHANIC CLEANED AND LU BED THE DOWNLOCK SWITCH IAW SD3-30 MM. MEL CLEARED AND OPS CHECK GOOD. 2 H 7 2 4T A41EU 1999012900100 19990129 00100 NM 1999 1 29 TWAA9901401 1 19990115 A 5754 SKIN BOEING 767 767205 1385121 NM NR 6 LE SLAT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 THE NR 6 LE SLAT PANEL TRAILING EDGE AT INBD TOP END HAD REPAIR BLOWN OFF. INSTALLED HOT BOND REPAIR AS REQUIRED BY SRM 51-70-10, PAGE 26 FIG 10. CHECK-C 10-28-98 LAX. 2 L 7 2 4F RT A1NM 1999012900101 19990129 00101 NM 1999 1 29 TWAA9901402 1 19990122 A 5754 SEAL BOEING 767 767231 1385131 NM NR 2 LE SLAT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DURING CHECK-C, FOUND THE INBD END OF THE NR 2 LE SLAT, LOWER AFT SEAL, REPAIR DELAMINATING ON UPPER SIDE. BONDED SURFA CES WITH 150 DEGREE CURE RESIN PER SRM 51-70-06, FIG 11. 2 L 7 2 4F RT A1NM 1999012900102 19990129 00102 NM 1999 1 29 SPAA9900001 1 19990115 A 3350 110049 BATTERY CHARGER BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING PREFLIGHT CHECK, THE LOWER EMERGENCY ESCAPE PATH LIGHTS AT BOTH OVERWING EXIT LOCATIONS WERE FOUND INOPERATIVE. B OTH BATTERY CHARGERS, FORWARD AND AFT, ASSOCIATED WITH THESE LIGHTS WERE REPLACED. SUBSEQUENT SYSTEM TEST WAS SATISFACT ORY PER BMM 33-51-11. 2 L 7 2 4F A16WE 1999012900103 19990129 00103 NM 1999 1 29 AT9900033 1 19990119 A 3397 WIRE BOEING 737 7372T4 1384492 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 467AT 22055 TWO EMERGENCY PATH LIGHTS INOPERATIVE. FOUND BROKEN WIRE. SPLICED WIRE AND REINSTALLED IAW DC-9 MM 33-21-27 AND OPS CH ECKED GOOD. 2 L 7 2 4F A16WE 1999012900104 19990129 00104 WP 1999 1 29 VJ9900032 1 19990117 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 10-14 BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 866AT 47168 PATH LIGHTING DOES NOT ILLUMINATE FROM ROW 10 TO ROW 14. REPAIRED BROKEN WIRE AT ROW 14 PER DC-9 MM 33-50. 2 L 7 2 4F A6WE 1999012900105 19990129 00105 EA 1999 1 29 JBXA9900065 1 19990124 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 572ML 7224 AFTER TAKEOFF HAD PASSENGER DOOR INDICATION WARNING IN FLIGHT. AIRCRAFT RETURNED TO RDU. OPERATIONAL CHECK GOOD OF PAS SENGER DOOR IAW AMM 52-11-00. NO FAULTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 1999012900106 19990129 00106 WP 1999 1 29 CALA9900039 1 19990120 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 FOUND INTERCOSTAL ANGLE FITTING UNDER UPPER FWD DOOR STOP CRACKED .5 INCH. REMOVED ANGLE, FABRICATED, TREATED, PRIMED A ND INSTALLED PER SRM 51-10-2, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999012900107 19990129 00107 NM 1999 1 29 CALA9900040 1 19990122 A 5347 141N51311 SEAT TRACK BOEING 757 757224 1384958 NM BS 377-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 TWO SEAT TRACKS CORRODED AT POSITION RBL 45.5 AND 24.75 BETWEEN BS 377.7 AND 440. REPLACED SEAT TRACKS. 2 L 7 2 4F RT A2NM 1999012900108 19990129 00108 NM 1999 1 29 CALA9900041 1 19990122 A 5320 143N56672 THRESHOLD BOEING 757 757224 1384958 NM CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 FORWARD HOLD THRESHOLD CORRODED THROUGH ATTACHMENT ANGLE PLATE. REPLACED THRESHOLD. 2 L 7 2 4F RT A2NM 1999012900109 19990129 00109 NM 1999 1 29 CALA9900042 1 19990107 A 5230 DOOR BOEING 727 727232 1384082 NM CARGO COMPT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 BOTTOM EDGE OF C2 DOOR AFT 25 HOLES AND GOUGES IN LIP. REMOVED AND REPLACED NEW BOTTOM EDGE PER SRM 51-10-1 AND 51-30-2 . 2 L 7 3 4F A3WE 1999012900110 19990129 00110 NM 1999 1 29 CALA9900043 1 19990108 A 5347 BAC152792 SEAT TRACK BOEING 727 727232 1384082 NM BS 1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 CORROSION AT BOTTOM OF SEAT TRACK STA 1090 RBL 47. REMOVED AND REPLACED CORRODED SEAT TRACK FROM STA 1090 TO STA 1130 R BL 47 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999012900111 19990129 00111 NM 1999 1 29 CALA9900044 1 19990108 A 2560 MEGAPHONE BOEING 727 727232 1384082 NM CABIN INOP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 AFT MEGAPHONE INOPERATIVE (NO SOUND). CLEANED CONTACTS AND OPS CHECK NORMAL PER MM 25-62-00. 2 L 7 3 4F A3WE 1999012900112 19990129 00112 NM 1999 1 29 CALA9900045 1 19990108 A 3350 90052 BATTERY PACK BOEING 727 727232 1384082 NM PAX DOORWAY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33785 20640 AFT ENTRY OVERHEAD EMERGENCY LIGHT INOPERATIVE WHEN TESTED. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK NORMAL PER MM 33-60-01. 2 L 7 3 4F A3WE 1999012900113 19990129 00113 NM 1999 1 29 CALA9900046 1 19990108 A 5752 652172642 TAB BOEING 727 727232 1384082 NM RT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 RIGHT WING OUTBOARD AILERON TAB IS DELAMINATED AT BOTH T/E'S (10). REMOVED AND REPLACED RIGHT WING OUTBOARD AILERON TAB PER MM 27-10-41. 2 L 7 3 4F A3WE 1999012900114 19990129 00114 NM 1999 1 29 CALA9900047 1 19990108 A 5512 SKIN BOEING 727 727232 1384082 NM RT HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 RIGHT HORIZONTAL STAB HAS BULGE IN UPPER SKIN AT AFT SPAR APPROX 12 INCHES FROM OUTBOARD END AT FIRST RIB FROM END. CUT OUT DAMAGE AND ACCOMPLISHED REPAIR PER 55-10-5 AND 12-30-8 MM. 2 L 7 3 4F A3WE 1999012900115 19990129 00115 NM 1999 1 29 CALA9900048 1 19990108 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 28-30 DISCONNECTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33785 20640 ESCAPE PATH WIRE DAMAGED AT SEAT 24 TO 30. DISCONNECTED OUT OF TRACKS. REPAIRED AND CONNECTED WIRE AT ROWS 28 TO 30. O PS CHECK GOOD PER MM 33-51-01. 2 L 7 3 4F A3WE 1999012900116 19990129 00116 NM 1999 1 29 CALA9900049 1 19990108 A 3397 WIRE BOEING 727 727232 1384082 NM EMERGENCY EXIT DISCONNECTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33785 20640 ESCAPE PATH LIGHTS AT MID CABIN OVERWING EXITS ARE LOOSE AND DISCONNECTED. REPAIRED AND SECURED PATH WIRING. OPS CHECK PER MM 33-51-0. 2 L 7 3 4F A3WE 1999012900117 19990129 00117 NM 1999 1 29 CALA9900050 1 19990109 A 2782 MOUNT BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 LEFT WING NR 2 KRUEGER FLAP ACTUATOR INBOARD MOUNT CRACKED AT TOP (1). REMOVED, FABRICATED AND INSTALLED BRACKET PER SR M 51-10-1. 2 L 7 3 4F A3WE 1999012900118 19990129 00118 NM 1999 1 29 CALA9900051 1 19990109 A 5720 ANGLE BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 A 2.875 PIECE OF ANGLE BROKEN OFF AT TOP OF LEFT WING JUST FWD OF O/B AILERON L/E AT I/B END. REMOVED FASTENERS AND DAM AGED T ANGLE. FABRICATED AND INSTALLED NEW T ANGLE PER SRM 51-30-2 AND 57-10-7. 2 L 7 3 4F A3WE 1999012900119 19990129 00119 NM 1999 1 29 CALA9900052 1 19990109 A 5720 TIP BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 RIGHT WING TIP AT LOWER SURFACE AFT OF MOUNT SCREWS HAS A 1 INCH LONG CRACK. STOP DRILLED CRACK, FABRICATED AND INSTALL ED DOUBLER PER SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999012900120 19990129 00120 NM 1999 1 29 CALA9900053 1 19990109 A 5230 CHANNEL BOEING 727 727232 1384082 NM C2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INBOARD SIDE OF C2 DOOR UPPER AFT CORNER METAL CHANNEL IS CRACKED (1) AT SEAL DEPRESSOR AREA. REMOVED CRACKED SECTION, FABRICATED, TREATED, PRIMED INSTALLED PER SRM 51-30-2, 51-10-6, AND 51-20-1. 2 L 7 3 4F A3WE 1999012900121 19990129 00121 NM 1999 1 29 CALA9900054 1 19990109 A 5720 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 RIGHT WING I/B OF I/B AILERON ANGLE IS CRACKED (.5) LOCATED ABOVE JACK SCREW AREA. REMOVED FASTENERS, FABRICATED AND IN STALLED NEW BRACKET PER SRM 51-30-2 AND 57-20-4. 2 L 7 3 4F A3WE 1999012900122 19990129 00122 NM 1999 1 29 CALA9900055 1 19990109 A 5720 TIP BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 LEFT WING LOWER WING TIP SURFACE HAS .5 INCH LONG HOLE WORK THROUGH AND .5625 INCH CRACK. CUT OUT DAMAGE, FABRICATED AN D INSTALLED REPAIR DOUBLER AND FILLER PER SRM 57-30-2. 2 L 7 3 4F A3WE 1999012900123 19990129 00123 NM 1999 1 29 CALA9900056 1 19990109 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 LEFT WING NR 1 L/E KRUEGER FLAP ACTUATOR I/B MOUNT BRACKET IS CRACKED .375 INCH. REMOVED BRACKET, FABRICATED AND INSTAL LED NEW BRACKET PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999012900124 19990129 00124 NM 1999 1 29 CALA9900057 1 19990109 A 5754 69179002 BRACKET BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 BRACKET HAS .3125 INCH CRACK AT INBOARD SIDE AT LEFT WING NR 1 SLAT WHERE INBOARD TRACK MOUNTS TO LOWER SKIN. REMOVED A ND REPLACED CRACKED BRACKET PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999012900125 19990129 00125 NM 1999 1 29 CALA9900058 1 19990109 A 5712 66147351 RIB BOEING 727 727232 1384082 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 TWO RIBS ATTACHED TO NR 7 SPOILER ACTUATOR CASTING ARE CRACKED (1). REPLACED RIBS PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1999012900126 19990129 00126 NM 1999 1 29 CALA9900059 1 19990111 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 FORWARD GALLEY CORROSION IN HOLES UPPER AND LOWER SURFACE ON FLOORBEAM STA 328 BL 0 TO R1 Z ANGLE. CUT OUT DAMAGED SECT ION OF CHORD, FABRICATED AND INSTALLED NEW CHORD PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999012900127 19990129 00127 WP 1999 1 29 CALA9900060 1 19990115 A 5312 991556173 BULKHEAD DOUBLER DOUG DC9 DC982 3022082 WP AFT PRESS BLKHD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 APB HAS CORROSION, BOTTOM AFT OF LONG 30. REMOVED AND REPLACED JACKPOST DOUBLER PER SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999012900128 19990129 00128 WP 1999 1 29 CALA9900061 1 19990116 A 5753 SKIN DOUG DC10 DC1030 3023501 WP RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13086 46917 RIGHT OUTBOARD FLAP UPPER SKIN CRACKED IN 4 PLACES, STATION 563.375, 4 AND 2 STATION 569.375, 7 AND STATION 581.377, 2. REMOVED AND REPLACED RIGHT OUTBOARD FLAP UPPER SKIN PER SRM 57-10-00. 2 L 7 3 4F A22WE 1999012900129 19990129 00129 WP 1999 1 29 CALA9900062 1 19990116 A 5752 5910047502 TAB DOUG DC9 DC932 3022066 WP RT AILERON DEBOND A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14524 47539 RIGHT AILERON INBOARD TAB HAS APPROXIMATELY 1 BY 10 DEBONDED LOWER SKIN. REMOVED AND REPLACED RIGHT AILERON PER MM 27-1 0-2. 2 L 7 2 4F A6WE 1999012900130 19990129 00130 WP 1999 1 29 CALA9900063 1 19990116 A 5330 5924802 SKIN DOUG DC9 DC982 3022082 WP BS 218-225 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 FORWARD FUSELAGE SKIN SCRATCHED AND DENTED STA 218 TO 225 BETWEEN LONG 15L AND 18L. REPAIRED PER EC/RA 5330-02445. 2 L 7 2 4F A6WE 1999012900131 19990129 00131 WP 1999 1 29 CALA9900064 1 19990117 A 5210 ASSIST BOTTLE DOUG DC10 DC1030 3023501 WP L1 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13086 46917 L1 DOOR ASSIST BOTTLE PRESSURE LOW. RECHARGED L1 DOOR ASSIST BOTTLE PER MM 52-12-06. 2 L 7 3 4F A22WE 1999012900132 19990129 00132 NM 1999 1 29 CALA9900065 1 19990117 A 3397 WIRE BOEING 737 7373T0 1384582 NM ROW 12 PINCHED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14358 23943 ROW 7 TO 12 EMERGENCY LIGHTS INOP. FOUND WIRE PINCHED IN SEAT TRACK AT ROW 12. REPAIRED WIRE, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999012900133 19990129 00133 WP 1999 1 29 CALA9900066 1 19990118 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 190 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 FLOOR SUPPORT CORRODED STA 190 APPROX BETWEEN PANEL K AND J FORWARD ENTRY, LIGHT CORROSION. FABRICATED FLOOR SUPPORT, P RIMED AND INSTALLED PER SRM 51-3-2. 2 L 7 2 4F A6WE 1999012900134 19990129 00134 NM 1999 1 29 UPS99228456 1 19990121 A 5753 65192086 FLAP TRACK BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI CORROSION ON WING ATTACH PAD AND FWD ATTACH LUGS OF NR 8 FLAP TRACK. REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1999012900135 19990129 00135 NM 1999 1 29 UPS99228457 1 19990121 A 5312 BULKHEAD BOEING 727 72725C 138400H NM BS 875 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI, RE-INFORCEMENT DOUBLER CORRODED AND BULKHEAD CRACKED AT BS STA 875 LBL 60 WL 182. REMOVED AND REPLA CED DOUBLER AND REPAIRED BULKHEAD PER SRM 53-10-9 FIG 4. 2 L 7 3 4F A3WE 1999012900136 19990129 00136 NM 1999 1 29 UPS99228458 1 19990121 A 5312 BULKHEAD BOEING 727 72725C 138400H NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI, RE-INFORCEMENT DOUBLER CORRODED AND BULKHEAD CRACKED AT BS STA 870 RBL 60 WL 182. REMOVED AND REPLA CED DOUBLER AND REPAIRED BULKHEAD PER SRM 53-10-9 FIG 4. 2 L 7 3 4F A3WE 1999012900137 19990129 00137 NM 1999 1 29 UPS99228459 1 19990121 A 5753 65192047 CARRIAGE BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI, CORROSION ON THRUST WASHER AND AFT SPINDLE BEARING SURFACE OF NR 8 MID FLAP CARRIAGE ASSEMBLY. REMO VED AND REPLACED CARRIAGE ASSEMBLY. 2 L 7 3 4F A3WE 1999012900138 19990129 00138 NM 1999 1 29 UPS99228460 1 19990120 A 5753 65192086 FLAP TRACK BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI, CORROSION (C57-581-01-1B) ON NR 2 FLAP TRACK FWD LUG AND INSIDE AFT MOUNT BARREL NUT HOLES. REMOVED CORRODED FLAP TRACK, INSTALLED SERVICEABLE FLAP TRACK IAW MM 51-30-2. TRACK WILL BE INSTALLED ON TC C57-581-04-3D. 2 L 7 3 4F A3WE 1999012900139 19990129 00139 NM 1999 1 29 UPS99228461 1 19990115 A 5347 BAC1520843 SEAT TRACK BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI, CRACKED SEAT TRACK FLANGE AT BS 1010, RBL 16, WL 156. REMOVED CRACKED SEAT TRACK SECTION FROM BS 95 0 TO 1010, RBL 16, WL 156. INSTALLED NEW SEAT TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999012900140 19990129 00140 NM 1999 1 29 UPS99228474 1 19990121 A 3350 LIGHT BOEING 727 72731C 1384011 NM COCKPIT LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 924UP 19234 COCKPIT EMERGENCY EXIT LIGHT FLICKERS IN THE ARMED POSITION. RE-SEATED COCKPIT EMERGENCY EXIT LIGHT ASSY INTO HOUSING. OPS CK OK, NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1999012900141 19990129 00141 NM 1999 1 29 UPS99228475 1 19990107 A 5320 FITTING BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:C, CRACK EMANATING FROM FASTENER HOLE IN BS 870 LT FITTING A FWD OUTBOARD FLANGE ABOVE STRINGER 9. REPA IR CARRIED OUT IAW APPENDIX C OF B727-5310-3057 AND DRAWING 65C35277. 2 L 7 3 4F A3WE 1999012900142 19990129 00142 NM 1999 1 29 UPS99428455 1 19990120 A 2820 CONNECTOR BOEING 747 747123 1384873 NM NR 4 CROSSFEED LOOSE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 674UP 20100 NR 4 FUEL CROSSFEED VALVE FAILED, CLOSED INFLIGHT. AIR TURNBACK TO ANC. LOCATED NR 4 FUEL CROSSFEED VALVE AND FOUND CA NNON PLUG OFF OF ACTUATOR. INSTALLED SYSTEM WITH PRESSURE ON, NO LEAKAGE NOTED. 2 L 7 4 4F A20WE 1999012900143 19990129 00143 WP 1999 1 29 UPS99828462 1 19990109 A 5320 3619434503N FITTING DOUG DC8 DC871F 302199D WP BS 1490 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, STA 1490 AT LONG 34R, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 36194343 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900144 19990129 00144 WP 1999 1 29 UPS99828463 1 19990115 A 5320 3750330505N FITTING DOUG DC8 DC871F 302199D WP BS 450 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, STA 450 AT LONG 35L, THE SPLICE FITTING IS DAMAGED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900145 19990129 00145 WP 1999 1 29 UPS99828464 1 19990105 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1745 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, STA 1745 AT STR 15L, THE LONG SPLICE FITTING IS CRACKED. REPAIRED LONG, BY SPLICING IAW SRM 53-2-2 FIG 11. 2 L 7 4 4F RT 4A25 1999012900146 19990129 00146 WP 1999 1 29 UPS99828465 1 19990106 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 7.095 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LT WING L/E RIB AT STA XILD7.095 IS CRACKED AT THE AFT UPPER END. REPAIRED AREA IAW SRM 57-2-2 FIG 2. 2 L 7 4 4F RT 4A25 1999012900148 19990129 00148 WP 1999 1 29 UPS99828467 1 19990115 A 5320 3750330505N FITTING DOUG DC8 DC871F 302199D WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, STA 450 AT STR 34R, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900149 19990129 00149 WP 1999 1 29 UPS99828468 1 19990104 A 5313 975491335N LONGERON DOUG DC8 DC871F 302199D WP BS 260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, STA 260 AT LONG 35R, THE LONGERON IS CRACKED. REMOVED AND REPLACED LONGERON IAW DWG 9754913 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900150 19990129 00150 WP 1999 1 29 UPS99828469 1 19990106 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 16.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E RIB AT STA XOLDI6.225 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012900151 19990129 00151 WP 1999 1 29 UPS99828470 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LT WING L/E RIB AT STA XFS622.5 IS CRACKED AT THE AFT LWR FAST. REPAIRED AREA IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012900152 19990129 00152 WP 1999 1 29 UPS99828471 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 435.789 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LT WING L/E RIB AT STA XFS435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012900153 19990129 00153 WP 1999 1 29 UPS99828472 1 19990107 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 341.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E LWR SKIN AT STA XFS341.5, THE T/E INTERNAL DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 57-3-0 FIG 7. 2 L 7 4 4F RT 4A25 1999012900154 19990129 00154 WP 1999 1 29 UPS99828473 1 19990121 A 3350 CONNECTOR DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 840UP 46140 AFTER T/O, THE EMERGENCY LIGHTS ILLUMINATED FOR NO APPARENT REASON. CYCLED THREE EM LT CBS TO NO AVAIL. CLEANED CONNEC TOR AT BATT PACK CK OK MM 33-50-01. 2 L 7 4 4F RT 4A25 1999012900168 19990129 00168 1999 1 29 99FDEA00024 4 19990122 A 3442 6225135001 DRIVE UNIT BOEING 727 72722 1384002 NM RADAR ANTENNA FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 185FE 18871 RADAR FAILED AFTER T/O PLUS 5 MIN REPEAT WRITEUP. REMOVED AND REPLACED RADAR ANTENNA DRIVE UNIT. OPER CK AND TEST CK G OOD PER 34-41-022. 2 L 7 3 4F A3WE 1999012900169 19990129 00169 EU 1999 1 29 99FDEA00025 1 19990122 A 2130 837101A SWITCH AIRBUS 310 A310203 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 401FE 191 99-0019 - AFT T/O CABIN WOULD NOT PRESSURIZE AND CLIMB AT A/C RATE. MANUAL PRESS SYS WOULD NOT CONTROL CABIN. REG 2 FW D AND AFT OUTFLOW VALVE REMAIN FULL OPEN AND IND AMBER ON ECAM WITH FAULT ON OV ERHEAD. REMOVED AND REPLACED LEFT MLG S HOCK ABSORBER RELAY 59GB,96GB. 2 L 7 2 4F RT A35EU 1999012900170 19990129 00170 NM 1999 1 29 99FDEA00026 1 19990123 A 2730 4016027217 COMPUTER BOEING 727 72725C 138400H NM ELEVATOR MALFUNCTIONED A FDEA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 25 133FE 19851 99-002O - ELEVATOR HAS 5 TO 6 INCH OF FREEPLAY IN THE YOKE (I.E.) MOVING THE YOKE AND NO RESPONSE FROM THE ELEVATOR. RE MOVED AND REPLACED ELEV FEEL COMPUTER, ADJUSTED AND TEST PER 727-100 MM 27-30-101-2. ADJUSTED AND TEST OF STAB TRIM POT ENTIOMETER C/W PER 727-100 MM 22-11-061-5 AND MM 22-11-06 1-4. INSTALL PNLS. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999012900171 19990129 00171 NM 1999 1 29 99FDEA00027 1 19990122 A 5312 65163006 BULKHEAD WEB BOEING 727 72725C 138400H NM BS 178 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DENT IN PRESSURE BULKHEAD AT BS 178, RBL 27, WL 210. *S/D* REPAIRED PART PER EA 7-5330-43765. 2 L 7 3 4F A3WE 1999012900172 19990129 00172 WP 1999 1 29 ABXA9900023 1 19990118 A 2710 CONTROLS DOUG DC8 DC862 3021970 WP LT AILERON FOD A ABXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 23 803AX 45917 DURING DESCENT, AIRCRAFT WOULD NOT TURN TO THE LEFT. PILOT REPORTED FEELING SOMETHING 'SNAP'. AFTERWARDS, AIRCRAFT WAS VERY SLUGGISH TURNING TO THE LEFT. TURNED OK TO RIGHT. CREW DECLARED EMERGENCY, LANDING WAS UNEVENTFUL. *S/D* VISUA LLY INSPECTED LEFT AND RIGHT AILERON POWER PACK AREAS. FOUND PARTS BAG (FOD) WRAPPED AROUND CABLE AND PULLEY BRACKET GU ARD IN LEFT INBOARD WING ROOT AREA. BAG WAS CAUSING INTERMITTENT BINDING. REMOVED BAG AND RERIGGED AILERONS IAW DC8 MM 27-10-00. 2 L 7 4 4F 4A25 1999012900173 19990129 00173 NM 1999 1 29 SWAA990130 1 19990120 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED APPROX 4 INCHES , LEFT SIDE AFT OF WING AND DIRECTLY BEHIND PREVI OUS REPAIR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999012900174 19990129 00174 NM 1999 1 29 SWAA990131 1 19990120 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 801 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED APPROX 1.5 INCH AT BS 801 S22L. INSTALLED REPAIR DOUBLER PER BOE ING SRM. 2 L 7 2 4F A16WE 1999012900175 19990129 00175 NM 1999 1 29 SWAA990132 1 19990119 A 5512 6554821 SKIN BOEING 737 7373H4 1384600 NM LT HORZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 634SW 27937 DURING SCHEDULED CHECK, FOUND LARGE DENT ON LT HORIZ STAB L/E APPROX 8 INCHES FROM WING ROOT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999012900176 19990129 00176 NM 1999 1 29 SWAA990133 1 19990119 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED BC1 CHECK, FOUND AFT SERVICE DOOR FRAME CUTOUT CRACKED APPROX 20. REPAIRED PER SWA RA 1-353-1985. 2 L 7 2 4F RT A16WE 1999012900177 19990129 00177 NM 1999 1 29 SWAA990134 1 19990119 A 3350 LAMP BOEING 737 7373H4 1384600 NM ROW 7 & 15 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT ROWS 7 AND 15. RELAMPED PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012900178 19990129 00178 NM 1999 1 29 SWAA990135 1 19990119 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED SC CHECK, FOUND RT OVERWING EXIT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012900179 19990129 00179 NM 1999 1 29 SWAA990136 1 19990119 A 3350 LAMP BOEING 737 7377H4 NM ROW 13 ABC FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 705SW 27839 DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. RELAMPED PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012900180 19990129 00180 NM 1999 1 29 SWAA990137 1 19990120 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 DURING PREFLIGHT CHECK, FOUND FLOOR EMERGENCY EXIT LIGHT WIRES EXPOSED, DAMAGED AND DISCONNECTED AT OVERWING EXITS. REP AIRED AND OP CHECKED LIGHTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012900181 19990129 00181 NM 1999 1 29 SWAA990138 1 19990119 A 3210 LANDING GEAR BOEING 737 7373H4 1384600 NM RIGHT DEER STRIKE A SWAA K NONE C F.O.D. LD LANDING 1 SW 07 652SW 27722 JUST AFTER MAIN GEAR TOUCH DOWN ON RWY 33L, AIRCRAFT STRUCK A DEER WITH RIGHT MAIN GEAR. ANIMAL PARTS FOUND ON RIGHT MA IN GEAR STRUT. ALSO, RIGHT MAIN GEAR BRAKE WAS LOST. INSPECTED RT MLG AREA, FOUND GROUND SHIFT CABLE, SHIMMY DAMPER, A NTISKID HARNESS AND BOTH BRAKE LINES DAMAGED. REMOVED AND REPLACED GROUND SHIFT CABLE, NR 3 TIRE AND BRAKE, NR 4 TIRE A ND BRAKE, RT MLG SHIMMY DAMPER, BOTH BRAKE LINES AND ANTISKID HARNESS PER BOEING MM. 2 L 7 2 4F RT A16WE 1999012900182 19990129 00182 NM 1999 1 29 SWAA990139 1 19990120 A 3350 CONNECTOR BOEING 737 7373T5 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 668SW 23060 DURING SCHEDULED BC3 CHECK, FOUND FWD CABIN EGRESS LIGHTS INOP. RECONNECTED LAMP CONNECTOR AND OP CHECKED PER BOEING MM . 2 L 7 2 4F RT A16WE 1999012900183 19990129 00183 NM 1999 1 29 SWAA990140 1 19990120 A 3350 CONNECTOR BOEING 737 7373T5 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 668SW 23060 DURING SCHEDULED BC3 CHECK, FOUND CENTER CABIN EGRESS LIGHTS INOP. REPAIRED LAMP CONNECTOR AND OP CHECKED PER BOEING MM . 2 L 7 2 4F RT A16WE 1999012900184 19990129 00184 NM 1999 1 29 SWAA990123 1 19990115 A 3220 FITTING BOEING 737 7372H4 138448C NM NLG DAMAGED A SWAA K NONE O OTHER LD LANDING 1 SW 07 091SW 22963 EN ROUTE, ISOLATION VALVE (REVERSE) ILLUMINATED. FOLLOWED QRH. NO ACTION REQUIRED. UPON LANDING GEAR DOWN RESULTED IN THREE LARGE NOISES AS EACH GEAR REACHED LOCKED POSITION. FOUND NOSE GEAR SERVICE FITTING DAMAGED. REPLACED FITTING, S ERVICED, RETRACTED GEAR PER MM. PERFORMED THRUST REVERSER SYS TEST PER MM. OPS CKD GOOD PER MM. 2 L 7 2 4F A16WE 1999012900185 19990129 00185 NM 1999 1 29 SWAA990124 1 19990116 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 757 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, S14R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER P ER BOEING SRM 53-00-01 FIG 202. 2 L 7 2 4F RT A16WE 1999012900186 19990129 00186 NM 1999 1 29 SWAA990125 1 19990118 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED 1/2D CHECK, FOUND BS 663 FRAME CRACKED AT S2L AND S3L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999012900187 19990129 00187 NM 1999 1 29 SWAA990126 1 19990118 A 5730 SKIN BOEING 737 7372H4 138448C NM LT WING GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D-CHECK, FOUND FIXED L/E SKIN WAS GOUGED AT CENTER UPSTOP CUTOUT FOR NR 5 SLAT, I/B AND O/B SIDE'S. CU T OUT DAMAGED FIXED LEADING EDGE SKIN, FABRICATED NEW LEADING EDGE SKIN AND SPLICE PLATES, TREATED REPAIR PARTS, INSTALL ED NEW SKIN AND SEALED AS PER TRAMCO EWO 98-1175. 2 L 7 2 4F A16WE 1999012900188 19990129 00188 NM 1999 1 29 SWAA990127 1 19990118 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1080 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 629SW 27704 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 1080, AT S27R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999012900189 19990129 00189 NE 1999 1 29 SWAA990128 2 19990119 A 7311 749965 FUEL/OIL COOLER BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 054SW 21535 AIR RETURN DUE TO REPORTED FLUID LEAK FROM NR 1 ENG COWLING AFTER T/O. FOUND FUEL VENTING FROM GEARBOX VENT AND EXCESSI VE FUEL IN OIL TANK. DURING INSPECTION FOUND FUEL IN OIL NR 1 ENG. REMOVED AND REPLACED FUEL/OIL COOLER. OPS AND LEAK CK NORMAL PER BOEING MM. 2 L 7 2 4F 4 F A16WE E2EA 1999012900222 19990129 00222 WP 1999 1 29 TWAA9901501 1 19990123 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 11-21 DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9420D 49824 CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 11 TO 21. REINSERTED WIRES IN EGRESS TRACK LIGHTING AND REPLACED THE BAT TERY PACK. CHECK-C 12-8-98 MCI. 2 L 7 2 4F RT A6WE 1999012900223 19990129 00223 WP 1999 1 29 TWAA9901502 1 19990122 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9402W 53138 FOUND EGRESS LIGHTS INOPERATIVE AT FORWARD GALLEY AND AT ROWS 4, 5, 17, 22, 26, AND 33. REPLACED LIGHT MODULES, MFG 010 5606-002 AND 0105606-003. CHECK-C 10-25-98 STL. 2 L 7 2 4F RT A6WE 1999012900224 19990129 00224 NM 1999 1 29 TWAA9901503 1 19990122 A 3397 59131 WIRE BOEING 757 757231 1384950 NM CABIN CONTAMINATED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 716TW 28484 THE EGRESS LIGHTING WAS INOPERATIVE IN THE AFT CABIN. CLEANED MOISTURE FROM EGRESS LIGHT TRACK. 2 L 7 2 4F RT A2NM 1999012900225 19990129 00225 1999 1 29 TWAA9901504 4 19990121 A 2565 22D2269632 SLIDE BOEING 727 727231 1384079 NM PAX DOOR LOW PRESS A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 24343 21630 THE FORWARD LEFT CABIN DOOR EVACUATION SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE SLIDE. CHECK-C 1-4-99 MCI. 2 L 7 3 4F A3WE 1999012900226 19990129 00226 WP 1999 1 29 TWAA9901505 1 19990124 A 3350 2232 LAMP DOUG DC9 DC982 3022082 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 922TW 48013 FOUND THE EVACUATION CHUTE LIGHT INOPERATIVE AT THE FORWARD LT AND RT CABIN DOORS. REPLACED LAMP IN EACH. CHECK-C 7-18 -98 STL. 2 L 7 2 4F A6WE 1999012900238 19990129 00238 WP 1999 1 29 AT9900035 1 19990101 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 SCHEDULED INSPECTION AT AERO CORP, FL. RIGHT HAND AFT VERTICAL SKIN IS CHAFED. REMOVED AND REPLACED THE SKIN IAW DC9 S RM 55-32-0 FIG 7, 51-10-2, 51-10-3 AND RES NR 982300. 2 L 7 2 4F A6WE 1999012900239 19990129 00239 NM 1999 1 29 AT9900036 1 19990121 A 3350 1691 LAMP BOEING 737 7372L9 1384497 NM LT FUSELAGE FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 LEFT FUSELAGE EMERGENCY LIGHT AFT OF WING DOES NOT ILLUMUNATE. RELAMPED LEFT AFT FUSELAGE EMERGENCY LIGHT IAW MM 33-51- 61, OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999012900240 19990129 00240 NM 1999 1 29 AT9900037 1 19990123 A 3350 LIGHT BOEING 737 7372L9 1384497 NM PASSENGER DOOR INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 CABIN EMERGENCY LIGHT ABOVE R-1 DOOR DID NOT ILLUMINATE DURING LAYOVER CHECK. SECURED FIXTURE PROPERLY INTO CONNECTOR A SSEMBLY, OPS CHECKED GOOD PER MM 33-50. (X) 2 L 7 2 4F RT A16WE 1999012900241 19990129 00241 WP 1999 1 29 AT9900038 1 19990121 A 3230 S243121510A030 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG LACK OF LUBE A ZZDA K NONE J WARNING INDICATION AP APPROACH 1 SO 15 831AT 47674 NO NOSE GEAR DOWNLOCK INDICATION ON GEAR EXTENSION, UPON ARRIVAL INTO ORLANDO MCO. RECYCLED GEAR, NO HELP. USED MANUAL PROCEDURES AND GOT DOWNLOCK INDICATION ON NOSE GEAR. DECLARED NO EMERGENCY MADE NORMAL LANDING. JACKED AIRCRAFT, CYCL ED GEAR TWICE IN NORMAL AND MANUAL PROCEDURES, NO DEFECT NOTED. LUBED GEAR OVER CENTRAL LINK, OPS CHECKED GOOD PER MM 3 2-20 AND 32-21 (P/N KIB14712UB) AND (P/N 39968-13). 2 L 7 2 4F A6WE 1999012900242 19990129 00242 NM 1999 1 29 AT9900039 1 19990117 A 5330 SKIN BOEING 737 737214 138446R NM COCKPIT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FUSELAGE CRACKED AT CAPTAINS FWD SKYLIGHT AND LOWER INBOARD WINDOW MOUNT SCREW. FABRICATED DOUBLER FROM 2024-T3 .0125 THOUSANDS IAW B737 SRM 51-30-8. INSTALLED REPAIRED IAW B737 SRM 53-30-3 AND AIRT RAN RES NR 9938. 2 L 7 2 4F A16WE 1999012900243 19990129 00243 NM 1999 1 29 AT9900040 1 19990114 A 5330 SKIN BOEING 737 737214 138446R NM BS 847 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. STA 847 STR 22R HAS RIPPED SKIN. FABRICATED DOUBLER AND INSTALLED REPAIR IAW B7 37 SRM'S 53-30-3, 51-30-2, AND AIRTRAN RES NR 9937. (X) 2 L 7 2 4F A16WE 1999012900244 19990129 00244 EU 1999 1 29 JBXA9900066 1 19990125 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU NLG FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 104ML 11445 AFTER SELECTING LANDING GEAR UP ON TAKEOFF THE NOSE GEAR INDICATOR INDICATED THAT IT WAS STILL DOWN AND LOCKED. THE LAN DING GEAR WAS CYCLED DOWN AND THEN UP TWICE WITH THE SAME RESULTING INDICATIONS. ALL OTHER (SECONDARY) INDICATIONS INDI CATED THE GEAR WAS UP. AIR RETURN TO RDU. FOUND NOSE LANDING GEAR LIGHT SOCKET ON LANDING GEAR POSITION INDICATOR SHOR TED. REMOVED AND REPLACED BULB IN NLG SOCKET IAW AMM 32-61-02. JACKED A/C AND SWUNG GEAR IAW AMM 07-11-00, OPS CHK GOO D. 2 L 7 2 4F RT 1999012900245 19990129 00245 1999 1 29 AWXA9900024 2 19990120 A 7530 1685MK7 ACTUATOR AIRBUS 320 A320231 3930325 EU NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 28 643AW 20123 315 ON CLIMBOUT, JUST PRIOR TO LEVEL OFF AT FL 220 THE NR 2 ENGINE COMPRESSOR STALLED AT FL 210. DURING CRUISE AT 220 IT OC CURRED TWO MORE TIMES. EXECUTED ATB TO PHX FOR REPAIRS. REMOVED AND REPLACED THE VSV ACTUATOR ON THE NR 2 ENG PER R5M75 303 POWER ASSURANCE TEST PER F5M71302 LEFT HPC ACTUATOR LINKAGE LUBE PER L5A75301. 2 L 7 2 4F RT A28NM 1999012900246 19990129 00246 EU 1999 1 29 AWXA9900025 1 19990121 A 2150 758A000002 VALVE AIRBUS 320 A320231 3930325 EU NR 1 PACK FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 632AW 81 ATB NR 2 PACK ON MEL NR 1 PACK BYPASS VALVE FAULTED. NR 1 PACK BYPASS VALVE FAULTED ON DEPARTURE. REMOVED AND REPLACED THE NR 1 PACK BYPASS VALVE. AWAITING TEARDOWN REPORT. 2 L 7 2 4F RT A28NM 1999012900247 19990129 00247 NM 1999 1 29 AWXA9900026 1 19990120 A 7722 WL202EED4 EGT GAUGE BOEING 737 73733A 1384673 NM NR 1 ENGINE MALFUNCTIONED A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 509DC 23636 NR 1 ENG EGT GAUGE VERY ERRATIC. NEEDLE FOLLOWS DIGITAL INDICATION WHICH INTERMITTENTLY BLANKS. BEGAN WORKING NORMAL F OR ABOUT THE LAST 15 MIN OF APPROACH. INSPECTED WIRE HARNESS AND ENGINE, ALL OK. REMOVED AND REPLACED NR 1 ENGINE EGT GAUGE. RAN ENGINE, OPS NORMAL. 2 L 7 2 4F RT A16WE 1999012900248 19990129 00248 SO 1999 1 29 RAAA99E9006 1 19990122 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 LT AFT EMERGENCY EXIT PULLDOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 4 4T 4A22 1999012900249 19990129 00249 SO 1999 1 29 RAAA99E9007 1 19990122 A 3350 CA31 BATTERY PACK LKHEED 188 188C 5262604 SO BS 555 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EXTERNAL EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1999012900250 19990129 00250 SO 1999 1 29 RAAA99E9008 1 19990122 A 3350 240498C RELAY LKHEED 188 188C 5262604 SO BS 555 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EXTERNAL EMERGENCY LIGHTS WOULD NOT EXTINGUISH ON SERVICE CHECK. CHANGED EXTERNAL EMERGENCY LIGHT RELAY DUE FAILED. 2 L 7 4 4T 4A22 1999012900251 19990129 00251 SO 1999 1 29 COMA9910017 1 19990121 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG LEAKING A COMA K NONE K FLUID LOSS CL CLIMB 1 SO 01 261CA 18259 1254 LT MLG DISAGREEMENT INDICATION WHEN LANDING GEAR RETRACTED. REPLACED THE LT MLG RETRACT ACTUATOR. 2 L 7 2 4T RT A31SO 1999012900252 19990129 00252 SO 1999 1 29 COMA9910018 1 19990119 A 5230 12038075003 GUIDE EMB 120 EMB120RT SO CARGO DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 159A 120159 DURING ROUTINE MAINTENANCE, THE UPPER CABLE GUIDE FITTING ON THE CARGO DOOR WAS FOUND TO HAVE SEVERE EXFOLIATION CORROSI ON. CORROSION WAS APPROX .1875 IN DEPTH OVER AN AREA OF 1X .50. THE FITTING WAS REPLACED WITH A SERVICEABLE FITTING AS PER EMB MAINTENANCE MANUAL CHAPTER 20. 2 L 7 2 4T RT A31SO 1999012900253 19990129 00253 1999 1 29 COMA9910019 3 19990122 A 6140 WARNING EMB 120 EMB120RT SO AUTOFEATHER SYS ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 261CA 254 DURING TAKEOFF ROLL, AUTOFEAHTER AURAL WARNING ACTIVATED. INSPECTED LT AND RT ENGINE SCU FOR CONDITION AND SECURITY. P ERFORMED OPERATIONAL CHECK OF THE AUTOFEATHER SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 1999012900254 19990129 00254 EA 1999 1 29 COMA9960037 1 19990121 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 991CA 2331 7216 CARGO SMOKE WARNING, FIRE BOTTLES DISCHARGED. FALSE WARNING. REPLACED FIRE BOTTLES AND SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 1999012900255 19990129 00255 EA 1999 1 29 COMA9960038 1 19990121 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 709CA 7238 CARGO SMOKE WARNING, BOTTLES DISCHARGED. FALSE WARNING. REPLACED FIRE BOTTLES AND SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 1999012900256 19990129 00256 EA 1999 1 29 COMA9960039 1 19990119 A 5320 FRAME CNDAIR CL600 CL6002B19 EA PAX DOORWAY DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 962CA 7123 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. CLEANED DIRT FROM DOOR FRAME AREA, DOOR OPERATION IS NORMAL. 2 L 7 2 4F RT A21EA 1999012900257 19990129 00257 1999 1 29 COMA9960040 4 19990118 A 3442 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA WEATHER RADAR TRIPPED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 927CA 7031 WEATHER RADAR IS INOP. RESET RADAR CIRCUIT BREAKERS, SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 1999012900258 19990129 00258 EA 1999 1 29 COMA9960041 1 19990123 A 3230 16600101 UPLOCK CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA K NONE O OTHER TO TAKEOFF 1 SO 01 983CA 7169 NOSE GEAR SLAMS VERY LOUDLY INTO GEARWELL WHEN RETRACTED. REMOVED AND REPLACED NLG UPLOCK ASSEMBLY. 2 L 7 2 4F RT A21EA 1999012900259 19990129 00259 EA 1999 1 29 COMA9960042 1 19990122 A 4990 387006 TRANSDUCER CNDAIR CL600 CL6002B19 EA APU OIL SYST FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 DURING CLIMBOUT, THE APU OIL PRESSURE WARNING ACTIVATED. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE OIL PRESSURE TRA NSDUCER. 2 L 7 2 4F RT A21EA 1999012900260 19990129 00260 NM 1999 1 29 UPS99228476 1 19990108 A 5320 STRAP BOEING 727 72725C 138400H NM BS 328-344 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, STABILIZER STRAP BETWEEN BS 328 AND BS 344 AT BL 0 WL 200 IS CRACKED. REMOVED CRACKED STRAP, FABRI CATED AND INSTALLED NEW STRAP IAW SRM 51-20-1, SRM 53-10-2, SRM 51-30-2. 2 L 7 3 4F A3WE 1999012900261 19990129 00261 NM 1999 1 29 UPS99228477 1 19990121 A 5711 FRONT SPAR BOEING 727 72725C 138400H NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C57-571-01.05-01) ON LEFT WING FRONT SPAR FUEL TANK ACCESS CUT OUT 7340 AFT SURFACE. REM OVED CORROSION AND REPAIRED PER EO 99-5020. 2 L 7 3 4F A3WE 1999012900262 19990129 00262 NM 1999 1 29 UPS99428478 1 19990122 A 3350 S1356B37 BATTERY PACK BOEING 747 747121 1384871 NM ENTRY DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-W/E, CREW ENTRY DOOR AFT EMERGENCY LIGHT INOP. ALSO, THE EMERGENCY LIGHT AFT OF THE UPPER DECK STAIR IS INOP. REPLACED LIGHT ASSY WITH BATTERY PACK. SYSTEM OPS CK GOOD REF 3317 P204. 2 L 7 4 4F A20WE 1999012900263 19990129 00263 NM 1999 1 29 UPS99528525 1 19990125 A 5311 HFAB53DB11 FRAME BOEING 757 75724APF 1384969 NM BS 1540 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE-C4, FRAME AT STA 1540 RBL 20.5, WL 154 IS DENTED IN AFT CGO BAY. REMOVED DAMAGED AREA AND FABRICATED DO UBLER AND INSTALLED PER SRM 51-70-11 SRM 51-30-2. 2 L 7 2 4F RT A2NM 1999012900264 19990129 00264 NM 1999 1 29 UPS99528526 1 19990125 A 5311 HFAB53DB11 FRAME BOEING 757 75724APF 1384969 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE-C4, FRAME AT STA 1480 LBL 29 WL 152 IS CRACKED IN AFT CGO BAY. REMOVED DAMAGED AREA AND FABRICATED REPA IR DOUBLER PER SRM 51-70-11 AND INSTALLED SRM 51-24-03, SRM 51-20-01. 2 L 7 2 4F RT A2NM 1999012900265 19990129 00265 NM 1999 1 29 UPS99528527 1 19990125 A 5311 HFAB53DB11 FRAME BOEING 757 75724APF 1384969 NM BS 1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE-C4, FRAME AT STA 1500 LBL 29 WL 151 IS CRACKED IN AFT CARGO BAY. REMOVED DAMAGED AREA, FABRICATED FRAME DOUBLER AND INSTALLED PER SRM 51-70-11 AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 1999012900266 19990129 00266 NM 1999 1 29 UPS99528528 1 19990125 A 5311 HFAB53DB11 FRAME BOEING 757 75724APF 1384969 NM BS 1260 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE-C4, FRAME IS DENTED AT BS 1260 STR 25 LT. REMOVED DAMAGED AREA, FABRICATED DOUBLER, HEAT TREATED AND IN STALLED PER SRM 51-70-11. 2 L 7 2 4F RT A2NM 1999012900267 19990129 00267 NM 1999 1 29 UPS99528529 1 19990125 A 5311 HFAB53DB11 FRAME BOEING 757 75724APF 1384969 NM BS 1300 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 412UP 23852 INSPECTION TYPE-C4, FRAME IS DENTED AT BS 1300 STR 25 RT. REMOVED DAMAGED AREA OF THE FRAME BS 1300 STR 25 RT. FABRICA TED DOUBLER, HEAT TREATED AND INSTALLED REPAIR PARTS PER SRM 51-70-11, SRM 51-40-02. 2 L 7 2 4F RT A2NM 1999012900274 19990129 00274 WP 1999 1 29 UPS99828486 1 19990105 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, FUSELAGE FRAME CRACKED AT FS 1480, LONG 33L. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012900275 19990129 00275 WP 1999 1 29 UPS99828487 1 19990109 A 5720 64687101 CLIP DOUG DC8 DC871F 302199D WP BS 855 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, FS 855 REAR SPAR IS CORRODED BEYOND LIMITS AT LBL 28. REMOVED AND REPLACED DAMAGED CLIP IAW SRM 51-1 -20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999012900276 19990129 00276 WP 1999 1 29 UPS99828488 1 19990112 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, UPPER TANG OF FLOORBEAM AT FS 879, RBL 68 IS CORRODED. REPAIRED FLOORBEAM IAW DHC SK701-677. 2 L 7 4 4F RT 4A25 1999012900277 19990129 00277 WP 1999 1 29 UPS99828489 1 19990118 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SHEAR TIE CRACKED AT FS 1480, BETWEEN LONG 34L AND 35L. CUT OUT DAMAGED SHEAR TIE AND REPAIRED IAW S RM 53-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 1999012900278 19990129 00278 WP 1999 1 29 UPS99828490 1 19990121 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1490-1500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SEAT TRACK CORRODED AT 1500 TO 1490, RBL 60. REMOVED DAMAGED SEAT TRACK FROM FS 1490 TO 1550, FABRIC ATED AND REPLACED SEAT TRACK IAW EO DC8-5320-5167-C, SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012900279 19990129 00279 WP 1999 1 29 UPS99828491 1 19990122 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SEAT TRACK CORRODED AT FS 1520, LBL 50. REMOVED DAMAGED SEAT TRACK FROM FS 1530 TO 1580, FABRICATED AND REPLACED SEAT TRACK IAW SRM EO DC8-5320-5167-C AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012900281 19990129 00281 WP 1999 1 29 UPS99828493 1 19990104 A 5320 3754946501 FITTING DOUG DC8 DC871F 302199D WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, CRACK AT UPPER FWD CORNER OF C-PIT DOOR FRAME SUPPORT FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012900282 19990129 00282 WP 1999 1 29 UPS99828494 1 19990104 A 5347 3657503501 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, SECOND OBS FWD SEAT TRACK HAS HEAVY CORROSION AROUND RT ATTACH SCREW. REMOVED AND REPLACED SEAT TRA CK IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012900283 19990129 00283 WP 1999 1 29 UPS99828495 1 19990104 A 5320 97555362 FITTING DOUG DC8 DC871F 302199D WP BS 1338 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FITTING IS CRACKED AT FS 1338, LT SIDE JUST BELOW THE CUSP. REMOVED AND REPLACED FITTING IAW SRM 51 -1-20D, 51-3-0. 2 L 7 4 4F RT 4A25 1999012900284 19990129 00284 WP 1999 1 29 UPS99828496 1 19990104 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 875-881 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 24R, HORIZ LEG IS CRACKED AT FS 875 TO 881. STOP DRILLED CRACK AND REPAIRED IAW SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 1999012900285 19990129 00285 WP 1999 1 29 UPS99828497 1 19990104 A 5320 37552171 SPLICE DOUG DC8 DC871F 302199D WP BS 200-220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 31R SPLICE ANGLE AT FS 200 TO 220 IS CRACKED. REMOVED AND REPLACED SPLICE IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900286 19990129 00286 WP 1999 1 29 UPS99828498 1 19990106 A 5320 5711283516 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, HEAVY CORROSION ON THE TORQUE BOX ATTACH FITTING AT FS 1220, LONG 31R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999012900287 19990129 00287 WP 1999 1 29 UPS99828499 1 19990106 A 5320 4758514507 FITTING DOUG DC8 DC871F 302199D WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 33R AT FS 1240, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900288 19990129 00288 WP 1999 1 29 UPS99828500 1 19990106 A 5320 37592221 FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, MODERATE TO HEAVY CORROSION ON LONG 36 SPLICE FITTING AT FS 1260 TO 1280. REMOVED AND REPLACED FITT ING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900289 19990129 00289 WP 1999 1 29 UPS99828501 1 19990110 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 60 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FUSELAGE SKIN AT FS 60, LONG 12L, HAS A .150 CRACK. CUT OUT DAMAGED AREA AND REPAIRED IAW DHC SK713 -223. 2 L 7 4 4F RT 4A25 1999012900290 19990129 00290 WP 1999 1 29 UPS99828502 1 19990110 A 5313 575527147 LONGERON DOUG DC8 DC871F 302199D WP BS 190-300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3 LONG 33R IS CORRODED AT FS 190 THRU 300. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900291 19990129 00291 WP 1999 1 29 UPS99828503 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, RT WING L/E RIB AT XFS 304.0 IS CRACKED AT THE FWD PNEU DUCT SUPPORT ROD MOUNT FITTING. STOP DRILLE D CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012900292 19990129 00292 WP 1999 1 29 UPS99828504 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING L/E RIB AT XFS 710.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0. 2 L 7 4 4F RT 4A25 1999012900293 19990129 00293 WP 1999 1 29 UPS99828505 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING L/E RIB AT XFS 304.0 IS CRACKED AT THE FWD PNEU DUCT SUPPORT ROD MOUNT FITTING. STOP DRILLE D CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012900294 19990129 00294 WP 1999 1 29 UPS99828506 1 19990108 A 5320 4647657 FITTING DOUG DC8 DC871F 302199D WP BS 1640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 34L END FITTING CORRODED AT FS 1640. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900295 19990129 00295 WP 1999 1 29 UPS99828507 1 19990110 A 5313 575527113 LONGERON DOUG DC8 DC871F 302199D WP BS 390-450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 390 TO 450, LONG 33L HAS CORROSION INSIDE HAT CHANNEL. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 51-1-20D, AND DWG 5755271. 2 L 7 4 4F RT 4A25 1999012900296 19990129 00296 WP 1999 1 29 UPS99828508 1 19990110 A 5313 575527113 LONGERON DOUG DC8 DC871F 302199D WP BS 390-450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 34L FS 390 TO 450 HAS SEVERE CORROSION. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5755 271 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900297 19990129 00297 WP 1999 1 29 UPS99828509 1 19990110 A 5313 575527145 LONGERON DOUG DC8 DC871F 302199D WP BS 438 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 32R AT FS 438 HAS CORROSION. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900298 19990129 00298 WP 1999 1 29 UPS99828510 1 19990110 A 5313 975491331 LONGERON DOUG DC8 DC871F 302199D WP BS 360-380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 35L AT FS 360 TO 380 HAS MODERATE CORROSION. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900299 19990129 00299 WP 1999 1 29 UPS99828511 1 19990111 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 127 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, TWO INCH CRACK IN RT WING T/E RIB AT XRS 127. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012900300 19990129 00300 WP 1999 1 29 UPS99828512 1 19990111 A 5320 9755878501 DOUBLER DOUG DC8 DC871F 302199D WP BS 340-400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, THE INTERNAL DOUBLER AT FS 340 TO 400, RT IS CORRODED BEYOND LIMITS, LONG 35L. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 9755878 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012900301 19990129 00301 WP 1999 1 29 UPS99828513 1 19990112 A 5320 561537411 DOUBLER DOUG DC8 DC871F 302199D WP BS 1490-1530 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 31L FINGER DOUBLER FS 1490 TO 1530 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615374 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012900302 19990129 00302 WP 1999 1 29 UPS99828514 1 19990112 A 5720 576989113 DOUBLER DOUG DC8 DC871F 302199D WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING L/E LWR SKIN, THE INTERNAL DOUBLER AT XOLDI 6.225 IS CRACKED. REMOVED, FABRICATED AND REPLA CED DOUBLER IAW DWG 5769891 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 1999012900303 19990129 00303 WP 1999 1 29 UPS99828515 1 19990115 A 5320 37558251 FITTING DOUG DC8 DC871F 302199D WP BS 220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, DOOR JAMB BACKUP FITTING AT FS 220 BETWEEN LONG 32R AND 33R HAS SEVERE CORROSION. REMOVED AND REPLA CED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900304 19990129 00304 WP 1999 1 29 UPS99828516 1 19990115 A 5320 37558251 FITTING DOUG DC8 DC871F 302199D WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, DOOR JAMB BACKUP FITTING AT FS 280 BETWEEN LONG 34R AND 35R HAS SEVERE CORROSION. REMOVED AND REPLA CED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900305 19990129 00305 WP 1999 1 29 UPS99828517 1 19990115 A 5320 37558241 FITTING DOUG DC8 DC871F 302199D WP BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, DOOR JAMB BACKUP FITTING AT FS 320 BETWEEN LONG 34R AND 35R HAS SEVERE CORROSION. REMOVED AND REPLA CED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900306 19990129 00306 WP 1999 1 29 UPS99828518 1 19990115 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 1210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 1210 ABOVE LONG 35R, THE TORQUE BOX WEB IS CORRODED BEYOND LIMITS. REPAIRED TORQUE BOX WEB IAW E O DC8-5350-7876-A. 2 L 7 4 4F RT 4A25 1999012900307 19990129 00307 WP 1999 1 29 UPS99828519 1 19990119 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 858 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, RT MLG W/W PRESSURE WEB APPROX FS 858, RBL 50, THE REPAIR ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED REPAIR ANGLE IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999012900308 19990129 00308 WP 1999 1 29 UPS99828521 1 19990103 A 2780 36511141 BRACKET DOUG DC8 DC871F 302199D WP NR 5 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING NR 5 SPOILER, I/B OPERATING CRANK MOUNT BRACKET, LWR ARM IS CRACKED. REMOVED AND REPLACED M OUNT BRACKET IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999012900309 19990129 00309 WP 1999 1 29 UPS99828522 1 19990105 A 5320 4610355 FITTING DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 36 AT FS 70 HAS SEVERE CORROSION. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900310 19990129 00310 WP 1999 1 29 UPS99828523 1 19990105 A 5313 3702969 LONGERON DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 36 AT FS 70 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 37029 69 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900311 19990129 00311 WP 1999 1 29 UPS99828524 1 19990119 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING L/E LWR SKIN IS CRACKED APPROX 5 I/B OF STA XOLDI 6.225. STOP DRILLED CRACK AND REPAIRED IA W EO DC8-5720-7767A. 2 L 7 4 4F RT 4A25 1999012900312 19990129 00312 WP 1999 1 29 MWEA99049 1 19990118 A 5320 9958214 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 896 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FUSELAGE FRAME AT STATION 896 SHEAR TIE CRACKED AT AFT FASTENER ROW ABOVE LONGERON 24 LEFT. MTC FABRICATED AND INSTALLE D NEW SHEAR TIE. 2 L 7 2 4F A6WE 1999012900313 19990129 00313 WP 1999 1 29 MWEA99050 1 19990120 A 5730 5910465 SKIN DOUG DC9 DC932 3022066 WP RT WING LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FOUND FOUR LIGHTNING STRIKE ARCS IN RIGHT WING LOWER PLATING SKIN. MTC REPAIRED WITH RIVET INSTALLATION. 2 L 7 2 4F A6WE 1999012900314 19990129 00314 NM 1999 1 29 DL75A990132 1 19990121 A 5400 313N3100156 FAIRING BOEING 757 757212 NM PWA 2037 PW2037 NE NR 2 ENGINE DETACHED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 757AT 23127 716339 NR 2 ENG FWD PYLON FAIRING DEPARTED AIRCRAFT DURING T/O. RETURNED TO DFW. REPLACED FAIRING. 2 L 7 2 4F 4 F RT A2NM E17NE 1999012900315 19990129 00315 NM 1999 1 29 DL73E990133 1 19990121 A 3350 BATTERY 334101877 BOEING 737 7372S3 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 367DL 21774 EMERGENCY EXIT LIGHT BATTERIES DEAD DUE TO GND POWER LOSS. REPLACED EMERGENCY EXIT BATTERIES AND BASE ASSY. 2 L 7 2 4F RT A16WE 1999012900316 19990129 00316 NM 1999 1 29 DL72W990134 1 19990121 A 2710 BEARING DPN274201533 BOEING 727 727247 138408F NM AILERON CONTROL RUSTED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 291WA 22109 DURING TAXI CONTROL CK WAS NORMAL, AFTER T/O AILERONS WERE VERY HEAVY AND ABRUPT MOVEMENT CAUSED WHAT FELT LIKE MANUAL R EVERSION. GROUND CHECKS AFTER LANDING SHOWS HEAVIER THAN NORMAL. FAST INPUT STILL SHOWS TENDENCY TO LOCK UP. REPLACED AILERON CENTERING SPRING BEARING. CHECKED CABLES AND SPRING CARTRIDGE AILERON FORCES WITHIN MM LIMITS. 2 L 7 3 4F A3WE 1999012900317 19990129 00317 WP 1999 1 29 DLL10990135 1 19990121 A 2170 COALESCER LKHEED 1011 10113851 5265010 WP CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 728DA 193C1173 SMOKE IN COCKPIT AND AFT CABIN. REPLACED WATER SEPARATORS. PERFORMED DUCT BURN-OUT. 2 L 7 3 4F A23WE 1999012900318 19990129 00318 NM 1999 1 29 DL72S990136 1 19990121 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 FOUND AT A-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT ENTRYWAY LT FRAME APPROX 6 INCHES BELOW UPPER STOP CASTING. REP AIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999012900319 19990129 00319 NM 1999 1 29 DL72S990137 1 19990121 A 5240 FRAME BOEING 727 727232 1384082 NM R-1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 FOUND AT A-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT FRAME OF R-1 DOOR AT FWD SIDE OF LWR STOP CASTING. REPAIRED PER MM 52-12-0. 2 L 7 3 4F A3WE 1999012900320 19990129 00320 NM 1999 1 29 DL76L990138 1 19990121 A 3350 POWER SUPPLY S283T0143 BOEING 767 767332 1382001 NM ROW 38 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 177DN 2980 25122 EMERGENCY TRACK LIGHTING INOP AFT OF ROW 38. REPLACED POWER SUPPLY, SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999012900321 19990129 00321 1999 1 29 DL72W990139 2 19990122 A 7200 ENGINE BOEING 727 727247 138408F NM NR 2 FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 2811W 46079 20649 NR 2 ENGINE OIL PRESSURE INDICATION WENT TO 100 PSI. ON ENGINE SHUTDOWN, INDICATION WENT TO 60 PSI. ALL OTHER ENGINE IN DICATIONS NORMAL WHEN ENGINE RUNNING. SHUTDOWN ENGINE PER POM, REPLACED ENGINE. 2 L 7 3 4F A3WE 1999012900322 19990129 00322 NM 1999 1 29 DL72W990140 1 19990120 A 5330 6586113 SKIN BOEING 727 727247 138408F NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUR HOLES WERE DISCOVERED CRACKED IN THE SKIN AT BS 940. THE HOLES WERE O/S THRU THE SKIN, STRINGER (18A) AND FITTING. FINAL HOLES ARE SHOWN ON FIGURE 1 OF ERA 332686-14. REPAIRED PER ERA 332686-14. 2 L 7 3 4F A3WE 1999012900323 19990129 00323 NM 1999 1 29 DL72W990141 1 19990120 A 5311 65561004 FRAME BOEING 727 727247 138408F NM BS 560 MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 2810W 20648 MTC DISCOVERED TWO MISDRILLED HOLES IN THE I/B CHORD OF THE BS 560 FRAME NEAR S27R. REPAIRED PER ERA 332713-14. 2 L 7 3 4F A3WE 1999012900324 19990129 00324 NM 1999 1 29 DL72W990142 1 19990120 A 5711 65162318 SPAR CHORD BOEING 727 727247 138408F NM WS 333 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 THE FRONT SPAR CHORD WAS FOUND WITH CRACKS IN THE FWD FLANGE AT A FASTENER HOLE AT APPROX WS 333. REPAIRED PER ERA 3326 87-14. 2 L 7 3 4F A3WE 1999012900325 19990129 00325 NM 1999 1 29 DL72W990143 1 19990120 A 5530 65168165 STRINGER BOEING 727 727247 138408F NM VERT STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 WEAR WAS FOUND ON THE S7L ON THE VERT STAB. DAMAGE IS TO THE O/B SURFACE OF THE UPPER FLANGE AT APPROX FIN STA 230. RE PAIRED PER ERA 332689-14. 2 L 7 3 4F A3WE 1999012900326 19990129 00326 NM 1999 1 29 DL72W990144 1 19990120 A 5312 65163007 BULKHEAD WEB BOEING 727 727247 138408F NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 BS 178 BULKHEAD WAS FOUND WITH CRACKS IN THE TYP LOCATIONS AS SHOWN IN THE BACO SRM 53-10-9, FIGURE 14. ADDITIONAL CRAC K FOUND OUTSIDE THE TYP LOCATION. REPAIRED PER ERA 332712-14. 2 L 7 3 4F A3WE 1999012900327 19990129 00327 NM 1999 1 29 DL72W990145 1 19990120 A 5330 65545661 SKIN BOEING 727 727247 138408F NM BS 673 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 SKIN WAS FOUND CORRODED AND THREE ADDITIONAL REPAIRS REMOVED AND ALL DAMAGE INCORPORATED INTO ONE REPAIR. DAMAGE IS LOC ATED AT BS 673, S28L. REPAIRED PER ERA 303790-14, REV C. 2 L 7 3 4F A3WE 1999012900328 19990129 00328 NM 1999 1 29 DLM88990146 1 19990122 A 5330 5920323211 SKIN DOUG MD88 MD88 3023688 NM BS 332-351 CREASED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 904DL 49535 CREASE FOUND IN FUSE SKIN BETWEEN STA 332 AND 351 BETWEEN LONGERONS 24R AND 25R. TRIMOUT IS 19.5 BY 3.8. REPAIRED PER ERA 332691-14. 2 L 7 2 4F RT A6WE 1999012900329 19990129 00329 NM 1999 1 29 DL72W990147 1 19990120 A 5311 651634234 FRAME BOEING 727 727247 138408F NM BS 1030 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 BS 1030 FRAME I/B OF LBL 40 WAS FOUND DENTED AT THE TOP AND EXCEEDED SRM ALLOWABLE LIMITS. A CUT OUT WAS NECESSARY. RE PAIRED PER ERA 332661-14 2 L 7 3 4F A3WE 1999012900330 19990129 00330 NM 1999 1 29 DL72S990148 1 19990118 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 FOUND DURING MV-1 CORROSION VISIT NRC 16, .25 INCH CRACK VISIBLE AT AFT ENTRY DOOR FRAME UPPER LT LOCATION. REPAIRED PE R SRM 53-10-9 FIG 11. 2 L 7 3 4F A3WE 1999012900331 19990129 00331 NM 1999 1 29 DL72S990149 1 19990118 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 FOUND DURING MV-1 CORROSION VISIT NRC 46, CORROSION AT FLOORBEAM STA 344 RBL 5 TO LBL 60 UPPER AND LOWER SIDES. REPAIRE D PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1999012900332 19990129 00332 NM 1999 1 29 DL72S990150 1 19990121 A 5330 6554567 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 DURING SPECIAL HFEC INSPECTION, THE STRINGER 4R SKIN LAP SPLICE WAS FOUND WITH 4 CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE INNER SKIN PANEL. THE ENTIRE LAP SPLICE WAS CUT (UPPER AND LOWER SKIN) AND REMOVED FOR FURTHER EVALUAT ION. THE CUT SKIN LAP WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STRUCTURAL FILLER PER ER/A 366490-14, REV A. 2 L 7 3 4F A3WE 1999012900333 19990129 00333 NM 1999 1 29 DL72S990151 1 19990120 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 480-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 DURING ACCOMPLISHMENT OF SPECIAL HFEC AND LFEC INSPECTIONS, 82 CRACK INDICATIONS WERE FOUND IN THE LOWER ROW OF THE LOWE R SKIN OF STRINGER 4R LAP SPLICE BETWEEN FS 480 TO 681. THE SKIN LAP AREA WAS CUT AWAY AND REMOVED. THE SPLICE WAS RES TORED WITH AND EXTERNAL ALUMINUM DOUBLER AND STRUCTURAL FILLER PER ER/A 366485-14, REV A. 2 L 7 3 4F A3WE 1999012900334 19990129 00334 WP 1999 1 29 DLL10990153 1 19990122 A 3020 307001045 VALVE LKHEED 1011 10113851 5265010 WP NR 1 ENGINE FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 728DA 193C1173 NR 1 ENGINE ANTI ICE INOP, C/B POPPED. DUE TO HISTORY FWD TO MCO AND PLAC PER MEL 30-21-01B. NEEDS VALVE ASSY P/N 30700 1045 NIS CVG VALVE LOCKED IN OPEN POSITION. 2 L 7 3 4F A23WE 1999012900335 19990129 00335 NM 1999 1 29 DL72L990154 1 19990122 A 5754 STIFFENER BOEING 727 727232 1384082 NM NR 6 SLAT TRACK CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 CHK D-1, O/B SPAR STIFFENER CRACKED, NR 6 L/E SLAT O/B TRACK BOX. REPLACED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999012900336 19990129 00336 NM 1999 1 29 DLM88990155 1 19990122 A 3350 POWER SUPPLY RPSB1 DOUG MD88 MD88 3023688 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 908DL 3798 49539 ON INSPECTION, FOUND APPROX ONE THIRD OF EMERGENCY PATH LIGHTS INOP IN CENTER PORTION OF CABIN. REPLACED AFT POWER SUPP LY FOR EMERGENCY PATH LIGHTS, OPN NORMAL. 2 L 7 2 4F RT A6WE 1999012900337 19990129 00337 NM 1999 1 29 DL72W990156 1 19990122 A 3350 SIGN 02019241001 BOEING 727 727247 138408F NM RT EMER EXIT MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 RT FWD OVERWING EXIT SIGN MISSING. REPLACED RT FWD OVERWING EXIT SIGN, OP CKS OK. 2 L 7 3 4F A3WE 1999012900338 19990129 00338 NM 1999 1 29 DL767990158 1 19990123 A 3230 321003012 ACTUATOR 321003012 BOEING 767 767232 1385132 NM LT MLG GEAR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 102DA DL191 22214 LEFT MAIN GEAR REMAINED DOWN ON DEPARTURE FROM LAX. LOWERD LANDING GEAR AND RECEIVED NORMAL INDICATION. RETURNED TO LA X. TROUBLESHOOTING REVEALED LT GEAR SIDE LOCK ACTUATOR BYPASSING. REMOVED ROD END AND FOUND UPPER PORTION OF ROD ATTAC HED TO PISTON SHEARED OFF. REPLACED ACTUATOR PER M/M 32-32-02-4. 2 L 7 2 4F RT A1NM 1999012900339 19990129 00339 NM 1999 1 29 DL72S990159 1 19990121 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 740 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 FOUND DURING MV-1 CHECK, CORROSION ON SUPPORT ANGLE AT STA 740 STR 27 RT. REPLACED ANGLE PER M/M 53-11-0 FIG 826. 2 L 7 3 4F A3WE 1999012900340 19990129 00340 NM 1999 1 29 DLM88990160 1 19990123 A 3350 BATTERY PACK 110049 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 985DL 8223 53312 AFT CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND CHARGER, NOW OPS NORMAL. 2 L 7 2 4F RT A6WE 1999012900341 19990129 00341 WP 1999 1 29 DHL99807001 1 19990122 A 3240 BRAKE DOUG DC8 DC873F 302199F WP LANDING GEAR VIBRATION A DHLA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SO 01 807DH 45990 AFTER REACHING V1 SPEED AND BEFORE ROTATION, SEVERE VIBRATION STARTED FROM UNDERNEATH AIRCRAFT. ANTISKID INOP LIGHT FLI CKERED ON FOLLOWED BY MAIN GEAR SPOILER INOP LIGHT ILLUMINATED. ANTISKID INOP LIGHT THEN EXTINGUISHED. INSPECTED AIR CRAFT FOR OBVIOUS DEFECTS, NONE NOTED. ANTISKID OPS CHECK GOOD IAW 32-43-0. BRAKES OPS CHECK GOOD BLED NR 7 AND NR 8 B RAKES AS PRECAUTIONARY PER MM 32-41-0. 2 L 7 4 4F RT 4A25 1999012900342 19990129 00342 NM 1999 1 29 VNAA9901020 1 19990120 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 432JS 82328 18871 3045 THE EMERGENCY LIGHTS AT THE MIDDLE SECTION OF THE AIRCRAFT WERE NOTED TO BE INOPERATIVE, DURING THE PREFLIGHT INSPECTION . MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT THE 5LK POSITION, IN ACCORDANCE WITH DORNIER M AINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900343 19990129 00343 NM 1999 1 29 VNAA9901021 1 19990114 A 3260 2240500004 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG DIRTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 432JS 86654 59224 3045 AFTER DEPARTURE, A RIGHT HAND MAIN LANDING GEAR UNLOCK INDICATION ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND L ANDED SAFELY. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT T OOK PLACE WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AND CLEANED SAND AND ICE FROM THE RIGHT HAND MAIN LANDING GEAR UP LOCK MECHANISM. GEAR SWING OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900344 19990129 00344 1999 1 29 VNAA9901022 4 19990118 A 3422 7010133 FLUX VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE VERT STAB DAMAGED A VNAA O OTHER C F.O.D. DE DESCENT 1 GL 07 422JS 12475 3018 THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE TO THE AIRCRAFT ON THE DESCENT INTO PIT. MAINTENANCE COMPLIED WITH A LIGH TNING STRIKE INSPECTION AND FOUND DAMAGE ON THE RIGHT ELEVATOR TRAILING EDGE. THE ELEVATOR DAMAGE WAS REPAIRED PER 51-7 7-10. ALSO, MAINTENANCE NOTED A TEN DEGREE HEADING SPLIT ON THE AIRCRAFT. THE AIRCRAFT WAS INSPECTED FOR A FERRY FLIGH T TO DAYTON FOR REPAIR. DAYTON MAINTENANCE INSPECTED AND REPLACED THE NR 1 FLUX VALVE, AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-21-12. OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999012900583 19990129 00583 NM 1999 1 29 HNAA9900016 1 19990121 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM FUSELAGE MALFUNCTIONED A HNAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 07 960HA 326 SMOKE WARNING LIGHT ILLUMINATES INTERMITTANTLY IN FLIGHT. COULD NOT DUPLICATE. REPLACED ANNUNCIATOR PANEL (P/N 75-0434 -1) (S/N 0075), SMOKE DETECTOR (P/N 473054) (S/N 0052) AND SMOKE DETECTION CONTROL AMPLFIER (P/N 30-326E7) (S/N 0354) AS A PRECAUTION. 2 H 7 2 4T RT A13NM 1999012900584 19990129 00584 NM 1999 1 29 HNAA9900017 1 19990123 A 5210 TAB DHAV DHC8 DHC8102 2809003 NM PAX DOOR BROKEN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 LOWER AFT CORNER OF PASSENGER DOOR ENTRANCE COMBING HAS TAB BROKEN OFF. REPAIRED AS NECESSARY. 2 H 7 2 4T RT A13NM 1999012900585 19990129 00585 NM 1999 1 29 HNAA9900018 1 19990122 A 7810 85411800005 SHROUD DHAV DHC8 DHC8102 2809003 NM NR 1 ENG EXHAUST CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 925HA 111 NR 1 ENGINE EXHAUST SHROUD HAS 1 INCH CRACK STA 223.4 AT 4 O'CLOCK POSITION, REAR I/B MOUNT BOLT OF FORWARD RADIATION SH IELD IS PULLED THROUGH, REAR O/B ANGLE BRACKET 1.5 INCH CRACK STA XN276.50, OUTLET SHROUD RING 5 CRACKS AT RIVETS STA XN 221.25 FROM 4 TO 6 O'CLOCK POSITIONS, DIAPHRAGM BRACKET STA XN236.50 2 INCH CRACK AT THE 8 O'CLOCK POSITION AND 1 INCH C RACK AT 6 O'CLOCK POSITION, .5 INCH CRACK STA XN240 AND 1 INCH CRACK STA XN275.50 ON O/B SIDE SKIN BRACKET, 3 INCH HOLE CHAFED IN CENTER RADIATION SHIELD STA 237.00, 6TH AND 7TH FRAME TO EXHAUST PLATE L ANGLES CRACKED, 3RD FRAME STA XN227.3 5 CRACKED, LOOSE RIVETS ON 3RD FRAME L ANGLE STA XN227.25, FRAME STA 236.50 CRACKED AT 4, 6 AND 8 O'CLOCK POSITIONS. RE 2 H 7 2 4T RT A13NM 1999012900587 19990129 00587 WP 1999 1 29 9900239883 1 19990116 A 5730 SKIN DOUG DC9 DC951 3022051 WP WS 195 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 671MC 47660 DURING PERIODIC CHECK, FOUND 4.5 INCH CRACK ON LOWER LEFT WING LEADING AT WS 195 FORWARD OF ACCESS DOOR 1132A. INSTALLE D INTERNAL AND EXTERNAL DOUBLERS PER EA 98-163654. 2 L 7 2 4F RT A6WE 1999012900588 19990129 00588 WP 1999 1 29 9900229977 1 19990120 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9341 47390 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTER IES IN POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999012900589 19990129 00589 WP 1999 1 29 9900241226 1 19990118 A 3260 SENSOR DOUG DC10 DC1030 3023501 WP RT MLG FAILED A NWAA O OTHER N FALSE WARNING LD LANDING 1 GL 01 226NW 46583 ON APPROACH TO GUM WHEN GEAR WAS LOWERED, THE RIGHT MAIN GEAR INDICATED UNSAFE ON BOTH THE PILOT'S AND SECOND OFFICER'S PANELS. TRIED MANUAL EXTENSION, INDICATION REMAINED UNSAFE. ACCOMPLISHED LOW ALTITUDE FLY-BY. DECLARED AN EMERGENCY A ND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN LANDING GEAR DOWNLOCK PROXIMITY SENSOR AND TARGET. ALSO REPLACED T HE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR AND PROXIMITY SENSOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999012900590 19990129 00590 SO 1999 1 29 COMA9910020 1 19990124 A 3230 19748 BUSHING ERAM 2094500102 EMB 120 EMB120RT SO LT MLG OUT OF POSITION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 179CA 581 120179 WHILE PERFORMING LANDING GEAR FREE-FALL CHECK, THE LEFT MAIN LANDING GEAR WOULD NOT GO TO THE LOCKED POSITION WITHOUT EX CEEDING THE MAX PULL LIMITS. FURTHER INVESTIGATION REVEALED THE OUTBOARD BUSHING FOR THE MAIN DRAG AND LOCKING STRUT HI NGE PIN TO HAVE MIGRATED FROM THE BORE APPROX .50MM. THE BUSHING APPEARS TO HAVE CAUSED THE SHIMS TO SHIFT AND LIMIT TH E DRAG AND LOCKING STRUST MOVEMENT DURING FREE-FALL. REMOVED DRAG AND LOCKING STRUT AND INSTALLED SERVICEABLE DRAG AND LOCKING STRUT IN ACCORDANCE WITH EMB MM CHAPTER 32. 2 L 7 2 4T RT A31SO 1999012900591 19990129 00591 SO 1999 1 29 COMA9910021 1 19990123 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5A BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 243CA 212 EMERGENCY EXIT SIGN AT 5A IS BROKEN. REPLACED EXIT SIGN AT 5A. 2 L 7 2 4T RT A31SO 1999012900592 19990129 00592 SO 1999 1 29 COMA9910022 1 19990123 A 5270 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT SECURED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 256CA 245 DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. SECURED FUEL SERVICE DOOR FASTENER. 2 L 7 2 4T RT A31SO 1999012900593 19990129 00593 SO 1999 1 29 COMA9910023 1 19990123 A 2752 3430001003 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 269CA 3975 263 WHEN SELECTING FLAPS TO 45 DEGREES, THE FLAP DISAGREE CAUTION ACTIVATED. REPLACED THE EIGHT OUTBOARD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1999012900594 19990129 00594 SO 1999 1 29 COMA9910024 1 19990124 A 3260 CONNECTOR EMB 120 EMB120RT SO RT MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 179CA 179 DURING CLIMBOUT FROM MCO WITH GEAR SELECTED UP, RT GEAR RED LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD. REINSTA LLED RT GEAR A AND B PROXIMITY SENSOR CONNECTOR. 2 L 7 2 4T RT A31SO 1999012900595 19990129 00595 EA 1999 1 29 COMA9960043 1 19990125 A 5210 LOCK CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 962CA 7123 AFTER TAKEOFF FROM YYZ, THE CABIN DOOR LATCH CAUTION MESSAGE ACTIVATED. AIRCRAFT RETURNED TO THE FIELD. REMOVED HYDRAU LIC LOCK FROM HANDLE ASSEMBLY. 2 L 7 2 4F RT A21EA 1999012900596 19990129 00596 EA 1999 1 29 COMA9960044 1 19990124 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 938CA 2479 7046 FLAP FAIL CAUTION AFTER TAKEOFF FROM CHA. AIRCRAFT RETURNED TO THE FIELD. FERRIED AIRCRAFT TO CVG FOR COMPLIANCE OF AD 98-20-01 (FLAP SYSTEM WOULD NOT RESET). REPLACED THE LT BPSU AND FECU. 2 L 7 2 4F RT A21EA 1999012900597 19990129 00597 EA 1999 1 29 COMA9960045 1 19990124 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 EA CARGO DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 989CA 7215 DURING CLIMBOUT OF CVG, CARGO DOOR CAUTION WARNING ACTIVATED. AIRCRAFT RETURNED TO THE FIELD. PERFORMED OPERATIONAL CH ECK FOR THE CARGO DOOR, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999012900598 19990129 00598 EA 1999 1 29 COMA9960046 1 19990124 A 2751 CAUTION LIGHT CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 759CA 7279 DURING DESCENT INTO DSM, FLAP FAIL CAUTION ACTIVATED. COMPLIED WITH AD 98-20-01 PARAGRAPH B, 1, 2, 3 A, B, C, E, FLAP S YSTEM RESET SUCCESSFULLY. 2 L 7 2 4F RT A21EA 1999012900599 19990129 00599 EA 1999 1 29 COMA9960047 1 19990123 A 3230 7179015 CONTROL BOX CNDAIR CL600 CL6002B19 EA LANDING GEAR FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 759CA 874 7279 DURING CLIMBOUT FROM DSM, THE LANDING GEAR WOULD NOT RETRACT, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE LANDING GEAR CONTROL BOX. 2 L 7 2 4F RT A21EA 1999012900600 19990129 00600 EA 1999 1 29 COMA9960048 1 19990123 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 914CA 7012 LAST SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. RECONNECTED THE CONNECTOR TO LIGHTING STRIP. 2 L 7 2 4F RT A21EA 1999012900601 19990129 00601 NM 1999 1 29 UPS99228530 1 19990125 A 5522 652564054 SKIN BOEING 727 72725C 138400H NM RT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE-C ,CORROSION RT ELEVATOR AROUND BASE OF O/B STATIC WICK. REPLACED SKIN PER SRM 51-30-2 AND SRM 55-20-3. 2 L 7 3 4F A3WE 1999012900602 19990129 00602 NM 1999 1 29 UPS99228531 1 19990122 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STRINGER BS 460 STR 21R WL 175. REMOVED CORRODED PORTION OF STRINGE R, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-10-3. 2 L 7 3 4F A3WE 1999012900603 19990129 00603 NM 1999 1 29 UPS99228532 1 19990126 A 3350 1000679 LIGHT BOEING 727 72762C 138402C NM COCKPIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE-N/A, REPEAT WRITE UP WITH EMERGENCY EXIT SWITCH IN THE ARMED POSITION, THE EMERGENCY EXIT LIGHT IN THE C OCKPIT IS ON. EMERGENCY EXIT LIGHT BY FWD ENTRY DOOR IS OFF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AS PER MM 33-50-01. OPS CK'D GOOD. (P/N F 10-0067-9) (S/N UP 18500) ON, (20246) OFF. 2 L 7 3 4F A3WE 1999012900604 19990129 00604 NM 1999 1 29 UPS99228533 1 19990122 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-S, CORROSION BEYOND LIMITS FS 1080 STR 17R EXTERNAL FUSELAGE SKIN. REPAIRED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1999012900605 19990129 00605 NM 1999 1 29 UPS99228534 1 19990124 A 3350 SWITCH BOEING 727 72731C 1384011 NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-N/A, EMERGENCY LIGHT COMES ON WHEN SWITCHED TO OFF POSITION AND POWER TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTS ON/OFF ARM SW. EMERGENCY LIGHTS CK GOOD IAW WDM 33-51-01. 2 L 7 3 4F A3WE 1999012900673 19990129 00673 WP 1999 1 29 ABXA9900024 1 19990108 A 5313 27779225 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATIONS 965 AND 980. REPLACED LONGERON 17 RIGHT SECTION IAW DC9 SR M 53-02. 2 L 7 2 4F A6WE 1999012900674 19990129 00674 WP 1999 1 29 ABXA9900025 1 19990107 A 5312 49125391 BULKHEAD FITTING DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND LEFT PYLON BULKHEAD AT STATION 965, LOWER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 5 1-30-01. 2 L 7 2 4F A6WE 1999012900675 19990129 00675 WP 1999 1 29 ABXA9900026 1 19990107 A 5312 49125401 BULKHEAD FITTING DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND LEFT PYLON BULKHEAD, LOWER FORWARD, SUPPORT FITTING AT STATION 965 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999012900676 19990129 00676 WP 1999 1 29 ABXA9900027 1 19990108 A 5313 27779225 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 980. REPLACED LONGERON SECTION IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999012900677 19990129 00677 WP 1999 1 29 ABXA9900028 1 19990111 A 5753 99575811 SKIN DOUG DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND CORROSION ON UPPER SURFACE OF LEFT FLAP AFT OF MOVEABLE VANE. REPLACED UPPER SKIN ON INBOARD FLAP TRAILING EDGE IAW DC9 SRM 51-30-01. 2 L 7 2 4F A6WE 1999012900678 19990129 00678 WP 1999 1 29 ABXA9900029 1 19990107 A 5313 27779224 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND LONGERON 3 LEFT CRACKED AT STATION 160. SPLICED IN NEW SECTION OF LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999012900679 19990129 00679 WP 1999 1 29 ABXA9900030 1 19990112 A 5312 5910130273 BULKHEAD WEB DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED. REPAIRED WEB CRACK IAW ABX REA D953-26127MR. 2 L 7 2 4F A6WE 1999012900680 19990129 00680 WP 1999 1 29 ABXA9900031 1 19990111 A 5510 5912481 FITTING DOUG DOUG DC9 DC932 3022066 WP HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND CRACKED FITTING ON HORIZONTAL STABILIZER CENTER SECTION AT NUT CHANNEL. REPLACED FITTING IAW DC9 SRM 51-30-01. 2 L 7 2 4F A6WE 1999012900681 19990129 00681 WP 1999 1 29 ABXA9900032 1 19990108 A 2760 3923254503 SUPPORT DOUG DOUG DC9 DC932 3022066 WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND LEFT INBOARD SPOILER TORQUE TUBE INBOARD SUPPORT CRACKED. REPLACED SUPPORT IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999012900682 19990129 00682 WP 1999 1 29 ABXA9900033 1 19990109 A 5320 995823870 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR TIE AT STATION 980 CRACKED ABOVE LONGERON 16 RIGHT. REPLACED SHEAR TIE IAW D C9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999012900683 19990129 00683 WP 1999 1 29 ABXA9900034 1 19990109 A 5320 995823869 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR TIE AT STATION 980 CRACKED AT LONGERON 15 LEFT. REPLACED SHEAR TIE IAW DC9 S RM 51-30-2. 2 L 7 2 4F A6WE 1999012900684 19990129 00684 GL 1999 1 29 DHL99801001 2 19990121 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL NR 4 FAILED A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 801DH 46033 693399 EN ROUTE APPROXIMATELY 90 MILES NORTH OF ICT, NR 4 ENGINE WAS SHUT DOWN DUE TO LOW OIL PRESSURE AND LOW QUANTITY. LANDE D AT CVG WITHOUT INCIDENT. REMOVED AND REPLACED ENGINE PER MM 71-00-01 THROUGH 71-11-32. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999012900716 19990129 00716 EU 1999 1 29 R7MA0000562 1 19990111 A 6210 709013001105 TIP CAP AGUSTA A109 A109K2 0260502 EU M/R BLADE SEPARATED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 1489 A50690 10018 MAIN ROTOR BLADE TIP CAP TRAILNG EDGE SEPARATING. (X) 1 G 7 2 3U RT H7EU 1999012900753 19990129 00753 NM 1999 1 29 99ZZZM37 1 19990103 A 3350 900835A BATTERY PACK BOEING 727 727231 1384079 NM RIGHT OVERWING DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 808MA 4379 21988 ON PREFLIGHT, TRANSIT FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHT WILL NOT TURN OFF. REPLACED BATTERY PACK, OPS CHECK NORMAL IAW 33-50-00. (M) 2 L 7 3 4F A3WE 1999012900815 19990129 00815 SO 1999 1 29 C2XA99IA002 1 19990105 A 3350 3071BPE BULB EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900826 19990129 00826 WP 1999 1 29 ARWA990102 1 19990105 A 3231 MECHANISM DOUG DC8 DC862F 3021972 WP MLG DOOR OUT OF ADJUST A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 791AL 46150 MIA - FLT 941 - AIR TURNBACK - AFTER DEPARTURE GEAR UPLATCH CHECK RESULTED IN 'DOORS NOT LATCHED' LIGHT ILLUMINATED. PE RFORMED ABNORMAL CHECKLIST WITH SAME RESULTS. THE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION. LETTER ON DURING DESCENT THE 'GEAR NOT LATCHED' LIGHT ALSO ILLUMINATED. PERFORMED ADJUSTMENT OF GEAR DOOR FOLLOWUP MECHANISM. OPS CHECK ED NORMAL IAW DC-8 MM 32-31-5. (M) 2 L 7 4 4F 4A25 1999012900840 19990129 00840 WP 1999 1 29 ORJA9905 1 19990105 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 17-20 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 878RA 53184 ORD - EMERGENCY LIGHTS ROWS 17-20 INOPERATIVE. FERRIED AIRCRAFT FROM ORD TO RNO. REMOVED AND REPLACED AFT OVER THE EXI T EMERGENCY BATTERY PACK. AIRCRAFT INSPECTED FOR FERRY FLIGHTS AND NO CONDITIONS EXIST THAT WOLD MAKE THE A/C UNSAFE. ( M) 2 L 7 2 4F RT A6WE 1999012900841 19990129 00841 WP 1999 1 29 ORJA9906 1 19990105 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 RNO - POWER PACK INOPERATIVE FOR EMERGENCY LIGHTS AT LOWER EMERGENCY EXIT DOOR MID CABIN. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012900844 19990129 00844 WP 1999 1 29 ORJA9901 1 19990102 A 3350 EM1267 BATTERY DOUG DC9 DC987 3022087 WP ROWS 16-20 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT RENO, OVERHEAD EMERGENCY LIGHTS INOPERABLE FROM ROW 16 TO ROW 20. REMOVED AND REPLACED BATTERIES. (M) 2 L 7 2 4F RT A6WE 1999012900845 19990129 00845 WP 1999 1 29 ORJA9902 1 19990101 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 15-18 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO, EMERGENCY LIGHTS 15-18 STAY ON. REMOVED AND REPLACED SEAT TRACK BATTERY PACK, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999012900846 19990129 00846 WP 1999 1 29 HALA9900002 1 19990102 A 2612 CONNECTOR DOUG DC9 DC951 3022051 WP NR 2 ENGINE FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 709HA 47764 FLT NR 70 - HNL - NR 2 ENGINE 'B' LOOP INOPERATIVE , 'A' TEST OK. REPLACED 'B' LOOP CONNECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012900847 19990129 00847 WP 1999 1 29 HALA9900003 1 19990104 A 3350 BATTERY DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 152AA 46707 FLT 24 - HNL - MID EMERGENCY LIGHT PACK SHOWS INOPERATIVE ON EMERGENCY LIGHT BITE TEST. REPLACED BATTERY PACK AT 2-1 DO OR. OPS CHECK GOOD, RESET FAULT BOX. (M) 2 L 7 3 4F A22WE 1999012900849 19990129 00849 WP 1999 1 29 ASAA9980001 1 19990101 A 3350 60030451 POWER SUPPLY MIDLANDROSS DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS FLASH WHEN THE AUXILIARY HYDRAULIC PUMP IS S WITCHED ON. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900850 19990129 00850 WP 1999 1 29 ASAA9980002 1 19990103 A 3350 60030451 POWER SUPPLY MIDLANDROSS DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 12 ILLUMINATE WHEN ELECTRIC POWER IS TURNED OFF. R EPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900851 19990129 00851 WP 1999 1 29 ASAA9980003 1 19990103 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 11 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 9 TO 13 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AT ROW 11 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900871 19990129 00871 WP 1999 1 29 ASAA9980007 1 19990105 A 3350 014597001 BATTERY MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900872 19990129 00872 WP 1999 1 29 ASAA9980004 1 19990104 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 3 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - PRIOR TO DEPARTURE OF FLIGHT 612, CREW REPORTED THE EMERGENCY FLOOR TRACK RED LIGHTS WERE INOPERATIVE. RECONNECTE D WIRING IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900873 19990129 00873 WP 1999 1 29 99ZZZM49 1 19990102 A 3350 CIRCUIT BREAKER DOUG DC10 DC1010 3022110 WP COCKPIT TRIPPED A RYNA O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 CE 07 572SC 46977 FLT 0102 - LAX - MAINTENANCE FOUND ALL EMERGENCY LIGHTS ARE 'ON' WITH EMERGENCY LEFT SWITCH IN EITHER 'ARM' OR 'ON'. RE SET EMERGENCY LIGHT CIRCUIT BREAKER, OPERATIONALLY CHECKS GOOD. (M) 2 L 7 3 4F A22WE 1999012900874 19990129 00874 WP 1999 1 29 99ZZZM50 1 19990102 A 3350 110049 BATTERY CHARGER DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 572SC 46977 FLT 0102 - LAX - MAINTENANCE FOUND RIGHT SIDE EMERGENCY FLOOR LIGHTS IN SECTION 'C' INOPERATIVE. REMOVED AND REPLACED E MERGENCY LIGHTING BATTERY CHARGER. (M) 2 L 7 3 4F A22WE 1999012900879 19990129 00879 NM 1999 1 29 TSAA9933001 1 19990102 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED BATTERY PACK IN POSITION 3 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900880 19990129 00880 NM 1999 1 29 TSAA9933002 1 19990101 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED EMERGENCY FLOOR LIGHT BATTERY PACK FOR POSITIONS 1 AND 2 DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999012900881 19990129 00881 NM 1999 1 29 TSAA9933003 1 19990101 A 3350 9221009 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED FORWARD PASSENGER DOOR EXIT IDENTIFIER BATTERY PACK FOR BEING TOO LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 1999012900882 19990129 00882 NM 1999 1 29 TSAA9933004 1 19990101 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F A16WE 1999012900883 19990129 00883 NM 1999 1 29 TSAA9933005 1 19990102 A 3350 1619 LAMP BOEING 737 737230 NM CABIN FAILED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 RELAMPED AFT ENTRY DOOR SLIDE LIGHT DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900884 19990129 00884 NM 1999 1 29 TSAA9933017 1 19990108 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 1 SEAT EMERGENCY ASSEMBLY BATTERY DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900885 19990129 00885 NM 1999 1 29 TSAA9933015 1 19990108 A 3350 86210026 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 1 POSITION BATTERY PACK FOR FLOOR PROXIMITY LIGHT ASSY DUE INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900886 19990129 00886 NM 1999 1 29 TSAA9933007 1 19990106 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900887 19990129 00887 NM 1999 1 29 TSAA9933008 1 19990106 A 3350 6013211 BATTERY BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED AFT EMERGENCY SLIDE BATTERY POWR SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999012900888 19990129 00888 NM 1999 1 29 TSAA9933009 1 19990106 A 3350 LIGHT BOEING 737 737230 NM SERVICE DOORWAY INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED AFT SERVICE DOOR EXIT IDENTIFIER LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900889 19990129 00889 NM 1999 1 29 TSAA9933010 1 19990106 A 3350 86210066 BATTERY BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 2 AND NR 4 EMERGENCY PATH LIGHTING BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4U RT A16WE 1999012900890 19990129 00890 NM 1999 1 29 TSAA9933011 1 19990106 A 3350 86210066 BATTERY BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 5 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY ASSEMBLY. DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1999012900891 19990129 00891 NM 1999 1 29 TSAA9933012 1 19990107 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED BATTERY PACK FOR FLOOR PROX AISLE LIGHT NR 2 AND NR 3 DUE AS WELL LIGHT INOPERATIVE. OPS CHECK OK. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900892 19990129 00892 NM 1999 1 29 TSAA9933013 1 19990107 A 3350 8731002511 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD SERVICE DOOR EMERGENCY IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT A16WE 1999012900960 19990129 00960 WP 1999 1 29 TWAA9901601 1 19990121 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, LONGERON 5R WAS CRACKED AT STA 737. CUT OUT DAMAGED SECTION OF LONGERON. INSTALLED NEW SECTI ON OF LONGERON AND SPLICES PER DRAWING SRO9530128 AND SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1999012900961 19990129 00961 WP 1999 1 29 TWAA9901602 1 19990118 A 5530 ANGLE DOUG DC9 DC983 3022083 WP BS 1426 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FUSELAGE TO VERTICAL STABILIZER TIE ANGLE CRACKED APPROX 1.5 INCH LONG AT STA 1426 BETWE EN LONGERON 1L AND 2L, INSIDE LOWER STABILIZER. REPLACED ANGLE PART NR 5912188-35 PER STANDARD PROCESSES MANUAL 6-70-01 . 2 L 7 2 4F RT A6WE 1999012900962 19990129 00962 NM 1999 1 29 TWAA9901603 1 19990120 A 5754 SKIN BOEING 767 767231 1385131 NM NR 1 LE SLAT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DURING CHECK-C MAINT, ON LT WING THE NR 1 LE SLAT LOWER SURFACE, O/B END HAD HOLE. INSTALLED 2 INCH BY 2 IN METAL TO ME TAL HOT BOND PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1999012900963 19990129 00963 WP 1999 1 29 TWAA9901604 1 19990119 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 743 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, THE CABIN FLOOR MEMBRANE WAS CORRODED AT STA 743 RT SIDE. REMOVED CORROSION PER STANDARD PROC EDURES MANUAL 6-80-01. FABRICATED AND INSTALLED DOUBLER PER SPM 6-70-01, PG 1. 2 L 7 2 4F RT A6WE 1999012900964 19990129 00964 WP 1999 1 29 TWAA9901605 1 19990119 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT FLOOR SUPPORT ANGLE ON TOP OF FORMER STA 1212 RBL CORRODED. REMOVED AND REINSTALLED ANGLE PER TWA STD PROCESSES 6-70-01. 2 L 7 2 4F RT A6WE 1999012900965 19990129 00965 WP 1999 1 29 TWAA9901606 1 19990118 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURNG OP 16 MAINT CHECK, FOUND IN CABIN, CORROSION IN CHAIR TRACK AT RBL 44 IN, STA 237, 262 TO 264, AND STA 275. REPLA CED TRACK RBL 44 FROM STA 237 TO 275 PER SRM 53-005, PG 10G. 2 L 7 2 4F RT A6WE 1999012900966 19990129 00966 NM 1999 1 29 TWAA9901701 1 19990119 A 3350 582243 POWER SUPPLY BOEING 767 767231 1385131 NM ROW 24 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 602TW 22565 FOUND FLOOR EGRESS LIGHTS OUT ON LT SIDE OF CABIN FROM ROW 24 TO ROW 33. REPLACED POWER SUPPLY. CHECK-C 11-17-98 MCI. 2 L 7 2 4F RT A1NM 1999012900967 19990129 00967 WP 1999 1 29 TWAA9901702 1 19990119 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 927 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR MEMBRANE AT STA 927 TO 946, 58.8 LBL. REMOVED 9 INCH BY 13 IN FLOOR MEMBRANE AND INSTALLED NEW 2024-T3 0.040 DOUBLER EXTENDING TWO FASTENER ROWS BEYOND CUT LINE PER SRM 53-01, FIG H, SHEET 3. 2 L 7 2 4F RT A6WE 1999012900968 19990129 00968 WP 1999 1 29 TWAA9901703 1 19990119 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 1271-1307 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE REPAIR DOUBLER CRACKED IN 2 PLACES AT STA 1271 TO 1307. REMOVED OLD DOUB LER AND INSTALLED NEW ONE PER SRM 53-05, PG 347 TO 351. USED AD FASTENERS PER SRM 6-30-07 PAGE 1 AND 2. 2 L 7 2 4F RT A6WE 1999012900969 19990129 00969 WP 1999 1 29 TWAA9901704 1 19990121 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1156 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND IN CABIN, WEB CRACKED AND CORRODED AT STA 1156 UNDER FLOOR. REMOVED CORROSION PER SRM 5 1-10-3, PARA 31 TO 42. REPAIRED WEB PER 53-01, PG 9 FIG 2 SHEET 3. 2 L 7 2 4F RT A6WE 1999012900970 19990129 00970 WP 1999 1 29 TWAA9901705 1 19990121 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 1156 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOORBEAM CAP CORRODED AT STA 1156 BETWEEN TRACK LBL 22 AND LBL 42. FABRICATED NEW PART FROM 7075 T6. INSTALLED PER TWA STD PROCESSES MANUAL 6-70-01. 2 L 7 2 4F RT A6WE 1999012900971 19990129 00971 WP 1999 1 29 TWAA9901706 1 19990121 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 1219 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 1219 APPROXIMATELY RBL 4 IN UNDERNEATH UPPER PART OF FORMER RING. REMO VED CORROSION PER SRM 6-80-01, PG 1 TO 3. REINSTALLED FORMER FOOT, AFTER CLEANING CORROSION, PER SPM 6-70-01, PG 3 AND USED AD FASTENERS. 2 L 7 2 4F RT A6WE 1999012900972 19990129 00972 WP 1999 1 29 TWAA9901707 1 19990123 A 5320 FITTING DOUG DC9 DC983 3022083 WP BS 1193 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FLOOR FITTING CORRODED AT STA 1193 AT CUSP LINE, RT SIDE OF AFT CARGO BIN. REMOVED LIGH T SURFACE CORROSION USING RUBBER BACK SANDING DISC AND ALUMINUM OXIDE DISC, PER SPM 6-80-01. REINSTALLED ORIGINAL BOLTS AND NUTS IN FITTING. 2 L 7 2 4F RT A6WE 1999012900973 19990129 00973 WP 1999 1 29 TWAA9901708 1 19990122 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1099 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1099, 44 IN LBL. REMOVED CORROSION PER TWA SPM 6-80-01. INSTALLED NEW TRACK PER SRM 53-05, FIG 4F. 2 L 7 2 4F RT A6WE 1999012900974 19990129 00974 WP 1999 1 29 TWAA9901709 1 19990120 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1203 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9304C 49530 DURING CHECK-C MAINT, FOUND AFT CARGO BIN DOOR JAM ATTACH ANGLE WITH CORROSION AT STA RW 1203, INTERIOR STRUCTURE OF DOO R JAM LIP. REMOVED ANGLE AND INSTALLED NEW ANGLE PER DOUGLAS PRINT 5930483. 2 L 7 2 4F RT A6WE 1999012900975 19990129 00975 WP 1999 1 29 TWAA9901710 1 19990120 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1155 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9304C 49530 DURING CHECK-C MAINT, FOUND DOOR JAM AT FUSELAGE STA 1155 ATTACH ANGLE WAS CORRODED, AFT CARGO COMPT. REMOVED ANGLE AND INSTALLED NEW ANGLE PER DOUGLAS PRINT 5930483. 2 L 7 2 4F RT A6WE 1999012900976 19990129 00976 NM 1999 1 29 TWAA9901711 1 19990120 A 5753 SKIN BOEING 767 767231 1385131 NM RT TE FLAP DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DURING CHECK-C MAINT, THE RT WING O/B TRAILING EDGE FLAP, BOTTOM SIDE HAD A 4.25 INCH BY 4.5 INCH REPAIR PULLED LOOSE, 1 4 INCHES FROM I/B END OF FLAP 30 INCHES FROM TRAILING EDGE. REPAIRED TRAILING EDGE FLAP WITH METAL TO METAL 5.5 INCH CI RCULAR PATCH. HOT BOND PER SRM 51-70-10, FIG 6 PAGE 22. SEALED EDGES AND PAINTED. 2 L 7 2 4F RT A1NM 1999012900977 19990129 00977 NM 1999 1 29 K3HA990004 1 19990122 A 3350 3071BPEGPL LENS BOEING 727 727225 1384077 NM PAX DOOR MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 RED FLOOR LIGHT AT FORWARD ENTRY DOOR MISSING. RELAMPED REPLACED RED LENS TEST, REF MM 33-50-01. 2 L 7 3 4F A3WE 1999012900978 19990129 00978 WP 1999 1 29 CALA9900068 1 19990122 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT LT FORWARD ENTRY STA 160, LBL 54. THE FASTENERS WERE REMOVED FROM FLOO R SUPPORT ANGLE IAW SRM 51-30-2. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-3, AND 53-02-00. 2 L 7 2 4F A6WE 1999012900979 19990129 00979 WP 1999 1 29 CALA9900069 1 19990122 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 260 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 260, LONGERON 19R. REPAIRED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1999012900980 19990129 00980 WP 1999 1 29 CALA9900070 1 19990123 A 5350 HANDLE DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 72822 49482 THE TAIL CONE EXTERIOR RELEASE HANDLE FAILED PULL TEST. THE HANDLE FAILED LOW AT 18 POUNDS. THE TAIL CONE EXTERIOR REL EASE HANDLE WAS RIGGED AND FELL WITHIN TEST LIMITS IAW MM 53-53-00. 2 L 7 2 4F A6WE 1999012900981 19990129 00981 NM 1999 1 29 CALA9900071 1 19990122 A 5314 KEEL BEAM BOEING 737 7373T0 1384582 NM BS 727 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND KEEL BEAM CORRODED AT STA 727, STRINGER 27L. A REPAIR WAS INSTALLED IAW ECRA 5310-03814. 2 L 7 2 4F RT A16WE 1999012900982 19990129 00982 NM 1999 1 29 CALA9900072 1 19990123 A 3350 20131A BATTERY PACK RADIANT BOEING 737 7373T0 1384582 NM BS 629 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59302 23353 THE BATTERY CHARGER ASSEMBLY AND BATTERY FAILED SYSTEM FUNCTIONAL CHECK, PACK M1135, STA 629R (28 VDC PRESENT AT PIN 2 O F PLUG POWER SUPPLY). REMOVED AND REPLACED TWO BATTERY PACKS. 2 L 7 2 4F RT A16WE 1999012900983 19990129 00983 NM 1999 1 29 CALA9900073 1 19990124 A 5330 SKIN BOEING 737 7373T0 1384582 NM CARGO DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN FUSELAGE SKIN AT FORWARD LOWER CORNER OF C-2 AFT CARGO DOOR CUTOUT. RE PAIRED IAW ECRA 5330-02763. 2 L 7 2 4F RT A16WE 1999012900984 19990129 00984 WP 1999 1 29 CALA9900074 1 19990123 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN DOOR SKIN AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-05, FIGURE 32. 2 L 7 2 4F A6WE 1999012900985 19990129 00985 NM 1999 1 29 CALA9900075 1 19990125 A 5320 CREASE BEAM BOEING 757 757224 1384958 NM BS 1630 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 INSPECTION FOUND CABIN FLOOR EDGE CREASE BEAM CORRODED AT BS 1630 RBL 64. A BEAM STRAP AND FILLER PLATE WERE INSTALLED IAW SRM 53-60-13. 2 L 7 2 4F RT A2NM 1999012900986 19990129 00986 NM 1999 1 29 CALA9900076 1 19990126 A 5320 BEAM BOEING 757 757224 1384958 NM BS 1147 FRETTING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 INSPECTION FOUND BEAM CHORD FRETTING ON FIXED UPPER T/E STRUCTURE, RT SIDE, STA 1147. A REPAIR WAS INSTALLED IAW SRM 53 -00-71 AND ECRA 5352-01011. 2 L 7 2 4F RT A2NM 1999012900987 19990129 00987 NM 1999 1 29 CALA9900077 1 19990126 A 5320 BEAM BOEING 757 757224 1384958 NM BS 1147 FRETTING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 INSPECTION BEAM OUTER CHORD FRETTING ON FIXED T/E STRUCTURE ON LT SIDE AT STA 1147. A REPAIR WAS INSTALLED IAW SRM 53-0 0-71 AND ECRA 5352-01011. 2 L 7 2 4F RT A2NM 1999012900988 19990129 00988 NM 1999 1 29 CALA9900078 1 19990126 A 5230 SKIN BOEING 757 757224 1384958 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 INSPECTION FOUND A .25 INCH CRACK ON EDGE OF AFT CARGO DOOR SKIN AT AFT CORNER. THE AREA WAS REPAIRED IAW SRM 52-30-01 AND ECRA 5230-01438. 2 L 7 2 4F RT A2NM 1999012900989 19990129 00989 NM 1999 1 29 CALA9900079 1 19990125 A 5730 SKIN BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 INSPECTION FOUND TWO CRACKS IN LT WING FIXED LEADING EDGE SKIN AT OSS 421. THE CRACKS WERE 5 AND 10 INCHES LONG. THE S KIN WAS REPAIRED IAW EA 5731-01010. 2 L 7 2 4F RT A2NM 1999012900990 19990129 00990 WP 1999 1 29 CALA9900080 1 19990126 A 5753 5910043510 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND RT WING FLAP O/B FIXED VANE I/B UPPER END DELAMINATED WITH CORROSION AT TOP AND BOTTOM AREAS. THE RT O /B VANE WAS REMOVED AND REPLACED IAW MM 27-51-3. 2 L 7 2 4F A6WE 1999012900991 19990129 00991 WP 1999 1 29 CALA9900081 1 19990126 A 5753 5910041503 VANE DOUG DC9 DC932 3022066 WP LT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND LT WING FLAP I/B FIXED VANE DELAMINATED ON LOWER SURFACE. THE LEFT I/B VANE WAS REMOVED AND REPLACED I AW MM 27-51-3. 2 L 7 2 4F A6WE 1999012900992 19990129 00992 WP 1999 1 29 CALA9900082 1 19990126 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 164 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND A 1.875 INCH CRACK IN RT WING LOWER SPAR CAP, UNDER THE I/B FLAP HINGE FITTING AT STA XRS 164.0. A REP AIR WAS INSTALLED IAW DOUGLAS DRAWING NR 506271. 2 L 7 2 4F A6WE 1999012900993 19990129 00993 NM 1999 1 29 CALA9900083 1 19990126 A 5330 SKIN BOEING 757 757224 1384958 NM BS 540 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 THE FUSELAGE SKIN WAS DENTED AT STA 540, STRINGER 16L. A FLUSH REPAIR AND STRINGER SECTION SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03, 53-30-05, AND ECRA 5331-01039. 2 L 7 2 4F RT A2NM 1999012900994 19990129 00994 WP 1999 1 29 CALA9900084 1 19990127 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR BEAM END FITTING AT AFT SIDE OF DOOR. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5, PAGE 4. 2 L 7 2 4F A6WE 1999012900995 19990129 00995 NM 1999 1 29 UPS99228537 1 19990125 A 5320 INTERCOSTAL BOEING 727 72725C 138400H NM BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-221-01-01-01) ON INTERCOSTAL AT BS 300, LBL 13, WL 208. FABRICATED AND REPLACED INTE RCOSTAL BS 294.5 TO BS 312 PER SRM 51-10-2 AND 51-20-01 AND 51-30-2. 2 L 7 3 4F A3WE 1999012900996 19990129 00996 NM 1999 1 29 UPS99228538 1 19990113 A 5522 652563973 SKIN BOEING 727 72725C 138400H NM LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE-C, CORROSION (C55-300-10.00-01) ON LT ELEVATOR AROUND I/B STATIC WICK BASE. REMOVED CORROSION OUT OF LIMITS, REPLACED SKIN PANEL. ALL WORK DONE PER SRM 55-20-1, 55-20-2 AND MM 23-61-00. 2 L 7 3 4F A3WE 1999012900997 19990129 00997 WP 1999 1 29 UPS99828535 1 19990103 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, FS 55 FRAME IS CRACKED AT LONG 24R. CUT OUT DAMAGED SECTION AND REPAIRED FRAME IAW SR DWG 0853008 AN D SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999012900998 19990129 00998 WP 1999 1 29 UPS99828536 1 19990112 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 8-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, INTERNAL DOUBLER FROM FS 8 TO 70, LONG 29L TO 33L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AN D REPLACED DOUBLER IAW SRM 51-1-21 AND 53-3-1. 2 L 7 4 4F RT 4A25 1999012901000 19990129 01000 WP 1999 1 29 UPS99828540 1 19990114 A 5320 4643295501 SPACER DOUG DC8 DC871F 302199D WP BS 780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, AIRCRAFT STRUCTURE UNDER VERTICAL FITTING AT FS 780 AND RBL 55 IS BADLY CORRODED. REMOVED AND REPLAC ED SHIM PLATE IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012901001 19990129 01001 WP 1999 1 29 UPS99828541 1 19990126 A 3350 BATTERY DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK OPS GOOD PER 33-50-00. 2 L 7 4 4F RT 4A25 1999012901002 19990129 01002 EU 1999 1 29 QXEA9900100 1 19990125 A 3320 SOCKET FOKKER F28 F28MK4000 4990810 EU CABIN MELTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 475AU 11222 SEA- ROW 2AB NO SMOKING SIGN IS INOP, WITH SMOKE COMING FROM THE PASSENGER SERVICE UNIT. MAINTENANCE INSPECTED AND FOUN D THE BULB SOCKET MELTED. REMOVED SOCKET AND PLACED ON MEL. 2 L 7 2 4F RT A20EU 1999012901003 19990129 01003 NM 1999 1 29 99UAL900031 1 19990115 A 3412 PAA102LA2AG TAT PROBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 570UA 26678 RETURNED TO FIELD DUE TO TAT PROBE EICAS MESSAGE. *S/D* TAT PROBE FAILED. REPLACED TAT PROBE PER APPLICABLE MM. 2 L 7 2 4F 4 F RT A2NM E17NE 1999012901004 19990129 01004 NM 1999 1 29 99UAL900032 1 19990115 A 3520 214C401110 SWITCH BOEING 214C401110 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA O OTHER G MULTIPLE FAILURE LD LANDING 1 WP 29 575UA 26689 OXYGEN MASKS DEPLOYED ON TOUCH DOWN. *S/D* RECEPTICLE ON S119 ALTITUDE PRESSURE SWITCH WAS FOUND DETACHED FROM SWITCH BODY. REPLACED S119 AND PERFORMED CALIBRATION CHECK PER MM 35-21-00. 2 L 7 2 4F 4 F RT A2NM E17NE 1999012901005 19990129 01005 NM 1999 1 29 99UAL900035 1 19990116 A 3240 BRAKES BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE MLG MALFUNCTIONED A UALA D RETURN TO BLOCK O OTHER UK UNKNOWN 1 WP 29 984UA 2 21642 EXCESSIVE BRAKE DECAY. *S/D* ACCOMPLISHED PARKING BRAKE SYSTEM TEST PER APPLICABLE MAINTENANCE MANUAL. OPERATIONAL CH ECK OF SYSTEM CHECKED OK. NO FAULTS FOUND. 2 L 7 2 4F 4 F A16WE E2EA 1999012901006 19990129 01006 NM 1999 1 29 99UAL900038 1 19990125 A 3350 POWER SUPPLY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ROW 26 INOP A UALA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 29 601UA 21862 EMERGENCY FLOOR LIGHTING AT RIGHT HAND AISLE FROM SEAT 26 REMAIN ILLUMINATED AFTER AIRCRAFT IS PUSHED BACK. SUSPECT DOO R RIGGING. *S/D* DOOR WARNING SENSORS OUT OF ADJUSTMENT AND SUSPECTED BATTERY POWER SUPPLY CHARGER. ADJUSTED SENSORS AND REPLACED BATTERY POWER SUPPLY, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1999012901007 19990129 01007 NM 1999 1 29 99UAL900039 1 19990118 A 2130 VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 603UA 21864 UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO FIELD. *S/D* OVERBOARD EXHAUST VALVE FAILED. REPLACED OVERBOARD EXHAUST VAL VE. AIRCRAFT PRESSURIZED NORMALLY. NO ADDITIONAL WRITE-UPS FOR EQUIPMENT COOLING OR PRESSURIZATION. 2 L 7 2 4F 4 F RT A1NM E3NE 1999012901008 19990129 01008 NM 1999 1 29 99UAL900040 1 19990118 A 2560 81020401 SENSOR GULTON INDUS 81020401 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1L FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 585UA 26709 DOOR 1L AND 3R ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS INOP. *S/D* REPLACED BOTH PROXIMITY SENSORS AT 3R DOOR AND CLEA NED PROXIMITY SENSORS AT 1L DOOR, OP CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1999012901009 19990129 01009 NM 1999 1 29 99UAL900044 1 19990119 A 2612 1061096316 FIRE DETECTOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE APU MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 29 991UA 21981 APU FIRE WARNING INDICATION. *S/D* FOUND APU FIRE DETECTOR ITEM M334 DEFECTIVE. REPLACED DETECTOR, BOTTLE AND DISCHAR GE DISC. 2 L 7 2 4F 4 F A16WE E2EA 1999012901010 19990129 01010 NM 1999 1 29 99UAL900046 1 19990116 A 4940 36166411 BEARING ALLIED SIGNA 38005501 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE APU STARTER FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 784UA 3169 P1107 26951 P1107 JUST AFTER LEVEL OFF THE RIGHT BACK-UP GENERATOR FAILED. CREW ATTEMPTED TO START APU AND APU FAILED. CREW ELECTED TO R ETURN TO MIA. *S/D* APU FAILED TO LIGHT AT 33,000 FT WITH FAULT LIGHT INDICATION ON 17 JAN, 1999. MIA MAINTENANCE REP ORTED APUC LATCHED FAULTS 49-11200 AND 49-11110. THESE FAULTS WERE FINALLY CLEARED PER FIM MM REF 49-53-804. THE SAME DAY MIA ACP TWO NORMAL APU STARTS. APU WAS REMOVED. FOUND AIR TURBINE STARTER CLUTCH BEARING (P/N 3616641-1) FAILED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999012901011 19990129 01011 NM 1999 1 29 99UAL900047 1 19990120 A 2751 WARNING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLAP SYST ACTIVATED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 575UA 26689 DIVERTED TO PHX UNDER AMBER ALERT DUE TO FLAP/SLAT PROBLEM. *S/D* CHECKS OF THE SYSTEM DID NOT REVEAL A ROOT CAUSE, AN D PROBLEM COULD NOT BE DUPLICATED. SYSTEM OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1999012901012 19990129 01012 NM 1999 1 29 99UAL900050 1 19990121 A 2150 213W31201 DOOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT PACK RAM AIR DAMAGED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 778UA 26940 VIBRATION FELT IN AIRFRAME CLIMBING TO 18,000 FT. VIBRATION DECREASED WHEN NR 2 THROTTLE BROUGHT TO FLIGHT IDLE. ALSO, DECREASED WHEN RIGHT AIR CONDITIONING PACK TURNED OFF. RESIDUAL VIBRATION REMAINED. AIRCRAFT RETURNED TO CDG. *S/D* FOUND RT PACK RAM AIR INLET DOOR ASSY DAMAGED (AFT PANEL OF DOOR). THE ROLLER BRACKETS INSTALLED ON DOOR AND THE LINKA GE BETWEEN DOOR AND TORQUE TUBE ASSY WERE FOUND BROKEN AWAY FROM THE DOOR PANEL. THE ROLLERS WERE FOUND WORN AND BROKEN . REPLACED DOOR ASSY (P/N 213W3120-1) AFT PANEL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999012901013 19990129 01013 NM 1999 1 29 99UAL900051 1 19990121 A 5270 694328314 SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR BENT A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 380UA 24655 AFT CARGO DOOR LIGHT CAME ON. *S/D* SENSOR ACTUATOR WAS BENT. REPLACED SENSOR ACTUATOR, CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999012901014 19990129 01014 NM 1999 1 29 99UAL900052 1 19990122 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 804 DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7442U 21896 LEFTHAND EXTERIOR OVERWING EMERGENCY LIGHTS INOP AT STATION 804 BETWEEN OVERWING DOORS. TROUBLESHOT AND FOUND BATTERY P ACK M654 BAD. REPLACED BATTERY PACK, OP CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1999012901015 19990129 01015 NM 1999 1 29 99UAL900053 1 19990120 A 5210 66109059 COVER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE L1 DOOR LOOSE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7453U 21907 ON CLIMBOUT, A CONTINUOUS LOUD SQUEAL CAME FROM MAIN CABIN DOOR 1L. AIRCRAFT RETURN TO ORD. *S/D * FOUND PASSENGER EN TRANCE DOOR LOWER HINGE COVER LOOSE. STAKED HINGE PIN AND SEALED. REPLACED LOWER HINGE COVER DOOR, OPS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999012901016 19990129 01016 WP 1999 1 29 ABXA9900036 1 19990126 A 5610 5613217507 WINDOW DOUG DC8 DC863 302198A WP LT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 CAPTAIN'S SLIDING WINDOW (EMERG EXIT) WAS HARD TO OPEN. FOUND WINDOW TRIM BINDING. RESECURED TRIM, CLEANED AND LUBRICA TED LINKAGE. 2 L 7 4 4F 4A25 1999012901017 19990129 01017 NM 1999 1 29 MWEA99051 1 19990125 A 5313 27779223 LONGERON DOUG MD88 MD88 3023688 NM BS 1309 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FOUND CRACK ON LONGERON 8 RIGHT AT STATION 1309. MTC FABRICATED AND INSTALLED NEW LONGERON AND SPLICE. 2 L 7 2 4F RT A6WE 1999012901018 19990129 01018 WP 1999 1 29 MWEA99052 1 19990125 A 5532 99184802 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FOUND SMALL FAIRING LIFTING AND RIVETS PULLING THROUGH SKIN ON AFT OUTBOARD CORNER OF RIGHT ELEVATOR. MTC FABRICATED AN D INSTALLED NEW DOUBLER AND SKIN. 2 L 7 2 4F A6WE 1999012901019 19990129 01019 1999 1 29 SWIA971367 4 19990108 A 3425 AHRS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 292SW 120319 TOTAL AHRS FAILURE EHSI, EADI. DIVERTED TO PSP. REPLACED RELAYS K0395, K0397, K0394 AND K0396. TESTED AHRS IAW MM 34- 21-00 AND PERFORMED OPERATIONAL TEST OF 70 PERCENT SWITCHING RELAYS, TEST GOOD. BACK UP BATTERY TEST GOOD IAW MM 24-00- 00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012901020 19990129 01020 SO 1999 1 29 SWIA971368 1 19990110 A 3020 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 227SW 120304 LEFT ENGINE AIR INLET INOP. RETURNED TO SFO. REPLACED BAD LEFT ENGINE DEICE SWITCH. RAN LEFT ENGINE DEICE BOOTS. INF LATE GOOD WITH NO INOP LIGHT. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012901021 19990129 01021 SO 1999 1 29 SWIA971369 1 19990110 A 3010 DEICE LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING ILLUMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 308SW 120326 MIDDLE LEFT WING DEICE LIGHT ILLUMINATED FOLLOWED BY SEVERAL OTHER DEICE LIGHTS. RETURNED TO BFL. REPLACED AIR ON RIGH T ENGINE. PERFORMED OPS CHECK OF DEICE SYSTEM AND OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012901022 19990129 01022 SO 1999 1 29 SWIA971370 1 19990110 A 3020 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 197SW 120186 LEFT ENGINE INLET DEICER INOP. ANNUNCIATION IN FLIGHT AND RETURNED TO SLC. REMOVED AND REPLACED LEFT ENGINE FLOW CONTR OL VALVE IAW EMB 120 MM 30-10-04. OP, CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012901023 19990129 01023 SO 1999 1 29 SWIA971371 1 19990102 A 3010 SWITCH EMB 120 EMB120RT SO PWA 118 PW118A NE LT WING INOP A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 LEFT MIDDLE WING DEICE BOOT INOP. RETURNED TO SFO. INSTALLED SERVICEABLE PRESSURE SWITCH. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012901024 19990129 01024 SO 1999 1 29 SWIA971372 1 19990103 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM FAILED A SWIA K NONE F FLT CONT AFFECTED CR CRUISE 1 NM 07 567SW 120342 ELEVATOR TRIM FREEZES INFLIGHT WITH AND WITHOUT AUTO PILOT. REMOVED AND REPLACED BOTH TRIM TAB ACTUATORS AS PER MM 27-0 0-01. 2 L 7 2 4T 4 T RT A31SO E20NE 1999012901025 19990129 01025 NM 1999 1 29 P5CA9900024 1 19990122 A 5320 STIFFENER BOEING 747 747122 1384872 NM BS 440 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 UPPER DECK VERTICAL STIFFENER AT BS 440L FOUND CRACKED. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901026 19990129 01026 NM 1999 1 29 P5CA9900025 1 19990122 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 2220 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BRACKET AT BS 2220L STR 21 L FOUND CRACKED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901027 19990129 01027 NM 1999 1 29 P5CA9900026 1 19990122 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1520 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BRACKET AT BS 1520 STR 21R FOUND CRACKED. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999012901028 19990129 01028 NM 1999 1 29 P5CA9900027 1 19990122 A 5210 PLATE BOEING 747 747122 1384872 NM L1 DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND AT L1 DOOR ASSY AFT FRAME CENTER GUIDE FITTING BASE PLATE. REPAIRED PER SRM 51-10-01 AND 51-10- 02. 2 L 7 4 4F A20WE 1999012901029 19990129 01029 NM 1999 1 29 P5CA9900028 1 19990122 A 5320 STRAP BOEING 747 747122 1384872 NM BS 620-680 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FWD CARGO COMPARTMENT STA 620 STR 680 LT SLOPE PANEL LOWER SUPPORT STRAP FOUND BROKEN. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901030 19990129 01030 NM 1999 1 29 P5CA9900029 1 19990122 A 5280 STOP BOEING 747 747122 1384872 NM RT MLG DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT WING LANDING GEAR WW DOOR FOUND BROKEN STOP ASSY. REPLACED PER MM 32-12-00. 2 L 7 4 4F A20WE 1999012901031 19990129 01031 NM 1999 1 29 P5CA9900030 1 19990122 A 5400 ANGLE BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 4 PYLON NACELLE STATION 221 INBOARD ANGLE CRACKED. REPAIRED PER SB 747-54-2042. 2 L 7 4 4F A20WE 1999012901032 19990129 01032 NM 1999 1 29 P5CA9900031 1 19990122 A 5400 BRACKET BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 4 PYLON LOWER SPAR STIFFENER INBOARD TIE BRACKET FOUND CRACKED NAC STA 160. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901033 19990129 01033 NM 1999 1 29 P5CA9900032 1 19990122 A 5330 SKIN BOEING 747 747122 1384872 NM BS 360-380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT FLAT SIDE SKIN HOLE AND CRACKS FOUND AT STA 360/380 STR 7/STR9. REPAIRED PER HX RS-R53-11-33999 AND SRM 51-40-02. 2 L 7 4 4F A20WE 1999012901034 19990129 01034 NM 1999 1 29 P5CA9900033 1 19990122 A 5330 SKIN BOEING 747 747122 1384872 NM BS 741-1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND AT FUSELAGE STATION 741 TO 1000 RIGHT SIDE. REPAIRED PER SRM 51-10-01 AND F1-10-02. 2 L 7 4 4F A20WE 1999012901035 19990129 01035 NM 1999 1 29 P5CA9900034 1 19990122 A 5350 FAIRING BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT BODY FAIRING PANEL 194B FOUND DAMAGE. REPAIRED PER SRM 51-48-14. 2 L 7 4 4F A20WE 1999012901036 19990129 01036 NM 1999 1 29 P5CA9900035 1 19990120 A 5751 PANEL BOEING 747 747122 1384872 NM AILERON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT WING UPPER SURFACE OF OUTBOARD AILERON FIX PANEL SMALL AREA OF CORROSION. REPAIRED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999012901037 19990129 01037 NM 1999 1 29 P5CA9900036 1 19990120 A 5350 FAIRING BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FUSELAGE FAIRING PANEL 194B FOUND 1.5 INCH HOLE. REPAIRED PER SRM 51-40-12 FIG 10. 2 L 7 4 4F A20WE 1999012901038 19990129 01038 NM 1999 1 29 P5CA9900037 1 19990120 A 5730 SKIN BOEING 747 747122 1384872 NM WS 860-1010 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON RIGHT WING UPPER SURFACE WS 860 TO 1010. REPAIRED PER SRM 51-10-01, 57-30-01, MM 51-24-01. 2 L 7 4 4F A20WE 1999012901039 19990129 01039 NM 1999 1 29 P5CA9900038 1 19990120 A 5730 SKIN BOEING 747 747122 1384872 NM WS 670-1080 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON UPPER SURFACE OF RT WING WS 670 TO 1080. REPAIRED PER SMR 51-60-01, 57-30-01 AND MM 51-24-07 . 2 L 7 4 4F A20WE 1999012901040 19990129 01040 NM 1999 1 29 P5CA9900039 1 19990120 A 5730 SKIN BOEING 747 747122 1384872 NM WS 400-500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON RIGHT WING SKIN STA 400 TO 500 UPPER SURFACE. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51- 04-07. 2 L 7 4 4F A20WE 1999012901041 19990129 01041 NM 1999 1 29 P5CA9900040 1 19990120 A 5730 SKIN BOEING 747 747122 1384872 NM WS 400-640 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND AT RIGHT WING UPPER SURFACE WING ROOT WS 400 TO 640. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07. 2 L 7 4 4F A20WE 1999012901042 19990129 01042 NM 1999 1 29 P5CA9900041 1 19990120 A 5730 SKIN BOEING 747 747122 1384872 NM WS 830 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION ON LEFT WING LEADING EDGE STATION 830. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07. 2 L 7 4 4F A20WE 1999012901043 19990129 01043 NM 1999 1 29 P5CA9900042 1 19990120 A 5711 SPAR BOEING 747 747122 1384872 NM WS 410-1390 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON LEFT WING UPPER SURFACE OF REAR SPAR WS 410 TO 1390. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07. 2 L 7 4 4F A20WE 1999012901044 19990129 01044 NM 1999 1 29 P5CA9900043 1 19990120 A 5730 SKIN BOEING 747 747122 1384872 NM WS 830-1390 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON UPPER SURFACE OF LEFT WING WS 830 TO 1390. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14- 07. 2 L 7 4 4F A20WE 1999012901045 19990129 01045 NM 1999 1 29 P5CA9900044 1 19990118 A 5330 STRAP BOEING 747 747122 1384872 NM BS 1240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND AT BS 124O R SPLICE STRAP A BOLT HOLES. REPAIRED PER OHM 62440006, SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1999012901046 19990129 01046 NM 1999 1 29 P5CA9900045 1 19990111 A 5400 FAIRING BOEING 747 747122 1384872 NM NR 2 PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 PYLON V FAIRING FORWARD LOWER AREA FOUND DELAMINATION. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999012901047 19990129 01047 NM 1999 1 29 P5CA9900046 1 19990118 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE PANEL 191DD FOUND CORNER DAMAGED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999012901048 19990129 01048 NM 1999 1 29 P5CA9900047 1 19990118 A 5730 PANEL BOEING 747 747122 1384872 NM TE WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 TRAILING EDGE PANEL 673BB FOUND CRACKED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999012901049 19990129 01049 NM 1999 1 29 P5CA9900048 1 19990118 A 5320 FASTENER BOEING 747 747122 1384872 NM BS 140-180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND AT STA 140 TO 180 S23R TO S34R ON FASTENERS. REPAIRED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999012901050 19990129 01050 NM 1999 1 29 P5CA9900049 1 19990118 A 5400 FASTENER BOEING 747 747122 1384872 NM NR 2 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 PYLON L/E FIXED PANEL FOUND 6 SHEARED FASTENERS. REPAIRED PER SRM 51-30-20. 2 L 7 4 4F A20WE 1999012901051 19990129 01051 NM 1999 1 29 P5CA9900050 1 19990118 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 ENG LT POWER COWL LOWER CHORD FOUND DAMAGED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901052 19990129 01052 NM 1999 1 29 P5CA9900051 1 19990118 A 5400 CHANNEL BOEING 747 747122 1384872 NM NR 3 ENGINE COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 ENG LEFT POWER COWL BETWEEN 6/7 FRAMES CHANNEL DAMAGED. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901053 19990129 01053 NM 1999 1 29 P5CA9900052 1 19990118 A 5400 BRACKET BOEING 747 747122 1384872 NM NR 3 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 LEFT POWER COWL FWD FRAME CRACKED BRACKET. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901054 19990129 01054 NM 1999 1 29 P5CA9900053 1 19990118 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 RIGHT POWER COWL LOWER CHORD FOUND CRACKED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901055 19990129 01055 NM 1999 1 29 P5CA9900054 1 19990118 A 5311 FRAME BOEING 747 747122 1384872 NM BS 2120 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FRAME AT BS 2120R STR 22 AND 23R FOUND CRACKED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901056 19990129 01056 NM 1999 1 29 P5CA9900055 1 19990118 A 5320 SKIN BOEING 747 747122 1384872 NM BS 520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BS 520/720 S19R FOUND SURFACE CORROSION. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901057 19990129 01057 NM 1999 1 29 P5CA9900056 1 19990118 A 5532 PANEL BOEING 747 747122 1384872 NM VERT STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT STABILIZER PANEL 334 NBL FOUND DELAMINATED. REPAIRED PER SRM 51-40-01. 2 L 7 4 4F A20WE 1999012901058 19990129 01058 NM 1999 1 29 P5CA9900057 1 19990118 A 5532 PANEL BOEING 747 747122 1384872 NM VERT STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT STABILIZER LOWER PANEL 344GB FOUND DELAMINATED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999012901059 19990129 01059 NM 1999 1 29 P5CA9900058 1 19990118 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT INBOARD ELEVATOR UPPER SURFACE FOUND A 1 BY 1 INCH AREA DELAMINATED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999012901060 19990129 01060 NM 1999 1 29 P5CA9900059 1 19990118 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT INBOARD ELEVATOR TRAILING EDGE SEVERAL AREAS DAMAGED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999012901061 19990129 01061 NM 1999 1 29 P5CA9900060 1 19990118 A 5751 LINK BOEING 747 747122 1384872 NM RT AILERON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT INBOARD AILERON/REACTION LINK FOUND WORN. REPAIRED AND REPLACED BEARINGS PER OHM 20-50-03. 2 L 7 4 4F A20WE 1999012901062 19990129 01062 NM 1999 1 29 P5CA9900061 1 19990118 A 5320 WEB BOEING 747 747122 1384872 NM RT MLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT WING GEAR WELL FWD LOWER PANEL FOUND CORROSION ON INBOARD SIDE. REPAIRED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999012901063 19990129 01063 NM 1999 1 29 P5CA9900062 1 19990114 A 5312 BULKHEAD BOEING 747 747122 1384872 NM BS 1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON BS 1480 FWD SIDE. REPAIRED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999012901064 19990129 01064 NM 1999 1 29 P5CA9900063 1 19990114 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1319 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION ON BS 1319L STR 16 AND 17. REPAIRED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999012901065 19990129 01065 NM 1999 1 29 P5CA9900064 1 19990114 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE PANEL 192MR FOUND SURFACE CORROSION. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999012901066 19990129 01066 NM 1999 1 29 P5CA9900065 1 19990114 A 5244 DOOR BOEING 747 747122 1384872 NM EXT POWER DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FWD EXTERNAL POWER RECEPTICAL DOOR FOUND DAMAGED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999012901067 19990129 01067 NM 1999 1 29 P5CA9900066 1 19990114 A 5532 PANEL BOEING 747 747122 1384872 NM VERT STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT STABILIZER PANEL 334MB FOUND DISBONDED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999012901068 19990129 01068 NM 1999 1 29 P5CA9900067 1 19990114 A 5532 PANEL BOEING 747 747122 1384872 NM VERT STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT STABILIZER PANEL 341BR-341CR FOUND DENTED. REPAIRED PER SRM 51-10-02 AND SRM 51-00-00. 2 L 7 4 4F A20WE 1999012901069 19990129 01069 NM 1999 1 29 P5CA9900068 1 19990126 A 5320 CLIP BOEING 747 747249F 1384849 NM BS 520 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 UPPER DECK STA 502L AT S-9R CLIP IS CRACKED. REPAIRED PER SRM 51-10-02 AND 51-30-02. 2 L 7 4 4F A20WE 1999012901070 19990129 01070 NM 1999 1 29 P5CA9900069 1 19990126 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 520 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 UPPER DECK STA 520 RIGHT SIDE FRAME IS CRACKED FROM STR 8R TO STR 10A. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1999012901071 19990129 01071 NM 1999 1 29 P5CA9900070 1 19990126 A 5730 PANEL BOEING 747 747249F 1384849 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 NR 2 KNEE CAP PANEL LEFT WING DELAMINATED ON INBOARD TRAILING EDGE CORNER. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999012901072 19990129 01072 NM 1999 1 29 P5CA9900071 1 19990126 A 5320 INTERCOSTAL BOEING 747 747249F 1384849 NM BS 380-400 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 INTERCOSTAL WEB CRACKED BETWEEN BS 380 TO 400R AT STRINGER 15R. REPAIRED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1999012901073 19990129 01073 NM 1999 1 29 P5CA9900072 1 19990125 A 5280 DOOR BOEING 747 747249F 1384849 NM LT MLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEFT WING GEAR UPPER STRUT DOOR CRACKED AT OUTBOARD TRAILING EDGE CORNER. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999020400002 19990204 00002 WP 1999 2 4 ABXA9900035 1 19990122 A 5610 KR3E6 ROD DOUG DOUG DC8 DC861 3021952 WP COCKPIT BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 845AX 46157 CAPTAIN'S WINDOW (EMERG EXIT) LATCH PIN WAS FOUND BROKEN DURING PREFLIGHT. REPLACED LOWER FORWARD LINKAGE ROD IAW DC8 M M 56-10-3, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999020500001 19990205 00001 CE 1999 2 5 99ZZZX455 1 19990108 A 2910 FITTING LEAR 24 24A 5170304 CE LT MLG WW LOOSE A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 63CK 119 HYDRAULIC SYSTEM PRESSURE LOSS. FOUND LOOSE LINE ON LEFT GEAR ACTUATOR. TIGHTENED LINE. REPLACED BOTH ENGINE HYDRAULI C PUMPS AND FILTERS. C/W RETRACTION CHECK. RAN AND LEAK CHECKED HYDRAULIC PUMPS AND FILTERS. 2 L 7 2 4J A10CE 1999020500031 19990205 00031 NE 1999 2 5 99ZZZX485 2 19990108 A 7321 5002T94G33 FUEL CONTROL LEAR 24 24 5170302 CE GE CJ610 CJ6106 30006 NE LT ENGINE MALFUNCTIONED A CKSA O OTHER O OTHER NR NOT REPORTED 1 GL 23 63CK 513 52138 119 251777A LEFT ENGINE COMPRESSOR STALLNG FROM ROTATION TO 2,000 FEET. REPLACED LEFT FUEL CONTROL UNIT. GROUND RUN, LEAK CHECKED, AND TEST FLEW AIRCRAFT, OPS CHECKED GOOD. NO RECOMMENDATIONS TO PREVENT RECURRENCE. 2 L 7 2 4J 4 J A10CE 1E16 1999020500037 19990205 00037 NM 1999 2 5 TWAA9901801 1 19990127 A 3397 WIRE BOEING 767 767231 1385131 NM ROW 31-35 CONTAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 FOUND FLOOR EGRESS LIGHTING ON RT SIDE OF CABIN INOPERATIVE FROM ROW 31 TO 35. DRIED WET WIRING IN AFT GALLEY AREA. CH ECK-C 11-12-98 LAX. 2 L 7 2 4F RT A1NM 1999020500038 19990205 00038 NM 1999 2 5 HNAA9900019 1 19990127 A 3231 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM LDG GEAR DOORS MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION LD LANDING 1 EA 07 927HA 117 LANDING GEAR DOORS WOULD NOT CLOSE UNTIL NOSE GEAR TOUCHED DOWN ON LANDING. REPLACED 3261-K9 (P/N DSC182-2) RELAY. 2 H 7 2 4T RT A13NM 1999020500039 19990205 00039 NM 1999 2 5 HNAA9900020 1 19990127 A 3297 WIRE DHAV DHC8 DHC8102 2809003 NM LT MLG BROKEN A HNAA O OTHER N FALSE WARNING DE DESCENT 1 EA 07 911HA 034 DURING GEAR EXTENSION LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED (RED LIGHT). CYCLED GEAR SEVERAL TIMES WITH SAME RESULTS. PERFORMED ALTERNATE EXTENSION AND ALTERNATE GEAR INDICATION 3 POINTS DOWN AND LOCKED. REPAIRED BROKEN WIRE AT STABILI ZER STAY STRUT PROXIMITY SENSOR. ALL INDICATIONS NORMAL. 2 H 7 2 4T RT A13NM 1999020500042 19990205 00042 WP 1999 2 5 AT9900044 1 19990127 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP ROW 1-18 DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 839AT 47089 OVERHEAD EMERGENCY LIGHTING LIGHTS FROM ROW 1 TO ROW 18 WILL NOT ILLUMINATE, DURING MAINTENANCE TESTING. REMOVED AND RE PLACED STATION 628 FORWARD POWER SUPPLY, REFERENCE MM 33-50. OPERATIONAL CHECKED GOOD. 2 L 7 2 4F A6WE 1999020500043 19990205 00043 WP 1999 2 5 AT9900045 1 19990125 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 927 CORROSION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL. A CUSP WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF CUSP WEB, FABRICATED A NEW SECTION OF WEB AND TWO SPLICES. INSTALLED REPAIR PARTS IAW DC9 SRM 51-10-2, 53-11-3 AND RES NR 99195 (P/N 1A-41895-1). 2 L 7 2 4F A6WE 1999020500047 19990205 00047 NM 1999 2 5 K3HA990005 1 19990128 A 3350 3071BPEGPL BULB BOEING 727 727225 1384077 NM ROW 2ABC FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 FORWARD EMERGENCY PATH TRACK LIGHTING MISSING A BULB AND LENS AT ROW 2ABC. INSTALLED LAMP AND LENS OK PER MAINTENANCE M ANUAL 33-50-00. (LENS 07912-3) 2 L 7 3 4F A3WE 1999020500048 19990205 00048 EU 1999 2 5 AWXA9900031 1 19990124 A 2611 SMOKE DETECTOR AIRBUS 320 A320231 3930325 EU LAVATORY DIRTY A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 621AW 053 AFT LAV SMOKE WARNING, INITIATED AIR RETURN TO MIA. CLEANED OUT CLOGGED AFT LAV DETECTOR GRILLS. ALSO, CHECKED REPORT OF THE SIDE WALL BEING HOT, THIS WAS NORMAL AS THE HOT WATER HEATER IS ON THE OTHER SIDE. NO PARTS REPLACED. 2 L 7 2 4F RT A28NM 1999020500049 19990205 00049 NM 1999 2 5 AWXA9900032 1 19990125 A 7931 ST104Z TRANSMITTER BOEING 737 737277 1384570 NM NR 2 ENG OIL SYS FAILED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 28 182AW 22649 OIL QTY CHECKED BEFORE ENGINE START NR 2 ENGINE HAD JUST OVER 3 GALLONS. T/O ROLL ENGINE INSTRUMENTS NORMAL, JUST AFTER ROTATION NOTICED OIL PRESSURE IN RED AND ENGINE OIL TEMP CLIMBING THROUGH 170 DEGREES C. SHUT ENGINE DOWN AND RETURNED TO SMF. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE TRANSMITTER IAW MM 79-32-0, LEAK AND OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999020500050 19990205 00050 NM 1999 2 5 AWXA9900033 1 19990124 A 3397 WIRE BOEING 737 7372E3 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 A 3 FOOT SECTION OF CABIN ESCAPE PATH LIGHTS INOP. REPAIRED WIRING. 2 L 7 2 4F RT A16WE 1999020500051 19990205 00051 NM 1999 2 5 AWXA9900034 1 19990126 A 2120 SENSOR BOEING 737 7373Y0 1384671 NM COOLING DUCT LOOSE A AWXA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 28 323AW 23684 EMERGENCY DECLARED, EQUIPMENT COOLING WAS INOP IN NORMAL AND ALTERNATE BUT STARTED TO WORK NORMAL ON DESCENT. UAL MX C/ W BMM CHECK, NO FAULTS. A/C RETURNED TO PHX WITH SAME PROBLEM. MX FOUND SENSOR LOOSE IN DUCT. INFORMATION OBTAINED FR OM MX CONTROL LOG SHEET, ADDITIONAL INFO TO FOLLOW. 2 L 7 2 4F RT A16WE 1999020500053 19990205 00053 WP 1999 2 5 9900259978 1 19990122 A 2120 DUCT DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 9342 47391 LOSS OF CABIN PRESSURIZATION OCCURRED AT 17,000 FEET. CABIN ALTITUDE REACHED 11,000 FEET AND AN EMERGENCY DESCENT WAS M ADE TO 10,000 FEET. CABIN PRESSURE WAS REGAINED. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED HOLE IN AIR CONDITIONING DUCT BY AIR CYCLE MACHINE. ALSO, REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999020500054 19990205 00054 SO 1999 2 5 COMA9910025 1 19990127 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 247CA 14680 1225 FORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTING. 2 L 7 2 4T RT A31SO 1999020500055 19990205 00055 EA 1999 2 5 COMA9960049 1 19990126 A 5270 SWITCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 710CA 7241 DURING CLIMBOUT OF YUL, THE AMBER CABIN DOOR LATCH MESSAGE ACTIVATED. ADJUSTED THE CABIN DOOR WARNING PROXIMITY SWITCH. 2 L 7 2 4F RT A21EA 1999020500056 19990205 00056 NM 1999 2 5 UPS99228543 1 19990127 A 2612 FIRE LIGHT BOEING 727 7272A1 138407F NM COCKPIT ILLUMINATED A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 213UP 21341 INSPECTION TYPE N/A, RED FIRE WARNING LIGHT ON MASTER GLARESHIELD ILLUMINATED ON CLIMBOUT. NO OTHER FIRE LIGHTS ASSOCIA TED WITH IT. SILENCED BELL AND LIGHT WENT OUT. ALL FIRE LIGHTS TESTED. PERFOMRED TEST ON FIRE WARNING A & B, CHECKED FIRE LOOPS A & B, FOUND NO DISCREPANCIES 2 L 7 3 4F A3WE 1999020500057 19990205 00057 WP 1999 2 5 UPS99828542 1 19990104 A 5320 575412527 FITTING DOUG DC8 DC871F 302199D WP BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, AFT TEE FITTING IN KEEL BEAM LT FS 920 HAS A 8.75 CRACK. REMOVED, FABRICATED, AND INSTALLED REPLACEM ENT ANGLES IAW DWG 5754125, SB-53-68, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500058 19990205 00058 WP 1999 2 5 UPS99828544 1 19990121 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1470-1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SEAT TRACK CORRODED AT FS 1470 TO 1480 UNDER FLOORBEAM FLANGE LBL 60 VIEWED FROM D PIT FLOOR LOOKING UP. REPAIRED IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999020500059 19990205 00059 WP 1999 2 5 UPS99828545 1 19990122 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SEAT TRACK CORRODED AT FS 1540 LBL 45. REPAIRED IAW SRM ADDN DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 1999020500060 19990205 00060 NM 1999 2 5 QXEA9900128 1 19990125 A 3350 61047811 BATTERY DHAV 6038441 DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 826PH 582 115 214 SEA - EMERGENCY EXIT FLOOR LIGHT INOP. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY AND BATTERY. OPERATIONAL CHECK GOOD . 2 H 7 2 4T RT A13NM 1999020500061 19990205 00061 WP 1999 2 5 ABXA9900037 1 19990125 A 3260 DC26A1415S CONNECTOR DOUG DC8 DC861 3021952 WP LT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 850AX 45894 ON APPROACH TO ILN WITH GEAR DOWN AND THREE SAFE LIGHTS, RED UNSAFE LIGHT CAME ON INTERMITTENTLY. RECYCLED GEAR, NO HEL P. LANDING WAS UNEVENTFUL. REPLACED P1-1398 CONNECTOR IAW DC8 WDGM 32-61-01. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999020500062 19990205 00062 WP 1999 2 5 ABXA9900038 1 19990126 A 5250 MR25291GR41 LATCH DOUG DC8 DC862 3021970 WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 DURING POSTFLIGHT CHECK, CABIN DOOR LOCK WAS STUCK IN LOCKED POSITION. FOUND OUTER LATCH ASSEMBLY MISADJUSTED 180 DEGRE ES. READJUSTED LATCH TO PROPER POSITION, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999020500063 19990205 00063 WP 1999 2 5 ABXA9900039 1 19990121 A 5250 MR25291GR41 LATCH DOUG DC8 DC862 3021970 WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 DURING POSTFLIGHT, FOUND COCKPIT DOOR KNOB STUCK. ADJUSTED AND LUBRICATED INTERNAL MECHANISM IAW DC8 SRM. 2 L 7 4 4F 4A25 1999020500064 19990205 00064 WP 1999 2 5 MWEA99053 1 19990127 A 3350 6003045 BATTERY PACK DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 THE EMERGENCY PEANUT LIGHTS IN COCKPIT REMAIN ON REGARDLESS OF COCKPIT EMERGENCY LIGHT SWITCH POSITION. MTC REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1999020500065 19990205 00065 NM 1999 2 5 SCNA99014 1 19990125 A 3150 WARNING BOEING 727 7272J4 1384006 NM COCKPIT SOUNDED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 285SC 21676 DURING START OF TAKEOFF ROLL, THE TAKEOFF WARNING SOUNDED WITH POWER SET ABOVE 1.4 EPR. FLAPS, TRIM AND SPEED BRAKES AT SET IN OPERATING/TAKEOFF SETTINGS. RETURNED AIRCRAFT TO GATE. RESET TAKEOFF WARNING CIRCUIT BREAKERS, MOVED STABILIZE R TRIM ALL THE WAY UP AND ALL THE WAY DOWN, RECYCLED FLAPS UP AND DOWN, CHECKED EPR TEST CARDS AND ALL CHECKED GOOD. 2 L 7 3 4F RT A3WE 1999020500066 19990205 00066 NM 1999 2 5 SCNA99015 1 19990123 A 3610 CLAMP BOEING 727 727259 138408J NM NR 1 PYLON LOOSE A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 289SC 22475 DURING CLIMBOUT FROM SFO, THE ENGINE NUMBER ONE STRUT OVERHEAT LIGHT ILLUMINATED. FOUND ENGINE DUCT IN THE NUMBER ONE P YLON LEAKING JUST BEFORE THE PRECOOLER. TIGHTENED CLAMP AND RAN THE NUMBER ONE ENGINE TO LEAK CHECK. NUMBER ONE ENGINE LEAK CHECKED GOOD IAW MM CHAPTER 2100. 2 L 7 3 4F A3WE 1999020500067 19990205 00067 WP 1999 2 5 SCNA99016 1 19990117 A 2170 COALESCER DOUG DC10 DC1015 3022118 WP NR 3 PACK CONTAMINATED A SCNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 154SY 48259 DURING CLIMB, CABIN FILLED WITH SMOKE. COMPLIED WITH COM AND SMOKE STOPPED WHEN NR 2 PNEUMATIC SUPPLY AND NR 2 PACK SEL ECTED TO OFF. DIVERTED AIRCRAFT TO ORD FOR A PRECAUTIONARY LANDING. FOUND NR 3 ENGINE WITH NR 3 PACK ON CAUSING OIL FU MES IN THE CABIN AT 91 PERCENT N1 FAN SPEED. FOUND OIL IN THE NR 3 PACK COALESCER BAG. REMOVED AND REPLACED THE NR 3 P ACK COALESCER BAG AND OPERATED ENGINES AT VARIOUS POWER SETTINGS WITH PACKS RUNNING. NO ODOR OR SMOKE NOTED. 2 L 7 3 4F A22WE 1999020500068 19990205 00068 WP 1999 2 5 SCNA99017 1 19990120 A 3350 BATTERIES DOUG DC10 DC1015 3022118 WP L2 DOOR SLIDE DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 153SY 48276 DURING A LINE MAINTENANCE CHECK, THE L2 EMERGENCY SLIDE LIGHT WAS FOUND TO BE INTERMITTENT AND THE SLIDE LIGHT BATTERY C ONTACTS WERE FOUND BROKEN. SECURED THE SLIDE LIGHT BATTERIES IN THE HOLDER. 2 L 7 3 4F A22WE 1999020500069 19990205 00069 NM 1999 2 5 SCNA99018 1 19990117 A 5610 5893543110 WINDSHIELD BOEING 727 7272J4 1384006 NM RT COCKPIT FAILED A SCNA K NONE O OTHER NR NOT REPORTED 1 GL 15 288SC 20765 THE FIRST OFFICER'S R1 WINDSHIELD WAS SEEN TO SPARK IN THE TOP RIGHT CORNER. REMOVED AND REPLACED THE R1 WINDOW IAW MM 561111. LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 3 4F RT A3WE 1999020500070 19990205 00070 NM 1999 2 5 SCNA99019 1 19990120 A 3350 1102833 LIGHT BOEING 727 7272A1 138407F NM ROW 10 INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, THE CENTER AISLE OVERHEAD EMERGENCY LIGHT ABOVE ROW 10 WAS FOUND TO BE INOPERATIVE. RE MOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999020500071 19990205 00071 NM 1999 2 5 SCNA99020 1 19990125 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INTERMITTENT. REMOVED AND RE PLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT BATTERY PACK IAW MM 335022. LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999020500072 19990205 00072 NM 1999 2 5 SCNA99021 1 19990123 A 2530 1430E1 OVEN BOEING 727 727227 1384078 NM GALLEY SPARKING A SCNA K NONE O OTHER NR NOT REPORTED 1 GL 15 275AF 244 22092 THE FRONT LEFT OVEN WAS OBSERVED TO HAVE SPARKS EMITTING FROM THE FRONT VENT AREA. OVEN WAS SHUT DOWN. REMOVED AND REP LACED THE FORWARD LEFT OVEN UNIT, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999020500073 19990205 00073 NM 1999 2 5 SCNA99022 1 19990125 A 3350 BATTERY BOEING 727 7272J4 1384006 NM AFT AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR EMERGENCY LIGHTS WERE FOUND TO BE DIM. REMOVED AND REPLACED THE BATTE RIES, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999020500074 19990205 00074 NM 1999 2 5 SWAA990141 1 19990121 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND EXTERIOR EMERGENCY OVERWING LIGHT AT BS 773R INOP. REMOVED AND REPLACED BATTERY PACK PE R BOEING MM. 2 L 7 2 4F A16WE 1999020500075 19990205 00075 NM 1999 2 5 SWAA990142 1 19990121 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 616SW 27699 DURING SCHEDULED SC CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER BOEING M M. 2 L 7 2 4F RT A16WE 1999020500076 19990205 00076 NM 1999 2 5 SWAA990143 1 19990121 A 3350 20121 CHARGER BOEING 737 7373Q8 1384670 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SC CHECK, FOUND LT AND RT OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER BOEING M M. 2 L 7 2 4F RT A16WE 1999020500077 19990205 00077 NM 1999 2 5 SWAA990144 1 19990121 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY PACKS PER BOE ING MM. 2 L 7 2 4F A16WE 1999020500078 19990205 00078 NM 1999 2 5 SWAA990145 1 19990121 A 2121 6454051 FAN BOEING 737 7373A4 1384585 NM AC BAY FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED 1/2D CHECK, NOTED A SMOKE SMELL WITH RECIRCULATING FAN RUNNING. REMOVED AND REPLACED FAN PER BOEING MM . 2 L 7 2 4F RT A16WE 1999020500079 19990205 00079 NM 1999 2 5 SWAA990146 1 19990120 A 3320 1060752 BALLAST BOEING 737 7372H4 138448C NM LAVATORY FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 89SW 22904 SMOKE IN COCKPIT, ENTERED IN STEADY HEAVY STREAM IN AREA OF BRACE IN C/B PANEL BY CAPT LEFT SHOULDER. LAVATORY MIRROR C /B FOUND TRIPPED. CHECKED P-18 PNL FOR BURN WIRE AND CIRCUIT BREAKER, ALL CHECK NORMAL. FOUND FWD LAV MIRROR LT BALLAS T BAD. PULLED AND COLLARED LAV MIRROR LT C/B. CONTINUED PER MEL 33-2. DURING OVERNIGHT CHECK, REMOVED AND REPLACED LI GHT BALLAST PER BOEING MM. 2 L 7 2 4F A16WE 1999020500080 19990205 00080 NM 1999 2 5 SWAA990147 1 19990124 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM ROW 5 DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SC CHECK, FOUND CABIN EMERGENCY EXIT LIGHT AT BULLNOSE AT ROW 5R INOP. REATTACHED LIGHT ASSEMBLY AND O P CHECKED PER BOEING MM. 2 L 7 2 4F RT A16WE 1999020500081 19990205 00081 NM 1999 2 5 SWAA990152 1 19990122 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED SC CHECK, FOUND CABIN FLOOR TRACK LIGHTS INOP AT EMERGENCY EXIT ROW. REPAIRED WIRES AND OP CHECKED PER BOEING MM. 2 L 7 2 4F RT A16WE 1999020500082 19990205 00082 NM 1999 2 5 SWAA990153 1 19990122 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 935 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 935, 4 BELOW S23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999020500083 19990205 00083 NM 1999 2 5 SWAA990154 1 19990122 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TIE STRAP CORRODED AT BS 727D+6. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999020500084 19990205 00084 NM 1999 2 5 SWAA990155 1 19990122 A 5315 BEAM BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AT BS 727E+3. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999020500085 19990205 00085 NM 1999 2 5 SWAA990156 1 19990122 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 515 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, S12R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999020500086 19990205 00086 NM 1999 2 5 SWAA990157 1 19990122 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACKED AT BS 727A-727E, ON CREASE LINE. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1999020500108 19990205 00108 WP 1999 2 5 TWAA9901901 1 19990129 A 3350 LIGHT DOUG DC9 DC983 3022083 WP ROW 11 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9420D 49824 FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM CABIN ROW 11 AFT. FOUND WIRE DISCONNECTED AND RECONNECTED SAME. CHECK-C 12- 8-98 MCI. 2 L 7 2 4F RT A6WE 1999020500109 19990205 00109 WP 1999 2 5 TWAA9901902 1 19990124 A 5312 BLKHD STIFFENER DOUG DC9 DC931 3022065 WP FWD PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT THE FWD PRESSURE BULKHEAD STIFFENER CRACKED IN CENTER APPROXIMATELY 1 .5 INCH LOCATED 18.5 INCHES FROM BOTTOM OF BULKHEAD. REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER WITH HI-LOKS PER SRM 51-60-0. 2 L 7 2 4F A6WE 1999020500110 19990205 00110 WP 1999 2 5 TWAA9901903 1 19990123 A 5312 BLKHD STIFFENER DOUG DC9 DC931 3022065 WP FWD PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, IN AFT CARGO COMPT THE FWD PRESSURE BULKHEAD STIFFENER WAS CRACKED IN CENTER 26.5 INCHES FROM BOTTOM OF PRESSURE BULKHEAD. REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER WITH HI-LOKS PER SRM 51-60-0. 2 L 7 2 4F A6WE 1999020500111 19990205 00111 WP 1999 2 5 TWAA9901904 1 19990119 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 980 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND STA 980 FORMER PREVIOUSLY REPAIRED AT STRINGER 17R. REPAIRED FORMER PER SRM 53-03, PAGE 131 TO 132, SHEET 2, AND PAGE 133 SHEET 3, AND PAGES 135 AND 137. 2 L 7 2 4F A6WE 1999020500112 19990205 00112 WP 1999 2 5 TWAA9901905 1 19990127 A 5542 SKIN DOUG DC9 DC983 3022083 WP RUDDER DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND RUDDER DELAMINATED ON RT SIDE AT AFT SIDE OF CENTER HINGE. REPAIRED PER SRM 51-90-0, PA GE 49, AND 51-70-1A PAGE 21. 2 L 7 2 4F RT A6WE 1999020500113 19990205 00113 WP 1999 2 5 TWAA9901906 1 19990127 A 5260 59161431 CASTING DOUG DC9 DC983 3022083 WP FWD AIRSTAIR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, THE FWD AIRSTAIRS FORWARD DOOR CASTING WAS CRACKED IN RADIUS APPROXIMATELY 1.5 INCH LONG. REM OVED AND REPLACED CASTING PER STANDARD PROCESSES MANUAL 6-70-01. 2 L 7 2 4F RT A6WE 1999020500114 19990205 00114 NM 1999 2 5 SPAA9900002 1 19990115 A 3350 BULB BOEING 737 7372T4 1384492 NM EXTERIOR FAILED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE EXTERIOR EMERGENCY EXIT LIGHT AFT OF THE RT BODY FAIRING WAS FOUND INOPERATIVE. THE BULB WA S REPLACED, SUBSEQUENT SYSTEM TEST WAS SATISFACTORY. 2 L 7 2 4F A16WE 1999020500121 19990205 00121 NM 1999 2 5 AT9900056 1 19990120 A 5512 SKIN BOEING 737 737214 138446R NM HORIZ STAB MISREPAIRED A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT HORIZONTAL STABILIZER STA 166 SKIN REPAIR HAS NO EDGE DISTANCE ON FI LLER. REMOVED EXISTING REPAIR AND FABRICATED DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED REPAIR PARTS PE R B737 SRM 51-30-2 AND RES 99178. 2 L 7 2 4F A16WE 1999020500131 19990205 00131 1999 2 5 MALA976301 4 19990122 A 3413 066500012804 VSI SAAB SF340 340B 7860101 EU NR 2 FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 9CJ 224 ON CLIMBOUT, NR 2 VERTICAL AIR SPEED INDICATOR FAILED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED NR 2 VERTICAL AI R SPEED INDICATOR. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999020500132 19990205 00132 EU 1999 2 5 MALA976302 1 19990121 A 3150 WARNING SYST SAAB SF340 SF340A 7850100 EU COCKPIT ACTIVATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 76XJ 076 CONFIGURATION WARNING ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO DTW. MAINTENANCE RAN MULTIPLE CHECKS OF CONFIG W ARNING SYSTEM, ALL CHECKS GOOD IAW SAAB 340 AMM CHAP 27. 2 L 7 2 4T RT A52EU 1999020500133 19990205 00133 EU 1999 2 5 MALA976303 1 19990118 A 5210 SEAL SAAB SF340 SF340A 7850100 EU PAX DOOR OUT OF ADJUST A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 79XJ 079 LOUD SQUEAL FROM CABIN DOOR. AIRCRAFT RETURNED TO DTW. MAINTENANCE ADJUSTED CABIN DOOR SEAL, PRESSURIZED AIRCRAFT. NO DEFECTS NOTED AT THIS TIME IAW SAAB AMM CHAP 21. 2 L 7 2 4T RT A52EU 1999020500134 19990205 00134 EU 1999 2 5 MALA976304 1 19990117 A 2613 HOT LIGHT SAAB SF340 340B 7860101 EU RT ENGINE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 407XJ 340B407 RIGHT TAIL PIPE HOT CWP CAME ON INTERMITTENTLY. REDUCED POWER AND LIGHT NEVER CAME ON AGAIN. AIRCRAFT RETURNED TO DTW. MAINTENANCE RAN ENGINES AT TAKEOFF POWER AND VISUALLY CHECKED WIRES. COULD NOT DUPLICATE THE PROBLEM. ALL CHECKS GOO D AT THIS TIME. 2 L 7 2 4T RT A52EU 1999020500135 19990205 00135 EU 1999 2 5 MALA976305 1 19990124 A 3350 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 433XJ 433 ARMED LIGHT FOR EMERGENCY LIGHTS ON THE F/A STATUS PANEL INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT SWITCH AND LIGHT OP S CHECKED GOOD. 2 L 7 2 4T RT A52EU 1999020500136 19990205 00136 EU 1999 2 5 MALA976306 1 19990119 A 3350 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST CR CRUISE 1 GL 15 446XJ 446 EN ROUTE TO MSP, F/A FOUND EMERGENCY LIGHT ARMED INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999020500137 19990205 00137 EU 1999 2 5 MALA976307 1 19990118 A 3213 AIR130210 AXLE SAAB SF340 340B 7860101 EU LT MLG FAILED A MALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 GL 15 448XJ 448 ON TAKEOFF, LEFT HAND INBOARD WHEEL ASSEMBLY SEPARATED FROM AXEL. CREW LOWER GEAR AND LANDED IN DTW WITHOUT INCIDENT. M AINTENANCE REPLACED AXLE ASSEMBLY IAW SAAB MM 32-11-20, SC CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999020500138 19990205 00138 EU 1999 2 5 MALA976308 1 19990121 A 3150 465465140 CIRCUIT BOARD BAC 146 AVRO146RJ85A 1500097 EU E & E COMPT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 511XJ E2326 AFTER SEPARTURE AT ABOUT 3000 FT MSO AMBER MASTER CAUTION LIGHT ILLUMINATED, MOMENTARILY. ALSO, ELECT LOOK UP LIGHT ON, BOTH WENT OUT AFTER 2 TO 3 SECONDS. REPEATED EVERY 3 TO 4 SECONDS FOR THE NEXT 1=30 UNTIL LANDING, CEASED ON TOUCH DOW N. THEN CHECKING STANDBY GEN SHOWED ABOUT 25V IN OFF POSITION, CYCLED ON/OFF AND VOLTAGE FINALLY ZEROED. NO OVERHEAD E LECT LIGHT ON. MAINTENANCE COULD NOT DUPLICATE, OPERATED IN GROUND/AIR MODE, NO DEFECTS AT THIS TIME. REPLACED PCB WQ5 . OPS CHECK GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 1999020500139 19990205 00139 1999 2 5 MALA976309 4 19990124 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DEPLOYED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 515XJ E2333 FRONT LEFT PAX DOOR ESCAPE SLIDE DEPLOYED. MAINTENANCE REPLACED FORWARD PAX DOOR SLIDE IAW 25-40-11-401, OPS CHECK GOOD . 2 H 7 4 4F RT A49EU 1999020500140 19990205 00140 EU 1999 2 5 MALA976310 1 19990119 A 7110 R3894123F26 COWL SAAB SF340 SF340A 7850100 EU RT NACELLE LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 107XJ 340A107 ON POST FLIGHT WALKAROUND, NOTED RIGHT COWL ABOVE PROP WAS LOOSE. LOOSE COWL HAD NICKED THE PROPS APPROXIMATELY 1 BY .5 INCH. MAINTENANCE INSPECTED RIGHT HAND PROP AND COWLING MAIN SPAR AND BLADES, INTAKE, SPEED TAPE OVER ONE HOLE THROUGH TOP OF FIGURE 8 COWLING. REMOVED AND REPLACED RIGHT PROP ASSEMBLY, AND RIGHT UPPER FIGURE 8 COWLING. ALL CHECKS AND R UNS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 1999020500141 19990205 00141 NE 1999 2 5 MALA976311 2 19990120 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A MALA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 15 413XJ 413 LEFT ENGINE HAD A ROLL BACK, LEFT IGNITION LIGHT CAME ON AND ENGINE PARAMETERS WERE NORMAL, IN ICING CONDITIONS, ICE ON, 13 DEGREES CELSIUS, 13,000 ALT. NO CHANGE IN ITT AT END OF EVENT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE COMP LIED WITH TROUBLESHOOTING TABLE 103 OF GE MM 72-00-00 (TROUBLE 5) NO CHANGE IN ITT NOTED. NO FURTHER ACTION REQUIRED AT THIS TIME. 2 L 7 2 4T 4 T RT A52EU E8NE 1999020500142 19990205 00142 EU 1999 2 5 MALA976312 1 19990123 A 2613 HOT LIGHT SAAB SF340 SF340A 7850100 EU RT TAIL PIPE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 115XJ 340A115 RIGHT TAIL PIPE HOT INDICATION ON CLIMBOUT. RETURNED TO SBN. MAINTENANCE PERFORMED GROUND RUNS WITH CREW, COULD NOT DU PLICATE. 2 L 7 2 4T RT A52EU 1999020500143 19990205 00143 EU 1999 2 5 MALA976313 1 19990125 A 3350 85 BULB SAAB SF340 340B 7860101 EU FA PANEL FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING WALKAROUND, EMERGENCY LIGHT ARMED, LIGHT INOP ON F/A PANEL. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999020500144 19990205 00144 EU 1999 2 5 MALA976314 1 19990124 A 5230 BLOW OUT DOOR SAAB SF340 340B 7860101 EU CARGO COMPT POPPED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 439XJ 439 CARGO FIRE WARNING IN FLIGHT, EXTINGUISHED WITH NR 2 CARGO BOTTLE. MAINTENANCE INSPECTED CARGO COMPARTMENT, LEFT BLOW O UT DOOR POPPED. RESECURED DOOR, REPLACED LEFT NR 2 SQUIB AND FIRE BOTTLE PER 2623-00, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999020500145 19990205 00145 EU 1999 2 5 MALA976315 1 19990124 A 3260 SWITCH SAAB SF340 340B 7860101 EU LT MLG OUT OF ADJUST A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 451XJ 451 LANDING GEAR LIGHT IN HANDLE ON WHEN GEAR UP. MAINTENANCE CLEANED AND ADJUSTED LEFT MLG UPLOCK SWITCH. ALL CHECKS GOOD IAW SAAB 340 AMM CHAP 32. 2 L 7 2 4T RT A52EU 1999020500146 19990205 00146 EU 1999 2 5 MALA976316 1 19990125 A 2435 23080031 STARTER GEN SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 15 416XJ 416 DURING CLIMBOUT, LEFT GENERATOR OVER TEMP LIGHT ILLUMINATED. PERFORMED QRH ELECTRICAL ITEMS WHICH LED TO SHUT DOWN OF L EFT GENERATOR. LEFT GEN OVER TEMP EXTINGUISHED AFTER A MINUTE. LEFT GEN OVER TEMP LIGHT RE-ILLUMINATED 10 MINUTES LATE R. LEFT ENGINE STARTED RUNNING VERY ROUGH AT WHICH TIME FLIGHT DIVERTED TO INDIANAPOLIS WITH ENGINE RUNNING VERY SMALL RPM FLUCTUATIONS. HOWEVER, TORQUE REMAINED SOMEWHAT STABLE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LE FT STARTER GENERATOR IAW SAAB 340 MM 24-31-05, OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999020500147 19990205 00147 EU 1999 2 5 MALA976317 1 19990121 A 2424 51634002 GCU SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 15 9CJ 224 RIGHT AC GEN LIGHT ILLUMINATED IN FLIGHT, UNABLE TO REST PER QRH. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED RT AC GEN CONTROL UNIT, OPS CHECK GOOD. ALL WORK IAW SAAB AMM. 2 L 7 2 4T RT A52EU 1999020500148 19990205 00148 EU 1999 2 5 MALA976318 1 19990124 A 3020 INLET DEICE SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 430XJ 430 ON CLIMBOUT, LEFT INTAKE LIGHT ILLUMINATED. COMPLETED QRH ITEMS LIGHT REMAINED ON. AIRCRAFT RETURNED TO DTW. MAINTENA NCE RAN AIRCRAFT AND SWAPPED CANNON PLUGS FOR THERMISTORS P1 & P3 TO J4 & J5. OPS CHECK GOOD. RAN AIRCRAFT FOR 30 MINU TES. 2 L 7 2 4T RT A52EU 1999020500149 19990205 00149 EU 1999 2 5 MALA976319 1 19990126 A 3020 INLET DEICE SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 68XJ 068 RIGHT ENGINE INTAKE ANTI ICE INOP ADVISORY LIGHT ILLUMINATED IN FLIGHT. NO ICE NOTED ON INTAKE IN TRACE ICING CONDITION , OCCURRED ONCE MORE AFTER RESET. AIRCRAFT RETURNED TO MSP. MAINTENANCE COMPLETED OPS CHECK OF INLET HEAT IAW SF3 MM 3 0-20-00 AND COMPLETED A 1 HOUR GROUND RUN OF RIGHT INLET HEAT, NO DEFECTS FOUND. ALL OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999020500150 19990205 00150 EU 1999 2 5 MALA976320 1 19990125 A 2611 CONNECTOR SAAB SF340 340B 7860101 EU CARGO SMOKE DET LOOSE A MALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 452XJ 452 CARGO SMOKE LIGHT ILLUMINATED ON THE GROUND, NO INDICATION OF SMOKE, DUST ETC IN CARGO HOLD. MAINTENANCE CLEANED AND RE SECURED FORWARD SMOKE DETECTOR CANNON PLUG, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999020500151 19990205 00151 EU 1999 2 5 MALA976321 1 19990127 A 3350 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 449XJ 449 THE ARM LIGHT DOES NOT ILLUMINATE ON THE F/A PANEL WHEN EMERGENCY LIGHTS ARE ARMED. MAINTENANCE RELAMPED, OPS CHECK GOO D. 2 L 7 2 4T RT A52EU 1999020500152 19990205 00152 EU 1999 2 5 MALA976322 1 19990126 A 2612 FIRE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 439XJ 439 CARGO 1 FIRE EXT LIGHT ILLUMINATED INFLIGHT. MAINTENANCE COMPLETED A CONT CHECK OF THE PSI SWITCH, CHECK GOOD. ALL OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 1999020500153 19990205 00153 EU 1999 2 5 MALA976323 1 19990128 A 2421 31342003 GENERATOR SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 422XJ 422 RIGHT AC GEN FAILED EN ROUTE. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RT AC GEN IAW AMM 24-20-00, OPS CHECK GOO D. 2 L 7 2 4T RT A52EU 1999020500154 19990205 00154 EU 1999 2 5 MALA976324 1 19990128 A 7933 522794 INDICATOR SAAB SF340 340B 7860101 EU RT ENG OIL TEMP FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 404XJ 340B404 DURING CLIMBOUT OF MSP, RIGHT ENGINE OIL TEMP INDICATING BETWEEN 150 DEGREES AND TOP OF GAUGE LIMIT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RIGHT ENGINE OIL TEMP INDICATOR AND ENGINE OIL TEMP DETECTOR. RAN AIRCRAFT AT ALL POWER S ETTINGS OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 1999020500155 19990205 00155 NM 1999 2 5 CALA9900085 1 19990127 A 2121 65771 COOLING FAN BOEING 737 737524 1384721 NM E & E COMPT SHORTED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14613 14791 27326 A BURNING ODOR WAS SMELLED IN THE CABIN DURING CLIMBOUT OF EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOU T INCIDENT. MAINTENANCE FOUND THE AVIONICS EQUIPMENT COOLING FAN SHORTED OUT. NO EVIDENCE OF FIRE WAS FOUND. THE FAN WAS REMOVED AND REPLACED IAW MM 21-58-12, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1999020500156 19990205 00156 NM 1999 2 5 CALA9900086 1 19990127 A 5753 SKIN BOEING 757 757224 1384958 NM LT & RT TE FLAPS FRETTING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 INSPECTION FOUND BOTH THE LEFT HAND AND RIGHT HAND OUTBOARD FLAP INBOARD SKIN PANELS FRETTING. THE PANELS WERE REMOVED AND REPLACED IAW ECRA 5753-01055. 2 L 7 2 4F RT A2NM 1999020500157 19990205 00157 NM 1999 2 5 CALA9900087 1 19990127 A 5220 HANDLE BOEING 757 757224 1384958 NM LT EMER EXIT LACK OF LUBE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 THE LT AFT OVERWING HATCH WAS STIFF IN OPERATION WHEN USING THE EXTERNAL HANDLE. THE HATCH OPERATING MECHANISM WAS LUBR ICATED AND OPERATIONAL CHECK WAS GOOD IAW MM 52-22-01, PAGE 204. 2 L 7 2 4F RT A2NM 1999020500158 19990205 00158 NM 1999 2 5 CALA9900088 1 19990127 A 5330 SKIN BOEING 757 757224 1384958 NM FUSELAGE PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33103 27293 A PERMANENT FLUSH REPAIR WAS PERFORMED TO FUSELAGE SKIN APPROXIMATELY SIX FEET FORWARD OF R-2 DOOR WHERE JETWAY HAD PUNC TURED A HOLE. THE REPAIR WAS DONE IAW ECRA 5331-01038. 2 L 7 2 4F RT A2NM 1999020500159 19990205 00159 NM 1999 2 5 UPS99228546 1 19990125 A 5753 65192086 TRACK BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, NR 7 FLAP TRACK HAS CORROSION ON FWD O/B MOUNT 106, O/B SIDE. REPLACED TRACK IAW MM 27-51-31. 2 L 7 3 4F A3WE 1999020500160 19990205 00160 NM 1999 2 5 UPS99228547 1 19990127 A 5210 ANGLE BOEING 727 72725C 138400H NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, FWD ENTRY DOOR TRANSVERSE BEAM IS CRACKED WL 223 BS 336 LBL 65. REMOVED AND REPLACED L ANGLE FWD LO WER AFT POSITION (DOOR CLOSED) AND REINSTALLED LOWER TRANSVERSE BEAM PANEL REMOVED FOR ACCESS PER 727 SRM 51-30-2, 51-20 -1 AND MM 52-11-0. 2 L 7 3 4F A3WE 1999020500161 19990205 00161 NM 1999 2 5 UPS99228548 1 19990127 A 5730 SKIN BOEING 727 72725C 138400H NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION ON UPPER AND LOWER SURFACE OF LEFT WING FUEL TANK ACCESS CUTOUT 7205. REPAIRED WING SKIN PER ER 99-5021. 2 L 7 3 4F A3WE 1999020500162 19990205 00162 NM 1999 2 5 UPS99228549 1 19990112 A 5521 RIB BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR 4 CRACK INDICATIONS NOTED ON X-RAYS VIEW 13 ALONG LEADING EDGE 79 TO 99 ELEV STA. RT EL EVATOR WAS REMOVED AND REPLACED ON NRC NR 838862. 2 L 7 3 4F A3WE 1999020500163 19990205 00163 NM 1999 2 5 UPS99228550 1 19990112 A 5521 RIB BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 31 ON 1ST RIB FWD OF REAR SPAR AT ELEVATOR STATION 200. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862. 2 L 7 3 4F A3WE 1999020500164 19990205 00164 NM 1999 2 5 UPS99228551 1 19990112 A 5521 SPAR BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 28, 8. RT ELEVATOR WAS REMOVED AND REPLACED ON CAR D NR 838862. 2 L 7 3 4F A3WE 1999020500165 19990205 00165 NM 1999 2 5 UPS99228552 1 19990112 A 5521 SPAR BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATIONS NOTED ON X-RAY VIEW 24, 8 AFT OF FRONT SPAR ELEV STA 167. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862. 2 L 7 3 4F A3WE 1999020500166 19990205 00166 NM 1999 2 5 UPS99228553 1 19990112 A 5521 SPAR BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAYS VIEW 22 FRONT SPAR OUT OF FASTENER HOLE AT ELEV STA 150 . RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862. 2 L 7 3 4F A3WE 1999020500167 19990205 00167 NM 1999 2 5 UPS99228554 1 19990112 A 5521 RIB BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 20 ELEV STA 130, 6 AFT OF FRONT SPAR. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862. 2 L 7 3 4F A3WE 1999020500168 19990205 00168 NM 1999 2 5 UPS99228555 1 19990112 A 5521 RIB BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY AT VIEW 16 10 AFT OF LEADING EDGE AT ELEV STA 125. RT E LEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862. 2 L 7 3 4F A3WE 1999020500169 19990205 00169 NM 1999 2 5 UPS99228556 1 19990112 A 5521 RIB BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 7 ON 1ST RIB AFT OF FRONT SPAR AT ELEV STA 40. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862. 2 L 7 3 4F A3WE 1999020500170 19990205 00170 NM 1999 2 5 UPS99228557 1 19990112 A 5521 RIB BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, RT ELEVATOR 2 CRACK INDICATIONS NOTED ON X-RAYS VIEW 14 AT ELEV STA 99 8 AND 10 FROM LEADING EDGE. R T ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862. 2 L 7 3 4F A3WE 1999020500171 19990205 00171 NM 1999 2 5 UPS99228558 1 19990127 A 5754 SKIN BOEING 727 72725C 138400H NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE-C, NR 4 K-FLAP AND BULLNOSE ARE CORRODED AT INBD LOWER BONDING JUMPER ATTACHMENT POINTS. REPLACED K-FLA P PER MM 27-81-01 AND ADJUST/TEST PER 727 MM 27-81-00. 2 L 7 3 4F A3WE 1999020500172 19990205 00172 WP 1999 2 5 ABXA9900040 1 19990127 A 5250 AR25291GR41 LATCH DOUG DC9 DC931 3022065 WP COCKPIT DOOR DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 COCKPIT ENTRY DOOR LATCH STICKS, WOULD NOT RELEASE. REPLACED COCKPIT ENTRY LATCH. 2 L 7 2 4F A6WE 1999020500173 19990205 00173 NM 1999 2 5 DL72L990161 1 19990123 A 5320 651751090 CHORD BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 THE I/B UPPER CHORD OF THE RT VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A 1 INCH TYPICAL CRACK AT FS 1273. THE DAMAGED SECTION OF CHORD WAS REMOVED AND A NEW SECTION SPLICED PER BAC S/B 727-53-0129. THE REPAIR WAS DOCUMENTED PER ER/A 366 542-14AD. 2 L 7 3 4F A3WE 1999020500174 19990205 00174 NE 1999 2 5 DL72S990167 2 19990126 A 7261 O RING BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 538DA 22076 ENGINE NR 2 LOW OIL PRESS LIGHT ON, QYT GAUGE TO ZERO AND OIL PRESS EVENTUALLY TO ZERO. SHUT DOWN NR 2 ENG PER POM. RE PAIRED OIL LEAK AT BANJO FITTING. 2 L 7 3 4F 4 F A3WE E2EA 1999020500175 19990205 00175 NE 1999 2 5 DL72S990168 2 19990124 A 7314 FUEL PUMP 3782018 BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 546DA 5390 22677 695201 AT FL 330, AFTER DEPARTURE SAT, NR 3 ENG FLAMEOUT. ALL IND NORMAL. FOUND FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACE D FUEL PUMP AND FUEL CONTROL RAN ENG PER PFHB TEST. 2 L 7 3 4F 4 F A3WE E2EA 1999020500176 19990205 00176 NM 1999 2 5 DL72S990169 1 19990126 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 480-500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 485 AND STRINGER 28R. THE CORROSION WAS REMOVED WITH A 7 X 3.5 CUTOUT. THERE WERE THREE OTHER REPAIR DOUBLERS NEAR THIS AREA FOR REPAIRS OF SIMILAR CUTOUTS. THE REPAIRS WERE REM OVED RESULTING IN 4 SKIN CUTOUTS BETWEEN FS 480 AND 500 AND BETWEEN S-27R AND 27L. THE CUTOUTS WERE REPAIRED WITH AN EX TERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 366528-14. 2 L 7 3 4F A3WE 1999020500177 19990205 00177 NM 1999 2 5 DL73K990170 1 19990126 A 5330 6545778 SKIN BOEING 737 737232 1384475 NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307DL 23079 THE AFT ENTRY DOOR CUTOUT WAS FOUND WITH A .25 INCH LONG TYPICAL CRACK IN THE LOWER DOOR HINGE CUTOUT. THE CRACK WAS IN THE SKIN AND BONDED DOUBLER ONLY. THE DAMAGED SKIN ASSY WAS CUT AWAY AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER A ND STEEL TRIPLER PER THE GUIDELINES OF B737 SRM 53-30-3, FIG 34. THE REPAIR WAS ACCOMPLISHED PER ER/A 366544-14, REV A. 2 L 7 2 4F RT A16WE 1999020500178 19990205 00178 NM 1999 2 5 DL72S990172 1 19990128 A 2782 BRACKET BOEING 727 727225 1384077 NM NR 8 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 REF E - 2 LETTER CHECK TPA, NR 8 SLAT ACT MOUNT BRACKETS CRACKED AT I/B AND O/B SIDES. INSTALLED DOUBLERS PER M/M 57-20 -21. 2 L 7 3 4F A3WE 1999020500182 19990205 00182 NM 1999 2 5 DL72S990176 1 19990127 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 405DA 6465 21149 FOUND ON PREFLIGHT, LT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS NORMAL. 2 L 7 3 4F A3WE 1999020500183 19990205 00183 NM 1999 2 5 DL72L990177 1 19990108 A 5753 652163262 SKIN BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 I/B DRIVE ROD CUTOUT IN COVE SKIN IS CRACKED AT O/B AFT CORNER. REPAIRED PER M/M 57-52-0 FIG 809, ON SHOP ORDER 643487. 2 L 7 3 4F A3WE 1999020500184 19990205 00184 NM 1999 2 5 DL72S990178 1 19990124 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 DURING ACCOMPLISHMENT OF LFEC INSPECTIONS OF THE LOWER ROW OF FASTENERS IN THE STRINGER 4R LAP SPLICE OF THE FS 360 TO 4 81 PANEL, CRACK INDICATIONS WERE NOTED. INTERNAL HFEC INSPECTION OF THE LOWER ROW OF FASTENERS OF THE LOWER SKI N PANEL CONFIRMED 11 CRACKS ALONG THE LENGTH OF THE LAP. THE ENTIRE LAP AREA WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND FILLER PER ER/A 366513-14, REV B. 2 L 7 3 4F A3WE 1999020500185 19990205 00185 NM 1999 2 5 DL72S990179 1 19990125 A 5330 655457460 SKIN BOEING 727 727232 1384082 NM BS 481-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE ON THE PANEL BETWEEN FS 481 AND 680 INDICATED POSSIBLE CRACKS. INTER NAL HFEC INSPECTION OF THE LOWER ROW OF FASTENERS IN THE LOWER SKIN PANEL CONFIRMED A TOTAL OF 46 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH. THE SKIN WAS RESPLICED WITH AN EXTERNAL ALUMINUM D OUBLER PER ER/A 366514-14, REV A. 2 L 7 3 4F A3WE 1999020500186 19990205 00186 NM 1999 2 5 DL72S990180 1 19990125 A 5330 655457463 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 LFEC INSPECTION OF THE STRINGER 4R LAP SPLICE ALONG THE PANEL LENGTH FROM FS 681 TO 740 INDICATED POTENTIAL CRACKS IN TH E LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 31 CRACKED FASTENER HOLES ALONG THE LOWER FASTENER ROW OF THE LOW ER SKIN PANEL. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE LENGTH OF THE SKIN PANELS. THE CUT SPLICE WAS RE PAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366515. 2 L 7 3 4F A3WE 1999020500187 19990205 00187 NM 1999 2 5 DL72S990182 1 19990128 A 5320 WEB BOEING 727 727232 1384082 NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 A .5 INCH CRACK AT UPPER TORQUE BOX VERTICAL WEB STA 1233 RT SIDE AT UPPER ROW OF HORIZONTAL RIVETS. REPAIRED PER M/M 5 3-11-0 FIG 819. 2 L 7 3 4F A3WE 1999020500188 19990205 00188 NM 1999 2 5 DL72S990183 1 19990128 A 5320 WEB BOEING 727 727232 1384082 NM BS 1213 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 A 1.5 INCH CRACK AT TORQUE BOX VERTICAL WEB STA 1213 LT SIDE AT HORIZONTAL ROW OF RIVETS. REPAIRED PER M/M 53-11-0 FIG 819. 2 L 7 3 4F A3WE 1999020500189 19990205 00189 NM 1999 2 5 DHL99721001 1 19990127 A 2780 H1010262 SWITCH BOEING 727 727228 NM NR 6 LE FLAP FAILED A DHLA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 721DH 19545 NR 6 L/E KRUEGER FLAP FAILED TO RETRACT AFTER TAKEOFF. COMPLETED ABNORMAL PROCEDURES, RETURNED TO SJU FOR LANDING. REM OVED ANF, REPLACED SWITCH ON NR 6 KRUEGER FLAP. 2 L 7 3 4F A3WE 1999020500190 19990205 00190 SO 1999 2 5 SWIA971373 1 19990104 A 3000 MONITOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DEICE SYST FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 234SW 120308 LEFT ENGINE INLET FAILED TWICE AND RIGHT INBOARD STABILIZER FAILED TWICE. RETURNED TO FAT. REMOVED AND REPLACED DEICE MONITOR, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999020500191 19990205 00191 SO 1999 2 5 SWIA971374 1 19990104 A 3020 16321 TIMER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 217SW 120286 LEFT ENGINE INLET FAILED 3 TIMES. RESET PER QRH AND AFTER 5 SECONDS KEPT ON FAILING. RETURNED TO FAT. REPLACED LEFT E NGINE INLET DEICE TIMER IAW MM 30-60-01, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999020500192 19990205 00192 SO 1999 2 5 SWIA971375 1 19990105 A 3020 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 217SW 120286 INFLIGHT LEFT ENGINE INLET DEICE FAIL. FOLLOWED QRH. RETURNED TO FAT. REPLACED LEFT INLET EJECTOR VALVE AND SERVICED DEICE SYSTEM WITH ALCOHOL LUBE MIX. 2 L 7 2 4T 4 T RT A31SO E20NE 1999020500193 19990205 00193 SO 1999 2 5 SWIA971376 1 19990105 A 3020 DEICE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE INLET FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 217SW 120286 IN FLIGHT LEFT ENGINE INLET DEICE FAILED, FOLLOWED QRH. RETURNED TO FAT. REPLACED FLEX HOSE TO LEFT ENGINE INLET DEICE BOOT. RAN ENGINES, COULD NOT DUPLICATE FAILURE. SWAPPED PRESSURE SWITCHES RIGHT TO LEFT INLETS FOR TROUBLESHOOTING. 2 L 7 2 4T 4 T RT A31SO E20NE 1999020500194 19990205 00194 EA 1999 2 5 SWIA971377 1 19990105 A 2913 PUMP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT ENGINE FAILED A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 409SW 7056 NUMBER ONE HYDRAULIC QUANTITY DROPPED TO 35 PERCENT EN ROUTE. RETURNED TO SLC. INSTALLED SERVICEABLE HYDRAULIC PUMP ON LEFT ENGINE IAW MM 29-13-00. OPS AND LEAKS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999020500195 19990205 00195 NM 1999 2 5 VNAA9901025 1 19990123 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DIRTY A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 425JS 3037 THE LEFT PROPELLER MOVED TO THE FEATHER POSITION WHEN POWER LEVERS WERE ADVANCED TO FLIGHT IDLE. THE AIRCRAFT RETURNED T O THE GATE. OUTSTATION MAINTENANCE CLEANED THE LT ENGINE SENSOR HARNESS CONNECTORS IN ACCORDANCE WITH DORNIER MAINTENAN CE MANUAL 73-21-00, 73-21-01 AND 61-23-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999020500196 19990205 00196 NM 1999 2 5 VNAA9901026 1 19990122 A 5522 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ELEVATOR LIGHTNING STRIKE A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 328LS 3025 DURING THE CRUISE FLIGHT INTO PIT, THE CREW REPORTED HAVING A LIGHTNING STRIKE. THE FLIGHT CONTINUED TO PIT WITHOUT FUR THER INCIDENT. PIT MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT HAND ELEVATOR AND R IGHT HAND FUSELAGE SIDE. THE AIRCRAFT WAS INSPECTED AND APPROVED FOR A FERRY FLIGHT TO CAK FOR REPAIRS. CAK MAINTENANC E INSPECTED AND REPLACED THE LEFT HAND ELEVATOR PER JIC 55-20-00. THE DAMAGE ON THE FUSELAGE WAS REPAIRED, IN ACCORDANC E WITH RAS 328-53-624. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999020500203 19990205 00203 NM 1999 2 5 VNAA9901023 1 19990125 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP GOV DIRTY A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 440JS 3058 THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A LEFT HAND PROPELLER OVERSPEED TEST FAILURE. MAINTENANCE INSPECTED AND CLE ANED THE CANNON PLUG ON THE LEFT HAND PROPELLER OVERSPEED GOVERNOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21- 01. OPERATIONAL CHECKS WERE COMLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999020500204 19990205 00204 1999 2 5 VNAA9901024 4 19990127 A 3425 HG2010AC02 AHRS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E & E COMPT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 424JS 80036 2268 3033 THE AIRCRAFT RETURNED TO THE FIELD AFTER RECEIVING A FLIGHT DIRECTOR, FLIGHT GUIDANCE AND A LEFT ATTITUDE FAIL WARNING M ESSAGES. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ATTITUDE HEADING REFERANCE (AHRS) COMPUTER, IN ACCORDANCE WITH DOR NIER MAINTENANCE MANUAL 34-21-20. OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999020500328 19990205 00328 EU 1999 2 5 MALA976325 1 19990129 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU AVIONICS COMPT MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 79XJ 079 AVIONICS SMOKE ILLUMINATED DURING FLIGHT, CREW COMPLETED QRH. MAINTENANCE COULD NOT DUPLICATE. REMOVED AVIONICS DOOR A ND INSPECTED AREA FOR SMOKE AND EVIDENCE FOR OVERHEAT, NOTHING NOTED. NO SMELL OF SMOKE. PERFORMED SMOKE DETECTOR TEST IAW 26-13-00. 2 L 7 2 4T RT A52EU 1999020500329 19990205 00329 1999 2 5 MALA976326 4 19990130 A 3425 6226190113 AHRS SAAB SF340 340B 7860101 EU LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 408XJ 408 LEFT HEADING RED/YELLOW FLAG INTERMITTMENT, UNABLE TO SYNC. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED LT AHRS COM PUTER. NR 1 AHRS TESTS GOOD IAW SAAB MM. 2 L 7 2 4T RT A52EU 1999020500330 19990205 00330 1999 2 5 MALA976327 4 19990131 A 3425 6226190113 AHARS SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 453XJ 453 HEADING COMPARTOR CAME ON IN FLIGHT AND WOULD NOT SLAVE 12 DEGREES DIFFERENCE, SLOWLY CORRECTED TO 8 DEGREES. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE AHARS COMPUTER. SYSTEM OPS CHECK GOOD IAW SF 340 MM 34-20-00. 2 L 7 2 4T RT A52EU 1999020500331 19990205 00331 NM 1999 2 5 AWXA9900035 1 19990127 A 2421 106122410 GENERATOR BOEING 737 7372U9 1384498 NM NR 1 ENGINE MALFUNCTIONED A AWXA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 28 149AW 22575 AIR TURNBACK, NR 1 GENERATOR TRIPPED OFF IN CLIMB. UNABLE TO CONNECT AUX PWR UNIT TO BUS. NR 1 ENG BUS OFF LIGHT ILLUM IN FLT, WOULD NOT RESET. APU GEN WOULD NOT CONNECT TO NR 1 MAIN BUS THOUGH APU SHOWED 115V 409HZ. APU DID CONNECT AT GATE ON GROUND AFTER ARRIVAL BUT DROPPED OFF AFTER 3 MINUTES. REMOVED AND REPLACED NR 2 BUS TIE BREAKER FOR APU (BAD AU X CONTACTS) PER A8M24001. REMOVED AND REPLACED NR 1 GEN FOR NR 1 GEN TRIP FAULT PER R5M24002, ALL FUNCTIONS NORMAL. 2 L 7 2 4F RT A16WE 1999020500332 19990205 00332 NE 1999 2 5 CALA9900089 2 19990129 A 7230 SEAL BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE BROKEN A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 13624 27528 859101 SMOKE APPEARED IN THE COCKPIT AND CABIN DURING CLIMB-OUT OF EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHO UT INCIDENT. A BOROSCOPE INSPECTION OF THE NR 1 ENGINE HPC 1ST, 2ND, AND 3RD STAGES FOUND EVIDENCE OF OIL LEAK IN ALL S TAGES. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AT TAKEOFF POWER WITH NO SMOKE OR DEFECTS NOTED. E NGINEERING INVESTIGATION REVEALED THE NR 3 BEARING STATIONARY AFT AIR/OIL SEAL HAD BROKEN INTO THREE PIECES AND WAS THE PRIMARY CAUSE OF ENGINE OIL LEAK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999020500333 19990205 00333 WP 1999 2 5 CALA9900090 1 19990127 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1871 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOOR SUPPORT CORRODED IN MAIN DECK AT STA 1871 NEAR LAV E. THE FLOOR SUPPORT WAS REMOVED AND A NEW SU PPORT WAS INSTALLED IAW SRM 53-70-00, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1999020500334 19990205 00334 WP 1999 2 5 CALA9900091 1 19990128 A 3350 60030431 POWER SUPPLY GRIMES DOUG DC9 DC932 3022066 WP EMER EXIT INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15525 47531 THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE B5-25 POWER SUPPLY AT STA 635 WAS REM OVED AND REPLACED. 2 L 7 2 4F A6WE 1999020500335 19990205 00335 WP 1999 2 5 CALA9900092 1 19990128 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND AFT CARGO DOOR THIRD BEAM END FITTING CRACKED AT AFT SIDE OF DOOR. THE CRACK WAS .1875 INCH LONG. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999020500336 19990205 00336 WP 1999 2 5 CALA9900093 1 19990129 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND THE ESCAPE PATH LIGHT INBOARD OF FORWARD FIRST CLASS COAT CLOSET INOPERATIVE. MAINTENANCE FOUND BROKEN WIRING. THE ESCAPE PATH LIGHT WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE 501. 2 L 7 2 4F A6WE 1999020500337 19990205 00337 WP 1999 2 5 CALA9900094 1 19990129 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A .75 INCH CRACK IN OUTBOARD RADIUS OF MAIN CABIN DOOR TOP NR 1 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999020500338 19990205 00338 WP 1999 2 5 CALA9900095 1 19990129 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A .5 INCH CRACK IN FORWARD SERVICE DOOR NR 4 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SR M 51-30. 2 L 7 2 4F A6WE 1999020500339 19990205 00339 WP 1999 2 5 CALA9900096 1 19990130 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP L1 DOOR DIRTY A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND THE L-1 PORTABLE EMERGENCY LIGHT INOPERATIVE. THE CONNECTOR WAS CLEANED AND SECURED AND OPERATION OF T HE LIGHT CHECKED GOOD. 2 L 7 2 4F A6WE 1999020500340 19990205 00340 NM 1999 2 5 9900262296 1 19990105 A 3232 731413 ACTUATOR BOEING 727 727251 138408H NM LT MLG DOOR INOP A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 296US 23863 8233 21788 DURING CLIMBOUT AFTER LANDING GEAR RETRACTION WITH LANDING GEAR HANDLE IN 'OFF' POSITION, THE LEFT MAIN LANDING GEAR DOO R LIGHT ILLUMINATED. CYCLED LANDING GEAR AND INDICATION REMAINED THE SAME. FLIGHT CONTINUED TO ORIGINAL DESTINATION AN D LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR ACTUATOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999020500341 19990205 00341 WP 1999 2 5 9900279997 1 19990122 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND FUSE, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999020500342 19990205 00342 WP 1999 2 5 9900281229 1 19990127 A 3350 BATTERY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 229NW 46551 DURING LINE CHECK, FOUND EMERGENCY PATH LIGHTS OUT IN FORWARD AFT SECTION OF CABIN. REPLACED BATTERY SOURCE, OPERATIONA L CHECK OK. 2 L 7 3 4F A22WE 1999020500343 19990205 00343 EA 1999 2 5 COMA9960053 1 19990128 A 2750 855D1003 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 986CA 329 7174 FLAPS FAIL MESSAGE WHILE CLIMBING THROUGH 21,000 FEET. REPLACED LEFT BPSU AND PERFORMED EO 27-046. 2 L 7 2 4F RT A21EA 1999020500344 19990205 00344 EA 1999 2 5 COMA9960052 1 19990128 A 2751 WARNING CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 986CA 7174 FLAP FAIL MESSAGE ILLUMINATED WHILE CLIMBING THROUGH 24,000 FEET. COMPLIED WITH EO 24-045 AND DEFERRED MAINT ACTION. 2 L 7 2 4F RT A21EA 1999020500345 19990205 00345 EA 1999 2 5 COMA9960050 1 19990130 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA ROW 8 LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 EMERGENCY FLOOR PATH LIGHTING AFT OF ROW 8 IS INOPERABLE. RECONNECTED STRIP LIGHTING, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1999020500346 19990205 00346 EA 1999 2 5 COMA9960051 1 19990130 A 2760 WARNING CNDAIR CL600 CL6002B19 EA SPOILERS ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 912CA 7011 TAKEOFF CONFIG WARNING SPOILERS. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF SPOILER SYSTEM WAS NORMAL. 2 L 7 2 4F RT A21EA 1999020500347 19990205 00347 NM 1999 2 5 UPS99228559 1 19990115 A 5753 6521631143 FOREFLAP BOEING 727 72725C 138400H NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE-C, LEFT WING O/B FOREFLAP HAS .25 X 3.5 AREA OF DELAMINATION. TAP TESTED, FOUND ADDITIONAL DELAMINATION . FOUND CORRSION ON SPAR. REPLACED O/B FOREFLAP. 2 L 7 3 4F A3WE 1999020500350 19990205 00350 WP 1999 2 5 UPS99828562 1 19990120 A 5320 564667429 STIFFENER DOUG DC8 DC871F 302199D WP BS 855 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, VERTICAL STIFFENER AT FS 855, LBL 55 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED STI FFENER IAW DWG 5646674 AND SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999020500351 19990205 00351 WP 1999 2 5 UPS99828563 1 19990104 A 5320 3754946501 FITTING DOUG DC8 DC871F 302199D WP BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 520 AT THE RT CUSP, THE FLOORBEAM TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW S RM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500352 19990205 00352 WP 1999 2 5 UPS99828564 1 19990104 A 5320 37502571 FITTING DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3 LONG 31R SPLICE FITTING IS CRACKED AT FS 440 TO 460. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500353 19990205 00353 WP 1999 2 5 UPS99828565 1 19990104 A 5320 3754220503 FITTING DOUG DC8 DC871F 302199D WP BS 200-220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 31L SPLICE FITTING AT FS 200 TO 220 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500354 19990205 00354 WP 1999 2 5 UPS99828566 1 19990106 A 5720 576985937 INTERCOSTAL DOUG DC8 DC871F 302199D WP WS 196 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING L/E, I/B OF THE I/B SLOT, STA XFS 196, THE INTERCOSTAL WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE INTERCOSTAL IAW DWG 5769859 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500355 19990205 00355 WP 1999 2 5 UPS99828567 1 19990110 A 5320 9754027509 DOUBLER DOUG DC8 DC871F 302199D WP BS 210-354 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 210 TO 354 AT LONG 31L, THE FINGER DOUBLER WASS CORRODED. REMOVED, FABRICATED AND REPLACED FINGE R DOUBLER IAW DWG 5755271 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 1999020500356 19990205 00356 WP 1999 2 5 UPS99828568 1 19990110 A 5320 5779921 DOUBLER DOUG DC8 DC871F 302199D WP BS 354-450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 354 TO 450 AT LONG 31L, THE FINGER DOUBLER WAS CORRODED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 AND 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 1999020500357 19990205 00357 WP 1999 2 5 UPS99828569 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING L/E RIB AT XOLDI 6.225, I/B SIDE IS CRACKED ABOVE THE PNEU DUCT. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999020500358 19990205 00358 WP 1999 2 5 UPS99828570 1 19990108 A 5330 SKIN DOUG DC8 DC871F 302199D WP SERVICE DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, THE FUSELAGE SKIN AT THE UPPER AFT CORNER OF THE RT AFT SERVICE DOOR WAS CRACKED. CUT OUT DAMAGED A REA AND REPAIRED IAW SRM 53-2-0 FIG 16. 2 L 7 4 4F RT 4A25 1999020500359 19990205 00359 WP 1999 2 5 UPS99828571 1 19990108 A 5313 37587301 LONGERON DOUG DC8 DC871F 302199D WP BS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 33R WAS CRACKED AT FS 1580. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500360 19990205 00360 NM 1999 2 5 99FDEA00031 1 19990129 A 5210 692842 STRAP BOEING 727 72725C 138400H NM PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 FWD ENTRY DOOR I/B TENSION STRAP ON NR 7 TRANSVERSE BEAM IS CORRODED (COUNTING FROM TOP). *S/D* REMOVED AND REPLACED N R 7 TRANSVERSE BEAM TENSION STRAP IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1999020500361 19990205 00361 NM 1999 2 5 99FDEA00029 1 19990127 A 5210 692842 STRAP BOEING 727 72725C 138400H NM PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 FORWARD ENTRY DOOR, I/B TENSION STRAP ON NR 1 TRANVERSE BEAM WAS CORRODED. *S/D* REMOVED AND REPLACED NR 1 TRANSVERSE BEAM TENSION STRAP PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1999020500362 19990205 00362 NM 1999 2 5 99FDEA00030 1 19990128 A 2120 AIR DIST BOEING 727 727233 138408A NM CABIN ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 219FE 21102 AN ODOR WAS NOTICED IN THE ENTRYWAY. INSPECTED UPPER DECK AREA, E & E COMP, LWR CARGO AREAS AND AFT AIRSTAIR AREA, RUN ENGINES AND OPERATED PACKS PER JET RUN HANDBOOK. COULD NOT DUPLICATE ODOR. OK TO CONTINUE. 2 L 7 3 4F RT A3WE 1999020500363 19990205 00363 WP 1999 2 5 ABXA9900041 1 19990128 A 5610 5912880508 SEAL DOUG DC9 DC932 3022066 WP RT COCKPIT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING MAINTENANCE CHECK, WAS UNABLE TO OPEN FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT). REPLACED FIRST OFFICER'S CL EARVIEW WINDOW SEAL. 2 L 7 2 4F A6WE 1999020500364 19990205 00364 NM 1999 2 5 MWEA99054 1 19990129 A 5330 49559471 SKIN DOUG MD88 MD88 3023688 NM PAX DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND NICKS AND GOUGES ON SKIN AROUND PASSENGER DOOR HOLD OPEN RECEPTICLE. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999020500365 19990205 00365 NM 1999 2 5 DL72L990184 1 19990126 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 500 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 A GOUGE WAS FOUND IN THE SKIN PANEL AT FS 500 BELOW THE STRINGER 26L LAP SPLICE. THE DAMAGE WAS TRIMMED OUT OF THE SKIN WITHOUT DAMAGING THE EXISTING LAP. THE CUTOUT WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366548- 14. 2 L 7 3 4F A3WE 1999020500366 19990205 00366 NM 1999 2 5 DL72S990185 1 19990128 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 480-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 AND 681 INDICATED POSSIBLE CRACKS IN THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 18 CRACK LOCATIONS IN LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE P ANEL. THE LAP SPLICE WAS CUT AWAY ALONG THE ENTIRE LENGTH OF THE LOWER SKIN PANEL AND REPAIRED WITH AND EXTERNAL ALUMIN UM DOUBLER PER ER/A 366543-14, REV B. 2 L 7 3 4F A3WE 1999020500367 19990205 00367 NM 1999 2 5 DL72S990187 1 19990129 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA 21144 TWO AISLE EMERGENCY EXIT SIGNS INOP AT AFT GALLEY AND AFT ENTRY DOOR. REPLACED BATTERY PACKS, OPS NORMAL. 2 L 7 3 4F A3WE 1999020500368 19990205 00368 NM 1999 2 5 DL72S990188 1 19990129 A 3350 LIGHT BOEING 727 727232 1384082 NM ROW 26DEF INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 517DA 21433 EMERGENCY PATH LIGHT OUT ROW 26DEF. REPAIRED EMERGENCY PATH LIGHTS ROW 26DEF. 2 L 7 3 4F A3WE 1999020500369 19990205 00369 WP 1999 2 5 DLL14990189 1 19990127 A 2421 IDG 729640 LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE FAILED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 1739D 5197 193C1237 5197 NR 2 ENG IDG DROPPED OFF LINE AT 33000 FT, LOW OIL PRESS ILLUMINATED, TEMP 100, RISE 25. DISCONNECT FAILED, 3G15 C/B PO PPED. RESET, DISCONNECT FAILED ON 2ND ATTEMPT, (PMG STILL ON) IDG OIL CLIMBED TO 150 RISE TO 35 DEG. IDG OIL CONTINUED TO RISE IN YELLOW ZONE. NR 2 ENGINE SHUTDOWN. REPLACED IDG. 2 L 7 3 4F A23WE 1999020500370 19990205 00370 NM 1999 2 5 DL76L990191 1 19990130 A 5210 RELEASE ROD BOEING 767 767332 1382001 NM L1 DOOR OUT OF ADJUST A DALA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 176DN 25061 L-1 DOOR WOULD NOT OPEN FROM INSIDE AFTER CYCLING SLIDE ARMING LEVER. ADJUSTED OUTER ARM/DISARM ROLLER RELEASE ROD, OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999020500371 19990205 00371 WP 1999 2 5 DLL14990192 1 19990130 A 3350 POWER SUPPLY LKHEED 1011 1011385115 5265015 WP L4 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 737D 193C1228 5197 L-4 AFT CABIN EMERGENCY LIGHTS AND L-4 EXTERIOR EMERGENCY LIGHTS FLASHING. REPLACED L-4 EMERGENCY LIGHT POWER SUPPLY, S YSTEM OPS CHECKS NORMAL. 2 L 7 3 4F A23WE 1999020500372 19990205 00372 NM 1999 2 5 DLM88990194 1 19990131 A 3350 61020 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 988DL 53339 FWD CABIN EMERGENCY FLASHLIGHT INDICATOR LIGHT INOP. REPLACED BATTERY AND BULB, NOW CKS GOOD. 2 L 7 2 4F RT A6WE 1999020500373 19990205 00373 NM 1999 2 5 SCNA99023 1 19990129 A 3350 1619 LIGHT BOEING 727 727282 138408T NM R1 DOOR INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE R1 DOOR EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED THE R1 DOOR EXTERIOR EMERGENCY LIGHT. LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999020500374 19990205 00374 NM 1999 2 5 SCNA99024 1 19990125 A 3150 SWITCH BOEING 727 7272J4 1384006 NM HORIZ STAB INOP A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 285SC 21676 DURING TAKEOFF ROLL, THE TAKEOFF WARNING HORN SOUNDED WHEN ENGINES NR 1 AND NR 3 REACHED 1.4 EPR. ABORTED TAKEOFF AND R ETURNED AIRCRAFT TO THE RAMP. REMOVED AND REPLACED THE STABILIZER UPPER TAKEOFF WARNING SWITCH S532 IAW MM 312624. OPE RATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999020500375 19990205 00375 WP 1999 2 5 SCNA99025 1 19990128 A 2530 8001070000 OVEN DOUG DC10 DC1015 3022118 WP GALLEY FAILED A SCNA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 153SY 398 48276 THE AFT OVEN, 2ND ONE FROM THE AFT, FAN SMOKES WHEN TURNED ON. REMOVED AND REPLACED THE OVEN, OPERATIONALLY CHECKS GOOD . 2 L 7 3 4F A22WE 1999020500376 19990205 00376 WP 1999 2 5 SCNA99026 1 19990131 A 3397 WIRE DOUG DC10 DC1015 3022118 WP R1 DOOR FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 151SY 48295 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK AFT OF THE R1 DOOR WAS FOUND TO BE INOPERATIVE. REPAIRED WIRE S ON THE EMERGENCY EXIT TRACK, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1999020500377 19990205 00377 NM 1999 2 5 DHL99717001 1 19990130 A 3297 WIRE BOEING 727 72723 1384004 NM NLG BROKEN A DHLA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 01 717DH 19389 ON DESCENT WITH THRUST LEVER TO IDLE, RED NOSE GEAR LIGHT DID NOT ILLUMINATE WITH GEAR HANDLE DOWN. ON GEAR EXT RED LIG HT DID NOT CYCLE GREEN LIGHT DID NOT ILLUMNATE. TOWER ADVISED L/G APPEARED NORMAL. ACCOMPLISHED NORMAL LANDING WITH GP WS AND HORN C/B PULLED. REPLACED NLG UPLOCK AND POS SWITCH. FOUND A REPAIRED BROKEN SPLICE ON NLG UPPER PSO SWITCH CAN NON PLUG GROUND WIRE. GREEN LIGHT OPS CHECK GOOD PER MM 33-00-00. 2 L 7 3 4F A3WE 1999020500378 19990205 00378 NM 1999 2 5 DHL99721002 1 19990130 A 2710 CONTROLS BOEING 727 727228 NM AILERON SYST MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 721DH 19545 WHEN AILERON INPUT IS APPLIED A NULL AREA OF 10 DEGREES LEFT AND RIGHT IS DETECTED WITH NO ROLL RESPONSE. AILERON TRIM SET 1 UNIT RT, RUDDER 0. INSPECTED AILERON MOVEMENT, NO DEFECT NOTED AND CHECK LOST MOTION DEVICE, FOUND TO BE WITHIN L IMITS PER MM 22-61-51. 2 L 7 3 4F A3WE 1999020500379 19990205 00379 NM 1999 2 5 DHL99724002 1 19990127 A 3230 1U108 VALVE BOEING 727 727228 NM LT MLG CRACKED A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 724DH 19862 DURING GEAR RETRACTION EXPERIENCED COMPLETE HYDRAULIC FLUID LOSS OF A SYSTEM. FOUND LEFT MAIN GEAR LOCK OPERATION SEQUE NCE VALVE CRACKED. REMOVED AND REPLACED VALVE PER MM 32-32-31, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999020500380 19990205 00380 NM 1999 2 5 DHL99741001 1 19990130 A 3150 CENTRAL WARNING BOEING 727 7272Q9 138448M NM COCKPIT MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 741DH 21931 INDICATOR LIGHTS AND APD TEST PERFORMED, THE FOLLOWING LIGHTS REMAINED ILLUMINATED AFTER SWITCH WAS RETURNED TO DIM OR B RIGHT POSITION: GPWS, PULL UP AND BELOW GS, ESS POWER WARNING, ENGINE LOW OIL PRESS, ELEVATOR LOW PRESS. CLEANED MASTER DIM AND TEST ON S 679 AND OPS CHECK OF SECTION 1 INDICATOR LIGHT GOOD PER MM 33-10-00. 2 L 7 3 4F RT A3WE 1999020500381 19990205 00381 NM 1999 2 5 HNAA9900021 1 19990130 A 5210 HANDLE DHAV DHC8 DHC8102 2809003 NM AIRSTAIR DOOR BINDING A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 914HA 053 UNABLE TO OPEN AIRSTAIR DOOR FROM OUTSIDE. HANDLE BINDING, REPLACED HANDLE STOP. 2 H 7 2 4T RT A13NM 1999020500382 19990205 00382 NM 1999 2 5 HNAA9900022 1 19990130 A 5310 STRUCTURE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 CORROSION RIGHT FUSELAGE ON STRINGER SPLICE AT STR 32S FRAME 488, SPLICE ON STR 29 AND AT FRAME 488, FRAME 433 LEG AT ST 31S, STR 29 .021 DEEP AT FRAME 529, SURFACE .006 DEEP ON SPLICE STR 28 AT FRAME 488, 7 AREAS RADIUS OF STR 31 MAX .013 DEEP BETWEEN FRAMES 291 AND 312, STR 31S AT FRAMES 253, 270, 291, 354, 333, 445, 370, 202, 312 AND 488, BETWEEN FRAMES 4 67 AND 488 .008 DEEP AND 467 (WITH VERTICAL MEMBER). SUPPORT BRACKET AT CROSS MEMBER FRAME 222, STR 28S AT FRAME 510, S TR 25S AT FRAME 255, STRINGERS 30S AND 29S AT FRAME 531, TENSION FITTINGS AT FRAME 202, STR 30S AT FRAME 259 .030 AND .0 24 DEEP, STRAP BOLTS BETWEEN FRAMES 467 AND 488, STRINGERS 30S, 31S, 29S AND 38S AT FRAME 488. 2 H 7 2 4T RT A13NM 1999020500384 19990205 00384 WP 1999 2 5 AT9900067 1 19990129 A 2820 FUEL DOUG DC9 DC932 3022066 WP RT WING VENTING A ZZDA O OTHER K FLUID LOSS CR CRUISE 1 SO 15 833AT 47489 FUEL VENTING FROM RIGHT WING FUEL VENT IN FLIGHT. BACK FLUSH FUEL SYSTEM BY TRANSFERRING FUEL BETWEEN ALL THREE TANKS. ALL FILL VALVES AND FUEL SHUT OFF VALVES OPERATE NORMAL. NO LEAKS OR VENTING OF FUEL NOTED, OK FOR SERVICE PER MM 28-2 0. 2 L 7 2 4F A6WE 1999020500386 19990205 00386 WP 1999 2 5 AT9900069 1 19990105 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT ELEVATOR OUTBOARD LOWER SIDE CORRODED. REPAIRED RIGHT ELEVATOR OUTB OARD LOWER SKIN BY FABRICATING SKIN AND FINGER DOUBLER. INSTALLED AND BALANCED IAW DC9 SRM 55-03 FIG 14 AND 51-30-2, 55 -20-01. 2 L 7 2 4F A6WE 1999020500388 19990205 00388 WP 1999 2 5 AT9900071 1 19990126 A 5730 SKIN DOUG DC9 DC932 3022066 WP BS 214 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ALL DOUBLERS DISBONDED AND CORROSION IN BETWEEN SKIN ON TOP OF LEFT WING T RAILING EDGE FLAP SKIN AT STA 214. REMOVED AND FABRICATED NEW SKIN AND 'T' CAP AND REINSTALLED IAW DC9 SRM 51-30-2, 51- 10-4, 51-10-2, 51-10-3 AND RES NR 99246. 2 L 7 2 4F A6WE 1999020500389 19990205 00389 WP 1999 2 5 AT9900072 1 19990130 A 3240 9560892 BRAKES DOUG DC9 DC932 3022066 WP LT MLG MALFUNCTIONED A ZZDA F ACTIVATE FIRE EXT. A FLAME/FIRE LD LANDING 1 SO 15 810AT 47277 UPON LANDING EVERYTHING WAS NORMAL, ON TAXI-IN IT FELT LIKE BRAKES WERE APPLIED, IT WOULD TAKE A SECOND OR TWO FOR IT TO RELEASE. AT NO TIME DID THE BRAKES DRAG TO THE EXTEND THAT THEY WERE GOING TO IGNITE. ON ARRIVAL AT THE GATE THE BRAK ES WERE SMOKING. THE FIRE DEPARTMENT ARRIVED, THE BRAKES WERE NOT BURNING. AFTER SEVERAL MINUTES FLAMES STARTED UP FR OM THE BRAKES AND AFTER A SHORT PERIOD THE FIRE WAS EXTINGUISHED. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE AND WHEEL AS SEMBLY DUE TO EXCESSIVE HEAT PER MM 32-40 AND 32-42-1. ALSO, BLED AND LEAKED CHECKED IAW MM 32-42-1. SYSTEM OPS CHECKE D GOOD. BRAKE ASSEMBLY (P/N 9560788-7) OFF. 2 L 7 2 4F A6WE 1999020500390 19990205 00390 WP 1999 2 5 AT9900073 1 19990129 A 3350 1819 LAMP DOUG DC9 DC932 3022066 WP TAIL CONE FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 814AT 47486 FOUND ON THE AFT ACCESSORY COMPARTMENT AFT POSITION TAIL CONE EVACUATION LAMPS LEFT AND RIGHT SIDE INOPERATIVE. REMOVED AND REPLACED LAMPS, SYSTEM CHECKED GOOD IAW MM 33-50. 2 L 7 2 4F A6WE 1999020500394 19990205 00394 EU 1999 2 5 MALA976328 1 19990128 A 5610 7256100502 WINDSHIELD SAAB SF340 SF340A 7850100 EU RT COCKPIT CRACKED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 46XJ 046 RIGHT FRONT WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO DTW. MAINTNENANCE REPLACED RIGHT WINDSHIELD IAW CHAP 56-10-05, OP S CHECK GOOD. 2 L 7 2 4T RT A52EU 1999020500395 19990205 00395 EU 1999 2 5 MALA976329 1 19990128 A 3610 7858023 VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 233CH 233 BLEED FAULT ILLUMINATED AFTER TAKEOFF ON RIGHT ENGINE, COMPLETED QRH AND BLEED FAULT STILL ILLUMINATES. AIRCRAFT RETURN ED TO DTW. MAINTENANCE REPLACED PRESSURE REGULATING VALVE AND BLEED PRESSURE SWITCH, OPS CHECK GOOD IAW SAAB AMM CHAPTE R 74. 2 L 7 2 4T 4 T RT A52EU E8NE 1999020500396 19990205 00396 EU 1999 2 5 AWXA9900036 1 19990129 A 2612 FIRE CARD AIRBUS 320 A320232 3930326 EU NR 2 ENGINE LOOSE A AWXA K NONE N FALSE WARNING CR CRUISE 1 WP 28 638AW 455 INFLIGHT ENG NR 2 FIRE LIGHT ON MASTER SWITCH PANEL AND OVERHEAD PUSH BUTTON ILLUMINATED AND STAYED ON, EVEN AFTER SHUTD OWN. TROUBLESHOT SYSTEM TO NR 2 ENGINE 'B' LOOP. SWAPPED AND REPACKED THE 5LP AND THE 18LP CARD PER MM-33-14-33, SYSTE M TESTED NORMAL. ALSO, FOUND THE LP5 CARD NOT SECURED. ALL CARDS SECURED, SYSTEM TEST GOOD AT THIS TIME. 2 L 7 2 4F RT A28NM 1999020500397 19990205 00397 EU 1999 2 5 AWXA9900037 1 19990130 A 3610 DUCT AIRBUS 320 A320232 3930326 EU BLEED AIR SYST FAILED A AWXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 28 638AW 455 DIVERSION, PRECAUTIONARY LANDING MADE AT DSM. AIR WING LEAK, AIR APU BLEED LEAK, DETECTED BY ECAM. PRESSURIZATION WAS LOST FOR A SHORT TIME. MESSAGE CLEARED AND SYSTEM RESET, OPS NORMAL AFTER THAT. FOUND SEPARATED BLEED DUCT AT GROUND A IR START TO MANIFOLD. REMOVED AND REPLACED DUCT ASSEMBLY, OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT LANDED IN DSM IN AN OVERWEIGHT CONDITION. AIRCRAFT WEIGHED 143,000 LBS. TOUCHDOWN VERTICAL SPEED LESS THAN 100 FEET PER MINUTE. EMERGENCY DECLARED, DISPATCH NOTIFIED. FOUND TO BE WELL WITHIN OVERWEIGHT LANDING LIMITS AS VERTICAL SPEED WAS LESS THAN 360 FEE T PER MINUTE AT TOUCHDOWN. NO FURTHER CHECKS REQUIRED. 2 L 7 2 4F RT A28NM 1999020500406 19990205 00406 NM 1999 2 5 RAAA99B1001 1 19990201 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 14 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 14 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999020500417 19990205 00417 SO 1999 2 5 COMA9910026 1 19990202 A 5411 12042266001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 LEFT NACELLE, FRAME WEB NR 10 CRACKED AT INBOARD RADIUS OF THE FLANGE. REPAIRED BY SPLICING IN A NEW FLANGE PER AERODES IGN REPORT NR 1076-2 AND EMB120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 1999020500418 19990205 00418 SO 1999 2 5 COMA9910027 1 19990131 A 2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 179CA 120179 FLAP DISAGREEMENT WARNING ATER TAKEOFF. CLEANED DIRT FROM FLAP TRUCKS. 2 L 7 2 4T RT A31SO 1999020500419 19990205 00419 SO 1999 2 5 COMA9910028 1 19990130 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 120233 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN ASSY. 2 L 7 2 4T RT A31SO 1999020500420 19990205 00420 EA 1999 2 5 COMA9960054 1 19990201 A 2751 WARNING CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 967CA 7134 FLAPS FAIL MESSAGE AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. INSPECTED FLAP SYSTEM, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999020500421 19990205 00421 WP 1999 2 5 UPS99828575 1 19990102 A 5320 370296 FITTING DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 35R END FITTING AT FS 55 IS CRACKED. REMOVED, FABRICATED AND REPLACED END FITTING IAW DWG 3702 969 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999020500422 19990205 00422 WP 1999 2 5 UPS99828576 1 19990103 A 5311 2641520 FRAME DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 55 FRAME AT LONG 24L IS CRACKED. CUT OUT DAMAGED FRAME SECTION AND REPAIRED IAW SRM 53-2-0 FIG 2 . 2 L 7 4 4F RT 4A25 1999020500423 19990205 00423 WP 1999 2 5 UPS99828577 1 19990104 A 5320 561306481 ANGLE DOUG DC8 DC871F 302199D WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 70 FRAME ANGLE AT LONG 25R IS CRACKED. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-5 FIG 8 C-2. 2 L 7 4 4F RT 4A25 1999020500424 19990205 00424 WP 1999 2 5 UPS99828578 1 19990105 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 25 FRAME AT LONG 35R IS CORRODED OUT OF LIMITS. CUT OUT DAMAGED SECTION OF FRAME AND REPAIRED IA W SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999020500425 19990205 00425 WP 1999 2 5 UPS99828579 1 19990106 A 5320 37592581 FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 35L SPLICE FITTING AT FS 1260 TO 1280 HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500426 19990205 00426 WP 1999 2 5 UPS99828580 1 19990106 A 5320 37592582 FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 35R SPLICE FITTING AT FS 1260 TO 1280 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 1999020500427 19990205 00427 WP 1999 2 5 UPS99828581 1 19990106 A 5320 37558451 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, HEAVY CORROSION ON BATHTUB FITTING, FWD SIDE OF FS 1220 BETWEEN LONG 34L TO 35L. REMOVED AND REPLAC ED FITTING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999020500428 19990205 00428 WP 1999 2 5 UPS99828582 1 19990108 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 1600-1670 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, INTERNAL DOUBLER AT LONG 31R FS 1600 TO 1670 IS CORRODED. REPAIRED DOUBLER IAW DHC SK713-220. 2 L 7 4 4F RT 4A25 1999020500429 19990205 00429 WP 1999 2 5 UPS99828583 1 19990110 A 5320 57552717 DOUBLER DOUG DC8 DC871F 302199D WP BS 400-450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 31R BETWEEN FS 400 TO 450 IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REPLACED DOUBLER IA W DWG 5755271 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999020500430 19990205 00430 WP 1999 2 5 UPS99828584 1 19990110 A 5320 5615377199 DOUBLER DOUG DC8 DC871F 302199D WP BS 1620-1670 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, INTERNAL DOUBLER AT LONG 31L FS 1620 TO 1670 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REP LACED FINGER DOUBLER IAW DHC SK713-220 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999020500431 19990205 00431 WP 1999 2 5 UPS99828585 1 19990111 A 5320 577991529 CLIP DOUG DC8 DC871F 302199D WP BS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 1080, FWD SIDE AT LONG 35L, THE INTERCOSTAL ATTACH CLIP IS CORRODED BEYOND LIMITS. REMOVED, FABR ICATED AND REPLACED CLIP IAW SRM 51-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500432 19990205 00432 WP 1999 2 5 UPS99828586 1 19990107 A 5711 FRAME DOUG DC8 DC873F 302199F WP WS 495 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, LT WING O/B LEADING EDGE STA 495 FRAME CRACKED AT PNEU DUCT SUPPORT. FABRICATED DOUBLER IAW DC8 S RM 57-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500433 19990205 00433 WP 1999 2 5 UPS99828587 1 19990111 A 5320 975962924 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1060-1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 1060 TO 1080 AT LONG 35L, THE INTERCOSTAL LWR T IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED A ND REPLACED T IAW DWG 9759629 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500434 19990205 00434 WP 1999 2 5 UPS99828588 1 19990104 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, MAIN CABIN, LONG 3L END FITTING CRACKED FWD SIDE OF STA 680. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500435 19990205 00435 WP 1999 2 5 UPS99828589 1 19990112 A 5320 47585721 FITTING DOUG DC8 DC871F 302199D WP BS 1560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 33R END FITTING AT FS 1560 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1999020500436 19990205 00436 WP 1999 2 5 UPS99828590 1 19990104 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, MAIN CABIN LONG END FITTING FWD SIDE OF STA 680 FRAME. REMOVED AND REPLACED FITTING IAW DC8 SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1999020500437 19990205 00437 WP 1999 2 5 UPS99828591 1 19990104 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, MAIN CABIN LONG 10R END FITTING CRACKED FWD SIDE OF STA 680 FRAME. REMOVED AND REPLACED FITTING I AW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500438 19990205 00438 WP 1999 2 5 UPS99828593 1 19990104 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, MAIN CABIN LONG 6R END FITTING CRACKED FWD SIDE OF STA 857 FRAME. REMOVED AND REPLACED FITTING IA W DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500439 19990205 00439 WP 1999 2 5 99FDEA00032 1 19990201 A 5711 SPAR WEB DOUG DC10 DC1010F 3022111 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 391FE 46625 NR 129 - RT WING REAR SPAR WEB HAS CRACK EMANATING INBD FROM RADIUS OF APU FUEL PUMP HOLE. CRACK APPROX 2.5 INCHES IN L ENGTH VER BY NDT. STOP DRILLED CRACK AND PLUG HOLE IAW SRM 51-00-02 AND 53-00-01 WEB DOUBLER INSTALL PER EA 8-5710-4041 7. 2 L 7 3 4F A22WE 1999020500440 19990205 00440 NM 1999 2 5 99FDEA00033 1 19990129 A 2782 ACTUATOR BOEING 727 727233 138408A NM LE FLAP FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 265FE 21671 TOTAL HYD SYS A FAILURE AT GEAR UP AFT T/O. BOTH FLUID A SWITCH OFF. ENG SHUTDOWN. REMOVED AND REPLACED NR 4 ACTUATOR IAW MM 27-81-22 PG 401. 2 L 7 3 4F RT A3WE 1999020500441 19990205 00441 NM 1999 2 5 99FDEA00034 1 19990130 A 3220 LANDING GEAR BOEING 727 72722 1384002 NM NOSE VIBRATED A FDEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 184FE 18870 VIBRATION IN THE AREA OF NOSE WHEEL AND A FLICKER OF A RED DOOR LIGHT ABOVE GEAR HANDLE. WHEN GEAR LEVER WAS RAISED NO ADDITIONAL VIB WERE FELT. INSPECTED NOSE GEAR WHEEL WELL DOOR CABLES AS PER MM 32-22-21 PG 601. NO DEFECTS FOUND. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999020500442 19990205 00442 WP 1999 2 5 ABXA9900042 1 19990128 A 5320 29207531 ANGLE DOUG DOUG DC9 DC932 3022066 WP BS 617 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING C-CHECK, FOUND INTERCOSTAL ANGLE CORRODED AT STATION 617 LONGERON 17 RIGHT. REPLACED INTERCOSTAL ATTACH ANGLE I AW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999020500443 19990205 00443 WP 1999 2 5 ABXA9900043 1 19990127 A 5313 27779224 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING C-CHECK, FOUND LONGERON 16 LEFT CRACKED AT STATION 965. REPLACED SECTION OF LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999020500444 19990205 00444 WP 1999 2 5 ABXA9900044 1 19990127 A 5313 27779224 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 965. REPLACED SECTION OF LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999020500445 19990205 00445 WP 1999 2 5 ABXA9900045 1 19990126 A 5313 27779224 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 980. REPLACED LONGERON 17 RIGHT FROM STATION 955 TO 965 IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999020500446 19990205 00446 WP 1999 2 5 ABXA9900046 1 19990126 A 5313 27779221 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 256 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING C-CHECK, FOUND LONGERON 16 CRACKED AT STATION 256. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999020500447 19990205 00447 WP 1999 2 5 ABXA9900047 1 19990125 A 7830 5958775186 FAIRING DOUG DOUG DC9 DC932 3022066 WP NR 1 ENGINE TR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER OUTBOARD ACTUATOR FAIRING CRACKED. REPLACED OUTBOARD AFT FAIRING IAW DC9 SRM 51-30-2 AND 51-30-8. 2 L 7 2 4F A6WE 1999020500448 19990205 00448 WP 1999 2 5 ABXA9900048 1 19990201 A 5210 991556525 CHANNEL DOUG DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING C-CHECK, FOUND THE AFT ENTRY DOOR INTERNAL STIFFENER CRACKED AT UPPER HINGE. REPAIRED DOOR IAW ABX REA D952-2656 3MR. 2 L 7 2 4F A6WE 1999020500449 19990205 00449 WP 1999 2 5 MWEA99055 1 19990131 A 2560 11331 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 212ME 47701 THE FORWARD ENTRANCE DOOR ESCAPE SLIDE FELL OFF. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999020500450 19990205 00450 WP 1999 2 5 MWEA99056 1 19990131 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 502ME 48132 FORWARD ENTRANCE DOOR EMERGENCY SLIDE FELL OFF. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999020500451 19990205 00451 NM 1999 2 5 DHL9971201C 1 19990108 A 5320 CHANNEL BOEING 727 72729 1384007 NM BS 777 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, CABIN INTERIOR HAT CHANNEL CRACKED AT RIVET, RT FWD OVERWING EXIT DOOR CUTOUT LOWER SILL I/B SIDE B/S 777. R EPLACED CHANNEL PER SRM 51-40-3 25 BY 1 X 12 X 4. 2 L 7 3 4F A3WE 1999020500452 19990205 00452 NM 1999 2 5 DHL9971202C 1 19990111 A 5347 SEAT TRACK BOEING 727 72729 1384007 NM BS 789 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, CABIN SEAT TRACK WORN AT BL 0 CENTER TRACK BS 789. REMOVED AND REPLACED SEAT TRACK FROM BS 789 TO STA 850 PER SRM 51-10-5. 2 L 7 3 4F A3WE 1999020500453 19990205 00453 NM 1999 2 5 DHL9971203C 1 19990111 A 5347 SEAT TRACK BOEING 727 72729 1384007 NM BS 785 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, SEAT TRACK AT BL 0 BS 785 WORN. REMOVED SEAT TRACK FROM STA 760 TO 850 AND REPLACED PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999020500454 19990205 00454 NM 1999 2 5 DHL9971204C 1 19990111 A 5347 SEAT TRACK BOEING 727 72729 1384007 NM BS 740 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, CABIN SEAT TRACK WORN AT BL 0 CENTER TRACK BS 740. REMOVED SEAT TRACK AND REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999020500455 19990205 00455 NM 1999 2 5 DHL9971205C 1 19990107 A 5330 SKIN BOEING 727 72729 1384007 NM BS 1110-1183 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, SKIN BULGING FROM BETWEEN NR 2 ENGINE INLET AND STRINGER 4 LEFT FROM FS 1110 TO 1183. FOUND CORROSION BEYON D LIMITS AT A UPPER AND LOWER SKIN BETWEEN STR 4 AND 3 STA 1143. CUT OUT DAMAGED SECTION AND INSTALLED EXTERNAL REPAIR PER SRM 53-30-3, 22 X 18. 2 L 7 3 4F A3WE 1999020500456 19990205 00456 NM 1999 2 5 DHL9971206C 1 19990109 A 5320 INTERCOSTAL BOEING 727 72729 1384007 NM BS 1010-1030 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, AFT CARGO INTERCOSTAL CRACKED BS 1010 TO 1030 STR 27 RT. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-3, 20 X 4. 2 L 7 3 4F A3WE 1999020500457 19990205 00457 NM 1999 2 5 DHL9971207C 1 19990109 A 5320 INTERCOSTAL BOEING 727 72729 1384007 NM BS 970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, AFT CARGO INTERCOSTAL CORREDED BS 970L LBL 20. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-3, 20 X 4. 2 L 7 3 4F A3WE 1999020500458 19990205 00458 NM 1999 2 5 DHL9971208C 1 19990106 A 5320 65184158 ANGLE BOEING 727 72729 1384007 NM NLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, NLG RT FWD ANGLE 50 PERCENT EXFOLIATED. REMOVED TRUNNION FOR ACCESS, REMOVED UPPER CHORD ANGLE AND INSTALLE D NEW CHORD PER SRM 53-10-2. 2 L 7 3 4F A3WE 1999020500459 19990205 00459 NM 1999 2 5 DHL9971209C 1 19990112 A 5753 SKIN BOEING 727 72729 1384007 NM RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, RT I/B FLAP TRAILING EDGE FLAP DELAMINATING. INSTALLED BONDED REPAIR PER SRM 51-40-6, 3 X 7. 2 L 7 3 4F A3WE 1999020500460 19990205 00460 NM 1999 2 5 DHL9971210C 1 19990105 A 5730 SKIN BOEING 727 72729 1384007 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, SKIN ON TOP OF RT WING CRACKED AT NR 12 SPOILER I/B HINGE CUTOUT. STOP DRILLED CRACK, HFEC, INSTALLED DOUB LER REPAIR PER SRM 57-30-4, 5.5 X 4. 2 L 7 3 4F A3WE 1999020500461 19990205 00461 NM 1999 2 5 DHL9971211C 1 19990108 A 5730 SKIN BOEING 727 72729 1384007 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, SKIN ON TOP OF RT WING CRACKED AT NR 11 SPOILER O/B HINGE CUTOUT. STOP DRILLED CRACK, HFEC, INSTALLED DOUBL ER REPAIR PER SRM 57-30-4, 5.5 X 4. 2 L 7 3 4F A3WE 1999020500462 19990205 00462 NM 1999 2 5 DHL9971212C 1 19990108 A 5751 86553283 FITTING BOEING 727 72729 1384007 NM RT AILERON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, RIGHT WING TRAILING EDGE I/B AILERON CENTER HINGE FITTING FASTENER HOLE CORRODED. REPLACED FITTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999020500463 19990205 00463 NM 1999 2 5 DHL9971213C 1 19990109 A 5720 TIP BOEING 727 72729 1384007 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LEFT WING TIP CRACKED AND POPPED RIVETS AT UPPER TRAILING EDGE I/B SEAM. STOP DRILLED CRACKS, HFEC, INSTALL ED DOUBLER REPAIR PER SRM 57-20-5, 4 X 6. 2 L 7 3 4F A3WE 1999020500464 19990205 00464 NM 1999 2 5 DHL9971214C 1 19990109 A 5753 SKIN BOEING 727 72729 1384007 NM LT TE FOREFLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LT WING I/B FOREFLAP HAS SEVERAL SMALL DENTS AT LOWER SKIN. INSTALLED FILLER REPAIR PER SRM 51-40-1, 3 X 3 X 7 X 5, 3 X 3. 2 L 7 3 4F A3WE 1999020500465 19990205 00465 NM 1999 2 5 DHL9971215C 1 19990109 A 5753 SKIN BOEING 727 72729 1384007 NM LT TE FOREFLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, I/B FOREFLAP HAS A DEEP GOUGE AT CENTER LEADING EDGE. REPLACED ACCESS PANEL PER SRM 51-30-2, 7 X 8. 2 L 7 3 4F A3WE 1999020500466 19990205 00466 NM 1999 2 5 DHL9971216C 1 19990108 A 5720 ANGLE BOEING 727 72729 1384007 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LEFT WING T/E COVE PANEL SUPPORT ANGLE IS CRACKED JUST BELOW NR 4 SPOILER I/B HINGE. REMOVED AND REPLACED C OVE PANEL SUPPORT ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999020500467 19990205 00467 NM 1999 2 5 DHL9971217C 1 19990108 A 5720 ANGLE BOEING 727 72729 1384007 NM WS 497 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LEFT WING T/E COVE PANEL SUPPORT ANGLE IS CRACKED JUST I/B OF NR 3 SPOILER ACTUATOR STA 497. REMOVED AND I NSTALLED SUPPORT ANGLE PER SRM 57-50-1. 2 L 7 3 4F A3WE 1999020500468 19990205 00468 NM 1999 2 5 DHL9971218C 1 19990108 A 5720 ANGLE BOEING 727 72729 1384007 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LEADING EDGE COVE PANEL SUPPORT ANGLE IS CRACKED JUST BELOW NR 3 SPOILER O/B HINGE. REMOVED AND INSTALLED A NGLE PER SRM 57-50-1. 2 L 7 3 4F A3WE 1999020500469 19990205 00469 NM 1999 2 5 DHL9971219C 1 19990108 A 5720 ANGLE BOEING 727 72729 1384007 NM WS 573 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LEFT WING COVE PANEL SUPPORT ANGLES ARE CRACKED AT STA 573. REMOVED SUPPORT ANGLES AND REPLACED PER SRM 51 -30-2. 2 L 7 3 4F A3WE 1999020500470 19990205 00470 NM 1999 2 5 DHL9971220C 1 19990108 A 5755 SKIN BOEING 727 72729 1384007 NM NR 6 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LEFT WING NR 6 SPOILER PANEL UPPER SURFACE AREA DELAMINATED AND HOLES DRILLED. INSTALLED BONDED REPAIR PER SRM 51-40-6, 16 X 11. 2 L 7 3 4F A3WE 1999020500471 19990205 00471 NM 1999 2 5 DHL9971221C 1 19990113 A 5751 PANEL BOEING 727 72729 1384007 NM LT AILERON WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, GROOVE WORN INTO I/B AILERON LEADING EDGE PANEL 8310. REPLACED ACCESS PANEL PER SRM 57-50-1, 13 X 9.5. 2 L 7 3 4F A3WE 1999020500472 19990205 00472 NM 1999 2 5 DHL9971222C 1 19990108 A 5755 PANEL BOEING 727 72729 1384007 NM NR 9 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, NR 9 SPOILER PANEL DELAMINATED AT TOP SURFACE I/B CORNER. INSTALLED BONDING REPAIR PER SRM 51-40-6, 15 X 11 . 2 L 7 3 4F A3WE 1999020500473 19990205 00473 NM 1999 2 5 DHL9971223C 1 19990108 A 5350 FAIRING BOEING 727 72729 1384007 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, CORROSION ON BODY FAIRING PANEL NR 3334 AT FWD SECTION OF LT HEAT EXCHANGER AIR INLET DOOR. REMOVED FORMER AT FAIRING PANEL AND INSTALLED NEW PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999020500474 19990205 00474 NM 1999 2 5 DHL9971224C 1 19990109 A 5730 PANEL BOEING 727 72729 1384007 NM LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LOWER T/E PANEL JUST BELOW AFT MAIN LANDING GEAR SUPPORT BEAM IS DELAMINATED. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 20 X 6. 2 L 7 3 4F A3WE 1999020500475 19990205 00475 NM 1999 2 5 DHL9971225C 1 19990109 A 7710 SKIN BOEING 727 72729 1384007 NM NR 3 COWLING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, CORROSION IS BENEATH SKIN NR 8 AND NR 9 RIB RT SIDE OF COWL EXTERIOR. CUT OUT SECTION OF SKIN, INSTALLED FL USH REPAIR PER SRM 54-10-3, 7 X 12. 2 L 7 3 4F A3WE 1999020500476 19990205 00476 NM 1999 2 5 DHL9971226C 1 19990108 A 5280 62529687 FITTING BOEING 727 72729 1384007 NM LT MLG DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LT MLG WING DOOR ACTUATOR ARM SUPPORT FITTING CORRODED AT UPPER FWD CORNER MOUNT FASTENER WORN ON LUG. REM OVED FITTING AND REPLACED PER S/B 32A-0384. 2 L 7 3 4F A3WE 1999020500477 19990205 00477 NM 1999 2 5 DHL9971227C 1 19990109 A 5720 DOUBLER BOEING 727 72729 1384007 NM LT WING MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, LEFT WING PANEL NR 8405 HAS PREVIOUS REPAIR COMING LOOSE. INSTALLED BONDING REPAIR PER SRM 51-20-3, 17 X 5 . 2 L 7 3 4F A3WE 1999020500478 19990205 00478 NM 1999 2 5 DHL9971228C 1 19990108 A 5347 SEAT TRACK BOEING 727 72729 1384007 NM BS 550 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, CABIN SEAT TRACK CRACKED AT STA 550 LBL 48. REMOVED SEAT TRACK FROM 540 TO 620. INSTALLED NEW SEAT TRACK PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999020500479 19990205 00479 NM 1999 2 5 DHL9971229C 1 19990108 A 5414 6521873 PANEL BOEING 727 72729 1384007 NM NR 3 PYLON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 AT C-CHECK, AFT UPPER PANEL ON NR 3 STUB WING HAS A LARGE DOUBLER AT WHICH 90 PERCENT OF FASTENERS HAVE SKIN BULGED AND ARE PULLING THROUGH. REMOVED DOUBLER, PANEL DELAMINATED, REMOVED PANEL, INSTALLED NEW PANEL PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999020500480 19990205 00480 NM 1999 2 5 SWAA990186 1 19990129 A 5610 5717623122 WINDOW BOEING 737 7373H4 1384600 NM RT COCKPIT CRACKED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 364SW 26575 CRUISING AT FL280 R2 WINDOW ARCING WAS NOTICED, FOLLOWED BY CRACKING OF OUTER PANE. APPROPRIATE CHECKLIST WAS ACCOMPLIS HED. FLIGHT RETURNED TO OAK DUE TO ICING CONDITIONS AT SEA, PDX, GEG. REMOVED AND REPLACED R2 WINDOW ASSY AND WINDOW H EAT CONTROLLER PER BOEING M/M AND OPS CK GOOD. CONTROLLER (P/N 83000-05602), (S/N 7670) 0FF, (S/N 3226) ON. 2 L 7 2 4F RT A16WE 1999020500481 19990205 00481 NM 1999 2 5 SWAA990187 1 19990129 A 5350 1001001X1 RADOME BOEING 737 7373Y0 1384671 NM FWD FUSELAGE BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SW 07 664WN 23495 AFTER TAKEOFF AT 1500 FT, LARGE BIRD HIT RADOME. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RADOME ASSY AS PER MM. C/W BIRD STRIKE INSPECTION COMPLIED WITH PER MM 05-51-37. NO OTHER DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A16WE 1999020500482 19990205 00482 NM 1999 2 5 SWAA990189 1 19990128 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 732 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED 1/4D CHECK, FOUND CARGO FLOORBEAM CORRODED AT BS 732D. REPAIRED PER SWA RA 1-353-1995. 2 L 7 2 4F RT A16WE 1999020500483 19990205 00483 NM 1999 2 5 SWAA990190 1 19990128 A 5312 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 RT O/B CHORD CRACKED IN RADIUS AT WL 201. REMOVED AND REPLACED CHORD PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1999020500484 19990205 00484 NM 1999 2 5 SWAA990191 1 19990128 A 5312 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED D-CHECK, FOUND BS 178 VERTICAL CHORD CRACKED AT WL 195. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999020500485 19990205 00485 NM 1999 2 5 SWAA990192 1 19990128 A 3350 20121A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SC CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/ M. 2 L 7 2 4F A16WE 1999020500486 19990205 00486 NM 1999 2 5 SWAA990193 1 19990128 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED 1/4D CHECK, FOUND BS 360 FRAME BETWEEN S27 AND 28 CORRODED ON LOWER FRAME FLANGE. REMOVED AND REPLACED SHEAR TIE PER BOEING SRM. 2 L 7 2 4F A16WE 1999020500487 19990205 00487 NM 1999 2 5 SWAA990194 1 19990201 A 3350 20121A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SC CHECK, FOUND MID CABIN CEILING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK AND POWE R SUPPLY PER M/M. 2 L 7 2 4F A16WE 1999020500488 19990205 00488 NM 1999 2 5 SWAA990195 1 19990130 A 3350 6128251 BATTERY BOEING 737 7373H4 1384600 NM ROW 19-23 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED CHECK, FOUND FLOOR EGRESS LIGHTS BETWEEN ROWS 19 THRU 23 FAILED TO ILLUMINATE. REMOVED AND REPLACED EM ERGENCY LIGHT POWER SUPPLY, OPS CHK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999020500500 19990205 00500 EA 1999 2 5 99ZZZX523 2 19990115 A 8530 VALVE PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA NR 1 CYLINDER LOOSE A BTHA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 AL 01 200HM 689 32R7680025 L1147848A DURING FLIGHT, ENGINE STARTED RUNNING VERY ROUGH, HAD POWER LOSS. AFTER LANDING, INSPECTION FOUND NR 1 CYLINDER EXHAUST VALVE ROCKER ARM SHAFT RETAINING PLATE HAD COME OFF ALLOWING THE ROCKER SHAFT TO SLIDE OUT. THE ROCKER THEN WAS PUSHED OUT BY THE PUSH ROD. DAMAGE TO THE VALVE COVER AND CLYLINDER HEAD ENSUED. NO OTHER ENGINE DAMAGE OCCURRED. SUBMITTER SUGGESTED A POSSIBLE CAUSE COULD BE STAR WASHERS UNDER SECURING NUTS FOR PLATE DID NOT RETAIN TORQUE ON NUTS. RECOMMEN D SPECIFIC ATTENTION BE GIVEN DURING INSPECTION TO RETAINING HARDWARE. 1 L 7 1 3O 3 O A3SO 1E4 1999020500511 19990205 00511 CE 1999 2 5 99ZZZX534 1 19990112 A 7160 AN373TW91 CLAMP CESSNA 210 T210N 2073456 CE INDUCTION SYSTEM LOOSE A IPMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 11 9371Y 21064490 ENGINE SUDDENLY LOST M.P. AT FL 17, DESCENDED TO FL 10 WHERE M.P. STABILIZED. DIVERTED TO NEAREST AIRPORT FOR INSPECTIO N. FOUND INDUCTION NOSE SEPARATED FROM INLET ADAPTER DUE TO LOOSE OR DEFECTIVE NOSE CLAMP. SECURED CLAMPS AND ENGINE. OPS CHECK OK. MALFUNCTION OCCURRED 16.0 HOURS AFTER MAINTENANCE IN THIS AREA. SUBMITTER RECOMMENDED RE-CHECKING CLAMP S MORE THAN ONCE AFTER INITIAL TORQUE. 1 H 7 1 3O 3A21 1999020500512 19990205 00512 WP 1999 2 5 99ZZZX535 1 19990113 A 7921 U16011 OIL COOLER DOUG DC3 DC3C 3021457 WP NR 2 LEAKING A VLLA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 05 9923S 33 45185 25964 OIL COOLER DEVELOPED LEAK IN CORE AT ONE END OF A COOLING TUBE. SUBMITTER STATED POSSIBLY CAUSED BY HIGH OIL PRESSURE O N START-UP WITH COLD OIL. 2 L 7 2 4R A669 1999020500517 19990205 00517 GL 1999 2 5 99ZZZX540 3 19990121 A 6110 PROP ASSY PIPER PA31 PA31350 7103110 SO HARTZL HCE3Y HCE3YR2 GL LT ENGINE FAILED A WVBA O OTHER O OTHER LD LANDING 1 AL 01 27755 2619 231 317852148 DJ11610A ON LANDING APPROACH, PILOT PULLED POWER BACK TO APPROXIMATELY 25 INCHES AND NOTICED LEFT PROPELLER RPM CONTINUED TO DECR EASE TO APPROXIMATELY 1,500 RPM. RE-POSITIONING THE PROPELLER LEVER SEEMED TO MAKE NO CHANGE. ENGINE POWER SEEMED OK. DID NOT TRY TO FEATHER. PROPELLER RPM SEEMED TO STABILIZE AT 1,500 JUST PRIOR TO LANDING. MAINTENANCE GROUND RAN TO F ULL THROTTLE, ENGINE MADE APPROXIMATELY 34 INCHES, BUT PROP RPM STAYED AT 1,500. REPLACED PROP. FOUND CENTER TUBE STUC K AFT APPROX .75 INCH. PROP TO BE SHIPPED TO REPAIR STA TO INSPECT/REPAIR AND DETERMINE CAUSE OF FAILURE. 1 L 7 2 3O A20SO 5 C P33EA 1999020500550 19990205 00550 EU 1999 2 5 USAAF99001 1 19990105 A 2530 500387D3 COFFEE MAKER FOKKER F28 F28MK0100 4990807 EU GALLEY LEAKING A USAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 899US 4521 11399 CLT - FLT 575 - AFTER DEPARTING CLT EN ROUTE TO TRI, THE FLIGHT ATTENDANT REPORTED A LARGE WATER LEAK IN THE FORWARD GAL LEY AREA. THE FLIGHT ATTENDANT SHUT OFF THE WATER SUPPLY AND THE LEAK STOPPED. FLIGHT RETURNED TO CLT AND LANDED WITHO UT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 COFFEE MAKER DUE TO A LEAKING WATER LINE ON THE UNIT. MAINTENANCE I NSPECTED THE AVIONICS BAYS AND THE CARGO COMPARTMENTS FOR WATER. NO WATER WAS FOUND IN ANY OF THE BAYS. (M) 2 L 7 2 4F RT 1999020500551 19990205 00551 WP 1999 2 5 USAAD99001 1 19990101 A 3260 0331881003 BASE DOUG DC9 DC931 3022065 WP RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 974VJ 47130 PHL-BNA - FLT 1281 - AFTER TAKEOFF THE RIGHT LANDING GEAR INDICATION GREEN LIGHT FLICKERED AND STAYED ON. THE LANDING G EAR WAS CYCLED BUT THE LIGHT REMAINED ON. THE AIRCRAFT DIVERTED TO PIT, DUE TO PHL WEATHER, AND LANDED WITHOUT INCIDENT . MAINTENANCE REPLACED THE RIGHT LANDIGN GEAR GREEN LIGHT BASE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1999020500552 19990205 00552 NM 1999 2 5 USAASB99004 1 19990105 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 233US 22273 DCA - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT AT THE AFT ENTRY DOOR FLICKERS OFF AND ON. MAINTENANCE REMOVED AND R EPLACED THE EMERGENCY EXIT LIGHT ABOVE THE AFT ENTRY DOOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999020500556 19990205 00556 WP 1999 2 5 USAAD99002 1 19990104 A 3260 SENSOR DOUG DC9 DC931 3022065 WP LANDING GEAR OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 987VJ 47210 PIT-CLT - FLIGHT 980 - AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE, THE AUTO SPOILER DO NOT USE LIGHT ILLUMINATED, AND THE FLAP HORN SOUNDED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE GR OUND SENSE SYSTEM. (M) 2 L 7 2 4F A6WE 1999020500564 19990205 00564 EU 1999 2 5 SIMA990011 1 19990101 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 194AE 10623 340B194 GGG - FLT 5086 - CABIN EMERGENCY LIGHTS FAIL TO ILLUMINATE AFTER ONE SECOND. REMOVED AND REPLACED TWO AFFECTED EMERGENC Y LIGHT POWR SUPPLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999020500565 19990205 00565 EU 1999 2 5 99ZZZM78 1 19990101 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 194AE 17986 340B194 GGG - FLT 5086 - CABIN EMERGENCY LIGHTS FAIL TO ILLUMINATE AFTER ONE SECOND. REMOVED AND REPLACED TWO AFFECTED EMERGENC Y LIGHT POWR SUPPLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999020500566 19990205 00566 EU 1999 2 5 SIMA990081 1 19990108 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AE 340B278 ABI - DURING ABV INSPECTION A CHAFE WAS FOUND ON THE INNER WALL OF THE RIGHT NACELLE, INBOARD BEAM AFT OF NS 212. PERFO RMED DYE PENETRANT INSPECTION, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER .025 THICK TO NACELLE. APPLIED FIRE S EAL AROUND DOUBLER WITH DC 730 RTV. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999020500571 19990205 00571 WP 1999 2 5 AALA990009 1 19990104 A 5320 PLUG DOUG DC10 DC1030 3023501 WP BS 1965 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - LAV TIE DOWN TRACK PLUG CORRODED IN NR 1 SEAT TRACK. INSTALLED NEW LAV TRACK PLUG PER SRM 57-21-01. (M) 2 L 7 3 4F A22WE 1999020500573 19990205 00573 WP 1999 2 5 AALA990007 1 19990105 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 2000-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND GALLEY SUPPORT CORRODED. REMOVED AND REPLACED GALLEY SUPPORT AARD 51-10-00-1. (M) 2 L 7 3 4F A22WE 1999020500574 19990205 00574 WP 1999 2 5 AALA990006 1 19990105 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1944-1964 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - GALLEY SUPPORT CORRODED. REMOVED AND REPLACED GALLEY SUPPORT AARD 51-10-00-1. (M) 2 L 7 3 4F A22WE 1999020500575 19990205 00575 WP 1999 2 5 AALA990005 1 19990105 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1944-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FLOOR SUPPORT CORRODED NR 2 GALLEY SUPPORT. FABRICATED FLOOR SUPPORT PER AARD 51-10-00-1. (M) 2 L 7 3 4F A22WE 1999020500580 19990205 00580 NM 1999 2 5 AALA990023 1 19990104 A 5720 ANGLE BOEING 727 727223 1384074 NM WS 760 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 DURING C-CHECK, GOUGE FOUND IN REINFORCEMENT ANGLE, OUTBOARD SIDE OF FUSELAGE ABOVE WING STATION 760.95. ANGLE REMOVED AND REPLACED. (M) 2 L 7 3 4F A3WE 1999020500608 19990205 00608 WP 1999 2 5 AALA990047 1 19990108 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1964-1975 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON STRINGER 51L. REPLACED STRINGER END PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1999020500610 19990205 00610 WP 1999 2 5 AALA990045 1 19990108 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1964-1978 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON L52 STATION 1964-1975. REPLACED STRINGER END PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1999020500611 19990205 00611 WP 1999 2 5 AALA990044 1 19990108 A 5320 CAP DOUG DC10 DC1030 3023501 WP BS 1987 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND STRINGER 50R END CAP CORRODED AT AFT HOLE IN SPLICE. REPLACED STRINGER END CAP PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1999020500612 19990205 00612 WP 1999 2 5 AALA990022 1 19990108 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1014-1099 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON LEFT ATTACH ANGLE OUTBOARD NR 1 ROLLER TRAY STATION 1014-1099. REMOVED AND REPLACED SIDE WALL TO ROLLER TRAY Z-ANGLE STATION 959 TO 1099 PER SRM 53-60-01. (M) 2 L 7 3 4F A22WE 1999020500614 19990205 00614 WP 1999 2 5 AALA990037 1 19990109 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446AA 49472 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN CABIN INOPERATIVE. REPAIR AND REPLACED WIRING AS REQU IRED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999020500615 19990205 00615 NM 1999 2 5 AALA990016 1 19990103 A 2150 VALVE BOEING 727 727227 1384078 NM AC BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 716AA 20608 ORD - FLT 1948 - DURING CLIMB-OUT AT FL 30, BOTH RIGHT AND LEFT DUCT AND PACK TEMPERATURES STARTED TO RISE WITH SMOKE RE PORTED IN AFT CABIN. CREW RAN CHECKLIST AND BOTH PACKS TRIPPED WITH SMOKE DISSIPATING. AIRCRAFT AIR INTERRUPTED AND RE TURNED ORD AND LANDED WITHOUT FURTHER INCDIENT. MAINTENANCE FOUND LEFT RAM AIR DOOR CHECK VALVE FROZEN SHUT AND LEFT 35 DEGREE VALVE NOT OPERATING. REPLACED 35 DEGREE VALVE AND REMOVED FROZEN OBSTRUCTION FROM RAM AIR DOOR CHECK VALVE. BO TH PACKS OPERATED NORMALLY AT VARIOUS SETTINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999020500616 19990205 00616 NM 1999 2 5 AALA990015 1 19990104 A 2130 10251831 CONTROL GARRTT BOEING 727 727223 1384074 NM AC BAY MALFUNCTIONED A AALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 6822 83166 19700 DFW - FLT 535 - DURING CRUISE AT FL22 AIRCRAFT LOST PRESSURIZATION. CREW INITIATED EMERGENCY DESCENT AND LANDED DFW WIT HOUT FURTHER INCIDENT. MAINTENANCE CHECKED DECAY RATE AND PRESSURIZED AIRCRAFT WITH ENGINES AND APU ON THE GROUND WITH NO ABNORMAL CONDITIONS NOTED. AS A PRECAUTIONARY, AUTO AND MANUAL PRESSURE CONTROLS WERE REPLACED. ALL REQUIRED CHECKS WERE PERFORMED WITH NORMAL OPERATION. FUNCTIONAL CHECK FLIGHT CHECKED NORMAL WITH NO PRESSURIZATION DISCREPANCIES. (M ) 2 L 7 3 4F A3WE 1999020500618 19990205 00618 NM 1999 2 5 AALA990042 1 19990108 A 2120 AIR DISTR BOEING 727 727227 1384078 NM CABIN SMOKE A AALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 728AA 20735 KIN - FLT 1504 - EN ROUTE KIN-MIA, FLIGHT ATTENDANT NOTICED SMOKE IN AFT AIRCRAFT AND AFT GALLEY AREA. SMOKE SMELLED EL ECTRICAL, TURNED OFF OVENS 3 AND 4, CIRCUIT BREAKERS, AND GALLEY POWER. SMOKE SEEMED TO DISSIPATE. RETURNED AND LANDED KIN WITHOUT INCIDENT. RAN AFT GALLEY OVENS AND AFT COFFEE MAKERS, CHECKED ALL LAVATORIES, INSPECTED DUCTING ON ALL 3 E NGINES. RAN ALL ENGINES AND OPERATED PACKS AND OVENS. ALL CHECKED NORMAL. UNABLE TO DUPLICATE ON GROUND. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999020500619 19990205 00619 WP 1999 2 5 AALA990041 1 19990107 A 4900 5940405503 APU DOUG DC9 DC982 3022082 WP APU COMPT LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 228AA P80418 49178 MIA - FLT 1246 - EN ROUTE MIA-LGA - ABOUT 3 TO 4 MINUTES AFTER TAKEOFF, EXPERIENCED SMOKE IN CABIN AT 3,000 FEET. ACCOM PLISHED AIR CONDITIONING SMOKE AND FUMES EMERGENCY PROCEDURE. SMOKE APPEARED TO BE COMING FROM AIR CONDITIONING SYSTEM. RETURNED AND MADE EMERGENCY LANDING AT MIA, UPON LANDING SMOKE DISSIPATED AND AIRCRAFT CONTINUED TO GATE. REPLACED AP U AND ACCOMPLISHED AIR CONDITIONING CLEAN OUT AND BURNOUT PROCEDURE PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 1999020500620 19990205 00620 EU 1999 2 5 AALA990040 1 19990110 A 3260 LAMP FOKKER F28 F28MK0100 4990807 EU LT MLG DIRTY A AALA K NONE O OTHER CR CRUISE 1 SW 07 1411G 11369 ORD - FLT 1215 - EN ROUTE BOS-ORD 0 DURING CRUISE LEFT LANDING GEAR DOWN LOCKED LIGHT ILLUMINATED WITH HANDLE IN THE UP POSITION. LANDED ORD WITHOUT INCIDENT. REMOVED DEBRIS FROM LANDING GEAR INDICATION LAMPS. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 2 4F RT 1999020500622 19990205 00622 WP 1999 2 5 AALA990002 1 19990101 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 3 DEF CHAFED A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 07 468AA 49598 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FLOO R PATH LIGHTING WIRE AT SEAT ROW 3DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999020500623 19990205 00623 WP 1999 2 5 AALA990003 1 19990101 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 12 DEF DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 586AA 53249 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 12 DEF WERE INOPERATIVE. REPLACED EMERGENCY F LOOR PATH LIGHT STRIP AT SEAT ROWS 12 DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999020500625 19990205 00625 NM 1999 2 5 AALA990001 1 19990102 A 3350 0201922001 SOCKET BOEING 767 767323 1385205 NM ROW 40 B DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387AM 27184 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 40B INOPERATIVE. REPLCED EMERGENCY EXIT PATH LIGH T SOCKET AT SEAT 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999020500627 19990205 00627 NM 1999 2 5 AALA990004 1 19990103 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 696AN 26976 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999020500692 19990205 00692 SO 1999 2 5 C2XA99IA001 1 19990103 A 4920 4501968B APU EMB 145 EMB145 SO APU COMPARTMENT FAILED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 14930 145011 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED SMOKE COMING FROM THE LEFT PACK. MAINTENANCE REMOVED AND REPLACED THE AUXILLARY POWER UNIT AND THE AIRCRFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999020500700 19990205 00700 NM 1999 2 5 K3HA990006 1 19990129 A 3350 S10637067001 BATTERY BOEING 727 727225 1384077 NM L2 DOOR DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 DURING POST FLIGHT INSPECTION, FOUND EMERGENCY EXIT SIGN FOR L2 NOT ILLUMINATING. REPLACED NICAD BATTERY FOR EMERGENCY EXIT SIGN AT L2, OPS CHECK GOOD REF MM CHAPTER 33-50-71. NICAD BATTERY S106/37067-001-(AQ506119701). 2 L 7 3 4F A3WE 1999020500711 19990205 00711 WP 1999 2 5 CALA9900097 1 19990201 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP RT MLG DOOR DIRTY A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 27509 47798 THE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR WAS EXTENDED ON APPROACH TO SDF. QRH PROCEDURES WERE FOLLOW ED AND THE AIRCRAFT LANDED AT SDF. THE GEAR DOORS DROPPED OUT ON ROLL OUT RESULTING IN DAMAGE TO THE RT MLG DOOR. MAIN TENANCE FOUND C/P TO LEFT GEAR DOOR SWITCH AT FAULT. BOTH THE LEFT AND RIGHT C/P'S TO THE GEAR DOOR SWITCHES WERE CLEAN ED AND RESECURED. AN OPERATIONAL CHECK WAS NORMAL THROUGH 20 CYCLES. IN ADDITION, THE RT MLG DOOR WAS REMOVED AND REPL ACED IAW MM 32-12-1 AND 32-31-4. SUBSEQUENT MAINTENANCE WAS ACCOMPLISHED AND INCLUDED REPLACEMENT OF THE RT MLG LATCH M ECHANISM, LINK ASSEMBLY, BOLTS AND SPACERS. 2 L 7 2 4F A6WE 1999020500712 19990205 00712 WP 1999 2 5 CALA9900098 1 19990130 A 5754 RIB DOUG DC10 DC1030 3023501 WP NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A .25 INCH CRACK IN NR 1 SLAT RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999020500715 19990205 00715 NM 1999 2 5 9900295501 1 19990130 A 3260 INDICATOR BOEING 757 757251 1384970 NM LT MLG MALFUNCTIONED A NWAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 01 501US 23190 UPON GEAR EXTENSION ON APPROACH INTO DTW, THE LEFT MAIN GEAR DOWN AND LOCKED INDICATOR FAILED TO ILLUMINATE. THE APPROA CH WAS ABORTED AND THE GEAR WAS RECYCLED. SUBSEQUENT APPROACH AND LANDING OCCURRED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE LEFT MAIN GEAR INDICATOR WITH A NEW UNIT. SYSTEM TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999020500716 19990205 00716 WP 1999 2 5 9900309864 1 19990129 A 3260 LIGHT DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 773NC 47775 DURING APPROACH INTO MSY, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW UTILIZED EMER GENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SIX TIMES AND NO PROBLEMS WERE FOUND. 2 L 7 2 4F RT A6WE 1999020500717 19990205 00717 WP 1999 2 5 9900319981 1 19990201 A 3230 PULLEY DOUG DC9 DC931 3022065 WP LANDING GEAR DIRTY A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 994Z 47097 AFTER TAKEOFF, GEAR HANDLE WOULD NOT GO TO UPLATCH POSITION OR DOWN POSITION. CREW UTILIZED EMERGENCY GEAR EXTENSION PR OCEDURES AND FLIGHT WAS RETURNED TO DTW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING GEAR CONTROL LEVER AND FOUND DEBRIS LODGED AROUND TURNAROUND PULLEY FOR CABLE RUNS 102-104 AT FS 74. REMOVED DEBRIS AND PERFORMED GE AR SWING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999020500718 19990205 00718 NM 1999 2 5 UPS99228332 1 19990108 A 7830 RELAY BOEING 727 72727C 138400J NM NR 3 ENGINE CONTAMINATED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SO 01 939UP 19532 INSPECTION TYPE-N/A, DURING DEPARTURE CLIMB PRIOR TO FLAP RETRACTION, THE NR 3 THROTTLE SNAPPED BACK TO IDLE WITH AN AMB ER TR WARNING LIGHT ILLUMINATED. NOW ACTUAL AIRFRAME VIBRATION NOTED. THROTTLE WOULD NOT ADVANCE, ENG WAS THEN SHUTDOW N. AIR TURNBACK TO SDF. FOUND CONDENSATION IN ANNUNCIATOR RELAY. REPLACED RELAY SYSTEM, OPS CHK GOOD PER 78-30-00. A DJUSTED AND TESTED. 2 L 7 3 4F A3WE 1999020500719 19990205 00719 NM 1999 2 5 UPS99228610 1 19990201 A 5755 651734863 SKIN BOEING 727 72725C 138400H NM NR 7 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, NR 7 SPOILER PANEL HAS SEVERAL SMALL AREAS OF CORROSION ON LOWER SURFACE AT TRAILING EDGE 7 INCHES I /B OF O/B END. REPLACED SPOILER IAW MM 27-62-1. 2 L 7 3 4F A3WE 1999020500720 19990205 00720 NM 1999 2 5 UPS99228611 1 19990201 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION ON LOWER SURFACE OF FLOORBEAM AT BS 600, RBL 12 TO RBL 21 WL 200. REMOVED CORROSION AND R EPAIRED FLOORBEAM PER ER 99-5042P3. 2 L 7 3 4F A3WE 1999020500721 19990205 00721 NM 1999 2 5 UPS99228612 1 19990201 A 5320 65317731 SUPPORT BOEING 727 72725C 138400H NM BS 1176.9 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION ON REINFORCEMENT CHORD BS 1176.9 FROM LBL 30 TO RBL 30 WL 208. REMOVED AND REPLACED CHORD . 2 L 7 3 4F A3WE 1999020500722 19990205 00722 NM 1999 2 5 UPS99228613 1 19990108 A 5315 BAC150510002 FLOORBEAM BOEING 727 72725C 138400H NM BS 1090 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON FLOORBEAM UPPER FLANGE BS 1090 LBL 56, WL 208. FLOORBEAM UPPER FLAN GE FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. PERFORMED STANDARD T-CHORD REPARIED PER SRM 53-10-8, SRM 51-30-2 AND OHM 20-41-03. 2 L 7 3 4F A3WE 1999020500723 19990205 00723 NM 1999 2 5 UPS99228614 1 19990111 A 5320 651946220 CHORD BOEING 727 72725C 138400H NM BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-111-01.05-01) RT MID NOSE CHORD (NOSE WHEEL WELL STRUCTURE) AT BS 320, RBL 10. RT MI D NOSE CHORD FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED CHORD REPAIR PER SRM 51-30-5, SRM 51-30-02, SMR 51-30 -04 AND MM 51-31-0. 2 L 7 3 4F A3WE 1999020500724 19990205 00724 NM 1999 2 5 UPS99228615 1 19990108 A 5311 HFAB53CN011 FRAME BOEING 727 72725C 138400H NM BS 520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-224-01.00-01) ON MAIN DECK FRAME UPPER FLANGE (TOP SURFACE) BS 520 STR 2R-STR 2L. MA IN DECK FRAME UPPER FLANGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED J CHANNEL REPAIR PER SRM 53-10-04 AND M M 51-20-1. 2 L 7 3 4F A3WE 1999020500725 19990205 00725 NM 1999 2 5 UPS99228616 1 19990108 A 5754 RIB BOEING 727 72725C 138400H NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, NR 4 SLAT O/B ACTUATOR RIB IS CRACKED. REMOVED AND REPLACED NR 4 SLAT WORK ACCOMPLISH ON NRC 838733 . 2 L 7 3 4F A3WE 1999020500726 19990205 00726 NM 1999 2 5 UPS99228617 1 19990106 A 5753 TRACK BOEING 727 72725C 138400H NM NR 3 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C57-581-01.02-01) ON NR 3 FLAP TRACK AT SPAR MOUNT PAD AND INSIDE HOLES. REMOVED AND REP LACED THE NR 3 FLAP TRACK DUE TO TIME RESTRAINTS MM 27-51-4. 2 L 7 3 4F A3WE 1999020500727 19990205 00727 NM 1999 2 5 UPS99228618 1 19990105 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 1063-1168 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) IN AFT CARGO BAY LBL 16 WL 150 BS 1063 TO 1168 (CARGO TRACK). REMOVED, FABRICATED AND INSTALLED NEW CARGO TRACK WORK DONE IAW SRM'S 53-10-1, 53-10-5, 51-10-3, 51-10-2, 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 1999020500728 19990205 00728 NM 1999 2 5 UPS99228619 1 19990202 A 3350 S106 BATTERY PACK BOEING 727 7272A1 138407F NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP IN COCKPIT AND ENTRY DOOR. REPLACED EMERGENCY BATTERY PACK ASSY'S. 2 L 7 3 4F A3WE 1999020500729 19990205 00729 NM 1999 2 5 UPS99228620 1 19990203 A 2612 FIRE LIGHT BOEING 727 727247 138408F NM APU MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 211UP 21700 INSPECTION TYPE-N/A, BLOCK TURN BACK DUE TO APU FIRE LIGHT ON INDICATION. PULLED THE SWITCH AND PRESS THE DISCHARGE BUT TON. DEFERRED APU PER MEL 49-1 AND DEFERRED FIRE WARNING SYSTEM PER MEL 26-11-0-2. 2 L 7 3 4F A3WE 1999020500730 19990205 00730 WP 1999 2 5 UPS99828592 1 19990113 A 5320 9754003507 DOUBLER DOUG DC8 DC871F 302199D WP CARGO DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, INTERNAL DOUBLER AROUND A PIT DOOR IS CORRODED AND CUT AT LONG 31R. REMOVED, FABRICATED AND REPLACE D DOUBLER IAW DWG 9754003 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500731 19990205 00731 WP 1999 2 5 UPS99828594 1 19990104 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, MAIN CABIN LONG 6L END FITTING CRACKED FWD SIDE OF STA 857 FRAME. REMOVED AND REPLACED FITTING IA W DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500733 19990205 00733 WP 1999 2 5 UPS99828596 1 19990114 A 5313 5615374195 LONGERON DOUG DC8 DC871F 302199D WP BS 1600-1670 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 31R AT FS 1600 TO 1670 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONGERON FROM FS 1570 T O 1660 IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500734 19990205 00734 WP 1999 2 5 UPS99828597 1 19990104 A 5520 FAIRING DOUG DC8 DC873F 302199F WP LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, LT ELEVATOR T/E STA XE117 FAIRING ATTACH HOLE CRACKED. REPAIRED AREA IAW DC8 SRM 55-2-0. ALODINE D AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999020500735 19990205 00735 WP 1999 2 5 UPS99828598 1 19990119 A 5320 37558241 FITTING DOUG DC8 DC871F 302199D WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, DOOR JAMB BACKUP FITTING AT FS 300 BETWEEN LONG 34R AND 35R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500736 19990205 00736 WP 1999 2 5 UPS99828599 1 19990115 A 5320 97540073 WEB DOUG DC8 DC871F 302199D WP BS 340-350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 340 TO 350, LONG 33L-33R, THE TORQUE BOX WEB IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 9754007 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500737 19990205 00737 WP 1999 2 5 UPS99828600 1 19990117 A 5320 3757794502 STIFFENER DOUG DC8 DC871F 302199D WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 1160 AT LONG 33R, THE STIFFENER IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED STIFFENER IAW SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999020500738 19990205 00738 WP 1999 2 5 UPS99828601 1 19990118 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 1660 AT LONG 17R, THE INTERCOSTAL FLANGE IS CRACKED. REPAIRED INTERCOSTAL IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999020500739 19990205 00739 WP 1999 2 5 UPS99828602 1 19990120 A 5320 4611067 FITTING DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 30R END FITTING AT FS 70 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1- 20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999020500740 19990205 00740 WP 1999 2 5 UPS99828603 1 19990122 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 536.655 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, RT WING L/E LWR SKIN AT XFS 536.655 IS CRACKED AND THE INTERNAL DOUBLER HAS A PIECE MISSING. REPAIR ED IAW DH SK713-942. 2 L 7 4 4F RT 4A25 1999020500741 19990205 00741 WP 1999 2 5 UPS99828604 1 19990123 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, SHEAR TIE AT FS 420 BETWEEN LONG 30R AND 31R IS CRACKED. REPAIRED CRACKED SHEAR TIE IAW SRM 53-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 1999020500742 19990205 00742 WP 1999 2 5 UPS99828605 1 19990126 A 5320 4611067 FITTING DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 27R END FITTING AT FS 70 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED END FITTING IAW SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1999020500743 19990205 00743 WP 1999 2 5 UPS99828606 1 19990128 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, KEEL SKIN AT FS 1070 BETWEEN LONG 35L AND 35R, IS CORRODED BEYOND LIMITS. REPAIRED SKIN IAW DH SK71 3-530. 2 L 7 4 4F RT 4A25 1999020500744 19990205 00744 WP 1999 2 5 UPS99828607 1 19990128 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1490 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 35R IS CRACKED AT FS 1490. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 3646937 AND SRM 5 3-2-2. 2 L 7 4 4F RT 4A25 1999020500746 19990205 00746 WP 1999 2 5 UPS99828609 1 19990110 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, FS 879 FLOORBEAM AT LBL 60 IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH SK701-681. 2 L 7 4 4F RT 4A25 1999020500756 19990205 00756 NM 1999 2 5 99FDEA00035 1 19990130 A 2742 TRIM ACTUATOR BOEING 727 727233 138408A NM HORIZ STAB INOP A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 278FE 22345 STAB TRIM LWR THAN 0 DEG LEVEL OFF AT 230. TRIM WOULD NOT GO LWR THAN 0 DEG AND THEN IT WOULD GO NOSE UP ON ITS OWN. C OMPLIED WITH RED TABS FOR JAM STAB. *S/D* REMOVED AND REPLACED AUTO PILOT STAB TRIM ACTUATOR AND JACKSCREW ACT ASSY PE R MM 27-40-31 AND 22-11-21. 2 L 7 3 4F RT A3WE 1999020500757 19990205 00757 EU 1999 2 5 99FDEA00036 1 19990203 A 7830 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU NR 1 TR UNIT INOP A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 667FE 771 NR 1 REV NOT STOWED, ECAM WARNING WITH THROTTLE ENG ROLL BACK DURING CRUISE. DIVERT TO DEN. SLIGHT VIB ASSOCIATED WITH IND. REVERSER PREV DEACTIVATE PER MEL 36-3. FOUND CANNON PLUGS REMOVED FROM CDU. CANNON PLUGS NOT REMOVED FROM DIREC T PILOT VALVE AND PRESS. SWITCHED AND REINSTALLED CANNON PLUGS ON CDU. 2 L 7 2 4F RT A35EU 1999020500758 19990205 00758 NM 1999 2 5 99FDEA00037 1 19990202 A 3297 WIRE BOEING 727 727227 1384078 NM NLG BROKEN A FDEA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 SO 25 489FE 21492 NOSE GEAR UNSAFE LIGHT CAME ON. ABLE TO GET 3 GREEN, BUT NOT EXTINGUISH THE NOSE GEAR RED LIGHT. NOSE GEAR VIEW PORT W AS USED BUT NOT ABLE TO SEE ALIGNMENT STRIPES. MANUAL EXTENSION OF NOSE GEAR DID NOT EXTINGUISH THE LIGHT. AFT LOW PAS S, UNEVENTFUL LAND ACCOMPLISH. TOWER CONFIRM GEAR APPEAR DOWN. REPEAT WRITEUP. *S/D* REMOVED AND REPLACED WIRE W1386 -018-20. RESAFTIED CONNECTORS. 2 L 7 3 4F A3WE 1999020500759 19990205 00759 1999 2 5 99FDEA00038 4 19990202 A 3460 FMC AIRBUS 300 A300F4605R 3930327 EU E & E COMPT INOP A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 676FE 790 RTO IN DEN DUE TO MASTER CAUTION LIGHT ILLUM AND AUTO PILOT DISCONNECT AT 80 KNOTS. NO FAIL NOTED, CREW TOOK THE ACTIVE AGAIN. RTO NR 2 AUTOTHROTTLE DID NOT ENGAGE WHEN TOGA WAS SELECTED. MAINTENANCE PERFORMED GROUND SCAN, SHOW NO FAULTS . AUTOTHROTTLE CK OK, NO FAULTS PER AMM 22-30-00. AFS/LAND TEST SHOW NO FAULT. RESET FMC'S, ALL SYS OK. 2 L 7 2 4F RT A35EU 1999020500760 19990205 00760 NM 1999 2 5 99FDEA00039 1 19990201 A 3610 CLAMP BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE LOOSE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 209FE 22931 FIRE WARNING ON ENGINE NR 1. REMOVED PYLON ACCESS PANELS AND OPENED ENGINE COWL, CHECKED FIRE LOOP AND CONNECTIONS, TIG HTENED DUCT CLAMPS. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999020500761 19990205 00761 NM 1999 2 5 99FDEA00040 1 19990202 A 3610 652673831 DUCT BOEING 727 72722 1384002 NM NR 2 ENGINE RUPTURED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 150FE 19141 NR 2 ENGINE FIRE HANDLE ILLUMINATED. FIRE LIGHT EXTINGUISHED WHEN NR 2 ENGINE RETARDED. REMOVED AND REPLACED NR 2 ENGI NE CSD HIGH PRESSURE DUCT ASSY DUE TO HOLE IN DUCT PER M/M 36-00-1. RAN ENGINE AT IDLE, NO LEAKS, CK NORM. 2 L 7 3 4F A3WE 1999020500762 19990205 00762 NM 1999 2 5 99FDEA00041 1 19990202 A 2612 CLAMP BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE DAMAGED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 209FE 22931 NR 1 ENGINE FIRE WARNING CAME ON INTERMITTENTLY. CHECKED SENSING ELEM AND SYS TESTED IAW MM 26-11-01. FOUND SOME OUT O F RUBBER CLAMPS, NO OTHER DEFECTS NOTED. 2 L 7 3 4F A3WE 1999020500763 19990205 00763 NM 1999 2 5 99FDEA00042 1 19990203 A 2121 215201 FAN BOEING 727 72725C 138400H NM COCKPIT FAILED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 120FE 19356 FUME IN THE COCKPIT, MASK UP AND RETURN TO MCI FOR INVESTIGATION. FOUND GASPER FAN C/B POPPED. REMOVED FAN IAW 727 M/M 20-23-0. *S/D* INSTALLED GASPER FAN PER MM 20-23-0, RAN OPER NORMAL. 2 L 7 3 4F A3WE 1999020500764 19990205 00764 NM 1999 2 5 99FDEA00043 1 19990203 A 2612 FIRE WARNING BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 209FE 22931 INTERMITTENT FIRE WARNING NR 1 ENGINE. REMOVED AND CLEANED GASKET, REPLACED AND RETORQUED ATTACH BOLTS PER 36-10. CLOS ED PANELS PER JPF, RAN ENGINE AT T/O AND MAX CONT POWER FOR 4 MIN PER JET RUN HKBK 4-21. NO FIRE WARNING NOTED. 2 L 7 3 4F A3WE 1999020500765 19990205 00765 NM 1999 2 5 99FDEA00044 1 19990203 A 5730 SKIN DOUG MD11 MD11F 3023600 NM CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 CENTER WING UPPER SKIN ROUND WITH EXFOLIATION CORROSION AT BS 1229 STR 13, BS 1256 STR 14 AND BETWEEN BS XCW 118 AND XCW 100 RT SIDE AT BS 1273 STR 10 AND BS 1289 STR 5-SNRM 0358. RBL 18 AT BS 1160 AND BS 1219-SNRM 0455. RT AREA OF BS 129 3 AND BS 1315-SNRM 0456. PANEL (P/N APB7447-), (P/N APB7441), (APB7445-1). *S/D* REMOVED AND REPLACED CENTER WING UPP ER AUX TANK UPPER PANEL STRUCTURE AS PER SRM 57-20-00 FIG 12 VOL 1 AND EA 1-5730-40268. 2 L 7 3 4F RT A22WE 1999020500766 19990205 00766 WP 1999 2 5 99UAL900019 1 19990123 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1839U 46633 EEL STRIP LIGHTS INOP RIGHT SIDE IN FIRST CLASS SECTION. REPLACED EEL LIGHT STRIP SECTION. 2 L 7 3 4F 4 F A22WE E23EA 1999020500767 19990205 00767 NM 1999 2 5 99UAL900055 1 19990123 A 3020 VALVE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR1 ENG ANTI ICE FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 996UA 22456 NR 1 ENGINE ANTI-ICE VALVE CIRCUIT BREAKER WILL NOT STAY IN. *S/D* REPLACED NR 1 ENGINE ANTI-ICE VALVE, OPERATIONAL CH ECK IS OK. 2 L 7 2 4F 4 F A16WE E2EA 1999020500768 19990205 00768 NM 1999 2 5 99UAL900056 1 19990119 A 2460 D25BD RELAY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 609UA 21870 LOAD SHED CIRCUIT BREAKER TRIPPED FOLLOWED BY MULTIPLE FWD GALLEY CB TRIPPING. ELECTRICAL ODOR NOTED. DIVERTED TO LAS. *S/D* AIRCRAFT WAS INSPECTED AND NO FAULTS WERE FOUND. AIRCRAFT RETURNED TO SERVICE AND HAD SEVERAL EVENTS WHERE THE GALLEY CB POPPED DURING FLIGHT BUT NO OTHER DIVERSIONS. EACH TIME, PHYSICAL AND ELECTRICAL CHECKS WERE ACCOMPLISHED AND NO FAULTS WERE FOUND. LAX ACCOMPLISHED INTENSIFIED TROUBLESHOOTING TO THE SYSTEM AND FOUND THAT RELAY K102 (GROUND SER VICE TRANSFER RELAY) WAS FAULTY. THE RELAY WAS CAUSING VOLTAGE SPIKES THROUGH THE GALLEY POWER SYSTEM RESULTING IN THE POPPED CB. THE RELAY WAS REPLACED AND THE AIRCRAFT HAS FLOWN TO DATE WITHOUT FURTHER GALLEY POWER PROBLEMS. 2 L 7 2 4F 4 F RT A1NM E3NE 1999020500769 19990205 00769 NM 1999 2 5 99UAL900057 1 19990123 A 2824 VALVE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE FUEL SYST MALFUNCTIONED A UALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 29 803UA 748 FUEL TRANSFERRING FROM RT WING TANK TO LT WING TANK IN FLIGHT WITH CROSSFEED VALVE CLOSED. NO ECAM WARNINGS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999020500770 19990205 00770 1999 2 5 99UAL900058 4 19990122 A 2210 25858028 CONTROL PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AUTOPILOT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7285U 21563 SMOKE IN COCKPIT. DIVERTED TO SLC AFTER FINDING AUTPILOT HOT TO TOUCH. *S/D* REPLACED AUTOPILOT MODE CONTROL PANEL DU E TO SHORTED OUT LIGHT PLATE. OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999020500771 19990205 00771 NM 1999 2 5 99UAL900060 1 19990126 A 2130 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7252U 21399 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO DEN. *S/D* MAINTENANCE SUSPECTED THE TASK VALVE. TASK VALVE REPLACED. TECHNICAL SERVICES COULD NOT IDENTIFY THE TASK VALVE REFERRED TO, NO PART NUMBER GIVEN. 2 L 7 3 4F 4 F A3WE E2EA 1999020500772 19990205 00772 NM 1999 2 5 99UAL900061 1 19990124 A 2170 HUMIDIFIER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT SMOKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 178UA 24385 SMOKE IN COCKPIT SUDDENLY OCCURRED DURING CRUISE FLIGHT. SELECTED HUMIDIFIER OFF AND SMOKE DISSIPATED. 2 L 7 4 4F 4 F RT A20WE E24NE 1999020500773 19990205 00773 NM 1999 2 5 99UAL900062 1 19990125 A 4920 0335201500 QUILL SHAFT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TURBINE SHEARED A UALA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 WP 29 399UA 11837 6659 24674 912143 AN APU TAILPIPE FIRE OCCURRED DURING APU STARTUP. THE APU HAD HEAT DAMAGE. THE AFT AND LT SIDE OF THE FUSELAGE TAIL C ONE INSTALLATION (P/N 65-46577-569) ALSO SUFFERED HEAT DAMAGE, AS WELL AS THE LWR I/B 2 FT OF THE LT ELEVATOR (P/N 65C25 746-131) & LOWER I/B 2 FT OF THE LT ELEVATOR TAB (P/N 65C26384-23). *S/D* REPLACED THE APU, APU TAILPIPE, FUSELAGE TAI L CONE SECTION, LT ELEVATOR AND ELEVATOR TAB ASSEMBLIES. APU QUILL SHAFT FAILURE WAS CAUSE OF THE INCIDENT. APIC S/B 1 70101-49-82 & 170101-49-85 ADDRESS THE QUILL SHAFT FAILURE AND HAVE BEEN APPROVED FOR USE ON UAL APU'S. FADEC SOFTWARE V16.1 S/B 171254-49-8 HAS BEEN RELEASED BY BOEING AND SUNDSTRAND ON 12-7-98 AND WILL BE IMPLEMENTED IN THE UAL FLEET. 2 L 7 2 4F 4 F RT A16WE E2GL 1999020500774 19990205 00774 NM 1999 2 5 99UAL900063 1 19990125 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 EMERGENCY FLASHLIGHT RT SIDE CROSS AISLE FWD OF 15CDE NOT FLASHING. *S/D* REPLACED BATTERY KIT AND TESTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1999020500775 19990205 00775 NE 1999 2 5 99UAL900064 2 19990128 A 7320 P & D VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE OUT OF ADJUST A UALA A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 7275U 21422 700101 NR 2 ENGINE VIBRATION FELT IN CLIMB, OK IN CRUISE. FLIGHT ATTENDANTS REPORTED LOUD NOISE AND VIBRATION FELT IN AFT ENT RY DOOR JUMP SEAT. ALSO, BURNING RUBBER SMELL REPORTED SEVERAL TIMES. DIVERTED TO ORD. *S/D* FOUND LOW FREQUENCY VIB RATION IN NR 1 ENGINE ONLY WHICH WAS CORRECTED BY ADJUSTING THE P & D VALVE. COULD NOT IDENTIFY SOURCE OF ODOR. THE LO UD NOISE REPORTED BY THE CREW WAS NOT ASSOCIATED WITH VIBRATION. 2 L 7 3 4F 4 F A3WE E2EA 1999020500776 19990205 00776 WP 1999 2 5 ABXA9900049 1 19990128 A 2421 976J2526 GENERATOR DOUG DC9 DC932 3022066 WP LT ENGINE FAILED A ABXA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION DE DESCENT 1 GL 23 901AX 43684 47381 EN ROUTE, ALL AIRCRAFT LIGHTING AND RADAR PICTURE INTENSITY STARTED FLUCTUATING. LEFT GENERATOR VOLTS AND FREQS WERE FL UCTUATING, WIND SHEAR ANNUNCIATOR AND WARNING CAME ON. ALL ELECTRICAL POWER FAILED. EMERGENCY POWER REMAINED ON. AC C ROSS-TIE ILLUMINATED. REPLACED LEFT ENGINE DRIVEN GENERATOR. 2 L 7 2 4F A6WE 1999020600002 19990206 00002 NM 1999 2 6 SWAA990129 1 19990120 A 5315 654680117 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM SCREW HOLE CORROSION, VARIOUS PLACES AT BS 986.5, AFT GALLEY AREA. 2 L 7 2 4F RT A16WE 1999020600004 19990206 00004 EU 1999 2 6 99UAL900041 1 19990116 A 3350 D31516113 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 WOULD NOT PASS EMERGENCY LIGHT TEST. *S/D* CAUSES CANNOT BE DETERMINED FROM THE WRITE-UP. EMER LIGHT BATTERY PACK, POWE R SUPPLY UNIT AND SLIDE WERE REPLACED. EMERGENCY LIGHT TEST WAS THEN CHECKED OK. BUT SHOP FINDINGS REVEALED NO AMP REA DINGS ON LIGHT SYSTEM OF THE SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 1999020600005 19990206 00005 EU 1999 2 6 99UAL900042 1 19990117 A 2120 AIR DIST AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 401UA 435 STRONG OIL ODOR THROUGHOUT CABIN. 2 L 7 2 4F 4 F RT A28NM E40NE 1999020600006 19990206 00006 EU 1999 2 6 99UAL900043 1 19990114 A 2930 WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST ACTIVATED A UALA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 29 442UA 780 GREEN SYSTEM HYD INDICATES AT AMBER BAR. 2 L 7 2 4F 4 F RT A28NM E40NE 1999020600007 19990206 00007 1999 2 6 99UAL900045 4 19990118 A 3425 PFD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT COCKPIT MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 407UA 456 ON APPROACH, F/O PFD AND ND SWAPPING POSITION AFTER TAKEOFF, INTERMITTANTLY DURING FLIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 1999020600008 19990206 00008 EU 1999 2 6 99UAL900048 1 19990120 A 5270 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMER EXIT DOOR OUT OF ADJUST A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 410UA 463 LEFT FWD OVERWING DOOR GIVING WARNING ECAM MSG. THE LEFT FWD OVERWING DOOR PROXIMITY SWITCH AND TARGET WAS MISALIGNED W HICH RESULTED IN THE ECAM WARNING MESSAGE. THE TARGET WAS ADJUSTED PER AMM TASK 52-71-13-400-001 TO CORRECT THE PROBLEM . 2 L 7 2 4F 4 F RT A28NM E40NE 1999020600009 19990206 00009 EU 1999 2 6 99UAL900049 1 19990120 A 3230 RETRACT MECH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR MALFUNCTIONED A UALA K NONE J WARNING INDICATION CL CLIMB 1 WP 29 419UA 487 ON CLIMBOUT, GEAR DID NOT FULLY RETRACT. CYCLED GEAR, CAME UP OK BUT GOT LGCIU FAULT WITH ASSOCIATED ECAM WARNING. 2 L 7 2 4F 4 F RT A28NM E40NE 1999020600010 19990206 00010 1999 2 6 99UAL900054 4 19990120 A 2211 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 & 2 FMGC TRIPPED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 411UA 464 MCDU NR 1 & 2 BLACKED OUT SEVERAL TIMES FOR SEVERAL MINUTES INDEPENDENTLY AND CAME BACK ON THEIR OWN. NR 2 FLIGHT DIRECT OR SEEMED TO WANDER BOTH VERTICALLY AND LATERALLY 300 FEET. *S/D* RESET FMGC 1 AND 2 CB'S, OPS CHECKS NORMAL. NO ADDI TIONAL PROBLEMS HAVE BEEN IDENTIFIED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999021200001 19990212 00001 WP 1999 2 12 TWAA9902001 1 19990202 A 3350 58222 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 935L 47603 JUST PRIOR TO DEPARTURE FOUND FLOOR EGRESS LIGHTS AT ROW 15 TO 19 REMAINED ON. REPLACED THE BATTERY PACK. CHECK-C 9-28 -98 STL. 2 L 7 2 4F A6WE 1999021200002 19990212 00002 WP 1999 2 12 TWAA9902002 1 19990202 A 5315 SUPPORT DOUG DC9 DC932 3022066 WP BS 197 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND FLOOR SUPPORT AT STA 197, OBL TO LBL 44, CORRODED. REPLACED FLOOR SUPPORT PER SPM 6-70- 01, PAGE 2. 2 L 7 2 4F A6WE 1999021200003 19990212 00003 WP 1999 2 12 TWAA9902003 1 19990129 A 5320 MEMBRANE DOUG DC9 DC932 3022066 WP BS 195 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR WITH APPROXIMATELY 12 INCH CRACK, LOCATED AT STA 195, LBL 4 TO 12. REPAIRED PER SRM 53-01, PG 9. 2 L 7 2 4F A6WE 1999021200004 19990212 00004 WP 1999 2 12 TWAA9902004 1 19990129 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CRACKED INTERCOSTAL AT STA 737, LONGERON 15L. REMOVED AND REPLACED INTERCOSTAL PER STAN DARD PROCESSES MANUAL 6-70-01. 2 L 7 2 4F A6WE 1999021200005 19990212 00005 WP 1999 2 12 TWAA9902005 1 19990129 A 5522 SKIN DOUG DC9 DC931 3022065 WP RT ELEVATOR DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND DENT IN LEADING EDGE OF RT ELEVATOR, APPROXIMATELY 2.25 BY 2.5 INCH AND 0.180 INCH DEEP, LOCATED JUST O/B OF ELEVATOR DAMPER. REPLACED DAMAGED PANEL PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999021200006 19990212 00006 WP 1999 2 12 AT9900077 1 19990202 A 3350 100865 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 846AT 47226 FOUND FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY POWER SUPPLY, S YSTEM OPS CHECK GOOD IAW MM 33-50. 2 L 7 2 4F A6WE 1999021200008 19990212 00008 SO 1999 2 12 COMA9910029 1 19990202 A 2750 WARNING EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 159A 120159 FLAP CONTROL FAULT WARNING DURING TAKEOFF. COULD NOT DUPLICATE, OPERATIONAL CHECK OF FLAP SYSTEM WAS NORMAL. 2 L 7 2 4T RT A31SO 1999021200009 19990212 00009 SO 1999 2 12 COMA9910030 1 19990202 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 264CA 15281 120256 AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1999021200010 19990212 00010 EA 1999 2 12 COMA9960055 1 19990203 A 2752 854D10010 ACTUATOR CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 NR 4 ACTUATOR ON RIGHT WING FLAP FAILED TORQUE CHECK DURING COMPLIANCE OF EO 27-046D. REMOVED AND REPLACED NR 4 ACTUATO R RIGHT WING FLAP. 2 L 7 2 4F RT A21EA 1999021200011 19990212 00011 EA 1999 2 12 COMA9960056 1 19990203 A 5320 60031535 STRIKER SEAL CNDAIR CL600 CL6002B19 EA PAX DOORWAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 PASSENGER DOOR STRIKER SEAL DAMAGED BY BOTTOM AFT LATCH PIN. REPAIRED DAMAGE TO PAX DOOR STRIKER SEAL PER REO 601R-52-1 1-008. 2 L 7 2 4F RT A21EA 1999021200012 19990212 00012 EU 1999 2 12 QXEA9900282 1 19990201 A 3350 XB864041 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 12 BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 BOI - SEAT MOUNTED EMERGENCY EXIT SIGN AT ROW 12 IS BROKEN. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 12. OPERATIONAL CHECK PERFORMED, NORMAL OPERATION RESTORED. 2 L 7 2 4F RT A20EU 1999021200013 19990212 00013 NM 1999 2 12 QXEA9900283 1 19990201 A 2611 WIRE DHAV DHC8 DHC8102 2809003 NM CARGO SMOKE DET BROKEN A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 822PH 106 SEA- SMOKE WARNING LIGHT CAME ON INTERMITTENTLY FOR ABOUT 5 SECONDS EACH TIME. MAINTENANCE INSPECTED AND FOUND NO EVIDE NCE OF FIRE OR SMOKE. FOUND 2 BROKEN WIRES AT THE CANNON PLUG ON THE NR 2 CARGO SMOKE DETECTOR. STOWED WIRES AND PLACE D ON MEL. 2 H 7 2 4T RT A13NM 1999021200014 19990212 00014 WP 1999 2 12 ABXA9900050 1 19990118 A 5712 RIB DOUG DOUG DC8 DC863 302198A WP WS 772 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING UPPER RIB CRACKED AT STATION XFS772. REPAIRED IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1999021200015 19990212 00015 WP 1999 2 12 ABXA9900051 1 19990118 A 5230 421464361 SKIN DOUG DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LOWER CARGO DOOR (C2) INTERIOR SKIN CRACKED AT LOWER FORWARD CORNER. REPAIRED IAW DC8 SRM 52-4-2. 2 L 7 4 4F 4A25 1999021200016 19990212 00016 WP 1999 2 12 ABXA9900052 1 19990118 A 5240 575553028 STRUCTURE DOUG DOUG DC8 DC863 302198A WP LT SERV DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT CENTER SERVICE DOOR HAD CRACK IN STRUCTURE. REPAIRED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 52-20-0. 2 L 7 4 4F 4A25 1999021200017 19990212 00017 WP 1999 2 12 ABXA9900053 1 19990117 A 5712 DH42146335 RIB DOUG DOUG DC8 DC863 302198A WP WS 753.750 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 UPPER RIB CRACKED AT LEFT WING OUTBOARD LEADING EDGE AT XFS 753.750. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999021200018 19990212 00018 WP 1999 2 12 ABXA9900054 1 19990117 A 5712 DH42146334 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIB CRACKED AT LEFT WING OUTBOARD SECTION AT XFS 772.5. REPAIRED IAW DC8 SRM 51-1-20D AND ABX DWG K05056. 2 L 7 4 4F 4A25 1999021200019 19990212 00019 WP 1999 2 12 ABXA9900055 1 19990116 A 5320 47504201 FITTING DOUG DOUG DC8 DC863 302198A WP BS 860 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 INTERCOSTAL FITTING CRACKED AT LONGERON 18 LEFT, STATION 860. REPLACED FITTING IAW DWG 4750420 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999021200020 19990212 00020 WP 1999 2 12 ABXA9900056 1 19990116 A 5320 561553053 INTERCOSTAL DOUG DOUG DC8 DC863 302198A WP BS 8-20 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 EXFOLIATED CORROSION ON INTERCOSTAL AT LONGERON 30L, STATION 8 TO 20 INSIDE AIR CONDITIONING BAY. REPLACED INTERCOSTAL IAW DWG 5615530 AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999021200021 19990212 00021 WP 1999 2 12 ABXA9900057 1 19990116 A 5320 3750257503AX FITTING DOUG DOUG DC8 DC863 302198A WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LONGERON 31L SPLICE FITTING CRACKED AT STATION 1040 TO 1060. REPLACED FITTING IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1999021200022 19990212 00022 WP 1999 2 12 ABXA9900058 1 19990116 A 5320 47504221 FITTING DOUG DOUG DC8 DC863 302198A WP BS 860 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 INTERCOSTAL END FITTING CRACKED AT LONGERON 19R, STATION 860. REPLACED FITTING IAW DWG 4750422 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999021200023 19990212 00023 WP 1999 2 12 ABXA9900059 1 19990116 A 5320 4645577502 ANGLE DOUG DOUG DC8 DC863 302198A WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 FLOORBEAM SUPPORT ANGLE CRACKED AT STATION 680, RBL 28. REPAIRED IAW DWG 4645377 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999021200024 19990212 00024 WP 1999 2 12 ABXA9900060 1 19990201 A 3260 LINK DOUG DC9 DC914 3022034 WP NLG OUT OF ADJUST A ABXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 925AX 45728 AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. GEAR CYCLED DOWN NORMAL LY. ON RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIR TURNBACK TO ILN. RESHIMMED NOSE LANDING GEAR ACTU ATOR LINK AND ADJUSTED NOSE LANDING GEAR DOOR. 2 L 7 2 4F A6WE 1999021200025 19990212 00025 NM 1999 2 12 DHL99742001 1 19990204 A 2611 302842 SMOKE DETECTOR BOEING 727 727225 1384077 NM CARGO COMPT DEFECTIVE A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 742DH 21290 AT FL 330 CARGO SMOKE WARNING LIGHT ILLUMINATED. DECLARED EMERGENCY AND DESCENDED INTO IAH. AT APPROX 2000 FT AGL THE LIGHT EXTINGUISHED. LANDED WITHOUT INCIDENT. FOUND NR 1 SMOKE DETECTOR DEFECTIVE. REMOVED AND REPLACED SMOKE DETECT OR. 2 L 7 3 4F A3WE 1999021200099 19990212 00099 EU 1999 2 12 MALA976330 1 19990201 A 3233 AIR864101 FITTING SAAB SF340 SF340A 7850100 EU LT MLG ACTUATOR BROKEN A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 107XJ 340A107 AFTER GEAR EXTENSION, HAD A HYDR FROM CWP, MAIN HYDRAULIC PRESSURE DECREASED TO ZERO AND HYDRAULIC QUANTITY DECREASED TO ZERO. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR ACTUATOR. BLED AND SERVICED HYD SYSTEMS IAW SAAB 340 AMM CHAP 32 AND 12. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021200100 19990212 00100 EU 1999 2 12 MALA976331 1 19990202 A 3350 7239610802 LIGHT SAAB SF340 SF340A 7850100 EU CABIN INOP A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 48XJ 048 DURING INSPECTION, EMERGENCY EXIT LIGHT AT SEAT 1 CD INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999021200101 19990212 00101 EU 1999 2 12 MALA976332 1 19990202 A 3230 RETRACT MECH BAC 146 AVRO146RJ85A 1500097 EU RT MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 513XJ E2329 AFTER TAKEOFF FROM DTW, THE RIGHT MAIN GEAR DID NOT FULLY RETRACT, RIGHT GEAR INTRANSIT LIGHT AND GEAR HANDLE REMAINED I LLUMINATED. CYCLED GEAR TWICE WITH SAME INDICATIONS. AFTER 2ND ATTEMPT THE LEFT MAIN UNSAFE LIGHT REAIMED LIT FOR 15-2 0 SECONDS, THEN WENT OUT, RIGHT SIDE STAYED ON. AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE CLEANED GEAR PO SITION SWITCHES, CANNON PLUG CONNECTIONS AND LUBED GEAR. PERFORMED A COMPLETE FUNCTIONAL TEST OF THE LANDING GEAR DETEC TION SYSTEM PER 32-30-14. MAINTENANCE PERFORMED A TEST FLIGHT AS A PRECAUTIONARY MEASURE. TEST FLIGHT SATISFACTORY. 2 H 7 4 4F RT A49EU 1999021200102 19990212 00102 EU 1999 2 12 MALA976333 1 19990202 A 7603 POWER LEVER BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE FROZEN A MALA O OTHER O OTHER DE DESCENT 1 GL 15 512XJ E2328 ON DESCENT OUT OF 310, NR 3 ENGINE POWER LEVER WAS FROZE AT 85 PERCENT N1, COULD NOT MOVE THE POWER LEVER FORWARD OR AFT . CREW BROUGHT ENGINE ANTI-ICE ON AND AT ABOUT FL 270 LEVER FREED UP AND OPERATED NORMAL. ENGINE PARAMETERS WERE NORMA L WITH NO EVIDENCE OF LIMITATIONS INDICATED. AIRCRAFT LANDED WITHOUT INCIDENCE. MAINTNENANCE INSPECTED AND FOUND ICE A ND WATER IN THE NR 3 PYLON JUST UNDER THE WING ROOT. MAINTNENANCE REMOVED WATER AND ICE, FOUND POWER LEVER TO MOVE FREE LY. OPS CHECK AND SECURITY CHECK GOOD. 2 H 7 4 4F RT A49EU 1999021200103 19990212 00103 EU 1999 2 12 MALA976334 1 19990203 A 3020 44730501 DEICE MODULE SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 68XJ 068 DURING CRUISE, RIGHT ENGINE ANTI-ICE INTAKE CAUTION LIGHT ILLUMINATED, CYCLED ON AND OFF APPROXIMATLY EVERY 30 SECONDS. CREW RAN QRH NO CHANGE, DE-ICE CHECKS WERE NORMAL. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RIGHT DE-ICE MODULE IAW SF3 MM 30-20, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999021200104 19990212 00104 EU 1999 2 12 MALA976336 1 19990203 A 3020 INTAKE DEICE SAAB SF340 SF340A 7850100 EU LT & RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 102XJ 340A102 EN ROUTE TO LAN TURNED INTAKE HEAT ON, WITHIN 5 SECONDS THE RIGHT INTAKE LIGHT ILLUMINATED, FOLLOWED QRH THEN LEFT INTAK E CAME ON. CREW EXITED ICING CONDITIONS AND RETURNED TO DTW. MAINTENANCE GROUND RAN ENGINE AND OPS CHECKED RIGHT AND L EFT INTAKE HEAT SYSTEMS, ALL CHECKS GOOD. NO DEFECTS NOTED. OPERATED SYSTEM SEVERAL TIMES, ALL INDICATIONS AND CHECKS ARE NORMAL. ALL WORK AND TROUBLE SHOOTING DONE IAW SAAB MM CHAP 30. 2 L 7 2 4T RT A52EU 1999021200105 19990212 00105 NM 1999 2 12 AWXA9900038 1 19990203 A 2121 5007024620 FAN BOEING 737 737277 1384570 NM CABIN FAILED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 182AW 25469 1032 22649 AIR TURNBACK, BURNING ODOR IN CABIN AND FLIGHT DECK. SLIGHT BURNING ODOR NOTICED IN CABIN AND FLIGHT DECK AFTER TAKEOFF . RETURNED TO PHOENIX. FOUND GASPER CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN PER MM21-24-21. OPERATIO NAL CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999021200106 19990212 00106 EU 1999 2 12 AWXA9900039 1 19990203 A 3260 CONNECTOR AIRBUS 320 A320231 3930325 EU RT MLG DOOR DIRTY A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 629AW 076 EMERGENCY LANDING, UNSAFE GEAR INDICATION. LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) FAULT ON SHORT FINAL. AFTER GEA R EXTENSION, LGCIU 1 AND LGCIU 2 FAULT, WITH RIGHT MAIN LANDING GEAR DOOR INTRANSIT INDICATION. LGCIU1 AND LGCIU 2 RESE TS. NO HELP. PERFORMED CFDS INTERROGATION LGCIU 2. NO CURRENT FAULTS NOTED. LAST LEG SHOWS 34GA OPEN. VISUALLY INSP ECTED. CLEANED CONNECTOR. CHECKED OPERATION AND NO FAULTS NOTED. 2 L 7 2 4F RT A28NM 1999021200107 19990212 00107 NE 1999 2 12 PNSA990101 2 19990104 A 7320 APR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 AL 03 675PA 206 RT APR FAILED TO ARM DURING TAKEOFF ROLL ABORTED TAKEOFF. SUBSEQUENT TEST OF SYSTEM WAS OK. NO FURTHER SQUAWKS WERE N OTED. 2 L 7 2 4T 4 T RT A52EU E8NE 1999021200108 19990212 00108 SW 1999 2 12 PNSA990102 1 19990120 A 5270 SWITCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR FROZEN A PNSA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 AL 03 41NE AC741B BEFORE ENGINE START, CARGO DOOR WARNING LIGHT WOULD NOT EXTINGUISH. THAWED FROZEN SWITCH SYSTEM, OPS CHECKED OK. 2 L 7 2 4T RT A8SW 1999021200109 19990212 00109 SW 1999 2 12 PNSA990103 1 19990112 A 5270 SWITCH SWRNGN SA227 SA227AC 8780603 SW PAX DOOR OUT OF ADJUST A PNSA K NONE N FALSE WARNING CR CRUISE 1 AL 03 2719H AC713B CABIN DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. RETURNED TO BASE. ADJUSTED RIGGING ON FWD LOWER SWITCH. OPS CHECKED O K. 2 L 7 2 4T RT A8SW 1999021200110 19990212 00110 SW 1999 2 12 PNSA990104 1 19990118 A 5270 SWITCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR FROZEN A PNSA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 AL 03 2719H AC713B BEFORE ENGINE START, CARGO DOOR WARNING LIGHT WOULD NOT EXTINGUISH. THAWED FROZEN SWITCH. OPS CHECK OK. 2 L 7 2 4T RT A8SW 1999021200111 19990212 00111 EU 1999 2 12 PNSA990105 1 19990106 A 2520 CEILING PANEL SAAB SF340 340B 7860101 EU ROW 5 FELL A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 675PA 206 DURING TAXI FOR TAKEOFF, THE OVERHEAD PANEL FELL LOOSE FROM CEILING LANDING IN ROW 5. AIRCRAFT RETURNED TO GATE SECURE D PANEL AIRCRAFT RELEASED. 2 L 7 2 4T RT A52EU 1999021200112 19990212 00112 EU 1999 2 12 PNSA990106 1 19990107 A 2781 LIGHT SAAB SF340 340B 7860101 EU TE FLAPS ILLUMINATED A PNSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 675PA 206 AFTER LEVELING OFF AT ALTITUDE, FLAP LIGHT ON TEST PANEL ILLUMINATED. FOLLOWED BY AN FLAP LIGHT ON THE CENTRAL WARNING PANEL. RETURNED TO BASE FOR A ZERO FLAP LANDING. CHECKED RIGGING ON FLAPS FOUND TO BE WITHIN LIMITS AIRCRAFT RELEASED FOR SERVICE. NO FURTHER SQUAWKS NOTED. 2 L 7 2 4T RT A52EU 1999021200123 19990212 00123 WP 1999 2 12 CALA9900099 1 19990131 A 5730 SKIN DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE DROOP PANEL UPPER SKIN. TWO RIBS WERE REMOVED AND REPLACED. TH E SKIN WAS REINFORCED WITH DOUBLER AND INSTALLED IAW SRM 57-10-00, FIGURE 55, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1999021200124 19990212 00124 WP 1999 2 12 CALA9900100 1 19990201 A 5520 ELEVATOR DOUG DC10 DC1030 3023501 WP RIGHT DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND IMPACT DAMAGE TO RT ELEVATOR TIP CAUSED BY HANGAR DOOR. A NEW ELEVATOR WAS INSTALLED IAW MM 27-30-09, PAGE 401. ELEVATOR OPERATION CHECKED GOOD IAW MM 27-30-03, PAGE 601. 2 L 7 3 4F A22WE 1999021200125 19990212 00125 WP 1999 2 12 CALA9900101 1 19990102 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 164 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND A .25 INCH CRACK IN RT WING AFT SPAR AT I/B ACTUATOR HINGE FORWARD FORGING FROM I/B LOWER BOLT AREA, AP PROXIMATELY XRS 164. THE FASTENERS WERE REMOVED AND THE CRACKED SECTION OF SPAR WAS CUT OUT. A NEW SPAR SECTION WAS IN STALLED USING SPLICES INSIDE AND OUTSIDE IAW DRAWING J060165 AND EA 5761-01001. 2 L 7 2 4F A6WE 1999021200126 19990212 00126 WP 1999 2 12 CALA9900102 1 19990202 A 3397 WIRE DOUG DC9 DC932 3022066 WP LT, RT EMER EXIT BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 THE LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501. 2 L 7 2 4F A6WE 1999021200127 19990212 00127 WP 1999 2 12 CALA9900103 1 19990202 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 13 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 THE CABIN EMERGENCY LIGHTS FROM COCKPIT TO ROW 13 WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF T HE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501. 2 L 7 2 4F A6WE 1999021200128 19990212 00128 WP 1999 2 12 CALA9900104 1 19990202 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 23 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 THE AFT CEILING EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 23 TO TAIL SECTION. MAINTENANCE FOUND WIRING TO BATTER Y POWER PACKS BROKEN. THE WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0. 2 L 7 2 4F A6WE 1999021200129 19990212 00129 WP 1999 2 12 CALA9900105 1 19990202 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 THE AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH WAS FOUND INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE ON SWITCH . THE LOOSE WIRE WAS TIGHTENED AND SYSTEM OPERATION CHECKED GOOD IAW MM 33-50-00, PAGES 203-204. 2 L 7 2 4F A6WE 1999021200130 19990212 00130 WP 1999 2 12 CALA9900106 1 19990202 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND TWO 1 CRACKS IN LT FUSELAGE SKIN BY THE AFT STAIR HANDLE IN THE UNPRESSURIZED AREA. THE SKIN WAS REPAI RED IAW SRM 53-01. 2 L 7 2 4F A6WE 1999021200131 19990212 00131 WP 1999 2 12 CALA9900107 1 19990202 A 2560 ESCAPE LINE DOUG DC9 DC982 3022082 WP LT, RT EMER EXIT FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND THE LT AND RT OVERWING EMERGENCY ESCAPE LINES FRAYED. NEW ESCAPE LINE WAS INSTALLED IAW SRM 51-30-1 AN D MM 25-61-00, FIGURE 202. 2 L 7 2 4F A6WE 1999021200132 19990212 00132 NM 1999 2 12 CALA9900108 1 19990203 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 480-500 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 480-500B, STRINGER 19L. A REPAIR WAS INSTALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 1999021200133 19990212 00133 NM 1999 2 12 UPS99228621 1 19990129 A 4920 36045242 CAP ASSY BOEING 727 72730C 1384009 NM APU CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C APU COMBUSTION UNIT HAS CRACK ON CAP ASSY. COMBUSTION UNIT LINER ASSY REPLACED IAW MM CHP 49-30-22. 2 L 7 3 4F A3WE 1999021200134 19990212 00134 NM 1999 2 12 UPS99228622 1 19990129 A 5340 69348161 FITTING BOEING 727 72730C 1384009 NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C SEAT TRACK ATTACH FITTING CORRODED AT BS 740 RBL 45. FITTING AT BS 740 RBL 45 REPLACED PER DWR NR 65C 13724. 2 L 7 3 4F A3WE 1999021200135 19990212 00135 NM 1999 2 12 UPS99228623 1 19990125 A 7830 06453010059 BRACKET BOEING 727 72730C 1384009 NM NR 3 ENGINE TR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C ENGINE NR 3 THRUST REV OUTER FAIRING MID AND AFT SUPPORT BRACKETS CRACKED. REPLACED BRACKETS IAW MM 7 8-30-00. 2 L 7 3 4F A3WE 1999021200136 19990212 00136 NM 1999 2 12 UPS99228624 1 19990125 A 7830 06453010037 BRACKET BOEING 727 72730C 1384009 NM NR 1 ENGINE TR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C ENGINE NR 1 THRUST REV OUTER FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 78-30-00. 2 L 7 3 4F A3WE 1999021200137 19990212 00137 NM 1999 2 12 UPS99228625 1 19990122 A 5754 SKIN BOEING 727 72730C 1384009 NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C NR 3 LE KRUEGER FLAP HAS CRACK ON ANTI-ICE SKIN. CRACK STOP DRILLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1999021200138 19990212 00138 NM 1999 2 12 UPS99228627 1 19990204 A 5320 SPAR WEB BOEING 727 72725C 138400H NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI WING CENTER SECTION REAR SPAR WEB IS CORRODED BS 870 RBL 22-46 LBL 46. REMOVED AND REPLACED WING CEN TER SECTION REAR SPAR WEB, UPPER CHORD, AND LOWER CHORD PER ER 99-5018. 2 L 7 3 4F A3WE 1999021200139 19990212 00139 NM 1999 2 12 UPS99228628 1 19990107 A 5754 651622346 RIB BOEING 727 72725C 138400H NM NR 2 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI NR 2 SLAT I/B TRACK I/B MOUNTING BRACKET SUPPORT RIB IS CRACKED. REPLACE NR 2 SLAT PER MM 27-81-11. 2 L 7 3 4F A3WE 1999021200140 19990212 00140 NM 1999 2 12 UPS99228629 1 19990202 A 5751 FITTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI R/W O/B AILERON, UPPER QUADRANT HINGE HAS PITTING AROUND HINGE BOLT. REMOVED PITTED FITTING, INSTAL LED NEW FITTING IAW SRM 51-30-2 PG 14 PARA 7 AND PG 8 PARA A5. 2 L 7 3 4F A3WE 1999021200141 19990212 00141 NM 1999 2 12 UPS99228630 1 19990108 A 5315 7075T6080 FLOORBEAM BOEING 727 72725C 138400H NM BS 598 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI CORROSION (SDN C53-111-01.00-02) ON LOWER SURFACE OF LONGITUDINAL FLOORBEAM AT BS 598, BL 0, WL 200. REMOVED ALL CORROSION, FLAT PEENED AREA, FABRICATED AND INSTALLED REPAIR STRAP IAW ER NR 99-5029. 2 L 7 3 4F A3WE 1999021200142 19990212 00142 NM 1999 2 12 UPS99228631 1 19990202 A 5530 STRINGER BOEING 727 72725C 138400H NM VERT FIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI INTERNAL VERTICAL FIN STRINGER 5-11R IS CRACKED AT BS 1362, 9 INCHES ABOVE FIN STA 6.0. REMOVED AND REPLACED STRINGER SEGMENT PER FER 99-5059. 2 L 7 3 4F A3WE 1999021200143 19990212 00143 NM 1999 2 12 UPS99228632 1 19990202 A 5755 652162222 FITTING BOEING 727 72725C 138400H NM NR 3 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI NR 3 FLIGHT SPOILER ACTUATOR SUPPORT FITTING HAS EXCESSIVE PITTING CORROSION ON I/B FACES OF BOTH I/B MOUNTING LUGS FOR SPOILER CENTER HINGE. REPLACED MOUNT (SUPPORT FITTING PN 65-21622-22) PER 727 MM 27-61-81. 2 L 7 3 4F A3WE 1999021200144 19990212 00144 NM 1999 2 12 UPS99228633 1 19990202 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:C WHILE ACCESSING OVERWING FRAMES FOUND SEAT TRACK AT STA 760 RBL 65 WL 208 CRACKED AT O/B FLANGE. REPL ACED SEAT TRACK FROM BS 760 TO BS 848 PER 727 SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F A3WE 1999021200145 19990212 00145 WP 1999 2 12 UPS99828626 1 19990122 A 5720 WEB DOUG DC8 DC871F 302199D WP WS 23 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C NR 2 MAIN TANK VERT WEB PREVIOUS REPAIRED CRACK HAS EXTENDED BEYOND DOUBLER AT STA XRS 23 STR 13. REP AIRED IAW DH SK 701-152 AND DH SK 701-453. 2 L 7 4 4F RT 4A25 1999021200146 19990212 00146 WP 1999 2 12 ABXA9900061 1 19990204 A 3297 WIRE DOUG DC9 DC941 302207N WP RT MLG DOWNLOCK BROKEN A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 979AX 47492 NO RIGHT MAIN LANDING GEAR INDICATION WITH THE GEAR HANDLE DOWN. PERFORMED GEAR RECYCLE, ALTERNATE GEAR INDICATION CONF IRMED GEAR DOWN AND LOCKED. GOT GPWS GEAR, TOO LOW ON FINAL. SATISFACTORY LANDING ACCOMPLISHED AFTER FLY-BY GEAR INSP ECTION. REPAIRED BROKEN WIRE TO RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH. 2 L 7 2 4F A6WE 1999021200147 19990212 00147 WP 1999 2 12 ABXA9900062 1 19990201 A 5320 3922423 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND FLOORBEAM SUPPORT FITTING ABOVE CENTER WING CRACKED AT LOWER END, STATION 680 , LBL 43. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999021200148 19990212 00148 WP 1999 2 12 ABXA9900063 1 19990201 A 5320 39224232 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND FLOORBEAM SUPPORT FITTING ABOVE CENTER WING CRACKED AT LOWER END, STATION 680, RBL 43. REPLACED F ITTING IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999021200149 19990212 00149 WP 1999 2 12 ABXA9900064 1 19990201 A 5753 99576008 BRACKET DOUG DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD, INTERIOR FITTING, INBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 S RM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999021200150 19990212 00150 WP 1999 2 12 ABXA9900065 1 19990201 A 5753 995760016 BRACKET DOUG DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C CHECK, FOUND RIGHT FLAP OUTBOARD HINGE INTERIOR FITTING, OUTBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IA W DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999021200151 19990212 00151 WP 1999 2 12 ABXA9900066 1 19990201 A 5753 995760015 BRACKET DOUG DOUG DC9 DC933F 302207A WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERIOR FITTING, OUTBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999021200152 19990212 00152 WP 1999 2 12 ABXA9900067 1 19990201 A 5753 995760019 BRACKET DOUG DOUG DC9 DC933F 302207A WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERIOR FITTING INBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC 9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999021200153 19990212 00153 WP 1999 2 12 ABXA9900068 1 19990201 A 5330 59114003 SKIN DOUG DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED AFT OF NOSE LANDING GEAR, AFT RIGHT DOOR HINGE. REPAIRED SKIN IAW DC9 SRM 5 3-05. 2 L 7 2 4F A6WE 1999021200154 19990212 00154 NM 1999 2 12 DHL99709001 1 19990203 A 3222 69154143 GLAND NUT BOEING 727 72782C 1384026 NM NLG STRUT LEAKING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 709DH 19968 DURING GEAR RETRACTION, NOSE GEAR DOOR LIGHT WOULD NOT EXTINGUISH. ON EXTENSION, ALL INDICATIONS WERE NORMAL. ABNORMAL INDICATIONS ON FWD AND F/E PANEL. FOUND GLAND NUT LEAKING. REPLACED SAME. CYCLED GEAR SEVERAL TIMES. SYS CKS NORMAL . 2 L 7 3 4F A3WE 1999021200155 19990212 00155 1999 2 12 SWIA971378 3 19990106 A 6140 NP INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PROPELLER MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 203SW 120240 RIGHT PROPELLER NP INDICATOR 102.7 PERCENT AFTER TAKEOFF. RETURNED TO FIELD. CHECKED RIGHT ENGINE CONTROL LINKAGE. PE RFORMED POWER RUN ON RIGHT ENGINE. RPM IS WITHIN PERIMETERS AND CONDITION LEVER RESPONSE IS NORMAL. SYSTEM OPS GOOD. C OULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021200156 19990212 00156 SO 1999 2 12 SWIA971379 1 19990108 A 2750 RETRACT MECH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 197SW 120186 AFTER TAKEOFF FLAPS WOULD NOT RETRACT. CONTROL FAULT ON OVERHEAD ILLUMINATED. FLAP AND ADVANCED STALL WARNING LIGHT ON MAP. FOLLOWED QRH PROCEDURE. RETURNED TO FIELD COULDN'T DUPLICATE PROBLEM. CANNON PLUGS VISUALLY CHECKED GOOD AT OUT BOARD AND INBOARD ACTUATORS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021200296 19990212 00296 1999 2 12 ARWA990201 4 19990130 A 3442 20412151102 INDICATOR DOUG DC8 DC863F 302198F WP COCKPIT FAILED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 441J 1498 45988 MIA - FLT 510 - DURING CLIMB-OUT, RADAR QUIT WORKING. RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED RADAR I NDICATOR, ANTENNA, AND R/T UNIT. SYSTEM OPS OK ON THE GROUND PER MM 34-42-0. REF: OPER CONTROL NR 98ZZZX562 AND 98ZZZ X563. (X) 2 L 7 4 4F 4A25 1999021200297 19990212 00297 1999 2 12 99ZZZX562 4 19990130 A 3442 ANT1P ANTENNA DOUG DC8 DC863F 302198F WP COCKPIT FAILED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 441J 1456 45988 MIA - FLT 510 - DURING CLIMB-OUT, RADAR QUIT WORKING. RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED RADAR I NDICATOR, ANTENNA, AND R/T UNIT. SYSTEM OPS OK ON THE GROUND PER MM 34-42-0. REF: OPER CONTROL NR ARWA990201 AND 98ZZ ZX563. 2 L 7 4 4F 4A25 1999021200298 19990212 00298 1999 2 12 99ZZZX563 4 19990130 A 3442 20671570153 RT UNIT DOUG DC8 DC863F 302198F WP COCKPIT FAILED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 441J 3516 45988 MIA - FLT 510 - DURING CLIMB-OUT, RADAR QUIT WORKING. RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED RADAR I NDICATOR, ANTENNA, AND R/T UNIT. SYSTEM OPS OK ON THE GROUND PER MM 34-42-0. REF: OPER CONTROL NR ARWA990201 AND 98ZZ ZX562. 2 L 7 4 4F 4A25 1999021200299 19990212 00299 1999 2 12 ARWA990202 4 19990130 A 3442 20671570153 RADAR DOUG DC8 DC863F 302198F WP COCKPIT INOPERATIVE A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 441J 6491 45988 MIA - FLT 510 - FLIGHT EN ROUTE ATL TO SJU DIVERTED TO MIA DUE TO WEATHER RADAR INOPERATIVE. REMOVED AND REPLACED RADAR R/T. OPS CHECK OK PER MM 34-42-0. (X) 2 L 7 4 4F 4A25 1999021200300 19990212 00300 WP 1999 2 12 USAAD99009 1 19990117 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG DISCHARGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 987VJ 47210 CMH/LGA - FLT 293 - AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AND A IRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NO SE STRUT FLAT. THE NOSE GEAR STRUT WAS SERVICED WITH OIL NITROGEN, NO LEAKS WERE NOTED. (X) 2 L 7 2 4F A6WE 1999021200301 19990212 00301 WP 1999 2 12 USAAD99008 1 19990112 A 2170 V1211 COALESCER BAG DOUG DC9 DC931 3022065 WP A/C BAY CONTAMINATED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 918VJ 48138 CLT/CLE - FLT 1174 - DURING APPROACH, THE LAVATORY SMOKE DETECTORS ACTIVATED. AFTER TURNING OFF THE ENGINE BLEEDS, THE SMOKE DETECTORS RETURNED TO NORMAL. MAINTENANCE CHECKED THE ENGINE INLET AND EXHAUST FOR EVIDENCE OF OIL LEAKS AND BOTH AIR CYLCE MACHINES FOR OPERATION AND OIL LEVEL, ALL APPEARED NORMAL. THE AIR CONDITIONING COALESCER BAGS WERE FOUND TO BE EXTREMELY DIRTY. THE COALESCER BAGS WERE REPLACED AND THE AIR CONDITIONING SYSTEMS OPERATED USING BOTH ENGINES AND AN EXTERNAL AIR SUPPLY CART. MAINTENANCE WAS UNABLE TO DETECT ANY FURTHER SMELL OR SMOKE. (X) 2 L 7 2 4F A6WE 1999021200302 19990212 00302 CE 1999 2 12 99ZZZX564 1 19990104 A 3230 11482014511 LINK BEECH 1900 1900D 1154162 CE NLG BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 830CA 13109 UE19 NOSE LANDING GEAR FAILED TO EXTEND. UPON INSPECTION OF AIRCRAFT, NOSE GEAR CENTERING LINK ASSEMBLY FOUND BROKEN. REPLA CED NOSE GEAR CENTERING LINK ASSEMBLY WITH NEW ASSEMBLY. PERFORMED INSPECTION OF NOSE GEAR CENTERING LINK ASSEMBLY ON A LL AIRCRAFT IN FLEET. (X) 2 L 7 2 4T RT A24CE 1999021200303 19990212 00303 NM 1999 2 12 P2EA99005 1 19990115 A 5230 10608217 SEAL BOEING 737 737222 1384473 NM CARGO DOOR TORN A P2EA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 208AU 19547 MSP - FLT 701 - DURING CRUISE FLIGHT, FELT NOSE AND VIBRATION. CABIN PRESSURE BEGAN TO RISE. SWITCHED TO STANDBY PRESS URE AND BEGAN DESCENT. CABIN PRESSURE STABILIZED AT FL 180. FOUND FORWARD CARGO DOOR SEAL TORN. REPLACED FORWARD CARG O DOOR SEAL PER MM 52-09-121. PRESSURIZED A/C TO 6.5 PSI FOR 15 MINUTES, NO DEFECTS FOUND. (X) 2 L 7 2 4F A16WE 1999021200309 19990212 00309 NM 1999 2 12 UIEA9901 1 19990101 A 2612 FIRE DETECTOR BOEING 747 747243B 1384830 NM APU BAY MALFUNCTIONED A UIEA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 15 518MC 23476 APU FIRE WARNING CAME ON SEVERAL TIMES. DISCHARGED BOTTLE AS PRECAUTION. MAINTENANCE AT ANC INSPECTED APU COMPARTMENT, NO DAMAGE OR FIRE NOTED. PLEASE NOTE, APU PREVIOUSLY DEFERRED DUE WILL NOT ACCELERATE ABOVE 60 PERCENT. APU FIRE WARN ING SYSTEM DEFERRED TO MAINTENANCE CHECK AT AMS ON 1-4-98, AT WHICH TIME THE APU WILL ALSO BE REPLACED. DURING C-CHECK, APU AND FIRE BOTTLES WERE REPLACED AND APU FIRE DETECTION SYSTEM WAS CHECKED AND FOUND SATISFACTORY PER MM 26-15-00. ( X) 2 L 7 4 4F A20WE 1999021200310 19990212 00310 EU 1999 2 12 USAAF99006 2 19990118 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 EU RIGHT LIGHTNING STRIKE A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 855US 11283 PIT - FLT 717 - DURING DESCENT INTO PIT, AT AN ALTITUDE OF 7,000 FEET, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. NUMER OUS FAULT MESSAGES ILLUMINATED. THE RIGHT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO. AT THIS TIME, THE CREW MOVED THE RIGHT ENGINE THROTTLE LEVER TO IDLE THRUST. THE CREW DECLARED AN EMERGENCY AND ASKED FOR IMMEDIATE CLEARANCE TO LAN D. THE WEATHER AT PIT WAS NOT GOOD FOR LANDING, SO THE FLIGHT DIVERTED TO AGC. THE FLIGHT LANDED AGC WITHOUT FURTHER I NCIDENT. AFTER LANDING, THE CREW SHUT DOWN THE RIGHT ENGINE. MAINTENANCE ACTION PENDING. (X) 2 L 7 2 4F 4 F RT E25NE 1999021200313 19990212 00313 WP 1999 2 12 ORJA9917 1 19990120 A 3350 60030451 BATERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 LAX - SECTIONS 12-16 SHIP RIGHT EMERGENCY EVAC LIGHTS FLICKER ON. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK. (X ) 2 L 7 2 4F RT A6WE 1999021200316 19990212 00316 NM 1999 2 12 USAA990032 1 19990120 A 5313 STRINGER BOEING 767 767201 1385125 NM BS 1564 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH, AT BS 1564 STR 37L. REPLACED STRINGER SECTION PER SR M 53-00-03 FIG 202. (X) 2 L 7 2 4F RT A1NM 1999021200317 19990212 00317 NM 1999 2 12 USAA990036 1 19990120 A 5347 118149 SEAT TRACK BOEING 767 767201 1385125 NM BS 347 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH BY 2 INCHES, BS 347 LBL 54.75 SEAT TRACK. REMOVED AND INSTALLED SEAT TRACK PER SRM 53-00-52. (X) 2 L 7 2 4F RT A1NM 1999021200318 19990212 00318 NM 1999 2 12 USAA990035 1 19990120 A 5350 FAIRING BOEING 767 767201 1385125 NM BS 1000 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION STA 1000 LEFT OF KEEL BEAM OF FAIRING FLANGE. REPAIRED PER SR M 53-50-12, PAGE 107. (X) 2 L 7 2 4F RT A1NM 1999021200319 19990212 00319 NM 1999 2 12 USAA990031 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 764 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STA'S 764, 777, 780, 795, 806, AND 814. REPLACE D SEAT TRACK FROM STA 764 TO STA 814 PER SRM 51-10-00. REF: OPERATOR CONTROL NR 99ZZZX566 THROUGH 99ZZZX570. (X) 2 L 7 2 4F RT A1NM 1999021200320 19990212 00320 NM 1999 2 12 99ZZZX566 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 777 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STA'S 764, 777, 780, 795, 806, AND 814. REPLACE D SEAT TRACK FROM STA 764 TO STA 814 PER SRM 51-10-00. REF: OPERATOR CONTROL NR USAA990031, AND, 99ZZZX567 THROUGH 99Z ZZX570. 2 L 7 2 4F RT A1NM 1999021200321 19990212 00321 NM 1999 2 12 99ZZZX567 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 780 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STA'S 764, 777, 780, 795, 806, AND 814. REPLACE D SEAT TRACK FROM STA 764 TO STA 814 PER SRM 51-10-00. REF: OPERATOR CONTROL NR USAA990031, AND, 99ZZZX566 THROUGH 99Z ZZX570. 2 L 7 2 4F RT A1NM 1999021200322 19990212 00322 NM 1999 2 12 99ZZZX568 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 795 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STA'S 764, 777, 780, 795, 806, AND 814. REPLACE D SEAT TRACK FROM STA 764 TO STA 814 PER SRM 51-10-00. REF: OPERATOR CONTROL NR USAA990031, AND, 99ZZZX566 THROUGH 99Z ZZX570. 2 L 7 2 4F RT A1NM 1999021200323 19990212 00323 NM 1999 2 12 99ZZZX569 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 806 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STA'S 764, 777, 780, 795, 806, AND 814. REPLACE D SEAT TRACK FROM STA 764 TO STA 814 PER SRM 51-10-00. REF: OPERATOR CONTROL NR USAA990031, AND, 99ZZZX566 THROUGH 99Z ZZX570. 2 L 7 2 4F RT A1NM 1999021200324 19990212 00324 NM 1999 2 12 99ZZZX570 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 814 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STA'S 764, 777, 780, 795, 806, AND 814. REPLACE D SEAT TRACK FROM STA 764 TO STA 814 PER SRM 51-10-00. REF: OPERATOR CONTROL NR USAA990031, AND, 99ZZZX566 THROUGH 99Z ZZX569. 2 L 7 2 4F RT A1NM 1999021200325 19990212 00325 NM 1999 2 12 USAA990037 1 19990120 A 5350 FAIRING BOEING 767 767201 1385125 NM BS 980 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION STA 980 RT SIDE KEEL BEAM FAIRING FLANGE NEAR SCREW HOLE. REP AIRED PER SRM 53-50-12 AND E.O. 5195T055, PART 2, STEPS 2, 4. (X) 2 L 7 2 4F RT A1NM 1999021200326 19990212 00326 NM 1999 2 12 USAA990033 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 625-754 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION LT OUTBOARD SEAT TRACK STA 625 THROUGH STA 754. REPAIRED PER SRM 53-00-52, FIG 101, AND SRM 51-20-01 AND SRM 51-21-01. (X) 2 L 7 2 4F RT A1NM 1999021200327 19990212 00327 NM 1999 2 12 USAA990030 1 19990120 A 5315 141T5140147 FLOORBEAM BOEING 767 767201 1385125 NM BS 325 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM 1 INCH BY 79 INCHES AT STA 325 RBL 23 TO RBL 56. INSTALLED DOUBLER PER SRM 53-00-51 FIG 201. (X) 2 L 7 2 4F RT A1NM 1999021200328 19990212 00328 NM 1999 2 12 USAA990034 1 19990120 A 5320 CLIP BOEING 767 767201 1385125 NM BS 1654 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK STA 1654.5 AND STR 30L AT TIE CLIP. REPAIRED PER SRM 51-10-00. (X) 2 L 7 2 4F RT A1NM 1999021200329 19990212 00329 NM 1999 2 12 USAA990038 1 19990120 A 5315 14T005511 FLOORBEAM BOEING 767 767201 1385125 NM BS 246 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK ON STIFFENER ANGLE STA 246 FLOORBEAM FORWARD FACE AT LB BL 17.0. REPAIRED FLOORBEAM ANGLE PER SRM 51-10-00. (X) 2 L 7 2 4F RT A1NM 1999021200330 19990212 00330 EU 1999 2 12 RAIA990110 1 19990107 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 971JX 10214 98 971 SAN - FLT 4710 - VIBRATION FELT IN-FLIGHT CONTROLS, SUSPECT RT ENGINE. MAINTENANCE REPLACED RT ENGINE STARTER. (X) 2 L 7 2 4T RT A56EU 1999021200331 19990212 00331 EU 1999 2 12 RAIA990111 1 19990112 A 2422 559012A INVERTER AEROSP ATR72 ATR72202 8680940 EU NR 2 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 721TE 217 STL - FLT 7398 - NR 2 INVERTER FAILED. MAINTENANCE REPLACED NR 2 INVERTER. (X) 2 H 7 2 4T RT A53EU 1999021200335 19990212 00335 EU 1999 2 12 RAIA990109 1 19990111 A 3243 ACM26810 MASTER CYLINDER BAG JETSTM JETSTM3201 1500217 EU RIGHT INOPERATIVE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 427AM 876 STL - FLT 7058 - RIGHT BRAKE INOPERATIVE. MAINTENANCE SERVICED CAPTAIN'S AND FIRST OFFICER'S RIGHT BRAKE MASTER CYLINDE R. (X) 2 L 7 2 4T RT A56EU 1999021200336 19990212 00336 WP 1999 2 12 TWAA9902101 1 19990206 A 3350 0105606002 MODULE DOUG DC9 DC983 3022083 WP ROW 22 WORN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9405T 53141 TAPE COVERING WIRES OF EGRESS FLOOR LIGHTS AT REAR OVERWING EXIT, ROW 22, WAS PULLED UP EXPOSING WIRES. REPLACED THE LA MP MODULE AND THE CRACKED LENS COVER, (P/N 0105607-001). CHECK-C 11-11-98 MCI. 2 L 7 2 4F RT A6WE 1999021200337 19990212 00337 WP 1999 2 12 TWAA9902102 1 19990206 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 22 LOOSE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9405T 53141 THE EGRESS LIGHTING PULLED UP AND DISCONNECTED AT THE OVERWING EXIT ROW 22. RECONNECTED AND SECURED EGRESS LIGHTING. C HECK-C 11-11-98 MCI. 2 L 7 2 4F RT A6WE 1999021200338 19990212 00338 WP 1999 2 12 TWAA9902103 1 19990129 A 5532 SKIN DOUG DC9 DC983 3022083 WP VERT STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 VERTICAL STABILIZER UPPER L/E HAD 5 BY 3 BY 0.400 INCH DEEP DENT AND 3 INCH CRACK. REPAIRED PER SPM 55-03, PAGE 5, CLAS S B REPAIR. CHECK-C 4-10-98 STL. 2 L 7 2 4F RT A6WE 1999021200339 19990212 00339 WP 1999 2 12 TWAA9902104 1 19990201 A 5347 TRACK DOUG DC9 DC983 3022083 WP BS 1212-1318 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 IN THE AFT CARGO COMPT THE LT CARGO TIE DOWN TRACK WAS CORRODED FROM STA 1212 TO 1318. REMOVED CORROSION PER SPM 6-80-0 1. REPLACED TRACK PER SPM 6-70-01. CHECK-C 4-10-98 STL. 2 L 7 2 4F RT A6WE 1999021200340 19990212 00340 WP 1999 2 12 TWAA9902105 1 19990201 A 5320 BRACKET DOUG DC9 DC983 3022083 WP BS 1297 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 FOUND CARGO TRACK TIEDOWN BRACKET TO FORMER CRACKED AND CORRODED AT STA 1297, ABOVE STRINGER 28L AND S28R. REPLACED BRA CKETS WITH (P/N 5956034-561), PER SPM 6-70-01, PG 1 ITEM 1. CHECK-C 4-10-98 STL. 2 L 7 2 4F RT A6WE 1999021200341 19990212 00341 WP 1999 2 12 TWAA9902106 1 19990201 A 5347 TRACK DOUG DC9 DC983 3022083 WP BS 1212-1318 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 FOUND RT CARGO TIE DOWN TRACK CORRODED FROM STA 1212 TO 1318. REMOVED CORROSION PER SPM 6-80-01. REPLACED TIE DOWN TRA CK PER SPM 6-70-01. CHECK-C 4-10-98 STL. 2 L 7 2 4F RT A6WE 1999021200342 19990212 00342 WP 1999 2 12 TWAA9902107 1 19990131 A 5311 FORMER DOUG DC9 DC983 3022083 WP BS 1155 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 FOUND CORROSION ON FORMER AT STA 1155, LONGERON 29L TO 29R. REPLACED FORMER PER SPM 6-70-01. CHECK-C 4-10-98 STL. 2 L 7 2 4F RT A6WE 1999021200343 19990212 00343 WP 1999 2 12 TWAA9902108 1 19990131 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1155-1160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 FOUND CORROSION ON BOX WEB AT STA 1155 AND 1160, BETWEEN LONGERON 29R AND 30. REPLACED WEB PER STANDARD PROCESSES MANUA L 6-70-1. CHECK-C 4-10-98 STL. 2 L 7 2 4F RT A6WE 1999021200344 19990212 00344 WP 1999 2 12 TWAA9902109 1 19990131 A 5311 FORMER DOUG DC9 DC983 3022083 WP BS 1250 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 FOUND CORROSION ON FORMER AT STA 1250, LONGERON 27L TO 27R. REMOVED CORROSION MECHANICALLY AND SAND BLASTING. TREATED AND PAINTED PER SPM 6-80-11. REPAIRED PER SRM 53-03, FIG 2A. CHECK-C 4-10-98 STL. 2 L 7 2 4F RT A6WE 1999021200345 19990212 00345 WP 1999 2 12 TWAA9902110 1 19990203 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 680 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND IN CABIN A VERTICAL ATTACH FITTING AT STA 680, RBL 44, BELOW FLOOR, CORRODED AT LOWER EN D. REMOVED AND REPLACED PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999021200346 19990212 00346 WP 1999 2 12 AT9900078 1 19990204 A 3397 WIRE DOUG DC9 DC932 3022066 WP L1 DOOR SHORTED A ZZDA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 15 849AT 47484 EMERGENCY PATH LIGHTING NOT WORKING FROM BUSINESS CLASS FORWARD TO AND INCLUDING THE L-1 DOOR. REPAIRED SHORTED WIRE ON FORWARD SIDE OF FLOOR TRACK LIGHTING, OPS CHECKED GOOD IAW MM 33-53. 2 L 7 2 4F A6WE 1999021200347 19990212 00347 WP 1999 2 12 AT9900079 1 19990126 A 5320 1A418341 WEB DOUG DC9 DC932 3022066 WP BS 889-937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION OUT OF LIMITS AT THE CUSP WEB STA 889 THRU 937 L-18R. FABRICATE D NEW CUSP WEB SECTION AND INSTALLED IAW DC9 SRM 51-30-2, AND RES NR 99198. 2 L 7 2 4F A6WE 1999021200348 19990212 00348 WP 1999 2 12 AT9900080 1 19990120 A 5330 1A41832 SKIN DOUG DC9 DC932 3022066 WP BS 218 & 220 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CREASE AT STA 218 L-18-19L AND A DENT AT STA 220 L-18-19L BOTH OUT OF LIMI TS. COLD WORKED DENTS, FABRICATED INTERNAL DOUBLER REPAIR, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED AND INSTALLE D INTERNAL REPAIR IAW DC9 SRM 51-10-4, 51-30-2, 53-04 FIG 38, RES NR 99189 AND 99234. 2 L 7 2 4F A6WE 1999021200349 19990212 00349 WP 1999 2 12 AT9900081 1 19990120 A 5320 1A41858 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 503 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD CARGO PIT CEILING CENTER LINE AT STA 503 INTERCOASTAL CRACKED AT FO UR WAY TIE SUPPORT. FABRICATED REPAIR, HEAT TREATED, DRILLED, DEBURRED, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 51- 30-2, 53-11-2 FIG 4, 51-10-2A, 51-10-4, 51-10-3, 51-30-2, AND RES NR 99197. 2 L 7 2 4F A6WE 1999021200350 19990212 00350 WP 1999 2 12 AT9900082 1 19990130 A 5260 9915570101 SKIN DOUG DC9 DC932 3022066 WP VENTRAL STAIR DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND NUMEROUS DENTS IN AFT VENTRAL STAIRS LOWER AFT SKIN FROM SPLICE. REMOVED AND REPLACED EXISTING SKIN FROM PREVIOUS SPLICE IAW DC9 SRM 51-10-4, 51-30-2, AND RES NR 99221. 2 L 7 2 4F A6WE 1999021200351 19990212 00351 WP 1999 2 12 AT9900083 1 19990201 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 927 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT CUSP WEB AT STA 927 CORRODED. REMOVED AND FABRICATED AND INSTALLED C USP WEB SECTION IAW DC9 SRM 51-10-2, 53-11-3 FIG 11, 51-30-2, AND RES NR 99195. 2 L 7 2 4F A6WE 1999021200352 19990212 00352 SO 1999 2 12 RAAA99E4001 1 19990128 A 5400 ANGLE LKHEED 188 188C 5262604 SO NR 2 NACELLE CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 2 CHECK PER CARD 42.03.67, FOUND NR 2 NACELLE LOWER I/B SKATE ANGLE CORRODED AT NAC STA 60. REPAIRE D PER SRM 54-2-6, FIG 2, SHEET 2. M-54 NR 280. 2 L 7 4 4T 4A22 1999021200353 19990212 00353 SO 1999 2 12 RAAA99E4002 1 19990128 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 167 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 2 CHECK PER CARD 42.03.66, FOUND RIGHT WING LOWER NR 8 PANEL CORRODED AROUND JACK POINT AT WS 167. C LEANUP REQUIRED REMOVAL OF FULL THICKNESS OF PANEL APPROX 4.3 X 4.4 INCH. REPAIRED PER LDS DWG NR 188346. M-54 NR 89. 2 L 7 4 4T 4A22 1999021200360 19990212 00360 SO 1999 2 12 RAAA99E9009 1 19990205 A 3350 240498C RELAY LKHEED 188 188C 5262604 SO BS 555 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EXTERNAL EMERGENCY LIGHTS FAILED SERVICE CHECK DUE NO TEST. CHANGED EXTERNAL EMERGENCY LIGHT K106 RELAY DUE FAILED. 2 L 7 4 4T 4A22 1999021200361 19990212 00361 SO 1999 2 12 RAAA99E9010 1 19990205 A 3350 CA31 BATTERY PACK LKHEED 188 188C 5262604 SO BS 555 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EXTERNAL EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1999021200362 19990212 00362 SO 1999 2 12 RAAA99E9011 1 19990205 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO RT OVERWING DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1999021200363 19990212 00363 WP 1999 2 12 CALA9900109 1 19990205 A 3260 49548191 SUPPORT DOUG DC9 DC982 3022082 WP LT MLG DOOR BROKEN A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14890 49114 THE LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION BOUND FOR EWR. THE GEAR WAS CYCLED TWICE, BUT TH E LIGHT WOULD NOT EXTINGUISH. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT PROBLEM. MAINTENANCE FOUND THE L T MAIN GEAR DOOR TARGET SUPPORT BROKEN OFF WITH TARGET GONE AND DAMAGE TO THE DOOR SENSOR. THE TARGET SUPPORT, TARGET A SSEMBLY AND SENSOR WERE REPLACED IAW MM 32-60-05. GEAR OPERATION AND INDICATIONS CHECKED GOOD. 2 L 7 2 4F A6WE 1999021200364 19990212 00364 NM 1999 2 12 CALA9900110 1 19990205 A 3232 731411 ACTUATOR BOEING 727 727232 1384082 NM LT MLG DOOR INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15781 20449 20636 THE LT MLG DOOR WOULD NOT RETRACT AFTER TAKEOFF FROM SFO. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCI DENT. MAINTENANCE REMOVED AND REPLACED THE LT MLG DOOR ACTUATOR IAW MM 32-32-81. LEAK AND OPERATIONAL CHECKS WERE GOOD . 2 L 7 3 4F A3WE 1999021200365 19990212 00365 NM 1999 2 12 CALA9900111 1 19990206 A 2120 AIR DIST BOEING 737 737524 1384721 NM CABIN ODOR A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 18658 28919 SMOKE WITH A PLASTIC BURNING ODOR IN THE CABIN AFTER TAKEOFF. THE GALLEY POWER WAS TURNED OFF AND THE ACFT WAS RETURNED TO IAH. THE SMOKE CLEARED AND LANDED WITHOUT INCIDENT. MX FOUND NO EVIDENCE OF FIRE OR OVERHEATING. THE GALLEY OVENS , COFFEMAKERS, AND WARMER PADS WERE CHECKED WITH NO EVIDENCE OF OVERHEATING FOUND. ALL GALLEY LIGHTS, LAVS, LAV MOTORS, AND TRASH CANS WERE CHECKED, PROBLEMS FOUND. ALL COACH PSU'S WERE INSPECTED, ABNORMALITIES FOUND. THE CEILING PANELS AT ROW 17 TO 20 WERE OPENED AND INSPECTION, NO ABNORMALITIES. IN ADDITION, BURNT OUT BULBS AT READING LIGHTS 12C AND 15 A WERE REPLACED. BOTH ENGINES WERE RUN AT CLIMB POWER, CABIN PRESSURIZED TO 4 PSI AND PROBLEM COULD NOT BE DUPLICATED. 2 L 7 2 4F RT A16WE 1999021200366 19990212 00366 NM 1999 2 12 CALA9900112 1 19990207 A 2750 65C26300101 RETRACT MECH BOEING 737 737524 1384721 NM LT TE FLAP DAMAGED A CALA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SW 09 37615 27328 THE FLAPS STUCK AT EIGHT DEGREES ON APPROACH TO EWR. THE FLAPS COULD NOT BE CYCLED HYDRAULICALLY OR ELECTRICALLY. A GO -AROUND WAS PERFORMED AND AN EMERGENCY LANDING WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND T HE LT FLAP TORQUE SHAFT CLEARANCE DOOR DAMAGED. THE TRACK FAIRING AND SHAFT CLEARANCE DOOR WERE REMOVED. CONFIGURATION DEVIATION LIST 57-53-01 WAS ISSUED PENDING DOOR REPLACEMENT AND THE TRACK FAIRING WAS REINSTALLED. THE FLAPS OPERATED NORMALLY THROUGHOUT ENTIRE TRAVEL. 2 L 7 2 4F RT A16WE 1999021200367 19990212 00367 NM 1999 2 12 CALA9900113 1 19990203 A 2560 416N222022 BOTTLE BOEING 757 757224 1384958 NM ESCAPE SLIDE LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17128 27567 INSPECTION FOUND LT EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE LOW. THE ESCAPE SLIDE BOTTLE WAS REMOVED AND REPLACED IAW MM 25-65-02, PAGE 419. BOTTLE PRESSURE AND SQUIB TEST WAS GOOD. 2 L 7 2 4F RT A2NM 1999021200368 19990212 00368 NM 1999 2 12 CALA9900114 1 19990203 A 3350 BPS73 BATTERY PACK BOEING 757 757224 1384958 NM L4 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17128 27567 INSPECTION FOUND THE L-4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED IAW MM 33-51-07. 2 L 7 2 4F RT A2NM 1999021200369 19990212 00369 WP 1999 2 12 9900329152 1 19990205 A 5330 FRAME DOUG DC9 DC914 3022034 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING PERIODIC CHECK, FOUND FRAME UPPER RIGHT CORNER SIDE CRACKED FS 83.5. REPAIRED PER EA 91-164891, REV A (P/N 99115 05-7). 2 L 7 2 4F A6WE 1999021200370 19990212 00370 WP 1999 2 12 9900339308 1 19990205 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1463 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 311RC 48089 DURING PERIODIC CHECK, FOUND FRAME CRACKED AT FS 1463. REPAIRED PER EA 93-163701. 2 L 7 2 4F A6WE 1999021200371 19990212 00371 WP 1999 2 12 9900349608 1 19990205 A 5414 SKIN DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608NW 608NW DURING PERIODIC CHECK, FOUND PYLON AREA SKIN CRACKED AT FS 1038, LONGERON 15R. REPAIRED PER EA 99-163248. 2 L 7 2 4F A6WE 1999021200374 19990212 00374 WP 1999 2 12 9900359311 1 19990204 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314RC 49110 DURING LINE MAINTENANCE INSPECTION, FOUND THE TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIE S, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999021200375 19990212 00375 WP 1999 2 12 9900369877 1 19990203 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999021200376 19990212 00376 WP 1999 2 12 9900379603 1 19990201 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603NW 47101 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK AND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999021200377 19990212 00377 WP 1999 2 12 9900389886 1 19990127 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 600TR 47783 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN SEAT ROW EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999021200378 19990212 00378 WP 1999 2 12 9900399883 1 19990204 A 2797 WIRE DOUG DC9 DC951 3022051 WP SPOILER ACTUATOR CHAFED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 671MC 47660 DURING CRUISE FLIGHT EN ROUTE BWI-DTW, SPARKS BEGAN EMITTING FROM CENTER COCKPIT PEDESTAL UNDER ADF, ARCING LASTED APPRO AIMATELY FIVE SECONDS. FLIGHT WAS DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED FORWARD PEDESTAL AREA AND FOUND WIRES BURNED AT P1-244 TO SPOILER ACTUATOR. COTTER PIN IN SPOILER ACTUATOR ROD WAS FOUND CHAFED TO WIRE BUNDLE. REPAIRED WIRES AND REROUTED WIRE BUNDLE AWAY FROM SPOILER ACTUATOR ROD, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999021200379 19990212 00379 NM 1999 2 12 9900402714 1 19990114 A 3260 MECHANISM BOEING 727 7272S7 138407Z NM NLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 718RC 22344 ON CLIMBOUT, CREW WAS UNABLE TO EXTINGUISH THE NOSE LANDING GEAR DOOR LIGHT. CREW PERFORMED GEAR CYCLE AND THE LIGHT RE MAINED ILLUMINATED. THE FLIGHT RETURNED TO DEPARTURE CITY WITHOUT INCIDENT. MAINTENANCE RIGGED DOORS AND PERFORMED GEA R SWING. ALL INDICATIONS CHECKED OK. 2 L 7 3 4F A3WE 1999021200380 19990212 00380 SO 1999 2 12 COMA9910031 1 19990203 A 3350 LENS EMB 120 EMB120RT SO ROW 5 MISSING A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 244CA 120217 EMERGENCY EXIT LIGHT COVER IS MISSING AT ROW 5. REPLACED LIGHT COVER. 2 L 7 2 4T RT A31SO 1999021200381 19990212 00381 EA 1999 2 12 COMA990057 1 19990204 A 2731 70607 CONTROL UNIT CNDAIR CL600 CL6002B19 EA ELEVATOR TRIM MALFUNCTION A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 912CA 7011 ELEVATOR TRIM INOPERABLE, NOSE DOWN. REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT. 2 L 7 2 4F RT A21EA 1999021200382 19990212 00382 EA 1999 2 12 COMA9960058 1 19990204 A 2121 AEO804AA1 FAN CNDAIR CL600 CL6002B19 EA E & E COMPT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 917CA 12852 7017 COOL CAUTION MESSAGE. REPLACED COOLING FAN. 2 L 7 2 4F RT A21EA 1999021200383 19990212 00383 EA 1999 2 12 COMA9960059 1 19990204 A 3242 50105201 BRAKE CNDAIR CL600 CL6002B19 EA LT MLG LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 3741 2253 7109 NOTICED LEFT OUTBOARD BRAKE LEAKING AFTER GROUND RUNS. REPLACED BRAKE. 2 L 7 2 4F RT A21EA 1999021200384 19990212 00384 EA 1999 2 12 COMA9960060 1 19990204 A 5320 601R3505025 BRACKET CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 CARGO DOOR TRACK, FORWARD SIDE, LOWER BRACKET BROKEN. REPLACED BRACKET. 2 L 7 2 4F RT A21EA 1999021200385 19990212 00385 EA 1999 2 12 COMA9960061 1 19990204 A 2730 10231107 DAMPENER CNDAIR CL600 CL6002B19 EA RT ELEVATOR LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 957CA 1684 7109 RIGHT OUTBOARD ELEVATOR FLUTTER DAMPENER IS LEAKING. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999021200386 19990212 00386 SO 1999 2 12 COMA9960062 1 19990209 A 5320 12005807007 BEAM EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 256CA 18922 5679 120245 DURING AN E5 PART A INSPECTION, CORROSION DAMAGE WAS FOUND ON THE UPPER SURFACE OF THE CENTER OMEGA BEAM AT FRAME 16. T HE DAMAGE CONSISTS OF 1 HOLE AND 4 AREAS OF PITTING. THE HOLE WAS CLEANED UP, DEBURNED AND SHARP EDGES REMOVED. THE 4 AREAS OF PITTING WAS ALSO CLEANED UP. AN EXTERNAL DOUBLER WAS THEN ADDED TO COVER ALL DAMAGED AREAS IAW AERODESIGN AIRC RAFT ENGINEERING REPORT NR 2181-7. 2 L 7 2 4T RT A31SO 1999021200387 19990212 00387 EA 1999 2 12 COMA9960063 1 19990206 A 2751 WARNING CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA K NONE N FALSE WARNING LD LANDING 1 SO 01 735CA 7267 FLAP FAIL MESSAGE DURING LANDING. COMPLIED WITH AD98-20-01 PARAGRAPH B 1, 2, 3 A, B, C AND E. FLAP SYSTEM RESET SUCCES SFULLY. 2 L 7 2 4F RT A21EA 1999021200388 19990212 00388 EA 1999 2 12 COMA9960064 1 19990205 A 2421 GENERATOR CNDAIR CL600 CL6002B19 EA NR 2 FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 01 984CA 7171 NR 2 GENERATOR FAULT MESSAGE DURING TAKEOFF. ABORTED AND RETURNED TO THE GATE. DEFERRED NR 2 GENERATOR. 2 L 7 2 4F RT A21EA 1999021200389 19990212 00389 EA 1999 2 12 COMA9960065 1 19990205 A 2750 85501007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 932CA 4794 7038 FLAP FAIL CAUTION MESSAGE DURING APPROACH. REPLACED THE LEFT AND RIGHT BPSU. 2 L 7 2 4F RT A21EA 1999021200390 19990212 00390 EA 1999 2 12 COMA9960066 1 19990205 A 5210 DOOR CNDAIR CL600 CL6002B19 EA PAX COMPT DIRTY A COMA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 01 729CA 7265 CABIN DOOR WARNING MESSAGE DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. REMOVED DEBRIS FROM MAIN CABIN DOOR JAMB. 2 L 7 2 4F RT A21EA 1999021200391 19990212 00391 NM 1999 2 12 UPS99228636 1 19990126 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 760-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, TO FACILITATE REPAIR OF FRAME 848.95 SEAT TRACK BETWEEN BS 760-870 L BL 62.5 HAD TO BE REMOVED ON REM OVAL OF THIS SEAT TRACK SECTION IT WAS FOUND TO BE CORRODED. SEAT TRACK SECTION REPLACED IAW SRM 53-10-5 FIG 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999021200392 19990212 00392 NM 1999 2 12 UPS99228637 1 19990125 A 5241 HINGE BOEING 727 72730C 1384009 NM GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CRACK (5MM) FOUND IN MID GALLEY DOOR HINGE FWD LOWER CUTOUT. REPAIR CARRIED OUT IAW EO B727-5330-106 3 APPENDIX B. 2 L 7 3 4F A3WE 1999021200393 19990212 00393 NM 1999 2 12 UPS99228638 1 19990122 A 5230 69191705 WEB BOEING 727 72730C 1384009 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, DURING INSPECTION OF AFT CARGO DOOR STOP FITTINGS SUSPECT CRACK FOUND IN WEB, FWD OF AFT DOOR HINGE I NSIDE DOOR WEB. REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1999021200394 19990212 00394 NM 1999 2 12 UPS99228639 1 19990122 A 5754 RIB BOEING 727 72730C 1384009 NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, NR 6 L/E SLAT CRACK IN RIB 6 O/B OF FLAP ACTUATOR. AREA REPAIRED IAW SRM 57-50-03 FIG 9. 2 L 7 3 4F A3WE 1999021200395 19990212 00395 NM 1999 2 12 UPS99228640 1 19990107 A 5312 65159682 BULKHEAD FITTING BOEING 727 72730C 1384009 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, BS 740 FITTING CRACKED RIGHT HAND SIDE BS 740 RT BULKHEAD FORGING. REPLACED PER EO B727-5310-7477-D. 2 L 7 3 4F A3WE 1999021200396 19990212 00396 NM 1999 2 12 UPS99228643 1 19990201 A 5753 65192086 TRACK BOEING 727 72722C 138400F NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-AD, FLAP TRACK NR 8 CRACKED AT TIP. FLAP TRACK REPLACED IAW MM 57-51-31. 2 L 7 3 4F A3WE 1999021200399 19990212 00399 EU 1999 2 12 QXEA9900137 1 19990115 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT-HAND APU ENCLOSURE HAD BEEN CHAFING ON LATERAL BEAM AT FRAME 17565. REPAIRED IAW HORIZON AIR EA 4-53-676. 2 L 7 2 4F RT A20EU 1999021200400 19990212 00400 EU 1999 2 12 QXEA9900138 1 19990119 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 50-2 FORWARD SIDE FRAME CASTELLATION IS CRACKED BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-10- 05 PAGE 601, SRM 51-31-01 PAGE 17 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999021200401 19990212 00401 EU 1999 2 12 QXEA9900139 1 19990115 A 2760 BEARING FOKKER F28 F28MK4000 4990810 EU SPEED BRAKES LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - SPEED BRAKE AIRFRAME CONNECTION LINK PIVOT POINT, UPPER AND LOWER BEARINGS ON LEFT-HAND AND RIGHT-HAND SIDES ARE L OOSE IN HOUSINGS. REPAIRED IAW HORIZON AIR EA 4-53-652. 2 L 7 2 4F RT A20EU 1999021200402 19990212 00402 EU 1999 2 12 QXEA9900140 1 19990116 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 32-2 FORWARD SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 7. REPAIRED IAW FOKKER SRM 53-02- 13 PAGE 5 FIGURE 3. 2 L 7 2 4F RT A20EU 1999021200403 19990212 00403 EU 1999 2 12 QXEA9900141 1 19990119 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 198.32 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE UPPER SHORT FRAME 198.32 AFT SIDE FRAME CASTELLATION IS CRACKED NEAR STRINGER 39. REPAIRED IAW FOKK ER SRM 51-31-01 AND HORIZON AIR EA 4-53-669. 2 L 7 2 4F RT A20EU 1999021200404 19990212 00404 EU 1999 2 12 QXEA9900142 1 19990117 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE UPPER SHORT FRAME19976 AFT SIDE FRAME CASTELLATION IS CRACKED NEAR STRINGER 39. REPAIRED IAW FOKKER SRM 53-10-2, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200405 19990212 00405 EU 1999 2 12 QXEA9900143 1 19990117 A 5310 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE UPPER SHORT FRAME 20075 AFT SIDE FRAME CASTELLATION IS CRACKED NEAR STRINGER 39. REPAIRED IAW FOKKE R SRM 51-31-01 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200406 19990212 00406 EU 1999 2 12 QXEA9900144 1 19990105 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SPEED BRAKE HAS SEVERAL RIVETS PULLING THROUGH SKIN ON BACK MIDDLE FRAME. REPAIRED IAW FOKKER SRM 51-31 -05 AND SRM 53-02-01, PAGE 11 FIGURE 9. 2 L 7 2 4F RT A20EU 1999021200407 19990212 00407 EU 1999 2 12 QXEA9900145 1 19990111 A 2760 BEARING FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND SPEED BRAKE CROSSHEAD TO SUPPORT LINK PUSH ROD AFT BEARING HAS APPROXIMATELY .030 RADIAL PLAY. REPAIRED IAW HORIZON AIR EA 4-53-651 AND EA 4-55-108. 2 L 7 2 4F RT A20EU 1999021200408 19990212 00408 EU 1999 2 12 QXEA9900146 1 19990104 A 5755 RIVET FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT-HAND SPEED BRAKE HAS THREE LOOSE RIVETS JUST BELOW SKID PLATE. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999021200409 19990212 00409 EU 1999 2 12 QXEA9900147 1 19990111 A 2760 SUPPORT LINK FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT-HAND SPEED BRAKE CROSSHEAD TO SUPPORT LINK PUSH ROD HAS APPROXIMATELY .050 RADIAL PLAY AT SUPPORT LINK. REP AIRED IAW HORIZON AIR EA 4-53-651 AND EA 4-55-108. 2 L 7 2 4F RT A20EU 1999021200410 19990212 00410 EU 1999 2 12 QXEA9900148 1 19990117 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 32-2 AFT SIDE FRAME CASTELLATION HAS BEEN STOP DRILLED THREE TIMES AND EXCEEDS LIMITATIONS AT STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 4. 2 L 7 2 4F RT A20EU 1999021200411 19990212 00411 EU 1999 2 12 QXEA9900149 1 19990113 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 41-2 AFT SIDE FRAME CASTELLATION IS CRACKED AT RIVET NEAR STRINGER 44. REPAIRED IAW FOKKER SR M 53-02-13 PAGE 6 FIGURE 4 AND MM 53-10-05 PAGE 601. 2 L 7 2 4F RT A20EU 1999021200412 19990212 00412 EU 1999 2 12 QXEA9900150 1 19990112 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 50-2 FORWARD SIDE FRAME CASTELLATION STOP DRILL REPAIR IS DRILLED INTO STRINGER AT STRINGER 53 . REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6 FIGURE 4 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200413 19990212 00413 EU 1999 2 12 QXEA9900151 1 19990116 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 32-2 AFT SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 21A. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 4. 2 L 7 2 4F RT A20EU 1999021200414 19990212 00414 EU 1999 2 12 QXEA9900152 1 19990117 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 32-2 AFT SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6, FIGURE 4 AND MM 53-10-05 PAGE 601A. 2 L 7 2 4F RT A20EU 1999021200415 19990212 00415 EU 1999 2 12 QXEA9900153 1 19990112 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 41-2 AFT SIDE FRAME CASTELLATION IS CRACKED AND STOP DRILLED BEYOND LIMITATIONS AT STRINGER 30 . REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1999021200416 19990212 00416 EU 1999 2 12 QXEA9900154 1 19990111 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 50-2 AFT SIDE FRAME CASTELLATION IS CRACKED BEYOND LIMITATION AT STRINGER 48. REPAIRED IAW FO KKER SRM 53-02-13, PAGE 6, REPAIR SCHEME 2. 2 L 7 2 4F RT A20EU 1999021200417 19990212 00417 EU 1999 2 12 QXEA9900155 1 19990113 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION HAS A PIECE MISSING AND A CRACK AT STRINGER 10. REPAIRE D IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200418 19990212 00418 EU 1999 2 12 QXEA9900156 1 19990113 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION IS CRACKED BEYOND STOP DRILL AT STRINGER 14. REPAIRED I AW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200419 19990212 00419 EU 1999 2 12 QXEA9900157 1 19990116 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION IS CRACKED AT STRINGER 13. REPAIRED IAW FOKKER SRM 53-0 2-13 PAGE 5, FIGURE 3 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200420 19990212 00420 EU 1999 2 12 QXEA9900158 1 19990114 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 17565 FORWARD SIDE FRAME CASTELLATION IS CRACKED BEYOND STOP DRILL AT STRINGER 21A. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 3, FIGURE 3 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200421 19990212 00421 EU 1999 2 12 QXEA9900159 1 19990113 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REAR FUSELAGE FRAME 41-2 AFT SIDE FRAME CASTELLATION IS CRACKED BEYOND STOP DRILL AT STRINGER 44. REPAIRED IAW FO KKER SRM 53-02-13, PAGE 6 FIGURE 4 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999021200422 19990212 00422 EU 1999 2 12 QXEA9900160 1 19990116 A 5320 CHANNEL FOKKER F28 F28MK4000 4990810 EU BS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - PANEL 92L UPPER MOUNTING Z CHANNEL HAS 5 CRACKS THROUGHOUT LENGTH OF CHANNEL, STATION 1700 RT BETWEEN FRAMES 9805 AND 11905. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999021200424 19990212 00424 EU 1999 2 12 QXEA9900284 1 19990205 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 2238 11224 PDX- SEVERAL EVACUATION LIGHTS WERE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPERATION CHECK IS GOOD. A IRCRAFT RETURNED TO SERVICE. BATTERY NR 2, (S/N 467), 2256 TOTAL TIME AND 2450 TOTAL CYCLES. 2 L 7 2 4F RT A20EU 1999021200425 19990212 00425 EU 1999 2 12 QXEA9900285 1 19990204 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU ROW 9A DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 5251 11152 PDX- WITH THE EMERGENCY LIGHT SWITCH IN ARMED POSITION, THE PATH LIGHTING FOR ROWS 5, 6, 8 AND 9 WERE ON. REMOVED AND REPLACED BATTERY PACK AND CONTACTS AT ROW 9A. SYSTEM OPERATES NORMAL. 2 L 7 2 4F RT A20EU 1999021200426 19990212 00426 NM 1999 2 12 99FDEA00046 1 19990205 A 3230 TRIM CYLINDER DOUG MD11 MD11F 3023600 NM LT MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 582FE 48420 LT MAIN GEAR DID NOT RETRACT. REMOVED AND REPLACED LT MAIN GEAR BEAM TRIM CYLINDER FOR MX PREVENTION PER MM 32-37-01-4. LEAK CK COND NORMAL. CANNIBALIZED TRIM CYLINDER FROM AC 617. 2 L 7 3 4F RT A22WE 1999021200427 19990212 00427 NM 1999 2 12 99FDEA00047 1 19990205 A 3260 SENSOR BOEING 727 727227 1384078 NM LT MLG BENT A FDEA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SO 25 477FE 21394 LEFT MAIN GEAR INDICATED UNSAFE GROUND OUT RED ON WARN HORN SOUND. REMOVED AND REPLACED MAIN DOWN LOCK SENSOR PER 727 M M 32-61-91. ALSO, JACK AC PER 727 MM 07-11-000-2, OP CK GOOD. 2 L 7 3 4F A3WE 1999021200428 19990212 00428 NE 1999 2 12 99FDEA00048 2 19990205 A 7261 OIL FILTER BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 25 477FE 21394 A +25 ENG OIL QUANTITY DECREASED. FILTER BYPASS LIGHT OUT. REMOVED AND REPLACED NR 3 MAIN OIL STRAINER IAW MM 79-00-00 -3, NEEDS LEAK CK FOR FILTER CHIP DETECTOR AND CONSUMPTION. REMOVED AND REPLACED O-RING BEHIND BOSS FITTING ON LP6 PER MM 70-00. LEAK CK OK. 2 L 7 3 4F 4 F A3WE E2EA 1999021200429 19990212 00429 NM 1999 2 12 99FDEA00049 1 19990205 A 2612 FIRE WARNING BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE ACTIVATED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 209FE 22931 NR 1 ENGINE FIRE WARN INTERMITTENTLY ACTIVATED. OPEN COWLS AND ENG LOWER STUB WING PANEL TO FOM, PERF RESISTANCE CK PER BOEING AC MM 26-11-001-1. INSP ALL DUCTS FOR LEAKS, NONE NOTED. CLEANED ALL CONNECTORS FOR LOOPS, TIGHTENED ALL BLD D UCTS AND ALUMINUM FOIL. 2 L 7 3 4F A3WE 1999021200430 19990212 00430 WP 1999 2 12 99FDEA00050 1 19990205 A 2612 FIRE DETECTOR DOUG DC10 DC1010F 3022111 WP NR 2 ENGINE INOP A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 054FE 47808 LOOP A LT ENG NR 2 ON S/O PANEL ALONG WITH NR 2 FIRE LT MASTER WARN AND FIRE LT ON FWD PNL. *S/D* REMOVED AND REPLACED BOTH NR 2 ENG AND APU FIRE BOTTLE PER MM 26-21-02-2. REMOVED AND REPLACED PYLON A LOOP, BOLTS AND GASKETS ON TCC FLANG E. 2 L 7 3 4F A22WE 1999021200431 19990212 00431 WP 1999 2 12 99FDEA00045 1 19990205 A 3230 RETRACT MECH DOUG DC10 DC1030F 3023504 WP LANDING GEAR MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 301FE 46800 LANDING GEAR WOULD NOT EXTEND, ALL LIGHTS STAYED RED, FRONT AND BACK PANEL. RAN CKLIST OK. *S/D* REMOVED AND REPLACED LANDING GEAR SEL VALVE PER DC10-30 MM 32-31-03-2, RIGGED CABLES BETWEEN LANDING GEAR CONTROL HANDLE AND SEL VALVE PER D CN -30 MM 32-31-01-5. PERF EXTENSION AND RETRACT TEST PER DC10-30 MM 32-31-03-2 NORM. 2 L 7 3 4F RT A22WE 1999021200432 19990212 00432 WP 1999 2 12 ABXA9900069 1 19990204 A 5313 59114277 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND LONGERON 16L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999021200433 19990212 00433 WP 1999 2 12 ABXA9900070 1 19990204 A 5400 49198641 FITTING DOUG DOUG DC9 DC933F 302207A WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND NR 1 ENGINE PYLON INTERIOR FITTING AT STATION 1038 LONGERON 15L CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-0. 2 L 7 2 4F A6WE 1999021200434 19990212 00434 WP 1999 2 12 ABXA9900071 1 19990204 A 5400 99581545 STRAP DOUG DOUG DC9 DC933F 302207A WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND NR 1 RIGHT PYLON SPAR UPPER CAP STRAP CRACKED. REPLACED SPAR CAP STRAP IAW ABX REA D954-26516 AND DWG 5917717. 2 L 7 2 4F A6WE 1999021200435 19990212 00435 WP 1999 2 12 ABXA9900072 1 19990201 A 5400 99581546 STRAP DOUG DOUG DC9 DC933F 302207A WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND NR 2 RIGHT PYLON SPAR UPPER CAP STRAP CRACKED. REPLACED SPAR CAP STRAP IAW ABX REA D954-26516 AND DWG 5917717. 2 L 7 2 4F A6WE 1999021200436 19990212 00436 WP 1999 2 12 ABXA9900073 1 19990201 A 5311 9919619502 FRAME DOUG DOUG DC9 DC933F 302207A WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND RIGHT FUSELAGE MAIN FRAME STATION 737 CRACKED AT OUTBOARD POCKET, UPPER FLANGE. REPAIRED IAW ABX REA D953-26518MR. 2 L 7 2 4F A6WE 1999021200437 19990212 00437 WP 1999 2 12 ABXA9900074 1 19990201 A 5313 59114087 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999021200438 19990212 00438 WP 1999 2 12 ABXA9900075 1 19990201 A 5312 3917624511 BULKHEAD FTG DOUG DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED BETWEEN 1ST AND 2ND RADIALS. REPLACED FITTING IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 1999021200439 19990212 00439 WP 1999 2 12 ABXA9900076 1 19990201 A 5320 99107555 WEB DOUG DOUG DC9 DC933F 302207A WP BS 955 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 955, LEFT SIDE. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999021200440 19990212 00440 WP 1999 2 12 ABXA9900077 1 19990201 A 5320 995773925N SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 14 LEFT AND 15 LEFT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999021200441 19990212 00441 WP 1999 2 12 ABXA9900078 1 19990201 A 5320 99577397N SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 15 RIGHT AND 16 RIGHT. REPLACED SHEAR TIE IAW D C9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999021200442 19990212 00442 WP 1999 2 12 ABXA9900079 1 19990205 A 3231 2714425 SPRING DOUG DOUG DC8 DC863 302198A WP RT MLG DOOR OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 825AX 46115 AFTER GEAR RETRACTION, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR TWICE, UNSAFE LIGHT REMAINED. USED AB NORMAL PROCEDURES TO DETERMINE RIGHT GEAR DOOR UNSAFE AND SECURED DOOR TO NORMAL. ADJUSTED CABLE TENSION AND REPLACED O VERCENTER SPRING. 2 L 7 4 4F 4A25 1999021200443 19990212 00443 WP 1999 2 12 MWEA99060 1 19990205 A 5230 59101577 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND AFT CARGO DOOR LOWER FORWARD DOOR PAN CRACKED. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999021200444 19990212 00444 WP 1999 2 12 MWEA99061 1 19990206 A 5711 9910010506 SPAR DOUG DC9 DC932 3022066 WP WS 109 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FOUND DAMAGED HOLE AT RIGHT WING STATION 109.0 AFT SPAR. MTC INSTALLED TEMPORARY REPAIR STRAP. 2 L 7 2 4F A6WE 1999021200445 19990212 00445 WP 1999 2 12 DLL14990216 1 19990202 A 3350 POWER SUPPLY 5165741 LKHEED 1011 1011385115 5265015 WP L4 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 737D 37559 193C1228 L4 EMERGENCY EXIT SIGNS INOP. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1999021200446 19990212 00446 NM 1999 2 12 DL76L990217 1 19990126 A 2620 212T300820 DISCHARGE LINE BOEING 767 767332 1382001 NM CARGO COMPT OUT OF POSITION A DALA F ACTIVATE FIRE EXT. N FALSE WARNING IN INSP/MAINT 1 SO 27 179DN 25144 THE APU PNEUMATIC DUCT INSULATION WAS REPLACED IN THE LT SIDEWALL OF THE C-2 CARGO COMPARTMENT AT FS 1351 DUE TO DAMAGED FROM CHAFING WITH THE CARGO COMPARTMENT FIRE EXTINGUISHER DISCHARGE LINE. THE FIRE EXTINGUISHER DISCHARGE LINE WAS REL OCATED TO PROVIDE CLEARANCE BETWEEN THE LINE AND DUCT AT THIS LOCATION. THE (P/N R180FS) INSULATION ON THE FIRE EXTINGU ISHER DISCHARGE LINE WAS ALSO REPLACED AT THIS LOCATION. 2 L 7 2 4F RT A1NM 1999021200447 19990212 00447 NM 1999 2 12 DL72W990218 1 19990202 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 FOUND DURING MV1 CORROSION VISIT NRC 126 ON OK TO INSTALL L-4 WINDOW, FOUND .375 INCH CRACK IN FUSELAGE SKIN AT BOTTOM I /B BOLT HOLE. REPAIRED PER SRM 53-30-3 FIG 8. 2 L 7 3 4F A3WE 1999021200448 19990212 00448 NM 1999 2 12 DLM88990220 1 19990203 A 2560 39618991 LANYARD 39618991 DOUG MD88 MD88 3023688 NM L1 DOOR SLIDE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 985DL 53312 FWD ENTRY L1 DOOR LANYARD BROKEN. REPLACED L-1 DOOR SLIDE LANYARD AND LOCK ASSY. 2 L 7 2 4F RT A6WE 1999021200449 19990212 00449 NM 1999 2 12 DL73K990221 1 19990203 A 2170 COALESCER 20405010 BOEING 737 737247 138448D NM CABIN DIRTY A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 237WA 23185 AIR TURNBACK TO RSW DUE TO F/A REPORTED SMOKE IN AFT CABIN AND FLIGHT CREW SENSED BURNING SMELL FROM DUCTING. LANDING W AS UNEVENTFUL. MCO MTC TO DRIVE OVER AND WORK. NO ABNORMAL INDICATIONS FROM ENGINES OR PACKS. CHECKED ALL PANELS FOR EVIDENCE OF SMOKE OR DAMAGE, NONE FOUND. PRESSURIZED AIRCRAFT AND RAN BOTH ENG, ALL FOUND OK. REPLACED BOTH COALESCER BAGS AND CHECKED GASPAR FAN. CHECKS GOOD. 2 L 7 2 4F A16WE 1999021200450 19990212 00450 NM 1999 2 12 DL72S990222 1 19990203 A 3350 S106 BATTERIES BOEING 727 727232 1384082 NM 2L DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 21702 2L EMERG EXIT LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999021200451 19990212 00451 NM 1999 2 12 DL72K990224 1 19990201 A 5312 65163508 BULKHEAD RING BOEING 727 727232 1384082 NM BS 1183 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING INITIAL INSPECTION, A FASTENER AFT OF BS 1183 AT RBL 24 WAS FOUND LOOSE. DURING REMOVAL OF THE FASTENER, TOOLING DAMAGE WAS DONE TO THE TENSION FITTING AND THE SKIN AND ATTACH RING OF THE BS 1183 BLKHD. THE FITTING WAS REPLACED. R EPAIRED PER ERA 332717-14. 2 L 7 3 4F A3WE 1999021200452 19990212 00452 NM 1999 2 12 DL72K990225 1 19990201 A 5330 65545803 SKIN BOEING 727 727232 1384082 NM BS 990 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 EXISTING TRIM OUTS AND ADDITIONAL GROUND DAMAGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. T HE DAMAGED AREAS ARE NEAR S24R. REPAIRED PER ERA 332684-14. 2 L 7 3 4F A3WE 1999021200453 19990212 00453 NM 1999 2 12 DL72K990226 1 19990201 A 5313 655624587 STRINGER BOEING 727 727232 1384082 NM BS 1018 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 S7L WAS GOUGED DURING INSTALLATION OF NEW GALLEY, DAMAGE IS IN INNER RADIUS AT BS 1018. REPAIRED PER ERA 332697-14. 2 L 7 3 4F A3WE 1999021200454 19990212 00454 NM 1999 2 12 DL72K990227 1 19990203 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1096 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 GOUGE/WORN AREA WAS FOUND IN THE FUSELAGE SKIN CAUSED BY THE ENGINE INLET SKATE ANGLE. REPAIRED PER ERA 332760-14AD. 2 L 7 3 4F A3WE 1999021200455 19990212 00455 NM 1999 2 12 DL72K990228 1 19990203 A 5312 6516350 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 CRACK FOUND IN THE LBL 36.83 VERT STIFFENER ON THE FWD SIDE OF BS 1183. CRACK LOCATED AT APPROX WL 238 AND WAS APPROX 2 INCHES LENGTH. REPAIRED PER ERA 332750-14. 2 L 7 3 4F A3WE 1999021200456 19990212 00456 NM 1999 2 12 DL72K990229 1 19990203 A 5312 6516350 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 CRACK FOUND IN VERT STIFFENER AT RBL 36.83 ON THE FWD SIDE OF BS 1183 BLKHD, CRACK IS LOCATED AT APPROX WL 238 AND IS NO LONGER THAN 2. REPAIRED PER ERA 332741-14. 2 L 7 3 4F A3WE 1999021200457 19990212 00457 NM 1999 2 12 DL72S990230 1 19990204 A 5712 65185221314 RIB BOEING 727 727232 1384082 NM BS 760 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 MULTIPLE CRACKS FOUND IN THE WING RIB UPPER CHORD AT BS 760 AT R/LBL 70.85 DURING INSPECTIONS PER SI 4-58560-12AD. ALL CRACKS FOUND WERE TYPICAL OF PER SB727-57-0112, R5. ALSO, TOOLING DAMAGE WAS DONE DURING REPAIR INSTALLATION. REPAIRED PER ERA 332730-14AD. 2 L 7 3 4F A3WE 1999021200458 19990212 00458 NE 1999 2 12 DL72S990231 2 19990204 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SO 27 494DA 53851 21074 700161 NR 1 ENG FAILED IN FLIGHT AT APPROX FL305. AIRCRAFT SHUTTERED FOR ABOUT 10 SEC THEN ENG FLAMED OUT, EGT ROSE TO ABOUT 7 80C, OIL TEMP ROSE TO 140C. RETURNED TO SLC. FOUND METAL IN TAILPIPE. REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999021200459 19990212 00459 NM 1999 2 12 DL733990232 1 19990204 A 3350 BATTERY PACK 20131A BOEING 737 73735B NM PWA JT8 JT8D15A 52051 NE ROW 20 DISCHARGED A DALA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SO 27 225DL 33036 25069 700161 EMER SEAT TRACK LIGHTING INOP AT ROWS 18 TO 24. FOUND BATTERY PACK BAD AT ROW 20. REPLACED SAME. 2 L 7 2 4F 4 F RT A16WE E2EA 1999021200460 19990212 00460 NM 1999 2 12 DL73K990233 1 19990201 A 5330 FS522 SKIN BOEING 737 737232 1384475 NM BS 522 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 THE FUSELAGE SKIN WAS FOUND WITH A 1 INCH LONG CRACK JUST ABOVE STRINGER 16R AT FS 522. THE CRACK WAS ROUTED OUT AND A REPAIR DOUBLER INSTALLED PER B737 SRM 53-30-3, FIG 1. BECAUSE THE REPAIR EXTENDED UNDR A WING-TO-FUSELAGE PANEL THE R EPAIR WAS DOCUMENTED PER ER/A 366606-14 TO ENSURE DTA EVALUATION WILL BE PERFORMED. 2 L 7 2 4F RT A16WE 1999021200461 19990212 00461 NM 1999 2 12 DL72S990234 1 19990203 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 513 & 632 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 541DA 22387 LFEC INSPECTION OF THE LOWER ROW OF FASTENERS IN THE STR 4R LAP SPLICE GAVE TWO CRACK INDICATIONS. INTERNAL HFEC INSPEC TION CONFIRMED ONLY TWO CRACKS, ONE AT FS 513, AND ONE AT FS 632. FASTENERS WERE REMOVED FWD AND AFT OF EACH CRACK AND HFEC SURFACE INSPECTION AGAIN REVEALED NO FURTHER CRACKS. THE CRACKS WERE CUTOUT OF THE LAP AND REPAIRED PER B727 SRM 5 3-30-3, FIG 5 AND DOCUMENTED PER ER/A 366612-14. 2 L 7 3 4F A3WE 1999021200462 19990212 00462 NM 1999 2 12 DLM88990235 1 19990204 A 7430 SWITCH 792055 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE COCKPIT BURNED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 997DL 53364 SMOKE FROM LEFT SIDE OF O/H PANEL WHEN IGNITION TURNED ON FOR TAKEOFF. DISSIPATED WHEN IGNITION WAS TURNED OFF. ABORTE D TAKEOFF AT 15 KTS. FOUND IGNITION SELECTOR COVERED WITH BLACK SOOT. REPLACED IGNITION SELECTOR SWITCH. 2 L 7 2 4F 4 F RT A6WE E9NE 1999021200463 19990212 00463 NM 1999 2 12 DLM88990236 1 19990204 A 3320 LIGHT BV03112N36 DOUG MD88 MD88 3023688 NM ROW 38 FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 918DE 49959 F/A NOTICED ELECTRICAL SMELL IN AFT OF CABIN NEAR LAVS. FOUND OVERHEAD FLUORSCENT LIGHT SHORTED OUT AT ROW 38 ABC. REM OVED WIRES FROM SOCKET AND CAPPED OFF. 2 L 7 2 4F RT A6WE 1999021200464 19990212 00464 NM 1999 2 12 DL72K990237 1 19990122 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1050-1030 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 AT HMV, FOUND SKIN CORRODED THROUGH AND ENTRAPPING WATER BETWEEN STA 1050 TO 1030 STRINGER 29L TO 28L. REMOVED FXD FLO OR RT STA 1030 TO 1060, REMOVED SKIN, REPAIRED PER MM 53-30-0 FIG 809 AND ERA 332746-14. FLOOR PANELS INSTALLED ON NR11 62. 2 L 7 3 4F A3WE 1999021200465 19990212 00465 NM 1999 2 12 DL76L990238 1 19990204 A 3510 MC1025104 MASK BOEING 767 767332 1382001 NM LT COCKPIT DIRTY A DALA K NONE L NO TEST CR CRUISE 1 SO 27 174DN 24802 CAPTS O2 MASK VALVE STICKS. HARD TO EXHALE, NEEDED CLEANING. REPLACED O2 MASK. 2 L 7 2 4F RT A1NM 1999021200466 19990212 00466 NM 1999 2 12 DL733990239 1 19990205 A 5330 SKIN BOEING 737 737347 1384647 NM BS 947 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 FUSELAGE SKIN FOUND DENTED AT BS 947 NEAR S19L. REPAIRED PER ERA 332751-14. 2 L 7 2 4F RT A16WE 1999021200467 19990212 00467 NM 1999 2 12 DL733990240 1 19990205 A 5313 STRINGER BOEING 737 737347 1384647 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 DURING ACCOMPLISHMENT OF EO 5-70166-3 OF S18A AT BS 727, A CRACK WAS FOUND BEYOND EO/SB LIMITS. REPAIRED PER ERA 332733 -14. 2 L 7 2 4F RT A16WE 1999021200468 19990212 00468 NM 1999 2 12 DL733990241 1 19990205 A 5312 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 BS 178 BLKHD WEB FOUND CRACKED IN 8 PLACES, LARGEST CUTOUT IS 5 BY 1. REPAIRED PER ERA 332734-14. 2 L 7 2 4F RT A16WE 1999021200469 19990212 00469 NM 1999 2 12 DL733990242 1 19990205 A 5330 SKIN BOEING 737 737347 1384647 NM C1 DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 AN EXISTING REPAIR WAS REMOVED AT THE C1 DOOR CUTOUT, ADDITIONAL DAMAGE FOUND. CUTOUTS ARE IN SKIN (1.25 X 3.5) AND BEA R STRAP (1.25 BY 1.5). REPAIRED PER ERA 332728-14. 2 L 7 2 4F RT A16WE 1999021200470 19990212 00470 NM 1999 2 12 DL72S990243 1 19990205 A 5330 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 DURING INSP PER SI 4-74176-12 ON S4R, LAP JOINT CRACK INDICATIONS WERE NOTED FROM BS 481 TO BS 681 APPROX 19 CRACK INDIC ATIONS WERE NOTED BY HFEC INSP. LAP JOINT CUT OUT AND REPAIRED PER ERA 332726-14. 2 L 7 3 4F A3WE 1999021200471 19990212 00471 NM 1999 2 12 DL733990244 1 19990205 A 5330 6545772188 SKIN BOEING 737 737347 1384647 NM BS 860-875 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 INSPECTION OF THE VERT STAB FOUND THE FUSE SKIN AT THE BLADE SEAL INTERFACE WORN FROM BS 860 TO BS 887. GREATEST DEPTH OF WEAR WAS 0.013. REPAIRED PER ERA 332744-14. 2 L 7 2 4F RT A16WE 1999021200472 19990212 00472 NM 1999 2 12 DL72K990245 1 19990205 A 5711 651620261 SPAR BOEING 727 727232 1384082 NM CENTER WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FOUR FASTENER HOLES WERE MISDRILLED DURING ACCOMPLISHMENT OF EO 4-72440-3AD. HOLES WERE OVERSIZED TO 0.312 DIA. REPAIR ED PER ERA 332757-14AD. 2 L 7 3 4F A3WE 1999021200473 19990212 00473 NM 1999 2 12 DL72W990246 1 19990204 A 5320 655612910 SILL BOEING 727 727247 138408F NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 THE OUTER CHORD OF THE C-2 DOOR SURROUND LOWER SILL WAS FOUND WITH CORROSION ON THE OUTER FLANGE BETWEEN THE DOOR FRAME JAMBS. THE CORRODED AREAS WERE TRIMMED OUT AND TWO STEEL REPAIR ANGLES WERE INSTALLED TO REPAIR THE CUTOUTS. THE REP AIR WAS ACCOMPLISHED PER ER/A 366609-14, REV B. 2 L 7 3 4F A3WE 1999021200474 19990212 00474 NM 1999 2 12 DL733990247 1 19990204 A 5330 6545800219 SKIN BOEING 737 737347 1384647 NM LT COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 THE FUSELAGE SKIN AND UNDERLYING STEEL GUSSET WERE FOUND WITH A .20 INCH CRACK AT THE UPPER AFT CORNER OF THE L1 COCKPIT WINDOW CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A STEEL DOUBLER AND ALUMINUM TRIPLER. THE REPAIR WAS ACCOMP LISHED PER ER/A 366614-14, REV C. 2 L 7 2 4F RT A16WE 1999021200475 19990212 00475 NE 1999 2 12 DL72S990248 2 19990205 A 7260 GEARBOX JT8D15HHK BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 543DA 687498 22392 687498 ON APPROACH INTO CVG PASSING THROUGH APPROX 9000 AGL, NR 2 LOW OIL PRESS LIGHT ILLUMINATED. OIL QTY WAS AND NOW OBSERVE D TO DECREASE, OIL TEMP NORMAL, INCREASED ABOVE 105 DEG C. ENGINE SHUT DOWN PER POM PROCEDURES. FOUND NR 2 ENG GEARBOX LEAKING AT 6 O'CLOCK POSITION. CHANGED NR 2 ENG GEARBOX. 2 L 7 3 4F 4 F A3WE E2EA 1999021200476 19990212 00476 NM 1999 2 12 DL73E990249 1 19990205 A 3350 0201720001 LIGHT BOEING 737 7372J8 1384489 NM ROW 12D INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 235WA 22859 EMERGENCY LIGHT ASSY SEAT 12D INOP. REPLACED LIGHT ASSY, TEST GOOD PER MM. 2 L 7 2 4F RT A16WE 1999021200477 19990212 00477 WP 1999 2 12 DLL10990250 1 19990206 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 1734D 37062 193C1225 EMERGENCY EXIT LIGHT FLOOR TRACK INOP FWD CABIN. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1999021200478 19990212 00478 1999 2 12 DL733990251 4 19990206 A 3441 IRU HG1050AD05 BOEING 737 7373B7 1384580 NM NR 1 INOP A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 952WP 5338 23378 NR 1 COMPASS FAILED. CYCLED CB, NO CHANGE. REPLACED NR 1 IRU. 2 L 7 2 4F RT A16WE 1999021200479 19990212 00479 NM 1999 2 12 DL72K990252 1 19990206 A 2780 H1010271 SWITCH BOEING 727 727232 1384082 NM NR 5 LE SLAT BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 479DA 20756 AFTER FLAP RETRACTION FROM 5 DEGREES TO 2 AMBER FLAP ANNUNCIATOR ILLUMINATED ON FWD PANEL. IN POSITION TEST, THE NR 5 S LAT INDICATED EXTEND. RAN V-LIST PER POM NR 5 SLAT WOULD NOT RETRACT. TROUBLESHOT SYSTEM, FOUND SWITCH S12 ROCKER ARM MISSING. REPLACED SWITCH DAL (P/N 274203783). SYSTEM CHKS NORMAL. 2 L 7 3 4F A3WE 1999021200480 19990212 00480 WP 1999 2 12 TWAA9902201 1 19990203 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND SURFACE CORROSION ON FLOORBEAM AT STA 218 TO 237, BL 0. MECHANICALLY REMOVED CORROSION PER TWA STD PROCESS MANUAL. REPAIRED MEMBER PER SRM 53-01, PAGE 10. 2 L 7 2 4F A6WE 1999021200481 19990212 00481 WP 1999 2 12 TWAA9902202 1 19990206 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND CRACK IN AFT SIDE OF FORMER RING, STA 1087, LBL 10 IN. INSTALLED NEW FORMER RING FOOT P ER STD PROCESS MANUAL 6-70-01. 2 L 7 2 4F A6WE 1999021200482 19990212 00482 WP 1999 2 12 TWAA9902203 1 19990207 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 1059 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND AFT ACCESSORY COMPT FORMER FOOT CRACKED AT STA 1059, LONGERON 15L. REPLACED FORMER FOOT PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999021200483 19990212 00483 WP 1999 2 12 TWAA9902204 1 19990207 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 214 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CHAIR TRACK AT STA 214, RBL 44 WITH CORROSION AND DEEP PITTING. INSTALLED NEW TRACK SEC TION FROM STA 200 TO 265, INSTALLED (P/N C03580-4) PER DOUGLAS PRINT 5910820. 2 L 7 2 4F A6WE 1999021200484 19990212 00484 WP 1999 2 12 TWAA9902205 1 19990205 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, LBL 44. REMOVED CORROSION PER SPM 6-80-01 . REPLACED SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999021200485 19990212 00485 WP 1999 2 12 TWAA9902206 1 19990205 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 197 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 197, LBL 45 TO 50. REPLACED SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999021200486 19990212 00486 WP 1999 2 12 TWAA9902207 1 19990205 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 170-215 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT, 0 IN BL, FROM STA 170 TO 215. REPLACED SUPPORT PER SP M 6-70-01. 2 L 7 2 4F A6WE 1999021200487 19990212 00487 WP 1999 2 12 TWAA9902208 1 19990204 A 5311 FORMER DOUG DC9 DC932 3022066 WP BS 1087 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CRACK IN AFT FUSELAGE INTERIOR FORMER RING FOOT AT STA 1087, LONGERON 1L. REMOVED AND R EPLACED FORMER FOOT CLIP AT STA 1087, LONGERON 1L PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999021200488 19990212 00488 WP 1999 2 12 TWAA9902209 1 19990206 A 5320 MEMBRANE DOUG DC9 DC932 3022066 WP BS 218 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CRACK IN MEMBRANE BELOW CABIN FLOOR AT STA 218, RBL 46 IN. REPAIRED WEB MEMBRANE PER SR M 51-01, FIG 2. 2 L 7 2 4F A6WE 1999021200489 19990212 00489 NM 1999 2 12 HNAA9900023 1 19990205 A 3350 6104799 BATTERY DHAV DHC8 DHC8201 2809001 NM ROW 4 DISCHARGED A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 995HA 460 EMERGENCY LIGHTS AFT OF ROW 4, 1ST AND 3RD CEILING EMERGENCY LIGHTS AND AFT LEFT AND RIGHT EGRESS LIGHTS WILL NOT EXTING UISH. REPLACED 3351-PS3 BATTERY AND BASE. 2 H 7 2 4T RT A13NM 1999021200490 19990212 00490 NM 1999 2 12 HNAA9900024 1 19990205 A 2611 CONNECTOR DHAV DHC8 DHC8102 2809003 NM BAGGAGE COMPT DIRTY A HNAA K NONE N FALSE WARNING LD LANDING 1 EA 07 964HA 343 SMOKE WARNING LIGHT ILLUMINATED FOR 3-4 SECONDS ON SHORT FINAL, AFTER LANDING AND DURING ROLLOUT FOR 3-4 SECONDS. POST FLIGHT INSPECTION FOUND NO SMOKE OR FUMES IN BAG BAY. CLEANED CANNON PLUGS ON BOTH SMOKE DETECTORS IN BAG BAY. TESTED OPERATIONAL CHECK OK. COULD NOT DUPLICATE. 2 H 7 2 4T RT A13NM 1999021200491 19990212 00491 WP 1999 2 12 AT9900084 1 19990105 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERTICAL STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT VERTICAL STABILIZER LOWER AND UPPER SKIN CHAFED, CORRODED AND HOL ES MISDRILLED IN PREVIOUS REPAIRED. MECHANICALLY REMOVED CORROSION, FABRICATED DOUBLERS, HEAT TREATED PARTS AND INSTALL ED ALL PARTS IAW DC9 SRM 51-01, 55-30-0, 51-10-3, 55-30-5, 55-01 FIG 4, 51-10-4, 51-70-2, 55-03 FIG 9, 55-02 FIG 16, RES NR 9944 AND NR 9924. 2 L 7 2 4F A6WE 1999021200492 19990212 00492 WP 1999 2 12 AT9900085 1 19990105 A 2760 TORSION BAR DOUG DC9 DC932 3022066 WP WS 50 & 68 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SPOILER SUPPORT ROD END AND TORSION BAR LEVER CORRODED AT STA 50 AND S TA 68. REMOVED AND REPLACED THE END SUPPORT ROD END AND TORSION BAR AND OPERATIONAL ADJUSTMENT TEST ACCOMPLISHED IAW DC 9 MM 27-61-2, 20-10-3, AND TERMINATED AD 97-02-08 PER EO 9-2760-29-E1415 1R. OFF (P/N 5954283-501) (P/N 3920944-503) (P /N 3923250-503) (P/N AN951REB3N) (P/N M83248-1). 2 L 7 2 4F A6WE 1999021200493 19990212 00493 WP 1999 2 12 AT9900086 1 19990105 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 218-446 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD CARGO CENTER FLOOR BOARD AT STA 218 THRU 446 CORRODED AROUND EDGES , TOP SIDE AND BETWEEN LAYERS. REMOVED AND REPLACED CORRODED FLOOR PANEL, FABRICATED NEW FLOOR PANELS, TREATED, PRIMED, DEBURRED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, AND 53-20-0. 2 L 7 2 4F A6WE 1999021200494 19990212 00494 WP 1999 2 12 AT9900087 1 19990104 A 5311 27779305 FRAME DOUG DC9 DC932 3022066 WP BS 180 & 27 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED AT STA 180 L-29L TO L-29R AND STA 275 L29-L TO L-29R. MECHANICALLY REMOVED CORROSION, FABRICATED AND INSTALLED NEW REPAIR IAW DC9 SRM 51-10-3, 53-01 FIG 1 AND 53-04 FIG 2A PAGE 4. 2 L 7 2 4F A6WE 1999021200495 19990212 00495 WP 1999 2 12 AT9900088 1 19990106 A 5720 ANGLE DOUG DC9 DC932 3022066 WP WS 137 &149 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT WING INBOARD FLAP ATTACHED ANGLE AND SPAR CAP AT STA 137.50 AND REAR SPAR ATTACHED ANGLE AT STA 149 CORRODED. REMOVED NECESSARY FASTENERS IN ORDER TO GAIN ACCESS, CLEANED CORROSION, FABRIC ATED RIB, DOUBLER, ANGLE, HEAT TREATED AND INSTALLED IAW DC9 SRM 51-10-2, 57-02-0, 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 1999021200496 19990212 00496 WP 1999 2 12 AT9900089 1 19990105 A 5230 49136441 HINGE DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO DOOR FORWARD AND AFT HINGE ASSEMBLY ATTACH BOLT HOLES WI TH CORROSION AND ELONGATED HOLES. REAMED ELONGATED HOLES AND CLEANED CORROSION, FABRICATED AND INSTALLED FREEZE PLUGS. REINSTALLED HINGE BRACKETS AND REDRILLED HINGE SPRING BOLT HOLES IAW DC9 SRM 51-30-4, 51-30-2 AND 52-31-0. 2 L 7 2 4F A6WE 1999021200497 19990212 00497 WP 1999 2 12 AT9900090 1 19990103 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 437 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTED FUSELAGE SKIN AT STA 437, 2 BELOW L-24R. CUT OUT DENTED SECTIONS, FABRICATED NEW SKIN SECTION AND REPAIR SPLICES IAW DC9 SRM 53-04 FIG 30, 51-10-2, 51-10-3, 51-10-4 AND RES NR 9920. (P/ N 105846-1) ON, (P/N 59204195) OFF. 2 L 7 2 4F A6WE 1999021200498 19990212 00498 WP 1999 2 12 AT9900091 1 19990107 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 968 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTED AREA AT STA 968 L-26R CREASED AND OUT OF LIMITS. CUT OUT DENTED AR EA, FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, SKIN SPLICES, STRINGER SPLICES, SHEAR TIES IAW DC9 SRM 53-0 4 FIG 16 AND RES NR 9940, 9922 AND 99284. 2 L 7 2 4F A6WE 1999021200499 19990212 00499 WP 1999 2 12 AT9900092 1 19990106 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 360 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND PREVIOUSLY EXISTING REPAIR DOUBLER AT STA 360 BETWEEN L-24 - 26R BULGING O UT OF LIMITS. CUT OUT DAMAGE SKIN, FABRICATED NEW SKIN, SHEAR TIE, LONGERON FINGER DOUBLER, SPLICE DOUBLERS, DRILLED, D EBURRED, PRIMED AND INSTALLED IAW DC9 SRM 53-04 FIG 30, 51-30-2, 51-10-3 AND RES NR 99134, 99179 AND 99285. 2 L 7 2 4F A6WE 1999021200500 19990212 00500 WP 1999 2 12 AT9900093 1 19990208 A 3350 LIGHT DOUG DC9 DC932 3022066 WP ROW 1 OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 EMERGENCY FLOOR LIGHTING WILL NOT STAY ON. REPLACED FLOOR COVER AND WIRING SPLICES AT ROW NR 1. OPERATIONAL TEST NORMA L IAW MM 33-50. 2 L 7 2 4F A6WE 1999021200502 19990212 00502 EU 1999 2 12 MALA976337 1 19990205 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 450XJ 450 DURING CLIMB, RIGHT HAND GEAR LIGHT ILLUMINATED INDICATING GEAR STILL DOWN. VISUALLY CHECKED, GEAR UP. QRH UNABLE TO E XTINGUISH LIGHT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED CONNECTOR, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021200503 19990212 00503 EU 1999 2 12 MALA976338 1 19990205 A 3244 50104882 TIRE SAAB SF340 340B 7860101 EU LT MLG FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 406XJ 406 ON CLIMBOUT, BLEW LHIB TIRE. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED LHIB TIRE, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021200504 19990212 00504 EU 1999 2 12 MALA976339 1 19990205 A 3350 86S0059975 BULB SAAB SF340 340B 7860101 EU ROW 5A-9A-9D FAILED A MALA K NONE L NO TEST CL CLIMB 1 GL 15 9CJ 224 EMERGENCY LIGHTS AT ROWS 5A, 9A AND 9D OUT. MAINTENANCE RELAMPED BULBS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021200505 19990212 00505 EU 1999 2 12 AWXA9900041 1 19990130 A 4990 OIL SYST AIRBUS 320 A320231 3930325 EU APU LEAKING A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 618AW 304 ACFT HAS A STENCH THAT CAUSED THE CREW TO BE NAUSEOUS AND DEVELOP HEADACHES. MX OBSERVED APU LEAKING 5-6 DROPS FROM COM PT INTO INLET. PLACED APU ON MEL 49-10-01, MEL MX PROCEDURES COMPLIED WITH. BOTH PACKS WERE OPERATED IN FULL HOT AND F ULL COLD FOR APPROX 5 MINS AT A TIME. SMELL DISSIPATED CONSIDERABLY WHILE RUNNING. THE ENG'S WERE INGESTING OWN BREATH ER EXHAUST AND A FAINT RESIDUAL ODOR WAS THERE. ODOR CLEARED WHILE ON GROUND, AIR CONDITIONING SOURCE. CHECKED THIS AP U OUT MANY TIMES AND NO REAL LEAK HAVE BEEN FOUND. THIS MUST BE AN INTERNAL APU PROBLEM AND WILL REMOVE AND REPLACED ON NEXT RON. APU REPLACED 07 FEB 99, PER TASK CARD R6D49301. OPS CHECKED GOOD, MEL REMOVED. 2 L 7 2 4F RT A28NM 1999021200506 19990212 00506 NM 1999 2 12 AWXA9900042 1 19990207 A 2150 PACK BOEING 737 7372A6 138448B NM RIGHT MALFUNCTIONED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 145AW 20194 AIR TURNBACK, SMOKE IN CABIN. CABIN SMELLED OF SMOKE AFTER DEPARTURE. SUSPECT SMELL CAME FROM RT PACK. AIR RETURNED T O ICT. MAINTENANCE INSPECTED RT PACK TURBINE OIL QTY AND WATER SEPARATOR, CHECKED NORMAL. DEACTIVATED RT PACK IAW MEL 21-01. DEFERRED PLACARD 21-01 ISSUED PER MAINT CONTROL. MX REACTIVATED RT PACK, RAN PACK OFF ENGINE BLEED AND NO SMELL OR SMOKE NOTED AT THIS TIME. COULD NOT DUPLICATE, OPS NORMAL. 2 L 7 2 4F A16WE 1999021200507 19990212 00507 NM 1999 2 12 CALA9900115 1 19990207 A 3610 DUCT BOEING 727 727243 138408D NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE BROKEN A CALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SW 09 17407 21270 649071 A FIRE WARNING INDICATION ON THE NR 3 ENGINE WAS RECEIVED AFTER TAKEOFF FROM BWI. CHECKLIST PROCEDURES WERE FOLLOWED, F UEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 3 ENGINE BLEED AIR DUCT FROM 6TH STAGE SADDLE TO NOSE COWL ANTI-ICE VALVE WAS FOUND BROKEN. THE BLEED AIR DUCT WAS REMOVED AND REPLACED. THE SURROUNDING AREA WAS CHECKED FOR DISCREPANCIES AND NONE WERE FOUND. 2 L 7 3 4F 4 F RT A3WE E2EA 1999021200508 19990212 00508 WP 1999 2 12 CALA9900116 1 19990205 A 5755 BRACE DOUG DC9 DC982 3022082 WP LT SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND A CRACK OF UNSPECIFIED LENGTH IN THE LT GROUND SPOILER ACTUATOR I/B ATTACH BRACKET CROSS BRACE. A NEW CROSS BRACE WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999021200509 19990212 00509 WP 1999 2 12 CALA9900117 1 19990205 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 218 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 218, LONGERON 17L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02766. 2 L 7 2 4F A6WE 1999021200510 19990212 00510 NM 1999 2 12 CALA9900118 1 19990207 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 456 CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19357 23841 INSPECTION FOUND THE RT FORWARD LOWER FUSELAGE SKIN CREASED AT STA 456, STRINGERS 29R-27R. THE SKIN WAS REPAIRED IAW EC RA 5330-02767. 2 L 7 2 4F RT A16WE 1999021200511 19990212 00511 NM 1999 2 12 UPS99228573 1 19990131 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-N/A, FLAP TRACK NR 8 CRACKED AT TIP. ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOMPL. ISSUED DMI NR 1670 87. FLAP TRACK REPLACED AND DMI NR 167087 WAS CLEARED. 2 L 7 3 4F A3WE 1999021200512 19990212 00512 NM 1999 2 12 UPS99228654 1 19990125 A 5512 SKIN BOEING 727 72730C 1384009 NM RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CORROSION ON UPPER SKIN OF RT HORIZONTAL STABILIZER STAB STA 68. REMOVED CORROSION IAW SRM 51-10-6. REPAIRED AREA IAW SMRO EO 99-03-008 UPS ENGINEERING FILE NR 727-55-0383. 2 L 7 3 4F A3WE 1999021200513 19990212 00513 NM 1999 2 12 UPS99228655 1 19990123 A 5311 FRAME BOEING 727 72730C 1384009 NM BS 848.95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CRACK AT FRAME STA 848.95 LT EMINATING FROM 4TH FASTENER HOLE ABOVE FLOOR. REPAIR CARRIED OUT TO FRA ME AT STA 848.95 LT IAW SMRO EO 99-03-010 AND UPS EO B727-5310-5474 UPS ENGINEERING FILE NR 5310-2095. 2 L 7 3 4F A3WE 1999021200514 19990212 00514 NM 1999 2 12 UPS99428644 1 19990205 A 3240 BRAKES BOEING 747 747212B 1384886 NM LANDING GEAR OUT OF ADJUST A IPXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 521UP 21944 INSPECTION TYPE-N/A, ALL BRAKE SYSTEM CABLES HAVE SLACK, NO BRAKE ACTION AFTER A/C ARRIVED ANC. HYD BRAKE SYSTEM ADJ AN D TEST C/W MM REF 32-41-00 PG 501. 2 L 7 4 4F A20WE 1999021200515 19990212 00515 NM 1999 2 12 UPS99428645 1 19990204 A 3240 BRAKES BOEING 747 747212B 1384886 NM LANDING GEAR OUT OF ADJUST A IPXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 520UP 21943 INSPECTION TYPE-N/A, MAIN A/C BRAKES VERY WEAK FROM BOTH CAPTS AND F/O'S POSITION. NORMAL BRAKE SOURCE SELECT SW, NO HE LP. BRAKE PEDALS, CAPT AND F/O BOTTOM OUT WHEN TRYING TO STOP. ALL HYD SYS PRESSURES NORMAL. INSPECTED MAIN BRAKE SYS , FOUND CABLES TENSION ON LOW, ADJ CABLE SYS PER 32-41-00 PG 501, BRAKES OPS CHKS OK. 2 L 7 4 4F A20WE 1999021200516 19990212 00516 WP 1999 2 12 UPS99828646 1 19990104 A 5330 57552713N1 SKIN DOUG DC8 DC871F 302199D WP BS 400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FUSELAGE SKIN HAS HEAVY CORROSION AT FS 400, LONG 36 TO 35L. REMOVED AND REPLACED SKIN PANEL FS 190 TO 450 LONG 31L-31R IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999021200517 19990212 00517 WP 1999 2 12 UPS99828647 1 19990129 A 5320 37558251 FITTING DOUG DC8 DC871F 302199D WP BS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, BATH TUB FITTING CORRODED OUT OF LIMITS BETWEEN LONG 33R AND 34R AT FS 340. REMOVED AND REPLACED FI TTING IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999021200518 19990212 00518 WP 1999 2 12 UPS99828648 1 19990129 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, THE INTERNAL DOUBLER AT 620, LONG 35R TO 36, HAS HEAVY CORROSION. REPAIRED DOUBLER IAW DH SK713-629 . 2 L 7 4 4F RT 4A25 1999021200519 19990212 00519 WP 1999 2 12 UPS99828649 1 19990202 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 220 LONG 30L TO 31L THE SHEAR TIE IS CRACKED. REPAIRED SHEAR TIE IAW SRM 53-2-0 FIG 2B. 2 L 7 4 4F RT 4A25 1999021200520 19990212 00520 WP 1999 2 12 UPS99828650 1 19990201 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 34L AT FS 1260 TO 1280 IS CRACKED. REPAIRED LONG 34L IAW DH SK713-862. 2 L 7 4 4F RT 4A25 1999021200521 19990212 00521 WP 1999 2 12 UPS99828651 1 19990201 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 35L AT FS 1260 TO 1280 IS CRACKED. REPAIRED LONG 35L IAW DH SK713-863. 2 L 7 4 4F RT 4A25 1999021200522 19990212 00522 1999 2 12 ABXA9900081 4 19990202 A 2211 2588789904 COMPUTER DOUG DC8 DC863 302198A WP E & E COMP DEFECTIVE A ABXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 816AX 46093 DURING CRUISE EXPERIENCED NOSE DOWN HYDRAULIC PITCH TRIM RUN-AWAY. DISCONNECTED WHEEL LONGITUDINAL TRIM CIRCUIT BREAKER S, NO PROBLEMS REMAINDER OF FLIGHT. REPLACED R-56 AND S-56 CIRCUIT BREAKERS. REPLACED PITCH AXIS COMPUTER AND INSPECTE D STABILIZER SHUT-OFF VALVE, CONTROL VALVE AND MOTOR AND NO DEFECTS NOTED. OPS CHECKED NORMAL IAW DC8 MM. SUBSEQUENT A UTOPILOT INFLIGHT EVALUATION WAS SATISFACTORY. 2 L 7 4 4F 4A25 1999021200523 19990212 00523 WP 1999 2 12 ABXA9900082 1 19990127 A 5320 37558442 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 BATH TUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DWG 3755844, ABX REA D853-219271MR AN D DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999021200524 19990212 00524 WP 1999 2 12 ABXA9900083 1 19990127 A 5320 3755842 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1260 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D85324928MR AND D C8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999021200525 19990212 00525 WP 1999 2 12 ABXA9900084 1 19990126 A 5320 9755584507 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1080 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT CUSP LOWER FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999021200526 19990212 00526 NM 1999 2 12 SCNA99031 1 19990205 A 2611 SMOKE DETECTOR BOEING 727 7272J4 1384006 NM RT LAVATORY INOP A SCNA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE AFT RIGHT LAVATORY SMOKE DETECTOR ALARM WAS FOUND TO OPERATE CONTINUOUSLY. REMOVED AND REPLACED THE RIGHT AFT LAVATORY SMOKE DETECTOR, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999021200527 19990212 00527 NM 1999 2 12 SCNA99032 1 19990203 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 420 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING A SCHEDULED MAINTENANCE CHECK, EVIDENCE OF CORROSION WAS FOUND AT THE RIGHT MOST OUTBOARD SEAT TRACK AT APPROXIMA TELY BS 420. REMOVED OUT OF LIMITS CORRODED SEAT TRACK AND INSTALLED A NEW SECTION OF SEAT TRACK IAW B727 SRM 53105. 2 L 7 3 4F RT A3WE 1999021200528 19990212 00528 WP 1999 2 12 SCNA99033 1 19990118 A 3230 CONTROL CABLE DOUG DC10 DC1015 3022118 WP RT MLG WW OUT OF ADJ A SCNA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 15 153SY 48276 DURING APPROACH, GEAR WOULD NOT EXTEND NORMALLY, GEAR HANDLE WOULD NOT MOVE FURTHER THAN HALF TRAVEL. LANDING GEAR EXTE NDED USING ALTERNATE SYSTEM. LANDED AIRCRAFT UNEVENTFULLY. FOUND EXTEND CABLE ABOVE RIGHT WHEEL WELL CEILING BULKHEAD OFF OF PULLEY. REINSTALLED CABLE AND PERFORMED TENSION CHECK PER MM 323101. ALSO, REPLACED TURNBUCKLE W AND TENSIONED CABLE 109. PERFORMED GEAR RETRACT/EXTEND TEST PER MM 323000 WITH NO TROUBLE FOUND. 2 L 7 3 4F A22WE 1999021200529 19990212 00529 1999 2 12 DHL99721003 4 19990205 A 2216 30363803 SERVO BOEING 727 727228 NM STAB TRIM MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 721DH 19545 AUTO-PILOT AND STAB CRUISE TRIM WILL NOT TRIM NOSE UP. REMOVED AND REPLACED AUTO PILOT STAB TRIM SERVO PER MM 22-11 -211, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999021200530 19990212 00530 NM 1999 2 12 TSAA9933014 1 19990107 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 4 BATTERY PACK DUE LIGHT DID NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999021200531 19990212 00531 NM 1999 2 12 TSAA9933016 1 19990110 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 1 POSITION FLOOR PROXIMITY LIGHT ASSY BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999021200532 19990212 00532 NM 1999 2 12 TSAA9933006 1 19990103 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 2 AND NR 5 SEAT EMERGENCY LIGHT ASSY BATTERY PACKS DUE TO NO 'ALL'S WELL LIGHT'. OPS CHECK OK. AIRCRAFT RE TURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999021200534 19990212 00534 EU 1999 2 12 RAIA990108 1 19990104 A 3241 14014920 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU NR 2 MLG FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 573HK 41092 DCA - FLT 7744 - ANTI-SKID FAIL LIGHT ILLUMINATED. MAINTENANCE REPLACED NR 2 MAIN WHEEL HUBCAP TRANSDUCER. (X) 2 L 7 2 4T RT A41NM 1999021200535 19990212 00535 1999 2 12 RAIA990107 4 19990110 A 3414 39948B2236 INDICATOR BAG JETSTM JETSTM3201 1500217 EU LT AIRSPEED FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 343TE 955 CMI - FLT 7448 - CAPTAIN'S AIRSPEED INDICATOR INOPERABLE. MAINTENANCE REPLACED CAPTAIN'S AIRSPEED INDICATOR. (X) 2 L 7 2 4T RT A56EU 1999021200536 19990212 00536 1999 2 12 RAIA990105 4 19990108 A 3418 1850068 SIGNAL PROCESSOR JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 564HK 41081 STL - FLT 7534 - RIGHT STALL LIGHTS ON COAMING PANEL WILL NOT TEST. MAINTENANCE REPLACED SIGNAL PROCESSOR. (X) 2 L 7 2 4T RT A41NM 1999021200537 19990212 00537 EU 1999 2 12 RAIA990104 1 19990106 A 3240 251130 CONTROL CABLE JETAIR JETSTM JETSTM4101 1500501 EU BRAKE SYSTEM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 559HK 41075 STL - FLT 7326 - PARKING BRAKE WILL NOT LOCK. MAINTENANCE REPLACED PARKING BRAKE CABLE. (X) 2 L 7 2 4T RT A41NM 1999021200538 19990212 00538 EU 1999 2 12 RAIA990103 1 19990103 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 433AM 885 STL - FLT 7024 - LEFT ENGINE FIRE LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT ENGINE FIRE LOOP. (X) 2 L 7 2 4T RT A56EU 1999021200540 19990212 00540 EU 1999 2 12 RAIA990115 1 19990115 A 2422 552019A INVERTER AEROSP ATR42 ATR42300 8680920 EU NR 1 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 423TE 119 STL - FLT 7406 - NR 1 INVERTER FAULTED. MAINTENANCE REPLACED NR 1 INVERTER. (X) 2 H 7 2 4T RT A53EU 1999021200541 19990212 00541 EU 1999 2 12 RAIA990116 1 19990115 A 7722 8924696 LEAD BAG JETSTM JETSTM3201 1500217 EU RT EGT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 427AM 876 SPI - FLT 7097 - RIGHT ENGINE EGT FLUCTUATING 300 DEGREES. MAINTENANCE REPLACED RT ENGINE EGT SHORT LEAD. (X) 2 L 7 2 4T RT A56EU 1999021200542 19990212 00542 EU 1999 2 12 RAIA990114 1 19990113 A 3260 900SEN36 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 435AM 889 EVV - FLT 7409 - NOSE LANDING GEAR INTRANSIT LIGHT ON WITH GEAR DOWN ALONG WITH 3 GREEN DOWN AND LOCKED INDICATED. MAIN TENANCE REPLACED NOSE DOWNLOCK SWITCH. (X) 2 L 7 2 4T RT A56EU 1999021200543 19990212 00543 EU 1999 2 12 RAIA990119 1 19990114 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 423AM 858 BMI - FLT 7321 - THREE GREEN DOWN AND LOCKED LIGHTS WITH LT GEAR INTRANSIT LIGHT ON ALSO. MAINTENANCE REPLACED LT MAIN GEAR DOWNLOCK SWITCH. (X) 2 L 7 2 4T RT A56EU 1999021200544 19990212 00544 EU 1999 2 12 RAIA990118 1 19990117 A 3243 ACM26810 MASTER CYLINDER BAG JETSTM JETSTM3201 1500217 EU LT SYSTEM REQUIRED SERVICE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 425AM 870 STL - FLT 7366 - CAPTAIN'S RIGHT BRAKE INOPERABLE. MAINTENANCE SERVICED CAPTAIN'S RIGHT MASTER CYLINDER. (X) 2 L 7 2 4T RT A56EU 1999021200545 19990212 00545 EU 1999 2 12 RAIA990113 1 19990115 A 5330 SKIN JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 559HK 41075 STL - AFT EQUIPMENT BAY ON LT SIDE OF AIRCRAFT WAS STRUCK BY A BAG CART ON RAMP. MAINTENANCE REPAIRED AIRCRAFT IAW E.O. NR J4100-53-001-1. ACFT TT: 7,734. (X) 2 L 7 2 4T RT A41NM 1999021200546 19990212 00546 EU 1999 2 12 RAIA990126 1 19990119 A 3260 622800200 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 864AE 864 FAT - FLT 4726 - LEFT MAIN INTRANSIT LIGHT TAKES APPROXIMATELY 45 SECONDS TO EXTINGUISH ON RETRACTION. MAINTENANCE REPA IRED BROKEN WIRE ON UPLOCK SWITCH. (X) 2 L 7 2 4T RT A56EU 1999021200547 19990212 00547 1999 2 12 RAIA990132 4 19990124 A 2312 7510700807 R/T UNIT JETAIR JETSTM JETSTM4101 1500501 EU NR 1 COMM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 553HK 41066 PHL - FLT 7760 - NR 1 RADIO WILL NOT TRANSMIT. MAINTENANCE REPLACED NR 1 COMM R/T. (X) 2 L 7 2 4T RT A41NM 1999021200548 19990212 00548 1999 2 12 RAIA990131 4 19990124 A 3418 C850176 STALL VANE JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 573HK 41092 JFK - FLT 7733 - LEFT STALL AMBER CAP ILLUMINATED. MAINTENANCE REPLACED LEFT STALL VANE. (X) 2 L 7 2 4T RT A41NM 1999021200549 19990212 00549 EU 1999 2 12 RAIA990129 1 19990122 A 3060 C40631 BRUSH BLOCK JETAIR JETSTM JETSTM4101 1500501 EU RT PROPELLER FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 570HK 41089 JFK - FLT 7635 - PROPELLER FAILED IN BOTH CYCLES. MAINTENANCE REPLACED RIGHT PROPELLER BRUSH BLOCK. (X) 2 L 7 2 4T RT A41NM 1999021200550 19990212 00550 EU 1999 2 12 RAIA990127 1 19990122 A 2120 S2L226 DUCT JETAIR JETSTM JETSTM4101 1500501 EU LEFT LEAKING A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 551HK 41040 STL - FLT 7412 - LEFT DUCT FAIL LIGHT ILLUMINATED. MAINTENANCE REPLACED SEALS IN LEFT DUCT ASSY. (X) 2 L 7 2 4T RT A41NM 1999021200551 19990212 00551 EU 1999 2 12 RAIA990134 1 19990125 A 6120 31058993A SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 550HK 41039 JFK - FLT 7654 - APR SYSTEM FIRED EARLY. MAINTENANCE REPLACED LEFT ENGINE NTS SWITCH. (X) 2 L 7 2 4T RT A41NM 1999021200552 19990212 00552 EU 1999 2 12 RAIA990133 1 19990125 A 3030 Q50AB1 CURRENT SENSOR BAG JETSTM JETSTM3201 1500217 EU NR 2 PITOT HEAT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 971JX 971 FAT - FLT 4793 - NR 2 PITOT HEAT TRIPS CIRCUIT BREAKER. MAINTENANCE REPLACED NR 2 PITOT HEAT CURRENT SENSOR. (X) 2 L 7 2 4T RT A56EU 1999021200553 19990212 00553 SO 1999 2 12 RAIA990128 1 19990122 A 3010 329445 VALVE EMB 145 EMB145 SO LT WING FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 801HK 145053 ORD - FLT 5776 - WING ANTI-ICE FAILED. MAINTENANCE REPLACED LEFT WING ANTI-ICE VALVE. (X) 2 L 7 2 4F RT T00011AT 1999021200554 19990212 00554 NM 1999 2 12 BJNA990102 1 19990119 A 3350 COVER BOEING 737 7372H4 138448C NM CABIN BROKEN A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 456TM 20336 WIRES EXPOSED, AFT PLASTIC PROTECTIVE COVER BROKEN ON EMERGENCY TRACK LIGHTING SYSTEM. PROTECTED EXPOSED WIRING IAW BMM 20-10-14, EMERGENCY LIGHTING OPERATES NORMALLY. PENDING INSTALLATION OF PLASTIC PROTECTIVE COVER. (X) 2 L 7 2 4F A16WE 1999021200555 19990212 00555 NM 1999 2 12 BJNA990103 1 19990112 A 3350 SPLICE BOEING 737 7372H4 138448C NM CABIN BAD A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 20336 CABIN EMERGENCY EXIT LIGHTS INTERMITTENT. FOUND BAD WIRE SPLICE AT CABIN, REPAIRED IAW BMM 33-51-0. OPS CHECKS GOOD. ( X) 2 L 7 2 4F A16WE 1999021200556 19990212 00556 WP 1999 2 12 ORJA9912 1 19990113 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 21 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SEA, EMERGENCY LIGHTS WERE ON AT ROW 21 DEF. REPLACED BATTERY PACK AT 21D. OPS NORMAL. BAD BATTERY PACKS IN E/E. ( M) 2 L 7 2 4F RT A6WE 1999021200557 19990212 00557 WP 1999 2 12 ORJA9916 1 19990114 A 5230 DOOR DOUG DC9 DC983 3022083 WP CARGO COMPT NOT CLOSED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 834RA 53124 SEA - AT START OF TAKEOFF ROLL IN ANC, FORWARD CARGO DOOR LIGHT ILLUMINATED. DISCONTINUED TAKEOFF AT APPROXIMATELY TAXI SPEED. RETURNED TO TERMINAL AND HAD DOOR OPENED AND RECLOSED. LIGHT WENT OUT AND A/C PRESSURIZED MANUALLY. CONTINUED TO SEA IAW MD80 QRH-12-1. (X) 2 L 7 2 4F RT A6WE 1999021200558 19990212 00558 WP 1999 2 12 USAAD99010 1 19990116 A 5240 MECHANISM DOUG DC9 DC982 3022082 WP SERVICE DOOR OUT OF SEQUENCE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 825US 49237 CLT/ORD - FLT 1527 - AFTER TAKEOFF, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT IN EITHER THE AUTO OR MANUAL MODE. T HE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT AFT SERVICE DOOR MECHANISM OU T OF SEQUENCE AND NOT SEALED. THE DOOR WAS CYCLED SEVERAL TIMES, ALL OPERATIONS CHECKED NORMAL. (X) 2 L 7 2 4F A6WE 1999021200559 19990212 00559 WP 1999 2 12 USAAD99004 1 19990108 A 2150 LT PACK DOUG DC9 DC931 3022065 WP COCKPIT ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 977VJ 48155 ATL-CLT - FLT 349 - AFTER TAKEOFF, THE CREW NOTICED A STRONG RUBBER SMELL THAT INCREASED WITH TIME. THE AIRCRAFT RETURN ED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE IDENTIFIED THE LEFT AIR CONDITIONING PACK AS THE SOURCE OF THE SMELL. THE AIRCRAFT WAS RELEASED FOR FLIGHT WITH THE LEFT AIR CONDITIONING PACK RENDERED INOPERATIVE UNDER THE MEL PRO CEDURES. (M) 2 L 7 2 4F A6WE 1999021200560 19990212 00560 NM 1999 2 12 USAASB99010 1 19990107 A 2130 PRESSURIZATION BOEING 737 737201 1384454 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 260AU 22866 PIT - FLT 1631 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY, OR MANUAL. NO DOOR WARNING LIGHTS WERE ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENA NCE PRESSURIZED AIRCRAFT TO 4 PSI AND CHECKED OUTFLOW VALVE IN AUTO AND MANUAL. OPS CHECKED GOOD. CHECKED ALL DOORS FO R LEAKS AND OPERATION. DOORS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4F A16WE 1999021200561 19990212 00561 NE 1999 2 12 MASA99009 2 19990112 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FOD A MASA A UNSCHED LANDING B C SMOKE/FUMES/ODORS/SPARKS F.O.D. TO TAKEOFF 1 SW 07 190YV UE190 114418 FLT 5872 - PIT-PKB - DURING TAKEOFF ROLL, ATC NOTIFIED THE CREW THAT THEY OBSERVED SPARKS FROM THE NR 2 ENGINE EXHAUST. ATC CALLED FOR EMERGENCY VEHICLES TO STANDBY. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. CREW REPORTED NO GAUGE FLUCTUATION OF ANY KIND. MAINTENANCE REPLACED THE NR 2 ENGINE DUE TO FOD DAMAGE. ALL OPS CHECKS GOOD. AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999021200562 19990212 00562 NM 1999 2 12 MASA99007 1 19990108 A 5210 85210241003 DOOR STRUT 85210001001 DHAV DHC8 DHC8202 2809007 NM PASSENGER DOOR BENT A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 437YV 437 PHX/PSP - FLT 8345 - PRIOR TO DEPARTURE. CREW REPORTED THE PASSENGER DOOR WOULD NOT CLOSE COMPLETELY. MAINTENANCE REPL ACED THE DOOR STRUTS, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1999021200563 19990212 00563 NE 1999 2 12 MASA99004 2 19990107 A 7261 R1310P022 O RING GE 6037T31G02 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 ENGINE CUT A MASA A B E UNSCHED LANDING EMER. DESCENT ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 17217 7217 872268 YYZ/CLT - FLT 5780 - AFTER DEPARTURE FROM YYZ. CAPTAIN REPORTED A NR 2 ENGINE OIL PSI MESSAGE ON THE EICAS. CREW PERF ORMED A NR 2 ENGINE SHUT DOWN AND DECLARED AN EMERGENCY. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAIN TENANCE SERVICED THE OIL THEN GROUND RAN TEST FLEW THE AIRCRAFT. AFTER VERIFYING THE OIL LEVEL, THE AIRCRAFT WAS FERRIE D TO BHM. BHM MAINTENANCE REMOVED AND REPLACED THE AFT 'F' AXIS O-RING FOR AGB HOUSING NEXT TO THE CARBON SEAL. OPS CH ECKED GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200564 19990212 00564 NM 1999 2 12 AT99000039 1 19990117 A 5330 SKIN BOEING 737 737214 138446R NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FUSELAGE CRACKED AT CAPTAIN'S FORWARD SKYLIGHT AND LOWER INBOARD WINDOW MOUNT SC REW. FABRICATED DOUBLER FROM 2024-T3 .0125 THOUSANDS IAW B737 SRM 51-30-8. INSTALLED REPAIRED IAW B737 SRM 53-30-3 AND AIRTRAN RES NR 9938. (X) 2 L 7 2 4F A16WE 1999021200565 19990212 00565 WP 1999 2 12 HALA9900009 1 19990107 A 3620 P195 VALVE DOUG DC10 DC1030 3023501 WP NR 3 ENGINE MALFUNCTIONED A HALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 WP 13 140AA 46712 HNL - FLT 09 - LOG PAGE: 4917181. DURING CRUISE (WITH NR 2 PNEU SELECTOR PLACARDED INOP AND NR 1 PNEU SYS TEMP HI LIGHT ILLUMINATED. PERFORMED EMERG CHKLST AND DOWNLOADED TO 2-PACK OPERATION (NR 1 AND NR 3 PACKS ON, SUPPLIED BY NR 3 PNEU SYS. WHEN NR 1 PNEU SELECTOR TURNED OFF, TEMP AND PRESS DECREASED. TEMP 265 DEREES CELSIUS PRESS 45 PSI). NR 3 PNEU S YS PRESS INDICATION DROPPED TO ZERO AND BEGAN FLUCTUATING BETWEEN ZERO - 60 PSI. APPEARED TO BE ONLY INDICATION AS NR 1 PRESS REMAINED CONSTANT AND CABIN RATE NEVER FLUCTUATED. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE TEMP CONTROL SENS OR. REMOVED AND REPLACED PNEU CONTROLLER. OPS LEAK AND CHECK OK. REF: OPER CNTRL NR 99ZZZX571 AND 99ZZX572. (X) 2 L 7 3 4F A22WE 1999021200566 19990212 00566 WP 1999 2 12 99ZZZX571 1 19990107 A 3620 SENSOR DOUG DC10 DC1030 3023501 WP NR 3 ENGINE MALFUNCTIONED A HALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 WP 13 140AA 46712 HNL - FLT 09 - LOG PAGE: 4917181. DURING CRUISE (WITH NR 2 PNEU SELECTOR PLACARDED INOP AND NR 1 PNEU SYS TEMP HI LIGHT ILLUMINATED. PERFORMED EMERG CHKLST AND DOWNLOADED TO 2-PACK OPERATION (NR 1 AND NR 3 PACKS ON, SUPPLIED BY NR 3 PNEU SYS. WHEN NR 1 PNEU SELECTOR TURNED OFF, TEMP AND PRESS DECREASED. TEMP 265 DEREES CELSIUS PRESS 45 PSI). NR 3 PNEU S YS PRESS INDICATION DROPPED TO ZERO AND BEGAN FLUCTUATING BETWEEN ZERO - 60 PSI. APPEARED TO BE ONLY INDICATION AS NR 1 PRESS REMAINED CONSTANT AND CABIN RATE NEVER FLUCTUATED. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE TEMP CONTROL SENS OR. REMOVED AND REPLACED PNEU CONTROLLER. OPS LEAK AND CHECK OK. REF: OPER CNTRL NR HALA9900009 AND 99ZZZX572. 2 L 7 3 4F A22WE 1999021200567 19990212 00567 WP 1999 2 12 99ZZZX572 1 19990107 A 3620 059C709 CONTROLLER DOUG DC10 DC1030 3023501 WP NR 3 ENGINE MALFUNCTIONED A HALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 WP 13 140AA 46712 HNL - FLT 09 - LOG PAGE: 4917181. DURING CRUISE (WITH NR 2 PNEU SELECTOR PLACARDED INOP AND NR 1 PNEU SYS TEMP HI LIGHT ILLUMINATED. PERFORMED EMERG CHKLST AND DOWNLOADED TO 2-PACK OPERATION (NR 1 AND NR 3 PACKS ON, SUPPLIED BY NR 3 PNEU SYS. WHEN NR 1 PNEU SELECTOR TURNED OFF, TEMP AND PRESS DECREASED. TEMP 265 DEREES CELSIUS PRESS 45 PSI). NR 3 PNEU S YS PRESS INDICATION DROPPED TO ZERO AND BEGAN FLUCTUATING BETWEEN ZERO - 60 PSI. APPEARED TO BE ONLY INDICATION AS NR 1 PRESS REMAINED CONSTANT AND CABIN RATE NEVER FLUCTUATED. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE TEMP CONTROL SENS OR. REMOVED AND REPLACED PNEU CONTROLLER. OPS LEAK AND CHECK OK. REF: OPER CNTRL NR HALA9900009 AND 99ZZX571. 2 L 7 3 4F A22WE 1999021200568 19990212 00568 WP 1999 2 12 HALA9900010 1 19990110 A 3620 SENSOR DOUG DC10 DC1030 3023501 WP NR 1 SYSTEM FAILED A HALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 WP 13 140AA 46712 HNL - FLT 01 - LOG PAGE: 4917190. NR 1 MANIFOLD FAIL AT 1730, COMP FIRST CLASS WAS VERY WARM, MANIFOLD TEMP WAS 240 DE GREES, THEN CAME 'DUCT, AVIONICS COMP OVERHEAT' CAME ON. ACCOMPLISHED CHECKLIST. PNEUMATIC TEMP HIGH WARNING LIGHT ILL UMINATED. EMERGENCY CHECKLIST COMPLETED. PACK SHUT DOWN. REPLACED HIGH RPESSURE, BLEED TEMP SENSOR. GROUND RUN CHECK OK. (X) 2 L 7 3 4F A22WE 1999021200569 19990212 00569 EU 1999 2 12 USAAF99007 1 19990122 A 2750 A83235419 SYNCHRONIZER FOKKER F28 F28MK0100 4990807 EU RT TE FLAP INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 883US 5745 11337 PIT - FLT 864 - AFTER TAKEOFF FROM PIT, A 'FLAP ASYMMETRY' WARNING ILLUMINATED. CREW PERFORMED THE ABNORMAL PROCEDURE C HECKLIST. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 RIGHT SIDE FL AP SYNCHRONIZER. (X) 2 L 7 2 4F RT 1999021200570 19990212 00570 EU 1999 2 12 USAAF99008 1 19990125 A 5610 WINDOW FOKKER F28 F28MK0100 4990807 EU LT COCKPIT LOOSE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 861US 11297 CLT - FLT 8076 - AFTER TAKEOFF FROM CLT, THE LEFT COCKPIT SLIDING WINDOW WAS MAKING A LARGE AIR LEAK NOISE. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT WINDOW OUT OF TRACK. THEY RE-INSTALLED THE WINDOW IN ITS TRACK. (X) 2 L 7 2 4F RT 1999021200571 19990212 00571 NM 1999 2 12 NOCA0199C 1 19990118 A 2160 6240142 TEMP SENSOR BOEING 757 75723A 1384967 NM NR 1 & 2 PACKS INOPERATIVE A NOCA O OTHER O OTHER CR CRUISE 1 EA 15 757NA 24567 DURING FLIGHT, CABIN TEMP INCREASE, CREW ATTEMPTED TO REGULATE BY USING TRIM AIR SWITCH. TRIM AIR SWITCH HAD NO EFFECT . CABIN ALTITUDE STARTED TO CLIMB. CREW COMMENCED DESCENT. EVALUATION CONDUCTED TO PREVENT RECURRENCE WITH CHKS OF TR IM AIR VALVE SYS TEST. ZONE TEMP SENSOR RESISTANCE CHK. PRESSURIZATION SYS CHK. OUTFLOW VALVE INSP AND TEST, AND BITE CHK OF ZONE TEMP CONTROLLER. ALL CHKS FOUND BOTH LT AND RT WATER EXTRACTOR NOZZLE SPRAY PATTERN NOT IAW MM 21-51-11. B OTH PACK WATER EXTRACTOR NOZZLES REPLACED. LOW LIMIT VALVE LT POSITION FAILED TEST. LT LOW LIMIT VALVE REPLACED. NO T EMP OR PRESS ITEMS REPORTED SINCE ORIGINAL DISCREPANCY 1-18-99. (X) 2 L 7 2 4F RT A2NM 1999021200572 19990212 00572 NM 1999 2 12 NOCA0199B 1 19990118 A 2150 32896961 VALVE BOEING 757 75723A 1384967 NM LT PACK INOPERABLE A NOCA O OTHER O OTHER CR CRUISE 1 EA 15 757NA 24567 DURING FLIGHT, CABIN TEMP INCREASE, CREW ATTEMPTED TO REGULATE BY USING TRIM AIR SWITCH. TRIM AIR SWITCH HAD NO EFFECT. CABIN ALTITUDE STARTED TO CLIMB. CREW COMMENCED DESCENT. EVALUATION CONDUCTED TO PREVENT RECURRENCE WITH CHECKS OF T RIM AIR VALVE SYS TEST, ZONE TEMP SENSOR RESISTANCE CHK, PRESS SYS CHK, OUTFLOW VALVE INSP AND TEST, AND BITE CHK OF ZON E TEMP CONTROLLER. ALL CHKS ACCOMPLISHED, FOUND LT AND RT WATER EXTRACTOR NOZZLE SPRAY PATTERN NOT IAW MM 21-51-11. BO TH PACK WATER EXTRACTOR NOZZLES REPLACED. LOW LIMIT VALVE LT POSITION FAILED TEST. LT LOW LIMIT VALVE REPLACED. NO TE MPERATURE OR PRESS ITEMS REPORTED SINCE ORIGINAL DISCREPANCY DATED 1-18-98. (X) 2 L 7 2 4F RT A2NM 1999021200573 19990212 00573 WP 1999 2 12 GTIA9800138 1 19990102 A 3350 362624 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERABLE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 ACY - FLT 168 - FORWARD FLOOR EMERGENCY TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT ST RIP. OPERATIONAL CHECKS GOOD IAW MM 33-51-1. (X) 2 L 7 2 4F A6WE 1999021200588 19990212 00588 EA 1999 2 12 VTZA99013 1 19990102 A 2611 P1190421R3 DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY FAILED A VTZA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 630BR 7255 IAD/JAX - FLT 6753 - DURING TAKEOFF AT 1850 HRS ON 1-2-99, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LAV SMOKE DETECTO R WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED COALESCER BAGS AND LAV SMOKE DETECTOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. REF: OPERATOR CONTROL NR 99ZZZX____. (X) 2 L 7 2 4F RT A21EA 1999021200589 19990212 00589 EA 1999 2 12 99ZZZX574 1 19990102 A 2170 7536893 COALESCER CNDAIR CL600 CL6002B19 EA CABIN FAILED A VTZA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 630BR 7255 IAD/JAX - FLT 6753 - DURING TAKEOFF AT 1850 HRS ON 1-2-99, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LAV SMOKE DETECTO R WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED COALESCER BAGS AND LAV SMOKE DETECTOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. REF: OPERATOR CONTROL NR VTZA99013. 2 L 7 2 4F RT A21EA 1999021200590 19990212 00590 NM 1999 2 12 NOCA0199A 1 19990118 A 2150 22030851 WATER NOZZLE BOEING 757 75723A 1384967 NM LT/RT PACK INOPERATIVE A NOCA O OTHER O OTHER CR CRUISE 1 EA 15 757NA 24567 DURING FLIGHT, CABIN TEMPERATURE INCREASE, CREW ATTEMPTED TO REGULATE BY USING THE TRIM AIR SWITCH. TRIM AIR SWITCH HAD NO EFFECT. CABIN ALTITUDE STARTED TO CLIMB. CREW COMMENCED DESCENT. EVALUATION CONDUCTED TO PREVENT RECURRENCE WITH CHKS OF TRIM AIR VALVE SYS TEST, ZONE TEMP SENSOR RESISTANCE CHK, PRESSURIZATION SYS CHK, OUTFLOW VALVE INSP AND TEST, A ND BITE CHK OF ZONE TEMP CONTROLLER. ALL CHKS ACCOMPLISHED AND FOUND LT AND RT WATER EXTRACTOR NOZZLE SPRAY PATTERN NOT IAW MM 21-51-11. BOTH PACK WATER EXTRACTOR NOZZLES REPLACED. LOW LIMIT VALVE LT POSITION FAILED TEST. LT LOW LIMIT V ALVE REPLACED. NO TEMPERATURE OR PRESSURIZATION ITEMS REPORTED SINCE ORIGINAL DISCREPANCY DATED 1-18-98. (X) 2 L 7 2 4F RT A2NM 1999021200591 19990212 00591 WP 1999 2 12 ORJA9908 1 19990113 A 3350 59306431 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 RNO - AFT TWO CABIN CEILING EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED BAD BATTERIES. OPS CHECK GOOD. (X) 2 L 7 2 4F A6WE 1999021200700 19990212 00700 NM 1999 2 12 USAABB99001 1 19990102 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 29 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 LAX - FOUND FLOOR EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1999021200705 19990212 00705 NM 1999 2 12 USAA019902 1 19990111 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS P2793 21244 FLT 6151 - BOS-LGA - FOUND ON L/S, CEILING EMERGENCY EXIT LIGHT AT ROW 18 INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999021200706 19990212 00706 NM 1999 2 12 USAA019901 1 19990105 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS N2109 20447 FLT 6181 - BOS-LGA - OVERHEAD EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS FLASHES INTERMITTENTLY. REPLACED BATTERY PACK, CHEC KS OK. (M) 2 L 7 3 4F A3WE 1999021200711 19990212 00711 WP 1999 2 12 USAAD99007 1 19990108 A 3350 20131ALP BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 946VJ 47026 PHL - THE COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE COCKPIT EMERGENCY LIGH T. (M) 2 L 7 2 4F A6WE 1999021200712 19990212 00712 WP 1999 2 12 USAAD990066 1 19990108 A 2913 AS66411LS66 PUMP DOUG DC9 DC931 3022065 WP LT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 976VJ 48147 CLT-ROA - FLT 1671 - AFTER TAKEOFF, THE LEFT HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. THE LEFT ENGINE HYDRAULIC PUMP W AS SWITCHED OFF AND THE PRESSURE RETURNED USING THE AUX/ALT PUMPS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOU T INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. (M) 2 L 7 2 4F A6WE 1999021200713 19990212 00713 WP 1999 2 12 USAAD99005 1 19990108 A 3010 129112 THERMOSTAT DOUG DC9 DC931 3022065 WP LEFT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 959VJ 47352 PIT-SBN - FLT 399 - DURING CLIMB AFTER TAKEOFF, THE LEFT ICE PROTECTION TEMP LOW LIGHT WOULD NOT EXTINGUISH UNLESS THE E NGINE POWER WAS SET ABOVE 78 PERCENT N2. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE R EPLACED THE LEFT AIRFOIL ANTI-ICE LOW TEMP THERMOSTAT. (M) 2 L 7 2 4F A6WE 1999021200715 19990212 00715 NM 1999 2 12 USAASB99005 1 19990106 A 3350 20121 BATTERY CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 779AU 24996 PIT - PILOT REPORTED THAT THE EMERGENCY EXIT SIGN AT SEAT ROW 21 AND THE EMERGENCY PATH LIGHTING AT SEAT ROW 11 ARE INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999021200716 19990212 00716 NM 1999 2 12 USAASB99008 1 19990101 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 426US 24548 IAH - MAINTENANCE FOUND THE LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999021200720 19990212 00720 WP 1999 2 12 USAAD99003 1 19990101 A 3350 20131ALP BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959VJ 47352 SYR - THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTING AND THE CATWALK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENA NCE REPLACED THE BATTERY PACK FOR THE FLOOR TRACK AND CATWALK EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999021200721 19990212 00721 NM 1999 2 12 USAASB99002 1 19990102 A 3020 655812310 DUCT BOEING 737 7372B7 1384560 NM NR 1 ENGINE LEAKING A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 271AU 22883 MCO - FLT 2740 - CLIMBING THROUGH FL110, THE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. ALL OTHER ENGINE INDICATIONS WERE NOR MAL. CREW LEVELED FLIGHT OFF AT FL120, THEN ADVISED ATC, RETURNING TO MCO. CAPT PULLED THE NR 1 ENGINE THROTTLE BACK T O IDLE, DECLARED AN EMERGENCY AND AT APPROX 3 MINUTES OUT OF MCO, ON FINAL APPROACH, SHUT DOWN NR 1 ENGINE. FLT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS THREE MINUTES. MX FOUND THE TOP NOSE COWL ANTI-ICE DUCT ASSEMLB Y WITH A BLOWN FLEXIBLE ASSY. REPLACED DUCT ASSY. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999021200722 19990212 00722 NM 1999 2 12 USAASB99001 1 19990101 A 8012 1G309 SWITCH BOEING 737 7372B7 1384560 NM NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 271AU 22883 BWI - FLT2679 - CLIMB THROUGH FL190, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW LEVELED THE AIRCRAFT AT F L230 AND WERE UNSUCCESSFUL AT CORRECTING THE PROBLEM. QUICK REFERENCE HANDBOOK PROCEDURES WERE FOLLOWED AND THE NR 1 EN GINE WAS SHUT DOWN. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BWI. FLIGHT LANDED WITHOUT FURTHER INCIDENT. T OTAL SINGLE ENGINE TIME 17 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE START VALVE OPEN LIGHT PRESSURE SW ITCH. SYSTEM OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999021200724 19990212 00724 NM 1999 2 12 TSAA9933020 1 19990112 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOP FOR POSITIONS 1, 2, 3 AND 4. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999021200725 19990212 00725 NM 1999 2 12 TSAA9933019 1 19990111 A 3350 6013211 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED FORWARD SLIDE LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999021200726 19990212 00726 NM 1999 2 12 TSAA9933018 1 19990111 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 2 SEAT EMERGENCY LIGHT ASSY BATTERY PACK DUE TO NO 'ALL WELL' LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 1999021200727 19990212 00727 EU 1999 2 12 SIMA990093 1 19990109 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 045 ORD - FLT 4065 - EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED TWO BATTERY PACKS. OPERATION AL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999021200728 19990212 00728 EU 1999 2 12 SIMA990071 1 19990107 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AM 11777 319 GRR - CENTER CABIN EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999021200729 19990212 00729 EU 1999 2 12 99ZZZM116 1 19990107 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AM 1338 319 GRR - CENTER CABIN EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999021200730 19990212 00730 NM 1999 2 12 P2EA99010 1 19990108 A 5330 SKIN BOEING 737 737222 1384473 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. DEFECT SIZE, LENGTH .375 INCH. REPAIRED HINGE CUTOUT AREA BETWEEN B S 945.5 TO BS 956, BETWEEN STRINGER 10 RT AND STRINGER 12 RT PER SRM 53-30-3 FIG 21A. (M) 2 L 7 2 4F A16WE 1999021200731 19990212 00731 NM 1999 2 12 P2EA99009 1 19990106 A 5330 SKIN BOEING 737 737222 1384473 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 FUSELAGE MAIN ENTRY DOOR CUTOUT, ANGLE CRACKED BETWEEN STOP FITTING NR 6 AND NR 7, DEFECT SIZE, LENGTH .375. ANGLE REPL ACED AT MAIN ENTRY DOOR, FORWARD SECTION PER SRM 51-10-1, PAGE 5, AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999021200732 19990212 00732 NM 1999 2 12 P2EA99008 1 19990106 A 5542 SKIN BOEING 737 737222 1384473 NM RUDDER DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - RUDDER TRAILING EDGE ERODED AT RUDDER STATION 233, RIGHT SIDE, DEFECT SIZE, LENGTH 6 INCHES, WIDTH 4 INCHES. REPA RIED RUDDER SECTION AT RUDDER STATION 233 PER SRM 51-40-9, PAR 3 AND 4. (M) 2 L 7 2 4F A16WE 1999021200733 19990212 00733 NM 1999 2 12 P2EA99007 1 19990106 A 5542 SKIN BOEING 737 737222 1384473 NM RUDDER DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - HOLE FOUND AT RUDDER STATION 214, LEFT SIDE, TRAILING EDGE. DEFECT SIZE, DIAMETER .250 INCH. REPAIRED RUDDER PER SRM 51-40-9, PAR 3 AND 4 AT RUDDER STATION 214. (M) 2 L 7 2 4F A16WE 1999021200734 19990212 00734 NM 1999 2 12 MASA99010 1 19990114 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 WHILE PERFORMING ROUTINE MAINTENANCE INSPECTION, FOUND THE F/A'S EMERGENCY LIGHT SWITCH FAILED TO ILLUMINATE IN THE NORM AL POSITION. REMOVED AND REPLACED THE BULBS, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1999021200735 19990212 00735 NM 1999 2 12 MASA99006 1 19990110 A 3350 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 FLT 6385 - PHX-YUM - CREW REPORTED ONE ESCAPE PATH LIGHTING BULB INOPERATIVE. MAINTENANCE ACTION WAS DEFERRED PER MEL 3 3-11. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE THE FORWARD EMERGENCY EXIT FLOOR TRACK WAS REPLACED. (M) 2 H 7 2 4T RT A13NM 1999021200736 19990212 00736 NM 1999 2 12 MASA99002 1 19990103 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 FLT 6335 - PHX-BFL - CREW REPORTED THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED A ND REPLACED THE BATTERY PACK, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999021200755 19990212 00755 EU 1999 2 12 C2XA99BT001 1 19990107 A 3260 C24589000 UPLOCK AEROSP ATR42 ATR42320 8680930 EU LT MLG MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 15823 165 FLT 4396 - REPORTED 'PRIMARY UNLOCK LIGHT STAYS ON FOR LEFT GEAR'. MAINTENANCE REMOVED AND REPLACED LEFT UPLOCK BOX AND OPERATIONALLY CHECK SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999021200758 19990212 00758 NM 1999 2 12 99ZZZM120 1 19990106 A 2781 INDICATOR BOEING 727 727225 1384077 NM LE FLAP MALFUNCTIONED A C8GA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 15 808EA 35688 22439 FLT 34 - KDAY-KELP - AFTER TAKEOFF, THE NR 2 LEADING EDGE FLAP FAILED TO INDICATE COMPLETE RETRACTION. CYCLED FLAPS SEV ERAL TIMES. NO FIX. AIRCRAFT RETURNED KDAY AND LANDED WITHOUT FURTHER INCIDENT. PERFORMED THOROUGH INSPECTION OF NR 2 LEADING FLAP AND PERFORMED FLAP OPS CHECK. NO DEFECTS NOTED. SUSPECT ICE ACCUMULATION IN THE FLAP SWITCH AREA. AIRCR AFT DEICED AND RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999021200759 19990212 00759 NM 1999 2 12 BJNA990101 1 19990107 A 2913 371380 PUMP BOEING 737 7372H4 138448C NM 'A' HYD SYSTEM FAILED A BJNA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 456TM 20336 NR 1 'A' SYSTEM ENGINE HYDRAULICS INOPERATIVE. REMOVED AND REPLACED NR 1 'A' SYSTEM ENGINE HYDRAULIC DRIVE PUMP IAW BMM 29011-31, OPS CHECKS GOOD AT THIS STATION. REPAIRED BROKEN WIRE IN LEFT GEAR WELL FOR LEFT ENGINE HYDRAULIC S/O VALVE, IAW BMM 20-10-13. GROUND CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1999021200761 19990212 00761 WP 1999 2 12 HALA9900007 1 19990108 A 3397 WIRE DOUG DC10 DC1010 3022110 WP CABIN SHORTED A HALA K NONE L NO TEST CR CRUISE 1 WP 13 153AA 46708 HNL - FLT 939 - EMERGENCY FLOOR LIGHTS ARE ON. REPAIRED SHORTED WIRE BEHIND L1 DOOR EXIT ICON. OPS CHECK OK. (M) 2 L 7 3 4F A22WE 1999021200762 19990212 00762 NM 1999 2 12 F3LA99003 1 19990118 A 2613 WARNING SYSTEM BOEING 737 7372P6 NM NR 2 ENGINE ILLUMINATED A F3LA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 03 1PC 21613 LAS - FLT 772 - AIR TURN BACK, FLIGHT CREW REPORTED NR 2 ENGINE OVERHEAT LIGHT ILLUMINATE INFLIGHT. NR 2 ENGINE WAS SHU T DOWN AND BOTH FIRE EXTINGUISHER BOTTLES WERE DISCHARGED. AIRCAFT RETURNED TO LAS WITHOUT INCIDENT. MAINTENANCE REPLA CED ENGINE/APU FIRE CONTROL MODULE AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999021200763 19990212 00763 NM 1999 2 12 TSAA9933025 1 19990116 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999021200764 19990212 00764 NM 1999 2 12 TSAA9933024 1 19990116 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 FLOOR EMERGENCY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999021200765 19990212 00765 NM 1999 2 12 TSAA9933023 1 19990116 A 3350 86210066 BATTERY BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 5 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY ASSY. DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999021200766 19990212 00766 NM 1999 2 12 USAA990010 1 19990117 A 5315 65468101 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 30727 23879 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 967 RBL 20. CORROSION TASK NR C53-107-02 . INSTALLED REPAIR ANGLE PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1999021200767 19990212 00767 NM 1999 2 12 USAA990009 1 19990117 A 5315 654581094 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 30727 23879 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FUOND CORROSION AROUND 2 SCREW HOLES 3 INCH BY 3 INCH TOP OF FLOORBEAM BS 312 BL 0. CORROSION TASK NR C53-107-02. SPLICED FLOORBEAM 'T' CAP AND INSTALLED ANGLE PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999021200768 19990212 00768 EU 1999 2 12 99ZZZM122 1 19990108 A 3230 SWITCH BAG JETSTM JETSTM3201 1500217 EU MLG MALFUNCTIONED A FYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 05 242BM 902 AIRCRAFT DEPARTED JUNEAU AND GEAR WOULD NOT RETRACT. RETURNED TO JUNEAU WITHOUT INCIDENT. AIRCRAFT IN HANGAR UNDERGOIN G MORE TROUBLESHOOTING, READJUSTED SQUAT SWITCH. CHECKED AND ADJUSTED NOSE GEAR STRUT EXTENSION. PERFORMED FUNCTIONAL FLIGHT CHECK. ALL SYSTEMS OPERATED NORMALLY. (M) 2 L 7 2 4T RT A56EU 1999021200770 19990212 00770 EU 1999 2 12 99ZZZM124 1 19990106 A 3230 5EN16 SWITCH BAG JETSTM JETSTM3201 1500217 EU MLG INOPERATIVE A FYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 05 242BM 902 AIRCRAFT DEPARTED JUNEAU AND GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO JUNEAU WITHOUT INCIDENT. TROUBLESHOTING REVE ALED BAD SQUAT SWITCH. REMOVED AND REPLACED SQUAT SWITCH. (M) 2 L 7 2 4T RT A56EU 1999021200774 19990212 00774 NE 1999 2 12 99ZZZM128 2 19990111 A 7200 ENGINE BOEING 757 75723APF 1384966 NM RROYCE RB211 RB211535E4 54555 NE NR 1 FAILED A CLCA C D ABORTED TAKEOFF RETURN TO BLOCK E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 571CA 24456 30710 FLT 96 - SEQU-CLO - ON TAKEOFF ROLL AT 0010Z, ON ROUTINE NORMAL TAKEOFF AT APPROXIMATELY 75 KNOTS A/C BEGAN TO MAKE VIOL ENT BANGING NOISE AND ABNORMALLY EXTREME SHUDDERING FOLLOWED BY A MODERATE YAW TO THE LEFT. THE REJECTED TAKEOFF PROCED URE WAS INITIATED AND A/C STOPPED ON RUNWAY. HTC REPORTED TO THE CREW THAT THERE WAS FLAMES AND FIRE COMING FROM THE LE FT ENGINE. THE EMERGENCY SHUT DOWN WAS COMPLETED ON BOTH ENGINES AND THE APU BOTH ENGINE FIRE EXTINGUISHERS WERE DISCHA RGED. FIRE EQUIPMENT WAS DISPATCHED, HOWEVER THERE WAS NOT FIRE, THE CREW EVACUATED THROUGH THE CREW DOOR USING THE EVA CUATION ROPES. NEITHER OF THE CREW INJURED. INSPECTION BY MAINTENANCE FOUND DAMAGE TO THE NR 1 ENGINE FAN CASE LINER, 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200775 19990212 00775 CE 1999 2 12 MASA99003 1 19990104 A 2120 AIR DIST BEECH 1900 1900D 1154162 CE COCKPIT SMOKE A MASA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 125YV UE125 FLT 5328 - BOS-MVY - DURING CRUISE AT 5000 FT, THE CREW VISUALLY DETECTED SMOKE IN THE COCKPIT ACCOMPANIED BY A BURNED S MELL. THE SMOKE LASTED APPROXIMATELY 30 SECONDS TO 1 MINUTE BEFORE IT DISSIPATED. THE CREW CONTINUED DESCENT INTO MVY, WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND RUNS AND ALL SYSTEMS CHECKED NORMAL. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999021200776 19990212 00776 CE 1999 2 12 MASA99001 1 19990102 A 5610 10138402522 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A MASA A B I UNSCHED LANDING EMER. DESCENT CABIN DEPRESSURIZATION O OTHER CR CRUISE 1 SW 07 93ZV UE93 FLT 6459 - FMN-PHX - IN FLIGHT, THE RIGHT PILOT WINDSHIELD CRACKED TOP TO BOTTOM WITH CRACKS RADIATING FROM BOTH SIDES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO INW. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS SUBSEQ UENTLY FERRIED TO FMN, WHERE THE WINDSHIELD WAS REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999021200777 19990212 00777 NM 1999 2 12 MASA99008 1 19990111 A 2611 473053 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 436YV 436 FLT 6348 - PSP-PHX - AFTER DEPARTURE FROM PSP, CREW REPORTED A CARGO BAY SMOKE DETECTOR ANNUNCIATOR ILLUMINATED IN FLIGH T. AIRCRAFT RETURNED TO THE FIELD. NO EVIDENCE OF FIRE OR SMOKE WAS NOTED. MAINTENANCE REPLACED THE SMOKE DETECTOR. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999021200778 19990212 00778 NM 1999 2 12 F3LA99002 1 19990113 A 5320 WEB BOEING 737 737201 1384454 NM BS 285 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PHX - DURING SERVICE CEHCK, MAINTENANCE REPORTED .5 INCH CRACK ON WEB OF LEFT NLG WHEEL WELL STATION 285. ONE RIVET BOR KEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG WHEEL WELL AT LEFT AFT ACCESS PANEL. MAINTENAN CE REPLACED NLG WHEEL WELL CHORD STATION 235-294 AND STANCHION PLR SRM 51-30-02 AND EA 737-5310-0001. (M) 2 L 7 2 4F A16WE 1999021200779 19990212 00779 NM 1999 2 12 F3LA99001 1 19990105 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 DEN - FLT 850 - UPON ARRIVAL, MAINTENANCE REPORTED HOLE IN FUSELAGE, AFT OF FORWARD LAV SERVICE DOOR STATION 328, STRING ER 24R TO STRINGER 25R. MAINTENANCE FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-5. (M) 2 L 7 2 4F A16WE 1999021200783 19990212 00783 WP 1999 2 12 ARWA990107 1 19990114 A 3231 UPLOCK DOUG DC8 DC862 3021970 WP RT MLG DOOR LACK OF LUBE A ARWA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 810BN 45905 MIA - FLT 1628 - AFTER TAKEOF IN SEGU, GEAR NOT LATCHED LIGHT ILLUMINATED, RECYCLED GEAR SEVERAL TIMES. COULD NOT GET S ATISFACTORY UPLATCH CHECK, DOOR NOT LATCHED, LIGHT DID NOT ILLUMINATE, PROCEEDED TO DESTINATION IN ACCORDANCE OF ABNORMA L CHECKLIST. CHECKED INDICATING SYSTEM, FOUND NORMAL. TROUBLESHOT, FOUND RIGHT MLG DOOR UPLATCH MECHANISM STIFF. LUBE D SAME, CYCLED MLG SEVERAL TIMES AND PERFORMED REPEATED UPLATCH CHECKS NO DISCREPANCIES NOTED. OPS NORMAL IAW DC-8 MM 3 2-30-0 AND 12-81-01 LUBE. (M) 2 L 7 4 4F 4A25 1999021200784 19990212 00784 EU 1999 2 12 C2XA99IA061 1 19990115 A 3350 7008123 BULB AEROSP ATR42 ATR42500 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT SYSTEM WAS FOUND TO BE POPPING THE CIRCUIT BREAKER. MAINTEN ANCE REMOVED AND REPLACED A BULB IN THE FORWARD EMERGENCY LIGHT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 1999021200785 19990212 00785 EU 1999 2 12 C2XA99IA015 1 19990104 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY FLOOD LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-320 JIC33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999021200786 19990212 00786 EU 1999 2 12 C2XA99IA014 1 19990104 A 5347 S5367800124002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU BS 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE LEFT INBOARD PASSENGER SEAT TRACK WAS FOUND TO BE CORRODED AT FRAME 36. MAINTENANC E REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR42-320 SRM 51-25-04, AND 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200787 19990212 00787 EU 1999 2 12 C2XA99IA013 1 19990104 A 5347 S5367800124002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU BS 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURNG C-CHECK INSPECTION, THE RIGHT INBOARD PASSENGER SEAT TRACK WAS FOUND TO BE CORRODED AT FRAME 36. MAINTENANC E REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR42-320 SRM 51-25-04, AND 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200788 19990212 00788 EU 1999 2 12 C2XA99IA012 1 19990104 A 5311 S5367240820051 FRAME AEROSP ATR42 ATR42320 8680930 EU BS 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, FRAME 39 RIGHT WAS FOUND TO BE CORRODED ON THE AFT SIDE ABOVE AND BELOW FLOOR LEVEL. M AINTENANCE REMOVED THE DAMAGED SECTION OF FRAME AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01102, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200789 19990212 00789 EU 1999 2 12 C2XA99IA011 1 19990104 A 5347 S5367800124002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU BS 34-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE LEFT INBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 34.5 TO FRAME 36. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR42-320 SRM 51-25-40, AND 51-25-02, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200790 19990212 00790 EU 1999 2 12 C2XA99IA010 1 19990104 A 5347 S5367800124002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU BS 34-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 34 TO FRAME 36. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR42-320 SRM 51-25-04, AND 51-25-02, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200791 19990212 00791 EU 1999 2 12 C2XA99IA009 1 19990104 A 5320 353678008216B00 BEAM AEROSP ATR42 ATR42320 8680930 EU BS 41 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED AT FRAME 41. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED SECTION OF CREASE BEAM IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 1999021200792 19990212 00792 EU 1999 2 12 C2XA99IA008 1 19990104 A 5315 S53372411200 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU BS 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 33 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED SE CTION OF FLOORBEAM AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC 5310-01037, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200793 19990212 00793 EU 1999 2 12 C2XA99IA003 1 19990104 A 3350 3011206 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE RIGHT LOWER FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESE CURED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200794 19990212 00794 EU 1999 2 12 C2XA99IA004 1 19990104 A 3350 301160 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD EMERGENCY LIGHT ON THE KICKPANEL WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200795 19990212 00795 EU 1999 2 12 C2XA99IA005 1 19990104 A 5320 S53671217210 WEB AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR THRESHOLD WEB WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED WEB IAW ATR42-320 SRM 51-21-17, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200796 19990212 00796 EU 1999 2 12 C2XA99IA006 1 19990104 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU BS 34-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 34 TO FRAME 36. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND 51-70-00, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200797 19990212 00797 EU 1999 2 12 C2XA99IA007 1 19990104 A 5315 S5367240802 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU BS 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAEM 39 WAS FOUND TO BE CORRODED. MAINTENACNE REMOVED AND REPLACED T HE AFFECTED FLOORBEAM IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200798 19990212 00798 EU 1999 2 12 C2XA99IA059 1 19990113 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT 3WL IAW ATR424-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200799 19990212 00799 EU 1999 2 12 C2XA99IA060 1 19990113 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO REMAIN ILLUMINATED AFTER A/C POWE R WAS REMOVED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERY PACKS AT 10WL AND 29WL IAW ATR 42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200800 19990212 00800 SO 1999 2 12 C2XA99CL008 1 19990117 A 3610 14530205405 DUCT EMB 145 EMB145 SO LT ENGINE CHAFFED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 14940 145033 CLE - FLT 4119 - CREW REPORTED THAT DURING CRUISE THEY RECEIVED A LEFT ENGINE BLEED LEAK LIGHT, THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT BLEED DUCT LOCATED IN FUSELAGE ABOVE THE LEFT WING IAW EMB-145 MM 36-11-09. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999021200801 19990212 00801 NE 1999 2 12 C2XA99CL007 2 19990116 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 27716 20304 120128 115212 CLE - FLT 3172 - CREW REPORTED THAT AT CLIMB POWER AT 13,000 FT THEY HEAR A LOUD BANG WITH A AIRCRAFT SHUTTER AND RADICA L POWER AND TEMPERATURE CHANGE ON THE RIGHT ENGINE. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENAN CE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXPRESS TASK CARDS NR 12771011 AND 1271012, OPERATIONAL AND LEA K CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999021200802 19990212 00802 NM 1999 2 12 HNAA9900025 1 19990208 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 962HA 331 CABIN EMERGENCY LIGHTS COME ON WHEN FLIGHT DECK SWITCH IS IN OFF POSITION. REPLACED EMERGENCY LIGHTS CONTROL BOX. 2 H 7 2 4T RT A13NM 1999021200803 19990212 00803 NM 1999 2 12 AT9900095 1 19990206 A 3350 1619 BULB BOEING 737 7372E1 138448F NM L2 DOOR FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 461AT 20976 DURING SCHEDULED MAINTENANCE FOUND EXTERIOR EMERGENCY LIGHT AT L-2 DOOR AND AFT SERVICE DOOR INOPERATIVE. RELAMPED BOTH EMERGENCY LIGHT AND OPS CHECKED THE SYSTEM IAW MM 33-00. 2 L 7 2 4F A16WE 1999021200804 19990212 00804 1999 2 12 AT9900096 4 19990209 A 2565 13621228DME SLIDE DOUG DC9 DC932 3022066 WP TAIL CONE LOW PRESSURE A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 819AT 47260 AFT TAIL CONE SLIDE PRESSURE IS LOW. REMOVED AND REPLACED TAIL CONE SLIDE IAW MM 25-62-1. 2 L 7 2 4F A6WE 1999021200805 19990212 00805 NM 1999 2 12 K3HA990007 1 19990205 A 3350 079123 LENS BOEING 727 727225 1384077 NM ROW 31 MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 EMERGENCY PATH LENSES ROW 31 MISSING. REPLACED RED EMERGENCY PATH LENSES AT ROW 31 IAW MM 33-50-01. 2 L 7 3 4F A3WE 1999021200806 19990212 00806 NM 1999 2 12 K3HA990008 1 19990206 A 3350 079123 LENS BOEING 727 727225 1384077 NM L1 DOOR MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY LIGHTING SYSTEM-FLOOR ESCAPE PATH LIGHTING MISSING INSIDE L1 CABIN DOOR. INSTALLED EMERGENCY PATH LIGHT ASSEM BLY (LENS) IAW MM 33-50-01. 2 L 7 3 4F A3WE 1999021200807 19990212 00807 NM 1999 2 12 K3HA990009 1 19990207 A 3350 079123 LIGHT BOEING 727 727225 1384077 NM ROW 2ABC INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 PASSENGER ROW 2ABC EMERGENCY PATH LIGHT INOP. REPLACED EMERGENCY PATH LIGHT LENS AT PAX ROW 2ABC IAW MM 33-50-01. 2 L 7 3 4F A3WE 1999021200808 19990212 00808 WP 1999 2 12 9900419878 1 19990204 A 3230 RETRACT MECH DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 787NC 48149 DURING APPROACH INTO ATL, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW RECYCLED GEAR WIT H SAME RESULTS. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PE RFORMED FUNCTIONAL CHECK OF NOSE GEAR, NO PROBLEMS WERE FOUND. REPLACED NOSE GEAR RETRACT ACTUATOR AND BUNGEE CYLINDER AS A PRECAUTION. ALSO, RERIGGED CONTROL VALVE AND ALTERNATE GEAR EXTENSION. REPLACED THE LEFT INBOARD GEAR DOOR DUE TO DAMAGE INCURRED ON LANDING. 2 L 7 2 4F RT A6WE 1999021200809 19990212 00809 WP 1999 2 12 9900429853 1 19990205 A 2121 313303 FAN DOUG DC9 DC951 3022051 WP RT LAVATORY FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 762NC 2863 2863 47710 AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMOKE ALARM IN RIGHT LAVATORY GOING OFF WITH A BURNING SMELL. CREW DECLARED AN EMERGENCY AND THE FLIGHT WAS RETURNED TO ATL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GROUN D COOLING FAN AND LAVATORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999021200810 19990212 00810 WP 1999 2 12 9900439983 1 19990208 A 2450 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP LT AC BUS FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 983US 47282 LOSS OF LEFT AC BUS AND ALL CAPTAIN'S INSTRUMENTS OCCURRED AFTER TAKEOFF. CREW RESET LEFT AC BUS, CIRCUIT BREAKER AND I NSTRUMENTS WERE REGAINED. CREW DECLARED AN EMERGENCY. RETURNED TO DTW AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANC E REPLACED LEFT AC BUS, CIRCUIT BREAKER AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999021200811 19990212 00811 WP 1999 2 12 9900441154 1 19990205 A 2740 SB1027020811 VALVE DOUG DC10 DC1040 3023508 WP HORIZ STAB LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 01 154US 37727 9530 46763 HYDRAULIC QUANTITY DECREASED TO ZERO DURING FLIGHT. FLIGHT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. FOUND LOWER HO RIZONTAL STABILIZER CONTROL VALVE LEAKING. REPLACED CONTROL VALVE, LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999021200812 19990212 00812 WP 1999 2 12 9900451227 1 19990206 A 3350 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 227NW 46969 DURING LINE CHECK, FOUND ALL FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED FIRST CLASS SECTION POWER SUPPLY AND BA TTERY PACK, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999021200813 19990212 00813 WP 1999 2 12 UPS99828656 1 19990106 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, RT WING L/E RIB AT XS 520.168 IS CRACKED ABOVE THE FUEL LINE. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999021200814 19990212 00814 WP 1999 2 12 UPS99828657 1 19990107 A 5347 3657504501 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, SECOND OBS SEAT TRACKS ARE CORRODED UNDER THE NUT PLATES. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999021200815 19990212 00815 WP 1999 2 12 UPS99828658 1 19990107 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 505 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, RT WING L/E LOWER T-CAP FLANGE, STA XRS505 ANGLE CRACKED. REMOVED DAMAGE FROM FLANGE FAB DOUBLER FOR REPAIR IAW DAC DRAWING NR R08570014. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999021200816 19990212 00816 WP 1999 2 12 UPS99828659 1 19990105 A 5720 ANGLE DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, LT WING LOWER LEADING EDGE I/B STA XWO ANGLE CRACKED AT O/B END OF ANGLE. FAB DOUBLER IAW 57-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-21. INSTALLED DOUBLERS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999021200817 19990212 00817 WP 1999 2 12 UPS99828660 1 19990103 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1135 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, AFT PIT STA 1135 L23R Z-FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999021200818 19990212 00818 WP 1999 2 12 UPS99828661 1 19990125 A 5320 FITTING DOUG DC8 DC873F 302199F WP LEFT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, TRAP FITTING AND O/B VERTICAL STIFFENER HAVE ELONGATED HOLES ON LT SIDE. BUSHINGS MATERIAL ID AND FABRICATION ON UPS NR 244479. INSTALLED BUSHINGS PER REO 06222. INSTALLED O/B VERTICAL STIFFENER IAW DC8 SRM 51-1-20D , 2 BOTTOM BOLTS TO BE INSTALLED ON UPS N/R 244479. 2 L 7 4 4F RT 4A25 1999021200820 19990212 00820 WP 1999 2 12 UPS99828663 1 19990107 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, STA 1180 RT AT C3 DOOR CUTOUT FLOORBEAM FITTING CRACKED. REMOVED CRACKED FITTING AND REPLACED WIT H NEW FITTING IAW DC8 SRM 51-1- 24, 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999021200821 19990212 00821 WP 1999 2 12 UPS99828664 1 19990107 A 5320 FASTENER DOUG DC8 DC873F 302199F WP BS 1540 SHEARED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, STA 1540, L334R HAS SHEARED FASTENERS THROUGH SKIN. FABBED REPAIR CHANNEL AND FILLER IAW REO 0620 1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1999021200822 19990212 00822 WP 1999 2 12 UPS99828665 1 19990104 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1889 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, FRAME AT STA 1889 IS CORRODED AND HAS DOUBLE DRILLED HOLES. REMOVED PREVIOUS CAP FRAME AND SPLICE ANGLES. GEN REO FOR REPAIR INFO. FABRICATED NEW FRAME SECTION AND 4 SPLICE ANGLES. ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS PER REO 06060. 2 L 7 4 4F RT 4A25 1999021200823 19990212 00823 WP 1999 2 12 UPS99828666 1 19990205 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE-D, FLOORBEAM CRACKED AT STA 1660 L21R AFT SIDE LOWER FLANGE. CUT OUT DAMAGED AREA, FABRICATED REPAIR AN GLE AND FILLER, ALODINED AND PRIMED REPAIR ANGLE FILLER IAW DC SRM 51, INSTALLED REPAIR ANGLE AND FILLER IAW TIMCO REO62 62. 2 L 7 4 4F RT 4A25 1999021200824 19990212 00824 WP 1999 2 12 UPS99828667 1 19990205 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE-AD, STA 1680 FLOORBEAM VERTICAL LEG CORRODED BETWEEN UPPER TEE AND 2ND ROW OF FASTENERS 3 INCHES INBOARD FROM L21R. SMOOTHED AND BLENDED OUT DAMAGE, FABRICATED REPAIR ANGLE, ALODINED AND PRIMED REPAIR ANGLE AND FLOORBEAM, I NSTALLED REPAIR ANGLE. ALL WORK DONE IAW TIMCO REO-06292 REV A. 2 L 7 4 4F RT 4A25 1999021200825 19990212 00825 WP 1999 2 12 UPS99828668 1 19990206 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE-AD, FASTENER HOLE OVERSIZED ON FLOORBEAM. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE, ALODINED AND P RIMED, INSTALLED REPAIR ANGLE. ALL WORK DONE IAW TIMCO DWG DC08-53-0351 R A SHEET 3. 2 L 7 4 4F RT 4A25 1999021200826 19990212 00826 WP 1999 2 12 UPS99828669 1 19990112 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, FS 1080 FRAME AT LONG 35R, THE LOWER FLANGE IS CORRODED BEYOND LIMITS. REPAIRED FRAME IAW SRM 53-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 1999021200827 19990212 00827 WP 1999 2 12 UPS99828670 1 19990114 A 5320 37592221 FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LONG 34L SPLICE FITTING AT FS 1260 TO 1280 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SPLICE F ITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999021200828 19990212 00828 1999 2 12 99FDEA00051 4 19990206 A 3442 RT UNIT AIRBUS 310 A310222 3930315 EU NR 1 RADAR FAILED A FDEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SO 25 420FE 339 SMOKE SMELL BY FLT CREW, AVIONICS SMOKE LT ILLUM. REMOVED AND REPLACED BOTH A/C PACKS WATER SEP BAGS, NO HELP. CHECKED COCKPIT, ALL PANELS OK. REMOVED AND REPLACED NR 1 WX RADAR TRANCEIVER PER MM 34-41-33-4. TEST SAT PER MM 34-41-00-5. 2 L 7 2 4F RT A35EU 1999021200829 19990212 00829 NM 1999 2 12 99FDEA00052 1 19990209 A 2612 WIRE BOEING 727 7272S2F 1384O81 NM FIRE DETECTOR DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 209FE 22931 THREE INSTANCES OF MASTER WARN LIGHT ILLUM AND WARN BELL. FOUND WIRE WITH INSULATION CUT ON LOWER AFT END OF FIRE LOOP. SPLICED WIRE AT SEP PER MM CHAPTER 20. FIRE TEST NORMAL. 2 L 7 3 4F A3WE 1999021200830 19990212 00830 NM 1999 2 12 99FDEA00053 1 19990202 A 3350 P4010020 BATTERY BOEING 727 72722C 138400F NM CABIN DISCHARGED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 107FE 19202 ENTRY DOOR EMERGENCY LIGHT BURNED OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ON FORWARD ENTRY DOOR. SYS OP ER CK GOOD IAW FEDEX MM 33-50-0. 2 L 7 3 4F A3WE 1999021200831 19990212 00831 NM 1999 2 12 99FDEA00054 1 19990209 A 2612 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM FIRE DETECTION MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 209FE 22931 WARNING LIGHT & WARN BELL WENT OFF. RED TABS PERF SYS TEST GOOD. 5TH REPEAT GRIPE. R&R ENG FIRE CONTROL UNIT,LOOP,ENG SENSING ELEMENT AT FIREWALL PER 26-11-000-5,26-11-002-5,26-11-012-4. OPS CK NORM. 2 L 7 3 4F A3WE 1999021200832 19990212 00832 1999 2 12 99FDEA00055 2 19990209 A 7310 FUEL LINE BOEING 727 72722 1384002 NM NR 2 ENGINE INOP A FDEA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 25 149FE 19087 LOSS OF NR 2 ENG FL 310 NO ABNORM PRIOR TO LOSS. REMOVED AND REPLACED FUEL LINE BETWEEN FUEL/OIL COOLER AND P & D VALVE . RAN ENG NR 2 PER JET RUNUP HANDBOOK. 2 L 7 3 4F A3WE 1999021200833 19990212 00833 NM 1999 2 12 99FDEA00056 1 19990210 A 3230 SWITCH BOEING 727 72725 1384006 NM NLG INOPERATIVE A FDEA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SO 25 155FE 18288 NO NOSE GEAR IND IN DIM POS WHEN SEL GEAR DOWN. REMOVED AND REPLACED S96 NOSE LANDING GEAR LOCK SWITCH REF THE FX72ING GEAR LOCK PINS. 2 L 7 3 4F A3WE 1999021200834 19990212 00834 NM 1999 2 12 99UAL900004 1 19990103 A 7830 6F10177504 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENG TR FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7251U 21398 TAKEOFF ABORTED AT APPROXIMATELY 90 KNOTS DUE TO NR 2 ENGINE REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL. *S/D* BAD STOW SWITCH. REPLACED STOW SWITCH. 2 L 7 3 4F 4 F A3WE E2EA 1999021200835 19990212 00835 1999 2 12 99UAL900065 4 19990129 A 3442 TR UNIT COLLINS 6225122103 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RADAR MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 996UA 22456 WEATHER RADAR DISPLAY WAS INCONSISTENT. *S/D* WEAK MESSAGE DURING SYSTEM TEST. REPLACED TRANSCEIVER TO CORRECT FOR 80 MILE RANGE. ALL GREEN RETURNS, OPS CHECK OK. 2 L 7 2 4F 4 F A16WE E2EA 1999021200836 19990212 00836 NM 1999 2 12 99UAL900066 1 19990130 A 3510 17343920 MASK HYDRAFLOW 17343920 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LEAKING A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 513UA 24810 DIVERTED TO ORD DUE TO DECREASING CREW OXYGEN PRESSURE. *S/D* THE HOSE TO THE OBSERVER OXYGEN MASK BOX WAS REPLACED BE CAUSE IT WAS FOUND LEAKING. 2 L 7 2 4F 4 F RT A2NM E17NE 1999021200837 19990212 00837 EU 1999 2 12 99UAL900067 1 19990129 A 2121 FAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E & E COMPT FAILED A UALA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 WP 29 416UA 479 VENT EXTRACT FAN BLOWER ECAM MESSAGE. CREW REPORTED SLIGHT VIBRATION IN COCKPIT AND SMOKE FROM AVIONICS COMPARTMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 1999021200838 19990212 00838 NE 1999 2 12 99UAL900068 2 19990201 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DETERIORATED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 655UA 1503 25393 724668 NR 2 ENGINE, MULTIPLE STALLS AT TAKEOFF. DIVERTED TO LHR. *S/D* ENGINE EXPERIENCED A GROUPE 3 SURGE EVENT. GROUPE 3 SU RGES ARE THE RESULT OF EXCESSIVE BLADE TIP CLEARANCES IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. ENGINE WAS RE MOVED FOR HIGH PRESSURE COMPRESSOR REFURBISHMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999021200839 19990212 00839 NM 1999 2 12 99UAL900069 1 19990202 A 2780 VALVE WATERMAN 1121S10100 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE LE FLAP FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 990UA 4186A 21980 LOST A SYSTEM HYDRAULIC QUANTITY AND PRESSURE AFTER GEAR EXTENSION AND DURING FLAP OPERATION. *S/D* FOUND THE FLAP FLOW LIMITING VALVE LEAKING. THIS UNIT WAS LEAKING BECAUSE THE BODY SEPARATED INTERNALLY. THE UNIT CONTAINS A FLOW RING WHICH FAILED DUE TO FATIGUE. THE UNIT ALSO HAD SEVERE EROSION IN A METERING ORIFICE HOLE. THE VALVE WAS REPLACED PER MM 2 7-53-03, OPS CHECK OK. 2 L 7 2 4F 4 F A16WE E2EA 1999021200840 19990212 00840 WP 1999 2 12 99UAL900070 1 19990201 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LAVATORY INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1844U 48260 EEL LIGHTING INOP AT MID LT LAV. REPLACED EEL LIGHT ASSEMBLY, OPS CHECK OK. 2 L 7 3 4F 4 F A22WE E23EA 1999021200841 19990212 00841 NE 1999 2 12 99UAL900071 2 19990203 A 7230 BLADE ABLE CORPORA 10607047 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENG COMP LACK OF LUBE A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 390UA 16 24665 MODERATE AIRFRAME VIBRATION FELT MAINLY IN THE FRONT OF THE AIRCRAFT AFTER FLAP AND GEAR RETRACTION. *S/D* AIRFRAME VI BRATION CONDITIONAL INSPECTIONS AND VIBRATION INSPECTIONS OF THE NR 1 ENGINE WERE ACCOMPLISHED. ALL FLIGHT CONTROLS WER E WITHIN INSERVICE LIMITS. NR 1 ENGINE REQUIRED A FAN BLADE LUBE. THE EQUIPMENT COOLING AUTOMATIC OUTFLOW VALVE WAS RE PLACED AS A PRECAUTION. OP CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999021200842 19990212 00842 NM 1999 2 12 99UAL900072 1 19990202 A 5270 189915 SENSOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR OUT OF ADJUST A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 935UA 26663 FORWARD CARGO DOOR WARNING LIGHT. *S/D* MECHANIC SUSPECTS FOD IN THE FORWARD PIT MAY HAVE CAUSED INDICATION PROBLEM. A DJUSTED DOOR SENSOR TARGET TO CORRECT POSITION. OPERATIONS CHECK ACCOMPLISHED ON DOOR WARNING SYSTEM CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999021200843 19990212 00843 1999 2 12 99UAL900073 4 19990202 A 2210 SC470037 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE YAW DAMPER LEAKING A UALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 29 430UA 568 HYDRAULIC FLUID LEAKING FROM RUDDER AREA. *S/D* YAW DAMPER ACTUATOR SEAL WAS LEAKING HYDRUALIC FLUID. REPLACED THE YA W DAMPER ACTUATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 1999021200844 19990212 00844 NM 1999 2 12 99UAL900075 1 19990203 A 2130 S212W3019 SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE AFT PRESS BLKHD TORN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 794UA 26936 FLIGHT RETURNED TO DEN, UNABLE TO MAINTAIN CABIN ALTITUDE AT CRUISE. *S/D* THE BOOT, REF: (P/N S212W301-9), IPC 36-12- 04-005, ITEM 155) AT THE PENETRATION OF THE APU DUCT INTO THE AFT DOME OF FUSELAGE, WAS FOUND TORN IN THE SEAM. FURTHER EXAMINATION OF THE BOOT REVEALED THAT THE STEEL RING (INSIDE THE BOOT) SNAPPED AT THE WELD. THE BOOT WAS REPLACED ACCO RDING AND THE A/C WENT TO REVENUE SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999021200845 19990212 00845 NE 1999 2 12 99UAL900076 2 19990202 A 7532 04P2310 SOLENOID BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE STICKING A UALA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 29 776UA 793 793 26937 222033 NR 2 ENGINE EXPERIENCED COMPRESSOR STALL SEVERAL TIMES DURING DESCENT FROM FLIGHT LEVEL 40.5 TO 24.0. *S/D* SURGES, WH ICH WERE RECOVERABLE, WERE ATTRIBUTED TO THE 2.9 STABILITY BLEED VALVE NOT OPENING WHEN COMMANDED. REPLACED 2.9 BLEED C ONTROL SOLENOID (P/N 04P23-10), DUE TO STICKING INTERMITTENTLY ON STABILITY SIDE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999021200846 19990212 00846 NM 1999 2 12 99UAL900077 1 19990203 A 3340 1431 TRANSFORMER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT WING FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 7465U 21919 ALL NAVIGATION LIGHTS ARE INOPERATIVE. AIRPLANE RESTRICTED TO DAYLIGHT OPERATION ONLY. *S/D* REPLACED TRANSFORMER T16 . 2 L 7 3 4F 4 F A3WE E2EA 1999021200847 19990212 00847 1999 2 12 99UAL900079 4 19990118 A 2564 TUBE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLIDE/RAFT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 409UA 462 MR25612-016 SLIDE/RAFT TOP TUBE SEAM FAILED DURING PROOF TEST. MECHANIC WAS LOWERING PRESSURE IN TOP TUBE FROM 4.4 PSI TO 2.2 PSI. SEAM SEPARATED (6 FT) AT APPROXIMATELY 2.8 PSI. 2 L 7 2 4F 4 F RT A28NM E40NE 1999021200848 19990212 00848 1999 2 12 99UAL900080 4 19990203 A 2564 62421107 TUBE AIR CRUISERS 62771105 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SLIDE/RAFT TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 770UA 0103 26925 DURING FLAT FIRING OF DOOR 1L SLIDE RAFT (P/N 62771-105) (S/N 0103) AT SHOP OVERHAUL, SLIDE FAILED TO RETAIN PRESSURE. F OUND SERIES OF SCUFFED AREAS RESULTING IN FOUR TEARS (HALF-INCH LENGTH) ON THE BOTTOM OF THE SLIDE RUNWAY SUPPORT LOG (C ROSS TUBE). SLIDE PREVIOUSLY REWORKED TO ACCOMPLISH VENDOR SERVICE BULLETIN SB777-107-25-2 ON 7/11/97. *S/D* VENDOR R EPORTED THAT HOLES WERE POSSIBLY CAUSED DURING PROCESSING OF THE SLIDE AT THE VENDOR AT PREVIOUS VISIT TO ACCOMPLISH SER VICE BULLETIN SB777-107-25-2. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999021200849 19990212 00849 NE 1999 2 12 99UAL900081 2 19990204 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 643UA 1827 25093 724698 NR 1 ENGINE COMPRESSOR STALL. THROTTLE TO IDLE CLEARED STALL. *S/D* THIS ENGINE EXPERIENCED A GROUP 3 SURGE EVENT. G ROUP 3 SURGES ARE THE RESULT OF EXCESSIVE BLADE TIP CLEARANCES IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. THIS ENGINE WAS REMOVED FOR HIGH PRESSURE COMPRESSOR REFURBISHMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999021200850 19990212 00850 1999 2 12 99UAL900087 4 19990206 A 2564 24D3005291 TUBE AIR CRUISERS D30080103 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL SLIDE RAFT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1835U 1436 1816 47967 SLIDE/RAFT FAILED AIR RETENTION TEST DUE TO SEAM SEPARATION IN TUBE ASSEMBLY. *S/D* SEAM SEPARATION IN INFLATABLE TUBE ASSEMBLY. UNIT IS BEYOND ECONOMICAL REPAIR AND WAS SCRAPPED. 2 L 7 3 4F 4 F A22WE E23EA 1999021200851 19990212 00851 1999 2 12 99UAL900088 4 19990201 A 2564 24D3005291 TUBE AIR CRUISERS D30080103 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL SLIDE RAFT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1835U 1405 1742 47967 SLIDE/RAFT FAILED AIR RETENTION TEST DUE TO SEAM SEPARATION IN TUBE ASSEMBLY. *S/D* SEAM SEPARATION IN INFLATABLE TUBE ASSEMBLY. UNIT IS BEYOND ECONOMICAL REPAIR AND WAS SCRAPPED. 2 L 7 3 4F 4 F A22WE E23EA 1999021200852 19990212 00852 1999 2 12 99UAL900090 4 19990201 A 2564 24D3005291 TUBE AIR CRUISERS D30080103 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL SLIDE RAFT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1834U 1428 1815 47966 SLIDE/RAFT FAILED AIR RETENTION TEST DUE TO SEAM SEPARATION IN TUBE ASSEMBLY. *S/D* SEAM SEPARATION IN INFLATABLE TUBE ASSEMBLY. UNIT IS BEYOND ECONOMICAL REPAIR AND WAS SCRAPPED. 2 L 7 3 4F 4 F A22WE E23EA 1999021200853 19990212 00853 WP 1999 2 12 ABXA9900085 1 19990127 A 5320 37558442 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1240 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 EXFOLIATED BATHTUB FITTING AT STATION 1240, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-2492 7MR. 2 L 7 4 4F 4A25 1999021200854 19990212 00854 WP 1999 2 12 ABXA9900086 1 19990127 A 5320 37558442 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1260 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 EXFOLIATED BATHTUB FITTING AT STATION 1260, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-2492 1. 2 L 7 4 4F 4A25 1999021200855 19990212 00855 WP 1999 2 12 ABXA9900087 1 19990127 A 5320 37558422 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1200 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CORRODED BATHTUB FITTING AT STATION 1200, LONGERON 29 LEFT. REPLACED FITTING IAW ABX REA D853-249279 AND DWG 93755842. 2 L 7 4 4F 4A25 1999021200856 19990212 00856 WP 1999 2 12 ABXA9900088 1 19990127 A 5320 37558421 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 EXFOLIATED BATHTUB FITTING AT LONGERON 29 LEFT, STATION 1220. REPLACED FITTING IAW ABX REA D853-24927 AND DC8 SRM 51-1- 21D. 2 L 7 4 4F 4A25 1999021200857 19990212 00857 WP 1999 2 12 ABXA9900089 1 19990127 A 5320 27558421 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1260 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 BATHTUB FITTING AT STATION 1260, LONGERON 30 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-21D, DWG 3755842 AND ABX REA D853- 249271. 2 L 7 4 4F 4A25 1999021200858 19990212 00858 WP 1999 2 12 ABXA9900090 1 19990123 A 5312 564660816 BKHD INTERCOSTAL DOUG DOUG DC8 DC863 302198A WP BS 1540 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CRACKED INTERCOSTAL ON AFT BULKHEAD, STATION 1540 RIGHT. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5646608. 2 L 7 4 4F 4A25 1999021200859 19990212 00859 WP 1999 2 12 ABXA9900091 1 19990123 A 5311 SR0853000861 FRAME DOUG DOUG DC8 DC863 302198A WP BS 1600 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CORROSION ON STATION 1600 FRAME, LOWER FLANGE, BETWEEN LONGERONS 34 LEFT AND 34 RIGHT. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999021200860 19990212 00860 NM 1999 2 12 ABXA9900080 1 19990208 A 3350 1000679 BATTERY PACK BOEING 767 767200 1385120 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 767AX 22785 FLIGHT DECK EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 1999021200861 19990212 00861 NM 1999 2 12 DHL99742002 1 19990209 A 7331 8TJ95EAB3 POWER SUPPLY 2G14R14 BOEING 727 727225 1384077 NM NR 1 FUEL FLOW FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 742DH S80 21290 ENGINE NR 1 EPR FLUCTUATED BY .04 TO .05 ON CLIMBOUT AND CRUISE AND FUEL FLOW FLUCTUATED BY 50 TO 100 PPH. REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER PER 727 MM 71-11-11. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY PER MM. GROUND R AN A/C, ALL ENGINE PARAMETERS NORMAL. 2 L 7 3 4F A3WE 1999021200862 19990212 00862 WP 1999 2 12 RRXA99105 1 19990206 A 2910 LINE DOUG DC8 DC873F 302199F WP NR 2 ENGINE BROKEN A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 796FT 46104 LOSS OF HYDRAULIC FLUID JUST PRIOR TO INITIAL DESCENT INTO BOSTON. FOUND HYD LINE ON NR 2 ENG HYD PUMP BROKEN. REMOVED AND REPLACED HYD LINE. RAN ENG IAW EWA RUN UP HANDBOOK. SYS OPS CKS AND LEAK CKS OK. 2 L 7 4 4F RT 4A25 1999021200863 19990212 00863 1999 2 12 RRXA99106 4 19990209 A 3425 1784775142 INDICATOR DOUG DC8 DC871F 302199D WP NR 1 ADI FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 8079U 45947 AT ROTATION ON T/O, CAPTS GYRO AND F/D FLAGS DISPLAYED ON CAPTS VERT GYRO. NO PITCH UP INDICATION GYRO FLAGS RETRACTED IN LEVEL FLIGHT THEN INTERMITTANT THERE AFTER. REMOVED AND REPLACED CAPTS ADI IND, OPS CK OF SYS OK IAW DC-8 MM CH 34. 2 L 7 4 4F RT 4A25 1999021200864 19990212 00864 NM 1999 2 12 SWAA990196 1 19990131 A 2120 AIR DIST BOEING 737 7375H4 138449D NM CARGO COMPT ODOR A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 501SW 24178 AT GATE NOTED VERY CAUSTIC FUMES IN FWD B/B, BURNED EYES AND THROAT. INSPECTED FWD CARGO BIN FOR EVIDENCE OF A SPILL, N ONE NOTED. CLEANED AREA FOR PRECAUTION, APPLIED VENTILATION AS REQUIRED FOR ODOR. 2 L 7 2 4F RT A16WE 1999021200865 19990212 00865 NM 1999 2 12 SWAA990197 1 19990201 A 3040 SWITCH BOEING 737 7373H4 1384600 NM COCKPIT OUT OF POSITION A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 320SW 23341 DURING CRUISE, SMELLED AND SAW WHITE SMOKE COMING FROM F/O NR 3 WINDOW AREA. SHUT OFF F/O'S FWD AND SIDE WINDOW HEAT SW ITCHES, SMOKE STOPPED. ALSO, FOUND GALLEY C/B TRIPPED ON P18-3 PANEL ROW B. CHECKED UNDER P5 OVERHEAD PANEL, CHECKED A LL RT SIDE WINDOWS AND HEAT CONNECTORS, REPOSITIONED SWITCH ON NR R5 WINDOW, RELAMPED RT SIDE C/B. INSPECTED LIGHT WITH CORRECT BULB, ACC OPS CK NORMAL IAW M/M. 2 L 7 2 4F RT A16WE 1999021200866 19990212 00866 NM 1999 2 12 SWAA990198 1 19990201 A 2170 COALESCER BOEING 737 7375H4 138449D NM CABIN CONTAMINATED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 525SW 26567 ODOR NOTED IN CABIN, BECAME MORE PRONOUNCED AFTER ENGINE START. ODOR BEST DESCRIBED AS BURNED TOAST, UNABLE TO DETERMIN E SOURCE OF ODOR. CHANGED LT WATER SEPARATOR AND RT SEPARATOR BAG AS PER M/M. RAN ENGINES AT POWER WITH A/C PACKS BOTH ON, NO NOTICEABLE ODOR IN CABIN OR COCKPIT. 2 L 7 2 4F RT A16WE 1999021200867 19990212 00867 1999 2 12 SWAA990199 4 19990201 A 2565 1061323478 SLIDE BOEING 737 7373H4 1384600 NM L1 & L2 DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED CHECK, FOUND L1 AND 2 SLIDE PRESSURES LOW. REMOVED AND REPLACED BOTH SLIDES PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999021200868 19990212 00868 NM 1999 2 12 SWAA990200 1 19990201 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 727, 941, 965 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 727, 772, 941 AND 965. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021200869 19990212 00869 NM 1999 2 12 SWAA990201 1 19990204 A 3020 176257 VALVE BOEING 737 7373H4 1384600 NM NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 626SW 27702 AIR RETURN DUE TO NR 2 ENGINE ANTI-ICE VALVE LIGHT FLICKERING AS IF INTRANSIT. LANDED WITHOUT INCIDENT. REMOVED AND RE PLACED VALVE, REGULATOR AND SYSTEM CHECKED OK. 2 L 7 2 4F RT A16WE 1999021200870 19990212 00870 NM 1999 2 12 SWAA990202 1 19990204 A 3020 176257 VALVE BOEING 737 7373H4 1384600 NM NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 626SW 27702 ON CLIMBOUT, NR 2 ENGINE ANTI-VALVE POSITION LIGHT WENT FROM DIM TO BRIGHT AND REMAINED BRIGHT (ANTI-ICE VALVE LIGHT). A IRCRAFT RETURNED TO PHX. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE VALVE PER M/M, OPS CKS GOOD. REMOVED AND REPLACED N R 2 ENG ANTI-ICE VALVE PER MM, OPS CHECKS GOOD PER MM (P/N 172625-7) (S/N 546) OFF, (S/N 293C). 2 L 7 2 4F RT A16WE 1999021200871 19990212 00871 NM 1999 2 12 SWAA990203 1 19990202 A 3350 20121A BATTERY BOEING 737 7372H4 138448C NM EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED SC CHECK, FOUND MID CABIN CEILING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK AND POWE R SUPPLY PER M/M, OP'S GOOD. 2 L 7 2 4F A16WE 1999021200872 19990212 00872 NM 1999 2 12 SWAA990204 1 19990204 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED IN LOWER AFT CORNER APPROX .375 INCH. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021200873 19990212 00873 NM 1999 2 12 SWAA990205 1 19990204 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 980 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCH AT BS 980 S25. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021200874 19990212 00874 NM 1999 2 12 SWAA990206 1 19990203 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED SC CHECK, FOUND BS 1016 BULKHEAD CRACKED NEAR S6L. REPAIRED PER SWA RA 1-353-2005. 2 L 7 2 4F RT A16WE 1999021200875 19990212 00875 NM 1999 2 12 SWAA990207 1 19990203 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 825 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 825, RBL 7.5. REPAIRED PER SWA RA 1-353-2008. 2 L 7 2 4F RT A16WE 1999021200876 19990212 00876 NM 1999 2 12 SWAA990208 1 19990203 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 328, ON FWD FLANGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021200877 19990212 00877 NM 1999 2 12 SWAA990209 1 19990203 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 773. REPAIRED PER SWA RA 1-353-2009. 2 L 7 2 4F RT A16WE 1999021200878 19990212 00878 NM 1999 2 12 SWAA990210 1 19990203 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED BC1 CHECK, FOUND A .125 INCH CRACK IN NR 6 SLAT LOWER T/E SKIN 18 INCHES FROM ACTUATOR. REPAIRED PER S WA RA 1-357-0634. 2 L 7 2 4F RT A16WE 1999021200879 19990212 00879 NM 1999 2 12 SWAA990211 1 19990203 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 939 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 939, AT A21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999021200880 19990212 00880 NM 1999 2 12 SWAA990212 1 19990203 A 5210 WEB BOEING 737 7372H4 138448C NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR WEB CRACKED AT FWD LOWER CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999021200881 19990212 00881 NM 1999 2 12 SWAA990213 1 19990202 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FWD FLANGE TOP SIDE OF FLOORBEAM BS 328, RBL 42,5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021200882 19990212 00882 NM 1999 2 12 SWAA990214 1 19990203 A 5754 SKIN BOEING 737 7372H4 138448C NM NR 3 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT HAD A CRACK, STOP DRILL AT OUTBOARD AUX TRACK CUTOUT PAST STOP DR ILL. REPAIRED CRACK PER RA NR 1-257-0063. 2 L 7 2 4F A16WE 1999021200883 19990212 00883 NM 1999 2 12 SWAA990216 1 19990204 A 3350 TERMINAL BOEING 737 7373H4 1384600 NM ROW 10 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 10 LT OVERHEAD BIN. TIGHTENED LOOSE TERMINAL ON LIG HT ASSY, OPS CK GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999021200884 19990212 00884 NM 1999 2 12 SWAA990217 1 19990206 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 370SW 26597 DURING SCHEDULED CHECK, FOUND R2 DOOR EMERGENCY LIGHT (INSIDE) AND L2 OUTSIDE EMERGENCY LIGHT AND LAST 6 FLOOR EMERGENCY LIGHTS TURN OFF AFTER APPROX 10 SEC. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT AFT ENTRY LIGHT POSITION, OPS CHEC K GOOD. 2 L 7 2 4F RT A16WE 1999021200885 19990212 00885 NM 1999 2 12 SWAA990218 1 19990206 A 3397 WIRE BOEING 737 7373H4 1384600 NM ROW 12-17 BROKEN A SWAA K NONE L NO TEST CR CRUISE 1 SW 07 628SW 27703 EMERGENCY EXIT LIGHTS ROW 12-17 INOP DUE TO BROKEN WIRE DISCOVERED IN FLIGHT. REPAIRED FLOOR TRACK LIGHTING PER M/M. 2 L 7 2 4F RT A16WE 1999021200886 19990212 00886 NM 1999 2 12 SWAA990220 1 19990206 A 2150 CONNECTOR BOEING 737 7372H4 138448C NM RT PACK FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 062SW 22060 CABIN WOULD NOT HOLD PRESSURIZATION DURING CLIMBOUT. RETURNED TO BWI AND MADE AN UNEVENTFUL LANDING. REPAIRED CANNON P LUG ON RT A/C PACK VALVE PER M/M. PRESSURIZATION AND A/C SYS OPS CHECKED OK. 2 L 7 2 4F A16WE 1999021200887 19990212 00887 NM 1999 2 12 SWAA990222 1 19990207 A 5330 SKIN BOEING 737 7375H4 138449D NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED 1/4D CHECK, FOUND FWD GALLEY DOOR HINGE CUTOUT HAS .5 INCH CRACK IN FUSELAGE SKIN OF LOWER CUTOUT. VER IFIED WITH HFEC AND MARKED END OF CRACK. REPAIRED PER DALFORT XEA X2-53-236. 2 L 7 2 4F RT A16WE 1999021200888 19990212 00888 NM 1999 2 12 SWAA990223 1 19990207 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 500 & 540 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CORROSION DAMAGE AT BS 540, 500C, 500D AT S28L. REPAIRED PER SWA RA 1-353-2 015. 2 L 7 2 4F RT A16WE 1999021200889 19990212 00889 NM 1999 2 12 SWAA990224 1 19990207 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CORROSION BULGING DAMAGE AT BS 727 AT S14R. REPAIRED PER SWA RA 1-353-2014. 2 L 7 2 4F RT A16WE 1999021200890 19990212 00890 NM 1999 2 12 SWAA990225 1 19990207 A 5320 STRAP BOEING 737 7373H4 1384600 NM E & E COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM STRAPS CRACKED IN E & E COMPT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021200891 19990212 00891 NM 1999 2 12 SWAA990226 1 19990207 A 5320 SHEAR TIE BOEING 737 7372T4 1384492 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND BS SHEAR TIE CRACKED BETWEEN S14 AND 15R. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1999021200892 19990212 00892 NM 1999 2 12 SWAA990227 1 19990207 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AT BS 727 TO 947, LBL 3. SPLICED IN NEW SECTION PER BOEING SRM . 2 L 7 2 4F A16WE 1999021200893 19990212 00893 NM 1999 2 12 SWAA990228 1 19990207 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN SIDE CHORD CRACKED AT BS 178, WL 195. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999021200894 19990212 00894 NM 1999 2 12 SWAA990229 1 19990207 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, PERFORMED FUSELAGE SKIN LAP JOINT REPAIR AT BS 360 TO 540 AT S10L. REPAIRED PER TRAMCO ACO 67 17-53. 2 L 7 2 4F A16WE 1999021200895 19990212 00895 NM 1999 2 12 SWAA990230 1 19990207 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 453/202 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 453, BELOW S26R AND BS 202, BELOW SKIN LAP. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1999021200896 19990212 00896 NM 1999 2 12 SWAA990231 1 19990207 A 5320 FRAME BOEING 737 7372T4 1384492 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CARGO DOOR FRAME CRACKED AT BS 492, RBL 36. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1999021300001 19990213 00001 EU 1999 2 13 MALA976335 1 19990129 A 3260 BULB SAAB SF340 340B 7860101 EU GEAR HANDLE FAILED A MALA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 15 451XJ 451 LEFT AND RIGHT GEAR LIGHTS DIDN'T ILLUMINATE WITH GEAR DOWN, NO CONFIG WARNING. AIRCRAFT LANDED WITHOUT INCIDENT. MAIN TENANCE RELAMPED LEFT AND RIGHT MAIN LANDING GEAR DOWN AND LOCK LIGHTS. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999021900041 19990219 00041 EU 1999 2 19 MALA976341 1 19990207 A 2560 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DISLODGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 508XJ E2317 SLIDE ON MAIN PASSENGER ENTRY DOOR FELL OUT WHEN DOOR WAS OPENED. MAINTENANCE REPLACED PAX DOOR SLIDE, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999021900042 19990219 00042 EU 1999 2 19 MALA976342 1 19990207 A 2131 CONTROLLER BAC 146 AVRO146RJ85A 1500097 EU CABIN FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 501XJ E2208 DURING CLIMB, CABIN HI ALT WARNING CAME ON AND MASTER WARNING CHIMED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED P RESSURE CONTROLLER, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999021900043 19990219 00043 EU 1999 2 19 MALA976343 1 19990107 A 3350 SIGN SAAB SF340 340B 7860101 EU ROW 6A LOOSE A MALA K NONE O OTHER CR CRUISE 1 GL 15 9CJ 224 EXIT SIGN OVER SEAT 6A FELL. MAINTENANCE RESECURED SIGN, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021900044 19990219 00044 EU 1999 2 19 MALA976344 1 19990207 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 991XJ 091 RT ENGINE FIRE WARNING CAME ON INFLIGHT, T HANDLE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED FI RE SENSE LOOP, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021900045 19990219 00045 EU 1999 2 19 MALA976345 1 19990207 A 2450 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU LT AVIONICS TRIPPED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 444XJ 444 LT AVIONICS BUS DEAD AND CONFIG WARNING LIGHT PROBLEM. AIRCRAFT RETURNED TO DTW. MAINTENANCE RESET CIRCUIT BREAKER, AL L CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021900046 19990219 00046 1999 2 19 MALA976346 2 19990205 A 7261 SEAL SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 103XJ 340A103 DURING FLIGHT, RECEIVED RT ENG OIL PRESSURE LOW LIGHT. AIRCRAFT DIVERTED TO DAYTON. MX FOUND BB AXIS SEALS LEAKING SEV ERELY CAUSING THE LOW PRESSURE. 2 L 7 2 4T RT A52EU 1999021900047 19990219 00047 NM 1999 2 19 K3HA990010 1 19990209 A 2913 5509801 HYDRAULIC PUMP BOEING 727 727225 1384077 NM NR 3 ENGINE FAILED A K3HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 25 353PA 20622 SYSTEM A FAILURE INFLIGHT. FOUND NR 1 ENGINE HYDRAULIC PUMP FAILED (CASE LEAK). REPLACED NR 1 PUMP PER MM 29-11-33 AND CHECKED AND REPLACED NR 1 ENGINE CASE DRAIN FILTER (P/N 7577741) AS PRECAUTIONARY. NO CONTAMINATION FOUND. SERVICED H YDRAULIC SYSTEM, BLED AIR FROM SYSTEM, RESERVICED. RAN ENGINE NR 1 OPS AND LEAK CHECKED NORMAL. 2 L 7 3 4F A3WE 1999021900048 19990219 00048 NM 1999 2 19 K3HA990011 1 19990210 A 2150 VALVE BOEING 727 727225 1384077 NM RT PACK OUT OF POSITION A K3HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 8880Z 21453 UNABLE TO CONTROL PRESSURIZATION DURING CLIMB IN ALL MODES. FOLLOWED ABNORMAL PROCEDURES PER FLIGHT MANUAL BUT CABIN CO NTINUED TO CLIMB. FOUND RIGHT PACK WATER SEPARATOR PLENUM AND CHECKED VALVE COCKED AND MIS-ALIGNED CANNISTER GASKET MIS SING A SECTION. REPOSITIONED AND INSTALLED NEW PACKING, CHECKED PNEUMATIC SYSTEM PER MM 36-12-01. NO DEFECTS NOTED. G ROUND RAN ENGINES, OPS CHECK OK PER MM 21-31-00. 2 L 7 3 4F A3WE 1999021900049 19990219 00049 EA 1999 2 19 JBXA9900067 1 19990210 A 3250 16650101 TILLER CNDAIR CL600 CL6002B19 EA NLG STEERING FAILED A JBXA K NONE O OTHER IN INSP/MAINT 1 SO 05 578ML 7270 NOSE WHEEL STEERING TILLER WILL NOT CENTER. REMOVED AND REPLACED NOSE WHEEL STEERING TILLER ASSY IAW AMM 32-51-00, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1999021900050 19990219 00050 NM 1999 2 19 CALA9900119 1 19990209 A 3230 VALVE BOEING 737 737724 NM LT MLG INOP A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 13718 28937 THE LT MLG INADVERTENTLY DEPLOYED IN FLIGHT AFTER DEPARTING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHO UT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LG CONTROL VALVE IAW MM 32-31-61, PAGE 401. LEAK AND OPERATIONAL CHE CKS WERE GOOD. A LEFT UPLOCK TEST WAS PERFORMED IAW MM 32-32-31 AND AN EMERGENCY EXTENSION WAS PERFORMED IAW MM 32-34-0 0 AND ALL CHECKED NORMAL. AN EVALUATION FLIGHT WAS COMPLETED WITH NO DISCREPANCIES. 2 L 7 2 4F RT A16WE 1999021900051 19990219 00051 WP 1999 2 19 CALA9900120 1 19990208 A 5743 SUPPORT DOUG DC10 DC1030 3023501 WP RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND THE RT MLG CYLINDER SUPPORT FRAME CORRODED IN ATTACHMENT BOLT HOLES. REPAIRED IAW ECRA 5743-01013. 2 L 7 3 4F A22WE 1999021900052 19990219 00052 WP 1999 2 19 CALA9900121 1 19990208 A 5220 DOOR DOUG DC9 DC932 3022066 WP LT EMER EXIT OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 THE LT AFT OVERWING EMERGENCY EXIT DOOR FAILED UNLOCK FORCE TEST. THE LATCH BAR SCREWS WERE ADJUSTED TO OBTAIN THE REQU IRED FORCE TO UNLOCK THE EXIT DOOR IAW MM 52-21-0, PAGE 504. 2 L 7 2 4F A6WE 1999021900053 19990219 00053 NM 1999 2 19 CALA9900122 1 19990209 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 344-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 344 TO 360. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INST ALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999021900054 19990219 00054 NM 1999 2 19 QXEA9900287 1 19990208 A 5210 HANDLE DHAV DHC8 DHC8102 2809003 NM PAX DOOR DIRTY A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 824PH 157 PDX- MAIN CABIN DOOR HANDLE IN CABIN IS HARD TO OPERATE. MAINTENANCE CLEANED THE SEAL CONTACT AREA FOR THE TOP OF THE M AIN CABIN DOOR. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999021900055 19990219 00055 NM 1999 2 19 P5CA9900151 1 19990208 A 3240 4308DA3 VALVE BOEING 747 747283B 1384867 NM NR 2 BRAKE SYST MALFUNCTION A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 921FT 21575 DURING TAXI, CAPT FOUND RIGHT SIDE BRAKES INOP WITH EITHER BRAKE SYSTEM 4 OR 1 SELECTED. ALL HYD PRESS IND NORMAL (3,00 0 LBS). PROBLEM REMAINS WITH ANTI-SKID ON OR OFF. SELECTED BRAKE SYS TO RES BRAKES (SYS 2) FULL BRAKES CAME ON WITHOUT TOUCHING BRAKE PEDALS. REMOVED RT NORMAL SYSTEM BRAKE METERING VALVE. INSTALLED IN RT RESERVE. BRAKE METERING VALVE IN THE NORMAL POSITION. NORMAL SYSTEM OPS CHECK NORMAL PER MM 32-41-03. REMOVED RES BRAKE VALVE AND INSTALLED NEW VALV E, OPS SYSTEM CHECK NORMAL. NO LEAKS IAW MM 32-41-14. 2 L 7 4 4F A20WE 1999021900056 19990219 00056 NE 1999 2 19 P5CA9900152 2 19990208 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 1 FAILED A P5CA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 WP 23 852FT 19757 662503 NR 1 ENGINE SHUT DOWN DUE TO STEADY STATE STALL AFTER DESCENDING FROM 370 TO 350. ATTEMPTED TO RESTART AT 350 AND 280, UNSUCCESSFUL. LAST START WAS AT 0050Z, WINDMILL TIME 1 HOUR AND 33 MIN. N1-30 PERCENT, N2-21 PERCENT, OIL PRESSURE 15 PSI, FL 280, IAS 295. INSPECTED FUEL FILTER, NO DEFECTS. CHECKED EVC AND CONDITION MOTOR, NO DEFECTS. GROUND START OP S CHECK GOOD. ALSO, COMPARED TO NR 4 ENG, ALL MATCH. OPS CHECK GOOD PER MM 73-23-00. 2 L 7 4 4F 4 F A20WE E20EA 1999021900057 19990219 00057 NM 1999 2 19 P5CA9900153 1 19990205 A 5320 STRAP BOEING 747 747122 1384872 NM BS 1241 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BS 1241 RIGHT SIDE SPLICE STRAP FOUND CRACKED AT FWD AND AFT HOLE OF STRINGER 18R. REPAIRED PER SERVICE BULLETIN 53-228 3. 2 L 7 4 4F A20WE 1999021900058 19990219 00058 NM 1999 2 19 P5CA9900154 1 19990205 A 5312 BULKHEAD SPLICE BOEING 747 747122 1384872 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BULKHEAD BS 1480 LEFT AND RIGHT SIDE FOUND CRACKS IN SPLICE FITTING. REPAIRED SPLICE FITTING CRACKS PER HX RS 53-43-340 21 AND BOEING SB 747-53A-2390. 2 L 7 4 4F A20WE 1999021900059 19990219 00059 NM 1999 2 19 P5CA9900155 1 19990205 A 5730 SKIN BOEING 747 747122 1384872 NM WS 1315 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON RIGHT WING LOWER SKIN STA 1315. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999021900060 19990219 00060 NM 1999 2 19 P5CA9900156 1 19990205 A 5753 CHORD BOEING 747 747122 1384872 NM RT TE MIDFLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT WING INBOARD MID FLAP LOWER CHORD FOUND CORROSION. REPAIRED PER SRM 51-40-04. 2 L 7 4 4F A20WE 1999021900061 19990219 00061 NM 1999 2 19 P5CA9900157 1 19990210 A 5311 FRAME BOEING 747 747122 1384872 NM BS 360 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 MAIN DECK BS 360R STRINGER 24R FOUND CRACK IN FRAME. REPAIRED PER SRM 53-12-00 AND HX RS 531234010. 2 L 7 4 4F A20WE 1999021900062 19990219 00062 NM 1999 2 19 P5CA9900158 1 19990210 A 5753 PANEL BOEING 747 747122 1384872 NM RT TE MIDFLAP DAMAGE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT INBOARD MID FLAP AFT BOTTOM PANEL FOUND DAMAGE. REPAIRED PER SRM 51-40-05. 2 L 7 4 4F A20WE 1999021900063 19990219 00063 NM 1999 2 19 P5CA9900159 1 19990210 A 5753 PANEL BOEING 747 747122 1384872 NM RT TE MIDFLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT WING INBOARD MID FLAP AFT LOWER PANEL FOUND DAMAGED. REPAIRED PER SRM 51-41-08. 2 L 7 4 4F A20WE 1999021900064 19990219 00064 NM 1999 2 19 P5CA9900160 1 19990210 A 7110 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 ENGINE LEFT SIDE FAN COWL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999021900065 19990219 00065 NM 1999 2 19 P5CA9900161 1 19990210 A 7110 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 LEFT SIDE FAN COWL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999021900066 19990219 00066 NM 1999 2 19 P5CA9900162 1 19990205 A 5730 SKIN BOEING 747 747122 1384872 NM WS 440-1390 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 SURFACE CORROSION FOUND ON LEFT WING UPPER SURFACE WS 440 - WS 1390. REPAIRED PER SRM 51-10-01 AND HXRS 57-25-3 4017. 2 L 7 4 4F A20WE 1999021900067 19990219 00067 NM 1999 2 19 P5CA9900163 1 19990205 A 5414 SKIN BOEING 747 747122 1384872 NM NR 1 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 1 PYLON OUTBOARD LOWER SPAR SKIRT PATCH INNER AND OUTER SKIN DAMAGED. REPAIRED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1999021900068 19990219 00068 NM 1999 2 19 P5CA9900164 1 19990205 A 2760 CONTROL CABLE BOEING 747 747122 1384872 NM NR 11 SPOILER WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 11 SPOILER CONTROL CABLE FOUND WORN AT DRUM ASSEMBLY. REPLACED PER MM 20-11-05. 2 L 7 4 4F A20WE 1999021900069 19990219 00069 NM 1999 2 19 P5CA9900165 1 19990205 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT INBOARD FOREFLAP ASSY INBOARD LOWER SURFACE FOUND DELAMINATION. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999021900070 19990219 00070 NM 1999 2 19 P5CA9900166 1 19990205 A 5321 FLOOR BOEING 747 747122 1384872 NM BS 520-600 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BS 520 TO 600 LBL 47 FLOOR PANEL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999021900071 19990219 00071 NM 1999 2 19 P5CA9900167 1 19990205 A 5321 FLOOR BOEING 747 747122 1384872 NM BS 540-600 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BS 540 TO 600 LBL 28 FLOOR PANEL FOUND DELAMINATED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999021900072 19990219 00072 NM 1999 2 19 P5CA9900168 1 19990205 A 5311 FRAME BOEING 747 747122 1384872 NM BS 380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 MAIN DECK STA 380 SRINGER 25R FOUND FRAME CRACKED. REPAIRED PER SRM 53-12-00 AND HX RS 53-12-34011. 2 L 7 4 4F A20WE 1999021900073 19990219 00073 NM 1999 2 19 P5CA9900169 1 19990205 A 2760 CONTROL CABLE BOEING 747 747122 1384872 NM NR 2 SPOILER WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT WING NR 2 SPOILER CONTROL CABLE WORN AT NR 3 AND NR 4 CONTROL DRUM AREA. REPLACED PER MM 20-11-03. 2 L 7 4 4F A20WE 1999021900074 19990219 00074 NM 1999 2 19 P5CA9900170 1 19990205 A 5414 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 PYLON LEFT EXTERNAL SKIN CRACKED AT LOWER CUTOUT AREA. REPAIRED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1999021900075 19990219 00075 NM 1999 2 19 P5CA9900171 1 19990205 A 5320 FRAME BOEING 747 747122 1384872 NM L5 DOORWAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION ON L5 DOOR FRAME ASSY AFT CUTOUT. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999021900076 19990219 00076 NM 1999 2 19 P5CA9900172 1 19990205 A 5280 65B1166837 DOOR BOEING 747 747122 1384872 NM LT MLG DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT OUTBOARD STRUT DOOR FOUND DELAMINATED. REPLACED DOOR PER MM 32-14-05. 2 L 7 4 4F A20WE 1999021900077 19990219 00077 NM 1999 2 19 P5CA9900173 1 19990205 A 5311 FRAME BOEING 747 747122 1384872 NM BS 520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION AT BS 520-540 UPPER DECK STRINGER 44L. REPAIRED PER SRM 53-10-05. 2 L 7 4 4F A20WE 1999021900078 19990219 00078 NM 1999 2 19 P5CA9900174 1 19990205 A 5400 SPAR BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 4 PYLON MIDSPAR CRACKED AND DEFORMED UNDER HYD S/O VALVE. REPAIRED PER SRM 54-10-03. 2 L 7 4 4F A20WE 1999021900079 19990219 00079 NM 1999 2 19 P5CA9900175 1 19990205 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 520-540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION ON SEAT TRACK ON UPPER DECK BS 520 TO 540. REPAIRED PER SRM 51-10-05. 2 L 7 4 4F A20WE 1999021900080 19990219 00080 NM 1999 2 19 P5CA9900176 1 19990205 A 3233 FITTING BOEING 747 747122 1384872 NM LT MLG ACTUATOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT SUPPROT FITTING FOR LEFT WLG ACTUATOR SUPPORT FOUND CRACKED. REPAIRED PER SRM 51-10-01 AND SB 747 53A2245. 2 L 7 4 4F A20WE 1999021900081 19990219 00081 NM 1999 2 19 P5CA9900177 1 19990205 A 3232 65B270844 FITTING BOEING 747 747122 1384872 NM RT MLG DOOR ACT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT WING LANDING GEAR DOOR ACTUATOR SUPPORT FITTING FWD INTERNAL KEEL BEAM FITTING FOUND CRACKED. REPLACED PER SRM 51-10 -01 AND BOEING SB 747 53A2242. 2 L 7 4 4F A20WE 1999021900082 19990219 00082 NM 1999 2 19 P5CA9900178 1 19990205 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 360 & 380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BS 360 TO BS 380 STRINGER 26R CHORD CRACKED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999021900083 19990219 00083 NM 1999 2 19 P5CA9900179 1 19990129 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 WING CENTER TANK FRONT SPAR SUPPORT STIFFENER T BRACKET FOUND CRACKED AT BS 1000 RBL10. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999021900084 19990219 00084 NM 1999 2 19 P5CA9900180 1 19990129 A 5320 JAMB BOEING 747 747122 1384872 NM L5 DOORWAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 SURFACE CORROSION FOUND ON MAIN DECK L5 DOOR CUTOUT. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999021900085 19990219 00085 NM 1999 2 19 P5CA9900181 1 19990129 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1500 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND CRACK ON FRAME AT BS 1500 STR 21L. REPAIRED PER SRM 51-30-01. 2 L 7 4 4F A20WE 1999021900086 19990219 00086 NM 1999 2 19 P5CA9900183 1 19990129 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 880 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND CRACKED SHEAR TIE BRACKET AT BS 880 S10L. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1999021900087 19990219 00087 NM 1999 2 19 P5CA9900184 1 19990129 A 5311 FRAME BOEING 747 747122 1384872 NM BS 380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND CRACK IN FRAME AT BS 380 STR 24L. REPAIRED PER SRM 53-12-00 AND HKRS 5312 340011. 2 L 7 4 4F A20WE 1999021900088 19990219 00088 NM 1999 2 19 P5CA9900185 1 19990129 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1500 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND CRACKED FRAME AT BS 1500 STR 21R. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999021900089 19990219 00089 NM 1999 2 19 P5CA9900186 1 19990129 A 5330 SKIN BOEING 747 747122 1384872 NM BS 740-1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION FOUND ON STA 740 TO STA 1000 LAP JOINT AT S12L. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999021900090 19990219 00090 NM 1999 2 19 VNAA9902002 1 19990206 A 2130 22260A20201 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 434JS 50757 3665 3051 THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A CPCS MISCOMPARE WARNING MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE P RESSURIZATION CONTROL PANEL, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-31-01. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999021900091 19990219 00091 NM 1999 2 19 VNAA9902003 1 19990207 A 3060 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP HEAT DIRTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 429JS 85384 35285 3043 THE AIRCRAFT RETURNED TO THE FIELD FOLLOWING A LEFT HAND PROPELLER HEAT FAIL WARNING MESSAGE. MAINTENANCE INSPECTED THE PROPELLER HEAT SYSTEM AND REPLACED THE 17VE PANEL AND CLEANED THE NP SENSOR CANNON PLUG CONNECTORS. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999021900092 19990219 00092 WP 1999 2 19 TWAA9902301 1 19990206 A 5320 FRAME DOUG DC9 DC932 3022066 WP SERVICE DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING CHECK-C MAINT, FOUND LOWER AFT CORNER OF SERVICE DOOR FRAME, OUTSIDE SKIN, WITH 1 INCH CRACK FROM FASTENER HOLE E DGE OF FRAME TO HOLE AND COMES OUT OF HOLE SRO207, 4 INCH UP FROM LONGERON 18R. STARTS AT EDGE OF FRAME. REPAIRED CRAC K PER ARA 15866. 2 L 7 2 4F A6WE 1999021900093 19990219 00093 NM 1999 2 19 TWAA9902302 1 19990207 A 5754 SKIN BOEING 767 767205 1385121 NM NR 5 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C, MAINTENANCE FOUND NR 5 L/E SLAT INBD TOP DELAMINATED 3 INCH BY 3 INCH. REMOVED DELAMINATED SKIN AND INS TALLED FILLER AND METAL HOT BOND REPAIR PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1999021900094 19990219 00094 WP 1999 2 19 TWAA9902303 1 19990208 A 5711 SPAR DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND RT WING WITH .375 INCH LONG CRACK IN REAR SPAR UPPER CAP AT UPPER OTBD HOLE AT CENTER FL AP HINGE OTBD ATTACH BOLT AT APPROX 1130 TO 1230 O'CLOCK POSITION. BLENDED AREA PER SRM 57-01, FIG 1. INSTALLED DOUBLE R AND FILLER PER ARA 16062. 2 L 7 2 4F A6WE 1999021900095 19990219 00095 WP 1999 2 19 TWAA9902304 1 19990208 A 5711 SPAR DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND RT WING WITH APPROXIMATELY .625 INCH CRACK IN REAR SPAR UPPER CAP AT UPPER INBD HOLE AT CENTER HINGE INBD ATTACH BOLT, APPROXIMATELY 10 TO 12 O'CLOCK POSITION. STOP DRILLED CRACK AND INSTALLED DOUBLER AND FI LLER PER ARA 16062. 2 L 7 2 4F A6WE 1999021900096 19990219 00096 WP 1999 2 19 AT0099104 1 19990119 A 5543 TRIM TAB DOUG DC9 DC932 3022066 WP RUDDER OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL. RUDDER TRIM TAB DOES NOT HAVE MINIMUM CLEARANCE AT TOP END PER DC9 MM 27-20-1 PG 602. TRIMMED TOP OF TRIM TAB TO 5/32 TO COMPLY WITH MM 27-20-0 PG 603, TREATED, AND PRIMED IAW DC9 SRM 51-10-3, 55-01 PG 1, AND RES NR 99236. 2 L 7 2 4F A6WE 1999021900103 19990219 00103 WP 1999 2 19 AT9900103 1 19990109 A 5311 99196182N FRAME DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A CRACK AT MAIN FRAME STA 718 RUNNING THROUGH 2 EA FASTENERS IN THE FORWARD INMEDIATE POCKET. REMOVED FITTING, DRILLED UP NEW FITTING, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-30- 1, 51-30-2, 51-30-5, MM 25-22-0, AND RES NR 9924 E/O 12-5311-29-B1044. 2 L 7 2 4F A6WE 1999021900104 19990219 00104 WP 1999 2 19 AT9900105 1 19990110 A 5512 SKIN DOUG DC9 DC932 3022066 WP RT VERT STAB CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SHEDULED INSPECTION AT AERO CORP, FL, FOUND RIGHT SIDE OF UPPER VERTICAL STABILIZER HAS CRACKED AND GOUGED SKIN AT STA 2 40 BELOW AFT BANANA FAIRING ATTACH POINTS. BLENDED RIGHT HAND VERTICAL STABILIZER. REMOVED AND FABRICATED NEW SKIN, TR EATED, PRIMED, SEALED AND INSTALLED IAW DC9 SRM 55-31-0, 51-10-3, 55-01 FIG. I, AND RES NR 99186. 2 L 7 2 4F A6WE 1999021900105 19990219 00105 WP 1999 2 19 AT9900106 1 19990109 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 889-899 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION ON INTERNAL DOUBLER AT STA 889-899 L-23L AFT CARGO COMPARMENT. R EMOVED FASTENERS TO GAIN ACCESS AND REMOVED CORRODED PORTION OF DOUBLER. ALODINE, PRIMED AREA, REINSTALLED NEW FASTENER S AS REQUIRED IAW DC9 SRM 53-04 FIG 38, 53-31-0 FIG 7 SHEET 2 AND 3 ITEM 8, AND RES NR 9942. 2 L 7 2 4F A6WE 1999021900106 19990219 00106 WP 1999 2 19 AT9900107 1 19990107 A 5320 THRESHOLD DOUG DC9 DC932 3022066 WP PAX DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT ENTRY THRESHOLD HAS SEVERAL ENLONGATED HOLES, ALSO E/E COMPARTMENT FLOORBOARD THRESHOLD WITH SURFACE CORROSION AROUND FASTENERS ON UNDERSIDE AND ENLONGATED HOLES. FABRICATED, HEAT TREATE D AND INSTALLED NEW THRESHOLDS IAW DC9 SRM 51-10-4, 51-10-2A, AND RES NR 99196. 2 L 7 2 4F A6WE 1999021900107 19990219 00107 WP 1999 2 19 AT9900108 1 19990106 A 5753 590043503 VANE DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LEFT FLAP VANE ACCESS PANELS 1529A, 1533A, 1544A, 1543A, 1518A, 1521A A ND THE LEFT WING OUTBOARD VANE CORRODED AND SEVERAL RIVETS POPPED THROUGH OUT INTERNAL CAVITIES AS VIEW THROUGH ACCESS O PENNINGS 1544A AND 1543A AT UPPER VANE SURFACE. REMOVED AND REPLACED LEFT WING FLAP VANE ACCESS PANEL, INSTALLED AND OP S CHECKED GOOD IAW DC9 SRM 51-30-1, 51-30-0, 57-00, AND MM 27-51-3. 2 L 7 2 4F A6WE 1999021900108 19990219 00108 WP 1999 2 19 AT9900109 1 19990108 A 2760 5913877503 PULLEY DOUG DC9 DC932 3022066 WP NR 2 SPOILER CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT WIND NR 2 SPOILER PULLEY QUADRANT HAS PITTING CORROSION ON TOP FORWARD AFT BOLT THROUGH HOLE. CHEMICALLY REMOVED CORROSION, REMOVED AND REPLACED INBOARD SPOILER PULLEY BRACKET, RIG CHECK CO MPLIED WITH ON SPOILER SYSTEM IAW DC9 MM 27-61-2, 27-61-0, AND SRM 51-10-3. 2 L 7 2 4F A6WE 1999021900109 19990219 00109 WP 1999 2 19 AT9900110 1 19990110 A 5321 1A419011 PANEL DOUG DC9 DC932 3022066 WP BS 351-503 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND FORWARD PIT FLOOR PANELS AT STA 351-503, FORWARD PIT AFT BULKHEAD LEFT AND RIGHT PANEL, FORWARD CARGO PIT FLAP VALVE AT STA 595 L-29-30, AND FORWARD CARGO FLOOR SUPPORT AT STA 218-237 WITH CORROS ION, ELONGATED HOLES AND MISDRILLED HOLES. CUT, DRILLED, TRIMMED, FABRICATED, DEBURRED, ALODINE AND PRIMED PANELS, FLOO R SUPPORT, WEB, AND REINSTALLED FLAP VALVE IAW DC9 SRM 51-04-4, 53-21-0 FIG 7A, 51-10-4, 51-10-3, 51-20-2, 51-10-2 PAGE 2, 51-10-1, AND MM 21-32-8. FLAP VALVE P/N OFF 5713641-5, FLOOR SUPPORT P/N 1A-41829-1, PANEL P/N 1A-41838-1. 2 L 7 2 4F A6WE 1999021900110 19990219 00110 WP 1999 2 19 AT9900111 1 19990122 A 5312 99155863N BLKHD ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND INTERCOSTAL TEE ANGLE AT STA 996 PRESSURE BULKHEAD Z-34 CORRODED. REMOVED AND REPLACED TEE ANGLE, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 51-10-4, AND 53- 01. 2 L 7 2 4F A6WE 1999021900111 19990219 00111 WP 1999 2 19 AT9900112 1 19990110 A 5320 ANGLE DOUG DC9 DC932 3022066 WP GALLEY DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND G-2 AND G-4 GALLEY LEFT AND RIGHT INBOARD LOWER CORNER ON SECTION 502, 503 AND 504 DOOR, ANGLE, AND BOTTOM TRASH COMPARTMENT CORRODED. MECHANICALLY REMOVED CORROSION, FABRICATED NEW DOOR, CORNER ANGLE, TRIM PIECES AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-1, 51-10-2, 51-10-3, 51-10-4, AND NORDSKOG OHM 25-38-338. 2 L 7 2 4F A6WE 1999021900112 19990219 00112 WP 1999 2 19 AT9900113 1 19990118 A 5321 1A418791 FLOOR DOUG DC9 DC932 3022066 WP BS 965-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 806AT 47379 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CABIN FLOORBOARD PANEL AT STA 680-756, STA 965-996, AND FLOOR BOARD NR 97 C ORRODED, MISSING CHAFFED STRIP, ELONGATED HOLES, RIVET HEADS PULLING UP, AND MISSING INSULATION. FABRICATED NEW FLOORBO ARD, HAT CHANNELS, INSULATION, TRIMMED, DEBURRED, ALODINE, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 53-21-0 FIG. 5C, 51 -10-2, 51-10-3, 51-30-2, 51-20-0, AND DPS 3.40-21 AND 3.40-18. HAT CHANNEL P/N OFF 1A-41889-1. 2 L 7 2 4F A6WE 1999021900113 19990219 00113 WP 1999 2 19 AT9900114 1 19990212 A 3350 CM3171BPEGPL BULB DOUG DC9 DC932 3022066 WP TAIL CONE EXIT FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 812AT 47359 DURING A B CHECK, FOUND THE TAIL CONE EMERGENCY EXIT INOPERATIVE. RELAMPED TAIL CONE EMERGENCY EXIT LIGHT IAW MM 33-53- 0, OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1999021900114 19990219 00114 NM 1999 2 19 AT9900115 1 19990213 A 3397 WIRE BOEING 737 7372L9 1384497 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 FOUND A SECTION OF EMERGENCY FLOOR PATH LIGHTING COVER PULLED-UP AND WIRE BROKEN AT ONE EACH LIGHT SOCKET. SPLICE WIRE AT LIGHT SOCKET AND SECURED TRACK COVER IAW MM 33-00. 2 L 7 2 4F RT A16WE 1999021900115 19990219 00115 WP 1999 2 19 AT9900116 1 19990211 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 389-598 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LOWER RIGHT FUSELAGE SKIN FROM STA 389 TO STA 598 L-18R TO L-26R WITH D ENTS IN DIFFERENT AREAS. REMOVED AND REPLACED FUSELAGE SKIN IAW DC9 SRM 51-30-2, 51-30-1, AND RES NR 99193. 2 L 7 2 4F A6WE 1999021900116 19990219 00116 NM 1999 2 19 AT9900117 1 19990105 A 5330 PANEL BOEING 737 737214 138446R NM WING DAMAGE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND PANEL 6403R HAS LEADING EDGE SCREW HOLE DAMAGE FROM WIND EROSION. PANEL HA S 15 PERCENT FLAME SPRAY MISSING. CLEANED PANEL AND REMOVED PAINT. APPLIED FIBERGLASS OVERLAY AND ASTRO STRIKE AND SEA LED IAW B737 SRM 51-40-9 AND DC9 SRM 51-70-9 AND RES NR 99116. CONTINUITY CHECK GOOD. 2 L 7 2 4F A16WE 1999021900117 19990219 00117 NM 1999 2 19 AT9900118 1 19990111 A 5330 SKIN BOEING 737 737214 138446R NM R-1 DOORWAY DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND RIGHT SIDE FUSELAGE SKIN HAS A PREVIOUS .5 BY .75 CUT OUT, WITH FILLER INST ALLED AT FORWARD LOWER CORNER OF FORWARD GALLEY SERVICE R-1 DOOR. REMOVED FORWARD COVER PLATE TO FACILITATE REPAIR. FA BRICATED NEW DOUBLERS, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-10-2, 51-30-2, MM 51-20-11, AND RES NR 9947. 2 L 7 2 4F A16WE 1999021900118 19990219 00118 NE 1999 2 19 CKSA99002 2 19990101 A 7314 65B1166837 FUEL PUMP DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE FAILED A CKSA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 WP 23 813CK 45893 642298 DURING CRUISE FL 340, NR 1 ENG BEGAN TO LOSE PWR AS EVIDENCED BY DECREASING EPR AND RPM IND. APPLIED ENG AND SCOOP ANTI -ICE, EPR AND RPM'S CONTINUED TO DROP. AFTER 5 MIN RPM DROPPED TO APPROX 85 PERCENT N2. AS RPM DECREASED NR 1 FUEL PRE SS IND DROPPED BELOW 0 PSI TO APPROX -5 PSI. OPENED ALL X-FEEDS, TURNED ON ALL PUMPS, FUEL PRESS REMAINED -5 PSI. ENG RPM CONT TO DECREASE AND NR 1 ENG FLAMED OUT. PERFORMED ENG FAILURE CHKLST, ENG AND RE-LIT AND ACCEL TO IDLE. WHEN ADV ANCED THROTTLE ENGINE FLAMED OUT AND WOULD NOT RE-START. PERFORMED CHKLIST AND SECURED ENGINE AT 0937Z. R/R'D NR 1 ENG 2 STAGE FUEL PUMP IAW MM 73-10-1. LEAK AND OPS CHK NORM DURING ENG RUN IAW MM 72. REPLACED DOOR PER MM 32-14-05. 2 L 7 4 4F 4 F 4A25 1E8 1999021900119 19990219 00119 WP 1999 2 19 CALA9900123 1 19990214 A 4990 38003681 OIL SYST DOUG DC9 DC982 3022082 WP APU OVERSERVICED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 13891 49102 A MODERATE AMOUNT OF SMOKE APPEARED IN THE COCKPIT AND CABIN AFTER TAKEOFF FROM EWR WITH THE PNEUMATIC PRESSURE GAUGE RE ADING 70 PSI. THE SMOKE SLOWLY DISSIPATED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINT ENANCE INSPECTED BOTH ENGINE SADDLE STRAPS WITH NO DEFECTS NOTED. THE APU WAS FOUND OVERSERVICED WITH OIL. THE OIL WAS DRAINED AND THE APU OIL WAS RESERVICED. BOTH COALESCER BAGS WERE REMOVED AND REPLACED. BOTH ACM'S WERE INSPECTED AND FOUND PROPERLY SERVICED WITH NO LEAKS NOTED. A HIGH POWER ENGINE RUN WAS PERFORMED FOR 10 MINUTES WITH NO SMOKE OR ODOR NOTED. 2 L 7 2 4F A6WE 1999021900120 19990219 00120 WP 1999 2 19 CALA9900124 1 19990210 A 3350 41B004AD07G3 BATTERIES AEROQUALITY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHT IDENTIFIERS INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATI ON CHECKED GOOD. 2 L 7 2 4F A6WE 1999021900121 19990219 00121 NM 1999 2 19 CALA9900125 1 19990210 A 5320 ANGLE BOEING 757 757224 1384958 NM CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND FORWARD HOLD DOOR THRESHOLD ATTACH ANGLE CORRODED. THE ANGLE WAS REPLACED IAW DRAWING NR 143N5366. 2 L 7 2 4F RT A2NM 1999021900122 19990219 00122 NM 1999 2 19 CALA9900126 1 19990210 A 5753 113N280095M SKIN BOEING 757 757224 1384958 NM RT TE FLAP PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND A 2 INCH DIAMETER HOLE IN RT I/B AFT FLAP UPPER SURFACE. THE FLAP WAS REPAIRED IAW SRM 57-53-01 AND 51 -70-17. 2 L 7 2 4F RT A2NM 1999021900123 19990219 00123 NM 1999 2 19 CALA9900127 1 19990211 A 5280 113N810014 DOOR BOEING 757 757224 1384958 NM RT MLG SPLIT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND RT MLG STRUT DOOR SPLIT AT LOWER END. REPAIRED IAW SRM 51-70-03. 2 L 7 2 4F RT A2NM 1999021900124 19990219 00124 WP 1999 2 19 CALA9900128 1 19990211 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 71828 49488 INSPECTION FOUND OVERHEAD EMERGENCY LIGHTS AT THREE ROWS IN COACH SECTION WOULD NOT OPERATE. THE POWER SUPPLY WAS REMOV ED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999021900125 19990219 00125 NM 1999 2 19 CALA9900129 1 19990211 A 5754 PANEL BOEING 737 7373T0 1384582 NM NR 3 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A 1 CRACK IN LT WING NR 3 SLAT PANEL AT FASTENER I/B OF SLAT ACTUATOR. A REPAIR WAS INSTALLED IAW BOEI NG DRAWING 65C30133. 2 L 7 2 4F RT A16WE 1999021900126 19990219 00126 WP 1999 2 19 CALA9900130 1 19990211 A 3350 AD4002P BATTERIES DOUG DC9 DC982 3022082 WP ROW 7-10 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 72824 49484 INSPECTION FOUND THE AISLE EMERGENCY CEILING LIGHTS INOPERATIVE BETWEEN ROWS 7-10. THE EMERGENCY LIGHT BATTERIES WERE R EPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00, PAGE 401. 2 L 7 2 4F A6WE 1999021900127 19990219 00127 NM 1999 2 19 CALA9900131 1 19990211 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 10 TO RBL 36. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999021900128 19990219 00128 NM 1999 2 19 CALA9900132 1 19990211 A 5330 SKIN BOEING 737 7373T0 1384582 NM LT COCKPIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN OF UPPER WINDOW POST AT CAPTAIN'S NR 2 SLIDING WINDOW. A REPAIR WAS INSTALLED IAW ECRA 5330-02769. 2 L 7 2 4F RT A16WE 1999021900129 19990219 00129 NM 1999 2 19 CALA9900133 1 19990211 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 947.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 947.5, BELOW CABIN FLOOR CENTERLINE. THE INTER COSTAL WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999021900130 19990219 00130 NM 1999 2 19 CALA9900134 1 19990212 A 5753 113N300319 PANEL BOEING 757 757224 1384958 NM LT TE FLAP FRETTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND FRETTING ON LT O/B FLAP I/B UPPER SURFACE PANEL. THE PANEL WAS REPAIRED IAW ECRA 5753-01057. 2 L 7 2 4F RT A2NM 1999021900131 19990219 00131 NM 1999 2 19 CALA9900135 1 19990212 A 5754 114N4005185A PANEL BOEING 757 757224 1384958 NM NR 4 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND A 2 INCH CRACK IN NR 4 SLAT CLOSURE PANEL. THE PANEL WAS REPAIRED IAW SRM 51-70-05. 2 L 7 2 4F RT A2NM 1999021900132 19990219 00132 NM 1999 2 19 CALA9900136 1 19990212 A 5753 113N300320 PANEL BOEING 757 757224 1384958 NM RT TE FLAP FRETTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND FRETTING ON RT O/B FLAP I/B UPPER SURFACE PANEL. THE PANEL WAS REPAIRED IAW ECRA 5753-01057. 2 L 7 2 4F RT A2NM 1999021900133 19990219 00133 NM 1999 2 19 CALA9900137 1 19990212 A 3397 WIRE BOEING 727 727224 1384076 NM ROW 5-15 SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND EMERGENCY PATH SEAT MOUNTED LIGHTS INOPERATIVE FROM ROW 5 TO 15. CAPPED SHORTED WIRES AND OPERATION CH ECKED NORMAL IAW MM 33-51-00, PAGE 112. 2 L 7 3 4F A3WE 1999021900134 19990219 00134 WP 1999 2 19 CALA9900138 1 19990212 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-229 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT T CHANNEL CORRODED BETWEEN STA 160 AND 229, BL 0. THE CHANNEL WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-60-0. 2 L 7 2 4F A6WE 1999021900135 19990219 00135 WP 1999 2 19 CALA9900139 1 19990212 A 5210 FITTING DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND A 1.5 INCH CRACK IN FITTING OF FORWARD ENTRY DOOR AT UPPER AFT STOP PAD AREA. THE FASTENERS AND FITTIN G WERE REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 52-03-00, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 52-03-00, PAGE 5, 51-10-3, AND 51-10-2. INSTALLED FITTING IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999021900136 19990219 00136 WP 1999 2 19 CALA9900140 1 19990212 A 5523 5910413503 TAB DOUG DC9 DC932 3022066 WP LT ELEVATOR DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND LT ELEVATOR CONTROL TAB DELAMINATED ON UPPER SURFACE. THE LT ELEVATOR CONTROL TAB WAS REMOVED AND REPL ACED IAW MM 27-30-00 AND 27-30-3. 2 L 7 2 4F A6WE 1999021900137 19990219 00137 WP 1999 2 19 CALA9900141 1 19990212 A 5247 RIB DOUG DC9 DC932 3022066 WP APU DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND A .5 INCH CRACK IN RT APU DOOR INNER RIB. THE RIB WAS REPAIRED IAW SRM 52-01-00, FIGURE 2 AND 51-10-3. 2 L 7 2 4F A6WE 1999021900138 19990219 00138 NM 1999 2 19 CALA9900142 1 19990212 A 3610 DUCT BOEING 727 727243 138408D NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE FAILED A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 17407 21270 649071 NR 3 ENG FIRE WARNING ACTIVATED AFTER T/O FROM BWI. THE A/C WAS RETURNED TO BWI WHERE IT LANDED W/O INCIDENT. MX FOUND THE PNEUMATIC DUCT LEADING TO NR 3 NOSE COWL ANTI-ICE VALVE BLOWN. THE NOSE COWL FLANGE FITTING FOR COWL ANTI-ICE INLE T WAS ALSO BLOWN. THE PNEUMATIC DUCT WAS REMOVED AND REPLACED. THE NOSE COWL WAS ALSO REMOVED AND REPLACED IAW MM 71-1 0-21, PAGE 401-403. THE NR 3 ENG WAS RUN AND OPS CHECKED GOOD. FOUND A BROKEN CLAMP AFTER REMOVING THE OUTER SKIN OF T HE NOSE COWL. THE CLAMP BREAKAGE WAS DETERMINED TO BE THE CAUSE OF THE DUCT FAILURE DUE TO THE MOVEMENT THAT THE DUCT W AS ALLOWED AFTER THE CLAMP HAD BROKEN. THIS MOVEMENT CONCENTRATED STRESS ON A SPECIFIC LOCATION CAUSING THE DUCT TO FAI 2 L 7 3 4F 4 F RT A3WE E2EA 1999021900139 19990219 00139 NM 1999 2 19 9900466625 1 19990209 A 3232 U11985 ACTUATOR BOEING 747 747251B 1384892 NM NLG DOOR LEAKING A NWAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 625US 71457 32266 21707 DURING CRUISE (TPE), NR 1 HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. TURNED NR 1 HYDRAULIC PUMP OFF AND AIRCRAFT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED OFF THE RUNWAY TO THE GATE. REPLACED THE NOSE LANDING GEAR DOO R ACTUATOR. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999021900140 19990219 00140 WP 1999 2 19 9900479877 1 19990210 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP TAIL CONE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ALONG CATWALK IN TAILCONE SECTION INOPERATIVE. REPLACED POWE R SUPPLY AND BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999021900141 19990219 00141 WP 1999 2 19 9900489877 1 19990208 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK AND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999021900142 19990219 00142 WP 1999 2 19 9900499608 1 19990205 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CATWALK CORRODED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 608NW 47233 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED CORRODED CONNECTOR NEAR POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999021900143 19990219 00143 SO 1999 2 19 COMA9910032 1 19990213 A 2751 WARNING EMB 120 EMB120RT SO TE FLAPS ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 258CA 120247 FLAP DISAGREE WARNING AFTER TAKEOFF COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999021900144 19990219 00144 SO 1999 2 19 COMA9910033 1 19990209 A 3350 1153871 SIGN EMB 120 EMB120RT SO ROW 8 INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 463CA 1267 ROW EIGHT EXIT SIGN INOPERABLE. REPALCED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999021900145 19990219 00145 EA 1999 2 19 COMA9960067 1 19990213 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA O OTHER N FALSE WARNING LD LANDING 1 SO 01 769CA 31 7292 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999021900146 19990219 00146 EA 1999 2 19 COMA9960068 1 19990212 A 5220 HATCH CNDAIR CL600 CL6002B19 EA COCKPIT LACK OF LUBE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 759CA 7279 WATER LEAKING IN THROUGH CREW HATCH. APPLIED DC-4 GREASE TO HATCH TO STOP WATER INTRUSION. 2 L 7 2 4F RT A21EA 1999021900147 19990219 00147 EA 1999 2 19 COMA9960069 1 19990208 A 5210 601R319001 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 719CA 1069 7253 WHILE CLIMBING THROUGH 23,000, PAX DOOR LATCH CAUTION AND PAX DOOR EMERGENCY WARNING ILLUMINATED. AIRCRAFT WAS DIVERTED TO SDF AND THEN FERRIED TO CVG WHERE THE UPPER CAMS AND CAM PROX SENSOR TARGETS WERE ADJUSTED. ALSO, CHECKED RIIGGING OF ENTIRE PAX DOOR. 2 L 7 2 4F RT A21EA 1999021900148 19990219 00148 NM 1999 2 19 UPS99228673 1 19990207 A 5713 STRINGER BOEING 727 72725C 138400H NM WS 171.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:SI L-W UPPER STRINGER NR 8 IS CRACKED AT WS 171.5. REPAIRED L-WING STRINGER NR 8 UPPER IAW SRM 57-10-4 . 2 L 7 3 4F A3WE 1999021900149 19990219 00149 NM 1999 2 19 UPS99228674 1 19990114 A 5400 S DUCT BOEING 727 72725C 138400H NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:C NR 2 ENGINE S DUCT HAS 5 INCH CRACK IN THE CENTER SECTION 4 RIBS FWD OF THE PRODUCTION BREAK, LT SIDE APPRX 8:00 POSITION. REMOVED DAMAGED AREA AND PERFORMED A FILLER AND DOUBLER REPAIR PER SRM 54-10-3, SRM 51-40-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1999021900150 19990219 00150 NM 1999 2 19 UPS99228675 1 19990206 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C SEAT TRACK AT STA 760 LBL 65 WL 208 CRACKED AT O/B FLANGE. REPLACED TRACK IAW SRM 51-30-5. 2 L 7 3 4F A3WE 1999021900151 19990219 00151 NM 1999 2 19 UPS99228676 1 19990210 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CARGO COMPT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 REPLACE EMERGENCY LIGHT RECEIVER BATTERIES. REMOVED AND REPLACED BATTERIES AS REQ'D A/C IN CARGO CONFIG. 2 L 7 3 4F A3WE 1999021900152 19990219 00152 NM 1999 2 19 UPS99228677 1 19990210 A 3350 LIGHT BOEING 727 72725C 138400H NM VENTRAL STAIR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 EMERG VENTRAL STAIR PATH LIGHT INOP. T/S FOUND CONTINUITY ON WIRE FROM PINS 11 BUT FOUND NOTHING ON PINS 12 OR 13 DEFER ED ITEM PER MEL33-16-02. 2 L 7 3 4F A3WE 1999021900153 19990219 00153 NE 1999 2 19 UPS99228684 2 19990210 A 7230 COMPRESSOR BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE STALLED A IPXA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 208UP 21701 COMPRESSOR STALL PASSING FL270. MAX TEMP 620 DEGREES. ALL OTHER LIMITS NORMAL. DID SHUT DOWN OF NR 3 ENGINE. REMOVED AND REPLACED THE NR 3 ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999021900154 19990219 00154 NM 1999 2 19 UPS99228685 1 19990211 A 3350 S106 BATTERIES BOEING 727 72751C 1384015 NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:PDC ON PDC, FWD ENTRY DOOR EMERGENCY EXIT LIGHT WOULD NOT TEST. FWD ENTRY DOOR EMERGENCY EXIT LIGHT BAT TERIES REPLACED AND TESTED AS PER M/M 33-50-101. OPS CHECKED SERVICEABLE. 2 L 7 3 4F A3WE 1999021900155 19990219 00155 NM 1999 2 19 UPS99228686 1 19990127 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 740 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C, RT BS 740 SKIN (STRINGERS 17 TO 22 INCLUSIVE AREA) HOLES ARE 2ND OVERSIZE. REPAIR CARRIED OUT IAW EO 99-03-001, UPS ENGINEERING FILE NR 5310-2098. 2 L 7 3 4F A3WE 1999021900156 19990219 00156 NM 1999 2 19 UPS99228687 1 19990125 A 7120 MOUNT BOEING 727 72730C 1384009 NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C ENGINE NR 3 PITTING CORROSION ON MOUNT HOLES, FWD O/B, AFT I/B. CORROSION IN MOUNT HOLES REMOVED IAW SMRO EO 99-03-003 UPS ENGINEERING FILE NR 727-71-0077. 2 L 7 3 4F A3WE 1999021900157 19990219 00157 NM 1999 2 19 UPS99228688 1 19990125 A 7120 MOUNT BOEING 727 72730C 1384009 NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C ENGINE NR 1 PITTING CORROSION ON BIG MOUNT HOLES, SMALL HOLES OK. CORROSION ON MOUNT HOLES REMOVED IA W SMRO EO 99-03-002 REV 1 UPS ENGINEERING FILE NR 727-71-0078, BUSHINGS INSTALLED IAW SMRO EO 99-03-005 REV 1 UPS ENGINE ERING FILE NR 727-71-0078. 2 L 7 3 4F A3WE 1999021900158 19990219 00158 NM 1999 2 19 UPS99228689 1 19990130 A 5713 STRINGER BOEING 727 72730C 1384009 NM WS 629 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE:C RT WING STA 629 STR 13 FWD LUG CRACKED. REPAIR CARRIED OUT IAW UPS EO B727-5710-0314. 2 L 7 3 4F A3WE 1999021900159 19990219 00159 NM 1999 2 19 UPS99228704 1 19990212 A 3350 BATTERY PACK BOEING 727 72751C 1384015 NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 ON PDC, FWD ENTRY EEL WOULD NOT TEST. REMOVED AND REPLACED EEL BATT PACKS, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999021900160 19990219 00160 WP 1999 2 19 UPS99828671 1 19990120 A 5320 3610130501 FITTING DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, LONGERON 21R FWD END FITTING IS CORRODED BEYOND LIMITS AT FS 70. REMOVED AND REPLACED FITTING IAW S RM 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999021900161 19990219 00161 WP 1999 2 19 UPS99828672 1 19990123 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 341.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3 RT, WING L/E LWR SKIN BUTT SPLICE DOUBLER HAS A 30 CRACK AT XFS 341.5. REPAIRED DOUBLER IAW DH SK713 -051. 2 L 7 4 4F RT 4A25 1999021900162 19990219 00162 WP 1999 2 19 UPS99828678 1 19990117 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, MAIN CABIN FRAME CRACKED AT STA 200 L20R. FAB REPAIR ANGLE AND FILLER IAW REO 06149 AL AND PRI IAW D C8 SRM 51-1-8 INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999021900163 19990219 00163 WP 1999 2 19 UPS99828679 1 19990114 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 857-869 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, FS 857-869 INTERCOSTAL CORROSION AT RADIUS 1ST INTERCOSTAL INBD OF SKIN FITTING. REPLACED INTERCOSTA L WITH NEW INTERCOSTAL. 2 L 7 4 4F RT 4A25 1999021900164 19990219 00164 WP 1999 2 19 UPS99828680 1 19990107 A 5350 FILLET DOUG DC8 DC873F 302199F WP KEEL BEAM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, FILLET PNL 191AA HAS CORROSION AND BARE METAL A-708 RACK NR 25. FAB -3 PANEL, -5 AND -7 FILLERS IAW DAC DWG 5701940. ALODINED AND PRIMED PANEL L AND FILLER IAW DC8 SRM 51-1-8. INSTALLED FILLERS IAW DC8 SRM 51-1- 21 AND DC8 SRM 71-2-2. 2 L 7 4 4F RT 4A25 1999021900165 19990219 00165 WP 1999 2 19 UPS99828681 1 19990106 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, AFT PIT LT TUNNEL FS 1220 AT L27L INSIDE TQ BOX HAS CRACKED FITTING. REMOVED DAMAGED FRAME SECTION F AB REPLACEMENT FRAME PER DAC DWG 9754 921. INSTALLED PER DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999021900166 19990219 00166 WP 1999 2 19 UPS99828682 1 19990204 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, STA 70, L20L REPAIR ON FRAME TOP CORNER CRACKED, GOUGED ON LWR AFT EDGE REPAIRED IAW REO-06184. 2 L 7 4 4F RT 4A25 1999021900167 19990219 00167 WP 1999 2 19 UPS99828683 1 19990106 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 781-798 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D MAIN CABIN, CORROSION ON INSIDE OF UPPER LIP ON LONG 12R STA 781-798. REMOVED CORROSION INTERCOSTAL A ND REPLACED WITH NEW INTERCOSTAL. 2 L 7 4 4F RT 4A25 1999021900168 19990219 00168 WP 1999 2 19 UPS99828690 1 19990105 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 680-702 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, MAIN CABIN CORROSION ON LONGERON 19R INTERCOSTAL STA 680-702. REPLACED CORROSION INTERCOSTAL WITH NE W INTERCOSTAL. 2 L 7 4 4F RT 4A25 1999021900169 19990219 00169 WP 1999 2 19 UPS99828691 1 19990107 A 5320 T CAP DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, AFT PIT FS 1040 T-CAP AT L33L CORRODED UNDER NUT PLATE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. FAB REPAIR ANGLE DOUBLER AND FILLER IAW DAC 08-53-0229. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTA LLED IAW DAC 08-53-0229. 2 L 7 4 4F RT 4A25 1999021900170 19990219 00170 WP 1999 2 19 UPS99828692 1 19990106 A 5712 BULKHEAD FITTING DOUG DC8 DC873F 302199F WP WS 408 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, LWR BULKHEAD TEE FITTING CRACKED INSIDE NR 1 MAIN TANK AT XW408 FROM STR 63 TO CORNER FITTING AT FRON T SPAR, VERIFIED WITH HFEC. RECEIVED NEW FITTINGS AND INSTALLED IAW DC8 SRM 51-1-28. 2 L 7 4 4F RT 4A25 1999021900171 19990219 00171 WP 1999 2 19 UPS99828693 1 19990106 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 50 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, STA 50, LBL 29 INTERCOSTAL CORROSION INBD LWR SIDE. REMOVED CORROSION, INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL. REMOVED CORROSION FOUND OUT OF LIMITS, FABBED REPAIR DOUBLER, ALODINED AND PRIMED INSTALLED REPAIR DO UBLER. 2 L 7 4 4F RT 4A25 1999021900172 19990219 00172 WP 1999 2 19 UPS99828694 1 19990105 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, AFT ACC STA 1690 L22R END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1 -20D. 2 L 7 4 4F RT 4A25 1999021900173 19990219 00173 WP 1999 2 19 UPS99828695 1 19990104 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1890-1916 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, LT MOST FWD TAIL CONE SKIN STA 1890-1916 IS CORRODED. FAB NEW SKIN IAW DAC DW3G 5644500 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999021900174 19990219 00174 WP 1999 2 19 UPS99828696 1 19990104 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1890-1916 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, RT MOST FWD TAIL CONE SKIN STA 1890-1916 IS CORRODED. FAB NEW SKIN IAW DAC DWG 5644500 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999021900175 19990219 00175 WP 1999 2 19 UPS99828697 1 19990104 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1916-1951 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, LT CENTER TAIL CONE SKIN STA 1916-1951 IS CORRODED. FAB NEW SKIN IAW DC8 DWG 5644500 ALODINED AND PR IMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999021900176 19990219 00176 WP 1999 2 19 UPS99828698 1 19990104 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1916-1951 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, RT CENTER TAIL CONE SKIN STA 1916-1951 IS CORRODED. FAB NEW SKIN IAW DC8 DAC DWG 5644500 ALODINED AN D PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999021900177 19990219 00177 WP 1999 2 19 UPS99828699 1 19990102 A 5220 BRACKET DOUG DC8 DC873F 302199F WP EMERGENCY EXIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, CORROSION BEHIND EMERGENCY STRAP BRACKET LT OVERWING ENTRY. REMOVED CORROSION BRACKET AND INSTALLED NEW BRACKET. REMOVED CORROSION OUT OF LIMITS AFT BLEND. GEN RFTS, MAT ID 7075T6.063. OK TO FAB. FABBED, OK TO ALODIN E AND PRIME. ALODINED AND PRIMED AND INSTALLED. 2 L 7 4 4F RT 4A25 1999021900179 19990219 00179 WP 1999 2 19 UPS99828701 1 19990102 A 5220 BRACKET DOUG DC8 DC873F 302199F WP EMERGENCY EXIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, CORROSION BEHIND EMERGENCY STRAP BRACKET, LT OVERWING ENTRY. REMOVED BRACKET, FABBED NEW ONE IAW DAC DWG 5779947 AND REO 06168. INSTALLED IAW DAC DWG 5779947. 2 L 7 4 4F RT 4A25 1999021900180 19990219 00180 WP 1999 2 19 UPS99828702 1 19990212 A 2612 BULB DOUG DC8 DC873F 302199F WP NR 4 T HANDLE SHORTED A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 818UP 46108 AT FL 350, NR 4 FIRE LIGHT INDICATION COMPLETED CHECKLIST. DECLARED EMERGENCY. DID NOT FIRE THE BOTTLE. INSPECTED NR 4 ENGINE LOOP AND DUCTING, NO DEFECTED NOTED. FOUND NR 4 T-HANDLE LIGHT BULB SHORTED TO GROUND. REPOSITIOND SAME, OPS CHK GOOD PER M-M 2610-00. 2 L 7 4 4F RT 4A25 1999021900181 19990219 00181 NM 1999 2 19 UPS99228705 1 19990203 A 5520 65274096 FITTING BOEING 727 72725C 138400H NM ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, CORROSION (C55-391-30.02-01) ON ELEVATOR CENTERING UNIT SPRING FWD ATTACH FITTING AROUND FASTENER HOL ES. FITITNG OUT OF LIMITS, REMOVED OLD FITTING, INSTALLED NEW FITTING PER MM 27-30-11 AND SRM 51-30-02. 2 L 7 3 4F A3WE 1999021900182 19990219 00182 NM 1999 2 19 UPS99228706 1 19990212 A 5320 SUPPORT BOEING 727 72725C 138400H NM BS 520-540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, CORROSION ON FLOOR SUPPORT (C53-113-01.07-01) AT FWD CARGO DOOR THRESHOLD BS 520-540 RBL 21.5 WL 156. REPLACED FLOOR SUPPORT BS 510 TO BS 600 PER 727 SRM 51-30-5 AND 53-10-1. 2 L 7 3 4F A3WE 1999021900183 19990219 00183 NM 1999 2 19 UPS99228707 1 19990204 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BS 1166, LBL 20, WHERE IT ATTACHES TO AFT BULKHEAD OF AFT CARGO BAY. REMO VED CORROSION ON SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK IAW 53-10-05. 2 L 7 3 4F A3WE 1999021900184 19990219 00184 NM 1999 2 19 UPS99228708 1 19990212 A 5320 WEB BOEING 727 72725C 138400H NM BS 1225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, AFT AIR STAIR AREA, 2 CRACKS IN LIGHTENING HOLE IN TORQUE BOX RT SIDE STATION 1225. REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1999021900185 19990219 00185 NM 1999 2 19 UPS99228709 1 19990212 A 5320 WEB BOEING 727 72725C 138400H NM BS 1174 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, CORROSION ON SHEAR WEB BS 1174, RBL 45, WL 208. REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1999021900186 19990219 00186 NM 1999 2 19 UPS99228710 1 19990210 A 5315 651758866 FLOORBEAM BOEING 727 72725C 138400H NM BS 267 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, CORROSION ON FLOORBEAM UPPER CHORD AT BS 267, LBL 2, COCKPIT FLOOR. CORROSION CLEAN UP WENT BEYOND A CCEPTABLE LIMITS. REMOVED AND REPLACED FLOORBEAM UPPER CHORD. 2 L 7 3 4F A3WE 1999021900187 19990219 00187 NM 1999 2 19 UPS99228711 1 19990209 A 5312 BULKHEAD BOEING 727 72725C 138400H NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, TRANSFERRED FROM LP 266457 ITEM 3 CRACK IN PRESSURE BULKHEAD LEFT WHEEL WELL STA 870. REMOVED DAMAGE D AREA AT 870 BULKHEAD LT WHEEL WELL. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS PER SRM 53-10-9 PGS 10-11 AND SRM 51-40-2 PGS 1-6. 2 L 7 3 4F A3WE 1999021900188 19990219 00188 NM 1999 2 19 UPS99228712 1 19990209 A 5320 SHEER TIE BOEING 727 72725C 138400H NM BS 306 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON SHEER TIE IN TRUNNION TORQUE BOX AT BS 306 RBL 18 WL 148. REMOVED CO RROSION, OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-4. INSTALLED LEVELING COMPOUND IAW SRM 51- 20-4. 2 L 7 3 4F A3WE 1999021900189 19990219 00189 NM 1999 2 19 UPS99228713 1 19990209 A 5311 FRAME BOEING 727 72725C 138400H NM BS 420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C CORROSION ON SUPPORTING FRAME AT BS 420 UNDER BATTERY TRAY. TRAY ALSO HAS CORROSION AROUND MOUNTING L UG BRACKETS. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER ON FRAME PER SRM 53-10-1. TRAY AND LUG BRACKETS WERE WITHI N LIMITS, ALL PARTS REINSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999021900190 19990219 00190 NM 1999 2 19 UPS99228715 1 19990207 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, FLOORBEAM UPPER CHORD CORRODED BS 344 RBL 15 WL 208. CORROSION CLEANUP BEYOND ACCEPTABLE LIMITS. RE PAIRED FLOORBEAM PER SRM 53-10-8 FIGURE 9. 2 L 7 3 4F A3WE 1999021900191 19990219 00191 NM 1999 2 19 UPS99228717 1 19990207 A 5320 WEB BOEING 727 72725C 138400H NM BS 1225 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:C, AFT AIR STAIR AREA CRACK IN LIGHTENING HOLE IN TORQUE BOX WEB LT SIDE AT STA 1225. STOP DRILLED AND REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1999021900192 19990219 00192 NM 1999 2 19 UPS99228718 1 19990208 A 2750 65209763 FITTING BOEING 727 72725C 138400H NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE:C, TORQUE TUBE SUPPORT FITTING JUST O/B OF MAIN LANDING GEAR BEAM CORRODED AT INBD AND OTBD LOWER FASTEN ERS HOLES. REMOVED AND REPLACED L/WING O/B FLAP TORQUE TUBE SUPPORT FITTING IAW MM 27-51-131. 2 L 7 3 4F A3WE 1999021900193 19990219 00193 WP 1999 2 19 UPS99828720 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 467.897 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C RT WING L/E RIB AT 467.897 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999021900194 19990219 00194 WP 1999 2 19 UPS99828721 1 19990103 A 5720 46495972 FITTING DOUG DC8 DC871F 302199D WP WS 410 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C RT WING STA 410 FLAP HINGE CANOE FITTING SIDE BRACE FITTINGS, 2EA ARE CRACKED. REMOVED AND REPLACED F ITTINGS IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999021900195 19990219 00195 WP 1999 2 19 UPS99828722 1 19990107 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 685 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C, LT WING L/E RIB AT XFS 685.0 IS CRACKED AT THE AFT UPPER FASTENER. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999021900196 19990219 00196 NM 1999 2 19 99FDEA00057 1 19990210 A 2611 774001 SMOKE DETECTOR BOEING 727 727233 138408A NM E & E COMPT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 218FE 21101 99-0045, MAIN CARGO SMOKE IND LIGHT CAME ON FOR ZONE NR 6 FOR 30 SEC. REMOVED AND REPLACED DETECTOR NR 6 PER 727-200 MM 26-16-011-4. OPER CK GOOD. 2 L 7 3 4F RT A3WE 1999021900197 19990219 00197 EU 1999 2 19 99FDEA00058 1 19990212 A 5210 PAD AIRBUS 310 A310222 3930315 EU PAX DOOR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 421FE 342 ECAM WARNING RT FWD CABIN DOOR NOT CLOSED. INSPECTED R-1 DOOR. REMOVED AND REPLACED RUBBER PAD, CK R-1 DOOR PER MM 52- 10-20-6. NO DEFECTS FOUND, OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999021900198 19990219 00198 GL 1999 2 19 99FDEA00059 2 19990209 A 7200 ENGINE DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL NR 3 FAILED A FDEA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 25 049FE 47803 99-0047 - NR 3 ENGINE SUFFERED CATASTROPHIC FAILURE JUST AFTER ROTATION NR 3 EGT 999 DEG FOR 35 SEC. REMOVED AND REPLAC ED NR 3 ENG IAW FEC DC-10 PWRPLT WORK CARD 71T01101 UP TO ITEM 24. COMPLIED WITH (SEE AML 01224000). 2 L 7 3 4F 4 F A22WE E23EA 1999021900199 19990219 00199 EU 1999 2 19 99FDEA00060 1 19990214 A 7830 UPLOCK AIRBUS 310 A310203 EU THRUST REVERSER MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 404FE 233 DURING T/O ROLL AT APPROX 80 KTS, THE NR 1 THRUST REVERSER UNLOCK LIGHT CAME ON. REJECT T/O. 2 L 7 2 4F RT A35EU 1999021900200 19990219 00200 NM 1999 2 19 99FDEA00061 1 19990215 A 5320 69154893 WEB BOEING 727 72722 1384002 NM BS 987-990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 CORROSION (C53-113-0 1/2) ON VERTICAL WEB AND ATTACH BRACKET, BS 987 TO 990, STR 28 RT, WL 140. * S/D* REMOVED AND RE PLACED VERTICAL WEB AND ATTACH BRACKET BS 987 TO 990, STR 28 RT, WL 140 IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1999021900201 19990219 00201 WP 1999 2 19 ABXA9900092 1 19990123 A 5720 56110209 CHANNEL DOUG DOUG DC8 DC863 302198A WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED, AFT SIDE OF LANDING GEAR CUTOUT. INSTALLED REPLACEMENT CHANNEL IAW DW G 5611020 AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999021900202 19990219 00202 WP 1999 2 19 ABXA9900093 1 19990123 A 5320 46549032 GUSSETT DOUG DOUG DC8 DC863 302198A WP BS 1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 GUSSETT HAS EXFOLIATION CORROSION AT STATION 1220, LONGERON 24L. REPLACED GUSSETT IAW DC8 SRM 51-1-20D AND ABX REA D853 -24930. 2 L 7 4 4F 4A25 1999021900203 19990219 00203 WP 1999 2 19 ABXA9900094 1 19990123 A 5320 4754903 GUSSETT DOUG DOUG DC8 DC863 302198A WP BS 1240 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 GUSSETT PLATE HAD EXFOLIATION CORROSION AT STATION 1240, LONGERON 24 L. REPLACED GUSSETT IAW DWG 9755849, DC9 SRM 51-1- 20 AND ABX REA D853-24930. 2 L 7 4 4F 4A25 1999021900204 19990219 00204 WP 1999 2 19 ABXA9900095 1 19990118 A 5751 57630901 FITTING DOUG DOUG DC8 DC863 302198A WP LT AILERON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT INBOARD AILERON INBOARD HINGE FITTING WAS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999021900205 19990219 00205 WP 1999 2 19 ABXA9900096 1 19990104 A 5720 5655441 WEB DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CRACKED WEB GUSSETT INSIDE RIGHT WING LEADING EDGE BETWEEN PANELS 519C AND 520A ABOVE ANTI-ICE VALVE. REPAIRED IAW DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1999021900206 19990219 00206 WP 1999 2 19 MWEA99062 1 19990210 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 212ME 47701 FOUND AFT LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED CEILING EMERGENCY BATTER Y PACK. 2 L 7 2 4F A6WE 1999021900207 19990219 00207 WP 1999 2 19 MWEA99063 1 19990209 A 3350 6011777 BATTERY PACK DOUG DC9 DC914 3022034 WP RT NACELLE DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FOUND RIGHT EMERGENCY NACELLE LIGHT INOPERATIVE. MAINTENACNE REMOVED AND REPLACED EMERGENCY NACELLE LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1999021900208 19990219 00208 WP 1999 2 19 MWEA99064 1 19990211 A 5311 9953208501 FRAME DOUG DC9 DC914 3022034 WP BS 623 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK ON LEFT SIDE FRAME AT STATION 623. MAINTENANCE DRILLED HOLES IN -9 DOUBLER AND -23 -25 -27 SHIMS AND INSTAL LED. 2 L 7 2 4F A6WE 1999021900209 19990219 00209 WP 1999 2 19 MWEA99065 1 19990211 A 5330 59114033 SKIN DOUG DC9 DC914 3022034 WP BS 79 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK IN FUSELAGE SKIN AT FS 79. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999021900210 19990219 00210 WP 1999 2 19 MWEA99066 1 19990211 A 5330 59114034 SKIN DOUG DC9 DC914 3022034 WP BS 78 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK IN FUSELAGE SKIN AT FS 78. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999021900211 19990219 00211 WP 1999 2 19 MWEA99067 1 19990211 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 602ME 48133 THE GIRT BAR FELL OFF. MAINTENANCE RESECURED FORWARD ENTRANCE DOOR GIRT BAR. 2 L 7 2 4F A6WE 1999021900212 19990219 00212 WP 1999 2 19 MWEA99068 1 19990208 A 5241 591008411 SKIN DOUG DC9 DC914 3022034 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK ON GALLEY SERVICE DOOR LOWER AFT CORNER EXTERIOR SKIN. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999021900213 19990219 00213 NM 1999 2 19 MWEA99069 1 19990209 A 5311 5920337503 FRAME DOUG MD88 MD88 3023688 NM BS 927 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 804ME 48030 FOUND A MISDRILLED HOLE ON FRAME AT FUSELAGE 927 AT L5L. MAINTENANCE FABRICATED AND INSTALLED BUSHING AND REPAIR DOUBLE R. 2 L 7 2 4F RT A6WE 1999021900214 19990219 00214 NM 1999 2 19 DL72K990254 1 19990208 A 5330 655456719 SKIN BOEING 727 727232 1384082 NM BS 720-730 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 WHILE ACCOMPLISHING LFEC INSPECTION PER SI 4-74176-12, REV B ON THE S4R LAP JOINT, CRACK INDICATIONS WERE FOUND BETWEEN BS 640 AND BS 740. AFTER GAINING INTERNAL ACCESS AND ACCOMPLISHING THE REQUIRED HFEC INSPECTIONS; ONE CRACK WAS CONFIRM ED AT A FASTENER LOCATED AT BS 720+10 ON THE LWR ROW OF THE LWR SKIN PANEL. REPAIRED PER ERA 332735-14. 2 L 7 3 4F A3WE 1999021900215 19990219 00215 NM 1999 2 19 DL72K990255 1 19990208 A 5330 6554583125 SKIN BOEING 727 727232 1384082 NM BS 1170 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 DURING ACCOMPLISHMENT OF EO 4-69078-3AD, THE BONDED INTERNAL DOUBLER WAS DAMAGED (TOOLING DAMAGE). REPAIRED PER ERA 332 737-14. 2 L 7 3 4F A3WE 1999021900216 19990219 00216 NM 1999 2 19 DL72K990256 1 19990208 A 5532 651746356 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 A SKIN PANEL REPAIR WAS FOUND ON THE RHS VERT STAB WHICH WAS INSTALLED W/ BLIND RIVETS PER SRM. REPAIRED PER ERA 332755 -14. 2 L 7 3 4F A3WE 1999021900217 19990219 00217 NM 1999 2 19 DL757990257 1 19990205 A 5330 143N36914 SKIN BOEING 757 757232 1384965 NM BS 681 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 FUSELAGE SKIN, FS 681 STRG 19L, REPAIR FOR SKIN GOUGES. THE FUSELAGE SKIN WAS FOUND GOUGED ON THE UPPER SKIN AT THE STR INGER 19L SKIN LAP SPLICE AT FS 681. THE DAMAGED AREA OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLE R PER ER/A 366611-14, REV A. 2 L 7 2 4F RT A2NM 1999021900218 19990219 00218 NM 1999 2 19 DL72S990258 1 19990206 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 528 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 FUSELAGE SKIN, FS 528, STRG 4, REPAIR FOR SKIN CRACK. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE GAVE A CRACK I NDICATION. HFEC INTERNAL INSPECTION WAS THEN ACCOMPLISHED ALONG THE ENTIRE LENGTH OF THE PANEL WITH ONLY ONE CRACK FIND ING. THE CRACK WAS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AND WAS LOCALLY TRIMMED OUT AN REPAIRED PER B727 SRM 53- 30-3, FIG 5. 10 FASTENERS FWD AND AFT OF THE CUTOUT WERE REMOVED AN HFEC INSPECTED WITH NO CRACKS. 2 L 7 3 4F A3WE 1999021900219 19990219 00219 NM 1999 2 19 DL72K990260 1 19990209 A 5531 654233015 RIB BOEING 727 727232 1384082 NM VERT STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 CORROSION FOUND ON THE INBD FACE OF THE INBD LUG ON THE LT FIN CLOSURE RIB CLEVIS. DAMAGE REMOVED WITH A 1.6 DIA SPOTFA CE W/DEPTH OF 0.062. REWORKED PER ERA 332753-14. 2 L 7 3 4F A3WE 1999021900220 19990219 00220 NM 1999 2 19 DL72K990261 1 19990209 A 5511 65434399 SPAR BOEING 727 727232 1384082 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 WEAR WAS FOUND ON THE I/B AND O/B PIVOT LUG FACES OF THE REAR SPAR CENTER FORGIN OF THE HORIZ STAB. ADDITIONALLY CORROS ION WAS FOUND IN THE BORES OF EACH OF THE TWO LUGS. REWORKED PER ERA 332761-14. 2 L 7 3 4F A3WE 1999021900221 19990219 00221 NM 1999 2 19 DLM88990262 1 19990209 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM BS 226 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DL 49539 GROUND DAMAGE INCURRED AT FS 226 BETWEEN S17L AND S18L, THE TIME LIMITED REPAIR WAS REMOVED AT THE CURRENT VISIT. CUTOU T WAS MADE LARGER TO REMOVE ALL FASTENER HOLES FROM T/L REPAIR. REPAIRED PER ERA 271221-14, REV B. 2 L 7 2 4F RT A6WE 1999021900222 19990219 00222 NM 1999 2 19 DL72K990263 1 19990122 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1030-1050 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 AT HMV, FOUND SKIN BULGED, EXT SKIN STA 1030 TO 1050 STRINGER 28L-27L. REPLACED SKIN ON N/R 297. 2 L 7 3 4F A3WE 1999021900223 19990219 00223 NM 1999 2 19 DL76L990264 1 19990209 A 3350 BATTERY PACK 20131A BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 197DN 3557 28454 DURING MTC, FOUND THAT RT AND LT OVERWING SLIDE SQUIBS WOULD NOT TEST. REPLACED THE BATTERY PACKS FOR THE OVERWING SLID E POWER SUPPLYS. THE SQUIBS THEN TESTED NORMALLY. 2 L 7 2 4F RT A1NM 1999021900224 19990219 00224 NM 1999 2 19 DL72K990265 1 19990125 A 5341 PIN BOEING 727 727232 1384082 NM RT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 AT HMV, FOUND BOTTLE PIN CORRODED. PITTED ON AFT FACE, RUSTY ON CAFER, AND BORE IS CORRODED. MACHINED BORE TO 40501 PE R SRM 53-40-1. REMOVED ALL PER SAME AND INSTALLED. 2 L 7 3 4F A3WE 1999021900225 19990219 00225 NM 1999 2 19 DL72S990266 1 19990209 A 5520 PANEL BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 2 INCH CRACK NR 2 BALANCE BOARD CLOSE OUT PANEL, RT ELEVATOR. REPAIR PER SRM 55-20-3. 2 L 7 3 4F A3WE 1999021900226 19990219 00226 NM 1999 2 19 DL72S990267 1 19990209 A 5530 CLIP BOEING 727 727232 1384082 NM LT VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 1 IN CRACK IN LT VERT FIN SKIN TO RIB ATTACH CLIP, STA 180.600 ABOVE STR 10. REPAIR PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1999021900227 19990219 00227 NM 1999 2 19 DL72S990268 1 19990209 A 5530 RIB BOEING 727 727232 1384082 NM RT VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 VERTICAL FIN RIB CHORD CRACKED 1.25 INCH FIN STA 133.800, AT STR 8 ATTACH BOLT RT SIDE. REPAIR PER M/M 55-30-0 FIG 802. 2 L 7 3 4F A3WE 1999021900228 19990219 00228 NM 1999 2 19 DL757990270 1 19990210 A 2121 FAN 6067723 BOEING 757 757232 1384965 NM RT CABIN FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 617DL 22907 ELECTRICAL SMELL IN CABIN. REPLACED RIGHT RECIRC FAN FOR PRODUCING ODOR. 2 L 7 2 4F RT A2NM 1999021900229 19990219 00229 NM 1999 2 19 DL73K990271 1 19990210 A 5343 654654319 FITTING BOEING 737 737232 1384475 NM BS 685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 FUSELAGE RT AND LT MLG SIDE STRUT SUPPORT FITTINGS, FS 685, REPAIR FOR LUG BORE CORROSION. THE LOWER LUGS OF THE LT AND RT MLG SIDE STRUT SUPPORT FITTINGS WERE FOUND TO HAVE CORROSION IN THE LOWER LUG BORES. THE LUG BORES WERE OVERSIZED T O REMOVE THE CORROSION AND OVERSIZE BUSHINGS WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 366656-14, REV A. 2 L 7 2 4F RT A16WE 1999021900230 19990219 00230 NM 1999 2 19 DL72S990272 1 19990209 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 FUSELAGE SKIN FS 360-481, STRG 4R, SKIN LAP SPLICE REPAIR FOR CRACKED FASTENER HOLES. LFEC INSPECTION OF THE STRINGER 4 R SKIN LAP SPLICE BETWEEN FS 360-481 REVEALED CRACK INDICATIONS. HFEC INTERNAL INSPECTION CONFIRMED A TOTAL OF 4 CRACKS IN TWO SEPERATE FRAME BAYS ALONG THE LOWER ROW OF FASTENERS. THE SKIN LAP WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIR ED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 366636-14, REV B. 2 L 7 3 4F A3WE 1999021900231 19990219 00231 NM 1999 2 19 DL72S990273 1 19990209 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 FUSELAGE SKIN FS 360-481, STRG 4L, SKIN LAP SPLICE, REPAIR FOR CRACKS. EXTERNAL LFEC INSPECTION REVEALED CRACK INDICATI ONS IN THE LOWER SKIN OF THE STRINGER 4L LAP SPLICE BETWEEN FS 360-481. INTERNAL HFEC INSPECTION CONFIRMED 10 CRACKS AL ONG THE LOWER ROW OF FASTENERS IN THE LAP. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366641-14, REV B. 2 L 7 3 4F A3WE 1999021900232 19990219 00232 NM 1999 2 19 DL72S990274 1 19990209 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 FUSELAGE SKIN FS 481-681, STRG 4R SKIN LAP SPLICE REPAIR FOR CRACKS. EXTERNAL LFEC INSPECTION OF THE STRINGER 4R SKIN L AP SPLICE REVEALED CRACK INDICATIONS IN THE PANEL BETWEEN FS 481 AND 681. INTERNAL HFEC INSPECTION CONFIRMED A TOTAL OF 48 CRACKS ALONG THE LOWER FASTENER ROW OF THE LAP SPLICE IN THE LOWER SKIN. THE SKIN LAP WAS CUTOUT ALONG THE LENGTH O F THE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366653-14, REV A. 2 L 7 3 4F A3WE 1999021900233 19990219 00233 NM 1999 2 19 DL72L990275 1 19990210 A 5720 656233513 SUPPORT BOEING 727 727232 1384082 NM LT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 WING MLG SUPPORT BEAM, LT AFT ATTACH LUG, REPAIR FOR CORRODED LUG. THE AFT ATTACH LUG OF THE LT MLG SUPPORT BEAM WAS FO UND CORRODED. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG HOLE BORE AND SPOTFACING THE SURFACE OF THE LUG. THE LUG WAS REPAIRED BY INSTALLING AN OVERSIZE FLANGED BUSHING. THE REPAIR WAS ACCOMPLISHED PER ER/A 366623-14. 2 L 7 3 4F A3WE 1999021900234 19990219 00234 NM 1999 2 19 DL72W990276 1 19990210 A 5330 655457416 SKIN BOEING 727 727247 138408F NM BS 548 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 FUSELAGE SKIN FS 548, STRG 4R SKIN LAP SPLICE, CRACK REPAIR. EXTERNAL LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SHOWE D A CRACK INDICATION AT FS 548. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL LENGTH CONFIRMED ONLY ONE CRACK AT FS 548 ALONG THE LOWER FASTENER ROW OF THE LAP. THE CRACK WAS TRIMMED OUT OF THE LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM D OUBLER PER B727 SRM 53-30-3, FIG 5. THE REPAIR WAS DOCUMENTED PER ER/A 366677-14. 2 L 7 3 4F A3WE 1999021900235 19990219 00235 NM 1999 2 19 SCNA99034 1 19990209 A 3350 BATTERY BOEING 727 7272J4 1384006 NM EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED T HE BATTERIES IN THE LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999021900236 19990219 00236 WP 1999 2 19 DHL99803003 1 19990210 A 2700 CONTROLS DOUG DC8 DC873F 302199F WP LT & RT WING ICED UP A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 803DH 46123 EXCESSIVE AND RAPID REVERSAL OF TRIM, BUFFET AND PARTIAL LOSS OF CONTROL WITH A/P OFF, IAS 350 KTS AT FL 310. DECLARED EMERGENCY AND LANDED AT LHR. UPON INVESTIGATION, FOUND FLIGHT CONTROLS COVERED WITH ICE IN LAYERS, INCLUDING FLAPS, SLO TS, SPOILERS SECTIONS AND WHEEL WELL AREAS. FOUND ICE DEPOSITS ON ACTUATOR OF AILERON. RIGHT SPOILER STAYED UP WITH AI LERON CENTERED. DEICED AIRCRFT PER WINTER OPS MANUAL. AIRCRAFT CHECKS NORMAL PER MM 27-13-0, 27-61-0 AND MM 27-20-0. A LL FLIGHT CONTROLS WORK NORMAL. 2 L 7 4 4F RT 4A25 1999021900287 19990219 00287 NM 1999 2 19 TWAA9902401 1 19990214 A 3350 BULB BOEING 767 767330 NM EXTERIOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 FOUND AFT RT EXTERIOR FUSELAGE LIGHT INOPERATIVE. REPLACED LAMP. CHECK-C 2-3-99 LAX. 2 L 7 2 4F RT A1NM 1999021900288 19990219 00288 WP 1999 2 19 TWAA9902402 1 19990214 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP ROW 11 & 18 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9402W 53138 CABIN EGRESS LIGHTS WERE FOUND INOPERATIVE AT ROWS 11 AND 18. REPLACED LAMPS AT BOTH POSITIONS. CHECK-C 10-25-98 STL. 2 L 7 2 4F RT A6WE 1999021900289 19990219 00289 WP 1999 2 19 TWAA9902403 1 19990212 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP AFT OVERWING INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 989Z 47135 THE AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 6-25-98 STL. 2 L 7 2 4F A6WE 1999021900290 19990219 00290 NM 1999 2 19 AT9900119 1 19990104 A 5713 STRINGER BOEING 737 737214 138446R NM LT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LEFT WING UPPER STRINGER NR 13 HAS 3 CRACK AT RIB AT WBL 135.00. REMOVED TEMPORARY REPAIR, FABRICATED NEW REPAIR PARTS, HEAT TREATED, PRIMED, PAINTED AND INSTALLED IAW B737 SRM 57-10-4 FIG 3, 5 7-40-4 FIG 3, 51-10-6, AND RES NR 99187. 2 L 7 2 4F A16WE 1999021900291 19990219 00291 NM 1999 2 19 AT9900120 1 19990111 A 5245 DOOR BOEING 737 737214 138446R NM BS 685 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT TURBO FAN EXHAUST LOUVER DOOR HAS CORROSION AND PULLING THRU FAS TENERS AT STA 685. REMOVED AND REPLACED RIGHT EXHAUST MODULATION ASSEMBLY IAW B737 MM 21-52-91. COMPLIED WITH RES NR 9 9335 AND INSTALLED BLANK OFF PLATE AND DISCONNECTED CANNON PLUG, OPS CHECKED GOOD. 2 L 7 2 4F A16WE 1999021900292 19990219 00292 NM 1999 2 19 AT9900121 1 19990121 A 5330 SKIN BOEING 737 737214 138446R NM BS 211 MISREPAIRED A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THREE EXISTING REPAIRS RIGHT FORWARD FUSELAGE AT COCKPIT NOT REPAIRED IAW SB 737-53-111. CUT OUT EXISTING REPAIRS, FABRICATED AND INSTALLED DOUBLERS, SPLICE PLATES, AND FILLER IAW SB737-53-111 AND BOEING DRAWING 65C33596. (P/N 1A-41385-1, 2, 3 & 4) OFF. 2 L 7 2 4F A16WE 1999021900293 19990219 00293 NM 1999 2 19 AT9900122 1 19990114 A 5310 STRUCTURE BOEING 737 737214 138446R NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND SEVERAL AREAS CORRODED. THE FORWARD CARGO DOOR FRAME AT STRINGER 25R, INT ERCOASTAL FRAME AT STA 500 TO 520 RBL 25 IN THE FORWARD PIT, THE AFT CARGO AFT BULKHEAD UPPER SUPPORT STA 947 FROM L-25L TO L-25R, AND THE FLOOR SUPPORT BEAM AT STA 947. MECHANICALLY REMOVED ALL CORROSION, REMOVED, REPLACED, FABRICATED SUP PORT, STRINGER, BEAM, DOUBLER, PRIMED, TREATED, AND INSTALLED IAW B737 SRM 51-40-3, 51-30-2, 53-10-9, AND 53-10-1. STRI NGER (P/N AMS5510), SUPPORT ANGLE (P/N 1A-42748-1), INTERCOSTAL (P/N 1A-42744-1). 2 L 7 2 4F A16WE 1999021900294 19990219 00294 NM 1999 2 19 AT9900123 1 19990110 A 5347 BAC15207927178 SEAT TRACK BOEING 737 737214 138446R NM BS 328-344 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT DIFFERENT LOCATIONS. FIRST, THE LAVATORY WALL HAT SECTION AT STA 300 L-35 TO 50, SECONDLY THE SEAT TRACK IN THE CABIN AT STA 328 TO 344 BL 24 TO 75R, AND THE SIDE WALL IS CRACKED A ND CORRODED AT STA 440 TO 420 ABOVE STRINGER 26R. CHEMICALLY REMOVED CORROSION. REMOVED, REPLACED, FABRICATED, HEAT TR EATED, PRIMED ALL PARTS, AND INSTALLED IAW B737 SRM 51-20-11, 51-10-2, 51-30-2, 51-21-31, 51-10-6, AND 53-10-1. 2 L 7 2 4F A16WE 1999021900295 19990219 00295 NM 1999 2 19 AT9900124 1 19990115 A 5310 STRUCTURE BOEING 737 737214 138446R NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLIGHT DECK FLOOR BULGING AND RIVETS PULLING THROUGH. ALSO, THE NOSE WHEEL WELL AT STA 243, STRINGER 28R FRAME HAS EXFOLIATION AND THE E/E COMPARTMENT AT STA 351 STRINGER 23L WEB WITH CORRO SION. REMOVED CORROSION, FABRICATED WEB AND ANGLES, ALODINE, PRIMED, AND INSTALLED IAW B737 SRM 51-40-3 FIG 1, 51-10-2, 51-40-3, 53-10-9, 51-40-2, 51-10-6, 53-10-1. WEB (P/N 1A-42704-1) OFF. 2 L 7 2 4F A16WE 1999021900296 19990219 00296 WP 1999 2 19 AT9900125 1 19990119 A 5311 99196181N FRAME DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT MAIN FRAME LOWER FORWARD POCKET AND LOWER FLANGE IN THE WHEEL WEL L AT STA 718 CRACKED. REMOVED AND REPLACED MAIN FRAME IAW EO 12-5511-29-B1044, EO 12-5511-29-B1044, AND SB 53-131 R4. F RAME (P/N 9919619-504N) OFF. 2 L 7 2 4F A6WE 1999021900297 19990219 00297 WP 1999 2 19 IXXA9900003 1 19990216 A 2121 X207256 FAN DOUG DC8 DC862 3021970 WP LT COCKPIT FAILED A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 21CX 1037 45955 EN ROUTE FROM AJK TO AVB, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT EMITTING FROM THE LEFT RECIRCULATION FAN. THE C REW TURNED OFF THE FAN AND THE ODOR DIMINISHED. MAINTENANCE INSPECTED AND FOUND THE FAN DEFECTIVE. MAINTENANCE DEFERRE D THE LEFT RECIRCULATION FAN AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999021900298 19990219 00298 SO 1999 2 19 RAAA99E9012 1 19990213 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 230 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 FUSELAGE SKIN DAMAGED BY CARGO EQUIPMENT DURING LOADING AT DUT. A 1.5 INCH DIA HOLE AND A .75 INCH DIA HOLE FS 230 BETW EEN STR 31 AND 32. INSTALLED TEMPORARY REPAIR AND FERRIED AIRCRAFT UNPRESSURIZED TO ANC. ANC REPAIRED PER SRM 53-2-1. M-54 NR 1. 2 L 7 4 4T 4A22 1999021900299 19990219 00299 GL 1999 2 19 RAAA99E9013 2 19990214 A 7250 6847100 TURBINE ALLSN 501D13 LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 4 ENGINE FAILED A RAAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 1968R 739 501745 188C2007 501745 EN ROUTE DUT TO ANC, NR 4 ENGINE SHUT DOWN INFLIGHT DUE OIL LOSS. FOUND 1, 4TH STAGE TURBINE BLADE SEPARATED APPROX .5 INCH FROM BLADE ROOT. RTBS DENTED BUT NOT PENETRATED. REAR TURBINE BEARING OIL SUPPLY LINE BROKEN AT AFT FLANGE FITTIN G. CHANGED ENGINE PER EF 71-1-0 DUE TURBINE FAILED. 2 L 7 4 4T 4 T 4A22 E282 1999021900300 19990219 00300 NM 1999 2 19 CALA9900143 1 19990215 A 3350 BATTERY IDDAEROSPACE BOEING 727 727243 138408D NM LT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND THE LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION CHECKED GOOD. 2 L 7 3 4F RT A3WE 1999021900301 19990219 00301 NM 1999 2 19 CALA9900144 1 19990212 A 5210 140N27411 PIN BOEING 757 757224 1384958 NM R4 DOOR SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14120 27562 THE DOOR ASSIST BOTTLE BLEW DUE TO R-4 DOOR TRIGGER FORK NOT DISENGAGING AND TRIGGER FORK SHEARED AT ROLL PIN, DURING C- CHECK PASSENGER DOOR EMERGENCY MECHANISM OPERATIONAL CHECK. THE R-4 DOOR TRIGGER FORK AND ROLL PIN WERE REPLACED. OPER ATIONAL CHECK OF R-4 DOOR EMERGENCY MECHANISM WAS GOOD IAW MM 52-11-32. 2 L 7 2 4F RT A2NM 1999021900302 19990219 00302 NM 1999 2 19 CALA9900145 1 19990212 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 332 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL AT STA 332, STRINGER 10R. THE INTERCOSTAL WAS REMOVED AND A REPAIR INT ERCOSTAL AND REPAIR PARTS WERE INSTALLED IAW EA 5363-01014. 2 L 7 2 4F RT A16WE 1999021900303 19990219 00303 NM 1999 2 19 CALA9900146 1 19990212 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 344-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 344 TO 360. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999021900304 19990219 00304 NM 1999 2 19 CALA9900147 1 19990212 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 52 TO RBL 10. A NEW FLOORBEAM CAP WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999021900305 19990219 00305 WP 1999 2 19 CALA9900148 1 19990213 A 5753 5910040509 VANE DOUG DC9 DC932 3022066 WP LT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND LT WING FLAP AFT MOVEABLE VANE DENTED AND ONE SPOT WORN THROUGH AT LOWER SURFACE NEAR I/B END. THE FLA P VANE WAS REMOVED AND REPLACED IAW MM 27-51-2. 2 L 7 2 4F A6WE 1999021900306 19990219 00306 WP 1999 2 19 CALA9900149 1 19990213 A 5730 5912737501 PANEL DOUG DC9 DC932 3022066 WP LT WING DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND THE LT WING UPPER T/E FIXED PANEL DEBONDED WITH SURFACE CORROSION ON BOTTOM, JUST I/B OF AILERON. THE PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1999021900307 19990219 00307 WP 1999 2 19 CALA9900150 1 19990213 A 5730 59134383 SKIN DOUG DC9 DC932 3022066 WP LT WING DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND LT WING LOWER SKIN PANEL DEBONDED AROUND SCREW HOLE FORWARD OF OUTER WHEEL WELL AREA. THE SKIN PANEL W AS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999021900308 19990219 00308 WP 1999 2 19 CALA9900151 1 19990213 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389 CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND A HOLE CHAFED IN LOWER CHORD OF FORWARD CARGO COMPARTMENT FLOORBEAM AT FS 389, RBL 2. A REPAIR WAS INS TALLED IAW SRM 53-05-00, FIGURE 20A, PAGE 31. 2 L 7 2 4F A6WE 1999021900309 19990219 00309 NM 1999 2 19 CALA9900152 1 19990213 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 277-294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 277 TO 294. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED I AW SRM 53-00-02, FIGURE 202. 2 L 7 2 4F RT A16WE 1999021900310 19990219 00310 NM 1999 2 19 CALA9900153 1 19990214 A 5730 114N210919 PANEL BOEING 757 757224 1384958 NM LT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND LT WING L/E ACCESS PANEL 521RB DELAMINATED AND DENTED. THE PANEL WAS REPAIRED IAW SRM 51-70-05, PAGE 2 5, PARAGRAPH 4C. 2 L 7 2 4F RT A2NM 1999021900311 19990219 00311 WP 1999 2 19 CALA9900154 1 19990215 A 3397 WIRE DOUG DC9 DC932 3022066 WP PAX DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 43537 47112 EMERGENCY LIGHT BATTERY PACKS FAILED TEST AT LT LAV AND FORWARD ENTRY. REPAIRED BROKEN WIRES, SECURED LOOSE GROUND, AND TIGHTENED BATTERY CONTACTS. OPERATION CHECKED NORMAL IAW MM 33-50-00, PAGE 203. 2 L 7 2 4F A6WE 1999021900312 19990219 00312 WP 1999 2 19 CALA9900155 1 19990215 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT TEE CHANNEL CORRODED AT STA 160, LBL 8. THE FLOOR SUPPORT T CHANNEL WAS RE MOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-60-0. 2 L 7 2 4F A6WE 1999021900313 19990219 00313 WP 1999 2 19 CALA9900156 1 19990215 A 5312 BLKHD BRACKET DOUG DC9 DC932 3022066 WP CARGO COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND TWO AFT CARGO FORWARD BULKHEAD SPLICE BRACKETS WITH .5 INCH CRACKS. NEW FITTINGS WERE INSTALLED IAW SR M 51-10-1 AND 51-00-00. 2 L 7 2 4F A6WE 1999021900314 19990219 00314 NM 1999 2 19 UPS99228723 1 19990210 A 7830 TR UNIT BOEING 727 72722C 138400F NM NR 3 ENGINE MALFUNCTIONED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 930UP 19096 INSPECTION TYPE-N/A, ON CLIMBOUT NR 3 THRUST LEVER RAPIDLY RETARD TO IDLE A/C YAWED, T/R WARNING LIGHT CAME ON, PERFORME D APPROPRIATE CHECKLIST AND SECURED THE ENGINE. PERFORMED E/O B727-7100-10130 C/W, NO DEFECTS FOUND. 2 L 7 3 4F A3WE 1999021900315 19990219 00315 WP 1999 2 19 UPS99828724 1 19990215 A 3350 5708458503 BATTERY DOUG DC8 DC871F 302199D WP BS 143 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-N/A, EMERGENCY LIGHT IN COCKPIT DID NOT TEST DURING PREFLIGHT. REMOVED AND REPLACED EMERG LIGHT BATT AN D RELAY UNIT WITH REF MM 33-50-01, OPS CK'ED NORMAL AT THIS TIME. (P/N 5708458-503), (S/N 925/084). 2 L 7 4 4F RT 4A25 1999021900316 19990219 00316 WP 1999 2 19 UPS99828725 1 19990106 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 781-798 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, MAIN CABIN HAS CORROSION ON INSIDE UPPER AND LOWER LIP ON LO9NG 11R STA 781 TO 798. REMOVED CORRO DED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL. 2 L 7 4 4F RT 4A25 1999021900317 19990219 00317 WP 1999 2 19 UPS99828726 1 19990205 A 5320 WEB DOUG DC8 DC873F 302199F WP L2 DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, STA 1580 TO 1620 LT CUSP WEB BARE METAL AND CORROSION. REMOVED CORROSION, NOT WITHIN LIMITS IAW D C8 SRM 53-2-0. REMOVED AND REPLACED DAMAGED SECTION OF CUSP IAW DC8 SRM 51-1-20D. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. 2 L 7 4 4F RT 4A25 1999021900319 19990219 00319 WP 1999 2 19 UPS99828729 1 19990107 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, AFT PIT FS 1020 BETWEEN L33R AND L32R CIRC FRAME CORRODED. CORROSION OUT OF LIMITS. REPLACED FRA ME SECTION IAW DC8 SRM 53-2-0 AND 53-4-1 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999021900320 19990219 00320 WP 1999 2 19 UPS99828730 1 19990107 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:C123, AFT PIT FS 1000 CIRC FRAME AT LONGERON 36 CRACKED AND HAS SHEARED FASTENERS. REMOVED DAMGED FRAME IAW SRM 53-2-0. FAB NEW ONE IAW DAC DWG 9755885 AND REO-06189. INSTALLED IAW REO-06189 AND DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999021900322 19990219 00322 EU 1999 2 19 QXEA9900288 1 19990209 A 2120 AIR DIST FOKKER F28 F28MK4000 4990810 EU CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 09 481US 11230 9780 BOI - DURING TAKEOFF ROLL, THERE WAS SMOKE SMELL IN CABIN. NO PRESSURE ABOVE 3 PSI, DUCT PRESSURE 10 PSI WITH ANTI-ICE ON. MAINTENANCE GROUND RUN AIRCRAFT, ENGINE 1 AND 2 SAME ACCELERATION RATE. RAN BOTH AT HIGH POWER, NO SMOKE SMELL IN CABIN. AIRCRAFT PRESSURE TO 4.0 PSI, AFT PRESSURE DROP. CHECK OK, NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1999021900323 19990219 00323 WP 1999 2 19 ABXA9900097 1 19990121 A 5712 K050565 RIB DOUG DOUG DC8 DC863 302198A WP WS 841 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING OUTBOARD LEADING EDGE UPPER RIB CRACKED INSIDE PANEL 517B AT STATION FS 841. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999021900324 19990219 00324 WP 1999 2 19 ABXA9900098 1 19990119 A 5730 5769859 SKIN DOUG DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT WING INBOARD NR 2 PYLON, LOWER AFT SKIN CRACKED AT LOWER TRAILING EDGE. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999021900325 19990219 00325 WP 1999 2 19 MWEA99070 1 19990209 A 5210 9955752501 BEAM DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK IN FORWARD PASSENGER DOOR AT FORWARD END OF NUMBER 1 BEAM. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999021900326 19990219 00326 NM 1999 2 19 DL733990278 1 19990211 A 5720 FITTING BOEING 737 737347 1384647 NM LT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 LT LANDING GEAR BEAM ATTACH FITTING CRACK IN FASTENER ATTACH HOLES. REPAIRED PER ERA 332754-14. 2 L 7 2 4F RT A16WE 1999021900327 19990219 00327 NM 1999 2 19 DL72K990279 1 19990211 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1096 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 WEAR IN FUSELAGE SKIN AT STA 1096 AT STR-1. REPAIRED PER ERA 332760-14AD. 2 L 7 3 4F A3WE 1999021900328 19990219 00328 NM 1999 2 19 DL73K990280 1 19990211 A 5330 SKIN BOEING 737 737232 1384475 NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 324DL 23096 THE FUSELAGE SKIN WAS FOUND CRACKED AT THE LOWER FWD CORNER OF THE L2 DOOR SURROUND LOWER HINGE CUTOUT. THE CRACK WAS . 25 INCH LONG IN THE SKIN ONLY. THE CRACK WAS ROUTED OUT, THE UNDERLYING BEAR STRAP INSPECTED, AND AN EXTERNAL REPAIR D OUBLER INSTALLED PER ER/A 366680-14, REV A. 2 L 7 2 4F RT A16WE 1999021900329 19990219 00329 NM 1999 2 19 DL767990281 1 19990211 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 112DL 22224 ON L/O, FOUND 9 AISLE LIGHTS WOULD NOT ILLUMINATE ON TEST. REPLACED M732 BATTERY PACK, OPS NOW NORMAL. 2 L 7 2 4F RT A1NM 1999021900330 19990219 00330 NM 1999 2 19 DL72K990282 1 19990212 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 FOUND AT C-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT ENTRYWAY LT FRAME APPROX 6 INCHES BELOW UPPER STOP PAD. REPAIRE D PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999021900331 19990219 00331 NM 1999 2 19 DL73K990283 1 19990211 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM ROW 4DEF & 8ABC INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 315DL 23087 ON S/C, FOUND LT OVERWING SLIDE LIGHT, RT OVERWING EXIT SIGN, AISLE LIGHT SEAT 4DEF AND AISLE LIGHT SEAT 8ABC INOP ON EM ERGENCY LIGHTS TEST. REPLACED BATTERY CHARGER M01135. 2 L 7 2 4F RT A16WE 1999021900332 19990219 00332 NM 1999 2 19 DL72W990285 1 19990212 A 3350 BATTERY PACK 900835A BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2819W 5734 21057 REAR AISLE EMERGENCY EXIT SIGN BATTERY WEAK. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999021900333 19990219 00333 NM 1999 2 19 DL73E990287 1 19990213 A 2421 GENERATOR 915F2127 BOEING 737 7372S3 NM NR 1 FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 369DL UG400 21776 NR 1 ENG GEN FAILED SHORTLY AFTER T/O. THERE WAS NO INDICATION ON THE OVERHEAD ELECT PANEL THAT THE GENERATOR HAD FAILE D. REPLACED GCU. 2 L 7 2 4F RT A16WE 1999021900335 19990219 00335 NM 1999 2 19 DL73K990289 1 19990213 A 2121 FAN 215201 BOEING 737 737232 1384475 NM E & E COMPT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 308DL 23080 SLIGHT SMELL IN CABIN. FOUND GASPER FAN BREAKER POPPED. DEFERRED PER MINIMUM EQUIPMENT LIST AND COLLARED BREAKER FOR F AN. REPLACED FAN. 2 L 7 2 4F RT A16WE 1999021900336 19990219 00336 NM 1999 2 19 DLM88990290 1 19990213 A 2170 COALESCER DOUG MD88 MD88 3023688 NM RT PACK DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 934DL 6997 49721 PACK SMOKE/SMELL ON TAKEOFF. TURNED BOTH PACKS OFF, SMELL DISSIPATED. LEFT PACK ON FOR REST OF FLT, NO SMELL. INSPECT ED APU INLET DOORS, FOUND OILY RESIDUE INSIDE FWD DOOR. INSPECTED LT AND RT ACMS AND REPLACED COALESCER BAGS. RAN ENGI NES WITH PACKS RUNNING, NO SMOKE OR ODOR PRESENT. FWD APU PNEUMATICS TO MCO ON SEPARATE LOG ITEM. 2 L 7 2 4F RT A6WE 1999021900337 19990219 00337 NM 1999 2 19 DL757990291 1 19990214 A 5220 GUIDE BOEING 757 757232 1384965 NM 2L DOOR WORN A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 627DL 22917 DOOR 2L UNABLE TO USE FROM OUTSIDE IN BHM. LINKAGE DAMAGED, REPLACED GUIDE. 2 L 7 2 4F RT A2NM 1999021900338 19990219 00338 NM 1999 2 19 DL72S990293 1 19990214 A 3350 RPS1 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 MID CABIN SEAT EMERGENCY LIGHTS INOP. REPLACED BATTERY RACK AND BATTERY PACK, ALL OPS NORMAL. 2 L 7 3 4F A3WE 1999021900339 19990219 00339 NM 1999 2 19 DL72S990294 1 19990214 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM PAX DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 LEFT AFT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED RACK, NOW CKS NORMAL. 2 L 7 3 4F A3WE 1999021900340 19990219 00340 NM 1999 2 19 DL72K990295 1 19990215 A 2560 146110016 SLIDE BOEING 727 727232 1384082 NM L1 DOOR DISLODGED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 524DA 21584 DURING TAKEOFF ROLL, L1 SLIDE PACK DISLODGED FROM DOOR. ACFT RETURNED TO BLOCK. RESECURED SLIDE PACK, CKS NORMAL. 2 L 7 3 4F A3WE 1999021900341 19990219 00341 1999 2 19 DLM11990297 4 19990213 A 2397 1302413006 WIRE DOUG MD11 MD11 3023602 NM ROW 13A SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 811DE 48566 ON GROUND IN LGW, ELECTRICAL SMELL PRESENT AT ROW 13 OF PASSENGER CABIN. FOUND SEAT 13A VIDEO MONITOR HARNESS SHORTED O UT IN SEAT 13A. FLT CREW VERBAL REPORT. DEACTIVATED SEAT 13A AT LGW. REPLACED HARNESS ASSY AND VIDEO MONITOR AT 13A A ND INSPECTED HARNESSES AND ROUTING OF HARNESS IN ALL BUSINESS CLASS SEATS. 2 L 7 3 4F RT A22WE 1999021900342 19990219 00342 NM 1999 2 19 DL72K990298 1 19990129 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 INB'D FLAP / INB'D TRACK / MLG BEAM ATTACH PAD: CORROSION AD 90-07-05 AND 90-06-09. CORROSION TO (1) MLG BEAM ATTACH H OLES AND (2) MLG DOOR AFT ATTACH FITTING BOLT HOLES. BOTH HOLES ARE WITHIN AD AREA. MLG BEAM ATTACH HOLES OVERSIZED AN D LEFT AS IS. MLG DOOR FITTING HOLE OVERSIZED AND OVERSIZED FASTENER INSTALLED. 2 L 7 3 4F A3WE 1999021900343 19990219 00343 NM 1999 2 19 DL72K990299 1 19990104 A 5753 652163361 SKIN BOEING 727 727232 1384082 NM LT TE MIDFLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING SHOP INSPECTION, THE LEADING EDGE WAS FOUND WORN AT THE O/B END OF FLAP. THE DAMAGE WAS REMOVED AND A DOUBLER AN D FILLER INSTALLED PER MM 57-52-0, FIG 803. 2 L 7 3 4F A3WE 1999021900344 19990219 00344 NM 1999 2 19 DL76G990300 1 19990215 A 3097 WIRE BOEING 767 7673P6 1385105 NM FWD GALLEY SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 156DL 25354 ELECTRICAL ARC NOTED SEVERAL TIMES IN FORWARD GALLEY RT SIDE NEAR DRAIN SHUT-OFF VALVE. FOUND FEEDER WIRE TO FWD GALLEY SUPPLY SIDE RIBBON HEATER B109 SHORTED TO GALLEY STRUCTURE. REPAIRED AND REROUTED WIRE, TRIM REINSTALLED IPC REF 3 0-71-02 PG 106 SHEET 1. 2 L 7 2 4F RT A1NM 1999021900345 19990219 00345 NM 1999 2 19 DL757990301 1 19990215 A 3397 WIRE BOEING 757 757232 1384965 NM ROW 27 BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 622DL 22912 MAIN CABIN EMERGENCY TRACK LIGHTS INOP ON FWD ONE THIRD OF TRACK. FOUND BROKEN WIRE AT ROW 27. SPLICED SAME PER M/M, T RACK LIGHTING CKS GOOD. 2 L 7 2 4F RT A2NM 1999021900346 19990219 00346 SO 1999 2 19 SWIA971390 1 19990209 A 7603 SOLENOID EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FLIGHT IDLE STOP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 580SW 120348 THE IDLE 2 UNLK LIGHT ILLUMINATED IN FLIGHT. AS PER FLIGHT OPS BULLETIN B-12, DATED NOV 24,1998, THERE IS NO QRH PROCED URE ASSOCIATED WITH ILLUMINATION OF THE LIGHT. RETURNED TO LAX. INSTALLED NEW FLIGHT IDLE STOP SOLENOID IAW 76-10-00. GROUND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900347 19990219 00347 SO 1999 2 19 SWIA971391 1 19990209 A 2750 SELECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 220SW 120288 FLAPS WOULD NOT RETRACT AFTER TAKEOFF (DISAGREEMENT). RETURNED TO LAX. REPLACED FLAP SELECTOR WITH SERVICEABLE UNIT. O PERATED NUMEROUS TIMES, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900348 19990219 00348 SO 1999 2 19 SWIA971392 1 19990209 A 3232 BOLT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG DOOR ACT MISSING A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 221SW 120290 WHEN GEAR WAS RETRACTED, LEFT SIDE SHOWED INTRANSIT LIGHT. CYCLED GEAR, SAME. RETURNED TO LAX. FOUND BOLTS MISSING FO RM LEFT INBOARD FOWARD GEAR DOOR ACTUATOR. INSTALLED PROPER HARDWARE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900349 19990219 00349 SO 1999 2 19 SWIA971393 1 19990209 A 3010 B NUT EMB 120 EMB120RT SO PWA 118 PW118A NE LT DEICE BOOT LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 LEADING EDGE MIDDLE LEFT WING DEICE BOOT FAILS BOTH TIMERS. RETURNED TO FIELD. TIGHTENED LOOSE B-NUT AT LEFT MIDDLE LE ADING EDGE DEICE BOOT PRESSURE SWITCH, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900350 19990219 00350 SO 1999 2 19 SWIA971394 1 19990209 A 3020 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE DEICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 198SW 120227 RIGHT ENGINE INLET DEICE FAILS. RETURNED TO SLC. CLEANED PRESSURE SWITCH ON RIGHT ENGINE INLET BOOT, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900351 19990219 00351 SO 1999 2 19 SWIA971395 1 19990209 A 3010 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 234SW 120308 TWO MINUTES INTO FLIGHT, RIGHT AND LEFT OUTBOARD WING DEICE INOP AND LIGHTS ILLUMINATED. TRIED DIFFERENT TIMERS 2 HEAVY VS LITE, LIGHTS STILL ILLUMINATED. RETURNED TO FAT. BOTH DEICE SYSTEM REGULATORS WERE REPLACED, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900352 19990219 00352 SO 1999 2 19 SWIA971396 1 19990209 A 3010 DEICE SYST EMB 120 EMB120RT SO PWA 118 PW118A NE LT WING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 LEADING EDGE MIDDLE LEFT WING DEICE BOOT FAILS BOTH TIMERS. RETURNED TO SFO. SWAPPED LEFT AND RIGHT MIDDLE DEICE BOOT PRESSURE SWITCHES FOR TROUBLESHOOTING. COULD NOT DUPLICATE PROBLEM. LEADING EDGE DEICE SYSTEM, CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900353 19990219 00353 SO 1999 2 19 SWIA971397 1 19990209 A 3010 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT HORIZ STAB FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 560SW 120334 LEFT INBOARD STABILIZER BOOT FAILS INFLIGHT AT ALL CONFIGURATIONS OF TIMERS AND SETTINGS. RETURNED TO PDX. REPLACED RI GHT PRESSURE REGULATOR DUE TO LOW OUTPUT (18 PSI) AND PATCHED BOOT, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900354 19990219 00354 SO 1999 2 19 SWIA971398 1 19990209 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ELEVATOR TRIM FAILED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 568SW 120343 ON DESCENT WHEN AUTO PILOT WAS DISCONNECTED, FOUND THAT TRIM WHEEL WAS FROZEN IN POSITION. AS DESCENDED BELOW FREEZING LEVEL TRIM SLOWLY BECAME FREE. NORMAL APPROACH AND LANDING. REMOVED BOTH LEFT AND RIGHT ELEVATOR TRIM ACTUATORS AND RE PLACED TRIM WITH A SERVICEABLE ONE, OPS IAW MM 27-31-00. ALSO, REMOVED ELEVATOR TRIM SERVO FOR TROUBLESHOOTING. OPS CH ECKS GOOD ON GROUND. CLEARED TEST FLIGHT. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900355 19990219 00355 SO 1999 2 19 SWIA971399 1 19990202 A 3230 RETRACT MECH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR ICED UP A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 190SW 120050 GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES. CYCLED 3 TIMES TO GET THE GEAR DOWN AND LOCKED. DEICED NOSE GEAR AND CY CLED LANDING GEAR SEVERAL TIMES. ALL INDICATION AND OPERATION NORMAL. ALL LOCKING MECHANISM CLEARED OF ICE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900356 19990219 00356 SO 1999 2 19 SWIA971400 1 19990202 A 2930 3D237225 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE GREEN HYD SYST FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 197SW 120186 LOW LEVEL AND LOW PRESSURE LIGHT CAME ON GREEN SYSTEM. DECLARED AN EMERGENCY AND LANDED IN SLC WITHOUT INCIDENT. REPLA CED HYDRAULIC HEAD PRESSURE REGULATOR AND DRAINED WATER FROM SYSTEM, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900357 19990219 00357 NM 1999 2 19 VNAA9902004 1 19990209 A 5610 001A561A0000207 WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 432JS 37046 3045 WHILE EN ROUTE TO BTV, THE RIGHT HAND SIDE WINDOW OUTER PANE CRACKED. THE AIRCRAFT DIVERTED TO PIT AND LANDED SAFELY. P IT MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND SIDE WINDSCREEN, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-1 2-00. OPERATIONAL CHECKS WERE SATISFACTORY. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999021900358 19990219 00358 NM 1999 2 19 VNAA9902005 1 19990210 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 436JS 83002 68903 3052 AFTER PUSHBACK, THE LEFT HAND PROPELLER FAILED TO UNFEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENA NCE INSPECTED AND REPLACED THE LEFT HAND PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999021900359 19990219 00359 NM 1999 2 19 VNAA9902006 1 19990214 A 6120 DOLN511F07SND01 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP GOV DIRTY A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 433JS 3047 THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED TO FUNCTION WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENAN CE INSPECTED AND CLEANED THE OVERSPEED GOVERNOR CANNON PLUG. OPERATIONAL CHECKS WERE COMPLETED, IN ACCORDANCE WITH DORN IER MAINTENANCE MANUAL 61-21-04. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999021900360 19990219 00360 NM 1999 2 19 SWAA990158 1 19990122 A 2750 69435312526 CONTROL CABLE BOEING 657190216 BOEING 737 7372H4 138448C NM RT TE FLAP FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 3N85 22062 DURING SCHEDULED D-CHECK, FLAP EXTENSION CHECKS, ON FUNCTIONAL FLT CK RT FLAP CABLES BROKE. REMOVED DAMAGED CABLES AND REPLACED WITH NEW ONES. REPAIRED ALL HIDDEN DAMAGE ON RT I/B MIDFLAP PER OHM 57-53-22. OPERATIONAL TESTED OK PER MM 57 -53-22. 2 L 7 2 4F A16WE 1999021900361 19990219 00361 NM 1999 2 19 SWAA990159 1 19990125 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 930 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED APPROX 3.5 INCHES LONG AT BS 930, S23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999021900362 19990219 00362 NM 1999 2 19 SWAA990160 1 19990122 A 2520 STRAP BOEING 737 7375H4 138449D NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 508SW 24185 AIRCRAFT RETURNED TO BNA DUE TO AFT SERVICE DOOR SAFETY STRAP HANGING OUTSIDE OF THE DOOR AND BANGING ON THE AIRCRAFT SK IN. INSPECTED AIRCRAFT WITH NO DAMAGE NOTED. PROPERLY SECURED STAP AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A16WE 1999021900363 19990219 00363 NM 1999 2 19 SWAA990161 1 19990125 A 5347 TRACK BOEING 737 7373H4 1384600 NM BS 787 & 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED 1/4D CHECK, FOUND RT FLOOR TRACK CRACKED UNDER TIEDOWN AT BS 787, AND 767. REPLACED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900364 19990219 00364 NM 1999 2 19 SWAA990162 1 19990125 A 5347 TRACK BOEING 737 7373H4 1384600 NM BS 793-847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED 1/4D CHECK, FOUND RT FLOOR TRACK HEAVILY CORRODED FROM BS 793 TO 847. REPLACED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900365 19990219 00365 NM 1999 2 19 SWAA990163 1 19990125 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER T CHORD CORRODED AT BS 294.5. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900366 19990219 00366 NM 1999 2 19 SWAA990164 1 19990125 A 5320 SPLICE BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900367 19990219 00367 NM 1999 2 19 SWAA990165 1 19990125 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED D-CHECK, FOUND UPPER FLOORBEAM CHORD CRACKED AT BS 947. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900368 19990219 00368 NM 1999 2 19 SWAA990167 1 19990122 A 3150 MCP BOEING 737 7373H4 1384600 NM COCKPIT INOP A SWAA D RETURN TO BLOCK O OTHER CR CRUISE 1 SW 07 323SW 23344 AIR RETURN WHEN MCP WENT INTO THE TEST MODE. REMOVED AND REPLACED THE MCP AND THE SYSTEM CHECK OK. 2 L 7 2 4F RT A16WE 1999021900369 19990219 00369 NM 1999 2 19 SWAA990168 1 19990126 A 3350 20121 BATTERY BOEING 737 7372H4 138448C NM GALLEY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SC CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/ M. 2 L 7 2 4F A16WE 1999021900370 19990219 00370 NM 1999 2 19 SWAA990169 1 19990125 A 5320 CHANNEL BOEING 737 7373H4 1384600 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED 1/4D CHECK, FOUND FLOOR CHANNEL HEAVILY CORRODED AT BOTTOM FASTENER HOLES AT BS 773. REPLACED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900371 19990219 00371 NM 1999 2 19 SWAA990170 1 19990126 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 787-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 787 TO 847, LBL 3. REPLACED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900372 19990219 00372 NM 1999 2 19 SWAA990171 1 19990126 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 4. REPAIRED DAMAGED SECTION PER SWA RA 1-353-19 93. 2 L 7 2 4F RT A16WE 1999021900373 19990219 00373 NM 1999 2 19 SWAA990172 1 19990126 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 488 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 488. SPLICED IN NEW SECTION PER SWA BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900374 19990219 00374 NM 1999 2 19 SWAA990173 1 19990126 A 5320 STRAP BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 VERTICAL STRAP CRACKED AT LBL 6.6. INSTALLED REPAIR DOUBLER PER SWA BOEING SR M. 2 L 7 2 4F RT A16WE 1999021900375 19990219 00375 NM 1999 2 19 SWAA990166 1 19990124 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602SW 27953 DURING PREFLIGHT, FOUND ROW 23 LEFT AFT 3 EMERGENCY FLOOR LIGHTS INOP. RESECURED LOOSE WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999021900376 19990219 00376 NM 1999 2 19 SWAA990174 1 19990128 A 3350 20121A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED SC CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CK'D GOO D PER M/M. 2 L 7 2 4F A16WE 1999021900377 19990219 00377 NM 1999 2 19 SWAA990175 1 19990127 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING HAD SEVERAL LAMPS BURNED OUT. RELAMPED PER BOEING M/M, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999021900378 19990219 00378 NM 1999 2 19 SWAA990176 1 19990126 A 3350 LIGHTS BOEING 737 7375H4 138449D NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 508SW 24185 DURING PREFLIGHT CHECK, FOUND 5 WHITE EMERGENCY EXIT FLOOR LIGHTS IN A ROW INOP. INSPECTED WIRE SPLICES AND OPS CHECK L IGHTS OK. 2 L 7 2 4F RT A16WE 1999021900379 19990219 00379 NM 1999 2 19 SWAA990177 1 19990126 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 310 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED A1 CHECK, FOUND 2 INCH SKIN CRACK AT BS 310 STRINGER 18R AND 2 INCH CRACK 2 INCHES BELOW TOP CRACK. RE PAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900380 19990219 00380 1999 2 19 SWAA990178 4 19990127 A 2565 22D229900131 SLIDE BOEING 737 7372H4 138448C NM CABIN LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1999021900381 19990219 00381 1999 2 19 SWAA990179 4 19990127 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM CABIN DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 655WN 28400 FORWARD ENTRY SLIDE INADVERTENTLY DEPLOYED AT GATE AFTER ENGINE SHUTDOWN. REMOVED AND REPLACED FWD ENTRY SLIDE ASSY PER M/M. 2 L 7 2 4F RT A16WE 1999021900382 19990219 00382 NM 1999 2 19 SWAA990180 1 19990127 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN WITH 6 RIVETS POPPED AND ANTENNA DOUBLER CORRODED THROUGH, BETWEEN BS 500 B AND C AND BETWEEN S28L AND R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900383 19990219 00383 NM 1999 2 19 SWAA990181 1 19990127 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, LBL 7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900384 19990219 00384 NM 1999 2 19 SWAA990182 1 19990127 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 310 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED 2 INCHES AT BS 310, AT S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900385 19990219 00385 NM 1999 2 19 SWAA990183 1 19990127 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 750 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 2.125 INCHES AT BS 750, AT S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999021900386 19990219 00386 NM 1999 2 19 SWAA990184 1 19990127 A 5730 SKIN BOEING 737 7372H4 138448C NM WS 163 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED C2 CHECK, FOUND LT WING AT WS 163 A 2.5 INCH CRACK FROM RIVET TO RIVET UPPER WING PANEL. REPAIRED PER SWA RA 1-257-0628. 2 L 7 2 4F A16WE 1999021900387 19990219 00387 NM 1999 2 19 SWAA990185 1 19990127 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 930 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED 3.5 INCHES AT BS 930, AT S22R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999021900388 19990219 00388 NM 1999 2 19 SWAA990232 1 19990209 A 5312 BULKHEAD CHORD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 T-CHORD CRACKED AT LBL 5.7, WL 184. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900389 19990219 00389 NM 1999 2 19 SWAA990233 1 19990209 A 3350 201314 BATTERY BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 ALL EMERGENCY EXIT FLOOR TRACK LIGHTS FWD OF THE OVERWING EXIT ARE INOP. REMOVED AND REPLACED BATTERY AND BASE PER MM, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 1999021900390 19990219 00390 NM 1999 2 19 SWAA990234 1 19990209 A 2131 7638101 CONTROLLER BOEING 737 7373Q8 1384670 NM CABIN MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 LOSS OF PRESSURIZATION ON ARRIVAL INTO SEA AT 4000 AGL AFTER SLOW DESCENT. DESCENT INTO SEA WAS NORMAL WITH NORMAL CABI N INDICATIONS UNTIL 4000 AGL. REMOVED AND REPLACED CABIN PRESS CONTROLLER PER M/M. 2 L 7 2 4F RT A16WE 1999021900391 19990219 00391 NM 1999 2 19 SWAA990235 1 19990209 A 3260 6558250295 PC BOARD BOEING 737 7373Y0 1384671 NM E & E BAY FAILED A SWAA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 664WN 23495 ON TAKEOFF FROM ABQ, LEFT MAIN GEAR RED LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR 2 TIMES, NO HELP. F/O VISUALLY CHECKED GEAR THRU VIEWING PORT AND GEAR APPEARED UP. CONTINUED TO SLC AND AFTER APPROX 15 MIN RED GEAR LIGHT EXTINGUISHED. RE PLACED THE M986 AND M988 CIRCUIT CARDS, OPS GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999021900392 19990219 00392 NE 1999 2 19 SWAA990236 2 19990209 A 7320 CIRCUIT BREAKER BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE COCKPIT MALFUNCTIONED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 501SW 24178 NR 1 ENGINE SHUTDOWN AFTER ENGINE START. RETURNED TO GATE. CYCLED NR 1 ENG, FUEL SHUT-OFF VALVE C/B, SYSTEM OP CKS NOR MAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999021900393 19990219 00393 NM 1999 2 19 SWAA990237 1 19990211 A 2740 AR7077M3 MOTOR BOEING 737 7375H4 138449D NM STAB TRIM FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 SW 07 521SW 25320 A/C RETURNED TO MDW FOR STAB TRIM PROBLEM. REPLACED MAIN STAB TRIM MOTOR PER M/M, OPS CHECKED OK. 2 L 7 2 4F RT A16WE 1999021900394 19990219 00394 NM 1999 2 19 SWAA990238 1 19990209 A 3350 20121A BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED CHECK, FOUND AFT EMERGENCY FLOOR EGRESS LIGHTS INOP. REMOVED AND REPLACED AFT EGRESS BATTERY PACK AND CHARGER, OPS CK'D OK PER M/M. 2 L 7 2 4F A16WE 1999021900395 19990219 00395 NM 1999 2 19 SWAA990239 1 19990210 A 3350 BULB BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED CHECK, FOUND EMERGENCY LIGHT INOP BEHIND CAPT SEAT. RELAMPED AND OPS GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999021900396 19990219 00396 NM 1999 2 19 SWAA990240 1 19990210 A 3350 CONNECTOR BOEING 737 7373H4 1384600 NM AFT GALLEY FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED C3 CHECK, FOUND AFT GALLEY CENTER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CANNON PLUG AT BATTE RY PACK AND REPAIRED WIRING PER BOEING M/M. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999021900397 19990219 00397 NM 1999 2 19 SWAA990241 1 19990212 A 3350 BULB BOEING 737 7373Y0 1384671 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED SC CHECK, FOUND EMERGENCY LIGHT ON LEFT FUSELAGE AFT OF WING INOP. RELAMPED EMERGENCY LIGHT ON LEFT F USELAGE PER M/M, OPS CHECK OK. 2 L 7 2 4F RT A16WE 1999021900398 19990219 00398 NM 1999 2 19 SWAA990242 1 19990211 A 3397 WIRE BOEING 737 7375H4 138449D NM ROW 15 & 18 OUT OF ADJ A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP BETWEEN SEAT ROWS 15 AND 18. READJUSTED FLOOR WIRI NG PER M/M. 2 L 7 2 4F RT A16WE 1999021900399 19990219 00399 NM 1999 2 19 SWAA990243 1 19990209 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 629SW 27704 F/A'S REPORTED STRONG SMOKE SMELL IN CABIN. ALSO, NOTICEABLE HAZE FROM ROW 7 FORWARD. REMOVED AND REPLACED GASPER FAN, COALESCER BAGS, AND HEPA FILTER PER MM. OPS CHECKED RECIRCULATION FAN AND RAN PACKS, PRESSURIZED TO 3 PSI WITH ENGINES AT 80 PERCENT N1, NO SMOKE SMELL OR HAZE NOTICEABLE. SYSTEM OPS, CHECKED GOOD PER MM AT THIS TIME. 2 L 7 2 4F RT A16WE 1999021900400 19990219 00400 NM 1999 2 19 SWAA990244 1 19990209 A 3211 161A11401 LINK BOEING 737 7377H4 NM RT MLG BROKEN A SWAA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 07 743SW 29279 RT MLG SEVERE VIBRATION ON LANDING. UPPER TORSION LINK BROKE. BOEING, ENGINEERING, QC AND SWA MX ALL ON SITE. INCIDEN T STILL UNDER INVESTIGATION. 2 L 7 2 4F RT A16WE 1999021900425 19990219 00425 EU 1999 2 19 CA990119032 1 19990106 A 3244 TIRE AIRBUS 320 A320211 3930320 EU MLG FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA (CAN) ON DEPARTURE, NR 4 MAIN WHEEL TIRE CAP SHREDDED, SLIGHT VIBRATION DURING GEAR RETRACTION. ON ARRIVAL, FOUND NR 4 WHEEL TIRE CAP MISSING, EVIDENCE OF INGESTION INTO RT ENGINE, FAN BLADES AND ACOUSTIC LINER DAMAGED. ALSO, DAMAGE ON RT INBD LAP TRAILING EDGE AND RT STABILIZER LEADING EDGE. NR 3 AND NR 4 WHEELS REPLACED, FAN BLADES REPLACED AND FLAPS AN D HORIZONTAL STABILIZER REPAIRED. 2 L 7 2 4F RT A28NM 1999021900426 19990219 00426 EA 1999 2 19 CA990119033 1 19990111 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE E/E BAY FAILED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 807373 (CAN) ON DEPARTURE, AIR TEMP PROBE, RIGHT ANGLE OF ATTACK, RIGHT STATIC HEAT MESSAGES ON EICAS. REPLACED AIR DATA SENSO R CONTROLLER. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900427 19990219 00427 NM 1999 2 19 CA990119034 1 19990109 A 2731 TRIM MODULE BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT PEDESTAL FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P709673 (CAN) SHORTLY AFTER TAKEOFF, RUDDER RATIO ENGINE INDICATING AND CREW ALERT SYSTEM MESSAGE FOLLOWED BY AILERON LOCKOUT ME SSAGE. SPEED AT TIME 270 KNOTS AND INCREASING ALTITUDE 11,000 FEET, ALL 3 AUTOPILOTS WOULD NOT ENGAGE. AIRCRAFT RETURN ED. CHANGED LEFT AND RIGHT STABILIZER TRIM/ELEVATOR ASYMMETRY MODULE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999021900428 19990219 00428 EA 1999 2 19 CA990119035 1 19990109 A 3260 BRACKET CNDAIR CL600 CL6002B19 EA NLG BENT W K NONE J WARNING INDICATION TO TAKEOFF 1 CA 4341 (CAN) AFTER TAKEOFF AND GEAR UP SELECTION, A DISAGREE WARNING MESSAGE ON. NOSE GEAR CENTERING SENSOR BRACKET FOUND BENT OUT OF LIMITS. BRACKET AND OLEO EXTENSION SENSORS ADJUSTED. TOTAL CYCLES: 3,763. 2 L 7 2 4F RT A21EA 1999021900429 19990219 00429 EA 1999 2 19 CA990119036 1 19990108 A 2750 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WINGS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 7844 807287 (CAN) FLAP FAIL MESSAGE ON APPROACH. SYSTEM RESET. FLAP CHECK CARRIED OUT NORMAL. TOTAL CYCLES: 6,860. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900430 19990219 00430 EA 1999 2 19 CA990119038 1 19990111 A 2133 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE CABIN PRESSURE MALFUNCTIONED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 7869 807281 (CAN) UNABLE TO PRESSURIZE AFTER TAKEOFF. SUSPECT OVERBOARD COOLING VALVE DID NOT CLOSE. TOTAL CYCLES: 6.668. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900431 19990219 00431 EA 1999 2 19 CA990119039 1 19990111 A 2750 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE WINGS MALFUNCTIONED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 9569 807157 (CAN) FLAP CAUTION MESSAGE APPEARED ON FLAP SELECTION. FLAPLESS LANDING CONDUCTED. FLAP ELECTRONIC CONTROL UNIT BITE C HECK AND OPERATIONAL CHECK CARRIED OUT, BUT NOTHING FOUND. CHECK AND OPERATIONAL CHECK CARRIED OUT, BUT NOTHING FOUND. TOTAL CYCLES: 8,282. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900432 19990219 00432 EU 1999 2 19 CA990119040 1 19990106 A 3231 CONTROL UNIT AIRBUS 320 A320211 3930320 EU NLG DOOR FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA (CAN) DURING GEAR RETRACTION NLG DOORS DID NOT CLOSE, GEAR CYCLED AND INDICATION RETURNED TO NORMAL. FLIGHT DIVERTED. R EPLACED NR 2 LANDING GEAR CONTROL INTERFACE UNIT. 2 L 7 2 4F RT A28NM 1999021900439 19990219 00439 WP 1999 2 19 CA990125005 1 19990114 A 6220 369H120321 LINK HUGHES 369D21200 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR HUB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4681 1905 0153 CAE832839 (CAN) LEAD/LAG LINK INSPECTION PER AD 95-03-13, LINKS FOUND CRACKED. REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 1999021900442 19990219 00442 EU 1999 2 19 CA990125008 1 19990111 A 2612 FIRE DETECTOR BRAERO 748 HS7482A 4231001 EU CABIN MALFUNCTIONED W E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) DURING CLIMB, A FIRE WARNING BELL SOUNDED AND A WARNING LIGHT OCCURRED. AN EMERGENCY FIRE DRILL WAS CARRIED OUT A ND THE AIRCRAFT LANDED UNEVENTFULLY. POST-FLIGHT INSPECTION FOUND THE FIRE WARNING TO BE A FAULT INDICATION. AN INTERM ITTENT FIRE CONTROL RELAY AND BASE UNIT WERE REPLACED. 2 L 7 2 3T A24EU 1999021900443 19990219 00443 NM 1999 2 19 CA990125012 1 19990116 A 7540 SENSOR LINE BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E437 54555 NE RT ENGINE LOOSE W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 30743 (CAN) RIGHT ENGINE BLEED OFF - EICAS MESSAGE WHEN TAKEOFF POWER APPLIED. MESSAGE WENT OUT WHEN POWER REDUCED. SECOND A TTEMPT NORMAL. RT ENGINE PRESSURE RELIEF SHUT OFF VALVE SENSOR LINE INSPECTED AND TIGHTENED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021900454 19990219 00454 NM 1999 2 19 SWAA990254 1 19990213 A 3350 6556633 BATTERY BASE BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED SC CHECK, FOUND LT OVERWING EMERG LIGHTS ILLUMINATED WHEN POWER WAS SELECTED OFF. REMOVED AND REPLACED BATTERY BASE PER BOEING M/M. 2 L 7 2 4F A16WE 1999021900455 19990219 00455 NM 1999 2 19 SWAA990255 1 19990213 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 83SW 22732 DURING PREFLIGHT CHECK, FOUND CAPT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER BOEING M/M. 2 L 7 2 4F A16WE 1999021900456 19990219 00456 NM 1999 2 19 SWAA990256 1 19990212 A 3350 6556633 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 83SW 22732 DURING PREFLIGHT, FOUND CAPT SIDE OVERWING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F A16WE 1999021900457 19990219 00457 NM 1999 2 19 SWAA990257 1 19990212 A 5610 5893543130 WINDSHIELD BOEING 737 7372H4 138448C NM RT COCKPIT CRACKED A SWAA K NONE O OTHER CR CRUISE 1 SW 07 73SW 22673 AT 24,000 FT MSL, F/O WINDOW OUTER PANE DEVELOPED MULTIPLE CRACKS. REMOVED AND REPLACED F/O NR 1 WINDSHIELD AS PER MM 5 6-11-011-4, WINDOW HEAT OPS CHECK OK. 2 L 7 2 4F A16WE 1999021900458 19990219 00458 1999 2 19 SWAA990258 4 19990212 A 2565 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 DURING PREFLIGHT CHECK, FOUND AFT SERVICE DOOR SLIDE OUT OF POSITION. REINSTALLED SLIDE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999021900459 19990219 00459 NM 1999 2 19 SWAA990259 1 19990212 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED SC CHECK, FOUND 2 CRACK INDICATIONS BETWEEN STR 7R AND 5L ON AFT ROW OF FASTENERS OF BS 1016 AFT PRESSU RE BULKHEAD. REMOVED DAMAGED WEB, FABRICATED, FIT, DRILLED AND INSTALLED REPAIR PARTS PER TRAMCO EWO 99-0138. 2 L 7 2 4F RT A16WE 1999021900460 19990219 00460 NM 1999 2 19 SWAA990260 1 19990214 A 3350 BULB BOEING 737 7377H4 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 714CB 27848 DURING SCHEDULED SC CHECK, FOUND AFT ENTRY DOOR EMERG LIGHT INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999021900461 19990219 00461 1999 2 19 SWAA990261 4 19990213 A 2565 23D22941453 SLIDE BOEING 737 7372H4 138448C NM RT AFT DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED A1 CHECK, FOUND AFT RT DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F A16WE 1999021900462 19990219 00462 NM 1999 2 19 SWAA990262 1 19990213 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 310 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND A 1.5 INCH CRACK, 10.5 INCHES BELOW FWD SERV DOOR CUTOUT, BS 310. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1999021900463 19990219 00463 NM 1999 2 19 SWAA990263 1 19990213 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN DENTED FWD OF AFT ENTRY DOOR AT S19L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999021900481 19990219 00481 SW 1999 2 19 HEEA060493 1 19990209 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DETERIORATED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 407MM 1244 53060 MAIN ROTOR GEARBOX MOUNT RUBBER DETERIORATION. 1 G 7 1 3U O H2SW 1999021900520 19990219 00520 SW 1999 2 19 HEEA060541 1 19990210 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DETERIORATED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 457PH 53147 MAIN ROTOR GEARBOX MOUNT RUBBER BAD. 1 G 7 1 3U O H2SW 1999021900565 19990219 00565 CE 1999 2 19 99ZZZX678 1 19990125 A 2612 875135 FIRE LOOP LEAR 24 24A 5170304 CE LT ENGINE MALFUNCTIONED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 93BP 24169 LEFT HAND ENGINE FIRE LIGHT CAME ON IN-FLIGHT. REPLACED LEFT FORWARD FIRE DETECT LOOP WITH NEW. OPS CHECK GOOD. SUBMI TTER RECOMMENDED TO CHECK FIRE LOOP - NOT CONTACTING ENGINE AND CHAFING. 2 L 7 2 4J A10CE 1999021900568 19990219 00568 GL 1999 2 19 C2XA99CL006 2 19990115 A 7250 BLADE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LT ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 3709 145022 CAE310013 CLE - DURING A SCHEDULED BORESCOPE INSPECTION THE LEFT ENGINE TURBINE BLADES WERE FOUND TO HAVE DAMAGE BEYOND MANUFACTUR ES LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL A ND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999021900571 19990219 00571 SO 1999 2 19 C2XA99IA058 1 19990106 A 5713 12016079001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT WING STRINGER AT ACCESS PANEL 522EB CRACKED. REMOVED DAMAGED SECTION AND SPLICED IN NEW. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900572 19990219 00572 SO 1999 2 19 C2XA99IA057 1 19990106 A 5230 12038713001 SKIN EMB 120 EMB120RT SO CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND CARGO DOOR LOWER CENTER OUTSIDE SKIN GOUGED AND CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900573 19990219 00573 SO 1999 2 19 C2XA99IA055 1 19990106 A 5320 12048716001 BRACKET EMB 120 EMB120RT SO CARGO BAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURNIG C-CHECK INSPECTION, FOUND TOP AFT RAIL SUPPORT BRACKET FOR CARGO DOOR CRACKED. REPLACED TOP AFT RAIL SUPPORT BRA CKET. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900574 19990219 00574 SO 1999 2 19 C2XA99IA038 1 19990106 A 5320 12006157005 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND OUTBOARD FLOOR SUPPORTS CORRODED FOR PANELS 261/262DF. REMOVED AND REPLACED OUTBOARD F LOOR SUPPORTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900575 19990219 00575 SO 1999 2 19 C2XA99IA037 1 19990106 A 5320 12027929001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND INBOARD FORWARD CORNER OF FLOOR SUPPORT 261EF CORRODED. REMOVED AND REPLACED BUTT STRA P. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900576 19990219 00576 SO 1999 2 19 C2XA99IA036 1 19990106 A 5320 12037024001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND OUTBOARD FLOOR SUPPORTS FOR PANELS 261CF/EF UNDERSIDE CORRODED AT NUTPLATES. REMOVED A ND REPLACED BUTT STRAP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900577 19990219 00577 SO 1999 2 19 C2XA99IA035 1 19990106 A 5320 12006158003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND 262EF FLOOR SUPPORT TOP STRAPS CORRODED BENEATH TAPE. REMOVED AND REPLACED BUTT STRAP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900578 19990219 00578 SO 1999 2 19 C2XA99IA032 1 19990106 A 5320 12042803019 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND FORWARD BRACKET CORRODED AND AFT BRACKET CRACKED TOP OF FLOOR PANEL 261BF. REMOVED AND REPLACED '2' EACH BRACKETS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900579 19990219 00579 SO 1999 2 19 C2XA99IA031 1 19990106 A 5320 12027929001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR PANEL 251CF FLOOR SUPPORT CORRODED AT '6' EACH NUTPLATES. REMOVED AND REPL ACED BUTT STRAP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900580 19990219 00580 SO 1999 2 19 C2XA99IA030 1 19990106 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO BS 1150-1213 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK CORRODED AT SCREW HOLES STATION 1150.0 THROUGH 1213. REMOVED A ND REPLACED SEAT TRACK. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900581 19990219 00581 SO 1999 2 19 C2XA99IA029 1 19990106 A 5315 12004149001 FLOORBEAM EMB 120 EMB120RT SO BS 1213 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR PANEL 252DF AFT FLOOR SUPPORT CORRODED AT STATION 1213. REMOVED AND REPLAC ED FLOORBEAM. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900582 19990219 00582 SO 1999 2 19 C2XA99IA028 1 19990106 A 5320 12006664003 SUPPORT EMB 120 EMB120RT SO BS 1143-1213 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR PANEL 252DF OUTBOARD FLOOR SUPPORT AT NUTPLATES ARE CORRODED STATION 1143 T HROUGH 1213. REMOVED AND REPLACED FLOOR SUPPORTS AND NUTPLATES. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900583 19990219 00583 SO 1999 2 19 C2XA99IA027 1 19990106 A 5320 12004171003 SUPPORT EMB 120 EMB120RT SO BS 9058-11150 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR PANEL 252BF INBOARD FLOOR SUPPORT CORRODED STATION 9058 THROUGH 11115. REM OVED AND REPLACED FLOOR SUPPORT. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900584 19990219 00584 SO 1999 2 19 C2XA99IA026 1 19990106 A 5320 12027928001 STRAP EMB 120 EMB120RT SO BS 10890-11150 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR PANEL 251AF OUTBOARD FLOOR SUPPORT CORRODED STATION 10870 THROUGH 11150. R EMOVED AND REPLACED BUTT STRAP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900585 19990219 00585 SO 1999 2 19 C2XA99IA025 1 19990106 A 5320 12046163003 STRAP EMB 120 EMB120RT SO BS 10870-11150 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FUOND CABIN FLOOR PANEL 252BF INBOARD FLOOR SUPPORT CORRODED STATION 10870 THROUGH 11150. RE MOVED AND REPLACED BUTT STRAP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900586 19990219 00586 SO 1999 2 19 C2XA99IA022 1 19990106 A 5414 12032356004 SKIN EMB 120 EMB120RT SO RT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE VENT TUBE WAS CHAFED INTO NACELLE FIREWALL DECK AT TAIL PIPE/ENGINE JUNCTI ON. WELDED IN REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900587 19990219 00587 SO 1999 2 19 C2XA99IA021 1 19990106 A 5414 12032356004 SKIN EMB 120 EMB120RT SO RT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE FUEL INLET TO NOZZLES LINE CHAFING INTO NACELLE DECK. INSTALLED REPAIR DO UBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900588 19990219 00588 SO 1999 2 19 C2XA99IA020 1 19990106 A 5400 12049053001 BEAM EMB 120 EMB120RT SO NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT ENGINE FORWARD COWL, CENTER BEAM WAS CRACKED, CHAFED AND DENTED AT AFT END. RETUR NED TO CONTOUR AND WELDED CHAF AND CRACKED AREA. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021900610 19990219 00610 EU 1999 2 19 PLGA990105A 1 19990105 A 6120 C821452 CONTROL CABLE SAAB SF340 340B 7860101 EU LT PROPELLER DISCONNECTED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NE 05 354BE 1066 340B246 LGA - FLT 6539 - AFTER TAKEOFF AND WHILE PASSING THROUGH 5000 FT, THE LEFT PROPELLER RPM DROPPED TO 1140. THE CREW WAS UNABLE TO CORRECT THE PROBLEM AND FOLLOWED PROCEDURES TO SHUT THE ENGINE DOWN. THE AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED THE LEFT PCU CONDITION LEVER CABLE BALL JOINT TO BEARING ROD END WHICH CONNECT S CONTROL CABLE TO PCU HAD DISCONNECTED. FURTHER INVESTIGATION REVEALED THAT THE IMPROPER PART NUMBER BALL JOINT HAD BE EN INSTALLED WHICH HAD NO SAFETY LOCKING FEATURES, THIS ALLOWED THE ROD END BEARING TO ROTATE AND DISCONNECT. THE CONTR OL CABLE WITH CORRECT PART NUMBER BALL JOINT WAS INSTALLED WITH PROPER SAFETY. THE OPERATOR ISSUED AN FCD TO INSPECT AL 2 L 7 2 4T RT A52EU 1999021900611 19990219 00611 NM 1999 2 19 TSAA9927007 1 19990105 A 2761 654456113 ACTUATOR BOEING 737 737297 1384480 NM NR 6 SPOILER LEAKING A TSAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 13 726AL 33108 22426 FLT 107 - OGG - HNL - DURING APPROACH TO HNL, 'A' HYDRAULIC SYSTEM FAILED DUE TO SLOW LOSS OF HYDRAULIC FLUID. QRH PROC EDURES PERFORMED. DECLARED EMERGENCY AND STOPPED ON RUNWAY. AIRCRAFT TOWED TO GATE. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR DUE TO ACTUATOR CASE LEAKING. COMPLIED WITH MM 27-61-51. REMOVED AND REPLACED 'A' SYSTEM CASE DRAIN FILTERS. RUN ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999021900612 19990219 00612 WP 1999 2 19 ARWA990108 1 19990116 A 2731 ARM DOUG DC8 DC863F 302198F WP ELEVATOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 MIA - FLT 617 - PERFORMED ELEVATOR CHECK, FELT NO RESISTANCE ON YOKE. EPI DOES NOT MOVE. TROUBLE SHOT FOUND LEFT ELEVA TOR GEAR TAB CRANK ARM ASSEMBLY INBOARD AND OUTBOARD BROKEN. REMOVED AND REPLACED BOTH INBOARD AND OUTBOARD ARM ASSEMBL IES. OPS NORMAL IAW MM 27-30-1. (M) 2 L 7 4 4F 4A25 1999021900613 19990219 00613 1999 2 19 ARWA9900109 4 19990118 A 3425 2588371901 INDICATOR DOUG DC8 DC862F 3021972 WP COCKPIT HSI MALFUNCTIONED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 791AL 8070240 46150 MIA - FLT 617 - CAPTAINS COURSE BAR WILL STAY CENTERED WITHIN 25 DEGREES OF COURSE. REPLACED CAPTAINS HSI INDICATOR, OP S NORMAL IAW MM 34-52-0. (M) 2 L 7 4 4F 4A25 1999021900614 19990219 00614 WP 1999 2 19 USAA990001 1 19990107 A 5240 PAN DOUG DC9 DC931 3022065 WP SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933VJ 79062 47216 PIT - DURING C-CHECK, FOUND 1 INCH CRACK IN FORWARD SERVICE DOOR PAN AFT SIDE AT HORIZONTAL BEAM END NR 6. INSTALLED PA N SPLICE (-39) PER SRM 52-05 FIG 27. (M) 2 L 7 2 4F A6WE 1999021900615 19990219 00615 WP 1999 2 19 USAA990000 1 19990107 A 5240 59100841 PAN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933VJ 79062 47216 PIT - DURING C-4 CHECK, FOUND 1.5 INCH LONG CRACK IN SERVICE DOOR PAN AT NR 6 HORIZONTAL BEAM AFT END. SPLICED IN NEW P AN SECTION PER SRM 52-05 FIG 27 VIEW T-T. (M) 2 L 7 2 4F A6WE 1999021900616 19990219 00616 NM 1999 2 19 P2EA99006 1 19990107 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 1064 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - STRINGER 9RT CRACKED AT BS 1064, WL 270.5, RBL 45. DEFECT SIZE, LENGTH .25 INCH. REPAIRED STRINGER 9RT BETWEEN B S 1056 AND BS 1067 PER SRM 10-3 FIG 2. (M) 2 L 7 2 4F A16WE 1999021900617 19990219 00617 NM 1999 2 19 P2EA99003 1 19990113 A 5330 SKIN BOEING 737 737205 NM BS 380 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 MDW - FLT 374 - AIRCRAFT SKIN DAMAGED BY BAGGAGE TUG (CART) AT STATION 380 RT, WL 185. REPAIRED PER SRM 53-30-3, FIG 1. (M) 2 L 7 2 4F A16WE 1999021900620 19990219 00620 CE 1999 2 19 99ZZZM131 1 19990103 A 2121 66001651 BLOWER LEAR 25 25 5170506 CE COCKPIT FAILED A EXOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 17 20HJ 024 AFTER DEPARTURE FROM BCT, CREW NOTICED ELECTRICAL BURNING ODOR IN COCKPIT/CABIN. DIVERTED TO FXE. FOUND COCKPIT AIRCON DITIONING BLOWER FAN DISTORTED AND JAMMED AGAINST HOUSING. CAUSE UNKNOWN. (M) 2 L 7 2 4J A10CE 1999021900685 19990219 00685 NM 1999 2 19 AALA990091 1 19990114 A 5311 FRAME BOEING 727 727223 1384074 NM BS 970 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 843AA 20984 TUL - INSTALLED DOUBLER PER SRM 51-40-3, DOUBLER .071 7075 T-6, INSTALLED WITH 3 ROW OF 12 EACH .1875 HI-LOCKS. (M) 2 L 7 3 4F A3WE 1999021900686 19990219 00686 NM 1999 2 19 AALA990088 1 19990120 A 5730 SKIN BOEING 727 727223 1384074 NM WS 830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - WING LOWER SKIN CORRODED ON LOWER SURFACE STATION 830 LBL 30 INCHES TO LBL 32 INCHES. REPAIRED CORRODED AREA PER 57-30-3 PAGE 27 FIG 10 (SHEET 3). (M) 2 L 7 3 4F A3WE 1999021900687 19990219 00687 NM 1999 2 19 AALA990090 1 19990115 A 5312 BULKHEAD BOEING 727 727227 1384078 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - 870 BULKHEAD CRACKED AT THE LOAD CONTROL VALVE CUT OUT, 5 O'CLOCK POSITION. STOP DRILLED CRACK TO .250 INCH FABRI CATED AND INSTALLED DOUBLER AND TRIPLER AROUND CUT OUT PER SRM 53-10-2 PAG 26. (M) 2 L 7 3 4F A3WE 1999021900688 19990219 00688 NM 1999 2 19 AALA990089 1 19990113 A 5720 BRACKET BOEING 727 727227 1384078 NM WS 513 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - FOUND CORROSION ON INBOARD SIDE OF OUTBOARD MOUNT BRACKET FOR NR 3 LE SLAT ACTUATOR. INSTALLED NEW MOUNT BRACKET ON INBOARD SIDE OF OUTBOARD MOUNT BRACKET NR 3 SLAT ACTUATOR. (M) 2 L 7 3 4F A3WE 1999021900689 19990219 00689 NM 1999 2 19 AALA994023 1 19990122 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - FLOORBEAM AT STATION 347 HAD CORROSION BLENDED. FABRICATE REPAIR STRAP. ALODINE ALL BARE ALUMINUM SURFACES. FIN ISH BLEND AND REPAIR PARTS WITH 2 COATS PRIMER. INSTALL STRAP WET WITH SEALANT. (M) 2 L 7 2 4F RT A1NM 1999021900690 19990219 00690 NM 1999 2 19 AALA994022 1 19990128 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 797 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - FLOORBEAMS AT LBL AND RBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLEND OUT CORROSION AND ROTO PEEN THE REWOR KED AREA PER SRM. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLEND AREAS WITH 2 COATS PRIMER. FILL BLENDS WITH BMS 5- 95. (M) 2 L 7 2 4F RT A1NM 1999021900691 19990219 00691 NM 1999 2 19 AALA993041 1 19990128 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 906 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - FLOORBEAM AT LBL 54.81 STATION 906 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLEND OUT CORROSION AND ROTO PEEN THE REWORKED AREA PER SRM. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDED AREAS WITH 2 COATS PRIMER. FILL BLENDS WIT H BMS5-95. (M) 2 L 7 2 4F RT A1NM 1999021900692 19990219 00692 NM 1999 2 19 AALA994020 1 19990129 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - FLOORBEAM AT STATION 347 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINE AND FINISH THE BLENDED AREAS WITH 2 COA TS PRIMER. FILL BLENDS WITH BMS5-95 AND INSTALLED SKIN AS REQUIRED. (M) 2 L 7 2 4F RT A1NM 1999021900693 19990219 00693 NM 1999 2 19 AALA994019 1 19990128 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 797 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - FLOORBEAMS AT LBL AND RBL 33 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLEND OUT CORROSION AND ROTO PEEN THE REWOR KED AREA PER SRM. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDED AREAS WITH 2 COATS PRIMER. FILL BLENDS WITH BMS5 -95. (M) 2 L 7 2 4F RT A1NM 1999021900694 19990219 00694 NM 1999 2 19 AALA994018 1 19990201 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 764 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - FLOORBEAM AT STATION 764 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINE ALL BARE ALUMINUM SURFACES FINISH BLEND ED AREAS WITH 2 COATS OF PRIMER. FILL BLEND WITH BMS5-95. (M) 2 L 7 2 4F RT A1NM 1999021900695 19990219 00695 NM 1999 2 19 AALA994017 1 19990128 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND SRM LIMITS. ACCOMPLISHED IAW SKETCHES. ALODINE AND PRIME S TRAP TO INSTALL. (M) 2 L 7 2 4F RT A1NM 1999021900696 19990219 00696 NM 1999 2 19 AALA994015 1 19990201 A 5347 SEAT TRACK BOEING 767 767323 1385205 NM BS 740-746 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 381AN 25450 AFW - SEAT TRACKS AT RBL AND LBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINE ALL BARE ALUMINUM SURFACES. FINIS H WITH 2 COATS PRIMER. FILL BLENDS WITH BMS5-95 AFTER SHIMMING PER SRM. (M) 2 L 7 2 4F RT A1NM 1999021900697 19990219 00697 WP 1999 2 19 ORJA9909 1 19990114 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 IN RNO - AFT LEFT EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. REPLACED AFT LEFT EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999021900698 19990219 00698 WP 1999 2 19 ORJA9910 1 19990115 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP ROW 20 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO - EMERGENCY EXIT ROW LIGHTS AT SEAT 12, 13, 14, 15 CAME ON COULD NOT EXTINGUISH. REMOVED AND REPLACED BATTERY CH ARGER AT SEAT 20A, SYSTEM OPS CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 1999021900700 19990219 00700 WP 1999 2 19 ORJA9914 1 19990114 A 3350 1001191 LIGHT DOUG DC9 DC987 3022087 WP ROW 2 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY LIGHT INOPERABLE AT ROW 2. REPLACED EMERGENCY LIGHT CABLE ASSEMBLY AT 2 DF. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 1999021900701 19990219 00701 WP 1999 2 19 AALA990066 1 19990114 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1501-1521 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON LONGERON 32R UNDER HAT SECTION. REPAIRED PER ESO 7349 DATED 01-14-99. (M) 2 L 7 3 4F A22WE 1999021900702 19990219 00702 WP 1999 2 19 AALA990075 1 19990114 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1521 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON LONGERON 31R UNDER HAT SECTION. REPAIRED PER SRM VOL 1 53-10-00. (M) 2 L 7 3 4F A22WE 1999021900703 19990219 00703 NM 1999 2 19 AALA990057 1 19990109 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1000-1020 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - SPLICE STRAP CORRODED BETWEEN STRINGER 29L AND STRINGER 30. CUTOUT CORRODED SPLICE STRAP AND REPAIRED PER ESO 116 97 DATED 1/8/99. 2 L 7 3 4F A3WE 1999021900704 19990219 00704 NM 1999 2 19 99ZZZM135 1 19990109 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1000-1020 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - SHEAR TIE CORRODED BETWEEN STRINGER 29L AND STRINGER 30. CUT OUT CORRODED LEG SHEAR TIE. FABRICATED AND INSTALL REPAIR ANGLE SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999021900705 19990219 00705 NM 1999 2 19 99ZZZM136 1 19990109 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1000-1020 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - SKIN CORRODED BETWEEN STRINGER 29L AND STRINGER 30 BOTH SIDES. CUT OUT CORRODED DAMAGED AREA. FABRICATED REPAIR DOUBLER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999021900706 19990219 00706 NM 1999 2 19 AALA990058 1 19990106 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1151-1156 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - FOUND STRINGER 30 CORRODED FROM STATION 1151 TO STATION 1156. INSTALLED .090 J-DOUBLER OF 7075-T6 STRINGER 30 STA TION 1148-1158 WITH 5 FASTENERS EACH SIDE OF DAMAGE PER 53-10-3 SRM. (M) 2 L 7 3 4F A3WE 1999021900707 19990219 00707 NM 1999 2 19 AALA990059 1 19990109 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - SHEAR TIE CORRODED STATION 1130 BETWEEN STRINGER 29 LEFT AND STRINGER 30 AFT CARGO REF E58-0132199. REMOVED AND R EPLACED WITH NEW SHEAR TIE SUPPORT ANGLE IAW CH SRM 51-30-3. (M) 2 L 7 3 4F A3WE 1999021900708 19990219 00708 NM 1999 2 19 AALA990060 1 19990109 A 5330 SKIN BOEING 727 727223 1384074 NM BS 586-596 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 882AA 21521 TUL - FOUND SKIN GOUGED AND DENTED FROM STRINGER 26R TO 27L FROM STATION 586 TO STATION 596. REMOVED DAMAGE. INSTALLED DOUBLERS, TRIPLER, AND QUADRUPLER PER ESO 11697 DATED 1-4-99. (M) 2 L 7 3 4F A3WE 1999021900710 19990219 00710 NM 1999 2 19 AALA990049 1 19990111 A 2750 ORING BOEING 727 727223 1384074 NM TE FLAP FAILED A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 849AA 20990 DFW - FLT 1503 - EN ROUTE DFW-MCI, DURING TAKEOFF WHILE PERFORMING FLAP RETRACTION LOSS ALL SYSTEM 'A' PRESSURE AND QUAN TITY. RETURNED DFW AND MANUALLY EXTENDED LANDING GEAR, LANDED DFW WITHOUT INCIDENT. REPLACED INBOARD FLAP DRIVE MOTOR. REPLACED FILTERS AND FLUSHED SYSTEM ACCORDING TO MM. REPLACED HYDRAULIC PUMP ON NR 1 ENGINE. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999021900711 19990219 00711 WP 1999 2 19 AALA990097 1 19990122 A 2450 5D03541 RELAY DOUG DC9 DC982 3022082 WP E/E BAY FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7518A 49895 DFW - FLT 1329 - DURING CLIMB-OUT, AIRCRAFT EMERGENCY BUS OFF LIGHT ILLUMINATED AND CAPTAINS INSTRUMENTS WENT BLANK. TH E FIRST OFFICER SMELLED SMOKE IN THE COCKPIT. AIRCRAFT AIR INTERRUPTED AND RETURNED DFW AND LANDED OVERWEIGHT WITHOUT F URTHER INCIDENT. MAINTENANCE FOUND EMERGENCY POWER TRANSFER RELAY FAULTY. REPLACED EMERGENCY POWER TRANSFER RELAY. AC COMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO FINDINGS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021900712 19990219 00712 WP 1999 2 19 AALA990098 1 19990125 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 485AA 49678 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS IN FORWARD COACH CABIN INOPERATIVE. REPLACED EMERGENCY E XIT PATH LIGHT JUMPER WIRE BETWEEN FIRST CLASS AND COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021900713 19990219 00713 NM 1999 2 19 AALA994003 1 19990108 A 5314 KEEL BEAM BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 303AA 22309 AFW - LEFT KEEL BEAM HAS CORROSION REMOVAL. REMOVED ALL CORROSION AND REFINISH THE SURFACE PER SRM. INSTALL SHIMS/WASH ERS BETWEEN THE FLANGE AND THE RETAINER TO PREVENT FASTENER PULL UP AND SEAL THE AREA WITH BMS5-95. (M) 2 L 7 2 4F RT A1NM 1999021900714 19990219 00714 NM 1999 2 19 AALA994004 1 19990111 A 5313 STRINGER BOEING 767 767223 1385123 NM BS 1400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 303AA 22309 AFW - STRINGER 35L AT APPROX STATION 1400 WAS CORRODED AT PRODUCTION SPLICE. CUT AND REMOVE CORRODED SECTION. ALODINE AND PRIME ALL BARE ALUMINUM. INSTALL NEW SPLICE AND REPAIR PER SKETCHES. (M) 2 L 7 2 4F RT A1NM 1999021900715 19990219 00715 WP 1999 2 19 AALA990105 1 19990124 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 579AA 53156 ORD - FLT 2015 - AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED A STRONG BURNING SMELL IN COACH CABIN. BURNING SMELL DISSIPAT ED ALMOST IMMEDIATELY AND DID NOT REOCCUR. FLIGHT CONTINUED TO ORD WITHOUT FURTHER INCIDENT. AS A PRECAUTIONARY, MAINT ENANCE REMOVED AND REPLACED COALESCER BAGS AND PERFORMED PACK BURN OUT PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATI ON. (M) 2 L 7 2 4F A6WE 1999021900716 19990219 00716 NM 1999 2 19 AALA990052 1 19990101 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 940 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - FOUND FASTENER HOLES DAMAGED 16 AFT OF STATION 940 IN STRINGER 18A, LEFT SIDE. OVERSIZED 16 FASTENER HOLES TO STD .3125 INCH AFT OF STATION 940 IN STRINGER 18A INSTALLED 16 BOLTS O/S PR ESO 11697 DATED 12-23-98. (M) 2 L 7 3 4F A3WE 1999021900717 19990219 00717 NM 1999 2 19 AALA990094 1 19990118 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 843AA 20984 TUL - STRINGER 26 LEFT INBOARD LEG CORRODED UNDER FLANGE STATION 560. INSTALLED STRINGER SPLICE PER SRM 53-10-3, (M) 2 L 7 3 4F A3WE 1999021900718 19990219 00718 NM 1999 2 19 AALA990093 1 19990113 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 527 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 843AA 20984 TUL - FOUND CORROSION ON STRINGER 27 LEFT AT STATION 527. INSTALLED STRINGER REPAIR AT STRINGER 27 LT STATION 527 PER S RM 53-10-3. (M) 2 L 7 3 4F A3WE 1999021900719 19990219 00719 NM 1999 2 19 AALA990092 1 19990113 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 483-486 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 843AA 20984 TUL - FOUND STRINGER 28R CORRODED. DRILLED NEW PRODUCTION SPLICE. INSTALLED PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999021900720 19990219 00720 EU 1999 2 19 SIMA990121 1 19990112 A 5330 SKIN AEROSP ATR72 ATR72212A 8680902 EU BS 3/4 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 540AM 540 ABI - DURING A VISIT INSPECTION, FOUND A DENT ON RIGHT FORWARD FUSELAGE SKIN PANEL BETWEEN FRAMES 3 AND 4. CUT OUT DAMA GED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATION OF CRACKS. APPLIED ALODINE TO EDGES OF CUT OUT. F ABRICATED AN EXTERNAL DOUBLER .050 THICK. TREATED AREA AND ATTACHED TO FUSELAGE. RESTORED SURFACE FINISH. (M) 2 H 7 2 4T RT A53EU 1999021900721 19990219 00721 EU 1999 2 19 SIMA990131 1 19990113 A 5330 SKIN AEROSP ATR72 ATR72212 EU BS 11/12 PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 ABI - PERFORM PERMANENT REPAIR OF PUNCTURE ON RT FORWARD FUSELAGE BETWEEN FRAMES 11 AND 12 AND BETWEEN STRINGER 19 AND 2 0. CUT OUT DAMAGED SKIN AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. REMOVED DAMAGED INTERC OSTAL. FABRICATED AN EXTERNAL DOUBLER .050 THICK ALSO FABRICATED INTERCOSTAL FROM AL 7075-0 AND HEAT TREATED TO 7075-T6 . APPLIED ALODINE TO CUT OUT EDGES. ALODINE AND ONE COAT EPOXY APPLIED TO DOUBLER AND INTERCOSTAL. INSTALLED ON AIRCR AFT, RESTORED SURFACE FINISH. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021900722 19990219 00722 EU 1999 2 19 99ZZZM137 1 19990113 A 5320 S53172222210 INTERCOSTAL AEROSP ATR72 ATR72212 EU BS 11/12 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 ABI - PERFORM PERMANENT REPAIR OF PUNCTURE ON RT FORWARD FUSELAGE BETWEEN FRAMES 11 AND 12 AND BETWEEN STRINGER 19 AND 2 0. CUT OUT DAMAGED SKIN AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. REMOVED DAMAGED INTERC OSTAL. FABRICATED AN EXTERNAL DOUBLER .050 THICK ALSO FABRICATED INTERCOSTAL FROM AL 7075-0 AND HEAT TREATED TO 7075-T6 . APPLIED ALODINE TO CUT OUT EDGES. ALODINE AND ONE COAT EPOXY APPLIED TO DOUBLER AND INTERCOSTAL. INSTALLED ON AIRCR AFT, RESTORED SURFACE FINISH. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021900723 19990219 00723 EU 1999 2 19 SIMA990094 1 19990109 A 3240 BRAKE AEROSP ATR72 ATR72212 EU MLG INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 270AT 270 MIA - FLT 5799 - FIRST OFFICERS BRAKES INOPERATIVE. BLED BRAKE SYSTEM. FUNCTIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999021900726 19990219 00726 EU 1999 2 19 SIMA990223 1 19990122 A 3240 50125873 BRAKE SAAB SF340 340B 7860101 EU LT MLG LEAKING A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 903AE OCT900500 340B282 BYW - FLT 5661 - WHEN PARKING AT THE GATE, THE HYDRAULIC CWP CAME ON. BOTH MAIN HYDRAULIC AND BRAKE PRESSURE INDICATION WENT TO ZERO. PUDDLE OF HYDRAULIC FLUID FOUND UNDER LEFT MAIN LANDING GEAR. REMOVED AND REPLACED LEFT OUTBOARD BRAKE ASSY DUE TO LEAKAGE FROM ONE OF THE PISTONS. SERVICED HYDRAULIC SYSTEM AND RETURNED TO AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999021900727 19990219 00727 EU 1999 2 19 SIMA990253 1 19990125 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 284AE 340B284 ABI - DURING MBV INSPECTION, A CHAFE WAS FOUND ON THE RT NACELLE FIRE FLOOR ATTACHMENT ANGLE TO INNER SKINS. REMOVED AN D REPLACED CHAFED FASTENER. FABRICATED AND ANGLE .040 THICK. NESTED THE ANGLE INTO THE EXISTING ANGLE. INSTALLED ANGL ES USING CR3523-6 FOR THE VERTICAL FLANGE OF THE ANGLES AND MS20615-6M FOR THE FASTENERS THROUGH THE FIRE FLOOR. RESTOR ED SILICON SEALING USING DOW CORNING DC730. NEGLIGIBLE CHANGE IN WEIGHT AND BALANCE. WORK DONE IAW SAAB REPAIR STATEME NT. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999021900728 19990219 00728 NE 1999 2 19 99ZZZM138 2 19990109 A 7200 ENGINE BOEING 727 72751C 1384015 NM PWA JT8 JT8D7B 52053 NE NR 1 DAMAGED A RYNA K NONE C F.O.D. IN INSP/MAINT 1 CE 07 413EX 19206 657337 NR 1 ENGINE HAS FOREIGN OBJECT DAMAGE AS FAR BACK AS C-7. AIRCRAFT WILL FERRY TO MIA FOR ENGINE CHANGE. NR 1 ENGINE WI LL BE REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999021900730 19990219 00730 NE 1999 2 19 99ZZZM140 2 19990108 A 7230 ENGINE BOEING 727 727151C 138404V NM PWA JT8 JT8D7B 52053 NE NR 1 DAMAGED A RYNA K NONE C F.O.D. IN INSP/MAINT 1 CE 07 432EX 19867 654099 FLT 645 - PHL - NR 1 ENGINE HAS C-1 AND C-2 DISK FOREIGN OBJECT DAMAGE, FOUND DURING MAINTENANCE DURING A DAILY SERVICE CHECK. FERRIED TO IND FOR MAINTENANCE. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999021900731 19990219 00731 NE 1999 2 19 99ZZZM141 2 19990107 A 7230 ENGINE BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 2 DAMAGED A RYNA O OTHER C F.O.D. LD LANDING 1 CE 07 421EX 19099 654329 AFTER LANDING AT LCQ, FOUND NR 2 ENGINE HAS FOREIGN OBJECT DAMAGE AS FAR BACK AS C-4 POSSIBLY MORE. NR 2 ENGINE WILL BE REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999021900734 19990219 00734 NM 1999 2 19 99ZZZM144 1 19990110 A 3350 900542 BATTERY PACK BOEING 727 727243 138408D NM CABIN DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 521DB 21266 FLT 441 MIA - VARIOUS EMERGENCY EXIT LIGHTS IN CABIN INOPERATIVE. REMOVED AND REPLACED VARIOUS EMERGENCY EXIT LIGHT POW ER SUPPLIES, FOUR BATTERY PACKS. 2 L 7 3 4F RT A3WE 1999021900735 19990219 00735 WP 1999 2 19 AALA990050 1 19990112 A 3232 59390745501 ACTUATOR DOUG DC9 DC982 3022082 WP LT MLG DOOR MALFUNCTIONED A AALA L ABORTED APPROACH J WARNING INDICATION CR CRUISE 1 SW 07 488AA 0075 49681 ORD - FLT 1556 - EN ROUTE LAS-ORD, AFTER BRINGING HYDRAULIC PUMPS TO OFF AND LOW, THE LEFT GEAR INDICATION RED LIGHT ILL UMINATED. LIGHT WENT OUT AND STAYED OUT AFTER RECYCLING HYDRAULIC PUMPS TO HIGH AND THEN TO LOW. LIGHT STAYED OUT FOR REMAINDER OF FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED LEFT GEAR DOOR ACTUATOR. ACCOMPLISHED LEAK CHECKS AND CHEC KED AND ADJUSTED LEFT MAIN GEAR UP AND LATCHED PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021900736 19990219 00736 WP 1999 2 19 AALA990067 1 19990114 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1401-1441 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION AT STRINGER 30 AT FUSELAGE RT ABOVE WING SURFACE STATION 1401 TO STATION 1441. REMOVED CORROSION IN STRINGER 30 AND INSTALLED SPLICE REPAIR PER SRM 53-10-60 VOL 1. (M) 2 L 7 3 4F A22WE 1999021900738 19990219 00738 NM 1999 2 19 TWAA9902501 1 19990214 A 3350 767 BULB BOEING 757 757231 1384950 NM R1 DOOR FAILED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 716TW 28484 THE EXTERIOR EMERGENCY LIGHT AT THE RIGHT SIDE NUMBER 1 DOOR WAS INOPERATIVE. REPLACED THE LAMP. 2 L 7 2 4F RT A2NM 1999021900739 19990219 00739 WP 1999 2 19 AT9900126 1 19990128 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION BULGED AT STA 937 L-26R. MECHANICALLY REMOVED CORROSION, FASTEN ERS AND DOUBLER. FABRICATED AND INSTALLED FASTENERS, DOUBLER IAW DC9 SRM 51-30-5, 51-30-2, 51-20-0, AND RES NR 99301. 2 L 7 2 4F A6WE 1999021900740 19990219 00740 WP 1999 2 19 AT9900127 1 19990121 A 5310 STRUCTURE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE FORWARD AND AFT CARGO COMPARTMENT. LOCATIONS ARE AS FOLL OW: CARGO DOOR FRAME LOWER EDGE AT STA 340 TO 427, FRAME STA 522 L-28L TO L-28R, AFT CARGO WEB STA 870 L-29R ON LEFT AN D RIGHT SIDE, AFT CARGO FRAME (SHEAR TIE) AFT SIDE STA 887 L-27L TO L-29R, AND AFT CARGO FRAME STA 965 L-28L TO L-28R AF T SIDE. MECHANICALLY REMOVED CORROSION, FABRICATED AND FORMED DOUBLERS, FRAME, INTERCOSTAL, ANGLES, CLIPS, SPLICE AND P LATES. HEAT TREATED, DRILLED, DEBURRED, PRIMED AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-10-3, 51-30-2, 51-30-5 , 53-03 FIG 2A, 51-10-2A, 53-11-3 FIG 12. SPLICE (P/N 1A-42022-1) OFF, (P/N 1A-42021-1), (P/N 1A-42020-1). 2 L 7 2 4F A6WE 1999021900741 19990219 00741 WP 1999 2 19 AT9900128 1 19990128 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 237, 560, 579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON LONGERONS AT STA 237 L-30 AND STA 560 TO STA 579 L-30. ALSO, CORRODED RIVETS AT T-CAP AT STA 598 L-24L TO L-24R. REMOVED AND REPLACED FASTENERS ON T-CAP, TREATED CORROSION, CUT OU T DAMAGE LONGERON SECTION, FABRICATED ANGLES, SPLICES, FINGER DOUBLERS AND INSTALLED IAW DC9 SRM 53-02 FIG 14, 51-10-3, 51-10-5, 53-02 FIG 2A, 51-30-2, 53-11-3, 51-10-2, AND 53-01 FIG 1. ANGLES AND SPLICE (P/N 1A-42057-1, 2) (P/N 1A-42056- 1), (P/N 1A-42059-1). 2 L 7 2 4F A6WE 1999021900742 19990219 00742 WP 1999 2 19 AT9900129 1 19990129 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 945 & 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND ON CUSP MEMBRANE AT RIGHT OUTBOARD STA 945 AND STA 965 CUSP A7. REMOVED CORROSION AND FABRICATED DOUBLERS AND FILLER IAW DC9 SRM 51-30-2, 51-10-3, 53-20-1. DOUBLER (P/N 1A-42076- 1) OFF. 2 L 7 2 4F A6WE 1999021900743 19990219 00743 WP 1999 2 19 AT9900130 1 19990114 A 5310 STRUCTURE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION. FIRST, AT STA 602 LONGERON L-29L. SECO NDLY, THE AFT PIT FORWARD SIDE AT STA 382 BETWEEN L-29R TO L-27L. THIRD, THE LEFT LAVATORY BULKHEAD LOWER PORTION AT ST A 965. LAST, CORROSION AROUND FASTENERS HOLES ON THE FLOORBEAM AT STA 996. REMOVED AND REPLACED FASTENERS, CLEANED COR ROSION, REMOVED DAMAGE FRAME SECTION, FABRICATED ANGLES, LONGERON, HEAT TREATED, PRIMED, AND INSTALLED ALL PARTS IAW DC9 SRM 51-10-2A, 51-10-3, 51-30-5, 51-30-2, 51-10-4, 51-10-1, 51-20-0, 53-05 FIG 20A. SPLICE (P/N 1A-34249-2) OFF, ANGLE (P/N 52912758-12000). 2 L 7 2 4F A6WE 1999021900744 19990219 00744 EU 1999 2 19 MALA976350 1 19990212 A 3610 VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT BLEED AIR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 456XJ 456 ON CLIMB, RIGHT BLEED AIR LEAK LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED PRESSURE REG SHUTOFF VALVE, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1999021900745 19990219 00745 EU 1999 2 19 MALA976351 1 19990212 A 3020 A00051 MODULE SAAB SF340 340B 7860101 EU LT ENG DEICE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 417XJ 340B417 LEFT INTAKE HEAT LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED DEICE MODULE, ALL CHE CKS GOOD. 2 L 7 2 4T RT A52EU 1999021900746 19990219 00746 NE 1999 2 19 MALA976352 2 19990211 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 408XJ 408 AT 17,000 FT, IN ICING CONDITIONS UPON APPROACH TO RFD THE NR 1 ENG EXPERIENCED A ROLLBACK WITH NO SHIFT IN DELTA DELTA T. ENGINE OPERATED WITHIN LIMITS PER GE MAINTENANCE MANUAL 72-00-00 PG 148 TROUBLE 5. 2 L 7 2 4T 4 T RT A52EU E8NE 1999021900747 19990219 00747 EU 1999 2 19 MALA976353 1 19990211 A 3350 ELB035 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 41XJ 041 CABIN EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACKS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999021900748 19990219 00748 EU 1999 2 19 MALA976354 1 19990211 A 5320 SKIN SAAB SF340 340B 7860101 EU BS 339-608 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 422 EO FOR GENERIC REPAIR FOR DENTS IN CABIN SKIN BETWEEN STA 339 TO 389 AND 487 TO 608 ONLY. THIS DOUBLER/TRIPLER REPAIR I S USED WHEN THE REPAIR FASTENERS OVERLAP THE CENTER CABIN .050 WINDOW REINFORCEMENT DOUBLER THAT IS BONDED TO THE FUSELA GE SKIN. MAINTENANCE APPLIED ALODINE 1200S TO EDGES OF CUTOUT. FAY SEAL THE EXTERNAL DOUBLERS ACCORDING TO CH 51-20-50 . INSTALLED EXTERNAL REINFORCEMENTS. PICK UP EXISTING RIVETS IN AFFECTED FRAMES AND STRINGERS. INSTALLED RIVETS ACCOR DING TO CH 51-40-21. FILLET SEAL ALL EDGES OF THE DOUBLERS IN ACCORDANCE WITH CH 51-20-56. 2 L 7 2 4T RT A52EU 1999021900749 19990219 00749 NM 1999 2 19 UPS99228733 1 19990216 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM L1 DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, L1 DOOR INTERIOR (FOOT LEVEL EMER LIGHT WILL NOT TEST). REMOVED AND REPLACED L1 BATTER PACK, TEST OK. 2 L 7 3 4F A3WE 1999021900750 19990219 00750 NM 1999 2 19 UPS99228734 1 19990208 A 3350 SWITCH BOEING 727 72725C 138400H NM CABIN DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, EMERGENCY LIGHTS DISARM SWITCH STICKS WHEN SELECTED OFF. LIGHT CAME ON ABOUT 3 MIN AFTER SWITCH SE LECTED OFF. CLEANED EMERGENCY LIGHT SWITCH, OPS GOOD. 2 L 7 3 4F A3WE 1999021900751 19990219 00751 NM 1999 2 19 UPS99228735 1 19990210 A 3350 CIRCUIT BREAKER BOEING 727 72725C 138400H NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, EMERGENCY LIGHTS ON WHILE IN ARMED POSITION. ILLUMINATED IN FLIGHT, DISARMED, CHECKS OK. REPLACED CIRCUIT BREAKER EMERGENCY EXIT LIGHT, OPS CK NORM. 2 L 7 3 4F A3WE 1999021900752 19990219 00752 WP 1999 2 19 UPS99828732 1 19990216 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS, OPS CKS OK. 2 L 7 4 4F RT 4A25 1999021900753 19990219 00753 WP 1999 2 19 UPS99828736 1 19990211 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE-N/A, EMER EXIT LIGHT INOP. REMOVED AND REPLACED EMER LIGHT BATTERY PACK PER M/M 33-50-01. (P/N T91189) , (S/N 7). 2 L 7 4 4F RT 4A25 1999021900754 19990219 00754 WP 1999 2 19 UPS99828737 1 19990214 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE-N/A, DURING EMER LIGHT BATTERY TEST ALL EMERGENCY LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED EME R BATTERY PACK PER MM 33-50-01, OPS CKS GOOD. 2 L 7 4 4F RT 4A25 1999021900755 19990219 00755 WP 1999 2 19 UPS99828738 1 19990212 A 3350 CIRCUIT BREAKER DOUG DC8 DC871F 302199D WP CABIN TRIPPED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-N/A, EMERG EXIT LIGHTS WILL NOT DISARM. RESET EMER EXIT LIGHT CIRCUIT BREAKER, OPS CKS GOOD. 2 L 7 4 4F RT 4A25 1999021900756 19990219 00756 EU 1999 2 19 QXEA9900289 1 19990211 A 3350 900542 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU ROW 1-4 DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 SEA- ROW 1 TO 4 EMERGENCY LIGHTS REMAIN ON WHEN NR 3 GENERATOR AND EXTERNAL POWER OFF. INSPECTED AND FOUND POWER SUPPLY UNIT UNDER SEAT ROW 1AB TO BE DAMAGED. REPLACED POWER SUPPLY UNIT AND CONTROL CIRCUITRY MOUNT, OP CK GOOD. 2 L 7 2 4F RT A20EU 1999021900757 19990219 00757 NM 1999 2 19 99FDEA00062 1 19990217 A 5313 STRINGER BOEING 727 7272D4 138407U NM BS 440 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 UPPER LOBE BS 440 STRINGER 8L TOP OF STRINGER GOUGED. BLENDED OUT GOUGE, OUT OF LIMITS. INSTALLED DOUBLER PER SRM 53-1 0-3 FIG 2. 2 L 7 3 4F A3WE 1999021900758 19990219 00758 NM 1999 2 19 99FDEA00063 1 19990217 A 5315 FLOORBEAM BOEING 727 7272D4 138407U NM BS 1148 & 1166 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 TWO DOUBLE DRILL HOLES BS 1130, LBL 25, 30 AND DOUBLE DRILL HOLES BS 1148 AND 1166. REPAIRED DAMAGE TO FLOORBEAMS DUE T O DOUBLE DRILL HOLES PER EA 7-5310-42962. TREATED AND PRIMED PER 51-20-0. 2 L 7 3 4F A3WE 1999021900759 19990219 00759 NM 1999 2 19 99FDEA00064 1 19990217 A 5315 FLOORBEAM BOEING 727 7272D4 138407U NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 UPPER LOBE, CORROSION FWD EDGE OF TOP FLANGE ON FLOORBEAM BS 1130, LBL 3 AND FLOORBEAM 1130, LBL 19 TOP FLANGE. REMOVED CORROSION WAS OUT OF LIMITS. INSTALLED FLOORBEAM REPAIR PER EA 7-5310-42947. 2 L 7 3 4F A3WE 1999021900760 19990219 00760 NM 1999 2 19 99FDEA00065 1 19990217 A 5720 ANGLE BOEING 727 7272D4 138407U NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 RT WING LWR SURFACE OF FRONT SPAR CHORD ANGLE HAS EXFOLIATED CORROSION AFT OF NR 5 L/E SLAT T DUCT. REMOVED CORROSION S PAR CHORD METAL. CORROSION BEYOND LIMITS (ORIG THICK 0.316 AFTER BLEND 0.0220). REPAIR STRAP INSTALLED ON UPPER SURFAC E OF FRONT SPAR CHORD LWR ANGLE PER AARD 57-30-00-2 PG 2 AND SRM 57-10-4 PG 1-10. 2 L 7 3 4F A3WE 1999021900761 19990219 00761 NE 1999 2 19 99UAL900085 2 19990205 A 7320 METERING UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 419UA 487 NR 1 ENGINE FUEL DRAINMAST IS LEAKING FUEL FROM THE FMU PORT IN A STEADY STREAM DURING ENGINE RUN. FUEL METERING UNIT L EAKING FROM DRAIN MAST. NOT A NEW PROBLEM. MRR NOT REQUIRED. COA IN PROCESS TO REDUCE FUEL LEAKS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999021900762 19990219 00762 GL 1999 2 19 99UAL900086 2 19990206 A 7250 TURBINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 WP 29 1836U 47968 451482 LOG READS, JUST AFTER TAKEOFF, NR 2 ENGINE FAILED. A LOUD BANG WAS HEARD AND EGT PEGGED. SHUT DOWN AND LANDED. *S/D* E NGINE WAS REPLACED. GE PRELIMINARY BORESCOPE SHOWS THAT THE ENGINE SUFFERED AN HPT STAGE 2 BLADE FAILURE. THE SUSPECT BLADES AS WELL AS SEVERAL OTHER BLADES WERE REMOVED FOR ANALYSIS AT THE GE MATERIALS LAB IN CINCINNATI, OHIO. 2 L 7 3 4F 4 F A22WE E23EA 1999021900763 19990219 00763 NM 1999 2 19 99UAL900091 1 19990201 A 2824 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL DIST MALFUNCTIONED A UALA O OTHER O OTHER UK UNKNOWN 1 WP 29 768UA 26919 UNABLE TO MOVE FUEL FROM LEFT TANK TO RIGHT. TRIED TO MANUALLY CLOSE LEFT FILL VALVES, NO HELP. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999021900764 19990219 00764 NM 1999 2 19 99UAL900092 1 19990207 A 4950 R53651 ACTUATOR GEC MARCONI R53651 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU INLET FAILED A UALA K NONE A FLAME/FIRE CR CRUISE 1 WP 29 771UA 931002 26932 P1008 APU WOULD NOT START IN THE AIR. *S/D* APU INLET DOOR ACTUATOR (R5365-1) FAILED. ACTUATOR WAS REMOVED AND REPLACED FEB 9,1999 AT IAD. OPS CHK OK. VENDOR ANALYSIS OF REMOVED UNIT INDICATED UNIT WAS COMPLETELY SEIZED. WATER WAS FOUND IN U NIT WHICH RESULTED IN UNIT SEIZURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999021900765 19990219 00765 NE 1999 2 19 99UAL900093 2 19990210 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 SMOKING A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 933UA 26659 724415 BLACK SMOKE WAS OBSERVED COMING FROM NR 1 ENGINE. *S/D* THIS WAS A NEW ENGINE INSTALLATION. POSSIBLE RESIDUAL OIL IN TH E EXHAUST PATH. NO CONFIRMED SMELLS NOTED IN CABIN. NO FUEL, OIL, OR HYDRAULIC LEAKS FOUND. NO OIL OR CARBON STREAKIN G IN THE EXHAUST. NO LEAKS FROM THE HYDRAULIC SYSTEM. NO LEAKS FROM THE WING AND PYLON AREA. ACCOMPLISHED ENGINE RUN TO 84 PERCENT N1 FOR 5 MINUTES THEN UP TO 87.5 PERCENT N1, OPS CHECK OK. NO OIL QUANTITY LOSS AFTER THE ENGINE RUN. NO REPEAT EVENTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999021900766 19990219 00766 NM 1999 2 19 99UAL900094 1 19990210 A 2613 355644310 OVERHEAT ELEMENT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 309UA 23670 RIGHT HAND WING-BODY OVERHEAT WARNING. *S/D* REPLACED THE RIGHT WING LEADING EDGE DETECTOR ELEMENT ITEM M1204, REFEREN CE MM 26-18-11 PG 401, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999021900767 19990219 00767 NM 1999 2 19 99UAL900095 1 19990211 A 2100 6067723 RT RECIRC FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 534UA 301 25129 DIVERTED TO OKC WITH PERSISTENT BURNING RUBBER ODOR IN THE CABIN. *S/D* CAUSE OF RUBBER ODOR WAS DETERMINED TO BE A FAUL TY RT RECIRCULATION FAN. THE FAN WAS REPLACED AND NO FURTHER REPORTS OF SMOKE HAVE OCCURRED SINCE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999021900768 19990219 00768 1999 2 19 99UAL900096 4 19990204 A 2565 101651303 SLIDE BF GOODRICH 101651303 BOEING 767 767322 1385200 NM DOOR 2L MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 DOOR 2L OPENED WITH SLIDE IN ARMED POSITION. SLIDE HAD PARTIAL DEPLOYMENT. *S/D* FLIGHT ATTENDANT OPENED DOOR HANDLE IN ARMED POSITION, HEARD POP SOUND WHICH WAS THE SLIDE LACES SNAPPING. SLIDE HAD DROPPED 1-2 INCHES AT WHICH TIME SHE CLO SED DOOR HANDLE. SHE BASICALLY STOPPED FULL DEPLOYMENT. THE SAFETY PIN WAS INSTALLED IN BOTTLE. THE SLIDE WAS REPLACE D. 2 L 7 2 4F RT A1NM 1999021900769 19990219 00769 WP 1999 2 19 ABXA9900099 1 19990119 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 822 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING LEADING EDGE UPPER RIB AT STATION XFS 822 CRACKED AT FASTENER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K050 56. 2 L 7 4 4F 4A25 1999021900770 19990219 00770 WP 1999 2 19 ABXA9900100 1 19990201 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 1041. REPLACED LONGERON 17 LEFT IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999021900771 19990219 00771 WP 1999 2 19 ABXA9900101 1 19990201 A 5313 5911427 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 DURING C-CHECK, FOUND LONGERON 16 RIGHT CRACKED AT STATION 1041. REPLACED LONGERON SECTION 16 RIGHT IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999021900772 19990219 00772 1999 2 19 DHL99741002 4 19990217 A 3452 6222224001 TRANSPONDER BOEING 727 7272Q9 138448M NM NR 1 & 2 INOPERATIVE A DHLA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 01 741DH 21931 TRANSPONDER NR 1 AND NR 2 INOP AS REPORTED BY ATC DURING CLIMBOUT. REMOVED AND REPLACED TRANSPONDERS PER MM 34-45-1. 2 L 7 3 4F RT A3WE 1999021900773 19990219 00773 SO 1999 2 19 SWIA971401 1 19990209 A 3060 DEICE SYST EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT PROP MALFUNCTIONED A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 212SW 120276 DURING CLIMBOUT, EXPERIENCED SEVERE ICING AND SIGNIFICANT VIBRATION ON PROPS. ADJUSTED PROP RPM SEVERAL TIMES, VIBRATIO N CONTINUED. DESCENDED INTO WARMER AIR AND THE ICE MELTED AND OPS WERE NORMAL. RETURNED TO SLC. INSPECTED SURFACE DEI CE AND PROP DEICE. PERFORMED OPERATIONAL CHECK OF ALL DEICE SYSTEMS, ALL CHECKS NORMAL. TESTED IAW 30 AND 30-60-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900774 19990219 00774 SO 1999 2 19 SWIA971402 1 19990209 A 2730 CONTROL CABLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ELEVATOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 BOTTOM RIGHT ELEVATOR CABLE SHOWING SIGNS OF WEAR AT BELLCRANK. WEAR CAUSED BY A SCREW BECOMING LODGED BETWEEN QUADRANT AND CABLE. EMBRAER MM IPC 27-31-00 ITEM 210 OF SECTION B PAGE 0 DATED JAN 10/87 SHOWS LOCATION OF QUADRANT. INSTALLED NEW CABLE ON RIGHT ELEVATOR LOWER SIDE IAW MM 27-00-01. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900775 19990219 00775 SO 1999 2 19 SWIA971403 1 19990209 A 7810 12033750401 EXHAUST PIPE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 LEFT EXHAUST PIPE HAS APPROXIMATE 8 INCH CRACK AT BREATHER TUBE. ALSO, THERMAL BLANKETS SCORCHED. INSTALLED LEFT EXHAU ST PIPE WITH SERVICEABLE UNIT PER MM 78-00-00. REPLACED THERMAL BLANKETS AS REQUIRED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999021900776 19990219 00776 NM 1999 2 19 VNAA9902008 1 19990213 A 3020 5570D01 SEPARATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 429JS 94441 3043 DURING THE TAXI OUT FOR TAKEOFF, A DEICE PRESSURE WARNING INDICATION ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND DEFERRED THE RIGHT HAND DEICE PRESSURE SENSOR, IN ACCORDANCE WITH THE DORNIER MINIMUM EQUIPMENT LIST. ON 16 FEB 99 CAK MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND WATER SEPARATOR, IN ACCORDANCE WITH DORNIER M AINTENANCE MANUAL 30-13-11. OPERATIONAL CHECKS WERE COMPLETED, AND THE DEFERRAL WAS REMOVED FROM THE AIRCRAFT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999022000003 19990220 00003 NM 1999 2 20 DL733990219 1 19990203 A 2613 OVERHEAT LIGHT BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE ILLUMINATED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 27 304WA 30585 23345 721286 ON APPROACH COS, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW DISCHARGED BOTH BOTTLES, LIGHT REMAINED ILLUMINATED EVEN AFTER ENGINE SHUTDOWN. PARTS ARRIVING FROM SLC AND DFW. REPLACED BOTH FIRE BOTTLES, FIRE TEST MODULE AND LOWER LOOP. 2 L 7 2 4F 4 F RT A16WE E2GL 1999022000004 19990220 00004 1999 2 20 SWAA990219 4 19990208 A 2312 514017 RECEIVER BOEING 737 7377H4 NM NR 1 COMM FAILED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 719SW 27853 APPROXIMATELY 10 MIN INTO FLIGHT, NR 1 COMM WOULD RECEIVE BUT NOT TRANSMIT, NR 2 WAS OK. PERFORMED AN AIR RETURN TO PHX . EVERY FREQ CHANGE (6 DIFF FREQ) TRIED. NR 1 COMM CONTINUED TO BE INOP AFTER LANDING, NR 1 COMM NOW WORKED. PERFORME D BITE CHECK OK OF BOTH NR 1, 2 COM, XCURS AND PSEU. AIR/GROUND BITE CHECKED. REMOVED AND REPLACED RECEIVER PER M/M. NR 1 RADIO OPS CHECKS AS PER MM. 2 L 7 2 4F RT A16WE 1999022000005 19990220 00005 NM 1999 2 20 SWAA990221 1 19990207 A 2612 FIRE LOOP BOEING 737 7373T0 1384582 NM APU FAILED A SWAA K NONE N FALSE WARNING CR CRUISE 1 SW 07 697SW 23838 EN ROUTE TO MDW, CREW STARTED APU AT FL250; APU FIRE LIGHT ILLUMINATED FOR APPROX 5-10 SECONDS. FIRE LIGHT EXTINGUISHED WITH NO CREW ACTION, ACCOMPLISHED QRH FOR APU FIRE. FIRE HANDLE PULLED; BOTTLE NOT DISCHARGED. INSPECTED APU FIRE LOO PS, NO DEFECTS NOTED. RERACKED FIRE DETECTION BOX PER M/M. SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1999022400002 19990224 00002 EU 1999 2 24 QXEA9900113 1 19990104 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 17065 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - AIRCRAFT SKIN AND STRUCTURE FORWARD OF ACCESS PANEL 41A TO FRAME 17065 IS DENTED AND RIPPLED FROM APPROXIMATELY ST RINGER 6 THROUGH 72 VARYING IN DEPTH UP TO .140. REPAIRED IAW FOKKER SRM 51-10-05 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999022400003 19990224 00003 EU 1999 2 24 QXEA9900119 1 19990105 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 3845 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - FLUSH SKIN REPAIR AT FRAME 3845 AND STRINGER 68A HAS BUTTON HEAD RIVETS SUBSTITUTED FOR COUNTER SUNK HEADS. REPAI RED IAW FOKKER SRM 53-02-02, PAGE 2, FIGURE 1 AND SRM 53-02-06, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1999022400006 19990224 00006 SO 1999 2 24 SWIA971404 1 19990106 A 3010 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT DEICE BOOT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 214SW 120280 CLIMBING THROUGH 5,000 FEET, LEFT OUTBOARD AND MIDDLE LEADING EDGE DE-ICE FAILURE. RECYCLED PER QRH BETWEEN TIMER 1 AND 2 WITH 5 SECONDS DELAY. THEN FAILURE OF LEFT OUTBOARD LEADING EDGE AND VERTICAL FIN DEICE. RETURNED TO FIELD. REPLAC ED LEFT MIDDLE AND LEFT OUTBOARD DE-ICE BOOT PRESSURE SWITCHES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600001 19990226 00001 WP 1999 2 26 TWAA9902601 1 19990202 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1300 BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND AFT CABIN FLOOR SUPPORT BROKEN AT STA 1300, BL 0 IN, AFT CABIN FLOOR BOARD NUMBER 94. I NSTALLED REPAIR ANGLE PER ARA 15736. 2 L 7 2 4F A6WE 1999022600002 19990226 00002 WP 1999 2 26 TWAA9902602 1 19990131 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND FUSELAGE FRAME LOWER SECTION AT STA 1322, BL 0, WITH CORROSION ABOVE STRINGER. REMOVED CORROSION PER TWA SPM 6-80-01. REPAIRED PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 1999022600003 19990226 00003 WP 1999 2 26 TWAA9902603 1 19990128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 1308-1319 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CORRODED BELOW LT FLOOR SUPPORT, BETWEEN STA 1308 AND 1319, LBL 16. INSTALL ED NEW INTERCOSTAL PER STANDARD PROCESSES MANAL 6-70-1, PAGE 3. 2 L 7 2 4F A6WE 1999022600004 19990226 00004 WP 1999 2 26 TWAA9902604 1 19990128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 1308 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL BELOW RT FLOOR TRACK AT STA 1308, RBL 16, WAS CORRODED. INSTALLED NEW INTER COSTAL PER STANDARD PROCESSES MANUAL 6-70-1, PAGE 3. 2 L 7 2 4F A6WE 1999022600005 19990226 00005 WP 1999 2 26 TWAA9902605 1 19990128 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 1212-1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 941AS 49925 DURING OP 16 MAINT CHECK, FOUND CORROSION AROUND FASTENER HOLES ON FLOOR TRACK RBL 16, BETWEEN STA 1212 AND 1271. INSTA LLED NEW FLOOR TRACK PER STANDARD PROCESSES MANUAL 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999022600006 19990226 00006 WP 1999 2 26 TWAA9902606 1 19990211 A 5510 BOLT DOUG DC9 DC931 3022065 WP LT HORIZ STAB RUSTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, THE LT UPPER HORIZ STAB FRONT SPAR CAP TO CENTER STAB BOX TIE AFT BOLT WAS EMITTING RUST FROM BARREL NUT. REPAIRED PER ARA 15737. 2 L 7 2 4F A6WE 1999022600007 19990226 00007 WP 1999 2 26 TWAA9902607 1 19990211 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT CORRODED AT STA 200, RBL 0 TO 20. MADE AND INSTALLED NEW FLOOR SUPPORT AN GLE PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999022600008 19990226 00008 WP 1999 2 26 TWAA9902608 1 19990206 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-217 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND IN GALLEY AREA CORRODED FLOOR TRACK AT RBL 44, STA 200 TO 208 AND 215 TO 217. REMOVED C ORROSION BY CUTTING SECTION OF TRACK AT STA 247. INSTALLED TRACK FROM STA 200 TO 247 WITH ALTERNATE SPLICE PER SRM 53- 05, FIG 40 PAGE 10C. 2 L 7 2 4F A6WE 1999022600009 19990226 00009 WP 1999 2 26 TWAA9902609 1 19990207 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 547 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND LIGHTNING STRIKE AT STA 547 AND 1 INCH OVER LONGERON 5L ON LT FUSELAGE. REPAIRED PER SR M 53-04, FIG 38 SHEET 7, PAGE 213. 2 L 7 2 4F A6WE 1999022600010 19990226 00010 WP 1999 2 26 TWAA9902610 1 19990211 A 5510 BOLT DOUG DC9 DC931 3022065 WP RT HORIZ STAB RUSTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, THE RT UPPER HORIZONTAL STAB FRONT SPAR CAP TO CENTER STAB BOX TIE AFT BOLT WAS EMITTING RUST FROM THE BARREL NUT. REPAIRED PER ARA 15737. 2 L 7 2 4F A6WE 1999022600011 19990226 00011 NM 1999 2 26 K3HA990013 1 19990215 A 3350 3071BPEQPL LIGHT BOEING 727 727225 1384077 NM ROW 26DEF INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 MISSING EMERGENCY PATH LIGHT AND LAMP PASSENGER ROW 26DEF. INSTALLED EMERGENCY PATH LIGHT AND LAMP REF MM 33-50-01, OPS CHECK OK. 2 L 7 3 4F A3WE 1999022600012 19990226 00012 SO 1999 2 26 RAAA99E9014 1 19990214 A 2140 85600 HEATER LKHEED 188 188C 5262604 SO COCKPIT FAILED A RAAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 1968R 188C2007 EN ROUTE FROM DUT TO ANC, FLIGHT CREW NOTED ELECTRICAL SMOKE SMELL IN COCKPIT. TURNED DUCT HEAT OFF AND SMELL DISAPPEAR ED. CHANGED FLIGHT STATION DUCT HEATER DUE FAILED. 2 L 7 4 4T 4A22 1999022600013 19990226 00013 SO 1999 2 26 RAAA99E9015 1 19990214 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST CR CRUISE 1 AL 03 1968R 188C2007 FLIGHT CREW REPORTED EMERGENCY LIGHTS ON AND UNABLE TO DISARM. CHANGED 7 EXIT IDENTIFIER BATTERIES DUE DISCHARGED. 2 L 7 4 4T 4A22 1999022600014 19990226 00014 SO 1999 2 26 RAAA99E9016 1 19990214 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST CR CRUISE 1 AL 03 1968R 188C2007 FLIGHT CREW REPORTED EMERGENCY LIGHTS ON AND UNABLE TO DISARM. CHANGED 4 FLOOR PROXIMITY EGRESS LIGHT BATTERIES DUE DIS CHARGED. 2 L 7 4 4T 4A22 1999022600015 19990226 00015 SO 1999 2 26 RAAA99E9017 1 19990215 A 3350 873100212 SIGN LKHEED 188 188C 5262604 SO RT EMER EXIT FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED, POOR RECEPT ION. 2 L 7 4 4T 4A22 1999022600016 19990226 00016 SO 1999 2 26 RAAA99E9018 1 19990215 A 3350 873100112 LIGHT LKHEED 188 188C 5262604 SO ROW 13 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 13 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 4 4T 4A22 1999022600017 19990226 00017 WP 1999 2 26 9900529903 1 19990216 A 5510 HINGE DOUG DC9 DC931 3022065 WP HORIZ STAB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 DURING PERIODIC CHECK, FOUND HORIZONTAL STABILIZER HINGE FITTING CORRODED LEFT AND RIGHT SIDES. REPAIRED PER EA 99-1637 78. 2 L 7 2 4F A6WE 1999022600018 19990226 00018 WP 1999 2 26 9900539954 1 19990216 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING PERIODIC CHECK, FOUND CRACKS AT FRAMES -5 AND -7 FS 83. REPAIRED PER EA 99-158010. 2 L 7 2 4F A6WE 1999022600019 19990226 00019 WP 1999 2 26 9900501149 1 19990211 A 3610 DUCT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE FAILED A NWAA A E F J UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 149US 46758 DURING INITIAL CLIMB AFTER TAKEOFF AT APPROXIMATELY 2000 FT MSL, THE NR 2 ENGINE FIRE WARNING ANNUNCIATED. THE ENGINE W AS SHUT DOWN PER THE FIRE WARNING CHECK LIST AND THE NR 1 FIRE BOTTLE WAS DISCHARGED. THE FIRE WARNING CEASED AFTER THE BOTTLE WAS DISCHARGED. AN EMERGENCY WAS DECLARED AND 127,000 LBS OF FUEL WAS DUMPED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE FINDING A CLAMP ON THE 15TH STAGE PNEUMATIC SUPPLY DUCT BROKEN. REPLACED THE CLAMP AND DUCT, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1999022600020 19990226 00020 NM 1999 2 26 9900512714 1 19990216 A 2450 CONDUIT BOEING 727 7272S7 138407Z NM NLG WW OUT OF POSITION A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 718RC 22344 ON TAKEOFF UPON GEAR RETRACTION, THE NOSE GEAR WARNING LIGHT DID NOT EXTINGUISH. CREW CYCLED THE GEAR, NO HELP. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPOSITIONED AND SECURED ELECTRICAL CONDUIT, OPERATIONAL CHEC K NORMAL. 2 L 7 3 4F A3WE 1999022600021 19990226 00021 1999 2 26 COMA9910034 3 19990216 A 6112 RFC11U16A DEICE EMB 120 EMB120RT SO RT PROP INOP A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 247CA 15353 120225 RIGHT HAND PROPELLER DEICE IS INOPERABLE. REPLACED THE NR 3 BLADE ON RIGHT HAND PROPELLER. 2 L 7 2 4T RT A31SO 1999022600022 19990226 00022 SO 1999 2 26 COMA9910035 1 19990218 A 5330 12027825001 SKIN EMB 120 EMB120RT SO BS 6462.6-6653 DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 20254 120217 DURING 1C INSPECTION, FOUND SMALL DENT IN FUSELAGE SKIN BETWEEN FS 6462.6 AND 6653.1 AND BETWEEN STRINGERS 19L AND 18L. REPAIRED DAMAGED AREA IAW EMB 120 SRM 53-00-01 PG 202-204. 2 L 7 2 4T RT A31SO 1999022600023 19990226 00023 SO 1999 2 26 COMA9910036 1 19990217 A 5414 12038646001 PLATE EMB 120 EMB120RT SO LT NACELLE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING ENGINE REPLACEMENT, THE LEFT NACELLE CENTER PLATE SECTION WAS FOUND TO HAVE A DENT AND CHAFING DAMAGE ON THE AFT OUTBOARD SIDE. BOTH THE DENT AND CHAFING DAMAGE WERE REPAIRED PER AERODESIGN REPORT NR 3133-1, REV IR, 2-12-99. 2 L 7 2 4T RT A31SO 1999022600024 19990226 00024 EA 1999 2 26 COMA9960070 1 19990216 A 2751 WARNING CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 941CA 7050 FLAPS FAIL MESSAGE ON EICAS. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 1999022600025 19990226 00025 EA 1999 2 26 COMA9960071 1 19990216 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 769CA 44 7292 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999022600026 19990226 00026 EA 1999 2 26 COMA9960072 1 19990217 A 3020 12681 SWITCH CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 927CA 8726 7031 RIGHT HAND ANTI-ICE IS INTERMITTENT. REPLACED ANTI-ICE PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 1999022600027 19990226 00027 EA 1999 2 26 COMA9960073 1 19990213 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 958CA 7111 EMERGENCY LIGHT, LEFT SIDE BELOW PAX WINDOW NR 6 INOPERABLE. REPLACED LAMP. 2 L 7 2 4F RT A21EA 1999022600028 19990226 00028 NM 1999 2 26 UPS99228740 1 19990122 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 1323-1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, CORROSION BETWEEN SKIN AND STIFFENER BS 1323 TO 1342, STRINGER 9L AND STRINGER 8L. REPAIRED IAW SMRO ENGINEERING ORDER 99-03-009, REF UPS ENGINEERING FILE NUMBER 727-53-2100. 2 L 7 3 4F A3WE 1999022600029 19990226 00029 NM 1999 2 26 UPS99228741 1 19990217 A 3350 BATTERY PACK BOEING 727 72721C 138400M NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FWD ENTRY DOOR INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK NORMAL P ER MM 33-50-01. A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 1999022600030 19990226 00030 NM 1999 2 26 99FDEA00066 1 19990216 A 3230 BUNGEE CYLINDER DOUG MD11 MD11F 3023600 NM LT MLG FAILED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 582FE 48420 LEFT MAIN GEAR UNSAFE WARNING SWAP LML BUNGEE CYLINDER WITH RML. REPLACED RML BUNGEE CYLINDER PART FLOWN IN FROM SIN. R EMOVED AND REPLACED ABOVE PER MM 32-33-02-04. BLED NR 3 HYD SYS USING NR 3 AUX PUMP. GREASED LMG PIVOT POINTS, CYCLE G EAR 10 TIMES PER MM 32-31-00. 2 L 7 3 4F RT A22WE 1999022600031 19990226 00031 NM 1999 2 26 99FDEA00067 1 19990218 A 3260 BULB BOEING 727 72722 1384002 NM LT MLG FAILED A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 190FE 19083 LT MAIN LANDING GEAR LIGHT DID NOT COME ON WHEN GEAR LOWERED. COMPLIED WITH RED TABS. REPLACED BOTH BULBS IN LT MAIN G EAR IND PER CHAPTER 20 STANDARD PRACTICES. LIGHTS GROUND CK GOOD. 2 L 7 3 4F A3WE 1999022600032 19990226 00032 WP 1999 2 26 ABXA9900102 1 19990116 A 5320 47504201 FITTING DOUG DOUG DC8 DC863 302198A WP BS 860 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 INTERCOSTAL FITTING CRACKED AT LONGERON 18 LEFT AND STATION 860. REPLACED FITTING IAW DWG 47504201 AND DC8 SRM 51-1-20D . 2 L 7 4 4F 4A25 1999022600033 19990226 00033 WP 1999 2 26 ABXA9900103 1 19990116 A 5320 561553053 INTERCOSTAL DOUG DOUG DC8 DC863 302198A WP BS 8-20 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 EXFOLIATED CORROSION ON INTERCOSTAL AT LONGERON 30 LEFT STATION 8 TO 20, INSIDE AIR CONDITIONING COMPARTMENT. REPLACED INTERCOSTAL IAW DWG 5615530 AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999022600034 19990226 00034 WP 1999 2 26 ABXA9900104 1 19990116 A 5320 3750257503 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LONGERON 31 LEFT SPLICE FITTING CRACKED AT STATION 1040 TO 1060. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999022600035 19990226 00035 WP 1999 2 26 ABXA9900105 1 19990116 A 5320 47504221 FITTING DOUG DOUG DC8 DC863 302198A WP BS 860 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 INTERCOSTAL END FITTING CRACKED AT LONGERON 19 RIGHT, STATION 860. REPLACED END FITTING IAW DWG 4750422 AND DC8 SRM 51- 1-20D. 2 L 7 4 4F 4A25 1999022600036 19990226 00036 WP 1999 2 26 ABXA9900106 1 19990116 A 5320 4645577502 ANGLE DOUG DOUG DC8 DC863 302198A WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 FLOORBEAM SUPPORT ANGLE CRACKED AT STATION 680, RBL 28. REPAIRED IAW DWG 4645517 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999022600037 19990226 00037 WP 1999 2 26 ABXA9900107 1 19990216 A 3040 13391 CONTROLLER DOUG DC8 DC861 3021952 WP WINDSHIELD DEFECTIVE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 849AX 2589 45891 DURING ENGINE START FOR REPOSITIONING FLIGHT, CREW REPORTED SMELL OF SMOKE IN COCKPIT. REPLACED LEFT AND CENTER WINDSHI ELD TEMPERATURE CONTROLLERS. DETERMINED BAD FILTER WAS CAUSING ODOR. 2 L 7 4 4F 4A25 1999022600038 19990226 00038 WP 1999 2 26 ABXA00108 1 19990217 A 3241 WARNING DOUG DC8 DC863 302198A WP ANTISKID SYST ILLUMINATED A ABXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 819AX 45927 DURING APPROACH, ANTISKID LIGHT CAME ON 'LF0 AND LFI' LIGHTS ON SKID CONTROL PANEL WERE ON. AFTER RECYCLING THE GEAR, L IGHTS WENT OUT. TROUBLESHOT ANTISKID SYSTEM IAW DC8 MM. NO DEFECTS WERE FOUND, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999022600039 19990226 00039 NM 1999 2 26 SCNA99035 1 19990216 A 3350 LIGHT BOEING 727 7272J4 1384006 NM AFT ENTRY DOOR INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT FLOOR TRACK IS CRACKED AT AFT ENTRY AREA. REMOVED AND REPLACED AFT SECTION OF EMERGENCY FLOOR TRACK COVER, ALL LIGHTS CHECK GOOD. 2 L 7 3 4F RT A3WE 1999022600040 19990226 00040 NM 1999 2 26 SCNA99036 1 19990216 A 3350 LIGHT BOEING 727 7272A1 138407F NM AFT AIRSTAIR INOP A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 287SC 21345 THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED AFT AIRSTAIR EMERGENCY LIGHT, LIGHT OPERATIONALL Y CHECKS GOOD. 2 L 7 3 4F A3WE 1999022600041 19990226 00041 NM 1999 2 26 SCNA99037 1 19990214 A 3350 81 BULB BOEING 727 7272J4 1384006 NM EMER EXIT FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE RIGHT OVERWING AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLAC ED THE BULB, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999022600042 19990226 00042 NE 1999 2 26 DHL99724003 2 19990107 A 7200 ENGINE BOEING 727 727228 NM PWA JT8 JT8D7 52053 NE NR 3 FAILED A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 724DH 19862 655473 NR 3 ENGINE OIL BYPASS LIGHT ILLUMINATED, OIL TEMP WENT TO 150. PERFORMED ENGINE SHUTDOWN. REMOVED AND REPLACED ENGINE PER MM 71-01-14. 2 L 7 3 4F 4 F A3WE E2EA 1999022600043 19990226 00043 WP 1999 2 26 ARWA990105 1 19990110 A 2710 DMD67C1502 BOLT DOUG DC8 DC862 3021970 WP AILERON WORN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 MIA - FLT 9627 - ON PRE-FLIGHT, FOUND RT AILERON INBD TO OTBD SECTION 2 INCH SPLIT. TROUBLESHOT, FOUND EYE BOLT ATTACHI NG INBD/OTBD AILERON LOOSE AND WORN. REPLACED SAME IAW 211-11-02. OPERATIONAL PER MM 27-11-02. (X) 2 L 7 4 4F 4A25 1999022600044 19990226 00044 WP 1999 2 26 GTIA9900004 1 19990125 A 3350 110049 LIGHT DOUG DC9 DC932 3022066 WP TAILCONE INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 483 0103 47113 DTW - EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. AFT OF BULKHEAD (TAIL CONE). REMOVED AND REPLACED EMERGENCY BATTERY CHA RGER AND OPERATIONAL CHECK GOOD IAW MM 33-50-00. PART TC: 321. (X) 2 L 7 2 4F A6WE 1999022600045 19990226 00045 WP 1999 2 26 GTIA9900005 1 19990124 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 MCO - AFT EMERGENCY FLOOR PATH LIGHTING, ONE EACH. RED LIGHT INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOO D PER MM 33-51-0. (X) 2 L 7 2 4F A6WE 1999022600052 19990226 00052 EU 1999 2 26 99ZZZX687 1 19990105 A 7810 109065001112 DUCT AGUSTA A109 A109K2 0260502 EU EXHAUST DAMAGED B K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 10016 FOUND EXHAUST DUCT DAMAGED, CRACKED. 1 G 7 2 3U RT H7EU 1999022600065 19990226 00065 NE 1999 2 26 99ZZZX694 1 19990121 A 6320 7635109035102 WEB SKRSKY S76 S76A 8143006 NE GEARBOX LOOSE A A HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 247 760076 THE AIRCRAFT EXPERIENCED A MAIN GEARBOX CHIP LIGHT IN-FLIGHT. INITIAL INVESTIGATION BY MAINTENANCE REVEALED THE CHIP DE TECTOR HAD PICKED UP A SHEARED BOLT/NUT COMBINATION. FURTHER EXAMINATION OF THE GEARBOX WITH A BORESCOPE REVEALED THE U PPER WEB ON THE SPUR GEAR ASSY WAS CRACKED. THERE ALSO WERE 4 BOLTS MISSING THAT SECURE THE WEB TO THE SHAFT OF THE SPU R GEAR ASSY. THIS IS THE SECOND FAILURE OF THIS TYPE WITH THIS OPERATOR. AN EXAMINATION OF THE GEARBOX AT THE OPERATOR 'S MAINTENANCE FACILITY IS BEING CORRDINATED WITH THE MANUFACTURER AND THE FAA BOSTON AIRCRAFT CERTIFICATION OFFICE. 1 G 7 2 3U H1NE 1999022600066 19990226 00066 NM 1999 2 26 SWAA990264 1 19990215 A 2130 327375 VALVE BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 354SW 25219 ON TAKEOFF WHEN GEAR CAME UP LOUD RUMBLE OCCURED AND PRESSURIZATION BEGAN +- 500 - 1000 FPM RATE OF CLIMB. AIRCRAFT RET URNED TO ABQ. REMOVED AND REPLACED AUTOMATIC FLOW CONTROL VALVE PER M/M. PRESSURIZED MANUALLY, VALVE OPS CK NORMAL IAW MM. 2 L 7 2 4F RT A16WE 1999022600067 19990226 00067 NM 1999 2 26 SWAA990265 1 19990215 A 2130 VALVE BOEING 737 7373H4 1384600 NM A/C BAY LACK OF LUBE A SWAA A UNSCHED LANDING O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 ON TAKEOFF PRESSURIZATION WAS NORMAL UNTIL APPROXIMATELY 500 FT WHEN LOUD RUMBLE OCCURRED AND PRESSURIZATION BEGAN =- 50 0 - 1000 FPM RATE OF CLIMB AND DESCENT. AIRCRAFT RETURNED TO ABQ. NOISE AND RUMBLE REMAINED UNTIL PRESS RESET FOR LAND ING. INSPECTED A/C DOORS AND SEALS, OUTFLOW VALVE AND LUBRICATED EQUIPMENT COOLING FAN FLOW CONTROL VALVE. PERFORMED P RESSURIZATION FUNCTION CHECK, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1999022600068 19990226 00068 NM 1999 2 26 SWAA990266 1 19990214 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED A2 CHECK, FOUND 2 DENTS 4 FT BELOW FWD SERV DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600069 19990226 00069 NM 1999 2 26 SWAA990267 1 19990214 A 5320 WEB BOEING 737 7372H4 138448C NM BS 180 & 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED A2 CHECK, FOUND CRACK IN HORIZ WEB AT LIGHTENING HOLE AT BS 180 AND 179. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600070 19990226 00070 NM 1999 2 26 SWAA990268 1 19990214 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4 D-CHECK, FOUND REPAIR DOUBLER CRACKED AT AFT SERV DOOR CUTOUT UPPER HINGE ARM CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600071 19990226 00071 NM 1999 2 26 SWAA990269 1 19990214 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 460 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4 D CHECK, FOUND CORROSION BULGE ON BOTTOM OF FUSELAGE AT BS 460 BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600072 19990226 00072 NM 1999 2 26 SWAA990270 1 19990214 A 3350 P4010021 POWER PACK BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED A2 CHECK, FOUND FWD UPPER EMERGENCY FLASHLIGHT WOULD NOT HOLD CHARGE. REMOVED AND REPLACED POWER MODUL E. 2 L 7 2 4F A16WE 1999022600073 19990226 00073 NM 1999 2 26 SWAA990271 1 19990215 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 73SW 22673 DURING PREFLIGHT, FOUND FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT FALLING OUT OF DOOR AND LIGHT BLINKING ON AND OFF INTE RMITTENTLY. SECURED EMERGENCY LIGHT ASSY INTO WALL PER M/M, OPS CK WAS NORMAL. 2 L 7 2 4F A16WE 1999022600074 19990226 00074 NM 1999 2 26 SWAA990272 1 19990215 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 371SW 26598 DURING PREFLIGHT, FOUND FLOOR TRACK LIGHTING IN MID CABIN INOP. REPLACED AND REPAIRED WIRING AS REQUIRED PER BOEING M/M . 2 L 7 2 4F RT A16WE 1999022600075 19990226 00075 NM 1999 2 26 SWAA990274 1 19990215 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED D-CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT, SECOND FROM AFT GALLEY INOP. RELAMPED FLOOR TRACK LIGHT PE R M/M, OPS CHECK GOOD. 2 L 7 2 4F A16WE 1999022600076 19990226 00076 NM 1999 2 26 SWAA990275 1 19990216 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED BC4 CHECK, FOUND CABIN AFT EMERGENCY TRACK LIGHT INOP AND ONE IS COVERED. RELAMPED LIGHT AND REPLACED END COVER ON FLOOR EGRESS LIGHTING PER M/M. 2 L 7 2 4F RT A16WE 1999022600077 19990226 00077 NM 1999 2 26 SWAA990276 1 19990217 A 3350 LIGHT BOEING 737 7373T5 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SC CHECK, FOUND (EMERGENCY EXIT ROW) ONE EMERGENCY FLOOR TRACK LIGHT INOP. RELAMPED FLOOR TRACK LIGHT PER M/M. 2 L 7 2 4F RT A16WE 1999022600108 19990226 00108 WP 1999 2 26 AT9900131 1 19990218 A 2560 113319 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 GALLEY DOOR SLIDE CAME OUT OF BIN. RESECURED GALLEY DOOR EVACUATION SLIDE IAW MM 25-62-0. 2 L 7 2 4F A6WE 1999022600109 19990226 00109 WP 1999 2 26 AT9900132 1 19990205 A 5320 591014211 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 370-375 MISDRILLED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO COMPARTMENT AT STA 370 TO STA 375 L-29R INTERCOASTAL UPPE R FLANGE AND WEB HAS MISDRILLED FASTENER HOLES. FABRICATED NEW INTERCOASTAL, FIT, DRILLED, TREATED AND PRIMED. LOCATED NEW WEB, DRILLED, DEBURRED AND INSTALLED IAW DC9 SRM 51-10-2A, 51-10-4, 51-10-3, 51-30-2, AND RES NR 99258. INTERCOAST AL P/N OFF 1A-49049-1. 2 L 7 2 4F A6WE 1999022600110 19990226 00110 WP 1999 2 26 AT9900133 1 19990101 A 5720 SPLICE DOUG DC9 DC932 3022066 WP WS 290 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT WING STA XOS 290.0 LEADING EDGE SKIN SPLICE CRACKED. REMOVED AND REPL ACED SPLICE PLATE, FABRICATED SPLICE PLATE, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-2 AND RE S NR 99199. 2 L 7 2 4F A6WE 1999022600111 19990226 00111 WP 1999 2 26 AT9900134 1 19990202 A 5320 59528041N SUPPORT DOUG DC9 DC932 3022066 WP BS 351-370 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND FORWARD CARGO COMPARTMENT STA 351 TO STA 370 L-29L INTERCOASTAL BENT, AND F LOOR SUPPORT WAS FOUND CRACKED. REMOVED AND FABRICATED NEW INTERCOASTAL, RECEIVED NEW SUPPORT, DRILLED, AND INSTALLED B OTH PARTS IAW DC9 SRM 51-10-4, 51-30-2, 51-30-5, 53-10-2, AND RES NR 99337. LONGERON P/N OFF 1A-42075-1. 2 L 7 2 4F A6WE 1999022600112 19990226 00112 NM 1999 2 26 K3HA990014 1 19990218 A 3350 1351 BULB BOEING 727 727225 1384077 NM ROW 32 FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 AFT CARGO DOOR AND PASSENGER ROW 32 EMERGENCY PATH LIGHTS INOP. REMOVE AND REPLACE LAMP ON AFT CARGO DOOR AND CLEAR LEN S WITH LAMP AT PASSENGER ROW 32 ON EMERGENCY PATH LIGHTING IAW 33-50-01 MM OPS CHECKED GOOD. (CLEAR LENS P/N 07912 NSN) 2 L 7 3 4F A3WE 1999022600113 19990226 00113 EU 1999 2 26 JBXA9900068 1 19990218 A 5247 D35165803 DOOR FOKKER F28 F28MK0100 4990807 EU APU MISSING A JBXA K NONE O OTHER IN INSP/MAINT 1 SO 05 104ML 15543 11445 ON WALK AROUND, FOUND APU SERVICE PANEL MISSING. REPLACED APU SERVICE PANEL IAW AMM 52-44-00. 2 L 7 2 4F RT 1999022600114 19990226 00114 NM 1999 2 26 CALA9900157 1 19990215 A 5753 MIDFLAP BOEING 727 727224 1384076 NM LT TE FLAP BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LT WING IB MIDFLAP BENT AT AFT IB AREA. THE BENT AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 57-50-2, PAGE 5. 2 L 7 3 4F A3WE 1999022600115 19990226 00115 NM 1999 2 26 CALA9900158 1 19990215 A 5720 BEAM BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND A .25 CRACK IN J BEAM ABOVE LT WING NR 7 SPOILER ACTUATOR. THE J BEAM WAS REMOVED IAW SRM 51-30-2. A N EW J BEAM WAS INSTALLED WITH NUT PLATE IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1999022600116 19990226 00116 NM 1999 2 26 CALA9900159 1 19990215 A 5755 651734781A SPOILER BOEING 727 727224 1384076 NM NR 11 POSITION DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND NR 11 SPOILER SPLIT AND DELAMINATED AT CENTER T/E TOP SURFACE AREA. THE SPOILER WAS REMOVED AND REPLAC ED IAW MM 27-61-1. 2 L 7 3 4F A3WE 1999022600117 19990226 00117 NM 1999 2 26 CALA9900160 1 19990215 A 5755 651734781A SKIN BOEING 727 727224 1384076 NM NR 4 SPOILER DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LT WING NR 4 SPOILER UPPER SURFACE OB T/E DEBONDED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61- 1. 2 L 7 3 4F A3WE 1999022600118 19990226 00118 NM 1999 2 26 CALA9900161 1 19990217 A 5320 ANGLE BOEING 757 757224 1384958 NM BS 1060 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND RT MLG WHEEL WELL CUTOUT FORWARD SEAL RETAINER CHANNEL SUPPORT ANGLES CRACKED AT STA 1060. THE CRACKS WERE 1 LONG. NEW ANGLES WERE INSTALLED IAW BOEING DRAWING NR 149N7550. 2 L 7 2 4F RT A2NM 1999022600119 19990226 00119 WP 1999 2 26 CALA9900162 1 19990217 A 5753 5910043501 VANE DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND LT WING FLAP O/B FIXED VANE I/B END LOWER SURFACE CORRODED WITH RIVETS PULLING THROUGH. THE LT O/B FLA P VANE WAS REMOVED AND REPLACED IAW MM 27-51-3. 2 L 7 2 4F A6WE 1999022600120 19990226 00120 NM 1999 2 26 CALA9900163 1 19990217 A 5754 114N4002155A SLAT BOEING 757 757224 1384958 NM NR 1 LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND A DENT IN NR 1 SLAT NOSE SKIN. THE AREA WAS REPAIRED IAW SRM 57-43-01. 2 L 7 2 4F RT A2NM 1999022600121 19990226 00121 NM 1999 2 26 CALA9900164 1 19990218 A 5320 CHORD BOEING 757 757224 1384958 NM BS 1147 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND A 1 CRACK IN LT MLG WHEEL WELL OUTER CHORD AT STA 1147. A NEW CHORD WAS INSTALLED IAW BOEING DRAWING N R 149N7222. 2 L 7 2 4F RT A2NM 1999022600122 19990226 00122 NM 1999 2 26 CALA9900165 1 19990218 A 5230 146N6603261 DOOR BOEING 757 757224 1384958 NM CARGO COMPT DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND IMPACT DAMAGE TO AFT CARGO DOOR AFT LOWER CORNER, FORWARD LOWER CORNER, AND LOWER EDGE BEAM. THE AFT L OWER CORNER, FORWARD LOWER CORNER, AND LOWER EDGE BEAM WERE REPLACED IAW SRM 52-30-02 AND BOEING DRAWING NR 146N6603. 2 L 7 2 4F RT A2NM 1999022600123 19990226 00123 NM 1999 2 26 CALA9900166 1 19990218 A 3397 WIRE BOEING 737 7373T0 1384582 NM LT EMER EXIT BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND LOWER EMERGENCY LOCATOR SIGN AT RT OVERWING EXIT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO LI GHT ASSEMBLY AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999022600124 19990226 00124 NM 1999 2 26 CALA9900167 1 19990218 A 5730 SKIN BOEING 757 757224 1384958 NM WS 400 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND RT WING FIXED LEADING EDGE SKIN DELAMINATED AT OSS 400. THE SKIN WAS REPAIRED IAW SRM 51-70-07 AND REF ITTED IAW MM 57-31-00. 2 L 7 2 4F RT A2NM 1999022600125 19990226 00125 NM 1999 2 26 CALA9900168 1 19990218 A 5712 RIB BOEING 757 757224 1384958 NM WS 420 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND TWO .25 INCH CRACKS IN RT WING FIXED LEADING EDGE RIB AT OSS 420. THE RIB WAS REPLACED IAW SRM 57-41-0 9. 2 L 7 2 4F RT A2NM 1999022600126 19990226 00126 WP 1999 2 26 9900549878 1 19990213 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F RT A6WE 1999022600127 19990226 00127 WP 1999 2 26 9900559906 1 19990212 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 956N 47252 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1999022600128 19990226 00128 WP 1999 2 26 9900569959 1 19990214 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CATWALK MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 919RW 47162 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED POWER SUPP LY AND BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999022600129 19990226 00129 WP 1999 2 26 9900579963 1 19990216 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. 2 L 7 2 4F A6WE 1999022600130 19990226 00130 WP 1999 2 26 9900589601 1 19990213 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP TAIL COMPT INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1999022600131 19990226 00131 WP 1999 2 26 9900599154 1 19990216 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTING IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATT ERIES IN POWER SUPPLY LOCATED IN LAVATORY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999022600132 19990226 00132 NM 1999 2 26 UPS99228742 1 19990217 A 5711 CHORD BOEING 727 72725C 138400H NM LT WING SPAR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE:C CORROSION (C57-581-03-00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIR ED IAW ERO 99-5030. 2 L 7 3 4F A3WE 1999022600133 19990226 00133 NM 1999 2 26 UPS99228743 1 19990216 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 850 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE:C WHILE WORKING (EO B727-5310-5474) DISCOVERED CRACK IN STRINGER 17 LT BS 850 BL 70.5 WL 208. INSTALLED RADIUS FILLERS BS 848-TO BS 856 AND FABRICATED AND INSTALLED INTERCOSTAL BS 848 TO 870 PER 727 SRM 51-30-2, 51-40-4 AND 51-20-4. 2 L 7 3 4F A3WE 1999022600134 19990226 00134 NM 1999 2 26 99FDEA00068 1 19990219 A 3260 CONNECTOR BOEING 727 7272S2F 1384O81 NM LT MLG DOOR LOOSE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 215FE 22936 99-0051 - LEFT GEAR REMAIN ON AT GEAR RETRACTION. RECYCLED GEAR AND LIGHT WORK PROPERLY. REPEAT WRITE-UP. LEFT LANDIN G GEAR DOOR WARNING SWITCH ADJUST PER MM 32-62-11. CLEANED AND RESECURED PLUG. SYSTEM GROUND CK OK. 2 L 7 3 4F A3WE 1999022600135 19990226 00135 1999 2 26 99FDEA00069 4 19990220 A 2213 4059001907 FCC DOUG MD11 MD11F 3023600 NM E&E COMPT INOP A FDEA A J UNSCHED LANDING DUMP FUEL J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 25 610FE 48603 99-0052 - ASYMMETRICAL SLAT ON SLAT RETRACTION 230 KTS. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FLT CONTROL COMPUTERS I AW MM 22-01-03-4 PERF RTS TEST, OPS CK GOOD. PERF CADC TEST RTS IAW MM 34-16-01-3. OPS CK NORM. NOTED ON ALL (3) CADC . 2 L 7 3 4F RT A22WE 1999022600136 19990226 00136 NM 1999 2 26 99FDEA00070 1 19990219 A 5320 651891562 SHEAR TIE BOEING 727 72722 1384002 NM BS 336 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 244 - SHEAR TIE ON WEB AT BS 336 HAS CRACK IND IN UPPER O/B RADIUS OF CUT OUT FOR STR 25 AND 26 RT. 2 L 7 3 4F A3WE 1999022600137 19990226 00137 NM 1999 2 26 99FDEA00071 1 19990221 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1150 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 LEFT SIDE OF FUSELAGE BS 1150 3 ABOVE STR S4L SHEAR FASTENER HEAD AND SKIN CRACK. REPAIRED PER SRM 53-30-3 FIG 13A. 2 L 7 3 4F A3WE 1999022600138 19990226 00138 NM 1999 2 26 99FDEA00072 1 19990219 A 5320 6516340 SHEAR TIE BOEING 727 72722 1384002 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 CORROSION (C53-113-01, 2) ON SHEAR TIE BS 990, LBL 17, WL 140. *S/D* REMOVED, FABBED AND INSTALLED NEW SHEAR TIE BS 99 0, LBL 17, WL 140 IAW FEDEX SRM 53-10-04. 2 L 7 3 4F A3WE 1999022600139 19990226 00139 WP 1999 2 26 ABXA9900109 1 19990118 A 5240 575553028 DOOR DOUG DOUG DC8 DC863 302198A WP LT SERV DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT CENTER SERVICE DOOR HAD CRACK IN STRUCTURE. INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 52-2-0. 2 L 7 4 4F 4A25 1999022600140 19990226 00140 WP 1999 2 26 ABXA9900110 1 19990118 A 5240 57555309 SKIN DOUG DOUG DC8 DC863 302198A WP LT SERV DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 TWO LIGHTENING HOLES IN FORWARD, LEFT SERVICE DOOR STRUCTURE WERE CRACKED. REPLACED SKIN PANEL IAW DC8 SRM 51-1-8, 51-3 -0 AND DWG 5755530. 2 L 7 4 4F 4A25 1999022600141 19990226 00141 WP 1999 2 26 ABXA9900111 1 19990117 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 753.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 UPPER RIB CRACKED AT LEFT WING OUTBOARD LEADING EDGE AT XFS 753.750. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056. 2 L 7 4 4F 4A25 1999022600142 19990226 00142 WP 1999 2 26 ABXA9900112 1 19990117 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIB CRACKED AT LEFT WING OUTBOARD SECTION AT STATION XFS 772.5. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056. 2 L 7 4 4F 4A25 1999022600143 19990226 00143 WP 1999 2 26 ABXA9900113 1 19990117 A 5320 4611067 FITTING DOUG DOUG DC8 DC863 302198A WP BS 70 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 STRINGER END CORRODED, STRINGER 4 RIGHT AND STATION 70. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F 4A25 1999022600144 19990226 00144 WP 1999 2 26 ABXA9900114 1 19990123 A 5311 SR0853000861 FRAME DOUG DOUG DC8 DC863 302198A WP BS 1600 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CORROSION FOUND ON STATION 1600 FRAME LOWER FLANGE BETWEEN LONGERON 34 LEFT AND 34 RIGHT. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F 4A25 1999022600145 19990226 00145 WP 1999 2 26 ABXA9900115 1 19990123 A 5512 5644310 SKIN DOUG DOUG DC8 DC863 302198A WP LT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT HORIZONTAL STABILIZER LEADING EDGE, UPPER SURFACE HAD BULGING CORROSION ALONG AFT END FROM STATION XFS235 TO XFS320 . REPAIRED IAW DC8 SRM 55-21. 2 L 7 4 4F 4A25 1999022600146 19990226 00146 WP 1999 2 26 ABXA9900116 1 19990123 A 5720 5611020 CHANNEL DOUG DOUG DC8 DC863 302198A WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED AT AFT SIDE OF LANDING GEAR CUT-OUT. REPLACED CHANNEL IAW DWG 5611020 AND DC8 SRM 51-01-21. 2 L 7 4 4F 4A25 1999022600147 19990226 00147 WP 1999 2 26 ABXA9900117 1 19990123 A 5320 46549032 GUSSET DOUG DOUG DC8 DC863 302198A WP BS 1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 GUSSET HAD EXFOLIATED CORROSION AT STATION 1220 LONGERON 24 LEFT. REPLACED GUSSET IAW DC8 SRM 51-01-20D AND ABX REA D85 3-24930. 2 L 7 4 4F 4A25 1999022600148 19990226 00148 WP 1999 2 26 ABXA9900118 1 19990123 A 5320 47549031 GUSSET DOUG DOUG DC8 DC863 302198A WP BS 1240 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 GUSSET PLATE HAD EXFOLIATED CORROSION AT STATION 1240 LONGERON 24 LEFT. REPLACED GUSSETT IAW DWG 9755849 AND DC8 SRM 51 -01-20D AND ABX RE AND 853-24930. 2 L 7 4 4F 4A25 1999022600149 19990226 00149 NM 1999 2 26 DL72S990303 1 19990212 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 FUSELAGE SKIN FS 681-740, STRINGER 4R, SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION REVEALED CRACKS IN THE LOWER SKIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION VERIFIED 15 CRACKS ALONG THE LO WER ROW OF FASTENERS IN THE LOWER SKIN. THE SKIN LAP WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL AL UMINUM DOUBLER PER ER/A 366662-14, REV A. 2 L 7 3 4F A3WE 1999022600150 19990226 00150 NM 1999 2 26 DL72S990304 1 19990212 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 FUSELAGE SKIN FS 481-681 STRINGER 4R SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION REVEALED CRACKS IN THE LOWER S KIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 481 AND 681. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS ALONG THE LOW ER FASTENER ROW OF THE LOWER SKIN PANEL. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIR WIT H AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366661-14, REV A. 2 L 7 3 4F A3WE 1999022600151 19990226 00151 WP 1999 2 26 DLL10990305 1 19990211 A 5312 1505220251 BULKHEAD CAP LKHEED 1011 10113851 5265010 WP BS 1363 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 FUSELAGE BULKHEAD FS 1363 LOWER CAP, LBL 91.5, REPAIR FOR CRACK. THE LOWER CAP OF THE FS 13636 BULKEAD WAS FOUND WITH A CRACK THROUGH THE HORIZONTAL FLANGE EXTENDING INTO THE VERTICAL FLANGE AT LBL 91.5. THE SECTION OF CAP WITH THE CRAC K WAS REMOVED FROM THE EXISTING SPLICE AT STRINGER 47 TO AN APPROVED SPLICE AT STRINGER 41. A NEW SECTION OF CAP WAS IN STALLED PER ER/A 366678-14AD. 2 L 7 3 4F A23WE 1999022600152 19990226 00152 NM 1999 2 26 DL72W990307 1 19990216 A 3150 CLACKER 9915 BOEING 727 727247 138408F NM COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 2815W 1133 20871 ATB - ELECT SMELL FROM RT SIDE OF COCKPIT. REPLACED OVERSPEED CLACKER. 2 L 7 3 4F A3WE 1999022600153 19990226 00153 NM 1999 2 26 DLM88990308 1 19990216 A 2910 LINE AS15308KO25 DOUG MD88 MD88 3023688 NM RT ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 976DL 53257 AT FLT LEVEL 220, JUST AFTER LIFT OFF, MASTER CAUTION LIGHT ILLUMINATED WITH RIGHT HYD PRESS LOW MSG. RIGHT HYD PRESS A ND QTY SHOWED ZERO. RIGHT HYD SYS FAILURE CHECKLIST RUN. MAIN LANDING GEAR DOORS CONTACTED THE RUNWAY RUNWAY ABOUT 7 0 KNOTS. FOUND HYD HOSE FROM RIGHT ENGINE PRESS FILTER TO SOILD LINE ON SIDE OF FUSELAGE LEAKING. MADE APPROVED REPAIR . HYD RESERVIOR STILL HAD FLUID INDICATING AT THE RESERVIOR, SERVICED FULL RAN ENGINE LEAK CKS OK. 2 L 7 2 4F RT A6WE 1999022600154 19990226 00154 NM 1999 2 26 DL72S990310 1 19990216 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 FOUND ON D1 LETTER CK AFT ENTRY DOOR FRAME CUTOUT CRACKED LEFT SIDE APPROX 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER S RM 53-10-9. 2 L 7 3 4F A3WE 1999022600155 19990226 00155 NM 1999 2 26 DL72S990311 1 19990216 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 FOUND ON D1 LETTER CK AFT ENTRY DOOR FRAME CUTOUT CRACKED RT SIDE APPROX 10 INCHES FROM THE TOP. REPAIRED PER SRM 53-10 -9. 2 L 7 3 4F A3WE 1999022600156 19990226 00156 NM 1999 2 26 DL72S990312 1 19990216 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM LT OVERWING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 419DA 21272 LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT MOST FWD INOP. REPLACED RACK AND BATTERY PACK, OP CKS OK. 2 L 7 3 4F A3WE 1999022600157 19990226 00157 NM 1999 2 26 DL72S990313 1 19990216 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 419DA 21272 OVERHEAD EXIT SIGN EMERGENCY LIGHT INOP ON TEST AT OVERWING EXITS. REPLACED M1094 RACK AND BATTERY PACK OP CKS OK. PAR TS BORROWED FROM AMERICA WEST PACK LOCATED ABOVE ROW 19 RT SIDE OF CTR DUCT. 2 L 7 3 4F A3WE 1999022600158 19990226 00158 NM 1999 2 26 DLM88990314 1 19990216 A 2560 37003103 SLIDE DOUG MD88 MD88 3023688 NM TAILCONE FAILED TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DL 49538 DURING OPN 6910 OF TAIL SLIDE DEPLOYMENT, TAIL CONE HAD PROBLEMS RELEASING AND THE SLIDE LANYARD SNAP POPPED OFF. THE V ELCRO GLUE DID NOT HOLD. HARNESS DID NOT ALLOW ENOUGH PULL ON LANYARD TO DEPLOY SLIDE. SLIDE MANUALLY DEPLOYED AFTER R ELEASING FWD STRAP TOGGLE PINS. A/C WAS IN FOR NORMAL HMV. 2 L 7 2 4F RT A6WE 1999022600159 19990226 00159 NM 1999 2 26 DL72W990315 1 19990217 A 2782 ACTUATOR 1U1110 BOEING 727 727247 138408F NM LT LE FLAP LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 292WA 8006DEFGK 22110 INFLIGHT 'A' SYS HYD QTY DECREASED TO NEAR ZERO, ACCOMPLISHED PROD IAW POM. REPLACED INBOARD KRUEGER FLAP ACTUATOR. 2 L 7 3 4F A3WE 1999022600160 19990226 00160 NM 1999 2 26 DL72W990319 1 19990217 A 5330 655457416 SKIN BOEING 727 727247 138408F NM BS 481-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FUSELAGE SKIN FS 481-680 STRINGER 4R SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SP LICE BETWEEN FS 481 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTIO N CONFIRMED 23 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS INSTALLED PER ER/A 366702-14, REV A. 2 L 7 3 4F A3WE 1999022600161 19990226 00161 NM 1999 2 26 DL72W990320 1 19990217 A 5330 65545672 SKIN BOEING 727 727247 138408F NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FUSELAGE SKIN FS 681-740 STRINGER 4R, SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS ALONG THE PANEL. THE LAP SPLICE WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AND EXTE RNAL ALUMINUM DOUBLER. THE REPAIR WAS INSTALLED PER ER/A 366703-14, REV A. 2 L 7 3 4F A3WE 1999022600162 19990226 00162 NM 1999 2 26 DL72W990321 1 19990217 A 3310 8100017501 LIGHT BOEING 727 727247 138408F NM COCKPIT INOP A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 2815W 20871 F/O MAP LIGHT SMOKED AND FUMED. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999022600163 19990226 00163 NM 1999 2 26 DL72S990322 1 19990217 A 5500 65312813 CORD ANGLE BOEING 727 727225A 1384077 NM NBR2 ENG AFT NEW A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 ON HUSH-KIT MOD, FOUND LT NR 2 ENG MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH ANGLE OF NEW MFG. 2 L 7 3 4F RT A3WE 1999022600164 19990226 00164 NM 1999 2 26 DL72S990323 1 19990218 A 5400 65312814 ANGLE BOEING 727 727225A 1384077 NM NR2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 ON HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH NEW MFG RT SIDE. 2 L 7 3 4F RT A3WE 1999022600165 19990226 00165 NM 1999 2 26 DL757990325 1 19990217 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM BS 620 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 FUSELAGE SKIN FS 619-623 STRINGER 15-16, REPAIR FOR GOUGES. THE FUSELAGE SKIN WAS FOUND WITH TWO GOUGES BETWEEN FS 619 AND 623 AND BETWEEN STRINGERS 15 AND 16. BOTH GOUGES WERE CUT OUT OF THE SKIN WITH APPROX 2 BY 2 CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER. INSTALLED PER ER/A 366676-14. 2 L 7 2 4F RT A2NM 1999022600166 19990226 00166 NM 1999 2 26 DL76G990326 1 19990217 A 5754 SKIN BOEING 767 7673P6 1385105 NM NR9 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 WING NR 9 SLAT TRAILING EDGE WEDGE, UPPER SKIN, REPAIR FOR DELAMINATION. THE UPPER SKIN OF THE TRAILING EDGE WEDGE OF T HE NR 9 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF DELAMINATION. THE DAMAGED AREA WAS CUT AWAY AND REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 366723-14AD. 2 L 7 2 4F RT A1NM 1999022600167 19990226 00167 NM 1999 2 26 DL72K990327 1 19990127 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 THE AFT LOWER CHORD ANGLE WAS FOUND DAMAGED 33 FROM OB END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1999022600168 19990226 00168 NM 1999 2 26 DL72K990328 1 19990127 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 34 FROM IB END OF FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0. 2 L 7 3 4F A3WE 1999022600169 19990226 00169 NM 1999 2 26 DL72K990329 1 19990127 A 5754 652163262 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED DURING SHOP INSPECTION 20 FROM IB END OF FLAP. THE ANGLE WAS REPAIRED PER M M 57-52-0 BY INSTALLING A DOUBLER AND NEW SECTION OF ANGLE. 2 L 7 3 4F A3WE 1999022600170 19990226 00170 NM 1999 2 26 DL72K990330 1 19990127 A 5753 652163262 SKIN BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 THE COVE SKIN WAS FOUND CRACKED 37 FROM IB END OF FLAP. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER MM 57-52-0, F IG 809. 2 L 7 3 4F A3WE 1999022600171 19990226 00171 NM 1999 2 26 DL72S990332 1 19990218 A 5320 WEB BOEING 727 727232 1384082 NM BS 1249&1236 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 RT INBOARD VERT TORQUE BOX WEB CRACKED AT UPPER FASTENER STA 1248 AND 1236. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999022600172 19990226 00172 NM 1999 2 26 DHL9974001C 1 19990203 A 5720 ANGLE BOEING 727 7272Q9 138448M NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, RT FIXED LEADING EDGE CAVITY LOWER INBD SUPPORT ANGLE FSS 130.7 IS CRACKED. CUT OUT ANGLE, INSTALLED NEW SU PPORT ANGLE PER SRM 51-40-3, 9.5 BY 1 BY 1, N/R 2911. 2 L 7 3 4F RT A3WE 1999022600173 19990226 00173 NM 1999 2 26 DHL9974002C 1 19990203 A 5311 ANGLE BOEING 727 7272Q9 138448M NM BS 1050 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, CORRSION AFT CARGO FRAME 1050 AT RIGHT FLOOR SUPPORT. FABRICATED FRAME REPAIR PER SRM 51-40-3, 10.5 BY 3.5, N/R 3161. 2 L 7 3 4F RT A3WE 1999022600174 19990226 00174 NM 1999 2 26 DHL9974003C 1 19990130 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 1140 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, DENT IN FUSELAGE SKIN AT FS 1140 AT STR 6R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER EXTERNAL SKIN REPAIR PE R SRM 53-30-3, 12.5 BY 10, N/R 3021. 2 L 7 3 4F RT A3WE 1999022600175 19990226 00175 NM 1999 2 26 DHL9974004C 1 19990203 A 5720 ANGLE BOEING 727 7272Q9 138448M NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, RT WING FIXED LEADING EDGE CAVITY LOWER OUTBD SUPPORT ANGLE AT FS 130.7 IS CRACKED. REMOVED AND REPLACED AN GLE PER SRM 51-40-3, 18 BY 1 BY 1, N/R 2072. 2 L 7 3 4F RT A3WE 1999022600176 19990226 00176 NM 1999 2 26 DHL9974005C 1 19990203 A 5720 ANGLE BOEING 727 7272Q9 138448M NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, ANGLE CRACKED AT LT WING 32 L/E SLAT WELL. REMOVED CRACKED ANGLE AND REPLACED PER SRM 51-30-2, 10 BY 5, N/R 1097. 2 L 7 3 4F RT A3WE 1999022600177 19990226 00177 NM 1999 2 26 DHL9974006C 1 19990203 A 5730 SKIN BOEING 727 7272Q9 138448M NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, LEFT WING COVE PANEL OUTBD OF NR 4 FLAP TRACK LOWER SKIN DAMAGED. INSTALLED FILLER REPAIR PER SRM 51-40-1, 9 BY 8, N/R 1248. 2 L 7 3 4F RT A3WE 1999022600178 19990226 00178 NM 1999 2 26 DHL9974007C 1 19990203 A 5751 SKIN BOEING 727 7272Q9 138448M NM LT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, L/W OUTBD AILERON UPPER SURFACE AT OUTSIDE UPPER SURFACE TRAILING EDGE DELAMINATED. INSTALLED BONDED REPAIR PER SRM 51-40-6, NO BALANCE REQUIRED PER SRM 51-80-4, 7 BY 2 N/R 1108. 2 L 7 3 4F RT A3WE 1999022600179 19990226 00179 NM 1999 2 26 DHL9974008C 1 19990203 A 5754 SHIELD BOEING 727 7272Q9 138448M NM NR 5 LE SLAT DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 5 SLAT AERODYNAMIC FENCE LEADING EDGE METAL SHIELD DELAMINATING. INSTALLED BONDING REPAIR PER SRM 51-20- 3, 6 BY 3, N/R 2029. 2 L 7 3 4F RT A3WE 1999022600180 19990226 00180 NM 1999 2 26 DHL9974009C 1 19990203 A 5754 FENCE BOEING 727 7272Q9 138448M NM NR 5 LE SLAT ERODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 5 SLAT AERODYNAMIC FENCE ERODED IN SEVERAL AREAS. INSTALLED FILLER REPAIR PER SRM 51-40-1, 9 BY 3, N/R 2 030. 2 L 7 3 4F RT A3WE 1999022600181 19990226 00181 NM 1999 2 26 DHL9974010C 1 19990202 A 5260 SUPPORT BOEING 727 7272Q9 138448M NM AFT AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, AIR STAIR GROUND OPERATION DOOR INSIDE AREA LEFT UPPER SIDE PLATE MISSING AND SUPPORT CRACKED. CUT OUT DAMA GED AREA AND INSTALLED ANGLE REPAIR AND COVER PLATE PER SRM 51-40-3, 1 BY 4 BY 8, N/R 3083. 2 L 7 3 4F RT A3WE 1999022600182 19990226 00182 NM 1999 2 26 DHL9974011C 1 19990204 A 5753 FAIRING BOEING 727 7272Q9 138448M NM NR 4 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 4 FLAP TRACK FIXED FAIRING CRACKED AT FWD END. REPLACED STRAP ON FLAP TRACK PER SRM 53-50-1, 13 BY 3, N/ R 1163. 2 L 7 3 4F RT A3WE 1999022600183 19990226 00183 NM 1999 2 26 DHL9974012C 1 19990203 A 5754 ANGLE BOEING 727 7272Q9 138448M NM NR 2 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, INNER STRUCTURE SUPPORT ANGLE IS CRACKED AT NR 2 L/E SLAT INNER NOSE BETWEEN L/E SLAT ACTUATOR AND ANTI-ICE DUCT. STOP DRILLED CRACK, HFEC STOP DRILL. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 BY 1 BY 17.5, N/R 1090. 2 L 7 3 4F RT A3WE 1999022600184 19990226 00184 NM 1999 2 26 DHL9974013C 1 19990203 A 5753 SKIN BOEING 727 7272Q9 138448M NM RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, RT OUTBD AFT FLAP TRAILING EDGE IS DELAMINATING 78 FROM OUTBD SIDE. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 8 BY 5, N/R 2088. 2 L 7 3 4F RT A3WE 1999022600185 19990226 00185 NM 1999 2 26 DHL9974014C 1 19990202 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 1088 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, SEAT TRACK LBL 45.5 HAS SURFACE CORROSION AND WORN AT STA 1088. REMOVED DAMAGED SEAT TRACK AND REPLACED PER SRM 53-10-5 AT STA 1010, 80 LONG, N/R 3105. 2 L 7 3 4F RT A3WE 1999022600186 19990226 00186 NM 1999 2 26 DHL9974015C 1 19990202 A 5311 CIRCUMFERENTIAL BOEING 727 7272Q9 138448M NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, AFT CARGO BILGE THERE IS CORROSION AT STA 950 C, CIRCUMFERENTIAL AT STR 291. REMOVED, FABRICATED AND INSTAL LED NEW ANGLE PER SRM 53-10-1, N/R 3030. 2 L 7 3 4F RT A3WE 1999022600187 19990226 00187 NM 1999 2 26 DHL9974016C 1 19990201 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 400 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, RT SIDE OF FUSE HAS DEEP GOUGE BELOW FWD GALLEY DOOR STA 400. CUT OUT DAMAGED SKIN, HFEC SKIN AND INSTALLED REPAIR PER SRM 53-30-3, 11 BY 8.5, N/R 3055. 2 L 7 3 4F RT A3WE 1999022600188 19990226 00188 NM 1999 2 26 DHL9974017C 1 19990203 A 5522 SKIN BOEING 727 7272Q9 138448M NM RT ELEVATOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, RT ELEVATOR T/E SEPARATING AND SPONGY AT O/B AREA OF TAB CUTOUT. APPLIED BONDING REPAIR PER SRM 51-20-3, 8 BY 1, N/R 4332. 2 L 7 3 4F RT A3WE 1999022600189 19990226 00189 NM 1999 2 26 DHL9974018C 1 19990203 A 5522 SKIN BOEING 727 7272Q9 138448M NM RT ELEVATOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, RT ELEVATOR I/B END T/E SEPARATING AND HAS BROKEN FASTENER O/B TAB CUT OUT. APPLIED BONDING REPAIR PER SRM 51-30-3, 8 BY 1, N/R 4330. 2 L 7 3 4F RT A3WE 1999022600190 19990226 00190 NM 1999 2 26 DHL9974019C 1 19990204 A 7110 RIB BOEING 727 7272Q9 138448M NM NR 3 ENG COWL BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 3 ENGINE LOWER COWL PANEL NR 5 INNER RIB IS GOUGED. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER S RM 54-10-3, 3 BY 7, N/R 6435. 2 L 7 3 4F RT A3WE 1999022600191 19990226 00191 NM 1999 2 26 DHL9974020C 1 19990203 A 7810 TAILPIPE BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 689907 AT C CHECK, NR 2 ENGINE, HOLE ON LEADING EDGE TAIL PIPE EXTERIOR LT SIDE ABOUT 7 O'CLOCK POSITION. CUT OUT DAMAGED AREA , INSTALLED DOUBLER, 12 BY 4 PER SRM 51-40-3, N/R 6399. 2 L 7 3 4F 4 F RT A3WE E2EA 1999022600192 19990226 00192 NM 1999 2 26 DHL9974021C 1 19990203 A 7110 COWL BOEING 727 7272Q9 138448M NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 1 ENGINE LOWER COWL NR 5 RIB AFT OF OIL BREATHER HAS HOLE WORN THROUGH. INSTALLED ANGLE REPAIR PER SRM 5 4-10-3, 3 BY 18, N/R 6341. 2 L 7 3 4F RT A3WE 1999022600193 19990226 00193 NM 1999 2 26 DHL9974022C 1 19990203 A 7110 COWL BOEING 727 7272Q9 138448M NM NR 1 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 1 ENGINE UPPER COWL FWD OUTBD LE CHAFF STRIP NEEDS REPLACEMENT. CUT OUT DAMAGED AREA, INSTALLED ANGLE RE PAIR PER SRM 51-10-3, 3 BY 20, N/R 6332. 2 L 7 3 4F RT A3WE 1999022600194 19990226 00194 NM 1999 2 26 DHL9974023C 1 19990203 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 710 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, TOP FLANGE OF SEAT TRACK BROKEN OFF BS 710 BL 0. REMOVED DAMAGED SECTION FROM 700 TO 730 PER AE DRAWING AE 727-2-063 AND REPLACED SAME, N/R 5730. 2 L 7 3 4F RT A3WE 1999022600195 19990226 00195 NM 1999 2 26 DHL9974024C 1 19990203 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 940 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, TOP FLANGE OF SEAT TRACK GOUGED BS 940 RBL 24. REMOVED DAMAGED SEAT TRACK AND REPLACED PER SRM 53-10-5, 90 LONG N/R 5732. 2 L 7 3 4F RT A3WE 1999022600196 19990226 00196 NM 1999 2 26 DHL9974025C 1 19990203 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 935 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, TOP FLANGE OF SEAT TRACK WORN IN TWO SPOTS BS 935 TO 945 RBL 48. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 F ROM BS 870 TO 960, N/R 5733. 2 L 7 3 4F RT A3WE 1999022600197 19990226 00197 NM 1999 2 26 DHL9974026C 1 19990202 A 7810 FAIRING BOEING 727 7272Q9 138448M NM NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 3 ENGINE REV TAIL PIPE FAIRING CRACKED FWD EDGE. REPLACED TAIL PIPE FAIRING PER SRM, 51-40-3, 6 BY 4, N/ R 6379. 2 L 7 3 4F RT A3WE 1999022600198 19990226 00198 NM 1999 2 26 DHL9974027C 1 19990204 A 7110 ANGLE BOEING 727 7272Q9 138448M NM NR 3 ENG COWL DETERIORATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, NR 3 ENGINE UPPER COWL PANEL FORWARD UPPER INNER LUG FITTING ATTACH ANGLE DETERIORATED. REPLACED ANGLE PE R SRM 54-10-2, 12 BY 5, N/R 6428. 2 L 7 3 4F RT A3WE 1999022600199 19990226 00199 NM 1999 2 26 DHL9974028C 1 19990203 A 5320 WEB BOEING 727 7272Q9 138448M NM BS 294 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, RT HORIZ WEB HAS CORROSION BULGING AND POPPED RIVETS AT RT INBD SIDE NEXT TO NOSE WHEEL WELL BOX STA 294 TO 360. REMOVED INTERNAL RT WEB CENTER WEB FOR REPAIR. REMOVED CHORD ANGLE. REMOVED FWD AND AFT VERTICAL STIFFENERS AND GEAR FITTING SUPPORT. CLEANED VERTICAL WEB AND WEB SUPPORT. FABRICATED NEW INBOARD HORIZ WEB PER SRM 53-10-1, 10.25 BY 56.5. REINSTALLED REMOVED COMPONENTS, N/R 3112. 2 L 7 3 4F RT A3WE 1999022600200 19990226 00200 NM 1999 2 26 DHL9974029C 1 19990210 A 5720 STIFFENER BOEING 727 7272Q9 138448M NM WS 170 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT LOWER LEG W/S 170. REMOVED WEB, INSTALLED ANGLE REPAIR PER S RM 51-40-4, 4 BY 6, N/R 2108. 2 L 7 3 4F RT A3WE 1999022600201 19990226 00201 NM 1999 2 26 DHL9974030C 1 19990209 A 5313 STRINGER BOEING 727 7272Q9 138448M NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, CORROSION ON STR 29 STA 950 F, FOUND STR 29R CRACKED AT STA 950D TO 950F AND CORROSION OUT OF LIMITS FROM 95 0 TO 990. FOUND FRAME TO SKIN CLIP CRACKED AT STA 990. FOUND VERTICAL U-CHANNEL FLOOR SUPPORT CRACKED. REPLACED STRIN GER 29 RT FROM STA 950 TO STA 1010 PER AVITAS EO 99PMSI259D-1. FABRICATED AND INSTALLED NEW ATTACH CLIP AND VERTICAL U -CHANNEL PER SRM 53-10-1 AND 51-30-2, 7.5 BY 6, N/R 3167. 2 L 7 3 4F RT A3WE 1999022600202 19990226 00202 NM 1999 2 26 DHL9974031C 1 19990201 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 950 MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, SCAB PATCH BELOW AFT CARGO DOOR BETWEEN STA 950D AND STA 950F NOT PER SRM. REMOVED DOUBLER, REPLACED STRIN GER FROM STA 950D TO 1010 PER AVIATAS EO 99PMSI259D-1. INSTALLED EXTERNAL REPAIR PER AVITAS EO 99 PMSI 259D1 AT STA 950 DD AND 950F, 16.5 BY 5.5 AND 14 BY 3. INSTALLED FRAMES AT STA 950F AND 970. REPAIRED PER AVITAS EO 99PMSI259-1, 12 BY 13 AND 9 BY 8, N/R 3052. 2 L 7 3 4F RT A3WE 1999022600203 19990226 00203 NM 1999 2 26 DHL9974032C 1 19990211 A 5320 INTERCOSTAL BOEING 727 7272Q9 138448M NM BS 360 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C CHECK, INTERCOSTAL CRACKED STRINGER 5 R, BS 360. REMOVED CRACKED INTERCOSTAL. REPLACED INTERCOSTAL WEB PER SRM 53 -10-1, 20 BY 4, N/R 5744. 2 L 7 3 4F RT A3WE 1999022600204 19990226 00204 GL 1999 2 26 DHL99804001 2 19990211 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C5 GL NR 4 FLAMED OUT A DHLA K NONE X ENGINE FLAMEOUT CR CRUISE 1 SO 01 804DH 46124 NR 4 ENGINE FLAMED OUT 200 MILES FROM JFK, TRIED RESTART AT FL 310 AND AT FL 180. NOTICED FUEL PRESSURE AT 50 PSI . ON RESTART ATTEMPT, NR 4 N1 DID NOT ACHIEVE FLIGHT IDLE. N1- 23 PERCENT, EGT 238 , F/F 600PPH. ACCOMPLISHED NR 4 MAIN FU EL TANK NEGATIVE PRESSURE CHECK. REMOVED AND REPLACED MAIN FUEL FILTER AS PRECAUTION. RAN ENGINE, OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999022600206 19990226 00206 CE 1999 2 26 CA990202001 1 19990106 A 2730 115610010325 TORQUE TUBE BEECH 100 100BEECH 1152916 CE ELEVATOR MISMANUFACTURED W O OTHER F W FLT CONT AFFECTED INADEQUATE Q C AP APPROACH 1 CA 1 (CAN) FIRST FLIGHT AFTER LEFT ELEVATOR TORQUE TUBE ASSY REPLACED, THE PILOT NOTICED AN OBSTRUCTED ELEVATOR CONTROL. ELE V MOVEMENTS JERKY. LANDED OK. LEFT ELEVATOR ATTACH BRACKET CUT-OUT SKIN FOULING WITH STAB ATTACH BRACKET. SPACERS INS TALLED. FURTHER EXAMINATION FOUND THAT THE NEW TORQUE TUBE ASSY WAS .1250 INCH SHORTER THAN THE ORIGINAL CAUSING THE EL EVATOR TO MOVE INBOARD. OK WHEN CHECKING ON GROUND, BUT IN AIR WITH AIR LOADS MOVED, THE ELEVATOR INBOARD ON SUPPORT BE ARING SURFACE JUST ENOUGH TO CAUSE INTERFERENCE FOULING. BEECH CONTACTED. 1 L 7 2 3T A14CE 1999022600212 19990226 00212 NM 1999 2 26 CA990203019 1 19990104 A 2710 SERVO AIRBUS A319 A319114 NM AILERON MALFUNCTIONED W K NONE O OTHER CR CRUISE 1 CA (CAN) FLIGHT CONTROL AILERON SERVO FAULT WITH ASSOCIATED UNCOMMANDED ROLL TO ABOUT 20 DEGREES, INDICATION LEFT AILERON B SERVO IN AMBER ON ELEVATOR/AILERON COMPUTER 1. CENTRALIZED D FAULT DISPLAY SYSTEM FAULTED B-MODE VALVE 33C23. REPLACE D LT AILERON B SERVO, OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A28NM 1999022600213 19990226 00213 NM 1999 2 26 CA990203020 1 19990116 A 2120 FILTER AIRBUS A319 A319114 NM NR 1 PACK CONTAMINATED W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CA (CAN) ON LANDING, THE CABIN FILLED WITH WHITE/GREY SMOKE LIKE THROUGH AIR VENTS/READING LIGHTS. AIRCRAFT STOPPED AT IDL E POWER, MIST SUBSIDED. PACK NUMBER ONE SHUT DOWN, MIST REAPPEARED WHEN NR 2 ENGINE POWERED UP. REPLACED CIRCULATION F ILTERS, POWER ASSURANCE CHECK CARRIED OUT, ALL PARAMETERS NORMAL. 2 L 7 2 4F RT A28NM 1999022600214 19990226 00214 1999 2 26 CA990203023 4 19990120 A 2300 6228125002 CONTROL PANEL COLLINS 6228125002 AIRBUS 320 A320211 3930320 EU COCKPIT FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) VISIBLE SMOKE FROM NUMBER 1 RADIO MANAGEMENT PANEL AND FREQUENCY INDICATORS. TURNED NR 1 RADIO MANAGEMENT PANEL O FF AND PULLED CIRCUIT BREAKER. CHANGED RADIO MANAGEMENT PANEL. 2 L 7 2 4F RT A28NM 1999022600215 19990226 00215 NM 1999 2 26 CA990203024 1 19990118 A 2710 ACTUATOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE AILERON FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA P709649 (CAN) ENGINE INDICATING AND CREW ALERT SYSTEM MESSAGE AILERON LOCK OUT, OVERHEAD LIGHT. CHANGED RT AILERON LOCK ACTUATO R AND SLAT/AILERON MODULE, SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999022600216 19990226 00216 EU 1999 2 26 CA990209017 2 19990122 A 7200 ENGINE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU NR 2 FAILED W A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CA 18621 4062 RH15119 (CAN) IN CRUISE, THE NR 2 ENGINE ABRUPTLY HAD AN UNCOMMANDED SHUTDOWN. THE AIRCRAFT CONTINUED TO DESTINATION AND MADE A SUCCESSFUL SINGLE ENGINE LANDING. POST-FLIGHT INSPECTION INDICATES A LAYSHAFT/NOSE CASE INTERNAL FAILURE. THE ENGINE WAS SENT FOR OVERHAUL AND INVESTIGATION. PART TC: 4,818. 2 L 7 2 3T 4 T A24EU A196 1999022600217 19990226 00217 WP 1999 2 26 TWAA9902701 1 19990216 A 2497 WIRE DOUG DC9 DC983 3022083 WP BS 1380 SHORTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 FOUND ONE PHASE OF THE LT GENERATOR FEEDER CABLE SHORTING IN TAIL CONE AREA, LT LOWER BELT RING. THE BULKHEAD AT STA 13 80 LT SIDE AT ABOUT LONGERON 19L HAD HOLE BURNED IN IT FROM THE GENERATOR FEEDER CABLE. CUT AND RE-TERMINATED ALL THREE PHASES OF LEFT ENGINE GENERATOR CABLE PER MM 20-50-01. REPAIRED DAMAGED AREA PER SRM 53-01 FIG 4. CHECK-C 1-15-99 MCI . 2 L 7 2 4F RT A6WE 1999022600218 19990226 00218 NM 1999 2 26 TWAA9902702 1 19990222 A 3397 WIRE BOEING 767 7673Q8 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 FOUND THE FIRST TWO EGRESS LIGHTS INOPERATIVE ON RT SIDE OF FIRST CLASS. RECONNECTED LOOSE WIRES NEAR PAX SEAT 1 TO 8. CHECK-C 12-16-98 LAX. 2 L 7 2 4F RT A1NM 1999022600219 19990226 00219 1999 2 26 TWAA9902703 4 19990220 A 2565 113317 SLIDE DOUG DC9 DC951 3022051 WP PAX DOOR AIR LEAK A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 418EA 47676 THE FWD LT CABIN DOOR ESCAPE SLIDE WAS FOUND WITH LOW AIR BOTTLE PRESSURE. REPLACED THE SLIDE PER MC82501. CHECK-C 3-3 0-98 STL. 2 L 7 2 4F RT A6WE 1999022600220 19990226 00220 NM 1999 2 26 TWAA9902704 1 19990221 A 3350 1000679 LIGHT BOEING 727 727231 1384079 NM GALLEY DOOR WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54334 20461 FOUND THE EMERGENCY LIGHT INOPERATIVE OVER THE AFT GALLEY DOOR. REPLACED THE LIGHT ASSEMBLY. CHECK-C 8-21-98 MCI. 2 L 7 3 4F A3WE 1999022600221 19990226 00221 WP 1999 2 26 TWAA9902705 1 19990215 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-207 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND IN CABIN THE LT O/B SEAT TRACK WITH CORROSION, STA 200 TO 207. REPAIRED PER SRM 53-05, FIG 4F, SHEET 6. REPLACED TRACK. 2 L 7 2 4F A6WE 1999022600222 19990226 00222 WP 1999 2 26 TWAA9902706 1 19990216 A 5320 DECK DOUG DC9 DC931 3022065 WP BS 47.8 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND UPPER PRESSURE DECK AT APPROXIMATELY STA 47.8 WITH A CRACK ABOUT 4 INCHES LONG. CONFIRM ED WITH EDDY CURRENT. REPLACED Y ANGLE PER SPM 6-70-01, DRAWING 9911500, AND SRM 51-60-0, PAGE 27 ITEM E. 2 L 7 2 4F A6WE 1999022600223 19990226 00223 NM 1999 2 26 TWAA9902707 1 19990214 A 5753 PANEL BOEING 757 757231 1384950 NM LT TE FLAP DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 714P 28482 DURING CHECK-C MAINT, FOUND THE LT WING I/B FLAP TRAILING EDGE AFT FLAP BOTTOM SIDE, LOWER WEDGE PANEL WITH A .375 INCH TEAR LOCATED APPROXIMATELY 4 FT O/B BY 11 INCHES HIGH FROM I/B END. REPAIRED PER SRM 51-70-17 (REFERRED FROM SRM 57-53- 01) WITH MINIMUM OF 2 PLYS PER NOTE B OF FIG 24, WITH 2 LAYERS OF ADHESIVE TOP AND BOTTOM. COOKED AT 200 DEG, SEALED AN D PAINTED. 2 L 7 2 4F RT A2NM 1999022600224 19990226 00224 NM 1999 2 26 TWAA9902708 1 19990204 A 5315 FLOORBEAM BOEING 727 727231 1384079 NM GALLEY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54344 21631 DURING CHECK-C MAINT, FOUND IN FORWARD GALLEY THE FLOORBEAM HAD CORROSION JUST FORWARD OF NR 2 GALLEY ON RT SIDE. REPLA CED FLOORBEAM SUPPORT PER DRAWING NR 65-64950, AND TRACK PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999022600225 19990226 00225 WP 1999 2 26 TWAA9902709 1 19990213 A 5320 CASTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND THE FLOOR SUPPORT CASTING CRACKED AT LOWER END, STA 680 LBL 44 IN. REMOVED OLD CASTING AND REPLACED WITH NEW CASTING PER STANDARD PROCESSES MANUAL 67-70-1. 2 L 7 2 4F A6WE 1999022600226 19990226 00226 NM 1999 2 26 CALA9900169 1 19990219 A 5230 BEAM BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR LOWER EDGE BEAM. THE LOWER EDGE BEAM WAS REPLACED IAW BOEING DRAWI NG NR 143N6603 AND SRM 52-30-02. 2 L 7 2 4F RT A2NM 1999022600227 19990226 00227 NM 1999 2 26 CALA9900170 1 19990219 A 3397 WIRE BOEING 727 727224 1384076 NM L2 DOOR LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND L-2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE AT POWER SUPPLY CONNECTOR. T HE WIRING WAS SECURED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-22, PAGE 201. 2 L 7 3 4F A3WE 1999022600228 19990226 00228 NM 1999 2 26 CALA9900171 1 19990219 A 3397 WIRE BOEING 727 727224 1384076 NM LT EMER EXIT FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND POWER WIRE AT BATTERY PACK AT FAULT. THE WIRING SPLICE WAS REPAIRED IAW MM 33-51-01. 2 L 7 3 4F A3WE 1999022600229 19990226 00229 NM 1999 2 26 CALA9900172 1 19990219 A 5753 652163491 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LT WING I/B AFT FLAP DELAMINATED. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-50-2. 2 L 7 3 4F A3WE 1999022600230 19990226 00230 NM 1999 2 26 CALA9900173 1 19990219 A 5744 69174013 FITTING BOEING 727 727224 1384076 NM RT AILERON TAB BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND RT O/B AILERON TAB SUPPORT FITTING (SECOND FROM O/B END) BROKEN OFF INSIDE AILERON. THE TAB SUPPORT FI TTING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-30-2. 2 L 7 3 4F A3WE 1999022600231 19990226 00231 NM 1999 2 26 CALA9900174 1 19990219 A 3397 WIRE BOEING 727 727224 1384076 NM CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND FORWARD AISLE EMERGENCY CEILING LIGHT INOPERATIVE. MAINTENANCE FOUND EMERGENCY AISLE LIGHT FORWARD SEC TION WIRING SPLICE AT FAULT. THE WIRING SPLICE WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-5, PAGE 501. 2 L 7 3 4F A3WE 1999022600232 19990226 00232 NM 1999 2 26 CALA9900175 1 19990220 A 5730 114N210812 PANEL BOEING 757 757224 1384958 NM RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND RT WING FIXED L/E PANEL O/B OF PYLON DELAMINATED. THE FIXED L/E PANEL WAS REMOVED AND REPAIRED IAW SRM 51-70-08. THE PANEL WAS RE-FIT IAW STANDARD PRACTICES. 2 L 7 2 4F RT A2NM 1999022600233 19990226 00233 NM 1999 2 26 CALA9900176 1 19990220 A 5730 114N210811 PANEL BOEING 757 757224 1384958 NM WS 320 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND LT WING FIXED L/E PANEL OUTBOARD OF PYLON AT WS 320 DELAMINATED. THE FIXED L/E PANEL WAS REMOVED AND R EPAIRED IAW SRM 51-70-08. THE PANEL WAS RE-FIT IAW STANDARD PRACTICES. 2 L 7 2 4F RT A2NM 1999022600234 19990226 00234 NM 1999 2 26 CALA9900177 1 19990222 A 5711 SPAR CHORD BOEING 727 727224 1384076 NM WS 355-367 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND TOP SURFACE OF LT WING FRONT SPAR LOWER CHORD CORRODED AT FS 355 TO 367. THE FASTENERS AND RIB WERE RE MOVED FOR ACCESS. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-1, 51-20-2, AND ECRA 5710-01945. 2 L 7 3 4F A3WE 1999022600235 19990226 00235 NM 1999 2 26 CALA9900178 1 19990222 A 5755 651734781A SKIN BOEING 727 727224 1384076 NM NR 2 SPOILER DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND THE LT WING NR 2 SPOILER DEBONDED AT TRAILING EDGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 2 7-61-81. 2 L 7 3 4F A3WE 1999022600236 19990226 00236 NM 1999 2 26 CALA9900179 1 19990222 A 5753 652163127 SKIN BOEING 727 727224 1384076 NM RT TE FOREFLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND RT O/B FOREFLAP CORRODED ON LOWER AND UPPER SURFACE I/B TO O/B. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11. 2 L 7 3 4F A3WE 1999022600237 19990226 00237 NM 1999 2 26 CALA9900180 1 19990222 A 5753 652163586 SKIN BOEING 727 727224 1384076 NM RT TE AFT FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND RT TRAILING EDGE O/B AFT FLAP LOWER SURFACE DELAMINATED. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-50-02. 2 L 7 3 4F A3WE 1999022600238 19990226 00238 NM 1999 2 26 CALA9900181 1 19990222 A 5754 651622292 SKIN BOEING 727 727224 1384076 NM NR 6 LE SLAT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LT WING NR 6 L/E SLAT O/B END UPPER AND LOWER SURFACES CORRODED AT SCREWS. THE SLAT WAS REMOVED AND RE PLACED IAW MM 27-80-00. 2 L 7 3 4F A3WE 1999022600239 19990226 00239 NM 1999 2 26 CALA9900182 1 19990222 A 5755 651734754 SKIN BOEING 727 727224 1384076 NM NR 13 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND THE LT WING NR 13 SPOILER UPPER TRAILING EDGE DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-00. 2 L 7 3 4F A3WE 1999022600240 19990226 00240 SO 1999 2 26 COMA9910037 1 19990220 A 5246 12047700001 FUEL DOOR EMB 120 EMB120RT SO RT WING MISSING A COMA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SO 01 267CA 120259 SINGLE POINT FUEL SERVICE DOOR MISSING. REPAIRED DAMAGE CAUSED BY SEPARATION OF FUEL SERVICE DOOR AND REPLACED DOOR. 2 L 7 2 4T RT A31SO 1999022600241 19990226 00241 NE 1999 2 26 COMA9910038 2 19990219 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 268CA 7213 120262 115480 LEFT ENGINE TEMP REACHED 820 DEGREES DURING TAKEOFF. REPLACED ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600242 19990226 00242 1999 2 26 COMA9960074 4 19990217 A 3417 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA ADC SYST TRIPPED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 995CA 7229 A 20 KNOT DIFFERENCE BETWEEN PILOT AND CO PILOT AIR SPEED INDICATORS. INSPECTED PITOT SYSTEM, FOUND NO DISCREPANCIES. R ESET ADC CIRCUIT BREAKERS AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A21EA 1999022600243 19990226 00243 EA 1999 2 26 COMA9960075 1 19990221 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA ROW 8 INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 EMERGENCY FLOOR LIGHTING AFT OF ROW 8 IS INOPERABLE. DISCONNECTED AND RECONNECTED LIGHT STRIP SYSTEM, OPERATION NORMAL. 2 L 7 2 4F RT A21EA 1999022600244 19990226 00244 EA 1999 2 26 COMA9960076 1 19990220 A 7830 CAUTION LIGHT CNDAIR CL600 CL6002B19 EA LT ENG TR SYST ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 934CA 7042 LEFT ENGINE THRUST REVERSER UNLOCKED CAUTION MESSAGE. INSPECTED THRUST REVERSER SYSTEM, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999022600245 19990226 00245 NM 1999 2 26 UPS99228745 1 19990220 A 3350 BULB BOEING 727 727108C 1384039 NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-N/A, EMER EXIT LIGHT ABOVE COCKPIT ENTRY DOOR VERY WEAK. RELAMPED, OPS CHECKS OK. 2 L 7 3 4F A3WE 1999022600246 19990226 00246 NM 1999 2 26 UPS99228746 1 19990219 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER EXIT LIGHT AT LOWER FWD END OF GALLEY DOOR INOP. REMOVED AND REPLACED EMER EXIT LIGHT BATTERY AT FWD GALLEY EXIT DOOR IAW MM 33-50- 81, OPS CHK NORMAL. 2 L 7 3 4F A3WE 1999022600247 19990226 00247 NM 1999 2 26 UPS99228747 1 19990219 A 3350 BULB BOEING 727 72725C 138400H NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER EXIT LIGHT AT LOWER FWD END OF ENTRY DOOR INOP. REMOVED AND REPLACED LIGHT BULBS AT LOWER FWD ENTRY DOOR EMER EXIT LIGHT, OPS CK NORMAL. 2 L 7 3 4F A3WE 1999022600248 19990226 00248 NM 1999 2 26 UPS99228748 1 19990204 A 5320 WEB BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE-C, CORROSION (C53-132-02-01-01) 870.5 WEB RBL WL 153 AROUND CANNON PLUG CONNECTORS (MARKED). REMOVED D AMAGED AREA AND INSTALLED REPAIR PARTS PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999022600249 19990226 00249 NM 1999 2 26 UPS99228749 1 19990215 A 5751 65192596 HINGE BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND O/B FWD HINGE HALF CORRODED, LT WING O/B AILERON. REMOVED C ORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999022600250 19990226 00250 NM 1999 2 26 UPS99228750 1 19990215 A 5751 651962012 HINGE BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER I/B FWD HINGE HALF CORRODED. REM OVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999022600251 19990226 00251 NM 1999 2 26 UPS99228751 1 19990215 A 5751 6521727U20 FITTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE-C, RT WING O/B AILERON ACTUATOR ROD END FITTING IS CORRODED. REMOVED CORROSION FITTING AND INSTALLED NE W FITTING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999022600252 19990226 00252 NM 1999 2 26 UPS99228752 1 19990215 A 5320 WEB BOEING 727 72725C 138400H NM BS 1147 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE-C, CORROSION ON SHEAR WEB BS 1147, LBL 50, WL 208. DAMAGED CLEAN-UP BEYOND ALLOWABLE LIMITS PER SRM 51- 10-06. AREA SIZE TO BE .013 X 2.5 X 2.5. DAMAGED AREA REMOVED AND WEB WAS REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1999022600253 19990226 00253 NM 1999 2 26 UPS99228753 1 19990203 A 5754 65162271 RIB BOEING 727 72725C 138400H NM NR 1 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE-C, CORROSION (C57-562-01.00-01) LT WING NR 1 K-FLAP CORRODED AROUND BONDING JUMPER BOLT HOLE ON BOTH SID ES OF RIB. CORROSION OUT OF LIMITS. REMOVED AND INSTALLED NEW K-FLAP. WORK DONE IAW SRM 57-50-1, MM 27-81-01. 2 L 7 3 4F A3WE 1999022600254 19990226 00254 NM 1999 2 26 UPS99228754 1 19990215 A 5751 65192596 HINGE BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD 866785 FOUND LT WING O/B AILERON CENTER O/B FWD HINGE HALF CORRODED. REM OVED CORRODED HINGE AND INSTALLED NEW HINGE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999022600255 19990226 00255 NM 1999 2 26 UPS99228755 1 19990208 A 3211 65844055 TRUNNION BOEING 727 72725C 138400H NM LT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE-C, LT MLG FORWARD TRUNNION FITTING CRACKED. REMOVED AND REPLACED LT MLG FORWARD TRUNNION FITTING IAW MM 32-11-51. 2 L 7 3 4F A3WE 1999022600256 19990226 00256 NM 1999 2 26 UPS99228756 1 19990209 A 5743 65999091725 FITTING BOEING 727 72725C 138400H NM LT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE-C, LT MLG FWD TRUNNION AFT SPAR SUPPORT CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING PER SRM 51-30-1, AND DWG 65-19297. 2 L 7 3 4F A3WE 1999022600257 19990226 00257 NM 1999 2 26 UPS99528744 1 19990219 A 2150 VALVE BOEING 757 75724APF 1384969 NM RT PACK MALFUNCTIONED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 414UP 23854 INSPECTION TYPE-N/A, DURING FLT RT PACK TEMP LIGHT ILLUMINATED WITH RT PACK ON AND LT PACK OFF. RT PACK INOP LIGHT THEN ILLUM MOMENTARILY, TURNED RT PACK OFF AND LT PACK ON. LARGE AMOUNT OF SMOKE STARTED OUT OF VENTS BELOW GLARESHIELD. T URNED RT PACK BACK ON AND SMOKE SUBSIDED AND DISSIPATED. REMOVED AND REPLACED RT PACK TEMP CONTROL VALVE PER M/M 21-51- 12, OPS CHKS GOOD. 2 L 7 2 4F RT A2NM 1999022600258 19990226 00258 NM 1999 2 26 UPS99528762 1 19990219 A 3350 BATTERY PACK BOEING 757 75724APF 1384969 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 426UP 25457 INSPECTION TYPE-N/A, EMER EXIT LIGHT FAILED TO COME ON DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK A ND OPERATIONAL FUNCTION CKS GOOD. ACFT OK FOR SERVICE PER MM 33-51-07. 2 L 7 2 4F RT A2NM 1999022600259 19990226 00259 1999 2 26 QXEA9900308 4 19990204 A 3455 71128417 CONTROL HEAD DHAV DHC8 DHC8102 2809003 NM ADF SYST FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 826PH 26916 3998 214 SEA- ELECTRICAL SMELL IN COCKPIT. MAINTENANCE INSPECTED AND DETERMINED TO BE FROM THE ADF CONTROL HEAD. REPLACED ADF C ONTROL HEAD, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999022600260 19990226 00260 NM 1999 2 26 QXEA9900309 1 19990212 A 5210 MECHANISM DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 826PH 526 SEA- FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBRICATED TH E MAIN CABIN DOOR STOPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999022600261 19990226 00261 NM 1999 2 26 QXEA9900310 1 19990219 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 824PH 157 SEA- THE MAIN CABIN DOOR LEVER IS VERY HARD TO OPEN FROM THE INSIDE. MAINTENANCE CLEANED AND LUBRICATED THE DOOR STOPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999022600262 19990226 00262 WP 1999 2 26 ABXA9900119 1 19990118 A 5751 57630901 FITTING DOUG DOUG DC8 DC863 302198A WP LT AILERON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT INBOARD AILERON, INBOARD HINGE FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999022600263 19990226 00263 WP 1999 2 26 ABXA9900120 1 19990114 A 5320 3755822 FITTING DOUG DOUG DC8 DC863 302198A WP BS 290 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 BATHTUB FITTING CORRODED AT STATION 290 AND LONGERON 29 LEFT. REPLACED FITTING IAW DC8 SRM 51-01-20D AND 53-2-0. 2 L 7 4 4F 4A25 1999022600264 19990226 00264 WP 1999 2 26 ABXA9900121 1 19990121 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 841 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING OUTBOARD LEADING EDGE UPPER RIB WAS CRACKED INSIDE PANEL 517B AT STATION FS 841. REPAIRED IAW DC8 SRM 51-1-2 0D. 2 L 7 4 4F 4A25 1999022600265 19990226 00265 WP 1999 2 26 ABXA9900122 1 19990119 A 5414 5769859 SKIN DOUG DOUG DC8 DC863 302198A WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT WING INBOARD NR 2 PYLON LOWER AFT SKIN CRACKED AT LOWER TRAILING EDGE. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999022600266 19990226 00266 WP 1999 2 26 ABXA9900123 1 19990119 A 5310 5616306 STRUCTURE DOUG DOUG DC8 DC863 302198A WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 ONE-HALF INCH CRACK IN LEFT MAIN LANDING GEAR WHEEL WELL STRUCTURE. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999022600267 19990226 00267 WP 1999 2 26 SCNA99038 1 19990218 A 3244 50003064 TIRE DOUG DC10 DC1015 3022118 WP MLG FAILED A SCNA K NONE O OTHER LD LANDING 1 GL 15 153SY 128 48276 DURING LANDING, THE NR 8 MAIN TIRE BLEW OUT. REMOVED AND REPLACED THE NR 8 AND NR 7 TIRE PER MM 324101. 2 L 7 3 4F A22WE 1999022600268 19990226 00268 NM 1999 2 26 SCNA99039 1 19990220 A 3350 LIGHT BOEING 727 7272A1 138407F NM ROW 32C INOP A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 287SC 21345 THE EMERGENCY EXIT FLOOR LIGHT BY SEAT 32C WAS FOUND TO BE INOPERATIVE. RELAMPED THE EMERGENCY EXIT FLOOR LIGHT AND REP LACED THE LENS AT 32C. 2 L 7 3 4F A3WE 1999022600269 19990226 00269 NM 1999 2 26 SCNA99040 1 19990216 A 3350 1495X LIGHT BOEING 727 7272A1 138407F NM AFT AIRSTAIR INOP A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED AFT AIRSTAIR EM ERGENCY LIGHT, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999022600270 19990226 00270 NM 1999 2 26 SCNA99041 1 19990219 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM RT EMER EXIT DISCHARGED A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE RIGHT EXTERIOR OVERWING FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOV ED AND REPLACED THE BATTERY FOR M655, SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999022600271 19990226 00271 WP 1999 2 26 RRXA99126 1 19990218 A 3411 PITOT SYST DOUG DC8 DC873F 302199F WP LT & RT CONTAMINATED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 870TV 46086 IN CRUISE, AIRSPEED WENT TO 60 KT AND STANDBY FLAGS IN BOTH AIRSPEED INDICATORS AND F/O'S ALTIMETER. REGAINED AIRSPEED INDICATOR JUST BEFORE LANDING. PURGED SYSTEM WITH NITROGEN AND PERFORMED OPERATIONAL LEAK CHECK WITH PITOT STATIC RAMP TESTER WITH NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999022600272 19990226 00272 1999 2 26 VNAA9902009 4 19990216 A 3425 7014300902 DISPLAY UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FLIGHT DECK FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 328JS 58357 3030 THE NUMBER ONE DISPLAY UNIT FAILED AFTER PUSHBACK. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLAC ED THE NUMBER ONE DISPLAY UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-14-00. OPERATIONAL CHECKS WERE COMPLET ED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999022600273 19990226 00273 NM 1999 2 26 VNAA9903010 1 19990223 A 3350 321473 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 5 & 6 FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 328JS 3030 DURING THE PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS AT ROWS FOUR AND SIX WERE NOTED TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE EMERGENCY BATTERY PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. LATER IN THE DAY THE POWER SUPPLY WAS REPLACED PER THE MAINTENANCE MANUAL FOR FAILURE HISTORY REASONS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999022600274 19990226 00274 NM 1999 2 26 VNAA9902011 1 19990220 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 460PS 61560 765 3061 DURING THE PREFLIGHT INSPECTION, TWO STRIPS OF EMERGENCY FLOOR LIGHTING WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPE CTED AND REPLACED THE EMERGENCY BATTERY PACK AT 5LK POSITION, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. O PERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999022600275 19990226 00275 NM 1999 2 26 VNAA9902012 1 19990221 A 3350 331430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 11 DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 458PS 68303 764 3068 DURING THE POSTFLIGHT INSPECTION, EMERGENCY LIGHTS AT ROW 11 WERE NOTED TO BE INOPERATIVE. OUTSTATION MAINTENANCE INSPE CTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FERRY FLIGHT TOOK PLACE WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT 7LK POSITION, IN ACCORDANCE WITH DORNIER MAINTEN ANC MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999022600276 19990226 00276 NM 1999 2 26 SWAA990283 1 19990217 A 2120 AIR DIST BOEING 737 7373T0 1384582 NM COCKPIT ODOR A SWAA O OTHER N B FALSE WARNING SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 697SW 23838 DURING CRUISE, CREW NOTICED FAINT ELECTRICAL ODOR. ALL ELECTRICAL INDICATIONS NORMAL EXCEPT NR 1 GENERATOR DRIVE RISE I NDICATED 25 TO 30 DEGREE CELSIUS. DURING APU START HAD APU FIRE WARNING INDICATION, APU EGT 380 DEGREE CELSIUS. PULLED APU FIRE HANDLE AND APU FIRE LIGHT EXTINGUISHED. NR 1 GEN RISE REMAINED AT 30 DEGREE CELSIUS. CHECKED ALL C/B PANELS FOR FAINT ODOR, PERFORMED NR 1 ENGINE RUN-UP FOR OIL TEMP INDICATION, ALL CHECKED NORMAL PER MM FOR APU FIRE WARNING. 2 L 7 2 4F RT A16WE 1999022600277 19990226 00277 NM 1999 2 26 SWAA990284 1 19990220 A 5730 SKIN BOEING 737 7372T4 1384492 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND NR 4 AND 5 SLATS O/B AUX FIXED L/E CUTOUT SKIN CRACKED. REPAIRED PER TRAMCO EWO 99-0111 . 2 L 7 2 4F A16WE 1999022600278 19990226 00278 NM 1999 2 26 SWAA990285 1 19990220 A 5320 CHORD BOEING 737 7372T4 1384492 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND Z CHORD CORRODED AT BS 270, LBL 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600279 19990226 00279 NM 1999 2 26 SWAA990286 1 19990220 A 5320 WEB BOEING 737 7372T4 1384492 NM BS 303.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 303.9, LBL 63, WL 215. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600280 19990226 00280 NM 1999 2 26 SWAA990287 1 19990220 A 5320 CHORD BOEING 737 7372T4 1384492 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FAIL-SAFE CHORD CRACKED AT BS 360, RBL 64. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600281 19990226 00281 NM 1999 2 26 SWAA990288 1 19990220 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED AT BS 907. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600282 19990226 00282 NM 1999 2 26 SWAA990289 1 19990220 A 5311 FRAME BOEING 737 7372T4 1384492 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600283 19990226 00283 NM 1999 2 26 SWAA990290 1 19990220 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 727 TO 947. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600284 19990226 00284 NM 1999 2 26 SWAA990291 1 19990220 A 5312 BULKHEAD ANGLE BOEING 737 7372T4 1384492 NM BS 380 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TO BULKHEAD SUPPORT ANGLE CORROSION AT BS 380. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600285 19990226 00285 NM 1999 2 26 SWAA990292 1 19990220 A 5320 TIE STRAP BOEING 737 7372T4 1384492 NM BS 430 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FLOOR TIE STRAP CORROSION AT BS 430, RBL 13 - LBL 24. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600286 19990226 00286 NM 1999 2 26 SWAA990293 1 19990218 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGE AT BS 500, S4L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600287 19990226 00287 NM 1999 2 26 SWAA990294 1 19990218 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE DAMAGE AT BS 360, S15R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600288 19990226 00288 NM 1999 2 26 SWAA990295 1 19990218 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 306 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED AT BS 306, 3 ABOVE S10L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600289 19990226 00289 NM 1999 2 26 SWAA990296 1 19990218 A 5320 CHORD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND SIDE CHORD CRACKED AT BS 178, WL 207 AND 195.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600290 19990226 00290 NM 1999 2 26 SWAA990297 1 19990220 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600291 19990226 00291 NM 1999 2 26 SWAA990298 1 19990220 A 5320 ANGLE BOEING 737 7372T4 1384492 NM BS 934 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH ANGLE CRACKED AT BS 934. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600292 19990226 00292 NM 1999 2 26 SWAA990299 1 19990217 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD SKIN CRACKED AT LBL AND RBL 12. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600293 19990226 00293 NM 1999 2 26 SWAA990300 1 19990217 A 5320 WEB BOEING 737 7372H4 138448C NM BS 180 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED 1/4D CHECK, FOUND HORIZONTAL WEB CRACKED AT BS 180, RBL 26. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600294 19990226 00294 NM 1999 2 26 SWAA990301 1 19990217 A 5230 CHORD BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR T CHORD CRACKED AT FWD STOP CASTING AND 2ND FROM BOTTOM. REMOVED AND REPLACED DOOR PER BOEING M/M. 2 L 7 2 4F A16WE 1999022600295 19990226 00295 NM 1999 2 26 SWAA990302 1 19990218 A 5320 STOP BOEING 737 7373H4 1384600 NM LT, RT EMER EXIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RT AND LT OVERWING EMERGENCY EXIT FWD STOP PADS CRACKED. REMOVED AND REPLACED STOP PAD S PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999022600296 19990226 00296 NM 1999 2 26 SWAA990303 1 19990218 A 1100 PLACARD BOEING 737 7373H4 1384600 NM OVERWING TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY PLACARD TORN. REPLACED PLACARD PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999022600297 19990226 00297 NM 1999 2 26 SWAA990304 1 19990218 A 5312 BULKHEAD STRAP BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND .125 INCH CRACK COMING FROM HI-LOK IN WEB STRAP WL 191.5 LBL 5 FWD SIDE OF BLKHD. DO UBLER REPAIR HAS BEEN INSTALLED PER SRM 51-40-02. 2 L 7 2 4F A16WE 1999022600298 19990226 00298 NM 1999 2 26 SWAA990305 1 19990218 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND INDICATION OF CORROSION ON OUTER SKIN AND FASTENERS STA 727+6 FROM STR 276 TO 27R. R EPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600299 19990226 00299 NM 1999 2 26 SWAA990306 1 19990218 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED CHECK, FOUND 4 INCH FUSELAGE SKIN CRACK ON RT SIDE ABOVE NR 24 PAX WINDOW. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600300 19990226 00300 NM 1999 2 26 SWAA990307 1 19990218 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK AT AFT SERV DOOR AT LOWER HINGE ARM CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600301 19990226 00301 NM 1999 2 26 SWAA990308 1 19990217 A 2760 WARNING BOEING 737 7373H4 1384600 NM SPEED BRAKE SOUNDED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 383SW 26589 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. SPEED BRAKE HANDLE WAS CYCLED AND WARNING HORN SILENCED. ALL SYST EMS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 1999022600302 19990226 00302 NM 1999 2 26 SWAA990309 1 19990217 A 5230 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT CRACKED AT AFT TOP CORNER APPROX .5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999022600303 19990226 00303 NM 1999 2 26 SWAA990310 1 19990218 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED CHECK, FOUND 4 INCH FUSELAGE SKIN CRACK ON RT SIDE ABOVE NR 24 PAX WINDOW. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600304 19990226 00304 NM 1999 2 26 SWAA990311 1 19990218 A 2931 LIGHT BOEING 737 7377H4 NM COCKPIT LOOSE A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 707SA 27841 ELECTRIC LOW PRESSURE CHECK LIGHT ILLUMINATED IN FLIGHT AND WOULD NOT GO OUT. RETURNED TO MDW. TIGHTENED CORY LIGHT BA SE, OPS CK OK PER MM. 2 L 7 2 4F RT A16WE 1999022600305 19990226 00305 NM 1999 2 26 SWAA990312 1 19990218 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND HFEC INDICATION OF A CRACK IN LT SIDE CHORD AT STA 178 LBL 26 WL 195. REMOVED AND RE PLACED CHORD ANGLE PER SRM. 2 L 7 2 4F A16WE 1999022600306 19990226 00306 NM 1999 2 26 SWAA990313 1 19990218 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND HFEC INDICATION OF A 1.25 INCH CRACK IN RT SIDE CHORD AT STA 178 RBL 29. REPAIRED PE R SRM. 2 L 7 2 4F A16WE 1999022600307 19990226 00307 NM 1999 2 26 SWAA990314 1 19990218 A 5230 CHORD BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND LOWER T CHORD CRACKED AT 3RD HI-LOK FROM AFT END. REPLACED DOOR PER BOEING M/M. 2 L 7 2 4F A16WE 1999022600308 19990226 00308 NM 1999 2 26 SWAA990315 1 19990218 A 5241 FRAME BOEING 737 7372H4 138448C NM GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/4D CHECK, FOUND FWD GALLEY DOOR, FWD UPPER STUB FRAME CRACKED AT UPPER STOP FITTING APPROX 2.5 INCHES , CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600309 19990226 00309 NM 1999 2 26 SWAA990316 1 19990217 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED 1/4D CHECK, FOUND FUSE SKIN CRACKED AT AFT ENTRY DOOR UPPER CUTOUT, 2 PLACES. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600310 19990226 00310 NM 1999 2 26 SWAA990317 1 19990219 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED SC CHECK, FOUND 2 INCH CRACK BELOW STRINGER 22L, BETWEEN BS 727C AND D. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999022600311 19990226 00311 NM 1999 2 26 SWAA990318 1 19990219 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986.5 CORRODED AT BL 5, 14.5, 31.5 AND 36. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999022600312 19990226 00312 NM 1999 2 26 SWAA990319 1 19990219 A 2560 SLIDE BOEING 737 7373A4 1384585 NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE FELL OUT OF SLIDE PACK WHEN DOOR WAS BEING CLOSED. RESECURED FORWARD LEFT EMERGEN CY ESCAPE SLIDE PER M/M. 2 L 7 2 4F RT A16WE 1999022600313 19990226 00313 NE 1999 2 26 SWAA990320 2 19990219 A 7320 7139M84G01 PMC BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA K NONE O OTHER CR CRUISE 1 SW 07 363SW 26574 DURING CRUISE, AFTER ADJUSTING THROTTLE NR 2 ENGINE N1, N2, EGT AND FUEL FLOW FLUCTUATED FOR APPROX 2 MINS BEFORE ENGINE STABILIZED. PLACED ON MEL NR 73-7. A/C OK FOR CONTINUED SERVICE. PLACARDS INSTALLED. DURING OVERNIGHT MX, REPLACED NR 2 PMC PER M/M, OPS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999022600314 19990226 00314 NM 1999 2 26 SWAA990321 1 19990219 A 2761 R530351 ACTUATOR BOEING 737 7372H4 138448C NM SPEED BRAKE FAILED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 92SW 22964 FIRST TAKEOFF REJECTED DUE TO TAKEOFF WARNING HORN. SPEED BRAKE CYCLED AND FOUND OK UNTIL LANDING. NO LIGHTS ASSOCIATE D WITH SPEED BRAKE SYSTEM AND AUTO SPOILERS INOP. REMOVED AND REPLACED AUTO SPEED BRAKE ACTUATOR, OPS CKD GOOD PER M/M. 2 L 7 2 4F A16WE 1999022600315 19990226 00315 NM 1999 2 26 SWAA990322 1 19990219 A 2613 2035008300 OVERHEAT LOOP BOEING 737 7372H4 138448C NM APU MALFUNCTIONED A SWAA D RETURN TO BLOCK N FALSE WARNING IN INSP/MAINT 1 SW 07 96SW 23055 WING BODY OVERHEAT CAME ON DURING PUSHBACK. COMPLIED WITH QRH AND RETURNED TO GATE. LIGHT REMAINED ON, CONTINUED PER M EL 26-12. REMOVED AND REPLACED APU O/H LOOP AND WINGBODY O/H LOOP PER M/M. OPS CK OK PER M/M. 2 L 7 2 4F A16WE 1999022600316 19990226 00316 NM 1999 2 26 SWAA990323 1 19990218 A 2133 40631997201AA OUTFLOW VALVE BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 600WN 27694 AFTER 10 MIN AT 37,000 FT CABIN ALTITUDE BEGAN CLIMBING TO 10,000 FT. DIFFERENTIAL PRESSURE STAYED AT 7.2, NO CHANGE IN ALTN MODE. BEGAN DESCENT AND CABIN PRESSURE DECREASED TO NORMAL RANGE. OUTFLOW VALVE SHOWED CLOSED ENTIRE SEQUENCE. R EMOVED AND REPLACED CABIN PRESSURIZATION OUTFLOW VALVE (AFT) PER M/M, OPS CHECKS GOOD PER MM. 2 L 7 2 4F RT A16WE 1999022600317 19990226 00317 NM 1999 2 26 SWAA990324 1 19990220 A 5320 WEB BOEING 737 7372T4 1384492 NM BS 1094 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND LIGHTENING HOLE LOWER TORQUE BOX UPPER WEB CRACKED AT BS 1094. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999022600319 19990226 00319 NM 1999 2 26 MASA99014 1 19990122 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERABLE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 YUM/PHX - FLT 6380 - DURING WALK-AROUND, THE FLIGHT ATTENDANT NOTICED THE FORWARD FLOOR EXIT LIGHTS HAD TWO ADJACENT LIG HTS INOPERABLE. AIRCRAFT WAS FERRIED TO PHX WHERE THE PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT WAS RETURNED TO SERVIC E. (X) 2 H 7 2 4T RT A13NM 1999022600320 19990226 00320 EA 1999 2 26 MASA99015 1 19990123 A 3350 RP4010021 BATTERY P2070001214 CNDAIR CL600 CL6002B19 EA COCKPIT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 SWF/CLT - FLT 5766 - ON THE PILOT'S WALK-AROUND, THE PILOT NOTICED THE F/O'S EMERGENCY FLASHLIGHT IN THE COCKPIT WAS NOT IN ITS HOLDER CORRECTLY, AND FOUND THE BATTERY WAS DEAD. THE AIRCRAFT WAS FERRIED TO PHL WHERE MAINTENANCE REMOVED AND REPLACED THE BATTERY. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999022600321 19990226 00321 WP 1999 2 26 HALA9900041 1 19990206 A 5730 SKIN DOUG DC9 DC951 3022051 WP RT WING DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 709HA 47764 HNL - FLT 388 - (LOG PAGE NR A151708). ON PRE-FLIGHT, OBSERVED EVIDENCE OF BIRD STRIKE ON RIGHT LEADING EDGE. DID A WA LK-AROUND INSPECTION. CHECKED ENGINE INLETS AROUND FUSELAGE AND WING. OSP CHECK OK. (X) 2 L 7 2 4F RT A6WE 1999022600322 19990226 00322 NM 1999 2 26 MASA99016 1 19990128 A 3350 MS25231316 LAMP HUNTNG 8335003001 DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 436YV 436 DURING A ROUTINE MAINTENANCE INSPECTION, MAINTENANCE PERSONNEL FOUND THE NR 3 OVERHEAD EMERGENCY LIGHT WAS NOT ILLUMINAT ING. MAINTENANCE REPLACED THE BURNED OUT BULBS, OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A13NM 1999022600323 19990226 00323 EA 1999 2 26 MASA99017 1 19990128 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERABLE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 DCA/BHM - FLT 5786 - DURING POST-FLIGHT INSPECTION, CREW FOUND SEVERAL EMERGENCY AISLE LIGHTS WOULD NOT ILLUMINATE. MAI NTENANCE INSPECTED THE LIGHTS. ALL LIGHTS OPERATED NORMAL, COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999022600325 19990226 00325 GL 1999 2 26 HALA9900039 2 19990204 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 FAILED A HALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 WP 13 171AA 46906 451131 HNL - FLT 21 - (LOG PAGE NR 4821636). DURING CRUISE, NR 1 ENGINE EXHIBITED CHARACTERISTICS OF COMPRESSOR STALLS. (RAIS ING EGT, AUDIBLE RUMBLES, AND N2 DECREASING). COMPLETED APPROPRIATE CHECKLIST AND SHUT DOWN ENGINE. (X) 2 L 7 3 4F 4 F A22WE E23EA 1999022600326 19990226 00326 WP 1999 2 26 HALA9900040 1 19990205 A 2612 WIRE DOUG DC10 DC1010 3022110 WP NR 3 ENGINE CHAFED A HALA O OTHER N FALSE WARNING CL CLIMB 1 WP 13 162AA 46943 LAS - (LOG PAGE NR 4970432). ENGINE NR 3 LOOP B LIGHT FLICKERED ON AND OFF FOR 5 MINUTES DURING CLIMB-OUT. ACCOMPISHED ABNORMAL PROCEDURE CHECK LIST AND SELECTED AND TESTED LOOP A. OPS NORMAL. FOUND CHAFED WIRE. REPAIRED AND REPOSITION ED WIRE, OP CHECKS OK. (X) 2 L 7 3 4F A22WE 1999022600327 19990226 00327 WP 1999 2 26 HALA9900047 1 19990210 A 3231 LINK DOUG DC10 DC1010 3022110 WP NLG DOOR BROKEN A HALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 13 160AA 46710 LAX - FLT 09 - (LOG PAGE NR 4832289). AFTER TAKEOFF, VIBRATION FROM NOSE WHEEL DOOR. F.A. OBSERVED RT DOOR NOT RETRACT ED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN LAX. INSPECTED, FOUND NOSE DOOR DRIVE LINK BROKEN. REMOVED AND REPLACED DR IVE LINK, OPS CHECK GOOD. (X) 2 L 7 3 4F A22WE 1999022600328 19990226 00328 WP 1999 2 26 HALA9900045 1 19990209 A 7603 CONTROL CABLE DOUG DC10 DC1010 3022110 WP NR 3 THROTTLE OUT OF POSITION A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 148AA 46703 HNL - FLT 25 - (LOG PAGE NR 2344159). NR 3 THROTTLE LEVER FROZEN. REPOSITIONED NR 3 THROTTLE PUSH/PULL CABLE. ROD END BINDING AT THROTTLE IDLER CRANK. INSPECTED FOR CONDITION AND SECURITY. OPS CHECK OK. (X) 2 L 7 3 4F A22WE 1999022600329 19990226 00329 WP 1999 2 26 HALA9900046 1 19990210 A 3234 SPRING DOUG DC10 DC1010 3022110 WP GEAR HANDLE FAILED A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 122AA 46522 SEA - FLT 11 - ON TAKEOFF ROLL LANDING GEAR UNSAFE LIGHT CAME ON. ABORTED TAKEOFF. REPLACED LANDING GEAR HANDLE LOCK L EVER SPRING. (X) 2 L 7 3 4F A22WE 1999022600341 19990226 00341 NM 1999 2 26 GAIA9923 1 19990209 A 2611 DETECTOR BOEING 727 727251 138408H NM CARGO COMPT DIRTY A GAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 EN ROUTE FROM MHR-TOL, THE CARGO SMOKE DETECTION CARGO LIGHT ILLUMINATED. THE AIRCRAFT DECLARED AN EMERGENCY AND DIVERT ED TO SLC. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFICULTIES. FOUND CONDENSATION ON SMOKE DETECTORS IN THE MAIN CAR GO BAY. CLEANED OFF THE CONDENSATION OF THE DETECTORS. OPERATIONAL TEST NORMAL ON GROUND. HEATED AND PRESSURIZATION C HECKED NORMAL AS WELL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999022600342 19990226 00342 EU 1999 2 26 99ZZZX737 1 19990122 A 3260 5316 SWITCH BAG JETSTM JETSTM3201 1500217 EU LANDING GEAR OUT OF ADJUST A FYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 05 242BM 902 AFTER TAKEOFF FROM JANEAU, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO JUNEAU AND LANDED WITHOUT INCIDENT. AI RCRAFT FERRIED JUNEAU TO KETCHIKAN FOR REPAIR, ADJUSTED SQUAT SWITCH, PERFORMED GEAR SWING. OPS CHECK GOOD. 2 L 7 2 4T RT A56EU 1999022600345 19990226 00345 WP 1999 2 26 ASAA9980028 1 19990122 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING MAINTENANCE CHECK THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERI ES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999022600346 19990226 00346 NM 1999 2 26 ASAA9910001 1 19990107 A 5210 6523464 SNUBBER BOEING 737 7372Q8C 138448S NM L2 DOOR INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 ANC - PRIOR TO FLT 22, THE LT AFT ENTRY DOOR HANDLE WAS DIFFICULT TO OPERATE. REPLACED SNUBBER AND LUBRICATED DOOR, DOO R OPERATED NORMALLY. ACFT TT: 51,541 HOURS. ACFT TC: 45,577. (X) 2 L 7 2 4F A16WE 1999022600347 19990226 00347 NM 1999 2 26 ASAA9940002 1 19990105 A 5210 90100722 SNUBBER BOEING 737 7374Q8 NM L1 DOOR INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 PDX - PRIOR TO FLT 471, THE L1 DOOR WAS DIFFICULT TO CLOSE. REPLACED SNUBBER AND LUBRICATED PIVOT POINTS, DOOR OPERATED NORMALLY. ACFT TT: 17,769 HOURS. ACFT TC: 10,554. (X) 2 L 7 2 4F RT A16WE 1999022600349 19990226 00349 NM 1999 2 26 ASAA9910002 1 19990114 A 3350 883200312 RECEIVERS BOEING 737 737290C 138448V NM ROWS 11,16,18 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 11, 16, AND 18 WOULD NOT TEST. REPLACED 2 EACH RECEIVERS AN D BATTERY PACKS, LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR 99ZZZX739. (X) 2 L 7 2 4F A16WE 1999022600350 19990226 00350 NM 1999 2 26 99ZZZX739 1 19990114 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM ROWS 11,16,18 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 11, 16, AND 18 WOULD NOT TEST. REPLACED 2 EACH RECEIVERS AN D BATTERY PACKS, LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL ASAA9910002. 2 L 7 2 4F A16WE 1999022600351 19990226 00351 NM 1999 2 26 ASAA9910003 1 19990118 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHT SYSTEM WOULD NOT TEST PROPERLY. REPLACED 2 BATTERY PACKS AND THE AFT TRANSMITTER BATTERY, LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NR 99ZZZX740. (X) 2 L 7 2 4F A16WE 1999022600352 19990226 00352 NM 1999 2 26 99ZZZX740 1 19990118 A 3350 6104781 BATTERY GRIMES BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHT SYSTEM WOULD NOT TEST PROPERLY. REPLACED 2 BATTERY PACKS AND THE AFT TRANSMITTER BATTERY, LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NR ASAA9910003. 2 L 7 2 4F A16WE 1999022600353 19990226 00353 NM 1999 2 26 ASAA9910004 1 19990120 A 3350 6104781 BATTERY GRIMES BOEING 737 737290C 138448V NM PALLET 5-3 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, EMERGENCY EXIT TRACK LIGHTS AT PALLET 5-3 WERE FOUND INOPERATIVE. REPLACED BATTERY AND THE LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999022600355 19990226 00355 NM 1999 2 26 ASAA9940001 1 19990105 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 SEA - PRIOR TO FLT 468, TWO EACH RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE FIRST CLASS SECTION . CLEANED AND RESECURED TRACK AND THE LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999022600356 19990226 00356 NM 1999 2 26 ASAA9940003 1 19990113 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 PDX - DURING MAINTENANCE CHECK, THE FORWARD TWO AND AFT TWO EMERGENCY EXIT TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNE CTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999022600357 19990226 00357 NM 1999 2 26 ASAA9940004 1 19990113 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROWS 22-25 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 22-25 WERE FOUND INOPERATIVE. RECONNECTED WIRIN G/LIGHTS AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999022600358 19990226 00358 NM 1999 2 26 ASAA9940005 1 19990114 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 SEA - DURING MAINTENANCE CHECK THE FORWARD TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTE D WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999022600359 19990226 00359 NM 1999 2 26 ASAA9940006 1 19990116 A 3350 20131A BATTERY BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE RT AFT CHARGER AND BATTERY, LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NR 99ZZZX741. (X) 2 L 7 2 4F RT A16WE 1999022600360 19990226 00360 NM 1999 2 26 99ZZZX741 1 19990116 A 3350 BPS73 BATTERY CHARGER BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE RT AFT CHARGER AND BATTERY, LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NR ASAA9940006. 2 L 7 2 4F RT A16WE 1999022600364 19990226 00364 WP 1999 2 26 ASAA9980009 1 19990105 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - PRIOR TO DEPARTURE OF FLT 264, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999022600365 19990226 00365 WP 1999 2 26 ASAA9980010 1 19990106 A 3350 014597001 BATTERIES MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 10 FORWARD WERE FOUND INOPERATIVE. REPLACED T HE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999022600366 19990226 00366 WP 1999 2 26 ASAA9980011 1 19990106 A 3350 014597001 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID-CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999022600367 19990226 00367 WP 1999 2 26 ASAA9980012 1 19990106 A 3350 1001191 LIGHT MIDLANDROSS DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 21308 363 53473 SEA - DURING MAINTENANCE CHECK THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. PART TC: 14,132. (X) 2 L 7 2 4F RT A6WE 1999022600368 19990226 00368 WP 1999 2 26 ASAA9980013 1 19990107 A 3350 1001191 LIGHT MIDLANDROSS DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 22691 3327 49103 LAX - AFTER ARRIVAL OF FLT 84, CREW REPORTED THE FORWARD PORTABLE EMERGENCY LIGHT ILLUMINATED IN-FLIGHT. REPLACED THE L IGHT ASSEMBLY AND OPERATED NORMALLY. PART TC: 13,341. (X) 2 L 7 2 4F A6WE 1999022600369 19990226 00369 WP 1999 2 26 ASAA9980014 1 19990108 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999022600370 19990226 00370 WP 1999 2 26 ASAA9980015 1 19990109 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND DIM. REPAIRED WIRING I N FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999022600371 19990226 00371 WP 1999 2 26 ASAA9980016 1 19990112 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUD INOPERATIVE. RECONNECTE D WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999022600372 19990226 00372 WP 1999 2 26 ASAA9980017 1 19990112 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK RED LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999022600373 19990226 00373 WP 1999 2 26 ASAA9980019 1 19990113 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999022600390 19990226 00390 WP 1999 2 26 TWAA9902801 1 19990222 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP ROW 19-20 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 917TW 49366 FOUND THE CABIN OVERHEAD EMERGENCY LIGHTS AT ROW 19 TO 21 INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 7-15-98 MCI. 2 L 7 2 4F A6WE 1999022600391 19990226 00391 WP 1999 2 26 TWAA9902802 1 19990221 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CORROSION ON SEAT TRACK, LT I/B AT STA 200 TO 237. INSTALLED NEW TRACK PER SPM 6-80-01. SPLICED PER SRM 53-05, FIG 4F, PG 10G. 2 L 7 2 4F A6WE 1999022600392 19990226 00392 WP 1999 2 26 TWAA9902803 1 19990220 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND THE ADF LOOP ANTENNA AFT MOUNTING HOLES IN SKIN WITH CRACKS. STOP DRILLED THREE CRACKS AT MOUNT HOLES AND INSTALLED REPAIR PER SRM 53-04, FIG 29. 2 L 7 2 4F A6WE 1999022600393 19990226 00393 WP 1999 2 26 TWAA9902804 1 19990219 A 5711 SPAR DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND LT WING TRAILING EDGE REAR SPAR CENTER UPPER FLAP ATTACH HOLES, I/B AND O/B WITH CRACKS. ACCOMP NDT HIGH FREQ EDDY CURRENT PER SRM 51-00-03, PART 6 CRACK CONTAINMENT. BLENDED AREA PER SRM 57-01, PG 5, FIG 1 SHEET 3. INSTALLED DOUBLERS, FILLERS AND SHIMS PER ARA 16062. 2 L 7 2 4F A6WE 1999022600394 19990226 00394 WP 1999 2 26 TWAA9902805 1 19990219 A 5320 FRAME DOUG DC9 DC931 3022065 WP CABIN WINDOW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 15 MAINT CHECK, FOUND CABIN WINDOW FRAME TIE CRACKED IN UPPER FWD CORNER, STA 680 ON RT SIDE. REPLACED WINDOW FRAME PER DOUGLAS PRINT NR 5912285, WITH (P/N 5912285-505). 2 L 7 2 4F A6WE 1999022600395 19990226 00395 WP 1999 2 26 AT9900135 1 19990120 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 69.5 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK ON UPPER NOSE SKIN RIGHT SIDE AT STA 69.5 AT SECOND FASTENER JUST TO THE RIGHT OF PREVIOUS REPAIR. REMOVED EXISTING FILLER, FASTENERS, ENLARGED EXISTING CUTOUT TO REMOVED CRACK, FABRICA TED, TREATED, PRIMED, AND INSTALLED FILLER WITH WET SEALER IAW DC9 SRM 51-10-4, DOUGLAS DRAWING SR09530239 REVISION A AN D SERVICE BULLETIN 53-262. 2 L 7 2 4F A6WE 1999022600396 19990226 00396 WP 1999 2 26 AT9900136 1 19990201 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 484 & 955 CREASED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CREASE OUT OF LIMITS AT STA 484 RIGHT SIDE L-19-20. ALSO, A COAX CABLE STAND OFF BROKEN AT STA 955 ABOVE L-20R. TRIMMED OUT CREASE, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-30-5, 51-3 0-2, 53-04 FIG 12B, AND RES NR 99293. ALSO, REMOVED, REPLACED AND FABRICATED NEW STAND OFF AT STA 955 (P/N 1A-42054) I AW DC9 SRM 51-10-4, 51-10-2, 51-30-2 AND RES NR 99255. 2 L 7 2 4F A6WE 1999022600397 19990226 00397 WP 1999 2 26 AT9900137 1 19990113 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 361 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT OUT OF LIMITS AT STA 361R L-28R. REMOVED FASTENERS, COLD WORKED DE NT, HFCE INSPECTED DENT WITH NO CRACKS NOTED. FABRICATED DOUBLER, FINGER DOUBLERS, DRILLED, COUNTERSUNK, DEBURRED, TREA TED, PRIMED, AND INSTALLED IAW DC9 SRM 53-04 FIG 38, 51-10-2, AND RES NR 99203. 2 L 7 2 4F A6WE 1999022600398 19990226 00398 WP 1999 2 26 AT9900138 1 19990119 A 5310 STRUCTURE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 816AT 47445 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATIONS WITH CORROSION, DELAMINATION AND ELONGATED HOLES. FIRST , AT THE FORWARD CARGO SIDE WALL STRAPS (4 EACH) AND THRESHOLD DOOR STRAP (AFT SIDE) CORRODED AND ENLONGATED HOLES. SEC OND, AT THE E/E COMPARTMENT AFT BULKHEAD LOWER FRAME L-28L TO L-28R. THIRD, AT THE RIGHT SIDE ELEVATOR GEAR TAB CORRODE D AND DELAMINATED AROUND HINGE BRACKET HOLES. REMOVED, REPLACED, FABRICATED, LOCATED AND DRILLED STRAPS AND ANGLE, DEBU RRED, TREATED, PRIMED, PAINT, INSTALLED ALL PARTS AND NEW ELEVATOR GEAR TAB IAW DC9 SRM 51-21-0, 51-10-2, 51-10-3, 53-21 -0, 51-30-1, 53-01 FIG 1, 51-10-4 AND MM 27-30-4. GEAR TAB (P/N 5910414-502). 2 L 7 2 4F A6WE 1999022600399 19990226 00399 WP 1999 2 26 AT9900139 1 19990212 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOORBEAM AT STA 965 HAS CORROSION AND BLUE WATER STAINS ON LOWER LEG AND AROUND NUT PLATES HOLES LEFT HAND LAVATORY. MECHANICALLY REMOVED CORROSION, FABRICATED TWO DOUBLERS AND INSTALLED I AW DC9 SRM 53-05 FIG 5, 20A AND 65, 53-01 FIG 1, AND RES NR 99288. 2 L 7 2 4F A6WE 1999022600400 19990226 00400 WP 1999 2 26 AT9900140 1 19990112 A 7830 FAIRING DOUG DC9 DC932 3022066 WP NR 2 ENG TRACT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 2 AFT INBOARD UPPER THRUST REVERSER ACTUATOR FAIRING IS CRACKED. R EMOVED THE THRUST REVERSER FAIRING, WELDED AND REINSTALLED IAW DC9 MM 78-00 AND RES NR 99244. 2 L 7 2 4F A6WE 1999022600401 19990226 00401 NM 1999 2 26 K3HA990015 1 19990219 A 3350 0816901 SOCKET BOEING 727 727225 1384077 NM CABIN BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY PATH LIGHT SOCKET WIRE BROKEN. INSTALLED SOCKET, LIGHT LAMP AND CLEAR LENSE. OPS CHECK OK AS PER MM 33-50-01 . LAMP (P/N 3071BPE6PL), LENSE (P/N 07912). 2 L 7 3 4F A3WE 1999022600402 19990226 00402 EA 1999 2 26 JBXA9900069 1 19990221 A 2120 AIR DIST CNDAIR CL600 CL6002B19 EA CABIN SMOKE A JBXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 05 572ML 7224 AFTER DEPARTING BDL, SMOKE TOILET MESSAGE DISPLAYED ON PRIMARY EICAS SCREEN, FOLLOWED IMMEDIATELY BY A CALL FROM THE FLI GHT ATTENDANT REPORTING SMOKE IN CABIN. RETURNED TO BDL WITHOUT INCIDENT. INSPECTED AIRCRAFT APU, AIR CONDITIONING, HY DRAULICS, AS WELL AS ENGINES FOR POSSIBLE SOURCE OF SMOKE, NO DEFECTS NOTED. RAN AIRCRAFT ENGINES, APU AND ECS SYSTEMS WITH NO FAULTS NOTED. INSPECTED AIRCRAFT ELECTRICAL SYSTEMS, RE-LAMPED LAV FASTEN SEATBELT SIGN, AND LAV FLUSH PUSH SWI TCH IAW CL-65 AMM 33-25-00. OPS CHECK GOOD, AIRCRAFT OK FOR RETURN TO SERVICE AT THIS TIME. 2 L 7 2 4F RT A21EA 1999022600403 19990226 00403 EU 1999 2 26 AWXA9900043 1 19990217 A 3251 C24736001 SERVO AIRBUS 320 A320231 3930325 EU NLG STEERING FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 WP 28 628AW 67 EMERGENCY LANDING, NOSE LANDING GEAR NOT CENTERED UPON LANDING. UPON LANDING IN CMH, ACFT LANDED WITH THE NOSE GEAR 90 DEG FROM CENTERLINE AXIS. LEFT AND RIGHT NOSE WHEEL TIRE ASSEMBLIES DAMAGED. REMOVED AND REPLACED STEERING SERVO CONTR OL, REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL TIRE ASSEMBLIES. PERFORMED DETAILED VISUAL INSPECTION OF NOSE LANDIN G GEAR. CHECKED BARREL/DRAG STRUT CONNECTION. ALL INSPECTIONS CHECK GOOD. 2 L 7 2 4F RT A28NM 1999022600404 19990226 00404 NM 1999 2 26 AWXA9900044 1 19990219 A 3397 WIRE BOEING 737 737301 1384611 NM ROW 5, 6 & 7 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 324AW 23261 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROW 5, 6, 7, INOP. REPAIRED BROKEN WIRE, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999022600405 19990226 00405 NM 1999 2 26 AWXA9900048 1 19990202 A 5315 65468101 FLOORBEAM BOEING 737 73733A 1384673 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 FOUND DURING ROUTINE MAINTENANCE CHECK, FLOORBEAM STA 967 LBL 28 TO LBL 50 CORRODED IN SEVERAL AREAS. FABRICATED REPAIR SECTION OF UPPER T CHORD PER SRM 53-00-51 PAGES 207 TO 211. 2 L 7 2 4F RT A16WE 1999022600406 19990226 00406 NM 1999 2 26 AWXA9900049 1 19990202 A 5315 6546809158 FLOORBEAM BOEING 737 73733A 1384673 NM BS 947.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON UPPER FLOORBEAM T CAP STATION 947.5 LBL 9 TO RBL 9. REPAIRED PER S RM 51-10-02, 51-20-01. 2 L 7 2 4F RT A16WE 1999022600407 19990226 00407 NM 1999 2 26 AWXA9900050 1 19990202 A 5315 654681143 FLOORBEAM BOEING 737 73733A 1384673 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON UPPER FLOORBEAM T CAP AT STATION 986.5 LBL 18 TO RBL 18. REPAIRED PER ER 3-53-16-35A. 2 L 7 2 4F RT A16WE 1999022600408 19990226 00408 NM 1999 2 26 CALA9900183 1 19990222 A 5755 SKIN BOEING 727 727224 1384076 NM NR 10 SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND THE LT WING NR 10 SPOILER CORRODED WITH SCREWS PULLING THROUGH SKIN AT TOP CENTER HINGE. THE SPOILER W AS REMOVED AND REPLACED IAW MM 27-62-1. 2 L 7 3 4F A3WE 1999022600409 19990226 00409 NM 1999 2 26 CALA9900184 1 19990222 A 5753 652163571 SKIN BOEING 727 727224 1384076 NM LT TE AFT FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LT TRAILING EDGE O/B AFT FLAP UPPER SURFACE DELAMINATED. THE LT O/B AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-12. 2 L 7 3 4F A3WE 1999022600410 19990226 00410 NM 1999 2 26 CALA9900185 1 19990222 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND STRINGER 26L CORRODED UNDER TRANSITION PANEL AT STA 500A TO 500B. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 1999022600411 19990226 00411 NM 1999 2 26 CALA9900186 1 19990222 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE MIDFLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LT O/B MIDFLAP UPPER TRAILING EDGE SKIN CORRODED AND SEPARATING I/B TO O/B END. INSTALLED NEW TRAILING EDGE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999022600412 19990226 00412 NM 1999 2 26 CALA9900187 1 19990222 A 5400 ACOUSTIC PANEL BOEING 727 727224 1384076 NM NR 2 ENG NACELLE TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND NR 2 ENGINE INLET ACOUSTIC PANEL TORN. THE TORN AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 54 -10-3. 2 L 7 3 4F A3WE 1999022600415 19990226 00415 WP 1999 2 26 9900619903 1 19990218 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 DURING PERIODIC CHECK, FOUND FUSELAGE EXTERIOR SKIN CRACKED AT FASTENERS AT FS 69.5 BETWEEN LONGERONS 14L THRU 17L. REP LACED SKIN PER EA 99-163379. 2 L 7 2 4F A6WE 1999022600416 19990226 00416 WP 1999 2 26 9900629756 1 19990218 A 5312 BULKHEAD DOUBLER DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING PERIODIC CHECK, FOUND AFT PRESSURE BULKHEAD VENTRAL LOWER RIGHT CORNER DOUBLER CRACKED AT LONGERONS 10R THRU 14R. REPAIRED PER EM 5310-01012. 2 L 7 2 4F A6WE 1999022600417 19990226 00417 WP 1999 2 26 9900639985 1 19990218 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERTICAL STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 985US 47479 DURING PERIODIC CHECK, FOUND VERTICAL STABILIZER LEADING EDGE STRUCTURE FORMER CRACKED AT FS 36, 43, 50 AND 148. FABRIC ATED AND INSTALLED DOUBLERS PER EA 99-162413. 2 L 7 2 4F A6WE 1999022600418 19990226 00418 WP 1999 2 26 9900641141 1 19990107 A 5743 LEVER DOUG DC10 DC1040 3023508 WP TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 141US 46750 DURING M-CHECK, FOUND CORROSION UNDER AND AROUND PIVOT BEARING SUPPORT BUSHING ON INBOARD FLAP DRIVE LEVER. REPAIRED PE R EA 11-162743. 2 L 7 3 4F A22WE 1999022600419 19990226 00419 WP 1999 2 26 9900651141 1 19990107 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1738 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 141US 46750 DURING M-CHECK, FOUND CORROSION AT FS 1738 ON LONGERON 50L. REPAIRED PER EA 11-162749. 2 L 7 3 4F A22WE 1999022600420 19990226 00420 EA 1999 2 26 COMA9960077 1 19990222 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933CA 7040 EMERGENCY LIGHT INOPERABLE, MAIN CABIN DOOR. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999022600421 19990226 00421 NM 1999 2 26 UPS99228757 1 19990221 A 5744 652165113 FITTING BOEING 727 72725C 138400H NM NR 4 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE-C, NR 4 FLAP TRACK FORWARD MOUNT FITTING HAS CORROSION IN MOUNT HOLE BORES. NR 4 FLAP TRACK FITTING WAS REPLACED IAW OHM 20-50-01 PG 1 PARA 2 AND TABLE 1 AND M/M 27-51-31 PARA D8, ON NRC 879844. 2 L 7 3 4F A3WE 1999022600422 19990226 00422 NM 1999 2 26 UPS99228758 1 19990208 A 3211 65844055 TRUNNION BOEING 727 72725C 138400H NM LT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE-C, LT MLG FORWARD TRUNNION FITTING CRACKED. REMOVED AND REPLACED LT MLG FORWARD TRUNNION FITTING IAW MM 32-11-51. 2 L 7 3 4F A3WE 1999022600423 19990226 00423 NM 1999 2 26 UPS99228760 1 19990217 A 5711 SPAR CHORD BOEING 727 72725C 138400H NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE-C,CORROSION (C57-581-03.00E-01) ON L/W UPPER REAR SPAR CHORD AT WBL 76, INSIDE FUEL HOSE SHROUD. REPAIR ED IAW ERO 99-5030. 2 L 7 3 4F A3WE 1999022600424 19990226 00424 NM 1999 2 26 UPS99628761 1 19990219 A 5320 SILL BOEING 767 76734AF 1385212 NM PAX DOOR DIRTY A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 304UP 27242 INSPECTION TYPE-N/A, LOUD AIR LEAK FOUND AT ENTRY DOOR. REMOVED DEBRIS FROM SILL/SEAL AREA, OK FOR CONTINUED OPS. 2 L 7 2 4F RT A1NM 1999022600425 19990226 00425 WP 1999 2 26 UPS99828764 1 19990223 A 3230 RETRACT MECH DOUG DC8 DC871F 302199D WP NLG OUT OF ADJUST A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 700UP 45900 INSPECTION TYPE-N/A, THE LANDING GEAR WOULD NOT RETRACT AFTER T/O. RAN THE GEAR HANDLE JAMMED CHECKLIST. THE GEAR RETR ACTED AFTER PUSHING THE GEAR HANDLE LATCH FLIGHT RELEASE BUTTON. FOUND THE NOSE GEAR GROUND SHIFT MECHANISIM WOULDN'T P ULL THE ANTI-RETRACTION LEVER FAR ENOUGH. ADJUSTED NOSE GEAR GROUND SHIFT PER MM 32-23-01, SYS OPS OK WITH A/C ON JACKS GEAR HAND AND ANTI-RETRACTION DEVICE CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999022600426 19990226 00426 NM 1999 2 26 99FDEA00073 1 19990222 A 5320 65442341 CHORD BOEING 727 72725C 138400H NM BS 1048 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 WHILE WORKING NR 515 FOUND CORROSION ON BL 0 CHORD AT BS 1048, RBL 2, WL 200. *S/D* REMOVED AND REPLACED BL 0 CHORD BS 950 TO 1060, WL 200 IAW FEDEX SRM 51-30-2, 53-10-1. 2 L 7 3 4F A3WE 1999022600427 19990226 00427 NM 1999 2 26 99FDEA00074 1 19990218 A 3230 LOCK ACTUATOR DOUG MD11 MD11F 3023600 NM RT MLG INOP A FDEA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SO 25 582FE 48420 RT MAIN GEAR DID NOT RETRACT. JACKED A/C PER MM 07-11-00-2 AND SWING LANDING GEAR PER MM 32-31-00-5. REMOVED AND REPLA CED RT MAIN LANDING GEAR DOWNLOCK CYLINDER ASSY PER MM 32-33-02-4. REMOVED AND REPLACED RT RESTRICTOR ASSY PER MM 32-33 -01-4. 2 L 7 3 4F RT A22WE 1999022600428 19990226 00428 NM 1999 2 26 99UAL900059 1 19990124 A 2170 HUMIDIFIER LUCAS M01AB0101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT DIRTY A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 178UA 518 24385 SMOKE IN COCKPIT SUDDENLY OCCURRED DURING CRUISE FLIGHT. SELECTED HUMIDIFIER OFF AND SMOKE DISSIPATED. *S/D* HEAVY CA LCIUM DEPOSITS IN UNIT. SUSPECT SMOKE WAS ACTUALLY CALCIUM IN DUCTS. SHOP CLEANED AND CHECKED UNIT SERVICEABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 1999022600429 19990226 00429 NM 1999 2 26 99UAL900074 1 19990202 A 3210 65242799 SIDE BRACE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG FRACTURED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 7272U 21419 UPON EXITING THE RUNWAY AFTER LANDING, FLIGHT CREW NOTED AN UNSAFE GEAR INDICATION LIGHT. AIRCRAFT WAS STOPPED ON TAXIW AY. RIGHT MAIN GEAR SIDE BRACE BROKE ON LANDING. *S/D* FOUND RIGHT HAND MLG SIDE BRACE CLEVIS ASSEMBLY FRACTURED AND SEPARATED FROM SIDE BRACE. REPLACED RIGHT HAND UPPER AND LOWER SIDE BRACE ASSEMBLIES. ALSO, REPLACED RIGHT HAND MLG DR AG STRUT DUE TO SCRATCH. ACCOMPLISHED HIGH DRAG/SIDE LOAD CHECK OF AIRCRAFT. CHECKED GEAR ACTUATOR AND SURROUNDING ARE A FOR DAMAGE. IN ADDITION, REPLACED LEFT HAND LOWER SIDE BRACE FOR ENGINEERING ANALYSIS. ACCOMPLISHED RETRACT TEST OF LEFT AND RIGHT HAND MAIN LANDING GEARS. 2 L 7 3 4F 4 F A3WE E2EA 1999022600430 19990226 00430 NE 1999 2 26 99UAL900097 2 19990213 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT BIRD STRIKE A UALA A UNSCHED LANDING C F.O.D. NR NOT REPORTED 1 WP 29 553UA 25277 726550 RETURNED TO FIELD DUE TO BIRD STRIKE. *S/D* BIRD STRIKE CAUSED RIGHT ENGINE DAMAGE. REPLACED FAN BLADE SET AND NOSE COW L. BORESCOPED 6TH STAGE BLADES, CHECKED OK. ACCOMPLISHED VIBRATION SURVEY, CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1999022600431 19990226 00431 NM 1999 2 26 99UAL900098 1 19990212 A 2410 LINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 CSD FAILED A UALA A UNSCHED LANDING K H J FLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 29 318UA 23950 THE NUMBER TWO ENGINE GENERATOR FAILED. *S/D* CSD SERVICING LINE WAS FOUND CRACKED. NR 2 ENGINE GENERATOR FELL OFF LI NE DUE TO LOW CSD OIL LEVEL. REPLACED CSD SERVICING LINE, CSD, GENERATOR AND OIL COOLER, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999022600432 19990226 00432 NM 1999 2 26 99UAL900099 1 19990213 A 2782 755299 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE SLAT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 588UA 26717 RETURNED TO ORD DUE TO A LEADING EDGE SLAT PROBLEM. *S/D* POSITION NR 15 LEADING EDGE SLAT ACTUATOR FAILED WHICH CAUSE D SYSTEM BINDING AND SHUTDOWN OF THE SLAT SYSTEM AT THE POWER DRIVE UNIT. ALSO, THE OVERLOAD INDICATOR POPPED. REPLACE D THE NR 15 SLAT ACTUATOR, RESET OVERLOAD INDICATOR, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1999022600433 19990226 00433 1999 2 26 99UAL900100 4 19990212 A 2210 SC470037 YAW DAMPER AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE NR 1 MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 822UA 948 RECEIVED UNCOMMANDED YAW INPUT WHICH RESULTED IN AUTOPILOT DISENGAGEMENT. *S/D* YAW DAMPER ACTUATOR HAS BEEN ISOLATED AS THE PROBLEM. THIS UNIT HAS NOT BEEN REPLACED ON THE AIRCRAFT AS OF 2/21/99. BUT THERE IS NO UNCOMMANDED YAW INPUT WIT H THE YAW DAMPER NR 1 DISCONNECTED AND THE HYD LINES CAPPED AND STOWED. THIS UNIT IS A KNOWN PROBLEM UNIT, ESPECIALLY O N THE NR 1 SIDE (LEFT). THE LEFT SYSTEM SEES A HIGHER CYCLE RATE FROM THE HYD SYSTEM AS CONFIRMED ON AIRBUS MESSAGE 953 .0811/99. 2 L 7 2 4F 4 F RT A28NM E40NE 1999022600434 19990226 00434 EU 1999 2 26 99UAL900101 1 19990214 A 3350 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 450UA 857 CABIN EMERGENCY LIGHT CHECK FAILED. FAULTED EPSU COMM FWD L AND EPSU COMM AFT L. *S/D* DURING THE OPS CHECK OF EMERGENC Y LIGHTS THROUGH THE PROGRAMMING AND TEST PANEL (PTP), NO SMOKING SWITCH 190RH WAS INADVERTENTLY SET TO THE ON POSITION. IT WAS SUPPOSED TO BE IN THE OFF POSITION PER AMM TASK 33-51-00-710-001. 2 L 7 2 4F 4 F RT A28NM E40NE 1999022600435 19990226 00435 NM 1999 2 26 99UAL900102 1 19990213 A 2820 VALVE HTE900034 AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE FUEL SYST FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 803UA 748 RIGHT SIDE FUEL BURNING MUCH FASTER THAN LEFT SIDE. IN 2:30 FLT TIME, FUEL IMBALANCE BECAME GREATER THAN 300 LBS AND CA USED A FUEL IMBALANCE ECAM WARNING. AT THAT TIME, THE XFEED VALVE INDICATED CLOSED. CROSSFEED VALVE FAILED OPEN. ECAM AND PB SWITCH BOTH SHOWED VALVE CLOSED. REMOVED AND REPLACED DEFUEL/CROSSFEED VALVE ASSEMBLY PER AMM 28-25-43. 2 L 7 2 4F 4 F RT A28NM E40NE 1999022600436 19990226 00436 NM 1999 2 26 99UAL900103 1 19990212 A 2752 240863 DRIVE MOTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAP LEAKING A UALA O OTHER J K WARNING INDICATION FLUID LOSS DE DESCENT 1 WP 29 7266U 21413 APPROXIMATELY 20 MINUTES BEFORE LANDING AT DSM HAD A COMPLETE LOSS OF SYSTEM A HYDRAULIC FLUID. PUMPS RAN WITH LOW PR ESSURE LIGHT ON FOR APPROXIMATELY 5 MINUTES. *S/D* FOUND OUTBOARD FLAP DRIVE MOTOR LEAKING. REPLACED MOTOR SYSTEM OPE RATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999022600437 19990226 00437 NM 1999 2 26 99UAL900104 1 19990213 A 5242 DOOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E & E COMPT NOT LATCHED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7265U 21412 UNABLE TO PRESSURIZE AIRPLANE ON TAKEOFF FROM MSN. RETURNED TO MSN. *S/D* E AND E DOOR FOUND OPEN ON ARRIVAL. WARNI NG LIGHT SYSTEM FOR E AND E DOOR INOPERATIVE DUE TO BROKEN WIRE AT SWITCH. WIRE REPAIRED, DOOR SECURELY LATCHED AND AIR CRAFT DISPATCHED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999022600438 19990226 00438 NM 1999 2 26 99UAL900105 1 19990215 A 3350 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR MALFUNCTIONED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 195UA 26892 EMERGENCY LIGHTS ON WHEN SELECTED TO OFF. *S/D* RESET EMERGENCY LIGHT SWITCH AT DOOR 1L, OVERHEAD SWITCH. NOW CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 1999022600439 19990226 00439 NM 1999 2 26 99UAL900106 1 19990215 A 3350 582214 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7284U 21562 EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 26 TO 28. *S/D* REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1999022600440 19990226 00440 NM 1999 2 26 99UAL900109 1 19990216 A 3097 BMS1351 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ENGINE ANTI ICE DAMAGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7450U 21904 ENGINE ANTI-ICE OVERHEAT LIGHT ON AT ALL TIMES. LIGHT STAYS ON FOR ANY ENGINE SELECTED. TEMPERATURE INDICATIONS ARE NORM AL. *S/D* MAINTENANCE REPAIRED BURNED AND DAMAGED WIRING IN AFT STAIRWELL, OPERATIONALLY CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999022600441 19990226 00441 1999 2 26 99UAL900113 4 19990215 A 2565 D31038201 TUBE AIR CRUISERS D31096201 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 1189 31296 0447 24890 SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALU ATION AND REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1999022600442 19990226 00442 NM 1999 2 26 99UAL900114 1 19990218 A 3350 321454 POWER SUPPLY 321430 AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 812UA 850 EMERGENCY LIGHTS TEST SHOWS EPSU COMM FWD L AND EPSU COMM EMER R, L. COMMUNICATION FAULT OCCURED BETWEEN EPSU'S (FWD L - 10WL, EMER R - 12WL AND EMER L - 11WL) AND CIDS. ALL THESE EPSU'S AND THEIR BATTERIES WERE REPLACED, AND SUBSEQUENT E MERGENCY LIGHT TEST WAS FOUND NORMAL. EPSU S/N REPLACED ARE AS FOLLOWS:2434, 6019, AND 6315. 2 L 7 2 4F 4 F RT A28NM E40NE 1999022600443 19990226 00443 NM 1999 2 26 99UAL900115 1 19990205 A 2421 4209990 WIRE HARNESS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 797UA 26924 DURING C-CHECK, INSPECTION REPORTED IDG (INTERGRATED DRIVE GENERATOR) WIRE BUNDLE DAMAGE ON BOTH ENGINES. WIRE BUNDLE I D IS W0623 (P/N 420990 / 50U629). ALSO REF AMM 73-21-73. *S/D* ANALYSIS REVEALED CONTRIBUTING DAMAGE WAS RESULT OF VI BRATION AND ENGINE BLEED AIR HEAT IN COMBINATION WITH ROUTING OF THE WIRE BUNDLE. BOEING AND PRATT AND WHITNEY WERE NO TIFIED AND THEY ARE LOOKING AT A PERMANENT FIX FOR THE PROBLEM. THE DAMAGED WIRE BUNDLES WERE REPAIRED USING STANDARD R EPAIR PROCEDURES. A FLEET INSPECTION IS UNDERWAY TO DETERMINE THE EXTENT OF THE PROBLEM AND TO REPAIR AS NECESSARY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999022600444 19990226 00444 WP 1999 2 26 ABXA9900124 1 19990127 A 5320 3755842 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1260 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D853-24928 AND DC 8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999022600445 19990226 00445 WP 1999 2 26 ABXA9900125 1 19990126 A 5320 9755584507 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1080 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT CUSP LOWER ATTACH FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999022600446 19990226 00446 WP 1999 2 26 ABXA9900126 1 19990127 A 5320 27558442 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 BATHTUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D AND ABX REA D853-2492 7-1MR. 2 L 7 4 4F 4A25 1999022600447 19990226 00447 WP 1999 2 26 ABXA9900127 1 19990122 A 5720 5769854 FORMER DOUG DOUG DC8 DC863 302198A WP WS 6.225 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LEFT WING INBOARD FORMER CRACKED ABOVE DUCT AT STATION XOLD 6.225. REPAIRED DAMAGE IAW DC8 SRM. 2 L 7 4 4F 4A25 1999022600448 19990226 00448 WP 1999 2 26 ABXA9900128 1 19990123 A 5312 564660816 BULKHEAD DOUG DOUG DC8 DC863 302198A WP BS 1540 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 CRACKED INTERCOSTAL ON AFT BULKHEAD, STATION 1540 RIGHT. REPAIRED IAW DC8 SRM AND DWG 5646608. 2 L 7 4 4F 4A25 1999022600449 19990226 00449 WP 1999 2 26 MWEA99071 1 19990218 A 5210 9955759501 BEAM DOUG DC9 DC915 3022036 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 MKE - FOUND CRACK ON FORWARD PASSENGER DOOR DOUBLER ON TOP SIDE OF NR 1 BEAM. MTC FABRICATED AND INSTALLED DOUBLER REPA IR. (X) 2 L 7 2 4F A6WE 1999022600450 19990226 00450 NE 1999 2 26 MWEA99072 2 19990219 A 7321 76960615 FUEL CONTROL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE INOPERATIVE A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 810ME F5996 48072 STL - FLT 302 - DURING CRUISE FLIGHT, THE RIGHT ENGINE PARAMETERS EPR N1 N2 WERE FLUCTUATING AND AIRCRAFT DIVERTED TO ST L. MTC REMOVED AND REPLACED RIGHT ENGINE FUEL CONTROL. (X) 2 L 7 2 4F 4 F A6WE E9NE 1999022600451 19990226 00451 NM 1999 2 26 MWEA99073 1 19990220 A 5330 5911428 SKIN DOUG MD88 MD88 3023688 NM BS 1362 NICKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 MKE - FOUND NICK IN SKIN AT STA 1362 ON LEFT FUSELAGE AT LONGERON 21. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. ACF T TT: 35,132. ACFT TC: 12,792. (X) 2 L 7 2 4F RT A6WE 1999022600452 19990226 00452 WP 1999 2 26 MWEA99074 1 19990221 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 202ME 687 47672 MKE - THE RIGHT NACELLE EMERGENCY BATTERY PACK INOPERABLE. MTC REMOVED AND REPLACED EMERGENCY BATTERY PACK. (X) 2 L 7 2 4F A6WE 1999022600453 19990226 00453 NM 1999 2 26 P5CA9900191 1 19990215 A 5314 KEEL BEAM BOEING 747 747249F 1384849 NM BS 1100-1300 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 LEVEL 1 CORROSION FOUND ON KEEL BEAM AFT END LEFT AND RIGHT SIDE BS 1100 TO 1300. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-01 AND 53-10-02. 2 L 7 4 4F A20WE 1999022600454 19990226 00454 NM 1999 2 26 P5CA9900192 1 19990219 A 5320 ANGLE BOEING 747 747249F 1384849 NM BS 1726L CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 AFT PIT STAT 1726 BL 30L ANGLE FOUND CRACKED JUST BELOW TRACK. REMOVED AND FABRICATED NEW ANGLE AND INSTALLED PER SRM 5 1-10-01, 51-10-03 AND 51-30-02. 2 L 7 4 4F A20WE 1999022600455 19990226 00455 NM 1999 2 26 TSAA9951053 1 19990119 A 5320 BRACKET BOEING 737 7372Q9 138448M NM BS 500 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CRACK NOTED ON Z-CHANNEL AND ATTACH BRACKET AT BS 500A STR 25L IN FORWARD CARGO PIT. REMOVED AND REPLACED ATTACHING BRA CKET PER SRM 51-10-1. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600456 19990226 00456 NM 1999 2 26 TSAA9953052 1 19990119 A 5320 BRACKET BOEING 737 7372Q9 138448M NM BS 380 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CRACK NOTED AT BS 380 STR 25L AT Z-CHANNEL IN FORWARD CARGO PIT. REPLACED BRACKET PER SRM 53-10-10. TAT: 47,785.0 HOU RS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600457 19990226 00457 NM 1999 2 26 TSAA9957051 1 19990119 A 3230 LINK BOEING 737 7372Q9 138448M NM LT MLG CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 LEFT HAND LANDING GEAR BEAM INBOARD ATTACH LINK HAS CORROSION; ALSO, HARDWARE HAS CORROSION AND DEEP PITTING. REPLACED LEFT HAND LINK ASSY IAW 57-15-0 AND SB 737-53-1038, AND REPLACED ALL HARDWARE. (X) 2 L 7 2 4F A16WE 1999022600458 19990226 00458 NM 1999 2 26 TSAA9951050 1 19990119 A 5531 SPAR BOEING 737 7372Q9 138448M NM VERT STABILIZER CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 POSSIBLE REAR SPAR CORROSION AT APPROXIMATELY RS 136.00 VERTICAL STABILIZER RIGHT HAND SIDE. REPAIRED PER ECO 2509R5 PA RT 2. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600459 19990226 00459 NM 1999 2 26 TSAA9951049 1 19990119 A 5531 SPAR BOEING 737 7372Q9 138448M NM VERT STABILIZER CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 POSSIBLE REAR SPAR CORROSION AT APPROXIMATELY RS 156.00 VERTICAL STABILIZER RIGHT HAND SIDE. REPAIRED PER ECO 2509R5 PA RT 2. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600460 19990226 00460 NM 1999 2 26 TSAA9951048 1 19990119 A 5522 SKIN BOEING 737 7372Q9 138448M NM LT ELEV TAB CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 LOWER LEFT HAND ELEVATOR TRIM TAB CRACKED AT HINGE CUT-OUT AREA ELEVATOR STA 39.02. REPAIRED PER SRM 51-40-7. TAT: 47 ,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600461 19990226 00461 NM 1999 2 26 TSAA9953047 1 19990119 A 5315 FLOORBEAM BOEING 737 7372Q9 138448M NM BS 500 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 FLOORBEAM IN FORWARD CARGO PIT CRACKED A BS 500 STR 26L. REPLACED SPLICED CRACKED SECTION OF CARGO FLOORBEAM PER SRM 53 -10-2. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600462 19990226 00462 NM 1999 2 26 TSAA9951046 1 19990119 A 5311 FRAME BOEING 737 7372Q9 138448M NM BS 480 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CRACK NOTED ON FRAME AT BS 480 STR 20L IN FORWARD CARGO PIT. SPLICED FRAME FROM STR 20L TO STR 25L ON STA 480 PER SRM 51-40-3. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600463 19990226 00463 NM 1999 2 26 TSAA9951045 1 19990119 A 5311 FRAME BOEING 737 7372Q9 138448M NM BS 480 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CRACK NOTED AT BS 480 STR 22L ON FRAME IN FORWARD CARGO PIT. SPLICED FRAME FROM STR 20L TO STR 25L ON STA 480 PER SRM 5 1-40-3. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600464 19990226 00464 NM 1999 2 26 TSAA9951044 1 19990119 A 5320 CHANNEL BOEING 737 7372Q9 138448M NM BS 440 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CRACK NOTED AT BS 440 STR 25L AT Z-CHANNEL IN FORWARD CARGO PIT. REMOVED AND REPLACED ATTACHING BRACKET PER SRM 51-10-1 . TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600465 19990226 00465 NM 1999 2 26 TSAA9951043 1 19990119 A 5311 FRAME BOEING 737 7372Q9 138448M NM BS 400 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CRACK NOTED IN FORWARD CARGO PIT ON FRAME BS 400 STR 25L. REPAIRED CRACK PER SRM 51-40-3. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600466 19990226 00466 NM 1999 2 26 TSAA9957042 1 19990119 A 5711 SPAR BOEING 737 7372Q9 138448M NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 LEFT WING FRONT SPAR LOWER CHORD AT NR 2 SLAT ACTUATOR HAS EXFOLIATION CORROSION. CLEANED AND TREATED PER SRM 51-10-6. REPAIRED PER ECO 2135R2. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600467 19990226 00467 NM 1999 2 26 TSAA9953041 1 19990119 A 5313 STRINGER BOEING 737 7372Q9 138448M NM BS 939 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 BULGE AT BS 939 STR 27L, POSSIBLE CORROSION UNDER SKIN. REMOVED, CLEANED, AND TREATED PER SRM 51-10-6. INSTALLED FUSEL AGE STRINGER REPAIR PER SRM 53-10-3 PAGE 10. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600468 19990226 00468 NM 1999 2 26 TSAA9953040 1 19990119 A 5320 RETAINER BOEING 737 7372Q9 138448M NM BS 312-328 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 FLOORBOARD RETAINER DAMAGE AT STA 312 - STA 328. REPAIRED PER ECO 2942. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600469 19990226 00469 NM 1999 2 26 TSAA9953039 1 19990119 A 5315 FLOORBEAM BOEING 737 7372Q9 138448M NM BS 312 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 UPON FLOORBOARDS REMOVAL, SCATTERED CORROSION SPOTTED ALONG UPPER SECTION, MAIN DECK BS 312 FLOORBEAM AS EVIDENT. CUT O UT CORRODED FLOORBEAM AND REPAIRED PER SRM 53-10-9. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600470 19990226 00470 NM 1999 2 26 TSAA9953038 1 19990119 A 5315 FLOORBEAM BOEING 737 7372Q9 138448M NM BS 294 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 UPON FLOORBOARDS REMOVAL, SCATTERED CORROSION SPOTTED ALONG UPPER SECTION, MAIN DECK BS 294.5 FLOORBEAM AS EVIDENT. REP AIRED PER SRM 53-10-9. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600471 19990226 00471 NM 1999 2 26 P2EA99046 1 19990107 A 5311 FRAME BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT BS 727 CHORD CRACKED AT STR 18A. DEFECT SIZE: LENGTH - 2.125 INCHES. REPLACED RIGHT BS 727 CHORD FITTING BETWEEN STR 18R TO STR 24R PER SB 737-53-1088, SEC III, FIG 2 AND 3, DRAWING NR 65C35722, DATED 12-14-89. SEE COOPESA W.O. M1-0003-1-128, VAM 100 NR 479 FOR TECHNICAL INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600472 19990226 00472 NM 1999 2 26 P2EA99045 1 19990109 A 5712 RIB BOEING 737 737222 1384473 NM WS 735 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIB CRACKED IN LEFT FUEL TANK BETWEEN STIFFENERS 2 AND 3 AT STA 735.5. DEFECT SIZE: LENGTH 2.0 IN CHES. REPAIRED RIB LOWER CHORD AT WBL 135.5 AND STR 2 AND STR 3 PER SB 737-57-1166, SEC III, PART III, FIG 3 DATED APRI L 13, 1989. SEE COOPESA W.O. M1-0003-5-109, VAM 100 NR 645 FOR TECHNICAL INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600473 19990226 00473 NM 1999 2 26 P2EA99044 1 19990109 A 5712 RIB BOEING 737 737222 1384473 NM WS 121 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT WING, INBOARD MID-FLAP CENTER TRACK RIB CRACKED AT WBL 121. DEFECT SIZE: LENGTH 4.5 INCHES. REPLACED RIB AT WBL 121 RIGHT WING PER 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-003-6-43, VAM 100 NR 627. (X) 2 L 7 2 4F A16WE 1999022600474 19990226 00474 NM 1999 2 26 P2EA99043 1 19990105 A 5712 RIB BOEING 737 737222 1384473 NM WS 479 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT WING, RIB CRACKED AT FRONT SPAR CAVITY AT FSS 479 (SLAT STA 231.84). DEFECT SIZE: LENGTH 0 .0250 INCH. SEE COOPESA W.O. M1-0003-6-3, VAM 100 NR 148. (X) 2 L 7 2 4F A16WE 1999022600475 19990226 00475 NM 1999 2 26 P2EA99042 1 19990107 A 5311 FRAME BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. BS 727 FUSELAGE OUTBOARD CHORD OF FRAME CRACKED AT STR 18L. DEFECT SIZE: LENGTH: 2.375 INCHES. R EPLACED FUSELAGE BS 727 LT CHORD BETWEEN STR 18L TO STR 24L PER SB 737-53-1088, SECTION III, FIG 2 AND FIG 3, AND DRAWIN G NR 65C33722 DATE 12-14-89. SEE COOPESA W.O. M1-0003-1-29, VAM 100 NR 480. (X) 2 L 7 2 4F A16WE 1999022600476 19990226 00476 NM 1999 2 26 P2EA99041 1 19990108 A 5730 SKIN BOEING 737 737222 1384473 NM RT WING DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT WING LOWER SURACE DENTED AT WBL 260 BETWEEN STIFFENER 6 AND STIFFENER 8. DEFECT SIZE: LENGT H 4.0 INCHES WIDTH 3.0 INCHES DEPTH 0.140 INCH. DENT FOUND STRUCTURALLY SATISFACTORY PER BOEING FAX COO-SJO-99-0043RR D ATED JAN 18, 1998. DOCUMENTED ON FAA FORM 8100-3. APPROVED AND SUBMITTED BY FAA DER M.A. LEHNERT DESIGNATION NM-1715 D ATED JAN 21, 1999. SEE COOPESA W.O. M1-0003-6-42, VAM 100 NR 722 FOR TECHNICAL INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600477 19990226 00477 NM 1999 2 26 P2EA99040 1 19990105 A 5712 RIB BOEING 737 737222 1384473 NM WS 595 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT WING, FRONT SPAR RIB CRACKED AT FSS 595 (SLAT STA 387) DEFECT SIZE: LENGTH 0.0375 INCH. REP LACED RIB PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-6-6, VAM 100 NR 151 FOR TECHNICAL AND PART FABRICATION INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600478 19990226 00478 NM 1999 2 26 P2EA99039 1 19990108 A 5755 654645232 SKIN BOEING 737 737247 138448D NM NR 5 SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP MA334SP2 19607 SJO - Q-CHECK ITEM. NR 5 SPOILER DELAMINATED. DEFECT SIZE: LENGTH 4.0 INCHES WIDTH 3.0 INCHES. REPAIRED NR 5 SPOILER PER SRM 57-50-5, FIG 2, SHEET 9. SEE COOPESA W.O. M1-0005-6-21, VAM 100 NR 189 FOR TECHNICAL INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600479 19990226 00479 NM 1999 2 26 P2EA99038 1 19990111 A 5330 SKIN BOEING 737 737247 138448D NM BS 480-495 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM. SKIN CRACKED AT FORWARD CARGO DOORWAY AFT LOWER CORNER. DEFECT SIZE: 0.500 INCH. REPAIRED FORWAR D CARGO DOOR CUT-OUT SKIN BETWEEN BS 480 AND BS 497 FROM STR 22R TO STR 26R PER COOPESSA B.O. COO-SJO-3-53-008-99 DATED 1-19-99 AND BOEING FAX COO-SJO-99-0041RR DATED DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER C.L. JE NSEN DESIGNATION NM-2605 DATED 1-26-99. SEE COOPESA W.O. M1-0005-1-94, VAN 100 NR 326 FOR TECHNICAL INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600480 19990226 00480 NM 1999 2 26 P2EA99029 1 19990126 A 2520 PSU BOEING 737 737244 138448U NM ROW 18-19 MALFUNCTIONED A P2EA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 05 620PC 19708 FLT 404 - ATL - DURING LANDING, SEVERAL PASSENGERS NOTED SPARKS EMITTING FROM PASSENGER SERVICE UNIT AT ROW 18-19 DEF (R T). 2 L 7 2 4F A16WE 1999022600481 19990226 00481 1999 2 26 99ZZZX743 4 19990131 A 3416 6229210003 ALTIMETER BEECH 1900 1900D 1154162 CE COCKPIT STUCK A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 846CA 10574 X3843 UE49 CAPTAIN'S ALTIMETER STUCK AT 16,000 FEET. UNIT STARTED OPERATING SHORTLY AFTERWARD. REPLACED ALTIMETER. 2 L 7 2 4T RT A24CE 1999022600482 19990226 00482 WP 1999 2 26 ORJA9946 1 19990204 A 3350 6011779 BATTERY DOUG DC9 DC983 3022083 WP ROWS 12,14,15,16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 ORD - FLOOR EMERGENCY EVACUATION LIGHT ON ROWS 12, 14, 15, 16. RECYCLED, SWITCH, DE-POWERED AFT, NO HELP. REPLACED BAT TERY POWER SUPPLY AT LEFT O/W EMERGENCY EXIT. USED SPARE FROM TAIL CONE AREA. (X) 2 L 7 2 4F RT A6WE 1999022600483 19990226 00483 WP 1999 2 26 ORJA9945 1 19990204 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 8-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 SJC - AISLE ESCAPE PATH LIGHTING INOPERATIVE ROWS 8, 9, 10, AND 11. REMOVED AND REPLACED BATTERY PACK AT RT FORWARD O/W EXIT DOOR AND OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999022600484 19990226 00484 1999 2 26 ORJA9944 4 19990120 A 2565 D29982107 SLIDE DOUG DC9 DC987 3022087 WP PASSENGER DOOR FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT PHX, R-1 DOOR EMERGENCY SLIDE FAILS. SLIDE LIGHT BATTERY OK PER MM 25-62-05. REPLACED EMERGENCY SLIDE ASSY WITH SER VICEABLE SLIDE ASSY. (X) 2 L 7 2 4F RT A6WE 1999022600485 19990226 00485 WP 1999 2 26 ORJA9943 1 19990202 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 LAS - EMERGENCY EXIT ROW LIGHTS 9-12 AND ROW 20 CAME ON IN-FLIGHT. COULD NOT EXTINGUISH. REPLACED EMERGENCY LIGHTS PAC K. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1999022600486 19990226 00486 WP 1999 2 26 ORJA9940 1 19990201 A 3397 00105606003 WIRE DOUG DC9 DC983 3022083 WP ROWS 8-9 DISCONNECTED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 879RA 53185 SJC - EMERGENCY EXIT LIGHT OUT AT ROWS 8-9. RECONNECTED WIRING. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999022600488 19990226 00488 WP 1999 2 26 ORJA9938 1 19990204 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 20 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 RNO - ROWS AND FORWARD LOWER EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT SEATS 20A C. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999022600489 19990226 00489 WP 1999 2 26 ORJA9937 1 19990131 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROW 12 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 SJC - BROKEN WIRE TO EMERGENCY LIGHTS AT SEAT 12F. REPAIRED BROKEN WIRE AT SEAT 12F. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999022600490 19990226 00490 WP 1999 2 26 ORJA9936 1 19990129 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROW 12 DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 755RA 49727 SJC - FOUND BARE WIRE FOR EMERGENCY LIGHTS. REPAIRED AND SECURED WIRES AT ROW 12 DEF. (X) 2 L 7 2 4F RT A6WE 1999022600491 19990226 00491 WP 1999 2 26 ORJA9934 1 19990201 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 RNO - EMERGENCY LIGHTING RT FORWARD BATTERY CHARGER INOPERATIVE. REPLACED EMERGENCY BATTERY CHARGER RT FORWARD. OPS CH ECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1999022600492 19990226 00492 WP 1999 2 26 ORJA9933 1 19990130 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 12-16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - EMERGENCY LIGHTS ROWS 12-16 OUT. REMOVED AND REPLACED BATTERY PACK PER MM. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1999022600493 19990226 00493 WP 1999 2 26 ORJA9930 1 19990115 A 3350 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 15-18 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT PHOENIX, ROWS 15 THROUGH 18 EMERGENCY SEAT LIGHT INOPERABLE. TROUBLESHOT SYSTEM, FOUND LOW VOLTAGE ON BATTERY PACK A ND CHARGED SYSTEM USING A/C POWER PER MM 33-53-00. SYSTEM OPERATIONS CHECK GOOD PER MM 33-53-00. (X) 2 L 7 2 4F RT A6WE 1999022600494 19990226 00494 WP 1999 2 26 ORJA9929 1 19990115 A 3350 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 1-9 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT PHOENIX ON ROWS 1 THROUGH 9, EMERGENCY SEAT LIGHTING IS INOPERABLE. TROUBLESHOT SYSTEM, FOUND LOW VOLTAGE ON EMERGEN CY BATTERY PACK. CHARGED SYSTEM PER MM 33-53-00. OPS CHECKS GOOD PER MM 33-53-00. (X) 2 L 7 2 4F RT A6WE 1999022600495 19990226 00495 WP 1999 2 26 ORJA9928 1 19990115 A 3350 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT PHOENIX, R-1 DOOR EMERGENCY EXIT IDENTIFIER INOPERABLE. TROUBLESHOT SYSTEM, FOUND LOW VOLTAGE ON EMERGENCY BATTERY P ACK. CHARGED SYSTEM PER MM 33-53-00. OPS CHECKS GOOD PER MM 33-53-00. (X) 2 L 7 2 4F RT A6WE 1999022600496 19990226 00496 WP 1999 2 26 ORJA9925 1 19990131 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 12-16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 RNO - EMERGENCY LIGHTS INOPERABLE ROWS 12 THROUGH 16 EXIT SIGN AT EMERGENCY EXIT FORWARD LEFT HAND SIDE. REMOVED AND RE PLACED BATTERY POWER PACK BY LEFT FORWARD EMERGENCY WING. OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1999022600497 19990226 00497 NM 1999 2 26 TSAA9957037 1 19990119 A 3230 LINK BOEING 737 7372Q9 138448M NM RT MLG CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 RIGHT HAND LANDING GEAR BEAM INBOARD ATTACH LINK HAS CORROSION; ALSO, HARDWARE HAS CORROSION AND DEEP PITTING. REPLACED RT LINK ASSY IAW MM 57-15-0 AND SB 737-53-1038, AND REPLACED ALL HARDWARE. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600498 19990226 00498 NM 1999 2 26 TSAA9951036 1 19990119 A 5532 SKIN BOEING 737 7372Q9 138448M NM VERT STABILIZER CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 EXFOLIATION CORROSION NOTED ON VERTICAL FIN AT FS 60.0 LEFT HAND SIDE. REPAIRED PER ECO 2509 PART 2. TAT: 47,785.0 HO URS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600499 19990226 00499 NM 1999 2 26 TSAA9951035 1 19990119 A 5542 PANEL BOEING 737 7372Q9 138448M NM RUDDER CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CORROSION ON RUDDER LEADING EDGE COVER PANEL, RUDDER STA 201.91. REPLACED EXISTING PANEL PER ECO 2938. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600500 19990226 00500 NM 1999 2 26 TSAA9951034 1 19990119 A 5542 PANEL BOEING 737 7372Q9 138448M NM RUDDER CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 CORROSION ON RUDDER LEADING EDGE COVER PANEL, RUDDER STA 92.92. REPLACED EXISTING PANEL PER ECO 2938. TAT: 47,785.0 H OURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600501 19990226 00501 NM 1999 2 26 TSAA9951033 1 19990119 A 5311 FRAME BOEING 737 7372Q9 138448M NM BS 420 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 FRAME CRACKED AT BS 420 ABOVE STR 25L. REPAIRED FRAME AT BS 430 IAW SRM 51-40-3. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600502 19990226 00502 NM 1999 2 26 TSAA9953029 1 19990119 A 5320 PRESSURE WEB BOEING 737 7372Q9 138448M NM NLG WW CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 NOSE LANDING GEAR WHEELWELL RIGHT HAND FORWARD PRESSURE PANEL CUT-OUT HAS 2.5 INCH CRACK AT LOWER EDGE BETWEEN RIVETS. R EPAIRED NOSE LANDING GEAR WHEELWELL RIGHT HAND FORWARD PRESSURE PANEL CUT-OUT PER ECO 2935. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600503 19990226 00503 NM 1999 2 26 TSAA9953028 1 19990119 A 5320 BRACKET BOEING 737 7372Q9 138448M NM NLG WW CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 NOSE LANDING GEAR ACTUATOR SUPPORT ANGLE HAS 2 INCH CRACK, HFEC CONFIRMED. REMOVED AND REPLACED WITH NEW SUPPORT ANGLE PER SRM 51-30-2 AND BOEING DRAWING 65-45819. TAT: 47,785.0 HOURS. TAC: 63,219. (X) 2 L 7 2 4F A16WE 1999022600504 19990226 00504 NM 1999 2 26 P2EA99059 1 19990106 A 5210 65299913 FITTING BOEING 737 737222 1384473 NM PASSENGER DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. MAIN ENTRY DOOR TORQUE TUBE LOWER SUPPORT FITTING CRACKED. DEFECT SIZE: LENGTH 0.500 INCH. REPLA CED MAIN ENTRY DOOR STOP FITTING AT BS 294.5, STR 13L PER 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-2-1 23, VAM 100 NR 218. (X) 2 L 7 2 4F A16WE 1999022600505 19990226 00505 NM 1999 2 26 P2EA99058 1 19990105 A 5320 ANGLE BOEING 737 737222 1384473 NM BS 664 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT WHEELWELL SUPPORT ANGLES CRACKED AT BS 664, WL 192, RBL 70. DEFECT SIZE: LENGTH 2.0 INCHES. PERFORMED ON STR 18A SHEER BEAM TO BE 664 FRAME ATTACHMENT MODIFICATION PER BOEING SB 737-53-1056, SEC III, FIG 1 DATE D DECEMBER 15, 1978 AND NOTICE OF STATUS CHANGE DATED JUNE 19, 1981 AND APRIL 20, 1979. SEE COOPESA W.O. M1-0003-1-6, V AM 100 NR 127. (X) 2 L 7 2 4F A16WE 1999022600506 19990226 00506 NM 1999 2 26 P2EA99057 1 19990110 A 5730 SKIN BOEING 737 737247 138448D NM LT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM - LEFT WING LEADING EDGE SKIN CRACKED AT 3 PLACES AT SS 196. DEFECT SIZE: AVERAGE LENGTH: 1.00 INC H. REPAIRED LEFT WING LEADING EDGE SKIN BETWEEN SS 182 AND SS 207.875 PER COOPESA E.O. COO-3-57-022-99 DATED JANUARY 21 , 1999, AND BOEING FAX COO-SJO-99-0047RR DATED 1-19-99. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA D ER F. ABADI DESIGNATION NM-1281 DATE JAN 1-20-99. REF: BOEING FAX COO-SJO-98-0778RR DATED 10-16-99. SEE COOPESA W.O. M1-0005-5-18, VAM 100 NR 292. (X) 2 L 7 2 4F A16WE 1999022600507 19990226 00507 NM 1999 2 26 P2EA99056 1 19990125 A 5320 BEAM BOEING 737 737247 138448D NM BS 685 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM. WHEELWELL LOWER TRANSVERSE BEAM AT BS 685, RBL 24.80. DEFECT SIZE: LENGTH: 2.00 INCHES. REPLACE D TRANSVERSE BEAM AT BS 685 BETWEEN LBL 50 INCH AND RBL 50 INCH PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2, PAGES 1 AND 5. S EE COOPESA W.O. M1-0005-1-112, VAM 100 NR 514. (X) 2 L 7 2 4F A16WE 1999022600508 19990226 00508 NM 1999 2 26 P2EA99055 1 19990203 A 5720 WEB BOEING 737 737247 138448D NM BS 663 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM. VERTICAL PRESSURE WEB CORRODED AT WING CENTER SECTION AT BS 663. REPLACED WING CENTER SECTION SPAR VERTICAL PRESSURE WEB RIGHT SIDE ONLY BS 663, RBL 24.98 AND RBL 45.64 PER BOEING SB 737-57-10-95, REV 6 DATED 4-27-89, FIG 2. SEE COOPESA W.O. M1-0005-1-115, VAM 100 NR 521. (X) 2 L 7 2 4F A16WE 1999022600509 19990226 00509 NM 1999 2 26 P2EA99054 1 19990123 A 5320 BEAM BOEING 737 737247 138448D NM BS 716 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM. LONGITUDINAL BEAM WEB CRACKED AT BS 716. DEFECT SIZE: LENGTH 2.0 INCHES. REPAIRED CENTER WING FL OORBEAM BL ZERO INCH BETWEEN BS 700 AND BS 717 PER BOEING SB 737-57-1210, SEC III, FIG 5, DATED APRIL 4, 1991. SEE COOP ESA W.O. M1-005-2-190, VAM 100 NR 510. (X) 2 L 7 2 4F A16WE 1999022600510 19990226 00510 NM 1999 2 26 P2EA99053 1 19990110 A 5311 FRAME BOEING 737 737222 1384473 NM BS 351 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. FRAME WEB CRACKED AT BS 351.2 BETWEEN STR 19L AND STR 20L. DEFECT SIZE: LENGTH 0.375 INCH. REPLA CED WEB AT BS 351.2 BETWEEN STR 18L AND STR 21L PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-1-133, VAM 100 NR 662. (X) 2 L 7 2 4F A16WE 1999022600511 19990226 00511 NM 1999 2 26 P2EA99052 1 19990116 A 5755 SKIN BOEING 737 737247 138448D NM NR 4 SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM. NR 4 GROUND SPOILER DELAMINATED. DEFECT SIZE: LENGTH 10 INCHES WIDTH 20 INCHES. REPAIRED SPOILER PER COOPESA B.O. COO-CMP-3-57-010-99 DATED JAN 19, 1999. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER ROBERT M. MANASHI DESIGNATION 710167-SW DATED JAN 19, 1999. SEE COOPESA W.O. M1-0005-43, VAM 100 NR 505. (X) 2 L 7 2 4F A16WE 1999022600512 19990226 00512 NM 1999 2 26 P2EA99051 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM BS 1006 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM. PROVISION REPAIRS (TWO) AT BS 1006, BETWEEN STR 12R AND SR 14R DEFECT SIZE: LENGTH 10.0 INCHES WIDT H 8.0 INCHES. FABRICATED AND REPLACED FUSELAGE SKIN SECTION FROM BS 986.5 TO BS 1016, BETWEEN STR 10R AND STR 14R PER C OOPESA E.O. COO-3-53-018-99 DATED 1-21-99 AND BOEING FAX COO-SJO-99-0059RR DATED 1-20-99. DOCUMENTED ON FAA FORM 8110-3 . APPROVED AND SUBMITTED BY FAA DER D.L. JENSEN DESIGNATION NM-2605 DATED JAN 27, 1999. SEE COOPESA W.O. M1-0005-2-183 , VAM 100 NR 491 FOR TECHNICAL INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600513 19990226 00513 NM 1999 2 26 P2EA99050 1 19990109 A 5753 SUPPORT BOEING 737 737222 1384473 NM FLAP TRACK WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT WING NR 7 CARRIAGE TRACK FAIRING SUPPORT WORN. DEFECT SIZE: LENGTH 2.0 INCHES. DEPTH 0.110 INCH. REWORKED CARRIAGE PER BOEING FAXES COO-SJO-99-0038RR DATED JAN 18, 1999 AND COO-SJO-99-0074RR DATED JAN 22, 1999 . DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER F. ABADI DESIGNATION NM-1281 DATED JAN 26, 1999. S EE COOPESA W.O. M1-0003-6-44, VAM 100 NR 628. (X) 2 L 7 2 4F A16WE 1999022600514 19990226 00514 NM 1999 2 26 P2EA99049 1 19990109 A 5753 SUPPORT BOEING 737 737222 1384473 NM FLAP TRACK WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIGHT WING NR 8 FLAP CARRIAGE FLAP TRACK FAIRING SUPPORT WORN. DEFECT SIZE: LENGTH 1.400 INCHES D EPTH 0.750 INCH. REWORKED CARRIAGE PER BOEING FAXES COO-SJO-99-0038RR DATED JAN 18, 1999 AND COO-SJO-99-0079RR JAN 22, 1999. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER F. ABADI DESIGNATION NM-1281 DATED JAN 26, 1999 . SEE COOPESA W.O. M1-0003-6-51, VAM 100 NR 635. (X) 2 L 7 2 4F A16WE 1999022600515 19990226 00515 NM 1999 2 26 P2EA99048 1 19990112 A 5320 BEAM BOEING 737 737247 138448D NM BS 685 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - Q-CHECK ITEM. BEAM LOWER CHORD CRACKED AT BS 685, BL ZERO INCH. DEFECT SIZE: LENGTH 2.00 INCHES. REPLACED FUSE LAGE LONGITUDINAL BEAM LOWER CHORD BL ZERO INCH BETWEEN BS 645 AND BS 727B PER 51-10-1, PAGE 5 AND SRM 51-30-2, PAGE 1. SEE COOPESA W.O. M1-0005-2-169, VAM 100 NR 402. (X) 2 L 7 2 4F A16WE 1999022600516 19990226 00516 NM 1999 2 26 P2EA99047 1 19990106 A 5712 RIB BOEING 737 737222 1384473 NM WS 390 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - Q-CHECK ITEM. RIB CRACKED IN FRONT SPAR CAVITY FSS 390 (SLAT STATION 144.96). DEFECT SIZE: LENGTH 0.500 INCH. R EPLACED LEADING EDGE RIB AT SS 144.96 PER SRM 51-10-1, PAGE 5, AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-5-69, VAM 100 NR 313 FOR TECHNICAL INFORMATION. (X) 2 L 7 2 4F A16WE 1999022600517 19990226 00517 EU 1999 2 26 USAAF99002 1 19990112 A 5610 D20543401 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 884US 3778 11338 PIT - FLT 864 - WHILE CLIMBING OUT FROM PIT AT FL 210, THE LEFT FRONT WINDSCREEN CRACKED. THE FLIGHT CREW FOLLOWED SPEC IAL PROCEDURES AND DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT WINDSHIELD PER AMM 56-11-00. (M) 2 L 7 2 4F RT 1999022600521 19990226 00521 NE 1999 2 26 HALA9900013 2 19990112 A 7532 BLEED VALVE DOUG DC10 DC1030 3023501 WP GE CF6 CF66K 30020 NE NR 1 ENGINE FAILED A HALA O OTHER M OVER TEMP CL CLIMB 1 WP 13 140AA 46712 LAX - FLT 1 - NR 1 PNEUMATIC HI TEMP LIGHT CAME ON IN CLIMB-OUT. PERFORM RED BOX ITEMS AND FOLLOWED PROCEDURE FOR ABNOR MALS. REMOVED AND REPLACED NR 1 ENGINE H/P BLEED VALVE. (M) 2 L 7 3 4F 4 F A22WE E23EA 1999022600522 19990226 00522 WP 1999 2 26 HALA9900020 1 19990117 A 2740 95901 MOTOR DOUG DC9 DC951 3022051 WP HORIZ STABILIZER FAILED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 672MC 122 47661 HNL - FLT 103 - PRIMARY STAB TRIM INOPERATIVE. WILL NOT MOVE WITH SUITCASE HANDLE OR EITHER CNTL WHEEL SWITCHES. ALT T RIM APPEARS TO BE NORMAL. (M) 2 L 7 2 4F RT A6WE 1999022600523 19990226 00523 WP 1999 2 26 HALA9900021 1 19990118 A 2150 20495054 ACM DOUG DC9 DC951 3022051 WP RIGHT MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 672MC 66134 47661 HNL - FLT 202 - TAIL COMPARTMENT HIGH TEMP LIGHT ON. ISOLATED TO RT PACK. REPLACED RT ACM, OPS AND LEAK CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999022600524 19990226 00524 WP 1999 2 26 HALA9900005 1 19990108 A 2610 RELAY DOUG DC10 DC1010 3022110 WP NR 3 ENGINE MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 125AA 46525 HNL - FLT 25 - NR 3 ENGINE 'A' LOOP WILL NOT TEST. LOOP 'B' TEST OK. REMOVED AND REPLACED R2-153 RELAY GRN TEST GOOD. (M) 2 L 7 3 4F A22WE 1999022600525 19990226 00525 WP 1999 2 26 HALA9900023 1 19990114 A 3232 ACTUATOR DOUG DC10 DC1010 3022110 WP NLG DOOR MALFUNCTIONED A HALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 13 162AA 46943 LAX - FLT 09 - AFTER TAKEOFF AFTER GEAR RETRACTION STRONG VIBRATION FROM NOSE GEAR AREA. EXTENDED GEAR AND DUMPED FUEL. AIRCRAFT RETURNED TO LAX WHERE IT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATORS, OPS CHEC K OK. (M) 2 L 7 3 4F A22WE 1999022600526 19990226 00526 WP 1999 2 26 HALA9900019 1 19990117 A 2610 SENSOR DOUG DC10 DC1010 3022110 WP NR 3 ENGINE MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 125AA 46525 HNL - FLT 482 - NR 3 ENGINE 'A' LOOP WILL NOT TEST, 'B' TEST OK. REMOVED AND REPLACED CONNECTOR PYLON LOOP 'A' NR 3 EN GINE. 'A' LOOP TEST OP CHECKED GOOD. (M) 2 L 7 3 4F A22WE 1999022600527 19990226 00527 WP 1999 2 26 HALA9900018 1 19990119 A 2612 FIRE LOOP DOUG DC9 DC951 3022051 WP NR 2 ENGINE CHAFED A HALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 WP 13 420EA 47689 FLT 509 - HNL - NR 2 ENGINE FIRE DET LOOP 'A' LIGHT CAME ON DURING FLIGHT. FIRE TEST OK. SELECTED LOOP 'B'. REPAIRED CHAFED WIRE, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999022600528 19990226 00528 NM 1999 2 26 MASA99005 1 19990108 A 3350 6104799 LIGHT GRIMES 6038443 DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING A ROUTINE LIE CHECK INSPECTION, MAINTENANCE PERSONNEL FOUND THE CENTER FORWARD EMERGENCY EXIT LIGHT FAILED TO ILL UMINATE. REPLACED THE NR 2 EMERGENCY POWER SUPPLY HOUSING, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1999022600529 19990226 00529 SO 1999 2 26 SIMA990091 1 19990109 A 3260 852701 SENSOR EMB 145 EMB145ER SO RT MLG FAILED A SIMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 21 600BK A6024 145044 ORD - FLT 4096 - ON GEAR RETRACTION OUT OF CVG, RIGHT MAIN LANDING GEAR EICAS MESSAGE AND LANDING GEAR LEVER DISAGREE WE RE NOTICED. CYCLED LANDING GEAR AND ALL INDICATIONS WERE NORMAL. ON GEAR EXTENSION INTO ORD, LANDING GEAR LEVER DISAGR EE (EICAS) MESSAGE APPEARED AND RMU DID NOT INDICATE DOWN AND LOCKED. PERFORMED EMERGENCY EXTENSION PROCEDURES WITH NO CHANGE IN INDICATIONS. RESET LANDING GEAR CIRCUIT BREAKERS 1 AND 2 AND RECYCLED GEAR. GEAR INDICATIONS WERE THEN NORMA L. REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOWNLOCK SENSOR. FUNCTIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT T00011AT 1999022600530 19990226 00530 EU 1999 2 26 SIMA990141 1 19990114 A 3350 GE1317 BULB SAAB SF340 340B 7860101 EU ROW 12C FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 240DS 340B240 DFW - FLT 3654 - EMERGENCY EXIT LIGHT AT SEAT 12C DOES ILLUMINATE. FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS ARMED SWITCH DOES NOT ILLUMINATE. REMOVED AND REPLACED BULBS FOR BOTH SEAT 12C AND F/A PANEL ARM LIGHT. OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4T RT A52EU 1999022600531 19990226 00531 EU 1999 2 26 99ZZZM145 1 19990114 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU ROW 12C FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 240DS 340B240 DFW - FLT 3654 - EMERGENCY EXIT LIGHT AT SEAT 12C DOES ILLUMINATE. FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS ARMED SWITCH DOES NOT ILLUMINATE. REMOVED AND REPLACED BULBS FOR BOTH SEAT 12C AND F/A PANEL ARM LIGHT. OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4T RT A52EU 1999022600534 19990226 00534 EU 1999 2 26 SIMA990134 1 19990113 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROWS 5-6 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 263AE 340B263 DFW - FLT 5104 - EMERGENCY FLOOR PROXIMITY LIGHTS AT SEAT 5BC AND 6BC DO NOT ILLUMINATE. REMOVED AND REPLACED BULBS. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999022600535 19990226 00535 SO 1999 2 26 C2XA99CL005 1 19990114 A 7933 D3899920KH53SN CONNECTOR EMB 145 EMB145 SO LT ENGINE MALFUNCTIONED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 15932 145015 CLE - FLT 4019 - CREW REPORTED THAT DURING CRUISE THE LEFT ENGINE OIL TEMPERATURE PEGGED OUT (135 DEGREES CELSIUS) AND W OULD NOT DECREASE WITH A THRUST DECREASE, A PRECAUTIONARY ENGINE SHUT DOWN WAS PERFORMED. AIRCRAFT RETURNED TO FIELD WI THOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A FAULTY CONNECTOR IN THE INDICATION SYSTEM. THE CONNECTOR WAS REMOVED AND REPLACED REFERENCES EMB-145 MM 79-30-50. (M) 2 L 7 2 4F RT T00011AT 1999022600536 19990226 00536 SO 1999 2 26 C2XA99CL004 1 19990111 A 3230 2112600000 ROD EMB 120 EMB120RT SO RT MLG WORN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12709 120101 CLE - FLT 3067 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. A IRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR ACTUAT OR LEVER ROD END IAW ERAM MM 32-12-01. THE LEVER WAS ALSO REPLACED FOR PRECAUTIONARY MEASURES IAW EMB-120 MM 32-32-10. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600537 19990226 00537 EU 1999 2 26 C2XA99IA062 1 19990114 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14451 512 IAH - DURING PREFLIGHT INSPECTION, THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE BATTERY FOR THE AFFECTED LIGHT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999022600539 19990226 00539 SO 1999 2 26 C2XA99IA064 1 19990118 A 3397 W182001124 WIRE EMB 120 EMB120RT SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING PREFLIGHT INSPECTION, TWO AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED T HE AFFECTED WIRES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600540 19990226 00540 CE 1999 2 26 C2XA99CL002 1 19990108 A 3250 993880047 ACTUATOR BEECH 1900 1900D 1154162 CE NLG STEERING INOPERATIVE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 81546 4705 225 UE187 CLE - FLT 3099 - CREW REPORTED THAT AFTER LANDING, WHILE TAXIING TO THE GATE THE NOSE WHEEL STEERING WAS INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING DISCONNECT ACTUATOR IAW B1900 MM 32-50-01, OPERATIONAL CHECKS WE RE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1999022600541 19990226 00541 CE 1999 2 26 C2XA99CL003 1 19990109 A 3230 1143610441 HARNESS BEECH 1900 1900D 1154162 CE RT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 81538 UE199 CLE - FLT 3069 - CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD WI THOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR SWITCH HARNESS ASSEMBLE IAW B1900D MM 32-60-02, ADJUSTMENTS WERE MADE IAW B1900D MM 32-60-05. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1999022600542 19990226 00542 SO 1999 2 26 C2XA99IA024 1 19990106 A 7110 12025602619 SKIN EMB 120 EMB120RT SO LT ENG COWL CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT ENGINE PANEL 418 INNER SKIN CHAFED THROUGH ON FORWARD EDGE. INSTALLED REPAIR DOUB LER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600543 19990226 00543 SO 1999 2 26 C2XA99IA034 1 19990106 A 5320 12006157007 SUPPORT EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND PANEL 262CF OUTBOARD FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT SILL. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600544 19990226 00544 SO 1999 2 26 C2XA99IA039 1 19990106 A 7500 12034290021 VENT TUBE EMB 120 EMB120RT SO BLEED SYSTEM CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT ENGINE VENT TUBE, INBOARD SIDE WAS CHAFED AT IGNITOR LEADS. REMOVED AND REPLACED LEFT ENGINE VENT TUBE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600545 19990226 00545 SO 1999 2 26 C2XA99IA040 1 19990106 A 5280 12019414002 ANGLE EMB 120 EMB120RT SO RT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT MLG, RIGHT FORWARD DOOR, AFT HINGE AFT ANGLE CRACKED. REMOVED AND REPLACED ANGLE . AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600546 19990226 00546 SO 1999 2 26 C2XA99IA041 1 19990106 A 5280 12012938002 ANGLE EMB 120 EMB120RT SO RT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION FOUND RT MLG, LEFT AFT DOOR, AFT HINGE FORWARD ANGLE CRACKED. REMOVED AND REPLACED ANGLE. AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600547 19990226 00547 SO 1999 2 26 C2XA99IA042 1 19990106 A 5280 12019412001 BRACKET EMB 120 EMB120RT SO LT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT MLG FORWARD DOOR CENTER ROD CONNECTION FORWARD ANGLE BRACKET CRACKED. REMOVED AND REPLACED ANGLE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600548 19990226 00548 SO 1999 2 26 C2XA99IA043 1 19990106 A 5280 12004499003 BRACKET EMB 120 EMB120RT SO LT MLG DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT MLG FORWARD, OUTBOARD DOOR, FORWARD HINGE BRACKET HOLE WAS ELONGATED, AIRFRAME SID E. REMOVED AND REPLACED LEFT MLG FORWARD, OUTBOARD DOOR, FORWARD HINGE BRACKET. AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A31SO 1999022600549 19990226 00549 SO 1999 2 26 C2XA99IA044 1 19990106 A 5280 12005599003 BRACKET EMB 120 EMB120RT SO LT MLG DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT MGL FORWARD, OUTBOARD DOOR, AFT HINGE BRACKET HOLE WAS ELONGATED, AIRFRAME SIDE. R EMOVED AND REPLACED LEFT MLG FORWARD, OUTBOARD DOOR, AFT HINGE BRACKET. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A31SO 1999022600550 19990226 00550 SO 1999 2 26 C2XA99IA050 1 19990106 A 7110 12025600611 FRAME EMB 120 EMB120RT SO RT ENGINE COWL DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND HOLE IN RIGHT ENGINE OUTBOARD COWL DOOR 424 FORWARD FRAME WHERE STAY ROD HAS PULLED LOO SE. INSTALLED 'L' ANGLE REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600551 19990226 00551 SO 1999 2 26 C2XA99IA049 1 19990106 A 7810 12020140635 SKIN EMB 120 EMB120RT SO LT ENG EXHAUST CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT EXHAUST PIPE COWLING SKIN CRACKED AT LEFT FORWARD LOWER CORNER. STOP DRILLED CRAC K AND INSTALLED DOUBLER REPAIR. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600552 19990226 00552 SO 1999 2 26 C2XA99IA048 1 19990106 A 7110 12025603620 COWL EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE COWL DOOR 428 LOWER FORWARD CORNER CHAFED AND CRACKED. REMOVED DAMAGED AR EA AND INSTALLED DOUBLER REPAIR AND CHAF STRIP. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600553 19990226 00553 SO 1999 2 26 C2XA99IA047 1 19990106 A 7810 12033744009 EXHAUST PIPE EMB 120 EMB120RT SO RT ENGINE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURNIG C-CHECK INSPECTION, FOUND RIGHT EXHAUST PIPE CRACKED AT AFT FAIRING AND RIVETS LOOSE IN SAME AREA. WELDED CRACKS AND REPLACED RIVETS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600554 19990226 00554 SO 1999 2 26 C2XA99IA052 1 19990106 A 7110 12026589001 BRACKET EMB 120 EMB120RT SO RT ENG COWL CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE COWL DOOR 428 AFT HINGE BRACKET ON DOOR INTERNAL SUPPORTS CRACKED AND SEPA RATED. REPLACED HINGE BRACKET. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600555 19990226 00555 SO 1999 2 26 C2XA99IA051 1 19990106 A 7110 12025600611 FRAME EMB 120 EMB120RT SO RT ENG COWL CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND HOLE CHAFED INTO FOWARD FRAME ABOVE COWL STAY AT RIGHT ENGINE OUTBOARD COWL DOOR 424. I NSTALLED 'L' ANGLE REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600556 19990226 00556 SO 1999 2 26 C2XA99IA053 1 19990106 A 7110 12025603619 PANEL EMB 120 EMB120RT SO LT ENG COWL CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND LEFT ENGINE PANEL 417 CHAFED AT LOWER CENTER ABOVE LATCH. WELDED CHAFED AREA. AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600557 19990226 00557 SO 1999 2 26 C2XA99IA056 1 19990106 A 5320 12015034001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND THE INTERCOSTAL SUPPORT FOR NUTPLATES ON ACCESS PANEL 1912 CRACKED AT AFT OUTBOARD END. REMOVED CRACKED PORTION AND SPLICED IN NEW. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600558 19990226 00558 SO 1999 2 26 C2XA99IA054 1 19990106 A 5280 12048448002 BRACKET EMB 120 EMB120RT SO RT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT MLG AFT INBOARD DOOR, FORWARD HINGE POINT, NACELLE RIB AFT MOUNT FITTING CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600559 19990226 00559 SO 1999 2 26 C2XA99IA045 1 19990106 A 5280 12004499003 BRACKET EMB 120 EMB120RT SO MLG DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT MLG FORWARD, INBOARD DOOR, FORWARD AIRFRAME HINGE HOLE ELONGATED. REMOVED AND RE PLACED RIGHT MLG FORWARD, INBOARD DOOR, FORWARD HINGE BRACKET FLANGE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600569 19990226 00569 SO 1999 2 26 C2XA99IA065 1 19990118 A 3350 F02A250V1A FUSE EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURNG PREFLIGHT INSPECTION, THE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE FUSE FOR THE AFFECTED LIGHTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600608 19990226 00608 WP 1999 2 26 GAIA9902 1 19990106 A 2140 88B812 HEATER CVAC 240 240D 2422660 WP COCKPIT CONTAMINATED A GAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 94226 48 KHA - FLT 184 - AFTER TAKEOFF FROM PIT, ON CLIMB-OUT, THE COCKPIT FILLED WITH A CARAMEL SMELLING SMOKE, THE FLIGHT CREW TURNER OFF THE COCKPIT HEATER ELIMINATING SMOKE, AIRCRAFT RETURNED TO PIT AND MADE AN UNEVENTFUL LANDING. INSPECTION FO UND DE-ICING FLUID HAD ENTERED INTO THE COCKPIT HEATER INLET WHICH CAUSED SMOKE AFTER THE HEATER WAS STARTED, HEATER INL ET AND DUCTING CLEANED, HEATER OPERATIONAL CHECKED NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R RT A793 1999022600609 19990226 00609 NM 1999 2 26 GAIA9901A 1 19990107 A 3233 65178197 ACTUATOR BOEING 727 727223 1384074 NM LT MLG MALFUNCTIONED A GAIA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 6831 20184 ON APPROACH TO BNA, CREW REPORTS LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. CRANKED GEAR DOWN LOCKED INDICATION. RECYCLED GEAR AFTER 1ST UNSAFE INDICATION, PRIOR TO MANUAL EXTENSION. REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK ACTUA TOR IAW B727 MM 32-32-61. OPERATIONAL AND LEAK CHECKED GOOD IAW B727 MM 32-32-0 AND 32-34-0. OPERATIONAL AND LEAK CHEC K GOOD WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999022600610 19990226 00610 NM 1999 2 26 GAIA9903 1 19990108 A 3222 STRUT BOEING 727 727223 1384074 NM NLG DISCHARGED A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 6838 20191 AFTER TAKEOFF FROM ROC, THE FLIGHT CREW NOTICED THAT THE NOSE GEAR 'RED' LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTIO N. AFTER APPROXIMATELY FIVE MINUTES AND A RECYCLE OF THE GEAR, THE FLIGHT CREW HEARD A 'CLUNK' SOUND AND THE NOSE GEAR 'RED' LIGHT WENT OUT. THE AMBER LIGHT ON THE FLIGHT ENGINEERS PANEL WENT OUT AS WELL. THE AIRCRAFT CONTINUED TO IND AN D LANDED WITHOUT FURTHER DIFFICULTIES. INSPECTED THE AIRCRAFT AT IND AND FOUND THE NOSE STRUT FLAT. SERVICED THE NOSE STRUT AND MAINTENANCE FERRIED THE AIRCRAFT TO OKC FOR A GEAR RETRACTION TEST. IN OKC, CLEANED AND LUBRICATED THE GEAR H ANDLE. PERFORMED AN OPERATIONAL CHECK OF THE NOSE LANDING GEAR RETRACTION SYSTEM. SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F A3WE 1999022600619 19990226 00619 WP 1999 2 26 USAAD99017 1 19990127 A 2820 89903601 LINE DOUG DC9 DC931 3022065 WP RT ENGINE BROKEN A USAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 EA 19 977VJ 48155 DCA-BUF - FLT 660 - AFTER TAKEOFF THE RIGHT ENGINE FLAMED OUT. THE AIRCRAFT LANDED AT BWI WITHOUT INCIDENT. MAINTENANC E REPLACED THE AFT SECTION OF THE PS4 LINE GOING TO THE FUEL CONTROL. (M) 2 L 7 2 4F A6WE 1999022600620 19990226 00620 NM 1999 2 26 USAA990058 1 19990120 A 5320 CLIP BOEING 767 767201 1385125 NM BS 1702 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 1702 AND STRINGER 30R AT TIE CLIP. INSTALLED S TRINGER TIE CLIP PER SRM 51-10-00. (M) 2 L 7 2 4F RT A1NM 1999022600621 19990226 00621 NM 1999 2 26 USAA990060 1 19990120 A 5347 SEAT TRACK BOEING 767 767201 1385125 NM BS 1065 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 1065 RBL 10 SEAT TRACK. INSTALLED SECTION SEAT T RACK PER EA 63457. (M) 2 L 7 2 4F RT A1NM 1999022600622 19990226 00622 NM 1999 2 26 USAA990059 1 19990120 A 5320 CLIP BOEING 767 767201 1385125 NM BS 1702 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 45951 23898 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STATION 1702 AND STRINGER 39 LT AT TIE CLIP. INSTALLE D STRINGER TIE CLIP PER SRM 51-10-00. (M) 2 L 7 2 4F RT A1NM 1999022600623 19990226 00623 NM 1999 2 26 USAASB99009 1 19990107 A 3260 189929 SENSOR BOEING 737 737401 1384701 NM LT MLG FAILED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 418US 23985 CLT - AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE LEFT MAIN LANDING GEAR UNSAFE ILLUMINATED AND REMAINED ON WITH GEAR RETRACTED. CREW RECYCLED THE GEAR WITH NO HELP. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK SENSOR PER MM 32-61-21. SYSTEM OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999022600624 19990226 00624 NM 1999 2 26 USAASB99016 1 19990120 A 3260 189929 SENSOR BOEING 737 737401 1384701 NM LT MLG MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 417US 23984 CLT - FLT 2210 - AFTER TAKEOFF, THE FLIGHT CREW REPORTED THE LEFT MAIN LANDING GEAR UNSAFE ILLUMINATED AND REMAINED ON A FTER GEAR RETRACTION. LIGHT WOULD NOT EXTINGUISH WITH THE GEAR HANDLE IN THE UP OR ON POSITION. FLIGHT RETURNED TO FIE LD AT CLT. CREW RECEIVED NORMAL GEAR INDICATION WHEN LANDING GEAR WAS LOWERED, THREE GREEN AND NO RED LIGHTS. FLIGHT L ANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR UPLOCK PROXIMITY SENSOR PER MM 32-61-21. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1999022600625 19990226 00625 NM 1999 2 26 USAABB99003 1 19990119 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 LAX - FOUND FOUR AISLE EMERGENCY LIGHTS LOW. MAINTENANCE REPLACED FOUR BATTERIES. (M) 2 L 7 2 4F RT A2NM 1999022600626 19990226 00626 NM 1999 2 26 USAABB99002 1 19990113 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM ROW 26 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 LAX - FOUND EMERGENCY FLOOR LEVEL LIGHTING AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT ROW 26, AN D BATTERY PACKS AT ROWS 9, 18, 23, 26, 29 AND 33. (M) 2 L 7 2 4F RT A2NM 1999022600627 19990226 00627 NM 1999 2 26 99ZZZM148 1 19990113 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 LAX - FOUND EMERGENCY FLOOR LEVEL LIGHTING AT ROW 26 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT ROW 26, AN D BATTERY PACKS AT ROWS 9, 18, 23, 26, 29 AND 33. (M) 2 L 7 2 4F RT A2NM 1999022600628 19990226 00628 NM 1999 2 26 USAA990041 1 19990117 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 30727 23879 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM BS 344.17 RBL 8 - RBL 22 CORROSION TASK NR C 53-1 07-02. INSTALLED 'T' CAP DOUBLER REPAIR PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999022600629 19990226 00629 NM 1999 2 26 USAA990040 1 19990117 A 5315 654681165 FLOORBEAM BOEING 737 737401 1384701 NM BS 986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 30727 23879 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FUOND CORROSIN ON FLOORBEAM STATION 986 BL 0 TO RBL 35 1 INCH BY 3 INCH, CORRO SION TASK NR C 53-107-02. INSTALLED 'T' CAP AND SHEAR TIES PER TR 53-60-01 AND SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999022600630 19990226 00630 NM 1999 2 26 USAA990042 1 19990117 A 5315 6546809 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 30727 23879 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FASTENER HOLES STATION 947 BETWEEN LBL 20 TO RBL 20 FLO ORBEAM. CORROSION TASK NR C 53-107-02. INSTALLED BEAM SECTION PER TR 53-60-02. (M) 2 L 7 2 4F RT A16WE 1999022600631 19990226 00631 EU 1999 2 26 SIMA990241 1 19990124 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU SEAT 9B FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AE 340B198 DFW - FLT 5020 - FLOOR PROXIMITY LIGHT AT SEAT 9B DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CH ECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999022600632 19990226 00632 EU 1999 2 26 SIMA990231 1 19990123 A 3397 WIRE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AM 319 MSN - FLT 9751 - PASSENGER DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. FOUND BROKEN WIRE AT THE LIGHT ASSEMBLY. DISASSEM BLED LIGHT CONNECTOR, INSTALLED NEW PINS FOR WIRES AND REASSEMBLED CONNECTOR. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999022600633 19990226 00633 EU 1999 2 26 SIMA990072 1 19990107 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 414 SGF - FLT 4370 - FLOOR PROXIMITY LIGHTS IN AFT CABIN AND SERVICE DOOR EMERGENCY EXIT SIGN DO NOT ILLUMINATE. REMOVED AN D REPLACED A BATTERY PACK FOR THE FLOOR PROXIMITY LIGHTS AND THE LIGHT BULBS IN THE EMERGENCY EXIT SIGN. OPERATIONAL CH ECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1999022600634 19990226 00634 EU 1999 2 26 99ZZZM149 1 19990107 A 3350 7012210 BULBS AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 414 SGF - FLT 4370 - FLOOR PROXIMITY LIGHTS IN AFT CABIN AND SERVICE DOOR EMERGENCY EXIT SIGN DO NOT ILLUMINATE. REMOVED AN D REPLACED A BATTERY PACK FOR THE FLOOR PROXIMITY LIGHTS AND THE LIGHT BULBS IN THE EMERGENCY EXIT SIGN. OPERATIONAL CH ECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1999022600635 19990226 00635 EU 1999 2 26 SIMA990086 1 19990108 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AE 340B329 DFW - FLT 5026 - SEVERAL FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHTS BULBS. O PERATINOAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999022600636 19990226 00636 EU 1999 2 26 SIMA990096 1 19990109 A 2611 CG7G010 SMOKE DETECTOR AEROSP ATR72 ATR72212 EU E/E BAY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 440AM 3239 440 CRP - FLT 3739 - ELECTRICAL SMOKE INDICATION ON CWP ILLUMINATED. REMOVED AND REPLACED FORWARD ELECTRONICS RACK SMOKE DE TECTOR. OPERATIONAL TESTS NORMAL. NO FURTHER SMOKE INDICATIONS NOTED. (M) 2 H 7 2 4T RT A53EU 1999022600637 19990226 00637 EU 1999 2 26 SIMA990101 1 19990110 A 3350 3012001 CONNECTOR AEROSP ATR72 ATR72212 EU BATTERY PACK LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AT 417 HOU - 3627 - SOME OF THE AFT EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. RESEATED THE CONNECTOR ON THE AFT BATTERY PACK. O PERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999022600638 19990226 00638 EU 1999 2 26 SIMA990135 1 19990113 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AT 1019 408 DFW - FLT 3656 - NINE BULBS ON FLOOR PROXIMITY LIGHT PATH DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK. OPERAT IONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999022600639 19990226 00639 EU 1999 2 26 SIMA990192 1 19990119 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 273AE 17904 340B273 SPS - FLT 3512 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROWS 6B, 7B AND 8B DO NOT ILLUMINATE. FERRIED AIRCRAFT TO DFW FOR REPAIR. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999022600640 19990226 00640 NM 1999 2 26 P2EA99014 1 19990109 A 5512 SKIN BOEING 737 737247 138448D NM HORIZ STAB DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - RIGHT HORIZONTAL STAB STATION 88.5 LOWER SURFACE WITH A PROVISIONAL REPAIR. REPAIRED HORIZONTAL STAB LOWER SKIN S ECTION BETWEEN STAB STATION 81.5 AND STAB STATION 95.5 PER 55-10-3 FIG 3. (M) 2 L 7 2 4F A16WE 1999022600641 19990226 00641 NM 1999 2 26 P2EA99013 1 19990112 A 5330 SKIN BOEING 737 737247 138448D NM BS 293-286 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - FORWARD SERVICE DOORWAY LOWER HINGE CUTOUT CRACKED. DEFECT SIZE, LENGTH 1 INCH. REPAIRED FORWARD SERVICE DOORWAY LOWER HINGE CUTOUT BETWEEN BS 293 AND BS 286 FROM STRINGER 13 RT TO STRINGER 14 RT PER SRM 53-30-3, FIG 32. (M) 2 L 7 2 4F A16WE 1999022600642 19990226 00642 NM 1999 2 26 P2EA99012 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM BS 389-397 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - PROVISIONAL FUSELAGE SKIN REPAIR AT BS 389 TO BS 397, STRINGER 4 RT. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 39 8 TO BS 389, FROM STRINGER 3 RT TO STRINGER 5 RT PER SRM 53-30-3, FIG 9. (M) 2 L 7 2 4F A16WE 1999022600643 19990226 00643 NM 1999 2 26 P2EA99011 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM BS 998-1009 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - PROVISIONAL REPAIR AT BS 1006, STRINGER 4 RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 998 TO BS 1009, FROM STRINGE R 3 RT TO STRINGER 5 RT PER SRM 53-30-3 FIG 4. (M) 2 L 7 2 4F A16WE 1999022600644 19990226 00644 NM 1999 2 26 P2EA99034 1 19990114 A 5320 DOUBLER BOEING 737 737222 1384473 NM BS 616-639 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - INTERNAL DOUBLER DISBONDED FROM BS 616 TO BS 639, STRINGER 8 LT TO STRINGER 9 LT. DEFECT SIZE, LENGTH 23 INCH WID TH 20 INCH. REPAIRED INTERNAL DOUBLER BETWEEN BS 616 TO BS 639, BETWEEN STRINGER 8 LEFT AND STRINGER 9 LEFT PER SRM 53- 30-3, FIG 17. (M) 2 L 7 2 4F A16WE 1999022600645 19990226 00645 NM 1999 2 26 P2EA99035 1 19990120 A 5313 STRINGER BOEING 737 737247 138448D NM BS 990-1016 MISDRILLED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - FUSELAGE STRINGER 15 RT AT BS 1006 WITH A DRILLED HOLE AT RADIUS. DEFECT SIZE, DIAMETER .1875 INCH. REPAIRED FUS ELAGE STRINGER 15 RT BETWEEN BS 990 AND BS 1016 PER SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 1999022600646 19990226 00646 NM 1999 2 26 P2EA99036 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM BS 877-887 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - PROVISIONAL REPAIR AT BS 877 TO BS 887, STRINGER 19 LEFT TO STRINGER 20 LEFT. REPAIRED FUSELAGE SKIN FROM BS 873 TO 889 BETWEEN STRINGER 19 LEFT TO STRINGER 21 LEFT PER COOPESA EO COO-SJO-99-0051RR DATED 1-20-00 AND BOEING FAX COO-SJ O-99-0051RR DATED 1-19-99. (M) 2 L 7 2 4F A16WE 1999022600647 19990226 00647 NM 1999 2 26 P2EA99037 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM BS 844-851 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - PROVISIONAL REPAIR AT BS 847, BETWEEN STRINGER 20 RT AND STRINGER 21 RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 8 44 TO BS 851, BETWEEN STRINGER 19 RT TO STRINGER 22 RT PER COOPESA EO COO-3-53-023-99 DATED 1-22-99 AND BOEING FAX COO-S JO-99-0050RR DATED 1-19-99. (M) 2 L 7 2 4F A16WE 1999022600648 19990226 00648 WP 1999 2 26 USAAD99016 1 19990127 A 3260 CONNECTOR DOUG DC9 DC931 3022065 WP NLG LOOSE A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 942VJ 47057 RIC-PHL - FLT 1244 - DURING APPROACH, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. THE APPRO ACH WAS ABORTED AND A VISUAL CHECK WAS MADE OF THE NOSE GEAR AND FOUND TO BE SAFE. THE AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE TIGHTENED A LOOSE ELECTICAL CONNECTOR IN THE NOSE WHEEL WELL. (M) 2 L 7 2 4F A6WE 1999022600649 19990226 00649 NM 1999 2 26 USAA990043 1 19990122 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 230AU 50711 21975 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FUSELAGE SKIN STATION 727B AND STRINGER 17L. INSTALL ED DOUBLER PER SRM 53-30-3 FIG 25. (M) 2 L 7 2 4F A16WE 1999022600650 19990226 00650 NM 1999 2 26 USAASB99023 1 19990129 A 3350 500000043 BATTERY CHARGER BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 257AU 22799 CMH - MAINTENANCE FOUND THE FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999022600651 19990226 00651 NM 1999 2 26 USAASB99022 1 19990122 A 3350 LIGHT BOEING 737 737201 1384454 NM 11C INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 227AU 21816 PHL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 11C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. O PS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999022600652 19990226 00652 NM 1999 2 26 USAASB99021 1 19990121 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 427US 24549 IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999022600653 19990226 00653 WP 1999 2 26 USAAD99018 1 19990123 A 5240 SEAL DOUG DC9 DC982 3022082 WP SERVICE DOOR MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 825US 49237 CLT-BUF - FLT 1223 - AFTER TAKEOFF, THE CABIN WOULD ONLY PRESSURIZE TO 1 PSI WITH THE OUTFLOW VALVE FULLY CLOSED. THE A IRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED SEALANT FROM THE AFT GALLEY SERVICE DOOR FRAME AND APPLIED FILLER AS REQUIRED. THE AIRCRAFT WAS PRESSURIZED AND NO LEAKS FOUND AT ANY DOOR. (M) 2 L 7 2 4F A6WE 1999022600654 19990226 00654 WP 1999 2 26 USAAD99015 1 19990127 A 3230 59516395001 CYLINDER DOUG DC9 DC931 3022065 WP NLG FAILED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 980VJ 48156 CLT-CMH - FLT 450 - DURING APPROACH THE NOSE LANDING GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES. THE EMERGENCY GEAR EXTENSION LEVER WAS USED TO EXTEND THE NOSE LANDING GEAR. MAINTENANCE REPLACED THE NOSE LANDING GEAR BUNGEE CYLINDER. ( M) 2 L 7 2 4F A6WE 1999022600655 19990226 00655 WP 1999 2 26 USAA990065 1 19990127 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 718 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 973VJ 80225 47099 PIT - DURING C-6 CHECK, FOUND .75 INCH CRACK RT FUSELAGE MAIN FRAME FS 718. INSTALLED BATHTUB FITTING AND PLATE PER TYP ICAL REPAIR 53-10-15A. (M) 2 L 7 2 4F A6WE 1999022600656 19990226 00656 WP 1999 2 26 USAAD99012 1 19990118 A 3350 145971 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 817US 48097 BUF - THE OVERHEAD EMERGENCY LIGHT AT SEAT ROW 30 AND BETWEEN THE AFT LAVATORIES WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999022600657 19990226 00657 WP 1999 2 26 USAAD99013 1 19990106 A 2410 696233B CSD DOUG DC9 DC931 3022065 WP RT ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 938VJ 48119 DAY-PHL - FLT 648 - AFTER TAKEOFF WITH THE AIRFOIL ANTI-ICE TURNED ON THE ELECTRIC BUS RELAYS STARTED CYCLING. THE FLIG HT CREW TURNED OFF THE RIGHT GENERATOR AND THE CYCLING STOPPED. THE RIGHT GENERATOR WAS RESET BUT 30 SECONDS LATER THE CYCLING STARTED AGAIN. THE RIGHT GENERATOR WAS SHUT OFF AND THE APU STARTED TO POWER THE RIGHT ELECTRICAL BUS. THE AIR CRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT WITH THE RIGHT GENERATOR INO PERATIVE UNDER THE MEL PROCEDURES. THE CSD WAS REPLACED DURING THE MAINTENANCE OVERNIGHT. (M) 2 L 7 2 4F A6WE 1999022600658 19990226 00658 EU 1999 2 26 USAA990054 1 19990114 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 11257/12791 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 854US 21601 11282 PIT - DURING CORROSION TRACK VISIT FOUND .75 INCH BY .25 INCH CORROSION AND .75 INCH BY .25 INCH CORROSION. BOTH AREAS CORRODED AT CENTER CARGO BEAM AT STRINGER 72 BETWEEN FRAME 11257 AND 12791. REMOVED CORROSION AND INSTALLED STRAP AT ST ATIN 11541 PER EA NR 51316. (M) 2 L 7 2 4F RT 1999022600659 19990226 00659 NM 1999 2 26 P2EA99033 1 19990114 A 5320 DOUBLER BOEING 737 737222 1384473 NM BS 616-639 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - INTERNAL DOUBLER DISBONDED FROM BS 616 TO BS 639, BETWEEN STRINGER 8 RT AND STRINGER 9 RT, DEFECT SIZE, LENGTH 23 INCHES, WIDTH 20 INCHES. REPAIRED INTERNAL DOUBLER BETWEEN BS 616 AND BS 639, BETWEEN STRINGER 8 RT AND STRINGER 9 RT P ER SRM 53-30-3, FIG 17. (M) 2 L 7 2 4F A16WE 1999022600660 19990226 00660 NM 1999 2 26 P2EA99032 1 19990110 A 2822 HOUSING BOEING 737 737222 1384473 NM BOOST PUMP DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - LEFT WING FUEL TANK, FORWARD CENTER TANK AFT BOOST PUMP HOUSING WITH TEMPORARY REPAIR. REPAIRED LEFT FUEL TANK BO OST PUMP HOUSING PER SRM 57-20-6, FIG 2. (M) 2 L 7 2 4F A16WE 1999022600661 19990226 00661 NM 1999 2 26 P2EA99031 1 19990106 A 5311 FRAME BOEING 737 737222 1384473 NM BS 440 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - FRAME LOWER FLANGE CRACKED AT BS 440, BETWEEN STRINGER 28 LEFT AND STRINGER 28 RT, DEFECT SIZE, LENGTH .50 INCH. R EPAIRED FRAME SECTION AT BS 440, BETWEEN STRINGER 28 LEFT AND STRINGER 28 RT PER SRM 53-10-4, FIG 10. (M) 2 L 7 2 4F A16WE 1999022600662 19990226 00662 NM 1999 2 26 P2EA99028 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM BS 798-807 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - PROVISIONAL REPAIR FROM BS 799 TO 807, STRINGER 4 RT. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 798 AND BS 807, F ROM STRINGER 3 RT TO STRINGER 5 RT PER SRM 53-30-3, FIG 9. (M) 2 L 7 2 4F A16WE 1999022600663 19990226 00663 NM 1999 2 26 P2EA99026 1 19990108 A 5320 ANGLE BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - ANGLE CRACKED AT BS 727, RBL 67, WL 208. DEFECT SIZE, LENGTH .375 INCH. FLOOR SUPPORT ANGLE REPAIRED FROM BS 716 TO BS 733, RBL 67, WL 208 PER SRM 51-40-1, FIG 1 DETAIL II. (M) 2 L 7 2 4F A16WE 1999022600664 19990226 00664 NM 1999 2 26 P2EA99025 1 19990106 A 5754 RIB BOEING 737 737222 1384473 NM NR 1 LE SLAT CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - LEADING EDGE FSS 594, NR 1 SLAT OUTBOARD MAIN TRACK, RIB CRACKED. DEFECT SIZE, LENGTH .0125 INCH. REPLACED RIB A T FSS 594 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999022600665 19990226 00665 NM 1999 2 26 P2EA99024 1 19990106 A 5320 SPLICE BOEING 737 737222 1384473 NM BS 538-550 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - STRINGER 10 LEFT SPLICE CRACKED AT BS 544, DEFECT SIZE, LENGTH .50 INCH. REPAIRED STRINGER 10 LEFT SPLICE BETWEEN BS 538 TO BS 550 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999022600666 19990226 00666 NM 1999 2 26 P2EA99023 1 19990106 A 5320 SPLICE BOEING 737 737222 1384473 NM BS 420-440 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - STRINGER 27 LEFT SPLICE CRACKED FROM BS 420 TO BS 440, DEFECT SIZE, LENGTH .312. REPAIRED STRINGER 27 LEFT FROM B S 420 TO BS 442 PER SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 1999022600667 19990226 00667 NM 1999 2 26 P2EA99022 1 19990114 A 5330 DOUBLER BOEING 737 737222 1384473 NM BS 951-986 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 951 TO BS 986.5, BETWEEN STRINGER 6 RT AND STRINGER 8 RT. DEFECT SIZE, LENGTH 34 INCHES, WIDTH 12 INCHES. REPAIRED INTERNAL DOUBLER BETWEEN BS 951 AND BS 986.5, BETWEEN STRINGER 6 RT AND STRINGER 8 RT PER SRM 53-30-3, FIG 17. (M) 2 L 7 2 4F A16WE 1999022600668 19990226 00668 NM 1999 2 26 P2EA99021 1 19990106 A 7110 COWL BOEING 737 737222 1384473 NM NR 2 ENGINE WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - NR 2 ENGINE NOSE COWL REAR MATTING SURFACE AT THE 6 O'CLOCK POSITION WORN. DEFECT SIZE, LENGTH 6 INCHES. NR 2 EN GINE NOSE COWL, REAR MATTING SURFACE FROM 5 O'CLOCK TO 7 O'CLOCK POSITION, STRAP REPAIRED PER SRM 54-10-3, FIG 4, SHEET 1, 2. (M) 2 L 7 2 4F A16WE 1999022600669 19990226 00669 NM 1999 2 26 P2EA99020 1 19990114 A 5320 DOUBLER BOEING 737 737222 1384473 NM BS 951-986 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - INTERNAL DOUBLER DISBONDED FROM BS 951-986.5, BETWEEN STRINGER 6 LEFT AND STRINGER 8 LEFT. DEFECT SIZE, LENGTH 34 INCH, WIDTH 12 INCH. REPAIRED INTERNAL DOUBLER FROM 951 TO BS 986.5, BETWEEN STRINGER LEFT AND STRINGER 8 LEFT PER SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1999022600670 19990226 00670 NM 1999 2 26 P2EA99019 1 19990112 A 5330 SKIN BOEING 737 737247 138448D NM BS 239 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - FUSELAGE SKIN CRACKED AT BS 239, WL 222 AND WL 227. DEFECT SIZE 1 INCH. REPAIRED FUSELAGE SKIN SECTION BETWEEN B S 228 AND BS 255, FROM WL 204 TO WL 229.5 PER SERVICE BULLETIN 737-53-1111, SEC III, PART II, REV 1 DATED APRIL 15, 1993 . ALSO, PER BOEING DRAWING 65C33596. APPROVED AND SUBMITTED BY BOEING FAX COO-SJO-99-0029RR DATED 1-14-99. (M) 2 L 7 2 4F A16WE 1999022600671 19990226 00671 NM 1999 2 26 P2EA99018 1 19990106 A 5330 SKIN BOEING 737 737222 1384473 NM BS 749-979 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - AFT RT SERVICE DOOR, LOWER FORWARD CORNER CRACKED. DEFECT SIZE, LENGTH .375 INCH. REPAIRED AFT GALLEY SERVICE DO OR FORWARD CUTOUT BETWEEN BS 749 TO BS 979 AND STRINGER 16 TO STRINGER 20 RT PER SRM 53-30-3, FIG 24. (M) 2 L 7 2 4F A16WE 1999022600672 19990226 00672 NM 1999 2 26 P2EA99017 1 19990112 A 5330 SKIN BOEING 737 737247 138448D NM BS 286-291 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - FORWARD SERVICE DOORWAY UPPER HINGE CUTOUT SKIN CRACKED. DEFECT SIZE, LENGTH .050 INCH. REPAIRED FUSELAGE SKIN S ECTION BETWEEN BS 291 AND BS 286, FROM STRINGER 9 RT TO STRINGER 12 RT PER 53-30-3, FIG 20. (M) 2 L 7 2 4F A16WE 1999022600674 19990226 00674 NM 1999 2 26 P2EA99015 1 19990109 A 5320 ANGLE BOEING 737 737247 138448D NM BS 664 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - ANGLE CRACKED AT BS 664, LBL 64, WL 194. DEFECT SIZE, LENGTH 3 INCH. PERFORMED STRINGER 18A SHEAR BEAM TO BS 664 FRAME ATTACHMENT MODIFICATION LEFT SIDE ONLY PER SERVICE BULLETIN 737-53-1056, SEC III, FIG 1 DATED 12-15-78. (M) 2 L 7 2 4F A16WE 1999022600680 19990226 00680 NM 1999 2 26 USAASB99013 1 19990114 A 3260 BACC45PT18A14P CONNECTOR BOEING 737 737401 1384701 NM LANDING GEAR FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 412US 23881 PHL - FLT 867 - AFTER TAKEOFF, CREW COULD NTO RETRACT THE LANDING GEAR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITH OUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND A WIRE PULLED LOOSE FROM THE AIR/GROUND SENSING SYS TEM ELECTRICAL CONNECTOR. REMOVED AND REPLACED ELECTRICAL CONNECTOR D4574P AND S105 AIR/GROUND SENSING PROXIMITY SENSOR AT THE GROUND SPOILER BYPASS VALVE IN THE RIGHT MAIN LANDING GEAR WHEELWELL PER MM 32-09-01. OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4F RT A16WE 1999022600681 19990226 00681 WP 1999 2 26 99ZZZM150 1 19990106 A 2130 CLAMP LKHEED 1011 10113851 5265010 WP ECS BAY LOOSE A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 826CR 193A1141 AT FLT LEVEL 28,000 FT, THE FLIGHT CREW HEARD A LOUD NOISE FOLLOWED BY THE CABIN VSI INDICATING A 1000 FT CLIMB. THE AI RCRAFT THEN DESCENDED TO 12,000 T. AT THAT POINT THE DECISION WAS MADE TO DIVERT TO SAN JUAN, PUERTO RICO TO INVESTIGAT E THE PROBLEM. FOUND THE NR 3 WATER SEPARATOR RUBBER BOOT CLAMP LOOSE. RECLAMPED BOOT AND ACCOMPLISHED PRESSURIZATION TEST AND LEAK CHECK IAW 21-31-00. (M) 2 L 7 3 4F A23WE 1999022600682 19990226 00682 WP 1999 2 26 99ZZZM151 1 19990105 A 2130 CLAMP HAMSTD LKHEED 1011 10113851 5265010 WP NR 3 ACM LOOSE A WRNA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 826CR 193A1141 CABIN PRESS FAULT LEGEND, CABIN ALT CLIMBING WITH BOTH OUTFLOW VALVES CLOSED. WHEN LEVELING FLT 350, CABIN PRESS WARNIN G HORN CAME ON FOLLOWED BY CABIN PRESS FAULT LIGHT ON AND DIFF PRESS AT 5000 AND CABIN ALT AT 11.5 COULD NOT CONTROL IN STANDBY OR MNL MODE. NO AIRFLOW IN AIRCRAFT. FOUND CLAMP ON RUBBER BOOT LOOSE AT NR 3 PACK WATER SEPARATOR. REPOSITIO NED BOOT AND RESECURED CLAMP IAW 21-31-00. (M) 2 L 7 3 4F A23WE 1999022600683 19990226 00683 NM 1999 2 26 USAASB99014 1 19990115 A 2170 V1211 COALESCER BOEING 737 7372B7 1384560 NM CABIN DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 274US 22886 FWA - FLT 1177 - EN ROUTE FROM BWI TO ORD AT FL310, ONE OF THE FLIGHT ATTENDANTS ADVISED THE COCKPIT CREW THAT THERE WER E FUMES IN THE CABIN AND THE FUMES WERE IRRITATING THE PASSENGERS. AN EMERGENCY DECLARED AND FLT DIVERT TO FWA. THE FU MES DISSIPATED ON DESCENT WHEN THE CREW SHUT DOWN ONE OF THE PACKS. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GA TE. TWENTY-FOUR PASSENGERS COMPLAINED OF THROAT IRRITATION AND WERE SEEN BY PARAMEDICS. MAINTENANCE ACCOMPLISHED A VIS UAL INSPECTION OF THE RIGHT AND LEFT AIR CONDITIONING BAYS AND ASSOCIATED COMPONENTS. NO DEFECTS WERE NOTED. REMOVED A ND REPLACED THE RIGHT AND LEFT WATER SEPARATOR BAGS PER MM 21-51-41. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999022600684 19990226 00684 NM 1999 2 26 USAASB99018 1 19990123 A 2612 FIRE LIGHT BOEING 737 7372B7 1384560 NM APU ILLUMINATED A USAA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 EA 19 269AU 22881 ILM - FLT 439 - ON DESCENT INTO ILM, THE CREW REPORTED THAT THE APU FIRE WARNIG LIGHT ILLUMINATD WITH THE APU ON MEL AND SHUTDOWN. THE APU IS SCHEDULED FOR REPLACEMENT DUE TO PERFORMANCE. CAPTAIN STATED THAT THE FLIGHT WAS AT 12,000 FEET WHEN THE FIRE WARNING LIGHT ILLUMINATED SO HE ELECTED TO DISCHARGE THE APU FIRE BOTTLE. THE LIGHT AND BELL REMAINED ON. FLIGHT LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED APU AND TAILPIPE ASSEMBLY. NO EVID ENCE OF FIRE WAS NOTED. REMOVED AND REPLACED FIRE BOTTLE AND RELEASED PER MEL 26-8. THE APU WAS LATER REPLACED AND RUN TO FULL AIR/ELECTRICAL LOAD. NO FAULTS WERE NOTED WITH THE FIRE WARNING SYSTEM. OPS CHECKED GOOD. MEL REMOVED. (M) 2 L 7 2 4F A16WE 1999022600685 19990226 00685 WP 1999 2 26 USAA990052 1 19990121 A 5320 3924814501 SPLICE DOUG DC9 DC931 3022065 WP BS 229 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 981VJ 41229 48157 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 4 INCHES OF CORROSION WITH CRACK IN SPLICE .5 INCH LONG AT LONGERON 23R FORW ARD OF STATION 229 PRODUCTION SPLICE AND SPLICE CRACKED OVER CORROSION. INSTALLED SPLICE REPAIR PER EA 51369. (M) 2 L 7 2 4F A6WE 1999022600686 19990226 00686 WP 1999 2 26 USAA990053 1 19990122 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 180 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 980VJ 48156 PIT - DURING C-6 CHECK, FOUND LEFT SIDE STATION 180, .1875 INCH LONG CRACK AT 4TH RIVET FORWARD STATION 180 RIVET LINE A T LONGERON 22 LEFT ON SKIN. INSTALLED EXTERNAL DOUBLER PER DOUGLAS DRAWING SR09530219 CLASS 1, 7001 AND EA 51344. (M) 2 L 7 2 4F A6WE 1999022600687 19990226 00687 EU 1999 2 26 USAA990051 1 19990114 A 5315 D20480001 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU BS 4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 854US 21601 11282 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CORROSION ON FLOORBEAM AT 1127R FROM STATION 4610 TO SPLICE AFT OF 5805. DO UBLERS WERE INSTALLED UNDER FLOORBEAM TO REPAIR OVERSIZE HOLES IN FLOORBEAM WEB PER EA NR 51337. (M) 2 L 7 2 4F RT 1999022600688 19990226 00688 NM 1999 2 26 USAA990006 1 19990103 A 5230 6546921523M WEB BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 44153 22754 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK IN LOWER INTERNAL WEB FORWARD END OF FORWARD CARGO DOO R. INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1999022600689 19990226 00689 NM 1999 2 26 USAA990039 1 19990114 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 47840 22352 CLT - DURING PCI CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON FUSE SKIN STATION 727 BELOW STRINGER 17R. INSTALLED D OUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999022600690 19990226 00690 NM 1999 2 26 USAA990007 1 19990112 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 44588 22752 CLT - DURING HM DROP INVISUAL INSPECTION, FOUND A 1 INCH CRACK STRINGER 18R 2 INCH AFT OF BS 727A SKIN. INSTALLED DOUBL ER PER SRM 53-30-3 FIG 6 AND EA 63480. (M) 2 L 7 2 4F A16WE 1999022600691 19990226 00691 NM 1999 2 26 USAA990008 1 19990112 A 5330 SKIN BOEING 737 737201 1384454 NM BS 793 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 44588 22752 CLT - DURING HM DROP IN VISUAL INSPECTION, FOUND A 2 INCH CRACK STRINGER 16L BS 793 SKIN. INSTALLED DOUBLER PER SRM 53- 30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999022600692 19990226 00692 EU 1999 2 26 99ZZZM152 1 19990102 A 3230 VALVE STBROS SD3 SD360 8100606 EU LANDING GEAR OUT OF POSITION A TY7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 350TA SH3757 TAKEOFF GEAR FAIL TO RETRACT EMERGENCY HANDLE APPEARED TO BE SLIGHTLY OUT OF POSITION 3 GREEN LIGHTS CONFIRMED GEAR DOWN AND LOCKED, LANDED FOR VERIFICATION CORRECTIVE ACTION. RESET LANDING GEAR EXTENSION HANDLE PER MM 32-30-00, VISUALLY V ERIFIED POSITION OF 3 WAY VALVE AT RIGHT ST-6 WING TEST FLIGHT A/C LANDING GEAR SYSTEM OPERATES NORMAL. (M) 2 H 7 2 4T A41EU 1999022600693 19990226 00693 NM 1999 2 26 99ZZZM153 1 19990114 A 2150 BACC45FT10C5S CONNECTOR BOEING 737 737291 138448W NM RT A/C BAY CORRODED A USVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 7375F P1682 20363 AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF OTU OF PIE, AIRCRAFT RETURNED TO PIE AND LANDED WITHOUT INCIDENT. CLEANED C ONNECTOR AT AIR CONDITIONER PACK VALVE AND OVERTEMP SWITCHES AND CONTROL PANEL, RIGHT PACK NORMAL AIRCRAFT PRESSURIZED O N THE GROUND OK PER MM 21-31-00 PLACARD REMOVED DMI CLEARED, AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999022600694 19990226 00694 NM 1999 2 26 P2EA99002 1 19990112 A 5210 69374185 ROLLER BOEING 737 737244 138448U NM L1 DOOR BROKEN A P2EA K NONE O OTHER CL CLIMB 1 CE 05 620PC 19708 MDW - FLT 560 - DURING CLIMB-OUT OF MCI, THE L-1 DOOR SEAL DID NOT SEAT PROPERLY ALLOWING LOUD WIND NOISE. AFTER SEVERA L MOMENTS THE SEAL DID SET CORRECTLY, PRESSURE WAS THEN NORMAL. FIVE MINUTES LATER, LOUD POP AT DOOR, NO PRESSURE PROBL EMS RESULTED FROM THIS NOISE. NOTIFIED MAINTENANCE CONTROL EN ROUTE TO MDW. FOUND AFT UPPER LATCH ROLLER ASSY BROKEN. REPLACED LATCH ROLLER ASSY PER MM 52-11-0. OPS CHECK NORMAL PER MM 52-11-0. (M) 2 L 7 2 4F A16WE 1999022600695 19990226 00695 NM 1999 2 26 P2EA99001 1 19990107 A 4950 10948661 VALVE BOEING 737 737281 138448P NM APU FAILED A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 219US 5019 20414 MSP - FLT 404 - DURAL BLEED INDICATION DURING TAKEOFF. ABORTED TAKEOFF AT 70 KNOTS, RETURNED TO GATE. DEFERRED PER MEL 36-6, CI M219725 ASSIGNED. FEF CI M219725. DUAL BLEED INDICATION INOPERATIVE. REPLACED APU LOAD CONTROL VALVE PER MM 49-52-11A, CLEARED CI M219725. (M) 2 L 7 2 4F A16WE 1999022600696 19990226 00696 NM 1999 2 26 P2EA99004 1 19990115 A 5101 STRUCTURE BOEING 737 737222 1384473 NM AIRFRAME VIBRATION A P2EA O OTHER E VIBRATION/BUFFET CR CRUISE 1 CE 05 208AU 19547 MDW - FLT 701 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. DURING CRUISE, FELT VIBRATION. CABIN PRESSURE BEGAN TO CLIM B 1500 FPM. BEGAN DESCENT AND SWAPPED TO STANDBY PRESS AT FL 180, CABIN PRESSURE STABILIZED. COMPLETED CABIN PRESS CHE CK. CHECKED AUTO PRESSURE CONTROLLER, INSPECTED ALL EXTERNAL DOORS FOR LEAKS, CHECKED WHEEL WELL FLOOR PANELS. CHECKED OUTFLOW VALVES, AIR CYCLE MACHINES AND PACK AREAS. NO LEAK FOUND, NO VIBRATION EXPERIENCED. (M) 2 L 7 2 4F A16WE 1999022600697 19990226 00697 WP 1999 2 26 USAAD99011 1 19990118 A 2170 1718566 HOSE DOUG DC9 DC931 3022065 WP WATER SEPARATOR RUPTURED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 933VJ 47216 EWR-PIT - FLT 537 - DURING CLIMB-OUT, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW OF A LOUD BANG AND THE SOUND OF AIR RUSHING. THE CAPTAIN NOTICED THERE WAS ONLY A 4 PSI CABIN PRESSURE DIFFERENTIAL AND THE CABIN ALTITUDE WAS CLIMBING AT 1100 FT PER MIN. THE AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLEX HOSE AT THE R IGHT WATER SEPARATOR. (M) 2 L 7 2 4F A6WE 1999022600698 19990226 00698 EU 1999 2 26 SIMA990095 1 19990109 A 3350 7239050 PANEL SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 350CF 2261992 340B350 LAX - FLT 3227 - FLIGHT ATTENDANT PANEL EMERGENCY ARM LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED COCKPIT EMERGENCY ARM SWITCH PANE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999022600699 19990226 00699 WP 1999 2 26 HALA9900024 1 19990114 A 2830 DUMP VALVE DOUG DC10 DC1010 3022110 WP LEFT MALFUNCTIONED A HALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 162AA 46943 LAX - FLT 9 - AFTER TAKEOFF AFTER GEAR RETRACTION STRONG VIBRATION FROM NOSE GEAR AREA. EXTENDED GEAR AND DUMPED FUEL. WHEN DUMPING FUEL ONLY RT DUMP VALVE OPENED, CHECKED CBS AND THEY WERE OK. AIRCRAFT RETURNED TO LAX, WHERE AN UNEVENTF UL LANDING WAS MADE. (M) 2 L 7 3 4F A22WE 1999022600700 19990226 00700 NM 1999 2 26 GAIA9906 1 19990120 A 3260 656021132 ACCESSORY UNIT BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE E/E BAY MALFUNCTIONED A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 855AA 20996 UPON APPROACH TO TOL, DURING GEAR EXTENSION, THE RIGHT MAIN LANDING GEAR INDICATED UNSAFE. THE SECONDARY INDICATORS DID INDICATE DOWN AND LOCKED. THE AIRCRAFT LANDED AT TOL WITHOUT FURTHER DIFFICULTY. REMOVED AND REPLACED THE MLG ACCESSO RY UNIT IAW MM. OPERATIONALLY CHECKS GOOD ON GROUND AND NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 L 7 3 4F 4 F A3WE E2EA 1999022600702 19990226 00702 NM 1999 2 26 99ZZZM155 1 19990114 A 3260 189929 SENSOR BOEING 737 737401 1384701 NM LANDING GEAR FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 412US 23881 PHL - FLT 867 - AFTER TAKEOFF, CREW COULD NTO RETRACT THE LANDING GEAR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITH OUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND A WIRE PULLED LOOSE FROM THE AIR/GROUND SENSING SYS TEM ELECTRICAL CONNECTOR. REMOVED AND REPLACED ELECTRICAL CONNECTOR D4574P AND S105 AIR/GROUND SENSING PROXIMITY SENSOR AT THE GROUND SPOILER BYPASS VALVE IN THE RIGHT MAIN LANDING GEAR WHEELWELL PER MM 32-09-01. OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4F RT A16WE 1999022600703 19990226 00703 NM 1999 2 26 TWRA9902 1 19990107 A 2612 MS24266R12 CONNECTOR BOEING 747 747212B 1384886 NM CARGO COMPT BROKEN A TWRA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 EA 15 620FF 21162 FLT 51 - SFO-JFK - AFT CARGO FIRE WARNING CAME ON DURING DESCENT, FOLLOWED EMERGENCY CHECKLIST, DISCHARGED NR 1 FIRE BOT TLE. LOWER CARGO FIRE BOTTLE NR 2 PUSHBUTTON WOULD NOT PUSH IN TO DISCHARGE THE FIRE BOTTLE. ON INSPECTION, FOUND BULK CARGO COMPT SMOKE DETECTOR CANNON PLUG BACK SHEEL BROKEN WITH TWO BROKEN WIRES. REPAIRED BROKEN WIRES AND REMOVED AND REPLACED BACKSHELL NR 6 SMOKE DETECTOR AND PLUG. REMOVED AND REPLACED ALL AFT CARGO COMPARTMENT SMOKE DETECTORS AND AMP S PRECAUTIONARY. REMOVED AND REPLACED NR 1 CARGO FIRE BOTTLE PER MM 26-23-01. SQUIB OPS CHECK OK PER MM 26-23-02. (M) 2 L 7 4 4F A20WE 1999022600704 19990226 00704 NM 1999 2 26 TWRA9901 1 19990107 A 2620 332632102001 SWITCH KORRY BOEING 747 747212B 1384886 NM FE PANEL FAILED A TWRA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 EA 15 620FF 21162 FLT 51 - SFO-JFK - AFT CARGO FIRE WARNING CAME ON DURING DESCENT, FOLLOWED EMERGENCY CHECKLIST, DISCHARGED NR 1 FIRE BOT TLE. LOWER CARGO FIRE BOTTLE NR 2 PUSHBUTTON WOULD NOT PUSH IN TO DISCHARGE THE FIRE BOTTLE. REMOVED AND REPLACED LOWE R CARGO FIRE PROTECTION MODULE DUE NR 2 FIRE BOTTLE PUSH BUTTON WOULD NOT PUSH IN PER MM 26-23-01. OPS CHECK OK PER MM 26-23-00, PAGE 501. (M) 2 L 7 4 4F A20WE 1999022600705 19990226 00705 EU 1999 2 26 USAAF99003 1 19990111 A 3234 D43229415 SELECTOR PANEL FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 891US 12894 11366 CLT - FLT 1492 - WHILE CLIMBING OUT FROM CLT, THERE WAS A VERY LOUD CLICKING NOISE COMING FROM BEHIND THE INSTRUMENT PAN EL. A FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY LIGHTS WERE FLASHING IN THE CABIN. AFTER 10 MINUTES THE PROBLEM SEE MED TO GO AWAY. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELE CTOR PANEL. (M) 2 L 7 2 4F RT 1999022600706 19990226 00706 EU 1999 2 26 USAAF99004 1 19990114 A 5230 569CL GAS SPRING FOKKER F28 F28MK0100 4990807 EU CARGO DOOR WEAK A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 852US 11280 CLT - FLT 2234 - AFTER TAKEOFF FROM CLT, A FORWARD CARGO DOOR WARNING MESSAGE ILLUMINATED. THE FLIGHT RETURNED TO CLT A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD AND AFT CARGO DOOR PRESSURE RELIEF DOOR STRUTS. ( M) 2 L 7 2 4F RT 1999022600707 19990226 00707 EU 1999 2 26 USAAF99005 1 19990117 A 7931 1130PGCP115 SWITCH FOKKER F28 F28MK0100 4990807 EU LT ENGINE MALFUNCTIONED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 19 859US 11293 PIT - FLT 1534 - AFTER TAKEOFF FROM PIT, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. THE LEFT ENGINE OIL PRESSURE INDICA TOR DROPPED TO ZERO AND THE FLIGHT CREW SHUT DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHE R INCIDENT. SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION. REPLACED THE LEFT ENGINE LOW OIL PRESSURE SWITCH AND THE LEFT OIL PRESSURE TRANSMITTER. (M) 2 L 7 2 4F RT 1999022600708 19990226 00708 EU 1999 2 26 99ZZZM156 1 19990117 A 7931 APTE173RT175G TRANSMITTER FOKKER F28 F28MK0100 4990807 EU LT ENGINE MALFUNCTIONED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 19 859US 11293 PIT - FLT 1534 - AFTER TAKEOFF FROM PIT, THE AIRCRAFT SUSTAINED A LIGHTNING STRIKE. THE LEFT ENGINE OIL PRESSURE INDICA TOR DROPPED TO ZERO AND THE FLIGHT CREW SHUT DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHE R INCIDENT. SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION. REPLACED THE LEFT ENGINE LOW OIL PRESSURE SWITCH AND THE LEFT OIL PRESSURE TRANSMITTER. (M) 2 L 7 2 4F RT 1999022600709 19990226 00709 SO 1999 2 26 C2XA99CL001 1 19990108 A 3610 38E966A REGULATOR EMB 120 EMB120RT SO RT ENGINE FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17728 20272 CI99551 120182 CLE - FLT 3063 - CREW REPORTED THAT WHILE CLIMBING THROUGH 10,000 FT THE RIGHT ENGINE DUCT LEAK LIGHT CAME ON, IT WOULD NOT GO OUT IN 3 MINUTES SO THE ENGINE WAS SHUT DOWN AND THEN THE LIGHT DID EXTINGUISH. AIRCRAFT RETURNED TO THE FIELD W ITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT BLEED SYSTEM PRESSURE REGULATOR IAW EMB120 MM 30-10 -06. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600713 19990226 00713 SW 1999 2 26 SIMA990092 1 19990109 A 3830 7253680117 PANEL SWRNGN SA227 SA227AC 8780603 SW FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 358AE AC688 ABI - EXCESSIVE CORROSION ON THE LAVATORY SERVICING PANEL. REMOVED AND REPLACED THE LAVATORY SERVICING PORT. (M) 2 L 7 2 4T RT A8SW 1999022600716 19990226 00716 SO 1999 2 26 C2XA99IA046 1 19990106 A 3231 12044443001 STRIKER EMB 120 EMB120RT SO LT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURNG C-CHECK INSPECTION, FOUND LEFT GEAR WELL AFT DOOR STRIKER PLATE CRACKED OUT. REMOVED AND REPLACED STRIKER PLATE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600717 19990226 00717 SO 1999 2 26 C2XA99IA033 1 19990106 A 5230 12036974601 ROLLER GUIDE EMB 120 EMB120RT SO CARGO DOOR BENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND CARGO DOOR BOTTOM FORWARD RAMP AND UNDER STRUCTURE BENT. REMOVED AND REPLACED ROLLER G UIDE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600718 19990226 00718 SO 1999 2 26 C2XA99IA023 1 19990106 A 7110 12025601625 DOOR EMB 120 EMB120RT SO RT COWLING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16724 120171 DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE COWL DOOR 423 CRACKED AT LOWER END OF DOOR NEAR CENTER. WELDED CRACKED SE CTION. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999022600719 19990226 00719 NE 1999 2 26 MASA99012 2 19990120 A 7261 310047001 TUBE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 1 ENGINE CRACKED A MASA A E UNSCHED LANDING ENGINE SHUTDOWN J K Y WARNING INDICATION FLUID LOSS ENGINE STOPPAGE CL CLIMB 1 SW 07 127ZV UE127 114289 FLT 5409 - BOS-BGR - AFTER TAKEOFF, CAPTAIN NOTED THE NR 1 ENGINE OIL PSI WAS DECREASING. THE CAPTAIN SHUT DOWN THE NR 1 ENGINE AS A PRECAUTIONARY MEASURE. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL TRANSFER TUBE ELBOW. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999022600720 19990226 00720 SO 1999 2 26 RAIA990117 1 19990115 A 2424 51515001B GCU EMB 145 EMB145 SO NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 CE 03 802HK 145066 FLT 5776 - ORD - NR 1 GENERATOR FELL OFF LINE. MAINTENANCE REPLACED NR 1 GENERATOR CONTROL UNIT. (M) 2 L 7 2 4F RT T00011AT 1999022600721 19990226 00721 EU 1999 2 26 RAIA990125 1 19990119 A 3010 30350261 VALVE BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 862JX 862 FLT 4724 - FAT - WING AND TAIL DE-ICE INOPERATIVE. MAINTENANCE REPLACED LEFT EJECTOR FLOW CONTROL VALVE. (M) 2 L 7 2 4T RT A56EU 1999022600722 19990226 00722 1999 2 26 RAIA990124 4 19990119 A 3418 C850176 STALL VANE JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 571HK 41090 FLT 7714 - JFK - LEFT STALL CAP ILLUMINATED. MAINTENANCE REPLACED LEFT STALL VANE. (M) 2 L 7 2 4T RT A41NM 1999022600723 19990226 00723 WP 1999 2 26 RAIA990123 2 19990119 A 7261 86504612 SCAVENGE PUMP BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 971JX 1298 971 66372 FLT 4718 - SMF - LEFT ENGINE OIL TEMP HIGH. MAINTENANCE REPLACED AFT SCAVENGE PUMP. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999022600724 19990226 00724 EU 1999 2 26 RAIA990122 1 19990119 A 3260 622800200 SWITCH BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 864AE 864 FLT 4746 - FAT - LEFT MAIN GEAR INTRANSIT LIGHT STAYED ON AFTER GEAR RETRACTION. MAINTENANCE REPLACED LEFT MAIN GEAR UP LOCK SWITCH. (M) 2 L 7 2 4T RT A56EU 1999022600725 19990226 00725 EU 1999 2 26 RAIA990121 1 19990119 A 7170 S7171200200200 DRAIN MAST AEROSP ATR72 ATR72202 8680940 EU RT ENGINE CLOGGED A RAIA E ENGINE SHUTDOWN A FLAME/FIRE LD LANDING 1 CE 03 723TE 283 FLT 7163 - MLI - NR 2 ENGINE FIRE INDICATION ILLUMINATED. MAINTENANCE REPLACED LEAKING FUEL NOZZLES AND UNCLOGGED FUEL DRAIN MAST. (M) 2 H 7 2 4T RT A53EU 1999022600726 19990226 00726 WP 1999 2 26 TWAA9902901 1 19990223 A 2120 AIR DIST DOUG DC9 DC982 3022082 WP CABIN SMOKE A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 953U 49267 SMOKE WAS REPORTED IN CABIN AFTER AIR FOIL ANTI-ICE WAS TURNED ON. SUSPECT DEICER FLUID. COMPLETED PACK BURN OUT. CHE CK-C 3-25-98 MCI. 2 L 7 2 4F A6WE 1999022600727 19990226 00727 WP 1999 2 26 TWAA9902902 1 19990218 A 5240 991158221 BEAM DOUG DC9 DC982 3022082 WP R1 DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 919TW 49368 FOUND THE FORWARD RIGHT CABIN DOOR HAD THE BOTTOM DOOR BEAM CRACKED. INSTALLED NEW DOOR BEAM PER SRM 51-30-2. CHECK-C 8-27-98 STL. 2 L 7 2 4F A6WE 1999022600728 19990226 00728 NM 1999 2 26 HNAA9900026 1 19990214 A 2161 754890 CONTROLLER DHAV DHC8 DHC8201 2809001 NM CABIN INOPERATIVE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 988HA 426 LAVATORY SMOKE DETECTOR WENT OFF SEVERAL TIMES WITH APU BLEED ON, NOTICEABLE SMOKE. REPLACED CABIN TEMPERATURE CONTROLL ER. AFTER RUNNING APU WITH BLEED ON, SHOWED NO EVIDENCE OF SMOKE. 2 H 7 2 4T RT A13NM 1999022600729 19990226 00729 NM 1999 2 26 HNAA9900027 1 19990212 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN CHAFED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 928HA 120 FORWARD CABIN EMERGENCY EXIT SIGNS INOPERATIVE. FOUND AFTER CHANGING EMERGENCY BATTERIES FOR SCHEDULED MAINTENANCE. RE PAIRED CHAFED WIRES AND REPLACED DIODE AT RIGHT HAND CABIN SIDE WALL, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999022600730 19990226 00730 NM 1999 2 26 HNAA9900028 1 19990223 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 984HA 377 NUMEROUS INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED 3351-PS2 POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999022600731 19990226 00731 EU 1999 2 26 MALA976355 1 19990216 A 3020 CONTROLLER SAAB SF340 340B 7860101 EU RT ENG DEICE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 417XJ 340B417 AFTER SELECTING ENG ICE, RT INTAKE LIGHT ILLUMINATED. QRH TO NO EFFECT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACE D DEICE CONTROLLER RT ENG, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999022600732 19990226 00732 1999 2 26 MALA976357 4 19990217 A 3425 6226190113 COMPUTER SAAB SF340 340B 7860101 EU NR 1 AHRS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 453XJ 453 DURING CLIMB, CAPT SIDE EHSI HAD A RED HDG FLAG. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED NR 1 AHRS COMPUTER, AL L CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999022600733 19990226 00733 EU 1999 2 26 MALA976358 1 19990201 A 3233 AIR864101 ACTUATOR SAAB SF340 SF340A 7850100 EU LT MLG FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 107XJ 340A107 AFTER GEAR EXTENSION, HYDRAULIC PRESSURE DECREASED TO ZERO. MAINTENANCE REPLACED LT MLG ACTUATOR, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999022600734 19990226 00734 NM 1999 2 26 AWXA9900045 1 19990219 A 5330 SKIN BOEING 737 7372M8 1384483 NM BS 727-747 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 DURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK AT STRINGER 19 RT SIDE AT BS 727 TO 747. REPAIRED PER ER 2-53-34-08 STEP 8, NEED TO REPLACE SKIN OR REPAIR WITH SRM APPROVED REPAIR WITHIN 24 MONTHS NOT TO EXCEED 6000 FLIGHT HO URS. 2 L 7 2 4F A16WE 1999022600735 19990226 00735 NM 1999 2 26 AWXA9900046 1 19990219 A 5330 SKIN BOEING 737 7372M8 1384483 NM BS 747-767 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 DURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK BELOW STRINGER 16 RT SIDE, AFT OF WING TO BODY FAIRING FRO M STATION 747 TO 767. REPAIRED PER ER 2-53-34-09 STEP 7, REPLACE SKIN OR REPAIR WITH SRM APPROVED REPAIR WITHIN 24 MONT HS NOT TO EXCEED 6000 FLIGHT HOURS. 2 L 7 2 4F A16WE 1999022600736 19990226 00736 NM 1999 2 26 AWXA9900047 1 19990219 A 5330 SKIN BOEING 737 7372M8 1384483 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 DURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK LEFT SIDE AT STRINGER 17, BS 727, BELOW TEMP REPAIR FWD OF BS 747. INSTALLED REPAIR USING BLIND FASTENERS IAW FIG 1 SHEET 2 OF SRM 53-30-3, REPLACE BLIND FASTENERS AFTER 10,000 FLIGHT CYCLES WITH SOLID RIVETS. 2 L 7 2 4F A16WE 1999022600737 19990226 00737 NM 1999 2 26 AWXA9900051 1 19990202 A 5321 65C321027 BEAM BOEING 737 73733A 1384673 NM LT MLG MISDRILL A AWXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 28 168AW 23629 LT MLG SUPPORT BEAM LOWER CHORD DAMAGED BY DRILL WHILE REMOVAL OF PANEL LOWER WBL 109.895. HOLES CLEANED UP BY BLENDING AND REAMING AT NR 2 AND 3 FLAP PEEN AREA. INSTALLED RIVET SLUG BACR 1580. ALODINED AND PRIMED AREAS OF HOLES PER AWA ER 2-57-43-18. 2 L 7 2 4F RT A16WE 1999022600738 19990226 00738 NM 1999 2 26 AWXA9900052 1 19990208 A 5330 SKIN BOEING 737 737277 1384570 NM BS 780 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 DURING ROUTINE MAINTENANCE CHECK, FOUND SKIN CRACK AT APPROX STA 780 RT BETWEEN TWO PREVIOUS REPAIRS. REMOVED OLD SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW 53-10-2 FIG 4, SRM 51-40-6, SRM 51-30-04, SRM 51-30-02. 2 L 7 2 4F RT A16WE 1999022600739 19990226 00739 NM 1999 2 26 AWXA9900053 1 19990208 A 5313 BAC149813870 STRINGER BOEING 737 737277 1384570 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 CABIN AFT OF RT STA 500B STRINGER 16R IS CRACKED FWD OF LIGHT ASSY. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR SECTION STRINGER, SPLICE ANGLES, AND U-CHANNEL OUT OF 7075-T6 IAW SRM 53-10-3 FIG 1. ALODINE D, PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-3 FIG 1 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 1999022600740 19990226 00740 NM 1999 2 26 AWXA9900054 1 19990208 A 5313 BAC14981557075 STRINGER BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 CABIN FWD OF RT STA 520 STR 16R IS CRACKED AFT OF LIGHT ASSY. REMOVED STRINGER PER SRM 51-30-02, FABRICATED REPLACEMENT STRINGER FROM BAC 1498-1557075-T6 R 608816 PER 53-10-2 FIG 9. INSTALLED PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 1999022600741 19990226 00741 NM 1999 2 26 AWXA9900055 1 19990208 A 5313 BAC1498595270 STRINGER BOEING 737 737277 1384570 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 STRINGER 16L AT STA 500B HAS 2 CRACKS AROUND FASTENERS TL-70. CUT OUT DAMAGED SECTION PER SRM 53-10-3 FIG 1, FABRICATED AND INSTALLED NEW STRINGER U-CHANNEL, AND J-ANGLES PER 53-10-3 FIG 1, SRM 51-30-0. APPLIED ALODINE AND PRIMER PER SRM 51-10-3. 2 L 7 2 4F RT A16WE 1999022600742 19990226 00742 NM 1999 2 26 AWXA9900056 1 19990208 A 5313 BAC14981557075 STRINGER BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 STRINGER 16L AT STA 520 HAS 3 CRACKS AROUND FASTENERS. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 51-30-0, FABRICATED AND INSTALLED STRINGER IAW SRM 51-30-2 FIG 9 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 1999022600743 19990226 00743 NM 1999 2 26 AWXA9900057 1 19990208 A 5313 BAC1498156 STRINGER BOEING 737 737277 1384570 NM BS 867-907 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 STRINGER 18L UNDER FLOORBEAMS 887 TO 907 HAS A HOLE WORN IN IT BY LOOSE AV CONNECTOR. REMOVED AND REPLACED STRINGER SEC TION IAW SRM 53-10-3. REPAIR WAS INSTALLED FROM FS 867 TO 907, SPLICED IN AT STA 877. REPAIR PARTS, CHANNEL AND ANGLE MADE FROM 7075-T6. 2 L 7 2 4F RT A16WE 1999022600744 19990226 00744 NM 1999 2 26 AWXA9900058 1 19990208 A 5315 6545812213 FLOORBEAM BOEING 737 737277 1384570 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 FLOORBEAM AT STA 328 RBL 20 CORRODED OUT OF LIMITS. REMOVED DAMAGED CAP, FABRICATED AND INSTALLED REPLACEMENT CAP PER S RM 53-10-9, 51-10-2, 51-30-2. 2 L 7 2 4F RT A16WE 1999022600745 19990226 00745 NM 1999 2 26 AWXA9900059 1 19990208 A 5315 6545808241 FLOORBEAM BOEING 737 737277 1384570 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 FLOORBEAM AT STA 294.5 LBL 36 CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA PER SRM 53-10-9 FIG 1. FABRICATED T-CAP PE R SRM 53-10-9 FIG 1. INSTALLED PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 1999022600746 19990226 00746 NM 1999 2 26 AWXA9900060 1 19990208 A 5350 FITTING BOEING 737 737277 1384570 NM BS 663 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 TOP OF RIGHT WING FILLET AREA, STA 663 SPLICE FITTING HAS A HOLE/DRILL START WBL 71.24. REMOVED FASTENER ON FITTING, SP OT FACED HOLE TO REMOVE DAMAGE, SHOT PEENED PER BAC 5730, ALODINED AND PRIMED PER SRM 51-10-2 IAW AND ER 2-57-31-17. RE INSTALLED FASTENER IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 1999022600747 19990226 00747 NM 1999 2 26 AWXA9900061 1 19990208 A 5311 6546575518 FRAME BOEING 737 737277 1384570 NM BS 1138 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 BS 1138, WL 262, RBL 26.5 FORWARD SIDE OF FRAME, THE FRAME IS CRACKED IN THE RADIUS. REMOVED CRACKED ANGLE, FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-30-2, SRM 51-40-3, BAC 5602, SRM 51-40-3, SRM 51-10-2, AND SRM 55-10-6. 2 L 7 2 4F RT A16WE 1999022600748 19990226 00748 NM 1999 2 26 AWXA9900062 1 19990208 A 5313 BAC1498155 STRINGER BOEING 737 737277 1384570 NM BS 603 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 STRINGER 15R AT STA 603 CRACKED ON END APPROX .25 INCH LONG. BLENDED STRINGER END TO REMOVE CRACK, NDT INSP RADIUS BLEN DED AREA, ALODINED AND PRIMED. MAT LOSS .020 AND NO EFFECT TO FASTENER EDGE MARGINS, WORK DONE PER SRM 53-10-1 FIG 1, 5 1-10-2 AND HFEC INSP PER B737 NTM PT.6 51-00-00 FIG 23. 2 L 7 2 4F RT A16WE 1999022600749 19990226 00749 NM 1999 2 26 AWXA9900063 1 19990208 A 5320 69353521 CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 STRINGER CLIPS CRACKED. REMOVED AND REPLACED CLIPS PER EO 53-12-01. 2 L 7 2 4F RT A16WE 1999022600750 19990226 00750 WP 1999 2 26 9900609870 1 19990220 A 3230 PIN DOUG DC9 DC951 3022051 WP NLG INCORRECT PART A NWAA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 GL 01 779NC 48101 NOSE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. CREW RECYCLED GEAR WITH SAME RESULTS. FLIGHT WAS RETURNED TO VPS AND L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND IMPROPER LOWER NOSE GEAR TORQUE LINK HINGE PIN INSTALLED. REMOVED AND INSTAL LED CORRECT HINGE PIN. OPERATIONAL CHECK NORMAL ON SEVERAL GEAR CYCLES. 2 L 7 2 4F RT A6WE 1999022600751 19990226 00751 EU 1999 2 26 9900663212 1 19990216 A 2530 1238A GUARD AIRBUS 320 A320211 3930320 EU GALLEY OVEN MISSING A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 312US 152 DURING CLIMB, FLIGHT ATTENDANT REPORTED FIRE IN AFT GALLEY OVEN AND ECAM MESSAGE SMOKE LAVATORY SMOKE WAS RECEIVED. FIR E EXTINGUISHER WAS USED TO PUT OUT THE FIRE AND THE AIRCRAFT RETURNED TO ORIGINATING FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSTALLED MISSING GUARD IN OVEN, CHECKED OK. 2 L 7 2 4F RT A28NM 1999022600752 19990226 00752 NM 1999 2 26 UPS99228766 1 19990223 A 3350 BULB BOEING 727 72725C 138400H NM AFT AIRSTAIRS FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, AFT 3 AIRSTAIR EMER LIGHTS INOP. RELAMPED. 2 L 7 3 4F A3WE 1999022600753 19990226 00753 NM 1999 2 26 99FDEA00075 1 19990223 A 2121 FAN BOEING 727 72722 1384002 NM COCKKPIT FAILED A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 188FE 19081 LIGHT SMOKE FUMES IN COCKPIT WHICH DISAPPEARED WHEN GASPER FAN WAS TURNED OFF. REMOVED AND REPLACED GASPER FAN. 2 L 7 3 4F A3WE 1999022600754 19990226 00754 WP 1999 2 26 MWEA99075 1 19990222 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD PASSENGER DOOR SLIDE FELL OFF DOOR. MTC REINSTALLED DOOR SLIDE. 2 L 7 2 4F A6WE 1999022600755 19990226 00755 WP 1999 2 26 MWEA99076 1 19990224 A 2560 GIRT BAR DOUG DC9 DC982 3022082 WP SERVICE DOOR LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 810ME 48072 MXE - FLT 406 - THE FORWARD GALLEY SERVICE DOOR SLIDE GIR BAR IS DIFFICULT TO DISARM. MTC CLEANED AND LUBRICATED SPRING AND LATCH AND REINSTALLED DOOR SLIDE GIRT BAR. (X) 2 L 7 2 4F A6WE 1999022600756 19990226 00756 NM 1999 2 26 SCNA99042 1 19990222 A 3230 A42006028305 SOLENOID BOEING 727 727225 1384077 NM GEAR LEVER INTERMITTENT A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 282SC 22558 DURING CLIMBOUT, THE GEAR HANDLE WOULD NOT RETRACT PAST THE OFF POSITION. ALL OTHER INDICATIONS WERE NORMAL. ACTIVATIN G THE OVERRIDE TRIGGER WOULD RETRACT THE GEAR NORMALLY. FOUND GEAR LEVER SOLENOID TO BE INTERMITTENT. REMOVED AND REPL ACED THE SOLENOID. GEAR RETRACTION OPERATIONL CHECK GOOD PER MM 3209121. 2 L 7 3 4F A3WE 1999022600757 19990226 00757 NE 1999 2 26 SWIA971405 2 19990209 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT OVERTEMP A SWIA L A ABORTED APPROACH UNSCHED LANDING E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION AP APPROACH 1 NM 07 223SW 120291 ON APPROACH INTO JAC, ENCOUNTERED SEVERE TURBULENCE AND WINDSHEAR. MAXIMUM POWER WAS REQUIRED AND T6 EXCEEDED 900 DEG. AIRCRAFT NEEDS SEVERE TURBULENCE INSPECTION. DID NOT LAND IN JAC BUT RETURNED TO SLC. COMPLIED WITH SEVERE TURBULENCE INSPECTION WITH NO DEFECTS NOTED. REPLACED BOTH ENGINE ASSEMBLIES AND INSPECTED BOTH PROPS IAW MM 61-10-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600758 19990226 00758 SO 1999 2 26 SWIA971406 1 19990209 A 7712 311694201 TSCU EMB 120 EMB120RT SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 289YV 120289 DURING CLIMB, RIGHT ENGINE WENT INTO AUTOFEATHER AT 1000 FT AGL WITH TORQUE ABOUT 144 PERCENT. RETURNED TO LAX. REPLAC ED RIGHT ENGINE TORQUE PROBE AND RIGHT ENGINE TSCU. MM INSPECTION STEPS WERE PERFORMED FOR OVER TORQUE OF PROPELLER AND ENGINE ON RIGHT SIDE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600759 19990226 00759 SO 1999 2 26 SWIA971407 1 19990202 A 3230 VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 129AM 120119 WHEN GEAR HANDLE WAS RETRACTED ALL 12 LIGHTS (RED AND GREEN) ILLUMINATED, EXCEPT RED LEFT A CIRCUIT LIGHT. GEAR WOULD N OT RETRACT, COULD NOT DUPLICATE PROBLEM ON GROUND. ADJUSTED RIGHT MAIN GEAR DOOR SEQUENCE VALVES. REMOVED AND REPLACED GEAR SELECTOR FOR TROUBLESHOOTING, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600760 19990226 00760 SO 1999 2 26 SWIA971408 1 19990203 A 3231 12043270501 RELAY EMB 120 EMB120RT SO PWA 118 PW118A NE GEAR DOORS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 251YV 120251 GEAR DOORS STAY OPEN AFTER GEAR IS RETRACTED. RETURNED TO FAT. REPLACED RELAY BOX AND CANNON PLUG AT P1112. GROUND RU N NORMAL. ALSO, GEAR EXTENSION/RETRACTION NORMAL. REPLACED CONNECTOR AT P1112, OPS NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600761 19990226 00761 SO 1999 2 26 SWIA971409 1 19990204 A 2131 22201T011400 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 290SW 120317 AUTO PRESSURIZATION INOP. RETURNED TO PSP. REMOVED ELECTRO PNEUMATIC OUTFLOW VALVE, INSPECTED SHAFT FOR STRAIGHTNESS A ND OHMED TORQUE MOTOR. ALL CHECKED GOOD. REINSTALLED VALVE. OHMED AND MEGGED WIRING FROM CONTROLLER TO VALVE, CHECKS OK. REPLACED RELAY K0127 AND INSTALLED SERVICEABLE ELECTRONIC PRESSURIZATION CONTROLLER. PERFORMED TEST FLIGHT AND CHE CKS OK. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600762 19990226 00762 SO 1999 2 26 SWIA971410 1 19990204 A 2131 22201T011400 CONTROLLER EMB 120 EMB120RT SO PWA 118 PW118A NE CABIN MALFUNCTIONED A SWIA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 07 270YV 120270 CRUISE FLIGHT, FL210 WITH CABIN PRESSURE SET IN AUTO. CABIN RATE INDICATOR NEEDLE PEGGED ITSELF OFF THE SCALE IN A CLIM B UNTIL CABIN PRESSURE WAS 10,000 FT. AFTER SEVERAL CLIMBS/ DESCENT OSCILLATIONS AND EMERGENCY DESCENT INDICATED PROBLE M CORRECTED IN CONTROLLED DESCENT AT FL 180. INSPECTED PRESSURE SYSTEM, PRESSURIZED AIRCRAFT TO 7 PSI. SYSTEM CHECKS G OOD ON GROUND AT THIS TIME. REPLACED ELECTRIC CONTROLLER. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600763 19990226 00763 NE 1999 2 26 SWIA971411 2 19990206 A 7314 7863904 FUEL PUMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 193SW 120088 AFTER TAKEOFF LEFT ENGINE LOST POWER, RPM AND NP FOR MAYBE 5 SECONDS THEN RPM AND TQ SURGED FOR ABOUT 4 MORE SECONDS. R ETURNED TO SLC. REMOVED AND REPLACED LEFT ENGINE FUEL PUMP AND HMU IAW MM 73-21-00. OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600764 19990226 00764 EA 1999 2 26 SWIA971412 1 19990206 A 5610 WINDOW CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT COCKPIT FAILED A SWIA K NONE O OTHER CR CRUISE 1 NM 07 412SW 7101 RIGHT SIDE WINDOW SHATTERED IN FLIGHT. NO APPARENT CONTACT OR LOSS OF PRESSURE. NORMAL LANDING IN FAT. REMOVED AND RE PLACED RIGHT SIDE COCKPIT WINDOW IAW MM 56-12-01. 2 L 7 2 4F 4 F RT A21EA E15NE 1999022600765 19990226 00765 SO 1999 2 26 SWIA971413 1 19990206 A 3020 DEICE SYST EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE INLET MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 234SW 120308 LEFT ENGINE AIR INLET INOP LIGHT CAME ON AFTER DEPARTURE. CYCLED 3 TIMES, STILL REMAINED INOP. RETURNED TO SFO. RAN L EFT ENGINE DEICE FOR 15 MINUTES AND CHECKED GOOD. PUT PSI GAUGE AT SWITCH, PRESSURE CHECKS GOOD. SWAPPED PRESSURE SWIT CH'S FROM LEFT TO RIGHT AND RAN ENGINE. DEICE CHECKS GOOD. COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600766 19990226 00766 SO 1999 2 26 SWIA971414 1 19990207 A 5753 ROLLERS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT TE FLAPS WORN A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 AFTER DEPARTURE, FLAPS INCURRED DISAGREEMENT FROM FLAPS 15 TO FLAPS UP. INBOARD PAIR DISAGREEMENT. TRIED THREE TIMES T O FIX/RECONFIGURE, UNSUCCESSFUL. RETURNED TO SLC. LANDING CONFIGURATION (FLAPS 25) WORKED PROPERLY. REPLACED 2 ROLLER S ON LEFT AND RIGHT INBOARD FLAPS, LEFT INBOARD OUTBOARD FIXED TRACK AND RIGHT INBOARD FLAP OUTBOARD TRACK. GROUND CHEC K GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600767 19990226 00767 SO 1999 2 26 SWIA971415 1 19990208 A 3010 38E966A REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT DEICE SYST FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 234SW 120308 DURING CLIMBOUT, LOST THE RIGHT ENGINE INLET DEICER ALL OUTBOARD LEADING EDGE BOOTS AND THE LEFT MIDDLE WING BOOT, BOTH TIMERS. RETURNED TO FAT. REMOVED AND REPLACED LEFT PRESSURE VALVE REGULATOR, OPS CHECK GOOD. DEICE SYSTEM FUNCTIONED NORMALLY. 2 L 7 2 4T 4 T RT A31SO E20NE 1999022600768 19990226 00768 NM 1999 2 26 VNAA9902013 1 19990216 A 2150 DIN651672854 RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PACK FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 442JS 3060 AFTER THE AIRCRAFT DEPARTED THE GATE, A LEFT HAND AIR CONDITIONING PACK FAIL WARNING INDICATION, AND LAV SMOKE INDICATIO N ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND DEFERRED THE LEFT HAND GROUND COOLING FAN, IN ACCORDANCE WITH THE DORNIER MINIMUM EQUIPMENT LIST. THE LAV SMOKE INDICATION WAS DETERMINED TO BE CAUSED BY THE LEFT AIR CONDITIONING PACK GROUND COOLING FAN MALFUNCTION. THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. ON 25 FEB 99 MAINTE NANCE INSPECTED AND REPLACED RELAY 56HB, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-51-00. OPERATIONAL CHECKS WER E COMPLETED, AND THE DEFERRAL WAS REMOVED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999022600769 19990226 00769 NM 1999 2 26 VNAA9902016 1 19990222 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 438JS 19778 3056 A SECTION OF EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE DURING THE POST-FLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY PACK AT THE 5LK POSITION. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030400001 19990304 00001 NM 1999 3 4 P5CA9900182 1 19990129 A 5720 FAIRING BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER UK UNKNOWN 1 WP 23 854FT 19754 LEFT WING UPPER SURFACE INBOARD OF OUTBOARD AILERON TRAILING EDGE FIXED FAIRING FOUND DELAMINATED. REPAIRED PER SRM 51- 40-12. 2 L 7 4 4F A20WE 1999030500001 19990305 00001 NM 1999 3 5 SWAA990325 1 19990221 A 2781 693784111 ROD END BOEING 737 7373H4 1384600 NM NR 1 LE FLAP OUT OF POSITION A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 621SW 28037 LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED WITH FLAP HANDLE IN THE UP POSITION. NR 1 LE FLAP ANNUNCIATOR INDI CATED AMBER, NOT IN THE FULL UP POSITION. RECYCLED FLAPS FROM 1 DEG TO 0 WITH NO CHANGE. AIRCRAFT RETURNED TO SLC. RE MOVED AND REPLACED LT O/B KRUEGER FLAP POSITION INDICATION ARM-ROD END, OPS CK GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999030500002 19990305 00002 NM 1999 3 5 SWAA990326 1 19990221 A 5210 SEAL BOEING 737 7373Q8 1384670 NM PAX DOOR OUT OF POSITION A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 689SW 23387 FWD ENTRY DOOR DEVELOPED AN EXTREMELY LOUD AIR LEAK IN THE VICINITY OF UPPER HINGE. PRESSURIZATION REMAINED NORMAL. RE POSITIONED FWD ENTRY DOOR UPPER HINGE SEAL COVER (INTERIOR COVER) PER M/M, OPS CK'D OK. 2 L 7 2 4F RT A16WE 1999030500003 19990305 00003 NM 1999 3 5 SWAA990327 1 19990222 A 2130 720737 MODULE BOEING 737 7373H4 1384600 NM PRESSURE SYST INOP A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 307SW 22947 AFTER TAKEOFF, PRESSURIZATION SYSTEM FAILED. RETURNED TO BWI AND MADE AN UNVENTFUL LANDING. REMOVED AND REPLACED PRESS URIZATION CONTROL MODULE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999030500004 19990305 00004 1999 3 5 SWAA990328 4 19990222 A 2565 1061323468 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 FWD ENTRY DOOR SLIDE WILL NOT STAY SECURE. REMOVED AMD REPLACED FWD ENTRY DOOR SLIDE PER M/M, GROUND OPS CK'S NORMAL. 2 L 7 2 4F RT A16WE 1999030500005 19990305 00005 NM 1999 3 5 SWAA990329 1 19990222 A 5610 571761 WINDOW BOEING 737 7372H4 138448C NM LT COCKPIT SMOKING A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 67SW 22356 IN FLIGHT, L1 WINDOW HEAT CAUSED SMOKE FROM SEALANT COMPOUND AROUND WINDOW. AIRCRAFT DIVERTED TO DAL. REMOVED AND REPL ACED WINDOW PER MM, LEAK AND OPS CHECK OK. 2 L 7 2 4F A16WE 1999030500006 19990305 00006 NM 1999 3 5 SWAA990330 1 19990220 A 1100 PLACARD BOEING 737 7372H4 138448C NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 EMERGENCY EXIT PLACARD ABOVE EXTERIOR DOOR HANDLE ON FORWARD SERVICE DOOR WAS WEARING OFF. REPLACED PLACARD PER M/M. 2 L 7 2 4F A16WE 1999030500007 19990305 00007 NM 1999 3 5 SWAA990331 1 19990220 A 3350 612851 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SC CHECK, FOUND FWD SECTION TRACK LIGHTS INOP. REMOVED AND REPLACED FWD CHARGER PER MM, OPS CHECK GOOD . 2 L 7 2 4F RT A16WE 1999030500008 19990305 00008 NM 1999 3 5 SWAA990332 1 19990220 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5 AT LBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999030500009 19990305 00009 NM 1999 3 5 SWAA990333 1 19990220 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 13 AND 14L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999030500010 19990305 00010 NM 1999 3 5 SWAA990334 1 19990220 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND WEB CORROSION AT BS 986.5 AND AT 295-328. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999030500011 19990305 00011 NM 1999 3 5 SWAA990335 1 19990220 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 227 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 227, STRINGER 15R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999030500012 19990305 00012 NM 1999 3 5 SWAA990336 1 19990220 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 986, AT LBL 4.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999030500013 19990305 00013 NM 1999 3 5 SWAA990337 1 19990219 A 3350 1330122 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED SC CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM, CKS GOOD . 2 L 7 2 4F RT A16WE 1999030500014 19990305 00014 NM 1999 3 5 SWAA990338 1 19990221 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SC CHECK, FOUND EMERGENCY LIGHT AT ROW 22 LEFT SIDE INOP. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 1999030500015 19990305 00015 NM 1999 3 5 SWAA990339 1 19990221 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 367SW 26578 DURING SCHEDULED SC CHECK, FOUND SIDEWALL EMERGENCY EXIT LAMP INOP AT ROW 7 RT. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 1999030500016 19990305 00016 NM 1999 3 5 SWAA990340 1 19990223 A 3397 WIRE BOEING 737 7375H4 138449D NM ROW 2 DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED CHECK, FOUND FLOOR TRACK LIGHTING LIGHT (NR 2 FROM FRONT) INOP. REPAIRED WIRING AT ROW 2 LIGHT SOCKET, OP CKS OK PER MM. 2 L 7 2 4F RT A16WE 1999030500017 19990305 00017 NM 1999 3 5 SWAA990341 1 19990224 A 3350 BULB BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED A1 CHECK, FOUND EGRESS LIGHT NR 12 FROM THE FRONT INOP. RELAMPED PER M/M, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999030500018 19990305 00018 NM 1999 3 5 SWAA990342 1 19990223 A 2751 967741812996 INDICATOR BOEING 737 7373H4 1384600 NM C/P INOP A SWAA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 07 307SW 22947 ON TAKEOFF FLAPS WOULD NOT COME UP, RETRACTION STOPPED BETWEEN 0 AND 1 POSITION. ELECTRIC FLAPS LOWERED FLAPS TO 10 DEG FOR LANDING. AIRCRAFT RETURNED TO LBB. FLAPS WERE SYMMETRICAL AND RETRACTED NORMAL ON THE GROUND UNDER HYD POWER. RE MOVED AND REPLACED POSITION INDICATOR PER MM, OPS CK NORMAL. CLEANED CANNON PLUGS TO BOTH TRANSMITTERS. 2 L 7 2 4F RT A16WE 1999030500019 19990305 00019 NM 1999 3 5 SWAA990277 1 19990216 A 2131 7638101 CONTROLLER BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 343SW 24151 WHILE CRUISING AT FL 330 CABIN ALT ROSE ABOVE 10,000 FT, HORN SOUNDED. DESCENDED TO FL 200 AND WENT TO PACKS ON HIGH, C ABIN CAME BACK UNDER CONTROL. REMOVED AND REPLACED PRESSURIZATION CONTROLLER AND CONTROL PANEL OPS CHECKS GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999030500020 19990305 00020 NM 1999 3 5 SWAA990278 1 19990216 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 234 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED C-CHECK, ROUTINE INSPECTION OF AIRCRAFT AFTER C-CHECK WASH, FOUND A 3.5 INCH LONG CRACK ON NOSE GEAR AC TUATOR SUPPORT FITTING FORWARD WEB. CRACK IS LOCATED AT BS 234.0 AND IS 7 INCHES AFT OF FORWARD BULKHEAD IN NOSE WHEEL WELL. REPAIRED NOSE GEAR ACTUATOR SUPPORT BRACKET PER SRM. 2 L 7 2 4F RT A16WE 1999030500021 19990305 00021 NM 1999 3 5 SWAA990279 1 19990217 A 3350 BULB BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED SC CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT (SECOND FROM AFT GALLEY) INOP. RELAMPED FLOOR TRACK LIGHT PER MM, OPS CHECK GOOD. 2 L 7 2 4F A16WE 1999030500022 19990305 00022 NM 1999 3 5 SWAA990280 1 19990217 A 3350 BULB BOEING 737 7373T5 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SC CHECK, FOUND (EMERGENCY EXIT ROW) ONE EMERGENCY LIGHT INOP FLOOR TRACK LIGHTING. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999030500023 19990305 00023 NM 1999 3 5 SWAA990281 1 19990216 A 3350 BULB BOEING 737 7373T0 1384582 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED C4 CHECK, FOUND 2 EGRESS LIGHTS INOP AND HAVE MISSING LENSES. REPLACED LENSES AND RELAMPED EGRESS LIGH TING PER MM. 2 L 7 2 4F RT A16WE 1999030500024 19990305 00024 NM 1999 3 5 SWAA990282 1 19990215 A 3350 HOUSING BOEING 737 7375H4 138449D NM CABIN UNKNOWN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED SC CHECK, FOUND LEFT OVERWING DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER HOUSING PER MM. 2 L 7 2 4F RT A16WE 1999030500050 19990305 00050 NM 1999 3 5 TWAA9903001 1 19990224 A 3350 BULB BOEING 767 7673Y0 NM NR 3 DOOR DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 THE EXTERIOR EMERGENCY LIGHT FOR THE NUMBER 3 DOOR ON THE LEFT SIDE OF THE AIRCRAFT WAS INOPERATIVE. CLEANED CONTACTS F OR THE LAMP. CHECK-C 12-5-98 LAX. 2 L 7 2 4F RT A1NM 1999030500051 19990305 00051 NM 1999 3 5 SPAA9900003 1 19990219 A 3350 110049 BATTERY CHARGER BOEING 737 7372T4 1384492 NM CABIN INOP A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING DID NOT ILLUMINATE. THE ASSOCIATED SYSTEM BATT ERY CHARGER WAS REMOVED AND REPLACED. SUBSEQUENT SYSTEM TEST WAS SATISFACTORY PER BMM 33-51-11. 2 L 7 2 4F A16WE 1999030500052 19990305 00052 1999 3 5 AT9900141 4 19990223 A 2565 39618991 CABLE DOUG DC9 DC932 3022066 WP ESCAPE SLIDE BROKEN A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 823AT 47529 FOUND THE R-1 DOOR SLIDE (LANYARD ASSEMBLY) PULL CABLE BROKEN. REMOVED AND REPLACED THE DOOR SLIDE CABLE LANYARD AND RE TURNED THE AIRCRAFT TO SERVICE IAW MM 25-60. 2 L 7 2 4F A6WE 1999030500053 19990305 00053 WP 1999 3 5 AT9900142 1 19990224 A 2560 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE LOOSE A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 805AT 47378 FOUND THE R-1 DOOR SLIDE COVER NEEDS TO BE SECURED AND INSPECTED FOR PROPER INSTALLATION. SECURED SLIDE COVER PER MM 25 -60. 2 L 7 2 4F A6WE 1999030500054 19990305 00054 NM 1999 3 5 K3HA990017 1 19990223 A 3350 276 FUSE BOEING 727 727225 1384077 NM L1 AND R1 DOOR FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 LEFT AND RIGHT FRONT DOORS EMERGENCY EXIT LIGHTS INOP. TROUBLESHOOT SYSTEM TO BLOWN FUSE. REMOVED AND REPLACED FUSE, O PS CHECKED OK PER MM REF 33-50-01. 2 L 7 3 4F A3WE 1999030500055 19990305 00055 SO 1999 3 5 LR7A9903 1 19990218 A 5313 3530594L4R FITTING LKHEED 382 382G 526414U SO BS 990 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 595 4606 CRACKED FITTINGS AT STA 990 BOTH LT AND RT SIDE. REPLACED FITTINGS IAW SMP 583 51-10. (P/N 353059-4L,-4R, 353042-8L). 2 H 7 4 4T A1SO 1999030500056 19990305 00056 EU 1999 3 5 JBXA9900070 1 19990225 A 3030 853BR PITOT HEAD FOKKER F28 F28MK0100 4990807 EU NR 3 INOPERATIVE A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 104ML 11445 FLT 112 RDU TO LGA, AFTER TAKEOFF PITOT NR 3 HEAT WARNING LMFDU. PITOT NR 3 HEAT FAULT WOULD NOT RESET. RETURNED TO RD U. REMOVED AND REPLACED NR 3 PITOT HEAD. OPS AND LEAK CHECKS GOOD IAW F-100 MM 34-11-01. 2 L 7 2 4F RT 1999030500057 19990305 00057 1999 3 5 PNSA990201 4 19990208 A 3413 2719139001 VSI SWRNGN SA227 SA227AC 8780603 SW PILOT PANEL SMOKING A PNSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 2708D 80 AC713B DURING CRUISE, SMOKE WAS EMITTED FROM CAPTAINS VSI, INSTRUMENT LIGHTING WAS DIMMED AND SMOKE WENT AWAY. 2 L 7 2 4T RT A8SW 1999030500058 19990305 00058 SO 1999 3 5 PNSA990202 1 19990223 A 2820 VALVE GRUMAV G21 G21A 3951204 SO RT SUMP TANK OUT OF POSITION A PNSA A UNSCHED LANDING X W ENGINE FLAMEOUT INADEQUATE Q C CL CLIMB 1 AL 03 741 B97 DURING CLIMB, PILOT NOTICED FUEL WAS NOT BURNING EVENLY FROM BOTH TANKS. UPON SELECTING THE RT TANK (THE FULLEST TANK) BOTH ENGINES LOST POWER. THE FUEL SELECTOR WAS RETURNED TO THE BOTH POSITION AND THE ENGINES STARTED. AFTER LANDING I T WAS DISCOVERED THE RT SUMP TANK FUEL VALVE WAS IN THE OFF POSITION. AFTE R THIS VALVE WAS PLACED IN THE ON POSITION BO TH ENGINES OPERATED NORMALLY ON ANY FUEL TANK SELECTED. 1 H 7 2 3R TC654 1999030500059 19990305 00059 NM 1999 3 5 CALA9900188 1 19990222 A 5753 651859919 FITTING BOEING 727 727224 1384076 NM NR 5 FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND A .5 INCH CRACK IN NR 5 FLAP TRACK CARRIAGE LOWER FORWARD ROLLER I/B YOKE FITTING. THE FLAP CARRIAGE W AS REMOVED AND REPLACED IAW MM 27-51-3. 2 L 7 3 4F A3WE 1999030500060 19990305 00060 NM 1999 3 5 CALA9900189 1 19990222 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND A 3.75 INCH CRACK IN RT ELEVATOR LOWER SKIN. REPAIRED IAW ECRA 5520-01207. 2 L 7 3 4F A3WE 1999030500061 19990305 00061 WP 1999 3 5 CALA9900190 1 19990222 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 229-237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF L-1 DOOR BETWEEN STA 229 AND 237 ABOVE LONGERON 18. A REPAIR WAS INSTALLED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1999030500062 19990305 00062 WP 1999 3 5 CALA9900191 1 19990224 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 226-232 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 226 TO 232. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPL ACED IAW SRM 53-05. 2 L 7 2 4F A6WE 1999030500063 19990305 00063 SO 1999 3 5 COMA9910039 1 19990223 A 3010 SWITCH EMB 120 EMB120RT SO RT HORIZ STAB FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 264CA 120256 RIGHT HAND STABILIZER DEICE FAIL WARNING. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE STABILIZER DEICE PRESSURE SWIT CH FOR FUTURE TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1999030500064 19990305 00064 EA 1999 3 5 COMA9960078 1 19990223 A 2750 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA TE FLAPS TRIPPED A COMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 989CA 7215 FLAPS FAIL CAUTION MESSAGE AFTER LANDING. RESET FLAP SYSTEM CIRCUIT BREAKERS, SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 1999030500065 19990305 00065 EA 1999 3 5 COMA9960079 1 19990224 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 915CA 7013 CABIN AFT OVERHEAD EMERGENCY LIGHT IS INOPERABLE. DEFERRED PER MEL. 2 L 7 2 4F RT A21EA 1999030500066 19990305 00066 NM 1999 3 5 99FDEA00076 1 19990224 A 2613 OVERHEAT LOOP BOEING 727 727225 1384077 NM NR 3 STRUT OUT OF POSITION A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 467FE 21449 ENGINE NR 3 STRUT OVERHEAT MOMENTARILY FLICKERED FOR 1 SEC ON APPROACH. INSP NR 3 ENGINE STRUT FOR LOOSE CLAMPS AND ADE QUATE CLEARANCE OF DETECTOR LOOP. TIGHTENED SEV CLAMPS PER MM 26-14-1. RAN ENG PER JET RUN HDBK, NO STRUT OVERHEAT LIG HT ILLUM. ALL INDICATIONS NORMAL. 2 L 7 3 4F A3WE 1999030500067 19990305 00067 NM 1999 3 5 VNAA9902010 1 19990217 A 6120 DOLN511F07SND01 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DIRTY A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 460PS 3061 THE LEFT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED ON THE TAXI PRIOR TO TAKEOFF. MAINTENANCE INSPEC TED AND CLEANED THE LEFT HAND PROPELLER OVERSPEED GOVERNOR CANNON PLUG. OPERATIONAL CHECKS WERE COMPLETED, IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 71-01-00, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500068 19990305 00068 NM 1999 3 5 SWAA990343 1 19990222 A 3350 BULB BOEING 737 7373H4 1384600 NM ROW 22 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 367SW 26578 DURING SCHEDULED SC CHECK, FOUND EMERGENCY LIGHT AT ROW 22 LEFT SIDE IS INOP. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 1999030500069 19990305 00069 NM 1999 3 5 SWAA990344 1 19990223 A 3397 WIRE BOEING 737 7375H4 138449D NM ROW 2 DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED CHECK, FOUND FLOOR TRACK LIGHTING LIGHT (NR 2 FROM FRONT) INOP. REPAIRED WIRING AT ROW 2 LIGHT SOCKET, OP CKS OK PER MM. 2 L 7 2 4F RT A16WE 1999030500070 19990305 00070 1999 3 5 SWAA990346 4 19990222 A 2565 1061323468 SLIDE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING PREFLIGHT, FOUND FWD ENTRY DOOR SLIDE WOULD NOT REMAIN SECURED. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999030500071 19990305 00071 NM 1999 3 5 SWAA990347 1 19990222 A 2781 TERMINAL BOEING 737 7373H4 1384600 NM NR 1 LE FLAP LOOSE A SWAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 373SW 26581 MDW-STL DURING TAXI OUT WHILE EXTENDING FLAPS TO POSITIONS, NR 1 L/E FLAP WENT TO AMBER ON EXT AND WOULD NOT ILLUMINATE GREEN, FLAPS POSITIONED UP AND DOWN WITH NO HELP. MAINT ADVISED FLAPS APPEARED TO BE IN NORMAL POSITION. RETURNED TO G ATE. REPLACED TERMINAL END TO NR 1 KRUEGER FLAP GROUND STUD PER M/M, ALL CKS NORMAL. 2 L 7 2 4F RT A16WE 1999030500072 19990305 00072 NM 1999 3 5 SWAA990348 1 19990222 A 5240 GATE BOEING 737 7373T5 NM SERVICE DOOR BENT A SWAA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 668SW 23060 AT FL330 LOST CABIN PRESS, WARNING HORN SOUNDED AND GAUGE READ 10,000 FT. ATTEMPTED TO RECOVER ALT WITH STANDBY, BUT MA NUAL AC WORKED. ALT 3500 FT AFTER EMER DESCENT TO FL240. PACKS HAD TO REMAIN ON HIGH TO KEEP PRESS. SUSPECTED FWD SER VICE DOOR SEAL. FOUND LOWER GATE COVER AND SEAL BENT L-1 DOOR. REMOVED AND REPLACED LOWER HINGE COVER PER M/M. ACFT P RESSURIZED NORMALLY PER M/M, LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 1999030500073 19990305 00073 NM 1999 3 5 TSAA9933021 1 19990112 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED POSTION 2 AND 5 BATTERY PACK FOR SEAT EMERGENCY LIGHT ASSY DUE TO NO 'ALL WELL' LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999030500074 19990305 00074 NM 1999 3 5 TSAA9933022 1 19990114 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 1 FLOOR PROXIMITY AISLE LIGHT BATTERY PACK DUE LED INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (X) 2 L 7 2 4F RT A16WE 1999030500076 19990305 00076 WP 1999 3 5 AALA990159 1 19990205 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 408AA 49319 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. REPAIRED EMERGENCY FLOOR PATH LIGHTI NG WIRE IN COACH CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999030500077 19990305 00077 WP 1999 3 5 AALA990163 1 19990208 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7538A 49992 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE IN FORWARD CABIN. REPAIRED EMERGENCY EXIT FLO OR PATH CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999030500078 19990305 00078 NM 1999 3 5 AALA990019 1 19990107 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 28B FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 363AA 24044 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH MARKER LIGHT INOPERABLE AT SEAT 28B. REPLACED CONNECTOR AT SEAT 28B . SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999030500079 19990305 00079 NM 1999 3 5 AALA990020 1 19990107 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 31B FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 363AA 24044 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH MARKER LIGHT INOPERABLE AT SEAT 31B. REPLACED CONNECTOR AT SEAT 31B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999030500080 19990305 00080 NM 1999 3 5 AALA990038 1 19990110 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383AN 26995 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PROXIMITY LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PROXIMITY CONNECTOR AT CABIN FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999030500081 19990305 00081 NM 1999 3 5 AALA990073 1 19990118 A 3397 WIRE BOEING 757 757223 1384957 NM 4L DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 615AM 24491 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS IN AFT COACH CABIN WERE INOPERATIVE. REPAIRED EMERGENCY EXIT PATH LIGHT JUMPER WIRE NEAR THE 4L DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999030500082 19990305 00082 NM 1999 3 5 AALA990156 1 19990207 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 628AA 24586 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD COACH INOPERATIVE. REPLACED EMERGENCY E XIT LIGHT STRIP AT FORWARD COACH CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999030500083 19990305 00083 NM 1999 3 5 AALA990157 1 19990207 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 34H DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH MARKER LIGHT INOPERATIVE AT SEAT 34H. REPLACED CONNECTOR AT SEAT 34 H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999030500084 19990305 00084 NM 1999 3 5 AALA990158 1 19990207 A 3350 B973521385 LIGHT GRIMES BOEING 767 767323 1385205 NM ROW 21B INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT PATH LIGHT ASSEMBLY AT SEAT ROW 21B INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT ASSEMBLY AT SEAT ROW 21B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999030500085 19990305 00085 SO 1999 3 5 C2XA99CL012 1 19990207 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 40717 120133 ALB - FLT 3172 - CREW REPORTED THEY HAD A RAPID DEPRESSURIZATION FROM FL 250 WITH A TOTAL LOSS OF ALL PRESSURIZATION. A IRCRAFT DIVERTED SCHEDULED ROUTE AND LANDED IN ABL WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CL E AND THE CARGO DOOR SEAL WAS REMOVED AND REPLACED IAW EMB-120 MM 52-30-01. OPERATIONAL CHECKS WERE SATISFACTORY IAW EM B-120 MM 21-30-00. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 1999030500086 19990305 00086 EU 1999 3 5 C2XA99BT002 1 19990125 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 DURING 1A INSPECTION, FOUND UPPER EXIT EMERGENCY LIGHTS (LT AND RT) INOPERABLE. REMOVED AND REPLACED POWER SUPPLY BATTE RY PACK. OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A53EU 1999030500087 19990305 00087 EU 1999 3 5 C2XA99BT003 1 19990124 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14825 170 DURING 2A INSPECTION, FOUND EMERGENCY LIGHTS NO TEST (FLOOR TRACK LIGHTS 1, 3, AND 5). REMOVED AND REPLACED BATTERY POW ER SUPPLY PACK. OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A53EU 1999030500088 19990305 00088 SO 1999 3 5 C2XA99CL013 1 19990207 A 3412 102AU1AF HEATER EMB 145 EMB145 SO NR 1 TAT PROBE INOPERABLE A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 13935 3487 A14305 145022 CLW - FLT 4091 - CREW REPORTED THAT DURING TAXI, THE NR 1 TAT HEAT WAS INOPERATIVE. AIRCRAFT RETURNED TO GATE. MAINTEN ANCE REMOVED AND REPLACED THE NR 1 TAT PROBE IAW EMB-145 MM 34-15-03. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT R ELEASED FOR SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999030500089 19990305 00089 EU 1999 3 5 C2XA99IA080 1 19990127 A 5330 S53571301200 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING C-CHECK INSPECTION, THE SKIN PANEL UNDER THE LEFT HAND AFT WING TO FUSELAGE ATTACH FITTING WAS FOUND CRACKE D. MAINTENANCE REPAIRED THE HOLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5340-01038, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,370.2 HOURS. CYCLES: 21,341. (X) 2 H 7 2 4T RT A53EU 1999030500090 19990305 00090 EU 1999 3 5 C2XA99IA079 1 19990127 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14833 188 EFD - DURING LINE CHECK INSPECTION, THE CENTER AND AFT AISLE PATH EMERGENCY LIGHTS WERE FOUND DIM. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACKS IAW WITH ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (X) 2 H 7 2 4T RT A53EU 1999030500091 19990305 00091 SO 1999 3 5 C2XA99IA078 1 19990127 A 2150 8611041 VALVE EMB 145 EMB145LR SO NR 1 PACK STUCK A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 13949 145057 IAH - FLT 968 - THE CREW REPORTED A BURNING SMELL FROM THE NR 1 AIR CONDITIONING PACK AT TAKEOFF THRUST. MAINTENANCE UN STUCK THE NR 1 PACK VALVE, SATISFACTORILY RAN THE ENGINES ON THE GROUND AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (X) 2 L 7 2 4T RT T00011AT 1999030500092 19990305 00092 SO 1999 3 5 C2XA99IA077 1 19990128 A 3350 GE1317 BULB EMB 145 EMB145 SO LT EMER EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14947 145054 IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT HAND OVERWING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (X) 2 L 7 2 4F RT T00011AT 1999030500093 19990305 00093 SO 1999 3 5 C2XA99BT005 1 19990212 A 3230 CONNECTOR EMB 145 EMB145 SO LANDING GEAR DIRTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16944 145045 FLT 4084 - CREW REPORTED 'UNABLE TO RAISE GEAR'. MAINTENANCE CLEANED LGEU CANNON PLUGS. PERFORMED SEVERAL GEAR RETRACT IONS AND EXTENSIONS OPERATIONAL, TESTED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 1,862.1 HOURS. ACFT CYC LES: 1,787. (X) 2 L 7 2 4F RT T00011AT 1999030500094 19990305 00094 EU 1999 3 5 C2XA99BT004 1 19990212 A 3350 3011206 LIGHT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 11835 194 LEFT FORWARD OUTSIDE EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A53EU 1999030500095 19990305 00095 EU 1999 3 5 C2XA99IA086 1 19990126 A 3230 RETRACT MECH AEROSP ATR42 ATR42500 EU LT MLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 19446 504 IAH - DURING FLT 3467 FROM BTR/IAH, CREW REPORTED THE LEFT MAIN LANDING GEAR UNLOCK LIGHT CAME ON AFTER TAKEOFF. THE LI GHT WENT OUT AFTER LEVELING OFF AT 4,000 FEET AND SLOWING TO 160 KIAS AND THE GEAR WAS THEN FELT TO COME UP. THE AIRCRA FT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND PERFORMED A FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW ATR 42-500 JIC 32-31-00 WHERE NO DEFECTSS WERE NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999030500096 19990305 00096 EU 1999 3 5 C2XA99IA085 1 19990127 A 2510 3A0630080023 SEAT AEROSP ATR42 ATR42320 8680930 EU RT COCKPIT CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING C-CHECK INSPECTION, THE FIRST OFFICER'S SEAT RIGHT HAND AFT STRUCTURE WAS FOUND CORRODED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW ATR 42-320 SRM 51-25-03, AND SRM 51-70-00, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999030500097 19990305 00097 EU 1999 3 5 C2XA99IA084 1 19990127 A 5320 S5317320620100 PLATE AEROSP ATR42 ATR42320 8680930 EU RT COCKPIT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING C-CHECK INSPECTION, THE FIRST OFFICER'S SEAT ATTACH PLATE WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED PLATE IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20, 370.2 HOURS. CYCLES: 21,341. (X) 2 H 7 2 4T RT A53EU 1999030500098 19990305 00098 EU 1999 3 5 C2XA99IA083 1 19990127 A 5320 SVL600000201 MOUNT AEROSP ATR42 ATR42320 8680930 EU GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING C-CHECK INSPECTION, THE INBOARD AFT GALLEY FLOOR MOUNT WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACE D THE AFFECTED MOUNT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,370.2 HOURS. CYCLES: 21,341. (X) 2 H 7 2 4T RT A53EU 1999030500099 19990305 00099 EU 1999 3 5 C2XA99IA082 1 19990127 A 5320 SVL600000101 MOUNT AEROSP ATR42 ATR42320 8680930 EU GALLEY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING C-CHECK INSPECTION, THE INBOARD FORWARD GALLEY FLOOR MOUNT WAS FOUND CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED MOUNT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,370.2 HOURS. CYCLES: 21,3 41. (X) 2 H 7 2 4T RT A53EU 1999030500100 19990305 00100 EU 1999 3 5 C2XA99IA081 1 19990127 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 38 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED FLOORBEAM IAW ATR 42-320 SRM 51-21-28, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,370.2 HO URS. CYCLES: 21,341. (X) 2 H 7 2 4T RT A53EU 1999030500101 19990305 00101 EU 1999 3 5 C2XA99IA067 1 19990117 A 5320 S52171031426 FRAME AEROSP ATR72 ATR72212 EU PASSENGER DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69901 379 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR FRAME UPPER FLANGE WAS FOUND CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW WITH AR-72 SRM 52-11-00, AND, THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERV ICE. ACFT TT: 11,711.6 HOURS. CYCLES: 11,964. (X) 2 H 7 2 4T RT A53EU 1999030500102 19990305 00102 EU 1999 3 5 C2XA99IA066 1 19990117 A 5320 S5397330120001 SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69902 385 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND BELLY FAIRING PANEL 193CL CENTER SUPPORT ON THE MAIN LANDING GEAR FITTING WAS FOUND CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR-72 SRM 51-70-00 AND SRM 5 1-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. ACFT TT: 11,578.2 HOURS. CYCLES: 11,730. (X) 2 H 7 2 4T RT A53EU 1999030500103 19990305 00103 EU 1999 3 5 C2XA99IA071 1 19990117 A 5320 S53973202206 STIFFENER AEROSP ATR72 ATR72212 EU FRAME 27 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69901 379 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BELLY FAIRING STIFFENER ON THE FORWARD SIDE OF FRAME 27 WAS FOUND CRACKE D. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW ATR-72 SRM 51-24-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 11,711.6 HOURS. CYCLES: 11,964. (X) 2 H 7 2 4T RT A53EU 1999030500104 19990305 00104 EU 1999 3 5 C2XA99IA069 1 19990117 A 5347 S536780012226 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAMES 29-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69901 379 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND AFT INBOARD SEAT TRACK WAS FOUND CORRODED FROM FRAME 29 TO FRAME 36. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR-72 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 11,711.6 HOURS. CYCLES: 11,964. (X) 2 H 7 2 4T RT A53EU 1999030500105 19990305 00105 EU 1999 3 5 C2XA99IA068 1 19990117 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69901 379 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FLIGHT ATTENDANT'S SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED SEAT TRACK IAW ATR-72 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 11,711.6. CYCLES: 11,964. (X) 2 H 7 2 4T RT A53EU 1999030500106 19990305 00106 EU 1999 3 5 C2XA99IA070 1 19990117 A 5320 S53973202210 INTERCOSTAL AEROSP ATR72 ATR72212 EU FRAME 27 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69901 379 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND BELLY FAIRING INTERCOSTAL CLIP ON THE AFT SIDE OF FRAME 27 WAS FOUND CRA CKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW ATR-72 SRM 51-24-00, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. ACFT TT: 117,11.6 HOURS. CYCLES: 11,964. (X) 2 H 7 2 4T RT A53EU 1999030500107 19990305 00107 SO 1999 3 5 C2XA99IA074 1 19990113 A 3350 GE1317 BULB EMB 145 EMB145LR SO EMERGENCY EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13955 145075 IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 1999030500108 19990305 00108 EU 1999 3 5 C2XA99IA072 1 19990120 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15827 175 EFD - DURING LINE CHECK INSPECTION, THE FORWARD AND AFT EMERGENCY AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE DIM. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS IAW ATR 42-320 JIC 33-51-20, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999030500109 19990305 00109 EU 1999 3 5 C2XA99IA073 1 19990121 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19812 99 IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THREE EMERGENCY LIGHTS REMAINED ILLUMINATED WHEN POWER WAS R EMOVED FROM THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999030500110 19990305 00110 SO 1999 3 5 C2XA99CL010 1 19990123 A 2613 M1160140242 SENSOR EMB 120 EMB120RT SO LT DUCT FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 17728 120182 GSO - FLT 3346 - CREW REPORTED THAT IN-FLIGHT, THEY RECEIVED A LEFT DUCT LEAK AURAL WARNING, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A DUCT TEMP SENSOR IAW EMB-120 MM 20-21-00, OPERATIONAL CHEC KS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 1999030500111 19990305 00111 CE 1999 3 5 C2XA99CL009 1 19990121 A 3610 12938000113 VALVE BEECH 1900 1900D 1154162 CE RT BLEED AIR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 81546 6032 5032 GWD10287MP UE187 CLE - FLT 3161 - CREW REPORTED THAT THE RIGHT HAND BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO FIE LD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND BLEED AIR SHUT OFF VALVE IAW B1900 MM 36-0 0-02, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1999030500112 19990305 00112 EU 1999 3 5 C2XA99IA151 1 19990209 A 5330 S53571301200 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE SKIN PANEL UNDER THE LEFT HAND AFT WING TO FUSELAGE ATTACH FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE HOLE IAW WITH CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5340- 01038, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500113 19990305 00113 EU 1999 3 5 C2XA99IA150 1 19990209 A 5320 S5367139028802 RETAINER AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR CUT-OUT LOWER AFT SEAL RETAINER WAS FOUND CRACKED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SEAL RETAINER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500114 19990305 00114 EU 1999 3 5 C2XA99IA149 1 19990209 A 5320 S5367139028401 RETAINER AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR CUT-OUT LOWER CENTER SEAL RETAINER WAS FOUND CRACKED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SEAL RETAINER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500115 19990305 00115 EU 1999 3 5 C2XA99IA148 1 19990209 A 5320 S5367139028602 RETAINER AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR CUT-OUT LOWER FORWARD SEAL RETAINER WAS FOUND CRACKED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED SEAL RETAINER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500116 19990305 00116 EU 1999 3 5 C2XA99IA147 1 19990209 A 5311 S53970916264 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 29 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE WINGBOX FRAME 29L WAS FOUND CRACKED AT THE AFT END OF PANEL 29AL. MAINTENANCE REPA IRED THE AFFECTED FRAME, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 2 2,334. (X) 2 H 7 2 4T RT A53EU 1999030500117 19990305 00117 EU 1999 3 5 C2XA99IA146 1 19990209 A 5311 S53970916265 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 29 CORRODED A C2XA I CABIN DEPRESSURIZATION O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE WINGBOX FRAME 29R WAS FOUND CRACKED AT THE AFT END OF PANEL 296AR. MAINTENANCE REP AIRED THE AFFECTED FRAME, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500118 19990305 00118 EU 1999 3 5 C2XA99IA145 1 19990209 A 5320 S53997140220302 CHORD AEROSP ATR42 ATR42320 8680930 EU FRAME 27 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE CHORD ON THE RIGHT HAND SIDE OF FRAME 27A UNDER PANE 196AR WAS FOUND CRACKED. MAIN TENANCE REPAIRED THE AFFECTED CHORD IAW ATR42-320 SRM 53-91-43, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AC FT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500119 19990305 00119 EU 1999 3 5 C2XA99IA144 1 19990209 A 5320 S53573003243 STIFFENER AEROSP ATR42 ATR42320 8680930 EU FRAME 27 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE STIFFENER ON THE RIGHT HAND SIDE OF FRAME 27A UNDER PANEL 196AR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW ATR42-320 SRM 51-91-43 AND SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. ACFT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500120 19990305 00120 EU 1999 3 5 C2XA99IA143 1 19990209 A 5313 S53070210208 STRINGER AEROSP ATR42 ATR42320 8680930 EU FRAMES 27-30 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, STR 17R WAS FOUND CORRODED FROM FRAME 27 TO FRAME 30. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER SPLICE IAW ATR42-320 SRM'S 51-25-02, 51-21-42, AND 51-25-01. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500121 19990305 00121 EU 1999 3 5 C2XA99IA142 1 19990209 A 5320 S5367800821602 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FRAMES 40-41 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND CREASE BEAM Z-CHANNEL WAS FOUND CORRODED FROM FRAMES 40 TO 41. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED Z-CHANNEL IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500122 19990305 00122 EU 1999 3 5 C2XA99IA141 1 19990209 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAMES 27-33 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND OUTBOARD SEAT TRACK WAS FOUND CORRODED FROM FRAMES 27 TO 33. MAINTENANC E REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR421-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500123 19990305 00123 EU 1999 3 5 C2XA99IA140 1 19990209 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAMES 27-33 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND INBOARD SEAT TRACK WAS FOUND CORRODED FROM FRAMES 27 TO 33. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500124 19990305 00124 EU 1999 3 5 C2XA99IA139 1 19990209 A 5320 S53678009201 SUPPORT AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE FLOOR BEAM SUPPORTS AT THE SERVICE DOOR THRESHOLD WERE FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS IAW ATR42-320 SRM 51-25-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. ACFT TT: 19271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500125 19990305 00125 EU 1999 3 5 C2XA99IA138 1 19990209 A 5315 S5367248202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR O N THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC 5310-01037, AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500126 19990305 00126 EU 1999 3 5 C2XA99IA137 1 19990209 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE FLOOR BEAM AT FRAME 36 WAS FOUND CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC 5310-01037, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500127 19990305 00127 EU 1999 3 5 C2XA99IA136 1 19990209 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAMES 36-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE LEFT HAND FLIGHT ATTENDANT SEAT TRACK WAS FOUND CORRODED FROM FRAMES 36 TO 40. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500128 19990305 00128 EU 1999 3 5 C2XA99IA135 1 19990209 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 38 WAS FOUND CORRODED. MAINTENANCE INSTALLED A DOUBLER REPAIR T O THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC 5310-01037, AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500129 19990305 00129 EU 1999 3 5 C2XA99IA134 1 19990209 A 5320 S53671217294 WEB AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE WEB AT THE PASSENGER DOOR THRESHOLD FROM FRAMES 36-39 WAS FOUND CORRODED. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED WEB IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500130 19990305 00130 EU 1999 3 5 C2XA99IA133 1 19990209 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND FORWARD FLIGHT ATTENDANT SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500131 19990305 00131 EU 1999 3 5 C2XA99IA132 1 19990209 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND AFT FLIGHT ATTENDANT SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A CFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500132 19990305 00132 EU 1999 3 5 C2XA99IA131 1 19990209 A 5320 S537126220 CHORD AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE INBOARD CHORD ABOVE STR 17L BETWEEN FRAMES 39 AND 40 WAS FOUND CORRODED. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED CHORD IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500133 19990305 00133 EU 1999 3 5 C2XA99IA130 1 19990209 A 5220 S5227700100000 DOOR AEROSP ATR42 ATR42320 8680930 EU RT EMERG EXIT OUT OF ADJUST A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND EMERGENCY EXIT DOOR FAILED THE FUNCTIONAL TEST. MAINTENANCE ADJUSTED TH E DOOR ASSEMBLY IAW ATR42-320 JIC 52-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOU RS. CYCLES: 22,334. (X) 2 H 7 2 4T RT A53EU 1999030500134 19990305 00134 EU 1999 3 5 C2XA99IA129 1 19990209 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PASSENGER DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 19,271.5 HOURS. CYCLES: 22,33 4. (X) 2 H 7 2 4T RT A53EU 1999030500135 19990305 00135 EU 1999 3 5 99ZZZX769 1 19990108 A 2497 117188001 WIRE BOLKMS 117 BK117B1 5626012 EU TERMINAL BROKEN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7059N 7154 CABLE CRACKED BEYOND SERVICEABLE LIMITS. BROKE AFTER LESS THAN .1 TIME. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500136 19990305 00136 EU 1999 3 5 99ZZZX770 1 19990108 A 6321 AH43906 CAP BOLKMS 117 BK117A3 5626015 EU M/R BRAKE CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 625MB 7108 CAP CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. THIS PART BEING RETURNED FOR PRODUCT INVESTIGATION. 1 G 7 2 3U H13EU 1999030500145 19990305 00145 1999 3 5 99ZZZX779 4 19990107 A 3160 900A3720002107 DISPLAY SYSTEM DOUG MD900 MD900 3027375 NM COCKPIT FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 102 008251001 90000012 IIDS WILL NOT RESPOND TO MENU KEY, DIGITAL READ-OUT OR DISPLAY EXCEPTION. CYCLING POWER OFF THEN ON SEEMS TO CORRECT PR OBLEM TEMPORALLY. RIGHT TURBINE EGT FLUCTUATION ON DISPLAY LED. CONSTANT IIDS BATTERY FAULT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999030500146 19990305 00146 EU 1999 3 5 99ZZZX780 1 19990108 A 2435 4639302039 BEARING BOLKMS 117 BK117A3 5626015 EU CLUTCH CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 1662 7058 CLUTCH BEARING REJECTED NEW OUT-OF-BOX. EXCESSIVE CORROSION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500147 19990305 00147 EU 1999 3 5 99ZZZX781 1 19990108 A 2435 4639302039 BEARING BOLKMS 117 BK117A3 5626015 EU CLUTCH CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 1660 7058 BEARING REJECTED NEW OUT-OF-BOX. EXCESSIVE CORROSION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500148 19990305 00148 EU 1999 3 5 99ZZZX782 1 19990108 A 2435 4639302039 BEARING BOLKMS 117 BK117A3 5626015 EU CLUTCH CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 1654 7058 BEARING REJECTED NEW OUT-OF-BOX. EXCESSIVE CORROSION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500149 19990305 00149 EU 1999 3 5 99ZZZX783 1 19990108 A 2435 4639302039 BEARING BOLKMS 117 BK117A3 5626015 EU CLUTCH CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 1644 7058 BEARING REJECTED NEW OUT-OF BOX. EXCESSIVE CORROSION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500150 19990305 00150 NM 1999 3 5 AALA990053 1 19990113 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 21AB FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361AA 24042 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROW 21AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT C ONNECTOR AT SEAT ROW 21AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999030500151 19990305 00151 WP 1999 3 5 TWAA9903101 1 19990223 A 5320 FRAME DOUG DC9 DC932 3022066 WP EMER EXIT DRWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, THE TOP OF LT AFT EMERGENCY EXIT FRAME WAS CRACKED .5 INCH AT STA 667. INSTALLED REPAIR DOUBL ER PER SRM 53-05, PAGE 79. 2 L 7 2 4F A6WE 1999030500152 19990305 00152 WP 1999 3 5 TWAA9903102 1 19990222 A 5720 ANGLE DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND THE RT WING OTBD HINGE CASTING INTERNAL ATTACH RIB ANGLES CRACKED INBD AND OTBD SIDE. T HE RIB AND HINGE CASTING WAS REPLACED WITH NEW SERVICEABLE PARTS PER SRM 27-50-01. 2 L 7 2 4F A6WE 1999030500153 19990305 00153 WP 1999 3 5 TWAA9903103 1 19990222 A 5720 ANGLE DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND THE LT WING INBD AND OTBD SIDE OF OTBD HINGE CASTING INTERNAL ATTACH RIB ANGLE CRACKED A T ATTACH HOLES. RIBS AND HINGE CASTING REPLACED WITH NEW SERVICEABLE PARTS PER SRM 27-50-01. 2 L 7 2 4F A6WE 1999030500154 19990305 00154 NM 1999 3 5 TWAA9903104 1 19990223 A 5330 SKIN BOEING 727 727231 1384079 NM PAX DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 84355 21987 DURING CHECK-C MAINT, THE FWD ENTRY DOOR UPPER FUSELAGE HINGE CUTOUT WAS CRACKED AT THE FWD END. INSTALLED REPAIR PER S RM 53-10-1. 2 L 7 3 4F A3WE 1999030500155 19990305 00155 EU 1999 3 5 MALA976359 1 19990222 A 7110 SCREW SAAB SF340 340B 7860101 EU ENGINE COWL LOOSE A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 446XJ 446 DURING CLIMB FROM RHI, NOTICED 3 SCREWS ON INBOARD FORWARD SECTION OF ENGINE COWL CAME LOOSE, COWL WAS SEPARATING AND NO T SECURE. RETURNED TO RHI. MAINTENANCE RETORQUED COWL FASTENERS AS NEEDED AND ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999030500156 19990305 00156 NE 1999 3 5 MALA976360 2 19990223 A 7510 5056T88P01 AIR VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 99XJ 099 RT AIR VALVE LIGHT CAME ON WHEN RIGHT ENGINE ANTI-ICE WAS SELECTED ON. THERE WAS ALSO A TQ AND ITT SHIFT NOTED. REPLAC ED AIR VALVE. 2 L 7 2 4T 4 T RT A52EU E8NE 1999030500157 19990305 00157 1999 3 5 MALA976361 4 19990224 A 3425 6226190113 COMPUTER SAAB SF340 SF340A 7850100 EU AHRS SYST INOP A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 109XJ 340A109 AFTER DEPARTURE, MASTER CAUTION AVIONICS ILLUMINATED. REPLACED THE AHRS COMPUTER. 2 L 7 2 4T RT A52EU 1999030500158 19990305 00158 NE 1999 3 5 MALA976362 2 19990223 A 7510 M8372395G1005N CONNECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 99XJ 099 RT AIR VALVE LIGHT ILLUMINATED IN CRUISE W/RT ENG ANTI-ICE SELECTED ON. REPLACED CONNECTOR. 2 L 7 2 4T 4 T RT A52EU E8NE 1999030500159 19990305 00159 EU 1999 3 5 MALA976363 1 19990222 A 2751 WARNING BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS ACTIVATED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 502XJ E2307 ON APPROACH INTO CVG, CREW RECEIVED A FLAP INOP AND FLAP FAULT WARNING. PERFORMED FLAP FAULT RESET PROCEDURE. 2 H 7 4 4F RT A49EU 1999030500160 19990305 00160 EA 1999 3 5 JBXA9900071 1 19990227 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 579ML 7277 AFTER TAKEOFF AT APPROXIMATELY 10,000 FEET HAD AMBER DOOR LATCH WARNING (PASSENGER DOOR). AT 22.000 RED PAX DOOR LIGHT ILLUMINATED. DESCENDING THROUGH 10,000 FEET MESSAGE TURNED AMBER (PAX DOOR LATCH). OPS TEST OF PASSENGER DOOR IAW AMM 52-11-00 GOOD. NO FAULT NOTED AT THIS TIME. AIRCRAFT RETURNED TOO SERVICE. 2 L 7 2 4F RT A21EA 1999030500161 19990305 00161 EA 1999 3 5 JBXA9900072 1 19990228 A 5240 LATCH CNDAIR CL600 CL6002B19 EA SERVICE DOOR NOT SECURED A JBXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 580ML 7289 EXTREMELY LOUD SQUEAL EMANATING FROM RIGHT NOSE COMPARTMENT IN FLIGHT. FOUND LATCH ON GROUND SERVICE DOOR LOOSE (NOT SE CURED), LATCHED DOOR. 2 L 7 2 4F RT A21EA 1999030500162 19990305 00162 WP 1999 3 5 IXX9900004 1 19990226 A 3240 37038375 BRAKE DOUG DC8 DC871F 302199D WP NLG WORN A IXXA K NONE O OTHER CL CLIMB 1 GL 23 825BX 78316 1191 45978 AFTER TAKEOFF FROM LAX EN ROUTE TO TOL, AFTER GEAR RETRACTION A LOUD NOISE AND VIBRATION WAS NOTICED IN THE COCKPIT. TH E CREW CYCLED THE LANDING GEAR BUT THE NOISE RETURNED. THE AIRCRAFT RETURNED TO LAX FOR AN UNEVENTFUL LANDING. MAINTEN ANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT GROUND COOLING FAN ACCESS PANEL NOT PROPERLY SECURED, AND WAS CORREC TED. FURTHER INSPECTION FOUND THE NOSE TIRE SPIN BRAKES WORN, AND WERE REPLACE. NO FURTHER DISCREPANCIES WERE NOTED AN D THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 1999030500163 19990305 00163 SO 1999 3 5 RAAA99E8047 1 19990218 A 2560 80217 GIRT BAR GLOBAL 80180 LKHEED 188 188C 5262604 SO BS 865 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 002 188C2010 DURING FLIGHT, CREW GROUND TRAINING THE AFT LT EMERGENCY EXIT EMERGENCY EVACUATION SLIDE WAS DEPLOYED FOR EVACUATION SIM ULATION. AFTER SLIDE WAS FULLY DEPLOYED THE GIRT BAR WAS FOUND BENT. INVESTIGATION REVEALED GIRT BAR CRACKED ONE HALF O F CIRCUMFERENCE AT GIRT BAR AFT SLIDE ATTACH SLOT. GIRT BAR REMOVED FROM SERVICE. 2 L 7 4 4T 4A22 1999030500164 19990305 00164 WP 1999 3 5 CALA9900193 1 19990225 A 3397 WIRE DOUG DC10 DC1030 3023501 WP ROW 29 & 36 SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING AT SEAT ROWS 29/36KL INOPERATIVE. A POWER WIRE WAS FOUND DAMAGED AND SHORTED UNDER SEAT 36L CAUSING POWER SUPPLY FUSES TO BLOW. THE WIRE WAS REPAIRED AND THE FUSES WERE REPLACED. 2 L 7 3 4F A22WE 1999030500165 19990305 00165 WP 1999 3 5 CALA9900194 1 19990225 A 3397 WIRE DOUG DC9 DC932 3022066 WP COCKPIT BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 43537 47112 THE EMERGENCY AISLE PATH LIGHTS DID NOT ILLUMINATE WHEN ON POSITION WAS SELECTED DURING A PREFLIGHT CHECK. MAINTENANCE FOUND A BROKEN WIRE ON SWITCH IN COCKPIT. THE SWITCH WIRE WAS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED. 2 L 7 2 4F A6WE 1999030500166 19990305 00166 NM 1999 3 5 CALA9900195 1 19990225 A 3397 WIRE BOEING 757 757224 1384958 NM ROW 33ABC CHAFED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND EMERGENCY LIGHTS AT ROWS 26-34 LEFT INOPERATIVE. A CHAFED WIRE WAS FOUND UNDER SEAT 33ABC. THE WIRE W AS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED. 2 L 7 2 4F RT A2NM 1999030500167 19990305 00167 NE 1999 3 5 99FDEA00077 2 19990226 A 7250 TURBINE BOEING 727 7272S2F 1384O81 NM PWA JT8 JT8D217C 52053 NE NR 2 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 SO 25 213FE 22935 NR 2 ENGINE WAS SHUTDOWN VIBRATION ENDED WITH ENGINE SHUTDOWN. ENGINE TURBINE BLADES BROKEN AND CRACKED. *S/D* REMOVE D AND REPLACED NR 2 ENGINE PER WORK CARD 70T0002, OPER AND LEAK CK GOOD. 2 L 7 3 4F 4 F A3WE E9NE 1999030500168 19990305 00168 WP 1999 3 5 MWEA99077 1 19990220 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 10999 48133 MKE - THE FORWARD ENTRANCE EMERGENCY LIGHTS COME ON WHEN ALL AIRCRAFT POWER IS REMOVED. MTC REMOVED AND REPLACED FORWAR D EMERGENCY LIGHT BATTERY PACK. (X) 2 L 7 2 4F A6WE 1999030500169 19990305 00169 WP 1999 3 5 MWEA99078 1 19990224 A 5347 9957871501 SEAT TRACK DOUG DC9 DC915 3022036 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 MKE - FOUND ELONGATED HOLES ON CAPTAIN'S RIGHT AFT SEAT TRACK. MTC FABRICATED AND INSTALLED NEW SEAT TRACK. (X) 2 L 7 2 4F A6WE 1999030500170 19990305 00170 WP 1999 3 5 MWEA99079 1 19990225 A 2560 1721115200630 PANEL DOUG DC9 DC982 3022082 WP DOOR SLIDE BROKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 MKE - THE AFT GALLEY SERVICE DOOR GIRT BAR ATTACH POINT TO THE SLIDE COVER BROKE. MTC REPLACED THE ATTACH POINT PANEL A ND REINSTALLED SLIDE. (X) 2 L 7 2 4F A6WE 1999030500171 19990305 00171 SO 1999 3 5 SWIA971416 1 19990228 A 3020 16321 BOOT EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE INLET FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 137H 120137 RIGHT ENGINE AIR INLET DEICE BOOT FAILED IN FLIGHT. RETURNED TO PDX. SHOP AIR TESTED GOOD FROM BOTH AIR INPUTS. SWAPP ED PRESSURE SWITCHES FROM LEFT TO RIGHT AND INSTALLED NEW TIMER FOR RIGHT INLET BOOT IAW MM 30-20-05. OPS CHECKS GOOD O N GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999030500172 19990305 00172 NE 1999 3 5 SWIA971417 2 19990228 A 7261 OIL SYST EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT ENGINE REQD SERVICE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 OIL AURAL WARNING AT V1 FOLLOWED WITHIN 30 SECONDS BY OIL PRESSURE FLUCTUATION BELOW GREEN ON RIGHT ENGINE. RETURNED TO FIELD. SERVICED BOTH ENGINES WITH 2 QUARTS OIL EACH. PERFORMED ENGINE RUN ON BOTH ENGINES. OIL PRESSURE INDICATION S TEADY. 2 L 7 2 4T 4 T RT A31SO E20NE 1999030500173 19990305 00173 SO 1999 3 5 SWIA971418 1 19990228 A 3610 38E966A VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 156CA 120156 EN ROUTE TO CLD LEFT DUCT LEAK LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT DID NOT EXTINGUISH. SHUT DOWN LEFT ENGINE AND RETURNED TO LAX. RAN AIRCRAFT AND DUPLICATED DISCREPANCY. ISOLATED REGULATOR/RELIEF VALVE AS FAULTY. INSTALLED SERVI CEABLE VALVE AND RAN AIRCRAFT EXTENSIVELY AT 100 PERCENT TQ. BLEEDS AUTO PACK NORMAL. NO DISCREPANCY OR DUCT LEAK LIGH T NOTED. OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999030500174 19990305 00174 SO 1999 3 5 SWIA971419 1 19990220 A 2120 FAN EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 269UE 120196 SMOKE IN COCKPIT. RETURNED TO FAT. REPLACED LEFT RECIRCULATION FAN. OPS CHECKED GOOD WITH NO DISCREPANCIES AND NO SMO KE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999030500175 19990305 00175 EA 1999 3 5 SWIA971420 1 19990220 A 5270 WARNING CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 416SW 7089 CLIMBING THROUGH 16,000 AN EICAS MESSAGE PAX DOOR LATCH WAS OBSERVED. FOLLOWED QRH AND AT 22,000 AN EICAS RED MESSAGE P AX DOOR CAME ON. FOLLOWED QRH AND DIVERTED TO IDA. CHECKED AIRCRAFT PSEU AND FOUND IN MEMORY S46 FAR IN MEMORY. HAD S LC MAINTENANCE FAX THE MM TO IDA FOR REFERENCE. USED MM 52-70-04. GROUND CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999030500176 19990305 00176 1999 3 5 SWIA971421 4 19990221 A 3425 HSI EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 212SW 120276 LEFT SIDE TOTAL F/S FAILURE, ADI AND GYRO FLAG HSI, HDG DISPLAY. DIVERTED FROM RNO TO SLC. REPLACED AHC 85 ON LEFT SID E. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999030500177 19990305 00177 EA 1999 3 5 SWIA971422 1 19990222 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 416SW 7089 PASSENGER DOOR LATCH RED MESSAGE CAME ON INFLIGHT. RETURNED TO OMA, ADJUSTED ROD END TO ROD THAT ROTATES UPPER TWO CAMS IAW MM 52-11-02. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999030500178 19990305 00178 SO 1999 3 5 SWIA971423 1 19990223 A 3610 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 221SW 120290 RIGHT ENGINE DUCT LEAK IN FLIGHT. DID NOT EXTINGUISH AFTER 3 MINUTES, SHUTDOWN ENGINE. AFTER ENGINE SHUT DOWN, LIGHT E XTINGUISHED. RETURNED TO LAX. REPLACED RIGHT ENGINE 18 PSI REGULATOR, CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999030500184 19990305 00184 NM 1999 3 5 CA990203007 1 19990125 A 5610 141T480149 WINDOW BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE COCKPIT CRACKED W O OTHER B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE AP APPROACH 1 CA 30690 (CAN) ON FINAL APPROACH, EXPLOSION, SMOKE AND THEN FIRE FROM BOTTOM OF PILOT'S NR 1 WINDOW, SHORTLY AFTER WINDOW CRACKED . TOTAL INCIDENT TIME APPROXIMATELY 15 TO 20 SECONDS. FIRE WAS EVIDENT FOR ABOUT 2 SECONDS. LEFT NR 1 WINDOW AND WIND OW HEAT, COMPUTER REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999030500186 19990305 00186 NM 1999 3 5 CA990203010 1 19990113 A 4920 9688252 COMPRESSOR DISK GTCP6604 BOEING 747 747* NM APU CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3511 1298 P37621 (CAN) INSPECTION OF THE AUXILIARY POWER UNIT FOUND 4TH STAGE COMPRESSOR DISC CRACKED AT THE ACUTE CORNER FORMED BY THE D OVE TAIL AND DISC FRONT FACE. THE SIZE OF THE CRACK WAS APPROXIMATELY 0.300 INCH. THE COMPRESSOR DISC WAS REMOVED AND SCRAPPED. 2 L 7 4 4F RT A20WE 1999030500187 19990305 00187 NM 1999 3 5 CA990203011 1 19990113 A 4920 38400203 TURBINE WHEEL GTCP331 BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE APU FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 10584 715 P118 P709694 (CAN) THE AUXILIARY POWER UNIT 3RD STAGE TURBINE WHEEL HAD A STRUCTURAL FAILURE, WITH TWO BLADES SEPARATING FROM THE INT EGRAL WHEEL. THE BLADE SEPARATIONS INITIATE FROM CRACKS ADJACENT TO COOLING RIVET HOLES. CRACKS ARE CAUSED BY HIGH TEM PERATURE GRADIENT ACROSS THE WHEEL, A RESULT OF STATIONARY FELT-METAL-SEAL DETERIORATION. SERVICE BULLETINS 49-6536R1, 49-5883, AND 49-5884 WERE DESIGNED TO REDUCE THIS PREMATURE FAILURE PROBLEM. THE BLADE SEPARATION ON THIS TURBINE (S/N NR 3-18040-500) IS AN EXAMPLE OF PRE-MOD TURBINE FAILURES NOT INDICATIVE OF POST-MOD SERVICE. PART TC: 15,464. 2 L 7 2 4F 4 F RT A1NM E3NE 1999030500194 19990305 00194 NE 1999 3 5 CA990203018 2 19990112 A 7240 JA803795 COMBUSTION CAN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 8405 38579 P657459D (CAN) ENGINE INDUCTED IN THE SHOP FOR 12 STAGE HP COMPRESSOR DISC BEING TX'D. DISASSEMBLY OF THE ENGINE FOUND TWO COMBU STION CANS (IGNITER CANS) WERE SHOWING SIGNS OF EXTREME BRITTLENESS AND AN EXCESSIVE NUMBER OF INTERGRANULAR CRACKS. TH E TWO CANS WERE SCRAPPED. PART TC: 6,538. 2 L 7 2 4F 4 F A6WE E2EA 1999030500196 19990305 00196 EU 1999 3 5 CA990209007 1 19990123 A 2910 NAS161212 O-RING AIRBUS 320 A320212 EU HYDRAULIC SYS FAILED W O OTHER K FLUID LOSS LD LANDING 1 CA (CAN) YELLOW SYSTEM HYDRAULIC FAILURE. QUANTITY AND PRESSURE LOW, ECAM ACTIONED. LANDED NORMAL. FOUND QUICK DISCONNECT COUPLING ON PTU TWO-WAY VALVE LOOSE AND 0-RING BLOWN OUT. REPLACED, SYSTEM SERVICED. 2 L 7 2 4F RT A28NM 1999030500203 19990305 00203 NE 1999 3 5 CA990210004 2 19990129 A 7261 3022375 GARLOCK SEAL 310428001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC PUMP LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA RGB120816 120815 (CAN) AT 16,000 FEET, OIL PRESSURE ON NR 1 ENGINE GRADUALLY DROPPED. PRECAUTIONARY SHUT DOWN WAS CARRIED OUT ON NR 1 EN GINE. POST-FLIGHT INSPECTION FOUND THE SOURCE OF THE OIL LEAK TO BE A LEAKING GARLOCK SEAL ON THE ENGINE DRIVEN HYDRAUL IC PUMP. GARLOCK CARRIED SEAL, O-RING, AND ENGINE DRIVEN PUMP SHAFT, O-RINGS WERE REPLACED. OIL SERVICED, ENGINE GROUN D RUN, NO FURTHER LEAKS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999030500205 19990305 00205 WP 1999 3 5 AALA990153 1 19990202 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1208 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 237AA 49523 TUL - FOUND CORROSION ON SEAT TRACK. REPLACED AFT SECTION OF SEAT TRACK NR 1 STATION 1174-1309 SRM 53-05. (M) 2 L 7 2 4F A6WE 1999030500206 19990305 00206 WP 1999 3 5 AALA990083 1 19990106 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1148-1156 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON LONGERON 52 FORWARD OF STATION 1156 FORWARD TO STATION 1148. REMOVED PART, TREATED, PRIMED AND PAINTED AND INSTALLED NEW PART AND FASTENERS PER AARD 51-10-00-1 PAGE 1. (M) 2 L 7 3 4F A22WE 1999030500207 19990305 00207 WP 1999 3 5 AALA990082 1 19990106 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1059-1079 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION AT STRINGER 51R. INSTALLED NEW STRINGER FROM STATION 1059-1079 AND SPLICES PER SRM 53-10 VOL 1 P- T PLUS P PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1999030500208 19990305 00208 WP 1999 3 5 AALA990100 1 19990114 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1521-1531 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION 12 INCHES FORWARD OF AFT BULKHEAD INSIDE RIGHT W/W ON SKIN PLATE BELOW STRINGER 32R. REPAIRED WIT H DOUBLERS PER ESO 7349, DATED 1-7-99. (M) 2 L 7 3 4F A22WE 1999030500209 19990305 00209 WP 1999 3 5 AALA990146 1 19990204 A 5312 BULKHEAD TEE DOUG DC10 DC1010 3022110 WP BS 1156 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND BS 1156 LOWER LEFT BULKHEAD TEE CUP ANGLE CORRODED. ACCOMPLISHED LEFT SIDE BS 1156 BULKHEAD TEE CUP REPAIR PER PRING SRM 10530073. (M) 2 L 7 3 4F A22WE 1999030500210 19990305 00210 WP 1999 3 5 AALA990147 1 19990202 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND SHEAR TIE CORRODED 50L TO 50R STATION 1964. ALODINED, PRIMED, PAINTED AND INSTALLED NEW SHEAR TIE SRM VOL I I. (M) 2 L 7 3 4F A22WE 1999030500211 19990305 00211 WP 1999 3 5 AALA990148 1 19990203 A 5312 BULKHEAD TEE DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - RIGHT TEE-CAP CRACKED STATION 1156 PERMANENT REPAIR REQUIRED AT 22985 CYCLE. INSTALLED REPAIR PER PRING SR1053007 3 RT SIDE (PERMANENT REPAIR). (M) 2 L 7 3 4F A22WE 1999030500212 19990305 00212 WP 1999 3 5 AALA990149 1 19990203 A 2550 TRAY DOUG DC10 DC1010 3022110 WP BS 795-895 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON NR 1 ROLLER TRAY IN FORWARD LOWER GALLEY. REPLACED NR 1 ROLLER TRAY PER AARD 51-10-00. (M) 2 L 7 3 4F A22WE 1999030500213 19990305 00213 WP 1999 3 5 AALA990150 1 19990204 A 5330 PANEL DOUG DC10 DC1010 3022110 WP BS 1370 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - LOWER INBOARD EDGE OF SLANT PANEL IN RIGHT W/W HAS AREAS OF CORROSION. BLENDED AND TREATED AFFECTED AREAS OF CORR OSION ON SLANT PANEL IAW SRM 51-21-01, ESO 7349 DATED 1-25-99 AND ESO7349 DATED 1-27-99. (M) 2 L 7 3 4F A22WE 1999030500214 19990305 00214 WP 1999 3 5 AALA990132 1 19990129 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1815 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - TWO DENTS/GOUGES AT STATION 1815 AT LONGERON 40R. INSTALLED DOUBLER PER SRM VOL 1 53-20-00. (M) 2 L 7 3 4F A22WE 1999030500215 19990305 00215 WP 1999 3 5 AALA990139 1 19990202 A 5320 FITTING DOUG DC10 DC1010 3022110 WP BS 776-791 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - END FITTING ON STATION 52 AT STATION 776-791 IS CORRODED. INSTALLED STRAP REPAIR IAW ESO 7349, DATED 2-2-99. (M) 2 L 7 3 4F A22WE 1999030500216 19990305 00216 WP 1999 3 5 AALA990142 1 19990203 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1741 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FORWARD LOWER FRAME ANGLE CORRODED. REPAIRED FRAME PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1999030500217 19990305 00217 WP 1999 3 5 AALA990115 1 19990128 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 775-795 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON LONGERON 52. REMOVED CORRODED SECTION OF LONGERON AND INSTALLED NEW SECTION IAW SRM 51-01-00-0 5. (M) 2 L 7 3 4F A22WE 1999030500218 19990305 00218 WP 1999 3 5 AALA990130 1 19990201 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 819 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON FLOORBEAM AT STATION 819 ABOVE STRINGER 43L. SPLICED IN NEW SECTION OF FLOORBEAM PER AARD 51-0 1-00 AND SRM 53-10-01. (M) 2 L 7 3 4F A22WE 1999030500219 19990305 00219 WP 1999 3 5 AALA990131 1 19990201 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON BOTTOM OF FRAME AT STATION 879 BETWEEN 51R AND 51L. SPLICED IN NEW SECTION OF FRAME PER SRM 53 -30-00. (M) 2 L 7 3 4F A22WE 1999030500220 19990305 00220 WP 1999 3 5 AALA990116 1 19990128 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 831 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON FRAME AT STATINO 831 BETWEEN 51L AND 51R. SPLICED IN NEW SECTION OF FRAME FLANGE PER AARD 51-1 0-00-01 TREATED, PRIMED AND PAINED PER SRM 51-21-01 VOL II. (M) 2 L 7 3 4F A22WE 1999030500221 19990305 00221 WP 1999 3 5 AALA990120 1 19990127 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 838-840 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON STRINGER 43L FROM STATION 838 TO 840. CUT OUT CORROSION AND SPLICED IN NEW SECTION OF STRINGER PER SRM 52-10-00. (M) 2 L 7 3 4F A22WE 1999030500222 19990305 00222 WP 1999 3 5 AALA990119 1 19990128 A 2720 WEIGHT DOUG DC10 DC1010 3022110 WP RUDDER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - UPPER BALANCE WEIGHT ON UPPER RUDDER CORRODED. REPAIRED BALANCE WEIGHT PER ESO 7349, DATED 01-25-99. (M) 2 L 7 3 4F A22WE 1999030500223 19990305 00223 WP 1999 3 5 AALA990118 1 19990128 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 831 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON SHEAR TIE AT STATION 831 BETWEEN 52 AND 51R. INSTALLED NEW SHEAR TIE PER AARD 51-10-00-01, TRE ATED AND PRIMED AND PAINTED PER SRM 51-21-01 VOL II. (M) 2 L 7 3 4F A22WE 1999030500224 19990305 00224 WP 1999 3 5 AALA990117 1 19990128 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1039 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON AFT SIDE OF SHEAR TIE AT LONGERON 49L-52. REPAIRED PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1999030500225 19990305 00225 WP 1999 3 5 AALA990161 1 19990204 A 5320 SILL DOUG DC10 DC1010 3022110 WP BS 1721-1781 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND DOOR SILL SKIN CORRODED AT BS 1721-1781. INSTALLED 2 REPAIR STRAPS AS PER ESO 7349 DATED 2-1-99. TREATED A ND PRIMED AS PER SRM 51-21-01 VOL II. (M) 2 L 7 3 4F A22WE 1999030500226 19990305 00226 WP 1999 3 5 AALA990081 1 19990119 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 899 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON SHEAR TIE AT STATION 899 BETWEEN STRINGER 52 AND 51R. CUT OUT SECTION OF SHEAR TIE SPLICE IN N EW SECTION PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1999030500227 19990305 00227 WP 1999 3 5 AALA990080 1 19990121 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP BS 1521-1701 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND LEFT LOWER 2 CHANNEL AT LONGER 42L HAS AREAS OF CORROSION FROM CENTER CARGO COMPARTMENT FORWARD BULKHEAD TO STATION 1701. TREATED AND PAINTED CHANNEL PER SRM 51-21-01, SPLICED CHANNEL WHERE REQUIRED SRM 53-70-00. (M) 2 L 7 3 4F A22WE 1999030500228 19990305 00228 WP 1999 3 5 AALA990079 1 19990121 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1780 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - SHEAR TIE CORRODED. REMOVED CORROSION PER SRM 51-21-01 CUT AND REPLACED SHEAR TIE PER SRM 53-30-00. ALSO, ALODIN ED AND PRIMED PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1999030500229 19990305 00229 WP 1999 3 5 AALA990099 1 19990120 A 2550 TRAY DOUG DC10 DC1010 3022110 WP BS 979-1099 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON CENTER ROLLER TRAY. REMOVED AND REPLACED CENTER ROLLER TRAY PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1999030500230 19990305 00230 WP 1999 3 5 AALA990112 1 19990125 A 2550 TRAY DOUG DC10 DC1010 3022110 WP BS 615-859 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON NR 2 ROLLER TRAY IN SEVERAL. SPLICED IN NEW SECTION OF TRAY PER SRM 53-70-00. (M) 2 L 7 3 4F A22WE 1999030500231 19990305 00231 WP 1999 3 5 AALA990138 1 19990130 A 3233 59370365501 ACTUATOR DOUG DC9 DC982 3022082 WP LT MLG DEFECTIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 488AA EE18561 49681 DFW - FLT 1528 - DURING CLIMB-OUT, THE LEFT RED GEAR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW RECYCLED GEA R AND THE LIGHT WENT OUT. FLIGHT CONTINUED TO DFW WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT AND FOUND THE LEF T RETRACT ACTUATOR CYLINDER WAS AT FAULT. REPLACED LEFT RETRACT ACTUATOR CYLINDER. SYSTEM LEAK CHECKED AND OPERATED NO RMALLY DURING GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500232 19990305 00232 WP 1999 3 5 AALA990162 1 19990207 A 3010 LINE DOUG DC9 DC982 3022082 WP AIRFOIL DEICE LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 225AA 49175 ORD - FLT 382 - DURING CLIMB-OUT, SMOKE WAS REPORTED IN THE CABIN WITH THE AIRFOIL ICE ACTIVATED. FLIGHT CREW RETURNED OFF THE AIRFOIL ICE AND THE SMOKE DISSIPATED. FLIGHT AIR INTERRUPTED AND RETURNED TO ORD WITHOUT FURTHER INCIDENT. MAI NTENANCE FOUND THE SENSE LINE HAD COME OFF THE AIRFOIL A/I PRSOV. MAINTENANCE REPLACED THE LINE AND ACCOMPLISHED REQUIR ED ADJUSTMENTS AND TESTS PER MAINTENANCE MANUAL REQUIREMENTS. COALESER BAGS WERE INSPECTED WITH NO CONTAMINATION. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500233 19990305 00233 WP 1999 3 5 AALA990160 1 19990205 A 4920 NHL60501 APU DOUG DC10 DC1030 3023501 WP TAIL DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 144AA 47848 DFW - FLT 102 - DURING TAKEOFF AND CLIMB, FUME SMELL IN CABIN WAS NOTICED BY CREW AND PASSENGERS AND DISSIPATED. ODOR R ETURNED DURING DESCENT AND LASTED THROUGH ENGINE SHUTDOWN. MAINTENANCE FOUND APU TO BE CAUSE OF ODOR. REMOVED AND REPL ACED APU, CHANGE COALESCER BAGS AND ACCOMPLISHED BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999030500234 19990305 00234 EU 1999 3 5 AALA990134 1 19990129 A 4990 OIL SYSTEM FOKKER F28 F28MK0100 4990807 EU APU OVERSERVICED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1420D 11403 TUL - FLT 768 - DURING TAKEOFF AFT LAVATORY SMOKE DETECTORS SOUNDED AND THE FLIGHT CREW SMELLED SMOKE IN THE AFT CABIN. AIRCRAFT AIR INTERRUPTED AND LANDED OVERWEIGHT TUL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU WAS OVER SERVIC ED. SERVICED APU TO PROPER LEVEL AND RAN WITH NO FURTHER ODOR NOTED IN CABIN. OVERWEIGHT LANDING INSPECTION REVEALED N O FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999030500235 19990305 00235 NM 1999 3 5 AALA990103 1 19990125 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT AIRSTAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6822 2616 19700 DFW - DURING OVERNIGHT MAINTENANCE AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY E XIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500236 19990305 00236 NM 1999 3 5 AALA990076 1 19990119 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT IN AFT COACH CABIN WERE INOPERATIVE. REPLACED EMERG ENCY EXIT FLOOR PATH LIGHT JUMPER WIRE IN COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500237 19990305 00237 NM 1999 3 5 AALA990077 1 19990119 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 DFW - DURING OVERNIGHT MAINTENANCE, THREE LIGHT SEGMENTS IN THE AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERAT IVE. REPLACED EMERGENCY FLOOR PATH LIGHT STRIPS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500238 19990305 00238 NM 1999 3 5 AALA990068 1 19990101 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 887AA 21526 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PA TH LIGHTING BROKEN WIRE IN COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500239 19990305 00239 NM 1999 3 5 AALA990039 1 19990110 A 3350 LIGHT BOEING 727 727223 1384074 NM AFT AIR STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6823 19701 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500240 19990305 00240 NM 1999 3 5 AALA990048 1 19990111 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT AIR STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIR EMERGENCY EXIT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LI GHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500254 19990305 00254 EU 1999 3 5 AALA990154 1 19990205 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU ROW 10/18 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1433B 11418 DFW - FLIGT 1657 - FLIGHT CRWE FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BETWEEN SEAT ROWS 10 AND 18. REPAIRED AND REPLACED WIRING AS REQUIRED BETWEEN SEAT ROWS 10 AND 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999030500255 19990305 00255 NM 1999 3 5 AALA990145 1 19990203 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM GALLEY DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 509 21387 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER AFT LEFT GALLEY DOOR INOPERATIVE. REPLACED OVERHEAD GALLE Y DOOR LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500258 19990305 00258 WP 1999 3 5 AALA990121 1 19990129 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 70524 49916 DFW - FLT 1213 - DURING CLIMB-OUT WITH GEAR RETRACTED, THERE WAS AN INTERMITTENT RED NOSE GEAR LIGHT ILLUMINATING. THER E WAS NO VIBRATION OR AIR NOISE SO FLIGHT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED UP POSITION PROXIMITY SENSOR AND AS A PRECAUTIONARY. REPLACED NOSE OVER CENTER SENSOR. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F A6WE 1999030500259 19990305 00259 WP 1999 3 5 AALA990136 1 19990201 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 33414 49325 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FLOO R PATH LIGHTING WIRE THAT WAS SHORTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500260 19990305 00260 WP 1999 3 5 AALA990137 1 19990202 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 412AA 49323 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT COACH CABIN INOPERATIVE. MAINTENANCE FOUND A BROKEN CO NNECTOR. REPLACED CONNECTOR TO EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500261 19990305 00261 WP 1999 3 5 AALA990123 1 19990131 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY EXIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 465A 49595 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT OVERWING EXITS INOPERATIVE. MAINTENANCE FOUND A LOOSE CONN ECTOR. RESECURED LOOSE CONNECTOR TO EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500262 19990305 00262 WP 1999 3 5 AALA990140 1 19990203 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7517A 49894 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. RESEATED EMERGENCY FLOOR PATH LIGHT WI RE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500263 19990305 00263 WP 1999 3 5 AALA990141 1 19990204 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 234AA 49181 DCA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTS IN AFT COACH CLASS WERE INOPERATIVE. REPAIRED BROKEN WIRE AT OVERHEAD BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500265 19990305 00265 EU 1999 3 5 C2XA99IA128 1 19990204 A 3230 1005383Y00 VALVE AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14832 187 IAH - FLT 3738 - THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WIT HOUT INCIDENT, WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE. THE AIRCRAFT WAS THEN APPROVED FO R RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500266 19990305 00266 SO 1999 3 5 C2XA99IA127 1 19990205 A 3350 GE1619 BULB EMB 120 EMB120RT SO RT EMER EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A31SO 1999030500267 19990305 00267 CE 1999 3 5 C2XA99IA126 1 19990203 A 3260 1003810061 SWITCH BEECH 1900 1900D 1154162 CE NLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 81536 UE152 IAH - FLT 3462 - THE CREW REPORTED THAT AFTER THE GEAR WAS RETRACTED THE RED INTRANSIT LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPL OCK SWITCH IAW B1900 MM 32-60-01. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999030500268 19990305 00268 SO 1999 3 5 C2XA99CL015 1 19990212 A 3260 P0950 CONNECTOR EMB 120 EMB120RT SO RT MLG DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 15732 120195 CLE - FLT 3221 - CREW REPORTED THAT UPON RAISING THE LANDING GEAR THE RIGHT MAIN RED 'A' INDICATION LIGHT STAYED ILLUMIN ATED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED CANNON PLUG P0950, OPERATIONAL CHEC KS WERE SATISFACTORY IAW EMB120 MM 32-30-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999030500269 19990305 00269 SO 1999 3 5 C2XA99CL014 1 19990211 A 2750 3075001017 CONTROL EMB 120 EMB120RT SO TE FLAPS FAILED A C2XA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 09 16723 3900 0154 120169 CMH - FLT 3350 - CREW REPORTED THAT THE LEFT INBOARD FLAP HAD A UNCONTROLLED EXTENSION TO ASYMMETRY 25 DEGREES. AIRCRAF T DIVERTED TO CMH WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120MM 27-50- 06, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999030500270 19990305 00270 SO 1999 3 5 C2XA99CL016 1 19990216 A 3010 3295542 VALVE EMB 145 EMB145 SO HORIZ STABILIZER FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 15926 3551 0010 145005 CLE - FLT 4099 - CREW REPORTED THAT DURING CRUISE, THE HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAILED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ANTI-ICE VALVE IAW EM B-145 MM 30-12-01, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-145 MM 30-00-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999030500271 19990305 00271 CE 1999 3 5 MASA99018 1 19990202 A 3230 MS24166D1 RELAY BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A MASA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 65YV UE65 FLT 5999 - MBS-PIT - ON APPROACH TO PIT, THE GEAR WOULD NOT EXTEND. THE LANDING GEAR CIRCUIT BREAKER POPPED AND THE CRE W RESET THE GEAR AND THE CIRCUIT BREAKER POPPED AGAIN. CREW MANUALLY EXTENDED THE GEAR AND RECEIVED A NORMAL INDICATION . EMERGENCY EQUIPMENT WAS STANDING BY AS AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LANDING GEAR K3 RELAY SHORTED AND SHOWED SIGNS OF OVERHEATING. REMOVED AND REPLACED THE LANDING GEAR RELAY. SWUNG GEAR, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999030500272 19990305 00272 EA 1999 3 5 MASA99024 1 19990214 A 3350 GE1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77181 7181 FLT 6020 - PHX-MRY - PRIOR TO DEPARTURE, CREW REPORTED THAT TWO OF THE FOUR CEILING EMERGENCY LIGHTS WERE INOP. MAINTEN ANCE REPLACED TWO BULBS, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999030500274 19990305 00274 EA 1999 3 5 MASA99019 1 19990207 A 3350 GE1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37178 7178 FLT 5002 - PHL-CMH - DURING PREFLIGHT WALK AROUND, CREW NOTICED THAT THE LEFT AFT EXTERIOR EMERGENCY LIGHT WAS INOPERATI VE. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999030500275 19990305 00275 NM 1999 3 5 MASA99020 1 19990207 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 FLT 6341 - PHX-PSP - DURING PREFLIGHT WALK AROUND, CREW NOTICED THE BATTERY SWITCHES IN THE ON POSITION. ALL EMERGENCY BATTERIES. THE MAIN BATTERY AND THE AUXILLARY BATTERY WERE DISCHARGED. MAINTENANCE REPLACED THE BATTERIES. AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999030500276 19990305 00276 1999 3 5 MASA99022 4 19990210 A 3425 6229882002 DPU BEECH 1900 1900D 1154162 CE NR 2 MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 4ZV UE4 FLT 5347 - BOS-HYA - AFTER DEPARTURE FROM BOS, THE CREW REPORTED THE MASTER WARNING FLASHED ON THE CONSOLE. THNE THE F/ O'S EFIS SCREENS STARTED TO BLANK OUT INTERMITTENTLY. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO BOS W ITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY BUT REPLACED THE NR 2 DPU AS A PRECAUTIONARY M EASURE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999030500277 19990305 00277 WP 1999 3 5 ASAA9980030 1 19990127 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L-1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 SEA - FLT 593 - CREW REPORTED L-1 DOOR WAS VERY DIFFICULT TO LOCK INTO POSITION. LUBED LOCKS AND OPERATED NORMALLY. (M ) 2 L 7 2 4F A6WE 1999030500278 19990305 00278 WP 1999 3 5 ASAA9980018 1 19990113 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1155-1174 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 957AS 49126 LCQ - DURING C-CHECK, CORROSION WAS FOUND ON FUSELAGE SKIN AT LOWER ANTENNA MOUNT AT FS 1163. REMOVED DAMAGED MATERIAL AND INSTALLED EXTERNAL DOUBLER IAW ASA EA 5330-01361. (M) 2 L 7 2 4F A6WE 1999030500279 19990305 00279 WP 1999 3 5 ASAA9980005 1 19990104 A 5313 51242886 LONGERON DOUG DC9 DC983 3022083 WP BS 1212-1250 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 53074 OAK - DURING C-CHECK, FOUND CORROSION ON LONGERON 29L AT FS 1231. SPLICED IN NEW SECTION OF LONGERON 29L IAW DC9 SRM 53 -02, PAGES 48-53. (M) 2 L 7 2 4F RT A6WE 1999030500281 19990305 00281 1999 3 5 ASAA9980008 4 19990105 A 2565 D29984109 SLIDE DOUG DC9 DC983 3022083 WP TAILCONE DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 960AS 530 53074 OAK - DURING C-CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE LIGHT TEST FIXTURE WAS FOUND MISSING. REPLACED THE T AILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1999030500282 19990305 00282 WP 1999 3 5 ASAA9980006 1 19990104 A 5610 WINDOW DOUG DC9 DC983 3022083 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - PRIOR TO DEPARTURE OF FLIGHT 231, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUST ED WINDOW MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999030500294 19990305 00294 NM 1999 3 5 USAASB99024 1 19990129 A 5210 411N25994 STRAP BOEING 737 737301 1384611 NM PAX DOOR OUT OF POSITION A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 587US 23932 CLT - FLT 83 - IMMEDIATELY AFTER DEPARTING CLT, A LOUD RAPPING NOISE AT THE AFT LEFT ENTRY DOOR WAS HEARD BY PASSENGERS AND THE FLIGHT ATTENDANTS IN THE REAR OF THE CABIN. CAPTAIN WAS NOTIFIED AND THE NOISE WAS DETERMINED TO BE THE YELLOW RESTRAINING STRAP FOR THE AFT ENTRY DOOR. FLIGHT RETURNED TO FIELD TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMER GENCY WAS DECLARED. MAINTENANCE REMOVED THE YELLOW RESTRAINING STRAP FROM THE AFT ENTRY DOOR AND INSPECTED AREA FOR DAM AGE. NO DAMAGE WAS NOTED. PERFORMED OVERWEIGHT LANDING INSPECTION. NO ABNORMALITIES FOUND. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1999030500295 19990305 00295 NM 1999 3 5 USAASB99012 1 19990113 A 2150 20405010 ACM BOEING 737 7373B7 1384580 NM LT PACK FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 518AU 23704 MCO - FLT 808 - CLIMBING THROUGH FL270, THE CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 11,000 FEET AND CLIMBED AS HIGH AS 13,000 FEET. EMERGENCY DESCENT WS MADE TO 10,000 FEET. FLIGHT RETURNED TO FIELD TO MCO AND LANDED W ITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND THE LEFT 35 DEGREE TEMPERATURE CONTROL BOX. OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A16WE 1999030500296 19990305 00296 NM 1999 3 5 99ZZZM157 1 19990113 A 2150 6075103 CONTROL BOX BOEING 737 7373B7 1384580 NM LT PACK FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 518AU 23704 MCO - FLT 808 - CLIMBING THROUGH FL270, THE CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 11,000 FEET AND CLIMBED AS HIGH AS 13,000 FEET. EMERGENCY DESCENT WS MADE TO 10,000 FEET. FLIGHT RETURNED TO FIELD TO MCO AND LANDED W ITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND THE LEFT 35 DEGREE TEMPERATURE CONTROL BOX. OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A16WE 1999030500297 19990305 00297 NM 1999 3 5 USAASB99017 1 19990121 A 3230 RETRACT MECH BOEING 737 7373B7 1384580 NM NLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 371US 22950 PIT - ON FINAL APPROACH AT 220 KNOTS, CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT COME DOWN WHEN THE GEAR HANDLE WA S LOWERED. CREW RECYCLED THE GEAR AND ALL GEAR CAME DOWN NORMALLY. DURING FIRST ATTEMPT, CREW DID NOT HEAR ANY NOISE F ROM THE NOSE LANDING GEAR AREA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR DRY OF GREASE AND LUBRICATION. PERFORMED GREASE AND LUBRICATION SERVICE OF ENTIRE NOSE LANDING GEAR PER MM 12-21-21. JACKED AIRCRAFT AND CYCLED NOSE LANDING GEAR NUMEROUS TIMES. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1999030500298 19990305 00298 NM 1999 3 5 USAASB99019 1 19990124 A 5610 PPG5893543110 WINDSHIELD BOEING 737 737301 1384611 NM FLT COMPARTMENT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 586US 25842 23931 IND - FLT125 - AT FL350, THE CAPTAIN NOTICED AN AREA OF SEVERAL SMALL CRACKS IN THE OUTER PANE AT THE TOP CENTER OF THE FIRST OFFICERS FORWARD WINDSHIELD. QUICK REFERENCE HANDBOOK PROCEDURES WERE FOLLOWED. FLIGHT DIVERTED TO PIT AND LANDE D WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE R-1 WINDSHIELD PER JOB PRO CEDURE CARD. ALSO, REPLACED WINDOW HEAT CONTROL UNIT (P/N 231-2) FOR THE R-1 WINDSHIELD AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999030500299 19990305 00299 NM 1999 3 5 USAA990061 1 19990125 A 5312 BULKHEAD CHORD BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 727 LBL 29 WL 153.5 BULKHEAD LOWER PRIMARY CHOR D. INSTALLED REPAIR DOUBLER ANGLE, FILLER AND VERTICAL STIFFENER PER EA 63469. (M) 2 L 7 2 4F RT A16WE 1999030500300 19990305 00300 NM 1999 3 5 USAA990057 1 19990125 A 5320 69353524 SHEAR TIE BOEING 737 737301 1384611 NM BS 948 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 948 STRINGER 27R SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500301 19990305 00301 NM 1999 3 5 USAA990056 1 19990125 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN RIVETS BS 908 STRINGER 4R. INSTALLED NEW TIE CLI P PER SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 1999030500302 19990305 00302 NM 1999 3 5 USAA990055 1 19990125 A 5320 CHANNEL BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .20 CRACK AND CORROSION BS 520 VHF NR 2 COMM ANTENNA MOUNT CHANNEL. R EMOVED AND REPLACED CHANNEL PER SB 737-53-1159 FIG 1 STEP 1. (M) 2 L 7 2 4F RT A16WE 1999030500303 19990305 00303 NM 1999 3 5 USAA990050 1 19990125 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP BS 727A STRINGER 2L. INSTALLED NEW TIE CLI P PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500304 19990305 00304 NM 1999 3 5 USAA990049 1 19990125 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURNIG Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP BS 727C STRINGER 6L, STRINGER 7L, STRINGER 8L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500305 19990305 00305 NM 1999 3 5 USAA990048 1 19990125 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN TIE CLIP BS 639 STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999030500306 19990305 00306 NM 1999 3 5 USAA990047 1 19990125 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER SPLICE BS 908 STRINGER 4R. INSTALLED NEW SPLI CE PER SRM 51-10-02 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999030500307 19990305 00307 NM 1999 3 5 USAA990046 1 19990125 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP PE R SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 1999030500308 19990305 00308 NM 1999 3 5 USAA990045 1 19990125 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT EDGE OF EQUIPMENT COOLING DUCT STATION 380 FUSELAGE SKIN. INSTALLED EXTERNAL DOUBLER PER BOEING DRAWING 65C33930. (M) 2 L 7 2 4F RT A16WE 1999030500309 19990305 00309 NM 1999 3 5 USAA990044 1 19990125 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK BETWEEN RIVETS BS 908 STRINGER 4L. INSTALLED NEW TIE C LIP PER SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 1999030500310 19990305 00310 NM 1999 3 5 USAA990029 1 19990125 A 5311 656229101 FRAME BOEING 737 737301 1384611 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 6 INCH AREA OF CORROSION AT STRINGER 27L BS 500D CARGO FLOOR LEVEL FRAME. CORROSION TASK NR C 53-208-01. FABRICATED REPAIR PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999030500311 19990305 00311 NM 1999 3 5 USAA990026 1 19990125 A 5320 654653931 ANGLE BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK AT LOWER FAST OF INNER CHORD ANGLE BS 616 WL 201 LT SID E. REPAIRED PER TR 53-10-23 AND EA 63358 INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A16WE 1999030500312 19990305 00312 NM 1999 3 5 USAA990025 1 19990125 A 5320 654653932 ANGLE BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK AT LOWER FASTENER OF INNER CHORD ANGLE BS 616 WL 201 RT SIDE. REPAIRED PER TR 53-10-23 AND EA 63358 INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A16WE 1999030500313 19990305 00313 NM 1999 3 5 USAA990024 1 19990125 A 5315 654680323 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .20 INCH CRACK STATION 520 LBL 25 FLOORBEAM. INSTALLED DOUBLER AND RE PAIR ANGLES PER EA 63326, SB 737-53-1120. (M) 2 L 7 2 4F RT A16WE 1999030500314 19990305 00314 NM 1999 3 5 USAA990023 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727A CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 8R BS 727A. REPAIRED PER SRM 51-1 0-02. (M) 2 L 7 2 4F RT A16WE 1999030500315 19990305 00315 NM 1999 3 5 USAA990022 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 4R BS 727B. REPAIRED PER SRM 51-1 0-02. (M) 2 L 7 2 4F RT A16WE 1999030500316 19990305 00316 NM 1999 3 5 USAABB99005 1 19990125 A 3350 20121 BATTERY CHARGER BOEING 767 7672B7 1385107 NM LT EMER EXIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND LOW LEVEL EMERGENCY LIGHTING AT LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. ( M) 2 L 7 2 4F RT A1NM 1999030500317 19990305 00317 EU 1999 3 5 USAA990067 1 19990131 A 5320 1710037 BEAM FOKKER F28 F28MK0100 4990807 EU BS 4175 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 852US 21911 11280 PIT - DURING C-1 CHECK, FOUND 1 INCH BY 1 INCH CORROSION AREA ON BEAM AT BL 0 STATION 4175. MANUFACTURED REPLACEMENT PA RT 171-0037 PER EA NR 51437. (M) 2 L 7 2 4F RT 1999030500318 19990305 00318 NM 1999 3 5 USAASB99028 1 19990202 A 3350 LIGHT BOEING 737 737201 1384454 NM RT EMER EXIT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 22866 BUF - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. WHEN SEAT PATH LIGHTS ARE ILLUMINATED, EME RGENCY EXIT LIGHT IS INOPERATIVE. WHEN SEAT PATH LIGHTS ARE EXTINGUISHED, EMERGENCY EXIT LIGHT ILLUMINATES. LIGHTS WIL L NOT WORK TOGETHER. (M) 2 L 7 2 4F A16WE 1999030500320 19990305 00320 NM 1999 3 5 USAASB99015 1 19990120 A 3350 20121 BATTERY CHARGER BOEING 737 737301 1384611 NM ROWS 5-10 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 338US 23234 LGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FOR THE INTERIO R EMERGENCY FLOOR LIGHTING AND REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 10ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999030500321 19990305 00321 NM 1999 3 5 99ZZZM158 1 19990120 A 3350 XB864041 LIGHT BOEING 737 737301 1384611 NM ROWS 5-10 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 338US 23234 LGA - PILOT REPORTED THAT THE INTERIOR EMERGNECY FLOOR LIGHTING FROM SEAT ROWS 5 THROUGH 10 AND THE LEFT EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT ROW 10ABC WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER FOR THE INTERIO R EMERGENCY FLOOR LIGHTING AND REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 10ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999030500322 19990305 00322 NM 1999 3 5 USAASB99032 1 19990208 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM BS 753 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 340US 23237 CMH - MAINTENANCE FOUND THE AFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT BS 753. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999030500323 19990305 00323 NM 1999 3 5 USAASB99031 1 19990207 A 3350 20131ALP BATTERY PACKS BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 444US 24862 CLE - MAINTENANCE FOUND THE AFT SERVIDC DOOR EMEGENCY EXIT SIGN AND EXTERIOR LIGHT INOP AND THE LOWER RIGHT FORWARD OVER WING EXIT SIGN AND BULLNOSE LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE M1134 AND M1197 BATTERY PACKS. OPERATIONA L CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999030500324 19990305 00324 NM 1999 3 5 USAA029905 1 19990208 A 2752 MS93911302E4C DRIVE MOTOR VICKERS BOEING 727 727254 138408L NM TE FLAPS FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 912TS MX314178D 20438 'A' SYSTEM HYDRAULICS WENT OT ZERO DURING CLIMB-OUT. PERFORMED ABNORMAL CHECK LIST, GEAR AND FLAPS WERE LOWERED USING A LTERNATE METHOD. REPLACED HYDRAULIC FLAP DRIVE MOTOR PER MM 27-51-62 DUE TO LEAK. REPLACED NR 1 ENGINE DRIVEN HYDRAULI C FLAP DRIVE MOTOR PER MM 27-51-62 DUE TO LEAK. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-00. REPLACED SYST EM 'A' HYDRAULIC DRAIN FILTER PER MM 29-11-41. PERFORMED HYDRAULIC 'A' SYSTEM INSPECTION AND CHECK PER MM 29-11-0. (M) 2 L 7 3 4F A3WE 1999030500325 19990305 00325 EU 1999 3 5 USAAF99009 1 19990207 A 3150 800610331 COMPUTER FOKKER F28 F28MK0100 4990807 EU E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 893US 19829 11373 CLT - FLT 331 - EN ROUTE TO PIT FROM MCI A 'WARN COMPUTER INOP' MESSAGE ILLUMINATED ON THE MULTI FUNCTION DISPLAY. DUE TO ICING CONDITIONS AT PIT, THE FLIGHT DIVERTED TO CLT. THE FLIGHT CREW DECLARED AN EMERGENCY. THE FLIGHT LANDED CLT W ITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLIGHT WARNING COMPUTER. (M) 2 L 7 2 4F RT 1999030500326 19990305 00326 1999 3 5 UIEA9903 4 19990131 A 3410 A4321710016 AIRSPEED BOEING 747 7472D7B 1384803 NM LT/RT COCKPIT DEFECTIVE A UIEA C D ABORTED TAKEOFF RETURN TO BLOCK G MULTIPLE FAILURE TO TAKEOFF 1 EA 15 522MC 21783 FLT TG891 - BTB - DURING TAKEOFF ROLL, F/O'S AIRSPEED INDICATOR DID NOT MOVE AND CAPTAINS AIRSPEED INDICATOR JUMPED FROM 70 TO 80 KNOTS. RETURNED TO BLOCKS AND DURING TROUBLESHOOTING CONFIRMED THAT BOTH AIRSPEED INDICATORS WERE DEFECTIVE. REPLACED CAPTAINS AND F/O'S AIRSPEED INDICATOR P/N A4321710016. PERFORMED PITOT/STATIC TEST AND BOTH SYSTEMS NOW OPERA TE NORMAL. (M) 2 L 7 4 4F RT A20WE 1999030500341 19990305 00341 WP 1999 3 5 USAAD99021 1 19990205 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG LACK OF LUBE A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 956VJ 47588 PHL-PWM - FLT 2225 - DURING APPROACH THE NOSE LANDING GEAR DID NOT EXTEND WHEN THE GEAR HANDLE WAS LOWERED UNTIL THE ALT ERNATE EXTENSION HANDLE WAS OPERATED. THE AIRCRAFT THEN LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE LANDIN G GEAR ASSEMBLY AND LUBRICATED THE NOSE LANDING GEAR PIVOT POINTS. AN OPERATIONAL CHECK OF THE NOSE LANDING GEAR WAS NO RMAL. (M) 2 L 7 2 4F A6WE 1999030500342 19990305 00342 WP 1999 3 5 USAAD99020 1 19990204 A 3010 10200075 SENSOR DOUG DC9 DC981 3022081 WP RIGHT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 813US 48093 IND-CLT - FLT 234 - ON TAKEOFF THE RIGHT ICE PROTECTION TEMP HIGH LIGHT ILLUMINATED WITH THE AIRFOIL ANTI-ICE SYSTEM OFF AND THE PNEUMATIC CROSSFEED CLOSED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE RIGHT ICE PROTECTION TEMP SENSOR. (M) 2 L 7 2 4F A6WE 1999030500343 19990305 00343 WP 1999 3 5 USAAD99025 1 19990121 A 3260 DC00F10SL3P CONNECTOR DOUG DC9 DC931 3022065 WP RT MLG DOOR FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 935VJ 48115 PIT-SBN - FLT 753 - DURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED. TURNING ON THE HYDRAULIC PUMPS AND REDU CING AIRSPEED DID NOT HELP. THE LIGHT EXTINGUISHED DURING DESCENT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED THE RIGHT GEAR DOOR PROXIMITY SENSOR ELECTRICAL RECEPTACLE. (M) 2 L 7 2 4F A6WE 1999030500344 19990305 00344 NM 1999 3 5 USAA019904 1 19990115 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 6101 21244 FLT 6141 - BOS-LGA - FOUND ON L/S FORWARD CABIN BULLNOSE EXIT LIGHT INOP. REPLACED BATTERY PACK, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999030500345 19990305 00345 NM 1999 3 5 USAA019903 1 19990114 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM AFT AIRSTAIRS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918TS 19952 20445 FLT 6073 - BOS-LGA - AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999030500346 19990305 00346 NM 1999 3 5 USAA019905 1 19990121 A 3350 90052 BATTERY PACK BOEING 727 727225 1384077 NM AFT ENTRY DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS UA5282 20447 FLT 6150 - LGA-BOS - FOUND ON L/S, AFT ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT BASE AND BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999030500347 19990305 00347 NM 1999 3 5 USAA029901 1 19990202 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 418 21244 FLT 6181 - BOS-LGA - OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 18. REPLACED BATTERY PACK, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999030500348 19990305 00348 NM 1999 3 5 USAA029902 1 19990202 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 3 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 14204 21244 FLT 6181 - BOS-LGA - OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 3. REPLACED BATTERY PACK, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999030500349 19990305 00349 NM 1999 3 5 USAA990021 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 5R BS 727B. REPAIRED PER SRM 51-1 0-02. (M) 2 L 7 2 4F RT A16WE 1999030500350 19990305 00350 NM 1999 3 5 USAA990020 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 7L, STRINGER 8L BS 727B. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500351 19990305 00351 NM 1999 3 5 USAA990019 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 7L BS 727D. REPAIRED PER SRM 51-1 0-02. (M) 2 L 7 2 4F RT A16WE 1999030500352 19990305 00352 NM 1999 3 5 USAA990018 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727C CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 4R, STRINGER 5R, STRINGER 6R AND S TRINGER 7R BS 727C. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500353 19990305 00353 NM 1999 3 5 USAA990017 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 5R AT BS 727D. REPAIRED PER SRM 5 1-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500354 19990305 00354 NM 1999 3 5 USAA990016 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727E CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 5R STRINGER 7R AT BS 727E. REPAIR ED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500355 19990305 00355 NM 1999 3 5 USAA990015 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN TIE CLIP STRINGER 4R AT BS 639. INSTALLED NEW TIE CL IP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999030500356 19990305 00356 NM 1999 3 5 USAA990014 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 7L, AT STATION 727D. REPLACED PAR T PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500357 19990305 00357 NM 1999 3 5 USAA990013 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 16L, AT BS 597. REPLACED PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500358 19990305 00358 NM 1999 3 5 USAA990012 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 8R, AT BS 727A. REPLACED PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500359 19990305 00359 NM 1999 3 5 USAA990011 1 19990125 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 4R, STRINGER 5R AT BS 727B. REPLA CED PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999030500360 19990305 00360 NM 1999 3 5 USAA980685 1 19990125 A 5315 654680323 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH LONG CRACK IN FLOORBEAM STATION 520 RBL 45. INSTALLED DOUBLERS AND FILLERS PER SB 737-53-1120 AND EA 63326. (M) 2 L 7 2 4F RT A16WE 1999030500361 19990305 00361 NM 1999 3 5 USAA980684 1 19990125 A 5315 654680323 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH LONG CRACK IN FLOORBEAM STATION 520 RBL 25. INSTALLED DOUBLERS AND FILLERS PER SB 737-53-1120 FIG 28 EA 63326. (M) 2 L 7 2 4F RT A16WE 1999030500362 19990305 00362 NM 1999 3 5 USAA980683 1 19990125 A 5315 654680323 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 37897 23231 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH LONG CRACK IN FLOORBEAM STATION 520 LBL 45. INSTALLED DOUBLERS AND FILLERS PER S/ 737-53-1120 EA 63326. (M) 2 L 7 2 4F RT A16WE 1999030500363 19990305 00363 NM 1999 3 5 USAA99068 1 19990131 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 663-727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 37286 23383 CLT - DURING RON VISUAL INSPECTION, FOUND THREE 2 INCH LONG CRACKS BETWEEN BS 663 AND BS 727 AT LBBL 6 AND RBBL 6 LOWER KEEL BEAM SKIN. INSTALLED INTERIM REPAIR DOUBLERS PER SRM 53-60-12. (M) 2 L 7 2 4F RT A16WE 1999030500364 19990305 00364 EU 1999 3 5 SIMA9900332 1 19990202 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 202KD 340B202 ABI - DURING MBV INSPECTION, CHAFE WAS DISCOVERED IN THE RIGHT NACELLE INBOARD SKIN AT FILLET FAIRING. BLENDED OUT DAMA GE FROM CHAFING TO VERY FINE SURFACE FINISH. PERFORMED EDDY CURRENT INSPECTION OF AREA WITH NO DEFECTS NOTED. FABRICAT ED DOUBLER .050 THICK AND CONTOUR TO NACELLE PANEL AND CUT TO DIMENSION. APPLIED SURFACE TREATMENT, INSTALLED DOUBLER I N RT NACELLE. RESTORED FINISH PAINT. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES . AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500365 19990305 00365 EU 1999 3 5 SIMA990333 1 19990202 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 202KD 340B202 ABI - DURING MBV INSPECTION, A CHAF WAS DISCOVERED IN THE REAR LEFT FUSELAGE PANEL AT THE HORIZONTAL STABILIZER LEADING EDGE SEAL. LIGHTLY BLENDED CHAFED AREA TO A FINE SURFACE FINISH. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOT ED. FABRICATED EXTERNAL DOUBLER .025 THICK. APPLIED SURFACE TREATMENT TO BLENDED AREA AND DOUBLER. INSTALLED CHAFING PROTECTION. RESTORED PAINT FINISH. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500366 19990305 00366 EU 1999 3 5 SIMA990331 1 19990202 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 202KD 340B202 DURING MBV INSPECTION, CHAF WAS DISCOVERED IN THE REAR RIGHT FUSELAGE PANEL AT THE HORIZONTAL STABILIZER LEADING EDGE SE AL. LIGHTLY BLENDED CHAFED AREA TO A FINE SURFACE FINISH. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FA BRICATED EXTERNAL DOUBLER .025 THICK. APPLIED SURFACE TREATMENT TO BLENDED AREA AND DOUBLER. ATTACHED DOUBLER TO DAMAG ED AREA, RESTORED PAINT FINISH. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES. AIR CRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500367 19990305 00367 EU 1999 3 5 SIMA990292 1 19990129 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 232AE 340B232 BPT - FLT 3876 - CAPTAIN REPORTED THE GEAR WOULD NOT EXTEND, GOT INTRANSIT LIGHT ONLY. TRIED TWICE AND ON THE THIRD TIM E IT WORKED. LANDED SAFELY, BUT HAD ALREADY DECLARED AN EMERGENCY. CIRCUIT BREAKER F7 (LANDING CONTROL) POPS WHEN SELE CTING GEAR DOWN. DEFERRED LANDING GEAR UNTIL 1-31-99. AT THAT TIME, ABI MAINTENANCE PERFORMED EXTENSION AND RETRACTION CHECK OF LANDING GEAR, INSPECTED LANDING GEAR HANDLE AND RELAY AREA, AND SERVICED STRUTS. PERFORMED FURTHER GEAR SWING S IN EXCESS OF TWENTY TIMES AND COULD NOT DUPLICATE DISCREPANCY. WORK DONE IAW SF3 AMM 12-32-00 AND 32-30-00. MEL CLEA RED. (M) 2 L 7 2 4T RT A52EU 1999030500368 19990305 00368 EU 1999 3 5 SIMA990291 1 19990129 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURNIG CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) 2 H 7 2 4T RT A53EU 1999030500369 19990305 00369 EU 1999 3 5 SIMA990283 1 19990128 A 5347 4650000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 638-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 202KD 340B202 ABI - DURING MBV INSPECTION SEAT TRACK BL 0 TO STATION 638-686 WAS FOUND CORRODED. CUT OUT 47.5 INCH SECTION OF SEAT TR ACK DEBURRED, ALODINE, PRIMERED, AND PAINTED EDGES. FABRICATED A 47.5 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76 511. FABRICATED A 15 INCH U-BEAM OF PLAL-7075-T7351 MATERIAL, DEBURRED, ALODINE, AND PAINTED. POSITIONED REPAIR BEAM I NSIDE EXISTING TRACK AND INSTALLED IN AIRCRAFT. REPAIR DONE IAW SAAB SRM 53-70-60 AND STANDARD SRM PROCEDURES. AIRCRAF T OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500370 19990305 00370 EU 1999 3 5 SIMA990282 1 19990128 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 445 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 184AE 340B184 ABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON FUSELAGE SKIN STATINO 445.5 BETWEEN SL 1501 AND 1502. CUT OUT DAMAG ED AREA, DEBURRED AND APPLIED ALODINE TO CUT OUT EDGES. PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRA CKS. FABRICATED AN EXTERNAL DOUBLER .050 THICK. ATTACHED DOUBLER TO FUSELAGE, APPLIED EPOXY PRIMER AND ONE COAT OF TOP COAT TO THE INTERIOR AND EXTERIOR SURFACE. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1352 AND SAAB 340 SRM 53-70-10 PAGE 215-216. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500371 19990305 00371 NM 1999 3 5 P2EA99066 1 19990125 A 5320 BEAM BOEING 737 737247 138448D NM BS 695 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - WHEEL WELL LOWER TRANSVERSE BEAM CRACKED AT BS 695, LBL 24.80, BL 0, DEFECT SIZE AVERAGE LENGTH 1.5 INCH. REPLACE D FUSELAGE TRANSVERSE BEAM AT BS 695, BETWEEN LBL 50 INCH AND RBL 50 INCH PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2 PAGE 1 AND 5. (M) 2 L 7 2 4F A16WE 1999030500372 19990305 00372 NM 1999 3 5 P2EA99065 1 19990110 A 5414 FAIRING BOEING 737 737247 138448D NM NR 1 PYLON WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - NR 1 ENGINE LEADING EDGE WORN. REPAIRED NR 1 ENGINE PYLON LEADING EDGE FAIRING PER COOPESA EO C00-3-54-031-99 DAT ED 1-23-99, BOEING FAXES COO-SJO-99-0075RR DATED JAN 1-22-99 AND COO-SJO-99-0083RR DATED 1-2-99. (M) 2 L 7 2 4F A16WE 1999030500373 19990305 00373 NM 1999 3 5 P2EA99064 1 19990109 A 5720 WEB BOEING 737 737247 138448D NM BS 663 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - RIGHT WHEEL WELL SKIN CRACKED AT BS 663, RBL 42, WL 195. DEFECT SIZE, AVERAGE LENGTH 2 INCHES. REPAIRED CENTER W ING SECTION SPAR VERTICAL PRESSURE WEB BETWEEN RBL 37 AND RBL 52, BS 663 FROM WL 190 TO WL 202 PER BOEING FAX COO-SJO-99 0036RR DATED 1-12-99. (M) 2 L 7 2 4F A16WE 1999030500374 19990305 00374 NM 1999 3 5 P2EA99062 1 19990125 A 5320 BEAM BOEING 737 737247 138448D NM BS 706 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - WHEEL WELL LOWER TRANSVERSE BEAM CRACKED AT BS 706, LBL 24.80 AND RBL 24.80. DEFECT SIZE, AVERAGE LENGTH 1.8 INCH ES. REPLACED FUSELAGE TRANSVERSE BEAM AT BS 706, BETWEEN LBL 50 INCH AND RBL 50 INCH PER SRM 51-10-1, PAGE 5 AND SRM 51 -30-2, PAGE 1 AND 5. (M) 2 L 7 2 4F A16WE 1999030500375 19990305 00375 NM 1999 3 5 P2EA99061 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM BS 907-952 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - PROVISIONAL REPAIRS FROM BS 947 TO BS 927, BETWEEN STRINGER 19 LEFT AND STRINGER 20 LEFT. REPAIRED FUSELAGE SKIN SECTION FROM BS 907 TO BS 952, FROM STRINGER 18 LEFT TO STRINGER 20 LEFT PER COOPESA EO C00-3-53-025-99 DATED JAN 22, 19 99 AND BOEING FAX COO-SJO-99-0067RR DATED JAND 21, 1999. (M) 2 L 7 2 4F A16WE 1999030500376 19990305 00376 NM 1999 3 5 P2EA99063 1 19990108 A 5720 ANGLE BOEING 737 737247 138448D NM RT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - RIGHT WING SPAR VERTICAL ANGLE CRACKED AT FSS 268. DEFECT SIZE, LENGTH .5 INCH. REPLACED FRONT SPAR VERTICAL ANG LE AT FSS 268 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2, PAGE 5. (M) 2 L 7 2 4F A16WE 1999030500377 19990305 00377 NM 1999 3 5 P2EA99060 1 19990121 A 5720 ANGLE BOEING 737 737247 138448D NM RT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - RIGHT WING FRONT SPAR ANGLE CRACKED AT FSS 270. DEFECT SIZE, LENGTH .5 INCH. REPLACED RIGHT WING FRONT SPAR ANGL E AT FSS 270 PER SRM 51-10-1, PAGE 5. (M) 2 L 7 2 4F A16WE 1999030500378 19990305 00378 EU 1999 3 5 SIMA990334 1 19990202 A 5413 LONGERON SAAB SF340 340B 7860101 EU RT NACELLE PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 202KD 340B202 ABI - DURNG MBV INSPECTION, A PUNCTURE DUE TO CHAFING WAS DISCOVERED IN RIGHT NACELLE OUTBOARD LOWER LONGERON AT NS 289. 33. BLENDED DAMAGED SURFACE TO VERY FINE SURFACE TEXTURE. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FAB RICATED REINFORCEMENT ANGLE. APPLIED SURFACE TREATMENT ON THE EDGE OF THE DAMAGE AND THE REINFORCEMENT ANGLE. INSTALLE D ANGLE IN NACELLE. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500379 19990305 00379 EU 1999 3 5 SIMA990335 1 19990202 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 202KD 340B202 ABI - DURING MBV INSPECTION, A DENT WAS DISCOVERED IN THE LEFT FUSELAGE CABIN SKIN JUST AFT OF THE ICE SHIELD BETWEEN ST ATION 339 AND STATION 363 AND BETWEEN SL 1515 AND SL 1516. STRAIGHTENED DENT OUT TO NORMAL CONTOUR. PERFORMED EDDY CUR RENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED TWO EXTERNAL DOUBLERS .050 THICK ONE MEASURING 4 INCH BY 11.25 INCH A ND THE OTHER MEASURING 5 INCH BY 12.5 INCH. APPLIED SURFACE TREATMENT OF ALODINE AND EPOXY PRIMER TO REPAIR AREAS DOUBL ERS AND CUT EDGES. INSTALLED DOUBLERS TO FUSELAGE. APPLIED SURFACE FINISH. WORK DONE IAW SAAB 340 SRM 53-70-10 PAGE 2 17 FIG 210 AND PAGE 218. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500381 19990305 00381 EU 1999 3 5 SIMA990281 1 19990128 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 425 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 184AE 340B184 ABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON FUSELAGE SKIN STATION 425.5 BETWEEN SL 1501 AND 1502. CUT OUT DAMAG ED AREA, DEBURRED AND APPLIED ALODINE TO CUT OUT EDGES. PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRA CKS. FABRICATED AN EXTERNAL DOUBLER .050 THICK. ATTACHED DOUBLER TO FUSELAGE, APPLIED EPOXY PRIMER AND ONE COAT OF TOP COAT TO THE INTERIOR AND EXTERIOR SURFACES. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1352 AND SAAB 340 SRM 53-70-10 PAGE 215-216. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500382 19990305 00382 EU 1999 3 5 SIMA990265 1 19990126 A 3350 9HB00593312 SIGN SAAB SF340 340B 7860101 EU ROW 8A BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 298AE 340B298 DFW - FLT 3587 - EMERGENCY EXIT SIGN ABOVE SEAT 8A IS UNSECURE. REMOVED AND REPLACED SIGN ABOVE SEAT 8A. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500383 19990305 00383 EU 1999 3 5 SIMA990264 1 19990126 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 432 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 ABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON LEFT UPPER FUSELAGE SKIN AT STATION 432.5 BETWEEN SL 1501 AND 1601. CUT OUT DAMAGED AREA, DEBURRED AND APPLIED ALODINE TO CUT OUT EDGES. PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDI CATIONS OF CRACKS. FABRICATED AN EXTERNAL DOUBLER .050 THICK. CLEANED DOUBLER, APPLIED ALODINE AND ONE COAT OF EPOXY P RIMER. ATTACHED DOUBLER TO FUSELAGE, RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1353 AND SAAB 3 40 SRM 53-70-10 PAGE 215. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500384 19990305 00384 EU 1999 3 5 SIMA990263 1 19990126 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 479 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON LEFT FUSELAGE SKIN AT STATION 479.2 BETWEEN SL 1504 AND 1505. CUT OUT DAM AGED AREA, DEBURRED AND APPLIED ALODINE TO CUT OUT EDGES. PERFORMED EDDY CURRENT INSPECTION WITH NO INDICATION OF CRACK S. FABRICATED AN EXTERNAL DOUBLER .050 THICK. CLEANED DOUBLER AND APPLIED ALODINE AND ONE COAT OF EPOXY PRIMER. INSTA LLED DOUBLER TO AIRCRAFT, RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1353 AND SAAB 340 SRM 53-70 -10 PAGE 215. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999030500385 19990305 00385 EU 1999 3 5 SIMA990262 1 19990126 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 503 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AE 340B391 ABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON LEFT UPPER FUSELAGE SKIN AT STATION 503 BETWEEN SL 1506 AND 1507. C UT OUT DAMAGED AREA, DEBURRED AND APPLIED ALODINE TO CUT OUT EDGES. PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICA TIONS OF CRACKS. FABRICATED TWO EXTERNAL DOUBLERS .050 THICK. APPLIED ALODINE AND ONE COAT OF EPOXY PRIMER. INSTALLED DOUBLERS ON AIRCRAFT. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1353 AND SAAB 340 SRM 53-70-1 0 PAGE 217. (M) 2 L 7 2 4T RT A52EU 1999030500386 19990305 00386 EU 1999 3 5 SIMA990222 1 19990122 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RI GHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500387 19990305 00387 EU 1999 3 5 99ZZZM160 1 19990122 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RI GHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500388 19990305 00388 EU 1999 3 5 99ZZZM161 1 19990122 A 5347 S5367800121002 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RI GHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500389 19990305 00389 EU 1999 3 5 99ZZZM162 1 19990122 A 5347 S5367000120102 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE RI GHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO 5300-013R2. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500390 19990305 00390 EU 1999 3 5 SIMA990221 1 19990122 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT OUTBOARD SEAT TRACK FLOORBEAM 35 DAMAGED. SPLICED FLOORBEAM IAW SRM 53-00-00 FIGURE 438. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500391 19990305 00391 EU 1999 3 5 SIMA990211 1 19990121 A 5330 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 13-14 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 ABI - AIRCRAFT ARRIVED FOR REPAIR OF DAMAGE ON LEFT FUSELAGE SKIN PANEL BETWEEN FRAMES 13 AND 14 DAMAGED JOINT STRIGNERS 10 AND 11. REMOVED DAMAGED JOINT STRINGERS 10 AND 11. RECONTOURED SKIN PANEL BETWEEN FRAMES 13 AND 14 AND PERFORMED A N EDDY CURRENT INSPECTION WITH NO CRACKS FOUND. FABRICATED AN EXTERNAL DOUBLER .063. TREATED DOUBLER AND JOINT STRINGE RS WITH ALODINE AND ONE COAT OF PRIMER. INSTALLED DOUBLER AND STRINGERS. APPLIED POLYURETHANE TOP COAT TO EXTERNAL AND INTERNAL SURFACES FO REPAIR AREA. APPLIED WATER REPELLENT PROTECTIVE COATING TO INNER REPAIR AREA. WORK DONE IAW ATR SRM 53-00-00 PAGE 418-421, FIG 405. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500392 19990305 00392 EU 1999 3 5 TY7A9901 1 19990102 A 3230 RETRACT MECH STBROS SD3 SD360 8100606 EU LANDING GEAR MALFUNCTIONED A TY7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 350TA SH3757 TAKEOFF, GEAR FAIL TO RETRACT, EMERGENCY HANDLE APPEARED TO BE SLIGHTLY OUT OF POS 3 GREEN LIGHTS CONFIMRED DOWN/LOCKED, LANDED FOR VERIFICATION. RESET LANDING GEAR EXTENSION HANDLE PER MM 32-30-00. VISUALLY VERIFIED POSITION OF 3-WAY VAL VE AT R/T STUB WING TEST FLIGHT A/C LANDING GEAR SYSTEM OPERATES NORMAL. REF LOG PAG 000703. (M) 2 H 7 2 4T A41EU 1999030500393 19990305 00393 WP 1999 3 5 ASAA9980020 1 19990115 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP ROW 13-15 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 15 ILLUMINATE WHEN ELECTRIC POWER IS TURNE D OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999030500394 19990305 00394 WP 1999 3 5 ASAA9980021 1 19990117 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999030500395 19990305 00395 WP 1999 3 5 ASAA9980022 1 19990117 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP ROW 24-28 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 28 WRE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999030500396 19990305 00396 WP 1999 3 5 ASAA9980023 1 19990118 A 3350 GROUND DOUG DC9 DC982 3022082 WP COCKPIT CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - AFTER ARRIVAL OF FLIGHT 731, CREW REPOTED THE OVERHEAD EMERGENCY LIGHT IN THE FLIGHT COMPARTMENT WAS DIM. CLEANED CORROSION FROM GROUND STUD 128 ON OVERHEAD PANEL AND OPERTED NORMALLY. (M) 2 L 7 2 4F A6WE 1999030500397 19990305 00397 WP 1999 3 5 ASAA9980024 1 19990119 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 1493 53063 PDX - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999030500398 19990305 00398 WP 1999 3 5 ASAA9980025 1 19990119 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERTED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999030500399 19990305 00399 1999 3 5 ASAA9980026 4 19990119 A 2565 D29982107 SLIDE AIRCRUISERS DOUG DC9 DC983 3022083 WP R1 DOOR FAILED TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 0099 53076 OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1999030500400 19990305 00400 WP 1999 3 5 ASAA9980027 1 19990122 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT GALLEY WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999030500401 19990305 00401 NM 1999 3 5 ASAA9910005 1 19990123 A 5210 COVER BOEING 737 737298C 1384490 NM L1 DOOR OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 ANC - PRIOR TO FLIGHT 41, THE L1 DOOR WOULD NOT CLOSE AND LATCH. REMOVED L1 DOOR UPPER HINGE COVER AND DOOR OPERATED NO RMALLY. (M) 2 L 7 2 4F RT A16WE 1999030500402 19990305 00402 NM 1999 3 5 ASAA9910006 1 19990126 A 3260 SWITCH BOEING 737 737290C 138448V NM NLG ICED UP A ASAA O OTHER L NO TEST CR CRUISE 1 NM 01 742AS 23136 ANC - FLT 65 - WHEN SELECTING THE OFF POSITION WITH THE GEAR LEVER, THE NOSE GEAR EXTENDS. WHEN SELECTING THE UP POSITI ON, THE RED NOSE GEAR LIGHT ILLUMINATES, BUT THE NOSE GEAR AND MAIN GEAR RETRACTED. INSPECTED AND FOUND THE NOSE GEAR A ND GRAVEL DEFLECTOR SLED ICED UP. DEICED NOSE GEAR AND SKIN. JACKED AND SWUNG GEAR, OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999030500404 19990305 00404 1999 3 5 COEA9901720 3 19990201 A 6140 MK5327R SWITCH FOKKER F27 F27MK500 4990629 EU NR 1 ENGINE MALFUNCTIONED A COEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 13 720FE 33308 14403 10464 DURING TAKEOFF ROLL, THE AUTOFEATHER LIGHT AND BELOW FLIGHT FINE LIGHT ON THE NR 1 ENGINE FLASHED SEVERAL TIMES. PILOT ABORTED TAKEOFF AND TAXIED TO RAMP, NO ASSISTANCE REQUIRED. MAINTENANCE TROUBLESHOT PROP SYSTEM. SERVICED ENGINE OIL A ND PERFORMED TWO ENGINE RUNS, BOTH SATISFACTORY. AIRCRAFT RETURNED TO SERVICE AS A PRECAUTION THE LOW TORQUE SWITCH WA S REMOVED AND REPLACED. (M) 2 H 7 2 4T A817 1999030500405 19990305 00405 NM 1999 3 5 USAABB99004 1 19990126 A 2120 AIR DIST BOEING 767 767201 1385125 NM CABIN ODOR A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 649US 23901 PHL - FLT 15 - CREW REPORTED STRONG BURNING ODOR APPROXIMATELY TEN MINUTES PRIOR TO LANDING. FLIGHT CONTINUED TO PHL AN D LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE COCKPIT, GALLEY, E/E BAY AND BOTH PACK BAYS. THE PACKS WE RE OPERATED FROM BOTH THE ENGINES AND APU. NO DISCREPANCIES OR ODORS WERE FOUND. (M) 2 L 7 2 4F RT A1NM 1999030500406 19990305 00406 EU 1999 3 5 SIMA990097 1 19990109 A 2611 CG7G010 SMOKE DETECTOR AEROSP ATR72 ATR72212 EU E/E COMPT MALFUNCTIONED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 440AM 2196 440 FLT 9724 - CRP - ELECTRICAL SMOKE INDICATION ON CWP ILLUMINATED. FERRIED AIRCRAFT TO DFW FOR REPAIR. REMOVED AND REPLA CED AVIONICS EXTRACTION FAN AND SMOKE DETECTOR. PERFORMED OPERATIONAL TESTS AND TEST FLIGHT WITH NO FURTHER SMOKE INDIC ATIONS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500407 19990305 00407 EU 1999 3 5 99ZZZM164 1 19990109 A 2121 011260500 FAN AEROSP ATR72 ATR72212 EU E/E COMPT FAILED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 440AM APK631 440 FLT 9724 - CRP - ELECTRICAL SMOKE INDICATION ON CWP ILLUMINATED. FERRIED AIRCRAFT TO DFW FOR REPAIR. REMOVED AND REPLA CED AVIONICS EXTRACTION FAN AND SMOKE DETECTOR. PERFORMED OPERATIONAL TESTS AND TEST FLIGHT WITH NO FURTHER SMOKE INDIC ATIONS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500408 19990305 00408 WP 1999 3 5 G6OA030 1 19990121 A 2510 SEAT DOUG DC10 DC1030F 3023504 WP COCKPIT SMOKING A G6OA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 601GC 47929 EN ROUTE FROM LSB TO SNN, THE FLIGHT CREW NOTICED A SMOKE ODOR AND SMOKE COMING FROM THE FLIGHT ENGINEER SEAT BASE. THE FLIGHT ENGINEER SEAT CONTROL CIRCUIT BREAKERS WERE OPENED. THE ODOR AND SMOKE CLEARED. AIRCRAFT CONTINUED ON MEL 25-1 . (M) 2 L 7 3 4F RT A22WE 1999030500409 19990305 00409 NM 1999 3 5 GAIA9909 1 19990129 A 3260 CONNECTOR BOEING 727 727222 1384073 NM NLG LOOSE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 90AX 20040 ON TAKEOFF, WITH GEAR RETRACTED, FLYING OUT OF HUF EN ROUTE TO IAH, THE GEAR DOOR LIGHT ON THE FRONT AND THE F/E'S AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. THE AIRCRAFT DIVERTED TO MCI AND LANDED WITHOUT FURTHER DIFFICULTIES. INSP ECTION OF THE NOSE GEAR AREA FOUND THE CANNON PLUG FOR THE NOSE GEAR POSITION SWITCH HAD BACKED OFF THE SWITCH AND HAD B ECOME DISENGAGED. INSPECTED THE CANNON PLUG AND NO DEFECTS WERE NOTED. REINSTALLED THE CANNON PLUG TO THE SWITCH AND O PERATIONALLY CHECKED THE SYSTEM AND FOUND TO BE NORMAL IAW MM 32-60. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999030500410 19990305 00410 NM 1999 3 5 EISA99005 1 19990120 A 2130 10251871 PRESS CONTROL BOEING 727 727223 1384074 NM COCKPIT FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 313NE 19702 CLIMBING THROUGH 10,000 FEET, CABIN PRESSURIZATION BECAME UNCONTROLLABLE IN AUTO OR MANUAL. REMOVED AND REPLACED AUTO P RESSURE CONTROL AND MANUAL PRESSURE CONTROL. SYSTEM OPS CHECK GOOD IAW MM 21-30-0. (M) 2 L 7 3 4F A3WE 1999030500412 19990305 00412 NM 1999 3 5 EISA99002 1 19990112 A 2130 7248272 VALVE BOEING 727 7272M7 138407S NM LEFT MALFUNCTIONED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 721RW 21200 CLIMBING THROUGH FL 27 RED CARGO DOOR LIGHT ILLUMINATED. RED DOOR WARNING LIGHT AND AMBER HOOKS UNLOCKED LIGHT ILLUMINA TED ON POWER MASTER CONTROL. LOUD BANG HEARD BEFORE RED CARGO DOOR ILLUMINATED. HIGH CABIN DIFFERENTIAL PRESURE (8) HA D TO CLOSE CABIN HEAT OUTFLOW VALVE TO MAINTAIN PRESSURIZATION AT 2,500 LIGHTS EXTINGUISHED. FOUND LEFT PRESSURE RELIEF VALVE OPENING AT (8.25) DIFFERENTIAL PRESSURE. REPLACED VALVE. CHECKED NORMAL PER MM 21-30-0. FOUND HOOK UNLOCK SWIT CHES ON MAIN CARGO DOOR OUT OF ADJUSTMENT. ADJUSTED SWITCHED PER AERONAUTICAL ENGINEERS MM CHAPTER 5. OPS CHECK NORMA L. (M) 2 L 7 3 4F A3WE 1999030500414 19990305 00414 WP 1999 3 5 AALA990069 1 19990117 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 599AA 53289 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999030500415 19990305 00415 WP 1999 3 5 AALA990063 1 19990114 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7518A 49895 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPLACED SPLICE IN EMERG ENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500416 19990305 00416 NE 1999 3 5 AALA990064 2 19990114 A 7250 500588701 STATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE RT ENGINE FAILED A AALA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 7542A 49996 717390 DFW - FLT 1171 - DURING CLIMB-OUT AT 20,000 FT F/A REPORTED LOUD NOISE. 5 MINUTES LATER, AT 31,000 WHILE LEVELING OFF, RT ENGINE HAD 3 MAJOR COMPRESSOR STALLS THEN ENG FAILED TO PRODUCE POWER. ACCOMP EMERG DIVERSION TO DFW. RAN ENG TO ID LE TO TOUCHDOWN, ENG COULD NOT PRODUCE ANY POWER WITH THROTTLE MOVEMENT. OIL PRESS WAS NORMAL AND RT OIL TEMP HIGH AT 1 30 DEGREES. REPLACED RT ENG, PERFORMED ENG RUN UP. SYSTEM GROUND CHECKED NORM OPS.INSPECTION OF THE ENG REVEALED VERY HEAVY DAMAGE TO THE FAN BLADES. THE FAN HADAPPROX 10 FAN BLADES WITH DAMAGE THAT APPEARED TO BE CAUSED BY ICE INGESTI ON. THE DAMAGE CONSISTED OF HEAVY TIP CURL, THE WORST HAD APPROX 1.5 INCH DEFLECTION WITH NO NICK OR TEARS. THE HEAVY 2 L 7 2 4F 4 F A6WE E9NE 1999030500417 19990305 00417 NM 1999 3 5 AALA990054 1 19990113 A 2130 711002 PANEL BOEING 727 727223 1384074 NM COCKPIT MALFUNCTIONED A AALA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 SW 07 877AA 21389 ORD - FLT 814 - EN ROUTE TUL-ORD, DURNG CRUISE, AUTO CONTROLLER FAILED PRIOR TO SWITCHING MANUALLY TO STANDBY MODE. CAB IN OXYGEN MASKS WERE DEPLOYED. LANDED ORD WITHOUT FURTHER INCIDENT. TROUBLESHOT SYSTEM AND COULD NOT DUPLICATE ON GROU ND. PRECAUTIONARY REPLACED CABIN PRESSURE CONTROL PANEL. SYSTEM GROUD CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500418 19990305 00418 WP 1999 3 5 AALA990065 1 19990113 A 5230 5912494301 PANE DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 447AA 49473 TUL - FOUND DOOR BEAM PAN CORRODED FROM STATION 370-427. CUT OUT FORWARD CARGO DOOR PANE AND REPAIRED PER SRM 53-05 FIG 44 SHEETS 1-5. (M) 2 L 7 2 4F A6WE 1999030500419 19990305 00419 WP 1999 3 5 AALA990114 1 19990128 A 2781 833703 SENSOR DOUG DC9 DC982 3022082 WP LT WING LACK OF LUBE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 7531A 49923 DFW - FLT 1821 - DURING CLIMB-OUT, SLATS WERE RETRACTED AND A SLAT DISAGREE LIGHT ILLUMINATED. CREW RAN CHECKLIST AND R ETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FUOND SENSOR ON LEFT WING STUCK. SENSOR WAS LUBRICATED AND OPS CHECKED NORMAL. OVERWEIGHT LANDING WAS ACCOMPLISHED WITH NO ABNORMAL FINDINGS. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999030500420 19990305 00420 NM 1999 3 5 UIEA9902 1 19990128 A 7830 TURNBUCKLES BOEING 747 7472D7B 1384803 NM NR 3 TR UNIT FAILED A UIEA O OTHER O OTHER LD LANDING 1 EA 15 526MC 22337 DURING LANDING WITH REVERSE ACTIVATED, NR 3 THRUST REVERSER LEVER SNAPPED FORWARD AND NR 3 ENGINE STAYED IN FULL REVERSE R. UNABLE TO REDUCE TO IDLE REVERSE. ENGINE SHUT DOWN. FOUND THE TURNBUCKLES FOR PUSH PULL CONTROL CABLE AT T3A-4 AND T3B-4 HAD COME APART. TURNBUCKLES RECONNECTED AND FULL RIGGING CHECK ACCOMPLISHED IAW MM 76-11-00. ENGINE RUN UP AND THRUST REVERSER OPERATION NOW NORMAL. (M) 2 L 7 4 4F RT A20WE 1999030500421 19990305 00421 NM 1999 3 5 USAASB99020 1 19990125 A 3350 71080201 POWER UNIT BOEING 737 7374B7 1384702 NM PAX DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 TPA - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD MAIN ENTRY DOOR ESCAPE SLIDE, THE ESCAP SLIDE DEPLOYED NORMALLY BUT THE ESCAPE SLIDE MOUNTED EMRGENCY LIGHTS FAILED TO ILLUMINATE. ESCAPE SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOU ND THE POWER UNIT ASSEMBLY FOR THE ESCAPE SLIDE MOUNTED EMERGENCY LIGHTS HAD FAILED. MAINTENANCE REMOVED AND REPLACED T HE FORWARD MAIN ENTRY DOOR ESCAPE SLIDE. TWO ADDITIONAL CHECKS ARE SCHEDULED TO BE CONDUCTED AT THE FORWARD MAIN ENTRY DOOR POSITION. (M) 2 L 7 2 4F RT A16WE 1999030500422 19990305 00422 EU 1999 3 5 VTZA99012 1 19990110 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 477UE 890 FLT 6418 - CLE-IAD - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRA FT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 43219 MEL 52-2. MAINTENANCE CLOSED DMI 43219 ON 1-10-99 BY CLEANING AND LUBING PASSENGER DOOR MICROSWITCHES OPS CHECK OK. AIRCRAFT WAS APPROVED AND RELEAS ED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999030500423 19990305 00423 EA 1999 3 5 VTZA99011 1 19990110 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A VTZA K NONE N FALSE WARNING AP APPROACH 1 EA 27 630BR 7255 FLT 6684 - FAR-ORD - DURING APPROACH, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP FAULT MESSAG E ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED AD 98-20-01 REV 1 A ND COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999030500424 19990305 00424 EU 1999 3 5 VTZA99010 1 19990108 A 3213 AIR830901 STRUT JETAIR JETSTM JETSTM4101 1500501 EU LT MLG REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 324UE 41017 FLT 6483 - IAD-CHS - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SERVICED LEFT MAIN LANDING GEAR STRUT AND PERFORMED GEAR SWING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999030500425 19990305 00425 EA 1999 3 5 VTZA99009 1 19990107 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 631BR 7261 FLT 6730 - SAV-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP FAIL MESSAG E ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED AD 98-20-01 REV 1 A ND COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999030500426 19990305 00426 EU 1999 3 5 VTZA99008 1 19990105 A 3222 STRUT BAG JETSTM JETSTM3201 1500217 EU NLG REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 476UE 884 FLT 6377 - IAD-CRW - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO NOSE GEAR INTRANSIT WARNING LIGHT STAYED ON. AI RCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPACKED NOSE LANDING GEAR STRUT. OPS CHEC K OK. AIRCRAFT WAS APPROVED AND RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999030500427 19990305 00427 WP 1999 3 5 VTZA99007 2 19990105 A 7260 1379035H427 PIPE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 480UE 894 FLT 6247 - IAD-BGM - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL SUCTION LINE. OIL PRESSURE TRANSD UCER AND OIL PRESSURE SWITCH, OPS CHECK OK. AIRCRAFT WAS APPROVED AND RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999030500428 19990305 00428 EU 1999 3 5 99ZZZM165 1 19990105 A 7931 1241013 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 480UE 894 FLT 6247 - IAD-BGM - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL SUCTION LINE. OIL PRESSURE TRANSD UCER AND OIL PRESSURE SWITCH, OPS CHECK OK. AIRCRAFT WAS APPROVED AND RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999030500429 19990305 00429 EU 1999 3 5 99ZZZM166 1 19990105 A 7931 1106P0208 SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 480UE 894 FLT 6247 - IAD-BGM - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL SUCTION LINE. OIL PRESSURE TRANSD UCER AND OIL PRESSURE SWITCH, OPS CHECK OK. AIRCRAFT WAS APPROVED AND RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999030500430 19990305 00430 1999 3 5 VTZA99005 4 19990103 A 3425 7003360948 AHRU JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 312UE 41025 FLT 6603 - IAD-EWR - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO NR 2 AHRU FAILURE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER PROBLEM. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 2 AHRU, OPS CHECK OK. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999030500431 19990305 00431 EA 1999 3 5 VTZA99004 1 19990103 A 3010 AOA HEAT CNDAIR CL600 CL6002B19 EA RIGHT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 630BR 7255 FLT 6795 - IAD-RSW - DURING TAKEOFF, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO RIGHT AOA HEAT CAUTION ILLUMINATED. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE (M) 2 L 7 2 4F RT A21EA 1999030500432 19990305 00432 EU 1999 3 5 VTZA99002 1 19990103 A 5610 14156002409 WINDHIELD JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT CRACKED A VTZA B EMER. DESCENT O OTHER CR CRUISE 1 EA 27 308UE 41023 FLT 6222 - JFK-IAD - DURING CRUISE, MADE AN EMERGENCY DESCENT DUE TO CAPTAINS WINDSCREEN CRACKED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED CAPTAINS WINDSCREEN. MAINTENANCE PERFORM ED PRESSURE CHECKS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999030500433 19990305 00433 EU 1999 3 5 VTZA99001 1 19990101 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR LACK OF LUBE A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 488UE 907 FLT 6601 - BWI-IAD - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO PASSSENGER DOOR WARNING LIGHT ILLUMINATED. ACFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 44130, MEL 52-3. MAINTENANCE CLOSED D MI 44130 ON 1-1-99 BY LUBING PASSENGER DOOR HANDLE MICROSWITCH. OPS CHECK OK. (M) 2 L 7 2 4T RT A56EU 1999030500441 19990305 00441 NM 1999 3 5 TSAA9953054 1 19990119 A 5320 BRACKET BOEING 737 7372Q9 138448M NM BS 500 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 SUSPECTED CRACK AT BS 500A STRINGER 25R AT Z-CHANNEL IN FORWARD CARGO PIT. REPLACED BRACKET AS PER SRM 53-10-10. (M) 2 L 7 2 4F A16WE 1999030500455 19990305 00455 CE 1999 3 5 99ZZZX793 1 19990204 A 3010 DEICER BEECH 99 99 1154002 CE VERT STABILIZER WORN A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 14MN U59 DURING A ROUTINE INSPECTION OF AIRCRAFT, NOTICED THE VERTICAL SURFACE DEICER HAD NUMEROUS PATCHES AND SURFACE WEATHER CH ECKING CRACKS BETWEEN PATCHES. AS THE CRACKS WOULD ALLOW WATER TO TRAVEL UNDER PATCHES, IT WAS DETERMINED THE DEICER SH OULD BE REPLACED. THE AGE OF THE BOOT AND/OR CONDITIONS OPERATED IN MAY HAVE CONTRIBUTED TO AN ACCELERATED WEAR PATTERN . THIS COMPANY PAYS PARTICULAR ATTENTION TO THE CONDITION OF SURFACE DEICERS AND APPLIES PRESERVATIVE AS NECESSARY. 1 L 7 2 3T A14CE 1999030500456 19990305 00456 CE 1999 3 5 99ZZZX794 1 19990129 A 2810 5038903412 FUEL CELL BEECH 99 99 1154002 CE RT WING LEAKING A TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 24BH U67 PILOT REPORTS RM FUEL LEAK, FUEL DRIPPING FROM GEAR DOOR. FUEL CELL REMOVED AND TESTED. REPLACED CELL. 1 L 7 2 3T A14CE 1999030500458 19990305 00458 CE 1999 3 5 99ZZZX795 1 19990129 A 2810 5038903412 FUEL CEL BEECH 99 99A 1154003 CE RT WING LEAKING A S TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 955AA U128 PILOT REPORTED EVIDENCE OF FUEL ON RT OUTBOARD GEAR DOOR. INSPECTION REVEALED FUEL LEAK SOURCE AT BOX FUEL CELL JUST OU TBOARD OF NACELLE, AFT OF SPAR. REPLACED FUEL CELL; POST-WORK OPS CHECKS OK. POSSIBLE CAUSE - FUEL CELL AGE AND/OR IMP ROPER INSTALLATION OF CELL. SUBMITTER STATED CELL MAY HAVE NOT BEEN PROPERLY POSITIONED CAUSING WORKING OR FLEXING IN N IPPLE TUBE REA. 1 L 7 2 3T A14CE 1999030500466 19990305 00466 CE 1999 3 5 99ZZZX803 1 19990129 A 2810 5038903412 FUEL CELL BEECH 99 99 1154002 CE RT WING LEAKING A S TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 95WA U6 ON POST-FLIGHT, PILOT REPORTED FUEL LEAKING FROM RT WING FROM GEAR DOOR, FUEL TRACED TO BOX CELL AFT OF SPAR, OUTBOARD O F NACELLE. REPLACED FUEL CELL, POST-WORK OPS CHECKS OK. POSSIBLE CAUSE OF LEAKAGE WAS CONDITION/AGE OF FUEL CELL AND/O R IMPROPER INSTALLATION. 1 L 7 2 3T A14CE 1999030500469 19990305 00469 CE 1999 3 5 99ZZZX806 1 19990208 A 3260 41EN456 SQUAT SWITCH CESSNA 650 650 2076802 CE NLG MALFUNCTIONED A DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 50DS 6500078 GEAR HANDLE WOULD NOT GO UP. TROUBLESHOT TO NOSE GEAR SQUAT SWITCH. REMOVED AND REPLACED SWITCH P/N 41EN45-6. OPERATI ONS CHECKED OK. 2 L 7 2 4F A9NM 1999030500470 19990305 00470 EU 1999 3 5 99ZZZX807 1 19990112 A 3232 125001 ACTUATOR FOKKER F28 F28MK4000 4990810 EU NLG DOOR LEAKING A QXEA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 09 498US 11181 NOSE GEAR DOOR ACTUATOR, MFG MENASCO, LEAKING CAUSING SYSTEM HYDRAULIC FLUID TO DRAIN. CREW HAD TO RELY ON BACKUP SYSTE M TO EXTEND LANDING GEAR DOOR. RE: QXEA. 2 L 7 2 4F RT A20EU 1999030500490 19990305 00490 NM 1999 3 5 HNAA9900029 1 19990225 A 3230 574205 VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR INOP A HNAA K NONE J WARNING INDICATION DE DESCENT 1 EA 07 960HA 326 GEAR WOULD NOT EXTEND ON FIRST TWO ATTEMPTS. REPLACED LANDING GEAR SELECTOR VALVE. 2 H 7 2 4T RT A13NM 1999030500491 19990305 00491 NM 1999 3 5 HNAA9900030 1 19990226 A 3297 WIRE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR LOOSE A HNAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 07 960HA 326 LANDING GEAR WOULD NOT EXTEND, GOT THREE RED LIGHTS. CYCLED HANDLE NUMEROUS TIMES. PERFORMED ALTERNATE GEAR EXTENSION, LANDED NORMAL. RESEATED CONNECTOR ON LANDING GEAR SELECTOR. TIGHTENED LOOSE WIRE ON LANDING GEAR INHIBIT SWITCH AND C ONFIRMED POWER TO LANDING GEAR SELECT HANDLE. 2 H 7 2 4T RT A13NM 1999030500492 19990305 00492 WP 1999 3 5 AT9900144 1 19990114 A 5320 3648583503 BRACKET DOUG DC9 DC932 3022066 WP BS 229 & 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION WITH CORROSION. FIRST, THE CABIN FLOOR PANEL NR 89 ON TH E UNDER SIDE AT FORWARD END. SECONDLY, THE CUSP WEB AND FITTING AT STA 229 LEFT SIDE AROUND RIVETS AND DOUBLER. THIRD, THE PULLEY BRACKET ON STA 965 FLOORBEAM AFT SIDE RBL 22. MECHANICALLY REMOVED ALL CORROSION, REMOVED PULLEY BRACKET, F ABRICATED REPAIR PANEL, COVER PLATES, DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 53-0 1 FIG 1 AND 2, 51-30-7, 53-20-1, AND MM 20-15-0. 2 L 7 2 4F A6WE 1999030500493 19990305 00493 WP 1999 3 5 AT9900145 1 19990112 A 5320 5220700023 SUPPORT DOUG DC9 DC932 3022066 WP BS 935-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS LOCATION CORRODED AND CRACKED. FIRST, THE AFT PIT LOWER SIDE WALL TIEDOWNS COVER ON THE LOWER SIDE. SECONDLY, THE AFT PIT CEILING SUPPORT CORRODED AND CRACKED AT STA 935 TO 996. ALSO, THE GLIDE SLOPE ANTENNA WAS CORRODED. MECHANICALLY REMOVED ALL CORROSION, REMOVED AND REPLACED GLIDE SLOPE ANTENNA, FA BRICATED FIVE STRAPS AND REPAIR SECTION, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 53-21-0, 51-30-2, 51-10-4, 51-10-3, AND MM 34-33-1. SUPPORT (P/N 1A-39286-1), STRAP (P/N 1A-39223-1). 2 L 7 2 4F A6WE 1999030500494 19990305 00494 WP 1999 3 5 AT9900146 1 19990113 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS FLOOR FRAME AT DIFFERENT LOCATIONS CRACKED. FIRST, THE FORWARD CA RGO FLOOR FRAME SCREW HOLE CRACKED/ELONGATED AT STA 237 BETWEEN L-29-30L. SECONDLY, STA 794 FRAME ON THE FORWARD SIDE B ETWEEN L-29-30R. THIRD, THE AFT PIT FRAME AT STA 851 HAS EIGHT CRACKS ABOVE LONGERONS 24L, 27 THRU 29L, 24-25R, AND 28- 29R. LAST, STA 857 FLOOR SUPPORT ANGLE L-29R. REMOVED ALL SUPPORTS AND SPLICES, FABRICATED REPAIR SPLICES, WELDED SUPP ORTS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-3, 51-10-2, 53-11-0, AND EA 12-5321-2 9-C1362. 2 L 7 2 4F A6WE 1999030500495 19990305 00495 NM 1999 3 5 AT9900147 1 19990211 A 5531 SPAR BOEING 737 7372L9 1384497 NM VERT STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 466AT 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE VERTICAL STABILIZER LEFT HAND AFT SPAR AT STA 183 TO 205.5 CORRODED. R EMOVED TWO PANELS TO GAIN ACCESS, REMOVED ALL CORROSION, TREATED, PRIMED AND REINSTALLED PANEL AND SEAL PANELS IAW B737 SRM 51-10-2, 51-10-6, 51-30-7, AND RES NR 99362. 2 L 7 2 4F RT A16WE 1999030500496 19990305 00496 NM 1999 3 5 AT9900148 1 19990211 A 5320 1A432461 SUPPORT BOEING 737 7372L9 1384497 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 466AT 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND SEVERAL FLOORBEAM SUPPORT CORRODED. THE STATION ARE AS FOLLOW: STA 279 L BL 12-27.5L, STA 294.5 BL 32L TO 50.5R, STA 312 LBL 50-RBL16, STA 328 LBL56-RBL 56. TWO FLOORBEAMS (P/N 60-893), FLOORB EAM (P/N 60-8004). 2 L 7 2 4F RT A16WE 1999030500497 19990305 00497 NM 1999 3 5 AT9900149 1 19990218 A 5347 B9C1520792 SEAT TRACK BOEING 737 7372L9 1384497 NM CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 466AT 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON SEAT TRACKS AND AROUND FASTENER HOLES AT THREE DIFFERENT LOCA TIONS. THE LOCATIONS ARE AS FOLLOWS: STA 267-294.5 RBL 41.8, STA 460-480 RBL 48, STA 827-927 LBL 48. MECHANICALLY RE MOVED CORROSION, REMOVED AND REPLACED SEAT TRACKS, FABRICATED SPLICES, AND INSTALLED NEW SECTIONS IAW B737 SRM 53-10-5 P G 5, 53-10-0, 51-30-2, AND 53-10-1 FIG 4. 2 L 7 2 4F RT A16WE 1999030500498 19990305 00498 WP 1999 3 5 AT9900150 1 19990217 A 3350 0L3071BPEGPI LIGHT DOUG DC9 DC932 3022066 WP ROW 24DEF INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 830AT 47723 FOUND THE FLOOR PATH LIGHTING ASSEMBLY MISSING AT ROW 24DEF. INSTALLED SERVICEABLE LIGHT ASSEMBLY IAW MM 33-53-01, OPS CHECKED GOOD. LENS (P/N 07912), SOCKET (P/N 08169-1). 2 L 7 2 4F A6WE 1999030500499 19990305 00499 WP 1999 3 5 AT9900151 1 19990227 A 3397 WIRE DOUG DC9 DC932 3022066 WP AFT LAVATORY BROKEN A ZZDA K NONE O OTHER CL CLIMB 1 SO 15 818AT 47320 FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN THE CABIN AFTER TAKEOFF. RETURNED TO GATE IN ATLANTA. CABIN WARNING SIGN POPS CIRCUIT BREAKER. REPAIRED BROKEN WIRE ON AFT LAVATORY RETURN TO CABIN SIGN IAW MM 33-21. ALL SYSTEMS CHECKED GOO D. 2 L 7 2 4F A6WE 1999030500500 19990305 00500 WP 1999 3 5 AT9900152 1 19990226 A 2130 10315411 VALVE DOUG DC9 DC932 3022066 WP CABIN DEFECTIVE A ZZDA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 SO 15 839AT 47089 LOST CABIN PRESSURE, UNABLE TO CONTROL IT MANUALLY. PASSENGER IN AFT CABIN REPORTED HEARING A POP JUST BEFORE THE MASK DROPPED. FOUND THE AFT CABIN PRESSURE SAFETY VALVE OFF IT'S SEAT. REMOVED AND REPLACED SAFETY VALVE PRESSURE IAW MM 21 -30, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999030500501 19990305 00501 NM 1999 3 5 RAAA99B1002 1 19990223 A 3350 900835A BATTERY PACK GRIMES 1000679 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 MID CABIN OVERHEAD EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999030500502 19990305 00502 NE 1999 3 5 CALA9900196 2 19990227 A 7230 FRAME DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENG COMP CRACKED A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 12064 47862 517398 THE NR 3 ENGINE A AND B FIRELOOP LIGHTS ILLUMINATED AND THE FIRE HANDLE FLASHED AFTER TAKEOFF FROM HNL. CHECKLIST PROCE DURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE N R 3 ENGINE 13TH STAGE MANIFOLD CRACKED. THE NR 3 ENGINE IS BEING REMOVED AND REPLACED. *S/D* ENGINEERING FOUND THE CO MPRESSOR REAR FRAME BOSS TO THE 14TH STAGE CDP CRACKED. 2 L 7 3 4F 4 F A22WE E23EA 1999030500503 19990305 00503 WP 1999 3 5 CALA9900197 1 19990227 A 2161 6273961 CONTROLLER DOUG DC10 DC1030 3023501 WP NR 1 PACK INOP A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14075 46922 THE AIRFLOW FROM PACKS WERE NOT EFFICIENT DURING FLIGHT. THE NR 1 PACK WAS PLACED IN MANUAL AND FLOW WAS ZERO. UPON IN CREASING FLOW ON NR 1 PACK, THE CABIN RATE INCREASED TO 1,000 FEET IN STANDBY AND SMOKE ENTERED THE COCKPIT. THE NR 1 P ACK WAS PUT TO FULL COLD IN MANUAL AND THE SMOKE CEASED. THE AIRCRAFT WAS RETURNED TO SCL WHERE IT LANDED WITHOUT INCID ENT. MAINTENANCE REMOVED AND REPLACED ZONE TEMP CONTROLLER. THE NR 1 ENGINE WAS RUN WITH THE NR 1 PACK AT FULL HOT FOR 45 MINUTES IAW MM 21-60-00 AND NO SMOKE WAS DETECTED. 2 L 7 3 4F A22WE 1999030500504 19990305 00504 NM 1999 3 5 CALA9900198 1 19990228 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND THE LAST FIVE AISLE PATH LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE FOUND A BROKEN WIRE AT AFT BATTERY P ACK. THE WIRE WAS REPAIRED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1999030500505 19990305 00505 WP 1999 3 5 9900679154 1 19990220 A 3350 BATTEIRIES DOUG DC9 DC914 3022034 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTING IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATT ERIES IN POWER SUPPLY AT AFT LEFT LAVATORY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999030500506 19990305 00506 NM 1999 3 5 9900685646 1 19990227 A 2913 3508806 PUMP BOEING 757 757251 1384970 NM RT HYD SYST FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 546US 31080 4850 26493 EN ROUTE PHX-DTW, THE RIGHT HYDRAULIC SYSTEM OVERHEATED. THE RIGHT HYDRAULIC PUMP WAS DEACTIVATED. RIGHT SYSTEM PRESSU RE WAS NORMAL FOR APPROXIMATELY 15 MINUTES THEN THE RIGHT SYSTEM QUANTITY SLOWLY DECREASED TO ZERO. THE FLIGHT DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP AND ITS ASSOCIATED FIL TERS. SYSTEM TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999030500507 19990305 00507 NM 1999 3 5 9900696622 1 19990224 A 2433 60B001775 TR UNIT BOEING 747 747251B 1384892 NM NR 2 BURNED A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 622US 21704 DURING TAXI, THE NR 2 TRANSFORMER RECTIFIER CAUGHT ON FIRE. EXTINGUISHED FIRE WITH FIRE EXTINGUISHER AND TAXIED TO GATE WITHOUT FURTHER INCIDENT. REPLACED THE NR 2 TRANSFORMER RECTIFIER, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999030500508 19990305 00508 NM 1999 3 5 9900706309 1 19990223 A 2560 GIRT BAR BOEING 747 747451 1384940 NM DOOR 5L LOOSE A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 669US 24224 DOOR 5L GIRT BAR WAS FOUND LOOSE AND HANGING INTO SLIP STREAM AFTER TAKEOFF. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOU T INCIDENT. REPLACED DOOR, SLIDE AND REPAIRED SKIN DAMAGE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999030500509 19990305 00509 EA 1999 3 5 COMA9960080 1 19990219 A 2710 272955 LINK CNDAIR CL600 CL6002B19 EA LT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 958CA 7111 LEFT AILERON FAILS BACKLASH CHECKS. REPLACED BOTH PCU LINKS. 2 L 7 2 4F RT A21EA 1999030500511 19990305 00511 EA 1999 3 5 COMA9960082 1 19990219 A 2740 601R751427 BUSHING CNDAIR CL600 CL6002B19 EA RT HORIZ STAB MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 958CA 1509 7111 DURING C-CHECK, FOUND RIGHT ELEVATOR OUTBOARD FLUTTER DAMPENER MOUNT BUSHING MISSING. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999030500512 19990305 00512 EA 1999 3 5 COMA9960083 1 19990228 A 2750 855D1000 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 916CA 2315 7014 FLAP FAIL AT 0 DEGREES IN CLIMB THRU 23,000 FT WITH NO INPUT TO FLAP LEVER SECOND EVENT. INTERROGATED FECU, FOUND RIGHT BPSU FAULT. REMOVED RIGHT BPSU (S/N 522), INSTALLED (S/N 0763A). COMPLIED WITH FLAP EO 27-046AD. 2 L 7 2 4F RT A21EA 1999030500513 19990305 00513 EA 1999 3 5 COMA9960084 1 19990227 A 2750 WARNING CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 916CA 7014 FLAPS FAIL MESSAGE DURING FLIGHT. RESET FLAP SYSTEM, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999030500514 19990305 00514 EA 1999 3 5 COMA60085 1 19990225 A 3350 58351 COVER CNDAIR CL600 CL6002B19 EA ROW 8 MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 EMERGENCY FLOOR TRACK LIGHTING AT ROW 8, IS NOT ORANGE. REPLACED ORANGE COVER. 2 L 7 2 4F RT A21EA 1999030500515 19990305 00515 EA 1999 3 5 COMA9960086 1 19990226 A 3411 PITOT CNDAIR CL600 CL6002B19 EA LEFT DIRTY A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 982CA 7168 AIRSPEED COMPARATOR WARNING DURING TAKEOFF. REMOVED FOREIGN MATERIAL FROM LEFT HAND PITOT HEAD. 2 L 7 2 4F RT A21EA 1999030500516 19990305 00516 NM 1999 3 5 UPS99228767 1 19990219 A 5240 DOOR BOEING 727 727173C 1384059 NM SERVICE DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, MGD OUTER SKIN CORRODED BETWEEN LOWER LT FRAME AND PRE-EXISTING REPAIR DOUBLER. FOUND SKIN CRACKED A ND BLENDED ALL CORROSION, CUT OUT ALL DAMAGED SKIN, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 52-00-3. 2 L 7 3 4F A3WE 1999030500517 19990305 00517 NM 1999 3 5 UPS99228768 1 19990218 A 5241 WEB BOEING 727 727173C 1384059 NM GALLEY DOOR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C WHILE WORKING NRC 890638, FOUND CORROSION ON MID GALLEY DOOR LWR HINGE CAVITY LWR WEB. REMOVED OLD WE B, FABRICATED AND INSTALLED NEW WEB IAW SRM 52-40-1, SRM 51-20-1, SRM 51-30-2, SRM 52-00-2. 2 L 7 3 4F A3WE 1999030500518 19990305 00518 NM 1999 3 5 UPS99228769 1 19990219 A 5241 ANGLE BOEING 727 727173C 1384059 NM GALLEY DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, ATTACH ANGLE FOR LOWER HINGE LOWER WEB CORRODED ON MID GALLEY DOOR. CORROSION FOUND TO BE OUT OF LIM ITS. REMOVED OLD ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 52-00-2, SRM 52-40-1, SRM 51-20-1, SRM 51-30-1. 2 L 7 3 4F A3WE 1999030500519 19990305 00519 NM 1999 3 5 UPS99228770 1 19990217 A 2782 WEB BOEING 727 727173C 1384059 NM NR 6 LE FLAP ACT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, NR 6 K-FLAP ACT MOUNTING STRUCTURE LWR WEB BETWEEN I/B AND O/B MOUNT IS CRACKED. REMOVED OLD WEB AND INSTALLED NEW WEB IAW SRM 51-30-2, SRM 51-20-1, OHM 20-50-01, SRM 51-10-2. 2 L 7 3 4F A3WE 1999030500520 19990305 00520 NM 1999 3 5 UPS99228771 1 19990217 A 5330 SKIN BOEING 727 727173C 1384059 NM BS 214.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, DURING NDI INSPECTION FOUND SKIN TO BE CRACKED AT TWO ADJACENT FASTENERS ON SECTION 41 SKIN, LEFT HAN D SIDE, BS 243.7 WL 214.5, FWD AND AFT FASTENER ROW FASTENERS CRACKED. REMOVED 1 X 3 AREA OF DAMAGED SKIN AND INSTALLED STANDARD DOUBLER AND FILLER REPAIR PER SRM 53-30-3 AND MM 51-20-31, SRM 51-30-8 AND OHM 20-50-01. 2 L 7 3 4F A3WE 1999030500521 19990305 00521 NM 1999 3 5 UPS99228773 1 19990226 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, ALL EMERG EXIT LIGHTS ABOVE WING EXIT DOORS INOP. REMOVED AND REPLACED ALL EMER EXIT LIGHTS BATTER Y PACKS, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999030500522 19990305 00522 EU 1999 3 5 QXEA9900311 1 19990224 A 2612 89345601 FIRE DETECTOR KIDDE FOKKER F28 F28MK4000 4990810 EU APU OUT OF POSITION A QXEA H F DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 NM 09 478US 859 11227 SEA - ON DESCENT AT 10,000 FT STARTED APU, 10 TO 15 SECONDS AFTER INITIAL START TGT HUNG AT ABOUT 400 DEG, UPON TURNING APU MAIN SWITCH OFF APU FIRE LIGHT ILLUMINATED AND EXTINGUISHER LIGHT CAME ON. WENT THROUGH APU FIRE CHECKLIST AND LAND ED WITHOUT INCIDENT. MX INSPECTED AND FOUND NO SIGN OF FIRE OR HEAT DAMAGE. THE APU ENG FIRE SENSING ELEMENT WAS FOUND BENT AND NEARLY TOUCHING THE COMBUSTION SECTION CASING. STRAIGHTENED SENSE ELEMENT TO ORIGINAL CONTOUR. TESTED IN ACCO RDANCE WITH MANUAL, RAN APU CHECKED FOR LEAKS, ALL FUNCTIONS NORMAL. REPLACED APU FIRE EXTINGUISHER CONTAINER, VALVE AN D CARTRIDGE. ALSO REPLACED DISCHARGE INDICATOR THE DISCHARGE LINE (TO THE INDICATOR). 2 L 7 2 4F RT A20EU 1999030500523 19990305 00523 NM 1999 3 5 QXEA9900312 1 19990223 A 2611 473054 DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTION A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 353PH 1038 521 496 PDX- SMOKE LIGHT FLASHED ON AND OFF IN FLIGHT, AND THEN WENT OUT. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FLAMES. REPLACED BOTH THE NR 1 AND NR 2 SMOKE DETECTOR IN THE CARGO COMPARTMENT, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999030500524 19990305 00524 NM 1999 3 5 QXEA9900313 1 19990223 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 363PH 520 SEA- 2 FLOOR EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY 3352 PS2, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999030500525 19990305 00525 NM 1999 3 5 99FDEA00078 1 19990227 A 3232 731414 ACTUATOR BOEING 727 727227 1384078 NM RT MLG DOOR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 482FE 21464 REPEAT, GEAR RETRACT BROUGHT GEAR HANDLE TO OFF AND RED DOOR LIGHT CAME ON. RT GEAR DOOR ON 2ND OFF PANEL, CYCLED ONCE AND LIGHT REMAINED ON. LEFT GEAR HANDLE UP AS PER RED TABS WITH HANDLE IN OFF POS. ALSO, THERE WAS NOISE AND SLIGHT VI BRATION. *S/D* REMOVED AND REPLACED RMG WHEEL WEEL DOOR ACTUATOR PER MM 32-32-0814, OPER CK OK. 2 L 7 3 4F A3WE 1999030500526 19990305 00526 NM 1999 3 5 99FDEA00079 1 19990226 A 3250 TORSION LINKS BOEING 727 72722 1384002 NM NLG STEERING WORN A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 198FE 19154 A/C SHAKES AND DRIFT RIGHT OF CENTER LINE. NOSE WHEEL STEER INOP. REMOVED AND REPLACED UPPER AND LOWER TORSION LINKS P ER MM 32-21-021-4. NOSE GEAR STEERING OPER CK GOOD PER MM 32-51-000-5. 2 L 7 3 4F A3WE 1999030500527 19990305 00527 1999 3 5 MWEA99080 4 19990224 A 3417 2587400176 ADC DOUG DC9 DC932 3022066 WP COCKPIT INOP A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 207ME 47794 ON TAKEOFF AT 20,000 FT THE FIRST OFFICER MAIN ALTIMETER FLAGGED AT 20,000 FT AND THE NEEDLE STUCK THERE. MTC REMOVED A ND REPLACED NUMBER TWO AIR DATA COMPUTER. 2 L 7 2 4F A6WE 1999030500528 19990305 00528 WP 1999 3 5 MWEA99081 1 19990223 A 2130 39271012 VALVE DOUG DC9 DC932 3022066 WP CABIN INOP A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401ME 47133 AIRCRAFT UNABLE TO PRESSURIZE, RETURNED TO MKE. MTC REMOVED AND REPLACED RIGHT AUGMENTATION VALVE. 2 L 7 2 4F A6WE 1999030500529 19990305 00529 NM 1999 3 5 DL76G990324 1 19990217 A 2612 FIRE LOOP BOEING 767 7673P6 1385105 NM NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 155DL 25269 EICAS MSG RT ENG OH LOOP -1- ON AFTER T/O AND STAYED ON. MTC IN PROGRESS. PREV MTC ACTION 17FEB. REPLACED WIRES W5316 -001R AND W5306-002R PINS AND TERMINALS. MSG STILL ON EICAS. REPLACED M690 LOOP -2- CARD, ALL CKS GOOD. RAN ENG, NO F AULTS NOTED. REMOVED MCO AND PLACARD. 2 L 7 2 4F RT A1NM 1999030500530 19990305 00530 NM 1999 3 5 DL72K990333 1 19990219 A 5720 VENT BOX BOEING 727 727232 1384082 NM BS 686.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 417DA 21259 FWD VENT BOX CRACKED AT AFT EAR TO RIB STA 686.5 ATTACH PT. CUT OUT ACCESS HOLE PER MM 57-13-0, FIG 803. DRILLED AFT A ND FWD ANGLE ASSY AND RADIUS FILLER. HFEC CRACK, FOUND CRACK, RUNS FROM BOLT HOLE AFT AND OUTWARD TO EDGE OF FLANGE. D RILLED RADIUS FILLERS PER MM 57-13-0, DRILLED ACCESS COVER. INSTALLED RADIUS FILLERS, FWD ANGLE AND COVER ASSY PER MM 5 7-13-0 804. 2 L 7 3 4F A3WE 1999030500531 19990305 00531 NM 1999 3 5 DL767990334 1 19990218 A 3350 BPS73 POWER SUPPLY BOEING 767 767232 1385132 NM ROW 37 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 102DA 22214 ROW 37 AND BACK EMERGENCY LIGHTS INOP. REPLACED BATTERY SUPPLY PACK M9010, CKS GOOD. 2 L 7 2 4F RT A1NM 1999030500532 19990305 00532 NM 1999 3 5 DLM88990335 1 19990219 A 5754 9955842501 RIB DOUG MD88 MD88 3023688 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 LEFT AND RIGHT NR 3 SLATS CAME TO HMV WITH BROKEN RIBS WHICH ASSIST IN HOLDING AND ADJUSTING THE SLAT POSITION ON THE A/ C. REPLACED SAME. 2 L 7 2 4F RT A6WE 1999030500533 19990305 00533 NM 1999 3 5 DL72K990336 1 19990127 A 5753 652163261 ANGLE BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 36 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAI RED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1999030500534 19990305 00534 NM 1999 3 5 DL72L990338 1 19990219 A 2150 39854021 VALVE BOEING 727 727232 1384082 NM LEFT INOP A DALA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SO 27 503DA 21305 AT FL250 ALTITUDE WARNING HORN WENT OFF WITH CABIN ALT AT 12,000 FT. CREW WENT ON 02, OUTFLOW VALVE SHOWED CLOSED. CAR GO VALVE CLOSED, LT PACK OFF, DUE TO PREVIOUS WRITE UP. FOUND LT PACK VALVE INOP AND LT ACM NOT TURNING. REPLACED LT PACK VALVE AND ACM CKS OK. 2 L 7 3 4F A3WE 1999030500535 19990305 00535 NE 1999 3 5 DLL10990339 2 19990219 A 7320 REGULATOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 1 ENGINE INOP A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 729DA 50566 10282 193C1180 10282 ABORTED TAKEOFF AT 60 KNOTS DUE TO FLUCTUATION OF NR 1 ENG INSTRUMENTS. ON STATIC R/U N1 EGT N3 THROTTLE POSTION ALL AT TAKEOFF EPR ONLY REACHED 1.365. REPLACED NR 1 ENGINE FFR AND PERFORMED ENGINE RUN PER PFHB, ALL CHECKS GOOD. 2 L 7 3 4F 4 F A23WE E12EU 1999030500536 19990305 00536 WP 1999 3 5 DLL19990340 1 19990219 A 3397 WIRE LKHEED 1011 10113853 5265020 WP ROW 21F BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 193H1216 STRIP OF EVAC LIGHTS INOP FWD RT SECTION OF C-ZONE. FOUND WIRE BROKEN UNDER SEAT 21F. SPLICED WIRE, CHECKS GOOD. 2 L 7 3 4F A23WE 1999030500537 19990305 00537 NM 1999 3 5 DLM11990342 1 19990219 A 3350 BULB DOUG MD11 MD11 3023602 NM ROW 10JH FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 811DE 48566 EMERGENCY LIGHTS AT 10 JH WILL NOT ILLUMINATE. REPLACED BULBS, OPS CK NORMAL. 2 L 7 3 4F RT A22WE 1999030500538 19990305 00538 WP 1999 3 5 DLL19990343 1 19990221 A 3350 CHARGER 5165741 LKHEED 1011 10113853 5265020 WP LEFT FAILED A DALA K NONE L NO TEST CR CRUISE 1 SO 27 768DL 54053 193H1216 CB J8 EMERG CHARGE LIGHT AFT TRIPS. FOUND CHARGER BAD. REPLACED SAME. 2 L 7 3 4F A23WE 1999030500539 19990305 00539 NM 1999 3 5 DL72L990344 1 19990110 A 5320 WEB BOEING 727 727232 1384082 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 ROUTED OUT .125 INCH CRACK IN 48 SECTION TORQUE BOX WEB RT SIDE AT LIGHTNING HOLE FWD OF STA 1243 PER M/M 53-11-0 PG 8 28. 2 L 7 3 4F A3WE 1999030500540 19990305 00540 NM 1999 3 5 DL73K990345 1 19990221 A 2424 948F4582 GCU BOEING 737 737232 1384475 NM LT & RT MALFUNCTIONED A DALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 314DA 23086 ON CLIMBOUT, APU OFF BOTH GEN ON, RECEIVED A SPIKE. LOST ALL ELECTRICAL PWR IN COCKPIT AND CABIN FOR A SPLIT SECOND. N O C/B POPPED, NO EQUIP LOSS. INSPECTED LT AND RT GEN HARNESS, NTF INSPEC ENG GEN AND BUSS TIE BREAKERS. NTF RAN GCU DI ODE TEST, BATTERY TEST AND STB POWER TEST, ALL PASSED. REPLACED LT AND RT ENG GCU. A/C PWR CKS NORMAL. GCU NR 1 (S/N ZG623) OFF. GCU NR 2 (S/N ZB3038DH) OFF. 2 L 7 2 4F RT A16WE 1999030500541 19990305 00541 NM 1999 3 5 DL757990346 1 19990221 A 3350 BATTERY PACK BPS73 BOEING 757 757232 1384965 NM BS 370 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 676DL 479 25981 ON INSPECTION, FOUND FIRST CLASS CENTER AISLE EMERGENCY LIGHTS INOP. FOUND BATTERY RACK INOP. REPLACED BATTERY RACK M9 001, LIGHTS CHECK NORMAL. 2 L 7 2 4F RT A2NM 1999030500542 19990305 00542 NM 1999 3 5 DL76L990347 1 19990222 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1557 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 179DN 25144 DENT IN SKIN AT STA 1557 BETWEEN STRINGERS 18R AND 19R. DAMAGE TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER AND TRIPLER W AS INSTALLED. ACTION TAKEN, ERA 267532-14 REV B. 2 L 7 2 4F RT A1NM 1999030500543 19990305 00543 NM 1999 3 5 DL72S990348 1 19990221 A 2913 PUMP AS19570C BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 407DA 149438 21151 700702 B-SYSTEM HYD WENT TO 0, FOLLOWED PROCEDURES. WHEN GEAR EXTENDED HYD PRESS WENT TO 1700 PSI. OPERATED BRAKE INTERCONNEC T, USED PNEUMATIC BRAKES TO STOP. TOWED ACFT TO GATE FROM RUNWAY. FOUND NR 2 B-HYD PUMP LEAKING. REPLACED SAME AND FI TTINGS, LEAK CKS OK. CHARGED XFER TUBE AND SERVICED PNEUMATIC BOTTLE. 2 L 7 3 4F 4 F A3WE E2EA 1999030500544 19990305 00544 NM 1999 3 5 DL72S990349 1 19990222 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 11 BROKEN A QS7R K NONE L NO TEST CR CRUISE 1 SO 27 539DA 999 22385 EMERGENCY TRACK LIGHTING INOP FROM ROW 11 FWD. REPAIRED WIRES AS PER WDM 33-51-03 AND CHAP 20. FOUND POWER SUPPLY M902 6 BAD. REPLD SAME, TRACK LIGHT OPN CKS NORMAL. 2 L 7 3 4F A3WE 1999030500545 19990305 00545 NE 1999 3 5 DL757990351 2 19990222 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE BIRD STRIKE A DALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 27 682DA 37658 716304 26958 716304 ON T/O, A/C HIT FLOCK OF BIRDS. REPLACED RT NOSE LAND AND TAXI LIGHT AND RT WING STATIC WICK. C/W BIRD STRIKE INSPECTI ON. REPLACED VOICE REC, NR 1 AND 2 ENG FAN BLADES AND PERFORM VIBRATION SURVEY PER PFHB. 2 L 7 2 4F 4 F RT A2NM E17NE 1999030500546 19990305 00546 NM 1999 3 5 DL72S990352 1 19990222 A 5270 SWITCH AN31671 BOEING 727 727232 1384082 NM AIRSTAIR LOOSE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 484DA 20864 YELLOW AFT AIRSTAIR LIGHT CAME ON DURING TAKEOFF ROLL. FOUND SWITCH (P/N AN3167-1) LOOSE IN BRACKET (P/N 69-20985-6), R EFERENCE IPC 52-70-00-49, ITEM 15 AND 20. TIGHTENED SWITCH, ADJUSTED SWITCH, CHECKS NORMAL. 2 L 7 3 4F A3WE 1999030500547 19990305 00547 NM 1999 3 5 DL72L990353 1 19990222 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM L2 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 511DA 21313 L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999030500548 19990305 00548 NM 1999 3 5 DL72S990354 1 19990205 A 5311 FRAME 6515934 BOEING 727 727232 1384082 NM BS 620 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 STA 620 FRAME UPPER FLANGE AT RBL 8 HAS CRACK IN RADIUS. CRACK TRIMMED OUT AND REPAIR DOUBLER INSTALLED PER ERA 332727- 14. ACTION TAKEN, ERA 332727-14. 2 L 7 3 4F A3WE 1999030500549 19990305 00549 NM 1999 3 5 DL72L990355 1 19990223 A 3340 BEACON G9325A1 BOEING 727 727232 1384082 NM FUSELAGE LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 UPPER ROTATING BEACON CAME OUT OF ITS RETAINER AND FELL AND ROLLED BETWEEN CEILING PANEL AND OVERHEAD COMPARTMENT IN CAB IN CAUSING A PASSENGERS BAG TO BE SCORCHED. NO OTHER DAMAGE. REINSTALLED BEACON, ALL CHECKED OK. 2 L 7 3 4F A3WE 1999030500550 19990305 00550 NM 1999 3 5 DL72S990356 1 19990222 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM R1 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 403DA 4825 21147 ON LAYOVER CK, FOUND R-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER M/M, CKS OK. 2 L 7 3 4F A3WE 1999030500551 19990305 00551 NM 1999 3 5 DL72S990357 1 19990223 A 2782 ACTUATOR 1U1110 BOEING 727 727232 1384082 NM NR 2 LE FLAP FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 495DA 9998DFGKL 21075 SLC- AFTER T/O, LOST -A- SYSTEM HYDRAULIC SYSTEM. FOUND NR 2 L/E FLAP ACTUATOR LEAKING AND ACTUATOR BRACKET BROKEN. RE PLACED SAME. 2 L 7 3 4F A3WE 1999030500552 19990305 00552 NE 1999 3 5 DL73K990358 2 19990223 A 7230 BLADES BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENG COMP DAMAGED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 314DA 23086 709161 AT CRUISE, CREW NOTE COMPRESSOR SURGING. DIVERTED TO BOS. FOUND NOSE BULLET LOOSE. DAMAGE INCURRED TO FIRST AND SECON D STAGE FAN BLADES, NOSE COWL ACCOUSTIC LINER AND N1 TACH GENERATOR HOUSING BULLET MOUNT STUDS. REPLACING 1ST AND 2 ND STAGE FANS, INLET COWL AND N1 TACH GENERATOR GEARBOX AND NOSE BULLET. 2 L 7 2 4F 4 F RT A16WE E2EA 1999030500553 19990305 00553 NM 1999 3 5 DL72S990359 1 19990223 A 2612 FIRE LOOP BOEING 727 727232 1384082 NM NR 2 ENGINE MALFUNCTIONED A DALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 27 539DA 22385 NR 2 ENG SHUT DOWN IN FLIGHT DUE TO FIRE WARNING. FIRST FIRE WARNING AFTER NR 2 ENGINE ANTI ICE TURNED ON. ACCOMPLISHE D SHUTDOWN PROCEDURES FROM HARD CARD CHECKLIST. AFTER 1ST BOTTLE DISCHARGED LIGHT WENT OUT. LIGHT CAME ON AGAIN AFTER FIRE WARNING TEST, DISCHARGED 2ND BOTTLE. REPLACED BOTH FIRE BOTTLES, LOWER ELEMENT AND CONTROLLER PER M/M, PERFORMED G ROUND TEST, OPS GOOD. CHECKED ALL ENG WIRING, UNABLE TO FIND ANY DEFECTS. RAN ENGINE WITH ANTI ICE ON, NO TROUBLE FOUN D. 2 L 7 3 4F A3WE 1999030500554 19990305 00554 NM 1999 3 5 DL72S990360 1 19990224 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1070 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FRAME DENTED LT FS 1070, STR 26L. REMOVED DAMAGED AREA, DYE CHECKED PER PS 900-6-3 NR 1. NO FURTHER DAMAGE FOUND. FAB RICATED DOUBLER, INSTALLED DOUBLER PER SRM 53-10-4 FIG 27. 2 L 7 3 4F A3WE 1999030500555 19990305 00555 NM 1999 3 5 DL72S990361 1 19990224 A 5311 FRAME BOEING 727 727232 1384082 NM BS 950 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950B ABOVE STR 26L. REMOVED DAMAGED PER SRM 53-10-4 FIG 27. DYE PE NETRANT CHECKED PER PS 900-6-3, NO CRACKS NOTED. DRILLED NEW DUCT PER SRM 53-10-4 FIG 27. REMOVED WEB FROM STA 950A TO 950B AT STR 25L. INSTALLED PER SRM 53-10-4 FIG 27. 2 L 7 3 4F A3WE 1999030500556 19990305 00556 NM 1999 3 5 DL72S990362 1 19990223 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 480-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 26L LAP SPLICE BETWEEN FS 48 0 AND 681. INTERNAL HFEC INSPECTION CONFIRMED A TOTAL OF 6 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE LOWER PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366709-14, REV A. 2 L 7 3 4F A3WE 1999030500557 19990305 00557 NM 1999 3 5 DL72S990363 1 19990223 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 12 CRACKS ALONG THE LENGTH OF THE PANEL. THE LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 366741-14, REV A. 2 L 7 3 4F A3WE 1999030500558 19990305 00558 NM 1999 3 5 DL72S990364 1 19990223 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 481 AND 680. INTERNAL HFEC INSPECTION CONFIRMED 31 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUTOUT ALONG THE PAN EL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366712-14, REV A. 2 L 7 3 4F A3WE 1999030500559 19990305 00559 NM 1999 3 5 DL72S990365 1 19990223 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION VERIFIED 27 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE ENTIR E PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366711-14, REV A. 2 L 7 3 4F A3WE 1999030500560 19990305 00560 NM 1999 3 5 DL72S990366 1 19990223 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL OF THE STRINGER 4R LAP SPLICE BETWEEN FS 360 AND 481. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366710-14, REV A. 2 L 7 3 4F A3WE 1999030500561 19990305 00561 NM 1999 3 5 DL72S990367 1 19990223 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 444 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 460 INDICATED A SINGLE CRACK. INTERNAL HFEC INSPE CTION CONFIRMED ONE CRACK ONLY AT FS 444. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED PER THE B727 SRM 53-30- 3, FIG 5. TEN FASTENERS FWD AND AFT OF THE CRACK WERE ADDITIONALLY REMOVED TO ALLOW FOR HFEC SURFACE SCAN WITH NO RIVET TAIL INTERFERENCE. NO OTHER CRACKS WERE NOTED. 2 L 7 3 4F A3WE 1999030500562 19990305 00562 NM 1999 3 5 DL72S990368 1 19990222 A 5330 651752999 SKIN BOEING 727 727225A 1384077 NM BS 1230 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 INCORPORATION OF SKIN DAMAGE INTO MODIFICATION DOUBLER WHILE ACCOMPLISHING A MODIFICATION TO THE AIRCRAFT. INSTALLED FE D-EX HUSHKITS AND EXISTING SKIN REPAIR WAS FOUND TO INTERFER WITH THE INSTALLATION OF A TITANIUM MODIFICATION DOUBLER ON THE SKIN. THE EXISTING REPAIR WAS REMOVED REVEALING A 2 INCH DIA SKIN CUTOUT BETWEEN FS 1223 AND 1243 S-15L & 16L. T HE MOD DOUBLER WAS ENLARGED TO ENCOMPASS AND REPAIR THE DAMAGE PER ER/A 366686-14. 2 L 7 3 4F RT A3WE 1999030500563 19990305 00563 NM 1999 3 5 DL73E990369 1 19990222 A 5330 SKIN BOEING 737 737247 138448D NM BS 955 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 23609 THE FUSELAGE SKIN AND BONDED DOUBLER WERE FOUND WITH A .68 CRACK AT THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT. THE CRACK DID NOT EXTEND INTO THE UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXT ERNAL DOUBLER AND TRIPLER PER B737 SRM 53-30-3, FIG 24. ER/A 366756-14, REV A WAS ISSUED TO ACCOMPLISH THE REPAIR WITH FASTENER DEVIATIONS. 2 L 7 2 4F A16WE 1999030500564 19990305 00564 NM 1999 3 5 DL73E990370 1 19990222 A 5330 SKIN BOEING 737 737247 138448D NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 23609 THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT (R2) WAS FOUND WITH A .26 CRACK IN THE SKIN AND BONDED DOUBLER. TH E UNDERLYING BEAR STRAP WAS NOT DAMAGED. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 21A. ER/A 366755-14, REV B WAS ISSUED TO ACCOMPLISH THE REPAIR WITH FASTENER DEVIATIONS. 2 L 7 2 4F A16WE 1999030500565 19990305 00565 NM 1999 3 5 DL72S990372 1 19990222 A 5330 65545826 SKIN BOEING 727 727232 1384082 NM BS 1100 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. I NTERNAL HFEC INSPECTION CONFIRMED 4 CRACK INDICATIONS AT APPROX FS 1100 WITH NO OTHER CRACK INDICATIONS FOR THE ENTI RE PANEL LENGTH. THE CRACKED AREA OF SKIN WAS TRIMMED OUT AND REPAIRED PER THE B727 SRM 53-30-3, FIG 5. THE REPAIR WAS DOCUMENTED PER ER/A 366742-14. 2 L 7 3 4F A3WE 1999030500566 19990305 00566 NM 1999 3 5 DL73K990373 1 19990220 A 5330 6545778 SKIN BOEING 737 737247 138448D NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE FUSELAGE SKIN AND BONDED DOUBLER AT THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A .25 INCH LONG TYPICAL CRACK IN THE LOWER HINGE CUTOUT. THE UNDERLYING BEAR STRAP WAS NOT CRACKED. THE CRACK WAS ROUTED OUT OF THE SKIN ASSY AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 35. ER/A 366744-14, REV A WAS ISSUED TO ACCOMPLISH THE REPA IR WITH FASTENER DEVIATIONS. 2 L 7 2 4F A16WE 1999030500567 19990305 00567 NM 1999 3 5 DL757990374 1 19990222 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM BS 1694 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 THE FUSELAGE SKIN WAS FOUND WITH A BAD GOUGE AT FS 1694 BETWEEN THE STRINGER 14L SKIN LAP SPLICE AND STRINGER 15L. THE DAMAGE WAS CUTOUT WITH A 3.5 X 1 CUTOUT AND REPAIRED WITH AND EXTERNAL DOUBLER AND FILLER TO OVERLAP THE EXISTING LAP J OINT. THE REPAIR WAS ACCOMPLISHED PER ER/A 366716-14, REV A. 2 L 7 2 4F RT A2NM 1999030500568 19990305 00568 NM 1999 3 5 DL73K990375 1 19990223 A 5330 SKIN BOEING 737 737232 1384475 NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 318DL 23090 THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS .4375 INCH LONG WITH NO CRACKING IN THE UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT OF THE SKIN ASS Y AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 21A. THE REPAIR WAS ACCOMPLISHED WITH FASTENER DEVIAT IONS PER ER/A 366761-14, REV A. 2 L 7 2 4F RT A16WE 1999030500569 19990305 00569 NM 1999 3 5 DLM11990377 1 19990224 A 5242 SEAL DOUG MD11 MD11 3023602 NM E & E DOOR FAILED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 811DE 48566 LOUD VIBRATION UNDER COCKPIT AFTER T/O. FOUND SEAL ON FWD WHEEL WELL TO E/E ACCESS DOOR OUT OF RETAINER AT LT UPPER COR NER AND RT LWR CORNER. REPLACED SAME. 2 L 7 3 4F RT A22WE 1999030500570 19990305 00570 NM 1999 3 5 DL72S990378 1 19990224 A 3510 MS219215C B-NUT BOEING 727 727225A 1384077 NM COCKPIT LOOSE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 8889Z 21858 CREW 02 WENT TO ZERO IN FLIGHT. TIGHTENED LOOSE B-NUT ON REGULATOR 3RD OFFICERS POSITION AND REPLACED O2 BOTTLE, LEAK C HECKS OK. 2 L 7 3 4F RT A3WE 1999030500571 19990305 00571 NM 1999 3 5 DL72S990379 1 19990215 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 SKIN CRACKED EMPENNAGE EXT LOC AT AFT I/B CORNER OF ACCESS PNL 3903 CUTOUT. FABRICATED DOUBLER PER M/M 53-30-0 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER PER MM 53-30-0 PG 803, IDENTIFIED PER PS 900-5-1 NR 4. 2 L 7 3 4F A3WE 1999030500572 19990305 00572 NM 1999 3 5 DL76L990380 1 19990224 A 3350 LIGHT 20131A BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 172DN 8184AND154 24775 ON S/C ITEM 31, EMERGENCY ESCAPE LEFT AND RIGHT WOULD NOT ILLUMINATE IN EITHER TEST 1 OR TEST 2 ON SQUIB TEST PANEL. 2 L 7 2 4F RT A1NM 1999030500573 19990305 00573 NM 1999 3 5 DL72K990381 1 19990222 A 5330 SKIN BOEING 727 727232 1384082 NM L1 DOORWAY GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 417DA 21259 FUSELAGE SKIN GOUGED JUST FWD OF L1 DOOR AT THE STRINGER 10L LAP SPLICE. GOUGE MEASURED 1 X 1. ACTION TAKEN, ERA 33281 6-14. 2 L 7 3 4F A3WE 1999030500574 19990305 00574 NM 1999 3 5 DL72K990382 1 19990222 A 5313 STRINGER 6556441 BOEING 727 727232 1384082 NM BS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 417DA 21259 STRINGER 29R CRACKED INCHES AFT OF STA 950E. DAMAGED STRINGER WILL BE TRIMMED OUT AND A NEW SECTION SPLICED IN. ACTION TAKEN, ERA 332797-14. 2 L 7 3 4F A3WE 1999030500575 19990305 00575 NM 1999 3 5 DL72K990383 1 19990222 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 629 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 417DA 21259 RT UPPER WING STRINGERS 13 AND 14 AT WS 629. CRACKED STRINGER TO RIB TAB. ACTION TAKEN, ERA 332815-14AD. 2 L 7 3 4F A3WE 1999030500576 19990305 00576 NM 1999 3 5 DLM88990384 1 19990224 A 5330 SKIN 5924802 DOUG MD88 MD88 3023688 NM BS 229-244 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 DENT IN FUSELAGE SKIN FROM STA 229-244 BETWEEN L-18L AND L-17L. DAMAGE TRIMMED OUT RESULTING IN A 15 FWD/AFT BY 9.5 UP/ DOWN HOLE IN SKIN. ACTION TAKEN, ERA 332849-14. 2 L 7 2 4F RT A6WE 1999030500577 19990305 00577 NM 1999 3 5 DL72S990385 1 19990224 A 5330 SKIN 6554580 BOEING 727 727232 1384082 NM BS 990 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 GOUGE IN SKIN AT THE AFT EDGE OF THE C-2 DOOR CUTOUT AT FS 990. DAMAGED AREA LOCATED AT 2-24R. SKIN, DOUBLER, TRIPLER AND BEAR STRAP ARE ALL DAMAGED. ACTION TAKEN, ERA 332858-14. 2 L 7 3 4F A3WE 1999030500578 19990305 00578 NM 1999 3 5 DL733990386 1 19990223 A 5414 SKIN BOEING 737 737347 1384647 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309WA 23442 CRACK IN NR 1 PYLON STRUT SKIN AT THE ACCESS OPENING 5727L. ACTION TAKEN, 332810-14. 2 L 7 2 4F RT A16WE 1999030500579 19990305 00579 NM 1999 3 5 DL733990387 1 19990224 A 5320 INTERCOSTAL BOEING 737 737347 1384647 NM BS 334 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309WA 23442 R1 DOOR INTERCOSTAL AT STRINGER 8A FOUND CRACKED AT STA 334. CRACK REPAIRED PER S/B 737-53A1108 (REF ERA 332823-14AD). ACTION TAKEN, 332823-14AD. 2 L 7 2 4F RT A16WE 1999030500580 19990305 00580 NM 1999 3 5 DL767990388 1 19990225 A 5754 114T310313A SKIN BOEING 767 767232 1385132 NM NR 3 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 110DL 22222 THE UPPER SKIN ON THE NR 3 SLAT TRAILING EDGE WAS FOUND WITH A 3 X 4 DENTED/DELAMINATED AREA. THE DAMAGED SKIN WAS TRIM MED AWAY AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 366773-14AD. 2 L 7 2 4F RT A1NM 1999030500581 19990305 00581 WP 1999 3 5 DLL10990389 1 19990225 A 2611 WIRE 30284AR41 LKHEED 1011 10113851 5265010 WP GALLEY BROKEN A DALA K NONE N FALSE WARNING CR CRUISE 1 SO 27 728DA 20476 193C1173 GALLEY SMOKE WARNING LIGHT ILLUM INTERMITTANTLY. AURAL WARNING DOES NOT ACTUATE, ALL OVENS OFF. SMOKE DETECTOR C/B PUL LED. REPLACED SMOKE DETECTOR AND AMPLIFIER. 2 L 7 3 4F A23WE 1999030500582 19990305 00582 NM 1999 3 5 DL72W990390 1 19990225 A 2782 ACTUATOR 1U11032 BOEING 727 727247 138408F NM NR 4 LE SLAT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 296WA 0000 22533 NR 4 SLAT DID NOT RETRACT. C/W POM. VISUALLY CONFIRMED. REPLACED NR 4 SLAT ACTUATOR. 2 L 7 3 4F A3WE 1999030500583 19990305 00583 NM 1999 3 5 DL72S990393 1 19990225 A 3350 LIGHT 1102839 BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 518DA 10733 21469 MID CEILING EMER LIGHT WOULD NOT ELIMINATE WHEN CHECKING EMERGENCY LIGHTS. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999030500584 19990305 00584 NM 1999 3 5 DL72S990394 1 19990225 A 3350 BATTERY PACK 61020 BOEING 727 727232 1384082 NM 1L DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 518DA 21469 BATTERY DEAD ON EMERGENCY FLASHLIGHT AT 1L DOOR. REPLACED BATTERY AND BULB. 2 L 7 3 4F A3WE 1999030500585 19990305 00585 NM 1999 3 5 DL72W990395 1 19990225 A 2782 1U1110 ACTUATOR BOEING 727 727247 138408F NM NR 2 LE SLAT LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 2820W 21058 LOST MAJORITY OF A SYS HYD FLUID WITH SYS A HYD PUMPS OFF. LEAK/LOSS STOPPED AT 1/2 GAL ON INDICATOR. FOUND NR 2 L/E F LAP ACTUATOR LEAKING. REPLACED ACTUATOR, LEAK CHKS NORMAL. 2 L 7 3 4F A3WE 1999030500586 19990305 00586 NM 1999 3 5 DL72S990397 1 19990223 A 5330 SKIN 6518420 BOEING 727 727232 1384082 NM BS 277 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 LIGHTNING STRIKE DAMAGE AT AN EXISTING FASTENER IN THE SKIN BETWEEN S-7R AND S-8R AT STA 277. ACTION TAKEN, ERA 255827- 14. 2 L 7 3 4F A3WE 1999030500587 19990305 00587 NM 1999 3 5 DL72S990398 1 19990223 A 5320 FRAME BOEING 727 727232 1384082 NM EMER EXIT DRWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 OVERWING EXIT FRAME STA 761 RT, 784 LT AND 784 RT FOUND CRACKED IN I/B FLANGE. ACTION TAKEN, ERA 361976-14AD. 2 L 7 3 4F A3WE 1999030500588 19990305 00588 NM 1999 3 5 DLM88990399 1 19990219 A 5330 SKIN 5936003 DOUG MD88 MD88 3023688 NM CARGO DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DL 49539 A 1 X 1 SECTION OF FUSELAGE SKIN TORN FROM THE FWD EDGE OF THE C-2 CARGO DOOR OPENING. ACTION TAKEN, ERA 266915-14. 2 L 7 2 4F RT A6WE 1999030500589 19990305 00589 NM 1999 3 5 DL72S990401 1 19990226 A 2497 BMS1358 WIRE BOEING 727 727225A 1384077 NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 ON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL CRACKS ON INSULATION ON ALL 3 GEN FEED CABLES IN MID PYLON AREA. REPLACED C ABLES FROM SPLICES IN RT 48SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS13-58 DL (P/N 012210733). 2 L 7 3 4F RT A3WE 1999030500590 19990305 00590 NM 1999 3 5 DL72S990402 1 19990225 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED 4 CRACKS IN TWO CONSECUTIVE FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH. THE LAP WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 366 743-14, REV A. 2 L 7 3 4F A3WE 1999030500591 19990305 00591 NM 1999 3 5 DL72S990403 1 19990225 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED 7 CRACK LOCATIONS ALONG THE PANEL. THE ENTIRE LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH. THE LAP WAS REPLACED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366740-14, REV A. 2 L 7 3 4F A3WE 1999030500592 19990305 00592 NE 1999 3 5 DLL10990404 2 19990225 A 7261 RB21122B02 PUMP LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE BYPASSING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 733DS 47343 010637 193C1224 010637 EXCESSIVE OIL CONSUMPTION, NR 1 ENGINE BEGAN FLT WITH FULL OIL QTY. AT TOP OF CLIMB, NR 1 ENG QTY WAS 15 QTS. CONSUMED 2.5 QTS IN THE NEXT 1 HR 15 MIN, INDICATED AS LOW AS 9 QTS AFTER 3.5 HRS OF FLT. REPLACED SCAVENGE/LUBE PUMP ASSEMBLY. RAN ENGINE, OPS AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A23WE E12EU 1999030500593 19990305 00593 NM 1999 3 5 DL72S990405 1 19990226 A 5754 651622370 SKIN BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 NR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999030500594 19990305 00594 NM 1999 3 5 DL72S990406 1 19990226 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 8 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 NR 8 SLAT ACT I/B MOUNT BRACKET CRACKED AT WEB. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1999030500595 19990305 00595 NM 1999 3 5 DL72S990407 1 19990226 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 TPA - LTR CHK C-1 02/26/99, WING LE SPAR STIFFENER CRACKED AT I/B SIDE NR 2 SLAT I/B TRACK BOX. REPLACED STIFFENER PER MM 57-20-21. 2 L 7 3 4F A3WE 1999030500596 19990305 00596 NM 1999 3 5 DL72S990408 1 19990226 A 3350 3114981 LIGHT BOEING 727 727232 1384082 NM L1 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 536DA 22049 L1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS NOW OK. 2 L 7 3 4F A3WE 1999030500597 19990305 00597 NM 1999 3 5 DL733990409 1 19990226 A 3350 20131A BATTERY PACK BOEING 737 737347 1384647 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305WA 23346 ON LAYOVER, FOUND IN THE AFT CABIN EMERGENCY TRACK LIGHTING TURNING OFF AFTER 30 SECONDS OF OPERATION. FOUND BATTERY PA CK VOLTAGE LOW. REPLACED BATTERY PACK, SYSTEM OPERATED NORMAL. 2 L 7 2 4F RT A16WE 1999030500598 19990305 00598 NM 1999 3 5 DL72S990410 1 19990226 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 540DA 22386 FOUND ON L/O, LT AFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATT PACK, CKS GOOD. 2 L 7 3 4F A3WE 1999030500599 19990305 00599 NE 1999 3 5 DL72S990411 2 19990226 A 7261 OIL FILTER BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE DIRTY A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 499DA 53937 700444 21143 700444 NR 3 ENGINE OIL FILTER INDICATED BYPASS IN CRUISE FL280. PRECAUTIONARY, SHUTDOWN PROCEDURE ACCOMPLISHED. REPLACED OIL FILTER, LOP SWITCH, FILTER BYPASS SWITCH, DRAINED OIL RES, PERFORMED OIL BREATHER PRESS CK TEST 'Z' PER PFHB AND OPN OK. REPLACED OIL FILTER PER M/M. 2 L 7 3 4F 4 F A3WE E2EA 1999030500600 19990305 00600 NM 1999 3 5 DL72L990412 1 19990227 A 5230 6556927102 BEAM BOEING 727 727232 1384082 NM C3 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 WEB AND OUTER CHORD FOUND CRACKED JUST AFT OF THE FWD PRESSURE STOP FITTING. OUTER CHORD IS TO BE REPLACED. WEB SPLICE REPAIR IS TO BE ACCOMPLISHED PER ER/A. 2 L 7 3 4F A3WE 1999030500601 19990305 00601 NM 1999 3 5 DL72K990415 1 19990228 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM L2 DOORWAY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA VA5917 21586 OVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUM WHEN TESTED. REPLACED BATTERY PACK, CKS NORMAL. 2 L 7 3 4F A3WE 1999030500602 19990305 00602 NM 1999 3 5 DL72S990416 1 19990215 A 5311 FRAME BOEING 727 727232 1384082 NM BS 950 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FRAME DENTED AFT CARGO COMPT RT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 25R TO STR 26R. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27. DYE PENETRANT INSPECTED CUTOUT PER PS 900-6-3 NO 1 AND FOUND OK. DRILLED DOUBLER AND FILLER PER SRM 5 3-10-4 FIG 27 AND TREATED PER PS 900-2-4-1, NR 2. PAINTED PER PS 900-3-6. INSTALLED REPAIR PARTS PER SRM 53-10-4 FIG 2 7. 2 L 7 3 4F A3WE 1999030500603 19990305 00603 NM 1999 3 5 SCNA99043 1 19990226 A 2530 3510004407 COFFEEMAKER BOEING 727 7272J4 1384006 NM GALLEY FAILED A SCNA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 284SC 21438 DURING FLIGHT OPERATION OF THE FORWARD GALLEY COFFEEMAKER PRODUCED SPARKS WHEN THE BREW CYCLE WAS SELECTED. COULD NOT D UPLICATE PROBLEM ON THE GROUND. AS A PRECAUTION REMOVED AND REPLACED THE FORWARD GALLEY COFFEEMAKER. 2 L 7 3 4F RT A3WE 1999030500604 19990305 00604 NM 1999 3 5 DHL99720001 1 19990221 A 3260 65602132 ACCESSORY UNIT BOEING 727 727228 NM LANDING GEAR FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 720DH 19544 DEPARTING JFK RIGHT GEAR WARNING LIGHT ILLUMINATED WITH GEAR IN UP POSITION. GEAR RECYCLED. WHEN GEAR WAS PLACED UP, LEFT MAIN & RT MAIN RED WARNING AND SECOND OFFICER LEFT MAIN & RT MAIN GEAR DOOR LIGHTS ILLUMINATED. PLACED GEAR DOWN, ALL LIGHTS NORMAL. FOUND LANDING GEAR ACCESSORY UNIT FAULTY. REPLACED AND TESTS OK PER MM 32-09-121. 2 L 7 3 4F A3WE 1999030500605 19990305 00605 WP 1999 3 5 RRXA99127 1 19990226 A 2760 CONNECTOR DOUG DC8 DC873F 302199F WP SPOILER SYST DIRTY A RRXA O OTHER N FALSE WARNING DE DESCENT 1 WP 15 795FT 46103 ON DESCENT, SPOILER PRESS FAILED TO INCREASE WHEN SWITCH WAS PLACED IN OVERRIDE. AC LOADMETER INDICATED PUMP WAS OPERAT ING. CYCLED C/B FOR PRESS IND AND PUMP CTRL, NO HELP. CURRENT LIMITERS CHECKS GOOD. ACCOMPLISHED QRH ABNORMAL SPOILER PROCEDURE. CHECKED RESERVOIR FLUID LEVEL IN SPOILER RESERVOIR. CLEANED CANNON PLUG ON SPOILER PRESSURE XMITTER, OPS C K SPOILER SYS AFTER CURRENT LIMITERS WERE CHANGED WITH EXT PWR. PERFORMED GROUND RUN TO CK SPOILER SYS WITH ENG DRIVEN PUMPS SYS, OPERATORS NORMAL AND NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999030500606 19990305 00606 NM 1999 3 5 VNAA9902017 1 19990224 A 3350 321473 PWR SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 5LK INOP A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 438JS 3056 ROW FOUR EMERGENCY FLOOR LIGHTING WAS NOTED TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AN D REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE 5LK POSITION, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500607 19990305 00607 NE 1999 3 5 VNAA9902018 3 19990227 A 6114 E62127 HUB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP CRACKED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 436JS 45895 4278 3052 A CRACK WAS FOUND ON THE RIGHT HAND PROPELLER HUB DURING COMPLIANCE OF HARTZELL ALERT SERVICE BULLETIN HD-ASB-61-021. M AINTENANCE REMOVED AND REPLACED THE RIGHT HAND PROPELLER, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-10-00. OPERA TIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500608 19990305 00608 NM 1999 3 5 VNAA9902019 1 19990225 A 3060 A56362 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROPELLER DIRTY A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 427JS 27417 8855 3039 DURING THE TAXI OUT FOR TAKEOFF, A LEFT HAND PROPELLER HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND PROPELLER HEAT BRUSH BLOCK. OPERATIONAL CHECKS WERE COMPLETE D, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-61-05, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500609 19990305 00609 NM 1999 3 5 AT9900153 1 19990301 A 5320 FRAME BOEING 737 7372L9 1384497 NM CARGO DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO PIT DOORWAY CRACKED AT STRINGER 21R. FABRICATED Z CHANN EL REPAIR AND DOUBLER, REINSTALLED T ANGLE AND INTERCOSTAL IAW SB 737-53-1051 AND RES NR 99142. 2 L 7 2 4F RT A16WE 1999030500610 19990305 00610 NM 1999 3 5 AT9900154 1 19990301 A 5320 BEAM BOEING 737 7372L9 1384497 NM BS 706 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE MAIN LEFT WHEEL WELL STRINGER 18A SHEAR BEAM CRACKED AT BS 706. REMOV ED FASTENERS TO GAIN ACCESS, STOPPED DRILL CRACKED, INSTALLED KIT (P/N 65C29228-15) IAW SB 737-53-1066 AND RES NR 99439. 2 L 7 2 4F RT A16WE 1999030500611 19990305 00611 NM 1999 3 5 AT9900155 1 19990228 A 3350 1000679 LIGHT BOEING 737 7372L9 1384497 NM L2 DOOR INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 737Q 21279 EMERGENCY EXIT LIGHT ABOVE L-2 DOOR DID NOT ILLUMINATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ABOVE L-2 DOOR PER B737 MM 33-51-01, OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999030500612 19990305 00612 NM 1999 3 5 AT9900156 1 19990223 A 5347 BAC1520792 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 947-967 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORRODED SEAT TRACK AT BS 947-967 RBL 48. REMOVED AND REPLACED SEAT TRACK IAW B737 SRM 53-10-1, AND 51-10-5. 2 L 7 2 4F RT A16WE 1999030500613 19990305 00613 NM 1999 3 5 AT9900157 1 19990224 A 5347 BAC1520792 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 827-927 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORRODED SEAT TRACK AT BS 827-927 LBL 24. REMOVED CORROSION OUT OF LIMITS , FABRICATED REPAIR SEAT TRACK, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-10-2, AND 51-30-2. 2 L 7 2 4F RT A16WE 1999030500614 19990305 00614 NM 1999 3 5 AT9900158 1 19990219 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 344-360 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORRODED SEAT TRACK AT BS 344 TO 360 LBL 24.75. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW TRACK IAW B737 SRM 53-10-1, AND 53-10-5. 2 L 7 2 4F RT A16WE 1999030500615 19990305 00615 NM 1999 3 5 AT9900159 1 19990217 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 312-360. CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORRODED SEAT TRACK AT BS 312 TO 360 RBL 41.8. REMOVED CORRODED SECTION O F TRACK, FABRICATED NEW REPAIR SECTION, TREATED, PRIMED, AND INSTALLED IAW B737 SRM 53-10-5, 51-10-2, AND 51-30-2. 2 L 7 2 4F RT A16WE 1999030500616 19990305 00616 NM 1999 3 5 AT9900160 1 19990217 A 5347 BAC1520792 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 312-480 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORRODED SEAT TRACK AT BS 312 TO 480 RBL 24. REMOVED CORRODED SECTION OF TRACK, FABRICATED REPAIR SECTION, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-10-2, 51-30-2, 53-10-5 FIG 2. 2 L 7 2 4F RT A16WE 1999030500617 19990305 00617 NM 1999 3 5 AT9900161 1 19990217 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 312-360 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORRODED SEAT TRACK AT BS 312 TO 360 RBL 50.5. REMOVED CORRODED SECTION O F SEAT TRACK, FABRICATED REPAIR SECTION, TREATED, PRIMED AND INSTALLED IAW B737 SRM 53-10-5, 51-10-2, AND 51-30-2. 2 L 7 2 4F RT A16WE 1999030500618 19990305 00618 NM 1999 3 5 AT9900162 1 19990214 A 5320 1A454131 SUPPORT BOEING 737 7372L9 1384497 NM BS 947-967 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON FLOOR SUPPORT AT BS 947 TO 967. FABRICATED NEW FLOOR SUPPORT REPAIR, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-10-1, 51-30-3, AND 51-40-4. 2 L 7 2 4F RT A16WE 1999030500619 19990305 00619 NM 1999 3 5 AT9900163 1 19990124 A 5315 BAC1518399 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 967 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CABIN FLOORBEAM CORRODED AT FASTENERS HOLES OF UPPER FLANGE AT BS 967 RBL 48. REMOVED CORROSION, FABRICATED REPAIR, ALODINED, PRIMED, AND INSTALLED IAW B737 SRM 53-10-9 FIG 2, 51-20-2, AND 51-2 1-31. 2 L 7 2 4F RT A16WE 1999030500620 19990305 00620 WP 1999 3 5 AT9900164 1 19990226 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 FOUND A CRACK IN SKIN OF RUDDER APPROXIMATELY AT STATION ZR 70, CRACK IS ABOUT SEVEN INCHES LONG RUNNING PARALLEL WITH R IBS. STOP DRILLED FORWARD END OF CRACK IAW RES NR 99541, AFT END OF CRACK TERMINATES AT A RIVET HOLE. APPLIED SPEED TA PE TO CRACK IAW RES NR 99541, AIRCRAFT IS IN SAFE CONDITION FOR FERRY FLIGHT FROM FORT LAUDERDALE TO LAKE CITY, FL. 2 L 7 2 4F A6WE 1999030500621 19990305 00621 EU 1999 3 5 MALA976364 1 19990301 A 3350 MS25231316 LAMP SAAB SF340 SF340A 7850100 EU ROW 2CD INOP A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119XJ 119 EMERGENCY LIGHT ABOVE SEAT 2 C & D INOP. REPLACED LAMP. 2 L 7 2 4T RT A52EU 1999030500622 19990305 00622 NM 1999 3 5 K3HA990018 1 19990225 A 3350 3071BP3GPL BULB BOEING 727 727225 1384077 NM ROW 16DEF FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 PASSENGER ROW 16DEF AND AFT CARGO DOOR 3 EMERGENCY PATH LIGHTS INOP. REMOVED AND REPLACED LAMPS AT PAX ROW 16 AND AFT C ARGO DOOR ON EMERGENCY PATH LIGHTING (P/N 81 NSN) IAW 33-50-01. OPS CHECK OK. 2 L 7 3 4F A3WE 1999030500623 19990305 00623 NM 1999 3 5 K3HA990019 1 19990226 A 3350 079123 LENS BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 AFT EMERGENCY PATH LIGHTS. REINSTALLED 2 RED LENS COVERS. 2 L 7 3 4F A3WE 1999030500624 19990305 00624 WP 1999 3 5 CALA9900199 1 19990225 A 5753 SKIN DOUG DC10 DC1010 3022110 WP RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT WING RT I/B TRAILING EDGE FLAP UPPER SKIN SURFACE UPPER LAP JOINT CORRODED. REPAIRED IAW ECRA 5752- 01027. 2 L 7 3 4F A22WE 1999030500625 19990305 00625 WP 1999 3 5 CALA9900200 1 19990225 A 5743 FITTING DOUG DC10 DC1010 3022110 WP RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT WING T/E CAVITY RT MLG MAIN FITTING CORRODED OVER SUPPORT ANGLE ON INBOARD END OVER LOWER WING BEAVE RTAIL. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED WITH FASTENERS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999030500626 19990305 00626 WP 1999 3 5 CALA9900201 1 19990226 A 5753 SKIN DOUG DC10 DC1030 3023501 WP LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A 5 INCH CRACK ON UPPER SURFACE SKIN OF LT INBOARD FLAP. A REPAIR WAS INSTALLED IAW SRM 57-00-01, FIGU RE 4, SHEET 2 AND ECRA 5752-01028. 2 L 7 3 4F A22WE 1999030500627 19990305 00627 WP 1999 3 5 CALA9900202 1 19990227 A 5320 FRAME DOUG DC9 DC982 3022082 WP WINDOW 15L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND NR 15L CABIN WINDOW FRAME CORRODED AT STA 419. THE WINDOW FRAME SECTION WAS REMOVED AND REPLACED IAW S RM 51-10-3. 2 L 7 2 4F A6WE 1999030500628 19990305 00628 WP 1999 3 5 CALA9900203 1 19990228 A 3350 20131A BATTERY PACK DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68044 46903 THE EMERGENCY EVACUATION LIGHT AT PASSENGER ZONE B WAS INTERMITTENT. THE BATTERY PACK WAS REPLACED AND OPERATION CHECKE D GOOD IAW MM 33-50-00. 2 L 7 3 4F A22WE 1999030500629 19990305 00629 WP 1999 3 5 CALA9900204 1 19990228 A 5720 BRACKET DOUG DC9 DC932 3022066 WP WS 254 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17557 47424 INSPECTION FOUND BRACKET CRACKED THROUGH AND A 2 INCH CRACK AT SPLICE INSIDE LT WING FIXED L/E AT JOINT BETWEEN NOSE RIB S, TEN INCHES O/B OF NR 2 SLAT O/B TRACK, XRS 254. AN ANGLE AND STRAP WERE INSTALLED IAW SRM 51-10-2, 51-00-00, 51-10-3 , 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999030500630 19990305 00630 WP 1999 3 5 CALA9900205 1 19990228 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17557 47424 INSPECTION FOUND A 1.5 AND 2 INCH CRACK IN NOSE RIB AT HI-LOK INSIDE RT WING FIXED LEADING EDGE I/B OF NR 5 SLAT CENTER TRACK. THE RIB WAS REMOVED AND A NEW RIB REPAIR WAS INSTALLED IAW SRM 57-01, PAGE 9. 2 L 7 2 4F A6WE 1999030500631 19990305 00631 EA 1999 3 5 COMA9960087 1 19990301 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 979CA 7159 AFT CABIN OVERHEAD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999030500632 19990305 00632 NM 1999 3 5 UPS99228774 1 19990212 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, LIGHT CORROSION ON FLOORBEAM LOWER FLANGE BS 680 RBL 25 APPROX. REPAIRED IAW SRM 51-10-02 AND 51-20- 151. 2 L 7 3 4F A3WE 1999030500633 19990305 00633 NM 1999 3 5 UPS99228775 1 19990212 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 285 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, DENT IN SKIN BS 285 BETWEEN S18L AND S17L. REPAIRED IAW SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1999030500634 19990305 00634 NM 1999 3 5 UPS99228776 1 19990217 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 269 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, DENT IN FUSELAGE SKIN BS 269 BETWEEN S2L AND S3L. REPAIRED AREA IAW SRM 53-30-03 FIG 1. 2 L 7 3 4F A3WE 1999030500635 19990305 00635 NM 1999 3 5 UPS99228778 1 19990216 A 5320 WEB BOEING 727 72731C 1384011 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, CRACKS ON LT MLG WHEEL WELL PRESSURE WEB AT BS 940 FWD SIDE. REPAIRED IAW EO B727-5310-0460 APPENDIX C. 2 L 7 3 4F A3WE 1999030500636 19990305 00636 NM 1999 3 5 UPS99228779 1 19990215 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, CRACK ON ANGLE BS 178, STR 17R APPROX. REPAIRED IAW SRM 51-40-03 FIG 1. 2 L 7 3 4F A3WE 1999030500637 19990305 00637 NM 1999 3 5 UPS99228780 1 19990215 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, CRACK ON ANGLE BS 178 STR 17L APPROX. REPAIRED IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1999030500638 19990305 00638 NM 1999 3 5 UPS99228781 1 19990212 A 5320 TIE BOEING 727 72731C 1384011 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, STRINGER TO FRAME TIE (TUNING FORK) CRACKED AT BS 740 AFT SIDE STR 7L MAIN CARGO DECK. STRINGER TO F RAME END TIE REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999030500639 19990305 00639 NM 1999 3 5 UPS99228784 1 19990211 A 5511 RIB BOEING 727 72731C 1384011 NM RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, SUSPECT CRACK RT HORIZ STAB T-EDGE RIB REPAIR ELEVATOR STA 50-5 AND REPAIRED AREA NOT STOP DRILLED. R IB REMOVED AND REPLACED IAW BOEING DRAWING NR 65-16929. 2 L 7 3 4F A3WE 1999030500640 19990305 00640 NM 1999 3 5 UPS99228787 1 19990210 A 5320 TIE BOEING 727 72731C 1384011 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, STRINGER TO FRAME TIE (TUNING FORK) CRACKED AT BS 740 S5L MAIN CARGO DECK. STRINGER TO FRAME END TIE REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999030500641 19990305 00641 NM 1999 3 5 UPS99228788 1 19990210 A 5320 WEB BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, SUSPECT CRACK IN WEB IN FWD CARGO INTERNAL STRUCTURE AFT OF NR 2 FWD DOOR STOP FITTING. WEB REPLACED IAW DRAWING NR 65-18620. 2 L 7 3 4F A3WE 1999030500642 19990305 00642 NM 1999 3 5 UPS99228789 1 19990217 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 960 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, SMALL GOUGE IN SKIN BS 960 S3 RT. REPAIRED IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1999030500643 19990305 00643 WP 1999 3 5 UPS99828782 1 19990213 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, RT WING L/E AT XFS 772.5, THE SKIN IS CRACKED BETWEEN 2 FASTENER HOLES. STOP DRILLED CRACK AND REPA IRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999030500644 19990305 00644 WP 1999 3 5 UPS99828783 1 19990213 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LT WING L/E SKIN AT FS 710.0 IS CRACKED BETWEEN FASTENERS. STOP DRILLED THE CRACK AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999030500645 19990305 00645 WP 1999 3 5 UPS99828785 1 19990213 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 711 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, RT WING L/E AT FS 711.0, THE SKIN HAS A CRACK AT 1 SCREW COUNTERSINK. STOP DRILLED THE CRACK AND RE PAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999030500646 19990305 00646 WP 1999 3 5 UPS99828786 1 19990213 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, RT WING UPPER L/E SKIN AT FS 560.0 IS CRACKED BETWEEN 2 FASTENERS. THE CRACK TERMINATES AT THE FAST ENER HOLES. REPAIRED SKIN IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999030500647 19990305 00647 WP 1999 3 5 UPS99828790 1 19990214 A 5753 WEB DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LEFT I/B FLAP, I/B WEB IS CRACKED AT THE AFT LWR CORNER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999030500648 19990305 00648 WP 1999 3 5 UPS99828791 1 19990214 A 5720 566989117 DOUBLER DOUG DC8 DC873F 302199F WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, RT WING L/E LWR INTERNAL DOUBLER, JUST O/B OF THE XOLDI 6.225 RIB IS CRACKED AT THE T/E. REMOVED, F ABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5669891 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500649 19990305 00649 WP 1999 3 5 UPS99828792 1 19990214 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 761 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LT WING L/E SKIN AT XW 761, IS CRACKED BETWEEN 2 FASTENERS. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1999030500650 19990305 00650 WP 1999 3 5 UPS99828793 1 19990214 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 711 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LT WING L/E SKIN AT FS 711 IS CRACKED AT 1 FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1, FIG 24. 2 L 7 4 4F RT 4A25 1999030500651 19990305 00651 WP 1999 3 5 UPS99828794 1 19990214 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, THE EXTERNAL REPAIR DOUBLER AT THE NR 1 PYLON CUTOUT IS CRACKED AND THE SKIN IS CRACKED PAST THE STO P DRILL HOLE. REMOVED OLD REPAIR DOUBLER, STOP DRILLED CRACK AND FABRICATED A NEW REPAIR DOUBLER AND INSTALLED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1999030500652 19990305 00652 WP 1999 3 5 UPS99828795 1 19990215 A 5320 46110672 FITTING DOUG DC8 DC873F 302199F WP BS 71 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LONGERON END FITTING AT FS 71, AND LONG 32R IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 1999030500653 19990305 00653 WP 1999 3 5 UPS99828796 1 19990214 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LT WING UPPER SKIN AT XRS 75, JUST FWD OF THE CENTER SPAR IS CRACKED. CUT OUT DAMAGE AND REPAIRED I AW SRM 57-2-1, FIG 10. 2 L 7 4 4F RT 4A25 1999030500654 19990305 00654 WP 1999 3 5 UPS99828797 1 19990214 A 5320 37535691 FITTING DOUG DC8 DC873F 302199F WP BS 240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LONG 25R END FITTING AT FS 240 HAS MODERATE CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1999030500655 19990305 00655 WP 1999 3 5 UPS99828798 1 19990214 A 5320 57799345 DOUBLER DOUG DC8 DC873F 302199F WP BS 80-120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LONG 31R FINGER DOUBLER FROM FS 80 TO 120 IS CRACKED AND PULLING LOOSE. REMOVED, FABRICATED AND REP LACED THE FINGER DOUBLER IAW DWG 5779934 AND SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500656 19990305 00656 WP 1999 3 5 UPS99828799 1 19990214 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LT WING RIB AT XILD .7095 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999030500657 19990305 00657 WP 1999 3 5 UPS99828800 1 19990214 A 5320 47504201 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, THE INTERCOSTAL END FITTING AT LONG 19L AND 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1999030500658 19990305 00658 WP 1999 3 5 UPS99828801 1 19990216 A 5320 37552222 FITTING DOUG DC8 DC873F 302199F WP BS 822.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, FS 822.5 FLOORBEAM AT LBL 24, THE AFT SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE SPLICE FI TTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999030500659 19990305 00659 WP 1999 3 5 UPS99828802 1 19990216 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP BS 1691 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, FS 1691 AT LONG 22R THE LONG END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500660 19990305 00660 WP 1999 3 5 UPS99828803 1 19990217 A 5320 37552221 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, FS 759, RBL 24, THE FLOORBEAM SPLICE/ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IA W SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500661 19990305 00661 WP 1999 3 5 UPS99828804 1 19990217 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 575.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LT WING L/E RIB AT FS 575.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999030500662 19990305 00662 WP 1999 3 5 UPS99828805 1 19990217 A 5320 4611422N FITTING DOUG DC8 DC873F 302199F WP BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, FS 960 AT BL 0, THE VERTICAL FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500663 19990305 00663 WP 1999 3 5 UPS99828806 1 19990217 A 5320 3649114N FITTING DOUG DC8 DC873F 302199F WP BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, FS 920, RBL 68, THE VERTICAL FITTING HAS A 6 INCH CRACK. REMOVED AND REPLACED THE FITTING IAW SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1999030500664 19990305 00664 WP 1999 3 5 UPS99828807 1 19990217 A 5320 26463481N FITTING DOUG DC8 DC873F 302199F WP BS 903 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, FS 903, LBL 68, THE CUSP SPLICE FITTING HAS HEAVY EXFOLIATION CORROSION. REMOVED AND REPLACED FITTI NG IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500665 19990305 00665 EU 1999 3 5 QXEA9900162 1 19990113 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - .25 INCH CRACK AT BELLY CENTER TUNNEL LEFT-HAND WALL CUTOUT FOR Z STRINGER 2.02 AT BL 225 LT. REPAIRED IAW HORIZO N AIR EA 4-53-638, STEPS 3 THROUGH 6. 2 L 7 2 4F RT A20EU 1999030500666 19990305 00666 EU 1999 3 5 QXEA9900163 1 19990110 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - .5 INCH CRACK AT BELLY CENTER TUNNEL LEFT-HAND WALL CUTOUT FOR Z STRINGER 2.01 AT BL 225 LT. REPAIRED IAW HORIZON AIR EA 4-53-638. 2 L 7 2 4F RT A20EU 1999030500667 19990305 00667 EU 1999 3 5 QXEA9900164 1 19990106 A 5741 FITTING FOKKER F28 F28MK4000 4990810 EU RT WING/FUS DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT WING TO FUSELAGE ATTACH CASTING AT FRONT SPAR HAS (2) DINGS APPROXIMATELY .010 DEEP, BY TOP MOUNT BOLT AT RA DIUS OF CASTING. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999030500668 19990305 00668 EU 1999 3 5 QXEA9900165 1 19990106 A 5741 FITTING FOKKER F28 F28MK4000 4990810 EU LT WING/FUS DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT WING TO FUSELAGE ATTACH CASTING AT FRONT SPAR HAS (3) DINGS APPROXIMATELY .010 DEEP, BY TOP MOUNT BOLT AT RAD IUS OF CASING. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999030500669 19990305 00669 EU 1999 3 5 QXEA9900166 1 19990111 A 5350 SUPPORT FOKKER F28 F28MK4000 4990810 EU FUSELAGE FAIRING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - 91J FAIRING SUPPORT ON FUSELAGE HAS APPROXIMATELY 10 INCH CRACK AT FORWARD CURVED SECTION JUST FORWARD OF NUT PLAT ES. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-03. 2 L 7 2 4F RT A20EU 1999030500670 19990305 00670 EU 1999 3 5 QXEA9900167 1 19990115 A 5321 FLOOR FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FLOOR PANEL 94AK HAD CORE DAMAGE ALONG EDGES AND SKIN PUNCTURE. FABRICATED A NEW PANEL IAW HORIZON AIR EA 4-53-66 6. 2 L 7 2 4F RT A20EU 1999030500671 19990305 00671 EU 1999 3 5 QXEA9900168 1 19990115 A 5321 FLOOR FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FLOOR PANEL 94AJ CORNER DAMAGED. REPAIRED IAW HORIZON AIR EA 4-53-672. 2 L 7 2 4F RT A20EU 1999030500672 19990305 00672 EU 1999 3 5 QXEA9900169 1 19990115 A 5321 FLOOR FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FLOOR PANEL 94AM CORE DAMAGED ALONG EDGES, LOWER SKIN PUNCTURE. REPAIRED IAW HORIZON AIR EA 4-53-666. 2 L 7 2 4F RT A20EU 1999030500675 19990305 00675 EU 1999 3 5 QXEA9900172 1 19990115 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU TE FLAP VANE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - OUTBOARD FLAP VANE UPPER SURFACE SKIN INBOARD END DENTED AT ROLLER CHAFE PAD. REPAIRED IAW FOKKER SRM 51-31-01 AN D SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999030500676 19990305 00676 EU 1999 3 5 QXEA9900173 1 19990107 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - WING REPAIR FOR ACCESS PANEL 72A HAS A CRACK RADIATING FROM A SCREW HOLE. REPAIRED IAW HORIZON AIR EA 4-57-203. 2 L 7 2 4F RT A20EU 1999030500677 19990305 00677 EU 1999 3 5 QXEA9900174 1 19990106 A 2720 LEVER FOKKER F28 F28MK4000 4990810 EU RUDDER WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - TOP AND MID RUDDER DAMPER LEVER ASSEMBLIES WORN. REMOVED AND REPLACED TOP AND MID RUDDER DAMPER LEVER ASSEMBLIES. 2 L 7 2 4F RT A20EU 1999030500678 19990305 00678 EU 1999 3 5 QXEA9900175 1 19990108 A 5712 RIB FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIB NR 6 HAS A CRACK APPROXIMATELY .25 INCH LENGTH. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999030500679 19990305 00679 EU 1999 3 5 QXEA9900176 1 19990114 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT-HAND FORWARD EMERGENCY DOOR EXIT HAS A DENT 6 INCHES BELOW WINDOW PANEL IN OUTER SKIN. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999030500680 19990305 00680 EU 1999 3 5 QXEA9900177 1 19990106 A 5220 FLANGE FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT-HAND AFT OVERWING EMERGENCY EXIT UPPER TORSION BOX TOP FLANGE HAS DOUBLE DRILLED RIVET HOLE. REPAIRED IAW H ORIZON AIR EA 4-53-655. 2 L 7 2 4F RT A20EU 1999030500681 19990305 00681 EU 1999 3 5 QXEA9900178 1 19990104 A 5320 RIVETS FOKKER F28 F28MK4000 4990810 EU FRAME 12875 MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CLIP REPAIRED AT STRINGER 28 HAS 2 RIVETS WITH IMPROPER BUCKED TAILS. REPAIRED IAW FOKKER SRM 51-31-0 1. 2 L 7 2 4F RT A20EU 1999030500682 19990305 00682 EU 1999 3 5 QXEA9900179 1 19990105 A 5320 RIVETS FOKKER F28 F28MK4000 4990810 EU FRAME 12875 MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CLIP REPAIR AT STRINGER R29 HAS 2 RIVETS THAT DO NOT FILL THE HOLES AT CLIP TO CASTILLATION. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999030500683 19990305 00683 EU 1999 3 5 QXEA9900180 1 19990103 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815 CASTILLATION CRACKED AT STRINGER 33. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999030500684 19990305 00684 EU 1999 3 5 QXEA9900181 1 19990106 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME12875-13345 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE IS LIGHT PITTING CORROSION ON THE INBOARD FLOOR SUPPORT FLANGE OF THE LEFT-HAND INBOARD SEAT TRACK BETWEEN F RAMES 12875 AND 13345. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 1999030500685 19990305 00685 EU 1999 3 5 QXEA9900182 1 19990103 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE TWO AREAS WITH LIGHT CORROSION ON OUTBOARD FLOOR SUPPORT FLANGE, ON LEFT-HAND OUTBOARD SEAT TRACK, JUST AFT OF FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999030500686 19990305 00686 EU 1999 3 5 QXEA9900183 1 19990113 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE IS A AREA OF LIGHT FRETTING CORROSION ALONG THE INBOARD EDGE OF FLOOR SUPPORT FLANGE ON THE LEFT-HAND INBOAR D SEAT TRACK, JUST AFT OF FRAME 14755. REPAIRED IAW HORIZON AIR EA 4-53-658. 2 L 7 2 4F RT A20EU 1999030500687 19990305 00687 EU 1999 3 5 QXEA9900184 1 19990106 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE IS A FRETTING CORROSION ON INBOARD FLOOR SUPPORT FLANGE ON LEFT-HAND INBOARD SEAT TRACK AT FRAME 6305. REPA IRED IAW HORIZON AIR EA 4-53-657. 2 L 7 2 4F RT A20EU 1999030500688 19990305 00688 EU 1999 3 5 QXEA9900185 1 19990103 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE IS LIGHT TO MODERATE PITTING CORROSION ON THE INBOARD FLOOR SUPPORT FLANGE OF THE RIGHT-HAND OUTBOARD SEAT T RACK AT FRAME 5805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999030500689 19990305 00689 EU 1999 3 5 QXEA9900186 1 19990111 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE TWO AREAS OF LIGHT TO MODERATE CORROSION IN CHANNEL OF RIGHT-HAND INBOARD SEAT TRACK BETWEEN FRAME 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999030500690 19990305 00690 NM 1999 3 5 99FDEA00080 1 19990207 A 5314 KEEL BEAM DOUG MD11 MD11F 3023600 NM BS 1401-1451 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 UNDERWING KEEL STRUCTURE WAS DAMAGED IN LAND INCIDENT AND HAS BEEN OPER UNDER REPETITIVE INSP PER EA 1-5330-33495 AND 1- 5330-39772 BS 1401 TO 1451 Z-60 TO Z-110. *S/D* COMPLIED WITH EA 1-5310-40320 FUSELAGE - UNDERWING KEEL STRUCTURE REP AIR. 2 L 7 3 4F RT A22WE 1999030500691 19990305 00691 NM 1999 3 5 99FDEA00081 1 19990119 A 5312 BULKHEAD DOUG MD11 MD11F 3023600 NM BS 595 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 FWD FUSELAGE WAS DAMAGED IN LAND INCIDENT AND HAS BEEN OPER UNDER REPETITIVE INSP PER EA 1-5330-39764. BULKHEAD AT BS 5 95 WAS STRESSED. *S/D* COMPLIED WITH EA 1-5310-40319- FUSELAGE, MAIN FRAME - REPAIR OF BS 595 PRESSURE BULKHEAD. 2 L 7 3 4F RT A22WE 1999030500692 19990305 00692 NM 1999 3 5 99FDEA00082 1 19990122 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 623 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 A/C SUSTAINED DAMAGE TO FUSELAGE SKIN DURING LANDING INCIDENT BS 623 FROM L36 TO L48 LT. *S/D* COMPLIED WITH EA 1-5330 -40318 FUSELAGE, SKINS-SPLICE REPAIR OF SKIN AT BS 623, L36-L48, LT AND RT. 2 L 7 3 4F RT A22WE 1999030500693 19990305 00693 WP 1999 3 5 ABXA9900129 1 19990222 A 2910 LINE DOUG DOUG DC8 DC862 3021970 WP NR 2 HYD SYST LOOSE A ABXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 801AX 46077 AFTER TAKEOFF AND PASSING 4000 FEET, THE HYDRAULIC RESERVOIR LOW PRESSURE LIGHT ILLUMINATED, ACCOMPANIED BY DECAYING FLU ID QUANTITY. PERFORMED LOSS OF HYDRAULICS EMERGENCY CHECKLIST. TIGHTENED LOOSE LINE ON NR 2 HYDRAULIC PUMP. BLED SYST EM, PERFORMED OPS AND LEAK CHECK. NO DEFECTS NOTED. SERVICED IAW DC8 MM. 2 L 7 4 4F 4A25 1999030500694 19990305 00694 WP 1999 3 5 ABXA9900130 1 19990223 A 5610 5912977 TRIM DOUG DOUG DC9 DC933F 302207A WP COCKPIT WINDOW LOOSE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 930AX 47363 FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. REMOVED LOOSE TRIM, WINDOW OPENS NORMALLY. 2 L 7 2 4F A6WE 1999030500695 19990305 00695 WP 1999 3 5 ABXA9900131 1 19990223 A 5610 5912977 TRIM DOUG DOUG DC9 DC933F 302207A WP COCKPIT WINDOW OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 FIRST OFFICER'S CLEARVIEW WINDOW WAS DIFFICULT TO OPEN. REPOSITIONED WINDOW TRIM AROUND FIRST OFFICER'S CLEARVIEW WINDO W. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999030500696 19990305 00696 WP 1999 3 5 ABXA9900132 1 19990219 A 2120 AIR DIST DOUG DC9 DC941 302207N WP COCKPIT ODOR A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 978AX 47628 CREW SMELLED SMOKE (RUBBER SMELL) ON TAKEOFF AND CLIMB. RETURNED FOR LANDING. INSPECTED E & E COMPARTMENT, EPC PANEL, AIRCRAFT BATTERIES AND ASSOCIATED WIRING. NO DEFECTS NOTED. RAN BOTH ENGINE TO POWER WITH ASSOCIATED PACKS IN AUTO. N OTED HINT OF NEW DUCTING SMELL FROM RIGHT PACK. RIGHT PACK HAD NEWLY INSTALLED DUCTING AND PLUMBING. ALSO, INSPECTED A FT ASSY COMP AND NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1999030500697 19990305 00697 WP 1999 3 5 ABXA9900133 1 19990221 A 2120 DUCT DOUG DC8 DC863 302198A WP RT HEAT XCHANGER LOOSE A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 818AX 46075 AIRCRAFT EXPERIENCED RAPID DECOMPRESSION. CABIN CLIMBED AT A RATE OF 2000 FPM WITH MANIFOLD PRESSURE IN EXCESS OF 35 PS I. THREE CTC'S WERE ON AT THE TIME. CABIN PRESSURE CONTROLLER LOCKED IN FULL INCREASE. OXYGEN WAS USED DUE TO LOSS OF CABIN PRESSURE. RESECURED DUCT FROM RIGHT HEAT EXCHANGER TO WARM AIR CHECK VALVE. CABIN PRESSURE CHECKED GOOD IAW DC8 MM 21-31-00. 2 L 7 4 4F 4A25 1999030500698 19990305 00698 NE 1999 3 5 ABXA9900139 2 19990225 A 7200 ENGINE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 1 FAILED A ABXA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 23 853AX 46037 669202 DURING CLIMB, NR 1 ENGINE CREATED LOUD BANG. N1 AND N2 RPM DROPPED BY ONE HALF, EGT WENT TO 640 DEGREES. ENGINE ANTI-I CE WAS ON. SHUT ENGINE DOWN. FIRE BOTTLES WERE NOT USED. REPLACED NR 1 ENGINE. 2 L 7 4 4F 4 F 4A25 1E8 1999030500699 19990305 00699 NE 1999 3 5 ABXA9900140 2 19990224 A 7230 COMPRESSOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE STALLED A ABXA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 23 819AX 45927 671067 NR 4 ENGINE COMPRESSOR STALLED WHEN REDUCING POWER FROM CLIMB TO CRUISE. ENGINE OIL QUANTITY DROPPED RAPIDLY FROM 3.1 T O 1.6 GALLONS. SHUT ENGINE DOWN. REPLACED NR 4 ENGINE IAW ABX JOB CARD J-8090507. OPS AND LEAK CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1999030500700 19990305 00700 WP 1999 3 5 ABXA9900141 1 19990225 A 5313 277792230 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK, FOUND LONGERON 2 LEFT, STATION 200 CRACKED. REPLACED LONGERON SECTION IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999030500701 19990305 00701 WP 1999 3 5 ABXA9900142 1 19990219 A 5313 59114277 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND LONGERON 16 LEFT CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999030500702 19990305 00702 WP 1999 3 5 ABXA9900143 1 19990219 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999030500703 19990305 00703 WP 1999 3 5 ABXA9900144 1 19990219 A 5315 99115441 FLOORBEAM DOUG DOUG DC9 DC941 302207N WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND UPPER CARGO COMPARTMENT FLOORBEAM CRACKED AT STATION 237, LBL 6.0. REPAIRED FLOORBEAM IAW DC9 SR M SUPP DWG K05011. 2 L 7 2 4F A6WE 1999030500704 19990305 00704 WP 1999 3 5 ABXA9900145 1 19990219 A 5280 59107834 PAN DOUG DOUG DC9 DC941 302207N WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND LEFT MAIN LANDING GEAR DOOR PAN CRACKED ON FORWARD OUTBOARD EDGE. REPAIRED DOOR PAN IAW DC9 SRM 52-05. 2 L 7 2 4F A6WE 1999030500705 19990305 00705 WP 1999 3 5 MWEA99082 1 19990301 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP CABIN DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 216ME 6361 47740 BDL - FLT 49 - THE GALLEY DOOR SLIDE CAME OUT OF COVER. MTC REINSTALLED GALLEY DOOR SLIDE. (X) 2 L 7 2 4F A6WE 1999030500706 19990305 00706 WP 1999 3 5 MWEA083 1 19990228 A 5512 SKIN DOUG DC9 DC915 3022036 WP RT HORIZ STAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 MKE - RIGHT HORIZONTAL STABILIZER HAS BLEND OUTS ON LEADING EDGE AT XFS 163.375 XFS 200.00 AND XFS 232.00 TO XH 209.125 . MTC FABRICATED AND INSTALLED DOUBLER REPAIR. (X) 2 L 7 2 4F A6WE 1999030500707 19990305 00707 NM 1999 3 5 SCNA99044 1 19990228 A 2530 72066000B OVEN BOEING 727 7272J4 1384006 NM GALLEY SMOKING A SCNA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 288SC 3856 20765 DURING FLIGHT, THE AFT NR 1 OVEN EMITTED SMOKE MOMENTARILY WHEN SWITCHED ON. REMOVED AND REPLACED THE OVEN. 2 L 7 3 4F RT A3WE 1999030500708 19990305 00708 WP 1999 3 5 RRXA99128 1 19990227 A 8012 LIGHT DOUG DC8 DC863 302198A WP NR 1 STARTER ILLUMINATED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 796AL 46054 ON LIFTOFF, NR 1 STARTER BUTTON LIGHT AND ENGINEERS STARTER VALVE OPEN LIGHT CAME ON FOR NR 1 ENGINE. REMOVED AND REPLA CED NR 1 ENG START VALVE ASSY, NO HELP. TRANSFERRED TO DMI C7526171-0593 IAW MEL 80-2, CAT C DUE DATE 3-9-99, PLACARD I NSTALLED, MANUAL START REQUIRED. 2 L 7 4 4F 4A25 1999030500709 19990305 00709 NM 1999 3 5 VNAA9902020 1 19990226 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 429JS 61870 3043 THE LEFT HAND PROPELLER FAILED TO COME OUT OF FEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INS PECTED AND REPLACED THE LEFT HAND PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OPERA TIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500710 19990305 00710 NM 1999 3 5 VNAA9902021 1 19990221 A 3610 4067B000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 328LS 3025 A RIGHT HAND BLEED FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE . MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LOW PRESSURE BLEED SHUTOFF VALVE, IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 36-11-03. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500711 19990305 00711 NM 1999 3 5 VNAA9902022 1 19990225 A 7603 001A761A1021002 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT POWER LEVER FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 430JS 3044 THE LEFT HAND PROPELLER FAILED TO COME OUT OF FEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE IN SPECTED AND REPLACED THE LEFT HAND POWER LEVER MICRO-SWITCH ASSEMBLY, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-1 1-05. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500712 19990305 00712 NE 1999 3 5 VNAA9903001 3 19990301 A 6114 HUB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP CRACKED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 424JS 68801 13329 3033 DURING THE INSPECTION FOR HARTZELL ALERT SERVICE BULLETIN HD-ASB-61-021, A SUSPECTED CRACK WAS NOTED ON THE RIGHT HAND P ROPELLER HUB. MAINTENANCE REPLACED THE PROPELLER, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-10-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500714 19990305 00714 EU 1999 3 5 Y2PA99013 1 19990125 A 5610 WINDSHIELD AMD FALCON FALCON20 2730103 EU LT COCKPIT FAILED A Y2PA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 818AA 036 IND - FLT 57284 - JUST AFTER LEVEL OFF AT FL 310, CREW HEARD A LOUD 'THUD' AND IMMEDIATELY NOTICED THE FRONT LEFT WINDSH IELD HAD SHATTERED. EMERGENCY DESCENT WAS INITIATED, CABIN ALTITUDE RAISED TO LOWER DIFFERENTIAL PRESSURE, AIRCRAFT SLO WED TO BELOW 230 KNOTS AND CREW ADVISED ATC THAT THEY WOULD LIKE TO DECLARE AN EMERGENCY AND LAND AT IND. AIRCRAFT WAS VECTORED TO IND AND LANDED WITHOUT FURTHER INCIDENT. USA JET MAINTENANCE WAS SENT TO IND TO EVALUATE CAUSE AND REPLACE WINDSHIELD. (X) 2 L 7 2 4F RT A7EU 1999030500715 19990305 00715 SO 1999 3 5 RAIA990106 1 19990108 A 4950 4501968B APU EMB 145 EMB145 SO APU COMPARTMENT CONTAMINATED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 803HK 921 145077 ORD - FLT 5788 - SMOKE IN COCKPIT AND CABIN. SMOKE WENT AWAY WITH APU OFF. MAINTENANCE RAN APU AND PERFORMED OPS CHECK OF ECS SYSTEM, DETERMINED TO BE GLYCOL IN APU INLET. (X) 2 L 7 2 4F RT T00011AT 1999030500723 19990305 00723 WP 1999 3 5 99ZZZX832 1 19990106 A 3350 D30170535 LIGHT LKHEED 1011 10113853 5265020 WP SLIDE INOPERABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 163AT 3215 1229 DURING PARTIAL EVACUATION DEMONSTRATION, THE R1 DOOR SLIDE/RAFT LIGHTS DID NOT ILLUMINATE AFTER DEPLOYMENT. REMOVED AND REPLACED SLIDE. 2 L 7 3 4F A23WE 1999030500729 19990305 00729 1999 3 5 99ZZZX836 4 19990115 A 2565 MR2561 SLIDE AIRBUS 320 A320231 3930325 EU PASSENGER DOOR DEPLOYED A RYNA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 GCPFR 437 SFO - FLT 8165 - L-1 SLIDE DEPLOYED BY R1 FLIGHT ATTENDANTS. REPLACED L-1 SLIDE. (X) 2 L 7 2 4F RT A28NM 1999030500730 19990305 00730 NE 1999 3 5 99ZZZX837 2 19990108 A 7230 COMPRESSOR BOEING 727 72721 1384003 NM PWA JT8 JT8D7B 52053 NE NR 3 DAMAGED A RYNA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 CE 07 359QS 19007 654372 BWI - FLT 705 - REJECTED TAKEOFF FROM BWI DUE TO COMPRESSOR STALLS NR 3 ENGINE. (ENGINE WAS FOUND TO HAVE FOREIGN OBJEC T DAMAGE TO THE C-1 AND C-2 DISK PLUS STATOR DAMAGE. A TWO ENGINE FERRY TO IND WAS ACCOMPLISHED FOR MAINTENANCE). REMO VED AND REPLACED NR 3 ENGINE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1999030500734 19990305 00734 EA 1999 3 5 RU3A99001 1 19990126 A 4930 3882081H COVER GTCP36150 CNDAIR CL600 CL6002B16 1900305 EA ECU BROKEN A RU3A O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SW 21 86 141 P208 5167 ANC - AIRPORT RAMP. AIRCRAFT OBSERVED TO BE LEAKING FUEL FROM THE LOWER TAIL SECTION WITHIN A FEW MINUTES FOLLOWING APU START. THE AIRCRAFT ENGINES WERE NOT STARTED. THE APU WAS SHUT DOWN WITHOUT FURTHER INCIDENT AND THE FLIGHT CANCELLED . INVESTIGATION REVEALED THE APU LOW-PRESSURE FUEL FILTER COVER MOUNTING EAR FAILED AT THE SCREW MOUNTING HOLE AND SEPA RATED FROM THE FUEL CONTROL UNIT. (X) 2 L 7 2 4F RT A21EA 1999030500735 19990305 00735 EU 1999 3 5 99ZZZX839 1 19990201 A 2120 17185630 LINE AIRESRCH 413458 BOLKMS 105 BO105CBS 5626008 EU ECU FAILED A HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 S677 SHORTLY AFTER TAKEOFF WHEN AIR CONDITIONER WAS TURNED ON, THE PILOT HEARD A LOUD NOISE. RETURNED TO BASE AND LANDED WIT HOUT INCIDENT. MAINTENANCE FOUND DUCT HOSE HAD BLOWN OFF. REPLACED SAME. REF: AIRESEARCH MANUAL 4-379, FIGURE 6, ITE M 20. 1 G 7 2 3U NC H3EU 1999030500737 19990305 00737 EU 1999 3 5 99ZZZX841 1 19990201 A 6520 350A33109100 GEAR SNIAS 350 AS350B2 8680813 EU T/R GEAR BOX MISMANUFACTURED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 93LG 2654 GEAR SET REJECTED NEW OUT-OF-BOX. UNABLE TO OBTAIN GOOD GEAR PATTERN. TRIED ON 2 SEPARATE GEARBOXES WITHOUT SUCCESS. R EPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999030500738 19990305 00738 EU 1999 3 5 99ZZZX842 1 19990107 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESSURE ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 279 13115 S754 PRESSURE TRANSMITTER ERRATIC. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1999030500752 19990305 00752 WP 1999 3 5 TWAA9903201 1 19990302 A 2120 AIR DIST DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE CABIN ODOR A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 9627R 53597 1475 MCI - ON CLIMBOUT HAD A HAZE AND HOT SMELL IN THE CABIN. ACCOMPLISHED PACK BURN OUT AND CHECKED TAIL COMPARTMENT FOR LE AKS, FOUND NONE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999030500753 19990305 00753 WP 1999 3 5 TWAA9903203 1 19990302 A 2120 AIR DIST DOUG DC9 DC982 3022082 WP CABIN ODOR A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 953U 49267 DURING PUSH BACK AND START OF RT ENGINE A BURN SMELL AND HAZE DEVELOPED IN THE AIRCRAFT. FOUND GLYCOL DRAINING FROM THE AFT FUSELAGE AREA. PERFORMED ENG RUNS AND APU TO CHECK FOR FUMES, NONE FOUND. CLEARED CABIN. 2 L 7 2 4F A6WE 1999030500754 19990305 00754 NM 1999 3 5 TWAA9903204 1 19990301 A 3230 RETRACT MECH BOEING 727 727231 1384079 NM NLG LACK OF LUBE A TWAA O OTHER J WARNING INDICATION DE DESCENT 1 CE 05 54351 21983 DURING GEAR EXTENSION FOR LANDING, THE NOSE GEAR DID NOT EXTEND NOR DID THE NOSE GEAR DOORS OPEN. RECYCLED THE GEAR LEV ER AND GEAR EXTENDED. LUBED THE NOSE GEAR, JACKED THE NOSE GEAR AND CYCLED SEVERAL TIMES. OPERATION FOUND NORMAL. 2 L 7 3 4F A3WE 1999030500755 19990305 00755 NM 1999 3 5 TWAA9903205 1 19990302 A 3260 CIRCUIT BREAKER BOEING 727 727231 1384079 NM GEAR INDICATION TRIPPED A TWAA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 CE 05 54344 21631 WHEN THE LANDING GEAR WAS LOWERED THE GREEN DOWN LIGHT WOULD NOT COME ON OR TEST. FOUND CIRCUIT BREAKER POPPED FOR THE MASTER DIMMING NUMBER 1. RESET BREAKER PER MM 33 AND 32. 2 L 7 3 4F A3WE 1999030500756 19990305 00756 WP 1999 3 5 TWAA9903206 1 19990226 A 5320 PRESSURE PANEL DOUG DC9 DC951 3022051 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 416EA 47751 DURING CHECK-C, FOUND THE HORIZONTAL PRESSURE PANEL AT STATION 83.5 ON THE RT SIDE TUNNEL AREA HAD A .5 INCH CRACK. STO P DRILLED THE CRACK, FABRICATED AND INSTALLED A REPAIR DOUBLER PER THE SRM 53-10-10.5. 2 L 7 2 4F RT A6WE 1999030500757 19990305 00757 WP 1999 3 5 TWAA9903207 1 19990226 A 5240 BEAM DOUG DC9 DC951 3022051 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 416EA 47751 DURING OP-9, FOUND .5 INCH CRACK IN THE TOP BEAM AFT CORNER OF THE FWD RT SERVICE DOOR. REPAIRED PER THE SRM 52-51.D. 2 L 7 2 4F RT A6WE 1999030500758 19990305 00758 EU 1999 3 5 AWXA9900065 1 19990301 A 5347 R53070089200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FRAME 20-23 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 IN MAINTENANCE, NUMBER 4 SEAT TRACK CORRODED OUT OF LIMITS AT FR20. SEAT TRACK FABRICATED PER DWG D531120922600 AND SPL ICED INTO EXISTING TRACK. REF SRM 51-71-11. 2 L 7 2 4F RT A28NM 1999030500759 19990305 00759 EU 1999 3 5 AWXA9900066 1 19990301 A 5347 R53070089202 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 765 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 626AW 65 IN MAINTENANCE, NUMBER 3 SEAT TRACK CORRODED OUT OF LIMITS AT FR20-24. SEAT TRACK FABRICATED PER DWG D5311209220500 AND SPLICED INTO EXISTING TRACK. REF SRM 51-72-11. 2 L 7 2 4F RT A28NM 1999030500760 19990305 00760 EU 1999 3 5 AWXA9900067 1 19990301 A 3350 CONNECTOR AIRBUS 320 A320231 3930325 EU ROW 1 LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 618AW 304 IN MAINTENANCE, EMERGENCY EXIT LIGHTS ON SEATS 1, 13, 17, 19 AND 24 INOP. RECONNECTED CANNON PLUG AT WALL FOR SEAT NR 1 , OPS CK GOOD. 2 L 7 2 4F RT A28NM 1999030500761 19990305 00761 NM 1999 3 5 AWXA9900068 1 19990301 A 3350 831862 BATTERY BOEING 737 7372E3 NM RT EMER EXIT DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 IN MAINTENANCE, RT EMERGENCY OVERWING LIGHT OUT. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999030500762 19990305 00762 WP 1999 3 5 9900719985 1 19990226 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 985US 47479 DURING PERIODIC CHECK, FOUND CORROSION ON FUSELAGE SKIN AT FS 218 BETWEEN LONGERONS 23R AND 24R. INSTALLED REPAIR PER S RM 53-04, FIG 12B AND EA 99-163457. 2 L 7 2 4F A6WE 1999030500763 19990305 00763 WP 1999 3 5 9900729952 1 19990228 A 3350 BULB DOUG DC9 DC931 3022065 WP TAIL CONE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. RELAMPED BULBS, OPERATIONAL CHECK NOR MAL. 2 L 7 2 4F A6WE 1999030500764 19990305 00764 WP 1999 3 5 9900739763 1 19990228 A 2133 OUTFLOW VALVE DOUG DC9 DC941 302207N WP CABIN MALFUNCTIONED A NWAA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 01 763NW 47396 LOSS OF CABIN PRESSURIZATION OCCURRED DURING CRUISE FLIGHT AT 29,000 FEET. CABIN ALTITUDE ROSE TO 17,000 FEET AND OXYGE N MASKS WERE DEPLOYED THROUGHOUT THE CABIN. CREW EXECUTED EMERGENCY DESCENT TO 11,000 FEET. FLIGHT WAS DIVERTED TO CRW AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO ATL FOR REPAIRS. MAINTENANCE REPLACED CABIN PRESSURE AMPLIFIER, OUTFLOW VALVE, AND RADIO RACK VENTURI VALVE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999030500765 19990305 00765 NM 1999 3 5 9900745639 1 19990226 A 2612 FIRE LOOP BOEING 757 757251 1384970 NM MLG WW MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 539US 26486 UPON LANDING GEAR EXTENSION, A WHEEL WELL FIRE WARNING EICAS MESSAGE ILLUMINATED. FIRE INDICATION APPEARED TO CORRESPON D WITH ACTUATION OF THE SPEED BRAKES. THE FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WHEEL WELL FIRE DETECTION LOOPS WITH SERVICEABLE UNITS. SYSTEM OPERATIONAL TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999030500766 19990305 00766 NM 1999 3 5 9900752289 1 19990225 A 5753 FASTENERS BOEING 727 727251 138408H NM LT TE FOREFLAP FAILED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 289US 21377 DURING CLIMB AFTER FLAP RETRACTION, AIRCRAFT WAS HARD IN TURNING LEFT. CREW RETURNED TO MSP WITHOUT INCIDENT. MAINTENA NCE FOUND LEFT OUTBOARD FOREFLAP ATTACH FITTING AT OUTBOARD FLAP TRACK HAD SHEARED FASTENERS. 2 L 7 3 4F A3WE 1999030500767 19990305 00767 NM 1999 3 5 UPS99228808 1 19990126 A 5330 6518382164 SKIN BOEING 727 72730C 1384009 NM BS 1090-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, ON CORROSION REMOVAL, PER NRC 811973 & 812094 & EO B727-5330-0509Q, FROM LAP STR 4L AND STR 4R, BS 11 20, CORROSION AND DISBOND FOUND ON CROWN SKIN AND DOUBLERS, BS 1090 TO 1130 RT AND BS 1100 TO 1130 LT STR 4. CORROSION OUT OF LIMITS. CROWN SKIN REPLACEMENT AND REPAIRS TO RT AND LT SKIN CARRIED OUT IAW SMRO EO 99-03-11, REF UPS ENGINEERI NG FILE NUMBER 5330-2101 AND BOEING DRAWING 65-18382. 2 L 7 3 4F A3WE 1999030500768 19990305 00768 NM 1999 3 5 UPS99228809 1 19990125 A 5753 SPACER BOEING 727 72730C 1384009 NM NR 1 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 INSPECTION TYPE-C, NR 1 FLAP TRACK FWD ATTACH FITTING OUTBD AFT SPACER CRACKED. BOLT REMOVED AND NEW SPACER, BOLT, WASH ER AND LOCKNUT INSTALLED IAW SRM 51-30-2 AND MM 20-80-01. 2 L 7 3 4F A3WE 1999030500769 19990305 00769 WP 1999 3 5 UPS99828810 1 19990218 A 5347 S4889189 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 55-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, FS 55 TO 70, RBL 45, THE DOUBLE TRACK IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FS 55 TO 130, RBL 45 IAW SRM 51-1-3. 2 L 7 4 4F RT 4A25 1999030500770 19990305 00770 WP 1999 3 5 UPS99828811 1 19990219 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 641 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 641 BETWEEN LONG 26L AND 27L, THE SHEAR TIE IS CRACKED. CUT OUT DAMAGED SHEAR TIE AND REPAIRED I AW SRM 53-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 1999030500771 19990305 00771 WP 1999 3 5 UPS99828812 1 19990219 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 641 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 641 BETWEEN LONG 26R AND 27R, THE SHEAR TIE IS CRACKED. CUT OUT DAMAGED SHEAR TIE AND REPAIRED I AW SRM 53-2-0 FIG 2B. 2 L 7 4 4F RT 4A25 1999030500772 19990305 00772 WP 1999 3 5 UPS99828813 1 19990219 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 209 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING L/E UPPER SKIN, JUST I/B OF THE I/B SLOT IS CRACKED, APPROX STA FS 209. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 1999030500773 19990305 00773 WP 1999 3 5 UPS99828814 1 19990219 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING LWR L/E SKIN AT FS 572.5 IS CRACKED AT THE SCREW HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4097-B. 2 L 7 4 4F RT 4A25 1999030500774 19990305 00774 WP 1999 3 5 UPS99828815 1 19990219 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING LWR L/E SKIN AT THE FWD I/B CORNER OF THE O/B SLOT IS CRACKED, STA XOLDI 6.225. REPAIRED SK IN IAW EO DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 1999030500775 19990305 00775 WP 1999 3 5 UPS99828816 1 19990219 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 304.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E LWR SKIN AT FS 304.5 IS CRACKED AT 1 FASTENER. STOP DRILLED CRACK AND REPAIRED IAW EO D C8-5720-4087-B. 2 L 7 4 4F RT 4A25 1999030500776 19990305 00776 WP 1999 3 5 UPS99828817 1 19990219 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E LWR SKIN AT FS 572.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 1999030500777 19990305 00777 WP 1999 3 5 UPS99828818 1 19990220 A 5320 3702571 FITTING DOUG DC8 DC873F 302199F WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LONG 31R SPLICE FITTING AT FS 1050 IS CRACKED IN 2 PLACES. REMOVED AND REPLACED FITTING IAW SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1999030500778 19990305 00778 WP 1999 3 5 UPS99828819 1 19990220 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 857, RT SIDE OF THE KEEL BEAM, THE ANGLE IS CRACKED. REPAIRED ANGLE IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999030500779 19990305 00779 WP 1999 3 5 UPS99828820 1 19990220 A 5320 37502571 FITTING DOUG DC8 DC873F 302199F WP BS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LONG 31L SPLICE FITTING IS CRACKED AT FS 610. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500780 19990305 00780 WP 1999 3 5 UPS99828821 1 19990221 A 5320 4610355 FITTING DOUG DC8 DC873F 302199F WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LONG 22L END FITTING AT FS 300 IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500781 19990305 00781 WP 1999 3 5 UPS99828822 1 19990221 A 5320 47505211 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LONG 1 END FITTING IS CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999030500782 19990305 00782 WP 1999 3 5 UPS99828823 1 19990221 A 5320 3779762501 FITTING DOUG DC8 DC873F 302199F WP BS 678 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LONG 9R END FITTING IS CRACKED AT FS 678. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999030500783 19990305 00783 WP 1999 3 5 UPS99828824 1 19990222 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 822.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E RIB AT FS 822.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SR M 57-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999030500784 19990305 00784 WP 1999 3 5 UPS99828825 1 19990222 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E RIB AT FS 785 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999030500785 19990305 00785 WP 1999 3 5 UPS99828826 1 19990222 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 753.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E RIB AT FS 753.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999030500786 19990305 00786 WP 1999 3 5 UPS99828827 1 19990222 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 728.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E RIB AT FS 728.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999030500787 19990305 00787 WP 1999 3 5 UPS99828828 1 19990222 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 716.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E RIB AT FS 716.25 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999030500788 19990305 00788 WP 1999 3 5 UPS99828829 1 19990222 A 5720 5769600 DOUBLER DOUG DC8 DC873F 302199F WP WS 570 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E LWR SKIN DOUBLER IS CRACKED AT FS 570, AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLA CED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999030500789 19990305 00789 WP 1999 3 5 UPS99828830 1 19990222 A 5320 37552221 ANGLE DOUG DC8 DC873F 302199F WP BS 702 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FLOORBEAM ATTACH ANGLE IS CRACKED AT FS 702, RBL 24. REMOVED AND REPLACED THE FITTING IAW SRM 51-3- 0. 2 L 7 4 4F RT 4A25 1999030500790 19990305 00790 WP 1999 3 5 UPS99828831 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 354 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E RIB AT FS 354 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 56-2-0. 2 L 7 4 4F RT 4A25 1999030500791 19990305 00791 WP 1999 3 5 UPS99828832 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 372.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E RIB AT FS 372.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999030500792 19990305 00792 WP 1999 3 5 UPS99828833 1 19990223 A 5720 576958122 CLIP DOUG DC8 DC873F 302199F WP WS 520.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LT WING L/E OUTBOARD ATTACH CLIP AT FS 520.168 IS CRACKED. REMOVED, FABRICATED AND REPLACED CLIP IA W DWG 5769580 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999030500793 19990305 00793 WP 1999 3 5 UPS99828834 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 738.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING L/E RIB AT FS 738.75 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999030500794 19990305 00794 WP 1999 3 5 UPS99828835 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 741.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING L/E RIB AT FS 741.25 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999030500795 19990305 00795 WP 1999 3 5 UPS99828836 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING L/E RIB AT FS 760.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SR M 57-2-0. 2 L 7 4 4F RT 4A25 1999030500796 19990305 00796 WP 1999 3 5 UPS99828837 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING L/E RIB AT FS 760 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0. 2 L 7 4 4F RT 4A25 1999030500797 19990305 00797 WP 1999 3 5 UPS99828838 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 766.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING L/E RIB AT FS 766.25 IS CRACKED BETWEEN THE AFT LWR TWO FASTENERS. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999030500798 19990305 00798 NM 1999 3 5 99UAL900089 1 19990209 A 2130 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E & E COMPT LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 7266U 21413 LOST CABIN PRESSURE, DESCENDED TO 10,000 FEET AND RETURNED TO ORD. *S/D* MAINTENANCE DETECTED DOOR 1 RIGHT LEAKING. A LSO, FOUND FWD E & E DRAIN VALVE LEAKING. REPLACED DRAIN VALVE AND REINSTALLED DOOR SEAL AND PERFORMED HULL LEAKAGE CH ECK. 2 L 7 3 4F 4 F A3WE E2EA 1999030500799 19990305 00799 NM 1999 3 5 99UAL900116 1 19990218 A 3246 BEA7300000497AFA BEARING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 3 MLG FAILED A UALA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 WP 29 366UA 23 24535 PLANE ARRIVED WITH NR 3 MAIN LANDING GEAR TIRE MISSING. *S/D* AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED NR 3 OUTBOARD WHEEL BEARING. FAILED OUTBOARD BEARING WAS FOUND TO BE 737-291 INBOARD WHEEL BEARING (P/N BEA7300-000497AFA). REPLACE D NR 3 WHEEL/TIRE AND BRAKE ASSEMBLIES. DUE TO HEAT DAMAGE CAUSED BY BEARING FAILURE, RIGHT HAND MAIN LANDING GEAR INNE R CYLINDER ALSO REQUIRED REPLACEMENT, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999030500800 19990305 00800 NM 1999 3 5 99UAL900117 1 19990220 A 3260 189983 SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT MLG FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 397UA 24672 LANDING GEAR UNSAFE LIGHT ILLUMINATED. *S/D* REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH PER MM 32-61-21 AND WDM32-6 4-01. PERFORMED OPS CK. FOUND OK PER MM 32-61-21. 2 L 7 2 4F 4 F RT A16WE E2GL 1999030500801 19990305 00801 NE 1999 3 5 99UAL900118 2 19990220 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 BIRD STRIKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 925UA 26646 727426 SLIGHT ELECTRICAL ODOR IN CABIN. *S/D* THERE WAS A BIRD STRIKE DOWN CORE OF NR 2 ENGINE. THE ENGINE WAS BORESCOPED AN D NO DAMAGE REPORTED. REPLACED COALESCER BAGS AND NO OTHER ABNORMAL SMELLS WERE NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999030500802 19990305 00802 NE 1999 3 5 99UAL900119 2 19990219 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DETERIORATED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN A M R FLAME/FIRE OVER TEMP PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 650UA 8451 25287 717541 NR 2 COMPRESSOR STALL AT 800 AGL. EGT 724 SUSTAINED WITH AUDIABLE SOUNDS. FLAMES REPORTED BY TOWER. ENGINE SHUT DOWN, E MERGENCY DECLARED. RETURNED TO MVD WITHOUT INCIDENT. *S/D* ENGINE EXPERIENCED A GROUP 3 SURGE EVENT. GROUPE 3 SURGES ARE THE RESULT OF EXCESSIVE BLADE TIP CLEARANCES IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. ENGINE WAS REMOVE D FOR HIGH PRESSURE COMPRESSOR REFURBISHMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999030500803 19990305 00803 EU 1999 3 5 99UAL900120 1 19990222 A 2121 FAN TECHNOFAN F EVT3454G AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT OVERHEATED A UALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 411UA 1399 464 FLIGHT CREW ADVISED DISPATCH OF FUMES IN THE COCKPIT (POSSIBLY DUE TO AN EXTRACT FAN OVERHEAT). CREW ON OXYGEN. DECLAR ED EMERGENCY FOR EXPEDITED LANDING AT ORD ON 14L. EXTRACT FAN OVERHEATED. NO REPORTED APU PROBLEMS. EXTRACT FAN REPLA CED PER MM 21-26-51. REPLACEMENT FAN OPERATES OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999030500805 19990305 00805 NM 1999 3 5 99UAL900123 1 19990222 A 3320 61482 BALLAST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LAVATORY FAILED A UALA A H J UNSCHED LANDING DEACTIVATE SYST/CIRCUITS DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7465U 21919 STRONG ELECTRICAL SMELL FROM THE FORWARD LAVATORY. CREW ISOLATED THE SMELL TO A PANEL WHERE THE LIGHT SWITCH IS LOCATED . CIRCUIT BREAKERS PULLED. SMELL DID NOT GO AWAY. DUMPED FUEL AND DIVERTED TO PIT. *S/D* LAVATORY MOTOR AND TIMER, UNDER SINK HOT WATER HEATER AND MIRROR LIGHT BALLAST REPLACED. AIRCRAFT OPERATED NORMALLY. 2 L 7 3 4F 4 F A3WE E2EA 1999030500806 19990305 00806 NM 1999 3 5 99UAL900124 1 19990221 A 2131 CONTROLLER 7632101 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER CR CRUISE 1 WP 29 7454U 21908 CABIN PRESSURE WENT TO 10,800 FEET AT 28,000 FEET ALTITUDE. THE OUTFLOW VALVE WAS FULLY CLOSED, WENT TO STANDBY, THEN T O MANUAL AND GOT THE PRESSURIZATION TO HOLD 8,000 FEET AT 10,000 FEET ALTITUDE. OPERATED IN MANUAL FOR THE REST OF THE TRIP. MAINTENANCE ACCOMPLISHED A LEAK CHECK AND NONE WERE FOUND. AS A PRECAUTION THE PRESSURE CONTROLLER WAS REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999030500807 19990305 00807 NM 1999 3 5 99UAL900125 1 19990216 A 3610 S212W3019 SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE AFT PRESS DOME TORN A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 795UA 5670 26927 CONSTANT VIBRATION FELT IN AFT GALLEY FLOOR. CREW ELECTED TO RETURN TO MIA. *S/D* THE BOOT, (P/N S212W301-9, IPC 36-1 2-04-005, ITEM 155) AT THE PENETRATION OF THE APU DUCT INTO THE AFT DOME OF FUSELAGE, WAS FOUND TORN IN THE SEAM. FURTH ER EXAMINATION OF THE BOOT REVEALED THAT THE STEEL RING (INSIDE THE BOOT) SNAPPED AT THE WELD. THE BOOT WAS REPLACED AN D THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999030500808 19990305 00808 NM 1999 3 5 99UAL900126 1 19990222 A 5270 834403 PROXIMITY SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMER EXIT DOOR OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 654UA 25392 LEFT WING SLIDE EICAS MSG INTERMITTENTLY DISPLAYED. PER IRREGULAR PROCEDURE, AIRCRAFT DIVERTED TO MIA. LOG READS: APPROX IMATELY 5 HRS INTO THE FLIGHT, L WING SLIDE EICAS MSG ILLUMINATED ALONG WITH EMER. DOORS ON OVHD PANEL BOTH LIGHTS CYCL ED ON AND OFF FOR APPROX 30 MINS. *S/D* FOUND SENSOR S218 OUT OF TOLERANCE. ADJUSTED SENSOR S218 PER MM, OPS CHECKS N ORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999030500809 19990305 00809 EU 1999 3 5 99UAL900127 1 19990221 A 3350 321454 POWER SUPPLY DIEHL GMBH & 321430 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 441UA 751 EMERGENCY LIGHT TEST FAILS WITH EPSU INT LOAD R MESSAGE. *S/D* INTERNAL LOAD FAULT WAS DETECTED AT THE EMERGENCY POWER S UPPLY UNIT (12WL). THE EMERGENCY POWER SUPPLY UNIT AND ITS BATTERY WERE THEN REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999030500810 19990305 00810 EU 1999 3 5 99UAL900128 1 19990222 A 7932 B NUT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OIL PRESS LINE CROSS THREAD A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 413UA 470 V10021 FLIGHT DIVERTED TO CUU DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY IN NR 2 ENGINE. ENGINE NR 2 OIL QUANTITY SHOWS 4.5 QT, FLASHING, ALL OTHER INDICATIONS NORMAL. OIL PRESSURE LINE FITTING WAS FOUND LOOSE AT T-FITTING ABOVE PRESSURE SWITC H, CAUSING OIL LEAKAGE AT CRUISE POWER SETTINGS. B-NUT APPEARED TO BE CROSS THREADED. THE DAMAGED TUBES HAVE BEEN RETU RNED TO LUFTHANSA, THE V2500 REPAIR SHOP, FOR QUALITY ASSURANCE INVESTIGATION. NOTIFIED ENGINE REPAIR VENDOR TO ENSURE TUBES ARE PROPERLY INSTALLED AT FUTURE ENGINE SHOP VISITS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999030500811 19990305 00811 NM 1999 3 5 99UAL900129 1 19990224 A 5523 HINGE BOEING 6973799 BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE ELEVATOR TAB FAILED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 982UA 21640 HEAVY VIBRATION FELT THROUGH OUT THE CABIN. *S/D* RIGHT ELEVATOR TAB INBOARD HINGE FITTING SEPARATED FROM THE TAB LEADIN G EDGE. TEAR OUT OF THE TAB SKIN INDICATES THAT AT LEAST THREE OF FOUR FASTENERS WERE INSTALLED WHEN SEPARATION OCCURRE D. SIGNS OF WEAR ON UPPER SURFACE OF HINGE FITTING AND MATING SURFACE ON TAB SKIN. HELI-COIL INSERT IN THE TOP OUTER H OLE OF THE FITTING WAS CRACKED IN THREE PLACES AND HELI-COIL INSERT IN THE LOWER OUTBOARD HOLE WAS CRACKED IN ONE PLACE. ELEVATOR AND TAB ASSEMBLY REPLACED PER MM 27-31-01-201, OPS CHECK OK. 2 L 7 2 4F 4 F A16WE E2EA 1999030500812 19990305 00812 NE 1999 3 5 99UAL900130 2 19990225 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT BIRD STRIKE A UALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 29 538UA 25222 RETURNED TO FIELD DUE TO A BIRD STRIKE IN THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999030500813 19990305 00813 WP 1999 3 5 ABXA9900146 1 19990130 A 5755 5910055517 BRACKET DOUG DOUG DC9 DC933F 302207A WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 LEFT WING SPOILER ACTUATOR BRACKET, LOWER SURFACE CRACKED. REPAIRED UNIT COMPLETE. 2 L 7 2 4F A6WE 1999030500814 19990305 00814 WP 1999 3 5 ABXA9900147 1 19990217 A 5320 99220431 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 294 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FRAME FITTING CRACKED AT STATION 294, BETWEEN LONGERONS 22 LEFT AND 23 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 1999030500815 19990305 00815 WP 1999 3 5 ABXA9900148 1 19990223 A 5320 9911840165 SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 1089 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND CORRODED SHEAR TIE AT STATION 1089, BETWEEN LONGERONS 2 LEFT AND 3 LEFT. REPLACED SHEAR TIE IAW D C9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999030500816 19990305 00816 WP 1999 3 5 ABXA9900149 1 19990223 A 5311 99118777 FRAME DOUG DOUG DC9 DC933F 302207A WP BS 1132 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FRAME CORRODED AT STATION 1132. REPLACED FRAME IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999030500817 19990305 00817 WP 1999 3 5 ABXA9900150 1 19990223 A 5320 39573171 BRACKET DOUG DOUG DC9 DC933F 302207A WP BS 370 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND BRACKET AT FORWARD CARGO STATION 370 CRACKED AND CORRODED. REPLACED BRACKET IAW DC9 SRM. 2 L 7 2 4F A6WE 1999030500818 19990305 00818 NM 1999 3 5 VNAA9902023 1 19990228 A 6120 3039242 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP MALFUNCTIONED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 430JS 1161 3044 THE LEFT HAND PROPELLER FAILED TO COME OUT OF FEATHER WHEN SELECTED, DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND REPLACED THE LEFT HAND PROPELLER SPEED SENSOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 77 -12-11. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030500819 19990305 00819 NM 1999 3 5 VNAA9903003 1 19990302 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 461PS 8415 67508 3075 THE RIGHT HAND PROPELLER WOULD NOT COME OUT OF FEATHER WHEN SELECTED DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 6 1-21-06. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999030900001 19990309 00001 NM 1999 3 9 DL72E990306 1 19990214 A 5330 655456414 SKIN BOEING 727 727247 138408F NM BS 530 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 FUSELAGE SKIN FS 520-540, STRINGER 25L-26L, REPAIR FOR PUNCTURE. THE FUSELAGE SKIN BETWEEN FS 520 AND 540 AND BETWEEN S TRINGERS 25L AND 26L WAS PUNCTURED. THE DAMAGED SKIN WAS CLEANED UP WITH A 9 BY 5 CUTOUT. THE CUTOUT WAS REPAIRED WI TH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3 AND DOCUMENTED PER ER/A 366704-14. 2 L 7 3 4F A3WE 1999030900002 19990309 00002 NM 1999 3 9 DL72L990316 1 19990214 A 5311 FRAME BOEING 727 727232 1384082 NM BS 761 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 FUSELAGE RT OVERWING EXIT FRAME, FS 761, FRAME CHORD REPAIR. THE FS 761 FRAME FOR THE RT OVERWING EXIT CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE INNER CHORD. THE FRAME WAS REPAIRED/MODIFIED PER BAC S/B 727-53-0197 WITH MODIFICATION S REQUIRED DUE TO EXISTING AUX. FUEL TANK MODIFICATION PARTS AND OTHER DISCREPANCIES. THE REPAIR WAS DOCUMENTED PER ER /A 366652-14AD. 2 L 7 3 4F A3WE 1999030900003 19990309 00003 NM 1999 3 9 DL72L990317 1 19990214 A 5311 FRAME BOEING 727 727232 1384082 NM BS 783.95 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 FUSELAGE RT OVERWING EXIT CUTOUT FRAME FS 783.95, REPAIR FOR DAMAGED HOLES. UPON INSPECTION FOR TYPICAL CRACKS IN THE I NNER CHORD OF THEFS 783.95 OVERWING EXIT CUTOUT FRAME, SEVERAL HOLES WERE FOUND MISDRILLED. THE PREVENTATIVE MODIFICATI ON PER BAC S/B 727-53-0197 WAS INSTALLED WITH CHANGES TO ACCOUNT FOR DISCREPANT CONDITIONS. THE REPAIR WAS DOCUMENTED PER ER/A 366645-14AD. 2 L 7 3 4F A3WE 1999030900004 19990309 00004 NM 1999 3 9 DL72L990318 1 19990214 A 5311 FRAME BOEING 727 727232 1384082 NM BS 784 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 FUSELAGE LT OVERWING EXIT CUTOUT FRAME FS 784, REPAIR FOR DISCREPANT FASTENER HOLES. WHILE ACCOMPLISHING INSPECTIONS OF THE LT OVERWING EXIT CUTOUT FRAME AT FS 784, SEVERAL FASTENER HOLES WERE FOUND OVERSIZED DAMAGED. THE MODIFICATION PER BAC S/B 727-53-0197 WAS INSTALLED WITH FASTENER DEVIATIONS TO CLEAR UP THE DAMAGE. THE REPAIR WAS DOCUMENTED PER ER/A 366646-14AD, REV A. 2 L 7 3 4F A3WE 1999031200001 19990312 00001 NM 1999 3 12 TWAA9903301 1 19990303 A 3350 767 BULB BOEING 767 767231 1385131 NM EMER EXIT FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 608TW 22571 LEFT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. RELAMP WAS NO HELP. COULD NOT DUPLICATE. CHECK-C 2-3-99 LAX. 2 L 7 2 4F RT A1NM 1999031200002 19990312 00002 NM 1999 3 12 TWAA9903302 1 19990303 A 3350 LIGHT BOEING 767 767330 NM R5 EXIT INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 EXTERIOR LIGHT LOCATED AT R5 EXIT INOP. SECURED AND ADJUSTED SOCKET. CHECK-C 12-19-98. 2 L 7 2 4F RT A1NM 1999031200003 19990312 00003 WP 1999 3 12 TWAA9903303 1 19990303 A 3340 8906K1268 SWITCH DOUG DC9 DC982 3022082 WP LANDING LIGHT FAILED A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 05 906TW 49160 ELECTRICAL SMOKE COMING FROM AREA AROUND THE LANDING LIGHT SWITCH. REMOVED AND REPLACED THE NOSE LANDING LIGHT SWITCH ( P/N 8906K1269) AND RT WING TAXI LIGHT SWITCH (P/N 8906K1268). CHECK-C 1-28-99 STL. 2 L 7 2 4F A6WE 1999031200004 19990312 00004 EU 1999 3 12 MALA976365 1 19990302 A 2450 A2042C PDU SAAB SF340 340B 7860101 EU LEFT FAILED A MALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 15 411XJ 411 ON INITIAL CLIMBOUT, THE LEFT MAIN BUS FAILED. REPLACED THE LEFT PDU. 2 L 7 2 4T RT A52EU 1999031200005 19990312 00005 EU 1999 3 12 MALA976366 1 19990302 A 2120 460250 SEAL BAC 146 AVRO146RJ85A 1500097 EU RT Y DUCT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 15 506XJ E2314 R-ZONE HIGH TEMP ILLUMINATED DURING TAKEOFF, LIGHT EXT WHEN ENG 3 AND 4 AIR VALVES WERE CLOSED. REPLACED WORN PERI-SEAL S ON RT Y-DUCT. RAN A/C, OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999031200006 19990312 00006 1999 3 12 CALA9900206 4 19990303 A 2565 5WD230600203 SLIDE DOUG DC10 DC1030 3023501 WP R-3 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19072 46576 THE R-3 DOOR EMERGENCY SLIDE LOW PRESSURE INDICATOR LIGHT WAS FOUND ILLUMINATED DURING A PRE-DEPARTURE CHECK. THE R-3 D OOR EMERGENCY SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-02, PAGE 201-208. 2 L 7 3 4F A22WE 1999031200007 19990312 00007 WP 1999 3 12 CALA9900207 1 19990301 A 3350 AD4002P BATTERIES AEROQUALITY DOUG DC9 DC932 3022066 WP TAIL CONE DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND THE TAIL CONE EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATION CHECKE D GOOD. 2 L 7 2 4F A6WE 1999031200008 19990312 00008 WP 1999 3 12 CALA9900208 1 19990302 A 3350 EA1CS2522D2 BATTERIES GE DOUG DC9 DC932 3022066 WP LT & RT NACELLE DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND BOTH NACELLE EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECK ED GOOD. 2 L 7 2 4F A6WE 1999031200009 19990312 00009 WP 1999 3 12 CALA9900209 1 19990302 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 10 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14524 47539 INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE FOUND LIGHT WIRE PULLED FROM SPLICE. T HE WIRE WAS RESPLICED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999031200010 19990312 00010 WP 1999 3 12 CALA9900210 1 19990302 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND E & E COMPARTMENT WEB MEMBRANE CORRODED AT STA 200, RT SIDE. THE AREA WAS REPAIRED IAW ECRA 5305-01049 AND SRM 53-05, FIGURE 55. 2 L 7 2 4F A6WE 1999031200011 19990312 00011 WP 1999 3 12 CALA9900211 1 19990303 A 5321 FLOORBOARD DOUG DC10 DC1030 3023501 WP FLT DECK CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND FLIGHT DECK FLOORBOARD NR 216AF DELAMINATED AND CORRODED. A NEW FLOORBOARD WAS INSTALLED AND SEALED IA W ECRA 5100-01844. 2 L 7 3 4F A22WE 1999031200012 19990312 00012 WP 1999 3 12 CALA9900212 1 19990303 A 5320 ANGLE DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 63 AND 51-30-5. 2 L 7 2 4F A6WE 1999031200013 19990312 00013 WP 1999 3 12 CALA9900213 1 19990303 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND LONGERON 30 CORRODED IN E & E COMPARTMENT AT STA 180. THE CORRODED SECTION OF LONGERON WAS REPLACED IA W SRM 51-10-3. 2 L 7 2 4F A6WE 1999031200014 19990312 00014 WP 1999 3 12 9900769310 1 19990223 A 5320 WEB DOUG DC9 DC982 3022082 WP FRAME 1463 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 313RC 48091 DURING PERIODIC CHECK, FOUND CANTED WEB CRACKED AT FRAME 1463, UPPER RIGHT SIDE. REPAIRED PER EA 93-160907. 2 L 7 2 4F A6WE 1999031200015 19990312 00015 WP 1999 3 12 9900779310 1 19990225 A 5320 FRAME DOUG DC9 DC982 3022082 WP WINDOW 34 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 313RC 48091 DURING PERIODIC CHECK, FOUND WINDOW 34 FRAME CRACKED AT UPPER FORWARD CORNER. FABRICATED AND INSTALLED REPAIR ANGLE PER EA 93-163706. 2 L 7 2 4F A6WE 1999031200016 19990312 00016 WP 1999 3 12 9900789310 1 19990225 A 5320 PAN DOUG DC9 DC982 3022082 WP WINDOW 34 L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 313RC 48091 DURING PERIODIC CHECK, FOUND WINDOW 34L PAN CORNER CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER PER EA 93-163706. 2 L 7 2 4F A6WE 1999031200017 19990312 00017 WP 1999 3 12 9900799310 1 19990225 A 5320 FRAME DOUG DC9 DC982 3022082 WP WINDOW 36L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 313RC 48091 DURING PERIODIC CHECK, FOUND INTERNAL WINDOW FRAME CRACKED AT 36L. INSTALLED DOUBLER PER EA 93-163707. 2 L 7 2 4F A6WE 1999031200018 19990312 00018 WP 1999 3 12 9900809985 1 19990224 A 5330 SKIN DOUG DC9 DC932 3022066 WP FRAME 598 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 985US 47479 DURING PERIODIC CHECK, FOUND CORROSION ON SKIN UNDER FRAME 598 ON FORWARD SIDE ONE INCH BELOW LONGERON 18R. REPAIRED PE R EA 99-165598. 2 L 7 2 4F A6WE 1999031200019 19990312 00019 WP 1999 3 12 9900819985 1 19990224 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218-229 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 985US 47479 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 26L BETWEEN FS 218 AND FS 229. SPLICED IN NEW LONGERON PER EA 99-163 380. 2 L 7 2 4F A6WE 1999031200020 19990312 00020 WP 1999 3 12 9900829903 1 19990224 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 DURING PERIODIC CHECK, FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD RIGHT SIDE STIFFENER CRACKED ON OUTBOARD END. REPAIR ED PER EA 99-163459. 2 L 7 2 4F A6WE 1999031200021 19990312 00021 WP 1999 3 12 9900831141 1 19990107 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1741-1771 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 141US 46750 DURING M-CHECK, FOUND CORROSION BETWEEN FS 1741 AND 1771 ON LONGERON 50L. REPAIRED PER EA 11-162749. 2 L 7 3 4F A22WE 1999031200022 19990312 00022 EA 1999 3 12 COMA9960089 1 19990303 A 3010 WARNING CNDAIR CL600 CL6002B19 EA WING ANTI ICE ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 916CA 7014 WING ANTI-ICE DUCT WARNING. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999031200023 19990312 00023 EA 1999 3 12 COMA9960090 1 19990303 A 3010 14463101 TUBE CNDAIR CL600 CL6002B19 EA LT WING CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 7014 WING ANTI-ICE DUCT WARNING. REPLACED LEFT HAND WING OUTBOARD PICCOLO TUBE. 2 L 7 2 4F RT A21EA 1999031200024 19990312 00024 EA 1999 3 12 COMA9960091 1 19990302 A 3020 12681 SWITCH CNDAIR CL600 CL6002B19 EA RT COWL ANTI ICE FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 958CA 7111 RIGHT HAND COWL ANTI-ICE CAUTION MESSAGE. REPLACED COWL ANTI-ICE PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 1999031200025 19990312 00025 EA 1999 3 12 COMA9960092 1 19990302 A 2613 OVERHEAT SYST CNDAIR CL600 CL6002B19 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 937CA 7044 AIRCRAFT MADE UNSCHEDULED LANDING WHEN ENCOUNTERING ICING CONDITIONS WITH GEAR DOWN WHILE MLG OVERHEAT SYSTEM WAS DEFERR ED. REPAIRED MLG OVERHEAT WARNING SYSTEM. 2 L 7 2 4F RT A21EA 1999031200026 19990312 00026 NM 1999 3 12 QXEA9900420 1 19990225 A 2611 WIRE DHAV DHC8 DHC8102 2809003 NM AFT SMOKE DET BROKEN A QXEA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 09 811PH 23 PDX- AFT SMOKE DETECTOR LIGHT STAYS ON. MAINTENANCE REPAIRED BROKEN WIRES 2612-4A22 AT CONNECTION 2612-P2. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999031200027 19990312 00027 NM 1999 3 12 QXEA9900421 1 19990228 A 5210 85210240005 STRUT DHAV 85210165003 DHAV DHC8 DHC8102 2809003 NM CABIN DOOR MALFUNCTION A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 816PH 54 YVR- MAIN CABIN DOOR WILL NOT OPEN. MAINTENANCE FERRIED FROM YVR TO PDX FOR REPAIRS. IN PDX, REPLACED FORWARD HANDRAIL STRUT. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999031200028 19990312 00028 NM 1999 3 12 QXEA9900422 1 19990228 A 5210 85210263102 STRUT DHAV 85210165003 DHAV DHC8 DHC8202 2809007 NM CABIN DOOR MALFUNCTIONED A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 828PH 526 SEA- MAIN CABIN DOOR HANDLE HARD TO PUSH UP. FERRIED FROM SEA TO PDX FOR REPAIRS. IN PDX, REPLACED UPPER AND LOWER DOO R SPRING STRUTS AND LUBRICATED DOOR. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999031200029 19990312 00029 EU 1999 3 12 QXEA9900423 1 19990301 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 BOI - AFT 3 EVACUATION LIGHTS IN CEILING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. OPERATIONAL CHECK S GOOD. 2 L 7 2 4F RT A20EU 1999031200030 19990312 00030 EU 1999 3 12 QXEA9900424 1 19990301 A 3350 6008905 BATTERY PACK GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 1 DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 BOI - WHEN POWER IS REMOVED FROM AIRCRAFT THE EMERGENCY AISLE LIGHTS IN ROWS 1 TO 5 REMAIN ON. MAINTENANCE REPLACED THE ROW 1 BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1999031200031 19990312 00031 EU 1999 3 12 QXEA9900425 1 19990302 A 3350 6008905 BATTERY PACK GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 11-14 DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 SEA - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 11 TO 14 ARE INOPERATIVE. MAINTENANCE REPLACED REAR MOST BATTERY PACK, OPER ATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1999031200032 19990312 00032 EU 1999 3 12 QXEA9900426 1 19990227 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU RT WING INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 PDX - RIGHT WING AFT UNDERWING EVACUATION LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, OPERATIO NAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1999031200033 19990312 00033 WP 1999 3 12 ABXA9900151 1 19990216 A 5320 59175331 ANGLE DOUG DOUG DC9 DC932 3022066 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK, FOUND LEFT MAIN LANDING GEAR 'Z' ANGLE CRACKED. REPLACED 'Z' ANGLE IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999031200034 19990312 00034 WP 1999 3 12 ABXA9900152 1 19990216 A 5313 27779224 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK, FOUND LONGERON 17 LEFT, STATION 980 CRACKED. REPLACED SEGEMENT OF LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999031200035 19990312 00035 WP 1999 3 12 ABXA9900153 1 19990216 A 5311 99196152 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK, FOUND RIGHT FUSELAGE FRAME STATION 658 CRACKED. REPAIRED IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999031200036 19990312 00036 WP 1999 3 12 ABXA9900154 1 19990216 A 5315 99581891 FLOORBEAM DOUG DOUG DC9 DC932 3022066 WP BS 699 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK, FOUND FLOORBEAM CORRODED, UPPER 'T' CAP AT STATION 699. REPAIRED IAW ABX REA D953-26839MR. 2 L 7 2 4F A6WE 1999031200037 19990312 00037 WP 1999 3 12 ABXA9900155 1 19990116 A 5311 991224310 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK, FOUND PYLON BULKHEAD FRAME CRACKED, STATION 965 AT LONGERONS 15 TO 16 LEFT. 2 L 7 2 4F A6WE 1999031200038 19990312 00038 WP 1999 3 12 ABXA9900156 1 19990302 A 5250 LATCH DOUG DC9 DC931 3022065 WP COCKPIT DOOR LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 COCKPIT DOOR WOULD NOT OPEN FROM CABIN. LATCH SLIPPED. SECURED DOOR KNOB LATCH SCREW. 2 L 7 2 4F A6WE 1999031200039 19990312 00039 WP 1999 3 12 ABXA9900157 1 19990302 A 2425 MS250022 SWITCH DOUG DC8 DC861 3021952 WP COCKPIT FAILED A ABXA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 848AX 46032 DURING TAKEOFF AT ROTATION SPEED, AC FREQ METER WENT OFF SCALE LOW IN ALL POSITIONS. UNABLE TO MONITOR GENERATORS. DUM PED FUEL AND RETURNED TO ONT. REPLACED VOLT AND FREQ SELECTOR SWITCH AND FREQ METER INDICATOR. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999031200040 19990312 00040 WP 1999 3 12 TC8A99002 1 19990304 A 2612 FIRE WARNING DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE ACTIVATED A TC8A A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 182SK 45817 642688 AFTER T/O PASSING THROUGH 9,000 FEET, RECEIVED FIRE WARNING INDICATION ENGINE NR 3. ACCOMPLISHED ENGINE FIRE SEPARATION OR SERVERE DAMAGE CHECKLIST. AFTER FIRE SHUTOFF LEVER MOVED TO SELECT AGENT POSITION, FIRE INDICATIONS CEASED. COMPLE TED FIRE WARNING SYSTEM CONTINUITY TEST. DECLARED EMERGENCY LANDING AND MADE UNEVENTFUL LANDING AT KIAH. (EGT SHOWED 5 00 DEGREES WHEN WARNING RECEIVED). 2 L 7 4 4F 4 F 4A25 1E8 1999031200166 19990312 00166 NM 1999 3 12 SWAA990349 1 19990223 A 5321 FLOOR BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR WEB AT BS 1016 LBL 38 TO 41.5 WL 208.5. REMOVED CORROSION ON FLOOR W EB BS 1016 LBL 38 - 41, WL 208.5 FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW WEB PER SRM. 2 L 7 2 4F RT A16WE 1999031200167 19990312 00167 NM 1999 3 12 SWAA990350 1 19990223 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND BS 344 FLOORBEAM HAS SURFACE CORROSION ON TOP SIDE AND BOTTOM SIDE OF UPPER CHORD BL 0, RBL 1.5, LBL 7, WL 208. BLENDED CORROSION REMOVED SECTION THAT WAS OUT OF LIMITS, FABRICATED REPAIR PARTS, ALODI NED AND PRIMED AND INSTALLED. ALL WORK DONE PER SRM. 2 L 7 2 4F RT A16WE 1999031200168 19990312 00168 NM 1999 3 12 SWAA990351 1 19990223 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CORROSION ON WEB AT BS 986.5 - 993, RBL 45, WL 208. REMOVED CORROSION, MAX MATERIAL. R EMOVED 4 BY 3 BY.013 OUT OF LIMITS PER SRM. REMOVED WEB BS 986.5-993, WL 208, RBL 45. DRILLED UP, ALODINED, PRIMED AN D INSTALLED NEW WEB PER SRM. 2 L 7 2 4F RT A16WE 1999031200169 19990312 00169 NM 1999 3 12 SWAA990352 1 19990223 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 295-328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, WEB BS 295-328, RBL 62, WL 208 HAS CORROSION. REMOVED CORROSION ON WEB AT BS 295-328, RBL 62, WL 208. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1 FIG 101. REMOVED DAMAGED WEB AND FABRICATED, DRILLED UP, ALODINE D, PRIMED AND INSTALLED REPLACEMENT WEB PER SRM. 2 L 7 2 4F RT A16WE 1999031200170 19990312 00170 NM 1999 3 12 SWAA990353 1 19990223 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND BS 947 FLOORBEAM IS CRACKED AT LT BL 54, WL 208. CUT OUT CRACK, FABRICATED REPAIR PARTS , LOCATED AND DRILLED REPAIR PARTS. ALODINED, PRIMED, SEALED AND INSTALLED REPAIR SECTION, STRAPS AND ANGLES PER SRM. 2 L 7 2 4F RT A16WE 1999031200171 19990312 00171 NM 1999 3 12 SWAA990354 1 19990223 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 13 AND 14, BS 360 LT. REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE, ALODINED AND PRIMED, INSTALLED NEW SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 1999031200172 19990312 00172 NM 1999 3 12 SWAA990355 1 19990223 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, CRACKED STRINGER CLIP AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 1999031200173 19990312 00173 NM 1999 3 12 SWAA990356 1 19990223 A 3220 65522350 FITTING BOEING 737 7373H4 1384600 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND LT MLG AFT STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999031200174 19990312 00174 NM 1999 3 12 SWAA990357 1 19990223 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CHANNEL STR 14L, BS 360. REMOVED AND REPLACED STRINGER CHANNEL PER SRM . 2 L 7 2 4F RT A16WE 1999031200175 19990312 00175 NM 1999 3 12 SWAA990358 1 19990223 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 14 AND 15 BS 360 LT SIDE. REPLACED SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 1999031200176 19990312 00176 NM 1999 3 12 SWAA990359 1 19990223 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 14 AND 15 BS 360 LT SIDE. REPLACED SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 1999031200177 19990312 00177 NM 1999 3 12 SWAA990360 1 19990223 A 5711 SPAR BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND DURING NDI INSPECTION, CRACK IN RIGHT WING REAR SPAR UPPER CHORD AT LOWER ROW OR VERTICA L FLANGE, FIRST HOLE I/B OF MLG BEAM FITTING CUTOUT. REMOVED CRACK FROM RIGHT WING UPPER SPAR CHORD ON LOWER ROW FIRST INBOARD HOLE OF MAIN LANDING GEAR BEAM FITTING BY OVERSIZING HOLE. INSTALLED FASTENERS PER TRAMCO EWO 99-0175. 2 L 7 2 4F RT A16WE 1999031200178 19990312 00178 NM 1999 3 12 SWAA990361 1 19990223 A 5240 SKIN BOEING 737 7377H4 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 706SW 28740 DURING SCHEDULED C3 CHECK, FOUND FORWARD SERVICE DOOR HAS 1.25 INCH CRACK AT LOWER AFT CORNER. CRACK IS .75 INCH FROM O /B SIDE AND .5 INCH FROM BOTTOM. REPAIRED PER SWA RA 1-753-2024. 2 L 7 2 4F RT A16WE 1999031200179 19990312 00179 NM 1999 3 12 SWAA990362 1 19990223 A 5240 SKIN BOEING 737 7375H4 138449D NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED 1/2D CHECK, FOUND 2 DOOR SKIN CRACKS COMING OUT OF THE SAME RIVET HOLE. FIRST CRACK IS .375 INCH LONG, SECOND IS .75 INCH LONG, AT LOWER AFT CORNER JUST ABOVE LOWER GATE HINGE. REPAIRED CRACK PER SRM. 2 L 7 2 4F RT A16WE 1999031200180 19990312 00180 NM 1999 3 12 SWAA990363 1 19990223 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN CHAFED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHTING WIRES CHAFED WHERE IT COMES THROUGH FLOOR. REPLACED BROKEN AND CH AFED WIRING AT FLOOR PANEL PER BOEING STANDARD WIRING PRACTICES. 2 L 7 2 4F RT A16WE 1999031200181 19990312 00181 NM 1999 3 12 SWAA990364 1 19990223 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED 1/2D CHECK, FOUND AFT CABIN FLOORBEAM BS 986 CORRODED AROUND FASTENER HOLE LBL9. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200182 19990312 00182 NM 1999 3 12 SWAA990366 1 19990223 A 5320 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED 1/2D CHECK, FOUND FWD STUB FRAME CRACKED AT FWD SERVICE DOOR UPPER STRAP. REMOVED AND REPLACED FRAME P ER SRM. 2 L 7 2 4F RT A16WE 1999031200183 19990312 00183 NM 1999 3 12 SWAA990367 1 19990224 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND 4 CRACKS AT STA 178 BULKHEAD, WL 188 AND 207, RBL 1 TO LBL 1, AND RBL 28.5 TO LBL 28.5. REPAIRED PER SRM 51-20-07, 51-40-05 AND 53-10-08. 2 L 7 2 4F RT A16WE 1999031200184 19990312 00184 NM 1999 3 12 SWAA990368 1 19990224 A 5312 BAC1518 BLKHD STIFFENER BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CRACK ON VERTICAL STIFFENER BS 663 BULKHEAD, WL 178, RBL 6. REPLACED PART PER SRM. 2 L 7 2 4F RT A16WE 1999031200185 19990312 00185 NM 1999 3 12 SWAA990369 1 19990224 A 5320 BAC1489 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BS 360, STR 14R. REPAIRED PART PER SRM 53-00-07, REPAIR 1, FIGURE 207 . 2 L 7 2 4F RT A16WE 1999031200186 19990312 00186 NM 1999 3 12 SWAA990370 1 19990224 A 5311 BAC15171470 FRAME BOEING 737 7373H4 1384600 NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED BETWEEN STRINGERS 8L-9L, FS 380 AND 400. REPAIRED PER SRM 53-00-07-2 A ND 51-40-02-0. 2 L 7 2 4F RT A16WE 1999031200187 19990312 00187 NM 1999 3 12 SWAA990371 1 19990224 A 5220 657912920 BLANKET BOEING 737 7373H4 1384600 NM OVERWING DOORS TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT OVERWING EXIT HATCHES INSULATION BLANKETS TORN AND CAUGHT ON FWD AND AFT SIDE LATCH ROLLERS. REPAIRED BLANKETS PER MM. 2 L 7 2 4F RT A16WE 1999031200188 19990312 00188 NM 1999 3 12 SWAA990372 1 19990224 A 5220 WEB BOEING 737 7373H4 1384600 NM BS 798 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CORRODED CREASE WEB, BS 798, RBL 67, WL 208. REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 1999031200189 19990312 00189 NM 1999 3 12 SWAA990373 1 19990224 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 798 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND 2 CRACKED FRAMES, FS 827 AND FS 867 BETWEEN STRINGERS 8L-8R. 2 L 7 2 4F RT A16WE 1999031200190 19990312 00190 NM 1999 3 12 SWAA990374 1 19990224 A 5220 6973977 STOP BOEING 737 7373H4 1384600 NM OVERWING DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED BC2 CHECK, FOUND RT OVERWING EXIT FRAME UPPER AFT STOP PAD CRACKED. REPLACED STOP PAD PER MM. 2 L 7 2 4F RT A16WE 1999031200191 19990312 00191 NM 1999 3 12 SWAA990375 1 19990224 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED CHECK, FOUND NR 2 FRONT FLOOR TRACK LIGHTING TRACK INOP. REPAIRED WIRING AT ROW 2 PER MM. 2 L 7 2 4F RT A16WE 1999031200192 19990312 00192 NM 1999 3 12 SWAA990376 1 19990224 A 2560 61621469 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED CHECK, FOUND R-2 SERVICE DOOR SLIDE LOW ON PRESSURE. REPLACED DOOR SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999031200193 19990312 00193 NM 1999 3 12 SWAA990377 1 19990225 A 2560 61621 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 647SW 27717 FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE NOT STOWED PROPERLY IN CONTAINER. REPOSITIONED SLIDE PROPERLY PER MM. 2 L 7 2 4F RT A16WE 1999031200194 19990312 00194 NE 1999 3 12 SWAA990378 2 19990225 A 7230 BLADE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE DAMAGED A SWAA O OTHER C F.O.D. CR CRUISE 1 SW 07 313SW 23335 723108 AT FL 310, FELT AND HEARD A LOUD THUMP, NOTED CHANGE IN NR 1 ENG N2 AND FUEL FLOW INCREASE. ENG VIBRATION MON ROSE TO P LUS 4. PERFORMED CHECKLIST, RAN ON REDUCED POWER. VIBRATION CONTINUED TO SHUTDOWN AT GATE. INSPECTED AND FOUND ICE DA MAGE TO C1 FAN. REPLACED FAN ASSY PER MM. NO OTHER DAMAGE NOTICED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200195 19990312 00195 NM 1999 3 12 SWAA990379 1 19990225 A 2497 WIRE BOEING 737 7373H4 1384600 NM COCKPIT CHAFED A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 302SW 22942 ON LAND ROLL, SPARKS AND SMOKE IN OVERHEAD PANEL BEHIND FUEL PANEL. SEVERAL LIGHTING CB'S POPPED (RT AND LT INBOARD, NO RMAL POSITION AND LT TURN OFF). FUEL RECALL LIGHT ON MASTER CAUTION ON. FOUND SEVERAL CHAFED WIRES BEHIND GEN DRIVE PA NEL. REPAIRED WIRES, ALL AFFECTED SYSTEMS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 1999031200196 19990312 00196 NM 1999 3 12 SWAA990380 1 19990225 A 3350 100031 SIGN BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 AFTER PARKING AT GATE, MID CABIN OVERHEAD EMERGENCY EXIT SIGN FELL FROM CEILING (HANGING BY ELECTRICAL WIRES). REPOSITI ONED SIGN PER MM. 2 L 7 2 4F A16WE 1999031200197 19990312 00197 NM 1999 3 12 SWAA990381 1 19990224 A 5320 BAC1517 FITTING BOEING 737 7373H4 1384600 NM R1 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED BC2 CHECK, FOUND RI DOOR FRAME UPPER FWD FITTING CRACKED. REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 1999031200198 19990312 00198 NM 1999 3 12 SWAA990382 1 19990224 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 664 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT STA 664, LBL 32. REPAIRED PER SWA RA NR 1-353-2033. 2 L 7 2 4F RT A16WE 1999031200199 19990312 00199 NM 1999 3 12 SWAA990383 1 19990224 A 5220 6553214 BRACKET BOEING 737 7372H4 138448C NM EMER EXIT DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EXIT FWD SIDE CENTER DOOR CASTING ATTACH BRACKET CRACKED. REPLACED BRACKET PER SRM. 2 L 7 2 4F A16WE 1999031200200 19990312 00200 NM 1999 3 12 SWAA990384 1 19990224 A 2560 WINDOW BOEING 737 7372H4 138448C NM AFT SVC DOOR NOT SECURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY SLIDE WINDOW NOT SECURED. SECURED WINDOW PER MM. 2 L 7 2 4F A16WE 1999031200201 19990312 00201 NM 1999 3 12 SWAA990385 1 19990224 A 2560 BOTTLE BOEING 737 7372H4 138448C NM SERVICE DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED CHECK, FOUND R-2 DOOR SLIDE ASSY HAS LOW BOTTLE PRESS. REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999031200202 19990312 00202 NM 1999 3 12 SWAA990386 1 19990226 A 2910 LINE BOEING 737 7372H4 138448C NM NR 1 ENGINE CHAFED A SWAA A UNSCHED LANDING K L FLUID LOSS NO TEST CL CLIMB 1 SW 07 103SW 23109 AIR TURNBACK DUE TO 'A' SYSTEM HYDRAULIC SYSTEM LOSS. FOUND ON NR 1 ENG TWO HYD LINES CHAFED CAUSING HOLE. REPLACED BO TH LINES PER MM. 2 L 7 2 4F A16WE 1999031200203 19990312 00203 NM 1999 3 12 SWAA990387 1 19990226 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING INSPECTION, FOUND SKIN CRACK IN CROWN RT SIDE ABOVE NR 3 WINDOW. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999031200204 19990312 00204 NM 1999 3 12 SWAA990388 1 19990226 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357SW 26594 DURING INSPECTION, FOUND TRACK LIGHTING IN FLOOR BY ROW 14 HAS EXPOSED WIRES. SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 1999031200205 19990312 00205 NM 1999 3 12 SWAA990389 1 19990226 A 7331 8TJ124GGM1 TRANSMITTER BOEING 737 7373H4 1384600 NM NR 2 FUEL FLOW ERRATIC A SWAA K NONE O OTHER CR CRUISE 1 SW 07 387SW 26602 NR 2 FUEL FLOW ERRATIC INDICATOR WILL ROLL BACK AT HIGH POWER SETTINGS. INDICATOR DOES NOT BLANK OR LOOSE POWER, BUT WE NT TO NEARLY ZERO INDICATION. REPLACED FUEL FLOW TRANSMITTER PER MM. 2 L 7 2 4F RT A16WE 1999031200206 19990312 00206 NM 1999 3 12 SWAA990390 1 19990226 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 605SW 27956 FLOOR TRACK LIGHTING COVER MISSING AT ACROSS OVERWING DOOR. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999031200207 19990312 00207 NM 1999 3 12 SWAA990391 1 19990226 A 3350 61621 SLIDE BOEING 737 7375H4 138449D NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 FORWARD ENTRY SLIDE DROPPED OUT OF MOUNT. INSPECTED AND SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999031200208 19990312 00208 NM 1999 3 12 SWAA990392 1 19990226 A 2910 887477 PUMP BOEING 737 7373H4 1384600 NM NR 1 ENGINE LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 399WN 27693 AIR TURNBACK DUE TO LOSS OF SYSTEM 'A' HYD FLUID AT CRUISE, 25 MIN AFTER TAKEOFF. REPLACED 'A' SYSTEM HYD PUMP AND CASE DRAIN FILTER PER MM. 2 L 7 2 4F RT A16WE 1999031200209 19990312 00209 NM 1999 3 12 SWAA990393 1 19990227 A 2781 189929 SWITCH BOEING 737 7373A4 1384585 NM LT LE FLAP INOP A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 678AA 23290 AIR TURNBACK DUE TO NR 2 KRUEGER FLAP AND LEADING ENG LIGHT FLASHING ON PANEL. REPLACED PROXIMITY SWITCH PER MM. 2 L 7 2 4F RT A16WE 1999031200210 19990312 00210 NM 1999 3 12 SWAA990394 1 19990228 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM ROW 1 BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 679AA 23291 DURING OVERNIGHT CHECK, FOUND EMERGENCY TRACK LIGHT BROKEN IN CABIN FLOOR BY SEAT NR 1. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031200211 19990312 00211 NM 1999 3 12 SWAA990395 1 19990228 A 5330 SKIN BOEING 737 7372H4 138448C NM GE CFM56 CFM56* 13802 NE BS 757 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED A2 CHECK, FOUND CRACK INDICATION AT 4 FASTENER HOLES, FS 757 BELOW ST 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F 4 F A16WE E2GL 1999031200212 19990312 00212 NM 1999 3 12 SWAA990396 1 19990228 A 2560 65C16820 GIRT BAR BOEING 737 7373H4 1384600 NM L1 DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR AFT GIRT BAR HOOK NOT SECURED. RESECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 1999031200213 19990312 00213 NM 1999 3 12 SWAA990397 1 19990228 A 2560 INDICATOR BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVACUATION SLIDE PRESS INDICATOR NOT VISIBLE IN WINDOW. REPOSITIONED PRESS IND ICATOR PER MM. 2 L 7 2 4F RT A16WE 1999031200214 19990312 00214 NM 1999 3 12 SWAA990398 1 19990228 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM GALLEY NOT SECURED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED C2 CHECK, FOUND EGRESS LIGHT NOT SECURED AT FWD GALLEY. SECURED EGRESS LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999031200215 19990312 00215 1999 3 12 SWAA990399 4 19990228 A 2565 D31354433 SLIDE BOEING 737 7375H4 138449D NM PAX DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED CHECK, FOUND AFT ENTRY EVACUATION SLIDE INDICATOR IS IN THE RED BAND. REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031200216 19990312 00216 NM 1999 3 12 SWAA990400 1 19990228 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM EMERGENCY EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999031200217 19990312 00217 NM 1999 3 12 SWAA990401 1 19990227 A 5320 FRAME BOEING 737 7373H4 1384600 NM R1 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED C1 CHECK, FOUND A CRACK 3.7 INCH AFT LOWER CORNER OF R1 DOOR FRAME OF FUSELAGE. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 1999031200218 19990312 00218 NM 1999 3 12 SWAA990402 1 19990224 A 5530 6552490 BEAM BOEING 737 7373H4 1384600 NM VERT STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND LEFT VERTICAL STAB TRAILING EDGE BEAM CRACKED 15 FROM BOTTOM OF STAB. REPLACED BEAM SEC TION FROM STA 13.33 TO 141.52 PER SRM. 2 L 7 2 4F RT A16WE 1999031200219 19990312 00219 NM 1999 3 12 SWAA990403 1 19990224 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 500-500A RBL 65, WL 208. REPLACED WEB SECTION PER SR M. 2 L 7 2 4F RT A16WE 1999031200220 19990312 00220 NM 1999 3 12 SWAA990404 1 19990224 A 5311 BAC15171470 FRAME BOEING 737 7373H4 1384600 NM BS 907, 787 ,747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND 3 FRAMES CRACKED BETWEEN STRINGERS 8L-9L AT BS 907, BS 787 AND BS 747. REPAIRED FRAMES PER SWA ER NR 99-0168. 2 L 7 2 4F RT A16WE 1999031200221 19990312 00221 NM 1999 3 12 SWAA990405 1 19990224 A 5311 BAC15171470 FRAME BOEING 737 7373H4 1384600 NM BS 827 ,867, 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND 3 FRAMES CRACKED BETWEEN STRINGERS 8R-9R AT BS 827, BS 867 AND BS 787. REPAIRED FRAMES PER SWA ER NR 99-0168. 2 L 7 2 4F RT A16WE 1999031200222 19990312 00222 NM 1999 3 12 SWAA990406 1 19990224 A 5311 BAC15171470 FRAME BOEING 737 7373H4 1384600 NM BS 440 & 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED BETWEEN STRINGERS 8L-9L AT BS 440, BS 500A. REPAIRED FRAMES PER SWA ER NR 99-0168. 2 L 7 2 4F RT A16WE 1999031200223 19990312 00223 NM 1999 3 12 SWAA990407 1 19990224 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 597 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE AT BS 597 BETWEEN STR 13-14 LEFT. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 1999031200224 19990312 00224 NM 1999 3 12 SWAA990408 1 19990224 A 5312 6516300 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND 2 CRACKS AT BS 178 BULKHEAD WEB, RBL 4.7 AND RBL 6.7, WL 211. REPAIRED BULKHEAD PER SRM . 2 L 7 2 4F RT A16WE 1999031200225 19990312 00225 NM 1999 3 12 SWAA990409 1 19990224 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 6, 21, 29, 36, 40.5, 44 AT WL 208. REPAIRED PER SWA ER NR 99-0158. 2 L 7 2 4F RT A16WE 1999031200226 19990312 00226 NM 1999 3 12 SWAA990410 1 19990224 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND STRINGER 16R CRACKED AT BS 500C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999031200227 19990312 00227 NM 1999 3 12 SWAA990411 1 19990224 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM BS 578, 747, 787 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND 3 STRINGERS DAMAGED AT BS 578 STR 5R, BS 747 ST 9L AND BS 787 STR 7L. REPAIRED STRINGER S PER SRM. 2 L 7 2 4F A16WE 1999031200228 19990312 00228 NM 1999 3 12 SWAA990412 1 19990224 A 5311 BAC15171470 FRAME BOEING 737 7372T4 1384492 NM BS 344 & 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED AT BS 344, LBL 45 AND AT BS 663, STR 2R. REPAIRED FRAMES PER SRM. 2 L 7 2 4F A16WE 1999031200229 19990312 00229 NM 1999 3 12 SWAA990413 1 19990224 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 955 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND A 5 INCH CRACK AT AFT ENTRY DOOR, FWD LOWER CUT OUT. REPAIRED CUT SECTION PER SRM. 2 L 7 2 4F A16WE 1999031200230 19990312 00230 NM 1999 3 12 SWAA990414 1 19990226 A 5311 BAC1517705 FRAME BOEING 737 7372T4 1384492 NM BS 663.75 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME THROUGH X-RAY INSPECTION AT BS 663.75, STR 3L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999031200231 19990312 00231 NM 1999 3 12 SWAA990415 1 19990226 A 5314 6546866 KEEL BEAM BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND RT KEEL BEAM CRACKED ON OUTBOARD HORIZONTAL FLANGE, BS 727 PLUS 12, WL 148.8. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999031200232 19990312 00232 NM 1999 3 12 SWAA990416 1 19990226 A 2560 6943819 BRACKET BOEING 737 7372T4 1384492 NM PAX DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR ESCAPE SLIDE MOUNT BRACKET SPACERS MISSING. REPLACED MOUNT BRACKETS PER_ OHM. 2 L 7 2 4F A16WE 1999031200233 19990312 00233 NM 1999 3 12 SWAA990417 1 19990226 A 5311 6546546 FRAME BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CRACK ON FRAME BS 727A, LBL 71, WL 212. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999031200234 19990312 00234 NM 1999 3 12 SWAA990418 1 19990228 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 500C AROUND TIE DOWNS. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999031200235 19990312 00235 NM 1999 3 12 SWAA990419 1 19990228 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 727D LBL 68 AND RBL 68. REPAIRED BEAM PER SWA RA NR 1-353 -2028. 2 L 7 2 4F RT A16WE 1999031200236 19990312 00236 NM 1999 3 12 SWAA990420 1 19990226 A 5230 FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER AFT CORNER. REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 1999031200237 19990312 00237 NM 1999 3 12 SWAA990421 1 19990228 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND NR 6 SLAT LOWER SKIN CRACKED BETWEEN ACTUATOR STOPS, CRACK LENGTH 1.5 INCH. REPAIRED SLAT PER SWA RA NR 1-357-0646. 2 L 7 2 4F RT A16WE 1999031200238 19990312 00238 NM 1999 3 12 SWAA990422 1 19990228 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 794, RBL 5. REPAIRED PER SWA RA NR1-353-2028. 2 L 7 2 4F RT A16WE 1999031200239 19990312 00239 NM 1999 3 12 SWAA990423 1 19990228 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 661 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BL 0, BS 661. REPAIRED BEAM PER SB 737-57-1210. 2 L 7 2 4F RT A16WE 1999031200240 19990312 00240 NM 1999 3 12 SWAA990424 1 19990227 A 5320 BAC1489286 FRAME BOEING 737 7373A4 1384585 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2D CHECK, FOUND STUB FRAME CRACKED AT UPPER FWD CORNER OF SERVICE DOOR, BS 294.5. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200293 19990312 00293 NE 1999 3 12 TWAA9903401 2 19990305 A 7200 ENGINE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE LEFT FAILED A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 715TW 28483 4930 DURING ETOPS FLIGHT SEGMENT, THE LT ENG OIL PRESSURE DROPPED TO ZERO AND LOW OIL PRESSURE LIGHT CAME ON. SHUT DOWN THE ENG AND MADE UNSCHEDULED LANDING AT SFO. FOUND METAL IN CHIP DETECTOR AND MAIN OIL SCREEN. CHANGED THE ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999031200294 19990312 00294 WP 1999 3 12 TWAA9903402 1 19990226 A 5315 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-226 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND FLOOR SUPPORT AT STA 160 TO 266, RBL 44 TO 54, WAS CORRODED. FABRICATED NEW SUPPORT, TR EATED, PRIMED AND PAINTED PART AND AREA. INSTALLED SUPPORT PER SPM 6-80-01. 2 L 7 2 4F A6WE 1999031200295 19990312 00295 WP 1999 3 12 TWAA9903403 1 19990226 A 5320 CASTING DOUG DC9 DC932 3022066 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND FUSELAGE FORMER CASTING CRACKED AT STA 718, AND SIDE BRACE HOLES CORRODED AT STA 718. R EPLACED CASTING AT STA 718 PER ARA 16061, AND OVERSIZED SIDE BRACE HOLES PER ARA 16063 AND SPM 6-80-01. 2 L 7 2 4F A6WE 1999031200296 19990312 00296 WP 1999 3 12 TWAA9903404 1 19990225 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 160-165 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION BETWEEN MEMBRANE LAYERS AT STA 160 TO 165, RBL 43 TO 53. REMOVED CORROS ION AREA BETWEEN MEMBRANE LAYERS AND FABRICATED ALUMINUM ALLOY REPAIR. PRIMED AND PAINTED AND INSTALLED PER SRM 53-01. 2 L 7 2 4F A6WE 1999031200297 19990312 00297 WP 1999 3 12 TWAA9903405 1 19990225 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND SKIN DAMAGED AND LONGERON 19L CRACKED AT STA 218. REPAIRED SKIN PER SRM 53-04 PAGE 218R . LONGERON REPAIRED PER SPM 6-70-01, PAGE 2. 2 L 7 2 4F A6WE 1999031200298 19990312 00298 WP 1999 3 12 TWAA9903406 1 19990225 A 5320 FORMER DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND FORMER FOOT CRACKED AT STA 965, BETWEEN LONGERON 13, 14, 15 AND 16, LEFT SIDE. REPLACED FORMER FOOT PER MO 72514 AND PER DWG J060119, AND EMLR 69313. 2 L 7 2 4F A6WE 1999031200299 19990312 00299 WP 1999 3 12 TWAA9903407 1 19990228 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 794 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 410EA 47731 FOUND THE OTBD FLANGE OF LONGERON 4L CRACKED .25 INCH WHERE IT ATTACHES TO FRAME AT STA 794. REMOVED AND REPLACED DAMAG ED SECTION OF LONGERON PER SRM 53-02, FIG 18. CHECK-C 2-28-99 STL. 2 L 7 2 4F RT A6WE 1999031200300 19990312 00300 WP 1999 3 12 TWAA9903408 1 19990228 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 794 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 410EA 47731 FOUND THE INBD FLANGE OF LONGERON 5R CRACKED .25 INCH WHERE IT ATTACHES TO FRAME AT STA 794. REPAIRED PER DC9 SRM 53-02 , FIG 18 SHEET 1. CHECK-C 8-12-98 STL. 2 L 7 2 4F RT A6WE 1999031200301 19990312 00301 NM 1999 3 12 HNAA9900031 1 19990219 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 LEFT FORWARD INBOARD SEAT TRACK HAS CORROSION BEYOND LIMITS. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 1999031200302 19990312 00302 NM 1999 3 12 HNAA9900032 1 19990302 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM COCKPIT ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 922HA 094 DURING TRAINING FLIGH, EXPERIENCED SMOKE-LIKE SMELL IN COCKPIT. UNABLE TO DUPLICATE. NO DISCREPANCY FOUND. 2 H 7 2 4T RT A13NM 1999031200303 19990312 00303 NM 1999 3 12 HNAA9900033 1 19990303 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 984HA 377 FIRST AND THIRD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY IN 3351-PS3. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999031200304 19990312 00304 NM 1999 3 12 HNAA9900034 1 19990304 A 2611 302313 DETECTOR DHAV DHC8 DHC8102 2809003 NM NR 2 INTERMITTANT A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 833MA 343 SMOKE WARNING ILLUMINATED IN FLIGHT. NO APPARENT CAUSE. COULD NOT DUPLICATE. REPLACED NR 2 (FORWARD) SMOKE DETECTOR A S A PRECAUTION. 2 H 7 2 4T RT A13NM 1999031200305 19990312 00305 NM 1999 3 12 AT9900148R1 1 19990211 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 279, 294, 312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND SEVERAL FLOORBEAM SUPPORT CORRODED. THE STATIONS ARE AS FOLLOW; BS 279 LBL 12-27.5L, BS 294.5 LBL 32L-50.5R, BS 312 LBL 50-16RBL, BS 328 LBL 56-56 RBL. MECHANICALLY REMOVED CORROSION AND REMOVE D FLOOR SECTION, FABRICATED REPAIR, TREATED, PRIMED, AND INSTALLED IAW B737 SRM 51-10-2, 53-10-9, 53-10-1, 53-10-9 FIG 5 , AND MM 51-21-31. FLOORBEAM P/N OFF 60-893 (2EA), FLOORBEAM P/N OFF 60-8004. 2 L 7 2 4F RT A16WE 1999031200306 19990312 00306 NM 1999 3 12 AT9900165 1 19990209 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 947-967 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE CABIN FLOOR SUPPORT AT BS 947-967 RBL 46 CORRODED. REMOVED AND FABRICA TED REPAIR SUPPORT, DRILLED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-4, 51-30-2, AND 51-10-6. 2 L 7 2 4F RT A16WE 1999031200307 19990312 00307 NM 1999 3 12 AT9900166 1 19990224 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 987-1006 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CABIN FLOOR ASSEMBLY BS 987-1006 LBL10-20 CORRODED AND EXISTING DOUBLE DRIL LED HOLES. FABRICATED THREE FLOOR SUPPORT, ALODINE, PRIMED, AND INSTALLED IAW B737 SRM 51-40-3, 51-10-2, AND MM 51-21-3 1. 2 L 7 2 4F RT A16WE 1999031200308 19990312 00308 WP 1999 3 12 AT9900168 1 19990209 A 5347 S295597812000 FLOOR TRACK DOUG DC9 DC932 3022066 WP BS 307-503 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CARGO FLOOR TRACK AT BS 307-503 CORRODED. MECHANICALLY REMOVED CORROSION, REMOVED, REPLACED AND FABRICATED NEW TRACK SECTION, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-10- 4, 53-05 FIG 4C, AND 51-10-3. 2 L 7 2 4F A6WE 1999031200309 19990312 00309 WP 1999 3 12 AT9900169 1 19990211 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND SIDE WALL TRIM STRAP AT BS 427 RIGHT SIDE CORRODED. MECHANICALLY REMOVED C ORROSION, FABRICATED STRAP, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1999031200310 19990312 00310 WP 1999 3 12 AT9900170 1 19990218 A 5330 PANEL DOUG DC9 DC932 3022066 WP BS 897-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND FLOOR PANEL AT BS 897-965 LEFT SIDE CORRODED AROUND FASTENER HOLES. REMOVE D AND REPLACED FASTENERS, CLEANED CORROSION, FABRICATED REPAIR FLOOR PANEL, ALODINE, PRIMED AND INSTALLED IAW DC9 SRM 51 -10-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999031200311 19990312 00311 NM 1999 3 12 AT9900171 1 19990220 A 5320 ANGLE BOEING 737 7372L9 1384497 NM BS 310-360 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND L ANGLE AT BS 310-360 LBL 62.5 CORRODED AROUND FASTENER HOLES. REMOVED COR ROSION, CUT OUT DAMAGE SECTION, FABRICATED REPAIR ANGLE, AND INSTALLED IAW B737 SRM 51-10-2, 51-30-2, 51-40-3, 53-10-1, 51-10-6, AND MM 51-21-31. 2 L 7 2 4F RT A16WE 1999031200312 19990312 00312 NM 1999 3 12 K3HA990020 1 19990228 A 3350 079123 LENS BOEING 727 727225 1384077 NM ROW 33 MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 FLOOR EMERGENCY LIGHT MISSING (REAR). REPLACED EMERGENCY PATH RED LENS AT ROW 33 IAW GMM 33-50. 2 L 7 3 4F A3WE 1999031200313 19990312 00313 EA 1999 3 12 JBXA9900073 1 19990305 A 3000 HEAT CNDAIR CL600 CL6002B19 EA RT AOA VANE FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 579ML 7277 FLIGHT 94 RDU, TO IND HAD RIGHT AOA VANE HEAT FAILED. AIRCRAFT RETURNED TO RDU MAINTENANCE CHECKED RT AOA WAS HEATING W ITH FAULT MESSAGE DISPLAYED. PULLED AND RESET ADS HEATER NR 2 C/B. RESET CLEARED FAULT PERFORMED ADS CONTROLLER TEST T ESTED GOOD IAW CL-65 MM 30-31-15. 2 L 7 2 4F RT A21EA 1999031200314 19990312 00314 NM 1999 3 12 AWXA9900069 1 19990303 A 2810 PANEL BOEING 737 7373S3 1384711 NM RT WING LEAKING A AWXA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 28 313AW 23712 EMERGENCY LANDING, INFLIGHT RIGHT WING FUEL LEAK. NON REV PILOT REPORTED FLUID LEAK ON RT WING UNDETERMINED QTY, TYPE, AND SOURCE. CAPTAIN INITIATED AN EMERGENCY LANDING. REMOVED AND REPLACED UPPER PANEL ON WING JUST AFT OF PYLON, LEAK CK GOOD, NO LEAKS. 2 L 7 2 4F RT A16WE 1999031200315 19990312 00315 EU 1999 3 12 AWXA9900070 1 19990302 A 3240 NAS161216 O RING AIRBUS 320 A320231 3930325 EU RT MLG WW CUT A AWXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 28 626AW 65 EMERGENCY DECLARED, LOSS OF GREEN HYDRAULIC QUANTITY. ON FINAL, GREEN HYDRAULIC QUANTITY DECREASING. UNEVENTFUL LANDIN G. LEAK FROM BRAKE SERVO VALVE MANIFOLD FILTER. FOUND O-RING PINCHED. RIGHT WHEEL WELL. REPLACED O-RING PACKING. LE AK CHECK AND OPS OK. 2 L 7 2 4F RT A28NM 1999031200316 19990312 00316 CE 1999 3 12 PNSA990107 1 19990114 A 3260 BULB CESSNA 441 441 2076020 CE LT MLG FAILED A PNSA L ABORTED APPROACH P NO WARNING INDICATION DE DESCENT 1 AL 03 544AL 4410120 LEFT MAIN WOULD NOT INDICATE DOWN AND LOCKED. LANDING GEAR APPEARED TO BE DOWN AND LOCKED. AN UNEVENTFUL LANDING WAS M ADE. FOUND BURNED OUT BULB IN INDICATOR, REPLACED BULB. OPERATIONAL CHECK FOUND OK. 1 L 7 2 3T RT A28CE 1999031200317 19990312 00317 SO 1999 3 12 PNSA990203 1 19990223 A 7721 41506003 INDICATOR PIPER PA31 PA31350 7103110 SO RT ENGINE INOP A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 3588Z 1337 318052130 RT CHT INDICATOR WAS OBSERVED INOPERATIVE DURING TAXI TO RUNWAY. RETURNED TO BLOCKS. REPLACED CHT INDICATOR. OPERATIO NAL CHECK OK. 1 L 7 2 3O A20SO 1999031200318 19990312 00318 SW 1999 3 12 PNSA990204 1 19990219 A 6120 GOVERNOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE OUT OF ADJUST A PNSA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 41NE AC741B P44744 AT ROTATION LT ENGINE RPM DROPPED 5 PERCENT. FLIGHT CREW REPORTED THAT POWER LEVER WAS NOT RESPONDING NORMALLY AND SPEE D COULD NOT BE RETURNED TO 100 PERCENT. FLIGHT CREW ELECTED TO BURN FUEL LOAD DOWN TO LANDING WEIGHT AND THEN MADE AN U NEVENTFUL LANDING. INVESTIGATION REVEALED THAT THE FUEL UNDER SPEED GOVERNORS WERE NOT WITHIN THEIR NORMAL OPERATING L IMITS. GOVERNORS WERE READJUSTED. SUBSEQUENT GROUND RUNS AND FLIGHT CHECK WERE NORMAL. 2 L 7 2 4T 4 T RT A8SW E4WE 1999031200319 19990312 00319 WP 1999 3 12 CALA9900214 1 19990305 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQD SERVICE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16887 49116 THE LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE NLG STRUT FLAT. A COMPLETE STRUT SERVICE WAS PERFORMED IAW MM 32-21-02. THE NOSE GEAR WAS CYCL ED AND LANDING GEAR HANDLE OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999031200320 19990312 00320 EU 1999 3 12 QXEA9900187 1 19990111 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305-8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE THREE AREAS OF LIGHT TO MODERATE CORROSION IN CHANNEL OF RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 7305 AN D 8305. REPAIRED IAW MM 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6. 2 L 7 2 4F RT A20EU 1999031200321 19990312 00321 EU 1999 3 12 QXEA9900188 1 19990111 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305-9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE THREE AREAS WITH LIGHT PITTING CORROSION INSIDE CHANNEL OF RIGHT INBOARD SEAT TRACK BETWEEN FRAME 8305 A ND 9305. REPAIRED IAW MM 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6. 2 L 7 2 4F RT A20EU 1999031200322 19990312 00322 EU 1999 3 12 QXEA9900189 1 19990111 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE IS A SMALL AREA WITH PITTING CORROSION IN RIGHT INBOARD SEAT TRACK, JUST AFT OF FRAME 9305A. REPAIRED IAW M M 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6. 2 L 7 2 4F RT A20EU 1999031200323 19990312 00323 EU 1999 3 12 QXEA9900190 1 19990103 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE TWO AREAS OF PITTING CORROSION ON INBOARD FLOOR SUPPORT FLANGE OF THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 10966 AND 11905. REPAIRED IAW MM 53-40-01, PAGE 201-202, PARAGRAPH B6, STEPS 1-6. 2 L 7 2 4F RT A20EU 1999031200324 19990312 00324 EU 1999 3 12 QXEA9900191 1 19990103 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE THREE AREAS WITH PITTING CORROSION INSIDE CHANNEL OF RIGHT OUTBOARD SEAT TRACK, BETWEEN FRAMES 10966 AND 12875. REPAIRED IAW SRM 51-10-4, PAGES 8 AND 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999031200326 19990312 00326 EU 1999 3 12 QXEA9900193 1 19990113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10790 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE IS A CIRCULAR GROOVE WORN INTO INBOARD FLOOR SUPPORT FLANGE OF THE LEFT INBOARD SEAT TRACK, JUST FORWARD OF FRAME 10790. REPAIRED IAW HORIZON AIR EA 4-53-675. 2 L 7 2 4F RT A20EU 1999031200327 19990312 00327 EU 1999 3 12 QXEA9900194 1 19990103 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12875 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE THREE AREAS WITH LIGHT GOUGES IN CHANNEL LIP ON THE LEFT OUTBOARD SEAT TRACK, BETWEEN FRAME 12875 AND 13 815. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999031200328 19990312 00328 EU 1999 3 12 QXEA9900195 1 19990113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE IS A GOUGE IN THE LEFT INBOARD SEAT TRACK JUST FORWARD OF FRAME 14285. REPAIRED IAW HORIZON AIR EA 4-53-564 . 2 L 7 2 4F RT A20EU 1999031200331 19990312 00331 EU 1999 3 12 QXEA9900198 1 19990113 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - SERVICE EMERGENCY DOOR APERTURE LOWER FORWARD CORNER REQUIRES DOUBLER MOD. COMPLIED WITH HORIZON AIR EA 4-53-593. 2 L 7 2 4F RT A20EU 1999031200332 19990312 00332 EU 1999 3 12 QXEA9900199 1 19990102 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - CRACK APPROXIMATELY 1.2 LONG ON LEFT SIDE FORWARD OVERWING EMERGENCY DOOR APERTURE AT FORWARD LOWER CORNER. REPAI RED IAW HORIZON AIR EA 4-53-633. 2 L 7 2 4F RT A20EU 1999031200334 19990312 00334 EU 1999 3 12 QXEA9900201 1 19990115 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM X AT BL1050R DOES NOT CONFORM TO SRM REPAIR, SRM 53-02-18, FIGURE 3. REPAIR ED IAW FOKKER SRM 53-02-18, FIGURE 3 AND HORIZON AIR EA 4-53-677. 2 L 7 2 4F RT A20EU 1999031200335 19990312 00335 EU 1999 3 12 QXEA9900202 1 19990115 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM XI BL425L DOES NOT CONFORM TO SRM REPAIR SRM 53-02-18, FIGURE 3. REPAIRED I AW FOKKER SRM 53-02-18, FIGURE 3, SRM 51-30-02 AND HORIZON AIR EA 4-53-677. 2 L 7 2 4F RT A20EU 1999031200336 19990312 00336 EU 1999 3 12 QXEA9900203 1 19990115 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM XII OUTBOARD OF BL425R DOES NOT CONFORM TO SRM REPAIR, SRM 53-02-18, FIGURE 3. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 3, SRM 51-30-02 AND HORIZON AIR EA 4-53-677. 2 L 7 2 4F RT A20EU 1999031200337 19990312 00337 EU 1999 3 12 QXEA9900204 1 19990115 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REPAIR ON REAR PRESSURE BULKHEAD BEAM XI BETWEEN BL1050R AND BL425R DOES NOT CONFORM TO SRM REPAIR, SRM 53-02-18, FIGURE 3. REPAIRED IAW FOKKER SRM 51-02-18, FIGURE 3, SRM 51-30-02 AND HORIZON AIR EA 4-53-677. 2 L 7 2 4F RT A20EU 1999031200344 19990312 00344 EU 1999 3 12 QXEA9900211 1 19990106 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - PASSENGER DOOR APERTURE DENTED AND CHAFED IN AREA ADJACENT TO THE CURVED LEVER AND FRICTION DISC ASSEMBLY WHEN THE DOOR IS IN THE OPEN POSITION. REPAIRED IAW HORIZON AIR EA 4-53-656. 2 L 7 2 4F RT A20EU 1999031200345 19990312 00345 EU 1999 3 12 QXEA9900212 1 19990103 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - CRACKED CLIP AT FRAME 16060 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-10, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200346 19990312 00346 EU 1999 3 12 QXEA9900213 1 19990103 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - CRACKED CLIP AT FRAME 16060 AND STRINGER 49. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200359 19990312 00359 EU 1999 3 12 QXEA9900226 1 19990103 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200360 19990312 00360 EU 1999 3 12 QXEA9900227 1 19990102 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 28A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PA GE 13, PARAGRAPH 7A, STEPS 1-5. 2 L 7 2 4F RT A20EU 1999031200366 19990312 00366 EU 1999 3 12 QXEA9900233 1 19990103 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 29A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200370 19990312 00370 NM 1999 3 12 99FDEA00083 1 19990304 A 3230 VALVE BOEING 727 727225 1384077 NM MAIN GEAR INOP A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 467FE 21449 GEAR HANDLE PLACED IN OFF POSITION, NOSE GEAR DOOR LIGHT AND MAIN GEAR DOOR LIGHT ILLUM. *S/D* REMOVED AND REPLACED LA NDING GEAR ASSY UNIT PER MM 32-09-221. REMOVED AND REPLACED MLG SEL VALVE PER 32-31-03-4. AC OK TO CONTINUE. 2 L 7 3 4F A3WE 1999031200371 19990312 00371 NM 1999 3 12 99FDEA00084 1 19990305 A 2782 651781823 ACTUATOR BOEING 727 727227 1384078 NM NR 2 LE SLAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 491FE 21529 DURING FLAP RETRACT, NR 2 SLAT ON LEFT WING WOULD NOT RETRACT. ACCOMPLISH RED TAB PROC, BUT NR 2 SLAT WOULD NOT RETRACT . *S/D* REMOVED AND REPLACED NR 2 LEAD EDGE SLAT ACTUATOR PER MM 27-81-032-4. LEAK AND OPERATION CHECK NORMAL. 2 L 7 3 4F A3WE 1999031200372 19990312 00372 NM 1999 3 12 99FDEA00085 1 19990305 A 5320 STRAP BOEING 727 72722C 138400F NM BS 440 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 BS 440 BONDED TEAR STRAP IS DELAMINATED FROM STR 4R TO STR 7R. 2 L 7 3 4F A3WE 1999031200373 19990312 00373 NM 1999 3 12 99FDEA00086 1 19990305 A 7110 COWL BOEING 727 72725 1384006 NM NR 1 ENGINE MISSING A FDEA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 508FE 18279 99-0061 - PRESSURE RELIEF PNL MISSING NR 1 ENG UPPER COWL. RAN NR 1 ENG, NO BLD AIR LEAKS NOTED. REMOVED UPPER COWL PE R 727 MM 71-10-011-4 AND ROUTED TO SHEET METAL SHOP FOR REPAIR. INSTALL VENT PNL PER BOEING 727 DRW 65-23772. 2 L 7 3 4F A3WE 1999031200374 19990312 00374 WP 1999 3 12 ABXA9900158 1 19990119 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 822 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING LEADING EDGE UPPER RIB AT STATION XFS 822 CRACKED AT FASTENER END. REPAIRED IAW DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1999031200375 19990312 00375 WP 1999 3 12 ABXA9900159 1 19990118 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 772 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING LEADING EDGE RIB CRACKED AT STATION ATXFS772. REPAIRED IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1999031200376 19990312 00376 WP 1999 3 12 ABXA9900160 1 19990118 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 736 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 736. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056. 2 L 7 4 4F 4A25 1999031200377 19990312 00377 WP 1999 3 12 ABXA9900161 1 19990118 A 5230 5645357 SKIN DOUG DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 LOWER CARGO C2 DOOR INTERIOR SKIN CRACKED AT LOWER FORWARD CORNER. REPAIRED IAW DC8 SRM 52-4-2 AND 51-1-20. 2 L 7 4 4F 4A25 1999031200378 19990312 00378 WP 1999 3 12 ABXA9900162 1 19990117 A 5730 9751896402 SKIN DOUG DOUG DC8 DC863 302198A WP WS 761 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825AX 46115 RIGHT WING LEADING EDGE HAD EXFOLIATED CORROSION AT INBOARD FORWARD LEADING EDGE, STATION XW 761. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999031200379 19990312 00379 WP 1999 3 12 ABXA9900163 1 19990223 A 5320 99220421 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 294 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FLOOR STRUT TO FUSELAGE FRAME ATTACH FITTING CRACKED AT STATION 294, LONGERON 24 LEFT. REPLACED A TTACH FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999031200380 19990312 00380 WP 1999 3 12 ABXA9900164 1 19990223 A 5320 995823869 SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT LONGERON 16 LEFT, STATION 980. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999031200381 19990312 00381 WP 1999 3 12 ABXA9900165 1 19990217 A 5320 99220431 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 389 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FRAME FITTING AT STATION 389 BETWEEN LONGERONS 22 LEFT AND 23 LEFT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999031200382 19990312 00382 WP 1999 3 12 ABXA9900166 1 19990217 A 5712 RIB DOUG DOUG DC9 DC933F 302207A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED, OUTBOARD OF NR 11 SLAT TRACK. REPLACED RIB IAW DC9 SRM 53-30 -2. 2 L 7 2 4F A6WE 1999031200383 19990312 00383 WP 1999 3 12 ABXA9900167 1 19990217 A 5313 59114279 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 945. REPLACED SECTION OF LONGERON IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 1999031200384 19990312 00384 NM 1999 3 12 P5CA9900212 1 19990225 A 5730 SKIN BOEING 747 747124 1384874 NM WS 614 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION LEFT HAD WING SURFACE AT WS 614 BETWEEN MID TO REAR SPAR AREA. CORROSION REMOVED AND TREATED PER SRM 57-30-01, 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031200385 19990312 00385 NM 1999 3 12 P5CA9900213 1 19990225 A 5730 SKIN BOEING 747 747124 1384874 NM WS 807 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON UPPER SURFACE AT FRONT SPAR WS 807 WBL 584L. CORROSION REMOVED AND TREATED PER SRM 57-30-01, 51-10-01, 51-10-02 AND 57-30-01. 2 L 7 4 4F A20WE 1999031200386 19990312 00386 NM 1999 3 12 P5CA9900214 1 19990225 A 5400 FAIRING BOEING 747 747124 1384874 NM NR 3 PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 3 PYLON V FAIRING HAS 2 AREAS OF DISBONDING. REPAIRED DELAMINATION PER SRM 51-10-02, 51-10-01 AND 57-30-01. 2 L 7 4 4F A20WE 1999031200387 19990312 00387 NM 1999 3 12 P5CA9900215 1 19990225 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 789 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK BODY STATION 789 RBL33 FLOOR SUPPORT CRACKED. SUPPORT REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031200388 19990312 00388 NM 1999 3 12 P5CA9900216 1 19990225 A 5320 SKIN BOEING 747 747124 1384874 NM BS 2658 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 EMP LT SIDE BUTT JOINT SKIN SURFACE CORROSION AT BS2658. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031200389 19990312 00389 NM 1999 3 12 P5CA9900217 1 19990225 A 4900 SKIN BOEING 747 747124 1384874 NM APU INLET DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 EMP APU AIR INLET DOOR CUT OUT FWD EDGE SKIN HAS SURFACE CORROSION. REPAIRED CORROSION PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031200390 19990312 00390 NM 1999 3 12 P5CA9900218 1 19990225 A 5247 HINGE BOEING 747 747124 1384874 NM APU DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 RIGHT APU DOOR HINGE MOUNT BOLT AREA SKIN SURFACE CORROSION. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031200391 19990312 00391 NM 1999 3 12 P5CA9900219 1 19990225 A 5313 STRINGER BOEING 747 747124 1384874 NM BS 2360 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK BS 2360 STR 14L STRINGER END FOUND CRACKED. MINOR CRACK TRIMMED OFF PER SRM 53-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031200392 19990312 00392 NM 1999 3 12 P5CA9900220 1 19990225 A 5522 SKIN BOEING 747 747124 1384874 NM LT ELEVATOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEFT INBOARD ELEVATOR TRAILING EDGE HAS DAMAGED AND CRACKED AREA. FIBERGLASS WET LAYUP REPAIR PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999031200393 19990312 00393 NM 1999 3 12 P5CA9900221 1 19990227 A 5753 FAIRING BOEING 747 747124 1384874 NM NR 1 FLAP TRACK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 1 FLAP TRACK MOVABLE CANOE FAIRING HAS SEVERAL AREAS OF DAMAGE. REPAIRED DAMAGE PER SRM 51-40-15 FIG 7. 2 L 7 4 4F A20WE 1999031200394 19990312 00394 NM 1999 3 12 P5CA9900222 1 19990227 A 5330 SKIN BOEING 747 747124 1384874 NM BS 2658-2742 LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 EMP TAIL CONE LT SKIN ATTACHED RIVETS FOUND LOOSE. TOTAL 140 FROM BS 2658 TO 2742 LEFT SIDE. RIVETS REPAIRED PER SRM 5 1-30-02. 2 L 7 4 4F A20WE 1999031200395 19990312 00395 NM 1999 3 12 P5CA9900223 1 19990225 A 5320 WALK WAY BOEING 747 747124 1384874 NM BS 1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 AFT CARGO RIGHT SIDE STA 1820 WALK WAY PANEL FOUND CORROSION. REMOVED CORROSION AND REPROTECTED PER SRM 51-20-01 AND 51 -10-02. 2 L 7 4 4F A20WE 1999031200396 19990312 00396 NM 1999 3 12 P5CA9900224 1 19990225 A 5320 WEB BOEING 747 747124 1384874 NM BS 660-680 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FWD CARGO STA 660-680 LBL30 FLOOR AREA WEB FOUND CRACKED. FLOOR WEB REPAIRED AT STA 660-680 LBL 30 AS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1999031200397 19990312 00397 NM 1999 3 12 P5CA9900225 1 19990226 A 7110 COWL BOEING 747 747124 1384874 NM NR 3 ENGING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 3 ENGINE TRANSLATING COWL INNER SKIN IS CRACKED AT T/E AT 7 TO 8 O'CLOCK POSITION. SLIGHTLY CRACKED SMOOTHED OUT PER SRM 51-10-02 AND TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031200398 19990312 00398 NM 1999 3 12 P5CA9900226 1 19990225 A 5753 FAIRING BOEING 747 747124 1384874 NM NR 6 FLAP TRACK DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 RIGHT WING NR 6 CANOE FAIRING FOUND DELAMINATION AT TWO LOCATIONS. REPAIRED DEFECTED AREA WITH FIBERGLASS LAYUP AT 150 DEGREES F CURED. REPAIRED PER SRM 51-40-15 FIG 7. 2 L 7 4 4F A20WE 1999031200399 19990312 00399 NM 1999 3 12 P5CA9900227 1 19990226 A 5320 ANGLE BOEING 747 747124 1384874 NM BS 1283 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON RIGHT WING WHEEL WELL BS 1283 RBL90 APPROX CEILING ANGLE END PLATE. REMOVED CORROSION AND TR EATED PER SRM 51-10-01 AND 51-10-02 WITHIN LIMITS. 2 L 7 4 4F A20WE 1999031200400 19990312 00400 NM 1999 3 12 P5CA9900228 1 19990225 A 5730 SKIN BOEING 747 747124 1384874 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON RIGHT WING UPPER SURFACE AT WS440, 443, 586, 947, 992, 1026, 1480, 1482, 1512, 1513, 1519 AND 1528. CORROSION REMOVED PER SRM 51-10-01 AND BLENDED OUT WITHIN SRM LIMITS PER 57-30-01. TREATED AREAS PER SRM 51-10- 02. 2 L 7 4 4F A20WE 1999031200401 19990312 00401 NM 1999 3 12 P5CA9900229 1 19990304 A 3350 51356B37 BATTERY PACK BOEING 747 747249F 1384849 NM CABIN DISCHARGED A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 920FT 22237 DURING COCKPIT CHECK, FOUND UPPER DECK EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED UPPER DECK BATTERY PACK PER MM 33-51-00. 2 L 7 4 4F A20WE 1999031200402 19990312 00402 WP 1999 3 12 RRXA99130 1 19990304 A 7720 CA11503 MANIFOLD DOUG DC8 DC873F 302199F WP NR 1 ENGINE EGT FAILED A RRXA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 15 961R 46133 CLIMBING THROUGH FL350, NR 1 EGT GAUGE INTERMITTENTLY AND RAPIDLY OSCILLATED SEVERAL TIMES PLUS/MINUS 400 DEG FROM APPRO XIMATELY 760DEG AVERAGE. THIS RESULTED IN A PRECAUTIONARY SHUTDOWN OF THE NR 1 ENGINE. AFTER SHUTDOWN, INTERMITTENTLY WENT FULL SCALE DEFLECTION BOTH HIGH AND LOW, 2 TIMES, THEN RETURNED TO 0 DEG. NO OTHER ABNORMALITIES NOTED. REMOVED A ND REPLACED RT EGT MANIFOLD IAW DC8 MM CH 77-20, OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 1999031200439 19990312 00439 WP 1999 3 12 TWAA9903501 1 19990306 A 4920 38420723 TURBINE DOUG DC9 DC983 3022083 WP APU FAILED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9405T 53141 THE APU SEIZED PRIOR TO DISPATCH. FOUND APU LOOSE IN AIRCRAFT DUE TO A FAILURE AT THE APU AIR BOX TO APU MOUNT. SOME T URBINE SECTION PIECES WERE EXPELLED THROUGH THE EXHAUST PIPE AND FOUND ON THE RAMP. REPLACED THE APU. CHECK-C 11-11-98 . *S/D* THE APU FAILURE WAS A TURBINE WHEEL SEPARATION DUE TO A HALFNIUM INCLUSION. THE SAME TYPE FAILURE OCCURRED NI NE TIMES IN 1998. 2 L 7 2 4F RT A6WE 1999031200440 19990312 00440 WP 1999 3 12 TWAA9903502 1 19990307 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP ROW 23 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9616G 53563 FOUND EGRESS LIGHTS INOPERATIVE AT SEAT ROWS 30 TO 32 AND AT ROW 23. RELAMPED AT ROW 23, AND RESECURED WIRING AT ROWS 3 0 TO 32. 2 L 7 2 4F RT A6WE 1999031200441 19990312 00441 NM 1999 3 12 AT9900172 1 19990208 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 947 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CABIN FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE OF AFT CARGO C OMPARTMENT CABIN CLIPNUTS AT BS 947 FROM LBL 24 TO RBL 36 WITH HEAVY CORROSION AT RBL 14. REMOVED ALL STRUCTURE ASSOCIA TED WITH REPAIR AT BS 947 LBL 31 TO RBL 50 AND CUTOUT DEFECTIVE T CAP. FABRICATED REPAIR PARTS, INSTALLED AND REINSTALL ED ALL PREVIOUS PARTS IAW B737 SRM 53-10-9, 51-30-2, AND RES NR 99384. 2 L 7 2 4F RT A16WE 1999031200442 19990312 00442 NM 1999 3 12 AT9900173 1 19990307 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 383 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTS AT BS 383L STR 19 OUT OF LIMITS. REPAIRED DENTED AREA USING C/R 320 0 SERIES BUTTON HEAD RIVET. INSTALLED WET WITH P/R 1422 SEALANT AS A PERMANENT REPAIR IAW RES NR 99553. 2 L 7 2 4F RT A16WE 1999031200443 19990312 00443 NM 1999 3 12 AT9900174 1 19990307 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 280 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTS OUT OF LIMITS AT BS 280L STR 19 TO 20. DRILLED DENT AND REPAIRED BY INSTALLING A C/R 3200 SERIES BUTTON HEAD RIVET IAW RES NR 99554. 2 L 7 2 4F RT A16WE 1999031200444 19990312 00444 NM 1999 3 12 AT9900175 1 19990225 A 5347 BAC1520841 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 559-727 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND SEAT TRACK SCRATCHED AND CORRODED AT BS 559 TO 727. REMOVED AND REPLACED A 16 FT 3.75 SECTION OF SEAT TRACK IAW B737 SRM 53-10-5 FIG 1 AND 51-30-2. 2 L 7 2 4F RT A16WE 1999031200445 19990312 00445 NM 1999 3 12 AT9900176 1 19990209 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 1006-1040 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CABIN FLOOR SUPPORTS AT BS 1006 TO 1040 LBL 18-28 CORRODED. REMOVED TWO S TRAPS AND TWO INTERCOSTALS. FABRICATED STRAPS, WEB REPAIR AND INSTALLED IAW B737 SRM 51-40-2, AND 51-40-3. 2 L 7 2 4F RT A16WE 1999031200446 19990312 00446 NM 1999 3 12 AT9900177 1 19990209 A 5320 1A454011 WEB BOEING 737 7372L9 1384497 NM BS 1016 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT AFT FLOOR WEB BETWEEN BS 1016 LBL 0-40 AND AFT PRESSURE BULKHEAD ALONG FLOORBEAM CORRODED AND WITH BLUE WATER STAINS ALONG LOWER EDGES. REMOVED CORROSION, FABRICATED ANGLE, T CAP, TREA TED, PRIMED, AND INSTALLED IAW B737 SRM 51-10-6, 53-10-1, 51-10-2, 51-40-3, 51-10-6, 51-30-2, AND 51-20-11. 2 L 7 2 4F RT A16WE 1999031200447 19990312 00447 SO 1999 3 12 RAAA99E4003 1 19990302 A 3350 873100212 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 RT AFT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY DUE FAILED. 2 L 7 4 4T 4A22 1999031200448 19990312 00448 SO 1999 3 12 RAAA99E4004 1 19990302 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO LT EMER EXIT FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 LT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT ASSEMBLY DUE FAILED. 2 L 7 4 4T 4A22 1999031200449 19990312 00449 WP 1999 3 12 CALA9900215 1 19990307 A 3260 SENSOR DOUG DC9 DC982 3022082 WP NLG INOP A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 809NY 49263 THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHE RE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR AT FAULT. THE NOSE GEAR DOWNL OCK PROXIMITY SENSOR WAS REMOVED AND REPLACED IAW MM 32-60-05. A NOSE GEAR SWING WAS PERFORMED AND ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F A6WE 1999031200450 19990312 00450 NM 1999 3 12 CALA9900216 1 19990304 A 5320 ANGLE BOEING 757 757224 1384958 NM BS 1060 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND A 1 INCH CRACK IN TWO RT MLG CUTOUT FORWARD SEAL RETAINER SUPPORT ANGLES AT STA 1060. TWO NEW ANGLES W ERE INSTALLED IAW BOEING DRAWING NR 149N7550. 2 L 7 2 4F RT A2NM 1999031200451 19990312 00451 WP 1999 3 12 CALA9900217 1 19990304 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERIOR BEAM NR 2 FLANGE AFT END. REPAIRED BEAM IAW SRM 5 2-05, FIGURE 31, SHEET 3. 2 L 7 2 4F A6WE 1999031200452 19990312 00452 WP 1999 3 12 CALA9900218 1 19990304 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17557 47424 INSPECTION FOUND A 2 INCH CRACK AND SEVERAL LOOSE RIVETS IN RT SIDE OF RUDDER UPPER SKIN. THE EFFECTED AREA OF SKIN WAS REMOVED AND A NEW SECTION OF SKIN WAS INSTALLED IAW SRM 55-03-00, FIGURE 12, PAGE 19. 2 L 7 2 4F A6WE 1999031200453 19990312 00453 NM 1999 3 12 CALA9900219 1 19990304 A 5320 ANGLE BOEING 757 757224 1384958 NM CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND THE FORWARD HOLD DOOR THRESHOLD ATTACHMENT ANGLE CORRODED. THE ANGLE WAS REPLACED IAW MM 53-20-00. 2 L 7 2 4F RT A2NM 1999031200454 19990312 00454 WP 1999 3 12 CALA9900220 1 19990304 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1117-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED AROUND SCREW HOLES FROM GALLEY NR 3 TO GALLEY NR 4 AREA, STA 1117 TO 11 74. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999031200455 19990312 00455 WP 1999 3 12 CALA9900221 1 19990304 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 1.5 INCH CRACK IN MID CARGO BIN DOOR PAN. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTAL LED IAW SRM 52-05, FIGURE 26A. 2 L 7 2 4F A6WE 1999031200456 19990312 00456 NM 1999 3 12 CALA9900222 1 19990304 A 3397 WIRE BOEING 737 7373T0 1384582 NM ROW 25 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND ROW 25 EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN/PULLED FROM SPLICE. THE SPL ICE WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY LIGHTING CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999031200457 19990312 00457 WP 1999 3 12 CALA9900223 1 19990304 A 3350 252005 FUSE FUSEUNLIMIT DOUG DC9 DC982 3022082 WP MID PWR SUPP BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 35836 49441 INSPECTION FOUND MIDDLE SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND MOST OUTBOARD FU SE OF MIDDLE POWER SUPPLY PACK BLOWN. THE FUSE WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTING WAS RESTORED. 2 L 7 2 4F A6WE 1999031200458 19990312 00458 WP 1999 3 12 CALA9900224 1 19990305 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237 ABOVE CUSP. A NEW SKIN SECTION WAS INSTALLED BETWEEN LONGERON 15L AND 18L IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1999031200459 19990312 00459 WP 1999 3 12 CALA9900225 1 19990304 A 2621 BRACKET DOUG DC10 DC1030 3023501 WP FIRE BOTTLE FAILED A CALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 09 EIDLA 46958 ON TAKEOFF, CONTROLS FELT LIKE HALF CONTROL ON YOKE WITH AILERONS AND STABILIZER. FULL FORWARD AND AFT TO CONTROL ACFT. RETURNED TO EWR, LANDED WITHOUT INCIDENT. MX CHECKED AILERON CABLES, ALL CHECKED NORMAL. THE ELEVATORS CHECKED NORMA L IAW MM 27-10-00. THE ACFT WAS TAKEN OUT OF SERVICE. THE ELEVATOR FEEL MECHANISM WAS FOUND DAMAGED DURING INSPECTION OF THE ELEVATOR SYSTEM. THE DAMAGE WAS CAUSED BY IMPACT FROM THE NR 2 ENGINE/APU O/B FIRE BOTTLE. THE BOTTLE THERMALLY DISCHARGED, BROKE LOOSE FROM ITS MOUNTING BRACKETS AND SUBSEQUENTLY STRUCK THE FEEL MECHANISM. THE ELEVATOR FEEL MECHA NISM, FIRE BOTTLE AND FIRE BOTTLE MOUNTING BRACKETS WERE REPLACED. 2 L 7 3 4F A22WE 1999031200460 19990312 00460 SO 1999 3 12 COMA9910040 1 19990306 A 2750 12042642507 SELECTOR EMB 120 EMB120RT SO TE FLAPS MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 179CA 11486 120179 FLAP CONTROL FAULT. REPLACED FLAP SELECTOR LEVER. 2 L 7 2 4T RT A31SO 1999031200461 19990312 00461 EA 1999 3 12 COMA9960093 1 19990227 A 2710 10231007 DAMPENER CNDAIR CL600 CL6002B19 EA LT AILERON LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 3426 7117 DURING C-CHECK, FOUND LEFT AILERON FLUTTER DAMPENER LEAKING AROUND PISTON SIGHT GLASS. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999031200462 19990312 00462 EA 1999 3 12 COMA9960094 1 19990302 A 3246 50105711 WHEEL 50105841 CNDAIR CL600 CL6002B19 EA MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 4839 34 MAY960919 7159 MECHANIC REMOVED BOTH MAIN WHEELS FROM A/C 7159 BECAUSE RIGHT O/B TIRE WAS FOUND FLAT. DURING A VISUAL LEAK CHECK IN WH EEL SHOP FOUND SUBASSEMBLY CRACKED AT BOTTOM OF KEY BOSS APPROXIMATELY 1 INCH LONG. WHEEL SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS. 2 L 7 2 4F RT A21EA 1999031200463 19990312 00463 EA 1999 3 12 COMA9960095 1 19990308 A 3246 50105841 WHEEL 50105711 CNDAIR CL600 CL6002B19 EA MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 4336 128 MAY960897 7235 MECHANIC REMOVED WHEEL ASSEMBLY FROM AIRCRAFT DUE TO TIRE FOUND FLAT. VISUALLY INSPECTED WHEEL IN TIRE SHOP WITH WATER AND SOAP LEAK CHECK AND FOUND WHEEL CRACKED AT BOTTOM OF KEY BOSS AREA APPROXIMATELY 1 INCH LONG. WHEEL SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS. 2 L 7 2 4F RT A21EA 1999031200464 19990312 00464 EA 1999 3 12 COMA9960096 1 19990306 A 2752 852D10011 ACTUATORS CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 710CA 1915 7241 FLAPS FAIL MESSAGE. REPLACED THE LEFT HAND INBOARD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 1999031200465 19990312 00465 EA 1999 3 12 COMA9960097 1 19990306 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 1577 7014 FLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999031200466 19990312 00466 EA 1999 3 12 COMA9960098 1 19990305 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 940CA 5883 7048 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999031200467 19990312 00467 WP 1999 3 12 UPS99828847 1 19990304 A 2740 TRIM SERVO DOUG DC8 DC871F 302199D WP HORIZ STAB FAILED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-N/A WHILE A/C WAS BEING LOADED, LOADERS COMPLAINED OF A STRANGE SMELL. MAINT WAS CALLED AND OBSERVED SM OKE IN A/C. A/C WAS EVACUATED AND THE FIRE DEPARTMENT WAS DISPATCHED. FOUND LONG TRIM SERVO UNIT 2 FROZEN EVIDENCE OF MOTOR BURNED UP. REMOVED AND REPLACED SERVO PER M/M 27-41-10 (P/N 300425-02) ON, (P/N 300425-01) OFF, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999031200468 19990312 00468 WP 1999 3 12 UPS99828849 1 19990305 A 3350 5708458503 BATTERY DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-N/A, EMERGENCY LIGHT'S INOP. SWITCH LEFT IN ON POSITION. REMOVED SERVICEABLE BATTERY PACK UNIT FROM A/ C 868 AND INSTALLED INT O A/C 750. OPS CHK'S GOOD, ALL SECURE. INSTALLED (P/N 5708458-503) (S/N 10382) ON, (P/N 5708458 -503) (S/N 925) OFF. 2 L 7 4 4F RT 4A25 1999031200469 19990312 00469 WP 1999 3 12 UPS99828850 1 19990222 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, LT O/B LOWER L/E RIB IS CRACKED AT STA FS 622.500. REPAIRED AREA IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999031200470 19990312 00470 WP 1999 3 12 UPS99828852 1 19990223 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 590 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 590 AT RBL 24 THE SEAT TRACK SPLICE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED SPLICE FITTING IAW SRM 53-2-3 FIG 6A. 2 L 7 4 4F RT 4A25 1999031200471 19990312 00471 WP 1999 3 12 UPS99828854 1 19990223 A 5720 57690016 DOUBLER DOUG DC8 DC873F 302199F WP WS 564 & 571 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, RT WING L/E AT STA FS 564 AND 571 THE LWR I/B SKIN DOUBLER IS CRACKED IN 3 PLACES. REPAIRED AREA IAW SRM 57-3-3 FIG 6. 2 L 7 4 4F RT 4A25 1999031200472 19990312 00472 WP 1999 3 12 UPS99828855 1 19990222 A 5320 97540242 BRACE DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 1220 ABOVE STR 27R THE FLOORBEAM SUPPORT BRACE IS CRACKED. REMOVED AND REPLACED BRACE IAW DWG 9754024 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031200473 19990312 00473 WP 1999 3 12 UPS99828856 1 19990222 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 520.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, RT WING L/E RIB AT STA 520.168 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999031200474 19990312 00474 EU 1999 3 12 QXEA9900237 1 19990103 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 46. REPAIRED IAW FOKKER SRM 51-31-01, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200475 19990312 00475 EU 1999 3 12 QXEA9900238 1 19990103 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 47. REPAIRED IAW FOKKER SRM 51-31-01, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200481 19990312 00481 EU 1999 3 12 QXEA9900244 1 19990103 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 14755 CASTELLATION CRACKED AT STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200488 19990312 00488 EU 1999 3 12 QXEA9900251 1 19990114 A 5220 FRAME FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT-HAND AFT OVERWING EMERGENCY EXIT HAS CRACK IN TOP FORWARD CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON AIR EO 4-52-21E. 2 L 7 2 4F RT A20EU 1999031200489 19990312 00489 EU 1999 3 12 QXEA9900252 1 19990114 A 5220 FRAME FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN TOP FORWARD CORNER FRAME PROFILE RADIUS. REPAIRED IAW HORI ZON AIR EA 4-52-21 E. 2 L 7 2 4F RT A20EU 1999031200490 19990312 00490 EU 1999 3 12 QXEA9900253 1 19990114 A 5220 FRAME FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN TOP AFT CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW H ORIZON EO 4-52-21E. 2 L 7 2 4F RT A20EU 1999031200491 19990312 00491 EU 1999 3 12 QXEA9900254 1 19990114 A 5220 FRAME FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN LOWER AFT CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON AIR EO 4-52-21 E. 2 L 7 2 4F RT A20EU 1999031200492 19990312 00492 EU 1999 3 12 QXEA9900255 1 19990114 A 5220 FRAME FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND FORWARD OVERWING EMERGENCY EXIT HAS CRACK IN LOWER FORWARD CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW HORIZON AIR EO 4-52-21E. 2 L 7 2 4F RT A20EU 1999031200493 19990312 00493 EU 1999 3 12 QXEA9900256 1 19990114 A 5220 FRAME FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND AFT OVERWING EMERGENCY EXIT HAS CRACK IN TOP FORWARD CORNER FRAME PROFILE AT RIVET LINE. REPAIRED IAW H ORIZON AIR EO 4-52-21E. 2 L 7 2 4F RT A20EU 1999031200494 19990312 00494 EU 1999 3 12 QXEA9900257 1 19990109 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME CLIP IN AFT PIT FRAME 13815B AND STRINGER 2 IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200495 19990312 00495 EU 1999 3 12 QXEA9900258 1 19990106 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FORWARD PIT FRAME 8305 CLIP BETWEEN STRINGERS 2 AND 72 HAVE LIGHT CORROSION AND MISSING PAINT. REPAIRED IAW FOKKE R SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999031200496 19990312 00496 EU 1999 3 12 QXEA9900259 1 19990106 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FORWARD CARGO PIT FRAME 8805 CLIPS BETWEEN STRINGERS 1 AND 72 HAVE MISSING PAINT AND LIGHT CORROSION. REPAIRED IA W FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999031200497 19990312 00497 EU 1999 3 12 QXEA9900260 1 19990106 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FORWARD PIT FRAME 7805 CLIPS BETWEEN STRINGERS 74 AND 72 HAS LIGHT SURFACE CORROSION, PAINT MISSING OR BUBBLY. RE PAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999031200498 19990312 00498 EU 1999 3 12 QXEA9900261 1 19990106 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU BS 4850 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499OS 11182 PDX - CORROSION ON STRINGER 68A AT STATION 4850. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200499 19990312 00499 EU 1999 3 12 QXEA9900262 1 19990106 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU BS 3820-4150 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - STRINGER 68A CRACKED BETWEEN STATION 3820 AND 4150. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200500 19990312 00500 EU 1999 3 12 QXEA9900263 1 19990115 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LOWER ATC ANTENNA/FUSELAGE MOUNT AREA HAS SURFACE CORROSION AND LIGHT PITTING ON FUSELAGE SKIN. REPAIRED IAW FOKK ER SRM 51-31-01 AND 53-02-01, PAGE 8 FIGURE 6. 2 L 7 2 4F RT A20EU 1999031200504 19990312 00504 EU 1999 3 12 QXEA9900267 1 19990115 A 5312 BULKHEAD SUPPORT FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - REPAIR LOCATED BETWEEN SUPPORTS III AND IV AT THE FORWARD PRESSURE BULKHEAD RIGHT SIDE DOES NOT CONFORM TO SRM 53- 02-18 PAGE 41-46. REPAIRED IAW HORIZON AIR EA 4-53-673. 2 L 7 2 4F RT A20EU 1999031200505 19990312 00505 EU 1999 3 12 QXEA9900268 1 19990106 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 3870-4175 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - A 3 TO 4 INCH CRACK BETWEEN RIVETS ON STRINGER 69 BETWEEN FRAMES 3870 AND 4175. REPAIRED IAW FOKKER SRM 53-02-02 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200507 19990312 00507 EU 1999 3 12 QXEA9900270 1 19990109 A 5230 BRACKET FOKKER F28 F28MK4000 4990810 EU CARGO DOOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FORWARD PIT AFT DOOR SUPPORT ROD FUSELAGE BRACKET LOOSE AND PREVIOUS REPAIR UNDER BRACKET APPEARS BENT AND BUCKLED . REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999031200508 19990312 00508 EU 1999 3 12 QXEA9900271 1 19990109 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AFT CARGO PIT CRACKED CLIP ON FRAME 13815A AT STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-11, FIGURE 1 AND SRM 53-0 2-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1999031200509 19990312 00509 EU 1999 3 12 QXEA9900272 1 19990109 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AFT CARGO PIT CRACKED CLIP ON FRAME 13815A AT STRINGER 73. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1999031200510 19990312 00510 EU 1999 3 12 QXEA9900273 1 19990103 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AFT CARGO PIT CRACKED CLIP AT FRAME 13815B BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-12M PAGE 4. 2 L 7 2 4F RT A20EU 1999031200511 19990312 00511 EU 1999 3 12 QXEA9900274 1 19990125 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AFT CARGO PIT CORROSION UNDER 6 NUT PLATES ON FRAME 14755 BETWEEN STRINGERS 3 AND 74. REPAIRED IAW FOKKER SRM 53- 02-12, PARAGRAPH 2, PAGE 7. 2 L 7 2 4F RT A20EU 1999031200512 19990312 00512 EU 1999 3 12 QXEA9900275 1 19990113 A 5320 RAIL FOKKER F28 F28MK4000 4990810 EU PEDESTAL CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND AND RIGHT-HAND SIDES OF PEDESTAL HAVE CORROSION ON THE BOTTOM SIDE OF THE LOWER RAILS AND AT THE MOUNT B OLT HOLES FROM THE CENTER MOUNT BOLTS AFT. REPAIRED IAW HORIZON AIR EA 4-53-649. 2 L 7 2 4F RT A20EU 1999031200513 19990312 00513 EU 1999 3 12 QXEA9900276 1 19990114 A 5312 BULKHEAD WEB FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRONT PRESSURE BULKHEAD WEB HAS CRACK AT THE VII BEAM AT BL100L. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 14. 2 L 7 2 4F RT A20EU 1999031200516 19990312 00516 EU 1999 3 12 QXEA9900279 1 19990117 A 5414 SKIN FOKKER F28 F28MK4000 4990810 EU NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - INSIDE PANEL 02C, AT THE OUTBOARD SIDE THE 7TH STAGE BLEED AIR NACELLE FLANGE AREA IS CRACKED FROM SEVERAL RIVET H EADS ALONG THE FORWARD EDGE. REPAIRED IAW FOKKER SRM 54-14-01, PAGE 405 AND SRM 54-02-01, PAGE 4, FIGURE 3. 2 L 7 2 4F RT A20EU 1999031200517 19990312 00517 EU 1999 3 12 QXEA9900280 1 19990107 A 7810 NOZZLE FOKKER F28 F28MK4000 4990810 EU RT ENG EXHAUST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THE RIGHT ENGINE EXHAUST PROPELLING NOZZLE HAS A CRACK AT INBOARD AND UPPER CENTER LOBE SUPPORT. REPAIRED IAW HOR IZON AIR EA 4-78-010. 2 L 7 2 4F RT A20EU 1999031200518 19990312 00518 EU 1999 3 12 QXEA9900281 1 19990107 A 7810 NOZZLE FOKKER F28 F28MK4000 4990810 EU ENGINE EXHAUST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THE PROPELLING NOZZLE AT SUPPORT HAS A CRACK ON THE OUTBOARD LEG. REPAIRED IAW HORIZON AIR EA 4-78-011. 2 L 7 2 4F RT A20EU 1999031200519 19990312 00519 EU 1999 3 12 QXEA9900294 1 19990107 A 5314 KEEL BEAM FOKKER F28 F28MK4000 4990810 EU RT MLG WW CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - MINOR PITTING CORROSION ON KEEL BEAM LOCATED ON FORWARD AND AFT END OF MAIN LANDING GEAR DOOR HINGE ATTACH POINT, RIGHT-HAND SIDE. REPAIRED IAW HORIZON AIR EA 4-53-647. 2 L 7 2 4F RT A20EU 1999031200520 19990312 00520 EU 1999 3 12 QXEA9900295 1 19990128 A 5522 PANEL FOKKER F28 F28MK4000 4990810 EU LT ELEVATOR TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND ELEVATOR HINGE PANEL 53K HAS BEEN TORN AT 2 PLACES DUE TO PANEL 53AB CONTACTING IT WHEN ROTATING ELEVATO R THOUGH TRAVEL RANGE. REPAIRED IAW HORIZON AIR EA 4-27-72. 2 L 7 2 4F RT A20EU 1999031200522 19990312 00522 EU 1999 3 12 QXEA9900297 1 19990101 A 2710 BRACKET FOKKER F28 F28MK4000 4990810 EU AILERON PULLEY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AILERON PULLEY CLUSTER BRACKET HAS CORROSION STARTING AT PULLEY ATTACH BOLT. REPAIRED IAW FOKKER MM 27-11-00, PAG E 602, PARAGRAPH 3C (1). 2 L 7 2 4F RT A20EU 1999031200525 19990312 00525 EU 1999 3 12 QXEA9900300 1 19990130 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU BS 1600 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIVET HEAD PARTIALLY MISSING ON FORWARD LEFT-HAND FUSELAGE SKIN AT FRAME/STATION 1600, STRINGERS 16 AND 17. REPAI RED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200526 19990312 00526 EU 1999 3 12 QXEA9900301 1 19990105 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU COCKPIT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - COCKPIT ROOF FORWARD SKIN PANEL ABOVE PILOT AND CO-PILOT WINDSHIELDS HAS SIGNIFICANT DAMAGE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200527 19990312 00527 EU 1999 3 12 QXEA9900302 1 19990105 A 2720 RUDDER PEDAL FOKKER F28 F28MK4000 4990810 EU LT & RT COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - CORROSION AT THE BASE OF PILOTS AND CO-PILOTS RUDDER PEDAL ASSEMBLY. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8, PARA GRAPH 3A. 2 L 7 2 4F RT A20EU 1999031200528 19990312 00528 EU 1999 3 12 QXEA9900303 1 19990119 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FORWARD CARGO PIT FRAME 9305 BETWEEN STRINGERS 74-1-2 HAS EXFOLIATION UNDER TOP FLANGE AROUND NUT PLATES. REPAIRE D IAW FOKKER 53-02-12 PAGE 9, FIGURE 3. 2 L 7 2 4F RT A20EU 1999031200530 19990312 00530 EU 1999 3 12 QXEA9900305 1 19990109 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AFT CARGO PIT FRAME 13815B AT STRINGER 74 UNDER TOP LIP OF CHANNEL FRAME HAS EXFOLIATION CORROSION UNDER NUT PLATE . REPAIRED IAW HORIZON AIR EA 4-53-644. 2 L 7 2 4F RT A20EU 1999031200531 19990312 00531 EU 1999 3 12 QXEA9900306 1 19990107 A 5280 HINGE FOKKER F28 F28MK4000 4990810 EU LT MLG DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND MAIN LANDING GEAR DOOR HINGE ATTACH AREA ALONG LEFT-HAND KEEL BEAM HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-650. 2 L 7 2 4F RT A20EU 1999031200532 19990312 00532 EU 1999 3 12 QXEA9900307 1 19990107 A 5280 HINGE FOKKER F28 F28MK4000 4990810 EU LT MLG DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND MAIN LANDING GEAR DOOR HINGE ATTACH AREA ALONG LEFT-HAND KEEL BEAM HAS PITTING CORROSION AT FORWARD CORN ER. REPAIRED IAW HORIZON AIR EA 4-53-650. 2 L 7 2 4F RT A20EU 1999031200533 19990312 00533 WP 1999 3 12 ABXA9900168 1 19990303 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1056 & 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 LONGERON 17 LEFT CRACKED AT STATION 1056 AND 1041. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999031200534 19990312 00534 WP 1999 3 12 ABXA9900169 1 19990303 A 5313 59114277 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 LONGERON 16 RIGHT CRACKED AT STATION 1041. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999031200535 19990312 00535 WP 1999 3 12 ABXA9900170 1 19990303 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 LONGERON 17 RIGHT CRACKED AT STATION 1041. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999031200536 19990312 00536 WP 1999 3 12 ABXA9900171 1 19990303 A 5320 991050313 WEB DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 RIGHT CUSP WEB CRACKED AT STATION 1041 UNDER RIGHT OUTBOARD SEAT TRACK. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999031200537 19990312 00537 WP 1999 3 12 ABXA9900172 1 19990303 A 5320 99105035 WEB DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 LEFT OUTBOARD CUSP WEB AT STATION 1041 FRAME, CRACKED IN 3 PLACES UNDER LEFT OUTBOARD SEAT TRACK, LBL 54. REPAIRED CUSP WEB IAW DC9 SRM 53-04. 2 L 7 2 4F A6WE 1999031200538 19990312 00538 WP 1999 3 12 MWEA99084 1 19990305 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP DOOR SLIDE DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 THE GALLEY SLIDE COVER FELL OFF. MTC REATTACHED THE GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1999031200539 19990312 00539 NM 1999 3 12 MWEA99085 1 19990305 A 5320 39146531 FITTING DOUG MD88 MD88 3023688 NM BS 1325 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 SHOVEL CLIP AT FS 1325 AT L24L IS CORRODED BEYOND LIMITS. MTC FABRICATED AND INSTALLED NEW SHOVEL CLIP FITTING. 2 L 7 2 4F RT A6WE 1999031200540 19990312 00540 NM 1999 3 12 DL76L990414 1 19990228 A 2722 ACTUATOR 75130 BOEING 767 767332 1382001 NM RUDDER LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 178DN 25143 A/C 178 ATB FOR PARTIAL LOSS OF LEFT SYS HYDRAULIC FLUID, REPORTED IN FLT. FOUND RUDDER RATIO ACT EHV LEAKING. REPLACE D SAME, OPS CHECK. 2 L 7 2 4F RT A1NM 1999031200541 19990312 00541 NM 1999 3 12 DL73K990419 1 19990226 A 5330 654576988 SKIN BOEING 737 737232 1384475 NM BS 380-400 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 A 2 INCH LONG CRACK WAS FOUND EXTENDING FROM THE E & E COMPARTMENT COOLING DUCT CUTOUT IN THE FUSELAGE SKIN AT FS 370 & STR 28L. ALSO, AN EXISTING SKIN REPAIR DOUBLER WAS IN THE AREA. THE SKIN WAS CUT FROM STRINGER 26L TO 26R AT FS 400 AN D THE ENTIRE SECTION OF SKIN REMOVED FROM FS 400 TO THE FACTORY BUTT SPLICE AT FS 360. A NEW SECTION OF SKIN WAS SPLICE D IN WITH EXTERNAL ALUMINUM SPLICE STRAPS PER ER/A 366725-14. 2 L 7 2 4F RT A16WE 1999031200542 19990312 00542 NM 1999 3 12 DL72L990420 1 19990226 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1050-1080 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 SEVERAL EXISTING SKIN DOUBLER REPAIRS WERE LOCATED ON THE BELLY SKIN PANEL BETWEEN STRINGERS 26L & 26R AND BETWEEN FS 10 10 AND 1080. THE REPAIRS WERE FOR CORROSION CUTOUTS. TO IMPROVE THE CONDITION OF SKIN AND ELIMINATE ADDITIONAL CORROSI ON, THE SKIN WAS CUT AT FS 1080 BETWEEN STRINGERS 26L & 26R AND THE SECTION REMOVED TO FS 1010. A NEW SECTION OF SKIN W AS SPLICED IN WITH ALUMINUM SPLICE STRAPS PER ER/A. 2 L 7 3 4F A3WE 1999031200543 19990312 00543 NM 1999 3 12 DL72W990421 1 19990227 A 5711 WEB BOEING 727 727247 138408F NM WING REAR SPAR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 WHILE ACCOMPLISHING THE CENTER WING REAR SPAR WEB MOD PER BAC S/B 57A0182, SEVERAL FASTENER HOLE LOCATIONS WERE DAMAGED. THE MODIFICATION DOUBLERS AND FILLERS WERE EXTENDED TO REPAIR THE EXTRA DAMAGE PER ER/A 366706-14AD. 2 L 7 3 4F A3WE 1999031200544 19990312 00544 NM 1999 3 12 DL72S990422 1 19990226 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 400-420 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC I NTERNAL INSPECTION OF THE ENTIRE PANEL CONFIRMED 7 CRACKS BETWEEN FS 400 AND 420. THE DAMAGED SECTION OF LAP SPLICE WA S CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366754-14. 2 L 7 3 4F A3WE 1999031200545 19990312 00545 NM 1999 3 12 DL72S990423 1 19990228 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 LFEC INSPECTION OF THE STRINGER 4R LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERN AL INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 360 AND 380. THE CRACKED AREA OF SKIN LAP WAS CUTOUT AND REPAIRED WITH AN E XTERNAL ALUMINUM DOUBLER PER ER/A 366753-14, REV A. 2 L 7 3 4F A3WE 1999031200546 19990312 00546 NM 1999 3 12 DL72S990424 1 19990228 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 48 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT O F THE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366752-14, REV A. 2 L 7 3 4F A3WE 1999031200547 19990312 00547 NM 1999 3 12 DL72S990425 1 19990228 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 & 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 94 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366751-14, REV A. 2 L 7 3 4F A3WE 1999031200548 19990312 00548 NE 1999 3 12 DLL10990426 2 19990301 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 FAILED A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 27 1734D 44817 193C1225 010672 ENG FLAME-OUT OCCURED 5 MINUTES AFTER T/O ON CLIMBOUT. APPARENTLY RESULTED FROM FAILURE OF NR 1 ENG FUEL HP SOV. REPLA CED ENGINE. 2 L 7 3 4F 4 F A23WE E12EU 1999031200549 19990312 00549 NM 1999 3 12 DLM88990428 1 19990301 A 3350 LIGHT RPS1 DOUG MD88 MD88 3023688 NM ROW 12 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 999DN 3027 53371 ON L/O CHECK, FOUND EMERGENCY LIGHTS INOP ROW 12 AND FWD. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 1999031200550 19990312 00550 NM 1999 3 12 DL72S990430 1 19990301 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 477DA 20754 EXTERIOR EMERGENCY LIGHT R/S BETWEEN OVERWING EMERGENCY EXITS INOP. REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999031200551 19990312 00551 NM 1999 3 12 DL72S990431 1 19990302 A 2913 PUMP 57186 BOEING 727 727232 1384082 NM B HYD SYST DAMAGED A DALA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 522DA 152892 21582 AFTER T/O ON INIT CLMB, BOTH HYD SYS B PUMPS LOW PRESS LIGHTS ILLUM. HYD QTY IN A SYS DROPPED TO 2.5 GALS, B QTY APPEAR ED NORMAL. PRESS THEN DROPPED TO NEAR ZERO, TURNED PUMPS OFF IAW POM 1 TO 2 MINS AFTER ILLUMINATION. FOUND O-RING ON N R 1 B SYS HYD PUMP CASE TO END PLATE BLOWN OUT. REPLACED BOTH CASE DRAIN FILTERS CHGD, NO CONTAMINATION. REPLACED NR 1 B SYS HYD PUMP, SERVICED SYSTEM. OPS CHECKS AND LEAK CHECKS GOOD. 2 L 7 3 4F A3WE 1999031200552 19990312 00552 1999 3 12 DL767990432 4 19990302 A 2565 SLIDE BOEING 767 767232 1385132 NM LT OVERWING DETACHED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 SO 27 110DL 22222 PASSING 21,000 FT MSL, FLT ATTENDANTS COMPLAINED OF LOUD NOISE. ALSO, HAD EICAS MSG LT SLIDE DOOR AND OVERHEAD DISCREET EMERG DOORS. AIR TURNBACK TO ATL. FOUND LT OVERWING SLIDE PANEL AND SLIDE DEPARTED AIRCRAFT. SEVERAL SMALL ABRASIONS AROUND SURROUNDING AREA. REPLACED SLIDE, REPAIRED SURROUNDING AREA. 2 L 7 2 4F RT A1NM 1999031200553 19990312 00553 NM 1999 3 12 DL72L990433 1 19990302 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM R1 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 511DA 21313 R1 OVER DOOR EMER LIGHT INOP. REPLACED LIGHT, CKS GOOD. 2 L 7 3 4F A3WE 1999031200554 19990312 00554 WP 1999 3 12 DLL10990434 1 19990302 A 3350 20131A BATTERY LKHEED 1011 10113851 5265010 WP COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718DA 193C1097 F/C EMER LIGHTS INOP. REPLACED BATTERY PACK AND POWER SUPPLY. 2 L 7 3 4F A23WE 1999031200555 19990312 00555 NE 1999 3 12 DL757990435 2 19990303 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 682DA 37725 26958 716304 LT OIL FILTER EICAS MESSAGE DURING CLIMBOUT. FOLLOWED POM, SHUTDOWN ENGINE. REPLACED NUMBER 1 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999031200556 19990312 00556 NM 1999 3 12 DL733990436 1 19990303 A 5312 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309WA 23442 BS 178 BLKHD WEB WAS FOUND WITH 6 CRACKS, MAX CRACK CUTOUT WAS 1.6 BY 1. REPAIRED PER ERA 332820-14. 2 L 7 2 4F RT A16WE 1999031200557 19990312 00557 NM 1999 3 12 DL733990437 1 19990303 A 5330 SKIN BOEING 737 737347 1384647 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309WA 23442 FUSELAGE SKIN WAS FOUND CRACKED AROUND THE AFT EDGE OF THE E/E COMPT COOLING AIR EXHAUST DUCT CUTOUT AT BS 380, BL 0.0. THE CRACK EXTENDS AFT FROM THE EDGE OF CUTOUT. REPAIRED PER ERA 366476-14, REV B. 2 L 7 2 4F RT A16WE 1999031200558 19990312 00558 NM 1999 3 12 DLM90990439 1 19990301 A 3350 LIGHT DOUG MD90 MD9030 3023690 NM ROW 1C BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 906DA 53386 EMERGENCY FLOOR LIGHT BY SEAT 1C IS BROKEN AND FLOOR LIGHT TRACK IS CRACKED. REPLACED LIGHT ASSY AND WIRING, OPS CKD NO RMAL. 2 L 7 2 4F RT A6WE 1999031200559 19990312 00559 NM 1999 3 12 DL757990440 1 19990303 A 2133 OUTFLOW VALVE 60683221 BOEING 757 757232 1384965 NM CABIN INOP A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 607DL 121236 22814 CABIN ALTITUDE AUTO INOP ON T/O. REPLACED OUTFLOW VALVE. 2 L 7 2 4F RT A2NM 1999031200560 19990312 00560 NM 1999 3 12 DL72S990441 1 19990303 A 5510 65168016 FITTING BOEING 727 727232 1384082 NM VERT STAB WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 WEAR WAS FOUND ON BOTH ATTACH LUGS FOR THE HORIZ STAB JACK SCREW MECHANISM. WEAR WAS ON BOTH I/B AND O/B FACES OF EACH LUG. REWORKED PER ERA 332860-14, REV A. 2 L 7 3 4F A3WE 1999031200561 19990312 00561 1999 3 12 DL767990442 4 19990302 A 2565 SLIDE BACT32G6410 BOEING 767 767232 1385132 NM LT WING DEPLOYED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 110DL 22222 LT OVERWING SLIDE DEPLOYED IN FLIGHT PASSING THRU FL 12 OUT OF ATL. MTC OBSERVED LINKAGE ON DOOR RELEASE MECHANISM, FOU ND THIRD LINKAGE FROM FORWARD EDGE BENT AND BROKEN, CAUSING CENTER TWO LATCHES TO RELEASE. FORWARD AND AFT LATCHES WERE FOUND INTACT WITH DOOR KEEPERS STILL IN PLACE. SLIDE AND DOOR WERE FOUND MISSING, AND FIVE SURROUNDING PANELS DAMAGED. SQUIBB WAS FOUND NOT FIRED AND SLIDE INFLATION BOTTLE EMPTY. (P/N 251205959) BROKEN LINAGE, (P/N BACT32G64-1072). RE PLACED SAME. 2 L 7 2 4F RT A1NM 1999031200562 19990312 00562 NM 1999 3 12 DL757990444 1 19990226 A 2550 BLANKET BOEING 757 757232 1384965 NM BS 1460-1480 BURNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 DURING MID VISIT ON ROUTINE INSPECTION, A INSULATION BLANKET WAS FOUND WITH THE OUTER PLY MELTED AND THE INSULATION HAD BLACK SPOTS WHICH APPEARED TO BE BURN SPOTS AT FS 1460 TO 1480 STR 26R AND STR 22R. THERE ARE NO OTHER SIGNS OF DAMAG E IN THE AREA WHICH IS BENEATH THE EQUIPMENT RACKS. THERE ARE NO SIGNS OF DAMAGE TO ANY RELAYS OR WIRES IN THE AREA ABO VE OR BELOW THE INSULATION BLANKET. 2 L 7 2 4F RT A2NM 1999031200563 19990312 00563 NM 1999 3 12 DL72S990446 1 19990226 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 686.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 LT WING UPPER STR-TO-RIB HOLE INSP, SHOWS CRACK INDICATION WS 686.5 STRINGER 11. CUT ACCESS HOLE IN STRINGER, BEGAN DRI LLING UP RADIUS BLOCKS. STOP DRILLED CRACK, REMOVED FUEL VENT TUBE FWD OF STRINGER 12 AT WS 686.5 TO FOM, REMOVED FUEL PROBE HARNESS STANDOFF AT STRINGER 10 WS 686.5 TO FOM. COMPLETED STEPS 6 AND 7 PER MM 57-13-0 FIG 804. *S/D* INSTALLE D REPAIR ANGLES PER MM 57-13-0 FIG 804. INSTALLED COVER PLATE COMPLETED STEPS 18-20, 57-13-0 FIG 804. REINSTALLED VENT TUBE AND HARNESS STANDOFF. 2 L 7 3 4F A3WE 1999031200564 19990312 00564 NM 1999 3 12 DL72S990448 1 19990226 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 686.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 RT WING STR-TO-RIB INSP AT WS 686.5 STRINGER 8 SHOWS CRACK INDICATION, MARKED (AFT UPPER STR). LOOSENED FUEL DUMP LINE FOR ACCESS, BEGAN DRILLING UP REPAIR PER M/M 57-13-0 FIG 802. STOP DRILLED CRACK REPAIR PER M/M 57-13-0 FIG 802. INSTA LLED REPAIR PER M/M 57-13-0 FIG 802. REPAIR INSTALLATION OK. FUEL LINE INSTALLED ON NR 1292. 2 L 7 3 4F A3WE 1999031200565 19990312 00565 NM 1999 3 12 DL72S990449 1 19990303 A 5320 WEB BOEING 727 727232 1384082 NM BS 1266 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 FOUND ON E2 LETTER CK, LT VERTICAL TORQUE BOX WEB CRACKED AT RIVET ALONG UPPER EDGE AT STA 1266. REPAIRED PER MM 53-11- 0. 2 L 7 3 4F A3WE 1999031200566 19990312 00566 NM 1999 3 12 DL72S990450 1 19990215 A 5311 FRAME BOEING 727 727232 1384082 NM BS 950 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 27L TO 25L. REMOVED DAMAGE PER SRM 53- 10-4 FIG 27, FABRICATED DOUBLER PER SRM 53-10-4 FIG 27. REMOVED FACTORY SPLICE. INSTALLED REPAIR PER SRM 53-10-4 FIG 2 7 REV NR 1170. 2 L 7 3 4F A3WE 1999031200567 19990312 00567 NM 1999 3 12 DL72S990451 1 19990226 A 5210 BEAM BOEING 727 727232 1384082 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 CRACK IN L-1 LOWER BEAM AFT CORNER HFEC TO CONFIRM CRACK MARK ENDS. FABRICATED REPAIR DOUBLER PER M/M 52-11-01 FIG 803. STOP DRILLED CRACK AT MARKED ENDS. INSTALLED PER M/M 52-11-01 FIG 803. COMPLETED INST PER M/M 52-11-01 FIG 803. 2 L 7 3 4F A3WE 1999031200568 19990312 00568 NE 1999 3 12 DL73K990453 2 19990303 A 7230 COMPRESSOR BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 329DL 52203 23101 700242 DURING CRUISE AT FL370 FROM MCO-BOS, CREW EXPERIENCED HEAVY COMPRESSOR STALLS ON THE NR 2 ENGINE. CREW REDUCED POWER AN D LANDED IN RDU. CONTRACT MTC INSPECTED ENGINE AND FOUND EXTENSIVE COMPRESSOR AND FAN BLADE DAMAGE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2EA 1999031200569 19990312 00569 NM 1999 3 12 DL73K990454 1 19990304 A 3320 10607521 BALLAST BOEING 737 737232 1384475 NM GALLEY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 331DL 23103 SMOKE AND FUMES IN FWD CABIN AND FLT DECK. DIVERTED TO ATL. REPLACED FWD GALLEY CEILING LIGHT BALLAST. 2 L 7 2 4F RT A16WE 1999031200570 19990312 00570 NM 1999 3 12 DL72S990457 1 19990304 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FOUND ON C2 LETTER CK, RT KEEL BEAM SUPPORT ANGLE CRACKED AT STA 870. REPLACED ANGLE PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999031200571 19990312 00571 NM 1999 3 12 DL73K990458 1 19990304 A 3244 TIRE BOEING 737 737247 138448D NM RT MLG FAILED A DALA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 237WA WHLDL4377 23185 NR 3 MAIN TIRE WORN, RECAP SEPARATED AND DAMAGED I/B FLAP ASSY AND SPOILER CONTROL VALVE CABLE AND BRAKE HYDR LINE. (S/ N DL 4377) TIRE (S/N 73361870). 2 L 7 2 4F A16WE 1999031200572 19990312 00572 NM 1999 3 12 DL72S990459 1 19990303 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL BE TWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 35 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE P ANEL LENGTH AND REPAIR WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366784-14, REV A. 2 L 7 3 4F A3WE 1999031200573 19990312 00573 NM 1999 3 12 DL72S990460 1 19990303 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED SEVERAL CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT O UT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366782-14, REV B. 2 L 7 3 4F A3WE 1999031200574 19990312 00574 NM 1999 3 12 DL72S990461 1 19990223 A 5341 FITTING BOEING 727 727232 1384082 NM RT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 AT HMV2, FOUND CORROSION IN BORES AND MATING SEAM OF AFT RT WING AND FUS REMINAL FITTINGS. BLENDED CORROSION, CHECKED, REWORKED PER ERA 366788-14, INSTALLED BUSHNG. 2 L 7 3 4F A3WE 1999031200575 19990312 00575 NM 1999 3 12 DL72S990462 1 19990116 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED IN TWO PLACES AT THE I/B AFT FLAP DRIVE ROD CUTOUT. THE CRACK W AS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809. 2 L 7 3 4F A3WE 1999031200576 19990312 00576 NM 1999 3 12 DL757990464 1 19990304 A 3350 BR9279117 SIGN BOEING 757 757232 1384965 NM R1 DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 FOUND ON L/O, EMERG DOOR EXIT IDENTIFIER DAMAGED AT R1 DOOR. REPLACED EXIT IDENTIFIER AT R1 DOOR, CKS GOOD. 2 L 7 2 4F RT A2NM 1999031200577 19990312 00577 NM 1999 3 12 DL72S990465 1 19990305 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 OVERWING RT SIDE EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND OPS CK GOOD. 2 L 7 3 4F A3WE 1999031200578 19990312 00578 NM 1999 3 12 DL767990466 1 19990304 A 3350 20131A BATTERY BOEING 767 767232 1385132 NM LT SERVICE DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 105DA 22217 EMERGENCY LIGHTS INOP LT AFT CEILING AND LT AFT SERVICE DOOR. REPLACED BATTERY PACK, OPS NORMAL. 2 L 7 2 4F RT A1NM 1999031200579 19990312 00579 NM 1999 3 12 DL72S990467 1 19990305 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 FLASHLIGHT HAD NO CHARGE. REPLACED BATTERY, OPS CK GOOD. 2 L 7 3 4F A3WE 1999031200580 19990312 00580 NM 1999 3 12 DL73E990468 1 19990305 A 3350 1000677 LIGHT BOEING 737 7372J8 1384489 NM L1 DOOR INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 235WA 22859 EMERGENCY EXIT LIGHT ABOVE L1 DOOR INOP. REPLACED LIGHT ASSY, OP CKS GOOD. 2 L 7 2 4F RT A16WE 1999031200581 19990312 00581 NM 1999 3 12 DL72L990469 1 19990305 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 FOUND DURING F-2 LETTER CHECK, .5 INCH CRACK LT ELEVATOR LOWER SKIN FROM RIVET FWD I/B SIDE OF TAB ROD CUTOUT. REPAIRED PER SRM 55-20-3 FIG 4. 2 L 7 3 4F A3WE 1999031200582 19990312 00582 NM 1999 3 12 DLM88990471 1 19990305 A 2780 59388301 PULLEY DOUG MD88 MD88 3023688 NM LT LE SLAT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 ON L/O, FOUND LT WING I/B SLAT POS NR 0 LOOSE. FOUND RETRACT CABLE PULLEY BROKEN FOR SLAT ZERO. PULLEY WAS SCARRED. F OUND SLAT 5 DRIVE CABLE PULLEY DENTED, FALSE RIB AT SLAT ZERO TORN, AND MAIN SLAT ZERO DRIVE CABLE IN BAG BIN KINKED. R EPLACED ALL BROKEN OR DAMAGED PARTS. 2 L 7 2 4F RT A6WE 1999031200583 19990312 00583 1999 3 12 DL767990475 4 19990307 A 3413 VSI 0665000110 BOEING 767 767232 1385132 NM LT COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 109DL 3395REMOVED 22221 CAPTAINS VSI BLANKED AFTER BLUE SPARK OCCURED UNDER AND BEHIND CAPTAINS CLOCK PANEL. REPLACED VSI. 2 L 7 2 4F RT A1NM 1999031200584 19990312 00584 NM 1999 3 12 DHL99717002 1 19990305 A 5230 B22RQ18A2 SWITCH BOEING 727 72723 1384004 NM CARGO DOOR FAILED A DHLA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 717DH 19389 CARGO DOOR UNLOCK LIGHT ILLUMINATED ON CLIMBOUT FOLLOWED BY LOSS OF PRESSURIZATION. DUMPED FUEL WAS INITIATED. REPLACE D LIGHT SOCKET AND SEQUENCE SWITCH. 2 L 7 3 4F A3WE 1999031200585 19990312 00585 NM 1999 3 12 VNAA9903005 1 19990303 A 3060 A56362 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROPELLER DIRTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 427JS 27869 452 3039 DURING CLIMBOUT, A LEFT HAND PROPELLER HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD (PIT) AND LANDED SAFELY. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND PROPELLER BRUSH BLOCK ASSEMBLY, IN ACCORDANCE WITH D ORNIER MAINTENANCE MANUAL 30-61-05. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999031200586 19990312 00586 NM 1999 3 12 VNAA9903006 1 19990301 A 3242 BRAKES DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG OVERHEATED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 460PS 3061 THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A BRAKE TEMPERATURE HIGH WARNING INDICATION. OUTSTATION MAINTENANCE INSPECT ED AND CYCLED THE BRAKES, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-00. OPERATIONAL TAXI CHECKS WERE COMPLETE D, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999031200587 19990312 00587 NM 1999 3 12 TWAA9903601 1 19990307 A 3397 WIRE BOEING 767 7673Y0 NM ROW 16-25 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 THE FLOOR EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 16 TO 25, LT SIDE OF CABIN. REPAIRED WIRING WITH A SPLICE REPAIR AT ROW 26. CHECK-C 3-3-99 LAX. 2 L 7 2 4F RT A1NM 1999031200588 19990312 00588 NE 1999 3 12 TWAA9903602 2 19990308 A 7250 TURBIN BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE DAMAGED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 CE 05 54336 20490 1533 TAKEOFF WAS ABORTED AT ABOUT 60 KTS DUE TO NUMBER 3 ENGINE LOSS OF POWER AND VIBRATION. FOUND THE TURBINE HAD FAILED, W ITH DEBRIS IN THE TAILPIPE. DAMAGE WAS SUSTAINED TO THE TAIL PIPE, COWLING AND PYLON. REPLACED THE ENGINE AND ACCOMPLI SHED METAL REPAIRS. CHECK-C 10-29-98 MCI. *S/D* FOUND 1 EACH 3RD STAGE TURBINE BLADE WAS SUBJECT TO IMPACT DAMAGE AND EVENTUALLY FRACTURED DUE TO FATIGUE, CAUSING SEVERE DAMAGE TO N1 TURBINE. 2 L 7 3 4F 4 F A3WE E2EA 1999031200589 19990312 00589 WP 1999 3 12 TWAA9903603 1 19990303 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 550 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND SHIP DRAIN FITTING AT STA 550 BETWEEN LONGERONS 29L AND 30, WITH CORROSION. REPLACED DR AIN FITTING WITH (P/N 17-52804) AND FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 1999031200590 19990312 00590 WP 1999 3 12 TWAA9903604 1 19990305 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND LONGERON 16L CRACKED AT STA 965. CONFIRMED BY NDT. REPAIRED CRACKED LONGERON 16L AT ST A 965 PER SRM 53-02, FIG 18, PER PAGE 1 PARAGRAPH B. 2 L 7 2 4F A6WE 1999031200591 19990312 00591 WP 1999 3 12 TWAA9903605 1 19990303 A 5311 FORMER DOUG DC9 DC932 3022066 WP BS 218 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND LOWER FLANGE OF FORMER RING CRACKED AND DAMAGED AT STA 218, LONGERON 19L, AT FORMER TO L ONGERON. REPAIRED FORMER RING PER SRM 53-03, PAGE 4A, FIG 2A. 2 L 7 2 4F A6WE 1999031200592 19990312 00592 WP 1999 3 12 TWAA9903606 1 19990303 A 5753 BOLTS DOUG DC9 DC932 3022066 WP TE FLAPS RUSTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND 4 I/B AFT FLAP CASTING ATTACH BOLTS ON REAR SPAR EMITTING RUST. REPLACED STUDS AND HING E FITTING PER MM 57-40-0 AND 27-51-1. 2 L 7 2 4F A6WE 1999031200593 19990312 00593 WP 1999 3 12 AT9900178 1 19990305 A 3397 WIRE DOUG DC9 DC932 3022066 WP COCKPIT OUT OF POSITION A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 835AT 47534 EMERGENCY LIGHTING IN COCKPIT DID NOT ILLUMINATE. REPOSITIONED WIRING ON CONNECTOR IN FORWARD AISLE LIGHTING RECEPTICAL . OPERATIONAL CHECKS GOOD IAW DC9 STANDARD PRACTICES CHAPTER 20-50. 2 L 7 2 4F A6WE 1999031200594 19990312 00594 WP 1999 3 12 AT9900179 1 19990305 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 835AT 47534 EMERGENCY LIGHTING AFT CABIN CEILING BY AFT DOOR DID NOT ILLUMINATED BRIGHTLY. CHARGED BATTERIES IAW 33-53-0, OPERATION AL CHECK GOOD. 2 L 7 2 4F A6WE 1999031200595 19990312 00595 WP 1999 3 12 AT9900180 1 19990303 A 5320 1A43984 ANGLE DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK IN VERTICAL LEG OF NR 2 PYLON UPPER ATTACH ANGLE AT BS 980. STOP DRILLED CRACK, HIGH FREQUENCT EDDY CURRENT VERIFIED CRACK WAS STOP, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2, AND RES NR 99442. 2 L 7 2 4F A6WE 1999031200596 19990312 00596 NM 1999 3 12 AT9900181 1 19990306 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 350 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 467AT 22055 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FORWARD FUSELAGE AT BS 350 AFT LOWER CORNER CRACKED AT AIRSTAIR CUTOUT. S TOP DRILLED CRACK, FABRICATED REPAIR DOUBLER, TREATED, PRIMED, PAINTED, AND INSTALLED IAW B737 SRM 51-10-2, MM 51-20-11, AND AERO CORP EO 99-1094. 2 L 7 2 4F A16WE 1999031200597 19990312 00597 1999 3 12 COMA9910041 4 19990305 A 3416 51928704E2101 ALTIMETER EMB 120 EMB120RT SO LT COCKPIT LOOSE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 256CA 18694 120245 PILOTS ALTIMETER VIBRATED DURING TAKEOFF. SECURED ALTIMETER. 2 L 7 2 4T RT A31SO 1999031200598 19990312 00598 EA 1999 3 12 COMA9960099 1 19990308 A 2750 855D109 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 940CA 8357 4 7048 FLAPS FAILED AT 8 DEGREES. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999031200599 19990312 00599 EA 1999 3 12 COMA9960100 1 19990308 A 5270 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 721CA 7259 CABIN DOOR WARNING AFTER TAKEOFF. ADJUSTED DOOR WARNING PROXIMITY SWITCHES. 2 L 7 2 4F RT A21EA 1999031200601 19990312 00601 EU 1999 3 12 QXEA9900291 1 19990127 A 2560 SLIDE FOKKER F28 F28MK4000 4990810 EU CABIN MISARMED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - EMERGENCY ESCAPE SLIDE NOT PROPERLY ARMED. ARMED ESCAPE SLIDE IAW SWITLIK OVERHAUL MANUAL 25-60-156, PAGE 516. 2 L 7 2 4F RT A20EU 1999031200602 19990312 00602 1999 3 12 QXEA9900292 4 19990127 A 2565 BOTTLE FOKKER F28 F28MK4000 4990810 EU EXCAPE SLIDE LOW PRESSURE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - ESCAPE SLIDE BOTTLE PRESSURE IS LOW. REMOVED AND REPLACED ESCAPE SLIDE IAW FOKKER MM 25-60-01, PAGE 201, PARAGRAP H 2A AND 2B. 2 L 7 2 4F RT A20EU 1999031200603 19990312 00603 EU 1999 3 12 QXEA9900293 1 19990126 A 5321 FLOOR FOKKER F28 F28MK4000 4990810 EU RT COCKPIT PUNCTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CO-PILOTS FLOOR AT INBOARD SEAT TRACK HAS A PUNCTURE IN FLOOR. REPAIRED IAW HORIZON AIR EA 4-53-686. 2 L 7 2 4F RT A20EU 1999031200604 19990312 00604 EU 1999 3 12 QXEA9900458 1 19990304 A 3350 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8A FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 488US 11240 SEA - EMERGENCY EXIT LIGHT AT 8A INTERMITTENTLY FLASHES. MAINTENANCE FOUND THE GROUND PAINTED AND THEN CLEANED OFF THE PAINT. RELAMPED AND OPERATIONALLY TESTED, TEST NORMAL. 2 L 7 2 4F RT A20EU 1999031200605 19990312 00605 NM 1999 3 12 99FDEA00087 1 19990308 A 5313 BAC1498142 STRINGER BOEING 727 72725C 138400H NM BS 1166-1183 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 WHILE WORKING NR-0620 FOUND STR 22 LT, BS 1166 TO BS 1183 CORRODED AND MECHANICALLY DAMAGED. *S/D* REMOVED AND REPLACE D STR 22 LT. 2 L 7 3 4F A3WE 1999031200606 19990312 00606 NM 1999 3 12 99FDEA00088 1 19990308 A 5330 6518420200 SKIN BOEING 727 72722C 138400F NM BS 234 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 PILLOWING SKIN AND DISHED RIVET HEADS BS 234, STR 23R AND 24R, (CORROSION C53-100-01). 2 L 7 3 4F A3WE 1999031200607 19990312 00607 WP 1999 3 12 99FDEA00089 1 19990305 A 2497 AJP9001506 WIRE DOUG DC10 DC1030F 3023504 WP BS 2007 MELTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 312FE 48300 APU GENERATOR FEEDER CABLE SHORTING OUT WHERE IT PASSES THRU BS 2007 - PRESSURE BULK HEAD. REMOVD AND REPLACED C PHASE CABLE AND THE PRESSURE SEAL FITTING ASSY. 2 L 7 3 4F RT A22WE 1999031200608 19990312 00608 NM 1999 3 12 99FDEA00090 1 19990309 A 3260 SWITCH BOEING 727 72722 1384002 NM NLG DOOR INOP A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 148FE 19086 RED DOOR LIGHT ON THE LAND GEAR PNL AND NOSE GEAR DOOR LIGHT ON THE S/O ANNUNCIATOR PNL REMAIN ILLUM AFTER GEAR WAS RETR ACTED. CHECKED NOSE GEAR DOOR LOCK SWITCH FOR PROPER GAP AND STIFFNESS. NO DEFECTS NOTED. ALL DOOR SWITCH OPS CK GOOD . REF M/M 32-62-11. 2 L 7 3 4F A3WE 1999031200609 19990312 00609 WP 1999 3 12 RRXA99132 1 19990305 A 2550 NET DOUG DC8 DC873F 302199F WP CARGO DOORWAY OUT OF POSITION A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 831AL 46146 UNABLE TO PRESSURIZE AIRCRAFT AT 14,000 FEET AIRCRAFT CABIN CLIMBING AT 1100 FEET PER MINUTE BOTH PAX MAX FLOW AND MAX T EMP. DUMPED 18,000 LBS OF FUEL AND RETURNED TO KDAY. FOUND CARGO NET STRAP/BUCKLE ASSY HANGING FROM ACFT WITH DOOR CLO SED CAUSING GAP BETWEEN DOOR AND FUSELAGE. STOWED STRAP, CLOSED DOOR AND PRESSURIZED ACFT. LEAK CHECK AT PIT DOOR AND MAIN CARGO DOOR GOOD. NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 1999031200610 19990312 00610 NM 1999 3 12 VNAA9903007 1 19990306 A 3350 321473 PWR SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7LK FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 458PS 67508 84 3068 DURING THE PREFLIGHT INSPECTION, A STRIP OF EMERGENCY FLOOR LIGHTING WAS NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY AT THE 7LK POSITION, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. O PERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999031200611 19990312 00611 NM 1999 3 12 VNAA9903009 1 19990307 A 7603 001A761A1010106 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COND LEVER FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 328LS 94009 3025 A NOSE WHEEL FAIL WARNING INDICATION WAS NOTED ON THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND CONDITION LEVER MICRO SWITCH ASSEMBLY, IN ACCORDANCE WITH DORNIER MAINTNENANCE MANUAL 76-11-05. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANC E. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999031200612 19990312 00612 NM 1999 3 12 SWAA990425 1 19990301 A 7331 WL203EED8 INDICATOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 FUEL FLOW FAULTY A SWAA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 341SW 24091 NR 1 FUEL FLOW INDICATOR DROPPED TO ZERO ON TAKEOFF ROLL, ALL OTHER ENG INDICATIONS NORMAL. RETURNED TO NORMAL FUEL FLO W INDICATION DURING ROTATION. REPLACED THE NR 1 FUEL FLOW INDICATOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200613 19990312 00613 NM 1999 3 12 SWAA990426 1 19990301 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 063SW 22061 DURING SERVICE CHECK, FOUND CABIN OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999031200614 19990312 00614 NM 1999 3 12 SWAA990427 1 19990301 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 24 NOT SECURED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 634SW 27937 DURING SCHEDULED BC3 CHECK, FOUND EGRESS LIGHTS BY SEAT ROW 24 NOT SECURED TO FLOOR. SECURED LIGHTS TO FLOOR PER MM. 2 L 7 2 4F RT A16WE 1999031200615 19990312 00615 NM 1999 3 12 SWAA990428 1 19990301 A 1100 BAC29PPS14952 PLACARD BOEING 737 7377H4 NM SRVICE DOOR PEELING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 740SW 29276 DURING SCHEDULED CI CHECK, FOUND FWD SERVICE DOOR ESCAPE SLIDE ARMED PLACARD PEELING. REPLACED PLACARD PER MM. 2 L 7 2 4F RT A16WE 1999031200616 19990312 00616 NM 1999 3 12 SWAA990429 1 19990302 A 3350 079123 COVER BOEING 737 7372H4 138448C NM ROW 8 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 FLOOR TRACK LIGHT COVER COMING OFF FLOOR AT ROW 8. SECURED FLOOR TRACK LIGHTING PER MM. 2 L 7 2 4F A16WE 1999031200617 19990312 00617 NM 1999 3 12 SWAA990430 1 19990302 A 2910 171K1416CR0360 LINE BOEING 737 7373H4 1384600 NM MLG WW LEAKING A SWAA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 311SW 23333 ON PUSH BACK GROUND CREW NOTICED SMOKE COMING FROM WHEEL WELL. TIGHTENED B NUT ABOVE SHUTTLE VALVE, ABOVE FLAP ACTUATOR . THEN SECOND PUSHBACK WITH B PUMPS ON AND BRAKE SET, THE SMOKE REAPPEARED. REPLACED LINE BETWEEN BRAKE MEETING VALVE AND BRAKE SHUTTLE VALVE PER MM. 2 L 7 2 4F RT A16WE 1999031200618 19990312 00618 NM 1999 3 12 SWAA990431 1 19990302 A 3350 P4010021 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 326SW 23690 FWD I/B FLASHLIGHT TEST LIGHT NOT FLASHING. REPLACED BATTERY ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031200619 19990312 00619 1999 3 12 SWAA990432 4 19990302 A 2565 65C31843 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DISENGAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 FORWARD ENTRY ESCAPE SLIDE FELL OUT WHILE TRYING TO CLOSE DOOR FOR DEPARTURE. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031200620 19990312 00620 NM 1999 3 12 SWAA990433 1 19990302 A 3350 BR2013 CONNECTOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE CABIN DIRTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 390SW 26593 DURING SERVICE CHECK CHECK, FOUND FLOOR TRACK LIGHTING OUT ON MID CABIN. CLEANED AND RESEATED SOCKET CONNECTORS PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200621 19990312 00621 NM 1999 3 12 SWAA990434 1 19990302 A 2560 6945143 WINDOW BOEING 737 7373L9 1384470 NM PAX DOOR SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SPECIAL VISIT CHECK, FOUND FWD ENTRY DOOR SLIDE PACK WINDOW CRACKED. REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 1999031200622 19990312 00622 NM 1999 3 12 SWAA990435 1 19990301 A 5312 6546568 BULKHEAD BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CORROSION ON PRESSURE BULKHEAD LOWER CENTRAL WEB BS 1016, WL 190. REPAIRED PER SWA ER N R 99-0094 AND BOEING DRAWING 65C28106. 2 L 7 2 4F A16WE 1999031200623 19990312 00623 NM 1999 3 12 SWAA990436 1 19990301 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 986 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER HINGE CUT OUT. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999031200624 19990312 00624 NM 1999 3 12 SWAA990437 1 19990301 A 5312 6516300 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND CRACK THRU EDDY CURRENT INSPECTION AT BULKHEAD FWD WEB BS 178, RBL 10, WL 234. REPAI RED PER SRM. 2 L 7 2 4F RT A16WE 1999031200625 19990312 00625 NM 1999 3 12 SWAA990438 1 19990301 A 5512 6573782 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB LOWER SURFACE SKIN CRACKED FWD OF REAR SPAR, (CRACK APPROX 2 LONG). REP AIRED STAB PER SWA ER NR 99-0169, AND SRM. 2 L 7 2 4F RT A16WE 1999031200626 19990312 00626 NM 1999 3 12 SWAA990439 1 19990301 A 5312 6516300 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2 D-CHECK, FOUND 4 CRACKS AT BULKHEAD WEB BS 178, RBL 7 WL 201, WL 213 AND RBL 5, WL 213, WL 198. RE PAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200627 19990312 00627 NM 1999 3 12 SWAA990440 1 19990301 A 5315 141A5170 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 294.5, RBL 20-RBL 57. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999031200628 19990312 00628 NM 1999 3 12 SWAA990441 1 19990301 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 664 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT STA 664, LBL 32. REPAIRED PER SWA RA NR 1-353-2029. 2 L 7 2 4F RT A16WE 1999031200629 19990312 00629 NM 1999 3 12 SWAA990454 1 19990304 A 3350 101078101 LIGHT BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 693SW 23174 EMERGENCY EXIT ROW LIGHT (RT SIDE) IN OVERHEAD LUGGAGE BIN LOOSE. RESECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999031200630 19990312 00630 NE 1999 3 12 SWAA990455 2 19990304 A 7230 9732M10P18 BEARING BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE LEAKING A SWAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 384SW 26590 857874 AIR TURNBACK DUE TO CABIN FILLED WITH SMOKE AFTER TAKEOFF. FOUND NR 3 BEARING LEAKING OIL ON NR 2 ENGINE. REMOVED AND REPLACED ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200631 19990312 00631 NM 1999 3 12 SWAA990456 1 19990305 A 2612 693730752 FIRE LOOP BOEING 737 7372H4 138448C NM NR 1 ENGINE SHORTED A SWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 07 080SW 22675 AIR TURNBACK, NR 1 ENG OVERHEAT LIGHT CAME ON DURING CLIMB. SHUT ENGINE DOWN AND RETURNED TO HOU. WHEN RETARDED NR 1 E NG ALL PARAMETERS REMAINED THE SAME (DID NOT LOWER). DISCHARGED LT AND RT BOTTLES. FOUND LOWER FIRE ELEMENT SHORTED OU T. REMOVED AND REPLACED LOWER LOOP PER MM. 2 L 7 2 4F A16WE 1999031200632 19990312 00632 NM 1999 3 12 SWAA990457 1 19990304 A 1100 65C19696 PLACARD BOEING 737 7372H4 138448C NM PAX DOOR DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING OVERNIGHT CHECK, FOUND EXTERIOR ESCAPE SLIDE CAUTION PLACARD AT FWD ENTRY DOOR DETERIORATED. REMOVED AND REPLACE D PLACARD PER MM. 2 L 7 2 4F A16WE 1999031200633 19990312 00633 NM 1999 3 12 SWAA990458 1 19990304 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 379 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED 1/2 D-CHECK, FOUND BROKEN STRINGER 3R AT BS 379. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200634 19990312 00634 1999 3 12 SWAA990459 4 19990305 A 2565 61323468 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DISENGAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING OVERNIGHT CHECK, FOUND FWD ENTRY DOOR SLIDE POPPED OUT OF RETAINER. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031200635 19990312 00635 NM 1999 3 12 SWAA990460 1 19990305 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM AT BS 326 BL 0. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999031200636 19990312 00636 NM 1999 3 12 SWAA990461 1 19990305 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 277 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM AT T-CAP NUT PLATE HOLES ON BS 277, LBL 30, LBL 38, AND LBL 49 . REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200637 19990312 00637 NM 1999 3 12 SWAA990462 1 19990305 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM AT BS 328 AROUND SCREW HOLES, RBL 25 TO RBL 43. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200638 19990312 00638 NM 1999 3 12 SWAA990463 1 19990305 A 5312 BULKHEAD ANGLE BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT STA 178, LBL 29, WL 207. REMOVED AND REPLACED CHORD ANGLE P ER SRM. 2 L 7 2 4F RT A16WE 1999031200639 19990312 00639 NM 1999 3 12 SWAA990464 1 19990306 A 2560 61323 SLIDE BOEING 737 7375H4 138449D NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 FWD ENTRY DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999031200640 19990312 00640 NM 1999 3 12 SWAA990465 1 19990305 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED BC4 CHECK, FOUND EGRESS LIGHT BY EMERGENCY EXIT ROW INOP. SECURED LIGHT ASSY IN TRACK PER MM. 2 L 7 2 4F RT A16WE 1999031200641 19990312 00641 NM 1999 3 12 SWAA990466 1 19990305 A 5320 65C27314 CLIP BOEING 737 7373A4 1384585 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2D CHECK, FOUND 2 STRINGER CLIPS CRACKED AT BS 663, STRINGERS 10L AND 10R. REMOVED AND REPLACED CLIP S PER SRM. 2 L 7 2 4F RT A16WE 1999031200642 19990312 00642 NM 1999 3 12 SWAA990442 1 19990303 A 7331 WL203EED8 INDICATOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 FUEL FLOW FLUCTUATES A SWAA K NONE O OTHER CR CRUISE 1 SW 07 307SW 22947 NR 1 ENG FUEL FLOW INDICATOR NEEDLE FLUCTUATES RAPIDILY AND INDICATES 7-800 PPH HIGHER THAN DIGITAL INDICATOR. REMOVED AND REPLACED FUEL FLOW INDICATOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200643 19990312 00643 1999 3 12 SWAA990453 4 19990303 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 FWD SERVICE DOOR SLIDE PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031200644 19990312 00644 NM 1999 3 12 SWAA990443 1 19990303 A 7331 WL203EEDS INDICATOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 FUEL FLOW INOP A SWAA K NONE O OTHER CR CRUISE 1 SW 07 341SW 24091 EN ROUTE, NR 2 ENG FUEL FLOW METER INDICATOR WENT INOP. REMOVED AND REPLACED FUEL FLOW METER INDICATOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200645 19990312 00645 NM 1999 3 12 SWAA990444 1 19990303 A 2560 D31591 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 FWD SERVICE DOOR SLIDE FELL OUT. SECURED BACK SLIDE ASSY ON TO DOOR PER MM. 2 L 7 2 4F RT A16WE 1999031200646 19990312 00646 NM 1999 3 12 SWAA990445 1 19990303 A 2150 39267831 VALVE BOEING 737 7373H4 1384600 NM LT PACK FAILED A SWAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 07 392SW 27379 EXTREMELY LOUD VIBRATION AT MID CABIN ACCOMPANIED BY THUMPING SOUND. FOUND LT TURBO FAN VALVE FAILED OPEN. SWAPPED LT AND RT TURBO FAN VALVES PER MM. OPS CHECK GOOD. NO VIBRATIONS OR OTHER IRREGULARITIES NOTED. 2 L 7 2 4F RT A16WE 1999031200647 19990312 00647 1999 3 12 SWAA990446 4 19990303 A 2565 22DD229131 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR PRESS LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING OVRNIGHT CHECK, FOUND L-1 DOOR EVAC SLIDE LOW AT 2700 PSI. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F A16WE 1999031200648 19990312 00648 NM 1999 3 12 SWAA990447 1 19990303 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 19-21 INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 646SW 28331 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 19 TO 21. RESPLICED CONNECTORS PER MM . 2 L 7 2 4F RT A16WE 1999031200649 19990312 00649 NM 1999 3 12 SWAA990448 1 19990303 A 2560 22D22900131 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 090SW 22905 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY AND SERVICE DOOR SLIDE PACK GAGES OUT OF VIEW. REPOSITIONED SLIDES PACKS PER MM. 2 L 7 2 4F A16WE 1999031200650 19990312 00650 NM 1999 3 12 SWAA990449 1 19990303 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM BS 350 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CORROSION ON STR 24R (BOTH SIDES), BS 350. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999031200651 19990312 00651 NE 1999 3 12 SWAA990450 2 19990303 A 7230 9527M99P11 BLADE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 7224004 DURING SCHEDULED C3 CHECK, FOUND RT ENGINE NR 31 FAN BLADE HAS DENT AT MIDSPAN FILLET RADIUS. REMOVED AND REPLACED NR 3 1 FAN BLADE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200652 19990312 00652 NM 1999 3 12 SWAA990451 1 19990303 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 340 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2D CHECK, FOUND CRACK IN SKIN AFT LWR CORNER OF FWD SERVICE DOOR CUTOUT. HFEC INSPECTION VERIFIED. R EPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200653 19990312 00653 NM 1999 3 12 SWAA990452 1 19990303 A 5312 6516300 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2D CHECK, FOUND THRU NDT INSPECTION 2 CRACKS ON PRESS BULKHEAD WEB AT BS 178, LBL 5 AT WL 211.5 AND 2 01 (CRACKS ARE APPROX 1.5 INCHES LONG). REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031200654 19990312 00654 NM 1999 3 12 SWAA990467 1 19990305 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505SW 24182 ESCAPE PATH LIGHTING HAS EXPOSED WIRES AT MID CABIN. RESECURED TRACK LIGHTING COVER PER MM. 2 L 7 2 4F RT A16WE 1999031200655 19990312 00655 NM 1999 3 12 SWAA990468 1 19990308 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 609SW 27929 ESCAPE PATH LIGHTING HAS EXPOSED WIRES AT MID CABIN. RESECURED TRACK LIGHTING COVER PER MM. 2 L 7 2 4F RT A16WE 1999031200656 19990312 00656 NM 1999 3 12 SWAA990469 1 19990308 A 3610 1074923 REGULATOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE INOP A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 663SW 23256 AIR TURNBACK DUE TO NR 2 ENG BLEED AIR VALVE C/B POPPED IN FLIGHT AND WOULD NOT RESET. REMOVED AND REPLACED NR 2 ENG BL EED AIR REGULATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200657 19990312 00657 1999 3 12 SWAA990470 4 19990306 A 2565 D31354418 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR PRESS LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 AFT ENTRY DOOR SLIDE HAS LOW PRESSURE. REMOVED AND REPLACED AFT ENTRY DOOR SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999031200658 19990312 00658 NM 1999 3 12 SWAA990471 1 19990306 A 7331 WL203EED11 INDICATOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 FUEL FLOW MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 NR 2 FUEL FLOW INDICATOR SPORADIC, RUNS TO ZERO AND BACK UP. REMOVED AND REPLACED FUEL FLOW INDICATOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031200659 19990312 00659 NM 1999 3 12 SWAA990472 1 19990307 A 5320 1D1331001 CHORD BOEING 737 7373H4 1384600 NM BS 180 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND T-CHORD CRACKED AT BS 180, RBL 25, WL 207. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999031200660 19990312 00660 NM 1999 3 12 SWAA990473 1 19990307 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND APPROXIMATE A 2.5 INCH CRACK IN FUSELAGE SKIN ON AFT LOWER CORNER OF FWD SERVICE DOOR CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999031200661 19990312 00661 NM 1999 3 12 SWAA990474 1 19990306 A 5312 6516300 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION 2 CRACKS AT BS 178 BULKHEAD WEB, LBL AND RBL 1, WL 187. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 1999031200662 19990312 00662 1999 3 12 SWAA990475 4 19990306 A 2210 D43387J CONNECTOR BOEING 737 7373H4 1384600 NM BS 1080 SHORTED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 331SW 23695 AIR TURNBACK DUE TO AIRCRAFT YAWED IN FLIGHT. YAW DAMPER INDICATION FULL SCALE LEFT. AIRCRAFT SENT TO DALFORT AND REPA IRED INTERMITTENT SHORT AT CANNON PLUG LOCATED AT BS 1080. OPS CHECKED SYSTEM PER SWA ACO 6960-22. 2 L 7 2 4F RT A16WE 1999031200688 19990312 00688 WP 1999 3 12 99T64R017 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 560 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT WING LEADING EDGE PANEL AF TNR 1 PYLON SURFACE CORROSION WS 560 TOP OF WING. REMOVED CORROSION, FABRICATED DOUBLER S AND INSTALLED PER EO DRAWING NR 98-028 ON 8110-3 DATED 10/30/98 UNDER W/O 1310. (M) 2 L 7 4 4F 4A25 1999031200689 19990312 00689 WP 1999 3 12 99T64R018 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 260 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT WING CORROSION AT SEAM OF LEADING EDGE AFT NR 2 PYLON WS 260 TOP OF WING BETWEEN XFS 291.5 AND 304. REMOVED CORROS ION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-040 ON 8110-3 DATED 11/18/98 UNDER WO 1310. (M) 2 L 7 4 4F 4A25 1999031200690 19990312 00690 WP 1999 3 12 99T64R019 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 250 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT WING LEADING EDGE CORROSION AT SCREW OUTBOARD NR 2 PYLON APPROX WS 250 TOP OF WING XFS 335.25. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-039 ON 8110-3, DATED 11/12/98 UNDER WO NR 1310. (M) 2 L 7 4 4F 4A25 1999031200691 19990312 00691 WP 1999 3 12 99T64R020 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 240.126 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT WING LEADING EDGE UPPER SURFACE PANEL HAS .5 INCH CRACK BEHIND NR 3 SLOT AND SMALL BULGE XFS 240.126. REMOVED COR ROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-030 ON 8110-3 DATED 10/30/98 UNDER WO 1310. (M) 2 L 7 4 4F 4A25 1999031200692 19990312 00692 WP 1999 3 12 99T64R021 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 250 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT WING LEADING EDGE CORRODED AT FASTENER HOLE AFT OF INBOARD SLOT DOOR APPROX WS 250. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-029 ON 8110-3 DATED 10/30/98 UNDER WO 1309. (M) 2 L 7 4 4F 4A25 1999031200693 19990312 00693 WP 1999 3 12 99T64R022 1 19990107 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1400 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 AFT ACCESSORY COMPARTMENT RIGHT LONERON 24 AT STATION 1400 HAS .875 INCH CRACK IN RADIUS. FABRICATED REPAIR CHANNEL AND INSTALLED PER EO DRAWING NR 98-024 ON 8110-3 DATED 10/22/98 UNDER WO 1310. (M) 2 L 7 4 4F 4A25 1999031200694 19990312 00694 WP 1999 3 12 99T64R023 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 220.19 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 NR 3 STUBWING INBOARD TOP TRAILING EDGE STATION XS 220.190 CORROSION BEYOND LIMITS. REMOVED CORROSION, FABRICATED DOUBL ERS AND INSTALLED PER EO DRAWING NR 98-030 ON 8110-3 DATED 10/30/98 UNDER WO 1309. (M) 2 L 7 4 4F 4A25 1999031200695 19990312 00695 WP 1999 3 12 99T64R024 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 213 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 NR 3 STUBWING FORWARD AND INBOARD SLOT WS XS 213 CORROSION REMOVAL BEYOND LIMITS. REMOVED CORROSION, FABRICATED DOUBLER S AND INSTALLED PER EO DRAWING NR 98-031 ON 8110-3 DATED 10/31/98 UNDER WO 1309. (M) 2 L 7 4 4F 4A25 1999031200696 19990312 00696 WP 1999 3 12 99T64R025 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 422.75 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT WING LEADING EDGE HAS CORROSION ON BOTTOM SKIN TRAILING EDGE APPROX WING STATION XFS 422.750. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-038 ON 8110-3 DATED 11/12/98 UNDER WO 1310. (M) 2 L 7 4 4F 4A25 1999031200697 19990312 00697 WP 1999 3 12 99T64R026 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 341.5 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT WING LEADING EDGE HAS CORROSION ON BOTTOM SKIN TRAILING EDGE AT WING STATION XFS 341.5. REMOVED CORROSION, FABRIC ATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-038 ON 8110-3 DATED 11/12/98 UNDER WO 1310. (M) 2 L 7 4 4F 4A25 1999031200698 19990312 00698 WP 1999 3 12 99T64R027 1 19990107 A 5320 573113502N FITTING DOUG DC8 DC862 3021970 WP BS 879 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 W/W RIGHT VERTICAL FITTING FROM LONGERON 24 TO FLOORBEAM AT 879 IS CORRODED. REPLACED FITTING PER 51-1-20 AND EO DRAWIN G NR 98-032 ON 8110-3 DATED 11/01/98 UNDER WO 1300. (M) 2 L 7 4 4F 4A25 1999031200699 19990312 00699 WP 1999 3 12 99T64R028 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP NR 4 STUB WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 FOUND CORROSION AT SCREW HOLES NR 4 STUBWING UPPER SURFACE. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-049 ON 8110-3 DATED 11/17/98 UNDER WO 1347. (M) 2 L 7 4 4F 4A25 1999031200700 19990312 00700 WP 1999 3 12 99T64R029 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT WING FIRST LEADING EDGE SECTION OUTBOARD NR 1 PYLON HAS CORROSION AT FASTENER HOLES MOST INBOARD AFT XFS 578.750. R EMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-035 ON 8110-3 DATED 11/09/98 UNDER WO 1347. (M ) 2 L 7 4 4F 4A25 1999031200701 19990312 00701 WP 1999 3 12 99T64R030 1 19990107 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 759 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 FOUND A 4.5 INCH CRACK IN FUSELAGE FRAME STATION 759 BETWEEN RL 17 AND 18. STOP DRILL CRACK, FABRICATED DOUBLERS AND IN STALLED PER EO DRAWING NR 98-055 ON 8110-3 DATED 12/03/98 UNDER WO NR 1347. (M) 2 L 7 4 4F 4A25 1999031200702 19990312 00702 WP 1999 3 12 99T64R031 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT WING OUTBOARD END AT LEADING EDGE CORROSION ATTACH HOLE AND FOUND CRACK SAME AREA. REMOVED CORROSION PER SRM 51-1- 8 AND INSTALLED DOUBLER PER SRM 57-2-1. (M) 2 L 7 4 4F 4A25 1999031200703 19990312 00703 WP 1999 3 12 99T64R034 1 19990107 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 46070 LEFT HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS EXFOLIATED CORROSION AROUND ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED PER EO DRAWING NR 98-047 ON 8110-3 DATED 11/16/98 UNDER WOR 1308. (M) 2 L 7 4 4F 4A25 1999031200704 19990312 00704 WP 1999 3 12 99T64R033 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT WING LEADING EDGE SECTION BETWEEN 3 AND 4 PYLONS CORROSION AT FASTENER ATTACH HOLES CENTER OF LEADING EDGE UPPER S URFACE. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-037 ON 8110-3 DATED 11/12/98 UNDER WO 1347. (M) 2 L 7 4 4F 4A25 1999031200705 19990312 00705 WP 1999 3 12 99T64R032 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT WING LEADING EDGE 2ND SECTION OUTBOARD NR 4 PYLON CORROSION AT FASTENER ATTACH HOLES UPPER SURFACE. REMOVED CORRO SION, FABRICATED DOUBLER AND INSTALLED PER EO DRAWING NR 98-054 ON 8110-3 DATED 11/23/98 UNDER WO 1347. (M) 2 L 7 4 4F 4A25 1999031200706 19990312 00706 WP 1999 3 12 99T64R035 1 19990107 A 5311 FRAME DOUG DC8 DC8F55 3021928 WP BS 173 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 45764 FOUND CORROSION LEFT SIDE END OF FLOORBEAM AND ATTACH ANGLE UNDER FLOOR STATION 173. REMOVED CORROSION, FABRICATED DOUB LERS AND INSTALLED PER EO DRAWING NR 99-001 ON 8110-3 DATED 01/01/99 UNDER WORK ORDER NR 1360. (M) 2 L 7 4 4F 4A25 1999031200707 19990312 00707 WP 1999 3 12 99T64R003 1 19990107 A 5400 NUT PLATE DOUG DC8 DC862 3021970 WP NR 3 PYLON STRIPPED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 NR 3 PYLON REMOVEABLE PLANK HAS 5 SCREWS THAT WILL NOT TORQUE. OPENED HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-026 ON 8110-3 DATED 10/27/98 UNDER WO NR 1308. (M) 2 L 7 4 4F 4A25 1999031200708 19990312 00708 WP 1999 3 12 99T64R002 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT WING CENTER LEADING EDGE CRACKED ON OUTSIDE SEVERAL PLACES. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-036 ON 8110-3 DATED 11/09/98 UNDER WO NR 1308. (M) 2 L 7 4 4F 4A25 1999031200709 19990312 00709 WP 1999 3 12 99T64R001 1 19990107 A 5241 SKIN DOUG DC8 DC862 3021970 WP R2 DOOR CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 STRIKE PLATE BULGING AROUND RIVETS AFT GALLEY DOOR R2. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAW ING NR 98-019 ON 8110-3 DATED 10/09/98 UNDER WO NR 1309. (M) 2 L 7 4 4F 4A25 1999031200710 19990312 00710 WP 1999 3 12 99T64R004 1 19990107 A 5400 NUT PLATE DOUG DC8 DC862 3021970 WP NR 2 PYLON LOOSE/MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 71377 46070 NR 2 PYLON REMOVEABLE PLANK HAS ONE NUT PLATE MISSING AND ONE NUT PLATE LOOSE. OPENED HOLES TO .260 DIAMETER AND INSTAL LED NAS 1670 PER EO DRAWING NR 98-026 ON 8110-3 DATED 10/27/98 UNDER WO NR 1308. (M) 2 L 7 4 4F 4A25 1999031200711 19990312 00711 WP 1999 3 12 99T64R005 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 697-885 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT WING LEADING EDGE FROM XRS 697 TO XRS 885 HAS SCREW HEADS WORKING DUE TO EXFOLIATED CORROSION UPPER SURFACE. REMO VED CORROSION FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-054 ON 8110-3 DATED 11/23/98 UNDER WO NR 1308. (M) 2 L 7 4 4F 4A25 1999031200712 19990312 00712 WP 1999 3 12 99T64R006 1 19990107 A 5512 SKIN DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT HORIZ STABILIZER OUTBOARD LEADING EDGE EXFOLIATED CORROSION TOP ATTACH SCREW HOLES. REMOVED CORROSION FABRICATED DOUBLERS AND INSTALLED PER EO NR 98-044 ON 8110-3 DATED 11/23/98 UNDER WO NR 1308. (M) 2 L 7 4 4F 4A25 1999031200713 19990312 00713 WP 1999 3 12 99T64R007 1 19990107 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS EXFOLIATED CORROSION AT TOP ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-045 ON 8110-3 DATED 11/16/98 WO NR 1308. (M) 2 L 7 4 4F 4A25 1999031200714 19990312 00714 WP 1999 3 12 99T64R008 1 19990107 A 5720 ANGLE DOUG DC8 DC862 3021970 WP BS 857 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 CENTER FUEL TANK TOP SIDE AT STATION 857 UNDER NR 4 FLOOR PANEL SURFACE CORROSION AFT TANK ANGLE. REMOVED CORROSION, FL AP PEEN BLENDED AREA PROTECT REWORKED AREA PER EO DRAWING NR 98-025 ON 8110-3 DATED 10/27/98 WO 1308. (M) 2 L 7 4 4F 4A25 1999031200715 19990312 00715 WP 1999 3 12 99T64R009 1 19990107 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 400-420 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 FOUND STATION 400-420 STRINGER 19R LOWER FLANGE REMOVED. INSTALLED REPAIR CHANNEL PER EO DRAWING NR 98-056 ON 8110-3 DA TED 12/04/98 UNDER WO 1347. (M) 2 L 7 4 4F 4A25 1999031200716 19990312 00716 WP 1999 3 12 99T64R010 1 19990107 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 LEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS EXFOLIATED CORROSION AT BOTTOM ATTACH SCREW HOLES. REMOVED CORROSI ON, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-046 ON 8110-3 DATED 11/17/98 UNDER WO 1308. (M) 2 L 7 4 4F 4A25 1999031200717 19990312 00717 WP 1999 3 12 99T64R011 1 19990107 A 5720 NUT PLATE DOUG DC8 DC862 3021970 WP LT WING MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 MISSING FASTENERS LEFT WING LEADING EDGE SECTION. OPEN HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-057 ON 8110-3 DATED 12/13/98 UNDER WO 1308. (M) 2 L 7 4 4F 4A25 1999031200718 19990312 00718 WP 1999 3 12 99T64R012 1 19990107 A 5720 NUT PLATE DOUG DC8 DC862 3021970 WP RT WING MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 MISSING FASTENERS RIGHT WING LEADING EDGE. OPENED HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-05 8 ON 8110-3 DATED 12/13/98 UNDER WO NR 1308. (M) 2 L 7 4 4F 4A25 1999031200719 19990312 00719 WP 1999 3 12 99T64R013 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 520.168 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 SKIN BULGED RIGHT WING CENTER SECTION UPPER SURFACE INBOARD OF OUTBOARD SLOT XFS 520 .168. REMOVED CORROSION, FABRICATE D DOUBLERS AND INSTALLED PER EO DRAWING NR 98-037 ON 8110-3 DATED 11/12/98 UNDER WO 1309. (M) 2 L 7 4 4F 4A25 1999031200720 19990312 00720 WP 1999 3 12 99T64R014 1 19990107 A 5720 36410042N FITTING DOUG DC8 DC862 3021970 WP RT MLG WW CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 RIGHT W/W LONGERON FITTING STATION 920 CORRODED ABOVE LANDING GEAR UPLOCK CYLINDER. REMOVED CORRODED FITTING AND REPLAC ED WITH NEW FITTING PER SRM 57-3-2 AND SRM 51-1-20 UNDER WO NR 1310. (M) 2 L 7 4 4F 4A25 1999031200721 19990312 00721 WP 1999 3 12 99T64R015 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 710-880 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 FOUND LEFT WING OUTBOARD LEADING EDGE PANEL RUSTY FASTENERS WS 710-880 TOP OF WING. FOUND CORROSION IN SCREW HOLES, REM OVED CORROSION. FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-027 ON 8110-3 DATED 10/29/98 UNDER WO NR 1309. ( M) 2 L 7 4 4F 4A25 1999031200722 19990312 00722 WP 1999 3 12 99T64R016 1 19990107 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 580 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8969U 61377 46070 FOUND LEFT WING LEADING EDGE PANEL OUTBOARD NR 1 PYLON WS 580 TOP OF WING SURFACE CORROSION XFS 641.250. REMOVED CORROS ION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-035 ON 8110-3 DATED 11/09/98 UNDER WO NR 1309. (M) 2 L 7 4 4F 4A25 1999031200723 19990312 00723 WP 1999 3 12 USAAD99026 1 19990212 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 928VJ 48131 IND - THE RIGHT NACELLE SCAN LIGHT AND THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACE D THE BATTERIES FOR THE RIGHT NACELLE SCAN AND FORWARD OVERWING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999031200724 19990312 00724 WP 1999 3 12 99ZZZM167 1 19990212 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 928VJ 48131 IND - THE RIGHT NACELLE SCAN LIGHT AND THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACE D THE BATTERIES FOR THE RIGHT NACELLE SCAN AND FORWARD OVERWING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999031200725 19990312 00725 WP 1999 3 12 USAAD99028 1 19990207 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913VJ 45846 DTW - THE GALLEY SERVICE DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE BATTERY FOR THE GALLEY SERVICE DO OR SLIDE EMERGENCY LIGHT. (M) 2 L 7 2 4F A6WE 1999031200726 19990312 00726 WP 1999 3 12 USAAD99027 1 19990215 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 933VJ 47216 IND - THE FORWARD ENTRY DOOR, SERVICE DOOR, AND TAILCONE SLIDE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR, SERVICE DOOR, AND TAILCONE SLIDE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999031200727 19990312 00727 NM 1999 3 12 USAA029909 1 19990217 A 3350 1000679 LIGHT GRIMES BOEING 727 727227 1384078 NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924TS TS1756 21041 FLT 6141 - BOS-LGA - FOUND ON POST FLIGHT INSPECTION, COCKPIT EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH WHEN EMERGENCY EX IT LIGHTS DISARMED. RESEATED LIGHT ASSEMBLY, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999031200728 19990312 00728 NM 1999 3 12 USAA029908 1 19990213 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM EMERGENCY EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 15600 21244 FLT 6141 - BOS-LGA - FOUND ON L/S, EXIT SIGN AT AISLE OVERWING INOPERATIVE. REPALCED BATTERY PACK, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999031200729 19990312 00729 NM 1999 3 12 USAA029907 1 19990212 A 3350 90052 CHARGER BOEING 727 727227 1384078 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS WA8049 21244 FLT 6181 - BOS-LGA - FOUND L/S, RIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK O K. (M) 2 L 7 3 4F A3WE 1999031200730 19990312 00730 NM 1999 3 12 USAASB99036 1 19990211 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 428US 24550 ORD - MAINTENANCE FOUND THE MID AND AFT CABIN EMERGENCY EXIT LIGHTS CONTROLLED BY BATTERY CHARGER M1136 INOPERATIVE. MA INTENANCE FOUND THE BATTERY CHARGER ASSEMBLY FAILED. REMOVED AND REPLACED THE M1136 BATTERY CHARGER ASSEMBLY. SYSTEM O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999031200731 19990312 00731 NM 1999 3 12 USAASB99034 1 19990209 A 3350 10604502 RELAY BOEING 737 737201 1384454 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 MEM - DURING PREFLIGHT, CREW FOUND THE SEAT LEVEL ESCAPE PATH EMERGENCY LIGHTS, THE CABIN DOOR LOWER EMERGENCY EXIT LIGH TS INOPERATIVE. MAINTENANCE TROUBLESHOT WIRING PROBLEM TO THE R121 RELAY ON THE J5 PANEL PER WIRING DIAGRAM MANUAL 33-2 1-11. REPLACED R121 RALAY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999031200732 19990312 00732 NM 1999 3 12 USAASB99037 1 19990214 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 350US 23553 LGA - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTER Y CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999031200733 19990312 00733 NM 1999 3 12 USAA029906 1 19990212 A 2750 SC2211 SCREW BOEING 727 727225 1384077 NM RT TE FLAP MISSING A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 919TS 20447 FLT 6161 - LGA-BOS - OUTBOARD FLAPS STUCK BETWEEN 2 DEGREES AND 5 DEGREES ON RETRACTION. THEN THE OUTBOARD FLAPS WOULD NOT EXTEND BEYOND FLAPS 15 DEGREE POSITION. EMERGENCY DECLARED. AIR RETURNED TO LGA. FOUND INBOARD TORQUE TUBE DISCON NECTED ON THE RIGHT OUTBOARD FLAP. RECONNECTED SAME AND REPLACED COUPLING SCREWS AND RIGGED FLAPS PER MM 27-51-0. OPER ATIONAL CHECKS OK. (M) 2 L 7 3 4F A3WE 1999031200734 19990312 00734 WP 1999 3 12 USAAD99019 1 19990204 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP ROW 19-21 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 987VJ 47210 IND - THE CEILING EMERGENCY LIGHTS AT ROWS 19 THROUGH 21 AND THE EMERGENCY LIGHTS ABOVE THE AFT FLIGHT ATTENDANT SEAT WE RE INOPERATIVE. (M) 2 L 7 2 4F A6WE 1999031200735 19990312 00735 WP 1999 3 12 USAAD99023 1 19990208 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913VJ 45846 DTW - THE GALLEY DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE GALLEY DOOR SLIDE EMERGENCY LIGHT BATTERY . (M) 2 L 7 2 4F A6WE 1999031200736 19990312 00736 WP 1999 3 12 USAAD99024 1 19990208 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 983VJ 48159 IND - THE GALLEY DOOR SLIDE EMERGENCY LGIHT WAS INOPERATIVE. MAINTENANCE REPLACED THE GALLEY DOOR SLIDE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999031200737 19990312 00737 NM 1999 3 12 USAA990081 1 19990210 A 5330 SKIN BOEING 737 737301 1384611 NM BS 375 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 35732 23936 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 2.125 INCH CRACK IN THE SKIN 1 INCH AFT OF THE EQUIPMENT COOLING EXHAUS T BL 0 AND BS 375. REPAIRED PER TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 1999031200738 19990312 00738 NM 1999 3 12 USAASB99027 1 19990203 A 2121 65771 FAN BOEING 737 7374B7 1384702 NM E/E COMPT FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 426US 33981 24548 PIT - FL 1674 - 30 MILES OUT FROM PIT, THE AFT FLIGHT ATTENDANTS COMPLAINED OF A VERY STRONG ELECTRICAL ODOR IN THE REAR OF THE AIRCRAFT. NO VISIBLE SMOKE WAS NOTED. CREW WAS NOTIFIED AND REQUESTED PRIORITY HANDLING FROM ATC. AN EMERGENC Y WAS DECLARED. EMERGENCY EQUIPMENT MET THE AIRCRAFT UPON LANDING AND CAPTAIN ADVISED PASSENGERS OF PROBLEM. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER AND PASSENGERS DEPLANED NORMALLY WITHOUT INCIDENT. MAINTENANCE FOUND THE NORMAL EQU IPMENT COOLING FAN CAUSING THE HOT ELECTRICAL SMELL IN THE CABIN. REMOVED AND REPLACED THE NORMAL EQUIPMENT COOLING FAN PER MM 21-58-12. OPERATIONAL CHECK GOOD. ALTERNATE FAN OPERATINOAL CHECK GOOD ALSO. (M) 2 L 7 2 4F RT A16WE 1999031200739 19990312 00739 NM 1999 3 12 USAASB99035 1 19990209 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 525AU 23860 LGA - MAINTENANCE FOUND THE LEFT MID AISLE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999031200740 19990312 00740 NM 1999 3 12 99ZZZM168 1 19990209 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 525AU 23860 LGA - MAINTENANCE FOUND THE LEFT MID AISLE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999031200741 19990312 00741 WP 1999 3 12 99T64R063AR 1 19990205 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 119 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 802BN 45909 FUSELAGE LONGERON 25L FRAME 119L FINGER DOUBLER AT FLOORBEAM COCKPIT SUB FLOOR CORROSION EXFOLIATION. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND INSTALLED PER EO DRAWING NR 99-006 WITH 8110-3 DATED 0/21/9 9. (M) 2 L 7 4 4F 4A25 1999031200742 19990312 00742 WP 1999 3 12 99T64R062AR 1 19990202 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 148 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 802BN 45909 FUSELAGE STATION 148 LEFT SIDE FUSELAGE SUB FLOOR FRAME ATTACH ANGLE CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANG LE, AND INSTALLED PER EO DRAWING NR 99-009 AND 8110-3 DATED 01/12/99. (M) 2 L 7 4 4F 4A25 1999031200743 19990312 00743 EU 1999 3 12 REXA99003 1 19990119 A 5321 FLOOR SAAB SF340 SF340A 7850100 EU CABIN DAMAGED A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 112PX 340A025 COCKPIT FLOOR ENTRY WAY DAMAGED. REPAIRED BY FABRICATING AN ANGLE FROM 2024T3 .040 IAW SRM. (M) 2 L 7 2 4T RT A52EU 1999031200744 19990312 00744 EU 1999 3 12 REXA99002 1 19990121 A 3320 AL5113 CONNECTOR SAAB SF340 SF340A 7850100 EU ROW 3A FAILED A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 402BH 340A058 SPARK AND SMOKE CAME FROM WINDOW LIGHT OVER SEAT 3A. REMOVED AND REPLACED TWO BULB CONNECTORS. (M) 2 L 7 2 4T RT A52EU 1999031200746 19990312 00746 NM 1999 3 12 P2EA99075 1 19990206 A 2760 HANDLE BOEING 737 737222 1384473 NM SPEED BRAKE OUT OF POSITION A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 603DJ 19955 FLT - 612 - MYR - TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, FLAPS 1, TRIM 5.4. CREW REPORTS, ABORTED AT 40 KNOTS. F OUND SPEED BRAKE HANDLE OUT OF DETENT. CYCLED SEVERAL TIMES, OPS CHECKED OK PER MM 31-26-0. (M) 2 L 7 2 4F A16WE 1999031200747 19990312 00747 NM 1999 3 12 P2EA99074 1 19990106 A 5312 BULKHEAD SKIN BOEING 737 737222 1384473 NM BS 178 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - FORWARD PRESSURE BULKHEAD SKIN CRACKED AT BS 178. REPAIRED FORWARD PRESSURE BULKHEAD WEB AT BS 178 BETWEEN LBL 5. 7 TO LBL 15.5 WL 231 TO 238.5, BETWEEN RBL 5.7 TO RBL 16 WL 231 TO WL 238.5, BETWEEN RBL 4.5 TO RBL 18.25, WL 216.3 TO W L 224.5 AND BETWEEN LBL 18 TO RBL 24 WL 213 TO WL 257 PER COOPESA EO COO-3-53-019-99 DATED JAN 28, 1999 AND BOEING FAXES COO-SJO-990052RR DATED 1-20-99 AND COO-SJO-99-0109RR DATED JAN 27 1999. (M) 2 L 7 2 4F A16WE 1999031200748 19990312 00748 NM 1999 3 12 P2EA99073 1 19990125 A 5330 SKIN BOEING 737 737222 1384473 NM BS 995-1008 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - PROVISIONAL REPAIR AT BS 1006, STRINGER 16 RT. REPAIRED FUSELAGE SKIN BETWEEN BS 995 AND BS 1008 FROM STRINGER 14 RT AND STRINGER 16 RT PER SRM SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999031200749 19990312 00749 NM 1999 3 12 P2EA99072 1 19990118 A 5753 6546435736 SKIN BOEING 737 737222 1384473 NM RT TE FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US BN375 19548 SJO - RIGHT WING OUTBOARD AFT FLAP DELAMINATED. DEFECT SIZE LENGTH 1 INCH. REPAIRED FLAP PER SRM 51-40-6, PAR 5 FIG 4. (M) 2 L 7 2 4F A16WE 1999031200750 19990312 00750 NM 1999 3 12 P2EA99071 1 19990108 A 5712 RIB BOEING 737 737222 1384473 NM LT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 19548 SJO - LEFT WING INBOARD MID FLAP CENTE RTRACK INBOARD/OUTBOARD SUPPORT RIBS CRACKED AT LOWR FLANGE AREA, DEFECT SIZE WL 116.5 94 INCH) RWL 119.5 (2 INCH). REPLACED CENTER TRACK ROLLER SUPPORT RIBS AT WL 116.5 AND WL 119.5 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999031200751 19990312 00751 NM 1999 3 12 P2EA99070 1 19990110 A 5220 FITTING BOEING 737 737222 1384473 NM LT EMERG EXIT CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - LEFT EMERGENCY EXIT DOOR FORWARD CENTRAL STOP CRACKED, LENGTH .187 INCH. REPLACED STOP FITTING PER SRM 51-10-1 PA GE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999031200752 19990312 00752 NM 1999 3 12 P2EA99069 1 19990118 A 7110 SKIN BOEING 737 737222 1384473 NM NR 2 ENG COWL WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 SJO - NR 2 ENGINE NOSE COWL UPPER SKIN SECTION WITH WEAR, DEFECT SIZE LENGTH 10 INCH WIDTH .5 INCH. REPAIRED NR 2 ENGIN E COWLING PER SRM 54-30-3, FIG 2. (M) 2 L 7 2 4F A16WE 1999031200753 19990312 00753 NM 1999 3 12 P2EA99068 1 19990108 A 5330 SKIN BOEING 737 737247 138448D NM BS 236-270 CANNED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - SKIN OIL CANNED BETWEEN BS 243.7 AND BS 259.5, WL 173 RIGHT SIDE. DEFECT SIZE, LENGTH 17 INCH, WIDTH 12 INCH. RE PAIRED FUSELAGE SKIN FROM BS 236 TO BS 270, BETWEEN WL 161 AND WL 181 PER COOPESA EO COO-3-53-033-99 DATED JAN 26, 1999 AND BOEING INSTRUCTINO SLIST ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1999031200754 19990312 00754 NM 1999 3 12 P2EA99067 1 19990114 A 5330 SKIN BOEING 737 737247 138448D NM PAX DOORWAY DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - PROVISIONAL REPAIR AT AFT ENTRY DOOR CUTOUT, AFT LOWER CORNER. REPAIRED FUSELAGE SKIN BETWEEN STRINGER 16 LEFT AN D STRINGER 20 LEFT PER COOPESA EO C00-3-53-014-99 DATED JAN 27, 1999 AND BOEING INSTRUCTIONS LIST ON FAA FORM 8110-3. ( M) 2 L 7 2 4F A16WE 1999031200764 19990312 00764 NM 1999 3 12 UIEA9904 1 19990206 A 2612 CARD BOEING 747 7472D7B 1384803 NM FIRE CONTROL LOOSE A UIEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 15 528MC 22472 FLT C1366 - ATO-AUH - AT APPROX 90 KNOTS, ENGINE FIRE BELL SOUNDED AND REJECTED TAKEOFF PROCEDURES ACCOMPLISHED. NO ENG INE OR APU FIRE LIGHTS 'ON'. COULD NOT SILENCE BELL USING NORMAL RESET. HIT COVER ON FIRE WARNING CONTROL MODULE AND B ELL SILENCED. DURING TROUBLESHOOTING FOUND THAT FIRE WARNING CONTROL MODULE RECEPTACLE FOR CARDS A6, A8 AND A9 WERE NOT PROPERLY SECURED. REMOVED ALL CARDS, REPAIRED RECEPTACLES AND REINSERTED CARDS FROM APU POSITION IN ENGINE POSITION A8 AND A9. OPERATIONAL CHECK NOW NORMAL. DEFERRED APU FIRE WARNING UNIT CARD ARE REPLACED. (M) 2 L 7 4 4F RT A20WE 1999031200765 19990312 00765 CE 1999 3 12 99ZZZM170 1 19990203 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG DEFECTIVE A JJBA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 01 857CA 1475 0534A UE71 RIGHT MAIN LANDING GEAR ACTUATOR INDICATOR SLOW TO ILLUMINATE DOWN AND LOCKED. TROUBLESHOOTING FOUND DEFECTIVE DOWN AND LOCKED SWITCH INSIDE ACTUATOR. REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. (M) 2 L 7 2 4T RT A24CE 1999031200766 19990312 00766 NM 1999 3 12 AALA990143 1 19990202 A 5711 SPAR BOEING 727 727223 1384074 NM WS 625 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 892AA 22008 TUL - FORWARD LOWER SPAR CHORD VERTICAL LEG HAS CORROSION BELOW NR 7 SLAT ACTUATOR. REPAIRED PER ESO 11697 DATED 1-25-9 9. (M) 2 L 7 3 4F A3WE 1999031200767 19990312 00767 NM 1999 3 12 AALA990129 1 19990127 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - BELLFRAME TOP DAMAGED HOLE FROM TOO LONG SCREW, STATION 1110 ABOVE STRINGER 27. REMOVED DAMAGED DOUBLER FABRICATE D AND INSTALLED NEW DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999031200768 19990312 00768 NM 1999 3 12 AALA990128 1 19990126 A 5320 ANGLE BOEING 727 727223 1384074 NM WS 734 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - WING FRONT SPAR LOWER CHORD ANGLE HEAVILY CORRODED BELOW NR 8 SLAT ACTUATOR DOGHOUSE CUTOUT. INSTALLED REPAIR STR AP AND ANGLE PER ESO 11697, DATED 1-26-99. (M) 2 L 7 3 4F A3WE 1999031200769 19990312 00769 NM 1999 3 12 AALA990127 1 19990128 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FOUND STATION 1130 BELLFRAME TOP DAMAGED, HOLE FROM TOO LONG OF A SCREW, ABOVE STRINGER 27R. REMOVED DAMAGED AND INSTALLED DOUBLER IAW SRM 53-10-4, AT STATION 1130 BELLFRAME STRINGER 27R. (M) 2 L 7 3 4F A3WE 1999031200770 19990312 00770 NM 1999 3 12 AALA990126 1 19990126 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FOUND STATION 1070 BELLFRAME TOP DAMAGED AND WEB BULGED ABOVE STRINGER 26R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999031200771 19990312 00771 NM 1999 3 12 AALA990125 1 19990128 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FOUND CORROSION BETWEEN SKIN LAP STATION 970, STRINGER 27R. REMOVED CORROSION, REMOVED AND SPLICED IN STRINGER 27 R FROM 950D PLUS 10 TO 1010 PER ESO 11697 DATED 1-28-99 AND SRM 51-40-4 FIG 1. (M) 2 L 7 3 4F A3WE 1999031200772 19990312 00772 NM 1999 3 12 AALA990124 1 19990127 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 930 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FOUND CORROSION ON VERTICAL STIFFENER ANGLE FOR APU INLET, AT LOWER AFT CORNER OF SCREEN. REMOVED CORROSION, INST ALLED 201 STAINLESS .071 L-ANGLE DOUBLER PER SRM 51-40-4 TYPICAL EXTRUSION REPAIR. (M) 2 L 7 3 4F A3WE 1999031200773 19990312 00773 WP 1999 3 12 AALA990111 1 19990127 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 829 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION INSIDE NR 1 SEAT TRACK. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW PIECE PER SRM 33 -70-00 FIG 3. (M) 2 L 7 3 4F A22WE 1999031200774 19990312 00774 WP 1999 3 12 AALA990110 1 19990127 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 959 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR TIE AND FILLER PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1999031200775 19990312 00775 WP 1999 3 12 AALA990109 1 19990127 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 839 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON FORWARD SIDE OF FRAME. SPLICED IN NEW S-ANGLE PER SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1999031200776 19990312 00776 WP 1999 3 12 AALA990107 1 19990127 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 839 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION FORWARD SIDE OF FRAME STRINGER 49L TO 51L. SPLICED IN NEW S-ANGLE PER SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1999031200777 19990312 00777 WP 1999 3 12 AALA990106 1 19990125 A 2550 TRAY DOUG DC10 DC1010 3022110 WP BS 675 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION NR 3 ROLLER TRAY STATION 675. CUT OUT DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM 53-57-0 0. ALODINED, PRIMED AND PAINTED AREA PER SRM 51-21-00. (M) 2 L 7 3 4F A22WE 1999031200778 19990312 00778 WP 1999 3 12 AALA990144 1 19990202 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 237AA 49523 TUL - FOUND ON SEAT TRACK NR 2. SPLICED IN NEW SECTION OF TRACK REF SRM 53-05 STATION 1155-1300. (M) 2 L 7 2 4F A6WE 1999031200779 19990312 00779 WP 1999 3 12 AALA990152 1 19990202 A 5347 S563979 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1278 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 237AA 49523 TUL - FOUND CORROSION ON SEAT TRACK. REPLACED AFT STATION OF SEAT TRACK NR 1 STATION 1174-1309 SRM 53-05. (M) 2 L 7 2 4F A6WE 1999031200780 19990312 00780 WP 1999 3 12 ORJA9959 1 19990207 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROW 14 LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 755RA 49727 FLIGHT ATTENDANT REPORTS EXPOSED WIRING ALONG SIDEWALL AT ROW 14. SECURED WIRING AT ROW 14 DEF. EMERGENCY SEAT WIRING. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A6WE 1999031200781 19990312 00781 WP 1999 3 12 ORJA9969 1 19990116 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP TAIL CONE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 AT SJC, TAIL CONE LIGHTS (ESCAPE) INOPERABLE. RELAMPED BATTERY PACK EMERGENCY ESCAPE LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200782 19990312 00782 WP 1999 3 12 ORJA9962 1 19990123 A 3350 602062004 SIGN DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 AT PHX, LEFT DIVIDER WALL (EXTERNAL), FIRST CLASS AND COACH EMERGENCY EXIT SIGN FAILED LUMINOSITY CHECK. REMOVED AND RE PLACED LEFT DIVIDER WALL AT FIRST CLASS AND COACH EMERGENCY EXIT SIGN PER MM 11-00-01. SIGN REPLACED AND RETESTED, INSP ECTION APPROVED. (M) 2 L 7 2 4F RT A6WE 1999031200783 19990312 00783 NM 1999 3 12 ORJA9965 1 19990308 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 609SW 27929 ESCAPE PATH LIGHTING HAS EXPOSED WIRES AT MID CABIN. RESECURED TRACK LIGHTING COVER PER MM. 2 L 7 2 4F RT A16WE 1999031200784 19990312 00784 WP 1999 3 12 ORJA9968 1 19990216 A 3397 00105606003 WIRE DOUG DC9 DC983 3022083 WP ROW 14 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 SJC - EMERGENCY LIGHTS AT ROWS 8-12 AND ROW 14 INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER PACK FOR ROWS 8-12. F OUND BROKEN WIRE ROW 14. REMOVED AND REPLACED LIGHT ASSEMBLY. ALL OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200785 19990312 00785 WP 1999 3 12 99ZZZM171 1 19990216 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROWS 8-12 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 SJC - EMERGENCY LIGHTS AT ROWS 8-12 AND ROW 14 INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER PACK FOR ROWS 8-12. F OUND BROKEN WIRE ROW 14. REMOVED AND REPLACED LIGHT ASSEMBLY. ALL OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200786 19990312 00786 WP 1999 3 12 ORJA9967 1 19990212 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP ROW 8-11 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 SJC - EMERGENCY SEAT LIGHTING INOP ON SEATS 8-11 DEF. REMOVED AND REPLACED BATTERY CHARGER ON RIGHT EMERGENCY EXIT. OP S CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200787 19990312 00787 WP 1999 3 12 ORJA9963 1 19990213 A 3350 PPSIB CHARGER DOUG DC9 DC982 3022082 WP RT EMER EXIT INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 IN RNO - FORWARD OVERWING EXIT EMERGENCY LIGHT PACK INOPERATIVE ON RIGHT SIDE. REMOVED AND REPLACED BATTERY CHARGER ASS Y, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999031200788 19990312 00788 WP 1999 3 12 ORJA9964 1 19990213 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP LT EMERG EXIT DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 IN RNO - AFT OVERWING EXIT EMERGENCY LIGHT PACK INOP ON LEFT SIDE. REMOVED AND REPLACED BATTERY PACK ASSY, OPS CHECK GO OD. (M) 2 L 7 2 4F A6WE 1999031200789 19990312 00789 WP 1999 3 12 ORJA9966 1 19990215 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 12-20 DISCHARGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO, IN SEAT EVAC LIGHTS INOPERATIVE AT ROWS 12-20. REMOVED AND REPLACED BATTERY PACK AT AFT RIGHT EMERGENCY EXIT AN D FORWARD LEFT EMERGENCY EXIT. REPLACED WIRES ON SEAT 12, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200790 19990312 00790 WP 1999 3 12 ORJA9961 1 19990211 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 20 DEF DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 RNO - EMERGENCY LIGHTS AT ROWS 8-11 AND FORWARD RIGHT OVERWING ARE OUT. REMOVED AND REPLACED BATTERY PACK AT ROW 20 DEF . OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200791 19990312 00791 NM 1999 3 12 ORJA9947 1 19990206 A 3397 WIRE DOUG MD90 MD9030 3023690 NM BS 1240 DISCONNECTED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 903RA 53551 IN SJC, OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT STATION 1240. REMOVED CEILING PANEL AND FOUND LOOSE WIRES, RECONNECTED . OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999031200792 19990312 00792 WP 1999 3 12 ORJA9958 1 19990206 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP PAX DOOR DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, FORWARD EXIT BATTERY PACK (EMERGENCY) IS BAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M ) 2 L 7 2 4F RT A6WE 1999031200793 19990312 00793 WP 1999 3 12 ORJA9957 1 19990206 A 3350 208347 LIGHT DOUG DC9 DC987 3022087 WP ROW 16 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, EMERGENCY LIGHT AT ROW 16 INOPERABLE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200794 19990312 00794 SW 1999 3 12 99ZZZM172 1 19990216 A 3250 1543011SN1 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG STEERING INOPERATIVE A MEJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 17 787C 1133 AC550 DURING TAKEOFF AT SJU, THE AMBER NOSE WHEEL STEERING FAIL LIGHT ILLUMINATED AND THE PILOT ABORTED THE TAKEOFF. MAINTENA NCE REMOVED AND REPLACED THE NOSE WHEEL STEERING PRESSURE SWITCH WITH A NEW UNIT. THE OPERATIONS CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1999031200795 19990312 00795 NM 1999 3 12 MASA99028 1 19990217 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 6321 - PHX-FLG - THE CREW REPORTED TWO OVERHEAD EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE E MERGENCY LIGHT BATTERIES, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999031200796 19990312 00796 EA 1999 3 12 MASA99027 1 19990217 A 3350 SWITCH CNDAIR CL600 CL6002B19 EA CABIN OUT OF POSITION A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5773 - CLT-LIT - THE CREW REPORTED THAT FIVE FLOOR LIGHTS AND ONE EMERGENCY DOOR LIGHT TO BE INOPERATIVE. MAINTENAN CE RESET THE SWITCH AND ALL LIGHTS OPERATED NORMALLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999031200797 19990312 00797 NM 1999 3 12 MASA99030 1 19990221 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 5335 - PHX-BFL - DURING PREFLIGHT CHECKS, THE CREW NOTED THE NR 1 AND NR 3 CEILING EMERGENCY LIGHTS WERE INOPERATIVE . MAINTENANCE T/S THE SYSTEM AND REPLACED THE BATTERY. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999031200798 19990312 00798 EA 1999 3 12 MASA99032 1 19990223 A 3350 1317 BULB BRUCE BMI0006002 CNDAIR CL600 CL6002B19 EA LT EMERG EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 FLT 5774 - CLT-YYZ - DURING PRE-FLIGHT WALK AROUND, CREW NOTICED THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERAT IVE. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999031200799 19990312 00799 WP 1999 3 12 HALA9900058 1 19990221 A 2781 SWITCH DOUG DC9 DC951 3022051 WP RT TE SLAT FAILED A HALA O OTHER N FALSE WARNING LD LANDING 1 WP 13 673MC 47726 FLT 201 - HNL - WITH SLAT EXTEND AND FLAP 50 DEGREES SET, ON FINAL 8L HNL SLAT EXTEND LIGHT WENT OUT, STALL INDICATION L IGHT ILLUMINATED AND JUST PRIOR TO TOUCHDOWN, STICK SHAKER. REMOVED AND REPLACED RIGHT SLAT EXTEND SWITCH, OPS CHECK OK . (M) 2 L 7 2 4F RT A6WE 1999031200800 19990312 00800 WP 1999 3 12 HALA9900057 1 19990220 A 2781 SENSOR DOUG DC10 DC1010 3022110 WP NR 4 LE SLAT FAILED A HALA O OTHER N FALSE WARNING CL CLIMB 1 WP 13 125AA 46525 FLT 939 - LAX - SLAT DISAGREE LIGHT ILLUMINATED WHEN FLAPS ARE SET FOR 2 DEGREE, TAKEOFF DISAGREE LIGHT DOES NOT GO OUT UNTIL FLAP SLAT RETRACTED. REPLACED RIGHT NR 4 SLAT 'A' AND 'B' SENSOR, OPS CHECK OK. (M) 2 L 7 3 4F A22WE 1999031200801 19990312 00801 WP 1999 3 12 HALA9900056 1 19990219 A 3610 CONTROLLER DOUG DC10 DC1010 3022110 WP CABIN FAILED A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 128AA 46984 HNL - FLT 10 - NR 2 MANIFOLD FAIL LIGHT FLICKERED ON CLIMB-OUT. PERFORMED PRESSURE DECAY CHECK PER MM 36-10-00 CHECK OK . REPLACED MANIFOLD FAILURE DETECTION CONTROLLER. GROUND RUN OK. (M) 2 L 7 3 4F A22WE 1999031200802 19990312 00802 NE 1999 3 12 HALA9900055 2 19990221 A 7230 COMPRESSOR DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE STALLED A HALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 13 603DC 966656 47784 696656 FLT 282 - HNL - LOUD BAND WHILE SPOOLING ENGINES. ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 1999031200803 19990312 00803 NE 1999 3 12 CLCA9901 2 19990111 A 7260 FILLER BOEING 757 75723APF 1384966 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE FAILED A CLCA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 571CA 24456 30710 FLT 96 - SEQU TO CLO - ON T/OF ROLL AT 0010Z. ON ROUTINE NORMAL T/O AT APPROX 75 KNOTS A/C BEGAN TO MAKE VIOLENT BANGIN G NOISE AND ABNORM EXTREME SHUDDERING FOLLOWED BY A MODERATE YAW TO THE LT. THE REJECTED T/O PROCEDURE WAS INITIATED AN D A/C STOPPED ON RUNWAY. HTC REPORTED TO THE CREW THERE WAS FLAMES AND FIRE COMING FROM THE LT ENG. THE EMERG SHUT DOW N WAS COMPLETED ON BOTH FIRE EQUIP WAS DISPATCHED, HOWEVER, THERE WAS NO FIRE. THE CREW EVACUATED THRU CREW DOOR USING THE EVAC ROPES. ENGS AND THE APU, BOTH ENG FIRE EXTINGUISHERS WERE DISCHARGED. NEITHER OF THE CREW INJURED. MX FOUND DAMAGE TO NR 1 ENG FAN CASE LINER, ENG TUBING, SMALL DENT IN HORIZ STAB AND SMALL HOLE IN FLAP. ENG CHANGED AND REPAIRE 2 L 7 2 4F 4 F RT A2NM E12EU 1999031200805 19990312 00805 WP 1999 3 12 GAIA9908 1 19990129 A 2497 WIRE CVAC 240 600240D 2422660 WP FS 109 SHORTED A GAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 94246 102 KHA - FLT 176 - AFTER DEPARTURE FROM CLE APPROX 10 MINUTES INTO FLIGHT, CREW SMELLED STRONG ELECTRICAL ODOR. FLIGHT CRE W NOTIFIED ATC DELARED AN EMERGENCY AND RETURNED TO CLE AND MADE AN UNEVENTFUL LANDING. A CLOSE INSPECTION OF THE EXTER NAL POWER WIRING SYSTEM REVEALED A SHORTED WIRE AT THE TERMINAL STRIP GOING TO THE EXTERNAL POWER LIGHT. THE DEFECTIVE WIRING WAS REPLACED IAW KHA CV-600 MAINTENANCE MANUAL CHAPTER 24-50-01 AND TESTED PER CHAPTER 24-40-01, NO DEFECTS NOTED . AIRCRAFT RETURNED TO SERVICE. (M) 1 L 7 2 4T RT 2L72 1999031200806 19990312 00806 NM 1999 3 12 GAIA9911 1 19990205 A 5755 6517348107A PANEL BOEING 727 727251 138408H NM NR 10 SPOILER CRACKED A GAIA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 07 252US 19971 EN ROUTE FROM CLT-TOL - DURING CRUISE AT FL280 BETWEEN MACH .74 TO .80, THE AIRCRAFT EXIBITED A MODERATE VIBRATION. (CO NTROL WHEEL CENTERED AND SPEED BRAKE HANDLE IN FORWARD DETENT). MOVING SPEED HANDLE BACK APPROXIMATELY 2 INCHES WOULD M AKE THE VIBRATION GO AWAY. RETURNING THE HANDLE TO THE FORWARD POSITION WOULD ALLOW THE MODERATE VIBRATION TO RETURN. T HE AIRCRAFT LANDED IN TOL WITHOUT FURTHER DIFFICULTY. FOUND NR 10 SPOILER PANEL CRACKED AT THE ACTUATOR HINGE. REMOVED AND REPLACED NR 10 SPOILER PANEL IAW B727 MM 27-61-01. OPERATIONAL CHECK NORMAL ON GROUND. NO DEFECTS NOTED. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999031200807 19990312 00807 NM 1999 3 12 GAIA9912 1 19990204 A 5270 SWITCH BOEING 727 727224 1384076 NM CARGO DOOR DIRTY A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 69739 20667 AFTER DEPARTING TOL, CARGO DOOR ANNUNCIATOR FLICKERED. AIRCRAFT RETURNED TO TOL AND MADE AN UNEVENTFUL LANDING. CLEANE D DIRT AND DEBRIS FROM (FORWARD BELLY) CARGO DOOR SEAL AND SWITCH. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999031200808 19990312 00808 WP 1999 3 12 GAIA9913 1 19990204 A 3230 CONNECTOR CVAC 240 240D 2422660 WP LANDING GEAR FAILED A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 94226 48 KHA - FLT 184 - PIT-CVG - AFTER TAKEOFF THE FLIGHT CREW WAS UNABLE TO RETRACT THE LANDING GEAR USING NORMAL PROCEDURES. THE GEAR WAS RETRACTED AND EXTENDED USING COCKPIT OPERATIONS MANUAL PROCEDURES. THE AIRCRAFT RETURNED TO PIT AND MADE AN UNEVENTFUL LANDING. A TERMINAL END ON THE LANDING GEAR CONTROL LEVER LOCKING SOLENOID WS REPLACED AND THE SYSTEM WAS TESTED PER THE CONVAIR MAINTENANCE MANUAL. THE AIRCRAFT WS THEN RETURNED BACK TO SERVICE. (M) 2 L 7 2 4R RT A793 1999031200809 19990312 00809 WP 1999 3 12 GAIA9914 1 19990204 A 3230 41EN9110 SWITCH CVAC 240 240D 2422660 WP LT MLG OUT OF ADJUST A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 94226 48 KHA - FLT 184 - PIT-CVG - AFTER TAKEOFF THE FLIGHT CREW WAS UNABLE TO RETRACT THE LANDING GEAR USING NORMAL PROCEDURES. THE GEAR WAS RETRACTED AND EXTENDED USING COCKPIT OPERATIONS MANUAL PROCEDURES. THE AIRCRAFT MADE AN UNEVENTFUL LANDIN G AT CVG. THE AIRCRAFT WAS FERRIED TO DFW. THE LANDING GEAR SAFETY SWITCH WAS ADJUSTED PER THE CONVAIR MM. THE AIRCRA FT WAS THEN RETURNED BACK TO SERVICE. (M) 2 L 7 2 4R RT A793 1999031200810 19990312 00810 WP 1999 3 12 GAIA9915 1 19990204 A 2810 FUEL CAP CVAC 240 240D 2422660 WP RT WING NOT SECURED A GAIA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 94226 48 KHA - FLT 226 - CVG-MEM TO DFW, AFTER TAKEOFF FROM MEM THE FLIGHT CREW WAS NOTIFIED BY ATC THAT THE RIGH WING WAS STREAM ING A LARGE PLUME OF FLUID. THE AIRCRAFT RETURNED TO MEM. THE RIGHT WING FUEL CAP WAS FOUND NOT SECURED. THE CAP WAS SECURED. THE CAP WAS SECURED AND THE AIRCRAFT WAS THEN RETURNED BACK TO SERVICE. (M) 2 L 7 2 4R RT A793 1999031200811 19990312 00811 NM 1999 3 12 GAIA9916 1 19990209 A 5320 WEB BOEING 727 727223 1384074 NM BS 1110-1130 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6811 19486 DURING SCHEDULED PHASE IN C-CHECK, THE WEB LOCATED AB BS 1110 TO 1130 AT RBL 60 WAS FOUND CRACKED. A REPLACEMENT PANEL WAS FABRICATED FROM .050 INCH THICK 7075-0 HT TO T6 AFTER IT WAS FORMED. STIFFENERS ANGLES FORMED FROM 7075-T6 BY .050 IN LIEU OF WELDED BEADS AS EPR B727 SRM 51-10-1. REPAIR ACCOMPLISHED IAW AIA EDR B2-06370. NON ROUTINE 52206. (M) 2 L 7 3 4F A3WE 1999031200812 19990312 00812 NM 1999 3 12 GAIA9910 1 19990129 A 3260 SWITCH BOEING 727 727222 1384073 NM NLG DOOR OUT OF ADJUST A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 90AX 20040 ON TAKEOFF, WITH GEAR RETRACTED, FLYING OUT OF MCI EN ROUTE TO IAH, THE GEAR DOOR LIGHT ON THE FRONT AND THE F/E'S AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. THE AIRCRAFT DIVERTED BACK TO MCI AND LANDED WITHOUT FURTHER DIFFICULTIES. CONDUCTED A MX FERRY TO OKC WHERE A HANGAR AND JACKS WERE AVAILABLE. CONDUCTED A MAINTENANCE GEAR SWING AND FOUND THE NLG DOOR WARNING OUT OF ADJUSTMENT. ADJUSTED THE SAME IAW MM 52-53-02. OPERATIONAL CHECK GOOD PER MM 32-63-04. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999031200813 19990312 00813 NM 1999 3 12 GAIA99022 1 19990209 A 5312 BULKHEAD BOEING 727 727223 1384074 NM BS 740 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6811 19486 DURING SCHEDULED PHASE IN C-CHECK, CORROSION WAS FOUND ALONG THE HORIZONTAL FLANGE, AT FS 740 BULKHEAD. THE DAMAGED ARE A TO THE BULKHEAD WAS REPAIRED AS EPR B727 SRM 53-10-1 FIG 1 DETAIL 1, AND AIA EDR B2-06357. REPAIR DOCUMENTED ON AIA N ON-ROUTINE 1710. (M) 2 L 7 3 4F A3WE 1999031200814 19990312 00814 NM 1999 3 12 GAIA9917 1 19990209 A 5720 TIP BOEING 727 727223 1384074 NM LT WING UNSERVICEABLE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6811 19486 DURING SCHEDULED PHASE IN C-CHECK, A INCORRECT STATIC WICK BASE WAS FOUND INSTALLED ON THE LEFT WING TIP. DURING REMOVA L FOUR .1875 INCH FASTENERS HOLES WERE LEFT. THE DAMAGED AREA WAS REMOVED A FILLER WAS FABRICATED USING SAME MATERIAL A S REMOVED. THE FILLER WAS THEN WELDED AS PER BOEING SPEC BAC5975. THE BARE AREA WAS THEN TOUCHED UP WITH A TOP COAT TO MATCH EXISTING FINISH. REPAIR ACCOMPLISHED IAW AIA EDR B2-06366. NON ROUTINE 51856. (M) 2 L 7 3 4F A3WE 1999031200815 19990312 00815 NM 1999 3 12 GAIA99020 1 19990209 A 5330 SKIN BOEING 727 727223 1384074 NM BS 352 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6811 19486 DURING SCHEDULED PHASE IN C-CHECK, A SMALL CRACK WAS FOUND IN THE SKIN LOCATED AT BS 352 STRINGER 27 RT. A REPAIR DOUBL ER WAS FABRICATED AND INSTALLED USING AIA EDR B2-06360 OVER THE DAMAGED AREA. REPAIR DOCUMENTED ON AIA NON-ROUTINE 5181 7. (M) 2 L 7 3 4F A3WE 1999031200816 19990312 00816 NM 1999 3 12 GAIA9918 1 19990209 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 MISDRILLED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6811 19486 DURING SCHEDULED PHASE IN C-CHECK, A MISDRILLED HOLE ON FRAME STATION 500 BETWEEN S-10L AND S14L. HOLES WERE REAMED AND DEBURRED. NAS1097AD6-XX RIVETS WERE INSTALLED. REPAIR ACCOMPLISHED IAW AIA EDR B206359. NON ROUTINE 52142. (M) 2 L 7 3 4F A3WE 1999031200817 19990312 00817 NM 1999 3 12 GAIA9919 1 19990209 A 5311 FRAME BOEING 727 727223 1384074 NM BS 480-660 MISDRILLED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 6811 19486 DURING SCHEDULED PHASE IN C-CHECK, ELONGATED HOLES ON THE RBL 45 UPPER CHORD AT FUSELAGE FRAME STATIONS 480 TO 680. HOL ES WERE DRILLED AND REAMED TO .03125 OVERSIZE. THE HOLES WERE DEBURRED, AND FASTENERS WERE INSTALLED AS CALLED OUT IN A IA EDR B2-06354. REPAIR DOCUMENTED ON AIA NON ROUTINE 52142. (M) 2 L 7 3 4F A3WE 1999031200818 19990312 00818 NM 1999 3 12 GAIA99021 1 19990209 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6811 19486 DURING SCHEDULED PHASE IN C-CHECK, CORROSION ON FLOORBEAM UPPER CHORD AT RBL 15 TO 44, FS 1130. AFTER CORROSION REMOVAL THE UPPER CHORD WAS FOUND BEYOND LIMITS. THE DAMAGED AREA TO THE FLOORBEAM WAS REPAIRED AS PE AIA EDR B2-06351, AIA/E/ 2922 REV ORIG. REPAIR DOCUMENTED ON AIA NON-ROUTINE 51850. THIS REPAIR RECEIVED FAA-ACO APPROVAL. (M) 2 L 7 3 4F A3WE 1999031200819 19990312 00819 NM 1999 3 12 GAIA9924 1 19990210 A 2910 106056340 HOSE BOEING 727 727223 1384074 NM NR 2 ENGINE FAILED A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 6821 19496 AFTER TAKEOFF FROM DFW, THE 'A' SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. THE AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT FURTHER DIFFICULTIES. REMOVED AND REPLACED HYDRAULIC HOSE TO NR 2 ENGINE DRIVE HYDRAULIC PUMP. ALSO, REPLACED NR 1 AN D NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND ASSOCIATED FILTERS IAW B727 MM 29-11. RESERVICED SYSTEM, THEN OPERATIONALLY AN D LEAK CHECKED GOOD. RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 1999031200820 19990312 00820 NM 1999 3 12 GAIA99025 1 19990215 A 2612 BACC18Z1 CIRCUIT BREAKER BOEING 727 727223 1384074 NM P6-3 PANEL FAILED A GAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 6811 19486 WHILE EN ROUTE TO YIP FROM IND, THE FLIGHT ENGINEER FOUND THE NR 1 ENGINE FIRE DETECTION CIRCUIT BREAKER HAD TRIPPED. A TTEMPTED ONE RESET, BUT THE CIRCUIT BREAKER WOULD NOT RESET. THERE WAS A BUNRING RUBBER SMELL NOTED IN THE COCKPIT. DE CLARED AN EMERGENCY INTO YIP. THE PLANE LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TRACED THE BURNING SMELL BACK TO THE CIRCUIT BREAKER. THE CIRCUIT BREAKER WAS REPLACED AND A OPERATIONAL TEST OF THE SYSTEM WAS CARRIED OUT OK. THE AIR CRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999031200821 19990312 00821 NM 1999 3 12 F3LA99004 1 19990217 A 3397 WIRE BOEING 737 737201 1384454 NM ROW 16, 17, 18 BROKEN A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 205AU 19421 DEN - DURING A-6 CHECK, INSPECTION REPORTED FLOOR PROXIMITY LIGHTING AT ROWS 16, 17 AND 18 INOPERATIVE. MAINTENANCE REP AIRED BROKEN WIRING AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1999031200822 19990312 00822 NM 1999 3 12 F3LA99005 1 19990219 A 3397 WIRE BOEING 737 7372P6 1C84609 NM PAX DOOR LOOSE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 1PC 21613 PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED LOOSE WIRE AT CHARGER AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999031200823 19990312 00823 NM 1999 3 12 USAABB99007 1 19990211 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 PVD - FOUND SEVEN EMERGENCY FLOOR LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1999031200824 19990312 00824 NM 1999 3 12 USAASB99040 1 19990216 A 2120 DUCT BOEING 737 7373B7 1384580 NM RIGHT BROKEN A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 532AU 24479 PVD - FLT 710 - FLIGHT WAS DISPATCHED WITH THE RIGHT PACK ON MEL DUE TO A RIGHT WING BODY OVERHEAT LIGHT ILLUMINATING. E N ROUTE FROM PIT TO PVD AT FL250, THE WARNING HORN SOUNDED DUE TO A PRESSURIZATION LOSS. CREW WAS UNABLE TO CONTROL PRE SSURIZATION IN MANUAL MODE AND ASKED AIR TRAFFIC CONTROL FOR A LOWER ALTITUDE. FLIGHT WAS CLEARED TO FL100 AND A RAPID DESCENT WAS ACCOMPLISHED TO THE ALTITUDE WITH NO PROBLEMS. NO OXYGEN MASKS WERE DEPLOYED AND NO EMERGENCY WAS DECLARED. FLIGHT CONTINUED AT LOWER ALTITUDE AND LANDED AT PVD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A BRO KEN DUCT TO THE RIGHT TURBOFAN. LEAK CHECK AND OPS CHECK GOOD. REMOVED MEL ON RIGHT PACK CONCERNING WING TO BODY OVER 2 L 7 2 4F RT A16WE 1999031200825 19990312 00825 NM 1999 3 12 USAASB99038 1 19990215 A 2131 7110025 CONTROLLER BOEING 737 7373B7 1384580 NM COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 518AU 26726 23704 PIT - FL777 - EN ROUTE FROM PIT-DFW, IN THE CMH AREA, CREW RECEIVED A WARNIGN OF PRESSURIZATION LOSS DURING CLIMB FROM F L330 TO FL350. FLIGHT DESCENDED TO FL250 AND WAS UNABLE TO MAINTAIN PRESSURIZATION. DESCENT WAS MADE TO FL110 AND DECI SION WAS MADE TO RETURN TO FIELD AT PIT. NO OXYGEN MASKS WERE DROPPED AND NO EMERGENCY WAS DECLARED. FLIGHT LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURIZATION SELECTOR PANEL. PERFORMED OPERATIONAL CHECK PER MM 21-31-00. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999031200826 19990312 00826 NM 1999 3 12 USAASB99039 1 19990216 A 2131 7102048 CONTROLLER BOEING 737 7373B7 1384580 NM E/E COMPT FAILED A USAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 19 518AU 59444 23704 PHL - FL255 - ON CLIMB-OUT FROM ATL, FLIGHT LOST BOTH AUTO AND STANDBY PRESSURIZATION CONTROL AT FL310. CREW DECLARED A N EMERGENCY AND DESCENDED TO FL100. OXYGEN MASKS WERE NOT DEPLOYED. AFTER DESCENDING TO FL090, THE CAPTAIN FELT IT WAS SAFE TO CONTINUE TO PHL, AND REQUESTED TO CONTINUE AT THE LOWER ALTITUDE. FLIGHT CONTINUED TO PHL IN MANUAL MODE AND L ANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER PER MM. PRESSURIZATION SYSTEM OPERATIONALLY CHECKS GOOD IN ALL MODES. (M) 2 L 7 2 4F RT A16WE 1999031200827 19990312 00827 EU 1999 3 12 SIMA990321 1 19990201 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU ROW 10WL DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423MQ 11775 030 SAW - DURING PS-2 INSPECTION, FOUND EMERGENCY LIGHT BATTERY PACK AT LOCATION 10WL WAS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999031200828 19990312 00828 EU 1999 3 12 SIMA990393 1 19990208 A 5330 S5367120120051 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - AIRCRAFT ARRIVED FOR REPAIR OF LARGE DENT AFT OF PASSENGER DOOR BETWEEN FRAMES 40 AND 41 AT STRINGER 12. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999031200829 19990312 00829 EU 1999 3 12 SIMA990395 1 19990208 A 5330 S536712890005 SKIN AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 SAW - DURING MBV-1 INSPECTION, FOUND A DENT IN FUSELAGE SKIN .050 INCH WIDE, 1 INCH LONG BY .018 DEEP BETWEEN FRAMES 43 AND 44 AND STRINGER 8 AND 9. REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999031200830 19990312 00830 EU 1999 3 12 SIMA990394 1 19990208 A 5330 S531722121405 SKIN AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 548AT 548 SAW - DURING MBV-1 INSPECTION, FOUND A DENT IN THE RIGHT SIDE FUSELAGE SKIN JUST FORWARD OF THE DC POWER ACCESS DOOR. R EPAIRED THE SKIN IAW SRM 53-11-28. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999031200831 19990312 00831 EU 1999 3 12 SIMA990322 1 19990201 A 5330 S536712890005 SKIN AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 538AT 538 SAW - AIRCRAFT ARRIVED FOR REPAIR OF ONE INCH HOLE IN SKIN, AFT OF PASSENGER DOOR, BETWEEN FRAMES 40 AND 41 AND STRINGER S 13 AND 14. REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999031200832 19990312 00832 EU 1999 3 12 SIMA990422 1 19990211 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FALSE WARNING A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 323AE A3189 340B323 DFW - FLT 3576 - CARGO SMOKE LIGHT CAME ON IN FLIGHT. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED AFT CARG O SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999031200833 19990312 00833 EU 1999 3 12 99ZZZM173 1 19990129 A 5347 S53375001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200834 19990312 00834 EU 1999 3 12 99ZZZM174 1 19990129 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200835 19990312 00835 EU 1999 3 12 99ZZZM175 1 19990129 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200836 19990312 00836 EU 1999 3 12 99ZZZM176 1 19990129 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200837 19990312 00837 EU 1999 3 12 99ZZZM177 1 19990129 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200838 19990312 00838 EU 1999 3 12 99ZZZM178 1 19990129 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200839 19990312 00839 EU 1999 3 12 99ZZZM179 1 19990129 A 5347 S53275001203 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200840 19990312 00840 EU 1999 3 12 99ZZZM180 1 19990129 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 223 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT INBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. (M) REF SIM A990291. 2 H 7 2 4T RT A53EU 1999031200854 19990312 00854 NM 1999 3 12 MZZA99023 1 19990111 A 5330 SKIN BOEING 727 7272F9 138407D NM FUSELAGE CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, CORROSION WAS FOUND ON FUSELAGE SKIN INNER SURFACE AT LEFT SIDE WING SCANNI NG LIGHT CUTOUT. THE CORRODED SKIN WAS CLEANUP AND REPAIRED PER B727 SRM 53-30-3 FIGURE 22. (M) 2 L 7 3 4F RT A3WE 1999031200858 19990312 00858 WP 1999 3 12 USAA990066 1 19990130 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 973VJ 80321 47099 PIT - DURING C-6 CHECK, FOUND .5 INCH RADIUS OF CORROSION AROUND ACCESS HOLES ON SKIN EXTERNAL DOUBLER FORWARD CARGO DOO R LOWER STOPS. REPLACED DEFECTIVE PART WITH IDENTICAL PART PER EA 5700A. (M) 2 L 7 2 4F A6WE 1999031200859 19990312 00859 NM 1999 3 12 USAA029903 1 19990201 A 2150 525374 ACTUATOR GARRTT BOEING 727 727227 1384078 NM COOLING DOOR INOPERATIVE A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 19 926TS 662021 20774 FLT 6161 - BOS-LGA - LEFT PACK FAN TRIPPED CIRCUIT BREAKER. AIR CONDITION SMOKE IN COCKPIT ON TAXI IN. LEFT PACK TEMP 110 DEGREES - 120 DEGREES BEFORE TURNING OFF PACK. FOUND LEFT PACK FAN DOOR INOPERATIVE CLOSED. REPLACED LEFT PACK FAN AIR INLET DOOR ACTUATOR PER MM 21-56-71. OPERATIONAL CHECKS OK. (M) 2 L 7 3 4F A3WE 1999031200860 19990312 00860 WP 1999 3 12 EISA99006 1 19990118 A 3350 MISC060 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A EISA K NONE L NO TEST UK UNKNOWN 1 SW 07 969VJ 47421 PASSENGER FLOOR EMERGENCY LIGHTS ILLUMINATED AFTER AIRCRAFT SHUTDOWN. EMERGENCY LIGHTS SWITCH VERIFIED IN OFF POSITION, BEFORE SHUTDOWN. REMOVED AND REPLAFED AFT AISLE EMERGENCY BATTERY WITH SERVICEABLE UNITS PER MM CHAPTER 33. (M) 2 L 7 2 4F A6WE 1999031200861 19990312 00861 WP 1999 3 12 GTIA9900012 1 19990129 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 DTW - ONE FLOOR TRACK LIGHT DOESN'T WORK. RELAMPED FLOOR TRACK, OPERATION CHECK GOOD IAW MM 33-50-00. (M) 2 L 7 2 4F A6WE 1999031200862 19990312 00862 CE 1999 3 12 99ZZZM183 1 19990127 A 3260 SWITCH CAM EATON BEECH 1900 1900C 1154161 CE MLG LOOSE A YADA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 01 1563C 322 UC20 AFTER DEPARTURE, GEAR SELECTED UP AND NOSE GEAR RETRACTED BUT MAINS DID NOT. GEAR SELECTED DOWN AND GEAR SHOWED DOWN AN D LOCKED. GEAR SELECTED UP AGAIN AND GEAR WOULD NOT RETRACT. GEAR SELECTED DOWN AND INDICATED THREE GREEN. AIRCRAFT R ETURNED TO AIRPORT AND MADE AN UNEVENTFUL LANDING. AIRCRAFT THEN FLOWN TO ANCHORAGE WITH GEAR DOWN. (M) 2 L 7 2 4T RT A24CE 1999031200863 19990312 00863 CE 1999 3 12 99ZZZM184 1 19990125 A 3240 MS2874140184 LINE BEECH 1900 1900C 1154161 CE LT/RT MLG WW RUPTURED A YADA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 AL 01 45GL UC45 PILOT REPORTED CAPTAINS LEFT BRAKE VERY WEAK. BRAKE SYSTEM BLEED, OPS CHECKED GOOD. THE NEXT DAY, THE FLEXIBLE BRAKE L INES (UPPER) IN THE GEAR WELLS, LEFT AND RIGHT, WERE FOUND TO BE LEAKING THROUGH THE HOSE. REPLACED UPPER FLEX LINE. ( M) 2 L 7 2 4T RT A24CE 1999031200866 19990312 00866 WP 1999 3 12 ARWA990203 1 19990212 A 3260 ST204HD32 LIGHT DOUG DC8 DC862 3021970 WP COCKPIT MALFUNCTIONED A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 802BN 45909 MIA - LANDING GEAR DOOR NOT LATCHED. REMAINED ON, WARNING LIGHT ILLUMINATED. AFTER ALL ABNORMAL PROCEDURES WERE PERFOR MED. RETURNED TO MIAMI WITHOUT INCIDENT. T/S FOUND DOOR NOT LATCHED WARNING LIGHT SOCKET DAMAGE. REMOVED AND REPLACED ELECTRICAL SOCKET IAW DC8 MM 32-60-0. TEST ON GROUND CHECK NORMAL IAW DC8 MM 32-31-5. (M) 2 L 7 4 4F 4A25 1999031200872 19990312 00872 WP 1999 3 12 EISA99012 1 19990118 A 5321 59100801 FLOOR DOUG DC9 DC931 3022065 WP BS 137 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 969VJ 47421 DURING ACCOMPLISHED OR ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON FLOOR WEB AT FS 137 LBL 20 BETWEEN CAPTAINS INBOARD AND OUTBOARD SEAT TRACKS. REMOVED CORROSION, FABRICATED DOUBLER PER SRM 53-04 FIGURE 4 AND INSTALLED PER SRM 51-30-8. (M) 2 L 7 2 4F A6WE 1999031200873 19990312 00873 WP 1999 3 12 EISA99010 1 19990118 A 5347 59100851 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 969VJ 47421 DURING ACCOMPLISHED OF ROUTINE C-CHECK, WORK CARD, CORROSION WAS FOUND ON SEAT TRACK AT FS 200-218 LBL 21. REMOVED DAMA GED SECTION OF SEAT TRACK, FABRICATED NEW SECTION OF TRACK AND INSTALLED PER SRM 51-10-1 AND 51-30-01. (M) 2 L 7 2 4F A6WE 1999031200874 19990312 00874 WP 1999 3 12 EISA99009 1 19990118 A 5320 59100851 ANGLE DOUG DC9 DC931 3022065 WP BS 200 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 969VJ 47421 DURING ACCOMPLISHED OF ROUTINE C-CHECK WORK CARD, FOUND CORROSION AT FS 200 RBL 60, FORWARD GALLEY DOOR JAMB AFT LOWER C ORNER. REMOVED DAMAGED ANGLE, FABRICATED NEW PART PER SRM 51-60-0 AND INSTALLED PART PER SRM 51-30-01. (M) 2 L 7 2 4F A6WE 1999031200875 19990312 00875 WP 1999 3 12 EISA99011 1 19990118 A 5755 59100531 SKIN DOUG DC9 DC931 3022065 WP RT SPOILER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 969VJ 47421 DURING ACCOMPLISHED ROUTINE C-CHECK WORK CARD, CORROSION WAS FOUND SKIN DISBOND RIGHT WING INBOARD SPOILER, INBOARD TRAI LING EDGE TOP SKIN. REMOVED DAMAGED AREA, REPAIRED HONEYCOMB PER SRM 57-04 FIG 4, AND INSTALLED NEW SKIN SECTION PER SR M 51-70-2. (M) 2 L 7 2 4F A6WE 1999031200876 19990312 00876 WP 1999 3 12 EISA99013 1 19990118 A 5753 5910028 SKIN DOUG DC9 DC931 3022065 WP LT TE FOREFLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 969VJ 47421 DURING ACCOMPLISHED OF ROUTINE C-CHECK WORK CARD, FOUND LEFT INBOARD FORE FLAP DELAMINATED ON LOWER SURFACE. CUT OUT DA MAGED AREA AND FABRICATED NEW SKIN PER SRM 57-50-9, INSTALLED REPAIR PER SRM 51-70-2. (M) 2 L 7 2 4F A6WE 1999031200877 19990312 00877 NM 1999 3 12 99ZZZM187 1 19990111 A 5320 6540867 WEB BOEING 737 737201 1384454 NM BS 285 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 69745 20215 LEFT NLG W/W STATION 285 HAS .5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. (M) 2 L 7 2 4F A16WE 1999031200878 19990312 00878 WP 1999 3 12 G60A027 1 19990126 A 2510 163VG2 MOTOR DOUG DC10 DC1030 3023501 WP LT COCKPIT SEAT MALFUNCTIONED A G6OA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 606GC 477 47929 ON CLIMB OUT FROM IST, THE FLIGHT CREW NOTICED SMOKE AROMA IN THE COCKPIT. THE SOURCE OF THE SMOKE WAS DETERMINED TO BE THE CAPTAINS SEAT CONTROL UNIT ASSEMBLY. THE CAPTAINS SEAT CONTROL CIRCUIT BREAKERS WERE PULLED AND THE AIRCRAFT RETUR NED TO IST. SEAT MOTOR HAD FAILED. UNIT WAS REMOVED AND REPLACED. (M) 2 L 7 3 4F A22WE 1999031200879 19990312 00879 NE 1999 3 12 GAIA9907 2 19990126 A 7311 LINE BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE LOOSE A GAIA A UNSCHED LANDING K J Y FLUID LOSS WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 SW 07 69740 20668 654368 DURING SCHEDULED FLIGHT BETWEEN ELP AND HUF, THE NR 2 ENGINE OIL QUANTITY WENT OT ZERO IN FLIGHT. LOW OIL PRESSURE LIGH T ILLUMINATED, AND OIL TEMPERATURE BEGAN TO CLIMB. THE ENGINE WAS SHUTDOWN IN FLIGHT. EMERGENCY LANDING WAS DECLARED I NTO MCI, AND LANDED IN MCI WITHOUT INCIDENT. THE ENGINE WAS INSPECTION. A LOOSE OIL LINE ON THE FUEL/OIL COOLER WAS FO UND. THE LINE WAS PROPERLY TORQUED, AND THE ENGINE WAS SERVICED WITH OIL. THE ENGINE RUN WAS COMPLIED WITH AND NO FURT HER OIL LEAKS WERE FOUND. THE AIRCRAFT WAS THEN RETURNED BACK TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999031200880 19990312 00880 CE 1999 3 12 99ZZZM188 1 19990119 A 3251 100951X063XE WASHER BEECH 1900 1900D 1154162 CE NLG STEERING FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 852CA 5459 UE55 UNABLE TO STEER AIRCRAFT FROM RUNWAY AFTER LANDING. INSPECTION OF AIRCRAFT FOUND RIGHT MAIN LANDING GEAR TORQUE KNEE SE PARATED DUE TO WASHER FAILURE, CAUSING CENTER TORQUE KNEE BOLT TO PULL THROUGH TORQUE KNEE. RIGHT MAIN LANDING GEAR, WH EEL ASSEMBLIES, AND BRAKE ASSEMBLIES REPLACED. FLEET INSPECTION INITIATED. (M) 2 L 7 2 4T RT A24CE 1999031200881 19990312 00881 WP 1999 3 12 GTIA9900008 1 19990120 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 DTW - AISLE PATH LIGHT BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY FLOOR LIGHTING TRIM AS REQUIRED. (M) 2 L 7 2 4F A6WE 1999031200883 19990312 00883 WP 1999 3 12 ORJA9907 1 19990107 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 19-22 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY LIGHTS AT ROWS 19, 20, 21, 22 INOPERABLE. REMOVED AND REPLACED BATTERY PACK ON RIGHT EXIT SIGN. (M) 2 L 7 2 4F RT A6WE 1999031200884 19990312 00884 WP 1999 3 12 ORJA9918 1 19990115 A 3350 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 1-9 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT PHOENIX IN ROWS 1 THROUGH 9 EMERGENCY LIGHTING WAS INOPERABLE, NEEDS TROUBLESHOT AND REPAIRED. TROUBLESHOT SYSTEM, F OUND LOW VOLTAGE ON EMERGENCY BATTERY PACK. CHARGED SYSTEM PER MM 33-53-00. OPS CHECK GOOD PER MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 1999031200885 19990312 00885 WP 1999 3 12 ORJA9919 1 19990115 A 3350 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 15-18 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT PHOENIX, AT ROWS 15 THROUGH 18 EMERGENCY SEAT LIGHTING WAS INOPERABLE, NEEDED TROUBLESHOOTING AND REPAIRING. TROUBLE SHOT SYSTEM, FOUND LOW VOLTAGE ON BATTERY PACKS. CHARGED SYSTEM, USING A/C POWER PER MM 33-53-00. SYSTEM OPS CHECKED G OOD PER MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 1999031200886 19990312 00886 WP 1999 3 12 ORJA9920 1 19990122 A 3350 EM1267 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 9-26 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 AT PHOENIX, FLOOR PROXIMITY LIGHTING IS OUT FROM SECTINOS 9-26, IN NEED OF TROUBLESHOOTING AND REPAIR. REMOVED AND REPL ACED BATTERIES IN BATTERY PACKS. ALL SEAT LIGHTING WORKS WELL AS PER MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 1999031200887 19990312 00887 NM 1999 3 12 ORJA9921 1 19990126 A 3350 8039251 BATTERY PACK DOUG MD90 MD9030 3023690 NM ROW 5 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 901RA 53489 IN SJC, EMERGENCY FLOOR LIGHTS INOPERATIVE FOR ROWS 6-20. REMOVED AND REPLACED BATTERY PACK AT ROW 5, OPS CHECK GOOD. ( M) 2 L 7 2 4F RT A6WE 1999031200888 19990312 00888 WP 1999 3 12 ORJA9922 1 19990122 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 11-14 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 SJC - EMERGENCY LIGHTS ON SEAT 11 THROUGH 14 ARE INOPERATIVE. REMOVED AND REPLACED FORWARD RIGHT EMERGENCY EXIT BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200890 19990312 00890 WP 1999 3 12 ORJA9924 1 19990125 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, AFT OVERWING EXIT LIGHTS WOULD NOT GO OFF. REMOVED AND REPLACED RIGHT AFT OVERWING EXIT BATTERY PACK. OPS CHEC KS GOOD. (M) 2 L 7 2 4F RT A6WE 1999031200892 19990312 00892 NE 1999 3 12 ARWA990104 2 19990108 A 7320 FFR LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122* 54555 NE NR 3 ENGINE OUT OF ADJUST A ARWA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 306GB 193U1138 BQN - FLT 508 - ABORTED TAKEOFF. NR 3 ENGINE SLOW TO ACCELERATE. MAX EPR ON TAKEOFF ROLL 1.200 (1500 RQD FOR REDUCED T /O POWER). RETURNED TO RAMP. ADJUSTED FUEL FLOW REGULATOR AND RUN NR 3 ENGINE PER MM 71-00-00, OPS CHECK NORMAL. (M) 2 L 7 3 4F 4 F A23WE A12EU 1999031200893 19990312 00893 NE 1999 3 12 ARWA990110 2 19990115 A 7200 ULI9625 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122* 54555 NE NR 2 VIBRATES A ARWA A J UNSCHED LANDING DUMP FUEL E VIBRATION/BUFFET CL CLIMB 1 SO 19 306GB EUH2 193U1138 MIA - FLT 501 - DURNG CLIMB, NR 2 EN AVM 2.5, LT ON, VIB FELT IN PEDALS VIB DECREASE WHEN POWER REDUCED, AVM SELECTED TO LOW POSITION (MED AND HIGH POSITIONS BELOW .8). REMOVED AND REPLACED BLADES IAW MM 72-31-11 RAN ENGIEN COMPLETED VIB S URVEY TEST NR 1 VIB WITHIN LIMITS. (M) 2 L 7 3 4F 4 F A23WE A12EU 1999031200894 19990312 00894 NE 1999 3 12 SIMA990201 2 19990120 A 7320 311489201 VALVE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE LT ENGINE FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 440AM 440 CRP - FLT 3674 - SMOKE IN THE COCKPIT. TURNED OFF NR 1 BLEED AD SMOKE CLEARED. DIVERTED TO CRP. FERRIED AIRCRAFT TO D FW FOR REPAIR. REMOVED AND REPLACED NR 1 P2.5 AND P3 AIR SWITCHING VALVE. GROUND RUN CHECKS GOOD. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999031200895 19990312 00895 WP 1999 3 12 TWAA9903701 1 19990226 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 37 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND FUSELAGE SKIN DAMAGED AT STA 37, 3 O'CLOCK POSITION, AND INTERIOR STRUCTURE DAMAGED AND CRACKS AT ALIGNMENT PINS. REPAIRED SKIN AND STRUCTURE PER ARA 16069 AND 16068. CRACK REPAIRED PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999031200896 19990312 00896 WP 1999 3 12 TWAA9903702 1 19990226 A 5620 WINDOW DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND STATIC BURNS ON RIGHT SIDE OF AIRCRAFT, CABIN WINDOWS 3, 4, 12, 30, 33 AND 35. BLENDED EACH PER SRM 53-05, FIG 3 AND ARA 16105, AND ALODINED BLEND. 2 L 7 2 4F A6WE 1999031200897 19990312 00897 WP 1999 3 12 TWAA9903703 1 19990308 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 160 & 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORTS AT STA 200 RBL 22 IN TO 42 IN, STA 160 TO 200 RBL 44 I N, STA 160 TO 200 LBL 54 IN, STA 200 RBL 44 TO 55, STA 200 LBL 0 TO 20, AND STA 180 RBL 1 TO 44. REPLACED AFFECTED FLOO R SUPPORTS PER SPM 6-70-01 PAGE 3. 2 L 7 2 4F A6WE 1999031200898 19990312 00898 WP 1999 3 12 AT9900182 1 19990309 A 3234 LEVER DOUG DC9 DC932 3022066 WP LANDING GEAR OUT OF ADJUST A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 815AT 47443 ON CLIMB, GEAR LEVER WILL NOT RAISE, AIR RETURN. RIGGED LANDING GEAR CONTROL LEVEL ANTI-RETRACTION LATCH IAW DC9 MM 32- 31-1. CHECKED RIG ON GROUND SENSE CONTROL, MECHANICAL RIG CHECK GOOD IAW DC9 MM 32-23-1. 2 L 7 2 4F A6WE 1999031200899 19990312 00899 WP 1999 3 12 AT9900183 1 19990309 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 1046 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE FRONT FACE OF CANTED WEB AT BS 1046.376. FABRICATED DOUB LER, ALODINE, PRIMED, AND INSTALLED REPAIR IAW DC9 SRM 53-01-0, AND 53-10-3. 2 L 7 2 4F A6WE 1999031200900 19990312 00900 WP 1999 3 12 AT9900184 1 19990224 A 5347 TRACK DOUG DC9 DC932 3022066 WP BS 332-465 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT TIEDOWN TRACK CORRODED ON BOTH SIDE AT BS 332 TO 465. REMOVED AND REPLACED TIEDOWN TRACK IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1999031200901 19990312 00901 1999 3 12 MALA976367 4 19990303 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DEPLOYED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 503XJ E2310 UPON BOARDING NOTICED THE RIGHT FORWARD CABIN DOOR SLIDE PARTIALLY DEPLOYED, BLOWN BY CATERING. MAINTENANCE REPLACED SL IDE, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999031200902 19990312 00902 EU 1999 3 12 MALA976368 1 19990218 A 2560 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 502XJ E2307 ON PREFLIGHT, FOUND FORWARD PASSENGER DOOR SLIDE HANGING DOWN FROM IT'S STOWED POSITION AND SLIDE COVER SEEMS TO BE AJAR . MAINTENANCE SECURED SLIDE AND TIGHTENED BOTTOM COVER. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999031200903 19990312 00903 EU 1999 3 12 MALA976369 1 19990307 A 3510 3705501 VALVE SAAB SF340 SF340A 7850100 EU OXYGEN SYST FAULTY A MALA O OTHER O OTHER CR CRUISE 1 GL 15 27XJ 027 THE O2 BOTTLE LEAKED TO 0 PSI DURING FLIGHT. MAINTENANCE REPLACED ALL THREE O2 BOTTLES AND OXYGEN TOGGLE SHUT OFF VALVE . OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031200904 19990312 00904 EU 1999 3 12 MALA976370 1 19990305 A 3020 SEPARATOR SAAB SF340 SF340A 7850100 EU RT ENG INLET DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 27XJ 027 RIGHT ENGINE INTAKE HEAT LIGHT CYCLED ON AND OFF FOR 20 MINUTES. RETURNED TO CWA. MAINTENANCE FOUND SEVERAL NICKS AND SCRATCHES IN RIGHT INLET SEPARATOR. REPAIRED IAW SAAB AMM CH 30-20-25-2. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031200905 19990312 00905 EU 1999 3 12 MALA976371 1 19990304 A 3020 NH2466805305 DUCT SAAB SF340 SF340A 7850100 EU RT INLET FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 27XJ 027 RIGHT INTAKE LIGHT CYCLES ON AND OFF. RETURNED TO MSP. MAINTENANCE REPLACED RIGHT UPPER INLET DUCT, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031200906 19990312 00906 EU 1999 3 12 MALA976372 1 19990224 A 2433 4493 CONVERTER SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 114XJ 340A114 CIRCUIT BREAKER L20 POPPED, SMOKE ODOR PRESENT ON RESET. MAINTENANCE REPLACED CONVERTER 12LL, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031200907 19990312 00907 EU 1999 3 12 MALA976373 1 19990305 A 3020 CONTROLLER SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 590MA 340B181 DURING CLIMBOUT OF DTW, RT ENGINE INTAKE HEAT CAUTION LIGHT ILLUMINATED. RAN THROUGH THE QRH ICE PROTECTION, LIGHT CONT INUED TO ILLUMINATE THEN IT STARTED TO CYCLE ON/OFF. RETURNED TO DTW. MAINTENANCE REPLACED RT LOAD MONITOR AND RT THER MOL CONTROLLER, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031200908 19990312 00908 EU 1999 3 12 MALA976374 1 19990306 A 2730 CONTROLS SAAB SF340 340B 7860101 EU ELEVATOR MALFUNCTIONED A MALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 15 407XJ 340B407 UPON ROTATION IN DTW, AIRCRAFT FELT ABNORMALLY LIGHT ON ELEVATOR CONTROL, CONTINUED THROUGH THE CLIMB. THE RESPONSE TO CONTROL INPUTS WERE NOT ADEQUATE/SLOW AND SLOPPY. RETURNED TO DTW. MAINTENANCE CHECK OF ELEVATOR TRAVEL AND OPS CHECK OF DEICE SYSTEMS. ALL CHECKS GOOD IAW SF340 CHAP 27. 2 L 7 2 4T RT A52EU 1999031200909 19990312 00909 EU 1999 3 12 MALA976375 1 19990303 A 2613 CONNECTOR SAAB SF340 340B 7860101 EU RT TAIL PIPE DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 414XJ 340B414 RIGHT TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF FROM ELM. AFTER PERFORMING MEMORY ITEMS AND REDUCING POWER ON RIGHT ENGINE THE LIGHT EXTINGUISHED. PER THE QRH, OPERATED THE RIGHT ENGINE AT REDUCED POWER AND RETURNED TO ELM. MAINTENAN CE REMOVED RIGHT ENGINE AFT COWL, CLEANED 12 O'CLOCK POSITION AFT CANNON PLUG, REINSTALLED AFT COWL. PERFORMED ENGINE G ROUND RUN FOR 10 MINUTES AND COULD NOT DUPLICATE. 2 L 7 2 4T RT A52EU 1999031200910 19990312 00910 EU 1999 3 12 MALA976376 1 19990306 A 2435 23080031 STARTER GEN SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 414XJ 340B414 LEFT GEN OFF LINE IN FLIGHT, QRH RESET, OFF LINE AGAIN, QRH EMERGENCY BACK TO SBN, GEN OVER TEMP WHILE GEN OFF. EMERGEN CY EXITS PULLED FOR EVACUATION. MAINTENANCE REPLACED LT STARTER GEN PER SAAB M/M 24-31-05 AND OPS CHECK GOOD. LEAK CHE CK GOOD. MAINTENANCE INSPECTED AND INSTALLED RIGHT FORWARD AND OVERWING EXIT DOORS. NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 1999031200911 19990312 00911 EU 1999 3 12 MALA976377 1 19990304 A 3060 666000219 BRUSH BLOCK SAAB SF340 340B 7860101 EU RT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 428XJ 428 RIGHT PROP HEAT FAILED IN FLIGHT. RETURNED TO MSP. MAINTENANCE REPLACED RIGHT BRUSH BLOCK, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031200912 19990312 00912 EU 1999 3 12 MALA976378 1 19990307 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 429XJ 429 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, FOLLOWED QRH, CYCLED GEAR 3 TIMES. RETURNED TO DTW. MAINTENANCE REMOVED ICE FROM LANDING GEAR AND COMPLETED GEAR SWINGS. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999031200913 19990312 00913 EU 1999 3 12 MALA976379 1 19990306 A 2434 23080031 GENERATOR SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 442XJ 442 LEFT DC GENERATOR OVERTEMP CAUTION LIGHT ILLUMINATED, PERFORMED QRH. RETURNED TO DTW. MAINTENANCE REPLACED LEFT DC GEN /STARTER. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999031200914 19990312 00914 EU 1999 3 12 MALA976380 1 19990307 A 3230 RELAY SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 446XJ 446 LANDING GEAR INOP, HYD QUANTITY AND PRESSURE NORMAL. CB F7 (LANDING CONTROL) POPPED AS GEAR HANDLE BROUGHT DOWN. SEPAR ATION BOLTS FIRED. MAINTENANCE REPLACED 20GA LOCKED DOWN RELAY AND SEPARATION BOLTS. OPS CHECKS PER IAW 32-30-00. 2 L 7 2 4T RT A52EU 1999031200915 19990312 00915 EU 1999 3 12 MALA976381 1 19990306 A 3230 6PP125012 SWITCH SAAB SF340 340B 7860101 EU HYD SYST FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 456XJ 456 ON GEAR RETRACTION THE INTRANSIT LIGHT AND HYDRAULIC PUMP REMAINED ON, CREW COMPLIED WITH QRH. RETURNED TO CID. MAINTE NANCE CLEANED CANNON PLUGS AT UPLOCK SWITCHES, FUNCTION CHECK GOOD. REPLACED HYD PRESSURE SWITCH AND DISCHARGED PRESSUR E IN AUTO MODE AND SYSTEM CHARGED NORMALLY. OPS CHECK GOOD IAW SAAB CH 29-10-00-2. 2 L 7 2 4T RT A52EU 1999031200916 19990312 00916 EU 1999 3 12 MALA976382 1 19990307 A 3260 SWITCH BAC 146 AVRO146RJ85A 1500097 EU RT MLG ICED UP A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 513XJ E2329 GEAR INDICATOR FOR RIGHT MAIN LANDING GEAR SHOWED RED AFTER DEPARTING DTW. RECYCLED TWICE, NO EFFECT. RETURNED TO DTW. MAINTENANCE INSPECTED AND FOUND EXCESSIVE ICE BUILD UP IN ALL THREE GEAR WELLS, DEICE BOTH MAIN AND NOSE GEAR AREAS AN D CLEANED GEAR PROX SWITCHES. TEST FLIGHT CHECKED GOOD. 2 H 7 4 4F RT A49EU 1999031200917 19990312 00917 EU 1999 3 12 MALA976383 1 19990307 A 3260 RETRACT MECH BAC 146 AVRO146RJ85A 1500097 EU RT MLG ICED UP A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 514XJ E2330 AFTER TAKEOFF WITH LANDING GEAR SELECTED UP, THE RIGHT MAIN RED RIGHT GEAR LIGHT STAYED ON ALONG WITH THE RED LIGHT IN T HE GEAR HANDLE. FOLLOWED QRH, CYCLED CB B2 AND THEN CYCLED GEAR DOWN, WHICH INDICATED THREE GREEN, RETURNED TO DTW. MA INTENANCE INSPECTED AND FOUND EXCESSIVE ICE BUILD UP ON BOTH MAIN GEAR, BOTH MAIN GEAR AREAS CLEANED OF ICE. TEST FLIGH T PROVED SATISFACTORY. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999031200918 19990312 00918 NM 1999 3 12 CALA9900226 1 19990308 A 3260 841602 PSEU BOEING 757 757224 1384958 NM E & E COMPT INOP A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 17128 27567 A GEAR DISAGREE EICAS MESSAGE WAS RECEIVED WITH A GEAR AMBER WARNING LIGHT AFTER TAKEOFF WITH GEAR HANDLE IN RETRACT POS ITION. QRH PROCEDURES WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC E FOUND THE PSEU AT FAULT. THE PSEU WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 1999031200919 19990312 00919 WP 1999 3 12 CALA9900227 1 19990305 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 117-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND SEAT TRACK CORRODED AROUND SCREW HOLES AT LT I/B POSITION, STA 1117-1174 AFT GALLEY AREA. NEW SEAT TRA CK SECTIONS WERE INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 1999031200920 19990312 00920 WP 1999 3 12 CALA9900228 1 19990306 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND TWO CRACKS IN THE NR 1 BEAM OF MAIN CABIN DOOR. THE BEAM HAD A .75 INCH CRACK ON AFT END AND A .375 IN CH CRACK ON FORWARD END. 2 L 7 2 4F A6WE 1999031200921 19990312 00921 WP 1999 3 12 CALA9900229 1 19990306 A 5350 59102331 RELEASE MECH DOUG DC9 DC982 3022082 WP TAIL CONE FAILED TEST A CALA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 09 76823 31235 49483 THE TAIL CONE RELEASE PULL WAS LOW AT 15 POUNDS DURING TEST. THE TAIL CONE WAS REMOVED AND A NEW TAIL CONE WAS INSTALLE D AND RIGGED IAW MM 53-53-00. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1999031200922 19990312 00922 NM 1999 3 12 CALA9900230 1 19990307 A 5230 WEB BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR WEB OVER THE CENTER SPRINGS. A DOUBLER WAS INSTALLED IAW ECRA 5230-01 450. 2 L 7 2 4F RT A16WE 1999031200923 19990312 00923 NM 1999 3 12 CALA9900231 1 19990308 A 5230 FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO BIN DOOR FORWARD LOWER CORNER FRAME. THE FORWARD CARGO DOOR FORWARD LO WER CORNER FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999031200924 19990312 00924 WP 1999 3 12 CALA9900232 1 19990308 A 5210 WEB DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND A 1 INCH CRACK AT AFT WEB PLATE LIGHTENING HOLE BETWEEN NR 6 AND NR 7 BEAMS OF MAIN CABIN DOOR. THE AR EA WAS REPAIRED IAW SRM 51-30-1, 51-30-2, AND 51-30-4. 2 L 7 2 4F A6WE 1999031200925 19990312 00925 WP 1999 3 12 CALA9900233 1 19990308 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1079-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1079 TO 1231. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-0 5, FIGURE 4F. 2 L 7 2 4F A6WE 1999031200926 19990312 00926 WP 1999 3 12 CALA9900234 1 19990308 A 5320 MEMBRANE DOUG DC9 DC982 3022082 WP BS 1155-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND AFT CARGO LEFT TUNNEL CUSP MEMBRANE CORRODED AT STA 1155 TO 1174. THE MEMBRANE WAS REPLACED IAW SRM 5 1-30-2. 2 L 7 2 4F A6WE 1999031200927 19990312 00927 NM 1999 3 12 CALA9900235 1 19990309 A 5320 ANGLE BOEING 757 757224 1384958 NM CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND AFT HOLD THRESHOLD ATTACHMENT ANGLE CORRODED. THE THRESHOLD ANGLE WAS REPLACED IAW BOEING DRAWING NR 1 46N5391. 2 L 7 2 4F RT A2NM 1999031200928 19990312 00928 WP 1999 3 12 CALA9900236 1 19990309 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 2.25 INCH CRACK IN AFT CARGO DOOR PAN AT FORWARD HOLD OPEN LATCH AND A .75 INCH CRACK IN AFT CARGO DO OR PAN AT AFT HOLD OPEN LATCH. INSTALLED REPAIRS IAW ECRA 5321-01010. 2 L 7 2 4F A6WE 1999031200929 19990312 00929 WP 1999 3 12 9900849943 1 19990303 A 2910 VALVE DOUG DC9 DC931 3022065 WP HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 1308T 47315 LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE OCCURRED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO DFW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING HYDRAULIC FLOW CONTROL VALVE. LEAK CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999031200930 19990312 00930 NM 1999 3 12 UPS99228916 1 19990308 A 5531 SPAR BOEING 727 727173C 1384059 NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, LT VERTICAL FIN REAR SPAR CHORD IS CRACKED AT INTERSECTION WITH BS 1342 BULKHEAD. STOP DRILLED CRACK , ALODINED AND PRIMED STOP DRILL HOLE, FABRICATED REPAIR ANGLE AND FILLER DRILLED UP AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, 51-20-01, 53-30-05, 51-30-02, SB 727-55-0076. 2 L 7 3 4F A3WE 1999031200931 19990312 00931 NM 1999 3 12 UPS99228917 1 19990308 A 5751 65192596 FITTING BOEING 727 727173C 1384059 NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, CORROSION RT WING O/B AILERON CENTER O/B HINGE FITTING. REMOVED AND REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999031200932 19990312 00932 NM 1999 3 12 UPS99228927 1 19990308 A 3350 BATT PACK BOEING 727 72725C 138400H NM ROW 10 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, EMERG EXIT ROW LIGHTS INOP ROW 10 BOTH SIDES OVERWING. REMOVED AND REPLACED BATTERY PACKS, OPS OK. 2 L 7 3 4F A3WE 1999031200933 19990312 00933 WP 1999 3 12 UPS99828918 1 19990219 A 5312 BULKHEAD WEB DOUG DC8 DC873F 302199F WP BS 621 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 621 BULKEAD WEB IS CRACKED ABOVE LONG 27L. REPAIRED BULKHEAD WEB IAW SRM 53-2-0 FIG 23. 2 L 7 4 4F RT 4A25 1999031200934 19990312 00934 WP 1999 3 12 UPS99828919 1 19990220 A 5320 37502571 FITTING DOUG DC8 DC873F 302199F WP BS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3 LONG 31R SPLICE FITTING IS CRACKED AT FS 610. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031200935 19990312 00935 WP 1999 3 12 UPS99828920 1 19990221 A 5320 577384659 FITTING DOUG DC8 DC873F 302199F WP BS 1754 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, HEAVY EXFOLIATION CORROSION ON FITTING AT FS 1754, BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1999031200936 19990312 00936 WP 1999 3 12 UPS99828921 1 19990221 A 5320 564881752 ANGLE DOUG DC8 DC873F 302199F WP BS 600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, STIFFENER ATTACH ANGLE CRACKED ON VERTICAL FLANGE, AFT SIDE OF THE FS 600 FRAME, AT LONG 19R. REMOV ED, FABRICATED AND REPLACED ANGLE IAW DWG 5648817 AND SRM 51-1-20D AND 1-1-21. 2 L 7 4 4F RT 4A25 1999031200937 19990312 00937 WP 1999 3 12 UPS99828922 1 19990222 A 5320 3779498508 FITTING DOUG DC8 DC873F 302199F WP BS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 902 AT LONG 19R THE TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031200938 19990312 00938 WP 1999 3 12 UPS99828923 1 19990222 A 5320 47504201 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 857 AT LONG 19L THE TIE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031200939 19990312 00939 WP 1999 3 12 UPS99828924 1 19990222 A 5320 4641324501 FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, LONGERON END FITTING AT FS 1690, LONG 26L IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 1999031200940 19990312 00940 WP 1999 3 12 UPS99828925 1 19990223 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 484.895 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT WING L/E RIB AT XS 484.895 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999031200941 19990312 00941 WP 1999 3 12 UPS99828926 1 19990225 A 5751 SKIN DOUG DC8 DC873F 302199F WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, RT I/B AILERON IS CRACKED, TOP O/B END UNDER THE WEIGHT COVER. CUT OUT DAMAGED AREA AND REPAIRED IA W SRM 57-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 1999031200942 19990312 00942 EU 1999 3 12 QXEA9900331 1 19990212 A 5320 CHANNEL FOKKER F28 F28MK4000 4990810 EU FRAME 10335 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - 91L FAIRING LOWER SUPPORT CHANNEL HAS (3) CRACKS RUNNING BETWEEN 3 RIVETS AT APPROXIMATELY FRAME 10335. REPAIRED IAW FOKKER SRM 53-02-17, FIGURE 6 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200943 19990312 00943 EU 1999 3 12 QXEA9900332 1 19990210 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT FUEL TANK ACCESS LOWER OPENING FOR PANEL 74B WING MATING SURFACE HAS FRETTING CORROSION AROUND NUT PLATE HOL ES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4A, PAGE 9. 2 L 7 2 4F RT A20EU 1999031200944 19990312 00944 EU 1999 3 12 QXEA9900333 1 19990210 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT FUEL TANK ACCESS LOWER OPENING FOR PANEL 74A WING MATING SURFACE HAS FRETTING CORROSION AROUND NUT PLATE HOL ES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4A AND B, PAGE 9. 2 L 7 2 4F RT A20EU 1999031200945 19990312 00945 EU 1999 3 12 QXEA9900334 1 19990210 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT FUEL TANK ACCESS LOWER OPENING FOR PANEL 72A WING MATING SURFACE HAS FRETTING CORROSION AROUND NUT PLATE HOL ES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4A, PAGE 9. 2 L 7 2 4F RT A20EU 1999031200946 19990312 00946 EU 1999 3 12 QXEA9900335 1 19990210 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT WING FUEL TANK ACCESS PANEL 74B HAS MINOR FRETTING CORROSION ON MATING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999031200947 19990312 00947 EU 1999 3 12 QXEA9900336 1 19990209 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT WING FUEL TANK ACCESS PANEL 74E HAS MINOR FRETTING CORROSION ON MATING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999031200948 19990312 00948 EU 1999 3 12 QXEA9900337 1 19990210 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT WING FUEL TANK ACCESS PANEL 72A HAS MINOR FRETTING CORROSION ON MATING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999031200949 19990312 00949 EU 1999 3 12 QXEA9900338 1 19990209 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT WING FUEL TANK ACCESS PANEL 74A HAS MINOR FRETTING CORROSION ON MATING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999031200950 19990312 00950 EU 1999 3 12 QXEA9900339 1 19990219 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU RT FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT WING FUEL TANK ACCESS PANEL 74F HAS MINOR FRETTING CORROSION ON MATING SURFACE AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-4 PARAGRAPH 4, PAGE 9, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999031200951 19990312 00951 EU 1999 3 12 QXEA9900340 1 19990209 A 2810 PANEL FOKKER F28 F28MK4000 4990810 EU FUEL TANK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LIGHT FRETTING CORROSION AROUND SCREW HOLES ON LOWER WING FUEL TANK ACCESS PANEL 73B. REPAIRED IAW FOKKER SRM 51- 10-04 PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 1999031200952 19990312 00952 EU 1999 3 12 QXEA9900341 1 19990218 A 5522 SKIN FOKKER F28 F28MK4000 4990810 EU LT ELEVATOR LIGHTNING STRIKE A QXEA K NONE C F.O.D. IN INSP/MAINT 1 NM 09 483US 11233 PDX - LEFT-HAND ELEVATOR HAS BURN MARK AT LIGHTENING EXIT HOLE AT TIP OUTBOARD EDGE, 9 FORWARD OF TRAILING EDGE. REPAIR ED IAW FOKKER SRM 51-31-05 PAGE 8-9, PARAGRAPH 7 A-E. 2 L 7 2 4F RT A20EU 1999031200953 19990312 00953 EU 1999 3 12 QXEA9900342 1 19990211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME 17565 HAS CRACKED CLIP BELOW STRINGER 52. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-07. 2 L 7 2 4F RT A20EU 1999031200954 19990312 00954 EU 1999 3 12 QXEA9900343 1 19990211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME 17565 HAS CRACKED CLIP AT STRINGER 49. REPAIRED IAW FOKKER SRM 51-31-07. 2 L 7 2 4F RT A20EU 1999031200955 19990312 00955 EU 1999 3 12 QXEA9900344 1 19990211 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME 17565 IS CRACKED AT PREVIOUS REPAIR AT STRINGER 71A. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200956 19990312 00956 EU 1999 3 12 QXEA9900345 1 19990211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 19075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME 19075 HAS CRACKED CLIP AT STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200957 19990312 00957 EU 1999 3 12 QXEA9900346 1 19990211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - OBLIQUE 16-2 HAS CRACKED CLIP ON AFT SIDE OF STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1999031200958 19990312 00958 EU 1999 3 12 QXEA9900347 1 19990211 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CASTELLATION IS CRACKED AT FRAME 9305, AT STRINGER 37. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 1. 2 L 7 2 4F RT A20EU 1999031200959 19990312 00959 EU 1999 3 12 QXEA9900348 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK LIGHT SCORING IN BOTTOM OF TRACK BETWEEN FRAMES 5805 AND 6305. BURNISHED SEAT TRACK S TO REMOVE DAMAGE. REMOVED APPROXIMATELY .007 MATERIAL, REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200960 19990312 00960 EU 1999 3 12 QXEA9900349 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK LIGHT SCORING ON TOP RAILS AT FRAME 6305. BURNISHED SEAT TRACK TO REMOVE DAMAGE. R EMOVED APPROXIMATELY .006 MATERIAL, REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200961 19990312 00961 EU 1999 3 12 QXEA9900350 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6805 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK LIGHT CHAFING ON INBOARD FLANGE BETWEEN FRAMES 5805 AND 6805. BURNISHED SEAT TRACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .009 MATERIAL, REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200962 19990312 00962 EU 1999 3 12 QXEA9900351 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK LIGHT SCORING IN BOTTOM OF SEAT TRACK BETWEEN FRAMES 6805 AND 7305. BURNISHED SEAT TRACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .007 MATERIAL, REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200963 19990312 00963 EU 1999 3 12 QXEA9900352 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805-8305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK LIGHT SCORING IN BOTTOM OF TRACK BETWEEN FRAMES 7805 AND 8305. BURNISHED SEAT TRACK TO REMOVED DAMAGE. REMOVED APPROXIMATELY .004 MATERIAL, REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200964 19990312 00964 EU 1999 3 12 QXEA9900353 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305-9305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK LIGHT SCORING IN BOTTOM OF SEAT TRACK BETWEEN FRAMES 8305 AND 9305B. BURNISHED SEAT TRACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .010 MATERIAL, REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200965 19990312 00965 EU 1999 3 12 QXEA9900354 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305-9305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK GOUGES AND SCORING AROUND TRACK HOLES BETWEEN FRAMES 8305 AND 9305B. BURNISHED SEAT TRACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .006 MATERIAL, REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200966 19990312 00966 EU 1999 3 12 QXEA9900355 1 19990212 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND INBOARD SEAT TRACK CAMLOC RECEPTACLE BROKEN AT FRAME 9305B. REPLACED RECEPTACLE PER FOKKER SRM 51-31-0 1. 2 L 7 2 4F RT A20EU 1999031200967 19990312 00967 NM 1999 3 12 99FDEA00091 1 19990310 A 3150 ANNUNCIATOR PANL BOEING 727 7272S2F 1384O81 NM RT COCKPIT MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 208FE 22930 CREW SAW BRIGHT FLASH AND A LITTLE SMOKE BEHIND 2ND OFFICER'S PANEL WHEN NR 3 FUEL BOOSTS WERE TURN OFF. BOOST TURNED B ACK ON, NO SMOKE EVIDENT. COULD NOT DUP. REMOVED 2ND OFFICER'S FUEL SYS ANNUNCIATOR PANELS AND INSPECTED BEHIND HIS ST ATION. FOUND NO EVIDENCE OF BURN OR FIRE. NO POPPED CIRCUIT BREAKERS, NO MAINTENANCE PERFORMED. 2 L 7 3 4F A3WE 1999031200968 19990312 00968 WP 1999 3 12 99FDEA00092 1 19990309 A 5711 SPAR DOUG DC10 DC1030F 3023504 WP WS 118-112 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 LEFT AFT UPPER CORNER OF THE CENTER WING BOX AT BS 118 TO 112 TO INCLUDE THE CLOS RIB AND ATTACH UPPER SKIN PLATES AT BS 1370 TO 1358 WERE FOUND WITH EXFOLIATION CORROSION DURING C-CHECK INSP IN THE LT MLG WHEEL WELL. ALL CORROSION HAS BEE N REMOVED, WAITING FOR THE ENG AUTH FOR REPAIR OR DISPOSITION. 2 L 7 3 4F RT A22WE 1999031200969 19990312 00969 NM 1999 3 12 SCNA99045 1 19990307 A 3350 LIGHT BOEING 727 727225 1384077 NM ROW 18DEF INOP A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE FLOOR EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE AT SEAT ROW 18DEF. RELAMPED T HE EMERGENCY FLOOR TRACK LIGHTING AT SEAT ROW 18DEF. LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999031600001 19990316 00001 EU 1999 3 16 MALA976356 1 19990215 A 3230 RELAY SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 424XJ 424 DURING FLIGHT, GEAR WOULD NOT COME DOWN WHEN SELECTED. CREW PERFORMED EMERGENCY EXTENSION. LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED RELAY AND RELAY SOCKET 156A, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999031600002 19990316 00002 NM 1999 3 16 MWEA99086 1 19990224 A 2560 113317 GIRT BAR DOUG MD88 MD88 3023688 NM GALLEY DOOR LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 810ME 48072 THE FORWARD GALLEY SERVICE DOOR SLIDE GIRT BAR IS DIFFICULT TO DISARM. MTC CLEANED AND LUBRICATED SPRING, LATCH AND REI NSTALLED DOOR SLIDE GIRT BAR. 2 L 7 2 4F RT A6WE 1999031700002 19990317 00002 WP 1999 3 17 AT9900167 1 19990215 A 5230 BRACKET DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A CORRODED ANGLE BRACKET ON FORWARD LOWER CARGO DOOR. REMOVED L ANGLE BRAC KET, FABRICATED NEW ANGLE, REPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-05 FIG 7 PAGE 8. 2 L 7 2 4F A6WE 1999031700003 19990317 00003 NM 1999 3 17 UPS99228915 1 19990308 A 5712 RIB BOEING 727 727173C 1384059 NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, 7TH RIB FROM I/B END CRACKED AT FASTENER HOLE. REPAIRED PER SRM 51-30-5. 2 L 7 3 4F A3WE 1999031700004 19990317 00004 NM 1999 3 17 ABXA9900173 1 19990304 A 3231 MECHANISM DOUG BOEING 767 767281 1385109 NM LDG GEAR DOORS LACK OF LUBE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 773AX 22788 LANDING GEAR DOORS SLOW TO CLOSE ON GEAR RETRACTION. GEAR DOOR AMBER LIGHT, NO EICAS MESSAGE. FOUND NOSE GEAR DOOR REL EASE MECHANISM NOT LOCKING PROPERLY. LUBRICATED MECHANISM, DOOR OPS CHECKED NORMAL. 2 L 7 2 4F TR A1NM 1999031800001 19990318 00001 1999 3 18 VTZA99003 4 19990103 A 3418 45150340 AOA SENSOR CNDAIR CL600 CL6002B19 EA E/E COMPT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 620BR 7179 FLT 6755 - IAD-JAX - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO STALL FAIL WARNING ILLUMINATED. AIRCRA FT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED AOA SENSOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999031800004 19990318 00004 WP 1999 3 18 AT9900143 1 19990122 A 5347 FLOOR TRACK DOUG DC9 DC932 3022066 WP BS 756 & 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FLOOR TRACKS AT THE AFT PIT STA 756 TO 780 AND ON THE RIGHT LOWER SIDE AT STA 935 TO 996 WITH CORROSION. MECHANICALLY REMOVED CORROSION, FABRICATED NEW SECTION OF FLOOR TRACKS, DRILLED, DEBURRE D, COUNTERSUNK, TREATED AND PRIMED IAW DC9 SRM 51-10-3, 51-10-4 AND 53-05-3. 2 L 7 2 4F A6WE 1999031800005 19990318 00005 NM 1999 3 18 DL738990341 1 19990219 A 3350 303 BULB BOEING 737 737832 13844CF NM ROW 10 DEF FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 371DA 29619 UPON L/O, FOUND SEAT 10 DEF EMERGENCY TRACK LIGHTING MISSING 2 BULBS AND COVER. REPLACED BULBS AND COVER, OPS CHKS NORM AL. 2 L 7 2 4F TR A16WE 1999031800006 19990318 00006 NM 1999 3 18 DL738990371 1 19990224 A 3350 BULB 767GE BOEING 737 737832 13844CF NM RT EMER EXIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 375DA 29623 RIGHT OVERWING EMERGENCY LIGHT INOP. RELAMPED, CHECKED GOOD PER MM. 2 L 7 2 4F TR A16WE 1999031800007 19990318 00007 NM 1999 3 18 DL72L990376 1 19990210 A 5320 BULKHEAD CHORD BOEING 727 727232 1384082 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 FOUND DURING MV2 CORROSION VISIT NRC 221, CORROSION ON LOWER CHORD OF STA 950 BULKHEAD JUST O/B OF STR 29 RT. REPAIRED PER SRM 53-10-9 FIG 12. 2 L 7 3 4F A3WE 1999031800008 19990318 00008 WP 1999 3 18 TWAA9903202 1 19990301 A 3350 20131A BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 15-33 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 985U 49703 EGRESS LIGHTING INOP AT ROW 15 TO 33. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1999031800009 19990318 00009 1999 3 18 99UAL900122 4 19990220 A 2330 176420F747 VIDEO BOX SEXTANT INFL BOEING 747 747422 1384935 NM ROW 2A ODOR A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 117UA 28810 SEAT 2A FOOTREST MOTOR HAD BAD ELECTRICAL BURNING SMELL COMING FROM IT. *S/D* THE CAUSE OF THE ODOR WAS FOUND TO BE EMAN ATING FROM THE VIDEO DISTRIBUTION BOX, LOCATED UNDER THE SEAT. THE VDB, PART OF THE B/E2000M IN-SEAT VIDEO SYSTEM, WAS R EPLACED. THE MANUFACTURER, SEXTANT IN-FLIGHT SYSTEMS, HAS BEEN ALERTED AND WILL PROVIDE ANY FINDINGS WHEN THE UNIT REAC HES THEIR REPAIR FACILITY. 2 L 7 4 4F RT A20WE 1999031900001 19990319 00001 WP 1999 3 19 TWAA9903801 1 19990226 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 200 LIGHTNING STRIKE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND A LIGHTNING BURN AT STA 700, 2 INCHES BELOW LONGER 27L. IT HAD BEEN BLENDED AND INDICAT ION OF CRACK. NDT CHECK FOUND NO CRACK INDICATION. REPAIRED PER SRM 53-04, PG 21 TABLE B, CONDITION PARAGRAPH 3. INST ALLED FLUSH 5/32 SOLID RIVET. 2 L 7 2 4F A6WE 1999031900002 19990319 00002 WP 1999 3 19 TWAA9903802 1 19990225 A 5320 BRACKET DOUG DC9 DC931 3022065 WP NLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND IN NLG WHEEL WELL A CRACK IN THE I/B BRACKET ON THE AFT BULKHEAD FOR HYD SWIVAL GLAND AN TI-ROTATION ARM. REMOVED CRACKED BRACKET AND FABRICATED NEW BRACKET WITH MATERIAL IDENTIFIED ON ORIGINAL BRACKET AND IN STALLED ORIGINAL FASTENERS. 2 L 7 2 4F A6WE 1999031900003 19990319 00003 WP 1999 3 19 TWAA9903803 1 19990222 A 5321 FLOOR DOUG DC9 DC931 3022065 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CORROSION AROUND THE RIVETS IN THE CENTER FLOOR PANEL, BETWEEN LAVATORIES. THE EDGE STI FFENERS WERE CRACKED AND WORN. REPLACED PANEL PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999031900004 19990319 00004 WP 1999 3 19 TWAA9903804 1 19990223 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 617 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND A CRACK IN THE INTERCOSTAL BELOW FLOORBEAM U-CHANNEL AT STA 617. REMOVED AND REPLACED C RACKED INTERCOSTAL PER SPM 6-70-01, PAGE 3, AND USED HI-LOK FASTENERS PER SPM 6-30-07, PAGE 1 AND 2. 2 L 7 2 4F A6WE 1999031900005 19990319 00005 WP 1999 3 19 TWAA9903805 1 19990303 A 5320 TEE CAP DOUG DC9 DC931 3022065 WP BS 699 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CORROSION ON TEE CAP AT STA 699, APPROX 58.2 IN ON SLANTED PANEL. MECHANICALLY REMOVED CORROSION PER TWA STD PROCESSES 6-80-01. 2 L 7 2 4F A6WE 1999031900006 19990319 00006 WP 1999 3 19 TWAA9903806 1 19990303 A 5320 WEB DOUG DC9 DC931 3022065 WP LT MLG WW CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CORROSION IN LT WHEEL WELL UNDER FWD SIDE OF OVERHEAD LIGHT. REMOVED SURFACE CORROSION PER SPM 6-80-01. 2 L 7 2 4F A6WE 1999031900007 19990319 00007 WP 1999 3 19 TWAA9903807 1 19990304 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND LONGERON CRACKED AT ATTACH TO FORMER RING STA 160, LONGERON 3L. REPLACED LONGERON FROM STA 160 TO 170 WITH NEW LONGERON SPLICE PER SRM 53-02 PAGE 48 AND SPM 6-70-01, FASTENERS PER 51-30-0. 2 L 7 2 4F A6WE 1999031900008 19990319 00008 WP 1999 3 19 TWAA9903808 1 19990305 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 1059 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND IN AFT ACCESSORY COMPT A FORMER AT STA 1059 WITH A WORN AREA AT LONGERON 8L. REPAIRED W ORN AREA IN FORMER RING PER SRM 53-03, FIG 4. 2 L 7 2 4F A6WE 1999031900009 19990319 00009 WP 1999 3 19 TWAA9903809 1 19990307 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 1066 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND A HOLE WORN IN LONGERON 8L AT STA 1066. REPLACED LONGERON FROM STA 1065 TO 1087. SPLIC ED PER SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 1999031900010 19990319 00010 WP 1999 3 19 TWAA9903810 1 19990307 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CENTER CABIN FLOOR CENTER SUPPORT BEAM WITH CORROSION AT STA 218. REPLACED FLOORBEAM PE R SPM 6-70-01, USING ORIGINAL TYPE HARDWARE, STA 160 TO 218. 2 L 7 2 4F A6WE 1999031900011 19990319 00011 WP 1999 3 19 TWAA9903811 1 19990303 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 1065 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND AFT ACCY COMPT WITH WORN AREA ON LONGERON 8R AT STA 1065. REPAIRED WORN AREA IN LONGERO N 8R AT STA 1065 WITH A SPLICE REPAIR PER SRM 53-02. 2 L 7 2 4F A6WE 1999031900012 19990319 00012 WP 1999 3 19 TWAA9903812 1 19990302 A 5320 PANEL DOUG DC9 DC931 3022065 WP NLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND IN NLG WHEEL WELL AN 8 INCH CRACK IN THE WW LOWER SURFACE OF CANTED PRESSURE PANEL, 2 IN FWD OF E & E DOOR. REMOVED AND REPLACED Y CHORD ANGLE PER DOUGLAS PRINT 9911500. 2 L 7 2 4F A6WE 1999031900013 19990319 00013 WP 1999 3 19 TWAA9903813 1 19990303 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 266 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 FOUND CHAIR TRACK NR 3 BLENDED OUT OF LIMITS AT STA 266, APPROX 22 IN LBL. INSTALLED NEW TRACK SPLICED IN AT STA 266 TO STA 198. SPLICED PER SEAT TRACK SPLICE REPAIR SRM 53-05 PG 7 FIG 4, SHEET 1. 2 L 7 2 4F A6WE 1999031900014 19990319 00014 WP 1999 3 19 TWAA9903814 1 19990305 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-315 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK RBL 22 AT STA 200 TO 315. REPLACED TRACK FROM STA 200 TO STA 3 15 PER SRM 53-05, FIG 4. 2 L 7 2 4F A6WE 1999031900015 19990319 00015 WP 1999 3 19 TWAA9903815 1 19990307 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 569-579 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND FUSELAGE SKIN CORRODED UNDER PREVIOUSLY INSTALLED REPAIR DOUBLER BETWEEN STA 569 AND 579 , LONGERON 29L TO 29R. REMOVED CORROSION PER SPM 6-80-01. REPAIRED PER SRM 53-04, FIG 43. 2 L 7 2 4F A6WE 1999031900016 19990319 00016 NM 1999 3 19 HNAA9900035 1 19990310 A 3260 864202841102 SENSOR DHAV DHC8 DHC8102 2809003 NM RT MLG DAMAGED A HNAA O OTHER N FALSE WARNING CL CLIMB 1 EA 07 909HA 018 AFTER DEPARTURE GEAR RETRACTED, RIGHT HAND MAIN GEAR RED LIGHT DID NOT ILLUMINATE AND THE GREEN LIGHT STAYED ON. CYCLED GEAR, NO CHANGE. REPLACED RIGHT HAND DOWNLOCK PROXIMITY SENSOR DUE TO DAMAGED WIRING AND CONDUIT. 2 H 7 2 4T RT A13NM 1999031900017 19990319 00017 NM 1999 3 19 AT9900185 1 19990110 A 5320 ANGLE BOEING 737 737214 138446R NM BS 420-440 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AND A CRACK ABOVE SIDE WALL AND FLOOR ATTACHMENT AT BS 420-440. MECHANICALLY CLEAN CORROSION, FABRICATED ANGLE SUPPORT REPAIR, HEAT TREATED, DRILLED, DEBURRED, PRIMED AND INSTALLED IA W B737 SRM 51-40-3, 51-10-6, 53-10-1, 51-10-2, 51-21-31, 51-30-2, AND HEAT TREATED IAW BAC 5602. 2 L 7 2 4F A16WE 1999031900018 19990319 00018 NM 1999 3 19 AT9900186 1 19990116 A 5320 ANGLE BOEING 737 737214 138446R NM BS 300 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 460AT 20158 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE LAVATORY WALL HAT SECTION AT BS 300 LBL 35-50 HEAVY EXFOLIATION. M ECHANICALLY REMOVED CORROSION, REMOVED HAT SECTION AND L ANGLE AND FABRICATED NEW REPLACEMENT SECTIONS, HEAT TREATED, PR IMED, AND INSTALLED IAW B737 SRM 51-10-6, 53-10-1, 51-40-3, 51-10-2, AND 51-21-31. 2 L 7 2 4F A16WE 1999031900019 19990319 00019 WP 1999 3 19 AT9900187 1 19990218 A 5347 5956039511N TIE DOWN DOUG DC9 DC932 3022066 WP BS 427-503 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO PIT TIEDOWN TRACK AT BS 427-503 RIGHT SIDE CORRODED. OR DERED A NEW SECTION OF TRACK AND INSTALLED IAW DC9 SRM 51-10-4, AND 53-05 PG 1014. 2 L 7 2 4F A6WE 1999031900020 19990319 00020 WP 1999 3 19 AT9900188 1 19990216 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 929 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT CABIN FRAME BS 929 LBL 2-3L AND LBL 3R. CUT OUT CORRODED SE CTIONS, INSTALLED TWO DOUBLERS, FILLERS, AND ANGLES IAW DC9 SRM 51-10-3, 51-30-2, AND 53-03 FIG 4. 2 L 7 2 4F A6WE 1999031900021 19990319 00021 WP 1999 3 19 AT9900189 1 19990214 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 965-985 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE AFT PIT WEB AT BS 965 TO 985 STRINGER 28-29R CORRODED ON BOTH SIDES . FABRICATED NEW INTERCOSTAL WEB, HEAT TREATED, PRIMED, AND INSTALLED REPAIR IAW DC9 SRM 51-10-2A, 51-10-5, 51-30-8, 53 -03 FIG 1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999031900022 19990319 00022 EU 1999 3 19 MALA976384 1 19990309 A 2435 23030031 STARTER GEN SAAB SF340 SF340A 7850100 EU LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 98XJ 098 AFTER DEPARTURE THE LEFT GEN OVERTEMP CAUTION LIGHT CAME ON. AMPERAGE LOAD WAS OBSERVED TO BE NORMAL, ABOUT 100 AMPS BE FORE SHUTTING OFF. RETURNED TO MSP. MAINTENANCE REPLACED LEFT STARTER GEN, IAW SF340 AMM 24-31-05, AND INSTALLED NEW L EFT GEN SWITCH, IAW SF340 AMM (P/N MS27406-2). OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031900023 19990319 00023 EU 1999 3 19 MALA976385 1 19990307 A 2421 31342003 GENERATOR SAAB SF340 SF340A 7850100 EU RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 112XJ 340A112 RIGHT ENGINE AC GEN FAILED IN CLIMBOUT. RETURNED TO MSP. MAINTENANCE REPLACED RT AC GEN. OPS AND LEAKS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999031900024 19990319 00024 EU 1999 3 19 MALA976386 1 19990307 A 3230 UPLOCK SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 420XJ 420 GEAR WOULD NOT LOCK UP AFTER DEPARTURE. RETURNED TO DTW. MAINTENANCE NOTED ICE ON ALL THREE GEAR UPLOCK ROLLERS. DEIC ED AFFECTED AREAS. TEST FLIGHT SATISFACTORY. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999031900025 19990319 00025 EU 1999 3 19 MALA976387 1 19990309 A 2434 23080031 GENERATOR SAAB SF340 340B 7860101 EU LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 438XJ 438 LEFT DC GEN OVERHEAD LIGHT ILLUMINATED WHILE IN FLIGHT, QRH PROCEDURE FOLLOWED. GEN WAS ABLE TO BE RESET BUT WITHIN 1 M INUTE TRIPPED AGAIN. AFTER ILLUMINATING FOR THE SECOND TIME THE LEFT GEN OVERTEMP LIGHT ILLUMINATED AND REMAINED ON. R ETURNED TO DTW. MAINTENANCE REPLACED LEFT DC GEN. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999031900026 19990319 00026 EU 1999 3 19 MALA976388 1 19990308 A 3230 D49410001 CONTROL UNIT SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 429XJ 429 WHEN GEAR SELECTED DOWN, GEAR MOTOR RAN CONTINUOUSLY WITH NO GEAR EXTENSION, FOUND F7 CB POPPED, RESET CB, GEAR FUNCTION ED NORMAL. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR CONTROL UNIT AND CB AT F7 (P/N M53320-5). ALL C HECKS GOOD. 2 L 7 2 4T RT A52EU 1999031900027 19990319 00027 NM 1999 3 19 K3HA990021 1 19990302 A 3350 3071BPEGPL LENS BOEING 727 727225 1384077 NM ROW 30D MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY PATH LIGHT AT 30D MISSING. INSTALLED BULB (P/N 07912-3) AND LENS ON ROW 30D RED LENS. 2 L 7 3 4F A3WE 1999031900028 19990319 00028 NM 1999 3 19 K3HA990022 1 19990306 A 3350 LIGHT BOEING 727 727225 1384077 NM ROW 2 INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY PATH LIGHT RED PAX ROW NR 2 INOP. REMOVED AND REPLACED LENS (P/N 07912-3), BULB (P/N 3071BPEGPL) AND LIGHT SO CKET CHECKS OK REF MM 33-50-01. 2 L 7 3 4F A3WE 1999031900029 19990319 00029 NM 1999 3 19 RAAA99B2004 1 19990310 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1132 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND SKIN DENTED BETWEEN STR 26R TO 29R AT BS 1132. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1999031900030 19990319 00030 NM 1999 3 19 RAAA99B2005 1 19990310 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1095 GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND SKIN GOUGED BETWEEN STR 27R TO 28R AT BS 1095. INSTALLED REPAIR DOUBLER IAW SRM 5330. 2 L 7 3 4F A3WE 1999031900031 19990319 00031 NM 1999 3 19 RAAA99B2006 1 19990310 A 5330 SKIN BOEING 727 72722C 138400F NM BS 660 GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND DEEP GOUGE IN SKIN BS 660 AT STR 25R. INSTALLED REPAIR IAW SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1999031900032 19990319 00032 NM 1999 3 19 RAAA99B2007 1 19990310 A 5320 SILL BOEING 727 72722C 138400F NM CARGO DOORWAY CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED S6 INSPECTION PER CARD S6 52103, FOUND LOWER FWD CARGO DOOR SILL VERTICAL WEB AT STR 26R AND BS 520 THR U 570 CORRODED. FABRICATED REPLACEMENT WEB IAW SRM 51-20-1 FIG 7 FROM 063 7075T6 IAW SRM 53-10-2 FIG 3 AND INSTALLED IA W 51-30-2. 2 L 7 3 4F A3WE 1999031900033 19990319 00033 NM 1999 3 19 CALA9900237 1 19990310 A 5753 SKIN BOEING 757 757224 1384958 NM RT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND RT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED AND DENTED O/B OF INBOARD TRACK. REPAIRED IAW SRM 57-53-01, PAGE 205 AND SRM 51-70-17, PARAGRAPH 3A. 2 L 7 2 4F RT A2NM 1999031900034 19990319 00034 NM 1999 3 19 CALA9900238 1 19990310 A 5730 SKIN BOEING 757 757224 1384958 NM WS 421 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND A 10 INCH CRACK IN LT WING LEADING EDGE SKIN BETWEEN NR 3 AND NR 4 SLATS AT OSS 421. REPAIRED SKIN IAW ECRA 5721-01009. A DIP WAS ISSUED TO REINSPECT REPAIR EVERY 1,000 FLIGHT HOURS AND MAKE A PERMANENT REPAIR WITHIN 18 M ONTHS OR AT NEXT 4C-CHECK, WHICHEVER COMES FIRST. 2 L 7 2 4F RT A2NM 1999031900035 19990319 00035 NM 1999 3 19 CALA9900239 1 19990310 A 5730 SKIN BOEING 757 757224 1384958 NM WS 421 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN BETWEEN NR 7 AND NR 8 SLATS AT OSS 421. REPAIRED SKIN IAW ECRA 5721-01009. A DIP WAS ISSUED TO REINSPECT REPAIR EVERY 1,000 FLIGHT HOURS AND MAKE A PERMANENT REPAIR WITHIN 18 MO NTH OR AT NEXT 4C-CHECK, WHICHEVER COMES FIRST. 2 L 7 2 4F RT A2NM 1999031900036 19990319 00036 NM 1999 3 19 CALA9900240 1 19990310 A 5230 STRUCTURE BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND IMPACT DAMAGE TO AFT CARGO DOOR AFT CORNER AND FORWARD CORNER. THE AFT CARGO DOOR AFT AND FORWARD CORN ERS WERE REMOVED AND NEW CORNERS WERE FITTED IAW SRM 52-30-02. 2 L 7 2 4F RT A2NM 1999031900037 19990319 00037 NM 1999 3 19 CALA9900241 1 19990310 A 5230 BEAM BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND IMPACT DAMAGE TO AFT CARGO HOLD DOOR LOWER EDGE BEAM. THE AFT CARGO HOLD DOOR LOWER EDGE BEAM WAS REMO VED AND A NEW LOWER EDGE BEAM WAS FITTED IAW SRM 52-30-02 AND SRM 52-30-03. 2 L 7 2 4F RT A2NM 1999031900038 19990319 00038 EA 1999 3 19 COMA9960101 1 19990309 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 710CA 7241 FLAPS FAILED AT 45 DEGREES. COULD NOT DUPLICATE. RESET FLAP SYSTEM AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999031900039 19990319 00039 EA 1999 3 19 COMA9960102 1 19990310 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER O OTHER AP APPROACH 1 SO 01 710CA 7241 FLAPS FAILED AT 45 DEGREES. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999031900040 19990319 00040 EU 1999 3 19 QXEA9900381 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND OUTBOARD SEAT TRACK MINOR NICKS AND GOUGES AROUND SEVERAL TRACK HOLES BETWEEN FRAMED 10966 AND 12405. B URNISHED SEAT TRACK TO REMOVED DAMAGE. REMOVED APPROXIMATELY .009 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900041 19990319 00041 EU 1999 3 19 QXEA9900382 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - RIGHT-HAND OUTBOARD SEAT TRACK MINOR SCORING IN BOTTOM OF TRACK BETWEEN FRAMES 10966 AND 15205. BURNISHED SEAT TR ACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .008 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900042 19990319 00042 EU 1999 3 19 QXEA9900383 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LEFT-HAND OUTBOARD SEAT TRACK MINOR SCORING IN BOTTOM OF SEAT TRACK BETWEEN FRAMES 6805 AND 7305. BURNISHED SEAT TRACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .003 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900043 19990319 00043 EU 1999 3 19 QXEA9900384 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LEFT-HAND OUTBOARD SEAT TRACK MINOR NICKS AND GOUGES AROUND TRACK HOLES 3 FORWARD OF FRAME 6305. BURNISHED SEAT T RACKS TO REMOVE DAMAGE. REMOVED APPROXIMATELY .004 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900044 19990319 00044 EU 1999 3 19 QXEA9900385 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305-8805 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LEFT-HAND OUTBOARD SEAT TRACK SCORING IN BOTTOM OF SEAT TRACK BETWEEN FRAMED 7305 AND 8805. BURNISHED SEAT TRACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .003 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900045 19990319 00045 EU 1999 3 19 QXEA9900386 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8805-9305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LEFT-HAND OUTBOARD SEAT TRACK SCORING IN BOTTOM OF SEAT TRACK BETWEEN FRAME 8805 AND 9305A. BURNISHED SEAT TRACK TO REMOVE DAMAGE. REMOVED APPROXIMATELY .005 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900046 19990319 00046 EU 1999 3 19 QXEA9900387 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805-10966 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LEFT-HAND OUTBOARD SEAT TRACK AREAS OF LIGHT SCORING IN TRACK BOTTOM BETWEEN FRAME 9805C AND 10966. BURNISHED SEA T TRACK TO REMOVE CORROSION. REMOVED APPROXIMATELY .004 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900047 19990319 00047 EU 1999 3 19 QXEA9900388 1 19990211 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13345 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LEFT-HAND OUTBOARD SEAT TRACK SCORING ON TRACK BOTTOM BETWEEN FRAMES 13345 AND 13815. BURNISHED SEAT TRACK TO REM OVE DAMAGE. REMOVED APPROXIMATELY .002 MATERIAL. REF FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031900048 19990319 00048 EU 1999 3 19 QXEA9900389 1 19990210 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 483US 11233 PDX - REPAIR CLIP HAD BEEN DAMAGED BY RIVET SET FROM RIVET GUN DURING RIVET INSTALLATION. REPAIRED IAW FOKKER SRM 53-02 -13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900049 19990319 00049 EU 1999 3 19 QXEA9900390 1 19990210 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - STRINGER 35 IS CRACKED BETWEEN FRAME 11905 AND 12405. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 8, SRM 51-10-05, 51- 10-4 AND 51-31-01. 2 L 7 2 4F RT A20EU 1999031900050 19990319 00050 EU 1999 3 19 QXEA9900391 1 19990209 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CLIP CRACKED AT FRAME 12405 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900051 19990319 00051 EU 1999 3 19 QXEA9900392 1 19990209 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CLIP CRACKED AT FRAME 13345 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900052 19990319 00052 EU 1999 3 19 QXEA9900393 1 19990209 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CLIP CRACKED AT FRAME 13345 AND STRINGER 36. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900053 19990319 00053 EU 1999 3 19 QXEA9900394 1 19990209 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CASTELLATION CRACKED AT FRAME 13815A AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900054 19990319 00054 EU 1999 3 19 QXEA9900395 1 19990209 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CASTELLATION CRACKED AT FRAME 13815A AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900055 19990319 00055 EU 1999 3 19 QXEA9900396 1 19990215 A 5220 BEAM FOKKER F28 F28MK4000 4990810 EU FRAME 11083 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - BOX BEAM ABOVE LEFT-HAND AFT EMERGENCY EXIT APERTURE HAS TOOLING MARK 9 INCHES AFT OF FRAME 11083. REPAIRED IAW H ORIZON AIR EA 4-53-691. 2 L 7 2 4F RT A20EU 1999031900056 19990319 00056 EU 1999 3 19 QXEA9900397 1 19990213 A 5240 FRAME FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - AFT LOWER CORNER OF SERVICE EMERGENCY DOOR SURROUND REQUIRES REPAIR PATCH. REPAIRED IAW HORIZON AIR EA 4-53-685. 2 L 7 2 4F RT A20EU 1999031900057 19990319 00057 EU 1999 3 19 QXEA9900398 1 19990216 A 5240 FRAME FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - UPPER AFT CORNER OF SERVICE EMERGENCY DOOR SURROUND REQUIRED REPAIR PS REPAIR PATCH. REPAIRED IAW HORIZON AIR EA 4-53-685. 2 L 7 2 4F RT A20EU 1999031900058 19990319 00058 EU 1999 3 19 QXEA9900399 1 19990213 A 5240 FRAME FOKKER F28 F28MK4000 4990810 EU SERVICE DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FORWARD LOWER CORNER OF SERVICE EMERGENCY DOOR SURROUND REQUIRES REPAIR PATCH. REPAIRED IAW HORIZON AIR EA 4-53-6 85. 2 L 7 2 4F RT A20EU 1999031900059 19990319 00059 EU 1999 3 19 QXEA9900400 1 19990209 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CASTELLATION CRACKED AT FRAME 8805 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900060 19990319 00060 EU 1999 3 19 QXEA9900401 1 19990210 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CASTELLATION CRACKED AT FRAME 9305 AND STRINGER 37. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8. 2 L 7 2 4F RT A20EU 1999031900061 19990319 00061 EU 1999 3 19 QXEA9900402 1 19990209 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CASTELLATION CRACKED AT FRAME 9305A AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900062 19990319 00062 EU 1999 3 19 QXEA9900403 1 19990210 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FUSELAGE CABIN FRAME CASTELLATION IS CRACKED AT FRAME 10966 BETWEEN STRINGERS 40 AND 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900063 19990319 00063 EU 1999 3 19 QXEA9900404 1 19990209 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FUSELAGE CABIN FRAME CASTELLATION IS CRACKED AT FRAME 10966 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PA GE 3, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900064 19990319 00064 EU 1999 3 19 QXEA9900405 1 19990210 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FUSELAGE CABIN STRINGER NR 42 IS CRACKED AT INSULATION TIE HOLE, APPROXIMATELY 8 INCHES FORWARD OF FRAME 12405. R EPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, 51-10-05, 51-10-4 AND 51-31-01. 2 L 7 2 4F RT A20EU 1999031900065 19990319 00065 EU 1999 3 19 QXEA9900406 1 19990209 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FRAME CLIP CRACKED AT FRAME 5805 AND STRINGER 16. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900066 19990319 00066 EU 1999 3 19 QXEA9900407 1 19990213 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 6500 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - DENT IN LEFT-HAND FUSELAGE SKIN .095 DEEP AND 5.0 WIDE AT STATION 6500 WL-560. REPAIRED IAW FOKKER SRM 53-02-01. 2 L 7 2 4F RT A20EU 1999031900067 19990319 00067 EU 1999 3 19 QXEA9900408 1 19990208 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - LOWER NAV/COMM ANTENNA MOUNTING SURFACE ON FUSELAGE HAS CORROSION ON FUSELAGE SKIN. REPAIRED IAW FOKKER SRM 53-01 -01, PAGE 6, PARAGRAPH B(2)(B). 2 L 7 2 4F RT A20EU 1999031900068 19990319 00068 EU 1999 3 19 QXEA9900409 1 19990210 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FUSELAGE SKIN FOR NR 2 DME ANTENNA HAS LIGHT SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4B. 2 L 7 2 4F RT A20EU 1999031900069 19990319 00069 EU 1999 3 19 QXEA9900410 1 19990208 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FUSELAGE SKIN MOUNTING SURFACE FOR LOWER ATC ANTENNA HAS LIGHT SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-0 4, PAGE 9, PARAGRAPH 4B(2). 2 L 7 2 4F RT A20EU 1999031900070 19990319 00070 EU 1999 3 19 QXEA9900411 1 19990208 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FUSELAGE SKIN FOR MARKER BEACON ANTENNA HAS LIGHT SURFACE CORROSION ON AFT END. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH A, B(2). 2 L 7 2 4F RT A20EU 1999031900071 19990319 00071 EU 1999 3 19 QXEA9900412 1 19990211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - AFT CARGO BAY FRAME 16660 STRINGER 74 CLIP CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900072 19990319 00072 EU 1999 3 19 QXEA9900413 1 19990211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - AFT CARGO PIT FRAME 16060 AND STRINGER 73 CLIP CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900073 19990319 00073 EU 1999 3 19 QXEA9900414 1 19990212 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - AFT CARGO PIT FRAME 13815A BETWEEN STRINGERS 2 AND 3 CLIP CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031900074 19990319 00074 EU 1999 3 19 QXEA9900415 1 19990224 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - AFT CARGO DOOR APERTURE AFT SIDE HAD NUMEROUS DEEP GOUGES. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031900075 19990319 00075 EU 1999 3 19 QXEA9900416 1 19990210 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - DENT IN FORWARD CARGO DOOR INNER SKIN .170 DEEP AND 2.0 WIDE, ABOVE AFT HOOK LATCH MECHANISM. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 1999031900076 19990319 00076 EU 1999 3 19 QXEA9900417 1 19990211 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - FORWARD CARGO DOOR APERTURE IS CRACKED UNDER SUPPORT STRUT FITTING. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031900077 19990319 00077 EU 1999 3 19 QXEA9900418 1 19990209 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - AFT CARGO DOOR UPPER AFT CORNER DAMAGED. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999031900078 19990319 00078 EU 1999 3 19 QXEA9900419 1 19990219 A 7110 SKIN FOKKER F28 F28MK4000 4990810 EU COWL DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 PDX - HOLE CHAFED THROUGH OUTBOARD COWL DOOR SKIN AT PREVIOUS REPAIR BETWEEN FRAME 6 AND 7. REPAIRED IAW FOKKER SRM 51- 31-01. 2 L 7 2 4F RT A20EU 1999031900079 19990319 00079 WP 1999 3 19 ABXA9900174 1 19990218 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND LONGERON 17R AT STATION 1041 CRACKED. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999031900080 19990319 00080 WP 1999 3 19 ABXA9900175 1 19990218 A 5312 9915558236 CLIP DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER AT LONGERON 14 RIGHT CRACKED. REPLACED CLIP IAW DC9 SRM 51 -30-5 AND DWG 9915558. 2 L 7 2 4F A6WE 1999031900081 19990319 00081 WP 1999 3 19 ABXA9900176 1 19990218 A 5312 9915558238 BLKHD STIFFENER DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT LONGERON 15R. REPLACED CLIP IAW DC9 SRM 51-30-5 . 2 L 7 2 4F A6WE 1999031900082 19990319 00082 WP 1999 3 19 ABXA9900177 1 19990218 A 5330 541287064 SKIN DOUG DOUG DC9 DC941 302207N WP BS 1072 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND SKIN CRACKED BELOW LONGERON 14 RIGHT AT STATION 1072. REPAIRED SKIN IAW ABX REA D953-26826 MR. 2 L 7 2 4F A6WE 1999031900083 19990319 00083 WP 1999 3 19 ABXA9900178 1 19990218 A 5320 5956034525 FITTING DOUG DOUG DC9 DC941 302207N WP BS 794 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND SEAT TRACK ATTACH FITTING EXFOLIATED AT STATION 794 AND LONGERON 3 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999031900084 19990319 00084 SO 1999 3 19 SWIA971424 1 19990203 A 3620 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1 ENG DUCT ILLUMINATED A SWIA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 NM 07 578SW 120346 IN FLIGHT ENGINE SHUT DOWN NR 1 DUE TO LEFT DUCT LEAK LIGHT ON. REMOVED LEFT INBOARD LEADING EDGE. INSPECTED ALL CLAMP S AND TUBING. INSPECTED ALL OVERWING CLAMPS AND TUBING AND PACK AREA. RAN LEFT ENGINE FOR 10 MINUTES AND INSPECTED FOR LEAKS. NO LEAKS FOUND, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900085 19990319 00085 SO 1999 3 19 SWIA971425 1 19990205 A 3010 3D237606 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT WING FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 220SW 120288 RIGHT AND LEFT MIDDLE WING DEICE BOOTS FAILED DURING CLIMBOUT (FIRST FLIGHT CHECKS ON GROUND PRIOR TO FLIGHT OPERATION N ORMALLY). RETURNED TO SFO. REPLACED RIGHT AND LEFT MIDDLE WING DEICE BOOT EJECTOR VALVE. OPS CHECKED GOOD. NO LEAKS NOTED UPON INSPECTION. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900086 19990319 00086 SO 1999 3 19 SWIA971426 1 19990207 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118A NE LT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 271YV 120271 LEFT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO SMF. REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR IAW EM B 120 MM 32-32-10. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900087 19990319 00087 SO 1999 3 19 SWIA971427 1 19990208 A 3020 BOOT EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENG INLET FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 129AM 120119 LEFT ENGINE INLET DEICE BOOT FAILED IN FLIGHT, OUTSIDE AIR TEMP -50. RETURNED TO PDX. INSPECTED ENTIRE DEICE SYSTEM, T IGHTEN UP NUMEROUS LINES AND REPLACED BOTH WATER SEPARATORS. INFLATED ALL BOOTS WITH SHOP AIR AND INSPECTED. OPS CHECK DEICE SYSTEM, CHECKS GOOD ON DECK (RAN 20 MINUTES). NO LEAKS DETECTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900088 19990319 00088 SO 1999 3 19 SWIA971428 1 19990309 A 3020 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT, RT ENG INLET FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 204SW 120243 AFTER TAKEOFF, BOTH INLET AIR DEICE BOOTS FAILED. RETURNED TO SLC. REMOVED AND REPLACED PRESSURE REGULATOR VALVE IAW E MB 120 30-10-06. LEAK AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900089 19990319 00089 EA 1999 3 19 SWIA971429 1 19990309 A 5753 SKIN CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS DIRTY A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 406SW 7030 AIRCRAFT NEEDS LEFT AILERON TRIM WHEN FLAPS SET TO 45 DEGREES. DISCOVERED LEADING EDGE OF FLAP HAD RIDGE OF PAINT BUILD -UP FROM RECENT AIRCRAFT RE-PAINTING. RE-SURFACED LEADING EDGE OF FLAP IAW SERVICE LETTER RJ-SL-27-022 DATED 8/28/96. 2 L 7 2 4F 4 F RT A21EA E15NE 1999031900090 19990319 00090 NM 1999 3 19 P5CA9900230 1 19990301 A 5512 PANEL BOEING 747 747122 1384872 NM RT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT LOWER TRAILING EDGE PANEL 334 IS BADLY DELAMINATED ON HORIZ STAB. REMOVED AND REPLACED PANEL PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999031900091 19990319 00091 NM 1999 3 19 P5CA9900231 1 19990301 A 5320 DOUBLER BOEING 747 747122 1384872 NM BS 1335 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON UPPER DOUBLER HORIZONTAL BEAM ON AND UNDER ATTACH FITTING AT STA 1335 LBL 90. REMOVED CORROS ION AND PRIMED AND PAINTED PER SRM 53-10-02. 2 L 7 4 4F A20WE 1999031900092 19990319 00092 NM 1999 3 19 P5CA9900232 1 19990301 A 5280 SKIN BOEING 747 747122 1384872 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT AFT MAIN LANDING GEAR DOOR INNER SURFACE CRACK IN SKIN. FABRICATED DOUBLER AND INSTALLED, TREATED AND PRIMED PER S RM 51-40-02 AND 51-30-01. 2 L 7 4 4F A20WE 1999031900093 19990319 00093 NM 1999 3 19 P5CA9900233 1 19990301 A 5320 BEAM BOEING 747 747122 1384872 NM LT MLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON LEFT WHEEL WELL CEILING BEAM. REMOVED LIGHT CORROSION AND TREATED AND PRIMED PER SRM 53-10-0 1 AND 51-10-02. 2 L 7 4 4F A20WE 1999031900094 19990319 00094 NM 1999 3 19 P5CA9900234 1 19990301 A 5730 SKIN BOEING 747 747124 1384874 NM WS 429 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND RIGHT HAND WING UPPER SKIN OUTER SURFACE AT MID SPAR WL 429 STR 14. CORROSION REMOVED PER SRM 5 1-10-01, WITHIN SRM LIMITS 57-30-01. TREATED AREA PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900095 19990319 00095 NM 1999 3 19 P5CA9900235 1 19990303 A 5330 SKIN BOEING 747 747124 1384874 NM BS 520-740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 520-740, STR 23L UPPER LAP JOINT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. TREATED AREA PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900096 19990319 00096 NM 1999 3 19 P5CA9900236 1 19990305 A 5330 SKIN BOEING 747 747124 1384874 NM WS 197 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND RIGHT WING LOWER SKIN OUTER SURFACE, REAR SPAR WBL 197. CORROSION REMOVED PER SRM 51-10-01, WIT HIN SRM 57-30-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900097 19990319 00097 NM 1999 3 19 P5CA9900237 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 270-340 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 270-340, RBL 94, FLOOR PANEL SUPPORT RAIL. CORROSION REMOVED PER SRM 51-10-01, WIT HIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900098 19990319 00098 NM 1999 3 19 P5CA9900238 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 420-440 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 420 TO 440, RBL 104, FLOOR PANEL SUPPORT RAIL. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900099 19990319 00099 NM 1999 3 19 P5CA9900239 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 640-670 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 640 TO 670, RBL 104, FLOOR PANEL SUPPORT RAIL. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900100 19990319 00100 NM 1999 3 19 P5CA9900240 1 19990301 A 5314 KEEL BEAM BOEING 747 747124 1384874 NM BS 1480-1420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT LEFT HAND BODY GEAR WHEEL WELL KEEL BEAM UPPER WEB ADJACENT BS 1480 AND 1420. CORROSION REMO VED AND AREA TREATED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031900101 19990319 00101 NM 1999 3 19 P5CA9900241 1 19990302 A 5314 KEEL BEAM BOEING 747 747124 1384874 NM LT MLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND LEFT HAND WING GEAR WHEEL WELL KEEL BEAR UPPER SURFACE. CORROSION REMOVED AND AREA TREATED AS P ER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031900102 19990319 00102 NM 1999 3 19 P5CA9900242 1 19990304 A 5320 WEB BOEING 747 747124 1384874 NM BS 420-440 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BODY STATION 420 TO 440, RBL 90, VERTICAL WEB SURFACE. CORROSION REMOVED PER SRM 51-1 0-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 53-10-02. 2 L 7 4 4F A20WE 1999031900103 19990319 00103 NM 1999 3 19 P5CA9900243 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 960-980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK FLOOR SUPPORT LOWER FACE, BS 960 TO 980 RBL 18. CORROSION REMOVED PER SRM 51-10-01, W ITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900104 19990319 00104 NM 1999 3 19 P5CA9900244 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1140, RBL 11 TO 33, FLOOR SUPPORT LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900105 19990319 00105 NM 1999 3 19 P5CA9900245 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1220, RBL 60 TO 74 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900106 19990319 00106 NM 1999 3 19 P5CA9900246 1 19990228 A 5313 STRINGER BOEING 747 747124 1384874 NM BS 1354 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK BS 1354 STRINGER 18R STRINGER END FOUND CRACKED. STRINGER END REPAIRED PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 1999031900107 19990319 00107 NM 1999 3 19 P5CA9900247 1 19990303 A 5320 DECK BOEING 747 747124 1384874 NM BS 1416-1372 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1416 TO 1372, RBL 11, PRESSURE DECK SURFACE. CORROSION REMOVED PER SRM 51-10-01, W ITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900108 19990319 00108 NM 1999 3 19 P5CA9900248 1 19990303 A 5320 FORGING BOEING 747 747124 1384874 NM BS 1416-1438 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK FS 1416 TO 1438, RT WINDOW FORGING FORWARD CORNER. CORROSION REMOVED PER SRM 51-10-01 , WITHIN SRM 56-20-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900109 19990319 00109 NM 1999 3 19 P5CA9900249 1 19990303 A 5311 FRAME BOEING 747 747124 1384874 NM BS 1760 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK BS 1760 STR 14 TO 15R FRAME FLANGE FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04. 2 L 7 4 4F A20WE 1999031900110 19990319 00110 NM 1999 3 19 P5CA9900250 1 19990301 A 5320 SHEAR TIE BOEING 747 747124 1384874 NM BS 1960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 BULK CARGO STATION 1960 RBL 10 SHEAR TIE FOUND CRACKED AND CORRODED. CRACKED AREA TRIMMED PER SRM 51-10-01 AND SHEAR TI E REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1999031900111 19990319 00111 NM 1999 3 19 P5CA9900251 1 19990303 A 5320 FORGING BOEING 747 747124 1384874 NM BS 1980-2020 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1980 TO 2020, STR 20R-22R WINDOW FORGING (SEVERAL LOCATIONS). CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 56-20-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900112 19990319 00112 NM 1999 3 19 P5CA9900252 1 19990303 A 5320 BRACKET BOEING 747 747124 1384874 NM BS 2080 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2080 STR 26R, FRAME ATTACH BRACKET AT HI-LOK AREA. CORROSION REMOVED PER SRM 51-10 -01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900113 19990319 00113 NM 1999 3 19 P5CA9900253 1 19990228 A 5320 SHEAR TIE BOEING 747 747124 1384874 NM BS 2080 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT SHEAR TIE, BULK CARGO STA 2080, STR 43-44R. CORROSION REMOVED AND AREA TREATED AS PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031900114 19990319 00114 NM 1999 3 19 P5CA9900254 1 19990303 A 5313 STRINGER BOEING 747 747124 1384874 NM BS 2220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2220 STR 2R. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. A REA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900115 19990319 00115 NM 1999 3 19 P5CA9900255 1 19990302 A 5320 WEB BOEING 747 747124 1384874 NM BS 2220 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK BS 2220 BELOW STR 22R, WEB FOUND CRACKED. WEB REPAIRED IAW SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 1999031900116 19990319 00116 NM 1999 3 19 P5CA9900256 1 19990301 A 5320 ANGLE BOEING 747 747124 1384874 NM BS 2140-2160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON SUPPORT ANGLE, BULK CARGO COMPARTMENT CEILING AREA RT STA 2140 TO 2160. SUPPORT ANGLE REPLAC ED AS PER SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1999031900117 19990319 00117 NM 1999 3 19 P5CA9900257 1 19990302 A 5330 SKIN BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 RIGHT WING L/E CAVITY LOWER SKIN HAS AREA OF DELAMINATION JUST AFT OF NR 15 K/FLAP. FIBER GLASS REPAIRED AS PER SRM 51- 40-05 FIG 7. 2 L 7 4 4F A20WE 1999031900118 19990319 00118 NM 1999 3 19 P5CA9900258 1 19990304 A 5320 WEB BOEING 747 747124 1384874 NM BS 160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 160 LBL 11 HORIZONTAL WEB SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-02 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900119 19990319 00119 NM 1999 3 19 P5CA9900259 1 19990304 A 5320 WEB BOEING 747 747124 1384874 NM BS 240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 240 LBL 17 TO RBL 14, HORIZONTAL WEB SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900120 19990319 00120 NM 1999 3 19 P5CA9900260 1 19990304 A 5320 FITTING BOEING 747 747124 1384874 NM BS 260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 260 LBL 60 HANDLING FLOOR FITTING AFT SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900121 19990319 00121 NM 1999 3 19 P5CA9900261 1 19990304 A 5320 FITTING BOEING 747 747124 1384874 NM BS 320 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 320 LBL 50 FLOOR HANDLING FITTING AFT SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900122 19990319 00122 NM 1999 3 19 P5CA9900262 1 19990304 A 5320 FITTING BOEING 747 747124 1384874 NM BS 360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 360 LBL 40 FLOOR HANDLING FITTING AFT SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900123 19990319 00123 NM 1999 3 19 P5CA9900263 1 19990303 A 5320 FORGING BOEING 747 747124 1384874 NM BS 638 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 638 STR 20L-21L, WINDOW FORGING AFT EDGE. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 56-20-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900124 19990319 00124 NM 1999 3 19 P5CA9900264 1 19990303 A 5320 BRACKET BOEING 747 747124 1384874 NM BS 680 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 680, WL 200, LT FRAME ATTACH BRACKET UPPER SURFACE. CORROSION REMOVED PER SRM 51-1 0-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900125 19990319 00125 NM 1999 3 19 P5CA9900265 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 910 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 910 LBL 19 FLOOR SUPPORT HAT SECTION. CORROSION REMOVED PER SRM 51-10-01, WITHIN S RM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900126 19990319 00126 NM 1999 3 19 P5CA9900266 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1689 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1689 LBL 114 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-0 1 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900127 19990319 00127 NM 1999 3 19 P5CA9900267 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1800 LBL 83 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIM ITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900128 19990319 00128 NM 1999 3 19 P5CA9900268 1 19990303 A 5313 STRINGER BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1800 STRINGER 15L. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900129 19990319 00129 NM 1999 3 19 P5CA9900269 1 19990303 A 5313 STRINGER BOEING 747 747124 1384874 NM BS 2000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2000 STRINGER 17L AROUND RIVIT AREA. CORROSION REMOVED PER SRM 51-10-01, WITHIN SR M 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900130 19990319 00130 NM 1999 3 19 P5CA9900270 1 19990303 A 5320 TIE CLIP BOEING 747 747124 1384874 NM BS 2160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2160 STR 21L TIE CLIP. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIM ITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900131 19990319 00131 NM 1999 3 19 P5CA9900271 1 19990303 A 5313 STRINGER BOEING 747 747124 1384874 NM BS 2360 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK BS 2360 STRINGER 15L STRINGER END FOUND CRACKED. REPAIRED STRINGER AS PER SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 1999031900132 19990319 00132 NM 1999 3 19 P5CA9900272 1 19990301 A 5320 WALL BOEING 747 747124 1384874 NM LT MLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND LEFT HAND BLG W/W, OUTER WALL CAVITY ABOVE U/C DOOR SEQUENCE VALVE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999031900133 19990319 00133 NM 1999 3 19 P5CA9900273 1 19990303 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 460-480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK TIE DOWN TRACK FLANGE, BS 460 TO 480 LBL 32 WL 200. CORROSION REMOVED PER SRM 51-10-0 1, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900134 19990319 00134 NM 1999 3 19 P5CA9900274 1 19990304 A 5320 SHEAR PANEL BOEING 747 747124 1384874 NM BS 1100-1010 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1100 TO 1010 LBL 11 TO RBL 11 BELOW FLOOR SHEAR PANEL AT BOTH FACES. CORROSION REM OVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900135 19990319 00135 NM 1999 3 19 P5CA9900275 1 19990304 A 5320 SHEAR PANEL BOEING 747 747124 1384874 NM BS 1170-1260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1170 TO 1260 CENTER BELOW FLOOR SHEAR PANEL. CORROSION REMOVED PER SRM 51-10-01, W ITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900136 19990319 00136 NM 1999 3 19 P5CA9900276 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 660 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 660 LBL 11 TO RBL 11 FLOORBEAM SURFACE. CORROSION REMOVED PER SRM 51-10-01, WIT HIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900137 19990319 00137 NM 1999 3 19 P5CA9900277 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1540 LBL 20 TO RBL 10 FLOORBEAM LOWER CHORD UPPER SURFACE. CORROSION REMOVED PER S RM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900138 19990319 00138 NM 1999 3 19 P5CA9900278 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1800 LBL 10 TO RBL 11 LATERAL FLOOR SUPPORT FLANGE. CORROSION REMOVED PER SRM 51-1 0-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900139 19990319 00139 NM 1999 3 19 P5CA9900279 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2040 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2040 LBL 10 TO RBL 10 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900140 19990319 00140 NM 1999 3 19 P5CA9900280 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2140 LBL 10 TO RBL 10 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900141 19990319 00141 NM 1999 3 19 P5CA9900281 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 160-180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 160 TO 180 RBL 44 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900142 19990319 00142 NM 1999 3 19 P5CA9900282 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 400 RBL 38 FLOORBEAM SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10- 01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900143 19990319 00143 NM 1999 3 19 P5CA9900283 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 440 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 440 RBL 47 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMI TS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900144 19990319 00144 NM 1999 3 19 P5CA9900284 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 463 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND UPPER DECK FLOOR SUPPORT UPPER CHORD BS 463 RBL R40. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900145 19990319 00145 NM 1999 3 19 P5CA9900285 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 520-528 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK FLOOR SUPPORT BS 520 TO 528 RBL R80. CORROSION REMOVED PER SRM 51-10-01, WITHIN S RM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900146 19990319 00146 NM 1999 3 19 P5CA9900286 1 19990228 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 640 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 640 RBL 48 FLOORBEAM SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10 -01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900147 19990319 00147 NM 1999 3 19 P5CA9900287 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 760 RBL 95-98 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 L IMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900148 19990319 00148 NM 1999 3 19 P5CA9900288 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 980 RBL 55 TO 77 FLOORBEAM UPPER TEE CHORD LOWER FACE. CORROSION REMOVED PER SRM 5 1-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900149 19990319 00149 NM 1999 3 19 P5CA9900289 1 19990305 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1261 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1261 RBL 33 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900150 19990319 00150 NM 1999 3 19 P5CA9900290 1 19990305 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1372 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1372 RBL 57 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIM ITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900151 19990319 00151 NM 1999 3 19 P5CA9900291 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1500 RBL 84 TO 94 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10- 01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900152 19990319 00152 NM 1999 3 19 P5CA9900292 1 19990228 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1580 RBL 84 TO 94 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10- 01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900153 19990319 00153 NM 1999 3 19 P5CA9900293 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 1940 RBL 50 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIM ITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900154 19990319 00154 NM 1999 3 19 P5CA9900294 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2040 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2040 RBL 21 FLOORBEAM UPPER CHORD LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900155 19990319 00155 NM 1999 3 19 P5CA9900295 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2140 RBL 38 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIM ITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900156 19990319 00156 NM 1999 3 19 P5CA9900296 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2140 RBL 85 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIM ITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900157 19990319 00157 NM 1999 3 19 P5CA9900297 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 2166-2168 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2166 TO 2168 RBL 97 LONGIT FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900158 19990319 00158 NM 1999 3 19 P5CA9900298 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 2178-2180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND MAIN DECK BS 2178 TO 2180 RBL 98 TO 102 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900159 19990319 00159 NM 1999 3 19 P5CA9900299 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 2231-2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2231 TO 2240 RT WL 200 O/B FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, W ITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900160 19990319 00160 NM 1999 3 19 P5CA9900300 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2240 RBL 66 TO 69 LATERAL FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WI THIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900161 19990319 00161 NM 1999 3 19 P5CA9900301 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 LBL 11 TO RBL 11 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900162 19990319 00162 NM 1999 3 19 P5CA9900302 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 1170-1260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1170 TO 1260 LBL 11 TO RBL 11 TIE DOWN TRACK FLANGE AROUND ANCHOR NUTS. CORROSI ON REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900163 19990319 00163 NM 1999 3 19 P5CA9900303 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 320 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 320 LBL 11 TO 33 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-1 0-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900164 19990319 00164 NM 1999 3 19 P5CA9900304 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 360 LBL 33 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 L IMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900165 19990319 00165 NM 1999 3 19 P5CA9900305 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 360 LBL 33 FLOOR HANDLING AFT SUPPPORT. CORROSION REMOVED PER SRM 51-10-01, WIT HIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900166 19990319 00166 NM 1999 3 19 P5CA9900306 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 382 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 382 LBL 45 TIE DOWN TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, W ITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900167 19990319 00167 NM 1999 3 19 P5CA9900307 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 460 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 460 LBL 68-95 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-0 1 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900168 19990319 00168 NM 1999 3 19 P5CA9900308 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 460-480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 460 TO 480 LBL 11 AND 22. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10- 01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900169 19990319 00169 NM 1999 3 19 P5CA9900309 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 500 LBL 20-30 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-0 1 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900170 19990319 00170 NM 1999 3 19 P5CA9900310 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 LBL 33 TO 70 FLOORBEAM AT UPPER SURFACE. CORROSION REMOVED PER SRM 51-10-01 , WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900171 19990319 00171 NM 1999 3 19 P5CA9900311 1 19990305 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 542 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 542 LBL 11 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10 -01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900172 19990319 00172 NM 1999 3 19 P5CA9900312 1 19990305 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 552-560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 552 TO 560 LBL 11 FLOOR SUPPORT. SEAT TRACK LBL 9 STA 550 TO 590 REPAIRED AS P ER SRM 53-10-05 FIG 4. 2 L 7 4 4F A20WE 1999031900173 19990319 00173 NM 1999 3 19 P5CA9900313 1 19990305 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 640 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FORWARD CARGO BS 640 LBL 45 FLOORBEAM UPPER CHORD FOUND BROKEN. CRACKED AREA TRIMMED OFF AS PER SRM 51-10-01 AND TREATE D PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900174 19990319 00174 NM 1999 3 19 P5CA9900314 1 19990305 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 680 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 680 LBL 12 FLOORBEAM LOWER FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN S RM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900175 19990319 00175 NM 1999 3 19 P5CA9900315 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 760 LBL 75-98 FLOORBEAM UPPER SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900176 19990319 00176 NM 1999 3 19 P5CA9900316 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 710-790 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 710 TO 790 LBL 11 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51- 10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900177 19990319 00177 NM 1999 3 19 P5CA9900317 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 800 LBL 82 TO 95 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-1 0-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900178 19990319 00178 NM 1999 3 19 P5CA9900318 1 19990304 A 5320 ANGLE BOEING 747 747124 1384874 NM BS 890 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 890 LBL 117 FLOOR SUPPORT ANGLE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900179 19990319 00179 NM 1999 3 19 P5CA9900319 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 980 LBL 11 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10- 01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900180 19990319 00180 NM 1999 3 19 P5CA9900320 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 980 LBL 8295 FLOORBEAM LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN S RM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900181 19990319 00181 NM 1999 3 19 P5CA9900321 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1416-1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1416 TO 1500 LBL 11-33 FLOORBEAM AND ATTACH TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900182 19990319 00182 NM 1999 3 19 P5CA9900322 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 LBL 60-75 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10- 01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900183 19990319 00183 NM 1999 3 19 P5CA9900323 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 LBL 82-96 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10- 01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900184 19990319 00184 NM 1999 3 19 P5CA9900324 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1560 LBL 10 FLOORBEAM LOWER CHORD UPPER AND LOWER SURFACE. CORROSION REMOVED PE R SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900185 19990319 00185 NM 1999 3 19 P5CA9900325 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1670 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1670 LBL 55 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10 -01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900186 19990319 00186 NM 1999 3 19 P5CA9900326 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1700 LBL 85 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900187 19990319 00187 NM 1999 3 19 P5CA9900327 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1920 LBL 90 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900188 19990319 00188 NM 1999 3 19 P5CA9900328 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2040 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2040 LBL 91 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900189 19990319 00189 NM 1999 3 19 P5CA9900329 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2100 LBL 92 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900190 19990319 00190 NM 1999 3 19 P5CA9900330 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2140 LBL 22 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900191 19990319 00191 NM 1999 3 19 P5CA9900331 1 19990304 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2140 LBL 73 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900192 19990319 00192 NM 1999 3 19 P5CA9900332 1 19990303 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2240 LBL 75 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900193 19990319 00193 NM 1999 3 19 P5CA9900333 1 19990304 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 2320 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2320 LBL 38 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10 -01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900194 19990319 00194 NM 1999 3 19 P5CA9900334 1 19990228 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 240-260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 240 TO 260 RBL 36 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900195 19990319 00195 NM 1999 3 19 P5CA9900335 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 480-520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 480 TO 520 RBL 68 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900196 19990319 00196 NM 1999 3 19 P5CA9900336 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 RBL 87 TIE DOWN PLATE SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN S RM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900197 19990319 00197 NM 1999 3 19 P5CA9900337 1 19990305 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 560-561 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 560 TO 561 RBL R46 SEAT TRACK. SEAT TRACK REPLACED FROM BS 480 TO 600 PER SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1999031900198 19990319 00198 NM 1999 3 19 P5CA9900338 1 19990305 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 610-613 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 610 TO 613 RBL R66 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900199 19990319 00199 NM 1999 3 19 P5CA9900339 1 19990305 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 650-690 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 650 TO 690 RBL 66 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900200 19990319 00200 NM 1999 3 19 P5CA9900340 1 19990305 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 660-670 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 660 TO 670 RBL R46 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900201 19990319 00201 NM 1999 3 19 P5CA9900341 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 680 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT BS 680 RBL 56 TIE DOWN PLATE SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-0 1 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900202 19990319 00202 NM 1999 3 19 P5CA9900342 1 19990305 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 750 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 750 RBL 10 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900203 19990319 00203 NM 1999 3 19 P5CA9900343 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 770 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 770 RBL 10 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900204 19990319 00204 NM 1999 3 19 P5CA9900344 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 940-980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 940 TO 980 RBL 11 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900205 19990319 00205 NM 1999 3 19 P5CA9900345 1 19990303 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 1140-1160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1140 TO 1160 RBL 32 TIE DOWN TRACK LOWER FACE. CORROSION REMOVED PER SRM 51-10- 01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900206 19990319 00206 NM 1999 3 19 P5CA9900346 1 19990303 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 1208-1223 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1208 TO 1223 RBL 32 TIE DOWN TRACK CROWN OUTBOARD EDGE. CORROSION REMOVED PER S RM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900207 19990319 00207 NM 1999 3 19 P5CA9900347 1 19990304 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1320 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1320 RBL 33 TIE DOWN FITTING ATTACH FLANGE LOWER FACE. CORROSION REMOVED PER SR M 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900208 19990319 00208 NM 1999 3 19 P5CA9900348 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1394 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1394 RBL 11 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900209 19990319 00209 NM 1999 3 19 P5CA9900349 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1413 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1413 RBL 10 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900210 19990319 00210 NM 1999 3 19 P5CA9900350 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 RBL 11 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900211 19990319 00211 NM 1999 3 19 P5CA9900351 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1500-1508 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 TO 1508 RBL 11 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900212 19990319 00212 NM 1999 3 19 P5CA9900352 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1752-1754 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1752 TO 1754 RBL 11 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10 -01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900213 19990319 00213 NM 1999 3 19 P5CA9900353 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1775-1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1775 TO 1780 RBL 75 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900214 19990319 00214 NM 1999 3 19 P5CA9900354 1 19990301 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1780 RBL 77 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900215 19990319 00215 NM 1999 3 19 P5CA9900355 1 19990303 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 800 RBL 15-16 TIE DOWN FITTING FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900216 19990319 00216 NM 1999 3 19 P5CA9900356 1 19990228 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1800 RBL 75 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900217 19990319 00217 NM 1999 3 19 P5CA9900357 1 19990301 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1800 RBL 77 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900218 19990319 00218 NM 1999 3 19 P5CA9900358 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1810-1812 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1810 TO 1812 RBL 11 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10 -01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900219 19990319 00219 NM 1999 3 19 P5CA9900359 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1830 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1830 RBL 75 SEAT TRACK CROWN AND FLANGE. CORROSION REMOVED PER SRM 51-10-01, WI THIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900220 19990319 00220 NM 1999 3 19 P5CA9900360 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1888 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1888 RBL 11 SEAT TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900221 19990319 00221 NM 1999 3 19 P5CA9900361 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1900 RBL 75 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900222 19990319 00222 NM 1999 3 19 P5CA9900362 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1916-1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1916 TO 1920 RBL 75 SEAT TRACK FLANGE AND CROWN. CORROSION REMOVED PER SRM 51-1 0-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900223 19990319 00223 NM 1999 3 19 P5CA9900363 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1924 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1294 RBL 33 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900224 19990319 00224 NM 1999 3 19 P5CA9900364 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1950-1970 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1950 TO 1970 RBL 11 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900225 19990319 00225 NM 1999 3 19 P5CA9900365 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1940 RBL 97 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900226 19990319 00226 NM 1999 3 19 P5CA9900366 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1967 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1967 RBL 33 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900227 19990319 00227 NM 1999 3 19 P5CA9900367 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2105-2108 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2105 TO 2108 RBL 87 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10 -01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900228 19990319 00228 NM 1999 3 19 P5CA9900368 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2140-2148 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2140 TO 2148 RBL 11 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10 -01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900229 19990319 00229 NM 1999 3 19 P5CA9900369 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2180 RBL 76 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 5 3-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900230 19990319 00230 NM 1999 3 19 P5CA9900370 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2198-2200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2198 TO 2200 RBL 34 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10 -01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900231 19990319 00231 NM 1999 3 19 P5CA9900371 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2226-2228 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2226 TO 2228 RBL 32 SEAT TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10- 01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900232 19990319 00232 NM 1999 3 19 P5CA9900372 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2234-2236 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2234 TO 2236 RBL 64 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10 -01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900233 19990319 00233 NM 1999 3 19 P5CA9900373 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 220-240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 220 TO 224 LBL 26 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900234 19990319 00234 NM 1999 3 19 P5CA9900374 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 240-260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 240 TO 260 LBL 36 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900235 19990319 00235 NM 1999 3 19 P5CA9900375 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 290 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 290 LBL 70 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900236 19990319 00236 NM 1999 3 19 P5CA9900376 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 324 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 324 LBL 36 TIE DOWN TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10 -01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900237 19990319 00237 NM 1999 3 19 P5CA9900377 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 378 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 378 LBL 80 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900238 19990319 00238 NM 1999 3 19 P5CA9900378 1 19990303 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 380-460 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 380 TO 460 LBL 80 TIE DOWN TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WI THIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900239 19990319 00239 NM 1999 3 19 P5CA9900379 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 420-460 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 420 TO 460 LBL 68 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51- 10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900240 19990319 00240 NM 1999 3 19 P5CA9900380 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 LBL 11 TIE DOWN CRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10 -01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900241 19990319 00241 NM 1999 3 19 P5CA9900381 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 480-520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 480 TO 520 LBL 69 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900242 19990319 00242 NM 1999 3 19 P5CA9900382 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 520-550 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 TO 550 LBL 11 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900243 19990319 00243 NM 1999 3 19 P5CA9900383 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 560-590 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK SEAT TRACK EDGE ATTACH HOLE LOWER AREA, BS 560 TO 590 LBL 40 AND 60. CORROSION RE MOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900244 19990319 00244 NM 1999 3 19 P5CA9900384 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 570-660 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 570 TO 660 LBL 11 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900245 19990319 00245 NM 1999 3 19 P5CA9900385 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 600-610 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK LEFT HAND BS 600 TO 610 LBL 66 SEAT TRACK CROWN FLANGE. SEAT TRACK REPAIRED AT LB L 66 STA 560 AND 640 PER SRM 53-10-05. 2 L 7 4 4F A20WE 1999031900246 19990319 00246 NM 1999 3 19 P5CA9900386 1 19990305 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 675-690 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 624, 675-690 LBL 25 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900247 19990319 00247 NM 1999 3 19 P5CA9900387 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 640-674 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 640 TO 674 LBL 75 TIE DOWN TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-1 0-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900248 19990319 00248 NM 1999 3 19 P5CA9900388 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 665 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 665 LBL 76 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900249 19990319 00249 NM 1999 3 19 P5CA9900389 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 670-690 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 670 TO 690 LBL 22 SEAT TRACK SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITH IN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900250 19990319 00250 NM 1999 3 19 P5CA9900390 1 19990305 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 750 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT UPPER DECK BS 750 LBL 44 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900251 19990319 00251 NM 1999 3 19 P5CA9900391 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 761 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 761 LBL 97 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900252 19990319 00252 NM 1999 3 19 P5CA9900392 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 770-790 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 770 TO 790 LBL 10 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900253 19990319 00253 NM 1999 3 19 P5CA9900393 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 789 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 789 LBL 10 TO RBL 10 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900254 19990319 00254 NM 1999 3 19 P5CA9900394 1 19990228 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 817 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 817 LBL 87 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900255 19990319 00255 NM 1999 3 19 P5CA9900395 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 865 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 865 LBL 97 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53 -10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900256 19990319 00256 NM 1999 3 19 P5CA9900396 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 910-914 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 910 TO 914 LBL 33 TIE DOWN TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WI THIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900257 19990319 00257 NM 1999 3 19 P5CA9900397 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 940 LBL 30 TIE DOWN PLATE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10 -01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900258 19990319 00258 NM 1999 3 19 P5CA9900398 1 19990304 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 960 LBL 17 TIE DOWN PLATE LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHI N SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900259 19990319 00259 NM 1999 3 19 P5CA9900399 1 19990303 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1000-1100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1000 TO 1100 LBL L11-R11 TIE DOWN TRACK FLOOR SUPPORT LOWER FACE ANCHOR NUT ATTA CH AREA. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999031900260 19990319 00260 NM 1999 3 19 P5CA9900400 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1510-1560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON M/D BS 1510 TO 1560 LBL 10 SEAT TRACK FLANGE. REMOVED CORROSION, BLENDED OUT AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900261 19990319 00261 NM 1999 3 19 P5CA9900401 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1530 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON SEAT TRACK BS 1530 LBL 77. REMOVED CORROSION PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900262 19990319 00262 NM 1999 3 19 P5CA9900402 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1540-1560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON SEAT TRACK BS 1540 TO 1560 LBL 75. REMOVED CORROSION PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900263 19990319 00263 NM 1999 3 19 P5CA9900403 1 19990303 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON MD BS 1760 LBL 88 TIE DOWN FITTING FLANGE PLATE. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900264 19990319 00264 NM 1999 3 19 P5CA9900404 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1770 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON SEAT TRACK BS 1770 LBL 97. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900265 19990319 00265 NM 1999 3 19 P5CA9900405 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION AT BS 1780 LBL 75 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900266 19990319 00266 NM 1999 3 19 P5CA9900406 1 19990304 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON BS 1780 LBL 88 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900267 19990319 00267 NM 1999 3 19 P5CA9900407 1 19990304 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON TIE DOWN FITTING BS 1800 LBL 55. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900268 19990319 00268 NM 1999 3 19 P5CA9900408 1 19990304 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON TIE DOWN FITTING BS 1800 LBL 12. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900269 19990319 00269 NM 1999 3 19 P5CA9900409 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1802 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON SEAT TRACK BS 1802 TO 1812 LBL 11. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900270 19990319 00270 NM 1999 3 19 P5CA9900410 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1804 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON SEAT TRACK BS 1804 LBL 35. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900271 19990319 00271 NM 1999 3 19 P5CA9900411 1 19990301 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND BS 1840 LBL 53 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900272 19990319 00272 NM 1999 3 19 P5CA9900412 1 19990303 A 5320 FITTING BOEING 747 747124 1384874 NM BS 1900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON TIE DOWN FITTING MD BS 1900 LBL 82. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900273 19990319 00273 NM 1999 3 19 P5CA9900413 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1910-1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON MD SEAT TRACK BS 1910 TO 1920 LBL 33. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900274 19990319 00274 NM 1999 3 19 P5CA9900414 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1912 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON SEAT TRACK BS 1912 LBL 97. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900275 19990319 00275 NM 1999 3 19 P5CA9900415 1 19990303 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1900-1980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON SEAT TRACK FROM BS 1900 TO 1980 LBL75 TO 77. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900276 19990319 00276 NM 1999 3 19 P5CA9900416 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2038-2250 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON SEAT TRACKS FROM BS 2038 TO 2250 LBL10 TO 11. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900277 19990319 00277 NM 1999 3 19 P5CA9900417 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2123 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON BS 2123 LBL 89 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900278 19990319 00278 NM 1999 3 19 P5CA9900418 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2123 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON SEAT TRACK AT BS 2123 LBL 97. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900279 19990319 00279 NM 1999 3 19 P5CA9900419 1 19990304 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 2138 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON SEAT TRACK BS 2138 LBL 75. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900280 19990319 00280 NM 1999 3 19 P5CA9900420 1 19990303 A 5347 TIE DOWN BOEING 747 747124 1384874 NM BS 2220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON MD BS 2220 LBL 97 TIE DOWN TRACK. CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900281 19990319 00281 NM 1999 3 19 P5CA9900421 1 19990302 A 5320 FITTING BOEING 747 747124 1384874 NM BS 2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON MD BS 2240 LBL 3 TIE DOWN FITTING FLANGE PLATE. REMOVED CORROSION PER SMR 51-10-01. 2 L 7 4 4F A20WE 1999031900282 19990319 00282 NE 1999 3 19 TC8A99004 2 19990310 A 7320 LINE BOEING 727 72721C 138400M NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE REPLACED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 1186Z 19134 653799 NR 1 ENGINE FAILED TO MAKE T/O POWER. FOUND BROKEN PS4 LINE AT NR 1 ENGINE FUEL CONTROL ASSY. REPLACED HARD LINE WITH F LEX HOSE ASSY IAW 20-10-12. PERFORMED GROUND MAINTENANCE RUN AT ALL POWER SETTINGS, CHECKED OUT IAW BMM CHAPTER 72-00, NO DEFECTS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1999031900635 19990319 00635 WP 1999 3 19 AT9900190 1 19990309 A 2560 COVER DOUG DC9 DC932 3022066 WP L1 DOOR SLIDE LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND DURING PREFLIGHT CHECK, THE L-1 DOOR SLIDE COVER LOOSE. RESECURED THE L-1 DOOR SLIDE COVER IAW MM 25-62. RII ACC OMPLISHED. 2 L 7 2 4F A6WE 1999031900636 19990319 00636 WP 1999 3 19 AT9900191 1 19990311 A 5730 PANEL DOUG DC9 DC932 3022066 WP WS 530 ELONGATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE VENT BOX FASTENER HOLES TO BE ELONGATED LEFT HAND WING AT XRS 530. RE AMED HOLES, INSTALLED FREEZE PLUGS AND DOUBLER IAW DAC NT SPMT06 AND AERO CORP EO NR 99-1095. 2 L 7 2 4F A6WE 1999031900637 19990319 00637 WP 1999 3 19 AT9900192 1 19990211 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 950 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK ON SKIN LEFT HAND SIDE JUST BELOW L-14L AT BS 950. NDT MARKED END S OF CRACK, REMOVED CRACK, FABRICATED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2, 53-04 FI G 3A, 51-10-3, AND RES NR 99391. 2 L 7 2 4F A6WE 1999031900638 19990319 00638 WP 1999 3 19 AT9900193 1 19990219 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 238 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT IN THE FORWARD CARGO PIT AT BS 238 OVER L-28R CORRODED. REMOVED FLOOR SUPPORT AND FABRICATED REPAIR, ALODINE, PRIMED, AND INSTALLED SUPPORT AND REPAIR IAW DC9 SRM 53-01-FIG 1, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999031900639 19990319 00639 1999 3 19 JBXA9900074 4 19990312 A 2350 G694620 AUDIO PANEL FOKKER F28 F28MK0100 4990807 EU LT COCKPIT INOP A JBXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 130ML 11329 AUDIO FAILED ON CAPTAINS SIDE. REMOVED AND REPLACED CAPTAINS HEADSET AUDIO PANEL INTERCONNECT BOX (AUDIO JACK PANEL). O PERATIONAL CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT 1999031900640 19990319 00640 WP 1999 3 19 CALA9900242 1 19990310 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A .25 INCH CRACK NEAR WING SKIN PANEL 515AB HOLE. A REPAIR WAS PERFORMED IAW SRM 57-00-01, FIGURE 4. 2 L 7 3 4F A22WE 1999031900641 19990319 00641 WP 1999 3 19 CALA9900243 1 19990310 A 5350 BAYONET DOUG DC9 DC982 3022082 WP TAIL CONE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 THE FORCE REQUIRED TO RELEASE TAIL CONE USING EXTERNAL HANDLE WAS LOW. THE LEFT LOWER TAIL CONE BAYONET WAS REMOVED AND REPLACED DUE TO WEAR. AN ADJUSTMENT/TEST OF THE TAIL CONE RELEASE MECHANISM WAS PERFORMED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1999031900642 19990319 00642 NM 1999 3 19 CALA9900244 1 19990311 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 312 FROM LBL 10 TO RBL 10. THE CORRODED SECTION WAS REMOVED AND FILLER A ND DOUBLERS WERE INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999031900643 19990319 00643 WP 1999 3 19 CALA9900245 1 19990311 A 5240 SKIN DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 1 INCH CRACK IN AFT SERVICE DOOR SKIN AT TOP AFT EDGE OF HOLD OPEN HOOK CUTOUT. REPAIRED IAW ECRA 52 05-01008. 2 L 7 2 4F A6WE 1999031900644 19990319 00644 WP 1999 3 19 9900859155 1 19990310 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE CHECK, FOUND CATWALK EMERGENCY EXIT LIGHTING INOPEATIVE AND WIRING PULLED BACK. MAINTENANCE REPLACED EMERGE NCY LIGHT BATTERIES AND REPOSITIONED WIRING. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1999031900645 19990319 00645 WP 1999 3 19 9900869959 1 19990309 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 919RW 47162 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT TAIL COMPARTMENT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999031900646 19990319 00646 NM 1999 3 19 9900876729 1 19990309 A 3260 WARNING LIGHT BOEING 747 747251F 1384898 NM LANDING GEAR ILLUMINATED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 629US 22388 DURING APPROACH, THE RED LANDING GEAR WARNING LIGHT ILLUMINATED. RECYCLED LANDING GEAR AND ALL INDICAITONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR SYSTEM VISUAL AND OPERATIONAL CHECKS WERE GOOD. EXACT PART CAUSING DISCREPANCY TO BE DETERMINED. 2 L 7 4 4F A20WE 1999031900647 19990319 00647 WP 1999 3 19 9900889878 1 19990310 A 3230 RESTRICTORS DOUG DC9 DC951 3022051 WP LANDING GEAR FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 787NC 48149 APPROACHING TO LAND AT MSP, THE NOSE LANDING GEAR DID NOT EXTEND. FLIGHT CREW FOLLOWED COM PROCEDURES AND ACTIVATED THE EMERGENCY LANDING GEAR EXTENSION LEVER, LANDING GEAR EXTENDED SUCCESSFULLY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED 2 HYDRAULIC RESTRICTORS IN THE NOSE LANDING GEAR WHEEL WELL, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999031900648 19990319 00648 WP 1999 3 19 9900899919 1 19990309 A 2420 WIRE DOUG DC9 DC932 3022066 WP LEFT GEN SYST FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 01 941N 47450 EN ROUTE MSP-IAD, C PHASE OF LEFT GENERATOR BUS CIRCUIT BREAKERS POPPED FOLLOWED BY ALL ROW H FUEL PUMP CIRCUIT BREAKERS . CREW DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO IND. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED C IRCUIT BREAKER B1-275 AND REPAIRED WIRING. OPERATIONAL CHECK NORMAL AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999031900650 19990319 00650 NM 1999 3 19 UPS99228959 1 19990223 A 5753 FLAP TRACK BOEING 727 72731C 1384011 NM RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, CORROSION (SURFACE) ON RT O/B FLAP TRACK O/B MOUNT LUG. REWORKED IAW SMRO EO 99-05-008 REF UPS ENGIN EERING FILE NUMBER 727-5 7-2039. 2 L 7 3 4F A3WE 1999031900651 19990319 00651 NM 1999 3 19 UPS99228960 1 19990223 A 5753 FLAP TRACK BOEING 727 72731C 1384011 NM RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D ON REMOVAL OF RT O/B FLAP I/B TRACKS, SURFACE CORROSION FOUND ON I/B FACES OF BOTH TRACK ATTACH LUGS. NR 7 FLAP TRACK WING SUPPORT LUG REWORKED IAW SMRO EO 99-05-007, REF UPS ENGINEERING FILE NUMBER 727-57-2038. 2 L 7 3 4F A3WE 1999031900652 19990319 00652 NM 1999 3 19 UPS99228961 1 19990219 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, CRACK ON FRAME AT BS 910 LT MLG WHEEL WELL BELOW STRINGER 18A. REPAIRED IAW EO B727-5310-1896. 2 L 7 3 4F A3WE 1999031900653 19990319 00653 NM 1999 3 19 UPS99228962 1 19990219 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM NR 2 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, NR 2 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. NR 2 FLAP CARRIAGE REPLACED IAW MM 27-51-13 AN D OHM 57-57-01. 2 L 7 3 4F A3WE 1999031900654 19990319 00654 NM 1999 3 19 UPS99228963 1 19990219 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM NR 1 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, NR 1 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE REPLACED IAW MM 27-51-13 AND OHM 57-5 8-01. 2 L 7 3 4F A3WE 1999031900655 19990319 00655 NM 1999 3 19 UPS99228964 1 19990219 A 5753 CARRIAGE BOEING 727 72731C 1384011 NM NR 8 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-C, NR 8 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE. CARRIAGE ASSY REPLACED IAW MM 27-51-13 AND OHM 57-58-01. 2 L 7 3 4F A3WE 1999031900656 19990319 00656 NM 1999 3 19 UPS99228965 1 19990218 A 5751 6521735 CASTING BOEING 727 72731C 1384011 NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, RT I/B AILERON ACTUATING ROD ATTACH CASTING HAS SEVERAL AREAS OF PITTING CORROSION. CASTING REPLACED IAW DRAWING 65-21765 AND SRM 51-30-02. 2 L 7 3 4F A3WE 1999031900657 19990319 00657 NM 1999 3 19 UPS99228966 1 19990218 A 5751 SUPPORT BOEING 727 72731C 1384011 NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, LT I/B AILERON CENTRE HINGE SUPPORT CORRODED. CENTER HINGE SUPPORT REPLACED IAW MM 27-10-01. 2 L 7 3 4F A3WE 1999031900658 19990319 00658 NM 1999 3 19 UPS99228967 1 19990218 A 5751 6521735U21 CASTING BOEING 727 72731C 1384011 NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, LT I/B AILERON I/B HINGE CASTING CORRODED. CASTING REPLACED IAW DWG 65-21765 AND SRM 51-30-02. 2 L 7 3 4F A3WE 1999031900659 19990319 00659 NM 1999 3 19 UPS99228968 1 19990215 A 5320 SUPPORT BOEING 727 72731C 1384011 NM BS 850 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, FLOOR BOARD SUPPORT CRACKED BS 850 RBL 45.5. FLOORBOARD SUPPORT REPAIRED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1999031900660 19990319 00660 NM 1999 3 19 UPS99228969 1 19990209 A 5755 65982965 SUPPORT BOEING 727 72731C 1384011 NM NR 8 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, NR 8 SPOILER I/B HINGE CASTING CRACKED. CASTING REPLACED IAW SRM 51-30-2 AND DRAWING 65-16216. 2 L 7 3 4F A3WE 1999031900661 19990319 00661 NM 1999 3 19 UPS99228970 1 19990311 A 3350 LIGHT BOEING 727 727180C 138406G NM CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER MED DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSY, OPS CK GOOD. 2 L 7 3 4F A3WE 1999031900662 19990319 00662 NM 1999 3 19 UPS99228971 1 19990311 A 3350 LIGHT BOEING 727 72727C 138400J NM CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 907UP 19118 INSPECTION TYPE-N/A, EMER EXIT LIGHT (ENTRANCE) ASSY ROBBED FOR A/C 820 (S/N 20896 A 450467). REPLACED ROBBED EMER EXIT LIGHT (P/N ON 10-0067-9) (S/N 22574), OPS CK PER MM 33-50-00. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1999031900663 19990319 00663 NM 1999 3 19 UPS99228972 1 19990311 A 3350 LIGHT BOEING 727 72725C 138400H NM EMER EXIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, RT AFT INTERIOR OVERWING EMER LIGHT INOP. REMOVED AND REPLACED EMER LIGHT ASSY, OPS CKS OK. 2 L 7 3 4F A3WE 1999031900664 19990319 00664 WP 1999 3 19 UPS99828973 1 19990311 A 2560 CLIP DOUG DC8 DC871F 302199D WP PAX DOOR SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE-N/A, MAIN ENTRY DOOR SLIDE PACK RETAINER CLIP BROKEN. REMOVED AND REPLACED SLIDE COVER RETAINER CLIP. 2 L 7 4 4F RT 4A25 1999031900665 19990319 00665 EU 1999 3 19 QXEA9900492 1 19990310 A 3350 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9 DETACHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 GEG - AISLE EXIT LIGHT AT ROW 9 FELL OFF. MAINTENANCE REPLACED THE SIGN ASSEMBLY, OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT A20EU 1999031900666 19990319 00666 EU 1999 3 19 QXEA9900493 1 19990310 A 3350 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8B BROKEN A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 478US 11227 BOI - EMERGENCY EXIT LIGHT AT SEAT 8B BROKEN. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHEC KS NORMAL. 2 L 7 2 4F RT A20EU 1999031900667 19990319 00667 EU 1999 3 19 QXEA9900494 1 19990310 A 3350 FUSE GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 484US 11234 PDX - RIGHT WING FORWARD EMERGENCY EVACUATION LIGHT INOPERATIVE. MAINTENANCE REPLACED A FAULTY FUSE ON THE POWER SUPPLY . OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT A20EU 1999031900668 19990319 00668 NM 1999 3 19 QXEA9900495 1 19990307 A 2611 473054 DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 369PH 619 520 PDX- SMOKE WARNING LIGHT ILLUMINATED INTERMITTANTLY. MAINTENANCE REPLACED BOTH CARGO COMPARTMENT SMOKE DETECTORS, OPERA TIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999031900669 19990319 00669 NM 1999 3 19 99FDEA00098 1 19990311 A 2130 CONNECTOR BOEING 727 727233 138408A NM OUT FLOW VALVE DIRTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 283FE 22350 99-0066 - AC WON'T PRESSURIZE. COMP RED TABS AND PULL CIRCUIT BREAKERS ON P2 PNL BUT CABIN OUTFLOW VALVE REMAIN STUCK I N THE FULL OPEN POS. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, NO HELP, CONTROLLER NEED LEAK CK. PERF LOW LEVEL STATIC LEAK CK OF AUTO PRESS. LEAK CK NORMAL PER M/M34-11-000-5. CLEAN CANNON PLUGS ON OUT FLOW VALVE. OPER CK NORM. 2 L 7 3 4F RT A3WE 1999031900670 19990319 00670 NM 1999 3 19 99FDEA00099 1 19990311 A 3260 H1010153 SWITCH BOEING 727 727100 1384036 NM NLG INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 143FE 19136 99-0067 - DOOR LIGHTS RED WOULD NOT GO OUT AT GEAR RETRACTION. NOSE GEAR HAD A FAULTY GREEN LIGHT, RED NOSE GEAR LIGHT NOW STAYS ON. REMOVED AND REPLACED DOWN LOCK SWITCH. OPER CK NORM PER MM 32-61-0-21-4. 2 L 7 3 4F RT A3WE 1999031900671 19990319 00671 EU 1999 3 19 99FDEA00100 1 19990311 A 3260 PROXIMITY SWITCH AIRBUS 300 A300F4605R 3930327 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 659FE 757 ON T/O, ROTATION FELT VIBRATION IN YOKE. GEAR HANDLE UP BUT GEAR DID NOT RETRACT. ECAM L/G WOULD NOT RET, AT DROPPED O FF AND WOULD NOT RESET. GPWS FAULT LIGHT ON. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT PER MM 32-31-71-4 PG 401. N O FAULTS ON BITE. 2 L 7 2 4F RT A35EU 1999031900672 19990319 00672 NM 1999 3 19 99FDEA00101 1 19990312 A 3260 PLUNGER BOEING 727 72722 1384002 NM MLG DOOR SWITCH DIRTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 185FE 18871 RT MAIN GEAR LIGHT ON 2ND OFFICERS PNL AND DOOR LIGHTS ON GEAR ANNUNCIATOR PNL REMAINED ON AFTER GEAR RETRACTION. RECYC LED AND LIGHTS WENT OUT. CLEANED PLUNGER AND ELECTRICAL CONN. OPER CK DOOR ON GROUND SEVERAL TIMES. OPER CK OK PER MM 32-62-011. 2 L 7 3 4F A3WE 1999031900673 19990319 00673 NM 1999 3 19 99FDEA00102 1 19990312 A 3260 H1010154 SWITCH BOEING 727 72721C 138400M NM NLG INOPERATIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 143FE 19136 UPON GEAR RETRACT, ALL GEAR DOORS ON 2ND OFFICERS PNL SHOW CLOSED. HOWEVER, GEAR HANDLE IN THE UP POSITION, THE RED INT RANSIT LIGHTS FOR THE GEAR REMAIN ILLUM. WHEN GEAR HANDLE IN OFF, THE RED LIGHT GOES OUT. WHEN GEAR IS PUT DOWN, ALL G REEN LIGHT ILLUM WITH THE NOSE GEAR RED INTRANSIT LIGHT ON AS WELL. REMOVED AND REPLACED NOSE LANDING GEAR POS SWITCH P ER MM 32-61-021-4. OPER CK NORM. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999031900674 19990319 00674 WP 1999 3 19 ABXA9900179 1 19990311 A 5753 5910042506 VANE DOUG DOUG DC9 DC941 302207N WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 RIGHT WING FLAP CENTER FIXED VANE DELAMINATED ON LOWER SURFACE AT INBOARD END. REPLACED VANE IAW DC9 MM 27-51-3. 2 L 7 2 4F A6WE 1999031900675 19990319 00675 WP 1999 3 19 ABXA9900180 1 19990226 A 5753 5914508504 FITTING DOUG DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 WHILE COMPLYING WITH C-CHECK, FOUND RIGHT FLAP CENTER HINGE INNER ATTACH FITTING CRACKED. REPLACED RIGHT FLAP CENTER HI NGE ATTACH FITTING IAW DC9 SRM 57-09. 2 L 7 2 4F A6WE 1999031900676 19990319 00676 WP 1999 3 19 ABXA9900181 1 19990226 A 5400 591326213 ANGLE DOUG DOUG DC9 DC933F 302207A WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND RIGHT PYLON ATTACH ANGLE CRACKED AT TOP CENTER OF PYLON. REPAIRED ATTACH ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1999031900677 19990319 00677 WP 1999 3 19 ABXA9900182 1 19990223 A 5320 99220421 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 256 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FITTING CRACKED AT STATION 256, BETWEEN LONGERONS 23 LEFT AND 22 LEFT. REPLACED FITTING IAW DC9 S RM 51-30-5. 2 L 7 2 4F A6WE 1999031900678 19990319 00678 WP 1999 3 19 ABXA9900183 1 19990218 A 5230 3914025501 FITTING DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND AFT LOWER CARGO DOOR NR 4 BEAM END FITTING CRACKED AT NR 4 DOOR STOP. REPLACED FITTING IAW DC9 SR M 51-30-5. 2 L 7 2 4F A6WE 1999031900679 19990319 00679 WP 1999 3 19 ABXA9900184 1 19990218 A 5230 3914025502N FITTING DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING C-CHECK, FOUND AFT LOWER CARGO DOOR NR 2 BEAM END FITTING CRACKED AT NR 2 DOOR STOP. REPLACED FITTING IAW DC9 SR M 51-30-5. 2 L 7 2 4F A6WE 1999031900680 19990319 00680 WP 1999 3 19 ABXA9900185 1 19990308 A 3230 CONTROL CABLE DOUG DOUG DC9 DC941 302207N WP LANDING GEAR LACK OF LUBE A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 990AX 47493 UNABLE TO LOWER GEAR LEVER. AFTER SEVERAL ATTEMPTS, WAS ABLE TO MOVE LEVER TO DOWN POSITION AND GEAR EXTENDED NORMALLY. SUSPECT ICE FORMED AROUND LANDING GEAR EXTENSION CONTROL CABLES. CLEANED WATER FROM AREA AND LUBRICATED CABLES. 2 L 7 2 4F A6WE 1999031900681 19990319 00681 WP 1999 3 19 ABXA9900186 1 19990310 A 3230 MECHANISM DOUG DOUG DC9 DC941 302207N WP LACK OF LUBE LACK OF LUBE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 951AX 47616 COULD NOT RETRACT GEAR AFTER TAKEOFF. OVER RODE GEAR HANDLE RELEASE AND PUT HANDLE IN UP POSITION. AUTO PRESSURE WAS I NOPERATIVE, AUTO SPOILER 'DO NOT USE' LIGHT WAS ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES. LUBRICATED GROUND SHIFT MEC HANICAL SECTOR. 2 L 7 2 4F A6WE 1999031900682 19990319 00682 WP 1999 3 19 ABXA9900187 1 19990310 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOP A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 988AX 47084 DURING PREDEPARTURE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHTS DIM AND FLICKERING. REPLACED EMERGENCY LIGHT POWER SUPP LY. 2 L 7 2 4F A6WE 1999031900683 19990319 00683 NM 1999 3 19 DL76L990470 1 19990306 A 3610 VALVE 361001835 BOEING 767 767332 1382001 NM NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 171DN 24759 000000 RIGHT/ENGINE BLEED OVERHEAT EICAS MSG AND ANNUNCIATOR LIGHT ILLUMINATED. USED RESET PROCEDURE LIGHT CAME BACK ON AFTER 10 MINS. DEACTIVATED HP VALVE. FWD TO MCO AND PLACARD PER MEL 36-11-02. 2 L 7 2 4F RT A1NM 1999031900684 19990319 00684 NM 1999 3 19 DL72W990476 1 19990301 A 5720 ANGLE BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 CRACK ORIGINATING UNDER I/B UPSTOP PAD ON NR 7 SLAT ANGLE RUNNING I/B .25 INCH. REPAIRED PER MM 57-40-0 PAGE 816. 2 L 7 3 4F A3WE 1999031900685 19990319 00685 NM 1999 3 19 DL72S990477 1 19990215 A 5330 SKIN BOEING 727 727232 1384082 NM AIRSTAIR DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 AT HMV2, FOUND SKIN CRACKED - EMPENNAGE EXIT, LOC AT FWD RT CORNER OF AFT AIRSTAIRS CUTOUT. FABRICATED DOUBLER PER MM 5 3-30-00 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER. 2 L 7 3 4F A3WE 1999031900686 19990319 00686 NM 1999 3 19 DL72S990478 1 19990308 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND AT E-1 LETTER CK, AFT ENTRY DOOR FRAME CUTOUT HAS .5 INCH VISIBLE CRACK LT SIDE. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999031900687 19990319 00687 NM 1999 3 19 DL72S990479 1 19990308 A 2782 MOUNT BOEING 727 727232 1384082 NM NR 1 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND ON E1 LETTER CK, 1 INCH VISIBLE CRACK NR 1 SLAT ACTUATOR O/B MOUNT WEB ABOVE TRUNNION FITTING. REPAIRED PER MM 57 -20-21. 2 L 7 3 4F A3WE 1999031900688 19990319 00688 NM 1999 3 19 DL72K990480 1 19990308 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM BS 800 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 415DA 1084 21257 AFT OVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUM WHEN TESTED. REPLACED BATTERY CARTRIDGE AND RACK ASSY CKS NORMAL. 2 L 7 3 4F A3WE 1999031900689 19990319 00689 NM 1999 3 19 DL73K990481 1 19990308 A 2913 PUMP 623337 BOEING 737 737247 138448D NM A HYD SYST MALFUNCTIONED A DALA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 239WA MX321405 23187 ON DESCENT INTO MCO, LOST BOTH A SYSTEM ENGINE DRIVEN HYDRAULIC PUMPS, LOW PRESSURE LIGHT ILLUMINATED. CHECKED AND REPL ACED ALL CASE DRAIN AND RETURN FILTERS, NO METAL. REPLACED COCKPIT OVERHEAD HYDRAULIC PANEL AND BOTH ENGINE DRIVEN HYDR AULIC PUMPS AS PRECAUTION. RAN ENGINES AND ALL FLIGHT CONTROLS, ALL OPERATION NORMAL. 2 L 7 2 4F A16WE 1999031900690 19990319 00690 NM 1999 3 19 DL767990482 1 19990302 A 2560 DOOR 101656305 BOEING 767 767232 1385132 NM LT SLIDE MISSING A DALA D RETURN TO BLOCK D INFLIGHT SEPARATION CL CLIMB 1 SO 27 110DL PH0142 22222 PASSING 12,000 FT, FLT ATTENDANT REPORTED LOUD NOISE. ALSO, HAD LT SLIDE DOOR EICAS MSG AND OVERHEAD DISCREET EMER DOOR S. SLIDE HAD DEPARTED A/C WITH FAILURE OF DOOR. REPLACED DOOR SLIDE AND DAMAGED PANELS. 2 L 7 2 4F RT A1NM 1999031900691 19990319 00691 NM 1999 3 19 DL72K990483 1 19990309 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 580 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. GA INING INTERNAL ACCESS AND CONDUCTING HFEC INSP CONFIRMED 29 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT. REPAIRED PER ERA 332874-14AD, REV A. 2 L 7 3 4F A3WE 1999031900692 19990319 00692 NM 1999 3 19 DL72K990484 1 19990309 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 700 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R, CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. C ONDUCTING HFEC INSP CONFIRMED 29 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT. REPAIRED PER ERA 332875-14 AD, REV A. 2 L 7 3 4F A3WE 1999031900693 19990319 00693 NM 1999 3 19 DL72S990485 1 19990309 A 5330 655458824 SKIN BOEING 727 727232 1384082 NM BS 720 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 THE UPPER SKIN OF THE S19R LAP SPLICE WAS FOUND TORN AT BS 720E-5 DUE TO MISALIGNMENT OF THE WING TO BODY FAIRING UPON I NSTALLATION. REPAIRED PER ERA 332901-14AD, REV A. 2 L 7 3 4F A3WE 1999031900694 19990319 00694 NM 1999 3 19 DL72S990486 1 19990310 A 5311 651766351 FRAME BOEING 727 727232 1384082 NM BS 600 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 BS 600 FRAME BELOW THE CARGO FLOOR AT STR 28R WAS FOUND CORRODED. THE UPPER FRAME OF THE LOWER LOBE CTR FRAME SECTION A ND SOME EXISTING REPAIRS WERE ALSO FOUND CORRODED. REPAIRED PER ERA 332893-14, REV A. 2 L 7 3 4F A3WE 1999031900695 19990319 00695 NM 1999 3 19 DL72S990487 1 19990310 A 5741 651621928 FITTING BOEING 727 727232 1384082 NM BS 870 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 CORROSION WAS FOUND IN THE BORE OF THE RT WING AFT TERMINAL FITTING. REPAIRED PER ERA 366788-14, REV A. 2 L 7 3 4F A3WE 1999031900696 19990319 00696 NM 1999 3 19 DL72S990488 1 19990310 A 5743 FITTING BOEING 727 727232 1384082 NM RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 CORROSION FOUND IN THE RT MLG SUPPORT BEAM O/B BORE AND IN THE FWD AND AFT FITTINGS. REWORKED PER ERA 332851-14. 2 L 7 3 4F A3WE 1999031900697 19990319 00697 NM 1999 3 19 DL72S990489 1 19990310 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1233 MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 411DA 21223 FUSELAGE SKIN WAS MISDRILLED AT S11R AT BS 1233. REPAIRED PER ERA 332842-14, REV A. 2 L 7 3 4F A3WE 1999031900698 19990319 00698 NM 1999 3 19 DL72S990490 1 19990310 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 430 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R LAP JOINT, 2 CRACK INDICATIONS WERE FOUND BETWEEN BS 360 AND 481. HFEC INSP VERIFIED CRACK INDICATIONS. REPAIRED PER ERA 332834-14AD, REV A. 2 L 7 3 4F A3WE 1999031900699 19990319 00699 NM 1999 3 19 DL72S990491 1 19990307 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 LFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE LOWER SKIN PANE AT THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 38 CRACKS ALONG THE LENGTH OF THE PANEL. THE SKI N LAP WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366796-14AD, REV A. 2 L 7 3 4F A3WE 1999031900700 19990319 00700 NM 1999 3 19 DL72S990492 1 19990307 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 LFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE LOWER SKIN AT THE STRINGER 4R SKIN LAP S PLICE BETWEEN FS 481 AND 680. INTERNAL HFEC INSPECTION CONFIRMED 54 CRACK INDICATIONS ALONG THE LENGTH OF THE PANE L. THE LAP SPLICE WAS CUTOUT ALONG ITS ENTIRE LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366795-14 AD, REV A. 2 L 7 3 4F A3WE 1999031900701 19990319 00701 NM 1999 3 19 DL72L990493 1 19990307 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 405 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 LFEC INSPECTION INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R SKIN LAP SPLICE NEAR FS 405. HFEC INTERNAL INSPECTION OF THE SKIN LAP CONFIRMED A CRACK AT FS 405. THE CRACK WAS REPAIRED PER B727 SRM 53-30- 3, FIG 5 AND DOCUMENTED PER ER/A 366843-14AD, REV A. 2 L 7 3 4F A3WE 1999031900702 19990319 00702 NM 1999 3 19 DL72L990494 1 19990307 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 442 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 LFEC INSPECTION REVEALED A CRACK INDICATION NEAR THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R SKIN LAP SP LICE NEAR FS 442. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE AT FS 442. THE CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366845-14AD, REV A. 2 L 7 3 4F A3WE 1999031900703 19990319 00703 NM 1999 3 19 DLM88990495 1 19990306 A 5320 591214186 ANGLE DOUG MD88 MD88 3023688 NM BS 1463 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 THE RT VERTICAL STABILIZER-TO-FUSELAGE ATTACH ANGLE WAS FOUND WITH A 1.5 INCH CRACK AT FS 1463. THE CRACK WAS ROUTED OU T AND A STEEL REPAIR ANGLE INSTALLED PER ER/A 366856-14, REV A. 2 L 7 2 4F RT A6WE 1999031900704 19990319 00704 NM 1999 3 19 DL72W990496 1 19990309 A 7120 65312813 ANGLE BOEING 727 727247 138408F NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 ON HUSH-KIT MOD FOUND LT NR 2 ENGINE AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REMOVED CHORD ANGLE AND REPLACED WITH NEW MFG PART. 2 L 7 3 4F A3WE 1999031900705 19990319 00705 NM 1999 3 19 DL72L990497 1 19990306 A 5532 651746160 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 THE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT FIN STA 42 AT STRINGER 1R BETWEEN RIB 3A AND 4. THE CRACK WAS LOCATED BELOW AN EXISTING REPAIR. THE EXISTING REPAIR WAS REMOVED AND BOTH DAMAGE LOCATIONS INCORPORATED INTO ONE REPAIR PER B 727 SRM 55-30-3, FIG 1. THE REPAIR WAS DOCUMENTED PER ER/A 366859-14. 2 L 7 3 4F A3WE 1999031900706 19990319 00706 NM 1999 3 19 DL72W990498 1 19990310 A 7120 65312814 ANGLE BOEING 727 727247 138408F NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 ON HUSH-KIT MOD FOUND RT NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REPLACED CHORD ANGLE WITH PART OF N EW MFG. 2 L 7 3 4F A3WE 1999031900707 19990319 00707 NM 1999 3 19 DL72E990499 1 19990310 A 3350 RPS1 POWER SUPPLY RPSI BOEING 727 727247 138408F NM CABIN INOP A DALA K NONE L NO TEST CR CRUISE 1 SO 27 2829W 0930 21481 EMERGENCY EXIT LIGHTING FLICKERED ON AND OFF DURING FLIGHT. REPLACED F/C EMER LIGHT POWER SUPPLY AND BATTERY TEST OK. 2 L 7 3 4F A3WE 1999031900708 19990319 00708 NM 1999 3 19 DL76L990500 1 19990310 A 3350 07912 LENS BOEING 767 767332 1382001 NM ROW 2C MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 186DN 27962 ON O/W 2 CHECK, FOUND ONE EMERGENCY TRACK LIGHT LENS AND BULB MISSING AT SEAT ROW 2C. RELAMPED AND REPLACED MISSING TRA CK LIGHT LENS, OPS CKS OK. 2 L 7 2 4F RT A1NM 1999031900709 19990319 00709 NM 1999 3 19 DL72S990501 1 19990310 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND ON F1 LETTER CK, AFT ENTRY DOOR FRAME CRACKED RT SIDE 10 INCHES BELOW THE TOP OF THE DOOR CUTOUT. REPAIRED PER SR M 53-10-9. 2 L 7 3 4F A3WE 1999031900710 19990319 00710 NM 1999 3 19 DL72E990502 1 19990310 A 3350 POWER SUPPLY RPS1 BOEING 727 727247 138408F NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 930 21481 ALL EMER LIGHTS TURN ON AND OFF WITHOUT CONTROL SWITCH TURNED ON. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 3 4F A3WE 1999031900711 19990319 00711 NM 1999 3 19 DL757990503 1 19990310 A 2560 D30654122 SLIDE BOEING 757 757232 1384965 NM L1 DOOR DEPLOYED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 638DL 23761 1L SLIDE FELL OUT ONTO JETWAY. DOOR OPENED WHILE SLIDE ARMED. REPLACED L1 SLIDE ASSY AND DOOR ASSIST BOTTLE. 2 L 7 2 4F RT A2NM 1999031900712 19990319 00712 NM 1999 3 19 DL73K990504 1 19990310 A 2530 COFFEEMAKER 5374AD BOEING 737 737232 1384475 NM GALLEY MALFUNCTIONED A DALA C D H ABORTED TAKEOFF RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 316DL 293 23088 DISCONTINUED TAKEOFF DUE TO ELECTRICAL ODOR IN AFT GALLEY. F/A REPORTED C/B PANEL WARM TO TOUCH. TURNED OFF GALLEY PWR AND RETURNED TO GATE. INSPECTED AFT GALLEY C/B PANEL AND WIRING, REPLACED BOTH COFFEEMAKERS AS A PRECAUTION. ALSO, CL EANED COFFEE RESIDUE FROM BENEATH COFFEEMAKERS. APPLIED ELECTRICAL PWR, SYS OPS NORMAL. 2 L 7 2 4F RT A16WE 1999031900713 19990319 00713 NM 1999 3 19 DL72S990505 1 19990310 A 5522 657278420 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 A .5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT FWD SPAR AREA. REPAIRED PER SRM 55-20-3 FIG 4. 2 L 7 3 4F A3WE 1999031900714 19990319 00714 NM 1999 3 19 DL733990506 1 19990310 A 2910 BACH8B04NN0166T LINE BOEING 737 737347 1384647 NM NOSE GEAR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 302WA 23182 AFTER INITIAL GEAR RETRACTION, NOSE GEAR RE-EXTENDED WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR HANDLE HAD NO E FFECT. NOSE GEAR REMAINED DOWN AND LOCKED. FOUND NOSE GEAR UPLOCK ACT UPPER LINE LEAKING HYD FLUID. LINE REPLACED. 2 L 7 2 4F RT A16WE 1999031900715 19990319 00715 NM 1999 3 19 DL72S990507 1 19990310 A 5754 STIFFENER BOEING 727 727232 1384082 NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND ON F1 LETTER CK, L/E SPAR STIFFENER CRACKED AT LOWER END NR 3 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999031900716 19990319 00716 NM 1999 3 19 DL72S990508 1 19990310 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND ON F1 LETTER CK, CRACK IN NR 1 SLAT ACTUATOR SUPPORT BRACKET WEB I/B SIDE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999031900717 19990319 00717 NM 1999 3 19 DL72S990509 1 19990310 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 A .25 INCH CRACK FUSELAGE SKIN AT FASTENER JUST AFT OF L-3 COCKPIT WINDOW. REPAIRED PER SRM 53-30-3 FIG 8. 2 L 7 3 4F A3WE 1999031900718 19990319 00718 NM 1999 3 19 DL72S990510 1 19990310 A 5754 65162232 ANGLE BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 REPAIR ANGLE CRACKED NR 7 SLAT STOP PAD I/B SIDE. REPAIRED PER MM 57-54-0 PG 816. 2 L 7 3 4F A3WE 1999031900719 19990319 00719 NM 1999 3 19 DL72W990511 1 19990310 A 3350 OL3071BPEGPL BULB BOEING 727 727247 138408F NM DOOR 2L FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2814W 20870 2L EMERGENCY EXIT SIGN INOP. RELAMPED EXIT SIGN, OPS CK NORMAL. 2 L 7 3 4F A3WE 1999031900720 19990319 00720 NM 1999 3 19 DL72K990512 1 19990311 A 2761 65C163002 ACTUATOR BOEING 727 727232 1384082 NM NR 14 SPOILER LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 410DA 21222 ON WALKAROUND INSPECTION, FOUND NR 14 SPOILER ACTUATOR LEAKING. 2 L 7 3 4F A3WE 1999031900721 19990319 00721 NM 1999 3 19 DL72E990513 1 19990311 A 3350 POWER SUPPLY RPS1 BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 2829W 1919 21481 EMERGENCY EXIT LIGHTS ILLUMINATED IN FLIGHT, CHECKED COCKPIT SWITCH. REPLACED AFT EMERGENCY LIGHTS POWER SUPPLY. 2 L 7 3 4F A3WE 1999031900722 19990319 00722 NM 1999 3 19 DL73K990514 1 19990311 A 3320 LIGHTS BOEING 737 737232 1384475 NM GALLEY ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 316DL 23088 2L AFT GALLEY HAS ELECTRIC SMELL WHEN GALLEY LIGHTS ON. INSP AFT GALLEY FLUORESCENT LIGHTS AND WIRING, NO SIGNS OF BURN ED WIRING. DEACTIVATED THRESHOLD AND WORK LIGHTS IN AFT GALLEY C/B PULLED AND COLLARD BEHIND CAPTS SEAT. 2 L 7 2 4F RT A16WE 1999031900723 19990319 00723 NM 1999 3 19 DLM88990515 1 19990311 A 2910 LINE 240S5895031 DOUG MD88 MD88 3023688 NM RT PYLON WORN A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 922DL 49646 RIGHT HYD SYSTEM PRESSURE INDICATES ZERO AND HYD QUANTITY SHOWS 3 QTS. FOUND PRESSURE LINE AT RT ENG PYLON WORN THRU BY CLAMP. REPLACED HOSE AND CLAMP. ALSO, CASE DRAIN FILTERS, NO METAL FOUND. SERVICED HYD, RAN ENG AND AUX PUMP , NO LEAKS FOUND. 2 L 7 2 4F RT A6WE 1999031900724 19990319 00724 SO 1999 3 19 SWIA971430 1 19990309 A 3620 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT BLEED DUCT ILLUMINATED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 578SW 120346 LEFT DUCT LEAK CAME ON SHORTLY AFTER TAKEOFF. SHUT DOWN NR 1 ENGINE AND THE LIGHT WENT OUT. RETURNED TO SAN. REMOVED INBOARD LEADING EDGE AND WING ROOT FAIRINGS (LEFT). INSPECTED ALL LINES, DUCTS AND CLAMPS, NO LEAKS NOTED. OHMED OUT A LL DUCT SENSORS, NO DEFECTS NOTED. CHECKED WATER SEPARATOR AND 18 PSI REGULATOR, NO LEAKS NOTED. COULD NOT DUPLICATE P ROBLEM. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900725 19990319 00725 SO 1999 3 19 SWIA971431 1 19990309 A 3297 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 190SW 120050 ON GEAR RETRACTION, RIGHT MAIN SYSTEM B LIGHT DID NOT ILLUMINATE. GREEN LIGHT SYSTEM REMAINED ILLUMINATED THE ENTIRE TI ME. DID NOT EXTINGUISH AFTER RETRACTION. RETURNED TO SLC. REMOVED AND REPLACED B WIRE HARNESS ON RIGHT MLG IAW EMB MM 32-61-01, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900726 19990319 00726 SO 1999 3 19 SWIA971432 1 19990309 A 3010 HOSE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT DEICE SYST FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 195SW 120127 LEFT AND RIGHT OUTBOARD AND VERTICAL STAB DEICE BOOTS FAILED, BOTH TIMERS, HEAVY AND LIGHT. RETURNED TO SLC. REMOVED A ND REPLACED FLEXIBLE BLEED AIR HOSE ON LEFT ENGINE IAW 30-00-00. OPS CHECK SYSTEM IAW 30-10-00. NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900727 19990319 00727 SO 1999 3 19 SWIA971433 1 19990309 A 3010 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT DEICE SYST FAILED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 578SW 120346 DUCT LEAKAGE LIGHT ILLUMINATED IN FLIGHT NR 1 ENGINE. LEFT ENGINE SHUT DOWN. RETURNED TO SBA. LIGHT EXTINGUISHED UPON ENGINE SHUT DOWN. REMOVED AND REPLACED LEFT DEICE PRESSURE REGULATING VALVE WITH A SERVICEABLE ONE IAW EMB 120 MM CH 3 0-10-06. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031900759 19990319 00759 NM 1999 3 19 TWAA9903901 1 19990311 A 3397 WIRE BOEING 767 767330 NM ROW 35-37 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 THE CABIN EGRESS LIGHTS WERE FOUND INOPERATIVE ON THE LT SIDE OF CABIN ROWS 35 TO 37, AND RT SIDE OF CABIN ROW 37. FOUN D SEVERAL LOOSE WIRES ON EGRESS LIGHT ASSEMBLY, AND RECONNECTED SAME. CHECK-C 2-6-99 LAX. 2 L 7 2 4F RT A1NM 1999031900760 19990319 00760 WP 1999 3 19 TWAA9903902 1 19990312 A 3350 LAMP DOUG DC9 DC983 3022083 WP ROW 3 & 21-24 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9413T 53188 FOUND EGRESS LIGHTS INOPERATIVE ON TEST AT ROW 21 TO 24, AND ROW 3. SECURED A LOOSE LIGHT SOCKET AT ROW 24, AND INSTALL ED A LOOSE LAMP AT ROW 3. CHECK-C 9-1-98 STL. 2 L 7 2 4F RT A6WE 1999031900761 19990319 00761 NM 1999 3 19 TWAA9903903 1 19990314 A 3350 767 BULB BOEING 767 7673Y0 NM ROW 3-5 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 FOUND CABIN EGRESS LIGHTS INOPERATIVE ON RT SIDE OF CABIN ROWS 3 TO 5, AND THE RT SIDE NUMBER 3 EXTERIOR DOOR EMERGENCY LIGHT INOPERATIVE. SECURED THE CONNECTOR FOR THE EGRESS LIGHTS, AND RELAMPED THE EMERGENCY LIGHTS. CHECK-C 3-3-99 LAX. 2 L 7 2 4F RT A1NM 1999031900762 19990319 00762 WP 1999 3 19 TWAA9903904 1 19990313 A 5620 WINDOW DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON CABIN WINDOWS ON RT SIDE OF ACFT NUMBERS 6, 7, 13, 14, AND 15. BLENDED P ER SRM 53-05 FIG 111. REPAIRED PER ARA 16117. 2 L 7 2 4F A6WE 1999031900763 19990319 00763 WP 1999 3 19 TWAA9903905 1 19990310 A 5620 WINDOW DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON CABIN WINDOWS ON LEFT SIDE OF CABIN NUMBERS 31 AND 32. BLENDED PER SRM 5 3-05 FIG III. REPAIRED PER ARA 16114A AND SERVICE REPAIR DRAWING SR09530053. 2 L 7 2 4F A6WE 1999031900764 19990319 00764 WP 1999 3 19 TWAA9903906 1 19990308 A 5315 SUPPORT DOUG DC9 DC931 3022065 WP BS 160-200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT CORRODED TOP AND BOTTOM SIDES AT STA 160 TO 200, RBL 44 IN. REPLACED PART PER SPM 6-70-1 AR 2 FROM STA 160 TO 200. 2 L 7 2 4F A6WE 1999031900765 19990319 00765 WP 1999 3 19 TWAA9903907 1 19990311 A 5620 WINDOW DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP1 6 MAINT CHECK, FOUND WINDOWS 3, 4, AND 5 ON LEFT SIDE OF AIRCRAFT WITH STATIC BURNS. BLENDED EACH PER SRM 53 -05 FIG III, AND ARA 16105. INSTALLED EXTERNAL REPAIR ON EACH PER DRAWING SR0950053 AND ARA 16105. 2 L 7 2 4F A6WE 1999031900766 19990319 00766 WP 1999 3 19 TWAA9903908 1 19990311 A 5347 TRACK DOUG DC9 DC931 3022065 WP BS 760-996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND EXFOIL CORROSION ON CARGO COMPT FLOOR TRACK IN THE AFT CARGO COMPT AT THE LT FWD TRACK, FWD OF DOOR CUTOUT ON RT SIDE FROM STA 760 TO 996. REPLACED WITH NEW TRACK PER TWA SPM 6-70-01, AND DOUGLAS PRINT 59560 33. 2 L 7 2 4F A6WE 1999031900767 19990319 00767 WP 1999 3 19 AT9900194 1 19990307 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 189 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND REAR SPAR LOWER CHORD AFT TANG HAS A CRACK INDICATION AT INB OARD BUTE DOOR THIRD HOLE FROM OUTBOARD END. STEPPED UP HOLE TO .437, FABRICATED AND INSTALLED BUSHING IAW DC9 SRM 51-1 0-3 AND SB 57-150 RZ AND DRAWING NR J060173 AND RES NR 99440. 2 L 7 2 4F A6WE 1999031900768 19990319 00768 WP 1999 3 19 AT9900195 1 19990312 A 5713 STRINGER DOUG DC9 DC932 3022066 WP RT WING ELONGATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND TWO ELONGATED BOLT HOLES IN THE RIGHT HAND CENTER WING STRINGER 11. REAME D TWO HOLES, AND INSTALLED TWO BUSHING IAW RES NR 99546, RES NR 99582, AND AERO CORP EO 96-406 REV IR DATED 12/21/96 APP ROVED BY DER NR NM-1824 DATED 12/9/96. 2 L 7 2 4F A6WE 1999031900769 19990319 00769 WP 1999 3 19 AT9900196 1 19990302 A 5320 124530212 WEB DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND FLOOR WEB AT BS 617 CRACKED. FORMED DOUBLERS, DRILLED, DEBU RRED, TREATED, PRIMED, AND COMPLIED WITH RES NR 99358. REINSTALLED REMOVED BAFFLES, AND INSTALLED REPAIR IAW DC9 SRM 51 -10-3, 53-20-1, 51-30-2, AND 51-10-4. 2 L 7 2 4F A6WE 1999031900770 19990319 00770 WP 1999 3 19 AT9900197 1 19990313 A 5414 SKIN DOUG DC9 DC932 3022066 WP BS 1030-1076 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 1 PYLON TRAILING EDGE PANEL LOWER SIDE SKIN REPAIR DISBONDED AND CO RNERS CRACKED OFF AT BS 1030 TO 1076. REMOVED SKIN, FABRICATED NEW SKIN, DRILLED, DEBURRED, COUNTERSUNK, TREATED, PRIME D, AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2, AND RES NR 99584. 2 L 7 2 4F A6WE 1999031900771 19990319 00771 WP 1999 3 19 AT9900198 1 19990212 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 195 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT OUT OF LIMITS AT BS 195R. FABRICATED DOUBLER AND FINGER DOUBLER, D RILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-2, AND RES NR 99443. 2 L 7 2 4F A6WE 1999031900772 19990319 00772 WP 1999 3 19 AT9900199 1 19990212 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 870 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT LEFT HAND FLOOR SUPPORT FRAME CRACKED AT BS 870. REMOVED CRAC KED FRAME, REPAIR FRAME IAW DC9 EA NR 12-5321-29-C1362 AND REINSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999031900773 19990319 00773 WP 1999 3 19 AT9900200 1 19990211 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 692 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND LOWER FUSELAGE FRAME FITTING AT BS 692 CRACKED AT THE BOLT H OLE IN UPPER FLANGE IN FORWARD LOWER INBOARD CORNER OF LEFT WHEEL WELL. STOP DRILLED CRACK, VERIFY BY HFEC, FABRICATED REPAIR ANGLE, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2A, 51-10-3, AND RES NR 99388. 2 L 7 2 4F A6WE 1999031900774 19990319 00774 WP 1999 3 19 AT9900201 1 19990309 A 5230 5714951503 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR DAMAGE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AEROCORP, FL. FOUND THE FORWARD CARGO DOOR LATCH SUPPORT FITTING REQUIRED REPLACEMENT. INSTALL ATION OF THE NEW FITTING REQUIRED TRIMMING OF THE DOOR INNER SKIN AROUND ONE OF THE LIGHTENING HOLES. THE BEADED FLANGE AT THE LOWER CORNERS OF THE TRAPEZODIAL CUTOUT WERE TRIMMED IN ORDER TO INSTALL THE NEW LATCH SUPPORT FITTING. REPAIR WAS ACCCOMPLISHED IAW DC9 SRM 52-05 FIG 7, 52-31-0 FIG 1, AND AERO CORP EO 99-1096. 2 L 7 2 4F A6WE 1999031900775 19990319 00775 1999 3 19 CKSA99003 4 19990308 A 2565 74A14122 SLIDE BOEING 747 747269B NM CREW DOOR DEPLOYED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 5477 21541 ON ARRIVING AT AIRCRAFT FOR PREFLIGHT, FOUND UPPER DECK CREW DOOR OPEN, CREW ESCAPE SLIDE PARTIALLY DEPLOYED. THE FOLLO WING WAS DETERMINED: SLIDE WAS IN PROPER POSITION FOR DEPLOYMENT, DOOR WAS FOUND OPEN WITH DOOR HANDLE IN ARMED POSITION , SLIDE BOTTLE TO DEPLOY SLIDE PACK OUT THE DOOR DISCHARGED, THE FORWARD CABLE ON SLIDE PACK RELEASED, THE AFT CABLE DID NOT, CAUSING THE SLIDE PACK TO COCK AND JAM AGAINST THE LAV BULKHEAD. THIS ACTION PREVENTED THE SLIDE FROM PROPERLY DE PLOYING. WITH SLIDE JAMMED THE HOSE FROM MAIN INFLATION BOTTLE WAS CUT TO PREVENT POSSIBLE DAMAGE. SLIDE PACK THEN REM OVED FROM AIRCRAFT. 2 L 7 4 4F RT A20WE 1999031900776 19990319 00776 EU 1999 3 19 JBXA9900075 1 19990314 A 3150 800610340 COMPUTER FOKKER F28 F28MK0100 4990807 EU E & E COMPT INOPERATIVE A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 103ML 11444 ON TAKEOFF ROLL, CREW ABORTED DUE TO GROUND/FLIGHT CONTROL FAULT ON LT MFDU. ALSO, LIFT DUMPER UNSAFE AND NO AUTO PILOT BELOW 500 FEET. REMOVED AND REPLACED FLIGHT WARNING COMPUTER IAW F-100 MM 31-51-01, OPS CHECK GOOD. 2 L 7 2 4F RT 1999031900777 19990319 00777 NM 1999 3 19 CALA9900246 1 19990312 A 3260 656021132 ACCESSORY UNIT BOEING 727 727232 1384082 NM E & E COMPT INOP A CALA O OTHER N FALSE WARNING DE DESCENT 1 SW 09 15781 19212 20636 BOTH RT MLG RED AND GREEN ANNUNCIATOR LIGHTS ILLUMINATED DURING DESCENT. THE GEAR HANDLE WAS CYCLED FROM UP TO OFF AND THE GEAR DOOR LIGHT CAME ON. WHEN GEAR WAS SELECTED TO DOWN, GOT THREE GREEN AND LANDING WAS NORMAL. THE LANDING GEAR AND DOORS WERE INSPECTED WITH NO DEFECTS NOTED. THE LANDING GEAR ACCESSORY UNIT WAS REPLACED. SLUGGED GEAR AND CHECKED INDICATIONS IN UP, OFF, AND DOWN AND ALL WERE NORMAL. GEAR DOOR OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1999031900778 19990319 00778 WP 1999 3 19 CALA9900247 1 19990312 A 5720 SUPPORT DOUG DC10 DC1030 3023501 WP LT & RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND LT AND RT MLG CYLINDER SUPPORT FRAME CORRODED IN ATTACHMENT BOLT HOLES. THE BOLT HOLES WERE REPAIRED I AW ECRA 5743-01015. 2 L 7 3 4F A22WE 1999031900779 19990319 00779 WP 1999 3 19 CALA9900248 1 19990312 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND A 4 INCH CRACK IN RT WING LEADING EDGE UPPER SKIN AT NR 8 L/E SLAT TRACK. THE AREA WAS REPAIRED IAW EC RA 5720-01725. A DIP WAS ISSUED TO PERFORM A VISUAL INSPECTION EVERY SERVICE CHECK AND PENETRANT EVERY SEVEN DAYS WITH PERMANENT REPAIR AT NEXT 1/4D CHECK. 2 L 7 2 4F A6WE 1999031900780 19990319 00780 NM 1999 3 19 CALA9900249 1 19990313 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND FLOORBEAM CAP CORRODED AROUND FASTENER HOLES AT STA 344 FROM RBL 12 TO LBL 15. REPLACED BEAM IAW SRM 5 3-10-51. 2 L 7 2 4F RT A16WE 1999031900781 19990319 00781 NM 1999 3 19 CALA9900250 1 19990313 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 11 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND LT EMERGENCY PATH LIGHT ON SEAT AT ROW 11 INOPERATIVE. INSPECTION FOUND PATH LIGHT WIRE BROKEN. THE W IRE WAS REPAIRED AND STOWED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00, PAGE 102. 2 L 7 3 4F A3WE 1999031900782 19990319 00782 WP 1999 3 19 CALA9900251 1 19990314 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1701 & 1781 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND CENTER CARGO DOOR APERTURE AFT FRAME AND FORWARD FRAME CORRODED AT STA 1781 AND 1701. THE FRAME AREAS WERE REPAIRED IAW SRM 53-50-00. 2 L 7 3 4F A22WE 1999031900783 19990319 00783 EA 1999 3 19 COMA9960103 1 19990307 A 7830 1217542 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT ENG TR UNIT SEPERATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 7117 RIGHT THRUST REVERSER NR 2 FLEXSHAFT HAS STRAND SEPARATION. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1999031900784 19990319 00784 EA 1999 3 19 COMA9960104 1 19990311 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 946CA 7072 FLAPS FAIL MESSAGE. INSPECTED FLAPS PER AD 98-20-01. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999031900785 19990319 00785 EA 1999 3 19 COMA9960105 1 19990311 A 2760 INDICATION CNDAIR CL600 CL6002B19 EA SPOILERS MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 941CA 7050 CONFIG SPOILERS WARNING. COULD NOT DUPLICATE, RESET SECU'S AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999031900786 19990319 00786 EA 1999 3 19 COMA9960106 1 19990312 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 776CA 7293 FLAPS FAILED AT 42 DEGREES. RESET FLAP SYSTEM IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 1999031900787 19990319 00787 EA 1999 3 19 COMA9960107 1 19990312 A 2750 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 776CA 105 7293 FLAPS STUCK AT 37 DEGREES. REPLACED LEFT HAND INBORAD FLAP ACTUATOR AND FLEX DRIVE CABLE. 2 L 7 2 4F RT A21EA 1999031900788 19990319 00788 EA 1999 3 19 COMA996108 1 19990313 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 776CA 7293 FLAPS FAILED AT 42 DEGREES. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999031900789 19990319 00789 NM 1999 3 19 UPS99228975 1 19990215 A 5320 WEB BOEING 727 72731C 1384011 NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, TAIL SKID RECESS, WEB CORRODED AT AFT OF BS 1183 BULKHEAD. WEB REMOVED PER SRM 51-30-02, FABRICATED IAW SRM 53-10-02 FIG 6 AND INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1999031900790 19990319 00790 NM 1999 3 19 UPS99228976 1 19990312 A 2710 652611811 FITTING BOEING 727 727185C 138406N NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE-C, LT WING I/B AILERON TURN-AROUND PULLEY FITTING AT PULLEY BOLT HOLE IS CORRODED. REMOVED CORRODED PUL LEY FITTING, DRILLED UP NEW FITTING AND INSTALLED IAW MM 20-10-20, SRM 51-30-05, 51-30-02. 2 L 7 3 4F A3WE 1999031900791 19990319 00791 NM 1999 3 19 UPS99228977 1 19990312 A 5751 65217662 SKIN BOEING 727 727185C 138406N NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE-C, RT OUTBOARD AILERON HAS CORROSION ON LOWER SKIN AFT OF NR 2 HINGE AREA. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED RT OUTBOARD AILERON IAW MM 27-10-31. 2 L 7 3 4F A3WE 1999031900792 19990319 00792 NM 1999 3 19 UPS99228978 1 19990217 A 5754 RIB BOEING 727 727173C 1384059 NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, NR 4 K FLAP I/B BULLNOSE BONDING JUMPER CORROSION ON NUT SIDE OF RIB OF K-FLAP (C57-562-01.00-02). R EMOVED DAMAGE ON RIB, FABRICATED AND INSTALLED REPAIR ANGLES AND DOUBLER IAW SRM 57-50-3. RELOCATED BONDING JUMPER TO I NBOARD RIB IAW UPS ADENDUM EO B727-5740-3980. 2 L 7 3 4F A3WE 1999031900793 19990319 00793 NM 1999 3 19 UPS99228979 1 19990306 A 5311 6516396 FRAME BOEING 727 727173C 1384059 NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, CRACK IN FRAME AT STA 930, STR 14R, RBL 65, WL 232. TRIMMED CRACKED MATERIAL AWAY AND INSTALLED FRAM E REPAIR PER BAC DWG 65C10084. 2 L 7 3 4F A3WE 1999031900794 19990319 00794 NM 1999 3 19 UPS99228980 1 19990218 A 5754 SKIN BOEING 727 727173C 1384059 NM NR 2 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, CRACKS IN FASTENER HOLES ON NR 2 K-FLAP TAI SKIN FROM 17 I/B OF O/B EDGE AND 31 I/B OF O/B EDGE AND A T 39 I/B OF O/B EDGE. REMOVED TAI SKINS AT 17, 31 AND 39 OF O/B EDGE AND INSTALLED 3 NEW TAI SKINS IAW SRM 51-30-2, OHM 20-50-01. 2 L 7 3 4F A3WE 1999031900795 19990319 00795 NM 1999 3 19 UPS99228981 1 19990217 A 5754 BRACKET BOEING 727 727173C 1384059 NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, NR 4 K-FLAP CORROSION AROUND I/B NUT OF I/B BULLNOSE HINGE MOUNTING BRACKET ON K FLAP (C57-562-01.00- 02). REMOVED BOLT, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED BRACKET IAW UPS ER NR 99-5145 AND REINSTALL ED BOLT IAW MM 27-81-01. 2 L 7 3 4F A3WE 1999031900796 19990319 00796 NM 1999 3 19 UPS99228982 1 19990226 A 5313 STRINGER BOEING 727 727173C 1384059 NM BS 930-940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, WHILE WORKING CUSTOMER CARD NR 890693 (INT61) FOUND CORROSION AROUND FASTENERS HEADS ON STRINGER 18 RT STA 930 TO 940, WL 201. REMOVED FASTENERS, BLENDED CORROSION, REPAIRED AND REINSTALLED FASTENERS IAW UPS ER NR 99-51 39. 2 L 7 3 4F A3WE 1999031900797 19990319 00797 NM 1999 3 19 UPS99228984 1 19990219 A 5754 CARRIAGE BOEING 727 72731C 1384011 NM NR 6 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, NR 6 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE. CARRIAGE REPLACED IAW OHM 57-52-01 AND MM 27-51-03. 2 L 7 3 4F A3WE 1999031900798 19990319 00798 NM 1999 3 19 UPS99228985 1 19990216 A 5754 BRACKET BOEING 727 72731C 1384011 NM NR 4 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, CRACK ON ANGLE BRACKET ATTACHED TO FLAP TRACK FWD O/B SIDE. FABRICATED ANGLE IAW SRM 51-40-04. 2 L 7 3 4F A3WE 1999031900799 19990319 00799 NM 1999 3 19 UPS99228986 1 19990211 A 5754 65185338 HINGE BOEING 727 72731C 1384011 NM NR 1 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, NR 1 LE FLAP MIDDLE MOUNTING CASTING HINGE CORRODED. REPLACED CASTING HINGE IAW DRAWING NR 65-18533. 2 L 7 3 4F A3WE 1999031900800 19990319 00800 NM 1999 3 19 UPS99228987 1 19990216 A 5754 BRACKET BOEING 727 72731C 1384011 NM NR 5 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, NR 5 FLAP TRACK ANGLE SUPPORT BRACKET CRACKED AT FWD RT SIDE. BRACKET FABRICATED FROM EXTRUSION AND REPLACED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1999031900801 19990319 00801 NM 1999 3 19 UPS99228993 1 19990314 A 3397 WIRE BOEING 727 72725C 138400H NM ROW 3 BROKEN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, POS NR 2 EMERGENCY EXIT LIGHT AT SEAT 3. FOUND BROKEN WIRE. REPAIRED BROKEN WIRE, OPS CHK GOOD. 2 L 7 3 4F A3WE 1999031900802 19990319 00802 NM 1999 3 19 UPS99228994 1 19990312 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, LT UPPER 2 OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED 3 EXTERNAL BATTS, OPS CHECK G OOD. 2 L 7 3 4F A3WE 1999031900803 19990319 00803 NM 1999 3 19 UPS99228995 1 19990312 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, AFT BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTS, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999031900804 19990319 00804 NM 1999 3 19 UPS99228996 1 19990312 A 3350 LIGHT BOEING 727 72725C 138400H NM ROW 2 INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, ROW 2 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999031900805 19990319 00805 WP 1999 3 19 UPS99828974 1 19990312 A 3310 BALLAST DOUG DC8 DC873F 302199F WP NA RT COCKPIT FAILED A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 866UP 45966 INSPECTION TYPE-N/A, SMOKE IN FLT DECK, COMING FROM UNDER F/O'S GLARESHIELD. FOUND GLARESHIELD FLOOD LIGHTS, BALLAST (T RANSFORMER) BAD. REMOVED AND REPLACED BALLAST. 2 L 7 4 4F RT 4A25 1999031900806 19990319 00806 WP 1999 3 19 UPS99828983 1 19990310 A 3233 57740355507 ACTUATOR DOUG DC8 DC871F 302199D WP NLG FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SO 01 701UP 45938 INSPECTION TYPE-N/A, UPON LOWERING LANDING GEAR HANDLE ON APPROACH, A VERY LOUD VIOLENT NOISE WAS HEARD FROM WHAT SEEMED LIKE THE AREA OF THE NOSE GEAR. THE RT AND NOSE GEAR INDICATED DOWN AND LOCKED, THERE WAS NO GREEN GEAR DOWN LIGHT FOR THE LEFT GEAR. AT THE SAME TIME HYD SYS PRESS INDICATED ZERO AND THE HYD QTY WAS MOVING QUICKLY TOWARDS EMERGENCY HYD PUMPS SELECT BYPASS. ACCOMPLISHED LOSS OF ALL HYD CHECKLIST, LANDED SAFELY. 2 L 7 4 4F RT 4A25 1999031900807 19990319 00807 WP 1999 3 19 UPS99828988 1 19990217 A 5311 RIB DOUG DC8 DC873F 302199F WP BS 1910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, CRACKED RIB JUST FWD OF THE TAIL CONE ACCESS PANEL 62, RT SIDE FS AREA 1910. FABRICATED DOUBLER IAW DC-8 SRM 53-2-0, STOP DRILLED CRACK IAW 53-2- 0, LOCATED AND DRILLED DOUBLER IAW DC-8 SRM 52-3-2, ALODINED AND PRIMED D OUBLER IAW DC-8 SRM 51-1-18, INSTALLED DOUBLER IAW DC-8 SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 1999031900808 19990319 00808 WP 1999 3 19 UPS99828989 1 19990217 A 5311 RIB DOUG DC8 DC873F 302199F WP BS 1920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, TAIL CONE THRU PANEL 62 ACCESS, CRACKED RIB LT SIDE, FS 1920 AREA AT BRACKET. FABRICATED DOUBLER I AW DC-8 SRM 53-2-0, STOP DRILLED IAW DC-8 SRM 53 -2-0, LOCATED AND DRILLED DOUBLER IAW DC-8 SRM 51-3-2, ALODINED AND PRI MED DOUBLER IAW DC-8 SRM 51-1-8, INSTALLED DOUBLER IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900809 19990319 00809 WP 1999 3 19 UPS99828990 1 19990220 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, MAIN CABIN STA 680 AND 46 RBL 2-WL FITTING CRACKED AFT SIDE OF FLOORBEAM. REMOVED CRACKED FLOOR SUP PORT FITTING AT STA 680, RBL 46 LOCATED, DRILLED NEW FITTING IAW DC-8 SRM 51-3-2, INSTALLED NEW FITTING AT STA 68 0, RBL 46 IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900810 19990319 00810 WP 1999 3 19 UPS99828991 1 19990220 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 702 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, MAIN CABIN AT STA 702 AND 23 RBL AND 1-WL FITTING CRACKED AFT SIDE OF FLOORBEAM. REMOVED CRACKED FI TTING AT STA 702, RBL 23, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2, INSTALLED NEW FITTING IAW DC8 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900811 19990319 00811 WP 1999 3 19 UPS99828992 1 19990221 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 920-940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, BELOW CABIN FLOOR, STA 90 TO 940 X=O FINGER DOUBLER CORRODED. REMOVED FINGER DOUBLER, FOUND DOUBLER OUT OF LIMITS IAW DC-8 SRM 53-2-0. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0, FABBED NEW DOUBLER IAW DAC DWG 5645332, ALODINED AND PRIMED IAW DC- 8 SRM 51-1-8, INSTALLED DOUBLER IAW DC-8 SRM 51-1-8 AND 51-1-21. 2 L 7 4 4F RT 4A25 1999031900812 19990319 00812 WP 1999 3 19 UPS99828997 1 19990228 A 5320 WEB DOUG DC8 DC873F 302199F WP WHEEL WELL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT L24L SUB-STRUCTURE DOOR JAM WEB HAS A CRACK IN FLANGE RADIUS ACID TEST FOR MATERIAL ID IAW MIL-S TD-271F. RECEIVED MATERIAL VERIFICATION, FABBED DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. I NSTALLED DOUBLER IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999031900813 19990319 00813 WP 1999 3 19 UPS99828998 1 19990219 A 5320 FRAME DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, MAIN CARGO DOOR AFT FRAME AT DOOR CUTOUT CRACKED ATTACH ANGLE DAMAGED TRIM. REMOVED FRAME SCUFFPLAT E, FABBED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. ALODINED AND PRIMED DOUBLER IAW DC8 SRM 51-1-8. INSTALLED DOUBLER ON FRAME SCUFFPLATE WITH RIVETS IAW DC8 SRM 51-1-21. INSTALLED FRAME SCUFFPLATE WITH RIVETS AND SCREWS IAW DC8S RM 51-1 -21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999031900814 19990319 00814 WP 1999 3 19 UPS99828999 1 19990218 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 940 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, STA 940 TRACK HAS A SCALLOP GOUGED AND TANG BROKEN OFF. REMOVED SEAT TRACK FROM SPLICE TO SPLICE. L OCATED AND DRILLED NEW SEAT TRACK (2 EA) AND SPLICE IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTA LLED IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999031900815 19990319 00815 WP 1999 3 19 UPS99829000 1 19990217 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1463 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, SKIN AT STA 1463, LONG 24R DENTED. REMOVED FASTENERS IAW DC8 SRM 51-1-21 AND CUT OUT DAMAGE SKIN IA W SRM 53-2-1, FABRICATED DOUBLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC8S SRM 51-1-8. INSTALLED DOUBLERS IAW S RM 53-2-1. 2 L 7 4 4F RT 4A25 1999031900816 19990319 00816 WP 1999 3 19 UPS99829001 1 19990217 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT UPPER FRAME FLANGE AT FS 1020 CORRODED UNDER NUT PLATE AT L35L AND L34R. CORROSION OUT OF L IMITS. FAB REPAIR ANGLE AND REPAIR FILLER IAW DC8 DD 53.0229. ALODINED AND PRIMED, REPAIRED PARTS AND INSTALLED IAW DC 8 SRM 51-1-2, 51-1-20 D, AND 51-1-16. 2 L 7 4 4F RT 4A25 1999031900817 19990319 00817 WP 1999 3 19 UPS99829002 1 19990217 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT UPPER FRAME FLANGE AT FS 1060 L36 CORRODED BEYOND LIMIT. REMOVED FRAME CAP, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND FILLER, ALODINED AND PRIMED, INSTALLED REPAIR ANGLE FILLER AND FRAME CAP. 2 L 7 4 4F RT 4A25 1999031900818 19990319 00818 WP 1999 3 19 UPS99829003 1 19990222 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, LT ELEV UPPER SKIN CRACKED STA XE77. REMOVED DAMAGED AREA IAW DC8 SRM 55-2-1, FABBED REPAIR DOUBLER AND FILLER IAW DC8 SRM 55-2-1, ALODINED IAW DC8 SRM 51-1-8, COLD BONDED REPAIR AND SEALED DOUBLER IAW DC8 SRM 51-1-9A, INSTALLED DOUBLERS IAW DC8 SRM 51-1-21A. 2 L 7 4 4F RT 4A25 1999031900819 19990319 00819 WP 1999 3 19 UPS99829004 1 19990221 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 960-980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, BELOW CABIN FLOOR STA 960 TO 980 X=0 CORR AT FINGER DOUBLER OUT OF LIMITS. ALSO, FOUND CRACK. FABR ICATED DOUBLER, FILLER AND REPAIR DOBULER IAW REO-06349. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900820 19990319 00820 WP 1999 3 19 UPS99829005 1 19990219 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1040 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, STA 1040 TRACK G SCALLOPS GOUGED. REMOVED DAMAGED SEAT TRACK, FAB SEAT TRACK AND SPLICES IAW DC8 SR M 5 3-2-3. ALODINED AND PRIMED IAW SRM DC8 51-1-8, INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999031900821 19990319 00821 WP 1999 3 19 UPS99829006 1 19990221 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT FS 1460 FLOOR SUPPORT CRACKED AT L34L. REMOVED CRACKED SUPPORT FITTING, FAB NEW FITTING, AL ODINED AND PRIMED, INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999031900822 19990319 00822 WP 1999 3 19 UPS99829007 1 19990220 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 80 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, CABIN FLOOR PRESSURE PANEL DOUBLER BULGED STA 80 RBL 20. REMOVED FINGER DOUBLER, MAT ID FROM DOUBLE R SRM 53-3-3. FAB DOUBLER IAW DAC DWG 5612298, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900823 19990319 00823 WP 1999 3 19 UPS99829008 1 19990222 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1198 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, LONG 33L AT STA 1190 CORROSION. FAB REPAIR ANGLE IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 S RM 51-1-8. INSTALLED IAW DC8 SRM 53-2-2. 2 L 7 4 4F RT 4A25 1999031900824 19990319 00824 WP 1999 3 19 UPS99829009 1 19990218 A 5320 RUB STRIP DOUG DC8 DC873F 302199F WP LT MLG DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, LT MLG DOOR FWD RUB STRIP WORN AND GOUGED. CUT OUT DAMAGED AREA, FAB REPAIR PARTS, FILLER ANGLES AN D STRAP. WELDED DOUBLER, DYEPENNED CK REPAIR ANGLES. NO CRACKS. INSTALLED IAW REO 06324. 2 L 7 4 4F RT 4A25 1999031900825 19990319 00825 WP 1999 3 19 UPS99829010 1 19990222 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1230-1240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT STA 1230 TO 1240 LONGERON 33L CORRODED. REMOVED LONG, SHEAR TIE AND FITTINGS, FABED LONGERO N, SHEAR TIE SPLICE, SPLICE ANGLES FOR FITTINGS AND FITTINGS IAW DC8 SRM 51-1-8, DAC DWG 9758504, SRM 51-1-20D, 53-4-1, 53-2-0. INSTALLED ALL IAW DC8 SRM 51-1-20D, 53-4-1, 53-2-0. 2 L 7 4 4F RT 4A25 1999031900826 19990319 00826 WP 1999 3 19 UPS99829011 1 19990217 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1120-1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT INTERCOSTAL AT L33R FS 1120 TO 1140 CORRODED BEYOND LIMIT. REMOVED INTERCOSTAL, FORMED NEW INTERCOSTAL IAW DAC 9754949. HEAT TREATED IAW DAC DWG 9754949. LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED IAW DAC DCWG 9754949 ADN DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900827 19990319 00827 NM 1999 3 19 QXEA9900427 1 19990303 A 5753 TRACK DHAV DHC8 DHC8102 2809003 NM RT TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - NR 3 RIGHT-HAND FLAP TRACK HAS LIGHT TO MODERATE SURFACE PITTING ON LOWER TRACK TOP SURFACE IN ROLLER PATH AND UPP ER TRACK BOTTOM SURFACE IN ROLLER PATH. REPAIRED IAW HORIZON AIR EA 9-57-406. 2 H 7 2 4T RT A13NM 1999031900828 19990319 00828 NM 1999 3 19 QXEA9900430 1 19990227 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - LADDER PLATE UNDER PANEL 521AT HAS FRETTING CORROSION. REPAIRED IAW RD 8-57-592. 2 H 7 2 4T RT A13NM 1999031900829 19990319 00829 NM 1999 3 19 QXEA9900433 1 19990302 A 5400 LINK DHAV DHC8 DHC8102 2809003 NM NACELLE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - EXCESSIVE AXIAL PLAY ON INBOARD SIDE OF LINK ASSEMBLY. REPAIRED IAW HORIZON AIR EA 9-54-192. 2 H 7 2 4T RT A13NM 1999031900830 19990319 00830 NM 1999 3 19 QXEA9900434 1 19990219 A 5311 CASTELLATION DHAV DHC8 DHC8102 2809003 NM FRAME 4 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME 4 HAS CRACKED CASTELLATION AT STRINGER 12P. REPAIRED IAW SRM 53-20-21. 2 H 7 2 4T RT A13NM 1999031900831 19990319 00831 NM 1999 3 19 QXEA9900435 1 19990219 A 5311 CASTELLATION DHAV DHC8 DHC8102 2809003 NM FRAME 4 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME 4 HAS CRACKED CASTELLATION AT STRINGER 12S. REPAIRED IAW SRM 53-20-21. 2 H 7 2 4T RT A13NM 1999031900832 19990319 00832 NM 1999 3 19 QXEA9900436 1 19990215 A 5415 FITTING DHAV DHC8 DHC8102 2809003 NM LT NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - LEFT-HAND NACELLE HAS MINOR FRETTING CORROSION UNDER MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING. RE PAIRED IAW RD 8-54-735. 2 H 7 2 4T RT A13NM 1999031900833 19990319 00833 NM 1999 3 19 QXEA9900437 1 19990228 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 618 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME 618 AT STRINGER 18 HAS 2 WEAR MARKS FROM GILE LINER SUPPORT BRACKET. REPAIRED IAW SRM 51-20-11 AND 51-20-16 . 2 H 7 2 4T RT A13NM 1999031900834 19990319 00834 NM 1999 3 19 QXEA9900438 1 19990228 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 646 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME 646 AT STRINGER 18 HAS 2 WEAR MARKS FROM GILE LINER SUPPORT BRACKET. REPAIRED IAW SRM 53-20-21, FIGURE 6. 2 H 7 2 4T RT A13NM 1999031900835 19990319 00835 NM 1999 3 19 QXEA9900439 1 19990224 A 5320 SILL DHAV DHC8 DHC8102 2809003 NM PILOT WINDOW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - PILOT SIDE WINDOW LOWER SILL JOINT TO SIDE POST HAS A 1 INCH CRACK. REPAIRED IAW RD 8-53-576. 2 H 7 2 4T RT A13NM 1999031900836 19990319 00836 NM 1999 3 19 QXEA9900440 1 19990302 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 618 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - CHAFE DAMAGE ON RIGHT-HAND CARGO PIT FRAME AT STATION 618 BETWEEN STRINGER 20 TO 22. REPAIRED IAW HORIZON AIR EA 9-53-443. 2 H 7 2 4T RT A13NM 1999031900837 19990319 00837 NM 1999 3 19 QXEA9900441 1 19990225 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 580.5 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - RIGHT-HAND CARGO PIT FRAME IS DENTED AT STATION 580.5 AND STRINGER 22. REPAIRED IAW HORIZON AIR EA 9-53-437. 2 H 7 2 4T RT A13NM 1999031900838 19990319 00838 NM 1999 3 19 QXEA9900442 1 19990227 A 5320 SILL DHAV DHC8 DHC8102 2809003 NM CARGO DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - BAGGAGE DOOR CUTOUT UPPER SILL INNER STRAPS HAVE CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 9-53-440. 2 H 7 2 4T RT A13NM 1999031900839 19990319 00839 NM 1999 3 19 QXEA9900443 1 19990305 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 312.35 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - DENT IN FUSELAGE SKIN JUST AFT OF LEFT-HAND ICE SHIELD AT STATION 312.350 AND STRINGER 12. REPAIRED IAW HORIZON A IR EA 9-53-442B. 2 H 7 2 4T RT A13NM 1999031900840 19990319 00840 NM 1999 3 19 QXEA9900444 1 19990225 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - LEFT-HAND AFT REAR WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999031900841 19990319 00841 NM 1999 3 19 QXEA9900445 1 19990225 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - RIGHT-HAND AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999031900842 19990319 00842 NM 1999 3 19 QXEA9900446 1 19990223 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - RIGHT-HAND FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-41-11. 2 H 7 2 4T RT A13NM 1999031900843 19990319 00843 NM 1999 3 19 QXEA9900447 1 19990222 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - LEFT-HAND FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999031900844 19990319 00844 NM 1999 3 19 QXEA9900448 1 19990221 A 5320 SILL DHAV DHC8 DHC8102 2809003 NM RT EMER EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - SLIGHT CORROSION ON TOP SURFACE OF LOWER SILL AT RIGHT-HAND CENTER EMERGENCY EXIT AT AFT INBOARD NUT PLATE. REPAI RED IAW SRM 51-00-04. 2 H 7 2 4T RT A13NM 1999031900845 19990319 00845 NM 1999 3 19 QXEA9900449 1 19990215 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM LT COCKPIT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - PILOTS SEAT TRACKS HAVE LOOSE OR MISSING REPAIR BUSHINGS. REPLACED BUSHINGS IAW RD 8-53-219. 2 H 7 2 4T RT A13NM 1999031900846 19990319 00846 NM 1999 3 19 QXEA9900450 1 19990305 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - THERE IS LIGHT FRETTING CORROSION IN THE FUSELAGE SKIN AROUND SEVEN SCREW HOLES UNDER THE RIGHT-HAND ICE SHIELD. R EPAIRED IAW -8 MM 20-13-11, PAGE 3. 2 H 7 2 4T RT A13NM 1999031900847 19990319 00847 NM 1999 3 19 QXEA9900451 1 19990305 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - THERE IS A DENT APPROXIMATELY 3 INCH DIAMETER IN THE FUSELAGE SKIN, UNDER THE RIGHT-HAND ICE SHIELD. REPAIRED IAW -8 MM 20-16-11. 2 H 7 2 4T RT A13NM 1999031900848 19990319 00848 NM 1999 3 19 QXEA9900452 1 19990221 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 222.7 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME CLIP CRACKED AT STRINGER 31R AND STATION 222.7. REPAIRED IAW SRM 53-20-21, PAGE 1. 2 H 7 2 4T RT A13NM 1999031900849 19990319 00849 NM 1999 3 19 QXEA9900453 1 19990222 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 510 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME CLIP CORRODED AT STRINGER 31R AND STATION 510. REPAIRED IAW SRM 53-00-16. 2 H 7 2 4T RT A13NM 1999031900850 19990319 00850 NM 1999 3 19 QXEA9900454 1 19990221 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME CLIP CORRODED AT STRINGER 31R AND STATION 545. REPAIRED IAW SRM 53-00-16, PARAGRAPH 1, TABLE 1. 2 H 7 2 4T RT A13NM 1999031900851 19990319 00851 NM 1999 3 19 QXEA9900455 1 19990221 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - FRAME CLIP CORRODED AT STRINGER 32R AND STATION 545. REPAIRED IAW SRM 53-00-16, PARAGRAPH 1, TABLE 1. 2 H 7 2 4T RT A13NM 1999031900852 19990319 00852 NM 1999 3 19 QXEA9900456 1 19990302 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - CORROSION ON BELLY SKIN AROUND TCAS ANTENNA DOUBLER RIVETS. REPAIRED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999031900853 19990319 00853 NM 1999 3 19 QXEA9900457 1 19990216 A 5320 WALL DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 823PH 110 PDX - LEFT-HAND WALL OF NOSE GEAR WHEEL WELL IS CRACKED THROUGH A PREVIOUS REPAIR AT STATION 57. REPAIRED IAW RD 8-53-6 75. 2 H 7 2 4T RT A13NM 1999031900854 19990319 00854 NE 1999 3 19 ABXA9900188 2 19990310 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 FAILED A ABXA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 GL 23 812AX 46126 669263 ON APPROACH TO ILN, NR 1 ENGINE OIL PRESSURE DROPPED TO 28 PSI. SECURED NR 1 ENGINE. FOUND OIL FILTER CONTAMINATED WIT H METAL. REPLACED NR 1 ENGINE. 2 L 7 4 4F 4 F 4A25 1E8 1999031900855 19990319 00855 WP 1999 3 19 ABXA9900189 1 19990312 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 844AX 45848 DURING PREFLIGHT, FOUND CAPTAIN'S AND FIRST OFFICER'S EMERGENCY LIGHTS VERY DIM, NOT USEABLE. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999031900856 19990319 00856 NM 1999 3 19 ABXA9900190 1 19990311 A 3231 LINKAGE BOEING 767 767281 1385109 NM NLG DOOR LACK OF LUBE A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 768AX 22786 WHEN LANDING GEAR WAS RETRACTED, THE 'DOORS' LIGHT REMAINED ILLUMINATED. RETURNED TO DFW. FOUND LEFT NOSE GEAR DOOR DO WN AND NOT LATCHED. INSPECTED DOOR AND LINKAGE. FOUND DOOR RELEASE STICKING. LUBRICATED LATCH AND RESECURED DOOR, OPS CHECKED GOOD. 2 L 7 2 4F TR A1NM 1999031900857 19990319 00857 WP 1999 3 19 ABXA9900191 1 19990308 A 5250 AR25291GR41 LATCH DOUG DC9 DC932 3022066 WP COCKPIT BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 COCKPIT DOOR WOULD NOT OPEN. REPAIRED COCKPIT DOOR LATCH. 2 L 7 2 4F A6WE 1999031900858 19990319 00858 WP 1999 3 19 MWEA99097 1 19990311 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP CABIN DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 301ME 47190 THE FORWARD ENTRANCE DOOR ESCAPE SLIDE COVER POPPED OFF. MTC REINSTALLED ESCAPE SLIDE GIRT BAR. 2 L 7 2 4F A6WE 1999031900859 19990319 00859 WP 1999 3 19 DHL99806001 1 19990312 A 3510 54251 REGULATOR DOUG DC8 DC873F 302199F WP OXYGEN BOTTLE FAILED A DHLA A B UNSCHED LANDING EMER. DESCENT O OTHER CR CRUISE 1 SO 01 806DH 46002 ALL OXYGEN QUANTITY IND WENT TO ZERO IN FLIGHT. PRESSURE INDICATION AT S/O STATION READ ZERO, BOTTLE PRESSURE READ NORM AL. CHECKED BOTTLE VALVE OPEN. REPLACED OXYGEN BOTTLE REGULATOR, OPS CHECKED NORMAL PER MM 35-10-3. 2 L 7 4 4F RT 4A25 1999031900860 19990319 00860 NM 1999 3 19 SWAA990490 1 19990310 A 2560 6545225 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 PLASTIC SHROUD AROUND ESCAPE SLIDE ON FWD SERVICE DOOR WAS LOOSE AT THE BOTTOM AND SLIDE FELL OUT. REPACKED SLIDE PER S WA WORK CARD. 2 L 7 2 4F A16WE 1999031900861 19990319 00861 NM 1999 3 19 SWAA990491 1 19990310 A 5330 6545871 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED C1 CHECK, FOUND .375 INCH CRACK RADIATING OUT OF UPPER CORNER OF LOWER HINGE CUTOUT ON DOOR SKIN. REPA IRED CRACK PER SWA RA NR 1-252-0322. 2 L 7 2 4F A16WE 1999031900862 19990319 00862 NM 1999 3 19 SWAA990492 1 19990310 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 948 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED C1 CHECK, FOUND A 2.5 INCH CRACK ON RT FUSELAGE SKIN, BS 948, STR 25R. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999031900863 19990319 00863 NM 1999 3 19 SWAA990493 1 19990310 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 868 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON STRINGER 25L UPPER FLANGE, BS 868. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031900864 19990319 00864 NM 1999 3 19 SWAA990494 1 19990310 A 5320 6551261 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR FRAME CRACKED AT LOWER HINGE CUTOUT, FWD LOWER RADIUS. REPAIRED PER S WA RA NR 1-353-2035. 2 L 7 2 4F RT A16WE 1999031900865 19990319 00865 NM 1999 3 19 SWAA990495 1 19990310 A 5320 WEB BOEING 737 7373Q8 1384670 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND LT WHEEL WELL PRESSURE DECK CRACKED AT BEADED WEB, BS 663.75, LBL 30 TO LBL 33. REPA IRED PER DALFORT XEA NR X2-53-238. 2 L 7 2 4F RT A16WE 1999031900866 19990319 00866 NM 1999 3 19 SWAA990496 1 19990311 A 2560 65C19696 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR FELL OUT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 SERVICE DOOR SLIDE FELL OUT OF CONTAINER. RESTOWED SLIDE CONTAINER PER MM. 2 L 7 2 4F RT A16WE 1999031900867 19990319 00867 NM 1999 3 19 SWAA990497 1 19990311 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 510 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH CRACK AT FUSELAGE SKIN BS 510, STR 18R. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999031900868 19990319 00868 NM 1999 3 19 SWAA990498 1 19990311 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 3-5 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT ROWS 3 TO 5. FOUND CANNON PLUG DISCONNECTED, RECONNECTED PER MM. 2 L 7 2 4F RT A16WE 1999031900869 19990319 00869 NM 1999 3 19 SWAA990499 1 19990311 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. FOUND DISCONNECTED CANNON PLUG. R ECONNECTED CANNON PLUG PER MM. 2 L 7 2 4F RT A16WE 1999031900870 19990319 00870 NM 1999 3 19 SWAA990500 1 19990311 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD CRACKED AT BS 178, RBL 10. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031900871 19990319 00871 NM 1999 3 19 SWAA990501 1 19990312 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 610WN 27696 THREE EMERGENCY EXIT FLOOR LIGHTS INOP. RECONNECTED WIRE SOCKET END AT FLOOR TRACK LIGHT NR 4, OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999031900872 19990319 00872 NM 1999 3 19 SWAA990502 1 19990312 A 5312 6516300 BULKHEAD WEB BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND 2 VERTICAL CRACKS, BS 178 BULKHEAD WEB WL 188 BL 0. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031900873 19990319 00873 NM 1999 3 19 SWAA990503 1 19990313 A 3260 189915 SENSOR BOEING 737 7373H4 1384600 NM LT MLG OUT OF ADJUST A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 320SW 23341 AIR TURNBACK DUE TO LT MAIN LANDING GEAR WARNING LIGHT REMAINED ON AFTER RETRACTION. ADJUSTED LT MAIN GEAR UP PROX SENS OR PER MM. 2 L 7 2 4F RT A16WE 1999031900874 19990319 00874 NM 1999 3 19 SWAA990504 1 19990313 A 2560 D31591 SLIDE BOEING 737 7373A4 1384585 NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 ON ARRIVAL, FWD ENTRY DOOR ESCAPE SLIDE FELL OUT UPON OPENING THE DOOR. STOWED FWD ENTRY DOOR SLIDE ASSY AND SECURED PA CK COVER PER MM. 2 L 7 2 4F RT A16WE 1999031900875 19990319 00875 NM 1999 3 19 SWAA990505 1 19990312 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AROUND SCREW HOLE, BS 727 RBL 8. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031900876 19990319 00876 NM 1999 3 19 SWAA990506 1 19990312 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND CRACK ON FLOORBEAM AROUND NET TIE DOWN HOLE, BS 787 RBL 14. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031900877 19990319 00877 NM 1999 3 19 SWAA990507 1 19990313 A 5312 6516300 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND 4 CRACKS AT BS 178 BULKHEAD WEB BETWEEN LBL 9-RBL 7. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031900878 19990319 00878 NM 1999 3 19 SWAA990508 1 19990313 A 5312 6516300 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND 5 CRACKS AT BS 178 BULKHEAD WEB BETWEEN LBL 32 AND RBL 5. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999031900879 19990319 00879 NM 1999 3 19 SWAA990509 1 19990313 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 664 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION A CRACK IN BEADED WEB AT BS 664 LBL 32. REPAIRED PER SW A RA NR 1-353-2033. 2 L 7 2 4F RT A16WE 1999031900880 19990319 00880 NM 1999 3 19 SWAA990510 1 19990313 A 5315 BAC15142320 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER T CHORD CRACKED AT BS 663 BL 0. REPAIRED PER SWA RA NR 1-357-0648. 2 L 7 2 4F RT A16WE 1999031900881 19990319 00881 NM 1999 3 19 SWAA990511 1 19990314 A 5210 6552873 SKIN BOEING 737 7373H4 1384600 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED AT LOWER CORNER (VERIFIED WITH EDDY CURRENT INSPECTION). REPAIRED SKIN CUT OUT PER SWA RA NR 1-352-0323. 2 L 7 2 4F RT A16WE 1999031900882 19990319 00882 NM 1999 3 19 SWAA990512 1 19990314 A 5230 FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FWD, LOWER FRAME CRACKED BELOW UPLATCH. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999031900883 19990319 00883 NM 1999 3 19 SWAA990513 1 19990314 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 326 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND A 1.5 INCH VERTICAL CRACK ON EXTERNAL FUSELAGE SKIN, BS 312 STR 19R. REPAIRED PER SR M. 2 L 7 2 4F RT A16WE 1999031900884 19990319 00884 NM 1999 3 19 SWAA990514 1 19990314 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 780-787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND 2 CRACKS ON EXTERNAL FUSELAGE SKIN BS 787 STR 19L AND ON BS 780 STR 18L. REPAIRED CR ACKS PER SRM. 2 L 7 2 4F RT A16WE 1999031900885 19990319 00885 NM 1999 3 19 SWAA990515 1 19990314 A 2560 D31591 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 EMERGENCY ESCAPE SLIDE CAME OUT OF COVER ON FWD ENTRY DOOR (DID NOT DEPLOY, JUST CAME OUT OF BRACKET). REINSTALLED SLID E ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031900886 19990319 00886 NM 1999 3 19 SWAA990517 1 19990314 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EXIT LIGHT INOP ABOVE AFT SERVICE DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999031900887 19990319 00887 NM 1999 3 19 SWAA990482 1 19990310 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOP. SPLICED WIRE TO LAMP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999031900888 19990319 00888 NM 1999 3 19 SWAA990483 1 19990309 A 7331 WL203EED11 INDICATOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 FUEL FLOW ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 NR 1 ENGINE FUEL FLOW INDICATOR ERRATIC AND UNRELIABLE, READS ZERO AT TIMES. ALL OTHER ENG INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 FLOW INDICATOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031900889 19990319 00889 NM 1999 3 19 SWAA990484 1 19990309 A 2130 106223111 SELECTOR BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA K NONE O OTHER DE DESCENT 1 SW 07 397SW 27691 DURING DESCENT, PASSING 29,000 FEET CABIN RATE WENT TO 2000 FPM DESCENT UNTIL PASSING 24000 FEET AND THEN RETURNED TO NO RMAL. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL PER MM. 2 L 7 2 4F RT A16WE 1999031900890 19990319 00890 NE 1999 3 19 SWAA990485 2 19990309 A 7230 3920028 BLADES BOEING 737 7373L9 1384470 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FOD A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 720799 DURING POST FLIGHT, FOUND DAMAGE ON NR 1 ENGINE FAN BLADES AND INLET LINING. REMOVED AND REPLACED FAN BLADE KIT PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999031900891 19990319 00891 NM 1999 3 19 SWAA990486 1 19990309 A 5311 6546569 FRAME BOEING 737 7372T4 1384492 NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 1138, STR 5-12 LEFT. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999031900892 19990319 00892 NM 1999 3 19 SWAA990487 1 19990309 A 5320 148A3380 STRAP BOEING 737 7372T4 1384492 NM BS 1088-1154 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER STRAP BETWEEN BS 1088 TO 1154, STR 12L. REPLACED STRINGER STRAP PER SR M. 2 L 7 2 4F A16WE 1999031900893 19990319 00893 NM 1999 3 19 SWAA990488 1 19990309 A 3350 101073 LIGHT BOEING 737 7373Y0 1384671 NM R2 DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED BC1 CHECK, FOUND FWD EMERGENCY LIGHT INOP AT R2 DOOR. REMOVED AND REPLACED EGRESS LIGHTING BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999031900894 19990319 00894 NM 1999 3 19 SWAA990489 1 19990310 A 5210 907809 SEAL BOEING 737 7373H4 1384600 NM PAX DOOR LEAKING A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 326SW 23690 AIR TURNBACK DUE TO FWD ENTRY DOOR HAVING A VERY LOUD PRESSURIZATION LEAK. ADJUSTED LOWER HINGE COVER SEAL PER MM. 2 L 7 2 4F RT A16WE 1999031900895 19990319 00895 NM 1999 3 19 SWAA990476 1 19990308 A 2131 71211997101AA CONTROLLER BOEING 737 7373H4 1384600 NM E & E BAY MALFUNCTIONED A SWAA K NONE O OTHER DE DESCENT 1 SW 07 397SW 27691 DURING DESCENT FROM 29,000 FT, AT 23,000 THE CABIN RATE WENT FROM 500 FPM TO 2000 FPM. AT 20,000 FEET CABIN RATE WENT 5 00 FPM CLIMB, THEN SETTLED BACK TO 500 FPM DESCENT. REMOVED AND REPLACED NR 2 PRESSURE CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 1999031900896 19990319 00896 NM 1999 3 19 SWAA990477 1 19990308 A 3233 6544624 FITTING BOEING 737 7372T4 1384492 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CORROSION IN ALL FOUR OF THE RT MAIN LANDING GEAR RETRACT ACTUATOR ATTACH FITTING BEAM H OLES. REMOVED AND REPLACED MLG ACTUATOR ATTACH FITTING PER MM AND EO-99-0188. 2 L 7 2 4F A16WE 1999031900897 19990319 00897 NM 1999 3 19 SWAA990478 1 19990308 A 5240 6551261 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, FWD LOWER STUB FRAME CRACKED AT FASTENER HOLE. REMOVED AND REPLACE D STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999031900898 19990319 00898 NM 1999 3 19 SWAA990479 1 19990308 A 3610 1947924 PRECOOLER BOEING 737 7373L9 1384470 NM NR 1 ENGINE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SPECIAL VISIT, FOUND NR 1 ENGINE PRECOOLER CRACKED. REMOVED AND REPLACED PRECOOLER PER MM. 2 L 7 2 4F RT A16WE 1999031900899 19990319 00899 NM 1999 3 19 SWAA990480 1 19990308 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 LIGHTS INOP ON AIRCRAFT FLOOR EMERGENCY EXIT. REPAIRED DAMAGED WIRES PER MM. 2 L 7 2 4F RT A16WE 1999031900900 19990319 00900 NM 1999 3 19 SWAA990481 1 19990309 A 3350 1000679 LIGHT BOEING 737 7372T4 1384492 NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999031900901 19990319 00901 NM 1999 3 19 SWAA990516 1 19990312 A 3397 WIRE BOEING 737 7375H4 138449D NM LT EMER EXIT LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 523SW 26565 WIRE LOOSE FROM EMERGENCY EXIT LIGHT AT LT OVERWING EXIT. RESECURED WIRE AND OPS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 1999031900902 19990319 00902 WP 1999 3 19 AT9900202 1 19990207 A 5347 TRACK DOUG DC9 DC932 3022066 WP BS 389-465 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK CORRODED AT BS 389 TO 465. FABRICATED, DRILL ED, DEBURRED, AND INSTALLED NEW SEAT TRACK IAW DC9 SRM 53-05 FIG 4C, 51-10-3 AND 51-10-4. 2 L 7 2 4F A6WE 1999031900903 19990319 00903 WP 1999 3 19 AT9900203 1 19990207 A 5347 TRACK DOUG DC9 DC932 3022066 WP BS 427-503 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK AT BS 427 TO 503 CORRODED. REMOVED CORROSION , FABRICATED, DRILLED, DEBURRED, AND INSTALLED NEW SEAT TRACK IAW DC9 SRM 53-05 FIG 4C, 51-10-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999031900904 19990319 00904 WP 1999 3 19 AT9900204 1 19990207 A 5347 TRACK DOUG DC9 DC932 3022066 WP BS 351-370 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO DOOR TRACK AT BS 351 TO 370 LEFT HAND SIDE CORRODED. REM OVED CORROSION, LOCATED AND DRILLED NEW TRACK IAW DC9 SRM 53-10-3, 51-10-3, AND 53-20-0. 2 L 7 2 4F A6WE 1999031900905 19990319 00905 WP 1999 3 19 AT9900205 1 19990207 A 5347 TRACK DOUG DC9 DC932 3022066 WP BS 318-370 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK AT BS 318 TO 370 RIGHT SIDE CORRODED. FABRIC ATED NEW SEAT TRACK, DRILLED, DEBURRED, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 53-10-3, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999031900906 19990319 00906 WP 1999 3 19 AT9900206 1 19990311 A 5720 FAIRING DOUG DC9 DC932 3022066 WP WS 91 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LEFT WING UPPER TOP SIDE BEAVER TAIL CORRODED. REMOVED CORROSION, CUT OUT AREA AND INSTALLED SEALANT REPAIR IAW DC9 SRM 57-03 FIG 27. 2 L 7 2 4F A6WE 1999031900907 19990319 00907 WP 1999 3 19 AT9900207 1 19990313 A 5320 BEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT CARGO PIT LOWER BEAM AT BS 980 RBL 36 CORRODED. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC9 SRM 53-05-0, 51-30-5, AND 53-01-0. 2 L 7 2 4F A6WE 1999031900908 19990319 00908 WP 1999 3 19 AT9900208 1 19990226 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 210-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED AND PART OF UPPER FLANGE HAS BEEN PREVIOUSLY REMOVED AT BS 210 TO 237 LBL 16. REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT, ALODINED, PRIMED, AND INSTAL LED IAW DC9 SRM 53-11-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999031900909 19990319 00909 WP 1999 3 19 AT9900209 1 19990301 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOORBEAM UPPER CAP CORRODED AROUND FASTENER HOLES AT BS 980 RBL 38 TO 42. REMOVED, FIT, TRIMMED, DRILLED, AND INSTALLED UPPER CAP REPAIR ANGLE IAW DC9 SRM 51-10-3, 53-01 FIG 1, 53-05 FIG 20 A, 51-10-4, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999031900910 19990319 00910 WP 1999 3 19 AT9900210 1 19990308 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 130 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION AROUND FASTENER HEADS ON ATTACH ANGLE AND WEB (TOP SIDE) AT BS 13 0 LBL 54 ON THE E/E BAY CEILING. REMOVED CORROSION AROUND FASTENER HEADS, FABRICATED REPAIR DOUBLER, LOCATED AND DRILLE D, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-3, 51-10-4, AND 53-01 FIG 2. 2 L 7 2 4F A6WE 1999031900911 19990319 00911 WP 1999 3 19 AT9900211 1 19990313 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE CABIN INTERIOR RIGHT AFT LAVATORY FRAME TO FLOOR BEAM ATTACHMENT EXFOLI ATED AT BS 996. FABRICATED WEB AND DOUBLER REPAIRS, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 53-05 FIG 108, 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND 53-11-3 FIG 11. 2 L 7 2 4F A6WE 1999031900912 19990319 00912 NE 1999 3 19 MALA976391 2 19990312 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE NR 2 SMOKING A MALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 31XJ 031 AFTER SHUT DOWN, NOTICED SMOKE COMING OFF INBOARD SIDE OF NR 2 ENGINE. MAINTENANCE RAN AIRCRAFT FOR SEVERAL MINUTES, NO SMOKE NOTED AT ANYTIME. INSPECTED ENGINE AFTER SHUTDOWN, NO LEAKS NOTED. SUSPECT RESIDUAL CLEANING FROM PREVIOUS PGB OIL LEAK CLEANUP AND SEAL REPLACEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999031900913 19990319 00913 NE 1999 3 19 MALA976392 2 19990314 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT75A2 30030 NE RIGHT POWER LOSS A MALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 15 402XJ 340B402 IN FLIGHT RIGHT ENGINE MOMENTARY POWER INTERRUPTION. ENGINE RECOVERED NORMALLY IN ICING CONDITIONS. NO POWER LEVER MOV EMENT OR CTOT. MAINTENANCE TROUBLE SHOT ROLLBACK IAW GEMM TABLE 103, F16, 101B, CHAP 72-00-00. DDT SHIFT WAS LESS THAN 25 DEGREES, NO FURTHER ACTION REQUIRED. ALL OTHER CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999031900914 19990319 00914 EU 1999 3 19 MALA976393 1 19990312 A 3610 5056T88P01 VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 99XJ 099 LEFT ENGINE ANTI-ICE AIR VALVE LIGHT ILUMINATED SHORTLY AFTER TURNING ENGINE ANTI-ICE SWITCH ON. QRH WAS COMPLETED WITH NO CHANGE. MAINTENANCE REPLACED LEFT BLEED AIR AND SHUTOFF VALVE AND LEFT AIR VALVE PN 6058T80P03. GROUND RAN AIRCRAF T FOR 20 MINUTES, ALL WORK DONE IAW GE MM. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999031900915 19990319 00915 EU 1999 3 19 MALA976394 1 19990314 A 2840 HTE690046 SWITCH BAC 146 AVRO146RJ85A 1500097 EU FUEL PRESSURE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 501XJ E2208 EN ROUTE FUEL 2 LOW PRESS ILLUMINATED WITH NO OTHER LIGHTS. MAINTENANCE REPLACED FUEL LOW PRESSURE SWITCH IAW AVRO MM. RAN FOR SEVERAL MINUTES, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1999031900916 19990319 00916 NM 1999 3 19 PCAA9900001 1 19990316 A 5210 MS24586C140 SPRING DHAV DHC8 DHC8102 2809003 NM PAX DOOR DETACHED A PCAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 13 845EX 344 PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE INSPECTED AND FOUND THE FLIP UP FLOOR BOARD SPRING DETACHED. REATTACHED SP RING, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999031900917 19990319 00917 NM 1999 3 19 AWXA9900071 1 19990307 A 3350 321452 POWER SUPPLY BOEING 737 737277 1384570 NM LT EMER EXIT INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, EMERGENCY EXIT LIGHT. EMERGENCY EXIT LIGHTS OUT AT LT OVERWING EXIT AND L-2, R-2 DOORS. REMOVED AND RE PLACED AFT POWER SUPPLY, L-2 AND R-2 CK GOOD. REMOVED AND REPLACED LIGHT ASSY AT THE LEFT J OVERWING EXIT. 2 L 7 2 4F RT A16WE 1999031900918 19990319 00918 NM 1999 3 19 AWXA9900072 1 19990301 A 5320 829186935352 CLIP BOEING 737 737277 1384570 NM FUSELAGE BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, STRINGER TIE CLIPS. STRINGER TIE CLIPS BROKEN, CRACKED, OR DAMAGED AT THE FOLLOWING LOCATIONS, STA 344 STR 6R, STA 500 STR 27R, STA 500A STR 27R, STA 706 STR 4L, STA 727A STR 4R, STA 727B STR 3R, STA 727B STR 4R, STA 727B S TR 8R, STA 747 STR 5R, STA 767 STR 5R, STA 767 STR 6R. REMOVED AND REPLACED TIE CLIPS PER EO 53 -12-01. 2 L 7 2 4F RT A16WE 1999031900919 19990319 00919 NM 1999 3 19 AWXA9900073 1 19990301 A 5330 SKIN BOEING 737 737277 1384570 NM BS 185 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, DENT REPAIR STA 185R EXISTING REPAIR DENTED. REMOVED EXISTING REPAIR AT STA 185. CUT OUT DAMAGE PER SR M 53-30-3 FIG 2. ALODINED AND PRIMED PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999031900920 19990319 00920 NM 1999 3 19 AWXA9900074 1 19990301 A 5315 BAC1505100617 FLOORBEAM BOEING 737 737277 1384570 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE FOUND CORRODED FLOORBEAM,STA 294.5 LBL 36 CORROSION. REMOVED DAMAGED AREA PER SRM 53-10-9 FIG 1. FABRIC ATED T CAP FROM BAC1505-100617 R642686 PER SRM 53-10-9 FIG 1 INSTALLED PER SRM 51-30-2. 2 L 7 2 4F RT A16WE 1999031900921 19990319 00921 NM 1999 3 19 AWXA9900075 1 19990301 A 5311 FRAME BOEING 737 737277 1384570 NM BS 1138 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, FOUND STA 1138 WL 262 RBL 26.5 FWD SIDE OF FRAME IS CRACKED IN RADIUS. REMOVED AND REPLACED CRACKED ANG LE IAW SRM 51-30-2, SRM 51-40-3 BAC 5602 AND SRM 51-10-2 SRM 55-10-6. MAT 7075-0 QQU250/3 HEAT TREATED TO T-6. 2 L 7 2 4F RT A16WE 1999031900922 19990319 00922 NM 1999 3 19 AWXA9900076 1 19990301 A 5313 BAC1498156 STRINGER BOEING 737 737277 1384570 NM BS 867-907 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, DAMAGED FLOORBEAM STRINGER 18L UNDER FLOORBEAMS 887 TO 907 HAS A HOLE WORN BY A LOOSE CONNECTOR. REMOVE D AND REPLACED STRINGER SECTION IAW 53-10-03 REPAIR WAS INSTALLED FROM FS 867-907 SPLICED IN AT STA 877. REPAIR PARTS M ADE FROM 7075-T6 .040 FOR CHANNEL, BAC 1498-156 7075-T6 .032 FOR STRINGER, 7075-T6 .040 FOR ANGLES. 2 L 7 2 4F RT A16WE 1999031900923 19990319 00923 NM 1999 3 19 AWXA9900077 1 19990301 A 5315 6545812213 FLOORBEAM BOEING 737 737277 1384570 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, FOUND CORRODED FLOORBEAM AT STA 328 RBL 20 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE DAMAGED POR TION OF FLOORBEAM CAP PER SRM 53-10-9, 51-10-2, 51-30-2. 2 L 7 2 4F RT A16WE 1999031900924 19990319 00924 NM 1999 3 19 AWXA9900078 1 19990301 A 5320 DOUBLER BOEING 737 737277 1384570 NM BS 1138 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, FOUND CRACKED DOUBLER BS 1138, WL 282, LBL 27.5, HAS A CRACKED INTERNAL DOUBLER. REMOVED AND REPLACED D OUBLER FABRICATED FROM 7075-T6 .063 AND QQA- 250/13 HEAT TREATED AND PRIMED, INSTALLED PER SRM 53-30-3 FIG 37. 2 L 7 2 4F RT A16WE 1999031900925 19990319 00925 NM 1999 3 19 AWXA9900079 1 19990301 A 5313 BAC14987075T6 STRINGER BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, CRACKED STRINGER 16L AT STA 520 HAS 3 CRACKS AROUND FASTENERS. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 51-30-0. FABRICATED AND INSTALLED STRINGER BAC 1498-1557075-T6 IAW SRM 51-10-2 FIG 9 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 1999031900926 19990319 00926 NM 1999 3 19 AWXA9900080 1 19990301 A 5313 BAC1498595270 STRINGER BOEING 737 737277 1384570 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, STRINGER CRACK STA 500B HAS 2 CRACKS AROUND FASTENERS. CUT OUT DAMAGED SECTION PER SRM 53-10-3 FIG 1. F ABRICATED AND INSTALLED NEW STRINGER, U-CHANNEL, AND J ANGLES PER SRM 53-10-3 FIG 1 AND SRM 51-30-0. ALODINED AND PRIME D PER SRM 51-10-2. STRINGER BAC1498- 595270 J-ANGLES 7075-T6 .040, U-CHANNEL 7075-T6 .040 2 L 7 2 4F RT A16WE 1999031900927 19990319 00927 NM 1999 3 19 AWXA9900081 1 19990301 A 5313 BAC14981557075 STRINGER BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, STRINGER CRACK CABIN FWD OF RT STA 520 STR 16R AFT OF LIGHT ASSY. REMOVED STRINGER PER SRM 51-30-02, FA BRICATED REPLACEMENT STRINGER FROM BAC 1498-1557075-T6 PER SRM 53-10-2, FIG 9. INSTALLED PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 1999031900928 19990319 00928 NM 1999 3 19 AWXA9900082 1 19990301 A 5313 BAC14981387075 STRINGER BOEING 737 737277 1384570 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE,STRINGER CRACKED, CABIN AFT OF RT STA 500B STR 16R IS CRACKED FWD OF LIGHT ASSY. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR SECTION STRINGER BAC 1498-138/7075-T6, SPLICE ANGLES 7075-T6, AND U CHANNEL 7075-T6 .040 IAW SRM 53-10-3 FIG 1. ALODINED AND PRIMED PARTS PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53- 10-3 FIG 1 AND SRM 51-30-0. 2 L 7 2 4F RT A16WE 1999031900929 19990319 00929 NM 1999 3 19 AWXA9900083 1 19990301 A 5320 BAC15103357075 SUPPORT BOEING 737 737277 1384570 NM BS 303.9 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, FLOOR STRUCTURE CORRODED UNDER FWD LAV (LAV WALL HAT SECTION) LBL 13 STA 303.9 EXFOLIATION CORROSION. R EMOVED DAMAGED SECTION FLOOR SUPPORT IAW SRM 51-30-2 AND DRAWING 65C33533 FABRICATED FLOOR SUPPORT IAW BAC1510-3357075-T 6 QQA 200/11. INSTALLED IAW DWG 65C33533 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1999031900930 19990319 00930 NM 1999 3 19 AWXA9900084 1 19990301 A 5330 SKIN BOEING 737 737277 1384570 NM BS 780 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 IN MAINTENANCE, FOUND SKIN CRACK, KEELBEAM SKIN CRACKED APPROX STA 780 RT BETWEEN TWO PREVIOIUS REPAIRS. REMOVED OLD SK IN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 53-10-2 FIG 4, SRM 51-40-6 AND SRM 51-30-04 AND SRM 51-30 -2, STA 700 KEELBEAM. 2 L 7 2 4F RT A16WE 1999031900931 19990319 00931 NM 1999 3 19 CALA9900252 1 19990315 A 5320 CHORD BOEING 757 757224 1384958 NM BS 1147 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND A 1 INCH CRACK IN OUTER CHORDS OF BOTH LEFT AND RIGHT MLG WHEEL WELL STRUCTURE AT STA 1147. THE CHORDS WERE REMOVED AND NEW CHORDS WERE INSTALLED IAW BOEING DRAWING 149N7222. 2 L 7 2 4F RT A2NM 1999031900932 19990319 00932 NM 1999 3 19 CALA9900253 1 19990315 A 5313 STRINGER BOEING 757 757224 1384958 NM BS 1400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND A 6 INCH CRACK IN FLOOR SUPPORT STRINGER AT STA 1400 ABOVE STRINGER 29R. THE CRACKED SECTION OF STRING ER WAS REPLACED IAW SRM 53-60-53 AND ECRA 5321-01041. 2 L 7 2 4F RT A2NM 1999031900933 19990319 00933 NM 1999 3 19 CALA9900254 1 19990315 A 5313 STRINGER BOEING 757 757224 1384958 NM BS 1325 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND A 4 INCH CRACK IN AFT HOLD FLOOR STRINGER AT STA 1325, RBL 11.5. A REPAIR WAS INSTALLED IAW ECRA 5321- 01040. 2 L 7 2 4F RT A2NM 1999031900934 19990319 00934 NM 1999 3 19 CALA9900255 1 19990316 A 5753 PANEL BOEING 757 757224 1384958 NM RT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND RT WING O/B FLAP UPPER SURFACE INBOARD PANEL GOUGED BY SPOILER. THE PANEL WAS REPAIRED IAW ECRA 5753-0 1061 AND REFITTED IAW MM 57-51-00. 2 L 7 2 4F RT A2NM 1999031900935 19990319 00935 NM 1999 3 19 CALA9900256 1 19990316 A 5330 SKIN BOEING 757 757224 1384958 NM BS 620 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT BS 620, STRINGER 17L. A REPAIR WAS INSTALLED IAW ECRA 5331-01043. 2 L 7 2 4F RT A2NM 1999031900936 19990319 00936 WP 1999 3 19 CALA9900257 1 19990316 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 47798 INSPECTION FOUND A 1 INCH CRACK AT LOWER FORWARD CORNER OF LEFT FORWARD AIRSTAIR DOOR CUTOUT AT STA 160, STRINGER 20-21L . THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 57A. 2 L 7 2 4F A6WE 1999031900937 19990319 00937 WP 1999 3 19 9900909985 1 19990303 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 148 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 985US 47479 DURING PERIODIC CHECK, FOUND WEB CRACKED AT FS 148 ABOVE LONGERON 27L AT FORWARD E/E COMPARTMENT. INSTALLED REPAIR PER EA 99-163382. 2 L 7 2 4F A6WE 1999031900938 19990319 00938 WP 1999 3 19 9900919963 1 19990305 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING PERIODIC CHECK, FOUND CRACK IN FRAME AT LONGERON 12R, FS 69.5. INSTALLED REPAIR PER EA 99-162-56. 2 L 7 2 4F A6WE 1999031900939 19990319 00939 WP 1999 3 19 9900929963 1 19990305 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 69 & 76 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING PERIODIC CHECK, FOUND CRACKS AT FS 69 BETWEEN LONGERONS 15R AND 20R AND AT FS 76 BETWEEN LONGERONS 15R AND 21R. I NSTALLED REPAIRS PER EA 99-165600. 2 L 7 2 4F A6WE 1999031900940 19990319 00940 WP 1999 3 19 9900939610 1 19990308 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING PERIODIC CHECK, FOUND FRAME CRACKED IN RADIUS; BOTTOM OF CANTED FRAME AT FS 1143. INSTALLED REPAIR PER EA 96-165 739. 2 L 7 2 4F A6WE 1999031900941 19990319 00941 WP 1999 3 19 9900949610 1 19990308 A 5311 FRAME DOUG DC9 DC932 3022066 WP AFT ACCESS COMPT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING PERIODIC CHECK, FOUND FRAME UNDER AIRSTAIR TORQUE TUBE CRACKED IN AFT ACCESSORY COMPARTMENT. BRACKET TO FRAME WA S ALSO BROKEN. INSTALLED REPAIR PER EA 96-165737. 2 L 7 2 4F A6WE 1999031900942 19990319 00942 EA 1999 3 19 COMA9960109 1 19990314 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 776CA 113 7293 FLAPS FAILED WHEN SELECTED UP. REPLACED 3 DEFECTIVE FLAP ACTUATORS AND 1 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 1999031900943 19990319 00943 EA 1999 3 19 COMA9960110 1 19990312 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 946CA 2291 7072 FLAPS FAILED AFTER TAKEOFF. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999031900944 19990319 00944 EA 1999 3 19 COMA9960111 1 19990313 A 2750 7805013 LEVER CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 946CA 3142 7072 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR HANDLE. 2 L 7 2 4F RT A21EA 1999031900945 19990319 00945 EA 1999 3 19 COMA9960112 1 19990312 A 2120 AIR DIST CNDAIR CL600 CL6002B19 EA GALLEY ODOR A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 991CA 7216 SMOKE SMELL FROM GALLEY AREA. COULD NOT DUPLICATE. INSPECTED GALLEY AREA AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 1999031900946 19990319 00946 EA 1999 3 19 COMA9960113 1 19990312 A 2750 860D10018 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 710CA 1946 7241 FLAPS FAILED AT 45 DEGREES. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999031900947 19990319 00947 EA 1999 3 19 COMA9960114 1 19990313 A 3340 601R560031 LIGHT CNDAIR CL600 CL6002B19 EA VERT STAB SHORTED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 735CA 7267 NAV LIGHT CIRCUIT BREAKER TRIPPED. REPLACED VERTICAL STAB NAV LIGHT ASSY. 2 L 7 2 4F RT A21EA 1999031900948 19990319 00948 EA 1999 3 19 COMA9960115 1 19990313 A 2760 601R910201 PCU CNDAIR CL600 CL6002B19 EA LT SPOILER OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 941CA 7050 CONFIG SPOILERS WARNING. ADJUSTED LEFT HAND SPOILERON PCU. 2 L 7 2 4F RT A21EA 1999031900949 19990319 00949 WP 1999 3 19 UPS99829012 1 19990220 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 CORROSION ON FLOORBOARD SUPPORT AT NUTPLATES FS180, 37 ABOVE L27R BLENDED BEYOND LIMITS IAW DC8 S RM 53-2-0, MATERIAL ID 7075-T6 X .050 AND 7075T6 X .032 PO NR 282694 AND PO NR 278914, DC8 SRM 51-2-0 AND DWG NR 377307 77, FAB DOUBLER, LOCATE DRILLED AND DEBURRED IAW DC8 SRM 51-2- 0. ALODINE AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1999031900950 19990319 00950 WP 1999 3 19 UPS99829013 1 19990220 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1166 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 C-3 DOOR, LOWER NR 1 T-BOLT FITTING CRACKED. REMOVED DOOR LATCH FITTING, DRILLED NEW FITTING, AND IN STALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999031900951 19990319 00951 WP 1999 3 19 UPS99829014 1 19990217 A 5321 FLOOR DOUG DC8 DC873F 302199F WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 AFT FLOOR PANEL F216A IS CRACKED. FABRICATED NEW PANEL IAW DAC DWG 5755032. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999031900952 19990319 00952 WP 1999 3 19 UPS99829015 1 19990217 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 FWD PIT FS240 LONG 30R HAS CORROSION UNDER LONG SHIM FROM PREVIOUS BLEND OUT AREA OF SKIN. REMOVED L ONG 30R AND END FITTING. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FABRICATED DOUBLER AND FILLER IAW D C8 SRM 53-2-0. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900953 19990319 00953 WP 1999 3 19 UPS99829016 1 19990221 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 20 CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2, FLT CABIN INTERCOSTAL CHAFED THROUGH AT STA 20 LBL 10 MAT ID, LOCATE, DRILL, DEBURRED, AND INSTALL I AW DC8 SRM 53-2-0, 51-1- 8, DWG 5641543. 2 L 7 4 4F RT 4A25 1999031900954 19990319 00954 WP 1999 3 19 UPS99829017 1 19990221 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 CABIN AFT STA 1700 CANTER FRAME CORRODED AND CORROSION BETWEEN VERTICAL ATTACH PLATE L-36. CUT OUT C ORRDED FRAME SECTION, VERTICAL ATTACH OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED NEW REPAIR ANGLE AND VERTICAL ATTACH PLATE AND SHIMS IAW REO 06339. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FRAME REPAIR AND VERTICAL PLATE IAW REO-06339 DC8 SRM 51-1-20D, 51-3-0, 51-1-8. 2 L 7 4 4F RT 4A25 1999031900955 19990319 00955 WP 1999 3 19 UPS99829018 1 19990223 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 BATHTUB FITTING AT FS 920 LEFT LONGERON 24 IS CRACKED AND CORRODED. DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-20D. FINAL INSTALLATION ON UPS N/R 875504. 2 L 7 4 4F RT 4A25 1999031900956 19990319 00956 WP 1999 3 19 UPS99829019 1 19990221 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 AFT PIT UPPER FRAME CAP AT FS 1000 EXFOLIATION CORROSION ON FRAME CAP AT L34R AND 33 OUT OF LIMITS, M AT ID AND FABRICATED DOUBLER REPAIR END SHIM IAW REO-06348. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER REPAIR AND SHIM IAW REO-06348. 2 L 7 4 4F RT 4A25 1999031900957 19990319 00957 WP 1999 3 19 UPS99829020 1 19990217 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1100-1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 AFT PIT INTERCOSTAL AT L33R FS 1100-1120 CORRODED BEYOND LIMIT. REMOVED INTERCOSTAL FROM STA 1100 TO 1120 AND L33R. FORMED AND HEAT TREATED INTERCOSTAL IAW DAC DWG 9754969. LOCATED AND DRILLED IAW DAC DWG 9754949. ALO DINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DAC DWG 975 4949 AND DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999031900958 19990319 00958 WP 1999 3 19 UPS99829021 1 19990221 A 5320 FLOOR DOUG DC8 DC873F 302199F WP BS 65 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 FLT CABIN FLOOR PRESSURE PANEL DOUBLER BULGED AND NUMEROUS RIVETS POP PED AT STA 65 LBL OUT OF LIMITS . FABRICATED REPAIR DOUBLER IAW DAC DWG SRO8530026. FABRICATED CHANNEL DOUBLER IAW DAC DWG 5612289. ALODINED AND PRIM ED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900959 19990319 00959 WP 1999 3 19 UPS99829022 1 19990221 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 FLT CABIN FLOOR PRESSURE PANEL DOUBLER BULGED AND NUMEROUS RIVETS POPPED AT STA 65 LBL 20 OUT OF LIMI TS. FABRICATED FINGER DOUBLER REPAIR IAW DAC DWG 5612298. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031900960 19990319 00960 WP 1999 3 19 UPS99829023 1 19990217 A 2760 BRACKET DOUG DC8 DC873F 302199F WP SPOILER CONTROLS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 LWW, FWD OF SPOILER LATERAL CONTROL MECHANISM BRACKET CORRODED. REMOVED SPOILER MINER MECHANISM AND REMOVED BRACKET AND VERIFIED MAT ID. BYE PEN TEST MIL STD 271F. NO CRACK NOTED. ALODINED AND PRIMED AND INSTALL. OPS CK TO BE DONE ON UPS T/C 875296. 2 L 7 4 4F RT 4A25 1999031900961 19990319 00961 WP 1999 3 19 UPS99829024 1 19990217 A 5210 SKIN DOUG DC8 DC873F 302199F WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:C2 L-1 DOOR LWR FWD CORNER, SKIN TORN AND CRACKED. REMOVED OLD DOUBLER REPAIR AND TRIM OUT DAMAGED AREA IAW DC8 SRM 52-2-0 MAT ID IAW DAC DWG 561-5403 AND DC8 SRM 52-3-1. HEAT TREATED IAW TPC 1003 REV A . FABRICATED CORNE R FILLER IAW DC8 SRM 52-3-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20A AND 51-1-21. 2 L 7 4 4F RT 4A25 1999031900962 19990319 00962 WP 1999 3 19 ABXA9900192 1 19990223 A 5400 5754700 DOUBLER DOUG DOUG DC8 DC863 302198A WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LEFT WING NR 2 PYLON INTERNAL DOUBLER CRACKED ABOVE PYLON OPENING AT FORWARD END. REPAIRED IAW DC8 SRM 57-2-1A AND 51-1 -20D. 2 L 7 4 4F 4A25 1999031900963 19990319 00963 WP 1999 3 19 ABXA9900193 1 19990203 A 5700 3755028503 CLIP DOUG DOUG DC8 DC863 302198A WP WS 22.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 FITTING CRACKED INSIDE NR 2 TANK AT STATION XRS 22.750 FORWARD OF AFT SPAR LOWER STRUCTURE. REPAIRED IAW DC8 SRM 51-1-2 0 AND 51-1-21. 2 L 7 4 4F 4A25 1999031900964 19990319 00964 WP 1999 3 19 ABXA9900194 1 19990223 A 5320 4645517502 SUPPORT DOUG DOUG DC8 DC863 302198A WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 STATION 680, RBL 48 FLOORBEAM SUPPORT ANGLE WAS CRACKED. REPLACED FLOORBEAM SUPPORT FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999031900965 19990319 00965 WP 1999 3 19 ABXA9900195 1 19990224 A 5720 576989114 STRAP DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 45141 RIGHT WING LEADING EDGE INNER BUTT SPLICE CRACKED AT LOWER AFT INBOARD END AT STATION XOLDI 6.225. REPAIRED IAW DC8 SRM 51-1-20 AND DWG 5769891. 2 L 7 4 4F 4A25 1999031900966 19990319 00966 WP 1999 3 19 ABXA9900196 1 19990224 A 5320 3646688505 SHEAR TIE DOUG DOUG DC8 DC863 302198A WP BS 660 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 FORWARD ACCESSORY COMPARTMENT SHEAR-TIE AT STATION 660 FRAME BETWEEN LONGERONS 21 AND 22 LEFT WAS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3646688. 2 L 7 4 4F 4A25 1999031900967 19990319 00967 WP 1999 3 19 MWEA99098 1 19990310 A 5210 9955759501 BEAM DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE FORWARD PASSENGER DOOR NUMBER 8 BEAM IS CRACKED AT FORWARD END UNDER HINGE. MAINTENANCE FABRICATED AND INSTALLED RE PAIR DOUBLER. 2 L 7 2 4F A6WE 1999031900968 19990319 00968 NM 1999 3 19 P5CA9900422 1 19990308 A 3010 69B425064 DUCT BOEING 747 747249F 1384849 NM RT WING DAMAGED A P5CA K NONE O OTHER CL CLIMB 1 WP 23 920FT 22237 RIGHT WING LEADING EDGE OVERHEAT LIGHT ON DURING CLIMB. USED ALTERNATE PROCEDURES PG 6-14-2. LIGHT OUT WITHIN 5 MIN. F OUND DUCT RUPTURE TO S DUCT BETWEEN L/E DUCT AND NR 4 RT KRUEGER FLAP PDU. REMOVED DAMAGED DUCT AND INSTALLED COVER PLA TES. NO LEAKS PER MM 27-81-00. 2 L 7 4 4F A20WE 1999031900969 19990319 00969 NM 1999 3 19 P5CA9900423 1 19990310 A 5230 SKIN BOEING 747 747249F 1384849 NM CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 DURING CLOSING LOWER FWD CARGO DOOR, AEROGROUND HIGH LOADER HIT DOOR AND CAUSED DAMAGE TO LOWER AFT CORNER. REWORKED LO WER CORNER OF FWD CARGO DOOR PER SRM 51-10-01. 2 L 7 4 4F A20WE 1999031900974 19990319 00974 1999 3 19 99ZZZX973 4 19990211 A 6122 B3124 CHAFT F628 PIPER PA23 PA23250 7102308 SO GOVERNOR BROKEN A S QGKA K NONE O OTHER IN INSP/MAINT 1 GL 03 40599 908 B808T 277405345 DURING CLIMB-OUT, LEFT PROPELLER WENT INTO UNWANTED FEATHER. AIRCRAFT MADE NORMAL SINGLE ENGINE LANDING. FOUND GOVERNO R CONTROL SHAFT BROKEN OFF WHERE THE NUT ATTACHES IT TO THE WHEEL. 1 L 7 2 3O 1A10 1999031900982 19990319 00982 SO 1999 3 19 99ZZZX981 2 19990122 A 8520 SA630826 BEARING CESSNA 402 402CESSNA 207590K CE CONT O520 TSIO520E 17040 SO CRANKSHAFT FAILED A IJZA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 05 412RW 1060 4020127 206079E PILOT REPORTED 20 MILES FROM DESTINATION, LOSS OF OIL PRESSURE. CONTINUED TO DESTINATION AND SHUT ENGINE DOWN WHEN PILO T HAD THE FIELD MADE. UPON INSPECTION, IT APPEARED THE NR 2 ROD BEARING FAILED CAUSING THE NR 2 ROD TO SEPARATE FROM TH E CRANKSHAFT CAUSING LOSS OF OIL PRESSURE, THEN THE NR 6 ROD FAILED AND SEPARATED FROM THE CRANKSHAFT. 1 L 7 2 3O 3 O A7CE E8CE 1999031901010 19990319 01010 NM 1999 3 19 HNAA9900036 1 19990314 A 5210 85210240055 STRUT DHAV DHC8 DHC8102 2809003 NM PAX DOOR BROKEN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 PASSENGER DOOR WOULD NOT OPEN. FORWARD UPPER DOOR SUPPORT STRUT BROKEN. REPLACED FORWARD SUPPORT STRUT (TUBE ASSY). 2 H 7 2 4T RT A13NM 1999031901011 19990319 01011 NM 1999 3 19 HNAA9900037 1 19990315 A 2520 SEAT DHAV DHC8 DHC8102 2809003 NM ROW 9 OUT OF POSITION A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 940HA 156 UNABLE TO REMOVE RIGHT HAND AFT FIRE BOTTLE FROM BULKHEAD. REPOSITIONED ROW 9 SEAT. 2 H 7 2 4T RT A13NM 1999031901012 19990319 01012 WP 1999 3 19 AT9900212 1 19990212 A 5312 BULKHEAD BRACKET DOUG DC9 DC932 3022066 WP BS 1180 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE CANTED BULKHEAD LEFT HAND LOWER ATTACH BRACKETS HAVE CORROSION RUNNING UNDER THEM AT LONGERON 11 ON THE BACK OF FRAME AT BS 1180. REMOVED BRACKETS AND CORROSION, CUT OUT AREA, FABRICATED FR AME REPAIR AND DOUBLER, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 53-01 FIG 1 AND 53-10-0 FIG 827. 2 L 7 2 4F A6WE 1999031901013 19990319 01013 WP 1999 3 19 AT9900213 1 19990223 A 3232 FITTING DOUG DC9 DC932 3022066 WP BS 699 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING IN WHEEL WELL WITH A DEEP CHAFE MARK FROM A HYDRAULIC LINE RUBBING AT BS 699. BLEND AREA SMOOTH, HFEC VERIFY NO CRACKS NOTED. RESTORED ORI GINAL FINISHED, ALODINE, PRIMED, PAINTED, AND INSTALLED IAW SRM 51-10-3, 53-01 FIG 1, AND RES NR 99450. 2 L 7 2 4F A6WE 1999031901014 19990319 01014 WP 1999 3 19 AT9900214 1 19990303 A 7830 THRUST REVERSER DOUG DC9 DC932 3022066 WP NR 1 ENGINE CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE NR 1 ENGINE THRUST REVERSER AT THE FORWARD MATING FLANGE TO THE ENG INE COWLING WITH A CHAFED AREA APPROXIMATELY FIVE INCHES LONG THRU THE BASE OF THE METAL. CUT OUT CHAFED AREA, FABRICAT ED, FORM FILLER AND INTERNAL DOUBLER, TREATED, PRIMED, AND INSTALLED CHAFED STRIP IAW DC9 SRM 51-30-2, 51-10-2, 51-10-4, AND RES NR 99560 AND RES NR 99562. 2 L 7 2 4F A6WE 1999031901015 19990319 01015 WP 1999 3 19 AT9900215 1 19990209 A 5210 ANGLE DOUG DC9 DC932 3022066 WP PAX DOOR CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE L-1 DOOR STRIKING BEHIND MOUNT U-CHANNEL ANGLE ON AFT DOOR JAMB AT UP PER STOP BOLT. BLENDED OUT DAMAGE AREA TO HAVE MINIMUM RADIUS, TREATED TRIMMED AREA, PRIMED AND DRESSED UP IAW DC9 53-0 1-0, 53-11-0, AND RES NR 99452. 2 L 7 2 4F A6WE 1999031901016 19990319 01016 WP 1999 3 19 AT9900216 1 19990315 A 3350 60030431 BATTERY CHARGER DOUG DC9 DC932 3022066 WP CABIN INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 832AT 47451 DURING 'B' CHECK, FOUND THE SERVICE ENTRANCE EMERGENCY LIGHTS, L-1 DOOR ENTRANCE AND COCKPIT EMERGENCY LIGHTS DIM AND BA TTERY PACK WILL NOT ACCEPT CHARGE. REMOVED AND REPLACED POWER SUPPLY (CHARGER) LOCATED ON THE FORWARD CABIN CEILING. S YSTEM OPS CHECKED GOOD IAW B737 MM 33-50-00. 2 L 7 2 4F A6WE 1999031901017 19990319 01017 NE 1999 3 19 MALA976395 2 19990315 A 7260 CHIP DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 402XJ 340B402 ON CLIMBOUT FROM DTW, THE RIGHT CHIP DETECT LIGHT CAME ON, COMPLIED WITH QRH. ALL ENGINE PARAMETERS WERE NORMAL. AIRCR AFT RETURNED TO DTW. MAINTENANCE FOUND ONE SLIVER HAIR LIKE PIECE ON CHIP DETECTOR. CLEANED CHIP DETECTOR AND SCAVANGE SCREENS. GROUND RAN AIRCRAFT FOR 15 MINUTES, RIGHT CHIP DETECTOR LIGHT DID NOT ILLUMINATE. ALL WORK DONE IAW CT7 MM F AULT ISOLATION 72-00-00 PAGE 198.17. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1999031901018 19990319 01018 EU 1999 3 19 MALA976396 1 19990316 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS COMPT DIRTY A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 590MA 340B181 AVIONIC SMOKE MASTER WARNING AND WARNING LIGHT (CWP) ILLUMINATED IN FLIGHT, NO INDICATION OF FIRE, SMOKE OR HEAT. AIRCR AFT RETURNED TO DTW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AVIONIC RACK SMOKE DETECTOR PER SF340A MM. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999031901019 19990319 01019 NM 1999 3 19 K3HA990023 1 19990313 A 3350 3071BPE BULB BOEING 727 727225 1384077 NM ROW 27 FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY PATH LIGHTING AT PASSENGER ROW 27 INOP. REMOVED AND REPLACED LAMP, OPS CHECK OK. REF MM 33-50-01. 2 L 7 3 4F A3WE 1999031901020 19990319 01020 NM 1999 3 19 K3HA990024 1 19990311 A 3350 3071BPEGPL LIGHT BOEING 727 727225 1384077 NM ROW 32DEF BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 ON POST FLIGHT, FOUND EMERGENCY PATH LIGHTING BROKEN ON 32DEF. REMOVED AND REPLACED EMERGENCY PATH LIGHTING SOCKET AND LAMP IAW 33-50-01. OPS CHECK OK. 2 L 7 3 4F A3WE 1999031901021 19990319 01021 NM 1999 3 19 RAAA99B2010 1 19990312 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 560-580 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND SEAT TRACK CORRODED AT LBL 45 FROM BS 560 TO 580. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-01, M54 NR 229. 2 L 7 3 4F A3WE 1999031901022 19990319 01022 NM 1999 3 19 RAAA99B2008 1 19990312 A 5330 SKIN BOEING 727 72722C 138400F NM BS 690 GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED CHECK PER CARD C53002, FOUND GROVE WORN IN FUS SKIN AT BS 690 AND STR 25R. INSTALLED REPAIR IAW SRM 5 3-30-3 FIG 1. M54 NR 36. 2 L 7 3 4F A3WE 1999031901023 19990319 01023 NM 1999 3 19 RAAA99B2009 1 19990312 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 1030-1096 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION PER CARD S354102, FOUND RT SEAT TRACK CORRODED IN THE UPPER SURFACE BS 1030 TO 1096. REMOVE D AND REPLACED SEAT TRACK IAW SRM 51-10-01, M54 NR 219. 2 L 7 3 4F A3WE 1999031901024 19990319 01024 NM 1999 3 19 9900956636 1 19990310 A 3350 CONNECTOR BOEING 747 747251B 1384892 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 636US 23547 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE IN ZONES A AND E. REPAIRED CONNECTOR AND REPLACED BATT ERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999031901025 19990319 01025 NM 1999 3 19 9900962767 1 19990310 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 727RW 21656 MAINTENANCE FOUND TWO THIRDS OF AIRCRAFT'S ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK O K. 2 L 7 3 4F A3WE 1999031901026 19990319 01026 NE 1999 3 19 9900979857 2 19990314 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RIGHT FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 GL 01 766NC 47739 688784 DURING CRUISE AT 33,000 FEET, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DUE TO CONTAINED FAILURE. 2 L 7 2 4F 4 F RT A6WE E2EA 1999031901027 19990319 01027 WP 1999 3 19 UPS99829027 1 19990222 A 5311 561214299 FRAME DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, STA 1700 FRAME AT STR 36 HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999031901028 19990319 01028 WP 1999 3 19 UPS99829028 1 19990307 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, STA 1700 FLOORBEAM IS CORRODED OUT OF LIMITS AT LBL 24. REPAIRED AREA IAW DHC SK 811-528. 2 L 7 4 4F RT 4A25 1999031901029 19990319 01029 WP 1999 3 19 UPS99829029 1 19990223 A 5313 575032229 LONGERON DOUG DC8 DC873F 302199F WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LONGERON 34L BTWEEN STA 1260 TO 1280 IS CRACKED. REPAIRED AREA IAW DHC SK 811-775. 2 L 7 4 4F RT 4A25 1999031901030 19990319 01030 WP 1999 3 19 UPS99829030 1 19990305 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, STA 1700 AT RBL 24, THE FLOORBEAM FLANGE HAS HEAVY CORROSION. REPAIRED AREA IAW DHC SK 811-080. 2 L 7 4 4F RT 4A25 1999031901031 19990319 01031 WP 1999 3 19 UPS99829031 1 19990222 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, LONGERON 31L AT STA 500 HAS HEAVY CORROSION. REPAIRED AREA IAW DHC SK 811-817. 2 L 7 4 4F RT 4A25 1999031901032 19990319 01032 WP 1999 3 19 UPS99829032 1 19990222 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP NR 2 FUEL TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, NR 2 MAIN TANK I/B AFT ACCESS PANEL INTERNAL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-2 FIG 3 6. 2 L 7 4 4F RT 4A25 1999031901033 19990319 01033 WP 1999 3 19 UPS99829033 1 19990215 A 5311 56402435 FRAME DOUG DC8 DC873F 302199F WP BS 1680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, STA 1680 AT STR 21L, THE FRAME HAS A 2.5 INCH CRACK. REMOVED, FABRICATED AND REPLACED FRAME IAW DWG 5640243 AND SRM 51 1-20D. 2 L 7 4 4F RT 4A25 1999031901034 19990319 01034 WP 1999 3 19 UPS99829034 1 19990223 A 5320 3755847502 FITTING DOUG DC8 DC873F 302199F WP BS 1228 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, STA 1228 AT STR 29R TO 33R, THE SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031901035 19990319 01035 WP 1999 3 19 UPS99829035 1 19990216 A 5320 3753568503 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE-C1, STA 1220 AT STR 32L, THE STR END FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITT ING IAW DWG 3753569 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999031901037 19990319 01037 NM 1999 3 19 99FDEA00103 1 19990316 A 3260 H1010154 SWITCH BOEING 727 72725 1384006 NM NLG INOPERATIVE A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 509FE 18280 ON APPROACH WITH GEAR AND FULL FLAPS, WARN HORN AND NOSEWHEEL DOWN LIGHT WENT OUT. REMOVED AND REPLACED NOSE GEAR POSIT ION SWITCH PER 727-100 MM 32-61-21 PG 406. COMPLETED ADJUSTMENT/TEST PER PG 501. OPS CK GOOD. 2 L 7 3 4F A3WE 1999031901038 19990319 01038 NM 1999 3 19 99FDEA00104 1 19990316 A 5610 5893543109 WINDOW BOEING 727 72725C 138400H NM COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 133FE 19851 PILOTS WINDOW CRACKED IN FLIGHT. INSTALL SERVICEABLE L-1 WINDOW, REFERENCE B727-100 MM 56-11-011-4. 2 L 7 3 4F A3WE 1999031901039 19990319 01039 NM 1999 3 19 99FDEA00105 1 19990317 A 3260 CONNECTOR BOEING 727 72721C 138400M NM NLG FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 143FE 19136 AFT T/O, NOSE GEAR FAILED TO RETRACT. CYCLED GEAR TWICE, STILL STAYED DOWN. RETURNED TO MEM, NORM GEAR EXTENSION. *S/ D* REMOVED AND REPLACED CANNON PLUG D-300, NOSE GEAR POS SWITCH. OPER CK NORMAL REF 727-100 WIR DIAG 32-64-01 AND 32-6 4-02, MM 32-61-000-0. 2 L 7 3 4F A3WE 1999031901040 19990319 01040 NM 1999 3 19 99FDEA00106 1 19990316 A 5320 65931157 SILL BOEING 727 72725C 138400H NM BS 500 - 580 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 WHILE WORKING NR 419, FOUND CORROSION ON MAIN CARGO DOOR LWR SILL CHORD AT BS 500-580, LBL 62.5, WL 208. REMOVED AND RE PLACED, FAB MAIN CARGO DOOR LWR SILL CHORD FROM BS 440-660, LBL 65, WL 208 IAW, DWG NR 65-40507 AND FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1999031901041 19990319 01041 WP 1999 3 19 ABXA9900198 1 19990227 A 5730 5611340 SKIN DOUG DOUG DC8 DC863 302198A WP WS 69 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LEFT WING UPPER SKIN CRACKED AT STATION XCW69 AND STRINGER 10. INSTALLED DOUBLER AND FILLET SUPPORT ANGLE IAW DC8 IAW D C8 SRM. 2 L 7 4 4F 4A25 1999031901042 19990319 01042 WP 1999 3 19 ABXA9900199 1 19990227 A 5320 5643454 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 35-55 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 HEAVY CORROSION FOUND AROUND AND UNDER FINGER DOUBLER, STATION 35 TO 55 AT LONGERON 31 LEFT. REPAIRED IAW DC8 SRM 51-1- 21 AND ABX REA D853-24944MR. 2 L 7 4 4F 4A25 1999031901043 19990319 01043 WP 1999 3 19 ABXA9900200 1 19990227 A 5753 4655126 FITTING DOUG DOUG DC8 DC863 302198A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT OUTBOARD FLAP, INBOARD END HAD CRACKED FITTING INSIDE FORWARD, INBOARD LIGHTENING HOLE. REPLACED FITTING IAW DC8 SRM 51-1-21 AND ABX REA D857-24945. 2 L 7 4 4F 4A25 1999031901044 19990319 01044 WP 1999 3 19 ABXA9900201 1 19990227 A 5313 575032225 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1260-1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LONGERON 36 CRACKED AT STATION 1260 TO 1280. REPAIRED IAW DC8 DC8 SRM 53-2-2 AND ABX REA D853-24938. 2 L 7 4 4F 4A25 1999031901045 19990319 01045 WP 1999 3 19 MWEA99099 1 19990315 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE FORWARD GALLEY ESCAPE SLIDE COVER FELL OFF. MTC REINSTALLED FORWARD GALLEY ESCAPE SLIDE COVER. 2 L 7 2 4F A6WE 1999031901046 19990319 01046 WP 1999 3 19 MWEA99100 1 19990316 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 THE AFT EMERGENCY STAIR AND EMERGENCY SLIDE LIGHTS DID NOT ILLUMINATE. MTC REPAIRED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1999031901047 19990319 01047 NM 1999 3 19 VNAA9903011 1 19990313 A 3260 OL3092 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FAILED A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 458PS 3068 THE LEFT HAND MAIN LANDING GEAR FAILED TO INDICATE A DOWN AND LOCKED CONDITION WHEN SELECTED. THE CREW DECLARED AN EMER GENCY, AND FOLLOWED THEIR QUICK REFERENCE HANDBOOK. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED SAFELY. MAINTENACE INSPECTED AND REPLACED THE POSITION INDICATOR LIGHT BULBS, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-14-00. OPER ATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999031901048 19990319 01048 NM 1999 3 19 VNAA9903012 1 19990315 A 2440 RECEPTICAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE DAMAGED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 328LS 3025 AFTER COMPLETION OF FLIGHT 4040 IAD-PIT, DAMAGE TO THE GROUND POWER RECEPTICAL WAS NOTED ON THE POST FLIGHT INSPECTION. PIT MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO CAK FOR REPAIR. THE FERRY FLIGHT TOOK PLACE WITHOUT INCIDENT. CAK MAINTENANCE REPAIRED THE DAMAGED GROUND POWER RECEPTICAL, IN ACCORDANCE WITH DORNIER RAS 328-24-6 78, AND RETURNED THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999031901049 19990319 01049 WP 1999 3 19 AALA990070 1 19990114 A 7333 8TJ85GCG2 FLOWMETER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 426AA AO132AC 49338 BOS - FLT 2221 - DURING CLIMB-OUT PVD, RIGHT FUEL FLOW INDICATOR BEGAN OPERATING ERRATICALLY WITH CLIMB POWER. FLIGHT A IR INTERRUPTED AND LANDED BOS WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT FUEL FLOW TRANSMITTER. RIGHT ENGINE WAS GRO UND RUN AT POWER WITH NO IRREGULARITIES OR LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999031901050 19990319 01050 NE 1999 3 19 ARWA990106 2 19990112 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 1 LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 19 802BN 45909 MIA - FLT 1628 - FL310, OIL QTY NR 1 ENGINE DROPPED TO .5 GALLON, OK OIL AND SUBSEQUENT ENGINE DAMAGE. PERFORMED PRECAU TIONARY ENGINE SHUTDOWN AS EPR ABNORMAL CHECKLIST. AFTER SHUTDOWN, N1 25 PERCENT, N2 40 PERCENT, OIL PRESS 21 PSI. REM OVED OIL SCREEN AND INSPECTED VISUALLY. NO DEFECTS NOTED. REINSTALLED OIL SCREEN. SERVICED ENGINE FULL WITH 2 QTS OIL . PERFORMED ENGINE RUN. ALL PARAMETERS NORMAL. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. NO FURTHER REPORTS. M OMENTARY QUANTITY INDICATION MALFUNCTION. (M) 2 L 7 4 4F 4 F 4A25 1E8 1999031901051 19990319 01051 NE 1999 3 19 HALA9900004 2 19990105 A 7321 7436025 FCU DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE MALFUNCTIONED A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 660HA 48122 HNL - FLT 102 - POWER SURGE RIGHT ENGINE AT MID RANGE EPR SETTINGS, CLIMB POWER. EPR VARIED PLUS/MINUS .05. N1 PLUS/MI NUS 2 PERCENT. NOT EVIDENT AT TAKEOFF POWER OR AT IDLE, A/C RETURNED TO HNL WHERE AN UNEVENTFUL LANDING WAS MADE. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 1999031901055 19990319 01055 EU 1999 3 19 RAIA990130 1 19990123 A 3243 ACM26810 MASTER CYLINDER BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 425AM 870 FLT 7328 - STL - CAPTAINS RIGHT BRAKE INOPERATIVE. MAINTENANCE SERVICED CAPTAINS RIGHT BRAKE MASTER CYLINDER. (M) 2 L 7 2 4T RT A56EU 1999031901056 19990319 01056 NM 1999 3 19 99ZZZM189 1 19990111 A 5320 6540867 WEB BOEING 737 737201 1384454 NM BS 285 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 69745 20215 LEFT NLG W/W STATIN 285, .5 INCH CRACK ON WEB, ONE RIVET BROKEN AND EVIDENCE OF INTERGRANULAR CORROSION ON VERTICAL CHOR D INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. CORROSION ON VERTICAL CHORD INSIDE NLG W/W AT LEFT AFT ACCESS PANEL. 2 L 7 2 4F A16WE 1999031901057 19990319 01057 EU 1999 3 19 RAIA990120 1 19990119 A 2910 137311D1619 LINE BAG JETSTM JETSTM3201 1500217 EU HYD FILTER FAILED A RAIA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 03 341TE 950 FLT 7075 - STL - LOST HYDRAULIC PRESSURE ON BOTH ENGINES HAD TO HAND PUMP GEAR DOWN. MAINTENANCE REPLACED HYDRAULIC LIN E AT MAIN HYDRAULIC FILTER. (M) 2 L 7 2 4T RT A56EU 1999031901058 19990319 01058 WP 1999 3 19 ORJA9927 1 19990108 A 5311 FRAME DOUG DC9 DC987 3022087 WP BS 1062 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 752RA 49780 AT PHOENIX LEVEL 2 CORROSION ON CAP OF FRAME AT FS 1062 IN AFT BAGGAGE PIT ABOVE S30. REMOVED CORRODED CAP. FABRICATED REPLACEMENT, TREATED AND PRIMED BARE METAL SURFACES. INSTALLED CAP IAW SRM REF 51-30-2. VERIFIED NO FURTHER CORROSION . (M) 2 L 7 2 4F RT A6WE 1999031901059 19990319 01059 WP 1999 3 19 ORJA9926 1 19990107 A 5320 ANGLE DOUG DC9 DC987 3022087 WP BS 1002 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 752RA 49780 AT PHOENIX LEVEL 2 CORROSION, LOWER CHORD ANGLE, STATION 1002, HAS CORROSION BEYOND LIMITS. REMOVED LOWER CHORD ANGLE 2 4542 1002. REMOVED TRACK SUPPORT ANGLES FOM. INSTALLED SPLICE, P/N 3936445-1 PO NR X9S454606. TRACK SUPPORT ANGLES TO BE INSTALLED ON WO NR 1499-17-K020. SRM FOR SPLICE INSTALLATION 51-30-0. VERIFIED WO NR 1499-17-K020, CORROSION REMOV ED. (M) 2 L 7 2 4F RT A6WE 1999031901060 19990319 01060 NE 1999 3 19 WRLA99010 2 19990122 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 1 MALFUNCTIONED A WRLA A UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 EA 27 277WA 48743 DURING INITIAL CLIMB AFTER TAKEOFF ON FLIGHT NR WOA972, FLIGHT CREW RECEIVED NOTIFICATION FROM AIRPORT TOWER THAT 'TWO F IREBALLS' WERE NOTED EXITING FROM THE NR 1 ENGINE DURING DEPARTURE. FLIGHT CREW NOTED THAT ALL ENGINES PARAMETERS WERE NORMAL. FLIGHT CREW ELECTED TO RETURN TO POINT OF DEPARTURE. AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER I NCIDENT. MAINTENANCE NOTED THAT THERE WERE NO 'OPEN FAULTS' IN THE CENTRAL FAULT DISPLAY SYSTEMS THAT WOULD INDICATE A MALFUNCTION WITH THE NR 1 ENGINE. ENGINE WAS RUN WITH ALL PARAMETERS NORMAL, AND WITH NO FAULTS NOTED IN THE CFDS. AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 1999031901066 19990319 01066 WP 1999 3 19 VTZA99006 2 19990104 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 301UE 41012 FLT 6267 - IAD-BRV - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED, CLEANED AND REINSTALLED. MAINTENANCE FOUND NO DEFECTS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T 3 T RT A41NM E3WE 1999031901067 19990319 01067 NE 1999 3 19 GAIA9926 2 19990209 A 7261 LINE BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LOOSE A GAIA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 EN ROUTE FROM SLC TO MHR, LOST OIL QUANTITY NR 1 ENGNE. SHUT DOWN NR 1 ENGINE. AIRCRAFT LANDED MHR WITHOUT ANY FURTHER DIFFICULTIES. FOUND AND RESEALED LOOSE LINE ON ENGINE GEARBOX HOUSING. INSPECTED ENGINE IAW PW MM CHAPTER 72. NO FUR THER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999031901070 19990319 01070 NE 1999 3 19 P2EA99027 2 19990125 A 7530 658385001 BLEED CONTROL 658385001 BOEING 737 737244 138448U NM PWA JT8 JT8D9A 52048 NE LEFT ENGINE FAILED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 0118 19708 MSP - FLT 416 - DURING THROTTLE ADVANCEMENT FOR TAKEOFF, HEARD LOUD NOIS FROM LEFT SIDE OF AIRCRAFT. TAKEOFF ABORTED (L ESS THAN 60 KNOTS), RETURNED TO GATE. REPLACED LEFT ENGINE PRESSURE RATIO BLEED CONTROL REGULATOR PER MM 75-31-11, OPER ATIONAL CHECK OK. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999031901073 19990319 01073 WP 1999 3 19 USAAD99029 1 19990218 A 2170 V1211 COALESCER BAG DOUG DC9 DC981 3022081 WP CABIN DIRTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 827US 48049 BOS-BUF - FLT 1022 - AFTER LANDING AT BUF THE FLIGHT CREW REPORTED FUMES IN THE FORWARD GALLEY AND COCKPIT 25 MINUTES AF TER TAKEOFF. SUSPECTED THE LEFT AIR CONDITIONING PACK AS THE SOURCE. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM A ND REPLACED THE WATER SEPARATOR COALESCER BAG AS A PRECAUTIONARY MEASURE. (M) 2 L 7 2 4F A6WE 1999031901074 19990319 01074 NM 1999 3 19 USAASB99041 1 19990218 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 288AU 23135 TPA - MAINTENANCE FOUND THE AFT ESCAPE DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999031901075 19990319 01075 NM 1999 3 19 USAASB99042 1 19990218 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM EMERGENCY EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 511AU 23594 ROC - MAINTENANCE FOUND THE CENTER RIGHT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999031901076 19990319 01076 NM 1999 3 19 USAASB99046 1 19990220 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 269AU 22881 BWI - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999031901077 19990319 01077 NM 1999 3 19 USAASB99047 1 19990220 A 3350 500000043 POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 267AU 22879 CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVI CE DOOR EMERGENCY EXIT LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999031901078 19990319 01078 NM 1999 3 19 99ZZZM194 1 19990220 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 267AU 22879 CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVI CE DOOR EMERGENCY EXIT LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999031901079 19990319 01079 NM 1999 3 19 99ZZZM195 1 19990220 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 267AU 22879 CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVI CE DOOR EMERGENCY EXIT LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999031901080 19990319 01080 NM 1999 3 19 USAASB99044 1 19990220 A 3350 20131ALP BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 409US 23879 CLE - MAINTENANCE FOUND THE CENTER CABIN FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTE RY PACK FOR THE M1136 POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999031901081 19990319 01081 NM 1999 3 19 USAASB99025 1 19990131 A 2612 FRF6E14S5S CONNECTOR BOEING 737 7372B7 1384560 NM NR 2 ENGINE SHORTED A USAA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 272AU 22884 BOS - FLT 1241 - DURING CLIMB-OUT FROM BOS AT FL 200, THE CREW RECEIVED A NR 2 ENGINE FIRE WARNING LIGHT AND HORN. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND IMMEDIATELY SHUT DOWN THE NR 2 ENGINE AND FIRE BOTH FIRE EXTINGUIS HING BOTTLES. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT BOS. AFTER EMERGENCY PROCEDURES WERE COMPL ETED, THE FIRE WARNING INDICATION CAME ON AGAIN WITH THE HORN AND RED WARNING LIGHTS INTERMITTENTLY CHIRPING AND FLASHIN G. APPROACH, LANDING AND TAXI WAS NORMAL FOR SINGLE ENGINE OPERATION. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINTE NANCE FOUND NO SIGNS OF FIRE OR HOT ENGINE. FOUND PINS A/D OF CANNON PLUG D1096 ON THE NR 2 ENGINE LOWER FIRE DETECTION 2 L 7 2 4F A16WE 1999031901082 19990319 01082 NM 1999 3 19 USAASB99026 1 19990201 A 3260 6552811109 ACCESSORY UNIT BOEING 737 737201 1384454 NM LANDING GEAR FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 241US 3690 22443 TPA - FLT2675 - ON APPROACH INTO TPA, ALL THREE LANDING GEAR RED UNSAFE LIGHTS ILLUMINATED. CREW EXECUTED A MISSED APPR OACH. CREW RECYCLED LANDING GEAR TWICE AND ALL THREE RED AND GREEN GEAR LIGHTS REMAINED ILLUMINATED. ON THIRD LANDING GEAR RECYCLE ATTEMPT, THE THREE RED GEAR LIGHTS EXTINGUISHED AND ONLY THE GHREE GREEN GEAR LIGHTS REMAINED ILLUMINATED. A NORMAL LANDING WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSOR Y UNIT. OPERATIONAL CHECK GOOD PER MM 32-09-100A. ACCOMPLISHED GEAR SWING. GEAR SWING CHECKS GOOD. (M) 2 L 7 2 4F A16WE 1999031901083 19990319 01083 WP 1999 3 19 ARWA990301 1 19990303 A 2910 LINE DOUG DC8 DC863F 302198F WP HYD SYSTEM FAILED A ARWA O OTHER B K J SMOKE/FUMES/ODORS/SPARKS FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 441J 45988 SJU - FLT 760 - IN CRUISE QTY DROPPED TO HALFWAY ON QTY GAUGE, FOLLOWED BY AN ODOR OF HYDRAULIC FLUID (NOXIOUS). INVEST IGATION REVEALED FLUID ESCAPING FROM CARGO DOOR SWIVEL JOINT. REMOVED AND REPLACED SWIVEL AND AUX PUMP PRESSURE LINE. O PS CHECK OK IAW MM 29-20-2, 52-36-1 AND 20-60-0. (M) 2 L 7 4 4F 4A25 1999031901084 19990319 01084 NM 1999 3 19 USAASB99033 1 19990208 A 2730 654476114 PCU BOEING 737 737201 1384454 NM ELEVATOR FAILED A USAA K NONE J K WARNING INDICATION FLUID LOSS AP APPROACH 1 EA 19 254AU 22796 BWI - FLT 2605, ON FINAL APPROACH, AFTER LANDING GEAR AND FLAPS WERE EXTENDED, THE 'A' SYSTEM HYDRAULIC QUANTITY DEPLETE D TO ZERO WITH THE LOW PRESSURE LIGHT ILLUMINATING. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED CLEAR OF THE RUNWAY. THE AIRCRAFT WAS TOWED TO THE GATE AND THE PASSENGERS DEPLANED NORMALLY. MAINTENANCE REMOVED AND REPLACED THE 'A' SYSTEM E LEVATOR PCU AND RIGGED PER MM 27-31-101A. (M) OPERATIONAL CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999031901085 19990319 01085 NM 1999 3 19 USAASB99030 1 19990205 A 7930 1163P181 SWITCH BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 19 223US 21665 PIT - FLT 8027 - ON DESCENT INTO PIT FROM YYZ, CAPT REPORTED THAT THE NR 1 ENGNIE OIL FILTER BYPASS LIGHT ILLUMINATED. C APT SHUT DOWN THE NR 1 ENGINE AND DECLARED AN EMERGENCY INTO PIT. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE . TOTAL SINGLE ENGINE TIME WAS 12 MINUTES. PRIOR TO DEPARTING YYZ, THE AIRCRAFT RETURNED TO THE GATE DUE TO THE NR 1 E NGINE OIL FILTER BYPASS LIGHT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE OIL FILTER AND FOUND THE OIL FILTER CO NTAMINATED WITH CARBON. AFTER DESCENDING INTO PIT WITH THE NR 1 ENGINE SHUTDOWN, MAINTENANCE REMOVED AND REPLACED THE N R 1 ENGINE OIL FILTER BYPASS SWITCH AND THE OIL PRESSURE SWITCH. RAN ENGINE TWO TIMES. LEAK CHECK AND OPERATIONAL CHE 2 L 7 2 4F A16WE 1999031901086 19990319 01086 NM 1999 3 19 99ZZZM196 1 19990205 A 7931 1163P181 SWITCH BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 19 223US 21665 PIT - FLT 8027 - ON DESCENT INTO PIT FROM YYZ, CAPT REPORTED THAT THE NR 1 ENGNIE OIL FILTER BYPASS LIGHT ILLUMINATED. C APT SHUT DOWN THE NR 1 ENGINE AND DECLARED AN EMERGENCY INTO PIT. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE . TOTAL SINGLE ENGINE TIME WAS 12 MINUTES. PRIOR TO DEPARTING YYZ, THE AIRCRAFT RETURNED TO THE GATE DUE TO THE NR 1 E NGINE OIL FILTER BYPASS LIGHT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE OIL FILTER AND FOUND THE OIL FILTER CO NTAMINATED WITH CARBON. AFTER DESCENDING INTO PIT WITH THE NR 1 ENGINE SHUTDOWN, MAINTENANCE REMOVED AND REPLACED THE N R 1 ENGINE OIL FILTER BYPASS SWITCH AND THE OIL PRESSURE SWITCH. RAN ENGINE TWO TIMES. LEAK CHECK AND OPERATIONAL CHE 2 L 7 2 4F A16WE 1999031901087 19990319 01087 NM 1999 3 19 USAASB99029 1 19990204 A 2761 654456114 ACTUATOR BOEING 737 737201 1384454 NM LT SPOILER LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 247US 43122 22754 BWI - FLT 2742 - ONE HOUR INTO FLIGHT, CAPTAIN REPORTED THAT THE SYSTEM 'A' HYDRAULIC QUANTITY STARTED DROPPING SLOWLY. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. NO LOSS OF HYDRAULIC PRESSURE OR AIRCRAFT ABILITY OCCURRED . UPON LANDING, HYDRAULIC QUANTITY READ ONE GALLON. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 3 FLIGHT SPOILER ACTUATOR PER MM 27-61-51. OPERATIONAL CHECK AND LE AK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999031901088 19990319 01088 NM 1999 3 19 USAA990063 1 19990112 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 44588 22752 CLT - DURING HM DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK ON SKIN STATION 727A STRINGER 18R. INSTALLED DOUBLER PE R SRM 53-30-3 AND EA 63480. (M) 2 L 7 2 4F A16WE 1999031901089 19990319 01089 NM 1999 3 19 USAA990062 1 19990112 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 44588 22752 CLT - DURING HM DROP IN VISUAL INSPECTION, FOUND A 2 INCH CRACK 6 INCH AFT OF STATION 727E STRINGER 16L. INSTALLED DOUB LER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999031901090 19990319 01090 NM 1999 3 19 USAA990064 1 19990209 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 41929 23114 CLT - DURING CHECK VISUAL INSPECTION, FOUND A .1 INCH CRACK STATION 727B PLUS 3 INCH STRINGER 18R ON SKIN. INSTALLED DO UBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999031901091 19990319 01091 EU 1999 3 19 PLGA990205 1 19990205 A 6120 SWITCH SAAB SF340 SF340A 7850100 EU AUTOCOARSEN FAILED A PLGA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 05 345BE 340A108 LGA - FLT 6545 - ON TO TAKEOFF ROLL, THE AUTOCOARSEN DID NOT ARM AND TO WAS ABORTED. THE SYSTEM WAS MEL'D AND AIRCRAFT REPOSITIONED TO ABL FOR REPAIRS. MAINTENACNE REPLACED THE CONTROL QUADRANT. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999031901092 19990319 01092 EU 1999 3 19 PLGA990206 1 19990206 A 3010 BOOT SAAB SF340 340B 7860101 EU RT WING PUNCTURED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 363BE 340B293 ALB - FLT 6500 - FLT 6500 - CREW REPORTED RIGHT OUTBOARD WING BOOT WOULD NOT INFLATE. AIRCRAFT DIVERTED TO ALB AND LAND ED WITHOUT INCIDENT. MAINTENANCE PATHCED THE BOOT AND A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999031901093 19990319 01093 EU 1999 3 19 PLGA990211 1 19990122 A 5101 STRUCTURE SAAB SF340 340B 7860101 EU AIRFRAME BIRDSTRIKE A PLGA A UNSCHED LANDING C F.O.D. CL CLIMB 1 NE 05 354BE 340B246 LGA - FLT 6549 - CREW REPORTED BIRD STRIKE AFTER TAKEOFF. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTE NANCE INSPECTED A/C NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999031901094 19990319 01094 EU 1999 3 19 PLGA990213 1 19990213 A 2421 31342001 GENERATOR SAAB SF340 340B 7860101 EU RIGHT FAILED A PLGA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NE 05 366BE 803 340B303 BOS - FLT 6528 - THE RIGHT AC GENERATOR FAILED, DUE TO WEATHER A/C DIVERTED TO BOS. MAINTENANCE REPLACED THE AC GENERAT OR AND GCU. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999031901095 19990319 01095 1999 3 19 PLGA990216 4 19990216 A 3452 TRANSPONDER SAAB SF340 340B 7860101 EU NR 2 FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 358BE 340B279 LGA - FLT 6514 - CREW REPORTED NR 2 TRANSPONDER FAILED ALONG WITH TCAS. NR 1 TRANSPONDER ALREADY MEL'D. A/C RETURNED T O LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600001 19990326 00001 NM 1999 3 26 TWAA9904001 1 19990315 A 3350 1000679 LIGHT BOEING 727 727231 1384079 NM ROW 18 WORN A TWAA K NONE O OTHER UK UNKNOWN 1 CE 05 54334 20461 THE EMERGENCY EXIT LIGHT AT ROW 18, RT SIDE OF CABIN, WAS FALLING OUT. REPLACED EMERGENCY LIGHT ASSY. CHECK-C 8-21-98 MCI. 2 L 7 3 4F A3WE 1999032600002 19990326 00002 NM 1999 3 26 TWAA9904002 1 19990308 A 5347 SEAT TRACK BOEING 727 727231 1384079 NM BS 360-450 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54352 21984 DURING CHECK-C MAINT, FOUND CHAIR TRACK WITH CORROSION AT RBL 45.5, STA 360 TO 450. REPLACED CHAIR TRACK PER SRM 53-10- 5 FROM STA 360 TO 450. 2 L 7 3 4F A3WE 1999032600003 19990326 00003 NM 1999 3 26 TWAA9904003 1 19990309 A 5347 SEAT TRACK BOEING 727 727231 1384079 NM BS 112 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54352 21984 DURING CHECK-C MAINT, FOUND CORROSION ON CHAIR TRACK AT STA 112, LBL 45. INSTALLED NEW TRACK AT LBL 45, STA 1010 TO 113 7, PER SPM 6-70-01. 2 L 7 3 4F A3WE 1999032600004 19990326 00004 NM 1999 3 26 TWAA9904004 1 19990221 A 5330 SKIN BOEING 727 727231 1384079 NM PAX DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 84355 21987 DURING CHECK-C MAINT, FOUND FORWARD ENTRY DOOR LOWER FUSELAGE HINGE CUTOUT CRACKED AT THE FWD END. INSTALLED A DOUBLER PER SRM 53-10-219, PAGE 210. 2 L 7 3 4F A3WE 1999032600005 19990326 00005 NM 1999 3 26 TWAA9904005 1 19990307 A 5754 WEDGE BOEING 767 767231 1385131 NM NR 11 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 DURING CHECK-C MAINT, FOUND THE NR 11 LEADING EDGE SLAT TRAILING EDGE WEDGE WITH DELAMINATION 4.5 INCHES IN DIAMETER, LO CATED 78 IN O/B OF I/B END. INSTALLED METAL TO METAL HOT BOND 6 IN BY 6 IN PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1999032600006 19990326 00006 NM 1999 3 26 TWAA9904006 1 19990307 A 5753 SKIN BOEING 767 767231 1385131 NM LT TE AFT FLAP DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 DURING CHECK-C MAINT, FOUND LT WING TRAILING EDGE AFT FLAP OF THE I/B FLAP WITH A HOLE 28 IN I/B OF O/B EDGE, 9 IN AFT O F LEADING EDGE. INSTALLED HOT BOND REPAIR PER SRM 57-53-01, 350 DEG CURE PERMANENT REPAIR, AND PAINTED HOT BOND REPAIR. 2 L 7 2 4F RT A1NM 1999032600007 19990326 00007 NM 1999 3 26 TWAA9904007 1 19990307 A 5730 SKIN BOEING 767 767231 1385131 NM LEFT WING DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 DURING CHECK-C MAINT, FOUND LT WING LOWER SURFACE ONE FOOT FROM I/B EDGE, WITH A 6 BY 4 IN DELAMINATION, 6 IN FROM THE T RAILING EDGE. REMOVED DELAMINATED AREA AND INSTALLED FILLER AND OVERLAY FIBERGLASS REPAIR PER SRM 51-70-05, PAINTED ARE A. 2 L 7 2 4F RT A1NM 1999032600008 19990326 00008 NM 1999 3 26 TWAA9904008 1 19990307 A 5753 SKIN BOEING 767 767231 1385131 NM LT TE FLAP DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 DURING CHECK-C MAINT, FOUND ON LT WING, THE O/B TRAILING EDGE FLAP WITH A .25 IN HOLE AT I/B END OF LOWER SURFACE. INST ALLED A 2 IN BY 2 IN WET LAY-UP PER SRM 51-70-06. 2 L 7 2 4F RT A1NM 1999032600009 19990326 00009 NM 1999 3 26 TWAA9904009 1 19990308 A 5347 SEAT TRACK BOEING 727 727231 1384079 NM BS 1070-1138 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54352 21984 DURING CHECK-C MAINT, FOUND CORROSION ON CHAIR TRACK APPROX STA 1070 TO 1138, LBL 55. REPLACED CHAIR TRACK PER SRM 53-1 0-5, STA 1070 TO 1138. 2 L 7 3 4F A3WE 1999032600010 19990326 00010 WP 1999 3 26 TWAA9904010 1 19990310 A 5620 WINDOW DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON CABIN WINDOW NR 36 ON LT SIDE OF AIRCRAFT, AFT EDGE AND FWD EDGE OF WINDO W. BLENDED PER SRM 53-05, FIG 3. INSTALLED DOUBLER PER DRAWING SRO9530053, AND ARA 16105. 2 L 7 2 4F A6WE 1999032600011 19990326 00011 WP 1999 3 26 TWAA9904011 1 19990314 A 5320 CHANNEL DOUG DC9 DC931 3022065 WP BS 598 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND FUSELAGE TO CENTER WING SECTION U ATTACH CHANNEL CRACKED AT STA 598, LONGERON 22R. REPL ACED PART PER SPM 06-70-01, PAGE 2 AND PAGE 3. 2 L 7 2 4F A6WE 1999032600012 19990326 00012 WP 1999 3 26 TWAA9904012 1 19990314 A 3230 BOLT DOUG DC9 DC931 3022065 WP RIGHT MLG CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND RT MAIN LANDING GEAR PULLEY QUADRANT ON FWD O/B BULKHEAD CABLE GUIDE PIN HAD CORRODED BO LT AND NUT. REPLACED BOLTS AND BUSHINGS AND CLEANED LARGE GUIDE PINS, AND REPLACED SMALL GUIDE PINS PER SPM 6-30-7. 2 L 7 2 4F A6WE 1999032600013 19990326 00013 WP 1999 3 26 TWAA9904101 1 19990317 A 3350 BULB DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 904TW 49156 THE EMERGENCY LIGHT IN THE TAIL COMPT THAT SHINES ON HANDLE WAS INOPERATIVE. REPOSITIONED AND SECURED THE BULB. CHECK- C 2-26-99 MCI. 2 L 7 2 4F A6WE 1999032600014 19990326 00014 WP 1999 3 26 TWAA9904102 1 19990311 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 224-294 SCRATCHED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING OP 15 MAINT CHECK, FOUND CHAIR TRACK CHANNEL SCRATCHED AT LBL 44, STA 224 TO 294. REPLACED CHAIR TRACK PER IPC 5 3-40-00 AND DOUGLAS DRAWING FROM STA 200 TO 294, LBL 44. 2 L 7 2 4F A6WE 1999032600015 19990326 00015 WP 1999 3 26 TWAA9904103 1 19990312 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 224 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AT STA 224, LBL 0. REPAIRED PER SPM 6-70-01, PAGE 2 ITEM 4 . INSTALLED SPLICE PER SRM 53-01, PAGE 10 FIG 2. REPLACED ANGLE FROM STA 218 TO 265. 2 L 7 2 4F A6WE 1999032600016 19990326 00016 WP 1999 3 26 TWAA9904104 1 19990310 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT TOP AND BOTTOM SIDES AT STA 160, RBL 1 TO 55. MADE NEW FLOOR SUPPORT OF 7075T6 ANGLE AND INSTALLED WITH HL - 40 HI-LOKS USING 870B2 SEALENT PER SRM 51-01, PAGE 1. 2 L 7 2 4F A6WE 1999032600017 19990326 00017 WP 1999 3 26 TWAA9904105 1 19990311 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 503 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT LBL 55 IN, STA 503. REMOVED CORROSION PER SPM 6-80-1. WITH IN LIMITS PER SRM 53-05, PAGE 8. 2 L 7 2 4F A6WE 1999032600018 19990326 00018 WP 1999 3 26 TWAA9904106 1 19990311 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 576 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT LBL 5 IN, STA 576. REMOVED CORROSION PER SPM 06-80-1. WITH IN LIMITS PER SRM 53-05, PAGE 8. 2 L 7 2 4F A6WE 1999032600019 19990326 00019 WP 1999 3 26 TWAA9904107 1 19990313 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 210 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT RBL 55, STA 210. REPLACED CHAIR TRACK AT RBL 55, STA 210 TO STA 797, PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999032600020 19990326 00020 NM 1999 3 26 TWAA9904108 1 19990309 A 5347 SEAT TRACK BOEING 727 727231 1384079 NM BS 344-420 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54352 21984 DURING CHECK-C MAINT, FOUND CHAIR TRACK WITH CORROSION AT RBL 24.75, STA 344 TO 420. REPLACED CHAIR TRACK FROM STA 344 TO 420, PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999032600021 19990326 00021 WP 1999 3 26 AT9900217 1 19990302 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND FLOOR WEB AT BS 617 CRACKED. FORMED DOUBLERS, DRILLED, DEBU RRED, TREATED, PRIMED, AND INSTALLED REPAIR AND REINSTALLED TWO PREVIOUSLY REMOVED BAFFLES IAW DC9 SRM 51-10-4, 53-20-1, 51-10-3, 51-30-2, AND RES NR 99358. 2 L 7 2 4F A6WE 1999032600022 19990326 00022 WP 1999 3 26 AT9900218 1 19990205 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-392 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT HAND FUSELAGE SKIN WITH NUMEROUS DENTS, DINGS AND GOUGES AT BS 2 29 TO 392 L18-26R. REMOVED OLD FUSELAGE SKIN, PLACED NEW SKIN, DRILLED, COUNTERSUNK, FABRICATED DOUBLER REPAIR, TREATED , PRIMED SKIN AND DOUBLER, AND INSTALLED IAW DC9 SRM 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3, AND RES NR 99574. 2 L 7 2 4F A6WE 1999032600023 19990326 00023 WP 1999 3 26 AT9900219 1 19990208 A 5311 LONGERON DOUG DC9 DC932 3022066 WP BS 598 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT HAND CABIN FLOOR LONGERON 18 CUSP MEMBRANE CRACKED FORWARD OF BS 598 MAIN FRAME RBL 56. FORMED DOUBLER REPAIR, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED DOUBLER REPAIRS IAW DC 9 SRM 51-10-2, 53-20-1 FIG 803 PG 805, 51-10-4, 51-10-3, AND RES NR 99357. 2 L 7 2 4F A6WE 1999032600024 19990326 00024 NM 1999 3 26 AT9900220 1 19990317 A 2910 NAS16126 O RING BOEING 737 7372L9 1384497 NM TR PRESS SWITCH DETERIORATED A ZZDA K NONE J WARNING INDICATION CL CLIMB 1 SO 15 464AT 21278 JUST AFTER TAKEOFF, HYDRAULIC FLUID LEVEL WENT FROM FULL INDICATION TO ONE GALLON. AIR RETURN. REMOVED AND REPLACED FA ULTY O-RING AT THRUST REVERSER PRESSURE SWITCH IAW MM 20-10-131. LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 1999032600025 19990326 00025 WP 1999 3 26 AT9900221 1 19990217 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 275 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN BULGE AT BS 275 L-18L. STRIPPED AREA, REMOVED FASTENERS , FOUND CORROSION. REMOVED SECTION OF SKIN ABOVE AND BELOW LONGERON 18. FABRICATED FINGER DOUBLER, FILLERS, AND EXTERN AL DOUBLERS, ALODINE, PRIMED, AND INSTALLED IAW DC9 SRM 53-04 FIG 12B, 51-10-3, 51-30-2, 51-30-5, AND RES NR 99577. 2 L 7 2 4F A6WE 1999032600026 19990326 00026 WP 1999 3 26 AT9900222 1 19990205 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERTICAL STAB CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE VERTICAL STABILIZER LEFT HAND UPPER PANEL 3703A SKIN CHAFED. BLENDED OUT CHAFE ON LEFT HAND VERTICAL STABILIZER SKIN, TREATED, PRIMED IAW DC9 SRM 55-01-0, 55-32-0, 55-01-0, 51-10-3, AND RES NR 99573. 2 L 7 2 4F A6WE 1999032600027 19990326 00027 WP 1999 3 26 AT9900223 1 19990205 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 218 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO COMPARTMENT FLOORING TIE IN MEMBER AT CUSP WEB HAS A CRA CK COMING OUT OF FASTENER HOLE TERMINATING AT EDGE OF AFT LOBE AT BS 218 RIGHT SIDE. REMOVED FLOORBOARD AND WEB ASSEMBL Y TO GAIN ACCESS TO FLOOR TIE IN MEMBER, CUT OUT CRACK VERIFY BY HFEC, REINSTALLED WEB ASSEMBLY AND FLOORBOARD IAW DC9 S RM 51-30-2, 53-20-1, 51-30-3, 51-10-3, 53-01 FIG 1, AND RES NR 99389. 2 L 7 2 4F A6WE 1999032600028 19990326 00028 WP 1999 3 26 AT9900224 1 19990205 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 237 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO FLOOR SUPPORT COMPARTMENT UPPER SURFACE CRACKED IN THE R ADIUS AT BS 237 LONGERON 27. REMOVED FLOOR SUPPORT, WELDED REPAIR SUPPORT USING 4951 FILLER ROD, TREAT, PRIMED AND INST ALLED IAW DC9 SRM 51-30-2, 51-10-3, 51-01 FIG 2, AND EA 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999032600029 19990326 00029 WP 1999 3 26 AT9900225 1 19990205 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 256 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO FLOOR SUPPORT MEMBER UPPER SURFACE CRACKED IN RADIUS AT BS 256 LONGERON 24R. REMOVED FLOOR SUPPORT, WELDED REPAIR SUPPORT USING 4951 FILLER ROD, AND REINSTALLED MEMBER IAW DC9 SRM 51-30-2, 51-10-3, 53-01 FIG 2, AND EA 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999032600030 19990326 00030 WP 1999 3 26 AT9900226 1 19990205 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 313 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT CRACK IN RADIUS AT BS 313 L-26 -27R. REMOVED FLOOR SUPPORT, WELD REPAIRED SUPPORT USING 4951 FILLER ROD, TREAT, PRIMED AND INSTALLED IAW DC9 SRM 51-30 -2, 53-03-0, 53-01 FIG 2, 51-10-3 AND EA 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999032600031 19990326 00031 WP 1999 3 26 AT9900227 1 19990205 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 351 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO FLOOR SUPPORT MEMBER AT BS 351 L-25-26R CRACKED. REMOVE D FLOOR SUPPORT, WELDED REPAIR SUPPORT USING 4951 FILLER ROD, AND INSTALLED MEMBER IAW DC9 SRM 51-10-4, 51-30-2, 53-03-0 , AND EA 12-5321-29-29-C1362. 2 L 7 2 4F A6WE 1999032600032 19990326 00032 WP 1999 3 26 AT9900228 1 19990206 A 5510 DOUBLER DOUG DC9 DC932 3022066 WP HORIZONTAL STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE HORIZONTAL STABILIZER BULLET FAIRING CORRODED ON METAL DOUBLER AT AFT END. REMOVED CORRODED DOUBLER, FABRICATED DOUBLER, HEAT TREATED, ALODINE, PRIMED, AND INSTALLED IAW DC9 SRM 55-01 FIG 1 , 51-10-2A, 51-10-3, 51-30-2, AND 51-30-1. 2 L 7 2 4F A6WE 1999032600033 19990326 00033 WP 1999 3 26 AT9900229 1 19990205 A 5312 BULKHEAD BRACKET DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT AFT BULKHEAD AFT SIDE ON THE LEFT HAND PULLEY BRACKET CORRODED ON THE LEGS. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER SECTOR BRACKET AND PRESSURE SEAL. RIGGED AND LEAK CHECK ED GOOD IAW DC9 SRM 51-10-3, AND MM 78-31-2. 2 L 7 2 4F A6WE 1999032600034 19990326 00034 WP 1999 3 26 AT9900230 1 19990207 A 5320 59133141 BRACKET DOUG DC9 DC932 3022066 WP BS 1143 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 821AT 47284 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT FUSELAGE TOP CONTROL CABLE PULLEY BRACKET CORRODED AT THE ATTACHME NT POINT AT BS 1143. REMOVED AND REPLACED TOP CONTROL CABLE PULLEY BRACKET IAW DC9 SRM 51-10-3, MM 27-20, AND OHM 27-00 . 2 L 7 2 4F A6WE 1999032600035 19990326 00035 WP 1999 3 26 AT9900231 1 19990319 A 5330 5967043 SKIN DOUG DC9 DC932 3022066 WP BS 1142 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LIGHT SURFACE CORROSION ON BARE METAL 22 INCHES BELOW CUSP WEB AT BS 1142 ON THE LEFT SIDE. FOUND CORROSION ON SKIN SPLICE DOUBLER OUT OF LIMITS, FORMED SKIN SPLICE DOUBLER, ORDER NEW SKIN, LOC ATED, DRILLED SKIN AND SPLICE DOUBLER AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-4, 51-30-2, 51-30-5, 51-30-1 AND RES NR 9 9599. 2 L 7 2 4F A6WE 1999032600036 19990326 00036 NM 1999 3 26 PCAA9900002 1 19990317 A 6120 78249050 PCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE MALFUNCTIONED A PCAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 13 820EX 12722 6513 019 120029 940604 AFTER TAKEOFF FROM MDT, THE CREW EXPERIENCED A NR 2 ENGINE TORQUE FLUCTUATION ASSOCIATED WITH A PROPELLER RPM FLUCTUATIO N, OIL PRESSURE REMAINED NORMAL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 2 PROP CONTROL UNIT AT FAULT. REMOVED AND REPLACED THE NR 2 PCU, TEST FLEW AIRCRAFT SATISFACTORILY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999032600037 19990326 00037 EU 1999 3 26 JBXA9900076 1 19990317 A 2910 NAS161210 O RING FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE WORN A JBXA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 05 106ML 11477 NR 1 HYDRAULIC SYSTEM QUANTITY LOW (FOLLOWED OPS PROCEDURE, ALT LG EXTENSION). FOUND NR 2 ENGINE HYDRAULIC PUMP QUICK D ISCONNECT FITTING O-RING WORN (LEAKING). REMOVED AND REPLACED O-RING, SERVICED HYDRAULIC SYSTEM TO FULL, ACCOMPLISHED L EAK CHECK WITH BOTH ELECTRIC PUMPS AND ENGINE DRIVEN PUMP. ALL CHECKS GOOD. 2 L 7 2 4F RT 1999032600038 19990326 00038 NM 1999 3 26 RAAA99B2011 1 19990317 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 520 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND BULGE IN SEAT TRACK OUTER FLANGE BS 520 AT LBL 45. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-01. M54 NR 230. 2 L 7 3 4F A3WE 1999032600039 19990326 00039 NM 1999 3 26 RAAA99B2012 1 19990317 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 580 BROKEN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND BROKEN LUG IN SEAT TRACK AT BS 580 AND BL 0. REPLACED SEAT TRACK SPLICE BS 540 T0 600 A T BL 0 IAW SRM 53-10-05. M54 NR 233. 2 L 7 3 4F A3WE 1999032600040 19990326 00040 NM 1999 3 26 RAAA99B2013 1 19990317 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1060 GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND DEEP GOUGE WORN IN EXTERIOR SKIN BS 1060 AT STR 18R. REMOVED DAMAGED AREA, INSTALLED RE PAIR DOUBLER IAW SRM 53-30-03 FIG 5. M54 NR 284. 2 L 7 3 4F A3WE 1999032600041 19990326 00041 NM 1999 3 26 RAAA99B2014 1 19990317 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 480-580 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION PER CARD B1 14010, FOUND RT OUTBOARD SEAT TRACK CORRODED BS 480, 500, 540, 560 AND 580. REP LACED SEAT TRACK FROM BS 380 T0 600 IAW SRM 53-10-05 FIG 7. M54 NR 291. 2 L 7 3 4F A3WE 1999032600042 19990326 00042 NM 1999 3 26 RAAA99B2015 1 19990318 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 1096-1136 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND RT SEAT TRACK IN AFT PIT CORRODED FROM BS 1096 TO 1136. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-20-9. M54 NR 294. 2 L 7 3 4F A3WE 1999032600043 19990326 00043 NM 1999 3 26 RAAA99B2016 1 19990318 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 783 WORN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK PER CARD B1-14010, FOUND SEAT TRACK LUG WORN BEYOND LIMITS AT BS 783 AND LBL 45. REMOVED AND R EPLACED SEAT TRACK SECTION FROM BS 760 TO 850 IAW SRM 53-10-2 FIG 7. M54 NR 297. 2 L 7 3 4F A3WE 1999032600044 19990326 00044 NM 1999 3 26 RAAA99B2017 1 19990318 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 916 WORN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK INSPECTION PER CARD B1 -114010, FOUND SEAT TRACK LUG WORN BEYOND LIMITS AT BS 916 AND LBL 25. R EMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FROM BS 870 TO 940 AT LBL 25. M54 NR 298A. 2 L 7 3 4F A3WE 1999032600045 19990326 00045 NM 1999 3 26 RAAA99B2018 1 19990318 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 480-640 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK PER CARD B1-14010, FOUND SEAT TRACK AT BS 480 TO 640 AT LBL 45 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-01. M54 NR 300. 2 L 7 3 4F A3WE 1999032600046 19990326 00046 NM 1999 3 26 CALA9900258 1 19990316 A 5330 SKIN BOEING 757 757224 1384958 NM BS 1520 & 1560 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN AT STA 1520 AND 1560 BETWEEN SRTINGER 29L AND 30L. SKIN REPAIRS WERE IN STALLED IAW ECRA 5331-01044. 2 L 7 2 4F RT A2NM 1999032600047 19990326 00047 NM 1999 3 26 CALA9900259 1 19990316 A 5753 SKIN BOEING 757 757224 1384958 NM LT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND LT WING O/B UPPER SURFACE INBOARD FLAP PANEL GOUGED BY SPOILER. THE PANEL WAS REMOVED AND REPAIRED IAW ECRA 5753-01061 AND REFITTED IAW MM 57-51-00. 2 L 7 2 4F RT A2NM 1999032600048 19990326 00048 NM 1999 3 26 CALA9900260 1 19990316 A 5730 PANEL BOEING 757 757224 1384958 NM WS 320 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND LT WING FIXED LEADING EDGE PANEL OUTBOARD OF PYLON AT WS 320 DELAMINATED. THE PANEL WAS REMOVED, REPAI RED IAW SRM 51-70-08, AND REFITTED IAW BOEING DRAWING 114N2108. 2 L 7 2 4F RT A2NM 1999032600049 19990326 00049 NM 1999 3 26 CALA9900261 1 19990316 A 5730 PANEL BOEING 757 757224 1384958 NM LEFT WING DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND LT WING LEADING EDGE PANEL NR 521CB DAMAGED. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-70-07, PARAGRA PH 4L, AND REFITTED IAW MM 57-41-01. 2 L 7 2 4F RT A2NM 1999032600050 19990326 00050 NM 1999 3 26 CALA9900262 1 19990316 A 5512 PANEL BOEING 757 757224 1384958 NM HORIZONAL STAB PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND RT HORIZONTAL STABILIZER PANEL NR 345DB PUNCTURED. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-70-05, P ARAGRAPH 4C, AND REFITTED. 2 L 7 2 4F RT A2NM 1999032600051 19990326 00051 NM 1999 3 26 CALA9900263 1 19990317 A 5753 FAIRING BOEING 757 757224 1384958 NM TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND FLAP FAIRING 572HB FORWARD EDGE OUTER SKIN PLIES DELAMINATED. THE FLAP FAIRING WAS REMOVED, REPAIRED I AW SRM 51-70-03, AND REFITTED IAW MM 27-51-30. 2 L 7 2 4F RT A2NM 1999032600052 19990326 00052 NM 1999 3 26 CALA9900264 1 19990317 A 5753 FAIRING BOEING 757 757224 1384958 NM LEFT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND LT WING FLAP FAIRING 574CB FORWARD EDGE OUTER SKIN PLIES DELAMINATING. THE FAIRING WAS REMOVED, REPAIR ED IAW SRM 51-70-04, AND REFITTED IAW MM 27-51-31. 2 L 7 2 4F RT A2NM 1999032600053 19990326 00053 NM 1999 3 26 CALA9900265 1 19990317 A 5730 114N210812 PANEL BOEING 757 757224 1384958 NM WS 320 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND RT FIXED L/E PANEL O/B OF PYLON AT WS 320 DELAMINATED. THE PANEL WAS REPAIRED IAW SRM 51-70-08 AND REF ITTED IAW BOEING DRAWING 114N2108. 2 L 7 2 4F RT A2NM 1999032600054 19990326 00054 NM 1999 3 26 CALA9900266 1 19990317 A 5730 114N15271 PANEL BOEING 757 757224 1384958 NM RIGHT WING DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND RT WING LEADING EDGE PANEL 611FB DAMAGED AT SCREW HOLE. THE PANEL WAS REPAIRED IAW SRM 51-70-04, PARAG RAPH 4L, AND REFITTED IAW MM 57-41-01. 2 L 7 2 4F RT A2NM 1999032600055 19990326 00055 NM 1999 3 26 CALA9900267 1 19990317 A 5315 FLOORBEAM BOEING 757 757224 1384958 NM BS 1640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1640, LBL 52 TO RBL 54. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-01, PAGE 20 9 TO 213 AND ECRA 5321-01039. 2 L 7 2 4F RT A2NM 1999032600056 19990326 00056 NM 1999 3 26 CALA9900268 1 19990317 A 5313 STRINGER BOEING 757 757224 1384958 NM BS 1787 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND STRINGERS 3-4L DENTED AT STA 1787. REPAIRED IAW ECRA 5331-01045. 2 L 7 2 4F RT A2NM 1999032600057 19990326 00057 NM 1999 3 26 CALA9900269 1 19990317 A 5230 143N66031 SKIN BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR LOWER EDGE. THE CARGO DOOR LOWER EDGE WAS REPLACED IAW SRM 52-30-0 3. 2 L 7 2 4F RT A2NM 1999032600058 19990326 00058 NM 1999 3 26 CALA9900270 1 19990317 A 5512 SKIN BOEING 757 757224 1384958 NM RT HORIZ STAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE DENTED AT FS 207.093. REPAIRED IAW SRM 51-70-10, PARAGRAPH 2M, F IGURE 7. 2 L 7 2 4F RT A2NM 1999032600059 19990326 00059 NM 1999 3 26 CALA9900271 1 19990317 A 5320 CHANNEL BOEING 757 757224 1384958 NM BS 324-345 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND CHANNEL BELOW GALLEY 1A MOUNT BETWEEN STA 345 AND 324, RBL 4 CORRODED. THE CHANNEL WAS REPLACED IAW BO EING DRAWING 141N5161. 2 L 7 2 4F RT A2NM 1999032600060 19990326 00060 NM 1999 3 26 CALA9900272 1 19990318 A 5330 SKIN BOEING 757 757224 1384958 NM BS 760 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14106 27296 INSPECTION FOUND IMPACT DAMAGE TO SKIN AT BS 760, STRINGERS 16L-17L. REPAIRED IAW ECRA 5331-01046. 2 L 7 2 4F RT A2NM 1999032600061 19990326 00061 NM 1999 3 26 CALA9900273 1 19990317 A 3350 20131A BATTERY PACK RADIANT BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND EMERGENCY PATH LIGHTING IN FORWARD SECTION OF FIRST CLASS CABIN INOPERATIVE. THE BATTERY PACK WAS REMO VED AND REPLACED IAW MM 33-51-00, PAGE 201. 2 L 7 3 4F A3WE 1999032600062 19990326 00062 NM 1999 3 26 CALA9900274 1 19990317 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 23-30 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND EMERGENCY PATH SEAT MOUNTED LIGHTING INOPERATIVE FROM ROW 23 TO 30. REPAIRED WIRING AND OPERATIONAL CH ECK WAS GOOD IAW MM 33-50-00, PAGE 201. 2 L 7 3 4F A3WE 1999032600063 19990326 00063 NM 1999 3 26 CALA9900275 1 19990317 A 5523 657279971 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR TAB SEPARATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND LT ELEVATOR CONTROL TAB TRAILING EDGE SKIN SEPARATING IN TWO PLACES. THE ELEVATOR CONTROL TAB WAS REMO VED AND REPLACED IAW 55-20-2. 2 L 7 3 4F A3WE 1999032600064 19990326 00064 NM 1999 3 26 CALA9900276 1 19990317 A 5512 SKIN BOEING 727 727232 1384082 NM LT HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND LT HORIZONTAL STABILIZER I/B LEADING EDGE AREA GOUGED. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51- 10-6 AND 51-30-2, PAGE 4. 2 L 7 3 4F A3WE 1999032600065 19990326 00065 NM 1999 3 26 CALA9900277 1 19990317 A 5753 6521630265 SKIN BOEING 727 727232 1384082 NM LT TE FOREFLAP DISBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND LT TRAILING EDGE I/B FOREFLAP DISBONDED AT UPPER AND LOWER SURFACE. THE FOREFLAP WAS REMOVED AND REPLA CED IAW MM 27-51-4. 2 L 7 3 4F A3WE 1999032600066 19990326 00066 WP 1999 3 26 9900981161 1 19990212 A 5347 SEAT TRACK DOUG DC10 DC1040 3023508 WP BS 1661-1700 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING M-CHECK, FOUND GOUGING AND CORROSION ON THE OUTBOARD AFT CABIN SEAT TRACK LBL 108 AT FS 1661 TO 1700. REPAIRED P ER EA 11-164769. 2 L 7 3 4F A22WE 1999032600067 19990326 00067 WP 1999 3 26 9900991161 1 19990217 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1009-1039 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING M-CHECK, FOUND CORROSION ON LONGERON 44R FROM FS 1009 TO 1039. REPAIRED PER EA 11-164772. REPAIRED PER EA 11-16 4772. 2 L 7 3 4F A22WE 1999032600068 19990326 00068 NM 1999 3 26 9901016729 1 19990113 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 360 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING M-CHECK, FOUND CRACK ON FRAME INBOARD FLANGE BETWEEN STR 0L AND 3L, FS 360. REPAIRED PER EA 67-164953. 2 L 7 4 4F A20WE 1999032600069 19990326 00069 NM 1999 3 26 9901026729 1 19990115 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING M-CHECK, FOUND CRACK ON FRAME WEB AT UPPER DECK FLOORBEAM TO BODY FRAME ATTACHMENT FS 400. REPAIRED PER EA 67-16 4964. 2 L 7 4 4F A20WE 1999032600070 19990326 00070 NM 1999 3 26 9901036729 1 19990113 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 360 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING M-CHECK, FOUND CRACK ON FRAME WEB AT FS 360, STR 1R-2R. REPAIRED PER EA 67-164950. 2 L 7 4 4F A20WE 1999032600071 19990326 00071 NM 1999 3 26 9901046729 1 19990115 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 420 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING M-CHECK, FOUND TWO HOLES CRACKED AT FRAME WEB AT UPPER DECK FLOORBEAM TO BODY FRAME ATTACHMENT, FS 420. REPAIRED PER EA 67-164965. 2 L 7 4 4F A20WE 1999032600072 19990326 00072 WP 1999 3 26 9901059881 1 19990317 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676MC 47652 DURING LINE CHECK, FOUND EMERGENCY LIGHTING IN FIRST CLASS SECTION INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN EMERG ENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999032600073 19990326 00073 WP 1999 3 26 9901061160 1 19990313 A 5610 WINDSHIELD DOUG DC10 DC1040 3023508 WP LT COCKPIT BROKEN A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 160US 46769 DURING CRUISE EN ROUTE TO AMS, THE CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED IN FLIGHT. FLIGHT DIVERTED TO BOS AND LAND ED WITHOUT INCIDENT. REPLACED WINDSHIELD AND HEAT CONTROLLER, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 1999032600074 19990326 00074 SO 1999 3 26 COMA9910042 1 19990316 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT LATCHED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 268CA 120262 SERVICE DOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT LATCHED PROPERLY. SECURED LATCHES AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999032600075 19990326 00075 EA 1999 3 26 COMA9960116 1 19990316 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA ROW 3-8 CONTAMINATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 7204 EMERGENCY FLOOR LIGHTING ROWS 3 TO 8 IS INOPERABLE. DRIED MOISTURE AT FLOOR LIGHTING CONNECTORS, SYSTEM OPERATION NORMA L. 2 L 7 2 4F RT A21EA 1999032600076 19990326 00076 EA 1999 3 26 COMA9960117 1 19990310 A 2810 FUEL CNDAIR CL600 CL6002B19 EA LEFT, RIGHT WING LEAKING A COMA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 01 945CA 7069 FLUID LEAKING FROM LEFT AND RIGHT WINGS AT THE FUEL VENT AREA. INSPECTED AIRCRAFT FOR FUEL LEAKS AND NONE FOUND. 2 L 7 2 4F RT A21EA 1999032600077 19990326 00077 EA 1999 3 26 COMA9960118 1 19990316 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 938CA 7046 FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999032600078 19990326 00078 NM 1999 3 26 QXEA9900499 1 19990316 A 2611 473054 DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTION A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 353PH 355 135 496 PUW- SMOKE WARNING LIGHT ILLUMINATED SEVERAL TIMES DURING FLIGHT. INSPECTED AND FOUND NO EVIDENCE OF SMOKE IN CARGO COM PARTMENT. REPLACED BOTH SMOKE DETECTORS, OPERATIONAL CHECKS GOOD. (S/N OFF 0819) 166 HRS & 243 CYCLES (TSN). 2 H 7 2 4T RT A13NM 1999032600079 19990326 00079 NM 1999 3 26 QXEA9900500 1 19990314 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTION A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 826PH 2022 306 526 PDX- FLOOR EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999032600080 19990326 00080 NM 1999 3 26 QXEA9900501 1 19990313 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 830PH 2303 2287 526 YYJ- PORTABLE COCKPIT OVERHEAD LIGHT INOP. MAINTENANCE REPLACED OVERHEAD LIGHT, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999032600081 19990326 00081 NM 1999 3 26 QXEA9900502 1 19990313 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 830PH 5 526 SEA- COCKPIT OVERHEAD EMERGENCY LIGHT VERY WEAK. MAINTENANCE REPLACED LIGHT, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999032600082 19990326 00082 EU 1999 3 26 QXEA9900496 1 19990313 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU ROW 8-9 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 BOI- OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 8 TO 9 INOP. REPLACED LIGHT PANEL, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999032600083 19990326 00083 EU 1999 3 26 QXEA9900497 1 19990314 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU COCKPIT DOOR INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11169 GEG- LEFT ARROW OF EXIT SIGN ABOVE COCKPIT DOOR INOP. REPLACED SIGN ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999032600084 19990326 00084 EU 1999 3 26 QXEA9900498 1 19990315 A 3350 6008905 BATTERY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 180 94 11159 GEG- FORWARD EMERGENCY 3 VOLT LIGHTS INOP. REPLACED NR 1 POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999032600085 19990326 00085 GL 1999 3 26 99FDEA00096 2 19990311 A 7200 ENGINE DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL NR 2 MALFUNCTIONED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 68051 47805 VIBRATION NOTED INCREASED WITH POWER CHG ON ENG NR 2. POWER REDUCED TO IDLE AND AC RETURN TO MEM. SWAPPED AC PACKS WIT H NO CHG IN VIBRATION ALL ENG AND HYD IND NORM. *S/D* REMOVED AND REPLACED NR 2 ENG IAW W/C 71T1101 & 71T1701. NR 2 E NG GROUND CKS NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 1999032600086 19990326 00086 EU 1999 3 26 99FDEA00107 1 19990317 A 2750 RETRACT MECH AIRBUS 310 A310222 3930315 EU TE FLAPS MALFUNCTIONED A FDEA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 25 452FE 313 ON FLAP EXT AT PHX WHEN EXTEND FLAPS FAULT LIGHT AND BOTH FLAP SYS FAULT LIGHT ILLUM ON OVHD IND FLAPS STUCK. C/W ECAM QRM PROCEDURE INCLUDES MOD SPD DUE TO LOSS OF A/S MOOK. 2 L 7 2 4F RT A35EU 1999032600087 19990326 00087 NM 1999 3 26 99FDEA00108 1 19990317 A 5320 65405072 SILL BOEING 727 72725C 138400H NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 WHILE WORKING NR 420 FOUND CORROSION ON MAIN CARGO DOOR LWR SILL WEB AT BS 480 TO 620 LBL 65 WL 200 TO 208. *S/D* REMO VED AND REPLACED MAIN CARGO DOOR LWR SILL WEB IAW FEDEX SRM 51-30-2 AND FEDEX DWG 65-40507. 2 L 7 3 4F A3WE 1999032600088 19990326 00088 WP 1999 3 26 ABXA9900202 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 616.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE AT STATION FS 616.250 LOWER RIB, FORWARD OF ACCESS HOLE IS CRACKED AT AFT END. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600089 19990326 00089 WP 1999 3 26 ABXA9900203 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 785 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE AT STATION FS 785 UPPER LEADING EDGE RIB CRACKED AT AFT END. REPAIRED IAW DC8 SRM 57-20-0. 2 L 7 4 4F 4A25 1999032600090 19990326 00090 WP 1999 3 26 ABXA9900204 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE STATION FS 772.508 UPPER RIB CRACKED. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600091 19990326 00091 WP 1999 3 26 ABXA900205 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 766.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE RIB CRACKED AT STATION FS 766.250. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600092 19990326 00092 WP 1999 3 26 ABXA9900206 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 747.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT STATION FS 747.500. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600093 19990326 00093 WP 1999 3 26 ABXA9900207 1 19990228 A 5712 RIB DOUG DOUG DC8 DC863 302198A WP WS 461.372 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LEFT WING CENTER LEADING EDGE RIB CRACKED AT STATION FS 461.372. REPAIRED IAW DWG K05056. 2 L 7 4 4F 4A25 1999032600094 19990326 00094 WP 1999 3 26 ABXA9900208 1 19990302 A 5320 37584001 FITTING DOUG DOUG DC8 DC863 302198A WP WS 22.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 FITTING INSIDE NR 2 TANK CRACKED AT STATION XRS 22.75. REPAIRED IAW DC8 SRM 51-1-3 AND ABX REA D857-24941. 2 L 7 4 4F 4A25 1999032600095 19990326 00095 WP 1999 3 26 ABXA9900209 1 19990302 A 5320 3755822515N FITTING DOUG DOUG DC8 DC863 302198A WP BS 300 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 BATHTUB FITTING CRACKED AT STATION 300, LONGERON 27 LEFT. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999032600096 19990326 00096 WP 1999 3 26 ABXA9900210 1 19990309 A 5320 575499213B DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 640-680 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 HEAVY INTERGRANULAR CORROSION IN MID ASSY COMP UNDER LONGERON 34 LEFT AT STATION 640 TO 680. REPAIRED IAW ABX REA D853- 277154. 2 L 7 4 4F 4A25 1999032600097 19990326 00097 WP 1999 3 26 ABXA9900211 1 19990309 A 5320 5779932 SHEAR TIE DOUG DOUG DC8 DC863 302198A WP BS 660 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 SHEAR TIE HAD CORROSION AT STATION 660, LONGERONS 35 RIGHT TO 34 LEFT. REPAIRED IAW DC8 SRM 53-4-1. 2 L 7 4 4F 4A25 1999032600098 19990326 00098 NM 1999 3 26 SCNA99046 1 19990314 A 3350 2371 BATTERY PACK BOEING 727 7272J4 1384006 NM AFT AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, AN EMERGENCY LIGHT IN THE AFT AIRSTAIR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLAC ED THE BATTERY PACK IN THE AFT AIRSTAIR EMERGENCY LIGHT, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999032600099 19990326 00099 1999 3 26 SCNA99047 4 19990311 A 3418 2568A13 SENSOR DOUG DC10 DC1015 3022118 WP RIGHT FAILED A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 154SY 499 48259 DURING A LINE MAINTENANCE CHECK, THE RIGHT STALL WARNING FAILED THE SELF TEST. REMOVED AND REPLACED THE ANGLE OF ATTACK SENSOR IAW MM 223301. SYSTEM OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1999032600100 19990326 00100 NM 1999 3 26 SCNA99048 1 19990312 A 3610 CLAMP BOEING 727 727259 138408J NM NR 1 ENGINE LOOSE A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 289SC 22475 DURING CLIMB, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH REDUCED POWER THEN ILLUMINATED AGAIN WHEN CLIMB POWER WAS SET. ALSO, LIGHT WAS ILLUMINATED WITH ASSOCIATED BLEED AND PACKS OFF. FOUND THE 13TH STAGE REGULATOR VALVE CLAMP LOOSE. TIGHTENED CLAMP AND RAN NR 1 ENGINE, OPERATIONALLY AND LEAK CHECKS GOOD. 2 L 7 3 4F A3WE 1999032600101 19990326 00101 SO 1999 3 26 SWIA971434 1 19990301 A 3234 SELECTOR EMB 120 EMB120RT SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 289YV 120289 AFTER TAKEOFF DURING GEAR RETRACTION, LEFT RED A LIGHT AND RIGHT RED B LIGHT REMAINED ON WITH A LOUD GRINDING NOISE OBSE RVED. CYCLED THE GEAR PER THE QRH AND SITUATION REMAINED FOR TWO CYCLES. ON THIRD ATTEMPT IT CORRECTED ITSELF. RETURN ED TO LAX. REMOVED AND REPLACED LANDING GEAR SELECTOR HANDLE. CYCLED GEAR SEVERAL TIMES. NO DISCREPANCIES NOTED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999032600102 19990326 00102 SO 1999 3 26 SWIA971435 1 19990302 A 3260 SENSOR EMB 120 EMB120RT SO PWA 118 PW118A NE LT MLG OUT OF ADJUST A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 289YV 120289 LEFT RED A LIGHT LANDING GEAR CAME ON INFLIGHT AND STAYED ON UNTIL GEAR DOWN SELECTED. JACKED AIRCRAFT AND CYCLED GEAR. FOUND LEFT RED A TRANSIT LIGHT STAYS ON. ADJUSTED A UP SENSOR TO MININUM GAP PER MM 32-61-01. CYCLED GEAR SEVERAL TI MES AND ALL INDICATION LIGHTS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999032600103 19990326 00103 SO 1999 3 26 SWIA971436 1 19990302 A 3297 WIRE HARNESS EMB 120 EMB120RT SO PWA 118 PW118A NE LT MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 289YV 120289 LEFT RED A LIGHT LANDING GEAR CAME ON INFLIGHT AGAIN. RETURNED TO SFO. FOUND PROBLEM TO BE IN A SYSTEM SENSOR HARNESS. SWAPPED A & B PLUGS AND DEFERRED B INTRANSIT PER MEL 32-60-1A. 2 L 7 2 4T 4 T RT A31SO E20NE 1999032600104 19990326 00104 SO 1999 3 26 SWIA971437 1 19990303 A 2150 PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT FAILED A SWIA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 288SW 120316 DIVERTED TO BUR WHEN THE LEFT PACK FAILED AND FILLED CABIN WITH SMOKE. OPERATIONAL CHECKED LEFT PACK, LEFT ENGINE HIGH STAGE BLEED SWITCHING SYSTEM, RAM AIR SYSTEM AND PACK FAIL SWITCH WIRING. NO DISCREPANCIES NOTED ANY WHERE. ALL SYSTEM S OPERATE NORMALLY. 2 L 7 2 4T 4 T RT A31SO E20NE 1999032600105 19990326 00105 SO 1999 3 26 SWIA971438 1 19990306 A 3260 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 579SW 120347 ON DEPARTURE, NOSE WHEEL INDICATED 1 B GREEN, 1 -B+ RED. RETURNED TO PSP. REPLACED NOSE GEAR B INDICATION DOWNLOCK PRO X SWITCH HARNESS. SWUNG GEAR NUMEROUS TIMES. ALL INDICATIONS GOOD. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999032600106 19990326 00106 NM 1999 3 26 P5CA9900491 1 19990312 A 5320 SKIN BOEING 747 747124 1384874 NM CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FUSELAGE FWD CARGO DOOR AFT CUTOUT LOWER CORNER EXTERIOR SKIN FOUND DAMAGED. SKIN REPAIRED PER RS 53-21-340531. 2 L 7 4 4F A20WE 1999032600107 19990326 00107 NM 1999 3 26 P5CA9900492 1 19990312 A 5313 STRINGER BOEING 747 747124 1384874 NM BS 1348 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK CROWN BS 1348 STR 11L STRINGER END FOUND CRACKED. CRACKED STRINGER REPAIRED PER SRM 53-10-03 FIG 5. 2 L 7 4 4F A20WE 1999032600108 19990326 00108 NM 1999 3 26 P5CA9900493 1 19990312 A 5311 FRAME BOEING 747 747124 1384874 NM BS 860 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK BS 860 CRACKED AT S13L CUTOUT AREA. FRAME REPAIRED PER RS R53-27-34052. 2 L 7 4 4F A20WE 1999032600109 19990326 00109 NM 1999 3 26 P5CA9900494 1 19990314 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION ON FLOORBEAM MAIN DECK BS 1580 LBL 9. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 1999032600110 19990326 00110 NM 1999 3 26 P5CA9900495 1 19990314 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON FLOORBEAM AT MAIN DECK BS 1580 LBL 34 TO 75. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 1999032600111 19990326 00111 NM 1999 3 26 P5CA9900496 1 19990314 A 5315 FLOORBEAM BOEING 747 747124 1384874 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON FLOORBEAM AT BS 1580 LBL 82 TO 96. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 1999032600112 19990326 00112 NM 1999 3 26 P5CA9900498 1 19990315 A 5347 TRACK BOEING 747 747124 1384874 NM BS 1140-1160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON MAIN DECK BS 1140 TO 1160 RBL 13 TIE DOWN TRACK LOWER FACE. CORROSION REMOVED PER SRM 51-10- 01 AND 53-10-01. 2 L 7 4 4F A20WE 1999032600113 19990326 00113 NM 1999 3 26 P5CA9900499 1 19990315 A 5347 SEAT TRACK BOEING 747 747124 1384874 NM BS 1808 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT BS 1808 TO 1814 RBL 11 SEAT TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01 AND 53- 10-01. 2 L 7 4 4F A20WE 1999032600114 19990326 00114 NM 1999 3 26 P5CA9900500 1 19990315 A 5347 TRACK BOEING 747 747124 1384874 NM BS 460-540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT BS 460 TO 540 LBL 33 TIE DOWN TRACK. CORROSION REMOVED PER SRM 51-10-01 AND 53-10-01. 2 L 7 4 4F A20WE 1999032600115 19990326 00115 NM 1999 3 26 P5CA9900501 1 19990315 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1360 LBL 33 FLOOR SUPPORT LOWER FACE. CORRSOSION REMOVED PER SRM 51-10-01 AND 5 3-10-01. 2 L 7 4 4F A20WE 1999032600116 19990326 00116 NM 1999 3 26 P5CA9900502 1 19990315 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1920-1940 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON MAIN DECK BS 1920 TO 1940 LBL 114 FLOOR SUPPORT. FLOOR SUPPORT REPAIRED PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 1999032600117 19990326 00117 NM 1999 3 26 P5CA9900503 1 19990315 A 5400 SPAR BOEING 747 747124 1384874 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 1 PYLON LOWER SPAR WEB HAS CRACK APPROX 2 INCHES LONG AT NAC STA 232 RT SIDE. REPAIRED PER SRM 54-10-03. 2 L 7 4 4F A20WE 1999032600118 19990326 00118 NM 1999 3 26 P5CA9900504 1 19990315 A 5400 SPAR BOEING 747 747124 1384874 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 4 PYLON LOWER SPAR WEB FOUND CRACKED AT NAC STA 230 TO 234. EPAIRED PER SRM 54-10-03 FIG 2 AND 3. 2 L 7 4 4F A20WE 1999032600155 19990326 00155 1999 3 26 99ZZZX1020 4 19990127 A 3197 WIRE PIPER PA60 PA60600 7106001 NM COCKPIT SHORTED A BSYA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 6896B 600919816126 ELECTRICAL SMELL IN COCKPIT GOING INTO BDL. FOUND LT, NAVIGATION LIGHT 28-VOLT WIRE SHORTING OUT AT SOCKET ASSY. REPAI RED WIRE. OPS CHECKS GOOD. 1 M 7 2 3O RT A17WE 1999032600179 19990326 00179 CE 1999 3 26 99ZZZX1044 1 19990129 A 5730 RIVETS CESSNA 208 208B 2073701 CE LT WING MISINSTALLED A A DEMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 03 751FX 208B0514 24 INCHES FROM WING ROOT ON BOTTOM OF LEFT WING, THE RIVETS FASTENING THE LEADING EDGE SKIN TO THE FRONT SPAR WERE SMOKI NG VERY BADLY IN AN AREA 12 INCHES IN LENGTH. IT APPEARS THAT CESSNA, WHEN BUILDNG THIS AIRCRAFT, COUNTERSUNK THE LEADI NG EDGE SKIN, THEN USED A REDUCED HEAD COUNTERSUNK RIVET, WHICH MAY HAVE BOTTOMED OUT AND DID NOT DRAW TIGHT AGAINST THE SKIN. THIS LETS THE HOLE IN THE SKIN WORK AROUND THE RIVET ENLARGING THE HOLE IN THE SKIN. THE RIVETS ARE STILL TIGHT IN THE HOLES. SUBMITTER STATED THERE IS EVIDENCE OF THIS SAME PROBLEM ON THE TOP OF THE WING ALSO. 1 H 7 1 3T A37CE 1999032600190 19990326 00190 CE 1999 3 26 99ZZZX1056 1 19990112 A 3230 VALVE 2129402 CESSNA 500 550 2076604 CE MLG LEAKING A ISYA O OTHER O OTHER CL CLIMB 1 GL 25 84EA 7 594 5500484 ON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT LANDED UNEVENTFULLY. TROUBLESHOOTING REVEALED VALVE ON EMERGENCY PNEUMATIC RESERVOIR (BLOW DOWN BOTTLE) LEAKED, PRESSURIZING DOWN SIDE OF LANDING GEAR RETRACTION SYSTEM. ASSEMBLY WAS R EMOVED AND SHIPPED OUT FOR REPAIR. 1 L 7 2 4F A22CE 1999032600197 19990326 00197 NM 1999 3 26 RAAA99B2019 1 19990319 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 500 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C CHECK, FOUND FLOORBEAM UPPER CHORD FORWARD FLANGE LOWER SURFACE CORRODED AT BS 500 AND LBL 55. INSTA LLED REPAIR IAW SRM 53-10-08 M54-306. 2 L 7 3 4F A3WE 1999032600198 19990326 00198 NM 1999 3 26 RAAA99B2020 1 19990319 A 5230 FITTING BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION PER AD 80-08-10, FOUND BS 500 MCD LATCH SUPPORT FITTING UPPER FLANGE CRACKED 3 IN. REMOVED AND REPLACED FITTING IAW BOEING SB 727-53A0177 M54-320. 2 L 7 3 4F A3WE 1999032600199 19990326 00199 NM 1999 3 26 RAAA99B2021 1 19990319 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 600 GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C CHECK, FOUND FLOORBEAM UPPER CHORD FORWARD FLANGE LOWER SURFACE GOUGED AT BS 600 AND LBL 2. BLENDED FLOORBEAM UPPER CHORD FWD FLANGE LOWER SURFACE IAW SRM 53-10-01. 2 L 7 3 4F A3WE 1999032600200 19990326 00200 NM 1999 3 26 RAAA99B2022 1 19990319 A 5230 FITTING BOEING 727 72722C 138400F NM CARGO DOOR GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION PER AD 80-08-10, FOUND MCD NO 8 LATCH SUPPORT FITTING GOUGED UPPER FLANGE LOWER SURFACE. BL ENDED LATCH SUPPORT FITTING IAW SRM 53-10-01 M54 NO 328. 2 L 7 3 4F A3WE 1999032600201 19990326 00201 NM 1999 3 26 CALA9900278 1 19990317 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND A .3125 INCH CRACK AT RT I/B MIDFLAP LOWER TRAILING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS I NSTALLED IAW SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999032600202 19990326 00202 NM 1999 3 26 CALA9900279 1 19990317 A 5753 6521630174 SKIN BOEING 727 727232 1384082 NM RT TE FOREFLAP TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND RT I/B FOREFLAP INBOARD MOST END UPPER LEADING EDGE SKIN TORN FORWARD OF SPRING DOOR. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3. 2 L 7 3 4F A3WE 1999032600203 19990326 00203 NM 1999 3 26 CALA9900280 1 19990317 A 5752 652172642K SKIN BOEING 727 727232 1384082 NM RT AILERON TAB DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND TWO SMALL DEBONDED AREAS IN RT O/B AILERON TAB TRAILING EDGE. THE RT O/B AILERON TAB WAS REMOVED AND R EPLACED IAW MM 27-10-41. 2 L 7 3 4F A3WE 1999032600204 19990326 00204 NM 1999 3 26 CALA9900281 1 19990317 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND A 1.25 INCH CRACK IN RT O/B FOREFLAP LEADING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLE D IAW SRM 57-50-4 AND 51-30-2, PAGE 7. 2 L 7 3 4F A3WE 1999032600205 19990326 00205 NM 1999 3 26 CALA9900282 1 19990317 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND A .125 INCH CRACK IN RT WING NR 7 SLAT LOWER SPANWISE CHORD ANGLE AT CUTOUT FOR I/B TRACK AND A .3125 I NCH CRACK AT STOP PAD AREA SIX INCHES INBOARD. THE ANGLE WAS REMOVED. AN ANGLE AND REPAIR SPLICE WERE INSTALLED IAW SR M 51-40-3, 51-10-2, AND 57-30-2. 2 L 7 3 4F A3WE 1999032600206 19990326 00206 NM 1999 3 26 CALA9900283 1 19990318 A 5755 SKIN BOEING 727 727232 1384082 NM NR 13 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND A .1875 INCH CRACK AT RT WING UPPER TRAILING EDGE AT CUTOUT FOR NR 13 SPOILER SECOND FROM O/B HINGE CUT OUT. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED AND EDGES WERE SEALED IAW SRM 51-10-1 AND 51-10-3, PAGE 4. 2 L 7 3 4F A3WE 1999032600207 19990326 00207 NM 1999 3 26 CALA9900284 1 19990318 A 5754 SKIN BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND TWO .5 INCH CRACKS COMING FROM SCREW HOLE TO RIVETS AT RT WING NR 7 SLAT UPPER TRAILING EDGE WHERE O/B HOOK MOUNTS. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-20-3. 2 L 7 3 4F A3WE 1999032600208 19990326 00208 NM 1999 3 26 CALA9900285 1 19990318 A 5521 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND A 1 INCH CRACK IN LEFT ELEVATOR LOWER SKIN JUST I/B AND AFT OF PANEL NR 9311. THE CRACK WAS STOP DRILL ED IAW SRM 55-20-3. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, 51-10-2, AND 51-30. A CALCULATED BALANCE WAS PERFORMED IA W SRM 51-80-7 AND WAS WITHIN LIMITS. 2 L 7 3 4F A3WE 1999032600209 19990326 00209 NM 1999 3 26 CALA9900286 1 19990318 A 3397 WIRE BOEING 727 727232 1384082 NM LAVATORY LOOSE A CALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND EXIT IDENTIFIER LIGHT AT LEFT AFT LAV WALL INOPERATIVE. MAINTENANCE FOUND A LOOSE GROUND WIRE. THE WI RE WAS SECURED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED. 2 L 7 3 4F A3WE 1999032600210 19990326 00210 NM 1999 3 26 CALA9900287 1 19990318 A 3397 WIRE BOEING 727 727232 1384082 NM L2 DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND THE EXIT IDENTIFIER LIGHT AT L-2 DOOR INOPERATIVE. MAINTENANCE FOUND A BROKEN GROUND WIRE. THE WIRE W AS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED. 2 L 7 3 4F A3WE 1999032600211 19990326 00211 NM 1999 3 26 CALA9900288 1 19990318 A 3397 WIRE BOEING 727 727232 1384082 NM R2 DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND EXIT IDENTIFIER LIGHT AT R-2 DOOR INOPERATIVE. MAINTENANCE FOUND EXIT LIGHT WIRE BROKEN. THE WIRE WAS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED. 2 L 7 3 4F A3WE 1999032600212 19990326 00212 NM 1999 3 26 CALA9900289 1 19990318 A 5510 69144106 BOLT BOEING 727 727232 1384082 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND BOTH HORIZONTAL STABILIZER HINGE PIN BOLTS CORRODED. BOTH HINGE PINS WERE REPLACED IAW MM 55-00. 2 L 7 3 4F A3WE 1999032600213 19990326 00213 NM 1999 3 26 CALA9900290 1 19990318 A 5510 HOUSING BOEING 727 727232 1384082 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND HORIZONTAL STABILER LEFT AND RIGHT HINGE BUSHING HOUSINGS CORRODED. THE BUSHINGS AND BEARINGS WERE REM OVED AND REPLACED IAW ECRA 555C028 AND ECRA 5550-01033. 2 L 7 3 4F A3WE 1999032600214 19990326 00214 NM 1999 3 26 CALA9900291 1 19990318 A 7110 65196854540 COWL BOEING 727 727232 1384082 NM NR 3 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND A 2 INCH CRACK IN NR 3 ENGINE NOSE COWL ACOUSTIC LINING WITH LINING ERODED IN SEVERAL AREAS. THE NR 3 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 54-00. 2 L 7 3 4F A3WE 1999032600215 19990326 00215 NM 1999 3 26 CALA9900292 1 19990318 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 6 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND A 1 INCH CRACK IN INBOARD SUPPORT BRACKET AT TOP AND BOTTOM OF NR 6 LEADING EDGE FLAP ACTUATOR. THE BR ACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999032600216 19990326 00216 NM 1999 3 26 CALA9900293 1 19990318 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 1128-1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND LOWER FLANGE OF INTERCOSTAL CORRODED IN AFT CARGO AREA AT STA 1128-1148 OUTBOARD OF STRINGER 28R. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1999032600217 19990326 00217 NM 1999 3 26 UPS99229057 1 19990318 A 5320 SUPPORT BOEING 727 72727C 138400J NM BS 1045 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION ON AFT CARGO BAY FLOOR SUPPORT AT BS 1045, RBL 3, WL 154. REMOVED AND REPLACED SEGMENT OF S UPPORT PER SRM 53-10-5 FIGURE 4. 2 L 7 3 4F A3WE 1999032600218 19990326 00218 NM 1999 3 26 UPS99229058 1 19990318 A 5320 SUPPORT BOEING 727 72727C 138400J NM BS 314-344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORRSION ON CHANNEL SUPPORT BS 314-344, RBL 13.5, WL 208 UNDER LAV DOORWAY. REMOVED AND REPLACED CHAN NEL SUPPORT PER SRM 51-10-02. 2 L 7 3 4F A3WE 1999032600219 19990326 00219 WP 1999 3 26 ABXA9900212 1 19990221 A 5320 375022571 SPLICE DOUG DOUG DC8 DC863 302198A WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 STATION 600-620 LONGERON 31 RIGHT SPLICE WAS CRACKED. REPLACED SPLICE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999032600220 19990326 00220 WP 1999 3 26 ABXA9900213 1 19990221 A 5313 575032231 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1260-1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LONGERON 32 LEFT CRACKED AT STATION 1260-1280. REPAIRED IAW ABX REA D853-24938MR. 2 L 7 4 4F 4A25 1999032600221 19990326 00221 WP 1999 3 26 ABXA9900214 1 19990222 A 5712 576953063 RIB DOUG DOUG DC8 DC863 302198A WP WS 410.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LEFT WING CENTER LEADING EDGE UPPER RIB CRACKED AT STATION FS 410.250. REPAIRED IAW DWG NR K05056. 2 L 7 4 4F 4A25 1999032600222 19990326 00222 WP 1999 3 26 ABXA9900215 1 19990222 A 5320 3750257503 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LONGERON 31 LEFT SPLICE FITTING CRACKED BETWEEN STATIONS 1040-1060. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999032600223 19990326 00223 WP 1999 3 26 ABXA9900216 1 19990223 A 5400 5769859 DOUBLER DOUG DOUG DC8 DC863 302198A WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LEFT WING LOWER DOUBLER CRACKED ON NR 2 PYLON. REPAIRED IAW DC8 SRM 51-1-26 AND 57-2-1A. 2 L 7 4 4F 4A25 1999032600224 19990326 00224 WP 1999 3 26 ABXA9900217 1 19990209 A 5320 975407352 WEB DOUG DOUG DC8 DC863 302198A WP BS 560-580 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 56141 MAIN CABIN FLOOR CUSP WEB AT STATION 560-580 WAS EXFOLIATED. REPAIRED IAW DC8 SRM 53-20. 2 L 7 4 4F 4A25 1999032600225 19990326 00225 WP 1999 3 26 ABXA9900218 1 19990219 A 5753 5642960 RIB DOUG DOUG DC8 DC863 302198A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT INBOARD FLAP WEDGE RIB WAS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999032600226 19990326 00226 WP 1999 3 26 ABXA9900219 1 19990219 A 5320 37558451 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 HEAVY CORROSION ON TORQUE BOX BATH TUB FITTING, STATION 1220, LONGERON 33 LEFT TO 34 LEFT. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999032600227 19990326 00227 WP 1999 3 26 ABXA9900220 1 19990220 A 5320 SR085380057 ANGLE DOUG DOUG DC8 DC863 302198A WP VERT STAB/FUS CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 VERTICAL STABILIZER TO FUSELAGE LOWER RIGHT DRAG ANGLE FLANGE CRACKED. REPAIRED IAW DC8 SRM 53-2-5. 2 L 7 4 4F 4A25 1999032600228 19990326 00228 WP 1999 3 26 ABXA9900221 1 19990221 A 5320 4645517502 FITTING DOUG DOUG DC8 DC863 302198A WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 FLOORBEAM SUPPORT ANGLE CRACKED AT STATION 680, RBL 24. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999032600229 19990326 00229 NE 1999 3 26 SCNA99051 2 19990314 A 7261 515107 OIL PUMP BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE INOPERATIVE A SCNA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 15 275AF 22092 DURING DESCENT AT APPROXIMATELY FL200, CREW OBSERVED LOW OIL PRESSURE LIGHT ON NR 2 ENGINE. OIL PRESSURE DECAYED TO 15 PSI, QUANTITY WAS 2 QTS AND TEMPERATURE STAYED IN GREEN BAND. ENGINE WAS SHUT DOWN AND SECURED PER COM PROCEDURES. THE APPROACH AND LANDING WAS UNEVENTFUL. REPLACED NR 2 ENGINE OIL PUMP AND SERVICED WITH OIL. ENGINE RUN AND LEAK CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999032600230 19990326 00230 NM 1999 3 26 SCNA99050 1 19990317 A 3350 900542 BATTERY CHARGER BOEING 727 7272J4 1384006 NM CARGO DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT ON THE AFT CARGO DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REP LACED THE BATTERY CHARGER M957. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1999032600231 19990326 00231 NM 1999 3 26 VNAA9903013 1 19990313 A 5243 001A524A0100014 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYDRAULIC COMPT MISSING A VNAA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 GL 07 459PS 3070 DURING THE INITIAL CLIMB-OUT, THE CREW NOTED A THUMP SOUND AND A SLIGHT VIBRATION ON THE RUDDER PEDALS. NO OTHER INDICA TIONS OF ANYTHING ABNORMAL WERE INDICATED, AND THE FLIGHT CONTINUED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. DURING THE POST FLIGHT INSPECTION, A PORTION OF THE HYDRAULIC SERVICE DOOR WAS NOTED TO BE MISSING FROM THE AIRCRAFT. MAINTENA NCE INSPECTED THE AIRCRAFT FOR ANY FURTHER DAMAGE, AND REPLACED THE HYDRAULIC ACCESS DOOR, IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 06-40-02. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999032600232 19990326 00232 NM 1999 3 26 VNAA9903014 1 19990314 A 5270 869701 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE SERVICE DOOR FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 328JS 3030 DURING CRUISE FLIGHT, A PROXI SYSTEM FAIL WARNING MESSAGE WAS NOTED BY THE CREW. AN EMERGENCY WAS NOT DECLARED, BUT THE CREW REQUESTED EMERGENCY EQUIPMENT UPON ARRIVAL. MX INSPECTED AND REPLACED THE PROXI SWITCH ELECTRONIC CONTROL UNIT, AN D RETURNED THE A/C TO SERVICE. LATER DURING THE SECOND ATTEMPT TO COMPLETE THE FLT, ANOTHER PROXI WARNING MESSAGE ILLUM INATED. THE A/C RETURNED TO PIT FIELD A SECOND TIME. MX INSPECTED AND REPLACED THE SERVICE DOOR OVER CENTER PROXI SWIT CH 4MC, IN ACCORDANCE WITH DORNIER MM 32-61-02. FUNCTION CHECKS, AND AN OPS CHECK FLIGHT, WERE COMPLETED WITH SATISFACT ORY RESULTS. THE A/C WAS THEN RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999032600233 19990326 00233 WP 1999 3 26 CKSA99004 1 19990315 A 2782 BOLTS LKHEED 1011 1011385115 5265015 WP NR 2 LE SLAT ACT SHEARED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING C-CHECK INSPECTION, FOUND LT WING NR 2 SLAT ACTUATOR MOUNT BOLTS, (3 OF 4) SHEARED. FOUND O/B TORQUE TUBE RESTIN G ON TORQUE TUBE GUIDE. REPLACED MOUNT BOLTS IAW MM 27-81-21, REPLACED TORQUE TUBE IAW MM 27-81-18. PERFORMED NDT OF S LAT ACTUATOR MOUNT BRACKET AND ACTUATOR ATTACHMENT TO FRONT SPAR, NO DEFECTS NOTED IAW NON DESTRUCTIVE TECH MANUAL 51-00 -00 PART 6. OPERATIONAL CHECKS GOOD IAW MM 27-81-00. REF GAMCO NRC NR 1020, 1040 AND 1041 FOR DETAILS. FOUND DURING S CHEDULED C-CHECK INSPECTION AT GAMCO, INC. 2 L 7 3 4F A23WE 1999032600234 19990326 00234 WP 1999 3 26 CKSA99005 1 19990315 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP E/E DOORWAY CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 MESC DOOR CUTOUT, BOTTOM AREA SKIN FOUND CRACKED AT 2 LOCATIONS (REFERENCE GAMCO NRC NR 5082). FOUND CRACK TO BE CAUSED BY CORROSION. REMOVED CORROSION AND INSTALLED REPAIR IAW AIA EA L1-53-058 REVISION ORIGINAL DATED 03-02-99. FOUND DUR ING SCHEDULED C-CHECK INSPECTION AT GAMCO, INC. 2 L 7 3 4F A23WE 1999032600235 19990326 00235 WP 1999 3 26 CKSA99006 1 19990315 A 5754 1600901901 SKIN LKHEED 1011 1011385115 5265015 WP NR 1 LE SLAT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 LT WING NR 1 SLAT FOUND CRACKED, I/B LOWER EDGE AREA. REPAIR OF CRACK COMPLIED WITH IAW AIA EA L1-057-058 REVISION ORIG INAL DATED 02-28-99 AND AIA DRAWING AIA/E/2940 REV ORIG DATED 3-1-99. FOUND DURING SCHEDULED C-CHECK INSPECTION AT GAMC O, INC. 2 L 7 3 4F A23WE 1999032600236 19990326 00236 WP 1999 3 26 CKSA99007 1 19990315 A 5754 RIB LKHEED 1011 1011385115 5265015 WP NR 7 LE SLAT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK INSPECTION WORK CARD NR 05-57-1006, FOUND LT SIDE NR 7 LEADING EDGE SLAT RIBS N R 4 AND 21 TO BE CRACKED. REMOVED LT SLAT NR 7 IAW MM 27-81-26, REPAIRED CRACKED RIBS IAW SRM 57-51-00, RE-INSTALLED LT NR 7 SLAT IAW MM 27-81-26. OPS CHECK GOOD IAW MM 27-81-00 PG 6. FOUND DURING SCHEDULED C-CHECK INSPECTION AT GAMCO, I NC. 2 L 7 3 4F A23WE 1999032600237 19990326 00237 WP 1999 3 26 CKSA99008 1 19990315 A 5754 RIB LKHEED 1011 1011385115 5265015 WP NR 4 LE SLAT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND ON LT SIDE, NR 4 L/E SLAT RIBS NR 3 AND 23 TO BE CRACKED. REMOVED NR 4 SLAT, ROUTED TO S/M SHOP IAW MM 27-81-26. S/M REPAIRED CRACKED RIBS IAW SRM 57-51-00. INSTALLED NR 4 SLAT IAW MM 27-81-26. SLAT OPS CHECK SATISFACTORY IAW MM 27-81-00 PARA C. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GAMC O, INC. WORK CARD 57686, C-CHECK CARD 05-57-1006, NON ROUTINE WORK CARD NR 1082. 2 L 7 3 4F A23WE 1999032600238 19990326 00238 WP 1999 3 26 CKSA99009 1 19990315 A 2782 7200113 MOUNT LKHEED 1011 1011385115 5265015 WP NR 2 LE SLAT ACT FAILED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING C-CHECK INSPECTION, FOUND LT WING NR 2 SLAT SCREW JACK SHEARED OFF FROM UPPER MOUNT. REMOVED NR 2 SLAT ACTUATOR IAW MM 27-81-00. DURING INSPECTION, FOUND TORQUE TUBE O/B OF NR 2 SLAT ACTUATOR DAMAGED. REMOVED AND REPLACED IAW MM 2 7-81-18. SLAT ACTUATOR UPPER MOUNT RE-INSTALLED WITH NEW BOLTS IAW MM 27-81-27. RE-INSTALLED NR 2 SLAT ACTUATOR IAW MM 27-81-21. OPS CHECK SATISFACTORY IAW MM 27-81-00. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GAMCO, INC. WO RK CARD 57686, C-CHECK CARD 05-00-1001, NON-ROUTINE WORK CARD NR 1020. 2 L 7 3 4F A23WE 1999032600239 19990326 00239 WP 1999 3 26 CKSA99010 1 19990315 A 5754 SKIN LKHEED 1011 1011385115 5265015 WP NR 3 LE SLAT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING C-CHECK INSPECTION, FOUND LT WING NR 3 SLAT INNER SURFACE CRACKS AT 4 PLACES. TRIMMED OUT CRACK AREA AND REMOVED SMALL NUMBER OF RIVETS TO FACILITATE REPAIR REQUIREMENTS AS PER SRM 51-40-01. FABRICATED REPAIR DOUBLER, TRIMMED TO SI ZE, DEBUR, PRIMED AND TREATED IAW SRM 51-21-02. INSTALLED REPAIR PARTS IN POSITION IAW SRM 57-40-01. REPAIR CARRIED OU T IAW SRM 57-50-01. TOUCH UP PAINT CARRIED OUT IAW MM 20-51-00. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GA MCO, INC. WORK CARD 57686, C-CHECK CARD 05-27-1000, NON-ROUTINE WORK CARD NR 1012. 2 L 7 3 4F A23WE 1999032600240 19990326 00240 WP 1999 3 26 CKSA99011 1 19990315 A 5754 SKIN LKHEED 1011 1011385115 5265015 WP NR 1 LE SLAT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK INSPECTION CARD 57-00-100, FOUND APPROX 4 INCH LONG CRACK AT RT NR 1 SLAT INNER SKIN FW D OF O/B TRACK. CUT OUT DAMAGED AREA AS PER SRM 51-10-04 TO FACILITATE REPAIR REQUIREMENTS. FABRICATE REPAIR DOUBLER, BACK DRILLED AND TRIMMED TO SHAPE REQUIRED AS PER LCP70461046B. RE-PROTECTED SURFACE AREA OF FABRICATED REPAIR DOUBLER AS PER SRM 51-21-02. INSTALLED REPAIR DOUBLER IN POSITION AS PER SRM 51-40-01. FOUND DURING ACCOMPLISHMENT OF SCHEDULE D C-CHECK AT GAMCO, INC. WORK CARD 57686, C-CHECK CARD 57-00-100, NON-ROUTINE WORK CARD NR 2014. 2 L 7 3 4F A23WE 1999032600241 19990326 00241 WP 1999 3 26 CKSA99012 1 19990315 A 5753 SKIN LKHEED 1011 1011385115 5265015 WP NR 2 TE FLAPVANE GROOVED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK, FOUND RT WING NR 2 FLAP VANE LEADING EDGE IS GROOVED 20 I/B FROM VANE O/B END. CUT OU T DAMAGED AREA AS REQUIRED PER SRM 51-53-00 FIG 812. FABRICATED REPAIR DOUBLERS, TRIMMED, DEBUR AND REPROTECTED IAW SRM 51-21-00. INSTALLED REPAIR DOUBLER IN POSITION AS PER SRM 51-40-01. REPAIR CARRIED OUT IAW SRM 57-53-00 FIG 812. FOU ND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GAMCO, INC. WORK CARD 57686, RO 107-307, NON-ROUTINE WORK CARD NR 2084 . 2 L 7 3 4F A23WE 1999032600242 19990326 00242 WP 1999 3 26 CKSA99013 1 19990315 A 5230 1522999101 FITTING LKHEED 1011 1011385115 5265015 WP CARGO DOOR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK, FOUND C2 CARGO DOOR LT STEPPED PANEL SUPPORT FITTING AT FS 1605 CRACKED. REMOVED CRAC K TEE GUIDE SUPPORT BRACKET AS PER SRM 51-40-01. PRE-INSTALLED FABRICATED PARTS TO FACILITATE BACK DRILLING OF EXISTING HOLES AS PER STANDARD SHOP PRACTICES. DEBUR AND PRE-PROTECT PARTS AS PER SRM 51-21-02. INSTALLED FABRICATED PART IN P OSITION AS PER SRM 51-40-01. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GAMCO, INC. WORK CARD 57686, C-CHECK CARD 01-53-1017, NON ROUTINE WORK CARD NR 2093. 2 L 7 3 4F A23WE 1999032600243 19990326 00243 WP 1999 3 26 CKSA99014 1 19990315 A 5230 1514790101 FITTING LKHEED 1011 1011385115 5265015 WP CARGO DOOR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK, FOUND C2 CARGO DOOR LT STEPPED PANEL SUPPORT FITTING AT FS 1565 CRACKED. REMOVED CRAC K TEE GUIDE SUPPORT BRACKET AS PER SRM 51-40-01. PRE-INSTALLED FABRICATED PARTS TO FACILITATE BACK DRILLING OF EXISTING HOLES AS PER STANDARD SHOP PRACTICES. DEBUR AND PRE-PROTECT PARTS AS PER SRM 51-21-02. INSTALLED FABRICATED PART IN P OSITION AS PER SRM 51-40-01. PAINTING CARRIED OUT IAW MM 20-51-11. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GAMCO, INC. WORK CARD 57686, C-CHECK CARD 01-53-1017, NON-ROUTINE WORK CARD NR 4094. 2 L 7 3 4F A23WE 1999032600244 19990326 00244 WP 1999 3 26 CKSA99015 1 19990315 A 5520 DOUBLER LKHEED 1011 1011385115 5265015 WP RT ELEV TIP CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK, FOUND RT ELEVATOR TIP, TOP ON/OFF PLATE CRACKED AND HAVING SHEARED RIVETS. REMOVED CR ACKED DOUBLER ON/OFF PLATE AS PER SRM 51-40-01. FABRICATED REPAIR DOUBLER, DEBUR AND PRE-PROTECT AS PER SRM 51-21-02. I NSTALLED DOUBLER AS PER SRM 51-40-01. REPAIR CARRIED OUT IAW SRM 51-50-02. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C- CHECK AT GAMCO, INC. WORK CARD 57686, C-CHECK CARD 03-55-1004, NON-ROUTINE WORK CARD NR 5008. 2 L 7 3 4F A23WE 1999032600245 19990326 00245 WP 1999 3 26 CKSA99016 1 19990315 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP FUSELAGE CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK INSPECTION, FOUND AFT PRECONDITION AIR CONNECTOR FUSELAGE CUT OUT CRACKED. REMOVED RIV ETS IN REPAIR AREA AS PER SRM 51-40-01. STOP DRILLED END OF CRACK AS PER SRM 51-10-04. FABRICATED REPAIR DOUBLER AS PE R SRM 53-81-20 FIG 828. PRE-PROTECT REPAIR DOUBLER AS PER SRM 51-21-02. REPAIR CARRIED OUT AS PER SRM 53-31-00 FIG 828 . LEAK CHECKED SATISFACTORY IAW MM 21-06-01, PAINT TOUCH UP CARRIED OUT IAW MM 20-51-11. FOUND DURING ACCOMPLISHMENT O F SCHEDULED C-CHECK AT GAMCO, INC. WORK CARD 57686, C-CHECK CARD 01-00-1000, NON-ROUTINE WORK CARD NR 5013. 2 L 7 3 4F A23WE 1999032600246 19990326 00246 WP 1999 3 26 CKSA99017 1 19990315 A 5312 BLKHD STIFFENER LKHEED 1011 1011385115 5265015 WP FWD BULKHEAD CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK INSPECTION, FOUND FWD BULKHEAD RT SIDE I/B STIFFENER BOTTOM CORNER PREVIOUSLY REPAIRED CRACK EXTENDING APPROX 1.5. REMOVED PREVIOUS REPAIR AND TRIMMED OUT PROPAGATED CRACK ON CITED AREA AS PER SRM 51-10-04. REPAIR CARRIED OUT IAW SRM 51-50-02. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GAMCO, INC. WORK CARD 57686 , C-CHECK CARD 01-00-1002, NON-ROUTINE WORK CARD NR 5031. 2 L 7 3 4F A23WE 1999032600247 19990326 00247 WP 1999 3 26 CKSA99018 1 19990315 A 5754 SKIN LKHEED 1011 1011385115 5265015 WP NR 7 LE SLAT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 107CK 193N1182 DURING ACCOMPLISHMENT OF C-CHECK INSPECTION, FOUND CRACK 4 INCHES LONG AT SLAT NR 7 RT I/B UPPER CORNER WITH 4 RIVETS SH EARED. STOP DRILLED CRACK AS PER SRM 51-10-04. FABRICATED REPAIR DOUBLER, BACK DRILLED, TRIMMED AND PRE-PROTECT AS PER SRM 51-21-02. INSTALLED REPAIR DOUBLER INTO POSITION AS PER SRM 51-40-01. REPAIR CARRIED OUT IAW SRM 57-51-00 FIG 807 . TOUCH UP PAINT CARRIED OUT IAW MM 20-51-11. FOUND DURING ACCOMPLISHMENT OF SCHEDULED C-CHECK AT GAMCO, INC. WORK CA RD 57686, C-CHECK CARD 57-00-100-2, NON-ROUTINE WORK CARD NR 2011. 2 L 7 3 4F A23WE 1999032600248 19990326 00248 WP 1999 3 26 TC8A99005 1 19990318 A 2910 LINE DOUG DC8 DC8F54 3021926 WP NR 3 HYD SYST LEAKING A TC8A D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 802CK 45679 NO FLIGHT, RETURN TO RAMP TO SERVICE HYDRAULICS. HYDRAULICS DROPPED APPROXIMATELY 5 GALLONS ON TAXI OUT. SERVICED HYDR AULICS, FIXED LEAK ON NR 3 ENGINE. 2 L 7 4 4F 4A25 1999032600249 19990326 00249 NM 1999 3 26 SWAA990526 1 19990316 A 3350 6042221 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULE SERVICE CHECK, FOUND FWD CABIN EMERGENCY TRACK LIGHTING INOP. REMOVED AND REPLACED CABIN FWD CABIN EMER GENCY TRACK LIGHT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999032600250 19990326 00250 NM 1999 3 26 SWAA990527 1 19990316 A 3350 BR9293 COVER BOEING 737 7373H4 1384600 NM ROW 12C CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED BC4 CHECK, FOUND 12-C FLOOR PROX LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999032600251 19990326 00251 NM 1999 3 26 SWAA990528 1 19990316 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 12-17 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY TRACK LIGHTS OUT AT ROW 12-17. REPAIRED LOOSE WIRE PER MM. 2 L 7 2 4F RT A16WE 1999032600252 19990326 00252 NM 1999 3 26 SWAA990529 1 19990316 A 5311 6546536 FRAME BOEING 737 7373A4 1384585 NM BS 629 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME CRACKED AT BOTTOM RIVET FWD SIDE OF LT BS 629, WL 202. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999032600253 19990326 00253 NM 1999 3 26 SWAA990530 1 19990317 A 2612 6558234 FIRE LOOP BOEING 737 7372H4 138448C NM NR 1 ENGINE SHORTED A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 61SW 21970 AIR TURNBACK DUE TO LEFT FIRE LIGHT ILLUMINATED ON CLIMB-OUT. AFTER LEFT OVERHEAT DETECTOR SWITCH WAS MOVED TO FIRE, TH E LIGHT WENT OUT. ON ENGINES SHUT DOWN THE PROBLEM STILL EXISTED. REMOVED AND REPLACED NR 1 ENG LOWER FIRE LOOP PER MM . 2 L 7 2 4F A16WE 1999032600254 19990326 00254 NM 1999 3 26 SWAA990531 1 19990317 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT OVERWING DOORS INOP. REMOVED AND REPLACED BATTER Y PACK PER MM. 2 L 7 2 4F A16WE 1999032600255 19990326 00255 NM 1999 3 26 SWAA990532 1 19990317 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED 1/4D CHECK, FOUND THROUGH EDDY CURRENT INSPECTION A CRACK INDICATION ON UPPER HINGE CUTOUT ON L-1 DOOR. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999032600256 19990326 00256 NM 1999 3 26 SWAA990533 1 19990317 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND 4 STRINGER CLIPS CRACKED AT BS 663, STR 12R AND 10L, BS 767, STR 13R, AND BS 787, STR 11L. REMOVED AND REPLACED CLIPS PER SRM. 2 L 7 2 4F RT A16WE 1999032600257 19990326 00257 NM 1999 3 26 SWAA990534 1 19990317 A 3350 OL3071BPEGPL BULB BOEING 737 7373H4 1384600 NM ROW 4 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHT INOP AT FWD, AFT AND ROW 4 SECTIONS. REMOVED AND REPLACED BULB PER M M. 2 L 7 2 4F RT A16WE 1999032600258 19990326 00258 NM 1999 3 26 SWAA990535 1 19990317 A 5312 6516300 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING SCHEDULED 1/2D CHECK, FOUND THROUGH EDDY CURRENT INSPECTION A .25 INCH CRACK AT BULKHEAD BS 178 WEB, LBL 12, WL 2 34. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 1999032600259 19990326 00259 NM 1999 3 26 SWAA990536 1 19990318 A 5320 BAC1498 CHANNEL BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED U-CHANNEL AT STR 15L, BS 360. REPAIRED CHANNEL PER SRM. 2 L 7 2 4F RT A16WE 1999032600260 19990326 00260 NM 1999 3 26 SWAA990537 1 19990318 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 927-395 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C4 CHECK, FOUND 2 CRACKS ON FUSELAGE SKIN APPROX 3 INCHES LONG, BS 927 STR 25L AND BS 935, STR 24L. RE PAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999032600261 19990326 00261 NM 1999 3 26 SWAA990538 1 19990318 A 3350 3051F BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 646SW 28331 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY BULL NOSE LIGHT OUT. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999032600262 19990326 00262 NM 1999 3 26 SWAA990539 1 19990318 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1020 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SKIN AROUND 4 FASTENERS UNDERNEATH DATA PLATE, BS 1020 BETWEEN STR 27L-2 7R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999032600263 19990326 00263 WP 1999 3 26 TWAA9904201 1 19990320 A 3330 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 16-23 DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 958U 49703 THE CABIN EGRESS LIGHTS AT ROWS 16 TO 23 STAYED ON AND WOULD NOT RESET. REPLACED THE BATTERY PACK. CHECK-C 9-30-98 STL . 2 L 7 2 4F A6WE 1999032600264 19990326 00264 WP 1999 3 26 TWAA9904202 1 19990310 A 5620 WINDOW DOUG DC9 DC931 3022065 WP CABIN DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CABIN WINDOW NR 36 ON RT SIDE WITH STATIC BURN AT AFT EDGE AND FWD EDGE. BLENDED PER SR M 53-05 FIG 3 NUMBER 25 AND 26 CASE 2. INSTALLED DOUBLER PER DRAWING SRO9530053 AND ARA 16105. 2 L 7 2 4F A6WE 1999032600265 19990326 00265 WP 1999 3 26 TWAA9904203 1 19990311 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 980 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND AT STA 980 LT AFT LAV AREA, CORROSION AROUND FASTENER HOLE ON TOP OF FLOOR SUPPORT, LBL 19 IN. REMOVED CORROSION AS NECESSARY PER TWA SPM 6-80-01 PAGE 1. REPAIRED FLOOR SUPPORT PER SRM 53-05 PAGE 31. 2 L 7 2 4F A6WE 1999032600266 19990326 00266 WP 1999 3 26 TWAA9904204 1 19990313 A 5320 CASTING DOUG DC9 DC931 3022065 WP BS 737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND AT STA 737 BETWEEN WING CENTER SECTION AND FLOOR LINE CASTING WAS CRACKED, ALSO 3 INCHES I/B OF CASTING, ON RT SIDE. INSTALLED NEW FRAME PER SERVICE BULLETIN 53-131. 2 L 7 2 4F A6WE 1999032600267 19990326 00267 WP 1999 3 26 TWAA9904205 1 19990313 A 5320 CASTING DOUG DC9 DC931 3022065 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND CASTING AT STA 756 LONGERON 20R TO 21R WAS CRACKED. REPLACED FRAME PER SERVICE BULLETIN 53-168. 2 L 7 2 4F A6WE 1999032600268 19990326 00268 WP 1999 3 26 TWAA9904206 1 19990315 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 617 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 FOUND LONGERON 7R CRACKED AT STA 617, .375 INCH OUT OF BOLT HOLE. REMOVED CRACKED LONGERON FROM STA 610R TO 644R. REPA IRED PER SRM 53-2 FIG 18 AND STANDARD PRACTICES. CHECK-C 8-25-98 STL. 2 L 7 2 4F A6WE 1999032600269 19990326 00269 WP 1999 3 26 TWAA9904207 1 19990315 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 220-228 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND SKIN DENTED AND GOUGED STA 220 TO 228, L5L TO JUST BELOW L7L. INSTALLED DOUBLER REPAIR PER SRM 53-04, FIG 12B SHEET 7. 2 L 7 2 4F A6WE 1999032600270 19990326 00270 WP 1999 3 26 AT9900232 1 19990315 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 235 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A GOUGE IN DENT AT BS 235 L-18L OUT OF LIMITS. FABRICATED EXTERNAL AND IN TERNAL FINGER DOUBLER AND DOUBLER, DRILLED AND TRIMMED DOUBLERS, ALODINED, PRIMED AND INSTALLED DOUBLERS WITH WET SEALAN T IAW DC9 SRM 51-10-4, 53-04 FIG 38, 51-10-3, 51-30-2, 51-30-5 AND RES NR 99614. 2 L 7 2 4F A6WE 1999032600271 19990326 00271 WP 1999 3 26 AT9900233 1 19990318 A 5260 FITTING DOUG DC9 DC932 3022066 WP VENTRAL STAIR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT VENTRAL STAIRS LOWER LEFT HAND SIDE CORNER FITTING CORRODED THROUG H OUT. REMOVED AND REPLACED CORRODED AND CRACKED VENTRAL STAIRS LEFT HAND SIDE CORNER FITTING IAW DC9 SRM 51-10-4, 51-1 0-3, 51-10-5 AND 51-30-2. 2 L 7 2 4F A6WE 1999032600272 19990326 00272 WP 1999 3 26 AT9900234 1 19990314 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 865-929 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE WEB AT BS 865 TO 929 L-18R CORRODED. CUT OUT CORRODED AREA, FABRICATE D AND INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 51-30-1, 51-10-3, 53-20-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999032600273 19990326 00273 NM 1999 3 26 AT9900235 1 19990208 A 5321 FLOOR BOEING 737 7372L9 1384497 NM BS 907-927 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO COMPARTMENT CABIN FLOOR PANEL (E17) LOWER SURFACE AT BS 907 TO 927 RBL 49 CORRODED. FABRICATED PANEL DUE TO EXTENSIVE CORROSION AND BREAKAGE IAW B737 53-20-1 AND 51-40-10 PG 4. 2 L 7 2 4F RT A16WE 1999032600274 19990326 00274 NM 1999 3 26 AT9900236 1 19990227 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 987-1006 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT LAVATORY WALL SUPPORT AT BS 987 TO 1006 LBL 18 TO 43 CORRODED. FA BRICATED REPAIR SUPPORT AND TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-40-3, 51-10-1, 51-10-2, 51-30-2 AND MM 51-21-2 1. 2 L 7 2 4F RT A16WE 1999032600275 19990326 00275 SO 1999 3 26 COMA9910043 1 19990318 A 3310 70LIN056F103W RHEOSTAT EMB 120 EMB120RT SO INSTRUMENT PANEL INOPERATIVE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 263CA 120255 OVERHEAD PANEL LIGHT IS INOPERABLE. REPLACED RHEOSTAT. 2 L 7 2 4T RT A31SO 1999032600276 19990326 00276 EA 1999 3 26 COMA9960119 1 19990313 A 2750 601R93106105 FLEXSHAFT CNDAIR CL600 CL6002B19 EA LT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 LEFT WING NR 1 FLEXSHAFT UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED LEFT WING NR 1 FLAP FLEXSHAFT. 2 L 7 2 4F RT A21EA 1999032600277 19990326 00277 EA 1999 3 26 COMA9960120 1 19990314 A 2710 601R130011 AILERON CNDAIR CL600 CL6002B19 EA LEFT WING WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 LEFT AILERON NEEDS TO BE REPLACED DUE TO FAILING THE BACKLASH CHECK. REPLACED LEFT AILERON. 2 L 7 2 4F RT A21EA 1999032600278 19990326 00278 EA 1999 3 26 COMA9960121 1 19990314 A 2710 601R130002 AILERON CNDAIR CL600 CL6002B19 EA RIGHT WING WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 RIGHT AILERON NEEDS TO BE REPLACED DUE TO FAILING THE BACKLASH CHECK. REPLACED RIGHT AILERON. 2 L 7 2 4F RT A21EA 1999032600279 19990326 00279 NM 1999 3 26 UPS99229064 1 19990319 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, EMERG LIGHT BY COCKPIT DOOR INOP. REPLACED BATTERY PACK, OPS CK GOOD (P/N 96-2-1015). 2 L 7 3 4F A3WE 1999032600280 19990326 00280 NM 1999 3 26 UPS99229065 1 19990319 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 11 DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, EEL EXIT LIGHT LT CEILNG ROW 11. REPLACED BATT PACK, OPS CHK GOOD. (P/N 96-2-1024). 2 L 7 3 4F A3WE 1999032600281 19990326 00281 NM 1999 3 26 UPS99429066 1 19990321 A 5313 BAC15171571 STRINGER BOEING 747 747212B 1384886 NM BS 260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE-N/A, S41 HAS 3 INCH CRACK AT STATION 260 RIGHT SIDE NOSE WHEEL WELL BOX WHERE IT ATTACHES TO CLIP. REMO VED CRACKED STRINGER, FABED NEW PART, INSTALLED APPLIED SEALANT PER EO 8934 D. 2 L 7 4 4F A20WE 1999032600282 19990326 00282 NM 1999 3 26 UPS99429067 1 19990321 A 2761 33206001 ACTUATOR BOEING 747 747212B 1384886 NM NR 6 SPOILER FAILED A IPXA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE-2ACK, NR 6 SPOILER ACTUATOR ROD BROKEN. THIS DISCREPANCY FOUND WHEN SPOILER LOCKS WERE INSTALLED FOR SC HEDULED 2A CHECK. WHEN HYDRAULIC PRESSURE WAS PUT ON SYSTEM, ACTUATOR ROD FAILED. SUSPECT THAT THE ROD HAD A PRE-EXIST ING CRACK. SPOILER ACTUATOR WAS REMOVED AND REPLACED PER M/M 27-62-00. 2 L 7 4 4F A20WE 1999032600283 19990326 00283 WP 1999 3 26 UPS99829059 1 19990311 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 1300 AT RBL 36, THE FLOORBEAM HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 808-576. 2 L 7 4 4F RT 4A25 1999032600284 19990326 00284 WP 1999 3 26 UPS99829060 1 19990222 A 5320 97540241 FITTING DOUG DC8 DC873F 302199F WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, FLOORBEAM SUPPORT FITTING AT STA 280 RT SIDE IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 975 4024 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600285 19990326 00285 WP 1999 3 26 UPS99829061 1 19990305 A 5320 3750545502 FITTING DOUG DC8 DC873F 302199F WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 1040 TO 1060 AT STR 35R, THE STR SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600286 19990326 00286 WP 1999 3 26 UPS99829062 1 19990222 A 5320 4751642 FITTING DOUG DC8 DC873F 302199F WP BS 798 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 798 AT STR 13L, THE TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751642 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600287 19990326 00287 WP 1999 3 26 UPS99829063 1 19990223 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1036 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 1036 RBL 24, THE SEAT TRACK HAS HEAVY CORROSION, ALSO AT STA 990. REMOVED AND REPLACED SEAT T RACK FROM STA 990 TO 1050 IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 1999032600288 19990326 00288 WP 1999 3 26 UPS99829068 1 19990311 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, FUSELAGE SKIN (EXT) AT STA 660 BETWEEN STR 35L-36 IS CORRODED. REPAIRED AREA IAW DH SK 808-237. 2 L 7 4 4F RT 4A25 1999032600289 19990326 00289 WP 1999 3 26 UPS99829069 1 19990308 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1340-1360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 1340 TO 1360 AT RBL 59, THE SEAT TRACK IS CORRODED OUT OF LIMITS. REPAIRED AREA IAW SRM 53-2- 3. 2 L 7 4 4F RT 4A25 1999032600290 19990326 00290 WP 1999 3 26 UPS99829070 1 19990311 A 5320 37540251 FITTING DOUG DC8 DC873F 302199F WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, FLOORBEAM SUPPORT BACK-UP FITTING AT STA 280 AT STR 27R IS CRACKED. REMOVED, FABRICATED AND REPLA CED FITTING IAW DWG 3754025 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600291 19990326 00291 WP 1999 3 26 UPS99829071 1 19990223 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 1480 AT BL 0, THE SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 1999032600292 19990326 00292 WP 1999 3 26 UPS99829072 1 19990307 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 150-180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 150 TO 180 RBL 30, THE SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 1999032600293 19990326 00293 WP 1999 3 26 UPS99829073 1 19990224 A 5720 3704841502 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, THE NR 3 MAIN TANK I/B SIDE OF THE XRS74 RIB, THE STR 51 FWD END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600294 19990326 00294 WP 1999 3 26 UPS99829074 1 19990223 A 5320 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 630 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 630 AT RBL 59, THE SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-7-3 FIG 2. 2 L 7 4 4F RT 4A25 1999032600295 19990326 00295 WP 1999 3 26 UPS99829075 1 19990311 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, STA 879 AT LBL 60, THE PRESSURE WEB IS CORRODED. REPAIRED AREA IAW DK SK808-444. 2 L 7 4 4F RT 4A25 1999032600296 19990326 00296 EU 1999 3 26 QXEA9900503 1 19990317 A 3350 CONNECTOR GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 12,13 & 14 DIRTY A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 SEA - ON APU SHUTDOWN ROW 12, 13 AND 14 FLOOR PROXIMITY LIGHTING CAME ON. MAINTENANCE CLEANED THE CANNON PLUG AT THE PO WER SUPPLY ROW 14. ALSO, FOUND THE CANNON PLUG AT ROW 9 LOOSE. RECONNECTED PLUG AND OPERATIONALLY TESTED, SYSTEM NORMA L. 2 L 7 2 4F RT A20EU 1999032600297 19990326 00297 EU 1999 3 26 QXEA9900504 1 19990317 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 & 9 INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 488US 11240 PDX - EXIT SIGN IN CENTER AISLE AT ROWS 8 AND 9 HAS SOME LIGHTS THAT ARE INOPERATIVE. MAINTENANCE REPLACED THE SIGN ASS EMBLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1999032600298 19990326 00298 NM 1999 3 26 99FDEA00109 1 19990319 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1148-1183 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 636 - WHILE WORKING NR 620 FOUND STR 20 LEFT BS 1148-1183 CORRODED ON OTBD SURFACE FROM 1170-1178. REMOVED STR 20 BS 1148-1183, FABRICATED AND INSTALLED NEW STR (LT) IAW FEDEX SRM 51-10-1, 51-30-2, FEDEX MM 51-20-151 AND FEDEX EA 7-5100 -44396. 2 L 7 3 4F A3WE 1999032600299 19990326 00299 NM 1999 3 26 99FDEA00110 1 19990322 A 5320 65405101 SILL BOEING 727 72722C 138400F NM BS 440-660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 UPON REMOVAL OF SEAT TRACK ON NR 313 FOUND CORROSION ON MCD SILL CHORD AT BS 440 TO 660 LBL 65 WL 208.1. 2 L 7 3 4F A3WE 1999032600300 19990326 00300 NM 1999 3 26 99FDEA00111 1 19990322 A 5320 65405102 WEB BOEING 727 72722C 138400F NM BS 480-620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 UPON REMOVAL OF SEAT TRACK ON NR 313 FOUND MCD LWR VERTICAL WEB TO BE CORRODED FROM BS 480 TO 620, WL 200 TO 208, LBL 65 . 2 L 7 3 4F A3WE 1999032600301 19990326 00301 WP 1999 3 26 ABXA9900222 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 779.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT STATION FS 779.250. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600302 19990326 00302 WP 1999 3 26 ABXA9900223 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 810 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT STATION FS 810.00. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600303 19990326 00303 WP 1999 3 26 ABXA9900224 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 816.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT STATION FS 816.250. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600304 19990326 00304 WP 1999 3 26 ABXA9900225 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 822.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT STATION FS 822.500. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600305 19990326 00305 WP 1999 3 26 ABXA9900226 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 828.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT STATION 828.750. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600306 19990326 00306 WP 1999 3 26 ABXA9900227 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 835 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT STATION FS 835. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999032600307 19990326 00307 WP 1999 3 26 ABXA9900228 1 19990318 A 7931 1G1741A SWITCH DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 1 OIL PRESS DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 817AX 45928 669228 NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED DURING CRUISE. OIL PRESSURE GAUGE READ 50 PSI. REDUCED POWER, NO HELP. SEC URED ENGINE IAW DC8, OPS MANUAL. REPLACED NR 1 ENGINE OIL LOW PRESSURE SWITCH AND MAIN ENGINE OIL FILTER. LEAK AND OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1999032600308 19990326 00308 WP 1999 3 26 ABXA9900229 1 19990215 A 5320 5769210 ANGLE DOUG DOUG DC8 DC863 302198A WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 FORWARD CARGO PIT L-ANGLE AT UPPER SIDEWALL AND LOWER SIDEWALL ATTACHMENT WAS CRACKED. REPAIRED IAW DC8 SRM 51-2-0 AND 51-1-12. 2 L 7 4 4F 4A25 1999032600309 19990326 00309 WP 1999 3 26 ABXA9900230 1 19990215 A 5730 57696009 SKIN DOUG DOUG DC8 DC863 302198A WP WS 710 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LEFT WING OUTBOARD LEADING EDGE SKIN CRACKED AT STATION FS 710. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999032600310 19990326 00310 WP 1999 3 26 ABXA9900231 1 19990216 A 5730 9751896401 SKIN DOUG DOUG DC8 DC863 302198A WP WS 920 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 LEFT WING LEADING EDGE HAD EXFOLIATED UPPER SURFACE INBOARD OF TIP AT STATION FS 920. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999032600311 19990326 00311 WP 1999 3 26 ABXA9900232 1 19990217 A 5320 575083766 SHEAR TIE DOUG DOUG DC8 DC863 302198A WP BS 641 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 SHEAR TIE CRACKED AT STATION 641 BETWEEN STATION 26 RIGHT AND 27 RIGHT. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999032600312 19990326 00312 WP 1999 3 26 ABXA9900233 1 19990218 A 5210 5615403 SKIN DOUG DOUG DC8 DC863 302198A WP PASSENGER DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 PANEL AROUND LOWER HINGE ARM ON FORWARD ENTRY DOOR WAS CRACKED. REPLACED PANEL IAW DC8 SRM 52-3-1 AND SRM 51-1-8. 2 L 7 4 4F 4A25 1999032600313 19990326 00313 WP 1999 3 26 MWEA99101 1 19990319 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP ROW 5-11 DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 212ME 47701 DURING 10 MINUTE BURN TEST RT EXTERIOR NACELLE EMERGENCY LIGHTS FAILED AND THE OVERHEAD EMERGENCY LIGHT BETWEEN ROWS 5 A ND 11 WERE EXTREMELY DIM. MTC REMOVED AND REPLACED NICAD BATTERIES AND EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1999032600314 19990326 00314 NM 1999 3 26 VNAA9903015 1 19990316 A 2130 22260A020201 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FLIGHT DECK FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 427JS 49848 24365 3039 THE AIRCRAFT FAILED TO PRESSURIZE IN AUTO OR MANUAL MODES WHEN SELECTED. DURING THE CLIMB PHASE OF THE FLIGHT. THE AIR CRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRC RAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FERRY FLIGHT WAS CARRIED OUT WITHOUT ANY FURTHER PROBLEMS. PIT MAINTENA NCE INSPECTED AND REPLACED THE PRESSURIZATION CONTROL PANEL, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-31-01. OP ERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999032600315 19990326 00315 NM 1999 3 26 VNAA9903016 1 19990317 A 2121 011390500 FAN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 07 426JS 49675 3038 DURING CLIMB AFTER TAKEOFF, THE CREW SMELLED AND NOTED SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED, AND THE AIRCRAF T RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND FOUND THE FORWARD RECIRC FAN TO BE INOPERATIVE. MAINTENANCE DEFERRE D THE FORWARD RECIRC FAN, PER THE MINIMUM EQUIPMENT LIST, AND RETURNED THE AIRCRAFT TO SERVICE. ON MARCH 19, 1999 MAINT ENANCE REPLACED THE FORWARD RECIRC FAN, PER DORNIER MAINTENANCE MANUAL 21-11-01. THE DEFERRAL WAS REMOVED AND THE AIRCR AFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999032600320 19990326 00320 NM 1999 3 26 99ZZZX1067 1 19990203 A 2434 ALV8421 ALTERNATOR PIPER PA60 PA60600 7106001 NM LT ENGINE FAILED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 90349 750101850812 600202090 LOST BOTH ALTERNATORS GOING INTO PORTLAND, MAINE. FOUND LEFT ALTERNATOR SHORTED CAUSING RT ALTERNATOR TO KICK OFF-LINE. REMOVED AND REPLACED LEFT ALTERNATOR. OPS CHECKS GOOD. 1 M 7 2 3O RT A17WE 1999032600366 19990326 00366 SO 1999 3 26 99ZZZX1113 2 19990223 A 7314 6467681A PUMP CESSNA 210 210N 2073453 CE CONT O520 IO520L 17032 SO FUEL SYSTEM FAILED A FPIA O OTHER O OTHER NR NOT REPORTED 1 SO 15 6490N 403 G149816BR 21063064 294924R WHEN ENGINE WAS BROUGHT BACK TO IDLE ON LANDING, ENGINE QUIT. 1 H 7 1 3O 3 O 3A21 E5CE 1999032600369 19990326 00369 SO 1999 3 26 99ZZZX1116 2 19990223 A 7314 6467681A1 PUMP CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO FUEL SYSTEM FAILED A FPIA O OTHER O OTHER NR NOT REPORTED 1 SO 15 6622N 130 F159809BK 21063125 294003R UNABLE TO TURN FUEL PRESSURE DOWN. UNABLE TO REGULATE PRESSURE. 1 H 7 1 3O 3 O 3A21 E8CE 1999032600376 19990326 00376 NM 1999 3 26 TWAA9904301 1 19990322 A 3350 LIGHT BOEING 767 7673Y0 NM ROW 23 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 THE CABIN EGRESS LIGHTS WERE INOPERATIVE ON THE LT SIDE OF THE AIRCRAFT, FROM THE NUMBER 2 DOOR TO ROW 23. RECONNECTED WIRE TO EGRESS LIGHT AT ROW 24, LT SIDE. CHECK-C 3-3-99 LAX. 2 L 7 2 4F RT A1NM 1999032600377 19990326 00377 WP 1999 3 26 TWAA9904302 1 19990315 A 5320 CASTING DOUG DC9 DC931 3022065 WP BS 658 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND FORMER CASTING CRACKED AT STA 658, APPROXIMATELY 58 IN RBL. REPLACED FORMER PER SPM 6-7 0-01, PAGE 3, ITEM 13. 2 L 7 2 4F A6WE 1999032600378 19990326 00378 WP 1999 3 26 TWAA9904303 1 19990316 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 150-160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND GALLEY FLOOR DRAIN ATTACH ANGLE CORRODED AT BOTTOM OF ANGLE, LOCATED STA 150 TO 160. SA NDED AND POLISHED CORRODED ATTACH ANGLE PER SPM 6-80-01, PAGE 1 AND REPLACED ATTACH ANGLE PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999032600379 19990326 00379 NM 1999 3 26 AT9900237 1 19990209 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 1006 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE CABIN FLOORBEAM ON UPPER FLANGE CORRODED AT BS 1006 LBL18 TO 28. REMO VED AFT CABIN FLOOR STRUCTURE, FABRICATED WEBS, FLOORBEAMS, ANGLE SUPPORTS, DOUBLER AND INSTALLED IAW B737 SRM 53-10-9, 51-30-2, 51-40-2, MM 51-21-31, AND RES NR 99401. 2 L 7 2 4F RT A16WE 1999032600380 19990326 00380 NM 1999 3 26 AT9900238 1 19990209 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 957 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE CABIN FLOOR SUPPORT AT BS 957 RBL9 TO 46 CORRODED. CLEANED CORROSION, REMOVED SUPPORTS FOR REPAIR, FABRICATED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-40-4. 2 L 7 2 4F RT A16WE 1999032600381 19990326 00381 NM 1999 3 26 AT9900239 1 19990209 A 5320 WEB BOEING 737 7372L9 1384497 NM BS 987-1006 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CABIN FLOOR WEB AROUND THE AFT LAVATORY WATER FITTING BETWEEN BS 987 TO 10 06 LBL 42 CRACKED AND CORRODED. REMOVED THE AFT LAVATORY DRAIN ASSEMBLY, MECHANICALLY REMOVED CORROSION, FABRICATED WEB , TREATED, PRIMED, AND INSTALLED REPAIR WEB AND AFT LAVATORY DRAIN ASSEMBLY IAW B737 SRM 51-10-6, 53-10-1, 51-30-2, 51-4 0-2, AND MM 51-20-11. 2 L 7 2 4F RT A16WE 1999032600382 19990326 00382 NM 1999 3 26 AT9900240 1 19990211 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 328-344 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LONGITUDINAL FLOOR SUPPORT AT BS 328 TO 344 RBL 12 CORRODED. REMOVED FLOOR SUPPORT, FORMED SUPPORT, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW B737 SRM 53-10-2 FIG 7, 51-10-3 AND 51-40-3. 2 L 7 2 4F RT A16WE 1999032600383 19990326 00383 NM 1999 3 26 AT9900241 1 19990211 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 312-360 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SEAT TRACK AT BS 312 TO 360 RBL 50.5 CORRODED. REMOVED CABIN SEAT TRA CK, FABRICATED REPAIR, TREATED, PRIMED, AND INSTALLED IAW B737 SRM 53-10-5 FIG 2 AND 51-30-2. 2 L 7 2 4F RT A16WE 1999032600384 19990326 00384 NM 1999 3 26 AT9900242 1 19990211 A 5320 SUPPORT BOEING 737 7372L9 1384497 NM BS 294-312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LONGITUDINAL FLOOR SUPPORT AT BS 294 TO 312 LBL 12 EXFOLIATED. REMOVE D STRAP AND TWO FLOOR SUPPORT, FORMED SUPPORTS AND STRAP, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW B737 51-4 0-3, 53-10-2 AND MM 51-10-2. 2 L 7 2 4F RT A16WE 1999032600385 19990326 00385 NM 1999 3 26 AT9900243 1 19990211 A 5320 CLIP BOEING 737 7372L9 1384497 NM BS 267 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FLOORBOARD SUPPORT CLIP AND FORMER FLANGE AT BS 267 RBL 3 CORRODED. REMOV ED FASTENERS, FABRICATED ANGLE, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-40-3, 51-30-2, AND 51- 10-6. 2 L 7 2 4F RT A16WE 1999032600386 19990326 00386 NM 1999 3 26 AT9900244 1 19990211 A 5320 ANGLE BOEING 737 7372L9 1384497 NM BS 306 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD LAVATORY WALL ATTACH ANGLE AT BS 306 LBL 12 TO 45.5 CORRODED. REMOVED AND FABRICATED ANGLE, ALODINED, PRIMED AND INSTALLED IAW B737 SRM 51-30-2, 53-10-1, 51-10-6, 51-40-3, 51-10-2 A ND MM 51-4-31. 2 L 7 2 4F RT A16WE 1999032600387 19990326 00387 NM 1999 3 26 AT9900245 1 19990211 A 5320 FITTING BOEING 737 7372L9 1384497 NM BS 312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE GIRT BAR ATTACH FITTING AT BS 312 LBL 52.5 CORRODED. REMOVED CORROSIO N, FABRICATED REPAIR ANGLE, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW B737 51-40-4, 51-10-2, 51-30-2 AND 51-2 0-11. 2 L 7 2 4F RT A16WE 1999032600388 19990326 00388 NM 1999 3 26 AT9900246 1 19990213 A 5321 FLOOR BOEING 737 7372L9 1384497 NM PASSENGER CABIIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOORBOARDS NR 2 AND 7 IN PASSENGER CABIN CORRODED AND WITH EXCESSIVE DAMAGE. REMOVED FLOORBOARDS AND FABRICATED NEW PANEL IAW B737 SRM 53-20-1, 51-40-10 PG 4 AND 53-20-2. 2 L 7 2 4F RT A16WE 1999032600389 19990326 00389 WP 1999 3 26 AT9900247 1 19990315 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-399 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT SIDE FUSELAGE SKIN WITH NUMEROUS DENTS, CREASES AND REPAIRS THAT ARE TO CLOSE TO EACH OTHER AT BS 229 TO 399 L18 TO 26R. REMOVED AND REPLACED SKIN SECTION IAW DC9 SRM 51-30-2, 51-10-3 , 51-10-4, AND RES NR 99583 AND NR 99589. 2 L 7 2 4F A6WE 1999032600390 19990326 00390 WP 1999 3 26 AT9900248 1 19990221 A 5313 52777922 LONGERON DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LONGERON IN THE FORWARD PIT AT BS 218L-23L CORRODED. REMOVED CUT OUT CORR ODED SECTION, FABRICATED REPAIR LONGERON SPLICES AND INSTALLED IAW DC9 SRM 51-30-2, 51-30-5 AND 53-02 FIG 18. 2 L 7 2 4F A6WE 1999032600391 19990326 00391 NM 1999 3 26 CALA9900294 1 19990318 A 5530 BOLTS BOEING 727 727232 1384082 NM VERT STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND VERTICAL STABILIZER TENSION TIE BOLTS (8) PITTED AND CORRODED. THE TENSION TIE BOLTS WERE REMOVED AND REPLACED IAW MM 55-30-51, PAGE 406-408. 2 L 7 3 4F A3WE 1999032600392 19990326 00392 NM 1999 3 26 CALA9900295 1 19990318 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1164 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND STRINGER 28R CORRODED AT BS 1164. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF ST RINGER WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1999032600393 19990326 00393 NM 1999 3 26 CALA9900296 1 19990318 A 5720 STIFFENER BOEING 727 727232 1384082 NM WS 249 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND STIFFENER CORRODED AT RT WING FRONT SPAR FS 249. THE CORRODED SECTION OF STIFFENER WAS REMOVED AND A N EW SECTION WAS INSTALLED IAW SRM 51-30-02, PAGE 4. 2 L 7 3 4F A3WE 1999032600394 19990326 00394 NM 1999 3 26 CALA9900297 1 19990319 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND FLOORBEAM CORRODED AT STA 294 FROM LBL 32 TO LBL 51. A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999032600395 19990326 00395 NM 1999 3 26 CALA9900298 1 19990319 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM L1 DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FORWARD ENTRY DOOR (L-1) Z-CHANNEL CORRODED. A NEW SECTION OF Z-CHANNEL WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999032600396 19990326 00396 NM 1999 3 26 CALA9900299 1 19990319 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 967, RBL 4. THE CORRODED AREA WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999032600397 19990326 00397 NM 1999 3 26 CALA9900300 1 19990321 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 330-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND NR 3 SEAT TRACK IN NR 2 GALLEY AREA CORRODED FROM STA 330 TO 360. A NEW SEAT TRACK WAS INSTALLED IAW S RM 53-00-52, FIGURE 202. 2 L 7 2 4F RT A16WE 1999032600398 19990326 00398 NM 1999 3 26 CALA9900301 1 19990321 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FLOORBEAM CAP IN FORWARD GALLEY AREA CORRODED AT STA 328. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53- 10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999032600399 19990326 00399 WP 1999 3 26 CALA9900302 1 19990320 A 5280 SKIN DOUG DC10 DC1030 3023501 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A .75 INCH CRACK IN LT MLG DOOR SKIN. REPAIRED IAW SRM 53-00-01. 2 L 7 3 4F A22WE 1999032600400 19990326 00400 NM 1999 3 26 CALA9900303 1 19990322 A 5755 651734866 PANEL BOEING 727 727232 1384082 NM NR 8 SPOILER BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND RT WING NR 8 SPOILER OUTBOARD AREA BENT UP. THE SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-62-1. 2 L 7 3 4F A3WE 1999032600401 19990326 00401 NM 1999 3 26 CALA9900304 1 19990322 A 3350 1000679 LIGHT GRIMES BOEING 727 727232 1384082 NM PASSENGER DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND O PERATION CHECKED GOOD IAW MM 33-50-00. 2 L 7 3 4F A3WE 1999032600402 19990326 00402 NM 1999 3 26 CALA9900305 1 19990322 A 5755 651734855 SKIN BOEING 727 727232 1384082 NM NR 9 SPOILER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77780 20635 INSPECTION FOUND RT WING NR 9 SPOILER DENTED ON LOWER END. THE NR 9 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1. 2 L 7 3 4F A3WE 1999032600403 19990326 00403 SO 1999 3 26 COMA9910044 1 19990321 A 6120 78249046 PCU EMB 120 EMB120RT SO RT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 267CA 12744 16 120259 RIGHT HAND PROPELLER OVER SPEED TO 103 DEGREES. REPLACED THE PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A31SO 1999032600404 19990326 00404 SO 1999 3 26 COMA9910045 1 19990319 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 8 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 257CA 120248 EMERGENCY EXIT SIGN AT ROW 8 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999032600405 19990326 00405 EA 1999 3 26 COMA9960122 1 19990321 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LEFT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 951CA 6817 7091 PILOTS WINDSHIELD SHATTERED DURING FLIGHT. REPLACED WINDSHEILD. 2 L 7 2 4F RT A21EA 1999032600406 19990326 00406 EA 1999 3 26 COMA9960123 1 19990321 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA ROW 4-5 FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931CA 7037 EMERGENCY LIGHTS ARE INOPERABLE BETWEEN ROWS 4 AND 5. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999032600407 19990326 00407 EA 1999 3 26 COMA9960124 1 19990320 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 716CA 7250 CABIN DOOR WARNING. ADJUSTED DOOR LATCHING MECHANISM. 2 L 7 2 4F RT A21EA 1999032600408 19990326 00408 EA 1999 3 26 COMA9960125 1 19990319 A 2750 7805013 SELECTOR CNDAIR CL600 CL6002B19 EA TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 966CA 2976 7132 FLAP FAIL MESSAGE DURING LANDING. REPLACED THE FLAP SELECTOR. 2 L 7 2 4F RT A21EA 1999032600409 19990326 00409 EA 1999 3 26 COMA9960126 1 19990319 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 966CA 7132 OVERHEAD EMERGENCY EXIT LIGHT IS INOPERABLE. REPLACED BULB. 2 L 7 2 4F RT A21EA 1999032600410 19990326 00410 EA 1999 3 26 COMA9960127 1 19990320 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA NR 1 SPOILER MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 989CA 3623 7215 CONFIG SPOILER WARNING DURING TAKEOFF. REPLACED THE NR 1 SEC U. 2 L 7 2 4F RT A21EA 1999032600411 19990326 00411 NM 1999 3 26 UPS99229076 1 19990318 A 5753 652466524 RIB BOEING 727 727173C 1384059 NM RT TE FOREFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C RT WING I/B FOREFLAP TRACK SUPPORT I/B RIB ASSY IS CRACKED. REMOVED AND REPLACED RIB ASSY PER SRM 51- 30-02. 2 L 7 3 4F A3WE 1999032600412 19990326 00412 NM 1999 3 26 UPS99229077 1 19990320 A 5320 FORGING BOEING 727 727173C 1384059 NM BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, CORROSION (B727-5310-5596A) ON BS 940 FORGING ON PRESSURE WEB ATTACH FLANGE RBL 65 TO 70 WL 200. STA NDARD REPAIR ACCOMPLISHED PER UPS EO B727-5310-4501A APP C. 2 L 7 3 4F A3WE 1999032600413 19990326 00413 NM 1999 3 26 UPS99229078 1 19990320 A 5320 WEB BOEING 727 727173C 1384059 NM BS 944 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE-C, CORROSION (B727-5310-5596A) ON PRESSURE WEB BS 944 WL 200 LBL 61. REPLACED PRESSURE WEB AT 944 WL 20 0 LBL 61 IAW SRM 53-10-1 SRM 51-20-1, 51-30-02. CORROSION WAS OUT OF LIMITS IAW SRM 51-10-6. 2 L 7 3 4F A3WE 1999032600414 19990326 00414 WP 1999 3 26 UPS99829079 1 19990310 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT FLOORBEAM ATTACH ANGLE AT FS 1320 RBL10 CORRODED ON UPPER SURFACE. CUT OUT DAMAGED AREA AND FABRICATED ATTACH ANGLE AND SPLICE ANGLE IAW REO6375 AND DAC DWG 9887940. 2 L 7 4 4F RT 4A25 1999032600415 19990326 00415 WP 1999 3 26 UPS99829080 1 19990217 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT FRAME CAP AT FS 1120 HAS SEVERAL MISSING FASTENERS AND CORRODED NUT PLATES. FABRICATED REPA IR ANGLES, FILLERS, ALODINED AND PRIMED. REMOVED FRAME CAP, CLEANED CORROSION. REMOVED INTERCOSTAL, CLEANED CORROSION. INSTALLED REPAIR ANGLES, FILLERS, FRAME CAP AND INTERCOSTAL IAW DC8 SRM 51-1-21 AND TIMCO DWG DC08-53-0229. 2 L 7 4 4F RT 4A25 1999032600416 19990326 00416 WP 1999 3 26 UPS99829081 1 19990217 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, SHIM BATHTUB FITTING AT STA 902 LT IS EXFOLIATED. REPLACED FITTING AND FABRICATED DOUBLER IAW REO-0 6350. INSTALLED ON N/R 876781. 2 L 7 4 4F RT 4A25 1999032600417 19990326 00417 WP 1999 3 26 UPS99829082 1 19990217 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, CORROSION BETWEEN LONGERON SPLICE FITTING AND LONGERON 34R AND BETWEEN FITTING AND FRAME STA 70. CO RROSION OUT OF LIMITS. CUT OUT FRAME SECTION, REPLACED IAW DC8 SRM 51-1-24, 53-2-25, 51-3-0, 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600418 19990326 00418 WP 1999 3 26 UPS99829083 1 19990217 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, AFT PIT FS 980 FRAME CAP CORRODED AT L35L AND BETWEEN L35R AND L34R. CORROSION OUT OF LIMITS. D YE PEN SHOWED CRACK IN FRAME CAP. REPLACED CAP ANGLE IAW REO-06336, FABED INTERCOSTAL IAW DWG 57299201. 2 L 7 4 4F RT 4A25 1999032600419 19990326 00419 WP 1999 3 26 UPS99829084 1 19990221 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 92 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C, FUSE EXT, KEEL BEAM STA 92 RT BEAM FITTING HAS A VISIBLE CRACK IN INBOARD RADUS. REMOVED CRACKED FIT TING, LOCATED AND DRILLED NEW FITTING (P/N 375851950 1) IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0 A ND 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600420 19990326 00420 WP 1999 3 26 UPS99829085 1 19990218 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 879 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C, L24R CRACKED AT STA 879. REMOVED AND REPLACED L24R IAW TIMCO SERVICE SKETCH 010123, DC8 SRM 5 10-1- 8, 51-1-24, 51-1-20D, 51-3-0, DC8 MM 20-50-01 AND WDM 32-60-03 AND 20-50-01. 2 L 7 4 4F RT 4A25 1999032600421 19990326 00421 WP 1999 3 26 UPS99829086 1 19990219 A 5320 BRACE DOUG DC8 DC873F 302199F WP BS 580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C, FLOORBEAM BRACE CORRODED AT STA 580, RT SIDE ABOVE L27R. REMOVED CORROSION IAW DC8- SRM 51-1-8, FABB ED REPAIR DOUBLER IAW DC8 SRM 53-2-0 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600422 19990326 00422 WP 1999 3 26 UPS99829087 1 19990220 A 5751 SKIN DOUG DC8 DC873F 302199F WP RT AILERON DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C, RT WING AILERON DENTED IN UPPER SKIN. CUT OUT DAMAGE, FABBED REPAIR DOUBLER IAW DC8 SRM 57-2-1- FIG 2, INSTALLED DOUBLER IAW DC8 SRM 51-1-21A (W & B DONE ON UPS NR 876762). 2 L 7 4 4F RT 4A25 1999032600423 19990326 00423 WP 1999 3 26 UPS99829088 1 19990220 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, FRAMED CORRODED STA 180, L35L TO L36. FABRICATED REPAIR DOUBLER (AFTER REMOVING CORROSION IAW DC8 S RM 51-1-8 IAW REO-06386 AND DC8 DWG DC08-53-0229. INSTALLED PER DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999032600424 19990326 00424 WP 1999 3 26 UPS99829089 1 19990220 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 160-180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, FWD PIT STA 160 TO 180 LONGERON 36 CORRODED. REMOVED AND REPLACED LONGERON AND SPLICE REPAIR PER DC 8 SRM 53-4-1, MAT ID IS IAW DC8 53-4-1. ALODINED, PRIMED AND INSTALLED IAW DC8 53-2-2. 2 L 7 4 4F RT 4A25 1999032600425 19990326 00425 WP 1999 3 26 UPS99829090 1 19990227 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-C2, FITTING CRACKED FS 940 AT L24R. FITTING INSTALLED ON UPS N/R 875503. 2 L 7 4 4F RT 4A25 1999032600426 19990326 00426 NE 1999 3 26 99FDEA00112 2 19990323 A 7200 ENGINE AIRBUS 310 A310203 EU GE CF6 CF680A3 30025 NE NR 2 FAILED A FDEA O OTHER Y ENGINE STOPPAGE DE DESCENT 1 SO 25 445FE 297 NR 2 ENG FAILED IN FLT, LOUD POP HEARD LVL AT 310. COMPLIED WITH ECAM. QRH PROC DUE TO POSSIBLE STRUCTURE DAMAGE. 2 L 7 2 4F 4 F RT A35EU E13NE 1999032600427 19990326 00427 NM 1999 3 26 99FDEA00113 1 19990322 A 5711 65185381 SPAR BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 CORROSION (C53-132-02,1) ON VERTICAL FLANGE ON 870 CHORD UPPER LBL 47 TO 54. 2 L 7 3 4F A3WE 1999032600428 19990326 00428 NM 1999 3 26 99FDEA00114 1 19990322 A 5312 6516202901 BULKHEAD WEB BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 WHILE WORKING NR 654, FOUND WING CENTER SECTION BULKHEAD WEB TO BE CORRODED 100 PERCENT AT RBL 4 TO LBL 4 BS 870. 2 L 7 3 4F A3WE 1999032600429 19990326 00429 NM 1999 3 26 99FDEA00115 1 19990322 A 5714 65185371 SPAR BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 WHILE WORKING NR 654, FOUND VERTICAL FLANGE OF LWR WING CTR SECTION SPAR CHORD TO BE CORRODED RBL 55-LBL 55, BS 870. 2 L 7 3 4F A3WE 1999032600430 19990326 00430 NM 1999 3 26 99FDEA00116 1 19990322 A 5320 65493989 FITTING BOEING 727 72722C 138400F NM BS 365 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 WHILE WORKING NR 310, FOUND CORROSION ON NET CASTING BS 365, LBL 60, WL 208 (MARKED). 2 L 7 3 4F A3WE 1999032600431 19990326 00431 WP 1999 3 26 ABXA9900234 1 19990322 A 3350 6012235 BATTERY DOUG DC8 DC861 3021952 WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 843AX 46017 DURING PRE-DEPARTURE CHECK, FOUND RIGHT SIDE EMERGENCY LIGHTING UNDER GLARESHIELD VERY DIM. REPLACED EMERGENCY LIGHT BA TTERY PACK IAW DC8 MM 33-50. 2 L 7 4 4F 4A25 1999032600432 19990326 00432 WP 1999 3 26 ABXA9900235 1 19990322 A 5610 5613217508 WINDOW DOUG DOUG DC9 DC933F 302207A WP RIGHT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 AFTER LANDING UNABLE TO OPEN FIRST OFFICER'S CLEARVIEW SLIDING WINDOW (EMERGENCY EXIT). ADJUSTED UPPER LOCK, LUBRICATED ALL PIVOT POINTS. 2 L 7 2 4F A6WE 1999032600433 19990326 00433 NM 1999 3 26 MWEA99102 1 19990322 A 5241 593049032 PAN DOUG MD88 MD88 3023688 NM GALLEY DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 THE AFT GALLEY DOOR HOLD OPEN HOOK BUMPER ASSEMBLY PAN IS DAMAGED. MTC REMOVED AND REPLACED BUMPER ASSEMBLY PAN. 2 L 7 2 4F RT A6WE 1999032600434 19990326 00434 NM 1999 3 26 MWEA99103 1 19990320 A 2560 11320 GIRT BAR DOUG MD88 MD88 3023688 NM PASSENGER DOOR LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 301ME 48072 THE FORWARD GIRT BAR LEFT SIDE IS HARD TO GET IN PLACE. MTC LUBED GIRT BAR LATCHES. 2 L 7 2 4F RT A6WE 1999032600435 19990326 00435 WP 1999 3 26 MWEA99104 1 19990320 A 5330 5911403 SKIN DOUG DC9 DC932 3022066 WP BS 37 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FOUND SKIN CRACKED AT STATION 37 L1. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999032600436 19990326 00436 NM 1999 3 26 MWEA99105 1 19990320 A 5320 5911412309 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 THE ANTENNA MOUNT PLATE DOUBLER HAS EXCESSIVE CORROSION. MTC REMOVED AND REPLACED MOUNT PLATE DOUBLER. 2 L 7 2 4F RT A6WE 1999032600439 19990326 00439 EU 1999 3 26 PLGA990106 1 19990106 A 2160 7769022 VALVE SAAB SF340 340B 7860101 EU LEFT DEFECTIVE A PLGA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NE 05 358BE 850998 340B279 BOS - FLT 6232 - AFTER TAKEOFF, CREW NOTED LT DUCT OVERTEMP LIGHT ILLUMINATED. CREW UNABLE TO CONTROL CABIN TEMP IN AUT O AND MANUAL MODES. A/C RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DUAL TEMP CONTROL VALVE. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600440 19990326 00440 EU 1999 3 26 PLGA990111 1 19990111 A 2820 TD028VF047 SWITCH SAAB SF340 SF340A 7850100 EU LT FUEL FILTER FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 743BA 237 340A093 BOS - FLT 6336 - AFTER DEPARTURE, THE LEFT FUEL FILTER BYPASS LIGHT ILLUMINATED. A/C RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL PRESSURE DIFFERENTIAL SWITCH. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600441 19990326 00441 EU 1999 3 26 PLGA990112 1 19990112 A 2820 FILTER SAAB SF340 SF340A 7850100 EU FUEL SYSTEM REQ'D SERVICE A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 743BA 340A093 BOS - FLT 6350 - AFTER DEPARTURE OUT OF BOS, LEFT FUEL FILTER LIGHT ILLUMINATED. ALL ENGINE PARAMETERS NORMAL. A/C RET URNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE DRAINED BOTH FUEL TANKS. REPLACED BOTH FUEL FILTERS, AND LEFT FU EL FILTER HOUSING. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600442 19990326 00442 EU 1999 3 26 PLGA990120 1 19990120 A 7712 INDICATION SAAB SF340 SF340A 7850100 EU RT ENG TO MALFUNCTIONED A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NE 05 749BA 340A152 BOS - FLT 6270 - ON TAKEOFF CREW NOTICED RIGHT ENGINE TORQUE BLOOM ABOVE VALUE SELECTED ON CTOT. TAKEOFF ABORTED. MAIN TENANCE COULD NOT DUPLICATE PROBLEM. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600443 19990326 00443 EU 1999 3 26 PLGA990120A 1 19990120 A 3240 50125893 BRAKE SAAB SF340 SF340A 7850100 EU NR 4 SPUN A PLGA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NE 05 344BE MAR960186R 340A104 BOS - FLT 6216 - DURING TAXI OUT, MAIN AND OUTBOARD BRAKE PRESSURE DROPPED TO ZERO. CREW STOPPED A/C ON TAXIWAY. A/C T OWED TO GATE. MAINTENANCE FOUND NR 4 BRAKE SPUN AND SWIVEL LINE BROKEN. BRAKE AND SWIVEL REPLACED. A/C RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A52EU 1999032600444 19990326 00444 EU 1999 3 26 PLGA990124 1 19990124 A 3020 NH2466808108 DUCT SAAB SF340 SF340A 7850100 EU RT ENG INTAKE FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 748BA L180806 340A149 LGA - FLT 6308 - BOS-PHL, CREW REPORTED RIGHT INTAKE HEAT INOP. AIRCRAFT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED THE LOWER DUCT. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600445 19990326 00445 EU 1999 3 26 PLGA990124B 1 19990124 A 7603 M83726282001 RELAY SAAB SF340 SF340A 7850100 EU E/E COMPT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 343BE 340A101 BOS - FLT 6357 - FLIGHT IDLE OPEN AMBER LIGHT ILLUMINATED UPON GEAR RETRACTION. AIRCRAFT RETURNED TO BOS AND LANDED WIT HOUT INCIDENT. MAINTENANCE REPLACED RELAY 82KA. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600446 19990326 00446 EU 1999 3 26 PLGA990124C 1 19990124 A 7603 5308214 CONTROL SAAB SF340 SF340A 7850100 EU QUADRANT FAILED A PLGA J DUMP FUEL J WARNING INDICATION CL CLIMB 1 NE 05 343BE 051 340A101 BOS - FLT 6317 - FLIGHT IDLE OPEN AMBER LIGHT ILLUMINATED AFTER GEAR RETRACTION. A/C RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CONTROL QUADRANT. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600447 19990326 00447 EU 1999 3 26 PLGA990124E 1 19990124 A 2810 SENSOR SAAB SF340 SF340A 7850100 EU RT TAIL PIPE CONTAMINATED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 345BE 340A108 HPN - FLT 6235 - AFTER TAKEOFF, RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. A/C RETURNED TO HPN AND LANDED WITHOUT INCIDENT. MAINTENANCE DRIED MOISTURE FROM SENSOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600448 19990326 00448 EU 1999 3 26 PLGA990202 1 19990202 A 2910 AE7127841 LINE SAAB SF340 340B 7860101 EU HYD SYSTEM RUPTURED A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NE 05 349BE 340B196 BTV - FLT 6242 - WILE IN CRUISE, A/C HYDRAULIC QUANTITY DROPPED TO ZERO AND MAIN ACCUMULATOR PRESSURE DROPPING TO 2200 P SI. A/C DIVERTED TO BTV AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN HYDRAULIC LINE. AFTER REPLACEMENT, AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600449 19990326 00449 EU 1999 3 26 PLGA990211A 1 19990211 A 2910 P240606040146 LINE SAAB SF340 SF340A 7850100 EU LT MLG WW FAILED A PLGA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 NE 05 741BA 340A090 LGA - FLT 6540 - AFTER GEAR EXTENSION, CREW LOST ALL HYDRAULIC PRESSURE. AIRCRAFT LANDED WITHOUT INCIDENT AND WERE TOWE D FROM RUNWAY. MAINTENANCE REPLACED RUPTURED LINE IN LT GEAR WELL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600450 19990326 00450 EU 1999 3 26 PLGA990203 1 19990203 A 3030 HEAT SYSTEM SAAB SF340 SF340A 7850100 EU LT PITOT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 343BE 340A101 BOS - FLT 6335 - DURING CRUISE, THE PITOT AND ALPHA HEAT FAILED. A/C RETURNED TO BOS DUE TO WEATHER IN YHZ. MAINTENANC E FOUND OPEN WHEELWELL CIRCUIT BREAKER. GROUND RUNS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600451 19990326 00451 EU 1999 3 26 PLGA990203A 1 19990203 A 7722 523402 GAUGE SAAB SF340 340B 7860101 EU RT ITT FAILED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 353BE 07887020 340B242 LGA - FLT 6516 - RIGHT ITT GAUGE FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENAN CE REPLACED THE GAUGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600452 19990326 00452 EU 1999 3 26 PLGA990204 1 19990204 A 7712 CTOT SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A PLGA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NE 05 358CA 340A047 ALB - FLT 6262 - DURING TAKEOFF, CTOT FAILED TO ARM AND TAKEOFF WAS ABORTED. MAINTENANCE COULD NOT DUPLICATE PROBLEM. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600453 19990326 00453 EU 1999 3 26 PLGA990222 1 19990222 A 2160 7828602 VALVE SAAB SF340 340B 7860101 EU RIGHT DEFECTIVE A PLGA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 NE 05 348BE 606422 340B190 BOS - FLT 6303 - EN ROUTE BOS-PHL, RIGHT DUCT OVERTEMP LIGHT ILLUMINATED, CREW SHUT OFF BLEED VALVE AND LIGHT WENT OUT. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT DUAL TEMP CONTROL VALVE AND SYSTE M OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999032600454 19990326 00454 EU 1999 3 26 PLGA990220 1 19990220 A 2421 31342001 GENERATOR SAAB SF340 SF340A 7850100 EU LEFT FAILED A PLGA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 NE 05 343BE 286 340A101 BOS - FLT 6335 - DURING FLIGHT FROM BOS TO YHZ, THE LEFT A/C GEN FAILED AND THE AIRCRAFT RETURNED TO BOS. AIRCRAFT LAND ED WITHOUT INCIDENT. BOS MAINTENANCE REPLACED DEFECTIVE LEFT A/C GENERATOR AND GENERATOR CONTROL UNIT. RAN AIRCRAFT AN D SYSTEM OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600455 19990326 00455 NM 1999 3 26 UIEA9905 1 19990217 A 2750 126344151 PDU BOEING 747 7472D7B 1384803 NM RT TE FLAP DEFECTIVE A UIEA A J UNSCHED LANDING DUMP FUEL F FLT CONT AFFECTED CL CLIMB 1 EA 15 526MC 22337 FLT 1358 - ANC/LAX - ATB - AFTER TAKEOFF, DURING FLAP RETRACTION, RIGHT NR 1 LEADING EDGE FLAP WOULD NOT RETRACT. TRIED TO USE ALT SYSTEM BUT LE FLAP DRIVE C/B TRIPPED. RESET CIRCUIT BREAKER AND TRIED AGAIN BUT NOT HELP. DUMPED 6,000 KIL OS OF FUEL AND RETURNED TO ANC. FOUND RIGHT NR 1 LE FLAP POWER DRIVE UNIT, P/N 126344-15-1 DEFECTIVE. REPLACED PDU AND OPERATION NOW NORMAL. (M) 2 L 7 4 4F RT A20WE 1999032600456 19990326 00456 WP 1999 3 26 ORJA9971 1 19990218 A 3350 603045 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 17-20 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 RNO - ON DESCENT, EMERGENCY EXIT ROW LIGHTS CAME ON SECTION OF ROWS 17-20. REPLACED EMERGENCY BATTERY PACK LEFT AFT POS ITIVE, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600457 19990326 00457 WP 1999 3 26 ORJA9972 1 19990218 A 3350 BR9687100 CHARGER DOUG DC9 DC983 3022083 WP ROW 29-32 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 RNO - EMERGENCY EXIT LIGHTS AT ROWS 29, 30, 31 AND 32 INOP. REPLACED AFT BATTERY PACK CHARGER, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600458 19990326 00458 WP 1999 3 26 ORJA9973 1 19990218 A 3350 PIN DOUG DC9 DC983 3022083 WP ROW 23 UNSECURED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 RNO - EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 23. RESECURED PIN IN WIRE TO LIGHT CONNECTION, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600459 19990326 00459 WP 1999 3 26 ORJA9974 1 19990217 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 12-16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN SFO - EMERGENCY LIGHTS ON SEATS ROWS 12-16 INOPERATIVE. FOUND FORWARD LEFT EXIT ROW BATTERY PACK SHORTED. REMOVED A ND REPLACED FORWARD LEFT BATTERY PACK AND AFT LIGHT EMERGENCY EXIT ROW BATTERY PACK FUNCTIONAL CHECK OF EMERGENCY PATH L IGHT IS NORMAL. (M) 2 L 7 2 4F RT A6WE 1999032600460 19990326 00460 WP 1999 3 26 ORJA9975 1 19990217 A 3350 EM1267 BATTERIES DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 AT RNO, SEVERAL CABIN EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600461 19990326 00461 WP 1999 3 26 ORJA9976 1 19990218 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 19-22 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY LIGHTS INOPERABLE AT ROWS 19 TO 22. REPAIRED CHAFED WIRINGS. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600462 19990326 00462 WP 1999 3 26 ORJA9977 1 19990220 A 3397 0105606303 WIRE DOUG DC9 DC987 3022087 WP ROWS 28/29 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT RNO, EMERGENCY LIGHTS INOPERABLE AT SEATS 28 AND 29 D-F. REWIRED CONNECTIONS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600463 19990326 00463 WP 1999 3 26 ORJA9942 1 19990207 A 5230 STRIKER DOUG DC9 DC983 3022083 WP CARGO DOOR BENT A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 834RA 53124 IN SJC, ABORTED TAKEOFF AT 90 KNOTS FORWARD CARGO DOOR ANNUNCIATION RETURN TO GATE. UPON RETURN TO GATE INSPECTED FORWA RD CARGO DOOR, FOUND TO BE LOCKED. FURTHER INSPECTION REVEALED STRIKER PLATE BENT, STRAIGHTENED AND ADJUSTED PLATE. CY CLED DOOR, OPS CHECK GOOD. OK FOR CONTINUE SERVICE, DOOR HAS BEEN VERIFIED IN THE CLOSED AND LOCKED POSITION. (M) 2 L 7 2 4F RT A6WE 1999032600464 19990326 00464 WP 1999 3 26 ORJA9978 1 19990216 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROW 20 DEF INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN SFO, EMERGENCY SEAT TRACK LIGHTING INOPERATIVE, ROWS 12-20. REPLACED POWER SUPPLY AT 20 DEF, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999032600465 19990326 00465 WP 1999 3 26 ORJA9979 1 19990220 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP ROW 20 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 LAS - EMERGENCY LIGHTS FROM ROWS 17-20 ILLUMINATED IN FLIGHT. REMOVED AND REPLACED ROW 20 OVERWING RIGHT EXIT BATTERY C HARGER, SYSTEM OPS GOOD PER MM 25-00. (M) 2 L 7 2 4F RT A6WE 1999032600466 19990326 00466 WP 1999 3 26 ORJA9981 1 19990219 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP GALLEY DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, FORWARD GALLEY EMERGENCY LIGHT FOR EXIT INOPERABLE. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK FROM FORWA RD GALLEY. OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 1999032600467 19990326 00467 WP 1999 3 26 ORJA9982 1 19990220 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 1-9 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT BUR, EMERGENCY AISLE LIGHTS ON ROWS 1-9 WILL NOT GO OUT. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999032600468 19990326 00468 WP 1999 3 26 ORJA9960 1 19990208 A 3350 PPSIB CHARGER DOUG DC9 DC987 3022087 WP SEAT 19 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, ROWS 17-20 ESCAPE LIGHTS ARE INOPERABLE. FOUND AND REPAIRED SHORTED WIRE ON SEAT 19. INSTALLED NEW CHARGER. O PS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600469 19990326 00469 WP 1999 3 26 AALA990263 1 19990222 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 463AA 49593 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED FORWARD EMERGENCY EX IT FLOOR PATH LIGHT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999032600470 19990326 00470 NM 1999 3 26 AALA990179 1 19990213 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM RT EMERG EXIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 847AA 20988 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT RIGHT OVERWING EXITS INOPERATIVE. MAINTENANCE FOUND THE LI GHT ASSEMBLY LOOSE. TIGHTENED LOOSE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999032600471 19990326 00471 NM 1999 3 26 AALA990264 1 19990224 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 848AA 20989 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH IN AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LI GHT SECTION IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999032600472 19990326 00472 NM 1999 3 26 AALA990252 1 19990221 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT AIR STAIR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 882AA 21521 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT AIR STAIR EMERGENCY E XIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999032600473 19990326 00473 NM 1999 3 26 AALA990177 1 19990214 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729AA 20736 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999032600474 19990326 00474 NM 1999 3 26 AALA990176 1 19990214 A 3350 1000679 LIGHT GRIMES BOEING 727 727227 1384078 NM GALLEY DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729AA 365 20736 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER FORWARD GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999032600475 19990326 00475 EU 1999 3 26 AALA990250 1 19990219 A 3230 10SD8001 SOLENOID FOKKER F28 F28MK0100 4990807 EU MLG DEFECTIVE A AALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SW 07 1438H 11428 ORD - DURING OVERNIGHT CHECK, MAIN LANDING GEAR DOORS WOULD NOT RETRACT. REPLACED ANTI-RETRACTION SOLENOID. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999032600476 19990326 00476 EU 1999 3 26 AALA990290 1 19990228 A 2910 O-RING FOKKER F28 F28MK0100 4990807 EU NR 1 HYD PUMP LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 1451N 11460 DFW - FLT 640 - DURING CRUISE, THE NR 1 HYDRAULIC SYSTEM LOW LIGHT ILLUMINATED ON THE MULTIFUNCTION DISPALY UNIT (MFDU). CREW ACCOMPLISHED CHECKLIST FOR HYDRAULIC SYSTEM LOW QUANTITY AND ALTERNATE FLAP EXTENSION AND GEAR EXTENSION AND GEAR EXTENSION WEAR USED. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 1 HYDRAULIC PUMP PRESSURE LIN E FITTING LEAKING. REPLACED NR 1 HYDRAULIC PUMP PRESSURE LINE FITTING O-RING AND SERVICED HYDRAULIC SYSTEM. SYSTEM WAS CHECKED UNDER PRESSURE WITH NO FURTHER LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999032600477 19990326 00477 EU 1999 3 26 AALA990274 1 19990225 A 2170 20D102 COALESCER AIRBUS 300 A300B4605R 3930308 EU ACM BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 14068 511 LHR - FLT 106 - EN ROUTE JFK-LHR, STRONG PUNGENT SMELL IN MID SECTION OF CABIN BY ROWS 23-25. STRONGEST ON RIGHT SIDE O F AIRCRAFT, CAUSING FLIGHT ATTENDANTS AND PASSENGERS TO EXPERIENCE BURNING EYES AND NAUSEA. LANDED LHR WITHOUT INCIDENT . RAN PACKS AND FOUND COALESCER BAGS CONTAMINATED. REPLACED COALESCER BAGS, ACCOMPLISHED OPERATIONS CHECKS AND LEAK CH ECKS. NO FURTHER SMELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999032600478 19990326 00478 WP 1999 3 26 AALA990273 1 19990224 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 234AA 49181 DFW - DURING OVERNIGHT CHECK, LAST 4 FEET OF EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT SECTION OF COACH INOPERATIVE. REPL ACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT SECTION OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999032600479 19990326 00479 WP 1999 3 26 AALA990277 1 19990225 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 423AA 49335 DFW - DURING OVERNIGHT CHECK, FORWARD HALF OF EMERGENCY EXIT FLOOR PATH LIGHTING NOT DUAL FEEDING. REPLACED CONNECTOR A ND PIG TAIL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999032600480 19990326 00480 WP 1999 3 26 AALA990293 1 19990301 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7517A 49894 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTS IN AFT COACH CLASS WERE INOPERATIVE. REPAIRED BROKEN WIRE AT OVERHEAD BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999032600481 19990326 00481 NM 1999 3 26 AALA990180 1 19990212 A 3397 WIRE BOEING 767 767223 1385123 NM ROW 2B CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 332AA 22331 ORD - FLT 83 - DURING MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROWS 2B THROUGH 9B INOPERATIVE. REPAIRED SHORT IN EMERGENCY EXIT WIRING AT AFT END OF E/E COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999032600482 19990326 00482 NM 1999 3 26 AALA990260 1 19990222 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 629AA 24587 DFW - DURING OVERNIGHT CHECK, EMERGENCY OVERWING EXIT SIGN INOPERATIVE. REPAIRED GROUND AT LIGHT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999032600483 19990326 00483 NM 1999 3 26 AALA990261 1 19990222 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 629AA 24587 DFW - DURING OVERNIGHT CHECK, MID FUSELAGE AISLE EXIT SIGN INOPERATIVE. REPAIRED GROUND AT LIGHT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999032600484 19990326 00484 NM 1999 3 26 AALA990280 1 19990226 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 22 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 381AN 25450 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT ROW 22B INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT SEAT ROWS 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999032600485 19990326 00485 NM 1999 3 26 AALA990285 1 19990227 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661AA 25295 DFW - DURING OVERNIGHT CHECK, OVERHEAD EMERGENCY EXIT SIGN LIGHT AT MID LAVATORY INOPERATIVE. RESEATED OVERHEAD EMERGEN CY EXIT SIGN LIGHT WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999032600486 19990326 00486 NM 1999 3 26 AALA990289 1 19990227 A 3350 LIGHT BOEING 757 757223 1384957 NM DOOR 2R DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 698AN 26980 ORD - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT STRIP AT 2R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999032600487 19990326 00487 NM 1999 3 26 AALA990181 1 19990215 A 3350 P4010049 BATTERY BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST CR CRUISE 1 SW 07 623AA 12294 24581 BOS - FLT 148 - DURING FLIGHT, EMERGENCY EXIT LIGHTS BY 2L AND 2R INTERMITTENTLY ILLUMINATED. REPLACED MODULE AND BATTE RY PACK FOR EMERGENCY EXIT LIGHTS AT 2R AND 2R DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999032600488 19990326 00488 EU 1999 3 26 AALA990294 1 19990301 A 2740 6227478411 COMPUTER COLLINS FOKKER F28 F28MK0100 4990807 EU E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1417D 780 11396 ORD - FLT 702 - DURING CLIMB-OUT AT 500 FT, STAB TRIM NR 1/2 ILLUMINATED ON MFDU AND WOULD NOT RESET. CREW ACCOMPLISHED JAMMED PROCEDURE CHECKLIST AND RETURNED AND LANDED ORD WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT SYSTEM AND F OUND NO FAULTS. A LAND 40 TEST WAS ACCOMPLISHED WITH NO FAULTS DETECTED. UNABLE TO DUPLICATE STAB TRIM 1/2 FAULT AND A S A PRECAUTIONARY. REPLACED FLIGHT AUGMENTATION COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999032600489 19990326 00489 EU 1999 3 26 SIMA990491 1 19990218 A 5311 S5367240820051 FRAME AEROSP ATR42 ATR42300 8680920 EU FRAME 39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE RIGHT SIDE OF FRAME 39 AT FLOOR LEVEL CORRODED. MAINTENANCE REPAIRED THE FRAM E IAW SRAS S53R0126 1182. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600490 19990326 00490 EU 1999 3 26 SIMA990572 1 19990226 A 5230 S52376300802 SKIN AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR MISDRILLED A SIMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING MBV-2 INSPECTION, FOUND 5 HI-LOCKS HOLES ON FORWARD CARGO DOOR SKIN UNDER THE HINGE WERE IMPROPERLY DRILLED . REPAIRED CARGO DOOR IAW SB 42-52-0058. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600491 19990326 00491 EU 1999 3 26 SIMA990524 1 19990221 A 5330 S5337142023805 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 15-16 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 269AT 269 SAW - DURNG MBV-1 INSPECTION, MAINTENANCE REPORTED A DENT IN THE RIGHT SIDE OF THE FUSELAGE 5 INCHES LONG, .375 INCH WID E AND .018 DEEP BETWEEN FRAMES 15 AND 16 AT STRINGER 20. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETUR NED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600492 19990326 00492 EU 1999 3 26 SIMA990523 1 19990221 A 5330 S5337130700205 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 22-23 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING MBV-2 INSPECTION, FOUND A DENT IN THE RIGHT SIDE OF THE FUSELAGE .25 INCH LONG .20 WIDE AND .039 DEEP BETWE EN FRAMES 22 AND 23 AT STRINGER 7A. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600493 19990326 00493 EU 1999 3 26 SIMA990522 1 19990221 A 5330 S5367125722151 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 39-42 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE RIGHT AFT OUTER CHORD BETWEEN FRAMES 39 AND 42 AT STRINGER 17 CORRODED. REMOV ED AND REPLACED THE CHORD IAW SRM 51-25-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600494 19990326 00494 EU 1999 3 26 SIMA990521 1 19990221 A 5347 S5337500121002 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT FORWARD OUTBOARD, THE LEFT AND RIGHT MIDDLE INBOARD, AND THE LEFT AND RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. (M) 2 H 7 2 4T RT A53EU 1999032600495 19990326 00495 EU 1999 3 26 99ZZZM197 1 19990221 A 5347 S53375001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT FORWARD OUTBOARD, THE LEFT AND RIGHT MIDDLE INBOARD, AND THE LEFT AND RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. (M) 2 H 7 2 4T RT A53EU 1999032600496 19990326 00496 EU 1999 3 26 99ZZZM198 1 19990221 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT FORWARD OUTBOARD, THE LEFT AND RIGHT MIDDLE INBOARD, AND THE LEFT AND RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. (M) 2 H 7 2 4T RT A53EU 1999032600497 19990326 00497 EU 1999 3 26 99ZZZM199 1 19990221 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT FORWARD OUTBOARD, THE LEFT AND RIGHT MIDDLE INBOARD, AND THE LEFT AND RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. (M) 2 H 7 2 4T RT A53EU 1999032600498 19990326 00498 EU 1999 3 26 99ZZZM200 1 19990221 A 5347 S53375001203 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD INBOARD, THE LEFT FORWARD OUTBOARD, THE LEFT AND RIGHT MIDDLE INBOARD, AND THE LEFT AND RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. (M) 2 H 7 2 4T RT A53EU 1999032600499 19990326 00499 EU 1999 3 26 SIMA990495 1 19990218 A 5313 S53572605203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FRAME 34-35 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING MBV-2 INSPECTION, FOUND STRINGER 21 RIGHT CORRODED BETWEEN FRAMES 34 AND 35. MAINTENANCE REPAIRED STRINGER 21 IAW SRM 53-00-00 FIGURE 428. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600500 19990326 00500 EU 1999 3 26 SIMA990494 1 19990218 A 5330 S533714002005 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 20 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING MBV-2 INSPECTION, FOUND DENT IN THE LEFT SIDE OF THE FUSELAGE JUST FORWARD OF FRAME 20 BETWEEN STRINGER 19 AND 20. IT MEASURED 1 INCH BY 1 INCH BY .070 DEEP. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 401. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600501 19990326 00501 EU 1999 3 26 SIMA990493 1 19990218 A 5320 S5367121721001 WEB AEROSP ATR42 ATR42300 8680920 EU FRAME 35-36 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AFT WEB BETWEEN FRAMES 35 AND 36 AND BETWEEN STRINGER 15 AND 16 CORRODED. MAINTENANCE REMOVED AND REPLACED THE WEB IAW SRM 51-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600502 19990326 00502 EU 1999 3 26 SIMA990492 1 19990218 A 5315 S5337241120002 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE MISDRILLED A SIMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING MBV-2 INSPECTION, FOUND FLOORBEAM 21 WITH AND OVERSIZED FLOORBOARD MOUNT HOLE. MAINTENANCE REPAIRED THE FL OORBEAM IAW SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600503 19990326 00503 SO 1999 3 26 RAIA990135 1 19990126 A 3412 102AU1AF PROBE EMB 145 EMB145 SO NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 802HK 145066 FLT 5783 - SBN - NR 2 TAT HEAT FAILED. MAINTENANCE REPLACED NR 2 TAT PROBE. (M) 2 L 7 2 4F RT T00011AT 1999032600504 19990326 00504 EU 1999 3 26 RAIA990201 1 19990203 A 7931 1241013 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 337TE 929 FLT 7443 - STL - LEFT ENGINE OIL PRESSURE FLUCTUATES. MAINTENANCE REPLACED LEFT OIL PRESS TRANSDUCER. (M) 2 L 7 2 4T RT A56EU 1999032600505 19990326 00505 1999 3 26 RAIA990204 4 19990204 A 2210 7003974605 COMPUTER AEROSP ATR42 ATR42300 8680920 EU AUTOFLIGHT SYST FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 422TE 106 FLT 7171 - MSN - AIR DATA UNIT WILL NOT RESET. MAINTENANCE REPLACED AFCS COMPUTER. (M) 2 H 7 2 4T RT A53EU 1999032600506 19990326 00506 1999 3 26 RAIA990210 4 19990209 A 2350 B692246 AUDIO PANEL BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 341TE 8769 950 FLT 7344 - STL - FIRST OFFICERS INTERCOM INTERMITTENT. MAINTENANCE REPLACED FIRST OFFICER'S AUDIO PANEL. (M) 2 L 7 2 4T RT A56EU 1999032600507 19990326 00507 NE 1999 3 26 RAIA990209 2 19990206 A 7260 310430212 GEARBOX JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FAILED A RAIA B EMER. DESCENT R PARTIAL RPM/PWR LOSS CR CRUISE 1 CE 03 557HK 41074 76092 FLT 7782 - JFK - OIL PRESSURE DROPPED BELOW RED LINE ALONG WITH TORQUE DROP ON RIGHT ENGINE. ENGINE WAS SHUTDOWN IN FLI GHT. MAINTENANCE REPLACED RIGHT ENGINE GEARBOX. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999032600508 19990326 00508 EU 1999 3 26 RAIA990207 1 19990206 A 3260 327 BULB BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 423AM 858 FLT 7512 - BEFORE LANDING GEAR WAS SELECTED UP, NOSE GEAR GREEN LIGHT BURNED OUT. MAINTENANCE REPLACED BULBS IN INDICAT OR. (M) 2 L 7 2 4T RT A56EU 1999032600509 19990326 00509 EU 1999 3 26 RAIA990208 1 19990204 A 3260 9EN1C11HB2BB2 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 429AM 879 FLT 7442 - STL - RIGHT MAIN GEAR INTRANSIT LIGHT REMAINS ON WITH GEAR UP. MAINTENANCE REPLACED RIGHT MAIN GEAR UPLOCK S WITCH. (M) 2 L 7 2 4T RT A56EU 1999032600510 19990326 00510 1999 3 26 RAIA990205 4 19990205 A 6122 89741016 GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT PROP FAILED A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 436AM 891 FLT 7478 - STL - RIGHT ENGINE ONLY MADE 50 PERCENT TORQUE. MAINTENANCE REPLACED RIGHT ENGINE PROP GOVERNOR. (M) 2 L 7 2 4T RT A56EU 1999032600511 19990326 00511 EU 1999 3 26 RAIA990206 1 19990208 A 3244 TIRE JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 552HK 41057 FLT 7461 - BHM - DURING TAKEOFF ROLL BOTH LEFT MAIN TIRES BURSTED. MAINTENANCE REPLACED BOTH LEFT MAIN WHEEL ASSY. (M) 2 L 7 2 4T RT A41NM 1999032600512 19990326 00512 EU 1999 3 26 RAIA990211 1 19990210 A 2750 5148YMK83 HANDLE BAG JETSTM JETSTM3201 1500217 EU TE FLAPS FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 426AM 14499 874 FLT 7356 - STL - WITH FLAPS SELECTED 10 DEGREES, FLAP INDICATOR READS ZERO. MAINTENANCE REPLACED FLAP POSITION HANDLE. (M) 2 L 7 2 4T RT A56EU 1999032600513 19990326 00513 EU 1999 3 26 RAIA990212 1 19990210 A 8011 31036061 INSERT BAG JETSTM JETSTM3201 1500217 EU LT STARTER FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 339TE 935 FLT 7290 - STL - LEFT RPM DROPS TO ZERO. MAINTENANCE REPLACED STARTER INSERT. (M) 2 L 7 2 4T RT A56EU 1999032600514 19990326 00514 WP 1999 3 26 RAIA990213 2 19990210 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CE 03 424AM 11348 865 66291 FLT 7364 - STL - LEFT ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999032600515 19990326 00515 EU 1999 3 26 RAIA990215 1 19990215 A 5330 SKIN JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE DAMAGED A RAIA K NONE C F.O.D. IN INSP/MAINT 1 CE 03 571HK 41090 DCA - FORWARD NOSE SECTION OF A/C WAS DAMAGED BY A TUG. MAINTENANCE REPAIRED DAMAGE IAW EO NR J4100-53-003-1. (M) 2 L 7 2 4T RT A41NM 1999032600516 19990326 00516 EU 1999 3 26 RAIA990216 1 19990215 A 5313 ZH249422 STRINGER JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE DAMAGED A RAIA K NONE C F.O.D. IN INSP/MAINT 1 CE 03 571HK 41090 DCA - FORWARD SECTION OF A/C WAS DAMAGED BY A TUG. MAINTENANCE REPAIRED DAMAGE IAW EO NR J4100-53-003-1. (M) 2 L 7 2 4T RT A41NM 1999032600517 19990326 00517 EU 1999 3 26 RAIA990217 1 19990215 A 5320 14153005291 CHANNEL JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE DAMAGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 571HK 6391 41090 DCA - FORWARD SECTION OF AIRCRAFT DAMAGED BY A TUG. MAINTENANCE REPAIRED DAMAGE IAW EO NR J4100-53-003-1. (M) 2 L 7 2 4T RT A41NM 1999032600518 19990326 00518 EU 1999 3 26 RAIA990218 1 19990215 A 5320 1415300592 CHANNEL JETAIR JETSTM JETSTM4101 1500501 EU 6391 DAMAGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 571HK 41090 DCA - FORWARD SECTION OF A/C WAS DAMAGED BY A TUG. MAINTENANCE REPAIRED DAMAGE IAW EO NR J4100-53-003-1. (M) 2 L 7 2 4T RT A41NM 1999032600519 19990326 00519 EU 1999 3 26 RAIA990219 1 19990215 A 5330 SKIN JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE CRACKED A RAIA K NONE C F.O.D. IN INSP/MAINT 1 CE 03 571HK 41090 DCA - FORWARD NOSE SECTION OF A/C WAS DAMAGED BY A TUB. MAINTENANCE REPAIRED DAMAGE IAW EO NR J4100-5300-1. (M) 2 L 7 2 4T RT A41NM 1999032600520 19990326 00520 EU 1999 3 26 RAIA990221 1 19990212 A 5700 DOUBLER BAG JETSTM JETSTM3201 1500217 EU RT WING CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 338TE 932 STL - RIGHT WING AFT SPAR CRACKED NEAR RIB NR 67. MAINTENANCE REPAIRED RIGHT WING SPR IAW NR J3200-57-012-1. (M) 2 L 7 2 4T RT A56EU 1999032600521 19990326 00521 EU 1999 3 26 RAIA990220 1 19990212 A 5720 DOUBLER BAG JETSTM JETSTM3201 1500217 EU RT WING CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 338TE 932 STL - RIGHT AFT WING SPAR CRACKED NEAR RIB NR 67. MAINTENANCE REPAIRED WING SPAR IAW EO NR J3200-57-012-1. (M) 2 L 7 2 4T RT A56EU 1999032600522 19990326 00522 EU 1999 3 26 RAIA990223 1 19990219 A 2160 7252C000 VALVE BAG JETSTM JETSTM3201 1500217 EU RIGHT CORRODED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 341TE 1996 950 FLT 7286 - STL - RIGHT OVERTEMP LIGHT ILLUMINATED, ALSO HAD AN ODOR OF SMOKE IN COCKPIT. MAINTENANCE CLEANED CORROSION FROM RIGHT TEMP CONTROL VALVE CANNON PLUG. (M) 2 L 7 2 4T RT A56EU 1999032600523 19990326 00523 EU 1999 3 26 RAIA990224 1 19990219 A 3242 AC63742 MAXERET BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 341TE 950 FLT 7100 - STL - LEFT BRAKE INTERMITTENT. MAINTENANCE REPLACED LEFT MAIN WHEEL MAXERET. (M) 2 L 7 2 4T RT A56EU 1999032600524 19990326 00524 WP 1999 3 26 RAIA990225 2 19990219 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 CE 03 436AM 13726 891 66066 FLT 7365 - PAH - LEFT ENGINE SHUTDOWN IN FLIGHT FOR HIGH OIL PRESSURE AND 20 PERCENT LOSS OF POWER. MAINTENANCE REPLACE D LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999032600525 19990326 00525 EU 1999 3 26 RAIA990227 1 19990221 A 2450 7271825 CIRCUIT BREAKER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424AM 865 FLT 7332 - STL - MAIN INVERTER CIRCUIT BREAKER BROKE DURING OPS CHECK. MAINTENANCE REPLACE MAIN INVERTER CIRCUIT BREAKE R. (M) 2 L 7 2 4T RT A56EU 1999032600526 19990326 00526 1999 3 26 RAIA990222 4 19990218 A 3420 9012100811 RMU JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 550HK 41039 FLT 7753 - JFK - NR 2 RMU WENT BLANK. MAINTENANCE REPLACED NR 2 RMU. (M) 2 L 7 2 4T RT A41NM 1999032600527 19990326 00527 NE 1999 3 26 RAIA990226 2 19990220 A 7320 31055016 P2 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 558HK 7719 41071 76088 FLT 7128 - STL - RIGHT ENGINE IEC FAULT LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT ENGINE P2 INLET SENSOR. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999032600528 19990326 00528 NE 1999 3 26 RAIA990230 2 19990222 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE NR 1 FAILED A RAIA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 CE 03 562HK 7046 41078 76094 FLT 7752 - ORF - NR 1 ENGINE SHUT ITSELF DOWN IN FLIGHT. MAINTENANCE REPLACED NR 1 ENGINE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999032600529 19990326 00529 EU 1999 3 26 RAIA990229 1 19990220 A 3241 428891 CONTROL JETAIR JETSTM JETSTM4101 1500501 EU ANTI-SKID SYST FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 558HK 41071 FLT - 7141 - MEM - ANTI-SKID FAULTED. MAINTENANCE REPLACED ANTI-SKID CONTROL UNIT. (M) 2 L 7 2 4T RT A41NM 1999032600530 19990326 00530 EU 1999 3 26 RAIA990228 1 19990223 A 2425 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 556HK 41073 FLT 7320 - STL - CAPTAINS EHSI SHOWING BLUE BOX IN THE MIDDLE AND BLUE BARS ALL OVER THE TUBE. MAINTENANCE REPLACED NR 1 SYMBOL GENERATOR. (M) 2 L 7 2 4T RT A41NM 1999032600531 19990326 00531 1999 3 26 RAIA990231 4 19990227 A 3418 C771076 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 340TE 939 FLT 7102 - STL - RIGHT STALL LIGHT WILL NOT GO OUT. MAINTENANCE REPLACED RIGHT LEFT TRANSDUCER. (M) 2 L 7 2 4T RT A56EU 1999032600532 19990326 00532 NM 1999 3 26 UIEA9909 1 19990225 A 5240 SKIN BOEING 747 747212B 1384886 NM R4 DOOR DAMAGED A UIEA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 808MC 21048 FLT GT065 - ATB - APPROX 3.5 HOURS INTO THE FLIGHT, AND ADDITIONAL CARGO CHECK WAS MADE AN A HOLE APPROXIMATELY 1 FT SQU ARE WAS DISCOVERED AT THE BOTTOM LEFT CORNER OF R4 MED. AIRCRAFT WAS AT FL 33, PRESSURIZATION WAS NORMAL (8.3). AFTER AIRCRAFT RETURNED TO MIA, INSPECTED FUSELAGE AND TAIL SECTION FOR FOD DAMAGE AND NONE FOUND. REPLACED R4 MED DOOR IAW M M 52-11-01. OPS CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1999032600533 19990326 00533 WP 1999 3 26 USAADD99030 1 19990223 A 3220 NAS110818D BOLT DOUG DC9 DC981 3022081 WP NLG SHEARED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 813US 48093 PIT-DFW - FLT 692 - ON GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR LIGHT REMAINED RED. THE GEAR WAS RECYCLED WITH THE SAME RESULTS. WHEN THE GEAR HANDLE WAS UP A LOUD WIND NOISE CONTINUED, BUT THE NOSE LANDING GEAR INDICATION PIN SHOWED THAT THE NOSE GEAR WAS RETRACTED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A6WE 1999032600534 19990326 00534 NM 1999 3 26 USAA029911 1 19990223 A 3350 900835A BATTERY BOEING 727 727227 1384078 NM COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 10246 21244 FLT 6091 - BOS-LGA - FOUND ON L/S, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999032600535 19990326 00535 NM 1999 3 26 USAA029910 1 19990218 A 7711 473107 PT7 TUBE BOEING 727 727225 1384077 NM NR 2 ENGINE BROKEN A USAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 19 922TS 20415 FLT 6410 - DCA-LGA - ON TAKEOFF ROLL, NR 2 ENGINE EPR DROPPED TO 1.7 AT 100 KNOTS. TAKEOFF ABORTED. ENGINE ANTI-ICE ON . CI NR M81495 ASSIGNED PER MEL SEQ 77-1. NR 2 ENGINEER INDICATION INOP. CI NR M841495 CLEARED, REPLACED NR 2 ENGINE REPLACED BROKEN PT7 LINE IN TURBINE EXHAUST AT 12 O'CLOCK POSITION, LEAK CHECKS OK. (M) 2 L 7 3 4F A3WE 1999032600536 19990326 00536 WP 1999 3 26 ORJA9983 1 19990224 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP CABIN DIRTY A ORJA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 11 824RA 53017 IN SJC, RETURNED TO GATE BECAUSE OF A BURNING SMELL AT FWD GALLEY. PERFORMED INSPECTION OF THE FWD GALLEY AREA AND NO E VIDENCE OF BURNING NOTICED. REMOVED AND REPLACED BOTH COALESCER BAGS AND PERFORMED ENGINE RUN AND NO EVIDENCE OF SMOKE OR BURNING. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999032600538 19990326 00538 WP 1999 3 26 GTIA9900020 1 19990213 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 LGA - FLT 381 - FIRST RED LIGHT IN GALLEY OF THE EMERGENCY TRACK FLOOR LIGHTING FAILS TO ILLUMINATE. DEFERRED MANTENANC E ITEM NR 591 ON 2/13/99. REPLACED MISSING LAMP ASSEMBLY. OPERATIONAL CHECK GOOD AIW DC9 MM 33-50-00. THIS CLEARS DEF ERRED MAINTENANCE ITEM NR 591. PLACARDS REMOVED. (M) 2 L 7 2 4F A6WE 1999032600539 19990326 00539 WP 1999 3 26 GTIA9900023 1 19990218 A 3397 WIRE DOUG DC9 DC931 3022065 WP ROW 20 BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - EMERGENCY FLOORTRACK LIGHTING FROM 20 THE ROW TO AFT CABIN DOOR INOPERATIVE, SIX LIGHTS. REPAIRED BROKEN WIRE. O PERATION CHECK GOOD IAW DC-9 MM 33-53-00. (M) 2 L 7 2 4F A6WE 1999032600540 19990326 00540 NM 1999 3 26 BJNA990201 1 19990217 A 3230 65178198 ACTUATOR BOEING 737 7372H4 138448C NM NLG FAILED A BJNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 456TM 20336 NOSE GEAR WOULD NOT RETRACT. REMOVE AND REPLACED NOSE GEAR LOCK ACTUATOR PER BMM 32-33-21. (M) 2 L 7 2 4F A16WE 1999032600541 19990326 00541 WP 1999 3 26 ASAA9980052 1 19990226 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 3-8 DAMAGED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 937AS 49364 SEA - PRIOR TO DEPARTURE OF FLIGHT 288, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 3 TO 8 WERE INOPERATIVE . REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999032600542 19990326 00542 WP 1999 3 26 ASAA9980047 1 19990218 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 8 WERE FOUND INOPERATIVE. RECONNECTED W IRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600543 19990326 00543 WP 1999 3 26 ASAA9980046 1 19990215 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 11470 49126 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND TO OPERATE INTERMITTENTLY. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999032600544 19990326 00544 WP 1999 3 26 ASAA9980042 1 19990212 A 3350 0105606003 BULB DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE AFT 2 RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE LAMP MO DULES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600545 19990326 00545 NM 1999 3 26 ASAA9940056 1 19990226 A 3350 20131A BATTERY BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING MAINTENANCE CHECK, MULTIPLE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FORWARD CABIN. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600546 19990326 00546 NM 1999 3 26 ASAA9940055 1 19990226 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 14-18 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-18. RECONNECTED LIGHTS AND WIRING AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600547 19990326 00547 NM 1999 3 26 ASAA9940051 1 19990217 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 PDX - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED W IRING AND LIGHTS, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600548 19990326 00548 NM 1999 3 26 ASAA9940050 1 19990216 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PDX - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED W IRING AND LIGHTS, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600549 19990326 00549 NM 1999 3 26 ASAA9910018 1 19990228 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER 'EXIT TO REAR' LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AN D LIGHT ASSEMBLY. LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600550 19990326 00550 NM 1999 3 26 99ZZZM201 1 19990228 A 3350 8731002142 LIGHT BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER 'EXIT TO REAR' LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AN D LIGHT ASSEMBLY. LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600551 19990326 00551 NM 1999 3 26 ASAA9910017 1 19990227 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM ROW 2 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 2. REPLACED B ATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600552 19990326 00552 NM 1999 3 26 ASAA9910016 1 19990217 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM ROW 12/18 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 742AS 23136 SEA - PRIOR TO FLIGHT 61, THE NUMEROUS EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AT RO W 12 AND BATTERY AND RECEIVER AT ROW 18, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600553 19990326 00553 NM 1999 3 26 ASAA9910015 1 19990216 A 3350 6104781 BATTERY BOEING 737 737298C 1384490 NM ROW 5 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 745AS 20794 SEA - PRIOR TO FLIGHT 61, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 5 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND R ECEIVER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600554 19990326 00554 NM 1999 3 26 99ZZZM202 1 19990216 A 3350 883200312 RECEIVER BOEING 737 737298C 1384490 NM ROW 5 INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 745AS 20794 SEA - PRIOR TO FLIGHT 61, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 5 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND R ECEIVER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600555 19990326 00555 NM 1999 3 26 ASAA9940017 1 19990210 A 5320 SUPPORT BOEING 737 7374Q8 NM BS 945 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING SCHEDULED SI, THE FLOOR SUPPORT IN THE LOWER AFT CARGO COMPARTMENT AT BS 945 WAS FOUND TO BE CORRODED. REP AIRED PER EA 5320-01358. (M) 2 L 7 2 4F RT A16WE 1999032600556 19990326 00556 NM 1999 3 26 ASAA9940016 1 19990210 A 5320 WEB BOEING 737 7374Q8 NM BS 294-312 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING SCHEDULED SI, GOUGES WERE FOUND IN THE SHEAR WEB ASSEMBLY UPPER SURFACE AT STATION 294-312 LBL 11. REPAIRE D PER EA 5310-01644 AND BOEING TELEX ASA-SEA-99-0053RR. (M) 2 L 7 2 4F RT A16WE 1999032600557 19990326 00557 NM 1999 3 26 ASAA9940015 1 19990210 A 5320 6978602 BRACKET BOEING 737 7374Q8 NM BS 727 FRETTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING SCHEDULED SI, FRETTING WAS FOUND ON THE ANGLE BRACKET LOWER FUSELAGE STATION 727 RBL 10. REPAIRED PER EA 5 320-01333. (M) 2 L 7 2 4F RT A16WE 1999032600558 19990326 00558 NM 1999 3 26 ASAA9940014 1 19990210 A 5315 FLOORBEAM BOEING 737 7374Q8 NM BS 772 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING SCHEDULED SI, THE UPPER FLANGE OF THE CARGO FLOORBEAM AT STATION 772 WAS FOUND TO BE CORRODED. REPAIRED PE R EA 5310-01646. (M) 2 L 7 2 4F RT A16WE 1999032600559 19990326 00559 NM 1999 3 26 ASAA9940013 1 19990210 A 4910 6566213 SHROUD BOEING 737 7374Q8 NM APU CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING SCHEDULED SI, THE APU LOWER SHROUD WAS FOUND TO BE CHAFED ON THE FORWARD LEFT SIDE. REPAIRED PER EA 4910-0 1028. (M) 2 L 7 2 4F RT A16WE 1999032600560 19990326 00560 NM 1999 3 26 ASAA9940053 1 19990217 A 2560 SLIDE BOEING 737 7374Q8 NM PAX DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 SAN - PRIOR TO FLIGHT 557, THE R2 DOOR SLIDE WAS NOT DISARMED WHEN DOOR WAS OPENED AND SLIDE DID NOT DEPLOY. FERRIED AI RCRAFT TO SEA FOR REPAIR DUE TO SLIDE NOT BEING ABLE TO BE RESTOWED. SEA MAINTENANCE REPLACED THE R1 DOOR SLIDE. THE S LIDE WAS ROUTED TO THE SHOP WHERE IT WAS ADJUSTED AND REPACKED. (M) 2 L 7 2 4F RT A16WE 1999032600561 19990326 00561 NM 1999 3 26 ASAA9940052 1 19990216 A 5210 MECHANISM BOEING 737 737490 1384715 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 791AS 28886 SEA - PRIOR TO FLIGHT 76, THE L1 DOOR WAS FOUND TO BE DIFFICULT TO OPEN OR CLOSE. INSPECTED DOOR, NO DEFECTS NOTED. LU BRICATED DOOR AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600562 19990326 00562 NM 1999 3 26 ASAA9940054 1 19990225 A 5240 MECHANISM BOEING 737 737490 1384715 NM L2 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 797AS 28892 LAX - PRIOR TO FLIGHT 675, THE L2 DOOR WAS REPORTED AS BINDING. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600563 19990326 00563 NM 1999 3 26 ASAA9940057 1 19990227 A 5240 69703751 LEVER BOEING 737 7374Q8 NM R1 DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 PDX - DURING MAINTENANCE CHECK, THE R1 DOOR WOULD NOT STAY OPEN WITH THE LEVER ASSEMBLY. REPLACED HOLD OPEN LEVER ASSEM BLY AND DOOR REMAINS OPEN NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600564 19990326 00564 NM 1999 3 26 ASAA9940018 1 19990210 A 5315 FLOORBEAMS BOEING 737 7374Q8 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING SCHEDULED SI, FOUND CORROSION IN THE UPPER FLANGE OF THE CARGO FLOORBEAMS BETWEEN BS 727F AND 727G. REPAIR ED PER EA 5310-01645. (M) 2 L 7 2 4F RT A16WE 1999032600565 19990326 00565 NM 1999 3 26 ASAA9940010 1 19990130 A 5210 MECHANISM BOEING 737 737490 1384715 NM L1 DOOR LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 794AS 28889 SEA - PRIOR TO FLT 681 - THE L1 DOOR WAS VERY DIFFICULT TO OPEN. LUBRICATED THE L1 DOOR CAM PLATES AND THE DOOR OPERATE D NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600566 19990326 00566 WP 1999 3 26 ASAA9980040 1 19990210 A 3350 6011779 POWER SUPPLY MIDLANDROSS DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 12041 0827 53063 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600567 19990326 00567 WP 1999 3 26 ASAA9980039 1 19990210 A 3397 WIRE MARATHON DOUG DC9 DC982 3022082 WP ROW 1-9 BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 9 WERE FOUND INOPERATIVE. REPAIRED WIRI NG IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999032600568 19990326 00568 WP 1999 3 26 ASAA9980036 1 19990209 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP ROW 21 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 21 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600569 19990326 00569 WP 1999 3 26 ASAA9980035 1 19990207 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 17 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY FLOOR TRACK LIGHTS AT ROW 17 WERE FOUND INOPERATIVE. REPLACED WIRIN G IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600570 19990326 00570 WP 1999 3 26 ASAA9980034 1 19990203 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600571 19990326 00571 WP 1999 3 26 ASAA9980033 1 19990202 A 3350 6011779 POWER SUPPLY MIDLANDROSS DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 24466 0189 53021 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600572 19990326 00572 WP 1999 3 26 ASAA9980032 1 19990128 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600573 19990326 00573 WP 1999 3 26 ASAA9980031 1 19990129 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 975AS 53451 PDX - FLT 583 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS IN FIRST CLASS WERE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999032600574 19990326 00574 NM 1999 3 26 ASAA9940012 1 19990205 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 14 DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 773AS 25106 LAX - PRIOR TO FLIGHT 137 - CREW REPORTED THAT THE EMERGENCY EXIT TRACK LIGHTS WERE INOPERATIVE AT ROW 14. RECONNECTED WIRING TO LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600575 19990326 00575 NM 1999 3 26 ASAA9940011 1 19990203 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 PDX - DURING MAINTENANCE CHECK, TWO FORWARD RED EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED L IGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600576 19990326 00576 NM 1999 3 26 ASAA9940009 1 19990127 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 15-18 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 705AS 29318 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15-18 WERE FOUND TO BE INOPERATIVE. RECON NECTED WIRING/LIGHT, AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600577 19990326 00577 NM 1999 3 26 ASAA9910014 1 19990209 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 745AS 20794 SEA - PRIOR TO FLIGHT 61, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED SMOKE BARRIER BATTERY, B ATTERY PACK AT ROW 12, AND MID POSITION TRANSMITTER BATTERY. ALL EMERGENCY LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600578 19990326 00578 NM 1999 3 26 99ZZZM203 1 19990209 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM ROW 12 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 745AS 20794 SEA - PRIOR TO FLIGHT 61, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED SMOKE BARRIER BATTERY, B ATTERY PACK AT ROW 12, AND MID POSITION TRANSMITTER BATTERY. ALL EMERGENCY LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600579 19990326 00579 NM 1999 3 26 99ZZZM204 1 19990209 A 3350 6104781 TRANSMITTER BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 745AS 20794 SEA - PRIOR TO FLIGHT 61, SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED SMOKE BARRIER BATTERY, B ATTERY PACK AT ROW 12, AND MID POSITION TRANSMITTER BATTERY. ALL EMERGENCY LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600580 19990326 00580 NM 1999 3 26 ASAA9910013 1 19990207 A 3350 RPSIB BATTERY CHARGER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 730AS 22577 ANC - PRIOR TO FLT 64, THE INTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY CHARG ER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600581 19990326 00581 NM 1999 3 26 ASAA9910012 1 19990203 A 3350 6104781 TRANSMITTER GRIMES BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 730AS 22577 SEA - AFTER RECON AND PRIOR TO FLIGHT 61, SEVERAL EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED MI D POSITION TRANSMITTER AND RECEIVER AT ROW 12, ALL LIGHTS OPERATE NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600582 19990326 00582 NM 1999 3 26 99ZZZM205 1 19990203 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 730AS 22577 SEA - AFTER RECON AND PRIOR TO FLIGHT 61, SEVERAL EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED MI D POSITION TRANSMITTER AND RECEIVER AT ROW 12, ALL LIGHTS OPERATE NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600583 19990326 00583 NM 1999 3 26 ASAA9910011 1 19990201 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE OVERWING EXIT SIGNS WERE FLASHING WITH THE EMERGENCY LIGHTS ON. REPLACED BATTERY PA CK AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600584 19990326 00584 NM 1999 3 26 ASAA9910010 1 19990131 A 3350 RPS1B BATTERY CHARGER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 730AS 22577 ANC - AFTER RECON AND PRIOR TO FLIGHT 64, BOTH OVERWING EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY C HARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600585 19990326 00585 NM 1999 3 26 99ZZZM206 1 19990131 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 730AS 22577 ANC - AFTER RECON AND PRIOR TO FLIGHT 64, BOTH OVERWING EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY C HARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600586 19990326 00586 NM 1999 3 26 ASAA9910009 1 19990128 A 3350 883200312 RECEIVER BOEING 737 737298C 1384490 NM PALLET 6 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHT AT PALLET 6 WOULD NOT EXTINGUISH. REPLACED BATTERY, NO HELP. REPLACED RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999032600587 19990326 00587 NM 1999 3 26 ASAA9910008 1 19990128 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM PALLET 6-8 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT PALLET 6-8 WERE OPERATING ERRATIC. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600588 19990326 00588 NM 1999 3 26 99ZZZM207 1 19990128 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM PALLET 6-8 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT PALLET 6-8 WERE OPERATING ERRATIC. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600589 19990326 00589 NM 1999 3 26 ASAA9910007 1 19990126 A 3350 8731002142 LIGHT BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999032600590 19990326 00590 WP 1999 3 26 ARWA990304 1 19990306 A 3246 26014112 WHEEL DOUG DC8 DC862 3021970 WP LT MLG FAILED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 802BN B2291 45909 MIA - FLT 807 - BLOCK TURN BACK, AT THE BEGINNING OF TAKEOFF HEARD A LOUD NOISE FROM LEFT MLG WHEEL WELL. RETURNED TO R AMP. MAINTENANCE FOUND NR 6 MLG WHEEL INBOARD HALF FLANGE HAD SEPARATED AND TIRE WAS MISSING. WHEEL PARTS AND TIRE WER E RECOVERED. NR 6 MLG TIRE ASSY WAS CHANGED, AND NR 5 WAS CHANGED AS A PRECAUTIONARY MEASURE. THE CAUSE OF THE WHEEL F AILURE REMAINS UNDER INVESTIGATION. (M) 2 L 7 4 4F 4A25 1999032600591 19990326 00591 WP 1999 3 26 ARWA990302 1 19990303 A 2910 SWIVEL JOINT DOUG DC8 DC863F 302198F WP HYD SYSTEM LEAKING A ARWA B EMER. DESCENT J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 19 441J 45988 SJU - FLT 760 - IN FLIGHT EMERGENCY DECLARED IN CRUISE HYD QTY DROPPED TO HALFWAY ON QTY GAUGE, FOLLOWED BY AN ODOR OF H YD FLUID (NOXIOUS). AIRCRAFT LANDED IN MIAMI WITHOUT INCIDENT. INVESTIGATION REVEALED FLUID ESCAPING FROM CARGO DOOR S WIVEL JOINT. REMOVED AND REPLACED SWIVEL AND AUX PUMP PRESSURE LINE. OPS CHECK OK IAW MM 29-20-2, 52-38-1 AND 20-60-0. (M) 2 L 7 4 4F 4A25 1999032600592 19990326 00592 1999 3 26 99ZZZM208 4 19990125 A 2565 24D30053111 SLIDE DOUG DC10 DC1010 3022110 WP L1 DOOR BLOWN A RYNA K NONE O OTHER TX TAXI/GRND HDL 1 CE 07 572SC 46977 FLT 6001 - SFO - L1- DOOR SLIDE INADVERTENTLY INFLATED/DEPLOYED. REPLACED L-1 DOOR SLIDE. (M) 2 L 7 3 4F A22WE 1999032600593 19990326 00593 NM 1999 3 26 99ZZZM209 1 19990207 A 3610 652673831 DUCT BOEING 727 727222 1384073 NM NR 2 ENGINE WORN A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 7635U 19908 FLT 397 - HAD AN AIR TURN BACK TO TPA, ON CLIMB-OUT, ENGINE NR 2 FIRE INDICATION ILLUMINATED, RETARDED LEVER, LIGHT STAY ED ILLUMINATED FOR A FEW SECONDS, DID INFLIGHT SHUTDOWN, RETURNED FOR LANDING. REPLACED NR 2 ENGINE 'Y' DUCTING FOR 13T H STAGE. (M) 2 L 7 3 4F A3WE 1999032600594 19990326 00594 NM 1999 3 26 99ZZZM210 1 19990205 A 2612 FIRE LOOP BOEING 727 727222 1384073 NM NR 2 ENGINE CHAFED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 7635U 19908 FLT 333 - HAD AN AIR TURN BACK TO TPA, NR 2 FIRE WARNING INDICATION ON CLIMB-OUT, LIGHT EXTINGUISHED WHEN THRUST LEVER W AS RETARDED. REQUIRED FIRE LOOP END CHAFING ON ENGINE COWL. NO FIRE DETECTION ON ENGINE RUN UP. (M) 2 L 7 3 4F A3WE 1999032600595 19990326 00595 NM 1999 3 26 99ZZZM211 1 19990213 A 3230 RETRACT MECH BOEING 727 72722C 138400F NM NLG LACK OF LUBE A RYNA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 428EX 19097 FLT 620 - DTW - NOSE GEAR FAILED TO EXTEND ON FIRST TWO ATTEMPTS, THIRD ATTEMPT GEAR EXTENDED NORMALLY. FOUND NOSE GEAR DRY. LUBED GEAR AND THEN SWUNG NOSE GEAR FIVE TIMES WITH LUBE BETWEEN EACH SWING. NOSE GEAR EXTENSION AND RETRACTION NORMAL. (M) 2 L 7 3 4F A3WE 1999032600596 19990326 00596 NE 1999 3 26 99ZZZM212 2 19990126 A 7200 ENGINE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 FAILED A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 GCRPH 424 V0105 FLT 8251 IN DEN, NR 1 ENGINE FIRE INDICATION FOLLOWED BY ENGINE FAILURE. RETURNED TO DEN, OVERWEIGHT LANDING. NR 1 EN GINE CHANGE IS SCHEDULED IN DEN. (M) 2 L 7 2 4F 4 F RT A28NM E311NE 1999032600597 19990326 00597 NM 1999 3 26 99ZZZM213 1 19990205 A 3610 R18950T CLAMP BOEING 727 727222 1384073 NM NR 2 ENGINE WORN A RYNA K NONE J WARNING INDICATION CR CRUISE 1 CE 07 7635U 19908 FLT 333 - EN ROUTE FROM TPA-DAY - NR 2 ENGINE FIRE WARNING ON MOMENTARILY. FOUND LEAKING DUCT CLAMP AT START VALVE UPPE R CLAMP. REPLACED SAME. (M) 2 L 7 3 4F A3WE 1999032600598 19990326 00598 WP 1999 3 26 99ZZZM214 1 19990202 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP ROW 23C LOOSE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 571SC 46645 FLT 008 IN SFO, EMERGENCY FLOOR LIGHT STRIP UNDER SEAT 23C IS LOOSE. REINSERT EMERGENCY FLOOR LIGHT STRIPS, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A22WE 1999032600599 19990326 00599 EU 1999 3 26 99ZZZM215 1 19990203 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU L2/R2 DOOR INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GCPFR 437 FLT 8160 - SFO - EXIT LIGHTS AT L2/R2 DOORS AND OVEWING INOPERATIVE WHEN CABIN LIGHTS ARE TURNED OFF. PERFORMED TASK 33 -51-00-710-00400 (CHECK OF ALL EMERGENCY CABIN LIGHTS AND SIGNS ILLUMINATED BY BATTERIES) FOUND SYSTEM NORMAL. (M) 2 L 7 2 4F RT A28NM 1999032600600 19990326 00600 NM 1999 3 26 F3LA99011 1 19990221 A 5753 WEDGE BOEING 737 737201 1384454 NM LT TE FLAP CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED 1 INCH BY 1.5 INCH CRACK IN LEFT WING TRAILING EDGE FLAP WEDGE. MAINTENANCE R EPAIRED PER SRM 57-50-1, FIG 16, DETAIL 15. (M) 2 L 7 2 4F A16WE 1999032600601 19990326 00601 NM 1999 3 26 F3LA99012 1 19990221 A 5730 SKIN BOEING 737 737201 1384454 NM RT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED A .125 INCH CRACK ON RIGHT WING UPPER WING SKIN AT NR 5 SPOILER CENTER HINGE. MAINTENANCE REPAIRED PER SRM 57-30-1, FIG 4, DETAIL 7. (M) 2 L 7 2 4F A16WE 1999032600602 19990326 00602 NM 1999 3 26 F3LA99013 1 19990221 A 5311 RIB BOEING 737 737201 1384454 NM BS 505 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, RERPORTED CRACK ON FORWARD SIDE OF RIB AT BS 505. MAINTENANCE REPLACED RIB PER SRM 51- 10-1, PAGE 5, AND 51-30-2. (M) 2 L 7 2 4F A16WE 1999032600603 19990326 00603 NM 1999 3 26 F3LA99014 1 19990221 A 5280 DOOR BOEING 737 737201 1384454 NM LT MLG BENT A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED LEFT MAIN GEAR AFT OUTER CORNER OF INBOARD DOOR BENT AND BULGING. MAINTENANCE REMOVED FASTENERS, CLEANED AREA, RESEALED AND INSTALLED NEW FASTENERS PER SRM 51-20-4 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1999032600604 19990326 00604 NM 1999 3 26 F3LA99022 1 19990221 A 5751 FITTING BOEING 737 737201 1384454 NM LT AILERON BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED LEFT WING CENTER AILERON HINGE FITTING AFT END BROKEN. MAINTENANCE REMOVED DA MAGED AREA, FABRICATED ATTACH ANGLE AND REPAIRED PER SRM 51-30-2, 51-20-3, AND 51-20-1 AND 51-40-4. (M) 2 L 7 2 4F A16WE 1999032600605 19990326 00605 NM 1999 3 26 F3LA99021 1 19990209 A 3350 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE RECHAR GED BATTERY PACK PER MM 33-51-11. (M) 2 L 7 2 4F A16WE 1999032600606 19990326 00606 NM 1999 3 26 F3LA99020 1 19990222 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN BROKEN A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED CABIN EMERGENCY LIGHTING AND FLOOR PROXIMITY LIGHTING INOPERATIVE. MAINTENANC E REPAIRED WIRING AT OVERWING BATTERY PCK PER WDM 33-51-01. (M) 2 L 7 2 4F A16WE 1999032600607 19990326 00607 NM 1999 3 26 F3LA99019 1 19990222 A 3397 WIRE BOEING 737 737201 1384454 NM L1 DOOR BROKEN A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED BROKEN WIRE IN L1 DOOR EXIT LIGHT. MAINTENANCE REPAIRED BROKEN WIRE PER SPWM 20-30-12. (M) 2 L 7 2 4F A16WE 1999032600608 19990326 00608 NM 1999 3 26 F3LA99015 1 19990221 A 5753 SKIN BOEING 737 737201 1384454 NM LT TE MIDFLAP CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION REPORTED A 1.25 INCH CRACK ON LEFT WING TRAILING EDGE INBOARD MIDFLAP INBOARD EDGE FLAP REAR SPAR T-CHORD. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-4, FIG 1 5 1-40-3 AND 51-30-02. (M) 2 L 7 2 4F A16WE 1999032600609 19990326 00609 NM 1999 3 26 F3LA99018 1 19990221 A 7830 STIFFENERS BOEING 737 737201 1384454 NM NR 2 TR UNIT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED WEB STIFFENERS ON FORWARD EDGE OF NR 2 ENGINE THRUST REVERSER COWL CRACKED. M AINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, FIG 1. (M) 2 L 7 2 4F A16WE 1999032600610 19990326 00610 NM 1999 3 26 F3LA99016 1 19990222 A 3610 BRACKET BOEING 737 737201 1384454 NM BLEED DUCT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED FASTENER MISSING AND CRACKED MOUNT FLANGE ON 8TH STAGE BLEED DUCT. MAINTENANC E INSTALLED FASTENER AND REPAIRED BRACKET/FLANGE PER 727 OHM 36-10-3, PAGE 5. (M) 2 L 7 2 4F A16WE 1999032600611 19990326 00611 NM 1999 3 26 F3LA99006 1 19990221 A 5311 FRAME BOEING 737 737201 1384454 NM BS 360 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED A 4.5 INCH CRACK IN FRAME AT BS 360, BETWEEN STRINGER 21R AND 22R. MAINTENANC E REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, 51-40-3, AND 53-10-4. (M) 2 L 7 2 4F A16WE 1999032600612 19990326 00612 NM 1999 3 26 F3LA99007 1 19990222 A 5312 BULKHEAD FRAME BOEING 737 737201 1384454 NM CARGO COMPT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED FORWARD CARGO RIGHT FORWARD BULKHEAD FRAME CRACKED. MAINTENANCE REMOVED DAMAG ED SECTION , FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-3, FIG 1. (M) 2 L 7 2 4F A16WE 1999032600613 19990326 00613 NM 1999 3 26 F3LA99008 1 19990220 A 5730 SKIN BOEING 737 737201 1384454 NM LT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED A .5 INCH CRACK IN LEFT WING UPPER SKIN AT WBL 157. MAINTENANCE STOP DRILLED CRACK, FABRICATED DOUBLER/TRIPLER AND REPAIRED PER EO B737-5723-0001 AND DRAWING 65C30113. (M) 2 L 7 2 4F A16WE 1999032600614 19990326 00614 NM 1999 3 26 F3LA99009 1 19990222 A 5730 SKIN BOEING 737 737201 1384454 NM RT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED DENT AND CRACK ON RIGHT WING OUTBOARD SIDE OF PYLON, FLAP SIDE LOAD ROLLER AND CORROSION UNDER FLAP ROLLER WEAR STRIP. MAINTENANCE REMOVED DAMAGED SECTION. FABRICATED REPLACEMENT PARTS AND REPAIRE D PER SRM 51-30-3 AND EA B737-5430-0021. (M) 2 L 7 2 4F A16WE 1999032600615 19990326 00615 NM 1999 3 26 F3LA99010 1 19990222 A 5311 FRAME BOEING 737 737201 1384454 NM BS 380 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED A 4 INCH CRACK IN FRAME AT BS 380, BETWEEN STRINGER 21R AND 22R. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-4, FIG 1. (M) 2 L 7 2 4F A16WE 1999032600616 19990326 00616 SO 1999 3 26 ASOA99028 1 19990220 A 2120 AIR DIST EMB 120 EMB120RT SO COCKPIT ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 285AS 120265 ON CLIMB-OUT ATL-VLD, CREW SMELLED STRONG SMOKE ODOR. AN EMERGENCY WAS DECLARED AND FLIGHT RETURNED TO ATL, WHERE LANDIN G WAS MADE SAFELY AND PASSENGERS DEPLANED AS QUICKLY AS POSSIBLE. ATL, MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY O N THE GROUND. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999032600617 19990326 00617 NE 1999 3 26 ASOA99025 2 19990216 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 11 275AS 20964 120234 115385 FLT 4069 - EN ROUTE ATL-CRW AT FL230, THE LEFT ENGINE 'ENGINE CONTROL' AND 'OIL PRESSURE' AURAL WARNINGS CAME ON. CREW NOTED THAT THE OIL PRESSURE, NH AND TORQUE ALL READ ZERO, WITH AN OIL PRESSURE LIGHT ON THE MAP. CREW SHUT DOWN THE LEF T ENGINE, DECLARED AN EMERGENCY, ELECTRICALLY FEATHERED THE LEFT ENGINE AND LANDED UNEVENTFULLY AT TRI. ASA MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999032600618 19990326 00618 SO 1999 3 26 ASOA99027 1 19990219 A 2131 22201T011400 CONTROLLER EMB 120 EMB120RT SO COCKPIT DEFECTIVE A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 280AS 23653 120231 EN ROUTE ATL-FLO, AT 19,000 FEET, CABIN STARTED TO CLIMB AT 2,000 FPM. CREW PERFORMED DECOMPRESSION CHECKLIST AND DESCEN DED TO 10,000 FEET. OXYGEN MASKS WERE NOT DEPLOYED AS CABIN NEVER EXCEEDED 10,500 FEET. FLIGHT CONTINUED TO FLO, PRESSU RE WAS CONTROLLED IN MANUAL MODE, AND LANDING WAS MADE WITHOUT FURTHER INCIDENT. ON THE RETURN TRIP TO ATL AT 10,000 FE ET, THE PRESSURIZATION WORKED NORMALLY IN AUTO AND MANUAL MODES. ATL MAINTENANCE REMOVED AND REPLACED THE AUTO CONTROLL ER. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999032600619 19990326 00619 EU 1999 3 26 ASOA99026 1 19990218 A 2730 WIRE AEROSP ATR72 ATR72212 EU ELEVATOR CHAFED A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 11 642AS 395 EN ROUTE MGM-ATL AT 11,000 FEET, A PITCH DISCONNECT WARNING OCCURRED. CREW DECLARED AN EMERGENCY AND LANDED IN ATL WITHO UT FURTHER INCIDENT. ATL MAINTENANCE FOUND CHAFFED WIRES AT THE DISCONNECT PROX SENSOR. REPLACED AND SECURED WIRES. OP ERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 H 7 2 4T RT A53EU 1999032600620 19990326 00620 WP 1999 3 26 USAA990106 1 19990212 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT UPPER AND LOWER HAT CHANNEL OF LONGERON AT STATION 965 LONGERON 17 RT. S PLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999032600621 19990326 00621 WP 1999 3 26 USAA990107 1 19990212 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN UPPER AND LOWER HAT SECTION OF LONGERON 17 LEFT STATION 965. MANUFACTURED REPAIR PIECES, LONGERON SPLICES PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999032600622 19990326 00622 WP 1999 3 26 USAA990108 1 19990212 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN UPPER AND LOWER HAT SECTION OF LONGERON 16 LEFT STATION 965. MANUFACTURED REPAIR PIECES, LONGERON SPLICES PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999032600623 19990326 00623 WP 1999 3 26 USAA990109 1 19990212 A 5312 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK AT STATION 965 BULKHEAD LEFT WEB. REPLACED WEB PER DACO DRAWING 9912243. (M ) 2 L 7 2 4F A6WE 1999032600624 19990326 00624 WP 1999 3 26 USAA990110 1 19990212 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756-775 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK, .25 INCH CRACK AND 4 INCH CRACK AT LONGERON 17 BETWEEN STATION 756-775. SP LICED IN NEW SECTION OF SKIN PER EA NR 51416. (M) 2 L 7 2 4F A6WE 1999032600625 19990326 00625 WP 1999 3 26 USAA990111 1 19990212 A 5210 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND .5625 INCH CRACK IN SKIN AT MED NEAR HANDLE CUTOUT AT STATION 179, Z=33.75. INSTALLED REP AIR DOUBLER PER 51395. (M) 2 L 7 2 4F A6WE 1999032600626 19990326 00626 WP 1999 3 26 USAA990112 1 19990212 A 5312 BULKHEAD FRAME DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AT STATION 965 BULKHEAD BELTFRAME OUTBOARD LONGERONS 16-17 LEFT. SPLICED I N A NEW SECTION OF FRAME PER DACO DRAWING NR 9912243. (M) 2 L 7 2 4F A6WE 1999032600627 19990326 00627 WP 1999 3 26 USAA990113 1 19990212 A 5230 59101417 PAN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND .375 INCH CRACK AT FORWARD CARGO DOOR OUTER PAN AT LOWER STOP RADIUS FORWARD SIDE. ROUTED CRACK AND INSTALLED TWO 'L' DOUBLERS PER EA 51383. (M) 2 L 7 2 4F A6WE 1999032600628 19990326 00628 WP 1999 3 26 USAA990115 1 19990212 A 5210 9955757 BEAM DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN MAIN ENTRANCE DOOR BEAM NR 6. INSTALLED DOUBLER AND REPAIRED PER EA 51375 . (M) 2 L 7 2 4F A6WE 1999032600629 19990326 00629 WP 1999 3 26 USAA990116 1 19990212 A 5210 PAN DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 3 INCH LONG CRACK AT FORWARD LOWER CORNER PAN SECTION AT HINGE CUTOUT. REPAIRED WITH IDEN TICAL PART NR 591412161N PER DACO DWG J060213. (M) 2 L 7 2 4F A6WE 1999032600630 19990326 00630 WP 1999 3 26 USAA990117 1 19990212 A 5320 CLIP DOUG DC9 DC931 3022065 WP BS 980 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK AND 1 INCH CRACK ON SKIN CLIP AT STATION 980 BETWEEN LONGERONS 16-14 RT. REP AIRED PER DACO DRAWING 9958238. (M) 2 L 7 2 4F A6WE 1999032600631 19990326 00631 WP 1999 3 26 USAA990118 1 19990212 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AT STATION 965 BULKHEAD RT, BELTFRAME BETWEEN LONGERON 16-15. SPLICED IN N EW SECTION OF FRAME PER DACO DRAWING NR 9912243. (M) 2 L 7 2 4F A6WE 1999032600632 19990326 00632 NM 1999 3 26 USAA990069 1 19990202 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 1070 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 44311 22882 TPA - DURING METRO JET CONVERSION VISUAL INSPECTION, FOUND 3 SMALL CRACKS .125 INCH, .25 INCH AND .5 INCH FROM RIVET HOL ES NEAR APU FIRE EXT INDICATOR CUTOUT STATION 1070 STRINGER 23R SKIN. INSTALLED DOUBLERS PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999032600633 19990326 00633 NM 1999 3 26 USAA990082 1 19990212 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 1141 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STRINGER 12R STATION 1141 ANGLE RADIUS. SPLICED ANGLE PE R SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1999032600634 19990326 00634 NM 1999 3 26 USAA990071 1 19990212 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT TOP SURFACE 'T' CAP STATION 312 LBL 40 - LBL 36 FLOORBEAM. REPAIRED ANGLES 'T' CAP PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999032600635 19990326 00635 NM 1999 3 26 USAA990072 1 19990212 A 5330 SKIN BOEING 737 737401 1384701 NM BS 795 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 4 INCH BS 795 BL 0 ON SKIN. REPAIRED DOUBLER EXTERN AL PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1999032600636 19990326 00636 NM 1999 3 26 USAA990073 1 19990212 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 8 INCH STATION 328 LBL 12 FLOORBEAM. REPAIRED 'T' CAP SLICE P ER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999032600637 19990326 00637 NM 1999 3 26 USAA990074 1 19990212 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 8 INCH CORROSION AT STATION 312 LBL 12 FLOOR SUPPORT. REMOVED AND REPLA CED SUPPORT PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999032600638 19990326 00638 NM 1999 3 26 USAA990076 1 19990212 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLES STATION 967 LBL 16 - LBL 50 FLOORBEAM. CORR OSION TASK NR C53-107-02. INSTALLED REPAIR STRAP PER SRM 53-00-57 FIG 203. (M) 2 L 7 2 4F RT A16WE 1999032600639 19990326 00639 NM 1999 3 26 USAA99075 1 19990212 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 859 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH CORRODED AREA AT BS 859 RBL 25 LBL 25 FLOOR SUPPORT. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER TR 53-10-06. (M) 2 L 7 2 4F RT A16WE 1999032600640 19990326 00640 NM 1999 3 26 USAA990077 1 19990212 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 30 INCH AREA OF CORROSION STATION 344 FLOORBEAM. SPLICED IN 'T' CAP A ND DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999032600641 19990326 00641 NM 1999 3 26 USAA990078 1 19990212 A 5347 CARGO TRACK BOEING 737 737401 1384701 NM BS 947.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION BS 947.5 LBL 14.5 AFT CORNER CARGO TRACK TIE DOWN CHANNEL. CORROSION TASK NR C53-202-01. SPLICED IN DOUBLER PER SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 1999032600642 19990326 00642 NM 1999 3 26 USAA990079 1 19990212 A 5347 CARGO TRACK BOEING 737 737401 1384701 NM BS 767-867 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 16 INCH AREA OF CORROSION BS 767-867 RBL 14.5 CARGO TRACK TIE DOWN CHANNEL. CORROSION TASK NR C53-202-01. SPLICED IN NEW TRACK SECTION PER SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 1999032600643 19990326 00643 NM 1999 3 26 USAASB99049 1 19990222 A 3350 20121 POWER SUPPLY BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 336US 23233 SYR - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999032600644 19990326 00644 WP 1999 3 26 ORJA9984 1 19990224 A 5230 59175501 SWITCH DOUG DC9 DC987 3022087 WP CARGO DOOR OUT OF ADJUST A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 11 752RA 49780 AT LAS, GATE RETURN, WHEN THROTTLES ADVACED FOR TAKEOFF, FORWARD CARGO COMPARTMENT DOOR LIGHT CAME ON. TAKEOFF DISCONTI NUED AT LOW SPEED. LIGHT WENT OUT DURING TAXI IN. ADJUSTED FORWARD CARGO DOOR SWITCH. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999032600645 19990326 00645 WP 1999 3 26 ORJA9985 1 19990222 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROW 1 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, EMERGENCY LIGHT AT SEAT ON ROW 1 INOPERABLE. FIXED BROKEN WIRE AT SEAT ON ROW 1 EMERGENCY LIGHT. OPS CHECK GOO D. (M) 2 L 7 2 4F RT A6WE 1999032600646 19990326 00646 WP 1999 3 26 ORJA9986 1 19990220 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 1-9 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT BUR, EMERGENCY AISLE LIGHT ON ROWS 1-9 WILL NOT GO OUT. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999032600647 19990326 00647 WP 1999 3 26 ORJA9987 1 19990223 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROW 29 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY LIGHT OUT AT SEAT 1, ROW 29. REWIRED EMERGENCY LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600648 19990326 00648 WP 1999 3 26 ORJA9988 1 19990222 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 8-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 SJC - EMERGENCY EXIT LIGHTS ON ROWS 8-11 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ON RIGHT SIDE LOWER POS, ON FOR WARD EMERGENCY ESCAP HATCH. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999032600649 19990326 00649 NM 1999 3 26 ORJA9989 1 19990219 A 3620 CONTROLLER DOUG MD90 MD9030 3023690 NM E/E BAY MALFUNCTIONED A ORJA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 11 904RA 53570 AT SNA - TAIL TEMP FAULT LIGHT ILLUMINATED ON RUNWAY BEFORE TAKEOFF SNA. INTERGRATED PNEUMATIC OVERHEAT DETECTION CONTR OLLER, FAULTS CLEARED. (M) 2 L 7 2 4F RT A6WE 1999032600650 19990326 00650 NM 1999 3 26 P2EA99076 1 19990223 A 2910 BACH5M0187CCR LINE BOEING 737 737247 138448D NM ELEVATOR CRACKED A P2EA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 912MP 19607 MCI - FLT 817 - 'B' SYSTEM LOW QUANTITY LIGHT CAME ON SHORTLY CAME ON SHORTLY AFTER TAKEOFF, LOST 'B' SYSTEM PRESSURE LA NDED AT MCI UNEVENTFUL. FOUND HYDRAULIC FLEX LINE AT ELEVATOR CENTERING UNIT RUPTURED, INSTALLED TEMPORARY FLEX LINE PE R GMM 14-00 PAR B. (M) 2 L 7 2 4F A16WE 1999032600651 19990326 00651 NM 1999 3 26 P2EA99077 1 19990228 A 2424 915F2125 GCU BOEING 737 737222 1384473 NM NR 1 ENGINE FAILED A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 209US SZ2234E 19548 MDW - FLT 703 - ABORTED TAKEOFF AT 103 KNOTS DUE TO FAILURE OF THE NR 1 GENERATOR BUS TRANSFER SYSTEM. THE NR 4 MAIN TI RE BLEW OUT DURING ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT IAW MM 24-21-81. OPS CHECK NORMAL . REMOVED AND REPLACED NR 4 MAIN TIRE IAW MM 32-45-11. (M) 2 L 7 2 4F A16WE 1999032600652 19990326 00652 NM 1999 3 26 P2EA99078 1 19990302 A 1100 DATA PLATE BOEING 737 737222 1384473 NM NLG WW OUT OF ADJUST A P2EA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 603DJ 19955 DFW - FLT 815 - UPON GEAR SELECTED DOWN, RECEIVED INTERMITTENT GEAR WARNING GEAR UNSAFE (RED) LIGHT. SAME THING DURING TAXI IN. REMOVED COVER FOR NLG DOWN LOCK SENSOR. FOUND DATA PLATE RESTING AGAINST SENSOR TERMINAL BLOCK. VERIFIED REP ORTED CONDITION BY REPOSITION DATA PLATE. REMOVED LOOSE DATA PLATE FROM TERMINAL BLOCK, INSTALLED SENSOR COVER. SYSTEM OPS NORMAL PER MM 32-21-0, 32-61-0. (M) 2 L 7 2 4F A16WE 1999032600653 19990326 00653 NM 1999 3 26 BJNA990202 1 19990226 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 20336 EMERGENCY EXIT TRACK LIGHTING STRIP IS LOOSE. RESET FLOOR TRACK AS NECESSARY, OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1999032600654 19990326 00654 1999 3 26 WRLA99013 4 19990225 A 3451 6224540023 DME DOUG MD11 MD11 3023602 NM COCKPIT OVERHEATED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 272WA 18349 48437 FLT 5129 - DURING CRUISE, FLIGHT CREW NOTED LIGHT SMOKE AND BURNING ELECTRICAL SMELL IN COCKPIT. ADDITIONALLY, NR 2 DME CIRCUIT BREAKER POPPED. SMOKE APPEARED IN VICINITY OF CAPTAIN'S OVERHEAD MAP LIGHT. NON-ESSENTIAL OVERHEAD LIGHTING W AS SWITCHED OFF. DME CIRCUIT BREAKER WAS NOT RESET. SMOKE AND SMELL DISSIPATED. FLIGHT CONTINUED TO DESTINATION WITHO UT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND NR 2 DME INTERROGATOR TO HAVE EVIDENCE OF OVERHEATING. FURTHER INVEST IGATION FOUND NO FURTHER EVIDENCE OF DAMAGE. REPLACEMENT INTERROGATEOR NOT AVAILABLE. CIRCUIT BREAKER REMAINED PULLED. COLLARED BREAKER AND ASSIGNED DEFERRAL PER MEL. (M) 2 L 7 3 4F RT A22WE 1999032600655 19990326 00655 CE 1999 3 26 99ZZZM216 1 19990218 A 2750 1005240741 GEARBOX BEECH 1900 1900D 1154162 CE TE FLAPS STRIPPED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA 2657 2313 UE41 FLAPS FAILED TO RETRACT, FLAP MOTOR GEAR BOX FAILURE. REPLACED FLAP MOTOR/GEAR BOX ASSEMBLY IAW RAYTHEON MM CHAPTER 27. (M) 2 L 7 2 4T RT A24CE 1999032600656 19990326 00656 EU 1999 3 26 REXA99004 1 19990220 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A REXA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 25 360PX 340B220 LANDING GEAR WOULD NOT COME DOWN, YELLOW INTRANSIT LIGHT ONLY. NO GEAR LIGHTS. RESET CB M5, AND F7. PERFORMED MULTIPL E GEAR SWINGS, COULD NOT DUPLICATE DISCREPANCY. (M) 2 L 7 2 4T RT A52EU 1999032600657 19990326 00657 NM 1999 3 26 SWAA990540 1 19990321 A 2611 PU499R3 DETECTOR BOEING 737 7373H4 1384600 NM AFT LAVATORY DEFECTIVE A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 378SW 26585 AIR TURNBACK DUE TO AFTER TAKEOFF, THE AFT LAV SMOKE ALARM WENT OFF. REMOVED AND REPLACED SMOKE DETECTOR PER MM. 2 L 7 2 4F RT A16WE 1999032600658 19990326 00658 NM 1999 3 26 SWAA990541 1 19990319 A 3350 6556633 COVER BOEING 737 7372H4 138448C NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 EMERGENCY EXIT LENS COVERS, RIGHT HAND AND LEFT HAND OVERWING EXITS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999032600659 19990326 00659 NM 1999 3 26 SWAA990542 1 19990319 A 3350 079123 COVER BOEING 737 7372H4 138448C NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED 1/4D CHECK, FOUND EPLS TRACK LIGHTING LENS COVER CRACKED AND BROKEN AT FIRST 6 FEET IN FWD SECTION. RE MOVED AND REPLACED PER MM. 2 L 7 2 4F A16WE 1999032600660 19990326 00660 NM 1999 3 26 SWAA990543 1 19990321 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM RT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS ON RT OVERWING AND AFT CABIN ARE INOP. REMOVED AND REPLACED BATT ERY ASSEMBLIES PER MM. 2 L 7 2 4F A16WE 1999032600661 19990326 00661 NM 1999 3 26 SWAA990544 1 19990319 A 5320 WEB BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 NOSE WHEEL WELL, AFT BULKHEAD CRACKED AND RIVET SHEARED AT LT LOWER CORNER, (DUE TO BIRD STRIKE). REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999032600662 19990326 00662 NM 1999 3 26 SWAA990545 1 19990319 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L CHANNEL CRACKED AT STUB FRAME BS 360. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999032600663 19990326 00663 NM 1999 3 26 SWAA990552 1 19990320 A 5320 BAC1505 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE DOOR UPPER FWD FRAME CRACKED AT ASSIST HANDLE. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999032600664 19990326 00664 NM 1999 3 26 SWAA990546 1 19990320 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME CRACKED AT BS 616 LT SIDE CABIN FLOOR. REPAIRED PER SWA RA NR1-353-2042. 2 L 7 2 4F RT A16WE 1999032600665 19990326 00665 NM 1999 3 26 SWAA990547 1 19990321 A 5320 FRAME BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION, CRACKED UPPER FRAME ON AFT ENTRY DOOR CUTOUT FOR DOOR A SSIST HANDLE. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999032600666 19990326 00666 NM 1999 3 26 SWAA990548 1 19990319 A 5313 BAC1498157 STRINGER BOEING 737 7372T4 1384492 NM BS 324-336 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER 24L, BS 324 TO 336. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999032600667 19990326 00667 1999 3 26 SWAA990549 4 19990320 A 2565 D31354433 SLIDE BOEING 737 7375H4 138449D NM PASSENGER DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 L2 DOOR SLIDE PRESSURE GAUGE IN RED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999032600668 19990326 00668 NM 1999 3 26 SWAA990550 1 19990321 A 3350 300432 LIGHT BOEING 737 7375H4 138449D NM EMER EXIT DOOR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 EGRESS FLOOR LIGHTS AT OVERWING EXIT INOP. REMOVED AND REPLACED LIGHT FIXTURE PER MM. 2 L 7 2 4F RT A16WE 1999032600669 19990326 00669 NM 1999 3 26 SWAA990551 1 19990319 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM LT TE FOREFLAP PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED A1 CHECK, FOUND LEFT I/B FOREFLAP HAS .75 INCH PUNCTURE AT BOTTOM SIDE, 36 INCHES FROM I/B END. REPAIR ED PER SWA RA NR 1-357-0655 AND SRM. 2 L 7 2 4F RT A16WE 1999032600683 19990326 00683 NE 1999 3 26 99ZZZX1136 2 19990108 A 7250 397780 TURBINE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE ENGINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 301HC 3192 194 BB1219 PCE93902 PROPELLER STRIKE. DUE INSPECTION DUE TO SUDDEN STOPPAGE. PART CYCLES: 3192. 1 L 7 2 4T 4 T A24CE E4EA 1999032600684 19990326 00684 GL 1999 3 26 99ZZZX1137 3 19990108 A 6111 BLADE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE MCAULY 3G34C7 3GFR34C701 GL PROPELLER DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 301HC 1009 BB1219 PCE93902 842080 PROPELLER DAMAGED DUE TO PROPELLER STRIKE. THREE EACH BLADES REMOVED, P/N 100LA-2. S/N'S EJ-015, EJ-023, EJ-046. TIME SINCE NEW: 1,008.2 HOURS. 1 L 7 2 4T 4 T A24CE E4EA 5 C P60GL 1999032600690 19990326 00690 EU 1999 3 26 99ZZZX1143 1 19990226 A 3260 LIGHT STBROS SD3 SD330 8100602 EU COCKPIT INOPERATIVE A DATA A UNSCHED LANDING P NO WARNING INDICATION NR NOT REPORTED 1 GL 13 335MV SH3017 THE NOSE GEAR DOWN INDICATION LIGHT WAS INOPERATIVE SO THE CAPTAIN DECLARED AN EMERGENCY INTO BGR AND LANDED WITHOUT INC IDENCE. THE NOSE GEAR DOWN INDICATION LIGHT WAS FOUND TO BE DIRTY. THE MECHANIC CLEANED AND LUBED IT. OPS CHECK GOOD. 2 H 7 2 4T A41EU 1999032600692 19990326 00692 EU 1999 3 26 99ZZZX1145 1 19990302 A 2611 21562B SMOKE DETECTOR STBROS SD3 SD360 8100606 EU CARGO BAY MALFUNCTIONED A DATA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 GL 13 4498Y 7545 SH3625 EN ROUTE TO SDF, APPROXIMATELY 10 MINUTES FROM LANDING, THE FORWARD SMOKE CWP LIGHT CAME ON. THE CAPTAIN INSTRUCTED THE F/O TO DISCHARGE THE FORWARD HAND HELD FIRE EXTINGUISHER BOTTLE INTO THE FORWARD COMPARTMENT. THE AIRCRAFT LANDED WITH OUT INCIDENT. THERE WAS NO SMOKE OR FIRE FOUND DURING THE POST-FLIGHT INSPECTION. THE FIRE EXTINGUISHER WAS MEL'D. THE 2 SMOKE DETECTORS GIVING THE FALSE WARNING WERE REPLACED. OPS CHECK GOOD. 2 H 7 2 4T A41EU 1999032600693 19990326 00693 EU 1999 3 26 99ZZZX1146 1 19990302 A 2611 21562B SMOKE DETECTOR STBROS SD3 SD360 8100606 EU CARGO BAY MALFUNCTIONED A DATA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 GL 13 4498Y 7049 SH3625 EN ROUTE TO SDF, APPROXIMATELY 10 MINUTES FROM LANDING, THE FORWARD SMOKE CWP LIGHT CAME ON. THE CAPTAIN INSTRUCTED THE F/O TO DISCHARGE THE FORWARD HAND HELD FIRE EXTINGUISHER BOTTLE INTO THE FORWARD COMPARTMENT. THE AIRCRAFT LANDED WITH OUT INCIDENT. THERE WAS NO SMOKE OR FIRE FOUND DURING THE POST-FLIGHT INSPECTION. THE FIRE EXTINGUISHER WAS MEL'D. THE 2 SMOKE DETECTORS GIVING THE FALSE WARNING WERE REPLACED. OPS CHECK GOOD. 2 H 7 2 4T A41EU 1999032600694 19990326 00694 EA 1999 3 26 99ZZZX1147 2 19990302 A 7314 RG37060A FUEL PUMP ROMEC BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 2 ENGINE FAILED A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 01 45GL 68 B965 UC45 PCE32413 67.6 HOURS AFTER OVERHAUL, DRIVESHAFT BROKE. PUMP TURNS NORMAL, NO DAMAGE DETECTED INSIDE PUMP. 2 L 7 2 4T 4 T RT A24CE E4EA 1999032600709 19990326 00709 WP 1999 3 26 TWAA9904401 1 19990323 A 4990 OIL SYSTEM DOUG DC9 DC983 3022083 WP APU LEAKING A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 05 931TW 49527 A SMOKY HAZE WAS REPORTED AT REAR OF CABIN DURING LANDING AND TAXI. FOUND AN APU OIL LEAK. DEACTIVATED APU PER MEL PROCE DURES, AND REPLACED THE WATER SEPARATORS IN THE AIR CONDITIONING SYSTEMS. CHECK-C 1-15-99 MCI. *S/D* APPARENT CAUSE O F SMOKE WAS OVERSERVICING OF APU OIL. EXCESS OIL WAS DISCHARGED OUT THE GEARBOX VENT PLUG AND INJESTED BY THE AIR INLET . DRAINED APU OIL TANK TO PROPER LEVEL AND LEAK CHECKED UNIT. 2 L 7 2 4F RT A6WE 1999032600710 19990326 00710 WP 1999 3 26 TWAA9904402 1 19990323 A 3350 58222 BATTERY PACK DOUG DC9 DC932 3022066 WP ROW 16-21 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 995Z 47027 THE CABIN EGRESS LIGHTS WERE FOUND INOPERATIVE FROM SEAT ROW 16 TO 21. REPLACED BATTERY PACK. CHECK-C 8-31-98 MCI. 2 L 7 2 4F A6WE 1999032600711 19990326 00711 NM 1999 3 26 AT9900249 1 19990210 A 5730 SKIN BOEING 737 7372L9 1384497 NM RIGHT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION BULGED ON RIGHT WING LEADING EDGE. CUT OUT CORRODED AREA, FORME D FILLERS AND DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED REPAIR IAW B737 SRM 57-30-4 FIG 3, 51-10-2 AND 51-40-5. 2 L 7 2 4F RT A16WE 1999032600712 19990326 00712 WP 1999 3 26 AT9900250 1 19990315 A 5313 527779225 LONGERON DOUG DC9 DC932 3022066 WP BS 932 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION IN THE AFT CARGO PIT AT BS 932 L-22R. REMOVED AND REPLACED LONG ERON IAW DC9 SRM 51-10-2, 51-10-4, AND 53-02 FIG 18. SPLICE (P/N 3924814-501N) OFF 2 L 7 2 4F A6WE 1999032600713 19990326 00713 WP 1999 3 26 AT9900251 1 19990315 A 5313 5277795 LONGERON DOUG DC9 DC932 3022066 WP BS 932 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION IN THE AFT CARGO PIT AT BS 932 L-21R. REMOVED AND REPLACED LONG ERON IAW DC9 SRM 51-10-3, 51-10-4, AND 53-02 FIG 18. 2 L 7 2 4F A6WE 1999032600714 19990326 00714 WP 1999 3 26 AT9900252 1 19990316 A 2520 PANEL DOUG DC9 DC932 3022066 WP BS 965-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT SIDE WALL PANEL NR 3 AT BS 965 TO 996 CORRODED ON THE UPPER AND LOWE R SURFACE AROUND FASTENER HOLES. REMOVED CORROSION, FABRICATED NEW FLOOR PANEL IAW DC9 SRM 53-01 FIG 1. 2 L 7 2 4F A6WE 1999032600715 19990326 00715 WP 1999 3 26 AT9900253 1 19990316 A 5347 TIE DOWN DOUG DC9 DC932 3022066 WP BS 351-370 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE TIE DOWN PANEL FORWARD PIT FORWARD OF DOOR ON THE LOWER SURFACE CORROD ED, SCRATCHED AND GOUGE ON THE UPPER SURFACE AT BS 351 TO 370. REMOVED CORROSION, FABRICATED REPAIR PANEL, TREATED, PRI MED IAW DC9 SRM 53-01 FIG 1 AND 51-10-3. 2 L 7 2 4F A6WE 1999032600716 19990326 00716 WP 1999 3 26 AT9900254 1 19990321 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 990 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LONGERON SKIN L25-26L AT BS 990 CRACKED AND CORRODED. REMOVED STRINGE R TIE AND REMOVED CRACK, FOUND CORROSION BETWEEN DOUBLERS AND SKIN. ROUTED OUT CORRODED SECTION, FABRICATED DOUBLER REP AIR AND INSTALLED IAW DC9 SRM 53-04 FIG 12B, AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1999032600717 19990326 00717 WP 1999 3 26 AT9900255 1 19990319 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 864-957 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT LEFT HAND FLOOR CARGO STRAP EXFOLIATED AROUND FASTENER HOLES A T BS 864 TO 957. MECHANICALLY REMOVED CORROSION, FABRICATED REPAIR STRAP, TREATED, AND PRIMED IAW DC9 SRM 53-01-0, 51-1 0-2, 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1999032600718 19990326 00718 WP 1999 3 26 AT9900256 1 19990320 A 5330 9915701 SKIN DOUG DC9 DC932 3022066 WP AFT STAIRWELL DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT VENTRAL STAIRS FUSELAGE SKIN AT YSD 27-98 WITH NUMEROUS DENT WITH CREASES. REMOVED STEPS TO GAIN ACCESS. REMOVED SKIN, LOCATED AND DRILLED NEW SKIN, AND INSTALLED SKIN AND REINSTALLED STEP IAW DC9 SRM 51-30-2, 51-30-1, 51-10-4, 51-30-8, AND RES NR 99595. 2 L 7 2 4F A6WE 1999032600719 19990326 00719 EU 1999 3 26 MALA976397 1 19990320 A 2120 AIR DISTRIBUTION SAAB SF340 340B 7860101 EU CABIN VAPOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 410XJ 410 AFTER NR 2 ENGINE START, FLIGHT ATTENDANT NOTICED VAPOR RISING FROM AISLE CARPET. MAINTENANCE REMOVED FLOOR PANEL, INSP ECTED, FOUND NO DEFECTS. GROUND RAN AIRCRAFT, NO DEFECTS NOTED. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999032600720 19990326 00720 EU 1999 3 26 MALA976398 1 19990319 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU ROW 4-6 LOOSE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 407XJ 340B407 THE LEFT SIDE REFLECTOR STRIP ON THE FLOOR HAS COME LOOSE (ROW 4-6) EMERGENCY PATH LIGHTING. MAINTENANCE REPLACED LIGHT ING STRIP. ALL CHECKS GOOD IAW SAAB 340 MM CHAPTER 33. 2 L 7 2 4T RT A52EU 1999032600721 19990326 00721 1999 3 26 MALA976399 4 19990320 A 3425 6226190113 AHRS SAAB SF340 SF340A 7850100 EU NR 1 INOP A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 98XJ 098 NR 1 ADI WENT BLANK ON CLIMBOUT, THE HORIZON TILTED OVER X-SIDE DATA CORRECTED IT. NR 1 ADI WAS THE LAST TO INITIALIZE. RETURNED TO MSP. MAINTENANCE REPLACED NR 1 AHRS COMPUTER. OPS CHECK GOOD IAW SF340 MM CH34. 2 L 7 2 4T RT A52EU 1999032600722 19990326 00722 EU 1999 3 26 MALA976400 1 19990316 A 2910 GPP125012 SWITCH SAAB SF340 SF340A 7850100 EU HYDRAULIC BAY LEAKING A MALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 15 48XJ 048 WHEN THE GEAR IS SELECTED UP THE HYDRAULIC PUMP RUNS CONTINOUSLY, EVEN THOUGH THE GEAR INDICATES UP AND LOCKED. WHEN TH E GEAR IS SELECTED DOWN THE AUTO FUNCTION WORKS PROPERLY AFTER THE GEAR IS DOWN AND LOCKED. MAINTENANCE REPLACED 9ML PR ESSURE SWITCH. SWUNG AC SERVERAL TIMES, ALL CHECKS GOOD. ALL WORK DONE IAW SF340 MM CHAPTER 29. 2 L 7 2 4T RT A52EU 1999032600723 19990326 00723 EU 1999 3 26 MALA976401 1 19990317 A 3260 PG24001 SWITCH SAAB SF340 SF340A 7850100 EU LT MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 48XJ 048 WHEN GEAR IS SELECTED UP THE HYDRAULIC PUMP IN AUTO MODE, RUNS CONTINUALLY, EVEN THROUGH GEAR INDICATES UP AND LOCKED. A IRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED LT MLG UPLOCK SWITCH, RIGGED NLG DOORS, PERFORMED GEAR SWINGS. 2 L 7 2 4T RT A52EU 1999032600724 19990326 00724 EU 1999 3 26 MALA976402 1 19990316 A 5230 HC523J0064211 SEAL BAC 146 AVRO146RJ85A 1500097 EU CARGO DOOR FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 501XJ E2208 ON APPROACH LOWER DOOR LIGHT CAME ON AT 9000A, NOTICED LOSS OF CABIN PRESSURE, DIFFERENTIAL WENT TO 0. LIGHT WENT OUT A T 2000 FT, STAYED OUT THROUGH SHUT DOWN CHECK. MAINTENANCE REPLACED LOWER DOOR SEAL OUTER CAGE, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999032600725 19990326 00725 1999 3 26 MALA976403 4 19990318 A 3460 4068300904 DFGC BAC 146 AVRO146RJ85A 1500097 EU E & E COMPT FAILED A MALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 15 507XJ E2316 TRIM RUNAWAY FUEL UP, TRIM BROKE LOOSE AFTER PHY 8. OVERPOWERED ELEVATOR 'FTC' 'ELECT TRIM' CAUTION LIGHTS ILLUMINATED. MAINTENANCE REPLACED DFGC. RETURNED TO SERVICE. 2 H 7 4 4F RT A49EU 1999032600726 19990326 00726 EU 1999 3 26 MALA976404 1 19990317 A 3020 CONNECTOR SAAB SF340 340B 7860101 EU RT ENG INTAKE LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 451XJ 451 RIGHT INTAKE LIGHT ILLUMINATED APPROX EVERY 10 SECONDS WITH ENGINE ANTI ICE SELECTED ON. AIRCRAFT RETURNED TO MSP. MAI NTENANCE VERIFIED HIGH RESISTANCE IN INTAKE HEAT CIRCUIT, FOUND CONNECTOR 161/162 UP LOOSE, TIGHTENED CONNECTOR. PERFOR MED GROUND RUNS/ OPERATIONAL. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999032600727 19990326 00727 EU 1999 3 26 MALA976405 1 19990317 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 142XJ 142 REPAIR FOR FUSELAGE DAMAGE IN THE REAR FUSELAGE SKIN IAW SAAB SRM 53-80-10. DOUBLER AND TRIPLER PLATE REPAIR FOR DAMAGE TO REAR FUSELAGE STA 622 TO 793. 2 L 7 2 4T RT A52EU 1999032600728 19990326 00728 SO 1999 3 26 LR7A9904 1 19990310 A 5320 35300428R FITTING LKHEED 382 382G 526414U SO BS 990 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 540 4698 FS 990 RT CRACKED TEE (P/N 353042-8R), WEB CRACKED, FS 990 LT FITTING CRACKED (P/N 353059-8). REMOVED AND REPLACED FITT INGS, TEE AND WEB IAW HERC SRM CH51-10 PG 4. 2 H 7 4 4T A1SO 1999032600729 19990326 00729 SO 1999 3 26 LR7A9905 1 19990322 A 5320 352896L FITTING LKHEED 382 382G 526414U SO BS 946 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 561 4698 BUTTERFLY FITTING CRACKED LT FS 946. REPLACED FITTING IAW SRM 51-10. 2 H 7 4 4T A1SO 1999032600730 19990326 00730 NM 1999 3 26 PCAA9900003 1 19990322 A 5542 85540001003 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 837EX 18823 2617 217 MDT- DURING A LIGHTNING STRIKE INSPECTION THE FORE RUDDER WAS FOUND TO HAVE NUMEROUS RIVETS PULLED THROUGH AND LOOSE. T HE RUDDER WAS REPAIRED IAW BOMBARDIER RD8-55-335. 2 H 7 2 4T RT A13NM 1999032600731 19990326 00731 EA 1999 3 26 JBXA9900077 1 19990323 A 3620 356024310 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT BLEED AIR FAILED A JBXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 05 578ML 7270 872391 FLIGHT 853 MYR TO RDU, 15 MINS FROM RDU HAD LEFT 14TH DUCT FAIL MESSAGE ON EICAS. PERFORMED PRECAUTIONARY SHUTDOWN NR 1 ENG ACCORDING TO OPERATIONAL PROCEDURES. REMOVED AND REPLACED LEFT HAND STUB WING DUCT LEAK SENSOR LOOP. OPS CHECK GO OD AT THIS TIME IAW CL-65 MM 36-21-04. 2 L 7 2 4F 4 F RT A21EA E15NE 1999032600732 19990326 00732 NM 1999 3 26 AWXA9900085 1 19990308 A 5322 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 520-540 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 520 TO 540 RBL 45-50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600733 19990326 00733 NM 1999 3 26 AWXA9900086 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 520-540 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 520 TO 540 RBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600734 19990326 00734 NM 1999 3 26 AWXA9900087 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 540-727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 540 TO 727 RBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED, AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600735 19990326 00735 NM 1999 3 26 AWXA9900088 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 540-727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 540 TO 727 LBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600736 19990326 00736 NM 1999 3 26 AWXA9900089 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727-907 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727B TO 907 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600737 19990326 00737 NM 1999 3 26 AWXA9900090 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727-920 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727B TO 920 LBL 45.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED, AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600738 19990326 00738 NM 1999 3 26 AWXA9900091 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 480-520 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 480 TO 520 RBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-30-52. 2 L 7 2 4F RT A16WE 1999032600739 19990326 00739 NM 1999 3 26 AWXA9900092 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727-887 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727E TO 887 RBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600740 19990326 00740 NM 1999 3 26 AWXA9900093 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727 TO 727B RBL 24.75 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-30-52. 2 L 7 2 4F RT A16WE 1999032600741 19990326 00741 NM 1999 3 26 AWXA9900094 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727 TO 727B RBL 24.75 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600742 19990326 00742 NM 1999 3 26 AWXA9900095 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727 TO 727B RBL 45.5 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600743 19990326 00743 NM 1999 3 26 AWXA9900096 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 480-520 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 480 TO 520 RBL 45.5 GOUGED OUT OF LIMITS AND CORRODED. REMOVED DA MAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-30-52. 2 L 7 2 4F RT A16WE 1999032600744 19990326 00744 NM 1999 3 26 AWXA9900097 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727 TO 727B LBL 45.5 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-30-52. 2 L 7 2 4F RT A16WE 1999032600745 19990326 00745 NM 1999 3 26 AWXA9900098 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 340-480 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 340 TO 480 RBL 45.50 GOUGED OUT OF LIMITS AND CORRODED. REMOVED D AMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600746 19990326 00746 NM 1999 3 26 AWXA9900099 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 520-540 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 520 TO 540 LBL 45.5 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SE CTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600747 19990326 00747 NM 1999 3 26 AWXA9900100 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 540-727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 540 TO 727 RBL 45.5 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK S ECTION, FABRICATED, TREATED AND INSTALLED PER 53-00-52. 2 L 7 2 4F RT A16WE 1999032600748 19990326 00748 NM 1999 3 26 AWXA9900101 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 520-540 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 520 TO 540 LBL 25.5 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK S ECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600749 19990326 00749 NM 1999 3 26 AWXA9900102 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 540-727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 540 TO 727 LBL 45.5 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK S ECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600750 19990326 00750 NM 1999 3 26 AWXA9900103 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 480-520 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 480 TO 520 LBL 25.5 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK S ECTION, FABRICATED, TREATED AND INSTALLED PER 53-00-52. 2 L 7 2 4F RT A16WE 1999032600751 19990326 00751 NM 1999 3 26 AWXA9900104 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727-907 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK DAMAGED AT BS 727B TO 907 RBL 45.50 GOUGED OUT OF LIMITS. REMOVED DAMAG ED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600752 19990326 00752 NM 1999 3 26 AWXA9900105 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 340-480 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK DAMAGED AT BS 340 TO 480 RBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGE D TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER 53-00-52. 2 L 7 2 4F RT A16WE 1999032600753 19990326 00753 NM 1999 3 26 AWXA9900106 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 727 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 727B TO 727C RBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRAC K SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600754 19990326 00754 NM 1999 3 26 AWXA9900107 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 344-480 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 344 TO 480 LBL 25.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600755 19990326 00755 NM 1999 3 26 AWXA9900108 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 480-520 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 480 TO 520 LBL 45.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600756 19990326 00756 NM 1999 3 26 AWXA9900109 1 19990308 A 5347 6546813 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 344-480 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, DAMAGED SEAT TRACK. SEAT TRACK AT BS 344 TO 480 LBL 45.50 GOUGED OUT OF LIMITS. REMOVED DAMAGED TRACK SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999032600757 19990326 00757 NM 1999 3 26 AWXA9900110 1 19990308 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 382 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 IN MAINTENANCE, SKIN DAMAGE. SKIN DENTED ON LEFT SIDE OF A/C 5 AFT OF FWD OUTFLOW VALVE AND 6 BELOW CREASE LINE AT STA 382. REMOVED DAMAGED SKIN SECTION, FABRICATED, TREATED AND INSTALLED PER SRM 53-00-01, 51-10-01, 51-10-02. 2 L 7 2 4F RT A16WE 1999032600758 19990326 00758 NM 1999 3 26 AWXA9900111 1 19990219 A 5315 6545812213 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, CORROSION. FLOORBEAM CORRODED OUT OF LIMITS AT BS 328. FABRICATED, TREATED AND INSTALLED STRAP PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 1999032600759 19990326 00759 NM 1999 3 26 AWXA9900112 1 19990219 A 5320 6545834289 SUPPORT BOEING 737 7373Q8 1384670 NM BS 298.5 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, GOUGED SUPPORT. AFT LOWER FLOOR SUPPORT ANGLE AT BS 298.5 RBL 13, GOUGED OUT OF LIMITS. REMOVED, FABRI CATED AND INSTALLED REPLACEMENT PART IAW SRM 53-10-04. 2 L 7 2 4F RT A16WE 1999032600760 19990326 00760 NM 1999 3 26 AWXA9900113 1 19990219 A 5320 6545810128 T CAP BOEING 737 7373Q8 1384670 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, CORRODED T-CAP. UPPER T-CAP AT FS 312 LBL 20-RBL 45 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED, TR EATED AND INSTALLED PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999032600761 19990326 00761 NM 1999 3 26 AWXA9900114 1 19990219 A 5313 STRINGER BOEING 737 7373Q8 1384670 NM BS 503 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, CRACKED STRINGER. STRINGER END CRACKED AT FS 503C STRINGER 16L. REMOVED, FABRICATED AND INSTALLED PER SRM 53-30-03, SRM 53-00-03. 2 L 7 2 4F RT A16WE 1999032600762 19990326 00762 NM 1999 3 26 AWXA9900115 1 19990224 A 5313 LONGERON BOEING 737 7373Q8 1384670 NM BS 31 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, LONGERON DAMAGED. LONGERON WEB BETWEEN STRINGER 13L AND 14L AT FUSELAGE STA 31 CHAFED AND GOUGED BEYOND LIMITS. REMOVED DAMAGED STRINGER WEB, FABRICATED WEB OUT OF 7075-T6 .050 QQA250/13 ALODINED PRIMED AND INSTALLED PER S RM 53-00-03. 2 L 7 2 4F RT A16WE 1999032600763 19990326 00763 NM 1999 3 26 AWXA9900116 1 19990219 A 5313 BAC1498139 STRINGER BOEING 737 7373Q8 1384670 NM BS 503 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, CRACKED STRINGER. CRACKED STRINGER END FS 503C STRINGER 16R. REMOVED, FABRICATED AND INSTALLED IAW SRM 53-30-03, SRM 53-00-03. 2 L 7 2 4F RT A16WE 1999032600764 19990326 00764 NM 1999 3 26 AWXA9900117 1 19990219 A 5320 SILL BOEING 737 7373Q8 1384670 NM BS 274-360 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, CORROSION. L-1 DOOR SEAL CHORD CORRODED OUT OF LIMITS AT FS 274 TO 360. REMOVED CORROSION AT BS 274 TO 318, CUT OFF AFT SECTION 318 TO 360, FABRICATED REPLACEMENT SECTION IAW SRM 53-10-15 FIG 1, INSTALLED PARTS IAW SRM 51- 40-02. 2 L 7 2 4F RT A16WE 1999032600765 19990326 00765 NM 1999 3 26 AWXA9900118 1 19990219 A 5320 602208020T3 CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, L FITTING BROKE. L FITTING BROKEN AT STRINGER 4L ATTACHMENT LOCATION. REMOVED, FABRICATED AND INSTALLE D IAW SRM 53-10-01. 2 L 7 2 4F RT A16WE 1999032600766 19990326 00766 NM 1999 3 26 AWXA9900119 1 19990219 A 5312 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 1088 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, BULKHEAD DAMAGE. AFT BULKHEAD FS 1088 IN AFT ACCY COMPARTMENT, DAMAGED TO THE INBOARD SIDE OF THE APU S HROUD CUT OUT RBL 19.50. REPAIRED PER AWA ENGINEERING REPAIR NR 3-53-16-47AG. 2 L 7 2 4F RT A16WE 1999032600767 19990326 00767 NM 1999 3 26 AWXA9900120 1 19990219 A 5510 ANGLE BOEING 737 7373Q8 1384670 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 327AW 23507 IN MAINTENANCE, CRACKED ANGLE. HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR AFT SPAR WEB ANGLE HAS .5 CRACK ABOVE LO WER RIGHT HAND INBOARD JACKSCREW SUPPORT FITTING. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED PER SRM 53-10-03. 2 L 7 2 4F RT A16WE 1999032600768 19990326 00768 NM 1999 3 26 AWXA9900121 1 19990322 A 5330 SKIN BOEING 737 737277 1384570 NM BS 787 & 607 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 NORMAL OPS, SKIN CRACK. SKIN AT STRINGER 17R BETWEEN STA 787 AND STA 607 HAS 2 CRACKS. VERIFIED WITH HFEC. REMOVED DA MAGED AREA, FABRICATED AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 1. PLACED ON MCK. INSPECT EVERY 3000 CYC'S, TERM AT C-CK. 2 L 7 2 4F RT A16WE 1999032600769 19990326 00769 WP 1999 3 26 CALA9900306 1 19990322 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1205-1225 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 1205 TO 1225. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A N EW SECTION WAS INSTALLED IAW SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 1999032600770 19990326 00770 NM 1999 3 26 CALA9900307 1 19990322 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, RBL 24 TO LBL 17. A REPAIR WAS INSTALLED IAW SRM 53-60-51. 2 L 7 2 4F RT A16WE 1999032600771 19990326 00771 NM 1999 3 26 CALA9900308 1 19990322 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND SEAT TRACK NR 2 CORRODED AT STA 344. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202. 2 L 7 2 4F RT A16WE 1999032600772 19990326 00772 WP 1999 3 26 CALA9900309 1 19990323 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BAGGAGE COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND AFT BAGGAGE BIN Z-ANGLE CORRODED AROUND HI-LOK FASTENERS. A REPAIR DOUBLER AND SPACER WERE INSTALLED I AW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1999032600773 19990326 00773 NM 1999 3 26 CALA9900310 1 19990323 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 767 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 767, TWO INCHES ABOVE L23R AND A 1.25 INCH CRACK WAS FOUND AT STA 767, TWO INCHES ABOVE L24R. DOUBLER REPAIRS WERE INSTALLED AT EACH CRACK LOCATION IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 1999032600774 19990326 00774 WP 1999 3 26 CALA9900311 1 19990323 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND WEB AND DOUBLER CORRODED AT STA 1338, LONGERON 30 TO 28R. THE CORRODED SECTION OF WEB WAS CUT OUT, JAC K POST DOUBLER WAS REPLACED AND A REPAIR WAS INSTALLED IAW SRM 51-30-0 AND 53-01. 2 L 7 2 4F A6WE 1999032600775 19990326 00775 WP 1999 3 26 CALA9900312 1 19990323 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1212-1221 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1212 TO 1221. A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 1999032600776 19990326 00776 WP 1999 3 26 CALA9900313 1 19990323 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1079-1250 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1079 TO 1250. A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-5 AND 53-05. 2 L 7 2 4F A6WE 1999032600777 19990326 00777 WP 1999 3 26 CALA9900314 1 19990323 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1098 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1098. A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-5 AND 53-05. 2 L 7 2 4F A6WE 1999032600778 19990326 00778 WP 1999 3 26 9901079155 1 19990312 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999032600779 19990326 00779 WP 1999 3 26 9901089880 1 19990311 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675MC 47651 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999032600780 19990326 00780 WP 1999 3 26 9901099964 1 19990317 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CATWALK INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1999032600781 19990326 00781 WP 1999 3 26 9901109964 1 19990318 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1999032600782 19990326 00782 NM 1999 3 26 9901115506 1 19990321 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM DOOR 4R DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 506US 23195 DOOR 4R EMERGENCY EXIT SIGN AND LIGHT INOPERATIVE UPON MAINTENANCE CHECK. MAINTENANCE REPLACED THE BATTERY PACK WITH A SERVICEABLE UNIT. OPERATIONAL TEST WAS SATISFACTORY. 2 L 7 2 4F RT A2NM 1999032600783 19990326 00783 NM 1999 3 26 9901125637 1 19990322 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM ROW 34-38 INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 537US 26484 ESCAPE PATH LIGHTING AT SEAT ROWS 34 TO 38 WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY WITH A SE RVICEABLE UNIT. OPERATIONAL TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999032600784 19990326 00784 EU 1999 3 26 QXEA9900505 1 19990320 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 482US 2838 11231 SEA - EXIT SIGN OVER COCKPIT DOOR WAS DIM THEN WENT OUT. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1999032600785 19990326 00785 EU 1999 3 26 QXEA9900506 1 19990320 A 3350 CONNECTOR GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9 LOOSE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 483US 11233 PDX - WITH THE EMERGENCY LIGHT SWITCH TURNED OFF AND AIRCRAFT POWER OFF, THE LAST THREE ROWS OF CHAIR FLOOR PROXIMITY LI GHTS STAY ON. MAINTENANCE REPLACED A WIRE CONNECTOR ON THE ESCAPE PATH LIGHT AT ROW 9. OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1999032600786 19990326 00786 EU 1999 3 26 QXEA9900507 1 19990321 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU RT EMER EXIT DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 4270 11161 SEA - RIGHT HAND SIDE OVERWING EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1999032600787 19990326 00787 EU 1999 3 26 QXEA9900508 1 19990317 A 3397 WIRE GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 10B BROKEN A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 498US 11181 PDX - EMERGENCY EVACUATION EXIT LIGHTS FROM SEATS 10B AND AFT ILLUMINATED. MAINTENANCE REPAIRED WIRES ON BATTERY PACK C ONNECTOR AT SEAT 14A, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1999032600788 19990326 00788 EU 1999 3 26 QXEA9900509 2 19990320 A 7250 TURBINE BLADE ROLLS ROYCE RB18355515P FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515P 54521 EU RT ENGINE FAILED A QXEA B E EMER. DESCENT ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 NM 09 481US 9277 11230 MWH - A/C EN ROUTE FROM SEA TO BIL, WHILE CLIMBING THROUGH 26,000 FT HEARD A BANG AND RIGHT ENGINE BEGAN TO VIBRATE, TGT ON RISE. SHUT DOWN ENGINE AND DIVERTED TO MWH. MAINTENANCE REPLACED THE ENGINE. A TURBIN BLADE ON THE NR 2 DISK OF T HE LP HAD EXITED THE ENGINE. THE RESULT OF THAT TEARDOWN WAS THE ENGINE HAD FAILED DUE TO A BLADE IN THE SECOND STAGE O F THE LPT BREAKING OFF JUST ABOVE THE FIR TREE AREA OF THE BLADE. ROLLS-ROYCE HAD AN ENGINEERING PERSON ON SIGHT TO CON DUCT THE DISASSEMBLY. 2 L 7 2 4F 4 F RT A20EU E2EU 1999032600789 19990326 00789 WP 1999 3 26 ABXA9900237 1 19990322 A 5320 5615677204 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1660-1700 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 INNER DOUBLER AT STATION 1660 TO 1700 CORRODED. REPAIRED IAW ABX REA B853-26997MR. 2 L 7 4 4F 4A25 1999032600790 19990326 00790 WP 1999 3 26 ABXA9900238 1 19990322 A 3210 57583301 BOSS DOUG DOUG DC8 DC863 302198A WP LT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 CORROSION FOUND IN LEFT MAIN LANDING GEAR PIN BOSS HOLE. REPAIRED IAW ABX REA D832-26975 MR. 2 L 7 4 4F 4A25 1999032600791 19990326 00791 NM 1999 3 26 MWEA99106 1 19990323 A 5311 99155643 FRAME DOUG MD88 MD88 3023688 NM BS 1385 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FRAME AT STATION 1385 HAS MODERATE CORROSION AT LONGERON 24R TO 27R. MTC FABRICATED AND INSTALLED FORMER. 2 L 7 2 4F RT A6WE 1999032600792 19990326 00792 NM 1999 3 26 MWEA99107 1 19990323 A 5320 991199121 JAMB DOUG MD88 MD88 3023688 NM VENTRAL STAIRWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 THE AFT VENTRAL STAIRWAY FORWARD LEFT JAMB HAS MODERATE CORROSION AT FORWARD END. MTC FABRICATED AND INSTALLED NEW ANGL E. 2 L 7 2 4F RT A6WE 1999032600793 19990326 00793 NM 1999 3 26 MWEA99108 1 19990323 A 5320 991556317 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 1380 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 804ME 48030 FOUND PREVIOUS REPAIR ON INTERCOSTAL FROM STATION 1380 TO 1395 AT L28L. MTC FABRICATED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F RT A6WE 1999032600794 19990326 00794 NM 1999 3 26 MWEA99109 1 19990323 A 5320 99576925 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 1407 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 THE INTERCOSTAL AT FS 1407 AT LONGERON 24L HAS MODERATE CORROSION. MTC FABRICATED AND INSTALLED INTERCOSTAL FRAME. 2 L 7 2 4F RT A6WE 1999032600795 19990326 00795 NM 1999 3 26 MWEA99110 1 19990323 A 5320 9912246115N ANGLE DOUG MD88 MD88 3023688 NM BS 1380 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 THE FRAME AT STATION 1380 TO SKIN ATTACH ANGLE HAS MODERATE CORROSION. MTC FABRICATED AND INSTALLED NEW TEE. 2 L 7 2 4F RT A6WE 1999032600796 19990326 00796 NM 1999 3 26 MWEA99111 1 19990323 A 5311 991187721 FRAME DOUG MD88 MD88 3023688 NM BS 1474 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FOUND CORROSION ON LEFT CARTED FRAME AT STATION 1474. MTC FABRICATED AND INSTALLED NEW FRAME. 2 L 7 2 4F RT A6WE 1999032600797 19990326 00797 NM 1999 3 26 MWEA99112 1 19990323 A 5311 991555965 WEB DOUG MD88 MD88 3023688 NM BS 1401 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FOUND CORROSION AT STATION 1401 FRAME AND FRAME TO SKIN ATTACH ANGLE. MTC FABRICATED AND INSTALLED FRAME WEB. 2 L 7 2 4F RT A6WE 1999032600798 19990326 00798 NM 1999 3 26 MWEA99113 1 19990323 A 5320 991556317 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 1380-1395 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 THE INTERCOSTAL HAS MODERATE CORROSION FROM STATION 1380 TO 1395. MTC FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F RT A6WE 1999032600799 19990326 00799 NM 1999 3 26 MWEA99114 1 19990323 A 5330 5911410 SKIN DOUG MD88 MD88 3023688 NM BS 562 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FUSELAGE SKIN CREASE FROM STATION 562 TO 601 BELOW LONGERON 20R EVALUATED TO CONDITION 2 OF TABLE C IN DC-9 SRM. MTC FA BRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F RT A6WE 1999032600800 19990326 00800 NM 1999 3 26 MWEA99115 1 19990323 A 5730 593358222 SKIN DOUG MD88 MD88 3023688 NM RIGHT WING OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 RIGHT LOWER WING SKIN AT AFT SPAR IN BETWEEN 2 EXISTING DOUBLERS JUST OUTBOARD OF INBOARD FLAP ACTUATOR HAS BLEND OUT EX CEEDING LIMITATIONS. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F RT A6WE 1999032600801 19990326 00801 NM 1999 3 26 MWEA99116 1 19990323 A 5313 2912727 LONGERON DOUG MD88 MD88 3023688 NM BS 1338-1401 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FOUND CORROSION ON LONGERON 24L AT STATION 1338 TO 1401. MTC FABRICTED AND INSTALLED NEW LONGERON. 2 L 7 2 4F RT A6WE 1999032600802 19990326 00802 NM 1999 3 26 MWEA99117 1 19990315 A 5311 995773917 FRAME DOUG MD88 MD88 3023688 NM BS 1287 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 REMOVED GALLEY MOUNTS FROM FRAME AT STATION 1287 LEAVING 2 UNPLUGGED HOLES. MTC REMOVED AND REPLACED UPPER PORTION OF F RAME. 2 L 7 2 4F RT A6WE 1999032600803 19990326 00803 WP 1999 3 26 MWEA99118 1 19990318 A 5311 9911839501 FRAME DOUG DC9 DC932 3022066 WP BS 1121 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FOUND CRACK AT STATION 1121 CANTED FRAME TO SKIN ATTACH ANGLE BETWEEN LONGERON 17 TO 18L. MTC FABRICATED AND INSTALLED DOUBLERS AND SHIMS. 2 L 7 2 4F A6WE 1999032600804 19990326 00804 WP 1999 3 26 MWEA99119 1 19990322 A 5311 591359577 FRAME DOUG DC9 DC932 3022066 WP FRAME 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FOUND CRACK ON FRAME 1076 AT LONGERON 2R AND 2L AFT ACCESSORY. MTC FABRICATED AND INSTALLED SPLICES AND DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999032600805 19990326 00805 WP 1999 3 26 MWEA99120 1 19990322 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP PASSENGER DOOR INOPERATIVE A MWEA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 400ME 45727 THE FORWARD ENTRY DOOR EMERGENCY FLASH LIGHT DOES NOT TURN ON. MTC REMOVED AND REPLACED EMERGENCY HANDHELD FLASHLIGHT A SSEMBLY. 2 L 7 2 4F A6WE 1999032600806 19990326 00806 WP 1999 3 26 DLL10990516 1 19990311 A 3350 5169741 BATTERY PACK LKHEED 1011 10113851 5265010 WP L4 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 193C1180 L-4 DOOR EMER LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1999032600807 19990326 00807 NM 1999 3 26 DL72W990517 1 19990312 A 2120 AIR DISTRIBUTION BOEING 727 727247 138408F NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 2817W 20873 STRONG BURNING SMELL IN MID CABIN NEAR OVERWING EXITS. CKD APU FOR SIGNS OF OIL LEAKS, NONE FOUND. CHECKED OPR OF PACK S AND PACK FANS, NORMAL. RAN PACKS NO ABNORMAL ODORS NOTED IN CABIN. 2 L 7 3 4F A3WE 1999032600808 19990326 00808 NM 1999 3 26 DLM88990518 1 19990312 A 3222 MS288892 VALVE DOUG MD88 MD88 3023688 NM NLG STRUT LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 936DL 49723 AFTER T/O, NOSE GEAR FAILED TO RETRACT, RED IND LIGHT ON. IND PIN WAS RETRACTED, NOISE FROM NOSE GEAR AREA. NOSE STRUT FOUND FLAT. REPLACED SCHRADER VALVE AND SERVICED STRUT. 2 L 7 2 4F RT A6WE 1999032600809 19990326 00809 NM 1999 3 26 DL72S990520 1 19990310 A 5311 65561212 FRAME BOEING 727 727232 1384082 NM BS 950 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 TWO DENTED AREAS WERE FOUND ON THE I/B CHORD OF THE BS 950C FRAME BETWEEN S24L AND 27L. REPAIRED PER ERA 332897-14, REV A. 2 L 7 3 4F A3WE 1999032600810 19990326 00810 NM 1999 3 26 DL72S990521 1 19990310 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 WHILE ACCOMPLISHING LFEC INSP PER SI 4-74176-12, ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 68 0. HFEC CONFIRMED 15 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT IN THE LWR SKIN. REPAIRED PER ERA 3328 38-14AD, REV A. 2 L 7 3 4F A3WE 1999032600811 19990326 00811 NM 1999 3 26 DL72S990522 1 19990310 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12 ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 681 AND BS 740. HFEC INSPECTION CONFIRMED 8 CRACK INDICAITONS IN THE LOWER FASTENER ROW OF THE LAP JOINT, IN THE LWR SKIN. REPAIRED PER ERA 332843-14AD, REV A. 2 L 7 3 4F A3WE 1999032600812 19990326 00812 NM 1999 3 26 DLM88990523 1 19990312 A 5330 5911401521 SKIN DOUG MD88 MD88 3023688 NM BS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 DENT FOUND IN SKIN AT STA 218, BETWEEN L18L AND L19L. REPAIRED PER ERA 332869-14 REV A. 2 L 7 2 4F RT A6WE 1999032600813 19990326 00813 NM 1999 3 26 DLM88990524 1 19990312 A 5330 5920323211 SKIN DOUG MD88 MD88 3023688 NM BS 522 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 DENT FOUND IN FUSELAGE SKIN AT STA 522 BETWEEN L20R AND L21R. REPAIRED PER ERA 332859-14. 2 L 7 2 4F RT A6WE 1999032600814 19990326 00814 NM 1999 3 26 DLM88990525 1 19990312 A 5330 595305059 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 DENT FOUND IN FUSELAGE SKIN LHS AT STA 237 AT THE CUSP LINE. REPAIRED PER ERA 332853-14 REV A. 2 L 7 2 4F RT A6WE 1999032600815 19990326 00815 NM 1999 3 26 DL73E990526 1 19990312 A 2720 CONTROLS BOEING 737 737247 138448D NM RUDDER MALFUNCTIONED A DALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 27 382DL 23609 ACFT EXPERIENCED RT RUDDER DISPLACEMENT FOR APPROX 2 SEC. RUDDER PEDALS DID NOT MOVE FROM NEUTRAL, A A/P ENGAGED. REMO VED MAIN PCU, STANDBY PCU, AND YAW DAMP COUPLER FOR TEST AND INSPECTION. 2 L 7 2 4F A16WE 1999032600816 19990326 00816 NM 1999 3 26 DL72S990527 1 19990312 A 5311 6516348118 FRAME BOEING 727 727232 1384082 NM BS 1148 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 STATION 1148 FRAME WAS FOUND WORN ON THE I/B HORIZ FLANGE AT S22L DUE TO CONTACT WITH A HYD LINE. REPAIRED PER ERA 3329 18-14. 2 L 7 3 4F A3WE 1999032600817 19990326 00817 NM 1999 3 26 DL72S990528 1 19990312 A 5313 65564414 STRINGER BOEING 727 727232 1384082 NM BS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 FUSELAGE STRINGER 29R WAS FOUND CRACKED 2 FWD OF BS 950E. ADDITIONALLY, CORROSION WAS NOTED 2 AFT OF BS 950D. A SECTIO N OF STRINGER FROM BS 950D+10 TO BS 950E+10 WILL BE CUT OUT AND REPLACED. REPAIRED PER ERA 332882-14. 2 L 7 3 4F A3WE 1999032600818 19990326 00818 NM 1999 3 26 DL72S990529 1 19990312 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1010 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 CORROSION WAS FOUND UNDER S28L AT BS 1010 AT THE SKIN BUTT JOINT. REPAIRED PER ERA 332920-14. 2 L 7 3 4F A3WE 1999032600819 19990326 00819 NM 1999 3 26 DL72W990530 1 19990312 A 2170 V1211 COALESCER BOEING 727 727247 138408F NM CABIN DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 2817W 20873 STRONG BURNING SMELL IN CABIN NEAR OVERWING EXITS WHEN MAIN SUPPLY TEMP EXCEEDS 80 DEGREES F. ISOLATED PACKS WITH APU A ND ALL ENG BLEED SOURCES. RAN SUPPLY TEMP TO 130 DEGREES F WITH EVERY COMBINATION POSSIBLE. NO SMELLS OF ANY KIND. RE PLACED BOTH WATER SEPARATOR BAGS AS PRECAUTIONARY. 2 L 7 3 4F A3WE 1999032600820 19990326 00820 NM 1999 3 26 DL72S990531 1 19990312 A 5320 WEB BOEING 727 727232 1384082 NM BS 1283 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 RT SIDE TORQUE BOX WEB HAS .125 INCH CRACK PROTRUDING PAST. ROUTE OUT REPAIR AT STA 1283 LOWER HOLE M/M 53-11-0 PG 832. 2 L 7 3 4F A3WE 1999032600821 19990326 00821 NM 1999 3 26 DL757990532 1 19990312 A 5610 WINDSHIELD BOEING 757 757232 1384965 NM RIGHT COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 616DL 22823 AT FL350 CREW REPORTED LOUD BANG AND NOTICED F/O WINDSCREEN HAD SHATTERED. CREW ALSO REPORTED SUBSEQUENT ARCING IN LOWE R CORNER OF WINDOW. WINDOW HEAT FOR THAT WINDOW WAS TURNED OFF. DISPATCH ELECTED TO DIVERT INTO ORD DUE TO ICING CONDI TIONS AT OTHER ALTERNATE AIRPORTS. MTC IN ORD IS REPLACING WINDOW. 2 L 7 2 4F RT A2NM 1999032600822 19990326 00822 NM 1999 3 26 DL72S990534 1 19990313 A 3350 BATTERY BOEING 727 727232 1384082 NM R1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 R1 DOOR EMERGENCY EXIT LIGHTS LOW. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999032600823 19990326 00823 NM 1999 3 26 DL72S990535 1 19990313 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM ROW 13 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 ROW 13 OVERHEAD EMERGENCY EXIT LIGHT DIM. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999032600824 19990326 00824 NM 1999 3 26 DL72E990536 1 19990312 A 3350 BATTERY 1001141 BOEING 727 727247 138408F NM ROW 1-26 SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 EMERGENCY EXIT LIGHTS ILLUMINATE WHEN ARMED SEAT 1 TO 26. FOUND LIGHTS ILLUM INTERMITTENTLY. ISOLATED PROBLEM TO RT CO NTROL SYSTEM, FOUND POWER AT PIN 4 AT FWD BATTERY PACK. INSPECTED WIRE BUNDLE IN CEILING, AT ALL BATTERY PACKS. FOUND AFT AIRSTAIR LIGHT AND BATTERY ASSY SHORTED INTERNALLY. REPLACED AFT AIRSTAIRS EMERGENCY EXIT LIGHT ASSY. ALL LIGHTS C HECK NORMAL. 2 L 7 3 4F A3WE 1999032600825 19990326 00825 WP 1999 3 26 DLL14990537 1 19990313 A 2612 87858101 CONNECTOR LKHEED 1011 1011385115 5265015 WP NR 3 ENGINE FAILED A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 740DA 193C1244 14874 DURING CLIMBOUT, FIRE WARNING LIGHT CAME ON WITH INTERMITTANT FIRE BELL B LOOP ON NR 3 ENG ILLUMINATED. A LOOP ALREADY ON MCO. SHUTDOWN NR 3 ENG PER POM PROCEDURE. RANG OUT B LOOP PER FIM, CLEANED ALL CONNECTORS, REPLACED CONNECTOR P715 ON A LOOP, RAN ENGS PER PFHB. NO LIGHTS, ALL NORMAL. 2 L 7 3 4F A23WE 1999032600826 19990326 00826 NE 1999 3 26 DLM90990538 2 19990312 A 7200 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE NR 1 FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 906DA 11372 53386 LEFT ENGINE FAILURE WHEN T/O POWER APPLIED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE A40NE 1999032600827 19990326 00827 NM 1999 3 26 DLM88990539 1 19990315 A 4920 APU DOUG MD88 MD88 3023688 NM APU COMPT MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 965DL 49984 EMERGENCY RETURN TO ATL FOR SMOKE IN CABIN. HEAVY WT LANDING 134.8 SMOOTH AND LESS THAN 360 FPM SINK RATE. FOUND OIL I N APU INLET. REPLACED APU, CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1999032600828 19990326 00828 NM 1999 3 26 DL72S990540 1 19990311 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC CONFIRMED 69 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE ENT IRE LENGTH OF THE PANEL AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366873-14, REV A. 2 L 7 3 4F A3WE 1999032600829 19990326 00829 NM 1999 3 26 DL72S990541 1 19990311 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 36 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGTH OF THE PANEL AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366872-14AD, REV A. 2 L 7 3 4F A3WE 1999032600830 19990326 00830 NM 1999 3 26 DL73K990542 1 19990311 A 5311 FRAME BOEING 737 737232 1384475 NM BS 332 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 330DL 23102 THE AFT DOOR JAMB FRAME OF THE R1 DOOR OPENING WAS FOUND WITH A 3 INCH LONG CRACK UNDER UPPER DOOR STOP FITTING. THE CR ACKED FRAME WAS REPAIRED PER THE REQUIREMENTS OF B737 SRM 53-10-4, FIG 1 AND DOCUMENTED PER ER/A 366934-14AD. 2 L 7 2 4F RT A16WE 1999032600831 19990326 00831 NM 1999 3 26 DL72W990543 1 19990312 A 5330 65545661 SKIN BOEING 727 727247 138408F NM BS 505 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 LFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE BETWEEN FS 360 AND 681 REVEALED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INSPECTION CONFIRMED TWO CRACKS/CORROSION AT FS 505. THE SKIN WAS CUTOUT WITH A 2 X 1 CUTOUT IN THE LAP AND REPAIRED PER THE B727 SRM 53-30-3 FIG 5 AND DOCUMENTED PER ER/A 366915-14AD, REV A. 2 L 7 3 4F A3WE 1999032600832 19990326 00832 NM 1999 3 26 DL72S990544 1 19990311 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366886-14AD, REV A. 2 L 7 3 4F A3WE 1999032600833 19990326 00833 NM 1999 3 26 DL72S990545 1 19990313 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 REVEALED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 86 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366885-14AD, REV A. 2 L 7 3 4F A3WE 1999032600834 19990326 00834 NM 1999 3 26 DL72S990546 1 19990313 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 510 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 360 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 500 AND 520. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED PER B727 SRM 53-30-3, FIGURE 5 AND DOCUMENTED PER ER/A 366894-14AD, REV A. 2 L 7 3 4F A3WE 1999032600835 19990326 00835 NM 1999 3 26 DL72S990547 1 19990308 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 440-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED TWO CRACKS BETWEEN FS 440 AND 460. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A366797 -14AD, REV B. 2 L 7 3 4F A3WE 1999032600836 19990326 00836 NM 1999 3 26 DL72S990548 1 19990309 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 400-420 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE SKIN PANEL CONFIRMED ONE CRACK BETWEEN FS 400 AND 420. THE CRACK AREA WAS ROUTED OUT OF THE SKIN PANEL LAP SPLICE AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 36685 3-14AD, REV A. 2 L 7 3 4F A3WE 1999032600837 19990326 00837 NM 1999 3 26 DL72S990549 1 19990309 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 660-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 REVEALED A CRACK BETWEEN FS 660 AND 681 IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE PANEL CONFIRMED THE SINGLE CRACK. THE CR ACK WAS ROUTED OUT OF THE SKIN LAP SPLICE AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366852-14AD, REV A. 2 L 7 3 4F A3WE 1999032600838 19990326 00838 WP 1999 3 26 DLL10990550 1 19990311 A 5330 SKIN LKHEED 1011 10113851 5265010 WP R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE UPPER AFT CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN ASSY AND TRIPLER. THE AREA WAS X- RAYED TO DETERMINE THE EXACT END OF THE CRACK AND REPAIRED PER L1011 SRM 53-31-00, FIG 836. THE REPAIR WAS DOCUMENTED P ER ER/A 366927-14. 2 L 7 3 4F A23WE 1999032600839 19990326 00839 NM 1999 3 26 DL72K990551 1 19990315 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 370 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON THE S4R LAP JOINT, TWO CRACK INDICATIONS WERE FOUND BETWEEN BS 360 AND BS 481. HFEC INSPECTION VERIFIED THE TWO CRACK INDICAITONS, BETWEEN BS 360 AND BS 380. THE CRACKS WERE IN T HE LWR ROW FASTENERS IN THE LAP JOINT, IN THE LWR SKIN. REPAIRED PER ERA 332925-14AD. 2 L 7 3 4F A3WE 1999032600840 19990326 00840 NM 1999 3 26 DL72S990552 1 19990316 A 5712 6483385 RIB BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 THE UPPER CHORD ANGLE OF THE LEFT WING RIB AT WS 171.5 WAS FOUND CRACKED. THE CRACK WAS LOCATED AT A FASTENER HOLE ON T HE HORIZONTAL FLANGE OF THE CHORD ANGLE UNDER S16. REPAIRED PER ERA 332872-14, REV B. 2 L 7 3 4F A3WE 1999032600841 19990326 00841 NM 1999 3 26 DL72S990553 1 19990316 A 5314 KEEL BEAM BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 V20019 KEEL BEAM LT LWR CHORD WAS FOUND CRACKED IN THE UPPER FLANGE TYPICAL OF THAT DESCRIBED BY SB 727-53-0208, REV 1. REPAIR ED PER ERA 332906-14. 2 L 7 3 4F A3WE 1999032600842 19990326 00842 NM 1999 3 26 DL73E990554 1 19990316 A 2760 HANDLE BOEING 737 737247 138448D NM SPEEDBRAKES OUT OF POSITION A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 245WA 23519 V20019 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. DISCONTINUED TAKEOFF BELOW 60 KTS SPEEDBRAKE/FLAPS/STAB TRIM APPEAR NORMA L. FOUND SPEEDBRAKE HANDLE NOT IN DETENT REPOSITIONED HANDLE. PERFORMED TAKEOFF WARN TEST, CKS OK. 2 L 7 2 4F A16WE 1999032600843 19990326 00843 NM 1999 3 26 DL72K990555 1 19990311 A 7110 COWLING BOEING 727 727232 1384082 NM NR 2 ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 V20019 WORN, NO 2 ENG COWLING LANDING - FROM 1 O'CLOCK TO 11 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF CHORD, FORMED AND DR ILLED REPAIR ANGLES FOR SPLICE. DRILLED NEW SECTION OF CHORD OK TO INSTALL. INSTALLED LT SPLICE. COMPLETED INSTALLATI ON OF RING AND RT SPLICE. REPAIRED PER M/M 53-11-0. OK TO INSTALL LOWER CLOSE OUT WEB 5 O'CLOCK TO 7 O'CLOCK. 2 L 7 3 4F A3WE 1999032600844 19990326 00844 1999 3 26 DLM11990556 4 19990316 A 2330 TH41JSK21W PROJECTOR DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 48474 V20019 MIDWAY DURING FLT STRONG ELEC FUMES WERE DETECTED FROM THE FWD Y CLASS CABIN, PROJECTOR APPEARS TO HAVE OVERHEATED. PUL LED C/BS FOR VIDEO SYSTEM AND FUMES APPEARED TO DISSIPATE AFTER VIDEO PROJECTOR WAS SHUTDOWN. REMOVED CEILING PANELS TH ROUGHT CABIN, INSPECTED WIRING AND COMPARTMENT, NO PROBLEM FOUND. INSPECTED CEILING LIGHTS, NO DEFECTS NOTED. FOUND Y CLASS PROJECTOR AT FAULT WITH BLACK SOOT INSIDE PROJECTOR. REMOVED CANNON PLUG FROM PROJECTOR AND PULLED RELATED C/B IN AFT CABIN BETWEEN 4L AND 4R DOORS. FWD TO MCO AND PLAC PER MEL 25-22-01. 2 L 7 3 4F RT A22WE 1999032600845 19990326 00845 NM 1999 3 26 DL72S990557 1 19990317 A 5330 SKIN BOEING 727 727232 1384082 NM BS 620-640 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 PERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATIONS WAS NOTED IN THE S4R LAP JOINT BETWEEN BS 620 AND 640. T HE INDICATION WAS LOCATED IN FASTENER ROW NR 11 AS IDENTIFIED IN FIGURE 6 OF THE SI. REPAIRED PER ERA 332909-14AD. 2 L 7 3 4F A3WE 1999032600846 19990326 00846 NM 1999 3 26 DL72S990558 1 19990317 A 5330 SKIN BOEING 727 727232 1384082 NM BS 570-580 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 PERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP JOINT BETWEEN BS 560 TO 580. TH E CRACK INDICATION WAS LOCATED AT FASTENER ROW 8 AS IDENTIFIED IN FIGURE 6 OF THE SI. REPAIRED PER ERA 332910-14AD. 2 L 7 3 4F A3WE 1999032600847 19990326 00847 NM 1999 3 26 DL72S990559 1 19990317 A 5330 SKIN BOEING 727 727232 1384082 NM BS 380-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 PERFORMING INSPECTIONS PER SI 4-74176-12AD, 12 CRACK INDICATIONS WERE FOUND BETWEEN BS 380 TO 460 IN THE SKIN LAP JOINT AT S4L. REPAIRED PER ERA 332914-14AD. 2 L 7 3 4F A3WE 1999032600848 19990326 00848 NM 1999 3 26 DL72S990560 1 19990310 A 5330 65654703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIREMD SEVERAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENT IRE LENGTH OF THE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366854-14AD. 2 L 7 3 4F A3WE 1999032600849 19990326 00849 NM 1999 3 26 DL72S990561 1 19990313 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGTH OF THE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOULBER PER ER/A 366884-14AD, REV A. 2 L 7 3 4F A3WE 1999032600850 19990326 00850 NM 1999 3 26 DL72S990562 1 19990311 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 360 AND 380. THE CRACKS WERE ROUTED OUT AND RE PAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366916-14AD. 2 L 7 3 4F A3WE 1999032600851 19990326 00851 WP 1999 3 26 DLL10990563 1 19990311 A 5330 SKIN LKHEED 1011 10113851 5265010 WP L3 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 A CRACK WAS FOUND IN SKIN ASSY OF THE UPPER FORWARD CORNER OF THE L3 DOOR CUTOUT. THE CRACK IS IN THE SKIN, DOOR SURROU ND DOUBLER, AND TRIPLER. THE SKIN ASSY WAS X-RAYED TO DETERMINE THE END OF THE CRACK AND THEN REPAIRED PER L1011 SR M 53-31-00, FIG 836. THE INSPECTION AND REPAIR WAS DOCUMENTED PER ER/A 366928-14. 2 L 7 3 4F A23WE 1999032600852 19990326 00852 NM 1999 3 26 DL76P990564 1 19990312 A 5330 146T35526 SKIN BOEING 767 767332 1382001 NM BS 1197-1307 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 143DA 25991 THE FUSELAGE SKIN AND UNDERLYING FRAME CHORD WERE PUNCTURED FROM CONTACT WITH GROUND EQUIPMENT. THE DAMAGE WAS CUT OUT OF THE SKIN WITH A 3.7 X 9.4 CUTOUT. THE DAMAGED AREA OF FRAME CHORD WAS ALSO CUTOUT. THE SKIN WAS REPAIRED WITH AN EX TERNAL ALUMINUM DOUBLER AND TRIPLER AND THE FRAME CHORD WAS REPAIRED WITH 2 ALUMINUM REPAIR ANGLES. THE REPAIR WAS ACCO MPLISHED PER ER/A 366930-14, REV A. 2 L 7 2 4F RT A1NM 1999032600853 19990326 00853 NM 1999 3 26 DL72S990565 1 19990311 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 720 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 TO 740 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 720 AND 720A. THE CRACKED AREA WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366917-14AD. 2 L 7 3 4F A3WE 1999032600854 19990326 00854 NM 1999 3 26 DL72S990566 1 19990311 A 5330 65654703 SKIN BOEING 727 727232 1384082 NM BS 400-420 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 400 AND 420. THE CRACKS WERE CUT OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5. THE REPAIR WAS DOCUMENTED PER ER/A 366923-14AD. 2 L 7 3 4F A3WE 1999032600855 19990326 00855 NM 1999 3 26 DL72S990567 1 19990311 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 560-580 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN LOWER FASTENER ROW OF TH E LOWER SKIN. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL CONFIRMED A SINGLE CRACK BETWEEN FS 560 AND 580. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366881-14AD. 2 L 7 3 4F A3WE 1999032600856 19990326 00856 NM 1999 3 26 DL72S990568 1 19990311 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT ALONG ITS ENTIRE LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366866-14, REV B. 2 L 7 3 4F A3WE 1999032600857 19990326 00857 NM 1999 3 26 DL72S990569 1 19990312 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 530 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW O F THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A CRACK BETWEEN FS 520 AND 540. THE CRACK WAS ROUTED OUT AND REPA IRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366882-14AD. 2 L 7 3 4F A3WE 1999032600858 19990326 00858 NM 1999 3 26 DL72S990570 1 19990316 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 460-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 2 CRACKS BETWEEN FS 460 AND 480. THE CRACKS WERE ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366964-14AD. 2 L 7 3 4F A3WE 1999032600859 19990326 00859 NM 1999 3 26 DL72S990571 1 19990315 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 590 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW O F THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED ONE CRACK BETWEEN FS 580 AND 600. THE CRACK WAS ROUTED OUT AND RE PAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A366963-14AD. 2 L 7 3 4F A3WE 1999032600860 19990326 00860 NM 1999 3 26 DL72S990572 1 19990313 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT A LONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366883-14AD, REV B. 2 L 7 3 4F A3WE 1999032600861 19990326 00861 NM 1999 3 26 DL72K990573 1 19990125 A 5753 652163391A ANGLE BOEING 727 727232 1384082 NM NR 1 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 DURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 21 INCHES FROM O/B END OF FLAP. THE ANGLE WAS REPAIR ED PER MM 57-52-0 BY INSTALLING A REPLACEMENT SECTION OF ANGLE AND A SPLICE DOUBLER. 2 L 7 3 4F A3WE 1999032600862 19990326 00862 NM 1999 3 26 DL72S990577 1 19990316 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 580 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON THE S26L LAP JOINT, CRACK INDICATIONS WERE NOTED BETWEEN BS 480 AND BS 681. HFEC INSPECTIONS CONFIRMED 4 CRACK INDICATIONS. ADDITIONALLY, A 2.5 INCH CRACK RUNNING FWD/AFT WAS NOT ED AT S25L AT BS 540. REPAIRED PER ERA 332881-14AD, REV E. 2 L 7 3 4F A3WE 1999032600863 19990326 00863 WP 1999 3 26 DLL10990578 1 19990317 A 3350 SIGN 5165741 LKHEED 1011 10113851 5265010 WP R3 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 60555 193C1226 ALL EMERGENCY EXIT SIGNS BY R3 DOOR INOP. REPLACED POWER SUPPLY, CHECK NORMAL. 2 L 7 3 4F A23WE 1999032600864 19990326 00864 WP 1999 3 26 DLL10990579 1 19990317 A 3350 SIGN 5165741 LKHEED 1011 10113851 5265010 WP L3 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 38241 193C1226 EMERGENCY EXIT SIGNS BY L3 DOOR INOP. REPLACED POWER SUPPLY, CHECK NORMAL. 2 L 7 3 4F A23WE 1999032600865 19990326 00865 NM 1999 3 26 DL72K990580 1 19990105 A 5753 652163262 SPAR BOEING 727 727232 1384082 NM RT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 CRACKS AT AFT SPAR RAIL AT 18, 32 & 61 FROM I/B END OF FLAP. REPAIRED ON N/R'S 010525, 010526 & 010527. REPAIRS WERE P ERFORMED PER M/M 57-52-0 FIG 802 . ON SHOP ORDER 655739. 2 L 7 3 4F A3WE 1999032600866 19990326 00866 NM 1999 3 26 DL72W990581 1 19990309 A 5713 STRINGER BOEING 727 727247 138408F NM WS 686.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 A .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 686.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0. 2 L 7 3 4F A3WE 1999032600867 19990326 00867 NM 1999 3 26 DL72W990582 1 19990309 A 5713 STRINGER BOEING 727 727247 138408F NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 A .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 656.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0. 2 L 7 3 4F A3WE 1999032600868 19990326 00868 NM 1999 3 26 DL72W990583 1 19990309 A 5713 STRINGER BOEING 727 727247 138408F NM WS 629 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 A .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 629 AT ATTACH BOLT. REPAIRED PER MM 57-13-0. 2 L 7 3 4F A3WE 1999032600869 19990326 00869 NM 1999 3 26 DL72W990585 1 19990304 A 2497 BMS1358 INSULATION BOEING 727 727247 138408F NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 0 DURING HUSH-KIT MOD FOUND INSULATION CRACKED ON GEN FEEDER CABLES IN PYLON ON NR 3 ENGINE. SPLICED IN NEW CABLE (P/N 01 22107330) FROM SPLICES IN 48 SECTION TO FIREWALL DISCONNECT. 2 L 7 3 4F A3WE 1999032600870 19990326 00870 NM 1999 3 26 DL72S990587 1 19990318 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND AT B-2 LETTER CK, .5 INCH CRACK AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER STOP CASTING. REPAIR PER SRM 53- 10-9. 2 L 7 3 4F A3WE 1999032600871 19990326 00871 NM 1999 3 26 DL72S990588 1 19990315 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366907-14AD, REV A. 2 L 7 3 4F A3WE 1999032600872 19990326 00872 NM 1999 3 26 DL72S990589 1 19990318 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 VERT FIN STR 10L CRACKED AT STA 180.600. INSTALLED DOUBLER PER M/M 55-30-0. 2 L 7 3 4F A3WE 1999032600873 19990326 00873 NM 1999 3 26 DL72K990590 1 19990309 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 WEB CRACKED VERTICAL STAB INTERIOR - WEB AT STA 1303 IS CRACKED AT BOTH RT AND LT LOWER CORNERS, MARKED. STOP DRILLED C RACKS AND DYE PENETRATE INSP RT AND LT SIDE PER SRM 53-10-4 FIG 17. FABRICATED REPAIR DOUBLERS AND TAPERED SHIM PER SRM 53-10-4 FIG 17. TREAT DOUBLERS AND SHIMS. PAINTED DOUBLER AND SHIMS PER PS900-3-6. OK TO INSTALL LT AND RT REPAIR. I NSTALLED LT REPAIR PER SRM 53-10-4 FIG 17. INSTALLED RT REPAIR FOR SRM 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1999032600874 19990326 00874 NM 1999 3 26 DL76P990592 1 19990319 A 5330 143T35217 SKIN BOEING 767 767332 1382001 NM BS 450 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 FUSELAGE SKIN WAS FOUND DENTED/GOUGED AT BS 457 BETWEEN S33R AND S34R JUST AFT OF AN EXISTING EXTERNAL REPAIR (FOR A SKI N CUTOUT ALSO BETWEEN S33R AND S34R). THE NEW CUTOUT IS APPROX 1 INCH DIA, THE EXISTING CUTOUT IS APPROX 9 BY 3. REPAI RED PER ERA 367009-14. 2 L 7 2 4F RT A1NM 1999032600875 19990326 00875 NM 1999 3 26 DL72S990593 1 19990317 A 5311 FRAME BOEING 727 727232 1384082 NM BS 761 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 DURING ACCOMPLISHMENT OF INSPECTIONS PER SI 4-61904-12AD, A CRACK WAS NOTED IN THE 2ND FAST HOLE ABOVE THE FLOORLINE. A LSO, THE 4TH FASTENER HOLE ABOVE THE FLOORLINE FELL OUT IN THE RADIUS OF THE REPAIR ANGLE. REPAIRED PER 332907-14AD. 2 L 7 3 4F A3WE 1999032600876 19990326 00876 NM 1999 3 26 DL72S990594 1 19990319 A 2121 FAN 215201 BOEING 727 727232 1384082 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 545DA 22494 ON TOP OF DESCENT, CREW AND PASSENGERS COMPLAINED OF AN ELECTRICAL SMELL IN CABIN WITH NO SIGN OF SMOKE. AFTER A SAFE L ANDING AND NORMAL DEPLANING, CONTRACT MAINTENANCE FOUND GASPER FAN CAUSING SMELL. REPLACED FAN. 2 L 7 3 4F A3WE 1999032600877 19990326 00877 NM 1999 3 26 DL72S990595 1 19990319 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM ROW 20-26 INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 519DA 8821 21470 ON S/C FOUND E PATH LIGHTING AT SECTION 20 TO 26 INOP. FOUND BAD FUSE ON AFT PWR SUPPLY. REPLACED AFT PWR SUPPLY, OPS NORMAL NOW. 2 L 7 3 4F A3WE 1999032600878 19990326 00878 WP 1999 3 26 DLL14990597 1 19990319 A 2612 CONNECTOR LKHEED 1011 1011385115 5265015 WP NR 3 ENGINE FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 740DA 193C1244 000000 NOTIFIED BY OPS AROUND 1900 THAT FLT 54 NR 3 ENG FIRE WARNING LIGHT ILLUMINATED AND SHUT ENG DOWN AND USED FIRE EXTINGUI SHER BOTTLE AND DUMPING FUEL. REPLACED PLUG AT NR 3 FDCU. 2 L 7 3 4F A23WE 1999032600879 19990326 00879 NM 1999 3 26 DL76L990598 1 19990320 A 2913 PUMP 887673 BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR2 ENGINE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 173DN MX520754 24800 724150 RIGHT SYSTEM HYDRAULIC QTY STARTED TO DROP SLOWLY. TURNED ENGINE DRIVEN PUMP OFF AND QTY STILL DROPPED SLOWLY. QTY STO PPED DROPPING AT 0.12. FOUND ENG DRIVEN HYD PUMP LEAKING AT CASE SPLIT LINE. REPLACED PUMP ASSY. ALSO, REPLACED PRESS URE FILTER AND CASE DRAIN FILTERS. NO EVIDENCE OF METAL CONTAMINATION. 2 L 7 2 4F 4 F RT A1NM E24NE 1999032600880 19990326 00880 1999 3 26 DL76L990599 4 19990320 A 2330 PROJECTOR BOEING 767 767332 1382001 NM CABIN FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 194DN 28451 A/C DIVERTED FOR BURNING ODOR IN Y/C CABIN. FOUND SMOKING Y/C FWD CTR OVERHEAD PROJECTOR. DISCONNECTED C/PS, PULLED C/ B AND FWD TO MCO DUE TO HISTORY. 2 L 7 2 4F RT A1NM 1999032600881 19990326 00881 NM 1999 3 26 DL76L990600 1 19990319 A 2530 OVEN BOEING 767 767332 1382001 NM GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1201P 28458 F/A REPORTED WHITE SMOKE COMING FROM NR 4 OVEN IN AFT GALLEY. TURNED OVEN OFF, CLOSED DOOR. SMOKE STOPPED. PULLED C/B FOR OVEN NR 4 INSPECTION SHOWED HEAVY GREASE ON OVEN RACKS. FOUND CAUSE OF SMOKE TO BE AN ADHESIVE LABEL ON A FOOD RAC K. CATERING SERVICE REMOVED ALL RACKS FROM A/C. OVEN OPERATES NORMALLY AND IS OK FOR SERVICE. 2 L 7 2 4F RT A1NM 1999032600882 19990326 00882 NM 1999 3 26 DL76L990601 1 19990320 A 2120 AIR DISTRIBUTION BOEING 767 767332 1382001 NM CABIN ORDER A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 194DN 28451 VERBAL FROM CABIN CREW, BURNING RUBBER LIKE SMELL ON LANDING AT JFK. RAN ALL EQUIP IN ECY AND MID GALLEY. INSPECTED AR EAS ABOVE OVERHEAD CEILING PANELS, ALL OK. DEACTIVATED VIDEO SYS WITH C/B'S AT P37 PULLED. REF MCO 737556003. CHEC KED RECIRC AND GASPER FANS, CK OK. 2 L 7 2 4F RT A1NM 1999032600883 19990326 00883 NM 1999 3 26 DLM88990602 1 19990320 A 4950 INLET DOUG MD88 MD88 3023688 NM APU CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 916DL 49591 ON CLIMBOUT, OILY SMELL OBSERVED WHILE ENGINE ANTI ICE IN USE. DISSIPATED AT ALTITUDE WHEN ANTI ICE TURNED OFF. FOUND OIL IN APU AIR INLET. CLEANED INLET, PERFORMED DUCT BURNOUT. REPLACED WATER SEPARATORS. 2 L 7 2 4F RT A6WE 1999032600884 19990326 00884 NM 1999 3 26 DL76S990604 1 19990321 A 3350 0201720001 LIGHT BOEING 767 767332 1382001 NM ROW 41F INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 122DL 23436 ON L/O, FOUND SEAT 41F EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A1NM 1999032600885 19990326 00885 NM 1999 3 26 DL72L990605 1 19990322 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 513DA 21315 FWD AND REAR OVER AISLE EMERG EXIT LIGHTS FLICKER WHEN STANDBY PWR SELECTED. REPLACED 2 BATTERY PACKS, OPS NORMAL. 2 L 7 3 4F A3WE 1999032600886 19990326 00886 NM 1999 3 26 DL72S990606 1 19990319 A 5330 65545901 SKIN BOEING 727 727232 1384082 NM BS 720-740 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 THE LOWER FUSELAGE SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND CORRODED BETWEEN FS 720 +17 AND FS 740 NEAR AN A/C DUCT CUTOUT. THE DAMAGED SECTION OF SKIN WAS CUT AWAY AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 366954-14, REV A. 2 L 7 3 4F A3WE 1999032600887 19990326 00887 NM 1999 3 26 DL72W990607 1 19990319 A 5330 SKIN BOEING 727 727247 138408F NM BS 680 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 THE FUSELAGE SKIN WAS FOUND CORRODED AT THE FS 680 BUTT SPLICE BETWEEN STRINGER 28L AND 28R. AN EXISTING LOCAL REPAIR W AS REMOVED AT THIS LOCATION AND ALL CORROSION AREAS WERE CUT OUT OF THE SKIN WITH A 1 X 3 CUTOUT AND A 10 X 5 CUTOUT. B OTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL REPAIR DOUBLER PER ER/A 366900-14, REV A. 2 L 7 3 4F A3WE 1999032600888 19990326 00888 NM 1999 3 26 DL72S990608 1 19990316 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 440-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS BETWEEN FS 440 AND 460. THE CRACKED AREA OF SKIN LAP SPLIC E WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366965- 14AD. 2 L 7 3 4F A3WE 1999032600889 19990326 00889 NM 1999 3 26 DL72S990609 1 19990317 A 5330 655457489 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 85 CRACKS INCLUDING A 15 INCH LONG CRACK LINK UP BETWEEN FS 640 AND 660. THE ENTIRE SKIN LAP SPLICE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366960-14AD, REV A. 2 L 7 3 4F A3WE 1999032600890 19990326 00890 NM 1999 3 26 DL72S990610 1 19990317 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 19 CRACK INDICATIONS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WA S CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366962-14AD, REV A. 2 L 7 3 4F A3WE 1999032600891 19990326 00891 NM 1999 3 26 DL72L990611 1 19990322 A 2751 INDICATOR 2061111 BOEING 727 727232 1384082 NM TE FLAPS FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 506DA 418 21308 OUTBOARD T/E FLAPS DID NOT EXTEND WHEN FLAP LEVER MOVED FROM UP TO 2 DEG. RETURNED LEVER TO UP, RAN THE POM CK LIST. T RAILING EDGE FLAP ABNORMAL ALTERNATE/FLAP EXTENSION ON I/B FLAPS WORKED FINE. CHECKED CABLES AND PULLEYS, ALL CKS OK. R EPLACED O/B FLAP POSITION IND I/B AND OUTBOARD FLAPS CHECKED OK. 2 L 7 3 4F A3WE 1999032600892 19990326 00892 NM 1999 3 26 DL72W990612 1 19990322 A 5320 WEB BOEING 727 727247 138408F NM BS 1213 & 1231 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 A .5 INCH CRACK TORQUE BOX VERT WEB FS 1213 RT SIDE. SEVERAL SMALL CRACKS LIGHTENING HOLE ON TORQUE BOX VERT WEB AT FS 1231 RT SIDE. REPAIRED PER MM 53-11-0 PG 833. ROUTED CRACKS PER MM 53-11-0 PG 828. 2 L 7 3 4F A3WE 1999032600893 19990326 00893 NM 1999 3 26 DL72K990614 1 19990319 A 5753 652163262 SPAR BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 526DA 21586 DURING SHOP VISIT AND ACCOMPLISHMENT OF EO 4-58705-3AD, MTC UNABLE TO INSTALL REQUIRED COLLAR FOR ONE OF THE UPPER SPAR- TO-UPPER SKIN ATTACH FASTENERS DUE TO PROXIMITY TO SPAR RADIUS. AUTHORIZED USE OF RADIUS BLOCK AND MINI NUT. 2 L 7 3 4F A3WE 1999032600894 19990326 00894 NM 1999 3 26 DL72S990615 1 19990315 A 5753 65192701 FLAP TRACK BOEING 727 727232 1384082 NM RT TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING OUTSIDE REPAIR OF COMPONENT AND OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND ON THE M LG BEAM AND SPOILER BEAM ATTACH PAD AND HOLES. AUTHORIZED OVERSIZED FASTENERS, BUSHING REPAIR AND LEAVING THE OVERSIZED MLG BEAM ATTACH HOLES AS-IS. 2 L 7 3 4F A3WE 1999032600895 19990326 00895 NM 1999 3 26 DL72S990616 1 19990315 A 5753 65192702 FLAP TRACK BOEING 727 727232 1384082 NM LT TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING OUTSIDE REPAIR, OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND TO THE FWD ATTACH LUGS A ND THE MLG BEAM AND SPOILER BEAM ATTACH PADS AND HOLES. AUTHORIZED BUSHING REPAIR FOR FWD ATTACH LUG AND OVERSIZED S POILER BEAM ATTACH HOLES. AUTHORIZED LEAVING OVERSIZED MLG BEAM ATTACH HOLE AS-IS. INSTALLED SPLICE PLATE REPAIR PER S B. 2 L 7 3 4F A3WE 1999032600896 19990326 00896 NM 1999 3 26 DL72W990617 1 19990323 A 2750 COUPLING BOEING 727 727247 138408F NM TE FLAP DRIVE FAILED A DALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 296WA 22533 DURING APPROACH TO ATL, UPON SEL 5 DEG FLAPS THE OUTBOARD NEEDLES SPLIT AND REMAINED AT 2 DEG. FOUND LT OUTBOARD T/E FL AP DRIVE (TORQUE) TUBE COUPLING, FAILED JUST INBOARD OF LT MLG SPAR. 2 L 7 3 4F A3WE 1999032600897 19990326 00897 NM 1999 3 26 DL72S990618 1 19990320 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED SEVERAL CRACKS IN SEPARATE FRAME BAYS ALONG THE PANEL LENGTH T HE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366971-14A D, REV A. 2 L 7 3 4F A3WE 1999032600898 19990326 00898 WP 1999 3 26 DLL19990619 1 19990320 A 5320 1559194103 INTERCOSTAL LKHEED 1011 10113853 5265020 WP L3 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 A .25 INCH TYPICAL CRACK WAS FOUND IN A RELIEF RADIUS OF THE NR 4 INTERCOSTAL AT THE L3 DOOR CUT OUT AFT DOOR JAMB. THE ADJACENT FITTING INTERCOSTALS WERE UNDAMAGED. THE CRACK WAS ALLOWED TO CONINUE INSERVICE PER THE REQUIREMENTS OF LACO S/B 93-53-270 AND WILL BE REPAIRED WITH A NEW INTERCOSTALS. THE REPAIR WAS DOCUMENTED PER E/R/A 367019-14. 2 L 7 3 4F A23WE 1999032600899 19990326 00899 NM 1999 3 26 DL72S990620 1 19990320 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED CRACKS IN CONSECUTIVE FRAME BAYS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366972-14AD, R EV A. 2 L 7 3 4F A3WE 1999032600900 19990326 00900 NM 1999 3 26 DL72S990621 1 19990320 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT A LONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366970-14AD, REV A. 2 L 7 3 4F A3WE 1999032600901 19990326 00901 NM 1999 3 26 DL76P990622 1 19990320 A 5330 143T35217 SKIN BOEING 767 767332 1382001 NM BS 435-465 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 THE FUSELAGE SKIN WAS DEEPLY DENTED ADJACENT TO AN EXISTING SKIN CUTOUT REPAIR AT FS 457, BETWEEN STRINGER 33R AND 34R. THE EXISTING REPAIR WAS REMOVED, THE NEW DAMAGE CUTOUT, AND A NEW EXTERNAL ALUMINUM REPAIR DOUBLER INSTALLED TO REPAIR BOTH DAMAGE CUTOUTS. THE REPAIR WAS ACCOMPLISHED PER ER/A 367009-14, REV A. 2 L 7 2 4F RT A1NM 1999032600902 19990326 00902 NM 1999 3 26 DL72S990623 1 19990320 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FAS TENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366914-14AD, REV A. 2 L 7 3 4F A3WE 1999032600903 19990326 00903 NM 1999 3 26 DL72S990624 1 19990320 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366911-14AD, REV A. 2 L 7 3 4F A3WE 1999032600904 19990326 00904 NM 1999 3 26 DL767990625 1 19990320 A 5754 114T410414A WEDGE BOEING 767 767232 1385132 NM NR 9 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 105DA 22217 THE TRAILING EDGE WEDGE OF THE NR 9 SLAT WAS FOUND WITH A 4 X 4 AREA OF DELAMINATION. THE DAMAGE AREA WAS CUT OUT AND R EPAIRED PER THE B767 SRM 57-43-02. THE REPAIR WAS DOCUMENTED PER ER/A 367010-14AD. 2 L 7 2 4F RT A1NM 1999032600905 19990326 00905 NM 1999 3 26 DL72S990626 1 19990320 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT A LONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366912-14AD, REV A. 2 L 7 3 4F A3WE 1999032600906 19990326 00906 NM 1999 3 26 DL757990627 1 19990320 A 5510 182N40022 STRUCTURE BOEING 757 757232 1384965 NM RT HORIZ STAB DAMAGED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 622DL 22912 THE FRONT SPAR WEB AND LOWER SKIN OF THE RT HORIZONTAL STABILIZER WERE FOUND GOUGED AND DENTED FROM A BUCKING BAR LEFT I NSIDE THE STAB BOX DURING ASSEMBLY. THE DAMAGED AREA OF SPAR WEB WAS CUT OUT AND A NEW SECTION SPLICED IN WITH ALUMINUM SPLICE STRAPS. THE DAMAGED AREA OF SKIN WAS CUT OUT AND REPAIRED WITH AN ALUMINUM DOUBLER. THE REPAIRS WERE ACCOMP LISHED PER ER/A 366841-14, REV A. 2 L 7 2 4F RT A2NM 1999032600907 19990326 00907 NM 1999 3 26 DL72S990628 1 19990323 A 5754 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FOUND ON E1 LETTER CK, NR 5 SLAT ACT I/B ATTACH RIB CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999032600908 19990326 00908 NM 1999 3 26 DL72S990630 1 19990323 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 FOUND ON MV2 CK, .5 INCH CRACK STA 1303 WEB RT AT LOWER RT CORNER. REF NR 143. FOUND ON MV2 CK, .5 INCH CRACK STA 1303 WEB RT AT THE CUTOUT FOR THE STRINGER. REF NR 142. BOTH CRACKS REPAIRED WITH THE SAME DOUBLER PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999032600909 19990326 00909 NM 1999 3 26 DL72S990631 1 19990323 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 FOUND ON MV2 CK, .5 INCH CRACK IN STA 1303 WEB LT LOWER CORNER. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999032600910 19990326 00910 NM 1999 3 26 DL733990632 1 19990323 A 3320 BALLAST 059341 BOEING 737 737347 1384647 NM ROW 17 & 18 FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 303WA 2703 23183 PASSENGERS AT ROW 17 AND 18 ABC REPORTED A BREIF PUFF OF SMOKE AROUND WINDOW AREA AND ASSOCIATED SMELL. ODOR WAS A MILD ELECTRIC SMELL AND DISSIPATED. WINDOW LIGHTS TURNED OFF AS PRECAUTION. REPLACED SIDEWALL LIGHT BALLAST. 2 L 7 2 4F RT A16WE 1999032600911 19990326 00911 NM 1999 3 26 DL72K990633 1 19990323 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM COCKPIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 415DA 21257 COCKPIT OVER DOOR EMERGENCY LIGHT FAILED TO TEST. REPLACED, OPS NORMAL. 2 L 7 3 4F A3WE 1999032600912 19990326 00912 WP 1999 3 26 DHL99804002 1 19990323 A 3230 4779333 LINKAGE DOUG DC8 DC873F 302199F WP LT MLG BROKEN A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804DH 46124 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. UNABLE TO VERIFY NOSE WHEEL ALIGNED, LEFT GEAR DOWN AND RETURNED FOR LAND ING. FOUND GROUND SHIFT MECHANISM BROKEN. REMOVED AND REPLACED LINKAGE PER MM 32-23-1. CYCLED HANDLE WITH NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999033000001 19990330 00001 NM 1999 3 30 DL76L990474 1 19990307 A 3620 9750172006 SENSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 171DN 24759 724681 RT BLEED OVERHEAT EICAS MESSAGE AND ANNUNCIATOR LIGHT. INSPECTED FLEXLINES TO FAV, INSPECTED WIRING AT FAV, PRV AND HPV , FOUND OK. REPLACED RT OVERHEAT TEMP SENSOR AND RT BLEED AIR CONTROL CARD PER M/M. RAN ENG, BLEED OPS AND INDICATON O K. NO EICAS MSG. 2 L 7 2 4F 4 F RT A1NM E24NE 1999040200001 19990402 00001 NE 1999 4 2 TWAA9904501 2 19990324 A 7230 809407 BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE LT ENGINE COMP FRACTURED A TWAA E ENGINE SHUTDOWN Y ENGINE STOPPAGE AP APPROACH 1 CE 05 9406W 53126 1230 DURING APPROACH THE LT ENGINE STOPPED PRODUCING POWER AND EGT ROSE TO 800 DEG. ENGINE WAS SHUT DOWN. ON THE GROUND THE N1 COMPRESSOR WOULD NOT ROTATE AND THERE WAS METAL IN THE TAILPIPE. THE ENGINE WAS CHANGED. CHECK-C 1-18-99 ST. *S/D * FOUND 2 SEVENTH STAGE TITANIUM COMPRESSOR BLADES HAD FRACTURED FROM FOD AND FATIGUE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999040200002 19990402 00002 WP 1999 4 2 TWAA9904502 1 19990324 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 12-24 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9420D 49824 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROWS 12 THROUGH 24. FOUND AND REPAIRED A BROKEN WIRE. CHECK-C 12-8-98 MCI. 2 L 7 2 4F RT A6WE 1999040200003 19990402 00003 WP 1999 4 2 TWAA9904503 1 19990324 A 2450 947F9463 PANEL DOUG DC9 DC915 3022036 WP BUS CONTROL WORN A TWAA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 CE 05 971Z 45773 WHILE PARKED AT THE GATE USING GROUND POWER, SMOKE WAS SEEN COMING INTO THE CABIN FROM THE LOWER ELECTRONIC COMPARTMENT. SHUT DOWN ELECTRICAL POWER. FOUND THE BUS CONTROL PANEL WITH BURNED WIRING. REPLACED THE BUS CONTROL PANEL. CHECK-C 7-6-98 STL. 2 L 7 2 4F A6WE 1999040200004 19990402 00004 NM 1999 4 2 HNAA9900038 1 19990318 A 2510 MAT DHAV DHC8 DHC8102 2809003 NM COCKPIT FLOOR OUT OF POSITION A HNAA K NONE O OTHER CL CLIMB 1 EA 07 906HA 009 NOSE GEAR DID NOT RETRACT WHEN SELECTED UP. FOUND ALTERNATE EXTENSION DOOR AJAR. SEATED DOOR AND CYCLED GEAR. OPERATI ON NORMAL. ON FOLLOWUP, TRIMMED RUBBER FLOOR MAT AWAY FROM DOOR. DOOR SEATS NORMALLY. 2 H 7 2 4T RT A13NM 1999040200005 19990402 00005 NM 1999 4 2 HNAA9900039 1 19990320 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM 1 & 2 FAILED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 981HA 378 DURING CLIMB-OUT, SMOKE WARNING LIGHT ILLUMINATED SEVERAL TIMES. NO EVIDENCE OF FIRE OR SMOKE. ELECTRICAL SMELL FOUND IN BAG BAY WHEN DOOR WAS OPENED. REPLACED BOTH SMOKE DETECTORS P/N 30-231-3 NR 1, S/N 31832, NR 2 S/N 0015W. 2 H 7 2 4T RT A13NM 1999040200006 19990402 00006 EU 1999 4 2 MALA976407 1 19990325 A 3234 D49410001 CONTROL PANEL SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 408XJ 408 AFTER TAKEOFF, UPON GEAR RETRACTION, GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. GEAR DOWN LIGHTS WERE EXTINGUISHED. F OLLOWED QRH PROCEDURE, GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED UPON CYCLING OF GEAR, GEAR SEEMED TO EXTEND AND RETRAC T NORMALLY. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LANDING GEAR CONTROL PANEL IAW SAAB AMM 32-31-05-2. OP S CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999040200007 19990402 00007 SW 1999 4 2 PNSA990301 1 19990323 A 2612 FIRE DETECTOR SWRNGN SA227 SA227AC 8780603 SW RIGHT ENGINE MALFUNCTIONED A PNSA O OTHER N FALSE WARNING DE DESCENT 1 AL 03 640PA AC759B ON SHORT FINAL, RT ENGINE FIRE LIGHT ILLUMINATED. LIGHT EXTINGUISHED ITSELF DURING THE FLARE FOR LANDING. LANDING WAS UN EVENTFUL AND ENGINE WAS SECURED ONCE CLEAR OF THE ACTIVE RUNWAY. NO EVIDENCE OF FIRE OR OVERHEATING WAS FOUND. THE FIR E DETECTION SYSTEM TESTED OK PER MAINT MANUAL. REPLACED ONE DETECTOR AS A PRECAUTIONARY PROCEDURE. SYSTEM OPERATIONALL Y TESTED OK. 2 L 7 2 4T RT A8SW 1999040200008 19990402 00008 EA 1999 4 2 COMA9960128 1 19990321 A 7830 22850229133 TR FAIRING CNDAIR CL600 CL6002B19 EA LT ENGINE BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 DURING C-CHECK, FOUND DIVERTER FAIRING BROKEN. REPLACED FAIRING. 2 L 7 2 4F RT A21EA 1999040200009 19990402 00009 EA 1999 4 2 COMA9960129 1 19990321 A 7830 1217545 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT ENGINE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 9761 7116 FOUND RIGHT ENGINE THRUST REVERSER FLEXSHAFT P/N 121754-5 WORN. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1999040200010 19990402 00010 EA 1999 4 2 COMA9960130 1 19990323 A 2750 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 929CA 7035 FLAPS FAIL CAUTION MESSAGE. INSPECTED FLAPS PER EO 27-045 AND AD 98-20-01. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999040200011 19990402 00011 EA 1999 4 2 COMA9960131 1 19990323 A 5210 H2912A SPRING CNDAIR CL600 CL6002B19 EA PAX DOOR LATCH WEAK A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 735CA 7267 CABIN DOOR OUTER HANDLE WARNING MESSAGE. REPLACED HANDLE LATCH SPRING. 2 L 7 2 4F RT A21EA 1999040200012 19990402 00012 NM 1999 4 2 UPS99229091 1 19990306 A 5315 BAC15091001A6T6 FLOORBEAM BOEING 727 72727C 138400J NM BS 575 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON CARGO FLOOR SUPPORT BS 575, LBL 15 WL 156. FABRICATED REPAIR PARTS PE R SRM 53-10-5 AND INSTALLED PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999040200013 19990402 00013 NM 1999 4 2 UPS99229092 1 19990320 A 5320 SUPPORT BOEING 727 72727C 138400J NM BS 1046 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION AFT CARGO FLOOR SUPPORT BS 1046, RBL 10, WL 157. REMOVED AND REPLACED FLOOR SUPPORT SEGMENT PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999040200014 19990402 00014 NM 1999 4 2 UPS99229093 1 19990321 A 5315 FLOORBEAM BOEING 727 72727C 138400J NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION ON FLOORBEAM TOP FLANGE BS 344 LBL 14 - RBL 12 WL 208. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 1999040200015 19990402 00015 NM 1999 4 2 UPS99229094 1 19990306 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION (C53-133-01-1B) ON FRAME SHIER TIE, BS 700 BETWEEN STR 28R AND STR 28L. SHEER TIE OUT OF LI MITS. FABRICATED NEW TIE AND INSTALLED PER SRM 51 -30-02, SRM 51-10-06, SRM53-10-1, SRM 53-10-4. 2 L 7 3 4F A3WE 1999040200016 19990402 00016 NM 1999 4 2 UPS99229095 1 19990306 A 5320 BAC1509100196T6 SUPPORT BOEING 727 72727C 138400J NM BS 575 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON CARGO FLOOR SUPPORT BS 575, RBL 10, WL 156. FABRICATED REPAIR PARTS P ER SRM 53-10-5 AND INSTALLED PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999040200017 19990402 00017 NM 1999 4 2 UPS99229096 1 19990314 A 5220 6517509 HANDLE BOEING 727 72727C 138400J NM LT EMER EXIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION ON LT AFT OVERWING EXIT DOOR HANDLE AT TORQUE TUBE ATTACHMENT AFTER THE CORROSION REMOVA L, THE HANDLE WENT BEYOND ALLOWABLE LIMITS PER SRM 52-00-2. REPLACED THE HANDLE WITH A NEW ONE AND INSTALLED IT ON THE TORQUE TUBE PER SRM 52-20-00. 2 L 7 3 4F A3WE 1999040200018 19990402 00018 NM 1999 4 2 UPS99229097 1 19990323 A 5320 SUPPORT BOEING 727 72727C 138400J NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION ON FLOOR SUPPORT BS 680 WL 156 LBL 9. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999040200019 19990402 00019 NM 1999 4 2 UPS99229098 1 19990321 A 5320 SUPPORT BOEING 727 72727C 138400J NM BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE:C CORROSION ON AFT CARGO PIT FLOOR TRACK SUPPORT ANGLE BS 960, RBL 13.5, WL 155. REMOVED AND REPLACED T RACK SUPPORT PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999040200020 19990402 00020 WP 1999 4 2 UPS99829099 1 19990325 A 2910 LINE DOUG DC8 DC873F 302199F WP BS 198-410 CRACKED A IPXA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 866UP 45966 INSPECTION TYPE:N/A, ODOR IN COCKPIT AFTER BLOCK, SMELLS LIKE DIRTY SNEAKERS. SMELL EXTREMELY IRRITATING TO THE THROAT AND NOSE. FOUND CRACKED HYD LINE AT THE MAIN DECK CARGO SHUTT-OFF VALVE. REPLACED LINE. 2 L 7 4 4F RT 4A25 1999040200021 19990402 00021 WP 1999 4 2 UPS99829100 1 19990324 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 1&4 ENGINE DAMAGED A IPXA K NONE O OTHER LD LANDING 1 SO 01 852UP 46052 NR 1 AND NR 4 ENGINE COWLINGS CONTACTED RUNWAY ON LANDING. REMOVED AND REPLACED FAN COWL ON BOTH NR 1 AND NR 4 ENGINES. REPLACED DRAIN MASTS. ALSO, ACCOMPLISHED HARD LANDING INSPECTION NACELLE CONTACT INSP AS PER M\M REF 05-56-00.AND EO DC8-7830-11028. (WAN NR 386924). 2 L 7 4 4F RT 4A25 1999040200022 19990402 00022 WP 1999 4 2 UPS99829101 1 19990305 A 5347 44157329 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 SEAT TRACK AT FS 1440, LBL 44 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABIRCATED, AND IN STALLED SEAT TRACK IAW EO DC8-5320-5167C AND SRM 53-2-3 FIG. 8A. 2 L 7 4 4F RT 4A25 1999040200023 19990402 00023 WP 1999 4 2 UPS99829102 1 19990221 A 5347 5750864567 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 SEAT TRACK HAS HEAVY CORROSION AT FS 500 LBL 50. CUT OUT DAMAGED SECTION, FABRICATED, AND REPLACED S EAT TRACK IAW SRM 52-2-3 FS 490 TO 580. 2 L 7 4 4F RT 4A25 1999040200024 19990402 00024 WP 1999 4 2 UPS99829103 1 19990225 A 5720 3704841501 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 NR 2 MAIN TANK, INBD SIDE OF THE XRS 74 BULKHEAD, THE FWD STR 51 END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999040200025 19990402 00025 WP 1999 4 2 UPS99829104 1 19990310 A 5347 S2772660T SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT FS 1220, LBL 48 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGE, FABRICATED AND R EPLACED SEAT TRACK FS 1190-1290 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200026 19990402 00026 WP 1999 4 2 UPS99829105 1 19990311 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1580 AT LBL 48, THE FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH S K808-839. 2 L 7 4 4F RT 4A25 1999040200027 19990402 00027 WP 1999 4 2 UPS99829106 1 19990311 A 5347 6015176 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT BL 0, FS 520 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED SEAT TRACK FS 450-590 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200028 19990402 00028 WP 1999 4 2 UPS99829107 1 19990224 A 5347 5750872 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1100-1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT FS 1140 TO 1100, BL 0, IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED, AND REPLACED SEAT TRACK FS 1070 TO 1150, BL 0, IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200029 19990402 00029 WP 1999 4 2 UPS99829108 1 19990223 A 5347 5750872531F SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1306 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1306, BL 0, THE MAIN CABIN SEAT TRACK HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION, FABRICATED, A ND REPLACED SEAT TRACK FS 1290-1430, BL0 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200030 19990402 00030 WP 1999 4 2 UPS99829109 1 19990206 A 5347 5750864593 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, FS 900 TO 960, RBL 45, IS CORRODED OUT OF LIMITS. CUT OUT DAMAGED SECTION, FA BRICATED, AND REPLACED SEAT TRACK FS 870 - 990 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200031 19990402 00031 WP 1999 4 2 UPS99829110 1 19990315 A 5347 272660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 320-340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS, FS 320-340, RBL 24. CUT OUT DAMAGED SECTION, FABRICATE D, REPLACED SEAT TRACK FS 290 TO 390, RBL 24, IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200032 19990402 00032 NE 1999 4 2 QXEA9900510 2 19990322 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT&RIGHT FLAMED OUT A QXEA O OTHER R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT DE DESCENT 1 NM 09 814PH 43 SEA- ON DESCENT INTO SEA, THE AIRCRAFT EXPERIENCED MODERATE TO SEVERE TURBULENCE WHILE IN INSTRUMENT METROLOGICAL CONDIT IONS (IMC). DURING THIS PERIOD, BOTH ENGINES APPARENTLY FLAMED-OUT, AND THEN BOTH IMMEDIATELY RELIT. THERE WAS A LOUD SURGE WITH THE POWER LEVERS IN FLIGHT IDLE. ACCOMPLISHED A UNEVENTFUL LANDING IN SEA. MAINTENANCE PERFORMED A TURBULAN CE INSPECTION WITH NO DEFECTS NOTED. ALSO, PERFORMED A GROUND RUN AT 80 PERCENT TORQUE FOR 10 MINUTES. ALL PARAMETERS WERE NOTED AS NORMAL, NO SURGE NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200033 19990402 00033 NM 1999 4 2 99FDEA00097 1 19990310 A 2820 ARL0119501 TEE DOUG MD11 MD11F 3023600 NM CTR WING DRAINS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 FUEL FND LEAKING AT RIGHT UPPER AUX TANK PUMP LEFT AND RIGHT FEED THROUGH LINE DURING FUEL DRAIN SHROUD LEAK TEST. LK C K L/FLOAT SW AND CONDUIT RT UPPER AUS TANK PUMP, NO LEAK; LK CK LT UPPER AUX PUMP CONDUIT, NO LEAK. PANEL AND BOTH LWR AUX PUMP WIRES REMOVED. TEE LEFT AND RIGHT REPLACED, WIRING AND LK CK ON TEE ADAPTER AND WIRING CONDUIT CONN. 2 L 7 3 4F RT A22WE 1999040200034 19990402 00034 NM 1999 4 2 99FDEA00117 1 19990323 A 5330 65183268 SKIN BOEING 727 72725C 138400H NM BS 1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 0620 015 - BULGING SKIN JUST BELOW LOWER FWD CORNER OR AFT LAV SERVICE DOOR BETWEEN BS 1166 AND 1183 AT STR 22L. REP AIRED SKIN AT BS 1166-1183 STR 19-26L PER EA FEDEX 7-5330-44712. 2 L 7 3 4F A3WE 1999040200035 19990402 00035 NM 1999 4 2 99FDEA00118 1 19990323 A 5311 65163491 FRAME BOEING 727 72725C 138400H NM BS 1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 0578 016 - CORROSION ON SHEAR TIE BS 1166 STR 29L AND STR 30 WL 138. REMOVED SHEAR TIES AT BS 1166 STR 29 L/R. FAB RICATED AND INSTALLED NEW SHEAR TIES IAW FEDEX SRM 51-30-2 53-10-4. 2 L 7 3 4F A3WE 1999040200036 19990402 00036 NM 1999 4 2 99FDEA00119 1 19990323 A 5311 6516349 FRAME BOEING 727 72725C 138400H NM BS 1166 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 NR 0632 017 - WHILE WORKING NRO 578, FOUND REINFORCEMENT CHORD FOR BS 1166 FRAME CRACKED AT STR 29R WL 140. REMOVED RE INFORCEMENT CHORD, FABRICATED NEW CHORD AND INSTALLED CHORD IAW FEDEX SRM 51-10-1 51-30-2. 2 L 7 3 4F A3WE 1999040200037 19990402 00037 NM 1999 4 2 99FDEA00120 1 19990323 A 5330 6518382166 SKIN BOEING 727 72722C 138400F NM BS 1180 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR 0562 011 - CORROSION (C53-100-01-5) ON EXTERIOR SURFACE OF SKIN AT BS 1180 BETWEEN STR 6R AND 7R. 2 L 7 3 4F A3WE 1999040200038 19990402 00038 EU 1999 4 2 99FDEA00121 1 19990324 A 3260 INDICATION PANEL AIRBUS 300 A300F4605R 3930327 EU COCKPIT INOP A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 660FE 759 ON GEAR EXT, NR 2 SYS NOSE GEAR RED LIGHT ON. MISSED APPROACH AND RECYCLED GEAR. NR 2 SYS NOSE GEAR LIGHT OFF, SILENCE D TOO LOW GEAR AND LANDED AFTER REVIEWING RED TABS. BOS MX, A/C RELEASED FOR SERVICE PER MEL/CDL 32-1, CAT B EXP 27MAR9 9, INTERROGATED PROX BOX DET UNIT FAULTS BOX. NO PARTS THIS STA, DEF PER MEL 32-1 SYS 2 (OVHD PNL) LANDING GEAR INDICAT OR PANEL INOP. 2 L 7 2 4F RT A35EU 1999040200039 19990402 00039 NM 1999 4 2 99FDEA00122 1 19990325 A 2150 PACK BOEING 727 7272S2F 1384O81 NM RIGHT ODOR A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 211FE 22933 AFTER TURNING ON R/PACK, HAD AN ACRID, SMOKEY SMELL TO COCKPIT. PACK TEMP APPROX 50C DUCT TEMP BELOW 20C. DUCT PRESS A PPROX 32 PSI. TURNED PACK OFF FOR REMAINDER OF FLT. SMELL SUBSIDED. RAN ENG PER CHAPTER 5 OF 727 JET RUN HANDBOOK. P ERF'D OPS CK OF R/PACK PER 727 MM CHAP 21 W/O NOTICEABLE ODOR OR SMOKEY SMELL OBSERVED. WILL REQ NO ACTION. OK TO CONT INUE. 2 L 7 3 4F A3WE 1999040200040 19990402 00040 WP 1999 4 2 ABXA9900240 1 19990305 A 5311 3921813505 FRAME DOUG DOUG DC9 DC933F 302207A WP BS 332 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FUSELAGE FRAME CORRODED AT STATION 332, BETWEEN LONGERON 29 LEFT AND 29 RIGHT. REPAIRED IAW DC9 S RM 53-03. 2 L 7 2 4F A6WE 1999040200041 19990402 00041 WP 1999 4 2 ABXA9900241 1 19990305 A 5320 992341714 ANGLE DOUG DOUG DC9 DC933F 302207A WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FLOORBEAM ATTACH ANGLE CRACKED AT STATION 617 RBL 44. REPAIRED IAW DC9 SRM 51-30-5 AND DWG 992341 7. 2 L 7 2 4F A6WE 1999040200042 19990402 00042 WP 1999 4 2 ABXA9900242 1 19990305 A 5320 992341713 ANGLE DOUG DOUG DC9 DC933F 302207A WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FLOORBEAM ATTACH ANGLE CRACKED AT STATION 617 AND LBL 44. REPAIRED IAW DC9 SRM 51-30-5 AND DOUGLA S DWG 9923417. 2 L 7 2 4F A6WE 1999040200043 19990402 00043 WP 1999 4 2 MWEA99121 1 19990321 A 2730 CONTROL CABLE DOUG DC9 DC914 3022034 WP ELEVATOR JAMMED A MWEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 31 600ME 45725 AIRCRAFT ELEVATOR CABLE FROZE AND JAMMED ELEVATOR CONTROL. EXCESSIVE ICE BUILDUP IN ELEVATOR QUADRANT AREA CLEANED LUBE D ALL ELEVATOR CONTROL CABLES AND PULLEYS CLEANED AND INSPECTED DRAIN HOLES. 2 L 7 2 4F A6WE 1999040200044 19990402 00044 NM 1999 4 2 SCNA99053 1 19990323 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM RT EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD EMERGENCY EXIT OVERWING LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED A ND REPLACED THE RIGHT FORWARD EMERGENCY EXIT OVERWING BATTERY PACK IAW MM 3350022. SYSTEM OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999040200045 19990402 00045 NM 1999 4 2 VNAA9903017 1 19990321 A 2133 2097H020900 OUTFLOW VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 427JS 9899 3039 THE A/C FAILED TO PRESSURIZE DURING THE CLIMB PHASE OF THE FLT. THE A/C RETURNED TO THE FIELD AND LANDED, W/O ANY FURTH ER PROBLEMS. OUTSTATION MX INSPECTED AND APPROVED THE A/C FOR A FERRY FLIGHT TO CAK MX BASE FOR REPAIR. CAK MX INSPECT ED AND TIGHTEND A LINE ON THE PNEUMATIC OUTFLOW VALVE AND CHECKED THE ENG CONTROL LEVER MICROSWITCH RIGGING. OP CHECKS WERE COMPLETED AND THE A/C WAS RETURNED TO SERVICE. LATER IN THE DAY, THE A/C FAILED TO PRESSURIZE INBOUND TO PIT. PIT MX INSPECTED AND REPLACED THE PNEUMATIC OUTFLOW VALVE, IAW DORNIER MM 21-31-03. OS CHECKS WERE COMPLETED, AND THE A/C WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999040200046 19990402 00046 CE 1999 4 2 99ZZZX1162 1 19990301 A 3150 MASTER WARNING LEAR 35 35A 5170602 CE COCKPIT MALFUNCTIONED A DBCA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 13 68UW 095 MASTER WARNING PANEL LIGHTS ILLUMINATED PRIOR TO TAKEOFF. TROUBLESHOT TO WIRE SHORTING OUT ON RADIO RACK. REPAIRED WIR E IN WIRE BUNDLE. OERATIONS CHECKED OK. 2 L 7 2 4F A10CE 1999040200051 19990402 00051 EU 1999 4 2 99ZZZX1167 1 19990222 A 2913 65WE010305 PUMP HWKSLY DH125 BH125400A 4230138 EU NR 2 ENGINE FAILED A B7PA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NE 05 808CC 1059 A24185 NA779 ON FLIGHT FROM CAE TO SDL, AIRCRAFT INSTRUMENTS INDICATED THE RIGHT-HAND HYDRAULIC PUMP FAILED. THE CREW LANDED AT LIT AND INSPECTED RIGHT ENGINE. HYDRAULIC FLUID NOTICED ON THE ENGINE NACELLE. MAINTENANCE INSPECTION SHOWED THAT THE NR 2 HYDRAULIC PUMP HAD FAILED AT THE 'CAP' END. A CRACK AND SEPARATION OF THE PUMP HEAD TO BODY HAD CAUSED THE LOSS OF FLU ID. INITIAL REPORTS CANNOT DETERMINE IF THE PUMP HAD FAILED DUE TO THE 'CAP' FAILURE OR IF THE PUMP FAILED INTERNALLY A ND CAUSED THE 'CAP' FAILURE AND FLUID LOSS. 2 L 7 2 4J A3EU 1999040200056 19990402 00056 EA 1999 4 2 99ZZZX1172 2 19990213 A 7230 COMPRESSOR STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA LT ENGINE FAILED A DATA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 13 939MA 15552 3056 SH3047 PCE84125 EN ROUTE TO GSP TO LIT, THE LEFT ENGINE FAILED. THE CREW ELECTED TO SHUT DOWN THE ENGINE. THE AIRCRAFT WAS LANDED IN M EMPHIS, TN WITH AN UNEVENTFUL LANDING. THIS GAS GENERATOR WAS IN FOR REPAIR ONLY 14.9 HOURS AND 9 CYCLES PRIOR TO THE S HUT DOWN. 2 H 7 2 4T 4 T A41EU E4EA 1999040200094 19990402 00094 SO 1999 4 2 99ZZZX1210 1 19990304 A 3232 458910 FITTING WIEBEL 21141 PIPER PA31 PA31350 7103110 SO DOOR ACTUATOR BROKEN A WVBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 01 3527U 3154 317952141 ON TAKEOFF, PILOT SELECTED GEAR UP. RED UNSAFE LIGHT REMAINED ILLUMINATED. PILOT RETURNED TO BASE, PUMPED GEAR DOWN BY HAND. LANDED WITHOUT INCIDENT. RIGHT MAIN INNER GEAR DOOR ACTUATOR UP-LINE FITTING WAS SNAPPED IN HALF. DURING GEAR INSPECTION, OBSERVATIONS SHOULD BE MADE TO ENSURE TIRE OR BRAKE PARTS DO NOT ENTANGLE HYDRAULIC LINES. 1 L 7 2 3O A20SO 1999040200100 19990402 00100 CE 1999 4 2 99ZZZX1216 1 19990124 A 3230 08421201 TUBE ASSY CESSNA 310 310L 2074230 CE NLG BROKEN A ESEA O OTHER O OTHER LD LANDING 1 SO 11 73NR 3963 310L0112 DRIVE TUBE FOR NOSE GEAR SYSTEM BROKE AT LANDING GEAR ACTUATOR DUE STRESS OF DRIVE TUBE. 1 L 7 2 3O 3A10 1999040200182 19990402 00182 NM 1999 4 2 CA990318002 1 19990303 A 5740 200012001 FITTING 200028508 PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3432 3432 L1298648A (CAN) CRACK FOUND IN BOTH THE RIGHT HAND WING LOWER FRONT SPAR AND LOWER REAR SPAR WING TO FUSELAGE FITTING. CRACKS CAN BE SEEN FROM MAIN WHEELWELL. COMPANY PLANS TO X-RAY WINGS, CAPS WEBS, ETC., AND ALSO TO CHECK THE REST OF THEIR FLEET. AIRCRAFT USED SOMETIMES IN 'BIRDDOG' ROLE. SUBMITTER SPOKE TO PIPER . 1 M 7 2 3O 3 O RT A17WE 1E4 1999040200183 19990402 00183 WP 1999 4 2 TWAA9904601 1 19990325 A 3350 0105606003 HARNESS DOUG DC9 DC983 3022083 WP ROW 15 & 16 WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9409F 53121 THE CABIN EGRESS LIGHTS TRACK COVERS WERE BROKEN AT ROWS 15 AND 16, CAUSING WIRES TO PULL OUT OF HARNESS. REPLACED HARN ESS AND TRACK COVERS. CHECK-C 5-6-98 STL. 2 L 7 2 4F RT A6WE 1999040200184 19990402 00184 EU 1999 4 2 MALA976408 1 19990323 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU RIGHT ENGINE FAILED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 102XJ 340A102 RIGHT FIRE DETECT FAIL LIGHT ILLUMINATED ON AND OFF SEVERAL TIMES, USUALLY AROUND 40 PERCENT TORQUE. AIRCRAFT LANDED WI THOUT INCIDENT. MAINTENANCE REPLACED RIGHT FORWARD FIRE LOOP, IAW SF340 AMM 26-11-00. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999040200185 19990402 00185 NM 1999 4 2 PCAA9900004 1 19990323 A 3297 WIRE DHAV DHC8 DHC8102 2809003 NM NLG BROKEN A PCAA O OTHER N FALSE WARNING DE DESCENT 1 EA 13 829EX 146 BWI-FLT 3616: UPON DESCENT, THE NLG FAILED TO INDICATE DOWN AND LOCKED. DOWN AND LOCKED VERIFIED VIA THE ALTERNATE INDI CATION. MAINTENANCE INSPECTED AND FOUND A BROKEN WIRE FOR THE NLG STAY STRUT SENSOR. WIRE WAS REPAIRED AND AN OPERATIO NAL CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999040200186 19990402 00186 NM 1999 4 2 PCAA9900005 1 19990324 A 2611 SMOKE DETECTOR 473054 DHAV DHC8 DHC8102 2809003 NM NR 2 FAILED A PCAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 13 831MA 00050W 335 ACY - FLT3698: AIRCRAFT WAS EN ROUTE TO PHL WHEN A BAG BAY SMOKE WARNING LIGHT ILLUMINATED. THE CREW DIVERTED INTO ACY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE. THEY FOUND THE NR 2 SMOKE D ETECTOR AT FAULT. THE DETECTOR WAS ISOLATED PER MEL INSTRUCTIONS AND THE AIRCRAFT WAS RETURNED TO SERVICE. SUBSEQUENTL Y, DURING OVERNIGHT MAINTENANCE THE SMOKE DETECTOR WAS REPLACED. 2 H 7 2 4T RT A13NM 1999040200187 19990402 00187 WP 1999 4 2 CALA9900315 1 19990324 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 604 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND TWO .5 INCH CRACKS IN LEFT LOWER FUSELAGE TO WING CENTER SECTION ANGLE AT FS 604, APPROXIMATELY LEFT LO WER BELLY FORWARD ADF SENSE ANTENNA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-45. 2 L 7 2 4F A6WE 1999040200188 19990402 00188 WP 1999 4 2 CALA9900316 1 19990324 A 2752 BRACKET DOUG DC9 DC982 3022082 WP LT TE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 1 CRACK IN LEFT WING NR 1 FLAP ACTUATOR FORWARD MOUNT BRACKET. A NEW FLAP MOUNT BRACKET WAS INSTALLE D IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999040200189 19990402 00189 WP 1999 4 2 CALA9900317 1 19990324 A 2752 FITTING DOUG DC9 DC931 3022065 WP LT TE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND A 1.6 CRACK IN LEFT FLAP O/B ACTUATOR AFT HINGE FITTING. THE LEFT FLAP O/B ACTUATOR AFT HINGE FITTING WAS REMOVED AND REPLACED IAW OHM 27-50-01, PAGE 505. 2 L 7 2 4F A6WE 1999040200190 19990402 00190 WP 1999 4 2 CALA9900318 1 19990324 A 5752 59100511 SKIN DOUG DC9 DC931 3022065 WP LT AILERON TAB DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND LEFT AILERON TAB DEBONDED. THE LEFT AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-51, PAGE 203. 2 L 7 2 4F A6WE 1999040200191 19990402 00191 WP 1999 4 2 CALA9900319 1 19990324 A 5245 SKIN DOUG DC10 DC1030 3023501 WP NR 3 PACK DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A 1.5 CRACK IN SKIN OF PACK DOOR NR 3. THE AREA WAS REPAIRED IAW SRM 53-50-00, FIGURE 3. 2 L 7 3 4F A22WE 1999040200192 19990402 00192 WP 1999 4 2 CALA9900320 1 19990324 A 7110 INLET DOUG DC10 DC1030 3023501 WP NR 3 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND TWO INCH CRACKS IN THE NR 3 ENGINE FAN INLET. REPAIRED IAW SRM 54-11-00, PAGE 23. 2 L 7 3 4F A22WE 1999040200193 19990402 00193 WP 1999 4 2 CALA9900321 1 19990324 A 5753 SKIN DOUG DC10 DC1030 3023501 WP RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A 1 CRACK IN RT WING OUTBOARD FLAP SKIN. THE SKIN WAS REPLACED IAW DOUGLAS DRAWING ARC1653. 2 L 7 3 4F A22WE 1999040200194 19990402 00194 NM 1999 4 2 CALA9900322 1 19990325 A 5330 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 AN INSPECTION OF THE LOWER SKIN OUTER SURFACE ALONG THE LOWEST ROW AT STRINGER 4R LAP SPLICE FROM BS 681 TO BS 740 FOUND CRACKS IN THE ENTIRE LENGTH OF THE PANEL. THE CRACKS MEASURED FROM .0625 INCH TO .25 INCH LONG. THE AREA WAS REPAIRED IAW ECRA 5330-02785. A DIP WAS ISSUED STATING THAT ENGINEERING WOULD PROVIDE FINAL DISPOSITION OF THE REPAIR WITHIN 23 MONTHS OF THIS REPAIR, AND UNTIL FINAL DISPOSITION LFEC INPECTION OF THE REPAIR WOULD BE PERFORMED IAW EA 5330-02762. 2 L 7 3 4F A3WE 1999040200195 19990402 00195 WP 1999 4 2 CALA9900323 1 19990325 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 1338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 1.5 CRACK IN AFT ENTRY DOOR JAMB FITTING BETWEEN LONGERON 14L AND 15L, STA 1338. A NEW FITTING WAS I NSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999040200196 19990402 00196 WP 1999 4 2 CALA9900324 1 19990325 A 3350 P4010021 BATTERY DOUG DC10 DC1030 3023501 WP ROW 1-4 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND FLASHLIGHTS INOPERATIVE AT FLIGHT ATTENDANT SEATS 1L-4L AFT. THE FLASHLIGHT BATTERIES WERE REPLACED IA W MM 25-60-00. 2 L 7 3 4F A22WE 1999040200197 19990402 00197 WP 1999 4 2 CALA9900325 1 19990325 A 5414 SKIN DOUG DC10 DC1030 3023501 WP NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A 1 CRACK IN NR 3 PYLON SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5450-01212. A DIP WAS ISSUED TO CHECK BLIND FASTENERS FOR SECURITY EVERY 1000 CYCLES UNTIL A PERMANENT REPAIR IS INSTALLED WITHIN 400 DAYS. 2 L 7 3 4F A22WE 1999040200198 19990402 00198 NE 1999 4 2 9901132703 2 19990323 A 7314 378200 FUEL PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE LEFT ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 GL 01 8878Z 35129 3286 21451 695266 DURING CLIMB-OUT, THE LEFT ENGINE EXPERIENCED A FLAMEOUT. AIRCRAFT RETURNED TO FAR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL PUMP AND FUEL CONTROL. ENGINE OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1999040200199 19990402 00199 NM 1999 4 2 9901142299 1 19990324 A 2913 323636 PUMP BOEING 727 727251 138408H NM B HYD SYST CRACKED A NWAA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 299US 1434 1434 22153 ON APPROACH TO MSP, THE B SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH B SYSTEM PUMPS AND CHECKED CASE DRAIN FILTER. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999040200200 19990402 00200 NM 1999 4 2 9901152702 1 19990324 A 2131 CONTROLLER BOEING 727 727225 1384077 NM CABIN FAILED A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 8877Z 21450 CLIMBING THROUGH FL240, AUTO PRESSURIZATION FAILED TO MAINTAIN CABIN ALTITUDE. MANUAL CONTROL WAS SELECTED AND A DESCEN T WAS INITIATED. AT APPROXIMATELY 15,000 FT CABIN ALTITUDE, THE WARNING HORN SOUNDED AND OXYGEN MASKS WERE DEPLOYED. F LIGHT DESCENDED TO 11,000 FT AND CONTINUED TO PHX LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAIBN CONTROLLER A ND CONTROL PANEL. PRESSURIZATION CHECKED OK. 2 L 7 3 4F A3WE 1999040200201 19990402 00201 WP 1999 4 2 UPS99829111 1 19990202 A 5347 S277260 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1050-150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, UPPER FLANGE, LWR SURFACE, FS 1050-1150, RBL 58, IS CORRODED BEYOND LIMITS. C UT OUT DAMAGED SECTION, FABRICATED, AND REPLACED SEAT TRACK FS 1050 TO 1170 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200202 19990402 00202 WP 1999 4 2 UPS99829112 1 19990222 A 5320 37540251 FITTING DOUG DC8 DC873F 302199F WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1160, LONGERON 27R, THE FITTING IS CRACKED AND CORRODED. REMOVED, FABRICATED, AND REPLACED THE FI TTING IAW DWG 3754025 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200203 19990402 00203 WP 1999 4 2 UPS99829113 1 19990228 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1040 FRAME, BETWEEN LONGERON 31R AND 32R, IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FAB RICATED, AND REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999040200204 19990402 00204 WP 1999 4 2 UPS99829114 1 19990303 A 5320 3773077509 SUPPORT BEAM DOUG DC8 DC873F 302199F WP BS 1260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1260 AT LONGERON 27R, THE FLOORBEAM SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND R EPLACED FLOORBEAM SUPPORT IAW DWG 3773077 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200205 19990402 00205 WP 1999 4 2 UPS99829115 1 19990220 A 5313 56470251 LONGERON DOUG DC8 DC873F 302199F WP BS 1675 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 EXFOLIATING CORROSION ON LONGERON 33L AT FS 1675. CUT OUT DAMAGED SECTION, FABRICATED AND SPLICED IN LONGERON 33L, IAW SRM 53-2-2 FIG 8. 2 L 7 4 4F RT 4A25 1999040200206 19990402 00206 WP 1999 4 2 UPS99829117 1 19990303 A 5320 975600266 SUPPORT DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FLOORBEAM SUPPORT AT FS 1220 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED, AND REPLACED SUPPORT IA W DWG 9754002 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200207 19990402 00207 WP 1999 4 2 UPS99829118 1 19990221 A 5320 37502571 FITTING DOUG DC8 DC873F 302199F WP BS 200-220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 LONGERON 31L SPLICE FITTING CRACKED AT FS 200-220. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200208 19990402 00208 WP 1999 4 2 UPS99829119 1 19990223 A 5320 37540252 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 SUPPORT FITTING AT FS 1220, LONGERON 21R IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW D WG 3754025 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200209 19990402 00209 WP 1999 4 2 UPS99829120 1 19990301 A 5320 3773077509 SUPPORT DOUG DC8 DC873F 302199F WP BS 1380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FLOORBEAM SUPPORT ANGLE CORRODED BEYOND LIMITS, FS 1380 AT LONGERON 27R. REMOVED, FABRICATED, AND RE PLACED SUPPORT IAW DWG 3773077 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200210 19990402 00210 WP 1999 4 2 UPS99829121 1 19990222 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1020 FRAME BETWEEN LONGERON 32R AND 35R IS CORRODED OUT OF LIMITS. CUT OUT DAMAGED SECTION AND RE PAIRED IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040200211 19990402 00211 WP 1999 4 2 UPS99829122 1 19990226 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 500 FRAME AT LONGERON 7L IS CORRODED OUT OF LIMITS. REPAIRED FRAME IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999040200212 19990402 00212 WP 1999 4 2 UPS99829123 1 19990301 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1020 FRAME AT LONGERON 33L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGE, AND REPAIRED IAW SRM 53-2-0 . 2 L 7 4 4F RT 4A25 1999040200213 19990402 00213 WP 1999 4 2 UPS99829124 1 19990302 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FS 1100 FRAME CAP LONGERON 31R TO 32R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED C AP IAW 53-2-0. 2 L 7 4 4F RT 4A25 1999040200214 19990402 00214 WP 1999 4 2 UPS99829125 1 19990306 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1746 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3 FUSELAGE SKIN IS CRACKED AT FS 1746, LONGERON 16R. CUT OUT DAMAGED AREA, AND REPAIRED IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 1999040200215 19990402 00215 WP 1999 4 2 UPS99829126 1 19990325 A 2910 AE246353050766 HYDRAULIC LINE DOUG DC8 DC873F 302199F WP NR 2 ENGINE FAILED A IPXA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 802UP 46100 INSPECTION TYPE-N/A, ON ARRIVAL TO SJU LOSS ON HYD PRESSURE. CHECKLIST COMPLETE, HAD TOTAL LOSS OF BRAKE PRESSURE AND D EPLOYED THE AIR BRAKE SYSTEM. REPLACED NR 2 HYD PUMP OUTLET LINE, REPLACED ENG FILTERS AND SERVICED SYS PER M/M 29-00-0 0 & 12-30-01, SERVICED EMERGENCY BRAKE ACC AND RAN ENGS OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999040200216 19990402 00216 WP 1999 4 2 UPS99829127 1 19990311 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C123 STA 660 BTWN STR 35L TO 36, THE FUSELAGE SKIN IS CORRODED. REPAIRED AREA IAW DH SK 808-237. 2 L 7 4 4F RT 4A25 1999040200217 19990402 00217 WP 1999 4 2 UPS99829128 1 19990306 A 5347 5750872 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1660-1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C123 SEAT TRACK BTWN STA 1660-1680 RBL 59 HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040200218 19990402 00218 WP 1999 4 2 UPS99829129 1 19990220 A 5320 3751193503 FITTING DOUG DC8 DC873F 302199F WP BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C123 RT FLOORBEAM ATTACH SPLICE AT STA 1660 IS CRACKED. REMOVED, FABRICATED AND REPLACED SPLICE IAW 375 1193 AND SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1999040200219 19990402 00219 WP 1999 4 2 UPS99829130 1 19990316 A 5320 564932949 DOUBLER DOUG DC8 DC873F 302199F WP BS 1756 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C123 STA 1756 AT BLO, THE INTERNAL DOUBLER HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 808-946. 2 L 7 4 4F RT 4A25 1999040200220 19990402 00220 WP 1999 4 2 UPS99829131 1 19990306 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1748 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C123 FUSELAGE EXTERIOR SKIN AT STA 1748 STR 16L IS CRACKED. REPAIRED AREA IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 1999040200221 19990402 00221 NM 1999 4 2 99FDEA00123 1 19990325 A 5320 65425451 WEB BOEING 727 72725C 138400H NM BS 440-650 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 WHILE WORKING NRO418, FOUND CORROSION ON WEB AT BS 440 TO 650 LBL 60 TO 65 WL 208.1. *S/D* REMOVED AND REPLACED WEB PER EA 7-5310-43763. 2 L 7 3 4F A3WE 1999040200222 19990402 00222 NM 1999 4 2 99FDEA00124 1 19990326 A 2710 WARNING LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 606FE 48602 AIL DEFLECT DISAG LVL 2 ALERT ON FLAP RETRACTION, STAYED ON SLAT RETRACTION, GOES AWAY WHEN FLAPS EXT FOR LANDING. A/C RELEASED FOR SERV PER MEL/CDL 27-2 CATEGORY C EXP 4APR99 FCC1-FCC2 REPT NO FAULTS LAST LEG. PERF'D FCC1/FCC2 AIL SYS TE ST PER MM 22-00-00-840-801. ALL TESTS PASSED. CONFIRMED CORRECT AIL IND ON CONFIG PG ON FLAP EXT/RET AND INBD AIL FAIR ED AND OUTBD DROOP NEUTRAL PER THE AIL NEUTRAL POS PLACARD (MM 27-10-00-5) C/W MSP 27-2 METHOD A PULLED AND TAGGED C/B A -07. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 1999040200223 19990402 00223 EU 1999 4 2 99FDEA00125 1 19990326 A 2130 VALVE AIRBUS 310 A310203 EU E & E COMPT FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 426FE 245 EQUIP COOLING OVBD VALVE FAILED TO CLOSE, COULD NOT PRESSURIZE CABIN. *S/D* REPLACED AIRFLOW SENSOR DET MM 21-23-00. R EMOVED AND REPLACED COOLING OVBD EXTRACTION VALVE MM 21-23-13. 2 L 7 2 4F RT A35EU 1999040200224 19990402 00224 NM 1999 4 2 99FDEA00126 1 19990327 A 2781 CONNECTOR BOEING 727 727227 1384078 NM NR 5 LE SLAT BENT A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 491FE 21529 AIR TURNBACK, FLT CREW REPORT LEAD EDGE SLAT NR 5 INTRANSIT LIGHT REMAINS ON. *S/D* FOUND BENT PIN CONN D5226P. REPLACE D PER WIRING DIAGRAM MANUAL 31-31-04. OPER CK GOOD PER MM 27-82-000-0. 2 L 7 3 4F A3WE 1999040200225 19990402 00225 WP 1999 4 2 ABXA9900243 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 733 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 733.000. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999040200226 19990402 00226 WP 1999 4 2 ABXA9900244 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 728.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE XFS 728.750, UPPER LEADING EDGE RIB CRACKED. REPAIIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999040200227 19990402 00227 WP 1999 4 2 ABXA9900239 1 19990304 A 5315 9922393501 FLOORBEAM DOUG DOUG DC9 DC933F 302207A WP BS 294 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FLOORBEAM CORRODED AT STATION 294. REPAIRED FLOORBEAM IAW ABX REA D953-26903MR. 2 L 7 2 4F A6WE 1999040200228 19990402 00228 WP 1999 4 2 ABXA9900245 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 697.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 697.500. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999040200229 19990402 00229 WP 1999 4 2 ABXA9900246 1 19990211 A 5712 5769600 RIB DOUG DOUG DC8 DC863 302198A WP WS 622.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 622.500. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999040200230 19990402 00230 WP 1999 4 2 ABXA9900247 1 19990219 A 5532 5644115401 SKIN DOUG DOUG DC8 DC863 302198A WP VERT STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 VERTICAL STABILIZER LEADING EDGE SKIN CORRODED. REPAIRED IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999040200231 19990402 00231 WP 1999 4 2 ABXA9900248 1 19990325 A 3350 1437 BULB DOUG DC8 DC861 3021952 WP COCKPIT FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 841AX 45908 DURING PREFLIGHT, CREW FOUND FIRST OFFICER'S EMERGENCY LIGHTING INOPERATIVE. RELAMPED EMERGENCY LIGHTING IAW DC8 MM 34- 50-0. 2 L 7 4 4F 4A25 1999040200232 19990402 00232 WP 1999 4 2 ABXA9900249 1 19990324 A 2910 NAS16126 O RING DOUG DC8 DC862 3021970 WP NR 3 HYD PUMP FAILED A ABXA O OTHER K FLUID LOSS CR CRUISE 1 GL 23 805AX 45906 DURING CRUISE, HYDRAULIC SYSTEM QUANTITY DECREASED. PERFORMED LOSS OF HYDRAULICS EMERGENCY PROCEDURES. REPLACED O-RING ON NR 3 ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 4 4F 4A25 1999040200233 19990402 00233 NE 1999 4 2 99ZZZX1220 2 19990201 A 7321 0164248700 FCU SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING H K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 6099P 1840 1134 C022B 2818 9365 FUEL COMING OUT OF P-2 SENSING LINE. FUEL SMELL IN COCKPIT HEATING SYSTEM. 1 G 7 1 3U 3 U H9EU E19EU 1999040200242 19990402 00242 SW 1999 4 2 99ZZZX1229 1 19990306 A 2910 70053H000A100A LINE BELL 206 206L3 1182108 SW HYDRAULIC SYSTEM LEAKING A ALGA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 343AL 51372 DURING FLIGHT, THE HYDRAULIC SYSTEM LOST PRESSURE. PRESSURE LINE FROM PUMP WAS FOUND LEAKING. 1 G 7 1 3U H2SW 1999040200251 19990402 00251 SW 1999 4 2 99ZZZX1238 1 19990303 A 6510 406040340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 407AL RNFS8779 53044 DURING COMPLIANCE OF AD 97-24-17 PTA, FOUND NR 6 D/S DISC PACK CRACKED. TWO DISC VISUALLY CRACKED APPROXIMATELY MID-WAY BETWEEN TWO BOLT HOLES. 1 G 7 1 3U O H2SW 1999040200255 19990402 00255 SW 1999 4 2 99ZZZX1242 1 19990304 A 3210 MS2774324 RELAY BELL 407 407 SW MLG FAILED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 477AL 53203 DURING FIRST TURNING ON OF BATTERY IN MORNING, LANDING LIGHT UPPER WAS ON AND WOULD NOT TURN OFF BY SWITCH. THIS IS THE SECOND RELAY INSTALLED FOR THE UPPER LANDING LIGHT ON THIS AIRCRAFT. TOTAL TIME OF THE RELAY IS UNKNOWN, BUT IS ALSO A PROBLEM FOR OTHER 407'S OPERATED HERE. 1 G 7 1 3U O H2SW 1999040200259 19990402 00259 EU 1999 4 2 99ZZZX1246 1 19990218 A 3500 EMS INTERIOR E428 BOLKMS 117 BK117B1 5626012 EU CABIN FAILED A OLJA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 121LF 2500 9101003 7226 AIRCRAFT ON RETURN FLIGHT WITH PATIENT ONBOARD. CREW NOTICED UNUSUAL ODOR AND LIGHT HAZE OF SMOKE IN CABIN/COCKPIT. PI LOT PERFORMED PRECAUTIONARY LANDING WITHOUT INCIDENT. UPON MAINTENANCE ARRIVAL, MECHANIC FOUND AIR PUMP CIRCUIT BREAKER TRIPPED. LOCATED AIR PUMP AND CONFIRMED PUMP HAD FAILED INTERNALLY. REPLACED WITH NEW. MANUFACTURER HAS NO PM SCHEDU LE. 1 G 7 2 3U H13EU 1999040200260 19990402 00260 SW 1999 4 2 99ZZZX1247 1 19990225 A 6320 204040129001 RETAINER 206040004101 BELL 206 206L1 1182107 SW M/R GEARBOX BROKEN B ZV1R K NONE O OTHER IN INSP/MAINT 1 SW 03 2611 20804 3147 BHC00049 45417 UPON TEAR-DOWN OF TRANSMISSION FOR INSPECTION, FOUND SCREEN ASSY FULL ON PLASTIC OR NYLON PIECES. INSPECTED PLANETARY A SSY FOUND 3 EACH GEAR ASSYS WITH NO RETAINERS REMAINING, ONE EACH RETAINER WAS IN PLACE. ONCE REMOVED, IT FELL APART. U PGRADE RETAINERS TO NEW P/N 214-040-515-001. 1 G 7 1 3U H2SW 1999040200287 19990402 00287 NM 1999 4 2 ASAA9940008 1 19990126 A 5210 BEARING BOEING 737 737490 1384715 NM L1 DOOR SEIZED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 793AS 28888 SEA - PRIOR TO FLT 322, THE L1 DOOR WAS FOUND TO BE HARD TO OPEN. REPLACED CRANK ARM BEARING AND DOOR OPERATED NORMALLY . 2 L 7 2 4F RT A16WE 1999040200288 19990402 00288 SO 1999 4 2 C2XA99IA152 1 19990212 A 3350 66364 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14945 145049 IAH - DURING 1A INSPECTION, THE AFT EMERGENCY AISLE PATH LIGHTSTRIP WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED LIGHTSTRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999040200289 19990402 00289 SO 1999 4 2 99ZZZX1273 1 19990209 A 3234 A4865 LEVER GULSTM G1159 G1159 3953505 SO COCKPIT CRACKED A COZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 27 102CX 102 AFTER TAKEOFF, CREW COULD NOT SELECT GEAR HANDLE TO THE RETRACT POSITION AND RETURNED TO BASE. INVESTIGATION REVEALED T HE LANDING GEAR HANDLE LEVER HAD BROKE PROVIDING TOO MUCH SIDE PLAY FOR THE GEAR HANDLE TO BE MOVED OUT OF THE DETENT. L EVER CRACKED WHERE A HOLE HAD BEEN DRILLED BY OEM TO ALLOW PASSAGE OF ELEC WIRE TO HANDLE LIGHTS. DEFECTIVE PART MFG BY AVIONICS PROD ENG INC., UNDER PN A486-5, SN 228. UNIT INSTALLED BY GAC ON 5-5-83. NO KNOWN TIMES LISTED. PART APPEAR ED TO HAVE BEEN MFG 3-83. TT 5,660.8 HRS, 2,743 CYCLES. GEAR HANDLE LEVER ASSY ROUTED TO GULFSTREAM, SAVANNAH, GEORGIA TO TECH SERVICE FOR EVALUATION. A REPORT HAS BEEN REQUESTED. (M) 2 L 7 2 4F RT A12EA 1999040200290 19990402 00290 1999 4 2 99ZZZX1274 4 19990203 A 2565 104328 SLIDE AIRCRUISERS 616010020 BOEING 737 737230 NM LE DOOR FAILED A E6RA K NONE O OTHER IN INSP/MAINT 1 CE 01 623AC 15137 23157 DURING MAINTENANCE SERVICE CHECK, FOUND LEFT AFT (L2) DOOR EMERGENCY EVACUATION SLIDE RESERVOIR PRESSURE LOW. REPLACED SLIDE ASSEMBLY. 2 L 7 2 4F RT A16WE 1999040200291 19990402 00291 WP 1999 4 2 GTIA9900007 1 19990128 A 2422 INVERTER DOUG DC9 DC982 3022082 WP E/E COMPARTMENT FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805RA 48087 EMERGENCY INVERTER CIRCUIT BREAKER TRIPS WHEN EMERGENCY POWER IS TURNED ON. AIRCRAFT EMERGENCY BUS LIGHT ALSO COMES ON. REMOVED AND REPLACED INVERTER PER MM 24-22-0 OPERATIONAL CHECKED NORMAL. 2 L 7 2 4F A6WE 1999040200292 19990402 00292 EA 1999 4 2 99ZZZX1275 1 19990203 A 5520 C6TPM102229 HINGE C6TP1001 DHAV DHC6 DHC6300 2802606 EA RT ELEVATGOR LOOSE A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 122SA 515 DURING SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND RT ELEVATOR HINGE PLATE RIVET FASTENERS WORKING LOOSE IN STABIL IZER END RIB. UPON RFEMOVAL OF RT ELEVATOR TO ALLOW REPAIR, FOUND RIVETS PULLED THROUGH ELEVATOR BOTTOM OUTBOARD AND TR AILING EDGE SKINS. REPAIRS WERE ACCOMPLISHED BY REPLACEMENT OF DAMAGED PARTS. 1 H 7 2 3T RT A9EA 1999040200293 19990402 00293 EA 1999 4 2 MASA99021 1 19990209 A 3350 GE1317 BULB BRUCE BM10006002 CNDAIR CL600 CL6002B19 EA RT EMERG EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 WHILE PERFORMING ROUTINE MAINTENANCE, MAINTENANCE FOUND THE FORWARD, RT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENAN CE REPLACED THE BULBS, OPS CHECKED GOOD. (X) 2 L 7 2 4F RT A21EA 1999040200294 19990402 00294 SO 1999 4 2 SIMA990251 1 19990125 A 3230 156221 SWITCH EMB 145 EMB145 SO HYDRAULIC SYSTEM LEAKING A SIMA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 21 606AE 0258 145062 CLE - FLT 4387 - NR 1 HYDRAULIC SYSTEM FAILED. LANDING GEAR HAD TO BE MANUALLY EXTENDED. REMOVED AND REPLACED LEAKING HYDRAULIC PRESSURE SWITCH. SERVICED SYSTEM AND PERFORMED OPERATIONAL CHECK WITH NO FURTHER DEFECTS NOTED. (X) 2 L 7 2 4F RT T00011AT 1999040200306 19990402 00306 NM 1999 4 2 TWAA9904701 1 19990326 A 3350 0105606003 LIGHT BOEING 767 7673Y0 NM ROW 5 MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 FOUND THE CABIN EGRESS LIGHT ASSEMBLY AND LENS MISSING AT ROW 5, RT SIDE OF AIRCRAFT. INSTALLED LIGHT ASSEMBLY AND LENS . LENS MFG 0105607-001. CHECK-C 3-6-99 LAX. 2 L 7 2 4F RT A1NM 1999040200307 19990402 00307 WP 1999 4 2 TWAA9904702 1 19990327 A 3350 PR2 BULB DOUG DC9 DC983 3022083 WP ROW 4 & 5 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951TW 53470 FOUND THREE CABIN EGRESS LAMPS INOPERATIVE AT ROWS 4 AND 5, AND THE EMERGENCY LIGHT INOPERATIVE AT THE FWD LT CABIN DOOR . RECONNECTED LIGHT ASSEMBLY AT CABIN ROW 4, AND RELAMPED THE EMERGENCY LIGHT ASSEMBLY. CHECK-C 6-14-98 STL. 2 L 7 2 4F RT A6WE 1999040200308 19990402 00308 NM 1999 4 2 TWAA9904703 1 19990328 A 3350 767 BULB BOEING 757 7572Q8 1384972 NM R4 DOOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 712TW 27624 THE EVACUATION SLIDE LIGHT WAS INOPERATIVE AT THE NUMBER 4 DOOR, RT SIDE OF THE AIRCRAFT. REPLACED THE LAMP. CHECK-C 1 2-11-98 LAX. 2 L 7 2 4F RT A2NM 1999040200309 19990402 00309 WP 1999 4 2 AT9900257 1 19990324 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-598 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT HAND FUSELAGE EXTERIOR SKIN WITH NUMEROUS DENTS AND REPAIRS FROM BS 229-598 L-18-26R. REMOVED AND REPLACED SKIN FROM BS 229 TO 598 IAW DC9 SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3, 51-1 0-4, AND RES NR 99413 AND 99587. 2 L 7 2 4F A6WE 1999040200310 19990402 00310 WP 1999 4 2 AT9900258 1 19990309 A 5320 1A436871 DOUBLER DOUG DC9 DC932 3022066 WP BS 464 OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN EXTERNAL DOUBLER THAT INTERFERES WITH WINDOW BELT DOUBLER AT BS 464 L-1 4 ON THE RIGHT SIDE. REMOVED EXISTING DOUBLER, FORMED NEW DOUBLER, DRILLED, COUNTERSUNK, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, 51-10-2, 51-20-0, 51-30-0, AND RES NR 99581 AND 99576. 2 L 7 2 4F A6WE 1999040200311 19990402 00311 WP 1999 4 2 AT9900259 1 19990113 A 5510 FAIRING DOUG DC9 DC932 3022066 WP HORIZONTAL STAB DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 825AT 47319 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DELAMINATION ON INBOARD AND OUTBOARD SIDES OF LEFT HAND UPPER HORIZONTAL S TABILIZER FAIRING. REMOVED INNER SKIN AND HONEYCOMB CORE FROM LEFT HAND UPPER HORIZONTAL STABILIZER FAIRING THAT WAS DE LAMINATED. TRIM NEW HONEYCOMB CORE TO FIT, FABRICATED SPLICE REPAIR, DOUBLER, BONDED HONEYCOMB SECTION AND INSTALLED SE CTION OF INNER SKIN AND SPLICE REPAIR IAW DC9 SRM 51-70-2 PG 80-83, 51-10-3, 51-10-2, AND 51-10-4. 2 L 7 2 4F A6WE 1999040200312 19990402 00312 WP 1999 4 2 AT9900260 1 19990322 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 965 LBL 24 CORRODED. FABRICATED FLOOR SUPPORT REP AIR ANGLE AND INSTALLED IAW DC9 SRM 53-05 FIG 28. 2 L 7 2 4F A6WE 1999040200313 19990402 00313 WP 1999 4 2 AT9900261 1 19990322 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOORBEAM AT BS 965 LBL 35 CORRODED. FABRICATED NEW FLOOR SUPPORT FIT TING AND INSTALLED IAW DC9 SRM 53-11-3. 2 L 7 2 4F A6WE 1999040200314 19990402 00314 WP 1999 4 2 AT9900262 1 19990325 A 5320 1A45141 SUPPORT DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 996 LBL 35 CORRODED. INSTALLED FLOORBEAM REPAIR I AW DC9 SRM 53-05 FIG 20A. 2 L 7 2 4F A6WE 1999040200315 19990402 00315 WP 1999 4 2 AT9900263 1 19990324 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 1070 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 1070 CORRODED. CUT AND DRILLED REPAIR ANGLE, INST ALLED REPAIR IAW DC9 SRM 51-30-5, AND 53-05-0. 2 L 7 2 4F A6WE 1999040200316 19990402 00316 WP 1999 4 2 AT9900264 1 19990318 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT GALLEY FLOORBOARD AROUND THE DRAIN FITTING AT BS 996 LEFT HAND COR RODED. REPLACED SKIN AND STRINGERS IAW DC9 SRM 51-70-0, 51-10-2, AND 53-21-0. 2 L 7 2 4F A6WE 1999040200317 19990402 00317 WP 1999 4 2 AT9900265 1 19990317 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT Z ANGLE ON TOP OF FLOORBEAM CRACKED AND CORRODED AT BS 9 65 LBL 24 TO RBL 24. REMOVED AND REPLACED TWO FLOOR SUPPORT Z ANGLES IAW DC9 SRM 51-10-4, 51-10-3, 51-10-2, 53-11-3 FIG 11 AND 51-30-2. 2 L 7 2 4F A6WE 1999040200318 19990402 00318 WP 1999 4 2 AT9900266 1 19990328 A 3610 491334 DUCT DOUG DC9 DC932 3022066 WP NR 1 ENGINE DEFECTIVE A ZZDA K NONE J WARNING INDICATION CL CLIMB 1 SO 15 809AT 47322 NR 1 ENGINE FIRE WARNING WITH CLIMB POWER THROTTLE TO IDLE WARNING CEASED IMMEDIATELY. REMOVED AND REPLACED HEAT DUCT I AW PRATT AND WHITNEY MM 72-00. 2 L 7 2 4F A6WE 1999040200319 19990402 00319 WP 1999 4 2 CALA9900326 1 19990326 A 5320 STRAP DOUG DC9 DC931 3022065 WP BS 937-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND AFT CARGO COMPARTMENT LONGERON 23L STRAP BETWEEN STA 937 AND 967 CORRODED. THE FASTENERS AND STRAP WER E REMOVED IAW SRM 51-30-2. THE SURFACE CORROSION WAS REMOVED IAW SRM 51-10-3. A NEW STRAP WAS INSTALLED IAW SRM 51-01- 0, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999040200320 19990402 00320 WP 1999 4 2 CALA9900327 1 19990326 A 5522 SKIN DOUG DC9 DC931 3022065 WP LEFT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND A 2.5 INCH CRACK IN LT ELEVATOR O/B TRAILING EDGE SKIN (JUST I/B OF STATIC WICK). THE CRACK WAS STOP D RILLED AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 51-70-1, PAGE 12. WEIGHT AND BALANCE WAS WITHIN LIMITS IAW SRM 55- 20-1, FIGURE 4. 2 L 7 2 4F A6WE 1999040200321 19990402 00321 WP 1999 4 2 CALA9900328 1 19990326 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 237 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT OVERHEAD FLOORBEAM AT STA 237, LBL 8. THE CRACKED AREA WAS CUT OUT IAW SRM 53-05, PAGE 216A. A DOUBLER AND REPAIR ANGLES WERE INSTALLED IAW SRM 53-05, PAGE 216A. 2 L 7 2 4F A6WE 1999040200322 19990402 00322 WP 1999 4 2 CALA9900329 1 19990326 A 5730 SKIN DOUG DC9 DC931 3022065 WP RIGHT WING DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND RT WING LOWER SKIN PANEL FORWARD OF RIGHT GEAR DEBONDED. THE PANEL WAS REMOVED, REPAIRED AND INSTALLED IAW SRM 51-30-2, PAGE 4. 2 L 7 2 4F A6WE 1999040200323 19990402 00323 WP 1999 4 2 CALA9900330 1 19990326 A 5730 ARB110658 PANEL DOUG DC10 DC1030 3023501 WP RIGHT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A 3 INCH CRACK IN RT WING LEADING EDGE ACCESS PANEL NR 617CT. THE PANEL WAS REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999040200324 19990402 00324 WP 1999 4 2 CALA9900331 1 19990326 A 5414 AUB7108157 PANEL DOUG DC10 DC1030 3023501 WP NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND A 3 INCH CRACK ON NR 3 PYLON PANEL NR 487ER. THE PANEL WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999040200325 19990402 00325 WP 1999 4 2 CALA9900332 1 19990327 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 790-805 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 790 TO 805. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999040200326 19990402 00326 WP 1999 4 2 CALA9900333 1 19990327 A 5751 SKIN DOUG DC10 DC1030 3023501 WP RIGHT AILERON CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND RT WING O/B AILERON LOWER SKIN CORRODED. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-02. 2 L 7 3 4F A22WE 1999040200327 19990402 00327 SO 1999 4 2 COMA9910046 1 19990326 A 5330 12022788003 SKIN EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 257CA 120248 DURING 2,000 FLIGHT CYCLE CHECK, FOUND CRACK EXTENDING FROM RIVET HOLE FORWARD ON RIGHT SIDE BETWEEN RIGHT DV WINDOW AND RJ WINDSHIELD (POST SKIN). REPAIRED DAMAGED AREA IAW EMB FAX EST 474/95 DATED 01 NOVEMBER 95. 2 L 7 2 4T RT A31SO 1999040200328 19990402 00328 EA 1999 4 2 COMA9960132 1 19990327 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 932CA 7038 FLAPS FAIL CAUTION MESSAGE. COMPLIED WITH INSPECTION OF FLAPS PER AD 98-20-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999040200329 19990402 00329 EA 1999 4 2 COMA9960133 1 19990328 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 778CA 7297 FLAPS FAILED DURING APPROACH. INSPECTED FLAPS PER AD 98-20-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999040200330 19990402 00330 EA 1999 4 2 COMA9960134 1 19990326 A 3397 WIRE CNDAIR CL600 CL6002B19 EA ROW 9-13 LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 EMERGENCY FLOOR LIGHTING INOPERABLE FROM ROW 9 TO ROW 13. CONNECTED LOOSE WIRING, SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 1999040200331 19990402 00331 NM 1999 4 2 UPS99229134 1 19990326 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, RT FLOOR LEVEL FWD EEL INOP. REMOVED AND REPLACED EEL BATTERY, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999040200332 19990402 00332 NM 1999 4 2 UPS99229135 1 19990326 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, RT AFT CEILING EMERGENCY LIGHT AT GALLEY INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999040200333 19990402 00333 WP 1999 4 2 UPS99829116 1 19990311 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FLOORBEAM HAS HEAVY CORROSION ON THE UPPER FLANGE AT FS 1300, LBL 48. REPAIRED FLOORBEAM IAW DH SK8 08-870. 2 L 7 4 4F RT 4A25 1999040200334 19990402 00334 WP 1999 4 2 UPS99829133 1 19990224 A 5711 97510822 SPAR CAP DOUG DC8 DC873F 302199F WP WS 115.122 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, RT WING AUX TANK L/E AT FS 115.122 HAS HEAVY CORROSION THAT IS OUT OF LIMITS, (SPAR CAP). REMOVED AND REPLACED CAP IAW 9751082 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200335 19990402 00335 WP 1999 4 2 UPS99829136 1 19990226 A 5347 44157239 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 740-880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C2, FS 740 TO 880, RBL 60 THE SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK FROM FS 710 TO 9 10, RBL 60, FABRICATED & REPLACED THE SEAT TRACK IAW SRM 53-2-3 FIG 2. 2 L 7 4 4F RT 4A25 1999040200336 19990402 00336 WP 1999 4 2 UPS99829137 1 19990312 A 5320 37549181 FITTING DOUG DC8 DC873F 302199F WP BS 1187 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1187 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200337 19990402 00337 WP 1999 4 2 UPS99829138 1 19990312 A 5320 37549181 FITTING DOUG DC8 DC873F 302199F WP BS 1210 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1210 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200338 19990402 00338 WP 1999 4 2 UPS99829139 1 19990312 A 5320 37549181 FITTING DOUG DC8 DC873F 302199F WP BS 1203 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1203 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200339 19990402 00339 WP 1999 4 2 UPS99829140 1 19990314 A 5320 57503215 DOUBLER DOUG DC8 DC873F 302199F WP BS 1110 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1110 AT LONG 21R, THE FINGER DOUBLER IS CRACKED. REMOVED, FABRICATED & REPLACED THE FINGER DOUBL ER IAW DWG 5750321 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999040200340 19990402 00340 WP 1999 4 2 UPS99829141 1 19990312 A 5320 37540321 FITTING DOUG DC8 DC873F 302199F WP BS 1196 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1196 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200341 19990402 00341 WP 1999 4 2 UPS99829142 1 19990312 A 5320 37540321 FITTING DOUG DC8 DC873F 302199F WP BS 1187 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1187 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200342 19990402 00342 WP 1999 4 2 UPS99829143 1 19990315 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1660 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1660 FLOORBEAM AT RBL 45 HAS DOUBLE DRILLED HOLES. REPAIRED FLOORBEAM IAW DH SK808-353. 2 L 7 4 4F RT 4A25 1999040200343 19990402 00343 WP 1999 4 2 UPS99829144 1 19990312 A 5320 37540322 FITTING DOUG DC8 DC873F 302199F WP BS 1177 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 1177 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040200344 19990402 00344 NM 1999 4 2 QXEA9900511 1 19990219 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - SEAT TRACK CORROSION RIGHT SIDE CENTER AT STATION 600. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 1999040200345 19990402 00345 NM 1999 4 2 QXEA9900512 1 19990225 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 607 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - DENT AND GOUGE ON FUSELAGE EXTERIOR AT STA 607 AND BELOW STRINGER 21. REPAIRED IAW RD 8-53-4026, DHC-8 SRM 51-20- 16 AND 51-20-36. 2 H 7 2 4T RT A13NM 1999040200346 19990402 00346 NM 1999 4 2 QXEA9900513 1 19990223 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 201-222 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - TWO DENTS ABOVE STRINGER 29, RIGHT-HAND SIDE BELOW LAVATORY SERVICE PANEL AT STA 201 TO 222. REPAIRED IAW DHC-8 R D 8-53-4086, SRM 51-40-00 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999040200347 19990402 00347 NM 1999 4 2 QXEA9900514 1 19990217 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 312.5-333 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - THREE DENTS BEYOND LIMITS FROM STATION 312.5 TO 333.3, ABOVE AND BELOW STRINGER 10, UNDER ICE SHIELD. REPAIRED IA W DHC-8 RD 8-53-403, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999040200348 19990402 00348 NM 1999 4 2 QXEA9900515 1 19990219 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 312-333 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - FOUR DENTS IN FUSELAGE SKIN AT STATION 312 TO 333 BELOW STRINGER 23 ON LEFT-HAND SIDE. REPAIRED IAW DHC-8 RD8-53- 4038 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999040200349 19990402 00349 NM 1999 4 2 QXEA9900516 1 19990223 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 270.5-291.4 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - DENT BETWEEN FRAMES 270.5 AND 291.4 AT LEFT-HAND SIDE OF STRINGERS 3 AND 4. REPAIRED IAW DHC-8 RD 8-53-4046. 2 H 7 2 4T RT A13NM 1999040200350 19990402 00350 NM 1999 4 2 QXEA9900517 1 19990223 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 580.5 & 600 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - DENT DAMAGE BETWEEN STRINGER 19S AND 20S AT FUSELAGE STATION 580.50 AND 600. REPAIRED IAW DHC-8 RD 8-53-4052. 2 H 7 2 4T RT A13NM 1999040200351 19990402 00351 NM 1999 4 2 QXEA9900518 1 19990219 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM RIGHT CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - RIGHT-HAND OUTBOARD SEAT TRACK HAS MINOR CORROSION. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-20-30. 2 H 7 2 4T RT A13NM 1999040200352 19990402 00352 NM 1999 4 2 QXEA9900519 1 19990219 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM RIGHT CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - MINOR CORROSION FOUND ON RIGHT-HAND INBOARD SEAT TRACK. REPAIRED IAW DHC-8 RD 53-1339, STEP 1, SRM 51-20-16 AND S RM 51-20-36. 2 H 7 2 4T RT A13NM 1999040200353 19990402 00353 NM 1999 4 2 QXEA9900520 1 19990219 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM LEFT CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION. REPAIRED IAW DHC-8 RD 53-1339, STEP 1, SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999040200354 19990402 00354 NM 1999 4 2 QXEA9900521 1 19990225 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 487.5-521 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - DENT ON FUSELAGE SKIN AT X487.5 TO S521 AND STRINGERS 21S AND 22S. REPAIRED IAW HORIZON AIR EA 9-53-939 AND DHC-8 RD 8-53-4082. 2 H 7 2 4T RT A13NM 1999040200355 19990402 00355 NM 1999 4 2 QXEA9900522 1 19990217 A 5320 SILL DHAV DHC8 DHC8102 2809003 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - GOUGING DAMAGE TO RIGHT-HAND SIDE WINDOW SILL AT BOTTOM FORWARD CORNER. REPAIRED IAW DHC-8 SRM 51-20-16, 51-20-36 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999040200356 19990402 00356 NM 1999 4 2 QXEA9900523 1 19990301 A 5540 HINGE DHAV DHC8 DHC8102 2809003 NM RUDDER CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - TRAILING RUDDER BOTTOM HINGE HAS PITTING DAMAGE TO FITTING BEARING RETAINING SURFACES. REPAIRED IAW HORIZON AIR E A 9-27-100, DHC-8 SRM 51-20-36, 51-40-00, PAGE 1, PARAGRAPH 2 AND PAGE 2, TABLE 1. 2 H 7 2 4T RT A13NM 1999040200357 19990402 00357 NM 1999 4 2 QXEA9900524 1 19990218 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - NR 2 NACELLE INBOARD AND OUTBOARD AT STA 130.60, RIVETS ARE PULLED THROUGH SKIN. REPAIRED IAW DHC-8 RD 8-54-953. 2 H 7 2 4T RT A13NM 1999040200358 19990402 00358 NM 1999 4 2 QXEA9900525 1 19990208 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - NR 2 NACELLE OUTBOARD SKIN AT STA 179.10 HAS RIVETS PULLED THROUGH STRAP. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20- 16 AND RD 8-54-215. 2 H 7 2 4T RT A13NM 1999040200359 19990402 00359 NM 1999 4 2 QXEA9900526 1 19990222 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - NR 1 NACELLE AFT FINGERNAIL DECK SKIN CHAFED AT STA 236. REPAIRED IAW DHC-8 RD 8-54-376, 8-54-1032 AND DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999040200360 19990402 00360 NM 1999 4 2 QXEA9900527 1 19990218 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - NR 1 NACELLE INBOARD AND OUTBOARD SIDE RIVETS PULLED THROUGH SKIN AT STA 134.55 AND ZN15. REPAIRED IAW CONAIR EO 2224, HORIZON AIR EA 9-54-188 AND DHC-8 RD 8-54-953. 2 H 7 2 4T RT A13NM 1999040200361 19990402 00361 NM 1999 4 2 QXEA9900528 1 19990215 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM WS 171.4-490 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - RIGHT-HAND WING UPPER AND LOWER SPAR CAP FLANGE, OUTBOARD OF NACELLE FROM STATION YW171.400 TO YW490 HAS MANY GOUG ES. REPAIRED IAW DHC-8 RD 8-57-1119 AND SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 1999040200362 19990402 00362 NM 1999 4 2 QXEA9900529 1 19990215 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM WS 5700 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - LEFT-HAND WING FORWARD SPAR AT YW5700 LOWER SPAR CAP FLANGE HAS FRETTING CORROSION AND BARE ALUMINUM AROUND ANCHOR NUTS. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999040200363 19990402 00363 NM 1999 4 2 QXEA9900530 1 19990218 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM WS 97 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - LEFT-HAND WING FORWARD SPAR CAP FLANGE SCRATCHED IN RADIUS AT STATION YW97.00. REPAIRED IAW DHC-8 SRM 51-20-16 AN D 51-20-36. 2 H 7 2 4T RT A13NM 1999040200364 19990402 00364 NM 1999 4 2 QXEA9900531 1 19990222 A 5720 TIP DHAV DHC8 DHC8102 2809003 NM RIGHT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - RIGHT-HAND WING TIP UPPER ANCHOR NUT LAND CRACKED. REPAIRED IAW DHC-8 RD 8-57-1331, CONAIR EO 2223 AND HORIZON AI R EA 9-57-403. 2 H 7 2 4T RT A13NM 1999040200366 19990402 00366 NM 1999 4 2 QXEA9900533 1 19990220 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM WS 288 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - RIGHT-HAND WING FUEL BAY INTERNAL STATION YW288 LOWER SPAR FLANGE HAS 2 SCRATCHES. REPAIRED IAW DHC-8 SRM 51-20-1 1 AND SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999040200367 19990402 00367 NM 1999 4 2 QXEA9900534 1 19990227 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - NR 1 NACELLE OUTBOARD LOWER CORNER AT FORWARD GEAR DOOR CUTOUT OUTER SKIN DAMAGED. REPAIRED IAW DHC-8 RD 8-54-104 3. 2 H 7 2 4T RT A13NM 1999040200368 19990402 00368 NM 1999 4 2 QXEA9900535 1 19990216 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - LEFT-HAND WING UPPER SURFACE LADDER PLATE CORROSION AND LADDER PLATE O-RING GROOVE CORROSION. REPAIRED IAW DHC-8 RD 8-57-1252, 8-57-984 AND DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999040200369 19990402 00369 NM 1999 4 2 QXEA9900536 1 19990216 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WS 171.2-261 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - LEFT-HAND WING UPPER SURFACE LADDER PLATE CORROSION AT STATION YW171.2 TO YW261.0. REPAIRED IAW DHC-8 RD 8-57-611 AND DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999040200370 19990402 00370 NM 1999 4 2 QXEA9900537 1 19990216 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WS 261-333 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - LEFT-HAND WING UPPER SURFACE LADDER PLATE CORROSION AND LADDER PLATE O-RING GROOVE CORROSION AT STATION YW261.0 TO YW333.0. REPAIRED IAW DHC 8 SRM 51-20-16 AND DHC-8 RD 8-57-633. 2 H 7 2 4T RT A13NM 1999040200371 19990402 00371 NM 1999 4 2 QXEA9900538 1 19990216 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WS 171.2-261 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - RIGHT-HAND WING UPPER SURFACE LADDER PLATE CORROSION AND O-RING GROOVE CORROSION AT STATION YW171.2 TO YW261.0. R EPAIRED IAW DHC-8 RD 8-57-1252 AND DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999040200372 19990402 00372 NM 1999 4 2 QXEA9900539 1 19990216 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WS 261-333 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - RIGHT-HAND WING UPPER SURFACE LADDER PLATE CORROSION AND LADDER PLATE O-RING GROOVE CORROSION AND SCRATCHES AT STA TION YW261.0 TO YW333.0. REPAIRED IAW DHC 8 RD 8-57-633, 8-57-1252 AND DHC 8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999040200373 19990402 00373 NM 1999 4 2 QXEA9900540 1 19990216 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WS 333-405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - RIGHT-HAND WING UPPER SURFACE LADDER PLATE CORROSION AND LADDER PLATE O-RING GROOVE CORROSION AT STATION YW333.0 T O YW405.0. REPAIRED IAW DHC 8 RD 8-57-1252 AND DHC 9 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999040200374 19990402 00374 NM 1999 4 2 QXEA9900541 1 19990225 A 5230 WEB DHAV DHC8 DHC8102 2809003 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - GOUGES ON WEB BESIDE BAGGAGE DOOR FITTINGS. REPAIRED IAW DHC 8 SRM 51-20-16, 51-20-36, CONAIR EO 2214, HORIZON AI R EA 9-53-425 AND DHC 8 RD 8-53-4033. 2 H 7 2 4T RT A13NM 1999040200375 19990402 00375 WP 1999 4 2 ABXA9900250 1 19990305 A 5311 59218871 FRAME DOUG DOUG DC9 DC933F 302207A WP BS 351 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FUSELAGE FRAME CORRODED AT STATION 351 FROM LONGERONS 29 LEFT TO 29 RIGHT. REPAIRED FRAME IAW DC 9 SRM 53-03-00. 2 L 7 2 4F A6WE 1999040200376 19990402 00376 WP 1999 4 2 ABXA9900251 1 19990305 A 5530 591218835 ANGLE DOUG DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND CRACKED ATTACH ANGLE AT VERTICAL STABILIZER WRAP AROUND PANEL. REPLACED ANGLE IAW DC9 SRM 51-30-5 . 2 L 7 2 4F A6WE 1999040200377 19990402 00377 WP 1999 4 2 ABXA9900252 1 19990305 A 5311 9923411502 FRAME DOUG DOUG DC9 DC933F 302207A WP BS 639 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT STATION 639 AND RBL 54. REPAIRED FUSELAGE FRAME IAW ABX REA D953-26902. 2 L 7 2 4F A6WE 1999040200378 19990402 00378 WP 1999 4 2 ABXA9900253 1 19990305 A 5412 39262451 BULKHEAD DOUG DOUG DC9 DC933F 302207A WP LEFT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND LEFT PYLON SUPPORT BULKHEAD CRACKED AT STATION 965 LOWER ATTACH ANGLE. REPLACED LEFT PYLON SUPPOR T BULKHEAD LOWER ATTACH ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999040200379 19990402 00379 WP 1999 4 2 ABXA9900254 1 19990305 A 5320 49262221 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND RIGHT PYLON BULKHEAD AFT MOUNT FOOT CRACKED AT STATION 965, RBL 44. REPLACED RIGHT PYLON SUPPORT BULKHEAD BOTTOM FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999040200380 19990402 00380 WP 1999 4 2 ABXA9900255 1 19990329 A 5343 991966017 FITTING DOUG DOUG DC9 DC932 3022066 WP LEFT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 LEFT AUX GEAR FITTING CRACKED. REPLACED LEFT AUX GEAR FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999040200381 19990402 00381 WP 1999 4 2 ABXA9900256 1 19990329 A 5320 99577121 INTERCOSTAL DOUG DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 INTERCOSTAL CRACKED AT STATION 1076 AND LONGERON 28 RIGHT. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999040200382 19990402 00382 WP 1999 4 2 ABXA9900257 1 19990329 A 5343 991966018 FITTING DOUG DOUG DC9 DC932 3022066 WP RIGHT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 RIGHT AUX GEAR FITTING CRACKED. REPLACED RIGHT AUX GEAR FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999040200383 19990402 00383 WP 1999 4 2 ABXA9900258 1 19990329 A 5311 991224699 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 1039 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 STATION 1039 CORRODED AFT OF APU ENCLOSURE AT RBL 18. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999040200384 19990402 00384 WP 1999 4 2 MWEA99122 1 19990326 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP CABIN DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 THE GALLEY DOOR ESCAPE SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1999040200385 19990402 00385 WP 1999 4 2 MWEA99123 1 19990326 A 5220 39145061 FITTING DOUG DC9 DC914 3022034 WP EMER EXIT DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 THE AFT PLUG DOOR LOWER FITTING IS CRACKED. MTC REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 1999040200386 19990402 00386 NM 1999 4 2 P5CA9900525 1 19990326 A 5720 FAIRING BOEING 747 747122 1384872 NM RIGHT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 RIGHT WING AFT SIDE FAIRING AT BL1120 FOUND DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200387 19990402 00387 NM 1999 4 2 P5CA9900526 1 19990326 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 5 TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 5 TRAILING EDGE FLAP FAIRING FOUND HOLE AT BL235. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200388 19990402 00388 NM 1999 4 2 P5CA9900527 1 19990326 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 6 TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 6 TRAILING EDGE FLAP FAIRING FOUND HOLE. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200389 19990402 00389 NM 1999 4 2 P5CA9900528 1 19990326 A 5730 PANEL BOEING 747 747122 1384872 NM LEFT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 TRAILING EDGE WING UPPER SKIN PANEL FOUND DELAMINATED ON LEFT WING. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200390 19990402 00390 NM 1999 4 2 P5CA9900529 1 19990326 A 5245 SKIN BOEING 747 747122 1384872 NM AIR COND DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 AIR CONDITIONING BAY DOOR 191E ON LEFT SIDE FOUND DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200391 19990402 00391 NM 1999 4 2 P5CA9900530 1 19990326 A 5755 SKIN BOEING 747 747122 1384872 NM NR 5 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 5 SPOILER SKIN DELAMINATED. REPAIRED PER SRM 51-40-05. 2 L 7 4 4F A20WE 1999040200392 19990402 00392 NM 1999 4 2 P5CA9900531 1 19990326 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 6 TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 6 TRAILING EDGE FLAP FAIRING DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200393 19990402 00393 NM 1999 4 2 P5CA9900532 1 19990326 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 8 TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 8 TRAILING EDGE FLAP FAIRING FOUND DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200394 19990402 00394 NM 1999 4 2 P5CA9900533 1 19990326 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LEVEL 1 CORROSION FOUND ON EXTERIOR SKIN AT BS 1580 STR 47 LEFT TO RIGHT. REPAIRED CORROSION PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999040200395 19990402 00395 NM 1999 4 2 P5CA9900534 1 19990326 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LEVEL 1 CORROSION FOUND ON FUSELAGE EXTERIOR SKIN AT BS 15620 STR 47 LEFT TO RIGHT. CORROSION REMOVED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999040200396 19990402 00396 NM 1999 4 2 P5CA9900535 1 19990326 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LEVEL 1 CORROSION FOUND ON EXTERION SKIN LOCATED AT BS 1960 RIGHT STRING 46. CORROSION REMOVED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999040200397 19990402 00397 NM 1999 4 2 P5CA9900536 1 19990326 A 5730 PANEL BOEING 747 747122 1384872 NM WS 340 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND DELAMINATED PANEL ON UPPER RIGHT WING AT WS 340. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200398 19990402 00398 NM 1999 4 2 P5CA9900537 1 19990326 A 5720 FAIRING BOEING 747 747122 1384872 NM RIGHT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND DELAMINATED CRACK ON RT WING AFT SIDE FAIRING AT BL 1120. REPAIRED CORROSION PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999040200399 19990402 00399 NM 1999 4 2 P5CA9900538 1 19990329 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1520 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND ANGLE SUPPORT FITTING AT BS 1520 BL ZERO CRACKED. REPLACED ANGLE PER SRM 51-10-02 AND 51-30-02. 2 L 7 4 4F A20WE 1999040200400 19990402 00400 NM 1999 4 2 P5CA9900539 1 19990329 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2685 LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND FUSELAGE EXTERIOR SKIN AT BS 2685 LEFT ELEVATOR AREA LOOSE RIVETS. REPLACED RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999040200401 19990402 00401 NM 1999 4 2 P5CA9900540 1 19990329 A 5210 HINGE BOEING 747 747122 1384872 NM PASSENGER DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LEVEL 1 CORROSION FOUND ON HINGE AT NR 3 MAIN ENTRY DOOR. REMOVED CORROSION PER SRM 51-10-02. 2 L 7 4 4F A20WE 1999040200402 19990402 00402 NM 1999 4 2 SWAA990561 1 19990325 A 2612 65509001 FIRE WARNING BOEING 737 7372H4 138448C NM APU MALFUNCTIONED A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SW 07 103SW 23109 APU FIRE WARNING BELL AND LIGHT ILLUMINATED DURING FLIGHT. PULLED FIRE HANDLE AND DISCHARGED APU FIRE BOTTLE. INSPECTE D APU AND TAILPIPE, NO EVIDENCE OF FIRE FOUND. OK TO CONTINUE PER MEL. REMOVED AND REPLACED FIRE BOTTLE DURING OVERNIG HT CHECK PER MM. 2 L 7 2 4F A16WE 1999040200403 19990402 00403 NM 1999 4 2 SWAA990562 1 19990324 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 3 & 23 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 315SW 23337 EMERGENCY EXIT FLOOR LIGHTS INOP AT ROWS 3 AND 23. REMOVED AND REPLACED LIGHT BULBS PER MM. 2 L 7 2 4F RT A16WE 1999040200404 19990402 00404 NM 1999 4 2 SWAA990563 1 19990324 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 885 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C4 CHECK, FOUND A 2.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 885, STR 24R, (CONFIRMED WITH EDDY CURRENT I NSPECTION). REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999040200405 19990402 00405 NM 1999 4 2 SWAA990564 1 19990324 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED A2 CHECK, FOUND A 4 INCH LONG CRACK AT APPROX BS 500D STR 11R. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040200406 19990402 00406 NM 1999 4 2 SWAA990565 1 19990324 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND THRU ULTRASONIC INSPECTION, BULKHEAD CRACKED AT BS 178, LBL 7, WL 212. REPAIRED PER SRM . 2 L 7 2 4F RT A16WE 1999040200407 19990402 00407 NM 1999 4 2 SWAA990566 1 19990324 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED 1/4D CHECK, FOUND THRU ULTRASONIC INSPECTION, 4 CRACKS AT BULKHEAD, BS 178, BETWEEN LBL 7 AND RBL 11 WL 198 TO 218. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040200408 19990402 00408 NM 1999 4 2 SWAA990567 1 19990324 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 8, 18 & 20 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOP AT ROWS 8, 18 AND 20. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999040200409 19990402 00409 NM 1999 4 2 SWAA990568 1 19990325 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND THRU ULTRASONIC INSPECTION 2 CRACKS AT BS 178 BULKHEAD, LBL 5-RBL 5. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040200410 19990402 00410 NM 1999 4 2 SWAA990569 1 19990325 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967 WITH AN OBLONG HOLE THRU UPPER CHORD, RBL 51.5, WL 208. REPAIRED BE AM PER SRM. 2 L 7 2 4F RT A16WE 1999040200411 19990402 00411 NM 1999 4 2 SWAA990553 1 19990323 A 2170 1808494 COALESCER BAG BOEING 737 7373H4 1384600 NM AC BAY OIL SOAKED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 378SW 26585 AIR TURNBACK DUE TO OIL SMELL AND HAZE BUILD UP IN AFT CABIN AFTER TAKEOFF. GASPER AND RECIRCULATING FAN TURNED OFF, HA ZE DISAPPEARED AFTER LANDING. REMOVED AND REPLACED RT WATER SEPARATOR COALESCER BAG, SERVICED RT AIR CYCLE MACHINE TO P ROPER LEVEL PER MM. 2 L 7 2 4F RT A16WE 1999040200412 19990402 00412 NM 1999 4 2 SWAA990554 1 19990321 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 1 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND NR 1 LE SLAT LOWER TRAILING EDGE CRACKED JUST I/B OF ACTUATOR. REPAIRED PER SWA RA 1-3 57-0658. 2 L 7 2 4F RT A16WE 1999040200413 19990402 00413 NM 1999 4 2 SWAA990555 1 19990322 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 815 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING WALKAROUND INSPECTION, FOUND APPROX A 2.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 815 STRINGERS 14-15L. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 1999040200414 19990402 00414 NM 1999 4 2 SWAA990556 1 19990322 A 3350 CA72720CR BATTERY BOEING 737 7372H4 138448C NM E & E COMP DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED AIRCRAFT BATTERY PER MM. 2 L 7 2 4F A16WE 1999040200415 19990402 00415 NM 1999 4 2 SWAA990557 1 19990322 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION A CRACK ON BEADED WEB AT BS 665, RBL 42 AT CABIN FLOOR. REPAIRED WEB PER SWA RA NR 1-353-2034. 2 L 7 2 4F RT A16WE 1999040200416 19990402 00416 NM 1999 4 2 SWAA990558 1 19990323 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 545.9 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND INTERGRANULAR CORROSION ON KEEL BEAM, RT O/B SIDE BS 545.9. REPAIRED BEAM PER SWA RA NR 1-353-2044. 2 L 7 2 4F RT A16WE 1999040200417 19990402 00417 NM 1999 4 2 SWAA990559 1 19990323 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 272-274 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND A 2 INCH LONG CRACK ON FUSELAGE OUTER SKIN, BS 272 TO 274 STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999040200418 19990402 00418 NM 1999 4 2 SWAA990560 1 19990322 A 3350 079123 LENS BOEING 737 7373H4 1384600 NM ROW 3ABC MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED C4 CHECK, FOUND FLOOR EMERGENCY LIGHT MISSING LENS AT ROW 3 ABC. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999040200419 19990402 00419 NM 1999 4 2 SWAA990570 1 19990326 A 2560 65C36533 SLIDE BOEING 737 7373Y0 1384671 NM L 1 DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 FWD ENTRY DOOR EVACUATION SLIDE OUT OF CASE. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999040200420 19990402 00420 NM 1999 4 2 SWAA990571 1 19990326 A 3350 6104791 POWER SUPPLY BOEING 737 7372H4 138448C NM RT EMER EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY ESCAPE LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY ASSY PER MM. 2 L 7 2 4F A16WE 1999040200421 19990402 00421 NM 1999 4 2 SWAA990572 1 19990326 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND THRU EDDY CURRENT INSPECTION .125 INCH LONG CRACK AT STRINGER 4R, BS 500D. REPAIR ED PER SRM. 2 L 7 2 4F A16WE 1999040200422 19990402 00422 NM 1999 4 2 SWAA990573 1 19990326 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, CORROSION AT KEEL BEAM RT SIDE BS 500D TO 515. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999040200423 19990402 00423 NM 1999 4 2 SWAA990574 1 19990326 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 665 RBL 40 AT WHEEL WELL. REPAIRED PER SWA RA NR 1-353-2048 . 2 L 7 2 4F RT A16WE 1999040200424 19990402 00424 NM 1999 4 2 SWAA990575 1 19990326 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION TWO, 2.5 INCH LONG CRACKS AT FUSE SKIN BS 500C TO 500D S TRINGER 10R. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040200425 19990402 00425 NM 1999 4 2 SWAA990576 1 19990326 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON NUT PLATE HOLES AT FLOORBEAM BS 312, LBL 20 - LBL 45. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040200426 19990402 00426 NM 1999 4 2 SWAA990577 1 19990326 A 5311 6551261 FRAME BOEING 737 7373H4 1384600 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND STUB FRAME CRACKED AT BS 295 RBL 54.5 WL 209. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999040200427 19990402 00427 NM 1999 4 2 SWAA990578 1 19990326 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND STRINGER 4L CRACKED AT TWO FASTENER HOLES BS 907. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040200428 19990402 00428 NM 1999 4 2 SWAA990579 1 19990327 A 5312 6516300 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND THRU ULTRASONIC INSPECTION 2 CRACKS AT BULKHEAD WEB BS 178 LBL 5 AND RBL 5. REPAIRED PE R SRM. 2 L 7 2 4F RT A16WE 1999040200429 19990402 00429 NM 1999 4 2 SWAA990580 1 19990327 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND 3 STRINGER CLIPS CRACKED AT BS 927 STRINGERS 27R, 26R AND 27L. REMOVED AND REPLACED CLI PS PER SRM. 2 L 7 2 4F RT A16WE 1999040200430 19990402 00430 NM 1999 4 2 SWAA990581 1 19990327 A 5320 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND 4 FRAMES CRACKED AT BS 400, 440, 500C, 500A BETWEEN STRINGERS 8R-9R. REPAIRED PER SRM A ND ER 99-0283. 2 L 7 2 4F RT A16WE 1999040200431 19990402 00431 NM 1999 4 2 SWAA990582 1 19990326 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 9, 13 & 24 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED C1 CHECK, FOUND FLOOR EMERGENCY TRACK LIGHT NOT SECURED AT ROWS 13, 9 AND 24. SECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999040200432 19990402 00432 NM 1999 4 2 SWAA990583 1 19990326 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LT LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED C1 CHECK, FOUND LT WING LEADING EDGE NR 2 SLAT LOWER SKIN AT TRAILING EDGE HAS SMALL CRACKS AT RIVET HO LES. REPAIRED SLAT PER SWA RA NR 1-357-0660. 2 L 7 2 4F RT A16WE 1999040200433 19990402 00433 NM 1999 4 2 SWAA990584 1 19990326 A 3350 100885 BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EMERGENCY EVACUATION FLOOR TRACK LIGHTING INOP. REMOVED AND REPLAC ED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999040200434 19990402 00434 NM 1999 4 2 SWAA990586 1 19990327 A 5754 6546430100 SKIN BOEING 737 7373H4 1384600 NM RT TE FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED AT 3 PLACES JUST INBOARD OF OUTBOARD END. REMOVED AND REPLACED FOREFLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040200435 19990402 00435 NM 1999 4 2 SWAA990587 1 19990327 A 5720 65C25286 BEAM BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SERVICE CHECK, WALKAROUND INSPECTION FOUND THE LEFT WING LOWER TRAILING EDGE BEAM CRACKED. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999040200436 19990402 00436 NM 1999 4 2 SWAA990588 1 19990327 A 5230 BAC1505 TEE BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND LOWER T-CHORD CRACKED THIRD FROM AFT END, FWD CARGO DOOR. REMOVED DOOR, REPAIRED AND REINSTALLED DOOR PER SRM AND MM. 2 L 7 2 4F RT A16WE 1999040200515 19990402 00515 NM 1999 4 2 99ZZZX1310 1 19990211 A 5754 ANGLE BOEING 727 727281 138408N NM NR 6 SLAT CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 906PG 20728 DURING A C-CHECK, CORROSION NOTED ON NR 6 LEADING EDGE SLAT INBOARD SLAT TRACK LOWER ATTACH ANGLE. 2 L 7 3 4F A3WE 1999040200537 19990402 00537 EU 1999 4 2 99ZZZX1332 1 19990102 A 6410 704A33633171 HINGE SNIAS 350 AS350D 8680803 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 779LF 369 1621 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999040200545 19990402 00545 NE 1999 4 2 R7MA0000579 2 19990130 A 7260 9560115450 MAGNETIC SEAL AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1 60030 NE NR 2 ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 109RX 10016 16020 STARTER SEAL LEAKING ON NR 2 ENGINE. (X) 1 G 7 2 3U 3 U RT H7EU E19EU 1999040200548 19990402 00548 NM 1999 4 2 TWAA9904801 1 19990329 A 3397 S417N5095 WIRE BOEING 767 7673Q8 NM ROW 30-41 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 FOUND EGRESS LIGHTS INOPERATIVE LT SIDE OF CABIN ROWS 30 TO 41 AND RT SIDE OF CABIN AT ROW 5. OUTSIDE EMERGENCY LIGHTS WERE INOPERATIVE ON LT SIDE FWD AND AFT OF THE MOST REAR CABIN DOOR AND ON RT SIDE OF AIRCRAFT AFT OF THE FLAPS. RECONN ECTED JUMPER WIRE AT ROW 30 AND REPLACED LIGHT ASSEMBLY AT ROW 5 FOR THE EGRESS LIGHTS. CLEANED SOCKETS FOR EACH OF THE 3 EXTERIOR EMERGENCY LIGHTS. CHECK-C 1-14-99 LAX. 2 L 7 2 4F RT A1NM 1999040200549 19990402 00549 WP 1999 4 2 TWAA9904802 1 19990329 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 9420D 49824 THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 12-8-98 MCI. 2 L 7 2 4F RT A6WE 1999040200550 19990402 00550 WP 1999 4 2 TWAA9904803 1 19990325 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 273 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 907TW 49165 DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN AROUND THE DRAIN FITTING DAMAGED AT STA 273 BETWEEN LONGERON 29R AND 30. D AMAGE IS .1875 INCH DEEP AND 8 INCHES LONG. CUT OUT DAMAGED SKIN AROUND DRAIN AND REPAIRED PER SRM 53-04 FIG 12B PAGES 35 AND 37. 2 L 7 2 4F A6WE 1999040200551 19990402 00551 WP 1999 4 2 AT9900267 1 19990319 A 5510 FAIRING DOUG DC9 DC932 3022066 WP HORIZONTAL STAB WORN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND UPPER HORIZONTAL FAIRING HAS AN ELONGATED FASTENER HOLE. FA BRICATED REPAIR ON LEFT HAND UPPER HORIZONTAL FAIRING IAW DC9 SRM 51-10-3 AND RES NR 99653. 2 L 7 2 4F A6WE 1999040200552 19990402 00552 WP 1999 4 2 AT9900268 1 19990319 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND POPPED RIVETS AT LOWER CAP OF FLOORBEAM AT BS 965 RBL 19 TO 23 CORRODED. R EMOVED CORROSION, FABRICATED AND INSTALLED REPAIRED ANGLE IAW DC-9 SRM 53-01 AND RES NR 99685. 2 L 7 2 4F A6WE 1999040200553 19990402 00553 WP 1999 4 2 AT9900269 1 19990318 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN L ANGLE ON THE FLOOR SUPPORT AT BS 996 RBL 29 CORRODED. REMOVED CORROS ION, REMOVED AND REPLACED L ANGLE AND INSTALLED IAW DC-9 SRM 51-10-03, 51-30-02, 51-30-05, 51-10-04 AND 53-05 FIG 1. 2 L 7 2 4F A6WE 1999040200554 19990402 00554 NM 1999 4 2 PCAA9900006 1 19990328 A 2611 3023143 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM NR 2 MALFUNCTIONED A PCAA O OTHER N FALSE WARNING CR CRUISE 1 EA 13 EICHP 258 BDL -FLT 3781 BAGGAGE SMOKE WARNING LIGHT CAME ON WITH NO EVIDENCE OF SMOKE OR FIRE DURING CRUISE FLIGHT INTO BDL. MAINT ENANCE INSPECTED, FOUND NO EVIDENCE OF SMOKE OR FIRE, FOUND THE NR 2 BAGGAGE SMOKE DETECTOR AT FAULT. DISBLED IT AND REL EASED AIRCRAFT UNDER MEL PROVISIONS. *S/D* MAINTENANCE REMOVED AND REPLACED THE NR 2 BAGGAGE BAY SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 1999040200555 19990402 00555 WP 1999 4 2 CALA9900334 1 19990327 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 218, LONGERON 30. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED I AW SRM 53-04 FIGURE 44, SHEET 3. 2 L 7 2 4F A6WE 1999040200556 19990402 00556 WP 1999 4 2 CALA9900335 1 19990329 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15069 46584 INSPECTION FOUND A CORRODED ANGLE IN AFT CARGO COMPARTMENT AT STA 1986 BETWEEN LONGERON 51L AND 51R. THE ANGLE WAS REMO VED, A NEW ANGLE WAS INSTALLED WITH HI-LOKS IAW SRM 51-33-01. 2 L 7 3 4F A22WE 1999040200557 19990402 00557 WP 1999 4 2 CALA9900336 1 19990330 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 604 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND A .625 INCH CRACK, RT LOWER FUSELAGE TO WING CENTER SECTION ANGLE AT FS 604. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999040200558 19990402 00558 WP 1999 4 2 CALA9900337 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 1038 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18563 47487 INSPECTION FOUND TWO, .5 INCH CRACKS IN AFT ACCESSORY COMPARTMENT SUPPORT AT STA 1038, RT SIDE. THE CRACKED AREA WAS CU T OUT AND A REPAIR WAS INSTALLED IAW SRM 53-11-4 PAGE 5. 2 L 7 2 4F A6WE 1999040200559 19990402 00559 WP 1999 4 2 CALA9900338 1 19990330 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR FORWARD LOWER DOOR STOP SUPPORT BRACKET. A NEW BRACKET WAS INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1999040200560 19990402 00560 WP 1999 4 2 9901169980 1 19990323 A 3350 FUSE DOUG DC9 DC931 3022065 WP GALLEY DOOR BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTING IN FIRST CLASS AND AT GALLEY DOOR INOPERATIVE. REPLACED BLOWN FUSE IN GALLEY DOOR POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999040200561 19990402 00561 WP 1999 4 2 9901179980 1 19990324 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP RT SERVICE DOOR INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE MAINTENANCE INSPECTION, FOUND ESCAPE PATH EMERGENCY LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED POWER SUP PLY AT RIGHT SERVICE DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999040200562 19990402 00562 WP 1999 4 2 9901181161 1 19990216 A 5315 FLOORBEAM DOUG DC10 DC1040 3023508 WP BS 791 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING M-CHECK, FOUND CRACK ON FLOOR I BEAM AT FS 791, LBL 18 TO RBL 18. REPAIRED PER EA 11-162954. 2 L 7 3 4F A22WE 1999040200563 19990402 00563 WP 1999 4 2 9901191161 1 19990205 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 1099 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING M-CHECK, FOUND CRACK IN FORWARD CARGO FLOOR FRAME AT FS 1099 AT LBL 38. REPAIRED PER EA 11-158134. 2 L 7 3 4F A22WE 1999040200564 19990402 00564 NM 1999 4 2 9901202762 1 19990131 A 5314 KEEL BEAM BOEING 727 7272B7 138407L NM BS 994-998 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 722RW 21201 DURING M-CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF LEFT KEEL BEAM FROM FS 994 TO 998 AT STR 29L. REPAIRED PER EA 27- 162906. 2 L 7 3 4F A3WE 1999040200565 19990402 00565 WP 1999 4 2 9901211156 1 19990114 A 5315 FLOORBEAM DOUG DC10 DC1040 3023508 WP BS 791 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 46765 DURING M-CHECK, FOUND CRACKS ON THE FLOORBEAM UPPER CHORD AT FS 791, LBL 6 TO RBL 2. REPAIRED PER EA 11-162058. 2 L 7 3 4F A22WE 1999040200566 19990402 00566 WP 1999 4 2 9901221156 1 19990103 A 5315 FLOORBEAM DOUG DC10 DC1040 3023508 WP BS 879 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 46765 DURING M-CHECK, FOUND CRACK ON THE FLOORBEAM UPPER CHORD AT FS 879 LBL 7. REPAIRED PER EA 11-162057. 2 L 7 3 4F A22WE 1999040200567 19990402 00567 WP 1999 4 2 9901231156 1 19990112 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1471-1531 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 46765 DURING M-CHECK, FOUND CORROSION ON HORIZONTAL SECTION OF LONGERON 31R AT FS 1471 AND 1491. CRACKS WERE ALSO FOUND ON HO RIZONTAL SECTION OF LONGERON 31R AT FS 1501 AND 1531. REPAIRED PER EA 11-162069. 2 L 7 3 4F A22WE 1999040200568 19990402 00568 WP 1999 4 2 9901241156 1 19990110 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1501-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 46765 DURING M-CHECK, FOUND CORROSION ON LONGERON 30L BETWEEN FS 1501 TO 1521. REPAIRED PER EA 11-162061. 2 L 7 3 4F A22WE 1999040200569 19990402 00569 WP 1999 4 2 9901251156 1 19990113 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1431-1503 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 46765 DURING M-CHECK, FOUND CORROSION ON HORIZONTAL SECTION OF LONGERON 30R AT FS 1450, 1470 AND 1503. ALSO, FOUND TWO INCH C RACK ON HORIZONTAL SECTION OF LONGERON 30R AT FS 1431. REPAIRED PER EA 11-162065. 2 L 7 3 4F A22WE 1999040200570 19990402 00570 WP 1999 4 2 9901261156 1 19990108 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1601 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 46765 DURING M-CHECK, FOUND CORROSION BEYOND SRM LIMITS ON LONGERON 44R AT FS 1601. REPAIRED PER EA 11-162068. 2 L 7 3 4F A22WE 1999040200571 19990402 00571 WP 1999 4 2 9901271156 1 19990110 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1521-1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 156US DURING M-CHECK, FOUND CORROSION ON LONGERON 34R AT FS 1521 AND 1531. REPAIRED PER EA 11-162072. 2 L 7 3 4F A22WE 1999040200572 19990402 00572 WP 1999 4 2 9901281156 1 19990112 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1501-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 156US 46765 DURING M-CHECK, FOUND CORROSION ON LONGERON 32L BETWEEN FS 1501 AND 1521. REPAIRED PER EA 11-162062. 2 L 7 3 4F A22WE 1999040200573 19990402 00573 EA 1999 4 2 COMA9960135 1 19990328 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 778CA 7297 FLAPS FAILED. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999040200574 19990402 00574 EA 1999 4 2 COMA9960136 1 19990329 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTIONED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 969CA 5219 7141 LANDING GEAR DID NOT EXTEND WHEN SELECTED TO DOWN POSITION. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1999040200575 19990402 00575 EA 1999 4 2 COMA9960137 1 19990329 A 2740 9960013 SWITCH CNDAIR CL600 CL6002B19 EA RT CONTROL WHEEL DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 767CA 7285 STABILIZER TRIM CAUTION MESSAGE. REPLACED THE CO-PILOTS PITCH TRIM SWITCH. 2 L 7 2 4F RT A21EA 1999040200576 19990402 00576 EA 1999 4 2 COMA9960138 1 19990329 A 2750 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 710CA 7241 FLAPS FAILED WHEN SELECTED FOR APPROACH. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LEFT HAND BPSU AND WIRING HARNE SS FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1999040200577 19990402 00577 SO 1999 4 2 COMA9910047 1 19990329 A 2750 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS TRIPPED A COMA D RETURN TO BLOCK J WARNING INDICATION UK UNKNOWN 1 SO 01 189CA 120189 FLAP CONTROL FAULT, INBOARD FLAPS WILL NOT OPERATE. RERACKED FLAP CONTROL UNIT, SYSTEM OPERATION NORMAL. 2 L 7 2 4T RT A31SO 1999040200578 19990402 00578 SO 1999 4 2 COMA9910048 1 19990328 A 6120 30005000052 CONDITIONER EMB 120 EMB120RT SO LT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 264CA 13214 120256 AUTOFEATHER WARNING DURING TAKEOFF. REPLACED THE LEFT ENGINE SIGNAL CONDITIONER. 2 L 7 2 4T RT A31SO 1999040200579 19990402 00579 WP 1999 4 2 UPS99829145 1 19990221 A 5320 J0602969 ANGLE DOUG DC8 DC873F 302199F WP BS 1110-1270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:C3, CUSP ANGLE AT FS 1150, RT SIDE IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FS 1110 TO 1270, FABRICATED AND REPLACED CUSP IAW SRM 53-2-5 FIG 15A. 2 L 7 4 4F RT 4A25 1999040200580 19990402 00580 WP 1999 4 2 UPS99829147 1 19990329 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-N/A, DURING EMERG LIGHTS TEST NO LIGHTS CAME ON. REMOVED AND REPLACED BATT PACK, OPS CK GOOD (P/N 57084 58-503) (S/N FLT004) ON, (S/N D95) OFF. 2 L 7 4 4F RT 4A25 1999040200581 19990402 00581 WP 1999 4 2 ABXA9900259 1 19990305 A 5330 99100733 PANEL DOUG DOUG DC9 DC933F 302207A WP BS 89 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND UPPER PRESSURE PANEL CRACKED AT STATION 89, LEFT CUSP. REPAIRED PRESSURE PANEL IAW ABX REA D953-2 7142MR AND DOUGLAS S/B NR 53-187. 2 L 7 2 4F A6WE 1999040200582 19990402 00582 WP 1999 4 2 ABXA9900260 1 19990311 A 5320 991224644 SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 1038 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 1038, ABOVE PYLON FEED THROUGH. REPLACED SHEAR TIE IAW DC9 SRM 51-30 -1 AND 51-30-2. 2 L 7 2 4F A6WE 1999040200583 19990402 00583 WP 1999 4 2 ABXA9900261 1 19990311 A 5315 9922393501 FLOORBEAM DOUG DOUG DC9 DC933F 302207A WP BS 370 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FLOORBEAM CORRODED AT STATION 370 AND BL 0 TO LBL 17. REPAIRED FLOORBEAM IAW ABX REA D953-27043. 2 L 7 2 4F A6WE 1999040200584 19990402 00584 WP 1999 4 2 ABXA9900262 1 19990322 A 5320 99100733 PANEL DOUG DOUG DC9 DC933F 302207A WP BS 89 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND UPPER PRESSURE PANEL CRACKED AT NOSE WHEEL WELL TUNNEL, STATION 89 LEFT CUSP. REPAIRED IAW ABX RE A D953-27142. 2 L 7 2 4F A6WE 1999040200585 19990402 00585 WP 1999 4 2 ABXA9900263 1 19990322 A 5753 5910041503 VANE DOUG DOUG DC9 DC933F 302207A WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND LEFT INBOARD FIXED VANE DELAMINATED. REPLACED LEFT INBOARD FIXED VANE IAW DC9 MM 27-51-3. 2 L 7 2 4F A6WE 1999040200586 19990402 00586 WP 1999 4 2 SCNA99054 1 19990325 A 3510 DOOR DOUG DC10 DC1015 3022118 WP L1 POSITION OUT OF ADJUST A SCNA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING A SCHEDULED MAINTENANCE CHECK, THE O2 MASK DOOR FAILED TO OPEN AT THE FLIGHT ATTEDNANT L1 POSITION. FOUND THE DO OR BINDING IN OPENING. ADJUSTED DOOR AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1999040200587 19990402 00587 WP 1999 4 2 SCNA99055 1 19990326 A 3530 5500CIABF23A OXYGEN BOTTLE DOUG DC10 DC1015 3022118 WP CABIN FAILED A SCNA K NONE O OTHER NR NOT REPORTED 1 GL 15 152SY 2079 48289 DURING FLIGHT, A PASSENGER PORTABLE OXYGEN BOTTLE FAILED. REMOVED AND REPLACED THE PORTABLE OXYGEN CYLINDER. 2 L 7 3 4F A22WE 1999040200588 19990402 00588 WP 1999 4 2 SCNA99056 1 19990326 A 3350 EMBS1392 BATTERY PACK EMBS1392 DOUG DC10 DC1015 3022118 WP CABIN DISCHARGED A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 152SY 2936 60940 48289 DURING A LINE MAINTENANCE CHECK, THE FORWARD AND MID CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. RE MOVED AND R EPLACED THE FORWARD AND MID CEILING LIGHT BATTERY PACKS. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A22WE 1999040200589 19990402 00589 WP 1999 4 2 SCNA99057 1 19990328 A 2560 COVER DOUG DC10 DC1015 3022118 WP L1 DOOR SLIDE OUT OF POSITION A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A LINE MAINTENANCE CHECK, THE L1 DOOR WOULD NOT RELEASE FROM THE DOOR OPENING. FOUND THE LOWER ESCAPE SLIDE COVE R JAMMED INTO DOOR FRAME WITH ENOUGH PRESSURE TO LOCK THE DOOR INTO THE FRAME. OBSTRUCTING DOOR SLIDE COVER REMOVED FRO M DOOR FRAME AND DOOR OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A22WE 1999040200590 19990402 00590 SO 1999 4 2 SWIA971439 1 19990302 A 5230 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR MISSING A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 566SW 120341 AT FLIGHT 240 EXPERIENCED RAPID DEPRESSURIZATION. RETURNED TO SFO. DISCOVERED PART OF CARGO DOOR SEAL MISSING. REPAIR ED CARGO DOOR SEAL BOTTOM. CHECKED PRESSURE SYSTEM ON GROUND, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999040200591 19990402 00591 1999 4 2 SWIA971440 3 19990304 A 6140 NP INDICATION EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT ENGINE OSCILLATION A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 1105G 120105 AFTER DEPARTURE AND ON CLIMBOUT NP OSCILLATES BETWEEN 99.2 PERCENT AND 1001 PERCENT. WHEN 85 PERCENT NP WAS SET, OSCI LLATIONS WERE +.4 PERCENT. RIGHT ENGINE NP FLUCTUATIONS ARE STILL WITHIN ACCEPTABLE LIMITS AT THIS TIME PER EMBRAER O PERATIONAL BULLETIN 120-003/92. (NP FLUXUATIONS OF +/- 1 PERCENT ARE ACCEPTABLE.) OPERATIONAL TEST FLIGHT CONFIRMS NP FLUCTUATIONS WITHIN LIMITS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999040200592 19990402 00592 SO 1999 4 2 SWIA971441 1 19990304 A 3010 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING DEICE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 221SW 120290 RIGHT INBOARD WING LEADING EDGE BOOT WENT INOP 15 MINUTES AFTER DEPARTURE FROM SFO. RETURNED TO SFO. REPLACED RIGHT IN BOARD WING DEICE BOOT PRESSURE SWITCH, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999040200593 19990402 00593 SO 1999 4 2 SWIA971442 1 19990304 A 3260 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT MLG MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 223SW 120291 DEPARTED LAS, LEFT MAIN SYSTEM A GREEN LIGHT REMAINED ILLUMINATED. FOLLOWED QRH PROCEDURE, CYCLED GEAR HANDLE. GEAR WO ULD NOT CYCLE DOWN. AFTER LEVEL OFF, LIGHT EXTINGUISHED. CONTINUED TO FAT. USED EMERGENCY GEAR EXTENSION PROCEDURES A ND GEAR EXTENDED. REPLACED LEFT GEAR SYSTEM A GREEN PROX HARNESS AND SWITCH IAW EMB 120 MM 32-61-01, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999040200594 19990402 00594 SO 1999 4 2 SWIA971443 1 19990304 A 3010 TIMER EMB 120 EMB120RT SO PWA 118 PW118A NE LEFT WING DEICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 271YV 120271 MIDDLE LEFT WING LEADING EDGE DEICE BOOT INOP BOTH TIMERS. RETURNED TO PDX. RAN ENGINES AND OPS CHECKS GOOD ON GROUND. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T 4 T RT A31SO E20NE 1999040200595 19990402 00595 SO 1999 4 2 SWIA971444 1 19990305 A 3080 D55201001 MONITOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WING DEICE FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 579SW 120347 ALL LEADING EDGE DEICING BOOTS FAIL (17,000 AUTO/NORM) INCLUDING ENGINE AIR INLET FAILURE (BOTH INLET BOOTS). DIVERTED TO PSP FROM LAX. REPLACED DEICE MONITOR. CYCLED ALL DEICE BOOTS SEVERAL TIMES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999040200596 19990402 00596 NM 1999 4 2 NOCA0299 1 19990221 A 3350 P4010021 LIGHT BOEING 757 75723A 1384967 NM L1 DOOR INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 757NA 24567 JFK - FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR FOUND INOPERATIVE DURING INSPECTION. REPLACED FLIGHT ATTENDANT E MERGENCY FLASHLIGHT AT L1 DOOR. OPS CHECKED OK. (M) 2 L 7 2 4F RT A2NM 1999040200597 19990402 00597 EU 1999 4 2 AALA990113 1 19990125 A 5320 TIE DOWN AIRBUS 300 A300B4605R 3930308 EU BS 52 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7083A 645 TUL - FOUND CORROSION IN LAV TIE DOWN AT X STATION 52 INCHES LEFT SIDE AT FRAME 73. REMOVED LAV TIE DOWN AND REPLACED W ITH NEW TIE DOWN ASSY PER 51-72-10 SRM. (M) 2 L 7 2 4F RT A35EU 1999040200598 19990402 00598 EU 1999 4 2 AALA990087 1 19990114 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7083A 645 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAMES 72 AND 73, X STATION 17.5 RIGHT. FABRICATED AND INSTALLED ST RAP REPAIR PER AARD 57-20-00-2 AFTER CORROSION REMOVAL PER 51-74-10-2. (M) 2 L 7 2 4F RT A35EU 1999040200599 19990402 00599 EU 1999 4 2 AALA990086 1 19990120 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 28 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7083A 645 TUL - FOUND SEAT TRACK NR 10 FORWARD OF R-2 DOOR HAS SMALL AREA OF CORROSION IN TRACK FORWRD OF FRAME 28. REMOVED AND R EPLACED SEAT TRACK NR 10 FORWARD OF R-2 DOOR PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999040200600 19990402 00600 EU 1999 4 2 AALA990085 1 19990119 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7083A 645 TUL - FOUND CORROSION ON TOP TRACK AT FRAME 31. REPLACED SECTION OF TRACK PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999040200601 19990402 00601 EU 1999 4 2 AALA990084 1 19990119 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 32 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7083A 645 TUL - FOUD LAV 'M' AFT OF DOOR FRAME AND AFT OF NR 9 TRACK HAS CORROSION TOP OF TRACK. REPLACED SECTION OF FLOOR TRACK PER SRM 51-72-10-02. (M) 2 L 7 2 4F RT A35EU 1999040200602 19990402 00602 EU 1999 4 2 AALA990074 1 19990115 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 29 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7083A 645 TUL - FLOORBOARD SUPPORT CORRODED FROM FORWARD OF FRAME 13 TO 13B AND STATION 29 LEFT. REMOVED AND REPLACED SUPPORT AT FRAME 13 TO 13B AND STATION 29 LEFT PER SRM 51-72-10 AND 51-21-10. (M) 2 L 7 2 4F RT A35EU 1999040200603 19990402 00603 NM 1999 4 2 AALA990166 1 19990202 A 2782 MOUNT BOEING 727 727223 1384074 NM NR 1 SLAT ACT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - FOUND NR 1 SLAT ACTUATOR OUTBOARD MOUNT CRACKED (INBOARD PIECE). INSTALLED NEW SLAT ACTUATOR OUTBOARD MOUNT. (M) 2 L 7 3 4F A3WE 1999040200604 19990402 00604 EU 1999 4 2 AALA990151 1 19990203 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 31-33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - FOUND LAV 'L' TIE DOWN AREAS CORRODED AT INBOARD SUPPORT BEAM. REMOVED AND BLENDED OUT CORROSION PER ESO 30595/01 -02-99, TREATED, PRIMED AND PAINTED. (M) 2 L 7 2 4F RT A35EU 1999040200605 19990402 00605 NM 1999 4 2 AALA990184 1 19990216 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 490 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND INSIDE STRINGER 28L CORRODED UNDER LEVELING COMPOUND STATION 490. REMOVED CORROSION PER 51-10-6, SPLICED ST RINGER 28L PER SRM 53-10-3. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999040200606 19990402 00606 NM 1999 4 2 AALA990183 1 19990213 A 5330 SKIN BOEING 727 727223 1384074 NM BS 700-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND SKIN CORRODED BELOW STRINGER 28L AND 28R STATION 700-720. CUTOUT DAMAGED AREAS AND INSTALLED 1 DOUBLER REPA IR PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999040200607 19990402 00607 NM 1999 4 2 AALA990185 1 19990213 A 5330 SKIN BOEING 727 727223 1384074 NM BS 480-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND CORROSION ON SKIN JUST OUTBOARD OF STRINGER 28L STATION 480 TO STATION 500. REMOVED CORROSION PER 51-10-6 S PLICED STRINGER 28L PER SRM 53-10-3. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999040200608 19990402 00608 NM 1999 4 2 AALA990186 1 19990210 A 5320 69191061 STIFFENER BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND ANGLE ATTACHED TO VERTICAL STIFFENER IS CRACKED. REMOVED AND INSTALLED NEW ANGLE AT STATION 1183, RBL 26, W L 271, IAW ESO 11697, FEB 9, 1999. (M) 2 L 7 3 4F A3WE 1999040200609 19990402 00609 NM 1999 4 2 AALA990187 1 19990213 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 715 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND STRINGER CORRODED AT STATION 715. INSTALLED STRINGER SPLICE PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200610 19990402 00610 NM 1999 4 2 AALA990188 1 19990213 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 708 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND STRINGER BLOW OUT (CORROSION) AT STATION 708 STRINGER 28L. INSTALLED STRINGER SPLICE PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200611 19990402 00611 NM 1999 4 2 AALA990189 1 19990209 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1223 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - LEFT CHORD ANGLE SPLICE PLATE IS CRACKED AT BS 1223 BELOW FIXED STAIR. REMOVED CRACKED SPLICE PLATE AND INSTALLED NEW SPLICE PLATE. (M) 2 L 7 3 4F A3WE 1999040200612 19990402 00612 NM 1999 4 2 AALA990190 1 19990209 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1223 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND RIGHT CHORD ANGLE SPLICE PLATE IS CRACKED STATION 1223 BELOW FIXED STAIR. REMOVED CRACKED SPLICE PLATE AND INSTALLED NEW SPLICE PLATE. (M) 2 L 7 3 4F A3WE 1999040200613 19990402 00613 NM 1999 4 2 AALA990191 1 19990213 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM BS 700-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - INBOARD SIDE OF INTERCOSTAL CORRODED. REMOVED AND REPLACED INTERCOSTAL STATION 700-720 OUTBOARD OF STRINGER 28R. (M) 2 L 7 3 4F A3WE 1999040200614 19990402 00614 NM 1999 4 2 AALA990192 1 19990213 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM BS 700-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND INBOARD SIDE OF INTERCOSTAL CORRODED STATION 700-720 OUTBOARD OF STRINGER 28R. REMOVED AND REPLACED INTERCO STAL STATION 700-720, STRINGER 28R. (M) 2 L 7 3 4F A3WE 1999040200615 19990402 00615 NM 1999 4 2 AALA990193 1 19990209 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1223 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND CORROSION ON CHORD ANGLE STATION 1223 BELOW FIXED STAIRS. BLENDED CORRODED AREA AND INSTALLED STRAP PER ESO 11697, DATED 2-8-99 CHORD ANGLE RT SIDE STATION 1223. (M) 2 L 7 3 4F A3WE 1999040200616 19990402 00616 NM 1999 4 2 AALA990249 1 19990218 A 5320 ANGLE BOEING 727 727223 1384074 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON TOP ANGLE AFT CARGO DOR CUTOUT AFT FRAME BETWEEN STRINGER 26R AND 27R. PERFORMED REPAIR OF AIR CRAFT CARGO DOORWAY AFT FRAME UPPER FLANGE IAW ESO 11697, DATED 1/18/99. (M) 2 L 7 3 4F A3WE 1999040200617 19990402 00617 NM 1999 4 2 AALA990248 1 19990121 A 5320 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - UPPER DOOR FRAME TORQUE BOX LOWER WEB AND ANGLE CRACKED, THREE PLACES, STATION 570-580 BELOW STRINGER 17R. REMOVE D AND REPLACED CRACKED SUPPORT ANGLE AND CUT OUT 2.75 INCH BY .75 INCH DAMAGED WEB. INSTALLED DOUBLER REPAIR PER SRM 51 -40-2 PAGE 1-6 .040 7075-T6 DOUBLER .032 7075-T6 FILLER, 20 FP6 HI-LOCK . (M) 2 L 7 3 4F A3WE 1999040200618 19990402 00618 NM 1999 4 2 AALA990247 1 19990121 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 303.9 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND HORIZONTAL STIFFENER CORRODED RIGHT STATION 303.9 OUTBOARD OF RIGHT GEAR TRUNNION FITTING. INSTALLED NEW HO RIZONTAL STIFFENER RIGHT SIDE STATION 303.9. (M) 2 L 7 3 4F A3WE 1999040200619 19990402 00619 NM 1999 4 2 AALA990246 1 19990121 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 307 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND HORIZONTAL STIFFENER CORRODED RIGHT STATION 307 JUST OUTBOARD OF RIGHT NOSE GEAR TRUNNION FITTING AT FORWARD END. INSTALLED NEW HORIZONTAL STIFFENER RIGHT SIDE STATION 307. (M) 2 L 7 3 4F A3WE 1999040200620 19990402 00620 NM 1999 4 2 AALA990245 1 19990218 A 5730 SKIN BOEING 727 727223 1384074 NM WS 830-831 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND WING LOWER SKIN CORRODED ON LOWER SURFACE. INSTALLED DOUBLER/TRIPLER OVER THE AREA WHERE CORROSION REMOVAL WAS BEYOND LIMITS PER SRM 57-30-3 AND SEALED PER 51-20-4. (M) 2 L 7 3 4F A3WE 1999040200621 19990402 00621 NM 1999 4 2 AALA990244 1 19990218 A 5730 SKIN BOEING 727 727223 1384074 NM WS 830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND WING LOWER SKIN CORRODED ON LOWER SURFACE STATION 830 LBL 30 INCH TO LBL 32 INCH. REPAIRED CORRODED AREA PE R 57-30-3 PAGE 27 FIG 10. (SHEET 3). (M) 2 L 7 3 4F A3WE 1999040200622 19990402 00622 NM 1999 4 2 AALA990243 1 19990113 A 5720 TRUNNION BOEING 727 727223 1384074 NM WS 736 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND NR 1 SLAT ACT OUTBOARD TRUNNION MOUNT HAS VISABLE INDICATION OF CRACK AT TOP BOLT. REMOVED DOUBLER PLATE WI TH CRACK IN IT AND INSTALLED NEW DOUBLER PER SRM 51-10-1. ALODINED AND PRIMED DOUBLER. (M) 2 L 7 3 4F A3WE 1999040200623 19990402 00623 NM 1999 4 2 AALA990241 1 19990122 A 5320 CLIP BOEING 727 727223 1384074 NM BS 1090 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STRINGER 1 TO BELT FRAME CLIP IMPROPERLY INSTALLED AND CRACKED STATION 1090. REMOVED AND REPLACED WITH SERV ICEABLE (NEW) CLIP PER SRM. (M) 2 L 7 3 4F A3WE 1999040200624 19990402 00624 NM 1999 4 2 AALA990240 1 19990125 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 870 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 870 VERTICAL STIFFENER, NEXT TO APU LOAD CONTROL VALUE HAS DEEP WEAR MARKS. INSTALLED DOUBLER (.050 STAINLESS) PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1999040200625 19990402 00625 NM 1999 4 2 AALA990239 1 19990121 A 5320 WEB BOEING 727 727223 1384074 NM BS 1213 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON WEB STATION 1213 LBL 4, AT TAIL SKID ACTUATOR MOUNTS. REMOVED AND REPLACED CORRODED WEB (7075- T6 .125) PER SRM 51-10-1 PAG 4. (M) 2 L 7 3 4F A3WE 1999040200626 19990402 00626 NM 1999 4 2 AALA990238 1 19990111 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 950-990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND AFT CARGO DOOR CUTOUT FRAME, LOWER CHORD OF FRAME HAS CORROSION IN SEVERAL PLACES AROUND NUTPLATE. SLIGHTLY SPOT FACED AREAS, TREATED AND PRIMED AREA AND REINSTALLED NUTPLATES PER ESO 11697. (M) 2 L 7 3 4F A3WE 1999040200627 19990402 00627 NM 1999 4 2 AALA990237 1 19990201 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND LOWER END OF VERTICAL STIFFENER CORRODED STATION 1183, INBOARD STRINGER 27L. REMOVED CORROSION, INSTALLED D OUBLER REPAIR PER ESO 11697, DATED 1-13-99. (M) 2 L 7 3 4F A3WE 1999040200628 19990402 00628 NM 1999 4 2 AALA990236 1 19990218 A 5321 FLOOR BOEING 727 727223 1384074 NM BS 1166-1162 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON LEFT AFT LAV FLOOR STATION 1166-1162 LBL 24-29. REPLACED LEFT LAV FLOOR PAN PER SRM 51-10-1 AN D ESO 11697, DATED 1-14-99. (M) 2 L 7 3 4F A3WE 1999040200629 19990402 00629 NM 1999 4 2 AALA990235 1 19990112 A 5320 CLIP BOEING 727 727223 1384074 NM BS 566 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - STRINGER CLIP CORRODED INSIDE STRINGER 26L AT STATION 566. REMOVED CORROSION ON STRINGER CLIP PER SRM 51-10-6, BE YOND MANUAL LIMITS. REPLACED STRINGER CLIP AT STATION 26L, STATION 566. (M) 2 L 7 3 4F A3WE 1999040200630 19990402 00630 NM 1999 4 2 AALA990234 1 19990201 A 5320 CHORD BOEING 727 727223 1384074 NM BS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 1183 LOWER CHORD CORRODED INBOARD STRINGER 27L BULKHEAD FITTING. REMOVED CORROSION AND INSTALLED DO UBLER REPAIR PER ESO 11697, DATED 1-13-99. (M) 2 L 7 3 4F A3WE 1999040200631 19990402 00631 NM 1999 4 2 AALA990233 1 19990121 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 1166 BELL FRAME SHEAR TIE CORRODED, AFT SIDE BETWEEN STRINGER 28L AND 29L. REPLACED SHEAR TIE PER S RM 51-10-01, TREATED AND PRIMED PER MM 51-20-0. (M) 2 L 7 3 4F A3WE 1999040200632 19990402 00632 NM 1999 4 2 AALA990232 1 19990121 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - AT STATION 1166 BELL FRAME SHEAR TIE CORRODED, AFT SIDE, BETWEEN STRINGER 29L AND 30L. REPLACED SHEAR TIE PER SRM 51-10-01, TREATED, PRIMED AND PAINTED PER MM 51-20-0. (M) 2 L 7 3 4F A3WE 1999040200633 19990402 00633 NM 1999 4 2 AALA990231 1 19990120 A 5320 STRAP BOEING 727 727223 1384074 NM BS 1004-995 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON STRINGER 29L REPAIR STRAP OUTBOARD LEG STATION 1004-995. FABRICATED AND INSTALLED NEW REPAIR S TRAP ON STRINGER 29L. (M) 2 L 7 3 4F A3WE 1999040200634 19990402 00634 NM 1999 4 2 AALA990230 1 19990121 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON SHEAR TIE AT STATION 990 INBOARD OF STRINGER 29R 1 INCH - 2 INCH FORWARD SIDE. CUT OFF DAMAGED SECTION AND SPLICED IN NEW SHEAR TIE PER SRM 53-10-04 FIG 13. (M) 2 L 7 3 4F A3WE 1999040200635 19990402 00635 NM 1999 4 2 AALA990229 1 19990126 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1015 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON OUTBOARD LEG OF STRINGER 29R AROUND 5 EACH FASTENERS STATION 1000-1015. REMOVED CORROSION INST ALLED STRAP REPAIR PER ESO 11697, DATED 1-19-99. (M) 2 L 7 3 4F A3WE 1999040200636 19990402 00636 NM 1999 4 2 AALA990228 1 19990111 A 5311 FRAME BOEING 727 727223 1384074 NM BS 580 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENTS IN BELT FRAME UPPER FLANGE ABOVE STRINGER 23L AND ABOVE STRINGER 24L. INSTALLED DOUBLER ON BELT FRAME STATION 580 STRINGER 22L - 24L. DOUBLER 18 INCH LONG MADE OF 7075T6 .050 USING 3 ROWS, 2 ON THE SIDE AND 1 ON TOP, USE D 44 MS20470D .375 RIVETS AND 4MS20470D .25 INCH RIVETS. (M) 2 L 7 3 4F A3WE 1999040200637 19990402 00637 NM 1999 4 2 AALA990227 1 19990218 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 930 LEFT BELL FRAME CRACKED AT STRINGER 14 LEFT. REPAIRED BELL FRAME AT STATION 930 LEFT, STRINGER 14L PER SRM 53-10-4 FIG 1 USING 1 CHANNEL 5530762 - .080 7075T6 AND 1 DOUBLER 5831870 - .071-7055 PLUS 6 - .25 INCH 1ST OVER HI-LOCKS IN PREVIOUS HOLES AND .375 1ST OVERSIZE INNEW HOLES. (M) 2 L 7 3 4F A3WE 1999040200639 19990402 00639 NM 1999 4 2 AALA990225 1 19990122 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1030 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 1030 FRAME DENTED AT STRINGER 25L. CUT OUT DAMAGED AREA OF FRAME. INSTALLED DOUBLER REPAIR PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999040200640 19990402 00640 NM 1999 4 2 AALA990224 1 19990122 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 1213 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON UPPER TAIL SKID ACTUATOR SUPPORT BEAM STATION 1213, RBL 6 TO LBL 6. INSTALLED NEW SUPPORT BEAM . (M) 2 L 7 3 4F A3WE 1999040200641 19990402 00641 NM 1999 4 2 AALA990223 1 19990122 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 1213 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON LOWER TAIL SKID ACTUATOR SUPPORT BEAM STATION 1213 LBL 6 FORWARD SIDE. INSTALLED NEW SUPPORT B EAM. (M) 2 L 7 3 4F A3WE 1999040200642 19990402 00642 NM 1999 4 2 AALA990222 1 19990122 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON FLOORBEAM STATION 1130 RBL 27 INCH. INSTALLED REPAIR PER ESO 11697, DATED 1-5-99. (M) 2 L 7 3 4F A3WE 1999040200643 19990402 00643 NM 1999 4 2 AALA990221 1 19990121 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STRINGER 15L CRACKED JUST FORWARD OF LEFT WING ICE LIGHTS. REMOVED DAMAGE SECTION OF STRINGER COMPLETED STR INGER REPAIR PER SRM 53-10-3 FIG 1 DETAIL II. (M) 2 L 7 3 4F A3WE 1999040200644 19990402 00644 NM 1999 4 2 AALA990220 1 19990121 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - 15R STRINGER END CRACKED JUST FORWARD OF RIGHT WING ICE LIGHT. REMOVED DAMAGED SECTION OF STRINGER, COMPLETED REP AIR OF STRINGER PER SRM 53-10-3 FIG 1 DETAIL II. (M) 2 L 7 3 4F A3WE 1999040200645 19990402 00645 NM 1999 4 2 AALA990219 1 19990119 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1030 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND LOWER LOBE BELL FRAME DENTED ON TOP FLANGE OF FRAME, STATION 1030 BETWEEN STRINGER 26R AND 25R. CUT OUT DAM AGED AREA AND INSTALLED DOUBLER REPAIR PER 53-10-4 PAGE 1-4. (M) 2 L 7 3 4F A3WE 1999040200646 19990402 00646 NM 1999 4 2 AALA990218 1 19990119 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 388 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND UPPER LEG OF STRINGER 24R AT STATION 388 BENT. REFORMED SMALL DENT AND INSTALLED DOUBLER PER SRM 53-10-3 FI G 2. (M) 2 L 7 3 4F A3WE 1999040200647 19990402 00647 NM 1999 4 2 AALA990217 1 19990118 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND BELL FRAME 620 DENTED BETWEEN STRINGERS 24L AND 25L, AND DENTED ABOVE STRINGER 25L. CUT OUT AREA 1 INCH BY 5 INCH, INSTALLED DOUBLER 13 INCH LONG 7075T6 AND .063, 39 UNIVERSAL .375 D RIVETS AND 4 UNIVERSAL HEAD .25 D RIVETS INS TALLED. (M) 2 L 7 3 4F A3WE 1999040200648 19990402 00648 NM 1999 4 2 AALA990216 1 19990122 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1090 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STRINGER 1 STATION 1090, CRACKED AROUND FASTENER HOLE ON RIGHT SIDE FORWARD HOLE AT STRINGER CLIP. CUTOUT D AMAGE STRINGER FROM STATION 1082 TO STATION 1096. HAD NEW PIECE FABRICATED FROM 7075-T6 .040 THICK. INSTALLED STRINGER AND CHANNEL STRAP (TAPERED FROM .125) TO SKIN WITH 23 EACH STANDARD .375 INCH HI-LOCKS. INSTALLED 4 .080 STRAPS TO OUT BOARD ENDS OF STRINGER CHANNEL SPLICE WITH 40 EACH .15625 INCH HI-LOCKS. INSTALLED 4 EACH .080 STRAPS TO THE LOWER FLAN GE OF STRINGER AT SPLICED WITH 40 EACH .15625 INCH HI-LOCKS. REPAIR IS PER SRM 53-10-3 FIG 3. (M) 2 L 7 3 4F A3WE 1999040200649 19990402 00649 NM 1999 4 2 AALA990215 1 19990118 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1010 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 1010 FRAME DENTED TWO PLACES ABOVE 26L. INSTALLED DOUBLER 7075 T-6 .050, 14.5 INCHES LONG WITH 2 RO WS FASTENERS ON SIDE, ONE ROW TOP PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999040200650 19990402 00650 NM 1999 4 2 AALA990214 1 19990114 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 990 FRAME DENTED STRINGER 26L TO 25L. INSTALLED DOUBLER AT STATION 990 STRINGER 26L TO 25L WET IAW SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999040200651 19990402 00651 NM 1999 4 2 AALA990213 1 19990218 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND STATION 950 CORROSION AT 2ND VERTICAL STIFFENER FROM KEEL BEAM TOP END. INSTALLED DOUBLER WET PER SRM 53-10 -9. (M) 2 L 7 3 4F A3WE 1999040200652 19990402 00652 NM 1999 4 2 AALA990212 1 19990121 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CRACK IN FRAME INBOARD TO OUTBOARD RADIUS. FRAME WAS CUT ABOVE STRINGER 13 RT NEW FRAME SPLICED IAW SRM 53- 10-4 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200653 19990402 00653 NM 1999 4 2 AALA990211 1 19990127 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1090 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND TOP OF BELL FRAME DENTED STATION 1090 STRINGER 27 LEFT. INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999040200654 19990402 00654 NM 1999 4 2 AALA990210 1 19990121 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 280 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - 5TH STRINGER UP FROM LINE RIGHT SIDE, STATION 280 CENTER OF STRINGER CHANNEL HAS VISUAL INDICATION OF CRACK AT TOO LING MARK. DYE CHECKED, NO CRACK FOUND. BLENDED TOOLING MARK PER SRM 51-10-1, INSTALLED DOUBLER IN STRINGER PER SRM 53 -10-3. (M) 2 L 7 3 4F A3WE 1999040200655 19990402 00655 NM 1999 4 2 AALA990209 1 19990218 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - STATION 1070 FRAME DENTED ON TOP BETWEEN STRINGER 26R AND 27R. INSTALLED DOUBLER WET AT STATION 1070 BETWEEN STR INGER 26R AND 27R PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999040200657 19990402 00657 NM 1999 4 2 AALA990207 1 19990218 A 5314 KEEL BEAM BOEING 727 727223 1384074 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - KEEL BEAM CRACKED AT LOWER CHORD, RIGHT SIDE, SECOND FASTENER AFT OF STATION 870. REMOVED DAMAGED (CRACK) PER ESO 11697 DATED 1/13/99. REPAIRED PER SERVICE BULLETIN 727-53-0208, DETAIL II. (M) 2 L 7 3 4F A3WE 1999040200658 19990402 00658 NM 1999 4 2 AALA990206 1 19990108 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENT AT BELL FRAME STATION 600 ABOVE STRINGER 24L DENT AT BELL FRAME STATION 600 ABOVE STRINGER 25L. REMOVE D DAMAGE AREA 1 INCH AND 1 INCH ABOVE 24L 1 INCH BY 1 INCH ABOVE STRINGER 25L. INSTALLED 20 INCH DOUBLER, 7075-T6 .063 INSTALLED 53 RIVETS .1875 AND FOUR .25 3 ROWS TOTAL PER SRM 51-40-3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200659 19990402 00659 NM 1999 4 2 AALA990205 1 19990113 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - BELL FRAME STATION 600 BETWEEN STRINGER 4R AND 5R CRACKED. REMOVED DAMAGED AREA 1..875 INCH. INSTALLED DOUBLER 1 5 INCHES LONG .071 7075-T6 INNER 15 INCH .080 7075-T6 OUTER, .050 2024-T3 FILLER 4 ROWS OF FASTENER 51 BACB30FA16. (M) 2 L 7 3 4F A3WE 1999040200660 19990402 00660 NM 1999 4 2 AALA990204 1 19990108 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENT AT BELL FRAME ABOVE STRINGER 23L. REMOVED DAMAGED AREA ABOVE STRINGER. REMOVED DAMAGED AREA ABOVE STR INGER 23L STATION 600 CUTOUT 1 INCH BY 1 INCH AREA. INSTALLED 8 INCH DOUBLER 7075-T6 .063 INSTALLED 21 RIVETS MS20470D 3 ROWS TOTAL PER SRM 51-40-3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200661 19990402 00661 NM 1999 4 2 AALA990203 1 19990108 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENT AT BELL FRAME STATION 500 BETWEEN STRINGER 22L AND 23L. DENT AT BELL FRAME STATION 500 BETWEEN STRINGE R 23L AND 24L. CUTOUT SECTION .75 INCH BY 2 INCH BETWEEN STRINGER 22L AND 23L, .75 INCH BY 1 INCH AND .75 INCH AND .5 I NCH STRINGER 23L AND 24L. INSTALLED DOUBLER 14.5 INCH LONG, 7075-T6 .050 INSTALLED 35 .1875 UNIVERSAL HEAD D RIVETS 3 R OWS TOTAL 2 ON SIDE 1 ON TOP PER SRM 51-40-3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200662 19990402 00662 NM 1999 4 2 AALA990202 1 19990111 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - DENT AT BELL FRAME STATION 680 BETWEEN 24L AND 25L. CUT OUT DAMAGED AREA 10 INCH BY .5 INCH. INSTALLED DOUBLER 7 075-T6 .050 15 INCHES LONG INSTALLED THREE ROWS OF RIVETS, 1 ON TOP, 2 ON SIDE, 33 D UNIVERSAL .1875 RIVETS AND 3 D UNIV ERSAL .25 RIVETS. (M) 2 L 7 3 4F A3WE 1999040200663 19990402 00663 NM 1999 4 2 AALA990201 1 19990118 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENT AT BELL FRAME STATION 560 BETWEEN 24L AND 25L. INSTALLED DOUBLER 8 INCHES LONG, 7075-T6 .050 WITH 3 RO WS OF FASTENERS, 1 ROW ON TOP, 2 ROWS ON SIDE, 39 .1875 D RIVETS, 4.25 INCH D RIVETS. (M) 2 L 7 3 4F A3WE 1999040200664 19990402 00664 NM 1999 4 2 AALA990200 1 19990118 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENTS AT BELL FRAME STATION 660 BETWEEN STRINGER 24R AND 25R. REMOVED DAMAGED AREA 1 INCH BY 2 INCH, INSTAL LED 7075-T6 .063 DOUBLER 8 INCHES LONG, RIVETS ARE MS 20470D, 19 EACH .1875 AND 4 EACH .25 , 3 ROWS TOTAL IAW SRM 51-40- 3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200665 19990402 00665 NM 1999 4 2 AALA990199 1 19990107 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - STATION 1110 FRAME DENTED ON TOP 2 PLACES AT STRINGER 26L. REMOVED DAMAGE. INSTALLED 7075-T6 .071 DOUBLER 13 INC HES LONG PER SRM 51-40-3 FIG 1. REFERRED FROM AARD 53-10-7-3 PAGE 1, 3 ROWS AD RIVETS ON WEB, R ROW .1875 RIVETS TOP FL ANGE 10 FASTENERS 21 EACH .1875 TWO ROWS, 11 EACH .25 ON ONE ROW. (M) 2 L 7 3 4F A3WE 1999040200666 19990402 00666 NM 1999 4 2 AALA990198 1 19990118 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENTS IN BELL FRAME AT BS 680 BETWEEN STRINGER 22R AND 23R. REMOVED DAMAGED AREA 1.25 INCH BY 1 INCH AND 1 INCH BY 1 INCH. INSTALLED 7075-T6 .063 DOUBLER 14 INCHES LONG, RIVETS ARE MS20470D, 34 EACH .1875, 3 ROWS TOTAL IAW SRM 51-40-3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1999040200667 19990402 00667 NM 1999 4 2 AALA990197 1 19990112 A 5311 FRAME BOEING 727 727223 1384074 NM BS 376 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND FORWARD DOOR OPENING FRAME CORRODED AT BOTTOM GOING UNDER FLOORBOARD TO SIDE CREASE ANGLE AT STATION 376. R EPAIRED PER SRM 51-40-3, MATERIAL USED 2024-T3 OF .063 THICKNESS FASTENERS USED WERE BACB30FM6, BACB30EN6, NAS6204 BOLTS . (M) 2 L 7 3 4F A3WE 1999040200668 19990402 00668 NM 1999 4 2 AALA990196 1 19990111 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 443 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON STRINGER 27R STATION 435-445. INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999040200669 19990402 00669 NM 1999 4 2 AALA990195 1 19990119 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CORROSION ON FUSE AT LEFT OVERWING ICE LIGHT INSIDE. REMOVED CORROSION AROUND LEFT ICE LIGHT CUTOUT, STRING ER 15L BS 720B AND C, DIGITAL THICKNESS HIGH.168, .132. INSTALLED DOUBLER PER SRM 53-30-3 PAGE 137-140. (M) 2 L 7 3 4F A3WE 1999040200670 19990402 00670 NM 1999 4 2 AALA994031 1 19990218 A 5320 SILL BOEING 767 767323 1385205 NM BS 625 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - LOWER AUXILIARY SILL INNER CHORD RBL 30, STATION 625 HAD CORROSION BLENDED ON LOWER SURFACE BEYOND SRM LIMITS. RE PAIRED PER MRB 767-7818. (M) 2 L 7 2 4F RT A1NM 1999040200671 19990402 00671 NM 1999 4 2 AALA994032 1 19990217 A 5320 SILL BOEING 767 767323 1385205 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - OUTER CHORD ON LOWER MAIN SILL HAS CORROSION REMOVAL ON VERTICAL LEG INNER SURFACE AS SHOWN. REPAIRED IAW MRB 767 -1819, DATED 11 FEB 99. (M) 2 L 7 2 4F RT A1NM 1999040200672 19990402 00672 NM 1999 4 2 AALA994033 1 19990118 A 5311 FRAME BOEING 767 767323 1385205 NM BS 1197 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - FUSELAGE FRAME INNER CHORD HAS CORROSION REMOVAL ON LOWER SURFACE AS SHOWN MATERIAL REMAINING IS BEYOND SRM 53-00- 07-1 LIMITS. BLENDED CORROSION IAW MRB 767-1816 DATED FEB 09, 1999. (M) 2 L 7 2 4F RT A1NM 1999040200673 19990402 00673 NM 1999 4 2 AALA994034 1 19990224 A 5311 FRAME BOEING 767 767323 1385205 NM BS 1219 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - AFT CARGO FRAME (J-CAP) AT STATION 1219 RBL 42 HAD CORROSION. REMOVED CORROSION UNDER NUTPLATE, ALODINED, PRIMED AND REINSTALLED NUTPLATES. (M) 2 L 7 2 4F RT A1NM 1999040200674 19990402 00674 NM 1999 4 2 AALA994035 1 19990217 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL AS SHOWN ON SKETCH. ALODINED AND PRIMED STATION 1480 LBL 50-51. R EPAIRED IAW MRB 767-1810. (M) 2 L 7 2 4F RT A1NM 1999040200675 19990402 00675 NM 1999 4 2 AALA994036 1 19990211 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 783 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - FOUND SMALL CRACK IN VERTICAL LEG OF FLOORBEAM AT STATION 783 RBL 11.06 AND LBL 11.06. REMOVED DAMAGED SECTION OF FLOORBEAM. SPLICED IN NEW SECTION OF FLOORBEAM. INSTALLED ALL REPAIR PARTS WET WITH BMS 5-95. (M) 2 L 7 2 4F RT A1NM 1999040200676 19990402 00676 NM 1999 4 2 AALA994039 1 19990218 A 5313 STRINGER BOEING 767 767323 1385205 NM BS 444 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - STRINGER 37L CORRODED AT APPROX STATION 444. REMOVED CORRODED PIECE. INSTALLED SIMILAR PIECE FASTENERS AND STRIN GER CLIP, TREATED AND PRIMED SURFACE. (M) 2 L 7 2 4F RT A1NM 1999040200677 19990402 00677 NM 1999 4 2 AALA994041 1 19990224 A 5313 STRINGER BOEING 767 767323 1385205 NM BS 444 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 352AA 24033 AFW - FOUND STRINGER 37L CORRODED AT APPROX STATION 444. REMOVE CORRODED PIECE OF STRINGER. REPLACE WITH SIMILAR LONGE R SPLICE WITHOUT A JOGGLE. USE SHIMS AND FILLERS. REPAIR PARTS AND BARE SURFACES FINISHED WITH ALODINE AND PRIMER. (M ) 2 L 7 2 4F RT A1NM 1999040200679 19990402 00679 1999 4 2 AALA990051 4 19990103 A 2397 WIRE AIRBUS 300 A300B4605R 3930308 EU PA SYSTEM SHORTED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 25071 514 BOS - FLT 121 - EN ROUTE LGW-BOS - DURING CRUISE, THE TRANSFORMER AT SEAT 29G SHORTED OUT CAUSING SPARKS AND SMOKE. ALL VIDEOS IN ZONE WERE BLANK. SECURED SYSTEM. LANDED BOS WITHOUT INCIDENT. REPLACED WIRING HARNESS AT SEAT 29G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999040200680 19990402 00680 WP 1999 4 2 AALA990172 1 19990211 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7517A 49894 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT OVERWING EXITS WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999040200682 19990402 00682 WP 1999 4 2 AALA990174 1 19990214 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 497AA 49735 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EM ERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999040200683 19990402 00683 NM 1999 4 2 AALA990254 1 19990219 A 2910 10612453 FUSE BOEING 767 767223 1385123 NM CTR HYD SYST TRIPPED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 301AA 22307 ORD - FLT 0177 - EN ROUTE JFK-SFO - CENTER HYDRAULIC QTY EICAS MESSAGE ILLUMINATED IN FLIGHT. ALL PUMPS WERE TURNED OFF WITH QTY STOPPING AT 46. LOWEST FLUID WAS 20. DECLARED EMERGENCY, AIR INTERRUPTED AND LANDED ORD WITHOUT INCIDENT. R EPLACED CENTER HYDRAULIC FUSE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999040200684 19990402 00684 WP 1999 4 2 AALA990251 1 19990221 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 215AA 49163 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE IN CABIN. REPAIRED WIRING ON EMERGENCY EXI T FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999040200685 19990402 00685 WP 1999 4 2 AALA990259 1 19990222 A 3350 BULB DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90511 49805 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT BULB INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR LIGHT BUL B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999040200686 19990402 00686 WP 1999 4 2 AALA990262 1 19990222 A 3350 LIGHT DOUG DC9 DC982 3022082 WP AIR STAIR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 463AA 49593 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AIR STAIR TAIL SECTION INOPERATIVE. REPLACED EMERGENCY EXI T LIGHT SECTION IN AFT AIR STAIR TAIL SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999040200687 19990402 00687 NM 1999 4 2 ASAA9940033 1 19990212 A 5320 6553844 SUPPORT BOEING 737 7374Q8 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 947 BETWEEN STRINGER 25L AND 26L WAS FOUND TO BE CORRODED. REPAIRED SECTION PER 53-00-53. (M) 2 L 7 2 4F RT A16WE 1999040200688 19990402 00688 NM 1999 4 2 ASAA9940032 1 19990212 A 5320 6017938 SUPPORT BOEING 737 7374Q8 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 947 STRINGER 26R WAS FOUND TO BE CORRODED. REPAIRED SECTION PER 53-00-53. (M) 2 L 7 2 4F RT A16WE 1999040200689 19990402 00689 NM 1999 4 2 ASAA9940031 1 19990212 A 5315 FLOORBEAM BOEING 737 7374Q8 NM BS 1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE UPPER SURFACE OF THE FLOORBEAM AT STATION 1016 LBL 29 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999040200690 19990402 00690 NM 1999 4 2 ASAA9940030 1 19990212 A 5315 6545818 FLOORBEAM BOEING 737 7374Q8 NM BS 360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE FLOORBEAM AT STATION 360 RBL 20-30 WAS FOUND TO BE CORRODED. REPLACED FLOORBEAM SECTION PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999040200691 19990402 00691 NM 1999 4 2 ASAA9940029 1 19990212 A 5347 BAC1520792 SEAT TRACK BOEING 737 7374Q8 NM BS 360-500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE RIGHT INBOARD SEAT TRACK FROM STATION 360-500E WAS FOUND TO BE CORRODED. REPLACED SEAT T RACK PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 1999040200692 19990402 00692 NM 1999 4 2 ASAA9940028 1 19990212 A 5320 6547690 SUPPORT BOEING 737 7374Q8 NM BS 867-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 867-947 STRINGER 25R WAS CORRODED. REPLAC ED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1999040200693 19990402 00693 NM 1999 4 2 ASAA9940027 1 19990212 A 5320 6547690 SUPPORT BOEING 737 7374Q8 NM BS 807-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 947-807 STRINGER 25L WAS CORRODED. REPLAC ED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1999040200694 19990402 00694 NM 1999 4 2 ASAA9940026 1 19990212 A 5320 6547690 SUPPORT BOEING 737 7374Q8 NM BS 727-807 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 727B-807 STRINGER 25L WAS CORRODED. REPLA CED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1999040200695 19990402 00695 NM 1999 4 2 ASAA9940025 1 19990212 A 5320 6547690 SUPPORT BOEING 737 7374Q8 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 727B-727E STRINGER 25L WAS CORRODED. REPL ACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1999040200696 19990402 00696 NM 1999 4 2 ASAA9940024 1 19990212 A 5320 6546740 SUPPORT BOEING 737 7374Q8 NM BS 727-769 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 727C-769 STRINGER 25R WAS CORRODED. REPLA CED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1999040200697 19990402 00697 NM 1999 4 2 ASAA9940023 1 19990212 A 5320 65C31847 INTERCOSTAL BOEING 737 7374Q8 NM BS 1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE UPPER SURFACE OF THE INTERCOSTAL AT STATION 1016 RBL 27 WAS CORRODED. REPLACED STRAP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999040200698 19990402 00698 NM 1999 4 2 ASAA9940022 1 19990212 A 5320 65C3184779 SUPPORT BOEING 737 7374Q8 NM BS 967-987 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE UPPER SURFACE OF THE FLOOR SUPPORT AT STATION 967-987 LBL 16 WAS CORRODED. REPLACED FLOO R SUPPORT PER SRM 51-40-00. (M) 2 L 7 2 4F RT A16WE 1999040200699 19990402 00699 NM 1999 4 2 ASAA9940021 1 19990212 A 5320 65C3184779 SUPPORT BOEING 737 7374Q8 NM BS 967-987 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE FLOOR SUPPORT AT STATION 967-987 RBL 16 WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51- 40-00. (M) 2 L 7 2 4F RT A16WE 1999040200700 19990402 00700 NM 1999 4 2 ASAA9940020 1 19990212 A 5320 BAC1505100403 SUPPORT BOEING 737 7374Q8 NM BS 328-344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE UPPER SURFACE SUPPORT AT STATION 328-344 LBL 13 WAS CORRODED. REPLACED SUPPORT PER SRM 5 1-40-2. (M) 2 L 7 2 4F RT A16WE 1999040200701 19990402 00701 NM 1999 4 2 ASAA9940019 1 19990212 A 5320 65176880165 SUPPORT BOEING 737 7374Q8 NM BS 303-348 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE FLOOR SUPPORT AT BS 303-348 LBL 70.53 WAS FOUND TO BE CORRODED. REPLACED CHORD PER SRM 5 1-40-2. (M) 2 L 7 2 4F RT A16WE 1999040200702 19990402 00702 EA 1999 4 2 MASA99035 1 19990302 A 3350 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 FLT 5840 - DCA-TYS - CREW REPORTED THE SECOND FROM REAR CEILING EMERGENCY LGIHT TO BE INOPERATIVE. MAINTENANCE ACTION W AS DEFERRED PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REP LACED. (M) 2 L 7 2 4F RT A21EA 1999040200703 19990402 00703 CE 1999 4 2 MASA99029 1 19990218 A 5210 PIN BEECH 1900 1900D 1154162 CE PAX DOOR DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 133YV UE133 FLT 5299 - IAD-SYR - PRIOR TO DEPARTURE, CREW REPORTED THAT THE EXTERIOR DOOR HANDLE SPINS FREELY. MAINTENANCE INSPECTE D THE DOOR HANDLE AND COULD NOT DUPLICATE THE DISCREPANCY, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. THAT EV ENING DURING ROUTINE MAINTENANCE IN RDG, THE DOOR HANDLE WAS RE-INSPECTED. MAINTENANCE FOUND THAT THE HANDLE WAS OPERAT IONAL BUT THE PIN WAS DAMAGED. THE DOOR HANDLE WAS RELACED. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1999040200704 19990402 00704 NM 1999 4 2 MASA99036 1 19990303 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 FLT 6282 - PHX-ASE - PRIOR TO DEPARTURE, CREW REPORTED THAT TWO ADJACENT FLOOR EMERGENCY PATH LIGHTING BULBS WERE INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999040200705 19990402 00705 WP 1999 4 2 HALA9900060 1 19990223 A 2751 WARNING LIGHT DOUG DC10 DC1010 3022110 WP TE FLAPS ILLUMINATED A HALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 125AA 46525 HNL - FLT 466 - AFTER LANDING SLAT YELLOW DISAGREE LIGHT REMAINED ON AFTER RETRACTING FLAPS. RECYCLED FLAPS TO 50 DEGRE ES AND BACK AND LIGHT REMAINED ON. SECURITY AND CONDITION OF SLAT CHECKED OK. CHECKED SLAT SENSORS CHECKED OK. CHECKE D SLAT HANDLE SWITCH CHECKED OK. BITE CHECK PROX BOX, CHECKED OK. OPERATED SLAT AND FLAP NUMEROUS TIMES, COULD NOT DUP LICATE AT THIS TIME. OK FOR SERVICE. (M) 2 L 7 3 4F A22WE 1999040200706 19990402 00706 WP 1999 4 2 USAAD99034 1 19990302 A 3260 0080004003 CONTROL BOX DOUG DC9 DC931 3022065 WP E/E COMPT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 924VJ 32032 48144 PIT-SBN - FLT 753 - AFTER TAKEOFF, THE RIGHT MLG UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE UP. THE LANDING WAS CYCL ED BUT THE LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SENSING CONTROL BOX. (M) 2 L 7 2 4F A6WE 1999040200707 19990402 00707 EU 1999 4 2 USAAF99011 1 19990301 A 3213 STRUT FOKKER F28 F28MK0100 4990807 EU LT MLG REQ'D SERVICE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 892US 11372 PIT - FLT 2160 - AFTER TAKEOFF FROM PIT THE FOLLOWING MESSAGES APPEARED ON THE MULTI FUNCTION DISPLAY UNIT, GND/FLT CTL, TO WARN CONFIG, STAB WARN. FLIGHT CREW DECIDED TO RETURN TO PIT TO HAVE MAINTENANCE LOOK AT THE AIRCRAFT. FLIGHT LAND ED PIT WITHOUT FURTHER INCIDENT. MAINTENANCE ISOLATED THE PROBLEM TO A LEFT MAIN LANDING GEAR SENSOR USING THE PROXIMIT Y SENSING COMPUTER HISTORICAL FAULT CODES. THE LEFT LANDING GEAR STRUT WAS LOW. MAINTENANCE SERVICED BOTH MAIN GEAR ST RUTS. (M) 2 L 7 2 4F RT 1999040200708 19990402 00708 NM 1999 4 2 USAA029913 1 19990224 A 3350 08199001205 LIGHT BOEING 727 727225 1384077 NM CABIN CRACKED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918TS 20445 FLT 6171 - BOS-LGA - FORWARD PORTION OF FLOOR EMERGENCY TRACK LIGHTING HAS BEEN TORN UP AND DOES NOT ILLUMINATE. REPAIR ED SECTION OF EMERGENCY EXIT TRACK LIGHTING, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999040200709 19990402 00709 NM 1999 4 2 USAA029912 1 19990225 A 3350 90052 BATTERY CHARGER BOEING 727 727227 1384078 NM PASSENGER DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927TS R3489 20837 FLT 6522 - FOUND ON L/S, AFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE AT AFT ENTRY DOOR. REPLACED BATTERY CHARGER BASE, O PS CHECKS OK. (M) 2 L 7 3 4F A3WE 1999040200710 19990402 00710 NM 1999 4 2 USAA029914 1 19990226 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM LT EMER EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 923TS AT8107 20441 FLT 6541 - LGA-DCA - FOUND ON L/S CHECK, LEFT OVERWING EXTERIOR CENTER EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTE RY PACK, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999040200711 19990402 00711 NM 1999 4 2 P2EA99087 1 19990218 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 312 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, CABIN FLOORBEAM AT BS 312, RBL 45 FOUND WITH CORROSION. THE FLOORBEAM UPPER SECTION AT STATION 31 2 FROM RBL 19 TO RBL 61 WAS REPLACED IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999040200712 19990402 00712 NM 1999 4 2 P2EA99086 1 19990218 A 5330 SKIN BOEING 737 737222 1384473 NM BS 1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE SKIN AT BS 1016, STRINGER 26R HAD BULGED SKIN. CORROSION WAS FOUND. AREA WAS REPAIRED IAW SR M 53-10-3 FIG 3, SHEET 7. (M) 2 L 7 2 4F A16WE 1999040200713 19990402 00713 NM 1999 4 2 P2EA99083 1 19990226 A 5330 SKIN BOEING 737 737222 1384473 NM BS 500 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A SKIN REPAIR AT BS 500A, STRINGER 26R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTE D AND REPAIRED AS PER SRM 53-30-3, FIGURE 16. (M) 2 L 7 2 4F A16WE 1999040200715 19990402 00715 NM 1999 4 2 P2EA99080 1 19990219 A 5330 SKIN BOEING 737 737222 1384473 NM BS 727 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, AN EXISTING SKIN REPAIR LOCATED AT BS 727A, STRINGER 8R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND A PERMANENT REPAIR WAS INSTALLED AS PER SRM 53-30-3 FIGURE 6. (M) 2 L 7 2 4F A16WE 1999040200716 19990402 00716 NM 1999 4 2 P2EA99085 1 19990221 A 5712 RIB BOEING 737 737222 1384473 NM WS 505 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A RIB WAS FOUND CRACKED IN THE RIGHT WING INTERNAL AREA AT WS 505 UPPER FLANGE. THE CRACK WAS REP AIRED IAW SRM 57-10-7 FIG 1. (M) 2 L 7 2 4F A16WE 1999040200717 19990402 00717 NM 1999 4 2 P2EA99084 1 19990223 A 5312 BULKHEAD CHORD BOEING 737 737222 1384473 NM BS 178 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE BS 178 PRESSURE BULKHEAD, FORWARD SIDE, LOWER HORIZONTAL CHORD. CRACK WA S REPAIRED IAW SRM 51-40-4 FIGURE 1. (M) 2 L 7 2 4F A16WE 1999040200718 19990402 00718 1999 4 2 TWRA9907 4 19990216 A 2565 D30440103 SLIDE AIRCRUISERS BOEING 747 747124 1384874 NM R2 DOOR CUT A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 602FF 190 19734 R2 MED SLIDE RAFT EXPIRATION DATE WA COMING DUE, THE SLIDE RAFT WAS USED FOR TRAINING PURPOSES AND INFLATED INTENTIONALL Y. DURING SLIDE DEPLOYMENT THE SLIDE WAS FOUND TO BE CUT AND LEAKING AT THE BAS. EVACUATION WAS COMPLETED PRIOR TO THE RAFT DEFLATING. LIFE RAFT WAS SENT TO THE VENDOR. (M) 2 L 7 4 4F A20WE 1999040200719 19990402 00719 WP 1999 4 2 99ZZZM217 1 19990219 A 3260 801813 SWITCH LKHEED 1011 1011385115 5265015 WP RT MLG DOOR SERVICEABLE A WRNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 75AA 193U1201 RIGHT MAIN GEAR OR DOOR LIGHT ON FLIGHT ENGINEERS ANNUNCIATOR PANEL STAYED ON AFTER GEAR RETRACTED. A/C RETURNED TO GSO . NO FUEL WAS DUMPED AND THE LANDING WAS NORMAL. CHECK AND ADJUSTED RIGHT GEAR DOOR PROXIMITY SWITCH IAW 32-61-07. OP S CHECKED GOOD IAW 32-12-01. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 1999040200720 19990402 00720 WP 1999 4 2 99ZZZM218 1 19990214 A 3230 PIN LKHEED 1011 10113851 5265010 WP NLG NOT REMOVED A WRNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 826CR 193A1141 DEPARTED MBJ, NOSE GEAR WOULD NOT RETRACT. DUMPED APPROX 40,000 LBS OF FUEL AND LANDED WITHOUT FURTHER INCIDENT. AT RE TURN TO MBJ, NOSE GEAR DOWNLOCK PIN WAS FOUND INSTALLED. REMOVED PIN AND RETURN AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A23WE 1999040200721 19990402 00721 NM 1999 4 2 USAASB99054 1 19990225 A 3350 210310005 FUSE BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 350US 23553 EWR - PILOT REPORTED THAT THE EMERGENCY EXIT ROW LIGHTS ON THE LEFT SIDE OF THE CABIN ARE INOPERATIVE. MAINTENANCE FOUN D A BLOWN FUSE (5 AMP) IN THE POWER SUPPLY. REMOVED AND REPLACED FUSE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200722 19990402 00722 NM 1999 4 2 USAASB99055 1 19990215 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 375US 22954 IAH - MAINTENANCE FOUND THE RIGHT FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200723 19990402 00723 NM 1999 4 2 USAABB99008 1 19990221 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM ROWS 13/18/23 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 PHL - FOUND THREE FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M) 2 L 7 2 4F RT A2NM 1999040200724 19990402 00724 NM 1999 4 2 USAASB99048 1 19990220 A 5210 65907373360 DOOR BOEING 737 7374B7 1384702 NM CABIN AIRLEAK A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 449US 24893 MCO - FLT 1148 - AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMB-OUT FROM MCO. THE FORWARD MAIN ENTRY DOOR DID NOT APPEAR TO BE CLOSED PROPERLY, RESULTING IN A LARGE AIR LEAK. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT . NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR AND THE FORWARD ENTRY DOOR TORQUE TUBE (IN AIRFRAME). ACCOMPLISHED RIGGING OF DOOR. DOOR OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200725 19990402 00725 NM 1999 4 2 99ZZZM219 1 19990220 A 5210 65907373416 TQ TUBE BOEING 737 7374B7 1384702 NM CABIN DAMAGED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 449US 24893 MCO - FLT 1148 - AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMB-OUT FROM MCO. THE FORWARD MAIN ENTRY DOOR DID NOT APPEAR TO BE CLOSED PROPERLY, RESULTING IN A LARGE AIR LEAK. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT . NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR AND THE FORWARD ENTRY DOOR TORQUE TUBE (IN AIRFRAME). ACCOMPLISHED RIGGING OF DOOR. DOOR OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200726 19990402 00726 NM 1999 4 2 USAA990080 1 19990212 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 411US 30775 23880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION BS 986 FLOORBEAM UPPER T-CAP BETWEEN LLBL 29 AND RLBL 29. COR ROSION TASK NR C53-107-02. REPAIRED PER TR 53-60-01. (M) 2 L 7 2 4F RT A16WE 1999040200727 19990402 00727 EU 1999 4 2 RAIA990317 1 19990311 A 5330 S53172101202 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 425TE 125 DURING SCHEDULED MAINTENANCE, FOUND DENT IN RIGHT AFT FUSELAGE. MAINTENANCE REPAIRED DENT IAW EO NR ATR42-53-007-1. (M ) 2 H 7 2 4T RT A53EU 1999040200728 19990402 00728 EU 1999 4 2 RAIA990315 1 19990311 A 5230 DEPRESSOR AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 425TE 125 DURING SCHEDULED MAINTENANCE, FOUND CARGO DOOR SEAL DEPRESSOR DAMAGED. MAINTENANCE REPAIRED DAMAGE IAW EO NR ATR42-53-0 07-1. (M) 2 H 7 2 4T RT A53EU 1999040200729 19990402 00729 EU 1999 4 2 RAIA990304 1 19990306 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 558HK 6939 41071 FLT 7461 - BHM - MAIN CARGO BAY SMOKE LIGHT ILLUMINATED. MAINTENANCE REPLACED MAIN CARGO BAY SMOKE DETECTOR. (M) 2 L 7 2 4T RT A41NM 1999040200730 19990402 00730 EU 1999 4 2 RAIA990318 1 19990303 A 7931 1241012 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 571HK 41090 FLT 7649 - JFK - LEFT ENGINE OIL PRESSUR GAUGE FLUCTUATES. MAINTENANCE REPLACED LEFT ENGINE OIL PRESS TRANSDUCER. (M) 2 L 7 2 4T RT A41NM 1999040200731 19990402 00731 1999 4 2 RAIA990319 4 19990312 A 3442 MI5853505 RADAR AEROSP ATR42 ATR42300 8680920 EU FUSELAGE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 424TE 124 FLT 7009 - STL - WEATHER RADAR INOPERATIVE. MAINTENANCE REPLACED RADAR R/T. (M) 2 H 7 2 4T RT A53EU 1999040200732 19990402 00732 1999 4 2 99ZZZM220 3 19990309 A 6140 8975427 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT PROP INOPERATIVE A MEJA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 17 368AE 1574 AC696 DURING TAKEOFF AT LCH, THE RIGHT BETA LIGHT REMAINED ILLUMINATED AND THE TAKEOFF WAS ABORTED. MAINTENANCE INSTALLED A N EW BETA PRESSURE SWITCH. OPERATIONS AND LEAK CHECK WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1999040200733 19990402 00733 EU 1999 4 2 SIMA990682 1 19990309 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-1 INSPECTION, FOUND RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS GOUGED. LEFT AFT INBOARD AND OUTBOARD, AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200734 19990402 00734 EU 1999 4 2 99ZZZM221 1 19990309 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-1 INSPECTION, FOUND RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS GOUGED. LEFT AFT INBOARD AND OUTBOARD, AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200735 19990402 00735 EU 1999 4 2 99ZZZM222 1 19990309 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-1 INSPECTION, FOUND RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS GOUGED. LEFT AFT INBOARD AND OUTBOARD, AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200736 19990402 00736 EU 1999 4 2 99ZZZM223 1 19990309 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-1 INSPECTION, FOUND RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS GOUGED. LEFT AFT INBOARD AND OUTBOARD, AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200737 19990402 00737 EU 1999 4 2 99ZZZM224 1 19990309 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN GOUGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-1 INSPECTION, FOUND RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS GOUGED. LEFT AFT INBOARD AND OUTBOARD, AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200738 19990402 00738 EU 1999 4 2 SIMA990681 1 19990309 A 5330 S5337132120005 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURIGN MBV-2 INSPECTION, FOUND A DENT IN THE LEFT SIDE OF THE FUSELAGE BELOW THE CARGO DOOR, BETWEEN FRAMES 14 AND 15 AT STRINGER 17. THE DENT MEASURED 1 INCH LONG BY .25 WIDE BY .040 DEEP. MAINTENANCE REPAIRED THE DENT IAW SRM 53-0 0-00. AIRCRAFT RETURNED TO SERVICE (M) 2 H 7 2 4T RT A53EU 1999040200739 19990402 00739 EU 1999 4 2 SIMA990675 1 19990308 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU PASSENGER DOOR INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 249AT 11507 0249 ORD - EMERGENCY EXIT LIGHT OVER LEFT FORWARD DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY AT 15WL.. OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200740 19990402 00740 EU 1999 4 2 SIMA990674 1 19990308 A 3350 6013211 BATTERY PACKS SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 354SB 20520 340B354 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE WITH MORNING PREFLIGHT CHECK. REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999040200741 19990402 00741 EU 1999 4 2 99ZZZM225 1 19990308 A 3350 6013211 BATTERY PACKS SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 354SB 17451 340B354 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE WITH MORNING PREFLIGHT CHECK. REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999040200742 19990402 00742 EU 1999 4 2 99ZZZM226 1 19990308 A 3350 6013211 BATTERY PACKS SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 354SB 17014 340B354 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE WITH MORNING PREFLIGHT CHECK. REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999040200743 19990402 00743 EU 1999 4 2 99ZZZM227 1 19990308 A 3350 6013211 BATTERY PACKS SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 354SB 17623 340B354 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE WITH MORNING PREFLIGHT CHECK. REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999040200744 19990402 00744 EU 1999 4 2 99ZZZM228 1 19990308 A 3350 6013211 BATTERY PACKS SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 354SB 17507 340B354 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE WITH MORNING PREFLIGHT CHECK. REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999040200745 19990402 00745 EU 1999 4 2 SIMA990683 1 19990309 A 3350 301160 SIGN AEROSP ATR42 ATR42300 8680920 EU PAX DOOR FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 223AT 223 ORD - FLT 4153 - EMERGENCY EXIT SIGN AT MAIN CABIN DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED EXIT SIGN. OPERATION AL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200746 19990402 00746 EU 1999 4 2 SIMA990591 1 19990228 A 3350 2LA00511520 SOCKET SAAB SF340 340B 7860101 EU ROW 6A FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 382AE 340B382 DFW - FLT 3812 - SEAT 6A EMERGENCY FLOOR LIGHT DOES NOT ILLUMINATE, ISSUED MEL. REMOVED AND REPLACED EMERGENCY FLOOR LI GHT SOCKET AT SEAT 6A. MEL ITEM WAS RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999040200747 19990402 00747 SO 1999 4 2 SIMA990532 1 19990222 A 2612 M8353613008L RELAY EMB 145 EMB145LR SO E/E COMPT FAILED A SIMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 21 602AE 145048 MKE - FLT 4300 - ON CLIMB-OUT, HAD BAGGAGE SMOKE DETECTION WARNING. DISCHARGED NR 1 FIRE EXTINGUISHER. DECLARED EMERGE NCY. LANDED SAFELY. DETERMINED TO BE A FALSE WARNING. SYSTEM DEFERRED PER MEL 26-13 AND 26-15. DURING THE WEEKEND OF 3/5-7, A RELAY WAS REPLACED. THE MEL ITEM WAS RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999040200748 19990402 00748 EU 1999 4 2 SIMA990644 1 19990305 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AT 18437 327 SAW - DURING PS-2 INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY PACK AT 18WL HAD A BROKEN TAB. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200749 19990402 00749 EU 1999 4 2 SIMA990433 1 19990212 A 3350 3012500 COVER AEROSP ATR72 ATR72212 EU CABIN MISSING A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 498AT 498 DFW - FLT 3651 - EXIT LIGHT COVER MISSING AT PASSENGER DOOR ENTRANCE. INSTALLED EXIT LIGHT COVER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040200750 19990402 00750 EU 1999 4 2 SIMA990396 1 19990208 A 3350 52113091111 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 270AT 270 MIA - FLT 5672 - ONE FLOOR PROXIMITY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999040200751 19990402 00751 WP 1999 4 2 ORJA99107 1 19990304 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 25-28 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAX, EMERGENCY EXI TLIGHTS ON AT ROWS 25, 26, 27, 28. REPLACED BATTERY PACK WITH SPARE IN AFT STAIRWELL. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999040200752 19990402 00752 NM 1999 4 2 USAASB99065 1 19990306 A 5270 AN32101 SWITCH BOEING 737 737301 1384611 NM ACCESS DOOR MALFUNCTIONED A USAA A UNSCHED LANDING L NO TEST TO TAKEOFF 1 EA 19 336US 23233 BWI - FLT 218, ON TAKEOFF, CAPT HEAD A LOUD NOISE AND WAS UNABLE TO PRESSURIZE THE AIRCRAFT. AT ABOUT 10,000 FT, CREW E LECTED TO RETURN TO FIELD AT BWI WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MX FOUND THE FOR WARD ACCESS DOOR IMPROPERLY SECURED AND THE DOOR WARNING LIGHT INOP. MAINTENANCE SECURED DOOR AND PLACED DOOR WARNING L IGHT ON MEL. ON 3-9-99, MAINTENANCE FOUND THE FORWARD ACCESS DOOR SWITCH S196 OPERATING MECHANISM STICKING. CLEANED AN D LUBRICATED MECHANISM. DOOR WARNING SYSTEM OPS CHECKS GOOD. CLEARED MEL. (M) 2 L 7 2 4F RT A16WE 1999040200753 19990402 00753 NM 1999 4 2 USAASB99064 1 19990306 A 2150 3219421 SHUTOFF VALVE BOEING 737 7373B7 1384580 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 505AU 23380 CLT - FLT 8054 - SHORTLY AFTER TAKEOFF, THE CREW NOTICED A BANGING NOISE COMING FROM THE LEFT PACK. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK 35 DEGREE SHUTOFF VALV E AND THE TEMPERATURE CONTROL BOX. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200754 19990402 00754 NM 1999 4 2 99ZZZM229 1 19990306 A 2150 6075103 CONTROL BOX BOEING 737 7373B7 1384580 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 505AU 23380 CLT - FLT 8054 - SHORTLY AFTER TAKEOFF, THE CREW NOTICED A BANGING NOISE COMING FROM THE LEFT PACK. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK 35 DEGREE SHUTOFF VALV E AND THE TEMPERATURE CONTROL BOX. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200755 19990402 00755 NM 1999 4 2 USAASB99058 1 19990227 A 2820 COUPLING BOEING 737 7373B7 1384580 NM FUEL SYSTEM LEAKING A USAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 371US 22950 BOS - FLT 2673 - SHORTLY AFTER TAKEOFF, TOWER NOTIFIED CAPTAIN THAT FUEL WAS VENTING/LEAKING OUT OF THE RIGHT WING. TOW ER NOTED THAT SEVERAL AIRCRAFT HAD REPORTED THE SAME. AT THE SAME TIME, THE CALL BELL IN THE AIRCRAFT WAS GOING OFF, AS PASSENGERS ALSO REPORTED SEEING FUEL LEAKING FROM THE WING. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT INCIDEN T. FLIGHT TAXIED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE REPAIRED A FUEL LINE COUPLING IN THE RIGHT WING TANK. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200756 19990402 00756 NM 1999 4 2 USAA990179 1 19990224 A 5230 6547952524M SKIN BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 38270 23379 CLT - HFEC FOUND A .3 INCH CRACK OUTER SKIN AT AFT UPPER CARGO DOOR HANDLE CUTOUT. INSTALLED REP DOUBLER PER EA NR 6389 5. CARGO DOOR RETURNED TO STOCK. (M) 2 L 7 2 4F RT A16WE 1999040200757 19990402 00757 NM 1999 4 2 USAA990102 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FUOND A CRACK RADIATING FROM RIVET HEAD BS 787 LB 8 LS 9 SUPPORT FRAME. INSTA LLED REPAIR ANGLE PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200758 19990402 00758 NM 1999 4 2 USAA990101 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 847 BETWEEN LS 8 AND LS 9 SUPP ORT FRAME. REPAIRED PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200759 19990402 00759 NM 1999 4 2 USAA990100 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURNIG Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD HOLE AREA STATIO N727 CABIN SIDEWALL B ETWEEN LS 8 AND LS 9 SUPPORT FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200760 19990402 00760 NM 1999 4 2 USAA990099 1 19990226 A 5312 BULKHEAD SKIN BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STATION 178 BULKHEAD SKIN LBL 1 WL 205.5. INSTALLED R EPAIR DOUBLER PER TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999040200761 19990402 00761 NM 1999 4 2 USAA990098 1 19990226 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 188/178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 18 AND STATION 178 SHEAR ANGLE AT RBL 29 WL 195. INSTALLED NEW ANGLE PER SRM 53-10-08 DRAWING 6-72038. (M) 2 L 7 2 4F RT A16WE 1999040200762 19990402 00762 NM 1999 4 2 USAA990097 1 19990226 A 5312 BLKHD STIFFENER BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 178 BULKHEAD VERTICAL STIFFENER INBOARD FLANGE LB L 5.5 WL 184. FABRICATED REPAIR ANGLE AND STRAP PER SRM 53-10-08 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999040200763 19990402 00763 NM 1999 4 2 USAA990096 1 19990226 A 5312 BLKHD STIFFENER BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 178 BULKHEAD VERTICAL STIFFENER OUTBOARD FLANGE LBL 6 WL 184. FABRICATED REPAIR ANGLE AND STRAP PER SRM 53-10-08 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999040200764 19990402 00764 NM 1999 4 2 USAA990095 1 19990226 A 5312 BULKHEAD SKIN BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK STATION 178 BULKHEAD/SKIN LBL 4.75 WL 201. INSTALLED D OUBLER PER TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999040200765 19990402 00765 NM 1999 4 2 USAA990103 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 827 BETWEEN LS 8 AND LS 9 SUPP ORT FRAME. INSTALLED REPAIR ANGLE PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200766 19990402 00766 NM 1999 4 2 USAA990104 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK FROM FASTENER HOLE STATION 616 FRAME INBOARD BOTTOM CHO RD ANGLE. INSTALLED DOUBLER PER EA 63678. (M) 2 L 7 2 4F RT A16WE 1999040200767 19990402 00767 NM 1999 4 2 USAA990124 1 19990226 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FUOND A 1 INCH CRACK AFT END ANTENNA MOUNT FUSELAGE SKIN BOTTOM CENTER STATION 727 BL 0 . FABRICATED FILLER AND DOUBLER REPAIR PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999040200768 19990402 00768 NM 1999 4 2 USAA990125 1 19990226 A 5321 FLOOR PANEL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CORROSION AREA FLOOR PANEL UNDER LEFT LAV TOILET TANK. INSTALLED REPA IR FLOOR PANEL PER SRM 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999040200769 19990402 00769 NM 1999 4 2 USAA990126 1 19990226 A 5320 652981854 ANGLE BOEING 737 737301 1384611 NM BS 350 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CORROSION AREA A NUTPLATE HOLE BS 350 LBL 64 SUPPORT ANGLE. REPAIRED PER SRM 51-00-00 AND BOEING DRAWING 65-29818. (M) 2 L 7 2 4F RT A16WE 1999040200770 19990402 00770 NM 1999 4 2 USAA990127 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 807 BETWEEN LS 8 AND LS 9 SUPP ORT FRAME. INSTALLED DOUBLER PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200771 19990402 00771 NM 1999 4 2 USAA990128 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 440 BETWEEN LS 8 AND LS 9 SUPP ORT FRAME. INSTALLED DOUBLER PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200772 19990402 00772 NM 1999 4 2 USAA990129 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 400 BETWEEN LS 8 AND LS 9 SUPP ORT FRAME. INSTALLED DOUBLER PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200773 19990402 00773 NM 1999 4 2 USAA990130 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 887 BETWEEN LS 8 AND LS 9 SUPP ORT FRAME. INSTALLED DOUBLER PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200774 19990402 00774 NM 1999 4 2 USAA990131 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 847 BETWEEN RS 8 AND RS 9 SUPP ORT FRAME. INSTALLED DOUBLER PER EA 63769. (M) 2 L 7 2 4F RT A16WE 1999040200775 19990402 00775 NM 1999 4 2 USAA990133 1 19990226 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 17 INCH CORROSION AREA AROUND SCREW HOLES BS 344 RBL 2 LBL 15 FLOORBEA M. CORROSION TASK NR C53-107-02. INSTALLED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999040200776 19990402 00776 NM 1999 4 2 USAA990134 1 19990226 A 5311 FRAME BOEING 737 737301 1384611 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 558AU 39281 23512 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK RADIATING FROM RIVET HEAD STATION 827 RS 8 RS 9 FRAME SUPPORT. I NSTALLED REPAIR PER EA 63769 AND SRM 53-30-07. (M) 2 L 7 2 4F RT A16WE 1999040200777 19990402 00777 NM 1999 4 2 USAA039902 1 19990309 A 2170 22D10 COALESCER BOEING 727 727254 138408L NM RT PACK DIRTY A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 913TS 20250 FLT 6161 - BOS-LGA - ON APPROACH, FLIGHT ATTENDANTS REPORT A BURNING SMELL IN FORWARD CABIN BY L1 DOOR. SMELL WAS BURNI NG PLASTIC OR WAX LIKE ORDER. TROUBLESHOT SMELL TO DEICING/ANTI-ICING FLUID IN RIGHT PACK SYSTEM. REPLACED RIGHT WATER SEPARATOR BAG PER MM 21-55-51. AIRATED CABIN FOR SEVERAL HRS, CHECK OK. (M) 2 L 7 3 4F A3WE 1999040200778 19990402 00778 WP 1999 4 2 USAAD99038 1 19990305 A 2130 591024349 DUCT DOUG DC9 DC981 3022081 WP AC BAY LEAKING A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 804US 48052 PHL-FLL - FLT 803 - WHLE CRUISING AT 35,000 FT THE AIRCRAFT LOST PRESSURIZATION AND THE OXYGEN MASKS DEPLOYED. THE AIRC RAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED DEBRIS FROM THE AFT PRESSURE RELIEF VALVE AND REP LACED THE GROUND AIR CHECK VALVE. (M) 2 L 7 2 4F A6WE 1999040200779 19990402 00779 NE 1999 4 2 USAABB99009 2 19990303 A 7230 COMPRESSOR BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN C E M F.O.D. VIBRATION/BUFFET OVER TEMP CL CLIMB 1 EA 19 607AU 22203 30557 PIT - FLT 534 - AFTER DEPARTURE, AT 3000 FEET AGL, SEVERE VIBRATIONS WERE FELT FROM THE RIGHT SIDE OF THE AIRCRAFT. THE RIGHT ENGINE EGT WAS IN THE RED ZONE. CREW SHUT DOWN RIGHT ENGINE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT A LOW COMPRESSOR ANNULUS FILLER HAD CRACKED AND WAS LIBERATED FROM ITS POSITION. THE RIGHT ENGINE WAS REPLACED. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1999040200780 19990402 00780 NM 1999 4 2 USAABB99012 1 19990306 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 DCA - FOUND R3 DOOR EMERGENCY EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 1999040200781 19990402 00781 NM 1999 4 2 USAABB99011 1 19990226 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM PAX DOOR MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 610AU 27122 LAX - FOUND THE L4 DOOR EXIT IDENTIFIER WOULD NOT TURN OFF. MAINTENANCE REPLACED THE EXIT IDENTIFIER. (M) 2 L 7 2 4F RT A2NM 1999040200782 19990402 00782 NM 1999 4 2 USAASB99053 1 19990224 A 5210 90100722 SNUBBER BOEING 737 7373B7 1384580 NM PAX DOOR MISINSTALLED A USAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 19 395US 17983 23317 TPA - FLT1795 - CAPTAIN REPORTED THAT DURING CLIMB-OUT FROM PBI, AN UNCOMFORTABLY LOUD NOISE WAS COMING FROM THE FORWARD ENTRY DOOR AREA. PRESSURIZATION AS NORMAL BUT A DECISION WAS MADE TO DIVERT TO TPA DUE TO EXCESSIVE NOISE. FLIGHT LAN DED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. IT WAS REPORTED THAT THE FORWARD ENTRY DOOR WAS PREVIOUSLY WO RKED ON THE DAY BEFORE FOR CLOSING TO QUICKLY (NO SNUBBER ACTION TO SLOW CLOSING OF DOOR). MAINTENANCE FOUND THE SNUBBE R FOR THE FORWARD ENTRY DOOR INSTALLED BACKWARDS. REPOSITIONED SNUBBER CORRECTLY. DOOR OPERATION NORMAL. NO PRESSURE LEAKS NOTED. (M) 2 L 7 2 4F RT A16WE 1999040200783 19990402 00783 NM 1999 4 2 USAASB99051 1 19990223 A 5610 5893543110 WINDSHIELD BOEING 737 7373B7 1384580 NM RT COCKPIT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 376US 14576 22955 BOS - FLT 1665 - ON CLIMB-OUT FROM PWM, AT FL190, THE FIRST OFFICERS WINDSHIELD SHATTERED. CAPTAIN DECLARED AN EMERGENC Y AND THE FLIGHT DIVERTED TO BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. PRIOR TO THE WINDSHIE LD SHATTERING, THE CREW NOTICED AN ELECTRICAL ARE AT THE TOP OF THE WINDSHIELD. MAINTENANCE REMOVED AND REPLACED THE FI RST OFFICERS WINDSHIELD PER JOB PROCEDURE CARD. ALSO, REPLACED THE RIGHT FORWARD WINDSHIELD HEAT CONTROL BOX (P/N 83000 -05602). OPERATIONAL CHECK OF WINDOW HEAT CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1999040200784 19990402 00784 WP 1999 4 2 USAAD99039 1 19990308 A 3350 41B030F00101 BATTERY DOUG DC9 DC931 3022065 WP CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 920VJ 48140 IND - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999040200785 19990402 00785 CE 1999 4 2 C2XA99CL017 1 19990214 A 6123 MS250851 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT OUT OF ADJUST A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 38537 UE158 CLE - FLT 4399 - CREW REPORTED THAT THE AUTO-FEATHER DISABLED AT 700 FEET WITH ENGINES AT FULL POWER AND IT FAILED TO RE -ARM. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE AUTOFEATHER POWER SWITCHES IAW B1900 MM 61-21-02, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1999040200786 19990402 00786 SO 1999 4 2 C2XA99IA162 1 19990216 A 5753 12040327007 SKIN EMB 120 EMB120RT SO RT TE FLAP WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP RIVETS PULLING THROUGH LOWER SKIN. FABRICATED A ND INSTALLED REPAIR DOUBLER IAW SRM 54-20-01 AND INSTALLED IAW SRM 51-40-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1999040200787 19990402 00787 SO 1999 4 2 C2XA99IA160 1 19990216 A 5411 12039761001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME CRACKED ON COWL FLANGE FOR PANEL 414. WELDED CR ACKED AREA IAW MIL-STD-2219, NDT PENETRANT REVEALS NO CRACK EXISTS AFTER REPAIR. AIRCRAFT APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1999040200788 19990402 00788 SO 1999 4 2 C2XA99IA159 1 19990216 A 5330 1202656031 SKIN EMB 120 EMB120RT SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED BELOW GPU RECEPTACLE DOOR. REMOVED DAMAGED, F ABRICATED FILLER AND DOUBLER REPAIR AND INSTALLED IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040200807 19990402 00807 NE 1999 4 2 99ZZZX1360 2 19990301 A 7310 299CU11P117 O RING GE LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE FUEL SYSTEM LEAKING A KKFA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 23 500JS 25020 249042A WHILE EN ROUTE, FLIGHT CREW NOTICED LT RPM FLUCTUATION. ADJUSTMENT OF POWER LEVER ONLY REDUCED RPM. ENGINE POWER WAS L OST. CREW ELECTED TO DIVERT TO TYS AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A FUEL LEAK AT A DEFECTIVE O- RING FITTING ON THE MAIN FUEL LINE. O-RING WAS REPLACED AND THE ENGINE PERFORMANCE RUN WAS SATISFACTORY. 2 L 7 2 4J 4 J A10CE 1E16 1999040200825 19990402 00825 CE 1999 4 2 99ZZZX1378 1 19990219 A 5533 1156400001 RIB BEECH 99 B99 1154004 CE VERTICAL STAB CRACKED A A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA 33008 US127 THE RUDDER HINGE BRACKETS ON THE RUDDER BECAME LOOSE WHICH APPARENTLY CAUSED A CRACK TO DEVELOP IN THE AFT/LEFT CORNER O F THE END (TOP) RIB OF THE VERTICAL STABILIZER. ALSO, WAS LOSING SOME OF THE RIVETS IN THE VERTICAL STABILIZER SPAR AT THE TOP HINGE ATTACH FITTING. 1 L 7 2 3T A14CE 1999040200834 19990402 00834 NM 1999 4 2 AT9900271 1 19990326 A 3350 216179 BATTERY BOEING 737 7372L9 1384497 NM L1 DOOR DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 L-1 DOOR PORTABLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED BATTERIES IN L-1 DOOR PORTABLE EMERGENCY LIGHT, OPS CH ECKED GOOD REF B737 33-51-101. 2 L 7 2 4F RT A16WE 1999040200835 19990402 00835 EU 1999 4 2 MALA976409 1 19990326 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU LT NACELLE FAILED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 31XJ 031 LEFT ENGINE FIRE WARNING CAME ON DURING TAXI THEN WENT OUT, THEN CAME BACK ON AGAIN, WENT OUT DURING TAXI BACK TO HANGER . MAINTENANCE REPLACED FIRE DETECTION LOOP IAW AMM 26-11-05, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999040200836 19990402 00836 EU 1999 4 2 MALA976410 1 19990329 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING INSPECTION 4C, EMERGENCY LIGHT INOP. REPLACED LAMP, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999040200837 19990402 00837 EU 1999 4 2 MALA976411 1 19990328 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU LT INTAKE DEICE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 416XJ 416 EN ROUTE TO MSP FROM MLI, LEFT INTAKE HEAT FAILED. LIGHT CONTINUED TO CYCLE, TURNED SWITCH TO OFF POSITION. MSP HAD RE PORTS OF ICE IN CLOUDS AND ALSO OVERCAST. AIRCRAFT DIVERTED TO ALO. MAINTENANCE REPLACED LEFT INTAKE HEAT DEICE MODULE . PERFORMED OPS CHECK OF LT INTAKE HEAT SYSTEM FOR 30 MINUTES. NO DEFECTS NOTED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999040200838 19990402 00838 EU 1999 4 2 MALA976412 1 19990327 A 3610 46000200 SEALS BAC 146 AVRO146RJ85A 1500097 EU NR 4 ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 513XJ E2329 RIGHT ZONE HI TEMP LIGHT CAME ON DURING CLIMBOUT FROM MSP. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED PERI SEALS O /B OF ENGINE NR 4, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1999040200839 19990402 00839 EU 1999 4 2 MALA976413 1 19990327 A 3260 7232000631 SWITCH SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 424XJ 424 LANDING GEAR WOULD NOT COME DOWN, GOT INTRANSIT LIGHT BUT NO GEAR DOWN INDICATION. LANDING GEAR CONTROL BREAKER POPPED. PERFORMED EMERGENCY GEAR EXTENSION, GEAR CAME DOWN WITH 3 GREENS. UPON LANDING IN DTW, NO NOSE WHEEL STEERING. MAINT ENANCE INSPECTED LANDING GEAR, FOUND CB F-7 POPPED. RESET CB, TAPED UP MAIN GEAR DOOR AND INSTALLED ALL THREE LANDING G EAR PINS, OPS CHECKING NOSE STEERING SYSTEM, OPERATES NORMALLY. MAINTENANCE REPLACED SWITCH 5GB. ALL NECESSARY OPS CHE CK GOOD IAW SF340 AMM. 2 L 7 2 4T RT A52EU 1999040200840 19990402 00840 NM 1999 4 2 RAAA99B2023 1 19990330 A 5311 FRAME BOEING 727 72722C 138400F NM BS 580 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND CRACK IN PREVIOUS REPAIR DOUBLER AT BS 580 FRAME WL 209 RT. REPLACED CRACKED DOUBLER IA W SRM 53-10-4 F 1 M54 NR 345. 2 L 7 3 4F A3WE 1999040200841 19990402 00841 NM 1999 4 2 RAAA99B2025 1 19990330 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 344 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND BS 344 FLOORBEAM FORWARD FLANGE CORRODED AT RBL 44 THRU 64. REPLACED BEAM UPPER CHORD B ETWEEN RBL 68 AND LBL 33 IAW SRM 53-10-8 FIG 9 M54 NR 368. 2 L 7 3 4F A3WE 1999040200842 19990402 00842 NM 1999 4 2 RAAA99B2026 1 19990330 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 303-315 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND CORROSION ON FLOORBEAM SUPPORT STRUCTURE AROUND FORWARD LAV DUMP PIPE BS 303 TO 315 RT. REMOVED SUPPORT ANGLES, FABRICATED SUPPORT ANGLES 7075T6 .094 IAW SRM 51-10-2. TREATED AND PRIMED IAW SRM 51-10-06. I NSTALLED ANGLES IAW SRM 51-30-02 M54 NR 417. 2 L 7 3 4F A3WE 1999040200843 19990402 00843 NM 1999 4 2 CALA9900339 1 19990330 A 5320 ANGLE BOEING 757 757224 1384958 NM BS 1376-1443 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND AFT HOLD THRESHOLD ATTACHMENT ANGLE CORRODED AT BS 1376.5 TO 1443.5. THE ATTACHMENT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 53-60-53. 2 L 7 2 4F RT A2NM 1999040200844 19990402 00844 WP 1999 4 2 CALA9900340 1 19990330 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR LOWER FORWARD STOP SUPPORT ANGLE BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1999040200845 19990402 00845 WP 1999 4 2 CALA9900341 1 19990330 A 5210 BEAM DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51 -30-5. 2 L 7 2 4F A6WE 1999040200846 19990402 00846 WP 1999 4 2 CALA9900342 1 19990330 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 503 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 2.5 INCH CRACK IN FRAME AT L6L AND A 2.5 INCH CRACK WAS FOUND IN FRAME AT L6R, STA 503. THE FRAME WA S REMOVED AND REPLACED IAW SRM 53-03, FIGURE 32. 2 L 7 2 4F A6WE 1999040200847 19990402 00847 WP 1999 4 2 UPS99829149 1 19990328 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C3, FS 55 FRAME AT LONG 24R IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040200848 19990402 00848 EU 1999 4 2 QXEA9900542 1 19990329 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU ROW 8AB INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 490US 11152 SEA- 1 SECTION OF ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE CORRECTED DEFECTIVE WIRING AT SEAT 8 A AND B. OPERATION AL TEST NORMAL. 2 L 7 2 4F RT A20EU 1999040200849 19990402 00849 EU 1999 4 2 99FDEA00127 1 19990331 A 3260 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 654FE 738 ON GEAR RETRACT AT SJC, GOT AMBER DOOR OPEN LIGHT ECAM. ALSO, CONFIRMED SAME. BOTH SYS AGREED WITH AMBER LIGHTS. 2 L 7 2 4F RT A35EU 1999040200850 19990402 00850 WP 1999 4 2 ABXA9900264 1 19990322 A 5315 99223951 FLOORBEAM DOUG DOUG DC9 DC933F 302207A WP BS 313 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND FLOORBEAM AT STATION 313 EXFOLIATED FROM BL 0 TO LBL 14. REPAIRED IAW REA D953-27121MR. 2 L 7 2 4F A6WE 1999040200851 19990402 00851 WP 1999 4 2 ABXA9900265 1 19990322 A 5320 39204051 SPLICE DOUG DOUG DC9 DC933F 302207A WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND OUTBOARD FLOORBEAM TO FRAME SPLICE CORRODED AT STATION 965 LEFT. REPLACED SPLICE FITTING IAW DC9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 1999040200852 19990402 00852 WP 1999 4 2 ABXA9900266 1 19990322 A 2780 3920511510 FITTING DOUG DOUG DC9 DC933F 302207A WP RT LE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND RIGHT WING INBOARD SLAT PULLEY ATTACH BRACKET CRACKED. REPLACED SUPPORT FITTING IAW DC9 SRM 51-10 -4 AND 51-30-5. 2 L 7 2 4F A6WE 1999040200853 19990402 00853 WP 1999 4 2 ABXA9900267 1 19990322 A 5210 9921687 BRACKET DOUG DOUG DC9 DC933F 302207A WP PASSENGER DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND BRACKET CRACKED IN UPPER FORWARD CORNER OF MAIN CARGO DOOR. REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999040200854 19990402 00854 WP 1999 4 2 ABXA9900268 1 19990322 A 2750 39208192 SUPPORT DOUG DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING C-CHECK, FOUND RIGHT FLAP CARRIAGE OSCILLATING ROLLER SUPPORT CRACKED. REPLACED SUPPORT IAW DC9 OHM 27-50-7. 2 L 7 2 4F A6WE 1999040200855 19990402 00855 WP 1999 4 2 DHL9980501C 1 19990107 A 5753 COVER DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT WING I/B FLAP END HAS TWO CRACKS AT FRAME SUPPORT OF SCISSORS COVER. STOP DRILLED CRACKS, FABRICATED AN GLE REPAIR AND INSTALLED PER SRM 51-1-21. N/R 1224. 2 L 7 4 4F RT 4A25 1999040200856 19990402 00856 WP 1999 4 2 DHL9980502C 1 19990201 A 5522 SKIN DOUG DC8 DC873F 302199F WP LEFT ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT ELEVATOR UPPER SURFACE FROM STA XE 39 TO XE 55 FOUND OILCAN SKIN. REMOVED DAMAGED SECTION OF SKIN, FAB RICATED AND INSTALLED NEW SKIN AND FILLER PER EO MHA-3119. 2 L 7 4 4F RT 4A25 1999040200857 19990402 00857 WP 1999 4 2 DHL9980503C 1 19990201 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP RIGHT COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, CO-PILOT FWD I/B SEAT TRACK BENT AND CRACKED. STOP DRILLED CRACK, INSTALLED REPAIR PARTS PER SRM 51-1-8. N /R 1196. 2 L 7 4 4F RT 4A25 1999040200858 19990402 00858 WP 1999 4 2 DHL9980504C 1 19990105 A 5753 BRACKET DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, O/B FLAP HINGE SUPPORT BRACKET XW 410 HAS CRACK. REMOVED, FABRICATED AND INSTALLED SUPPORT BRACKET PER SRM 51-1-21, 2 X 6 N/R 1204. 2 L 7 4 4F RT 4A25 1999040200859 19990402 00859 WP 1999 4 2 DHL9980505C 1 19990107 A 5520 COVER DOUG DC8 DC873F 302199F WP RIGHT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT ELEVATOR HINGE COVER CRACKED. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER PER SRM 51-1-8. N/R 1177. 2 L 7 4 4F RT 4A25 1999040200860 19990402 00860 WP 1999 4 2 DHL9980506C 1 19990107 A 5753 PANEL DOUG DC8 DC873F 302199F WP LT TE FLAP BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT O/B FLAP O/B CORNER BENT AND CRACKED. REMOVED DAMAGED T/E PANEL, FABRICATED NEW T/E SECTION PER SRM 51 -1-8, 39 X 8 N/R 1178. 2 L 7 4 4F RT 4A25 1999040200861 19990402 00861 WP 1999 4 2 DHL9980507C 1 19990201 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 240 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, MAIN CARGO COMPARTMENT STA 240 INTERCOSTAL CUSP LINE CRACK. CUT OUT DAMAGED AREA OF FRAME FROM FS 240 BETWE EN L21R THROUGH 19R AND FABRICATED NEW FRAME PER EO MHA 3117, 4 X 9 N/R 1123. 2 L 7 4 4F RT 4A25 1999040200862 19990402 00862 WP 1999 4 2 DHL9980508C 1 19990201 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 220 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, MAIN CARGO COMPT FS 220 INTERCOSTAL AT CUSP LINE AREA HAS A CRACK. CUT OUT DAMAGED SECTION OF FRAME BETWEEN L21R THROUGH L19R AND FABRICATED PER EO MHA-3118 AND FABRICATED SPLICE AND ANGLE. INSTALLED REPAIR PARTS 4 X 9. N/R 1124. 2 L 7 4 4F RT 4A25 1999040200863 19990402 00863 WP 1999 4 2 DHL9980509C 1 19990125 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, C-3 DOOR EXTERIOR LOWER SURFACE SHOWS DAMAGE TO THE LEADING EDGE AREA. CUT OUT DAMAGED AREA, INSTALLED NEW SKIN AND SPLICE PER SRM 51-1-21, 54 X 6. N/R 1117 2 L 7 4 4F RT 4A25 1999040200864 19990402 00864 WP 1999 4 2 DHL9980510C 1 19990201 A 5540 WEB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RUDDER L/E AT STA ZR 159 HAS DAMPER HOUSING CRACKED. REMOVED CRACKED WEB, FABRICATED REPAIR PARTS AND INST ALLED PER SRM 51-1-21 AND DRAWING NR MHA 3115. N/R 1071 2 L 7 4 4F RT 4A25 1999040200865 19990402 00865 WP 1999 4 2 DHL9980511C 1 19990207 A 5755 PANEL DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING NR 5 SPOILER HAS PANEL DELAMINATED. REMOVED AND REPLACED PANEL PER MM 27-60-0. N/R 1330 2 L 7 4 4F RT 4A25 1999040200866 19990402 00866 WP 1999 4 2 DHL9980512C 1 19990128 A 5522 SKIN DOUG DC8 DC873F 302199F WP LEFT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT ELEVATOR UPPER O/B SKIN XE 297 FASTENER TOO HIGH. CUT OUT CRACKED SECTION OF SKIN BETWEEN STA XE 246 T O XH 285. FABRICATED NEW SECTION AND INSTALLED NEW SECTION OF SKIN PER SRM 51-1-21. N/R 1044 2 L 7 4 4F RT 4A25 1999040200867 19990402 00867 WP 1999 4 2 DHL9980513C 1 19990101 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1746 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, ON EMPENNAGE LEFT SIDE AT STA 1746 ZT 32 A CRACK ONE INCH LONG. CUT OUT CRACKED SECTION OF SKIN AND FABRIC ATED REPAIR DOUBLER PER SRM 51-1-8, 12 X 10. N/R 1045 2 L 7 4 4F RT 4A25 1999040200868 19990402 00868 WP 1999 4 2 DHL9980514C 1 19990110 A 5522 SKIN DOUG DC8 DC873F 302199F WP LEFT ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT ELEVATOR T/E OUTBOARD LOWER SIDE 24 FROM TIP FASTENERS DETERIORATED AT 48 FROM TIP FASTENERS AND PREVIOUS REPAIR LOOSE APPROX XE 270 AND 290. REMOVED DAMAGED SECTION OF T/E FROM STA XE 270 TO XH 285. FABRICATED NEW AND INS TALLED PER SRM 51-1-21. N/R 1046 2 L 7 4 4F RT 4A25 1999040200869 19990402 00869 WP 1999 4 2 DHL9980515C 1 19990108 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT WING I/B FLAP UPPER WITH 3 DENTS, 2 IN CENTER AND 1 T/E AREA. CUT OUT DAMAGED AREA AND FABRICATED REPAI R DOUBLER 2 X 2 AND FABRICATED AND REPLACED T/E AREA 40 X 7.5 PER SRM 51-1-21A. N/R 934 2 L 7 4 4F RT 4A25 1999040200870 19990402 00870 WP 1999 4 2 DHL9980516C 1 19990106 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1746 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, MCC FLOOR PANEL STA 1746 BOTTOM CHANNEL IS DETERIORATED AND HOLE CRACKED. FABRICATED DOUBLER REPAIR PER SRM 53-2-0 AND INSTALLED PER SRM 51-1-21. N/R 947 2 L 7 4 4F RT 4A25 1999040200871 19990402 00871 WP 1999 4 2 DHL9980517C 1 19990110 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1680 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT CHECK, MAIN CARGO COMPT FLOOR PANEL LT SIDE STA 1680 HAS PREVIOUS REPAIR. REMOVED COVER FROM PANEL AND CRACKED CHAN NELS AT LEFT SIDE STA 1680, FABRICATED NEW COVER (20 X 20) AND 2 CHANNELS 20 X 3 PER SRM 53-7-3. N/R 952 2 L 7 4 4F RT 4A25 1999040200874 19990402 00874 WP 1999 4 2 DHL9980520C 1 19990102 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 1160-1200 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FWD AFT LOWER CARGO COMPT BETWEEN STA 1160 TO 1200 FLOOR STRAP BROKEN. FABRICATED AND INSTALLED REPAIR SPLI CE 4 X 1.5' PER SRM 53-2-0. N/R 867 2 L 7 4 4F RT 4A25 1999040200875 19990402 00875 WP 1999 4 2 DHL9980521C 1 19990102 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 1140 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FED AFT CLOWER CARGO COMPT STA 1140 LONGERON 31R FLOOR STRAP CRACKED. STOP DRILLED CRACK, FABRICATED AND IN STALLED REPAIR DOUBLER 3 X 2. INSTALLED DOUBLER PER SRM 51-1-21. N/R 868 2 L 7 4 4F RT 4A25 1999040200876 19990402 00876 WP 1999 4 2 DHL9980522C 1 19990116 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 100 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING TRAILING AREA ON LOWER SURFACE NR 2 PANEL AT APPROX XRS 100 DELAMINATED. REMOVED, REPAIRED AND REI NSTALLED PANEL PER SRM 51-1-21. N/R 59 2 L 7 4 4F RT 4A25 1999040200877 19990402 00877 WP 1999 4 2 DHL9980523C 1 19990122 A 5730 PANEL DOUG DC8 DC873F 302199F WP RIGHT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RIGHT WING FLAP LOWER SCISSORS PANEL DELAMINATED. REMOVED AND INSTALLED SERVICEABLE PANEL PER SRM 51-3-0. N/R 60 2 L 7 4 4F RT 4A25 1999040200878 19990402 00878 WP 1999 4 2 DHL9980524C 1 19990121 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 3 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING NR 3 FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1999040200879 19990402 00879 WP 1999 4 2 DHL9980525C 1 19990110 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 2 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING NR 2 FLAP VANE DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-51-14. N/R 62 2 L 7 4 4F RT 4A25 1999040200880 19990402 00880 WP 1999 4 2 DHL9980526C 1 19990129 A 5523 TAB DOUG DC8 DC873F 302199F WP RIGHT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT ELEVATOR GEAR TAB HAS DENT AT MID SECTION OF T/E AND UPPER SURFACE. REMOVED AND INSTALLED SERVICEABLE GE AR TAB PER MM 27-30-00. N/R 50 2 L 7 4 4F RT 4A25 1999040200881 19990402 00881 WP 1999 4 2 DHL9980527C 1 19990129 A 5523 TAB DOUG DC8 DC873F 302199F WP LEFT ELEVATOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT ELEVATOR DELAMINATED ON UPPER SURFACE. REMOVED AND INSTALLED REPAIRED TAB PER MM 27-30-2. N/R 51 2 L 7 4 4F RT 4A25 1999040200882 19990402 00882 WP 1999 4 2 DHL9980528C 1 19990131 A 5752 TAB DOUG DC8 DC873F 302199F WP RIGHT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RIGHT I/B AILERON TRIM TAB DELAMINATED AT LOWER SURFACE. REMOVED TAB AND INSTALLED SERVICEABLE TAB PER MM 2 7-31-1. N/R 54 2 L 7 4 4F RT 4A25 1999040200883 19990402 00883 WP 1999 4 2 DHL9980529C 1 19990131 A 5543 TAB DOUG DC8 DC873F 302199F WP RUDDER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RUDDER TAB DELAMINATED AT LT LOWER AREA. REMOVED TAB, REPAIRED AND REPAINTED AND REBALANCED. N/R 55 2 L 7 4 4F RT 4A25 1999040200884 19990402 00884 WP 1999 4 2 DHL9980530C 1 19990114 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 47 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING T/E AREA ON LOWER SURFACE NR 1 PANEL AT STA 47 DELAMINATED. REMOVED DELAMINATED PANEL AND INSTALLED SERVICEABLE PER SRM 51-1-21. N/R 57 2 L 7 4 4F RT 4A25 1999040200885 19990402 00885 WP 1999 4 2 DHL9980531C 1 19990110 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 178 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RIGHT WING T/E ON LOWER SURFACE NR 3 PANEL AT XRS 178 DELAMINATED. REMOVED DELAMINATED WING, REPAIRED AND I NSTALLED PER SRM 51-1-21. N/R 58 2 L 7 4 4F RT 4A25 1999040200886 19990402 00886 WP 1999 4 2 DHL9980532C 1 19990113 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 69.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, COMPLETE PERMANENT REPAIR AT WING STA XCW 69.5 PER AD 88-21-01 AND S/B 57-88. RAISED LEVEL AND SHORED A/C. REMOVED FITTING 5761689 AND INSTALLED 060095-22, DOUBLER -23 AND TRIPLER -25. SEALED AREAS, LEAK CHECKED AND INSTALLED FWD SKIN SECTION PREVIOUSLY REMOVED TO FACILITATE REPAIR. TORQUED FITTING LOWER BOLTS PER SRM 51-3-0. REPAIR ACCOMPL ISHED PER DRAWING J0660095. N/R 0026 2 L 7 4 4F RT 4A25 1999040200887 19990402 00887 WP 1999 4 2 DHL9980533C 1 19990131 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 69.5 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, COMPLETE PERMANENT REPAIR AT XCW 69.5 HOLE INTERIM REPAIR. RAISED AND SHORED A/C. REMOVED FITTING, DOUBLER AND TRIPLER. INSTALLED DOUBLER, TRIPLER AND FITTING PER SRM 51-3-2. REINSTALLED STRUCTURAL COMPONENTS, SEALED ALL FAS TENERS AND LEAK CHECK AREA. INSTALLED SKIN SECTIONS PREVIOUSLY REMOVED TO FACILITATE MAINTENANCE. RETORQUED BOLTS PER SRM 51-3-0. N/R 27 2 L 7 4 4F RT 4A25 1999040200888 19990402 00888 WP 1999 4 2 DHL9980534C 1 19990128 A 3610 BRACKET DOUG DC8 DC873F 302199F WP LEFT PNEU DUCT BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT WING L/E LOWER PANEL SUPPORT BRACKET FOR PNEU DUCT BROKEN. REMOVED AND INSTALLED FABRICATED BRACKET PE R SRM 51-1-8. N/R 1416 2 L 7 4 4F RT 4A25 1999040200889 19990402 00889 WP 1999 4 2 DHL9980535C 1 19990129 A 5712 RIB DOUG DC8 DC873F 302199F WP LEFT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LOWER L/E LOWER PANEL 522 B INT RIB ON I/B SIDE FWD CORNER HAD CRACK. REMOVED EXISTING PARTS, FABRICATED A NGLES AND CLIPS INSTALLED PARTS PER SRM 51-1-21. N/R 1426 2 L 7 4 4F RT 4A25 1999040200890 19990402 00890 WP 1999 4 2 DHL9980536C 1 19990110 A 5314 KEEL BEAM DOUG DC8 DC873F 302199F WP BS 880 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WHEEL WELL KEEL BEAM AT STA 880 THERE IS SPLICE CRACK 5 INCHES LONG. STOP DRILLED CRACKED AREAS. FABRIC ATED REPAIR ANGLES 7 X 2 X 3. INSTALLED PER SRM 51-1-20. 2 L 7 4 4F RT 4A25 1999040200891 19990402 00891 WP 1999 4 2 DHL9980537C 1 19990104 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT WING T/E TEMP REPAIR AROUND GEAR DOWN IND. REMOVED REPAIR, FABRICATED REPAIR DOUBLER PER SRM 51-1-9, 4 X 6.5 X .25. N/R 796 2 L 7 4 4F RT 4A25 1999040200892 19990402 00892 WP 1999 4 2 DHL9980538C 1 19990128 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 162 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT WING T/E XRS 162 TEMP REPAIR BEHIND REAR SPAR. REMOVED OLD REPAIR, FABRICATED REPAIR DOUBLER, 8.O X 7. 82 PER EO MHA-3111 AND INSTALLED PER EO. N/R 802 2 L 7 4 4F RT 4A25 1999040200893 19990402 00893 WP 1999 4 2 DHL9980539C 1 19990121 A 5313 S141599712000 STRINGER DOUG DC8 DC873F 302199F WP BS 1660 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, EXFOLIATION CORROSION AT INTERSECTION OF FRAME FUSELAGE STA 1660 AND LONG 23 LEFT BELOW CUSP LINE. CUT OUT STRINGER AT FS 1650 AND REMOVED TO PRODUCTION SPLICE STA 1690. PREPARED NEW SECTION OF STRINGER, FABRICATED SPLICING S TRAPS AND INSTALLED PER SRM 51-1-8. N/R 757 2 L 7 4 4F RT 4A25 1999040200894 19990402 00894 WP 1999 4 2 DHL9980540C 1 19990111 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 69.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FWD ADF ANTENNA AFT ATTACH FRAME CRACKED STA 69.5 LEFT SIDE. STOP DRILLED CRACK AND FABRICATED ANGLE REPA IR 2 X 5' PER SRM 53-2-0 AND INSTALLED PER SRM 51-1-21. N/R 720 2 L 7 4 4F RT 4A25 1999040200896 19990402 00896 WP 1999 4 2 DHL9980542C 1 19990121 A 7830 3053256596 FITTING DOUG DC8 DC873F 302199F WP NR 3 ENG TR UNIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 3 ENGINE RT AFT REVERSER COWL AT COLD STREAM UPPER AFT AREA AT 12 O'CLOCK POSITION SLIDING TRACK HOUSING FITTING IS CRACKED AT AFT AREA. DRILLED NEW FITTING AND INSTALLED PER SRM 51-1-20C. N/R 656 2 L 7 4 4F RT 4A25 1999040200897 19990402 00897 WP 1999 4 2 DHL9980543C 1 19990119 A 5753 GUIDES DOUG DC8 DC873F 302199F WP RT TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING FLAP TRACK ICE SHIELD RETAINING GUIDE ANGLE DAMAGED. REMOVED AND REPLACED PER SRM 51-3-0. N/R 591 2 L 7 4 4F RT 4A25 1999040200901 19990402 00901 WP 1999 4 2 DHL9980547C 1 19990129 A 3320 58942694 TRAP FITTING DOUG DC8 DC873F 302199F WP RIGHT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT MLG SUPPORT TRAPEZOIDAL FITTING SHOW CRACK AT FLANGE AFT SECTION ATTACH POINT TO LONG 24 AND STA 902. H FEC COMPLETED, CRACK VERIFIED. VISUAL INDICATION OF PREV REPAIR PER S/B 53-61. REMOVED O/B SPLICE FITTING AND ATTACHIN G PARTS, PREPARED NEW FITTING AND INSTALLED PER SRM PER S/B 53-61. N/R 310 2 L 7 4 4F RT 4A25 1999040200902 19990402 00902 WP 1999 4 2 DHL9980548C 1 19990106 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 860 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WHEEL WELL TOP CEILING STA 860 HAS CRACKED ANGLE. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE 31.25 X 1. 75 X 2.25, INSTALLED PER SRM 51-1-21. N/R 323 2 L 7 4 4F RT 4A25 1999040200903 19990402 00903 WP 1999 4 2 DHL9980549C 1 19990131 A 2710 BRACKET DOUG DC8 DC873F 302199F WP RIGHT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING AILERON POWER PACK COMPARTMENT DRIVE SECTOR QUADRANT BASE CRACKED LOWER O/B HOLE. REMOVED AND REPLA CED BRACKET PER MM 27-13-2. 2 L 7 4 4F RT 4A25 1999040200904 19990402 00904 WP 1999 4 2 DHL9980550C 1 19990115 A 5753 FITTING DOUG DC8 DC873F 302199F WP RIGHT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING FLAP HINGE FITTING CRACKED XW 339. REMOVED ATTACHING PARTS AND CRACKED HINGE SUPPORT FITTING AND INSTALLED A NEW FITTING PER S/B 27-249. N/R 359 2 L 7 4 4F RT 4A25 1999040200905 19990402 00905 WP 1999 4 2 DHL9980551C 1 19990108 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1310 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 2 SEAT TRACK WORN FS 1310. REMOVED DAMAGED FOUR HOLE REPAIR AND FABRICATED AND INSTALLED PER SRM 53-2-3. N/R 299 2 L 7 4 4F RT 4A25 1999040200906 19990402 00906 WP 1999 4 2 DHL9980552C 1 19990112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1330 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 1 SEAT TRACK WORN AT FS 1330. CUT OUT DAMAGED SECTION OF TRACK AND INSTALLED REPAIR PARTS PER SRM 53-2- 3. N/R 300 2 L 7 4 4F RT 4A25 1999040200907 19990402 00907 WP 1999 4 2 DHL9980553C 1 19990112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1580 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 6 SEAT TRACK WORN AT STA 1580. CUT OUT DAMAGED SECTION OF SEAT TRACK, FABRICATED FIVE HOLE SEAT TRACK RE PAIR PLUG AND INSTALLED PER SRM 51-1-8. N/R 303 2 L 7 4 4F RT 4A25 1999040200908 19990402 00908 WP 1999 4 2 DHL9980554C 1 19990112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1590 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, 36 SEAT TRACK WORN AT FS 1590. CUT OUT DAMAGED AREA AND FABRICATED REPAIR PLUG AND REINSTALLED PER SRM 53-2 -23. N/R 5347 2 L 7 4 4F RT 4A25 1999040200909 19990402 00909 WP 1999 4 2 DHL9980555C 1 19990112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1590 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 2 SEAT TRACK WORN FS 1590. CUT OUT DAMAGED SECTION OF SEAT TRACK, FABRICATED NEW AND INSTALLED PER SRM 53-2-3. N/R 305 2 L 7 4 4F RT 4A25 1999040200912 19990402 00912 WP 1999 4 2 DHL9980558C 1 19990112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 325 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 3 SEAT TRACK WORN AT STA 325. CUT OUT DAMAGED SECTION, FABRICATED PLUG, CHANNEL AND INSTALLED PER SRM 51 -1-18. N/R 288 2 L 7 4 4F RT 4A25 1999040200913 19990402 00913 WP 1999 4 2 DHL9980559C 1 19990107 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 325 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 5 SEAT TRACK WORN AT STA 325. REMOVED, REPLACED EXISTING TRACK AND INSTALLED PER SRM 51-18. N/R 289 2 L 7 4 4F RT 4A25 1999040200914 19990402 00914 WP 1999 4 2 DHL9980560C 1 19990110 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 329 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 3 SEAT TRACK WORN AT STA 329. REMOVED EXISTING TRACK AND FABRICATED NEW, INSTALLED PER SRM 53-2-3. N/R 290 2 L 7 4 4F RT 4A25 1999040200915 19990402 00915 WP 1999 4 2 DHL9980561C 1 19990110 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1260 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 5 SEAT TRACK WORN. CUT OUT DAMAGED AREA AT FS 1260. INSTALLED REPAIR PARTS PER SRM 53-2-3. N/R 298 2 L 7 4 4F RT 4A25 1999040200917 19990402 00917 WP 1999 4 2 DHL9980563C 1 19990110 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 785 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 8 SEAT TRACK WORN AT APPROX 785. REMOVED AND INSTALLED REPAIR PER SRM 53-2-3. N/R 258 2 L 7 4 4F RT 4A25 1999040200918 19990402 00918 WP 1999 4 2 DHL9980564C 1 19990110 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 690 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 4 SEAT TRACK WORN AT STA 690. REMOVED EXISTING REPAIR AND FABRICATED NEW REPAIR PER SRM 53-2-3. N/R 259 2 L 7 4 4F RT 4A25 1999040200919 19990402 00919 WP 1999 4 2 DHL9980565C 1 19990108 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 690 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 3 SEAT TRACK WORN AT STA 690. REMOVED DAMAGED SEAT TRACK AND INSTALLED FABRICATED NEW TRACK PER SRM 53-2 -3. N/R 262 2 L 7 4 4F RT 4A25 1999040200920 19990402 00920 WP 1999 4 2 DHL9980566C 1 19990113 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 600 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 6 SEAT TRACK WORN AT APPROX 600. CUT OUT DAMAGED SECTION AND FABRICATED HOLE PLUG AND CHANNEL. INSTALLE D PARTS PER SRM 53-2-3. N/R 268 2 L 7 4 4F RT 4A25 1999040200922 19990402 00922 WP 1999 4 2 DHL9980568C 1 19990122 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FLIGHT ENGINEER ELONGATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FLT ENGINEER LEFT AND RIGHT SEAT TRACKS SHOW ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS PER SRM 53-2 1-1. N/R 234 2 L 7 4 4F RT 4A25 1999040200923 19990402 00923 WP 1999 4 2 DHL9980569C 1 19990122 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP RIGHT COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, F/O LEFT AND RIGHT REAR SEAT TRACK IS CRACKED AND CHAFED. REMOVED SEAT TRACK AND INSTALLED NEW TRACK PER SR M 51-1-21. N/R 409 2 L 7 4 4F RT 4A25 1999040200924 19990402 00924 WP 1999 4 2 DHL9980570C 1 19990122 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP RIGHT COCKPIT CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, F/O FWD LEFT AND RIGHT SEAT TRACKS SHOWS CHAFING MARKS. REMOVED, FABRICATED NEW TRACK AND INSTALLED PER SR M 51-1-8. N/R 410 2 L 7 4 4F RT 4A25 1999040200925 19990402 00925 WP 1999 4 2 DHL9980571C 1 19990122 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP LEFT COCKPIT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, CAPTAIN'S REAR SEAT TRACK BOTH SHOWS SIGNS OF CHAFING AND ELONGATED HOLES. REMOVED REAR SEAT TRACK AND INST ALLED NEW TRACK PER SRM 51-1-8. N/R 411 2 L 7 4 4F RT 4A25 1999040200926 19990402 00926 WP 1999 4 2 DHL9980573C 1 19990116 A 5240 DOOR DOUG DC8 DC873F 302199F WP RIGHT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING DOOR ACCESS PANEL DELAMINATED NR 577B. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-3-0. N/R 251 2 L 7 4 4F RT 4A25 1999040200927 19990402 00927 WP 1999 4 2 DHL9980574C 1 19990112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 858 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 7 SEAT TRACK WORN AT STA 858. CUT OUT DAMAGED SECTION, FABRICATED REPAIR PLUG AND INSTALLED PER SRM 53-2 -3. N/R 253 2 L 7 4 4F RT 4A25 1999040200928 19990402 00928 WP 1999 4 2 DHL9980575C 1 19990112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 815 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 3 SEAT TRACK WORN AT APPROX STA 815. CUT OUT DAMAGED SECTION, FABRICATED REPAIR PLUG AND CHANNEL PER SRM 51-1-8. N/R 254 2 L 7 4 4F RT 4A25 1999040200929 19990402 00929 WP 1999 4 2 DHL9980576C 1 19990122 A 5280 DOOR DOUG DC8 DC873F 302199F WP RIGHT MLG DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT MLG CENTER DOOR DELAMINATED. REMOVED DOOR AND REPLACED WITH REPAIRED DOOR PER MM 32-10-0. N/R 101 2 L 7 4 4F RT 4A25 1999040200930 19990402 00930 WP 1999 4 2 DHL9980577C 1 19990126 A 5240 DOOR DOUG DC8 DC873F 302199F WP RIGHT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING ACCESS DOOR 557A DELAMINATED AT LOWER SURFACE. REMOVED AND INSTALLED SERVICEABLE DOOR PER SRM 51-3- 0. N/R 102 2 L 7 4 4F RT 4A25 1999040200931 19990402 00931 WP 1999 4 2 DHL9980578C 1 19990115 A 5240 DOOR DOUG DC8 DC873F 302199F WP RIGHT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING ACCESS DOOR NR 540 DELAMINATED. REMOVED AND REINSTALLED OVERHAULED DOOR PER MM. N/R 103 2 L 7 4 4F RT 4A25 1999040200932 19990402 00932 WP 1999 4 2 DHL9980579C 1 19990128 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FUSELAGE LT SIDE LONG CENTER WING AREA SPOT OF CORROSION AT STA 680. CUT OUT CORRODED SECTION, FABRICATED F ILLER, DOUBLER, TRIPLER PER EO MHA-3109. FILLER 125 X 4 X 4', DOUBLER 15 X 17, TRIPLER 14 X 16. N/R 186 2 L 7 4 4F RT 4A25 1999040200933 19990402 00933 WP 1999 4 2 DHL9980580C 1 19990107 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 507 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 4 SEAT TRACK WORN AT STA 507. REMOVED SEAT TRACK AND INSTALLED REPAIR PER SRM 53-2-3. N/R 191 2 L 7 4 4F RT 4A25 1999040200934 19990402 00934 WP 1999 4 2 DHL9980581C 1 19990117 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 340-390 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT WING T/E SURFACE STA 390 TO 340 PANEL DELAMINATED. REMOVED AND INSTALLED SERVICEABLE PANEL PER SRM 51-1- 21. N/R 080 2 L 7 4 4F RT 4A25 1999040200935 19990402 00935 WP 1999 4 2 DHL9980582C 1 19990207 A 5755 SKIN DOUG DC8 DC873F 302199F WP LT NR 2 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT WING NR 2 SPOILER PANEL DELAMINATED. REMOVED AND REPLACED SPOILER PANEL PER MM 27-61-1. N/R 81 2 L 7 4 4F RT 4A25 1999040200936 19990402 00936 WP 1999 4 2 DHL9980583C 1 19990114 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 5-98 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT WING LOWER T/E PANEL DELAMINATED SEVERAL PLACES STA 5 TO 98. REMOVED DELAMINATED PANEL AND INSTALLED S ERVICEABLE PER SRM 51-1-21. N/R 83 2 L 7 4 4F RT 4A25 1999040200937 19990402 00937 WP 1999 4 2 DHL9980584C 1 19990108 A 5753 VANE DOUG DC8 DC873F 302199F WP LEFT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT WING NR 2 FLAP VANE DELAMINATED. REMOVED FLAP VANE AND INSTALLED NEW VANE AND OPS CHECK PER MM 27-50-00. N/R 85 2 L 7 4 4F RT 4A25 1999040200938 19990402 00938 WP 1999 4 2 DHL9980585C 1 19990112 A 5753 VANE DOUG DC8 DC873F 302199F WP RIGHT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING NR 6 FLAP VANE DELAMINATED. REMOVED AND REINSTALLED SERVICEABLE VANE PER MM 27-51-14. N/R 90 2 L 7 4 4F RT 4A25 1999040200939 19990402 00939 WP 1999 4 2 DHL9980587C 1 19990207 A 5755 PANEL DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 5 SPOILER PANEL DELAMINATED. REMOVED AND REINSTALLED NEW PANEL PER MM 27-61-1. N/R 95 2 L 7 4 4F RT 4A25 1999040200940 19990402 00940 WP 1999 4 2 DHL9980588C 1 19990207 A 5755 PANEL DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 3 SPOILER PANEL DELAMINATED. REMOVED AND REPLACED PANEL PER MM 27-61-1. N/R 96 2 L 7 4 4F RT 4A25 1999040200941 19990402 00941 WP 1999 4 2 DHL9980589C 1 19990207 A 5755 HARDWARE DOUG DC8 DC873F 302199F WP NR 3 SPOILER WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LEFT WING NR 3 SPOILER PANEL HAS EXCESSIVE PLAY. REMOVED AND REPLACED WORN HARDWARE PER MM 27-61-1. N/R 97 2 L 7 4 4F RT 4A25 1999040200942 19990402 00942 WP 1999 4 2 DHL9980590C 1 19990207 A 5755 PANEL DOUG DC8 DC873F 302199F WP NR 1 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NR 1 SPOILER PANEL DELAMINATED. REMOVED AND REPLACED WITH OVERHAULED PANEL PER MM 27-61-1. N/R 99 2 L 7 4 4F RT 4A25 1999040200943 19990402 00943 WP 1999 4 2 DHL9980686C 1 19990112 A 5755 PANEL DOUG DC8 DC873F 302199F WP NR 4 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT WING NR 4 SPOILER PANEL DELAMINATED. REMOVED AND REINSTALLED PER MM 27-5-13. N/R 90 2 L 7 4 4F RT 4A25 1999040200944 19990402 00944 WP 1999 4 2 RRXA99189 1 19990326 A 3260 CONNECTOR DOUG DC8 DC871F 302199D WP 1 & 2 GND CONTL DIRTY A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 8177U 45983 AFTER T/O FROM KMCO, GEAR WAS RETRACTED, LANDING GEAR WARNING HORN SOUNDED AND COULD NOT BE SILENCED UNTIL FLAPS CAME TO 0 DEG. CLEANED CANNON PLUGS ON GROUND CONTROL SWITCHES NR 1 AND 2. OPS CHECKED SYSTEM AS PER UAL 27-00-12, OPS NORMAL ON GROUND. 2 L 7 4 4F RT 4A25 1999040200945 19990402 00945 NE 1999 4 2 RRXA99190 2 19990329 A 7230 COMPRESSOR DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE STALLED A RRXA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 WP 15 964R 169 46000 669627 AT ROTATION EXPERIENCED COMPRESSOR STALLS NR 4 ENG. RETARTED ENGINE, 30 SECONDS LATER ENGINE FAILED. NO FIRE, PERFORME D EMERGENCY FIRE AND DAMAGE SHUT DOWN. REMOVED AND REPLACED NR 4 ENG IAW EWA MEL 77. OPS CKS LEAK, CKS GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1999040200946 19990402 00946 NM 1999 4 2 TC8A99007 1 19990328 A 2781 INDICATION BOEING 727 727173C 1384059 NM NR 7 LE FLAP MALFUNCTIONED A TC8A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 704A 19504 WITH FLAP RETRACTED, LEADING EDGE DEVICE AMBER LIGHT REMAINS ILLUMINATED ON FWD PANEL AND NR 7 LED AMBER LIGHT REMAINS I LLUMINATED ON FE AUX PANEL. ACFT INSPECTED AND FOUND TO BE SAFE FOR INTENDED FERRY FLIGHT. FOUND TO BE INDICATION PROB LEM, SLAT OPERATES NORMALLY. 2 L 7 3 4F A3WE 1999040200947 19990402 00947 WP 1999 4 2 TC8A99008 1 19990331 A 2931 CONNECTOR DOUG DC8 DC862F 3021972 WP HYDRAULIC SYST LOOSE A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 187SK 46022 ON TAXI-OUT, SPOILER HYDRAULIC PRESSURE WENT TO 2200 PSI AND REMAINED THERE. FOUND LOOSE CONNECTOR AT TRANSMITTER CONNE CTOR. SECURED IAW 27-0-0. 2 L 7 4 4F 4A25 1999040600001 19990406 00001 WP 1999 4 6 AT9900273 1 19990315 A 5754 SKIN DOUG DC9 DC932 3022066 WP NR 1 LE SLAT DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT SIDE NR 1 SLAT LOWER EXTERNAL SURFACE DENTED JUST INBOARD OF ANT I-ICE DUCT. CUT INNER SKIN FOR ACCESS, FABRICATED DOUBLER AND SKIN SPLICE DOUBLER, DRILLED, COUNTERSUNK, TREAT, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 57-09 FIG 10 AND 10A, 51-30-2, 51-30-8, AND RES NR 99603. 2 L 7 2 4F A6WE 1999040600002 19990406 00002 WP 1999 4 6 SCNA99052 1 19990316 A 3244 50003604 TIRE DOUG DC10 DC1015 3022118 WP MLG FAILED A SCNA O OTHER O OTHER LD LANDING 1 GL 15 153SY 261 48276 DURING LANDING ROLL, THE NR 8 MAIN LANDING GEAR TIRE BLEW. ROLL OUT WAS UNEVENTFUL. REMOVED AND REPLACED THE NR 8 MAIN LANDING GEAR TIRE ASSEMBLY. 2 L 7 3 4F A22WE 1999040600003 19990406 00003 WP 1999 4 6 USAA990114 1 19990212 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 936VJ 47609 48116 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT UPPER AND LOWER HAT SECTION OF LONGERON AT STATION 965 LONGER 16 RT. SPL ICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 1999040900001 19990409 00001 WP 1999 4 9 AT9900270 1 19990323 A 5320 99105035 WEB DOUG DC9 DC932 3022066 WP BS 935-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND CUSP WEB AREA AT BS 935-965 CORRODED. REMOVED FLOOR WEB AREA, DRILLED NEW WEB AND INSTALLED IAW DC9 SRM 51-30-2, 51-20-0, 51-30-0, 51-10-2, 51-10-3, 51-10-4 AND 51-30-1. 2 L 7 2 4F A6WE 1999040900002 19990409 00002 EA 1999 4 9 JBXA9900078 1 19990401 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PASSENGER DOOR LACK OF LUBE A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 577ML 7269 FLIGHT 930 RDU TO DCA OUT OF RDU HAD PAX DOOR OUT HANDLE MESSAGE AFTER TAKEOFF. LUBED PASSENGER DOOR INSIDE LOCK HANDLE ROLLER SWITCH AND TRACK AND LATCH MECHANISM COMPLETED IAW AMM 52-11-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999040900003 19990409 00003 SO 1999 4 9 COMA9910049 1 19990329 A 3231 SEQUENCE VALVE EMB 120 EMB120RT SO RT MLG DOOR LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 255CA 120238 HYDRAULIC LEAK, RIGHT HAND WHEEL WELL. REPLACED O RING AT DOOR SEQUENCE VALVE. 2 L 7 2 4T RT A31SO 1999040900004 19990409 00004 SO 1999 4 9 COMA9910050 1 19990330 A 3350 1013073 LIGHT EMB 120 EMB120RT SO ROW 2 INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 246CA 120223 EMERGENCY FLOOR LIGHT, ROW 2 IS INOPERABLE. REPLACED LIGHT. 2 L 7 2 4T RT A31SO 1999040900005 19990409 00005 SO 1999 4 9 COMA9910051 1 19990331 A 5280 12012347001 HANDLE EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 266CA 120258 LEFT MAIN LANDING GEAR DOOR WILL NOT CLOSE. REPLACED GEAR DOOR HANDLE. 2 L 7 2 4T RT A31SO 1999040900006 19990409 00006 EA 1999 4 9 COMA9960139 1 19990331 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 776CA 6552 107 7293 FLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999040900007 19990409 00007 EA 1999 4 9 COMA9960140 1 19990331 A 2751 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA TE FLAP ACTIVATED A COMA O OTHER N FALSE WARNING LD LANDING 1 SO 01 934CA 7042 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM PER AD98-20-01. 2 L 7 2 4F RT A21EA 1999040900008 19990409 00008 EA 1999 4 9 COMA9960141 1 19990330 A 2751 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA TE FLAP ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 917CA 7017 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM PER AD98-20-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999040900009 19990409 00009 EA 1999 4 9 COMA9960142 1 19990328 A 2752 854D1001 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 721CA 7259 FLAPS FAILED AT 13 DEGREES. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 1999040900010 19990409 00010 NM 1999 4 9 UPS99229146 1 19990330 A 5230 HINGE BOEING 727 72722C 138400F NM AFT CARGO DOOR CRACKED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 928UP 19091 INSPECTION TYPE-N/A, AFT LOWER CARGO DOOR FORWARD HINGE CRACKED OFF DOOR. REPLACED FWD FITTING AND CHECKED GAPS AND CLEA RANCES PER M/M 52-31-01, OPS CHECK GOOD (P/N 19667-4) ON, OFF (P/N 6-19667-3A) TAG 21956. 2 L 7 3 4F A3WE 1999040900011 19990409 00011 NM 1999 4 9 UPS99529150 1 19990317 A 5347 146N52181 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1180-1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE-C, MAIN DECK SEAT TRACK HAS CORROSION ALONG BOTH FLANGES AT BS 1180 TO 1200 RBL 25 WL 208. REMOVED AND I NSTALLED NEW SEAT TRACK, WORK DONE IAW SRM 51-40-05, 51-40-08 AND SRM 51-40-09. 2 L 7 2 4F RT A2NM 1999040900012 19990409 00012 NM 1999 4 9 UPS99529151 1 19990324 A 5320 BEAM BOEING 757 75724APF 1384969 NM BS 1064 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYP-C, MAIN DECK OVERWING LONGITUDINAL BEAM HAS CORROSION ON OUTBOARD FLANGE AT BS 1064 RBL 47 WL 208. REMOVE D CORROSION ON LONGITUDINAL BEAM, FOUND TO BE OUT OF LIMITS. REMOVED LONGITUDINAL BEAM AT BS 1040 TO 1080, RBL 45.5 AND INSTALLED NEW LONGITUDINAL BEAM AT BS 1040 TO 1080 ALL WORK DONE IAW SRM 51-40-02, SRM 53-00-51, SRM 51-40-05 AND SRM 51 -20-05. 2 L 7 2 4F RT A2NM 1999040900013 19990409 00013 NM 1999 4 9 UPS99529153 1 19990324 A 5320 BEAM BOEING 757 75724APF 1384969 NM BS 900-1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 413UP 23853 INSPECTION TYPE-C, MAIN DECK OVERWING LONGITUDINAL BEAM HAS CORROSION ALONG OUTBOARD FLANGE AT BS 900 TO 1040 RBL 45 WL 208. REMOVED CORROSION ON LONGITUDINAL BEAM FROM BS 900 TO 1040, FOUND SEVERAL AREAS OUT OF LIMITS. REMOVED CORRODED LON GITUDINAL BEAM AND INSTALLED NEW LONGITUDINAL BEAM. ALL WORK DONE IAW SRM 51-40-02, SRM 53-00-51, SRM 51-40-05 AND SRM 51-20-05. 2 L 7 2 4F RT A2NM 1999040900014 19990409 00014 WP 1999 4 9 UPS99829152 1 19990224 A 5720 370484102 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE-C123, NR 3 MAIN TANK O/B SIDE OF THE XRS 74 RIB, THE STRINGER AFT END FITTING IS CRACKED. REMOVED AND RE PLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900015 19990409 00015 EU 1999 4 9 99UAL900132 1 19990225 A 3510 REGULATOR RCF6705600U AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 411UA 2792 464 FLIGHT DIVERTED TO DEN WHEN SUPPLEMENTAL OXYGEN WAS LOST. WHILE SEARCHING FOR O2 LEAK FOUND CREW O2 REGULATOR TRANSMITT ER ASSY LEAKING MASSIVLY. LEAK IS AT THE BACK OF THE TRANSMITTER HOUSING. REPLACED REGULATOR ASSY. LEAK CHECKED REGUL ATOR. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900016 19990409 00016 NM 1999 4 9 99UAL900133 1 19990301 A 2133 OUTFLOW VALVE FL AEROSPACE 322684007 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 928UA 50230 26651 AIRCRAFT DID NOT PRESSURIZE. *S/D* FORWARD OUTFLOW VALVE WAS STICKING OPEN. REPLACED FORWARD OUTFLOW VALVE, OPS CHECK O K. 2 L 7 2 4F 4 F RT A16WE E2GL 1999040900017 19990409 00017 NM 1999 4 9 99UAL900134 1 19990301 A 2612 APU 655280915 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CABIN MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. J N WARNING INDICATION FALSE WARNING DE DESCENT 1 WP 29 994UA M00071 22384 APU FIRE WARNING. *S/D* INSPECTED APU, FOUND NO EVIDENCE OF FIRE. CHECKED LOOPS, CONNECTORS AND OHMED OUT. FOUND NO SH ORTS OR OPENS. FOUND OIL ON CONNECTOR AND CLEANED. REPLACED FIRE DETECTION UNIT AS A PRECAUTION. REPLACED FIRE BOTTLE AND SQUIB. RAN APU, OPERATION NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1999040900018 19990409 00018 NM 1999 4 9 99UAL900137 1 19990228 A 3244 APS01339 TIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 WP 29 510UA 24780 RETURNED TO DEN WHEN BLOWN TIRE CAUSED FLAP DAMAGE WITH LOSS OF SYSTEM HYDRAULICS. *S/D* REPORT FROM BRIDGESTONE ACFT TIRE, INC. TIRE SUFFERED A 3 PIECE FLEX BREAK (2 SIDEWALL/BEAD SECTIONS AND 1 CAP SECTION) DUE TO POSSIBLE RUNNING OF T IRE WHILE UNDER INFLATED. CONSIDERABLE CORD FRAYING THAT WAS EVIDENT SHOWED LONG TERM EXPOSURE TO EXCESSIVE FLEXING (UN DERINFLATION). THERE IS THE POSSIBILITY THAT FOD CAUSED THE DAMAGE. REPLACED WHEEL ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900019 19990409 00019 NM 1999 4 9 99UAL900135 1 19990226 A 7931 5007431 SHAFT COUPLING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 5 SCAVENGE SHEARED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 560UA 26660 726649 DIVERTED TO DEN UNDER AMBER ALERT DUE TO LOSS OF OIL PRESSURE ON THE NR 2 ENGINE. *S/D* FOUND OIL LUBE SCAVENGE UNIT WIT H A SHEARED SHAFT. ENGINE WAS REPLACED. UPON DISASSEMBLY OF OIL LUBE SCAVENGE FOUND 8/40 BOLT INSIDE THE NR 5 SCAVENGE PUMP. UPON ENGINE DISASSEMBLY ALL BEARINGS WERE REPLACED AND EXPOSED AREAS WERE INSPECTED. NO METAL WAS FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900020 19990409 00020 NM 1999 4 9 99UAL900136 1 19990226 A 2780 W3486100418 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE FLAP FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 575UA 26689 RETURNED TO FIELD AT ORD UNDER AMBER ALERT DUE TO A LEADING EDGE ASYMMETRY LIGHT. *S/D* FOUND A WIRE ASSOCIATED WITH THE LEADING EDGE SLAT SYSTEM SHORTING TO GROUND WHICH CAUSED THE SYSTEM FAULT AND SHUTDOWN. REPLACED THE WIRE AND RETURNED AIRCRAFT TO SERVICE WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900021 19990409 00021 NM 1999 4 9 99UAL900144 1 19990306 A 5300 141U8007502 INTERCOSTAL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 322 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 AT APPROXIMATELY BODY STATION 322, THERE EXISTS A CRACK IN THE 141U8007-502 INTERCOSTAL. THE CRACK EXISTS IN THE LOWER H ORIZONTAL FLANGE AND EXTENDS TO THE SECOND FASTENER HOLE COMMON TO THE 141U8007-501 SPLICE. *S/D* 141U8007-502 TRIMMED OUT AROUND CRACKED AREA. 141U8007-501 SPLICE STRAP EXTENDED TO PICK UP ADDITIONAL FASTENERS BEYOND CRACKED AREA. PART ROUTED TO BAC FOR ANALYSIS. 2 L 7 4 4F 4 F RT A20WE E24NE 1999040900022 19990409 00022 NM 1999 4 9 99UAL900146 1 19990306 A 2761 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SPOILER MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 552UA 26641 RETURNED TO FIELD AT LAX DUE TO FLOATING SPOILER PROBLEM. *S/D* CAUSE OF SPOILER EICAS MESSAGE WAS NOT FOUND AND COULD NOT BE DUPLICATED DURING TROUBLESHOOTING. SPOILER FLOAT WAS NOT VERIFIED. ALL OPERATIONAL AND VISUAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900023 19990409 00023 EU 1999 4 9 99UAL900147 1 19990308 A 2911 887673 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 HYD SYSTEM LEAKING A UALA K NONE K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 406UA 17537 454 INTERMITTENT GREEN HYD SYSTEM LOW ECAM WARNING. PRESSURE NORMAL AND NO FLUCTUATION. FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED PUMP PER MM29-11-51. LEAK AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900024 19990409 00024 1999 4 9 99UAL900148 4 19990305 A 2330 271150055001 VIDEO UNIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 17AB FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 780UA 26944 EN ROUTE DEN-ORD, SMOKE/ODOR FROM VIDEO UNIT AT SEAT 17AB. AIRCRAFT DIVERTED TO IND. *S/D* THE UNIT HAS NOT BEEN RECO VERED. IT IS SUSPECTED THAT THE SEAT VIDEO UNIT SVU (SEAT VIDEO UNIT) TO SVU CABLE BECAME PARTIALLY DISCONNECTED FROM T HE SVU CAUSING ELECTRICAL ARCING AT THE JUNCTION OF THE CABLE AND SVU. THE SVU WAS REPLACED BUT THE CABLE WAS NOT. THI S COULD INDICATE THE CABLE SUSTAINED LITTLE IF ANY DAMAGE. UA ENGINEERING HAS ISSUED A SPECIAL PROJECT TO SAFETY WIRE T HE CONNECTORS TO THE SVU TO PREVENT REOCCURENCE IN THE FUTURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999040900025 19990409 00025 NM 1999 4 9 99UAL900149 1 19990310 A 3230 273T610010 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT MLG TRUCK BROKEN A UALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 WP 29 643UA 25093 UNABLE TO RAISE LEFT MAIN LANDING GEAR. RETURNED TO FIELD. AMBER ALERT DECLARED. *S/D* TRUCK POSITION ACTUATOR FOUND L EAKING INTERNALLY AT PRESSURE RELIEF VALVE. REPLACED ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 1999040900026 19990409 00026 NM 1999 4 9 99UAL900150 1 19990311 A 2120 AIR DIST BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 662UA 27159 WITH RT RECIRC FAN OFF HAD CHEMICAL SMELL SIMILAR TO CHLORINE, THEN HAD HOT ELECTRICAL BURNING SMELL WITH RECIRC FAN BAC K ON. THIS CONDITION OCCURRED ON THREE SEPARATE OCCASIONS. COULD NOT ISOLATE SOURCE. DIVERT YJT, EMERGENCY DECLARED, OVERWEIGHT LANDING. *S/D* CHEMICAL AND/OR ELECTRICAL SMELLS COULD NOT BE DUPLICATED ON THE POSITION FERRY FLIGHT TO IA D. IAD MAINTENANCE COULD NOT DUPLICATE THE CONDITION LISTED ABOVE. AIRCRAFT HAS NOT EXPERIENCED A REPORT OF CHEMICAL O R ELECTRICAL SMELL SINCE THIS OCCURANCE. SMELL MAY BE NON-AIRCRAFT RELATED. 2 L 7 2 4F 4 F RT A1NM E24NE 1999040900027 19990409 00027 NM 1999 4 9 99UAL900151 1 19990311 A 2450 91252ZC7C4001 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AC POWER DIST FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 391UA 24666 EXPERIENCED ELECTRICAL FAILURES STARTING WITH FLIGHT RECORDER OFF LIGHT, ACARS, GPWS YAW DAMPENER, CAPTAIN'S HSI AND ADI . NR 1 AC BUS POPPED AFTER LANDING. *S/D* FAULTY R3 (NR 1 TRANSFER BUS) RELAY, REPLACED R3 RELAY. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999040900028 19990409 00028 NM 1999 4 9 99UAL900141 1 19990302 A 2130 VALVE ALLIEDSIGNAL 39606411 BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE LEFT PACK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 982UA 21640 UNABLE TO PRESSURIZE AIRCRAFT. *S/D* LEFT PACK FLOW CONTROL VALVE FAILED. REPLACED LEFT PACK FLOW CONTROL VALVE, OPS CH ECK OK. 2 L 7 2 4F 4 F A16WE E2EA 1999040900029 19990409 00029 NM 1999 4 9 99UAL900152 1 19990311 A 3350 900835A BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7285U 21563 EMERGENCY EXIT LIGHT OVER DOOR INSIDE COCKPIT IS ON AND WILL NOT GO OFF. *S/D* REPLACED BATTERY, OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999040900030 19990409 00030 NM 1999 4 9 99UAL900153 1 19990311 A 2611 824PTY SMOKE DETECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LAVATORY FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 7253U 21400 FORWARD LAVATORY SMOKE DETECTOR SYSTEM INOPERATIVE. FORWARD LAVATORY SMOKE DETECTOR UNIT REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999040900031 19990409 00031 NM 1999 4 9 99UAL900154 1 19990313 A 3397 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 19-26 BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7272U 21419 EEL TRACK LIGHTING INOPERATIVE FROM ROW 19 THROUGH 26. *S/D* FOUND BREAK IN WIRE WHERE IT COMES OUT OF SIDEWALL. MADE INTERIM REPAIR, MUST BE PERMANENTLY REPAIRED WITHIN 45 DAYS. 2 L 7 3 4F 4 F A3WE E2EA 1999040900032 19990409 00032 1999 4 9 99UAL900155 4 19990214 A 3414 AIRSPEED IND SPERRY 4057800901 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE COCKPIT MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 1855U 80061318 47837 AIRSPEED FLAG ON SIDE AT 90 KTS, 0 AIRSPEED AND AIRSPEED FLAG. ABORTED TAKEOFF 110 TO 115 KTS. PRIOR TO TURN OFF, FLAG W ENT AWAY. *S/D* UNABLE TO DUPLICATE INDICATOR PROBLEM ON THE GROUND. REPLACED MACH/AIRSPEED INDICATOR PRECAUTIONARY. 2 L 7 3 4F 4 F A22WE E23EA 1999040900033 19990409 00033 NE 1999 4 9 99UAL900158 2 19990314 A 7530 VSV BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LT ENGINE OUT OF ADJUST A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 956UA 26704 856670 LEFT ENGINE EXPERIENCED POWER SURGES. *S/D* ACCOMPLISHED ENGINE BORESCOPE AND TROUBLESHOOTING FOUND VARIABLE STATOR VA NES (VSV) OUT OF RIG, NO LIMITING DEFECTS NOTED IN GAS PATH AND VSV'S WERE PROPERLY RIGGED PER MAINTENANCE MANUAL. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999040900034 19990409 00034 NM 1999 4 9 99UAL900160 1 19990315 A 3260 257T11039 MODULE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LANDING GEAR MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 602UA 21863 ON APPROACH, AMBER GEAR LIGHT ILLUMINATED AFTER LOWERING THE LANDING GEAR HANDLE. RECEIVED GREEN LEFT, NOSE, AND RIGHT LIGHTS, 'GEAR' DID NOT EXTINGUISH. ALSO, RECEIVED GPWS BELOW 500 FEET, AMBER ALERT. *S/D* DOWN SWITCH IN LANDING GEA R LEVER MODULE FAILED. GEAR WAS EXTENDED AND LOCKED. REPLACED LANDING GEAR LEVER MODULE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999040900035 19990409 00035 NM 1999 4 9 99UAL900161 1 19990309 A 5310 STRUCTURE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE FUSELAGE DAMAGED A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 974UA 21597 DAMAGE CAUSED BY BAGGAGE TRACTOR ON RIGHT SIDE OF AIRCRAFT, JUST FORWARD OF NR 2 SERVICE DOOR ENCOMPASSING A 42 INCH ARE A WITH APPROXIMATELY AN 18 INCH HOLE ACROSS ONE STRINGER. *S/D* SHEAR TIE REPAIRED AT STA 344 BETWEEN STR 19R AND 20R PE R SRM 53-10-4, FIGURE 9. SKIN WAS REPAIRED BETWEEN BS 312 AND BS 355 PER SRM 53-30-3, FIGURES 1 & 9. 2 L 7 2 4F 4 F A16WE E2EA 1999040900036 19990409 00036 NM 1999 4 9 99UAL900162 1 19990315 A 2750 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS LACK OF LUBE A UALA L ABORTED APPROACH O OTHER AP APPROACH 1 WP 29 7448U 21902 MADE GO AROUND AT DEN FOR NR 1 INBOARD HYDRAULIC MOTOR PROBLEM. LEFT WING TRAILING EDGE FLAP ELEPHANT EAR FAIRING UPPER BEARING IS CHATTERING AND WILL ALMOST LOCK UP THE FLAP TRANSMISSION WHEN HAND PRESSURE IS APPLIED TO THE FAIRING. AIRC RAFT CAME IN TO GATE WITH HYDRAULIC FLAPS INOPERATIVE. LUBED FLAPS PER MM 27-00-20 LUBE CHART 7-27-5. OPERATED FLAPS T HROUGH FULL RANGE OF TRAVEL UNABLE TO DUPLICATE. 2 L 7 3 4F 4 F A3WE E2EA 1999040900037 19990409 00037 WP 1999 4 9 99UAL900164 1 19990305 A 2910 AYG7056501 MANIFOLD DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 HYD SYST CRACKED A UALA K NONE K FLUID LOSS NR NOT REPORTED 1 WP 29 1828U 46627 NR 3 HYD SYSTEM TRANSFER VALVE MANIFOLD CRACKED AT FILTER BOWL BOSS LOCATED IN RIGHT WHEEL WELL. *S/D* LARGE FATIGUE CRA CK FOUND IN THE PRESSURE FILTER THREADED BOSS DIRECTLY BEHIND THE FLIGHT CONTROL BYPASS VALVE. MANIFOLD ASSEMBLY WAS RE PLACED. 2 L 7 3 4F 4 F A22WE E23EA 1999040900038 19990409 00038 NM 1999 4 9 99UAL900165 1 19990313 A 2497 W2833 WIRE HARNESS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE E & E BAY DAMAGED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 794UA 6405 26936 AIRCRAFT ARRIVED AT GATE AND APU WOULD NOT POWER AC BUS. RIGHTHAND BUS TIE IS OPEN AND WILL NOT CLOSE. *S/D* THIS REP ORT IS DIRECTLY RELATED TO REPORT 99UAL900166 RELATED. REFER TO 99UAL900166 FOR THE DETAILS RELATED TO CAUSE AND CORREC TIVE ACTION. THE LOSS OF ELECTRICAL SIGNAL DUE TO WIRE DAMAGE GAVE NON-VALID SIGNALS TO THE AIRCRAFT ELECTRICAL POWER S YSTEM LOGIC ASSOCIATED WITH THE APU (AUXILIARY POWER GENERATOR) POWER AVAILABILITY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999040900039 19990409 00039 NM 1999 4 9 99UAL900166 1 19990313 A 2450 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE CABIN MISINSTALLED A UALA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 794UA 26936 FOUND SHORTED AND BURNED WIRING ABOVE CEILING AT THE P300 PANEL. *S/D* THE CAUSE OF THE PROBLEM WAS DAMAGE TO WIRES IN WIRE BUNDLE W2833. THE PROBABLE CAUSE WAS METHOD OF SECURING THE WIRE BUNDLE TO A STANDOFF OR DAMAGE TO THE WIRE DURIN G THE INITIAL INSTALLATION. THE DAMAGED WIRES WERE REPLACED. THE ELECTRICAL POWER SYSTEM WAS CHECKED AND FOUND TO OPER ATE PROPERLY. BOEING WAS NOTIFIED OF THE PROBLEM. UNITED WILL INSPECT THIS AREA ON THE REST OF THE FLEET TO ASSURE THI S WIRE BUNDLE IS ROUTED CORRECTLY AND PROPERLY SECURED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999040900040 19990409 00040 NE 1999 4 9 99UAL900167 2 19990316 A 7530 1B7610 STATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING R A PARTIAL RPM/PWR LOSS FLAME/FIRE NR NOT REPORTED 1 WP 29 526UA 3659 24994 727112 PASSING FL280 LEFT ENGINE INSTRUMENTS RAPIDLY ROLLED BACK. FLIGHT ATTENDANT REPORTED LEFT ENGINE ON FIRE. LEFT ENGINE WAS SHUTDOWN. AIRCRAFT RETURNED TO LAX. *S/D* UPON ARRIVAL AT LAX FOUND METAL IN THE TAILPIPE DUE TO AN HPC FAILURE, THE FIRE WAS INTERNAL DUE TO THE FAILURE. THE ENGINE WAS REPLACED. SHOP FINDINGS WERE THAT A 10TH STAGE HPC STATOR HAD FAILED. THIS FAILURE IS A KNOWN MODE AND THIS EVENT IS STILL UNDER INVESTIGATION BY UA AND PWA. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900041 19990409 00041 1999 4 9 99UAL900168 4 19990317 A 3442 DRIVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RADAR SYST MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 661UA 27158 WEATHER RADAR FAILED. RETURNED TO FIELD. *S/D* THE WEATHER RADAR MALFUNCTION COULD NOT BE DUPLICATED ON THE GROUND. S INCE THE RT UNIT HAD BEEN PREVIOUSLY REPLACED IT WAS DECIDED TO REPLACE THE ANTENNA DRIVE UNIT AND THE ANTENNA FLAT PLAT E. A NON-REV VERIFICATION FLIGHT WAS PERFORMED AND THE SYSTEM OPERATION WAS NORMAL. AT THIS TIME THE REMOVED UNITS HAV E NOT BEEN RETURNED FOR SHOP TESTING TO DETERMINE WHICH UNIT WAS THE CAUSE OF THE MALFUNCTION. 2 L 7 2 4F 4 F RT A1NM E24NE 1999040900042 19990409 00042 EU 1999 4 9 99UAL900170 1 19990319 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ROW 22C INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 420UA 489 SEAT 22C EEL LIGHT INOP. REPLACED EEL LIGHT ASSEMBLY (P/N BR9644-21), OP-CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900043 19990409 00043 1999 4 9 99UAL900131 4 19990226 A 2211 B546CCM0103 FMGC AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE E & E COMPT MALFUNCTIONED A UALA K NONE J WARNING INDICATION AP APPROACH 1 WP 29 816UA 871 AUTOPILOT DISENGAGED ON APPROACH ALONG WITH THE MAP NOT AVAIL FLAG ON THE CAPTAIN SIDE NAV DISPLAY. PFR SHOWS FAILURE ME SSAGES FMGC2 AND FAC2. *S/D* THE POSTFLIGHT REPORT IDENTIFIED THE FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC) NR 2 A ND FLIGHT AUGMENTATION COMPUTER (FAC) NR 2 AS THE POSSIBLE FAULTS. THE FMGC 1 AND 2 WERE RERACKED AND SWAPPED BETWEEN P OSITIONS. NO FURTHER FAILURES HAVE OCCURED. THIS MAY BE RELATED TO THE SOFTWARE ANOMALIES IDENTIFIED BY SEXTANT, AIRBU S AND AD 97-21-10. AIRBUS HAS BEEN NOTIFIED OF THIS EVENT. ADDITIONALLY COA 403350/1 HAS BEEN GENERATED TO TERMINATE A D 97-21-10. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900044 19990409 00044 NE 1999 4 9 99UAL900138 2 19990302 A 7532 7200006 ACTUATOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE FAILED A UALA K NONE J WARNING INDICATION CL CLIMB 1 WP 29 614UA 2368 21875 707504 ON CLIMBOUT AT SFO OUT OF 3000 FT, NR 1 ENGINE STARTED AUDIBLE SURGING WITH EPR FLUX 1.41 TO 1.50, N1 FLUX 91-93 PERCENT , AND EGT RUNNING 60 DEG HIGHER THAN NR 2 ENGINE. CONTINUED SURGING WITH AUTOTHROTTLES ON OR OFF. NO SPLIT ON DUCT PRESS URE. AT LEVEL OFF AT FL320 ENGINE RETURN TO NORMAL. ALSO NOTED EXCEEDENCE OF EPR CAUTION RADIAL WITH CLIMB POWER SET. *S/D* REPLACED 3.O BLEED ACTUATOR REF MM 75-32-03. TRIMMED REF MM 71-01-00 PG 501, ALL CHECK NORMAL. REPLACED NR 1 ENGINE EVBC PRECAUTIONARY REF MM 75-31-01. 2 L 7 2 4F 4 F RT A1NM E3NE 1999040900045 19990409 00045 EU 1999 4 9 99UAL900142 1 19990301 A 3350 BATTERY PACK DIEHL GMBH & 321430 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 443UA 820 EMERGENCY LIGHT TEST FAILED. SHOWS EPSU 28VDC EMER L. SUPPLEMENTAL DATA UPDATE 28 VDC FAULT WAS DETECTED AT THE EMERGENC Y POWER SUPPLY UNIT (11WL) AND GAVE A FAULT MESSAGE 'EPSU 28 VDC EMER L'. THE BATTERY WAS REPLACED AND THE TEST WAS FOUN D NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900046 19990409 00046 NM 1999 4 9 99UAL900143 1 19990301 A 5754 114N4002147A PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 LE SLAT DAMAGED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 567UA 26673 NR 1 SLAT, FIXED LEADING EDGE, AUXILIARY SPAR, AND LOWER ACCESS PANELS DAMAGED. *S/D* AIRCRAFT TOWED INTO SERVICE TRUCK . MAJOR REPAIR NR 090 REPLACED THE NR 1 SLAT (P/N 114N4002-147A), AND REPAIRED DAMAGE TO FIXED LE, AUXILIARY SPAR, AND LOWER ACCESS PANELS PER APPLICABLE SRM SECTIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900047 19990409 00047 NM 1999 4 9 99UAL900156 1 19990312 A 5270 WARNING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 4L DOOR ACTIVATED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 510UA 24780 ABORTED TAKEOFF AT 100 KNOTS DUE TO DOOR 4L UNSAFE INDICATION. *S/D* CHECKED DOOR PER MEL5271C AND FOUND TO BE SECURE ON INSIDE AND FAIRED ON OUTSIDE. NO OTHER ABNORMALITIES FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900048 19990409 00048 1999 4 9 99UAL900159 4 19990316 A 2565 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT SLIDE DOOR NOT LATCHED A UALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C NR NOT REPORTED 1 WP 29 551UA 25399 RETURNED TO BOS DUE TO LEFT OVERWING SLIDE DOOR INDICATION. *S/D* INSPECTED PER MM 25-65-00 AND FOUND SLIDE DOOR AFT LAT CH NOT LOCKED. RESET ROUND CRANK HANDLE AND SLIDE DOOR LATCHES PER MM 25-65-00. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900049 19990409 00049 1999 4 9 99UAL900171 4 19990319 A 3420 IRS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E & E COMPT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 603UA 21864 RETURNED TO BOS WHEN INTERTIAL REFERENCE UNITS WOULD NOT ALIGN. OVERWEIGHT LANDING. *S/D* CREW ATTEMPTED A QUICK ALIG N WITH THE AIRCRAFT IN MOTION. IRS SYSTEMS WERE SUCCESSFULLY ALIGNED ONCE THE AIRED AND NORMAL ALIGNMENT PROCEDURES WER E FOLLOWED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999040900050 19990409 00050 EU 1999 4 9 99UAL900173 1 19990324 A 7110 B71131102 COWL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE DAMAGE A UALA A E UNSCHED LANDING ENGINE SHUTDOWN D INFLIGHT SEPARATION CL CLIMB 1 WP 29 425UA 508 V10058 NUMBER 1 ENGINE FAN COWLS OPENED IN FLIGHT. RETURNED TO FIELD FOR A NORMAL LANDING. FAN COWL LATCHES WERE NOT SECURED FROM MAINTENANCE ACTION PREVIOUS NIGHT. LINE MAINTENANCE MANAGEMENT INSTITUTED A REQUIREMENT FOR A SECOND PAIR OF EYES TO VERIFY FAN COWL LATCHES ARE SECURED. A LINE COA HAS BEEN PUBLISHED AND IN PROCESS TO MODIFY LATCHES TO MAKE THEM MOR E VISIBLE IF NOT LATCHED. THE MANUFACTURER IS DEVELOPING A FAN COWL HOLD-OPEN-DEVICE THAT WILL PROVIDE ADDITIONAL VISUAL REFERENCE OF AN UNLATCHED CONDITION. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900051 19990409 00051 NM 1999 4 9 99UAL900174 1 19990314 A 5230 STRUCTURE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 153UA 20102 FORWARD CARGO DOOR DAMAGED BY LOADER, STATION 629.98 FROM 0400 TO 0700 O'CLOCK POSITIONS AT LOWER PORTION OF DOOR. ALSO, THE THE SKIN AND BONDED DOUBLER WERE CREASED ALONG A SPAN FROM STATION 613 TO 635 FROM THE S-38R REFERENCE LINE DOWN NI NE INCHES. CAUSE, CONTACT BY GROUND EQUIPMENT LOADER. REMANUFACTURED PER BOEING BLUEPRINT DRAWNINGS. THE OUTER SKIN A ND BONDED DOUBLER WERE REPAIRED BY INSTALLING AN EXTERNAL DOUBLER. 2 L 7 4 4F 4 F A20WE E20EA 1999040900052 19990409 00052 NM 1999 4 9 99UAL900175 1 19990325 A 2612 FIRE WARNING 89931507 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ENGINE MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 389UA 0596 24664 ABORTED TAKEOFF OF 100 KNOTS DUE TO A FALSE ENGINE FIRE WARNING INDICATION. *S/D* REPLACED ENGINE AND APU FIRE DETECTION ACCESSORY UNIT (M279). OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999040900053 19990409 00053 NM 1999 4 9 99UAL900176 1 19990325 A 3310 61482 BALLAST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT SMOKING A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 7291U 21569 AT 29,000 FEET AND 30 MINUTES OUT OF DEN, CREW REPORTED AN ELECTRICAL ODOR, VISUAL HAZE AND SMOKE IN COCKPIT. SMOKE AL ARM IN FORWARD LAVATORY WENT OFF. DISIPATED AFTER 5 MINUTES. CONTINUED TO DEN. REPLACED BALLAST FOR FWD THRESHOLD LI GHT. LIGHTS OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999040900067 19990409 00067 NM 1999 4 9 98UAL900627 1 19990107 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4090 PW4090 52122 NE DOOR 5L INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 197UA 26901 EMERGENCY AISLE LIGHT INOP AT DR 5L DROP CEILING PANEL. RELAMPED LIGHT, OPS CK OK. 2 L 7 4 4F 4 F RT A20WE E46NE 1999040900072 19990409 00072 WP 1999 4 9 DHL99873001 1 19990331 A 2820 O RING DOUG DC8 DC873F 302199F WP NR 2 PYLON LEAKING A DHLA K NONE X ENGINE FLAMEOUT AP APPROACH 1 SO 01 873SJ 46091 NR 1 ENGINE FLAMED OUT ON FINAL APPROACH. ENGINE IGNITION WAS ON, COMPLETED ABNORMAL PROCEDURES. FOUND FUEL LINE LEAKING ON NR 2 PYLON. REMOVED AND REPLACED TWO PACKINGS PER MM 28-24-14. LEAK CHECKED OK. 2 L 7 4 4F RT 4A25 1999040900084 19990409 00084 EA 1999 4 9 99ZZZX1398 2 19990228 A 7414 FLANGE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MAGNETO BROKEN A WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 3527U 456 317952141 THE FLANGE SECTION OF THE HOUSING DESIGNED TO BE SECURED BY THE BOTTOM CLAMP, BROKE OFF DURING FLIGHT. MAGNETO CONTINUED TO FUNCTION NORMALLY, BUT PILOT REPORTED AN OIL LEAK IN THE RIGHT ENGINE, OBSERVED DURING WALK-AROUND AFTER LANDING. HO USING SHOULD HAUL A STEEL MOUNTING FLANGE. 1 L 7 2 3O 3 O A20SO E14EA 1999040900094 19990409 00094 EA 1999 4 9 99ZZZX1408 2 19990212 A 8520 LW1321 BEARING BEECH B80 B80 1153010 CE LYC O540 IGSO540A1A 41532 EA ROD WORN A IJZA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 05 65RW 648 LD404 L240950 PILOT REPORTED LOW OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND A LANDING WAS MADE AT CHILLICOTHE, MO. OIL PRESSURE RELIEF VALVE CLEANED, STARTED ENGINE AND OIL PRESSURE APPEARED NORMAL. AIRCRAFT FLOWN TO IRK, OIL PRESSURE FLUCTUATED AND WAS LOW. ENGINE WAS TORN DOWN FOR INSPECTION, RE-ASSEMBLED WITH TAGGED CRANK, NEW BEARINGS, ROD BOLTS, AND PISTON PINS. 1 L 7 2 3O 3 O RT 3A20 1E7 1999040900112 19990409 00112 NM 1999 4 9 SPAA9900004 1 19990323 A 3350 110049 BATTERY CHARGER BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING DID NOT ILLUMINATE. THE ASSOCIATED SYSTEM BATTE RY CHARGER WAS REMOVED AND REPLACED. SUBSEQUENT SYSTEM TEST WAS SATISFACTORY PER BMM 33-51-11. 2 L 7 2 4F A16WE 1999040900113 19990409 00113 EU 1999 4 9 MALA976414 1 19990330 A 2910 SWIVEL SAAB SF340 SF340A 7850100 EU RIGHT MLG LEAKING A MALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 110XJ 340A110 AFTER TAKEOFF FROM FORT DODGE, GEAR WAS SELECTED UP FOLLOWED BY A HYDRAULIC CAUTION LIGHT, HYDRAULIC QUANTITY WAS NEAR R ED LINE AND MAIN ACCUMULATOR WAS AT ZERO. CREW FOLLOWED QRH , UPON ARRIVAL AND SHUTDOWN IN MCW, NOTED HYDRAULIC FLUID PU DDLING UNDER RIGHT MAIN WHEEL WELL. MAINTENANCE REPLACED SWIVEL ON DRAG STRUT. PERFROMED ALL LEAK AND OPS CHECKS PER AM M 32-34-00, ALL OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999040900114 19990409 00114 1999 4 9 MALA976415 4 19990330 A 3425 6226190113 AHRS SAAB SF340 SF340A 7850100 EU NR 2 FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 109XJ 340A109 RIGHT AHRS COMPUTER INOP, EADI FLICKERS TO BLACK IN NORMAL/REVERSING/X-SIDE DATA MODES, HDG FLAGS, NO AUTO PILOT OR YAW DAMP. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED NR 2 AHRS COMPUTER AND MPU. OPS CHECK GOOD IAW SF340 M/M. 2 L 7 2 4T RT A52EU 1999040900115 19990409 00115 SW 1999 4 9 PNSA990302 1 19990328 A 2150 20475546 ACM SWRNGN SA227 SA227AC 8780603 SW LEFT FAILED A PNSA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 AL 03 41NE AC741B UPON LANDING WITH SPEED LEVERS AT LOW RPM, CABIN STARTED TO ACCUMULATE SMOKE. BOTH BLEEDS WERE TURNED OFF. SMOKE CLEARED DURING TAXI TO GATE. PROBLEM WAS DETERMINED TO BE LEFT ACM WHICH HAD SEIZED. ACM WAS REPLACED NO FURTHER PROBLEMS NOT ED. 2 L 7 2 4T RT A8SW 1999040900116 19990409 00116 WP 1999 4 9 9901299603 1 19990329 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603NW 47101 DURING PERIODIC CHECK, FOUND TAIL COMPARTMENT CATWALK AND TAILCONE RELEASE HANDLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND RESEATED PIN TO CATWALK LIGHTS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999040900117 19990409 00117 WP 1999 4 9 UPS99829154 1 19990324 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 1040-1060, THE STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900118 19990409 00118 WP 1999 4 9 UPS99829155 1 19990322 A 5320 577327558 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 680 AT RBL 24, THE FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 577 3275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900119 19990409 00119 WP 1999 4 9 UPS99829156 1 19990321 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT L/E OUTBOARD OF THE NR 1 PYLON HAS MODERATE CORROSION ON THE LWR SKIN AT STA XFS560. REPAIRED AR EA IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 1999040900120 19990409 00120 WP 1999 4 9 UPS99829157 1 19990327 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E AT STA XFS640.00, THE L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRE D IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900121 19990409 00121 WP 1999 4 9 UPS99829158 1 19990322 A 5320 47516432 FITTING DOUG DC8 DC871F 302199D WP BS 742 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 742 AT STR 13L, THE TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900122 19990409 00122 WP 1999 4 9 UPS99829159 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E RIB IS CRACKED AT STA XFS622.500, (LWR RIB). STOP DRILLED CRACK AND REPAIRED IAW SRM 57 -2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900123 19990409 00123 WP 1999 4 9 UPS99829160 1 19990324 A 5320 46143972N FITTING DOUG DC8 DC871F 302199D WP BS 75 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 75 AT STR 31R, THE STR END FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 4614 397 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900124 19990409 00124 WP 1999 4 9 UPS99829161 1 19990327 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 634 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E RIB AT STA XFS 634.000 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900125 19990409 00125 WP 1999 4 9 UPS99829162 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E RIB (LWR) IS CRACKED AT STA XFS660.0. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FI G 2. 2 L 7 4 4F RT 4A25 1999040900126 19990409 00126 WP 1999 4 9 UPS99829163 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E AT STA XFS 660.0, THE UPPER L/E RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900127 19990409 00127 WP 1999 4 9 UPS99829164 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E LWR RIB IS CRACKED AT STA XFS 660.0. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900128 19990409 00128 WP 1999 4 9 UPS99829165 1 19990322 A 5320 38877991N FITTING DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 440-460 STR 14L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3887799 AND SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1999040900129 19990409 00129 WP 1999 4 9 UPS99829166 1 19990324 A 5320 564101515 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 1420 AT STR 21L-25L, THE SHEAR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING ( SHEAR TIE) IAW DWG 5641015 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900130 19990409 00130 EU 1999 4 9 QXEA9900543 1 19990330 A 3350 FUSE GRIMES FOKKER F28 F28MK4000 4990810 EU RT EXTERIOR EEL BLOWN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 PDX - WHILE AIRCRAFT WAS IN THE HANGAR FOR OTHER MAINTENANCE A NON-ROUTINE WAS GENERATED FOR THE RIGHT FORWARD BELLY FAI RING EMERGENCY LIGHT INOPERATIVE. A FUSE ON THE EMERGENCY BATTERY PACK WAS REPLACED. OPERATIONAL CHECKS SATISFACTORY. 2 L 7 2 4F RT A20EU 1999040900131 19990409 00131 NM 1999 4 9 99FDEA00128 1 19990331 A 3610 CLAMP BOEING 727 727233 138408A NM LEFT PACK LOOSE A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 270FE 22035 99-82 - LWR AFT BODY OVERHEAT LIGHT CAME ON. AFT PULL THE NR 2 THROTTLE BACK, THE LIGHT WENT OFF. FOUND 1 EA CLAMP ON LE FT PACK AFT OF FLOW CONTROL VALVE LEAKING. TIGHTEN SAME. LEAK CK NORM AS PER MM 36-00-1. 2 L 7 3 4F RT A3WE 1999040900132 19990409 00132 NM 1999 4 9 99FDEA00129 1 19990401 A 2613 65249203 DETECTOR BOEING 727 727233 138408A NM NR 2 ENGINE FAILED A FDEA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 270FE 22035 99-83 - AFT SWITCH BLEED AIR TO NR 2 BLEED LWR AFT BODY OVERHEAT LIGHT ON. REMOVED AND REPLACED FIRE AND OVERHEAT DETECT OR IN REF WITH OVERHEAT DETECTION TROUBLESHOOT CHART 26-14-000-1. OPS CK NORMAL. 2 L 7 3 4F RT A3WE 1999040900133 19990409 00133 NM 1999 4 9 SCNA99058 1 19990325 A 4920 GTCP8598CK APU BOEING 727 727225 1384077 NM APU FIRE A SCNA F ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION IN INSP/MAINT 1 GL 15 283SC 36273 7953 22559 DURING LINE MAINTENANCE ACTIVITIES, THE APU AUTO SHUT DOWN. UPON RESTART THE APU CAUGHT FIRE. EMERGENCY PROCEDURES FOLLO WED AND AND FIRE BOTTLE DISCHARGED EXTINGUISHING THE FLAMES. REMOVED AND REPLACED THE APU IAW MM PROCEDURES. 2 L 7 3 4F A3WE 1999040900134 19990409 00134 NE 1999 4 9 SWAA990589 2 19990330 A 7261 6590305 OIL SCREEN BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE DIRTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 103SW 23109 AIR TURBACK, IN FLIGHT ENGINE SHUT DOWN. OIL FILTER BYPASS LIGHT ILLUMINATED ON NR 2 ENG DID NOT GO OUT AT IDLE. OIL TEM P WAS STEADILY CLIMBING ABOVE 120 DEGREES C. FOUND CARBON DEPOSIT ON MAIN OIL SCREEN. REMOVED AND REPLACED OIL SCREEN PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999040900135 19990409 00135 NM 1999 4 9 SWAA990590 1 19990328 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 CREW REPORTS EGRESS LIGHT COVER MISSING IN REAR PAX CABIN. REMOVED AND REPLACEDR EGRESS LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 1999040900136 19990409 00136 NM 1999 4 9 SWAA990591 1 19990329 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374SW 26582 CABIN EMERGENCY ESCAPE FLOOR TRACK LIGHTING INOP AT FWD SECTION. RESECURED LOOSE WIRE AT SECTION. 2 L 7 2 4F RT A16WE 1999040900137 19990409 00137 NM 1999 4 9 SWAA990592 1 19990328 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 12 EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379SW 26586 EGRRESS WIRING EXPOSED AT ROW 12. REPLACED FLOOR TRACK LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999040900138 19990409 00138 NM 1999 4 9 SWAA990593 1 19990328 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM LT EMER EXIT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 624SW 27934 EMERGENCY EXIT SIGN LENS MISSING FROM MID CABIN ABOVE LEFT OVERWING DOOR (PASSENGER TOOK IT). REINSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 1999040900139 19990409 00139 NM 1999 4 9 SWAA990594 1 19990328 A 2560 61620 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 626SW 27702 FWD ENTRY DOOR SLIDE ASSY LOOSE. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900140 19990409 00140 NM 1999 4 9 SWAA990595 1 19990328 A 5320 BAC1505 ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA CHORDS CRACKED AT LBL AND RLB 28.5, BS 178. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900141 19990409 00141 NM 1999 4 9 SWAA990596 1 19990328 A 5240 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, AFT DOOR FRAME CRACKED IN TWO LOCATIONS; 3RD AND 4TH FRAME CUT OUTS . REPLACED DOOR ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900142 19990409 00142 NM 1999 4 9 SWAA990597 1 19990328 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 13R CRACKED AT BS 290. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999040900143 19990409 00143 NM 1999 4 9 SWAA990598 1 19990328 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D CHECK, FOUND 5 EA FRAMES CRACKED BETWEEN STR 8-9L, BS 827, 867, 907, AND BETWEEN STR 8-9R, BS 787, 86 7. REAPAIRED FRAMES PER ER NR 99-0283. 2 L 7 2 4F RT A16WE 1999040900144 19990409 00144 NM 1999 4 9 SWAA990599 1 19990329 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 3 & 6 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED BC3 CHECK, FOUND 2 EA EMERGENCY ESCAPE LIGHT TRACKS OUT AT ROWS 6 AND 3. RELAMPED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999040900145 19990409 00145 NM 1999 4 9 SWAA990600 1 19990329 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED BC3 CHECK, FOUND MAIN ENTRY AISLE EMERGENCY EXIT LIGHT MISSING LENS. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999040900146 19990409 00146 NM 1999 4 9 SWAA990601 1 19990329 A 3350 MS24693530 SCREW BOEING 737 7373H4 1384600 NM LT EMER EXIT EEL MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND LEFT OVERWING EXIT SIGN LAMP RETAINING SCREW MISSING. REMOVED AND REPLACED SCREW PER MM. 2 L 7 2 4F RT A16WE 1999040900147 19990409 00147 NM 1999 4 9 SWAA990602 1 19990329 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM REAR CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 94SW 23053 DURING SCHEDULED OVERNIGHT CHECK, FOUND OVERHEAD EXIT LIGHTS FLICKERING AT REAR OF CABIN. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F A16WE 1999040900148 19990409 00148 NM 1999 4 9 SWAA990603 1 19990330 A 3350 079123 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 EMERGENCY FLOOR TRACK LIGHT HAS MID CABIN LENS MISSING. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999040900149 19990409 00149 NM 1999 4 9 SWAA990604 1 19990330 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 626SW 27702 FWD ENTRY ESCAPE SLIDE FELL OUT WHILE TRYING TO CLOSE DOOR FOR DEPARTURE. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900150 19990409 00150 1999 4 9 SWAA990605 4 19990330 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 644SW 28329 L-2 DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900151 19990409 00151 NM 1999 4 9 SWAA990606 1 19990330 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED 1/4D CHECK, FOUND THROUGH ULTRASONIC INSPECTION 4 EA CRACKS AT BS 178 BULKHEAD, LBL14-RBL13. REPAIRED C RACKS PER DALFORT XEA'S X2-53-242 AND X2-53-243. 2 L 7 2 4F A16WE 1999040900152 19990409 00152 NM 1999 4 9 SWAA990607 1 19990330 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAMS, BS 727E LBL3, BS 767, LBL8, BS 807, LBL18, AND BS 827, LBL 1 8. REPAIRED BEAMS PER SWA REPAIR AUTH 1-A53-2021. 2 L 7 2 4F RT A16WE 1999040900153 19990409 00153 NM 1999 4 9 SWAA990608 1 19990330 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LT LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED C2 CHECK, FOUND NR 2 LE SLAT INBD AUX TRACK CUT OUT CRACKED AT BOTH CORNERS. REPAIRED PER SWA RA NR 135 7-0423. 2 L 7 2 4F RT A16WE 1999040900154 19990409 00154 NM 1999 4 9 SWAA990609 1 19990330 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 3 & 5 INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP AT ROWS 3 AND 5. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999040900155 19990409 00155 NM 1999 4 9 SWAA990610 1 19990330 A 3350 65C27095 BATTERY CHARGER BOEING 737 7373H4 1384600 NM RT EMER EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999040900156 19990409 00156 NM 1999 4 9 SWAA990611 1 19990330 A 5320 6546529 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CRACK AT DOOR CUT OUT FRAME, BS 492. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999040900157 19990409 00157 NM 1999 4 9 SWAA990612 1 19990330 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 359 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CRACK AT STRINGER 14L, BS 359. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900158 19990409 00158 NM 1999 4 9 SWAA990613 1 19990330 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 440 & 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND 2 EA CRACKED FRAMES AT BS 440 AND 480, BETWEEN STRINGERS 8L-9L. REPAIRED PER SRM AND ER NR 99-0283. 2 L 7 2 4F RT A16WE 1999040900159 19990409 00159 NM 1999 4 9 SWAA990614 1 19990330 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 4 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND NR 4 SLAT 2 EA CRACKS AT LAST ROW OF RIVETS JUST OUTBOARD OF ACTUATOR ROD END. REPAIR ED PER BOEING DRAWING 65C30133 AND ER 99-5204. 2 L 7 2 4F RT A16WE 1999040900160 19990409 00160 NM 1999 4 9 SWAA990615 1 19990330 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND 3EA CRACK AT BS 178 BULKHEAD, BETWEEN RBL1-RBL7. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900161 19990409 00161 NM 1999 4 9 SWAA990616 1 19990331 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 900 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED STRINGER 24R, BS 900. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999040900162 19990409 00162 NM 1999 4 9 SWAA990617 1 19990331 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING WALKAROUND INSPECTION, FOUND A 3.1 INCH LONG CRACK AT FUSELAGE SKIN, BS 5OOB, STRINGER 10R. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 1999040900169 19990409 00169 EU 1999 4 9 99ZZZX1434 1 19990225 A 6320 4638001001 TRANSMISSION BOLKMS 105 BO105C 5626005 EU MAIN ROTOR MAKING METAL A NYSA O OTHER O OTHER NR NOT REPORTED 1 EA 23 90752 9556 1179 690 S156 PILOT REPORTED TRANSMISSION CHIP LIGHT. FOUND NO DEBRIS. RETURNED AIRCRAFT TO SERVICE. PILOT REPORTED TRANSMISSION CHIP LIGHT AGAIN. FOUND ONE SLIVER ON CHIP DETECTOR. AIRCRAFT TAKEN OUT OF SERVICE TO EVALUATE TRANSMISSION FOR BEARING FA ILURES. 1 G 7 2 3U H3EU 1999040900181 19990409 00181 NE 1999 4 9 99ZZZX1446 2 19990222 A 8530 VALVE DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE LT ENGINE INOPERATIVE A VLLA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 05 36AP 6183 305 13439 CP363471 DAY/NB9 - EN ROUTE AT CRUISE POWER, LEFT ENGINE STARTED RUNNING ROUGH. DIVERTED TO TDZ. FOUND ALL REAR CYLINDER VALVES N OT MOVING. SUSPECT REAR CAM RING FAILURE. 2 L 7 2 4R 4 R A669 5E4 1999040900194 19990409 00194 SO 1999 4 9 99ZZZX1459 2 19990326 A 8530 649166R CYLINDER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO ENGINE LEAKING A ACSA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 6790B 707 011698 402C0442 811195R DURING ROUTINE ENGINE, 100-HOUR INSPECTION FOUND CYLINDER NR 3 COMPRESSION 15/80 LEAKING BY INTAKE VALVE AND RINGS. 1 L 7 2 3O 3 O A7CE E8CE 1999040900198 19990409 00198 WP 1999 4 9 TWAA9904901 1 19990401 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 2 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9413T 53188 THE EGRESS LIGHT AT CABIN ROW 2 HAD WIRE LOOSE FROM THE LIGHT AND THE COVER WAS MISSING. REPLACED THE WIRE SEGMENT AND I NSTALLED COVER. CHECK-C 9-1-98 STL. 2 L 7 2 4F RT A6WE 1999040900199 19990409 00199 NM 1999 4 9 TWAA9904902 1 19990403 A 3350 CONNECTOR BOEING 767 767231 1385131 NM ROW 23-30 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 606TW 22569 FOUND FLOOR EGRESS LIGHT INOPERATIVE ON RT SIDE AT CABIN ROWS 23 TO 30. FOUND CONNECTOR NOT SECURE AND RESEATED THE CONN ECTOR ON THE POWER SUPPLY. CHECK-C 3-21-99 LAX. 2 L 7 2 4F RT A1NM 1999040900200 19990409 00200 WP 1999 4 9 TWAA9904903 1 19990404 A 5530 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT CHECK, FOUND .75 INCH CRACK AT THE LT DORSAL FIN ATTACH ANGLE AT STA 1421. INSTALLED NEW ATTACH ANG LE PER SVC BULLETIN 53-2234, SB 09530162. 2 L 7 2 4F A6WE 1999040900201 19990409 00201 WP 1999 4 9 TWAA9904904 1 19990323 A 5320 CASTING DOUG DC9 DC931 3022065 WP BS 639 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND FORMER CASTING CRACKED AT STA 639, APPROX 58.2 IN RBL. REPLACED FORMER PER SPM 6-70-01, PAGE 3 ITEM B. 2 L 7 2 4F A6WE 1999040900202 19990409 00202 WP 1999 4 9 TWAA9904905 1 19990323 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP BS 636 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, THE RT FUSELAGE AT STA 636, LONGERON 24R TO 25R, HAD DAMAGE AT C2 CARGO FORWARD THRESHOLD EDGE . CUT OUT DAMAGED AREA OF THRESHOLD EDGE AND REPAIRED PER SRM 53-05, FIG 82. 2 L 7 2 4F A6WE 1999040900203 19990409 00203 WP 1999 4 9 TWAA9904906 1 19990322 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 208 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND CORROSION ON DOOR CUTOUT ATTACH TO FLOOR AT STA 208, LONGERON 18L. REPLACED FLOOR ATTACH ANGLE PER TWA STD PROCESSES MANUAL 6-70-01, PARA B. 2 L 7 2 4F A6WE 1999040900204 19990409 00204 WP 1999 4 9 TWAA9904907 1 19990322 A 5321 FLOOR DOUG DC9 DC982 3022082 WP GALLEY DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, THE FIRST FLOOR PANEL I/B OF FWD GALLEY DOOR JAMB HAD CORROSION. FABRICATED FLOOR PANEL AND 2 NEW EVAC SLIDE CASTINGS. PRIMED AND PAINTED WHITE. 2 L 7 2 4F A6WE 1999040900205 19990409 00205 WP 1999 4 9 TWAA9904908 1 19990318 A 5620 WINDOW DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON FWD EDGE AND AFT EDGE OF WINDOW 31 ON RT SIDE. BLENDED PER SRM 53-05, FIG 111 AND INSTALLED DOUBLER PER ARA 16105. 2 L 7 2 4F A6WE 1999040900206 19990409 00206 WP 1999 4 9 TWAA9904909 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 579 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND LT SIDE WALL SUPPORT CRACKED AT LOWER END, STA 579 AND WL 167. FABRICATED NEW ANGLE AND REINSTALLED WITH AD RIVETS, PER SRM 51-01 PAGE 1 ITEM C. 2 L 7 2 4F A6WE 1999040900207 19990409 00207 WP 1999 4 9 TWAA9904910 1 19990327 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND BELOW ELECTRIC POWER CABLE RACEWAY AT STA 718 APPROX LBL 54 IN, A CRACKED T FITTING. REP LACED FITTING PER SPM 6-70-01 AND INSTALLED HI-LOKS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1999040900208 19990409 00208 WP 1999 4 9 TWAA9904911 1 19990329 A 5320 FLOOR DOUG DC9 DC982 3022082 WP BS 1280 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CRACKED AT LT STA 1280 AT SIDEWALL. CRACKS WERE REPAIRED PER SRM 53-05, P G 349. 2 L 7 2 4F A6WE 1999040900209 19990409 00209 WP 1999 4 9 TWAA9904912 1 19990315 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND LONGERON 4L CRACKED AT STA 160, AT O/B FASTENER. SPLICED IN NEW SECTION PER SRM 51-01, P G 1 AND 53-02, PAGE 48, FROM STA 148 TO 170. 2 L 7 2 4F A6WE 1999040900210 19990409 00210 WP 1999 4 9 TWAA9904913 1 19990325 A 5320 FLOOR DOUG DC9 DC982 3022082 WP BS 1287-1309 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED AND CORRODED APPROX STA 1287 TO 1309, RBL 52 IN. REPLACED M EMBRANE PART NR 9930612-11, PER SPM 6-70-01, PAGE 3. INSTALLED WITH FASTENERS PER SPM 6-30-07 PG 1 AND 2. 2 L 7 2 4F A6WE 1999040900211 19990409 00211 WP 1999 4 9 TWAA9904914 1 19990325 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 1271-1287 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED AND CORRODED AT STA 1271 TO 1287, RBL 52 IN. REPLACED MEMBR ANE WITH (P/N 9930612-11), PER SPM 6-70-01, PG 3. INSTALLED WITH FASTENERS PER SPM 6-30-01, PG 1 AND 2. 2 L 7 2 4F A6WE 1999040900212 19990409 00212 WP 1999 4 9 TWAA9904915 1 19990326 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1256 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND SKIN CORRODED UNDER 27R, STA 1256. CUT OUT CORRODED SECTION OF SKIN PER SRM 53-04 AND IN STALLED DOUBLER PER SRM 53-04. 2 L 7 2 4F A6WE 1999040900213 19990409 00213 WP 1999 4 9 TWAA9904916 1 19990325 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 110 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND RT SIDE OF FUSELAGE WITH STATIC BURN AT STA 110, 24 IN BELOW RT SLIDING WINDOW. BLENDED OUT PER SRM 53-04. NDT SHOWED CRACK WHICH WAS REPAIRED PER SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1999040900214 19990409 00214 WP 1999 4 9 TWAA9904917 1 19990325 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 826 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CABIN CHAIR TRACK AT LBL 55 IN, STA 826. REMOVED CORROSION PER SPM 6-80-2. FOUND OUT OF LIMITS PER SRM 53-05, FIG 4B. INSTALLED NEW TRACK PER SPM 6-70-01, PG 3. 2 L 7 2 4F A6WE 1999040900215 19990409 00215 WP 1999 4 9 TWAA9904918 1 19990325 A 5347 TIE DOWN DOUG DC9 DC982 3022082 WP BS 322-370 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND FWD CARGO COMPT RT TIE DOWN TRACK GROUND BEYOND LIMITS AT STA 322 TO 370. REPLACED RT TI E DOWN TRACK PER SPM 6-70-01, PG 2 AND 3, PARA 4A. 2 L 7 2 4F A6WE 1999040900216 19990409 00216 WP 1999 4 9 TWAA9904919 1 19990324 A 5320 FASTENER DOUG DC9 DC982 3022082 WP BS 1452 MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND FASTENER HEAD MISSING 6 INCHES UP FROM FUSELAGE STA 1452. INSTALLED 2 HL439-6-7 PER TWA STD PROCESSES MANUAL 6-70-01. 2 L 7 2 4F A6WE 1999040900217 19990409 00217 WP 1999 4 9 TWAA9904920 1 19990324 A 5510 LUG DOUG DC9 DC982 3022082 WP HORIZ STAB CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND HORIZ STAB LT PIVOT BEARING LUG WITH CORROSION. REAMED AND SPOT FACED PER SRM 55-02, MAN UFACTURED AND INSTALLED BUSHING PER SRM 55-02. INSTALLED NEW PIVOT BEARING PER MM 55-10-00. 2 L 7 2 4F A6WE 1999040900218 19990409 00218 WP 1999 4 9 TWAA9904921 1 19990324 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 218 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND IN FWD CARGO COMPT A CRACK AT CARGO FLOOR SUPPORT CHANNEL, STA 218, ABOVE LONGERON 25L. EDDY CURRENT CHECK INDICATED CRACK IN FORMER RADIUS. REPAIRED CRACKED FORMER PER SRM 53-01, PAGE 10 FIG 2. 2 L 7 2 4F A6WE 1999040900219 19990409 00219 WP 1999 4 9 TWAA9904922 1 19990326 A 5320 PRESSURE DECK DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING OP 16 MAINT CHECK, FOUND IN LT WHEEL WELL APPROX .5 IN CRACK AFT SIDE OF 718 CASTING, IN PRESSURE DECK. REPLACED NEW PLATE AND FASTENERS PER SRM 51-30-0. MADE NEW PART PER SPM 6-70-01, ITEM 4A, DRAWING 991015. 2 L 7 2 4F A6WE 1999040900220 19990409 00220 WP 1999 4 9 TWAA9904923 1 19990323 A 5320 FRAME DOUG DC9 DC982 3022082 WP PAX DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING OP 16 MAINT CHECK, FOUND DOOR CUT OUT FRAME FOOT O/B OF LONGERON 30 AND STA 629, HAD CORROSION. REMOVED FASTENER AND REMOVED AND CLEANED CORROSION FROM AREA. REMOVED BRACKET TO ACCESS AREA. REINSTALLED BRACKET PER SPM 6-70-01, PG 2 AND 3. 2 L 7 2 4F A6WE 1999040900221 19990409 00221 NM 1999 4 9 TWAA9904924 1 19990331 A 5310 STRUCTURE BOEING 767 767231 1385131 NM BS 478 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 THE FUSELAGE SKIN WAS DAMAGED AT ST 478, STRINGER 35L, WITH STRINGER PUSHED IN .5 IN BY 7 IN BY 9 IN AREA. SKIN ON FORME R RING WAS BUCKLED .25 IN. SPLICED DOUBLER ON STRINGER. REPLACED SHEAR TIES AND RIVETS PER SRM 51-10-00. REMOVED DAMAG ED AREA AND INSTALLED 24 IN BY 24 IN DOUBLER PER SRM 53-00-01 AND 53-30-01. CHECK-C WAS ACCOMPLISHED DURING THE REPAIR. 2 L 7 2 4F RT A1NM 1999040900222 19990409 00222 WP 1999 4 9 AT9900274 1 19990401 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP BATTERY PACK DIRTY A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 810AT 47277 RIGHT HAND NACELLE LIGHT WILL NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS TURNED ON. CLEANED CANNON PLUG PINS AT BATTE RY PACK PER MM 33-35-0, OPS CHECKS GOOD. 2 L 7 2 4F A6WE 1999040900223 19990409 00223 WP 1999 4 9 AT9900275 1 19990325 A 5320 JAMB DOUG DC9 DC932 3022066 WP PAX DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT ENTRANCE LOWER DOOR JAMB LEFT CORNER CORRODED. DISASSEMBLE AFT ENTR ANCE THRESHOLD AREA, REMOVED CORRODED WEB ON LEFT AND RIGHT SIDES. FORMED NEW WEBS, DRILLED, TRIMMED, DEBURRED, ALODINE D, PRIMED, AND INSTALLED AND REINSTALLED ALL PARTS PREVIOUSLY REMOVED FOR ACCESS IAW DC9 SRM 51-10-4, 51-10-3, 51-10-2, 51-30-2, 51-30-5, DRAWING NR 5917579, AND RES NR 99591. 2 L 7 2 4F A6WE 1999040900224 19990409 00224 WP 1999 4 9 AT9900276 1 19990302 A 5347 1A436191 TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT RIGHT HAND TRACK BOTTOM SIDE CORRODED THROUGHOUT. REMOVED C ORROSION, LOCATED NEW TRACK, DRILLED, COUNTERSUNK, DEBURRED, TREATED, AND PRIMED IAW DC9 SRM 53-05 FIG 4C, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999040900225 19990409 00225 WP 1999 4 9 AT9900277 1 19990303 A 5347 1A436171 TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT RIGHT SIDE FLOOR TRACK CORRODED ON BOTTOM FULL LENGTH. FABRICAT ED, DRILLED, DEBURRED, PRIMED, AND TREATED IAW DC9 SRM 53-05 FIG 4C, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999040900226 19990409 00226 NM 1999 4 9 CALA9900343 1 19990331 A 5230 BEAM BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND IMPACT DAMAGE TO AFT CARGO DOOR LOWER EDGE BEAM AND FORWARD CORNER PIECE. THE LOWER EDGE BEAM AND FORWA RD CORNER PIECE WERE REPLACED IAW BOEING DRAWING 143N6603 AND SRM 52-30-02. 2 L 7 2 4F RT A2NM 1999040900227 19990409 00227 NM 1999 4 9 CALA9900344 1 19990331 A 5230 BEAM BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND IMPACT DAMAGE TO AFT VERTICAL EDGE BEAM, LOWER BEAM, AFT AND FORWARD CORNER PIECES OF FORWARD CARGO DOO R. THE BEAMS AND CORNER PIECES WERE REPLACED IAW BOEING DRAWING 143N6603 AND SRM 52-3-02. 2 L 7 2 4F RT A2NM 1999040900228 19990409 00228 NM 1999 4 9 CALA9900345 1 19990331 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 727 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FLOOR SUPPORT ANGLES AT LBL 3, RBL 3, LBL 8, AND RBL 8, STA 727D CORRODED. A REPAIR DOUBLER WAS INSTALL ED AT EACH LOCATION IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 1999040900229 19990409 00229 WP 1999 4 9 CALA9900346 1 19990331 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO PIT DOOR BRACKET AT AFT DOOR LATCHING MECHANISM. A NEW BRACKET WAS IN STALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1999040900230 19990409 00230 NM 1999 4 9 CALA9900347 1 19990331 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND A 9 INCH CRACK IN FUSELAGE SKIN JUST UNDER FORWARD END OF NR 3 ENGINE PYLON. REPAIRED IAW SRM 53-30-3, FIGURE 3 SHEET 1. 2 L 7 3 4F A3WE 1999040900231 19990409 00231 WP 1999 4 9 CALA9900348 1 19990401 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A .75 INCH CRACK AT BOTH ENDS OF NR 1 BEAM AND A .75 INCH CRACK AT FORWARD END OF NR 4 BEAM OF FORWARD SERVICE DOOR. BOTH BEAMS WERE REPLACED IAW SRM 51-30-2 AND 51-30-3. 2 L 7 2 4F A6WE 1999040900232 19990409 00232 NM 1999 4 9 CALA9900349 1 19990401 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. A REPAIR WAS INSTALLED IAW ECRA 5310-03836. 2 L 7 2 4F RT A16WE 1999040900233 19990409 00233 WP 1999 4 9 CALA9900350 1 19990401 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 1338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A 1 INCH CRACK IN FINGER DOUBLER AT STA 1338, LONGERON 18R JUST FORWARD OF APB T-CAP. A NEW FINGER DOUB LER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999040900234 19990409 00234 WP 1999 4 9 CALA9900351 1 19990401 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND DOUBLER CORRODED AT STA 1338, LONGERON 18L. A NEW SPLICE DOUBLER WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999040900235 19990409 00235 NM 1999 4 9 CALA9900352 1 19990401 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND C-1 DOOR SKIN DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 1999040900236 19990409 00236 WP 1999 4 9 CALA9900353 1 19990402 A 5210 SKIN DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND A .5 INCH CRACK IN FORWARD ENTRY DOOR SKIN AT LOWER FORWARD CORNER OF DOOR EDGE. A REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 32, SHEET 2 AND 3. 2 L 7 2 4F A6WE 1999040900238 19990409 00238 1999 4 9 COMA9910053 4 19990403 A 3442 6222504001 ANTENNA EMB 120 EMB120RT SO RADAR SYSTEM INOPERATIVE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 258CA 27855 120247 RADAR TILT FUNCTION IS INOPERABLE. REPLACED ANT 318. 2 L 7 2 4T RT A31SO 1999040900239 19990409 00239 SO 1999 4 9 COMA9910054 1 19990403 A 3230 CONNECTOR EMB 120 EMB120RT SO LANDING GEAR LOOSE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 255CA 120238 LANDING GEAR SELECTOR LOCK DID NOT RELEASE AFTER TAKEOFF. SECURED LOOSE AIR/GROUND SENSOR WIRING CONNECTION (PO316). 2 L 7 2 4T RT A31SO 1999040900240 19990409 00240 SO 1999 4 9 COMA9910055 1 19990405 A 5320 12020235003 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 264CA 120256 DURING REPLACEMENT OF A BROKEN CARGO DOOR LIFTING MECHANISM TORSION BAR, THE FORWARD STRUCTURAL SUPPORT BRACKET FOR THE TORSION BARS WERE FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORTS NR 1397-1, REV IR, DATED 2/15/95, AND NR 1397-2, REV IR, DATED 4/5/99. 2 L 7 2 4T RT A31SO 1999040900241 19990409 00241 EA 1999 4 9 COMA9960143 1 19990402 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937CA 7044 FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. CLEANED WIRING CONNECTIONS AT FLOOR LIGHTING. 2 L 7 2 4F RT A21EA 1999040900242 19990409 00242 EA 1999 4 9 COM A996014 1 19990404 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA EMERGENCY EXIT FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 991CA 7216 OVERWING EMERGENCY EXIT SIGN IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999040900243 19990409 00243 NM 1999 4 9 UPS99229167 1 19990403 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMERGENCY EXIT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, R-1 DOOR EMERGENCY EXIT LIGHT ON CEILING FWD POSTION INOP. REMOVED AND REPLACED BATTERY PACK, OPS C HECK NORMAL. 2 L 7 3 4F A3WE 1999040900244 19990409 00244 NM 1999 4 9 UPS99229168 1 19990403 A 3520 MASK BOEING 727 72725C 138400H NM ROW 6 FELL OUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, O2 MASKS ROW C ON LEFT SIDE OF CABIN FELL OUT. STOWED O2 MASKS AT ROW 6 LT SIDE. 2 L 7 3 4F A3WE 1999040900245 19990409 00245 NM 1999 4 9 UPS99229169 1 19990402 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM R1 DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, R-1 DOOR EMERGENCY EXIT LIGHT ON CEILING FWD POSTION INOP. REMOVED AND REPLACED BATTERY PACK, OPS C HECK NORMAL. 2 L 7 3 4F A3WE 1999040900246 19990409 00246 WP 1999 4 9 ABXA9900269 1 19990331 A 5720 59161751 FITTING DOUG DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 KEEL WEB FORWARD ATTACH ANGLE FITTING CRACKED AT LEFT SIDE. REPLACED ANGLE IAW DC9 SRM 51-30-3 AND 51-30-1. 2 L 7 2 4F A6WE 1999040900247 19990409 00247 WP 1999 4 9 ABXA9900270 1 19990402 A 5753 5910041506 VANE DOUG DOUG DC9 DC931 3022065 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 RIGHT FLAP INBOARD FIXED VANE DELAMINATED 2 PLACES ON LOWER SURFACE. REPLACED VANE ASSEMBLY IAW DC9 MM 27-51-3. 2 L 7 2 4F A6WE 1999040900248 19990409 00248 WP 1999 4 9 ABXA9900271 1 19990330 A 5320 9919402505 TRAPEZOID PANEL DOUG DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LEFT TRAPEZOIDAL PANEL UPPER OUTBOARD FLANGE CRACKED STARTING AT 6TH FASTENER HOLE RUNNING THROUGH 8TH FASTENER HOLE INT O RADIUS OF THE VERTICAL FLANGE. REPLACED TRAPEZOIDAL PANEL IAW DC9 S/B'S 53-10D, 53-115 AND 53-182. 2 L 7 2 4F A6WE 1999040900249 19990409 00249 WP 1999 4 9 ABXA9900272 1 19990401 A 5320 56191999501 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1640-4680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 DOUBLER CRACKED AT STATION 1640 TO 1680. REPAIRED DOUBLER IAW ABX REA D853-27021MR. 2 L 7 4 4F 4A25 1999040900250 19990409 00250 WP 1999 4 9 ABXA9900273 1 19990329 A 3230 7000010101 SWITCH DOUG DC9 DC933F 302207A WP RT MLG INTERMITTENT A ABXA K NONE O OTHER CR CRUISE 1 GL 23 931AX 47384 RIGHT MAIN LANDING GEAR FAILED UPLATCH CHECK ON INITIAL TRY. RECYCLED GEAR, OPS CHECKED GOOD. REPLACED RIGHT MAIN LANDIN G GEAR UP LIMIT SWITCH. 2 L 7 2 4F A6WE 1999040900251 19990409 00251 NM 1999 4 9 DL72K990661 1 19990325 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM L2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 417DA 21259 L2 EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS GOOD. 2 L 7 3 4F A3WE 1999040900252 19990409 00252 NM 1999 4 9 DL72K990662 1 19990326 A 5330 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 DURING ACCOMPLISHMENT OF SI 4-74176-12AD, SEVERAL CRACK INDICATIONS WERE NOTED IN THE S4L LAP JOINT BETWEEN BS 360 AND 4 80. FOUR CRACKS WERE CONFIRMED, IN THREE DIFFERENT STRINGER BAYS. REPAIRED PER ERA 332943-14AD, REV A. 2 L 7 3 4F A3WE 1999040900253 19990409 00253 NM 1999 4 9 DL72K990663 1 19990326 A 5330 SKIN BOEING 727 727232 1384082 NM BS 420 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 DURING ACCOMPLISHMENT OF INSPECTIONS PER SI 4-74176-12AD SIX CRACK INDICATIONS WERE NOTED AT THE S4R LAP JOINT FROM BS 3 60 TO 480. THE SIX CRACKS WERE LOCATED IN THREE DIFFERENT FRAME BAYS. REPAIRED PER ERA 332940-14AD. 2 L 7 3 4F A3WE 1999040900254 19990409 00254 NM 1999 4 9 DL72K990664 1 19990326 A 5330 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 INSPECTION PER SI 4-74176-12AD, RESULTED IN 24 CRACK INDICATIONS FOUND IN THE S4R LAP JOINT BETWEEN BS 481 AND BS 681. T HE 24 CRACK INDICATIONS WERE LOCATED IN SEVEN DIFFERENT FRAME BAYS. REPAIRED PER ERA 332941-14AD. 2 L 7 3 4F A3WE 1999040900255 19990409 00255 NM 1999 4 9 DL72K990666 1 19990326 A 5330 SKIN BOEING 727 727232 1384082 NM BS 681-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 INSPECTIONS PER SI 4-74176-12AD, RESULTED IN FINDING 15 CRACK INDICATIONS IN THE S4R LAP JOINT BETWEEN BS 681 AND BS 740 . THE 15 CRACK INDICATIONS WERE LOCATED IN THREE DIFFERENT FRAME BAYS. REPAIRED PER ERA 332942-14AD. 2 L 7 3 4F A3WE 1999040900256 19990409 00256 NM 1999 4 9 DL72K990668 1 19990326 A 5753 652163262 SKIN BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 NR 3 MIDFLAP/UPPER SKIN WBL 70 TO 106, WEAR DAMAGE FOUND TO NR 3 MIDFLAP UPPER SKIN DUE TO INTERFERENCE WITH FOREFLAP. W EAR AREA IS APPROX 37.5 SPAN-WISE X 7.5 CHORD-WISE. INSTALLED INTERNAL TITANIUM DOUBLER FOR FLUSH REPAIR. 2 L 7 3 4F A3WE 1999040900257 19990409 00257 WP 1999 4 9 DLL19990669 1 19990326 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 760DH 37560 193Y1194 EMERGENCY LIGHT BATTERY WILL NOT HOLD CHARGE. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1999040900258 19990409 00258 NM 1999 4 9 DL72S990675 1 19990328 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 409DA 21153 FWD AISLE EMERGENCY LIGHT STAYED ON. REPLACED EMERGENCY LIGHT RACK AND BATTERY, OPS CK OK. 2 L 7 3 4F A3WE 1999040900259 19990409 00259 NM 1999 4 9 DL72W990677 1 19990319 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BONDED DOUBLER - CORRODED FS 72OB AND JUST BELOW STR 4R. REPAIRED PER SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900260 19990409 00260 NM 1999 4 9 DL72W990678 1 19990318 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 620 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BONDED DOUBLER, CORRODED FS 620 FROM STR 1R TO 4L. REPAIRED PER SRM 53-30-4, METHOD 2, (4). WITHIN LIMITS PER SRM 53-30 -4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900261 19990409 00261 NM 1999 4 9 DL72W990679 1 19990318 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 600 & 620 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BONDED DOUBLERS, CORRODED FS 600 TO 620 AT STR 4R O/B SIDE OF STR AND SPLICE CORRODED ON I/B SIDE OF STR 22. REPAIRED PE R SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, H. OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900262 19990409 00262 NM 1999 4 9 DL72W990680 1 19990318 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 580 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BONDED DOUBLER, CORRODED FS 580 FROM STR 4L TO 4R. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30- 4 METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900263 19990409 00263 NM 1999 4 9 DL72W990681 1 19990318 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 560 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BONDED DOUBLER, CORRODED FS 560 STR 4L TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 MET HOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900264 19990409 00264 NM 1999 4 9 DL72W990682 1 19990318 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 560-580 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 DOUBLER CORRODED FS 560 TO 580 STR 1-2R. REPAIRED PER SRM 53-30-4, METHOD 2, H. WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900265 19990409 00265 NM 1999 4 9 DL72W990683 1 19990318 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 520-540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BONDED DOUBLER, CORRODED FS 520 TO 540 FROM STR 4R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900266 19990409 00266 NM 1999 4 9 DL72W990684 1 19990318 A 5320 DOUBLER BOEING 727 727247 138408F NM BS 500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BONDED DOUBLER, CORRODED FS 500 STR 3R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4, ME THOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K). 2 L 7 3 4F A3WE 1999040900267 19990409 00267 WP 1999 4 9 DLL13990665 1 19990325 A 5414 PANEL LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 100 193A1143 010527 FOUND ON WALKAROUND, NR 1 ENG PYLON PANEL 451FT DAMAGED. FABRICATED NEW PANEL PER ERA 367054-14. 2 L 7 3 4F 4 F A23WE E12EU 1999040900268 19990409 00268 NM 1999 4 9 DL72S990667 1 19990326 A 3610 CLAMP BOEING 727 727232 1384082 NM AC BAY BROKEN A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 531DA 21814 AFTER PUSHBACK, HEARD LOUD BANG AND EXPERIENCED SMOKE IN CABIN. FOUND CLAMP OFF DUCT IN AREA OF FLOW MULT REF IPC 21-10- 0-4 ONLY AFFECTS AIR FROM APU. PUT APU AIR TO MCO AND PLACARD. 2 L 7 3 4F A3WE 1999040900269 19990409 00269 NM 1999 4 9 DL72S990671 1 19990327 A 2497 WIRE BOEING 727 727232 1384082 NM LT GENERATOR FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 533DA 22046 LT GENERATOR ON LANDING, LOUD SOUND OF GENERATOR FAILING. ELECTRICAL SMELL IN COCKPIT. DIFF FAULT LIGHT ON ANN PANEL. M TC FOUND BURNT WIRES GOING TO DISTRIBUTION 1 SECT X C/B C829. REPAIRED WIRING PER M/M. 2 L 7 3 4F A3WE 1999040900270 19990409 00270 1999 4 9 DLM88990673 4 19990327 A 3425 4608000307 AHRS DOUG MD88 MD88 3023688 NM E/E COMPT MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 977DL 53258 AT APPROX 100 KTS ON T/O ROLL, GOT HORIZON, NO AUTO LAND AND MONITOR LIGHTS ON FMA. F/O'S ATTITUDE DISPLAY INDICATED FAI LURE (NO HORIZON). ABORT SPEED 120 KTS, MAX BRAKE TEMP 250 DEG CELSIUS. REMOVED AND REPLACED NR 2 AHRS UNIT PER M/M 34 -21-10, ALL CKS OK. 2 L 7 2 4F RT A6WE 1999040900271 19990409 00271 WP 1999 4 9 DLL14990674 1 19990326 A 2612 FIRE WIRE LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 741DA 193C1245 NR 2 ENG A LOOP WARNING OCCURRED AFTER TAKEOFF AT 1500 FT AGL. REPAIRED WIRING ON ENGINE AND IN SPLITTER AREA. 2 L 7 3 4F A23WE 1999040900272 19990409 00272 NM 1999 4 9 DL76S990685 1 19990329 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 123DN 23437 DURING ROUTINE MAINTENANCE, THE LEFT AND RIGHT EMERGENCY EXIT THRESHOLD LIGHTS FOUND INOP. REPLACED POWER SUPPLY, OPS CK NORMAL. 2 L 7 2 4F RT A1NM 1999040900273 19990409 00273 NM 1999 4 9 DLM88990686 1 19990325 A 2910 AE7055381 LINE DOUG MD88 MD88 3023688 NM NR 2 ENGINE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 903DE 53380 LOST RIGHT HYDRAULIC QUANTITY AND PRESSURE ON CLIMBOUT FROM KJAX. REPLACED ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE TH ROUGH PYLON. SERVICED RIGHT HYD SYSTEM. LEAK CHECK GOOD. REPLACED NR 2 ENG CASE DRAIN AND PRESSURE FILTERS. NO METAL FOUND. OPN AND LEAK GOOD. 2 L 7 2 4F RT A6WE 1999040900274 19990409 00274 NM 1999 4 9 DL757990687 1 19990329 A 3040 WIRE 141T480119 BOEING 757 757232 1384965 NM LT WINDSHIELD FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 601DL 22808 STRONG FUMES IN COCKPIT. DIVERTED TO RDU. FOUND WIRING AT 1L FWD WINDSHIELD SMOKING. DEACTIVATED WINDOW HEAT SYS PER M EL 30-41-01A. 2 L 7 2 4F RT A2NM 1999040900275 19990409 00275 NM 1999 4 9 DL72S990688 1 19990329 A 5245 ANGLE BOEING 727 727232 1384082 NM DOOR 3448R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 FOUND ON D2 LETTER CK, CORROSION ON ATTACH ANGLE FOR A/C DOOR 3448R. REPAIRED PER MM 53-30-1. 2 L 7 3 4F A3WE 1999040900276 19990409 00276 NM 1999 4 9 DLM88990689 1 19990329 A 3350 41B004ADO73 BATTERY DOUG MD88 MD88 3023688 NM BS 211 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DE 53416 EMERGENCY LIGHT IN COCKPIT OVERHEAD AND GALLEY/FWD ENTRY OVERHEAD EMERGENCY LIGHTS WOULD NOT TEST DURING LAYOVER. REPLAC ED BATTERIES AT FS 211 LOCATED IN OVERHEAD DROP DOWN PANEL. 2 L 7 2 4F RT A6WE 1999040900277 19990409 00277 NM 1999 4 9 DL72W990691 1 19990330 A 5330 655458041 SKIN BOEING 727 727247 138408F NM BS 990 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 A GOUGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE IS LOCATED ABOVE S24R. THE SK IN, DOUBLER AND TRIPLER WERE DAMAGE, BUT NOT THE BEAR STRAP. REPAIRED PER ERA 332963-14, REV A. 2 L 7 3 4F A3WE 1999040900278 19990409 00278 NM 1999 4 9 DL76S990692 1 19990329 A 3520 MASK BOEING 767 767332 1382001 NM CABIN FELL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 THE O2 MASK ZONE C HANGING DOWN. REINSTALLED MASK AND SECURED PANEL. 2 L 7 2 4F RT A1NM 1999040900279 19990409 00279 NM 1999 4 9 DL72W990693 1 19990330 A 5311 6516348118 FRAME BOEING 727 727247 138408F NM BS 1148 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 BS 1148 FRAME WAS FOUND WORN ON THE I/B HORIZ FLANGE RADIUS AT S22L. THE WEAR WAS CAUSED BY CONTACT WITH A HYD LINE. RE PAIRED PER ERA 332949-14, REV A. 2 L 7 3 4F A3WE 1999040900280 19990409 00280 NM 1999 4 9 DL72W990694 1 19990330 A 5712 6583385 RIB BOEING 727 727247 138408F NM WS 171 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 UPPER CHORD ANGLE OF LT WING RIB AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS ARE LOCATED AT S16 AND S17. REPAIRED PER ERA 332958-14, REV A. 2 L 7 3 4F A3WE 1999040900281 19990409 00281 NM 1999 4 9 DL767990695 1 19990329 A 3260 SWITCH 387 BOEING 767 767232 1385132 NM LT MLG DIRTY A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 102DA 22214 LEFT MAIN GEAR GREEN LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS LOWERED. THE LIGHTS DID NOT PRESS TO TEST WITH GEAR HANDLE UP OR DOWN. CLEANED SWITCH CONTACTS AND RELAMPED, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1999040900282 19990409 00282 NM 1999 4 9 DL73K990696 1 19990330 A 5313 STRINGER BOEING 737 737232 1384475 NM BS 1006 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 STRINGER 27L FS 1006 HAD CORROSION. REPAIRED PER SRM 53-10-3 FIG 1. 2 L 7 2 4F RT A16WE 1999040900283 19990409 00283 NM 1999 4 9 DLM88990697 1 19990330 A 5244 SENSOR DOUG MD88 MD88 3023688 NM ACCESS COMPT DR OUT OF ADJUST A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 923DL 49705 ACCESS COMPT DOOR LIGHT ILLUMINATED IMMEDIATELY AFTER T/O. AIRCRAFT WOULDN'T PRESSURIZE. VISUAL INSPECTION CONFIRMED CO MPT DOOR PROPERLY CLOSED. PRESSURIZED A/C TO 6.25 PSI DIFF, OPS NORMAL. DOOR WARNING SYS DEFERRED, ADJUSTED PROX SENSO R. 2 L 7 2 4F RT A6WE 1999040900284 19990409 00284 NM 1999 4 9 DLM11990698 1 19990330 A 3350 CONNECTOR M390290411 DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 812DE 48601 EMERGENCY LIGHT TEST SHOWS LT BATT 6 LOW. FOUND PIN 6 ON CONNECTOR R1-272 MAKING INTERMITTENT CONTACT, ALSO PIN 6 ON CON NECTOR P1-272 MISALIGNED. REPLACED PIN CONTACT NR 6. 2 L 7 3 4F RT A22WE 1999040900285 19990409 00285 NM 1999 4 9 DLM88990700 1 19990330 A 2421 696233B GENERATOR DOUG MD88 MD88 3023688 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING B H J SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 971DL 53214 RT ENG CSD EXCEEDED HI TEMP LIMITS. DISCONNECTED IN FLT. ELECT SMOKE OR FUMES REPORTED IN AFT CABIN. REPLACED CSD AND GENERATOR. 2 L 7 2 4F RT A6WE 1999040900286 19990409 00286 NM 1999 4 9 DL72L990701 1 19990327 A 5330 655457489 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF TH E LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT FOR THE ENTIRE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367051-14AD, REV B. 2 L 7 3 4F A3WE 1999040900287 19990409 00287 NM 1999 4 9 DL73K990702 1 19990327 A 5330 6545778 SKIN BOEING 737 737232 1384475 NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 THE LOWER HINGE CUTOUT OF THE AFT ENTRY DOOR CUTOUT SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER. THE BEAR STRAP WAS NOT CRACKED. THE CRACKED AREA OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 367062-14, REV A. 2 L 7 2 4F RT A16WE 1999040900288 19990409 00288 NM 1999 4 9 DL72S990703 1 19990325 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS IN TWO SEPARATE FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366999-14AD, REV A. 2 L 7 3 4F A3WE 1999040900289 19990409 00289 NM 1999 4 9 DL76K990704 1 19990326 A 5330 143T32627 SKIN BOEING 767 767332 1382001 NM BS 654-687 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DZ 29692 THE FUSELAGE SKIN AT FS 654+33 WAS STRUCK BY GROUND EQUIPMENT RESULTING IN MULTIPLE PUNCTURES AND GOUGES BETWEEN STRINGE R 37R AND BL 0. THE DAMAGED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED PER ER/A 367045-14, RE V A. 2 L 7 2 4F RT A1NM 1999040900290 19990409 00290 NM 1999 4 9 DL72S990705 1 19990323 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 FOUND DURING MV2 CORROSION VISIT NRC 134, .375 INCH VISIBLE CRACK LT CUTOUT FRAME, AFT ENTRY DOORWAY AT SECOND FROM UPPE R STOP CASTING. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999040900291 19990409 00291 NM 1999 4 9 DL72S990706 1 19990330 A 2131 7638101 CONTROLLER BOEING 727 727225A 1384077 NM E & E COMP MALFUNCTIONED A DALA G O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 SO 27 8891Z 21860 ON DESCENT INTO SEA, LOST PRESSURIZATION AT ABOUT 17,000 FEET. AUTO FAIL LT ILLUMINATED, TRIED STANDBY, NO JOY. CABIN C LIMBED, MASKS DEPLOYED. FINALLY GOT CONTROL USING MANUAL AC/DC CONTROL. MTC REPLACED AUTO PRESS CONTROLLER. 2 L 7 3 4F RT A3WE 1999040900292 19990409 00292 NM 1999 4 9 DL73K990707 1 19990331 A 5313 BAC1498157 STRINGER BOEING 737 737232 1384475 NM BS 948 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 STR 27 LT AT FS 948 CORRODED. REPAIRED PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 1999040900293 19990409 00293 NM 1999 4 9 DL73K990708 1 19990331 A 5313 BAC1498157 STRINGER BOEING 737 737232 1384475 NM BS 988 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 STR 27 LT AT FS 988 CORRODED. REPAIRED PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 1999040900294 19990409 00294 NM 1999 4 9 DL73K990709 1 19990331 A 5313 BAC1498157 STRINGER BOEING 737 737232 1384475 NM BS 978 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 STR 26R AT FS 978 CORRODED. REPAIRED PER SRM 53-10-3. 2 L 7 2 4F RT A16WE 1999040900295 19990409 00295 NM 1999 4 9 DL72W990710 1 19990331 A 5320 WEB BOEING 727 727247 138408F NM BS 1271 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 A TYPICAL CRACK WAS FOUND IN THE INBOARD VERTICAL WEB OF THE RT AFT ENTRY DOOR TORQUE BOX AT FS 1271. THE CRACK WAS REPA IRED PER BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 367089-14AD. 2 L 7 3 4F A3WE 1999040900296 19990409 00296 NM 1999 4 9 DL72S990711 1 19990330 A 5330 65545661 SKIN BOEING 727 727232 1384082 NM BS 486 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 LFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN NEAR F S 486. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL LENGTH CONFIRMED A SINGLE CRACK AT FS 486. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367069-14AD. 2 L 7 3 4F A3WE 1999040900297 19990409 00297 NM 1999 4 9 DL72S990712 1 19990330 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 480-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 71 TOTAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LE NGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367028-14AD, REV A. 2 L 7 3 4F A3WE 1999040900298 19990409 00298 NM 1999 4 9 DL72S990713 1 19990330 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 43 TOTAL CRACKS ALONG THE PANEL. THE SKIN LAP SPLICE WAS CUT OUT AL ONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367029-14AD, REV A. 2 L 7 3 4F A3WE 1999040900299 19990409 00299 NM 1999 4 9 DL72S990714 1 19990330 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN THREE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 367026-14AD, REV A. 2 L 7 3 4F A3WE 1999040900300 19990409 00300 WP 1999 4 9 DLL10990715 1 19990331 A 5220 COUNTERBALANCE 1313T10013 LKHEED 1011 10113851 5265010 WP R4 DOOR FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 251 193C1200 A/C IS IN FOR LETTER CHECK, OPNS 52148 & 68115 BOTH PERTAINING TO INSPECTION AND OPERATION OF PASSENGER AND EMERGENCY DO ORS. FOUND R4 DOOR WOULD NOT OPEN COMPLETELY. NON-ROUTINE CARD 160 WAS INITIATED. FURTHER EVALUATION FOUND FAILURE OF THE COUNTERBALANCE TO BE THE CAUSE. REPLACED SAME. 2 L 7 3 4F A23WE 1999040900301 19990409 00301 NM 1999 4 9 DL72S990716 1 19990331 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 FOUND ON C1 LETTER CK, AFT RT ENTRY DOOR FRAME CRACKED. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999040900302 19990409 00302 NM 1999 4 9 DL73E990719 1 19990401 A 2530 COFFEEMAKER BOEING 737 737247 138448D NM AFT GALLEY SMOKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 373DL 23520 ABOUT 15 MIN AFTER T/O AT APPROX 20,000 ALT, F/A REPORTED A STRONG ELECT SMELL IN AFT LAV AREA. SHUT OFF GALLEY PWR AND PULLED AFT LAV C/B. RETURNED TO CVG. ON DESCENT, F/A REPORTED SMELL DIMINISHING. INSPECTED, SUSPECT BURNING COFF EE. 2 L 7 2 4F A16WE 1999040900303 19990409 00303 NM 1999 4 9 DL72S990721 1 19990331 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 480-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERN AL HFEC INSPECTION CONFIRMED CRACKS IN 4 DIFFERENT FRAME BAYS. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITH AN EXT ERNAL REPAIR DOUBLER PER ER/A 367068-14AD, REV B. 2 L 7 3 4F A3WE 1999040900304 19990409 00304 NM 1999 4 9 DL72S990722 1 19990322 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 REPAIRED CRACK AT UPPER STRINGER TO RIB FASTENER HOLE AT RT WING STA 656.50 STR 14 PER M/M 57-13-0. 2 L 7 3 4F A3WE 1999040900305 19990409 00305 NM 1999 4 9 DL72E990723 1 19990401 A 3350 BATTERY 900835A BOEING 727 727247 138408F NM EMER EXIT DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 CENTER LT OVERWING EMERG LIGHT INOP. REPLACED BATTERY AT M954, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999040900306 19990409 00306 NM 1999 4 9 DLM88990725 1 19990401 A 3350 POWER SUPPLY 8039001 DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 920DE 30086 53423 COCKPIT OVERHEAD EMERGENCY LIGHTS INOP. FOUND POWER SUPPLY INOP. REPLACED SUPPLY AND BATTERIES CKS OK. 2 L 7 2 4F RT A6WE 1999040900307 19990409 00307 NM 1999 4 9 DLM88990727 1 19990402 A 5340 SCUFF PLATE DOUG MD88 MD88 3023688 NM SERVICE DOOR CRACKED A DALA K NONE O OTHER CL CLIMB 1 SO 27 932DL 49719 IN CLIMB PASSING THRU FL 360, A LOUD NOISE AND VIBRATION STARTED. F/C GALLEY AREA WAS MOST EXCESSIVE. VIBRATION STOPPED IN DESCENT THRU FL 185. FOUND R1 DOOR SCUFF PLATE BENT AND CRACKED. REPLACED SAME. 2 L 7 2 4F RT A6WE 1999040900308 19990409 00308 NM 1999 4 9 DL757990729 1 19990403 A 2120 AIR DISTRIBUTION PW2037 BOEING 757 757232 1384965 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 608DA 22815 ON T/O, F/A REPORTED A STRONG BURNING SMELL FROM THE MID RT GALLEY AREA AND FWD. PERFORMED COMPRESSOR WASH ON LEFT ENGIN E. 2 L 7 2 4F RT A2NM 1999040900309 19990409 00309 NM 1999 4 9 DLM88990730 1 19990403 A 4910 36280 INLET DOUG MD88 MD88 3023688 NM APU DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 915DE 3226 53420 80226 LIGHT SMOKE IN CABIN AFTER T/O. FOUND APU AIR INLET COACKED UP WITH OIL. CLEANED AND PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1999040900310 19990409 00310 NM 1999 4 9 DL72S990732 1 19990403 A 2910 VALVE BOEING 727 727225 1384077 NM B HYD SYST LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 8882Z 21579 LOSS OF B HYD IN FLT. REPLACED LEAKING CHECK VALVE IN LEFT WHEEL WELL. 2 L 7 3 4F A3WE 1999040900311 19990409 00311 NM 1999 4 9 DL72E990733 1 19990403 A 3350 BATTERY PACK BOEING 727 727247 138408F NM RT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831WA VA5959 21483 EMERGENCY EXIT LIGHT SIGN OVER RT OVERWING EXIT INOP ON TEST. REPLACED RACK AND BATTERY PACK, OPN CKS OK. 2 L 7 3 4F A3WE 1999040900312 19990409 00312 NM 1999 4 9 DLM88990734 1 19990403 A 3350 CHARGER RPS1 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DE 1902 49959 FWD SECTION EMERGENCY LIGHTS INOP. REPLACED CHARGER. 2 L 7 2 4F RT A6WE 1999040900313 19990409 00313 NM 1999 4 9 DL76P990736 1 19990404 A 3260 SWITCH 4346741033 BOEING 767 767332 1382001 NM COCKPIT CORRODED A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 1402A 25989 IN LANDING CONFIG, NOSE GEAR GREEN LIGHT WOULD NOT ILLUMINATE. LIGHT WOULD NOT ILLUMINATE WHEN LIGHTS TEST BUTTON PUSHED , BUT WOULD ILLUMINATE WITH PUSHING THE LIGHT. ACCOMP ABNORMS, LIGHT DID NOT ILLUMINATE WITH MTC DIRECT. RECYCLED GEAR , LIGHT STILL NOT ILLUMINATED. CONTINUED TO WIGGLE LIGHT AND IT FINALLY ILLUMINATED. LANDED WITH NORMAL INDS. REPLACE D SWITCH. 2 L 7 2 4F RT A1NM 1999040900314 19990409 00314 NM 1999 4 9 DLM88990737 1 19990404 A 2150 ACM DOUG MD88 MD88 3023688 NM AFT FUSELAGE OVERSERVICED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 918DL 49583 PASSING 31,000 FEET IN CLIMB, FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN AFT PASSENGER COMPARTMENT AND SMOKE DETECTORS IN AFT LAV WERE ON. BEGAN DESCENT AND SMOKE DISSIPATED AND CLEARED CABIN FOR DURATION OF FLIGHT. FOUND RT ACM OVERSERVICED . SERVICED TO PROPER LEVEL AND PERFORMED DUCT BURNOUT AND WATER SEPARATOR BAG REPLACEMENT PER M/M. NO FURTHER SMELLS O R SMOKE. 2 L 7 2 4F RT A6WE 1999040900315 19990409 00315 NM 1999 4 9 SCNA99059 1 19990401 A 3350 900835A BATTERY PACK BOEING 727 7272A1 138407F NM ROW 5 DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 36273 21601 DURING A LINE MAINTENANCE CHECK, THE FORWARD AISLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT THE CENTER AISLE ROW 5. SYSTEM OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999040900316 19990409 00316 WP 1999 4 9 TC8A99010 1 19990401 A 3610 DUCT DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE LEAKING A TC8A A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 182SK 45817 642688 ON CLIMBOUT FROM KBRO, NR 3 ENGINE FIRE WARNING ON. COMPLETED CHECKLIST AND SHUTDOWN NR 3 ENGINE. REPAIRED AIR LEAK IN R EVERSER AREA, OPS CHECK GOOD ON GROUND RUN IAW MM 78-00 AND 75-00. 2 L 7 4 4F 4 F 4A25 1E8 1999040900317 19990409 00317 NE 1999 4 9 TC8A99011 2 19990401 A 7200 ENGINE BOEING 727 727173C 1384059 NM PWA JT8 JT8D7B 52053 NE NR 3 VIBRATION A TC8A A UNSCHED LANDING E VIBRATION/BUFFET UK UNKNOWN 1 GL 23 704A 19504 653415 NR 3 ENGINE VIBRATES WHEN THRUST IS SET BETWEEN 53 TO 56 PERCENT N1. OIL TEMP ROSE TO 120 AND EGT CLIMBED TO 410. AT ALL OTHER THRUST SETTINGS, ENGINE OIL TEMP RUNS 20 DEGREES HOTTER. PERFORMED BORESCOPE REF M-40 51190, NO DEFECTS NOTED. P ERFORMED ENGINE VIBRATION SURVEY, CHECKED WITHIN LIMITS REF M-40 51192. 2 L 7 3 4F 4 F A3WE E2EA 1999040900318 19990409 00318 WP 1999 4 9 TC8A99012 1 19990404 A 2612 FIRE LOOP DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE MALFUNCTIONED A TC8A A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 182SK 45817 642688 CLIMBOUT FROM KBRO, NR 3 ENGINE FIRE WARNING ON. COMPLETED CHECKLIST, SHUT DOWN NR 3 ENGINE. REMOVED AND REPLACED AFT P YLON FIRE LOOP, OPS CHECK GOOD ON GROUND RUN IAW DC8 MM 26-2-1. 2 L 7 4 4F 4 F 4A25 1E8 1999040900333 19990409 00333 NM 1999 4 9 TWAA9905001 1 19990331 A 3350 6104783 BATTERY PACK BOEING 727 727231 1384079 NM RT EMER EXIT DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64346 21633 THE RT MIDDLE OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 9-11-98 MCI. 2 L 7 3 4F A3WE 1999040900334 19990409 00334 EU 1999 4 9 MALA976416 1 19990401 A 3020 NH2466813102 DUCT SAAB SF340 340B 7860101 EU LEFT NACELLE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 443XJ 443 LEFT INTAKE LIGHT ILLUMINATED, CYCLED PER QRH STILL REMAINED ON. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED UPPER DU CT ASSEMBLY AND SWAPPED TO SPARE THERMISTER ON LOWER DUCT. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999040900335 19990409 00335 EU 1999 4 9 MALA976417 1 19990405 A 2730 CIRCUIT BREAKER BAC 146 AVRO146RJ85A 1500097 EU COCKPIT TRIPPED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 519XJ E2344 Q FEEL HTR FAIL LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO MSP. MAINTENANCE FOUND Q HTR C/B POPPED. RESET C/B, A LL CHECKED GOOD. 2 H 7 4 4F RT A49EU 1999040900336 19990409 00336 EU 1999 4 9 MALA976418 1 19990404 A 3234 D49412001 CONTROL BOX SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 15 418XJ 418 GEAR LIGHT IN HANDLE WILL NOT ILLUMINATE. MAINTENANCE REPLACED GEAR SELECTOR HANDLE CONTROL BOX. OPS CHECK GOOD, GEAR SW ING CHECK GOOD. 2 L 7 2 4T RT A52EU 1999040900337 19990409 00337 EU 1999 4 9 MALA976419 1 19990403 A 7933 CONNECTOR SAAB SF340 340B 7860101 EU LT ENG OIL TEMP LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 402XJ 340B402 IN FLIGHT LT ENGINE OIL TEMP GAUGE FULL HOT, TALKED TO MX AND RETURNED TO DTW. ALL OTHER ENGINE INDICATIONS NORMAL. MAIN TENANCE FOUND LT ENGINE TEMP BULB CANNON PLUG LOOSE. RESECURED CANNON PLUG, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999040900338 19990409 00338 NM 1999 4 9 CALA9900354 1 19990402 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 906 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 906, S10L. REPAIRED IAW ECRA 5330-02793. 2 L 7 2 4F RT A16WE 1999040900339 19990409 00339 WP 1999 4 9 CALA9900355 1 19990402 A 5350 3918323509 HANDLE DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 THE TAIL CONE EXTERIOR RELEASE HANDLE CATCHES ON LOWER LIP OF SKIN CUTOUT PREVENTING PULL OF HANDLE. INSPECTED HANDLE AN D ADJUSTED CATCH WITHIN LIMITS AND PERFORMED ADJUSTMENT/TEST OF TAIL CONE RELEASE SYSTEM IAW MM 53-53-00. 2 L 7 2 4F A6WE 1999040900340 19990409 00340 WP 1999 4 9 CALA9900356 1 19990402 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND BELTFRAME CORRODED AT STA 1338, RT LAV, APPROXIMATELY SIX INCHES UP FROM FLOOR. A SPLICE REPAIR WAS INS TALLED IAW ECRA 5310-03837. 2 L 7 2 4F A6WE 1999040900341 19990409 00341 WP 1999 4 9 CALA9900357 1 19990403 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 1336 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND DOUBLER CORRODED AT STA 1336 BETWEEN S18R AND S17R IN RT LAV. NEW FILLER WAS INSTALLED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1999040900342 19990409 00342 NM 1999 4 9 CALA9900358 1 19990405 A 5330 SKIN BOEING 757 757224 1384958 NM BS 780 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN PANEL AT STA 780, STRINGER 15L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53- 00-01. 2 L 7 2 4F RT A2NM 1999040900343 19990409 00343 NM 1999 4 9 9901305519 1 19990329 A 2530 OVEN BOEING 757 757251 1384970 NM FORWARD GALLEY MALFUNCTIONED A NWAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 519US 23207 IN CRUISE FLIGHT, THE CREW DETECTED A BURNING ODOR THAT SEEMED TO ORIGINATE FROM THE FORWARD GALLEY OVEN AREA. THE OVENS WERE TURNED OFF BUT THE ODOR DID NOT DISSIPATE. THE FLIGHT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE DE ACTIVATED THE OVEN UNIT AND RELEASED THE AIRCRAFT FOR SERVICE. THE OVEN WAS REPLACED DURING SUBSEQUENT OVERNIGHT MAINTE NANCE. 2 L 7 2 4F RT A2NM 1999040900344 19990409 00344 WP 1999 4 9 9901319936 1 19990401 A 7332 SWITCH DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RIGHT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 799U 47370 667114 DURING TAKEOFF ROLL AT 100 KNOTS, THE RIGHT ENGINE FUEL PRESSURE DROP LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURN ED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL LOW PRESSURE SWITCH AND FUEL FILTER, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1999040900345 19990409 00345 NE 1999 4 9 9901329851 2 19990403 A 7314 384301 FUEL PUMP DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17A 52049 NE LEFT ENGINE FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 01 760NC 36348 11973 47708 68827 DURING CLIMB, THE LEFT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAI NTENANCE REPLACED THE LEFT ENGINE FUEL PUMP AND FUEL CONTROL, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1999040900346 19990409 00346 NM 1999 4 9 UPS99229170 1 19990403 A 3350 1000677 BATTERY PACK BOEING 727 72751C 1384015 NM L1 DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-N/A, EMER LIGHT AT L-1 DOOR WILL NOT SHUT OFF. REMOVED AND REPLACED EMER BATT PACK PER MM 33-50-01, OPS CK GOOD. (P/N 10-0067-7) (S/N 3893) ON, (S/N 26993) OFF. 2 L 7 3 4F A3WE 1999040900347 19990409 00347 WP 1999 4 9 UPS99829171 1 19990322 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, RT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED AT THE I/B UPPER SIDE. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900348 19990409 00348 WP 1999 4 9 UPS99829172 1 19990322 A 5712 RIB DOUG DC8 DC871F 302199D WP LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, LT WING CENTER L/E HAS UPPER RIB THAT IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900349 19990409 00349 WP 1999 4 9 UPS99829173 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, LT WING L/E LWR RIB AT STA FS 778.750 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900350 19990409 00350 WP 1999 4 9 UPS99829174 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 816.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, LT WING L/E AT STA FS 816.250, THE LWR RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 1999040900351 19990409 00351 WP 1999 4 9 UPS99829175 1 19990323 A 5320 47516251N FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 680 AT LONG 11L, THE LONGERON END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 47516 25 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900352 19990409 00352 WP 1999 4 9 UPS99829176 1 19990322 A 5320 577327557 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, WING BOX FLOORBEAM SUPPORT ANGLE IS CRACKED AT STA 680, LBL 25. REMOVED, FABRICATED AND REPLACED FIT TING IAW DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900353 19990409 00353 WP 1999 4 9 UPS99829177 1 19990322 A 5320 577327577 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, WING BOX FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 680 AT LBL 48. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900354 19990409 00354 WP 1999 4 9 UPS99829178 1 19990401 A 5320 3754916501 FITTING DOUG DC8 DC871F 302199D WP BS 270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 270 AT LONG 30R, THE SUPPORT FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED SUPPO RT FITTING IAW DWG 3754916 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900355 19990409 00355 WP 1999 4 9 UPS99829179 1 19990323 A 5512 SKIN DOUG DC8 DC871F 302199D WP RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, RT HORIZ STAB L/E SKIN AT MID SPAN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED AREA IAW SRM 55-2 -1 FIG 4. 2 L 7 4 4F RT 4A25 1999040900356 19990409 00356 WP 1999 4 9 UPS99829181 1 19990405 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CKS OK. 2 L 7 4 4F RT 4A25 1999040900357 19990409 00357 EU 1999 4 9 QXEA9900544 1 19990401 A 3350 A42052 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 484US 11234 PDX - THE EXIT SIGN OVER THE COCKPIT DOOR FELL AND BROKE A WIRE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN, OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1999040900358 19990409 00358 EU 1999 4 9 QXEA9900545 1 19990402 A 3350 6008905 BATTERY PACK GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 1750 11167 PDX - LOWER EMERGENCY EXIT LIGHTS IN CABIN NEXT TO OVERWING EXITS WILL NOT EXTINGUISH. MAINTENANCE REPLACED THE EMERGENC Y BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1999040900359 19990409 00359 NE 1999 4 9 99FDEA00130 2 19990402 A 7310 FILTERS DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE 1, 2 & 3 ENGINE CONTAMINATED A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 617FE 48748 LEVEL 1 ENG 3 FUEL FILTER ALERT AND LEVEL 1 FUEL CONTAMINATION ALERT DISPLAY. CREW DUMP FUEL TO REDUCE DOWN TO MAX WT. R EMOVED AND REPLACED ALL THREE ENG FILTERS PER 73-11-04-04-1. 2 L 7 3 4F 4 F RT A22WE E31N3 1999040900361 19990409 00361 NM 1999 4 9 99FDEA00132 1 19990405 A 5313 655612910 STRINGER BOEING 727 727247 138408F NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-111-01, 3) ON STR 27R AT BS 990. *S/D* REMOVED AND REPLACED STR 27R PER FEDEX EA 7-5310-45210A. 2 L 7 3 4F A3WE 1999040900362 19990409 00362 NM 1999 4 9 99FDEA00133 1 19990405 A 5330 651758866 BEAM BOEING 727 727247 138408F NM BS 264 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-221-01) ON FWD EDGE OF 25 G-BEAM BS 264, LBL 4 TO LBL 7, WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM, BS 264, LBL 8 TO RBL 21, WL 208 IAW FEDEX EA NR 7-5310-45212. 2 L 7 3 4F A3WE 1999040900363 19990409 00363 NM 1999 4 9 99FDEA00134 1 19990405 A 5313 65548352 STRINGER BOEING 727 727247 138408F NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-111-01, 3) ON STR 25R AT BS 1176. *S/D* REMOVED AND REPLACED 25R FROM BS 1158 TO 1183 IAW FEDEX SRM 53- 10-3 FIG 1. 2 L 7 3 4F A3WE 1999040900364 19990409 00364 NM 1999 4 9 99FDEA00135 1 19990405 A 5313 655623630 STRINGER BOEING 727 727247 138408F NM BS 494 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-111-01,2) ON STRINGER 26L, BS 494. *S/D* REMOVED AND REPLACED STR 26L, BS 482-496 IAW FEDEX SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999040900365 19990409 00365 WP 1999 4 9 ABXA9900274 1 19990224 A 5400 57530296 ANGLE DOUG DOUG DC8 DC862 3021970 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND NR 2 PYLON INBOARD VERTICAL ATTACH ANGLE CRACKED AFT OF FOOTSTOOL FITTING. REPAIRED IAW DC8 SRM 54 -22. 2 L 7 4 4F 4A25 1999040900366 19990409 00366 WP 1999 4 9 ABXA9900275 1 19990218 A 5400 57530055N LINK DOUG DOUG DC8 DC862 3021970 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND NR 2 PYLON OUTBOARD THRUST LINK CRACKED. REPLACED PYLON THRUST LINK IAW DC8 MM 71-20-1. 2 L 7 4 4F 4A25 1999040900367 19990409 00367 WP 1999 4 9 ABXA9900276 1 19990218 A 5320 4641324N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1530 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND PRODUCTION SPLICE FITTING AT STATION 1530 LONGERON 34 RIGHT CRACKED AND CORRODED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F 4A25 1999040900368 19990409 00368 WP 1999 4 9 ABXA9900277 1 19990223 A 5313 57577781 LONGERON DOUG DOUG DC8 DC862 3021970 WP BS 1500 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON LONGERON 33 RIGHT AT STATION 1500. REPLACED LONGERON 33 RIGHT IAW DC8 SRM 51- 1-21 AND 51-1-20D. 2 L 7 4 4F 4A25 1999040900369 19990409 00369 WP 1999 4 9 ABXA9900278 1 19990218 A 5320 4645516501N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 940-960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND 3 FITTINGS CRACKED AT BOTTOM OF KEEL BEAM BETWEEN MAIN LANDING GEAR DOORS, STATION 940 TO 960. REP LACED KEEL BEAM FITTINGS IAW DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1999040900370 19990409 00370 WP 1999 4 9 ABXA9900279 1 19990218 A 5320 4641324N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1530 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND PRODUCTION SPLICE FITTING CRACKED AT STATION 1530, LONGERON 34 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F 4A25 1999040900371 19990409 00371 1999 4 9 MWEA99124 4 19990405 A 3418 8009817 AOA TRANSDUCER DOUG DC9 DC932 3022066 WP COCKPIT OUT OF LIMITS A MWEA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 GL 31 202ME 47672 SIF LIGHT ILLUMINATED WITH STICK SHARERS ON CLIMBOUT. REMOVED AND REPLACED RT AOA VANE, FOUND TO BE OUT OF LIMITS. 2 L 7 2 4F A6WE 1999040900372 19990409 00372 WP 1999 4 9 MWEA99125 1 19990327 A 5320 99578605 STIFFENER DOUG DC9 DC914 3022034 WP BS 690 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND THE VERTICAL STIFFENER CRACKED AT UPPER END AT STATION Y 690 AND X 100. MTC REMOVED AND REPLACED VERTICAL STIFFENE R. 2 L 7 2 4F A6WE 1999040900373 19990409 00373 WP 1999 4 9 MWEA99126 1 19990327 A 5320 99115673 BEAM DOUG DC9 DC914 3022034 WP BS 690 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 THE HORIZONTAL BEAM IS CRACKED AT FORWARD END AT STATION Y 690 AND X 100. MTC REMOVED AND REPLACED HORIZONTAL BEAM. 2 L 7 2 4F A6WE 1999040900374 19990409 00374 WP 1999 4 9 MWEA99127 1 19990329 A 5210 9955752501 BEAM DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND CRACK ON FORWARD PASSENGER DOOR ON NUMBER 1 BEAM FORWARD END. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999040900375 19990409 00375 NM 1999 4 9 MWEA99128 1 19990331 A 5730 59358222 SKIN DOUG MD88 MD88 3023688 NM LEFT WING OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 THE LEFT WING LOWER SKIN AFT SPAR AT XRS 477 HAS A BLEND OUT REPAIR. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999040900376 19990409 00376 NM 1999 4 9 DHL99720002 1 19990405 A 2424 10605002 CONTROLLER BOEING 727 727228 NM NR 1 ENGINE INOPERATIVE A DHLA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 DURING CLIMBOUT, GEN NR 1 CARRIED ALL ELECTRICAL LOAD AT 50 KW. NR 1 CSD IN TEMP 120 DEGREES. NR 2 AND 3 GEN CARRIED NO LOAD. NR 2 AND 3 CSD IN TEMP 80 DEGREES C. ALL THREE GEN VOLTS AND FREQS NORMAL. FIVE MINUTES AFTER DEPARTURE THE LOA DS EQUALLED OUT AND ALL INDICATIONS NORMAL. FIVE MIN LATER, NR 2 GEN TRIP LIGHT ILLUMINATED AND VOLTS AND FREQS NORMAL. REMOVED AND REPLACED NR 1 LOAD CONTROLLER. 2 L 7 3 4F A3WE 1999040900377 19990409 00377 SO 1999 4 9 99ZZZX1476 1 19990209 A 3234 A4865 LEVER GULSTM G1159 G1159 3953505 SO COCKPIT CRACKED A COZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 27 102CX 5661 102 AFTER TAKEOFF, CREW COULD NOT SELECT GEAR HANDLE TO THE RETRACT POSITION AND RETURNED TO BASE. INVESTIGATION REVEALED TH E LANDING GEAR HANDLE LEVER HAD BROKEN PROVIDING TOO MUCH SIDE PLAY FOR THE GEAR HANDLE TO BE MOVED OUT OF THE DETENT. T HE LEVER CRACKED WHERE THE OEM TO ALLOW PASSAGE OF AN ELECTRICAL WIRE TO THE HANDLE LIGHTS HAD DRILLED A HOLE. TT USED, 5,660.8 HOURS, 2,743 CYCLES. GEAR HANDLE LEVER ASSY ROUTED TO GULFSTREAM, SAVANNAH, GEORGIA, TO TECH SERVICE FOR EVALU ATION. 2 L 7 2 4F RT A12EA 1999040900378 19990409 00378 WP 1999 4 9 GTIA9900013 1 19990202 A 3350 362624 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805RA 48087 DTW - THREE LIGHTS OUT ON THE EMERGENCY TRACK FLOOR. REMOVED AND REPLACED EMERGENCY TRACK LIGHTING AS REQUIRED IAW MD80 MM 33-50-00. (X) 2 L 7 2 4F A6WE 1999040900379 19990409 00379 1999 4 9 99ZZZX1477 4 19990213 A 2565 D31517109 SLIDE AIRBUS 320 A320231 3930325 EU R2 DOOR DEPLOYED A RYNA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 07 GCVYE 394 MSP - FLT 987 - AT GATE, RIGHT HAND AFT R2 DOOR SLIDE DEPLOYED. REMOVED AND REPLACED RIGHT HAND R2 AFT DOOR SLIDE. 2 L 7 2 4F RT A28NM 1999040900380 19990409 00380 SO 1999 4 9 SIMA990512 1 19990220 A 2120 AIR DIST EMB 145 EMB145 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 609AE 145069 SHV - FLT 4109 - WITH TEMPERATURE CONTROL IN AUTO, THE FLIGHT ATTENDANT REPORTED A SMELL AND SMOKE IN THE CABIN. AFTER S WITCHING TEMPERATURE CONTROL TO MANUAL, THE SMELL CLEARED. INSPECTED NR 2 AIR CONDITIONING PACK AREA AT WING ROOT AND AU TO. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999040900381 19990409 00381 NM 1999 4 9 99ZZZX1478 1 19990212 A 5414 65B940521 SKIN BOEING 747 747230B 1384889 NM NR 2 PYLON DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 DURING STRUT MODIFICATION, THE SKIN BELOW MID-SPAR CHORD BETWEEN NAC STA 286 AND NAC STA 300 ON THE RIGHT SIDE OF NR 2 E NGINE PYLON WAS FOUND WITH HEAT DAMAGE WRINKLES. THE DAMAGED AREA WAS REPAIRED AS FOLLOWS: HEAT DAMAGED SKIN AREA WAS TR IMMED AND REMOVED. REPAIR AREA WAS NDT INSPECTED, NEW DOUBLER AND TRIPLER, MADE FROM TITANIUM SHEET WERE INSTALLED TO PI CK UP AFT END OF TITANIUM SKIN DOUBLER MID-SPAR CHORD, LOWER STIFFENER FRAME AT NAC STA 286 AND FRAME AT NAC STA 300. S TRUCTURAL SUBSTANTIATION OF ENGINEERING FOR ABOVE REPAIR MADE BY BOEING DER ON FORM 8110-3. (X) 2 L 7 4 4F A20WE 1999040900382 19990409 00382 SO 1999 4 9 SIMA990496 1 19990218 A 3350 744412 BULB EMB 145 EMB145LR SO ROW 3BC FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 616AE 145092 ORD - FLT 4031 - EMERGENCY EXIT LIGHT ON FORWARD BULKHEAD OF ROW 3BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPE RATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 1999040900383 19990409 00383 NM 1999 4 9 AALA990288 1 19990227 A 3397 WIRE BOEING 757 757223 1384957 NM ROWS 18-26 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 679AN 29589 DFW - FLIGHT CREW FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BETWEEN SEAT ROWS 18 AND 26. REPAIRED WIRE SPLICE A T SEAT ROW 22. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999040900384 19990409 00384 NE 1999 4 9 MASA99025 2 19990215 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 2 VIBRATION A MASA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 77286 7286 PHX/DSM - FLT 6009 - APPROXIMATELY TEN MINUTES AFTER DEPARTURE FROM PHX, THE CREW REPORTED THE NR 2 ENGINE VIBRATION IND ICATOR TURNED YELLOW AT 2.7 PERCENT. CREW DECLARED AN EMERGENCY DUE TO THE FACT THE AIRCRAFT WAS OVERWEIGHT. THE AIRCRAF T RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. A HEAVY LANDING INSPECTION WAS PERFORMED, AND THE AIRCRAFT WAS FERRIE D TO FAT, WHERE A VISUAL INSPECTION AND POWER RUNS WERE PERFORMED, WITH ENGINE VIBRATIONS FOUND TO BE WITHIN LIMITS. TH E AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F RT A21EA E15NE 1999040900385 19990409 00385 WP 1999 4 9 GTIA9900024 1 19990224 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 DTW - EMERGENCY FLOOR TRACK LIGHTING NEAR AFT LAVATORY INOPERATIVE. FOUND FLOOR TRACK STRIP DISCONNECTED, RECONNECTED. O PERATIONAL CHECK GOOD IAW MM 33-50-00. (X) 2 L 7 2 4F A6WE 1999040900386 19990409 00386 NM 1999 4 9 W7NR9900001 1 19990210 A 2910 BACH8A06NN0360T LINE BOEING 737 737236 1384476 NM NR 2 BRAKE LOOSE A W7NA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 920WA 21791 SLC - FLT 504 - AT TOP OF CLIMB, NOTED INDICATION OF ZERO HYDRAULIC QUANTITY. NO LIGHTS AND NO OTHER HYDRAULIC INDICATIO NS. ASSUMING AN INDICATION ERROR, FLIGHT PROCEEDED. WHILE ON A 15 MILE FINAL APPROACH TO SLC, AN ASSIGNED SPEED OF 170 KNOTS CAUSED CREW TO EXTEND FLAPS. AT FLAPS 2 DEGREES, A LOSS OF A-SYSTEM PRESSURE WITH ALL ASSOCIATED WARNING LIGHTS H APPENED. PROCEDURES WERE FOLLOWED FOR THE LOSS OF A-SYSTEM. A MANUAL GEAR EXTENSION AND ALTERNATE FLAP EXTENSION PROCE DURES WAS FOLLOWED AND A NORMAL FLAPS 15 DEGREE LANDING WAS ACCOMPLISHED. SERVICED HYDRAULIC A-SYSTEM AND ON WALK-AROUN D, FOUND NR 2 BRAKE LINE LOOSE. SECURED LINE. OPS CHECKED GOOD PER MM 12-12-0. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A16WE 1999040900389 19990409 00389 NM 1999 4 9 99ZZZX1481 1 19990210 A 3020 600231 SEAL BOEING 727 72721 1384003 NM ANTIICE VALVE FAILED A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 329QS 19038 PHX - FLT 731 - AIR TURN-BACK. AFTER ADDING CLIMB POWER, GOT NR 2 FIRE LIGHT AND BELL. SHUT DOWN NR 2 ENGINE PER CHECK L IST, BUT DID NOT USE THE FIRE BOTTLE SINCE THE LIGHT WENT OUT AFTER SHUTTING DOWN NR 2 ENGINE. ON UPPER SIDE OF ENGINE, FOUND ON TIGHT HAND, ANTI-ICE VALVE FOUND SEAL BLOWN OUT, REMOVED AND REPLACED SEAL. 2 L 7 3 4F A3WE 1999040900390 19990409 00390 NM 1999 4 9 SWAA990618 1 19990401 A 5341 SKIN BOEING 737 7372H4 138448C NM GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED 1/4D CHECK, FOUND FWD GALLEY DOOR, LOWER HINGE CUTOUT HAS A .5 INCH LONG CRACK AT FUSELAGE SKIN. REPAIR ED SKIN PER DALFORT XEA NR X2-53-241. 2 L 7 2 4F A16WE 1999040900391 19990409 00391 NM 1999 4 9 SWAA990619 1 19990401 A 3350 6104781 POWER SUPPLY BOEING 737 7372H4 138448C NM RT EMER EXIT WEAK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED 1/4D CHECK, FOUND RT OUTSIDE OVERWING EMERGENCY LIGHT WEAK. REMOVED AND REPLACED POWER SUPPLY PER MM. 2 L 7 2 4F A16WE 1999040900392 19990409 00392 1999 4 9 SWAA990620 4 19990402 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 FWD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900393 19990409 00393 NM 1999 4 9 SWAA990621 1 19990402 A 3350 7024091009 LIGHT BOEING 737 7373H4 1384600 NM RT EMER EXIT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373SW 26581 COVER MISSING FROM RT EMERGENCY EXIT MARKER LIGHT. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900394 19990409 00394 NM 1999 4 9 SWAA990622 1 19990401 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM BS 1006, LBL 13-15. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999040900395 19990409 00395 NM 1999 4 9 SWAA990623 1 19990401 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FWD LOWER FACE OF BELTFRAME BS 907 RBL 8. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900396 19990409 00396 NM 1999 4 9 SWAA990624 1 19990401 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 45. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900397 19990409 00397 NM 1999 4 9 SWAA990625 1 19990401 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900398 19990409 00398 NM 1999 4 9 SWAA990626 1 19990401 A 5320 6551261 FRAME BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND UPPER FWD STUB FRAMES CRACKED ON FWD GALLEY AND AFT ENTRY DOOR CUTOUTS. REMOVED AND R EPLACED FRAMES PER SRM. 2 L 7 2 4F RT A16WE 1999040900399 19990409 00399 NM 1999 4 9 SWAA990627 1 19990401 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT 4 FLOORBEAM SECTIONS BS 727E, BS 767, BS 845 AT RBL 8 AND BS 727D, RBL 1 4. REPAIRED BEAMS PER SRM. 2 L 7 2 4F RT A16WE 1999040900400 19990409 00400 NM 1999 4 9 SWAA990628 1 19990401 A 5320 6520722 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CORROSION ON AFT CARGO DOOR CUTOUT FRAME, BS 794 BETWEEN STRINGERS 22R TO 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999040900401 19990409 00401 NM 1999 4 9 SWAA990629 1 19990401 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 480, BETWEEN STRINGERS 8R TO 9R. REPAIRED FRAME PER ER NR 99-0306. 2 L 7 2 4F RT A16WE 1999040900402 19990409 00402 NM 1999 4 9 SWAA990630 1 19990401 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CRACKS EMITTING FROM NR 6 SLAT ON LOWER LE SKIN AT I/B AUX TRACK. REPAIRED PER ER 99-022 8P1 AND BOEING DRAWING 65C30133. 2 L 7 2 4F RT A16WE 1999040900403 19990409 00403 NM 1999 4 9 SWAA990631 1 19990401 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM TOP FLANGE BS 947, LBL 53. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900404 19990409 00404 NM 1999 4 9 SWAA990632 1 19990401 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM BS 996-1005 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CORROSION AT FUSELAGE SKIN AT BS 996 TO 1005 BETWEEN STRINGERS 2L-3L. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999040900405 19990409 00405 NM 1999 4 9 SWAA990633 1 19990401 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 931-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 931 TO 986 WEB, WL 208, RBL 48 TO 55. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 1999040900406 19990409 00406 NM 1999 4 9 SWAA990634 1 19990401 A 5320 65C27314 CLIPS BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND 2 STRINGER CLIPS CRACKED AT BS 500D, STRINGERS 19L AND 19R. REPAIRED CLIPS PER SRM. 2 L 7 2 4F RT A16WE 1999040900407 19990409 00407 NM 1999 4 9 SWAA990635 1 19990402 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND STRINGER 19L CRACKED AT BS 500D. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999040900408 19990409 00408 NM 1999 4 9 SWAA990636 1 19990402 A 5312 6516300 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB BS 178 CRACKED IN 5 PLACES, RBL 6 TO LBL 11. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 1999040900409 19990409 00409 NM 1999 4 9 SWAA990637 1 19990402 A 2560 6518621 PLATE BOEING 737 7373H4 1384600 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND CORROSION AT FWD ENTRY DOOR GIRT BAR MOUNTING PLATES. REMOVED AND REPLACED PLATES PER SR M. 2 L 7 2 4F RT A16WE 1999040900410 19990409 00410 SO 1999 4 9 C2XA99IA158 1 19990216 A 5411 12039761001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FORWARD FRAME CRACKED AT INBOARD COWL STAY FITTING. ST OP DRILLED CRACK AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900411 19990409 00411 SO 1999 4 9 C2XA99IA157 1 19990216 A 5400 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE BYPASS DUCT SUPPORT ANGLE CRACKED. FABRICATED REPLACEM ENT ANGLE IAW SRM 51-70-05 AND INSTALLED IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900412 19990409 00412 SO 1999 4 9 C2XA99IA156 1 19990216 A 5330 SKIN EMB 120 EMB120RT SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FUSELAGE SKIN CHAFED BY HEAT EXCHANGER. REMOVED DAMAGE, FABRICATED EXTERNAL DOUBLER REPAIR AND INSTALLED IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900413 19990409 00413 SO 1999 4 9 C2XA99IA163 1 19990216 A 5413 12020151002 STRINGER EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE PANEL 425 IMPROPERLY REPAIRED AT FORWARD INBOARD END. REMOVED RIVETS FROM EXISTING REPAIR AND FOUND EXTENSIVE DAMAGE TO STRINGER. REPLACED STRINGER IAW SRM 51-40-02 AND 51-7 0-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900414 19990409 00414 SO 1999 4 9 C2XA99IA161 1 19990216 A 5411 12039761001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME CRACKED AT OUTBOARD COWL STAY FITTING. STOP DRIL LED CRACKS, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 51-70-05 AND SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900415 19990409 00415 SO 1999 4 9 C2XA99IA164 1 19990216 A 5400 12022766002 STIFFENER EMB 120 EMB120RT SO RT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP WELL STIFFENER CHAFED. REPLACED STIFFENER IAW SR M 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900416 19990409 00416 EU 1999 4 9 C2XA99IA165 1 19990226 A 2424 243230 GCU AEROSP ATR42 ATR42500 EU COCKPIT FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 17448 506 SHV - FLT 3639 - PILOT REPORTED SMOKE IN THE COCKPIT IN CONJUNCTION WITH A NR 2 ACW FAULT INDICATION. THE AIRCRAFT LANDE D AT SHV WITHOUT INCIDENT, WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 ACW GENERATOR CONTROL UNIT. THE AIRCRAFT OPER ATIONALLY CHECKED GOOD AND THEN WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040900417 19990409 00417 GL 1999 4 9 C2XA99CL023 2 19990303 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SW 09 13935 1959 145022 CAE310067 PIT - FLT 4131 - CREW REPORTED THAT THE LEFT ENGINE FLAMED OUT ON LANDING ROLL WITH REVERSER ON, THE ENGINE WOULD NOT RE START ON EITHER FADEC USING THE APU OR CROSS BLEED. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEMS AND FOUND THAT THE LEFT E NGINE HAD EXCEEDED MANUFACTURES LIMITS FOR ITT. THE LEFT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CA RD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999040900418 19990409 00418 SO 1999 4 9 C2XA99CL022 1 19990228 A 2750 3082001007 ACTUATOR EMB 120 EMB120RT SO LT NACELLE FLAP MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16710 6662 0430 120106 CLE - FLT 3194 - CREW REPORTED THAT THEY RECEIVED A NACELLE FLAP ASYMMETRY AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT NACELLE FLAP ACTUATOR IAW EMB-120 MM 27-50-08, OPER ATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900419 19990409 00419 SO 1999 4 9 C2XA99IA153 1 19990213 A 2120 UNKNOWN EMB 120 EMB120RT 3260202 SO CABIN SMOKE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 12715 120125 VCT - DURING FLT 3612, THE CREW REPORTED THE APPEARANCE AND SMELL OF SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO VCT WH ERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS APPROVED FOR FERRY FLIGHT FROM VCT TO IAH DURING WHICH TIME THE ENVIRON MENTAL SYSTEM WAS OPERATIONALLY CHECKED WITH NO EVIDENCE OF SMOKE FOUND. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WH ERE MAINTENANCE APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. NO FURTHER INCIDENTS HAVE BEEN REPORTED TO DATE. (M) 2 L 7 2 4T RT A31SO 1999040900420 19990409 00420 SO 1999 4 9 C2XA99CL020 1 19990223 A 5753 12026791018 BRACKET EMB 120 EMB120ER 3260203 SO TE FLAP BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16718 120136 CLE - FLT 3116 - CREW REPORTED THAT THEY RECEIVED A FLAP DISAGREEMENT LIGHT AFTER TAKEOFF WHEN THE FLAP SELECTOR WAS MOV ED INTO THE UP POSITION. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A DAM AGED GROUND STRAP BRACKET ON THE RIGHT INBOARD FLAP IAW EMB-120MM 27-50-00 AND 20-30-00. OPERATIONAL CHECKS WERE SATISF ACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900421 19990409 00421 SO 1999 4 9 C2XA99CL018 1 19990215 A 2750 3203001005 ACTUATOR EMB 120 EMB120RT SO TE FLAP FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16731 17813 0305 120190 CLE - FLIGHT 3176 - CREW REPORTED THAT THEY RECEIVED A FLAP CONTROL FAULT IN FLIGHT. AIRCRAFT RETURNED TO THE FIELD WITH OUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-07, OPERATIO NAL AND LEAK CHECKS WERE SATISFACTORY IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900422 19990409 00422 SO 1999 4 9 C2XA99CL021 1 19990225 A 2120 AIR DIST EMB 145 EMB145ER SO CABIN ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14943 145040 CLE - FLT 4056 - CREW REPORTED THAT DURING CLIMB THEY RECEIVED SMOKE IN THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO FIEL D WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE APU AS WELL AS THE APU COMPARTMENT FULL OF GLYCOL. THE AREAS WERE CLEANED OF GLYCOL IAW STANDARD MAINTENANCE PRACTICES, OPERATIONAL CHECKS WERE SATISFACTORY. AIR CRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999040900423 19990409 00423 SO 1999 4 9 C2XA99CL019 1 19990217 A 2150 LT PACK EMB 145 EMB145 SO CABIN ODOR A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 13936 145025 CLE - FLT 4011 - CREW REPORTED THE LEFT PACK FILLED THE COCKPIT WITH SMOKE, AFTER THE PACK WAS TURNED OFF THE SMOKE CLEA RED. AIRCRAFT WAS RELEASED IAW MEL 21-51-00 NR 173666. THE NEXT DAY MAINTENANCE INSPECTED THE NR 1 PACK ASSOCIATED COMPO NENTS AND PERFORMED OPERATIONAL CHECKS WITH APU AND ENGINE BLEED AIR WITH NO DEFECTS NOTED IAW EMB-145 MM 21-51-00. REM OVED FROM MEL. (M) 2 L 7 2 4F RT T00011AT 1999040900424 19990409 00424 WP 1999 4 9 USAA990122 1 19990222 A 5330 SKIN DOUG DC9 DC982 3022082 WP STATION 1380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823US 42344 49142 PIT - DURING C-3 CHECK, FOUND .25 INCH CRACK ON SKIN AT STATION 1380 BETWEEN LONGERONS 13L AND 14L. INSTALLED DOUBLER, S TOP DRILLED PER SRM 53-01 FIG 2 SHEET. (M) 2 L 7 2 4F A6WE 1999040900425 19990409 00425 WP 1999 4 9 USAA990119 1 19990222 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 932VJ 76355 47189 PIT - DURING C-6 CHECK, FOUND 1.5 INCH LONGERON CRACKED IN HALF LONGERON NR 4 AND NR 5 AT STATION 756 LT SIDE. INSTALLED DOUBLER PER SRM 53-02 FIG 18, 119-5572 SPLICE AND 119-5573 LONGERON. (M) 2 L 7 2 4F A6WE 1999040900426 19990409 00426 WP 1999 4 9 USAAD99037 1 19990304 A 3350 60030451LB BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 935VJ 48115 CMH - THE MID CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE MID CABIN CEILING EMERGENCY LIGH T POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999040900427 19990409 00427 WP 1999 4 9 USAAD99036 1 19990303 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959VJ 47352 IND - THE EMERGENCY LIGHTS AFT OF ROW 19 AND THE LIGHT ABOVE THE AFT FLIGHT ATTENDANT SEAT WERE INOPERATIVE. MAINTENANCE REPLACED THE NECESSARY EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999040900428 19990409 00428 WP 1999 4 9 USAAD99032 1 19990228 A 3350 110049 BATTERY CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 982VJ 48158 IND - THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR TRACK EMER GENCY LIGHT BATTERY CHARGER. (M) 2 L 7 2 4F A6WE 1999040900429 19990409 00429 WP 1999 4 9 USAAD99031 1 19990228 A 3350 41B001TD05G1 BATTERY DOUG DC9 DC931 3022065 WP CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 937VJ 48117 IND - THE RIGHT NACELLE EMERGENCY LIGHT AND TWO SECTIONS OF THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTEN ANCE REPLACED THE BATTERIES FOR THE INOPERATIVE LIGHTS. (M) 2 L 7 2 4F A6WE 1999040900430 19990409 00430 WP 1999 4 9 99ZZZM230 1 19990228 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 937VJ 48117 IND - THE RIGHT NACELLE EMERGENCY LIGHT AND TWO SECTIONS OF THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTEN ANCE REPLACED THE BATTERIES FOR THE INOPERATIVE LIGHTS. (M) 2 L 7 2 4F A6WE 1999040900431 19990409 00431 WP 1999 4 9 USAAD99033 1 19990301 A 3350 6011777LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CARGO BAY FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 958VJ 47351 IND - THE RIGHT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999040900432 19990409 00432 WP 1999 4 9 USAA990160 1 19990227 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 965 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 2 INCH BY 1 INCH AREA OF CORROSION AT STATION 965 OUTBOARD SIDE OF LT LAV THRESHOLD SUPPOR T FLOORBEAM. REMOVED CORRODED SECTION OF CAP ANGLE AND INSTALLED NEW SECTION AND REPAIR ANGLES PER TYPICAL REPAIR 53-10- 14. (M) 2 L 7 2 4F A6WE 1999040900433 19990409 00433 WP 1999 4 9 USAA990159 1 19990227 A 5220 DOOR PAN DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK FORWARD LEFT EMERGENCY EXIT LOWER AFT DOOR PAN. STOP DRILLED AND INSTALLED DO UBLER PER SRM 52-20-03. (M) 2 L 7 2 4F A6WE 1999040900434 19990409 00434 WP 1999 4 9 USAA990158 1 19990227 A 5220 DOOR PAN DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK AFT RIGHT EMERGENCY EXIT TOP FORWARD DOOR PAN. STOP DRILLED AND INSTALLED DOU BLER PER SRM 52-20-03. (M) 2 L 7 2 4F A6WE 1999040900435 19990409 00435 WP 1999 4 9 USAA990157 1 19990227 A 5220 DOOR PAN DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK RIGHT FORWARD EMERGENCY EXIT TOP FORWARD DOOR PAN. STOP DRILLED AND INSTALLED DOUBLER PER SRM 52-20-03. (M) 2 L 7 2 4F A6WE 1999040900436 19990409 00436 WP 1999 4 9 USAA990156 1 19990227 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK ON SKIN AT STATION 965 LONGERON 6R. CUT OUT CRACK. INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F A6WE 1999040900437 19990409 00437 WP 1999 4 9 USAA990155 1 19990227 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 560-579 LIGHTNING STRIKE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND .25 INCH DIAMETER LIGHTNING STRIKE IN SKIN BETWEEN STATION 560 AND 579 ABOVE LONGERON 7R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 1999040900438 19990409 00438 WP 1999 4 9 USAA990154 1 19990227 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 560 LIGHTNING STRIKE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND .25 INCH DIAMETER LIGHTNING STRIKE IN SKIN AT STATION 560 LONGERON 7R. DRILLED OUT AND INS TALLED RIVET PER SRM 53-04. (M) 2 L 7 2 4F A6WE 1999040900439 19990409 00439 WP 1999 4 9 USAA990153 1 19990227 A 5413 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN WEB AT LEFT PYLON LOWER FLANGE STATION 1030. STOP DRILLED AND INSTALLED DO UBLER PER SRM 54-01. (M) 2 L 7 2 4F A6WE 1999040900440 19990409 00440 WP 1999 4 9 USAA990152 1 19990227 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK AT LONGERON 13R STATION 965. REMOVED CRACKED LONGERON SECTION, INSTALLED NEW SECTION WITH SPLICE PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999040900441 19990409 00441 WP 1999 4 9 USAA990150 1 19990227 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1074 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 48117 PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACK CANTED BELTFRAME STATION 1074. INSTALLED DOUBLER PER SRM 53-03 FIG 30 AND EA 51559. (M) 2 L 7 2 4F A6WE 1999040900442 19990409 00442 WP 1999 4 9 USAA990149 1 19990227 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 953 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47732 48117 PIT - DURING Q-1 CHECK, FOUND .75 INCH CRACK IN FUSELAGE SKIN AT RIGHT SIDE STATION 953 BETWEEN L14 AND L15. INSTALLED T ITANIUM FINGER DOUBLER PER EA 51542. (M) 2 L 7 2 4F A6WE 1999040900443 19990409 00443 WP 1999 4 9 USAA990148 1 19990227 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1074 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUDN 3 INCH CRACK AT CANTED FRAME STATION 1074, LONGERON 6 RT. INSTALLED/FABRICATED 27 DOUBLER, 11 CLIP, 23 DOUBLER. REPETITIVE INSPECTION RED EA NR 51559. TEMP REPAIR PER SRM 53-03 FIG 30. (M) 2 L 7 2 4F A6WE 1999040900444 19990409 00444 WP 1999 4 9 USAA990147 1 19990227 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 560-579 LIGHTNING STRIKE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 48117 PIT - DRUING Q-1 CHECK, FOUND .25 INCH DIAMETER LIGHTNING STRIKE ON SKIN BETWEEN STATION 560-579, 2 INCHES ABOVE 7R. INS TALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 1999040900445 19990409 00445 WP 1999 4 9 USAA990146 1 19990227 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK ON SKIN AT STATION 965 BELOW 6R. INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F A6WE 1999040900446 19990409 00446 WP 1999 4 9 USAA990145 1 19990227 A 5320 ANGLE DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 48602 48037 PIT - DURING C-2 CHECK, FOUND ONE .5 INCH CRACK AT UPPER PYLON ATTACH ANGLE AT STATION 1463 CANTED. STOP DRILLED AND FIL LED PER TYPICAL REPAIR 54-10-06A. (M) 2 L 7 2 4F A6WE 1999040900447 19990409 00447 WP 1999 4 9 USAA990144 1 19990227 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1474 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 48602 48037 PIT - DURING C-2 CHECK, FOUND CANTED FRAME CRACK 3 INCH LONG AT STATION 1474, LONGERON 18 LT. STOP DRILLED CRACKED AND D OUBLER. INSTALLED PER SRM 53-01, FIG 2 SH 4. (M) 2 L 7 2 4F A6WE 1999040900448 19990409 00448 WP 1999 4 9 USAA990161 1 19990227 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1038 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 2 INCH CRACK ON SKIN 4 INCH FORWARD OF FS 1038 AT LONGERON 18L. INSTALLED DOUBLER REPAIR P ER SRM 54-01 FIG 2 (4.5 INCH BY 4 INCH). (M) 2 L 7 2 4F A6WE 1999040900449 19990409 00449 WP 1999 4 9 USAA990120 1 19990222 A 5313 2777922325000 LONGERON DOUG DC9 DC931 3022065 WP BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 932VJ 76355 47189 PIT - DURING C-6 CHECK, FOUND LONGERON CRACKED IN HALF 2 INCHES BY 1 INCH, DISCONTINUITY AT INTERSECTION OF L5R AT STATI ON 639. DETECTED BY EDDY CURRENT. REPAIRED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999040900450 19990409 00450 WP 1999 4 9 USAA990121 1 19990222 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823US 42344 49142 PIT - DURING C-3 CHECK, FOUND .75 INCH CRACK ON SKIN AT STATION 1380 BETWEEN LONGERON 13R AND 14R. INSTALLED DOUBLER, ST OP DRILLED PER SRM 53-01 FIG2, SHT 3. (M) 2 L 7 2 4F A6WE 1999040900451 19990409 00451 NM 1999 4 9 USAA990092 1 19990223 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT FRAME 1360 ON INNER CHORD BETWEEN STRINGER 25R AND 27R. COR ROSION TASK NR'S C53-155-02, C53-156-02, AND C53-163-02. REMOVED CORROSION PER SRM 53-00-07. (M) 2 L 7 2 4F RT A2NM 1999040900452 19990409 00452 NM 1999 4 9 USAA990090 1 19990223 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 1340-1360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL BETWEEN STATION 1340-1360 STRINGER 27R. CORROSION TASK NR'S C53-155-02, C53-156-02, AND C53-163-02. REPAIRED PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999040900453 19990409 00453 NM 1999 4 9 USAA990093 1 19990223 A 5320 WEB BOEING 757 757225 1384959 NM BS 1418 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION 6 INCH BY 1 INCH VERTICAL WEB STATION 1418 LBL 15 SKIN. CORROS ION TASK NR C53-155-02. INSTALLED NEW WEB PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999040900454 19990409 00454 NM 1999 4 9 USAA990089 1 19990223 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 1480-1500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION INERCOSTAL BETWEEN STATION 1480-1500 LBL 25. CORROSION TASK NR C53-155-02, C53-156-02, AND C53-163-02. REPAIRED PER SRM. (M) 2 L 7 2 4F RT A2NM 1999040900455 19990409 00455 NM 1999 4 9 USAA990088 1 19990223 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 1620-1640 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT TOP OF WEB FUSELAGE BS 1620-1640 BL 0 INTERCOSTAL WEB . REPAIRED PER SRM 53-60-51 AND 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999040900456 19990409 00456 NM 1999 4 9 USAA990091 1 19990223 A 5320 STRINGER CLIP BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION STRINGER TIE CLIP AND STRINGER END S29R AT STATION 1640. CORRO SION TASK NR'S C53-155-02, C53-156-02, AND C53-163-02. REPAIRED PER SRM 53-60-53. (M) 2 L 7 2 4F RT A2NM 1999040900457 19990409 00457 NM 1999 4 9 USAA990094 1 19990223 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 1680 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH BY ALONG TOP OF FLOORBEAM AND PAN BS 1680. CO RROSION TASK NR C53-252-03 AND C53-251-03. INSTALLED FILLER ANGLES PER EA 63713 AND EA 63740. (M) 2 L 7 2 4F RT A2NM 1999040900458 19990409 00458 NM 1999 4 9 USAA990070 1 19990223 A 5320 ANGLE BOEING 757 757225 1384959 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES IN FLOORBEAM 377.7 UPPER CAP LOWER SURF LBL 56 AND 61 'T' ANGLE. CORROSION TASK NR C53-221-03. REPAIRED PER SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1999040900459 19990409 00459 NM 1999 4 9 USAA990140 1 19990223 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 1270-1280 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 45672 22205 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL AT STATION 1270-1280 STRINGER 27R UPPER CHORD. COR ROSION TASK NR'S C53-155-02, C53-156-02, AND C53-163-02. REMOVED CORRODED ANGLE AND REPLACED PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999040900460 19990409 00460 NM 1999 4 9 USAASB99057 1 19990223 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 CLE - MAINTENANCE FOUND THE CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK SHORTED. REPLACE D SAME. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999040900461 19990409 00461 NM 1999 4 9 USAASB99061 1 19990228 A 3350 500000043 BATTERY CHARGER BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 LGA - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT SEAT ROWS 15-21 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE B ATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999040900462 19990409 00462 NM 1999 4 9 USAASB99062 1 19990303 A 3350 LIGHT BOEING 737 737301 1384611 NM SEAT 10C INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 356US 23559 ROC - MAINTENANCE FOUND THE FLOOR PROXIMITY IDENTIFIER LIGHT ON SEAT 10C END BAY INOPERATIVE. MAINTENANCE REPLACED DEFEC TIVE WIRE SLICES T END BAY ON SEAT 10C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040900463 19990409 00463 NM 1999 4 9 USAASB99059 1 19990228 A 3350 LIGHT BOEING 737 737201 1384454 NM SERVICE DOOR SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 229US 21818 SDF - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT FOR THE AFT RIGHT SERVICE DOOR FLASHES INTERMITTENTLY DURING TURBULEN CE AND TAXI. MAINTENANCE REPAIRED WIRING TO THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999040900464 19990409 00464 WP 1999 4 9 ORJA99106 1 19990303 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC987 3022087 WP ROW 19-26 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAX, EMERGENCY LIGHTS AT ROWS 19-26 OUT. REMOVED AND REPLACED 3 EACH, BATTERY CHARGERS AT 21A, 20A AND 21F. SYSTEM OP S CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900465 19990409 00465 WP 1999 4 9 ORJA99105 1 19990301 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 23-26 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAX, EMERGENCY LIGHTS REMAIN ON AT ROWS 23-26. CAME ON AT 10,000 IN DESCENT. REMOVED AND REPLACED LEFT BATTERY PACK. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900466 19990409 00466 WP 1999 4 9 ORJA99104 1 19990208 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC987 3022087 WP ROW 17-20 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, ROWS 17-20 ESCAPE LIGHTS INOPERABLE. FOUND AND REPAIRED SHORTED WIRE ON SEAT 19. INSTALLED NEW CHARGER. OPS CHE CKS GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900467 19990409 00467 WP 1999 4 9 ORJA99108 1 19990309 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN SJC - EMERGENCY ESCAPE PATH LIGHTS REMAIN ON IN SECTOR NEAR ROW 16. REMOVED AND REPLACED EMERGENCY LIGHT PACK AT ROW 16, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999040900468 19990409 00468 NM 1999 4 9 P2EA990088 1 19990218 A 5320 SPLICE BOEING 737 737222 1384473 NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, AT BS 360, STRINGER 15L, A CRACK WAS FOUND ON THE STRINGER SPLICE. THE SPLICE WAS REPLACED IAW SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999040900469 19990409 00469 EA 1999 4 9 VTZA99020 1 19990224 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 622BR 7187 FLT 7789 - IAD-SAV - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NO NOSE DOWN TRIM IN FLIGHT. AIRCRAFT RE TURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND HORIZONTAL TRIM ACTUATOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999040900470 19990409 00470 EA 1999 4 9 VTZA99018 1 19990219 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 620BR 7179 FLT 7710 - DAY-IAD - DURING TAKEOFF, EXPERIENCED A PROBLEM WITH THE LANDING GEAR NOT RETRACTING. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DAY. AIRCRAFT LANDED WITH NO PROBLEM. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT MAINTENA NCE WAS DISPATCHED. MAINTENANCE TROUBLESHOT THE SYSTEM AND CONDUCTED NUMEROUS GEAR SWINGS IAW APPLICABLE MM PROCEDURES. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 1999040900471 19990409 00471 EU 1999 4 9 VTZA99016 1 19990131 A 3260 327 BULB BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A VTZA B EMER. DESCENT N FALSE WARNING DE DESCENT 1 EA 27 481UE 895 FLT 6348 - IAD-JFK - DURING DESCENT, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WS RIGHT GEAR WARNING LIGHT DI D NOT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LIGHT BULB, OPS CHECK OK. AIRCRAFT WAS APPROVED AND RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999040900472 19990409 00472 EU 1999 4 9 VTZA99015 1 19990127 A 3310 2LA00691301 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 324UE 41017 FLT 6503 - LGA-IAD - DURING CRUISE, MADE AN EMERGENCY DESCENT INTO LNS DUE TO SMOKE IN COCKPIT. AIRCRAFT WENT TO GATE WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 46994, MEL 33-1 ON CONSOLE LIGHT. MAINTENANCE CLOSED DMI 4 6994 ON 2-4-99 BY REMOVING AND REPLACING CONSOLE LIGHT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999040900473 19990409 00473 EU 1999 4 9 VTZA99014 1 19990114 A 2612 551224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE MALFUNCTIONED A VTZA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 EA 27 481UE 895 FLT 6537 - IAD-RIC - DURING APPROACH, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LEFT ENGINE FIRE WARNING I LLUMINATED. CREW SHUTDOWN ENGINE AND BLEW NR 1 FIRE BOTTLE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT FIRE BOTTLE, LEFT FIRE WIRE LOOP AND FLEX HOSE. MAINTENANCE GROUND RAN AIRCRAF T. OPS CHECK OK. AIRCRAFT WAS APPROVED AND RELEASED AND RETURNED TO SERVICE (M) 2 L 7 2 4T RT A56EU 1999040900474 19990409 00474 WP 1999 4 9 ARWA990306 1 19990319 A 3230 RETRACT MECH DOUG DC8 DC862 3021970 WP LANDING GEAR LACK OF LUBE A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 810BN 45905 MIA - FLT 656 - AIR TURNBACK, ON UPLATCH CHECK, GEAR NOT LATCHED LIGHT ON. PROCEEDED WITH ABNORMAL CHECKLIST. WITH ENGIN E PUMPS OFF, GEAR NOT LATCHED LIGHT CAME ON ABOUT 1 OR 2 MINUTES LATER. UNABLE TO DUMP FUEL ELECTRICALLY, MANUAL STARTE D THEN GOT EXTREMELY HARD, RETRACTED. CHUTE WOULD NOT EXTEND. FLIGHT RETURNED TO MIA WITHOUT INCIDENT. MAINTENANCE FO UND LEFT MLG UPLATCH MECH STIFF AND DRY OF LUBE. LUBED NLG, RIGHT, LEFT MLG UPLATCHED. CYCLED MLG SEVERAL TIMES. NO D EFECTS NOTED IAW 32-30-0. FUEL DUMP ELECTRICAL WIRE NORMAL IAW WDG 28-1-4. FOUND RIVET LEFT DUMP CHUTE OBSTRUCTING TRA VEL. REPLACED RIVET IAW SRM 51-12-8. OPS DUMP SYSTEM NORMAL IAW 28-30-0. PERFORMED OVERWEIGHT LANDING INSPECTION. NO 2 L 7 4 4F 4A25 1999040900475 19990409 00475 WP 1999 4 9 USAA990123 1 19990222 A 5240 RIVET DOUG DC9 DC982 3022082 WP SERVICE DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823US 42344 49142 PIT - DURING C-3 CHECK, FOUND TWO RIVET HEADS POPPED AT NR 1 HORIZ BEAM FORWARD END ON OUTER SKIN OF SERVICE DOOR. REPAI RED AND REPLACED RIVETS PER SRM 52-01 PAGE 1. (M) 2 L 7 2 4F A6WE 1999040900476 19990409 00476 NM 1999 4 9 USAABB99010 1 19990304 A 2160 32148621 VALVE BOEING 767 7672B7 1385107 NM CABIN FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 654US 34485 25225 LGW - FLT 43 - EN ROUTE AMS-PHL, OVER BELFAST, CREW REPORTED THAT THEY WERE UNABLE TO CONTROL THE CABIN TEMPERATURE (TOO COLD). FLIGHT DIVERTED TO LGW AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TRIM AIR VALVE. (M) 2 L 7 2 4F RT A1NM 1999040900477 19990409 00477 SO 1999 4 9 C2XA99CL026 1 19990307 A 3230 RETRACT MECH EMB 145 EMB145ER SO LANDING GEAR MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14943 145040 CLE - FLT 4053 - CREW REPORTED THAT THEY RECEIVED A LANDING GEAR DISAGREEMENT AFTER LIFT OFF, AND AFTER SEVERAL ATTEMPTS THE MAIN LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM AND NO DEFECT WERE NOTED. THE OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-145 MM 32-10-00, AI RCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999040900478 19990409 00478 1999 4 9 ORJA9996 4 19990303 A 3425 FLIGHT DIRECTOR DOUG DC9 DC983 3022083 WP LT/RT FAILED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 879RA 53185 SJC - FLT 241 - RETURNED TO GATE, FLIGHT DIRECTORS ON BOTH SIDES INOPERATIVE, WHEN TAKEOFF/GO AROUND SWITCHES ENGAGED. P LACING BOTH FLIGHT DIRECTORS ON DMI AS PER 34-16 THIS AIRCRAFT IS NOT CATII DMI NR 16374 19552 LED. (M) 2 L 7 2 4F RT A6WE 1999040900479 19990409 00479 WP 1999 4 9 ORJA9997 1 19990225 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROW 24 DEF BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 755RA 49727 AT SJC, SEAT MOUNTED 'E' PATH LIGHT WIRE BROKEN AT SIDEWALL CONNECTOR AT 24 DEF. REPAIRED WIRE AT SEAT 24 DEF 'E' PATH C ONNECTOR LIGHT. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900480 19990409 00480 WP 1999 4 9 ORJA99100 1 19990301 A 3350 BR9961106 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 22-26 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT RNO, INFLIGHT EMERGENCY LIGHTS CAME ON AT ROWS 22-26. REPLACED LEFT AFT O/W EXIT SIGN BATTERY PACK ASSY. OPS CHECK OK . (M) 2 L 7 2 4F RT A6WE 1999040900481 19990409 00481 WP 1999 4 9 ORJA9999 1 19990228 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROW 14 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 AT SJC, EMERGENCY LIGHT AT ROW 14 INOPERABLE. REPAIRED WIRING AT TWO PLACES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900482 19990409 00482 WP 1999 4 9 ORJA9998 1 19990228 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC987 3022087 WP GALLEY DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, EMERGENCY TRACK LIGHTING FORWARD PART OF CABIN CAME ON IN FLIGHT. COULD NOT BE TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IN FORWARD GALLEY. OPS CHECK GOOD. DONE IAW 33-50 MM. (M) 2 L 7 2 4F RT A6WE 1999040900483 19990409 00483 WP 1999 4 9 ORJA99101 1 19990302 A 3350 5100303 BATTERIES DOUG DC9 DC983 3022083 WP EMPENNAGE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 879RA 53185 RNO - EMERGENCY LIGHT INOPERATIVE IN EMPENNAGE. REPLACED BATTERIES, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900484 19990409 00484 WP 1999 4 9 ORJA99102 1 19990302 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC983 3022083 WP RIGHT EMER EXIT FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 881RA 49941 RNO - FORWARD RIGHT EMERGENCY EXIT EMERGENCY LIGHT BATTERY CHARGER BAD. REMOVED AND REPLACED BAD CHARGER. OPS CHECKED GO OD. (M) 2 L 7 2 4F RT A6WE 1999040900485 19990409 00485 WP 1999 4 9 ORJA9993 1 19990228 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC983 3022083 WP ROW 20F FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO - EMERGENCY FLOOR LIGHTS STAY ON. REMOVED AND REPLACED BATTERY CHARGER AT SEAT ROW 20F. SYSTEM CHECK NORMAL AT TH IS TIME. (M) 2 L 7 2 4F RT A6WE 1999040900486 19990409 00486 WP 1999 4 9 ORJA9992 1 19990227 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC983 3022083 WP RT EMER EXIT FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RON - EMERGENCY LIGHTS AT SEATS 17-20 WILL NOT STAY ILLUMINATED. FOUND BROKEN WIRING AT SEATS 17, 18, 19, 20. RECONNE CTED WIRING FROM WALL TO SEATS ASSY AND INSTALLED NEW BATTERY PACK/CHARGER AT AFT RIGHT O/W EXIT OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999040900487 19990409 00487 WP 1999 4 9 ORJA9991 1 19990227 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN LAS, EXIT ROW LIGHTING CAME ON IN FLIGHT SOME FLICKERING AND SOME STEADY NOT ALL LIGHTS WERE REFLECTED. SECURED LOOSE BATTERIES OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999040900488 19990409 00488 WP 1999 4 9 ORJA9990 1 19990227 A 3350 41B004AD073 BATTERIES DOUG DC9 DC983 3022083 WP GALLEY DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN SNA, EXIT ROW LIGHTING INOPERATIVE IN CABIN LIGHTS FOR SEATS 16, 17, 18, 19, 20 CAME ON IN FLIGHT. ROWS 16-20 CHECK O K. FOUND ROWS 3-7 INOPERATIVE, CHANGED BATTERIES IN FORWARD GALLEY POWER SUPPLY ALL EMERGENCY LIGHTS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999040900489 19990409 00489 WP 1999 4 9 ORJA9995 1 19990225 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 29-32 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 RNO - EMERGENCY LIGHTS ROW 29 THROUGH 32 ILLUMINATED AND WILL NOT SHUT OFF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FOR ROW 29-32 IAW MM 33-00. OPS CHECK NORMAL, OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 1999040900490 19990409 00490 WP 1999 4 9 ORJA9994 1 19990226 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 14-19 DEF DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 SJC - EMERGENCY SEAT LIGHTING INOPERATIVE 14-19 DEF. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900491 19990409 00491 WP 1999 4 9 99ZZZM231 1 19990113 A 3231 H2014B SWITCH DOUG DC8 DC8F54 3021926 WP RT MLG DOOR FAILED A FXLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 57FB 69159 45669 DURING CRUISE GEAR UNSAFE LIGHT ILLUMINATED. CYCLED GEAR AND RECEIVED THREE GREEN LIGHTS FOR LANDING GEAR. LANDED AT MIA WITHOUT INCIDENT. GROUND INSPECTION REVEALED RIGHT MAIN LANDING GEAR DOOR NOT FULLY CLOSED. REPLACED LEFT AND RIGHT D OOR MICROSWITCHES, LUBED DOOR UPLATCH MECHANISM AND PULLEY SYSTEM. PERFORMED GEAR RETRACTION AND SYSTEM OPERATED NORMAL . RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1999040900492 19990409 00492 WP 1999 4 9 99ZZZM232 1 19990217 A 7120 BOLT DOUG DC8 DC861 3021952 WP NR 1 ENGINE BROKEN A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 47801 46159 DURING MAINTENANCE CHECK, FOUND OUTBOARD AFT ENGINE MOUNT ARM BOLT BROKEN IN THREADED AREA ON NR 1 ENGINE. REMOVED AND R EPLACED AFT ENGINE MOUNT ASSEMBLY. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1999040900493 19990409 00493 1999 4 9 TWRA9908 4 19990309 A 3454 38091393 RMI BENDIX BOEING 747 747131 1384881 NM RT COCKPIT FAILED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 608FF 7005572 19672 DURING CRUISE, SMOKE WAS OBSERVED AS COMING FROM VICINITY OF CO-PILOT'S RMI. CIRCUIT BREAKER WAS PULLED AND SMOKE DISSIP ATED. REPLACED NR 2 RMI INDICATOR. CHECKED CONNECTIONS AND AREA FROM SMOKE AND OR OTHER DAMAGE. NO ADDITIONAL DAMAGE W AS FOUND. NEW INDICATOR OPS CHECK OK AS PER MM 34-30-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1999040900494 19990409 00494 1999 4 9 MASA99038 4 19990304 A 2330 CHIME DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 6255 - PHX-DRO - PRIOR TO DEPARTURE, PILOT REPORTED THE EMERGENCY CALL CHIME AND LIGHT INOPERATIVE. THE DISCREPANCY WAS DEFERRED PER MEL 23-3. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, IT WAS TROUBLESHOT, NO DISCRE PANCY WAS NOTED. (M) 2 H 7 2 4T RT A13NM 1999040900495 19990409 00495 EA 1999 4 9 MASA99011 1 19990119 A 3350 100865B POWER SUPPLY CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5755 - PHL-STL - DURING PREFLIGHT, FOUND TWO FLOOR ESCAPE PATH LIGHTS WERE NOT ILLUMINATING. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BATTERY WAS RECHARGED, PERFO RMED GROUND TEST, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 1999040900496 19990409 00496 NM 1999 4 9 BJNA990301 1 19990307 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM RT EMER EXIT FAILED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 20336 RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE ON TEST. REPLACED EMERGENCY EXIT LIGHT ASSY, IAW BMM 33-51-31, GROUND C HECKS NORMAL IAW BMM 33-51-21. (M) 2 L 7 2 4F A16WE 1999040900497 19990409 00497 NM 1999 4 9 BJNA990302 1 19990309 A 3350 1102833 LIGHT BOEING 737 7372H4 138448C NM CABIN FAILED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 20336 FOUND FORWARD BULLNOSE EMERGENCY LIGHT OUT. REMOVED AND REPLACED LIGHT ASSY IAW 33-51-11, OPS CHECKS OK. (M) 2 L 7 2 4F A16WE 1999040900498 19990409 00498 WP 1999 4 9 ASAA9980043 1 19990212 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 FAI - AFTER ARRIVAL OF FLIGHT 115, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. LUBRICATED DOOR OPERATING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999040900499 19990409 00499 WP 1999 4 9 ASAA9980044 1 19990213 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 ANC - AFTER ARRIVAL OF FLIGHT 88, CREW REPORTED THE L1 DOOR IS DIFFICULT TO OPEN AFTER CABIN HAS BEEN PRESSURIZED, OPERA TION NORMAL ON SUBSEQUENT OPENINGS. INSPECTED L1 DOOR AND ACCOMPLISHED GROUND PRESSURIZATION CHECK TO 6.0 PSID, NO DEFEC T NOTED AND FOUND OPENING FORCE WITHIN DC9 MM LIMITS. ADJUSTED DOOR ROTATION ROD AS PRECAUTION AND OPERATED NORMALLY. ( M) 2 L 7 2 4F RT A6WE 1999040900500 19990409 00500 WP 1999 4 9 ASAA9980045 1 19990214 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WOULD NOT CLOSE FROM OUTSIDE. RERIGGED THE L1 DOOR IAW DC9 MM AND OPERATED N ORMALLY. (M) 2 L 7 2 4F A6WE 1999040900501 19990409 00501 NM 1999 4 9 ASAA9940061 1 19990301 A 5542 65C2584151 SKIN BOEING 737 7374Q8 NM RUDDER SEPARATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 SEA - DURING SCHEDULED C-CHECK, THE RIGHT SIDE OF THE RUDDER SKIN FIRST PLY WAS FOUND TO BE SEPARATED. REPAIRED PER EA 5 540-01030 AND BOEING TELEX ASA-SEA-99-0114RR. (M) 2 L 7 2 4F RT A16WE 1999040900502 19990409 00502 NM 1999 4 9 ASAA9940062 1 19990301 A 5730 SKIN BOEING 737 7374Q8 NM WS 340 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 778AS 25110 SEA - DURING SCHEDULED C-CHECK, FOUND DAMAGE TO THE NR 1 SLAT CENTER AUXILIARY TRACK CUTOUT SKIN AT SS 340.70. REPAIRED PER EA 5740-01159. (M) 2 L 7 2 4F RT A16WE 1999040900503 19990409 00503 NM 1999 4 9 ASAA9940059 1 19990301 A 5210 DOOR MECHANISM BOEING 737 737490 1384715 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 SEA - FLIGHT 429 - L1 DOOR DIFFICULT TO OPEN AND WAS MAKING A POPPING SOUND WHEN OPENING AND CLOSING. INSPECTED DOOR AND FOUND CAM PLATE DRY. LUBRICATED DOOR HINGES AND SNUBBER. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999040900504 19990409 00504 NM 1999 4 9 ASAA9940049 1 19990212 A 5315 65C345973 FLOORBEAM BOEING 737 7374Q8 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOORBEAM AT STATION 947 LBL 4 AND RBL 5 WAS FOUND TO BE CORRODED . REPAIRED PER EA 5310-01642. (M) 2 L 7 2 4F RT A16WE 1999040900505 19990409 00505 NM 1999 4 9 ASAA9940048 1 19990212 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7374Q8 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOORBEAM AT STATION 967 RBL 18 WAS FOUND TO BE CORRODED. INSTALL ED REPAIR SECTION, SPLICE AND STRAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999040900506 19990409 00506 NM 1999 4 9 ASAA9940047 1 19990212 A 5320 INTERCOSTAL BOEING 737 7374Q8 NM BS 294.5-312 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE INTERCOSTAL AT BS 294.5-312 STRINGER 4L WAS FOUND TO BE CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1999040900507 19990409 00507 NM 1999 4 9 ASAA9940046 1 19990212 A 5320 6547690 SUPPORT BOEING 737 7374Q8 NM BS 867-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT FROM STATION 867-947 STRINGER 25R WAS FOUND TO BE COR RODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1999040900508 19990409 00508 NM 1999 4 9 ASAA9940045 1 19990212 A 5320 65C333756 SUPPORT BOEING 737 7374Q8 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT AT STATION 947 BETWEEN RBL 24 AND RBL 50 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999040900509 19990409 00509 NM 1999 4 9 ASAA9940044 1 19990212 A 5320 65C340597 SUPPORT BOEING 737 7374Q8 NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT AT STATION 947-967 RBL 16 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-00. (M) 2 L 7 2 4F RT A16WE 1999040900510 19990409 00510 NM 1999 4 9 ASAA9940043 1 19990212 A 5320 65C340593 SUPPORT BOEING 737 7374Q8 NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT BETWEEN STATION 947-967 LBL 16 WAS FOUND TO BE CORR ODED. REPLACED FLOOR SUPPORT PER SRM 51-40-01. (M) 2 L 7 2 4F RT A16WE 1999040900511 19990409 00511 NM 1999 4 9 ASAA9940042 1 19990212 A 5320 65C333701 SUPPORT BOEING 737 7374Q8 NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT BETWEEN STATION 947-967 LBL 24 WAS FOUND TO BE CORR ODED. REPLACED FLOOR SUPPORT PER SRM 51-40-01. (M) 2 L 7 2 4F RT A16WE 1999040900512 19990409 00512 NM 1999 4 9 ASAA9940041 1 19990212 A 5320 BAC1505100403 SUPPORT BOEING 737 7374Q8 NM BS 54 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE FLOOR SUPPORT AT BS 334 RBL 54 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 5 1-30-02. (M) 2 L 7 2 4F RT A16WE 1999040900513 19990409 00513 NM 1999 4 9 ASAA9940040 1 19990212 A 5320 SUPPORT BOEING 737 7374Q8 NM BS 312-328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE FORWARD CABIN UPPER SURFACE FLOOR SUPPORT AT STATION 312-328 LBL 13 WAS FOUND TO BE CORRO DED. REPLACED FLOOR SUPPORT PER SRM 51-30-02 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999040900514 19990409 00514 NM 1999 4 9 ASAA9940039 1 19990212 A 5753 SKIN BOEING 737 7374Q8 NM LT TE MIDFLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE LEFT WING OUTBOARD T/E MIDFLAP WAS FOUND TO BE WORN AT THE LEADING EDGE. REPAIRED PER EA 5750-01311. (M) 2 L 7 2 4F RT A16WE 1999040900515 19990409 00515 NM 1999 4 9 ASAA9940038 1 19990212 A 5753 SKIN BOEING 737 7374Q8 NM LT TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE LEFT WING T/E INBOARD FOREFLAP LOWER SURFACE WAS FOUND TO HAVE THREE DENTS. REPAIRED PER SRM 57-53-02 AND SRM 51-70-10 REPAIR NR 20. (M) 2 L 7 2 4F RT A16WE 1999040900516 19990409 00516 NM 1999 4 9 ASAA9940037 1 19990212 A 5347 BAC1520792 SEAT TRACK BOEING 737 7374Q8 NM BS 480-500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, FOUND CORROSION ON THE RIGHT OUTBOARD SEAT TRACK AT STATION 480-500A. REPLACED SEAT TRACK PER SRM 53-30-52. (M) 2 L 7 2 4F RT A16WE 1999040900517 19990409 00517 NM 1999 4 9 ASAA9940036 1 19990212 A 5315 6511681179 FLOORBEAM BOEING 737 7374Q8 NM BS 987 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOORBEAM AT STATION 987 LBL 36 - RBL 43 WAS FOUND TO BE CORRODED . REPAIRED FLOORBEAM PER EA 5310-01641. (M) 2 L 7 2 4F RT A16WE 1999040900518 19990409 00518 NM 1999 4 9 ASAA9940035 1 19990212 A 5315 6545815 FLOORBEAM BOEING 737 7374Q8 NM BS 344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE FORWARD CABIN UPPER SURFACE FLOORBEAM AT STATION 344 LBL 14-55 WAS FOUND TO BE CORRODED. REPLACED UPPER CHORD FLOORBEAM PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999040900519 19990409 00519 NM 1999 4 9 ASAA9940034 1 19990212 A 5315 FLOORBEAM BOEING 737 7374Q8 NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 PHX - DURING SCHEDULED SI, THE FORWARD CABIN UPPER SURFACE FLOORBEAM AT STATION 312 LBL 13 - RBL 10 WAS FOUND TO BE CORR ODED. REPLACED T-CHORD PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999040900520 19990409 00520 SO 1999 4 9 ASOA99024 1 19990211 A 5400 12008527001 ANGLE EMB 120 EMB120RT SO LT NACELLE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 215AS 120010 DURING C-CHECK INSPECTION, THE FRAME 2 ANGLE ON LEFT ENGINE NACELLE WERE FOUND BROKEN. REMOVED AND REPLACED FRAME ANGLE ON LEFT ENGINE NACELLE. (M) 2 L 7 2 4T RT A31SO 1999040900521 19990409 00521 NE 1999 4 9 ASOA99025S 2 19990216 A 7260 DRIVE SHAFT EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 11 275AS 120234 115385 EN ROUTE ATL-CRW AT FL230, THE LEFT ENGINE 'ENGINE CONTROL' AND 'OIL PRESSURE' AURAL WARNINGS CAME ON. CREW NOTED THAT T HE OIL PRESSURE, NH AND TORQUE ALL READ ZERO, WITH AN OIL PRESSURE LIGHT ON THE MAP. CREW SHUT DOWN THE LEFT ENGINE, DEC LARED AN EMERGENCY, ELECTRICALLY FEATHERED THE LEFT ENGINE AND LANDED UNEVENTFULLY AT TRI. ASA MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. TEA RDOWN REPORT INDICATES THE ACCESSORY DRIVE SHAFT FAILED AT THE UPPER END. THIS LEAD TO THE LOSS OF FUEL PUMP DRIVE AND SUBSEQUENT ENGINE FLAME OUT. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999040900522 19990409 00522 SO 1999 4 9 ASOA99029 1 19990306 A 5330 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 244AS 120073 DURING INSPECTION, FOUND CORROSION AT FRAME 21 BETWEEN STRINGERS 21 LEFT AND 21 RT. REPAIR CORROSION DAMAGE PER INSTRUCT IONS CONTAINED IN ASA EO120-53-0057, EAC FAX 283/96, 246/95, 97/TA1325, SST-348/97, SRM 51-00-00, SRM 53-00-00, AND HBDK -5, 3.2.3, 8.1, 8.1.2 AND ENSURE CORROSION PREVENTATIVE COMPOUND IS APPLIED TO AFFECTED AREA. (M) 2 L 7 2 4T RT A31SO 1999040900523 19990409 00523 SO 1999 4 9 ASOA99003 1 19990104 A 5720 12016806001 ANGLE EMB 120 EMB120RT SO LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 225AS 120022 DURING INSPECTION FOUND LEFT WING, RIB 17, SPAR ANGLE CRACKED. MCN MAINTENANCE REPAIRED WING SPAR IAW ASA EO120-57-0066, REFERENCE DATA EAC FAX SST-2447/98 AND SRM 51-00-00. (M) 2 L 7 2 4T RT A31SO 1999040900524 19990409 00524 SO 1999 4 9 ASOA99004 1 19990111 A 5330 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 225AS 120022 DURING INSPECTION, FOUND CORROSION ON FRAME 23 BETWEEN STRINGERS 17 RT AND 18 RT. REPAIRED IAW EO120-53-0093, REFERENCES EAC FAXS EST 246/95, EST 226/96, EST 283/96, SRMS 51-00-00 AND 53-00-00, AND HBDK5 REFS 3.2.3, 8.1 AND 8.1.2. (M) 2 L 7 2 4T RT A31SO 1999040900525 19990409 00525 SO 1999 4 9 ASOA99005 1 19990110 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR DETACHED A ASOA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 284AS 120249 EN ROUTE ATL-ILM AND LEVELED OFF AT 20,000 FEET, EXPERIENCED RAPID DEPRESSURIZATION. CREW EXECUTED AN EMERGENCY DESCENT AND DIVERTED TO FLO, WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. LOCAL MTC C/W MEL PROCEDURES AND THE AI RCRAFT CONTINUED FLIGHT UNPRESSURIZED. ATL MAINTENANCE FOUND THE RIGHT SECTION OF THE CARGO DOOR SEAL DETACHED FROM DOO R AND RESECURED. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE DEFER LOG WAS CLEARED AND THE AIRCRAFT RELEASED FOR FURTHE R SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900526 19990409 00526 EU 1999 4 9 ASOA99007 1 19990113 A 3350 NEC3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DEFECTIVE A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 641AS 387 CREW REPORTED THAT THE AFT EMERGENCY FLOOR TRACK LIGHTING REMAINS ON, AND ALSO WHEN THE EMERGENCY EXIT LIGHT IS ARMED. T HE LIGHTS REMAIN ON WITH AIRCRAFT POWER ON. ATL MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLIES A T 62WL AND 73WL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040900527 19990409 00527 SO 1999 4 9 ASOA99008 1 19990118 A 3397 WIRE EMB 120 EMB120RT SO CABIN CHAFED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 283AS 120236 MAINTENANCE WAS ADVISED THAT THE FLIGHT ATTENDANT EMERGENCY LIGHTS TESTS SWITCH POPS THE EMERGENCY LIGHTS C/B. ATL, MAIN TENANCE FOUND A CHAFED WIRE AT CANNON PLUG P0389 (AT NR 2 BATTERY PACK) AND REPAIRED WIRE AS NEEDED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900528 19990409 00528 SO 1999 4 9 ASOA99009 1 19990118 A 2121 EVAC2322C2 FAN EMB 120 EMB120RT SO RT PACK FAILED A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 500AS 20855 120272 ON TAXI OUT, CREW ADVISED THAT THE RIGHT PACK FAILED AND REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO THE GATE AND DEBOARDED. ATL, MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK GROUND COOLING FAN. OPERATIONAL CHECKS WERE GOOD AND TH E AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900529 19990409 00529 SO 1999 4 9 ASOA99010 1 19990119 A 5411 12003852001 FRAME EMB 120 EMB120RT SO LT/RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 243AS 120072 DURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999040900530 19990409 00530 SO 1999 4 9 ASOA99011 1 19990119 A 5320 12019522001 SUPPORT BRACKET EMB 120 EMB120RT SO BS 14280/14615 SEPARATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 243AS 120072 DURING C-CHECK INSPECTION, FS X14280 AND FS X14616 FUSELAGE FRAMES ATTACHED TO CARGO DOOR OPENING UPPER FRAME SUPPORT BR ACKETS FOUND TO BE SEPARATED AT BOTH FRAME STATIONS. REMOVED AND REPLACES UPPORT BRACKETS. (M) 2 L 7 2 4T RT A31SO 1999040900531 19990409 00531 SO 1999 4 9 ASOA99012 1 19990119 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT/RT NACELLE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 243AS 120072 DURING C-CHECK INSPECTION, THE FRAME 2 ANGLE ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND BROKEN. REMOVED AND REPLACED F RAME ANGLES ON LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999040900532 19990409 00532 EU 1999 4 9 RAIA990322 1 19990315 A 3060 A403 TERMINAL JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 573HK 41092 FLT 7744 - DCA - RIGHT PROP DE-ICE FAULTED. MAINTENANCE REPLACED BRUSH BLOCK TERMINAL STRIP ON RIGHT PROP. (M) 2 L 7 2 4T RT A41NM 1999040900533 19990409 00533 WP 1999 4 9 RAIA990321 2 19990312 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA E ENGINE SHUTDOWN Y ENGINE STOPPAGE LD LANDING 1 CE 03 867AE 14697 867 66074 FLT 4774 - LAX - LEFT ENGINE FAILED IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999040900534 19990409 00534 EU 1999 4 9 RAIA990320 1 19990308 A 3060 B40610 DE-ICE LEAD JETAIR JETSTM JETSTM4101 1500501 EU RT PROP DE-ICE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 551HK 41040 FLT 7516 - STL - RIGHT PROP DE-ICE FAULTED. MAINTENANCE REPLACED A PROP DE-ICE LEAD ON RIGHT PROP. (M) 2 L 7 2 4T RT A41NM 1999040900535 19990409 00535 1999 4 9 RAIA990325 4 19990317 A 2312 6226152001 TRANSCEIVER BAG JETSTM JETSTM3201 1500217 EU NR 1 COMM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 342TE 14608 954 FLT 7033 - STL - NR 1 COMM INOP. MAINTENANCE REPLACED NR 1 COM TRANSCEIVER. (M) 2 L 7 2 4T RT A56EU 1999040900536 19990409 00536 1999 4 9 RAIA990324 4 19990317 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 572HK 5607 41091 FLT 7739 - JFK - HEADING COMPARITOR ERROR FLAGGED ON TAXI. MAINTENANCE REPLACED NR 2 AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999040900537 19990409 00537 EU 1999 4 9 RAIA990323 1 19990316 A 3610 31081961 GASKET BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 429AM 879 FLT 7377 - UIN - LEFT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED BLEED AIR GASKET ON LEFT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999040900538 19990409 00538 EU 1999 4 9 RAIA990329 1 19990320 A 3244 TIRE JETAIR JETSTM JETSTM4101 1500501 EU NLG FLAT A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 570HK 41089 FLT 7570 - DCA - NOSEWHEEL FAILED TO RESPOND DURING TAXI. MAINTENANCE REPLACED BOTH NOSE WHEEL ASSY, BECAUSE THEY WERE F LAT. (M) 2 L 7 2 4T RT A41NM 1999040900539 19990409 00539 EU 1999 4 9 RAIA990328 1 19990319 A 2120 AIR DIST AEROSP ATR72 ATR72202 8680940 EU CABIN ODOR A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7158 - STL - ON TAXI OUT, NOTICED AN UNIDENTIFIABLE ODOR. MAINTENANCE PERFORMED GROUND RUN AND OPERATED AIR COND SYS TEM. NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A53EU 1999040900540 19990409 00540 WP 1999 4 9 RAIA990313 2 19990309 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 337TE 14332 929 66152 FLT 7468 - STL - LEFT ENGINE MAKING A LOUD WHINING NOISE. MAINTENANCE REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999040900541 19990409 00541 EU 1999 4 9 RAIA990312 1 19990309 A 3010 EAS10910515 LINE JETAIR JETSTM JETSTM4101 1500501 EU LT HORIZ STAB FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 566HK 41084 FLT 7779 - DCA - AIRFRAME DE-ICE FAILED IN AUTO AND MANUAL CIRCUITS NR 1 AND NR 2. MAINTENANCE REPLACED LINE TO LEFT HOR IZONTAL STABILIZER. (M) 2 L 7 2 4T RT A41NM 1999040900542 19990409 00542 NM 1999 4 9 UIEA9913 1 19990310 A 5730 65B067212 PANEL BOEING 747 7472D7B 1384803 NM RT WING MISSING A UIEA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 EA 15 526MC 22337 DURING WALKAROUND, FOUND 6 INCH BY 12 INCH PIECE OF RIGHT WING FUSELAGE PANEL MISSING. NO OTHER ABNORMALITIES NOTED. REP LACED PANEL P/N 65B067212. (M) 2 L 7 4 4F RT A20WE 1999040900543 19990409 00543 NM 1999 4 9 UIEA9911 1 19990225 A 2410 705117E CSD BOEING 747 747243B 1384830 NM NR 4 ENGINE FAILED A UIEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 15 516MC 22507 FLT 7127 - MIA/VCP - NR 4 CSD OIL LIGHT 'ON', CSD OIL TEMPERATURE HIGH (OUT OF RANGE 150 PLUS). ATTEMPT TO DISCONNECT CS D UNSUCCESSFUL. CSD RPM '0', PMG VOLTS '70'. FOLLOWED ALL DISCONNECT PROCEDURES THEN SHUTDOWN NR 4 ENGINE. ON ARRIVAL AT VCP MAINTENANCE FOUND NR 4 CSD DEFECTIVE. REPLACED NR 4 CSD, OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1999040900544 19990409 00544 NM 1999 4 9 UIEA9910 1 19990222 A 3246 260356112 WHEEL BOEING 747 7472D3B 1384805 NM LT MLG FAILED A UIEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 506MC 21252 FLT 1871 - BTB - DURING TAXI OUT, CREW REPORTED THAT THEY FELT A BUMP AND HEARD A LOUD BANG. AIRCRAFT STOPPED AND AREA C HECKED. FOUND NR 8 WHEEL RIM BROKE, DAMAGE TO NR 11 RIM, LEFT BODY GEAR DOORS, WIRING CONDUITS AND TRUCK BEAM. PERFORME D FAILED TIRE INSPECTION IAW MM 5-51-34 AND NO FURTHER DAMAGE FOUND. REPLACED BODY GEAR DOOR ASSEMBLIES, CONDUIT, TRUCK AND WHEEL ASSEMBLIES/BRAKES FOR POSITIONS NR 7, 8 AND 11. OPERATIONAL CHECKS SATISFACTORY. (M) 2 L 7 4 4F RT A20WE 1999040900545 19990409 00545 NM 1999 4 9 TSAA9933149 1 19990316 A 3350 8731002511 LIGHT BOEING 737 737230C 1384472 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSEMBLY NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999040900546 19990409 00546 NM 1999 4 9 ORJA99111 1 19990308 A 3350 BR9661106 BATTERY PACK DOUG MD90 MD9030 3023690 NM ROW 27 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 902RA 53490 SJC - EMERGENCY EXIT LIGHTS OVERWING EXITS ARE FLASHING INTERMITTENTLY. REMOVED AND REPLACED E-PATH LIGHT BATTERY PACK A T 27, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999040900547 19990409 00547 NM 1999 4 9 ORJA99113 1 19990309 A 3350 BR9661106 BATTERY PACK DOUG MD90 MD9030 3023690 NM ROW 22/19 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 902RA 53490 SJC - OVERWING EMERGENCY LIGHT STAY ILLUMINATED. REMOVED AND REPLACED BATTERY PACKS AT ROW 22 AND 19. OPS CHECK EMERGENC Y LIGHTS OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999040900548 19990409 00548 WP 1999 4 9 ORJA99110 1 19990309 A 3350 BR9661105 LIGHT DOUG DC9 DC983 3022083 WP ROW 17-20 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 ORD - EMERGENCY LIGHTS ON RIGH SEATS ROWS 17-20 WOULD NOT GO OUT. REPLACED LIGHT MODULE AT LEFT EXIT LIGHT, ACCOMPLISHED CHECK, NO FAULTS. (M) 2 L 7 2 4F RT A6WE 1999040900549 19990409 00549 NM 1999 4 9 MZZA99054 1 19990318 A 2752 49275890002 ACTUATOR BOEING 727 7272F9 138407D NM RT TE FLAP FAILED A MZZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 75429 21427 FLT 921 - GUM - AIR RETURN DUE TO SYSTEM 'A' HYDRAULIC LEAK. MAINTENANCE FOUND FLAP HYDRAULIC MOTOR FAILED. REMOVED AND REPLACED FLAP ACTUATOR HYDRAULIC MOTOR IAW MM 27-51-62. INSPECTED CASE DRAIN FILTERS ALL CHECKED GOOD. AIRCRAFT RELEAS ED FOR SERVICE. (M) 2 L 7 3 4F RT A3WE 1999040900550 19990409 00550 NM 1999 4 9 EISA99018 1 19990129 A 2131 1061209714 CONTROLLER BOEING 727 72725 1384006 NM COCKPIT MALFUNCTIONED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 290NE 18972 COULD NOT MAINTAIN CABIN ALTITUDE BELOW 10,000 FEET. CABIN RATE OF CLIMB 1700 FEET PER MINUTE WITH ONE PACK OPERATING. AIR TURN BACK TO BUD. RAN PACK PER MM 21-50. PERSSURIZATION CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1999040900551 19990409 00551 NM 1999 4 9 EISA99028 1 19990216 A 3297 H1010153 WIRE BOEING 727 727223 1384074 NM COCKPIT BROKEN A EISA K NONE N FALSE WARNING DE DESCENT 1 SW 07 6813 19488 NOSE GEAR RED UNSAFE LIGHT ON AND GREEN LIGHT ON WITH GEAR EXTENDED. REPAIRED GROUND WIRE FROM LOCK SWITCH. (M) 2 L 7 3 4F A3WE 1999040900552 19990409 00552 NM 1999 4 9 EISA99027 1 19990216 A 3260 H1010153 SWITCH BOEING 727 727223 1384074 NM NLG FAILED A EISA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 6813 19488 AFTER NOSE GEAR EXTENSION, BOTH GREEN AND RED ILLUMINATED. AFTER MAIN GEAR EXTENDED, ONLY GREEN LIGHT ON. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH, PERFORMED GEAR SWING NUMEROUS TIMES. OPS CHECK GOOD PER MM 32-61-7. (M) 2 L 7 3 4F A3WE 1999040900553 19990409 00553 NM 1999 4 9 EISA99021 1 19990119 A 3610 65594241 DUCT BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 07 6813 19488 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED WHILE ENGINE ANTI-ICE WING ANTI-ICE WERE IN USE. CLOSING THE WING ANTI-ICE AN D A CO-INCIDENTAL REDUCTION IN POWER DURING AN APPROACH EXTINGUISHED LIGHT. LOG PAGE 58944 MEL 30-2 PLACARD 980. REMOV ED AND REPLACED CRACKED PNEUMATIC DUCT ABOVE APU NEAR KEEL BEAM IAW MM 36-00-1, PAGE 201. LEAKS CHECK GOOD PER MM 30-13 -0A, PAGE 506, PLACARD REMOVED. (M) 2 L 7 3 4F A3WE 1999040900554 19990409 00554 WP 1999 4 9 EISA99025 1 19990213 A 3350 6030451LB BATTERY PACK DOUG DC9 DC931 3022065 WP BS 629 DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 943VJ 47058 AUXILIARY (FORWARD) OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT FS 629 OVERHEAD. EM ERGENCY LIGHTS OPS CHECK GOOD PER MM 33-51-01. (M) 2 L 7 2 4F A6WE 1999040900555 19990409 00555 WP 1999 4 9 EISA99024 1 19990209 A 3350 08164120 LIGHTS DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 943VJ 47058 EMERGENCY LIGHTS WILL NOT GO OUT ON THE RIGHT AFT FLOOR TRACK. CYCLED BATTERY EMERGENCY POWER SWITCHES. LIGHTS WENT OU T, CUT POWER TO AIRCRAFT, LIGHTS STILL OUT. OPS CHECK GOOD PER MM 33-51-0. (M) 2 L 7 2 4F A6WE 1999040900556 19990409 00556 WP 1999 4 9 EISA99022 1 19990201 A 3230 59104475005 MECHANISM DOUG DC9 DC931 3022065 WP NLG OUT OF ADJUST A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 969VJ 47421 AFTER TAKEOFF AND RAISING GEAR AIRCRAFT GROUND SHIFT MECHANISM NEVER WENT TO FLIGHT MODE, FOLLOWED PROCEDURES AND RETURN ED TO AEX. ADJUSTED GROUND SENSING MECHANISM IAW DC-9 MM 32-23-1. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1999040900557 19990409 00557 WP 1999 4 9 EISA99019 1 19990129 A 2560 11331DGDME SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR LOOSE A EISA K NONE O OTHER UK UNKNOWN 1 SW 07 945VJ 370 47066 RIGHT FORWARD DOOR ESCAPE SLIDE LOOSE FROM DOOR. REINSTALLED FORWARD GALLEY DOOR ESCAPE SLIDE, REINSTALLED LOCK RELEASE CABLE IAW MM 25-62-0. (M) 2 L 7 2 4F A6WE 1999040900558 19990409 00558 NM 1999 4 9 EISA99016 1 19990121 A 2133 10328051 OUTFLOW VALVE BOEING 727 72725 1384006 NM LEFT FAILED A EISA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 290NE 18972 CLIMBING THROUGH FLIGHT LEVEL 280, CABIN PRESSURIZATION FAILED IN AUTO MODE AND MANUAL MODE. REMOVED AND REPLACED LEFT AND RIGHT OUTFLOW VALVES. OPS CHECK GOOD PER MM 21-30-51. (M) 2 L 7 3 4F A3WE 1999040900559 19990409 00559 NM 1999 4 9 99ZZZM233 1 19990121 A 2133 10328051 OUTFLOW VALVE AIRESRCH BOEING 727 72725 1384006 NM RIGHT FAILED A EISA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 290NE 1061091 18972 CLIMBING THROUGH FLIGHT LEVEL 280, CABIN PRESSURIZATION FAILED IN AUTO MODE AND MANUAL MODE. REMOVED AND REPLACED LEFT A ND RIGHT OUTFLOW VALVES, OPS CHECK GOOD PR MM 21-30-51. (M) 2 L 7 3 4F A3WE 1999040900560 19990409 00560 WP 1999 4 9 EISA99020 1 19990130 A 2560 1133169 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR INOPERATIVE A EISA K NONE O OTHER UK UNKNOWN 1 SW 07 950VJ 47564 PASSENGER EMERGENCY ESCAPE SLIDE INOPERATIVE AT FORWARD GALLEY. INSTALLED EMERGENCY SLIDE PER MM 25-62-0. (M) 2 L 7 2 4F A6WE 1999040900561 19990409 00561 NM 1999 4 9 EISA99015 1 19990120 A 3610 132712 PNEUMATIC LINE BOEING 727 727231 1384079 NM EMPENNAGE FRACTURED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 12305 19562 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT AFTER TAKEOFF. FOUND HOLE IN BRAIDED HIGH PRESSURE LINE IN THE E NGINE STRUT AREA. REMOVED AND REPLACED LINE IAW MM 36-12. LEAK AND OPS CHECK GOOD ON GROUND IAW 26-14 MM. (M) 2 L 7 3 4F A3WE 1999040900562 19990409 00562 NM 1999 4 9 EISA99031 1 19990224 A 2720 59100501 PCU BOEING 727 727223 1384074 NM RUDDER LEAKING A EISA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 6815 19490 IMMEDIATELY AFTER TAKEOFF UNCOMMANDED RUDDER INPUT LEFT AND RIGHT. SYSTEM 'A' AND 'B' RUDDER POWER OFF RUDDER INPUT STO PS. REMOVED AND REPLACED UPPER RUDDER PCU IAW MM 27-20-141. (M) 2 L 7 3 4F A3WE 1999040900563 19990409 00563 NM 1999 4 9 EISA99026 1 19990212 A 3230 BACR24E2L70 ROD BOEING 727 727231 1384079 NM CARGO DOOR LOOSE A EISA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 74318 64367 20051 SEVERE VIBRATION IN FLIGHT. RETURNED TO EDI. ON POST FLIGHT WALK AROUND FOUND REAR AFT CARGO DOOR OPEN. VISUAL INSPEC TION OF AFT CARGO DOOR REVEALED INTERNAL HANDLE AND ROD LOOSE, DOOR LOCKS CONFIRMED OPERATIONAL. RESECURED DEACTIVATION BAR IAW MM 52-35-51. NO FURTHER DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 1999040900564 19990409 00564 NM 1999 4 9 EISA99017 1 19990126 A 2133 10328051 OUTFLOW VALVES BOEING 727 727231 1384079 NM FUSELAGE DIRTY A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 74318 20051 CABIN PRESSURIZATION CONTINUES TO CLIMB AFTER LEVEL OFF AT 100-200 FEET PER MINUTE. MANUAL AND AUTO MODES FAIL TO CONTR OL CABIN RISE. AIR TURN BACK TO BGY. CLEANED OUTFLOW VALVES, WIPED DOWN SEALS. GRUOND TEST OK FOR SERVICE IAW MM 21-3 0. (M) 2 L 7 3 4F A3WE 1999040900565 19990409 00565 EU 1999 4 9 C2XA99BT008 1 19990311 A 2611 FR3222 SMOKE DETECTOR AEROSP ATR42 ATR42320 8680930 EU CARGO BAY MALFUNCTIONED A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 09 14825 132 170 AFT SMOKE ILLUMINATED ON TAXI. REMOVED AND REPLACED AFT SMOKE DETECTION. OPS CHECK GOOD IAW ATR JIC 26-15-00. (M) 2 H 7 2 4T RT A53EU 1999040900566 19990409 00566 SO 1999 4 9 C2XA99IA180 1 19990302 A 3350 3071BPE BULB EMB 120 EMB120RT SO ROW 9A FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12703 120084 EFD - DURING LINE CHECK INSPECTION, THE AISEL PATH EMERGENCY LIGHT AT SEAT 9A WAS FOUND TO BE INOPERATIVE. MAINTENANCE P LACED THE LIGHT ON MEL 33-50-1C CONTROL NUMBER 174665, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB AND CLEARED THE MEL. THE AIRCRAFT WAS THE N APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900567 19990409 00567 EU 1999 4 9 C2XA99IA182 1 19990306 A 3260 141FL01D3 SWITCH AEROSP ATR42 ATR42500 EU RT MLG FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR UNLOCK LIGHT WAS INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999040900568 19990409 00568 NM 1999 4 9 USAA039908 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 630-645 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE LAP SEAM 4R, STATION 630 THORUGH 645 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED R EPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M) 2 L 7 3 4F A3WE 1999040900569 19990409 00569 NM 1999 4 9 USAA039907 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 560-580 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE LAP SEAM 4R, STATION 560 THROUGH 580 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED R EPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M) 2 L 7 3 4F A3WE 1999040900570 19990409 00570 NM 1999 4 9 USAA039906 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 700-720 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE LAP SEAM 4R, STATION 700 THROUGH 720 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED R EPAIR IAW 727 SRM 53-30-3 FIGURE 15A. (M) 2 L 7 3 4F A3WE 1999040900571 19990409 00571 NM 1999 4 9 USAA039905 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 725-730 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE LAP SEAM 4R, STATION 725C THROUGH 730C HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M) 2 L 7 3 4F A3WE 1999040900572 19990409 00572 NM 1999 4 9 USAA039904 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720-725 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE LAP SEAM 4R, STATION 720B THROUGH 725B HAS CRACK INDICATIONS FOUND DURING CURRENT INSPECTION. ACCOMPLISHED REPA IR IAW 727 SRM 53-30-3 FIGURE 5. (M) 2 L 7 3 4F A3WE 1999040900573 19990409 00573 WP 1999 4 9 USAA990190 1 19990305 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1155/1688 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913VJ 72599 45846 PIT - DURING MAINTENANCE WALK AROUND, FOUND 3 INCH CRACK AND 9 INCH VERTICAL CRACK ON FUSELAGE SKIN BETWEEN STATION 1155 .335 AND STATION 1168.895 LEFT SIDE. INSTALLED EXTERNAL DOUBLER, CUTOUT DAMAGE PER SRM 53-04 FIG 12B CLASS II REPAIR. (M ) 2 L 7 2 4F A6WE 1999040900574 19990409 00574 WP 1999 4 9 USAA990191 1 19990306 A 5320 59174631 JAMB DOUG DC9 DC931 3022065 WP BS 53.625 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 63713 47593 PIT - DURING RON VISIT, FOUND 6 INCH CRACK AT STATION Z53.625 DOOR JAMB, AFT PAX LEFT SIDE. INSTALLED REPAIR ANGLE PER E A 51672. (M) 2 L 7 2 4F A6WE 1999040900575 19990409 00575 WP 1999 4 9 USAA990195 1 19990305 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP CABIN CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FUOND 1.25 INCH CRACK IN INTERCOSTAL BETWEEN CABIN FLOORBEAMS NR 965-980, C/L OF A/C UPPER FLANG E. INSTALLED DOUBLER MANUFACTURED FROM 7075T6 .032 INCH PER SRM 53-01, FIG 2. (M) 2 L 7 2 4F A6WE 1999040900576 19990409 00576 WP 1999 4 9 USAA990196 1 19990305 A 5320 CUSP DOUG DC9 DC931 3022065 WP BS 598 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND CRACKS 1.75 AND 3.5 INCH LEFT SIDE OF CABIN STATION 598 CUSP MEMBRANE. CUT OUT AND INSTALL ED NEW SECTION PER EA 51628. (M) 2 L 7 2 4F A6WE 1999040900577 19990409 00577 WP 1999 4 9 USAA990197 1 19990305 A 5311 FRAME DOUG DC9 DC931 3022065 WP FRAME 1019 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND CHAF .372 INCH BY .196 INCH WIDE BY .029 INCH DEEP AT FRAME 1019 BELOW LONGERON 13R. CUT O UT DAMAGE AREA OF FRAME AND SPLICED IN A NEW SECTION OF FRAME AND SPLICED IN A NEW SECTION OF FRAME PER SRM 53-03 FIG 4. (M0 2 L 7 2 4F A6WE 1999040900578 19990409 00578 WP 1999 4 9 USAA990198 1 19990305 A 5320 9911840200 BRACKET DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK ON TAIL INTERIOR ON VERTICAL ATTACH BRACKET FOR 'Y' DUT STATION 1087 BELOW 5R . REPLACED DEFECTIVE PART WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F A6WE 1999040900579 19990409 00579 WP 1999 4 9 USAA990201 1 19990305 A 5320 JAMB DOUG DC9 DC931 3022065 WP CARGO DOORWAY DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND SMALL HOLE IN AFT CARGO DOOR JAMB WEB JUST ABOVE 29 RIGHT. REMOVED DAMAGED SECTION OF WEB, MANUFACTURED NEW WEB PIECE FROM C/C 109-5712. MADE SPLICES FROM 7075-T6 .050 INCH AND INSTALLED PER EA NR 51599. (M) 2 L 7 2 4F A6WE 1999040900580 19990409 00580 WP 1999 4 9 USAA990200 1 19990305 A 5311 FRAME DOUG DC9 DC931 3022065 WP FRAME 1059 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND .5 INCH LENGTH BY .21875 INCH WIDE BY .019 INCH DEEP CHAFE IN FRAME NR 1059 LONGERON 15L. INSTALLED DOUBLER PER SRM 53-01, FIG 2 SHEET 4 AND EA 51616. (M) 2 L 7 2 4F A6WE 1999040900582 19990409 00582 WP 1999 4 9 USAAD99043 1 19990310 A 5241 MECHANISM DOUG DC9 DC982 3022082 WP L2 DOOR NOT LATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 825US 49237 FLL-PHL FLT 1430 - AFTER TAKEOFF THE CABIN PRESSURE FLOW LIGHT ILLUMINATED AND TEH CABIN WOULD NOT PRESSURIZE IN AUTO OR MANUAL. THE AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED THE L2 DOR AND ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1999040900583 19990409 00583 WP 1999 4 9 USAAD99040 1 19990309 A 2130 1036361 VALVE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 804US 48052 RSW-PIT FLT 352 - WHILE CRUISING AT 33,000 FT, THE PRESSURIZATION FLOW LIGHT ILLUMINATED WITH THE CABIN CLIMBING A 1500 FPM. THE CABIN ALTITUDE HORN SOUNDED AND THE CABIN PRESSURE COULD NOT BE CONTROLLED IN STANDBY OR MANUAL PRESSURIZATION MODES. THE AIRCRAFT MADE AN EMERGENCY DESCENT TO 10000 FT, DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE RE PLACED THE AFT CABIN SAFETY VALVE AND ALSO AS A PRECAUTION REPLACED THE NR 1 CABIN PRESSURE CONTROLLER. (M) 2 L 7 2 4F A6WE 1999040900584 19990409 00584 WP 1999 4 9 USAAD99044 1 19990310 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP LANDING GEAR ICED UP A USAA A UNSCHED LANDING L NO TEST CL CLIMB 1 EA 19 970VJ 47050 BUF-LGA - FLT 1731 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THE LEFT GEAR INDICATED UNSAFE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEARS COVERED WITH ICE SLUSH. ALL THREE LANDING GE AR WERE DEICED AND OPERATION NOW CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1999040900585 19990409 00585 NM 1999 4 9 USAA039913 1 19990317 A 3350 38931002 BATTERY BOEING 727 727225 1384077 NM AFT AIRSTAIR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 922TS 20415 FLT 6530 - DCA-LGA - AFT AIRSTAIR EXIT LIGHT INOP. REPLACED BATTERIES, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999040900586 19990409 00586 NM 1999 4 9 USAA039912 1 19990317 A 3350 900542 POWER SUPPLY BOEING 727 727227 1384078 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927TS R3489 20837 FLT 6460 - DCA-LGA - EMERGENCY LIGHT OVER AFT FLIGHT ATTENDANT JUMPSEAT NOT FUNCTIONING PROPERLY. REPLACED EMERGENCY LIG HT POWER SUPPLY AND BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999040900587 19990409 00587 NM 1999 4 9 USAA039903 1 19990315 A 3350 900835A BATTERY BOEING 727 727227 1384078 NM ROW 18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 17447 21244 FLT 6181 - BOS-LGA - EXIT LIGHT ON CEILING AT ROW 18 INOPERATIVE. REPLACED BATTERY, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999040900588 19990409 00588 WP 1999 4 9 USAA990222 1 19990305 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 965 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND RIGHT LAV CENTER FLOOR SUPPORT CORRODED AND CRACKED .75 INCH AT STATION 965. CORROSION LE VEL 1, CORROSION TASK NR C58-5330. CLEANED CORROSION, TREATED AND PRIMED PER SRM. MANUFACTURED NEW FLOOR SUPPORT TAB F ROM 7075-T6.040 PER SRM 51-10-03. (M) 2 L 7 2 4F A6WE 1999040900589 19990409 00589 WP 1999 4 9 USAA990194 1 19990305 A 5320 STRAP DOUG DC9 DC931 3022065 WP BS 897-925 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND CORROSION ON CARGO TIE DOWN STRAP .75 INCH DIAMETER BY .008 DEEP AT LEFT SIDE BETWEEN STAT ION 897-925 ON STRAP. CORROSION LEVEL 1, CORROSION TASK NR C57-53300. SPLICED IN NEW PART MANUFACTURED SPLICE ANGLES A ND INSTALLED PER DRAWING NR 5956033, CHANGED PART DUE TO ECONOMIC REASONS. (M) 2 L 7 2 4F A6WE 1999040900590 19990409 00590 WP 1999 4 9 USAA990199 1 19990305 A 5320 CUSP DOUG DC9 DC931 3022065 WP BS 935/945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN CUSP MEMBRANE LEFT BETWEEN STATION NR 935 AND 945. FABRICATED CUSP MEMBRAN E AND INSTALLED PER EA 51628. (M) 2 L 7 2 4F A6WE 1999040900591 19990409 00591 WP 1999 4 9 USAA990193 1 19990305 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FOUND 41.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 39 EXTRUSION, LIGHT CORROSION FULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REPLACED SUPPORT WITH MODIFIED PART NR 992348429. (M) 2 L 7 2 4F A6WE 1999040900592 19990409 00592 WP 1999 4 9 USAA990192 1 19990305 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 42478 48139 PIT - DURING Q-1 CHECK, FUOND 4.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 23 EXTRUSION, LIGHT CORROSION F ULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-533013. REPLACED SUPPORT WITH MODIFIED PART NR S265247912000. (M) 2 L 7 2 4F A6WE 1999040900593 19990409 00593 CE 1999 4 9 MASA99039 1 19990310 A 3350 1317 BULB BRUCE BC10020004 CESSNA 310 310R 2074245 CE ROW 11 FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 310R0959 FLT 5819 - CVG-PHL - CREW REPORTED THE EMERGENCY CEILING FLOODLIGHT AT ROW 11 INOP. MAINTENANCE REMOVED AND REPLACED THE BULB, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 3O 3A10 1999040900594 19990409 00594 NM 1999 4 9 MASA99041 1 19990311 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM ROW 1 MALFUNCTIONED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 FLT 6370 - YUM-PHX - AFTER ARRIVAL IN PHX, THE PILOT REPORTED ROW ONE FLOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999040900595 19990409 00595 NM 1999 4 9 MASA99042 1 19990311 A 3350 SWITCH DHAV DHC8 DHC8202 2809007 NM COCKPIT OUT OF POSITION A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 FLT 6230 - PHX-MTJ - DURING PREFLIGHT WALK AROUND, THE CREW NOTICED THAT ONE FORWARD EMERGENCY LIGHT WAS INOPERATIVE. T HE DISCREPANCY WAS DEFERRED PER MEL 33-10. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE COCKPIT SW ITCH WAS RESET, OPS CHECK GOOD. NO DISCREPANCY FOUND WITH THE LIGHT. (M) 2 H 7 2 4T RT A13NM 1999040900596 19990409 00596 NM 1999 4 9 TSAA9933136 1 19990311 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 6 FLOOR EMERGENCY PATH LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999040900597 19990409 00597 NM 1999 4 9 TSAA9933139 1 19990312 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY IN POSITION NR 5 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999040900598 19990409 00598 NM 1999 4 9 TSAA9933140 1 19990312 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM LT EMER EXIT INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED LEFT OVERWING IDENTIFER ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999040900599 19990409 00599 NM 1999 4 9 TSAA9933141 1 19990312 A 3350 9221009 BATTERY PACK BOEING 737 7372T4 1384492 NM RT EMER EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED RIGHT OVERWING IDENTIFIER BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999040900600 19990409 00600 NM 1999 4 9 TSAA9933142 1 19990312 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM RT EMER EXIT INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED RIGHT OVERWING IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999040900601 19990409 00601 NM 1999 4 9 TSAA9933143 1 19990313 A 3350 1000679 LIGHT BOEING 737 737230 NM PAX DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED AFT ENTRY DOOR OVERHEAD EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECKS OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999040900602 19990409 00602 NM 1999 4 9 TSAA9933144 1 19990314 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 6 EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1999040900603 19990409 00603 NM 1999 4 9 TSAA9933145 1 19990315 A 3350 1102833 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999040900604 19990409 00604 NM 1999 4 9 TSAA9933146 1 19990315 A 3350 9221009 POWER PACK BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED RIGHT OVERWING EMERGENCY POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999040900605 19990409 00605 NM 1999 4 9 TSAA9933147 1 19990315 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED RIGHT OVERWING EXIT IDENTIFIER LIGHT ASSY DUE TO NOT SHUTTING OFF. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 1999040900606 19990409 00606 NM 1999 4 9 TSAA9933148 1 19990315 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED POSITION 1, 2, 3 AND 4 EMERGENCY FLOOR BATTERY PACKS DUE TO LOW VOLTAGE. OPS CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999040900607 19990409 00607 EA 1999 4 9 UHLA99203 1 19990201 A 3610 4672ACPW397 VALVE DHAV DHC8 DHC8311 1386006 EA LT ENGINE BROKEN A UHLA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 03 804SA 375 UHLA - FLT 220 - BUF-BDL - THE FLIGHT ATTENDANT NOTIFIED THE CREW OF SMOKE (IN THE CABIN SHORTLY AFTER TAKEOFF. THE CREW CLOSED THE BLEEDS AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 1 AIR SWITCHING VALVE BROKEN AND REPLACED AS REQUIRED. GROUND RAN AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999040900608 19990409 00608 EA 1999 4 9 VTZA99019 1 19990303 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A VTZA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 27 630BR 7255 FLT 7821 - ORD-SGF - DURING CRUISE, AIRCRAFT EXPERIENCED A FLAP FAIL MESSAGE. FLIGHT CREW CONTACTED DISPATCH AND MAINTEN ANCE CONTROL AIRCRAFT LANDED AT ROD AFTER DECLARING AN EMERGENCY DUE TO FLAP MESSAGE. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE FLAP SYSTEM AND ACCOMPLISHED AD 98-20-01 PAR 2 AND FOUND RIGHT BPSU FAILURE. MAINTENANCE REMOVED AND REPLACED RIGHT BPSU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999040900609 19990409 00609 NM 1999 4 9 P2EA99092 1 19990224 A 7120 69466652 BOLTS BOEING 737 737222 1384473 NM NR 2 ENGINE WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, NR 2 ENGINE, FORWARD MOUNT THRUST LINKS ATTACH BOLTS FOUND WITH WEAR. REPLACED ATTACH BOLTS AS PER MM 71-20-11. (M) 2 L 7 2 4F A16WE 1999040900610 19990409 00610 NM 1999 4 9 P2EA99091 1 19990301 A 7120 69374734 BOLT BOEING 737 737222 1384473 NM NR 2 ENGINE WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE NR 2 ENGINE, AFT MOUNT ATTACH BOLT, WAS FOUND WITH WEAR. NR 2 ENGINE AFT MOUNT ATTACH BOLT REP LACED IAW MM 71-21-11. (M) 2 L 7 2 4F A16WE 1999040900611 19990409 00611 NM 1999 4 9 P2EA99090 1 19990312 A 2750 65C807391 MECHANISM BOEING 737 737281 138448P NM RT TE FOREFLAP WORN A P2EA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 CE 05 219US 20414 MCI - FLT 819 - RETRACTING FLAPS FROM 5 TO 1 DEGREE OUT OF MDW, FELT HEAVY FLUTTER. GOING FROM FLAPS 1 TO 5 ON LANDING A T MCI FELT MINOR FLUTTER. LANDING AT MCI, SELECTED FLAPS 25 AND GAUGE INDICATED 15. SELECTED FLAPS 30 AND GAUGE INDICAT ED BETWEEN 25 AND 30. ON GROUND, GAUGE MATCHES SELECTED FLAP POSITION. REPLACED RIGHT INBOARD FOR FLAP AND SEQUENCE CA RRIAGES PER MM 27-51-41. OPS CHECK OK, INDICATION SYSTEM CHECKS OK. NO DISCREPANCIES NOTED DURING POST MAINTENANCE EVA LUATION FLIGHT. (M) 2 L 7 2 4F A16WE 1999040900612 19990409 00612 NM 1999 4 9 P2EA99089 1 19990224 A 7120 69766652 BOLT BOEING 737 737222 1384473 NM NR 1 ENGINE WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, ENGINE NR 1 FORWARD MOUNT THRUST LINK ATTACH BOLTS FOUND WITH WEAR. BOLTS REPLACED AS PER MM 71-20 -11. (M) 2 L 7 2 4F A16WE 1999040900613 19990409 00613 NM 1999 4 9 ORJA99103 1 19990304 A 7931 6A5082 LINE DOUG MD90 MD9030 3023690 NM LT ENGINE DAMAGED A ORJA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 11 905RA 53573 SJC - ON ARRIVAL INTO SJC, LOST OIL QUANTITY AND PRESSURE IN LEFT ENGINE. FLIGHT CREW FOLLOWED THEIR PROCEDURES IN THE QRH AND SHUT DOWN THE NR 1 ENGINE. EMERGENCY WAS DECLARED WITH ATC. FOUND DAMAGED OIL LINE. REMOVED AND REPLACED OIL PRESSURE SCAVAGE LINE. PERFORMED LEAK CHECK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999040900614 19990409 00614 1999 4 9 RAIA990301 3 19990301 A 6140 56787108012 INDICATOR AEROSP ATR42 ATR42300 8680920 EU NR 1 FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 426TE 228 FLT 7120 - STL - NR 1 NP INDICATION PEGGED ON HIGH SIDE. MAINTENANCE REPLACED NR 1 INDICATOR. (M) 2 H 7 2 4T RT A53EU 1999040900615 19990409 00615 EU 1999 4 9 RAIA990232 1 19990228 A 6120 31058993 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 556HK 3319 41073 FLT 7515 - GRR - RIGHT ENGINE APR FIRED WITH TORQUE AT 65 PERCENT. MAINTENANCE REPLACED LEFT ENGINE NTS SWITCH. (M) 2 L 7 2 4T RT A41NM 1999040900616 19990409 00616 EU 1999 4 9 RAIA990233 1 19990226 A 7712 MT938T11F55 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 570HK 41089 FLT 7663 - JFK - LEFT TTL LIGHT LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT ENGINE TORQUE RING CANNON PLUG. (M) 2 L 7 2 4T RT A41NM 1999040900617 19990409 00617 1999 4 9 RAIA990303 4 19990304 A 3418 C771076 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 340TE 33 939 FLT 7054 - STL - RIGHT STALL LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT LIFT TRANSDUCER. (M) 2 L 7 2 4T RT A56EU 1999040900618 19990409 00618 1999 4 9 RAIA990302 4 19990304 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 41039 FLT 7795 - PIT - HEADING COMPARITOR ON AHRS. MAINTENANCE REPLACED NR 1 AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999040900619 19990409 00619 EU 1999 4 9 RAIA990311 1 19990309 A 2910 1379305A157 HYDRAULIC LINE BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 424AM 865 FLT 7034 - STL - LOST ALL HYDRAULIC PRESSURE. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR RADIUS ROD HYDRAULIC LINE. (M) 2 L 7 2 4T RT A56EU 1999040900620 19990409 00620 SO 1999 4 9 RAIA990310 1 19990309 A 2932 APTE2410005000A TRANSDUCER EMB 145 EMB145 SO LT HYD SYSTEM FAILED A RAIA O OTHER N FALSE WARNING CR CRUISE 1 CE 03 804HK 920 145082 FLT 6844 - RDU - LEFT ENGINE HYDRAULIC PRESSURE INOPERATIVE. MAINTENANCE REPLACED LEFT ENGINE HYDRAULIC PRESSURE TRANSDU CER. (M) 2 L 7 2 4F RT T00011AT 1999040900621 19990409 00621 EU 1999 4 9 RAIA990308 1 19990308 A 7722 56B17A SENSOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENG INLET FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 559HK 41075 FLT 7330 - STL - IEC FAULT ON LEFT ENGINE. MAINTENANCE REPLACED INLET SENSOR ON LEFT ENGINE. (M) 2 L 7 2 4T RT A41NM 1999040900622 19990409 00622 EU 1999 4 9 RAIA990307 1 19990308 A 2910 1379305A77 HOSE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 03 340TE 939 FLT 7479 - LEX - LOST ALL HYDRAULIC PRESSURE. MAINTENANCE REPLACED RIGHT ENGINE HYDRAULIC PUMP PRESSURE HOSE. (M) 2 L 7 2 4T RT A56EU 1999040900623 19990409 00623 1999 4 9 RAIA990309 4 19990308 A 3414 39948B2236 INDICATOR BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 433AM 16588 885 FLT 7301 - DEC - CAPTAINS AIRSPEED INDICATOR STUCK AT 70 KNOTS. MAINTENANCE REPLACED CAPTAINS AIRSPEED INDICATOR. (M) 2 L 7 2 4T RT A56EU 1999040900624 19990409 00624 EU 1999 4 9 RAIA990314 1 19990301 A 5210 1371166C SKIN BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DENTED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 430AM 880 DURING SCHEDULED MAINTENANCE, FOUND A DENT IN THE PASSENGER DOOR. MAINTENANCE REPAIRED DOOR IAW EO NR J3200-52-004-1. (M ) 2 L 7 2 4T RT A56EU 1999040900625 19990409 00625 EU 1999 4 9 RAIA990316 1 19990311 A 5330 S53172101202 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 425TE 125 DURING SCHEDULED MAINTENANCE, FOUND DENT IN LEFT FORWARD FUSELAGE. MAINTENANCE REPAIRED DAMAGE IAW EO AR42-53-007-1. (M) 2 H 7 2 4T RT A53EU 1999040900626 19990409 00626 SO 1999 4 9 C2XA99IA181 1 19990304 A 3350 1013073 LENS EMB 120 EMB120RT SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING POST-FLT INSPECTION, A RED EMERGENCY AISLE PATH EMERGENCY LIGHT WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LENS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040900627 19990409 00627 NM 1999 4 9 USAASB99067 1 19990226 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 266AU 22878 TPA - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EXIT LIGHT ON THE FUSELAGE INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999040900628 19990409 00628 NM 1999 4 9 USAASB99074 1 19990314 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 269AU 22881 ALB - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CARGO COMPARTMENT, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999040900629 19990409 00629 NM 1999 4 9 USAASB99069 1 19990312 A 3350 20131ALP BATTERY PACK BOEING 737 737401 1384701 NM ROW 11 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 CLT - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN HALF THE CABIN INOPERATIVE. ALSO, FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 11, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY AT SEAT ROW 20. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040900630 19990409 00630 NM 1999 4 9 99ZZZM234 1 19990312 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM ROW 11 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 CLT - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN HALF THE CABIN INOPERATIVE. ALSO, FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 11, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY AT SEAT ROW 20. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999040900631 19990409 00631 WP 1999 4 9 TWAA9905101 1 19990405 A 5530 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT, FOUND .1875 INCH CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE, STA 1421. REMOVED AND REPLACED ATTAC H ANGLE PER SERVICE BULLETIN 53-223, AND PER MD9-AD-13. 2 L 7 2 4F A6WE 1999040900632 19990409 00632 WP 1999 4 9 TWAA9905102 1 19990402 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND STRINGER 4L CRACKED AT STA 160. SPLICED IN NEW STRINGER PER SRM 53-02, FIG 17 AND 18. 2 L 7 2 4F A6WE 1999040900633 19990409 00633 WP 1999 4 9 AT9900278 1 19990313 A 5320 991556531 STRUCTURE DOUG DC9 DC932 3022066 WP PAX DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT ENTRY DOORWAY THRESHOLD WEB, JAMB SUPPORT AND SPLICE AND LOWER CHAN NEL FRAME CORRODED. REMOVED CORROSION, FABRICATED DOOR SILL, FITTING, ANGLE, SPLICE PLATE AND CHANNEL. DRILLED, COUNTER SUNK, DEBURRED, PRIMED AND INSTALLED ALL PARTS IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 53-11-3, 53-01 FIG 1, 51-20-0 AND 51-30-0. FITTING (P/N 4924659-501N). 2 L 7 2 4F A6WE 1999040900634 19990409 00634 WP 1999 4 9 AT9900279 1 19990224 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 229 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT CUSP WEB AT BS 229 L-18 CORRODED. REMOVED CORRODED PORTION OF WEB, REMOVED SUPPORT FITTING FOR ACCESS AND FLOOR SUPPORT SECTION. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLE D NEW SECTION AND REINSTALLED PREVIOUSLY REMOVED PARTS IAW DC9 SRM 53-20-1 FIG 8, 51-10-2, 51-10-4, 51-10-3, 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1999040900635 19990409 00635 WP 1999 4 9 AT9900280 1 19990227 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA L ABORTED APPROACH O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT CENTER FLOOR PANEL CORRODED ALONG THE EDGES AND ELONGATED H OLES WITH NO EDGE DISTANCE. FABRICATED REPAIR FLOOR PANEL, LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9 SRM 51 -10-3, 53-01 FIG 1, 53-21-0 FIG 7 AND 51-10-4. 2 L 7 2 4F A6WE 1999040900636 19990409 00636 WP 1999 4 9 AT9900281 1 19990226 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-279 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN SEAT TRACK AT BS 200 TO 279 RBL 22 CORRODED. REMOVED FLOO R PANELS, FABRICATED NEW SEAT TRACK AND SPLICE, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 53-05 FIG 4 , 51-10-3, 51-30-1, 51-30-2, AND 53-20-1. 2 L 7 2 4F A6WE 1999040900637 19990409 00637 WP 1999 4 9 AT9900282 1 19990303 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT TRACK CORRODED ON THE BOTTOM SIDE. FABRICATED, LOCATED, DRI LLED, DEBURRED, COUNTERSUNK, PRIMED, TREATED, AND INSTALLED IAW DC9 SRM 53-05 FIG 4C, 51-10-3 AND 51-10-4. 2 L 7 2 4F A6WE 1999040900638 19990409 00638 WP 1999 4 9 AT9900283 1 19990221 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT COMPARTMENT LEFT HAND HAT CHANNEL ADJACENT TO THE LOWER BULKHEAD PR ESSURE CAP CORRODED AT BS 996 ON THE LOWER END. REMOVED CORROSION, REMOVED AND REPLACED HAT CHANNEL, LOCATED, DRILLED AN D INSTALLED IAW DC9 SRM 51-30-5, 51-30-7, AND 51-30-2. 2 L 7 2 4F A6WE 1999040900639 19990409 00639 WP 1999 4 9 AT9900284 1 19990313 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT BOTTOM OF FLOORBEAM WITH PREVIOUS REPAIR GOUGED, DENTED AND APPEARS TO HAVE A CRACK RUNNING TOWARDS CENTER OF BEAM AT BS 389. CUT OUT DAMAGE AREA, HFEC VERIFIED NO FURTHER CRACKS IN THE AREA. FABRICATED FILLERS STRAP, SHIM AND ANGLE, DRILLED, DEBURRED, TREATED, PRIMED IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 53-05 FIG 86, AND EO 99-1109. 2 L 7 2 4F A6WE 1999040900640 19990409 00640 WP 1999 4 9 AT9900285 1 19990219 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE G-4 FLOOR PAN SKIN CORRODED. REMOVED FLOOR PAN HAT SECTION, FABRICATED NEW SKIN, TREATED, PRIMED, INSTALLED SKIN AND REINSTALLED HAT SECTION IAW DC9 SRM 51-30-2, 51-10-3 AND 51-10-2. 2 L 7 2 4F A6WE 1999040900641 19990409 00641 WP 1999 4 9 AT9900286 1 19990225 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND AFT PIT BULKHEAD LINER SUPPORT ANGLE CORRODED AND GILLINER PA NEL MISSING. FORMED SUPPORT ANGLE, CUT, DRILLED, TRIMMED ANGLE AND GILLINER PANEL, TREATED, PRIMED AND INSTALLED ANGLE T O GILLINER PANEL IAW DC9 SRM 51-10-4, 51-10-2, 53-21-0 FIG 10, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999040900642 19990409 00642 WP 1999 4 9 AT9900287 1 19990220 A 5320 59572561 BRACKET DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO COMPARTMENT FUEL SHUT OFF BRACKET AT BS 935 CORRODED. RELIEVE D CABLE TENSION, REMOVED AND REPLACED BRACKET ASSEMBLY, RIGGED SYSTEM AND ALL OPS CHECKS GOOD IAW DC9 MM 20-18-0, 76-12- 0 PG 206, 20-16-0, AND 76-00 FIG 202. 2 L 7 2 4F A6WE 1999040900643 19990409 00643 WP 1999 4 9 AT9900288 1 19990220 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND UPPER CAP CRACKED AND CORRODED ON FLOORBEAM WEB AT BS 996 RBL 54. REMOVED P ULLEY TOWERS, REMOVED FLOOR UPPER BEAM CAP. LOCATED AND DRILLED NEW FLOORBEAM CAP, ALODINED, PRIMED, AND INSTALLED FLOO RBEAM AND REINSTALLED PULLEY TOWERS IAW DC9 SRM 53-11-3, 51-10-4, 51-10-2, 51-10-3, 51-30-1, 51-30-2 AND MM 20-16-0. 2 L 7 2 4F A6WE 1999040900644 19990409 00644 WP 1999 4 9 AT9900289 1 19990331 A 5320 49125151N FITTING DOUG DC9 DC932 3022066 WP BS 980-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON AFT PRESSURE BEHIND TIE FITTING AT BS 989 TO 996 L-28L. REMOVE D AND REPLACED FITTING IAW DC9 SRM 53-01 FIG 1, 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1999040900645 19990409 00645 WP 1999 4 9 AT9900290 1 19990220 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 237 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE GILLINER ATTACH ANGLE CRACKED AT BS 237 L-24. PERFORMED HFEC TO VERIFIE D CRACK. REMOVED CRACKED ATTACH ANGLE, WELDED REPAIR CRACK ON ANGLE IAW EA 12-5321-29-C1362 USING AMS 4951 FILLER WIRE AND INSTALLED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999040900646 19990409 00646 WP 1999 4 9 AT9900291 1 19990325 A 7110 COWLING DOUG DC9 DC932 3022066 WP BS 124 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT ON NR 2 ENGINE LOWER COWLING AT BS 124. CUT OUT DEFECTIVE AREA, FABR ICATED AND INSTALLED REPAIR IAW DC9 SRM 54-02 FIG 2 AND RES NR 99688. 2 L 7 2 4F A6WE 1999040900647 19990409 00647 WP 1999 4 9 AT9900292 1 19990226 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 157-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED ON THE UPPER SURFACE AND ON BOTTOM OF UPPER FLANGE AROUND CLIP NUTS AT BS 157 TO 218. REMOVED CORROSION, FABRICATED REPAIR ANGLE, DRILLED, DEBURRED, TREAT ED, PRIMED AND INSTALLED IAW DC9 SRM 53-10-1, 51-10-4, 51-10-2, 51-10-3 AND 51-30-1. 2 L 7 2 4F A6WE 1999040900648 19990409 00648 WP 1999 4 9 AT9900293 1 19990219 A 5510 4918114501N BRACKET DOUG DC9 DC932 3022066 WP LT HORIZ STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SIDE ROLLER BEARING FITTING CORRODED ON THE INBOARD LEFT SIDE OF THE HO RIZONTAL STABILIZER. REMOVED AND REPLACED LEFT HAND INBOARD BRACKET ON THE HORIZONTAL STABILIZER IAW DC9 MM 55-10-0. 2 L 7 2 4F A6WE 1999040900649 19990409 00649 WP 1999 4 9 AT9900294 1 19990220 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT FORWARD LOWER FLOOR PANEL BRACKET CORRODED AT BS 218 LBL 42. REMOV ED BRACKET, CUT, DRILLED, TRIM, ALODINED, PRIMED, INSTALLED NUT PLATE ON BRACKET AND INSTALLED IAW DC9 SRM 51-30-2, 53-2 1-0 FIG 2D, 51-10-3 AND 53-20-0. 2 L 7 2 4F A6WE 1999040900650 19990409 00650 WP 1999 4 9 AT9900295 1 19990218 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 69.5 & 76.5 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 813AT 47318 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND LIGHTNING STRIKES ON THE LEFT SIDE NOSE AT Y-69.550 AND RIGHT SIDE NOSE AT Y-69.550 AND Y-76.550. REMOVED E/E ACCESSORY DOOR, BULKHEAD VENT AND LIGHT BRACKET. CUT OUT LIGHTNING STRIKE AND FOUR FASTENER CRACKS. FORMED REPAIR FILLERS, DOUBLERS AND INSTALLED REPAIRS AND REINSTALLED ALL PREVIOUSLY REMOVED COMPONENT S IAW DC9 SRM 51-30-2, 51-10-3, 51-10-4, 51-30-5, 51-30-1, E0 12-5330-29-B1048 STEP 12.3, DRAWING NR SR09530239, SB 53-2 62 AND MM 52-43-1 PG 201. 2 L 7 2 4F A6WE 1999040900651 19990409 00651 WP 1999 4 9 AT9900296 1 19990401 A 3350 110049 BATTERY CHARGER DOUG DC9 DC932 3022066 WP ROW 12 DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 809AT 47322 EMERGENCY TRACK LIGHTING FROM ROW 12 THROUGH BUSINESS CLASS SECTION WILL NOT ILLUMINATE. REMOVED AND REPLACED FORWARD BA TTERY CHARGER LIGHTING, OPERATIONAL CHECK NORMAL IAW MM 33-50-00. 2 L 7 2 4F A6WE 1999040900652 19990409 00652 NM 1999 4 9 AWXA9900126 1 19990401 A 3150 TERMINAL BOEING 737 7373G7 1384595 NM GLARESHIELD LOOSE A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 154AW 23776 PILOTS DETECTED A BURNING WIRE SMELL IN THE COCKPIT, SEEMED TO DISSIPATE AFTER TAPPING LEFT MASTER CAUTION PANEL. PILOT EXECUTED AN AIR TURNBACK. WHILE INSPECTING THE CAPT'S MASTER CAUTION WIRING HARNESS, NOTICED A TERMINAL ON THE MASTER CA UTION HAD COME OFF AND TOUCHED AN ADJACENT TERMINAL. NO DAMAGE WAS NOTED, SO TERMINAL WAS RECONNECTED MASTER CAUTION, O PS CK GOOD. 2 L 7 2 4F RT A16WE 1999040900653 19990409 00653 WP 1999 4 9 UPS99829180 1 19990322 A 5347 5758872003 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 580-600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 580 TO 600 AT RBL 60, THE SEAT TRACK HAD HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED SEAT TRACK FROM STA 550 TO 650 RBL 60 IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 1999040900654 19990409 00654 WP 1999 4 9 UPS99829182 1 19990322 A 5347 57455395 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 902 AT RBL 48, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED SEAT TRACK F ROM STA 889 TO 1050 RBL 48 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999040900655 19990409 00655 WP 1999 4 9 UPS99829184 1 19990322 A 5320 47516401N FITTING DOUG DC8 DC871F 302199D WP BS 710 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 710 AT STR 18R, THE TIE FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DWG 4751640-1. 2 L 7 4 4F RT 4A25 1999040900656 19990409 00656 WP 1999 4 9 UPS99829185 1 19990324 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 260, LONGERON 35L IS CRACKED ON TOP. REPAIRED AREA BY SPLICING IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1999040900657 19990409 00657 WP 1999 4 9 UPS99829186 1 19990321 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 249 & 250 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, RT WING L/E UPPER SKIN IS CRACKED AT STA XS 249 AND 250 AT THE SPAR. STOP DRILLED CRACK AND REPAIRED IAW DC8-5720-7767. 2 L 7 4 4F RT 4A25 1999040900658 19990409 00658 WP 1999 4 9 UPS99829187 1 19990402 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 341 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, RT WING L/E SKIN HAS HEAVY CORROSION AT STA XFS 341. REPAIRED AREA IAW SRM 57-3-1. 2 L 7 4 4F RT 4A25 1999040900659 19990409 00659 WP 1999 4 9 UPS99829188 1 19990325 A 5320 3755854502 FITTING DOUG DC8 DC871F 302199D WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 1180 AT STR 27L, THE DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED F ITTING IAW DWG 3755854 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999040900660 19990409 00660 WP 1999 4 9 UPS99829189 1 19990322 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 227.335 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, LT WING L/E UPPER RIB IS CRACKED AT STA FS 227.335. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 F IG 2. 2 L 7 4 4F RT 4A25 1999040900661 19990409 00661 WP 1999 4 9 UPS99829190 1 19990322 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 431.798 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, RT WING LOWER SKIN AT STA FS 431.798, 5 INCHES FWD OF THE FRONT SPAR IS CRACKED AT 2 FASTENERS. REPA IRED AREA IAW DC8-5720-4087. 2 L 7 4 4F RT 4A25 1999040900662 19990409 00662 WP 1999 4 9 UPS99829191 1 19990324 A 5320 37502571 FITTING DOUG DC8 DC871F 302199D WP BS 1020-1040 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 1020 TO 1040 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900663 19990409 00663 WP 1999 4 9 UPS99829192 1 19990325 A 5320 37558541 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 1220 AT STR 27L, THE DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW D WG 3755854 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999040900664 19990409 00664 WP 1999 4 9 UPS99829194 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 816.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, LT WING L/E UPPER RIB IS CRACKED AT STA FS 816.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 F IG 2. 2 L 7 4 4F RT 4A25 1999040900665 19990409 00665 WP 1999 4 9 99FDEA00136 1 19990406 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP BS 1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 MAIN CARGO DECK OVER MLG WHEEL WELL AREA, FUSELAGE FRAME AT BS 1521 HAS CORROSION. ** S/D ** REMOVED 3 FLOOR PNL FOR ACCESS TO CTR WHEEL WELL. REMOVED CORROSION, NDT CK HOLES AND THICKNESS. ALODINED AND PAINTED. INSTALLED FASTENERS P ER 53-33-00. INSTALLED FLOORBOARDS IAW 53-21-08. LEAK CHECK OK. 2 L 7 3 4F RT A22WE 1999040900666 19990409 00666 NM 1999 4 9 99UAL900177 1 19990326 A 2782 S251N502 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FLAPS FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 505UA 24626 LANDED UNDER AMBER ALERT DUE TO SLAT DISAGREE EICAS MESSAGE AND SYSTEM SHUTDOWN. *S/D* LEADING EDGE SLAT ACTUATOR FAI LED CAUSING ACTUATOR TO BIND THE SLAT SYSTEM AND SUBSEQUENT SHUTDOWN. REPLACED THE POSITION NR 12 SLAT ACTUATOR AND RET URNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900667 19990409 00667 NM 1999 4 9 99UAL900178 1 19990328 A 3350 321454 BATTERY DIEHL GMBH & 321430 AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 806UA 788 CABIN EMERGENCY LIGHT TEST FAILS FROM PTP PANEL. *S/D* EPSU AND BATTERY WERE REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900668 19990409 00668 NM 1999 4 9 99UAL900179 1 19990329 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 643UA 25093 FORWARD GALLEY OVEN NR 12 GENERATED A SMALL AMOUNT OF SMOKE AND ELECTRICAL ODOR. OVEN ISOLATED AND SWITCHED OFF BY PULL ING CB09 FOR OVEN NR 12. 2 L 7 2 4F 4 F RT A1NM E24NE 1999040900669 19990409 00669 WP 1999 4 9 99UAL900180 1 19990329 A 2120 AIR DIST DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1835U 47967 STRONG SMELL REPORTED IN REAR CABIN FOR THE FIRST 10 MINUTES FOLLOWING TAKEOFF. DEBRIEF CABIN CREW FOR ADDITIONAL DETAI LS. FLIGHT ATTENDANT REPORTED APPROXIMATELY 6-8 ATTENDANTS AND PASSENGER BECAME ILL DURING FLIGHT WITH HEADACHES AND FE ELING NAUSEA. *S/D* BURNED OUT ALL PACKS. NO EVIDENCE OF APU LEAKS OR FLUID INGESTION. 2 L 7 3 4F 4 F A22WE E23EA 1999040900670 19990409 00670 NM 1999 4 9 99UAL900181 1 19990330 A 2530 GALLEY MODULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FWD GALLEY LOOSE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7282U 21560 DURING POWER UP, THE FORWARD GALLEY SHIFTED AND PUSHED UP AGAINST THE FORWARD SERVICE DOOR HANDLE. THE FORWARD DOOR WAR NING LIGHT ILLUMINATED. ABORTED TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS. MAINTENANCE SECURED UNIT. FLEET ENGINEERING W ILL FORWARD THIS ITEM TO THE APPROPRIATE CATERING VENDOR AND RECOMMEND A LATCH AND PULL TEST BE PART OF THEIR INSTALLATI ON TRAINING PROCEDURE. 2 L 7 3 4F 4 F A3WE E2EA 1999040900671 19990409 00671 NM 1999 4 9 99UAL900182 1 19990330 A 2530 GALLEY MODULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FWD GALLEY LOOSE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 7289U 21567 FORWARD GALLEY SLID OUT ON TAKEOFF AND BROKE OFF THE ASSIST HANDLE ON THE SERVICE DOOR. MAINTENANCE SECURED UNIT. FLE ET ENGINEERING WILL FORWARD THIS ITEM TO THE APPROPRIATE CATERING VENDOR AND RECOMMEND A LATCH AND PULL TEST BE PART OF THEIR INSTALLATION TRAINING PROCEDURE. 2 L 7 3 4F 4 F A3WE E2EA 1999040900672 19990409 00672 NM 1999 4 9 99UAL900183 1 19990330 A 3350 58851 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7253U 21400 EMERGENCY EXIT LIGHT AT DOOR 2 RIGHT WILL NOT GO OUT. REPLACED BATTERIES. OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999040900673 19990409 00673 NM 1999 4 9 99UAL900184 1 19990331 A 5210 MECHANISM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR 1L NOT LATCHED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 396UA 24671 ABORTED TAKEOFF AT 120 KTS DUE TO DOOR 1L WARNING LIGHT. *S/D* CHECKED OPERATION OF DOOR LIGHTS, OPERATES NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999040900674 19990409 00674 NM 1999 4 9 99UAL900185 1 19990401 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7444U 21898 OVERHEAD EMERGENCY EXIT SIGN AT AFT GALLEY LOCATION IS INOP. REPLACED BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999040900675 19990409 00675 NM 1999 4 9 99UAL900186 1 19990325 A 3040 1168172 HEATER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE DOOR 2L & 2R MALFUNCTIONED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 788UA 26942 KEROSENE SMELL REPORTED ON GROUND AND ONCE IN CRUISE AROUND DOOR 2L. FLIGHT EN ROUTE EWR-LHR AND DIVERTED TO YQX. *S/D * ACCOMPLISHED IDLE AND HIGH POWER ENGINE RUNS. INSPECTED AND SEARCHED CARGO PITS WITH AIRCRAFT PRESSURIZED AND UNPRES SURIZED, NOTHING FOUND. CHECKED FOR BOTH EXTERNAL AND INTERNAL FUEL LEAKS OF THE CENTER FUEL TANK AND APU FUEL LINE. N O EVIDENCE OF FUEL LEAK WAS FOUND. REPLACED DOOR 2L AND 2R HEATERS (P/N 116817-2) PRECAUTIONARY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999040900676 19990409 00676 WP 1999 4 9 MWEA99129 1 19990405 A 5313 591022859 LONGERON DOUG DC9 DC932 3022066 WP BS 1010 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 22L AT STATION 1010 IS CHAFED. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999040900677 19990409 00677 WP 1999 4 9 MWEA99130 1 19990328 A 5330 59114033 SKIN DOUG DC9 DC914 3022034 WP BS 87 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND CRACK THROUGH FASTENER ON NOSE SKIN AT FS 87 LEFT SIDE. MTC TRIMMED OUT CRACK, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999040900726 19990409 00726 NM 1999 4 9 SWAA990638 1 19990314 A 3397 BR2013 WIRE BOEING 737 7372T4 1384492 NM ROW 6 EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 TRACK LIGHTING WIRES EXPOSED ON EMERGENCY ESCAPE LIGHT ON FLOOR ROW 6. SECURED WIRES AND TRACK COVER PER MM. 2 L 7 2 4F A16WE 1999040900727 19990409 00727 NM 1999 4 9 SWAA990639 1 19990401 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE FELL OUT. REPACKED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900728 19990409 00728 1999 4 9 SWAA990640 4 19990401 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OUT. REPACKED SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999040900729 19990409 00729 NM 1999 4 9 SWAA990641 1 19990402 A 2560 D31354 SLIDE BOEING 737 7373L9 1384470 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 FWD GALLEY DOOR EMERGENCY ESCAPE SLIDE FELL OUT. REPACKED SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999040900730 19990409 00730 NM 1999 4 9 SWAA990642 1 19990404 A 3350 P4010021 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 FWD AND AFT EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F RT A16WE 1999040900731 19990409 00731 NM 1999 4 9 SWAA990643 1 19990404 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 1 & 2 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 EMERGENCY EXIT LIGHTS OUT ON ROWS 1 AND 2. RESECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999040900732 19990409 00732 NM 1999 4 9 SWAA990644 1 19990404 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 20 BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EMERGENCY EXIT LIGHTS AT FLOOR TRACK ROW 20 HAD BROKEN WIRES. REPAIRED WIRES PER MM. 2 L 7 2 4F RT A16WE 1999040900733 19990409 00733 NM 1999 4 9 SWAA990645 1 19990404 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 FWD ENTRY DOOR SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900734 19990409 00734 NM 1999 4 9 SWAA990646 1 19990404 A 3350 100031 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 67SW 22356 EMERGENCY EXIT LIGHT ABOVE FWD SERVICE DOOR CONTINUES TO FALL OUT. ADJUSTED LATCHES PER MM. 2 L 7 2 4F A16WE 1999040900735 19990409 00735 NM 1999 4 9 SWAA990647 1 19990405 A 3397 100031 WIRE BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REPAIRED BROKEN W IRE AND REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F A16WE 1999040900736 19990409 00736 1999 4 9 SWAA990648 4 19990405 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR PRESSURE LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999040900737 19990409 00737 NM 1999 4 9 SWAA990649 1 19990405 A 5320 6545409 WEB BOEING 737 7373H4 1384600 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED A1 CHECK, FOUND BEADED PRESSURE WEB HAVING SEVERAL CRACKS AT BS 665, RBL 40, AND LBL 32. REPAIRED WEB P ER SWA RA'S NR 1-353-2054 AND NR 1-353-2053. 2 L 7 2 4F RT A16WE 1999040900738 19990409 00738 NM 1999 4 9 SWAA990650 1 19990405 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND 5 CRACKS AT FRAMES BS 827, 867 BETWEEN STRINGERS 8L-9L AND BS 727B, 747 AND 867, BETWEEN STRINGERS 8R-9R. REPAIRED PER SRM AND ER 99-5198. 2 L 7 2 4F RT A16WE 1999040900739 19990409 00739 NM 1999 4 9 SWAA990651 1 19990405 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BS 616 WL 201 LBL 65. REPAIRED FRAME PER SRM AND ER NR 99-5197. 2 L 7 2 4F RT A16WE 1999040900740 19990409 00740 NM 1999 4 9 SWAA990652 1 19990405 A 5311 6516323 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAMES AT BS 400, 440 BETWEEN STRINGERS 8L-9L AND AT BS 380, 400, BETWEEN STRING ERS 8R-9R. REPAIRED PER SRM AND ER NR 99-5198. 2 L 7 2 4F RT A16WE 1999040900741 19990409 00741 NM 1999 4 9 SWAA990653 1 19990405 A 5320 SPLICE BOEING 737 7373H4 1384600 NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND STRINGER 4L SPLICE CRACKED AT BS 908. REPAIRED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 1999040900742 19990409 00742 NM 1999 4 9 SWAA990654 1 19990405 A 3350 079123 LENS BOEING 737 7373H4 1384600 NM ROW 11 INCORRECT A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED C2 CHECK, FOUND FLOOR EMERGENCY ESCAPE EXIT LIGHT LENS AT ROW 11 HAS INCORRECT COLOR LENS. REPLACED LEN S WITH CORRECT COLOR PER MM. 2 L 7 2 4F RT A16WE 1999040900743 19990409 00743 NM 1999 4 9 SWAA990655 1 19990405 A 3150 WARNING BOEING 737 7373H4 1384600 NM COCKPIT ACTIVATED A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 332 W 23696 ABORTED TAKEOFF, GOT A WARNING HORN, AFTER CLEARING THE RUNWAY CYCLED THE FLAPS, TRIM AND SPEEDBRAKE. ALL INDICATIONS GO OD. SECOND TAKEOFF WAS NORMAL. MX NOTED INFO AND NO OTHER OCCURRENCES REPORTED. 2 L 7 2 4F RT A16WE 1999041700001 19990417 00001 NM 1999 4 17 TWAA9905201 1 19990408 A 3230 65404676 ACTUATOR BOEING 727 727231 1384079 NM NLG DOWNLOCK CRACKED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 05 54348 21967 HAD HYDRAULIC SYSTEM FAILURE AND WAS NECESSARY TO MANUALLY EXTEND THE NOSE LANDING GEAR. FOUND THE NOSE LANDING GEAR DO WN LOCK CYLINDER SPLIT. REPLACED THE NLG DOWN LOCK ACTUATOR. CHECK-C 12-13-98 MCI. 2 L 7 3 4F A3WE 1999041700002 19990417 00002 1999 4 17 TWAA9905202 4 19990409 A 2565 100504107 SLIDE DOUG DC9 DC983 3022083 WP PASSENGER DOOR LOW PRESS A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9617R 53564 THE FWD LEFT SIDE CABIN DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE ESCAPE SLIDE. 2 L 7 2 4F RT A6WE 1999041700003 19990417 00003 NM 1999 4 17 HNAA9900042 1 19990404 A 3350 601321 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 943HA 167 LEFT AFT EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY 3351-P5. 2 H 7 2 4T RT A13NM 1999041700004 19990417 00004 WP 1999 4 17 AT9900297 1 19990402 A 3510 10100C2F MASK DOUG DC9 DC932 3022066 WP COCKPIT DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 849AT 47484 CAPTAIN'S PORTABLE OXYGEN FULL FACE MASK LENS SEPARATED FROM RUBBER. REMOVED AND REPLACED MASK IAW MM 25-00. 2 L 7 2 4F A6WE 1999041700005 19990417 00005 WP 1999 4 17 AT9900298 1 19990325 A 5320 1A451411 SUPPORT DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND FLOOR SUPPORT AT BS 996 LBL-35 CORRODED. FABRICATED AND INSTALLED REPAIR I AW DC9 SRM 53-05 FIG 20. 2 L 7 2 4F A6WE 1999041700006 19990417 00006 WP 1999 4 17 AT9900299 1 19990319 A 5320 STRAP DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LEFT HAND CEILING PANEL FORWARD PIT STRAP CORRODED AND BROKEN. FABRICA TED A REPAIR STRAP, DRILLED, COUNTERSUNK, DEBURRED, AND PRIMED IAW DC9 SRM51-10-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999041700007 19990417 00007 WP 1999 4 17 AT9900300 1 19990307 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD PIT CARGO TIE DOWN TRACK CORRODED ON BACK SIDE. REMOVED AND RE PLACED TRACK IAW DC9 SRM 53-21-0. 2 L 7 2 4F A6WE 1999041700008 19990417 00008 WP 1999 4 17 AT9900301 1 19990322 A 5320 1A453811 SUPPORT DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR SUPPORT AT BS 965 LBL-24 CORRODED. REMOVED, FABRICATED AND INSTA LLED REPAIR IAW DC9 SRM 53-05 FIG 20, AND 53-01. 2 L 7 2 4F A6WE 1999041700009 19990417 00009 WP 1999 4 17 AT9900302 1 19990406 A 5313 1A444731 LONGERON DOUG DC9 DC932 3022066 WP BS 229-370 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LONGERON 19R AT BS 229-370 CORRODED. REMOVED CORRODED LONGERON, FABRICATED REPAIR, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 53-02 FIG. 18, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999041700010 19990417 00010 NM 1999 4 17 CKSA99019 1 19990406 A 5347 BAC152015667178T SEAT TRACK BOEING 747 747269B NM BS 2110 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF C CHECK AND CPCP TASK CARDS, FOUND SEAT TRACK AT MID DECK ZONE 220, BS 2110, LBL 33 SEAT TRACK CORRODED 1X2 AREA, BEYOND LIMITS PER SRM 53-10-01. REPAIRED IAW SRM 51-10-01, 53-10-05 FIG 1A. ACCOMPLISHED AT HAECO H ONG KONG, CONTRACT NR 2FE, JOB NR SU67638, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR 915502. 2 L 7 4 4F RT A20WE 1999041700011 19990417 00011 NM 1999 4 17 CKSA99020 1 19990406 A 5347 BAC152015667178T SEAT TRACK BOEING 747 747269B NM BS 1770-1980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, JOB NR SU67638, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD . 2 L 7 4 4F RT A20WE 1999041700012 19990417 00012 NM 1999 4 17 CKSA99021 1 19990406 A 5347 BAC152015667178T SEAT TRACK BOEING 747 747269B NM BS 1836-1840 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK FLANGE CORRODED AT ZONE 220, FW D DECK UPPER, BS 1836 TO 1840, LBL 75, 1X3 AREA. BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. AC COMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, JOB NR SU67638, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD N R SU66945. 2 L 7 4 4F RT A20WE 1999041700013 19990417 00013 NM 1999 4 17 CKSA99022 1 19990406 A 5347 BAC152015667178T SEAT TRACK BOEING 747 747269B NM BS 1780-1810 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK FLANGE CORRODED AT ZONE 220, BS 1780-1810, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAEC O HONG KONG, CONTRACT NR 2FE, JOB NR SU67638, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU66960. 2 L 7 4 4F RT A20WE 1999041700014 19990417 00014 NM 1999 4 17 CKSA99023 1 19990406 A 5347 BAC152015667178T SEAT TRACK BOEING 747 747269B NM BS 1834-1837 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK FLANGE CORRODED AT ZONE 220, BS 1834-1837, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAEC O HONG KONG, CONTRACT NR 2FE, JOB NR SU67638, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU66978. 2 L 7 4 4F RT A20WE 1999041700015 19990417 00015 NM 1999 4 17 CKSA99024 1 19990406 A 5347 BAC152015667178T SEAT TRACK BOEING 747 747269B NM BS 1860-1880 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK FLANGE CORRODED AT ZONE 220, BS 1860-1880, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAEC O HONG KONG, CONTRACT NR 2FE, JOB NR SU67638, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU66986. 2 L 7 4 4F RT A20WE 1999041700016 19990417 00016 NM 1999 4 17 CKSA99025 1 19990406 A 5347 BAC152015667178T SEAT TRACK BOEING 747 747269B NM BS 1905-0920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK FLANGE AREA 1X3 CORRODED AT ZON E 220, BS 1905-1920, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHE D AT HAECO HONG KONG, CONTRACT NR 2FE, JOB NR SU67638, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU67000 . 2 L 7 4 4F RT A20WE 1999041700017 19990417 00017 NM 1999 4 17 CKSA99026 1 19990406 A 5347 7178T6511RK SEAT TRACK BOEING 747 747269B NM BS 1660-1780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED AREA 1X20 AT ZONE 220 , BS 1660-1780, RBL75. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, JOB NR 000128, CPCP TASK CARD NR C53-210-01-03, NON-ROUTINE WORK CARD NR SU68024. 2 L 7 4 4F RT A20WE 1999041700018 19990417 00018 NM 1999 4 17 CKSA99027 1 19990406 A 5347 SEAT TRACK BOEING 747 747269B NM BS 1540 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK AREA 1X3 CORRODED AT ZONE 220, BS 1540, RBL98. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAECO H ONG KONG, CONTRACT NR 2FE, JOB NR 000125, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68198. 2 L 7 4 4F RT A20WE 1999041700019 19990417 00019 NM 1999 4 17 CKSA99028 1 19990406 A 5347 SEAT TRACK BOEING 747 747269B NM BS 1640-0644 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK FLANGE CORRODED AREA 1X3 AT FWD UD CAB, ZONE 220, BS 1640-1644, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, JOB NR 000122, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68537. 2 L 7 4 4F RT A20WE 1999041700020 19990417 00020 NM 1999 4 17 CKSA99029 1 19990406 A 5347 SEAT TRACK BOEING 747 747269B NM BS 1640-1780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK FLANGE AND CROWN CORRODED AREA 1X20 AT ZONE 220, BS 1640-1780, RBL11. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 14. A CCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, JOB NR 915449, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD N R SU68545. 2 L 7 4 4F RT A20WE 1999041700021 19990417 00021 NM 1999 4 17 CKSA99030 1 19990406 A 5320 BACN10TN4K FITTING BOEING 747 747269B NM BS 1047 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SUPPORT FITTING CORRODED AREA 1X2 AT ZONE 130, BS 1047, LBL48. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-01 PG 18. ACCOMPLISHED AT HAE CO HONG KONG, CONTRACT NR 2FE, C CHECK TASK CARD NR 7CI1306, NON-ROUTINE WORK CARD NR SU55773. 2 L 7 4 4F RT A20WE 1999041700022 19990417 00022 NM 1999 4 17 CKSA99031 1 19990406 A 5230 BACN10JR3F DOUBLER BOEING 747 747269B NM CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND DOUBLER CORRODED, 2 AREAS APPROX 1X2 AT ZO NE 823, UNDER AFT CARGO DOOR SCUFF PLATE. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 51-40-01 FIG 1. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, C CHECK TASK CARD NR 7CI1222, NON-ROUTINE WORK CARD NR SU60534. 2 L 7 4 4F RT A20WE 1999041700023 19990417 00023 NM 1999 4 17 CKSA99032 1 19990406 A 5320 65B096371 DOUBLER BOEING 747 747269B NM BS 980-987 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SKIN DOUBLER CORRODED, AREA APPROX 3X3 AT ZONE 130,BS 980-987, WATER SERVICE BAY. FOUND TO BE BEYOND LIMITS IAW SRM 53-30-01. REPAIRED IAW SRM 51-10-01 PG 18. A CCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, C CHECK TASK CARD NR 7CI1006, NON-ROUTINE WORK CARD NR SU60971. 2 L 7 4 4F RT A20WE 1999041700024 19990417 00024 NM 1999 4 17 CKSA99033 1 19990406 A 5753 CHORD BOEING 747 747269B NM LT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND CHORD CORRODED, AREA 2X6 AT ZONE 578, W/S 418, WBL128.45-130, LT T/E INBD WING FLAP. FOUND TO BE BEYOND LIMITS IAW SRM 57-50-01 FIG 3. REPAIRED IAW SRM 51-40-04 . ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C57-560-10-01, NON-ROUTINE WORK CARD NR SU62332. 2 L 7 4 4F RT A20WE 1999041700025 19990417 00025 NM 1999 4 17 CKSA99034 1 19990406 A 5320 BACB30M6 WEB BOEING 747 747269B NM BS 1900-1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND VERT WEB CORRODED, AREA 2X2 AT ZONE 140, B S 1900-1920, STR R44. FOUND TO BE BEYOND LIMITS IAW SRM 51-10-01. REPLACED IAW SRM 51-10-01 PG 18. ACCOMPLISHED AT HA ECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-100-01-03, NON-ROUTINE WORK CARD NR SU64494. 2 L 7 4 4F RT A20WE 1999041700026 19990417 00026 NM 1999 4 17 CKSA99035 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 400-403 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X2 AT ZONE 220, BS 400-403, LBL11. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 4. ACCOMPLISHED AT HAEC O HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-02, NON-ROUTINE WORK CARD NR SU65236. 2 L 7 4 4F RT A20WE 1999041700027 19990417 00027 NM 1999 4 17 CKSA99036 1 19990406 A 5320 BACC30M6 DOUBLER BOEING 747 747269B NM BS 680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND DOUBLER SLIGHTLY CORRODED, AREA 1X1 AT ZON E 821, RT BS 680, RBL 54. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 51-40-02 FIG 1. ACCOMPLISHED A T HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-100-01-03, NON-ROUTINE WORK CARD NR SU65921. 2 L 7 4 4F RT A20WE 1999041700028 19990417 00028 NM 1999 4 17 CKSA99037 1 19990406 A 5320 BACB307M88 ANGLE BOEING 747 747269B NM BS 1917 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND WEB ANGLE CORRODED, AREA 1X1 AT ZONE 140, RT BS 1917, STR R44. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 51-10-01 PG 18. ACCOMPLISHED AT HAE CO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-100-01-03, NON-ROUTINE WORK CARD NR SU65954. 2 L 7 4 4F RT A20WE 1999041700029 19990417 00029 NM 1999 4 17 CKSA99038 1 19990406 A 5347 BAC152018907178T SEAT TRACK BOEING 747 747269B NM BS 2250 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X3 AT ZONE 220, BS 2250-2277, LBL10. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 51-10-01 PG 18. ACCOMPLISHED AT HA ECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-100-01-04, NON-ROUTINE WORK CARD NR SU66598. 2 L 7 4 4F RT A20WE 1999041700030 19990417 00030 NM 1999 4 17 CKSA99039 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1800-1802 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X6 AT ZONE 220, BS 1800-1802, RBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT H AECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU66762. 2 L 7 4 4F RT A20WE 1999041700031 19990417 00031 NM 1999 4 17 CKSA99040 1 19990406 A 5320 65B140581 ANGLE BOEING 747 747269B NM BS 1468 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SUPPORT ANGLE CORRODED, AREA 1X10 AT ZONE 149, BS 1468, LBL16-RBL16. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 51-10-01 PG 18. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-190-01-01, NON-ROUTINE WORK CARD NR SU54834. 2 L 7 4 4F RT A20WE 1999041700032 19990417 00032 NM 1999 4 17 CKSA99041 1 19990406 A 5320 65B140612 BRACKET BOEING 747 747269B NM BS 1290 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SUPPORT BRACKET CORRODED, AREA 1X1 AT ZONE 139, BS 1290 RBL 16. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01 FIG 1. REPAIRED IAW SRM 51-10-01 PG 18. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-190-01-01, NON-ROUTINE WORK CARD NR SU55369. 2 L 7 4 4F RT A20WE 1999041700033 19990417 00033 NM 1999 4 17 CKSA99042 1 19990406 A 5510 BAC30M6 BRACKET BOEING 747 747269B NM HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND EMPENNAGE, HORIZ STAB SCREWJACK COMPT DOOR FWD LEFT CORNER FRAME BRACKET OUTER CHORD CORRODED, AREA 1X1 AT ZONE 310, BS 2410, RBL10. FOUND TO BE BEYOND LIMITS IA W SRM 53-30-01. REPAIRED IAW SRM 51-10-01 PG 18 FIG 1. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, C CHECK TASK CARD NR 7CI1010, NON-ROUTINE WORK CARD NR SU60542. 2 L 7 4 4F RT A20WE 1999041700034 19990417 00034 NM 1999 4 17 CKSA99043 1 19990406 A 5330 SKIN BOEING 747 747269B NM BS 2400-2412 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND BELLY SKIN IN TAIL COMP EMPENNAGE CORRODED , AREA 1X2 AT ZONE 310, BS 2400-2412, STR L51-R42. FOUND TO BE BEYOND LIMITS IAW SRM 53-30-01. REPAIRED IAW SRM 51-10- 01 PG 18. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, C CHECK TASK CARD NR 7CI3118, NON-ROUTINE WORK CARD NR SU64 882. 2 L 7 4 4F RT A20WE 1999041700035 19990417 00035 NM 1999 4 17 CKSA99044 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1656-1668 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X3 AT ZONE 220, BS 1656-1668, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT H AECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68560. 2 L 7 4 4F RT A20WE 1999041700036 19990417 00036 NM 1999 4 17 CKSA99045 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1520-1566 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TIE DOWN TRACK CORRODED, AREA 1X3 AT ZONE 220, BS 1669, RBL97. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68610. 2 L 7 4 4F RT A20WE 1999041700037 19990417 00037 NM 1999 4 17 CKSA99046 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1690-1710 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X10 AT ZONE 220 , BS 1690-1710, RBL75. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68644. 2 L 7 4 4F RT A20WE 1999041700038 19990417 00038 NM 1999 4 17 CKSA99047 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1720-1778 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X30 AT ZONE 260 , BS 1720-1778, LBL98. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01 FIG A. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISH ED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68693. 2 L 7 4 4F RT A20WE 1999041700039 19990417 00039 NM 1999 4 17 CKSA99048 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1740-0778 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X20 AT ZONE 260 , BS 1740-1780, RBL11. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 14. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68743. 2 L 7 4 4F RT A20WE 1999041700040 19990417 00040 NM 1999 4 17 CKSA99049 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1750-1810 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X20 AT ZONE 260 , BS 1750-1810, RBL75. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 14. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68750. 2 L 7 4 4F RT A20WE 1999041700041 19990417 00041 NM 1999 4 17 CKSA99050 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X3 AT ZONE 260, BS 1780, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 14. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68818. 2 L 7 4 4F RT A20WE 1999041700042 19990417 00042 NM 1999 4 17 CKSA99051 1 19990406 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X2 AT ZONE 220, BS 980, LBL97. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 1A. ACCOMPLISHED AT HAECO H ONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU69501. 2 L 7 4 4F RT A20WE 1999041700043 19990417 00043 NM 1999 4 17 CKSA99052 1 19990401 A 5347 BAC15201566 SEAT TRACK BOEING 747 747269B NM BS 1760-1820 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21543 DURING ACCOMPLISHMENT OF ROUTINE C CHECK AND SCHEDULED CPCP TASK CARDS, FOUND SEAT TRACK CORRODED, AREA 1X10 AT ZONE 260 , BS 1760-1820, LBL76. FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 53-10-05 FIG 14. ACCOMPLISHED AT HAECO HONG KONG, CONTRACT NR 2FE, CPCP TASK CARD NR C53-210-01-04, NON-ROUTINE WORK CARD NR SU68784. 2 L 7 4 4F RT A20WE 1999041700044 19990417 00044 EA 1999 4 17 JBXA9900079 1 19990409 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PASSENGER DOOR ACTIVATED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 577ML 7269 FLIGHT 48, ATL TO RDU, AIR RETURN TO ATL - PAX DR LATCH WARNING CAME ON DURING CLIMB-OUT. AIRCRAFT WOULD NOT PRESSURIZE . CHECKED PSEU CODES, CHECKED DOOR OPERATION ON GROUND. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A21EA 1999041700045 19990417 00045 EA 1999 4 17 JBXA9900080 1 19990409 A 2421 O RING CNDAIR CL600 CL6002B19 EA NR 1 IDG FAILED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 577ML 7269 FLIGHT 1, RDU TO DCA - ABORTED TAKEOFF, NR 1 GENERATOR FAILED. REMOVED AND REPLACED SCANVENGE FILTER AND O-RINGS ON NR 1 IDG IAW CRJ MM 24-12-04. SERVICED IDG WITH OIL AND OPS AND LEAK CHECK GOOD, NO DEFECTS NOTED. AIRCRAFT OK FOR SERVIC E. 2 L 7 2 4F RT A21EA 1999041700046 19990417 00046 NM 1999 4 17 AWXA9900127 1 19990405 A 3040 SCREW BOEING 737 73733A 1384673 NM RT WINDSHIELD LOOSE A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 173AW 23632 AIR TURN BACK - SMOKE IN COCKPIT, ON CLIMB-OUT FROM PHX, AN ARCING SOUND AND PUFF OF SMOKE WAS NOTED ON RIGHT SIDE OF CO CKPIT. NO BREAKERS POPPED. UPON FURTHER INSPECTION NOTED ARC BURN MARK AT POWER LEAD OF F/O'S WINDSHIELD. PILOT EXECU TED AIR RETURN TO PHX PER DISPATCH AND MX CONTROL. FOUND A LOOSE SCREW ON THE F/O'S AND FWD WINDOW HEAT ELEMENT CAUSING ARCING. NO DAMAGED NOTED. TIGHTED SCREW AND FUNCTIONAL TEST PER A1B31003. 2 L 7 2 4F RT A16WE 1999041700047 19990417 00047 NM 1999 4 17 AWXA9900128 1 19990402 A 3350 900542 POWER SUPPLY BOEING 737 737112 1384412 NM L1 DOOR INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 IN MAINTENANCE, L-1 DOOR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED L-1 DOOR EMERGENCY LIGHT POWER SUPPLY, OPS CK GOOD. 2 L 7 2 4F A16WE 1999041700048 19990417 00048 NM 1999 4 17 AWXA9900129 1 19990405 A 3350 PIN BOEING 757 7572G7 1384963 NM ROW 20 SHORTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 909AW 24522 IN MAINTENANCE, SEAT EMERGENCY EXIT LIGHTS FROM ROW 19L TO OVERWING EXITS INOP, OVERWING LOWER EXIT LIGHTS DIM. REPLACE D BATTERY PACK AND POWER SUPPLY. ALSO, FOUND PIN SHORTED TO SEAT TRACK, REINSERTED PIN. EMERGENCY LIGHTS OPS CK GOOD. 2 L 7 2 4F RT A2NM 1999041700049 19990417 00049 NM 1999 4 17 CALA9900371 1 19990407 A 5523 657579979K TAB BOEING 727 727243 138408D NM LEFT ELEVATOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND LEFT ELEVATOR CONTROL TAB LOWER O/B LEADING EDGE SKIN DENTED. THE LEFT ELEVATOR CONTROL TAB WAS REMOVE D AND REPLACED IAW MM 27-30-11. 2 L 7 3 4F RT A3WE 1999041700050 19990417 00050 NM 1999 4 17 CALA9900372 1 19990407 A 5753 652497862 WEDGE BOEING 727 727243 138408D NM RT TE MID FLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND RT WING O/B MID FLAP T/E WEDGE DEBONDED. THE TRAILING WAS REMOVED AND REPLACED IAW SRM 51-30-2, PAGE 1 . 2 L 7 3 4F RT A3WE 1999041700051 19990417 00051 WP 1999 4 17 CALA9900373 1 19990407 A 5230 FRAME DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND A 3 CRACK ON AFT CARGO DOOR FRAME AT AFT CORNER. A REPAIR WAS INSTALLED IAW SRM 52-10-00, FIGURE 7. 2 L 7 3 4F A22WE 1999041700052 19990417 00052 WP 1999 4 17 CALA9900374 1 19990407 A 5730 SKIN DOUG DC10 DC1030 3023501 WP LEFT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND AN 8 INCH CRACK IN LEFT WING SKIN PANEL NR 517CT. NEW SKIN WAS INSTALLED IAW SRM 57-31-01, FIGURE 1A A ND SRM 51-31-01. 2 L 7 3 4F A22WE 1999041700053 19990417 00053 WP 1999 4 17 CALA9900375 1 19990407 A 3350 20131A BATTERY PACK DOUG DC10 DC1030 3023501 WP ROW 29-35 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTS FROM SEAT 29AB TO SEAT 35AB INOPERATIVE. REPLACED BATTERY PACK AND OP ERATION CHECKED GOOD IAW MM 33-51-00. 2 L 7 3 4F A22WE 1999041700054 19990417 00054 NM 1999 4 17 CALA9900376 1 19990409 A 5330 SKIN BOEING 757 757224 1384958 NM BS 595 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 A PERMANENT FLUSH REPAIR TO FUSELAGE SKIN AT STA 595, BETWEEN S17L AND S16L WAS INSTALLED IAW ECRA 5331-01050. THE AREA HAD PREVIOUSLY BEEN REPAIRED FOR A .375 CRACK AND HAD BEEN PLACED ON DIP. 2 L 7 2 4F RT A2NM 1999041700055 19990417 00055 NM 1999 4 17 CALA9900377 1 19990409 A 3350 10617844 POWER SUPPLY BOEING 727 727243 138408D NM LT EMER EXIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17407 21270 THE INTERIOR EMERGENCY EXIT LIGHTS FOR LEFT OVERWING DOOR WOULD NOT ILLUMINATE. THE POWER SUPPLY WAS REMOVED AND REPLAC ED. 2 L 7 3 4F RT A3WE 1999041700056 19990417 00056 WP 1999 4 17 9901369308 1 19990402 A 2781 833605 PSEU DOUG DC9 DC982 3022082 WP LE SLATS MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 311RC 32980 6 48089 DURING APPROACH INTO MSP, SLAT DISAGREEMENT LIGHT ILLUMINATED WHEN FLAP LEVER WAS MOVED FROM 11 TO 15 DEGREES. FLIGHT C REW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSOR ELECTRONIC UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999041700057 19990417 00057 WP 1999 4 17 9901379883 1 19990403 A 2933 SRL12J INDICATOR DOUG DC9 DC951 3022051 WP RT HYD SYSTEM MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CR CRUISE 1 GL 01 671MC 43403 2154 47660 LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY OCCURRED DURING CRUISE FLIGHT. CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AT DESTINATION STATION AND FLIGHT WAS CONTINUED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT HYDRAU LIC SYSTEM QUANTITY INDICATOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1999041700058 19990417 00058 WP 1999 4 17 9901389877 1 19990404 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP TAIL CONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999041700059 19990417 00059 WP 1999 4 17 9901399301 1 19990404 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 301RC 48054 COCKPIT AND FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES IN FORWARD CABIN CEILING. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999041700060 19990417 00060 WP 1999 4 17 9901409859 1 19990405 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK. OPERATIONA L CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999041700061 19990417 00061 NM 1999 4 17 UPS99229209 1 19990402 A 5754 RIB BOEING 727 72727C 138400J NM NR 3 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C, NR 3 SLAT OUTBOARD ACTUATOR RIB IS CRACKED. REMOVED 2 EA RIBS O/B ACTUATOR RIB AND NEXT ONE O/B FOR ACCESS, DRILLED NEW RIB AND INSTALLED, INSTALLED ACCESSED RIB IAW SRM 51-30-02, 51-30-05, 51-10-01. 2 L 7 3 4F A3WE 1999041700062 19990417 00062 NM 1999 4 17 UPS99229210 1 19990402 A 5751 FITTING BOEING 727 72727C 138400J NM LEFT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C LEFT WING OUTBOARD AILERON CENTER INBOARD HINGE FITTING CORRODED AILERON SIDE. REPLACED HINGE FITTIN G PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999041700063 19990417 00063 NM 1999 4 17 UPS99229211 1 19990319 A 5510 65174524 FITTING BOEING 727 72727C 138400J NM RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C, RT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED FITTING PE R SRM 51-30-02. 2 L 7 3 4F A3WE 1999041700064 19990417 00064 NM 1999 4 17 UPS99229212 1 19990319 A 5510 65174523 FITTING BOEING 727 72727C 138400J NM LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C, LEFT HORIZONTAL STAB RUB PAD BULGING FROM CORROSION ON ATTACH FITTING. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-02. 2 L 7 3 4F A3WE 1999041700065 19990417 00065 NM 1999 4 17 UPS99229213 1 19990324 A 2810 7178T651 SKIN BOEING 727 72727C 138400J NM CTR FUEL CELL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C WHILE WORKING NRC 923405, FOUND CENTER FUEL CELL UPPER SKIN CORRODED UNDER SEAL RETAINER RBL 50-65. R EPAIRED PER ER 99-5206. 2 L 7 3 4F A3WE 1999041700066 19990417 00066 NM 1999 4 17 UPS99229214 1 19990305 A 5320 LINK BOEING 727 72727C 138400J NM BS 868 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C CORROSION EMANATING FROM AROUND AFT BUSHING LBL 24 EXPANSION LINK BS 868 WL 205. REMOVED EXPANSION LI NK FROM AIRCRAFT, REMOVED CORROSION FROM AROUND BUSHING HOLES AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW EXPANSION L INK AND INSTALLED IAW SRM 51-30-05, 53-10-01, 51-30-02. 2 L 7 3 4F A3WE 1999041700067 19990417 00067 NM 1999 4 17 UPS99229215 1 19990321 A 5720 65195385 CHORD BOEING 727 72727C 138400J NM CENTER WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C, CORROSION ON WING CENTER SECTION AFT LOWER CHORD RBL 42-48 AND AFT UPPER CHORD RBL 38-42. REPLACED U PPER AND LOWER CHORD PER SRM 51-30-2 AND ER 99-5195. 2 L 7 3 4F A3WE 1999041700068 19990417 00068 NM 1999 4 17 UPS99229216 1 19990408 A 5753 651859930 CARRIAGE BOEING 727 72731C 1384011 NM NR 3 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581-04.00-03) NR 3 FLAP CARRIAGE. REMOVED AND REPLACED NR 3 FLAP CARRIAGE IAW MM 27- 57-21. 2 L 7 3 4F A3WE 1999041700069 19990417 00069 NM 1999 4 17 UPS99229217 1 19990408 A 5313 BAC14192785 STRINGER BOEING 727 72731C 1384011 NM BS 655 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CRACK IN STR 10L, BS 655, REMOVED DAMAGED SECTION OF STRINGER 10L AT BS 655. FABRICATED REPAIR PART S. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS PER SRM 51-40-4 AND 51-30-2. 2 L 7 3 4F A3WE 1999041700070 19990417 00070 NM 1999 4 17 UPS99229218 1 19990405 A 5310 STRUCTURE BOEING 727 72731C 1384011 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CRACK AROUND UPPER FASTENER IN STR 7 RT COMMON TO BS 400 FRAME. REMOVED CRACKED SECTIONS AT STRINGE R 7 RT, BS 400. FABRICATED REPAIR PARTS FOR THE STRINGER AND FRAME. ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SR M 53-10-3 AND 53-10-4. 2 L 7 3 4F A3WE 1999041700071 19990417 00071 NM 1999 4 17 UPS99229219 1 19990324 A 5330 STRINGER BOEING 727 72731C 1384011 NM BS 1094 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION ON STRINGER 3R BS 1094 .375 BY .375. REPAIRED PER SRM 53-10-3 FIG 2. 2 L 7 3 4F A3WE 1999041700072 19990417 00072 NM 1999 4 17 UPS99229220 1 19990402 A 5320 651841566 STIFFENER BOEING 727 72731C 1384011 NM BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION ON STIFFENER BS 320 RBL 15 WL 170-175. REMOVED AND REPLACED STIFFENER PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999041700073 19990417 00073 NM 1999 4 17 UPS99229221 1 19990404 A 5313 829482 STRINGER BOEING 727 72731C 1384011 NM BS 484 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:D CORROSION (C53-224-01-04-01) ON STR 7 BS 484. REMOVED CORRODED STR 7 FROM BS 480-508, FABRICATED NEW PART OF INSTALLED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999041700074 19990417 00074 NM 1999 4 17 UPS99229222 1 19990408 A 5315 BAC150529222 FLOORBEAM BOEING 727 72731C 1384011 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:S,I WHILE WORKING CARD 888501 DISCOVERED CORROSION ON FLOORBEAM BS 344 RBL 16-25 WL 208. REPAIR FLOORBE AM PER SRM 51-30-2 SRM 53-10-08. 2 L 7 3 4F A3WE 1999041700075 19990417 00075 NM 1999 4 17 UPS99229223 1 19990408 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CRACKS AROUND FASTENERS IN STR 5R COMMON TO FRAME AT BS 400. REMOVED AND REPLACED STRINGER SEGMENT FROM BS 380-440 PER SRM 53-10-3 FIGURE 3. 2 L 7 3 4F A3WE 1999041700076 19990417 00076 NM 1999 4 17 UPS99229224 1 19990402 A 5751 FITTING BOEING 727 72727C 138400J NM LEFT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 INSPECTION TYPE:C, LEFT WING OUTBOARD AILERON CENTER OUTBOARD HINGE FITTING CORROED (AILERON SIDE). REPLACED PER SRM 51 -30-2. 2 L 7 3 4F A3WE 1999041700077 19990417 00077 NM 1999 4 17 QXEA9900549 1 19990328 A 2610 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 364PH 914 520 YVR - SMOKE DETECTOR WARNING LIGHT FLASHED BRIEFLY. MAINTENANCE PLACED NR 2 SMOKE DETECTOR ON MEL 26-5/2. NR 1 DETECTO R CHECKED OK. MAINTENANCE IN GEG, REPLACED NR 2 SMOKE DETECTOR, MEL CLEARED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 1999041700078 19990417 00078 NM 1999 4 17 99FDEA00139 1 19990408 A 5315 65402732 FLOORBEAM BOEING 727 72725C 138400H NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 WHILE WORKING ON 72C201-01 DISCOVERED CORROSION ON FLOORBEAM BS 1050, RBL 20, WL 200. ** S/D ** REPAIRED FLOORBEAM P ER FEDEX EA 7-5310-43772A. 2 L 7 3 4F A3WE 1999041700079 19990417 00079 NM 1999 4 17 99FDEA00138 1 19990406 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 905 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 CRACK APPROX 10 INCHES LONG FOUND ON SEAT TRACK AT STA 905, X= 27.5 (RT) ON UPPER CARGO AREA. 2 L 7 3 4F RT A22WE 1999041700080 19990417 00080 WP 1999 4 17 ABXA9900281 1 19990405 A 3246 3774567507 WHEEL DOUG DC8 DC861 3021952 WP RT MLG BROKEN A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 841AX 45908 ON TAXI-OUT, TOWER REPORTED SMOKE COMING FROM RIGHT MAIN LANDING GEAR. NR 4 BRAKE ASSEMBLY WAS LOCKED UP. FOUND NR 4 W HEEL ASSEMBLY BROKEN. REPLACED NR 4 WHEEL AND NR 4 BRAKE ASSEMBLY IAW DC8 MM. BROKEN WHEEL ASSEMBLY WAS SENT TO ALLIED SIGNAL BRAKE DIV FOR FURTHER ANALYSIS. 2 L 7 4 4F 4A25 1999041700081 19990417 00081 EA 1999 4 17 SWIA971445 1 19990309 A 3260 PSEU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 413SW 7102 PROXIMITY SYSTEM FAULT STATUS MESSAGE. PERFORMED MANUAL EXTENSION OF LANDING GEAR. RETURNED TO SLC. REMOVED AND REPLA CED PSEU. PERFORMED SELF TEST. ALL WORK DONE IAW 32-61-01. 2 L 7 2 4F 4 F RT A21EA E15NE 1999041700082 19990417 00082 1999 4 17 SWIA971446 4 19990330 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE STALL WARNING MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 411SW 7067 STALL FAIL MESSAGE ON RIGHT AFTER TAKEOFF. RETURNED TO SLC. INSTALLED SERVICEABLE STALL WARNING COMPUTER. OPS CHECK G OOD IAW 27-34-00. 2 L 7 2 4F 4 F RT A21EA E15NE 1999041700083 19990417 00083 SO 1999 4 17 SWIA971447 1 19990331 A 3231 PIN EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG DOOR BENT A SWIA K NONE J WARNING INDICATION CR CRUISE 1 NM 07 196CA 120196 RIGHT MAIN FORWARD GEAR DOOR HAS COME UNLATCHED TWO TIMES IN LAST TWO FLIGHTS. STRAIGHTENED LOCK PIN AND FUNCTION APPEA RS NORMAL ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700084 19990417 00084 SO 1999 4 17 SWIA971448 1 19990331 A 3020 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT/RT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 579SW 120347 BOTH ENGINE INLET DEICER BOOTS FAILED IN FLIGHT. RETURNED TO SBA. INSPECTED LEFT AND RIGHT ENGINE INLET DEICE BOOTS AN D BLEED LINES. PERFORMED MONITOR TEST AND RAN AIRCRAFT FOR LEFT AND RIGHT ENGINE INLET DEICE BOOTS. OPS CHECKS GOOD ON GROUND . 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700085 19990417 00085 1999 4 17 SWIA971449 4 19990409 A 3418 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE SAS SYST FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 216SW 120285 STICK SHAKER ACTIVATED DURING CRUISE FLIGHT WITH AUTO PILOT ENGAGED. RETURNED TO LAX. CHECKED STALL PANEL, SAS COMPUTE RS, AOA VANE AND ALL CHECKED GOOD. REPLACED KD127 AIR/GROUND RELAY. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700086 19990417 00086 SO 1999 4 17 SWIA971450 1 19990409 A 3230 12043270501 RELAY EMB 120 EMB120RT SO PWA 118 PW118 NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 200CD 120200 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW MM 32-31-02. GEAR SWING CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700087 19990417 00087 SO 1999 4 17 SWIA971451 1 19990409 A 3150 WARNING EMB 120 EMB120RT SO PWA 118 PW118A NE COCKPIT ACTIVATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 268UE 120207 AURAL WARNING (AUTOPILOT) WILL NOT CANCEL IN FLIGHT. RETURNED TO SFO. SWUNG LANDING GEARS TO DUPLICATE THE PROBLEM. A URAL WARNING SYSTEM OPERATES NORMALLY. DID NOT DUPLICATE THE PROBLEM. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700088 19990417 00088 SO 1999 4 17 SWIA971452 1 19990409 A 2910 LINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT HYD SYST CHAFED A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 NORMAL HYDRAULIC OIL LEVEL ON GROUND, BUT RIGHT AFTER TAKEOFF LOW PRESSURE LIGHT CAME ON FOLLOWED BY LOW OIL LEVEL AND M AIN PUMP LOW PRESSURE LIGHTS CAME ON. TRIED TO BALANCE RIGHT SYSTEM OIL WITH LEFT BUT IT WOULD ONLY MAINTAIN FOR 30 SEC ONDS. RETURNED TO SLC. REPLACED CHAFED HYDRAULIC PRESSURE LINE FROM LEFT ENGINE DRIVEN PUMP TO HYDRAULIC PACK. OPS AN D LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700089 19990417 00089 1999 4 17 SWIA971453 4 19990409 A 3414 AIRSPEED IND EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT COCKPIT STUCK A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 214SW 120280 FIRST OFFICER'S AIRSPEED INDICATOR STUCK AT 64 KNOTS. RETURNED TO LAX. REPLACED FIRST OFFICER'S AIRSPEED INDICATOR. O PS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700090 19990417 00090 SO 1999 4 17 SWIA971454 1 19990409 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 235SW 120310 SERVICE DOOR WARNING INDICATION CAME ON JUST AFTER TAKEOFF. RETURNED TO SMF. ADJUSTED MICROSWITCH ON INBOARD FUEL SERV ICING DOOR. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700091 19990417 00091 1999 4 17 SWIA971455 4 19990409 A 3425 EHSI EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 NM 07 197SW 120186 CAPTAIN'S EHSI WILL NOT INITIALIZE THEN CORRECTED ITS SELF ON THE GROUND, BUT TWICE DISCONNECTED AUTOPILOT IN FLIGHT. W HEN NR 1 GYRO COMPUTER FLAG APPEARED NR 1 HSI LOST HEADING. RETURNED TO SLC. RERACKED NR 1 AHC85 AND REINITIALIZED REO RIENTED. PERFORMED AHRS TEST CHECK OK. 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700092 19990417 00092 WP 1999 4 17 TWAA9905301 1 19990411 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP ROW 22 FAILED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9630A 53561 THE EGRESS LIGHT AT CABIN ROW 22 WOULD NOT LIGHT AND LENS WAS BROKEN. REPLACED THE LAMP AND LENS. 2 L 7 2 4F RT A6WE 1999041700093 19990417 00093 WP 1999 4 17 CALA9900378 1 19990408 A 3230 39370335501 CYLINDER DOUG DC9 DC982 3022082 WP RT MLG LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 16804 27836 49246 THE RT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO APPROXIMATELY 10 MINUTES FROM LANDING AT EWR. ABNORMAL PR OCEDURES WERE FOLLOWED AND ALTERNATE GEAR EXTENSION WAS USED. THE LT MLG DOOR SUSTAINED DAMAGE ON LANDING. MAINTENANCE FOUND THE RT MLG BUNGEE CYLINDER LEAKING. THE RT MLG BUNGEE CYLINDER WAS REMOVED AND REPLACED AND OPERATION CHECKED GO OD IAW MM 32-32-03. THE LT MLG DOOR WAS REMOVED AND REPLACED IAW MM 32-12-01. A GEAR RETRACTION WAS PERFORMED AND OPER ATION CHECKED GOOD. IN ADDITION, THE RT ENGINE DRIVEN HYDRAULIC PUMP AND RT AUX ELECTRIC HYDRAULIC PUMP WERE REMOVED AN D REPLACED. 2 L 7 2 4F A6WE 1999041700094 19990417 00094 NM 1999 4 17 CALA9900379 1 19990410 A 5753 113N300319H SKIN BOEING 757 757224 1384958 NM LT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND LT WING OUTBOARD FLAP INBOARD UPPER PANEL GOUGED BY SPOILER FITTING BOLTS. THE FLAP UPPER PANEL WAS RE PAIRED IAW SRM 51-70-10, PAGE 10 AND ECRA 5753-01062. 2 L 7 2 4F RT A2NM 1999041700095 19990417 00095 NM 1999 4 17 CALA9900380 1 19990410 A 5753 113N300320H SKIN BOEING 757 757224 1384958 NM RT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND THE RT WING OUTBOARD FLAP INBOARD UPPER PANEL GOUGED BY SPOILER FITTING BOLTS. THE FLAP UPPER PANEL WA S REPAIRED IAW SRM 51-70-10, PAGE 10 AND ECRA 5753-01062. 2 L 7 2 4F RT A2NM 1999041700096 19990417 00096 NM 1999 4 17 CALA9900381 1 19990410 A 5730 114N21065 SKIN BOEING 757 757224 1384958 NM WS 397 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND THE LT FIXED LEADING EDGE PANEL DELAMINATED AT WS 397. THE L/E PANEL WAS REPAIRED IAW SRM 51-70-07. 2 L 7 2 4F RT A2NM 1999041700097 19990417 00097 NM 1999 4 17 CALA9900382 1 19990410 A 5330 SKIN BOEING 757 757224 1384958 NM BS 620-640 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND FUSELAGE SKIN GOUGED BETWEEN STA 620 AND 640 AT S16L AND S17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLE D IAW SRM 53-00-01, FIGURE 204. A DIP WAS ISSUED TO INSPECT BLIND RIVETS EVERY 2500 FLIGHT CYCLES AND TO REPLACE THE RE PAIR NO LATER THAN 12,00 FLIGHT CYCLES PER SRM 53-00-01, FIGURE 204. 2 L 7 2 4F RT A2NM 1999041700098 19990417 00098 NM 1999 4 17 CALA9900383 1 19990412 A 5730 114N210425 SKIN BOEING 757 757224 1384958 NM WS 590 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND LT FIXED LEADING EDGE PANEL DELAMINATED AT WS 590 BETWEEN SLATS NR 1 AND 2. THE L/E PANEL WAS REPAIRED IAW SRM 51-70-07. 2 L 7 2 4F RT A2NM 1999041700099 19990417 00099 NM 1999 4 17 CALA9900384 1 19990412 A 5753 652163492 SKIN BOEING 727 727243 138408D NM RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .3125 INCH CRACK IN RT INBOARD AFT FLAP LOWER LEADING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-02. 2 L 7 3 4F RT A3WE 1999041700100 19990417 00100 NM 1999 4 17 CALA9900385 1 19990412 A 5730 SKIN BOEING 727 727243 138408D NM RIGHT WING DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND RT WING UPPER AND LOWER SKIN DEBONDED O/B AND AFT OF APU EXHAUST AREA. THE SKIN PANEL WAS REPAIRED IAW SRM 51-30-08 PAGE 1. 2 L 7 3 4F RT A3WE 1999041700101 19990417 00101 NM 1999 4 17 CALA9900386 1 19990412 A 5753 6521630173 SKIN BOEING 727 727243 138408D NM LT TE FOREFLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND LT I/B FOREFLAP UPPER SURFACE DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-14. 2 L 7 3 4F RT A3WE 1999041700102 19990417 00102 NM 1999 4 17 CALA9900387 1 19990412 A 5753 6521631273 SKIN BOEING 727 727243 138408D NM LT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .5 INCH CRACK IN LT O/B FOREFLAP I/B END CASTING AT LEADING EDGE AND TRAILING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11. 2 L 7 3 4F RT A3WE 1999041700103 19990417 00103 WP 1999 4 17 CALA9900388 1 19990412 A 5712 RIB DOUG DC10 DC1030 3023501 WP WS 795 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 1.5 INCH CRACK RT WING LEADING EDGE DOUBLER AND SUPPORT RIB AT STA XORS 795. THE LEADING EDGE DOUBLE R AND SUPPORT RIB WERE REPAIRED IAW SRM 57-10-00, PAGE 163 AND SRM 57-31-01. 2 L 7 3 4F A22WE 1999041700104 19990417 00104 SO 1999 4 17 COMA9910059 1 19990410 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5A INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 179CA 120179 EMERGENCY EXIT SIGN AT 5A IS INOPERABLE. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999041700105 19990417 00105 EA 1999 4 17 COMA9960150 1 19990411 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA PASSENGER DOOR INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 915CA 7131 EMERGENCY FLOOR LIGHT AT CABIN DOOR IS INOPERABLE. COULD NOT DUPLICATE, SYSTEM TEST OK. 2 L 7 2 4F RT A21EA 1999041700106 19990417 00106 EA 1999 4 17 COMA9960151 1 19990408 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 987CA 7199 NLG DID NOT RETRACT. COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECK WAS NORMAL. 2 L 7 2 4F RT A21EA 1999041700107 19990417 00107 EA 1999 4 17 COMA9960152 1 19990411 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 759CA 721 7279 EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES. 2 L 7 2 4F RT A21EA 1999041700108 19990417 00108 GL 1999 4 17 UPS99829204 2 19990406 A 7230 COMPRESSOR DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL NR 2 ENGINE STALLED A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SO 01 868UP 45968 693224 INSPECTION TYPE-N/A, ON DESCENT NR 2 ENG SLIGHT VIBRATION AND COMP STALL PLUS OR MINUS 10 TO 15 PERCENT, N1 FLUCT, NO TE MP CHANGE. PUSHED THROTTLE UP TO TROUBLESHOOT AND ENG FLAMED OUT. SHUTDOWN ENG IN ACCORDANCE WITH QRH. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999041700109 19990417 00109 WP 1999 4 17 UPS99829225 1 19990320 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, LT WING LEADING EDGE O/B SLOT, O/B END HAS FASTENERS PULLING THRU SKIN. REPAIRED PER TIMCO REO NR 0 6403. 2 L 7 4 4F RT 4A25 1999041700110 19990417 00110 WP 1999 4 17 UPS99829226 1 19990321 A 5240 BEAM DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, RT AFT SERVICE DOOR INTERNAL AFT BOTTOM CORNER NR 6 HORIZ BEAM CRACKED. STOP DRILLED CRACKS, FABBED DOUBLER IAW3 DC-8 SRM 52-2-0 FIG 2, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED WITH HI-LOKS AND RIVETS IAW DC- 8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999041700111 19990417 00111 WP 1999 4 17 UPS99829227 1 19990323 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 347 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C, FWD PIT STA 347 INTERIOR OF C1 DOOR FWD TORQUE BOX FORMED ANGLE CORRODED AT L35L. REMOVED ANGLE IAW DC-8 SRM 51-1-24, OUT OF LIMITS IAW DCF-8 SRM 53-20, FABBED NEW ANGLE IAW DAC DWG 9754020, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW DC-8 51-1-20D. 2 L 7 4 4F RT 4A25 1999041700112 19990417 00112 WP 1999 4 17 UPS99829228 1 19990409 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT BATT PACK, OPS CK GOOD. (P/N 5708458-5 03), (S/N FTL070) ON, (S/N 1146) OFF. 2 L 7 4 4F RT 4A25 1999041700113 19990417 00113 WP 1999 4 17 UPS99829229 1 19990321 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1705 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C, CORROSION ON FRAME UNDERSIDE AT STA 1705 BETWEEN L20 AND L21 RT SIDE. REMOVED CORRODED IAW DC-8 SRM 51-1-8 OUT OF LIMITS, REO REC, FABBED DOUBLER ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW REO 06 410. 2 L 7 4 4F RT 4A25 1999041700114 19990417 00114 WP 1999 4 17 UPS99829230 1 19990323 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C, FWD PIT STA 340 AT L27R INTERNAL TORQUE BOX CRACKED FITTING. REMOVED ANGLE SWITCH AND STRIKER IAW DC -8 SRM 51-3-0, DRILLED FITTING IAW DC-8 SRM 51-1-20D, ALODINED AND PRIMED IAW DC08 SRM 51-1-8, INSTALLED IAW DC-8 SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1999041700115 19990417 00115 WP 1999 4 17 UPS99829231 1 19990323 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1510 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, AFT PIT LONG TIE FITTING AT STA 1510 LONG 29L HAS BLEND OUT OF LIMITS. REMOVED SPLICE FITTING, FABR ICATED REPAIR STRAP IAW REO 06413, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED STRAP AND SPLICE IAW DC-8 SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1999041700116 19990417 00116 WP 1999 4 17 UPS99829232 1 19990405 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, LT LONGERON NR 11, STA 660 CRACKED. REMOVED DAMAGE, FAB DOUBLER ANGLES AND FILTER REPAIR IAW REO-06 405. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED REPAIR IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999041700117 19990417 00117 WP 1999 4 17 UPS99829233 1 19990323 A 5312 BULKHEAD ANGLE DOUG DC8 DC873F 302199F WP BS 176 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C, MAIN CABIN AT STA 176 AND L9R CORNER OF PRESS BULK ANGLE CRACKED. REMOVED EXISTING ANGLE -24 AND DYE PENED, INSPECTED AERA TO FIND END CRACK. STOP DRILLED CRACK, FOUND PREVIOUSLY REPAIRED, REINSTALLED ANGLE. 2 L 7 4 4F RT 4A25 1999041700118 19990417 00118 WP 1999 4 17 UPS99829234 1 19990323 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, FLOOR ATTACH SUPPORT ANGLE IS CRACKED AT FS 1230 AFT OF TORQUE BOX AT LONG 36. CUT OUT DAMAGE, FABR ICATED REPAIR ANGLE, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8 AND REPAIR ANGLE IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999041700119 19990417 00119 WP 1999 4 17 UPS99829235 1 19990324 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, FITTING AT STA 1180, LONG 34R CRACKED. REMOVED CRACKED FITTING, SPLICE ANGLE FABRICATED PER SRM 53- 2-0 FIG 26. DRILLED FITTING AND SPLICE ANGLE IAW DC-8 SRM 53-2-0, FABRICATED FILLERS IAW DC-8 SRM 53-2-0, ALODINED AND PRIMED IAW DC-8 SRM 51-1- 8, INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999041700120 19990417 00120 WP 1999 4 17 UPS99829236 1 19990324 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1 Z FITTING AT STA 1180, LONG 28R-27R CORRODED. REMOVED CRACKED FITTING IAW DC-8 SRM 51-1-20D, ALODINE D AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999041700121 19990417 00121 WP 1999 4 17 UPS99829237 1 19990326 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, AFT PIT FS 1100 CORROSION UNDER LOWER SURFACE OF FRAME FLANGE AT L36. FABRICATED ANGLE DOUBLER, FIL LER AND SHIMS IAW DWG DC-8-53-0229, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED ANGLER DOUBLER, FILLER SHIMS FRAM E CAP AND GUSSETS IAW DWG DC-8 53-0229 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999041700122 19990417 00122 WP 1999 4 17 UPS99829238 1 19990326 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, AFT PIT FS 1040 CORROSION UNDER LOWER SURFACE OF FRAME FLANGE AT L36 WHERE NUT PLATE IS MISSING. F ABRICATED REPAIR PARTS IAW DC-8 DWG 53-0229, ALODINED AND PRIMED IAW DC-8 51-1-8, INSTALLED PARTS IAW DC-8 SRM 51-1-21 ( 51-1-16 AND 51- 3-0). 2 L 7 4 4F RT 4A25 1999041700123 19990417 00123 WP 1999 4 17 UPS99829239 1 19990323 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, AFT PIT FS 1120 FRAME SECTION AT L31L AND L33L CORRODED. REMOVED SHEAR TIE, FABRICATED NEW SHEAR TI E IAW DAC DWG 9758049, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW DC-8 SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 1999041700124 19990417 00124 WP 1999 4 17 UPS99829240 1 19990323 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1680-1700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C1, AFT CABIN STA 1680 TO 1700 RBL 28 INTERCOSTAL HAS A CRACK AND CORROSION ON BOTTOM SIDE. INSTALLED R EPAIRED ANGLE, STOP DRILLED CRACK, ALODINED AND PRIMED. 2 L 7 4 4F RT 4A25 1999041700125 19990417 00125 EU 1999 4 17 QXEA9900561 1 19990409 A 3350 6008905 BATTERY GRIMES FOKKER F28 F28MK4000 4990810 EU RT EMER EXIT DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 496US 11169 SEA- RIGHT HAND OVERWING EMERGENCY LIGHTS WERE DIM. REMOVED AND REPLACED FORWARD AND AFT POWER SUPPLIES, OPERATIONAL CH ECK GOOD. 2 L 7 2 4F RT A20EU 1999041700126 19990417 00126 EU 1999 4 17 QXEA9900562 1 19990411 A 3350 CONNECTOR GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 4B DISCONNECTED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 486US 11237 GEG- EVACUATION LIGHT AT SEAT 4B IS INOPERATIVE. FOUND ELECTRICAL CONNECTOR WAS DISCONNECTED. RECONNECTED THE CONNECTO R AND THE LIGHT OPERATED NORMAL. 2 L 7 2 4F RT A20EU 1999041700127 19990417 00127 NM 1999 4 17 99FDEA00140 1 19990412 A 5210 507945238 BEAM BOEING 727 727247 138408F NM PASSENGER DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 LT FWD ENTRY DOOR GATE BEAM CRACKED AT LOWER FORWARD STOP FITTING. ** S/D ** STOP DRILLED LT FWD ENTRY DOOR GATE BEA M AT LWR FWD STOP FITTING AND INSTALLED DOUBLER IAW FEDEX SR 27-52-015 STEP 1 THRU 10. 2 L 7 3 4F A3WE 1999041700128 19990417 00128 WP 1999 4 17 ABXA9900282 1 19990224 A 5330 5615614515 SKIN DOUG DOUG DC8 DC862 3021970 WP SERVICE DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND SKIN CRACKED AT RIGHT AFT CORNER OF RIGHT FORWARD SERVICE DOOR CUTOUT. REPAIRED IAW DC8 SRM 53-2- 0. 2 L 7 4 4F 4A25 1999041700129 19990417 00129 WP 1999 4 17 ABXA9900283 1 19990224 A 5330 5615373535 SKIN DOUG DOUG DC8 DC862 3021970 WP PAX DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN AT UPPER AFT CORNER OF LEFT AIRCRAFT PASSENGER DOOR CUTOUT. REPAIRED IAW D C8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999041700130 19990417 00130 WP 1999 4 17 ABXA9900284 1 19990224 A 5730 57698576 SKIN DOUG DOUG DC8 DC862 3021970 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND LOWER SURFACE OF RIGHT OUTBOARD LEADING EDGE CRACKED AT SCREW HOLES AT STATIONS FS 743, 746, 762, 765, 768, 771 AND 780. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999041700131 19990417 00131 WP 1999 4 17 ABXA9900285 1 19990309 A 5730 57695894 SKIN DOUG DOUG DC8 DC862 3021970 WP RIGHT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND LEVEL-2 CORROSION AROUND LEADING EDGE SCREW HOLE FORWARD OF INBOARD END OF OUTBOARD SLOT PANEL, RI GHT WING. REPAIRED IAW ABX REA D827-26073MR. 2 L 7 4 4F 4A25 1999041700132 19990417 00132 WP 1999 4 17 MWEA99134 1 19990407 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP EMERGENCY EXIT INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 202ME 47672 THE FORWARD ENTRANCE EMERGENCY LIGHT SWITCH IS FAULTY. MTC REMOVED AND REPLACED THE FORWARD EMERGENCY ENTRANCE LIGHT AN D BATTERIES. 2 L 7 2 4F A6WE 1999041700133 19990417 00133 WP 1999 4 17 MWEA99135 1 19990408 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 THE EMERGENCY ESCAPE SLIDE PACK FELL OFF THE GALLEY DOOR. MTC REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999041700134 19990417 00134 WP 1999 4 17 MWEA99136 1 19990408 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 500ME 45711 THE FORWARD ENTRANCE DOOR ESCAPE SLIDE FELL OFF. MTC REINSTALLED DOOR SLIDE. 2 L 7 2 4F A6WE 1999041700135 19990417 00135 NM 1999 4 17 SCNA99060 1 19990312 A 3610 CLAMP BOEING 727 727259 138408J NM NR 1 ENGINE LOOSE A SCNA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 290SC 22475 DURING CLIMBOUT, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH REDUCED POWER. ALSO, LIGHT WAS ILLUMINATED WITH BLEED AND PACKS OFF. FOUND THE 13TH STAGE PNEUMATIC VALVE CLAMP LOOSE. TIGHTENED THE CLAMP AND RA N ENGINE TO POWER. OPERATIONALLY AND LEAK CHECKS GOOD. 2 L 7 3 4F A3WE 1999041700136 19990417 00136 NM 1999 4 17 SCNA99061 1 19990314 A 2530 1430E OVEN BOEING 727 727225 1384077 NM GALLEY DIRTY A SCNA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 282SC 51 22558 SMOKE CAME OUT OF THE NR 1 OVEN IN THE FORWARD GALLEY. TURNED OFF THE OVEN AND PULLED THE CIRCUIT BREAKER. FOUND LOWER HEATING ELEMENT DIRTY. CLEANED ELEMENT AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999041700137 19990417 00137 WP 1999 4 17 SCNA99062 1 19990405 A 2150 20497511 ACM DOUG DC10 DC1015 3022118 WP NR 1 MALFUNCTIONED A SCNA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 152SY 48289 DURING CLIMBOUT, THE DUCT-AVIONIC COMPARTMENT OVERHEAT LIGHT ILLUMINATED. CABIN ALTITUDE COULD NOT BE REGULATED AND CON TINUED CLIMBING A 750 FPM. RETURNED AIRCRAFT TOMSP. ON TAXI IN SMOKE REPORED IN THE AFT CABIN. FOUND THE NR 1 AIR CYC LE MACHINE TO BE WEAK AND TEMPERATURE CONTROL VALVE INDICATION TOB EE INOPERATIVE. REMOVED AND REPLACED BOTH TEMPERATUR E CONTROL VALVE AND NR 1 AIR CYCLE MACHINE. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1999041700138 19990417 00138 NM 1999 4 17 SWAA990656 1 19990407 A 2560 BACB30LK34 SCREW BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 AFT ENTRY DOOR AFT GIRT BAR RETAINING FLOOR MOUNT LOOSE. REPLACED AND SECURED WITH NEW HARDWARE (ORIGINAL SCREWS TOO SH ORT). 2 L 7 2 4F RT A16WE 1999041700139 19990417 00139 NM 1999 4 17 SWAA990657 1 19990407 A 2910 MS21902 FITTING BOEING 737 7373H4 1384600 NM NR 1 ENGINE LOOSE A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 359SW 26596 AIR TURNBACK DUE TO LOSS OF SYSTEM A ENGINE PUMP AND SYSTEM FLUID UPON GEAR RETRACTION AFTER TAKEOFF. USED ALTERNATE GE AR EXTENTION TO LAND. FOUND NR 1 ENG HYD RETURN LINE FITTING LOOSE. REMOVED AND REPLACED FITTING AND O RING ASSY. INS PECTED RETURN FILTER FOR CONTAMINATION, ALL LEAK AND OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999041700140 19990417 00140 1999 4 17 SWAA990658 4 19990407 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 652SW 27722 LEFT AFT ENTRY DOOR EMERGENCY EVACUATION SLIDE, BOTTLE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999041700141 19990417 00141 NM 1999 4 17 SWAA990659 1 19990406 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 1 BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 396SW 27690 FLOOR TRACK LIGHTING COVER MISSING AT ROW 1. ALSO, WIRES EXPOSED AND BROKEN. REPAIRED WIRES AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999041700142 19990417 00142 NM 1999 4 17 SWAA990660 1 19990406 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND 11 CRACKS AT BS 178 BULKHEAD BETWEEN LBL 17.5-RBL 17.5. REPAIRED BULKHEAD PER SWA RA NR 1-353-2055. 2 L 7 2 4F RT A16WE 1999041700143 19990417 00143 NM 1999 4 17 SWAA990661 1 19990406 A 5311 6516323 FRAME BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BS 360, STRINGER 15R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999041700144 19990417 00144 NM 1999 4 17 SWAA990662 1 19990407 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF COVER A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 AFT GALLEY DOOR EVACUATION SLIDE COMING OUT OF COVER. REPACKED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999041700145 19990417 00145 NM 1999 4 17 SWAA990663 1 19990407 A 5230 BAC1505 CHORD BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR T-CHORD CRACKED AT FWD LOWER CORNER. REMOVED AND REPLACED DOOR ASSY P ER MM AND SWA RA NR 1-352-0325. 2 L 7 2 4F A16WE 1999041700146 19990417 00146 NM 1999 4 17 SWAA990664 1 19990407 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND 4 CRACKS AT BS 178 BULKHEAD BETWEEN LBL12.5-RBL 9.5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999041700147 19990417 00147 NM 1999 4 17 SWAA990665 1 19990407 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 616, WL 202. REPAIRED FRAME PER ER NO NR 99-0270. 2 L 7 2 4F RT A16WE 1999041700148 19990417 00148 NM 1999 4 17 SWAA990666 1 19990407 A 5711 6545321 SPAR BOEING 737 7373H4 1384600 NM LEFT WING REAR CRACK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND THRU EDDY CURRENT INSPECTION, LT WING REAR SPAR CRACKED AT FASTENER HOLE (APPROX FROM WS 285 TO I/B). REPAIRED SPAR PER ER 99-0263. 2 L 7 2 4F RT A16WE 1999041700149 19990417 00149 NM 1999 4 17 SWAA990667 1 19990407 A 5315 6546569 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986 WL 208 ON PREVIOUS REPAIR. REPAIRED BEAM PER ER 99-0269. 2 L 7 2 4F RT A16WE 1999041700150 19990417 00150 NM 1999 4 17 SWAA990668 1 19990408 A 3350 20121 BATTERY CHARGER BOEING 737 7373H4 1384600 NM ROW 3 & 5 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND EMERGENCY LIGHTING BY SEATS 3 AND 5 INOP. REMOVED AND REPLACED BATTERY CHAR GER PER MM. 2 L 7 2 4F RT A16WE 1999041700151 19990417 00151 NM 1999 4 17 SWAA990669 1 19990408 A 3350 MS1557081 BULB BOEING 737 7373H4 1384600 NM RT EMER EXIT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND EMERGENCY RT OVERWING LIGHT INOP. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999041700152 19990417 00152 WP 1999 4 17 CALA9900389 1 19990412 A 5320 SPACER DOUG DC9 DC982 3022082 WP BS 636-693 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND MAIN BAGGAGE BIN Z-ANGLE CORRODED ON REPAIR SPACER AT STA 636 TO 693. THE SPACER WAS REMOVED AND REPLA CED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1999041700153 19990417 00153 NM 1999 4 17 CALA9900390 1 19990413 A 5730 114N210811 PANEL BOEING 757 757224 1384958 NM WS 320 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND LT FIXED L/E PANEL DELAMINATED OUTBOARD OF PYLON AT WS 320. THE PANEL WAS REMOVED, REPAIRED AND REINST ALLED IAW SRM 51-70-08 AND MM 51-40-02. 2 L 7 2 4F RT A2NM 1999041700154 19990417 00154 NM 1999 4 17 CALA9900391 1 19990413 A 5730 114N210812 PANEL BOEING 757 757224 1384958 NM WS 370 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND RT FIXED L/E PANEL DELAMINATED OUTBOARD OF PYLON AT WS 370. THE PANEL WAS REMOVED, REPAIRED AND REINST ALLED IAW SRM 51-70-08 AND MM 51-40-02. 2 L 7 2 4F RT A2NM 1999041700155 19990417 00155 NM 1999 4 17 CALA9900392 1 19990413 A 5730 114N152312 PANEL BOEING 757 757224 1384958 NM LEFT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND LT WING LEADING EDGE PANEL NR 511DB DELAMINATED AT ATTACHMENT HOLES. THE PANEL WAS REMOVED, REPAIRED A ND REINSTALLED IAW SRM 51-70-04 AND MM 51-40-02. 2 L 7 2 4F RT A2NM 1999041700156 19990417 00156 NM 1999 4 17 CALA9900393 1 19990413 A 5320 CHORD BOEING 757 757224 1384958 NM BS 1147 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND A 1 INCH CRACK IN LT MLG WHEEL WELL CHORD AT STA 1147. THE CHORD WAS REPLACED IAW BOEING DRAWING 149N7 222. 2 L 7 2 4F RT A2NM 1999041700157 19990417 00157 NM 1999 4 17 CALA9900394 1 19990413 A 5730 114N19875 PANEL BOEING 757 757224 1384958 NM LEFT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND LT WING PANEL NR 551BB DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-05 A ND 57-51-01. 2 L 7 2 4F RT A2NM 1999041700158 19990417 00158 NM 1999 4 17 CALA9900395 1 19990413 A 5730 114N151910 PANEL BOEING 757 757224 1384958 NM RIGHT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND RT WING INBOARD L/E PANEL NR 611HB DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SR M 51-70-08 AND 51-41-01. 2 L 7 2 4F RT A2NM 1999041700159 19990417 00159 NM 1999 4 17 CALA9900396 1 19990413 A 5523 657279980K CONTROL TAB BOEING 727 727243 138408D NM RIGHT ELEVATOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND THE RT ELEVATOR CONTROL TAB UPPER O/B TRAILING EDGE SKIN DENTED. THE ELEVATOR TAB WAS REMOVED AND REPL ACED IAW MM 27-30-11. 2 L 7 3 4F RT A3WE 1999041700160 19990417 00160 NM 1999 4 17 CALA9900397 1 19990413 A 5753 SKIN BOEING 727 727243 138408D NM LT TE MIDFLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND LT WING I/B MIDFLAP I/B END OF TRAILING EDGE SKIN DEBONDED. THE DEBONDED AREA WAS CUT OUT, A SKIN AND DOUBLER HOT BOND REPAIR WAS PERFORMED IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1999041700161 19990417 00161 NM 1999 4 17 CALA9900398 1 19990413 A 2782 BRACKET BOEING 727 727243 138408D NM NR 5 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .125 INCH CRACK AT UPPER END OF OUTBOARD BRACKET AT RT WING LEADING EDGE WHERE NR 5 L/E FLAP ACTUATOR MOUNTS. THE FASTENERS AND SUPPORT BRACKET WERE REMOVED IAW SRM 51-20-2. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 5 1-10-1, PARAGRAPH 4 AND 51-10-2. 2 L 7 3 4F RT A3WE 1999041700162 19990417 00162 EA 1999 4 17 COMA9960153 1 19990412 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LEFT MALFUNCTIONED A COMA K NONE O OTHER CR CRUISE 1 SO 01 917CA 1434 7017 FLAPS FAIL MESSAGE. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999041700163 19990417 00163 NM 1999 4 17 QXEA9900551 1 19990401 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - CHAFE MARK ON UPPER SKIN OF LEFT-HAND INBOARD FLAP STATION YW 74.35, 1 AFT OF FLAP FRONT SPAR. REPAIRED IAW DASH 8 RD 8-57-1361. 2 H 7 2 4T RT A13NM 1999041700164 19990417 00164 NM 1999 4 17 QXEA9900552 1 19990324 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WS 171.2-261 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - LEFT-HAND WING LADDER PLATE HAS CORROSION ON UPPER SURFACE LADDER PLATE STATION YW 171.2 TO YW 261.0. REPAIRED IA W DASH-8 RD 51-20-16. 2 H 7 2 4T RT A13NM 1999041700165 19990417 00165 NM 1999 4 17 QXEA9900553 1 19990329 A 5730 SKIN DHAV DHC8 DHC8102 2809003 NM WS 279 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - LEFT-HAND WING HAS DENT ON LOWER SKIN SURFACE STATION YW 279.00. REPAIRED IAW DASH 8 RD 8-57-1359. 2 H 7 2 4T RT A13NM 1999041700166 19990417 00166 NM 1999 4 17 QXEA9900554 1 19990401 A 7110 COWL DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - NR 2 ENGINE PANEL 432AL CRACKING AROUND RIVET ON GUSSET AND CHANNEL AT COOLING DUCT ATTACH FLANGE. REPAIRED IAW C ONAIR EO 2251 AND HORIZON AIR EA 9-71-105. 2 H 7 2 4T RT A13NM 1999041700167 19990417 00167 NM 1999 4 17 QXEA9900555 1 19990401 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - NR 2 NACELLE HAS RIVETS PULLED THROUGH SKIN AT NACELLE STATION 134.68 AT LOWER LONGERON OUTBOARD SIDE. REPAIRED I AW SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999041700168 19990417 00168 NM 1999 4 17 QXEA9900556 1 19990331 A 5412 FIREWALL DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - CRACK IN NR 1 FIREWALL, INBOARD SIDE JUST ABOVE CUT OUT FOR ATTACHMENT HARDWARE OF MAIN LANDING GEAR RETRACT ACTUA TOR ATTACH FITTING. REPAIRED IAW DASH 8 RD 8-54-10147, CONAIR EO 2254 AND HORIZON AIR EA 9-54-193. 2 H 7 2 4T RT A13NM 1999041700169 19990417 00169 NM 1999 4 17 QXEA9900557 1 19990330 A 5530 SHROUD DHAV DHC8 DHC8102 2809003 NM VERT STAB DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - VERTICAL STABILIZER RIGHT-HAND TRAILING EDGE SHROUD BETWEEN RIB 8 AND RIB 9 DENTED. REPAIRED IAW DASH 8 RD 8-555- 718. 2 H 7 2 4T RT A13NM 1999041700170 19990417 00170 NM 1999 4 17 QXEA9900558 1 19990401 A 5400 HOUSING DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - NR 1 HORSE COLLAR INBOARD FORWARD LATCH HOUSING CHAFED BADLY AND CRACKED. REPAIRED IAW DASH 8 RD 8-71-154, CONAIR EA 2240 AND HORIZON AIR EA 9-71-103. 2 H 7 2 4T RT A13NM 1999041700171 19990417 00171 NM 1999 4 17 QXEA9900559 1 19990319 A 5320 STRAP DHAV DHC8 DHC8102 2809003 NM CABIN CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - CHAFE FOUND ON LEFT-HAND MID CABIN EXIT CAP STRAP AT FORWARD UPPER CORNER. REPAIRED IAW HORIZON AIR EA 9-53-77C. 2 H 7 2 4T RT A13NM 1999041700172 19990417 00172 NM 1999 4 17 QXEA9900560 1 19990330 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 148 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 YXX - FORWARD LEFT-HAND SIDE AT STATION X148.000 DENT FOUND OUT OF SRM LIMITS, CHAPTER 53-00-16, PAGE 4. REPAIRED IAW D ASH 8 RD 8-53-4107. 2 H 7 2 4T RT A13NM 1999041700173 19990417 00173 NM 1999 4 17 99FDEA00141 1 19990413 A 2910 HOSE DOUG MD11 MD11F 3023600 NM NR 7 BRAKE INOPERATIVE A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 619FE 48770 RT MLG DID NOT RETRACT. CYCLED GEAR, NO HELP. REMOVED AND REPLACED NR 7 BRAKE HOSE AND SUPPORT IN RT MLG LOWER TORQUE LINK PER 32-40-00 AND 32-45-00-5, 32-31-00-5. AC OK FOR RELEASE. 2 L 7 3 4F RT A22WE 1999041700174 19990417 00174 WP 1999 4 17 MWEA99138 1 19990411 A 2560 11331 SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 212ME 47701 THE FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF. MTC REINSTALLED FORWARD ENTRANCE DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999041700175 19990417 00175 NM 1999 4 17 MWEA99139 1 19990409 A 3350 60030451 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 701ME 49760 THE INSIDE FORWARD OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 1999041700176 19990417 00176 WP 1999 4 17 MWEA99140 1 19990409 A 5320 39161842N FITTING DOUG DC9 DC932 3022066 WP RT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE RIGHT AFT WHEEL WELL JAMB TO KEEL FITTING IS CRACKED. MTC FABRICATED, INSTALLED NEW FITTING, REMOVED AND REPLACED S HANKED OUT BOLT. 2 L 7 2 4F A6WE 1999041700177 19990417 00177 WP 1999 4 17 MWEA99141 1 19990412 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 400ME 45727 THE GALLEY DOOR SLIDE COVER FELL OFF. MTC RESECURED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999041700178 19990417 00178 WP 1999 4 17 MWEA99142 1 19990411 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 500ME 45711 THE GALLEY DOOR EVACUATION SLIDE DOOR FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1999041700179 19990417 00179 NM 1999 4 17 AALA990332 1 19990306 A 5330 SKIN BOEING 727 727223 1384074 NM BS 682-686 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 860AA 21087 FUSELAGE SKIN CORRODED OUTBOARD SIDE OF STR 28R, STA 684. CUT OUT CORRODED SKIN, INSTALLED REPAIR IAW SRM 53-30-3, FIG 1. TST: 61,081.50 HOURS. CYCLES: 38,758. (X) 2 L 7 3 4F A3WE 1999041700180 19990417 00180 NM 1999 4 17 AALA990331 1 19990306 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 689 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 860AA 21087 TUL - CORROSION INSIDE STRINGER 28R, STA 689. INSTALLED STRINGER REPAIR IAW SRM 53-10-3 FIGURE 1. TST: 61,081.50 HOU RS. CYCLES: 38,758. (X) 2 L 7 3 4F A3WE 1999041700181 19990417 00181 NM 1999 4 17 AALA990333 1 19990303 A 5210 SKIN BOEING 727 727223 1384074 NM PASSENGER DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 860AA 21087 TUL - FORWARD ENTRY DOOR LOWER HINGE CUT-OUT IS CRACKED. REPAIRED PER SB 727-53-0198 FIG 4. DOUBLER IS .063 INCH AISI 15-5PH HEAT TREATED TO 150-170 KSI CADMIUM PLATED. FASTENERS ARE BACB30KK6A AND BACB30KK8A. TST: 61,081.50 HOURS. C YCLES: 38,758. (X) 2 L 7 3 4F A3WE 1999041700182 19990417 00182 NM 1999 4 17 AALA990322 1 19990308 A 5330 SKIN BOEING 727 727223 1384074 NM BS 499-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 712AA 22468 TUL - SKIN CORROSION, STR 276 TO STR 286, STA 490 TO STA 500. INSTALLED REPAIR DOUBLER AND TRIPLER IAW ESO 11697. TST : 61,081.50 HOURS. CYCLES: 38,758. (X) 2 L 7 3 4F A3WE 1999041700183 19990417 00183 NM 1999 4 17 AALA990347 1 19990305 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 484 & 496 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 712AA 22468 TUL - CORROSION ON STR 28L AT STA 484 AND STA 496. REMOVED DAMAGED AREA AND INSTALLED NEW STRINGER SECTION AND REPAIR S PLICE PER 53-10-3 USING NEW STRINGER MATERIAL AND SPLICE MATERIAL BAC 1498-132 WITH 4 EACH .1875 INCH RIVETS EACH SIDE I N HAT CHANNEL AND 6 EACH .1875 INCH RIVETS IN EACH SIDE IN LOWER CHANNEL. TST: 47,819 HOURS. CYCLES: 25,533. (X) 2 L 7 3 4F A3WE 1999041700184 19990417 00184 NM 1999 4 17 AALA994046 1 19990316 A 5347 SEAT TRACK BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 383AN 26995 AFW - SEAT TRACK AT STA 347 LBL 22 HAD CORROSION BLEND FROM OUTBOARD. REPAIRED IAW MRB 767-1824. TST: 26,387 HOURS. C YCLES: 4,095. (X) 2 L 7 2 4F RT A1NM 1999041700185 19990417 00185 NM 1999 4 17 AALA994047 1 19990311 A 5315 141T5113 FLOORBEAM BOEING 767 767323 1385205 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 383AN 26995 AFW - FLOORBEAM AT STA 325 RBL 34 HAD CORROSION BLENDED. FLOORBEAM AT STA 325 RBL 34 HAD CORROSION BLENDED, TOP AND LOW ER SURFACE. TST: 26,387 HOURS. CYCLES: 4,095. (X) 2 L 7 2 4F RT A1NM 1999041700186 19990417 00186 NM 1999 4 17 AALA994048 1 19990318 A 5315 141T5113 FLOORBEAM BOEING 767 767323 1385205 NM BS 385 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 383AN 26995 AFW - FLOORBEAM AT STA 385 RBL 34 HAD CORROSION BLENDED TOP AND LOWER SURFACE BEYOND SRM LIMITS. BLENDED CORROSION FROM FLOORBOARD HOLES. ALODINED AND PRIMED. TST: 26,387 HOURS. CYCLES: 4,095. (X) 2 L 7 2 4F RT A1NM 1999041700187 19990417 00187 NM 1999 4 17 AALA994045 1 19990317 A 5754 114T4105 RETAINER BOEING 767 767323 1385205 NM NR 5 LE SLAT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 383AN 26995 AFW - NR 5 SLAT HAS A SMALL CRACK ON THE INBOARD EDGE AT SEAL RETAINER. INSTALLED AN EXTERNAL DOUBLER AND FILLER. INST ALLED ALL REPAIR PARTS WET WITH BMS5-95. CHAMFER EDGES, ALODINED AND PAINTED. 2 L 7 2 4F RT A1NM 1999041700188 19990417 00188 WP 1999 4 17 AALA990320 1 19990309 A 2150 INLET DOUG DC10 DC1030 3023501 WP NR 3 PACK FOD A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 137AA 47847 DFW - FLT T0005 - DURING CRUISE, FLIGHT ATTENDANTS IN AFT CABIN REPORTED SMOKE IN AFT GALLEY AREA. FLIGHT CREW TURNED O FF RECIRCULATION FANS AND SMOKE DISSIPATED. FLIGHT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE F OUND DEBRIS IN NR 3 PACK INLET. MAINTENANCE CLEARED DEBRIS FROM NR 3 PACK INLET. GROUND RAN ALL THREE ENGINES AND PAC KS WITH NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1999041700189 19990417 00189 WP 1999 4 17 AALA990429 1 19990328 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROWS 17-19 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 271AA 49293 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEAT ROWS 17 THROUGH 19 WERE INOPERATIVE. RE-SEATED EMERGENCY FLOOR PATH LIGHT WIRE CONNECTOR AT SEAT ROW 17. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999041700190 19990417 00190 WP 1999 4 17 AALA990401 1 19990317 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP RT MLG DOOR DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 242AA 49255 DFW - FLT T1911 - AFTER TAKEOFF, THE RIGHT MAIN GEAR OPEN LIGHT STAYED ILLUMINATED AFTER RAISING THE GEAR HANDLE. CREW RAN CHECK LIST PROCEDURES AND THE RIGHT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOOR SENSOR, CYCLED LANDING GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED, NORM AL OPERATION. (X) 2 L 7 2 4F A6WE 1999041700191 19990417 00191 NM 1999 4 17 AALA990407 1 19990320 A 2782 5006397R ACTUATOR BOEING 767 767323 1385205 NM NR 10 LE SLAT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 354AA 5144 24035 JFK - FLT T0354 - DURING CRUISE, LEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED. CREW ACCOMPLISHED SLAT DISAGREE ALTERNAT E PROCEDURES. FLIGHT AIR INTERRUPTED INTO LGA AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS FERRIED TO JFK FOR REP AIRS. MAINTENANCE FOUND NR 10 LEADING EDGE SLAT ACTUATOR FAULTY. REPLACED NR 10 LEADING EDGE SLAT ACTUATOR. SYSTEM OP ERATED NORMALLY WITH NO LEAKS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999041700192 19990417 00192 WP 1999 4 17 AALA990324 1 19990311 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT AIR STAIRS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 259AA 49289 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRING TO THE AFT AIR STA IRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999041700193 19990417 00193 WP 1999 4 17 AALA990406 1 19990320 A 3350 1001191 LIGHT GRIMES 2920 DOUG DC9 DC982 3022082 WP EMERGENCY EXIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 275AA 49272 DFW - DURING OVERNIGHT MAINTENANCE, EXTERIOR OVER WING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE LIGHT AS SEMBLY AT FAULT. REPLACED EXTERIOR OVER WING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 2 4F A6WE 1999041700194 19990417 00194 WP 1999 4 17 AALA990338 1 19990315 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 226AA 49176 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHT IN FORWARD CABIN INOPERATIVE. FORWARD CABIN. SYSTEM GR OUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999041700195 19990417 00195 WP 1999 4 17 AALA990402 1 19990318 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 552AA 53034 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999041700196 19990417 00196 WP 1999 4 17 AALA990316 1 19990310 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 29 DEF DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 410AA 49321 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 29 DEF WERE INOPERATIVE. REPLACED EMER GENCY FLOOR PATH LIGHT STRIP AT SEAT ROW 29 DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999041700197 19990417 00197 WP 1999 4 17 AALA990335 1 19990314 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROWS 10 AND 27 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 410AA 49321 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 10 DEF AND 27 DEF WERE INOPERATIVE. REPLACED EM ERGENCY FLOOR PATH LIGHT STRIPS AT SEAT ROWS 10 DEF AND 27 DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999041700198 19990417 00198 EU 1999 4 17 99ZZZX1484 1 19990330 A 7603 2100350003 CAMBOX GE 665038061469 SAAB SF340 340B 7860101 EU RT ENGINE WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 235AE WYG70136A 340B235 POWER AND CONDITION CAMBOX FOUND SPLINES WORN BETWEEN HMU AND CAMBOX ASSY. PROPELLER RPM RT ENGINE FOUND ABNORMAL DUE T O SEVERELY WORN CAMBOX AND HMU SPLINES. 2 L 7 2 4T RT A52EU 1999041700199 19990417 00199 EU 1999 4 17 SIMA990501 1 19990219 A 5210 SKIN SAAB SF340 340B 7860101 EU PASSENGER DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 261AE 340B261 ABI - DURING AN MBV INSPECTION, FOUND A DENT ON THE MAIN ENTRANCE DOOR. CUT OUT DAMAGED AREA, DEBURRED, AND SMOOTHED ED GES. PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A FILLER PLATE FOR THE CUT OUT AND DOUBLER PLATE .032 INCH THICK. FILLED THE HONEYCOMB CORE WITH EPOXY FILLER LY/HY 5052, INSTALLED FILLER PLATE AND APPL IED PRESSURE. CLEANED THE REPAIR AREA AND THE DOUBLER. INSTALLED DOUBLER TO SKIN WITH ADHESIVE EA 9330. APPLIED A DIS TRIBUTED PRESSURE UNTIL CURE. APPLIED SEALANT AROUND EDGES OF DOUBLER PLATE, AND REPAINTED THE REPAIR AREA. WORK DONE IAW SAAB 340 SRM 52-10-10, PAGE 210-203. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700200 19990417 00200 EU 1999 4 17 SIMA990502 1 19990219 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 261AE 340B261 ABI - DURING AN MBV INSPECTION, FOUND DENT ON THE CARGO DOOR. CUT OUT DAMAGED AREA, DEBURRED, AND SMOOTHED EDGES. PERF ORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A FILLER PLATE FOR THE CUT-OUT. FABRICATED A DOUBLER PLATE .032 INCH THICK. FILLED THE HONEYCOMB CORE WITH EPOXY FILLER LY/HY 5052, INSTALLED FILLER PLATE AND APP LIED PRESSURE. CLEANED THE REPAIR AREA AND THE DOUBLER, INSTALLED THE DOUBLER PLATE TO THE SKIN WITH ADHESIVE EA 9330. APPLIED A DISTRIBUTED PRESSURE UNTIL CURED. APPLIED SEALANT AROUND EDGES OF DOUBLER PLATE, AND REPAINTED THE REPAIRED AREA. WORK DONE IAW SAAB 340 SRM 52-10-10, PAGE 210-203. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700201 19990417 00201 EU 1999 4 17 SIMA990432 1 19990212 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 ABI - DURING AN MBV INSPECTION, FOUND A CHAFE ON RT NACELLE OUTBOARD INNER SKIN. CUT OFF AND REMOVED THE CHAFED CORNER ANGLE BETWEEN THE FIRE FLOOR AND THE CHAFED INNER WALL. CUT OFF AND REMOVED THE FORWARD SECTION OF THE CHAFED SIDE WALL . FABRICATED A NEW SIDE FROM CRES 301 1/4 HARD .025 INCH THICK. FABRICATED A REPLACEMENT ANGLE FROM CRES 301 1/4 HARD .040 INCH THICK. APPLIED SEALANT TO THE CONTACT SURFACE OF THE REPAIR PARTS, REPOSITIONED, AND INSTALLED FASTENERS WET. APPLIED FIRE SEAL DOW CORNING DC 730. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1383. AIRCRAFT OK FOR SERVICE. (X ) 2 L 7 2 4T RT A52EU 1999041700202 19990417 00202 EU 1999 4 17 SIMA990431 1 19990212 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 ABI - DURING MBV INSPECTION, FOUND SEVERAL DENTS ON THE CARGO DOOR. CUT OUT DAMAGED AREAS AND PERFORMED AN EDDY CURRENT INSPECTION OF CUT EDGES WITH NO INDICATIONS OF CRACKS. FABRICATED FILLER PLATES FOR THE CUT OUTS FROM AL 2024-T3 MATE RIAL. FABRICATED A DOUBLER PLATE FROM AL 2024-T3 MATERIAL. FILLED THE HONEYCOMB CORE WITH EPOXY FILLER LY/HY 5052, INS TALLED THE FILLER PLATES AND APPLIED PRESSURE. CLEANED THE REPAIR AREA AND DOUBLER, APPLIED ADHESIVE EA 9930 TO CONTACT SURFACE OF DOUBLER. POSITIONED DOUBLER AND APPLIED A DISTRIBUTED PRESSURE DURING CURING. RESTORED SURFACE FINISH. WO RK DONE IAW SAAB RS NR 72SDS1383 AND SAAB SRM 52-10-10. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700203 19990417 00203 EU 1999 4 17 SIMA990421 1 19990211 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 834,839,853 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 210AE 340210 ABI - ACFT FERRIED FOR REPAIR TO SKIN, STR, AND LONG SPLICE ON RT SIDE OF TAILCONE BTWN FRAMES 839 AND 853. PERFORMED C UT-OUT OF DAMAGED SKIN, STR, AND LONG SPLICE OBSERVING MIN RADII OF .04 INCH STATED IN SAAB RS 72SDS1377. PERFORMED EDD Y CURRENT INSP OF CUT-OUT AND CUT EDGES. SECTION CUT FROM STR P/N 7253900-132 TO EXTEND FROM AFT PRESS BULKHD FWD OF ST A 834 AND SECTION OF STR FROM SAME CUT AS SPLICE. LONG SPLICE FAB FROM 2024-T3, .032. REPAIR DBLR 18 INCHES BY 15.5 IN CHES, TRIPLER 10.5 INCHES BY 12.5 INCHES, BOTH FAB FROM 2024-T3 .016; ALL WORK DONE IAW SAAB RS 72SDS1377 AND SAAB 340 S RM. ACFT OK FOR SERVICE. REF: OPER CNTRL NR 99ZZZX1485 AND 99ZZZX1486. (X) 2 L 7 2 4T RT A52EU 1999041700204 19990417 00204 EU 1999 4 17 99ZZZX1485 1 19990211 A 5313 7253900132 STRINGER SAAB SF340 340B 7860101 EU BS 834,839,853 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 210AE 340210 ABI - ACFT FERRIED FOR REPAIR TO SKIN, STR, AND LONG SPLICE ON RT SIDE OF TAILCONE BTWN FRAMES 839 AND 853. PERFORMED C UT-OUT OF DAMAGED SKIN, STR, AND LONG SPLICE OBSERVING MIN RADII OF .04 INCH STATED IN SAAB RS 72SDS1377. PERFORMED EDD Y CURRENT INSP OF CUT-OUT AND CUT EDGES. SECTION CUT FROM STR P/N 7253900-132 TO EXTEND FROM AFT PRESS BULKHD FWD OF ST A 834 AND SECTION OF STR FROM SAME CUT AS SPLICE. LONG SPLICE FAB FROM 2024-T3, .032. REPAIR DBLR 18 INCHES BY 15.5 IN CHES, TRIPLER 10.5 INCHES BY 12.5 INCHES, BOTH FAB FROM 2024-T3 .016; ALL WORK DONE IAW SAAB RS 72SDS1377 AND SAAB 340 S RM. ACFT OK FOR SERVICE. REF: OPER CNTRL NR SIMA990421 AND 99ZZZX1486. 2 L 7 2 4T RT A52EU 1999041700205 19990417 00205 EU 1999 4 17 99ZZZX1486 1 19990211 A 5320 SPLICE SAAB SF340 340B 7860101 EU BS 834,839,853 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 210AE 340210 ABI - ACFT FERRIED FOR REPAIR TO SKIN, STR, AND LONG SPLICE ON RT SIDE OF TAILCONE BTWN FRAMES 839 AND 853. PERFORMED C UT-OUT OF DAMAGED SKIN, STR, AND LONG SPLICE OBSERVING MIN RADII OF .04 INCH STATED IN SAAB RS 72SDS1377. PERFORMED EDD Y CURRENT INSP OF CUT-OUT AND CUT EDGES. SECTION CUT FROM STR P/N 7253900-132 TO EXTEND FROM AFT PRESS BULKHD FWD OF ST A 834 AND SECTION OF STR FROM SAME CUT AS SPLICE. LONG SPLICE FAB FROM 2024-T3, .032. REPAIR DBLR 18 INCHES BY 15.5 IN CHES, TRIPLER 10.5 INCHES BY 12.5 INCHES, BOTH FAB FROM 2024-T3 .016; ALL WORK DONE IAW SAAB RS 72SDS1377 AND SAAB 340 S RM. ACFT OK FOR SERVICE. REF: OPER CNTRL NR SIMA990421 AND 99ZZZX1485. 2 L 7 2 4T RT A52EU 1999041700206 19990417 00206 SO 1999 4 17 SIMA990778 1 19990318 A 2611 PYD431R1 SMOKE DETECTOR EMB 145 EMB145LR SO BAGGAGE COMPT FALSE INDICATION A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 602AE 059800507 145048 XNA - FLT 3603 - DURING APROACH, THE CARGO SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. VERIFI ED EVENT AS A FALSE WARNING. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS IAW EMB-145 AMM 26-15-00. NO FURTHER DEFE CTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 1999041700207 19990417 00207 EU 1999 4 17 SIMA990786 1 19990319 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 201AE 340B201 ABI - DURING MBV INSPECTION, FOUND CHAFE ON RT AFT FUSELAGE SKIN PANEL AT HORIZONTAL STABILIZER FILLET FAIRING CONTACT A REA. BLENDED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED AN EXTERNAL DOUBL ER .025 INCH THICK. APPLIED PROTECTIVE TREATMENT TO THE DOUBLER INCLUDING POLYURETHANE TOP COAT. APPLIED SEALANT TO TH E CONTACT SURFACE OF THE DOUBLER AND ATTACHED TO AIRCRAFT. APPLIED SEALANT AROUND THE DOUBLER EDGE STEP. INSTALLED CHA FING PROTECTION PLATED IAW SAAB 340 SB 340-53-042. ALL OTHER WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1439 AND STAND ARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700208 19990417 00208 EU 1999 4 17 SIMA990785 1 19990319 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 201AE 340B201 ABI - DURING MBV INSPECTION, FOUND CHAFE ON RT NACELLE INBOARD OUTER SKIN PANEL. BLENDED AREA AND PERFORMED AN EDDY CUR RENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED AN EXTERNAL DOUBLER .050 INCH THICK. APPLIED SEALANT TO THE CONTACT SURFACE OF THE DOUBLER, ATTACHED DOUBLER TO AIRCRAFT. APPLIED SEALANT AROUND THE DOUBLER EDGE STEP AND RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1439 AND STANDARD SRM PROCEDURES. AIRCRAFT RETURNED TO SE RVICE. (X) 2 L 7 2 4T RT A52EU 1999041700209 19990417 00209 EU 1999 4 17 SIMA990784 1 19990319 A 5220 SKIN SAAB SF340 340B 7860101 EU RT EMERG EXIT DR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 201AE 340B201 ABI - DURING MBV INSPECTION, FOUND DENT ON THE RT FORWARD EMERGENCY EXIT. REMOVED PAINT 1.5 INCHES OUT FROM PLANNED CUT -OUT. CUT OUT DAMAGED AREA, FABRICATED A DOUBLER PLATE WITH DIMENSIONS WHICH OVERLAP THE CUT-OUT BY 1.0 INCH. FILLED H ONEYCOMB CORE WITH EPOXY FILLER LY/HY 5052, INSTALLED FILLER PLATE AND APPLIED PRESSURE. CLEANED THE REPAIR AREA AND TH E DOUBLER, BONDED THE DOUBLER PLATE TO THE SKIN WITH ADHESIVE EA 9330 AND APPLIED DISTRIBUTED PRESSURE UNTIL CURED. APP LIED SEALANT AROUND DOUBLER EDGE AND RESTORED SURFACE FINISH. WORK DONE IAW SAAB 340 SRM 52-10-10, PAGES 201-202 AND ST ANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700210 19990417 00210 EU 1999 4 17 SIMA990776 1 19990318 A 5347 4650000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 594.5-696 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION, SEAT TRACK 18.3L FS 594.5 - FS 696.0 WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT 91.5 IN CH SECTION OF EXISTING SEAT TRACK. FABRICATED A 91.5 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76511 EXTRUDED MATE RIAL. FABRICATED A 15 INCH LONG U-BEAM OF PLAL 075-T7351 MATERIAL. INSTALLED U-BEAM AND EXTRUSION IN AIRCRAFT. WORK D ONE IAW SAAB 340 SRM 53-70-60 AND STANDARD PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700211 19990417 00211 EU 1999 4 17 SIMA990774 1 19990318 A 5350 SKIN SAAB SF340 340B 7860101 EU TAIL CONE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION, A DENT WAS DISCOVERED ON THE RT UPPER TAIL CONE STA 813.5. CUT OUT THE DAMAGED AREA AND RE STORED SURFACE TREATMENT OF THE CUT-OUT. REMOVED FASTENERS AND LIFTED THE VERTICAL STABILIZER FAIRING MOUNT ANGLE TO AL LOW FOR THE INTRODUCTION OF THE DOUBLER. FABRICATED A DOUBLER AND TRIPLER .016 INCH THICK. APPLIED PROTECTIVE TREATMEN T INCLUDING POLYURETHANE TOP COAT. INSTALLED DOUBLER AND TRIPLER TO AIRCRAFT. APPLIED SEALANT AROUND DOUBLER AND TRIPL ER EDGE STEP AND RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1435 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700212 19990417 00212 EU 1999 4 17 SIMA990772 1 19990318 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION, A CHAFE WAS DISCOVERED ON THE RT NACELLE INBOARD SKIN PANEL FROM WING FILLET FAIRING SEAL. CUT OUT AND BLENDED THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS NOTED. RESTORE D PROTECTIVE TREATMENT TO THE REPAIR AREA. FABRICATED A DOUBLER .050 INCH THICK. ATTACHED DOUBLER TO AIRCRAFT, APPLIED SEALANT AROUND DOUBLER EDGE STEP AND RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1435 AND STA NDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700213 19990417 00213 EU 1999 4 17 SIMA990762 1 19990317 A 5347 4650000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-311 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 201AE 340B201 ABI - DURING MBV INSPECTION, SEAT TRACK 18.3L FS 297-311 WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT 14 INCH SECTION OF EXISTING SEAT TRACK. FABRICATED 14 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T7351 MATERIAL. FABRICATED A 15 IN CH LONG U-BEAM OF PLAL 7075-T76511 MATERIAL. INSTALLED U-BEAM AND NEW EXTRUSION IN AIRCRAFT. WORK DONE IAW SAAB 340 SR M 53-70-60 AND STANDARD SRM PROCEDURES. (X) 2 L 7 2 4T RT A52EU 1999041700214 19990417 00214 EU 1999 4 17 SIMA990787 1 19990319 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 201AE 340B201 ABI - DURING MBV INSPECTION, FOUND CHAFE ON RT NACELLE INNER SKIN. BLENDED AREA AND PERFORMED AN EDDY CURRENT INSPECTIO N WITH NO INDICATIONS OF CRACKS. FABRICATED A REINFORCEMENT DOUBLER .025 INCH THICK. APPLIED SEALANT TO THE CONTACT SU RFACE OF THE DOUBLER AND ATTACHED TO AIRCRAFT. APPLIED FIRE SEAL AROUND THE DOUBLER WITH DOW CORNING DC 730 RTV. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1439 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700215 19990417 00215 EU 1999 4 17 SIMA990777 1 19990318 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 295 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION, AN AREA ON TOP FUSELAGE SKIN PANEL FS 295, WAS DISCOVERED TO HAVE CORROSION REMOVED TO DEPT H BEYOND SRM LIMITS. CLEANED AREA WITH MEK AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS. FABRICA TED A REPAIR DOUBLER FROM ALSH 2024-T3 .050 INCH THICK. CLEANED DOUBLER, APPLIED A PROTECTIVE COAT OF ALODINE AND ONE C OAT OF EPOXY PRIMER. APPLIED SEALANT TO THE CONTACT SURFACE OF THE DOUBLER. INSTALLED DOUBLER ON AIRCRAFT. APPLIED PR IMER AND ONE COAT OF TOP COAT TO THE INTERIOR AND EXTERIOR SURFACES. RESTORED PAINT FINISH. WORK DONE IAW SAAB 340 SRM 53-70-10, PAGE 215 AND STANDARD PROCEDURES. (X) 2 L 7 2 4T RT A52EU 1999041700216 19990417 00216 EU 1999 4 17 SIMA990673 1 19990308 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 174AE 340B174 ABI - REPAIRED DENT IN CARGO DOOR. INSPECTED AND DETERMINED THE LARGEST EXTENT OF DAMAGED AREA TO BE REPAIRED. A CUT- OUT WITH A MINIMUM RADIUS OF .5 INCH WAS MADE IN THE SKIN TO REMOVE DAMAGE. FABRICATED A FILLER PLATE WITH DIMENSIONS E QUAL TO CUT-OUT, THICKNESS EQUAL TO THE EXISTING SKIN. FAB A DOUBLER PLATE .032 INCH THICK WHICH OVERLAPPED CUT-OUT BY 1.0 INCH. APPLIED EPOXY FILLER LY/HY 5052 TO EXPOSED HONEYCOMB AND INSTALLED FILLER PLATE. BONDED DOUBLER TO CARGO DOO R WITH ADHESIVE EA 9330 AND APPLIED PRESSURE TO REPAIR DURING CURING. FILLET SEALED AROUND REPAIR AND RESTORED SURFACE PROTECTION. WORK DONE IAW SAAB 340B SRM 52-10-10, PAGES 201-203, AND STD SRM PRACTICES. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700217 19990417 00217 EU 1999 4 17 SIMA990641 1 19990305 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 338SB 340B338 ABI - DURING A MBV INSP, DENTS DISCOVERED ON THE CARGO DOOR SKIN BEYOND SRM LIMITS. PERFORMED EDDY CURRENT INSP AND A B OND TEST. CUT OUT DAMAGED AREA OF ONE OF THE DENTS, SECOND DENT WAS NOT TO BE CUT OUT. DEBURRED AND SMOOTHED EDGES OF THE CUT-OUT. FABRICATED A FILLER PLATE AND A DOUBLER PLATE .032 INCH THICK. FILLED HONEYCOMB CORE WITH EPOXY FILLER LY /HY 5052. INSTALLED THE FILLER PLATE AND APPLIED PRESSURE. CLEANED THE REPAIR AREA AND THE DOUBLER AND BONDED DOUBLER PLATE TO THE SKIN WITH ADHESIVE EA 9330. APPLIED DISTRIBUTED PRESSURE TO THE DOUBLER UNTIL CURED. RESTORED SURFACE FIN ISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1416 AND SAAB 340 SRM 52-10-10. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700218 19990417 00218 EU 1999 4 17 SIMA990511 1 19990222 A 2910 93026310002 LINE SAAB SF340 340B 7860101 EU HYDRAULIC SYSTEM BROKEN A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 343SB 340B343 LAX - FLT 3223 - MAIN HYDRAULIC PRESSURE INDICATION DROPPED TO ZERO IMMEDIATELY AFTER TAKEOFF. EMERGENCY GEAR EXTENSION HANDLE PULLED PER QRH. AIRCRAFT RETURNED TO LAX AND LANDED SAFELY. FOUND FLEXIBLE HYDRAULIC LINE FROM HYDRAULIC PUMP TO FILTER BROKEN, RESULTING IN SYSTEM FLUID LOSS. REMOVED AND REPLACED HYDRAULIC LINE AND SERVICED HYDRAULIC SYSTEM. A IRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700219 19990417 00219 EU 1999 4 17 SIMA990773 1 19990318 A 5220 SKIN SAAB SF340 340B 7860101 EU RT EMER EXIT DR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSP, A SHARP DENT DISCOVERED ON RT FWD EMERGENCY EXIT BEYOND SRM LIMITS. REMOVED PAINT 1.5 INCHES OUT FROM EDGE OF PLANNED CUT-OUT. CUT OUT DAMAGED AREA, DEBURRED, AND SMOOTHED EDGES. FAB A FILLER PLATE WITH DIMENSIONS EQUAL TO CUT-OUT. FAB A DOUBLER PLATE WITH DIMENSIONS WHICH OVERLAP CUT-OUT BY 1.0 INCH. FILLED HONEYCOMB CORE WITH EP OXY FILLER LY/HY 5052, INSTALLED FILLER PLATE, APPLIED PRESSURE. CLEANED THE REPAIR AREA AND DOUBLER, BONDED DOUBLER PL ATE TO THE SKIN WITH ADHESIVE EA 9330, APPLIED PRESSURE UNTIL CURED. APPLIED SEALANT AROUND DOUBLER EDGE STEP, RESTORED SURFACE FINISH. WORK DONE IAW SAAB 340 SRM 52-10-10 PGS 201-202, AND STD SRM PROCEDURES. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700220 19990417 00220 EU 1999 4 17 SIMA990771 1 19990318 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339 DENTS A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - DURING MBV INSPECTION, DENTS ON RT FUSELAGE SKIN PANEL WERE DISCOVERED BETWEEN SL 1616/1617 AFT OF FRAME 339 BEYON D SRM LIMITS. RECONTOURED DAMAGED AREA AND PERFORMED AN EDDY CURRENT WITH NO INDICATIONS OF CRACK. FABRICATED A REPAIR DOUBLER .050 INCH THICK. CLEANED THE DOUBLER AND APPLIED A PROTECTIVE COAT OF ALODINE AND ONE COAT OF EPOXY PRIMER. A TTACHED DOUBLER TO AIRCRAFT AND APPLIED SEALANT TO THE EDGE STEP OF THE DOUBLER. CLEANED THE REPAIR AREA AND APPLIED ON E COAT OF EPOXY PRIMER TO EXTERIOR AND SHOP HEADS. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72S DS1435 AND SAAB 340 SRM 53-70-10 PAGES 215-216. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700221 19990417 00221 EU 1999 4 17 SIMA990761 1 19990317 A 5347 4650000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-327 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 201AE 340B201 ABI - DURING MBV INSPECTION, SEAT TRACK BL ZERO FS 297 - BS 327, WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT 30 INCH SECTION OF EXISTING SEAT TRACK. FABRICATED 30 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76511 EXTRUDED MATERIAL. F ABRICATED A 15 INCH LONG U-BEAM OF PLAL 7075-T7351 MATERIAL. INSTALLED U-BEAM AND NEW SECTION EXTRUSION IN AIRCRAFT. WO RK DONE IAW SAAB 340 SRM 53-70-60 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700222 19990417 00222 EU 1999 4 17 SIMA990461 1 19990215 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 174AE 340B174 ABI - AIRCRAFT ARRIVED FOR PERMANENT REPAIR TO A DENT IN THE CARGO DOOR. EVALUATED AREA AND REMOVED PAINT. A CUT-OUT W ITH A MINIMUM RADIUS OF .5 INCH WAS MADE IN THE SKIN TO REMOVE THE DAMAGE. FABRICATED A FILLER PLATE WITH DIMENSIONS EQ UAL TO THE CUT-OUT, THICKNESS EQUAL TO THE EXISTING SKIN. FABRICATED A DOUBLER PLATE WHICH OVERLAPS CUT-OUT BY 1.0 INCH . APPLIED EPOXY FILLER LY/HY 5052 TO EXPOSED HONEYCOMB AND INSTALLED FILLER PLATE. BONDED DOUBLER TO CARGO DOOR WITH A DHESIVE EA 9330 AND APPLIED PRESSURE TO THE REPAIR DURING CURING. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR S TATEMENT 72SDS1332 AND SAAB 340 SR 52-30-10, PAGE 203, 52-10-10, PAGES 201-203. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700223 19990417 00223 EU 1999 4 17 SIMA990442 1 19990213 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 ABI - DURING AN MBV INSPECTION, FOUND A CHAFE ON LT NACELLE INNER SKIN. BLENDED CHAFE AREA AND PERFORMED AN EDDY CURREN T INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A DOUBLER FROM CRES 301 1/4 HARD .025 INCH THICK. APPLIED SEALA NT TO THE CONTACT SURFACE OF THE DOUBLER, REPOSITIONED, AND INSTALLED FASTENERS WET. APPLIED FIRE SEAL WITH DOW CORNING DC 730 RTV. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1383. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700224 19990417 00224 EU 1999 4 17 SIMA990441 1 19990213 A 5347 4650000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-308 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 339SB 340B339 ABI - DURING AN MBV INSPECTION, SEAT TRACK 18.3L WAS FOUND CORRODED FROM STA 297.0 - STA 308.0. CUT OUT A 11 INCH SECTI ON OF SEAT TRACK, DEBURRED, ALODINED, PRIMERED, AND PAINTED EDGES. FABRICATED A 15 INCH LONG U-BEAM OF PLAL 7075-T76511 EXTRUDED MATERIAL. POSITIONED REPAIR U-BEAM INSIDE EXISTING SEAT TRACK AND DRILLED HOLES. INSTALLED SEAT TRACK IN AIR CRAFT. WORK DONE IAW SAAB 340 SRM 53-70-60. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700225 19990417 00225 EU 1999 4 17 SIMA990392 1 19990208 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 BL ZERO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 194AE 340B194 ABI - DURING AN MBV INSPECTION, SEAT TRACK BL ZERO AT STA 297 WAS FOUND CORRODED. CUT OUT 11 INCH SECTION OF SEAT TRACK . FABRICATED A 11 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76511. FABRICATED A 15 INCH LONG U-BEAM OF PLAL 7075- T7351. POSITIONED U-BEAM INSIDE EXISTING SEAT TRACK. INSTALLED SEAT TRACK IN AIRCRAFT. WORK DONE IAW SAAB REPAIR STAT EMENT 72SDS1375 AND SAAB 340 SRM 53-70-60. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700226 19990417 00226 EU 1999 4 17 SIMA990391 1 19990208 A 5350 FAIRING SAAB SF340 340B 7860101 EU STAB/FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 194AE 340B194 ABI - DURING AN MBV INSPECTION, A CHAFE WAS DISCOVERED AT LT STABLIZER TO FUSELAGE FILLET FAIRING CONTACT AREA. BLENDED CHAFE AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. APPLIED PROTECTIVE TREATMENT INCLUDING T OP COAT TO BLENDED AREA. FABRICATED AN EXTERNAL DOUBLER .025 INCH THICK. APPLIED PROTECTIVE TREATMENT INCLUDING POLYUR ETHANE TOP COAT. INSTALLED DOUBLER TO AIRCRAFT. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1375, SB 340-53-042 AND SAAB SRM 51-20-52. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999041700227 19990417 00227 EU 1999 4 17 SIMA990701 1 19990311 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 710 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AE 340B232 ABI - REPAIRED DENT ON BOTTOM AFT FUSELAGE SKIN PANEL FS 710. RECONTOURED DENT AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A REPAIR DOUBLER .063 INCH THICK. POLISHED SKIN UNDER DOUBLER WITH SCOTCHBRITE. CLEANED SKIN AND DOUBLER THEN APPLIED SURFACE TREATMENT. ATTACHED DOUBLER TO AIRCRAFT, APPLIED FILLET SEALANT AROUND EDGES OF DOUBLER. APPLIED TOP COAT AND PREVENTIVE COMPOUND TO THE REPAIR AREA. RESTORED SURFACE FINISH TO THE OUTER SU RFACE. WORK DONE IAW SAAB 340 SRM 53-80-10 PAGES 201-203 AND STANDARD SRM PROCEDURES. (X) 2 L 7 2 4T RT A52EU 1999041700228 19990417 00228 EA 1999 4 17 MASA99040 1 19990215 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 2 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 47239 FEB981239 7239 FOUND HYDRAULIC FLUID LEAKING FROM NR 2 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR 99ZZZX1487 THROUGH 99ZZZX1522. (X) 2 L 7 2 4F RT A21EA 1999041700229 19990417 00229 EA 1999 4 17 99ZZZX1487 1 19990215 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 1 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 47239 FEB981242 7239 FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700230 19990417 00230 EA 1999 4 17 99ZZZX1488 1 19990215 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKAING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 47239 FEB980237 7239 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700231 19990417 00231 EA 1999 4 17 99ZZZX1489 1 19990203 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17231 AUG971064 7231 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700232 19990417 00232 EA 1999 4 17 99ZZZX1490 1 19990125 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 27173 JAN930155 7173 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700233 19990417 00233 EA 1999 4 17 99ZZZX1491 1 19990112 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 27173 JAN960640 7173 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700234 19990417 00234 EA 1999 4 17 99ZZZX1492 1 19990103 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 27191 OCT960888 7191 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700235 19990417 00235 EA 1999 4 17 99ZZZX1493 1 19990101 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17217 OCT971120 7217 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700236 19990417 00236 EA 1999 4 17 99ZZZX1494 1 19990101 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 2 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 27172 OCT960848 7172 FOUND HYDRAULIC FLUID LEAKING FROM NR 2 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700237 19990417 00237 EA 1999 4 17 99ZZZX1495 1 19990101 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 27172 OCT960889 7172 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700303 19990417 00303 CE 1999 4 17 99ZZZX1561 1 19990319 A 5312 FIREWALL BEECH 58 58 1152740 CE ENGINE BAY DAMAGED A A8JA K NONE O OTHER IN INSP/MAINT 1 SW 09 6037U TH1021 ACTT: 9,619.9 HOURS. UPON ENGINE REMOVAL AND MOUNT REMOVAL, MOUNTING HOLES IN FIREWALL WERE FOUND ELONGATED AND MUSHROO MED. 1 L 7 2 3O 3A16 1999041700306 19990417 00306 NM 1999 4 17 SWAA990670 1 19990409 A 5320 6554402262 WEB BOEING 737 7373H4 1384600 NM BS 663.75 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 663.75, RBL 52, WL 177, RT MAIN LANDING GEAR WHEEL WELL. REPAIRED WEB PER SWA RA NR 1-353-2052. 2 L 7 2 4F RT A16WE 1999041700307 19990417 00307 NM 1999 4 17 SWAA990671 1 19990409 A 5320 BAC15061777 ANGLE BOEING 737 7373H4 1384600 NM BS 695 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND BS 695, STRINGER 18A LT, ANGLE CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999041700308 19990417 00308 NM 1999 4 17 SWAA990672 1 19990409 A 5330 65C330495 SKIN BOEING 737 7373Q8 1384670 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C3 CHECK, FOUND CRACK ON OUTER FUSELAGE SKIN COMING OUT OF AFT SERVICE DOOR LOWER HINGE CUT OUT. REPAI RED SKIN PER SWA RA NR 1-353-2058 AND SRM. 2 L 7 2 4F RT A16WE 1999041700309 19990417 00309 NM 1999 4 17 SWAA990673 1 19990409 A 5311 BAC14902808 FRAME BOEING 737 7373Q8 1384670 NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED C3 CHECK, FOUND CRACK ON FWD CARGO FWD FRAME 6.625 INCHES ABOVE LOWER END. REPAIRED PER SWA RA NR 1-35 3-2059. 2 L 7 2 4F RT A16WE 1999041700310 19990417 00310 NM 1999 4 17 SWAA990674 1 19990409 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING FAA INSPECTING AIRCRAFT, FOUND EMERGENCY ESCAPE PATH LIGHTING INOP. FOUND LIGHT DISCONNECTED. RECONNECTED LIGHT S PER MM, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999041700311 19990417 00311 NE 1999 4 17 SWAA990675 2 19990410 A 7320 1853M33P02 HMU BOEING 737 7377H4 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE CONTAMINATED A SWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 07 701GS 27836 874200 INFLIGHT SHUT DOWN, NR 2 ENGINE ROLLED BACK AT 31,000 FEET AND 87 PERCENT N1, WINDMILLED AND APU RESTART UNSUCCESSFUL AT 25,000 FEET, 280 KNOTS. APU RESTARTED AT 19,000 FEET 280 KNOTS, ENGINE RAN FOR APPROXIMATE 20 MINUTES AND ROLLED BACK AGAIN AT 12,000 FEET, 35 PERCENT N1 (ENGINE FLAMED OUT). REMOVED AND REPLACED NR 2 HMU AND FUEL PUMP (SUSPECT CONTAMINA TION), OPS AND LEAK CHECKED GOOD PER MM. PUMP (P/N 828300-3), (S/N YA010103-F). 2 L 7 2 4F 4 F RT A16WE E2GL 1999041700312 19990417 00312 NM 1999 4 17 SWAA990676 1 19990411 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 FWD ENTRY DOOR SLIDE DROPPED OUT OF BASKET. REINSTALLED L1 SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999041700313 19990417 00313 NM 1999 4 17 SWAA990677 1 19990411 A 3350 11032 LENS BOEING 737 7373H4 1384600 NM ROW 18 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 EMERGENCY EXIT LENS MISSING ON OVERHEAD BIN, ROW 18D. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 1999041700314 19990417 00314 NM 1999 4 17 SWAA990678 1 19990411 A 3230 D4536 PIN BOEING 737 7373H4 1384600 NM RT MLG BROKEN A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 311SW 23333 AIR TURNBACK DUE TO AN UNSAFE LIGHT, REMAINED ON AT RIGHT MAIN LANDING GEAR AFTER TAKEOFF. GEAR WAS LOWERED AND 3 GREEN LIGHTS WERE NORMAL. FOUND BROKEN PIN LOCK AT DISCONNECT D4536, PIN NR 3, WIRE 424-A-R. REMOVED AND REPLACED PIN PER M M GEAR RETRACTION GOOD. 2 L 7 2 4F RT A16WE 1999041700315 19990417 00315 NM 1999 4 17 SWAA990679 1 19990411 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 8 INCHES LONG AT BS 500C, STRINGER 3L. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999041700316 19990417 00316 NM 1999 4 17 SWAA990680 1 19990410 A 5311 6546570 FRAME BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT BS 1016 FRAME, BETWEEN STRINGERS 26L-26R. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999041700317 19990417 00317 NM 1999 4 17 SWAA990681 1 19990409 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM EXTERIOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND LEFT AND RIGHT SIDE, OUTER EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY SUPPL Y PER MM. 2 L 7 2 4F A16WE 1999041700318 19990417 00318 NM 1999 4 17 SWAA990682 1 19990410 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD, BS 328, LBL 28. REPAIRED BEAM PER SWA RA NR 1-35 3-2049. 2 L 7 2 4F RT A16WE 1999041700319 19990417 00319 NM 1999 4 17 SWAA990683 1 19990410 A 3397 W1460 WIRE BOEING 737 7373H4 1384600 NM SERVICE DOOR CUT A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY SLIDE ESCAPE LIGHT AT FWD GALLEY DOOR INOP. FOUND WIRE ASSY TO LAMP CUT. S PLICED WIRE PER MM. 2 L 7 2 4F RT A16WE 1999041700320 19990417 00320 NM 1999 4 17 SWAA990684 1 19990411 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED C3 CHECK, FOUND AFT SECTION OF FLOOR TRACK EMERGENCY LIGHTING INOP. REPLACED BATTERY PACK AND HOUSING ASSY. 2 L 7 2 4F RT A16WE 1999041700321 19990417 00321 NM 1999 4 17 SWAA990685 1 19990411 A 2560 655463 GIRT BAR BOEING 737 7373H4 1384600 NM PASSENGER DOOR NOT LATCHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR HOOK NOT LATCHING. REMOVED AND REPLACED BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 1999041700322 19990417 00322 WP 1999 4 17 TWAA9905401 1 19990413 A 3350 58222 BATTERY PACK DOUG DC9 DC951 3022051 WP ROW 12-16 DIRTY A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 405EA 47688 THE EGRESS LIGHTS WOULD NOT EXTINGUISH AT CABIN ROWS 12 TO 16. CLEANED THE CONNECTION AT THE BATTERY PACK. CHECK-C 3-3 0-99 STL. 2 L 7 2 4F RT A6WE 1999041700323 19990417 00323 WP 1999 4 17 TWAA9905402 1 19990405 A 5530 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT, FOUND .1875 INCH CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE AT STA 1421. REMOVED AND REPLACED AT TACH ANGLE PER SB 53-223 AND PER MD9-AD-13. 2 L 7 2 4F A6WE 1999041700324 19990417 00324 WP 1999 4 17 TWAA9905403 1 19990404 A 5530 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT, FOUND .1875 INCH CRACK AT THE LT DORSAL FIN ATTACH ANGLE STA 1421. INSTALLED NEW ATTACH ANGLE PER SB 53-223 AND SRO9530162. 2 L 7 2 4F A6WE 1999041700325 19990417 00325 NM 1999 4 17 TWAA9905404 1 19990409 A 5330 SKIN BOEING 767 7673Q8 NM BS 1439 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 635TW 28207 DURING CHECK-C MAINT, FOUND DEEP SCRATCHES WITH CRACK INDICATION, CONFIRMED BY EDDY CURRENT, AT STA 1439 JUST ABOVE STR 35L UP TO JUST BELOW BULK CARGO ENTRY. REMOVED DAMAGED AREA AND INSTALLED 12 IN BY 12 IN .125 THICK 2024T3 DOUBLER PER SRM 53-00-01. 2 L 7 2 4F RT A1NM 1999041700332 19990417 00332 NM 1999 4 17 CALA9900400 1 19990413 A 5720 ANGLE BOEING 727 727243 138408D NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 2.75 INCH CRACK IN LT WING REAR SPAR O/B SUPPORT ANGLE WHERE NR 2 SPOILER ACTUATOR AND FLAP DRIVE CAS TING MOUNTS. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F RT A3WE 1999041700333 19990417 00333 NM 1999 4 17 CALA9900401 1 19990413 A 3397 WIRE BOEING 727 727243 138408D NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17402 21265 THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW WPM 20-10-13, PAGE 1. OPERATION OF THE EXIT LIGHT CHECKED GOOD. 2 L 7 3 4F RT A3WE 1999041700334 19990417 00334 NM 1999 4 17 CALA9900402 1 19990413 A 5320 CHANNEL BOEING 757 757224 1384958 NM RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND A .25 INCH CRACK IN RT MLG WHEEL WELL FORWARD SEAL RETAINER SUPPORT CHANNEL. THE SEAL RETAINER SUPPORT CHANNEL WAS REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A2NM 1999041700335 19990417 00335 WP 1999 4 17 CALA9900403 1 19990413 A 5755 SPOILER DOUG DC10 DC1030 3023501 WP NR 2 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14074 46911 INSPECTION FOUND THE RT WING NR 2 SPOILER DAMAGED. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-60-01, PAGE 401. 2 L 7 3 4F A22WE 1999041700336 19990417 00336 WP 1999 4 17 CALA9900404 1 19990414 A 5320 SILL DOUG DC10 DC1030 3023501 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND THE FORWARD CARGO BAY FORWARD LOWER DOOR SILL CORRODED IN FORWARD CORNER. THE DOOR SILL WAS REPAIRED I AW SRM 53-50-00, FIGURE 9. 2 L 7 3 4F A22WE 1999041700337 19990417 00337 NM 1999 4 17 CALA9900405 1 19990414 A 5330 SKIN BOEING 757 757224 1384958 NM BS 600 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 600 BETWEEN STRINGERS 18L AND 19L. THE SKIN WAS REPAIRED IAW ECRA 5331-010 51. 2 L 7 2 4F RT A2NM 1999041700338 19990417 00338 NM 1999 4 17 CALA9900406 1 19990414 A 3350 38931002 BATTERIES AEROQUALITY BOEING 727 727232 1384082 NM ROW 8 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 511PE 20634 THE OVERHEAD EMERGENCY LIGHT AT ROW 8 WAS FOUND INOPERATIVE. THE LIGHT BATTERIES WERE REMOVED AND REPLACED AND OPERATIO N OF THE LIGHT WAS RESTORED. 2 L 7 3 4F A3WE 1999041700339 19990417 00339 NM 1999 4 17 CALA9900407 1 19990414 A 5751 652176623 SKIN BOEING 727 727243 138408D NM LT AILERON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .5 AND .375 INCH CRACK IN LT O/B AILERON LOWER SKIN WITH A BEND AT I/B EDGE. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-31. 2 L 7 3 4F RT A3WE 1999041700340 19990417 00340 WP 1999 4 17 CALA9900408 1 19990414 A 5320 571658841 BOLT DOUG DC10 DC1030 3023501 WP LT MLG SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LT MLG BAY TRAPEZOIDAL FRAME UPPER FLANGE BOLT SHEARED. THE BOLT, NUT AND WASHERS WERE REPLACED IAW MM 20-20-01. 2 L 7 3 4F A22WE 1999041700341 19990417 00341 WP 1999 4 17 9901411224 1 19990403 A 3260 SWITCH DOUG DC10 DC1030 3023501 WP RT MLG DOOR FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 224NW 46581 ON DEPARTURE FROM AMS, THE RIGHT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE. RECYCLED GEAR, LIGH T WENT OUT, ILLUMINATED, AND THEN WENT OUT AGAIN. LIGHT WAS ONLY VISIBLE ON FORWARD PANEL AND NOT ON SECOND OFFICER'S P ANEL. REPLACED DOOR PROXIMITY SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A22WE 1999041700342 19990417 00342 NM 1999 4 17 9901425503 1 19990410 A 2910 LINE BOEING 757 757251 1384970 NM NLG STEERING BROKEN A NWAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 01 503US 23192 UPON GEAR EXTENSION ON LANDING, THE LEFT HYDRAULIC SYSTEM LOST ALL PRESSURE AND SYSTEM QUANTITY DECREASED TO ZERO. ALL THREE GEAR WERE DOWN AND LOCKED. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TOW ED FROM THE RUNWAY TO THE GATE. MAINTENANCE FOUND THE RIGHT OUTBOARD NOSE WHEEL STEERING HYDRAULIC LINE BROKEN. REPL ACED THE HYDRAULIC LINE, BOTH LEFT SYSTEM HYDRAULIC PUMPS, AND ASSOCIATED FILTERS. SYSTEM TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999041700343 19990417 00343 WP 1999 4 17 9901439877 1 19990408 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F RT A6WE 1999041700344 19990417 00344 WP 1999 4 17 9901449877 1 19990412 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999041700345 19990417 00345 WP 1999 4 17 UPS99829241 1 19990412 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999041700346 19990417 00346 WP 1999 4 17 UPS99829242 1 19990324 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 280-300 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, MAIN CABIN SEAT TRACK NR 6R GOUGED STA 280-300. REMOVED CORRODED GOUGED SEAT TRACK STA 230-3501. INSTALLED NEW SEAT TRACK FROM STA 230-350. INSTALLED SPLCIES STA 230, 270, AND 350 IAW DC8 SRM 53-2-3 AND DC8 SRM 51-3 -0. INSTALLED FLOORBEAMS EACH SIDE OF THE SEAT TRACK STA 270-350 IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999041700347 19990417 00347 WP 1999 4 17 UPS99829243 1 19990325 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 857-1020 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, SEAT TRACK F HAS AREAS OF CORROSION ENTIRE LENGTH FROM FS 857-1020. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED SEAT TRACKS RBL 60 FROM STA 1020, FABRICATED NEW SEAT T RACK AND SEAT TRACK SPLICES IAW DC8 SRM 53-2-3 AND DC8 532 0-8309. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SE AT TRACK AND REPAIR SPLICES IAW DC8 SRM 51-3-0 AND 53-2-3. 2 L 7 4 4F RT 4A25 1999041700348 19990417 00348 WP 1999 4 17 UPS99829244 1 19990325 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 50 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, FWD A/C BAY STA 50 L33R CORRODED BEYOND LIMITS. MAT'L ID IAW DC8 SRM 53-2-3. LOCATED AND DRILLED AND DEBURRED NEW LONGERON AND END FITTING AND SPLICE IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INS TALLED LONGERON FITTING LONGERON AND LONGERON SPLICE IAW DC8 SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1999041700349 19990417 00349 WP 1999 4 17 UPS99829245 1 19990327 A 5313 FRAME DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, FS 70 L33R CORRODED FRAME. CORRODED BEYOND LIMITS MATERIAL ID IAW DC8 SRM 53-2-5. FABRICATED IAW DC8 SRM 53-2-5, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999041700350 19990417 00350 WP 1999 4 17 UPS99829246 1 19990324 A 5230 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, MAIN CARGO DOOR FITTING IS CRACKED VERIFY B-1 NDT. REMOVED AND REPLACED FITTING IAW UPS DC8 SRM 5 1-1-21 AND SRM 51-1-24. 2 L 7 4 4F RT 4A25 1999041700351 19990417 00351 WP 1999 4 17 UPS99829247 1 19990322 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1650-1660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, LONGERON 33 RIGHT CORRODED AT STA 1650-1660. REMOVED EXISTING LONG SECTION, REPLACED WITH NEW SEC TION (P/N 575777 8-1). 2 L 7 4 4F RT 4A25 1999041700352 19990417 00352 WP 1999 4 17 UPS99829248 1 19990322 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1560-1590 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, LONGERON 25 RIGHT HAS REPAIR AT FS 1560-1590 CORRODED BULGED. REMOVED PREVIOUS REPAIR ANGLE IAW D C8 SRM 51-1-21, CORROSION WAS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMGED SECTION OF LONGERON AND SPLC IED IN NEW SECTION IAW DC8 SRM 53-4-1, 53-2-2 AND 51-1-20D. APPLIED ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999041700353 19990417 00353 WP 1999 4 17 UPS99829249 1 19990322 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRAKCED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, INTERCOSTAL END FITTING STA 857, LONGERON 18L IS CRACKED. REMOVED CRACKED END FITTING IAW DC8 SRM 51-1-20D. MATERIAL ID FOR NEW FITTING 7075-T651 IAW DAC DWG 4750423 PO 265699, FABRICATED NEW END FITTING IAW DAC DWG 4750423. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED NEW FITTING IAW DC8 51-1-20D. 2 L 7 4 4F RT 4A25 1999041700354 19990417 00354 WP 1999 4 17 UPS99829250 1 19990403 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, INTERCOSTAL END FITTING AT STA 857 LONGERON 19L IS CRACKED. REMOVED CRACKED END FITTING IAW DC8 S RM 51-1-20D. MATERIAL ID FOR NEW END FITTING 7075-T651 PLATE PO 265699 IAW DAC DWG 4750422. FABRICATED NEW END FITTING IAW DAC DWG 4750422, PERFORMED DYE-PENETRANT INSPECTION IAW MIL-S-271F, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTA LLED NEW END FITTING DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999041700355 19990417 00355 WP 1999 4 17 UPS99829251 1 19990327 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, REMOVED AND REPLACED MAIN FRAME STA 920 LEFT HAND LOWER DUE TO CORR BLENDOUT. REMOVED CUSP MEMBRA NE WEB, MAINFRAME AND LONG 21 AND INTERCOSTAL AT FS 920 LEFT HAND IAW DC8 SRM 51-1-20D AND 51-1-21. MAIN FRAME FOUND TO BE WITHIN LIMITS AFTER BLENDOUT IAW REO 06417, MATERIAL ID FOR SPLCIES ON CUSP WEB 301 1/2 HARD STAINLESS STEEL .025 P O 211819 IAW UPS EO DC8 5330-2159B, ALODINED AND PRIMED ALL PARTS IAW DC8 51-1-8. 2 L 7 4 4F RT 4A25 1999041700356 19990417 00356 WP 1999 4 17 UPS99829252 1 19990327 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 280-300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, MAIN CABIN SEAT TRACK NR 7 R EXFOLIATED BELOW STA 280-300. REMOVED FLOOR PANELS CORROSION OUT OF LIMITS IAW DC8 SRM 51-1-8 ON SEAT TRACK. REMOVED CORROSION IAW DC8 SRM 51-1-8, UNDER SEAT. REMOVED SEAT TRACK FS 290 T O 610, DRILLED NEW SEAT TRACK AND SPLCIES IAW DC8 S RM 51-1-24, ALODINED AND PRIMED SEAT TRACK SPLICES IAW DC8 SRM 51-1 -8, INSTALLED SPLICES IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999041700357 19990417 00357 WP 1999 4 17 UPS99829253 1 19990323 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-C/CK, FWD CARGO BAY, RIGHT HAND BAY TUNNEL AREA STA 200 FLOORBEAM AND WEB AT CUSP AREA IS CORRODED. COR ROSION EXFOLIATED OUT OF LIMITS IAW SRM 53-2-0. REMOVED FLOORBEAM, ALODINED AND PRIMED IAW DC8S RM 51-1-8, INSTALLED D OUBLER ON CUSP IAW DC8-5330-2159-B AND SRM 51-1-21, INSTALLED PREVIOUSLY REMOVED SEAT TRACK IAW DC8 SRM 51-3-0, INSTALLE D FLOORBEAM IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999041700358 19990417 00358 WP 1999 4 17 UPS99829254 1 19990414 A 3350 CONNECTOR DOUG DC8 DC871F 302199D WP CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-N/A, EMERGENCY LIGHT DISARM LIGHT WILL NOT ILLUMINATE. REPLACED BULB TWICE AND STILL INOP. RESEATED CAN NON PLUG AND RE-LAMPED, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999041700359 19990417 00359 WP 1999 4 17 UPS99829255 1 19990412 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WHEN ARMED. REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999041700360 19990417 00360 WP 1999 4 17 UPS99829256 1 19990413 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-N/A, EMERGENCY LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATT PACK, OPS CHECK GOOD. P/N OF F 5708458-503,P/N ON 60-1223-5, S/N ON 335, OFF 3310 2 L 7 4 4F RT 4A25 1999041700361 19990417 00361 NM 1999 4 17 QXEA990550 1 19990410 A 3220 88357 TRAILING ARM DHAV DHC8 DHC8202 2809007 NM NLG DAMAGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 363PH 520 SEA- DAMAGE TO THE NOSE GEAR TRAILING ARM NOTED DURING PUSHBACK. MAINTENANCE INSPECTED AND FOUND SAFE FOR FERRY FLIGHT SEA-PDX. IN PDX REPLACED THE NOSE GEAR TRAILING ARM, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999041700362 19990417 00362 EU 1999 4 17 99FDEA00142 1 19990414 A 3230 DAMPENER AIRBUS 310 A310203 EU LEFT MLG INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 425FE 264 LAND GEAR LEVER UPON RETRACTION IND RETRACT FAULT. TRIED TO RECYCLE GEAR DOWN TO UP & SAME IND. *S/D* REMOVED AND REP LACED LT MLG PITCH DAMPENER IAW 32-11-15. RECHARGED NITROGEN PRESSURE MM 12-12-32. TEST OK. 2 L 7 2 4F RT A35EU 1999041700363 19990417 00363 1999 4 17 99FDEA00143 2 19990414 A 7200 ENGINE BOEING 727 727227 1384078 NM NR 2 FAILED A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 25 493FE 21531 99-88 - OIL PRESSURE ON NR AND ENGINE HI (57 PSI). RUN OIL PRESSURE HI CKLIST AND OIL QUANTITY INCREASE ENG WAS SHUTDOW N ACCORD TO CKLIST. REMOVED AND REPLACED NR 2 ENG PER WC 70T0002 AND PERF ENG RUNS PER WC 70T0301. NO LEAKS. AC OK FO R SERVICE 2 L 7 3 4F A3WE 1999041700364 19990417 00364 1999 4 17 99UAL900107 4 19990203 A 2565 D31038201 TUBE AIR CRUISERS D31096201 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 390 12596 0480 24763 SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALU ATION AND REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1999041700365 19990417 00365 1999 4 17 99UAL900108 4 19990204 A 2565 D31038201 TUBE AIR CRUISERS D31096201 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 501UA 1090 12996 0534 24622 SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALU ATION AND REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1999041700366 19990417 00366 1999 4 17 99UAL900110 4 19990203 A 2565 D31042205 TUBE AIR CRUISERS D31101205 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 533UA 789 91696 0469 25073 SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALU ATION AND REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1999041700367 19990417 00367 1999 4 17 99UAL900111 4 19990203 A 2565 D31393109 TUBE AIR CRUISERS D31394105 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 557UA 1090 7996 0377 26653 SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALU ATION AND REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1999041700368 19990417 00368 1999 4 17 99UAL900112 4 19990203 A 2565 D31039202 TUBE AIR CRUISERS D31098202 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 511UA 589 83195 0368 24799 SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALU ATION AND REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1999041700369 19990417 00369 NE 1999 4 17 99UAL900157 2 19990315 A 7530 SEAL ARKWIN 1211175011 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VSV ACTUATOR LEAKING A UALA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 WP 29 339UA 24243 855357 FUEL LEAKING OUT OF DRAIN. *S/D* FUEL LEAKAGE FOUND AT NUMBER 1 ENGINE LEFT VSV ACTUATOR SEAL AND SHROUD DRAIN WITH EN GINE OFF. THE VARIABLE STATOR VANE (VSV) ACTUATOR SEALS SOMETIMES TAKE A STATIC SET CAUSING SLIGHT LEAKAGE BETWEEN THE ACTUATOR PISTON AND SEALS. ONCE THE ACTUATOR IS CYCLED, THE SEALS RESET AND NO LEAKAGE IS DETECTED. ACCOMPLISHED AN EN GINE RUN, NO LEAKAGE DETECTED. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999041700370 19990417 00370 NM 1999 4 17 99UAL900187 1 19990401 A 2530 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY DIRTY A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 611UA 21872 FORWARD GALLEY OVEN 401, RIGHT SIDE OVEN SMOKING/SPARKING. CAPTAIN ADVISED TO PULL CB. OVEN REPLACED IN SFO ON 02APR99 . SHOP FINDINGS ON REMOVED OVEN MR25350-170 FOUND IT TO BE EXTREMELY DIRTY ESPECIALLY BEHIND THE SIDE AND REAR BAFFLE P LATES. THIS CAUSED THE RESIDUE TO SMOKE AT HIGH TEMPS. 2 L 7 2 4F 4 F RT A1NM E3NE 1999041700371 19990417 00371 NM 1999 4 17 99UAL900188 1 19990402 A 5270 SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 661UA 27158 ON CLIMBOUT, FORWARD CARGO WARNING LIGHT AND EICAS MESSAGE SHOWN. DIVERTED LHR. *S/D* ACCOMPLISHED DOOR SENSOR CHECKS PER MM AND FOUND SENSOR S215 OUT OF RANGE. RESHIMMED PER MM. ACCOMPLISHED PSEU BITE CHECK AND ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999041700372 19990417 00372 NM 1999 4 17 99UAL900189 1 19990402 A 7830 TR UNIT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE MALFUNCTIONED A UALA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 668UA 30024 ON LANDING ROLL, LEFT ENGINE STAYED IN REVERSE, HAD GREEN REV ON EICAS. SHUTDOWN ENGINE FOR TAXI. REVERSER DEPLOYS WIT H REVERSER HANDLE. WHEN HANDLE STOWED, REVERSER GREEN LIGHT STAYS ON INDEFINITELY. MOVING THRUST LEVER TO FORWARD THRU ST STOWS REVERSER IMMEDIATELY. 2 L 7 2 4F 4 F RT A1NM E24NE 1999041700373 19990417 00373 NM 1999 4 17 99UAL900190 1 19990402 A 3020 59T473 HOSE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ENGINE LOSE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 776UA 26937 EICAS ANTI-ICE R ON TAKEOFF ROLL WITH ENG ANTI-ICE SELECTED TO ON. AIRCRAFT RETURNED TO BLOCKS. *S/D* MAINTENANCE FOU ND EAI (ENGINE ANTI- ICE) VALVE MUSCLE LINE (59T473) B-NUT DISCONNECTED AT 6:00 POSITION. SECURE SAME. ALSO REPLACED P RESSURE SENSOR AS PRECAUTIONARY. PERFORMED HIGH POWER ENGINE RUN CHECK. ALL EAI VALVE INDICATIONS NOW NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999041700374 19990417 00374 NM 1999 4 17 99UAL900191 1 19990405 A 5754 651622294 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 6 LE SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7457U 21911 NR 6 SLAT HAS CRACK APPROXIMATELY 5 INCHES LONG. REPLACED SLAT PER 727 MM 27-81-03. 2 L 7 3 4F 4 F A3WE E2EA 1999041700376 19990417 00376 NM 1999 4 17 99UAL900194 1 19990328 A 7603 PULLEY BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 THROTTLE DIRTY A UALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 29 156UA 20105 AFTER ARRIVAL, NR 2 THROTTLE EXCESSIVELY STIFF. FOUND DEBRIS AT PULLEY TOP OF THE NR 2 PYLON. CLEANED DEBRIS AND OPS C HECKED OK. 2 L 7 4 4F 4 F A20WE E20EA 1999041700377 19990417 00377 NE 1999 4 17 99UAL900195 2 19990406 A 7230 BLADES BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COMPRESSOR DAMAGED A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 608UA 21869 707516 NUMBER 2 ENG COMPRESSOR STALLED IN FLIGHT. ENG RECOVERED AND CONTINUED OPERATING. IMMEDIATELY PRECEDING STALL, ENG POW ER WAS STEADY HIGH POWER (CRUISE OR CLIMB). *S/D* PERFORMED BORESCOPE INSPECTION ON NR 2 ENGINE AND FOUND 6TH, 8TH AND 9TH STG COMPRESSOR BLADES DAMAGED PER MM. REPLACED NR 2 ENGINE. REPLACED ENGINE AS PER MM. 2 L 7 2 4F 4 F RT A1NM E3NE 1999041700378 19990417 00378 NE 1999 4 17 99UAL900196 2 19990408 A 7261 OIL PUMP PWA 515107MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A UALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7270U RM1125 21417 649135 AT 23,000 FEET NR 2 ENGINE OIL SHOWED 1 GALLON. CONTINUED TO DECREASE TO ALMOST ZERO OIL. OIL TEMPERATURE WAS 114 DEGR EES. PULLED THROTTLE BACK AND OIL TEMPERATURE RACED INTO THE YELLOW ARC AND OIL PRESSURE STABILIZED AT 47 PSI. SHUT EN GINE DOWN IN FLIGHT. WIND MILLED FOR 25 MINUTES. *S/D* BEARING BORE WEAR, .039 ON THE MAIN OIL PUMP INNER COVER ALLO WED OIL FROM THE HIGH PRESSURE PUMP SECTION TO MIGRATE TO THE GEARBOX. THE EXCESS OIL INTRODUCED TO THE GEARBOX WAS SPI LLED OVERBOARD BY THE DEOILER CAUSING OIL STARVATION IN THE TANK. THE ENGINE WAS REPLACED BEFORE THE AIRCRAFT RETURNED TO SERVICE, AND THE MAIN OIL PUMP IS UNDER ANALYSIS TO AVOID A RECURRENCE. 2 L 7 3 4F 4 F A3WE E2EA 1999041700379 19990417 00379 NM 1999 4 17 99UAL900197 1 19990408 A 2933 019012003 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD QUANTITY FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 501UA 24622 AIRCRAFT RETURNED TO EWR UNDER AMBER ALERT DUE TO CENTER HYDRAULIC QUANTITY EICAS MESSAGE. *S/D* THE C HYD QTY EICAS M ESSAGE APPEARED AND QUANTITY SHOWED .38. SYSTEM AND PUMP LOW PRESSURE LIGHTS DID NOT COME ON. HYD QUANTITY WAS VERIFIE D FULL AFTER LANDING. PIN NR 3 ON CENTER QUANTITY TRANSMITTER WAS FOUND PUSHED BACK. TRANSMITTER REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999041700380 19990417 00380 NM 1999 4 17 99UAL900198 1 19990407 A 3350 EMERGENCY LIGHTS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT MISWIRED A UALA K NONE W INADEQUATE Q C UK UNKNOWN 1 WP 29 7288U 21566 THE EMERGENCY LIGHTS UNDER THE GLARE SHIELD ARE ON. LIGHTS ARE TIED INTO THE PILOTS BACKGROUND LIGHTS. RELAMPED BACKGRO UND LIGHTS AND CORRECTED EMERGENCY LIGHT MISWIRE. 2 L 7 3 4F 4 F A3WE E2EA 1999041700381 19990417 00381 NE 1999 4 17 99UAL900199 2 19990408 A 7314 FUEL PUMP ARGO TECH IN MR73111 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT ENGINE LOOSE A UALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 29 908UA 17897 25008 724463 RIGHT ENGINE FUEL LEAK. *S/D* THE MAIN FUEL PUMP FILTER COVER WAS PULLED BACK FROM THE HOUSING. FOUR OF THE SIX FUEL FILTER COVER ATTACH BOLTS WERE FOUND BACKED FROM THE PUMP HOUSING. RIGHT ENGINE WAS REPLACED, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999041700382 19990417 00382 WP 1999 4 17 MWEA99143 1 19990413 A 5320 3915134517N FITTING DOUG DC9 DC932 3022066 WP BS 756 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE RIGHT KEEL AT STATION 756 BATHTUB FITTING HAS A HEAVY CORROSION. MTC FABRICATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999041700383 19990417 00383 NM 1999 4 17 MWEA99144 1 19990404 A 5230 59101419 PAN DOUG MD88 MD88 3023688 NM CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE AFT EDGE OF AFT BAG PIT DOOR INNER PAN EDGE IS CHAFED AT TORQUE TUBE AREA. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 1999041700384 19990417 00384 NM 1999 4 17 MWEA99145 1 19990404 A 5230 59101419 PAN DOUG MD88 MD88 3023688 NM CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE AFT BAG PIT DOOR INNER PAN IS CHAFED AT TORQUE TUBE ON FORWARD SIDE OF DOOR. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 1999041700385 19990417 00385 NM 1999 4 17 USAASB99071 1 19990315 A 3350 1012621 LIGHT BOEING 737 7373B7 1384580 NM ROW 10 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAINTENANCE FOUND THE FLOOR EMERGENCY LIGHTS AT SEAT ROW 10 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIG HT ASSEMBLY AT SEAT ROW 10. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999041700386 19990417 00386 WP 1999 4 17 AALA990337 1 19990311 A 2170 1808492 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 297AA 49309 DFW - FLT 1274 - AFTER TAKEOFF LAS, A STRONG ODOR AND LIGHT SMOKE WAS REPORTED BY FLIGHT ATTENDANT. ODOR AND SMOKE DISS IPATED WHILE CLIMBING TO FL 15,000. FLIGHT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND COA LESCER BAGS DIRTY. MAINTENANCE REPLACED COALESCER BAGS AND PERFORMED PACK BURNOUT. AFTER BURNOUT WAS ACCOMPLISHED, COA LESCER BAGS WERE REPLACED AS A PRECAUTIONARY. PACKS WERE OPERATED WITH NO LEAKS, ODOR, OR SMOKE NOTED. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700387 19990417 00387 WP 1999 4 17 AALA990321 1 19990311 A 2560 39522732 LATCH DOUG DC9 DC983 3022083 WP GALLEY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 571AA 49353 ORD - FLT 2326 - DURING MAINTENANCE, AFT GALLEY DOOR GIRT BAR LATCH IS BROKEN. MAINTENANCE REPLACED AFT GALLEY DOOR GIR BAR LATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999041700388 19990417 00388 WP 1999 4 17 AALA990319 1 19990308 A 2130 FLOW LIGHT DOUG DC9 DC982 3022082 WP PRESS SYSTEM ILLUMINATED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 70404 49315 CLE - FLT 772 - DURING CRUISE AT FL38, AIRCRAFT REPRESSURIZATION FLOW LIGHT ILLUMINATED. AIRCRAFT AIR INTERRUPTED AND L ANDED CLE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED CABIN PRESSURE CONTROL BITE TEST WITH NO FAULT. DUCT WORK WA S INSPECTED WITH NO SIGNS OF LEAKS. UNABLE TO DUPLICATE FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700389 19990417 00389 WP 1999 4 17 AALA990292 1 19990227 A 2130 1500P0228 SWITCH DOUG DC9 DC982 3022082 WP E/E COMPT DEFECTIVE A AALA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 07 70425 49337 DFW - FLT 1946 - DURING CRUISE AT FL370, BOTH PACKS FAILED AT THE SAME TIME. CREW INITIATED AN EMERGENCY DESCENT AND DE PLOYED OXYGEN MASKS. AT FL100 THE AIRCRAFT LEVELED OFF AND THE RIGHT PACK STARTED WORKING AGAIN. LEFT PACK WAS CYCLED AND STARTED TO WORK AGAIN. FLIGHT REMAINED AT FL100 FOR THE REMAINDER OF THE FLIGHT WITH PACKS OPERATING NORMALLY. AIR CRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT AND LEFT PACK AUTO SHUTOFF RELAYS TO BE FAULTY. REP LACED RIGHT AND LEFT PACK AUTO SHUTOFF RELAYS AND AS A PRECAUTIONARY, REPLACED ENGINE DIFFERENTIAL PRESSURE SWITCHES. A IRCRAFT WAS FLOW ON A FUNCTIONAL FLIGHT TEST AND THE SYSTEM OPERATED NORMALLY. SYSTEM GROUND CHECKED NORMALY OPERATION. 2 L 7 2 4F A6WE 1999041700390 19990417 00390 WP 1999 4 17 AALA990283 1 19990225 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 275AA 49272 DFW - FLT 1004 - EN ROUTE DFW-BDL, AFTER TAKEOFF, THE NOSE GEAR RED LIGHT STAYED ILLUMINATED AFTER RAISING THE GEAR HAND LE. WHEN AIRCRAFT WAS AT 320 KNOTS A VERY LOUD AIR NOISE ABRUPTLY STARTED AT THE NOSE WHEEL AREA. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR UPLOCK SENSOR, CYCLED LANDING GEAR SEVERAL TIMES. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700391 19990417 00391 WP 1999 4 17 AALA990267 1 19990223 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 484AA 49677 DFW - FLT 1900 - EN ROUTE SLC-DFW - AFTER TAKEOFF AND PLACING HYDRAULIC PUMPS TO LOW SETTING THE RED NOSE GEAR ANNUNCIAT OR LIGHT ILLUMINATED. AIRCRAFT SLOWED AND PLACED HYDRAULIC PUMPS TO HIGH AND CYCLED GEAR. AFTER HYDRAULC PUMPS WERE RE PLACED TO LOW AGAIN ALL GEAR INDICATOR LIGHTS REMAINED EXTINGUISHED. LANDED DFW WITHOUT INCIDENT. REPLACE NOSE GEAR UP SENSOR AND CYCLED LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700392 19990417 00392 WP 1999 4 17 AALA990266 1 19990223 A 2612 59585701 SUPPORT DOUG DC9 DC983 3022083 WP RT ENG FIRE DET DEFECTIVE A AALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 563AA 49345 MIA - FLT 1453 - EN ROUTE MIA-AUS - DURNIG CRUISE AT 35,000 FEET, RECEIVED A RIGHT ENGINE FIRE WARNING. ENGINE PARAMETE RS APPEARED NORMAL. ACCOMPLISHED EMERGENCY PROCEDURES. BOTH FIRE BOTTLES WERE DISCHARGED. LIGHT EXTINGUISHED BRIEFLY, THEN CAME BACK ON FOR REMAINDER OF FLIGHT. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT ENGINE FIRE DETEC TOR AMP AND ENGINE FIRE DETECTOR SUPPORT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999041700393 19990417 00393 WP 1999 4 17 AALA990317 1 19990310 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 262AA 49290 DFW - FLT 1215 - DURING CRUISE, THE RED NOSE GEAR LIGHT ILLUMINATED. THERE WAS NO VIBRATION OR AIR NOISE, FLIGHT CONTIN UED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED UP/DOWNLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700394 19990417 00394 WP 1999 4 17 AALA990253 1 19990219 A 2530 2510000308 OVEN DOUG DC9 DC982 3022082 WP GALLEY SMOKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 436AA 91070508 49454 BOS - FLT 449 - EN ROUTE BOS-MIA, DURING CLIMB-OUT FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN CABIN. SMOKE STARTED IN BAC K OF THE AIRCRAFT AND WORKED FORWARD, THEN SMOKE DISSIPATED. AIRCRAFT RETURNED BOTH AND LANDED WITHOUT INCIDENT. INSPE CTED APU AREA FOR OIL LEAKS, ENGINE INLETS AND EXHAUSTS, AND BOTH ENGINE CROSSOVER DUCTS. NO EVIDENCE OF OIL LEAKS NOTE D. CHECKED RECIRCULATION FAN AND FILTERS, CHECKED GALLEY OVENS OPERATION AND FOR RESIDUE. NO FAULTS FOUND, FLIGHT ODOR FROM NR 3 OVEN. PRECAUTIONARY REPLACED WATER SEPARATOR COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT PER MM. PRECAUTIO NARY REPLACED NR 3 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700395 19990417 00395 NM 1999 4 17 AALA990286 1 19990227 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 850AA 20991 DFW - DURING OVERNIGHT MAINTENANCE, THREE LIGHT SEGMENTS IN THE AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERAT IVE. REPLACED EMERGENCY FLOOR PATH LIGHT STRIPS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999041700396 19990417 00396 NM 1999 4 17 AALA990287 1 19990227 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 859AA 21086 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT JUMPER WIRE BETWEEN COACH AND FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999041700397 19990417 00397 NM 1999 4 17 AALA990281 1 19990226 A 3260 AAP2448A ACCESSORY UNIT BOEING 727 727223 1384074 NM E/E COMPARTMENT DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 867AA M00544 21372 DFW - FLT 535 - EN ROUTE TUL-DFW - DURING GEAR RETRACTION, UNABLE TO RAISE GEAR HANDLE FROM OFF TO UP WITHOUT PULLING OV ERRIDE TRIGGER. LEVER LATCH CIRCUIT BREAKER ON P6-3 WAS NORMAL. GEAR EXTENSION WAS NORMAL. AL OTHER SYSTEMS NORMAL. L ANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT. PERFORMED OPERATIONS CHECK PER MM. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999041700398 19990417 00398 WP 1999 4 17 AALA990255 1 19990219 A 3233 39281375001 ACTUATOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 70524 3355 49916 DFW - FLT 2213 - EN ROUTE - ORD-DFW - AFTER TAKEOFF AND RETRACTING GEAR, RED NOSE GEAR LIGHT STAYED ILLUMINATED. ALL O THER INDICATIONS WERE THAT THE NOSE GEAR WAS RETRACTED. LIGHT STAYED ILLUMINATED UNTIL LEVELING AT 11,000 FEET. ON DES CENT, GOT THREE RED GEAR LIGHTS AFTER RETARDING THE THROTTLES. WHEN THROTTLES ADVANCED ON LEVEL OFF RED NOSE GEAR LIGHT EXTINGUISHED. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACTION EXTENSION ACTUATOR AND PERFORMED ALL REQUIRED CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700399 19990417 00399 WP 1999 4 17 AALA990310 1 19990305 A 3350 LIGHT DOUG DC9 DC982 3022082 WP GALLEY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445AA 49471 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT FORWARD GALLEY WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999041700400 19990417 00400 NM 1999 4 17 AALA990265 1 19990222 A 2121 6054578 FAN DOUG MD11 MD11 3023602 NM ACM BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1756 708589 48491 ANC - FLT 157 - EN ROUTE DFW-KIX - CREW NOTED AN ELECTRICAL SMELL IN CABIN CABIN. CREW DECLARED AN EMERGENCY AND AIR IN TERRUPTED. LANDED ANC WITHOUT INCIDENT. REPLACED NR 2 RECIRCULATING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999041700401 19990417 00401 NM 1999 4 17 AALA990276 1 19990223 A 2497 WIRE DOUG MD11 MD11 3023602 NM CARGO BAY CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 ORD - FLT 0154 - DURING OVERNIGHT MAINTENANCE, AIRCRAFT WOULD NOT ACCEPT ELECTRICAL POWER OF ANY KIND. FOUND WIRE BURNE D AND SHORTED IN THE FORWARD CARGO BAY LEFT SIDE JUST AFT OF DOOR OPENING. MAINTENANCE REPLACED AND REPAIRED WIRING ACC ORDING TO ESTABLISHED PROCEDURES. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999041700402 19990417 00402 NM 1999 4 17 AALA990296 1 19990301 A 3610 32146451 VALVE BOEING 727 727223 1384074 NM NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 713AA 1079379 22469 MIA - FLT 2115 - DURING CLIMB-OUT, NR 1 BLEED OVER PRESSURE LIGHT ILLUMINATED. CREW RAN CHECKLIST AND AIR INTERRUPTED, RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 1 ENGINE BLEED VALVE DEFECTIVE. REPLACED NR 1 ENGINE BLEED VALVE AND ENGINE RUN INDICATED NO LEAKS WITH SYSTEM OPERATING NORMALLY. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 3 4F A3WE 1999041700403 19990417 00403 NM 1999 4 17 USAABB99014 1 19990315 A 3350 FUSE BOEING 767 7672B7 1385107 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 653US 24894 PHL - FOUND LEFT MID SECTION EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE BATTERY PACK, WHICH THEN FAILED AGAIN. UPON FURTHER INVESTIGATION, FOUND A WIRE SHORTED TO SEAT 13AB. THE WIRE WAS REPAIRED. (M) 2 L 7 2 4F RT A1NM 1999041700404 19990417 00404 NM 1999 4 17 USAA990178 1 19990308 A 5330 SKIN BOEING 737 737401 1384701 NM BS 867-887 DISTORTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SKIN DISTORTED ON FUSELAGE BETWEEN STATION 867 TO 887 BETWEEN STRINGER 2 2R TO 23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700405 19990417 00405 NM 1999 4 17 USAA990177 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 787 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700406 19990417 00406 NM 1999 4 17 USAA990176 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700407 19990417 00407 NM 1999 4 17 USAA990175 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 867L BETWEEN S8L AND 9L FRAME. INSTALLED DOUBL ER PER EA 63838A AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700408 19990417 00408 NM 1999 4 17 USAA990174 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 827 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700409 19990417 00409 NM 1999 4 17 USAA990173 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 747 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700410 19990417 00410 NM 1999 4 17 USAA990172 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 747L BETWEEN S8L AND 9L FRAME. INSTALLED DOUBL ER PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700411 19990417 00411 NM 1999 4 17 USAA990171 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 727F BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLE R PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700412 19990417 00412 NM 1999 4 17 USAA990170 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 727B BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLE R PER EA 63838A AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700413 19990417 00413 NM 1999 4 17 USAA990169 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500D BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLE R PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700414 19990417 00414 NM 1999 4 17 USAA990168 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500A BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLE R PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700415 19990417 00415 NM 1999 4 17 USAA990167 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 500A BETWEEN S8L AND 9L. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700416 19990417 00416 NM 1999 4 17 USAA990166 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 480 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700417 19990417 00417 NM 1999 4 17 USAA990165 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 440 BETWEEN S8R AND 9R FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700418 19990417 00418 NM 1999 4 17 USAA990164 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 400 BETWEEN S8L AND 9L FRAME. INSTALLED DOUBLER PER EA 63838A AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700419 19990417 00419 NM 1999 4 17 USAA990143 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN S8R AND 9R. INSTALLED DOUBLER PER E A 63838A AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999041700420 19990417 00420 NM 1999 4 17 USAA990142 1 19990308 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN S8L AND 9L. INSTALLED DOUBLER PER E A 63838A AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700421 19990417 00421 NM 1999 4 17 USAA990138 1 19990308 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .5 BY .5 INCH AT BS 967 RBL 18 FLOORBEAM, CORROSION TASK NR C5 3-107-02. INSTALLED 'T' CAP WITH REPAIR ANGLES PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999041700422 19990417 00422 NM 1999 4 17 USAA990136 1 19990308 A 5320 BEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH STATION 312 LBL 11 BEAM. REPAIRED PER SRM 53 -10-51. (M) 2 L 7 2 4F RT A16WE 1999041700423 19990417 00423 NM 1999 4 17 USAA990137 1 19990308 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .5 BY .5 INCH AT BS 947 LBL 15 RBL 15 AROUND NUT PLATE HOLES FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED 'T' CAP WITH REPAIR ANGLES PER SRM 53-00-5 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999041700424 19990417 00424 SO 1999 4 17 ASOA99001 1 19990102 A 3610 CLAMP EMB 120 EMB120RT SO RT ENGINE LOOSE A ASOA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 11 285AS 16186 120265 FLT 4831 - CRP-DFW - WHILE LEVEL AT 6,000 FEET ON DESCENT INTO DFW, RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED, FOLLOWED B Y AURAL WARNING. CREW C/W DUCT LEAK EMERGENCY CHECKLIST, AND WHEN AFTER 3 MINUTES LIGHT WAS STILL ILLUMINATED, SHUT DOW N THE RT ENGINE. CREW DECLARED AN EMERGENCY AND PERFORMED A SINGLE ENGINE LANDING AT DFW SAFELY AND WITHOUT FURTHER INC IDENT. DFW MAINTENANCE FOUND RIGHT ENGINE DEICE PRESSURE REGULATING VALVE BLEED LINE CLAMP LOOSE AND SECURED CLAMP. OP ERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999041700425 19990417 00425 SO 1999 4 17 ASOA99013 1 19990119 A 5230 12023120003 SEAL EMB 120 EMB120RT SO CARGO DOOR DETACHED A ASOA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 SO 11 286AS 120268 FLT 4067 - EN ROUTE ATL-CRW, LOST PRESSURIZATION AT 25,000 FEET AND PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. OXYG EN MASKS WERE DEPLOYED IN THE CABIN. LANDING WAS MADE SAFELY AT CRW WITHOUT FURTHER INCIDENT. LOCAL MTC FOUND CARGO DO OR SEAL DETACHED FROM LOWER FORWARD CORNER OF DOOR AND RESECURED SEAL, ALSO RESTOWED THE OXYGEN MASKS. FOLLOWUP INSPECT ION BY ATL MTC DETERMINED THAT THE FORWARD LOWER SECTION OF THE CARGO DOOR SEAL RETAINER WAS FAULTY AND REPLACED THE RET AINER. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999041700426 19990417 00426 NE 1999 4 17 ASOA99014S 2 19990123 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN A FLAME/FIRE CR CRUISE 1 SO 11 130AM 21339 120134 FLT 4825 - EN ROUTE DFW-AMA, A LOUD BANG WAS HEARD FOLLOWED BY AIRCRAFT VIBRATION, SMOKE IN CABIN AND COCKPIT, AND REDUC ED POWER IN LEFT ENGINE (20 PERCENT TORQUE). CREW FOLLOWED THE ENGINE FAILURE CHECKLIST, DECLARED AN EMERGENCY AND DIVE RTED TO SPS WHERE SINGLE ENGINE LANDING WAS MADE SAFELY WITHOUT FURTHER INCIDENT. PAX AND F/A NOTICED SPARKS AND FLAME FROM ENGINE JUST PRIOR TO 'BANG'. DFW AND TXK MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LEFT ENGINE. OPS AND LEAK CHECKS WERE GOOD AND THE A/C WAS RELEASED FOR FURTHER SERVICE. TEARDOWN REPORT INDICATES THERMAL DISTRESS TO THE HP VA NES LEAD TO MATERIAL BEING RELEASED TO FLOW DOWNSTREAM. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999041700427 19990417 00427 CE 1999 4 17 99ZZZM235 1 19990308 A 3230 993880071R SENSOR BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 190GA 800A UB1 FLT 9149 - FPO-FLL, LANDING GEAR WILL NOT EXTEND HAD TO MANUALLY EXTEND GEAR. REPLACED HYDRAULIC LOW LEVEL SWITCH. PER FORMED LANDING GEAR EXTENSION/RETRACTION CHECK. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 1999041700428 19990417 00428 CE 1999 4 17 99ZZZM236 1 19990219 A 3230 571302 POWER PACK BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 199GA 611A UB13 FLT 9332 - EYW-TPA - LANDING GEAR CIRCUIT BREAKER POPPED IN FLIGHT. RESET AND POPPED AGAIN. EXTENDED GEAR VIA ALTERNAT E GEAR EXTENSION PROCEDURES. REPLACED POWER PACK MOTOR. PERFORMED SATISFACTORY LANDING GEAR RETRACTION/EXTENSION CHECK S. (M) 2 L 7 2 4T RT A24CE 1999041700429 19990417 00429 CE 1999 4 17 99ZZZM237 1 19990310 A 2612 FIRE LIGHT BEECH 1900 1900C 1154161 CE LEFT ENGINE ILLUMINATED A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 86UE UC86 FLT 9376 - MIA-FLL - LEFT FIREWALL FUEL VALVE ILLUMINATED ON TAXIWAY IN MIA. NO SMOKE OR FLAMES OBSERVED BUT HANDLE STA YED LIT UNITL BATTERY TURNED OFF. INSPECTED LEFT ENGINE FIRE LOOP FOR CHAFING OR LOOSE CONNECTIONS. NO DEFECTS NOTED. GROUND RUN LEFT ENGINE AND OBSERVED NO FIRE ALERT INDICATIONS. (M) 2 L 7 2 4T RT A24CE 1999041700430 19990417 00430 CE 1999 4 17 99ZZZM238 1 19990305 A 3230 16001260 CIRCUIT BREAKER BEECH 1900 1900C 1154161 CE LANDING GEAR TRIPPED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 105GL UC105 FLT 9233 - FLL-EYW - LANDING GEAR WOULD NTO GO DOWN. HAD TO PUMP DOWN. INSPECTED SYSTEM. FOUND 60 AMP CIRCUIT BREAKER IN LEFT NACELLE TO BE TRIPPED. RESET CIRCUIT BREAKER. PERFORMED SEVERAL SATISFACTORY RETRACTION CHECKS. (M) 2 L 7 2 4T RT A24CE 1999041700432 19990417 00432 WP 1999 4 17 ORJA99123 1 19990321 A 3350 BR9661115 POWER PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 878RA 53184 SJC - RIGHT SIDE FORWARD EMERGENCY POWER PACK INOPERATIVE. REMOVED AND REPLACED RIGHT SIDE EMERGENCY POWER PACK, FORWAR D. (M) 2 L 7 2 4F RT A6WE 1999041700433 19990417 00433 WP 1999 4 17 ORJA99118 1 19990320 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 LAS - LAST SECTINO OF EMERGENCY LIGHTS CAME ON IN CRUISE. REMOVED AND REPLACED LEFT MAIN BATTERY CHARGER, SYSTEM OPS CH ECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999041700434 19990417 00434 WP 1999 4 17 ORJA99119 1 19990319 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 IN SJC - EMERGENCY LIGHT INOPERATIVE AT SEAT 11. REPAIRED AND REPLACED BATTERY PACK AND REPAIRED BROKEN WIRE IAW MM, OP S CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999041700435 19990417 00435 WP 1999 4 17 ORJA99121 1 19990320 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 2D BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 823RA 49889 IN SJC - EMERGENCY LIGHT INOPERATIVE AT SEAT 2D. REPAIRED GROUND WIRE REPAIRED BROKEN WIRE, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999041700436 19990417 00436 WP 1999 4 17 ORJA99120 1 19990319 A 3350 BR9687100 CHARGER DOUG DC9 DC983 3022083 WP EMER EXIT INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO, OVERWING EMERGENCY LIGHT ON THE SEATS INOPERATIVE. REPLACED EMERGENCY LIGHT CHARGER, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999041700437 19990417 00437 NM 1999 4 17 ORJA99117 1 19990312 A 3350 TERMINAL DOUG MD90 MD9030 3023690 NM ROW 7 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 902RA 53490 IN SJC, OVERHEAD CEILING EMERGENCY LIGHTS OUT FROM ROWS 7 TO AFT CABIN. FOUND BROKEN TERMINAL AT 33-550 NR 11. REPAIRE D AND SECURED, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999041700439 19990417 00439 WP 1999 4 17 ORJA99114 1 19990316 A 3350 BR9661116 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 12-16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO - EMERGENCY EXIT PATH LIGHTS WILL NOT ILLUMINATE AT ROWS 12-16 WILL NOT EXTINGUISH AT ROWS 17-20. REMOVED AND RE PLACED OVERWING AND AFT BATTERY PACKS OPS CHECK GOOD WORK DONE IAW BRUCE IND 400-079. (M) 2 L 7 2 4F RT A6WE 1999041700440 19990417 00440 WP 1999 4 17 ORJA99109 1 19990309 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC983 3022083 WP ROWS 11-14 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 RNO - EMERGENCY LIGHTS AT ROWS 11-14 INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER FOR EMERGENCY LIGHT AT ROWS 11-1 4. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999041700441 19990417 00441 1999 4 17 HALA9900087 4 19990322 A 3442 RADAR INDICATOR DOUG DC10 DC1030 3023501 WP RT COCKPIT FAILED A HALA K NONE A FLAME/FIRE CR CRUISE 1 WP 13 141AA 46713 FLT 5 - HNL - RADAR/TCAS, F/O SIDE, A SPARK ARCED BETWEEN THE LOWER INST PANEL EYEBALL AIR OUTLET AND RADAR/TCAS DISPLAY UNIT. THE LOUD ARCING SOUNDS WAS 1 TO 2 SEC, AND LOOKED WHITE OR YELLOW. THEN 3 HOURS INTO THE FLIGHT AT 2100 HOURS I T ARCED 2 MORE TIMES IN QUICK SPACES. PULLED C/B D-29 ABOVE F/E. FIRST ARC WAS ABOUT 1/2 HR INTO FLIGHT. REPLACED THE F/O'S RADAR INDICATOR. THE GROUND CHECK WAS OK ON TEST AND THE TCAS SYSTEM TESTED OK. (M) 2 L 7 3 4F A22WE 1999041700442 19990417 00442 EU 1999 4 17 RAIA990330 1 19990322 A 3340 4553 BULB BAG JETSTM JETSTM3201 1500217 EU LANDING LIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 879 FLT 7496 - STL - SECOND LANDING LIGHT BURNED OUT. MAINTENANCE REPLACED LANDING LIGHT BULB. (M) 2 L 7 2 4T RT A56EU 1999041700443 19990417 00443 WP 1999 4 17 RAIA990331 2 19990302 A 7310 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 426AM 874 FLT 7332 - STL - RIGHT ENGINE TORQUE FLUCTUATING AND SRL CAP ILLUMINATED. MAINTENANCE REPLACED RIGHT ENGINE FUEL BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999041700444 19990417 00444 EU 1999 4 17 RAIA990332 1 19990322 A 7331 TNAS1024L1182 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33114 01514 NE LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 860AE 860 66195R FLT 4793 - SBN - FUEL FLOW GAUGE AND FULL COUNTER ON NR 1 ENGINE INOPERATIVE. MAINTENANCE REPLACED FUEL FLOW TRANSMITTE R ON LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E18NE 1999041700445 19990417 00445 1999 4 17 RAIA990333 4 19990322 A 3442 MI5853505 RT UNIT AEROSP ATR42 ATR42300 8680920 EU RADAR FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 423TE 21359 119 RADAR INOPERATIVE. MAINTENANCE REPLACED RADAR R/T. (M) 2 H 7 2 4T RT A53EU 1999041700446 19990417 00446 EU 1999 4 17 RAIA990335 1 19990223 A 5320 BRACKET BAG JETSTM JETSTM3201 1500217 EU NLG WW CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 339TE 935 STL - DURING ROUTINE MAINTENANCE, FOUND CRACKS IN NOSE LANDING GEAR BAY ON LEFT SIDE. MAINTENANCE REPAIRED DAMAGE IAW E O NR J3200-53-012-1. (M) 2 L 7 2 4T RT A56EU 1999041700447 19990417 00447 EU 1999 4 17 RAIA990336 1 19990323 A 5320 DOUBLER BAG JETSTM JETSTM3201 1500217 EU FUSELAGE CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 339TE 935 STL - DURING ROUTINE MAINTENANCE LOWERED A/C OFF JACKS WITHOUT REMOVING TAIL STAND. MAINTENANCE REPAIRED DAMAGE IAW NR J3200-53-013-1. (M) 2 L 7 2 4T RT A56EU 1999041700448 19990417 00448 SO 1999 4 17 RAIA990334 1 19990317 A 3250 7287103503 CONTROL VALVE EMB 145 EMB145 SO NLG STEERING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 801HK 145053 FLT 5791 - ROA - NOSE WHEEL STEERING SYSTEM INOPERATIVE. MAINTENANCE REPLACED STEERING CONTROL VALVE. (M) 2 L 7 2 4F RT T00011AT 1999041700449 19990417 00449 EU 1999 4 17 RAIA990326 1 19990318 A 2435 8260121 STARTER GEN AEROSP ATR42 ATR42300 8680920 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 422TE 17190 106 FLT 7120 - STL - STRONG ODOR FROM FORWARD CARGO. MAINTENANCE REPLACED RIGHT ENGINE STARTER/GENERATOR. (M) 2 H 7 2 4T RT A53EU 1999041700450 19990417 00450 EU 1999 4 17 RAIA990327 1 19990318 A 3243 ACM26810 MASTER CYLINDER BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 428AM 877 FLT 7100 - STL - CAPTAINS LEFT BRAKE WEAK. MAINTENANCE SERVICED CAPTAINS LEFT BRAKE MASTER CYLINDER. (M) 2 L 7 2 4T RT A56EU 1999041700451 19990417 00451 WP 1999 4 17 USAA990249 1 19990308 A 5320 49157601 PAN DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 929VJ 50924 48118 PIT - DURING RON VISIT FOUND .25 INCH TO .375 INCH HOLE IN SERVICE DOOR HOLD OPEN PAN ASSEMBLY RIGHT SIDE OF FUSELAGE. I NSTALLED NEW PAN ASSEMBLY PER EA 51678. (M) 2 L 7 2 4F A6WE 1999041700452 19990417 00452 NE 1999 4 17 USAAD99047 2 19990306 A 7250 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE DAMAGED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 830US 49443 708454 BDL-PIT - FLT 1147 - AFTER TAKEOFF AND CLIMBING THROUGH 26,000 FT, THE AIRCRAFT BEGAN TO VIBRATE. THE RIGHT ENGINE N1 I NCREASED 6 PERCENT AND A SHUDDER WAS FELT IN THE COCKPIT. SHORTLY THEREAFTER ALL WAS NORMAL. WHEN THE AIRCRAFT LEVELED AT 28,000 FT THE SAME INDICATIONS OCCURRED. THE AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOU ND 10 BENT FAN BLADES ON THE RIGHT ENGINE. THE FIRST STAGE FAN WAS REPLACED. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999041700453 19990417 00453 EU 1999 4 17 USAASB99079 2 19990321 A 7200 ENGINE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU LEFT FAILED A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 392US 33642 23314 721444 CLT - FLT 858 - FLIGHT RETURNED TO FIELD AT CLT DUE TO A 6 INCH THROTTLE SPLIT AND A NR 1 EGINE OVERTEMP. DURING TAKEOF F ROLL, THE CREW GOT THE THROTTLE SPLIT AS THEY APPROACHDED TAKEOFF SPEED. CREW CONTINUED THE TAKEOFF BECAUSE THEY HAD GOOD TAKEOFF POWER. DURING CLIMB, THEY RECEIVED THE OVERTEMP AND TEH THROTTLE SPLIT REMAINED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE A SSEMBLY. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1999041700454 19990417 00454 NM 1999 4 17 TWRA9912 1 19990329 A 5220 65B10360505 HATCH ASSY BOEING 747 747121 1384871 NM COCKPIT LOOSE A TWRA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 15 617FF 19650 ON TAKEOFF COCKPIT ESCAPE HATCH ASSY CAME OUT OF CLOSE AND LOCKED POSITION UNABLE TO RECLOSE IN FLIGHT. INSPECTED DOOR, NO DAMAGE FOUND. (M) 2 L 7 4 4F A20WE 1999041700455 19990417 00455 NM 1999 4 17 TWRA9913 1 19990414 A 2120 BCREF10689 DUCT BOEING 747 747136 1384883 NM COCKPIT LOOSE A TWRA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 EA 15 606FF 20273 DURING FLT CONTROL CHECK WHILE TAXIING, CAPTAINS RIGHT RUDDER PEDAL RESTRICTED FROM FULL TRAVEL. RESECURED INSTR PANEL EQUIPMENT COOLING DUCT BEHIND CAPTAINS RUDDER PEDAL. (M) 2 L 7 4 4F A20WE 1999041700456 19990417 00456 NM 1999 4 17 TWAA9911 1 19990322 A 5743 65B112603 PIN BOEING 747 747130 1384880 NM RT MLG CORRODED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 19746 DURING A CHECK INSPECTION, FOUND THE RIGHT WING GEAR SUPPORT BEAM FITTING PIN FOR BEARING THREADS CORRODED UNDER RETAINE R NUT. REMOVED AND REPLACED BOTH BEARING PIN AND RETAINER NUT. (M) 2 L 7 4 4F A20WE 1999041700457 19990417 00457 NM 1999 4 17 TWRA9910 1 19990322 A 5743 65B0104213 FITTING BOEING 747 747130 1384880 NM RT MLG CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 19746 DURING 'A' CHECK INSPECTION, FOUND THE RIGHT LANDING SUPPORT BEAM END FITTING (FORWARD SIDE) CRACKED. REMOVED AND REPLA CED BOTH FORWARD AND AFT FITTINGS. (M) 2 L 7 4 4F A20WE 1999041700458 19990417 00458 NM 1999 4 17 TWRA9909 1 19990322 A 2710 65B822154 ROD BOEING 747 747130 1384880 NM AILERON CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 19746 DURING 'A' INSPECTION, FOUND THE FORCE LIMITER ROD CONNECTING THE L/R AILERON PROGRAMMER CRACKED (TWO PLACES). REMOVED AND REPLACED ROD ASSY. (M) 2 L 7 4 4F A20WE 1999041700459 19990417 00459 NM 1999 4 17 TSAA9933166 1 19990322 A 3350 8731002511 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999041700460 19990417 00460 NE 1999 4 17 99ZZZM239 2 19990325 A 7200 ENGINE BOEING 727 727134C 138404H NM PWA JT8 JT8D7B 52053 NE NR 1 WORN A RYNA K NONE J WARNING INDICATION IN INSP/MAINT 1 CE 07 424EX 20042 NR 1 ENGINE REQUIRES CHANGE DUE TO A HISTORY OF HIGH OIL CONSUMPTION. REPLACED NR 1 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999041700461 19990417 00461 WP 1999 4 17 99ZZZM240 1 19990315 A 2612 87823902 CONNECTOR LKHEED 1011 10113851 5265010 WP NR 3 ENGINE CORRODED A WRNA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 05 826CR 193A1141 DURING DESCENT FIRE WARNING OCCURRED ON NR 3 ENGINE. ENGINE FIRE DRILL COMPLETED. A/C LANDED WITHOUT INCIDENT. CORREC T ACTION IAW FIM 26-11-00 REG 112. FOUND CORRODED CONNECTOR. FALSE FIRE WARNING, REMOVED AND REPLACED CONNECTOR IAW SR M 20-24-06. OPS CHECK NORMAL. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 1999041700462 19990417 00462 NE 1999 4 17 UIEA9915 2 19990325 A 7310 9068M44G01 MANIFOLD BOEING 747 747230B 1384889 NM GE CF6 CF650C2 30018 NE NR 1 ENGINE CRACKED A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 EA 15 509MC 21221 517675 FLT 322 - BOG/MIA-IFSD - NR 1 ENGINE FUEL FLOW FLUCTUATED ERRATICALLY, NO OTHER ENGINE PROBLEMS. AFTER APPROX 5 MINUTES ENGINE FLAMED UNEVENTFULLY. DECIDED NOT TO ATTEMPT A RELIGHT. CONTINUED TO MIA, DECLARED AND EMERGENCY AND LANDED. D URING TROUBLESHOOTING MAINTENANCE FOUND FUEL MANIFOLD LINE GOING TO P/D VALVE FROM FUEL FLOW TRANSMITTER CRACKED BY FLAN GE WELD. ALSO, FOUND OIL LINE GOING TO GEAR CASE DAMAGED ALONG WITH BRACKET, REF IPC 73-11-01, FIG 1, PAGE OC, ITEM 5, P/N 9068M44G01. REPLACED NR 1 ENGINE, OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 4 4F 4 F A20WE E23EA 1999041700463 19990417 00463 NM 1999 4 17 P2EA99127 1 19990313 A 5314 KEEL BEAM BOEING 737 737222 1384473 NM BS 630 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A SECTION OF THE KEEL BEAM AT BS 630, RBL 5 WAS FOUND WITH CORROSION. THE AREA WAS REPAIRED AS PE R COOPESA EO C00-3-53-176-99 AND BOEING FAX NR COO-SJO-0384RR. (M) 2 L 7 2 4F A16WE 1999041700464 19990417 00464 NM 1999 4 17 P2EA99126 1 19990222 A 7830 SUPPORT BOEING 737 737222 1384473 NM NR 1 TR UNIT WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE NR 1 ENGINE THRUST REVERSER, RIGHT ACTUATOR SUPPORT WAS WORN TO LIMITS. THE ACTUATOR SUPPORT WAS REPLACED IAW SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999041700465 19990417 00465 NM 1999 4 17 P2EA99125 1 19990221 A 5412 6546998230 FIREWALL BOEING 737 737222 1384473 NM NR 2 PYLON WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE NR 2 ENGINE PYLON FORWARD FIREWALL WAS FOUND WORN. THE FIREWALL PANEL WAS REPAIRED AS PER COO PESA EO NR 3-54-189-99 AND BOEING FAX COO-SJO-99-0389. (M) 2 L 7 2 4F A16WE 1999041700466 19990417 00466 NM 1999 4 17 P2EA99124 1 19990221 A 5320 INTERCOSTAL BOEING 737 737222 1384473 NM BS 294.5/312 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A STIFFENER AND INTERCOSTAL IN THE E/E COMPARTMENT BETWEEN BS 294.5 AND BS 312 AT STRINGER WERE FO UND WITH CORROSION. THE INTERCOSTAL AND STIFFENER WERE REPLACED AS PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999041700467 19990417 00467 NM 1999 4 17 P2EA99123 1 19990220 A 5311 FRAME BOEING 737 737222 1384473 NM BS 685 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE BS 685 RIGHT FRAME FITTING WAS FOUND CRACKED. THE CRACK WAS REPAIRED AS PER BOEING FAX NR COO -SJO-99-0388RR AND COOPESA EO NR COO-3-53-155-99. (M) 2 L 7 2 4F A16WE 1999041700468 19990417 00468 NM 1999 4 17 P2EA99122 1 19990219 A 5730 SKIN BOEING 737 737222 1384473 NM WS 497 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE RIGHT WING OUTBOARD MID-FLAP SKIN AT WS 497 WAS BULGED. REPAIRED SKIN AS PER BOEING FAX COO-S JO-99-0330RR. (M) 2 L 7 2 4F A16WE 1999041700469 19990417 00469 NM 1999 4 17 P2EA99121 1 19990218 A 5320 SPLICE BOEING 737 737222 1384473 NM BS 359 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE STRINGER SPLICE AT BS 359, STRINGER 14L WAS FOUND CRACKED. THE STRINGER SPLICE WAS REPLACED A S PER SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999041700470 19990417 00470 NM 1999 4 17 P2EA99120 1 19990216 A 5320 WEB BOEING 737 737222 1384473 NM BS 286 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A CRACK WAS FUOND AT THE NLG WHEEL WELL, UPPER WEB AT BS 286, RBL 9. AREA WAS REPAIRED AS PER COO PESA EO NR COO-3-53-137-99 AND BOEING FAX NR COO-SJO-99-0267. (M) 2 L 7 2 4F A16WE 1999041700471 19990417 00471 NM 1999 4 17 P2EA99119 1 19990220 A 5330 SKIN BOEING 737 737222 1384473 NM L1 DOORWAY CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE L1 DOOR CUT OUT LOWER AFT CORNER OUTER SKIN WAS FOUND CRACKED. THE SKIN WAS REPAIRED FROM BS 322 TO 355 IAW SB 53-1083 REV 3, PART IV AND DRAWING NR 65C27253. (M) 2 L 7 2 4F A16WE 1999041700472 19990417 00472 NM 1999 4 17 P2EA99118 1 19990223 A 5240 MECHANISM BOEING 737 737222 1384473 NM R2 DOOR CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE R2 DOOR HANDLE MECHANISM HOUSING WAS FOUND WITH CORROSION AT THE LOWER TORQUE TUBE POSITION. R EWORKED BEARING BORE AND MOUNTING HOLES AS PER OHM 52-46-05. (M) 2 L 7 2 4F A16WE 1999041700473 19990417 00473 NM 1999 4 17 P2EA99117 1 19990223 A 5240 BEARING BOEING 737 737222 1384473 NM R1 DOOR CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE R1 DOOR WAS FOUND WITH CORROSION ON THE UPPER TORQUE TUBE BEARING POSITION. THE BEARING BORE AND MOUNTING HOLES WERE REWORKED AS PER OHM 52-46-06. (M) 2 L 7 2 4F A16WE 1999041700474 19990417 00474 NM 1999 4 17 P2EA99116 1 19990219 A 5210 MECHANISM BOEING 737 737222 1384473 NM L2 DOOR CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE L2 DOOR HANDLE MECHANISM HOUSING HAD CORROSION AT LOWER TORQUE TUBE BEARING HOLE. THE HOLE AN D BUSHING WERE REWORKED IAW OHM 52-16-03. (M) 2 L 7 2 4F A16WE 1999041700475 19990417 00475 NM 1999 4 17 P2EA99115 1 19990219 A 5753 SKIN BOEING 737 737222 1384473 NM LT TE MIDFLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, INBOARD MID FLAP LE SKIN AT INBOARD TRACK CUTOUT. THE CRACK W AS REPAIRED IAW BOEING FAX COO-SJO-99-0279RR. (M) 2 L 7 2 4F A16WE 1999041700476 19990417 00476 NM 1999 4 17 P2EA99114 1 19990219 A 5753 SKIN BOEING 737 737222 1384473 NM LT TE MIDFLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, OUTBOARD MIDFLAP LE SKIN AT OUTBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX NR COO-SJO-99-0279RR. (M) 2 L 7 2 4F A16WE 1999041700477 19990417 00477 NM 1999 4 17 P2EA99113 1 19990102 A 2750 CAM BOEING 737 737222 1384473 NM RT TE MIDFLAP MISMANUFACTURED A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURNIG Q-CHECK, THE RIGHT INBOARD MIDFLAP MAIN CARRIAGE CAM WAS FOUND WITH SHARP EDGES. THE AREA WAS REWORKED IAW COOPESA EO NR COO-3-27-139-99. (M) 2 L 7 2 4F A16WE 1999041700478 19990417 00478 NM 1999 4 17 P2EA99112 1 19990218 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, TO VERIFY SRM COMPLIANCE, A REPAIR AT BS 1016 STRINGER 18L WAS REMOVED FOR INVESTIGATION. THE ARE A WAS CLEANED, INSPECTED, AND REPAIRED AS PER COOPESA EO NR COO-3-53-152-99. (M) 2 L 7 2 4F A16WE 1999041700479 19990417 00479 WP 1999 4 17 GTIA9900030 1 19990225 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP LT/RT EMER EXIT LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 DTW - AFT OVERWING EMERGENCY EXIT LIGHTS LEFT AND RIGHT SIDE (ABOVE PLUG WINDOWS) INOPERATIVE. RESECURED AND CLEANED CO NTACTS ON BATTERY PACKS FOR OVERWING LIGHTS ALL CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1999041700480 19990417 00480 WP 1999 4 17 HALA9900072 1 19990305 A 5310 STRUCTURE DOUG DC10 DC1010 3022110 WP BS 561-565 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 TUL - FOUND CORROSION ON FRAME STATION 564 IN TWO PLACES FORWARD OF AC EXHAUST DUCT. CORROSION ON 1/B TEE OF CHORD STAT ION 561 TO 565. SKIN CORROSION STATION 575 AT EXHAUST DUCT (AC BAY) CORROSION ON FITTING INBOARD OF EXHAUST DUCT. INST ALLED REPAIR PER ESO 7349, DATED 3/3/99. (M) 2 L 7 3 4F A22WE 1999041700481 19990417 00481 WP 1999 4 17 HALA9900073 1 19990310 A 5730 PANEL DOUG DC10 DC1010 3022110 WP WS 399 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 DURING C-21 CHECK, FOUND AREA OF CORROSION ON OUTER WING PANEL .5 INCH BY .5 INCH WITH DEPTH OF .070 AT STATION XORS 399 . FOUND BY VISUAL INSPECTION. INSPECTION WAS INTERNAL. BLENDED CORROSION AND REWORKED AREA IAW E50 7349, DATED 03/09/ 99. (M) 2 L 7 3 4F A22WE 1999041700482 19990417 00482 WP 1999 4 17 HALA9900076 1 19990318 A 2170 17946081 COALESCER BAG DOUG DC9 DC951 3022051 WP CABIN CONTAMINATED A HALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 709HA 47764 HNL - FLT 348 - SMOKE IN THE CABIN ON TAXI OUT. SEEMS TO ORIGINATE IN AFT AREA OF CABIN. SMOKE STOPPED WHEN A/C SWITCH ES TURNED OFF. REPLACED LEFT AND RIGHT COALESCER BAG ASSEMBLIES. OPERATION AND LEAK CHECK OF BOTH SEPARATOR BAGS OK. ( M) 2 L 7 2 4F RT A6WE 1999041700483 19990417 00483 WP 1999 4 17 HALA9900077 1 19990312 A 5311 ABA7223 FRAME DOUG DC10 DC1010 3022110 WP BS 410 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 TUL - DURING CHECK FOUND FUSELAGE FRAME CORRODED AT THE FORWARD LAVATORY SERVICE PANEL 9 INCHES BY 2 INCHES AT FORWARD E /E STATION 410. DEPTH IS .063. FRAME SPLICED WITH FILLER PLATE INSTALLED PER ESO 7349, DATED 3/12/99. (M) 2 L 7 3 4F A22WE 1999041700484 19990417 00484 WP 1999 4 17 HALA9900069 1 19990310 A 3246 26X6612PR WHEEL DOUG DC9 DC951 3022051 WP NLG OUT OF BALANCE A HALA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 WP 13 601AP 47658 HNL - FLT 186 - FOUND SEVERE NOSE SHIMMY AT START OF TAKEOFF, RETURNED TO THE RAMP. REMOVED AND REPLACED BOTH NOSE TIRE ASSEMBLIES. SPIN CHECKS OK. INSPECTED NOSE LANDING GEAR AND NO DEFECT NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 1999041700485 19990417 00485 NM 1999 4 17 TSAA9933162 1 19990319 A 3350 8731002511 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999041700486 19990417 00486 NM 1999 4 17 TSAA9933163 1 19990320 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM PAX CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED POSITION 1, 4, AND 6 BATTERIES FOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F RT A16WE 1999041700487 19990417 00487 NM 1999 4 17 TSAA9933164 1 19990320 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 3 POSITION FLOOR PROXIMITY EMERGENCY LIGHT ASSEMBLY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999041700488 19990417 00488 NM 1999 4 17 TSAA9933165 1 19990320 A 3350 9221009 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED BATTERY IN FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999041700489 19990417 00489 EU 1999 4 17 SIMA990702 1 19990311 A 5230 S52376105202 FRAME AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING MBV-2 INSPECTION, FOUND THE FORWARD AND THE TWO AFT FRAMES OF THE CARGO DOOR CRACKED. REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700490 19990417 00490 EU 1999 4 17 99ZZZM241 1 19990311 A 5230 52376104202 FRAME AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING MBV-2 INSPECTION, FOUND THE FORWARD AND THE TWO AFT FRAMES OF THE CARGO DOOR CRACKED. REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700491 19990417 00491 EU 1999 4 17 99ZZZM242 1 19990311 A 5230 S52376104204 FRAME AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING MBV-2 INSPECTION, FOUND THE FORWARD AND THE TWO AFT FRAMES OF THE CARGO DOOR CRACKED. REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700492 19990417 00492 EU 1999 4 17 99ZZZM243 1 19990311 A 5230 S52376105208 FRAME AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING MBV-2 INSPECTION, FOUND THE FORWARD AND THE TWO AFT FRAMES OF THE CARGO DOOR CRACKED. REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700493 19990417 00493 EU 1999 4 17 C2XA99IA196 1 19990313 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 42836 200 EFD - DURING MAINTENANCE INSPECTION, THE CENTER AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700494 19990417 00494 EU 1999 4 17 C2XA99IA195 1 19990314 A 3350 3012500 SIGN AEROSP ATR42 ATR42500 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING POST FLIGHT INSPECTION, THE EMERGENCY EXIT SIGN BY THE SERVICE DOOR WAS FOUND TO BE BROKEN. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED SIGN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700495 19990417 00495 SO 1999 4 17 C2XA99IA194 1 19990317 A 3350 3025101 LIGHT EMB 145 EMB145 SO LT/RT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16927 145006 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999041700496 19990417 00496 SO 1999 4 17 C2XA99IA193 1 19990317 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145 SO LT/RT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16927 145006 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999041700497 19990417 00497 CE 1999 4 17 C2XA99IA192 1 19990317 A 3230 RETRACT MECH BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 09 87552 UE216 TYR - DURING FLIGHT TRAINING, THE CREW REPORTED THAT THE EMERGENCY GEAR EXTENSION WAS INOPERATIVE. THE AIRCRAFT WAS FER RIED TO IAH WHERE MAINTENANCE PERFORMED AN OPERATION CHECK OF THE AIRCRAFT EMERGENCY EXTENSION SYSTEM WITH NO DEFECTS NO TED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999041700498 19990417 00498 SO 1999 4 17 C2XA99IA191 1 19990315 A 3350 AD2047 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL AISLE PATH AND CEILING EMERGENCY LIGHTS WERE INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRA FT WAS APPROVED FOR RETURN T SERVICE. (M) 2 L 7 2 4T RT A31SO 1999041700499 19990417 00499 EU 1999 4 17 C2XA99B015 1 19990324 A 3350 3011232 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 EWR - RT AFT EMERGENCY LIGHT LENS CRACKED. MAINTENANCE REMOVED AND REPLACED RIGHT AFT EMERGENCY LIGHT ASSEMBLY. OPS CH ECKED EMERGENCY LIGHTS GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700500 19990417 00500 EU 1999 4 17 C2XA99BT016 1 19990324 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 EWR REPORTED SEVERAL EMERGENCY AISLE PATH LIGHTS ARE OUT. MAINTENANCE RELAMPED EMERGENCY AISLE PATH LIGHTING AS NECESSA RY. OPERATIONALLY CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700501 19990417 00501 EU 1999 4 17 C2XA99BT017 1 19990302 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 09 14813 100 IN BOUND CREW EWR FLIGHT 3410, REPORTED LOWER EMERGENCY EXIT BULB INOPERATIVE ON SERVICE ENTRY, ENTRY RIGHT FORWARD EMER GENCY LIGHT. PASSENGER EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULBS AND OPERATIONALLY CHECKED L IGHTS GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700502 19990417 00502 EU 1999 4 17 C2XA99BT018 1 19990322 A 3350 FUSE AEROSP ATR42 ATR42320 8680930 EU POWER SUPPLY BLOWN A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 09 14813 100 EWR - FLIGHT 3410, CREW REPORTED, 5 A/B AND 7 A/B, AND 8 A/B EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE REP LACED FUSES IN POWER SUPPLY AND OPS CHECKED LIGHTING GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700503 19990417 00503 EU 1999 4 17 C2XA99BT019 1 19990323 A 3350 3011232 LENS AEROSP ATR42 ATR42320 8680930 EU CABIN CRACKED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 09 14819 156 EWR - RIGHT FORWARD EMERGENCY EXIT LIGHT LENS REPORTED CRACKED BY FLIGHT CREW INBOUND 3507. MAINTENANCE REPLACED CRACKE D LENS WITH SERVICEABLE UNIT. OPS CHECKED LIGHT GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700504 19990417 00504 EU 1999 4 17 C2XA99BT014 1 19990323 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14813 100 BTV - MAINTENANCE REPORTED, ONLY EVERY OTHER AISLE PATH LIGHTS OPERATE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECKED EMERGENCY LIGHTS GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700505 19990417 00505 EU 1999 4 17 C2XA99BT013 1 19990324 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15823 165 BTV - MAINTENANCE REPORTED PASSENGER DOOR AREA EMERGENCY LIGHTS VERY DIM. CLEANED CORROSION FROM SOCKET AND REPLACED BU LB. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700506 19990417 00506 EU 1999 4 17 C2XA99BT012 1 19990324 A 5330 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 DURING LINE CHECK INSPECTION IN BTV, MAINTENANCE FOUND DENT TO FUSELAGE ABOVE FUELING CONTROL PANEL. REPAIRED DENT IN F USELAGE IAW ATR42SRM PRESSURIZED LEAK CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700507 19990417 00507 EU 1999 4 17 C2XA99BT011 1 19990323 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU ROW 1,3,4 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14822 163 BTV - MAINTENANCE REPORTED EMERGENCY AISLE PATH LIGHTING AT 1A/B, 3 A/B, 4 A/B NOT WORKING. REMOVED AND REPLACED EMERGE NCY POWER SUPPLY UNIT. OPS CHECK OF LIGHTING GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700508 19990417 00508 EU 1999 4 17 C2XA99BT010 1 19990323 A 3350 3011232 LENS AEROSP ATR42 ATR42320 8680930 EU EXTERNAL CRACKED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14822 163 BTV - MAINTENANCE REPORTED FORWARD RIGHT EXTERNAL EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY LIGHT LE NS AND OPS CHECKED LIGHT GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700509 19990417 00509 EU 1999 4 17 C2XA99BT009 1 19990323 A 3350 3011206 LIGHT AEROSP ATR42 ATR42320 8680930 EU EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15816 105 BTV MAINTENANCE REPORTED RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999041700510 19990417 00510 NM 1999 4 17 WRLA99014 1 19990318 A 2910 1489951 VALVE DOUG MD11 MD11 3023602 NM NR 3 HYD SYSTEM LEAKING A WRLA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 275WA 48631 DURING INITIAL CLIMB-OUT ON FLT NR MH6203, FLIGHT CREW NOTED NR 3 HYD 'OFF' LIGHT ILLUMINATED, AND LOSS OF HYDRAULIC FLU ID IN NR 3 SYSTEM TO 4.8 GAL. NR 3 SYSTEM WAS SHUT DOWN. FLIGHT CREW CONTACTED MAINTENANCE CONTROL, AND BASED UPONITS RECOMMENDATION, FLIGHT CREW ELECTED TO RETURN TO POINT OF DEPARTURE FOR MAINTENANCE ACTION. AIRCRAFT RETURNED TO AIRPOR T OF DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND NR 3 HYD SYSTEM REVERSIBLE MOTOR PUMP S HUTOFF VALVE LEAKING. SHUTOFF VALVE WAS REPLACED. SYSTEM WAS RESERVICED. OPERATIONAL CHECK COMPLETED WITHOUT MALFUNCT ION. AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT WAS OUT OF SERVICE FOR 5 HOURS 30 MINUTES. (M) 2 L 7 3 4F RT A22WE 1999041700511 19990417 00511 NM 1999 4 17 AALA990300 1 19990225 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1177 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 861AA 21088 TUL - FOUND STATION 1177 BELLY SKIN CORRODED AT STRINGER 29 RIGHT. REMOVED CORRODED SECTION STRINGER 29R AT STATION 117 7 AND SPLICED IN NEW STRINGER PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999041700512 19990417 00512 NM 1999 4 17 AALA990299 1 19990224 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 670 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 861AA 21088 TUL - FOUND STATION 670 STRINGER 27L CORRODED. REPAIRED PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999041700513 19990417 00513 NM 1999 4 17 AALA990298 1 19990225 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 861AA 21088 TUL - FRAME BENT AT FLANGE AND WEB STATION 950F STRINGER 25L TO 26L. REPAIRED FRAME PER SRM 51-40-3 WITH .071 INCH 7075 -T6 MATERIAL MS2047008 FASTENERS MS20470D6 FASTENERS IN WEB AND BACB30FQ6 FASTENERS IN FLANGE. (M) 2 L 7 3 4F A3WE 1999041700514 19990417 00514 NM 1999 4 17 AALA990297 1 19990225 A 5311 FRAME BOEING 727 727223 1384074 NM BS 970 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 861AA 21088 TUL - FRAME BENT AT FLANGE AND WEB STATION 970 BETWEEN STRINGER 25L AND 26L. FRAME REPAIRED PER SRM 51-40-3 WITH .071 I NCH 7075T6 MATERIAL, MS2047008 FASTENERS, MS20970D6 FASTENERS IN WEB AND BACB30FQ6 FASTENERS IN FLANGE. (M) 2 L 7 3 4F A3WE 1999041700515 19990417 00515 EU 1999 4 17 AALA990173 1 19990211 A 5320 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 74-75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 3075A 606 TUL - FLOOR CROSS BEAM BETWEEN FRAME 74 AND FRAME 75 RIGHT SIDE 10 INCH IN FROM R4 DOOR SILL HAS DEEP CORROSION UNDER SI DE OF BEAM. REMOVED FLOOR CROSS BEAM AND FABRICATED NEW CROSS BEAM PER SRM 51-72-10-0 AND INSTALLED. (M) 2 L 7 2 4F RT A35EU 1999041700516 19990417 00516 EU 1999 4 17 AALA990256 1 19990218 A 5320 5467688 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FRAME 32 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 3075A 606 TUL - FOUND CORROSION ON BOTTOM OF NR 1 ROLLER TRAY, JUST FORWARD OF SPLICE AT FRAME 32. INSTALLED NEW SECTION OF NR 1 ROLLER TRAY PER SRM 51-72-10 AND 53-10-15. (M) 2 L 7 2 4F RT A35EU 1999041700517 19990417 00517 EU 1999 4 17 AALA990272 1 19990223 A 5320 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 1449 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 3075A 606 TUL - FASTENER HOLES HAS CORROSION NR 1 ROLLER TRAY FROM FRAME 20-24 ON INBOARD SIDE. INSTALLED REPAIR AT FRAME 21 PER SRM 53-30-00. (M) 2 L 7 2 4F RT A35EU 1999041700518 19990417 00518 EU 1999 4 17 AALA990279 1 19990224 A 5320 5467688 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 2110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 3075A 606 TUL - FOUND NR 6 ROLLER TRAY IN FORWARD CARGO HAS CORROSION DAMAGE AT FRAME 33. REPLACED SECTION OF NR 6 ROLLER TRAY PE R AARD 51-10-00-5 AND SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1999041700519 19990417 00519 WP 1999 4 17 AALA990171 1 19990209 A 2710 CASTING DOUG DC10 DC1010 3022110 WP RT AILERON CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - RIGHT INBOARD AILERON ACTUATOR CASTING IS CRACKED AT FORWARD LOWER INBOARD LOCATION. ACCOMPLISHED INTERIM REPAIR PER ESO 7349 DAGED 2-9-99. (M) 2 L 7 3 4F A22WE 1999041700520 19990417 00520 WP 1999 4 17 AALA990170 1 19990210 A 5320 BEAM DOUG DC10 DC1010 3022110 WP BS 1676-1681 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON SHEAR TIES AND LOWER CARGO DOOR BEAM FROM LONGERON 42R-48R AT STATION 1676-1681. REPLACED SHEA R TIES AND BEAM IAW SRM 51-01-00-05 AND ESO 7349, DATED 2-9-99. (M) 2 L 7 3 4F A22WE 1999041700521 19990417 00521 WP 1999 4 17 AALA990169 1 19990205 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1195-1481 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION AROUND LOWER DRAIN HOLES IN SKIN FROM STATION 1195.6 TO 1421. REPAIRED IAW SRM VOL I 53-40-00. ( M) 2 L 7 3 4F A22WE 1999041700522 19990417 00522 WP 1999 4 17 AALA990168 1 19990205 A 5320 CLIP DOUG DC10 DC1010 3022110 WP BS 1319.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 128AA 46984 TUL - FOUND CORROSION ON FORWARD SIDE OF CLIP AT STATION 1319.2 BETWEEN LONGERON 51L-52. REPAIRED IAW SRM 53-20-00 VOL I. (M) 2 L 7 3 4F A22WE 1999041700523 19990417 00523 WP 1999 4 17 AALA990304 1 19990304 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-797.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 249AA 49269 TUL - FOUND DEEP CORROSION IN NR 6 SEAT TRACK. REMOVED OLD SEAT TRACK AND INSTALLED NEW SECTION OF SEAT TRACK STATION 2 00-797.5. (M) 2 L 7 2 4F A6WE 1999041700524 19990417 00524 WP 1999 4 17 AALA990284 1 19990225 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 479AA 49654 TUL - FOUND LONGERON NR 2 HAS CRACK AND AMAGE FASTENER 2 EACH HOLES. SPLICE IN NEW LONGERON AND INSTALLED DOUBLER ON EX TERNAL FUSELAGE PER 53-01 AND 53-02-12. (M) 2 L 7 2 4F A6WE 1999041700525 19990417 00525 WP 1999 4 17 AALA990271 1 19990220 A 5347 593054716 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 483/516 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 446AA 49472 TUL - FOUND NR 6 SEAT TRACK CORRODED AT STATION 483 AND 516. INSTALLED SEAT TRACK PLUGS AT STATION 483 AND 516 PER SRM 53-05 PAGE 8C. (M) 2 L 7 2 4F A6WE 1999041700526 19990417 00526 WP 1999 4 17 AALA990270 1 19990220 A 5347 5444078 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1193 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 446AA 49472 TUL - FOUND NR 2 SEAT TRACK HAS CORROSION AT STATION 1193. INSTALLED SEAT TRACK PLUG PER SRM 53-05 PAGE 8C. (M) 2 L 7 2 4F A6WE 1999041700527 19990417 00527 WP 1999 4 17 AALA990269 1 19990220 A 5347 593054715 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 731 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 446AA 49472 TUL - FOUND NR 1 SEAT TRACK HAS CORROSION AT STATION 731. INSTALLED SEAT TRACK PLUG PER 53-05 SRM. (M) 2 L 7 2 4F A6WE 1999041700528 19990417 00528 WP 1999 4 17 AALA990268 1 19990220 A 5347 59305477 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 229 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 446AA 49472 TUL - FOUND NR 3 SEAT TRACK CORRODED AT STATION 229. INSTALLED SEAT TRACK PLUG REPAIR AT STATION 229 NR 3 TRACK PER SRM 53-05-8C. (M) 2 L 7 2 4F A6WE 1999041700529 19990417 00529 NM 1999 4 17 AALA994042 1 19990305 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 764 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 382AN 25451 AFW - FLOORBEAM AT STATION 764 HAS CORROSION REMOVAL ON UPPER SURFACE MATERIAL REMAINING IS BEYOND SRM LIMITS. BLENDED AREA. FABRICATED REPAIR STRAP OUT OF 301.5 HARD STAINLESS STEEL .050 INCH THICK. ALODINED ALL BARE ALUMINUM SURFACES A ND FINISHED BLENDS WITH BMS-5-92. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALANT. (M) 2 L 7 2 4F RT A1NM 1999041700530 19990417 00530 NM 1999 4 17 USAASB99075 1 19990318 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 269AU 22881 CLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE , AND THE POWER SUPPLY M192, LEFT SIDE, IN THE AFT CARGO COMPARTMENT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999041700531 19990417 00531 NM 1999 4 17 99ZZZM244 1 19990318 A 3350 6013211 POWER SUPPLY BOEING 737 7372B7 1384560 NM CARGO COMPT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 269AU 22881 CLE - DURING OPERATIONAL TEST OF EMERGENCY LGIHT SYSTEM, MAINTENANCE FOUND THE AFT ENTRY DOOR, AFT SERVICE DOOR AND THE LEFT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M572, RIGHT SIDE , AND THE POWER SUPPLY M192, LEFT SIDE, IN THE AFT CARGO COMPARTMENT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999041700532 19990417 00532 SO 1999 4 17 ASOA99021 1 19990108 A 5720 12016806001 ANGLE EMB 120 EMB120RT SO LT/RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 239AS 120057 DURING INSPECTION, FOUND LEFT AND RIGHT WING RIB 17, SPAR ANGLE CRACKED. MCN MAINTENANCE REPAIRED WING SPAR IAW ASA EO1 20-57-0067, REF DATA EAC FAX SST-0216/99, SST-2447/98 AND SRM 51-00-00. (M) 2 L 7 2 4T RT A31SO 1999041700533 19990417 00533 SO 1999 4 17 ASOA99022 1 19990111 A 5720 12016806001 ANGLE EMB 120 EMB120RT SO LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 229AS 120042 DURING INSPECTION FOUND LEFT WING, RIB 17, SPAR ANGLE CRACKED. MCN MAINTENANCE REPAIRED WING SPAR IAW ASA EO120-57-0067 , REFERENCE DATA EAC FAX SST-0251/99 AND SRM 51-00-00. (M) 2 L 7 2 4T RT A31SO 1999041700534 19990417 00534 SO 1999 4 17 ASOA99023 1 19990211 A 5411 12003852001 FRAME EMB 120 EMB120RT SO LT/RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 215AS 120010 DURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999041700535 19990417 00535 SO 1999 4 17 ASOA99020 1 19990201 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT/RT NACELLE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURING C-CHECK INSPECTION, THE FRAME 2 ANGEL ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND BROKEN. REMOVED AND REPLACED FRAME ANGLES ON LEFT AND RIGHT NACELLES. (M) 2 L 7 2 4T RT A31SO 1999041700536 19990417 00536 SO 1999 4 17 ASOA99019 1 19990201 A 5400 12003852001 FRAME EMB 120 EMB120RT SO LT/RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 258AS 120131 DURNG C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999041700537 19990417 00537 SO 1999 4 17 ASOA99017 1 19990202 A 3240 SWITCH EMB 120 EMB120RT SO COCKPIT STUCK A ASOA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 258AS 120131 FLT 9258 - DURING TEST FLIGHT OUT OF CKB, CREW NOTICED BOTH PARKING BRAKE LIGHTS CAME ON WITH ASSOCIATED GEAR PROBLEM (L ANDING GEAR SYSTEM 'B', ALL 3 RED 'B' LIGHTS CAME ON UPON RETRACTION). CREW DECLARED AN EMERGENCY AND RETURNED TO CKB W HERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. CKB MAINTENANCE FOUND PARKING BRAKE 'PRESS TO TEST' SWITCH S TUCK IN THE TEST POSITION AND CLEANED TEST SWITCH IAW MM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FO R FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999041700539 19990417 00539 NM 1999 4 17 P2EA99111 1 19990224 A 5751 654645424 SKIN BOEING 737 737222 1384473 NM RT AILERON DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURIGN Q-CHECK RIGHT AILERON WAS FOUND WITH DELAMINATION. AILERON WAS REPAIRED AS PER COOPESA NR COO-CMP-3-57-151 -99. (M) 2 L 7 2 4F A16WE 1999041700540 19990417 00540 NM 1999 4 17 P2EA99110 1 19990218 A 5320 WEB BOEING 737 737222 1384473 NM BS 278 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE NLG WHEEL WELL UPPER WEB AT BS 278, RBL 10. THE UPPER WEB WAS REPAIRED I AW COOPESA EO NR COO-SJO-99-0267. (M) 2 L 7 2 4F A16WE 1999041700541 19990417 00541 NM 1999 4 17 P2EA99109 1 19990218 A 5753 SKIN BOEING 737 737222 1384473 NM RT TE MIDFLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE RIGHT WING INBOARD MIDFLAP, LE SKIN AT WBL 87.75. CRACK REPAIRED IAW BOE ING FAX COO-SJO-99-0280. (M) 2 L 7 2 4F A16WE 1999041700542 19990417 00542 NM 1999 4 17 P2EA99208 1 19990414 A 5330 SKIN BOEING 737 737205 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, LEFT EXTERNAL SKIN WAS CRACKED THREE PLACES FROM BS 727 TO 727 'A' AND STRINGER 14L TO 17L REPAIR ED PER EO COO-3-53-314-99 DATED 5/22/99. (M) 2 L 7 2 4F A16WE 1999041700543 19990417 00543 NM 1999 4 17 P2EA99107 1 19990222 A 5330 SKIN BOEING 737 737222 1384473 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, LFEC DETECTED A CRACK IN A FASTENER HOLE AT BS 492.4, BETWEEN STRINGERS 23 AND 24 RIGHT. THE AREA WAS REPAIRED AS PER COOPESA EO NR COO-2-53-157-99 AND BOEING FAX NR COO-SJO-99-0319. (M) 2 L 7 2 4F A16WE 1999041700544 19990417 00544 NM 1999 4 17 P2EA99106 1 19990223 A 5751 65464542 SKIN BOEING 737 737222 1384473 NM LT AILERON DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, DELAMINATION WAS FOUND ON THE LEFT AILERON. THE AILERON WAS REPAIRED PER COOPESA EO COO-CMP-3-57- 127-99. (M) 2 L 7 2 4F A16WE 1999041700545 19990417 00545 NM 1999 4 17 P2EA99105 1 19990219 A 5753 SKIN BOEING 737 737222 1384473 NM RT TE FORFLAP WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE SKIN ON THE LEADING EDGE OF THE RIGHT WING OUTBOARD FOREFLAP WAS FOUND WITH WEAR. THE SKIN WA S REPAIRED FROM WSL 498 TO 505 AS PER SRM 57-50-40- FIG 1. (M) 2 L 7 2 4F A16WE 1999041700546 19990417 00546 NM 1999 4 17 P2EA99104 1 19990219 A 5753 65507655 RIB BOEING 737 737222 1384473 NM LT TE MIDFLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, LEFT WING OUTBOARD MID FLAP INTERNAL LE RIB AT WBL 298 WAS FOUND CRACKED. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999041700547 19990417 00547 NM 1999 4 17 P2EA99103 1 19990219 A 5753 65937565 RIB BOEING 737 737222 1384473 NM LT TE MIDFLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE LEFT INBOARD MID FLAP STRUCTURE, FOREFLAP CENTER TRACK SUPPORT FITTING RIB (INBOARD) WAS CRACK ED AT TWO PLACES. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999041700548 19990417 00548 NM 1999 4 17 P2EA99102 1 19990218 A 5712 RIB BOEING 737 737222 1384473 NM WS 213 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, RIGHT WING, UPPER CHANNEL OF THE LE RIB AT WS 213 WAS FOUND CRACKED. THE CHANNEL WAS REPLACED IAW SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999041700549 19990417 00549 NM 1999 4 17 P2EA99101 1 19990225 A 5730 657094724 PANEL BOEING 737 737222 1384473 NM RT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE RIGHT WING FIXED TRAILING EDGE PANEL, P/N 65-70947-24 WAS FOUND DELAMINATED. THE PANEL WAS RE PAIRED IW EO NR COO-CMP-3-57-159-99. (M) 2 L 7 2 4F A16WE 1999041700550 19990417 00550 NM 1999 4 17 P2EA99100 1 19990225 A 5753 6546422193M SKIN BOEING 737 737222 1384473 NM NR 2 TE SLAT DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE LEFT WING NR 2 TRAILING EDGE SLAT WAS FOUND WITH DELAMINATION. THE SLAT WAS REPAIRED IAW EO N R COO-CMP-3-57-149-99. (M) 2 L 7 2 4F A16WE 1999041700551 19990417 00551 NM 1999 4 17 P2EA99099 1 19990221 A 5312 BULKHEAD WEB BOEING 737 737222 1384473 NM BS 294.5 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE WEB OF THE PRESSURE BULKHEAD AT BS 294.5 BETWEEN STRINGER 27 AND 28 RT IN THE E/E COMPARTMENT. WEB SECTION WAS REPAIRED IAW EO NR COO-3-53-146-99 AND BOEING FAX NR COO-SJO-99-0293. (M) 2 L 7 2 4F A16WE 1999041700552 19990417 00552 NM 1999 4 17 P2EA99098 1 19990220 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 668.75 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE UPPER FLANGE OF THE FLOORBEAM AT BS 668.75, LBL 25 WAS FOUND CRACKED. REPAIRED FLOORBEAM AS P ER COOPESA EO NR COO-3-53-154-99 AND BOEING FAX NR COO-SJO-98-0993RR. (M) 2 L 7 2 4F A16WE 1999041700553 19990417 00553 NM 1999 4 17 P2EA99097 1 19990224 A 5755 654645123 SKIN BOEING 737 737222 1384473 NM NR 3 SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, FLIGHT SPOILER NR 3 WAS FOUND WITH DELAMINATION. FLIGHT SPOILER REPAIRED AS PER COOPESA EO NR COO -CMP-3-57-150-00. (M) 2 L 7 2 4F A16WE 1999041700554 19990417 00554 NM 1999 4 17 P2EA99096 1 19990218 A 5320 SUPPORT BOEING 737 737222 1384473 NM BS 996 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE PASSENGER CABIN FLOOR SUPPORT LOCATED AT BS 996, LBL 12, WAS FOUND WITH CORROSION. THE SUPPOR T WAS REPLACED FROM BS 996 TO BS 1009 IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999041700555 19990417 00555 NM 1999 4 17 P2EA99895 1 19990218 A 5347 CARGO TRACK BOEING 737 737222 1384473 NM BS 468 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE FORWARD CARGO COMPARTMENT CARGO TRACK AT BS 468, RBL 14, WAS FOUND WITH CORROSION. THE TRACK WAS REPAIRED AS PER SRM 53-10-5 FIG 5. (M) 2 L 7 2 4F A16WE 1999041700556 19990417 00556 NM 1999 4 17 P2EA99094 1 19990217 A 5712 RIB BOEING 737 737222 1384473 NM WS 279.25 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE RIGHT WING, LEADING EDGE RIB AT WBL 279.25 HAD WEAR ON THE LOWER FLANGE. THE AREA WAS REPAIRE D BY APPLYING PRIMER AND ALODINE AS PER BOEING FAX NR COO-SJO-0261-RR. (M) 2 L 7 2 4F A16WE 1999041700557 19990417 00557 NM 1999 4 17 P2EA99093 1 19990219 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 767 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, A REPAIR LOCATED AT BS 767, STRINGER 9L WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTE D AND REPAIRED AS PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999041700558 19990417 00558 NM 1999 4 17 MZZA9953 1 19990224 A 2760 BACP30J4 PULLEY BOEING 727 727277 138408S NM NR 4 SPOILER STUCK A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 627DH 22641 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, STUCK BEARING WAS FOUND ON LEFT WING SPOILER CONTROL PULLEY BEA RING AT INBOARD END OF NR 4 SPOILER. THE DAMAGED SPOILER CONTROL PULLEY P/N BACP30J4, WAS REMOVED AND REPLACED PER B727 MM 27-61-41. (M) 2 L 7 3 4F RT A3WE 1999041700559 19990417 00559 NM 1999 4 17 MZZA99052 1 19990225 A 5330 65585183 SKIN BOEING 727 727277 138408S NM BS 848.95 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 627DH 22641 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT FUSELAGE SKIN SPLICE PLATE AT B S 848.95 ABOVE STRINGER 18A. THE CORRODED FUSELAGE SKIN SPLICE PLATE WAS REPAIRED PER EC/RA NR 5310-03822 DATED 02 MAR 1999. (M) 2 L 7 3 4F RT A3WE 1999041700560 19990417 00560 NM 1999 4 17 MZZA99051 1 19990223 A 5320 6517510256 WEB BOEING 727 727277 138408S NM BS 1293/1313 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 627DH 22641 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BOX VER TICAL WEB BETWEEN BS 1293 AND BS 1313. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT ST IFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999041700561 19990417 00561 NM 1999 4 17 MZZA99050 1 19990223 A 5320 6517510256 WEB BOEING 727 727277 138408S NM BS 1243/1253 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 627DH 22641 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BOX VER TICAL WEB BETWEEN BS 1243 AND BS 1253. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT ST IFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999041700562 19990417 00562 NM 1999 4 17 MZZA99049 1 19990223 A 5320 6517510256 WEB BOEING 727 727277 138408S NM BS 1223/1233 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 627DH 22641 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BOX VER TICAL WEB BETWEEN BS 1223 AND BS 1233. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT ST IFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999041700563 19990417 00563 NM 1999 4 17 MZZA99048 1 19990223 A 5320 6517510255 WEB BOEING 727 727277 138408S NM BS 1303/1323 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 627DH 22641 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERT ICAL WEB BETWEEN BS 1303 AND BS 1323. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STI FFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999041700564 19990417 00564 NM 1999 4 17 MZZA99047 1 19990223 A 5320 6517510255 WEB BOEING 727 727277 138408S NM BS 1253/1293 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 627DH 22641 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERT ICAL WEB BETWEEN BS 1253 AND BS 1293. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STI FFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999041700565 19990417 00565 NM 1999 4 17 USAA039914 1 19990319 A 2910 65178232 MODULE BOEING 727 727254 138408L NM 'A' HYD SYSTEM LEAKING A USAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 916TS 4850 20437 FLT 6470 - DCA-LGA - EN ROUTE LOST ALL SYSTEM 'A' HYDRAULIC FLUID. EMERGENCY DECLARED. MANUAL LANDING GEAR EXTENSION P ERFORMED. FOUND SYSTEM 'A' AILERON MODULAR PACKAGE SEPARATED. REPLACED AILERON PACKAGE PER MM 27-10-141. REPLACED NR 1 AND NR 2 ENGINE HYDRAULIC PUMPS. REPLACED CASE DRAIN, PRESSURE AND RETURN FILTERS. REPLACED SYSTEM 'A' RESERVOIR AIR PRESSURE REGULATOR. SERVICED HYDRAULIC SYSTEM. (M) 2 L 7 3 4F A3WE 1999041700566 19990417 00566 NM 1999 4 17 USAABB99017 1 19990323 A 3350 20121 BATTERY CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656US 26847 CDG - LEFT FORWARD EXTERIOR EMERGENCY LIGHTS POWER SUPPLY IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M ) 2 L 7 2 4F RT A1NM 1999041700567 19990417 00567 NM 1999 4 17 USAABB99015 1 19990319 A 3350 LIGHT BOEING 757 7572B7 1384964 NM CABIN ILLUMINATED A USAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 19 633AU 27811 PIT - CABIN EMERGENCY LIGHTS ILLUMINATED ON TAXI OUT OF GATE. MAINTENANCE PERFORMED THE FUNCTIONAL TEST OF THE SYSTEM. NO FAULTS FOUND. (M) 2 L 7 2 4F RT A2NM 1999041700568 19990417 00568 NM 1999 4 17 USAABB99016 1 19990319 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM L4 DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 CLT - THE L4 DOOR EMERGENCY EXIT IDENTIFIER WAS ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. MAINTENANCE REPLACED T HE BATTERY. (M) 2 L 7 2 4F RT A2NM 1999041700569 19990417 00569 NM 1999 4 17 USAA039915 1 19990320 A 5210 6990196 COVER BOEING 727 727227 1384078 NM L1 DOOR BENT A USAA A UNSCHED LANDING P NO WARNING INDICATION TO TAKEOFF 1 EA 19 924TS 21041 FLT 6400 - DCA-LGA - EXTREMELY LOUD NOISE (AIR FLOW) AROUND L-1 DOOR IMMEDIATELY AFTER TAKEOFF. RETURNED TO BASE. PRES SURIZATION INDICATION NORMAL OPERATION. FOUND LOWER DOOR HINGE COVER BENT AND OUT OF ALIGNMENT. INSTALLED NEW HINGE CO VER AND REALIGNED. PRESSURIZED AIRCRAFT ON GROUND AND CHECKED FOR AIR LEAK, NONE FOUND. (M) 2 L 7 3 4F A3WE 1999041700570 19990417 00570 NM 1999 4 17 USAASB99073 1 19990316 A 3240 ST107R TRANSMITTER BOEING 737 7374B7 1384702 NM BRAKE PRESSURE FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 780AU 7812 24997 CLT - FLT 1144 - ON APPROACH TO CLT, THE BRAKE PRESSURE INDICATOR DROPPED TO 1,000 PSI. CREW ABORTED THE LANDING, DECLA RED AN EMERGENCY AND ACCOMPLISHED A GO-AROUND FOR THE LONGER RUNWAY. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE G ATE ON ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED THE BRAKE PRESSURE TRANSMITTER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999041700571 19990417 00571 NM 1999 4 17 USAASB99077 1 19990320 A 3350 20121 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 395US 23317 PHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 1 THROUGH 4 INOPERATIVE AND THE LAST 6 SEAT ROWS IN THE AFT CA BIN INOPERATIVE. MAINTENANCE REPAIRED SHORTED AND BROKEN WIRES FOR SEAT ROWS 1 THROUGH 4 AND REMOVED AND REPLACED THE B ATTERY CHARGER FOR THE LAST 6 SEAT ROWS IN THE AFT CABIN. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999041700572 19990417 00572 WP 1999 4 17 USAAD99046 1 19990318 A 2781 WARNING DOUG DC9 DC981 3022081 WP LE FLAPS ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 828US 48028 FLL-LGA - FLT 2168 - AFTER TAKEOFF AND SLAT RETRACTION THE SLAT DISAGREE LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO MC O AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CLEANED AND RESET THE LIGHT SOCKET ASSEMBLY. (M) 2 L 7 2 4F A6WE 1999041700573 19990417 00573 NM 1999 4 17 USAA990221 1 19990302 A 5240 6545871523 SKIN BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 37494 23236 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK EXTERNAL SKIN FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER EA 64060 AND SB 52-1096. (M) 2 L 7 2 4F RT A16WE 1999041700574 19990417 00574 1999 4 17 USAABB99006 4 19990203 A 2565 2174109 SHEAR PIN BOEING 767 767201 1385125 NM EMER EXIT SLIDE SHEARED A USAA K NONE O OTHER LD LANDING 1 EA 19 650US 23902 AMS - FLT 42 - ON TOUCH DOWN AT AMS, THE RIGHT OVERWING SIDE DEPLOYED. MAINTENANCE FOUND THE OVERWIG DOOR LATCH ACTUATO R SQUIBS HAD NOT FIRED, BUT THE PIN THAT SHEARS WHEN THE ACTUATOR SQUIB FIRES (ALLOWING THE LATCHES TO OPEN) HAD SHEARED . IT IS NOT KNOWN WHETHER THE PIN SHEARED AS A RESULT OF THE DOOR OPENING (RIGGING PROBLEM), OR IF THE PIN HAD BEEN PRE VIOUSLY SHEARED AND THE JOLT OF THE LANDING CAUSED THE DOOR TO OPEN, INITIATING THE SLDIE DEPLOYMENT. THE SLIDE, SLIDE BOTTLE, LATCH ACTUATOR, BOTH DOOR ACTUATORS AND UPPER DOORSTOP BRACKET (DAMAGED AS A RESULT OF THE SLIDE DEPLOYMENT AND AIRCRAFT MOTION ON THE GROUND) WERE REPLACED. (M) 2 L 7 2 4F RT A1NM 1999041700575 19990417 00575 NM 1999 4 17 GAIA99045 1 19990319 A 2780 MECHANISM BOEING 727 727223 1384074 NM TE FLAPS LACK OF LUBE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6838 20191 DURING CLIMB-OUT FROM TOL TO DFW, WITH FLAPS SELECTED TO 2 DEGREES FROM 5 DEGREES THE LEADING EDGE AMBER LIGHT REMAINED ON. IN ADDITION, NEITHER OUTBOARD OR INBOARD FLAP INDICATORS EVER INDICATED IN THE WHITE RADIAL AREA OF THE GAUGE. THE CREW DECIDED TO RETURN TO TOL AND DECLARED AN EMERGENCY. THE AIRCRAFT MADE A SUCCESSFUL LANDING WITH OUT FURTHER INCID ENT. MAINTENANCE RAN THE FLAPS UP AND DOWN USING BOTH THE NORMAL AND ALTERNATE METHODS OF EXTENSION. LUBRICATED ALL FL AP JACKS, AND COCKPIT HANDLE. ALL INDICATIONS WHERE NORMAL AND WERE IN THE WHITE RADIAL AREA. THE GREEN LEADING EDGE L IGHT ILLUMINATED EVERY TIME. SYSTEM OPERATIONAL CHECKED PER 727 MM WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO 2 L 7 3 4F A3WE 1999041700576 19990417 00576 WP 1999 4 17 GAIA9938A 1 19990318 A 3231 CONTROL CABLE DOUG DC9 DC915F 3022037 WP RT MLG DOOR FROZEN A GAIA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 562PC 47012 KHA - FLT 805 - SFO-SEA - ON APPROACH TO SEA THE FLIGHT CREW FOUND THE LANDING GEAR HANDLE STUCK IN THE UP POSITION. TH E CREW ELECTED TO USE ALTERNATE GEAR EXTENSION PROCEDURES AND MADE AN UNEVENTFUL LANDING. THE GEAR DOOR DRAGGED ON THE RUNWAY SURFACE ON TAXIING TO PARK. THE GEAR DOORS WERE REMOVED, REPAIRED AND REINSTALLED IAW CHAPTER 32-12-0 OF THE DC9 MM. INSPECTION FOUND A ICE BLOCK HANGING ON THE LANDING GEAR CONTROL VALVE CABLES IN THE RIGHT WHEEL WELL, THE ICE WAS REMOVED THE AIRCRAFT JACKED AND THE LANDING GEAR RETRACTED SEVERAL TIMES, NO DEFECTS NOTED WITH THE LANDING GEAR RETRAC T SYSTEM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999041700577 19990417 00577 NM 1999 4 17 ASAA9940065 1 19990315 A 5240 HINGE COVER BOEING 737 7374Q8 NM L2 DOOR BENT A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 778AS 25110 PDX - FLT 604 - PRIOR TO 604, THE L2 DOOR UPPER FORWARD HINGE COVER WAS FOUND TO BE BENT, CAUSING INTERFERENCE WITH DOOR OPENING. REMOVED HINGE COVER AND RELEASED PER CDL 52-40-6. DOOR OPERATED NORMALLY. MAINTENANCE SUBSEQUENTLY INSTALLE D A NEW UPPER FORWARD HINGE COVER AND THE DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999041700578 19990417 00578 WP 1999 4 17 ASAA9980064 1 19990318 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 3220 53077 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WOULD NOT TURN OFF. REPLACED THE LIGHT ASSEMBLY AN D OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999041700579 19990417 00579 NM 1999 4 17 ASAA9940066 1 19990316 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 15 DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 754AS 25095 PDX - PRIOR TO FLIGHT 343 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERTIVE AT ROW 15. RECONNECTED WI RING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999041700580 19990417 00580 NM 1999 4 17 ASAA9910021 1 19990313 A 3350 10617838 LIGHT GRIMES BOEING 737 737298C 1384490 NM BS 925 MISWIRED A ASAA K NONE L W NO TEST INADEQUATE Q C IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. INSPECTED AND FOUND S IGN L748 AT STATION 925 WIRING INOPERATIVE. REWIRED SIGN. LIGHT SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999041700581 19990417 00581 WP 1999 4 17 ASAA9980066 1 19990318 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999041700582 19990417 00582 NM 1999 4 17 ASAA9910022 1 19990316 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM ROW 10 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 740AS 22578 ANC - PRIOR TO FLIGHT 153, WOME EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED WITH THE SWITCH IN THE 'ARMED' OR 'OFF' PO SITION. REPLACED BATTERY AT ROW 10 AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999041700583 19990417 00583 NM 1999 4 17 ASAA9910024 1 19990321 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ON NR 1 SEAT PALLET. REPLACED BATTERY AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999041700584 19990417 00584 NM 1999 4 17 ASAA9910023 1 19990319 A 3350 6104781 BATTERY GRIMES BOEING 737 737290C 138448V NM ROW 3 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 730AS 22577 SEA - FLT 61 - AFTER RECON, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 3 WOULD NOT EXTINGUISH. REPLACED BATTERY AND THE LIG HTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999041700585 19990417 00585 EU 1999 4 17 SIMA990751 1 19990316 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 304AE 340B304 LAW - FLT 3848 - THE SECOND FROM THE FRONT DOOR PROXIMITY LIGHT DOES NOT ILLUMINATE. ISSUED MEL AGAINST THE EMERGENCY L IGHTING SYSTEM. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT ASSEMBLY ON 3-17-99. OPERATIONAL CHECK GOOD. RESTORED MEL ITEM AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999041700586 19990417 00586 EU 1999 4 17 SIMA990732 1 19990314 A 5330 S5367140620201 DOUBLER AEROSP ATR42 ATR42300 8680920 EU FRAME 32-33 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE INNER ANTENNA DOUBLER BETWEEN FRAME 32 AND 33 CORRODED. REMOVED AND REPLACED DOUBLER IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700587 19990417 00587 EU 1999 4 17 SIMA990731 1 19990314 A 5320 S5367800826451 PLATE AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE RIGHT FORWARD LAVATORY HOLD DOWN GUSSET PLATE CORRODED ON FRAME 40. REMOVED A ND REPLACED THE GUSSET PLATE IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700588 19990417 00588 EU 1999 4 17 SIMA990721 1 19990313 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY FALSE WARNING A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 381AE A5304 340B381 DFW - FLT 5054 - LAVATORY SMOKE ON CWP ILLUMINATED INFLIGHT. FLIGHT ATTENDANT FOUND THE LAVATORY WAS OCCUPIED, AND THE PERSON WAS REMOVED. AOM VOL 1 PROCEDURES WERE COMPLIED WITH. VERIFIED THE EVENT AS A FALSE WARNING. REMOVED AND REPLA CED THE LAV SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999041700589 19990417 00589 SO 1999 4 17 SIMA990691 1 19990310 A 2611 SMOKE DETECTOR EMB 145 EMB145LR SO BAGG COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 602AE 145048 DSM - FLT 4017 - ON APPROACH BAGGAGE SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. DECLARED EME RGENCY. LANDED SAFELY. DETERMINED TO BE A FALSE WARNING. DEFERRED BAGGAGE SMOKE WARNING SYSTEM. PERFORMED OPERATIONA L CHECK OF BAGGAGE SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. MEL ITEM RESTORED ON 3-18-99. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT T00011AT 1999041700590 19990417 00590 WP 1999 4 17 GTIA9900034 1 19990306 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 DTW - EMERGENCY FLOOR TRACK LIGHTS. FIRST LIGHT MISSING BULB AND COVER. REPLACED BULB AND COVER. OPERATION CHECKS GOO D. (M) 2 L 7 2 4F A6WE 1999041700591 19990417 00591 WP 1999 4 17 GTIA9900038 1 19990318 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 3-6 DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 ACY - INSTANTLY PRIOR TO DEPARTURE, CAPTAIN FOUND APPROXIMATELY SIX FEET OR FLOOR EMERGENCY LIGHTING OUT. ROW THREE TO SIX. FOUND DAMAGED WIRE HARNESS ROW SIX. REPAIRED WIRES. SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F A6WE 1999041700592 19990417 00592 WP 1999 4 17 GTIA9900039 1 19990310 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 DTW - FLT 675 - TWO SECTIONS OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. CHARGED BATTERY PACK SYSTEM. OPERATION CHE CK GOOD. (M) 2 L 7 2 4F A6WE 1999041700593 19990417 00593 WP 1999 4 17 GTIA9900033 1 19990303 A 3350 LIGHT DOUG DC9 DC932 3022066 WP ROW 17/18 MISWIRED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 12505 45788 DTW - EMERGENCY LIGHTS AT ROW 17 AND 18 WON'T LIGHT, OVERHEAD. UNCROSSED EMERGENCY AND STANDBY LIGHT WIRES. OPERATION CHECK GOOD IAW DC-9 MM 33-50-0. (M) 2 L 7 2 4F A6WE 1999041700594 19990417 00594 SO 1999 4 17 C2XA99IA179 1 19990304 A 3397 W220029624 WIRE EMB 120 EMB120RT SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999041700595 19990417 00595 SO 1999 4 17 C2XA99IA178 1 19990303 A 3350 GE1436 BULB EMB 145 EMB145 SO LT EMER EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15932 145015 IAH - DURING AIRCRAFT MODIFICATION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999041700596 19990417 00596 SO 1999 4 17 C2XA99IA177 1 19990222 A 5530 14531597601 ANGLE EMB 145 EMB145 SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14925 145004 IAH - DURING C-CHECK INSPECTIONI, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FO RWARD END. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW EMB145 SST 0391/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999041700597 19990417 00597 SO 1999 4 17 C2XA99IA176 1 19990222 A 5530 14531597601 ANGLE EMB 145 EMB145 SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14925 145004 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORW ARD END. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW EMB 145 SST 0391/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999041700598 19990417 00598 SO 1999 4 17 C2XA99IA190 1 19990313 A 3230 WHEEL EMB 145 EMB145LR SO NLG OUT OF POSITION A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 13949 145057 IAH - FLT 4126 - ON CLIMB, THE CREW REPORTED THAT THE NOSE GEAR WOULD NOT RETRACT. A FLY-BY OF THE TOWER WAS PERFORMED AND IT WAS DISCOVERED THAT THE NOSE WHEELS WERE TURNED AT A NINTY DEGREE ANGLE TO THE STRUT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, WHERE THE DISCREPANCY IS CURRENTLY UNDER INVESTIGATION. (M) 2 L 7 2 4T RT T00011AT 1999041700599 19990417 00599 NE 1999 4 17 C2XA99IA188 2 19990313 A 7261 OIL SYSTEM AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE REQ'D SERVICE A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 86842 286 120532 AEX - FLT 3373 - DURING TAKEOFF ROLL, THE CREW REPORTED THAT THE NR 2 ENGINE OIL MASTER WARNING LIGHT ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WHERE MAINTENANCE SERVICED THE NR 2 ENGINE WITH OIL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999041700600 19990417 00600 SO 1999 4 17 C2XA99IA187 1 19990315 A 3350 AD2047 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY AISLE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A31SO 1999041700601 19990417 00601 SO 1999 4 17 C2XA99IA184 1 19990311 A 2150 22051201 ACM EMB 120 EMB120RT SO RIGHT INOPERATIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 12709 120101 IAH - FLT 3686 - DURING CLIMB, THE CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT, WHE RE MAINTENANCE UNSTUCK THE RIGHT ACM AND OPERATIONALLY CHECKED IAW EMB120 SRM 21-60-00, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. THE PROBLEM REPEATED ON FINAL FOR FLIGHT 3686 WHERE THE AIRCRAFT LANDED AT MLU WITHOUT INCIDENT. M AINTENANCE PLACED THE RIGHT ACM ON MEL NR 21-50-2 CONTROL NR 173565, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1999041700602 19990417 00602 SO 1999 4 17 C2XA99BT007 1 19990309 A 3230 355022002 LGEU EMB 145 EMB145LR SO LANDING GEAR MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 09 14950 1102 145061 LG AIR/GND FAIL MESSAGE IN FLIGHT. REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT (LGEU) IAW EMB145 MM 32-32-01. OP S CHECK GOOD. THIS WAS AN AIR RETURN. (M) 2 L 7 2 4T RT T00011AT 1999041700603 19990417 00603 EU 1999 4 17 C2XA99IA185 1 19990309 A 2612 MT30K1407PN CONNECTOR AEROSP ATR42 ATR42320 8680930 EU NR 2 ENGINE DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SW 09 86842 286 CRP - FLT 3432 - THE CREW REPORTED AN INTERMITTENT FIRE WARNING ON THE NR 2 ENGINE, THE AIRCRAFT RETURNED TO CRP WHERE I T LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE CANNON PLUGS FOR BOTH THE 'A' AND 'B' FIRE LOOPS AND OPERATIONALLY C HECKED IAW ATR42-320 JIC 26-12-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999041700604 19990417 00604 SO 1999 4 17 C2XA99IA166 1 19990301 A 3350 1149 CHARGER EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14950 145061 IAH - DURING 3A CHECK, FOUND LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NR 4 EMERGENCY BATTERY PACK CHARGER/INVERTER IAW EMB-145 MM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999042100001 19990421 00001 NM 1999 4 21 PCAA9900008 1 19990405 A 7997 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 OIL TEMP BROKEN A PCAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 13 808EX 299 120889 BDL-FLT3871, DURING CRUISE FLIGHT THE NR 1 ENGINE OIL TEMPERATURE WAS ERRATIC, TEMPERATURE PEGGED AT 150 DEGREES CELSIUS FOR 60 SECONDS. CREW SECURED NR 1 ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPAIRED A BROKEN WIR E AT THE TEMP BULB ELECTRICAL CONNECTOR. GROUND RUN SATISFACTORY. 2 H 7 2 4T 4 T RT A13NM E20NE 1999042100002 19990421 00002 SO 1999 4 21 PNSA990303 1 19990319 A 7714 576AW INDICATOR PIPER PA31 PA31350 7103110 SO RT ENGINE RPM INOPERATIVE A PNSA A UNSCHED LANDING O OTHER AP APPROACH 1 AL 03 15PR 318052011 ON APPROACH TO MYU, RT ENGINE RPM INDICATION WENT TO ZERO, ENGINE RUNNING OK. RETURNED TO BET FOR UNEVENTFUL LANDING. R EPLACED RPM INDICATOR, OPS CHECKED OK. 1 L 7 2 3O A20SO 1999042100003 19990421 00003 SW 1999 4 21 PNSA990304 1 19990327 A 2131 SEAL SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR OUT OF ADJUST A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 650PA AC775B ON CLIMBOUT FROM BET, AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO BET FOR MAINTENANCE. PRESSURIZATION DEFERRED. AIRCRA FT RETURNED TO ANC. ADJUSTED CARGO DOOR SEAL INFLATION VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4T RT A8SW 1999042100004 19990421 00004 WP 1999 4 21 CALA9900359 1 19990406 A 5530 ANGLE DOUG DC10 DC1030 3023501 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 3 INCH CRACK IN LT AND RT DRAG ANGLES BELOW NR 2 ENGINE AT THIRD BANJO FITTING. THE CRACKS WERE STOP DRILLED AND REPAIR ANGLES WERE INSTALLED IAW SRM 55-20-00, FIGURE 3. 2 L 7 3 4F A22WE 1999042100005 19990421 00005 WP 1999 4 21 CALA9900360 1 19990406 A 5280 DOOR DOUG DC10 DC1030 3023501 WP LT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 4 INCH CRACK IN Z SECTION AT FORWARD CORNER OF LT MLG DOOR. THE DOOR WAS REPAIRED IAW SRM 52-10-00, FIGURE 15. 2 L 7 3 4F A22WE 1999042100006 19990421 00006 NM 1999 4 21 CALA9900361 1 19990406 A 3350 20131A BATTERY PACK RADIANT BOEING 757 757224 1384958 NM ROW 28 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND MID CABIN (ROW 28) EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK AND CHARGER WERE REMOVED AND RE PLACED IAW MM 33-51-07. 2 L 7 2 4F RT A2NM 1999042100007 19990421 00007 NM 1999 4 21 CALA9900362 1 19990407 A 5753 652163479 SKIN BOEING 727 727243 138408D NM LT TE FLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND LT INBOARD AFT FLAP LOWER SURFACE DEBONDED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-2. 2 L 7 3 4F RT A3WE 1999042100008 19990421 00008 NM 1999 4 21 CALA9900363 1 19990407 A 5753 SKIN BOEING 727 727243 138408D NM LT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND LT O/B FLAP AFT SEGMENT UPPER SURFACE DENTED AND DEBONDED. THE FLAP WAS REPAIRED IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1999042100009 19990421 00009 NM 1999 4 21 CALA9900364 1 19990407 A 5753 652163586A SKIN BOEING 727 727243 138408D NM RT TE FLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND RT O/B FLAP AFT SEGMENT DEBONDED AT TRAILING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11. 2 L 7 3 4F RT A3WE 1999042100010 19990421 00010 NM 1999 4 21 CALA9900365 1 19990407 A 5315 FLOORBEAM WEB BOEING 727 727243 138408D NM BS 294 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 3 INCH CRACK IN FLOORBEAM WEB AT FS 294, RBL 48. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTAL LED IAW SRM 51-40-2 FIGURE 1, SHEET 6. 2 L 7 3 4F RT A3WE 1999042100011 19990421 00011 NM 1999 4 21 CALA9900366 1 19990407 A 5754 CHORD BOEING 727 727243 138408D NM NR 7 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 3 INCH AND .375 INCH CRACK AT RT WING NR 7 SLAT LOWER CHORD. THE LOWER SLAT PANEL WAS REMOVED FOR AC CESS AND REMOVED ANGLE IAW SRM 51-30-2, PAGE 1. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-20 AND 51-30-2. REINSTALLED AC CESS PANEL IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 1999042100012 19990421 00012 NM 1999 4 21 CALA9900367 1 19990407 A 5754 CHORD BOEING 727 727243 138408D NM NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .3125 INCH CRACK AT LT WING NR 1 SLAT LOWER CHORD AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRA CK WAS STOP DRILLED AND AN ANGLE REPAIR WAS INSTALLED IAW SRM 57-30-2. 2 L 7 3 4F RT A3WE 1999042100013 19990421 00013 NM 1999 4 21 CALA9900368 1 19990407 A 5754 CHORD BOEING 727 727243 138408D NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .375 INCH AND .125 INCH CRACK AT LT WING NR 2 SLAT LOWER CHORD BELOW TELESCOPING ANT-ICE TUBE. THREE ACCESS PANELS WERE REMOVED PER SRM 51-30-2 AND THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1, PAGE 6B. AN ANGLE REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 51-40-1. THE THREE ACCESS PANELS WERE REINSTALLED IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 1999042100014 19990421 00014 NM 1999 4 21 CALA9900369 1 19990407 A 5320 PRESSURE DECK BOEING 727 727243 138408D NM BS 270 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 3.5 INCH CRACK IN NOSE WHEEL WELL PRESSURE DECK AT FS 270, LBL 14. THE CRACKED AREA WAS CUT OUT, A D OUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F RT A3WE 1999042100015 19990421 00015 NM 1999 4 21 CALA9900370 1 19990407 A 5312 BULKHEAD ANGLE BOEING 727 727243 138408D NM BS 870 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .75 INCH CRACK IN FWD BULK VERT ANGLE AT RT WHEEL WELL BS 870 KEEL BEAM. THE FWD BULK VERT ANGLE WAS REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-30-5, PAGE 1. 2 L 7 3 4F RT A3WE 1999042100016 19990421 00016 WP 1999 4 21 9901331147 1 19990307 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1473 1513 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 147US 46756 DURING M-CHECK, FOUND CORROSION ON LONGERON 29R AT FS 1473 TO 1513 AT WS XCW118-XCW119. REPAIRED PER EA 164779. 2 L 7 3 4F A22WE 1999042100017 19990421 00017 WP 1999 4 21 9901341161 1 19990218 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1522 1540 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING M-CHECK, FOUND CORROSION ON LONGERON 27R WEB STRUCTURE AT FS 1522 TO 1540. REPAIRED PER EA 11-162951. 2 L 7 3 4F A22WE 1999042100018 19990421 00018 WP 1999 4 21 9901359902 1 19990405 A 5712 RIB DOUG DC9 DC931 3022065 WP WS 520.509 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 47073 DURING PERIODIC CHECK, FOUND LEADING EDGE RIB CRACKED AT WS 520.937. REPAIRED PER EA 99-164056. 2 L 7 2 4F A6WE 1999042100019 19990421 00019 SO 1999 4 21 COMA9910056 1 19990406 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT SECURED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 258CA 120247 SERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND SECURED FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1999042100020 19990421 00020 SO 1999 4 21 COMA9910057 1 19990406 A 5610 NP1513111 WINDSHIELD EMB 120 EMB120RT SO LEFT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 462CA 157 120264 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4T RT A31SO 1999042100021 19990421 00021 SO 1999 4 21 COMA9910058 1 19990407 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 256CA 120245 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN. 2 L 7 2 4T RT A31SO 1999042100022 19990421 00022 EA 1999 4 21 COMA9960145 1 19990403 A 2910 60075239806 TUBE CNDAIR CL600 CL6002B19 EA NR 3 HYD PUMP LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 HYDRAULIC LINE LEAKING AT SYSTEM NR 3 PUMP. REPLACED LINE. 2 L 7 2 4F RT A21EA 1999042100023 19990421 00023 EA 1999 4 21 COMA9960146 1 19990404 A 2710 10231007 DAMPENER CNDAIR CL600 CL6002B19 EA LEFT WING LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 3685 7031 DURING C-CHECK, FOUND LEFT AILERON FLUTTER DAMPENER LEAKING. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999042100024 19990421 00024 EA 1999 4 21 COMA9960147 1 19990403 A 2750 601R93106505 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 RIGHT WING FLEXSHAFT WORN BEYOND LIMITS. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1999042100025 19990421 00025 EA 1999 4 21 COMA9960148 1 19990407 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DEFECTIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 948CA 7079 EMERGENCY FLOOR LIGHTING, AFT SECTION, IS INOPERABLE. REPLACED WIRE CONNECTOR. 2 L 7 2 4F RT A21EA 1999042100026 19990421 00026 EA 1999 4 21 COMA9960149 1 19990406 A 2120 AIR DISTRIBUTION CNDAIR CL600 CL6002B19 EA COCKPIT ODOR A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 713CA 7245 EXHAUST FUMES IN COCKPIT AND CABIN DURING FLIGHT. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999042100027 19990421 00027 NM 1999 4 21 UPS99229205 1 19990408 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-N/A, PREFLIGHT COCKPIT EMERGENCY EXIT LIGHT OPS CHECK BAD. REPLACED BATT PACK, OPS CK GOOD. 2 L 7 3 4F A3WE 1999042100028 19990421 00028 WP 1999 4 21 UPS99829195 1 19990321 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 766.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, LT WING L/E UPPER RIB IS CRACKED AT FS 766.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042100029 19990421 00029 WP 1999 4 21 UPS99829196 1 19990321 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 257 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, RT WING L/E SKIN AT FS 257 IS CRACKED ON TOP. REPAIRED AREA IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1999042100030 19990421 00030 WP 1999 4 21 UPS99829197 1 19990322 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 16.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, LT WING L/E LOWER SKIN AT STA, XOLDI6.225 IS CRACKED. REPAIRED AREA IAW DC8-5720-7767A. 2 L 7 4 4F RT 4A25 1999042100031 19990421 00031 WP 1999 4 21 UPS99829198 1 19990324 A 5320 37544731 FITTING DOUG DC8 DC871F 302199D WP BS 390 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, STA 390 AT STR 31L, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042100032 19990421 00032 WP 1999 4 21 UPS99829199 1 19990322 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 291.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1 LT WING L/E UPPER RIB IS CRACKED AT FS 291.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2 . 2 L 7 4 4F RT 4A25 1999042100033 19990421 00033 WP 1999 4 21 UPS99829200 1 19990322 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 759-766 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1 MAIN CABIN AT STA 759 TO 766 RBL 60, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED SEAT T RACK FROM STA 749 TO 970 AT RBL 60 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999042100034 19990421 00034 WP 1999 4 21 UPS99829201 1 19990322 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 590 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, MAIN CABIN AT STA 590, LBL 59, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED TRACK FROM STA 570 TO 690 AT LBL 60 IAW SRM 53-7-1. 2 L 7 4 4F RT 4A25 1999042100035 19990421 00035 WP 1999 4 21 UPS99829202 1 19990322 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, MAIN CABIN AT STA 1140 AND RBL 48, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED SEAT TR ACK FROM STA 1050 TO 1190 AT RBL 48 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999042100036 19990421 00036 WP 1999 4 21 UPS99829203 1 19990401 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE-C1, RT WING L/E RIBS AT THE FOLLOWING STA'S ARE CRACKED: FS 467.323, FS 442.185, XOLDI6.225, FS 366.50 0, FS 360.250 AND FS 354. STOP DRILLED CRACK'S AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042100037 19990421 00037 WP 1999 4 21 UPS99829206 1 19990406 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-N/A, ON PRE-DEPARTURE FOUND EMER EXIT LIGHTS INOP. REMOVED AND REPLACED EMER EXIT LIGHT BATT PACK, OPS CKS OK. (P/N 570 8458-503) (S/N 177) ON, (P/N 60-1223-5) (S/N 356) OFF. 2 L 7 4 4F RT 4A25 1999042100038 19990421 00038 NM 1999 4 21 QXEA9900546 1 19990403 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTION A QXEA K NONE N FALSE WARNING AP APPROACH 1 NM 09 360PH 515 PDX- ON APPROACH, MASTER WARNING LIGHT ILLUMINATED WITH SMOKE WARNING LIGHT (BAGGAGE COMPARTMENT) INTERMITTENTLY ILLUMIN ATED. MAINTENANCE REPLACED BOTH CARGO COMPARTMENT SMOKE DETECTORS, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999042100039 19990421 00039 NM 1999 4 21 QXEA9900547 1 19990401 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTION A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 369PH 197 513 PDX- VERY BRIEF AND INTERMITTENT MASTER WARNING LIGHT ILLUMINATED WITH SMOKE WARNING LIGHT. BAGGAGE SMOKE DETECTORS TES T OK. MAINTENANCE REPLACED NR 2 SMOKE DETECTOR, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999042100040 19990421 00040 NM 1999 4 21 QXEA9900548 1 19990331 A 3220 88357 TRAILING ARM DHAV DHC8 DHC8102 2809003 NM NLG GOUGED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 825PH 26688 5206 213 SEA- NOSE WHEEL SWIVEL GOUGED APPROX .035 DEEP. AIRCRAFT FERRIED FROM SEA TO PDX FOR REPAIRS. IN PDX, MAINTENANCE REMO VED THE DAMAGED TRAILING ARM, AND THE UNDAMAGED AXLE AS A UNIT. REPLACED WORN CONNECTION LINK PIN. INSTALLED OVERHAULE D TRAILING ARM, AND NEW AXLE IAW CMM 32-20-01, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999042100041 19990421 00041 NM 1999 4 21 99FDEA00137 1 19990407 A 5320 65429491 SPLICE BOEING 727 727247 138408F NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 UPON REMOVAL OF STR ON NR 303 FOUND CORROSION ON STR SPLICE STR 26L, BS 480. *S/D* REMOVED AND REPLACED STR SPLICE PER IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1999042100042 19990421 00042 WP 1999 4 21 ABXA9900280 1 19990407 A 2720 57155A PUMP DOUG DC8 DC862 3021970 WP RUDDER CONTROL LEAKING A ABXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 808AX 81515 1516 45954 DURING CRUISE, ONE HOUR AND TWENTY MINUTES INTO FLIGHT EXPERIENCED LOSS OF HYDRAULIC QUANTITY DOWN TO STANDPIPE. PERFOR MED LOSS OF HYDRAULICS PROCEDURES. REPLACED STANDBY RUDDER PUMP IAW DC8 MM 29-27-00, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999042100043 19990421 00043 WP 1999 4 21 MWEA99131 1 19990406 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP ROW 11-14 DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE MAIN CABIN CEILING EMERGENCY LIGHTS ARE INOPERATIVE FROM ROW 11 TO ROW 14. MTC REMOVED AND REPLACED EMERGENCY BATTE RY PACK BATTERIES. 2 L 7 2 4F A6WE 1999042100044 19990421 00044 NM 1999 4 21 MWEA99132 1 19990407 A 5320 575468828 DOUBLER DOUG MD88 MD88 3023688 NM COCKPIT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FOUND COUNTER SINK CRACKS ON STEEL DOUBLER AT UPPER AFT CORNER OF RIGHT CLEARVIEW RETAINER. MTC FABRICATED AND INSTALLE D DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999042100045 19990421 00045 WP 1999 4 21 MWEA99133 1 19990407 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 THE GALLEY DOOR SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999042100046 19990421 00046 NM 1999 4 21 DL76L990650 1 19990325 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM ROW 6-20 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 177DN 25122 SEAT 6 TO 20 EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK, CKS OK. 2 L 7 2 4F RT A1NM 1999042100047 19990421 00047 NM 1999 4 21 DL76L990676 1 19990328 A 3350 BATTERY PACK 20131A BOEING 767 767332 1382001 NM 2L DOOR. DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 177DN 6282 25122 ON LAYOVER CHECK, FOUND 2L DOOR AREA EMERGENCY LIGHTS OUT. REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1999042100048 19990421 00048 1999 4 21 DL76L990720 4 19990331 A 2330 MONITOR BOEING 767 767332 1382001 NM CABIN FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 180DN 25985 ACFT DIVERTED TO YYT WITH SMOKE FROM FWD VIDEO MONITOR. FERRIED TO ATL FOR EVALUATION. INSPECTED ALL FWD CABIN AREA, V IDEO SYSTEM COMPONETS, SEATS AND GALLEY AREA AND NO SIGNS OF OVERHEATING FOUND OR NOTED. REPLACED RT FWD BULKHEAD VIDEO MONITOR AND VDU AS PRECAUTIONARY. OPERATED SYSTEMS FOR THREE HOURS ON GROUND, NO PROBLEMS NOTED DURING THIS PERIOD OF TESTING. 2 L 7 2 4F RT A1NM 1999042100049 19990421 00049 NM 1999 4 21 DL72S990738 1 19990405 A 3350 0201720001 LIGHT BOEING 727 727232 1384082 NM ROW 20 DEF BROKEN A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 489DA 21019 SEAT 20D EMERGENCY LIGHT AND WIRES HANGING OUT. REPAIRED OR REPLACED SAME. 2 L 7 3 4F A3WE 1999042100050 19990421 00050 NM 1999 4 21 DL733990739 1 19990405 A 3260 SWITCH BOEING 737 7373L9 1384470 NM GEAR HANDLE STICKING A DALA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 SO 27 232DZ 24220 LANDING GEAR SHOWED 3 GREEN AND 3 RED GEAR LIGHTS ON EXTENSION. FOUND GEAR HANDLE SWITCH STUCK. CLEANED WITH CONTACT C LEANER, ALL GEAR INDICATION NOW NORMAL. CLEANED VIEWING PORTS AND LAND WARNING INHIBIT SYSTEM, ALL CKS GOOD. 2 L 7 2 4F RT A16WE 1999042100051 19990421 00051 NM 1999 4 21 DL72K990740 1 19990405 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 910 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 A .25 INCH CRACK ON ANGLE FWD SIDE OF FS 910 RT ABOVE AND FWD OF H BRACKET. REPAIRED PER MM 53-11-0, TIME LIMITED REPAI R. 2 L 7 3 4F A3WE 1999042100052 19990421 00052 NM 1999 4 21 DL76G990741 1 19990405 A 2613 LOGIC CARD 285N002817 BOEING 767 767324 NM GE CF6 CF680C2B6 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 394DL 27394 704233 LEFT ENGINE OVERHEAT LIGHT PASSING 10,000 FT, LIGHT EXTINGUISHED WHEN POWER REDUCED. INSPECTED OVERHEAT LOOP AT LEFT EN GINE, CHECKS OK. MOTORED ENGINE, INSPECTED FOR AIR LEAKS AT LOOP AREA, NO LEAKS. REPLACED LOGIC TEST CARD M10224. RAN ENGINE AT T/O POWER, SYSTEM NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 1999042100053 19990421 00053 NM 1999 4 21 DL72S990742 1 19990404 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 460-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTER NAL HFEC INSPECTION CONFIRMED 14 CRACKS IN 6 DIFFERENT FRAME BAYS. THE ENTIRE SKIN LAP WAS CUTOUT TO REMOVE ALL CRACKS AND REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 367077-14AD, REV B. EXISTING ADJACENT CORROSION REPAIRS WERE INCORPORATE D INTO THE LAP REPAIR. 2 L 7 3 4F A3WE 1999042100054 19990421 00054 NM 1999 4 21 DL72S990743 1 19990403 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 480-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A FEW CRACKS IN CONSECUTIVE SKIN FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR. THE SKIN FROM FS 480 TO 520 WAS REPLACED WITH A NEW PIECE TO ELIMINATE EXISTING CORROSION REPAIRS. 2 L 7 3 4F A3WE 1999042100055 19990421 00055 NM 1999 4 21 DL72S990744 1 19990404 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367111-14AD. 2 L 7 3 4F A3WE 1999042100056 19990421 00056 NM 1999 4 21 DL72S990745 1 19990403 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 LFEC INSPECTION OF THE STINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CUT OUT ALONG T HE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367110-14AD. 2 L 7 3 4F A3WE 1999042100057 19990421 00057 NM 1999 4 21 DL72S990746 1 19990401 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 25 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG TH E PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366977-14AD, REV D. 2 L 7 3 4F A3WE 1999042100058 19990421 00058 NM 1999 4 21 DL72S990747 1 19990401 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 11 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT OVER THE LENGTH OF THE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366976-14AD, REV B. 2 L 7 3 4F A3WE 1999042100059 19990421 00059 NM 1999 4 21 DL72W990748 1 19990402 A 5330 65545664 SKIN BOEING 727 7272Q8 138407W NM BS 540-560 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED A CRACK IN THE LOWER FASTENER ROW O F THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 540 AND 560. THE CRACKS WERE CUT OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367107- 14AD. 2 L 7 3 4F A3WE 1999042100060 19990421 00060 NM 1999 4 21 DL72S990751 1 19990217 A 5753 652163361 SKIN BOEING 727 727232 1384082 NM LT TE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 LOWER L/E SKIN WORN O/B END OF FLAP APPROX 6 INCHES LONG. REPAIRED PER MM 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999042100061 19990421 00061 NM 1999 4 21 DL72W990752 1 19990406 A 5330 6518420119 SKIN BOEING 727 727247 138408F NM BS 300 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 THE FUSELAGE SKIN PANEL BETWEEN FS 259.5 AND 360 AND BETWEEN STRINGER 19R AND 24R WAS FOUND WITH SEVERAL AREAS OF CORROS ION. THE PANEL WAS REMOVED AND A NEW BOEING SKIN PANEL INSTALLED PER ER/A 366991-14. 2 L 7 3 4F A3WE 1999042100062 19990421 00062 NM 1999 4 21 DL72W990753 1 19990406 A 5330 65545672 SKIN BOEING 727 727247 138408F NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 9 CRACKS IN THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE LE NGTH OF THE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367124-14AD. 2 L 7 3 4F A3WE 1999042100063 19990421 00063 NM 1999 4 21 DL72W990754 1 19990407 A 5330 651842012 SKIN BOEING 727 727247 138408F NM BS 259.5-360 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 ON HUSH-KIT MOD OPN 57118, LOWER SKIN LAP JOINT INSPECTION FOUND CORROSION ON FUSELAGE SKIN BETWEEN BONDED METAL SKIN LA YERS AT STATION 259.5R TO 360R. REPLACED SKIN SECTION WITH A/C SKIN SECTION FROM MANUFACTURER. 2 L 7 3 4F A3WE 1999042100064 19990421 00064 NM 1999 4 21 DL72W990755 1 19990406 A 5330 655457416 SKIN BOEING 727 727247 138408F NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 41 CRACKS ALONG THE PANEL. THE LAP SPLICE WAS CUT OUT ALONG THE PAN EL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367123-14AD. 2 L 7 3 4F A3WE 1999042100065 19990421 00065 NM 1999 4 21 DL72W990756 1 19990406 A 5330 65545703 SKIN BOEING 727 727247 138408F NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN TWO CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CU T OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367122-14AD. 2 L 7 3 4F A3WE 1999042100066 19990421 00066 NM 1999 4 21 DLM88990757 1 19990407 A 3260 PSEU 833604 DOUG MD88 MD88 3023688 NM LANDING GEAR MALFUNCTIONED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 930DL 658 49717 FLAPS AT 11 DEGREES GEAR HANDLE UP, NOSE RED LIGHT CAME ON. ALSO, FLAP/SLAT IND DISAG / AUTO/LAND WERE FLICKERING ON. W HEN GEAR HANDLE DOWN, RT MAIN GREEN IND HAD RED LIGHTS FLICKERING. INSPECTED GEAR AND FLAPS/SLATS, CLEANED NOSE AND MLG DOWNLOCKS, UPLOCKS AND AIR GROUND, SENSORS. REPLACED PSEU AND TESTED OK PER MAINT MANUAL. 2 L 7 2 4F RT A6WE 1999042100067 19990421 00067 NM 1999 4 21 DLM88990758 1 19990407 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 973DL P80509 53241 AFT LAV SMOKE ALARM SET OFF FOLLOWING TAKEOFF AND DURING CLIMB. F/A SMELLED SMOKE AND VERIFIED NO FIRE. RETURNED TO JF K, SMOKE ALARM RESET ITSELF AND F/A STATED SMOKE ODOR DISAPPEARED. INSPECTED LAVS, AFT GALLEY, TAIL COMP, FOUND NO ODOR . VISUAL CHECK NORMAL. FOUND APU INLET SATURATED WITH OIL. RAN ENGS AND PACKS NO ODOR AND NO SMOKE. REPLACED COALESC ER BAGS. CLEANED APU INLET AND PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1999042100068 19990421 00068 NM 1999 4 21 DLM88990759 1 19990405 A 2121 FAN 6054578 DOUG MD88 MD88 3023688 NM COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 995DL 53362 CLIMBING THRU 14,000 FT, ELECTRICAL ODOR IN COCKPIT AND FWD CABIN. AIR TURNBACKTO MEM. FOUND RECIRC FAN AT FAULT. REP LACED SAME. 2 L 7 2 4F RT A6WE 1999042100069 19990421 00069 NM 1999 4 21 DL73K990760 1 19990407 A 3510 MC1025104 MASK BOEING 737 737232 1384475 NM COCKPIT LEAKING A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 303DL 23075 IN CRUISE, O2 GAUGE INDICATED ZERO. SUPPLY AT MASK NIL. ACCOMPLISHED POM PROCEDURE. REPLACED BOTTLE AND FOUND OBS MASK LEAKING. REPLACED MASK, SYS LEAK CHECKS OK. 2 L 7 2 4F RT A16WE 1999042100070 19990421 00070 NM 1999 4 21 DL73E990762 1 19990407 A 3233 FITTING 69598862 BOEING 737 737247 138448D NM RT MLG ACT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 ON TRANS CHECK, FOUND RT MAIN GEAR RETRACT ACTUATOR O/B ATTACH FITTING BROKEN FREE FROM SPAR. REPLACED SHEARED BOLTS, C RACKED FITTING AND INSPECTED SPAR. 2 L 7 2 4F A16WE 1999042100071 19990421 00071 NM 1999 4 21 DL72K990763 1 19990406 A 3350 6013211 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA 21232 POWER SUPPLY FOR EXTERNAL EMERGENCY LIGHTING INOPERATIVE. PART REPLACED (P/N 60-1321-1 DDL) (P/N 334701742) (S/N 8869). EMERGENCY LIGHTING CHECKS GOOD. 2 L 7 3 4F A3WE 1999042100072 19990421 00072 NM 1999 4 21 DL72L990764 1 19990407 A 3350 BATTERY 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 505DA A10622 21307 RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY AT M957, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999042100073 19990421 00073 WP 1999 4 21 DLL19990765 1 19990407 A 3350 3071 BULB LKHEED 1011 10113853 5265020 WP ROW 20 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 769DL 193H1218 EMERGENCY TRACK LIGHTING MISSING BY SEAT 20C, TRACK BROKEN. RELAMPED AND REPLACED TRACK, OPS CHECK GOOD. 2 L 7 3 4F A23WE 1999042100074 19990421 00074 WP 1999 4 21 DLL19990766 1 19990407 A 3350 5165741 BATTERY LKHEED 1011 10113853 5265020 WP ROW 13 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 769DL 193H1218 EMERGENCY EXIT LIGHT BY L-2 DOOR INOP ON FUSELAGE. REPLACED EMERGENCY BATTERY ABOVE SEAT ROW 13 SEATS A AND B, OPS CHEC K GOOD. 2 L 7 3 4F A23WE 1999042100075 19990421 00075 1999 4 21 DHL99727001 4 19990408 A 3425 2588370908 ADI BOEING 727 727228 NM RIGHT COCKPIT FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 727DH 20204 FIRST OFFICERS ADI FAILED, HAS OFF FLAG AND ADI TUMBLED. RERACKED ADI. 2 L 7 3 4F A3WE 1999042100076 19990421 00076 GL 1999 4 21 DHL99805001 2 19990403 A 7314 6411194 FUEL PUMP DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C5 GL NR 1 ENGINE FAILED A DHLA K NONE X ENGINE FLAMEOUT CR CRUISE 1 SO 01 805DH 46125 NR 1 ENGINE FLAMED OUT TWICE WITH TWO HUNG STARTS. REPLACED NR 1 NASH PUMP, CHECKED BOOST PUMPS AND REPLACED NR 1 ENG F UEL FILTER. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999042100077 19990421 00077 EU 1999 4 21 CA990318012 2 19990307 A 7250 EU33245 BLADE FOKKER F28 F28MK3000 4990809 EU RROYCE SPEY SPEY55515P 54521 EU NR 1 ENGINE FAILED W E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA 26076 9241 (CAN) IN CRUISE AT FL 325, THE CREW HEARD A LOUD BANG FROM NR 1 ENGINE, FOLLOWED BY ALL ENGINE PARAMETERS DROPPING OFF. ENGINE WAS SHUTDOWN AND AIRCRAFT CONTINUED TO ITS DESTINATION WHERE AN UNEVENTFUL LANDING WAS CARRIED OUT. INITIAL INS PECTION FOUND NR 1 ENGINE LOW PRESSURE TURBINE HAD SUFFERED A MULTIPLE BLADE FAILURE. FURTHER INSPECTION REVEALED THE E XHAUST PIPE SHOWED VARIOUS DENTS AND HOLES WHERE BLADE FRAGMENTS HAD EXITED REARWARD. AUDIT OF THE ENGINES HISTORY SHOW S THE TURBINE MODULE HAD RECEIVED A LEVEL 2 AND 3 SHOP VISIT 3,095 CYCLES AGO. THE SUBJECT LP2 TURBINE IS HIGH CYCLE AT 25,997 CYCLES, OUT OF SERVICE AT 30,000 CYCLES. THE ENGINE IS PRE-MOD NR 6329. 2 L 7 2 4F 4 F RT A20EU E2EU 1999042200001 19990422 00001 EU 1999 4 22 MALA976406 1 19990323 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 402XJ 340B402 FA REPORTED SMOKE IN CABIN ADJACENT TO SEAT 3D IN AREA OF SIDEWALL LIGHT. SMOKE SUBSIDED WHEN SIDEWALL LIGHTS TURNED OF F. MAINTENANCE FOUND SIDEWALL WINDOW LIGHTING SEAT 3D CHARRED AT CONNECTION AS WELL AS THE SOCKET. 2 L 7 2 4T RT A52EU 1999042200002 19990422 00002 SO 1999 4 22 C2XA99IA019 1 19990111 A 3350 7287103503 CONTROL MODULE EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16961 145103 IAH - DURING CONFORMITY CHECK WHILE PERFORMING EMERGENCY LIGHT FUNCTIONAL CHECK, FOUND THE EICAS INDICATED 'EMERGENCY LI GHTS NOT ARMED' WITH THE LIGHTS PLACED IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROL MODULE IAW EMB-145 MM 33-21-01 AND PERFORMED FUNCTIONAL CHECK OF THE EMERGENCY LIGHTS IAW EMB-145 MM 33-50-00. THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999042300227 19990423 00227 NM 1999 4 23 TWAA9905501 1 19990415 A 5754 SKIN BOEING 767 767231 1385131 NM NR 9 LE SLAT MISREPAIRED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 604TW 22567 DURING CHECK-C, MAINT FOUND NUMBER 9 LE SLAT WITH A REPAIR HAVING SEALANT PEELING OFF. INSTALLED A 7 IN BY 3 IN HOT BON D REPAIR PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1999042300228 19990423 00228 NM 1999 4 23 HNAA9900043 1 19990409 A 2540 SPRING DHAV DHC8 DHC8102 2809003 NM LAV TRASH BIN BROKEN A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 936HA 145 LAVATORY TRASH BIN DOOR WILL NOT STAY CLOSED. REPLACED BROKEN SPRING ON TRASH BIN DOOR. 2 H 7 2 4T RT A13NM 1999042300229 19990423 00229 NM 1999 4 23 HNAA9900044 1 19990410 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 961HA 333 SECOND FROM LAST FLOOR EMERGENCY LIGHT INOPERATIVE. REATTACHED WIRE. 2 H 7 2 4T RT A13NM 1999042300230 19990423 00230 NM 1999 4 23 HNAA9900045 1 19990410 A 5320 RAIL DHAV DHC8 DHC8102 2809003 NM BS 215 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 975HA 176 CORROSION ON RT CENTER FLOORBOARD RAIL AT FRAME 215.00 ON TOP FLANGE .025 DEEP, ON OUTER FLANGE .035 DEEP AND ON INBOARD SIDE OF OUTER FLANGE .016 DEEP. BLENDED CORROSION FROM RAILS. 2 H 7 2 4T RT A13NM 1999042300231 19990423 00231 NM 1999 4 23 HNAA9900046 1 19990411 A 5400 INTERCOSTAL DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 009 NR 1 NACELLE DOOR OUTBOARD INTERCOSTAL CRACKED AT FORWARD HINGE BRACKET. REPAIRED INTERCOSTAL. 2 H 7 2 4T RT A13NM 1999042300232 19990423 00232 NM 1999 4 23 HNAA9900047 1 19990408 A 5400 RIVETS DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE LOOSE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 975HA 176 TWELVE WORKING RIVETS ON INBOARD WALL OF NR 2 NACELLE (ALL RIVETS ON STRAP) AT GROUND POWER CONNECTOR. REPLACED RIVETS. 2 H 7 2 4T RT A13NM 1999042300233 19990423 00233 SO 1999 4 23 LR7A9906 1 19990411 A 5320 39148114 BEAM LKHEED 382 382G 526414U SO BS 528 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND FS 528 RT MLG BEAM, INNER BEAM CRACKED AT BL62R, WL 256. REPAIRED BY CUTTING OUT CRACK AND INSTALL FILLER, STRAPS AND ANGLES IAW SPAR MPP L100-404-99-001. LAC MEA 382-53-99-004. 2 H 7 4 4T A1SO 1999042300234 19990423 00234 SO 1999 4 23 LR7A9907 1 19990411 A 5400 3701311L CHANNEL LKHEED 382 382G 526414U SO BS 512.64 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND NR 2 UPPER AFT NACELLE LOWER LT CHANNEL CRACKED AT FS 512.64, PP WL -5.38. RE PAIRED BY INSTALLING REPAIR DOUBLER IAW SPAR MPP L100-404-99-004. LAC MEA 382-53-99-006. 2 H 7 4 4T A1SO 1999042300235 19990423 00235 SO 1999 4 23 LR7A9908 1 19990411 A 5311 FRAME LKHEED 382 382G 526414U SO BS 297 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND CENTER FUSELAGE RT FS 297 RING SEGMENT CORRODED FROM WL 166 - 190. REPAIRED I AW SPAR MPP L100-404-99-005. LAC MEA 382-53-99-007. 2 H 7 4 4T A1SO 1999042300236 19990423 00236 SO 1999 4 23 LR7A9909 1 19990411 A 5312 33914936 BULKHEAD LKHEED 382 382G 526414U SO BS 617 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND FS 617 RT AFT MLG BULKHEAD ASSY DAMAGED BEYOND 2.5 IN LIMIT AT BL 61.62R, WL 2 00. REPLACED BULKHEAD ASSY IAW SPAR MPP L100-404-99-008. LAC MEA 382-53-99-010. 2 H 7 4 4T A1SO 1999042300237 19990423 00237 SO 1999 4 23 LR7A9910 1 19990411 A 5312 33914935 BULKHEAD LKHEED 382 382G 526414U SO BS 617 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND FS 617 LT AFT MLG BULKHEAD ASSY DAMAGED BEYOND 2.5 IN LIMIT AT BL 61.62L, WL 2 00. REPLACED BULKHEAD ASSY IAW SPAR MPP L100-404-99-009. LAC MEA 382-53-99-011. 2 H 7 4 4T A1SO 1999042300238 19990423 00238 SO 1999 4 23 LR7A9911 1 19990411 A 5320 3704957 CHANNEL LKHEED 382 382G 526414U SO BS 517 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND FS 517 VERTICAL CHANNELS DAMAGED AT BL 40L AND 40R. REPAIRED BY INSTALLING RE PAIR DOUBLERS IAW SPAR MPP L100-404-99-012. LAC MEA 382-53-99-014. 2 H 7 4 4T A1SO 1999042300239 19990423 00239 SO 1999 4 23 LR7A9912 1 19990411 A 5312 3561926 BULKHEAD CAP LKHEED 382 382G 526414U SO BS 657 MISDRILLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND 2 EA HOLES MISDRILLED IN FS 657 UNDER FLOOR BULKHEAD LOWER BEAM CAP. REPAIRED BY BUSHING, REPAIR ANGLE, AND DOUBLER INSTALL IAW SPAR MPP L100-404-99-015. LAC MEA 382-53-99-016. 2 H 7 4 4T A1SO 1999042300240 19990423 00240 SO 1999 4 23 LR7A9913 1 19990411 A 5320 38809875 WEB LKHEED 382 382G 526414U SO BS 200 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND FS 200 NOSE WHEEL WELL AFT PRESSURE WEB CRACKED CORRODED AT WL 126, BL 9L TO 9 R REPLACED IAW SPAR MPP L100-404-99-016. LAC MEA 382-53-99-017. 2 H 7 4 4T A1SO 1999042300241 19990423 00241 SO 1999 4 23 LR7A9914 1 19990411 A 5311 FRAME LKHEED 382 382G 526414U SO BS 797 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND FS 797 RING FRAME CORRODED AT FROM BL 5.0L TO BL 10.0R. REPAIRED WITH ANGLE I NSTALL IAW SPAR MPP L100-404-99-017. LAC MEA 382-53-9-018. 2 H 7 4 4T A1SO 1999042300242 19990423 00242 SO 1999 4 23 LR7A9915 1 19990411 A 5312 3707841 BULKHEAD WEB LKHEED 382 382G 526414U SO BS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK BRIDGING INSPECTION, FOUND FS 477 RT MLG FWD BULKHEAD ASSY CRACKED AT RISERS WL 230, 234 AND 240. REPLAC ED BULKHEAD ASSY IAW SPAR MPP L100-404-99-018. LAC MEA 382-53-99-019. 2 H 7 4 4T A1SO 1999042300243 19990423 00243 NM 1999 4 23 PCAA9900009 1 19990410 A 3230 574205 VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 13 820EX 10394 10394 019 CLE-FLT 3775 - ON APPROACH INTO CLE, LANDING GEAR FAILED TO EXTEND WHEN SELECTED. GEAR INDICATED INTRANSIT. CREW PERFO RMED SUCCESSFUL ALTERNATE GEAR EXTENSION AND LANDED IN CLE WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO BGM WHERE MAINTENA NCE REPLACED LANDING GEAR SELECTOR VALVE. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999042300244 19990423 00244 SO 1999 4 23 RAAA99E9019 1 19990324 A 3350 873100212 SIGN LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY DUE FAILED. 2 L 7 4 4T 4A22 1999042300245 19990423 00245 NE 1999 4 23 CALA9900409 2 19990412 A 7230 SEAL BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE LEAKING A CALA A G UNSCHED LANDING O2 MASK DEPLOYED B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 09 19623 27527 856996 SMOKE ENTERED THE AFT CABIN DURING TAKEOFF WITH THE ENG BLEEDS ON AND APU RUNNING. THE O2 MASKS WERE MANUALLY DEPLOYED. ACFT RETURNED AND THE SMOKE HAD STABILIZED BY LANDING TIME. A HIGH POWER ENG RUN WAS PERFORMED, SMOKE WAS DUPLICATED USING RT PACK AND RT ENG BLEED. THE NR 2 ENG WAS FOUND TO BE LEAKING OIL AT COMPRESSOR CASE AND WAS REMOVED AND REPLACE D. THE RT ACM WAS REPLACED AS PRECAUTIONARY. A NR 2 ENG HIGH POWER RUN WAS PERFORMED TO CLEAR PNEUMATIC DUCTS OF OIL. THE O2 GENERATORS WERE REPLACED AND O2 MASKS WERE REPACKED IAW MM 35-22-11 AND 35-22-31. *S/D* TEARDOWN REVEALED A FA ILED NR 3 BEARING STATIONARY AFT AIR/OIL SEAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999042300246 19990423 00246 NM 1999 4 23 CALA9900410 1 19990414 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND FLOORBEAM UPPER FLANGE OF T CORRODED AT STA 312, LBL 10 TO RBL 30. A NEW FLOORBEAM WAS INSTALLED IAW S RM 53-10-51. 2 L 7 2 4F RT A16WE 1999042300247 19990423 00247 WP 1999 4 23 CALA9900411 1 19990414 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 383 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 383 BETWEEN L30 AND L29R. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22. 2 L 7 2 4F A6WE 1999042300248 19990423 00248 WP 1999 4 23 CALA9900412 1 19990415 A 3350 08163014524 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12508 47797 INSPECTION FOUND TWO FORWARD RED TRACK LIGHTS INOPERATIVE AND TRACK WAS LOOSE. THE FORWARD TRACK AND LIGHTS WERE REPLAC ED. 2 L 7 2 4F A6WE 1999042300249 19990423 00249 SO 1999 4 23 COMA9910061 1 19990415 A 5320 ANGLE EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 263CA 18186 1784 120255 WHILE PERFORMING TASK 5320-252-04E ON A 2000 FLIGHT CYCLE INSPECTION, FOUND AFT EXIT PIN RECEPTACLES TO BE CORRODED BETW EEN RECEPTACLES AND FLOOR ANGLE. REMOVED FLOOR ANGLE AND PIN RECEPTACLES AND REPLACED WITH SERV UNITS IAW EMB-120-SRM. 2 L 7 2 4T RT A31SO 1999042300250 19990423 00250 SO 1999 4 23 COMA9910060 1 19990415 A 5320 ANGLE EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 263CA 18186 1784 120255 WHILE PERFORMING TASK 5320-252-04E ON 2000 FLIGHT CYCLE INSPECTION, FOUND LOWER FLOOR ANGLE OF AFT EXIT TO BE CORRODED B ETWEEN ANGLE AND PIN RECEPTACLES. REMOVED ANGLE AND PINS AND REPLACED WITH SERVICEABLE UNITS IAW EMB-120 SRM. 2 L 7 2 4T RT A31SO 1999042300251 19990423 00251 EA 1999 4 23 COMA9960154 1 19990401 A 2710 601R30001 BRACKET CNDAIR CL600 CL6002B19 EA LT AILERON BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 876 7050 LEFT AILERON WILL NOT TRAVEL TO FULL DOWN 20.8 DEGREES. TRAVEL STOPS AT 18 DEGREES. FOUND AILERON PCU ATTACHMENT BRACK ET CRACKED. REMOVED AND REPLACED LEFT AILERON ASSEMBLY WITH SERVICEABLE UNIT. 2 L 7 2 4F RT A21EA 1999042300252 19990423 00252 EA 1999 4 23 COMA9960185 1 19990413 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA K NONE O OTHER LD LANDING 1 SO 01 965CA 4368 1076 7131 FLAPS FAILED AFTER LANDING. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999042300253 19990423 00253 NM 1999 4 23 UPS99229257 1 19990401 A 5330 65185111 PANEL BOEING 727 72731C 1384011 NM WS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI NR 1 FUEL TANK OB BOOST PUMP ACCESS PANEL CORRODED. PANEL REPLACED PER MM 28-22-21. 2 L 7 3 4F A3WE 1999042300254 19990423 00254 NM 1999 4 23 UPS99229258 1 19990401 A 5330 65185111 PANEL BOEING 727 72731C 1384011 NM WS 230 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI NR 1 FUEL TANK INBD BOOST PUMP ACCESS PANEL CORRODED. PANEL REPLACED IAW MM 28-22-21. 2 L 7 3 4F A3WE 1999042300255 19990423 00255 NM 1999 4 23 UPS99229259 1 19990325 A 5320 PRESSURE WEB BOEING 727 72731C 1384011 NM BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI 3 CRACKS ON RT MLG WHEEL WELL PRESSURE FLOOR BBL10 TO BBL12 APPROX A T BS920. CRACKS REPAIRED IAW EO B727-5310-0088-K APPX C. 2 L 7 3 4F A3WE 1999042300256 19990423 00256 NM 1999 4 23 UPS99229260 1 19990324 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 848.95 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI FRAME 848.95 LT 2ND FASTENER HOLE ABOVE FLOORLINE IS AT 0.341 AFTER CLEAN UP OF MECHANICAL DAMAGE. THIS IS OUTSIDE LIMITS OF MAX 0.313. REPAIR CARRIED OUT IAW APPENDIX B OF EO B727-5310-5474 AND SMRO EO 9 9-08-001 (UP S FILE NO 727-53-2115). 2 L 7 3 4F A3WE 1999042300257 19990423 00257 NM 1999 4 23 UPS99229261 1 19990326 A 5230 HINGE HALF BOEING 727 72731C 1384011 NM BS 480-620 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI TO FACILITATE CLEANING OF MAIN CARGO DOOR HINGES, REMOVE HINGES FROM CARGO DOOR AND FUSELAGE. REF IT S HINGES 6 OF 8 HINGES FOUND OUT OF LIMITS ON INSPECTION. 6 HINGE SECTIONS REPLACED. HINGE SECTIONS ON DOOR CLEANED AND PROTECTED IAW OHM52-36-62 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999042300258 19990423 00258 NM 1999 4 23 UPS99229262 1 19990325 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI SUSPECT CRACK ON ANGLE BS178 RT FLOOR LEVEL. HFEC CONFIRMED CRACK. REPAIR CARRIED OUT IAW SRM 51- 40-3 FIG 1. 2 L 7 3 4F A3WE 1999042300259 19990423 00259 NM 1999 4 23 UPS99229263 1 19990325 A 7830 SKIN BOEING 727 72731C 1384011 NM NR 3 TR UNIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR3 ENGINE THRUST REVERSER LOWER DOOR SKIN (INNER) HAS WEAR. REPAIR CARRIED OUT PER SRM 54-10-03 FIG 203. 2 L 7 3 4F A3WE 1999042300260 19990423 00260 NM 1999 4 23 UPS99229264 1 19990324 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 441 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, SUSPECT CORROSION AT BUTT JOINT BS 441 BETWEEN S20R TO S21R. REPAIR CARRIED OUT IAW EO B727-5310- 1371 APPX 8.5. 2 L 7 3 4F A3WE 1999042300261 19990423 00261 NM 1999 4 23 UPS99229265 1 19990403 A 5753 65413351 CASTING BOEING 727 72731C 1384011 NM NR 1 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 1 FLAP TRACK MID FAIRING FWD ATTACH CASTING CRACKED. CASTING REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999042300262 19990423 00262 NM 1999 4 23 UPS99229266 1 19990403 A 5753 65413352 CASTING BOEING 727 72731C 1384011 NM NR 8 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 8 FLAP TRACK MID FAIRING FWD ATTACH CASTING CORRODED. CASTING REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1999042300263 19990423 00263 NM 1999 4 23 UPS99229267 1 19990329 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 243.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACK FOUND ON FUSELAGE SKIN BS 243.7 AFT ROW 6TH FASTENER DOWN (BET WEEN S14 AND S15 LH). REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1999042300264 19990423 00264 NM 1999 4 23 UPS99229268 1 19990325 A 5230 652533720 BEAM BOEING 727 72731C 1384011 NM BS 480-620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI DURING REMOVAL OF ACCORDIAN SEAL FOR HINGE INSPECTION TOP BEAM OF MA IN CARGO DOOR FOUND CORRODED I N SEVERAL AREAS. UPPER BEAM REMOVED AND REPLACED IAW BOEING DRAWING 65-25337. 2 L 7 3 4F A3WE 1999042300265 19990423 00265 NM 1999 4 23 UPS99229269 1 19990330 A 5754 SKIN BOEING 727 72731C 1384011 NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 3 LE FLAP HAS CRACK AROUND RIVET ON ANTI-ICE SKIN CENTER SKIN BETWEEN CENTER HINGE AND INBOARD HINGE. ANTI-ICE SKIN REPAIRED PER EO B727-5750-3082. 2 L 7 3 4F A3WE 1999042300266 19990423 00266 NM 1999 4 23 UPS99229270 1 19990325 A 5320 69144691 FITTING BOEING 727 72731C 1384011 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, DURING INSPECTION OF BS 870 TERMINAL FITTING CRACK WAS FOUND BY NDT METHOD ON STRINGER TO FRAME TI E END STRINGER 10 AFT RT. NEW TIE END INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999042300267 19990423 00267 NM 1999 4 23 UPS99229271 1 19990323 A 5754 RIB BOEING 727 72731C 1384011 NM NR 3 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, SUSPECT CRACK IN NR 3 LE SLAT RIB AT SLAT STA 200 APPROX. CRACK CONFIRMED BY HFEC. SLAT RIB REPA IRED IAW SRM 57-50-3 FIG 9. 2 L 7 3 4F A3WE 1999042300268 19990423 00268 NM 1999 4 23 UPS99229272 1 19990329 A 5754 SKIN BOEING 727 72731C 1384011 NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 3 LEADING EDGE FLAP HAS A CRACK AROUND RIVET ON ANTI ICE SKIN. ANTI-ICE SKIN REPAIRED IAW EOB7 27-5750-3082. 2 L 7 3 4F A3WE 1999042300269 19990423 00269 NM 1999 4 23 UPS99229273 1 19990409 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CRACKS AROUND UPPER FASTENER ON STR 16R COMMON TO BS 500 FRAME. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999042300270 19990423 00270 NM 1999 4 23 UPS99229274 1 19990409 A 5320 SHEAR TIE BOEING 727 72731C 1384011 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CRACKED SHEAR TIE AT BS 400 BETWEEN STR 14R AND STR 15R. REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999042300271 19990423 00271 NM 1999 4 23 UPS99229275 1 19990329 A 5320 SUPPORT BOEING 727 72731C 1384011 NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI DUCT SUPPORT CRACKED BS1090 LBL 45.5. NEW STRAP FABRICATED PER SRM 51-20-1 AND FITTED PER SRM 51-3 0-2. 2 L 7 3 4F A3WE 1999042300272 19990423 00272 NM 1999 4 23 UPS99229276 1 19990325 A 5400 WEB BOEING 727 72731C 1384011 NM BS 1376 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, WEB CRACKED ABOVE NR 2 ENGINE BS1376 LT. REPLACED WEB IAW BOEING DWG 65-17555. 2 L 7 3 4F A3WE 1999042300273 19990423 00273 NM 1999 4 23 UPS99229277 1 19990323 A 7830 06453010059 BRACKET BOEING 727 72731C 1384011 NM NR 3 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 3 ENGINE THRUST REVERSER FAIRING MOUNT BRACKET CRACKED. BRACKET REPLACED IAW MM 20-80-01. 2 L 7 3 4F A3WE 1999042300274 19990423 00274 NM 1999 4 23 UPS99229278 1 19990409 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 806 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION AT BS 806 STR 2 FOUND TO BE OUT OF LIMITS. REPAIRED SRM 53-10-3. 2 L 7 3 4F A3WE 1999042300275 19990423 00275 NM 1999 4 23 UPS99229279 1 19990323 A 7830 06453010059 BRACKET BOEING 727 72731C 1384011 NM NR 1 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 1 ENGINE THRUST REVERSER ACTUATOR FAIRING HAS 2 CRACKED MOUNT BRACKETS. BRACKETS REPLACED IAW MM 20-80-01. 2 L 7 3 4F A3WE 1999042300276 19990423 00276 NM 1999 4 23 UPS99229280 1 19990409 A 5320 DOUBLER BOEING 727 72731C 1384011 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI WHILE WORKING NRC 888366 (FUSE 123) LT 870 ACCESS COVER (PANEL) DOUBLER RING IS CORRODED LBL 58, BS 8 70, WL 180. AFTER THE CORROSION REMOVAL, THE DOUBLER RING WENT BEYOND THE SRM LIMITS. REMOVED DOUBLER RING AND FABRICA TED A NEW ONE. ALODINED AND PRIMED AND INSTALLED DOUBLER RING PER SRM 51-10-2, 51-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1999042300277 19990423 00277 NM 1999 4 23 UPS99229281 1 19990409 A 5347 BAC1510140 SEAT TRACK BOEING 727 72731C 1384011 NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CORROSION C53-224-01.05-01, ON FLANGE OF SEAT TRACK BS 740, LBL 25, WL 208, CUT OUT DAMAGED SECTION D UE TO THE EXTENT OF CORROSION. FABRICATED REPAIR PARTS (SEAT TRACK AND STRAPS). ALODINE, PRIMED AND INSTALLED REPAIR P ARTS PER SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F A3WE 1999042300278 19990423 00278 NM 1999 4 23 UPS99229282 1 19990325 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CORROSION (C53-224-01.00-02) MAIN DECK FRAME OUTBOARD TOP SURFACE BS 780 STR 8R-STR1. FOUND CORROSIO N OUT OF LIMITS PER SRM 53-10-01 BETWEEN STRINGERS 4 AND 5. REMOVED DAMAGED AREA AND INSTALLED STANDARD FRAME REPAIR PE R SRM 53-10-4 PG 9 AND SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 1999042300279 19990423 00279 NM 1999 4 23 UPS99229283 1 19990411 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CORROSION ON FLOORBEAM BS 312, LBL 3.5, WL 208. REMOVED AND REPLACED UPPER CHORD SEGMENT PER SRM 53- 10-8 FIG 9. 2 L 7 3 4F A3WE 1999042300280 19990423 00280 NM 1999 4 23 UPS99229284 1 19990325 A 5347 BAC1520792 SEAT TRACK BOEING 727 72731C 1384011 NM BS 775-780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CORROSION C53-224-01.05-02 MAIN DECK SEAT TRACK BS 775-780 LBL 60 WL 208 O/B FLANGE. REMOVED AND REP LACED SEAT TRACK FROM BS 760-848 WL 208 LBL 60 PER SRM 53-10-1. 2 L 7 3 4F A3WE 1999042300281 19990423 00281 NM 1999 4 23 UPS99229285 1 19990404 A 5347 BAC15201432 SEAT TRACK BOEING 727 72731C 1384011 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI WHILE WORKING CARD NR 888993 FOUND SEAT TRACK AT BS 344 RBL 22 WL 208 TO BE CORRODED ON LWR SURFACE. REPLACED SECTION OF SEAT TRACK FROM BS 344-390 RBL 25 WL 208 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999042300282 19990423 00282 NM 1999 4 23 UPS99229286 1 19990409 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI CRACKS AROUND UPPER AND LOWER FASTENERS IN STRINGER 15R COMMON TO BS 400 FRAME. REPAIRED PER SRM 53- 10-3. 2 L 7 3 4F A3WE 1999042300283 19990423 00283 WP 1999 4 23 UPS99829287 1 19990322 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E RIB AT STA XS250.089 IS CRACKED AT THE UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300284 19990423 00284 WP 1999 4 23 UPS99829288 1 19990406 A 5720 37048412 FITTING DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 RT WING, THE STRINGER 51 END FITTING AT STA XRS74.00 IS CRACKED. REMOVED AND REPLACED FITTING IAW DW G 3704841 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300285 19990423 00285 WP 1999 4 23 UPS99829289 1 19990325 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 55 FRAME AT STR 24L IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300286 19990423 00286 WP 1999 4 23 UPS99829290 1 19990322 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 257 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING L/E SKIN AT STA XW257.000 IS CRACKED AT THE I/B END. REPAIRED AREA IAW DC8-5720-7767. 2 L 7 4 4F RT 4A25 1999042300287 19990423 00287 WP 1999 4 23 UPS99829291 1 19990329 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 1100 BTWN STR 10L-11L, THE FRAME IS CORRODED OUT OF LIMITS. REPAIRED AREA IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300288 19990423 00288 WP 1999 4 23 UPS99829292 1 19990322 A 5320 3755827501 FITTING DOUG DC8 DC871F 302199D WP BS 270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 270 AT STR 30R-31R, THE DOOR JAMB FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755827-501 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300289 19990423 00289 WP 1999 4 23 UPS99829293 1 19990406 A 5720 370484112 FITTING DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 WING STA XRS74.0, THE STR 51 END FITTING IS CRACKED (LT WING). REMOVED AND REPLACED FWD AND AFT END FITTINGS IAW DWG 3704841 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300290 19990423 00290 WP 1999 4 23 UPS99829294 1 19990322 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1, RT WING L/E RIB AT STA XS 250.089 IS CRACKED. REPAIRED AREA IAW SRM 57-3-0. 2 L 7 4 4F RT 4A25 1999042300291 19990423 00291 WP 1999 4 23 UPS99829295 1 19990406 A 5320 38884061 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 RT FWD TYPE 1 DOOR LOWER AFT FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3888406 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300292 19990423 00292 WP 1999 4 23 UPS99829296 1 19990322 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 533.375 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1, NR 1 STUB LWR SKIN IS CRACKED AT STA XFS533.375 AND XOLDO57.500. REPAIRED AREA IAW SRM 57-2-1A. 2 L 7 4 4F RT 4A25 1999042300293 19990423 00293 WP 1999 4 23 UPS99829297 1 19990322 A 5720 56412521 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1, RT WING L/E LWR SKIN INTERNAL DOUBLER IS CRACKED FWD OF ACCESS PANEL 524B. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999042300294 19990423 00294 WP 1999 4 23 UPS99829298 1 19990330 A 5347 52772660 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1, SEAT TRACK AT STA 1400, LBL58 HAS HEAVY CORROSION. SPLICED TRACK FROM STA 1370-1430 BLB58 IAW SRM 5 3-2-3. 2 L 7 4 4F RT 4A25 1999042300295 19990423 00295 WP 1999 4 23 UPS99829299 1 19990325 A 5320 36471171 FITTING DOUG DC8 DC871F 302199D WP BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 RT WHEEL WELL AT STA 960 AND LONGERON 24R, THE FITTING ABOVE THE LONGERON IS CORRODED. REMOVED AND R EPLACED FITTING IAW DWG 3647117 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300296 19990423 00296 WP 1999 4 23 UPS99829300 1 19990323 A 5542 5644210505 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 RUDDER SKIN IS CRACKED IN 2 PLACES LEFT SIDE JUST ABOVE THE TAB. REMOVED AND REPLACED RUDDER ASSY IA W MM 27-21-01. 2 L 7 4 4F RT 4A25 1999042300297 19990423 00297 WP 1999 4 23 ABXA9900286 1 19990406 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 844AX 45848 EMERGENCY EXIT LIGHTS WOULD NOT DISARM. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECKED NORMAL. 2 L 7 4 4F 4A25 1999042300298 19990423 00298 NM 1999 4 23 DL72S990767 1 19990407 A 3350 LIGHT BOEING 727 727232 1384082 NM AFT STAIR LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 21077 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT. 2 L 7 3 4F A3WE 1999042300299 19990423 00299 1999 4 23 DL757990768 4 19990409 A 2562 6076902 ELT BOEING 757 757232 1384965 NM COCKPIT MALFUNCTIONED A DALA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 27 618DL 22908 MTC COORDINATION RECIEVED MESSAGE THAT THE MILITARY IS RECIEVING A ELT SIGNAL FROM SHIP 618. REPLACED ELT. 2 L 7 2 4F RT A2NM 1999042300300 19990423 00300 NM 1999 4 23 DL72W990769 1 19990318 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 STR RT CRACKED INSIDE VERT STA AT B/H STA 133.8 LOC INSIDE VERT STAB. BEGAN FABRICATING REPAIR ANGLE. FABRICATED REPAI R ANGLES PER M/M 55-30-0 PG 803. OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 PG 803. 2 L 7 3 4F A3WE 1999042300301 19990423 00301 NM 1999 4 23 DL72K990770 1 19990408 A 3350 900542 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 524DA 21584 EMERGENCY EXIT LIGHT IN BETWEEN OVERWING EXITS INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999042300302 19990423 00302 NM 1999 4 23 DL73K990771 1 19990409 A 3320 LIGHT BOEING 737 737232 1384475 NM GALLEY DAMAGED A DALA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 313DL 23085 LIGHT IN GALLEY SMOKED AND C/B POPPED. PULLED AND COLLARD GALLEY LIGHT C/B ON P18 PANEL. FOUND AFT LEFT GALLEY LIGHT A SSY TO BE THE PROBLEM. REPLACED SAME. 2 L 7 2 4F RT A16WE 1999042300303 19990423 00303 NM 1999 4 23 DL72S990772 1 19990408 A 2131 CONTROLLER 7638101 BOEING 727 727232 1384082 NM CABIN FAILED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 499DA 21143 DURING CLIMB-OUT, CABIN ALT BEGAN TO CLIMB AT 1000 FT, BOTH PACKS APPEARED TO OP. NORMAL CABIN CLIMBED TO AN ALT OF 12, 000 AND DESCENT BEGAN. POM PREC FOLLOWED STBY AND DC HAD NEG EFFECT TO CLOSE OUTFLOW FURTHER CARGO V. CLOSED LIGHT ILL UMINATED ENTIRE TIME ANOMALLY OCCURED. REPLACED PRESSURE CONTROLLER, REMOVED AND REPLACED RT PACK FWD VLV. PERF ORMED TEST PER M/M. PRESS OF A/C TO CK FOR LEAKS. NO LEAKS NOTED A/C PRESSURIZATION GRD CKS NORMAL. PRESSURIZED A/C A LL INDICATION NORMAL. 2 L 7 3 4F A3WE 1999042300304 19990423 00304 NM 1999 4 23 DL72S990773 1 19990409 A 5753 652163233 SPAR BOEING 727 727225 1384077 NM NR 3 TE MIDFLAP MISREPAIRED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 8875Z 21293 NR 2 MIDFLAP/UPPER SPAR CHORD, WBL 124 ALT FASTENER INSTALL DURING ACCOMPLISHMENT OF EO 4-58705-3AD (REF SB 727-57-160). MAINTENANCE UNABLE TO INSTALL REQUIRED HI-LOCK COLLAR ON SPAR-TO-SKIN ATTACH HOLE DUE TO INTERFERENCE WITH SPAR RADIUS . AUTHORIZED USE OF RADIUS BLOCK AND MINI-NUT. 2 L 7 3 4F A3WE 1999042300305 19990423 00305 NM 1999 4 23 DL72W990774 1 19990409 A 2910 LINE 000AE908D03 BOEING 727 7272Q8 138407W NM LT MLG DOOR ACT LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 831L 21826 SYSTEM 'A' FAILED UPON GEAR RETRACTION PRESSURE WENT TO ZERO QUANTITY WENT TO 1 QT, PERFORMED CKLIST PROCEDURES IAW POM. MAINTENANCE FOUND HYD LINE LEAKING ON LT GEAR DOOR ACTUATOR. REPLACED LINE, SERVICED HYD, ALL CKS NORMAL. 2 L 7 3 4F A3WE 1999042300306 19990423 00306 NM 1999 4 23 DL72L990775 1 19990409 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 1.25 CRACK ON NR 7 SLAT I/B TRACK O/B SPAR STIFFENER. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999042300307 19990423 00307 1999 4 23 DL72S990776 2 19990410 A 7261 FILTER BOEING 727 727232 1384082 NM NR 1 ENGINE DIRTY A DALA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 27 521DA 21472 OIL FILTER BYPASS LIGHT ILLUMINATED ON T/O, REDUCED PWR FOR CLIMB AND LIGHT WENT OUT. DURING CRUISE, LIGHT CAME BACK ON , PULLED THROTTLES BACK AND LIGHT WENT OUT. SHORT TIME LATER, LIGHT CAME ON WITH THROTTLES AT IDLE. CREW SHUTDOWN PER POM. REPLACED OIL FILTER RAN ENGINE. 2 L 7 3 4F A3WE 1999042300308 19990423 00308 NM 1999 4 23 DL757990778 1 19990410 A 2530 1811150417 COFFEEMAKER BOEING 757 757232 1384965 NM GALLEY UNSERVICEABLE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 606DL 22813 UNIDENTIFIED SMOKE IN AFT GALLEY. DIVERTED TO JFK FOR LANDING. FOUND AFT LT COFFEE MAKER OVERFLOWING. REPLACED COFFE E MAKER AND OPS CHECK OK. ALSO, REMOVED OVENS AND INSPECTED WIRING. ALL CHECKS OK. 2 L 7 2 4F RT A2NM 1999042300309 19990423 00309 NM 1999 4 23 DL757990779 1 19990410 A 2750 340545 VALVE BOEING 757 757232 1384965 NM TE FLAPS FAILED A DALA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SO 27 648DL 24372 DURING APPROACH WITH FLAPS AT 1 DEG, THE /LE SLAT ASYM/EICAS MSG AND WARNING LIGHT ABOVE FLAP GAUGE CAME ON. ACCOMPLISH ED CHECKLIST IN ATTEMPT TO ELECTRICALLY DRIVE FLAPS TO 20 DEG, BUT NOTHING CHANGED FROM THE 1 DEG POSITION. FLT DIVERTE D TO JFK. REPLACED TRAILING EDGE BYPASS VALVE. 2 L 7 2 4F RT A2NM 1999042300310 19990423 00310 NM 1999 4 23 DL73K990781 1 19990410 A 2150 6075103 CONTROLLER BOEING 737 737232 1384475 NM RT PACK MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 315DL 23087 DURING CLIMB-OUT WITH BOTH AIR MIX VALVE IND INDICATING FULL COLD, DUCT TEMP WENT TO 120. NO TEMP CONTROL IN AUTO OR MA NUAL EITHER PACK. AIR TURNBACK TO MCO. REPLACED RT PACK 35 DEG CONTROLLER AND SENSOR. ALL CKS OK FOR RT PACK. FOUND LT PACK ACM FROZEN. REPLACED SAME. 2 L 7 2 4F RT A16WE 1999042300311 19990423 00311 NM 1999 4 23 DL72S990782 1 19990410 A 2560 CASE MV10 BOEING 727 727232 1384082 NM MEGAPHONE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 9531143 21062 FWD MEGAPHONE CRACKED CASE. REPLACED SAME. 2 L 7 3 4F A3WE 1999042300312 19990423 00312 NM 1999 4 23 DL72E990783 1 19990410 A 3350 BATTERY 900835A BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 283WA T4159 21485 LT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATT M955. OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999042300313 19990423 00313 NE 1999 4 23 DL76S990785 2 19990410 A 7310 FITTING BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 ENGINE LEAKING A DALA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 27 137DL 25306 AT TOP OF DESCENT, NR 1 ENGINE ROLLED BACK AND OIL PRESSURE STARTED TO DECAY WITH N1 AND N2 STILL INDICATING DOUBLE DIGI TS. REPLACED T-BONE FITTING AT 10 O'CLOCK POSITION. 2 L 7 2 4F 4 F RT A1NM E13NE 1999042300314 19990423 00314 NE 1999 4 23 DL72W990787 2 19990411 A 7314 FUEL PUMP BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 291WA 48808 22109 700436 ENGINE NR 1 FLAME OUT ON TAKEOFF ROLL. REPLACING NR 1 ENGINE FUEL AND FUEL PUMP IN PROGRESS. 2 L 7 3 4F 4 F A3WE E2EA 1999042300315 19990423 00315 NM 1999 4 23 DL72L990788 1 19990411 A 3350 330201663 LENS BOEING 727 727232 1384082 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 509DA 21311 EMERGENCY TRACK LIGHTING 10C MISSING BULB/FROM 27 TO REAR OF ACFT EMERGENCY TRACK LIGHTING INOP. REPAIRED SHORTED WIRE IN FLOOR AND RELAMPED 10C. 2 L 7 3 4F A3WE 1999042300316 19990423 00316 NM 1999 4 23 DL72S990789 1 19990412 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 534DA 0335 22047 EMERGENCY TRACK LIGHTING IN F/C WOULD NOT WORK. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 1999042300317 19990423 00317 NM 1999 4 23 DL757990791 1 19990411 A 3350 331202129 BULB BOEING 757 757232 1384965 NM EMER EXIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 658DL 24420 EXTERNAL EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A2NM 1999042300318 19990423 00318 NM 1999 4 23 DL72S990793 1 19990331 A 5400 S DUCT BOEING 727 727225 1384077 NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FLANGE CRACKED AND DENTED SEVERAL PLACES, FWD FLANGE ON UPPER S DUCT SECT. BEGAN REMOVAL OF FASTENERS ON UPPER S DUCT F LANGES. COMPLETED REMOVAL OF FASTENERS. BEGAN FABRICATIONS REPAIR PIECES. COMPLETED FABRICATING REPAIR PIECES PER SRM 54-10-3 FIG 13. DYE CHECKED PER PS 900-6-3 NR 1. NO CRACKS FOUND. OK TO INST OR INSTALLED REPAIR PIECES. REPAIR OK OK CLOSE. BEGAN REMOVAL OF FASTENERS ON LOWER S DUCT FLANGE. 2 L 7 3 4F A3WE 1999042300319 19990423 00319 NE 1999 4 23 DL73K990795 2 19990411 A 7510 VALVE 320115C BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE STUCK A DALA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 SO 27 311DL 26050 23083 709134 NR 1 ENG OIL TEMP IN YELLOW BAND. ENG FUEL HEAT VLV STUCK IN THE OPEN POSITION. SHUT DOWN ENG AS PRECAUTIONARY. FLIGH T DIVERTED INTO CAE. VLV DEFERRED PER MEL. AT BDL LAYOVER, THE VLV WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1999042300320 19990423 00320 NM 1999 4 23 DL757990796 1 19990411 A 5754 114N4002138 WEDGE BOEING 757 757232 1384965 NM NR 10 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 627DL 22917 AD 90-23-06: NR 10 LE SLAT TE WEDGE REPLACEMENT, FASTENER SUBSTITUTION. DURING REPLACEMENT OF THE TE WEDGE PER EO 6-716 53-3AD AND SRM 57-43-02, FIGURE 202 (REF SB 757-57A0038). SEVERAL EXISTING COVE SKIN-TO-WEDGE ATTACH FASTENERS WERE CSK FOR TENSION HEAD HI-LOCKS. REQUIRED FASTENERS ARE SHEAR HEAD FLUSH FASTENERS. AUTHORIZED USE OF TENSION HEAD HI-LOCKS IN EXISTING OVER-CSK HOLES. 2 L 7 2 4F RT A2NM 1999042300321 19990423 00321 NM 1999 4 23 DL72L990798 1 19990411 A 3350 RPS1B POWER SUPPLY BOEING 727 727232 1384082 NM ROW 27 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 509DA 21311 EMERGENCY ESCAPE PATH LIGHTING FROM ROW 27 BACK WAS INOP. FOUND SHORTED WIRE AT FLOOR DISCONNECT. REPAIRED WIRING AND REPLACED BATTERY POWER SUPPLY. 2 L 7 3 4F A3WE 1999042300322 19990423 00322 NM 1999 4 23 DL72E990800 1 19990412 A 3397 WIRE BOEING 727 727247 138408F NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 282WA 21484 A/C ESCAPE PATH LIGHTING FOUND INOP IN SEVERAL LOCATIONS. REPAIRED AND REPLACED GROUND WIRING AT THE FWD BATTERY PACK M ULTI SPLICE AREA. ALL CK'S OK. 2 L 7 3 4F A3WE 1999042300323 19990423 00323 NM 1999 4 23 DL72S990802 1 19990412 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FUSELAGE SKIN FS 360-480 STRINGER 4R SKIN LAP SPLICE: CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 TOTAL CRACKS. THE ENTIRE SKIN LAP WAS CUTOUT ALONG THE LENGTH OF THE PANEL AND REPAIRED WITH AN EXTERNAL DOUBLER PE R ER/A 367136-14AD, REV A. 2 L 7 3 4F A3WE 1999042300324 19990423 00324 NM 1999 4 23 DL72S990803 1 19990412 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 FUSELAGE SKIN FS 360-481 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN 3 CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALU MINUM DOUBLER PER ER/A 367160-14AD. 2 L 7 3 4F A3WE 1999042300325 19990423 00325 NM 1999 4 23 DL72K990804 1 19990409 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 FUSELAGE SKIN FS 481-681 STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRME D 12 CRACKS. THE SKIN LAP WAS CUTOUT ALONG THE LENGTH OF THE PANEL AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER E R/A 367138-14AD, REV B. 2 L 7 3 4F A3WE 1999042300326 19990423 00326 NM 1999 4 23 DL72K990805 1 19990409 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 440-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 FUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRME D A SINGLE CRACK BETWEEN FS 440 AND 460. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED PER B727 SRM 53-30-5, FI G 5 AND DOCUMENTED PER ER/A 367142-14AD. 2 L 7 3 4F A3WE 1999042300327 19990423 00327 NM 1999 4 23 DL72S990806 1 19990411 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 420-440 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FUSELAGE SKIN FS 420-440 STRINGER 4L, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRM ED A SINGLE CRACK BETWEEN FS 420 AND 440. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B 727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367158-14AD. 2 L 7 3 4F A3WE 1999042300328 19990423 00328 NM 1999 4 23 DL72S990807 1 19990411 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FUSELAGE SKIN FS 360-481 STRG 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETW EEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 C RACKS IN 3 SEPARATE FRAME BAYS. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL AL UMINUM DOUBLER PER ER/A 367155-14AD. 2 L 7 3 4F A3WE 1999042300329 19990423 00329 NM 1999 4 23 DL72S990808 1 19990411 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FUSELAGE SKIN FS 481-68, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BET WEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER P ER ER/A 367156-14AD. 2 L 7 3 4F A3WE 1999042300330 19990423 00330 NM 1999 4 23 DL72S990809 1 19990411 A 5330 655456715 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FUSELAGE SKIN FS 680-740, STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLIC E BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRM ED 45 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE LENGTH OF THE PANEL AND REPAIRED WITH AND EXTERN AL ALUMINUM DOUBLER PER ER/A 367157-14AD. 2 L 7 3 4F A3WE 1999042300331 19990423 00331 NM 1999 4 23 DL72S990810 1 19990408 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FUSELAGE SKIN FS 481-681 STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CO NFIRMED 4 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 367137-14AD. 2 L 7 3 4F A3WE 1999042300332 19990423 00332 NM 1999 4 23 DL72K990811 1 19990409 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 700-720 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 FUSELAGE SKIN FS 700-720B STRINGER 4R, SKIN LAP SPLICE:CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRME D CRACKS BETWEEN FS 700 AND 720 AND BETWEEN FS 720A AND 720B. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED W ITH EXTERNAL ALUMINUM DOUBLERS PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367139-14AD. 2 L 7 3 4F A3WE 1999042300333 19990423 00333 NM 1999 4 23 DL72L990812 1 19990409 A 5711 65192923 SPAR WEB BOEING 727 727232 1384082 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 WING CENTER SECTION REAR SPAR WEB, RBL 13 CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A 1.5 TYPICAL CRAC K IN A CHEM-MILL RADIUS NEAR THE UPPER SPAR CAP AT RBL 13. THE CRACK WAS ROUTED OUT OF THE SPAR WEB AND REPAIRED WITH A N ALUMINUM DOUBLER PER ER/A 367140-14AD, REV A. 2 L 7 3 4F A3WE 1999042300334 19990423 00334 NM 1999 4 23 DL72W990814 1 19990319 A 5753 652163434 ANGLE BOEING 727 727247 138408F NM NR 3 TE MIDFLAP CRACKED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT SPAR ANGLE WAS FOUND CRACKED 2 PLACES 35 FROM IB END OF FLAP. A NEW SECT ION OF SPAR ANGLE WAS DRILLED UP AND INSTALLED PER MM 57-52-01, FIG. 802. 2 L 7 3 4F A3WE 1999042300335 19990423 00335 NM 1999 4 23 DLM88990816 1 19990410 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DE 53417 CRACKS AT L2R AND L2L ON THE FS 1418 FRAME WERE FOUND IN THE TYPICAL LOCATIONS. THE CRACKS WERE 1.25 EACH. REPAIRED PE R ERA 332990-14. 2 L 7 2 4F RT A6WE 1999042300336 19990423 00336 NM 1999 4 23 DLM88990817 1 19990410 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 250 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DE 53417 AT HMV, A DENT WAS TRIMMED OUT IN THE FUSELAGE SKIN; DAMAGE CUTOUT IS APPROX 30 BY 8; AND IS LOCATED AT APPROX FS 250 AN D L19L. REPAIRED PER ERA 266889-14, REV B. 2 L 7 2 4F RT A6WE 1999042300337 19990423 00337 NM 1999 4 23 DLM88990818 1 19990410 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DE 53417 A DENT WAS FOUND ON THE FUSELAGE SKIN AT FS 237 JUST BELOW L17L. CUTOUT MEASURED APPROX 6 BY 2.5. REPAIRED PER ERA 332 994-14, REV A. 2 L 7 2 4F RT A6WE 1999042300338 19990423 00338 NM 1999 4 23 DLM88990819 1 19990410 A 5330 593600731 SKIN DOUG MD88 MD88 3023688 NM CARGO DOORWAY GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DE 53417 A GOUGE WAS NOTED ON THE AFT EDGE OF THE C3 DOORWAY. THE DAMAGE WAS REMOVED W/A 1 BY 1.4 TRIM OUT IN THE SKIN AND SURRO UND DOUBLER. REPAIR PER ERA 333011-14, REV. A. 2 L 7 2 4F RT A6WE 1999042300339 19990423 00339 NM 1999 4 23 DL72S990820 1 19990413 A 5330 65545662 SKIN BOEING 727 727225 1384077 NM BS 570 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 WHILE ACCOMPLISHING HFEC INSPECTIONS PER SI 4-47176-12AD, REV F, A CRACK INDICATION WAS FOUND AT TWO FASTENER LOCATIONS BETWEEN BS 560 AND BS 580 AT S26L. REPAIRED PER ERA 332999-14AD. 2 L 7 3 4F A3WE 1999042300340 19990423 00340 NM 1999 4 23 DL72S990821 1 19990413 A 5530 STRINGER BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 VERTICAL STAB S7 WAS FOUND CRACKED AT STA 157.2 DURING INSP PER SI 4-59253-12AD. REPAIRED PER ERA 333025-14A.D 2 L 7 3 4F A3WE 1999042300341 19990423 00341 NM 1999 4 23 DL72W990822 1 19990122 A 5753 652163233 SPAR BOEING 727 727247 138408F NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 REAR SPAR CRACKED 19 AND 37 FROM I/B END. REPAIRED PER M/M 57-52-0. 2 L 7 3 4F A3WE 1999042300342 19990423 00342 NM 1999 4 23 DL72S990823 1 19990413 A 5713 STRINGER BOEING 727 727225 1384077 NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 TWO CRACKS WERE FOUND; ONE IN S9L AND THE OTHER IN S10L ON THE LT WING AT WS 656.5. BOTH CRACKS ARE LOCATED ON THE LWR HORIZ LEG OF THE ZEE STRINGERS. REPAIRED PER ERA 333023-14AD. 2 L 7 3 4F A3WE 1999042300343 19990423 00343 NM 1999 4 23 DL72W990824 1 19990413 A 5330 6554574157 SKIN BOEING 727 727247 138408F NM BS 690 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 WHILE ACCOMPLISHING HFEC INSP PER SI 4-74176-12AD, REV F, A CRACK INDICATION WAS FOUND BETWEEN BS 681 AND BS 700; AT S4R . REPAIRED PER ERA 332945-14AD, REV A. 2 L 7 3 4F A3WE 1999042300344 19990423 00344 NM 1999 4 23 DL72W990825 1 19990413 A 5330 6554574155 SKIN BOEING 727 727247 138408F NM BS 600 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 WHILE ACCOMPLISHING HFEC INSPECTIONS PER SI 4-74176-12AD, REV F, CRACK INDICATIONS WERE NOTED BETWEEN BS 520 AND 681 AT S4R. ADDITIONALLY, GROUND DAMAGE WAS INDUCED TO THE AREA WHILE ACCOMPLISHING THE STANDARD REPAIR. REPAIRED PER ERA 332 946-14AD, REV F. 2 L 7 3 4F A3WE 1999042300345 19990423 00345 NM 1999 4 23 DL72S990828 1 19990413 A 5711 SPAR BOEING 727 727232 1384082 NM LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 INBOARD FWD LWR SIDE OF AUX SPAR GOUGED LEFT SIDE. REPAIRED PER MM 57-43-0 P 801. 2 L 7 3 4F A3WE 1999042300346 19990423 00346 WP 1999 4 23 DLL10990831 1 19990413 A 5312 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP BS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 733DS 193C1224 FUSELAGE BULKHEAD FS 1212 RBL 6, WEB CRACK REPAIR. THE FS 1212 BULKHEAD WEB WAS FOUND WITH A CRACK AT RBL 6. THE CRACK IS TYPICAL TO THOSE COVERED IN LAC S/B 093-53-277 AND AD 96-20-10. THE CRACK WAS REPAIRED PER LAC DWG. LCC-7622-385 ( AS CALLED FOR IN THE S/B) AND DOCUMENTED PER ER/A 367169-14AD. 2 L 7 3 4F A23WE 1999042300355 19990423 00355 EU 1999 4 23 99ZZZX1572 1 19990406 A 2780 703515509 SWITCH ISRAEL 1124 1124 4500102 EU TE FLAP FAILED A DQIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 46BK 214 FLAPS WOULD EXTEND, BUT WOULD NOT RETRACT. REPLACED SLIDER SWITCH WITH OVERHAULED. OPS CHECK OK. 2 M 7 2 4F A2SW 1999042300364 19990423 00364 CE 1999 4 23 99ZZZX1581 1 19990326 A 2140 5056434169 VALVE BEECH 90 F90 1152909 CE AIR DIST MALFUNCTIONED A PRIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 03 236JS 574 LA90 AIR VALVE STUCK IN OPEN POSITION CAUSING FULL HOT AIR TO CABIN. SMOKE STARTED TO FLOW INTO CABIN AFTER TAKEOFF. AIRCRA FT RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE CLEANED VALVES AND OPS CHECKED OK. BOTH BYPASS VALVES WILL BE REP LACED. 1 L 7 2 4T A31CE 1999042300370 19990423 00370 CE 1999 4 23 99ZZZX1587 1 19990322 A 7910 3020907 FILLER CAP BEECH 99 C99 1154006 CE ENGINE LOOSE A FFSA E ENGINE SHUTDOWN K J W FLUID LOSS WARNING INDICATION INADEQUATE Q C CR CRUISE 1 AL 01 575W U204 OIL PRESSURE ON RIGHT ENGINE STARTED DROPPING SHORTLY AFTER TAKEOFF. FINDINGS: OIL LOSS DUE TO UNSECURED OIL CAP. 1 L 7 2 3T A14CE 1999042300372 19990423 00372 1999 4 23 99ZZZX1589 3 19990331 A 6140 451B41 STRIKER PIPER PA31T PA31T3 7103128 SO STOP SWITCH WORN A CSAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 AL 01 217CS 3118275014 THE PILOT REPORTED AFTER TAKEOFF FROM WAA DURING CLIMB-OUT PASSING THROUGH 1,000 FEET, THE LT PROPELLER SPEED SLOWLY STA RTED TO DECREASE, PILOT RETARDED POWER LEVER TO KEEP THE TORQUE DOWN. ALSO, LT ENGINE BETA LIGHT WAS ILLUMINATED. PIL OT CONTACTED MAINTENANCE ON THE RADIO AND THEY ADVISED PILOT TO PULL LT ENGINE HTB/BETA CIRCUIT BREAKER WHICH ALLOWED PR OPELLER TO RESUME NORMAL OPERATION. FLIGHT CONTINUED TO OME. ACFT INSPECTED ON ARRIVAL. THE LOW PITCH STOP SWITCH WAS FOUND ACTUATING OUT OF LIMITS DUE TO WEAR ON THE SWITCH STRIKER. A NEW STRIKER WAS INSTALLED AND RIGGED IAW PIPER SM 7 6-14-03. ENGINE GROUND RUN FOR PERFORMANCE, BETA, AND MTG TESTS PERFORMED SATISFACTORILY. 1 L 7 2 3T A8EA 1999042300378 19990423 00378 WP 1999 4 23 TWAA9905601 1 19990414 A 5320 SPLICE DOUG DC9 DC931 3022065 WP BS 577 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND A CRACKED SPLICE AT STA 577, LONGERON 26L. REMOVED AND REPLACED LONGERON FITTING SPLICE PER PRINT 5910068, AND SRM FASTENER DESCRIPTION AND OPERATION. 2 L 7 2 4F A6WE 1999042300379 19990423 00379 WP 1999 4 23 TWAA9905602 1 19990414 A 5320 SPLICE DOUG DC9 DC931 3022065 WP BS 565 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CRACKED SPLICE AT STA 565, LONGERON 27L. REMOVED AND REPLACED LONGERON FITTING SPLICE P ER PRINT 5910068, AND SRM FASTENER DESCRIPTION AND OPERATION. 2 L 7 2 4F A6WE 1999042300380 19990423 00380 WP 1999 4 23 TWAA9905603 1 19990414 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 590 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT AT STA 590, ABOVE AND OTBD OF LONGERON 28L, WAS CORRODED THROUGH. REMOVED CORROSION BY INSTALLING NEW SUPPORT PART AND INSTALLED PER SRM 51-01, PAGE 1 ITEM C. 2 L 7 2 4F A6WE 1999042300381 19990423 00381 NM 1999 4 23 HNAA9900048 1 19990415 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGGAGE COMPT WON'T TEST A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 909HA 018 BAGGAGE COMPARTMENT NR 2 SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 1999042300382 19990423 00382 WP 1999 4 23 9901519998 1 19990412 A 2133 BRACKET DOUG DC9 DC931 3022065 WP OUTFLOW VALVE BROKEN A NWAA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 8934E 47143 APPROACHING TOP OF CLIMB, CABIN PRESSURE WARNING LIGHT ILLUMINATED WITH CABIN ALTITUDE AT 9500 FEET. MANUAL CONTROL HAD NO EFFECT. CREW DECLARED AN EMERGENCY AND FLIGHT WAS CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAI NENANCE REPLACED BROKEN BRACKET TO PULLEY CABLE ABOVE OUTFLOW VALVE ACTUATOR AND REINSTALLED CABLE. ALSO, REPLACED CABI N PRESSURE AMPLIFIER. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999042300383 19990423 00383 NE 1999 4 23 9901529990 2 19990414 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LEFT FAILED A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 8950E 47186 666774 DURING DESCENT, THE LEFT ENGINE OIL PRESSURE BEGAN FLUCTUATING, OIL QUANTITY DROPPED TO ZERO AND THE LOW OIL PRESSURE LI GHT ILLUMINATED. CREW SHUT DOWN THE LEFT ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENG INE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1999042300384 19990423 00384 WP 1999 4 23 9901531147 1 19990413 A 3234 HANDLE DOUG DC10 DC1040 3023508 WP LANDING GEAR LACK OF LUBE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 147US 46756 ON FINAL APPROACH INTO SFO, CYCLED GEAR DOWN TWICE, FOUR RED LIGHTS ILLUMINATED BOTH TIMES. ALL CIRCUIT BREAKERS IN AND HYDRAULICS WERE GOOD. FOLLOWED COM PROCEDURE AND THIRD TIME DOWN ALL GREEN LIGHTS ILLUMINATED. CLEANED AND LUBED GEAR HANDLE CONTROL. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999042300385 19990423 00385 WP 1999 4 23 9901549947 1 19990413 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMPARTMENT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8938E 47161 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1999042300386 19990423 00386 WP 1999 4 23 UPS99829301 1 19990329 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 1380 AT STR 19L, THE FRAME HAS HEAVY CORROSION. REPAIRED FRAME IAW DH SK797-464. 2 L 7 4 4F RT 4A25 1999042300387 19990423 00387 WP 1999 4 23 UPS99829302 1 19990403 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1030 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 STA 1030 AT STR 19L, THE EXTERNAL SKIN HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK797-045. 2 L 7 4 4F RT 4A25 1999042300388 19990423 00388 WP 1999 4 23 UPS99829303 1 19990322 A 2810 AUX TANK DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:C1 LEFT WING AUX TANK AT STA XFS 1.250 HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999042300389 19990423 00389 WP 1999 4 23 UPS99829304 1 19990415 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 1999042300390 19990423 00390 WP 1999 4 23 ABXA9900287 1 19990218 A 5320 47723981 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1540 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND CORROSION ON LONGERON FITTING, STATION 1540, LONGERON 32 RIGHT AT AFT PRESSURE BULKHEAD. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F 4A25 1999042300391 19990423 00391 WP 1999 4 23 ABXA9900288 1 19990218 A 5320 46413261N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1530 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND CORROSION ON STATION 1530 PRODUCTION SPLICE FITTING AT LONGERON 34 RIGHT. REPLACED FITTING IAW DC 8 SRM 51-30-0 AND 51-1-20D. 2 L 7 4 4F 4A25 1999042300392 19990423 00392 WP 1999 4 23 ABXA9900289 1 19990218 A 5320 46401621N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1200 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND CORROSION ON CUSP FITTING AT STATION 1200 LT SIDE. REPLACED FITTING IAW DC8 SRM 51-30-0 AND 51-1- 20D. 2 L 7 4 4F 4A25 1999042300393 19990423 00393 WP 1999 4 23 ABXA9900290 1 19990304 A 5320 97540101 WEB DOUG DOUG DC8 DC862 3021970 WP BS 477 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND UPPER CARGO COMPARTMENT RIGHT CUSP WEB AT STATION 477 CORRODED. REPAIRED CUSP WEB IAW ABX REA D85 3-26780MR. 2 L 7 4 4F 4A25 1999042300394 19990423 00394 WP 1999 4 23 ABXA9900291 1 19990224 A 5240 56157013 PAN DOUG DOUG DC8 DC862 3021970 WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND CRACK IN FORWARD SERVICE DOOR PAN AT SECOND DOOR STOP FROM BOTTOM, FORWARD SIDE OF DOOR. REPAIRE D IAW ABX REA D853-27050MR. 2 L 7 4 4F 4A25 1999042300395 19990423 00395 WP 1999 4 23 MWEA99147 1 19990414 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP BS 832 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE AFT PIT FLOOR FRAME AT STATION 832 AFT LOWER SIDE HAS SEVERAL AREAS OF CORROSION FROM 29R TO 29L. MAINTENANCE FABRI CATED AND INSTALLED REPAIR SPLICE PARTS. 2 L 7 2 4F A6WE 1999042300396 19990423 00396 WP 1999 4 23 MWEA99148 1 19990410 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOOR DISCONNECTED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 400ME 45727 THE GALLEY DOOR EVACUATION SLIDE DISCONNECTED FORWARD DOOR. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999042300397 19990423 00397 WP 1999 4 23 MWEA99149 1 19990414 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 502ME 48132 THE FORWARD PASSENGER DOOR GIRT BAR CABLE FELL OFF. MAINTENANCE REINSTALLED LANYARD ON GIRT BAR. 2 L 7 2 4F A6WE 1999042300398 19990423 00398 NM 1999 4 23 MWEA99151 1 19990411 A 5320 4943785503 CUP DOUG MD88 MD88 3023688 NM SERVICE DOORWAY DETERIORATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE AFT SERVICE DOOR HOLD OPEN HOOK PIN MOUNTED IN FUSELAGE RUBBER HAS DETERIORATED. MAINTENANCE REMOVED AND REPLACED C UP. 2 L 7 2 4F RT A6WE 1999042300399 19990423 00399 NM 1999 4 23 MWEA99152 1 19990411 A 5320 49568771 ANGLE DOUG MD88 MD88 3023688 NM BS 69 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE FORWARD ACCESSORY COMPARTMENT AT STATION 69 VERTICAL TO HORIZONTAL BEAM ATTACH ANGLE IS CRACKED. MAINTENANCE REMOVE D AND REPLACED ANGLE. 2 L 7 2 4F RT A6WE 1999042300400 19990423 00400 NM 1999 4 23 MWEA99153 1 19990403 A 5320 591214127 DOUBLER DOUG MD88 MD88 3023688 NM BS 1440 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND CRACKED DOUBLER IN AFT ACCESORY COMPARTMENT BETWEEN LONGERON 2R AND 3R AT APPORXIMATELY STATION 1440. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999042300401 19990423 00401 NM 1999 4 23 DHL9974101C 1 19990226 A 5720 HEAT SHIELD BOEING 727 7272Q9 138448M NM LEFT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING LEADING EDGE INTERIOR ANTI-ICE HEAT SHIELD IS CRACKED AT 3 ATTACH RIVETS. CUT OUT DAMAGED SECTION INSTALLED DOUBLER PER SRM 57-30-4, 13 BY 7, N/R 1440. 2 L 7 3 4F RT A3WE 1999042300402 19990423 00402 NM 1999 4 23 DHL9974102C 1 19990225 A 5730 SKIN BOEING 727 7272Q9 138448M NM RIGHT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT WING SURF PANEL OVER MLG SUPPORT MAIN BEAM WARPED AND DELAMINATED. INSTALLED HOT BOND REPAIR PER SRM 51- 20-3, 84 BY 1, N/R 2861. 2 L 7 3 4F RT A3WE 1999042300403 19990423 00403 NM 1999 4 23 DHL9974103C 1 19990225 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 1010-1025 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE EXTERIOR SEVERAL BROKEN FASTENERS STA 1010 TO 1025 SRT 29R. REMOVED INNER SKIN CORROSION. REMOVED BROKEN RIVETS AND INSTALLED SKIN REPAIR SPLICES FILLER AND DOUBLER PER SRM 53-30-31, 3 BY 11, N/R 3339. 2 L 7 3 4F RT A3WE 1999042300404 19990423 00404 NM 1999 4 23 DHL9974104C 1 19990225 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 1010 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, CRACKED FRAME AT STA 1010 UPPER FLANGE BETWEEN STR 25R AND 26R. CUT OUT DAMAGED AREA, FABRICATED FRAME REPA IR PER SRM 51-40-3, 13.5 BY 3.5 BY 1, AND INSTALLED PER SRM 51-40-3, N/R 3352. 2 L 7 3 4F RT A3WE 1999042300405 19990423 00405 NM 1999 4 23 DHL9974105C 1 19990226 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 1050 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, CORROSION AT FRAME AND INTERCOSTAL AT BS 1050 BETWEEN STR 27R AND 28R. REMOVED INTERCOSTAL, FOUND CORROSION ON SKIN, OUT OF LIMITS. REMOVED EXISTING DOUBLER FROM BS 1050 TO 1079. CUT OUT DAMAGED AREA. INSTALLED EXTERNAL SKIN REPAIR PER SRM 53-30-3, 31.5 BY 13.5. REPLACED INTERCOSTAL PER SRM 53-10-1, N/R 3412. 2 L 7 3 4F RT A3WE 1999042300406 19990423 00406 NM 1999 4 23 DHL9974106C 1 19990226 A 5754 SKIN BOEING 727 7272Q9 138448M NM NR 1 LE SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NR 1 SLAT LEADING EDGE EXTERIOR HAS FILLER MATERIAL IN DENTS. REMOVED DAMAGED AREA AND INSTALLED DOUBLER RE PAIR PER SRM 57-30-3, 8 BY 4.5, N/R 1351. 2 L 7 3 4F RT A3WE 1999042300407 19990423 00407 NM 1999 4 23 DHL9974107C 1 19990226 A 5720 ANGLE BOEING 727 7272Q9 138448M NM LEFT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING LEADING EDGE CAVITY INBD MOUNT SUPPORT ANGLE FOR THE NR 2 LEADING EDGE FLAP ACTUATOR IS CRACKED AT THE UPPER CORNER RADIUS. REPLACED MOUNT SUPPORT ANGLE PER SRM 51-30-2, 10 BY 6. REPLACED O/B MOUNT SUPPORT PER SRM 51 -30-2, 10 BY 6, N/R 1398. 2 L 7 3 4F RT A3WE 1999042300408 19990423 00408 NM 1999 4 23 DHL9974108C 1 19990226 A 5320 SUPPORT BOEING 727 7272Q9 138448M NM BS 305 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, AREA FWD OF E/E COMPARTMENT FS 305 CORROSION ON UNDER SIDE OF FLOOR SUPPORT CHANNEL RBL 0-15. REMOVED FLOOR SUPPORT CHANNEL. FABRICATED ANGLE FLOOR SUPPORT PER SRM 53-10-2, 12 BY 2.5. INSTALLED FLOOR PANELS, N/R 3438. 2 L 7 3 4F RT A3WE 1999042300409 19990423 00409 NM 1999 4 23 DHL9974109C 1 19990225 A 2782 ANGLE BOEING 727 7272Q9 138448M NM NR 2 LE SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING LEADING EDGE CAVITY INBD VERTICAL SUPPORT ANGLE FOR NR 2 SLAT ACTUATOR IS CRACKED. REMOVED AND RE PLACED VERTICAL SUPPORT ANGLE PER SRM 51-30-2. INSTALLED STAINLESS STEEL DOUBLER ON THE SUPPORT ANGLES PER S/B 57-130, N/R 1356. 2 L 7 3 4F RT A3WE 1999042300410 19990423 00410 NM 1999 4 23 DHL9974110C 1 19990225 A 5320 SUPPORT BOEING 727 7272Q9 138448M NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, CRACKED AFT CARGO COMPARTMENT FLOOR SUPPORT U CHANNEL BS 950D, RBL 12. CUT OUT DAMAGED SECTION, 10 INSTALLE D EXTRUDED ANGLE PER SRM 51-40-4, 18 LONG, N/R 3357. 2 L 7 3 4F RT A3WE 1999042300411 19990423 00411 NM 1999 4 23 DHL9974111C 1 19990225 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 580 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUS INTERIOR EVIDENCE OF CORROSION CRACK AT SKIN STA 580 AND STR 27L. CUT OUT CORRODED SKIN, INSTALLED DOUB LER REPAIR FROM STA 520 TO 610 BETWEEN STR 26L- 29L, 36.5 BY 23.5 AND 34 BY 15.5 PER AVITAS ENGINEERING ORDER 99AVHM 00 2RO-01, N/R 3369. 2 L 7 3 4F RT A3WE 1999042300412 19990423 00412 NM 1999 4 23 DHL9974112C 1 19990227 A 2150 PLENUM BOEING 727 7272Q9 138448M NM AIR COND SYST CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, CORROSION ON LEFT AND UPPER WALL OF AIR CONDITIONING PLENUM. INSTALLED SKIN REPAIR PER AVITAS ENGINEERING ORDER 99AVHM 004R0-01, FILLER 19 BY 18, DOUBLER 14 BY 10, TRIPLER 13 BY 9, N/R 3472/3454. 2 L 7 3 4F RT A3WE 1999042300413 19990423 00413 NM 1999 4 23 DHL9974113C 1 19990304 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 970 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, INNER SKIN GOUGED AT STA 970 BETWEEN STR 29R AND 28R. CUT OUT DAMAGE, INSTALLED DOUBLER/FILLER PER AVITAS EO 99AVHM001R0-1, FILLER 13.5 BY 3, DOUBLER 25 BY 15.75, N/R 3174. 2 L 7 3 4F RT A3WE 1999042300414 19990423 00414 NM 1999 4 23 DHL9974114C 1 19990225 A 5320 ANGLE BOEING 727 7272Q9 138448M NM BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WW STR 18A FWD RIB ATTACH ANGLE STA 940 FITTING IS CRACKED ON INBD END. REMOVED AND INSTALLED NEW ATTA CH ANGLE PER SRM 53-10-1, 6 BY 4.5, N/R 7078. 2 L 7 3 4F RT A3WE 1999042300415 19990423 00415 NM 1999 4 23 DHL9974115C 1 19990226 A 5313 STRINGER BOEING 727 7272Q9 138448M NM BS 615-628 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, CORROSION AT FWD CARGO COMPT BILGE INTERIOER ON STR 27R FS 615 -620 AND 628 RBL 14. CUT OUT DAMAGED SECTION . REPLACED SECTION OF STRINGER FROM 610 TO 630 PER SRM 53-10-3, N/R 3394. 2 L 7 3 4F RT A3WE 1999042300416 19990423 00416 NM 1999 4 23 DHL9974116C 1 19990225 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, EVIDENCE OF CORROSION AND SMALL CRACK AT BS 950C FRAME UPPER FLANGE BETWEEN S-26 L AND STR 27 L. CUT OUT DA MAGED AREA AT UPPER FLANGE, HFEC, INSTALLED FRAME REPAIR AT BS 950C PER SRM 51-40-3, N/R 3360. 2 L 7 3 4F RT A3WE 1999042300417 19990423 00417 NM 1999 4 23 DHL9974117C 1 19990228 A 5754 RIB BOEING 727 7272Q9 138448M NM NR 8 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, R/W ING NR 8 SLAT, INBD RIB CRACKED. INSTALLED DOUBLER REPAIR PER SRM 57-30-3, 2 BY 6, N/R 2882. 2 L 7 3 4F RT A3WE 1999042300418 19990423 00418 NM 1999 4 23 DHL9974118C 1 19990225 A 5730 PANEL BOEING 727 7272Q9 138448M NM RIGHT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT WING UPPER SURFACE PANEL AT RT SIDE OF APU EXHAUST OLD REPAIR PULLING FASTENERS. REMOVED PANEL AND INSTA LLED BONDING REPAIR PER SRM 51-40-6, 50 BY 6, N/R 2860. 2 L 7 3 4F RT A3WE 1999042300419 19990423 00419 NM 1999 4 23 DHL9974119C 1 19990219 A 5754 SKIN BOEING 727 7272Q9 138448M NM NR 5 LE SLAT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, PERFORM PERMANENT REPAIR UPPER L/E SLAT NR 5. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-50-3, 6 BY 7, N/R 2801. 2 L 7 3 4F RT A3WE 1999042300420 19990423 00420 NM 1999 4 23 DHL9974120C 1 19990226 A 5754 SKIN BOEING 727 7272Q9 138448M NM NR 4 LE SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NR 4 SLAT LEADING EDGE EXTEIOR HAS FILLER MATERIAL IN DENT, 16 INCHES FROM OUTBD EDGE. CUT OUT DAMAGED AREA , INSTALLED REPAIR PER SRM 57-30-3, 2 BY 2, 6 BY 6, N/R 1383. 2 L 7 3 4F RT A3WE 1999042300421 19990423 00421 NM 1999 4 23 DHL9974121C 1 19990306 A 5753 SKIN BOEING 727 7272Q9 138448M NM RT TE AFT FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT WING O/B AFT FLAP T/E DELAMINATED. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 10 BY 5, N/R 289 8. 2 L 7 3 4F RT A3WE 1999042300422 19990423 00422 NM 1999 4 23 DHL9974122C 1 19990226 A 5754 SKIN BOEING 727 7272Q9 138448M NM NR 3 LE SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NR 3 SLAT L/E LEADING EDGE EXTERIOR HAS FILLER IN DENT LOCATED 23 FROM OUTBD EDGE. CUT OUT DAMAGED AREA, FA BRICATED REPAIR DOUBLER 6 BY 9 AND FILLER 2.5 BY 5, PER SRM 57-50-3, N/R 1381. 2 L 7 3 4F RT A3WE 1999042300423 19990423 00423 NM 1999 4 23 DHL9974123C 1 19990225 A 5720 TIP BOEING 727 7272Q9 138448M NM LEFT WING GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING TIP LEADING EDGE THE INBD SIDE WHICH MATES NEXT TO SLAT IS GOUGED ON THE LOWER SURFACE. CUT OUT D AMAGED AREA. INSTALLED DOUBLER AND FILLER REPAIR PER SRM 51-30-2, 11 BY 8, N/R 1349. 2 L 7 3 4F RT A3WE 1999042300424 19990423 00424 NM 1999 4 23 DHL9974124C 1 19990301 A 2730 BOB WEIGHT BOEING 727 7272Q9 138448M NM RT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT ELEVATOR TAB BOB WEIGHT CRACKED AND CORROSION ON CENTER OF O/B BOB WEIGHTS. REMOVED AND REPLACED BOB WEIG HTS PER BOING O/M 55-20-1 AND SRM 51-80-9. N/R 4099 2 L 7 3 4F RT A3WE 1999042300425 19990423 00425 NM 1999 4 23 DHL9974125C 1 19990225 A 5280 HINGE BOEING 727 7272Q9 138448M NM LT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT MLG STRUT DOOR FWD HINGE HINGED FAIRING HAS CRACKED, HINGE AT DOOR ATTTACH. REPLACED HINGE PER SRM 51- 30-2, N/R 7004. 2 L 7 3 4F RT A3WE 1999042300426 19990423 00426 NM 1999 4 23 DHL9974126C 1 19990225 A 5753 SKIN BOEING 727 7272Q9 138448M NM LT TE FLAP DELAMIANTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT OUTBD FORE FLAP TRAILING EDGE ON UNDERSIDE SEPARATING. INSTALLED FIBERGLASS OVERLAY REPAIR AT LEFT OU TBD FORE FLAP TRAILING EDGE PER SRM 51-40-8, 9 BY 6. 2 L 7 3 4F RT A3WE 1999042300427 19990423 00427 NM 1999 4 23 DHL9974127C 1 19990225 A 5753 SKIN BOEING 727 7272Q9 138448M NM LT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT OUTBD TRAILING EDGE FLAP HAS SKIN SEPARATING ALONG TRAILING EDGE WS 436 THROUGH 656. INSTALLED FIBERGL ASS OVERLAY REPAIR PER SRM 51-40-8, 9 BY 6, 5 FT BY 5 AND 7 BY 4, N/R 1368. 2 L 7 3 4F RT A3WE 1999042300428 19990423 00428 NM 1999 4 23 DHL9974128C 1 19990225 A 5753 SKIN BOEING 727 7272Q9 138448M NM LT TE FOREFLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING I/B FLAPS FORE FLAP LOWER SURFACE I/B EDGE CHAFFING. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 18 BY 15, N/R 1379. 2 L 7 3 4F RT A3WE 1999042300429 19990423 00429 NM 1999 4 23 DHL9974129C 1 19990226 A 5720 ANGLE BOEING 727 7272Q9 138448M NM LEFT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING FIXED LEADING EDGE CAVITY UPPER OUTBD SUPPORT ANGLE AT SLAT STA 0 IS CRACKED AT AFT ATTACH FASTENE RS. REMOVED ANGLE, FABRICATED NEW SUPPORT ANGLE, PER SRM 51-40-3, 16 BY 1.625, N/R 1390. 2 L 7 3 4F RT A3WE 1999042300430 19990423 00430 NM 1999 4 23 DHL9974130C 1 19990226 A 5720 652165828 ANGLE BOEING 727 7272Q9 138448M NM WS 543 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING TRAILING EDGE TEMPORARY COVE PANEL SUPPORT ANGLE INSTALLED AT WS 543 CRACKED. REMOVED AND REPLAC ED ANGLES PER SRM 51-30-2, N/R 1422. 2 L 7 3 4F RT A3WE 1999042300431 19990423 00431 NM 1999 4 23 DHL9974131C 1 19990226 A 5713 STRINGER BOEING 727 7272Q9 138448M NM BS 560-567 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, EVIDENCE OF EXFOLIATION CORROSION AT STRINGER 27R BS 560-567 RBL 14. CUT OUT DAMAGED SECTION AND REPAIRED PER SRM 53-10-3, 12 INCHES LONG, N/R 3396. 2 L 7 3 4F RT A3WE 1999042300432 19990423 00432 NM 1999 4 23 DHL9974132C 1 19990225 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 1088 GALLED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, STA 1088 NR 1 SEAT TRACK GALLED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5, N/R 5729. 2 L 7 3 4F RT A3WE 1999042300433 19990423 00433 NM 1999 4 23 DHL9974133C 1 19990225 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 852 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NR 1 SEAT TRACK HAS LUGS BROKEN OFF GALLED AND CORRODED AT STA 852. REMOVED TRACK AND INSTALLED NEW TRACK PER SRM 51-30-2, N/R 5723. 2 L 7 3 4F RT A3WE 1999042300434 19990423 00434 NM 1999 4 23 DHL9974134C 1 19990312 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 480-600 GALLED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NR 2 SEAT TRACK GALLED STA 387. REMOVED SEATTRACK FROM STA 480 TO 600 AND REPLACED PER SRM 53-10-5, N/R 571 6. 2 L 7 3 4F RT A3WE 1999042300435 19990423 00435 NM 1999 4 23 DHL9974135C 1 19990227 A 5313 STRINGER BOEING 727 7272Q9 138448M NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, STRINGER 29R HAS CORROSION FROM STA 950 B TO STA 1010. CUT OUT FRAMES AT STA 950F AND 970, CUT OUT DAMAGED SECTION OF STRINGER 29R FROM STA 950D PLUS 8. REMOVED FRAMES AT STA 950D PLUS 5 RT AND 980. INSTALLED REPAIR ON 950 B -950C PER AVITAS EO 99AVHM001RO-1 L ANGLE 16.5. REPLACED STRINGER 950D TO 1000. INSTALLED STRINGER SPLICE REPAIRS ON STR 29R AT STA 950D PLUS 9 AND 950F PLUS 9 PER AVITAS EO. INSTALLED CIRCUMERENTIAL REPAIR AT STA 950 F STR 29R, 11 N/R 3477/3453. 2 L 7 3 4F RT A3WE 1999042300436 19990423 00436 NM 1999 4 23 DHL9974136C 1 19990226 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 312 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, INNER FUSELAGE SKIN CHAFFED BY FWD ENTRY DOOR. CUT OUT DAMAGED AREA BETWEEN STR 11L AND 10 L STA 312 PER S/ B 53-0198, VISUAL, HFEC AND X-RAY INSPECTED. INSTALLED EXTERNAL DOUBLER REPAIR PER DHLMIA 99-0004RR, 20.5 BY 14.5, N/R 3397/3476. 2 L 7 3 4F RT A3WE 1999042300437 19990423 00437 NM 1999 4 23 DHL9974137C 1 19990225 A 5320 SUPORT BOEING 727 7272Q9 138448M NM BS 950 BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FLOOR SUPPORT L CHANNEL BS 950D, RBL 16 BENT. CUT OUT DAMAGED SECTION, INSTALLED EXTRUDED ANGLE REPAIR, 11 PER SRM 51-40-4. 2 L 7 3 4F RT A3WE 1999042300438 19990423 00438 NM 1999 4 23 DHL9974138C 1 19990223 A 5320 WEB BOEING 727 7272Q9 138448M NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NOSE GEAR W/W LEFT SIDE WEB LIGHTING HOLE HAS CRACK FWD END. REMOVED WEB, INSTALLED NEW WEB PER SRM 51-40-2 , N/R 7026. 2 L 7 3 4F RT A3WE 1999042300439 19990423 00439 NM 1999 4 23 DHL9974139C 1 19990301 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 720 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE FRAME DENTED AT BS 720 ABOVE STR 17R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 51-40 -3, 7 BY 4.75, N/R 5745. 2 L 7 3 4F RT A3WE 1999042300440 19990423 00440 NM 1999 4 23 DHL9974140C 1 19990301 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 700 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE FRAME IS DENTED AT BS 700 ABOVE STRINGER 17R. CUT OUT DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-40-3, 7 BY 6 FT, N/R 5744. 2 L 7 3 4F RT A3WE 1999042300441 19990423 00441 NM 1999 4 23 DHL9974141C 1 19990225 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NR 1, 2, 3, 4 AND 5 SEAT TRACKS HAS CORRSION AND GALLED AT STA 950D. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 1 FROM 950C TO 950E AND INSTALLED NEW PER SRM 53-10-5, 40 N/R 5727. 2 L 7 3 4F RT A3WE 1999042300442 19990423 00442 NM 1999 4 23 DHL9974142C 1 19990225 A 5347 SEAT TRACK BOEING 727 7272Q9 138448M NM BS 438 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, NR 1,2,3,4, AND 5 SEAT TRACKS GALLED AT STA 438. SEAT TRACKS BURNISHED, NR 5 OUT OF LIMITS PER SRM. CUT OU T DAMAGED SEAT TRACK AT STA 420 TO 480 AND REPLACED PER SRM 51-30-2, N/R 5719. 2 L 7 3 4F RT A3WE 1999042300443 19990423 00443 NM 1999 4 23 DHL9974143C 1 19990223 A 5320 WEB BOEING 727 7272Q9 138448M NM BS 1277 CANNING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, AFT AIRSTAIRS RT LOWER TORQUE BOX HAS VERTICAL WEB OIL CANNING AT STA 1277. REPLACED REPAIR DOUBLER PER S/B 53-129, 30 BY 17, N/R 4055. 2 L 7 3 4F RT A3WE 1999042300444 19990423 00444 NM 1999 4 23 DHL9974144C 1 19990227 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 520 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE FRAME BS 520 IS DAMAGED AT STR 17R. STOP DRILLED AREA, HFEC, INSTALLED DOUBLER PER SRM 51-40-3, 7 BY 6, N/R 3449. 2 L 7 3 4F RT A3WE 1999042300445 19990423 00445 NM 1999 4 23 DHL9974145C 1 19990226 A 5320 SUPPORT BOEING 727 7272Q9 138448M NM BS 999 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, CORRSOIN ON SUPPORT WEB LOWER END FWD PF 999 CIR O/B OF STR 29R. REMOVED AND REPLACED WEB SUPPORT PER SRM 5 1-30-2, 4 BY 38, N/R 3437. 2 L 7 3 4F RT A3WE 1999042300446 19990423 00446 NM 1999 4 23 DHL9974146C 1 19990227 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 540 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE INTERIOR FRAME BODY STA 540 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA,HFEC, INSTALLED DOUBLER REP AIR PER SRM 51-40-3, 5.5 BY 6.5, N/R 3430. 2 L 7 3 4F RT A3WE 1999042300447 19990423 00447 NM 1999 4 23 DHL9974147C 1 19990227 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 560 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE INTERIOER FRAME BS 560 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-40 -3, 7 BY 5.25, N/R 3429. 2 L 7 3 4F RT A3WE 1999042300448 19990423 00448 NM 1999 4 23 DHL9974148C 1 19990227 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 580 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE INTERIOR FRAME BODY STATION 580 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-40-3, 6 BY 4.5, N/R 3428. 2 L 7 3 4F RT A3WE 1999042300449 19990423 00449 NM 1999 4 23 DHL9974149C 1 19990227 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE INTERIOR FRAME BS 600 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SR M 51-40-3, 7 BY 5.25, N/R 3427. 2 L 7 3 4F RT A3WE 1999042300450 19990423 00450 NM 1999 4 23 DHL9974150C 1 19990227 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 640 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE INTERIOR FRAME BS 640 CRACKED AT STR 17R. CUT OUT DAMAGED AREA, HFEC INSTALLED DOUBLER PER SRM 51- 40-3, 7 BY 5 FT, N/R 3426. 2 L 7 3 4F RT A3WE 1999042300451 19990423 00451 NM 1999 4 23 DHL9974151C 1 19990227 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 660 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, FUSELAGE INTERIOR BS 660 IS DAMAGED STR 17R. CUT OUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-40-3, 6.5 BY 5.25, N/R 3425. 2 L 7 3 4F RT A3WE 1999042300452 19990423 00452 NM 1999 4 23 DHL9974152C 1 19990226 A 5320 ANGLE BOEING 727 7272Q9 138448M NM BS 580 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, INDICATION OF CORROSION AT FWD CARGO COMPARTMENT INTERIOR BS 580 STRINGER 28R RBL 8. REMOVED AND FABRICATED NEW L ANGLE PER SRM 53-10-4, 7 BY 1 BY 1, N/R 3398. 2 L 7 3 4F RT A3WE 1999042300453 19990423 00453 NM 1999 4 23 DHL9974153C 1 19990225 A 5720 CHANNEL BOEING 727 7272Q9 138448M NM WS 495 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT WING LOWER T/E COVE PANEL I/B SUPPORT CHANNEL CRACKED I/B OF NR 12 SPOILER ACTUATOR STA 495. REMOVED AN D REPLACED SUPPORT CHANNEL PER SRM 51-30-2, N/R 2852. 2 L 7 3 4F RT A3WE 1999042300454 19990423 00454 NM 1999 4 23 DHL9974154C 1 19990225 A 5730 CHANNEL BOEING 727 7272Q9 138448M NM WS 500 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT WING COVE PANEL SUPPORT CHANNEL CRACKED, O/B OF NR 13 SPOILER ACTUATOR STA 500. REMOVED AND REPLACED SUP PORT CHANNEL PER SRM 51-30-2, N/R 2849. 2 L 7 3 4F RT A3WE 1999042300455 19990423 00455 NM 1999 4 23 DHL9974155C 1 19990225 A 5720 CHANNEL BOEING 727 7272Q9 138448M NM WS 601 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT WING LOWER T/E PANEL SUPPORT CHANNEL CRACKED, O/B OF NR 14 SPOILER ACTUATOR STA 601. REMOVED AND REPLACE D SUPPORT CHANNEL PER SRM 51-30-2, N/R 2848. 2 L 7 3 4F RT A3WE 1999042300456 19990423 00456 NM 1999 4 23 DHL9974156C 1 19990224 A 5720 ANGLE BOEING 727 7272Q9 138448M NM WS 349 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, RT WING UPPER L/E INTERIOR WEB AT STA 0 O/B SUPPORT ANGLE CRACKED L/E STA 349. REMOVED AND FABRICATED SUPPO RT ANGLE PER SRM 51-40-3 1, 65 BY 15, 65 N/R 2826. 2 L 7 3 4F RT A3WE 1999042300457 19990423 00457 NM 1999 4 23 DHL9974157C 1 19990303 A 5753 SKIN BOEING 727 7272Q9 138448M NM LT TE FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING I/B FORE FLAP DELAMIANTED IN TWO AREAS AT CENTER SECTION. INSTALLED BONDED REPAIR PER SRM 57-40-6 , 10 BY 8 AND 13 BY 17 FT, N/R 1457. 2 L 7 3 4F RT A3WE 1999042300458 19990423 00458 NM 1999 4 23 DHL9974158C 1 19990302 A 5753 SKIN BOEING 727 7272Q9 138448M NM LT TE MIDFLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, L/T WING I/B MID FLAP LOWER SURFACE LOWER SKIN PANEL HAS A CRACK JUST O/B OF NR 4 TRACK FAIRING. TRIMMED OU T DAMAGED, INSTALLED REPAIR AT LEFT WING MID FLAP PER SRM 57-50-4, 4 BY 22.5, N/R 1452. 2 L 7 3 4F RT A3WE 1999042300459 19990423 00459 NM 1999 4 23 DHL9974159C 1 19990225 A 5753 STRAP BOEING 727 7272Q9 138448M NM LT TE FOREFLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C CHECK, LEFT WING I/B FORE FLAP DELAMINATED AT I/B END AND CHAFE STRAP BROKEN. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, 15 BY 12 FT, N/R 1451. 2 L 7 3 4F RT A3WE 1999042300460 19990423 00460 SO 1999 4 23 SWIA971456 1 19990409 A 3020 INLET BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 227SW 120304 RIGHT ENGINE AIR INLET FAILURE. RETURNED TO FIELD. RAN ENGINE RIGHT INLET BOOT. OPS CHECK GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999042300461 19990423 00461 1999 4 23 SWIA971457 4 19990409 A 3425 AHC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1 FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 294SW 120321 FO'S ALTITUDE INDICATOR WAS IN A CONSTANT 15 DEGREE RIGHT BANK AND 20 DEGREE PITCH UP. CAPTAINS FLIGHT DIRECTOR WAS GIV ING ERRONEOUS INFORMATION AND AUTO PILOT WOULD NOT WORK AS WELL. RETURNED TO LAX. REINITIALIZED NUMBER TWO AHRS COMPUT ER. REMOVED AND REPLACED NUMBER ONE AHC 85. GROUND TEST AND OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999042300462 19990423 00462 SO 1999 4 23 SWIA971458 1 19990409 A 7712 TQ INDICATOR EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 156CA 120156 LARGE RIGHT ENGINE TORQUE FLUCTUATIONS FROM 60 PERCENT TO 84 PERCENT ON CLIMB THROUGH 5000. RETURNED TO PDX. RAN RIGHT ENGINE BUT COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T 4 T RT A31SO E20NE 1999042300463 19990423 00463 SO 1999 4 23 SWIA971459 1 19990409 A 7722 T6 INDICATOR EMB 120 EMB120RT SO PWA 118 PW118A NE NR 2 ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 270YV 120270 NUMBER TWO T6 INDICATOR FAILED AFTER DEPARTURE. RETURNED TO SEA. REMOVED AND REPLACED NUMBER TWO T6 INDICATOR IAW MM 7 7-20-00. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999042300464 19990423 00464 SO 1999 4 23 SWIA971460 1 19990409 A 3230 12025262501 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR FAILED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 190SW 120050 LANDING GEAR FAILED TO COME DOWN NORMALLY, HAD TO DROP IT BY ELECTRICAL OVERRIDE. REMOVED AND REPLACED LANDING GEAR REL AY BOX. GEAR SWING OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999042300465 19990423 00465 SO 1999 4 23 SWIA971461 1 19990403 A 2751 INDICATION EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 NM 07 194SW 120120 FLAP CONTROL FAULT UPON APPROACH TO AIRPORT, DID A GO AROUND AND FLAPS RESET. MADE NORMAL LANDING. OPS CHECKED FLAPS F OUR TIMES WITH NO PROBLEMS NOTED. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T 4 T RT A31SO E20NE 1999042300466 19990423 00466 1999 4 23 SWIA971462 4 19990403 A 2350 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 227SW 120304 THE FO'S PUSH TO TALK SWITCH ON THE EYEBROW PANEL STICKS. RETURNED TO FAT DUE TO INABILITY OF CREW TO COMMUNICATE. REP LACED FO'S PUSH TO TALK SWITCH ON GLARESHIELD WITH SERVICEABLE UNIT. OPS CHECK ON PUSH TO TALK SWITCH IS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999042300515 19990423 00515 WP 1999 4 23 RRXA99600 1 19990201 A 5730 5769600501 SKIN DOUG DC8 DC863 302198A WP WS 708-710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LEFT WING, LEADING EDGE, SKIN SCREW HOLES AT XFS 708 TO XFS 71 0, 2 INCHES BELOW TOP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER REO-05829. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) 2 L 7 4 4F 4A25 1999042300523 19990423 00523 WP 1999 4 23 TWAA9905701 1 19990416 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 953U 49267 THE EMERGENCY EXIT SIGNS AT FWD SIDE OF BOTH FWD EMERGENCY EXIT DOORS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHE CK-C 3-26-99 STL. 2 L 7 2 4F A6WE 1999042300524 19990423 00524 WP 1999 4 23 TWAA9905702 1 19990417 A 3350 COVER DOUG DC9 DC983 3022083 WP CABIN MISSING A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9413T 53188 THE EGRESS LIGHTS AT AFT CABIN WAS MISSING THE COVER AND THE RED LENS. REPLACED THE COVER 0105601-003PA40, LAMP 7732, L EN 0105607-301, AND THE END PIECE 015609-001. CHECK-C 9-1-98 STL. 2 L 7 2 4F RT A6WE 1999042300525 19990423 00525 WP 1999 4 23 TWAA9905703 1 19990415 A 5320 BRACKET DOUG DC9 DC931 3022065 WP BS 996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FORMER AT STA 996, LOWER ATTACH BRACKET AT RBL 22 IN TO LBL 22 IN. LOWER B RACKET WAS REMOVED AND NEW ONE INSTALLED PER SRM 51-01. 2 L 7 2 4F A6WE 1999042300526 19990423 00526 WP 1999 4 23 AT9900303 1 19990314 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 756-776 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT INBOARD SEAT TRACK AT BS 756-776 CORRODED. REMOVED CORRODED AREA , FABRICATED REPAIR SECTION, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 53-05 FIG 4F, 51-30-1, 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1999042300527 19990423 00527 WP 1999 4 23 AT9900304 1 19990326 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN UNDER THE LEFT HAND STATIC PORT CORRODED. REMOVED STATI C PORT, FABRICATED DOUBLER, FILLER AND INSTALLED SKIN REPAIR IAW DC9 SRM 53-04 FIG 31, 51-30-2, 51-10-3 AND REINSTALLED STATIC PORT. 2 L 7 2 4F A6WE 1999042300528 19990423 00528 WP 1999 4 23 AT9900305 1 19990411 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 617-640 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THREE RIVETS MISSING AND SKIN BOWED OUT AT BS 617-640 LONGERON 29L-29R. R EMOVED LEFT ADF PANEL AND BOX BEAM PANEL FOR ACCESS, MECHANICALLY REMOVED CORROSION, TREATED AND PRIMED SKIN, FABICATED DOUBLER AND FOUND TWO LONGERON TIES CRACKED. RECEIVED TWO LONGERON TIES, DRILLED, DEBURRED AND INSTALLED ALL PARTS AND REINSTALLED PREVIOUSLY REMOVED PANELS IAW DC9 SRM 53-04 FIG 42, 51-10-3, 51-10-4, 51-30-1, MM 20-15-0 AND MM 34-31-0. A LL SYSTEM CHECKED GOOD. 2 L 7 2 4F A6WE 1999042300529 19990423 00529 WP 1999 4 23 AT9900306 1 19990328 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE BELLY SKIN ON RIGHT SIDE AT BS 937 L-28-29 JUST FORWARD OF EXISTING RE PAIR CORRODED AND WITH A ONE INCH CRACK. REMOVED OUT EXISTING REPAIR, CUT OUT CORRODED AND CRACKED SECTION, FABRICATED DOUBLER, FINGER DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC9 SRM 53-04 FIG 12B AND RE S NR 99683. 2 L 7 2 4F A6WE 1999042300530 19990423 00530 WP 1999 4 23 AT9900307 1 19990328 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 965 CORRODED. FABRICATED FLOOR SUPPORT SECTION, F ORMED DOUBLER REPAIRS AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999042300531 19990423 00531 WP 1999 4 23 AT9900308 1 19990409 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 345 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN AT BS 345 L-27L CORRODED AROUND LEFT HAND ALTERNATE STAT IC PORT. FABRICATED AND INSTALLED FLUSH SKIN REPAIR IAW DC9 SRM 53-04 FIG 30 AND EO NR 99-1126. 2 L 7 2 4F A6WE 1999042300532 19990423 00532 WP 1999 4 23 AT9900309 1 19990315 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 390-410 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LOWER AND INNER SKIN AT BS 390-410 ON THE RIGHT SIDE CORRODED. FABRIC ATED REPAIR AND INSTALLED ON LOWER SKIN BELOW FORWARD CARGO DOOR IAW DC9 SRM 51-30-2, 51-30-5 AND 51-10-3. 2 L 7 2 4F A6WE 1999042300533 19990423 00533 EU 1999 4 23 JBXA9900081 2 19990416 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 FAILED A JBXA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 05 133ML 11330 17525 ON DESCENT TO RDU AIRPORT THE CAPTAIN REPORTED A NR 1 GEN FAILURE FAULT FOLLOWED BY A NR 1 ENG SURGE. TRIED TO REDUCE P OWER ON THE NR 1 ENG AND RECEIVED A NR 1 ENG FAILURE MESSAGE. THE CAPTAIN SHUT DOWN THE NR 1 ENG, DECLARED AN EMERGENCY , CONTINUED DESCENT AND LANDED IN RDU WITHOUT INCIDENT. IN PROGRESS AWAITING ENG FOR NR 1 ENG CHANGE. 2 L 7 2 4F 4 F RT 1999042300534 19990423 00534 NM 1999 4 23 AWXA9900131 1 19990410 A 2421 106122412 GENERATOR 735511A BOEING 737 73733A 1384673 NM NR 2 ENGINE FAILED A AWXA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS H M J ELECT. POWER LOSS-50 PC OVER TEMP WARNING INDICATION CR CRUISE 1 WP 28 172AW 10616 3115 B1149 23631 GEN DROPPED OFF LINE. P/N 03-2411-9-0003, P/N 03-2411-9-0002. DURING CRUISE AT FL 290, NR 2 ENGINE GEN DROPPED OFF LIN E. THEN GOT A NR 2 CSD LOW OIL PRESS LIGHT. FOLLOWED THE QRH, PUT THE APU ON LINE AND DISCONNECTED THE CSD, THEN CHECK ED RESIDUAL VOLTS. FOUND 10 VOLTS STILL SHOWING, CSD OIL TEMP CONTINUED TO RISE. FLIGHT CREW ASSUMED NO DISCONNECT AND DIVERTED TO ABQ. CLEANED CONNECTOR AND DISCONNECTED CSD NO VOLTS, TEMP 0, MEL UNIT. REMOVED AND REPLACED NR 2 CSD OIL COOLER, NR 2 ENGINE GENERATOR NR 2 ENGINE CSD. 2 L 7 2 4F RT A16WE 1999042300535 19990423 00535 EU 1999 4 23 AWXA9900132 1 19990406 A 5347 D5311209220600 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 CABIN SEAT TRACK NR 4 FRAME 20 CORRODED BEYOND SRM LIMITS. SEAT TRACK REMOVED, FABRICATED NEW TRACK PER DRAWING D531120 92, SPLICED NEW SEAT TRACK INTO EXISTING STRUCTURE PER SRM 53-11-14. SURROUNDING STRUCTURE TREATED AND PRIMED. 2 L 7 2 4F RT A28NM 1999042300536 19990423 00536 EU 1999 4 23 AWXA9900133 1 19990406 A 5347 209220600 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 CABIN SEAT TRACK NR 3 FRAME 20 CORRODED BEYOND SRM LIMITS. TRACK REMOVED, FABRICATED NEW TRACK PER DRAWING D53112092, S PLICED NEW SEAT TRACK INTO EXISTING STRUCTURE PER SRM 53-11-14. SURROUNDING STRUCTURE TREATED AND PRIMED. 2 L 7 2 4F RT A28NM 1999042300537 19990423 00537 EU 1999 4 23 AWXA9900134 1 19990406 A 5315 D53111414200 FLOORBEAM AIRBUS 320 A320231 3930325 EU BS 254 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 FWD CABIN FLOORBEAM AT Y254 RT SURFACE CORRODED BEYOND SRM LIMITS FRAME 12 TO FRAME 16. FLOORBEAM REMOVED, FABRICATED N EW FLOORBEAM AS PER DWG D53112836, SPLICED NEW FLOORBEAM TO EXISTING STRUCTURE AS PER SRM 53-11-14. SURROUNDING STRUCTU RE TREATED AND PRIMED. 2 L 7 2 4F RT A28NM 1999042300538 19990423 00538 EU 1999 4 23 AWXA9900135 1 19990406 A 5315 D53111414200 FLOORBEAM AIRBUS 320 A320231 3930325 EU BS 189 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 FWD CABIN FLOORBEAM AT Y189 RT UPPER FLANGE CORRODED BEYOND SRM LIMITS FRAME 21 TO FRAME 22. FLOORBEAM REMOVED, FABRICA TED NEW DUMMY RAIL PER DWG D53112836, SPLICED NEW DUMMY RAIL TO EXISTING STRUCTURE PER SRM 53-11-14. SURROUNDING STRUCT URE TREATED AND PRIMED. 2 L 7 2 4F RT A28NM 1999042300539 19990423 00539 EU 1999 4 23 AWXA9900136 1 19990406 A 5311 FRAME AIRBUS 320 A320231 3930325 EU FUSELAGE BENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 622AW 054 FWD CARGO FLOOR FRAME AT FRAME 31, STR 39, LT RIVETS SHEARED AND FRAME BENT. FABRICATED NEW ANGLE PER DWG 59511600202 A ND SRM 51-22-11, ANCHOR NUTS REPLACED AND STRUCTURAL AREA RIVETED PER SRM 51-72-11 & 51-73-00. 2 L 7 2 4F RT A28NM 1999042300540 19990423 00540 1999 4 23 AWXA9900137 2 19990414 A 7200 ENGINE BOEING 737 737297 1384480 NM NR 1 FAILED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 WP 28 147AW 22630 AIR TURNBACK, ENGINE SHUT DOWN. ON CLIMBOUT OIL TEMP ON NR 1 ENG WAS IN THE RED BAND. ENGINE WAS SHUTDOWN INFLIGHT PER QRH. DRAINED 1 GALLON ENGINE OIL FROM NR 1 ENG. RAN ENGINES AT T/O POWER, OPS NORMAL AT THIS TIME. AIRCRAFT WAS RELE ASED FOR REVENUE SERVICE PER THE WRONG FIM CHART (USED -15 CHART SHOULD HAVE BEEN -9 ) AND FLEW PHX-DEN-PHX. MAINTENANC E DETERMINED ENGINE OIL TEMP EXCEEDED PARAMETERS AND ENGINE HAD TO BE CHANGED. 2 L 7 2 4F A16WE 1999042300541 19990423 00541 NM 1999 4 23 AWXA9900138 1 19990413 A 2782 ACTUATOR BOEING 757 757225 1384959 NM NR 1 LE SLAT FAILED A AWXA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 914AW 22208 AIR TURNBACK, SLAT LOCKED OUT. TAKEOFF FROM PHX, UPON FLAP RETRACTION LEADING EDGE SLAT DISAGREE LIGHT CAME ON. QRH FO LLOWED LANDED AT PHX WEIGHT 196,000. REMOVED AND REPLACED NR 1 SLAT ROTARY ACTUATOR, CK AND ADJUSTED THE PRELOAD FOR TH E NR 10 SLAT, LUBED ALL SLATS. UPDATE: 16 APR 99 A/C EXPERIENCED 2 EMERGENCY LANDINGS BOTH INVOLVE SLAT DISAGREE MESSAG ES. 2 L 7 2 4F RT A2NM 1999042300542 19990423 00542 EU 1999 4 23 AWXA9900139 1 19990414 A 2752 ACTUATOR AIRBUS 320 A320231 3930325 EU TE FLAPS FAILED A AWXA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 637AW 099 AIR TURNBACK, FLAPS LOCK OUT (P/N 26-2700-9-0002) (S/N 0541) AFTER T/O, FLAP RETRACT ECAM ADVISED FLIGHT CONTROL FLAPS LOCKED OUT WING TIP BREAK ON. SOC ADVISED TO RETURN TO PHX. LANDING WEIGHT 138,000, L ANDING UNEVENTFUL. REMOVED AND REPLACED RT WING TIP BRAKE PER MM CH 27-51-401, WTB TEST GOOD. REMOVED AND REPLACED NR 4 FLAP ACTUATOR. OPERATED SEVERAL TIMES, UNABLE TO GET FLAPS TO LOCK OUT. RIG CHECK ON ALL 4 ACTUATORS IS GOOD. 2 L 7 2 4F RT A28NM 1999042300543 19990423 00543 EU 1999 4 23 AWXA9900140 1 19990319 A 2931 O RING AIRBUS 320 A320231 3930325 EU GREEN HYD SYST LEAKED A AWXA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 626AW 65 GREEN HYDRAULIC RESERVOIR LOW ECAM FOLLOWED, THEN WITH LGCIU FAULT NR 1 HIGH LIGHTED NORMAL LANDING, THRUST REVERSERS AN D NOSE WHEEL STEERING INDICATIONS AFTER TOUCH DOWN. REMOVED AND REPLACED O RING AT GREEN SYSTEM PRESSURE SWITCH (P/N 11 51GN), OPS CK AND LEAK CK GOOD IAW AIRBUS MM 29-32-401. 2 L 7 2 4F RT A28NM 1999042300544 19990423 00544 WP 1999 4 23 CALA9900413 1 19990415 A 5320 BRACKET DOUG DC10 DC1030 3023501 WP TAIL CONE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND TAIL CONE CENTER RT, UPPER RT, AND UPPER LT SPIGOT MOUNTING BRACKETS CRACKED. EACH BRACKET HAD A 3 INC H CRACK. THE BRACKETS WERE REPAIRED IAW SRM 53-30-00, FIGURE 3. 2 L 7 3 4F A22WE 1999042300545 19990423 00545 WP 1999 4 23 CALA9900414 1 19990415 A 5320 BEAM DOUG DC10 DC1030 3023501 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND SUPPORT BEAM CORRODED AT CENTER CARGO BAY CENTER ROLLER CHANNEL ADJOINING BULK CARGO AREA. THE SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 53-42-00. 2 L 7 3 4F A22WE 1999042300546 19990423 00546 WP 1999 4 23 CALA9900415 1 19990415 A 5320 SILL DOUG DC10 DC1030 3023501 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND CENTER CARGO BAY DOOR SILL LOWER AFT FRAME AND LOWER FORWARD FRAME CORRODED. THE LOWER AFT AND LOWER F ORWARD FRAMES WERE REPAIRED IAW SRM 53-50-00, PAGES 119-130. 2 L 7 3 4F A22WE 1999042300547 19990423 00547 WP 1999 4 23 CALA9900416 1 19990415 A 5320 ANGLE DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED AROUND HI SHEARS. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1999042300548 19990423 00548 NM 1999 4 23 CALA9900417 1 19990415 A 5313 STRINGER BOEING 727 727243 138408D NM BS 1183-1161 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 4 INCH CRACK IN STRINGER 23L BETWEEN STA 1183 AND 1161, JUST BELOW LAV SERVICE PANEL INSIDE AFT CARGO COMPARTMENT. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A NEW STRINGER, DOUBLER AND FILLER COVER PLATE WERE INSTALLE D IAW SRM 51-10-2 AND ECRA 5330-02798. 2 L 7 3 4F RT A3WE 1999042300549 19990423 00549 NM 1999 4 23 CALA9900418 1 19990415 A 5330 SKIN BOEING 727 727243 138408D NM LAV SERVICE PNL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND AFT LAV SERVICE PANEL AFT LOWER SKIN CORRODED. THE PANEL WAS REMOVED AND THE CORRODED INNER SKIN WAS R EMOVED. A NEW SKIN AND INTERNAL AND OUTER DOUBLER WERE INSTALLED AND THE PANEL WAS REINSTALLED IAW SRM 51-10-2, PAGE 1, 51-30-2, PAGE 1 AND ECRA 5330-02799. 2 L 7 3 4F RT A3WE 1999042300550 19990423 00550 WP 1999 4 23 CALA9900419 1 19990416 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 1801-1841 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND DAMAGED CHANNEL SECTION IN CENTER CARGO BAY AT STA 1801-1841. THE CHANNEL WAS REPLACED WITH A NEW CHAN NEL IAW MM 25-52-01. 2 L 7 3 4F A22WE 1999042300551 19990423 00551 WP 1999 4 23 CALA9900420 1 19990416 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 237 BETWEEN LONGERON 17L AND 18L. THE SKIN AND LOWER SECTION OF FINGER DOUBLER WERE REPLACED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1999042300552 19990423 00552 WP 1999 4 23 CALA9900421 1 19990416 A 5210 INTERCOSTAL DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL OF FORWARD ENTRY DOOR JUST AFT OF INTERNAL DOOR HANDLE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999042300553 19990423 00553 WP 1999 4 23 CALA9900422 1 19990416 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-265 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 200-265. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05 . 2 L 7 2 4F A6WE 1999042300554 19990423 00554 SO 1999 4 23 COMA9910063 1 19990415 A 3397 WIRE EMB 120 EMB120RT SO CABIN CHAFED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 463CA 120267 EMERGENCY LIGHTS C/B TRIPPED. REPAIRED CHAFED WIRING AT F/A LIGHTING PANEL. 2 L 7 2 4T RT A31SO 1999042300555 19990423 00555 EA 1999 4 23 COMA9960156 1 19990416 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 924A 7026 LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 1999042300556 19990423 00556 EA 1999 4 23 COMA9960157 1 19990416 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A COMA K NONE N FALSE WARNING DE DESCENT 1 SO 01 716CA 7250 CARGO SMOKE WARNING. REPLACED CARGO COMPARTMENT SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 1999042300557 19990423 00557 EA 1999 4 23 COMA9960158 1 19990414 A 3230 864807 PROX SENSOR CNDAIR CL600 CL6002B19 EA RT MLG MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 959CA 11686 7116 LANDING GEAR DISAGREE AFTER TAKEOFF. REPLACED THE RIGHT HAND MLG UPLOCK SENSOR. 2 L 7 2 4F RT A21EA 1999042300558 19990423 00558 EA 1999 4 23 COMA9960159 1 19990414 A 2750 860D10018 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 01 934CA 6796 7042 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999042300559 19990423 00559 EA 1999 4 23 COMA9960160 1 19990418 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 959CA 6058 7116 FLAP CAUTION MESSAGE AFTER LANDING. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999042300560 19990423 00560 NM 1999 4 23 UPS99229321 1 19990328 A 5753 65192699 TRACK BOEING 727 72731C 1384011 NM NR 5 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACK ON NR 5 FLAP TRACK. TRACK REPLACED, REF TC C57-581-04-4D FOR INSTALLATION. 2 L 7 3 4F A3WE 1999042300561 19990423 00561 NM 1999 4 23 UPS99229322 1 19990322 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 294.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CORROSION AT LAP S24R BS 294.5. CRACK CONFIRMED IN FASTENER HOLE. REPAIR CARRIED OUT PER EO B727 -533 0-0509 APPX 8.3 AND DWG 69-61590. 2 L 7 3 4F A3WE 1999042300562 19990423 00562 NM 1999 4 23 UPS99229323 1 19990322 A 5330 SKIN BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+S1, LIGHT SURFACE CORROSION ON SKIN UNDER NR 2 ADF ANTENNA (LWR AFT). CORROSION CONFIRMED ON EXTRUDED STIFFENER. STIFFENER REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999042300563 19990423 00563 NM 1999 4 23 UPS99229324 1 19990323 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACKS ON O/B FLANGE BS 740 RT BETWEEN S18 R AND S24R. CRACKS CONFIRMED BY HFEC. REPAIR CARRIED OUT IAW UPS EO B727-5310-74 97. 2 L 7 3 4F A3WE 1999042300564 19990423 00564 NM 1999 4 23 UPS99229325 1 19990409 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 700 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, DAMAGE STR 22 BS 700 RT AT FRAME ATTACH POINT. STRINGER REPAIRED AS PER SRM 53-10-3 FIG 1 DETAIL 2. 2 L 7 3 4F A3WE 1999042300565 19990423 00565 NM 1999 4 23 UPS99229326 1 19990408 A 5330 106003145 PANEL BOEING 727 72731C 1384011 NM WS 550 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, ACCESS PANEL NR 8 FOR NR 3 FUEL TANK CORRODED. PANEL REPLACED PER MM 28-11-21. 2 L 7 3 4F A3WE 1999042300566 19990423 00566 NM 1999 4 23 UPS99229327 1 19990407 A 5753 65281096 CASTING BOEING 727 72731C 1384011 NM TE FLAPS WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 5 JACKSCREW FAIRING, AFT BEARING WORN. BEARING CASTING REPLACED PER DWG 65-26786 AND SRM 51-30 -2. 2 L 7 3 4F A3WE 1999042300567 19990423 00567 NM 1999 4 23 UPS99229328 1 19990406 A 5320 6930033010 RING BOEING 727 72731C 1384011 NM WS 400-725 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, RT WING NR 3 FUEL TANK ACCESS PANEL CLAMP UP RINGS CORRODED ON NR 2 THRU NR 14. CLAMP UP RINGS RE PLACED IAW MM 28-11-21. 2 L 7 3 4F A3WE 1999042300568 19990423 00568 NM 1999 4 23 UPS99229329 1 19990406 A 5330 BAC10600313002 PANEL BOEING 727 72731C 1384011 NM WS 180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 1 ACCESS PANEL RHS FOR NR 2 INTEGRAL SECTION CORRODED. PANEL REPLACED IAW MM 28-11-21. 2 L 7 3 4F A3WE 1999042300569 19990423 00569 NM 1999 4 23 UPS99229330 1 19990405 A 5755 69669662 CASTING BOEING 727 72731C 1384011 NM NR 8 SPOILER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 8 SPOILER O/B HINGE CASTING WORN ON RT WING T/E. CASTING REPLACED IAW DWG 65-16216. 2 L 7 3 4F A3WE 1999042300570 19990423 00570 NM 1999 4 23 UPS99229331 1 19990405 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CORROSION IN STR 23, BS 700 RHS. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 1999042300571 19990423 00571 NM 1999 4 23 UPS99229332 1 19990403 A 5753 CHANNEL BOEING 727 72731C 1384011 NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 5 FLAP TRACK AFT FAIRING CRACK IN CHANNEL SECTION AT UPPER O/B ATTACH POINT. CHANNEL SECTION R EPLACED IAW SRM 51-20-1 FIG 7 AND SRM 57-20-2 FIG 4. 2 L 7 3 4F A3WE 1999042300572 19990423 00572 NM 1999 4 23 UPS99229333 1 19990403 A 5753 65413425 CASTING BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 6 FLAP TRACK MID FAIRING FWD HINGE CASTING CORRODED AT LUGS. CASTING REPLACED IAW DWG 65-21795 . 2 L 7 3 4F A3WE 1999042300573 19990423 00573 WP 1999 4 23 UPS99829305 1 19990403 A 5320 4641326 FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, STA 1690, THE STR 28R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300574 19990423 00574 WP 1999 4 23 UPS99829306 1 19990406 A 5320 57502571 FITTING DOUG DC8 DC873F 302199F WP BS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, STA 610, THE STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300575 19990423 00575 WP 1999 4 23 UPS99829307 1 19990409 A 5320 37538451 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, STA 1180, THE LONGERON END FITTING IS CORRODED (STR 35R). REMOVED AND REPLACED FITTING IAW DWG 37 53845-1. 2 L 7 4 4F RT 4A25 1999042300576 19990423 00576 WP 1999 4 23 UPS99829308 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 828.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 828.750 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300577 19990423 00577 WP 1999 4 23 UPS99829309 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 835 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 835 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300578 19990423 00578 WP 1999 4 23 UPS99829310 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 572.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300579 19990423 00579 WP 1999 4 23 UPS99829311 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 647.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 647.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300580 19990423 00580 WP 1999 4 23 UPS99829312 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 603.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, LT WING L/E RIB AT STA FS 603.75 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300581 19990423 00581 WP 1999 4 23 UPS99829313 1 19990407 A 5320 577327558 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, MAIN CABIN AT STA 680 BL 0, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTI NG IAW DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300582 19990423 00582 WP 1999 4 23 UPS99829314 1 19990407 A 5320 577327558 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, MAIN CABIN AT STA 680 AND RBL 24, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300583 19990423 00583 WP 1999 4 23 UPS99829315 1 19990407 A 5320 37739062 FITTING DOUG DC8 DC873F 302199F WP BS 717 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123 MAIN CABIN AT STA 717 AND RBL 24, THE SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300584 19990423 00584 WP 1999 4 23 UPS99829316 1 19990407 A 5320 37739062 FITTING DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, MAIN CABIN AT STA 781 AND RBL 24, THE SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IA W DWG 3773906 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300585 19990423 00585 WP 1999 4 23 UPS99829317 1 19990407 A 5320 37739062 FITTING DOUG DC8 DC873F 302199F WP BS 822 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, MAIN CABIN AT STA 822 LBL 24, THE SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DW G 3773906 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999042300586 19990423 00586 WP 1999 4 23 UPS99829318 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 741.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, RT WING L/E RIB AT STA FS 741.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300587 19990423 00587 WP 1999 4 23 UPS99829319 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 735 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123, RT WING L/E RIB AT STA FS 735.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999042300588 19990423 00588 WP 1999 4 23 UPS99829334 1 19990417 A 3350 BULB DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:N/A, CAPT'S EMERGENCY INSTRUMENT LIGHT OUT. RELAMPED CAPT'S EMERGENCY INSTRUMENT LIGHT, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999042300589 19990423 00589 WP 1999 4 23 UPS99829335 1 19990417 A 3240 3053230001 VALVE DOUG DC8 DC873F 302199F WP LT MLG BRAKE INOPERATIVE A IPXA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 801UP 46101 INSPECTION TYPE:N/A, AFTER LANDING LEFT BRAKE DID NOT APPEAR TO BE APPLYING BRAKE PRESSURE. FOUND LEFT FORK ON HYD PWR BRAKE BROKEN. REMOVED AND REPLACED VALVE PER 32-42-02. LEAK CHECKS, PRESSURE CHECKS AND DECAY CHECKS GOOD PER MM REFER ENCED ABOVE. (P/N 3053230-0-0-1), (S/N 66X 0341CT) ON, (S/N P715) OFF. 2 L 7 4 4F RT 4A25 1999042300590 19990423 00590 NE 1999 4 23 99FDEA00144 2 19990417 A 7200 ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 3 MALFUNCTIONED A FDEA J A DUMP FUEL UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 25 583FE 48421 99-89 - NR 3 ENG N1 INTERMITTENTLY DROPS AND A/C SHUDDERS. REMOVED AND REPLACED NR 3 ENG AS PER MM 71-00-02-4. REF WOR K CARD 71T0101. 2 L 7 3 4F 4 F RT A22WE E31N3 1999042300591 19990423 00591 NM 1999 4 23 99FDEA00145 1 19990417 A 5242 DOOR BOEING 727 727233 138408A NM E & E COMPT NOT LATCHED A FDEA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 25 221FE 20932 AFT T/O, EQUIPMENT DOOR CAME OPEN AND A/C WOULD NOT PRESSURIZE. FOUND E & E DOOR UNLOCKED. LOCKED AND PRESSURIZED ON G ROUND IN HRL. 2 L 7 3 4F RT A3WE 1999042300592 19990423 00592 NM 1999 4 23 99FDEA00146 1 19990417 A 2613 OVERHEAT LIGHT BOEING 727 727233 138408A NM AFT BODY ILLUMINATED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 258FE 20940 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. CLOSED LEFT PACK SWITCH AND NR 1 ENG BLD VALVE AFT RETARD NR 1, THROTTLE LIG HT WENT OUT AND STAY OUT. RAN NR 1 AND NR 2 ENGINE, NO LEAK FOUND. INSPECTED LOWER AFT BODY OVERHEAT DETECTOR, NORM PE R MM 26-14-00. 2 L 7 3 4F RT A3WE 1999042300593 19990423 00593 NM 1999 4 23 99FDEA00147 1 19990417 A 3260 SWITCH BOEING 727 727233 138408A NM RT MLG DOOR INOP A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 268FE 21674 99-92 - RT MAIN GEAR DOOR LIGHT ON S/O PNL AND RED DOOR LIGHT ON FWD IND. PNL BOTH REMAIN ILLUMINATED. REMOVED AND REP LACED RT GEAR DOOR WARN SWITCH PER 727-200 MM 32-62-11. OPS CK GOOD. 2 L 7 3 4F RT A3WE 1999042300594 19990423 00594 NM 1999 4 23 99FDEA00148 1 19990416 A 5313 655624540 STRINGER BOEING 727 727247 138408F NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 WHILE WORKING NR 802, FOUND CORROSION ON STRINGER 28R, BS 950E+1. 2 L 7 3 4F A3WE 1999042300595 19990423 00595 NM 1999 4 23 99FDEA00149 1 19990416 A 5315 65208359 FLOORBEAM BOEING 727 727247 138408F NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 NR 794 - CORROSION (C53-111-01(3)) ON FLOORBEAM LWR CHORD AT BS 1070, WL 200, LBL 40 - RBL 48. REMOVED AND REPLACED BS 1070 FLOORBEAM IAW FEDEX EA 7-5310-45262A. 2 L 7 3 4F A3WE 1999042300596 19990423 00596 NM 1999 4 23 99FDEA00150 1 19990416 A 5311 651634443 FRAME BOEING 727 727247 138408F NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 NR 790 - CORROSION (C53-111-01(3)) ON FRAME AT BS 1070, STR 27R. REPAIRED FRAME AT BS 1070, STR 27R, IAW FEDEX SRM 51-4 0-3 FIG 1. 2 L 7 3 4F A3WE 1999042300597 19990423 00597 WP 1999 4 23 MWEA99154 1 19990415 A 2560 113317 DOOR SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 207ME 47794 THE MAIN ENTRANCE DOOR SLIDE DETACHED WHEN MAIN CABIN WAS OPENED. MTC REINSTALLED EVACUATION SLIDE. 2 L 7 2 4F A6WE 1999042300598 19990423 00598 WP 1999 4 23 MWEA99155 1 19990407 A 5320 9958212502 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 754 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 REMOVED INTERCOSTAL FROM STATION 754 70 AT LONGERON 28 R DUE TO HEAVY TOOL MARKS. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999042300599 19990423 00599 WP 1999 4 23 MWEA99156 1 19990414 A 5320 99582123 TEE DOUG DC9 DC932 3022066 WP BS 760 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 STATION 760 TEE IS BLENDED BEYOND LIMITS BETWEEN LONGERON 28 & 29L. MTC FABRICATED AND INSTALLED NEW TEE SECTION. 2 L 7 2 4F A6WE 1999042300600 19990423 00600 WP 1999 4 23 MWEA99157 1 19990412 A 5313 1242886 LONGERON DOUG DC9 DC932 3022066 WP BS 804-950 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND HEAVY CORROSION ON LONGERON 30 FROM STATION 804 TO 950. MTC FABRICATED, INSTALLED LONGERON AND -9 FITTING. 2 L 7 2 4F A6WE 1999042300601 19990423 00601 NM 1999 4 23 SCNA99063 1 19990413 A 3350 LIGHTS BOEING 727 7272A1 138407F NM AFT AIRSTAIR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 DURING A LINE MAINTENANCE CHECK, TWO AFT AIRSTAIR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. RELAMPED 2 AIRSTAIR LI GHTS AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999042300602 19990423 00602 NM 1999 4 23 DHL9974160C 1 19990226 A 5320 ANGLE BOEING 727 7272Q9 138448M NM BS 307 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 741DH 21931 AT C-CHECK, FS 307 RBL 12-15 FLANGE OF FLOOR SUPPORT ANGLE DAMAGED AND HAS CORROSION. REMOVED DAMAGED FLOOR SUPPORT, F ABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-10-2, 20 X 24. 2 L 7 3 4F RT A3WE 1999042300603 19990423 00603 NM 1999 4 23 VNAA9904001 1 19990412 A 3231 LATCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG DOORS MALFUNCTIONED A VNAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 442JS 3060 HEAVY VIBRATION WAS NOTED WHEN LANDING GEAR WAS IN A RETRACTED CONDITION. WHEN THE LANDING GEAR WAS EXTENDED, THE VIBRA TION WOULD GO AWAY. UPON LANDING, OUTSTATION MAINTENANCE INSPECTED AND RELATCHED THE NOSE GEAR DOOR, IN ACCORDANCE WITH JIC 52-18-00. THE GEAR WELL AREA WAS INSPECTED WITH NO OTHER DEFECTS NOTED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999042300604 19990423 00604 NM 1999 4 23 VNAA9904002 1 19990411 A 3260 OL3092 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FAILED A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 427JS 3039 ON APPROACH, THE LEFT HAND MAIN LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED. AN EMERGENCY WAS DECLARED AND FLIGHT H ANDBOOK PROCEDURES WERE FOLLOWED. THE FLIGHT CREW REPLACED A GEAR INDICATOR LIGHT BULB. AFTER THE REPLACEMENT, THE IND ICATOR ILLUMINATED A DOWN AND LOCKED GEAR CONDITION. THE FLIGHT CONTINUED THE APPROACH AND LANDED WITHOUT FURTHER INCID ENT. OUTSTATION MAINTENANCE INSPECTED THE INDICATOR BULBS FOR DEFECTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999042300605 19990423 00605 NM 1999 4 23 VNAA9904003 1 19990409 A 3230 PIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG NOT REMOVED A VNAA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 GL 07 433JS 3047 AFTER TAKEOFF, THE RIGHT HAND MAIN LANDING GEAR FAILED TO RETRACT WHEN SELECTED. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED. MAINTENANCE INSPECTED AND FOUND A GEAR SAFETY PIN INSTALLED ON THE GEAR LEG . MAINTENANCE REMOVED THE GEAR PIN AND RETURNED THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999042300606 19990423 00606 NM 1999 4 23 VNAA9904004 1 19990407 A 2722 84282 ACTUATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RUDDER FAILED A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 461PS 7058 3075 VIBRATIONS ORIGINATING FROM THE REAR OF THE AIRCRAFT WERE NOTED BY THE CREW AFTER TAKEOFF. THE CREW DECLARED AN EMERGEN CY AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED. MAINTENANCE INSPECTED AND REPLACED THE RUDDER LIMIT ACTUATOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-23-04. OPERATIONAL CHECKS AND A FUNCTIONAL CHECK FLIGHT WERE COMPLETED, A ND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999042300607 19990423 00607 NE 1999 4 23 TC8A99013 2 19990417 A 7320 545790 P & D VALVE DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE FAILED A TC8A D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 GL 23 184SK 45981 669157 NR 1 ENGINE FLAME-OUT AFTER ENGINE START. FUEL FLOW INDICATOR SHOWING FLUCTUATION OF 1,000 +/- 500 PSI. FUEL PRESSURE ENGINE DRIVEN PUMP. NORMAL RANGE - FUEL PRESSURE INDICATION FUEL PUMP TANK PRESSURE/FEED. REMOVED AND REPLACED P & D V ALVE AND FUEL FILTERS, OPS CHECK GOOD ON GROUND RUN AT IDLE AND POWER. LEAK CHECK GOOD IAW DC8 MM 73-00. 2 L 7 4 4F 4 F 4A25 1E8 1999042300608 19990423 00608 NM 1999 4 23 SWAA990688 1 19990412 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 884 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION A CRACK AT FASTENER HOLE , LOWER ROW OF SKIN LAP AT BS 8 84, STRINGER 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999042300609 19990423 00609 NM 1999 4 23 SWAA990689 1 19990412 A 3350 6013211 POWER SUPPLY BOEING 737 7372H4 138448C NM CARGO COMPT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT CONTROL CURCUIT BREAKER POPPED DURING ENGINE RUN. REMOVED AND R EPLACED BATTERY POWER SUPPLY PER MM. 2 L 7 2 4F A16WE 1999042300610 19990423 00610 NM 1999 4 23 SWAA990690 1 19990412 A 5313 6545776 STRINGER BOEING 737 7372H4 138448C NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 26R, BS 1006. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999042300611 19990423 00611 NM 1999 4 23 SWAA990691 1 19990412 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR LOWER HINGE CUT OUT (VERIFIED WITH EDDY CUR RENT INSPECTION). REPAIRED SKIN PER SWA RA NR 1-253-2060. 2 L 7 2 4F A16WE 1999042300612 19990423 00612 NM 1999 4 23 SWAA990692 1 19990412 A 5512 65C27494 SKIN BOEING 737 7373H4 1384600 NM RT HORZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED 1 INCH FWD OF REAR SPAR CENTER LINE AT STA 1 25 (CRACK IS APPROX 1 INCH LONG). REPAIRED SKIN PER ER 99-5225. 2 L 7 2 4F RT A16WE 1999042300613 19990423 00613 NM 1999 4 23 SWAA990693 1 19990412 A 3397 W115055320 WIRE BOEING 737 7373A4 1384585 NM BS 540-700 DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLOOR TRACK ESCAPE LIGHTING BETWEEN BS 540 TO 700 WITH EXPOSED AND CRUSH ED WIRING. REMOVED AND REPLACED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999042300614 19990423 00614 NM 1999 4 23 SWAA990694 1 19990413 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 605SW 27956 EMERGENCY FLOOR TRACK LIGHTING LOOSE AT FWD END. RESECURED TRACK LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999042300615 19990423 00615 NM 1999 4 23 SWAA990695 1 19990413 A 3350 100885 BATTERY PACK BOEING 737 7372H4 138448C NM RT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS (INNER AND OUTER) INOPERATIVE. REMOVED AND REPL ACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999042300616 19990423 00616 NM 1999 4 23 SWAA990696 1 19990413 A 3350 300593 LIGHT BOEING 737 7372H4 138448C NM LT EMER EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, BATTERY PACK, (P/N 61-0478-1) PER MM. 2 L 7 2 4F A16WE 1999042300617 19990423 00617 NM 1999 4 23 SWAA990686 1 19990412 A 3350 BR2013 LIGHT BOEING 737 7372T4 1384492 NM ROW 15 & 17 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 EMERGENCY LIGHTING TRACK CAME LOOSE AT ROW 17 AND INOPERATIVE AT ROW 15. SECURED LIGHT AT ROW 17 AND REPLACED TRACK SEC TION AT ROW 15 PER MM. 2 L 7 2 4F A16WE 1999042300618 19990423 00618 NM 1999 4 23 SWAA990687 1 19990412 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 15-16 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 EMERGENCY TRACK LIGHTS AT ROWS 14 TO 16 INOPERATIVE. DISCOVERED WIRING DISCONNECTED. RECONNECTED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999042300619 19990423 00619 NM 1999 4 23 SWAA990697 1 19990413 A 5314 6545866 KEEL BEAM BOEING 737 7372H4 138448C NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED C4 CHECK, FOUND CORROSION AT KEEL BEAM BS 500B. REPAIRED BEAM PER SWA RA NR 1-253-2062. 2 L 7 2 4F A16WE 1999042300620 19990423 00620 NM 1999 4 23 SWAA990698 1 19990413 A 5752 654645521C TAB BOEING 737 7373H4 1384600 NM LT AILERON DELAMINATION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED BC4 CHECK, FOUND LT AILERON TAB DELAMINATED AT TRAILING EDGE I/B SIDE. REMOVED AND REPLACED TAB PER MM . 2 L 7 2 4F RT A16WE 1999042300621 19990423 00621 NM 1999 4 23 SWAA990699 1 19990412 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA RA NR 1-253-2061. 2 L 7 2 4F A16WE 1999042300622 19990423 00622 NM 1999 4 23 SWAA990700 1 19990412 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM AND SWA RA NR 1-251-0057. 2 L 7 2 4F A16WE 1999042300623 19990423 00623 NM 1999 4 23 SWAA990712 1 19990416 A 5730 65C26714 SKIN BOEING 737 7372H4 138448C NM RT WING LE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND RT WING LEADING EDGE CRACKED AT NR 5 AND NR 6 SLAT I/B TRACK CUTOUTS. REPAIRED PER T I-1-257-008 AND SWA RA NR 1-257-0670. 2 L 7 2 4F A16WE 1999042300624 19990423 00624 NM 1999 4 23 SWAA990713 1 19990416 A 5730 65C26714 SKIN BOEING 737 7372H4 138448C NM RT WING LE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND RT WING LEADING EDGE CRACKED AT NR 4 AND NR 5 SLAT O/B TRACK CUTOUTS. REPAIRED PER T I-1-257-008 AND SWA RA NR 1-257-0670. 2 L 7 2 4F A16WE 1999042300625 19990423 00625 NM 1999 4 23 SWAA990714 1 19990416 A 5312 BAC1490 STRAP BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION 2 CRACKS AT BS 178 STRAP, LBL 6.25. REPAIRED STRAP PER SRM. 2 L 7 2 4F A16WE 1999042300626 19990423 00626 NM 1999 4 23 SWAA990715 1 19990416 A 5312 6552298 WEB BOEING 737 7372H4 138448C NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED STRAP AT LT HORIZONTAL STABILIZER REAR SPAR FWD FACE OF WEB, BL 10.878. REPA IRED PER SWA RA NR 1-255-0291. 2 L 7 2 4F A16WE 1999042300627 19990423 00627 NM 1999 4 23 SWAA990716 1 19990418 A 2560 655463 GIRT BAR BOEING 737 7373H4 1384600 NM PASSENGER DOOR NOT LATCHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE AFT GIRT BAR HOOK NOT LATCHING. REMOVED AND REPLACED L ATCH - HOOK ASSY PER SRM. 2 L 7 2 4F RT A16WE 1999042300628 19990423 00628 NM 1999 4 23 SWAA990717 1 19990418 A 3350 20121 BATTERY CHARGER BOEING 737 7375H4 138449D NM LT EMER EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999042300629 19990423 00629 NM 1999 4 23 SWAA990718 1 19990419 A 7930 1032698 SWITCH BOEING 737 7372H4 138448C NM NR 2 ENGINE MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 103SW 23109 DURING CRUISE, NR 2 ENGINE OIL BYPASS FILTER LIGHT CAME ON. DIVERTED TO LAS WITH THRUST LEVER BACK TO IDLE, LIGHT REMAI NED ON AND WENT OUT DURING DESCENT. INSPECTED NR 2 OIL FILTER AND FOUND NO CONTAMINANTS. DRAINED ALL OIL FROM TANK AND RESERVICED. OIL FILTER BYPASS STILL REMAINED LIT. REMOVED AND REPLACED OIL DIFFERENTIAL SWITCH AND ALL CHECKED GOOD P ER MM. 2 L 7 2 4F A16WE 1999042300630 19990423 00630 NM 1999 4 23 SWAA990719 1 19990419 A 3397 6556633 WIRE BOEING 737 7373H4 1384600 NM LT EMER EXIT BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 365SW 26576 EMERGENCY EXIT LIGHTING WIRES BROKEN AT LT OVERWING EXIT SIGN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 1999042300631 19990423 00631 NM 1999 4 23 SWAA990720 1 19990419 A 5312 6516300 BULKHEAD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C1 CHECK, FOUND BS 178 BULKHEAD CRACKED BELOW RADAR RT MOUNT, BL 0. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999042300632 19990423 00632 NM 1999 4 23 SWAA990710 1 19990417 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 UNABLE TO READ SLIDE PRESSURE GAGE ON THE AFT SERVICE DOOR. REPOSITIONED SLIDE PACK ASSY PER MM. 2 L 7 2 4F A16WE 1999042300633 19990423 00633 NM 1999 4 23 SWAA990711 1 19990419 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 EMERGENCY FLOOR TRACK EGRESS LIGHT COVERS CAME LOOSE AT FWD SECTON. SECURED COVERS PER MM. 2 L 7 2 4F RT A16WE 1999042300634 19990423 00634 NM 1999 4 23 SWAA990721 1 19990419 A 5311 6546570 FRAME BOEING 737 7372T4 1384492 NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 1138, STRINGER 12L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999042300635 19990423 00635 NM 1999 4 23 SWAA990722 1 19990419 A 5752 654645521C TAB BOEING 737 7373Q8 1384670 NM LT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND LEFT AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 1999042300636 19990423 00636 NM 1999 4 23 SWAA990723 1 19990419 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 787, BETWEEN STRINGERS 8R-9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999042300637 19990423 00637 NM 1999 4 23 SWAA990701 1 19990415 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM ROW 4 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 54SW 21535 DURING REPAIR OVERNIGHT CHECK, FOUND FLOOR TRACK EMERGENCY LIGHT INOPERATIVE AT ROW 4. SECURED LOOSE BULB IN SOCKET PER MM. 2 L 7 2 4F A16WE 1999042300638 19990423 00638 NM 1999 4 23 SWAA990702 1 19990414 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND THRU EDDY CURRENT INSPECTION 3 CRACKS AT BS 178 BULKHEAD RBL 10 TO 13. REPAIRED BULK HEAD PER SRM. 2 L 7 2 4F A16WE 1999042300639 19990423 00639 NM 1999 4 23 SWAA990703 1 19990414 A 5320 FRAME BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND 2 CRACKS AT FWD SERVICE DOOR AFT DOOR FRAME, NEXT TO 3RD AND 4TH STOP FITTINGS. REPL ACED DOOR ASSY PER MM. 2 L 7 2 4F A16WE 1999042300640 19990423 00640 NM 1999 4 23 SWAA990704 1 19990415 A 5312 BAC1505 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178 LBL 26, WL 197. REPAIRED CHORD PER SRM. 2 L 7 2 4F A16WE 1999042300641 19990423 00641 NM 1999 4 23 SWAA990705 1 19990414 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM RT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK/C HARGER PER MM. 2 L 7 2 4F A16WE 1999042300642 19990423 00642 NM 1999 4 23 SWAA990706 1 19990415 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 713-720 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED D-CHECK, FOUND CORROSION AT KEEL BEAM RT SIDE BS 713 TO 720. REPAIRED BEAM PER ER N99-5203A. 2 L 7 2 4F RT A16WE 1999042300643 19990423 00643 NM 1999 4 23 SWAA990707 1 19990414 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 23 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374SW 26582 EMERGENCY LIGHT FLOOR TRACK INOPERATIVE AT ROW 23. REMOVED AND REPLACED TRACK SECTION PER MM. 2 L 7 2 4F RT A16WE 1999042300644 19990423 00644 NM 1999 4 23 SWAA990708 1 19990415 A 5330 6545770 SKIN BOEING 737 7372H4 138448C NM BS 579 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED A2 CHECK, FOUND AT BS 579 STRINGER 4L, SKIN LAP CRACKED AT 14 FASTENER HOLES AND STRINGER 4R CRACKED AT 4 FASTENER HOLES. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999042300645 19990423 00645 NM 1999 4 23 SWAA990709 1 19990415 A 5330 6545774 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C4 CHECK, FOUND ONE 2.5 INCH CRACK, ONE 2 INCH CRACK AT FUSELAGE SKIN BS 727B, WL 200. ALSO, FOUND A 4 .5 INCH CRACK AT BS 727A, WL 200. REPAIRED SKIN CRACKS PER SRM. 2 L 7 2 4F A16WE 1999042300646 19990423 00646 NM 1999 4 23 HNAA9900049 1 19990419 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGGAGE COMPT MALFUNCTIONED A HNAA K NONE N FALSE WARNING CR CRUISE 1 EA 07 963HA 337 INTERMITTENT BAGGAGE BAY SMOKE WARNING LIGHT IN FLIGHT (CONFIRMED NO SMOKE). INSPECTED WIRING/CONNECTORS AT BOTH SMOKE DETECTORS. SYSTEM TESTS NORMAL. 2 H 7 2 4T RT A13NM 1999042300647 19990423 00647 WP 1999 4 23 IXXA9900005 1 19990325 A 3310 BA170 BALLAST DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 829BX 45994 EN ROUTE TO DFW, A STRONG ODOR WAS SENSED IN THE COCKPIT WHEN THE GLARESHIELD LIGHT WAS ILLUMINATED. THE LIGHTING SYSTE M WAS TURNED OFF AND THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO DFW. MAINTENANCE INSPECTED AND FOUND THE GLARESHIELD LIGHT BALLAST DEFECTIVE. THE GLARESHIELD LIGHTING WAS PLACED ON DEFERRAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 1999042300648 19990423 00648 WP 1999 4 23 IXXA9900006 1 19990415 A 3397 WIRE DOUG DC8 DC871F 302199D WP COCKPIT BROKEN A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 825BX 78562 1437 45978 EN ROUTE FROM DFW TO TOL, SMOKE EMITTED FROM UNDER THE FIRST OFFICER'S INSTRUMENT PANEL, ACCOMPANIED BY AN ODOR. THE FI RST OFFICER'S INSTRUMENT PANEL FLOOD LIGHTING WAS EXTINGUISHED AND ASSOCIATED CIRCUIT BREAKERS OPENED, SMOKE SUBSIDED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE INSTRUMENT FLOOD LIGHT CIRCUITY WHICH REVEALED A BROKEN WIRE, WHICH WAS REPAIRED IN ACCORDANCE WITH THE MAINTENANCE MANUAL STANDARD PRACTICES. A SUCCESSFUL OPERATIONAL TEST RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 4 4F RT 4A25 1999042300649 19990423 00649 NE 1999 4 23 IXXA9900007 2 19990420 A 7250 TURBINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE LT ENGINE FAILED A IXXA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 23 728PL 50745 2158 45918 671300 EN ROUTE FROM PKWA TO PHIK DURING CLIMB, A LOUD NOISE WAS HEARD FROM THE NUMBER TWO ENGINE, ACCOMPANIED BY INCREASING EN GINE GAS TEMPERATURE AND A DECLINE IN OIL PRESSURE. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND CONTINUED TO PHIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WITH TURBINE BLADE DISCREPANCIES NOTED I N THE EXHAUST AREA. THE ENGINE WILL BE REPLACED PRIOR TO THE AIRCRAFT RETURNING TO SERVICE. 2 L 7 4 4F 4 F 4A25 1E8 1999042300650 19990423 00650 NM 1999 4 23 CALA9900423 1 19990418 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND THE NR 2 ENGINE RT O/B PYLON SKIN CRACKED AT FORWARD UPPER CORNER AND AFT LOWER CORNER AT ACCESS PANEL NR 5824. THE CRACKS WERE .5 AND 2 INCH LONG. REPAIRED IAW ECRA 5430-01204. 2 L 7 2 4F RT A16WE 1999042300651 19990423 00651 NM 1999 4 23 CALA9900424 1 19990419 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 INSPECTION FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 344, BL 0 TO LBL 15. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999042300652 19990423 00652 WP 1999 4 23 CALA9900425 1 19990419 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND THE FORWARD CARGO DOOR JAMB LOWER PAN SECTION CORRODED. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 4 4. 2 L 7 2 4F A6WE 1999042300653 19990423 00653 WP 1999 4 23 CALA9900426 1 19990419 A 5210 BEAM DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A .5 INCH CRACK AT FORWARD AND AFT ENDS OF MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999042300654 19990423 00654 EA 1999 4 23 COMA9960161 1 19990418 A 2150 601R95201 DUCT CNDAIR CL600 CL6002B19 EA FUSELAGE DETACHED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 946CA 7072 DURING TAXI, AFTER NR 1 ENGINE START, COCKPIT FILLED WITH SMOKE. AIR DUCT BETWEEN LEFT HAND ACM AND HEAT EXCHANGER CAME OFF. REINSTALLED DUCT. 2 L 7 2 4F RT A21EA 1999042300655 19990423 00655 EA 1999 4 23 COMA9960162 1 19990418 A 3010 32144424 VALVE CNDAIR CL600 CL6002B19 EA LEFT WING MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 920CA 12299 7022 LEFT WING ANTI-ICE CAUTION. REPLACED THE LEFT HAND 14TH STAGE PRSOV. 2 L 7 2 4F RT A21EA 1999042300656 19990423 00656 EA 1999 4 23 COMA9960163 1 19990417 A 3260 864807 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTION A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 918CA 6012 7018 WHEN LANDING GEAR SELECTED DOWN, THE NLG DID NOT EXTEND. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1999042300657 19990423 00657 EA 1999 4 23 COMA9960164 1 19990417 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA RIGHT COCKPIT CRACKED A COMA K NONE O OTHER LD LANDING 1 SO 01 735CA 7267 COPILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1999042300658 19990423 00658 NM 1999 4 23 UPS99229336 1 19990330 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, SURFACE CORROSION ON NR 5 FLAP TRACK FWD ATTACH LUG. REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (FI LE NR 727-57-2052). 2 L 7 3 4F A3WE 1999042300659 19990423 00659 NM 1999 4 23 UPS99229337 1 19990330 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON NR 8 FLAP TRACK FWD ATTACH LUG I/B SIDE. REPAIR CARRIED OUT IAW SMRO E O 99-08-003 (FILE NR 727-57-2052). 2 L 7 3 4F A3WE 1999042300660 19990423 00660 NM 1999 4 23 UPS99229338 1 19990330 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON NR 7 FLAP TRACK FWD ATTACH LUG I/B AND O/B. REPAIR CARRIED OUT IAW SMR O EO 99-08-003 (FILE NR 727-57-2052). 2 L 7 3 4F A3WE 1999042300661 19990423 00661 NM 1999 4 23 UPS99229339 1 19990330 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON NR 6 FLAP TRACK FWD ATTACH LUG. REPAIR CARRIED OUT IAW SMRO EO 99-08-0 03 (FILE NR 727-57-2052). 2 L 7 3 4F A3WE 1999042300662 19990423 00662 NM 1999 4 23 UPS99229340 1 19990325 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 740-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, ON INSPECTION OF UNDERWING FAIRING NR 3430 HAS SUSPECT CORROSION ON FWD FRAME. FWD FRAME REPAIRED IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1999042300663 19990423 00663 NM 1999 4 23 UPS99229341 1 19990325 A 5350 FAIRING BOEING 727 72731C 1384011 NM WING/FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI ON INSPECTION OF FAIRINGS, NR 3335 UPPER SIDE OF FAIRING EXTRUSION FOUND TO BE CORRODED. INTERCOST AL REPLACED PER SRM 51-10-6 AND 51-30-2. 2 L 7 3 4F A3WE 1999042300664 19990423 00664 NM 1999 4 23 UPS99229342 1 19990325 A 5350 FRAME BOEING 727 72731C 1384011 NM WING/FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI ON INSPECTION OF UNDERWING FAIRINGS, NR 3430 FOUND TO HAVE A NUMBER OF SMALL GOUGES ON MAIN CENTER FRAME AND CORROSION ON FWD FRAME LOWER CHORD I/B. SMALL GOUGES BLENDED OUT AND FOUND WITHIN LIMITS. FWD FRAME LOWER C HORD REPAIRED IAW SRM 51-40-4 FIG 3. 2 L 7 3 4F A3WE 1999042300665 19990423 00665 NM 1999 4 23 UPS99229343 1 19990327 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1323-1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1323 & 1342 S9L. REPAIR CARRIED OUT IAW SMRO EO 99-08-004 (FILE NR 727-53-2117). 2 L 7 3 4F A3WE 1999042300666 19990423 00666 NM 1999 4 23 UPS99229344 1 19990324 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON TOP FLOORBEAM CAP BS 344 LBL 25.75 TO 0. REPAIR CARRIED OUT IAW SRM 53 -10-8 FIG 7. 2 L 7 3 4F A3WE 1999042300667 19990423 00667 NM 1999 4 23 UPS99229345 1 19990322 A 5312 BRACKET BOEING 727 72731C 1384011 NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, BULKHEAD BS 740 TENSION TIE BRACKET FOUND CORRODED. REMOVED BRACKET IAW SRM 51-30-02 IAW SRM, RE- INSTALLED NEW BRACKET IAW SRM 51-30-02, RE-INSTALLED BOLTS IAW MM 20-80-01. 2 L 7 3 4F A3WE 1999042300668 19990423 00668 NM 1999 4 23 UPS99229346 1 19990325 A 5543 SKIN BOEING 727 72731C 1384011 NM RUDDER TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LOWER RUDDER TAB HAS NUMEROUS PREVIOUS REPAIRS WITH DELAMINATION. REPAIRED IAW SRM 51-40-10 FIG 1 . 2 L 7 3 4F A3WE 1999042300669 19990423 00669 NM 1999 4 23 UPS99229347 1 19990404 A 5753 BRACKET BOEING 727 72731C 1384011 NM TE FLAP FAIRING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 3 FLAP TRACK MID FAIRING ANGLE BRACKET CRACKED AT FWD END OF O/B ROLLER TRACK. CRACKED ANGLE B RACKET REPLACED PER SRM 51-10-1 AND SRM 57-20-2 FIG 4. 2 L 7 3 4F A3WE 1999042300670 19990423 00670 NM 1999 4 23 UPS99229348 1 19990405 A 5755 HINGE BOEING 727 72731C 1384011 NM NR 9 SPOILER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 9 SPOILER I/B AND O/B HINGE CASTINGS WORN ON RT WING TRAILING EDGE. WORN CASTINGS REMOVED AND REPLACED WITH NEW CASTINGS IAW SRM 51-30-2 & DRAWING 65-16216. 2 L 7 3 4F A3WE 1999042300671 19990423 00671 NM 1999 4 23 UPS99229349 1 19990329 A 5320 CLEAT BOEING 727 72731C 1384011 NM BS 487.1 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACKED CLEAT DETECTED AT BS 487.1 BELOW MAIN CARGO DOOR SUPPORT FITTING. CLEAT STOP DRILLED PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999042300672 19990423 00672 NM 1999 4 23 UPS99229350 1 19990329 A 5320 CLEAT BOEING 727 72731C 1384011 NM BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACKED CLEAT FOUND AT BS 520 BELOW MAIN CARGO DOOR SUPPORT FITTING. CRACK STOP DRILLED PER SRM 5 1-10-1, REPAIRED ANGLES IAW SRM 51-20-3. 2 L 7 3 4F A3WE 1999042300673 19990423 00673 NM 1999 4 23 UPS99229351 1 19990329 A 5320 CLEAT BOEING 727 72731C 1384011 NM BS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACKED CLEAT DETECTED AT BS 560 BELOW MAIN CARGO DOOR SUPPORT FITTING. REPAIRED ANGLES IAW SRM 5 1-40-3. 2 L 7 3 4F A3WE 1999042300674 19990423 00674 NM 1999 4 23 UPS99229352 1 19990329 A 5347 SEAT TRACK BOEING 727 72731C 1384011 NM BS 910 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, SEAT TRACK AT BS 910 LBL 45.5 BADLY GOUGED. NEW SEAT TRACK SPLICED IN IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1999042300675 19990423 00675 NM 1999 4 23 UPS99229353 1 19990324 A 5751 SKIN BOEING 727 72731C 1384011 NM LEFT AILERON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LT I/B AILERON HAS DAMAGE ON UPPER SKIN AT FWD O/B END. DAMAGED AREA TRIMMED IAW SRM 57-50-5. 2 L 7 3 4F A3WE 1999042300676 19990423 00676 NM 1999 4 23 UPS99229354 1 19990419 A 3350 BATTERY PACK BOEING 727 727180C 138406G NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999042300677 19990423 00677 EU 1999 4 23 UPS99229358 2 19990415 A 7200 ENGINE BOEING 727 72730C 1384009 NM RROYCE TAY TAY65154 EU NR 2 MALFUNCTIONED A IPXA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 01 906UP 19314 INSPECTION TYPE:N/A ON TEST FLIGHT, PERFORMED TEST EVENT SHUT DOWN OF NR 2 ENGINE. ENGINE NR 2 WAS THEN RESTARTED WITH ALL PARAMETERS NORMAL. MINUTES LATER AS NR 2 ENGINE WAS ADVANCED TO CRUISE SETTING, ENGINE WOULD NOT RESPOND TO THROTTL E MOVEMENT. PRECAUTIONARY SHUTDOWN ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E25NE 1999042300678 19990423 00678 NM 1999 4 23 UPS99429355 1 19990401 A 5753 SKIN BOEING 747 747212B 1384886 NM LT TE MIDFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:A/CK, LT MID FLAP CRACKED. 2 L 7 4 4F A20WE 1999042300679 19990423 00679 WP 1999 4 23 UPS99829356 1 19990418 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:A/CK, CRACK AT FLOORBEAM AFT OF SERVICE DOOR. UPON FURTHER INVESTIGATION FOUND CRACK AT CIRCUMFERENTIAL FRAME AT STA 1680 STR 21 NOT AT FLOORBEAM AS FIRST REPORTED. *S/D* REMOVED DAMAGED SECTION OF FRAME, FABED SPLICES AN D INSTALLED REPAIR PER SRM 51-1-20 AND PER DOUGLAS DRAWING PLSRO8530008. 2 L 7 4 4F RT 4A25 1999042300680 19990423 00680 WP 1999 4 23 UPS99829357 1 19990418 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1667 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:A/CK, CORROSION FOUND AT THE FLOORBEAM BY THE LT SERVICE DOOR. UPON FURTHER INVESTIGATION THE LT CIRCUM FERENTIAL FRAME AT STA 1667 FROM STR 21 TO STR 23 TO HAVE EXTENSIVE CORRISION. *S/D* REMOVED LOWER SECTION OF FRAME, F ABED SPLICES AND INSTALLED PARTS PER SRM 53-02-00. 2 L 7 4 4F RT 4A25 1999042300681 19990423 00681 EU 1999 4 23 QXEA9900563 1 19990406 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT TE FLAP SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - SCRATCHES ON UPPER SURFACE OF LEFT-HAND FLAP OUTBOARD AT STATION 5864.2MM TO 5941.0MM AND 431MM TO 482MM FROM TRAI LING EDGE. REPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999042300682 19990423 00682 EU 1999 4 23 QXEA9900564 1 19990406 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT TE FLAP SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - SCRATCHES ON UPPER SURFACE OF LEFT FLAP TO STATION 7693.6MM TO 7769.8MMM AND 254MM TO 381MM FROM TRAILING EDGE. R EPAIRED IAW FOKKER SRM 57-01-01 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4 (B, C). 2 L 7 2 4F RT A20EU 1999042300683 19990423 00683 EU 1999 4 23 QXEA9900565 1 19990412 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - SCRATCHES ON UPPER SURFACE OF RIGHT FLAP TO STATION 2179.3MM TO 2280.9MM AND 533MM TO 635MM FROM TRAILING EDGE. R EPAIRED IAW HORIZON AIR EA 4-57-260. 2 L 7 2 4F RT A20EU 1999042300684 19990423 00684 EU 1999 4 23 QXEA9900566 1 19990406 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - SCRATCHES ON UPPER SURFACE OF RIGHT FLAP TO STATION 7515.8MM TO 7553.9MM AND 279MM TO 342MM FROM TRAILING EDGE. R EPAIRED IAW FOKKER SRM 57-01-01. 2 L 7 2 4F RT A20EU 1999042300685 19990423 00685 EU 1999 4 23 QXEA9900567 1 19990412 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - SCRATCHES ON UPPER SURFACE OF RIGHT FLAP AT STATION 5915.6MM TO 5995.8MM AND 355MM TO 406MM FROM TRAILING EDGE. R EPAIRED IAW HORIZON AIR EA 4-57-3+0. 2 L 7 2 4F RT A20EU 1999042300686 19990423 00686 EU 1999 4 23 QXEA9900568 1 19990406 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT TE FLAP DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT-HAND WING INBOARD FLAP BOTTOM SKIN HAS A AREA OF NUMEROUS DENTS CONCENTRATED IN APPROXIMATELY 49 SQUARE, BEGI NNING 33 FROM INBOARD EDGE AT TRAILING EDGE. REPAIRED IAW HORIZON AIR EA 4-57-257. 2 L 7 2 4F RT A20EU 1999042300687 19990423 00687 EU 1999 4 23 QXEA9900569 1 19990405 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU BS 4790 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - TAILBOX STRUCTURE AT STATION 4790 CRACKED BETWEEN RIVETS ATTACHING SHROUD DOOR BELL CRANK PIVOT BRACKET TO TAILBOX . REPAIRED IAW HORIZON AIR EA 4-57-244. 2 L 7 2 4F RT A20EU 1999042300688 19990423 00688 EU 1999 4 23 QXEA9900570 1 19990326 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 52. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 AND SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999042300689 19990423 00689 EU 1999 4 23 QXEA9900571 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 53. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, AND SR M 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999042300690 19990423 00690 EU 1999 4 23 QXEA9900572 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED PAST STOP DRILL AT STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-1 3 PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999042300691 19990423 00691 EU 1999 4 23 QXEA9900573 1 19990325 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 56. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10- 4, PARAGRAPH 3C AND 4B. 2 L 7 2 4F RT A20EU 1999042300692 19990423 00692 EU 1999 4 23 QXEA9900574 1 19990326 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999042300693 19990423 00693 EU 1999 4 23 QXEA9900575 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999042300694 19990423 00694 EU 1999 4 23 QXEA9900576 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 24. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999042300695 19990423 00695 EU 1999 4 23 QXEA9900577 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17525 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17525 IS CRACKED AT STRINGER 22. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3 AND SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 1999042300696 19990423 00696 EU 1999 4 23 QXEA9900578 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU BS 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 21A. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGUR E 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999042300697 19990423 00697 EU 1999 4 23 QXEA9900579 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 21. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999042300698 19990423 00698 EU 1999 4 23 QXEA9900580 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED PAST STOP DRILL AT STRINGER 15. REPAIRED IAW FOKKER SRM 53-02-1 3, PAGE 5, FIGURE 3 AND SRM 51-31-1. 2 L 7 2 4F RT A20EU 1999042300699 19990423 00699 EU 1999 4 23 QXEA9900581 1 19990326 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AROUND ALL 4 RIVETS BETWEEN STRINGER 9 AND 10. REPAIRED IAW SRM 53-02-13, PAGE 5, FIGURE 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999042300700 19990423 00700 EU 1999 4 23 QXEA9900582 1 19990325 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED AT STRINGER 10. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5, FIGURE 3 AND SRM 53-13-02. 2 L 7 2 4F RT A20EU 1999042300701 19990423 00701 EU 1999 4 23 QXEA9900583 1 19990326 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 174565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 17565 IS CRACKED PAST STOP DRILL TO SECOND RIVET AT STRINGER 8. REPAIRED IAW FOK KER SRM 53-02-13, PAGE 5, FIGURE 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999042300702 19990423 00702 EU 1999 4 23 QXEA9900584 1 19990407 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 18075 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 18075 IS CHAFED IN THREE PLACES BY SPEED BRAKE ACCUMULATOR LINE. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZ ON AIR EA 4-53-766. 2 L 7 2 4F RT A20EU 1999042300703 19990423 00703 EU 1999 4 23 QXEA9900585 1 19990330 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 20075 IS CRACKED AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, 51-31-01 AND 51-30-02. 2 L 7 2 4F RT A20EU 1999042300704 19990423 00704 EU 1999 4 23 QXEA9900586 1 19990328 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 20075 IS CRACKED AT STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGUR E 3. 2 L 7 2 4F RT A20EU 1999042300705 19990423 00705 EU 1999 4 23 QXEA9900587 1 19990328 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE FOR FRAME 20075 IS CRACKED AT STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGUR E 3. 2 L 7 2 4F RT A20EU 1999042300706 19990423 00706 NM 1999 4 23 99UAL900200 1 19990411 A 2121 S210N7014 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 515UA 24840 ELECTRIC SMOKE ODOR DETECTED IN COCKPIT. LATER, EQUIPMENT COOLING OVERHEAT LIGHT CAME ON, AND FWD EQUIPMENT COOLING SUP PLY FAN 1 CB POPPED. SMOKE ODOR DISSIPATED WHEN ALTERNATE FAN WAS SELECTED. *S/D* ELECTRICAL SMOKE ODOR WAS CAUSED BY A FAULTY EQUIPMENT COOLING FAN. THE FAN WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999042300707 19990423 00707 NM 1999 4 23 99UAL900201 1 19990409 A 2450 91252ZC7C4001 RELAY BOEING 2299 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 335UA 2337 24230 LOST ALL INSTRUMENT SYSTEM POWER ON CAPTAIN'S SIDE OF FLIGHT DECK AND THE POWER FOR THE CABIN PRESSURE CONTROLLER. *S/D * MAINTENANCE REPLACED R3 TRANSFER RELAY AND NR 1 TRANSFORMER RECTIFIER, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999042300708 19990423 00708 1999 4 23 99UAL900202 4 19990410 A 2210 COUPLER HONEYWELL 4030952906 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE YAW DAMPER FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 387UA 92083693 24662 UNEXPLAINED YAW FELT BY CREW ON FLIGHT DECK. YAW DAMPER COUPLER BITE TEST WAS PERFORMED BUT NO FAILURES WERE FOUND. RE PLACED THE YAW DAMPER COUPLER PER MM 22-12-31 AS PRECAUTION. A BENCH TEST ON THE REPLACED COUPLER DETERMINED THAT THE T RANSISTOR (Q11) IN THE OUTPUT VOLTAGE CIRCUIT WAS BAD. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999042300709 19990423 00709 NM 1999 4 23 99UAL900203 1 19990410 A 2150 ACM 20405011 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RIGHT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 921UA 21554 21554 815516 25388 AIRCRAFT WOULD NOT PRESSURIZE. FOUND RIGHT PACK AIR CYCLE MACHINE SEIZED. REPLACED RIGHT AIR CYCLE MACHINE. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999042300710 19990423 00710 NM 1999 4 23 99UAL900204 1 19990410 A 2910 UNION BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE B HYD SYST LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 356UA 24362 PARTIAL LOSS OF 'B' SYSTEM HYDRAULIC FLUID. *S/D* FOUND LEAK AT UNION ON MAINTENANCE VALVE IN LEFT SIDE OF TAIL. REPL ACED PACKING, SERVICED B HYDRAULIC SYSTEM. LEAK CHECKED SYSTEM. NO LEAK NOTED, CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999042300711 19990423 00711 NM 1999 4 23 99UAL900205 1 19990411 A 2822 568129115002 BOOST PUMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE LEFT INOPERATIVE A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 793UA 7488 26946 ABOUT 45 MIN AFTER DEPART (ORD-FRA) FLT CREW RECEIVED ADVISORY MSG, FUEL PUMP L FWD INDICATING LEFT FORWARD (BOOST) FUE L PUMP OUTPUT PRESSURE LOW. ETOPS RESTRICTIONS APPLIED PER MEL. *S/D* RELAY (L FWD FUEL BOOST PUMP SWITCH) IN P320 IS NOT IN THE COMMANDED POSITION. TRIED TO RESET BY ACCOMPLISHING FIM 28-22 TASK 826, NO HELP. MSG BECAME NOT ACTIVE BUT PUMP STILL INOPERATIVE. CHECKED PHYSICALLY AND PUMP NOT OPERATING. PERFORMED QUICK CHECK FOR ELECTRICAL POWER AT CONN ECTOR AND FOUND AVAILABLE. REPLACED LEFT FORWARD BOOST PUMP (P/N: 568-1-29115-002) AND PERFORMED OPS CHECKS PER AMM 28- 22-05. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999042300712 19990423 00712 NM 1999 4 23 99UAL900206 1 19990225 A 5320 STIFFENER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BS 246 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 766UA 16010 26917 VERTICAL STIFFENERS AT STA 246 FLOORBEAM BUCKLED AND/OR CRACKED IN BEND RADIUS. LOCATIONS WERE AT RBL 50.0 (P/N 144W851 8-69), RBL 44.95 (P/N 141W8518-69), RBL 38.0 (P/N 141W8518-87), RBL 26.06 (P/N 141W8518-72), RBL 7.88 (P/N 141W8518-73), LBL 7.88 (P/N 141W8518-69), LBL 26.06 (P/N 141W8518-88). *S/D* FABRICATED AND INSTALLED NEW STIFFENERS. NEW STIFFENE RS FABRICATED FROM SAME MATERIAL AS ORIGINAL PART NUMBER, EXCEPT MADE FROM FROM ONE GAGE THICKER SHEET. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999042300713 19990423 00713 NM 1999 4 23 99UAL900207 1 19990314 A 5320 STIFFENER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BS 246 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 767UA 16025 26918 VERTICAL STIFFENERS AT STA 246 FLOORBEAM BUCKLED AND/OR CRACKED IN BEND RADIUS. LOCATIONS WERE AT RBL 50.0 (P/N 144W851 8-69), RBL 44.95 (P/N 141W8518-69), RBL 38.0 (P/N 141W8518-87), RBL 32.0, RBL 26.06 (P/N 141W8518-72), RBL 17.21 (P/N 14 1W8518-73), RBL 7.88 (P/N 141W8518-73) LBL 7.88 (P/N 141W8518-69), LBL 26.06 (P/N 141W8518-88). *S/D* FABRICATED AND I NSTALLED NEW STIFFENERS. NEW STIFFENERS FABRICATED FROM SAME MATERIAL AS ORIGINAL PART NUMBER, EXCEPT MADE FROM FROM ON E GAGE THICKER SHEET. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999042300714 19990423 00714 NM 1999 4 23 99UAL900208 1 19990329 A 5320 STIFFENER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BS 246 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 16051 26919 VERTICAL STIFFENERS AT STA 246 FLOORBEAM BUCKLED AND/OR CRACKED IN BEND RADIUS. LOCATIONS WERE AT RBL 50.0 (P/N 144W851 8-69), RBL 44.95 (P/N 141W8518-69), RBL 38.0 (P/N 141W8518-87), RBL 26.06 (P/N 141W8518-72), RBL 7.88 (P/N 141W8518-73), LBL 7.88 (P/N 141W8518-69), LBL 21.26 (P/N 141W8518-88), LBL 26.06 (P/N 141W8518-88) AND LBL 38.5 (P/N141W8518-64). *S /D* FABRICATED AND INSTALLED NEW STIFFENERS. NEW STIFFENERS FABRICATED FROM SAME MATERIAL AS ORIGINAL PART NUMBER, EXC EPT MADE FROM FROM ONE GAGE THICKER SHEET. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999042300715 19990423 00715 NM 1999 4 23 99UAL900209 1 19990413 A 4940 106170755 EXCITER UNISON MR49410161 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 517UA 92524967 24861 61977 RETURNED TO THE FIELD AT SFO DUE TO THE LOSS OF THE NR 1 IDG AND THE INABILITY TO START THE APU. *S/D* APU EXCITER WAS REPLACED. FLIGHT CREW SUCCESSFULLY OPERATED APU AT FL 370. SHOP TESTED EXCITER AND NO DISCREPANCIES WERE FOUND. THER E IS THE POSSIBILITY OF MOISTURE ACCUMULATION AROUND THE IGNITION PLUG OR LEAD. UNITED IS IMPLEMENTING THREE UNISON SER VICE BULLETINS TO IMPROVE START RELIABILITY, AND DECREASE THE MOISTURE ACCUMULATION THAT CAN CAUSE A NO FLAME CONDITION. 2 L 7 2 4F 4 F RT A2NM E17NE 1999042300716 19990423 00716 NM 1999 4 23 99UAL900210 1 19990413 A 2421 IDG SUNDSTRAND 729825G BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 FAILED A UALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 517UA C1112 24861 RETURNED TO THE FIELD AT SFO DUE TO THE LOSS OF THE NR 1 IDG AND THE INABILITY TO START THE APU. *S/D* REPLACED LEFT ( NR 1) INTEGRATED DRIVE GENERATOR (IDG). THE IDG HAD INTERNAL PISTON FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999042300717 19990423 00717 NM 1999 4 23 99UAL900211 1 19990414 A 3070 304311026182 HEAT TAPE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 618UA 21878 FLIGHT ATTENDANT REPORTED SMOKE IN CABIN/COCKPIT AREA, NOTIFIED MAINTENANCE. *S/D* HEATER TAPE B109 FAILED CAUSING INS ULATION ON FORWARD GALLEY CHILLER DUCT TO IGNITE. 767 ENGINEERING ISSUED CALLOUT TO INSPECT 767 AIRCRAFT WITH THIS HEATE R TAPE CONFIGURATION FOR EVIDENCE OF CHAFING AND/OR HEAT DISCOLORATION AND TO CORRECT DESCREPANCIES. THE INSULATION MATE RIAL ON THE CHILLER DUCT IS BEING EVALUATED BY 767 ENGINEERING TO DETERMINE IF IT SHOULD BE A MORE FIRE RESISTANT MATERI AL, OR BE WRAPPED WITH A FIRE RESISTANT TAPE. THE 767 MAINTENANCE PROGRAM WILL BE CHANGED TO REPLACE ALL HEATER TAPES O N A 4C INTERVAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1999042300718 19990423 00718 WP 1999 4 23 ABXA9900292 1 19990218 A 5320 47516252 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND FITTING CRACKED AT LONGERON 11 LEFT, STATION 680. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0 . 2 L 7 4 4F 4A25 1999042300719 19990423 00719 WP 1999 4 23 ABXA9900293 1 19990218 A 5320 47516252 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 682 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND FUSELAGE FRAME FITTING CRACKED AFT SIDE AT BOTTOM OF LONGERON 11 RIGHT, STATION 682. REPLACED FR AME FITTING IAW DC8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F 4A25 1999042300720 19990423 00720 WP 1999 4 23 ABXA9900294 1 19990218 A 5320 46401621N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1180 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON FITING AT 1180, RIGHT SIDE OF CUSP. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F 4A25 1999042300721 19990423 00721 WP 1999 4 23 ABXA9900295 1 19990218 A 5311 5640123NC FRAME DOUG DOUG DC8 DC862 3021970 WP BS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND FRAME CRACKED AT STATION 1180 RIGHT, AT FLOOR LEVEL. REPAIRED FRAME IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999042300722 19990423 00722 WP 1999 4 23 ABXA9900296 1 19990218 A 5320 47731511 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1458 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON FRAME TO CUSP ATTACH FITTING AT STATION 1458 RIGHT. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F 4A25 1999042300723 19990423 00723 WP 1999 4 23 ABXA9900297 1 19990330 A 5311 99582387 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 FRAME AT STATION 980 CRACKED AT LONGERON 16 LEFT. REPAIRED FRAME IAW DC9 SRM 53-03 AND DACO DWG 9958238. 2 L 7 2 4F A6WE 1999042300724 19990423 00724 WP 1999 4 23 ABXA9900298 1 19990330 A 5313 991075527 LONGERON DOUG DOUG DC9 DC931 3022065 WP FRAME 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 18R CRACKED AT FRAME STATION 996. REPLACED ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999042300725 19990423 00725 WP 1999 4 23 ABXA9900299 1 19990330 A 5320 995823869 SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 SHEAR TIE FORMER CRACKED AT STATION 980 BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE IAW DC9 SRM 53-30-02. 2 L 7 2 4F A6WE 1999042300726 19990423 00726 WP 1999 4 23 ABXA9900300 1 19990330 A 5313 59114269 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 12 RIGHT CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999042300727 19990423 00727 WP 1999 4 23 ABXA9900301 1 19990330 A 5315 99115451 FLOORBEAM DOUG DOUG DC9 DC931 3022065 WP BS 351 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 FLOORBEAM CRACKED AT STATION 351 BL 0 TO LBL 5. REPAIRED FLOORBEAM IAW ABX REA D953-27445MR. 2 L 7 2 4F A6WE 1999042300728 19990423 00728 WP 1999 4 23 ABXA9900302 1 19990330 A 5313 5914258501 LONGERON DOUG DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 20 LEFT CRACKED AT AFT END OF TRAPEZOIDAL PANEL. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999042300729 19990423 00729 WP 1999 4 23 MWEA99158 1 19990417 A 2560 11331DG SLIDE DOUG DC9 DC915 3022036 WP GALLEY DOORWAY LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 900ME 45841 THE GALLEY SLIDE WAS FOUND LOOSE. MTC REINSTALLED GALLEY SLIDE. 2 L 7 2 4F A6WE 1999042300730 19990423 00730 WP 1999 4 23 MWEA99159 1 19990419 A 5330 5911412513 SKIN DOUG DC9 DC932 3022066 WP BS 313 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 206ME 47791 FOUND MISDRILLED HOLE AT FS 313 BETWEEN LONGERON 28 AND 29R ON FUSELAGE SKIN. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999042300731 19990423 00731 WP 1999 4 23 MWEA99160 1 19990419 A 5330 991152612 SKIN DOUG DC9 DC932 3022066 WP BS 313 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 206ME 47791 THE SHEAR TIE AT FS 313 BETWEEN LONGERON 28 AND 29R IS MISDRILLED THROUGH SKIN. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999042300732 19990423 00732 WP 1999 4 23 MWEA99161 1 19990419 A 5520 5918045502 TIP DOUG DC9 DC932 3022066 WP RT ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE RIGHT ELEVATOR TIP HAD TEMPORARY DOUBLER INSTALLED. MTC REMOVED TEMPORARY DOUBLER AND INSTALLED PERMANENT. 2 L 7 2 4F A6WE 1999042300733 19990423 00733 NM 1999 4 23 MWEA99162 1 19990419 A 3350 60030400 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 701ME 49760 THE LEFT AND RIGHT FORWARD EMERGENCY EXIT LIGHTED SIGNS ARE INOPERATIVE. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 1999042300734 19990423 00734 NM 1999 4 23 MWEA99163 1 19990419 A 2560 11320 GIRT BAR DOUG MD88 MD88 3023688 NM PASSENGER DOOR LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE GIRT BAR AT FORWARD ENTRANCE DOOR IS VERY HARD TO ARM/DISARM. MTC LUBRICATED GIRT BAR ATTACH FITTINGS. 2 L 7 2 4F RT A6WE 1999042300735 19990423 00735 WP 1999 4 23 DHL99807002 1 19990418 A 3110 PANEL DOUG DC8 DC873F 302199F WP COCKPIT FIRE A DHLA H F DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. A FLAME/FIRE AP APPROACH 1 SO 01 807DH 45990 ON FINAL APPROACH TO MIA , HEARD LOUD POPPING NOISE BEHIND S/O PANEL, F/O REPORTED SMOKE AND S/O SAW FLAMES BEHIND PANE L. USED HALON EXTINGUISHER TO PUT OUT FIRE. ACCOMPLISHED EMERGENCY LANDING. 2 L 7 4 4F RT 4A25 1999042300738 19990423 00738 SO 1999 4 23 99ZZZX1595 1 19990329 A 2750 1763400 TORQUE TUBE 1643300 PIPER PA23 PA23250 7102308 SO TE FLAP CRACKED A P BQTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 NE 05 62BA 11000 274859 DURING A PART 91 TRAINING FLIGHT, IT WAS NOTED THAT THERE WAS AN ASYMMETRICAL FLAP CONDITION (SLIGHT). CREW RETURNED TO BASE AND MAINTENANCE FOUND FLAP TORQUE TUBE 80 PERCENT CRACKED THROUGH AT LEFT BELLCRANK AREA. 1 L 7 2 3O 1A10 1999042300758 19990423 00758 CE 1999 4 23 99ZZZX1615 1 19990322 A 3230 HMX5FG ROD END BEECH 58 58 1152740 CE NLG FAILED A PA9A O OTHER O OTHER NR NOT REPORTED 1 SO 03 46US TH294 NOSE GEAR ROD END FAILED UPON LANDING GEAR EXTENSION. NOSE GEAR CLEARED THE GEAR WELL, BUT FAILED TO DOWN AND LOCK. RO D END BROKE AND CAME FREE OF NOSE GEAR STRUT. ENSURE ALL PAINT HAS BEEN REMOVED FROM GEAR LINKAGE AND INSPECTION A REGU LAR BASIS. 1 L 7 2 3O 3A16 1999042300778 19990423 00778 SO 1999 4 23 99ZZZX1635 1 19990406 A 7120 3711200 MOUNT PIPER PA34 PA34200T 7103406 SO RT ENGINE BROKEN A P OVOA K NONE O OTHER IN INSP/MAINT 1 CE 05 36107 3795 347870294 THIS AIRCRAFT WAS IN THE SHOP FOR A DUAL ENGINE CHANGE. WHEN THE RIGHT ENGINE WAS REMOVED AND ENGINE MOUNT INSPECTED, I T WAS FOUND TO BE BROKEN. 1 L 7 2 3O A7SO 1999042300787 19990423 00787 1999 4 23 WVBA005/99 4 19990403 A 2210 KA132MOD2 SWITCH KING PIPER PA31 PA31350 7103110 SO AFCS FAILED A WVBA K NONE L NO TEST IN INSP/MAINT 1 AL 01 4082T 181 3511 318152089 AUTOPILOT: UNIT FAILED TEST FUNCTION IN THE UP POSITION. UNIT IS NEWER, MOD SEEMS TO FAIL WITHIN SAME TIME FRAME AS PR EVIOUS MODEL. RECOMMEND ELIMINATING THIS SWITCH FROM SYSTEM AS PILOT CAN OVERRIDE AN EXTREME PITCH UP OR DOWN MANUALLY. (X) 1 L 7 2 3O A20SO 1999042300788 19990423 00788 SO 1999 4 23 WVBA004/99 1 19990402 A 2140 A23D0475 FUEL REGULATOR PIPER PA31 PA31350 7103110 SO HEATER LEAKING A WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 35270 547 317952141 PART LEAKING FUEL AT PARTING SEAMS. ALL SCREWS WERE FOUND LOOSE. PROBLEM DISCOVERED AT INSPECTION. FUEL STAINS OBSERV ED COMING OUT OF DRAIN. THIS IS THE THIRD ONE DISCOVERED IN THE PAST SIX INSPECTIONS. (X) 1 L 7 2 3O A20SO 1999042300799 19990423 00799 EU 1999 4 23 C2XA99IA175 1 19990228 A 3350 OL3112 BULB AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT WHEN THE EMERGENCY EXIT LIGHT SWITCH WAS MOVED TO THE DISARM POSITION, THE 'DISARM' ANNUNCIATOR WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS IN THE ANNUNCIAT OR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300800 19990423 00800 EU 1999 4 23 C2XA99IA174 1 19990227 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93840 271 EFD - DURING MAINTENANCE INSPECTION, THE AFT SECTION AISLE PATH EMERGENCY EXIT LIGHTS WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR 42-320 MM 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300801 19990423 00801 SO 1999 4 23 C2XA99IA173 1 19990225 A 5312 12033696003 BULKHEAD EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND APU BULKHEAD CRACKED AT FIRE BOTTLE DISCHARGED TUBE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMBRAER DOCUMENT NR SST-0360/99. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300802 19990423 00802 SO 1999 4 23 C2XA99IA172 1 19990225 A 5320 12036805001 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND SUPPORT BRACKET CRACKED UNDER CARGO FLOOR FORWARD ROLLER GUIDE. RE PLACED BRACKET IAW SRM 51-40-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300803 19990423 00803 SO 1999 4 23 C2XA99IA171 1 19990225 A 5753 12022766001 STIFFENER EMB 120 EMB120RT SO LT TE FLAP CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP WELL LOWER HAT SECTION CHAFED. REPLACED HAT SECT ION IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300804 19990423 00804 SO 1999 4 23 C2XA99IA170 1 19990225 A 5753 SKIN EMB 120 EMB120RT SO LT TE FLAP CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP LOWER FORWARD SKIN CHAFED. INSTALLED DOUBLER REP AIR IAW SRM 54-20-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300805 19990423 00805 SO 1999 4 23 C2XA99IA169 1 19990225 A 5414 SKIN EMB 120 EMB120RT SO LT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE INBOARD SIDE DENTED AT FRAME 2. INSTALLED DOUBLER REP AIR IAW SRM 51-70-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300806 19990423 00806 SO 1999 4 23 C2XA99IA168 1 19990225 A 5753 12040327003 SKIN EMB 120 EMB120RT SO RT TE FLAP CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP, TOP SKIN CHAFED. INSTALLED DOUBLER REPAIR IAW SRM 54-20-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300807 19990423 00807 SO 1999 4 23 C2XA99IA167 1 19990225 A 5330 12026335005 SKIN EMB 120 EMB120RT SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT FUSELAGE DENTED BELOW GPU PLUG DOOR. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300808 19990423 00808 NM 1999 4 23 GAIA9930 1 19990302 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING C-CHECK, FOUND FLOORBEAM LOWER CAP CORRODED OUT OF SRM LIMTIS AT STATION 1130, BL 0 TO LBL 24. REMOVED DAMAGED L OWER CHORD, FABRICATED REPAIR PARTS, AND INSTALLED IAW AIA EDR B2-06264, REV 'A'. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999042300809 19990423 00809 NM 1999 4 23 GAIA9935 1 19990304 A 7920 FITTING BOEING 727 727251 138408H NM NR 1 ENGINE LEAKING A GAIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 278US 21157 EN ROUTE TO TOL, DURING CRUISE, THE NR 1 ENGINE LOST OIL AND QTY WENT TO ZERO. SHUT DOWN ENGINE AND DECLARED AN EMERGEN CY. THE AIRCRAFT LANDED AT TOL WITHOUT FURTHER DIFFICULTY. FOUND A BAD HELI-COIL FOR A GEARBOX FITTING. INSTALLED NEW HELI-COIL AND CHECKED ENGINE OIL FILTER. FILTER FOUND TO BE CLEAN. RAN ENGINE AND NO LEAKS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999042300810 19990423 00810 WP 1999 4 23 GAIA9936 1 19990308 A 7603 700470SHT9 ROD CVAC 240 600240D 2422660 WP NR 2 ENGINE DISCONNECTED A GAIA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 07 94246 102 FLT 485 - AFTER DEPARTURE FROM CVG, RIGHT ENGINE TEMP STARTED TO RISE AFTER CLIMB POWER WAS SET, TRIMMER MOTOR HAD NO EF FECT ON TEMP, POWER WAS REDUCED TO KEEP TEMPS IN LIMITS. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO CVG AND MADE AN UNEVENTFUL LANDING. FOUND NR 2 ENGINE TRIMMER CONTROL PICKUP ROD DISCONNECTED. INSTALLED TRIMMER PICK UP ROD BOLT, WASHER, NUT TORQUED AND SAFTIED WITH STEEL COTTER KEY. ENGINE OPERATIONAL CHECKED NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE (M) 1 L 7 2 4T RT 2L72 1999042300811 19990423 00811 NM 1999 4 23 GAIA9934 1 19990215 A 3350 1000677 LIGHT BOEING 727 7272J0 138407E NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 281KH 21105 ON POSTFLIGHT, FOUND THE FORWARD COCKPIT EMEGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE FORWARD COCKPIT EMER GENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 1999042300812 19990423 00812 NM 1999 4 23 GAIA9933 1 19990209 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 255US 19974 FOUND DURING POSTFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT IN COCKPIT DIM AND INTERMITTENT. REMOVED AND REPLACED EMER GENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 1999042300813 19990423 00813 NM 1999 4 23 GAIA9932 1 19990205 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 252US 19971 COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE DURING POSTFLIGHT INSPECTION. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGH T. OPERATIONALLY CHECKS GOOD. RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 1999042300814 19990423 00814 NM 1999 4 23 GAIA9931 1 19990303 A 2611 GE186A BULB PYROTECTOR 302842 BOEING 727 727223 1384074 NM CARGO SMOKE DET FAILED A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 6827 20180 EN ROUTE FROM YIP TO HUF, THE CARGO SMOKE LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES. T HERE WAS NO SMOKE OR SMELL INTHE COCKPIT OR THE CARGO COMPARTMENT. LIGHT EXTINGUISHED 15 MINUTES LATER. ALL TEST WERE GOOD. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND BURNED OUT SMOKE DETECTOR BEACON LIGHT BULB. REPLACE D BULB AND OPS CHECKED GOOD IAW KITTY HAWK CARGO CONVERSION MAINTENANCE MANUAL. THE AIRCRAFT WAS THEN RETURNED BACK TO SERVICE. (M) 2 L 7 3 4F A3WE 1999042300815 19990423 00815 WP 1999 4 23 ASAA9980063 1 19990312 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 962AS 53076 SEA - PRIOR TO DEPARTURE OF FLIGHT 326, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 3 WAS OUT OF TRACK. R EPAIRED WIRE IN FLOOR TRACK AND REPLACED COVER AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300816 19990423 00816 WP 1999 4 23 ASAA9980062 1 19990310 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 2457 53453 OAK - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300817 19990423 00817 WP 1999 4 23 ASAA9980061 1 19990310 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING MAINTENANCE CHECK, THE FORWARD RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AT ROW 1 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300818 19990423 00818 WP 1999 4 23 ASAA9980059 1 19990308 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 PDX - DURING MAINTENANCE CHECK, THE FORWARD 3 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING I N FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300819 19990423 00819 WP 1999 4 23 ASAA9980058 1 19990306 A 3350 014597001 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 13 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300820 19990423 00820 WP 1999 4 23 ASAA9980057 1 19990304 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 2869 53471 OAK - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LGIHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300821 19990423 00821 WP 1999 4 23 ASAA9980056 1 19990303 A 3350 0105610001 MODULE GULTON DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PDX - DURING MAINTENANCE CHECK, THE FORWARD 3 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED DEFECTIVE L AMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300822 19990423 00822 WP 1999 4 23 ASAA9980049 1 19990223 A 3350 6011779 POWER SUPPLY MIDLANDROSS DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 964AS 22617 2252 53078 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300823 19990423 00823 WP 1999 4 23 ASAA9980048 1 19990222 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999042300825 19990423 00825 NM 1999 4 23 ASAA9940063 1 19990303 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 PDX - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BROKEN LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999042300826 19990423 00826 NM 1999 4 23 ASAA9940060 1 19990302 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 14 FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT TRACK LIGHTS INOPERATIVE AT ROW 14. REPAIRED WIRING AND RELAMPED S EVERAL RECEPTICLE, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999042300827 19990423 00827 NM 1999 4 23 ASAA9940058 1 19990301 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 6 FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 760AS 25098 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT ROWS 6-9. REPLACED WIR ING HARNESS AT ROW 6, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999042300828 19990423 00828 NM 1999 4 23 ASAA9910020 1 19990310 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - AFTER RECON, THE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED COLD SOAKED BATTERY P ACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999042300829 19990423 00829 NM 1999 4 23 ASAA9910019 1 19990304 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM ROWS 15/18 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 743AS 21821 BRW - FLT 146 - CREW REPORTED TWO EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15 AND 18 WERE FOUND INOPERATIVE DURING TEST . RELEASED PER MEL 33-19. SUBSEQUENTLY REPLACED BATTERY PACKS IN ANC AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999042300830 19990423 00830 CE 1999 4 23 99ZZZM245 1 19990124 A 2810 FUEL SYSTEM BEECH 200 B200 1152922 CE LEFT/RIGHT CONTAMINATED A FFSA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 01 4277C BB1309 RIGHT ENGINE SURGED WITH LARGE FUEL FLOW FLUCTUATIONS, AND WAS SHUT DOWN AFTER TRYING STANDBY FUEL PUMPS, OAT -47 DEGREE S CELSIUS. DRAINED FUEL SUMPS. CLEANED FUEL BOWLS. INSPECTED TANKS FOR CONTAMINATION, ETC. OPERATIONAL CHECK AFTERWA RDS WAS AIRWORTHY. (M) 1 L 7 2 4T A24CE 1999042300831 19990423 00831 SO 1999 4 23 99ZZZM246 1 19990312 A 2731 HL67367 TRIM WHEEL GULSTM G1159 G1159 3953505 SO COCKPIT WORN A COZA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 WP 27 102CX 102 PITCH TRIM KICKED OFF JUST PRIOR TO DESCENT AND TRIM WAS FROZEN T 1 DEGREE NOSE UP. CREW COULD NOT MOVE THE TRIM WHEEL ELECTRICALLY OR MANUALLY. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED REVEALED THAT THE ROLL PIN HOLES ATTACHING THE T RIM WHEEL TO THE CROSSOVER TORQUE TUBE ASSEMBLY HAD WORN ON THE PILOTS TRIM WHEEL, ALLOWING THE INDICATOR INNER DRIVER T O RUB AGAINST THE BRONZE INNER BUSHING AND WELDING THE ASSEMBLY TOGETHER, NOT ALLOWING THE TRIM WHEEL TO MOVE. THIS ARE A IS NOT COVERED BY THE INSPECTION PROGRAM. TRIM WHEEL IS NOT OPENED FOR INSPECTION. (M) 2 L 7 2 4F RT A12EA 1999042300832 19990423 00832 NM 1999 4 23 F3LA99026 1 19990313 A 2612 6937307112 FIRE MODULE BOEING 737 7372L9 1384497 NM NR 2 ENGINE MALFUNCTIONED A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 270FL 22733 UPON TAKEOFF, FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY DURING CLIMB-OUT. AIR CRAFT RETURNED TO LAS VEGAS WITHOUT INCIDENT. MAINTENANCE REPLACED FIRE CONTROL MODULE AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999042300833 19990423 00833 NM 1999 4 23 F3LA99027 1 19990313 A 3610 655812310 DUCT BOEING 737 7372L9 1384497 NM NR 2 ENGINE FAILED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 270FL 22733 LAS - UPON TAKEOFF, FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY AFTER TAKEOFF. A IRCRAFT RETURNED TO LAS VEGAS WITHOUT INCIDENT. MAINTENANCE REPLACED 13TH STAGE DUCT AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999042300834 19990423 00834 NM 1999 4 23 USAA990180 1 19990305 A 5320 654581951 WEB BOEING 737 7373B7 1384580 NM BS 233 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 373US 40856 22952 CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 233, BL 0, WL 192.5 WEB. INSTALLED DOUBLER PER BOEIN G SRM 51-70-13. (M) 2 L 7 2 4F RT A16WE 1999042300835 19990423 00835 WP 1999 4 23 USAA990151 1 19990225 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 130 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND 1.5 INCH CRACK IN FLOORBEAM ATTACH ANGLE AND SUBFLOOR CRACKED AT STATION 130 OUTBOARD OF L EFT SEAT TRACK. INSTALLED FLOORBEAM REPAIR PER SRM 53-05 FIG 25. (M) 2 L 7 2 4F A6WE 1999042300836 19990423 00836 NM 1999 4 23 USAA039901 1 19990303 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 17 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924TS 22863 21041 FLT 6160 - LGA-BOS - OVERHEAD AISLE EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 17. REPLACED BATTERY PACK, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999042300837 19990423 00837 NM 1999 4 23 USAA039911 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 385 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE STATION 385, DENT AND GOUGE FOUND ABOVE STRINGER 1R. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 1999042300838 19990423 00838 NM 1999 4 23 USAA039910 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE LAP SEAM 4R, STATION 720 THROUGH 720A HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M) 2 L 7 3 4F A3WE 1999042300839 19990423 00839 NM 1999 4 23 USAA039909 1 19990315 A 5330 SKIN BOEING 727 727227 1384078 NM BS 500-555 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FUSELAGE LAP SEAM 4R, STATION 500 THROUGH 555 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M) 2 L 7 3 4F A3WE 1999042300840 19990423 00840 NM 1999 4 23 MZZA99059 1 19990315 A 5313 STRINGER BOEING 727 727264 138408M NM BS 318 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON FUSELAGE STRINGER S-20R AT BS 318. THE CORRODED STRINGER 2 INCH LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 1999042300841 19990423 00841 NM 1999 4 23 TSAA9933172 1 19990328 A 5511 6573782 SPAR BOEING 737 737230 NM HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 LEFT HORIZONTAL STABILIZER UPPER SURFACE. TRAILING EDGE AROUND NR 4 AND NR 5 HINGE. METAL SURFACE LIFTING UP. REPAIRE D IAW ECO1889R4. (M) 2 L 7 2 4F RT A16WE 1999042300842 19990423 00842 NM 1999 4 23 TSAA9933171 1 19990328 A 5711 6573720 SPAR CAP BOEING 737 737230 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 RIGHT WING FORWARD UPPER SPAR CAP FROM WBL 198.6 TO WING TIP CORRODED. REPAIRED IAW ECO 2959. (M) 2 L 7 2 4F RT A16WE 1999042300843 19990423 00843 NM 1999 4 23 TSAA9933167 1 19990327 A 3350 900835A BATTERY BOEING 737 737282 13844AT NM EMERG EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY CARTRIDGE FOR OVERWING EMERGENCY EXIT LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 1999042300844 19990423 00844 NM 1999 4 23 TSAA9933168 1 19990327 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM PAX DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300845 19990423 00845 NM 1999 4 23 TSAA9933202 1 19990406 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED AFT EMERGENCY LIGHT TRANSMITTER BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300846 19990423 00846 NM 1999 4 23 TSAA9933203 1 19990406 A 3350 9221009 BATTERY PACK BOEING 737 7372S5C 1384499 NM LT EMER EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED LEFT OVERWING EXIT IDENTIFIER BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300847 19990423 00847 NM 1999 4 23 TSAA9933189 1 19990405 A 3350 963100211 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY DUE TO LED'S NOT OPERATING. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1999042300848 19990423 00848 NM 1999 4 23 TSAA9933185 1 19990404 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED ROW 17 FLOOR LIGHT EMERGENCY BATTERY PACK DUE TO WEAK. OPS CHECK OK. AIRCRAFT RETURNED TO SERICE. (M) 2 L 7 2 4F RT A16WE 1999042300849 19990423 00849 NM 1999 4 23 TSAA9933188 1 19990405 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 5 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300850 19990423 00850 NM 1999 4 23 TSAA9933199 1 19990405 A 3350 6012311 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED LEFT OVERWING EMERGENCY SLIDE LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1999042300851 19990423 00851 NM 1999 4 23 TSAA9933181 1 19990403 A 3350 9221009 BATTERY PACK BOEING 737 7372T4 1384492 NM SERVICE DOORWAY INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED AFT SERVICE DOOR EXIT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999042300852 19990423 00852 NM 1999 4 23 TSAA9933184 1 19990404 A 3350 86210066 BATTERY PACKS BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 4, 5, 6 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 1999042300853 19990423 00853 NM 1999 4 23 TSAA9933180 1 19990403 A 3350 6012311 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED AFT EMERGENCY SLIDE LIGHT BATTERY PACK DUE TO WEAK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999042300854 19990423 00854 NM 1999 4 23 TSAA9933183 1 19990403 A 3350 8731002511 LIGHT BOEING 737 737282C 13844AU NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED FORWARD ENTRY EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300855 19990423 00855 NM 1999 4 23 TSAA9933182 1 19990403 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300856 19990423 00856 NM 1999 4 23 TSAA9933170 1 19990401 A 3350 963100211 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 5 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300857 19990423 00857 NM 1999 4 23 TSAA9933173 1 19990330 A 3350 1000679 LIGHT BOEING 737 737230 NM PAX DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300858 19990423 00858 NE 1999 4 23 99ZZZM247 2 19990316 A 7250 TURBINE BOEING 727 72751C 1384015 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE DAMAGE A RYNA O OTHER E VIBRATION/BUFFET CR CRUISE 1 CE 07 436EX 19289 653575 FLT 611 - IND-EWR - NR 1 ENGINE VIBRATES BETWEEN 45 PERCENT AND 68 PERCENT N1. INSPECTED ENGINE, FOUND TURBINE DAMAGE. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999042300859 19990423 00859 NM 1999 4 23 99ZZZM248 1 19990329 A 5347 BAC15201430 SEAT TRACK BOEING 727 72722C 138400F NM CABIN BROKEN A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 428EX 19097 PALLET POSITION NR 2 AFT, NR 1 SEAT TRACK BROKEN. REMOVED AND REPLACED BROKEN SEAT TRACK POSITION NR 2 AFT, NR 1 TRACK. WORK ACCOMPLISHED PER 727 SHEETMETAL REPAIR MANUAL CHAPTER 53-10-5. (M) 2 L 7 3 4F A3WE 1999042300860 19990423 00860 NM 1999 4 23 MZZA99061 1 19990403 A 3230 A42006028305 SOLENOID BOEING 727 727264 138408M NM LANDING GEAR INOPERATIVE A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING POST MAINTENANCE CHECK FLIGHT ON AIRCRAFT AT AIR ASIA, LANDING GEAR WAS FOUND NOT RETRACTED. THE LANDING G EAR LEVER LATCH SOLENOID, P/N A420-060283-05 WAS REMOVED AND REPLACED PER B727 MM 32-31-0 AND OPERATIONAL CHECK FOUND SA TISFACTORY. (M) 2 L 7 3 4F A3WE 1999042300861 19990423 00861 EU 1999 4 23 SIMA990872 1 19990328 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 253AE 340B253 SBA - FLT 3208 - SEAT 9A EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT BU LB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999042300862 19990423 00862 EU 1999 4 23 SIMA990911 1 19990401 A 3320 6500110 LIGHT SAAB SF340 340B 7860101 EU LAVATORY FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 375AE 340B375 TYR - FLT 5372 - LAVATORY SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. SMOKE WAS PRESENT IN LAVATORY. DIVERTED TO TYR. M AINTENANCE INSPECTED AND FOUND A LAMP HOLDER ASSEMBLY BURNED. DEACTIVATED LAVATORY LIGHTING SYSTEM AND OPENED MEL AGAIN ST LAVATORY LIGHTING AND LAVATORY. ON 4-2-99, THE LAMP HOLDER WAS REPLACED AND OPERATIONAL CHECKED IAW AMM 32-21-20 AND WORK CARD NR 2252. THE MEL ITEMS WERE RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999042300863 19990423 00863 EU 1999 4 23 SIMA990783 1 19990319 A 5330 S5367140002205 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 SAW - DURING CPCP-4 INSPECTION, FOUND SKIN DENTED ON THE RIGHT SIDE OF THE FUSELAGE THREE INCHES FORWARD OF FRAME 38 BET WEEN STRINGER 19 AND 20, MEASURING 30 MM BY 50 MM BY 2 MM DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300864 19990423 00864 EU 1999 4 23 SIMA990843 1 19990325 A 5313 S5307021020800 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 SAW - DURING CPCP-4 INSPECTION, FOUND STRINGER 15 RIGHT CORRODED BETWEEN FRAME 39 AND 40. REPAIRED STRINGER 15 IAW SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300865 19990423 00865 EU 1999 4 23 SIMA990842 1 19990325 A 5313 S5307021020801 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 SAW - DURING CPCP-4 INSPECTION, FOUND STRINGER 17 RIGHT CORRODED BETWEEN FRAME 29 AND 30. REPAIRED STRINGER 17 IAW SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300866 19990423 00866 EU 1999 4 23 SIMA990781 1 19990319 A 5230 FRAME AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE FORWARD CARGO DOOR DOOR HAD FRAMES 2, 3, 4, 5, 7 AND 8 FROM FORWARD TO AFT CRA CKED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR IAW JIC 523100-RAI-10000-003. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300867 19990423 00867 EU 1999 4 23 SIMA990841 1 19990325 A 5315 SS5367240720202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAM 38 AND 39 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS IAW SRM 51-25- 02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300868 19990423 00868 EU 1999 4 23 99ZZZM249 1 19990325 A 5315 S5367240820202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAM 38 AND 39 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS IAW SRM 51-25- 02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300869 19990423 00869 EU 1999 4 23 SIMA9900881 1 19990329 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, RIGHT AFT INBOARD AND OUTBOARD, RIGHT FORWARD OUTBOAR D, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300870 19990423 00870 EU 1999 4 23 99ZZZM250 1 19990329 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, RIGHT AFT INBOARD AND OUTBOARD, RIGHT FORWARD OUTBOAR D, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300871 19990423 00871 EU 1999 4 23 99ZZZM251 1 19990329 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, RIGHT AFT INBOARD AND OUTBOARD, RIGHT FORWARD OUTBOAR D, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300872 19990423 00872 EU 1999 4 23 99ZZZM252 1 19990329 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, RIGHT AFT INBOARD AND OUTBOARD, RIGHT FORWARD OUTBOAR D, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300873 19990423 00873 EU 1999 4 23 99ZZZM253 1 19990329 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AT 327 DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, RIGHT AFT INBOARD AND OUTBOARD, RIGHT FORWARD OUTBOAR D, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999042300874 19990423 00874 EU 1999 4 23 SIMA990782 1 19990319 A 5347 S53375001204 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE RIGH T AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO-E9-5300-013R2. AIRCRAFT RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 1999042300875 19990423 00875 EU 1999 4 23 99ZZZM254 1 19990319 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE RIGH T AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO-E9-5300-013R2. AIRCRAFT RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 1999042300876 19990423 00876 EU 1999 4 23 99ZZZM255 1 19990319 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE RIGH T AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO-E9-5300-013R2. AIRCRAFT RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 1999042300877 19990423 00877 EU 1999 4 23 99ZZZM256 1 19990319 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE RIGH T AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO-E9-5300-013R2. AIRCRAFT RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 1999042300878 19990423 00878 EU 1999 4 23 99ZZZM257 1 19990319 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AT 325 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FORWARD OUTBOARD, THE LEFT AND RIGHT AFT OUTBOARD, AND THE RIGH T AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO-E9-5300-013R2. AIRCRAFT RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 1999042300879 19990423 00879 NM 1999 4 23 USAASB99085 1 19990401 A 3350 323975 SPLICE BOEING 737 737301 1384611 NM ROW 16 DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 354US 23557 ROC - WHOLE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT ON SEAT ROW 16 END BAY INOPER ATIVE. MAINTENANCE REPLACED DEFECTIVE WIRE SPLICES AND SECURED WIRING BENEATH SEAT ADJACENT TO END BAY. OPERATIONAL CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999042300880 19990423 00880 NM 1999 4 23 USAA039920 1 19990327 A 3350 90052 LIGHT BOEING 727 727227 1384078 NM RT EMER EXIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927TS VA8991 20837 FLT 6471 - LGA-DCA - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT BASE AND BATTERY. (M) 2 L 7 3 4F A3WE 1999042300881 19990423 00881 NM 1999 4 23 USAA039919 1 19990327 A 3350 90052 LIGHT BOEING 727 727227 1384078 NM RT EMER EXIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927TS WA6848 20837 FLT 6471 - LGA-DCA - RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT OVERWING EMERGENCY EXIT LI GHT BASE AND BATTERY. (M) 2 L 7 3 4F A3WE 1999042300882 19990423 00882 NM 1999 4 23 USAASB99083 1 19990328 A 3350 CONNECTOR BOEING 737 737201 1384454 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 263AU 22869 ATL - PILOT REPORTED THA THE FLOOR LEVEL EMERGENCY LIGHTING ILLUMINATED SEVERAL TIMES DURING FLIGHT. MAINTENANCE FOUND A LOOSE CONNECTION AT THE MAIN HARNESS POWER SENSE WIRE. REPLACED CONNECTOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999042300883 19990423 00883 NM 1999 4 23 USAASB99082 1 19990328 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 592US 23937 ALB - MAINTENANCE FOUND THE LOWER SIDEWALL EMERGENCY EXIT SIGNS FOR THE FORWARD ENTRY DOOR AND SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999042300884 19990423 00884 NM 1999 4 23 USAASB99080 1 19990325 A 3350 101EN1522 SWITCH BOEING 737 737201 1384454 NM LT EMER EXIT OUT OF ADJUST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 263AU 22869 PHL - FLT 2241 - EMERGENCY EXIT LIGHTS (SEAT LIGHTS ONLY) ILLUMINATED IN FLIGHT. MAINTENANCE IN PHL CHECKED OUT THE SYS TEM AND FOUND NOTHING WRONG. THE PROBLEM RETURNED, AND MAINTENANCE IN PVD ADJUSTED THE LEFT SIDE EMERGENCY EXIT OPERATE D EMERGENCY LIGHT SWITCH. (M) 2 L 7 2 4F A16WE 1999042300885 19990423 00885 EA 1999 4 23 MASA99056 1 19990406 A 3350 OL3071 BULB BRUCE BR9279232 CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5781 - CRW-PHL - CREW DISCOVERED ON POST FLIGHT THE EMERGENCY FLOOR LIGHT AT THE PASSENGER DOOR INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE BULB, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999042300886 19990423 00886 NM 1999 4 23 MASA99043 1 19990314 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING ROUTINE MAINTENANCE, FOUND FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH BACKLIGHTING WOULD NOT ILLUMINATED. REMOVED AND REPLACED BULB. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1999042300887 19990423 00887 NM 1999 4 23 MASA99050 1 19990325 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN CHAFED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 6362 - PHX-TEX - DURING PREFLIGHT WALK AROUND, THE CREW REPORTED THAT THE FORWARD RED FLOOR PATH LIGHTING LIGHTS WOU LD NOT ILLUMINATE. THE AIRCRAFT WAS FERRIED TO GJT WHERE MAINTENANCE REPAIRED A CHAFED WIR AT PS2, OPS CHECKED GOOD. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999042300888 19990423 00888 NM 1999 4 23 MASA99045 1 19990318 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 FLT 6280 - PHX-ASE - CRWE REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTE RY PACKS, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999042300889 19990423 00889 EA 1999 4 23 MASA99047 1 19990320 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5389 - BNA-DCA - CREW REPORTED THE FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE ACTION WAS DEFERRED PER MEL 31-51-1. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1999042300890 19990423 00890 1999 4 23 MASA99048 4 19990324 A 3442 6222501001 ANTENNA BEECH 1900 1900D 1154162 CE RADAR SYSTEM NOISY A MASA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 105YV UE105 FLT 444 - ABQ-ROW - THE CREW HEARD A NOISE LIKE PELLETS HITTING THE AIRCRAFT COMING FROM NEAR THE NOSE GEAR AREA. AN EM ERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NOISE TO BE CO MING FROM THE WEATHER RADAR ANTENNA. THERE WERE NO DEFECTS FOUND IN THE WEATHER RADAR SYSTEM. AS THE SYSTEM WAS FULLY OPERATIONAL. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE RADAR ANTENNA WAS REPLACED AS A PREC AUTIONARY MEASURE. (M) 2 L 7 2 4T RT A24CE 1999042300891 19990423 00891 EA 1999 4 23 MASA99051 1 19990326 A 3350 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5774 - TYS-CLT - DURING PREFLIGHT WALK AROUND, CREW NOTICED THE FORWARD CEILING EMERGENCY LIGHT WAS NOT ILLUMINATING . MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, T HE BULB WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1999042300892 19990423 00892 EA 1999 4 23 MASA99054 1 19990331 A 3350 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA LT EMER EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37178 7178 FLT 5122 - CMH-MDW - ON PREFLIGHT, CREW REPORTED THE LEFT WING FORWARD EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANC E ACTION WAS DEFERRED PER MEL 33-51-2 AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1999042300893 19990423 00893 WP 1999 4 23 ORJA99127 1 19990303 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC987 3022087 WP ROW 19-26 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAX, EMERGENCY LIGHTS AT ROWS 19-26 OUT. REMOVED AND REPLACED 3 BATTERY CHARGERS AT 21A, 20A AND 21F. SYSTEM OPS CH ECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999042300894 19990423 00894 WP 1999 4 23 ORJA99126 1 19990327 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 30 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - EMERGENCY LIGHTS BETWEEN ROWS 29-32 ILLUMINATED DURING DESCENT, WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK AT AFT LEFT LAVATORY. REPAIRED BROKEN WIRE AT ROW 30 REF 33-50-00. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999042300895 19990423 00895 WP 1999 4 23 ORJA99125 1 19990326 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 12-15 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO - EMERGENCY LIGHTS ROW 12-15 RIGHT SIDE ILLUMINATED. REMOVED AND REPLACED LIGHT BATTERY PACK AT LEFT FORWARD ESC APE HATCH IAW MM 33-00-00. ALL EMERGENCY LIGHTS OPS CHECK NORMAL WITH NO DISCREPANCIES NOTED. (M) 2 L 7 2 4F RT A6WE 1999042300896 19990423 00896 WP 1999 4 23 ORJA99129 1 19990331 A 3350 EM1267 BATTERY DOUG DC9 DC982 3022082 WP BS 206 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 821RA 49931 RNO - ROW 6 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AT BS 206, OPS CHECK GOOD IAW 33-51-00. (M) 2 L 7 2 4F A6WE 1999042300897 19990423 00897 WP 1999 4 23 ORJA99128 1 19990331 A 3350 60034051 BATTERY PACK DOUG DC9 DC983 3022083 WP LT EMER EXIT DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 RNO - LEFT LOWER FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT LOWER FORWARD OVERWING BA TTERY PACK IAW MM 33-53-00, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999042300898 19990423 00898 WP 1999 4 23 ORJA99124 1 19990326 A 3260 TARGET DOUG DC9 DC982 3022082 WP LT MLG OUT OF ADJUST A ORJA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 11 823RA 49889 IN RNO - STALL INDICATION FAILURE CAME ON SHORTLY AFTER TAKEOFF WHEN SLATS EXTENDED IN FLIGHT SYSTEM PERFORMED TEST AS T HOUGH ON THE GROUND AND WENT TO FULL SLATS THEN BACK TO TAKEOFF. A/C RETURNED TO RNO, A STALL FAILURE LIGHT WENT OUT AT GROUND SHIFT ON LANDING AUTO SLAT FAIL ILLUMINATED WHEN FLAPS RETRACTED 15 DEGREES ON GROUND. FOUND LEFT MAIN WOW PROX TARGET OUT OF ADJUST INDICATING FAR WHEN SHOULD BE CLOSE ADJUSTMENT PER MM SPEC PREFORMED. OPS CHECK OF S1F 4 TIMES, A LL INDICATIONS NORMAL PER MM 34-19-00 REQUIRES FCF. (M) 2 L 7 2 4F A6WE 1999042300899 19990423 00899 EU 1999 4 23 REXA99007 1 19990318 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A REXA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 25 109PX 340A021 RIGHT ENGINE FIRE LIGHT CAME ON SHORT FINAL. REMOVED AND REPLACED RIGHT ENGINE NACELLE FIRE LOOP. (M) 2 L 7 2 4T RT A52EU 1999042300900 19990423 00900 EU 1999 4 23 REXA99006 1 19990316 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG INOPERATIVE A REXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 406BH 340A074 AIRCRAFT LOST ALL HYDRAULIC FLUID. FLUID CAME FROM HYDRAULIC SWIVEL ON RIGHT GEAR. REMOVED AND REPLACED HYDRAULIC SWIV EL ON RIGHT MAIN GEAR. REMOVED AND REPLACED EXPLOSION BOLTS. (M) 2 L 7 2 4T RT A52EU 1999042300901 19990423 00901 EA 1999 4 23 MASA99026 1 19990215 A 3244 TIRE CNDAIR CL600 CL6002B19 EA NR 1/2 MLG FAILED A MASA O OTHER O OTHER TO TAKEOFF 1 SW 07 27185 7185 FLT 6132 - DSM-PHX - UPON TAKEOFF ROLL, THE NR 1 AND NR 2 MLG TIRES BLEW OUT. THE CREW ABORTED TAKEOFF AND PARKED ON TH E TAXI WAY. THE CAUSE OF THE TIRES BLOWING OUT IS CURRENTLY UNDER INVESTIGATION. (M) 2 L 7 2 4F RT A21EA 1999042300902 19990423 00902 EA 1999 4 23 MASA99044 1 19990314 A 7830 22850741102 STRIKER PLATE CNDAIR CL600 CL6002B19 EA LT ENGINE DISCONNECTED A MASA O OTHER N FALSE WARNING LD LANDING 1 SW 07 77286 7286 FLT 5128 - LGA-CMH - CREW REPORTED A LEFT THRUST REVERSER UNLOCKED MESSAGE ON EICAS. MAINTENANCE FOUND THE STRIKER PLAT E FOR THE MICROSWITCH BROKEN OFF AND IN THE NACELLE. MAINTENANCE RESECURED THE STRIKER PLATE. OPS CHECK GOOD. THE AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999042300907 19990423 00907 SO 1999 4 23 ASOA99032 1 19990319 A 5210 12047825001 DOOR SEAL EMB 120 EMB120RT SO AIR STAIR DOOR DEFECTIVE A ASOA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 284AS 120249 FLT 4971 - EN ROUTE ATL-LEX AT 25,000 FEET, LOST PRESSURIZATION. CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. O XYGEN MASKS WERE NOT DEPLOYED. FLIGHT CONTINUED TO LEX AND LANDING WAS MADE WITHOUT FURTHER INCIDENT. ATL MAINTENANCE REMOVED AND REPLACED THE AIRSTAIR DOOR SEAL. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FU RTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999042300908 19990423 00908 NM 1999 4 23 TSAA9933176 1 19990401 A 3350 6013211 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED FORWARD AND SERVICE DOOR SLIDE LIGHTS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999042300909 19990423 00909 NM 1999 4 23 TSAA9933177 1 19990401 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1999042300910 19990423 00910 EU 1999 4 23 RAIA990406 1 19990408 A 7922 L85039 VERNITHERM BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 341TE 950 FLT 7098 - STL - RIGHT OIL TEMP WENT TO 145 DEGREES. MAINTENANCE C/W PROCEDURES IN GARRETT MM FOR GOING ABOVE RED LINE BY PERFORMING SOAP SAMPLE, THEN THEY REPLACED OIL VERNITHERM. (M) 2 L 7 2 4T RT A56EU 1999042300911 19990423 00911 WP 1999 4 23 RAIA990403 2 19990402 A 7314 8974007 FUEL PUMP BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 337TE 929 66146 FLT 7478 - STL - LEFT ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE FUEL PUMP. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999042300912 19990423 00912 WP 1999 4 23 RAIA990404 2 19990403 A 7210 310703611 TORQUE RING BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CE 03 431AM 881 66157 FLT 7099 - SPI - LEFT ENGINE TORQUE WENT OT 120 PERCENT, ENGINE WAS SHUTDOWN. MAINTENANCE REPLACED TORQUE RING IN LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999042300913 19990423 00913 WP 1999 4 23 GTIA9900044 1 19990326 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 DTW - AFT HALF OF EMERGENCY FLOOR TRACK LIGHTS ARE INOPERATIVE. RESECURED PLUG AND SOLDERED BROKEN LIGHTS. OPERATION C HECKS GOOD. (M) 2 L 7 2 4F A6WE 1999042300914 19990423 00914 WP 1999 4 23 GTIA9900043 1 19990326 A 3397 WIRE DOUG DC9 DC932 3022066 WP RT EMER EXIT BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 DTW - AFT LEFT AND AFT RIGHT OVERWING EXIT DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. SOLDERED BROKEN WIRE. OPERATIONAL C HECKS GOOD. (M) 2 L 7 2 4F A6WE 1999042300915 19990423 00915 NM 1999 4 23 GAIA9947 1 19990408 A 3350 BATTERY BOEING 727 727224 1384076 NM LT EMER EXIT DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 69740 20668 DURING P/S CHECK, FOUND L-1 EMERGENCY EXIT LIGHT BATTERY DEAD. CHARGED BATTERIES FOR EMERGENCY LIGHTS. OPERATIONAL CHE CK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999042300916 19990423 00916 SO 1999 4 23 99ZZZM258 1 19990312 A 2730 HL67367 TRIM WHEEL GULSTM G1159 G1159 3953505 SO ELEVATOR WORN A COZA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 WP 27 102CX 12029 102 PITCH TRIM KICKED OFF JUST PRIOR TO DESCENT AND TRIM WAS FROZEN AT 1 DEGREE NOSE UP. CREW COULD NOT MOVE THE TRIM WHEEL ELECTRICALLY OR MANUALLY. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION REVEALED THAT THE ROLL PIN HOLES ATTACHING THE TRIM WHEEL TO THE CROSSOVER TORQUE TUBE ASSEMBLY HAD WORN ON THE PILOT'S TRIM WHEEL, ALLOWING THE INDICATOR INNER DRIVE R TO RUB AGAINST THE BRONZE INNER BUSHING AND WELDING THE ASSEMBLY TOGETHER, NO ALLOWING THE TRIM WHEEL TO MOVE. (M) 2 L 7 2 4F RT A12EA 1999042300917 19990423 00917 NM 1999 4 23 ASAA9940070 1 19990328 A 3350 S283T0143 BATTERY PACKS BOEING 737 737490 1384715 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 792AS 28887 PDX - DURING MAINTENANCE CHECK, FOUND THAT THE EMERGENCY EXIT LIGHT SWITCH HAD BEEN LEFT ON AND SEVERAL EMERGENCY EXIT F LOOR TRACK LIGHTS INOPERATIVE. REPLACED ALL BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999042300918 19990423 00918 NM 1999 4 23 ASAA9940069 1 19990327 A 3397 WIRE BOEING 737 7374Q8 NM ROW 16/17 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14 THROUGH 17 . RECONNECTED WIRING AND LIGHTS AT ROWS 16 AND 17, AND RELAMPED. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999042300919 19990423 00919 NM 1999 4 23 ASAA9910027 1 19990327 A 3397 WIRE BOEING 737 737210C 1384459 NM ROW 5 FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING RECON, FOUND EMERGENCY EXIT TRACK LIGHTS INOPERATIVE AT ROW 5 (2 WHITE). MAINTENANCE RELEASED PER MEL 33-1 9A. SEAT PALLET 3-9 WS SUBSEQUENTLY REMOVED FROM THE AIRCRAFT AND ROUTED TO THE SHOP WHERE LIGHTS/WIRING WERE REPAIRED. (M) 2 L 7 2 4F A16WE 1999042300920 19990423 00920 NM 1999 4 23 ASAA9910026 1 19990326 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM ROW 12 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 745AS 20794 SEA - FLT 65 - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 12. REPLACED BATTERY P ACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999042300921 19990423 00921 NM 1999 4 23 ASAA9940079 1 19990401 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 PDX - DURING MAINTENANCE CHECK, THREE EMERGENCY EXIT FLOOR TRACK LIGHTS AT THE AFT OVERWING EXIT WERE FOUND TO BE INOPER ATIVE. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999042300922 19990423 00922 WP 1999 4 23 ASAA9980071 1 19990329 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 4 BROKEN A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 934AS 49235 SEA - PRIOR TO DEPARTURE OF FLIGHT 624, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 4 WAS OUT OF TRACK. R EPAIRED WIRE IN FLOOR TRACK AND REPLACED COVER AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999042300923 19990423 00923 WP 1999 4 23 ASAA9980070 1 19990327 A 3350 0105610001 LAMP DOUG DC9 DC983 3022083 WP ROW 28 DEFECTIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 972AS 53448 SEA - AFTER ARRIVAL OF FLIGHT 251, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS ILLUMINATE BRIEFLY WHEN THE AUXILIARY HYDRAULIC PUMP IS TURNED ON. REPLACED DEFECTIVE LAMP MODULE AT ROW 28 AND SECURED LOOSE CONNECTIONS IN FLOOR TRACK FROM ROWS 24 AND 28 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300924 19990423 00924 WP 1999 4 23 ASAA9980069 1 19990325 A 3350 CONNECTORS DOUG DC9 DC983 3022083 WP ROW 20 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING MAINTENANCE CHECK, TWO RED EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 WERE FOUND INOPERATIVE. RECONNECTED CONN ECTORS AND SECURED FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999042300925 19990423 00925 NM 1999 4 23 ASAA9910025 1 19990325 A 3350 8731002142 LIGHT BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIG HT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999042300926 19990423 00926 NM 1999 4 23 ASAA9940067 1 19990324 A 5210 SNAP-RING BOEING 737 737490 1384715 NM L1 DOOR DETACHED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 799AS 29270 JNU - UPON ARRIVAL OF FLIGHT 62, THE L1 DOOR WOULD NOT OPEN. INSPECTED DOOR AND FOUND THE SNAP-RING DETACHED ON THE UPP ER HINGE DOOR RELEASE MECHANISM. REINSTALLED SNAP-RING AND DOOR OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 1999042300927 19990423 00927 EU 1999 4 23 RAIA990342 1 19990326 A 7714 31036061 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 428AM 877 FLT 7332 - STL - LEFT ENGINE RPM FELL TO 35 PERCENT. MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR INSERT. (M) 2 L 7 2 4T RT A56EU 1999042300928 19990423 00928 EU 1999 4 23 RAIA990339 1 19990325 A 3340 4553 BULB BAG JETSTM JETSTM3201 1500217 EU LT LANDING LIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 423AM 858 FLT 7437 - CMI - TAXI AND BOTH LANDING INOPERATIVE. MAINTENANCE REPLACED LEFT LANDING LIGHT. (M) 2 L 7 2 4T RT A56EU 1999042300929 19990423 00929 EU 1999 4 23 RAIA990338 1 19990325 A 3340 4553 BULB BAG JETSTM JETSTM3201 1500217 EU RT LANDING LIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 423AM 858 FLT 7437 - CMI - TAXI LIGHT AND BOTH LANDING LIGHTS INOPERATIVE. MAINTENANCE REPLACED RIGHT LANDING LIGHT BULB. (M) 2 L 7 2 4T RT A56EU 1999042300930 19990423 00930 EU 1999 4 23 RAIA990340 1 19990325 A 3340 4551 BULB BAG JETSTM JETSTM3201 1500217 EU TAXI LIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 423AM 858 FLT 7437 - CMI - TAXI AND BOTH LANDING LIGHTS INOPERATIVE. MAINTENANCE REPLACED TAXI LIGHT. (M) 2 L 7 2 4T RT A56EU 1999042300931 19990423 00931 GL 1999 4 23 RAIA990402 2 19990402 A 7200 23060570 SEAL EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 804HK 145082 310140 FLT 6845 - JFK - SMOKE SMELL IN COCKPIT AND CABIN. MAINTENANCE REPLACED ZERO CARBON SEAL IN NR 1 ENGINE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999042300932 19990423 00932 1999 4 23 RAIA990401 4 19990401 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 563HK 7635 41079 FLT 7140 - STL - NR 2 AIR DATA COMPUTER INOPERATIVE. MAINTENANCE REPLACED NR 2 AIR DATA COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999042300933 19990423 00933 EU 1999 4 23 RAIA990344 1 19990329 A 2120 S2L226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 554HK 41067 FLT - 7663 - JFK - LEFT DUCT FAIL LIGHT ILLUMINATED. MAINTENANCE REPLACED DUCT SEAL IN LEFT ECS DUCT. (M) 2 L 7 2 4T RT A41NM 1999042300934 19990423 00934 1999 4 23 RAIA990343 4 19990326 A 3425 2578719343 GYRO BAG JETSTM JETSTM3201 1500217 EU NR 1 LOOSE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424AM 865 FLT 7096 - STL - NR 1 COMPASS IS 30 DEGREE OFF. MAINTENANCE REPLACED MOUNTING SCREWS FOR DIRECTIONAL GYRO. (M) 2 L 7 2 4T RT A56EU 1999042300935 19990423 00935 1999 4 23 RAIA990337 3 19990325 A 6140 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 428AM 11446 877 FLT 7448 - STL - RIGHT RPM INDICATION FLUCTUATING. MAINTENANCE REPLACED RIGHT TACH GENERATOR. (M) 2 L 7 2 4T RT A56EU 1999042300936 19990423 00936 EU 1999 4 23 PLGA990225 1 19990225 A 3010 FD238162 VALVE SAAB SF340 340B 7860101 EU EMPENNAGE STUCK A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 364BE N486 340B294 BOS - FLT 6313 - ON FLIGHT BOS-PHL, THE STABILIZER DE-ICE BOOT INFLATION LIGHT BECAME INOPERATIVE. DUE TO WEATHER AND I CING THE CREW RETURNED TO BOS AND LANDED WITHOUT INCIDENT. BOS MAINTENANCE REPLACED THE STABILIZER DISTRIBUTION VALVE A ND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999042300937 19990423 00937 EU 1999 4 23 PLGA990226A 1 19990226 A 6120 8524M2 COMPUTER SAAB SF340 340B 7860101 EU AUTOCOARSEN UNIT INOPERATIVE A PLGA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 05 361BE 190 340B290 SYR - FLT 6272 - DURING TAKEOFF ROLL FOR FLIGHT 6272, THE AUTOCOARSEN HIGH LIGHT DID NOT COME ON AND THE TAKEOFF WAS ABO RTED. MAINTENANCE REPLACED THE AUTOCOARSEN COMPUTER, PERFORMED REQUIRED OPERATIONAL CHECKS, AND RETURNED THE AIRCRAFT T O SERVICE. (M) 2 L 7 2 4T RT A52EU 1999042300938 19990423 00938 1999 4 23 PLGA990226B 4 19990226 A 3140 6229849012 MFDU SAAB SF340 340B 7860101 EU COCKPIT SMOKING A PLGA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 05 348BE 148 340B190 LGA - FLT 6525 - DURNG TAXI OUT, THE CREW NOTICED SMOKE IN THE COCKPIT AND EVACUATED THE AIRCRAFT ON THE TAXIWAY. MAINT ENANCE PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE MULTI-FUNCTION DISPLAY UNIT TO BE AT FAULT. THE SYSTEM HAD PREVIO USLY BEEN MEL'D. MAINTENANCE REPLACED THE MULTI-FUNCTION DISPLAY UNIT, PERFORMED REQUIRED OPERATIONAL CHECKS, AND RETUR NED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999042300939 19990423 00939 EU 1999 4 23 PLGA990301B 1 19990301 A 2421 31342001 GENERATOR SAAB SF340 SF340A 7850100 EU RIGHT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 342BE 1663 199 340A096 BOS-HPN - FLT 6269 - AFTER DEPARTURE OUT OF BOS, THE RIGHT A/C GENERATOR LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO BOS AN D LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE A/C GENERATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999042300940 19990423 00940 WP 1999 4 23 USAAD99042 1 19990309 A 3350 8732030153 MODULE DOUG DC9 DC982 3022082 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 818US 48098 PIT - THE PASSENGER CABIN LOW LEVEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE PASSENGER CABIN LOW LEVE L EMERGENCY LIGHT BATTERIES AND AFT CONTROL MODULE. (M) 2 L 7 2 4F A6WE 1999042300941 19990423 00941 WP 1999 4 23 USAAD99045 1 19990311 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 LGA - THE LOW LEVEL EMERGENCY LIGHTS WERE FLICKERING DURING AIRCRAFT ELECTRICAL POWER SHUTDOWN. MAINTENANCE REPLACED TH REE OF THE LOW LEVEL EMERGENCY LIGHTS BATTERIES. (M) 2 L 7 2 4F A6WE 1999042300942 19990423 00942 NM 1999 4 23 USAA039917 1 19990325 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 25381 21244 FLT 6791 - BOS-LGA - FORWARD OVERHEAD EMERGENCY EXIT LIGHT WON'T TEST. REPLACED BATTERY. (M) 2 L 7 3 4F A3WE 1999042300943 19990423 00943 NM 1999 4 23 USAA039918 1 19990325 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 13384 21244 FLT 6791 - BOS-LGA - FOUND ON L/S, OVERHEAD EMERGENCY LIGHT AT ROW 18 WON'T TEST. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999042300944 19990423 00944 WP 1999 4 23 USAAD99048 1 19990326 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG DOOR MALFUNCTIONED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 982VJ 48158 DAY-PHL - FLT 648 - AFTER TAKEOFF AND UPON RETRACTING, THE LANDING GEAR THERE WAS A VIBRATION COMING FROM THE NOSE GEAR AREA. THE CAPTAIN DECIDED TO RETURN TO THE FIELD. THE VIBRATION CONTINUED UNTIL THE NOSE GEAR WAS EXTENDED AT ABOUT 18 0 KTS WHEN THE VIBRATION SUDDENLY STOPPED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE GEA R DOOR AND WHEELS. ALL DOORS, LINKAGES, AND HINGES WERE NORMAL. IT IS SUSPECTED A NOSE GEAR DOOR WAS NOT LATCHED UP UN TIL THE LANDING WAS LOWERED FOR LANDING AND THE NOSE GEAR DOOR MECHANISM WAS CYCLED. (M) 2 L 7 2 4F A6WE 1999042300945 19990423 00945 WP 1999 4 23 HALA9900086 1 19990302 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1821 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 TUL - DURING C-1 CHECK, FOUND CORROSION ON STRINGER NEAR FORWARD FITTINGS. INSTALLED REPAIR DOUBLER PER 53-40-00 FIGURE 20 AND ESC 7349, DATED 3/17/99. (M) 2 L 7 3 4F A22WE 1999042300946 19990423 00946 WP 1999 4 23 HALA9900083 1 19990302 A 5720 SPLICE DOUG DC10 DC1010 3022110 WP WS 372 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 TUL - FOUND LEFT LONGERON 16 TO 22 SPLICE CRACKED INSIDE NR 1 FUEL TANK WING STATION XORS 372. INSTALLED AND SECURED SE RVICEABLE LONG 16 TO 22 IAW AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1999042300947 19990423 00947 WP 1999 4 23 HALA9900084 1 19990302 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 2007 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 TUL - FOUND CORROSION AT LAV SUPPORT TO BULKHEAD TEE AFT OF SEAT TRACK NR 1. REPLACED LAV SUPPORT PER AARD 51-10-00-10. (M) 2 L 7 3 4F A22WE 1999042300948 19990423 00948 WP 1999 4 23 HALA9900085 1 19990302 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1124 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 TUL - FOUND CORROSION ON STRINGER 48 LEFT. REPLACED STRINGER SECTION FROM STATION 1099 TO 1139 PER 51-01-00-05 CARD. ( M) 2 L 7 3 4F A22WE 1999042300949 19990423 00949 NM 1999 4 23 AALA990348 1 19990225 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1030-1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STRINGER 28R HAS CORROSION ON BOTTOM SURFACE AT FS 1040 TO 1070. REPAIRED STRINGER ACCORDING TO SRM 53-10-3 . (M) 2 L 7 3 4F A3WE 1999042300950 19990423 00950 NM 1999 4 23 AALA990349 1 19990225 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1040-1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STRINGER 28R HAS CORROSION ON BOTTOM SURFACE AT FS 1040 TO 1070. REPAIRED STRINGER ACCORDING TO SRM 53-10-3 . (M) 2 L 7 3 4F A3WE 1999042300951 19990423 00951 NM 1999 4 23 AALA990350 1 19990301 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STRINGER 15R CRACKED AT END OF STRINGER FORWARD OF ICE LIGHT. HFEC TO CONFIRM CRACK, REMOVED CRACKED SECTIO N OF STRINGER 1.25 INCH. HFEC TO CONFIRM CRACK REMOVAL AND INSTALLED REPAIR, FILLER AND CHANNEL PER 53-10-3 PAGE 12-17. (M) 2 L 7 3 4F A3WE 1999042300952 19990423 00952 NM 1999 4 23 AALA990351 1 19990219 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 660 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STRINGER CRACKED AT PREVIOUS RADIUS AREA, FS 660 STRINGER 15R. STOP DRILLED CRACK, HFEC. INSTALLED STRINGE R REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999042300953 19990423 00953 NM 1999 4 23 AALA990352 1 19990225 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 708 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND HEAVY CORROSION ON STRINGER 28L, STATION 708. REPAIRED FUSELAGE STRINGER PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999042300954 19990423 00954 NM 1999 4 23 AALA990353 1 19990225 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 702 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION DOWN INSIDE STRINGER 27L AROUND DOME NUT, NUT PLATE STATION 702. REPAIRED FUSELAGE STRINGER PER S RM 53-10-3. (M) 2 L 7 3 4F A3WE 1999042300955 19990423 00955 NM 1999 4 23 AALA990354 1 19990216 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION AFT END STRINGER 27R, STATION 740. PERFORMED STRINGER SPLICE REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999042300956 19990423 00956 NM 1999 4 23 AALA990355 1 19990225 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1050-1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STRINGER 28L CORRODED FROM STATIN 1050 TO 1070. CUT OUT DAMAGED STRINGER SECTION, AND INSTALLED STRINGER S PLICE PER SRM 53-10-3, FIGURE 1. (M) 2 L 7 3 4F A3WE 1999042300957 19990423 00957 NM 1999 4 23 AALA990356 1 19990225 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1055-1095 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND SKIN CORRODED ON EXTERIOR OF AIRCRAFT. REPAIRED CORRODED THROUGH PORTION OF SKIN PER SRM 53-30-3. ALODINED AND PRIMED SKIN, PATCH AND SURFACE ON EXTERIOR OF SKIN PER SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1999042300958 19990423 00958 NM 1999 4 23 AALA990357 1 19990216 A 5330 SKIN BOEING 727 727223 1384074 NM BS 9505 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STATION 9505 PLUS 16, APPROX 3 INCHES BELOW STRINGER 25L, SKIN HAS DEEP GOUGE. BLENDED GOUGE, ALODINED AND PRIMED AREA, BLEND OUT OF LIMITS. REPAIRED WITH DOUBLER PER SRM 53-30-3 PAGE 5, 6, 7, 8. (M) 2 L 7 3 4F A3WE 1999042300959 19990423 00959 NM 1999 4 23 AALA990358 1 19990222 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1097 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HOLE STATION 1097 RIGHT SIDE OF STRINGER 1. INSTALLED REPAIR PER SB NR 727-5 3-A0204 PARB, P615 (SRM 53-30-3 F 16.3). (M) 2 L 7 3 4F A3WE 1999042300960 19990423 00960 NM 1999 4 23 AALA990359 1 19990225 A 5330 SKIN BOEING 727 727223 1384074 NM BS 708 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STATION 708 BETWEEN STRINGER 27L AND 28L FUSELAGE SKIN HAS CORROSION. REPAIRED FUSELAGE SKIN PER SRM 53-30- 3. (M) 2 L 7 3 4F A3WE 1999042300961 19990423 00961 NM 1999 4 23 AALA990360 1 19990225 A 5330 SKIN BOEING 727 727223 1384074 NM BS 708 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION ON EXTERIOR SKIN, STATION 708 STRINGER 28L. REPAIRED FUSELAGE SKIN PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999042300962 19990423 00962 NM 1999 4 23 AALA990361 1 19990222 A 5400 S-DUCT BOEING 727 727223 1384074 NM NR 2 ENGINE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - NR 2 ENGINE S-DUCT INNER SKIN BLISTERED AROUND 2 RIVETS APPROX 2 INCH DIAMETER LOCATED 2 SKIN LAPS PLUS RIVET ROWS UP FROM AFT END BETWEEN 6 AND 7 O'CLOCK POSITION. BLENDED CORROSION PER SRM 51-10-1, INSTALLED DOUBLER PER SRM 54-10-3 . (M) 2 L 7 3 4F A3WE 1999042300963 19990423 00963 NM 1999 4 23 AALA990362 1 19990222 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION ON SKIN AROUND LEFT ICE LIGHT HOUSING BETWEEN STRINGER 14L AND 16L STATION 720B-720C. REMOVED COR ROSION AND BLENDED CORRODED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 137-140 ALODINED AND PRIMED ALL PARTS PER SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1999042300964 19990423 00964 NE 1999 4 23 TWAA9905801 2 19990419 A 7200 ENGINE BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE LEFT FAILED A TWAA A UNSCHED LANDING X M J ENGINE FLAMEOUT OVER TEMP WARNING INDICATION CR CRUISE 1 CE 05 608TW 22571 4609 THE LEFT ENGINE SHUT ITSELF DOWN AND OVERTEMPED. FLIGHT DIVERTED TO YHZ. THE ENGINE WAS CHANGED. CHECK-C 2-3-99 LAX. 2 L 7 2 4F 4 F RT A1NM E3NE 1999042300965 19990423 00965 WP 1999 4 23 TWAA9905802 1 19990420 A 3350 58222 POWER SUPPLY DOUG DC9 DC951 3022051 WP ROW 12 & 13 WORN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 405EA 47688 THE EGRESS LIGHTS ILLUMINATED BETWEEN CABIN ROWS 12 AND 13. REPLACED THE POWER SUPPLY. CHECK-C 3-30-99 STL. 2 L 7 2 4F RT A6WE 1999042300966 19990423 00966 WP 1999 4 23 CALA9900427 1 19990420 A 5210 SKIN DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A .5 INCH CRACK IN HOLD OPEN HOOK CUTOUT OF FORWARD ENTRY DOOR. THE CRACK WAS STOP DRILLED AND A DOUBL ER WAS INSTALLED IAW SRM 52-05, FIGURE 20A. 2 L 7 2 4F A6WE 1999042300967 19990423 00967 NM 1999 4 23 CALA9900428 1 19990420 A 5400 SPAR BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON OUTBOARD AFT SPAR CHORD. A DOUBLER WAS INSTALLED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 1999042300968 19990423 00968 NM 1999 4 23 CALA9900429 1 19990421 A 5542 SKIN BOEING 737 7373T0 1384582 NM RUDDER GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17326 23456 INSPECTION FOUND LT SIDE LOWER SECTION OF RUDDER LEADING EDGE SKIN GOUGED. REPAIRED IAW ECRA 5540-01110 AND SRM 51-70-1 7. 2 L 7 2 4F RT A16WE 1999042300969 19990423 00969 NM 1999 4 23 9901556718 1 19990405 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 380 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CRACKS AT FS 380, STR 25L FRAME WEB AND STR 25R FRAME. REPAIRED PER EA 67-164976. 2 L 7 4 4F A20WE 1999042300970 19990423 00970 WP 1999 4 23 9901569872 1 19990417 A 3800 FITTING DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE WATER SYST LOOSE A NWAA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 GL 01 781NC 48121 688206 DURING DESCENT, THE NR 2 ENGINE THROTTLE SETTING WOULD NOT MOVE FROM CURRENT POSITION. CREW SHUT DOWN THE NR 2 ENGINE A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SECURED WATER LINE FITTING AND REMOVED ICE. 2 L 7 2 4F 4 F RT A6WE E2EA 1999042300971 19990423 00971 NM 1999 4 23 UPS99229359 1 19990417 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1010 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, AFT CARGO BAY FRAME DENTED STA 1010 STR 25L-26L. REPAIRED FRAME AT STA 1010 STR 25L-26L PER SRM 51- 40-3. 2 L 7 3 4F A3WE 1999042300972 19990423 00972 NM 1999 4 23 UPS99229360 1 19990416 A 5310 65453132 CLIP BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACK IN STRINGER CLIPS STA 990 STR 6 AND 8 RT. REMOVED CRACKED STRINGER CLIPS STA 990 STR 6 AND 8 RT AND INSTALLED NEW STRINGER CLIPS IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1999042300973 19990423 00973 NM 1999 4 23 UPS99229361 1 19990415 A 5320 CLIP BOEING 727 72725C 138400H NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACK IN STRINGER CLIP STA 1070 STR 9 RT. REMOVED CRACKED STRINGER CLIP AT BS 1070 AND INSTALLED NE W STR CLIP IAW SRM 51-30-02, 51-10-01, 51-20-01. 2 L 7 3 4F A3WE 1999042300974 19990423 00974 NM 1999 4 23 UPS99229362 1 19990415 A 5311 FRAME BOEING 727 72725C 138400H NM BS 277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACK ON FRAME AT STA 277 JUST ABOVE STR 26 RT. STOP DRILLED CRACK IN FRAME, FABRICATED REPAIR DOUB LER, FABRICATED STIFFENER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02, 51-10-02, MM 51-20-151. 2 L 7 3 4F A3WE 1999042300975 19990423 00975 NM 1999 4 23 UPS99229363 1 19990415 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 782-788 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, DAMAGE TO SEAT TRACK IN WELL AT BS 782 TO 788 LBL 62 WL 208. ALSO, FOUND CORROSION ON O/B FLANGE BS 760- LBL 66 FOUND OUT OF LIMITS. REPLACED SEAT TRACK FROM BS 750 TO BS 850 PER SRM 51-30-2 AND 53-10-5. 2 L 7 3 4F A3WE 1999042300976 19990423 00976 NM 1999 4 23 UPS99229364 1 19990416 A 5315 BAC1505100246 FLOORBEAM BOEING 727 72725C 138400H NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON STA 328 FLOORBEAM UPPER CHORD LBL 50. REPAIRED FLOORBEAM AT STA 328 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999042300977 19990423 00977 NM 1999 4 23 UPS99229365 1 19990416 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CORROSION ON FLOORBEAM UPPER FLANGE LBL 50 TO RBL 50. REPAIRED FLOORBEAM SRM 53-10-8. 2 L 7 3 4F A3WE 1999042300978 19990423 00978 NM 1999 4 23 UPS99229366 1 19990413 A 5530 ANGLE BOEING 727 72725C 138400H NM BS 180.6 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, VERTICAL FIN STA 180.6, STR 7, ANGLE IS CRACKED AT FASTENER HOLE. REMOVED FASTENERS COMMON TO REPAI R, FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS. INSTALLED REPAIR PARTS IAW SRM 55-30-02, 55-30-05. 2 L 7 3 4F A3WE 1999042300979 19990423 00979 NM 1999 4 23 UPS99229367 1 19990416 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 720 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, SHEAR TIE CRACKED AND FASTENER SHEARED STA 720 BETWEEN STR 20R AND 21R. REPAIRED SHEAR TIE AT STA 7 20 BETWEEN STR 20R AND 21R PER SRM 53-10-4 AND 51-20-1. 2 L 7 3 4F A3WE 1999042300980 19990423 00980 NM 1999 4 23 UPS99229368 1 19990416 A 5320 TENSION STRAP BOEING 727 72725C 138400H NM BS 720 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, LWR FLOORBEAM TENSION STRAP CRACKED STA 720, RBL 25, WL 200. STOP DRILLED CRACK, FABRICATED AND INS TALLED REPAIR TO TENSION STRAP AT LWR FLOORBEAM TENSION STAP AT STA 720, RBL 25, WL 200 PER SRM 53-10-8, 51-30-2. 2 L 7 3 4F A3WE 1999042300981 19990423 00981 NM 1999 4 23 UPS99229369 1 19990416 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, SHEAR TIE CRACKED STA 680 BETWEEN STR 17R AND 18R. REPAIRED SHEAR TIE AT STA 680 BETWEEN STR 17R AN D 18R PER SRM 51-20-1. 2 L 7 3 4F A3WE 1999042300982 19990423 00982 NM 1999 4 23 UPS99229370 1 19990415 A 5320 CLIPS BOEING 727 72725C 138400H NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACK IN STRINGER CLIPS STA 1050 RT STRINGERS 5 AND 6. REPLACED BOTH CLIPS PER 727 SRM 51-30-2 AND 51-30-5. 2 L 7 3 4F A3WE 1999042300983 19990423 00983 NM 1999 4 23 UPS99229371 1 19990419 A 5720 CHORD BOEING 727 72725C 138400H NM BS 171.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, RT WING TANK UPPER CHORD CRACKED AT STRINGER 21 STA 171.5. REMOVED AND REPLACED THE CHORD IAW SRM 5 1-30-2. CHORD REPLACEMENT LOCATED AT RT WING, STRINGER 21 WS 171.5. 2 L 7 3 4F A3WE 1999042300984 19990423 00984 NM 1999 4 23 UPS99229372 1 19990419 A 5720 CHORD BOEING 727 72725C 138400H NM BS 171.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, UPPER RIB FLANGE CRACKED AT LT WING (FUEL TANK) UPPER STRINGER NR 16 WS 171.5. REMOVED AND REPLACED CHORD PER SRM 51-30-2. CHORD REPLACEMENT LOCATED AT UPPER STRINGER 16 WS 171.5 AT LT WING. 2 L 7 3 4F A3WE 1999042300985 19990423 00985 NM 1999 4 23 UPS99229373 1 19990416 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM LT EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, LT AFT OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED LT AFT OVERWING BATTERY PACK, OPS CHECKS GO OD. 2 L 7 3 4F A3WE 1999042300986 19990423 00986 NM 1999 4 23 UPS99229374 1 19990416 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 11 & 12 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP AT LT FWD EMERGENCY EXIT DOOR OVERWING LOWER ROW 11/12. REMOVED AND REP LACED 2 BATTERY PACKS FOR EMERGENCY EXIT DOORS, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999042300987 19990423 00987 WP 1999 4 23 ABXA9900303 1 19990419 A 7931 42D491C SWITCH DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 23 828AX 45999 671397 DURING DESCENT INTO ONT, WITH POWER REDUCED TO IDLE, NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED. OIL PRESS IND 42 PSI. S HUT NR 1 ENGINE DOWN, OIL PRESS WAS 7 PSI DURING DESCENT AND APPROACH FOR 8 MINUTES. INSPECTED MAIN OIL FILTER, NO CONT AMINATION FOUND. CHECKED CONNECTORS AND WIRING, CLEANED CONTACTS ON OIL PRESSURE WARNING SWITCH AND OIL PRESSURE WARNIN G SWITCH, NO DEFECTS NOTED. NON SUBSEQUENT FLIGHT DURING TAXI OUT, NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED, OIL PRESS I NDICATED 42 PSI AT IDLE. VERIFIED OIL PRESSURE SWITCH DEFECTIVE. REPLACED SWITCH. 2 L 7 4 4F 4 F 4A25 1E8 1999042300988 19990423 00988 WP 1999 4 23 MWEA99174 1 19990417 A 5230 3914025502 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT CARGO DOOR AFI I/B STOP FITTING CORRODED AROUND AND UNDER RADIUS BLOCK. INSTALLED NEW FITTING AND FABRICATED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999042300989 19990423 00989 WP 1999 4 23 MWEA99175 1 19990417 A 5311 3912237511 FRAME DOUG DC9 DC932 3022066 WP BS 813 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 AFT PIT FLOOR FRAME STA 813 LOWER SIDE HAS SEVERAL AREAS OF CORROSION FROM 28R TO 27L. BLENDED CORROSION, INSTALLED REP AIR SPLICE. 2 L 7 2 4F A6WE 1999042300990 19990423 00990 WP 1999 4 23 MWEA99176 1 19990416 A 5330 5920303501 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 BULGING AFT BAG AT BELLY SKIN AROUND HI-LOKS AT SKIN SPLICE. FABRICATED AND INSTALLED NEW BELLY SKIN. 2 L 7 2 4F A6WE 1999042300991 19990423 00991 WP 1999 4 23 MWEA99177 1 19990407 A 2710 50132383 BUSHING DOUG DC9 DC914 3022034 WP LT WING WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 BUSHING WORN IN LT WING AILERON SECTOR SUPPORT. FABRICATED REPAIR BUSHINGS. 2 L 7 2 4F A6WE 1999042300992 19990423 00992 WP 1999 4 23 MWEA99178 1 19990407 A 5753 YTS1748 BUSHING DOUG DC9 DC914 3022034 WP RT TE FLAP VANE WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 BUSHING WORN RIGHT HAND AFT MOVEABLE VANE CLEVIS FITTING. FABRICATED BUSHING AND INSTALLED. 2 L 7 2 4F A6WE 1999042300993 19990423 00993 WP 1999 4 23 MWEA99179 1 19990407 A 5315 2777896 FLOORBEAM DOUG DC9 DC914 3022034 WP BS 313 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 700ME 45696 FLOORBEAM AT FS 313 RBL 6 TO RBL 20 HAS MISDRILLED HOLES IN RADIUS OF BEAM. FABRICATED FLANGE REPAIR. 2 L 7 2 4F A6WE 1999042300994 19990423 00994 WP 1999 4 23 MWEA99180 1 19990406 A 5320 29129015 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 465 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO COMPARTMENT HAS A CRACKED ATTACH POINT RADIUS ON INTERCOSTAL FS 465. FABRICATED AND INSTALLED INTERCOSTAL REPAIR. 2 L 7 2 4F A6WE 1999042300995 19990423 00995 WP 1999 4 23 MWEA99181 1 19990406 A 5520 S24312154011 BUSHING DOUG DC9 DC914 3022034 WP LT ELEVATOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT HAND ELEVATOR HAS WORN BUSHING. FABRICATED OVERSIZED REPAIR BUSHING. 2 L 7 2 4F A6WE 1999042300996 19990423 00996 WP 1999 4 23 MWEA99182 1 19990407 A 5320 5910137 WEB DOUG DC9 DC914 3022034 WP BS 503 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FUSELAGE CABIN WEB CRACKED AT FS 503 RT. REPLACED WEB. 2 L 7 2 4F A6WE 1999042300997 19990423 00997 WP 1999 4 23 MWEA99183 1 19990327 A 5210 995572501 BEAM DOUG DC9 DC914 3022034 WP L 1 DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 L1 DOOR VERTICAL BEAM CRACKED IN RADIUS. REMOVED CRACKED FRAME, FABRICATED, PRIMED AND INSTALLED REPAIR FRAME. 2 L 7 2 4F A6WE 1999042300998 19990423 00998 NE 1999 4 23 DLM11990836 2 19990414 A 7230 COMPRESSOR DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE DAMAGED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 813DE 30974 48600 723872 AT APPROX 95 KTS ON TAKEOFF, COMPRESSOR STALL ON RT ENGINE. REPLACED ENGINE. 2 L 7 3 4F 4 F RT A22WE E24NE 1999042300999 19990423 00999 NM 1999 4 23 DL72K990838 1 19990414 A 5330 655457415 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS IN THE PANEL. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE EN TIRE LENGTH OF THE PANEL AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 367179-14AD. 2 L 7 3 4F A3WE 1999042301000 19990423 01000 NM 1999 4 23 DL72K990839 1 19990414 A 5330 655456715 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS IN THE SKIN. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE ENT IRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367178-14AD. 2 L 7 3 4F A3WE 1999042301001 19990423 01001 NM 1999 4 23 DLM88990841 1 19990415 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN CONTAMINATEDN A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 999DN 53371 BOTH AFT SMOKE DETECTORS ACTIVATED AFTER TAKEOFF FOR 2-3 MINUTES. LIGHT SMOKE PRESENT BRIEFLY. REPLACED COALESCER BAG S. 2 L 7 2 4F RT A6WE 1999042301002 19990423 01002 NM 1999 4 23 DLM88990843 1 19990416 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 916DL 49591 FLT 1407 DCA-ATL. NOSE GEAR WILL NOT RETRACT. DIVERTED INTO IAD. SERVICED STRUT. 2 L 7 2 4F RT A6WE 1999042301003 19990423 01003 NM 1999 4 23 DLM88990845 1 19990416 A 4910 INLET DOUG MD88 MD88 3023688 NM APU CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 911DL 49542 ON FINAL APPROACH WITH AIRSPEED AT 150 KTS THE F/A AND PILOTS SMELLED A HOT ODOR WITH BOTH ENG AND WING A/I ON. SMELL D ISSIPATED WHEN WING A/I TURNED OFF. FOUND OIL ON APU INLET. PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1999042301004 19990423 01004 NM 1999 4 23 DLM88990848 1 19990417 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 904DE 53409 NLG WOULD NOT RETRACT. SERVICED NOSE STRUT. 2 L 7 2 4F RT A6WE 1999042301005 19990423 01005 NM 1999 4 23 DL72S990855 1 19990417 A 5330 655456716 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 40 CRACKS ALONG THE LENGTH OF THE PANEL. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTENRAL ALUMINUM DOUBLER PER ER/A 367208-14AD. 2 L 7 3 4F A3WE 1999042301006 19990423 01006 NM 1999 4 23 DL72S990856 1 19990417 A 5330 6554574132 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 57 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CU TOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367207-14AD. 2 L 7 3 4F A3WE 1999042301007 19990423 01007 NM 1999 4 23 DL72W990857 1 19990419 A 5330 655457489 SKIN BOEING 727 727247 138408F NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SP LICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367191-14AD. 2 L 7 3 4F A3WE 1999042301008 19990423 01008 NM 1999 4 23 DL72W990858 1 19990419 A 5330 65545703 SKIN BOEING 727 727247 138408F NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367190-14AD. 2 L 7 3 4F A3WE 1999042301009 19990423 01009 NM 1999 4 23 DL72W990859 1 19990419 A 5330 65545671 SKIN BOEING 727 727247 138408F NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367192-14AD. 2 L 7 3 4F A3WE 1999042301010 19990423 01010 NM 1999 4 23 DL72S990860 1 19990416 A 5311 FRAME BOEING 727 727232 1384082 NM BS 620 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 THE AFT FRAME OF THE C1 CARGO DOOR OPENING WAS FOUND WITH A 1 INCH CRACK IN THE FRAME WEB BELOW THE LOWER DOOR STOP FITT ING. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A DOUBLER PER ER/A 367202-14. 2 L 7 3 4F A3WE 1999042301011 19990423 01011 NM 1999 4 23 DL72W990861 1 19990419 A 5320 FRAME BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 FOUND AT B-2 LETTER CHECK, .5 INCH CRACK ON RT AFT ENTRY DOOR FRAME. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999042301012 19990423 01012 NM 1999 4 23 DL72W990862 1 19990419 A 5320 FRAME BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 FOUND AT B-2 LETTER CHECK, .5 INCH CRACK ON LT AFT ENTRY DOOR FRAME. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999042301013 19990423 01013 NM 1999 4 23 DL72W990863 1 19990419 A 5522 SKIN BOEING 727 727247 138408F NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 A 2.5 INCH CRACK IN RT ELEVATOR LOWER SKIN AFT OF NR 4 BALANCE BOARD. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1999042301014 19990423 01014 NM 1999 4 23 DL72S990864 1 19990420 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 FOUND AT E-1 LETTER CK, RT AFT ENTRY DOOR FRAME HAS VISABLE CRACK AT UPPER CUT OUT. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999042301015 19990423 01015 NM 1999 4 23 DL72S990865 1 19990420 A 2782 ANGLE BOEING 727 727232 1384082 NM NR 3 SPOILER ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 FOUND ON E-1 LETTER CK, NR 3 SPOILER O/B ACTUATOR ATTACH CASTING CRACKED. REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1999043000001 19990430 00001 WP 1999 4 30 AALA990409 1 19990319 A 5320 53610607205 FITTING DOUG DC9 DC982 3022082 WP BS 1340 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7512A 49806 TUL - FORWARD SIDE FRAME 18, STR 44R, HAS CORROSION ON FRAME 18. CORROSION REMOVED PER SRM 51-74-10, AND REPAIRED PER S RM 51-71-50. TST: 29,628.53 HOURS. CYCLES: 10,098. (X) 2 L 7 2 4F A6WE 1999043000002 19990430 00002 SO 1999 4 30 SIMA990779 1 19990318 A 3350 AD20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 617AE 66556 145093 ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, A ND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 I AW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR 99ZZZX1654 THROUGH 99ZZZX1656. (X) 2 L 7 2 4T RT T00011AT 1999043000003 19990430 00003 SO 1999 4 30 99ZZZX1654 1 19990318 A 3350 AD20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 617AE 66424 145093 ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, A ND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 I AW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR SIMA990779, AND, 99ZZZX1655 AND 99ZZZX1656. 2 L 7 2 4T RT T00011AT 1999043000004 19990430 00004 SO 1999 4 30 99ZZZX1655 1 19990318 A 3350 AD20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 617AE 66557 145093 ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, A ND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 I AW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR SIMA990779, AND, 99ZZZX1654 AND 99ZZZX1656. 2 L 7 2 4T RT T00011AT 1999043000005 19990430 00005 SO 1999 4 30 99ZZZX1656 1 19990318 A 3350 AD20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 617AE 66545 145093 ORD - FLT 4023 - WHEN FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS, THEY INITIALLY CAME ON, THEN IMMEDIATELY WENT DIM, A ND THEN, FAILED TO ILLUMINATE AT ALL AFTER 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS 1 THROUGH 4 I AW EMB-145 AMM 33-90-04. OPERATIONAL CHECK GOOD. REF: OPER CNTRL NR SIMA990779, AND, 99ZZZX1654 AND 99ZZZX1655. 2 L 7 2 4T RT T00011AT 1999043000006 19990430 00006 EU 1999 4 30 SIMA990672 1 19990308 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSP, DENTS EXCEEDING SRM LIMITS DISCOVERED ON CARGO DOOR. CUT OUT DAMAGED AREAS, DEBURRED, SMOOTHED E DGES, AND PERFORMED EDDY CURRENT INSP. FABRICATED FILLER PLATES MAT'L WITH DIMENSIONS EQUAL TO CUT-OUTS. FABRICATED A REPAIR DOUBLER PLATE, MAT'L DIMENSIONS OVERLAP CUT-OUTS BY 1 INCH. FILLED HONEYCOMB CORE WITH EPOXY FILLER LY/HY 5052, INSTALLED FILLER PLATES, APPLIED PRESSURE. CLEANED REPAIR AREA AND THE DOUBLER, INSTALLED DOUBLER PLATE TO THE SKIN WIT H ADHESIVE EA 9330. APPLIED DISTRIBUTED PRESSURE UNTIL CURED. APPLIED SEALANT AROUND EDGES OF THE DOUBLER PLATE, RESTO RED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1419 AND SAAB SRM 52-10-10. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999043000007 19990430 00007 EU 1999 4 30 SIMA990671 1 19990308 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSPECTION, A CHAFE WAS DISCOVERED ON THE RT NACELLE FILLET FAIRING SEAL CONTACT AREA. BLENDED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR DOUBLER AND TRIPLER BOTH .050 INCH THICK. APPLIED P ROTECTIVE TREATMENT TO BOTH THE DOUBLER AND TRIPLER INCLUDING THE POLYURETHANE TOP COAT. FABRICATED SHIMS .020 INCH THI CK. INSTALLED REPAIR DOUBLER, TRIPLER, AND SHIMS. APPLIED FILLET SEALANT AROUND EDGES OF REPAIR AND RESTORED SURFACE F INISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1419 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999043000008 19990430 00008 EU 1999 4 30 SIMA990643 1 19990305 A 5347 465000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-329 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSPECTION, SEAT TRACK 18.3L WAS FOUND CORRODED BEYOND SRM LIMITS AT FS 297 - FS 329. CUT OUT 32 INCH SECTION OF SEAT TRACK, DEBURRED, ALODINED, AND PAINTED EDGES. FABRICATED A 32 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76511 EXTRUDED MATERIAL, DEBURRED, ALODINED, AND PAINTED. FABRICATED A 15 INCH U-BEAM OF PLAL 7075-T7351 MATERIAL , DEBURRED, ALODINED AND PAINTED SURFACES. INSTALLED U-BEAM AND SEAT TRACK IN AIRCRAFT. WORK DONE IAW SAAB 340 SRM 53- 70-60, AND STANDARD PROCEDURES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999043000009 19990430 00009 EU 1999 4 30 SIMA990642 1 19990305 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340RC 340B340 ABI - DURING MBV INSPECTION, SEAT TRACK BL ZERO WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED FASTENER AND EXISTING SEA T TRACK. DRILLED FASTENER HOLES ON NEW SEAT TRACK EXTRUSION AND TREATED. INSTALLED NEW SEAT TRACK AND SECURED. TRACK AND SECURED. APPLIED DINOTROL TO SEAT TRACK AND SUPPORTS. WORK DONE IAW SAAB 340 SRM 53-70-60 AND STANDARD SRM PROCEDU RES. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999043000011 19990430 00011 WP 1999 4 30 99ZZZX1658 1 19990129 A 7603 CONDITION LEVER CVAC 440 440 2422902 WP RIGHT BINDING A RENA O OTHER O OTHER AP APPROACH 1 WP 01 73163 366 NTD - ON APPROACH, RIGHT THROTTLE WOULD NOT RETARD PAST 1,500 HP IN-FLIGHT. BINDING IN THROTTLE LINKAGE. IN-FLIGHT SHU T DOWN. 2 L 7 2 4R 6A6 1999043000012 19990430 00012 1999 4 30 99ZZZX1659 4 19990322 A 3421 RCA26BK1 GYRO HUGHES 369 369D 4470706 WP COCKPIT MALFUNCTIONED B LS1R K NONE O OTHER IN INSP/MAINT 1 EA 13 369AW 1263 W3077 470117D GYRO WILL NOT CAGE. REMOVED AND REPLACED. 1 G 7 1 3U H3WE 1999043000013 19990430 00013 SO 1999 4 30 C2XA99IA186 1 19990309 A 3350 78241 POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 IAH - FLT 4215 - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHTS WERE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IAW EMB145 MM 33-50-11, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999043000014 19990430 00014 SO 1999 4 30 C2XA99IA189 1 19990310 A 2612 FIRE LIGHT EMB 145 EMB145 SO BAGG COMPT ILLUMINATED A C2XA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 09 27962 145110 IAH - FLT 4210 - DURING TAXI TO GATE, THE CREW REPORTED THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED. MAINTENANCE PERFORM ED AN OPERATIONAL TEST OF THE BAGGAGE FIRE DETECTION SYSTEM VERIFYING NORMAL OPERATION IAW EMB145 MM 26-15-00, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY HAS NOT REPEATED TO-DATE. (X) 2 L 7 2 4F RT T00011AT 1999043000015 19990430 00015 NE 1999 4 30 GAIA99043A 2 19990315 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A GAIA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 07 6807 19482 665162 SEA/DFE - DURING CLIMB-OUT, SEVERE ENGINE VIBRATION AND ROLL BACK OF NR 2 ENGINE INDICATING INSTRUMENTS. THE CREW PERFO RMED ENGINE FAILURE CHECK LIST, AND RETURNED BACK TO SEA. THE CREW MADE AN UNEVENTFUL LANDING WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY IAW KITTY HAWK MM WORK CARD BH-719401. LEAKED AND TRIMMED CHECKED ENGINE IA W KITTY HAWK MM WORK CARD BH-719518. ALL SYSTEMS WERE CHECKED NORMAL. AIRCRAFT WAS THEN RETURNED TO SERVICE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1999043000016 19990430 00016 NM 1999 4 30 GAIA99039 1 19990302 A 5753 652163395A SKIN BOEING 727 727223 1384074 NM TE MID FLAP DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6807 19482 DURING C-CHECK, DAMAGE WAS FOUND ALONG THE OUTBOARD MID-FLAP LOWER SKIN. THE PART HAS A MILLED OPENING FOR AN ACCESS PA NEL. THE NUTPLATE HOLES WERE DAMAGED. A REPAIR DOUBLER WAS FABRICATED FROM 2024-T3 BY .0100 INCH CLAD ALUMINUM. THE R EPAIR WAS ACCOMPLISHED IAW AIA EDR NR B206402. (X) 2 L 7 3 4F A3WE 1999043000017 19990430 00017 NM 1999 4 30 GAIA99040 1 19990302 A 5720 6562333516 BEAM BOEING 727 727223 1384074 NM WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6807 19482 DURING ROUTINE C-CHECK, CORROSION WAS FOUND IN THE MLG BEAM AT NR 4 FLAP TRACK OUTBOARD ATTACH POINT. THE CORROSION WAS REMOVED AND IT WAS DETERMINED TO BE BEYOND LIMITS. INSTALLED OVERSIZED BUSHING PER BOEING IPC. THE REPAIR WAS CARRIED OUT IAW AIA ENGINEERING DEVIATION REPORT NR B2 06407 AND AIA NON-ROUTINE M40 53402. (X) 2 L 7 3 4F A3WE 1999043000018 19990430 00018 NM 1999 4 30 GAIA99041 1 19990302 A 5315 BAC1518347 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6807 19482 DURING ROUTINE C-CHECK, A CRACK WAS FOUND ALONG THE FLOORBEAM, UPPER CAP AT FS 1130 LBL 45. THE REPAIR WAS CARRIED OUT IAW AIA ENGINEERING DEVIATION REPORT NR B2 06407 AND AIA NON-ROUTINE M40 53403. THIS REPAIR IS AFFECTED BY AD 98-26-21 AND WAS SENT TO THE FAA ACO FOR APPROVAL. (X) 2 L 7 3 4F A3WE 1999043000019 19990430 00019 NM 1999 4 30 GAIA99042 1 19990302 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1183 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6807 19482 DURING ROUTINE C-CHECK, CORROSION WAS FOUND AROUND AFT LAVATORY DRAIN, BOX STRUCTURE, AND SKIN. LOCATED AT STR 20, LEFT FS 1183. THE CORROSION WAS REMOVED AND IT WAS DETERMINED TO BE BEYOND LIMITS. REPAIR WAS CARRIED OUT IAW AIA ENGINEER ING DEVIATION REPORT NR B2 06413, AIA NON-ROUTINE M40 52862 AND BOEING REPAIR SKETCH CKF-ORD-99-0017RR. (X) 2 L 7 3 4F A3WE 1999043000020 19990430 00020 NE 1999 4 30 TWRA9903 2 19990118 A 7200 ENGINE BOEING 747 747283B 1384867 NM PWA JT9 JT9D7Q 52054 NE NR 1 FAILED A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN A FLAME/FIRE CL CLIMB 1 EA 15 622FF 22496 702391 JFK/SFO - FLT 23 - ATB DUE AT 13,500 FEET. FELT VIBRATION IN AIRCRAFT. INITIALLY, ALL PARAMETERS NORMAL. A FEW SECOND S LATER, CAPTAIN CALLED, LOSING NR 1 ENGINE, NR 1 EGT STARTED CLIMBING AND VIBRATION INCREASED. NR 1 ENGINE WAS SHUT DO WN IAW ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECK LIST. APPROXIMATELY 30 SECONDS LATER, NR 1 FIRE HANDLE ILLUMINATE D WITH THE NR 1 B-LOOP CLIMBING TO TOP OF SCALE. NR 1 LEFT FIRE BOTTLE WAS DISCHARGED AND IN-FLIGHT INDICATIONS WERE TH AT FIRE WAS EXTINGUISHED. FOUND NR 3 BEARING COMPT BREATHER TUBE FITTING BURNED THROUGH CAUSING OIL FIRE. REMOVED AND REPLACED NR 1 ENGINE. INITIAL CAUSE TO BE DETERMINED UPON REMOVED ENGINE TEAR DOWN REPORT. (X) 2 L 7 4 4F 4 F A20WE E3NE 1999043000021 19990430 00021 EU 1999 4 30 99ZZZX1660 1 19990317 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU RT EMERG EXIT DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GCVYD 393 YYZ - FLT 6000 - FOUND AT A-CHECK, RIGHT HAND OVERWING EXIT LIGHT WILL NOT COME ON. REMOVED AND REPLACED RIGHT HAND OVE RWING BATTERY UNIT. (X) 2 L 7 2 4F RT A28NM 1999043000022 19990430 00022 EU 1999 4 30 99ZZZX1661 1 19990317 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU RT EMERG EXIT INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GCVYD 393 YYZ - FLT 6000 - FOUND AT A-CHECK, RIGHT OVERWING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING POWER SUP PLY. (X) 2 L 7 2 4F RT A28NM 1999043000023 19990430 00023 NM 1999 4 30 USAABB99013 1 19990311 A 3260 284T02694 SENSOR BOEING 767 767201 1385125 NM NLG DOOR OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 646US 23898 PIT - FLT 48 - DURING CLIMB OUT OF PIT, CREW RECEIVED THE EICAS MESSAGE 'GEAR DOORS'. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. AIRCRAFT WAS FERRIED TO CLT. MAINTENANCE FOUND THE SYSTEM 1 RIGHT NOSE GEAR DOOR P2 CLOSED SENSOR (S235) GAP EXCEEDING THE MM LIMITS AND ADJUSTED IT. GEAR WAS SWUNG TO VERIFY OPERATION. (X) 2 L 7 2 4F RT A1NM 1999043000041 19990430 00041 EU 1999 4 30 99ZZZX1680 1 19990406 A 6420 350A33200405 SPIDER 350A33020005 SNIAS 350 AS350B2 8680813 EU TAIL ROTOR FAILED A P A HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 6095S 869 22 M1638 2777 AIRCRAFT EXPERIENCED LOSS OF TAIL ROTOR CONTROL DURING FLIGHT. PILOT REPORTED HE COULD ONLY SLIGHTLY MOVE TAIL ROTOR PE DALS. PILOT EXECUTED A SUCCESSFUL RUN-ON LANDING ON A HARD SURFACE RUNWAY WITHOUT CAUSING ANY DAMAGE TO ACFT. EXAMINAT ION OF THE ACFT REVEALED THE ROTATING SPIDER (PN 350A33-2129-00) HAD BEEN COMPLETELY SEVERED AND THE TAIL ROTOR WAS BEIN G DRIVEN BY PITCH CHANGE LINKS. THE SPIDER BEARING (PN 6010-2RS1MT33CA) APPARENTLY SEIZED AND CUT THROUGH THE ROTATING SPIDER. SPIDER ASSY WAS REMOVED FROM ACFT FOR FURTHER EVALUATION. PART TAGGED WITH FAA FORM 8020-2 (ACFT/PARTS IDENTI FICATION AND RELEASE). ROTORCRAFT CERTIFICATION OFFICE (ASW-170) WAS NOTIFIED OF THE MALFUNCTION AND PART DISPOSITION. 1 G 7 1 3U H9EU 1999043000042 19990430 00042 SW 1999 4 30 99ZZZX1681 1 19990308 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW MAIN ROTOR CORRODED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 1068S 1785 A2697 45436 CORROSION BENEATH GRIP FINGER DOUBLER EXTENDING APPROXIMATELY 3 INCHES OUTBOARD ALONG SPAR. 1 G 7 1 3U H2SW 1999043000058 19990430 00058 EU 1999 4 30 99ZZZX1697 1 19990319 A 6510 350A34011007 SHAFT SNIAS 350 AS350D1 8680804 EU TAIL ROTOR MISMANUFACTURED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 57731 M1885 1434 TAIL ROTOR SHAFT REJECTED NEW OUT-OF-BOX. SHAFT WOULD NOT BALANCE. .006 INCH OUT OF ROUND FORWARD OF NR 6 BEARING. RE PLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999043000097 19990430 00097 CE 1999 4 30 CA990111004 1 19990104 A 2730 115610010325 TORQUE TUBE BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE50617 (CAN) INSPECTED PER SB 2145. FOUND A SMALL CRACK IN THE LEFT TORQUE TUBE ASSEMBLY AT THE TAPER FIN HOLE ON THE INBOARD SUPPORT CASTING. TAPER PIN HAD BEEN REPLACED 1,000 HOURS PRIOR. NO PLAY FOUND IN TORQUE TUBE. 1 L 7 2 3T 4 T A14CE E4EA 1999043000100 19990430 00100 EU 1999 4 30 CA990310088 2 19990101 A 7250 BLADE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 1 ENGINE SEPARATED W E A ENGINE SHUTDOWN UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CR CRUISE 1 CA 9539 (CAN) DURING FLIGHT AT FL 300, THE NR 1 ENGINE FLAMED OUT AND THE HP FUEL LEVER MOVED TO THE SHUTOFF POSITION UNINITIATE D. AIRCRAFT LANDED WITHOUT INCIDENT AND THE ENGINE WAS REPLACED. THE AIRCRAFT RETURNED TO SERVICE. OBSERVATIONS ON TH E REPLACED ENGINE WERE; ONE LP TURBINE BLADE MISSING; MANY GOUGES ON OTHER TURBINE BLADES; 2 OF THE LPT2 SHROUD SEGMENT MISSING; LPT2 VANE SEGMENTS GOUGES; LP COMPRESSOR VERY DIRTY. 2 L 7 2 4F 4 F RT A20EU E2EU 1999043000101 19990430 00101 NM 1999 4 30 CA990310096 1 19990209 A 5210 852205283001 CABLE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE PAX DOOR STUCK W O OTHER O OTHER NR NOT REPORTED 1 CA 123030 (CAN) CREW COULD NOT OPEN MAIN CABIN DOOR DUE TO ASSIST CABLE SNAGGING ITSELF ON DOOR. CREW THEN ATTEMPTED TO DEPLANE P ASSENGERS OUT SERVICE EMERGENCY EXIT, BUT IT WAS FROZEN. PASSENGERS DEPARTED THROUGH REAR BAGGAGE COMPARTMENT VIA CABIN ACCESS DOOR. REPLACED MAIN DOOR CABLE AND STRUTS. EMERGENCY DOOR HANDLE FOUND VERY STIFF AND HARD TO MOVE, HOWEVER, COULD STILL OPEN DOOR. DOOR REMOVED AND INTERNAL RIGGING LUBBED. THIS SECOND OCCURRENCE OF EMERGENCY DOOR BEING FROZEN AND DIFFICULT TO OPEN IN RECENT MONTHS. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000117 19990430 00117 EU 1999 4 30 99ZZZX1712 1 19990128 A 7110 DOOR BOLKMS 117 BK117B2 5626013 EU ENGINE COWL SEPARATED A HEEA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SW 03 134AE 6061 7237 IN CRUISE FLIGHT, PILOT NOTICED A CHANGE IN SOUND. CONTINUED FLIGHT (7 MILES AWAY) TO DESTINATION. POST-FLIGHT INSPECT ION REVEALED RT ENGINE COWL SIDE DOOR MISSING. COWLING HAD MADE MINOR CONTACT WITH ONE M/R BLADE. REF: BK-117 IPC, FI GURE 221, ITEM 10. 1 G 7 2 3U NC H13EU 1999043000134 19990430 00134 SO 1999 4 30 99ZZZX1729 1 19990413 A 3230 40616002 BRACKET PIPER PA31T PA31T 7103124 SO MLG SHEARED A IPMA K NONE O OTHER IN INSP/MAINT 1 WP 11 419R 6654 31T7820034 FOUND MLG UPLOCK SUPPORT BRACKET SHEARED ON PRE-FLIGHT. INSPECTION OF THE LINK ROD ASSY INDICATED NORMAL OPERATION AND CORRECT LUBRICATION. UNABLE TO DETERMINE CAUSE. NO EVIDENCE OF UPLOCK STICKING INDICATED. 1 L 7 2 3T A8EA 1999043000135 19990430 00135 1999 4 30 99ZZZX1730 4 19990304 A 2250 501113303 COMPUTER LEAR 35 35LEAR 5170600 CE SPOILERON MALFUNCTIONED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 1140A 35045 AUG-AIL - BLEW CIRCUIT BREAKER GOING INTO (BDL). MEL'D AUG-AIL SYSTEM AND FLEW TO CMH. REMOVED AND REPLACED SPOILERON COMPUTER. OPS CHECKS GOOD. 2 L 7 2 4F A10CE 1999043000142 19990430 00142 NM 1999 4 30 99ZZZX1735 1 19990316 A 2410 ALTERNATOR PIPER PA60 PA60600 7106001 NM ENGINE FAILED A BSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 6076L 600713796122 BOTH ALTERNATORS FAILED AFTER TAKEOFF OUT OF UTICA, NY. FOUND NR 6 WIRE TO RT DIODE SHORTED. ALSO, REMOVED AND REPLACE D LEFT ALTERNATOR AND VOLTAGE REGULATOR. OPS CHECKED GOOD. 1 M 7 2 3O RT A17WE 1999043000143 19990430 00143 NM 1999 4 30 99ZZZX1736 1 19990323 A 3244 TIRE PIPER PA60 PA60600 7106001 NM RT MLG FAILED A BSYA O OTHER O OTHER LD LANDING 1 GL 07 7512S 600144064 BOS - RIGHT MAIN TIRE BLEW ON LANDING. REMOVED AND REPLACED TIRE AND WHEEL ASSEMBLY. 1 M 7 2 3O RT A17WE 1999043000144 19990430 00144 CE 1999 4 30 99ZZZX1737 1 19990309 A 3260 POINTER BEECH 58 58 1152740 CE NLG LOOSE A BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 9189Q TH148 MECHANICAL NOSE GEAR POINTER DID NOT SHOW NOSE GEAR DOWN AND LOCK. INDICATOR SHOWED OK. DID A FLY-BY AT LITTLE ROCK TO WER AND LANDED OK. RE-ATTACHED MECHANICAL POINTER AND ADJUSTED AS REQUIRED. 1 L 7 2 3O 3A16 1999043000145 19990430 00145 NM 1999 4 30 99ZZZX1738 1 19990310 A 3260 INDICATION PIPER PA60 PA60600 7106001 NM NLG MALFUNCTIONED A BSYA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 07 6892R 600887816125 AFTER DEPARTING FROM UTICA, NY, AIRCRAFT DID NOT GET A NOSE LANDING GEAR UP LIGHT, FLEW PAST CONTROL TOWER FOR VERIFICAT ION, GEAR WAS UP. FLEW AIRCRAFT TO BDL MAINTENANCE BASE. SERVICED NOSE STRUT, CYCLED GEAR. OPS CHECKED GOOD. 1 M 7 2 3O RT A17WE 1999043000204 19990430 00204 WP 1999 4 30 TWAA9906001 1 19990425 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9307R 49663 THE CABIN EMERGENCY EGRESS LIGHTS WIRING WAS EXPOSED AND LIFTING FROM THE FLOOR. REPLACED THE LAMP AND COVER AT ROWS 2, 22, 25, 29, AND 32. CHECK-C 11-18-98 STL. 2 L 7 2 4F RT A6WE 1999043000205 19990430 00205 WP 1999 4 30 TWAA9906002 1 19990422 A 3350 BULB DOUG DC9 DC983 3022083 WP ROW 22-24 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9630A 53561 THE EGRESS LIGHTS WERE INOPERATIVE AT FWD END OF FIRST CLASS, AND AT CABIN ROWS 22, 23, AND 24. AT FWD END OF FIRST CLA SS SECURED LAMP IN THE SOCKET. FOR AFT CABIN SECURED CONNECTOR AT ROW 24. CHECK-C 6-7-98 MCI. 2 L 7 2 4F RT A6WE 1999043000206 19990430 00206 WP 1999 4 30 TWAA9906003 1 19990420 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND THE CABIN FLOOR TRACK CORRODED AT STA 200, LBL 22 INCHES. REMOVED CORRODED TRACK AND RE PLACED PER SPM 6-70-01, PAGE 2 ITEM 4 A AND 4B. 2 L 7 2 4F A6WE 1999043000207 19990430 00207 WP 1999 4 30 TWAA9906004 1 19990419 A 5320 DEPRESSOR DOUG DC9 DC931 3022065 WP CARDO DOORWAY DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND A CRACK FROM RIVET HOLE LOWER FWD CORNER OF AFT CARGO DOOR CUT OUT. REMOVED LOWER SECTI ON OF DEPRESSOR, LOCATED AND DRILLED NEW DEPRESSOR, SEALED AND INSTALLED PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999043000208 19990430 00208 NM 1999 4 30 TWAA9906005 1 19990419 A 5754 SKIN BOEING 767 767205 1385121 NM NR 4 LE SLAT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 THE TOP SURFACE OF NR 4 LE SLAT, AFT EDGE WEDGE, HAD A 2 IN CRACK WITH .125 IN HOLE APPROX 42 IN INBD AND 9 IN FROM TE. INSTALLED DOUBLER REPAIR PER 767 SRM 51-70-10, PAGE 20, AND SEALED EDGES. CHECK-C 2-10-99 LAX. 2 L 7 2 4F RT A1NM 1999043000209 19990430 00209 WP 1999 4 30 AT9900321 1 19990422 A 5320 50602283 THRESHOLD DOUG DC9 DC932 3022066 WP BS 370-420 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO COMPARTMENT THRESHOLD PAN AT BS 370-420 CORRODED ALONG EN TIRE LENGTH OF BOTTOM. REMOVE SLANT PANELS FORWARD AND AFT OF PIT DOOR, ALSO THE THRESHOLD PAN. TRIMMED NEW SPLICE DOU BLERS AND PAN SECTION, DRILLED, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 53-05 FIG 44, 51-30-1, AND MM 25-50-1. 2 L 7 2 4F A6WE 1999043000210 19990430 00210 WP 1999 4 30 AT9900322 1 19990422 A 5330 1A443811 SKIN DOUG DC9 DC932 3022066 WP BS 636 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FUSELAGE SKIN BULGING AT BS 636 BETWEEN L-29-30L. ACCESSED AREA FOR RE PAIR ON LEFT HAND CANTED AREA, FORMED INTERNAL DOUBLER, CUT, DRILLED, TRIMMED AND REINSTALLED ALL PARTS IAW DC9 53-01 FI G 1, AND MM 30-10-7. 2 L 7 2 4F A6WE 1999043000211 19990430 00211 WP 1999 4 30 AT9900323 1 19990408 A 5754 2914521 TEE DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A TEE CORRODED ON LEFT HAND INBOARD FLAP TRAILING EDGE ASSEMBLY. REMOVED T EE, LOCATED, FIT, TRIMMED, DRILLED, AND INSTALLED IAW DC9 SRM 51-10-2, 57-50-3, 51-10-4, AND 51-10-2. 2 L 7 2 4F A6WE 1999043000212 19990430 00212 WP 1999 4 30 AT9900324 1 19990425 A 3610 600300 SEAL DOUG DC9 DC932 3022066 WP TAILCONE DUCT WORN A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 866AT 47168 HI TEMPERATURE IN TAIL COMPARTMENT ANNUNCIATOR LIGHT AND MASTER CAUTION ILLUMINATED AFTER TAKEOFF. OVERWEIGHT LANDING A LSO OCCURED. REMOVED LEFT PNEUMATIC DUCT DOWNSTREAM OF ACM AND REPLACED TWO EACH FAULTY SEALS. LEAK AND OPERATIONAL CH ECK GOOD IAW MM 21-20. NO HI TEMPERATURE LIGHT NOTED. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION IAW MM 5-51-0 PG 601. NO DAMAGE NOTED IN ANY A ITEM INSPECTION. 2 L 7 2 4F A6WE 1999043000213 19990430 00213 WP 1999 4 30 AT9900325 1 19990316 A 2710 59137501 BRACKET DOUG DC9 DC932 3022066 WP LT AILERON CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LEFT HAND WING AILERON RUN AROUND CABLE PULLEY BRACKET CORRODED. REMOV ED AND REPLACED LEFT HAND AILERON BUS CABLE RUN AROUND PULLEY BRACKET IAW DC9 MM 27-10-0 AND 20-16-0. RIG AND OPERATION AL CHECK GOOD IAW DC9 MM 27-10-0. 2 L 7 2 4F A6WE 1999043000214 19990430 00214 WP 1999 4 30 AT9900326 1 19990316 A 5321 FLOOR DOUG DC9 DC932 3022066 WP LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION ON THE ATTACH ANGLE AND THE FLOOR BOARD BELOW FORWARD LAVATORY. M ECHANICALLY REMOVED CORROSION, REMOVED THRESHOLD AT FORWARD LAVATORY DOOR AND FLOOR TRIM TO GAIN ACCESS TO ATTACH ANGLE. FABRICATED REPAIR AND ANGLE, TREATED, COUNTERSUNK, DEBURRED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-30-7, 51-10- 3, 51-30-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999043000215 19990430 00215 WP 1999 4 30 AT9900327 1 19990317 A 5320 39559971 BRACKET DOUG DC9 DC932 3022066 WP NLG CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE NOSE LANDING GEAR PROXIMITY CABLE UPPER PULLEY BRACKET CORRODED. REMOV ED AND REPLACED NOSE LANDING GEAR GROUND PROXIMITY CABLES UPPER PULLEY BRACKET IAW DC9 MM 20-16-0, 20-17-0, 32-23-1 PG 2 07 10A THROUGH 10D AND RECONNECTED PROXIMITY CABLES, RIGGED/TENSION ALL OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1999043000216 19990430 00216 WP 1999 4 30 AT9900328 1 19990316 A 2760 59242741 BRACKET DOUG DC9 DC932 3022066 WP SPOILER SYST CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND PITTING CORROSION ON SPOILER MIX SUPPORT FRAME BRACKET ON LEFT WHEEL WELL. REMOVED AND REPLACED LEFT HAND WHEEL WELL SPOILER MIX SUPPORT FRAME BRACKET IAW DC9 SRM 51-10-3, MM 27-61-4, 27-10-0, 2 7-52-0, AND 27-61-0. 2 L 7 2 4F A6WE 1999043000217 19990430 00217 SO 1999 4 30 LR7A9916 1 19990412 A 5320 SUPPORT LKHEED 382 382G 526414U SO BS 657 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND FS 657 FLOOR SUPPORT UPPER CAP CORRODED AT BL 20R. REPAIRED BY FILLER AND REP AIR ANGLES IAW SPAR MPP L100-404-99-019, DWG R99-0002-10. LAC MEA 382-53-99-020. 2 H 7 4 4T A1SO 1999043000218 19990430 00218 SO 1999 4 30 LR7A9917 1 19990412 A 5531 WEB LKHEED 382 382G 526414U SO VERT STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND FS 1095 VERTICAL STABILIZER WEB CRACKED FROM VSS 9 TO 12. REPAIRED BY DOUBLER INSTALL IAW SPAR MPP L100-404-99-061, DWG R99-0002-08. LAC MEA 382-53-99-027. 2 H 7 4 4T A1SO 1999043000219 19990430 00219 SO 1999 4 30 LR7A9918 1 19990424 A 5320 NAS110511 BOLT LKHEED 382 382G 526414U SO BS 576.5 BROKEN A LR7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 403LC 4590 DURING CLIMB-OUT OF QPG MAX DIFFERENTIAL PRESSURE 7.0 IN HG AND AUDIBLE PRESSURE LEAK AT FS 577, RBL 61, APPROX WL 250. RETURNED TO QPG AND LANDED WITHOUT INCIDENT. FOUND 2 EA MLG VERTICAL BEAM ATTACHMENT BOLTS BROKEN AT FS 576.5, RBL 61, WL 256. ACCOMPLISHED LAC JOB CARD HST5315 MLG VERTICAL BEAM BOLT INSPECTION, NDT INSPECTION OF HOLES, CLEAN OUT AND BOL T REPLACEMENT PER LAC EDG88-2. 2 H 7 4 4T A1SO 1999043000220 19990430 00220 NM 1999 4 30 AWXA9900141 1 19990417 A 3350 S106 BATTERY PACK BOEING 737 7372A6 138448B NM R2 DOOR DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 IN MAINTENANCE, EMERGENCY LIGHTS DISCREPANCY, R2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTER Y PACK. OPS CK NORMAL. 2 L 7 2 4F A16WE 1999043000221 19990430 00221 NM 1999 4 30 AWXA9900142 1 19990417 A 2120 AIR DIST BOEING 737 737277 1384570 NM CABIN ODOR A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 188AW 22655 NORMAL OPS, ODOR IN CABIN DISCREPANCY: IN BOUND SMELL OF OIL IN CABIN, MID-CABIN TO AFT FROM RT PACT. CK'D RIGHT PACK F OR LEAKS, NO LEAKS FOUND. RAN PACKS AND NO SMELL NOTED AT THIS TIME. 2 L 7 2 4F RT A16WE 1999043000222 19990430 00222 NM 1999 4 30 AWXA9900143 1 19990417 A 2934 4006454 TRANSMITTER BOEING 737 737277 1384570 NM HYDRAULIC SYST MALFUNCTIONED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 180AW 22647 DIVERSION: HYDRAULIC QTY INDICATION DISCREPANCY: 'A' SYSTEM HYDRAULIC QUANITY WAS NORMAL DURING PREFLIGHT AND T/O, 3.5 G ALLONS. 'A' SYSTEM QUANITY DECREASED AFTER T/O TO 2.1 GALLONS AND THEN TO 1.4 DIVERTED TO LAS. SYSTEM RETURN TO 3.0 GA LLONS UPON LANDING. ALL OTHER INDICATIONS WERE NORMAL FOR BOTH SYSTEMS. REMOVED AND REPLACED 'A' SYSTEM HYDRAULIC QUAN ITY TRANSMITTER PER MM 29-33-1. FIRST ONE WAS BAD FROM STOCK. 2 L 7 2 4F RT A16WE 1999043000223 19990430 00223 WP 1999 4 30 CALA9900432 1 19990423 A 2560 AZ763 BATTERY DOUG DC10 DC1030 3023501 WP MEGAPHONES DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 49082 47927 FWD AND AFT MEGAPHONES HAVE BATTERY DISHARGED. REPLACED BATTERY AND PERFORMED CHECK PER MM 25-60-00. 2 L 7 3 4F A22WE 1999043000224 19990430 00224 WP 1999 4 30 CALA9900434 1 19990425 A 5350 4913353503 LATCH DOUG DC9 DC982 3022082 WP TAILCONE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 UPPER RIGHT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REPLACED LATCH PIN, RIGGED CABLES PER MM 53-33-00 AND TESTED TAIL CONE PER CARD 08-5350-1-0008. 2 L 7 2 4F A6WE 1999043000225 19990430 00225 WP 1999 4 30 CALA9900435 1 19990425 A 5350 4913353503 LATCH DOUG DC9 DC982 3022082 WP TAILCONE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 UPPER LEFT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REMOVED AND REPLACED LATCH. PERFORMED FUNCTIONAL TEST PER CARD 08-5350-1-0008. 2 L 7 2 4F A6WE 1999043000226 19990430 00226 WP 1999 4 30 CALA9900436 1 19990425 A 5350 3913359545 CABLE DOUG DC9 DC982 3022082 WP TAILCONE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 UPPER LEFT TAILCONE RELEASE CABLE WORN AND FRAYED WHERE IT PASSES OVER UPPER PULLY. REMOVED AND REPLACED PULLY PER MM 5 3-53-00. 2 L 7 2 4F A6WE 1999043000227 19990430 00227 WP 1999 4 30 CALA9900437 1 19990425 A 5350 59133509 PIPE DOUG DC9 DC982 3022082 WP TAILCONE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 TAIL CONE RELEASE CABLE GUIDE TUBE LOWER RIGHT HAS SEVERAL DAMAGED AREAS, DENTS, AND SHARP CREASES. REMOVED AND REPLACE D PIPE ASSY PER MM 53-50-00. 2 L 7 2 4F A6WE 1999043000228 19990430 00228 1999 4 30 CALA9900438 4 19990424 A 2565 35124389001 WIRE DOUG DC10 DC1030 3023501 WP R1&R3 DOOR DISCONNECTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 49082 47927 DOOR 1 AND 3 RT LOW PRESSURE LIGHT SLIDE BOTTLES DONT WORK. REINSTALLED TERMINALS WIRE LIGHT SLIDE ON DOOR 1 AND 3 RIGH T SIDE. PERFORMED TEST PER MM 25-60-00. 2 L 7 3 4F A22WE 1999043000229 19990430 00229 WP 1999 4 30 CALA9900439 1 19990424 A 5230 AGA72773 FRAME DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 49082 47927 AFT CARGO DOOR HAS INTERNAL STRUCTURE CRACKED. PERFORMED REPAIR PER EC/RA 5230-01461. 2 L 7 3 4F A22WE 1999043000230 19990430 00230 NM 1999 4 30 CALA9900440 1 19990423 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 907 - 930 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 CABIN RIGHT SIDE INBOARD SEAT TRACK HEAVY CORROSION BS 907 - BS 930. SPLICED IN NEW SEAT TRACK SECTION AT STA 827 - 947 PER SRM 5300-00-52 FIG 204. 2 L 7 2 4F RT A16WE 1999043000231 19990430 00231 WP 1999 4 30 CALA9900441 1 19990423 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 HI-SHEAR HOLE IS CRACKED (.25) IN FWD BAG BIN DOOR. FABRICATED AND INSTALLED STRAP PER EC/RA 5230-01462. 2 L 7 2 4F A6WE 1999043000232 19990430 00232 WP 1999 4 30 CALA9900443 1 19990426 A 3233 08323090001 ACTUATOR DOUG DC9 DC981 3022081 WP LT MLG LEAKING A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 37882 48027 WITH APU AIR ON AND PACKS ON, CABIN FILLS WITH SMOKE AND STRONG BURNING SMELL. FOUND LEFT GEAR RETRACT ACTUATOR IN TRAN SIT LEAK. REMOVED AND REPLACED ACTUATOR PER MM 32-32-02. PERFORMED BURN OUT OF PNEUMATIC DUCT PER MM 21-20-02. 2 L 7 2 4F A6WE 1999043000233 19990430 00233 WP 1999 4 30 9901579751 1 19990422 A 5754 TRACK DOUG DC9 DC941 302207N WP RT LE FLAP BROKEN A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 751NW 47115 SLAT DISAGREEMENT OCCURRED ON LANDING INTO MSP, CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AND AIRCRAFT LANDED WITHOU T INCIDENT USING FLAPS ONLY. MAINTENANCE FOUND CRACK IN NR 1 RIGHT SLAT DRIVE TRACK AND DAMAGE TO RETRACT CABLE. REPLA CED TRACK AND CABLE. ALSO, RIGGED ANTI-ICE T DUCT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999043000234 19990430 00234 WP 1999 4 30 9901589964 1 19990421 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999043000235 19990430 00235 WP 1999 4 30 9901599962 1 19990419 A 2120 AIR DIST DOUG DC9 DC931 3022065 WP CABIN ODOR A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 914RW 47362 FLIGHT ATTENDANT REPORTED SMOKE IN AFT CABIN AFTER TAKEOFF. SMOKE DETECTOR DID ACTIVATE. CREW DECLARED AN EMERGENCY AN D FLIGHT WAS RETURNED TO ATL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RAN AIR CONDITIONING PACKS TO FULL HOT AND NO SMOKE OR FUMES WERE APPARANT. IT IS SUSPECTED THAT SMOKE WAS CAUSED BY RESIDUAL ENGINE OIL. REPLACED LEFT AND RIGH T WATER SEPARATORS. LEAK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999043000236 19990430 00236 WP 1999 4 30 9901609951 1 19990416 A 3397 WIRE DOUG DC9 DC932 3022066 WP TAILCONE LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9347 45827 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAILCONE AND LIGHT ABOVE TAILCONE RELEASE HANDLE I NOPERATIVE. MAINTENANCE FOUND BAD CONNECTION AT BROWN DISARM WIRE AT SPLICE NEAR POWER SUPPLY. REPLACED WIRE. OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999043000237 19990430 00237 SO 1999 4 30 COMA9910065 1 19990422 A 5610 12018651001 BELLCRANK 1204159100 EMB 120 EMB120RT SO LT CABIN CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 19930 1600 120228 UPON REINSTALLATION OF THE PILOT'S DIRECT VISION WINDOW AFTER REPLACEMENT OF THE SEAL, FOUND AFT LOWER BELL CRANK TO BE CRACKED .25 INCH THROUGH WEB BY ROLLER. REMOVED AND REPLACED LOWER BELL CRANK AND RIGGED IAW EMB-120 MM CH 52-22-01. 2 L 7 2 4T RT A31SO 1999043000238 19990430 00238 SO 1999 4 30 COMA991066 1 19990422 A 2120 AIR DIST EMB 120 EMB120RT SO COCKPIT ODOR A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 269CA 120263 SMOKE IN COCKPIT AND CABIN, FOR APPROXIMATELY 20 SECONDS DURING LANDING APPROACH. INSPECTED AIRCRAFT COOLING AND RECIRC ULATION SYSTEM. NO DEFECTS FOUND. 2 L 7 2 4T RT A31SO 1999043000239 19990430 00239 SO 1999 4 30 COMA9910067 1 19990422 A 2750 3472001001 FCU EMB 120 EMB120RT SO E&E COMPT MALFUNCTIONED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 189CA 19481 120189 FLAP CONTROL FAULT. REPLACED THE FLAP CONTROL UNIT. 2 L 7 2 4T RT A31SO 1999043000240 19990430 00240 EA 1999 4 30 COMA9960167 1 19990422 A 5240 MECHANISM CNDAIR CL600 CL6002B19 EA SERVICE DOOR NOT LATCHED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 952CA 7092 LOUD NOISE IMMEDIATELY AFTER TAKEOFF. 02 SERVICE DOOR OPEN. CLOSED 02 SERVICE DOOR. 2 L 7 2 4F RT A21EA 1999043000241 19990430 00241 EA 1999 4 30 COMA9960168 1 19990423 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 729CA 1130 7265 FLAPS FAILED AT 8 DEGREES. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999043000242 19990430 00242 EA 1999 4 30 COMA9960169 1 19990423 A 5210 HANDLE CNDAIR CL600 CL6002B19 EA PAX DOOR NOT LATCHED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 929CA 7035 OUTER DOOR HANDLE MESSAGE AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999043000243 19990430 00243 EA 1999 4 30 COMA9960170 1 19990423 A 3411 PITOT SYST CNDAIR CL600 CL6002B19 EA FUSELAGE CONTAMINATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 710CA 7241 EFIS COMPARITOR MESSAGE. PURGED THE PITOT SYSTEM. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1999043000244 19990430 00244 EA 1999 4 30 COMA9960171 1 19990423 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA RT SPOILER MALFUNCTION A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 931CA 12511 7037 FLIGHT SPOILER FAULT MESSAGE. REPALCED FLIGHT SPOILER PCU. 2 L 7 2 4F RT A21EA 1999043000245 19990430 00245 EA 1999 4 30 COMA9960172 1 19990423 A 3230 864806 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 936CA 7377 7043 LANDING GEAR WILL NOT EXTEND. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1999043000246 19990430 00246 WP 1999 4 30 UPS99829381 1 19990406 A 5320 37544731 FITTING DOUG DC8 DC873F 302199F WP BS 380-400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123 STA 380-400 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000247 19990430 00247 WP 1999 4 30 UPS99829382 1 19990406 A 5320 464641631N FITTING DOUG DC8 DC873F 302199F WP BS 1220-1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123 STA 1220-1240 STR 4L SPLICE FITTING IS CRACKED. REMOVERD AND REPLACED FITTING IAW DWG 4646163 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000248 19990430 00248 WP 1999 4 30 UPS99829383 1 19990407 A 5320 46413241N FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123 STA 1690, THE AFT LONG 26R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000249 19990430 00249 WP 1999 4 30 UPS99829384 1 19990406 A 5320 375041501N FITTING DOUG DC8 DC873F 302199F WP BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123 STA 320 AT LONG 27L, THE FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 375041 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000250 19990430 00250 WP 1999 4 30 UPS99829385 1 19990407 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123 STA 1690, THE AFT LONG 30R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000251 19990430 00251 WP 1999 4 30 UPS99829386 1 19990407 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C123 AFT SIDE OF STA 1690, THE LONG 26L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 46 41324 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000252 19990430 00252 WP 1999 4 30 UPS99829388 1 19990405 A 5320 4611067N FITTING DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LONG 32L END FITTING AT FS 70 IS GOUGED AND CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000253 19990430 00253 WP 1999 4 30 UPS99829389 1 19990406 A 5320 3779659501 FITTING DOUG DC8 DC873F 302199F WP BS 902-920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LONG 4L END FITTING AT FS 902 TO 920 IS CRACKED. REMOVED AND REPLACED THE END FITING IAW SRM 51-1-20 D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000254 19990430 00254 WP 1999 4 30 UPS99829390 1 19990416 A 5532 SKIN DOUG DC8 DC873F 302199F WP VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 VERTICAL STAB L/E SKIN AT ZFS 30.5 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 1999043000255 19990430 00255 WP 1999 4 30 UPS99829391 1 19990406 A 5320 3754041501 FITTING DOUG DC8 DC873F 302199F WP BS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 300, ABOVE LONG 27L, THE FRAME FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1999043000256 19990430 00256 WP 1999 4 30 UPS99829392 1 19990403 A 5320 4641326N FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LONG 28L END FITTING IS CRACKED JUST FWD OF FS 1690. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D A ND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000257 19990430 00257 WP 1999 4 30 UPS99829393 1 19990408 A 5720 564125521 DOUBLER DOUG DC8 DC873F 302199F WP WS 598 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E AT XFS 598, THE LWR SKIN T/E DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND INSTALLED DOUBLER IAW DWG 5641255 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999043000258 19990430 00258 WP 1999 4 30 UPS99829394 1 19990406 A 5320 37540432 FITTING DOUG DC8 DC873F 302199F WP BS 1178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 1178 AT LONG 21R, THE FRAME TO CUSP TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000259 19990430 00259 WP 1999 4 30 UPS99829395 1 19990408 A 5720 975329423 CLIP DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING UPPER L/E RIB, ABOVE THE NR 2 PYLON STA XW 239, THE FWD ATTACH CLIP IS CRACKED. REMOVED, FAB RICATED, AND INSTALLED CLIP IAW DWG 9753294 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000260 19990430 00260 WP 1999 4 30 UPS99829396 1 19990407 A 5320 4641324502 FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 1690, THE AFT LONG 32R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000261 19990430 00261 WP 1999 4 30 UPS99829397 1 19990409 A 5720 37048411 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 INBD SIDE OF THE STA XRS 74 BULKHEAD, THE STRINGER 51 AFT END FITTING IS CRACKED. REMOVED AND REPLAC ED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000262 19990430 00262 WP 1999 4 30 UPS99829398 1 19990415 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 180 FLOORBEAM AT RBL 24 IS CORRODED OUT OF LIMITS. REPAIRED FLOORBEAM IAW DH SK840-665. 2 L 7 4 4F RT 4A25 1999043000263 19990430 00263 WP 1999 4 30 UPS99829399 1 19990406 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 260 SHEAR TIE BETWEEN LONG 32R AND 31R IS CRACKED. REPAIRED SHEAR TIE IAW SRM 53-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 1999043000264 19990430 00264 WP 1999 4 30 UPS99829400 1 19990415 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 100 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 100 FRAME AT LONG 20R HAS A HOLE DRILLED IN THE RADIUS. REPAIRED FRAME IAW DH SK840-071. 2 L 7 4 4F RT 4A25 1999043000265 19990430 00265 WP 1999 4 30 UPS99829401 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 484.895 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E RIB AT XS 484.895 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999043000266 19990430 00266 WP 1999 4 30 UPS99829402 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 435.789 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E RIB AT XS 435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999043000267 19990430 00267 WP 1999 4 30 UPS99829403 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 461.372 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E RIB AT XS 461.372 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999043000268 19990430 00268 WP 1999 4 30 UPS99829404 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 372.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E RIB AT XFS 372.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999043000269 19990430 00269 WP 1999 4 30 UPS99829405 1 19990404 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E LWR SKIN AT THE INBD AFT CORNER OF THE INBD SLOT IS CRACKED, STA XILD .7095. REPAIRED L/ E SKIN IAW EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 1999043000270 19990430 00270 WP 1999 4 30 UPS99829406 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 841.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 RT WING L/E RIB AT XFS 841.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999043000271 19990430 00271 WP 1999 4 30 UPS99829407 1 19990408 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 847.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E RIB AT XFS 847.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999043000272 19990430 00272 WP 1999 4 30 UPS99829408 1 19990411 A 5320 561561412 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 120-140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 120-140 AT LONG 14R, THE INTERCOSTAL UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL IAW DWG 5615614 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999043000273 19990430 00273 WP 1999 4 30 UPS99829409 1 19990408 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 761 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E SKIN AT XW 761 IS CORRODED BEYOND LIMITS. REPAIRED IAW EO DC8-5720-7767. 2 L 7 4 4F RT 4A25 1999043000274 19990430 00274 WP 1999 4 30 UPS99829410 1 19990424 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 WHILE PERFORMING EMERGENCY EXIT LIGHT TEST FOUND LIGHTS VERY DIM. REMOVED AND REPLACED BATT PACK. SYSTEM OPS CHECK GOO D PER MM 35-52-0. 2 L 7 4 4F RT 4A25 1999043000275 19990430 00275 WP 1999 4 30 UPS99829411 1 19990408 A 5320 46112841 FITTING DOUG DC8 DC873F 302199F WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LONG 1 END FITTING AT STA 70 IS CRACKED AND CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-1. 2 L 7 4 4F RT 4A25 1999043000276 19990430 00276 WP 1999 4 30 UPS99829412 1 19990408 A 5720 576964679 ANGLE DOUG DC8 DC873F 302199F WP WS 7.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING INBD L/E UPPER INBD AFT L/E ATTACH ANGLE IS CRACKED, STA XFS 7.5. REMOVED, FABRICATED, AND I NSTALLED ANGLE IAW DWG 5269646 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999043000277 19990430 00277 WP 1999 4 30 UPS99829413 1 19990404 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT WING L/E SKIN ABOVE THE NR 2 PYLON HAS A CRACKED REPAIR DOUBLER. REMOVED, FABRICATED REPAIR DOUBL ER IAW SRM 57-2-1A FIG 1. 2 L 7 4 4F RT 4A25 1999043000278 19990430 00278 WP 1999 4 30 UPS99829414 1 19990402 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1567 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK UPPER INBD FLANGE HAS HEAVY CORROSION UNDER THE DOME AT FS 1567, LBL 59. REMOV ED, FABRICATED, AND REPLACED THE SEAT TRACK, FS 1550-1667 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999043000279 19990430 00279 WP 1999 4 30 UPS99829415 1 19990403 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1560-1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK INBD FLANGE HAS HEAVY CORROSION, FS 1560-1580, RBL 59. CUT OUT DAMAGE SECTION OF SEAT TRACK FS 1560-1600 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999043000280 19990430 00280 WP 1999 4 30 UPS99829416 1 19990407 A 5320 37739061 FITTING DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 MAIN CABIN AREA, FS 781, LBL 24, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FIT TING IAW SRM 51-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000281 19990430 00281 WP 1999 4 30 UPS99829417 1 19990407 A 5320 3755843501 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 1220 AT 34R, THE BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING SRM 53-2 -0 FIG 2D. 2 L 7 4 4F RT 4A25 1999043000282 19990430 00282 WP 1999 4 30 UPS99829418 1 19990415 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 847.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 RT WING L/E RIB AT XFS 847.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999043000283 19990430 00283 WP 1999 4 30 UPS99829419 1 19990408 A 5320 37739061 FITTING DOUG DC8 DC873F 302199F WP BS 742 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 MAIN CABIN, FS 742 AT RBL 24, THE SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED THE FI TTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999043000284 19990430 00284 EU 1999 4 30 QXEA9900638 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16060 BETWEEN STRINGERS 42 AND 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000285 19990430 00285 EU 1999 4 30 QXEA9900639 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16060 BETWEEN STRINGERS 33 AND 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 3. 2 L 7 2 4F RT A20EU 1999043000286 19990430 00286 EU 1999 4 30 QXEA9900640 1 19990326 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16060 BETWEEN STRINGERS 32 AND 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000287 19990430 00287 EU 1999 4 30 QXEA9900641 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16060 BETWEEN STRINGERS 26 AND 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000288 19990430 00288 EU 1999 4 30 QXEA9900642 1 19990326 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16660 BETWEEN STRINGERS 49 AND 50. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000289 19990430 00289 EU 1999 4 30 QXEA9900643 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16660 BETWEEN STRINGERS 35 AND 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000290 19990430 00290 EU 1999 4 30 QXEA9900644 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16660 BETWEEN STRINGERS 34 AND 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000291 19990430 00291 EU 1999 4 30 QXEA9900645 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16660 BETWEEN STRINGERS 32 AND 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000292 19990430 00292 EU 1999 4 30 QXEA9900646 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP AT FRAME 16660 BETWEEN STRINGERS 30 AND 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000293 19990430 00293 EU 1999 4 30 QXEA9900647 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP AT FRAME 16660 BETWEEN STRINGERS 29 AND 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000294 19990430 00294 EU 1999 4 30 QXEA9900648 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP AT FRAME 16660 BETWEEN STRINGERS 25 AND 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043000295 19990430 00295 EU 1999 4 30 QXEA9900649 1 19990318 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 3450 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT FORWARD FUSELAGE FRAME 3450 CRACKED AT FRAME/SKIN JOINT, APPROXIMATELY 7 LONG BETWEEN STRINGERS 51 AND 52. R EPAIRED IAW FOKKER SRM 53-02-12, PAGE 14, FIGURE 6. 2 L 7 2 4F RT A20EU 1999043000296 19990430 00296 EU 1999 4 30 QXEA9900650 1 19990329 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - AFT CARGO BAY FRAME 13815A CASTELLATION IS CRACKED THROUGH 2 RIVET HOLES BETWEEN STRINGERS 72 AND 73. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000297 19990430 00297 EU 1999 4 30 QXEA9900651 1 19990330 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - AFT CARGO BAY FRAME 13815A CASTELLATION HAS CORROSION AT RIVET HOLE AND EDGE OF CLIP AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 4C, STEP 1. 2 L 7 2 4F RT A20EU 1999043000298 19990430 00298 EU 1999 4 30 QXEA9900652 1 19990405 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 13815A CLIP BETWEEN STRINGER 1 AND 2 HAS CORROSION AND CRACK AROUND OUTBOARD RIVET. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000299 19990430 00299 EU 1999 4 30 QXEA9900653 1 19990412 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 5305 HAS CORROSION UNDER NUT PLATE AT STRINGER 1. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-53-7 48. 2 L 7 2 4F RT A20EU 1999043000300 19990430 00300 EU 1999 4 30 QXEA9900654 1 19990412 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 5305 HAS CORROSION UNDER NUT PLATE AT STRINGER 3. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-53-7 48. 2 L 7 2 4F RT A20EU 1999043000301 19990430 00301 EU 1999 4 30 QXEA9900655 1 19990322 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 15205 BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - U CHANNEL FRAME SUPPORT FLAT AND BENT IN NUMEROUS PLACES AT FRAME 15205. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000302 19990430 00302 EU 1999 4 30 QXEA9900656 1 19990406 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FORWARD CARGO BAY CENTER DOOR HAS A DEEP DENT ON INNER SKIN, NEXT TO AFT LATCH HOOK ASSEMBLY. REPAIRED IAW FOKKER SRM 52-02-01, FIGURE 1 AND HORIZON AIR EA 4-52-209. 2 L 7 2 4F RT A20EU 1999043000303 19990430 00303 EU 1999 4 30 QXEA9900657 1 19990317 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CRACK AT FRAME SUPPORT, FRAME 16660 BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1999043000304 19990430 00304 EU 1999 4 30 QXEA9900658 1 19990317 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CRACK AT FRAME SUPPORT, FRAME 16660 BETWEEN STRINGERS 4 AND 5. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1999043000305 19990430 00305 EU 1999 4 30 QXEA9900659 1 19990317 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CRACK IN FRAME SUPPORT, FRAME 15205 BETWEEN STRINGERS 5 AND 6. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1999043000306 19990430 00306 EU 1999 4 30 QXEA9900660 1 19990320 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION ON TOP OF AND UNDER NUT PLATES FOR FLOOR 4 WAY SUPPORT, FRAME 13815BM STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-726. 2 L 7 2 4F RT A20EU 1999043000307 19990430 00307 EU 1999 4 30 QXEA9900661 1 19990319 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION ON FRAME WHERE 2 NUT PLATES ARE ATTACHED, FRAME 13815B, ABOVE STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-726. 2 L 7 2 4F RT A20EU 1999043000308 19990430 00308 EU 1999 4 30 QXEA9900662 1 19990317 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - 2 CRACKS IN FRAME SUPPORT, FRAME 13815B, BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIG URE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000309 19990430 00309 EU 1999 4 30 QXEA9900852 1 19990422 A 2530 CONECTOR FOKKER F28 F28MK4000 4990810 EU GALLEY FAILED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 488US 11240 GEG - CREW UNABLE TO REMOVE UPPER COFFEE POT, ELECTRIC SMELL NOTED. MAINTENANCE TROUBLESHOT ELECTRIC SMELL TO LOWER JUG . REMOVED AND REPLACED THE LOWER JUG. COLLARD UPPER JUG CIRCUIT BREAKERS, PLACED ON MEL. PDX MAINTENANCE REMOVED AND REPLACED THE UPPER JUG, CLEARED THE MEL. LATER THE SAME DAY ACRID SMELL NOTED COMING FROM NR 1 AND NR 2 COFFEE POTS, TU RNED BOTH POTS OFF. MAINTENANCE INSPECTED AND FOUND THE LOWER COFFEE JUG TO BE CAUSING THE SMELL. PLACED ON MEL. ON 9 90424 MAINTENANCE CLEARED THE MEL BY REPLACING THE FEMALE (AIRFRAME) CONNECTOR. 2 L 7 2 4F RT A20EU 1999043000310 19990430 00310 EU 1999 4 30 QXEA9900853 1 19990425 A 2611 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAV MALFUNCTIONED A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 486US 11237 SEA - LAV SMOKE DETECTOR SOUNDS INTERMITTENT ALARMS. MAINTENANCE PLACED ON MEL. REMOVED AND REPLACED SMOKE DETECTOR IN LAVATORY, OPERATIONAL CHECK NORMAL. CLEARED MEL. 2 L 7 2 4F RT A20EU 1999043000311 19990430 00311 NM 1999 4 30 99FDEA00158 1 19990423 A 3610 DUCT BOEING 727 727233 138408A NM LOWER AFT BODY LEAKED A FDEA H DEACTIVATE SYST/CIRCUITS J M WARNING INDICATION OVER TEMP CR CRUISE 1 SO 25 258FE 20940 99-95 - LWR AFT BODY OVERHEAT. STEP 19 IND BLD AIR LEAK IS BETWEEN BLEED VALVE AND PACK VALVE. ENG RUN ON NR 1, 2 AND 3 ENG NO FAULTS PER MM 24-14-1 PG 204CK. INSULATION RESISTANCE ABOVE LOOPS FND IN LIMITS. CTR CONDUCTOR LOOPS M322, M3 65, M767, M367 FND IN LIMITS. 2 L 7 3 4F RT A3WE 1999043000312 19990430 00312 NM 1999 4 30 99FDEA00159 1 19990423 A 2613 OVERHEAT LIGHT BOEING 727 727233 138408A NM LWR AFT BODY ILLUMINATED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 270FE 22035 LWR AFT BODY OVERHEAT LIGHT CAME ON. AT STEP 13 THE LIGHT WENT OUT. RESTORED NR 1 THRUST LEVER. *S/D* REMOVED AND RE PLACED D1086 REF WIRING DIAG MM 26-14-1. 2 L 7 3 4F RT A3WE 1999043000313 19990430 00313 NE 1999 4 30 99FDEA00160 2 19990427 A 7200 ENGINE BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 2 FAILED A FDEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 508FE 18279 OIL TEMP ON NR 2 ENG WAS NOTICED TO BE 120 DEG AND CLIMBING. EXECUTED RED TABS, OIL TEMP RED LINED AT 165 DEG SECURED E NG IAW RED TABS. DUMPED FUEL TO LAND. *S/D* REMOVED AND REPLACED NR 2 ENG IAW WORK CARD 70T0502, LEAK CHECK GOOD. RA N ENG, ALL INDICATIONS ARE NORM. 2 L 7 3 4F 4 F A3WE E2EA 1999043000314 19990430 00314 NM 1999 4 30 99FDEA00161 1 19990426 A 5730 ARB126824 ACCESS DOOR DOUG MD11 MD11F 3023600 NM R7 WING DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 604FE 48460 RT WING LEAD EDGE, SLAT DRIVE MECH ACCESS DOOR OPEN DURING AC TEST FLT CAUSING DAMAGE TO THE DOOR, SLAT NR 3 RT AND THE WING LEAD EDGE ADJACENT TO SLAT NR 3. REMOVED AND REPLACED SLAT DRIVE MECH PER MM 20-50-02-2. SKIN REPAIRED PER 57-10- 00, RIB REPAIR STA 526.18 PER 57-00-01. 2 L 7 3 4F RT A22WE 1999043000315 19990430 00315 WP 1999 4 30 ABXA9900316 1 19990320 A 5320 5755095401 ANGLE DOUG DOUG DC8 DC863 302198A WP BS 220 CRACKED A ABXA K NONE C F.O.D. IN INSP/MAINT 1 GL 23 813AX 46136 STATION 220 , LONGERON 31 RIGHT, FLOOR PANEL SUPPORT ANGLE CRACKED. REPAIRED ANGLE IAW REA D853-24965 AND DC8 SRM 51-1- 20. 2 L 7 4 4F 4A25 1999043000316 19990430 00316 WP 1999 4 30 ABXA9900317 1 19990318 A 5730 5769545508 SKIN DOUG DOUG DC8 DC863 302198A WP WS 890 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 RIGHT WING STATION 890.000, CRACK IS EMINATING FROM SCREW COUNTERSINK. REPAIRED IAW DC8 SRM 51-1-26. 2 L 7 4 4F 4A25 1999043000317 19990430 00317 WP 1999 4 30 ABXA9900318 1 19990419 A 5313 59114279 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 980. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999043000318 19990430 00318 WP 1999 4 30 ABXA9900319 1 19990419 A 5313 59114279 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 980. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999043000319 19990430 00319 WP 1999 4 30 ABXA9900320 1 19990419 A 5412 991550034 RIB DOUG DC9 DC931 3022065 WP WS 1038-1048 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND RIB UNDER PANEL AT TOP OF NR 2 PYLON, STATION 1038-1048 CRACKED. REPAIRED RIB IAW DC9 SRM 54-01. 2 L 7 2 4F A6WE 1999043000320 19990430 00320 WP 1999 4 30 MWEA99219 1 19990407 A 5320 4616493 SUPPORT DOUG DC9 DC914 3022034 WP BS 718 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FLOOR SUPPORT CORRODED AT FS 718 LBL 00 TO LBL 22. FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 1999043000321 19990430 00321 WP 1999 4 30 MWEA99220 1 19990407 A 5313 27779485 LONGERON DOUG DC9 DC914 3022034 WP BS 718-758 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON 29R AT FS 718 TO FS 758 IS CORRODED. FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 1999043000322 19990430 00322 WP 1999 4 30 MWEA99221 1 19990330 A 5320 591015891 FRAME DOUG DC9 DC914 3022034 WP CARGO DOORWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT CARGO COMPARTMENT DOOR FRAME HAS CORROSION AT FS 718 TO FS 758. INSTALLED NEW WEB. 2 L 7 2 4F A6WE 1999043000323 19990430 00323 WP 1999 4 30 MWEA99222 1 19990330 A 5320 1109618 SHEAR TIE DOUG DC9 DC914 3022034 WP BS 817 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT CARGO COMPARTMENT FS 817 SHEAR TIE IS CRACKED. FABRICATED AND INSTALLED SHEAR TIE CLIPS AND SPLICE PLATE. 2 L 7 2 4F A6WE 1999043000324 19990430 00324 WP 1999 4 30 MWEA99223 1 19990331 A 5720 4911462 CLIP DOUG DC9 DC914 3022034 WP WS 137 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 RIGHT WING TANK LOWER SHEAR CLIP STR 11 AND REAR SPAR IS CORRODED STA XRS 137. FABRICATED AND INSTALLED REPAIR CLIP. 2 L 7 2 4F A6WE 1999043000325 19990430 00325 WP 1999 4 30 MWEA99224 1 19990407 A 5311 27779305 FRAME DOUG DC9 DC914 3022034 WP BS 294 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FRAME CORRODED AT FS 294 L28L TO L28R. INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 1999043000326 19990430 00326 WP 1999 4 30 MWEA99225 1 19990407 A 5320 29129015 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 285 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 INTERCOSTAL CORRODED AT FS 285 L29R. FABRICATED AND INSTALLED REPAIR INTERCOSTAL. 2 L 7 2 4F A6WE 1999043000327 19990430 00327 WP 1999 4 30 MWEA99226 1 19990407 A 5320 5910668 BRACKET DOUG DC9 DC914 3022034 WP BS 313 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 L BRACKET CORRODED AT FS 313 L25R. FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 1999043000328 19990430 00328 WP 1999 4 30 MWEA99227 1 19990407 A 5510 5910401503 LUG DOUG DC9 DC914 3022034 WP LT HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT HORIZONTAL STABILIZER ATTACH LUG IS CORRODED. REPAIRED BY BORING LUG HOLE. 2 L 7 2 4F A6WE 1999043000329 19990430 00329 WP 1999 4 30 MWEA99228 1 19990331 A 5320 591060641 FITTING DOUG DC9 DC914 3022034 WP BS 484 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON 28R END FITTING AT FS 484 IS CORRODED. DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999043000330 19990430 00330 WP 1999 4 30 MWEA99229 1 19990331 A 5320 591060641 FITTING DOUG DC9 DC914 3022034 WP BS 484 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON 29R END FITTING AT FS 484 HAS CORROSION ON LOWER SURFACE. DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999043000331 19990430 00331 WP 1999 4 30 MWEA99230 1 19990331 A 5320 3916174501 FITTING DOUG DC9 DC914 3022034 WP BS 484 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON 29L END FITTING FS 484 HAS CORROSION. DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999043000332 19990430 00332 WP 1999 4 30 MWEA99231 1 19990407 A 5320 5916064IN FLANGE DOUG DC9 DC914 3022034 WP BS 464 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 VERTICAL FLANGE IS CRACKED AT FS 464 L30. INSTALLED NEW PART. 2 L 7 2 4F A6WE 1999043000333 19990430 00333 WP 1999 4 30 MWEA99232 1 19990331 A 5320 59106064A FITTING DOUG DC9 DC914 3022034 WP BS 490 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON END CAP FS 490 L 26 RIGHT IS CRACKED AND CORRODED. DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999043000334 19990430 00334 WP 1999 4 30 MWEA99233 1 19990331 A 5320 59160641 FITTING DOUG DC9 DC914 3022034 WP BS 490 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON END CAP FS 490 L28 LT IS CRACKED AND CORRODED. DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999043000335 19990430 00335 WP 1999 4 30 MWEA99234 1 19990331 A 5320 591060641 FITTING DOUG DC9 DC914 3022034 WP BS 490 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FUSELAGE STATION 490 L27R END FITTING IS CORRODED AND PITTED. DRILLED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999043000336 19990430 00336 NM 1999 4 30 DLM11990868 1 19990420 A 3320 1691 BULB DOUG MD11 MD11 3023602 NM ROW 38B FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 OVERHEAD READING LIGHT AT SEAT 38B SHORTED OUT. WHEN BULB REPLACED, IT BEGAN TO PRODUCE SMOKE. LIGHTS TURNED OFF FOR R EMAINDER OF FLT. REPLACED BULB. 2 L 7 3 4F RT A22WE 1999043000337 19990430 00337 1999 4 30 DL73K990875 4 19990422 A 2350 63999004 MICROPHONE BOEING 737 737232 1384475 NM LT COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 315DL 23087 DURING CLIMB-OUT, LOST ALL RADIOS, BOTH TRANSMIT AND RECIEVE FOR ABOUT 2 MIN, THEN THEY CAME BACK ON, THEN WENT OUT AGAI N. REPEATED THIS CYCLE ABOUT 4 TIMES. RETURNED TO MCO. ALL RADIOS OPERATE NORMAL AT GATE. CAPT SUSPECT CAPT HANDMIC. REPLACED SAME. REPLACED NR 1 VHF TRANCEIVER AND NR 2 AUDIO SELECT PANEL AS PRECAUTION. ALL RADIOS CK OK. PART NR HA ND MIC- 63999-004 SERIAL NR 9206, TRANSCIEVER 064-1005-02 SERIAL NR 3960, AUDIO SEL PNL G6560 SERIAL NR 34. 2 L 7 2 4F RT A16WE 1999043000338 19990430 00338 NM 1999 4 30 DLM88990879 1 19990423 A 3340 6011779 BATTERY PACK DOUG MD88 MD88 3023688 NM EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 913DE 49956 OVERWING EMERGENCY LIGHTS INOP. REPLACED OVERWING BATTERY PACK, OPS CKD GOOD. 2 L 7 2 4F RT A6WE 1999043000339 19990430 00339 NM 1999 4 30 DL757990880 1 19990423 A 2133 OUTFLOW VALVE 60683221 BOEING 757 757232 1384965 NM CABIN MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 620DL 34226 22910 AFTER TAKEOFF, CABIN AUTO INOP EICAS MSG AND AUTO INOP ON PRESS PANEL. OK IN MANUAL. BITE CK ON NR 1 CONT FAULTS CONT AND BITE CK ON NR 2 CONT FAULTS NR 2 AC MOTOR. REPLACED NR 1 CONT AND OUTFLOW VALVE ASSY. 2 L 7 2 4F RT A2NM 1999043000340 19990430 00340 NM 1999 4 30 DL757990882 1 19990420 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM BS 610-630 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 665DN 25013 FUSELAGE SKIN FS 610-630, STRG 17L-18L, SKIN PUNCTURE REPAIR. THE FUSELAGE SKIN BETWEEN FS 610 AND 630 AND BETWEEN STRI NGER 17L AND 18L WAS CRACKED/PUNCTURED BY A JETWAY. THE DAMAGE WAS CUTOUT OF THE SKIN WITH A 19 BY 4 CUTOUT. THE CU TOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B757 SRM 53-00-01, FIG 204 AND DOCUMENTED PER ER/A 367215-14, RE V A. 2 L 7 2 4F RT A2NM 1999043000341 19990430 00341 NM 1999 4 30 DL72S990883 1 19990420 A 5320 FRAME BOEING 727 727232 1384082 NM CARGO DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 FUSELAGE FRAME C1 DOOR CUTOUT AFT FRAME WEB, CRACK REPAIR. THE AFT FRAME OF THE C1 DOOR CUTOUT WAS FOUND WITH A 1.5 CRA CK IN THE FRAME WEB JUST INBD OF THE DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A TITANIU M REPAIR DOUBLER PER ER/A 367224-14. 2 L 7 3 4F A3WE 1999043000342 19990430 00342 NM 1999 4 30 DL72W990884 1 19990423 A 5320 ANGLE BOEING 727 727247 138408F NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 TORQUE BOX HORIZONTAL Z ANGLE CRACKED AT STA 1273. TORQUE BOX HORIZONTAL ANGLE FWD SIDE OF Z ANGLE CRACKED AT STA 1273. REPLACED PARTS PER SRM 53-10-10. 2 L 7 3 4F A3WE 1999043000343 19990430 00343 NM 1999 4 30 DL757990885 1 19990423 A 3810 24E50704G04 WATER HEATER 24E507040G04 BOEING 757 757232 1384965 NM LAVATORY INOP A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 660DL 249 24422 FLT ATTENDANT CALLED AFTER T/O BNA AND REPORTED SMOKE SMELL IN AFTCABIN. FLT CREW REPORTED SMELL DISIPATED BEFORE LAND ING. CONTRACT MTC CHECKED AFT GALLEY COFFEE MAKERS AND OVENS, NO TROUBLE FOUND. FOUND RT AFT LAV WATER HEATER INOP. R EPLACED SAME. 2 L 7 2 4F RT A2NM 1999043000344 19990430 00344 NM 1999 4 30 DL757990886 1 19990424 A 2530 OVEN 831610403M0 BOEING 757 757232 1384965 NM GALLEY SMOKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 615DL 51 22822 FLT ATTENDANT REPORTED SMOKE IN MID GALLEY AREA, MADE EMERGENCY LANDING BOS. INSPECTED AIRCRAFT, PERFORMED PWR RUN. PR ESSURIZED AIRCRAFT, FOUND MID GALLEY FWD OVEN SMOKING. REPLACED SAME. 2 L 7 2 4F RT A2NM 1999043000345 19990430 00345 NM 1999 4 30 DL73E990887 1 19990424 A 2751 INDICATION 2061141 BOEING 737 737247 138448D NM TE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 374DL 1253 23521 IRR FLAPS WOULD NOT EXTEND WHEN FLAP HANDLE WAS PUT IN THE 1 POSITION. FOUND FLAP INDICATOR WITH SPLIT NEEDLE INDICATIO N ON ARRIVAL. TROUBLESHOT IN ACCORDANCE WITH M/M. REPLACED AND TESTED FLAP INDICATOR IN ACCORDANCE WITH M/M. I NSPECTED AND LUBED FLAP JACKSCREWS, CYCLED FLAPS. OP CK OK IN ACCORDANCE WITH M/M. 2 L 7 2 4F A16WE 1999043000346 19990430 00346 NM 1999 4 30 DL76L990889 1 19990424 A 3350 BATTERY 20131A BOEING 767 767332 1382001 NM RT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 197DN 32438 28454 DURING OW2 CHECK, SLIDE/SPOILER SQUIB TEST FAILED. FOUND VOLTAGE OF RIGHT ESCAPE BATTERY LOW. REPLACED BATTERY AND PER FORMED GOOD TEST OF SQUIBS. 2 L 7 2 4F RT A1NM 1999043000347 19990430 00347 NM 1999 4 30 DL72W990893 1 19990425 A 3350 POWER SUPPLY RPS1 BOEING 727 727247 138408F NM ROW 26 INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 295WA 3629 22532 AFT ZONE OF EMERGENCY LIGHTS AFT OF SEAT 26 INOP. DURING SVC CK TEST, REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 1999043000348 19990430 00348 WP 1999 4 30 DLL19990894 1 19990423 A 2450 CONTACTOR 50087007 LKHEED 1011 10113853 5265020 WP E&E COMPT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 760DH 383 193Y1194 SMOKE AND ELECTICAL SMELL IN FWD E/E. REPLACED NR 1 BTB SYS CKS OK. 2 L 7 3 4F A23WE 1999043000349 19990430 00349 NM 1999 4 30 DL72S990895 1 19990423 A 5755 65192709 BEAM BOEING 727 727225A 1384077 NM SPOILER CORRODED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 AD 90-07-05 AND 90-06-09, NR 4 INB'D FLAP TRACK, TYP CORROSION AT MLG BEAM AND SPOILER BEAM ATTACH PADS. DURING OVERHAU L OF FLAP TRACK, CORROSION WAS FOUND AT THE MLG BEAM AND SPOILER BEAM ATTACH PADS AND BOLT HOLES. THE PADS WERE MACHINE D AND THE HOLES OVERSIZED TO REMOVE THE CORROSION. THE MLG BEAM ATTACH HOLES WERE LEFT AS-IS. THE SPOILER BEAM ATTA CH HOLES WERE BUSHED. 2 L 7 3 4F RT A3WE 1999043000350 19990430 00350 NM 1999 4 30 VNAA9904005 1 19990419 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 9A DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 437JS 5003 895 3055 DURING THE POST FLIGHT INSPECTION, THE EMERGENCY LIGHTS AT SEAT 9A WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT POSITION 7LK. OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999043000351 19990430 00351 NM 1999 4 30 AALA990363 1 19990303 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION ON SKIN AROUND ICE LIGHT STRINGER 14R-17R STATION 720B-C. INSTALLED DOUBLER AT RIGHT ICE LIGHT CU TOUT PER SRM 53-30-3 PAGE 137-140 FIG 22 AND ECO 11697, DATED 3/3/99. (M) 2 L 7 3 4F A3WE 1999043000352 19990430 00352 NM 1999 4 30 AALA990364 1 19990225 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1060-1067 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND SKIN CORRODED ON EXTERIOR OF AIRCRAFT FROM STATION 1060 TO 1067 AT STRINGER 28L. CUTOUT DAMAGED SKIN. REPA IRED WITH DOUBLER PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1999043000353 19990430 00353 NM 1999 4 30 AALA990365 1 19990226 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK STATION 480 INBOARD, OUTBOARD LEGS AT FASTENER HOLES. REMOVED CORROD ED SECTION OF SEAT TRACK. SPLICED IN NEW SECTION PER SRM 53-10-5 FROM STATION 480-560 RIGHT. (M) 2 L 7 3 4F A3WE 1999043000354 19990430 00354 NM 1999 4 30 AALA990366 1 19990227 A 5311 FRAME BOEING 727 727223 1384074 NM BS 420 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STATION 420 FRAME CRACKED AT STRINGER 10L. REPAIRED DAMAGED FRAME STATION 420 STRINGER 10L WITH DOUBLER AS PER SRM 53-10-4 PAGE 3-6 FIG 1 SHEET 4. INSTALLED DOUBLER ONE GAUGE HEAVIER THAN ORIGINAL AND USED HI-LOCK .15625 DIAME TER. (M) 2 L 7 3 4F A3WE 1999043000355 19990430 00355 NM 1999 4 30 AALA990367 1 19990223 A 5315 BOEING 727 727223 1384074 NM UNKNOWN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STATION 344 LBL 30 TOP FLANGE OF FLOORBEAM CRACKED AT FASTENER HOLE. CUT OUT DAMAGED SECTION OF TOP FLANGE. INSTALLED DOUBLER REPAIR PER SRM 53-10-8 FIG 9 SHEETS 1-5. (M) 2 L 7 3 4F A3WE 1999043000356 19990430 00356 NM 1999 4 30 AALA990368 1 19990306 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - TOP OF BELL FRAME GOUGED (FROM TOO LONG OF FAST), BELL FRAME STATION 1130 BELOW RT TIEDOWN FIITTING. CUT OUT DAMA GED AREA, INSTALLED DOUBLER PER AARD 3-10-07-3 DOUBLER 7075-T6 .063 THICK BY 9.5 INCH LONG, 16 BACB30FP8 AND 17 BACB30FP L HI-LOCKS, 2 ROWS IN WEB AND 1 ROW ON TOP. (M) 2 L 7 3 4F A3WE 1999043000357 19990430 00357 NM 1999 4 30 AALA990369 1 19990311 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND UPPER FLANGE OF BELLFRAME 990 DENTED ABOVE STRINGER 26L. INSTALLED DOUBLER PER AARD 53-10-07-3. (M) 2 L 7 3 4F A3WE 1999043000358 19990430 00358 NM 1999 4 30 AALA990370 1 19990223 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND TOP OF BELL FRAME DENTED AT STAITON 950F 5 INCHES ABOVE STRINGER 26L. CUTOUT DAMAGED AREA, DUE CHECKED, FAB RICATED DOUBLER, AND INSTALLED PER SRM 53-10-4 PAGE 4 FIG 1. (M) 2 L 7 3 4F A3WE 1999043000359 19990430 00359 NM 1999 4 30 AALA990371 1 19990303 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION ON 720E FRAME, FORWARD SIDE, FROM STRINGER 7L TO STRINGER 4L, 7 SPOTS (MARKED). REMOVED CORROSION AND INSTALLED FRAME REPAIRS AT STRINGER 4L, 5L, 6L, PER SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 1999043000360 19990430 00360 NM 1999 4 30 AALA990372 1 19990308 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND BELT FRAME 1130 SHEAR TIE CORRODED AFT SIDE OF BELT FRAME JUST OUTBOARD OF STRINGER 28R. REMOVED AND REPLAC ED SHEAR TIE STATION 1130 AFT SIDE OF BELT FRAME JUST OUTBOARD OF STRINGER 28R ACCORDING TO SRM 53-10-2 PAGE 28, SEALED PER SRM 51-20-40. (M) 2 L 7 3 4F A3WE 1999043000361 19990430 00361 NM 1999 4 30 AALA990373 1 19990308 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND SHEAR TIE CORRODED AT 1166 BELL FRAME STRINGER 29R AND STRINGER 30. REMOVED CORRODED SHEAR TIE, INSTALLED N EW SHEAR TIE. (M) 2 L 7 3 4F A3WE 1999043000362 19990430 00362 NM 1999 4 30 AALA990374 1 19990302 A 5320 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER FRAME WEB CORRODED STATION 560, STRINGER 26R. INSTALLED DOUBLER ON WEB PER SRM 51-40-2, DOUBLER 5.5 BY 4.25 INCH, 3 ROWS FASTENERS BACB3OMC8-6 W/BACC30M8 COLLARS MATERIAL 2024T3 .080. ( M) 2 L 7 3 4F A3WE 1999043000363 19990430 00363 NM 1999 4 30 AALA990375 1 19990227 A 5320 WEB BOEING 727 727223 1384074 NM BS 1213 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION AND CRACKS ON UPPE RLOWER SIDE ANGLES AND WEB OF TAIL SKID ACT MOUNT RIB STATION 1213 LBL 18 TO RB L 18, LBL 30 TO RBL 30. REMOVED AND INSTALLED NEW ANGLES AND WEB PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999043000364 19990430 00364 NM 1999 4 30 AALA990376 1 19990222 A 5744 CASTING BOEING 727 727223 1384074 NM WS 385 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - INBOARD AILERON QUAD MOUNT CASTING CORRODED ON CASTING AND AROUND BEARING BORES. REMOVED AND REPLACED CORRODED CA STING PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1999043000365 19990430 00365 NM 1999 4 30 AALA990377 1 19990308 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - TOP SECTION OF BELL FRAME DENTED 4 PLACES FS 1050 STRINGER 25R TO 27R. REMOVED DAMAGE, INSTALLED .063 7075T6 DOUB LER WITH 15 MS20470-D-8 RIVETS, 10MS20470-D-6 RIVETS, 10 BACR15CE-6 RIVETS, 1BACB30FP6 HI-LOCKS, 1BACB30FP6 HI-LOCKS PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999043000366 19990430 00366 NM 1999 4 30 AALA990378 1 19990301 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1090 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - TOP OF BELT FRAME HAS 2 EACH WORN SPOTS ABOVE STRINGER 27L FROM FASTENER PROTRUSION AT CARGO TIEDOWN CASTING, STAT ION 1090 AND 27L STRINGER. INSTALLED DOUBLER .071 INCH WITH 19 EACH .25 INCH HI-LOCKS PER SRM 51-40-3 PAGE 3 AND 9 .187 5 INCH HI-LOCKS. THE DOUBLER IS 8.5 INCH BY 4 INCH, NO CUTOUT OF MATERIAL, JUST WEAR. (M) 2 L 7 3 4F A3WE 1999043000367 19990430 00367 NM 1999 4 30 AALA990379 1 19990306 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 BUCKLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - BELL FRAME STATION 1110 BENT, WEB AREA BUCKLED ABOVE STRINGER 26L ITEM 2 TOP OF BELL FRAME STATION 1110 GOUGED FRO M TOO LONG FAST. CUT OUT DAMAGE, REPAIRED BELL FRAME PER SRM 51-40-3 DOUBLER 7075-T6 .063 BY 20 INCH LONG 2 ROWS 43 BAC B30FP8 HI-LOCKS AND 1 ROW OF 19 BACB30FC6 AND 2BACB306F10 HI-LOCKS. (M) 2 L 7 3 4F A3WE 1999043000368 19990430 00368 NM 1999 4 30 AALA990380 1 19990219 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 334-337 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION AT TOP OF NLG DOGHOUSE AT TOP WALL TO SIDE WALL JOINT CORNER. INSTALLED DOUBLER REPAIR IAW SRM 51 -40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999043000369 19990430 00369 NM 1999 4 30 AALA990381 1 19990223 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STATION 660 BELT FRAME DENTED AT 24L. INSTALLED DOUBLER (7075T-6, .063, 7.5 INCH LONG) 3 ROWS OF RIVETS (1 ROW TOP, 2 ROWS SIDE) WITH 20 EACH .1875 D-RIVETS PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999043000370 19990430 00370 NM 1999 4 30 AALA990382 1 19990212 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - STATION 500 BELL FRAME HAS 3 DENTS ON UPPER LEG FROM STR 22R TO 25R. CUTOUT DAMAGED AREA, REPAIRED BELT FRAME AT STATION 500, STRINGER 22R TO 25R PER SRM 51-40-3 FIG 1, PAGE 3. 1 DOUBLER 8 INCHES LONG .0637075-T6 20 EACH .1875 MS204 70D RIVETS 3 ROWS, 2ND DOUBLER 20 INCHES LONG .063 7075-6, 2 EACH .1875 AND 4 EACH .25 MS20470D RIVETS 3 ROWS. (M) 2 L 7 3 4F A3WE 1999043000371 19990430 00371 NM 1999 4 30 AALA990383 1 19990219 A 5320 CLIP BOEING 727 727223 1384074 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION ON STRINGER CLIP TO FRAME AT FS 660 STRINGER 15R. REPLACED STRINGER CLIP. (M) 2 L 7 3 4F A3WE 1999043000372 19990430 00372 NM 1999 4 30 AALA990384 1 19990222 A 5320 FITTING BOEING 727 727223 1384074 NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION ON FORWARD LEFT MLG TRUNNION FITTING BEARING ATTACHMENT BORES 4 EACH. REAMED HOLES AND INSTALLED OVERSIZE BUSHING PER ESO 11697 (2-22-97) AND SB 727-57-132. (M) 2 L 7 3 4F A3WE 1999043000373 19990430 00373 NM 1999 4 30 AALA990385 1 19990216 A 5320 FITTING BOEING 727 727223 1384074 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STRINGER 27L OUTBOARD END FITTING HEAVILY CORRODED. INSTALLED NEW END FITTING CPN5624412. (M) 2 L 7 3 4F A3WE 1999043000374 19990430 00374 NM 1999 4 30 AALA990386 1 19990223 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - STATION 680 BELL FRAME DENTED AT STRINGER 23L. INSTALLED DOUBLER PER SRM 51-40-3 7075T6.063, 3 ROWS OF RIVETS 1 R OW TOP 2 ROWS SIDE 20 .1875 D-RIVETS. (M) 2 L 7 3 4F A3WE 1999043000375 19990430 00375 NM 1999 4 30 AALA990387 1 19990223 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - SMALL DENT, UPPER FLANGE OF STATION 680 BELL FRAME, BELOW STRINGER 24L. INSTALLED DOUBLER PER SRM 51-40-3 7075T6. 063, 3 ROWS OF RIVETS 2 ROWS SIDE SIXTEEN .1875 D-RIVETS, FOUR .25 INCH D-RIVETS. (M) 2 L 7 3 4F A3WE 1999043000376 19990430 00376 NM 1999 4 30 AALA990388 1 19990217 A 5311 FRAME BOEING 727 727223 1384074 NM BS 580 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - STATION 580 BELL FRAME HAS TWO DENTS AT STRINGER 23L TO STRINGER 24L. INSTALLED DOUBLER 7075T6 .063, 3 ROWS OF RI VETS 1 ROW IN TOP, 2 ROWS ON SIDE WITH THIRTY .1875 D-RIVETS AND FOUR EACH HI-LOCKS IN SHEAR TIE, STD .15625 ATTACHING T O STRINGER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999043000377 19990430 00377 NM 1999 4 30 AALA990389 1 19990223 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - UPPER FLANGE OF BELL FRAME DENTED AT STATION 600 AND STRINGER 24 TO 25L. CUT OUT DAMAGED AREA AND INSTALLED REPAI R DOUBLER PER SRM 51-40-3, 7075T6 .063 SEVEN INCHES LONG, 3 ROWS RIVETS 1 TOP, 2 ON SIDE, NINTEEN .1875 INCH D-RIVETS, O NE .25 INCH D-RIVETS. (M) 2 L 7 3 4F A3WE 1999043000378 19990430 00378 NM 1999 4 30 AALA990390 1 19990223 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND UPPER FLANGE OF BELL FRAME IS DENTED AT STATION 620 AT STATION 24L TO 25L. CUT OUT DAMAGED SECTION AND INST ALLED REPAIR DOUBLER PER SRM 51-40-3, 7075T6 .063, 16.5 INCH LONG, 3 ROWS RIVETS 1 ON TOP 2 ON SIDE WITH FORTY-EIGHT .18 75 INCH D-RIVETS, FOUR .25 INCH D-RIVETS. (M) 2 L 7 3 4F A3WE 1999043000379 19990430 00379 NM 1999 4 30 AALA990391 1 19990217 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STATION 680 BELL FRAME DENTED ABOVE STRINGER 24R. INSTALLED DOUBLER (7075 T-6 .063) 3 ROWS OF RIVETS, 1 ROW TOP, 2 ROWS SIDE WITH SEVENTEEN .1875 D-RIVETS AND FOUR .25 INCH RIVETS, DOUBLE 7.5 INCH LONG PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999043000380 19990430 00380 NM 1999 4 30 AALA990392 1 19990217 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STATION 700 BELL FRAME DENTED ABOVE STRINGER 24R. INSTALLED DOUBLER (7075T-6 .063) 3 ROW OF RIVETS, 1 ROW T OP, 2 ROWS SIDE WITH EIGHTTEEN .1875 D-RIVETS, DOUBLER 7.5 INCH LONG PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999043000381 19990430 00381 NM 1999 4 30 AALA990393 1 19990222 A 5720 FITTING BOEING 727 727223 1384074 NM WS 224 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FORWARD TRUNNION FITTING BEARING BORES CORRODED. REPLACED RMG FORWARD TRUNNION FITTING PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999043000382 19990430 00382 NM 1999 4 30 AALA990394 1 19990219 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 323-326 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION AT TOP OF NLG DOGHOUSE AT TOP WALL TO SIDE WALL JOINT (CORNER) LEFT SIDE. INSTALLED DOUBLER REPAI R IAW SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999043000383 19990430 00383 NM 1999 4 30 AALA990395 1 19990303 A 5320 FITTING BOEING 727 727223 1384074 NM BS 1176 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 893AA 22009 TUL - RIGHT CREASE BEAM 1183 END FITTING MIS-DRILLED ZERO EDGE DISTANCE ON FORWARD FASTENER, STATION 1176 STRINGER 17R. REMOVED 7 FASTENERS AND INSTALLED DOUBLER AND FILLERS PER ESO 11697 DATED 2-26-99. (M) 2 L 7 3 4F A3WE 1999043000384 19990430 00384 NM 1999 4 30 AALA990396 1 19990219 A 5320 BEAM BOEING 727 727223 1384074 NM WS 36-60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CORROSION IN 16 EACH FASTENER HOLE OUTBOARD NR 4 FLAPTRACK IN LEFT MLG GEAR BEAM. REAMED HOLES TO REMOVED C ORROSION AND INSTALLED BUSHINGS IN HOLES PER ESO 11697, DATED 2-19-99. (M) 2 L 7 3 4F A3WE 1999043000385 19990430 00385 NM 1999 4 30 AALA990397 1 19990226 A 5720 CASTING BOEING 727 727223 1384074 NM BS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CRACK IN RADIUS AND VERTICAL AREA OF LEFT 760 CASTING (BEHIND RIB). REPAIRED LEFT 760 CASTING PER BOEING SE RVICE BULLETIN 727-57-0112 REV 5 LARGE REPAIR. (M) 2 L 7 3 4F A3WE 1999043000386 19990430 00386 NM 1999 4 30 AALA990399 1 19990222 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CRACK IN LEADING EDGE SKIN OUTBOARD EDGE OF INBOARD ROLLER, CUTOUT AT BOTTOM FLANGE NR 8 SLAT. REMOVED DAMA GED AREA AND INSTALLED DOUBLER REPAIR PER SRM 57-30-4. (M) 2 L 7 3 4F A3WE 1999043000387 19990430 00387 NM 1999 4 30 AALA990398 1 19990222 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND CRACK IN LEADING EDGE SKIN AT INBOARD ROLLER TRACK CUTOUT FOR NR 6 SLAT. REMOVED DAMAGE AND INSTALLED DOUBL ER REPAIR PER SRM 57-30-4. (M) 2 L 7 3 4F A3WE 1999043000388 19990430 00388 NM 1999 4 30 AALA990449 1 19990317 A 5711 SPAR BOEING 727 727223 1384074 NM WS 538 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FRONT SPAR LOWER CHORD HAS CORROSION 12 INCHES INBOARD OF NR 3 SLAT OUTBOARD TRACK. INSTALLED REPAIR STRAP PER AA RD 57-30-00-2. (M) 2 L 7 3 4F A3WE 1999043000389 19990430 00389 NM 1999 4 30 AALA990444 1 19990308 A 5320 WEB BOEING 727 727223 1384074 NM BS 1223 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - FOUND CRACK IN WEB STATION 1223 LEFT 3 INCH ABOVE STRINGER 14L INBOARD ON FRAME 18 INCHES. CUT OUT DAMAGED SECTIO N OF WEB AND INSTALLED REPAIR PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1999043000390 19990430 00390 NM 1999 4 30 AALA990443 1 19990226 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1243 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - TOOL MARK IN STRINGER 17 LEFT STATION 1243. INSTALLED TWO STRINGER REPAIRS AND SPLICES PER 53-10-3, DETAIL 1 FORW ARD 8 AFT OF BELL FRAME. (M) 2 L 7 3 4F A3WE 1999043000391 19990430 00391 NM 1999 4 30 AALA990412 1 19990315 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 615-619 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FRAME SPLICE STRIP HEAVILY CORRODED ON UNDERSIDE OF CARGO DOOR FRAME UPPER CHORD AT STATION 615 TO 619 STRINGER 26 R, AFT LOWER CORNER OF DOOR OPENING. INSTALLED NEW FRAME SPLICE STRIP ON UNDERSIDE OF CARGO DOOR FRAME 615 TO 619 STRIN GER 26R. (M) 2 L 7 3 4F A3WE 1999043000392 19990430 00392 NM 1999 4 30 AALA990413 1 19990316 A 5311 FRAME BOEING 727 727223 1384074 NM BS 910 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND STATION 910 UPLOCK FRAME CRACKED ON FORWARD FLANGE. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-2 PAGE 28. (M) 2 L 7 3 4F A3WE 1999043000393 19990430 00393 NM 1999 4 30 AALA990414 1 19990316 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1090 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND STATION 1090, 3 INCH BELOW STRINGER 17 LT HAS DEEP DENT IN FUSE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-3 0-3, AFTER CUT OUT DAMAGED AREA. (M) 2 L 7 3 4F A3WE 1999043000394 19990430 00394 NM 1999 4 30 AALA990415 1 19990315 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND CORROSION ON STRINGER 28R AT STATION 560. INSTALLED STRINGER REPAIR AT STATION 554 AND STATION 566 IAW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999043000395 19990430 00395 NM 1999 4 30 AALA990416 1 19990312 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND BELL FRAME AT BS 1050 DENTED. REMOVED DENTED PORTION OF BELL FRAME AND INSTALLED REPAIR SECTION PER SRM 53- 10-4. (M) 2 L 7 3 4F A3WE 1999043000396 19990430 00396 NM 1999 4 30 AALA990417 1 19990315 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 495 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND CORROSION ON STRINGER 27L AT STATION 495. CUT AND REMOVED DAMAGED SECTION OF STRINGER 27L FROM STATION 491 TO 509 MANUFACTURED AND INSTALLED REPAIR FILLER AND SPLICE IAW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999043000397 19990430 00397 NM 1999 4 30 AALA990418 1 19990418 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 481-486 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND CORROSION ON STRINGER 26L AT STATION 481 TO 486. CUT OUT CORRODED END OF STRINGER AND INSTALLED EXTENDED PR ODUCTION SPLICE PER ESO11697 3/17/99. (M) 2 L 7 3 4F A3WE 1999043000398 19990430 00398 NM 1999 4 30 AALA990419 1 19990311 A 5711 SPAR BOEING 727 727223 1384074 NM WS 468 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND CORROSION ON FRONT SPAR LOWER CHORD, LOWER WING L/E PANEL LAND AT NR 3 SLAT INBOARD TRACK. BLENDED OUT CORR OSION. INSTALLED REPAIR STRAP PER B727 AARD 57-30-00-2 PAGE 1 AND 2 AND 3. TREATED, PRIMED AND PAINTED AREA. (M) 2 L 7 3 4F A3WE 1999043000399 19990430 00399 NM 1999 4 30 AALA990420 1 19990319 A 5320 ANGLE BOEING 727 727223 1384074 NM NLG WW CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 895AA 22011 TUL - FOUND CORROSION ON UPPER AFT SUPPORT ANGLE IN RIGHT TRUNNION BOX (MARKED) INBOARD OF SWIVEL VALVE REF E58 NR 31461 90. REMOVED CORROSION ON UPPER AFT SUPPORT ANGLE. INSTALLED EXTRUDED SECTION REPAIR PER SRM 51-40-4 PAGE 5. (M) 2 L 7 3 4F A3WE 1999043000400 19990430 00400 WP 1999 4 30 AALA990462 1 19990403 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - FOUND CORROSION ON FRAME STATION 1309, L22L TO L18L. NEW SECTION OF FRAME INSTALLED PER SRM 53-03. (M) 2 L 7 2 4F A6WE 1999043000401 19990430 00401 NM 1999 4 30 AALA990470 1 19990406 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1967 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - FOUND NR 1 SEAT TRACK CORRODED AT STATION 1967. ACCOMPLISHED A SEAT TRACK SPLICE REPAIR PER SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1999043000402 19990430 00402 NM 1999 4 30 AALA990471 1 19990406 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1321 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - FOUND NR 2 SEAT TRACK HAS CORROSION JUST FORWARD OF PLUG REPAIR INBOARD OF LAV 'L' TIE DOWN STATION 1321. PERFORM ED SEAT TRACK SPLICE REPAIR PER MD-11 SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1999043000403 19990430 00403 NM 1999 4 30 AALA990472 1 19990406 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1361 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - FOUND NR 2 SEAT TRACK HAS CORROSION STATION 1361, FORWARD AND AFT OF PLUG REPAIR. PERFORMED SEAT TRACK REPAIR PER MD-11 SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1999043000404 19990430 00404 NM 1999 4 30 AALA990473 1 19990406 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - AFT END OF RIGHT FLOORBOARD SUPPORT AT T-ANGLE HAS CORROSION AT BOTTOM SIDE OF SUPPORT X STATION 20 RIGHT. INSTAL LED NEW MANUFACTURED FLOORBOARD SUPPORT AT RIGHT SIDE PER 51-21-01. (M) 2 L 7 3 4F RT A22WE 1999043000405 19990430 00405 NM 1999 4 30 AALA990474 1 19990406 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 1967-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - UNDERSIDE OUTBOARD FLANGE HAS CORROSION AT FASTENERS OF FLOORBOARD SUPPORT, FIRST SUPPORT FROM RIGHT SIDE FUSE FRO M STATION 1967-2007 (VIEWED FROM BOTTOM WAIST TANK). REPLACED SUPPORT FIRST FROM RIGHT SIDE SRM 51-21-01 VOL II. (M) 2 L 7 3 4F RT A22WE 1999043000406 19990430 00406 NM 1999 4 30 AALA990475 1 19990406 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 2000-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - RIGHT FLOOR SUPPORT HAS CORROSION AT AFT ATTACH AREA STATION 2000-2007. MANUFACTURED NEW FLOORBOARD SUPPORT DUE T O CORROSION BEYOND LIMITS ON E58-4 NR 0100040, INSTALLED ON SAME E-58-4 SRM 51-21-01. (M) 2 L 7 3 4F RT A22WE 1999043000407 19990430 00407 EU 1999 4 30 AALA990452 1 19990401 A 5320 MOUNT AIRBUS 300 A300B4605R 3930308 EU LAVATORY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70072 515 TUL - MOUNTING FOOT FORWARD OF LAV V DOOR IS CORRODED. REPLACED IN SHOP ON SHOP ORDER NR YFT6. (M) 2 L 7 2 4F RT A35EU 1999043000408 19990430 00408 WP 1999 4 30 99ZZZM259 1 19990404 A 2913 PV32402F PUMP VICKERS DOUG DC10 DC1030 3023501 WP RT ENGINE DEFECTIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 143AA MX277050 46555 DFW - FLT 123 - DURING CLIMB-OUT, THE NR 2 ENGNE RIGHT HYDRAULIC PUMP HIGH TEMPERATURE LIGHT ILLUMINATED, FOLLOWED SHORT LY BY THE LEFT HYDRAULIC PUMP HIGH TEMPERATURE LIGHT ILLUMINATING. BOTH PUMPS WERE TURNED OFF BY THE ABNORMAL CHECKLIST , AND BOTH HIGH TEMPERATURE LIGHTS EXTINGUISHED AFTER 5 MINUTES. AIRCRAFT AIR INTERRUPTED AND LANDED DFW WITHOUT FURTHE R INCIDENT. MAINTENANCE CHECKED AND INSPECTED SYSTEM AND DETERMINED THE PUMPS WERE FAULTY. MAINTENANCE REPLACED BOTH E NGINE DRIVEN HYDRAULIC PUMPS AND FILTERS. RAN RIGHT ENGINE AND PUMPS WITH NO OVER HEATING OR LEAKS NOTED. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999043000409 19990430 00409 WP 1999 4 30 AALA990461 1 19990331 A 2497 WIRE DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 77421 49333 STL - FLT 2257 - NEAR TOP OF CLIMB, CREW HEARD A LOUD POP AND SAW A FLASH OF LIGHT FROM THE EPC CIRCUIT BREAKER PANEL. N O BREAKERS WERE TRIPPED. MINUTES LATER ANOTHER POP AND FLASH CAME FROM THE EPC CIRCUIT BREAKER PANEL. AN ACRID SMELL O F BURNING INSULATION WAS NOTED AT FL 30. FLIGHT LANDED STL AND CREW PERFORMED EMERGENCY FIRE/ELECTRICAL CHECKLIST WITH NO SMOKE OR FIRE DETECTED. MAINTENANCE TROUBLESHOT AND FOUND PASSENGER POWER PORT FEEDER CABLE CHAFFED AT COCKPIT DOOR SOLENOID. SYSTEM WAS DEACTIVATED PER ECO. GROUND RAN BOTH ENGINES AND OPERATED PACKS WITH BUSSES LOADED AND NO ABNORMA L SMELL NOTED. AIRCRAFT OPERATED TO DFW AND OVERNIGHTED. MAINTENANCE REPAIRED DAMAGED POWER PORT FEEDER CABLE. REROU 2 L 7 2 4F A6WE 1999043000410 19990430 00410 WP 1999 4 30 AALA990453 1 19990404 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3515 49892 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FL OOR LIGHTING WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999043000411 19990430 00411 WP 1999 4 30 AALA990454 1 19990401 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 485AA 49678 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. RECONNECTED EMERG ENCY EXIT FLOOR PATH LIGHT WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999043000412 19990430 00412 WP 1999 4 30 AALA990455 1 19990403 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 426AA 49338 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH CONNEC TOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999043000413 19990430 00413 WP 1999 4 30 AALA990426 1 19990326 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7517A 49894 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. RESEATED EMERGENCY FLOOR PATH LIGHT WI RE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999043000414 19990430 00414 NM 1999 4 30 AALA990301 1 19990303 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 4 AB LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372AA 25199 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH MARKER LIGHT INOPERATIVE AT SEAT 4AB. RESEATED CONNECTOR AT SEA T 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999043000415 19990430 00415 NM 1999 4 30 AALA990431 1 19990329 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 32-41 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361AA 24042 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH EXIT LIGHTS BETWEEN SEAT ROWS 32HJ THROUGH 41HJ INOPERATIVE. MAINTEN ANCE FOUND A FAULTY CONNECTOR. REPLACED CONNECTOR TO EMERGENCY EXIT PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (M) 2 L 7 2 4F RT A1NM 1999043000416 19990430 00416 WP 1999 4 30 AALA990434 1 19990327 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 7509 49803 ORD - FLT 631 - DURING CRUISE AT FL 370, FLIGHT ATTENDANTS NOTICED A STRONG ODOR WITH SMELL OF SMOKE IN AFT CABIN. SMEL L DISSIPATED AFTER A FEW MINUTES WITH NO REOCCURRENCE FOR THE REMAINDER OF THE FLIGHT. FLIGHT LANDED ORD WITHOUT FURTHE R INCIDENT. MAINTENANCE REPLACED BOTH COALESCER BAGS, RAN PACKS WITH ENGINES AND APU WITH NO ODOR OR SMOKE NOTED. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999043000417 19990430 00417 NM 1999 4 30 ASAA9940086 1 19990330 A 5320 65C33582 WEB BOEING 737 7374Q8 NM BS 991 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE SHEAR WEB UNDER LEFT TRANSVERSE BEAM AT L-2 DOOR THRESHOLD CORRODED AT STATION 991, LBL 37. REPAIRED PER SRM 51-40-02 AND SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1999043000418 19990430 00418 NM 1999 4 30 ASAA9940085 1 19990330 A 5320 65C80735116 BEAM BOEING 737 7374Q8 NM BS 949-997 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE L-2 DOOR LOWER SEAL TRANSVERSE BEAM CORRODED FROM STATION 949 TO 997. REPAIRED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999043000419 19990430 00419 NM 1999 4 30 ASAA9910074 1 19990330 A 5320 WEB BOEING 737 7372X6C 1384552 NM BS 767-787 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND CRACKED WEB AT THE AFT CARGO COMPARTMENT, FORWARD SIDE DOOR, STRINGER 25R, STATION 767 TO 78 7. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999043000420 19990430 00420 NM 1999 4 30 ASAA9910075 1 19990330 A 5320 INTERCOSTAL BOEING 737 7372X6C 1384552 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND AFT CARGO COMPARTMENT ATTACH PLATE AT WEB INTERCOSTAL CORRODED AT STATION 787. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999043000421 19990430 00421 NM 1999 4 30 ASAA9910076 1 19990330 A 5320 6941757 INTERCOSTAL BOEING 737 7372X6C 1384552 NM BS 500-520 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND INTERCOSTAL AT STATION 500B TO 520 CRACKED AND DENTED. REPAIRED PER SRM 51-40-3 AND DRAWING 69-41757. (M) 2 L 7 2 4F RT A16WE 1999043000422 19990430 00422 WP 1999 4 30 ASAA9980072 1 19990402 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP CARGO COMPT FAILED A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 01 935AS 5464 49236 LAX - AIR TURN BACK OF FLIGHT 559, FLIGHT ATTENDANT REPORTED SMOKE/ODOR IN THE REAR OF THE CABIN ON TAKEOFF. FOUND THE AIR CONDITIONING RECIRCULATION FAN CIRCUIT BREAKERS POPPED. REPLACED THE FAN AND FILTER AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999043000423 19990430 00423 WP 1999 4 30 ASAA9980073 1 19990403 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 SEA - AFTER ARRIVAL OF FLIGHT 160, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. CLEANED AND LUBRICATED DOOR BAYONET CAM AND FOLLOWER ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999043000424 19990430 00424 NM 1999 4 30 ASAA9940084 1 19990405 A 5210 MECHANISM BOEING 737 737490 1384715 NM L-1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 797AS 28892 SEA - FLT 62 - L-1 DOOR BINDS. LUBRICATED DOOR MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999043000425 19990430 00425 NM 1999 4 30 ASAA9940083 1 19990403 A 5400 311A1710 BUSHING BOEING 737 737490 1384715 NM NR 2 PYLON FRETTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 SEA - DURING SI CHECK, FOUND THE NR 2 ENGINE PYLON UPPER LINK FORWARD OF FRONT SPAR, FORWARD END BUSHING FRETTING AND HA D GAP. REPAIRED PER EA 5440-01011. (M) 2 L 7 2 4F RT A16WE 1999043000426 19990430 00426 NM 1999 4 30 ASAA9940082 1 19990330 A 5315 BAC1505100008 FLOORBEAM BOEING 737 7374Q8 NM BS 947.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE UPPER HORIZONTAL CAP OF THE FLOORBEAM AT STATION 947.5 CORRODED FROM RBL 13 TO LBL 13. REPAIRED PER EA 5310-01665. (M) 2 L 7 2 4F RT A16WE 1999043000427 19990430 00427 NM 1999 4 30 ASAA9940081 1 19990330 A 5315 FLOORBEAM BOEING 737 7374Q8 NM BS 360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE UPPER HORIZONTAL CAP OF THE FLOORBEAM AT STATION 360 CORRODED FROM RBL 14 TO RBL 28. R EPAIRED PER EA 5310-01666. (M) 2 L 7 2 4F RT A16WE 1999043000428 19990430 00428 NM 1999 4 30 ASAA9940080 1 19990330 A 5315 BAC1505100849 FLOORBEAM BOEING 737 7374Q8 NM BS 986.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE UPPER HORIZONTAL CAP OF THE FLOORBEAM AT STATION 986.5 CORRODED IN NUMEROUS AREAS FROM LBL 45 TO RBL 31. REPAIRED PER EA 5310-01667. (M) 2 L 7 2 4F RT A16WE 1999043000429 19990430 00429 NM 1999 4 30 ASAA9910069 1 19990327 A 5320 6567393 ANGLE BOEING 737 7372X6C 1384552 NM BS 979-986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT ENTRY AREA TORQUE BOX FOR AIRSTAIR MECHANISM HAS CORRODED ANGLE EXTRUSIONS AT STATIO N 979 TO 986, LBL 48. REPAIRED PER SRM 51-40-4 AND DRAWING 65-67393. (M) 2 L 7 2 4F RT A16WE 1999043000430 19990430 00430 NM 1999 4 30 ASAA9910070 1 19990330 A 5315 65549011 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOORBEAM AT STATION 947 CORRODED FROM LBL 32 TO RBL 54, TOP AND BOTTOM OF UP PER CHORD. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999043000431 19990430 00431 NM 1999 4 30 ASAA9910071 1 19990330 A 5320 WEB BOEING 737 7372X6C 1384552 NM BS 847 CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT WEB CORRODED AT STATION 847 FROM STRINGER 19R TO 25R. REPAIRED PE R EM 5300-01014. (M) 2 L 7 2 4F RT A16WE 1999043000432 19990430 00432 NM 1999 4 30 ASAA9910073 1 19990405 A 3230 RETRACT MECH BOEING 737 737290C 138448V NM NLG ICED UP A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 742AS 23136 FLT 66 - YAK-JNU - FLIGHT DIVERTED TO SEA DUE TO NOSE LANDING GEAR TRANSIT LIGHT REMAINED ILLUMINATED AFTER DEPARTURE YA K WHEN LANDING GEAR LEVER WAS PLACED IN THE UP POSITION. WHEN GEAR LEVER WAS POSITIONED TO OFF, THE NOSE LANDING GEAR F REE FELL TO AN EXTENDED POSITION. CYCLED GEAR TO THE DOWN POSITION AND THREE GREEN LIGHTS ILLUMINATED. PLACED GEAR HAN DLE IN THE UP POSITION AND THE NOSE LANDING GEAR TRANSIT LIGHT REMAINED ILLUMINATED. MADE UNSCHEDULED LANDING IN YVR DU E TO MEDICAL EMERGENCY ONBOARD AND LANDED WITHOUT INCIDENT. ICE WAS NOTED IN NOSE LANDING GEAR AREA. FERRIED AIRCRAFT FROM YVR TO SEA FOR TROUBLESHOOTING. AIRCRAFT LANDED IN SEA WITHOUT INCIDENT. INSPECTED NOSE LANDING GEAR SYSTEM, PERF 2 L 7 2 4F A16WE 1999043000433 19990430 00433 WP 1999 4 30 ASAA9980074 1 19990402 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 975AS 53451 SEA - PRIOR TO DEPARTURE OF FLIGHT 463, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999043000434 19990430 00434 NM 1999 4 30 ASAA9910072 1 19990405 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM ROW 10-11 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 10-11 WERE FOUND INOPERATIVE. REPLACED BA TTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999043000435 19990430 00435 NM 1999 4 30 ASAA9910068 1 19990402 A 3350 6104781 BATTERY GRIMES BOEING 737 737298C 1384490 NM ROW 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WERE FOUND INOPERATIVE. REPLACED BATTER Y AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999043000436 19990430 00436 NM 1999 4 30 ASAA9910067 1 19990329 A 3350 1060091102 LIGHT BOEING 737 7372X6C 1384552 NM R1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND TO BE MISSING. INSTALLED R1 DOOR EM ERGENCY EXIT LIGHT ASSY, OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 1999043000437 19990430 00437 NM 1999 4 30 ASAA9910066 1 19990328 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT LIGHT, SMOKE BARRIER LIGHT, AND THE RIGHT OVERWING EXIT LIGHTS WE RE INOPERATIVE. REPLACED AFT EMERGENCY EXIT LIGHT AND SMOKE BARRIER LIGHT BATTERIES AND THE RIGHT OVERWING EMERGENCY EX IT LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999043000438 19990430 00438 NM 1999 4 30 99ZZZM260 1 19990328 A 3350 1060091102 LIGHT BOEING 737 7372X6C 1384552 NM RT EMER EXIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT LIGHT, SMOKE BARRIER LIGHT, AND THE RIGHT OVERWING EXIT LIGHTS WE RE INOPERATIVE. REPLACED AFT EMERGENCY EXIT LIGHT AND SMOKE BARRIER LIGHT BATTERIES AND THE RIGHT OVERWING EMERGENCY EX IT LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999043000439 19990430 00439 NM 1999 4 30 ASAA9910065 1 19990328 A 3350 RPS1B CHARGER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - FLT 9000 - CREW REPORTED THAT THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER. LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999043000440 19990430 00440 NM 1999 4 30 99ZZZM261 1 19990328 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - FLT 9000 - CREW REPORTED THAT THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER. LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999043000441 19990430 00441 NM 1999 4 30 ASAA9910064 1 19990327 A 3350 1060091102 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 PHX - AFTER TEST FLIGHT CREW REPORTED THAT THE AFT CABIN OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999043000442 19990430 00442 WP 1999 4 30 USAA990264 1 19990326 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1463 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 815US 48095 PIT - DURING C-06 CHECK, FOUND 4 INCH CRACK AT CANTED FRAME WEB STATION 1463 BETWEEN LONGERON 8 AND 9R. SPLICED IN SECT ION. REPAIRED PER EA TYPICAL REPAIR 53-10-25. (M) 2 L 7 2 4F A6WE 1999043000443 19990430 00443 WP 1999 4 30 USAA990268 1 19990327 A 5320 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND CORROSION AT INTERCOSTAL 'T' FITTINGS (1 INCH BY .5 INCH AREA) AT LOWER FORWARD CARGO DOOR STOP, BOTH SIDES OF WEB. CORROSION TASK NR C51-53300, CORROSION LEVEL 1. CLEANED AND TREATED PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1999043000444 19990430 00444 WP 1999 4 30 USAA990267 1 19990327 A 5220 SKIN DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN SKIN COMING OUT FROM UNDER TOP AFT STOP AT AFT LEFT EMERGENCY EXIT. INSTA LLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03. (M) 2 L 7 2 4F A6WE 1999043000445 19990430 00445 WP 1999 4 30 USAA990269 1 19990327 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND CORROSION AT INERCOSTAL 'T' FITTINGS (1 INCH BY .5 INCH AREA) AT FORWARD CARGO DOOR LOWER AFT DOOR STOP, BOTH SIDES OF WEB. CORROSION TASK NR C51-53300, CORROSION LEVEL 1. CLEANED AND TREATED PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1999043000446 19990430 00446 WP 1999 4 30 USAA990271 1 19990327 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH LONG CRACK AT LONGERON 4L STATION 160 (AROUND HI-LOCK HEAD). SPLICED IN NEW SECTIO N OF LONGERON PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999043000447 19990430 00447 WP 1999 4 30 USAA990273 1 19990330 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND .25 INCH CRACK EMINATING FROM SHEAR TIE ATTACH FASTENER ON FUSELAGE SKIN AT STRINGER 14L S TATION 965. INSTALLED PERMANENT CLASS 1 REPAIR PER DC-9 SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 1999043000448 19990430 00448 WP 1999 4 30 USAA990272 1 19990327 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 945/965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND TWO .25 INCH CRACKS AND TWO EACH 1.5 INCH CRACKS ON SKIN BETWEEN STATION 945 AND 965 AND B ETWEEN L14R AND L15R. CUT OUT TWO CRACKS AND FILLED. STOP DRILLED TWO CRACKS AND INSTALLED TITANIUM DOUBLER PER EA 516 58. (M) 2 L 7 2 4F A6WE 1999043000449 19990430 00449 WP 1999 4 30 USAA990348 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP GALLEY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND 6 INCH LONG CORROSION AT GALLEY FLOOR SUPPORT NR 2 CORROSION LEVEL 1. REPLACED FLOOR SUPP ORT. (M) 2 L 7 2 4F A6WE 1999043000450 19990430 00450 WP 1999 4 30 USAA990347 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 230/252 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND 22 INCH LONG CORROSION AT CENTER FLOOR SUPPORT BETWEEN STATIONS 230 AND 252. CORROSION LE VEL 1. FABRICATED PART PER TYPICAL REPAIR 53-10-21A. (M) 2 L 7 2 4F A6WE 1999043000451 19990430 00451 WP 1999 4 30 USAA990346 1 19990330 A 5320 BRACKET DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK AT RIGHT LAV 965 INBOARD BEAM TRIM ATTACH BRACKET. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 4. (M) 2 L 7 2 4F A6WE 1999043000452 19990430 00452 WP 1999 4 30 USAA990345 1 19990330 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 1038 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND .25 INCH HOLE AND CHAFE MARK VENTRAL AREA FORWARD SIDE STATION 1038 WEB AT LT TEMP CONT VL V. INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M) 2 L 7 2 4F A6WE 1999043000453 19990430 00453 WP 1999 4 30 USAA990270 1 19990327 A 5400 ANGLE DOUG DC9 DC931 3022065 WP BS 1019 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND .375 INCH CRACK IN UPPER RIGHT PYLON ATTACH ANGLE AT VERT LEG OF ATTACH ANGLE AT STATION 1 019 RIGHT. INSTALLED DOUBLER PER SRM 54-04 FIG 10. (M) 2 L 7 2 4F A6WE 1999043000454 19990430 00454 WP 1999 4 30 USAA990344 1 19990330 A 5320 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND .25 INCH CRACK IN ANGLE RIGHT PYLON AT FORWARD WALL OF CANNON PLUG BAY. FABRICATED NEW AN GLE OUT OF 2024 T3 .025. (M) 2 L 7 2 4F A6WE 1999043000455 19990430 00455 WP 1999 4 30 USAA990343 1 19990330 A 5320 WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND TWO CRACKS .25 INCH AND .75 INCH AT RIGHT PYLON CANTED WEB IN CANNON PLUG BAY. INSTALLED DOUBLER PER SRM 54-01 FIG 2 SHEET 2. (M) 2 L 7 2 4F A6WE 1999043000456 19990430 00456 WP 1999 4 30 USAA990342 1 19990330 A 5320 BRACKET DOUG DC9 DC931 3022065 WP PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND .50 INCH CRACK IN MIDDLE LEFT DOOR BRACKET ON INSIDE DOOR JAMB. DEFECTIVE PART REPLACED W ITH PART NR 3917624515. (M) 2 L 7 2 4F A6WE 1999043000457 19990430 00457 WP 1999 4 30 USAA990341 1 19990330 A 5320 3917624515 BRACET DOUG DC9 DC931 3022065 WP PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT UPPER RIGHT DOOR STOP BRACKET ON DOOR JAMB. REPLACED WITH NEW BRACKET. ( M) 2 L 7 2 4F A6WE 1999043000458 19990430 00458 WP 1999 4 30 USAA990339 1 19990330 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACKS (SEVERAL) AT FORWARD SIDE STATION 965 BULKHEAD FORWARD WALL OF LAV AT FLOOR LEVEL. REPAIRED PER SRM 53-03 FIG 19. (M) 2 L 7 2 4F A6WE 1999043000459 19990430 00459 WP 1999 4 30 USAA990338 1 19990330 A 5320 CUSP DOUG DC9 DC931 3022065 WP BS 617 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND 3 INCH LONG CRACK AT RIGHT SIDE CUSP AT STRINGER NR 18 STATION 617. REMOVED AND REPLACED DEFECTIVE PART. (M) 2 L 7 2 4F A6WE 1999043000460 19990430 00460 WP 1999 4 30 USAA990337 1 19990330 A 5320 WINDOW FRAME DOUG DC9 DC931 3022065 WP BS 598 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND .25 INCH CRACK IN WINDOW FRAME AT UPPER FORWARD CORNER OF WINDOW FRAME AT STATION 598 RIGH T. STOP DRILLED, DOUBLER INSTALLED PER TYPICAL REPAIR 533006A. (M) 2 L 7 2 4F A6WE 1999043000461 19990430 00461 WP 1999 4 30 USAA990336 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND 2 INCH CRACKS IN FLOOR SUPPORT AT STATION 965 AT 29R. STOP DRILLED PER TYPICAL REPAIR 53- 2-08 PAGE 1. (M) 2 L 7 2 4F A6WE 1999043000462 19990430 00462 WP 1999 4 30 USAA990335 1 19990330 A 5312 9912243107UNK BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND TWO CRACKS IN SKIN AT BULKHEAD WEB STATION 965 AT RIGHT FLOOR LINE. REPLACED DAMAGED AREA WITH NEW SPLICED WEB PER SRM 53-03 FIG 119. (M) 2 L 7 2 4F A6WE 1999043000463 19990430 00463 NM 1999 4 30 HNAA9900054 1 19990427 A 3231 MECHANISM DHAV DHC8 DHC8102 2809003 NM RT MLG DOOR OUT OF ADJUST A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 931HA 132 RIGHT HAND MAIN LANDING GEAR DOORS WOULD NOT OPEN. ADJUSTED CABLE AT NR 2 NACELLE FOR AFT DOORS. CYCLED DOOR SERVERAL TIMES OPENING DOORS WITH RELEASE HANDLE. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999043000464 19990430 00464 WP 1999 4 30 AT9900333 1 19990429 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE CABIN FLOOR SUPPORT AT STA 200 TO 218 BL-0 CORRODED. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 53-11-01, 51-30-2, 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1999043000465 19990430 00465 WP 1999 4 30 AT9900334 1 19990422 A 5248 991556515 DOUBLER DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN EXISTING REPAIR DOUBLER CHAFED THRU AFT VENTRAL DOOR UPPER SECTION. RE MOVED, ORDERED, LOCATED, DRILLED, AND INSTALLED UPPER CHANNEL AND Z ANGLE IAW DC9 SRM 51-10-4, 51-30-2, 51-30-4, AND BOE ING DRAWING NR 9915565. Z ANGLE (P/N 9915565-133) OFF. 2 L 7 2 4F A6WE 1999043000466 19990430 00466 WP 1999 4 30 AT9900335 1 19990415 A 5330 1A4437011 SKIN DOUG DC9 DC932 3022066 WP BS 229-399 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN AT BS 229-399 L-18-26R DENTED AND CREASED. REMOVED AND REPLACED FUSELAGE SKIN IAW DC9 SRM 51-30-1, 51-10-2, 51-30-5, 51-20-0 AND RES NR 99749. SKIN (P/N 1A44467-1) OFF. 2 L 7 2 4F A6WE 1999043000467 19990430 00467 WP 1999 4 30 AT9900336 1 19990427 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT AT BS 200-218 LBL 18 CORRODED. REMOVED AND FABRICATED F LOOR SUPPORT, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-5, 51-10-4, 53-11-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999043000468 19990430 00468 NM 1999 4 30 AWXA9900144 1 19990419 A 2612 FIRE LIGHT BOEING 737 7373G7 1384595 NM APU ILLUMINATED A AWXA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 28 150AW 23218 APU FIRE INDICATION. APU FIRE LIGHT, FELT SLIGHT SHUDDER IN AIRFRAME PRIOR TO APU FIRE LIGHT. APU FIRE HANDLE PULLED A ND BOTTLE DISCHARGED, APU FIRE LIGHT EXTINGUISHED WITHIN 10 SECONDS. EGT ABOUT 680 AT OCCURRENCE. APU UNLOADED AND AT IDLE. CRUISE FLIGHT AT 35,000 FT, APU EGT DROPPED TO 0 WITHIN 20 MINUTES OF SHUTDOWN. EMERGENCY WAS DECLARED AND DIVER TED TO ABQ. INSPECTED APU FOUND NO EVIDENCE OF FIRE, RAN APU NO LOAD, UNDER LOAD, OPS NORMAL, BLEED GOOD. NO FURTHER D EFECTS NOTED AT THIS TIME C/W APU PERFORMANCE TEST IAW 6RD49001. 2 L 7 2 4F RT A16WE 1999043000469 19990430 00469 NM 1999 4 30 AWXA9900145 1 19990420 A 5314 KEEL BEAM BOEING 737 737277 1384570 NM BS 700 CRACKED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 183AW 22650 STATION 700 KEEL BEAM CLOSEOUT PANEL BOTTOM SIDE OF FUSELAGE AT MLG HAS 1.5 INCH CRACK. REMOVED CRACKED SKIN, FABRICATE D AND INSTALLED REPLACEMENT SKIN PER SRM 51-10-2, 51-30-2, 53-10-2 FIG 4. 2 L 7 2 4F RT A16WE 1999043000470 19990430 00470 NM 1999 4 30 AWXA9900146 1 19990420 A 5320 DOUBLER BOEING 737 737277 1384570 NM BS 967-986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 FLOOR SUPPORT, MAIN CABIN FS 967 - 986.5, RBL 18 TOP OF FLOOR SUPPORT HAS CORROSION. REMOVED FLOOR SUPPORT DOUBLER, FAB RICATED, ALODINED AND PRIMED DOUBLER IAW SRM 53-10-2 FIG 7 AND SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999043000471 19990430 00471 NM 1999 4 30 AWXA9900147 1 19990420 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 607 & 787 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 RT SKIN AT STR 17R BETWEEN STA 787 AND 607 HAD TWO CRACKS VERIFIED BY HFEC. CUT OUT CRACK, VERIFIED WITH HFEC. FABRICA TED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-3, QQA-250/5. 2 L 7 2 4F RT A16WE 1999043000472 19990430 00472 NM 1999 4 30 AWXA9900148 1 19990420 A 5312 BULKHEAD DOUBLER BOEING 737 737277 1384570 NM AFT PRESS BLKHD MISREPAIRED A AWXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 28 183AW 22650 AFT PRESSURE BULKHEAD, FUSELAGE STATION 1016, RBL 20, EXISTING REPAIR DOES NOT CONFORM TO SRM 53-10-4 FIG 3. REMOVED DO UBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-10-4 FIG 3. 2 L 7 2 4F RT A16WE 1999043000473 19990430 00473 NM 1999 4 30 AWXA9900149 1 19990420 A 5320 FRAME BOEING 737 737277 1384570 NM APU DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 APU COWL DOOR RIGHT AFT LATCH MOUNT STRUCTURE FRAME IS BROKEN AND CRACKED ON BOTH THE FORWARD AND AFT FRAMES. REMOVED C RACKED FRAMES, FABRICATED AND INSTALLED REPAIRED FRAMES PER SRM 52-40-1, 51-30-2, 51-10-2. 2 L 7 2 4F RT A16WE 1999043000474 19990430 00474 NM 1999 4 30 AWXA9900150 1 19990420 A 5320 SILL BOEING 737 737277 1384570 NM L1 DOORWAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 CORROSION ON FWD LT DOOR SILL, I/B OF L-1 DOOR. REMOVED CORRODED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53-10-2, 51-40-3, 51-10-2. 2 L 7 2 4F RT A16WE 1999043000475 19990430 00475 NM 1999 4 30 AWXA9900151 1 19990420 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 968.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 EXISTING FLOORBEAM REPAIR AT STA 968.5 RBL 49 CORRODED BEYOND LIMITS. REMOVED EXISTING T-CHORD PER SRM 51-30-2, FABRICA TED T-CHORD REPLACEMENT PER SRM 53-10-9 FIG 2, TREATED AND PRIMED PARTS PER SRM 51-10-6 AND INSTALLED REPAIR IAW SRM 51- 30-2. 2 L 7 2 4F RT A16WE 1999043000476 19990430 00476 NM 1999 4 30 AWXA9900152 1 19990420 A 5320 SUPPORT BOEING 737 737277 1384570 NM BS 992 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 CORROSION ON SECONDARY SUPPORT STRUCTURE AT FS 992 LT BL 15-20. REMOVED CORRODED SUPPORT IAW SRM 51-10-3 FIG 2, ALODINE D AND PRIMED IAW 51-10-2, AND INSTALLED PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 1999043000477 19990430 00477 NM 1999 4 30 AWXA9900153 1 19990420 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 1016 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 CORROSION ON BEAM FS 1016 LT BL 6 12 AFT LAV GALLEY FLOOR. CUT OUT CORROSION, FABRICATED NEW PARTS, TREATED, PRIMED AND INSTALLED IAW SRM 53-10-09, 51-30-2. 2 L 7 2 4F RT A16WE 1999043000478 19990430 00478 NM 1999 4 30 AWXA9900154 1 19990420 A 5320 6552878097 SUPPORT BOEING 737 737277 1384570 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 CORROSION ON THRESHOLD SUPPORT FOR L-2 DOOR FS 947 LT BL 54-55. REMOVED DAMAGED PART AND INSTALLED NEW PART PER SRM 51- 30-2. 2 L 7 2 4F RT A16WE 1999043000479 19990430 00479 NM 1999 4 30 AWXA9900155 1 19990420 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 CORROSION ON BEAM FS 986.5 LBL 42-46. REMOVED DAMAGED CAP, FABRICATED NEW CAP, TREATED PRIMED AND INSTALLED IAW SRM 53- 10-9, SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999043000480 19990430 00480 NM 1999 4 30 AWXA9900156 1 19990326 A 5315 654681143 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 CORROSION AROUND SCREW HOLES TOP AND BOTTOM OF UPPER TEE CHORD RBL 21-56, FRAME STA 328 RT. FABRICATED T-CHORD AND REPA IR AS PER AWA ER 3-53-1529 INSTRUCTIONS. 2 L 7 2 4F RT A16WE 1999043000481 19990430 00481 NM 1999 4 30 AWXA9900157 1 19990326 A 5315 654681143 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 FLOORBEAM UPPER CHORD CORRODED RBL 6 TO RBL 52 AT STA 294.5. FABRICATED T-CHORDS AND REPAIRED AS PER AWA ER 3-53-1529 I NSTRUCTIONS. 2 L 7 2 4F RT A16WE 1999043000482 19990430 00482 NM 1999 4 30 AWXA9900158 1 19990316 A 5315 654681143 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 FLOORBEAM 986.5 REQUIRES REPAIR SPLICES IAW AWA ER 3-53-1529 DUE TO CORROSION ON T-CAP. FABRICATED T-CHORDS AND REPAIRE D ANGLES PER AWA ER 3-53-1529 INSTRUCTIONS, 986.5 FLOORBEAM T-CAP REPLACED RT BL TO LT BL ALL INCLUSIVE SPLICE. 2 L 7 2 4F RT A16WE 1999043000483 19990430 00483 NM 1999 4 30 CALA9900445 1 19990426 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 907 - 917 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 CABIN RIGHT O/B SEEAT TRACK HEAVY CORROSION AT STA 907 - 917. REMOVED CABIN SEAT TRACK AT STA 907 TO END OF TRACK PER S RM 53-00-52. 2 L 7 2 4F RT A16WE 1999043000484 19990430 00484 NM 1999 4 30 CALA9900446 1 19990427 A 3350 7024091001 LIGHT BOEING 737 737724 NM L2 DOOR CRACKED A CALA K NONE L NO TEST NR NOT REPORTED 1 SW 09 13718 28937 EXIT SIGN DOOR 2L AFT GALLY WILL NOT STAY ON. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT L2 DOOR. 2 L 7 2 4F RT A16WE 1999043000485 19990430 00485 NM 1999 4 30 CALA9900447 1 19990428 A 5320 141N517011 INTERCOSTAL BOEING 757 757224 1384958 NM BS 324-345 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 INTERCOSTAL CORRODED STATION 324 - 345 RBL 40 BETWEEN FLOORBEAMS. CORRODED INTERCOSTAL REPLACED PER DRAWING NUMBER 141N 5170. 2 L 7 2 4F RT A2NM 1999043000486 19990430 00486 NM 1999 4 30 CALA9900448 1 19990428 A 5310 146N52932 STRUCTURE BOEING 757 757224 1384958 NM BS 1640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 K LAVTORY AFT ATTACHMENT POINTS CORRODED. REPLACED BOTH AFT ATTACH POINTS PER SRM 51-40-01. 2 L 7 2 4F RT A2NM 1999043000487 19990430 00487 NM 1999 4 30 CALA9900449 1 19990428 A 5310 65B578392 STRUCTURE BOEING 757 757224 1384958 NM BS 335 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 A LAVATORY ANCHOR POINT AT STA 353 LBL 20 CORRODED. REPLACED ANCHOR POINT PER SRM 51-10-00. 2 L 7 2 4F RT A2NM 1999043000488 19990430 00488 NM 1999 4 30 UPS99229426 1 19990407 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STR 25 LT DAMAGED AT FRAME ATTACH POINTS BS 420 LT. CRACKED STRINGER REPAIRED IAW SRM 53-10-2 FIG 1 DETAIL 2. 2 L 7 3 4F A3WE 1999043000489 19990430 00489 NM 1999 4 30 UPS99229427 1 19990406 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STRINGER 25 RT DAMAGED BS 420 AT FRAME ATTACH POINTS. CRACKED STRINGER 25 RT REPLACED BETWEEN BS 360 AND BS 440 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999043000490 19990430 00490 NM 1999 4 30 UPS99229428 1 19990330 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 4 FLAP TRACK FWD ATTACH LUG ON WING HAS LIGHT SURFACE CORROSION. REPAIR CARRIED OUT IAW SMRO E O 99-08-003 (UPS FILE NO 727-57-2052). 2 L 7 3 4F A3WE 1999043000491 19990430 00491 NM 1999 4 30 UPS99229429 1 19990330 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 3 FLAP TRACK FWD ATTACH LUG HAS LIGHT SURFACE CORROSION ON I/B FACE (ON WING). REPAIR CARRIED OUT IAW SMRO EO 99-08-003 (UPS FILE NR 727-57-2052). 2 L 7 3 4F A3WE 1999043000492 19990430 00492 NM 1999 4 30 UPS99229430 1 19990407 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STR 22 LT DAMAGED AT FRAME ATTACH POINT BS 400. CRACKED STR 22 LT SECTION REPLACED BETWEEN BS 390 AND BS 440 IAW SRM 53-10-2. 2 L 7 3 4F A3WE 1999043000493 19990430 00493 NM 1999 4 30 UPS99229431 1 19990407 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STR 23 LT CRACKED AT FRAME ATTACH POINT BS 400 STR 23 LT. REPLACED IAW SRM 53-10-2 BETWEEN BS 360 AND BS 440. 2 L 7 3 4F A3WE 1999043000494 19990430 00494 NM 1999 4 30 UPS99229432 1 19990407 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STR 23 RT CRACKED AT FRAME ATTACH POINTS BS 380 STR 23 RT. REPLACED BETWEEN BS 360 AND 440 IAW SR M 51-30-2. 2 L 7 3 4F A3WE 1999043000495 19990430 00495 NM 1999 4 30 UPS99229433 1 19990407 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STR 21 RT CRACKED AT FRAME ATTACH POINTS BS 380. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999043000496 19990430 00496 NM 1999 4 30 UPS99229434 1 19990407 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STR 24 LT CRACKED AT FRAME ATTACH POINTS. BS 420 STR 24L REPLACED BETWEEN BS 360 AND BS 440 IAW S RM 51-30-2. 2 L 7 3 4F A3WE 1999043000497 19990430 00497 NM 1999 4 30 UPS99229435 1 19990406 A 5313 BAC1498138 STRINGER BOEING 727 72731C 1384011 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STRINGER 24 RT CRACKED AT FRAME ATTACH POINTS. STR 24 RT REPLACED BETWEEN BS 360 AND BS 440 IAW S RM 51-30-2. 2 L 7 3 4F A3WE 1999043000498 19990430 00498 NM 1999 4 30 UPS99229436 1 19990323 A 5320 PLUG BOEING 727 72731C 1384011 NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON WINDOW PLUG BS 600 S13L. WINDOW PLUG REPLACED IAW MM 52-30-00. 2 L 7 3 4F A3WE 1999043000499 19990430 00499 NM 1999 4 30 UPS99229437 1 19990403 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 600-620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON LAP AT BS 600-620 STR 19 RT SIDE INTERNAL SURFACE. LAP REPAIRED IAW UP S EO B727-5330-0509 APPENDIX 8.3/8.4 FROM BS 600-700 STR 19 RT. 2 L 7 3 4F A3WE 1999043000500 19990430 00500 NM 1999 4 30 UPS99229438 1 19990327 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1160-1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 1160 TO 1183 BETWEEN S18L AND 19L. REPAIR CARRIED OUT IAW SMRO EO 99-08-009 (UPS FILE NR 727-53-2120). 2 L 7 3 4F A3WE 1999043000501 19990430 00501 NM 1999 4 30 UPS99229439 1 19990413 A 5751 6524646501 HINGE BOEING 727 72731C 1384011 NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, RT I/B AILERON CENTERING HINGE CORRODED. CENTERING HINGE REMOVED AND REPLACED IAW 27-10-01. 2 L 7 3 4F A3WE 1999043000502 19990430 00502 NM 1999 4 30 UPS99229440 1 19990412 A 5320 65194441 FITTING BOEING 727 72731C 1384011 NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, STRINGER 8 AFT OF BS 1183 LT LOWER FITTING FOUND CRACKED. FITTING REMOVED AND NEW FITTING INSTALL ED IAW SRM 51-30-2 AND MM 53-11-00. 2 L 7 3 4F A3WE 1999043000503 19990430 00503 NM 1999 4 30 UPS99229441 1 19990406 A 5320 FRAME BOEING 727 72731C 1384011 NM CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, AFT CARGO DOOR MOVABLE FAIRING IS CRACKED AT THE LOWER RAIL FWD FRAME ATTACH POINT. REPAIRED FRAM E IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1999043000504 19990430 00504 NM 1999 4 30 UPS99229442 1 19990329 A 5260 STAIR BOEING 727 72731C 1384011 NM AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CORROSION EVIDENT ABOVE NR 7 STAIRTHREAD FORWARD SUPPORT ANGLE ON RISER LOWER SURFACE. REPAIRED I AW SRM ADDENDUM EO 10-26-95. 2 L 7 3 4F A3WE 1999043000505 19990430 00505 NM 1999 4 30 UPS99229443 1 19990329 A 5320 POST BOEING 727 72731C 1384011 NM LT WINDOW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACK FOUND IN INTERNAL DOUBLER LT WINDOW POST 5 INCHES ABOVE POINT F. WINDOW POST REPAIRED IAW U PS EO B727-5310-0012 APP D. 2 L 7 3 4F A3WE 1999043000506 19990430 00506 NM 1999 4 30 UPS99229444 1 19990325 A 5320 6519850126 WINDOW FRAME BOEING 727 72731C 1384011 NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, ON REMOVAL OF WINDOW FRAME TWO SUSPECT CRACKS FOUND AT BS 1090 RT. WINDOW FRAME REPLACED IAW DRG 65-18384 AND SMRO EO 99-08-002R1 UPS ENG FILE NR 727-53-2119. 2 L 7 3 4F A3WE 1999043000507 19990430 00507 NM 1999 4 30 UPS99229445 1 19990322 A 5754 BULLNOSE BOEING 727 72731C 1384011 NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CORROSION ON NR 4 LEADING EDGE FLAP BULLNOSE. BULLNOSE REMOVED AND REPLACED IAW MM 27-81-01. 2 L 7 3 4F A3WE 1999043000508 19990430 00508 NM 1999 4 30 UPS99229446 1 19990405 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 670 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON LAP STR 19 BETWEEN BS 660 AND 680 RT SIDE. LAP REPAIRED IAW UPS EO B72 7-5330-0509 APP 8.3. 2 L 7 3 4F A3WE 1999043000509 19990430 00509 NM 1999 4 30 UPS99229447 1 19990322 A 5753 65236574 CASTING BOEING 727 72731C 1384011 NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CRACK ON OUTBOARD FLAP CONTROL VALVE SUPPORT CASTING IN ROOF OF RT MLG WHEEL WELL. REPLACED HOUSI NG IAW MM 27-51-51 AND OHM 20-50-02. 2 L 7 3 4F A3WE 1999043000510 19990430 00510 NM 1999 4 30 UPS99229448 1 19990322 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 1090 TO 1110, STR 10R STR 14R. REPAIR CARRIED OUT IAW SMRO EO 99-08-002R1 UPS ENG FILE NR 727-53-211 9. 2 L 7 3 4F A3WE 1999043000511 19990430 00511 NM 1999 4 30 UPS99229449 1 19990328 A 5753 65192067 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 3 FLAP TRACK SUSPECT CRACK AT AFT END OF TRACK. FLAP TRACK REMOVED AND REPLACED IAW TC C57-581 -04-03. 2 L 7 3 4F A3WE 1999043000512 19990430 00512 NM 1999 4 30 UPS99229450 1 19990327 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1175 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, LIGHT SURFACE CORROSION ON SKIN BS 1175 STR 6L. SKIN REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 1 BET WEEN STR 5L AND STR 8L BS 1183 TO 1170. 2 L 7 3 4F A3WE 1999043000513 19990430 00513 NM 1999 4 30 UPS99229455 1 19990424 A 5320 BEAM BOEING 727 72725C 138400H NM BS 1052 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CORROSION ON TRANSVERSE BEAM BL 0 STA 1052, WL 208. REPAIRED PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999043000514 19990430 00514 NM 1999 4 30 UPS99229456 1 19990424 A 5320 CLIP BOEING 727 72725C 138400H NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE-SI, CRACK IN STRINGER CLIP STA 1090 STR 3 RT. REPLACED CLIP IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999043000515 19990430 00515 NM 1999 4 30 UPS99229457 1 19990424 A 5320 CLIP BOEING 727 72725C 138400H NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACKED STRINGER CLIP STA 9 LT STA 1030. REPLACED CLIP IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999043000516 19990430 00516 NM 1999 4 30 UPS99229459 1 19990420 A 5320 BEAM BOEING 727 72725C 138400H NM BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACK IN VERTICAL BEAM WEB BS 1180 WL 281 RBL 26.83. INSTALLED REPAIR KIT PER UPS EO B727-5310-1137 . 2 L 7 3 4F A3WE 1999043000517 19990430 00517 NM 1999 4 30 UPS99229460 1 19990421 A 5753 651859930 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CORROSION (C57-581-04-00-03) ON NR 3 FLAP CARRIAGE INNER AND OUTER SURFACE OF SPINDLE AND NUMEROUS A REAS ON REST OF CARRIAGE. REPLACED CARRIAGE ASSEMBLY. 2 L 7 3 4F A3WE 1999043000518 19990430 00518 NM 1999 4 30 UPS99229461 1 19990421 A 5753 651920219 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CORROSION (C57-581.04.00-03) ON NR 1 FLAP CARRIAGE SPINDLE FORWARD OF THRUST WASHER. REPLACED CARRI AGE ASSEMBLY. 2 L 7 3 4F A3WE 1999043000519 19990430 00519 NM 1999 4 30 UPS99229462 1 19990421 A 5753 65185996 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, NR 5 FLAP CARRIAGE CORRODED ON I/B OF SPINDLE CORROSION (C57-581-04.00-04). REPLACED CARRIAGE ASSEM BLY. 2 L 7 3 4F A3WE 1999043000520 19990430 00520 WP 1999 4 30 UPS99829451 1 19990419 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C1, LT WING L/E SKIN AT FS 710 IS CRACKED AT THE AFT LWR CORNER. REPAIRED SKIN IAW SRM 51-2-1. 2 L 7 4 4F RT 4A25 1999043000521 19990430 00521 WP 1999 4 30 UPS99829452 1 19990413 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1240 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 1240 FRAME ABOVE LONGERON 21L HAS A HOLE DRILLED THRU THE RADIUS. REPAIRED FRAME IAW DH SK840-04 9. 2 L 7 4 4F RT 4A25 1999043000522 19990430 00522 WP 1999 4 30 UPS99829453 1 19990406 A 5320 3779659501 FITTING DOUG DC8 DC873F 302199F WP BS 902-920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, LONGERON 5L END FITTING AT FS 902-920 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000523 19990430 00523 WP 1999 4 30 UPS99829454 1 19990409 A 5720 3704841501 FITTING DOUG DC8 DC873F 302199F WP WS 74.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, RT WING O/B OF THE XRS 74.5 BULKHEAD, BOTH STRINGER 51 END FITTINGS ARE CRACKED. REMOVED AND REPLAC ED FITTINGS IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000524 19990430 00524 WP 1999 4 30 UPS99829458 1 19990405 A 5347 601517670T6 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1040 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, SEAT TRACK RBL 24 AT FS 1040 IS CRACKED AND CORRODED. REMOVED SEAT TRACK FROM FS 970 TO 1090, FABRI CATED AND INSTALLED SEAT TRACK IAW EO DC8-5320-5167. 2 L 7 4 4F RT 4A25 1999043000525 19990430 00525 EU 1999 4 30 QXEA9900705 1 19990325 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, FRAME 13815A BETWEEN STRINGER 2 AND 3 THE CASTELLATION IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-1 3 PAGE 4. 2 L 7 2 4F RT A20EU 1999043000526 19990430 00526 EU 1999 4 30 QXEA9900706 1 19990323 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, FRAME 13815B AND BETWEEN STRINGERS 74 AND 73 IS CRACKED AT THE CASTELLATION. REPAIRED IAW FOKKER S RM 53-02-13, PAGE 4 AND SRM 51-31-1. 2 L 7 2 4F RT A20EU 1999043000527 19990430 00527 EU 1999 4 30 QXEA9900707 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, CORROSION ON THE CASTELLATION ABOVE STRINGER 74 AT FRAME 13815A. REPAIRED IAW FOKKER SRM 51-10-4 P AGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000528 19990430 00528 EU 1999 4 30 QXEA9900708 1 19990324 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, THE CASTELLATION AT FRAME 13815B HAS A CRACK AT STRINGER 2. REPAIRED IAW FOKKER SRM 52-02-13, PAGE 4 AND SRM 51-31-01, PAGE 13. 2 L 7 2 4F RT A20EU 1999043000529 19990430 00529 EU 1999 4 30 QXEA9900709 1 19990325 A 5320 DRAIN FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, THE DRAIN PLATE HAS CORROSION AT NUT PLATES, LOCATED BETWEEN FRAMES 14755 AND 14285 AND STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999043000530 19990430 00530 EU 1999 4 30 QXEA9900710 1 19990324 A 5320 WASHER FOKKER F28 F28MK4000 4990810 EU FRAME 15025 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, AT FRAME 15205 AND STRINGER 94 THE WASHER ON THE CASTELLATION IS CORRODED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-1. 2 L 7 2 4F RT A20EU 1999043000531 19990430 00531 EU 1999 4 30 QXEA9900711 1 19990322 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, FRAME 15205 THERE IS CORROSION ON THE CASTELLATION BETWEEN STRINGERS 5 AND 6. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000532 19990430 00532 EU 1999 4 30 QXEA9900712 1 19990317 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, THERE ARE FIVE SPOTS OF CORROSION ON SKIN SURFACE LOCATED BETWEEN FRAMES 15635, 15205 AND STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000533 19990430 00533 EU 1999 4 30 QXEA9900713 1 19990318 A 5532 DOUBLER FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, THERE IS CORROSION ON AND IN THE NR 3 VHF COMM DOUBLER AND STIFFENER, LOCATED BETWEEN FRAMES 15635, 15205 AND STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000534 19990430 00534 EU 1999 4 30 QXEA9900714 1 19990317 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, 40MM FORWARD OF FRAME 15635 AND BETWEEN STRINGERS 1 AND 2 CORRODED. REPAIRED IAW FOKKER SRM 51-10- 4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000535 19990430 00535 EU 1999 4 30 QXEA9900715 1 19990325 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, FRAME 16660 THE CASTELLATION IS CRACKED AT STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999043000536 19990430 00536 EU 1999 4 30 QXEA9900716 1 19990323 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, FRAME 16660 THE CASTELLATION IS CRACKED AT STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999043000537 19990430 00537 EU 1999 4 30 QXEA9900717 1 19990323 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, FRAME 16660 THE CASTELLATION IS CRACKED AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000538 19990430 00538 EU 1999 4 30 QXEA9900718 1 19990325 A 5320 WASHER FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY, THE CASTELLATION WASHER AT FRAME 14755 AND STRINGER 74 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-1 0-4, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999043000539 19990430 00539 EU 1999 4 30 QXEA9900719 1 19990319 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME 8305 HAS CORROSION AT STRINGER 74 AT RIVET BY LIGHTENING HOLE UNDER NUT PLATE. REPAIRED IAW FOKKER SRM 51-1 0-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000540 19990430 00540 EU 1999 4 30 QXEA9900720 1 19990324 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION AT FRAME 7805 AND STRINGER 74 UNDER NUT PLATES. REPAIRED IAW HORIZON AIR EA 4-53-723. 2 L 7 2 4F RT A20EU 1999043000541 19990430 00541 EU 1999 4 30 QXEA9900721 1 19990318 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 7305 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - DENT IN FUSELAGE AT FRAME 7305 AND STRINGER 67. REPAIRED IAW FOKKER SRM 51-10-04, PAGES 8 AND 9. 2 L 7 2 4F RT A20EU 1999043000542 19990430 00542 EU 1999 4 30 QXEA9900722 1 19990323 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON FRAME 7305 BETWEEN STRINGERS 2 AND 73. REPAIRED IAW HORIZON AIR EA 4-53-722. 2 L 7 2 4F RT A20EU 1999043000543 19990430 00543 EU 1999 4 30 QXEA9900723 1 19990321 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON FRAME 6805 BETWEEN STRINGERS 2 AND 73, UNDER NUT PLATES AND LOWER SURFACE. REPAIRED IAW FOKKER SRM 5 3-01-01. 2 L 7 2 4F RT A20EU 1999043000544 19990430 00544 EU 1999 4 30 QXEA9900724 1 19990319 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6065 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON INSIDE SKIN OF ANTENNA MOUNTING AREA BETWEEN FRAMES 5805, 6065 AND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000545 19990430 00545 EU 1999 4 30 QXEA9900725 1 19990319 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 6305-6565 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON STRINGER 74 BETWEEN FRAMES 6305 AND 6565. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000546 19990430 00546 EU 1999 4 30 QXEA9900726 1 19990319 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 6305-6565 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON STRINGER 1 BETWEEN FRAMES 6305 AND 6565. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000547 19990430 00547 EU 1999 4 30 QXEA9900727 1 19990401 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FRAME 12075 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND MAIN LANDING GEAR HINGE MOUNTING BEAM ON AIRCRAFT HAS STEP WEAR AND CORROSION AT FORWARD AND AFT ENDS. A LSO, ON BEAM BOTTOM BETWEEN FRAMES 12075 AND 13109. REPAIRED IAW HORIZON AIR EA 4-53-733. 2 L 7 2 4F RT A20EU 1999043000548 19990430 00548 EU 1999 4 30 QXEA9900728 1 19990320 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO DOOR, FORWARD FACE OF CARGO DOOR IS DENTED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999043000549 19990430 00549 EU 1999 4 30 QXEA9900729 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT STRINGER AND FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000550 19990430 00550 EU 1999 4 30 QXEA9900730 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT FRAME 7805 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000551 19990430 00551 EU 1999 4 30 QXEA9900731 1 19990318 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACK AT FRAME 8305 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000552 19990430 00552 EU 1999 4 30 QXEA9900732 1 19990318 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT FRAME 8805 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000553 19990430 00553 EU 1999 4 30 QXEA9900733 1 19990318 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT FRAME 8805 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000554 19990430 00554 EU 1999 4 30 QXEA9900734 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT FRAME 8805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000555 19990430 00555 EU 1999 4 30 QXEA9900735 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT FRAME 8805 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000556 19990430 00556 EU 1999 4 30 QXEA9900736 1 19990318 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT FRAME 9305 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000557 19990430 00557 EU 1999 4 30 QXEA9900737 1 19990324 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CRACKED CLIP AT FRAME 9305A AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000558 19990430 00558 EU 1999 4 30 QXEA9900738 1 19990407 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - TWO CHAFES AT SERVICE EMERGENCY DOOR APERTURE IN FRAME 4610 OUTBOARD OF MAIN GUIDE TRACK. REPAIRED IAW HORIZON AI R EA 4-53-752. 2 L 7 2 4F RT A20EU 1999043000559 19990430 00559 EU 1999 4 30 QXEA9900739 1 19990324 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 12875 CLIP CRACKED AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-0 1. 2 L 7 2 4F RT A20EU 1999043000560 19990430 00560 EU 1999 4 30 QXEA9900740 1 19990324 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 12875 CLIP CRACKED AT TOP SIDE OF STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000561 19990430 00561 EU 1999 4 30 QXEA9900741 1 19990324 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10340 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 10340 CLIP CRACKED AT TOPSIDE OF STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000562 19990430 00562 EU 1999 4 30 QXEA9900742 1 19990321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 11405 CLIP CRACKED AT TOP SIDE OF STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000563 19990430 00563 EU 1999 4 30 QXEA9900743 1 19990320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 13815 CLIP CRACKED AT TOP SIDE OF STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000564 19990430 00564 EU 1999 4 30 QXEA9900744 1 19990323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 13815A CLIP CRACKED AT TOP SIDE OF STRINGER 58. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000565 19990430 00565 EU 1999 4 30 QXEA9900745 1 19990321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 14285 CLIP HAS 3 INCH CRACK BETWEEN STRINGERS 33 AND 34. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 5, FI GURE 1, SHEET 2 OF 2. 2 L 7 2 4F RT A20EU 1999043000566 19990430 00566 EU 1999 4 30 QXEA9900746 1 19990321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 14285 CLIP CRACKED FROM STRINGER 32 TO 33. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 5, FIGURE 1, SHEET 2 OF 2. 2 L 7 2 4F RT A20EU 1999043000567 19990430 00567 EU 1999 4 30 QXEA9900747 1 19990326 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 14755 CLIP CRACKED AT TOP SIDE OF STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000568 19990430 00568 EU 1999 4 30 QXEA9900748 1 19990326 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 14755 CLIP CRACKED AT TOP SIDE OF STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000569 19990430 00569 EU 1999 4 30 QXEA9900749 1 19990320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 59. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000570 19990430 00570 EU 1999 4 30 QXEA9900750 1 19990320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000571 19990430 00571 EU 1999 4 30 QXEA9900751 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000572 19990430 00572 EU 1999 4 30 QXEA9900752 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000573 19990430 00573 EU 1999 4 30 QXEA9900753 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000574 19990430 00574 EU 1999 4 30 QXEA9900754 1 19990319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000575 19990430 00575 EU 1999 4 30 QXEA9900755 1 19990324 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 53. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000576 19990430 00576 EU 1999 4 30 QXEA9900756 1 19990324 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 52. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000577 19990430 00577 EU 1999 4 30 QXEA9900757 1 19990318 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13, PARAGRAPH 4, FIGU RE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000578 19990430 00578 EU 1999 4 30 QXEA9900758 1 19990318 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP AND BOTTOM SIDE OF STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13, PARAGRAPH 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000579 19990430 00579 EU 1999 4 30 QXEA9900759 1 19990318 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000580 19990430 00580 EU 1999 4 30 QXEA9900760 1 19990326 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000581 19990430 00581 EU 1999 4 30 QXEA9900761 1 19990326 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP SIDE OF STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000582 19990430 00582 EU 1999 4 30 QXEA9900762 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT BOTTOM SIDE OF STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000583 19990430 00583 EU 1999 4 30 QXEA9900763 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 CLIP CRACKED AT TOP AND BOTTOM SIDE OF STRINGER 23. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, F IGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000584 19990430 00584 EU 1999 4 30 QXEA9900764 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT BOTTOM SIDE OF STRINGER 22. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000585 19990430 00585 EU 1999 4 30 QXEA9900765 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 21 THROUGH TWO RIVET HOLES. REPAIRED IAW FOKK ER SRM 53-02-11 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000586 19990430 00586 EU 1999 4 30 QXEA9900766 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 20. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000587 19990430 00587 EU 1999 4 30 QXEA9900767 1 19990312 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000588 19990430 00588 EU 1999 4 30 QXEA9900768 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CABIN FRAME 15205 FORWARD SIDE CLIP CRACKED AT TOP SIDE OF STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000589 19990430 00589 EU 1999 4 30 QXEA9900769 1 19990322 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 4875-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 4875 AND 5305 HAS ONE AREA OF PITTING CORROSION ON I NBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000590 19990430 00590 EU 1999 4 30 QXEA9900770 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5305-9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 5305 AND 9805 HAS PITTING AND FRETTING CORROSION ON FLANGES ALONG LENGTH AFT OF STATION 5700. REPAIRED IAW FOKKER SRM 53-40-01, FIGURE 204. 2 L 7 2 4F RT A20EU 1999043000591 19990430 00591 EU 1999 4 30 QXEA9900771 1 19990409 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805-14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 9805 AND 14285 HAS PITTING AND FRETTING CORROSION A LONG ENTIRE LENGTH ON FLANGES. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000592 19990430 00592 EU 1999 4 30 QXEA9900772 1 19990319 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND INBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 14285 AND 15635 HAS LIGHT FRETTING CORROSION ALONG ENTIRE LENGTH OF FLANGE AND TWO GOUGES IN LEFT-HAND FLANGE AT FRAME 14755. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SEC TION 4. 2 L 7 2 4F RT A20EU 1999043000593 19990430 00593 EU 1999 4 30 QXEA9900773 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 14285 AND 15635 HAS FRETTING AND PITTING CORROSION IN FLANGES FORWARD OF FRAME 15205. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043000594 19990430 00594 EU 1999 4 30 QXEA9900774 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805-14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 9805 AND 14285 HAS PITTING AND FRETTING CORROSION ALONG ENT IRE LENGTH OF FLANGES. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043000595 19990430 00595 EU 1999 4 30 QXEA9900775 1 19990415 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805-14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND INBOARD SEAT TRACK SECTION BETWEEN SPLICES AT FRAME 9805 AND 114285 HAS LIGHT FRETTING CORROSION ALONG ENTIRE LENGTH OF FLANGE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000596 19990430 00596 EU 1999 4 30 QXEA9900776 1 19990319 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU SERVICE DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - UPPER AFT CORNER OF SERVICE EMERGENCY DOOR APERTURE REQUIRES EXTERNAL DOUBLER INSTALLATION. REPAIRED IAW HORIZON AIR EA 4-53-703. 2 L 7 2 4F RT A20EU 1999043000597 19990430 00597 EU 1999 4 30 QXEA9900777 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14323 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 14323. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000598 19990430 00598 EU 1999 4 30 QXEA9900778 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 11794 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 11794. REPAIRED IAW FOKKER SRM 51-10-14, SECT ION 4 PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000599 19990430 00599 EU 1999 4 30 QXEA9900779 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 9305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000600 19990430 00600 EU 1999 4 30 QXEA9900780 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 7805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 , SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000601 19990430 00601 EU 1999 4 30 QXEA9900781 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 6305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 6305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 , SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000602 19990430 00602 EU 1999 4 30 QXEA9900782 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 16745 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 16745. REPAIRED IAW FOKKER SRM 53-40-01, PAG E 206, FIGURE 205 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999043000603 19990430 00603 EU 1999 4 30 QXEA9900783 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 16203 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 16203. REPAIRED IAW FOKKER SRM 53-40-01, PAG E 206, FIGURE 205 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999043000604 19990430 00604 EU 1999 4 30 QXEA9900784 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 15733 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 15733. REPAIRED IAW FOKKER SRM 53-40-01, PAG E 206, FIGURE 205 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999043000605 19990430 00605 EU 1999 4 30 QXEA9900785 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 14323 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 14323. REPAIRED IAW FOKKER SRM 53-40-01, PAG E 206, FIGURE 205 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999043000606 19990430 00606 EU 1999 4 30 QXEA9900786 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13353 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION IN TWO AREAS INSIDE TRACK AT STATION 13353. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SECTION 4, PARAGRAPH B1 AND 2. 2 L 7 2 4F RT A20EU 1999043000607 19990430 00607 EU 1999 4 30 QXEA9900787 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 10203 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION IN TWO AREAS INSIDE TRACK AT STATION 10203. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999043000608 19990430 00608 EU 1999 4 30 QXEA9900788 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 11253 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 11253. REPAIRED IAW FOKKER SRM 53-40-01, PAG E 206, FIGURE 205 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999043000609 19990430 00609 EU 1999 4 30 QXEA9900789 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION 9305. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043000610 19990430 00610 EU 1999 4 30 QXEA9900790 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS SCORING 8 INCHES LONG WITH CORROSION AT STATION 8805. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, FIGURE 205. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999043000611 19990430 00611 EU 1999 4 30 QXEA9900791 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION 7805. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, F IGURE 205 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999043000612 19990430 00612 EU 1999 4 30 QXEA9900792 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE TRACK IN 4 INCH AREA ADJACENT TO FRAME 15205. REPAIRED I AW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B1 AND 2. 2 L 7 2 4F RT A20EU 1999043000613 19990430 00613 EU 1999 4 30 QXEA9900793 1 19990413 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT SCRATCHES INSIDE IN A 2 INCH AREA ADJACENT TO FRAME 14755. REPAIRED IAW F OKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999043000614 19990430 00614 EU 1999 4 30 QXEA9900794 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL AREA OF SURFACE CORROSION ADJACENT TO FRAME 13815. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999043000615 19990430 00615 EU 1999 4 30 QXEA9900795 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13345 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS 2 SMALL GOUGES BETWEEN FRAMES 13345 AND 13815. REPAIRED IAW FOKKER SRM 53-01-01 , PAGE 5. 2 L 7 2 4F RT A20EU 1999043000616 19990430 00616 EU 1999 4 30 QXEA9900796 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11703 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS TWO GOUGES IN CIRCUMFERENCE OF SEAT TRACK HOLE 2 INCHES AFT OF FRAME 11703. REP AIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000617 19990430 00617 EU 1999 4 30 QXEA9900797 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12875 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SCRATCH 6 INCHES AFT OF FRAME 12875. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 2 06, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043000618 19990430 00618 EU 1999 4 30 QXEA9900798 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11703 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN FRAME 11703 AND 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000619 19990430 00619 EU 1999 4 30 QXEA9900799 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL AREA OF CHAFE DAMAGE 2 INCHES FORWARD OF FRAME 11405. REPAIRED IAW FOKK ER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000620 19990430 00620 EU 1999 4 30 QXEA9900800 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION BETWEEN FRAME 10966 AND 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000621 19990430 00621 EU 1999 4 30 QXEA9900801 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL AREA OF CORROSION 2 INCHES FORWARD OF FRAME 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000622 19990430 00622 EU 1999 4 30 QXEA9900802 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION EXTENDING 5 INCHES FORWARD AND AFT OF FRAME 10346. REPAIRED IAW FOKKE R SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999043000623 19990430 00623 EU 1999 4 30 QXEA9900803 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION BETWEEN FRAME 9305C AND 9805. REPAIRED IAW FOKKER SRM 53-40-1, PAGE 2 01, PARAGRAPH 4(B). 2 L 7 2 4F RT A20EU 1999043000624 19990430 00624 EU 1999 4 30 QXEA9900804 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION EXTENDING 5 INCHES FORWARD AND AFT OF FRAME 9305B. REPAIRED IAW FOKKER SRM 53-40-1, PAGE 201, PARAGRAPH 4(B). 2 L 7 2 4F RT A20EU 1999043000625 19990430 00625 NM 1999 4 30 99FDEA00162 1 19990426 A 5315 654202736 FLOORBEAM BOEING 727 727116C NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 115FE 19814 FLOORBEAM BLENDED THRU AT RBL - 9.0 & LBL 4.0 REPAIR PER DALFORT XEA-X1-53-698 DATED 4/19/99. THE ABOVE MENTIONED NR CR EATED AN XEA TO ACCOMPLISH THE REPAIR. REPAIR IN PROGRESS. *S/D* REPAIRED PER FEDEX ENG AUTH NR 7-5310-45238 & DAL AE RO LP XEA-X1-53-698. 2 L 7 3 4F A3WE 1999043000626 19990430 00626 WP 1999 4 30 ABXA9900322 1 19990427 A 3231 RETRACT MECH DOUG DC8 DC861 3021952 WP NLG DOOR MALFUNCTIONED A ABXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 23 846AX 46158 LEFT NOSE GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION. RECYCLED GEAR. DUE TO EXCESSIVE VIBRATION, RETURNED TO DAL. C REW REPORTED DOOR CLOSED AT TOUCHDOWN AND DOOR WAS CLOSED UPON ARRIVAL AT GATE. INSPECTED GEAR DOORS, FORWARD DOOR LATC HES, LINKAGE AND FUSELAGE. NO DAMAGE OR DISCREPANCIES FOUND. 2 L 7 4 4F 4A25 1999043000627 19990430 00627 EU 1999 4 30 R7MA0000559 1 19990312 A 6730 280073 BEARING AGUSTA A109 A109K2 0260502 EU SERVO SPALLED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 10016 BEARING SPALLING. (X) 1 G 7 2 3U RT H7EU 1999043000628 19990430 00628 EU 1999 4 30 R7MA0000564 1 19990311 A 2823 DV1368 VALVE AGUSTA A109 A109K2 0260502 EU FUEL SYSTEM CLOGGED A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 109RX 10016 BOTH VALVES CLOGGED AND LEAKING. (X) 1 G 7 2 3U RT H7EU 1999043000629 19990430 00629 EU 1999 4 30 R7MA0000565 1 19990310 A 2810 RUBBER 109070805105 AGUSTA A109 A109K2 0260502 EU FUEL TANK FLAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 65090 10016 RUBBER FLAKING JUST INSIDE FILLER NECK. 1 G 7 2 3U RT H7EU 1999043000631 19990430 00631 NE 1999 4 30 99ZZZX1798 2 19990225 A 7210 230001302 BEARING BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE GEARBOX WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 404EM 299 98199142755 47514 LE47003EA BEARING WORN BEYOND SERVICEABLE LIMITS. INSTALLED AT ASE GREER FACILITY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H9SW E5NE 1999043000633 19990430 00633 EU 1999 4 30 99ZZZX1800 1 19990402 A 2150 JBS8803 MIXING VALVE UROCOP EC135 EC135P1 8680990 EU HEATER INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 294 036 EC1350054 MIXING VALVE UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999043000634 19990430 00634 NE 1999 4 30 99ZZZX1801 2 19990328 A 7250 411105067 ROTOR ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 755 BE9396 7077 LE45111EA SECONDARY DAMAGE TO LAB SEAL FAILURE. EXCESSIVE DAMAGE TO KNIFE EDGES AND GP BLADES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TC: 1,061.9. 1 G 7 2 3U 3 U H13EU E5NE 1999043000635 19990430 00635 NE 1999 4 30 99ZZZX1802 2 19990328 A 7230 411104059 SEAL ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE LABYRINTH DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 1775 7077 LE45111EA EXCESSIVE WARPAGE WHICH RESULTED IN COLLATERAL DAMAGE TO THE GP ROTOR AND SHROUD. REPLACED WITH NEW UNIT, CORRECTED PRO BLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000636 19990430 00636 EU 1999 4 30 99ZZZX1803 1 19990319 A 7714 L772M10C1002 INDICATOR UROCOP EC135 EC135P1 8680990 EU COCKPIT INOPERATIVE A R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 11 135SJ 150 0035 EC1350054 TOT INDICATOR INOPERATIVE. UNIT INOPERATIVE. WOULD NOT SELF-TEST WHEN POWER APPLIED. WILL NOT OPERATE WHILE ENGINE IS RUNNING. 1 G 7 2 3U O H88EU 1999043000637 19990430 00637 EU 1999 4 30 R7MA0000607 1 19990413 A 2810 RUBBER 109090021 AGUSTA A109 A109K2 0260502 EU FUEL CELL PEELING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 65180 10018 RUBBER COATING PEELING OFF EXTERIOR FUEL CELL. (X) 1 G 7 2 3U RT H7EU 1999043000638 19990430 00638 EU 1999 4 30 R7MA0000608 1 19990413 A 2810 RUBBER 109090021 AGUSTA A109 A109K2 0260502 EU FUEL CELL PEELING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 65131 10018 RUBBER COATING PEELING OFF EXTERIOR FUEL CELL. (X) 1 G 7 2 3U RT H7EU 1999043000639 19990430 00639 CE 1999 4 30 R7MA0000595 1 19990408 A 7331 903800097 TRANSMITTER BEECH 200 B200 1152922 CE FUEL FLOW FLUCTUATING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 301HC 3179EX BB1219 TRANSMITTER CAUSES INDICATING FLUCTUATIONS. (X) 1 L 7 2 4T A24CE 1999043000643 19990430 00643 1999 4 30 R7MA0000594 4 19990407 A 3422 6226136002 GYRO COMPASS BEECH 200 B200 1152922 CE COCKPIT INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 501HC 3711 BB1306 NR 1 SYSTEM FAILED ON GROUND DURING TROUBLESHOOTING OF NR 2 SYSTEM. NR 1 SYSTEM INOPERATIVE. (X) 1 L 7 2 4T A24CE 1999043000646 19990430 00646 EU 1999 4 30 99ZZZX1809 1 19990319 A 7714 L772M10C1002 INDICATOR UROCOP EC135 EC135P1 8680990 EU COCKPIT FAILED A R7MA E ENGINE SHUTDOWN W INADEQUATE Q C IN INSP/MAINT 1 NM 11 135SJ 0024 EC1350054 INDICATOR REJECTED NEW OUT-OF-BOX. WOULD NOT SELF-TEST WHEN POWER APPLIED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999043000647 19990430 00647 SO 1999 4 30 99ZZZX1810 2 19990401 A 8530 646476 CONNECTING ROD BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO LT ENGINE FAILED A PA9A E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 03 103GA TH213 298988R THE LEFT ENGINE APPARENTLY EXPERIENCED A FAILURE OF THE NR 6 CYLINDER PISTON CONNECTING ROD DURING NORMAL FLIGHT CONDITI ONS. THE PILOT RETURNED TO THE AIRPORT WITHOUT FURTHER INCIDENT. THE ENGINE WAS SHUT DOWN WHEN THE OIL PRESSURE DROPPE D RAPIDLY. ENGINE TOTAL TIME WAS APPROXIMATELY 985.0 HOURS. THIS IS A FACTORY RE-MANUFACTURED ENGINE. 1 L 7 2 3O 3 O 3A16 E5CE 1999043000664 19990430 00664 CE 1999 4 30 99ZZZX1827 1 19990401 A 3260 426EN98 SWITCH LEAR 35 35A 5170602 CE RT MLG FAILED A IF1A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 23 358PG 35A358 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE AIRPORT WITHOUT INCIDENT. UPON MAINTEN ANCE EXAMINATION, DETERMINED THE RIGHT MAIN GEAR 'SQUAT SWITCH' HAD MALFUNCTIONED AND ELECTRICALLY PREVENTED GEAR RETRAC TION. THE SWITCH WAS REPLACED AND NORMAL OPERATION WAS RESTORED. 2 L 7 2 4F A10CE 1999043000668 19990430 00668 NM 1999 4 30 HNAA9900051 1 19990423 A 3350 6104791X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 930HA 126 FORWARD LEFT HAND INTERIOR FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 H 7 2 4T RT A13NM 1999043000669 19990430 00669 NM 1999 4 30 HNAA9900052 1 19990423 A 5730 BRACKET DHAV DHC8 DHC8102 2809003 NM LT WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 132 LEFT WING FLAP WELL PANEL MOUNT BRACKET (SECONDARY STRUCTURE) UNDER OUTBOARD ROLL SPOILER ACTUATING HINGE CRACKED ON FOR WARD OUTBOARD EDGE OF OUTBOARD LIGHTENING HOLE. REPAIRED CRACK. 2 H 7 2 4T RT A13NM 1999043000670 19990430 00670 NM 1999 4 30 HNAA9900053 1 19990423 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 202 DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 132 DENT ON RIGHT FUSELAGE FROM LAVATORY CAP HANDLE, LOCATED .5 INCHES BELOW STRINGER 265 RIVET ROW 2 INCHES FORWARD OF FRAM E X202. DENT IS .020 INCHES DEEP, 1.2 INCHES LONG AND .4 INCHES WIDE. INSPECTED DENT AND DEFERRED. 2 H 7 2 4T RT A13NM 1999043000671 19990430 00671 WP 1999 4 30 AT9900329 1 19990322 A 5540 59133161 BRACKET DOUG DC9 DC932 3022066 WP RUDDER CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE YAW DAMPER MOUNT BRACKET CORRODED AT ALL FOUR ATTACHED LUGS. REMOVED AND REPLACED RUDDER YAW DAMPER MOUNT BRACKET, COMPLETE RUDDER SYSTEM CABLE TENSION AND RIG CHECK GOOD IAW DC9 MM 22-11-2 , 20-16-0, AND 27-20-0. 2 L 7 2 4F A6WE 1999043000672 19990430 00672 WP 1999 4 30 AT9900330 1 19990322 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 832-915 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO PIT CENTER FLOOR PANEL AT BS 832-915 CORRODED, PUNCTURED AND DENTED. FABRICATED FLOOR PANEL, DRILLED, DEBURRED, ALODINED IAW DC9 SRM 51-10-2, 51-10-3 AND 53-21-0 FIG 10. 2 L 7 2 4F A6WE 1999043000673 19990430 00673 WP 1999 4 30 AT9900331 1 19990322 A 5347 52955978 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 756-845 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO PIT SEAT TRACK ON THE RIGHT SIDE AT BS 756-845 CORRODED. ME CHANICALLY REMOVED CORROSION, DRILLED, COUNTERSINK, TREATED, AND PRIMED REPAIR TRACK IAW DC9 SRM 51-10-3, 51-10-4, AND 5 3-05 FIG 4C. 2 L 7 2 4F A6WE 1999043000674 19990430 00674 WP 1999 4 30 AT9900332 1 19990325 A 5330 PANEL DOUG DC9 DC932 3022066 WP BS 340 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT LEFT SLANT ACCESS PANEL COVER AT BS 340 CORRODED AND GOUGE D. FABRICATED NEW ACCESS PANEL, ALODINED AND PRIMED IAW DC9 SRM 51-10-3, 51-10-2, 53-21-0 AND 51-10-4. 2 L 7 2 4F A6WE 1999043000675 19990430 00675 EU 1999 4 30 MALA976438 1 19990422 A 2613 HOT LIGHT SAAB SF340 340B 7860101 EU RT ENGINE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 421XJ 421 RIGHT ENGINE TAIL PIPE HOT LIGHT ILLUMINATED ON DEPARTURE. POWER REDUCED TO 20-30 PERCENT TORQUE AND LIGHT EXTINGUISHED . MAINTENANCE COULD NOT DUPLICATE PROBLEM, INSPECTED FIRE DETECTORS IN TAIL PIPE AND OHMED ALL WIRES. NO DEFECTS NOTED IN RIGHT ENGINE. 2 L 7 2 4T RT A52EU 1999043000676 19990430 00676 EU 1999 4 30 MALA976439 1 19990422 A 3040 SWITCH SAAB SF340 SF340A 7850100 EU LT WINDSHIELD MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 103XJ 340A103 LEFT FRONT WINDSHEILD LIGHT ILLUMINATES IN FLIGHT WITH ASSOCIATED MASTER CAUTION. AT FIRST, LIGHT WOULD CYCLE ON AND OF F BY ITSELF, BUT LATER IT CAME ON AND REMAINED ON UNLESS SWITCH WAS CYCLED. FOLLOWED QRH. MAINTENANCE REPLACED LEFT FR ONT WINDSHEILD LIGHT SWITCH. SECURITY AND OPS CHECKED GOOD. 2 L 7 2 4T RT A52EU 1999043000677 19990430 00677 EU 1999 4 30 MALA976440 1 19990422 A 3350 LIGHT SAAB SF340 340B 7860101 EU ROW 4 & 5 LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 423XJ 423 EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 4 & 5 COMING UNSECURED. MAINTENANCE RESECURED EMERGENCY FLOOR TRACK LIGHTIN G BETWEEN ROWS 4 & 5. 2 L 7 2 4T RT A52EU 1999043000678 19990430 00678 NE 1999 4 30 MALA976441 2 19990422 A 7200 COVER SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MISSING A MALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 GL 15 424XJ 424 AFTER TAKEOFF APPROX 300-400 FT, THE RIGHT ENGINE OIL PRESSURE WARNING ILLUMINATED PROCEEDED WITH QRH CHECK LIST. WHILE IN THAT CHECK LIST, ENGINE FAILED. COMPLETED QRH AND RETURNED TO MSP. ENGINE OIL PRESSURE WAS INDICATING 0 PSI. ON P OST FLIGHT, OIL ON NACELLE AND COMING OUT OF ENGINE. MAINTENANCE INSPECTED AND FOUND AXIS-A COVER OR RADIAL DRIVE SHAFT COVER DISLODGED, RESULTING IN OIL LOSS. MAINTENANCE REPLACED RIGHT ENGINE AND CLEARED ALL DISCREPANCIES NOTED DURING ENGINE CHANGE. ALL LEAK AND OPS CHECKS GOOD PER 71-00-00. PERFORMED GPA RUNS AND BREAKIN RUNS. ALL RUNS CHECKED GOOD PER 71-00-00 AND 72-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 1999043000679 19990430 00679 SO 1999 4 30 LR7A9919 1 19990412 A 5730 3631871R PANEL LKHEED 382 382G 526414U SO BS 617 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C-CHECK/BRIDGING INSPECTION, FOUND FS 617 AFT RT CENTER WING PRESSURE PANEL CORRODED. REPAIRED BY CORROSION BLEN D OUT AND DOUBLER INSTALLATION PER SPAR MPP L100-404-99-056. LAC MEA 382-57-99-054. 2 H 7 4 4T A1SO 1999043000680 19990430 00680 SO 1999 4 30 LR7A9920 1 19990412 A 5320 3305021 SPLICE LKHEED 382 382G 526414U SO BS 766.75 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C-CHECK/BRIDGING INSPECTION, FOUND FS 737E TO 817E RT AFT CHINE PLATE SPLICE CRACKED. ACCOMPLISHED TEMPORARY REP AIR BY STOP DRILLING CHINE ANGLE CRACK AND INSTALLING NEW REPAIR ANGLES IAW SPAR MPP L100-404-99-058, DWG R99-0002-11. L AC MEA 382-53-99-056. CHINE PLATE DUE REPLACEMENT BY 42301.5 TAT. 2 H 7 4 4T A1SO 1999043000681 19990430 00681 SO 1999 4 30 LR7A9921 1 19990412 A 5320 38968113 ANGLE LKHEED 382 382G 526414U SO BS 574.7-576 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C-CHECK/BRIDGING INSPECTION, FOUND LT CHINE ANGLE, CENTER FUSELAGE CRACKED AT FS 574.7 TO 576, RBL 61.6, WL 143. REPAIRED BY STOP DRILLING CRACK AND INSTALLING REPAIR ANGLE AND FILLER IAW SPAR MPP L100-404-99-059. LAC MEA 382-53-99 -057. 2 H 7 4 4T A1SO 1999043000682 19990430 00682 SO 1999 4 30 LR7A9922 1 19990412 A 5330 SKIN LKHEED 382 382G 526414U SO BS 777 MISDRILLED A LR7A K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 404LC 4763 DURING C-CHECK/BRIDGING INSPECTION, FOUND 2 MISDRILLED HOLES AT FS 777.0E FUSELAGE SKIN. REPAIRED BY INSTALLING DOUBLER S IAW SPAR MPP L100-404-99-057, DWG R99-0002-03. LAC MEA 382-53-99-055. 2 H 7 4 4T A1SO 1999043000683 19990430 00683 SO 1999 4 30 LR7A9923 1 19990412 A 5711 3705365 SPAR CAP LKHEED 382 382G 526414U SO CENTER WING CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C-CHECK/BRIDGING INSPECTION, FOUND CENTER WING, REAR BEAM, UPPER CAP CORRODED AT RBL 57 TO 62. REPAIRED WITH FIL LER AND DOUBLER INSTALL IAW SPAR MPP L100-404-99-060. LAC MEA 382-53-9-058. 2 H 7 4 4T A1SO 1999043000684 19990430 00684 NM 1999 4 30 CALA9900444 1 19990426 A 2560 D306XX SPRING BOEING 757 757224 1384958 NM R2 DOOR SLIDE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 R2 DOOR SLIDE RETAINING PIN STRING WORN. REPLACED SLIDE PACK RETAINING STRING PER AIR CRUISERS COMPANY SLIDE FOLDING PR OCEDURE MM P-11883. 2 L 7 2 4F RT A2NM 1999043000685 19990430 00685 EA 1999 4 30 COMA9960173 1 19990426 A 2750 860D10018ABC FECU 855D1009 CNDAIR CL600 CL6002B19 EA LT TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 769CA 6645 201A 7292 FLAPS FAIL MESSAGE. REPLACED THE LEFT HAND BPSU AND THE FECU. 2 L 7 2 4F RT A21EA 1999043000686 19990430 00686 EA 1999 4 30 COMA9960174 1 19990426 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 769CA 2020 70 7292 FLAP FAIL MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999043000687 19990430 00687 EA 1999 4 30 COMA9960175 1 19990424 A 3260 16215107 BRACKET CNDAIR CL600 CL6002B19 EA NLG BENT A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 991CA 7216 NLG DISAGREE MESSAGE. REPLACED THE NLG CENTERING PROXIMITY SWITCH BRACKET. 2 L 7 2 4F RT A21EA 1999043000688 19990430 00688 EA 1999 4 30 COMA9960176 1 19990425 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 769CA 727 7292 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999043000689 19990430 00689 NM 1999 4 30 UPS99229420 1 19990401 A 5230 ANGLE BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C+SI, SUSPECT CRACK FWD CARGO DOOR (LWR) FWD HINGE AT FRAME SUPPORT ANGLE. SUPPORT ANGLE FABRICATED AND INSTALLED PER DWG 69-18203. 2 L 7 3 4F A3WE 1999043000690 19990430 00690 NM 1999 4 30 UPS99229421 1 19990401 A 5230 69182036 FRAME BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C+SI, SUSPECT CRACK CARGO DOOR (FWD) FWD HINGE FRAME (DOOR INTERIOR). FWD HINGE FRAME REPLACED IAW DWG 69-18203. 2 L 7 3 4F A3WE 1999043000691 19990430 00691 WP 1999 4 30 UPS99829422 1 19990426 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-A, FLOORBEAM MOUNT HOLES ELONGATED AT STA 1680 AT LT O/B SEAT TRACK. THIS ITEM ACCOMPLISHED ON N/R CARD 544810. 2 L 7 4 4F RT 4A25 1999043000692 19990430 00692 WP 1999 4 30 UPS99829423 1 19990404 A 5720 46522012 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE-C3, RT WING T/E AT WS 5.812. THE FLAP SUPPORT FITTING ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 4652201 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999043000693 19990430 00693 WP 1999 4 30 UPS99829424 1 19990426 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1667 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:A L/H CIRCUMFERENTIAL FRAME @ STA 1667 FROM STR 21 TO STR 23 HAS SEVER AL POPPED FASTENERS AND EXTENSIVE CORROSION. REMOVED LOWER SECTION OF CIR FRAME. THIS ITEM ACCOMPLISHED ON N/R CARD 544806. 2 L 7 4 4F RT 4A25 1999043000694 19990430 00694 WP 1999 4 30 UPS99829425 1 19990426 A 5313 STRINGER DOUG DC8 DC873F 302199F WP BS 1660-1667 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-A, STRINGER 24L HAS EXTENSIVE CORROSION FROM STA 1660 TO STA 1667. ITEM ACCOMPLISHED ON N/R CARD 544808 . 2 L 7 4 4F RT 4A25 1999043000695 19990430 00695 EU 1999 4 30 QXEA9900663 1 19990317 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME SUPPORT CRACKED, FRAME 13815B BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000696 19990430 00696 EU 1999 4 30 QXEA9900664 1 19990317 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME SUPPORT CRACKED, FRAME 13815B BETWEEN STRINGERS 73 AND 72. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000697 19990430 00697 EU 1999 4 30 QXEA9900665 1 19990328 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION ON FRAME SUPPORT, FRAME 13815A BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-01-01. 2 L 7 2 4F RT A20EU 1999043000698 19990430 00698 EU 1999 4 30 QXEA9900666 1 19990329 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FRAME 16060 BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - WEBB FLANGE BENT AT BL 600R, BETWEEN FRAMES 16060 AND 16660. REPAIRED IAW HORIZON AIR EA 4-53-710. 2 L 7 2 4F RT A20EU 1999043000699 19990430 00699 EU 1999 4 30 QXEA9900667 1 19990314 A 5230 ANGLE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION ON CONNECTION ANGLE 70 ON STEP STRUCTURE FOR AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-01-01, PARAGRAP H 4 AND SRM 52-30-00, PAGE 12. 2 L 7 2 4F RT A20EU 1999043000700 19990430 00700 EU 1999 4 30 QXEA9900668 1 19990314 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION UNDER LIP OF BEAM 320 AND BEAM FRAME 90 OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-01-01, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000701 19990430 00701 EU 1999 4 30 QXEA9900669 1 19990314 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LIGHT CORROSION UNDER BEAM 325 AND WEBB 180 ON AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-01-01, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999043000702 19990430 00702 EU 1999 4 30 QXEA9900670 1 19990314 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION UNDER LIP OF BEAM 325 BETWEEN WEBB 180 AND FLANGE MEMBER 30 OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30-00, PAGE 8. 2 L 7 2 4F RT A20EU 1999043000703 19990430 00703 EU 1999 4 30 QXEA9900671 1 19990314 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION ON FLANGE MEMBER 30 AND BEAM 340 OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30-00, PAGE 8. 2 L 7 2 4F RT A20EU 1999043000704 19990430 00704 EU 1999 4 30 QXEA9900672 1 19990314 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION ON BEAM 350 NEAR LIGHTNING HOLE BETWEEN NR 85 ANGLE AND NR 305 WEB OF AFT CARGO DOOR. REPAIRED IAW FOKK ER SRM 52-30-00, PAGE 8. 2 L 7 2 4F RT A20EU 1999043000705 19990430 00705 EU 1999 4 30 QXEA9900673 1 19990314 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION UNDER LIP OF FLANGE MEMBER 30 BETWEEN BEAMS 340 AND 350 OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-3 0-00, PAGE 8. 2 L 7 2 4F RT A20EU 1999043000706 19990430 00706 EU 1999 4 30 QXEA9900674 1 19990314 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CORROSION ON BEAM FRAME, UNDER FLANGE, BETWEEN WEBS 295 AND 270 OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30- 00, PAGE 8. 2 L 7 2 4F RT A20EU 1999043000707 19990430 00707 EU 1999 4 30 QXEA9900675 1 19990325 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FORWARD CARGO BAY FLOOR FRAME 7805 HAS EXFOLIATION CORROSION UNDER FRAME TOP ANGLE AND UNDER NUT PLATE, LOCATED J UST ABOVE STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-714. 2 L 7 2 4F RT A20EU 1999043000708 19990430 00708 EU 1999 4 30 QXEA9900676 1 19990319 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FORWARD CARGO BAY FLOOR FRAME 8305 CASTELLATION HAS HEAVY CORROSION ON IT BETWEEN STRINGERS 1 AND 74. REPAIRED IA W FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4BC AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000709 19990430 00709 EU 1999 4 30 QXEA9900677 1 19990323 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FORWARD CARGO BAY FLOOR STRINGER 74 HAS EXFOLIATION CORROSION ON THE UNDER SIDE OF STRINGER AT FRAME 8805. REPAIR ED IAW FOKKER SRM 53-02-11 PAGE 3, FIGURE 1 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000710 19990430 00710 EU 1999 4 30 QXEA9900678 1 19990314 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - AFT LOWER CORNER OF AFT CARGO DOOR DENTED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000711 19990430 00711 EU 1999 4 30 QXEA9900679 1 19990322 A 5320 CHANNEL FOKKER F28 F28MK4000 4990810 EU NLG WW DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THE RIGHT-HAND FORWARD VERTICAL CHANNEL, INSIDE THE NLG WHEEL WELL, HAS .5 INCH HOLE AND A DENT. REPAIRED IAW HOR IZON AIR EA 4-53-727. 2 L 7 2 4F RT A20EU 1999043000712 19990430 00712 NM 1999 4 30 QXEA9900851 1 19990424 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 824PH 8517 157 SEA- COCKPIT OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE COCKPIT OVERHEAD LIGHT. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999043000713 19990430 00713 EU 1999 4 30 QXEA9900680 1 19990324 A 5330 PANEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - PANEL 29AH DETERIORATED. FABRICATED NEW PANEL 29AH FROM 090 GILNER STOCK. INSTALLED USING PANEL CARD PC29A. 2 L 7 2 4F RT A20EU 1999043000714 19990430 00714 EU 1999 4 30 QXEA9900681 1 19990405 A 5312 BULKHEAD WEB FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - REAR PRESSURE BULKHEAD WEB IS CRACKED IN TWO PLACES ABOVE HORIZONTAL BEAM I AT BL 575R AND BL 765R. REPAIRED IAW FOKKER SRM 53-02-18, PAGE 39 AND 40. 2 L 7 2 4F RT A20EU 1999043000715 19990430 00715 EU 1999 4 30 QXEA9900682 1 19990324 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME 14755 CASTELLATION FLANGE BETWEEN STRINGERS 1 AND 2 IS MISSING RIVETS. REMOVED LIGHT CORROSION, ALDOINED, P RIMED AND INSTALLED RIVETS IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000716 19990430 00716 EU 1999 4 30 QXEA9900683 1 19990324 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 15205 MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME 15205 CASTELLATION FLANGE BETWEEN STRINGERS 1 AND 2 IS MISSING FOUR RIVETS. REMOVED LIGHT CORROSION ALDOINE D, PRIMED AND INSTALLED RIVETS IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000717 19990430 00717 EU 1999 4 30 QXEA9900684 1 19990325 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME 15205 ENTIRE CASTELLATION FLANGE BETWEEN STRINGERS 5 AND 6 HAS BEEN CUT OUT TO REMOVE CRACK. FABRICATED PAT CH ALDOINED, PRIMED, INSTALLED IAW FOKKER SRM 53-02-12, PAGE 5. 2 L 7 2 4F RT A20EU 1999043000718 19990430 00718 EU 1999 4 30 QXEA9900685 1 19990324 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME 13815B ENTIRE CASTELLATION FLANGE BETWEEN STRINGERS 72 AND 73 HAS BEEN CUT OUT TO REMOVE TWO CRACKS. FABRIC ATED PATCH, ALDOINED, PRIMED AND INSTALLED IAW FOKKER SRM 53-02-11, PAGE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999043000719 19990430 00719 EU 1999 4 30 QXEA9900686 1 19990404 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - THE CENTER CARGO DOOR AFT APERTURE HAS CHAFE DAMAGE 10 INCHES LONG AT THE OUTBOARD EDGE. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999043000720 19990430 00720 EU 1999 4 30 QXEA9900687 1 19990316 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FORWARD CARGO DOOR INNER SKIN HAS 3 DENTS JUST BELOW HINGE. REPAIRED IAW FOKKER SRM 52-02-01 PAGE 3, FIGURE 2. 2 L 7 2 4F RT A20EU 1999043000721 19990430 00721 EU 1999 4 30 QXEA9900688 1 19990315 A 5230 ANGLE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FOUND LARGE OUT OF ROUND HOLES IN ANGLES FOR FORWARD CARGO DOOR. REPAIRED IAW FOKKER SRM 51-11-04, 51-31-01 AND 5 1-10-05. 2 L 7 2 4F RT A20EU 1999043000722 19990430 00722 EU 1999 4 30 QXEA9900689 1 19990320 A 5230 WEB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO PIT DOOR FORWARD LOWER WEB IS CRACKED AT NUT PLATE. REPAIRED IAW FOKKER SRM 51-10-04 AND 51-31-01. 2 L 7 2 4F RT A20EU 1999043000723 19990430 00723 EU 1999 4 30 QXEA9900690 1 19990317 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THERE IS CORROSION ON ATTACH ANGLE TO FRAME 13345 BETWEEN STRINGERS 2 AND 1. REPAIRED IAW FOKKER SR M 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000724 19990430 00724 EU 1999 4 30 QXEA9900691 1 19990317 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 13865 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THERE IS CORROSION ON THE SKIN AT STRINGER 2 BETWEEN FRAME 13865 AND 13345. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000725 19990430 00725 EU 1999 4 30 QXEA9900692 1 19990317 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE SKIN IS CORRODED UNDER CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOK KER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000726 19990430 00726 EU 1999 4 30 QXEA9900693 1 19990317 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE SKIN IS CORRODED UNDER CASTELLATION AT FRAME 13815 AND STRINGER 2. REPAIRED IAW FOKKER SRM 51-1 0-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000727 19990430 00727 EU 1999 4 30 QXEA9900694 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE CASTELLATION HAS CORROSION AT FRAME 13815 AND STRINGER 71. REPAIRED IAW FOKKER SRM 51-10-4, PAG E 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000728 19990430 00728 EU 1999 4 30 QXEA9900695 1 19990318 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE SKIN HAS CORROSION AT FRAME 13815 AND STRINGER 73. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, STR INGER 4 B-C. 2 L 7 2 4F RT A20EU 1999043000729 19990430 00729 EU 1999 4 30 QXEA9900696 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 74 AND 72 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000730 19990430 00730 EU 1999 4 30 QXEA9900697 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 1 AND 74 HAS CORROSION. REPAIRED IAW FOKKER SRM 5 1-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000731 19990430 00731 EU 1999 4 30 QXEA9900698 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815 BETWEEN STRINGERS 2 AND 1 HAS CORROSION. REPAIRED IAW FOKKER SRM 51 -10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000732 19990430 00732 EU 1999 4 30 QXEA9900699 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY THE CASTELLATION AT FRAME 13815A, 13815 AND STRINGER 2 THE SKIN IS CORRODED. REPAIRED IAW FOKKER SR M 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000733 19990430 00733 EU 1999 4 30 QXEA9900700 1 19990318 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY FRAME 13815A AT STRINGER 2 THE SKIN HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRA PH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000734 19990430 00734 EU 1999 4 30 QXEA9900701 1 19990318 A 5320 SPLICE FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY AT FRAME 13815A BETWEEN STRINGERS 1 AND 74 THERE IS CORROSION ON THE OUTER SPLICE PIECES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000735 19990430 00735 EU 1999 4 30 QXEA9900702 1 19990325 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY FRAME 13815A BETWEEN STRINGERS 73 AND 72 HAS A CRACK IN THE CASTELLATION. REPAIRED IAW FOKKER SRM 5 3-02-13, PAGE 4, FIGURE 3. 2 L 7 2 4F RT A20EU 1999043000736 19990430 00736 EU 1999 4 30 QXEA9900703 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY FRAME 13815A BETWEEN STRINGERS 74 AND 73 THE CASTELLATION HAS CORROSION. REPAIRED IAW FOKKER SRM 51 -10-4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000737 19990430 00737 EU 1999 4 30 QXEA9900704 1 19990318 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY FRAME 13815A BETWEEN STRINGER 1 AND 2 THE CASTELLATION HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10 -4, PAGE 9, PARAGRAPH 4 B-C. 2 L 7 2 4F RT A20EU 1999043000738 19990430 00738 NE 1999 4 30 99UAL900213 2 19990415 A 7200 ENGINE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 1 FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 990UA 21980 687731 NR 1 ENGINE EGT LIMIT EXCEEDED, HIGH OIL PRESSURE AND HIGH OIL TEMPERATURE. *S/D* THE THROTTLE LINKAGE BECAME DETACHED AND NORMAL ENGINE VIBRATION CAUSED THE THROTTLE TO ADVANCE ON ITS OWN. THE EGT LIMIT WAS EXCEEDED AND THE ENGINE WAS S HUT DOWN. THE ENGINE WAS CHANGED AND THE AIRCRAFT PUT BACK INTO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1999043000739 19990430 00739 1999 4 30 99UAL900214 4 19990413 A 2210 YAW DAMPER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E & E COMPT MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 394UA 24669 IN CRUISE, FL 310 AND ON 'B' SYSTEM HYDRAULICS. WITHOUT WARNING, THE AIRCRAFT ROLLED HARD LEFT AT APPROXIMATELY A 20-3 0 DEGREE BANK. BOTH PILOTS GRABBED THE CONTROLS AND ROLLED AIRCRAFT UPRIGHT. ACCOMPLISHED TESTS OF THE YAW DAMPER SYST EM, SPOILER SYSTEM, AILERON SYSTEM, AND RUDDER PCU AND NO DISCREPANCIES WERE NOTED. ACCOMPLISHED CAT III TEST OF AUTOPI LOT AND NO DISCREPANCIES WERE NOTED. REPLACED THE RUDDER PCU AS A PRECAUTION AND MODIFIED THE YAW DAMPER SYSTEM PER BOE ING SERVICE BULLETIN 737-27A1206. THE RUDDER PCU WAS TESTED IN THE REPAIR SHOP WITH FAA REPRESENTATIVES PRESENT AND NO DISCREPANCIES WERE NOTED. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999043000740 19990430 00740 NM 1999 4 30 99UAL900216 1 19990417 A 3350 BPS73 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMER EXIT DOOR DISCHARGED A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 104UA 26902 UPPER DECK RIGHT HAND EXIT DOOR BATTERY WOULD NOT TEST. *S/D* REMOVED AND RESET BATTERY ON PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 1999043000741 19990430 00741 NM 1999 4 30 99UAL900217 1 19990417 A 3610 3985401 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LOWER AFT BODY LEAKING A UALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 29 7458U 21912 CLIMBING THROUGH 8,000 FEET LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO SFO. *S/D* MIANTENANCE REPLACED A LEAKING LEFT HAND PACK VALVE AND FAULTY CLAMP ON THE KEEL BEAM DUCT. NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1999043000742 19990430 00742 NM 1999 4 30 99UAL900218 1 19990418 A 2130 VALVE TSK56697 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE PRESSURE SYS FOD A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7289U 21567 CABIN FAILED TO PRESSURIZE. THE CABIN ALTITUDE WAS UNCONTROLLABLE. DESCENDED TO 14,000 FEET TO STABILIZE PRESSURE. DI VERTED BACK TO DEN. *S/D* FOUND BIRD JAMMED IN SHUTOFF VALVE. REPLACED VALVE AND REMOVED REMAINS OF BIRD. 2 L 7 3 4F 4 F A3WE E2EA 1999043000743 19990430 00743 NM 1999 4 30 99UAL900219 1 19990419 A 2497 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT BROKEN A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 533UA 25073 RETURNED TO IAD DUE TO PARTIAL ELECTRICAL FAILURE. TERMINAL LUGS L2 (PHASE B) AND L3 (PHASE C) WERE FOUND BROKEN AT LEF T GENERATOR CIRCUIT BREAKER C901. LOSS OF PHASE B AND PHASE C AT L GEN CB CAUSED PARTIAL ELECTRICAL FAILURE. THE WIRE TERMINALS WERE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999043000744 19990430 00744 NM 1999 4 30 99UAL900220 1 19990419 A 2130 CONTROL PANEL HAMILTON STA 7110024 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT MALFUNCTIONED A UALA B EMER. DESCENT O OTHER CR CRUISE 1 WP 29 7285U 21563 CREW REPORTS AT 33,000 FEET THE CABIN PRESSURE BEGAN TO CLIMB TO 11,000 FEET. MADE AN EMERGENCY DESCENT TO 24,000 FEET. STANDBY OPERATION OK. *SD* REPLACED PRESSURE CONTROL PANEL. 2 L 7 3 4F 4 F A3WE E2EA 1999043000745 19990430 00745 NM 1999 4 30 99UAL900221 1 19990419 A 5240 HANDLE BOEING 747 747422 1384935 NM PWA DOOR 5R NOT SECURED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 117UA 28810 DOOR LIGHT OPEN 5 RIGHT ON TAKEOFF ROLE. ABORTED TAKEOFF AT 80 KNOTS. PER CREW, DOOR UNSAFE MESSAGE WENT AWAY AFTER DO OR HANDLE WAS CYCLED. CREW MEMBER REPORTED HANDLE NOT FULLY SECURED. OPS CHECKED DOOR AT IAD, OPS CHECKED NORMAL. 2 L 7 4 4F RT A20WE 1999043000746 19990430 00746 NM 1999 4 30 99UAL900222 1 19990420 A 2612 FIRE LOOP BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE OUT OF POSITION A UALA E ENGINE SHUTDOWN N FALSE WARNING LD LANDING 1 WP 29 992UA 22089 NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. *S/D* FOUND LOWER FIRE LOOP CONTACTING CSD. REPOSITIONED LOWER FIRE LOOP, OPS CHECK OK. 2 L 7 2 4F 4 F A16WE E2EA 1999043000747 19990430 00747 NM 1999 4 30 99UAL900223 1 19990420 A 2121 FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLIGHT DECK FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 643UA 25093 'FWD EQ EXH FAN' EICAS MESSAGE DISPLAYED. SMOKE ON FLIGHT DECK. CB H21 ON P6 PULLED AS PRECAUTION. SMOKE EVAC PERFORME D AND SMOKE DISSIPATED. *S/D* SMOKE IN FLIGHT DECK WAS PROBABLY CAUSED BY A BEARING FAILURE IN FORWARD EQUIPMENT EXHAU ST FAN. THIS FAN WAS REPLACED PER MM 21-59-06. THERE HAS BEEN NO ADDITIONAL REPORTS OF SMOKE. THIS FAN IS NOT AN MR U NIT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999043000748 19990430 00748 NM 1999 4 30 99UAL900224 1 19990416 A 4920 38005501 SEAL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU COMPRESSOR FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 769UA 4750 26921 OUTBOUND CREW SMELLED OIL IN COCKPIT. PREVIOUS REPORT OF SMOKE AND SMELL IN CABIN AND COCKPIT ON FLIGHT 918-12. *S/D* APU (S/N 1059) (P/N 3800550-1) WAS REMOVED FROM A/C 2069 ON 4/23/99. APU HAD SUFFERED SEVERE ENGINE COMPRESSOR DAMAGE DUE TO SOFT (ICE) FOD. THE DAMAGE WAS EXTENSIVE. THE RESULTING EFFECT OF THE DAMAGE WAS LEAKAGE OF OIL PAST THE ENGIN E COMPRESSOR SEAL ALLOWING OIL INTO THE BLEED AIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999043000749 19990430 00749 NM 1999 4 30 99UAL900225 1 19990421 A 3397 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7266U 21413 EEL STRIPS INOP IN 1ST CLASS SECTION. REPLACED EEL STRIPS, REPLACED DAMAGED POWER STRIP FROM COCKPIT TO FWD END OF STRI P. FIRST CLASS BATTERY PACK, FOUND WIRE FROM BATT TO STRIP GROUNDING OUT ON METAL RETURN AIR GRILLED. REPAIRED AND REP LACED FEEDER STRIP FROM POWER SUPPLY TO FIRST CLASS EEL STRIP. OPS CK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999043000750 19990430 00750 NM 1999 4 30 99UAL900226 1 19990422 A 2132 SELECTOR PANEL HAMILTON STA 91100442 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 955UA 26703 UNABLE TO MAINTAIN CABIN ALTITUDE. *S/D* DELTA P MODULE FASTENER LOOSE AND NOT COMPLETELY CONNECTED, AND RIGHT HAND PA CK VALVE BIASED TO THE CLOSED POSITION, AND AFT OUTFLOW VALVE HAD LOW RESISTANCE. REPLACED THE CABIN ALTITUDE INDICATOR AND THE CABIN PRESSURE SELECTOR PANEL. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999043000751 19990430 00751 NM 1999 4 30 99UAL900227 1 19990421 A 2740 SWITCH 65C255296 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE STAB TRIM FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 930UA 26655 ELECTRIC STABILIZER TRIM IS INOP. FOUND THAT FLAP UPLIMIT SWITCH (S245) HAD A FAILED RESISTANCE (68+) WHEN MEASURED BET WEEN D4514P PINS 32 AND 34. THE SWITCH WAS REPLACED. LATER TROUBLESHOOTING FOLLOWING ANOTHER WRITE-UP FOR INOP STABILI ZER TRIM FOUND THAT THE SYSTEM WORKED NORMALLY WHEN THE CUTOUT SWITCH WAS PUT IN OVERRIDE. ACCORDINGLY, THE M1201 COLUM N SWITCHING MODULE WAS REPLACED. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999043000752 19990430 00752 EU 1999 4 30 99UAL900228 1 19990419 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 434UA 492 EMERGENCY EXIT LIGHTS, FLOOR LIGHT DAMAGED. ALL EXIT LIGHTS REMAIN ON AT ALL TIMES EVEN WITH FLT DECK SWITCH OFF. *S/D * THE EXIT SIGNS AND ALL RELATED LIGHTS ARE SWITCHED ON WHEN THE NO SMOKING SWITCH IS IN THE AUTO POSITION AND THE LAND ING GEAR IS EXTENDED. SYSTEM OPERATION WAS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1999043000753 19990430 00753 NM 1999 4 30 99UAL900229 1 19990422 A 3244 TIRE MICHELIN 0398070 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MLG FAILED A UALA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 WP 29 654UA 25392 STRONG VIBRATION ON TAKEOFF, AMBER ALERT DECLARED. ACFT LANDED IN MIA WITH NR 3 FRONT MLG TIRE BLOWN, OTHERWISE NORMAL LANDING. *S/D* PROBABLE FOD, ANTI-SKID CHECKED OK. REPLACED WHEEL ASSEMBLY. 2 L 7 2 4F 4 F RT A1NM E24NE 1999043000754 19990430 00754 NM 1999 4 30 99UAL900230 1 19990422 A 3350 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE EMER EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7449U 21903 AFT EXIT EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY BASE ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1999043000755 19990430 00755 WP 1999 4 30 ABXA9900321 1 19990423 A 3246 3887315505 WHEEL DOUG DC8 DC863 302198A WP RT MLG FAILED A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 820AX 307 46155 BEAD FLANGE SEPARATED FROM NR 5 MAIN LANDING GEAR ASSEMBLY, DAMAGING NR 5 MAIN GEAR BRAKE ASSEMBLY. REPLACED NR 5 WHEEL ASSEMBLY AND NR 5 MAIN GEAR BRAKE ASSEMBLY. 2 L 7 4 4F 4A25 1999043000756 19990430 00756 WP 1999 4 30 DHL9980701C 1 19990331 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 680 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LOWER FUS EXT BS 680 AND LONG 32R FORMING SUPPORT ANGLE CRACKED. FABRICATED ANGLE REPAIR PER SRM 53-20-0, 1 X 7.8. 2 L 7 4 4F RT 4A25 1999043000757 19990430 00757 WP 1999 4 30 DHL9980702C 1 19990313 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 680 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LOWER FUS BS 680 AND LONG 32L SUPPORT ANGLE CRACKED. REMOVED AND REPAIRED DAMAGED ANGLE PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999043000758 19990430 00758 WP 1999 4 30 DHL9980703C 1 19990324 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1040 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LOWER FUS BS 1040 LONG 34R SUPPORT ANGLE CRACKED. STOP DRILLED CRACK AND FABRICATED REPAIR PER SRM 53-2-3, 2 X 6. 2 L 7 4 4F RT 4A25 1999043000759 19990430 00759 WP 1999 4 30 DHL9980704C 1 19990401 A 5320 FRAME DOUG DC8 DC873F 302199F WP C4 DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LOWER FUS EXT C-4 CUT OUT FWD UPPER CORNER SHOWS CRACK AT FS 1405 AND 26R. CUT OUT DAMAGED AREA AND FABRICA TED REPAIR DOUBLER AND TRIPLER, INSTALLED PER SRM 51-1-8. FILLET 1 X 1, DOUBLER 20 X .90 AND TRIPER 18 X 17. 2 L 7 4 4F RT 4A25 1999043000760 19990430 00760 WP 1999 4 30 DHL9980705C 1 19990313 A 5512 PANEL DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT HORIZ STAB REAR SPAR STA XE 270.9 CRACKED ON COVER PANEL. REMOVED AND FABRICATED NEW COVER AND INSTALLED PER SRM 52-3-0. 2 L 7 4 4F RT 4A25 1999043000761 19990430 00761 WP 1999 4 30 DHL9980706C 1 19990314 A 5532 PANEL DOUG DC8 DC873F 302199F WP VERT STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, VERTICAL STABILIZER T/E AT STA 225 REAR SPAR COVER PANEL CRACKED. REMOVED PANEL, STOP DRILLED AND INSTALLED FIBREGLASS REPAIR PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999043000762 19990430 00762 WP 1999 4 30 DHL9980707C 1 19990314 A 5532 PANEL DOUG DC8 DC873F 302199F WP VERT STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, VERTICAL STAB T/E AREA STA 195 REAR SPAR METAL COVER CRACKED. STOP DRILLED END OF CRACK, FABRICATED DOUBLER REPAIR 3 X 3 AND INSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999043000763 19990430 00763 WP 1999 4 30 DHL9980708C 1 19990314 A 5751 PANEL DOUG DC8 DC873F 302199F WP LT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT I/B AILERON I/B LOWER SURFACE ON ACCESS PANEL HAS CRACKED PLATE. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-21, 5 X 4. 2 L 7 4 4F RT 4A25 1999043000764 19990430 00764 WP 1999 4 30 DHL9980709C 1 19990314 A 5320 ANGLE DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, FWD LOWER CARGO COMPT AFT DOOR AFT FRAME ANGLE FLANGE IS CRACKED SEVERAL PLACES. REMOVED DAMAGED ANGLE, F ABRICATED NEW ANGLE AND INSTALLED PER SRM 51-3-0, 29 X 3. 2 L 7 4 4F RT 4A25 1999043000765 19990430 00765 WP 1999 4 30 DHL9980710C 1 19990322 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 90 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, RT WING T/E PANEL LOWER WS 90 DELAMINATED WITH CRACK DAMAGE. CLEANED DAMAGED AREA, FABRICATED REPAIR DOUBLE R AND INSTALLED PER SRM 51-1-9, 4 X 4 . 2 L 7 4 4F RT 4A25 1999043000766 19990430 00766 WP 1999 4 30 DHL9980711C 1 19990315 A 5321 FLOOR DOUG DC8 DC873F 302199F WP GALLEY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, FLOOR PANEL GALLEY CENTER CHANNEL FRAME IS CRACKED. REMOVED DAMAGED PANEL, FABRICATED NEW AND INSTALLED P ER SRM 51-1-21, 25 X 4. 2 L 7 4 4F RT 4A25 1999043000767 19990430 00767 WP 1999 4 30 DHL9980712C 1 19990315 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT HORIZONTAL STAB L/E I/B SECTION O/B INTERIOR LOWER AREA AT APPROX FS 166 HAS CRACK DAMAGE. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER SRM 55-2-0, 1 X 1 X 7 AND 10 X 1 X 6. 2 L 7 4 4F RT 4A25 1999043000768 19990430 00768 WP 1999 4 30 DHL9980714C 1 19990322 A 5512 SKIN DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT HORIZ STAB L/E I/B SECTION I/B INTERIOR LOWER AREA AT APPROX STA FS 53.75 HAS CRACK DAMAGE ON SURFACE AT FASTENER HOLE POINT. STOP DRILLED CRACK, FABRICATED ANGLE REPAIR 6 X 1 X 1 AND 5 X 1 X 1 PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999043000769 19990430 00769 WP 1999 4 30 DHL9980715C 1 19990322 A 5510 ANGLE DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT HORIZONTAL STABILIZEER L/E INTERIOR AREA AT STA FS 60 VERTICAL ANGLE IS CRACKED. STOP DRILLED CRACK AND FABRICATED REPAIR PER SRM 51-1-8, 2 X 6. 2 L 7 4 4F RT 4A25 1999043000770 19990430 00770 WP 1999 4 30 DHL9980716C 1 19990329 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1350 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, AFT CARGO COMPT INTERIOR LONG FS 1350 BULGING CORROSION FINGER DOUBLER IS CRACKED. REMOVED LONGERON SPLICE, REMOVED CORROSION FROM PRODUCTION SPLICE, FABRICATED NEW FINGER DOUBLER AND INSTALLED PER SRM 53-4-1. INSTALLED SPLICE 60 X 6.25. 2 L 7 4 4F RT 4A25 1999043000771 19990430 00771 WP 1999 4 30 DHL9980717C 1 19990331 A 5540 SPACER DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, FOUND RUDDER TORQUE TUBE SPACER CRACKED. REMOVED AND REPLACED SPACER ON RUDDER TORQUE TUBE IAW DC-8 MM 27-2 1-3. REMOVED AND REPLACED SHIM ON TORQUE TUBE IAW DC-8 MM 27-21-3. 2 L 7 4 4F RT 4A25 1999043000772 19990430 00772 WP 1999 4 30 DHL9980718C 1 19990322 A 5720 FRAME DOUG DC8 DC873F 302199F WP WS 90 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK FOUND RT WING FLAP WELL AT STA 90.00 UPPER FRAME FOR L/E FLAP CONTOUR CRACKED. FABRICATED NEW COVER PANEL RT WING O/B FLAP L/E STA 90.00 IAW DC-8 SRM 51-1-7. 2 L 7 4 4F RT 4A25 1999043000773 19990430 00773 WP 1999 4 30 DHL9980719C 1 19990322 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, RT MLG STA 950 AND XCW 46 FITTING SUPPORT CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999043000774 19990430 00774 WP 1999 4 30 DHL9980720C 1 19990331 A 5321 FLOOR DOUG DC8 DC873F 302199F WP CABIN CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, FLOOR PANEL IN FRONT OF CAPTAIN SEAT HAS CRACK APPROX 3 INCHES LONG. STOP DRILLED CRACK IN FLOOR PANEL, INS TALLED REPAIR DOUBLER PER SRM 51-1-21, 5 X 5. 2 L 7 4 4F RT 4A25 1999043000775 19990430 00775 WP 1999 4 30 DHL9980721C 1 19990401 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP AFT PRESS BLKHD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, AFT FUSELAGE AFT PRESSURE BULKHEAD AFT LOWER AREA CRACKED APPROX 3 INCHES LONG ON HORIZONTAL STIFFENER. RE MOVED FASTENERS, STOP DRILLED AND INSTALLED BRACKETS PER MHA ENG EO NR F-99-011 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999043000776 19990430 00776 WP 1999 4 30 DHL9980722C 1 19990321 A 5510 COVER DOUG DC8 DC873F 302199F WP RT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, RT HORIZONTAL STAB REAR SPAR AT STA XE 219.9 COVER IS CRACKED. REMOVED COVER, FABRICATED NEW COVER AND INST ALLED PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999043000777 19990430 00777 WP 1999 4 30 DHL9980723C 1 19990311 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 515.7 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LEFT WING LOWER L/E STA 515.7 O/B OF NR 1 SLOT SKIN IS BROKEN AWAY ALONG SCREW HOLES. REMOVED AND FABRICAT ED NEW PANEL PER SRM 51-3-0, 6 X 8. 2 L 7 4 4F RT 4A25 1999043000778 19990430 00778 WP 1999 4 30 DHL9980724C 1 19990319 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 4 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, NR 4 ENGINE LT T/R HALF CORE COWL INTERIOR AREA AT 8 O'CLOCK FOUND CRACK ON SURFACE SKIN. CUT OUT DAMAGED SECTION, FABRICATED REPAIR PER CFM MM AND INSTALLED PER SRM 51-1-21A, 5 X 5. 2 L 7 4 4F RT 4A25 1999043000779 19990430 00779 WP 1999 4 30 DHL9980725C 1 19990319 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 4 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, NR 4 ENGINE LT T/R HALF CORE COWL FWD INTERIOR AREA AT 10 O'CLOCK FOUND CRACK DAMAGE ON SKIN. CUT OUT DAMA GED SECTION OF SKIN, FABRICATED REPAIR AND INSTALLED PER SRM 51-1-21A, 3 X 3. 2 L 7 4 4F RT 4A25 1999043000780 19990430 00780 WP 1999 4 30 DHL9980726C 1 19990327 A 5312 BULKHEAD ANGLE DOUG DC8 DC873F 302199F WP AFT PRESS BLKHD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, UPPER CARGO COMPT AFT PRESSURE BULKHEAD FWD SIDE LONGERON NR 5 LT SIDE AUX ATTACH ANGLE CRACKED. REMOVED CR ACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-1-21A, 4.5 X 1 X 1. 2 L 7 4 4F RT 4A25 1999043000781 19990430 00781 WP 1999 4 30 DHL9980727C 1 19990312 A 5350 FAIRING DOUG DC8 DC873F 302199F WP BS 1000 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT FAIRING PANEL FRAME TO FUSELAGE AT LONGERON APPROX STA 1000 HAS FORMED ANGLE CRACKED AT LOWER SURFACE. S TOP DRILLED END OF CRACK, FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 51-21, 1 X 1 X 3.5. 2 L 7 4 4F RT 4A25 1999043000782 19990430 00782 WP 1999 4 30 DHL9980728C 1 19990307 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT WING LOWER SURFACE T/E HINGED PANEL 710 DELAMINATED. REPAIRED AREA PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999043000783 19990430 00783 WP 1999 4 30 DHL9980729C 1 19990307 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, RT WING LOWER ACCESS PANEL NR 525 IS DELAMINATED. REMOVED AND REPAIRED PANEL, REINSTALLED PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999043000784 19990430 00784 WP 1999 4 30 DHL9980730C 1 19990307 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT WING LOWER ACCESS PANEL NR 525 IS DELAMINATED. REMOVED PANEL AND REPAIRED PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999043000785 19990430 00785 WP 1999 4 30 DHL9980731C 1 19990315 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 90 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, RT WING T/E LOWER I/B PANEL HAS CRACK DAMAGE ON SURFACE AT WS 90. CUT OUT DAMAGED AREA, FABRICATED REPAIR D OUBLER AND INSTALLED PER SRM 51-1-91. 2 L 7 4 4F RT 4A25 1999043000786 19990430 00786 WP 1999 4 30 DHL9980732C 1 19990327 A 5312 BULKHEAD ANGLE DOUG DC8 DC873F 302199F WP FWD PRESS BLKHD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, UPPER CARGO COMPT AFT PRESS BULKHEAD FWD SIDE LONGERON 5 RT AUX ATTACH ANGLE CRACKED. REMOVED ANGLE, FABRIC ATED NEW ANGLE AND INSTALLED PER SRM 51-1-8, 4.5 X 1 X 1. 2 L 7 4 4F RT 4A25 1999043000787 19990430 00787 WP 1999 4 30 DHL9980733C 1 19990312 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, NR 1 ENGINE RT CORE COWL REAR UPPER REPAIR CRACKED. CUT OUT DAMGED SECTION OF INNER SKIN, FABRICATED REPA IR PER CFM 56 MM 78-31-10 AND INSTALLED PER DC-8 SRM 51-1-21A, 3 X 2.5. 2 L 7 4 4F RT 4A25 1999043000788 19990430 00788 WP 1999 4 30 DHL9980734C 1 19990310 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 69.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, FOUND CRACK PROGRESSING THROUGH STEP HOLE AT STA 69.5 WW 5. CUT OUT DAMAGED SECTION OF SKIN AND FABRICATED FILLER 4 X 4' AND DOUBLER 9.75 X 6 PER SRM 57-2-0 AND 57-2-1. 2 L 7 4 4F RT 4A25 1999043000789 19990430 00789 WP 1999 4 30 DHL9980735C 1 19990310 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, NR 2 ENGINE RT T/R HALF CORE COWL INNER SURFACE FWD AREA CRACKED. CUT OUT CRACKED AREA PER CFM 56 MM, FABRI CATED DOUBLER AND INSTALLED PER CFM 56 MM 78-31-10, 4 X 3. 2 L 7 4 4F RT 4A25 1999043000790 19990430 00790 WP 1999 4 30 DHL9980736C 1 19990310 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, NR 2 ENGINE LT T/R HALF CORE COWL I/B SURFACE AFT LOWER AREA CRACKED. STOP DRILLED CRACK AND FABRICATED REP AIR DOUBLER PER SRM 51-1-20, 3 X 4. 2 L 7 4 4F RT 4A25 1999043000791 19990430 00791 WP 1999 4 30 DHL9980737C 1 19990310 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, NR 3 ENGINE I/B T/R TRANSLATING COWL OUTER ACCESS PANEL AT APPROX 7 O'CLOCK POSITION MOUNTING SURFACE HAS A CRACK. REMOVED DAMAGED MOUNTING SURFACE, FABRICATED NEW AND INSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999043000792 19990430 00792 WP 1999 4 30 DHL9980738C 1 19990327 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, RT MLG WW AT STA 940 FRAME CRACKED AT BASE. REMOVED DAMGED FRAME, FABRICATED NEW FRAME AND INSTALLED PER S RM 51-1-21. 2 L 7 4 4F RT 4A25 1999043000793 19990430 00793 WP 1999 4 30 DHL9980740C 1 19990309 A 5753 ANGLE DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT O/B FLAP EXHAUST GATE CUTOUT AT I/B SECTION INTERIOR OF T/E HAS CRACK ON FORMED ANGLE. REMOVED DAMAGED T /E SECTION ON EXHAUST GATE CUTOUT, FABRICATED NEW SECTION AND NEW ANGLE AND INSTALLED PER SRM 51-1-20B, 8.5 X 26 AND 55 X 26. 2 L 7 4 4F RT 4A25 1999043000794 19990430 00794 WP 1999 4 30 DHL9980741C 1 19990309 A 5753 PANEL DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT WING T/E AREA INNER WING FLAP MECHANISM SUPPORT FITTING HAS UPPER PANEL WITH CRACK ON SURFACE. STOP DRI LLED END OF CRACK, FABRICATED DOUBLER PER SRM 51-1-8 AND INSTALLED PER 51-1-21, 6.375 X 3.5. 2 L 7 4 4F RT 4A25 1999043000795 19990430 00795 WP 1999 4 30 DHL9980742 1 19990309 A 5753 BRACKET DOUG DC8 DC873F 302199F WP LT TE FLAP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C-CHECK, LT WING FLAP VANE NR 4 O/B ATTACHING BRACKET AT L/E BROKEN. REMOVED AND REPLACED O/B ATTACH BRACKET PER M M 27-51-14. 2 L 7 4 4F RT 4A25 1999043000796 19990430 00796 NM 1999 4 30 DHL99727002 1 19990426 A 5730 652165827 PANEL BOEING 727 727228 NM WS 543 BROKEN A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 727DH 20204 AIRFRAME VIBRATION AT 285 KTS ABOVE 300 KTS VIBRATION IS SEVERE. FOUND THREE FLAP COVE PANELS BROKEN, ONE AT STA 543 AN D TWO AT STA 521. REPLACED PER MM 57-30-0. 2 L 7 3 4F A3WE 1999043000797 19990430 00797 WP 1999 4 30 AT9900316 1 19990409 A 3297 WIRE DOUG DC9 DC932 3022066 WP NLG BROKEN A ZZDA O OTHER N FALSE WARNING AP APPROACH 1 SO 15 849AT 47484 WHEN LANDING GEAR WAS EXTENDED DURING APPROACH, THE NOSE GEAR UNSAFE (RED) LIGHT STAYED ON, GREEN LIGHT WAS OUT. RECYCL ED GEAR, NO HELP. FOUND BROKEN WIRES TO NOSE GEAR GROUND PROXIMITY SWITCH. REPAIRED WIRES AND CYCLED NOSE GEAR FIVE TI MES, ALL OPERATIONAL CHECKS GOOD IAW DC9 MM 32-30. 2 L 7 2 4F A6WE 1999043000798 19990430 00798 WP 1999 4 30 AT9900317 1 19990318 A 5321 FLOOR DOUG DC9 DC932 3022066 WP LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE CENTER AFT FLOOR BOARD BETWEEN AFT LAVATORY AND G-4 CORRODED, CRACKED A ND WORNED HAT CHANNELS. FABRICATED NEW FLOOR BOARD AND HAT CHANNELS, ALODINED, PRIMED AND INSTALLED ALL PARTS AND INSUL ATION IAW DC9 SRM 51-30-2, 51-10-4, AND DPS 3-40-9. 2 L 7 2 4F A6WE 1999043000799 19990430 00799 WP 1999 4 30 AT9900318 1 19990317 A 5321 PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR BOARD PANEL NR 61D SKIN BULGING/CORRODED. FABRICATED NEW PANEL A ND HAT SECTIONS, DRILLED, DEBURRED, TREATED, PRIMED ALL PARTS AND INSTALLED PANEL AND CHAFFED STRIPS IAW DC9 SRM 51-30-2 , 53-21-0, 51-30-1, 51-10-3, AND 51-30-7. 2 L 7 2 4F A6WE 1999043000800 19990430 00800 WP 1999 4 30 AT9900319 1 19990323 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION ON FLOOR AT BS 965 LBL-50 JUST AFT OF WALL. REMOVED CORROSION, F ABRICATED NEW DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 53-01 FIG 1, 51-10-4, 53-2 0-1, AND 51-30-2. 2 L 7 2 4F A6WE 1999043000801 19990430 00801 WP 1999 4 30 AT9900320 1 19990311 A 5320 FRAME DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 814AT 47486 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO DOOR CUT OUT FRAME CORRODED ON THE AFT LOWER CORNER. REM OVED EXISTING REPAIR, DRILLED, DEBURRED NEW PAN SECTION, ALODINED, PRIMED, AND INSTALLED REPAIR IAW DC9 SRM 53-10-0, 51- 10-4, 51-30-2, 51-10-3, AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1999043000802 19990430 00802 EU 1999 4 30 MALA976431 1 19990415 A 3297 531706 WIRE SAAB SF340 340B 7860101 EU RT MLG DAMAGED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 425XJ 425 AFTER TAKEOFF, FI STOP LIGHT OPEN ILLUMINATED. RETURNED TO MSP. AFTER LANDING FI STOP LIGHT DIDN'T ILLUMINATE, PULLED KNOB. LIGHT ILLUMINATED WHEN PARKED. MAINTENANCE REPAIRED WIRE DG605-22 IN RIGHT MLG, REPLACED CONTROL QUADRANT AND LH PDU. PERFORMED OPS AND FUNCTIONAL CHECKS IAW SAAB AMM 76-10-60-5. 2 L 7 2 4T RT A52EU 1999043000803 19990430 00803 EU 1999 4 30 MALA976428 1 19990416 A 2460 MS24142D1 RELAY SAAB SF340 SF340A 7850100 EU MX BAY FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 99XJ 099 ON CLIMB-OUT, RIGHT ESS BUS LIGHT ILLUMINATED, ACCOMPLISHED QRH AND RESET BREAKERS, UNSUCCESSFULL AT GETTING IT BACK ON LINE. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RELAY 56PC. OPS CHECK OF ESS GOOD. 2 L 7 2 4T RT A52EU 1999043000804 19990430 00804 1999 4 30 MALA976429 3 19990414 A 6140 523535 INDICATOR SAAB SF340 SF340A 7850100 EU LT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 114XJ 340A114 LEFT ENGINE OIL PRESS CWP ON THAN OFF IN FLIGHT, LEFT ENGINE OIL PRESSURE NORMAL, LEFT PROP OIL PRESSURE FLUX RAPIDLY. P ERFORMED QRH, EXAUSTED LEFT PROP. NORMAL OPS. RETURNED TO DTW. MAINTENANCE REPLACED LEFT PROP OIL PRESS/TEMP INDICATO R. OIL LEVEL CHECKS GOOD, RAN AIRCRAFT AND ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999043000805 19990430 00805 EU 1999 4 30 MALA976430 1 19990416 A 3020 447301 INLET HEAT SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 410XJ 410 RIGHT INTAKE HEAT ILLUMINATED ON CLIMB-OUT, PERFORMED QRH AND ILLUMINATED AGAIN. RETURN TO MSP. MAINTENANCE CHECKED TH ERMISTORS AND OHMED CHECKED HEATER ELEMENTS OF RIGHT INTAKE. REPLACED RIGHT SHOE BOX AND RAN AIRCRAFT FOR SEVERAL MINUT ES. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999043000806 19990430 00806 EU 1999 4 30 MALA976432 1 19990415 A 3150 006WS00 WEU SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 115XJ 340A115 DURING CLIMB-OUT, LEFT CHIP DETECT LIGHT ILLUMINATED. AFTER CANCELLING THE MASTER CAUTION, THE CHIP LIGHT WOULD RE-ILLU MINATE ALMOST IMMEDIATELY. THE LIGHT EXTINGUISHED AFTER REDUCING POWER BELOW APPROXIMATELY 60 PERCENT TORQUE. LIGHT RE MAINED EXTINGUISHED BELOW 60 PERCENT TORQUE, AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED WEU. OPS CHECK GOOD IAW SA AB AMM. NO CHIP DETECTOR LIGHT ILLUMINATED, RAN AIRCRAFT ON THE GROUND AT GROUND IDLE FOR 15 MINUTES. 2 L 7 2 4T RT A52EU 1999043000807 19990430 00807 EU 1999 4 30 MALA976433 1 19990415 A 7930 HARNESS SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 115XJ 340A115 AFTER TAKEOFF, ENGINE LIGHT ILLUMINATED WITH CHIME, LEFT CHIP DETECT LIGHT ALSO ILLUMINATED. LIGHTS WOULD NOT CANCEL AN D REMAINED ILLUMINATED UNTIL POWER WAS REDUCED TO 50 PERCENT TORQUE, ALL OTHER ENGINE GAUGES INDICATED NORMAL. RETURNED TO DTW. MAINTENANCE REPLACED LEFT ENGINE GREEN HARNESS IAW GEMM 74-00-00. TEST FLIGHT SATISFACTORY, COMPLETED WALK AR OUND, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 1999043000808 19990430 00808 EU 1999 4 30 MALA976434 1 19990416 A 7930 CONNECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 115XJ 340A115 IN FLIGHT, THE LEFT ENGINE OIL TEMP GAUGE WENT FULL SCALE TO THE RIGHT. ALL OTHER ENGINE PARAMETERS NORMAL. AIRCRAFT R ETURNED TO DTW. MAINTENANCE CLEANED AND RESECURED CANNON PLUG, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 1999043000809 19990430 00809 1999 4 30 MALA976435 3 19990419 A 6140 522795 TEMP GAUGE SAAB SF340 SF340A 7850100 EU LT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 115XJ 340A115 ON CLIMB-OUT OF DTW, OIL PROP PSI AND TEMP FLUCTUATED INTO YELLOW ON TEMP AND DOWN TO 50 PSI ON OIL. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT PROP OIL TEMP AND PRESS GAUGE. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999043000810 19990430 00810 1999 4 30 MALA976436 3 19990417 A 6140 CTOT PANEL SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 414XJ 340B414 ON CLIMB-OUT, WITH POWER LEVERS AHEAD OF 64 DEGREE SWITCH, AUTOCOARSEN HIGH LIGHT AND LOW LIGHT ALTERNATE RESPECTIVELY. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED CTOT PANEL. OPS CHECK GOOD ON GROUND. ALL IAW SAAB MM 61-22-00. 2 L 7 2 4T RT A52EU 1999043000811 19990430 00811 EU 1999 4 30 MALA976437 1 19990419 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 429XJ 429 AT CRUISE ALTITUDE, CARGO SMOKE LIGHT ON CWP CAME ON, ACTIVATED NR 1 CARGO EXTINGUISHER, LIGHT WENT OUT. FOLLOWED QRH F OR CARGO SMOKE, AS PER QRH ACTIVATED BOTH CARGO EXTINGUISHERS, NR 1 FOLLOWED BY NR 2 BOTTLE, AFTER 5 MINUTES FIRED BECAU SE CARGO SMOKE ILLUMINATED ON CWP AGAIN. AIRCRAFT DIVERTED IN CMH. MAINTENANCE CLEANED BOTH SMOKE DETECTOR PHOTO OPTIC S AND CONNECTOR PER MM 26-13-00-7. ALL CHECKS AND TEST NORMAL. 2 L 7 2 4T RT A52EU 1999043000812 19990430 00812 WP 1999 4 30 CALA9900430 1 19990422 A 5240 GUSSET DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A .5 INCH CRACK IN GUSSET AT FORWARD END OF NR 1 BEAM ON FORWARD SERVICE DOOR. A NEW GUSSET WAS INSTAL LED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999043000813 19990430 00813 WP 1999 4 30 CALA9900431 1 19990422 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15820 49480 INSPECTION FOUND A .5 INCH CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. THE BEAM WAS REMOVED AND REPLACED IA W SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999043000814 19990430 00814 NE 1999 4 30 COMA9910064 2 19990420 A 7310 12018198035 FUEL LINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 257CA 120248 FUEL LEAK LEFT ENGINE. REPLACED LEAKING FUEL LINE AT LEFT HAND ENGINE FUEL CONTROL UNIT. 2 L 7 2 4T 4 T RT A31SO E20NE 1999043000815 19990430 00815 EA 1999 4 30 COMA9960165 1 19990420 A 3350 60206 SIGN CNDAIR CL600 CL6002B19 EA EMER EXIT INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 979CA 7159 LEFT OVERWING EMERGENCY EXIT SIGN IS INOPERABLE. REPLACED EXIT SIGN. 2 L 7 2 4F RT A21EA 1999043000816 19990430 00816 EA 1999 4 30 COMA9960166 1 19990420 A 5210 H2912A SPRING CNDAIR CL600 CL6002B19 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 952CA 7092 CABIN DOOR WARNING AFTER TAKEOFF. REPLACED OUTER HANDLE LATCH SPRING. 2 L 7 2 4F RT A21EA 1999043000817 19990430 00817 NM 1999 4 30 UPS99229375 1 19990409 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 851 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI BS 851 STR 2 RT FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 53-10-3 CPCP. 2 L 7 3 4F A3WE 1999043000818 19990430 00818 NM 1999 4 30 UPS99529376 1 19990416 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 1375 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:C AFT CARGO COMPARTMENT FLOOR TO S/W SUPPORT PLATE STA 1375 RT IS PUNCTURED. REMOVED DAMAGED SECTION. F ABRICATED A NEW DOUBLER. ALODINED AND PRIMED DOUBLER. INSTALLED DOUBLER. ALL WORK ACCOMPLISHED IAW SRM 51-70-13 AND 5 1-40-2 2 L 7 2 4F RT A2NM 1999043000819 19990430 00819 WP 1999 4 30 UPS99829377 1 19990421 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 702UP 45902 EMERGENCY LIGHTS INOP, BATTERY VOLTAGE 22V ON BISE CK. REMOVED AND REPLACED EMERGENCY BATTERY PACK, PER MM-33-50-01, OP S CK NORMAL P/N OFF 60-1223-5, P/N ON 5708458-503, P/N OFF 230 S/N ON 187. 2 L 7 4 4F RT 4A25 1999043000820 19990430 00820 WP 1999 4 30 UPS99829378 1 19990420 A 5610 WINDOW DOUG DC8 DC871F 302199D WP RT COCKPIT LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 F/O WINDOW WILL NOT OPEN. GUIDE PIN JAMMED. FREEDED UP TRACK PIN AND LUBED TRACK OPS OK. 2 L 7 4 4F RT 4A25 1999043000821 19990430 00821 NM 1999 4 30 99FDEA00151 1 19990421 A 5751 HINGE BOEING 727 72722 1384002 NM RT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 415 76C030-00, RT WING-OUTBD AILERON 2ND AILERON HINGE OB HING CASTING HAS DEEP PITTED CORROSION TO MAGNESIUM CASTING . REMOVED AND REPLACED CASTING WITH NEW TYPE SANDCAST ALUM IAW BOEING INSTALL DRAW NR 65-19260 AND FASTENERS WITH SRM 5 1-30-2 AND STANDARD PRACTICES. 2 L 7 3 4F A3WE 1999043000822 19990430 00822 NM 1999 4 30 99FDEA00152 1 19990421 A 5751 HINGE BOEING 727 72722 1384002 NM RT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 417 76C030-00 RT WING OUTBD AILERON-HINGE CASTING HAS DEEP PITTED CORROSION IN MAGNESIUM CASTING. REMOVED AND REPLAC ED CASTING WITH NEW SAND CASTED ALUM CASTING PER DRW BOEING NR 65-12959 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACT ICE. 2 L 7 3 4F A3WE 1999043000823 19990430 00823 NM 1999 4 30 99FDEA00153 1 19990421 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 0063 71C709-02 HEAVY CORROSION ON SHEAR TIE AT BS 990 FWD SIDE OF LWR BILGE AREA AT OTBD SIDE OF STR 29 RT. REMOVED AND REPLACED CORROSION. TREATED AND PAINTED PER SRM 51-20-0. 2 L 7 3 4F A3WE 1999043000824 19990430 00824 NE 1999 4 30 99FDEA00154 2 19990421 A 7314 243600 PUMP BOEING 727 72725C 138400H NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 25 119FE 19301 99-0093 - NR 2 ENG FLAMED OUT PASSING 4,000 FT, 240 KNOT IND. REMOVED AND REPLACED NR 2 FUEL PUMP AND CENTRAL IAW MM 73 -21-000-4 AND MM 73-41-0001. OPS LEAK PWR CK GOOD. OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1999043000825 19990430 00825 NM 1999 4 30 99FDEA00155 1 19990422 A 2751 INDICATOR BOEING 727 7272S2F 1384O81 NM TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 207FE 22929 99-94 - ASSYMMETRIC INBD FLAP FROM 5 DEG TO 2 DEG RAN RED TABS FLAPS DID NOT LOCK OUT WHEN FLAPS EXTEND PER CKLIST. REM OVED INBD FLAP POS IND PER MM 27-52-021. OPER CK NORM. 2 L 7 3 4F A3WE 1999043000826 19990430 00826 WP 1999 4 30 ABXA9900304 1 19990330 A 5313 59114277 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 905 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 16 RIGHT WAS CRACKED AT STATION 905. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999043000827 19990430 00827 WP 1999 4 30 ABXA9900305 1 19990327 A 5313 59114279 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 17 RIGHT CRACKED AT STATION 945. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999043000828 19990430 00828 WP 1999 4 30 ABXA9900306 1 19990327 A 5313 591142235 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 3 RIGHT CRACKED AT STATION 718. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999043000829 19990430 00829 WP 1999 4 30 ABXA9900307 1 19990327 A 5320 995773925 SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 FUSELAGE FRAME SHEAR TIE CRACKED BELOW LONGERON 15 LEFT AT STATION 945. REPLACED SHEAR TIE IAW DC9 SRM 51-10-4 AND 51-3 0-2. 2 L 7 2 4F A6WE 1999043000830 19990430 00830 WP 1999 4 30 ABXA9900308 1 19990327 A 5313 59114267 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 LONGERON 13 LEFT CRACKED AT STATION 965 LOWER ATTACH BOLT. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999043000831 19990430 00831 WP 1999 4 30 ABXA9900309 1 19990327 A 5311 99113832 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 389 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 FUSELAGE FRAME CRACKED AT STATION 389 AND LONGERON 5 RIGHT. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999043000832 19990430 00832 WP 1999 4 30 MWEA99184 1 19990420 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR LOW PRESSURE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 THE GALLEY DOOR ESCAPE SLIDE PRESSURE IS LOW. MAINTENANCE REMOVED AND REPLACED GALLEY SLIDE. 2 L 7 2 4F A6WE 1999043000833 19990430 00833 WP 1999 4 30 MWEA99185 1 19990420 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 THE FORWARD GALLEY DOOR SLIDE FELL OFF. MAINTENANCE REINSTALLED FORWARD GALLEY SERVICE DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999043000834 19990430 00834 WP 1999 4 30 MWEA99186 1 19990330 A 5320 29129015 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 465-480 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FORWARD CARGO COMPARTMENT L27R INTERCOSTAL IS CRACKED FS 465 TO 480. FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 1999043000835 19990430 00835 WP 1999 4 30 MWEA99187 1 19990407 A 5320 5910157 PAN DOUG DC9 DC914 3022034 WP BS 258 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT CARGO OUTER PAN CRACKED AT FUSELAGE 758. FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 1999043000836 19990430 00836 WP 1999 4 30 MWEA99188 1 19990407 A 5312 591016342N BLKHD STIFFNER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT PRESSURE BULKHEAD NUMBER 14R RADIAL STIFFENER IS CRACKED. REPLACED STIFFENER. 2 L 7 2 4F A6WE 1999043000837 19990430 00837 WP 1999 4 30 MWEA99189 1 19990407 A 5320 591016341N STIFFNER DOUG DC9 DC914 3022034 WP BS 908 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT PRESSURE BULKHEAD NUMBER 14 RADIAL STIFFENER IS CRACKED FUSELAGE 908. REPLACED STIFFENER. 2 L 7 2 4F A6WE 1999043000838 19990430 00838 WP 1999 4 30 MWEA99190 1 19990407 A 5312 591016342N BLKHD STIFFNER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT PRESSURE BULKHEAD NUMBER 4 RADIAL STIFFENER IS CRACKED. REPLACED STIFFENER. 2 L 7 2 4F A6WE 1999043000839 19990430 00839 WP 1999 4 30 MWEA99191 1 19990407 A 5312 591016343N BLKHD STIFFINER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT PRESSURE BULKHEAD NUMBER 4L RADIAL STIFFENER IS CRACKED. REPLACED STIFFENER. 2 L 7 2 4F A6WE 1999043000840 19990430 00840 WP 1999 4 30 MWEA99192 1 19990407 A 5312 591016343N BLKHD STIFFINER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 AFT PRESSURE BULKHEAD NUMBER 9L RADIAL STIFFENER IS CRACKED. REPLACED STIFFENER. 2 L 7 2 4F A6WE 1999043000841 19990430 00841 WP 1999 4 30 MWEA99193 1 19990407 A 5713 5911280 STRINGER DOUG DC9 DC914 3022034 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT WING STRINGER NUMBER 22 HAS CORROSION. FABRICATED AND INSTALLED STRAP. 2 L 7 2 4F A6WE 1999043000842 19990430 00842 WP 1999 4 30 MWEA99194 1 19990407 A 5713 5911279 STRINGER DOUG DC9 DC914 3022034 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT WING STRINGER 20 HAS CORROSION. FABRICATED AND INSTALLED STRAP. 2 L 7 2 4F A6WE 1999043000843 19990430 00843 WP 1999 4 30 MWEA99195 1 19990407 A 5713 5911276 STRINGER DOUG DC9 DC914 3022034 WP WS 585 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LEFT HAND WING STRINGER NUMBER 15 HAS INTERGRANULAR CORROSION XCW 585 TEE CAP AREA. FABRICATED AND INSTALLED STRAP. 2 L 7 2 4F A6WE 1999043000844 19990430 00844 NM 1999 4 30 P5CA9900549 1 19990419 A 5730 PANEL BOEING 747 747123 1384873 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FOUND RIGHT WING FLYING PANEL CRACKED. REPAIRED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1999043000845 19990430 00845 NM 1999 4 30 P5CA9900550 1 19990419 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM BS1800 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FOUND FLOORBEAM AFT CARGO PIT STA 1800R DAMAGED. REPAIRED PER SRM 51-30-02 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1999043000846 19990430 00846 NM 1999 4 30 P5CA9900551 1 19990414 A 7110 COWL BOEING 747 747123 1384873 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 OUTBOARD POWER COWL IS CRACKED AT PREVIOUS WELD AREA. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999043000847 19990430 00847 NM 1999 4 30 P5CA9900552 1 19990414 A 7110 COWL BOEING 747 747123 1384873 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 INBOARD POWER COWL EXTERNAL DOUBLER REPAIR FOUND 2 INCH CRACK. REPAIRED DOUBLER PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999043000848 19990430 00848 NM 1999 4 30 P5CA9900553 1 19990414 A 7110 COWL BOEING 747 747123 1384873 NM NR 3 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FOUND NR 3 INBD POWER COWL FWD END CENTER STIFFENER ATTACH ANGLE BROKEN. REPAIRED PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1999043000849 19990430 00849 NM 1999 4 30 P5CA9900554 1 19990414 A 7830 FITTING BOEING 747 747123 1384873 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FOUND NR 1 ENGINE STRINGER ASSY ATTACH FITTING CRACKED. REPAIRED PER SRM 51-10-01 AND MM 78-11-01. 2 L 7 4 4F A20WE 1999043000850 19990430 00850 NM 1999 4 30 P5CA9900555 1 19990414 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1780 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT CARGO PIT AREA BS 1780 STR 25R T CAP SECTION CRACKED. REPAIRED PER SRM 51-40-03 AND 51-30-02. 2 L 7 4 4F A20WE 1999043000851 19990430 00851 NM 1999 4 30 P5CA9900556 1 19990414 A 7110 COWL BOEING 747 747123 1384873 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 INBD POWER COWL NR 4 LATCH AREA FOUND TEAR. REPAIRED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1999043000852 19990430 00852 NM 1999 4 30 P5CA9900557 1 19990414 A 7110 DOUBLER BOEING 747 747123 1384873 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 OUTBOARD POWER COWL INNER DOUBLER FOUND CRACKED. REPAIRED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1999043000853 19990430 00853 NM 1999 4 30 P5CA9900558 1 19990414 A 7110 FRAME BOEING 747 747123 1384873 NM NR 3 ENGINE COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 INBOARD POWER COWL NR 3 LATCH AREA HAS FRAME/OUTER SKIN DAMAGE. REPAIRED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1999043001055 19990430 01055 WP 1999 4 30 RRXA99191 1 19990407 A 3233 PIN DOUG DC8 DC871F 302199D WP RT MLG ACTUATOR FAILED A RRXA O OTHER E VIBRATION/BUFFET AP APPROACH 1 WP 15 8084U 45974 UPON GEAR DOWN SELECTION, LOUD (EXPLOSIVE) BANG CAUSED AIRCRAFT TO SHUTTER VIOLENTLY ALL INDICATIONS NORMAL. FOUND RT M AIN LANDING GEAR ACTUATOR PIN BROKEN SECURED ACTUATOR TO GEAR. INSTALLED 3 GEAR PINS AND SAFTIED. I HAVE INSPECTED THI S ACFT AND FOUND IT SAFE FOR FLIGHT INTENDED. REMOVED AND REPLACED RIGHT MLG RETRACT PIN AND REWORK OF MLG PIN BOSS IAW S/B 32-102 AND APPROVED 8110-3 DATED 04/13/99. GEAR SWING C/W PER DC-8 M/M 32-10-00. OPS CHECKS GOOD PER DC-8 MM 32-1 0-00. 2 L 7 4 4F RT 4A25 1999043001056 19990430 01056 WP 1999 4 30 RRXA99661 1 19990416 A 3610 D51P58111101 BLEED DUCT DOUG DC8 DC873F 302199F WP NR 4 ENGINE BLOWN A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 2674U 46062 REDUCED EPR TO AT 3000 FT, ALT NR 4 ENG FIRE WARNING WHEN THROTTLE WAS PULLED TO IDLE LT AND BFW WENT OUT RTB TO KGSO. F OUND BLOWN DUCT REMOVED AND REPLACED DUCT IAW MM CHAPTER 75 ENGINE OPS CK GOOD ON ENGINE RUN, NO DEFECTS NOTED ON NR 4 E NGINE. 2 L 7 4 4F RT 4A25 1999043001057 19990430 01057 WP 1999 4 30 RRXA99662 1 19990417 A 2130 PRESSURIZATION DOUG DC8 DC873 302199C WP CABIN MALFUNCTIONED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 105WP 46095 UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT FERRIED TO BIRMINGHAM FOR DOOR MAINTENANCE. 2 L 7 4 4F RT 4A25 1999043001058 19990430 01058 WP 1999 4 30 TWAA9905901 1 19990421 A 5320 RIVET DOUG DC9 DC982 3022082 WP BS 50 LOOSE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 913TW 49184 A .25 INCH PULLED RIVET WAS FOUND AT STA 50, LONGERON 20. EDDY CURRENT SHOWED NO CRACK. INSTALLED .25 INCH IN SOLID RI VET PER SRM 53-01, FIG 1. CHECK-C 1-10-99 STL. 2 L 7 2 4F A6WE 1999043001059 19990430 01059 NM 1999 4 30 RAAA99B2027 1 19990421 A 5320 CHANNEL BOEING 727 72722C 138400F NM BS 340 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C CHECK, FOUND FORWARD LAV AFT BULKHEAD FLOORBEAM CHANNEL CORRODED AT BS 340 AND RBL 20 T0 RBL 26. REM OVED FLOORBEAM CHANNEL, FABRICATED NEW CHANNEL IAW SRM 51-10-02-TREATED AND PRIMED IAW SRM 51-10-06. INSTALLED CHANNE L IAW SRM 51-30-02, M54 NO 418. 2 L 7 3 4F A3WE 1999043001060 19990430 01060 NM 1999 4 30 RAAA99B2028 1 19990421 A 5321 FLOOR BOEING 727 72722C 138400F NM BS 320-340 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C CHECK, FOUND CORROSION ON FORWARD LAV FLOORBOARD ATTACH HOLES AND CAP SECTION OF CHANNEL BS320 TO 340 7 RBL14 TO RBL16. REMOVED CORROSION ON FLOORBOARD AND CAP SECTION AND TREATED AND PRIMED IAW SRM 51-10-06. REMOVED CH ANNEL AND FABRICATED NEW CHANNEL 7075 T6 .094 IAW 51-10-02. TREATED AND PRIMED IAW SRM 51-10-06. INSTALLED IAW 51-3-02 M54-420. 2 L 7 3 4F A3WE 1999043001061 19990430 01061 NM 1999 4 30 RAAA99B2029 1 19990421 A 5321 FLOOR BOEING 727 72722C 138400F NM BS 303-340 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C CHECK, FOUND CORROSION ON FLOOR PLATE AROUND FWD LAV DUMP PIPE TOP AND BOTTOM SURFACES BS 303 TO 344. REMOVED CORROSION IAW SRM 51-10-06. TREATED AND PRIMED IAW SRM 51-10-06. REMOVED SUPPORT ANGLES AND FABRICATED NEW A NGLES OF 7075T6 .094 IAW SRM 51-10-02 TREATED AND PRIMED IAW SRM 51-10-06. INSTALLED IAW SRM 51-30-02, M54-422. 2 L 7 3 4F A3WE 1999043001062 19990430 01062 NM 1999 4 30 RAAA99B2030 1 19990421 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 340-360 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C CHECK, FOUND SEAT TRACK CORRODED FROM BS340 TO 360 RT. INSTALLED NEW SEAT TRACK IAW SRM 51-10-01. 2 L 7 3 4F A3WE 1999043001063 19990430 01063 NM 1999 4 30 UPS99229379 1 19990422 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 MAIN CABIN EMERGENCY EXIT LIGHT ABOVE REAR DOOR, AND MAIN CABIN OVERWING EMERGENCY LIGHT (LT SIDE AFT LOWER) INOP. REMO VED AND REPLACED BOTH LIGHTS. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999043001064 19990430 01064 WP 1999 4 30 UPS99829380 1 19990422 A 3397 WIRE DOUG DC8 DC871F 302199D WP CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 797UP 45897 COCKPIT DOME LIGHT DOSE NOT ILLUMINATE ON PREFLIGHT CHECK OF EMERGENCY LIGHTS DETERMINED 3 EACH PWR WIRES ARE INOP A T JUNCTION. REF WDM 33-50-01 REPAIRED WIRES, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999043001065 19990430 01065 EU 1999 4 30 QXEA9900588 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 5305-9805 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT INBOARD SEAT TRACK FROM STATION 5305 TO 9805 REQUIRES REPLACEMENT DUE TO NUMEROUS DAMAGE SPOTS. REPLACED IA W FOKKER SRM 53-02-15, FIGURE 1. 2 L 7 2 4F RT A20EU 1999043001066 19990430 01066 EU 1999 4 30 QXEA9900589 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805-9305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L HAS 1 LONGITUDINAL WEAR MARK INSIDE CHANNEL FROM FRAME 9805 TO 9305C. REPAIRED I AW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001067 19990430 01067 EU 1999 4 30 QXEA9900590 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L INSIDE CHANNEL HAS 11 LONG CHAFE MARK AT FRAME 11405. REPAIRED IAW FOKKER MM 53- 40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001068 19990430 01068 EU 1999 4 30 QXEA9900591 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS FROM FRAME 11905. REPAIRED IAW FOKK ER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001069 19990430 01069 EU 1999 4 30 QXEA9900592 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L, (2) SEAT PEG HOLES HAVE GOUGES INSIDE BORE AND INSIDE CHANNEL AT FRAME 13815B. R EPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001070 19990430 01070 EU 1999 4 30 QXEA9900593 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L INBOARD FLANGE TOP SIDE HAS .25 DIAMETER BY APPROXIMATELY .010 DEEP CHAFE MARK WI TH CORROSION, 6 AFT OF FRAME 14285. REPAIRED IAW HORIZON AIR EA 4-53-736. 2 L 7 2 4F RT A20EU 1999043001071 19990430 01071 EU 1999 4 30 QXEA9900594 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305-7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L INBOARD AND OUTBOARD FLANGES HAVE FRETTING CORROSION ON TOPSIDE FROM FRAME 8305 TO 7305. REPAIRED IAW FOKKER MM 53-40-1, PAGE 206. 2 L 7 2 4F RT A20EU 1999043001072 19990430 01072 EU 1999 4 30 QXEA9900595 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8805-8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L INBOARD AND OUTBOARD FLANGES HAVE FRETTING CORROSION ON TOPSIDE FROM FRAME 8805 TO 8305. REPAIRED IAW FOKKER MM 53-40-1, PAGE 206. 2 L 7 2 4F RT A20EU 1999043001073 19990430 01073 EU 1999 4 30 QXEA9900596 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8805-8305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL RUNNING BETWEEN FRAMES 8805 AND 8305. RE PAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001074 19990430 01074 EU 1999 4 30 QXEA9900597 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL FRAME 9305. REPAIRED IAW FOKKER MM 53-40 -01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001075 19990430 01075 EU 1999 4 30 QXEA9900598 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL AT FRAME 9305B AND RUNS 12 FORWARD. REPA IRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001076 19990430 01076 EU 1999 4 30 QXEA9900599 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805-9305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL BETWEEN FRAME 9805 AND 9305C. REPAIRED I AW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001077 19990430 01077 EU 1999 4 30 QXEA9900600 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905-9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L INBOARD AND OUTBOARD FLANGES TOPSIDE AREAS MARKED WITH FRETTING CORROSION BETWEEN F RAME 11905 AND 9805. REPAIRED IAW FOKKER MM 53-40-1 AND EA 4-53-736. 2 L 7 2 4F RT A20EU 1999043001078 19990430 01078 EU 1999 4 30 QXEA9900601 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11405 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL FROM FRAME 11405 TO 10966. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001079 19990430 01079 EU 1999 4 30 QXEA9900602 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL FROM FRAME 11905 TO 12405. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001080 19990430 01080 EU 1999 4 30 QXEA9900603 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, INBOARD AND OUTBOARD FLANGES HAVE FRETTING CORROSION AREAS BETWEEN FRAME 13345 AND 11905. REPAIRED IAW FOKKER MM 53-40-01, PAGE 204. 2 L 7 2 4F RT A20EU 1999043001081 19990430 01081 EU 1999 4 30 QXEA9900604 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL 8 FORWARD OF FRAME 13815. REPAIRED IAW F OKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001082 19990430 01082 EU 1999 4 30 QXEA9900605 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT SEAT TRACK BL600L, INBOARD AND OUTBOARD FLANGES HAVE AREAS OF FRETTING CORROSION BETWEEN FRAME 14285 AND 1381 5. REPAIRED IAW FOKKER MM 53-40-1, PAGE 204. 2 L 7 2 4F RT A20EU 1999043001083 19990430 01083 EU 1999 4 30 QXEA9900606 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL APPROXIMATELY 12 LONG AT FRAME 14755. RE PAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001084 19990430 01084 EU 1999 4 30 QXEA9900607 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT INBOARD SEAT TRACK BL600L, 2 .5 DIAMETER BY .008 DEEP WEAR MARKS ON INBOARD FLANGE 6 AFT OF FRAME 14755. REP AIRED IAW FOKKER MM 53-40-1 AND HORIZON AIR EA 4-53-736. 2 L 7 2 4F RT A20EU 1999043001085 19990430 01085 EU 1999 4 30 QXEA9900608 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT INBOARD SEAT TRACK BL600R, 2 SEAT PEG HOLES HAVE GOUGES INSIDE BORE AND TOP OF TRACK AT FRAME 6305. REPAIRE D IAW FOKKER 53-40-01AND 51-10-4, PAGE 9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999043001086 19990430 01086 EU 1999 4 30 QXEA9900609 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT INBOARD SEAT TRACK BL600R INSIDE CHANNEL HAD 2 LONGITUDINAL WEAR MARKS BETWEEN FRAME 5805 AND 6305. REPAIRE D IAW FOKKER MM 53-40-1, PAGE 205, FIGURE 204. 2 L 7 2 4F RT A20EU 1999043001087 19990430 01087 EU 1999 4 30 QXEA9900610 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INBOARD FLANGE ON TOP SIDE HAS CORROSION AT FRAME 4610. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001088 19990430 01088 EU 1999 4 30 QXEA9900611 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 4 SEAT PEG HOLES HAVE GOUGES AND CORROSION INSIDE BORE AND TOP SURFACE OF TRACK AT FRAME 6305. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001089 19990430 01089 EU 1999 4 30 QXEA9900612 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS FROM FRAME 5805 TO 6305. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001090 19990430 01090 EU 1999 4 30 QXEA9900613 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5305-6305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R HAS SURFACE CORROSION ON INBOARD AND OUTBOARD FLANGES TOPSIDE FROM FRAME 5305 TO 6305. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001091 19990430 01091 EU 1999 4 30 QXEA9900614 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, SEAT PEG HOLE HAS CORROSION INSIDE BORE 4 FORWARD OF FRAME 6805. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001092 19990430 01092 EU 1999 4 30 QXEA9900615 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, SEAT PEG HOLE HAS GOUGES INSIDE BASE AND CORROSION AT FRAME 6805. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001093 19990430 01093 EU 1999 4 30 QXEA9900616 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS 7 FORWARD AND 7 AFT OF FRAME 9305. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001094 19990430 01094 EU 1999 4 30 QXEA9900617 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS 13, BETWEEN FRAME 6805 AND 7305. R EPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001095 19990430 01095 EU 1999 4 30 QXEA9900618 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305-8805 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS 12 LONG BETWEEN FRAMES 8305 AND 88 05. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001096 19990430 01096 EU 1999 4 30 QXEA9900619 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL112R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS FROM FRAME 9305A TO 9305B. REPAIRE D IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001097 19990430 01097 EU 1999 4 30 QXEA9900620 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 3 SEAT PEG HOLES HAVE GOUGES INSIDE BORE AT FRAME 9305B. REPAIRED IAW FOKKER M M 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001098 19990430 01098 EU 1999 4 30 QXEA9900621 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 2 SEAT PEG HOLES HAVE GOUGES AROUND TOP SURFACE OF TRACK AT FRAME 9305C. REPAI RED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE205. 2 L 7 2 4F RT A20EU 1999043001099 19990430 01099 EU 1999 4 30 QXEA9900622 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS, 7 FORWARD AND 7 AFT OF FRAME 1034 6. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001100 19990430 01100 EU 1999 4 30 QXEA9900623 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS BETWEEN FRAME 10966 TO 11405. REP AIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001101 19990430 01101 EU 1999 4 30 QXEA9900624 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11405 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 4 SEAT PEG HOLES HAVE GOUGES INSIDE BORE AT FRAME 11405. REPAIRED IAW FOKKER M M 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001102 19990430 01102 EU 1999 4 30 QXEA9900625 1 19990319 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 1 SEAT PEG HOLE HAS GOUGES INSIDE BORE 4 AFT OF FRAME 11905. REPAIRED IAW FOKK ER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001103 19990430 01103 EU 1999 4 30 QXEA9900626 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS AT FRAME 11905. REPAIRED IAW FOKK ER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001104 19990430 01104 EU 1999 4 30 QXEA9900627 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12875 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS RUNNING 10 AFT OF FRAME 12875. R EPAIRED IAW FOKKER MM 53-40-01, PAGE 205, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001105 19990430 01105 EU 1999 4 30 QXEA9900628 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12875 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 2 SEAT PEG HOLES HAVE DEEP GOUGES AT INSIDE BORE AT FRAME 12875. REPAIRED IAW FOKKER MM 51-3101, 51-11-04 AND 51-30-02. 2 L 7 2 4F RT A20EU 1999043001106 19990430 01106 EU 1999 4 30 QXEA9900629 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 2 SEAT PEG HOLES HAVE GOUGES AT TOP SURFACE OF TRACK 6 AFT OF FRAME 13815A. RE PAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001107 19990430 01107 EU 1999 4 30 QXEA9900630 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INSIDE CHANNEL HAS 2 LONGITUDINAL WEAR MARKS RUNNING FROM FRAME 13815B TO 14285 . REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001108 19990430 01108 EU 1999 4 30 QXEA9900631 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 2 SEAT PEG HOLES HAVE GOUGES AT TOP OF SEAT TRACK AT FRAME 13815B. REPAIRED IA W FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001109 19990430 01109 EU 1999 4 30 QXEA9900632 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 5 SEAT PEG HOLES HAVE GOUGES AT TOP OF SEAT TRACK BETWEEN FRAMES 14755 AND14285 . REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001110 19990430 01110 EU 1999 4 30 QXEA9900633 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 5 SEAT PEG HOLES HAVE GOUGES AND CORROSION INSIDE BORE AND TOP SURFACE OF TRACK BETWEEN FRAMES 6805 AND 7305. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001111 19990430 01111 EU 1999 4 30 QXEA9900634 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305-7805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, 5 SEAT PEG HOLES HAVE GOUGES AND CORROSION AROUND INSIDE BORE BETWEEN FRAMES 73 05 AND 7805. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001112 19990430 01112 EU 1999 4 30 QXEA9900635 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, HAS PITTING CORROSION ON TOP SURFACE OF TRACK AROUND SEAT PEG HOLE, 2 FORWARD O F FRAME 8805. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001113 19990430 01113 EU 1999 4 30 QXEA9900636 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK BL1127R, INBOARD AND OUTBOARD FLANGES TOPSIDE HAVE LIGHT SURFACE CORROSION BETWEEN FRAME S 11905 AND 10966. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999043001114 19990430 01114 EU 1999 4 30 QXEA9900637 1 19990325 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16060 BETWEEN STRINGERS 25 AND 26. REPAIRED IAW FOKKER SRM 53-02-03, PAGE 4, FIG URE 2. 2 L 7 2 4F RT A20EU 1999043001115 19990430 01115 NM 1999 4 30 99FDEA00156 1 19990421 A 5315 654027512 FLOORBEAM BOEING 727 727247 138408F NM BS 1090 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FOUND FLOORBEAM TO BE CORRODED AT BS 1090, RBL 45, WL 208. *S/D* REMOVED AND REPLACED UPPER FLANGE OF FLOORBEAM PER FE DEX EA 7-5310-45246. 2 L 7 3 4F A3WE 1999043001116 19990430 01116 NM 1999 4 30 99FDEA00157 1 19990421 A 5330 6554583164 SKIN BOEING 727 727247 138408F NM BS 1115 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 SKIN BULGING AT BS 1115 BETWEEN STR 26L AND 27L. *S/D* REMOVED AND REPLACED SKIN BULGE PER IAW FEDEX EA 7-5330-45222. 2 L 7 3 4F A3WE 1999043001117 19990430 01117 WP 1999 4 30 ABXA9900310 1 19990414 A 5720 591047278ABX1 TIP DOUG DOUG DC9 DC931 3022065 WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND RIGHT WING TIP, UPPER AND LOWER INTERIOR SURFACE CORRODED. REPLACED WING TIP. 2 L 7 2 4F A6WE 1999043001118 19990430 01118 WP 1999 4 30 ABXA9900311 1 19990414 A 5720 5912156157 DOUBLER DOUG DOUG DC9 DC931 3022065 WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 FOUND RIGHT WING TRAILING EDGE DOUBLER CORRODED JUST INBOARD OF INBOARD SPOILER PANEL. REPLACED DOUBLER IAW DACO DWG 591 2156 AND DC9 SRM 57-31-3. 2 L 7 2 4F A6WE 1999043001119 19990430 01119 WP 1999 4 30 ABXA9900312 1 19990414 A 5730 5912156214 SKIN DOUG DOUG DC9 DC931 3022065 WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE SKIN CORRODED INBOARD OF INBOARD SPOILER PANEL. REPAIRED SKIN IAW DC9 SR M 57-01. 2 L 7 2 4F A6WE 1999043001120 19990430 01120 WP 1999 4 30 ABXA9900313 1 19990414 A 5720 99100483 ANGLE DOUG DOUG DC9 DC931 3022065 WP RT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND RIGHT TRAPEZOIDAL PANEL ATTACH ANGLE EXFOLIATED. REPLACED ATTACH ANGLE IAW DC9 SRM 57-30-1. 2 L 7 2 4F A6WE 1999043001121 19990430 01121 WP 1999 4 30 ABXA9900314 1 19990414 A 5315 9915527505 FLOORBEAM DOUG DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND FLOORBEAM CRACKED AT STATION 680, UNDER FLOOR TRACK AT LBL54. REPLACED FLOORBEAM IAW DC9 SRM 51-3 0-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999043001122 19990430 01122 WP 1999 4 30 ABXA9900315 1 19990415 A 5312 5910130275 BULKHEAD WEB DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD WEB CORRODED BETWEEN LONGERONS 29 LEFT AND 29 RIGHT. REPAIRED IAW ABX R EA D953-28164MR. 2 L 7 2 4F A6WE 1999043001123 19990430 01123 1999 4 30 DL76L990780 4 19990410 A 2330 ENTERTAIN SYS BOEING 767 767332 1382001 NM PAX CABIN SMOKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 180DN 23630 25985 IR - ELECTRICAL ODOR NOTICED BETWEEN MID-LAVS. ENTERTAINMENT SYSTEM AND LAV SYS CB'S PULLED. FLT DIVERTED TO SNN. VID EO ENTERTAINMENT SYSTEM COMPLETELY DE-ACTIVATED. GALLEY OVEN CB'S PULLED. PANELS REMOVED IN AREA OVERHEAD MID-LAVS AND GALLEYS. NO EVIDENCE OF SMOKE. REPLACED OVEN AND BOTH MID GALLEY COFFEE MAKERS. RAN ENGINES AND PRESSURIZED A/C. RAN ALL GALLEY CHILLERS, COFFEE MAKERS, ENTERTAINMENT SYSTEM. NO EVIDENCE OF FUMES. A/C OK FOR SERVICE. 2 L 7 2 4F RT A1NM 1999043001124 19990430 01124 NM 1999 4 30 DL76L990799 1 19990411 A 2530 811150415 COFFEE MAKER BOEING 767 767332 1382001 NM GALLEY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 180DN 25985 MAINTENANCE: WORKING MSU ON HISTORY OF ELECTRIC SMELL IN MIDGALLEY AREA. FOUND MID GALLEY FWD COFFEE MAKER BURNER LOOSE AND RESTING ON STAINLESS STEEL SCUPPER DRAIN, WHICH IN TURN MELTED THE PLASTIC TRIM BELOW. REPLACED COFFEE MAKER, CK'D FOR VERIFICATION OF NO FURTHER SMELL. 2 L 7 2 4F RT A1NM 1999043001125 19990430 01125 NM 1999 4 30 DL76G990813 1 19990412 A 2530 OUTLET BOEING 767 767332 1382001 NM GALLEY SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1603 29695 UTILITY OUTLET IN FIRST CLASS GALLEY EXTREMELY HOT TO THE POINT OF FUMES IN THE CABIN. ACFT DIVERTED TO ORD. DEACTIVAT ED AS PER ERA 370761-14. 2 L 7 2 4F RT A1NM 1999043001126 19990430 01126 NM 1999 4 30 DL76L990815 1 19990412 A 3697 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR1 ENGINE BROKEN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 172DN 24775 724692 LEFT ENGINE BLEED LIGHT ILLUMINATED AT FLT LEVEL 280. FOUND TWO BROKEN WIRES AT HPSOV, STUD 3. INSTALLED NEW TERMINAL, SYSTEM CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999043001127 19990430 01127 1999 4 30 DL76L990829 2 19990411 A 7200 ENGINE BOEING 767 767332 1382001 NM NR 1 FAILED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 178DN 15560 25143 724636 FOUND METAL ON NR 3 BEARING CHIP DETECTOR. REPLACED ENGINE. 2 L 7 2 4F RT A1NM 1999043001128 19990430 01128 NM 1999 4 30 DL76G990834 1 19990414 A 2613 OVERHEAT LOOP BOEING 767 767324 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 394DL 7962 27394 704234 AT FL330, LEFT ENGINE OVHT LIGHT ON PEDESTAL. RETARDED ENG TO IDLE, LIGHT REMAINED ON FOR APPROX 3 MINUTES. NO ASSOCIA TED MASTER CAUTION OR EICAS MESSAGE. REPLACED OVHT DET LOOP M684 AND LOGIC TEST CARD. ALSO, CHECKED ALL CLAMPS ON ENGI NE AND TIGHTENED SAME. SYSTEM CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 1999043001129 19990430 01129 NM 1999 4 30 DL76S990847 1 19990406 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM LT EMER EXIT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 131DN 24852 LT OVERWING EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED POWER SUPPLY SLED M736. OPS CHKS NML. 2 L 7 2 4F RT A1NM 1999043001130 19990430 01130 NM 1999 4 30 DL76L990849 1 19990417 A 3350 BULB BOEING 767 767332 1382001 NM ROW 23 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 172DN 24775 MCO 23F EMERG LIGHT INOP. RELAMPED AND INSTALLED LENSE LIGHT CKS GOOD. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 1999043001131 19990430 01131 NM 1999 4 30 DL76G990853 1 19990418 A 2530 OUTLET BOEING 767 767332 1382001 NM GALLEY 1R INOP A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1603 29695 CABIN CREW REPORTS BURNING ODOR IN GALLEY 1R. SUSPECT COFFEE MAKER. REPLACED 1R UTILITY OUTLET SOCKET. REACTIVATED CI RCUIT. SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999043001132 19990430 01132 NM 1999 4 30 DL76L990854 1 19990416 A 3350 BULB BOEING 767 767332 1382001 NM LT EMER EXIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 196DN 28453 DURING L/O, FOUND LT EXTERIOR OVERWING EMERGENCY LIGHTING AFT, TWO LIGHTS INOP. 2 L 7 2 4F RT A1NM 1999043001133 19990430 01133 NM 1999 4 30 DLM11990867 1 19990420 A 2530 OVEN 72077500 DOUG MD11 MD11 3023602 NM GALLEY SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 810DE 48565 SMOKE COMING FROM MID GALLEY OVEN IN FLIGHT. OVEN SHUTDOWN. OVEN SHUT OFF AND CIRCUIT BREAKER PULLED. SMOKE STOPPED. FLT ATTN REPORTS HAPPENED DURING MEAL PREPARATION. SMOKE WASNOT ELECTRICAL AND FLT ATTN DID NOT THINK IT WAS STEAM. M TC DEACTIVATED OVEN. CIRCUIT BREAKERS PULLED AND COLLARED. REPLACED OVEN AT DOWNLINE STATION. 2 L 7 3 4F RT A22WE 1999043001134 19990430 01134 NM 1999 4 30 DLM88990873 1 19990422 A 2910 LINE DOUG MD88 MD88 3023688 NM RT HYD SYST LOOSE A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 939DL 49812 UPON ARRIVAL RDU, RT HYD QTY DECREASED TO 1 QT AFTER GEAR AND PLAP EXTENSION, TIGHTENED B-NUT AT SPOILER CONTROL VALVE. 2 L 7 2 4F RT A6WE 1999043001135 19990430 01135 NM 1999 4 30 DL72W990877 1 19990422 A 2782 BRACKET BOEING 727 727247 138408F NM NR 7 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 REF NRC 83 C-2 LETTER CHECK, NR 7 SLAT ACT INBD MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-42-0. 2 L 7 3 4F A3WE 1999043001136 19990430 01136 NM 1999 4 30 DL72W990878 1 19990422 A 2782 BRACKET BOEING 727 727247 138408F NM NR 8 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 REF NRC 84 C-2 LETTER CHECK, NR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-20-22. 2 L 7 3 4F A3WE 1999043001137 19990430 01137 1999 4 30 TC8A99014 4 19990423 A 3442 RADAR BOEING 727 727173C 1384059 NM COCKPIT MALFUNCTIONED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 704A 19504 TRIP NR 3305, RADAR ONLY PAINTS TO LEFT, WON'T PAINT FWD OR RIGHT. SWAPPED NR 1 WITH NR 2 VG, GROUND TAXIED, RADAR OPS CHECK GOOD IAW BMM 34-41-00. UNABLE TO DUPLICATE ON GROUND, SWAPPED FOR T/S. 2 L 7 3 4F A3WE 1999050700037 19990507 00037 WP 1999 5 7 99ZZZX1867 2 19990414 A 7230 SEAL CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7313 01518 WP LT ENGINE FAILED A DBCA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 13 50DS 6500078 P87270 PILOT DETECTED SMOKE IN CABIN. TROUBLESHOT TO NR 4 AND NR 5 LABRYNTH SEALS IN LEFT ENGINE, SN 87270. REMOVED ENGINE SN 87270 AND INSTALLED LOANER ENGINE SN P-87267. NOTE: REPAIRED AT GARRETT SPRINGFIELD W.O. NR 73041. 2 L 7 2 4F 4 F A9NM E6WE 1999050700040 19990507 00040 CE 1999 5 7 99ZZZX1870 1 19990408 A 3233 571304034 LUG CESSNA 414 414A 2075907 CE NLG ACTUATOR BROKEN A GJAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 6562C 4162 414A0015 DURING A 135 CHARTER OPERATION, THE PILOTS WERE UNABLE TO GET A GEAR-UP SAFE LIGHT AFTER DEPARTING. UPON RETURNING TO A IRPORT WITH 3 GREEN SAFE LIGHTS, THE NOSE GEAR COLLAPSED ON LANDING ROLL-OUT, DAMAGING BOTH PROPELLERS AND SLIGHT DAMAGE TO NOSE GEAR DOORS AND NOSE STRUCTURE. INVESTIGATION REVEALED THE UPPER NOSE GEAR ACTUATOR LUGS HAD FAILED, P/N 571304 0-34. 1 L 7 2 3O A7CE 1999050700055 19990507 00055 SO 1999 5 7 99ZZZX1885 2 19990405 A 8520 SA628488 LIFTER CESSNA 210 T210M 2073451 CE CONT O520 TSIO520R 17040 SO ENGINE SPALLED A QGKA K NONE O OTHER IN INSP/MAINT 1 GL 03 761VH 481 21062549 511444 DURING 100-HOUR INSPECTION, FOUR CYLINDERS SHOWED LOW COMPRESSION. UPON REMOVAL OF CYLINDERS, NOTED THE NR 5 CYLINDER E XHAUST CAM FOLLOWER WAS SPALLED BAD. INSPECTION OF CAM LOBE DID NOT APPEAR NEARLY AS BAD AS CAM FOLLOWER. CAMSHAFT AND CAM FOLLOWERS WERE REPLACED AT THIS TIME. ENGINE HAD 481.0 HOURS SMOH. CAMSHAFT AND CAM FOLLOWERS HAD 481.0 HOURS SIN CE NEW. SUPERIOR PMA PART. 1 H 7 1 3O 3 O 3A21 E8CE 1999050700060 19990507 00060 NE 1999 5 7 TWAA9906101 2 19990427 A 7230 798404 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE TURBINE FRACTURED A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 905TW 49157 1229 CLIMBING THROUGH 12,000 FEET A LOUD BOOM WAS HEARD FROM THE LT ENGINE. THERE WAS NO THROTTLE RESPONSE. SHUT DOWN THE E NGINE AND RETURNED TO SEA. FOUND SIGNIFICANT DAMAGE TO THE COMPRESSOR AND TURBINE. CHANGED THE ENGINE. CHECK-C 12-15- 98 STL. *S/D* FOUND A FOURTH STAGE TURBINE BLADE FRACTURED DUE TO FATIGUE AND BLADE TIP RUB, CAUSING THE FRACTURE OF A LL OTHER FOURTH STAGE BLADES AND DAMAGE TO THIRD AND SECOND STAGE INNER SHROUDS. 2 L 7 2 4F 4 F A6WE E9NE 1999050700061 19990507 00061 NM 1999 5 7 TWAA9906102 1 19990427 A 3350 CONNECTOR BOEING 757 7572Q8 1384972 NM ROW 26-34 CONTAMINATED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 703TW 27620 FOUND THE EGRESS LIGHTS DIM AT ROWS 26 TO 34. DRIED OUT THE POWER SUPPLY CABLE AND THE LAMP CONNECTIONS. CHECK-C 5-9-9 8 LAX. 2 L 7 2 4F RT A2NM 1999050700062 19990507 00062 NM 1999 5 7 TWAA9906103 1 19990425 A 5754 SKIN BOEING 767 767231 1385131 NM NR 7 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 THE NR 7 LEADING EDGE SLAT TRAILING EDGE WEDGE HAD DELAMINATION APPROX 8.5 FT FROM I/B EDGE. AREAS APPROX 2.5 INCHES IN DIAMETER AND 1.5 INCH APART ON LOWER SURFACE, 2.5 INCHES FROM THE TRAILING EDGE. INSTALLED PERMANENT REPAIR PER SRM 51 -70-10, WITH CORE AND SKIN REPLACEMENT AND DOUBLER. CHECK-C 2-26-99 LAX. 2 L 7 2 4F RT A1NM 1999050700063 19990507 00063 WP 1999 5 7 AT9900334R1 1 19990422 A 5320 991556515 CHANNEL DOUG DC9 DC932 3022066 WP VENTRAL DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND AN EXISTING REPAIR DOUBLER CHAFED THRU AFT VENTRAL DOOR UPPER SECTION. RE MOVED, ORDERED, LOCATED, DRILLED, AND INSTALLED UPPER CHANNEL AND Z ANGLE IAW DC9 SRM 51-10-4, 51-30-2, 51-30-4 AND DOUG LAS DRAWING NR 9915565. Z ANGLE (P/N 9915565-133) OFF. 2 L 7 2 4F A6WE 1999050700064 19990507 00064 WP 1999 5 7 AT9900337 1 19990427 A 3610 22017931 DUCT DOUG DC9 DC932 3022066 WP LT ACM LOOSE A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 866AT 47168 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON AFTER TAKEOFF, LIGHT WENT OUT WHEN LEFT THROTTLE PULLED BACK TO IDLE. A IR RETURN. RESECURED DUCT BEFORE LEFT HAND AIR CYCLE MACHINE PER MM 36-10. OPS CHECK AND LEAK CHECK GOOD PER 36-10. 2 L 7 2 4F A6WE 1999050700065 19990507 00065 WP 1999 5 7 IXXA9900008 1 19990429 A 3350 OL3071BPE BULB DOUG DC8 DC862 3021970 WP CABIN FAILED A IXXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 31CX 1954 45911 THE FLIGHT CREW PERFORMED A POST FLIGHT CHECK LIST AT OKO, WHICH REVEALED TWO PASSENGERS EMERGENCY EXIT AISLE PATHWAY LI GHTS INOPERATIVE. MAINTENANCE REPLACED TWO LIGHT BULBS AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK. 2 L 7 4 4F 4A25 1999050700066 19990507 00066 EA 1999 5 7 COMA9960177 1 19990428 A 5270 WARNING CNDAIR CL600 CL6002B19 EA EMER EXIT DOOR ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 977CA 7157 EMERGENCY DOOR CAUTION MESSAGE. DEFERRED DOOR WARNING SYSTEM. 2 L 7 2 4F RT A21EA 1999050700067 19990507 00067 EU 1999 5 7 QXEA9900854 1 19990426 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 487US 363 11238 BOI- RIGHT HAND EVACUATION LIGHTS WERE INOPERATIVE AT BOTH EMERGENCY EXITS AND EXIT SIGN IN CENTER OF CABIN. REMOVED AN D REPLACED BATTERY POWER SUPPLY AT ROW 9, RIGHT HAND SIDE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999050700068 19990507 00068 EU 1999 5 7 QXEA9900805 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS SMALL GOUGE 2 INCHES AFT OF FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999050700069 19990507 00069 EU 1999 5 7 QXEA9900806 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS 2 SMALL GOUGES AROUND SEAT TRACK HOLES BETWEEN FRAMES 9305 AND 9305A. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999050700070 19990507 00070 EU 1999 5 7 QXEA9900807 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A SMALL GOUGE, 5 INCHES AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999050700071 19990507 00071 EU 1999 5 7 QXEA9900808 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805-8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS A 3 INCH AREA OF CORROSION BETWEEN FRAME 7805 AND 8305. REPAIRED IAW FOKKER SRM 51-40-1, PAGE 201, PARAGRAPH 4 (B). 2 L 7 2 4F RT A20EU 1999050700072 19990507 00072 EU 1999 5 7 QXEA9900809 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS CORROSION AROUND SEAT TRACK HOLE, 6 INCHES FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-40-1 PAGE 201, PARAGRAPH 4 (B). 2 L 7 2 4F RT A20EU 1999050700073 19990507 00073 EU 1999 5 7 QXEA9900810 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS SMALL GOUGES AROUND 4 SEAT TRACK HOLES, 6 INCHES FORWARD OF FRAME 7305. REPAIRE D IAW FOKKER SRM 51-10-04 AND SRM 53-40-1 PAGE 201, PARAGRAPH 4 (B). 2 L 7 2 4F RT A20EU 1999050700074 19990507 00074 EU 1999 5 7 QXEA9900811 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS SMALL GOUGES AROUND SEAT TRACK HOLE AT FRAME 6805. REPAIRED IAW FOKKER SRM 53-4 0-01. 2 L 7 2 4F RT A20EU 1999050700075 19990507 00075 EU 1999 5 7 QXEA9900812 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT FRAME 6805 AND EXTENDS 10 INCHES FORWARD. REPAIRED IAW FOKKE R SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999050700076 19990507 00076 EU 1999 5 7 QXEA9900813 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS WEAR ON TOP OF THE TRACK 3 INCHES LONG AND IS LOCATED 3 INCHES FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999050700077 19990507 00077 EU 1999 5 7 QXEA9900814 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS WEAR INSIDE THE TRACK BETWEEN FRAME 5805 AND 6305. REPAIRED IAW FOKKER SRM 51-1 0-04. 2 L 7 2 4F RT A20EU 1999050700078 19990507 00078 EU 1999 5 7 QXEA9900815 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE TRACK 2 INCHES FORWARD OF FRAME 5805. REPAIRED IAW FOKKE R SRM 51-10-04 AND SRM 53-40-01. 2 L 7 2 4F RT A20EU 1999050700079 19990507 00079 EU 1999 5 7 QXEA9900816 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS PITTING CORROSION BETWEEN FRAMES 13815A AND 13815B. REPAIRED IAW FOKKER SRM 51-1 0-04 AND SRM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700080 19990507 00080 EU 1999 5 7 QXEA9900817 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS AN AREA OF CORROSION 3 INCHES AFT OF FRAME 13815. REPAIRED IAW FOKKER SRM 51-10- 4 AND SRM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700081 19990507 00081 EU 1999 5 7 QXEA9900818 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS AN AREA OF CORROSION 8 INCHES AFT OF FRAME 13345. REPAIRED IAW FOKKER SRM 51-10- 4. 2 L 7 2 4F RT A20EU 1999050700082 19990507 00082 EU 1999 5 7 QXEA9900819 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12875 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS SMALL GOUGES 5 INCHES FORWARD OF FRAME 12875. REPAIRED IAW FOKKER SRM 51-10-4 PA GE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700083 19990507 00083 EU 1999 5 7 QXEA9900820 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11703 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE BETWEEN FRAME 11703 AND 13345. REPAIRED IAW FOKKER SRM 53 -40-01 PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700084 19990507 00084 EU 1999 5 7 QXEA9900821 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS LIGHT CORROSION INSIDE TRACK BETWEEN FRAMES 10966 AND 11405. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201-202, STEPS 2-6. 2 L 7 2 4F RT A20EU 1999050700085 19990507 00085 EU 1999 5 7 QXEA9900822 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305-9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION AND WEAR INSIDE TRACK BETWEEN FRAMES 9305C AND 9805. REPAIRED IAW FOKK ER SRM 53-40-1, PAGE 201, PARAGRAPH 4(B) AND SRM 51-10-04, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700086 19990507 00086 EU 1999 5 7 QXEA9900823 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK EXTENDING 6 INCHES FORWARD AND AFT OF FRAME 9305B. REPAIR ED IAW FOKKER SRM 51-10-04 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700087 19990507 00087 EU 1999 5 7 QXEA9900824 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS LIGHT CORROSION AND WEAR INSIDE TRACK BETWEEN FRAME 9305 AND 9305A. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700088 19990507 00088 EU 1999 5 7 QXEA9900825 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8805 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK THAT EXTENDS FROM 3 INCHES AFT TO 12 INCHES FORWARD OF FRAME 88 05. REPAIRED IAW FOKKER SRM 51-10-9 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700089 19990507 00089 EU 1999 5 7 QXEA9900826 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK THAT EXTENDS FROM FRAME 7805 TO 9 INCHES AFT OF FRAME 7805. RE PAIRED IAW FOKKER SRM 51-10-4 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700090 19990507 00090 EU 1999 5 7 QXEA9900827 1 19990312 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK FROM FRAME 6805 TO 7305. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700091 19990507 00091 EU 1999 5 7 QXEA9900828 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION INSIDE TRACK 3 INCHES FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 5 1-10-4 PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700092 19990507 00092 EU 1999 5 7 QXEA9900829 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT-HAND INBOARD SEAT TRACK HAS WEAR INSIDE TRACK BETWEEN FRAMES 5805 AND 6305. REPAIRED IAW FOKKER SRM 53-40-01 , PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700093 19990507 00093 WP 1999 5 7 ABXA9900323 1 19990428 A 3260 0080004003 PROX BOX DOUG DC9 DC941 302207N WP E & E COMP DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 955AX 2193 47619 AFTER TAKEOFF, RIGHT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR, NO CHANGE. REPLACED PROXIMITY SWITCH CONTROL BOX. 2 L 7 2 4F A6WE 1999050700094 19990507 00094 WP 1999 5 7 ABXA9900324 1 19990427 A 5610 5613217508 WINDOW DOUG DC9 DC933F 302207A WP RT COCKPIT BINDING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED FIRST OFFICER'S CLEARVIEW WINDOW MECHANISM, O PERATED NORMAL IAW DC9 MM. 2 L 7 2 4F A6WE 1999050700095 19990507 00095 WP 1999 5 7 ABXA9900325 1 19990423 A 5250 AR25291GR41 LATCH DOUG DC9 DC932 3022066 WP COCKPIT DOOR LOOSE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 903AX 47427 COCKPIT DOOR INITIALLY JAMMED IN THE CLOSED AND LOCKED POSITION. AFTER DOOR WAS OPENED, THE LOCK MECHANISM WOULD NOT LA TCH IN THE CLOSED POSITION. TIGHTENED SCREWS ON LATCH MECHANISM AND LUBRICATED MECHANISM. 2 L 7 2 4F A6WE 1999050700096 19990507 00096 WP 1999 5 7 MWEA99237 1 19990428 A 5330 59114004 SKIN DOUG DC9 DC932 3022066 WP BS 83 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 DENT IN FUSELAGE SKIN AT STATION 83 FORWARD OF RAT PROBE. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999050700097 19990507 00097 WP 1999 5 7 MWEA99239 1 19990428 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP PASSENGER DOOR DISCONNECTED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE FORWARD ENTRANCE DOOR GIRT BAR DISCONNECTED FROM SLIDE. MTC REINSTALLED LANYARD TO GIRT BAR. 2 L 7 2 4F A6WE 1999050700098 19990507 00098 WP 1999 5 7 MWEA99240 1 19990428 A 2560 11331 SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 212ME 47701 THE FORWARD ENTRANCE DOOR SLIDE PACK IS LOOSE. MTC REINSTALLED LANYARD TO FORWARD ENTRANCE DOOR SLIDE. 2 L 7 2 4F A6WE 1999050700099 19990507 00099 WP 1999 5 7 TWAA9906201 1 19990409 A 5320 SPLICE DOUG DC9 DC915 3022036 WP BS 370 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 DURING CHECK-C MAINT, FOUND LONGERON 28L SPLICE AT STA 370, CRACKED AND CORRODED. CRACK .75 IN LONG. INSTALLED REPAIR PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1999050700100 19990507 00100 SO 1999 5 7 LR7A9924 1 19990428 A 5320 3431947 STRUT LKHEED 382 382G 526414U SO BS 858 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 ON ARRIVAL ANC, FOUND FS 858 STRUT CRACKED AT UPPER GUSSET ATTACH, WL 256, RBL 61. REPLACED STRUT IAW SMP 583 51-10, PG 4. 2 H 7 4 4T A1SO 1999050700101 19990507 00101 SO 1999 5 7 LR7A9925 1 19990428 A 5320 342718R GUSSET LKHEED 382 382G 526414U SO BS 858 BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING ACCESS FOR FS 858 STRUT REPLACEMENT, FOUND FS 858 UPPER GUSSET BROKEN AT UPPER STRUT ATTACH BOLT HOLE, WL 256, RB L 61. REPLACED GUSSET IAW SMP 583 51-10, PG 4. 2 H 7 4 4T A1SO 1999050700102 19990507 00102 WP 1999 5 7 CALA9900452 1 19990429 A 2560 4953611501 ESCAPE LINE DOUG DC9 DC982 3022082 WP LT EMER EXIT FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 LEFT OVERWING EMERGENCY EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00. 2 L 7 2 4F A6WE 1999050700103 19990507 00103 WP 1999 5 7 CALA9900453 1 19990429 A 2560 4953611501 ESCAPE LINE DOUG DC9 DC982 3022082 WP RT EMER EXIT FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 RIGHT OVERWING EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00. 2 L 7 2 4F A6WE 1999050700104 19990507 00104 NE 1999 5 7 CALA9900454 2 19990426 A 7310 MANIFOLD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE CRACKED A CALA K NONE O OTHER TO TAKEOFF 1 SW 09 14814 49112 JT8D217A NUMBER 2 FUEL FLOW INDICATES HIGHER THAN NUMBER 1 ON TAKEOFF. AT CLIMB POWER NUMBER 2 FUEL FLOW IS 1000 POUNDS HIGHER A ND AT CRUISE 500 POUNDS HIGHER. FUEL USED AND FUEL REMAINING VERIFY THE HIGHER FUEL FLOW. FOUND CRACKED FUEL MAINFOLD. REMOVED AND REPLACED ENGINE PER CITEXT WORK CARD 08-7100-1-9900 AND TRIMMED PER CITEXT WORK CARD 08-7100-1-8900. 2 L 7 2 4F 4 F A6WE E9NE 1999050700105 19990507 00105 WP 1999 5 7 9901619860 1 19990422 A 2780 GUIDE DOUG DC9 DC951 3022051 WP RT LE FLAP LACK OF LUBE A NWAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 GL 01 769NC 47757 SLAT DISAGREEMENT OCCURRED ON LANDING INTO ALB. FLIGHT CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AND AIRCRAFT LANDE D WITHOUT INCIDENT USING FLAPS ONLY. MAINTENANCE LUBRICATED THE LEFT AND RIGHT ANTI-ICE TELESCOPING DUCTS IN ALB. OPER ATIONAL CHECK NORMAL. REPLACED THE RIGHT T DUCT LOWER GUIDE IN MSP AND ADJUSTED SAME. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999050700106 19990507 00106 NM 1999 5 7 9901626641 1 19990425 A 2910 AV16E12154 VALVE BOEING 747 747212B 1384886 NM NR 4 HYD SYST LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 641NW 21941 DURING CLIMB, THE NR 4 HYDRAULIC SYSTEM LOW QUANTITY LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INC IDENT. REPLACED THE NR 4 HYDRAULIC SHUTOFF VALVE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999050700107 19990507 00107 NM 1999 5 7 UPS99229465 1 19990401 A 3350 9621019 BATTERY PACK BOEING 727 72725C 138400H NM PASSENGER DOOR DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 EMERGENCY EXIT MARKER LIGHT ASSY ABOVE FWD ENTRY DOOR FAILED TEST PER TASK CARD 7-1 STEP 1B (1) E. STEADY GREEN LIGHT F AILED TO ILLUMINATE. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD IAW T/C 7-1 STEP 1B (1)E P/N ON/OFF 96-2-1019. 2 L 7 3 4F A3WE 1999050700108 19990507 00108 WP 1999 5 7 UPS99829464 1 19990401 A 2420 WIRE DOUG DC8 DC871F 302199D WP NR 3 GENERATOR CHAFED A IPXA O OTHER B H J SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 700UP 45900 NR 3 UNPARELLED LIGHT CAME ON AFTER LANDING. TOTAL ELECTRICAL FAILURE APPROX 1-2 MIN. THEN DETECTED SMOKE IN COCKPIT, EVACUATED A/C. REF L/P 183785 ITEM 2. FOUND WIRE W103-T1-5X2 (WDM 24-20-03) INSIDE NR 3 GEN CURRENT X-FORMER CHAFFING WITH COVER MOUNTING SCREW EXPOSING STRAND OF WIRE. ALSO, FOUND TERMINAL LUG OF ABOVE WIRE HAS NO CLEARENCE WITH FWD LOW ER NUT. REPAIRED CHAFED AREA OF WIRE REMOUNTED CLIP NUT 180 FOR CLEARENCE. ACFT POWER SYSTEMS, OPS CK OK. 2 L 7 4 4F RT 4A25 1999050700109 19990507 00109 EU 1999 5 7 QXEA9900830 1 19990313 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT WING FUEL PANEL 73G HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5. 2 L 7 2 4F RT A20EU 1999050700110 19990507 00110 EU 1999 5 7 QXEA9900831 1 19990405 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT WING FUEL PANEL 73D HAS SURFACE CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 28-11-06, PAGE 404, PAR AGRAPH 3A, STEPS 1-10. 2 L 7 2 4F RT A20EU 1999050700111 19990507 00111 EU 1999 5 7 QXEA9900832 1 19990405 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT WING FUEL PANEL 71A HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 28-11-06, PAGE 404, PARAGRAPH 3 A, STEPS 1-10. 2 L 7 2 4F RT A20EU 1999050700112 19990507 00112 EU 1999 5 7 QXEA9900833 1 19990318 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WS 2230 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT WING FUEL PANEL 71A AT STATION 2230 HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW 51-10-4, PAGE 9, PARAGRAP H 4B. 2 L 7 2 4F RT A20EU 1999050700113 19990507 00113 EU 1999 5 7 QXEA9900834 1 19990318 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT WING FUEL ACCESS APERTURE 73B HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARA GRAPH 4B. 2 L 7 2 4F RT A20EU 1999050700114 19990507 00114 EU 1999 5 7 QXEA9900835 1 19990405 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFTWING FUEL ACCESS PANEL 73A HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 28-11-06, PAGE 404, PARAG RAPH 3A, STEPS 1-10. 2 L 7 2 4F RT A20EU 1999050700115 19990507 00115 EU 1999 5 7 QXEA9900836 1 19990318 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT WING FUEL PANEL 73A APERTURE HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAG RAPH 4B. 2 L 7 2 4F RT A20EU 1999050700116 19990507 00116 EU 1999 5 7 QXEA9900837 1 19990405 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LEFT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT WING FUEL ACCESS PANEL 73C HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRA PH 4. 2 L 7 2 4F RT A20EU 1999050700117 19990507 00117 EU 1999 5 7 QXEA9900838 1 19990331 A 5520 BRACKET FOKKER F28 F28MK4000 4990810 EU ELEVATOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - 3 HOLES IN ATTACHMENT BRACKET FOR THE ELEVATOR BOOSTER UNIT ARE WORN SO THAT THE BUSHINGS ARE LOOSE. REPAIRED IAW HORIZON AIR EA 4-55-126. 2 L 7 2 4F RT A20EU 1999050700118 19990507 00118 EU 1999 5 7 QXEA9900839 1 19990323 A 5521 RIB FOKKER F28 F28MK4000 4990810 EU ELEVATOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FALSE RIB ASSEMBLY FOR LEADING EDGE 51E HAS .5 CRACK UNDER CORNER OF FLANGE. REPAIRED IAW HORIZON AIR EA 4-55-121 . 2 L 7 2 4F RT A20EU 1999050700119 19990507 00119 EU 1999 5 7 QXEA9900840 1 19990322 A 5520 HOUSING FOKKER F28 F28MK4000 4990810 EU ELEVATOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - ELEVATOR GUSTLOCK HOUSING HAS POSSIBLE CRACK AT ATTACH LEGS. REPAIRED SB F28-27-182. 2 L 7 2 4F RT A20EU 1999050700120 19990507 00120 EU 1999 5 7 QXEA9900841 1 19990405 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - THERE IS A CRACK AT THE LOWER, AFT EDGE, OF RIB NR 4, ON THE HORIZONTAL STAB LEADING EDGE PANEL NR 51E. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-55-130. 2 L 7 2 4F RT A20EU 1999050700121 19990507 00121 EU 1999 5 7 QXEA9900842 1 19990331 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU LT HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - THERE IS A CRACK IN THE TOP, FORWARD EDGE OF THE LEFT, HORIZONTAL STAB, INBOARD MOST RIB AT STATION 215. REPAIRED IAW HORIZON AIR EA 4-57-250. 2 L 7 2 4F RT A20EU 1999050700122 19990507 00122 EU 1999 5 7 QXEA9900843 1 19990331 A 5511 RIB FOKKER F28 F28MK4000 4990810 EU LT HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - THERE IS A CRACK IN THE LOWER, FORWARD EDGE OF THE LEFT HORIZONTAL STAB, INBOARD MOST RIB AT STATION 215. REPAIRE D IAW HORIZON AIR EA 4-57-250. 2 L 7 2 4F RT A20EU 1999050700123 19990507 00123 EU 1999 5 7 QXEA9900844 1 19990401 A 5511 SKIN FOKKER F28 F28MK4000 4990810 EU HORIZ STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - INTERNAL SKIN OF HORIZONTAL STAB LEADING EDGE PANEL 51C IS PEELING BACK AT RIB 1 AND BETWEEN RIBS 3 AND 4. REPAIR ED IAW HORIZON AIR EA 4-55-124. 2 L 7 2 4F RT A20EU 1999050700124 19990507 00124 EU 1999 5 7 QXEA9900845 1 19990321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME CLIP REPAIR IS CRACKED ON FRAME 50-2 BETWEEN STRINGER 24 AND 25. REPAIRED IAW FOKKER SRM 53-10-5, PARAGRAPH 2B, STEP 1 AND 2, PAGE 601 AND SRM 53-10-5. 2 L 7 2 4F RT A20EU 1999050700125 19990507 00125 EU 1999 5 7 QXEA9900846 1 19990321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME CLIP CRACKED ON FRAME 32-2 BETWEEN STRINGERS 29 AND 31. REPAIRED IAW FOKKER SRM 53-10-5, PAGE 601, PARAGRAP H 2B, STEP 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700126 19990507 00126 EU 1999 5 7 QXEA9900847 1 19990321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FRAME CLIP REPAIR CRACKED ON FRAME 50-2 BETWEEN STRINGERS 46 AND 48. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PA RAGRAPH 2B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700127 19990507 00127 EU 1999 5 7 QXEA9900848 1 19990321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FUSELAGE TAIL SECTION AT FRAME 50-2 BETWEEN STRINGERS 23 AND 24 CLIP IS CRACKED. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PARAGRAPH 2B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700128 19990507 00128 EU 1999 5 7 QXEA9900849 1 19990323 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FUSELAGE TAIL SECTION FRAME 50-2 AT STRINGER 44 IS CRACKED. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PARAGRAPH 2 B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700129 19990507 00129 EU 1999 5 7 QXEA9900850 1 19990323 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - FUSELAGE TAIL SECTION FRAME 50-2 AT STRINGER 48 IS CRACKED. REPAIRED IAW FOKKER MM 53-10-5, PAGE 601, PARAGRAPH 2 B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999050700130 19990507 00130 NM 1999 5 7 QXEA9900940 1 19990428 A 2611 SMOKE WARNING DHAV DHC8 DHC8202 2809007 NM COCKPIT ACTIVATED A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 369PH 520 SEA- EN ROUTE, THE SMOKE WARNING WENT OFF FOR APPROXIMATELY 15 SECONDS THEN WENT OUT. MAINTENANCE PERFORMED A OPERATION AL CHECK OF THE DETECTORS WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999050700131 19990507 00131 NE 1999 5 7 DL72S990832 2 19990413 A 7261 OIL FILTER BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE CONTAMINATED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 499DA 54253 21143 700444 NR 3 OIL FILTER BYPASS LIGHT CAME ON AT 17K FT. OIL PRESS TEMP AND QTY ARE GOOD POM PROCEDURES COMPLIED WITH. LIGHT RE MAINED ON AND NR 3 ENGINE WAS SHUT DOWN IAW POM PROCEDURES. REMOVED FILTER, FOUND CARBON BUILDUP. INSTALLED NEW FILTER AND RAN ENG PER MM. REMOVED NEW FILTER AND FOUND MORE CONTAMINATION, CARBON CONTAMINATION IS WITHIN MM. LIMITS FOR 50 HOUR FLY BACK. INSTALLED NEW OIL FILTER. GOOD FOR SERVICE. MCC AND EQUIPMENT CONTROL WERE NOTIFIED. 2 L 7 3 4F 4 F A3WE E2EA 1999050700132 19990507 00132 WP 1999 5 7 DLL10990844 1 19990416 A 2560 DPN257212647 SMOKE GOGGLES LKHEED 1011 10113851 5265010 WP COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 FAA - SMOKE GOGGLES AT THREE LOCATIONS FOUND WITH CRACKS. LENS CRACKED FROM NOSE BRIDGE TO TOP. LENS CRACKED FROM NOSE BRIDGE UP FOR 1 INCH. LENS CRACKED FROM NOSE BRIDGE UP FOR 1 INCH. ALL THREE GOGGLES WERE PROPERLY STOWED AND IN THER E PROPER CLOTH POUCH. NOTED THAT GOGGLES WITH DAMAGE WERE LOCATED IN COMPARTMENT BEHIND FLIGHT CREW SEATS AND/OR ABOVE THE SECOND OBSERVERS SEAT. REPLACED GOGGLES. 2 L 7 3 4F A23WE 1999050700133 19990507 00133 NM 1999 5 7 DL73E990846 1 19990416 A 3350 CONNECTOR 62A1223 BOEING 737 7372S3 NM CABIN LOOSE A DALA K NONE L NO TEST LD LANDING 1 SO 27 367DL 21774 EMERGENCY EXIT LIGHTS ALONG AISLE AND LOWER DOORS COME ON AND GO OFF ON THEIR OWN. FOUND WIRE LOOSE ON AFT FLT ATTENDAN T PANEL EMERGENCY SWITCH. TIGHTENED CONNECTOR ON SWITCH. LIGHTS OPS CHK NML. 2 L 7 2 4F RT A16WE 1999050700134 19990507 00134 NM 1999 5 7 DL72L990871 1 19990422 A 3350 LIGHT 900542 BOEING 727 727232 1384082 NM CARGO INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 501DA 24510 21303 C2 DOOR EMERGENCY SLIDE LIGHT INOP. 2 L 7 3 4F A3WE 1999050700135 19990507 00135 NE 1999 5 7 DL72E990874 2 19990422 A 7261 OIL SCREEN BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 27 283WA 77766 21485 657390 NR 3 ENG OIL ZERO, SHUT DOWN ENG. FOUND MAIN OIL SCREEN LEAKING. REPLACED MAIN OIL SCREEN AND O-RING SEAL PER MM 71-00 PG 212L AND 212M. NO LEAKS ON ENG RUN. 2 L 7 3 4F 4 F A3WE E2EA 1999050700136 19990507 00136 NM 1999 5 7 DL76L990876 1 19990422 A 2520 WIRE BOEING 767 767332 1382001 NM ROW 4E SHORTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 172DN 24775 SEAT 4E SPARKS ACCOMPANIED BY BURNING SMELL WHEN OPERATED ELECTRICALLY. REPAIRED WIRING HARNESS. REROUTED AND SECURE D SAME, CKS OK. 2 L 7 2 4F RT A1NM 1999050700137 19990507 00137 NM 1999 5 7 DL72S990897 1 19990424 A 5330 655456414 SKIN BOEING 727 727232 1384082 NM BS 560-580 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FUSELAGE SKIN FS 560-580, STRG 28L, SKIN CORROSION REPAIR. AN AREA OF CORROSION WAS FOUND IN THE FUSELAGE SKIN NEAR STR INGER 28L BETWEEN FS 559 AND 564. THE CORROSION WAS CUTOUT WITH A 7 BY 1.85 CUTOUT. THERE WAS AN EXISTING REPAIR D OUBLER ADJACENT TO THIS LOCATION FOR THE REPAIR OF TWO SMALLER SKIN CUTOUTS. THE EXISTING REPAIR DOUBLER WAS REMOVED AN D A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED TO REPAIR ALL CUTOUTS PER ER/A 367221-14, REV B. 2 L 7 3 4F A3WE 1999050700138 19990507 00138 NM 1999 5 7 DL72S990898 1 19990424 A 5311 65561322 FRAME BOEING 727 727232 1384082 NM BS 1142 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FUSELAGE C3 DOOR CUTOUT AFT FRAME FS 1142 STRINGER 28R:CORROSION REPAIR. THE SKIN ATTACH FLANGE OF THE AFT FRAME OF THE C3 DOOR CUTOUT WAS FOUND CORRODED AT STRINGER 28R. THE CORRODED FLANGE WAS TRIMMED AWAY AND REPAIRED WITH AN ALUM INUM REPAIR ANGLE PER ER/A 367222-14, REV A. 2 L 7 3 4F A3WE 1999050700139 19990507 00139 NM 1999 5 7 DL72S990899 1 19990424 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1050 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FUSELAGE SKIN FS 1010-1080 STRG 26L-26R, CORROSION REPAIR. THE FUSEALAGE SKIN WAS FOUND CORRODED BETWEEN FS 1046 AND 10 55 BELOW STRINGER 27. THERE WERE SEVERAL OTHER SKIN PANEL. REPAIR DOUBLERS IN THE AREA. TO ELIMINATE THE DAMAGE AND E XISTING REPAIRS, THE SKIN WAS CUT AT FS 1080 BETWEEN STRINGER 16R AND 26L AND THE SECTION REMOVED TO FS 1010. A NEW SKI N SECTION WAS SPLICED IN PLACE PER ER/A 367217-14. 2 L 7 3 4F A3WE 1999050700140 19990507 00140 NM 1999 5 7 DL72W990901 1 19990424 A 5330 65545703 SKIN BOEING 727 727247 138408F NM BS 440-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 FUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION OF THE E NTIRE PANEL CONFIRMED A SINGLE CRACK BETWEEN FS 440 AND 460. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367251-14. 2 L 7 3 4F A3WE 1999050700141 19990507 00141 NM 1999 5 7 DL72S990902 1 19990424 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 440-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CO NFIRMED A SINGLE CRACK BETWEEN FS 440 AND 460. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DO CUMENTED PER ER/A 367248-14AD. 2 L 7 3 4F A3WE 1999050700142 19990507 00142 NM 1999 5 7 DL72S990903 1 19990424 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FUSELAGE SKIN FS 481-681 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN TWO ADJACENT FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 367247-14AD. 2 L 7 3 4F A3WE 1999050700143 19990507 00143 NM 1999 5 7 DL72S990904 1 19990424 A 5711 65192923 SPAR WEB BOEING 727 727232 1384082 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 WING CENTER SECTION, REAR SPAR WEB, RBL 13. CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A 1.5 INCH LONG TYPICAL CRACK AT RBL 13, JUST BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE SPAR WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 367243-14AD. 2 L 7 3 4F A3WE 1999050700144 19990507 00144 NM 1999 5 7 DL72L990905 1 19990424 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 FUSELAGE SKIN FS 481-681, STRINGER 26L SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLI CE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIR MED MULTIPLE CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINU M DOUBLER PER ER/A 367232-14AD, REV A. 2 L 7 3 4F A3WE 1999050700145 19990507 00145 NM 1999 5 7 DL72W990906 1 19990424 A 5330 655457416 SKIN BOEING 727 727247 138408F NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 FUSELAGE SKIN FS 481-681,STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRME D 13 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMIN UM DOUBLER PER ER/A 367249-14AD. 2 L 7 3 4F A3WE 1999050700146 19990507 00146 NM 1999 5 7 DL72W990907 1 19990425 A 5330 65545672 SKIN BOEING 727 727247 138408F NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 FUSELAGE CK REPAIR, LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LO WER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SK IN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367250-14AD. 2 L 7 3 4F A3WE 1999050700147 19990507 00147 NM 1999 5 7 DL72L990908 1 19990422 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 520-540 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 FUSELAGE SKIN FS 520-540, STRINGER 26L SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLI CE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFI RMED A SINGLE CRACK BETWEEN FS 520 AND 540. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367229-14AD. 2 L 7 3 4F A3WE 1999050700148 19990507 00148 NM 1999 5 7 DL73K990909 1 19990423 A 5330 SKIN BOEING 737 737232 1384475 NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 314DA 23086 FUSELAGE AFT GALLEY DOOR CUTOUT SKIN UPPER HINGE CUTOUT, CRACK REPAIR. THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR CU TOUT SKIN WAS FOUND WITH A .25 LONG TYPICAL CRACK AT THE UPPER CORNER. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DO UBLER PER ER/A 367237-14, REV A AND BASED ON A REPAIR PER B737 SRM 53-30-3, FIG 21A. 2 L 7 2 4F RT A16WE 1999050700149 19990507 00149 NM 1999 5 7 DL72S990910 1 19990423 A 5330 SKIN BOEING 727 727232 1384082 NM BS 960 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FUSELAGE SKIN FS 950F-970, STRINGER 28L, CORROSION CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND CORRODED AT STRINGER 28L BETWEEN FS 950F AND FS 970. THE CORROSION WAS REMOVED WITH A 26 BY 3 CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITHA N EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 367230-14. 2 L 7 3 4F A3WE 1999050700150 19990507 00150 NM 1999 5 7 DL72S990911 1 19990426 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 FOUND AT C-2 LETTER CK, LEFT AFT ENTRY WAY DOOR FRAME HAS .375 IN VISIBLE CRACK AT UPPER CUTOUT. REPAIRED PER SRM 53-10 -9. 2 L 7 3 4F A3WE 1999050700151 19990507 00151 NM 1999 5 7 DL72S990912 1 19990426 A 5320 WEB BOEING 727 727232 1384082 NM BS 1289 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 FOUND ON C2 LETTER CK, RT VERTICAL TORQUE BOX WEB CRACKED .375 INCH AT STA 1289. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999050700152 19990507 00152 NE 1999 5 7 DL73E990913 2 19990426 A 7200 ENGINE BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 378DL 28302 23605 717158 NR 1 OIL TEMP UNCONTROLLABLE DID NOT EXCEED RED BAND BEFORE ENG WAS SHUTDOWN. MAINTENANCE IN PROGRESS A/C PREPARED FOR FERRY FLT TO ATL. REPLACED ENGINE. 2 L 7 2 4F 4 F A16WE E2EA 1999050700153 19990507 00153 WP 1999 5 7 DLL19990914 1 19990426 A 3340 8906K1665 SWITCH LKHEED 1011 10113853 5265020 WP RT LANDING LIGHT BROKEN A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 754DL 193Y1181 ELECTRICAL SMOKE ODOR IN COCKPIT ISOLATED A/C AND D/C POWER. NO EXCESSIVE LOADS ON ANY BUSS. FOUND RT WING LANDING LIG HT SWITCH BROKEN. REPLACED SWITCH. 2 L 7 3 4F A23WE 1999050700154 19990507 00154 NM 1999 5 7 DL72L990915 1 19990427 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FUSELAGE SKIN FS 680-740 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367266-14AD. 2 L 7 3 4F A3WE 1999050700155 19990507 00155 NM 1999 5 7 DL72L990916 1 19990427 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FUSELAGE SKIN FS 360-480 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CON FIRMED 5 CRACKS IN THREE DIFFERENT FRAME BAYS. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367264-14AD. 2 L 7 3 4F A3WE 1999050700156 19990507 00156 NM 1999 5 7 DL72L990917 1 19990427 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FUSELAGE SKIN FS 360-481 STRINGER 4L, SKIN LAP SPLICE, CRACK REPAIR. INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED 6 CRACKS IN THREE CONSECUTIVE FRA ME BAYS. THE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367262-14AD. 2 L 7 3 4F A3WE 1999050700157 19990507 00157 NM 1999 5 7 DL72W990918 1 19990319 A 5753 652163234 SPAR BOEING 727 727247 138408F NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 TEMP SPLICE AFT SPAR AT 57 AND 46 FROM I/B END OF FLAP. THIS DAMAGE WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011 626, LISTED ON SHOP ORDER 709228. 2 L 7 3 4F A3WE 1999050700158 19990507 00158 NM 1999 5 7 DL72W990919 1 19990319 A 5753 652163234 SPAR BOEING 727 727247 138408F NM RT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 AFT SPAR CRACKED 22 FROM I/B END OF FLAP, THIS DAMAGED WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011630 LOCATED SH OP ORDER 709228. 2 L 7 3 4F A3WE 1999050700159 19990507 00159 NM 1999 5 7 DL72L990921 1 19990427 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FUSELAGE SKIN FS 481-681, STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRME D 52 CRACKS ALONG THE PANEL. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367 261 -14AD. 2 L 7 3 4F A3WE 1999050700160 19990507 00160 NM 1999 5 7 DL72W990922 1 19990426 A 5330 655457416 SKIN BOEING 727 727247 138408F NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 FUSELAGE SKIN FS 481-681, STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLIC E BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRM ED 20 CRACKS. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367259-14AD. 2 L 7 3 4F A3WE 1999050700161 19990507 00161 NM 1999 5 7 DL72W990923 1 19990427 A 5330 65545703 SKIN BOEING 727 727247 138408F NM BS 360-380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 FUSELAGE SKIN FS 360-380 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRME D A SINGLE CRACK BETWEEN FS 360 AND 380. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENT ED PER ER/A 367260-14AD. 2 L 7 3 4F A3WE 1999050700162 19990507 00162 NM 1999 5 7 DL733990924 1 19990426 A 5343 654654325 FITTING BOEING 737 73735B NM BS 685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 225DL 25069 FUSELAGE LT MLG SIDE STRUT SUPPORT FITTING FS 685, CORRODED LUG REPAIR. THE FS 685 LEFT MLG SIDE STRUT SUPPORT FITTING WAS FOUND WITH CORROSION IN THE LUG BORE. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLE. AN OVERSIZE BUSHING WAS IN STALLED PER ER/A 367246-14, REV A. 2 L 7 2 4F RT A16WE 1999050700163 19990507 00163 NM 1999 5 7 DL73K990925 1 19990426 A 3244 B737M TIRE BOEING 737 737232 1384475 NM NR 2 WHEEL FAILED A DALA K NONE K FLUID LOSS LD LANDING 1 SO 27 329DL 23101 A/C BLEW NR 2 TIRE ON T/O FROM EWR. UPON LANDING IN MCO, LOST ALL 'A' SYSTEM HYDS AND HAD TO BE TOWED IN AFTER TIRE REP LACEMENT. REPLACED NR 1 AND 2 TIRES AND BRAKES, AFT FLAP, ANTI-SKID WIRING HARNESS, AND ASSOCIATED HARDWARE. 2 L 7 2 4F RT A16WE 1999050700164 19990507 00164 NM 1999 5 7 DL72S990926 1 19990427 A 3040 2312 CONTROLLER BOEING 727 727232 1384082 NM L-1 WINDOW FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 545DA 22494 NOTIFIED OF SMELL IN THE CABIN, PERFORMED EMERGENCY DESCENT. AFTER LANDING, FOUND L-1 AC CONTROL CIRCUIT BREAKER POPPED IN WINDOW HEAT SECTION. ALSO, FOUND WINDOW HEAT NR 1L CIRCUIT BREAKER POPPED ON LOWER P-6 PANEL. AIRCRAFT DIVERTED TO YKM. MAINTENANCE FOUND L-1 WINDOW CONTROLLER FAILED. REPLACED L-1 CONTROLLER, FUNCTIONAL TEST SYSTEM. ALL CKS NML. 2 L 7 3 4F A3WE 1999050700165 19990507 00165 NM 1999 5 7 DL72S990927 1 19990427 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 8 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 NR 8 SLAT ACTUATOR I/B ATTACH BRACKET IS CRACKED. REPAIRED PER M/M 57-20-21 PG 812. 2 L 7 3 4F A3WE 1999050700166 19990507 00166 NM 1999 5 7 DL73K990928 1 19990427 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 324DL 23096 ON TEST, EMERGENCY LIGHT PACK M1137 NOT ILLUMINATING RESPECTIVE LIGHTS. REPLACE BATTERY PACK. 2 L 7 2 4F RT A16WE 1999050700167 19990507 00167 NM 1999 5 7 DL76S990929 1 19990427 A 2560 BOTTLE 130104233 BOEING 767 767332 1382001 NM RT EMER EXIT LOW PRESSURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 133DN 3389 24982 RIGHT OVERWING SLIDE BOTTLE PRESSURE LOW ALMOST EMPTY. 2 L 7 2 4F RT A1NM 1999050700168 19990507 00168 NM 1999 5 7 DL72S990933 1 19990428 A 7331 POWER SUPPLY 8TJ95GAB3 BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE FUEL FLOW SYST MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 534DA X0059 22047 WHEN TAKEOFF POWER WAS APPLIED FUEL FLOW INDICATORS, INCREASED IN UNISION AND THEN FLUCTUATED IN UNISION BETWEEN BETWEEN 1000-5000 PPH. WITH T/O EPR ESTABLISHED ALL 3 FUEL FLOW GAUGES INDICATED 1000 PPH STEADY. ALL OTHER ENGINE INDICATION S NORMAL. TAKEOFF ABORTED AT LESS THAN 65 KNOTS. REPLACED FUEL FLOW POWER SUPPLY. CKD OK ON ENG RUN. 2 L 7 3 4F 4 F A3WE E2EA 1999050700169 19990507 00169 NM 1999 5 7 DL72E990934 1 19990428 A 5753 BUSHING BOEING 727 727247 138408F NM TE FLAPS LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 NR 4 FLAPTRACK FWD MOUNT PORKCHOP FITTING BUSHING LOOSE. REMOVED FITTING, BUSHING REMOVED. CORROSION FOUND, REWORKED O N N/R 642. 2 L 7 3 4F A3WE 1999050700170 19990507 00170 NM 1999 5 7 DL76S990935 1 19990428 A 2120 AIR DISTRIBUTION BOEING 767 767332 1382001 NM GALLEY ODOR A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 126DL 24076 AT TOP OF DESCENT INTO ATL, WE HAD A REPORT OF ELECTRICAL FUMES AT THE 2R DOOR (NEAR AFT GALLEY). WE PULLED ALL BREAKER S IN GALLEY, SHUTOFF LIGHTS AND CKED AFT RIGHT LAV. WHILE LATE INTO DESCENT, THE SMELL OF ELECT FUMES WAS DISSIPATING. ALL PROCEDURES WERE EXECTUTED IAW THE POM FROM THE C/PIT. TURNED ON ALL POWER TO GALLEY AND LAV INCLUDING LIGHTS, CHEC KED ABOVE CEILING AND BELOW FLOOR. NO FUMES PRESENT AND NO PROBLEMS FOUND. 2 L 7 2 4F RT A1NM 1999050700171 19990507 00171 NM 1999 5 7 SCNA99700 1 19990414 A 5347 SEAT TRACK BOEING 727 727282 138408T NM BS 400 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING A HEAVY LINE MAINTENANCE CHECK, THE RIGHT HAND OUTBOARD SEAT TRACK AT STA 400 RBL 44 WAS CORRODED OUT OF LIMITS. REMOVED CORROSION FROM SEAT TRACK IAW B727 SRM 531001. FABRICATED NEW SEAT TRACK FROM BAC1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED PER SRM 531005. 2 L 7 3 4F RT A3WE 1999050700172 19990507 00172 NM 1999 5 7 SCNA99701 1 19990422 A 5347 SEAT TRACK BOEING 727 727282 138408T NM BS 1090-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING A HEAVY LINE MAINTENANCE CHECK, THE SEAT TRACK AT STA 1090 TO 1130 WAS CORRODED OUT OF LIMITS IN VARIOUS PLACES. REMOVED CORROSION FROM SEAT TRACK IAW B727 SRM 531001. FABRICATED NEW SEAT TRACK FROM BAC1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED PER SRM 531005. 2 L 7 3 4F RT A3WE 1999050700173 19990507 00173 NM 1999 5 7 SCNA99702 1 19990414 A 5315 FLOORBEAM BOEING 727 727282 138408T NM BS 380 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING A HEAVY LINE MAINTENANCE CHECK, THE FLOORBEAM AT STA 380 RBL 24 THROUGH 30 WAS FOUND CORRODED OUT OF LIMITS. REM OVED CORROSION ON FLOORBEAM IAW B727 SRM 531001. CUT DAMAGED AREA OUT, FABRICATED REPAIR PARTS FROM 7075 T6 BAC 1490283 1, 14902785, 150051001617, 15123353, 15123396 IAW B727 SRM 531008. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002 . INSTALLED IAW SRM B727 531008 AND 513002. 2 L 7 3 4F RT A3WE 1999050700174 19990507 00174 NM 1999 5 7 SCNA99064 1 19990426 A 3350 BULB BOEING 727 7272J4 1384006 NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE FORWARD EMERGENCY PATH LIGHTING WAS FOUND TO BE INOPERATIVE. RELAMPED THE EMERGENC Y PATH LIGHTING IN THE FORWARD SECTION OF THE AIRCRAFT BY THE GALLEY. PATH LIGHTING OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999050700175 19990507 00175 NM 1999 5 7 SCNA99065 1 19990427 A 3397 WIRE BOEING 727 7272J4 1384006 NM ROW 30-32 FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT SEATS 30DEF TO 32DEF. REPAIRED WIRING IN FLOOR TRACK AT SEATS 30DEF AND RESECURED FLOOR TRACK. EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHEC KS GOOD. 2 L 7 3 4F RT A3WE 1999050700176 19990507 00176 SO 1999 5 7 SWIA971463 1 19990405 A 2910 HYD SYST EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT HYD SYST REQD SERVICE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 207SW 120266 SHORTLY AFTER TAKEOFF REACHING CRUISE ALTITUDE THE LEFT HYDRAULIC RESERVOIR LOW PRESSURE LIGHT CAME ON AND WAS ACCOMPANI ED BY A FLUID QUANTITY INDICATION IN MID GREEN ARC. WITHIN 5 MINUTES THE RIGHT LOW PRESS CAME ON. BOTH REMAINED TO 15, 000 FEET. INSPECTED BOTH HYDRAULIC GREEN AND BLUE. FOUND FLUID QUANTITY IN GREEN SERVICED IAW 12-13-01 AND PURGE IAW 2 9-12-00. BOTH OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999050700177 19990507 00177 1999 5 7 SWIA971464 4 19990406 A 3425 AHRS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT COCKPIT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 299SW 120329 CAPTAIN'S AHRS FAILED AFTER TAKEOFF, WOULD NOT RESET (GYRO FLAG AND RED HEADING). RETURNED TO ACV. PERFORMED REORIENTA TION OF AHRS (PILOTS). CHECKED OK. 2 L 7 2 4T 4 T RT A31SO E20NE 1999050700178 19990507 00178 1999 5 7 SWIA971465 4 19990409 A 3418 HEAT MESSAGE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT AOA ACTIVATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 405SW 7029 RIGHT AOA HEAT MESSAGE CAME ON AFTER TAKEOFF. RETURNED TO SLC. POWERED SYSTEM DOWN AND BACK UP. OPS CHECK GOOD. COUL DN'T DUPLICATE PROBLEM. 2 L 7 2 4F 4 F RT A21EA E15NE 1999050700179 19990507 00179 EA 1999 5 7 SWIA971466 1 19990401 A 3260 BRACKET CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 403SW 7028 NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. NOSE GEAR DOORS OPEN AND NOSE GEAR LIGHT REMAINED GREEN. FOUND BRACKET FOR NOSE GEAR TARGET WAS DAMAGED. REPLACED BRACKET AND SET GAP PER MM 32-64-05. OPS CHECK SHOWS ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 1999050700180 19990507 00180 SO 1999 5 7 SWIA971467 1 19990402 A 2120 PRESSURIZATION EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 215SW 120281 LOST CABIN PRESSURIZATION DURING CLIMB AT 7000 AGL. CABIN ALTITUDE AT 6500. RETURNED TO LAX. PRESSURIZED AIRCRAFT. A LL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999050700181 19990507 00181 NE 1999 5 7 SWIA971468 2 19990408 A 7261 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENG BREATHER FAILED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 297SW 120327 CREW REPORTS SMOKE FROM LEFT ENGINE EXHAUST AT TAKEOFF POWER. RETURNED TO SFO, REMOVED AND REPLACED LEFT ENGINE BREATHE R TUBE CARBON SEAL IAW MM 72-20-00. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999050700182 19990507 00182 SO 1999 5 7 SWIA971469 1 19990406 A 5230 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR FAILED A SWIA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 NM 07 291SW 120318 LOST ALL CABIN PRESSURIZATION, UNABLE TO MAINTAIN WITH AUTOMATIC OR MANUAL MODE. CABIN OXYGEN MASKS DEPLOYED. PERFORME D RAPID DESCENT. REPAIRED LOWER SECTION OF CARGO DOOR SEAL AND REPLACED LOWER CARGO DOOR SEAL RETAINING BRACKET. GROUN D CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999050700183 19990507 00183 1999 5 7 SWIA971470 4 19990406 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE STALL WARNING TRIPPED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 411SW 7067 STALL FAIL MESSAGE ILLUMINATED EN ROUTE. RETURNED TO SLC. RESET MEMORY ON STALL COMPUTER. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999050700293 19990507 00293 WP 1999 5 7 USAA990334 1 19990330 A 5320 CEILING DOUG DC9 DC931 3022065 WP BS 154/158 CRACKS A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND 2 CRACKS 1 INCH LONG ON CABIN FLOOR CEILING STATION 154 AND 158 OUTBOARD SIDE RIGHT. INST ALLED DOUBLER PER SRM 53-01 PAGE 9. (M) 2 L 7 2 4F A6WE 1999050700294 19990507 00294 WP 1999 5 7 USAA990318 1 19990401 A 5400 ANGLE DOUG DC9 DC931 3022065 WP LT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 976VJ 41828 48147 PIT - DURING C-6 CHECK, FOUND .5 INCH CRACK IN UPPER LEFT PYLON ATTACH ANGLE AT STATION 1019. STOP DRILLED CRACK. INST ALLED TYPICAL REPAIR 54-10-06A. (M) 2 L 7 2 4F A6WE 1999050700295 19990507 00295 WP 1999 5 7 USAA990317 1 19990401 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 976VJ 41828 48147 PIT - DURING C-6 CHECK, FOUND .375 INCH LONG CRACK AT NOSE SKIN PANEL 5911403-1 AT RIVET HOLE 10 INCH AFT OF CENTER PITO T. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 51841. (M) 2 L 7 2 4F A6WE 1999050700296 19990507 00296 WP 1999 5 7 USAA990316 1 19990401 A 5320 JAMB DOUG DC9 DC931 3022065 WP CARGO DOOR CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 976VJ 41828 48147 PIT - DURING C-6 CHECK, FOUND 2 INCH BY 2 INCH AREA OF CORROSION AFT CARGO DOOR JAMB AT FORWARD LOWER STOP. CORROSION L EVEL 1. REMOVED LOWER DOOR JAMB SECTION AND SPLICED IN A NEW SECTION PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 1999050700297 19990507 00297 WP 1999 5 7 USAA990332 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 6 INCH CORROSION AT FLOOR SUPPORT AT STATION 200 INBOARD OF SERVICE DOOR. CORRO SION LEVEL 1, CORROSION TASK NC C46-53303. FLOOR SUPPORT CUT FROM STOCK EXTRUSION 70 75-T6. (M) 2 L 7 2 4F A6WE 1999050700298 19990507 00298 WP 1999 5 7 USAA990331 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 160-200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 30 INCH CORROSION AT FLOOR SUPPORT AT STATION 160-200 JUST AFT EPC PANEL. CORRO SION LEVEL 1, CORROSION TASK NR C46053303. REPLACED WITH ANGLE IN STOCK. (M) 2 L 7 2 4F A6WE 1999050700299 19990507 00299 WP 1999 5 7 USAA990329 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 218-236 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 10 INCH CORROSION AT FLOOR SUPPORT AT STATION 218 TO 236 INBOARD OF LT OUTBOARD SEAT TRACK. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REPLACED WITH ANGLE IN STOCK. (M) 2 L 7 2 4F A6WE 1999050700300 19990507 00300 WP 1999 5 7 USAA990328 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 160 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND .5 INCH BY 4 INCH CORROSION AT FLOOR SUPPORT AT STATION 160 CENTER LINE TO FORWARD SERVIEC DOOR. CORROSION LEVEL 1, CORROSION TASK NRC46-53303. CLEANED CORROSION, ALODINED, PRIMED, MFG FLOOR SUPPORT NR 36 AND INSTALLED SUPPORT. (M) 2 L 7 2 4F A6WE 1999050700301 19990507 00301 WP 1999 5 7 USAA990327 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 18 INCH CORROSION AT FLOOR SUPPORT AT STATION 200 RIGHT SIDE CENTER LINE. CORRO SION LEVEL 1, CORROSION TASK NR C46-53303. CLEANED CORROSION, ALODINED, PRIMED, MFG NR 25 SUPPORT AND INSTALLED SUPPOR T. (M) 2 L 7 2 4F A6WE 1999050700302 19990507 00302 WP 1999 5 7 USAA990326 1 19990330 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 2 INCH CORROSION AT SEAT TRACK AT STATION 200 RIGHT INBOARD. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REMOVED AND SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 1999050700303 19990507 00303 WP 1999 5 7 USAA990325 1 19990330 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 270 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 3 INCH SECTION CORROSION WITH 1 INCH CRACK, LEVEL 1 SUSPECT LEVEL 2 AT RIGHT SIDE INBOARD TRACK STATION 270. CORROSION LEVEL 1. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 1999050700304 19990507 00304 WP 1999 5 7 USAA990324 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 160-200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 15 INCH CORROSION ON FLOOR SUPPORT AT STATION 160 TO 200 FORWARD OF RIGHT OUTBOA RD SEAT TRACK. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53- 11-1 PAGE 53. (M) 2 L 7 2 4F A6WE 1999050700305 19990507 00305 WP 1999 5 7 USAA990323 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 160-200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND .5 INCH BY 30 INCH CORROSION ON FLOOR SUPPORT AT STATION 160 TO 200 INBOARD OF MED. CORRO SION LEVEL 1, CORROSION TASK NR C646-53303. DEFECTIVE PART REPLACED WTH IDENTICAL PART PER SRM 53-11-1 PAGE 53. (M) 2 L 7 2 4F A6WE 1999050700306 19990507 00306 WP 1999 5 7 USAA990322 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 18 INCH CORROSION ON FLOOR SUPPORT AT STATION 200 LEFT SIDE CENTER LINE. CORROS ION LEVEL 1, CORROSION TASK NR C46-53303. DEFECTIVE PART REPLACED WITH IDENTICAL PART MANUFACTURED FROM STOCK EXTRUSION 171-9673. (M) 2 L 7 2 4F A6WE 1999050700307 19990507 00307 WP 1999 5 7 USAA990321 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 8 INCH CORROSION ON GALLEY FLOORBEAM BETWEEN BEAMS NR 26 AND NR 36. CORROSION L EVEL 1, CORROSION TASK NR C46-53303. REMOVED AND REPLACED PART WITH IDENTICAL PART NUMBER PER SRM 53-11-1 PAGE 53. (M) 2 L 7 2 4F A6WE 1999050700308 19990507 00308 WP 1999 5 7 USAA990320 1 19990330 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 160-218 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 30 INCH CORROSION ON FLOOR SUPPORT AT STATION 160 TO 218 CENTER LINE. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REMOVED AND REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F A6WE 1999050700309 19990507 00309 WP 1999 5 7 USAA990319 1 19990330 A 5320 591014221 BEAM DOUG DC9 DC931 3022065 WP CARGO DOORWAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND FORWARD CARGO DOOR FRAME CORRODED (2 INCH BY 3 INCH AREA) ON DOOR FRAME BETWEEN STATION 37 0-427. SPLICED IN NEW SECTION OF DOOR FRAME PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 1999050700310 19990507 00310 NM 1999 5 7 USAASB99096 1 19990412 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM SERVICE DOOR INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 21665 CLE - MAINTENANCE FOUND BOTH AFT SERVICE DOORS EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999050700311 19990507 00311 NM 1999 5 7 99ZZZM262 1 19990412 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM SERVICE DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 21665 CLE - MAINTENANCE FOUND BOTH AFT SERVICE DOORS EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999050700312 19990507 00312 NM 1999 5 7 USAASB99094 1 19990410 A 3397 WIRE BOEING 737 7372B7 1384560 NM BS 360 BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 285AU 23132 ROC - MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRE A T STATION 360 TERMINAL BLOCK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999050700313 19990507 00313 NM 1999 5 7 USAASB99081 1 19990325 A 2410 731753 CSD BOEING 737 7372Q9 138448M NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 231US 39927 21976 CLE - FLT 1055 - ON CLIMB-OUT FROM CLE, THE NR 1 ENGINE GENERATOR DROPPED OFF LINE. CREW COULD NOT RESET THE GENERATOR. DUE TO THE APU BEING ON MEL, THE FLIGHT RETURNED TO FIELD AT CLE AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WA S DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE CONSTANT SPEED DRIVE, GENERATOR AND OIL COOLER. OPERATION AL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999050700314 19990507 00314 NM 1999 5 7 USAASB99087 1 19990331 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM ROW 10 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 353US 23556 ALB - MAINTENANCE FOUND THE CENTER AISLE EXIT SIGN, THE LEFT EMERGENCY HATCH EXIT SIGN, THE LEFT SIDEWALL EXIT SIGN, SEA T 10C EXIT LOCATOR AND THE BULLNOSE EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999050700315 19990507 00315 NM 1999 5 7 USAA990281 1 19990331 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 39871 23382 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION AT BS 344, LBL 50 TO RBL 10 CLIPNUT HOLES FLOORBEAM 'T' CAP. CORROSION TASK NR C53-107-02. FABRICATED 'T' CAP REPAIR PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999050700316 19990507 00316 NM 1999 5 7 USAASB99060 1 19990301 A 2910 LINE BOEING 737 7372B7 1384560 NM LT MLG FAILED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 280AU 22892 PIT - FLT 2333 - FLIGHT DIVERTED TO PIT DUE TO AN 'A' SYSTEM HYDRAULIC FAILURE. FLIGHT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE DUE TO THE LOSS OF NOSE GEAR STEERING. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED T HE FLEX LINE TO THE LEFT MAIN LANDING GEAR DOWNLOCK ACTUATOR. SERVICED HYDRAULIC SYSTEM. LEAK CHECK GOOD. HYDRAULIC S YSTEM DID NOT RUN DRY. (M) 2 L 7 2 4F A16WE 1999050700317 19990507 00317 NM 1999 5 7 USAA990139 1 19990225 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 53397 21666 CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 2 INCH CRACK IN FUSELAGE SKIN BS 727A PLUS 19 INCHES S18R. INSTALLED DO UBLER PER SRM 53-30-03. (M) 2 L 7 2 4F A16WE 1999050700318 19990507 00318 NM 1999 5 7 USAA990182 1 19990309 A 5330 SKIN BOEING 737 737201 1384454 NM BS 943 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 45585 22444 TPA - DURING CX-3 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK IN SKIN STATION 943 STRINGER 24L. INST ALLED DOUBLER PER SRM 53-30-3 FIG 6 AND EA 63860. (M) 2 L 7 2 4F A16WE 1999050700319 19990507 00319 NM 1999 5 7 USAASB99070 1 19990314 A 5240 SEAL BOEING 737 737201 1384454 NM SERVICE DOOR LOOSE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 256AU 22798 CLT - FLT 2675 - AT FL 330, THE FORWARD SERVICE DOOR DEVELOPED A LOUD SQUEAL. CREW DESCENDED TO FL200 BUT SOUND CONTINU ED AND BECAME QUITE ANNOYING. CAPTAIN DECIDED TO DIVERT TO CLT. WHILE DIVERTING TO CLT, SOUND CEASED AT 8,000 FEET. F LIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD SERVICE DOOR SEAL DETACHED AT LOWER FORWARD CORNER. REINSTALLED DOOR SEAL. PRESSURIZED CABIN. NO LEAKS NOTED. (M) 2 L 7 2 4F A16WE 1999050700320 19990507 00320 NM 1999 5 7 USAASB99072 1 19990315 A 5240 SEAL BOEING 737 737201 1384454 NM SERVICE DOOR OUT OF ADJUST A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 256AU 22798 TPA - FLT 2638 - CLIMBING THROUGH FL310, THE FORWARD SERVICE DOOR DEVELOPED A LOUD PITCHED NOISE. SOUND WAS LOUD ENOUGH THAT CAPTAIN DECIDED TO RETURN TO FIELD AT TPA. FLIGHT LANDED WITHOUT INCIDENT. EARLIER IN THE DAY, THE SAME LOUD PIT CHED NOISE CAME FROM THE FORWARD SERVICE DOOR ON CLIMB-OUT FROM CLT. FLIGHT CONTINUED ONTO TPA BUT COULD NOT CLIMB ABOV E FL160. AT THAT TIME, MAINTENANCE FOUND THE UPPER AND LOWER HINGE CUTOUT SEALS CAUSING THE PROBLEM. THEY REPLACED THE UPPER HINGE CUTOUT SEAL AND PROGRAMMED THE LOWER. MAINTENANCE ADJUSTED THE FORWARD SERVICE DOOR LOWER GATE DOOR. PRES SURIZED CABIN TO 7.6 PSI. DOOR SEAL OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999050700321 19990507 00321 NM 1999 5 7 USAA990224 1 19990318 A 5330 6545871523 SKIN BOEING 737 737201 1384454 NM GALLEY DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 45046 22752 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK IN UPPER CORNER OF LOWER FORWARD GALLEY DOOR CUTOUT E XTERNAL SKIN. INSTALLED DOUBLER PER EA 62369. (M) 2 L 7 2 4F A16WE 1999050700322 19990507 00322 NM 1999 5 7 USAA990223 1 19990318 A 5330 SKIN BOEING 737 737201 1384454 NM BS 733-736 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 45046 22752 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK IN EXTERNAL SKIN LOCATED BETWEEN STATION 733 AND 736 A ND STRINGER 8L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1 A 64060 AND SB 52-1096. (M) 2 L 7 2 4F A16WE 1999050700323 19990507 00323 NM 1999 5 7 USAA990245 1 19990323 A 5330 6545871523 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 239US 47438 22354 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SKIN AFT UPPER CORNER OF UPPER HINGE CUTOUT DOOR SK IN. INSTALLED DOUBLER PER TR 52-40-03A. (M) 2 L 7 2 4F A16WE 1999050700324 19990507 00324 NM 1999 5 7 USAA990287 1 19990328 A 5330 SKIN BOEING 737 737201 1384454 NM BS 947.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 40814 22961 TPA - DURING C-4 CHECK VISUAL INSPECTION, FOUND A CRACK 1.25 INCH IN SKIN RIGHT AFT GALLEY SERVICE DOOR LOWER HINGE CUTO UT STRINGER 11R STATION 947.5. INSTALLED DOUBLER PER SRM 53-30-3 FIG 33. (M) 2 L 7 2 4F A16WE 1999050700325 19990507 00325 NM 1999 5 7 USAASB99089 1 19990404 A 2782 654465116 ACTUATOR BOEING 737 7372B7 1384560 NM RT LE SLAT FAILED A USAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 EA 19 278AU 4304 22890 CLE - FL2636 - CAPTAIN STATED THAT THE NR 4 LEADING EDGE SLAT AMBER LIGHT ILLUMINATED ON INITIAL APPROACH. CREW CONFIRM ED VISUALLY THAT THE SLAT WAS NOT FULLY EXTENDED AND DECLARED AN EMERGENCY. AFTER ABOUT 5 MINUTES AT FLAPS 15, THE SLAT DID FULLY EXTEND. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 4 LEADING EDGE SLAT ACTUATOR PER MM 27-81-41. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999050700326 19990507 00326 NM 1999 5 7 USAA990244 1 19990323 A 5330 SKIN BOEING 737 737201 1384454 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 239US 47438 22354 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN SKIN AT STATION 867 STRINGER 19R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999050700327 19990507 00327 NM 1999 5 7 USAA990285 1 19990328 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 40814 22961 TPA - DURING C-4 CHECK VISUAL INSPECTION, FOUND A CRACK .625 INCH SKIN STATION 767 AND STRINGER 19R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999050700328 19990507 00328 NM 1999 5 7 USAA990286 1 19990328 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 40814 22961 TPA - DURING C-4 CHECK VISUAL INSPECTION, FOUND A CRACK 1.25 INCH SKIN STATION 727B STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1 AND EA 64209. (M) 2 L 7 2 4F A16WE 1999050700329 19990507 00329 NM 1999 5 7 USAA990243 1 19990323 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 239US 47438 22354 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN SKIN AT STATION 727A STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999050700330 19990507 00330 NE 1999 5 7 USAABB99018 2 19990407 A 7200 ENGINE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE LEFT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 612AU 27124 30542 PIT - FLT 1 - DURING CLIMB-OUT FROM PIT, AT APPROXIMATELY FL230, THE CREW NOTICED A HEAVY OIL SMELL IN THE CABIN. ALSO, NOTED THAT THE LEFT ENGINE OIL QTY DECREASED SLIGHTLY. THE FLIGHT CREW CLOSED OFF THE LEFT ENGINE BLEED AIR. THE FLIG HT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE ASSEMBLY. (M) 2 L 7 2 4F 4 F RT A2NM A12EU 1999050700331 19990507 00331 EU 1999 5 7 USAAF99020 1 19990405 A 2910 NAS161216 O-RING FOKKER F28 F28MK0100 4990807 EU LT HYD SYSTEM LEAKING A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS DE DESCENT 1 EA 19 895US 11380 BOS - FLT 674 - DURING DESCENT A HYDRAULIC SYSTEM 1 LOW QUANTITY MESSAGE APPEARED. THE FLIGHT CREW DECLARED AN EMERGENC Y AND DIVERTED TO BOS WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE NOTED THAT THE SYSTEM 1 HYDRAULIC S QUANTITY WAS AT 44 PERCENT. REPLACED AN O-RING ON THE LEFT ENGINE SYSTEM 1 HYDRAULIC PUMP SUPPLY LINE. LEAK CHECK AN D SYSTEM TEST WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE (M) 2 L 7 2 4F RT 1999050700332 20000609 00332 EU 2000 6 9 USAAF99021 1 19990403 A 3231 A11320464 DOOR FOKKER F28 F28MK0100 4990807 EU RT MLG DOOR CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 856US 7722 11286 CLT - FLT 2276 - AFTER TAKEOFF FROM CLT, THE LEFT AND RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR DOOR CRACKED. THE DOOR WAS REMOVED AND THE AIRCRAFT OPERATED UNDER CDL 52-05, UNTIL THE DOOR WAS REPLACED 4/6/99. (M) 2 L 7 2 4F RT 1999050700333 19990507 00333 EU 1999 5 7 USAAF99022 1 19990408 A 2131 21185265 CONTROLLER FOKKER F28 F28MK0100 4990807 EU AVIONICS BAY INOPERATIVE A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 896US 16565 11391 ORD - FLT 1543 - EN ROUTE TO MSP FROM CLT AT FL310, THE CABIN PRESSURE ALTITUDE CLIMBED OVER 10,000 FEET. CREW PERFORME D AN EMERGENCY DESCENT. DURING DESCENT THE MANUAL PRESSURIZATION OPERATED INTERMITTENTLY. THE FLIGHT DIVERTED TO ORD A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AIRCRAFT SAFE FOR A FERRY FLIGHT TO PIT. AT PIT, MAINTENANCE REPLACED BOTH CABIN PRESSURE CONTROLLERS. (M) 2 L 7 2 4F RT 1999050700334 19990507 00334 NM 1999 5 7 USAASB99084 1 19990331 A 5240 MECHANISM BOEING 737 737301 1384611 NM SERVICE DOOR NOT LATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 575US 23740 EWR - FLT 605 - AFTER TAKEOFF, CLIMBING THROUGH 2000 FEET, THE AUTO FAIL LIGHT ILLUMINATED. CREW COULD NOT CONTROL CABI N PRESSURIZATION IN STANDBY OR MANUAL MODE. FLIGHT RETURNED TO FIELD TO EWR AND LANDED WITHOUT FURTHER INCIDENT. NO EM ERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT SERVICE DOOR AJAR ON FORWARD SIDE OF DOOR. AFT SIDE OF DOOR WAS CLOSED WHICH CLOSED THE DOOR WARNING SWITCH. RECYCLED DOOR AND OPERATIONALLY CHECKED DOOR. DOOR OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1999050700335 19990507 00335 NM 1999 5 7 USAA990279 1 19990331 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 38624 23316 CLT - DURING A RON VISUAL INSPECTION, FOUND A 1.25 INCH CRACK LEFT SIDE OF FUSELAGE AT STRINGER 24L, 24 INCHES AFT OF AF T WING TO BODY FAIRING SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1999050700336 19990507 00336 EU 1999 5 7 USAAF99019 1 19990402 A 3610 HTE440007 VALVE FOKKER F28 F28MK0100 4990807 EU APU FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 856US 11286 CLT - FLIGHT 861 - AFTER TAKEOFF FROM CLT, A BLEED NR 2 DUCT FAULT OCCURRED. THE FLIGHT RETURNED TO CLT AND LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU CHECK VALVE AND THE OPSOV SEALS. THEY ALSO PERFORMED A BLEED SYSTEM BALANCING ADJUSTMENT. BLEED SYSTEM TESTED NORMAL AFTER REPAIRS. (M) 2 L 7 2 4F RT 1999050700337 19990507 00337 EU 1999 5 7 99ZZZM263 1 19990402 A 3610 BE20062 SEAL FOKKER F28 F28MK0100 4990807 EU APU FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 856US 11286 CLT - FLIGHT 861 - AFTER TAKEOFF FROM CLT, A BLEED NR 2 DUCT FAULT OCCURRED. THE FLIGHT RETURNED TO CLT AND LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU CHECK VALVE AND THE OPSOV SEALS. THEY ALSO PERFORMED A BLEED SYSTEM BALANCING ADJUSTMENT. BLEED SYSTEM TESTED NORMAL AFTER REPAIRS. (M) 2 L 7 2 4F RT 1999050700338 19990507 00338 EU 1999 5 7 USAAF99018 1 19990401 A 2120 AIR DIST FOKKER F28 F28MK0100 4990807 EU CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 859US 11293 ALB - FLT 701 - WHILE CLIMBING THROUGH 2000 FEET, A FLIGHT ATTENDANT INFORMED THE FLIGHT CREW OF A BURNING ODOR IN THE C ABIN AROUND LEFT ROW 17. THE CREW DECLRED AN EMERGENCY AND ELECTED TO DIVERT THE FLIGHT TO ALB. ON APPROACH TO ALB, TH E DOOR DISSIPATED. THE FLIGHT LANDED AT ALB WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIR CONDITIONING PACKS , THE RECIRCULATION FANS AND THE OVERHEAD PANEL. ALL SYSTEMS OPERATED NORMALLY. NO SYSTEM DEFECTS WERE NOTED. THE AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT 1999050700339 19990507 00339 EU 1999 5 7 USAAF99014 1 19990315 A 3230 RETRACT MECH FOKKER F28 F28MK0100 4990807 EU NLG ICED UP A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 896US 11391 IND - FLT 569 - ON APPROACH TO IND WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR DID NOT INDICATE DOWN AND LOCK ED. CREW PERFORMED A GO AROUND PROCEDURE AND RECYCLED THE LANDING GEAR BUT THE GEAR STILL DID NOT INDICATE DOWN AND LOC KED. AN ALTERNATE GEAR EXTENSION WAS NOT SUCCESSFUL IN EXTENDING THE NOSE GEAR. AS A TOWER FLY BY WAS ABOUT TO BE ACCO MPLISHED, THE NOSE GEAR EXTENDED AND A PROPER DOWN AND LOCKED INDICATION ILLUMINATED. THE FLIGHT LANDED IND WITHOUT FUR THER INCIDENT. MAINTENANCE FOUND ICE AND SNOW IMPACTED AROUND THE NOSE GEAR DOWN/LOCKED SWITCH. THEY CLEANED AND LUBRI CATED THE NOSE GEAR ACTUATION SYSTEM. THE LANDING GEAR AND INDICATION SYSTEM THEN TESTED PROPERLY. (M) 2 L 7 2 4F RT 1999050700340 19990507 00340 EU 1999 5 7 USAAF99013 1 19990312 A 3244 TIRE FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA K NONE O OTHER LD LANDING 1 EA 19 857US 11289 PIT - FLT 7881 - AFTER LANDING PIT DURING ROLLOUT, BOTH LEFT MAIN GEAR TIRES BLEW OUT WHEN MODERATE BRAKING WAS APPLIED. MAINTENANCE REPLACED BOTH LEFT MAIN GEAR TIRE ASSEMBLIES AND THE LEFT GEAR GROUND/FLIGHT SWITCH. THE ANTI-SKID SYSTEM AND THE NOSE GEAR STEERING TESTED NORMAL. (M) 2 L 7 2 4F RT 1999050700341 19990507 00341 EU 1999 5 7 USAAF99012 1 19990313 A 5610 D21518405 WINDOW FOKKER F28 F28MK0100 4990807 EU LT COCKPIT CRACKED A USAA K NONE O OTHER CR CRUISE 1 EA 19 897US 10613 11392 CLT - FLT 8076 - EN ROUTE TO CLT AT FL240, THE OUTER PANE OF THE LEFT COCKPIT SLIDING WINDOW CRACKED. FLIGHT WAS A NON- REVENUE FERRY FLIGHT. AIRCRAFT LANDED CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT SLIDING WINDOW. (M) 2 L 7 2 4F RT 1999050700342 19990507 00342 EU 1999 5 7 USAAF99015 1 19990317 A 5610 ROLLER FOKKER F28 F28MK0100 4990807 EU LT COCKPIT OUT OF POSITION A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 894US 11379 PIT - FLT 864 - AFTER DEPARTURE FROM PIT, THERE WAS AN EXCESSIVE AMOUNT OF AIR NOISE FROM THE LEFT SLIDING WINDOW EVEN T HOUGH THE WINDOW WAS CLOSED AND LOCKED. FLIGHT RETURNED AND LANDED AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AFT ROLLER WAS OUT OF ITS TRACK. REINSTALLED THE WINDOW IN THE TRACK. (M) 2 L 7 2 4F RT 1999050700343 19990507 00343 EU 1999 5 7 USAAF99017 1 19990318 A 3230 715381 VALVE FOKKER F28 F28MK0100 4990807 EU NLG FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 851US 11278 MCI - FLT 1075 - WHEN LANDING GEAR WAS EXTENDED FOR APPROACH INTO MCI, CREW RECEIVED A 'NOSE GEAR UNSAFE' WARNING AND TH E GREEN 'NOSE' GEAR SAFE INDICATOR DID NOT ILLUMINATE. CREW RECYCLED THE LANDING GEAR AND ALL GEAR EXTENDED NORMALLY. F LIGHT LANDED AT MCI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE AND THE NOSE GEAR DO OR UPLOCK ACTUATOR. A GEAR SWING WAS SUCCESSFULLY ACCOMPLISHED. (M) 2 L 7 2 4F RT 1999050700344 19990507 00344 EU 1999 5 7 99ZZZM264 1 19990318 A 3232 125005 ACTUATOR FOKKER F28 F28MK0100 4990807 EU NLG DOOR FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 851US 11278 MCI - FLT 1075 - WHEN LANDING GEAR WAS EXTENDED FOR APPROACH INTO MCI, CREW RECEIVED A 'NOSE GEAR UNSAFE' WARNING AND TH E GREEN 'NOSE' GEAR SAFE INDICATOR DID NOT ILLUMINATE. CREW RECYCLED THE LANDING GEAR AND ALL GEAR EXTENDED NORMALLY. F LIGHT LANDED AT MCI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE AND THE NOSE GEAR DO OR UPLOCK ACTUATOR. A GEAR SWING WAS SUCCESSFULLY ACCOMPLISHED. (M) 2 L 7 2 4F RT 1999050700345 19990507 00345 EU 1999 5 7 USAAF99016 1 19990311 A 3260 WARNING LIGHT FOKKER F28 F28MK0100 4990807 EU LANDING GEAR ILLUMINATED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 851US 11278 CLT - FLT 1037 - WHEN LANDING GEAR WAS EXTENDED FOR DESCENT INTO CLT, CREW RECEIVED AN 'UNSAFE GEAR' WARNING ON THE MULT I-FUNCTION DISPLAY. THE GREEN 'NOSE' GEAR SAFE INDICATOR DID NOT ILLUMINATE. THE CREW RECYCLED THE LANDING GEAR AND AL L GEAR EXTENDED NORMALLY. THE FLIGHT LANDED AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NOSE GEAR ASSY, JACKED THE AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS. THE GEAR FUNCTIONED NORMALLY. (M) 2 L 7 2 4F RT 1999050700346 19990507 00346 EU 1999 5 7 USAA990250 1 19990316 A 5530 DOUBLER FOKKER F28 F28MK0100 4990807 EU VERT STAB GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 861US 21283 11297 PIT - DURING C-1 CHECK, FOUND ICE SCRAPER SCREWS GOUGED DOUBLER IN 3 PLACES (.250 L BY .03125 D) (.9375 L BY .032 D) (1. 750 L BY .015625 D) AT LEFT VERT STABILIZER, RIB 5 LEFT SIDE. INSTALLED DOUBLER AND BLENDED PER EA 31078A. (M) 2 L 7 2 4F RT 1999050700347 19990507 00347 NM 1999 5 7 USAASB99088 1 19990401 A 2120 470044 FILTERS BOEING 737 7374B7 1384702 NM AC BAY DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 776AU 24934 SJU - FLT 2134 - AFTER CLIMB-OUT FROM STX AND JUST PASSING SJU, FLIGHT ATTENDANTS NOTICED A BURNING RUBBER TYPE SMELL IN AFT CABIN AT SEAT ROW 21. ON TAKEOFF, THE NR 2 ENGINE HAD A BLEED TRIP BUT IT RESET OK. CREW CYCLED LEFT AND RIGHT PA CKS AND RECIRCULATION FANS OFF AND ON WITH NO EFFECT A SMELL CONTINUED. FLIGHT DIVERTED TO SJU AND LANDED WITHOUT FURTH ER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT CABIN TEMPERATURE BULB AND THE RECI RCULATION FAN FILTERS. SYSTEM CHECKS NORMAL. NO SMELL NOTED. (M) 2 L 7 2 4F RT A16WE 1999050700348 19990507 00348 NM 1999 5 7 USAASB99086 1 19990326 A 3350 500000043 CHARGER BOEING 737 737201 1384454 NM ROW 16 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 CLT - MAINTENANCE FOUND THE SEAT EMERGENCY LIGHTING FROM SEAT ROW 16 ABC AND AFT INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE BATTERY CHARGER AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999050700349 19990507 00349 NM 1999 5 7 99ZZZM265 1 19990326 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM ROW 16 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 CLT - MAINTENANCE FOUND THE SEAT EMERGENCY LIGHTING FROM SEAT ROW 16 ABC AND AFT INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE BATTERY CHARGER AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999050700350 19990507 00350 NM 1999 5 7 USAASB99090 1 19990405 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 387US 22959 ROC - MAINTENANCE FOUND THE AFT CABIN OVERHEAD CEILING EMERGENCY EXIT SIGN AND THE RIGHT EMERGENCY EXIT DOOR SIGN WILL N OT STAY ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999050700351 19990507 00351 NM 1999 5 7 99ZZZM266 1 19990323 A 3242 DISC BOEING 727 727227 1384078 NM NR 4 BRAKE BROKEN A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 772AT 22003 AFTER LANDING AND HOLDING FOR GATE BRAKES DID NOT RELEASE. VIBRATION FELT DURING LANDING. REMOVED AND REPLACED NR 4 BR AKE ASSEMBLY PER MM 32-41-32, OPS CHECK GOOD. BRAKE DISC WAS BROKEN. (M) 2 L 7 3 4F A3WE 1999050700352 19990507 00352 NM 1999 5 7 99ZZZM267 1 19990217 A 8012 97907821 START VALVE BOEING 727 727227 1384078 NM NR 2 ENGINE FAILED A AMTA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 768AT 21996 NR 2 ENGINE START VALVE OPEN LIGHT ILLUMINATED DURING CLIMB-OUT. COMPLIED WITH ABNORMAL PROCEDURE AND SHUTDOWN ENGINE. DIVERTED TO ORD. REPLACED THE NR 2 ENGINE START VALVE, OPS CHECK SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999050700353 19990507 00353 NE 1999 5 7 99ZZZM268 2 19990208 A 7250 TURBINE BOEING 727 727214 138407R NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE FAILED A AMTA C D ABORTED TAKEOFF RETURN TO BLOCK Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 GL 11 786AT 21692 07919B MDW - ABORTED TAKEOFF, TAXIED BACK TO GATE. THE NR 2 ENGINE FAILED AND SOME DEBRIS WERE NOTED ON THE RUNWAY. THE NR 3 AND NR 4 TURBINE BLADES FAILED FOR UNKNOWN REASON. ENGINE WAS REPLACED AND TESTED OK. AIRCRAFT RETURNED TO SERVICE. C ONTAINED DAMAGE, LIMITED DAMAGE THRUST REV. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999050700354 19990507 00354 NM 1999 5 7 99ZZZM269 1 19990203 A 2752 1U1110 ACTUATOR BOEING 727 7272B7 138407L NM TE FLAPS FAILED A AMTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 770AT 21953 DURING CLIMB-OUT, 'A' SYSTEM HYDRAULIC WAS LOST AIR TURN BACK. FOUND LEADING EDGE ACTUATOR FAILED. REMOVED AND REPLACE D ACTUATOR AFT HINGE OF ACTUATOR WAS BROKEN. TESTED FOR LEAKS. (M) 2 L 7 3 4F A3WE 1999050700355 19990507 00355 NM 1999 5 7 99ZZZM270 1 19990129 A 2782 1U1110 ACTUATOR BOEING 727 727227 1384078 NM LE FLAPS FROZEN A AMTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 769AT 21998 DURING CRUISE AT FL100 ENCOUNTERED FLAP PROBLEM. AIR TURN BACK. MAINTENANCE FOUND THE NR 5 LEADING EDGE ACTUATOR FROZE N. MAINTENANCE REPLACED ACTUATOR AND OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999050700356 19990507 00356 NM 1999 5 7 99ZZZM271 1 19990101 A 2131 7638101 CONTROLLER BOEING 727 727227 1384078 NM CABIN FAILED A AMTA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 766AT 21999 AT FL220, CABIN BEGAN TO CLIMB AT 1500 FPM, CREW DONNED OXYGEN MASKS. EMEREGNCY DECLARED AND DIVERTED TO ORD, WITHOUT F URTHER INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, CHECKED SYSTEM AND GOOD. (M) 2 L 7 3 4F A3WE 1999050700357 19990507 00357 WP 1999 5 7 99ZZZM272 1 19990129 A 2420 UL8 RAM AIR TURB LKHEED 1011 10113851 5265010 WP AUX POWER FAILED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 197AT 193P1082 HKG - DURING D-CHECK, THE 'RAT' RAM AIR TURBINE DEPLOYMENT FAILED BY MOTOR ACTUATOR OR MANUAL RELEASE. ACTUATOR FOUND I NTERNALLY SEIZED. REMOVED AND REPLACED ACTUATOR. (M) 2 L 7 3 4F A23WE 1999050700358 19990507 00358 WP 1999 5 7 99ZZZM273 1 19990205 A 3240 213675 BRAKE LKHEED 1011 10113851 5265010 WP LANDING GEAR FAILED A AMTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 11 195AT 4230 193P1041 AFTER TAXI SET PARKING BRAKES, WHEN TRYING TO RELEASE BRAKES, BRAKES WOULD NOT RELEASE. FOUND 2F BRAKE WOULD NOT RELEAS E. REMOVED AND REPLACED BRAKE ASSEMBLY. (M) 2 L 7 3 4F A23WE 1999050700359 19990507 00359 WP 1999 5 7 99ZZZM274 1 19990204 A 2810 O-RING LKHEED 1011 1011385115 5265015 WP NR 3 FUEL TANK FAILED A AMTA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 11 194AT 193B1230 ON PREFLIGHT, FUEL LEAK LOCATED RIGHT WING INBOARD UNDERSIDE FORWARD OF AFT SPARE. REMOVED AND REPLACED NR 3 FUEL TANK OUTBOARD FUELING VALVE PLUG IN ELEMENT O-RING. CHECKED FOR LEAKS WHILE FUELING, NO LEAKS NOTED. (M) 2 L 7 3 4F A23WE 1999050700360 19990507 00360 WP 1999 5 7 99ZZZM275 1 19990226 A 2913 3508807 PUMP LKHEED 1011 10113851 5265010 WP NR 3 HYD SYSTEM FAILED A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 190AT 193C1086 DURING CRUISE, SYSTEM 'D' ENGINE DRIVEN PUMP LO-RR LIGHT ON, PRESS INDICATIONS ZERO. REPLACED NR 3 ENGINE DRIVEN HYD PU MP. LEAK AND OPS CHECK OK PER MM 29-11-07. (M) 2 L 7 3 4F A23WE 1999050700361 19990507 00361 WP 1999 5 7 99ZZZM276 1 19990223 A 2820 VALVE LKHEED 1011 10113851 5265010 WP NR 1 FUEL TANK CONTAMINATED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 187AT 193C1077 DURING CRUISE (FROM M-92 FERRY PERMIT) TANK 1 WAS INCREASING 100 LBS EVERY 38 SECONDS WITH 2L PUMPS ON. REMOVED DEBRIS FROM NR 1 TANK BOOST PUMP HOUSING BYPASS CHECK VALVE PER (F1M-28-24600 FIG 112) VERIFIED 0 FUEL TRANSFER. (M) 2 L 7 3 4F A23WE 1999050700362 19990507 00362 WP 1999 5 7 99ZZZM277 1 19990223 A 2780 72007J BRAKE LKHEED 1011 10113851 5265010 WP LT LE FLAPS FAILED A AMTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 11 193AT 418 193C1017 DURING DESCENT, THE FLAP/SLAT LOCK ANNUNCIATOR LIGHT WILL NOT EXTEND (FIRM 27-81-12-00). REMOVED AND REPLACED LEFT SLAT ASYMMETRY BRAKE PER MM 27-81-31. OPS CHECK GOOD. (M) 2 L 7 3 4F A23WE 1999050700363 19990507 00363 WP 1999 5 7 G6OA031 1 19990404 A 2730 H21881 LATCHES DOUG DC10 DC1030F 3023504 WP LT ELEVATOR FAILED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 600GC 46965 ON TRANSIT WALK AROUND INBOARD DETACHABLE ELEVATOR IN DETACHED POSITION. LATCH PINS FOUND SHEARED. REMOVED AND REPLACE D LEFT DETACHABLE ELEVATOR LATCHES, TWO P/N H2188-1, AND INSTALLED ALL REQUIRED FASTENERS. RELATCHED ELEVATOR AND CHECK ED FOR PROPER MOVEMENT PER MM 27-30-03. REPAIR APPROVED BY MDC, REF FOR 8110-3, 4/5/99, BURCH, DN-DERY-605071-NM. PERM ANENT REPAIR REQUIRED WITHIN 4800 FLT HOURS OR NEXT C-CHECK, REF EO 99-2740-007. (M) 2 L 7 3 4F RT A22WE 1999050700364 19990507 00364 NM 1999 5 7 WRLA99017 1 19990408 A 2421 IDG DOUG MD11 MD11 3023602 NM NR 2 FAILED A WRLA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 272WA 48437 NR 2 IDG FAULTED ON ENGINE START, REPORTED BY FLIGHT CREW. DOWN POWERED AIRCRAFT AND THEN RESET FAULT THROUGH CFDS. SY STEM THEN OPS CHECK OK. (M) 2 L 7 3 4F RT A22WE 1999050700365 19990507 00365 NM 1999 5 7 WRLA990 1 19990409 A 2450 763222 RELAY DOUG MD11 MD11 3023602 NM NR 2 BUS FAILED A WRLA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 EA 27 272WA 48437 NR 2 BUS TIE RELAY FAILED CAUSING LOSS OF NR 2 GENERATOR BUS DURING FLIGHT RESULTING IN AN AIR TURNBACK TO WMKK. MAINTE NANCE REMOVED AND REPLACED NR 2 BUS TIE RELAY AND THE ELECTRICAL POWER CONTROL UNIT. OPERATIONAL CHECKS OF THE SYSTEM C HECKED OK. (M) 2 L 7 3 4F RT A22WE 1999050700366 19990507 00366 EU 1999 5 7 PLGA990405 1 19990405 A 2121 EVCTA465A FAN SAAB SF340 SF340A 7850100 EU CABIN FAILED A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 05 343BE 163 340A101 PWM - FLT 6324 - BOS-PQI - EN ROUTE, THE FLT ATTENDANT NOTED A SMELL OF SMOKE IN THE CABIN. THE F/O'S WENT BACK AND CON FIRMED SMOKE SMELL. THE CRWE DIVERTED INTO PORTLAND AND LANDED WITHOUT INCIDENT. THE FLIGHT CREW DID DECLARE AN EMERGE NCY. THERE WERE 11 PASSENGERS ONBOARD. MAINTENANCE TROUBLESHOT THE SYSTEM AND COULD NOT FIND THE SOURCE OF THE SMOKE S MELL. THE LEFT RECIRCULATING FAN WAS REPLACED AS A PRECAUTION, ALL REQUIRED OPS CHECK PERFORMED AND THE A/C RETURNED TO SERVICE. A SUBSEQUENT TEST FLT WAS PERFORMED WITH NO RECURRENCE OF THE SMOKE SMELL. THE AIRCRAFT HAS OPERATED SINCE W ITH NO RECURRENCE SINCE REPLACING THE RECIRCULATING FAN. (M) 2 L 7 2 4T RT A52EU 1999050700367 19990507 00367 NM 1999 5 7 BJNA990401 1 19990407 A 2910 BACH8A06NN0360T HOSE BOEING 737 7372H4 138448C NM 'A' HYD SYSTEM DAMAGED A BJNA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 11 456TM 20336 LOSS OF SYSTEM 'A' HYDRAULIC SYSTEM IN FINAL APPROACH. REMOVE AND REPLACE BRAKE FLEX LINE IAW MM 20-10-52. INSPECTED C ASE DRAIN FILTER MAGNETIC PLUGS IAW MM 29-11-41, SERVICED HYDRAULIC SYSTEM IAW 12-12-0. RAN ENGINES, OPS AND LEAK CHECK ED OK. (M) 2 L 7 2 4F A16WE 1999050700368 19990507 00368 SO 1999 5 7 C2XA99IA203 1 19990330 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR SO EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13949 145057 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EXTERIOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999050700369 19990507 00369 EU 1999 5 7 C2XA99BT022 1 19990402 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15823 165 DURING 2A INSPECTION IN BTV, FOUND PASSENGER GALLEY/DOOR EMERGENCY EXIT SIGNS AND OUTSIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AT 15WL IAW ATR 42 JIC 33-51-21. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999050700370 19990507 00370 EU 1999 5 7 C2XA99BT021 1 19990401 A 3234 F96GA0102 CONTROL LEVER AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR INOPERATIVE A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 17831 377 185 BTV - FLT 3692 - CREW REPORTED LANDING GEAR TOOK SEVERAL SECONDS TO SECONDS TO EXTEND. LOUD BANGING NOISE DURING DELAY AND UNLOCK LIGHT FLASHED. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW ATR 42 JIC 32-31-81. OPS CHE CKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999050700371 19990507 00371 EU 1999 5 7 C2XA99IA202 1 19990325 A 3246 L610549 BEARING AEROSP ATR42 ATR42320 8680930 EU LT MLG FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 86842 286 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED A POSSIBLE BRAKE PROBLEM ON THE NR 1 BRAKE. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE NR 1 MAIN WHEEL ASSEMBLY OUTBOARD WHEEL BEARING HAD FAILED CAUSING AXLE DAMAGE. MA INTENANCE REMOVED AND REPLACED THE SWING LEVER ASSEMBLY, BRAKE ASSEMBLY, AND WHEEL ASSEMBLY, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999050700372 19990507 00372 CE 1999 5 7 C2XA99C1029 1 19990330 A 7120 BOLT BEECH 1900 1900D 1154162 CE RT ENGINE MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 81536 UE152 CLE - DURING A SCHEDULED INSPECTION THE RIGHT ENGINE AND TRUSS ASSEMBLE WAS FOUND TO HAVE EXCESSIVE MOVEMENT. THE ASSEM BLE WAS INSPECTED FURTHER AND WAS FOUND TO HAVE THE INBOARD UPPER TRUSS ATTACHMENT BOLT MISSING. THE REPAIR OF ASSOCIAT ED CHAFE DAMAGE IS PENDING EVALUATION BY THE MANUFACTURE AND CONTINENTAL EXPRESS ENGINEERING DEPT. (M) 2 L 7 2 4T RT A24CE 1999050700373 19990507 00373 SO 1999 5 7 C2XA99CL027 1 19990302 A 2120 AIR DIST EMB 145 EMB145 SO COCKPIT ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 14933 145018 CLE - FLT 4059 - CREW REPORTED THAT AFTER SETTING TAKEOFF POWER THEY RECEIVED A SMOKE SMELL IN THE COCKPIT. AIRCRAFT RE TURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IT IAW MEL 21-51-00 CONTROL NR 173359. ON 3/24/99 MAINTENANCE PERFORMED A SYSTEM OPERATIONAL CHECK OF THE LEFT PACK, NO DEFECT WERE NOTED IAW EMB145 MM 21-51-00. AIRCRAF T REMOVED FROM MEL. (M) 2 L 7 2 4F RT T00011AT 1999050700374 19990507 00374 CE 1999 5 7 C2XA99IA201 1 19990325 A 7603 SWITCH BEECH 1900 1900D 1154162 CE RT POWER LEVER OUT OF ADJUST A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 17534 UE141 IAH - FLT 3450 - CREW REPORTED RED GEAR LIGHT INDICATION AND HORN WARNING WHEN RETRACTING THE GEAR ON TAKEOFF. THE CREW CYCLED THE GEAR TWICE WITH THE SAME RESULTS AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT POWER LE VER HORN MICROSWITCH OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE MICROSWITCH AND PERFORMED OPERATIONAL CHECK OF THE GEA R RETRACTION. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999050700375 19990507 00375 SO 1999 5 7 C2XA99IA197 1 19990325 A 3350 GE1317 BULB EMB 145 EMB145 SO EXTERNAL FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13936 145025 IAH - DURING MAINTENANCE INSPECTION, THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999050700376 19990507 00376 SO 1999 5 7 C2XA99IA200 1 19990321 A 5315 FLOORBEAM EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15932 145015 IAH - DURING C-CHECK INSPECTION, THE LEFT FLOORBEAM AT FRAME TWENTY WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE DAMAGED SECTION OF FLOORBEAM IAW WITH CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999050700377 19990507 00377 SO 1999 5 7 C2XA99IA199 1 19990321 A 5530 14531597602 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15932 145015 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTENENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01 101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999050700378 19990507 00378 SO 1999 5 7 C2XA99IA198 1 19990321 A 5530 14531597601 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15932 145015 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED A ND REPLACED THE DAMAGED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-011 01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999050700379 19990507 00379 EU 1999 5 7 C2XA99BT020 1 19990324 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 BTV - DURING INSPECTION MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE IN FRONT OF CABIN. REMOVED AND REPLACED EMERGENC Y LIGHT BATTERY LOCATION 3WL. (M) 2 H 7 2 4T RT A53EU 1999050700380 19990507 00380 SO 1999 5 7 C2XA99CL028 1 19990324 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 15732 0216 120195 CLE - FLT 3183 - CREW REPORTED THAT THEY RECEIVED A FLAP CONTROL FAULT ON TAXI OUT, AIRCRAFT RETURNED TO THE GATE. MAIN TENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCR AFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999050700381 19990507 00381 NM 1999 5 7 TSAA9955215 1 19990408 A 5510 BEAM BOEING 737 737297 1384480 NM RT HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 NOTED CORROSION ON UPPER SECTION RIGHT HORIZONTAL STAB TRAILING EDGE BEAM AT RIB STATION 230. MANUFACTURED DOUBLERS FOR REPAIR AT ELEVATOR STATION NUMBERS 39.02, 121.59, AND 176.54. REPAIRED IAW SRM 55-10-7 PAGE 1 THROUGH 13. (M) 2 L 7 2 4F A16WE 1999050700382 19990507 00382 NM 1999 5 7 TSAA9933216 1 19990412 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999050700383 19990507 00383 NM 1999 5 7 TSAA9933217 1 19990412 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 2 FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999050700384 19990507 00384 NM 1999 5 7 TSAA9933206 1 19990409 A 3350 86210151 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED AFT CONTROL MODULE BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999050700385 19990507 00385 NM 1999 5 7 TSAA9933207 1 19990409 A 3350 9221009 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED BATTERY PACK FOR FORWARD PASSENGER EXIT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F A16WE 1999050700386 19990507 00386 NM 1999 5 7 TSAA9933208 1 19990409 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED BATTERY PACK FOR NR 1 FLOOR EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F A16WE 1999050700387 19990507 00387 WP 1999 5 7 HALA9900091 1 19990406 A 3230 HOSR029 HOSE DOUG DC10 DC1010 3022110 WP RT MLG FAILED A HALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 171AA 46906 SEA - FLT 21 - AIR RETURN - CAN'T RAISE GEAR AFTER TAKEOFF UNABLE TO RAISE GEAR HANDLE. THUS GEAR WOULD NOT COME UP. A TTEMPTED GEAR HANDLE RELEASE BUTTON. INSPECTED MAIN GEAR AND FOUND RIGHT MAIN TRIM CYLINDER SUPPLY HOSE RUPTURED AT AFT END OF RT MAIN TRUCK. REPLACED HOSE ASSY WITH REF TO MM TRIM CYLINDER REPLACEMENT, LEAK CHECK GOOD. SERVICED NR 3 HYD RES TO FULL. OK FOR SERVICE. (M) 2 L 7 3 4F A22WE 1999050700388 19990507 00388 WP 1999 5 7 ARWA990401 1 19990416 A 2150 VALVE LKHEED 1011 1011385115 5265015 WP NR 1 PACK FAILED A ARWA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 19 308GB 193U1133 MIA - FLT 508 - CABIN SMOKE ALARM, VERY ACRID SMELL. FOUND NR 1 PACK, OIL IN SYSTEM. NR 1 PACK ON DMI NR 9904 PER MEL 21-51-07. NR 1 PACK VALVE LOCKED IN CLOSE POSITION. (M) 2 L 7 3 4F A23WE 1999050700389 19990507 00389 NM 1999 5 7 ASAA9910063 1 19990327 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 420 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE FLOORBEAM END CAP UPPER SURFACE CORRODED AT STATION 420, LBL 60. REPAIRED PER EA 5310-0 1658. (M) 2 L 7 2 4F RT A16WE 1999050700390 19990507 00390 NM 1999 5 7 ASAA9910062 1 19990327 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT FLOORBEAM LOWER SURFACE CORRODED AT STATION 787, LBL 20 TO LBL 24. REPAIRED PER EA 5310-01656. (M) 2 L 7 2 4F RT A16WE 1999050700391 19990507 00391 NM 1999 5 7 ASAA9910061 1 19990327 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE FLOORBEAM LOWER CAP, LOWER SURFACE, FORWARD FLANGE CORRODED AT STATION 500B BETWEEN LBL 25 AND LBL 45. REPAIRED PER EA 5310-01655. (M) 2 L 7 2 4F RT A16WE 1999050700392 19990507 00392 NM 1999 5 7 ASAA9910060 1 19990327 A 5320 6550568503 SILL BOEING 737 7372X6C 1384552 NM L2 DOORWAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE L2 DOOR THRESHOLD AREA INBOARD CHORD OF DOOR SILL CORRODED AT STATION 947 TO 986, LBL 55 . REPAIRED PER SRM 51-40-4. (M) 2 L 7 2 4F RT A16WE 1999050700393 19990507 00393 NM 1999 5 7 ASAA9910058 1 19990327 A 5311 6546580505 FRAME BOEING 737 7372X6C 1384552 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT FRAME AT STATION 947 CORRODED FROM STRINGER 23L TO 24L. REPAIRED PER SRM 51-40-3 AND 51-40-4. (M) 2 L 7 2 4F RT A16WE 1999050700394 19990507 00394 NM 1999 5 7 ASAA9910057 1 19990327 A 5311 FRAME BOEING 737 7372X6C 1384552 NM BS 807 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT STATION 807 FRAME CORRODED AT STRINGER 25R. REPAIRED PER 51-40-3. (M) 2 L 7 2 4F RT A16WE 1999050700395 19990507 00395 NM 1999 5 7 ASAA9910056 1 19990327 A 5320 BAC5171481 INTERCOSTAL BOEING 737 7372X6C 1384552 NM BS 270 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE INTERCOSTAL AND 'Z' ANGLE CORRODED AT STATION 270, LBL 60-RBL 60. REPAIRED PER SRM 51-4 0-2. (M) 2 L 7 2 4F RT A16WE 1999050700396 19990507 00396 NM 1999 5 7 ASAA9910055 1 19990327 A 5347 605016 SEAT TRACK BOEING 737 7372X6C 1384552 NM BS 375-520 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE SEAT TRACK CORRODED FROM STATION 375 TO 520, LBL 60. REPAIRED PER SRM 51-30-0. (M) 2 L 7 2 4F RT A16WE 1999050700397 19990507 00397 NM 1999 5 7 ASAA9910054 1 19990327 A 5320 THRESHOLD BOEING 737 7372X6C 1384552 NM BS 294-328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE R1 DOOR THRESHOLD CORRODED IN VARIOUS PLACES FROM STATION 294 TO 328. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999050700398 19990507 00398 NM 1999 5 7 ASAA9910053 1 19990327 A 5320 THRESHOLD BOEING 737 7372X6C 1384552 NM BS 259-360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE L1 DOOR THRESHOLD HAS CORROSION IN VARIOUS LOCATIONS ALONG ENTIRE LENGTH STATION 259.5 T O 360. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999050700399 19990507 00399 NM 1999 5 7 ASAA9910052 1 19990327 A 5315 6554907 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND TEH MAIN CABIN FLOORBEAM CORRODED AT STATION 727B FROM RBL 25 TO RBL 60, LBL 45 TO LBL 60. R EPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999050700400 19990507 00400 NM 1999 5 7 ASAA9910051 1 19990327 A 5320 65621101 SILL BOEING 737 7372X6C 1384552 NM CARGO DOORWAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE MAIN CARGO DOOR SHEAR WEB LOWER SILL CORRODED AT STATION 344 TO 520. REPAIRED PER SRM 5 1-30-2. (M) 2 L 7 2 4F RT A16WE 1999050700401 19990507 00401 NM 1999 5 7 ASAA9940078 1 19990331 A 5320 654587570 BEAM BOEING 737 7374Q8 NM BS 280-344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE R1 DOOR TRANSVERSE BEAM CORRODED AT STATION 280-344. (M) 2 L 7 2 4F RT A16WE 1999050700402 19990507 00402 NM 1999 5 7 ASAA9940077 1 19990331 A 5330 SKIN BOEING 737 7374Q8 NM BS 440 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE FORWARD CARGO DOOR CUTOUT, FORWARD SIDE DENTED BETWEEN S23R AND S24R. REPAIRED PER EA 5330-01369. (M) 2 L 7 2 4F RT A16WE 1999050700403 19990507 00403 NM 1999 5 7 ASAA9940076 1 19990331 A 5315 101362404 FLOORBEAM BOEING 737 7374Q8 NM BS 294.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE FLOORBEAM AT STATION 294.5, BL 0 - RBL 5 UPPER CAP CORRODED. REPAIRED PER EA 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999050700404 19990507 00404 NM 1999 5 7 ASAA9940075 1 19990331 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7374Q8 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE FLOORBEAM UPPER HORIZONTAL CAP CORRODED AT STAITON 967, LBL 18. REPAIRED PER SRM 53-00 -51. (M) 2 L 7 2 4F RT A16WE 1999050700405 19990507 00405 NM 1999 5 7 ASAA9940074 1 19990331 A 5315 BAC1505100778 FLOORBEAM BOEING 737 7374Q8 NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE FLOORBEAM UPPER HORIZONTAL CAP, TO SURFACE, CORRODED AT STATION 312 LBL 2 - RLB 7. REP AIRED PER SRM 53-10-51 AND DRAWING 65C33941. (M) 2 L 7 2 4F RT A16WE 1999050700406 19990507 00406 NM 1999 5 7 ASAA9940073 1 19990331 A 5330 SKIN BOEING 737 7374Q8 NM BS 490-500 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE RIGHT FUSELAGE SKIN AT STATION 490-500, STRINGER 22R-24R NICKED. REPAIRED PER SRM 53-0 0-01. (M) 2 L 7 2 4F RT A16WE 1999050700407 19990507 00407 NM 1999 5 7 ASAA9940072 1 19990331 A 5320 654580772 FRAME BOEING 737 7374Q8 NM R1 DOORWAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 PHX - DURING SI CHECK, FOUND THE R1 DOOR CUTOUT FORWARD FRAME AT STATION 296 WL 209 CRACKED. REPAIRED PER EA 5310-01664 . (M) 2 L 7 2 4F RT A16WE 1999050700408 19990507 00408 NM 1999 5 7 ASAA9940068 1 19990326 A 5210 65648367 LATCH BOEING 737 7374Q8 NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 782AS 25113 PDX - PRIOR TO FLT 348, THE ATTENDANT REPORTED THAT THE L1 DOOR WAS HARD TO CLOSE. LUBRICATED HINGE POINTS AND ADJUSTED THE FORWARD UPPER LATCH CAM FITTING. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999050700409 19990507 00409 NM 1999 5 7 ASAA9940071 1 19990329 A 5610 ROD BOEING 737 737490 1384715 NM RT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 793AS 28888 ANC - PRIOR TO FLT 92, THE CREW REPORTED THAT THEY WERE UNABLE TO CLOSE THE FIRST OFFICERS SLIDING WINDOW. INSPECTED AN D FOUND THE PIN GUIDE ROD OUT OF ADJUSTMENT. REPOSITIONED PIN GUIDE ROD AND THE WINDOW SLIDING WINDOW OPERATED NORMALLY . (M) 2 L 7 2 4F RT A16WE 1999050700410 19990507 00410 NM 1999 5 7 ASAA9910050 1 19990327 A 5320 6941473 INTERCOSTAL BOEING 737 7372X6C 1384552 NM BS 927-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT INTERCOSTAL CORRODED AT STATION 927 TO 947 BETWEEN STRINGER 25R AN D 26R. REPAIRED PER SRM 51-20-1 AND DRAWING 69-41473. (M) 2 L 7 2 4F RT A16WE 1999050700411 19990507 00411 NM 1999 5 7 ASAA9910049 1 19990327 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE FLOORBEAM CORRODED AT STATION 328, RLB 73. REPAIRED PER SRM 51-10-6 AND 53-10-9. (M) 2 L 7 2 4F RT A16WE 1999050700412 19990507 00412 NM 1999 5 7 ASAA9910048 1 19990327 A 5320 6918388 INTERCOSTAL BOEING 737 7372X6C 1384552 NM BS 380-400 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE INTERCOSTAL CORRODED AT STATION 380 TO 400, STRINGER 25L. REPAIRED PER SRM 51-10-6. (M ) 2 L 7 2 4F RT A16WE 1999050700413 19990507 00413 NM 1999 5 7 ASAA9910047 1 19990327 A 5320 655169815 SPLICE BOEING 737 7372X6C 1384552 NM BS 907 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT STRINGER 25R SPLICE AT STATION 907 TO 927 CORRODED. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999050700414 19990507 00414 NM 1999 5 7 ASAA9910046 1 19990327 A 5347 605013 SEAT TRACK BOEING 737 7372X6C 1384552 NM BS 340-460 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE SEAT TRACK CORRODED AT STATION 340 TO 460, LBL 45. REPAIRED PER SRM 51-10-1, 51-30-2 AN D 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700415 19990507 00415 NM 1999 5 7 ASAA9910045 1 19990327 A 5312 BAC5602 BULKHEAD BOEING 737 7372X6C 1384552 NM BS 1156 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE BULKHEAD LOWER SECTION CORRODED AT STATION 1156, LBL 6. REPAIRED PER 51-30 AND 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700416 19990507 00416 NM 1999 5 7 ASAA9910044 1 19990327 A 5315 ASA0071230022 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 520 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE FLOORBEAM CORRODED AT STATION 520, LBL 45 TO RBL 60. REPAIRED PER SRM 51-30. (M) 2 L 7 2 4F RT A16WE 1999050700417 19990507 00417 NM 1999 5 7 ASAA9910043 1 19990327 A 5532 SKIN BOEING 737 7372X6C 1384552 NM VERT STABILIZER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE RIGHT SIDE OF THE VERTICAL STABILIZER DENTED 10 INCHES ABOVE PITOT TUBE FIN STATION 81.1 . REPAIRED PER SRM 5530-30-3. (M) 2 L 7 2 4F RT A16WE 1999050700418 19990507 00418 NM 1999 5 7 ASAA9910042 1 19990327 A 5315 BAC1518431 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 460 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE FORWARD CARGO COMPARTMENT FLOORBEAM LOWER FLANGE CORRODED AT STATION 460, LBL 24 TO LBL 44. REPAIRED PER EA 5310-01663. (M) 2 L 7 2 4F RT A16WE 1999050700419 19990507 00419 NM 1999 5 7 ASAA9910041 1 19990327 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOORBEAM CORRODED ON THE UPPER CAP AT STATION 967, RLB 8 TO RBL 45. REPAIRE D PER EA 5310-01662. (M) 2 L 7 2 4F RT A16WE 1999050700420 19990507 00420 NM 1999 5 7 ASAA9910040 1 19990327 A 5312 BULKHEAD WEB BOEING 737 7372X6C 1384552 NM BS 1016 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD WEB CRACKED FROM FOUR CONSECUTIVE FASTENERS AT AFT ROW WHERE IT AT TACHES TO THE 'Y' CHORD AT STATION 1016. REPAIRED PER EA 5310-01659. (M) 2 L 7 2 4F RT A16WE 1999050700421 19990507 00421 NM 1999 5 7 ASAA9910039 1 19990327 A 5330 65458295 SKIN BOEING 737 7372X6C 1384552 NM BS 344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE INTERNAL SKIN CORRODED AT STATION 344, STRINGER 27L. REPAIRED PER EA 5310-01651. (M) 2 L 7 2 4F RT A16WE 1999050700422 19990507 00422 NM 1999 5 7 ASAA9910038 1 19990327 A 5315 FLOORBEAM BOEING 737 7372X6C 1384552 NM BS 294.5 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE FLOORBEAM GOUGED AT STATION 294.5, LBL 10 TO RBL 50. REPAIRED PER SRM 53-10-09. (M) 2 L 7 2 4F RT A16WE 1999050700423 19990507 00423 NM 1999 5 7 ASAA9910037 1 19990327 A 5320 BAC14902807 SHEAR TIE BOEING 737 7372X6C 1384552 NM BS 747 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT SHEAR TIE AT FRAME CORRODED AT STATION 747 BETWEEN STRINGER 26R AN D STRINGER 27R. REPAIRED PER 53-10-4, 51-10-1, AND 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700424 19990507 00424 NM 1999 5 7 ASAA9910036 1 19990327 A 5320 6551627 DOUBLER BOEING 737 7372X6C 1384552 NM BS 967-986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT SKIN DOUBLER AROUND THE OUTFLOW VALVE CORRODED BETWEEN STATION 967 -986, STRINGER 22R STRINGER 25R. REPAIRED PER 53-10-3 AND DRAWING 6551627. (M) 2 L 7 2 4F RT A16WE 1999050700425 19990507 00425 NM 1999 5 7 ASAA9910035 1 19990327 A 5347 BAC15201432 SEAT TRACK BOEING 737 7372X6C 1384552 NM BS 727-787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK CORRODED FROM STATION 727B TO 787, LBL 25. REPAIRED PER SRM 53-10 -2 AND 53-10-5. (M) 2 L 7 2 4F RT A16WE 1999050700426 19990507 00426 NM 1999 5 7 ASAA9910034 1 19990327 A 5313 STRINGER BOEING 737 7372X6C 1384552 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND STRINGER 22L CORRODED AT STATION 947. REPAIRED PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700427 19990507 00427 NM 1999 5 7 ASAA9910033 1 19990327 A 5313 STRINGER BOEING 737 7372X6C 1384552 NM BS 804 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND STRINGER 26L CORRODED AT STATION 804. REPAIRED PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700428 19990507 00428 NM 1999 5 7 ASAA9910032 1 19990327 A 5320 SILL BOEING 737 7372X6C 1384552 NM BS 787-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT INNER DOOR WEB CORRODED AT STATION 787-847 IN LOWER DOOR SILL. RE PAIRED PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700429 19990507 00429 NM 1999 5 7 ASAA9910031 1 19990327 A 5320 BAC14902807 SHEAR TIE BOEING 737 7372X6C 1384552 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT SHEAR TIE AT THE FRAME CORRODED AT STATION 787 BETWEEN STRINGER 26 R AND 27R. REPAIRED PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700430 19990507 00430 NM 1999 5 7 ASAA9910030 1 19990327 A 5347 BAC15201331 SEAT TRACK BOEING 737 7372X6C 1384552 NM BS 727-767 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE SEAT TRACK CRACKED AT STATION 727B TO 767, BL 0. REPAIRED PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999050700431 19990507 00431 NM 1999 5 7 ASAA9910029 1 19990327 A 5320 SUPPORT BOEING 737 7372X6C 1384552 NM BS 707 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOOR SUPPORT CORRODED AT STATION 707, RBL 25 - RBL 45. REPAIRED PER SRM 53- 10-1 AND DRAWING 65-54988. (M) 2 L 7 2 4F RT A16WE 1999050700432 19990507 00432 NM 1999 5 7 ASAA9910028 1 19990327 A 5320 6567140509 SUPPORT BOEING 737 7372X6C 1384552 NM BS 663 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 PHX - DURING D-CHECK, FOUND THE MAIN CARGO FLOOR SUPPORT CORRODED AT STATION 663, RBL 45 - RBL 60. REPAIRED PER SRM 53- 10-01. (M) 2 L 7 2 4F RT A16WE 1999050700433 19990507 00433 NM 1999 5 7 99ZZZM278 1 19990406 A 3230 656021123 MODULE BOEING 727 727208 138407W NM LANDING GEAR FAILED A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 780AT 22295 IND-PIE - DURING CLIMB, THE LANDING GEAR SELECTOR LEVER GOT STUCK IN THE MID POSITION, LANDING GEAR STAYED EXTENDED. CR EW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR ELECTRONIC CONTROL MODULE, SWUNG GEARS AND TES TED OK. (M) 2 L 7 3 4F RT A3WE 1999050700434 19990507 00434 NE 1999 5 7 TWAA9906401 2 19990403 A 7250 TURBINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 1 ENGINE FAILED A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 05 914TW 49185 1210 DURING TAKEOFF, THERE WAS A LOUD NOISE FROM THE NUMBER 1 ENG FOLLOWED BY HIGH EGT INDICATION. THE ENG WAS SHUT DOWN AND THE FLIGHT RETURNED TO STL. FOUND THE TURBINE HAD FAILED. REPLACED THE ENGINE. CHECK-C 2-13-99 MCI. 2 L 7 2 4F 4 F A6WE E9NE 1999050700435 19990507 00435 WP 1999 5 7 TWAA9906402 1 19990502 A 2131 10256862 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN WORN A TWAA B EMER. DESCENT G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 CE 05 987Z 47137 AIRCRAFT LOST CABIN PRESSURIZATION AT FL 350. OXYGEN MASKS DROPPED AUTOMATICALLY. ACCOMPLISHED EMERGENCY DESCENT AND L ANDED AT SCHEDULED STATION, AUS. DEFERRED AUTO PRESSURIZATION CONTROL PER MEL AND OPERATED TO STL. AT STL REPLACED THE AUTO PRESSURIZATION CONTROLLER AND PERFORMED A HULL LEAK CHECK AND TEST. CHECK-C 4-21-99 STL. 2 L 7 2 4F A6WE 1999050700436 19990507 00436 1999 5 7 TWAA9906403 4 19990502 A 2565 100504203 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR LOW PRESSURE A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 901TW 49166 THE FORWARD GALLEY DOOR EVACUATION SLIDE PRESSURE WAS LOW. REPLACED THE SLIDE. CHECK-C 7-4-98 STL. 2 L 7 2 4F A6WE 1999050700437 19990507 00437 WP 1999 5 7 TWAA9906404 1 19990503 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 926L 47172 THE RT ENGINE EMERGENCY NACELLE LIGHT, OVERWING EXIT LIGHTS, AND THE AFT CABIN EXIT LIGHTS WERE INOPERATIVE. REPLACED T HE NACELLE LIGHT BATTERY PACK PN B030CF00101, THE OVERWING LIGHT BATTERY PACK PN 41B004AD07G3, AND BOTH AFT CABIN EXIT B ULBS PN 1315. CHECK-C 1-31-99 STL. 2 L 7 2 4F A6WE 1999050700438 19990507 00438 WP 1999 5 7 TWAA9906405 1 19990429 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE BELOW CABIN FLOOR AT RBL 45 TO RBL 55 IN, AT STA 218 TO 237. REMO VED CORRODED MEMBRANE AND INSTALLED NEW ONE PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999050700439 19990507 00439 NM 1999 5 7 AT9900349 1 19990503 A 3350 1000679 LIGHT BOEING 737 7372T4 1384492 NM L1 DOOR DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 467AT 22055 OVER DOOR ( L-1 ) EMERGENCY EXIT LIGHT INOPERATIVE IN ARM POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. 2 L 7 2 4F A16WE 1999050700440 19990507 00440 NM 1999 5 7 AT9900350 1 19990422 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 203 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLAPPER VALVE FORWARD OF THE NOSE COMPARTMENT INNER SKIN AT BS 203 BL-0 CORRODED. REMOVED SKIN, FABRICATED AND INSTALLED REPAIR IAW B737 SRM 53-30-2, 51-21-11, 53-30-3, AND 51-10-2. 2 L 7 2 4F RT A16WE 1999050700441 19990507 00441 NM 1999 5 7 AT9900351 1 19990429 A 2560 BRACKET BOEING 737 7372L9 1384497 NM L1 DOOR SLIDE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE L-1 DOOR SLIDE FLOOR MOUNT AFT HOOK ATTACH BRACKET CORRODED AND FASTENE R MISSING. REMOVED AND REPLACED BRACKET, TREATED, PRIMED, AND INSTALLED FASTENERS ON BRACKET IAW B737 SRM 51-10-4, 51-1 0-2, 51-30-2, 53-10-1, AND 51-21-31. 2 L 7 2 4F RT A16WE 1999050700442 19990507 00442 NM 1999 5 7 AT9900352 1 19990429 A 5320 6941752504 INTERCOSTAL BOEING 737 7372L9 1384497 NM BS 500-520 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE INTERCOSTAL FLANGE AT BS 500-520 STR 26R CORRODED. REMOVED INTERCOSTAL , PROCURED NEW PART, DRILLED, DEBURRED, TREATED IAW B737 SRM 53-10-1, 51-30-5, AND 51-10-2. 2 L 7 2 4F RT A16WE 1999050700443 19990507 00443 NM 1999 5 7 AT9900353 1 19990502 A 7110 COWL BOEING 737 7372L9 1384497 NM N1 ENGINE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND NR 1 ENGINE COWLING PANEL NR 5102 CORRODED. FABRICATED DOUBLER AND INSTALL ED IAW B737 SRM 51-40-2, 51-10-2, AND MM 51-21-31. 2 L 7 2 4F RT A16WE 1999050700444 19990507 00444 WP 1999 5 7 AT9900354 1 19990224 A 5720 5920285502 BRACKET DOUG DC9 DC932 3022066 WP WS 238 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 238 BRACKET CORRODED. REMOVED A ND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2. 2 L 7 2 4F A6WE 1999050700445 19990507 00445 WP 1999 5 7 AT9900355 1 19990224 A 5720 39202772 BRACKET DOUG DC9 DC932 3022066 WP WS 222 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 222 BRACKET CORRODED. REMOVED A ND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2. 2 L 7 2 4F A6WE 1999050700446 19990507 00446 WP 1999 5 7 AT9900356 1 19990224 A 5720 5920286502 BRACKET DOUG DC9 DC932 3022066 WP WS 209 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND ON THE RIGHT WING FORWARD SPAR AREA AT XOS 209 BRACKET CORRODED. REMOVED A ND REPLACED BRACKET. TENSION AND RIG CHECKS ACCOMPLISH IAW DC9 SRM 51-10-0, MM 20-17-0, 27-80-4, AND 27-80-2. 2 L 7 2 4F A6WE 1999050700447 19990507 00447 SO 1999 5 7 LR7A9926 1 19990429 A 2150 CLAMP LKHEED 382 382G 526414U SO BS 467 LOOSE A LR7A H DEACTIVATE SYST/CIRCUITS J M WARNING INDICATION OVER TEMP CR CRUISE 1 AL 03 404LC 4763 CARGO COMPARTMENT AIR CONDITIONING OVERHEAT LIGHT CAME ON IN-FLIGHT. SHUTDOWN CARGO COMPARTMENT AIR CONDITIONING SYSTEM IAW AFM EMERGENCY PROCEDURES AND ISOLATED WING. DEFERRED CARGO COMPARTMENT AIR CONDITIONING SYSTEM PER MEL 21-1, DMI L OG NR 00082. SPECIAL PROCEDURE NR 1 C/W, CARGO COMPARTMENT FLOW CONTROL AND SHUT OFF VALVE SECURED CLOSED IAW SMP 581 2 1A-50, PG 208. CLEARED DMI 00082 5/4/99, TAT: 39998. TIGHTENED CLAMPS NEAR TURBINE BYPASS AREA CARGO COMPARTMENT AIR C ONDITIONING. LEAK AND OPS CHECK PER SMP 581 21A-50-201. 2 H 7 4 4T A1SO 1999050700448 19990507 00448 NM 1999 5 7 AWXA9900159 1 19990424 A 5330 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 IN MAINTENANCE, FOUND SKIN CRACK, FUSELAGE LT SIDE AFT OF UPPER WING TO BODY FAIRING, 1 INCH LONG. VERIFIED BY HFEC AND MARKED ENDS. REPAIRED WITH BLIND RIVET REPAIR PER SRM 53-30-3, FIG 6, INSPECT BLIND RIVET REPAIR AT 3000 FLT CYC THEN 2500 FLT CYC THERE AFTER. REPLACE WITH SOLID RIVET REPAIR IF LOOSE RIVET FOUND OR AT 10,000 FLT CYC. 2 L 7 2 4F RT A16WE 1999050700449 19990507 00449 NM 1999 5 7 AWXA9900160 1 19990423 A 2910 LINE BOEING 737 737277 1384570 NM A HYD SYST LEAKED A AWXA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS F J K FLT CONT AFFECTED WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 28 188AW 22655 AIR TURN BACK, HYD FLUID LOSS. AIRCRAFT TOOK OFF FROM PHOENIX AND LOST HYDRAULIC FLUID IN THE 'A' SYSTEM. AIRCRAFT AIR RETURNED TO PHX. 'A' SYS AILERON PRESSURE LINE FOUND TO BE LEAKING. REMOVED AND REPLACED AILERON PRESSURE LINE OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999050700450 19990507 00450 NM 1999 5 7 AWXA9900161 1 19990424 A 2910 FLUID BOEING 737 737277 1384570 NM A HYD SYST LOSS A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 188AW 22655 HYD FLUID LOSS. LOSS OF 'A' SYS HYD QUANITY INFLIGHT. (DROPPED TO APPR .75 GAL) ACCOMPLISHED LOSS OF SYS 'A' CHECKLIST DIVERTED TO LAS. SERVICE HYD SYS WITH 6 QUARTS. RAN ELEC PUMPS, INTERCONNECT OPEN AND CLOSED, NO LEAKS FOUND. RAN ENG INES WITH PUMPS ON. NO LEAKS FOUND, HYD QUANTITY AND PRESS NORMAL. A/C IS OK FOR CONTINUE SERVICE. 2 L 7 2 4F RT A16WE 1999050700451 19990507 00451 NM 1999 5 7 AWXA9900162 1 19990423 A 2913 5718603 PUMP BOEING 737 7373S3 1384711 NM A HYD SYST LEAKED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 316AW 13957 10676 23713 AIR TURN BACK, HYD FLUID LOSS ME PN 03-2914-9-0003. LOSS OF 'A' SYS HYD FLUID RETURN TO PHX. FOUND A LEAK ON THE PRESS URE SIDE OF THE ELECTRIC HYD PUMP. REMOVED AND REPLACED PUMP, OPS AND LEAK CK GOOD. 2 L 7 2 4F RT A16WE 1999050700452 19990507 00452 NM 1999 5 7 AWXA9900163 1 19990420 A 5320 693535213 CLIP BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 183AW 22650 IN MAINTENANCE, FOUND CRACKS, STRINGER CLIPS AT THE FOLLOWING LOCATIONS ARE CRACKED CABIN FS 947.6 STR 25R, FS 787 STR 1 , FS 767 STR 5L, 6R, 6L, 7R, FS 727A STR 4L, 7R, FS 727B STR 5R, FS 688 STR L2, FS 639 STR L2. REMOVED AND REPLACED STR INGER CLIPS PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 1999050700453 19990507 00453 EU 1999 5 7 AWXA9900164 1 19990423 A 5347 ASNA2223 FLOOR TRACK AIRBUS 320 A320231 3930325 EU BS 765 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 IN MAINTENANCE, FOUND CORROSION SEAT TRACK Y765 LEFT CORRODED FR 20. REPAIRED PER SRM 53-00-15, NRC 5159871, ZONE 1D SE Q 022. 2 L 7 2 4F RT A28NM 1999050700454 19990507 00454 EU 1999 5 7 AWXA9900165 1 19990423 A 5320 ASNA2199 RAIL AIRBUS 320 A320231 3930325 EU BS 189 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 IN MAINTENANCE, FOUND CORROSION DUMMY RAIL Y189 RT CORRODED AT FR 21. FABRICATED NEW RAIL Y189 AS PER SRM 51-72-11. TR EATED, PRIMED AND PAINTED PER SRM 51-75-00. INSTALLED RAIL PER DWG D5312836. NRC 5159872, ZONE 1D SEQ 023. 2 L 7 2 4F RT A28NM 1999050700455 19990507 00455 EU 1999 5 7 AWXA9900166 1 19990423 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 254 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 IN MAINTENANCE, FOUND CORROSION ON FLOOR RAIL Y254 CORRODED FROM FR 16 TO FR 20. FABRICATED NEW TRACK AS PER DWG D53112 782200. TREATED, PRIMED AND PAINTED PER SRM 51-75-00. INSTALLED RAIL PER SRM 53-11-14. NRC 5159873, ZONE 1D SEQ 024. 2 L 7 2 4F RT A28NM 1999050700456 19990507 00456 EU 1999 5 7 AWXA9900167 1 19990423 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 1292 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 IN MAINTENANCE, FOUND CORROSION ON FLOOR RAIL Y1292 RT CORRODED FROM FR 16 TO TRACK SPLICE AT C-20. FABRICATED NEW RAIL PER DWG D53112781202. TREATED, PRIMED AND PAINTED PER 51-75-00. INSTALLED RAIL PER SRM 51-72-11. NRC 5159876, ZONE 1 D SEQ 026. 2 L 7 2 4F RT A28NM 1999050700457 19990507 00457 EU 1999 5 7 AWXA9900168 1 19990423 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 254 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 IN MAINTENANCE, FOUND CORROSION ON FLOOR RAIL Y254 LT, FR 16-23 CORROSION AROUND MOUNT SCREW HOLES, CORROSION ON UPPER A ND LOWER SURFACES. CORROSION REMOVAL BEYOND LIMITS. FABRICATED NEW RAIL PER DWG D5311281200. TREATED, PRIMED AND PAIN TED AS PER SRM 51-75-00. INSTALLED RAIL PER SRM 51-72-11, NRC5159866, ZONE 1D SEQ 017. 2 L 7 2 4F RT A28NM 1999050700458 19990507 00458 NM 1999 5 7 AWXA9900170 1 19990428 A 5330 SKIN BOEING 737 737277 1384570 NM BS 747 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 FUSELAGE SKIN CRACK ABOVE WTB AT STRINGER 17, FWD OF STATION 747, REPAIRED. 2 L 7 2 4F RT A16WE 1999050700459 19990507 00459 NM 1999 5 7 AWXA9900171 1 19990428 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 FUSELAGE SKIN CRACK ABOVE WTB FAIRING AT STRINGER 17 BETWEEN 727A AND 727, REPAIRED. 2 L 7 2 4F RT A16WE 1999050700460 19990507 00460 NM 1999 5 7 AWXA9900172 1 19990428 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 FUSELAGE SKIN CRACK ABOVE WTB FAIRING RT AT STRINGER 15 BETWEEN 727A AND 727, REPAIRED. 2 L 7 2 4F RT A16WE 1999050700461 19990507 00461 NM 1999 5 7 AWXA9900173 1 19990428 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 FUSELAGE SKIN CRACK AT STRINGER 16R AT FS 727A, REPAIRED. 2 L 7 2 4F RT A16WE 1999050700462 19990507 00462 NM 1999 5 7 AWXA9900174 1 19990428 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 FUSELAGE SKIN CRACK AT STRINGER 19R AT FS 727B, REPAIRED. 2 L 7 2 4F RT A16WE 1999050700463 19990507 00463 NM 1999 5 7 AWXA9900175 1 19990420 A 5311 STRINGER BOEING 737 737277 1384570 NM BS 967-1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 183AW 22650 CORROSION OUT OF LIMITS ON STRINGER 27L AT FRAME 967. REMOVED STRINGER 27L AT STA 967 TO 1016. FABRICATED 3 EA STRINGE RS 6 EA SPLICE ANGLES 2 EA N CHANNELS. TREATED PRIMED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-2, 57-30-3 FIG 1 A ND TORQUED 2 EA STRINGER END FITTING BOLTS IAW SRM 51-40-4N 2 L 7 2 4F RT A16WE 1999050700464 19990507 00464 NM 1999 5 7 AWXA9900176 1 19990402 A 3350 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 D-EMERGENCY EXIT LIGHT ON CEILING PANEL FOR OVERWING EXIT IS NOT WORKING. REPAIRED BROKEN WIRE AT CONNECTOR ON TOP OF EMERGENCY LIGHT, CHECKS OK. 2 L 7 2 4F RT A16WE 1999050700465 19990507 00465 NM 1999 5 7 CALA9900468 1 19990503 A 5330 6518420 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 FUSELAGE SKIN CRACKED UPPER LEFT CORNER OF CAPTAINS WINDSHIELD 1/2 TO RIVET. CONFIRMED WITH HFEC. REPAIRED PER EC/RA 5 330-02802. 2 L 7 2 4F RT A16WE 1999050700466 19990507 00466 WP 1999 5 7 CALA9900469 1 19990503 A 5330 59164341 SKIN DOUG DC9 DC982 3022082 WP BS 383 HOLE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 TEMPORARY REPAIR APPROXIMATELY STA 383 L-29LT WHERE PREVIOUS PHONE ANTENNA INSTALLED. INSTALLED DOUBLERS PER SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1999050700467 19990507 00467 WP 1999 5 7 CALA9900470 1 19990503 A 5312 991556173 BULKHEAD DOUBLER DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 CORROSION AT AFT PRESSURE BULKHEAD AND VERTICAL BULKHEAD INTERSECTION AT STA 1338 FROM L-29LT TO L-29RT. REMOVED CORROS ION AND INSTALLED SERVICEABLE JACK PAD DOUBLER PER SRM 51-10-3 AND DRAWING NR PL J936439 AND J936667. 2 L 7 2 4F A6WE 1999050700468 19990507 00468 WP 1999 5 7 CALA9900471 1 19990505 A 3350 08330030002 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33506 47765 TWO RED FLOOR PROX LIGHTS AT FORWARD END INOP. RELAMPED FORWARD RED EMERGENCY PROX LIGHT. SPLICED IN NEW SOCKET FOR OT HER LIGHT. OPS CHECK NORMAL. 2 L 7 2 4F A6WE 1999050700469 19990507 00469 WP 1999 5 7 CALA9900472 1 19990505 A 3350 276005 FUSE DOUG DC9 DC932 3022066 WP L1-L2 DOOR FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33506 47765 L1 AND L2 DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED FUSES IN BATTERY PACK IN FORWARD O/H CEILING. 2 L 7 2 4F A6WE 1999050700470 19990507 00470 WP 1999 5 7 CALA9900473 1 19990505 A 5754 SKIN DOUG DC10 DC1030 3023501 WP LT LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 NR 1 LEFT SLAT OUTER SKIN CRACKED. REPAIRED PER SRM 57-10-00, NR 6 LEADING EDGE RIB FOUND CRACKED. NEW RIBS FABRICATED PER DWG NRB6223 OP 3 AND ARB1583-405 OP 1. 2 L 7 3 4F A22WE 1999050700471 19990507 00471 NM 1999 5 7 CALA9900475 1 19990504 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 400-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 CABIN FLOOR INTERCOSTAL CRACKED (10) ON TOP FLANGE 0 BL FS 400 - 420. REMOVED DAMAGED FLANGE AND FABRICATED NEW FLANGE, TREATED, PRIMED, AND INSTALLED PER SRM 51-10-1, 51-30-2, AND 51-10-6. 2 L 7 3 4F A3WE 1999050700472 19990507 00472 NM 1999 5 7 CALA9900476 1 19990504 A 5754 RIB BOEING 727 727224 1384076 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 APPROX 1.25 CRACK AT 3RD FROM INBOARD END RIB INSIDE LEFT WING NR 2 SLAT. STOP DRILLED CRACK. FABRICATED AND INSTALLED TYPICAL FORM DOUBLER FROM 2024 T3 PER SRM 51-40-3. INSTALLED ACCESS PANEL PER 51-30-2. 2 L 7 3 4F A3WE 1999050700473 19990507 00473 NM 1999 5 7 CALA9900477 1 19990504 A 5754 BAC15141559 MOUNT BOEING 727 727224 1384076 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 APPROX .375 VISIBLE BRANCHING CRACK AT LEFT WING NR 2 SLAT WHERE INBOARD UP STOP PAD MOUNTS. CUT OUT DAMAGED AREA. FAB RICATED AND INSTALLED EXTRUDED ANGLE REPAIR PER 51-4-4 FIG 3. INSTALLED PANELS PER 51-30-2. 2 L 7 3 4F A3WE 1999050700474 19990507 00474 NM 1999 5 7 CALA9900478 1 19990504 A 5755 HINGE BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 APPROX .25 CRACK AT LEFT WING UPPER T/E AT 2ND FROM O/B CUT OUT FOR NR 4 SPOILER HINGE. STOP DRILLED CRACK PER SRM 57-3 0-4. FABRICATED REPAIR PER SRM 57-30-04 PAGE 29. TREATED PRIMED AND INSTALLED PER SRM 51-10-2 AND 57-30-04 PAGE 27. 2 L 7 3 4F A3WE 1999050700475 19990507 00475 NM 1999 5 7 CALA9900479 1 19990504 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 FORWARD CARGO COMPARTMENT OVERHEAD FLOOR BEAM SUPPORT SIDE BRACE BETWEEN STA 720 - 720A CRACKED IN THREE PLACES. REMOVE D AND FABRICATED NEW ANGLE, TREATED PRIMED AND INSTALLED ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999050700476 19990507 00476 NM 1999 5 7 CALA9900480 1 19990504 A 5754 MOUNT BOEING 727 727224 1384076 NM NR 6 FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 OUTBOARD BRACKET HAS .25 VISIBLE CRACK AT LOWER CORNER WHERE NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. REPAIRED BRACKET P ER SRM 51-30-2 AND 51-20-1. 2 L 7 3 4F A3WE 1999050700477 19990507 00477 NM 1999 5 7 CALA9900481 1 19990504 A 5753 DOUBLER BOEING 727 727224 1384076 NM LT TE FLAP CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 LEFT OUTBOARD FLAP AFT SEGMENT UPPER L/E HAS CHAFED AREA AT DOUBLER 24 FROM OUTBOARD END. REMOVED PREVIOUS REPAIR. FAB RICATED, TREATED, PRIMED, AND INSTALLED REPAIR PER SRM 57-50-4, 51-10-2, 57-51-4, AND 51-30-2. 2 L 7 3 4F A3WE 1999050700478 19990507 00478 NM 1999 5 7 CALA9900482 1 19990504 A 5531 SPAR BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 VERTICAL STAB UPPER RIGHT LEADING EDGE SPAR CRACKED (.25) AROUND RIVET AT STIFFENER PLATE JUST BELOW TENSION TIE FORWARD ATTACH BOLT. REMOVED FASTENERS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 55-30-6 AND 51-1-20. 2 L 7 3 4F A3WE 1999050700479 19990507 00479 NM 1999 5 7 CALA9900483 1 19990504 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 400 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 FLOORBEAM CORRODED AT SCREW HOLE FS 400 RBL 35. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS, PICKED UP HOLES, TRE ATED, PRIMED, AND INSTALLED REPAIR PER SRM 51-10-6 AND 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1999050700480 19990507 00480 WP 1999 5 7 CALA9900484 1 19990504 A 5347 593054765 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 RIGHT CENTER SEAT TRACK CORRODED STA 200 AND 237. REMOVED AND REPLACED SEAT TRACK STA 200 - 247 PER SRM 51-30-1. 2 L 7 2 4F A6WE 1999050700481 19990507 00481 NM 1999 5 7 CALA9900485 1 19990504 A 5753 RIB BOEING 727 727224 1384076 NM LT TE MID FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 RIGHT OUTBOARD MID FLAP HAS .5 CRACK AT INBOARD MOST RIB LOWER END. INSTALLED DOUBLER AT RIB LOWER END OF MID FLAP PER SRM 51-40-3. 2 L 7 3 4F A3WE 1999050700482 19990507 00482 NM 1999 5 7 CALA9900486 1 19990504 A 5753 SKIN BOEING 727 727224 1384076 NM NR 4 LE SLAT CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 LEFT WING NR 4 SLAT LOWER TRAILING EDGE UPPER SURFACE CHAFED INBOARD TO OUTBOARD END. BURNISHED AREA. FOUND OUT OF LIM ITS. FABRICATED, TREATED, PRIMED, AND INSTALLED DOUBLER PER SRM 57-50-3 PABE 2B. 2 L 7 3 4F A3WE 1999050700483 19990507 00483 WP 1999 5 7 CALA9900487 1 19990505 A 5347 5930566 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1105 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 LEFT MOST INBOARD SET TRACK HAS CORROSION AT CENTER CHANNEL STA 1105. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FRO M STA 1041 - 1309. 2 L 7 2 4F A6WE 1999050700484 19990507 00484 NM 1999 5 7 9901636729 1 19990429 A 2910 LINE BOEING 747 747251F 1384898 NM NR 1 HYD SYST LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 GL 01 629US 22388 THE NR 1 HYDRAULIC SYSTEM LOST FLUID EN ROUTE FROM TPE-NRT. AIRCRAFT CONTINUED TO NRT, LANDED WITHOUT INCIDENT, AND WAS TOWED INTO THE GATE. RETIGHTENED THE HYDRAULIC PRESSURE LINE FOR THE LEFT BODY LANDING GEAR TRUCK POSITION ACTUATOR. O PERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999050700485 19990507 00485 WP 1999 5 7 9901641238 1 19990429 A 3350 BATTERY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 238NW 48267 DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD EMERGENCY LIGHT BATTERY AND POWER SUPPL Y. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999050700486 19990507 00486 1999 5 7 COMA9910070 2 19990502 A 7532 3038004 VALVE EMB 120 EMB120RT SO LT ENGINE MALFUNCTIONED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 269CA 120263 SMOKE IN COCKPIT COMING FROM AIRCRAFT VENTS. REPLACED THE LEFT ENGINE 2.5 SWITCHING VALVE. 2 L 7 2 4T RT A31SO 1999050700487 19990507 00487 EA 1999 5 7 COMA9960179 1 19990502 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 708CA 988 520 7235 FLAP CAUTION MESSAGE. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999050700488 19990507 00488 NM 1999 5 7 UPS99229481 1 19990429 A 5754 6917900 BRACKET BOEING 727 72725C 138400H NM NR 8 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, NR 8 SLAT ATTACHMENT BRACKET AT I/B TRACK CRACKED. REPLACED BRACKET PER OHM 20-50-01. 2 L 7 3 4F A3WE 1999050700489 19990507 00489 NM 1999 5 7 UPS99229482 1 19990429 A 5754 651727614 RIB BOEING 727 72725C 138400H NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, NR 4 SLAT RIB CRACKED AT ACTUATOR ROD END BOLT O/B SIDE. REPLACED RIB PER SRM 51-30-5. 2 L 7 3 4F A3WE 1999050700490 19990507 00490 NM 1999 5 7 UPS99229483 1 19990429 A 5754 6516222 SKIN BOEING 727 72725C 138400H NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACK RUNNING FROM NR 6 SLAT O/B GUIDE HOOK MOUNT HOLE TO O/B RIVET HOLE. REMOVED AND REPLACED NR 6 SLAT PER MM 27-81-11. 2 L 7 3 4F A3WE 1999050700491 19990507 00491 NM 1999 5 7 UPS99229484 1 19990429 A 5754 BRACKET BOEING 727 72725C 138400H NM NR 6 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE:SI, CRACKED NR 6 K-FLAP ACTUATOR I/B MOUNT BRACKET, LWR FWD RADIUS. FABRICATED AND REPLACED MOUNT BRACK ET PER SRM 51-20-1. 2 L 7 3 4F A3WE 1999050700492 19990507 00492 WP 1999 5 7 UPS99829480 1 19990504 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 EMERGENCY EXIT LIGHTING INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTING BATT PACK. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999050700493 19990507 00493 WP 1999 5 7 UPS99829485 1 19990426 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT WING L/E RIBS AT XFS 566.25, 855.0, 885.0, 878.75, 829.75, 816.25 803.75, 785.0, 766.25, 747.5, 7 28.75, 722.5, AND 716.25 ARE CRACKED. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700494 19990507 00494 WP 1999 5 7 UPS99829486 1 19990420 A 5320 37584982 FITTING DOUG DC8 DC873F 302199F WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, INTERCOSTAL AT LONG 35R ATTACH FITTING IS CRACKED AT FS 1240. REMOVED, AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999050700495 19990507 00495 WP 1999 5 7 UPS99829487 1 19990418 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT WING L/E UPPER SKIN AT XFS 710.0 IS CRACKED AT 1 SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED I AW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999050700496 19990507 00496 WP 1999 5 7 UPS99829488 1 19990425 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1446 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, FS 1446 FRAME AT LONG 34R IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 13. 2 L 7 4 4F RT 4A25 1999050700497 19990507 00497 WP 1999 5 7 UPS99829489 1 19990421 A 5320 3755854502 FITTING DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, FS 1180, THE 'C' PIT DOOR FRAME FWD STOP FITTING IS CRACKED AT LONG 26L. REMOVED AND REPLACED THE F ITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999050700498 19990507 00498 WP 1999 5 7 UPS99829490 1 19990427 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 467.323 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT WING L/E RIB AT XS 467.323 IS CRACKED AT THE AFT LWR END. STOP DRILLED, AND REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700499 19990507 00499 WP 1999 5 7 UPS99829491 1 19990419 A 5753 4649592 FITTING DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, THE RT STA 410 FLAP CANOE FITTING, OTBD SIDE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING I AW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999050700500 19990507 00500 WP 1999 5 7 UPS99829492 1 19990421 A 5510 SKIN DOUG DC8 DC873F 302199F WP RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT HORIZ STAB OTBD L/E, INBD FWD SECTION, STA. XFS 210, HAS BULGING CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 55-2-1, FIG 4. 2 L 7 4 4F RT 4A25 1999050700501 19990507 00501 WP 1999 5 7 UPS99829493 1 19990418 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT WING L/E LWR SKIN AT XFS 710 IS CRACKED AT 1 FASTENER HOLE. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 57-2-0 FIG 24. 2 L 7 4 4F RT 4A25 1999050700502 19990507 00502 WP 1999 5 7 UPS99829494 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 641.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 641.25 IS CRACKED AT THE AFT UPPER FASTENER STOP DRILLED AND REPAIRED IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700503 19990507 00503 WP 1999 5 7 UPS99829495 1 19990418 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E UPPER SKIN AT XFS 660 IS CRACKED AT 1 FASTENER. CUT OUT DAMAGED AREA AND REPAIRED IAW S RM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999050700504 19990507 00504 WP 1999 5 7 UPS99829496 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700505 19990507 00505 WP 1999 5 7 UPS99829497 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 622.5 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700506 19990507 00506 WP 1999 5 7 UPS99829498 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 628.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700507 19990507 00507 WP 1999 5 7 UPS99829499 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 628.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700508 19990507 00508 WP 1999 5 7 UPS99829500 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 635.0 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999050700509 19990507 00509 WP 1999 5 7 UPS99829501 1 19990418 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 370-530 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, FS 370 TO 530, RBL 60, LWR FLANGE IS CORRODED BEYOND LIMITS. REMOVED SEAT TRA CK FROM FS 370 TO 530, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999050700510 19990507 00510 WP 1999 5 7 UPS99829502 1 19990405 A 5347 601517670T6 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, HEAVY CORROSION AROUND SEAT TRACK PLUG AT FS 500, RBL 48. REMOVED DAMAGED SEAT TRACK FROM FS 450 TO 727. FABRICATED, AND INSTALLED SEAT TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999050700511 19990507 00511 WP 1999 5 7 UPS99829503 1 19990423 A 5313 S2594747 LONGERON DOUG DC8 DC873F 302199F WP BS 540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, LONG 18L AT FS 540 IS CRACKED. REMOVED DAMAGED SECTION, FABRICATED, AND REPLACED LONGERON IAW SRM 5 3-2-2. 2 L 7 4 4F RT 4A25 1999050700512 19990507 00512 WP 1999 5 7 UPS99829504 1 19990417 A 5320 4888754502 FITTING DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, MAIN CABIN SUPPORT FITTING AT FS 55, RBL 48, FWD OTBD IS CRACKED. REMOVED AND REPLACED FITTING EAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999050700513 19990507 00513 WP 1999 5 7 UPS99829505 1 19990423 A 5320 4888756501 FITTING DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 SUPPORT FITTING AT FS 55, LBL 48 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1- 21. 2 L 7 4 4F RT 4A25 1999050700514 19990507 00514 WP 1999 5 7 UPS99829506 1 19990416 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1260-1280 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, REPAIR FUSELAGE SKIN AT LONG 31R BETWEEN FS 1260 AND 1280 IAW DH SK 840-431. COMPLIED WITH DH SK 84 0-431. 2 L 7 4 4F RT 4A25 1999050700515 19990507 00515 WP 1999 5 7 UPS99829507 1 19990407 A 5347 37552221 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 789 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 798 AT RBL 24, THE FRAME IS CRACKED AT THE SEAT TRACK ATTACH POINT. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999050700516 19990507 00516 EU 1999 5 7 QXEA9900905 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT INBOARD SEAT TRACK FROM FRAME 14285 TO FRAME 15635, REQUIRES REPLACEMENT DUE TO IT BEING WORN OUT OF LIMITS. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999050700517 19990507 00517 EU 1999 5 7 QXEA9900906 1 19990414 A 5210 HINGE FOKKER F28 F28MK4000 4990810 EU PASSENGER DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - MAIN CABIN DOOR HINGE 3RD, 4TH, 5TH AND CENTER LUG HAVE GOUGE MARKS. REPAIRED IAW HORIZON AIR EA 4-53-757. 2 L 7 2 4F RT A20EU 1999050700518 19990507 00518 EU 1999 5 7 QXEA9900907 1 19990326 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PASSENGER DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A SCREW THREAD IMPRESSION ON MAIN CABIN DOOR SKIN FORWARD OF HINGE POINT. REPAIRED IAW FOKKER SRM 52-01- 01, PAGE 3, PARAGRAPH 3D AND E. 2 L 7 2 4F RT A20EU 1999050700519 19990507 00519 EU 1999 5 7 QXEA9900908 1 19990326 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 3050 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CRACKED CLIP AT FRAME 3050 AND STRINGER 58. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999050700520 19990507 00520 EU 1999 5 7 QXEA9900909 1 19990327 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FRAME 3450-3820 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FLOORBEAM BL1127R WL-560 FROM FRAME 3450 TO FRAME 3820 IS CRACKED IN TWO SPOTS. REPAIRED IAW FOKKER SRM 53-01-01 (3)(A) AND SRM 53-02-01, FIGURE 5. 2 L 7 2 4F RT A20EU 1999050700521 19990507 00521 EU 1999 5 7 QXEA9900910 1 19990329 A 5320 TIE FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - TWO CRACKS IN FLOORBEAM TIES BL600R WL-560 AT FRAME 4610. REPAIRED IAW FOKKER SRM 53-01-01 (3)(A). 2 L 7 2 4F RT A20EU 1999050700522 19990507 00522 EU 1999 5 7 QXEA9900911 1 19990423 A 5210 HOOK FOKKER F28 F28MK4000 4990810 EU PASSENGER DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - MAIN CABIN DOOR HOOKS HAVE 2MM PLAY BETWEEN HOOK AND ACTUATING HANDLE, AFT HOOK HAS PLAY AT LINK. REPAIRED IAW FO KKER MM 52-10-4, PAGE 410, PARAGRAPH 7C, 1-5. 2 L 7 2 4F RT A20EU 1999050700523 19990507 00523 EU 1999 5 7 QXEA9900913 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L HAS TWO LONGITUDINAL WEAR MARKS INSIDE CHANNEL FROM FRAME 6305-5805. REPAIRED IA W FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700524 19990507 00524 EU 1999 5 7 QXEA9900914 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L HAS LONGITUDINAL WEAR MARKS INSIDE CHANNEL AT FRAME 6805 AND RUNNING 10 AFT. REP AIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700525 19990507 00525 EU 1999 5 7 QXEA9900915 1 19990323 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L HAS 3 SEAT PEG HOLES 5 FORWARD OF FRAME 7305 HAVE GOUGES INSIDE BORE AND TOP OF T RACK. REPAIRED IAW FOKKER MM 53-40-01, PAGE 202, PARAGRAPH 4B, STEP 5. 2 L 7 2 4F RT A20EU 1999050700526 19990507 00526 EU 1999 5 7 QXEA9900916 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L HAS LONGITUDINAL WEAR MARKS INSIDE CHANNEL, 5 FORWARD AND 5 AFT OF FRAME 7805. R EPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700527 19990507 00527 EU 1999 5 7 QXEA9900917 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT SEAT TRACK BL1127L, WEAR MARKS INSIDE CHANNEL AND GOUGES AROUND SEAT PEG HOLES, 6 AFT OF FRAME 8305. REPAIRE D IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700528 19990507 00528 EU 1999 5 7 QXEA9900918 1 19990318 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT OUTBOARD SEAT TRACK BL1127L, HAS 2 LONGITUDINAL WEAR MARKS INSIDE CHANNEL AT FRAME 9305B AND RUNNING 11 FORWA RD. REPAIRED IAW FOKKER MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999050700529 19990507 00529 EU 1999 5 7 QXEA9900919 1 19990421 A 2150 INLET FOKKER F28 F28MK4000 4990810 EU RT ACM CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT ACM INLET HAS A CRACK APPROXIMATELY 3.5 INCHES LONG. REPAIRED IAW HORIZON AIR EA 4-53-790. 2 L 7 2 4F RT A20EU 1999050700530 19990507 00530 EU 1999 5 7 QXEA9900920 1 19990412 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 9305B HAS CORROSION UNDER NUT PLATE BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 3, PAGE 9, SRM 51-31-01, 51-31-05, 51-31-02 AND HORIZON AIR EA 4-53-748. 2 L 7 2 4F RT A20EU 1999050700531 19990507 00531 EU 1999 5 7 QXEA9900921 1 19990328 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FORWARD CARGO BAY FRAME 7305 BETWEEN STRINGERS 74 AND 1 HAS CORRODED CASTELLATION. REPAIRED IAW SRM 53-02-13, PAG E 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999050700532 19990507 00532 EU 1999 5 7 QXEA9900922 1 19990410 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LOWER BELLY SKIN MOUNT SURFACE FOR LOWER ATC ANTENNA HAS CORROSION PITTING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND SRM 53-01-01, PAGE 6, PARAGRAPH B2. 2 L 7 2 4F RT A20EU 1999050700533 19990507 00533 EU 1999 5 7 QXEA9900923 1 19990416 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FUSELAGE BELLY SKIN MOUNT SURFACE FOR NR 2 DME ANTENNA HAS CORROSION PITTING. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999050700534 19990507 00534 EU 1999 5 7 QXEA9900924 1 19990331 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISINSTALLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - SKIN ATTACH CLIP ON RIGHT SIDE OF HORIZONTAL BEAM I HAS MS20470AD6 RIVETS INSTALLED WHERE IT ATTACHES TO BEAM. RE PAIRED IAW HORIZON AIR EA 4-53-750. 2 L 7 2 4F RT A20EU 1999050700535 19990507 00535 EU 1999 5 7 QXEA9900925 1 19990414 A 5320 CONSOLE FOKKER F28 F28MK4000 4990810 EU COCKPIT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - UPPER CONSOLE AT 425L HAS TOOLING DAMAGE AT LOWER OUTBOARD DUCT. REPAIRED IAW HORIZON AIR EA 4-53-765. 2 L 7 2 4F RT A20EU 1999050700536 19990507 00536 EU 1999 5 7 QXEA9900926 1 19990327 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FORWARD CARGO BAY FLOOR FRAME 8305 HAS EXFOLIATION CORROSION UNDER FRAME TOP ANGLE AND UNDER NUT PLATE, ABOVE STRI NGER 74. REPAIRED IAW HORIZON AIR EA 4-53-739. 2 L 7 2 4F RT A20EU 1999050700537 19990507 00537 EU 1999 5 7 QXEA9900927 1 19990322 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - AFT CARGO PIT FRAME 13815A HAS SURFACE CORROSION, TOP FLANGE, TOP AND BOTTOM SIDE AT STRINGER 74, WHERE FOUR WAY F LOOR SUPPORT ATTACHES TO FRAME. REPAIRED IAW CORROSION PREVENTION AND CONTROL MANUAL CHAPTER 5, PAGE 51, FIGURE 2. 2 L 7 2 4F RT A20EU 1999050700538 19990507 00538 EU 1999 5 7 QXEA9900928 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CLIP ON EXTERIOR FRAME AT 13815B IS CRACKED AT INBOARD LEFT END. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999050700539 19990507 00539 EU 1999 5 7 QXEA9900929 1 19990317 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CLIP ON EXTERIOR FRAME AT 13815B IS CRACKED AT INBOARD RIGHT END. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999050700540 19990507 00540 EU 1999 5 7 QXEA9900930 1 19990322 A 5312 BULKHEAD WEB FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - 2 CRACK ON REAR PRESSURE BULK HEAD, JUST ABOVE HORIZONTAL BEAM. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 13. 2 L 7 2 4F RT A20EU 1999050700541 19990507 00541 EU 1999 5 7 QXEA9900931 1 19990317 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - ANGLE CRACKED FORWARD SIDE OF FRAME 14755 ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-04. 2 L 7 2 4F RT A20EU 1999050700542 19990507 00542 EU 1999 5 7 QXEA9900932 1 19990319 A 2750 BEARINGS FOKKER F28 F28MK4000 4990810 EU LT TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT MAIN LANDING GEAR WHEEL WELL FLAP TORQUE TUBE JUST INBOARD OF FLAP HYDRAULIC MOTOR, BOTH INBOARD AND OUTBOARD BEARINGS ON TORQUE TUBE HAVE AXIAL PLAY. REPAIRED IAW FOKKER MM 27-51-04, PAGE 201-202. 2 L 7 2 4F RT A20EU 1999050700543 19990507 00543 EU 1999 5 7 QXEA9900933 1 19990402 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT MAIN LANDING GEAR WHEEL WELL HAS A CRACK AT FRAME 13345 INBOARD LOWER CORNER. REPAIRED IAW HORIZON AIR EA 4- 53-730. 2 L 7 2 4F RT A20EU 1999050700544 19990507 00544 EU 1999 5 7 QXEA9900934 1 19990401 A 5320 WINDOW FRAME FOKKER F28 F28MK4000 4990810 EU RT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT COCKPIT D WINDOW FRAME HAS CRACK AT TOP ROW, THIRD ATTACH HOLE FROM FORWARD END. REPAIRED IAW SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999050700545 19990507 00545 EU 1999 5 7 QXEA9900935 1 19990401 A 5320 WINDOW FRAME FOKKER F28 F28MK4000 4990810 EU LT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT COCKPIT D WINDOW FRAME HAS CRACK AT TOP ROW, THIRD ATTACH HOLE FROM FORWARD END. REMOVED AND REPLACED INNER FRAME IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999050700546 19990507 00546 EU 1999 5 7 QXEA9900936 1 19990401 A 5320 WINDOW FRAME FOKKER F28 F28MK4000 4990810 EU LT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT COCKPIT D WINDOW FRAME INNER LAYER HAS CRACK AT 12 O'CLOCK POSITION SHIM TACK RIVET. REPLACED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999050700547 19990507 00547 EU 1999 5 7 QXEA9900937 1 19990326 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU INSTRUMENT PANEL CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - INSTRUMENT PANEL SUPPORT FRAME IN BACK OF PANEL 12C OPENING IS HEAVILY CHAFFED. REPAIRED IAW HORIZON AIR EA 4-53- 744. 2 L 7 2 4F RT A20EU 1999050700548 19990507 00548 EU 1999 5 7 QXEA9900938 1 19990321 A 5320 POST FOKKER F28 F28MK4000 4990810 EU RT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACK IN THE COCKPIT RIGHT NR 2 WINDOW POST LOWER ATTACHMENT FLANGE AREA. REPAIRED IAW FOKKER SRM 51-3 1-01 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999050700549 19990507 00549 EU 1999 5 7 QXEA9900939 1 19990320 A 5320 POST FOKKER F28 F28MK4000 4990810 EU LT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACK IN THE COCKPIT LEFT NR 2 WINDOW POST LOWER ATTACHMENT FLANGE AREA. REPAIRED IAW FOKKER SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1999050700550 19990507 00550 NM 1999 5 7 99UAL900163 1 19990316 A 2530 GALLEY MODULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT GALLEY LOOSE A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 7283U 21561 AFT GALLEY AFT UNIT CAME ON FLOOR BLOCKING DOOR NR 2 RIGHT. MAINTENANCE SECURED UNIT. FLEET ENGINEERING WILL FORWARD T HIS ITEM TO THE APPROPRIATE CATERING VENDOR AND RECOMMEND A LATCH AND PULL TEST BE PART OF THEIR INSTALLATION TRAINING P ROCEDURE. 2 L 7 3 4F 4 F A3WE E2EA 1999050700551 19990507 00551 NM 1999 5 7 99UAL900231 1 19990423 A 5523 SA414A4 BEARING BOEING 65C26384 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ELEV TAB HINGE WORN A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 342UA 3189 24246 SIGNIFICANT AIRFRAME VIBRATION FELT IN CONTROLS, FLOOR, AND GLARESHIELD. *S/D* THE VIBRATION WAS CAUSED BY A WORN BEAR ING AND BUSHINGS ON THE LEFT HAND ELEVATOR TAB INBOARD HINGE. THE WORN PARTS WERE REPLACED. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999050700552 19990507 00552 1999 5 7 99UAL900232 4 19990425 A 3417 ADC HONEYWELL 4061100901 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 FAILED A UALA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 WP 29 956UA 93051515 26704 ALL ALTIMETERS AND AIRSPEED INDICATORS DISAGREE IN FLIGHT. *S/D* FAULTY AIR DATA COMPUTER. THE NR 2 AIR DATA COMPUTER WAS REPLACED, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999050700553 19990507 00553 NM 1999 5 7 99UAL900233 1 19990423 A 2150 3964421 VALVE HAMILTON STA 7110035 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT PACK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 955UA 17499 10658 FK45030 26703 AIRCRAFT HAD AN UNCONTROLLED LOSS OF PRESSURE IN AUTO. THE OXYGEN MASKS WERE NOT DEPLOYED. *S/D* AFTER EXTENSIVE TROU BLESHOOTING, FOUND DELTA P MODULE LOOSE AT MOUNTING BRACKET, RIGHT HAND PACK VALVE BIASED TO THE CLOSED POSITION, AND LO W RESISTANCE TO THE AFT OUTFLOW VALVE. REPLACED AND SECURED THE DELTA P MODULE, RIGHT PACK VALVE, AND THE AFT OUTFLOW V ALVE. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999050700554 19990507 00554 NE 1999 5 7 99UAL900234 2 19990424 A 7321 MEC WOODWARD GOV MR7320479 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 344UA 60525 24248 722283 NR 2 ENGINE SURGED. *S/D* ACCOMPLISHED MM TROUBLESHOOTING AND REPLACED MAIN ENGINE CONTROL UNIT (MEC). AIRCRAFT RETUR NED TO SERVICE AND NO FURTHER DISCREPANCIES NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999050700555 19990507 00555 EU 1999 5 7 99UAL900235 1 19990424 A 2560 LANYARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT SERVICE DOOR DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 AFT RIGHT DOOR LIFE RAFT LANYARD NEEDS TO BE RESTOWED. IT IS INHIBITING ARMING THE DOOR. LANYARD WAS PULLED FROM ITS A TTACHMENT POINT ON THE GIRT BAR TRIGGER BY A F/A. MAINTENANCE SUBSEQUENTLY REATTACHED THE LANYARD TO ITS PROPER LOCATIO N ON THE GIRT BAR TRIGGER. 2 L 7 2 4F 4 F RT A28NM E40NE 1999050700556 19990507 00556 1999 5 7 99UAL900236 4 19990408 A 2210 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE YAW DAMPER FAILED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 414UA 472 HYDRAULIC FLUID LEAKING LT EMPENNAGE SECTION, APPEARS TO BE COMING FROM RUDDER. *S/D* YAW DAMPER SERVO ACTUATOR LEAKIN G. ACTUATOR WAS REPLACED BY IMC ON 4/26/99 AND CORRECTED THE PROBLEM. 2 L 7 2 4F 4 F RT A28NM E40NE 1999050700557 19990507 00557 NM 1999 5 7 99UAL900237 1 19990422 A 5312 69414171 BLKHD FASTENERS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 1016 LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 354UA 31400 24360 WATER LEAK AT PRESSURE BULKHEAD ABOVE APU GENERATOR FEED CABLES. *S/D* UPON INSPECTION AND DISASSEMBLY IT WAS FOUND TH AT THE HI-LOKS ATTACHING THE AFT END OF STRINGER 2A RIGHT TO THE BS 1016 FRAME SUPPORT STRUCTURE (69-41417-1) WERE ATTAC HED WITH SELF LOCKING NUTS AND WERE LOOSE. THE FITTING WAS INSPECTED AND REASSEMBLED WITH HI-LOK COLLARS AND RETURNED T O SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999050700558 19990507 00558 1999 5 7 99UAL900238 4 19990425 A 3417 HG480B3 ADC BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E & E COMPT FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 7289U 21567 ALL INSTRUMENT FLAGS ASSOCIATED WITH CADC IN VIEW, CAPTAINS ALTIMETER, ALTITUDE ALERT, GPWS FALL, WINDSHEAR INOPERATIVE, TAS OFF. RETURNED TO ORD. *S/D* REPLACED NR 1 CENTRAL AIR DATA COMPUTER. 2 L 7 3 4F 4 F A3WE E2EA 1999050700559 19990507 00559 NM 1999 5 7 99UAL900239 1 19990424 A 3510 198201 VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE COCKPIT DEFECTIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 205UA 28714 EN ROUTE CDG-SFO, FLIGHT CREW OXYGEN PRESSURE DECLINING AT RATE OF 20 PSI PER MINUTE. FLIGHT DIVERTED TO KEF. *S/D* O N ACCOMPLISHMENT OF LEAK CHECK, FOUND OXYGEN BLEED VALVE, (P/N 19820-1), LEAKING OUT AT THE EXHAUST PORT. VALVE WAS REP LACED WITH A NEW VALVE AND LEAK CHECK ACCOMPLISHED. NO FURTHER LEAKS WERE NOTED. VALVE SENT TO VENDOR FOR FAILURE ANAL YSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999050700560 19990507 00560 NM 1999 5 7 99UAL900240 1 19990425 A 2120 AIR DIST BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN ODOR A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 613UA 21874 ON CLIMBOUT, FLIGHT ATTENDANTS REPORTED SMOKE OF AN ELECTRICAL NATURE COMING FROM THE TOP OF ALL GALLEYS. PERFORMED APP ROPRIATE COCKPIT CHECKLISTS REMOVING POWER FROM UTILITY BUSES, SMOKE DISSIPATED. SMOKE SMELL RETURNED ON DESCENT. NO SMELL NOTICED ON GROUND. *S/D* UPON ARRIVAL, MECHANICS RAN ALL ELECTRICAL SYSTEMS AND ACCOMPLISHED EXTENSIVE PHYSICAL CHECKS IN THE AREA. PROBLEM WAS NOT DUPLICATED. NO FAULTS WERE FOUND. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER IN CIDENT. 2 L 7 2 4F 4 F RT A1NM E3NE 1999050700561 19990507 00561 NM 1999 5 7 99UAL900241 1 19990426 A 2150 DUCT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 9 LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 7270U 21417 EMERGENCY EXIT LIGHT IN OVERHEAD FRONT PART OF COACH CABIN HAS WATER INSIDE. REMOVED CEILING PANELS AT ROW 9. FOUND WA TER COMING FROM AIR CONDITIONING DUCTS. RAN PACKS AT FULL HOT TO DRY DUCTS. REPLACED EMERGENCY LIGHT AND CEILING PANEL S. 2 L 7 3 4F 4 F A3WE E2EA 1999050700562 19990507 00562 NM 1999 5 7 99UAL900242 1 19990426 A 2781 31EN946 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE SLAT FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 530UA 25043 LANDED ORD UNDER AMBER ALERT DUE TO L/E SLAT ASYMMETRY. *S/D* FAILURE OF ONE OF THE TWO INBOARD SLAT LOSS INDICATION S WITCHES CAUSED THE SYSTEM SHUTDOWN. REPLACED THE BAD SWITCH AND RETURNED AIRCRAFT TO SERVICE WITHOUR FURTHER INCIDENT. THIS IS A KNOWN INDUSTRY PROBLEM WITH THE 757 AIRCRAFT. UNITED IS CORRECTING THE PROBLEM DURING HEAVY MAINTENANCE VISI TS. 2 L 7 2 4F 4 F RT A2NM E17NE 1999050700563 19990507 00563 WP 1999 5 7 99UAL900243 1 19990427 A 2560 BATTERY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL 4R DOOR DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 1847U 48263 FOUR RIGHT EVACUATION SLIDE-RAFT REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM INOP. LIGHT LENS DAMAGED. *S/D* SYST EM INOP DUE TO DEAD BATTERIES. BATTERIES REPLACED AND SYSTEMS OPERATIONS CHECK - OK. 2 L 7 3 4F 4 F A22WE E23EA 1999050700564 19990507 00564 NE 1999 5 7 99UAL900244 2 19990427 A 7200 ENGINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 2 MALFUNCTIONED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 163UA 21353 685696 OIL SMELL PERMEATED THE ENTIRE CABIN AND COCKPIT DURING DESCENT. *S/D* FOUND OIL RESIDUE ON NR 1 ACM. REPLACED ACM, N O OIL LEAKS FOUND. INVESTIGATION REVEALED ACM INGESTED FOD, NO DAMAGE FOUND, THE OIL SEALS WERE INTACT. A 2ND ACM WAS REMOVED, DISASSEMBLED AND TESTED, NO LEAKS FOUND. ACM'S WERE NOT THE CAUSE OF THE SMELL. NR 2 MAIN ENGINE WAS REPLACED ON 5/2. AFTER THE REPLACEMENT OF 2 ACMS, 2 PACK BURNOUTS, SMELL STILL EXISTED. AFTER NR 2 ENGINE REPLACEMENT THE OIL SMELL DISAPPEARED. THE NR 2 ENGINE WAS LIKELY THE CAUSE OF THE OIL SMELL. 2 L 7 4 4F 4 F A20WE E20EA 1999050700565 19990507 00565 EU 1999 5 7 99UAL900245 1 19990429 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 411UA 464 CABIN EMERGENCY SYSTEM TEST FAIL. *S/D* BAD BATTERY WAS FOUND ON LEFT OVERWING POWER SUPPLY UNIT. BATTERY WAS REPLACE D. 2 L 7 2 4F 4 F RT A28NM E40NE 1999050700566 19990507 00566 NM 1999 5 7 99UAL900246 1 19990429 A 7933 1122514 TEMP SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 361UA 24454 724382 NR 2 ENGINE OIL TEMPERATURE INDICATION WAS FLUCTUATING FROM 100 DEGREES UP INTO THE RED BAND INTERMITTENTLY. ALL OTHER ENGINE PARAMETERS WERE NORMAL. *S/D* ACCOMPLISHED MM TROUBLESHOOTING. REPLACED TEMP BULB PER MM 79-34-01. ENGINE LEA K CHECK ACCOMPLISHED AND AIRCRAFT RETURNED TO SERVICE. NO FURTHER DISCREPANCIES. 2 L 7 2 4F 4 F RT A16WE E2GL 1999050700567 19990507 00567 NE 1999 5 7 99UAL900247 2 19990428 A 7314 FUEL PUMP ARGOTECH 7313635 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 WP 29 7259U 6889 21406 700251 NR 1 ENGINE FLAMED OUT ON TUS TAKEOFF ROLL AT 90 KNOTS. ABORTED TAKEOFF. *S/D* THE FLAME-OUT WAS CAUSE BY THE FUEL PU MP SPLINE DRIVE SHAFT EXCESSIVE WEAR. THE FUEL PUMP AND FUEL CONTROL UNIT WERE REPLACED BEFORE THE AIRCRAFT WENT BACK T O SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1999050700568 19990507 00568 NM 1999 5 7 99UAL900248 1 19990429 A 2781 H1010272U1 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 LE SLAT FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7256U 21403 LEADING EDGE FLAPS AMBER LIGHT ON AT P2 PANEL AND NR 5 LEADING EDGE SLAT AMBER LIGHT WAS ON AT SECOND OFFICERS PANEL WIT H FLAPS UP. RETURNED TO MIA. *S/D* REPLACED NR 4 LEADING EDGE SLAT EXTEND SWITCH, SYSTEM OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1999050700569 19990507 00569 NM 1999 5 7 99UAL900249 1 19990430 A 5310 STRUCTURE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BS 1270 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 602UA 21863 CORROSION DAMAGE-AFT CARGO AREA. *S/D* AFT CARGO PIT AREA, STRINGERS 34L AND 37L HAVE SEVERAL AREAS OF CORROSION. CAR GO DOOR CUTOUT FAIL-SAFE STRAP AT STA 1270 HAD SURFACE CORROSION, BETWEEN 44 RBL TO 36 RBL. CARGO DOOR CUTOUT, DOOR SIL L INNER CHORD HAS SURFACE CORROSION AT VARIOUS LOCATIONS FROM STA 1278 TO 1303. ALL CORROSION WAS FOUND AT A C15 VISIT FROM NON-ROUTINE WRITE-UPS. CORROSION IS LEVEL 2 ENVIROMENTAL CORROSION. ALL CORROSION WAS REMOVED AND REPAIRS EFFECTE D BY UAL ENGINEERING VARIATION AUTORITY (EVA). 2 L 7 2 4F 4 F RT A1NM E3NE 1999050700570 19990507 00570 WP 1999 5 7 ABXA9900333 1 19990316 A 5512 56443301 SKIN DOUG DOUG DC8 DC863 302198A WP RT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 RIGHT HORIZONTAL STABILIZER LEADING EDGE AT STATION XFS 147.5 HAD INTERGRANULAR CORROSION. REPAIRED IAW DC8 SRM 55-2-1. 2 L 7 4 4F 4A25 1999050700571 19990507 00571 WP 1999 5 7 ABXA9900334 1 19990317 A 5712 5769859 RIB DOUG DOUG DC8 DC863 302198A WP WS 227.335 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 RIGHT WING LEADING EDGE RIB AT STATION XS 227.335 CRACKED AT AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999050700572 19990507 00572 WP 1999 5 7 ABXA9900335 1 19990326 A 5320 37502571N FITTING DOUG DOUG DC8 DC863 302198A WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LOWER FORWARD CARGO COMPARTMENT, STATION 440-460, LONGERON 31 LEFT SPLICE CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999050700573 19990507 00573 WP 1999 5 7 ABXA9900336 1 19990313 A 5712 5789470 RIB DOUG DOUG DC8 DC863 302198A WP WS 735 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LEFT WING LEADING EDGE UPPER RIB CRACKED AT FASTENER EDGE AT STATION XFS 735. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999050700574 19990507 00574 WP 1999 5 7 ABXA9900337 1 19990313 A 5712 769471 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LEFT WING LEADING EDGE LOWER RIB CRACKED AT FASTENER END, FORWARD OF PANEL 518B, AT STATION XFS 772.5. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999050700575 19990507 00575 WP 1999 5 7 ABXA9900338 1 19990317 A 5720 5769859 ANGLE DOUG DOUG DC8 DC863 302198A WP WS 250.084 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 RIGHT WING LEADING EDGE, INBOARD OF STATION XS 250.084 RIB AT THE AFT SIDE OF THE SLOT, VERTICAL ANGLE IS CRACKED. REPL ACED VERTICAL ANGLE IAW DRAWING 5769859 AND DC8 SRM 57-3-3 AND 51-1-20D. 2 L 7 4 4F 4A25 1999050700576 19990507 00576 WP 1999 5 7 ABXA9900339 1 19990317 A 5320 37502571 FITTING DOUG DOUG DC8 DC863 302198A WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 STRINGER 31 LEFT SPLICE FITTING CRACKED BETWEEN STATIONS 600 AND 620. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999050700577 19990507 00577 WP 1999 5 7 ABXA9900340 1 19990316 A 5720 3704841501 FITTING DOUG DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 NR 2 MAIN TANK, INBOARD OF XRS 74 BULKHEAD, FORWARD STRINGER 51, END FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1 -20D. 2 L 7 4 4F 4A25 1999050700578 19990507 00578 WP 1999 5 7 ABXA9900341 1 19990315 A 5320 3754473501N SPLICE DOUG DOUG DC8 DC863 302198A WP BS 1260-1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 SPLICE CRACKED BETWEEN STATION 1260 AND 1280, AT LONGERON 31 LEFT. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999050700579 19990507 00579 WP 1999 5 7 ABXA9900342 1 19990318 A 5720 5769943 CLIP DOUG DOUG DC8 DC863 302198A WP WS 6.225 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 RIGHT WING LEADING EDGE RIB CLIP CRACKED AT STATION XOLDI 6.225. REPLACED CLIP IAW DC8 SRM 57-3-0. 2 L 7 4 4F 4A25 1999050700580 19990507 00580 WP 1999 5 7 SCNA99500 1 19990418 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1986 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, 2EA FLOOR SUPPORTS STA Y=1986 CL=0 AND X+27.5 ARE CRACKED AT INBD ENDS AND ALSO WERE F OUND CORRODED. REMOVED FABRICATED ALODINED PRIMED AND INSTALLED FLOOR SUPPORTS 2EA PER SRM 511000 512101 AND 513000. 2 L 7 3 4F A22WE 1999050700581 19990507 00581 WP 1999 5 7 SCNA99501 1 19990418 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1910 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, AFT GALLEY FLOOR SUPPORT AT STA 1910 WAS FOUND TO BE CORRODED BETWEEN X=27.5 AND X=MIN US 27.5 RT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS FABBED STRAP FOR FLOOR PANEL SUPPORT TREATED PRIMED AND INSTALL ED PER SRM REFS 512101 537000 FIG 18 SHEET 1 AND 573501. 2 L 7 3 4F A22WE 1999050700582 19990507 00582 WP 1999 5 7 SCNA99502 1 19990421 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1902 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, AFT GALLEY FLOOR SUPPORT AT STA 1902 WAS FOUND TO BE CORRODED ON UPPER AND LOWER SURFA CES RHX=8 AND BARE METAL X=1 TO X=23 CRACKS WERE FOUND AT FOOT ATTACHMENTS. FABBED NEW FLOOR SUPPORT INSTALLED PER SRM 513501. 2 L 7 3 4F A22WE 1999051200002 19990512 00002 NM 1999 5 12 SWAA990585 1 19990327 A 3350 NAS1291 NUT PLATE BOEING 737 7373Y0 1384671 NM LT EXTERIOR EEL DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 665WN 23497 DURING OVERNIGHT CHECK, FOUND DAMAGED ATTACH NUT PLATE FOR EMERGENCY LIGHT ON LEFT FUSELAGE AFT OF WING. REMOVED AND RE PLACED NUT PLATE PER MM AND SRM. 2 L 7 2 4F RT A16WE 1999051200003 19990512 00003 NM 1999 5 12 RAAA99B2024 1 19990330 A 5330 SKIN BOEING 727 72722C 138400F NM BS 480 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND SKIN BULGED AT STR 19R BS 480 TO 500. REMOVED CORROSION FROM SKIN LAP, FOUND OUT OF LIM ITS IAW SRM 53-30-01. INSTALLED FILLER AND DOUBLER IAW SRM 53-30-3 M54 NR 363. 2 L 7 3 4F A3WE 1999051400001 19990514 00001 WP 1999 5 14 TWAA9906501 1 19990503 A 3597 WIRE DOUG DC9 DC982 3022082 WP OXYGEN SYST SHORTED A TWAA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 CE 05 916TW 49187 AT 20,000 FT THE PSU OXY MASKS DROPPED ON THE LEFT SIDE OF CABIN. THERE WAS NO REASON FOR THEM TO HAVE DROPPED. FOUND WIRE W638K20 OF OXYGEN MASK CIRCUIT BREAKER SHORTED INTO FWD LAV PUMP 115 VOLT WIRES UNDER THE FORWARD LAVATORY. REPAIR ED WIRING UNDER THE FWD LAV CABINET. CHECK-C 2-22-99 MCI. 2 L 7 2 4F A6WE 1999051400002 19990514 00002 NM 1999 5 14 HNAA9900056 1 19990504 A 2910 DSC252B40124 HOSE DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYST LEAKING A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 924HA 105 LOSS OF NR 2 HYDRAULIC QUANTITY AND PRESSURE AFTER TAKEOFF (LEAK FROM NOSE GEAR AREA). REPLACED NOSE GEAR DRAG STRUT AC TUATOR HOSE ASSEMBLY. INSPECTED ENGINE DRIVEN PUMP PER MM PROCEDURE 05-50-33. NO CONTAMINATION FOUND IN CASE DRAIN FIL TER. GROUND RAN AIRCRAFT IAW PROCEDURE. RUNUP AND LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 1999051400003 19990514 00003 1999 5 14 MALA976445 4 19990502 A 3460 GNSX DISPLAY BAC 146 AVRO146RJ85A 1500097 EU COCKPIT SMOKING A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 517XJ E2335 DURING START UP FOR ENGINE NR 4, A NOTICABLE ELECTRICAL SMOKE SMELL WAS APPARENT IN THE COCKPIT. MAINTENANCE VERIFIED S MOKE SMELL TO THE RIGHT GNSX DISPLAY THAT WAS JUST DEFERRED. MAINTENANCE PULLED AND COLLARED NMV2 CB ON PANEL 131-12-00 . ELECTRICAL SMELL NO LONGER PRESENT. 2 H 7 4 4F RT A49EU 1999051400004 19990514 00004 WP 1999 5 14 IXXA9900009 1 19990504 A 3230 UPLATCH DOUG DC8 DC862 3021970 WP LT MLG WW LACK OF LUBE A IXXA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 61CX 61896 191 46142 AFTER TAKEOFF FROM AVB EN ROUTE TO FRA, WHEN THE LANDING GEAR WAS RETRACTED THE MAIN GEAR DOOR NOT LATCHED LIGHT REMAINE D ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONT INUED TO FRA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT GEAR DOOR WARNING SYSTEM AND LUBRICATED THE LEFT GEAR DOOR UPLATCH MECHANISM AND PERFORMED A SUCCESSFUL GEAR SWING IN ACCORDANCE WITH THE MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 1999051400005 19990514 00005 NM 1999 5 14 CALA9900488 1 19990506 A 5230 146N6603261 FRAME BOEING 757 757224 1384958 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 AFT CARGO DOOR FORWARD CORNER IS DENTED AND BEYOND SRM LIMITS. DAMAGED CORNER REMOVED, NEW CORNER FITTED PER SRM 52-00- 00. 2 L 7 2 4F RT A2NM 1999051400006 19990514 00006 NM 1999 5 14 CALA9900489 1 19990506 A 5230 146N660261 FRAME BOEING 757 757224 1384958 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 AFT CARGO DOOR AFT CORNER IS DAMAGED BEYOND LIMITS. DAMAGED CORNER REMOVED, NEW CORNER FITTED PER SRM 52-00-00. 2 L 7 2 4F RT A2NM 1999051400007 19990514 00007 WP 1999 5 14 CALA9900490 1 19990506 A 5320 FRAME DOUG DC10 DC1030 3023501 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 CENTER CARGO BAY DOOR FRAME LOWER SECTION CORRODED. REPAIRED PER SRM 53-50-00. 2 L 7 3 4F A22WE 1999051400008 19990514 00008 SO 1999 5 14 COMA9910072 1 19990504 A 3242 21585 BRAKE EMB 120 EMB120RT SO LT MLG FAILED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 249CA 16619 1500 120230 DURING PUSH BACK AIRCRAFT LURCHED. REPLACED THE LEFT HAND INBORAD BRAKE ASSY. 2 L 7 2 4T RT A31SO 1999051400009 19990514 00009 EA 1999 5 14 COMA9960180 1 19990504 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 918CA 7018 FLAPS FAILED. RESET FLAP SYSTEM IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 1999051400010 19990514 00010 EA 1999 5 14 COMA9960181 1 19990504 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 915CA 9514 1639 7013 FLAPS FAILED. REPLACED THE LEFT AND RIGHT BPSU FECU. 2 L 7 2 4F RT A21EA 1999051400011 19990514 00011 EA 1999 5 14 COMA9960182 1 19990505 A 2750 855D109 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 719CA 1562 1000 7253 FLAPS FAIL MESSAGE. REPLACED THE LEFT AND RIGHT BPSU. 2 L 7 2 4F RT A21EA 1999051400012 19990514 00012 NM 1999 5 14 UPS99229510 1 19990406 A 5730 65217065 PANEL BOEING 727 72731C 1384011 NM NR 3 TANK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE:C+SI, NR 3 TANK I/B AND O/B BOOST PANELS CORRODED. PANELS REPLACED IAW MM 12-30-06. 2 L 7 3 4F A3WE 1999051400013 19990514 00013 WP 1999 5 14 UPS99829508 1 19990407 A 5320 37739061 FITTING DOUG DC8 DC873F 302199F WP BS 798 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 798 AT RBL 24, THE SEAT TRACK ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51 -1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999051400014 19990514 00014 WP 1999 5 14 UPS99829509 1 19990421 A 5320 5779936501 DOUBlER DOUG DC8 DC873F 302199F WP BS 1360-1390 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 1360 TO 1390, LT CUSP, THE FINGER DOUBLER IS CRACKED IN 2 PLACES. REMOVED, FABRICATED AND INSTAL LED FINGER DOUBLER IAW DWG 5779936 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999051400015 19990514 00015 WP 1999 5 14 UPS99829511 1 19990426 A 5311 5640242509 FRAME DOUG DC8 DC873F 302199F WP BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:SV, FUSELAGE STATION 1660 L34L FRAME SPLICE CRACKED. REPAIRED IAW REO 06455 REPLACED DAMAGED FRAME SEGM ENT AT FUSELAGE STATION 1660 BETWEEN L27L AND RIGHT PER DAC 564024209 FIG 1 AND REPLACED CLIP 5640242-65 PER DWG AND 561 5374DW USING 7075T6 ALUMINUM SHEET. UPS REPAIR AUTHORIZATION DC8-53-2578 2 L 7 4 4F RT 4A25 1999051400016 19990514 00016 WP 1999 5 14 UPS99829512 1 19990424 A 5320 CUSP DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:SV, FLOORBEAM STATION 1580 LEFT CUSP HAS CORROSION. REPAIRED IAW REO 06440 REV A TIMCO DWG DC08-53-0351 REV A-501 INSTALLATION AND UPS REPAIR AUTHORIZATION DC8-53-2588. 2 L 7 4 4F RT 4A25 1999051400017 19990514 00017 WP 1999 5 14 UPS99829513 1 19990424 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:SV, FLOORBEAM STATION 1600 AFT FACE 36 FROM LEFT CUSP HAS CORROSION. REPAIRED IAW REO 06439 REV A PER T IMCO DWG DC08-53-0351 REV A -501 INSTALLATION AND UPS REPAIR AUTHORIZATION DC8-53-2583. 2 L 7 4 4F RT 4A25 1999051400018 19990514 00018 WP 1999 5 14 UPS99829514 1 19990427 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1660 DRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:SV, LONGERON AT STATION 1660 L34R HAS DOUBLE DRILLED HOLE. REPAIRED PER REO 06451. 2 L 7 4 4F RT 4A25 1999051400019 19990514 00019 NM 1999 5 14 UPS99229515 1 19990429 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 873-877 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, INTERIOR FUSELAGE SKIN AT STA 873-877 RT WL 261 ALONG EDGE OF 5-10R IS CORRODED. BLENDED CORROSION ON LOWER SKIN, HFEC FASTENER HOLES, FLAT PEENED THE BLENDED AREA. ALODINED AND PRIMED BLENDED AREA, FABRICATED REPAIR D OUBLER AND REPAIR FILLER, ALODINED AND PRIMED REPAIR PARTS AND INSTALLED. 2 L 7 3 4F A3WE 1999051400020 19990514 00020 NM 1999 5 14 UPS99229516 1 19990327 A 5753 65216512 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) NR 5 FLAP TRACK FWD ATTACH FITTING. REPLACED FITTING BEYOND ECONOMICAL REPAIR PER ESR NR 16, ON NRC 888880. 2 L 7 3 4F A3WE 1999051400021 19990514 00021 NM 1999 5 14 UPS99229517 1 19990503 A 5320 65956001723 CHORD BOEING 727 72731C 1384011 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, 740 UPPER CHORD CORRODED RBL 65-70 WL 202. REMOVED AND REPLACED CHORD SEGMENT RBL 53-55 TO RIGHT O/ B END. 2 L 7 3 4F A3WE 1999051400022 19990514 00022 NM 1999 5 14 UPS99229518 1 19990505 A 3350 BATTERY PACK BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:N/A, COCKPIT AND CABIN ENTRY EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN BOTH PACKS. LIGHTS OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999051400023 19990514 00023 EU 1999 5 14 QXEA9901012 1 19990503 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 475AU 82 11222 SEA- RIGHT HAND AND LEFT HAND OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED POSITION NR 5 AND PO SITION NR 6 EMERGENCY LIGHT POWER SUPPLY. NO DEFECTS NOTED. 2 L 7 2 4F RT A20EU 1999051400024 19990514 00024 WP 1999 5 14 ABXA9900343 1 19990411 A 5311 97599356 FRAME DOUG DOUG DC8 DC863 302198A WP BS 520 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 FRAME AT STATION 520 AT LONGERON 34 RIGHT CRACKED. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999051400025 19990514 00025 WP 1999 5 14 ABXA9900344 1 19990316 A 5320 3755840 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1220 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 STATION 1220 BETWEEN LONGERONS 33 RIGHT AND 34 RIGHT, SHEAR TIE FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999051400026 19990514 00026 WP 1999 5 14 ABXA9900345 1 19990317 A 5712 5769859 RIB DOUG DOUG DC8 DC863 302198A WP WS 250.089 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XS 250.089. REPLACED ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999051400027 19990514 00027 WP 1999 5 14 ABXA9900347 1 19990316 A 5320 47507681 FITTING DOUG DOUG DC8 DC863 302198A WP TAIL SKID CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 TAIL SKID UPPER HORIZONTAL ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999051400028 19990514 00028 WP 1999 5 14 ABXA9900348 1 19990421 A 5320 5597646 INTERCOSTAL DOUG DOUG DC8 DC863 302198A WP BS 25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 FORWARD ENTRANCE DOOR JAMB INTERCOSTAL AT STATION 25, LONGERON 15 LEFT WAS CRACKED. REPAIRED IAW ABX REA B853-27620MR. 2 L 7 4 4F 4A25 1999051400029 19990514 00029 WP 1999 5 14 MWEA99249 1 19990505 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP CABIN DISENGAGED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 401ME 47133 THE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1999051400030 19990514 00030 WP 1999 5 14 MWEA99250 1 19990501 A 5230 59101415 PAN DOUG DC9 DC914 3022034 WP CARGO DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND TOOLING MARKS ON EXTERIOR CARGO DOOR PAN FLANGE AT LOWER AFT CORNER. MTC FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 1999051400031 19990514 00031 WP 1999 5 14 MWEA99251 1 19990501 A 5230 99576649 INTERCOSTAL DOUG DC9 DC914 3022034 WP CARGO DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FOUND TOOLING MARKS ON FORWARD UPPER INTERCOSTAL FORWARD OF FORWARD CARGO DOOR. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999051400032 19990514 00032 WP 1999 5 14 MWEA99252 1 19990501 A 5210 9955752501 BEAM DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE MAIN CABIN DOOR NUMBER ONE BEAM CRACKED AT AFT END. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999051400033 19990514 00033 WP 1999 5 14 MWEA99253 1 19990503 A 5312 9915562505 BLKHD FORMER DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 THE VENTRAL DOOR RIGHT CORNER IS CRACKED ON FORMER. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1999051400034 19990514 00034 NM 1999 5 14 TC8A99016 1 19990506 A 3610 CLAMP BOEING 727 72721C 138400M NM PWA JT8 JT8D7B 52053 NE NR 3 STRUT LOOSE A TC8A A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 705A 19134 654663 KMSP-KMSP TRIP NR 03341. ENG NR 3 STRUT O/H OCCURED IN CLIMB, COMPLIED WITH ENG STRUT O/H CHECKLIST. ENG NR 3 FIRE WAR NING LIGHT CAME ON DURING CLIMB, COMPLIED WITH ENG FIRE SEVERE DAMAGE SEPARATION CHECKLIST AND SHUT ENG DOWN AND FIRED T HE EXTINGUISHER. LIGHT REMAINED ILLUM AND FIRE BELL SOUNDED. FIRED THE 2ND BOTTLE, FIRE LIGHT REMAINED ILLUM. INSPECT NR 3 STRUT, FOUND HIGH PRESS S/O VALVE CLAMP OFF. REINSTALLED. REPAIRED WIRING AT HIGH PRESS S/O VALVE IAW B727 MM 36 -13-0, OPS CHECK NORM. REPAIRED WIRING AT NR 3 STRUT FIRE WARNING CANNON PLUG, OPS CHECK NORM IAW B727 MM 26-11-01. R/ R'D LT AND RT FIRE BOTTLES AND SQUIBS IAW B727 MM 26-21-00. INSPECTED ENG AND PYLON FOR DAMAGE, NONE NOTED. PERFORMED 2 L 7 3 4F 4 F A3WE E2EA 1999051400035 19990514 00035 WP 1999 5 14 CALA9900523 1 19990511 A 5330 5932717501 SKIN DOUG DC9 DC982 3022082 WP BS 1041 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 FUSELAGE SKIN IS GOUGED UNDER AFT END OF ADF ANTENNA. BLENDED GOUGE AND INSTALLED REPAIR PER SRM 53-04 FIG 38 VIEW G. 2 L 7 2 4F A6WE 1999051400036 19990514 00036 WP 1999 5 14 CALA9900524 1 19990512 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 AFT LAV FRAME SUPPORT OUTBOARD FITTING FS 996 STR 18L IS CORRODED. REPAIRED PER SRM 53-05 FIG 20 AND FIG 72. 2 L 7 2 4F A6WE 1999051400037 19990514 00037 WP 1999 5 14 CALA9900525 1 19990511 A 5220 49144121 BRACKET DOUG DC9 DC982 3022082 WP LT EMER EXIT DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 LEFT FORWARD EMERGENCY EXIT DOOR SEAL RETAINER SUPPORT BRACKET CRACKED AT RIVET (.5). REPLACED FORWARD LOWER RETAINER B RACKET PER SRM 51-30-2. 2 L 7 2 4F A6WE 1999051400038 19990514 00038 WP 1999 5 14 CALA9900526 1 19990511 A 5315 2921948 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 313 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 CABIN FS 313 FLOORBEAM UPPER FLANGE IS GOUGED BETWEEN RBL 12A AND LBL 12A. AFTER BLEND OUT OF GOUGED, FOUND OUT OF LIMI TS. FABRICATED TREATED, PRIMED AND INSTALLED REPAIR ANGLE AND FILLERS PER SRM 53-05 FIG 20A, 53-01-01, 53-10-4 AND 53-0 5 FIG 20. 2 L 7 2 4F A6WE 1999051400039 19990514 00039 WP 1999 5 14 CALA9900527 1 19990511 A 5350 TAIL CONE DOUG DC9 DC982 3022082 WP BS 1510 OUT OF ADJUST A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 35836 49441 TAIL COMPARTMENT INTERIOR TAIL CONE RELEASE HANDLE PULL TOO HIGH (45 LBS). RIGGED TAIL CONE RELEASE MECHANISM PER MM 53 -53-00. 2 L 7 2 4F A6WE 1999051400040 19990514 00040 EU 1999 5 14 QXEA9901016 1 19990509 A 3610 VALVE GARRTT 38075412 FOKKER F28 F28MK4000 4990810 EU NR 1 BLEED AIR FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 478US P37494 11227 PDX - AUXILLARY POWER UNITS TURBINE GAS TEMPERATURE WAS 660 DEGREES WITH 1 PACK ON. ALSO, NOTICED EXHAUST SMELL COMING FROM COCKPIT AIR VENTS. PLACED APU ON MEL. THE MEL WAS CLEARED AFTER REMOVING AND REPLACING THE BLEED AIR LOAD CONTROL VALVE. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A20EU 1999051400041 19990514 00041 NM 1999 5 14 99UAL900250 1 19990501 A 2560 SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT EMER EXIT OUT OF ADJUST A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 654UA 25392 LEFT WING SLIDE EICAS MESSAGE CAME ON INTERMITTENTLY DURING FINAL DESCENT. *S/D* LT OVERWING DOOR CHECKED CLOSED, SEC URE AND LATCHED. FOUND SENSORS S218 AND S198 OUT OF ADJUSTMENT. ADJUSTED SENSORS PER MM, OPS CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1999051400042 19990514 00042 WP 1999 5 14 99UAL900251 1 19990501 A 5270 SWITCH DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL DOOR 4L OUT OF ADJUST A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 1828U 46627 DOOR 4L SETS OFF EVAC ALARM WHEN DOOR IS ARMED. *S/D* THE CAUSE FOR THE EVAC ALARM SOUND WAS THAT WHEN THE DOOR WAS AR MED THE EVAC ALARM SWITCH WAS OUT OF ADJUSTMENT. REPLACED AND ADJUSTED EVAC ALARM SWITCH (P/N: BAN70241). EVAC ALARM W AS OP CHECKED AND FOUND TO OPERATE NORMALLY. 2 L 7 3 4F 4 F A22WE E23EA 1999051400043 19990514 00043 NM 1999 5 14 99UAL900252 1 19990501 A 2121 210N7014 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 554UA 6112 26644 FLIGHT DIVERTED TO EWR DUE TO THE SMELL OF SMOKE IN THE COCKPIT. *S/D* ELECTRICAL SMELL WAS ATTRIBUTED TO THE LEFT REC IRCULATION FAN. THE LEFT FAN WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999051400044 19990514 00044 NM 1999 5 14 99UAL900253 1 19990502 A 2910 PACKING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE A HYD SYST LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 324UA 23956 'A' HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED AND QUANTITY DROPPED ONE QUARTER. *S/D* REPLACED PACKING ON PRESSU RE MODULE, SERVICED HYDRAULIC SYSTEM 'A'. TESTED FLIGHT CONTROLS AND NUMBER 1 ENGINE. NO LEAKS NOTED, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999051400045 19990514 00045 EU 1999 5 14 99UAL900254 1 19990501 A 3242 BRAKE BFGOODRICH 21600 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FAILED A UALA O OTHER O OTHER LD LANDING 1 WP 29 444UA 0177 824 BRAKE EXTREMELY SENSITIVE, MOST NOTICABLE ON THE LEFT BRAKE. ON LANDING AIRCRAFT JERKED ABRUPTLY TO THE LEFT. *S/D* F OUND NR 1 BRAKE SEIZED WITH YELLOW PISTONS STUCK IN ACTUATED POSTION. REPLACED NR 1 BRAKE. TAXI TESTED, ALL FUNCTIONS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1999051400046 19990514 00046 EU 1999 5 14 99UAL900255 1 19990430 A 2420 RAM AIR TURB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AUX POWER FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 419UA 487 RAT FAILED AUX HYD SYS OPS TEST. *S/D* DURING FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT, RAM AIR TURBINE FAILED C HECK. REPLACED RAT PER AMM AND OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1999051400047 19990514 00047 NM 1999 5 14 99UAL900256 1 19990504 A 5400 FASTENERS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 PYLON FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 610UA 21871 NR 1 PYLON AFT LWR SPAR FITTING, 3 FASTENERS FAILED ADJACENT TO DIAG BRACE. *S/D* IT IS ASSUMED THE JOINT OPENED UNDER LIMIT LOADS OR TENSILE FATIGUE LOADS FROM THE DIAG BRACE. WHEN THESE LOADS OCCUR, 1 OR MORE OF THE FASTENERS CAN FAIL AS OUTLINED IN SB 767-54-0070, EFFECTIVE FOR 767-322 AIRCRAFT. REPLACED ALL 8 FASTENERS ON THE VERT FLANGE OF THE AFT L WR SPAR FITTING, INSPECTION OF THE RADII BETWEEN LUG AND VERT FLANGE FOR CRACKS, AND FASTENERS COMMON TO THE HORIZ FLANG E FOR LOOSENESS OR OTHER ANOMALIES. AN ULTRASOUND INSPECTION OF THE NR 2 PYLON AFT LWR SPAR FITTING VERT FLANGE FASTENE RS WAS ACCOMPLISHED WITH NO ANOMALIES FOUND. 2 L 7 2 4F 4 F RT A1NM E3NE 1999051400048 19990514 00048 1999 5 14 99UAL900257 4 19990504 A 2350 8990850004 RMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT COCKPIT SMOKING A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 408UA 6432 6432 457 FIRST OFFICER'S RADIO MANAGEMENT PANEL SMOKING. RADIO MANAGEMENT PANEL (RMP) WAS REMOVED FOR THIS PROBLEM. LATER THE PA NEL WAS FOUND TO BE OK AND REINSTALLED IN THE AIRCRAFT. MR23131-0135. 2 L 7 2 4F 4 F RT A28NM E40NE 1999051400049 19990514 00049 NM 1999 5 14 99UAL900258 1 19990503 A 3260 BR20AXH5V3 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG FAILED A UALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 29 388UA 24663 NOSE GEAR UNSAFE LIGHT ILLUMINATED. *S/D* FAULTY NOSE GEAR LATCHING RELAY. REPLACED NOSE GEAR LATCHING RELAY ITEM R37 4. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999051400050 19990514 00050 EU 1999 5 14 99UAL900259 1 19990504 A 3150 MCDU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT & RT COCKPIT FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 432UA 587 CAPT MCDU FAILED, THEN F/O MCDU FAILED-WENT BLANK. *S/D* THIS WAS CODED IN CHAPTER 45 NOT 34. BOTH THE CAPT'S AND FO' S MCDU CBS WERE RESET AND SYSTEM OP'S CHECK NORMAL. NO FURTHER MAINTENANCE HAS BEEN PERFORMED AND NO FURTHER PROBLEMS W ITH THE MCDU HAVE HAPPENED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999051400051 19990514 00051 NM 1999 5 14 99UAL900260 1 19990505 A 2130 VALVE SUNDSTRAND TSK56697 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7441U 21895 UNABLE TO PRESSURIZE IN AUTO OR STANDBY. RETURNED TO DEN. *S/D* REPLACED FLOW CONTROL VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1999051400052 19990514 00052 NM 1999 5 14 99UAL900261 1 19990504 A 2781 H1010272U1 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 LE SLAT FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 7459U 21913 NR 4 LEADING EDGE FLAP INDICATOR ILLUMINATED ON SECOND OFFICERS PANEL. RETURNED TO DEN. *S/D* REPLACED NR 4 LEADING E DGE SLAT EXTEND SWITCH, SYSTEM OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1999051400053 19990514 00053 NM 1999 5 14 99UAL900262 1 19990505 A 2121 6067723 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 520UA 24890 AIRCRAFT DIVERTED TO DEN DUE TO STRONG ELECTRICAL SMELL IN CABIN. *S/D* SMELL WAS CAUSED BY A FAILED RT RECIRCULATION FAN. RT FAN WAS REPLACED AND NO FURTHER DISCREPANCIES WERE NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999051400054 19990514 00054 WP 1999 5 14 99UAL900263 1 19990506 A 2560 CONNECTOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL 4L DOOR BENT A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 1828U 46627 EVAC SIGNAL SOUNDS WHEN DOOR 4L IS ARMED. *S/D* THE CAUSE OF THE EVAC SIGNAL SOUNDING WAS GIRT BAR ARM SWITCH CONNECTO R BENT PINS AND SWITCH (S1-702) AT DOOR 4 LT CLOSED WHEN SHOULD BE NORMALLY OPENED. SWITCH WAS FOUND NORMAL. REPLACED THE FOLLOWING PARTS, PIN (MS20392-2C11), PIN (MS214665-151), LINK (AGA3340-41) AND BUSHING (ADA2650-1). OPS CHECK GOOD . 2 L 7 3 4F 4 F A22WE E23EA 1999051400055 19990514 00055 WP 1999 5 14 ABXA9900356 1 19990421 A 5315 9910078147 FLOORBEAM DOUG DOUG DC9 DC941 302207N WP BS 180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND FLOORBEAM WEB CRACKED AT STATION 180, LBL 22. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999051400056 19990514 00056 WP 1999 5 14 ABXA9900357 1 19990421 A 5730 992341931 PANEL DOUG DOUG DC9 DC941 302207N WP CENTER WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND RIGHT CENTER WING SLANT PANEL CORRODED. REPLACED SLANT PANEL IAW ABX EA 53200018-301. 2 L 7 2 4F A6WE 1999051400057 19990514 00057 WP 1999 5 14 ABXA9900358 1 19990510 A 5711 59113011 SPAR CAP DOUG DOUG DC9 DC941 302207N WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK, FOUND LEFT WING REAR SPAR CAP CRACKED AT NUMEROUS HOLES. REPAIRED IAW ABX REA D957-28455MR. 2 L 7 2 4F A6WE 1999051400058 19990514 00058 WP 1999 5 14 ABXA9900359 1 19990510 A 5312 J0600923 BULKHEAD JAMB DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB UPPER CORNER CRACKED. REPAIRED CRACK IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999051400059 19990514 00059 WP 1999 5 14 ABXA9900360 1 19990510 A 5312 J0600929N BULKHEAD JAMB DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB, RIGHT UPPER CORNER CRACKED. REPAIRED IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999051400060 19990514 00060 NM 1999 5 14 DL76G990964 1 19990502 A 7910 UNION BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 NE NR 1 ENGINE LEAKING A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 153DL 18133 24985 695307 EXCESSIVE OIL CONSUMPTION ON LEFT ENG OIL QTY PRIOR TO ENG START. AFTER LANDING OIL 3, AFTER ENG SHUTDOWN 7. PERFORME D CHECK OUT PER FIM 71-05-00. FOUND LEAK BELOW SERVO FUEL. UNION WAS NOT CORRECTLY INSTALLED. INSTALLED NEW UNION AND AFTER ENG RUN NO LEAKS FOUND. 2 L 7 2 4F 4 F RT A1NM E13NE 1999051400061 19990514 00061 NM 1999 5 14 DL72K990966 1 19990430 A 7120 65312813 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 WHILE PERFORMING HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLES CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLES WITH ANGLES OF NEW MFG. 2 L 7 3 4F A3WE 1999051400062 19990514 00062 NM 1999 5 14 DL72S990967 1 19990501 A 7120 65312814 ANGLE BOEING 727 727225 1384077 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 WHILE WORKING HUSH-KIT, FOUND NR 2 ENG RT AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED PART WITH ONE OF NE W MFG. 2 L 7 3 4F A3WE 1999051400063 19990514 00063 NM 1999 5 14 DL72E990969 1 19990503 A 2121 215201 FAN 215201 BOEING 727 727247 138408F NM CARGO COMPT FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 282WA AA39565 21484 SMELL OF SMOKE NOTED IN CABIN PRIOR TO TAKEOFF. RETURNED TO GATE, GASPER FAN C/B POPPED. REPLACED GASPER FAN, OPS CKS OK. FAN HAD CAUSED SMOKE IN CABIN. 2 L 7 3 4F A3WE 1999051400064 19990514 00064 NM 1999 5 14 DL72L990970 1 19990503 A 8012 START VALVE 97907821 BOEING 727 727232 1384082 NM NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 504DA 7013 21306 NR 1 START VALVE LIGHT ILLUMINATED IN FLIGHT. ENG SHUT DOWN PER PILOTS CK LIST. REPLACED START VALVE. 2 L 7 3 4F A3WE 1999051400065 19990514 00065 NM 1999 5 14 DL72S990971 1 19990502 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 489DA 21019 INTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 TO 480 REVEALED MULTIPLE CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. THE ENTIRE LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXT ERNAL ALUMINUM DOUBLER PER ER/A 367304-14AD. 2 L 7 3 4F A3WE 1999051400066 19990514 00066 NM 1999 5 14 DL72S990972 1 19990502 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 489DA 21019 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 19 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUTOUT AN D REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367303-14AD. 2 L 7 3 4F A3WE 1999051400067 19990514 00067 NM 1999 5 14 DL72S990973 1 19990502 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 489DA 21019 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED MULTIPLE CRACKS IN MULTIPLE FRAME BAYS ALONG THE PANEL LENGTH. THE SKIN LAPS SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367302-14AD. 2 L 7 3 4F A3WE 1999051400068 19990514 00068 NM 1999 5 14 DL72K990975 1 19990120 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND WORN 35 FROM O/B END OF FLAP. A REPAIR DOUBLER WAS INSTALLED PER MM 57- 52-0, FIG 809. 2 L 7 3 4F A3WE 1999051400069 19990514 00069 NM 1999 5 14 DL72K990976 1 19990204 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING SHOP INSPECTION, A HOLE WAS FOUND IN COVE SKIN PANEL AT 2ND FROM I/B AFT FLAP TRACK. THE SKIN WAS REPAIRED PER M M 57-52-0, FIG 809. 2 L 7 3 4F A3WE 1999051400070 19990514 00070 NM 1999 5 14 DL72K990977 1 19990120 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING SHOP INSPECTION, THE AFT COVE SKIN WAS FOUND WITH TOOL DAMAGE 60 FROM O/B END. THE SKIN WAS REPAIRED BY INSTALLI NG A DOUBLER PER MM 57-52-0 PAGE 819. 2 L 7 3 4F A3WE 1999051400071 19990514 00071 WP 1999 5 14 DLL13990978 1 19990504 A 2910 LINE LKHEED 1011 10113851 5265010 WP LT MLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 786DL 193A1123 LOST C-HYD SYS QUANTITY DROPPED TO QUARTER. NECESSARY TO LOWER MLG VIA ALT GEAR EXTENSION. FOUND LEAK AT GEAR UP LINE. INSTALLED TEMP LINE. 2 L 7 3 4F A23WE 1999051400072 19990514 00072 1999 5 14 DL73K990979 4 19990504 A 2210 4030952906 COUPLER BOEING 737 737232 1384475 NM YAW DAMPER FAILED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 334DL 23105 CONTINUOUS VIBRATION (AIRFRAME) IN CLIMB AND CRUISE. VIBRATION STARTED AT FL 290 STEADY UP TO FL 350, SPEED 310 KTS. S LOWED TO 250 KTS, NO CHANGE. SECURED YAW DAMPER AT 13,000 FT, VIBRATION CEASED. PERFORMED VIBRATION INSPECTION PER M/M 5-51-281, ALSO REF. T/S CHART M/M 27-31-00. REPLACED YAW DAMPER COUPLER PER M/M. RAN INTERLOCK AND SYTEM TEST PER M/ M 22-11-0 PAGE 539. ALL TESTS NORMAL. 2 L 7 2 4F RT A16WE 1999051400073 19990514 00073 NM 1999 5 14 DL72S990980 1 19990504 A 5754 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 ONE INCH CRACK NR 2 SLAT L/E NOSE RIB I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0 PG 805. 2 L 7 3 4F A3WE 1999051400074 19990514 00074 NM 1999 5 14 DL72E990981 1 19990505 A 5350 FAIRING BOEING 727 727247 138408F NM BS 740-774 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 FUSELAGE FAIRING RT AC BAY FRAME, CORROSION AROUND HINGES FOR ACCESS PANEL 3448 RBL 9 STA 740 TO 774. REMOVED PANEL 344 8 DAMAGED T/E. BEGAN FABRICATING REPAIR PER M/M 53-30-1. OK TO PAINT AND INSTALL. COMPLETED FABRICATION PRIOR TO TREA T AND PAINT. INSTALLED ANGLE PER M/M 53-30-1 FIG 804. INSTALLED PANEL 3448. 2 L 7 3 4F A3WE 1999051400075 19990514 00075 WP 1999 5 14 DLL14990982 1 19990504 A 3350 OL3071BPEGPL LIGHT LKHEED 1011 1011385115 5265015 WP ROW 1 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 740DA 193C1244 EMERGENCY TRACK LIGHTING ALONG SIDE SEAT 1D IS DAMAGED. RELAMPED AND REPLACED LENS. OPS CK GOOD. 2 L 7 3 4F A23WE 1999051400076 19990514 00076 WP 1999 5 14 DLL19990983 1 19990505 A 3510 REGULATOR LKHEED 1011 10113853 5265020 WP LT OXYGEN MASK FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 755DL 193Y1184 CAPTS 02 MASK HAS CONTINUOUS FLOW IN ON POSITION ON REGULATOR PANEL. PANEL SWITCH MUST BE TURNED OFF TO CEASE FLOW. CR EW 02 PRESSURE NOW AT 800 PSI. REPLACED CAPTS REGULATOR AND SERVICED CREW 02 BOTTLE, BOTH LEAK CHECK OK. 2 L 7 3 4F A23WE 1999051400077 19990514 00077 NM 1999 5 14 DLM88990984 1 19990505 A 2150 CONTROLLER 60714622 DOUG MD88 MD88 3023688 NM RT PACK INOPERATIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 913DE 031C4463 49956 AFTER TAKEOFF FROM MKE, NOTICED RIGHT PACK PRESSURE AT 55 PSI (LEFT PACK PRESSURE 25 PSI) AFT F/A COULD SMELL BURNING OD OR. THEN RIGHT PACK SHUTDOWN AND PRESSURE DROPPED TO 12 PSI. RAN ABNORMAL CHECKLIST AND LEFT THE RIGHT PACK OFF. RIGH T PACK OPERATED NORMALLY ON GROUND WITH APU AIR IN MANUAL MODE. CHECKED LT AND RT PACKS AND DUCTING ACMS OPERATING NORM AL. REPLACED RT PACK A/C CONTROLLER RT PACK OPERATES IN NORMAL MODES. NO SMELLS NOTED, PACK SYSTEM CKS NORMAL. 2 L 7 2 4F RT A6WE 1999051400078 19990514 00078 NM 1999 5 14 DL72S990985 1 19990505 A 5320 FRAME BOEING 727 727232 1384082 NM L2 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 A .75 INCH VISIBLE CRACK AT L-2 DOOR FWD FRAME AT UPPER LOCK ROLLER. REPAIRED PER M/M 52-12-0. 2 L 7 3 4F A3WE 1999051400079 19990514 00079 NE 1999 5 14 DL767990986 2 19990506 A 7200 ENGINE BOEING 767 767232 1385132 NM GE CF6 CF680A 30025 NE NR 2 FAILED A DALA B EMER. DESCENT X ENGINE FLAMEOUT AP APPROACH 1 SO 27 101DA 40030 22213 580112 IN DESCENT RT ENGINE FAILED, OIL PRESS WENT TO ZERO. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 1999051400080 19990514 00080 NM 1999 5 14 DL72S990988 1 19990506 A 2560 MEGAPHONE 1MV10 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 540DA 22386 AFT CABIN MEGAPHONE INOP ON PREFLIGHT. REPLACED AFT CABIN MEGAPHONE. 2 L 7 3 4F A3WE 1999051400081 19990514 00081 NM 1999 5 14 DL72S990990 1 19990506 A 5313 655860710 STRINGER BOEING 727 727225 1384077 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 A 4 INCH CRACK WAS FOUND IN THE VERT FLANGE (SKIN ATTACH) OF S18A AT APPROX BS 941. REPAIRED PER ERA 333079-14, REV A. 2 L 7 3 4F A3WE 1999051400082 19990514 00082 NM 1999 5 14 DLM88990991 1 19990506 A 2530 50459 OVEN DOUG MD88 MD88 3023688 NM GALLEY DIRTY A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 900DE 53372 DURING TAXI OUT, SMOKE FROM FIRST CLASS OVEN. FOUND BURNED PAPER MEAL TAG ATTACHED TO MEAL CARRIER. AIRCRAFT TAXIED BA CK TO RAMP. MAINTENANCE REMOVED REMAINS OF TAG. CLEANED AND OPERATED OVEN. NO FURTHER SMOKE, OVEN OPERATED NORMALLY . 2 L 7 2 4F RT A6WE 1999051400083 19990514 00083 NM 1999 5 14 DL72E990992 1 19990428 A 5531 RIB BOEING 727 727247 138408F NM VERT FIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 LT STR TO RIB ATTACH FLANGE CRACKED INSIDE VERTICAL FIN AT RIB STA 179 STR 8L. FABRICATED REPAIR PER M/M 55-30-0 FIG 80 3. OK TO INSTALL. REPAIRED PER M/M 55-30-0 RIG 803. 2 L 7 3 4F A3WE 1999051400084 19990514 00084 NM 1999 5 14 DL72S990993 1 19990421 A 5753 652163368 SKIN BOEING 727 727225 1384077 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 TEMP REPAIR L/E SKIN I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999051400085 19990514 00085 NM 1999 5 14 DL72S990994 1 19990421 A 5753 652163368 SKIN BOEING 727 727225 1384077 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 TEMP REPAIR L/E SKIN O/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999051400086 19990514 00086 NM 1999 5 14 DLM88990996 1 19990507 A 3260 INDICATOR 833605MODA DOUG MD88 MD88 3023688 NM LANDING GEAR MALFUNCTIONED A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 931DL 517 49718 NOSE WHEEL AND MAIN LANDING GEAR INDICATORS INDICATED UNSAFE UNTIL INDICATOR LIGHTS WERE PRESS. THIS CAUSED A GO-AROUND . REPLACED PROX BOX, JACKED A/C, RAN SEVERAL TIMES AND NO FAULTS. CHECKED PROX SWITCHES, ALL GEAR AND NO FAULTS. A/C CKS GOOD FOR SERVICE PER MM CHAP 31, 32. 2 L 7 2 4F RT A6WE 1999051400087 19990514 00087 NM 1999 5 14 DL72S990997 1 19990506 A 5320 WEB BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 THE FS 1263 WEB OF THE RT LOWER VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A TYPICAL CRACK. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED PER B727 S/B 53-0129 AND ER/A 367330-14AD. 2 L 7 3 4F A3WE 1999051400088 19990514 00088 WP 1999 5 14 DLL14990998 1 19990505 A 5512 1524132104 SKIN LKHEED 1011 1011385115 5265015 WP RT HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 THE NR 4 UPPER SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A .05 CRACK AT THE RUNOUT OF AN INTEGRAL STIFFE NER AT HSS 80. THE CRACK WAS ROUTED OUT OF THE PANEL AND AN ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 367318 -14. 2 L 7 3 4F A23WE 1999051400089 19990514 00089 NM 1999 5 14 DL72K990999 1 19990505 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER PANEL. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS C UTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367317-14AD. 2 L 7 3 4F A3WE 1999051400090 19990514 00090 NM 1999 5 14 DL72K991000 1 19990505 A 5330 655456716 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 4 CRACKS IN CONSECUTIVE FRAME BAYS. THE ENTIRE SKIN LAP WA S CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367316-14AD. 2 L 7 3 4F A3WE 1999051400091 19990514 00091 NE 1999 5 14 DL72W991001 2 19990506 A 7230 COMPRESSOR BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE STALLED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 2819W 56728 21057 695301 DEPARTING DFW AFT CARGO DOOR CAME OPEN DURING ROTATION AT T/O. NUMBER 3 ENGINE PRECAUTIONARY SHUT DOWN IN FLIGHT DUE TO MULTIPLE COMPRESSOR STALLS. ONE FAN BLADE NICKED AND MINOR DAMAGE TO ACCOUSTICAL PANEL. 2 L 7 3 4F 4 F A3WE E2EA 1999051400092 19990514 00092 NM 1999 5 14 DL733991002 1 19990506 A 3350 CONNECTOR 323975 BOEING 737 737347 1384647 NM ROW 18 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 307WA 23440 FLOOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROWS 18 THROUGH 22 ARE INOP. FOUND OPEN SPLICE CONNECTOR UNDER SEAT 22D. REM OVED AND REPLACED CONNECTOR SPLICE, OPS NORMAL. 2 L 7 2 4F RT A16WE 1999051400093 19990514 00093 NM 1999 5 14 DLM11991003 1 19990507 A 2530 OVEN DOUG MD11 MD11 3023602 NM CABIN DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 802DE 48473 F/C OVENS 102 AND 103 HAD BURNING SMELL. THE OVENS WERE OFF AND HAD BEEN OFF FOR APPROX 30 MIN. RAN OVENS AT MEDIUM FO R 30 MIN. NO TROUBLE FOUND. 2 L 7 3 4F RT A22WE 1999051400094 19990514 00094 NM 1999 5 14 DL72E991004 1 19990507 A 5754 65162222 SKIN BOEING 727 727247 138408F NM RT LE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 INNER SKIN CUT TO GAIN ACCESS TO RIBS. REPAIRED SKIN PER M/M 57-54-0 FIG 80. 2 L 7 3 4F A3WE 1999051400095 19990514 00095 NM 1999 5 14 DL72K991005 1 19990111 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING SHOP INSPECTION THE COVE SKIN WAS FOUND TO HAVE A TEMPORARY REPAIR INSTALLED 34 FROM I/B END OF FLAP. THE SKIN W AS REPAIRED BY INSTALLING A PERMANENT REPAIR DOUBLER PER MM 57-52-0, FIG 809. 2 L 7 3 4F A3WE 1999051400096 19990514 00096 NM 1999 5 14 DL72K991006 1 19990111 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 31 INCHES FROM I/B END. A REPAIR DOUBLER WAS INSTALLED PER MM 5 7-52-0, FIG 809. 2 L 7 3 4F A3WE 1999051400097 19990514 00097 NM 1999 5 14 DL72S991008 1 19990507 A 5320 WEB BOEING 727 727232 1384082 NM BS 1214 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 LEFT I/B TORQUE BOX VERT WEB CRACKED .5 INCH AT UPPER FASTENER STA 1214. REPAIRED PER MM 53-11-0 FIG 819. 2 L 7 3 4F A3WE 1999051400098 19990514 00098 NE 1999 5 14 DL757991012 2 19990508 A 7230 COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 643DL 23518 23997 716582 ON DEPARTURE HAD SEVERAL ENGINE AUDIBLE COMPRESSOR STALLS ON THE RT ENG RPM FLUCTUATED 5 TO 6 PERCENT SEVERAL TIMES, THE N SETTLED AT NORMAL SETTING. BORESCOPED 12TH AND 13TH STAGE HPC PER FIM. FOUND 20, 12TH HPC BLADES WITH DAMAGE AN D 21, 13TH STAGE BLADES DAMAGED OUT OF LIMITS PER M/M 72-00-00-6. ENG CHANGE IN PROGRESS. 2 L 7 2 4F 4 F RT A2NM E17NE 1999051400099 19990514 00099 NM 1999 5 14 DL72S991013 1 19990508 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805EA 9108 22436 FWD F/C EMER EXIT LIGHT STROBES INOP DURING TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999051400100 19990514 00100 NE 1999 5 14 DL76S991016 2 19990508 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 FAILED A DALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 27 135DL 43674 25145 580109 LEFT ENGINE FAILED AT 6,000 FT. CLIMBOUT EGT REACHED 1,100, LITE ENGINE VIBRATION FELT FOLLOWED BY EGT SPIKE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 1999051400101 19990514 00101 NM 1999 5 14 DL72S991019 1 19990509 A 3320 BALLAST 9781 BOEING 727 727225 1384077 NM CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 805EA 22436 AFT CABIN AISLE FLUORESCENT LIGHTING (OVERHEAD) WAS SMOKING AND HAD ELECTRICAL SMELL WITH SPARKING. UPON INSPECTION CEI LING RAFTER C/B WAS POPPED. REPLACED LIGHT BALLAST. 2 L 7 3 4F A3WE 1999051400102 19990514 00102 NM 1999 5 14 DL72S991020 1 19990416 A 5753 652163367 SKIN BOEING 727 727225 1384077 NM LT TE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 LOWER L/E SKIN WORN APPROX 3 INCH LONG AREA O/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999051400103 19990514 00103 NM 1999 5 14 DL72S991021 1 19990510 A 5720 65162906 FITTING BOEING 727 727225 1384077 NM RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 DURING RTN INSP OF THE RT MLG BEAM FWD SUPPORT FITTING, CORROSION WAS FOUND ON THE INNER SURFACE OF THE MLG ATTACHMENT B OLT BORE. FINAL DIAMETER OF 1.875 WAS NEEDED TO REMOVE ALL DAMAGE. REPAIRED PER ERA 333106-14, REV A. 2 L 7 3 4F A3WE 1999051400104 19990514 00104 NM 1999 5 14 DL72S991022 1 19990510 A 5530 STRINGER BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 VERT STAB S7 WAS FOUND CRACKED AT STA 157.2 DURING INSPECTIONS PER SI 4-59253-12AD. REPAIRED PER ERA 333133-14AD. 2 L 7 3 4F A3WE 1999051400105 19990514 00105 NM 1999 5 14 DL72S991023 1 19990507 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL AT THE STRINGER 4L SKIN LAP SPLICE REVEALED 8 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNA L ALUMINUM DOUBLER PER ER/A 367344-14AD. 2 L 7 3 4F A3WE 1999051400106 19990514 00106 NM 1999 5 14 DL72S991024 1 19990508 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS ALONG THE PANEL. THE SKIN LAP WAS COMPLETELY CUTOUT AND R EPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367345-14AD. 2 L 7 3 4F A3WE 1999051400107 19990514 00107 NM 1999 5 14 DL72S991025 1 19990508 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 700-720 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS. ONE CRACK WAS NOTED BETWEEN FS 700 AND 720 AND 3 CRACKS WERE NOTED BETWEEN FS 720A AND 720B. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS PER B727 SRM 53-30-03, FIG 5 AND ER/A 367346-14. 2 L 7 3 4F A3WE 1999051400108 19990514 00108 WP 1999 5 14 SCNA99503 1 19990509 A 3520 SWITCH DOUG DC10 DC1015 3022118 WP CABIN OXYGEN SYS FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, 2 ANEROID SWITCHES FOR THE PASSENGER OXYGEN SYSTEM FAILED TEST FOR SCA WORK CARD X1036 . THE SUBJECT ANEROID SWITCHES 2 WERE REMOVED AND REPLACED PER MM 352102, OPERATION CHECK WAS GOOD. 2 L 7 3 4F A22WE 1999051400109 19990514 00109 WP 1999 5 14 SCNA99504 1 19990509 A 5730 SKIN DOUG DC10 DC1015 3022118 WP RT WING CHAFED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, THE RIGHT LEADING EDGE SKIN ARB1074 WAS FOUND TO BE CHAFED AT STA XOS 551 TO XOS 555 W ITH .043 REMAINING OF ORIGINAL THICKNESS OF .063. THE SUBJECT LEADING EDGE WAS REPAIRED PER SRM 571000 FIG 15 AND EO 57 -5678-1. 2 L 7 3 4F A22WE 1999051400110 19990514 00110 WP 1999 5 14 SCNA99505 1 19990510 A 5511 SPAR DOUG DC10 DC1015 3022118 WP LT HORIZ STAB CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, THE LEFT HORIZONTAL STABILIZER OUTBOARD SECTION UPPER SPAR CAP FORWARD WAS FOUND CRACK ED AT THE FORWARD CLOSING RIB PLANE THE CRACK WAS APPROXIMATELY 4.40 INCHES WHICH EXCEED ALLOWABLE LIMITS PER SB DC10 55 -24. THE SUBJECT SPAR CAP WAS REMOVED, A REPAIR CAP WAS FABRICATED AND INSTALLED IAW SRM 55-20-00 FIG 8 VOL I AND SCA E O 5556711. 2 L 7 3 4F A22WE 1999051400111 19990514 00111 WP 1999 5 14 SCNA99506 1 19990510 A 5320 ANGLE DOUG DC10 DC1015 3022118 WP BS 567-595 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, THE 'L' ANGLE AT STATION 567 TO 595 AT LONGERON 44L WAS FOUND TO HAVE CORROSION AND M ATERIAL LOSS WAS GREATER THAN 20 PERCENT THE ORIGINAL THICNESS WAS .090 AND FOUR AREAS AFTER WERE .060 AND .074 AND .072 AND .073. THE SUBJECT CORROSION WAS REMOVED AND BLENDED 'L' ANGLES WERE FABRICATED AND INSTALLED IAW DC10 SRM 53-10-00 , 53-00-01 SCA EO 5356841 AND DIMENSION EA DC10 5310 0027. 2 L 7 3 4F A22WE 1999051400112 19990514 00112 WP 1999 5 14 SCNA99507 1 19990507 A 3350 BATTERY PACK DOUG DC10 DC1015 3022118 WP ROW 8-15 DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE CHECK, THE EMERGENCY PATH LIGHTING WAS FOUND TO BE INOPERATIVE FROM SEAT 8L TO 15L AND 8R TO 15R. REMOVED AND REPLACED THE BATTERY PACK PER MEXICANA EO 1033014, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 1999051400113 19990514 00113 WP 1999 5 14 SCNA99508 1 19990510 A 3260 SENSOR DOUG DC10 DC1015 3022118 WP LT MLG MISINSTALLED A SCNA L ABORTED APPROACH N W FALSE WARNING INADEQUATE Q C AP APPROACH 1 GL 15 154SY 48259 DURING A HEAVY MX CHECK TEST FLT, THE LT MAIN GEAR UNSAFE RED LIGHT ILLUM WHILE ROTATING AND EXTINGUISHED IN FLIGHT. TH E CREW TROUBLESHOT AND RETURNED TO POINT OF ORIGIN. THE FLT CREW VERIFIED THE DOWN POSITION WITH THE VIEWING PORTS, BRI EFED THE PASSENGERS AND INFORMED THE TOWER. CONDUCTED APPROACH AND REQUESTED A VISUAL VERIFICATION FROM THE TOWER OF TH E DOWN POSITION OF THE SUBJECT GEAR. LANDED ON THE SECOND APPROACH WITHOUT INCIDENT. THE PROXIMITY SENSOR FOR DOWN AND LOCK FOR THE LT MAIN GEAR WAS INSTALLED INCORRECTLY. THE SENSOR WAS REINSTALLED IAW SRM 326103, OPS CHECK OK. 2 L 7 3 4F A22WE 1999051400114 19990514 00114 NM 1999 5 14 SCNA99706 1 19990417 A 3233 BEAM BOEING 727 727282 138408T NM NLG ACTUATOR CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING A HEAVY MAINTENANCE CHECK, FOUND NOSE LANDING GEAR ACTUATOR SUPPORT BEAM LEFT HAND FORWARD MOUNT WITH DEEP PITTED CORROSION. REMOVED SUPPORT IAW B727 SRM 513002. CORROSION WAS FOUND OUT OF LIMITS IAW 727 SRM 531001. FOUND MATERIAL TO BE 7075 T6 IAW WITH CONDUCTIVITY TEST B727 SRM 511003. FABRICATED NEW PART IAW B727 SRM 511003. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 1999051400121 19990514 00121 CE 1999 5 14 99ZZZX1931 1 19990426 A 7930 LINE BEECH 18 E18S 1151006 CE COCKPIT LEAKING A KKFA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 16SL BA65 OIL LEAK IN COCKPIT. FOUND OIL LINE TO OIL PRESSURE GAUGE WITH A HOLE WORN IN IT. REPLACED LINE, LEAK CHECKS GOOD. RE COMMENDATION: INSPECT ALL LINES CAREFULLY FOR CHAFING. 1 L 7 2 3R A765 1999051400127 19990514 00127 SO 1999 5 14 WVBA00699 1 19990413 A 5280 4752932 HINGE 4752931 PIPER PA31 PA31350 7103110 SO RT MLG DOOR CRACKED A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 792FC 317552108 RIGHT MAIN LANDING GEAR FORWARD INNER DOOR HINGE BROKEN. REPLACED BROKEN HINGE. (X) 1 L 7 2 3O A20SO 1999051400128 19990514 00128 EA 1999 5 14 WVBA00799 2 19990401 A 8550 7708 REGULATOR 77808 PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA CRANKCASE LEAKING A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3527U 665 317952141 L515561A OIL WAS OBSERVED ON SIDE OF COWLING ON POST-FLIGHT AND IN THE BOTTOM OF COWL. ALSO, AFTER REMOVING COWL, OIL WAS OBSERV ED COMING FROM AROUND THE THREADS OF OIL PRESSURE REGULATOR. REGULATOR WAS REPLACED. (X) 1 L 7 2 3O 3 O A20SO E14EA 1999051400137 19990514 00137 CE 1999 5 14 99ZZZX1945 1 19990413 A 2121 714709 MOTOR 8259HR2 CESSNA 310 310R 2074245 CE BLOWER FAILED A CZUA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 25 69610 214 6984 310R0102 ON A 135 FLIGHT, PILOT REPORTED ODOR IN CABIN. INITIATED PRECAUTIONARY LANDING UNEVENTFULLY. UPON LANDING, PILOT NOTED HEATER CIRCUIT BREAKER TRIPPED. INVESTIGATION REVEALED HEATER COMBUSTION AIR MOTOR FROZEN. INSTALLED OVERHAULED MOTOR . HEATER OPERATED NORMALLY. NO FURTHER ODOR NOTED. AS THE CIRCUIT BREAKER OPERATED NORMALLY, THERE WAS NEVER ANY THRE AD OF FIRE. 1 L 7 2 3O 3A10 1999051400141 19990514 00141 NM 1999 5 14 SWAA990801 1 19990503 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED C3 CHECK, FOUND NR 6 SLAT I/B END CRACKED BETWEEN 3 RIVET HOLES. REPAIRED SLAT PER SWA RA NR 1-357-068 6. 2 L 7 2 4F RT A16WE 1999051400142 19990514 00142 NM 1999 5 14 SWAA990802 1 19990503 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM RT EMER EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED BC4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999051400143 19990514 00143 NM 1999 5 14 SWAA990803 1 19990503 A 3350 6556633 LENS BOEING 737 7373H4 1384600 NM LT EMER EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED BC4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999051400144 19990514 00144 NM 1999 5 14 SWAA990804 1 19990503 A 5330 6552880 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SWA RA NR 1-353-2073. 2 L 7 2 4F RT A16WE 1999051400145 19990514 00145 NM 1999 5 14 SWAA990805 1 19990503 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED BC4 CHECK, FOUND NR 6 SLAT CRACKED NEXT TO ACTUATOR CUT OUT. REPAIRED SLAT ASSY PER SRM AND SWA RA NR 1-357-0687. 2 L 7 2 4F RT A16WE 1999051400146 19990514 00146 NM 1999 5 14 SWAA990806 1 19990504 A 3350 079123 COVER BOEING 737 7372H4 138448C NM ROW 11 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTING COVER CRACKED NEXT TO SEAT ROW 11. REMOVED AND R EPLACED COVER PER MM. 2 L 7 2 4F A16WE 1999051400147 19990514 00147 NM 1999 5 14 SWAA990807 1 19990504 A 5312 951440 BULKHEAD STRAP BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND CENTER SUPPORT STRAP CRACKED AT BS 178 BULKHEAD, WL 188. REPAIRED STRAP PER SRM. 2 L 7 2 4F RT A16WE 1999051400148 19990514 00148 NM 1999 5 14 SWAA990808 1 19990504 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT FLOORBEAM BS 860 LBL 12- RBL 2.5. REPAIRED BEAM PER SWA RA NR 1-A53-202 1. 2 L 7 2 4F RT A16WE 1999051400149 19990514 00149 NM 1999 5 14 SWAA990809 1 19990504 A 5720 65C27043 STRAP BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND LT WING UPPER STRAP FWD OF AILERON CRACKED. REMOVED AND REPLACED STRAP PER SRM. 2 L 7 2 4F RT A16WE 1999051400150 19990514 00150 NM 1999 5 14 SWAA990810 1 19990504 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED BC1 CHECK, FOUND FLOOR PROXIMITY LIGHTING TRACK LOOSE FWD OF AFT GALLEY. REATTACHED TRACK PER MM. 2 L 7 2 4F RT A16WE 1999051400151 19990514 00151 NM 1999 5 14 SWAA990794 1 19990503 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM ROW 13-14 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 COVER MISSING ON EMERGENCY EXIT LIGHT BY OVERHEAD BIN BETWEEN ROWS 13-14. INSTALLED LENS COVER PER MM. 2 L 7 2 4F RT A16WE 1999051400152 19990514 00152 1999 5 14 SWAA990795 4 19990503 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM ESCAPE SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR SLIDE PACK CABLE ROUTED INCORRECTLY. REROUTED CABLE PER MM. 2 L 7 2 4F A16WE 1999051400153 19990514 00153 NM 1999 5 14 SWAA990796 1 19990503 A 5743 65C36545 FITTING BOEING 737 7373H4 1384600 NM LT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND REAR SPAR ATTACH FITTING CRACKED AT LEFT MAIN LANDING GEAR BEAM STABILIZER LINK, FWD END. REMOVED AND REPLACED ATTACH FITTING PER SRM. 2 L 7 2 4F RT A16WE 1999051400154 19990514 00154 NM 1999 5 14 SWAA990797 1 19990503 A 5712 654544555 RIB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD CRACKED BETWEEN STRINGERS 2 AND 3. REPAIRED RIB PER SWA RA N R 1-357-0677. 2 L 7 2 4F RT A16WE 1999051400155 19990514 00155 NM 1999 5 14 SWAA990798 1 19990503 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND 2 CRACKS AT BS 178 BULKHEAD LBL 5 - RBL 5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999051400156 19990514 00156 NM 1999 5 14 SWAA990799 1 19990503 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY DOORWAY FWD GIRT BAR LATCH FITTING CORRODED. REMOVED AND REPLACED FITTING PER OHM. 2 L 7 2 4F RT A16WE 1999051400157 19990514 00157 NM 1999 5 14 SWAA990800 1 19990503 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D-CHECK, FOUND CORROSION ON BS 344 FLOORBEAM LBL 38, 31 AND 12 INSIDE CABIN. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999051400158 19990514 00158 NM 1999 5 14 SWAA990785 1 19990501 A 5315 6623737 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 667 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND CRACK EXTENDING FROM OVAL CUTOUT OF FLOORBEAM, BS 667, LBL 24.75 UNDER SEAT TRACK. R EPAIRED BEAM PER SWA RA NR 1-357-0680. 2 L 7 2 4F RT A16WE 1999051400159 19990514 00159 NM 1999 5 14 SWAA990786 1 19990501 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 714 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED BC1 CHECK, FOUND KEEL BEAM PANEL CRACKED APPROX 1 INCH LONG AT LT SIDE OF BS 714. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999051400160 19990514 00160 NM 1999 5 14 SWAA990787 1 19990501 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM BS 299-333 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D-CHECK, FOUND A CREASE AT FUSELAGE SKIN, BS 299 TO 333, ABOVE STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999051400161 19990514 00161 NM 1999 5 14 SWAA990788 1 19990501 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED SERVICE CHECK, FOUND L-2 DOOR ESCAPE SLIDE PRESSURE GAGE READING LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999051400162 19990514 00162 NM 1999 5 14 SWAA990789 1 19990501 A 5320 6545409 WEB BOEING 737 7373H4 1384600 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND CRACK AT PRESSURE WEB, BS 665, LBL 34. REPAIRED WEB PER SWA RA NR 1-353-2072. 2 L 7 2 4F RT A16WE 1999051400163 19990514 00163 NM 1999 5 14 SWAA990790 1 19990502 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 3 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED C3 CHECK, FOUND NR 3 LE SLAT LOWER SKIN CRACKED ON AFT RIVET ROW, 5 INCHES FWD OF ACTUATOR ATTACH POINT . REPAIRED SLAT ASSY PER SWA RA NR 1-357-0685. 2 L 7 2 4F RT A16WE 1999051400164 19990514 00164 NM 1999 5 14 SWAA990791 1 19990502 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED 1/4D CHECK, FOUND A CRACK AT BS 178 BULKHEAD RBL 6. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999051400165 19990514 00165 NM 1999 5 14 SWAA990792 1 19990502 A 5315 6546569 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AROUND FASTENER HOLES AT BS 947, LBL 5-RBL 5. REPAIRED FLOORB EAM PER SRM. 2 L 7 2 4F RT A16WE 1999051400166 19990514 00166 NM 1999 5 14 SWAA990781 1 19990501 A 2910 BACH8A06 LINE BOEING 737 7372H4 138448C NM RT MLG BRAKE FAILED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 74SW 22674 AIR TURNBACK - AFTER TAKEOFF, EXPERIENCED TOTAL LOSS OF 'A' HYDRAULIC SYSTEM, ALL OTHER SYSTEMS OPERATED NORMAL. REPLAC ED RUPTURED NR 3 BRAKE ASSY LINE PER MM. 2 L 7 2 4F A16WE 1999051400167 19990514 00167 NM 1999 5 14 SWAA990782 1 19990501 A 2424 948F4585 GCU BOEING 737 7373H4 1384600 NM NR 2 FAILED A SWAA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 07 321SW 23342 NR 2 GENERATOR DROPPED OFF THE LINE. APU SWITCHED AND POWER RESUMED NORMAL. APPROX 4 MINUTES LATER NR 2 GENERATOR BUS POWER DROPPED OFF THE LINE AND IT WOULD NO LONGER POWER. FLIGHT ATTENDANT REPORTED A LOUD GRINDING NOISE AND WHAT THEY DESCRIBED AS A ENGINE BACKFIRING. APU GEN BUS VOLTS AND FREQUECY WERE NORMAL, APU AMP GAGE WAS FLUCTUATING. SHUT DOWN APU AND DIVERTED TO BHM. REMOVED AND REPLACED NR 2 ENGINE GENERATOR CONTROL UNIT, OPS CKD GOOD PER MM. 2 L 7 2 4F RT A16WE 1999051400168 19990514 00168 NM 1999 5 14 SWAA990783 1 19990503 A 8012 10609242 CONNECTOR BOEING 737 7372H4 138448C NM PWA JT8 JT8* 52044 NE NR 1 ENGINE FAILED A SWAA E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 83SW 22732 674648 INFLIGHT ENGINE SHUT DOWN, AIR RETURN WITH THE NR 1 ENGINE SHUT DOWN DUE TO START VALVE OPEN LIGHT ILLUMINATED. REMOVED AND REPLACED START VALVE AND OPEN LIGHT REMAINED ON AFTER ENG START. FOUND START VALVE CANNON PLUG CONNECTOR BAD. REM OVED AND REPLACED CONNECTOR, OPS CKD GOOD PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999051400169 19990514 00169 NM 1999 5 14 SWAA990784 1 19990501 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999051400170 19990514 00170 NM 1999 5 14 SWAA990793 1 19990503 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 EMERGENCY FLOOR TRACK LIGHTING COVER CAME OFF AT MID CABIN. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999051400182 19990514 00182 NM 1999 5 14 GAIA99037 1 19990306 A 7930 BYPASS LIGHT BOEING 727 727223 1384074 NM NR 2 ENGINE ILLUMINATED A GAIA E ENGINE SHUTDOWN Y ENGINE STOPPAGE DE DESCENT 1 SW 07 6807 19482 ATL/JFK - DURING INITIAL DESCENT, OIL FILTER BYPASS LIGHT ILLUMINATED ON NR 2 ENGINE. PRIOR TO SHUT DOWN, OIL PRESSURE 45 PSI, OIL TEMP 102 DEGREES CELSIUS. FUEL HEAT HAD BEEN APPLIED FOR 1 MINUTE. CREW FOLLOWED OIL BYPASS LIGHT ILLUMINA TION PROCEDURES. LIGHT EXTINGUISHED WITH REDUCTION IN THRUST. AFTER APPROX 1 MINUTE, LIGHT CAME ON AND STAYED ON. PRE CAUTIONARY SHUT DOWN OF ENG CARRIED OUT. CREW DECLARED AN EMERGENCY INTO JFK, MADE AN UNEVENTFUL LANDING. MAINT ACCOMP LISHED NR 2 ENGINE OIL FILTER INSPECTION. NO METAL FOUND. THE FILTER WAS CLEANED AND REPLACED. ENGINE RUN CARRIED OUT AND FILTER WAS LEAK CHECKED GOOD. OIL FILTER BYPASS LIGHT REMAINED OUT. ACCOMPLISHED IAW BOEING 727 MM 79-33-00. (X) 2 L 7 3 4F A3WE 1999051400189 19990514 00189 SO 1999 5 14 C2XA99CL025 1 19990306 A 2120 AIR DIST EMB 145 EMB145ER SO CABIN ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 12946 145052 CLE - FLT 4007 - CREW REPORTED THEY RECEIVED SMOKE IN THE COKPIT AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEMS AND FOUND THE SMOKE WAS CAUSED BY EXCESSIVE AMOUNTS OF DE- ICE FLUID IN THE APU COMPARTMENT. THE COMPARTMENT WAS CLEANED AND THE OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-145 MM 21-00-06. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999051400190 19990514 00190 SO 1999 5 14 C2XA99IA155 1 19990222 A 3350 GE1317 BULB EMB 145 EMB145 SO LT OVERWING FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14959 145091 IAH - FLT 4206 - CREW INFORMED MAINTENANCE THE LEFT OVERWING FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE LIGHT BULB AS REQUIRED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999051400191 19990514 00191 SO 1999 5 14 C2XA99CL024 1 19990306 A 3230 MLG EMB 145 EMB145ER SO MLG WW CONTAMINATED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15948 145056 CLE - FLT 4115 - CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A LANDING GEAR DISAGREEMENT WARNING. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND LARGE QUANTITIES OF SNOW AND I CE IN THE WHEELWELLS. THE SNOW AND ICE WAS CLEANED OUT AND THE LANDING GEAR OPERATIONAL CHECKS WERE SATISFACTORY IAW EM B-145 MM 32-32-00. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999051400192 19990514 00192 EU 1999 5 14 C2XA99IA154 1 19990213 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 EFD - DURING LINE CHECK INSPECTION, THE FORWARD AND AFT AISLE PATH EMERGENY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACKS IAW ATR 42-500 JIC 33-51-21, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999051400193 19990514 00193 EU 1999 5 14 C2XA99IA183 1 19990306 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU EMERGENCY EXIT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED BATTERY PACK IAW ATR 42-500 JIC 33-51-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999051400194 19990514 00194 WP 1999 5 14 99ZZZX1955 2 19990128 A 7321 89737519 FUEL CONTROL WOODWARD BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110 01514 WP RT ENGINE MALFUNCTIONED A C37A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 05 650JX 1155 1711070 650 P42107 RIGHT ENGINE TORQUE WOULD ONLY REACH 96 PERCENT AT FULL POWER. REPLACED RT ENGINE FUEL CONTROL UNIT. 2 L 7 2 4T 4 T RT A21EU E4WE 1999051400196 19990514 00196 EA 1999 5 14 99ZZZX1957 2 19990214 A 7320 3031829 PE LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE BROKEN A FFSA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 01 575P UC95 PCE32327 KTN/FAI - EN ROUTE, RIGHT ENGINE TORQUE WENT TO ZERO. N1 STABLE AT IDLE. FUEL FLOW NORMAL FOR IDLE. POWER LEVER AND C ONDITION LEVER HAD NO EFFECT. DIVERTED TO JUNEAU. REPLACED P1 LINE. 2 L 7 2 4T 4 T RT A24CE E4EA 1999051400197 19990514 00197 NM 1999 5 14 99ZZZX1958 1 19990315 A 3350 O13071BPEGTL BULB DHAV DHC8 DHC8103 1386005 NM EMERGENCY EXIT FAILED A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806WP 357 EMERGENCY PATH LIGHT IS OUT AT FORWARD EMERGENCY EXIT. REMOVED AND REPLACED LAMP. 2 H 7 2 4T RT A13NM 1999051400198 19990514 00198 EA 1999 5 14 MASA99037 1 19990303 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 17231 7231 RDU/BOS - FLT 5816 - APPROXIMATELY 15 MINUTES OUT OF BOS, THE NR 1 FORWARD WINDSHIELD CRACKED. AIRCRAFT LANDED WITHOUT INCIDENT AND DID NOT DECLARE AN EMERGENCY. MAINTENANCE INSPECTED THE WINDSHIELD AND NOTED 15 INCHES OF VERTICAL CRACKIN G IN THE MIDDLE PLY AND 3 TO 4 INCHES OF CRACKING IN THE INNER PLY. MAINTENANCE REPLACED THE WINDSHIELD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999051400200 19990514 00200 CE 1999 5 14 RU3A9903 1 19990329 A 6120 SCREW BEECH 90 F90 1152909 CE PROPELLER SHEARED A RU3A K NONE O OTHER IN INSP/MAINT 1 SW 21 18 LA145 AT PROPELLER CHANGE RUN-UP, SAFETY SCREW WHICH HOLDS DOWN LINK PIN TO LINK ARM SHEARED OFF CAUSING THE BLADE TO MOVE INT O FEATHER. (X) 1 L 7 2 4T A31CE 1999051400201 19990514 00201 NM 1999 5 14 UIEA9916 1 19990405 A 5311 FRAME BOEING 747 747228F 1384895 NM BS 1319 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 536MC 21576 INSPECTION OF STA 1319 FRAME REVEALED CORROSION ABOVE THE LEFT HAND LONGERON BEAM. THE AREA WAS REPAIRED IAW ATLAS AIR EO 4753A085. (X) 2 L 7 4 4F A20WE 1999051400202 19990514 00202 NM 1999 5 14 UIEA9914 1 19990314 A 3411 41071 HOSE BOEING 747 747271C 1384869 NM LT PITOT SYSTEM LEAKS A UIEA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 539MC 21965 MIA/AMS - ATB - FLT GT1878/14 - CAPTAIN'S ALTIMETER WAS OBSERVED TO BE 500 FEET IN ERROR ON TAKEOFF AND CLIMB COMPARED T O THE F/O'S STANDBY ALTIMETER INDICATORS. INDICATOR READ -980 FEET ON TOUCH DOWN. ALSO, CAPTAIN'S MACH/AIRSPEED INDICA TOR STICKS AT 164 IAS. DUMPED 71.6 KGS OF FUEL AND RETURNED TO MIA. DURING TROUBLESHOOTING, FOUND LEAK IN CAPTAIN'S PI TOT SYSTEM. ISOLATED PROBLEM TO FLEX LINE BEHIND LT UPPER PITOT PROBE. IPC REF 34-11-05, FIG 4 ITEM 12, P/N 17071. RE PLACED FLEX LINE, PITOT/STATIC AND OPERATIONAL CHECK NORMAL. (X) 2 L 7 4 4F A20WE 1999051400203 19990514 00203 1999 5 14 UHLA99284 4 19990224 A 3454 5203137317 RMI DHAV DHC8 DHC8311 1386006 EA NR 2 MALFUNCTIONED A UHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 03 803SA 9229 221 FLT 111 - LG TO ORF - CREW NOTICED A SLIGHT SMOKE SMELL FOLLOWED BY THE NR 2 RMI CIRCUIT BREAKER TRIPPING. THE SMELL CL EARED WITH THE RMI BREAKER OUT. FLIGHT CONTINUED NORMALLY TO DESTINATION WITH NO FURTHER SMELL OR DISCREPANCY. MAINTEN ANCE DEFERRED NR 2 RMI AND TIE WRAPPED THE CIRCUIT BREAKER. INSPECTION CONFIRMED NO FAULTS OR SHORTS ON RMI WIRING. AI RCRAFT CONTINUED IN SERVICE. 2-26-99. REMOVED AND REPLACED NR 2 RMI. OPERATIONAL CHECKS GOOD. CLEARED MEL. ALL OPER ATIONS NORMAL. TEAR DOWN REPORT SHOWS BURNED COIL AND BAD SWITCHES AND FUSE. POINTERS WERE FOUND STICKY. (X) 2 H 7 2 4T RT A13NM 1999051400204 19990514 00204 EA 1999 5 14 VTZA99017 1 19990219 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA RT COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 633BR 7274 ORD/CRW - DURING CRUISE ON 2-17-99 AT 1430 HOURS, EXPERIENCED A SHATTERING OF THE FIRST OFFICER'S MIDDLE PANE OF THE WIN DSHIELD. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED INTO CVG. AIRCRAFT LANDED WITH NO PROBLEM. MAINTENANCE CONTRO L WAS NOTIFIED AND AIRCRAFT MAINTENANCE WAS DISPATCHED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S WINDSHIELD IAW APPLICABLE MAINTENANCE PUBLICATIONS PROCEDURES. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1999051400205 19990514 00205 NM 1999 5 14 W7NR9900002 1 19990310 A 2612 1061096114 FIRE LOOP BOEING 737 7372Y5 1384554 NM NR 2 ENGINE FAILED A W7NA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 NM 07 921WA 23039 LAS - FLT 518 - NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ENGINE OVERHEAT CHECKLIST. ACCOMPLISHED ENGINE FI RE SEVERE DAMAGE OR SEPARATION CHECKLIST. USED BOTH FIRE EXTINGUISHERS. REMOVED AND REPLACED BOTH ENGINE FIRE BOTTLES IAW MM 26-21-11. INSPECTED ENGINE FOR FIRE SCORCHING, OVERHEATING, AND HOT DUCT PROBLEMS. NO INDICATIONS OF OVERHEAT C ONDITIONS. INSPECTED FIRE LOOP AND FOUND ELEMENT GROUNDED TO SHIELD. REMOVED CENTER CONDUCTOR AWAY FROM SHIELD. CHECK ED GOOD PER MM 26-11-0. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4U RT A16WE 1999051400206 19990514 00206 WP 1999 5 14 TWAA9906601 1 19990506 A 3350 58222 POWER SUPPLY DOUG DC9 DC934 302207E WP ROW 8 INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 936L 47711 THE FORWARD OVERHEAD COACH EMERGENCY LIGHTS WERE DIM. REPLACED THE POWER SUPPLY FOR FORWARD OVERHEAD LIGHTS, AND SECURE D THE GROUND STUD FOR LIGHT AT ROW 8. CHECK-C 6-17-98 STL. 2 L 7 2 4F RT A6WE 1999051400207 19990514 00207 WP 1999 5 14 TWAA9906602 1 19990505 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 THE UPPER FUSELAGE LONGERON 5R HAD .25 IN CRACK AT FASTENERS, STA 699. REPAIRED CRACK IN LONGERON 5R PER SRM 53-02, FIG 18. CHECK-C 9-4-98 STL. 2 L 7 2 4F A6WE 1999051400208 19990514 00208 WP 1999 5 14 AT9900357 1 19990422 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 389-427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND AN EXISTING SKIN REPAIR DOUBLER AT THE FORWARD CARGO DOOR THRESHOLD, FORWAR D AND AFT CORNERS AT BS 389-427 CORRODED. FABRICATED AND INSTALLED REPAIR TRIPLERS AT FORWARD AND AFT CORNERS IAW DC9 S RM 53-05 FIG 105 ( -7009 AND -7011 ) AND RES NR 99849. 2 L 7 2 4F A6WE 1999051400209 19990514 00209 WP 1999 5 14 AT9900358 1 19990428 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 332-370 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD SKIN PANEL DENTED AND CRACKED AT BS 332-370 L23-25R. CUT OUT D ENT AREA, COLD WORKED REMAINING DENTS. FABRICATED AND INSTALLED REPAIR DOUBLER, INCORPORATING AN EXISTING DOUBLER IAW D C9 SRM 51-30-1, 51-10-2, 53-04 FIG 12B PAGE 9 (CLASS 2 REPAIR), AND RES NR 991014. 2 L 7 2 4F A6WE 1999051400210 19990514 00210 WP 1999 5 14 AT9900359 1 19990329 A 5320 ANGLE DOUG DC9 DC932 3022066 WP GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND IN THE AFT GALLEY WORK AREA UNDER THE COFFEE AND SNACK DOOR AN ANGLE CORROD ED. REMOVED ANGLES FOR ACCESS, FABRICATED NEW REPAIR U CHANNEL, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED TWO EA CH ANGLES AND U CHANNEL IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, 51-30-5 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1999051400211 19990514 00211 WP 1999 5 14 AT9900360 1 19990504 A 5313 5920302501 LONGERON DOUG DC9 DC932 3022066 WP BS 757 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A LONGERON CORRODED ON THE LOWER FLANGE AT BS 757 L29R. REMOVED AND REPLAC ED LONGERON WITH REPAIR FITTING IAW DC9 SRM 51-10-4, 51-30-2, 53-03 FIG.24, AND 51-30-1. 2 L 7 2 4F A6WE 1999051400212 19990514 00212 WP 1999 5 14 AT9900361 1 19990502 A 5321 1A471681 FLOOR DOUG DC9 DC932 3022066 WP BS 170-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION ON THE SUB FLOOR AT BS 170-200 RBL 55. CUT OUT CORRODED PORTION OF SUB FLOOR. FORMED NEW DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED DOUBLER IAW DC9 SRM 51-10-4, 51-10- 3, 51-30-2, AND 53-20-1 FIG 804. 2 L 7 2 4F A6WE 1999051400213 19990514 00213 WP 1999 5 14 AT9900362 1 19990422 A 5321 1A471301 FLOOR DOUG DC9 DC932 3022066 WP BS 130 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE COCKPIT FLOOR BOARD JUST AFT OF FIRST OFFICER SEAT BOTTOM SEAT TRACK AT BS 130 LBL 20 CORRODED. FABRICATED REPAIR FLOOR BOARD. CUT, TRIMMED, DRILLED HOLES, DEBURRED, COUNTERSUNK, TREATED, P RIMED, AND INSTALLED HAT CHANNELS IAW DC9 SRM 53-21-0, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999051400214 19990514 00214 WP 1999 5 14 AT9900363 1 19990422 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-238 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR BOARD SUPPORT BRACKET AT BS 200-238 LBL 18 CORRODED ON TOP AND BO TTOM. FABRICATED REPAIR FLOOR BOARD SUPPORT, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-30-1, 53- 11-1, 51-10-2, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999051400215 19990514 00215 WP 1999 5 14 AT9900364 1 19990506 A 3350 110049 BATTERY CHARGER DOUG DC9 DC932 3022066 WP CABIN DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 815AT 47443 FOUND THE AFT SECTION OF THE EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPACED BATTERY CHARGER IAW MM 33-54-0, OPS CHE CKED GOOD. 2 L 7 2 4F A6WE 1999051400216 19990514 00216 SO 1999 5 14 LR7A9927 1 19990412 A 5330 3417453 PANEL LKHEED 382 382G 526414U SO BS 140.5-160 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND BATTERY COMPARTMENT UPPER PANEL CRACKED AND GOUGED FS 140.5 TO 165. REPAIRED BY FABRICATING AND INSTALLING A REPAIR PANEL IAW SPAR MPP L100-404-99-065. LAC MEA 382-24-99-071. 2 H 7 4 4T A1SO 1999051400217 19990514 00217 SO 1999 5 14 LR7A9928 1 19990412 A 5330 3631451R PANEL LKHEED 382 382G 526414U SO BS 497-517 MISDRILLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND NEW REPLACEMENT FS 497 TO 517 RT FWD PRESSURE PANEL WITH MISDRILLED HOLES, BEL OW MINIMUM EDGE DISTANCE. REPAIRED BY TRIMMING OUT DAMAGED AREA AND INSTALLING REPAIR DOUBLER IAW SPAR MPP L100-404-9-0 69. LAC MEA 382-57-99-79. 2 H 7 4 4T A1SO 1999051400218 19990514 00218 SO 1999 5 14 LR7A9929 1 19990412 A 5330 3631451R PANEL LKHEED 382 382G 526414U SO BS 477 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND NEW REPLACEMENT FS 477 RT FWD PRESSURE PANEL SUB STRUCTURE ATTACH REQUIRES INS TALLATION OF HL37PB6 PINS AND KFN542-3 COLLARS IN LIEU OF STANDARD MS90353-06 BLIND BOLTS DUE PANEL PRELOAD. INSTALLED PINS AND COLLARS IAW SPAR MPP L100-404-99-071. LAC MEA 382-57-99-80. 2 H 7 4 4T A1SO 1999051400219 19990514 00219 SO 1999 5 14 LR7A9930 1 19990412 A 5320 FITTING LKHEED 382 382G 526414U SO BS 474 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53262, FOUND FS 477 LT FWD END FITTING CRACKED AT WL 145, LBL 61. REPAIRED PE R SMP 583 53-40-40. NR 183. 2 H 7 4 4T A1SO 1999051400220 19990514 00220 SO 1999 5 14 LR7A9931 1 19990412 A 5320 FITTING LKHEED 382 382G 526414U SO BS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53262, FOUND FS 617 LT AFT END FITTING CRACKED AT WL 145, LBL 61. REPAIRED PE R SMP 583 53-40-40. 2 H 7 4 4T A1SO 1999051400221 19990514 00221 SO 1999 5 14 LR7A9932 1 19990412 A 5320 33050202 CAP LKHEED 382 382G 526414U SO BS 245-345 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC05397, FOUND LT FWD CHINE CAP CORRODED FS 245 TO 345E. REPLACED LT FWD CHINE C AP IAW SMP 583 AND DWG 3305020. NR 188. 2 H 7 4 4T A1SO 1999051400222 19990514 00222 SO 1999 5 14 LR7A9933 1 19990412 A 5320 3723519 CAP LKHEED 382 382G 526414U SO BS 597-737 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC 0529,7 FOUND TH AFT FS 597 TO 737 CHINE CAP CORRODED. REPLACED CHINE CAP PER SMP 583 53-40-01. NR 189. 2 H 7 4 4T A1SO 1999051400223 19990514 00223 SO 1999 5 14 LR7A9934 1 19990412 A 5320 37234919 CAP LKHEED 382 382G 526414U SO BS 357-517 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND FS 357 TO 517 LT CHINE CAP CORRODED. REPLACED CHINE CAP IAW SMP 5 83 52-60 AND DWG 372342. NR 190. 2 H 7 4 4T A1SO 1999051400224 19990514 00224 NM 1999 5 14 PCAA9900010 1 19990429 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PASSENGER DOOR OUT OF ADJUST A PCAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 13 817EX 191 PHL FLT 3810 - AIRSTAIR DOOR WAS DIFFICULT TO OPEN WHEN DEPLANING PASSENGERS. MAINTENANCE INSPECTED AND FOUND THE DOOR LIFT MECHANISM AT FAULT. ADJUSTED IAW BOMBARDIER PROCEDURES CHAPTER 52. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999051400225 19990514 00225 NM 1999 5 14 PCAA9900011 1 19990504 A 5210 BUMPER DHAV DHC8 DHC8102 2809003 NM PASSENGER DOOR OUT OF POSITION A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 840EX 327 MHT FLT 3758 - PASSENGER DOOR HANDLE RECESSED. UNABLE TO OPEN DOOR FROM THE OUTSIDE. MAINTENANCE INSPECTED, FOUND RUBB ER BUMPER FOR HANDLE AT FAULT. SHIMMED BUMPER, OPERATED DOOR SEVERAL TIMES, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999051400226 19990514 00226 NM 1999 5 14 UPS99529522 1 19990506 A 2910 HYD LINE BOEING 757 75724APF 1384969 NM CARGO DOOR CHAFED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 01 444UP 27389 INSPECTION TYPE:N/A, ON DESENT RECIEVED A LEFT HYD QTY EICAS MESSAGE, NOTICED QTY WAS ABOUT HALF FULL AND DECREASING. A FTER LANDING MX FOUND A HYD LINE TO CARGO DOOR MANUAL PUMP HAD A HOLE WHERE ELEC PUMP WIRE BUNDLE CHAFED IT. ALSO, FOUN D NR 1 AND NR 3 LT ELEC HYD PUMP WIRES BURNED FROM ARCING WHERE IT RUBBED ON HYD LINE. REPAIRED HYD LINE IAW MM 20-10-0 9, LEAK CHECK GOOD. REPAIRED WIRES IAW MM 20-10-13, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1999051400227 19990514 00227 WP 1999 5 14 UPS99829519 1 19990418 A 5320 BASE DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C CRACKED BASE FOR LEFT GEAR WELL HYD. RESERVOIR OUTBOARD FWD SIDE CRACK PREVIOUSLY REPAIRED IAW DC-8 S RM57-2-0, DOUBLER WAS INSTALLED. 2 L 7 4 4F RT 4A25 1999051400228 19990514 00228 WP 1999 5 14 UPS99829520 1 19990419 A 5720 FITTING DOUG DC8 DC873F 302199F WP BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C2 LONG 24 RT UPPER FITTING AT FS 940 HAS CORROSION AT BOTTOM ATTACHMENT HOLES. REMOVED CORRODED FITTIN G, LOCATE NEW FITTING DRILL REAMED EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51-1 -20D,CP CP. 2 L 7 4 4F RT 4A25 1999051400229 19990514 00229 WP 1999 5 14 UPS99829521 1 19990419 A 5720 FITTING DOUG DC8 DC873F 302199F WP BS 879 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C2 RT LONG 24 UPPER FITTING AT FS 879 HAS CRACK AT ATTACHMENT HOLES. REMOVED CRACK FITTING, LOCATE NEW FITTING, DRILL, AND REAM EXISTING HOLES IN FITTING IAW DC-8 SRM 51-3-2 AND INSTALLED IAW DC-8 SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1999051400230 19990514 00230 WP 1999 5 14 UPS99829523 1 19990405 A 5347 5750864565 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 HEAVY CORROSION ON SEAT TRACK FS 600, RBL 24. REMOVED CORRODED SEAT TRACK, FS 580 - 610. FABRICATED , AND REPLACED SEAT TRACK IAW SRM 53-2-3, CPCP. 2 L 7 4 4F RT 4A25 1999051400231 19990514 00231 WP 1999 5 14 UPS99829524 1 19990411 A 5320 J0602969 CUSP DOUG DC8 DC873F 302199F WP BS 390-400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 LT CUSP AT FS 390 TO 400, THE UPPER SURFACE IS CORRODED BEYOND LIMITS. REMOVED CUSP BEAM FROM FS 370 TO 470. FABRICATED CUSP AND REPAIR ANGLES IAW SRM 53-2-5 FIG 15A. CPCP 2 L 7 4 4F RT 4A25 1999051400232 19990514 00232 WP 1999 5 14 UPS99829525 1 19990409 A 5720 37048411 FITTING DOUG DC8 DC873F 302199F WP WS 74.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 INBD SIDE OF THE XRS 74.5 BULKHEAD, THE STR 51 FWD END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20 AND 51-1-23. 2 L 7 4 4F RT 4A25 1999051400233 19990514 00233 WP 1999 5 14 UPS99829526 1 19990426 A 5320 37558471 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 1220 FRAME, FWD FLANGE AT LONGERON 33R IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FITTIN G IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999051400234 19990514 00234 WP 1999 5 14 UPS99829527 1 19990418 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, HEAVY CORROSION ON T FITTING, FS 660 AT LONG 36. REPAIRED FITTING IAW DHC SK880-110. CPCP 2 L 7 4 4F RT 4A25 1999051400235 19990514 00235 WP 1999 5 14 UPS99829528 1 19990503 A 5320 577991321 DOUBLER DOUG DC8 DC873F 302199F WP BS 610 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FS 610, LONGERON 31L TO 31R, THE FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5779913 AND SRM 51-1-21. CPCP 2 L 7 4 4F RT 4A25 1999051400236 19990514 00236 WP 1999 5 14 UPS99829529 1 19990418 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 40 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 EXTERIOR FUSELAGE SKIN CRACKED AT FS 40, LONGERON 30L AT DOOR CUTOUT. CUT OUT DAMAGED AREA AND REPAI RED IAW SRM 53-2-0 FIG 13. 2 L 7 4 4F RT 4A25 1999051400237 19990514 00237 WP 1999 5 14 UPS99829530 1 19990419 A 5510 FITTING DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C2 LEFT HORIZONTAL STAB AT STA X 70 APPROX 18 INCHS IN FRONT OF SPAR VERTICAL SUPPORY FITTING CRACKED. R EMOVED AND REPLACED FITTING DOUBLER IAW DC-8 SRM 55-2-0. 2 L 7 4 4F RT 4A25 1999051400238 19990514 00238 WP 1999 5 14 UPS99829531 1 19990416 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C LEFT WHEEL WELL FITTING AT STA 880, LONG 24R CORRODED DOT M940. REMOVED CORRODED FITTING FABRICATED R EPAIR ANGLES IAW DC-8 SRM 53-2- 0, ALODINED AND PRIMED REPAIRED PARTS IAW DC-8 SRM 51-1-8. CUT NEW FITTING IAW DC-8 SRM 53-2-0 AND INSTALLED FITTING AND REPAIRED ANGLES IAW DC-8 SRM 51-1-20D. CPCP 2 L 7 4 4F RT 4A25 1999051400239 19990514 00239 WP 1999 5 14 UPS99829532 1 19990416 A 5320 FITTING DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C RT WHEEL WELL TRAP FITTING CRACKED IN AFT WEB DOT M942. REMOVED CRACKED TRAP FITTING, REPLACED TRAP F ITTING AS PER JOB CARD NR 90432100 (UPS NR 929640). 2 L 7 4 4F RT 4A25 1999051400240 19990514 00240 WP 1999 5 14 UPS99829533 1 19990503 A 5320 577991323 STRAP DOUG DC8 DC873F 302199F WP BS 610 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FS 610, LONGERON 31L TO 31R, THE STRAP IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED STRAP IAW DWG 5779913 CPCP. 2 L 7 4 4F RT 4A25 1999051400241 19990514 00241 WP 1999 5 14 UPS99829534 1 19990416 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C RT WHEEL WELL LONG 24R CRACKED AT STA 940 DOT M-944. REMOVED CRACKED LONGERON, REPLACED LONGERON 24R AS PER JOB CARD NR 904 53100. 2 L 7 4 4F RT 4A25 1999051400242 19990514 00242 WP 1999 5 14 UPS99829535 1 19990414 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1080 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C GILINER NUT PLATES INSTALLED INCORRECTLY AT STA 1080 LONG 34-35 1100, LONG 32-33R. REMOVED DAMAGE, AN D FABBED DOUBLER, STRAP AND FILLER IAW REO-06431 A ND DWG NR DC-8-53-229, LOCATED DRILLED PARTS PER DC-8 SRM 51-3-2. REP A IRS IAW DC-8 SRM 51-1-20D AND REO-0641 AND DWG. DC-8-53-229. 2 L 7 4 4F RT 4A25 1999051400243 19990514 00243 WP 1999 5 14 UPS99829536 1 19990423 A 5330 561537271 SKIN DOUG DC8 DC873F 302199F WP BS 1240-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FUSELAGE SKIN AT FS 1240 TO 1280, APPROX LONG 33R, AT THE D-PIT DOOR CUT OUT IS CRACKED AND HAS HEAVY CORROSION. REMOVED AND REPLACED THE SKIN IAW SRM 51-1-20D AND 51-3-0. CPCP 2 L 7 4 4F RT 4A25 1999051400244 19990514 00244 WP 1999 5 14 UPS99829537 1 19990421 A 5510 564431021 DOUBLER DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LT HORIZ STAB INBD SIDE OF THE STA XE 221.0 FRAME IS CRACKED AND TORN. REMOVED, FABRICATED, AND INST ALLED FINGER DOUBLER IAW DWG 5644310 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999051400245 19990514 00245 WP 1999 5 14 UPS99829538 1 19990427 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 38.75-45 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 RT WING L/E LWR SURFACE BETWEEN XFS 38.75 AND 45.00 IS CORRODED BEYOND LIMITS. REPAIRED IAW DHC SK88 0-933. CPCP 2 L 7 4 4F RT 4A25 1999051400246 19990514 00246 WP 1999 5 14 UPS99829539 1 19990427 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XFS 710 IS CRACKED BETWEEN SCREW HOLES. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087B. 2 L 7 4 4F RT 4A25 1999051400247 19990514 00247 WP 1999 5 14 UPS99829540 1 19990422 A 5320 37502571 SPLICE DOUG DC8 DC873F 302199F WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LONGERNON 31L SPLICE AT FS 450 IS CRACKED. REMOVED AND REPLACED SPLICE IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999051400248 19990514 00248 WP 1999 5 14 UPS99829541 1 19990423 A 5530 WEB DOUG DC8 DC873F 302199F WP VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 VERT STAB BASE, FS 1781 THROUGH 1818, RT WEB BETWEEN THE CENTER AND REAR SPARS HAS HEAVY EXFOLIATION CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 51-1-9A. CPCP 2 L 7 4 4F RT 4A25 1999051400249 19990514 00249 WP 1999 5 14 UPS99829542 1 19990418 A 5320 37504972 FITTING DOUG DC8 DC873F 302199F WP FRAME 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FRAME 660 ATTACH FITTING AT LONG 36 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999051400250 19990514 00250 EU 1999 5 14 QXEA9901013 1 19990504 A 2150 2046002 PACK FOKKER F28 F28MK4000 4990810 EU NR 1 INOPERATIVE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 486US 3985 11237 SEA - AFTER TAKEOFF, SMOKE DETECTOR IN LAVATORY SOUNDED. FLIGHT ATTENDANT OBSERVED A LIGHT HAZE IN CABIN. AFTER 4 MINU TES THE SMOKE DETECTOR STOPPED, HAZE DISAPPEARED. AFTER LANDING, GROUND RUN AIRCRAFT AT POWER, CYCLED NR 1 PACK, NOTICE D ACRID SMELL. WITH NR 1 OFF, NO ACRID SMELL. PLACED NR 1 PACK ON MEL. AT BOI, REMOVED AND REPLACED NR 1 PACK. OPER ATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999051400251 19990514 00251 NM 1999 5 14 QXEA9901014 1 19990505 A 2422 DHC103024600CS2B INVERTER DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTION A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 831PH 18035 328 SEA - STRANGE ODOR NOTED IN COCKPIT. MAINTENANCE FOUND SMELL TO BE COMING FROM PRIMARY INVERTER. REPLACED INVERTER. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999051400252 19990514 00252 EU 1999 5 14 QXEA9900942 1 19990402 A 5720 STRAP FOKKER F28 F28MK4000 4990810 EU WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - SCREW GOUGE IN LOWER WING BUTT STRAP AT FORWARD END. REPAIRED IAW HORIZON AIR EA 4-57-226, STEP 2. 2 L 7 2 4F RT A20EU 1999051400253 19990514 00253 EU 1999 5 14 QXEA9900943 1 19990322 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERT STAB DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - DENT ON LEFT SIDE OF VERTICAL STAB AFT OF LEADING EDGE. REPAIRED IAW HORIZON AIR EA 4-55-122. 2 L 7 2 4F RT A20EU 1999051400254 19990514 00254 EU 1999 5 14 QXEA9900944 1 19990324 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 19275-19525 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - DENT IN FUSELAGE BELLY SKIN AT STATION 19275 TO 19525. REPAIRED IAW HORIZON AIR EA 4-53-683A. 2 L 7 2 4F RT A20EU 1999051400255 19990514 00255 EU 1999 5 14 QXEA9900945 1 19990418 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 18075 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION BETWEEN FRAME 18075 AND 17565 AT STRINGER 58. REMOVED SURFACE CORROSION, ALODINED AND PRIMED. 2 L 7 2 4F RT A20EU 1999051400256 19990514 00256 EU 1999 5 14 QXEA9900946 1 19990404 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT OUTBOARD PASSENGER SEAT TRACKS FROM SECTION 4875 TO 5305, FRAME 5305 TO FRAME 9805 AND FRAME 14285 TO FRAME 16535 REQUIRED REPLACEMENT. REPLACED IAW FOKKER SRM 51-31-01 AND 51-10-5. 2 L 7 2 4F RT A20EU 1999051400257 19990514 00257 EU 1999 5 14 QXEA9900947 1 19990414 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT INBOARD PASSENGER SEAT TRACK SECTIONS FROM FRAME 5305 TO 9805, FRAME 9802 TO 14285 AND FRAME 14285 AND 15635 REQUIRE REPLACEMENT. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400258 19990514 00258 EU 1999 5 14 QXEA9900948 1 19990324 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISMANUFACTURED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT DIMPLED LAP JOINT REPAIR DOES NOT CONFORM TO FOKKER DRAWING. REPAIRED IAW HORIZON AIR EA 4-53-738. 2 L 7 2 4F RT A20EU 1999051400259 19990514 00259 EU 1999 5 14 QXEA9900949 1 19990321 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT INBOARD SEAT TRACK SECTION BETWEEN SPLICES FRAME 14285 AND 15635 HAS LIGHT FRETTING CORROSION ON FLANGES ALON G ENTIRE LENGTH WITH ON PITTED AREA ON RIGHT FRAME. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999051400260 19990514 00260 EU 1999 5 14 QXEA9900950 1 19990319 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT INBOARD SEAT TRACK SECTION BETWEEN SPLICES FRAME 14285 AND 15635 HAS LIGHT FRETTING CORROSION ALONG ENTIRE L ENGTH OF FLANGE OF FLANGES AND TWO GOUGES IN LEFT FLANGE AT FRAME 14755. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTI ON 4, 2 L 7 2 4F RT A20EU 1999051400261 19990514 00261 EU 1999 5 14 QXEA9900951 1 19990412 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5305-9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT INBOARD SEAT TRACK SECTION BETWEEN FRAME 5305 AND 9805 HAS PITTING AND FRETTING CORROSION ON FLANGES ALONG E NTIRE LENGTH. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400262 19990514 00262 EU 1999 5 14 QXEA9900952 1 19990317 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 4875-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - RIGHT INBOARD SEAT TRACK SECTION BETWEEN FRAME 4875 AND 5305 HAS DEEP CORROSION ON FLANGES ALONG ENTIRE LENGTH. R EPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, SECTION 4, PARAGRAPH B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999051400263 19990514 00263 EU 1999 5 14 QXEA9900953 1 19990325 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - UPPER FORWARD CORNER OF SERVICE EMERGENCY DOOR CUTOUT HAS ON CRACK APPROXIMATELY 1.5 INCHES LONG. REPAIRED IAW HO RIZON AIR EA 4-53-703. 2 L 7 2 4F RT A20EU 1999051400264 19990514 00264 EU 1999 5 14 QXEA9900954 1 19990410 A 5320 SILL FOKKER F28 F28MK4000 4990810 EU PAX DOORWAY CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - MAIN CABIN DOOR SILL FORWARD LOWER CORNER IS CHAFED. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999051400265 19990514 00265 EU 1999 5 14 QXEA9900955 1 19990316 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 4805-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - LEFT INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF TRACK BETWEEN FRAME 4805 AND 5305. REPAIRED IAW FOK KER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999051400266 19990514 00266 EU 1999 5 14 QXEA9900956 1 19990331 A 5320 INTERCOSTAL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CUT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - INTERCOSTAL CUT ON FLANGE ADJACENT TO INNER SKIN. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400267 19990514 00267 EU 1999 5 14 QXEA9900957 1 19990310 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - INNER SKIN REINFORCE CLIP CUT AT FLANGE ADJACENT TO INNER SKIN. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400268 19990514 00268 EU 1999 5 14 QXEA9900958 1 19990403 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FRAME 16660 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - MAIN CABIN FLOORBEAM STRUCTURE IS DISTORTED BETWEEN FRAME 16660 AND 16060. REPAIRED IAW HORIZON AIR EA 4-53-713. 2 L 7 2 4F RT A20EU 1999051400269 19990514 00269 EU 1999 5 14 QXEA9900959 1 19990318 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY FRAME 16060 LEFT OUTBOARD CABIN FLOOR SUPPORT HAS CORROSION AT LOWER NUT PLATE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. 2 L 7 2 4F RT A20EU 1999051400270 19990514 00270 EU 1999 5 14 QXEA9900960 1 19990325 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY FRAME 16060 THE CASTELLATION AT STRINGER 74 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1999051400271 19990514 00271 EU 1999 5 14 QXEA9900961 1 19990323 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - AFT CARGO BAY FRAME 16060, THE CASTELLATION OUTBOARD OF STRINGER 4 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400272 19990514 00272 EU 1999 5 14 QXEA9900963 1 19990319 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON FRAME 9305A AT STRINGER 11, TOP SURFACE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 4, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999051400273 19990514 00273 EU 1999 5 14 QXEA9900964 1 19990323 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON FRAME 9305 BETWEEN STRINGER 2 AND 72. REPAIRED IAW HORIZON AIR EA 4-53-721. 2 L 7 2 4F RT A20EU 1999051400274 19990514 00274 EU 1999 5 14 QXEA9900965 1 19990324 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON FRAME 8805 AND STRINGER 1 TO 74, UNDER NUT PLATES. REPAIRED IAW HORIZON AIR EA 4-53-720. 2 L 7 2 4F RT A20EU 1999051400275 19990514 00275 EU 1999 5 14 QXEA9900966 1 19990319 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 6305-6565 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 497US 11173 PDX - CORROSION ON INSIDE OF SKIN AT ANTENNA MOUNTING AREA BETWEEN FRAME 6565 AND 6305 AND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999051400276 19990514 00276 NM 1999 5 14 99FDEA00167 1 19990506 A 3260 SWITCH DOUG MD11 MD11F 3023600 NM LANDING GEAR INOPERATIVE A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 620FE 48791 99-101 - GEAR LWR AT 2300 ABOVE GROUND LEVEL. ALL GEAR UNSAFE POS. REMOVED AND REPLACED LANDING GEAR POSITION SWITCH P ER MM 32-61-04-4. OPS CK NORM. 2 L 7 3 4F RT A22WE 1999051400277 19990514 00277 NM 1999 5 14 99FDEA00168 1 19990506 A 3260 694710566 PANEL BOEING 727 727233 138408A NM RT MLG INTERMITTENT A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 275FE 22040 99-102 - RIGHT MAIN GEAR LIGHT FLICKERING, CYCLED GEAR UP TEST LIGHT. RM GREEN WOULD NOT TEST. CK CIRCUIT BREAKERS AND REPLACED BULBS GEAR THEN IND DOWN AND LOCK. TROUBLE SHOT AS PER BOEING MM 727-32-61-001-1 CK GOOD. RIGHT GREEN DOWNLO CK WILL NOT PRESS TO TEST. REMOVED AND REPLACED LAND GEAR LIGHT PANEL. OPER CK GOOD. 2 L 7 3 4F RT A3WE 1999051400278 19990514 00278 NM 1999 5 14 99FDEA00169 1 19990506 A 3260 B2732012601 ACCESSORY UNIT BOEING 727 72725 1384006 NM LANDING GEAR MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 504FE 18274 99-103 - WITH GEAR HANDLE UP HAD RED GEAR UNSAFE LIGHT ON FRONT CONSOLE ON 2ND OFF ANNUNCIATOR PNL LEFT, RIGHT AND NOSE DOOR LIGHT OUT WITH TAILSKID LIGHT ON. CYCLED GEAR HAND AND IND OK. REMOVED AND REPLACED LANDING GEAR ELECTRICAL MODUL E PER B727-100 MM 32-09-111-4. SYS OPER CK NORM. 2 L 7 3 4F A3WE 1999051400279 19990514 00279 NM 1999 5 14 99FDEA00170 1 19990507 A 2910 LINE BOEING 727 7272S2F 1384O81 NM B HYD SYST CHAFED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 210FE 22932 99-104 - LOST 'B' SYS HYD FLUID AND PRESS ON TAXI IN. A/C TOWED IN. INSTALLED NEW HYD PRESS LINE FROM NR 1 B PUMP TO B : MODULE PER 727-200 STANDARD MM 12-12-000. OPERATIONAL AND LEAK CK GOOD. 2 L 7 3 4F A3WE 1999051400280 19990514 00280 1999 5 14 99FDEA00171 4 19990507 A 3417 HG480B13 CADC BOEING 727 727233 138408A NM NR 1 FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 222FE 20933 99-105 - CAPT AIRSPEED, ALTIMETER AND VSI INSTR MALFUNCTION AFT T/O. REMOVED AND REPLACED NR 1 CADC AS PER MM 34-12-011 -4, SYS OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1999051400281 19990514 00281 EU 1999 5 14 99FDEA00172 1 19990508 A 3230 RETRACT MECH AIRBUS 300 A300F4605R 3930327 EU RT MLG DIRTY A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 672FE 779 99-106 - A/C DRIVEN OFF TAXI-WAY BY FLT CREW, RIGHT MAIN GEAR ASSY BAGGED IN GRD. CLEANED GEAR AND INSPECTED AS PER 32- 40-00-06. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999051400282 19990514 00282 WP 1999 5 14 ABXA9900349 1 19990429 A 3234 SELECTOR DOUG DC8 DC863 302198A WP LANDING GEAR LACK OF LUBE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 823AX 46122 DURING CLIMB, UNSATISFACTORY GEAR UPLATCH CHECK WITH NOSE GEAR NOT LATCHED LIGHT ILLUMINATED. PERFORMED ALTERNATE UPLAT CH CHECK PROCEDURE. FOUND LANDING GEAR LEVER STIFF AND HARD TO GO IN UPLATCH DETENT. CLEANED AND LUBED LEVER MECHANISM . OPS CHECKED GOOD. PERFORMED ADJ/TEST NOSE LANDING GEAR CONTROL VALVE IAW DC-8 MM 32-32-11. OPS CHECKED GOOD. PERFO RMED GEAR SWING IAW DC-8 SMM 32-60-0. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999051400283 19990514 00283 WP 1999 5 14 MWEA99254 1 19990501 A 5320 99579101 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 446 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 THE INTERCOSTAL IS BENT AND DAMAGED AT STATION 446 IN FORWARD CARGO COMPARTMENT. MAINTENANCE FABRICATED AND INSTALLED N EW INTERCOSTAL. 2 L 7 2 4F A6WE 1999051400284 19990514 00284 WP 1999 5 14 MWEA99255 1 19990507 A 5320 3915132505 FITTING DOUG DC9 DC932 3022066 WP RT MLG BRAKE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 THE RIGHT WHEEL WELL FITTING IS CRACKED INBOARD OF AFT END OF THE BRAKE VALVE BRACKET. MAINTENANCE FABRICATED AND INSTA LLED NEW FITTING. 2 L 7 2 4F A6WE 1999051400285 19990514 00285 WP 1999 5 14 MWEA99256 1 19990428 A 5230 952008945 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE AFT CARGO DOOR OUTER PAN IS CRACKED AT THE FORWARD LOWER STOP AREA. MAINTENANCE FABRICATED AND INSTALLED DOUBLER RE PAIR. 2 L 7 2 4F A6WE 1999051400286 19990514 00286 WP 1999 5 14 MWEA99257 1 19990505 A 5210 5914121SSN PAN DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE MAIN CABIN DOOR PAN IS CRACKED AT AFT SIDE OF NR 1 BEAM. MAINTENANCE FABRICATED AND INSTALLED NEW PAN. 2 L 7 2 4F A6WE 1999051400287 19990514 00287 WP 1999 5 14 MWEA99258 1 19990502 A 5210 5910075 DOUBLER DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 THE PASSENGER DOOR HOLD OPEN HOOK POCKET EXTERNAL DOUBLER IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPA IR. 2 L 7 2 4F A6WE 1999051400288 19990514 00288 WP 1999 5 14 MWEA99259 1 19990504 A 5330 59114004 SKIN DOUG DC9 DC932 3022066 WP BS 110 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 THE RIGHT SIDE OF FUSELAGE AT STATION 110 HAS A SMALL CRACK THROUGH A FASTENER. MAINTENANCE FABRICATED AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F A6WE 1999051400289 19990514 00289 WP 1999 5 14 MWEA99260 1 19990505 A 5280 5913421 DOUBLER DOUG DC9 DC932 3022066 WP NLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 THE LEFT AFT NOSE GEAR DOOR HINGE CUT OUT DOUBLER PLATE IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR . 2 L 7 2 4F A6WE 1999051400290 19990514 00290 WP 1999 5 14 MWEA99261 1 19990505 A 5280 5913421 DOUBLER DOUG DC9 DC932 3022066 WP NLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 THE RIGHT AFT NOSE GEAR DOOR HINGE CUT OUT DOUBLER PLATE IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAI R. 2 L 7 2 4F A6WE 1999051400291 19990514 00291 NM 1999 5 14 MWEA99262 1 19990507 A 2560 11320 GIRT BAR DOUG MD88 MD88 3023688 NM GALLEY DOORWAY LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE AFT GALLEY SERVICE DOOR GIRT BAR IS HARD TO INSERT. MAINTENANCE CLEANED AND LUBED GIRT BAR LATCH. 2 L 7 2 4F RT A6WE 1999051400292 19990514 00292 NM 1999 5 14 MWEA99263 1 19990506 A 2560 100502121 SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOORWAY DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 808ME 48070 ASSEMBLY WHICH HOLDS THE COVER IN PLACE FOR THE AFT GALLEY DOOR EVACUATION SLIDE CAME OFF. MAINTENANCE INSTALLED SLIDE RELEASE PIN. 2 L 7 2 4F RT A6WE 1999051400293 19990514 00293 NM 1999 5 14 MWEA99264 1 19990506 A 2560 100502121 SLIDE DOUG MD88 MD88 3023688 NM SERVICE DOORWAY DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 809ME 48071 AFT GALLEY EVAC SLIDE COVER CAME OFF. MAINTENANCE REINSTALLED. 2 L 7 2 4F RT A6WE 1999051400294 19990514 00294 NM 1999 5 14 SCNA99705 1 19990426 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 312 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING A HEAVY MAINTENANCE CHECK, FOUND CORROSION OUT OF LIMITS ON FLOORBEAM AT BS312 BL0. REMOVED CORROSION IAW SRM 51 1006, OUT OF LIMITS PER SRM 531001. CUTOUT DAMAGED AREA IAW SRM 514004. FABRICATED REPAIR DOUBLER FROM EXTRUSION BAC14 902831 7075 T6 IAW SRM 514004. TREATED AND PRIMED IAW SRM 511002 AND MM 512002. INSTALLED REPAIR IAW SRM 514004 AND 51 3002. 2 L 7 3 4F A3WE 1999051400295 19990514 00295 WP 1999 5 14 DHL9980743C 1 19990317 A 5720 36435001 FITTING DOUG DC8 DC873F 302199F WP WS 46 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, CENTER WING TANK, THROUGH LOWER ACCESS PANEL 516A RT SIDE BAY ON STA 46 STR 67 UPPER AREA CRACK ON FITTING APPROX 1 LONG. REMOVED AND FABRICATED FITTING PER DER DRAWING MHA 3123 AND INSTALLED PER SRM 51-120D. N/R 1234 2 L 7 4 4F RT 4A25 1999051400296 19990514 00296 WP 1999 5 14 DHL9980744C 1 19990405 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, NR 1 ENG LEFT T/R COWL BLOCKER DOOR COMPT INLET L/E SECTION AT 6 O' CLOCK POSITION CRACKED. STOP DRILLED CR ACK, FABRICATED REPAIR DOUBLER AND FILLER PER SRM 78-30-00. N/R 1238 2 L 7 4 4F RT 4A25 1999051400297 19990514 00297 WP 1999 5 14 DHL9980745C 1 19990322 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, NR3 ENG I/B T/R FAN COWL FWD MATING FLANGE HAS CRACK AT 12 O'CLOCK. CUT OUT DAMAGED AREA. FABRICATED REAPI R ANGLE 3.5 BY 3.5 FT AND FILLER 3 BY 1.5 PER EO18R78310191. N/R 1160. 2 L 7 4 4F RT 4A25 1999051400298 19990514 00298 WP 1999 5 14 DHL9980746C 1 19990321 A 5320 ANGLE DOUG DC8 DC873F 302199F WP COCKPIT MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, COCKPIT FLOOR PANEL 674A HAS MISSING FWD ANGLE. FABRICATED NEW ANGLE 1 BY 1.5 BY 10 PER SRM 51-121, N/R 10 36. 2 L 7 4 4F RT 4A25 1999051400299 19990514 00299 WP 1999 5 14 DHL9980747C 1 19990317 A 5210 ANGLE DOUG DC8 DC873F 302199F WP PASSENGER DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, AFT PASSANGER DOOR FWD LOWER CORNER HAS 1.75 CRACK INDICATION UNDER DOUBLER. REMOVED DOUBLER AND FOUND THRE E ANGLES CRACKED. FABRICTED DOUBLER ANGLE ANGLE SUPPORT AND SPLICE PER EO DN6 NR 18R5321092 . 2 L 7 4 4F RT 4A25 1999051400300 19990514 00300 WP 1999 5 14 DHL9980748C 1 19990315 A 5751 HINGE DOUG DC8 DC873F 302199F WP LT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LT WING AILERON HINGE NR 6 HAS CRACK ON AILERON MOUNT FLANGE. REMOVED HINGE AND INSTALLED NEW HINGE PER MM 27-10-1. N/R 896 2 L 7 4 4F RT 4A25 1999051400301 19990514 00301 WP 1999 5 14 DHL9980749C 1 19990315 A 5210 ANGLE DOUG DC8 DC873F 302199F WP PASSENGER DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, FWD PASSANGER UPPER DOOR HINGE POCKET HAS GOUGE ON METAL. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE 5 BY 6 AND INSTALLED. N/R 872 2 L 7 4 4F RT 4A25 1999051400302 19990514 00302 WP 1999 5 14 DHL9980750C 1 19990315 A 5321 FLOOR DOUG DC8 DC873F 302199F WP GALLEY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, GALLEY FLOOR PANEL HAS SURFACE CORROSION ON UPPER AND LOWER SIDES. ALSO, 2 CHANNEL FRAME ARE CRACKED STA 5- 25. CORROSION REMOVED ON PANEL AND WITHIN LIMITS AND REMOVED CHANNEL AND REPLACED PER SRM 51-1-21, 34.25 BY 4 N/R 64 7. 2 L 7 4 4F RT 4A25 1999051400303 19990514 00303 WP 1999 5 14 DHL9980751C 1 19990314 A 5240 DOOR DOUG DC8 DC873F 302199F WP SERVICE DOOR MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, UPPER FUS FWD SERVICE DOOR AT FWD TOP CORNER PREVIOUS REPAIR. REMOVED REPAIR AND INSTALLED DOUBLER PER SRM 53-2-0 N/R 741. 2 L 7 4 4F RT 4A25 1999051400304 19990514 00304 WP 1999 5 14 DHL9980752C 1 19990314 A 5210 DOOR DOUG DC8 DC873F 302199F WP PASSENGER DOOR MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, FWD ENTRY DOOR FWD TOP CORNER PREVIOUS REPAIR FS 25 LONG 10L. REMOVED PREVIOUS REPAIR AND FABRICATED AND I NSTALLED DOUBLER PER SRM 53-2-0. N/R 742. 2 L 7 4 4F RT 4A25 1999051400305 19990514 00305 WP 1999 5 14 DHL9980753C 1 19990314 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1761 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, AFT FUSELAGE LOWER EXTERIOR AREA AT STA 1761 ACCESS PANEL N-60 INTERIOR AREA AND LINKAGE HAS LIGHT SURFACE C ORROSION. REMOVED CORROSION, AREA OUT OF LIMITS. CUT OUT DAMAGED AREA, AND FABRICATED DOUBLER AND INSTALLED PER EO 18R 5311087. N/R 730 2 L 7 4 4F RT 4A25 1999051400306 19990514 00306 WP 1999 5 14 DHL9980754C 1 19990309 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 LEFT O/B FLAP AT T/E LOWER AREA O/B SECTION HAS DENT DAMAGE ON SURFACE STA XW 456.5. REMOVED DAMAGED SECTION. FABRICAT ED NEW SECTION AND INSTALLED PER SRM 51-1-21, 40 BY 10. N/R 261 2 L 7 4 4F RT 4A25 1999051400307 19990514 00307 WP 1999 5 14 DHL9980755C 1 19990309 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LT O/B FLAP L/E I/B LOWER SECTION HAS FASTENER HOLES ELONGATED. FABRICATED DOUBLER PER SRM 57-2-0, 3.375 B Y 2.5. N/R 267 2 L 7 4 4F RT 4A25 1999051400308 19990514 00308 WP 1999 5 14 DHL9980756C 1 19990313 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 190-200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LOWER FUS EXT FS 190 TO 200 LONG AND 35R BULGING CORROSION. REMOVED LONGERON, FABRICATED NEW SECTION 12 BY 1 FT AND INSTALLED PER SRM 51-120A. N/R 640 2 L 7 4 4F RT 4A25 1999051400309 19990514 00309 WP 1999 5 14 DHL9980757C 1 19990311 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 4 ENGINE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, NR 4 ENG T/R HALF CORE COWL SIDEWALL FWD AREA AT 12 O'CLOCK SKIN DAMAGED. REMOVED AND INSTALLED SERVICABLE T/R HALF PER MM 78-30-0. N/R 520 2 L 7 4 4F RT 4A25 1999051400310 19990514 00310 WP 1999 5 14 DHL9980758C 1 19990311 A 5312 BULKHEAD ANGLE DOUG DC8 DC873F 302199F WP AFT PRESS BLKHD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, UPPER CARGO COMPT AFT PRESS BULKHEAD RT FWD SIDE CEILING PANEL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE AND INSTALLED PER SRM 51-1-21, 4.5 BY 1 BY 1. N/R 448 2 L 7 4 4F RT 4A25 1999051400311 19990514 00311 WP 1999 5 14 DHL9980759C 1 19990310 A 5512 SKIN DOUG DC8 DC873F 302199F WP LT HORIZ STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LEFT HORIZONTAL STAB L/E UPPER AREA AT STA XFS 172.5, FOUND CORROSION UNDER SKIN SURFACE. CUT OUT DAMAGED AREA FABRICATED FILLERS AND REPAIR DOUBLER PER EO 18R5511079. INSTALLED FILLER S AND DOUBLER PER EO FILLER 4 BY 2 AND 1 BY 1, DOUBLER 5.75 BY 33. N/R 422 2 L 7 4 4F RT 4A25 1999051400312 19990514 00312 WP 1999 5 14 DHL9980760C 1 19990310 A 5512 SKIN DOUG DC8 DC873F 302199F WP LT HORIZ STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHEK, LEFT HORIZONTAL STA L/E I/B LOWER AREA AT STA XFS 60 FOUND CORROSION UNDER SKIN SURFACE. CUT OUT DAMAGED SE CTION, FABRICATED FILLER AND DOUBLER PER EO 18R5511080 AND INSTALLED PER SRM 51-1-8. N/R 426 2 L 7 4 4F RT 4A25 1999051400313 19990514 00313 WP 1999 5 14 DHL9980761C 1 19990311 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LEFT ELEVATOR T/E UPPER AREA AT STA XE 226 INTERM REPAIR ON SKIN. REMOVED REPAIR, CUT OUT DAMAGED AREA. FA BRICATED REPAIR DOUBLER, PER EO 18R5521081 AND INSTALLED PER EO REBALANCED PER SRM 51-4-4. N/R 428 2 L 7 4 4F RT 4A25 1999051400314 19990514 00314 WP 1999 5 14 DHL9980762C 1 19990317 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1350 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, AFT LOWER CARGO COMPT FS 1350 AND LONG 31L/32L AREA WITH BULGING CORROSION. CUT OUT DAMAGED SECTION OF SKIN PER EO 18R5331086. N/R 955 2 L 7 4 4F RT 4A25 1999051400315 19990514 00315 WP 1999 5 14 DHL9980763C 1 19990411 A 5523 TAB DOUG DC8 DC873F 302199F WP LT ELEVATOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LEFT ELEVATOR GEAR TAB IS DELAMINATED. REPAIRED AND INSTALLED PER MM 27-30-3. N/R 38. 2 L 7 4 4F RT 4A25 1999051400316 19990514 00316 WP 1999 5 14 DHL9980764C 1 19990307 A 5523 TAB DOUG DC8 DC873F 302199F WP RT ELEVATOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHEK, RT ELEVATOR CONTROL TAB DELAMIANTED. REMOVED ELEVATOR TAB AND OVERHAULED AND INSTALLED PER MM 27-30-00. N/ R 39 2 L 7 4 4F RT 4A25 1999051400317 19990514 00317 WP 1999 5 14 DHL9980765C 1 19990310 A 7830 TR UNIT DOUG DC8 DC873F 302199F WP NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, NR 2 ENGINE RT T/R HALF TOP BLOCKER DOOR COWL CORE FIXTURE CRACKED. REMOVED DAMAGED FITTING. REMOVED REVER SER FIXED STRUCTURE. REMOVED NR 2 T/R I/B HALF. INSTALLED SERVICABLE T/R UNIT PER MM 78-30-0. N/R 384 2 L 7 4 4F RT 4A25 1999051400318 19990514 00318 WP 1999 5 14 DHL9980766C 1 19990310 A 7830 TR UNIT DOUG DC8 DC873F 302199F WP NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, NR 3 ENG I/B T/R FAN COWL FWD UPPER SEAL TRACK AT 12 O' CLOCK POSITION IS CRACKED. REMOVED DAMAGED MOUNTING METAL RETAINER SEAL AT NR 3 ENGINE I/B T/R AT 12 O' CLOCK POSITION. FABRICATED SEAL RETAINER 1.5 BY 4.0 AND INSTALLED PER SRM 51-1-21. N/R 353 2 L 7 4 4F RT 4A25 1999051400319 19990514 00319 WP 1999 5 14 DHL9980767C 1 19990307 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 3 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, RT FLAP VANE FLAP PANEL NR 3 DELAMINATED. REMOVED VANE AND REPAIRED AND REINSTALLED PER MM 27-50-0.. 2 L 7 4 4F RT 4A25 1999051400320 19990514 00320 WP 1999 5 14 DHL9980768C 1 19990307 A 5752 TAB DOUG DC8 DC873F 302199F WP LT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LEFT WING AILERON TRIM TAB IS DELAMINATED. REMOVED AND REPLACED AILERON TAB AND RERIGGED PER MM 27-10-0. N /R 41 2 L 7 4 4F RT 4A25 1999051400321 19990514 00321 WP 1999 5 14 DHL9980769C 1 19990307 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 4 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 AT C CHECK, LEFT WING NR 4 FLAP VANE IS DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-51-14. N/R 42 2 L 7 4 4F RT 4A25 1999051400322 19990514 00322 1999 5 14 DHL99873004 4 19990505 A 2210 2588787904 TRANSDUCER DOUG DC8 DC873F 302199F WP YAW DAMPER FAILED A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 873SJ 46091 UNCOMMANDED RUDDER INPUTS, TURNED YAW DAMPER OFF AND NO SIGNIFICANT CHANGE. INSPECTED AND FOUND YAW CHANNEL COMPUTER F AILED SEVERAL TESTS. REMOVED AND REPLACED YAW COMP PER MM 22-11-1. ALSO, REMOVED AND REPLACED RUDDER POSITION TRANSDUC ER TRANSFORMER PER MM 27-21-0. OPS CHECKED GOOD. 2 L 7 4 4F RT 4A25 1999051400323 19990514 00323 WP 1999 5 14 TWAA9906701 1 19990509 A 2170 COALESCER BAG DOUG DC9 DC983 3022083 WP CABIN DIRTY A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 05 9619V 53566 ON TAKEOFF CABIN FILLED WITH SMOKE. FLIGHT RETURNED TO DTW. FOUND SMOKE COMING FROM APU AIR SYSTEM. PLACARD THE APU A IR INOPERATIVE PER MEL. CHECK-C 10-31-98 STL. *S/D* NO APU OIL LEAKS WERE FOUND. REPLACED THE WATER SEPARATOR BAGS A ND ACCOMPLISHED DUCT BURN OUT PROCEDURES. 2 L 7 2 4F RT A6WE 1999051400324 19990514 00324 WP 1999 5 14 TWAA9906702 1 19990424 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965. REPLACED LONGERON PER SRM 53-02 FIG 18 AND LONGERON ID ENTIFICATION 53-11-3. LONGERON REPLACED FROM STA 950 TO 996. 2 L 7 2 4F A6WE 1999051400325 19990514 00325 NM 1999 5 14 HNAA9900057 1 19990508 A 3610 SWITCH DHAV DHC8 DHC8201 2809001 NM NR 1 & 2 ENGINE FAILED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 986HA 421 TORQUE FLUX ON BOTH ENGINES FOLLOWED BY AN OIL SMELL. SHUT BOTH BLEEDS OFF AND IT STABILIZED FOR APPROXIMATELY 5 MINUTE S, THEN NR 2 TORQUE DECREASED TO 45 PERCENT. REPLACED NR 1 AND NR 2 HP BLEED SWITCHES (P/N 7G899) (S/N 356), (S/N 272) OFF. ALSO, FOUND NR 2 HP BLEED VALVE GASKET BLOWN. REPLACED GASKET. 2 H 7 2 4T RT A13NM 1999051400326 19990514 00326 WP 1999 5 14 AT9900365 1 19990504 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND SIX FLOORBOARD SUPPORT BRACKETS AT BS 160-218 BL 0-53R CORRODED ON TOP AND BOTTOM. FABRICATED SIX FLOORBOARD SUPPORT BRACKETS, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-4, 5 1-10-2, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999051400327 19990514 00327 WP 1999 5 14 AT9900366 1 19990428 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CABIN FLOOR PANEL NR 5857 CORRODED UNDER FASTENERS. FABRICATED, TREATED, PRIMED, AND INSTALLED CABIN FLOOR PANEL IAW DC9 SRM 51-01 FIG 1, 53-05 FIG 1, 51-10-2, 51-10-3, 51-30-2, AND 51-30-1. 2 L 7 2 4F A6WE 1999051400328 19990514 00328 WP 1999 5 14 AT9900367 1 19990502 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 761 & 763 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION BULGE ON LOWER BELLY SKIN AT BS 761.5 LBL 3 AND BS 763 RBL 6. F ABRICATED EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER AND INSTALLED IAW TIMCO LAKE CITY EO 99-1134. 2 L 7 2 4F A6WE 1999051400329 19990514 00329 WP 1999 5 14 AT9900368 1 19990509 A 2612 FIRE LIGHT DOUG DC9 DC932 3022066 WP CARGO COMPT ILLUMINATED A ZZDA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SO 15 823AT 47529 FORWARD CARGO DETECTION LIGHT ILLUMINATED DURING CRUISE. CHECKED PER CHECKLIST, AFTER TEST MAINTENANCE CONTROL AGREED W ITH CREW, VALID CARGO FIRE. FIRE TRUCKS MET AIRCRAFT, DETERMINED NO EVIDENCE OF FIRE. MAINTENANCE INSPECTED FORWARD CA RGO BIN RELAY, RADAR ALTIMETER BOX AND AREA, ELEVATOR SERVO COMPARTMENT, E & E COMPARTMENT, NO DEFECTS NOTED. FOUND PAS SENGER DUFFEL BAG WITH A POWDERED MILK CONTAINER WHICH HAD BURST OPEN POSSIBLY CAUSING FIRE WARNING. 2 L 7 2 4F A6WE 1999051400330 19990514 00330 NE 1999 5 14 AT9900369 2 19990506 A 7321 7436023 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE DEFECTIVE A ZZDA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 15 814AT 47486 NR 1 ENGINE EPR FLUCTUATES, N1 AND FUEL FLOW FOLLOW. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL IAW MM73-20-1. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1999051400331 19990514 00331 WP 1999 5 14 AT9900370 1 19990422 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 163 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN AT BS 163 L-3L DENTED. REPAIRED THE DENTED FUSELAGE SKI N BY COLD WORKING DENT AND REMOVING EXISTING REPAIR DOUBLER AND ENLARGING REPAIR DOUBLER TO INCORPORATE DENTED AREA IAW DC9 SRM 53-04 FIG 38, 51-10-2, 51-10-4, 51-10-3 AND RES 99846. 2 L 7 2 4F A6WE 1999051400332 19990514 00332 NM 1999 5 14 CAL9900495 1 19990507 A 5230 146N6619 SKIN BOEING 757 757224 1384958 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 AFT CARGO DOOR AFT LOWER CORNER SKIN HAS DAMAGE BEYOND SRM LIMITS. REPAIRED AFT CARGO DOOR AFT LOWER SKIN PER EC/RA 523 0-01464. 2 L 7 2 4F RT A2NM 1999051400333 19990514 00333 NM 1999 5 14 CALA9900491 1 19990507 A 5320 6518420 POST BOEING 737 7373T0 1384582 NM LT COCKPIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 CAPTAINS WIND SHIELD OUTBOARD UPPER CORNER OF POST HAS .375 INCH CRACK. INSTALLED REPAIR DOUBLERS AND FILLER PER EC/RA 5330-02806. 2 L 7 2 4F RT A16WE 1999051400334 19990514 00334 WP 1999 5 14 CALA9900492 1 19990508 A 5220 39146641 RETAINER DOUG DC9 DC982 3022082 WP LT EMER EXIT DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 LEFT FORWARD EMERGENCY EXIT DOOR CORROSION FOUND AT LOWER AFT CORNER SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER PER SRM 51-30-2. 2 L 7 2 4F A6WE 1999051400335 19990514 00335 NM 1999 5 14 CALA9900493 1 19990509 A 5315 6545838 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 951 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 FLOOR SUPPORT (CABIN) HAS CORROSION AT STA 951 RBL 47. REPLACED PER EC/RA 5310-03585. 2 L 7 2 4F RT A16WE 1999051400336 19990514 00336 NM 1999 5 14 CALA9900494 1 19990507 A 5230 146N6619 SKIN BOEING 757 757224 1384958 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 AFT CARGO DOOR FORWARD CORNER SKIN (LOWER) IS CRACKED (1). REPAIRED PER SRM 5230-01464. 2 L 7 2 4F RT A2NM 1999051400337 19990514 00337 WP 1999 5 14 CALA9900496 1 19990507 A 5347 593056671 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1136-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 SEAT TRACK NR 2 CORROSION AT NUT PLATE HOLES FROM STA 1136 - 1174. REPLACED SEAT TRACK LEFT CENTER STA 1079 - 1305 PER SRM 51-30-01. 2 L 7 2 4F A6WE 1999051400338 19990514 00338 WP 1999 5 14 CALA9900498 1 19990507 A 5240 BOTTLE DOUG DC10 DC1030 3023501 WP L4 DOOR BLOWN A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 17085 47957 DOOR 4L DOOR ASSIST BOTTLE BLOWN. RESET HANDLE AND SERVICED DOOR ASSIST BOTTLE, OPERATES NORMAL. 2 L 7 3 4F A22WE 1999051400339 19990514 00339 NM 1999 5 14 CALA9900499 1 19990507 A 5313 BAC1498158 STRINGER BOEING 737 7373T0 1384582 NM BS 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 STRINGER 26L IS CORRODED FROM STA 500 TO 500D ALONG WITH STRINGER ATTACH CLIP AT STA 500D FORWARD CARGO PIT. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A16WE 1999051400340 19990514 00340 WP 1999 5 14 CALA9900500 1 19990507 A 5240 DOUBLER DOUG DC9 DC982 3022082 WP AFT SERV DOOR CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 35836 49441 AFT SERVICE DOOR DOUBLER AROUND HOLD OPEN HOOK CRACKED (1) OUTER SKIN. INSTALLED DOUBLER REPAIR PER EC/RA 5205-01008. 2 L 7 2 4F A6WE 1999051400341 19990514 00341 NM 1999 5 14 CALA9900501 1 19990506 A 5320 65C807351 ANGLE BOEING 737 7373T0 1384582 NM BS 907-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 R2 DOOR THRESHOLD Z ANGLE CORRODED STA 907 - 986. REMOVED AND REPLACED R-2 Z ANGLE PER SRM 51-10-02. 2 L 7 2 4F RT A16WE 1999051400342 19990514 00342 WP 1999 5 14 CALA990497 1 19990507 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 FORWARD CORGO DOOR JAMB PAN LOWER SECTION IS CORRODED. INSTALLED SPLICE REPAIR ON DOOR JAMB PER SRM 53-05 FIG 44. 2 L 7 2 4F A6WE 1999051400343 19990514 00343 SO 1999 5 14 COMA9910073 1 19990505 A 2611 SMOKE DETECTOR EMB 120 EMB120RT SO LAV MALFUNCTIONED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 164D 120164 LAV SMOKE DETECTOR ACTIVATED. F/A AND PASSENGERS REPORTED SMOKE SMELL. REPLACED THE SMOKE DETECTOR. 2 L 7 2 4T RT A31SO 1999051400344 19990514 00344 EA 1999 5 14 COMA9960183 1 19990506 A 3397 64643 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 FORWARD SECTION OF EMERGENCY FLOOR LIGHTS IS VERY DIM. REPLACED FLOOR LIGHTING POWER STRIP. 2 L 7 2 4F RT A21EA 1999051400345 19990514 00345 EA 1999 5 14 COMA9960184 1 19990508 A 2752 852D1009 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 719CA 6816 7253 FLAPS FAILED 42 DEGREES ON APPROACH. REMOVED AND REPLACED BOTH LEFT INBOARD FLAP ACTUATORS (FAILED TORQUE CHECK). 2 L 7 2 4F RT A21EA 1999051400346 19990514 00346 EA 1999 5 14 COMA9960186 1 19990506 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 719CA 5354 3 7253 FLAPS FAIL MESSAGE. REPLACED THE LT BPSU. 2 L 7 2 4F RT A21EA 1999051400347 19990514 00347 NM 1999 5 14 UPS99229548 1 19990504 A 5230 5887281 FITTING BOEING 727 72722C 138400F NM BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:AD, DURING NDT INSPECTION OF MAIN CARGO DOOR CAM SUPPORT FITTINGS. CRACK FOUND ON FITTING AT BS 520. F ITTING BS 520 REPLACED IAW UPS EO B727-5230-0005 APPENDIX B. 2 L 7 3 4F A3WE 1999051400348 19990514 00348 WP 1999 5 14 UPS99829543 1 19990503 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 761 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT O/B LEADING EDGE SKIN IS CRACKED BETWEEN FASTENERS AT XW 761. REPAIRED SKIN IAW SRM 57-2-1 FIG 2 H. 2 L 7 4 4F RT 4A25 1999051400349 19990514 00349 WP 1999 5 14 UPS99829544 1 19990418 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, FS 55 FRAME IS CRACKED AT LONG 24R, AROUND THE ROD ATTACHMENT. CUT OUT DAMAGED AREA AND REPAIRED IA W SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999051400350 19990514 00350 WP 1999 5 14 UPS99829545 1 19990427 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 461 & 484 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT WING L/E RIBS AT XS 461.372 AND XS 484.895 ARE CRACKED AAND& REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999051400351 19990514 00351 WP 1999 5 14 UPS99829546 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 491.193 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT WING L/E RIB AT XS 491.193 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999051400352 19990514 00352 WP 1999 5 14 UPS99829547 1 19990421 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 38.75 & 45 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, RT WING L/E LWR SURFACE BETWEEN FS 38.75 AND 45.00 IS CORRODED BEYOND LIMITS. REPAIRED IAW DHC SK88 0-933. 2 L 7 4 4F RT 4A25 1999051400353 19990514 00353 EU 1999 5 14 QXEA9901015 1 19990506 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU ROW 9B MISSING A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 GEG- EXIT SIGN MISSING AT ROW 9. INSTALLED NEW SIGN AT SEAT 9B, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999051400354 19990514 00354 WP 1999 5 14 ABXA9900350 1 19990506 A 5250 AR25291GR41 LATCH DOUG DOUG DC9 DC931 3022065 WP COCKPIT DOOR LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 COCKPIT DOOR WOULD NOT OPEN FROM CABIN SIDE. LUBRICATED COCKPIT DOOR LATCH MECHANISM, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999051400355 19990514 00355 WP 1999 5 14 ABXA990351 1 19990507 A 5753 5912168501 VANE DOUG DOUG DC9 DC941 302207N WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND LEFT FLAP FORWARD MOVEABLE VANE ARM CRACKED. REPLACED LEFT FORWARD FLAP MOVEABLE VANE IAW DC9 MM 27-51-2. 2 L 7 2 4F A6WE 1999051400356 19990514 00356 WP 1999 5 14 ABXA9900352 1 19990507 A 5752 5910047501 CONTROL TAB DOUG DOUG DC9 DC941 302207N WP LT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND LEFT AILERON CONTROL TAB DELAMINATED. REPLACED LEFT AILERON CONTROL TAB IAW DC9 MM 27-10-2. 2 L 7 2 4F A6WE 1999051400357 19990514 00357 WP 1999 5 14 ABXA9900353 1 19990507 A 2910 113965650 RELIEF VALVE DOUG DC8 DC861 3021952 WP LT MLG LEAKING A ABXA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 23 841AX 45908 ON LANDING AT OAK, HYDRAULIC QUANTITY DECREASED TO ZERO, HYDRAULIC PRESSURE WENT TO ZERO, BRAKE PRESSURE REDUCED TO 900 PSI. STEERING AND BRAKES WERE UNUSEABLE. REPLACED LEFT MAIN GEAR PRESSURE RELIEF VALVE IAW DC8 MM 32-33-2, OPS AND LEA K CHECKED GOOD. 2 L 7 4 4F 4A25 1999051400358 19990514 00358 WP 1999 5 14 ABXA9900354 1 19990508 A 5347 9753257 SEAT TRACK DOUG DC8 DC863 302198A WP RT COCKPIT DAMAGED A ABXA K NONE O OTHER LD LANDING 1 GL 23 817AX 45928 DURING TAKEOFF AND LANDING, FIRST OFFICER'S SEAT CAME OUT OF LOCKED POSITION. REMOVED FIRST OFFICER'S SEAT, REAMED HOLE S FOR SEAT LOCK PINS IAW DC8 MM 25-11-01. REINSTALLED SEAT, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999051400359 19990514 00359 WP 1999 5 14 ABXA9900355 1 19990508 A 5610 5613217507 WINDOW DOUG DC8 DC863 302198A WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER LD LANDING 1 GL 23 817AX 45928 CAPTAIN'S SLIDING WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. LUBRICATED CAPTAIN'S SLIDING WINDOW MECHANISM, OPS CHECKED G OOD. 2 L 7 4 4F 4A25 1999051400360 19990514 00360 WP 1999 5 14 MWEA99265 1 19990509 A 5210 5934796501 FITTING DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE MAIN CABIN DOOR BEAM NUMBER 1 AFT END FITTING IS CRACKED IN HALF. MTC FABRICATED AND INSTALLED NEW END FITTING. 2 L 7 2 4F A6WE 1999051400361 19990514 00361 WP 1999 5 14 MWEA99266 1 19990509 A 5210 995575213 BEAM DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE MAIN CABIN DOOR NUMBER 1 BEAM IS CRACKED AT FORWARD END UNDER FITTING. MTC FABRICATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999051400362 19990514 00362 NE 1999 5 14 TC8A99017 2 19990508 A 7230 COMPRESSOR BOEING 727 7272B6 138407J NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STALLED A TC8A D RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 721SK 21298 688572 KLRD-KLRD, WHILE SETTING T/O POWER, NUMBER 2 ENGINE COMPRESSOR STALLED. TRIMMED AND INSPECTED NR 2 ENGINE IAW 72-00, NO DEFECTS NOTED ON GROUND RUN. 2 L 7 3 4F 4 F A3WE E2EA 1999051400369 19990514 00369 CE 1999 5 14 99ZZZX1966 1 19990422 A 2430 26800141 VOLT REGULATOR BENDIX LEAR 35 35A 5170602 CE DC SYSTEM FAILED A IMJA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 25 50MJ 687U 164 UPON START-UP, NR 1 GENERATOR WAS SELECTED ON. NO AMPERAGE LOAD SHOWED ON AMMETER. SUBMITTER SUGGESTED CAUSE OF FAILUR E, INTERNAL PART. 2 L 7 2 4F A10CE 1999051400372 19990514 00372 EA 1999 5 14 99ZZZX1970 1 19990323 A 3246 10D34761 AXLE FLUIDYNE DHAV DHC2 DHC2MK1 2800102 EA SKI CRACKED A ECRA K NONE O OTHER IN INSP/MAINT 1 SO 15 345KA 2500 1306 FEDERAL/FLUIDYNE C5000 ONE-PIECE SKI AXLES (PN 10D3476-1) SHOWED STRESS FRACTURES WHERE SKI ACTUATOR ARM ROTATES. 1 H 7 1 3R A806 1999051400374 19990514 00374 CE 1999 5 14 99ZZZX1972 1 19990316 A 3110 6838 BULB LEAR 25 25B 5170511 CE INSTRUMENT PANEL FAILED A IJDA O OTHER N L FALSE WARNING NO TEST LD LANDING 1 WP 01 251JA 150 NOSE GEAR DOWN LOCKED INDICATOR INOPERABLE ON EXTENSION FOR LANDING. INDICATOR LIGHT DID NOT TEST. AIRCRAFT LANDED NOR MALLY; MAINTENANCE REPLACED LAMP AND INDICATION SYSTEM, OPERATED NORMALLY. 2 L 7 2 4J A10CE 1999051400398 19990514 00398 WP 1999 5 14 TWAA9906801 1 19990510 A 3231 3937030501 LINK DOUG DC9 DC982 3022082 WP LT MLG DOOR BROKEN A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 919TW 49368 AFTER TAKEOFF AND GEAR RETRACTION THE LEFT GEAR RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON. RECYCLED THE GEA R, NO HELP. FLIGHT RETURNED TO STL. FOUND THE LEFT GEAR DOOR ACTUATOR UPLINK BROKEN. REPLACED THE LINK ASSEMBLY. CHE CK-C 4-19-99 MCI. 2 L 7 2 4F A6WE 1999051400399 19990514 00399 EU 1999 5 14 MALA976446 1 19990507 A 8012 6058T80P03 VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 RIGHT INTAKE LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO MSP. MAINTENANCE CANNOT DUPLICATE PROBLEM. FOLLOWING F LIGHT REPLACED START AIR VALVE IAW CT7 MM 75-00-00 PG 403-404 A/B, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999051400400 19990514 00400 1999 5 14 MALA976447 4 19990505 A 2565 D31003101 SLIDE BAC 146 AVRO146RJ85A 1500097 EU RT SERVICE DOOR DEPLOYED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 524XJ E2349 RIGHT FORWARD SLIDE PARTIALLY DEPLOYED. MAINTENANCE REPLACED SLIDE PACK ASSEMBLY IAW AMM 25-60-11. 2 H 7 4 4F RT A49EU 1999051400401 19990514 00401 SO 1999 5 14 LR7A9935 1 19990412 A 5320 37234920 CAP LKHEED 382 382G 526414U SO BS 357-517 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION - PER HC05297, FOUND RT CHINE CAP CORRODED AND CRACKED IN 10K TIE DOWN WELLS, FS 357 TO 517. REPLACED CHINE CAP PER SMP 538 51-70 AND DWG 372349. 2 H 7 4 4T A1SO 1999051400402 19990514 00402 SO 1999 5 14 LR7A9936 1 19990412 A 5320 3541047 CAP LKHEED 382 382G 526414U SO BS 760-844 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION - PER HC05297, FOUND RAMP LT CHINE CAP CORRODED AND CRACKED. REPLACED CHINE CAP IAW SMP 583-52-60 AND DWG 354104. 2 H 7 4 4T A1SO 1999051400403 19990514 00403 SO 1999 5 14 LR7A9937 1 19990412 A 5320 3541048 CAP LKHEED 382 382G 526414U SO BS 760-844 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION - PER HC05297, FOUND RAMP RT CHINE CAP CORRODED AND CRACKED. REPLACED CHINE CAP IAW SMP 583 52-60 AND DWG 354104. 2 H 7 4 4T A1SO 1999051400404 19990514 00404 SO 1999 5 14 LR7A9938 1 19990412 A 5320 35360829 CAP LKHEED 382 382G 526414U SO CARGO DOOR BENT A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION - PER HSP53131, FOUND RAMP BEAM CAP BENT AT RAMP STA 10. REPLACED BEAM CAP IAW SMP 5 83 AND DWG 353608. 2 H 7 4 4T A1SO 1999051400405 19990514 00405 SO 1999 5 14 LR7A9939 1 19990412 A 5343 360587 TRUNNION LKHEED 382 382G 526414U SO NLG CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION - PER HSP5368, FOUND LT NOSE GEAR TRUNNION CRACKED. REPLACED LT NOSE GEAR TRUNNION I AW SMP 581-53-40 AND DWG 360587. 2 H 7 4 4T A1SO 1999051400406 19990514 00406 EU 1999 5 14 AWXA9900177 1 19990506 A 3232 BOLT AIRBUS 320 A320231 3930325 EU NLG DOOR ACT FAILED A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 28 635AW 092 AIR TURNBACK DUE TO LT NLG DOOR NOT RETRACTING. CREW SELECTED GEAR DOWN, THEN FELT VIBRATION IN NLG AREA. CREW RETURNE D TO PHL (SINK RATE GOOD -- NO OVERWEIGHT LANDING). MAINTENANCE FOUND THE ATTACH BOLT FOR NLG DOOR ACTUATING CYLINDER B ROKEN AND FOUND A BUSHING MISSING ON THE BOLT SIDE OF ATTACH POINT. FOUND NOSE LANDING GEAR DOOR ACTUATOR ROD BOLT FAIL ED. INSTALLED NEW BOLT AND HARDWARE IAW MM32-31-16-401. FUNCTIONAL TEST OF DOORS NORMAL AND NO FAULTS NOTED. 2 L 7 2 4F RT A28NM 1999051400407 19990514 00407 EU 1999 5 14 AWXA9900178 1 19990508 A 2910 B NUT AIRBUS 320 A320231 3930325 EU YELLOW HYD SYST LOOSE A AWXA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 28 643AW 315 DIVERSION AND EMERGENCY LANDING AT COLUMBUS, OHIO, FOR LOSS OF PRESSURE IN YELLOW HYDRAULIC SYSTEM. IN-FLIGHT INDICATIO NS FOR HYDRAULIC YELLOW ENGINE PUMP LOW PRESSURE, YELLOW SYSTEM LOW PRESSURE, AND YELLOW HYDRAULIC QUANTITY LOW. FOLLOW ED QRH PROCEDURES FOR OVERWEIGHT LANDING; TOUCHDOWN APPROX 0-50 FPM. NO OVERWEIGHT INSPECTION REQUIRED PER FLIGHT OPS M AUAL 04-02-10 AND AMM 5-51-11. WALK AROUND FOUND NO DEFECTS. FOUND 'B' NUT ON BRAKE ACCUMULATOR LOOSE. TIGHTENED SAME AND SERVICED HYDRAULIC SYSTEM, LEAK CHECK AND OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 1999051400408 19990514 00408 SW 1999 5 14 PNSA990401 1 19990404 A 3060 BRUSH BLOCK MCAULY C40331 SWRNGN SA227 SA227AC 8780603 SW RT PROP SHORTED A PNSA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 AL 03 41NE AC741B NOTICED SMELL OF SOMETHING BURNING (NO SMOKE). CO-PILOT NOTICED RT PROP DE-ICE CB WAS POPPED AND SAW SPARKS EMITING FRO M BETWEEN COWLING AND SPINNER. LANDING WAS UNEVENTFUL. FOUND PROP BRUSH BLOCK SHORTED. REPLACED BRUSH BLOCK, OPS CHEC K OK. 2 L 7 2 4T RT A8SW 1999051400409 19990514 00409 SO 1999 5 14 PNSA990402 1 19990406 A 3260 SWITCH PIPER PA31 PA31350 7103110 SO LANDING GEAR LACK OF LUBE A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 15PR 318052011 UPON GEAR RETRACTION UNSAFE LIGHT WOULD NOT EXTINGUISH AND SELECTOR WOULD NOT GO TO NEUTRAL. RETURNED TO AIRPORT FOR UN EVENTFUL LANDING. CLEANED AND LUBED ALL GEAR SWITCHES, OPS CHECK WAS FOUND NORMAL. 1 L 7 2 3O A20SO 1999051400410 19990514 00410 EU 1999 5 14 PNSA990403 1 19990418 A 2460 BUS SAAB SF340 340B 7860101 EU LEFT DISCONNECTED A PNSA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 675PA 206 DURING TAXI FOR TAKEOFF, LT MAIN BUS DISCONNECTED. AIRCRAFT RETURNED TO GATE. AFTER REPEATED ATTEMPTS TO DUPLICATE THE PROBLEM, NO FAULT COULD BE FOUND. 2 L 7 2 4T RT A52EU 1999051400411 19990514 00411 EU 1999 5 14 PNSA990404 1 19990421 A 2460 9301736116 RELAY SAAB SF340 340B 7860101 EU E&E COMPT INTERMITTANT A PNSA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 AL 03 675PA 206 ON CLIMBOUT, LT MAIN BUS WENT OFF LINE. RETURNED TO AIRPORT VFR FOR NORMAL LANDING. REPLACED TIME DELAY RELAY, OPS CHE CK WAS OK. 2 L 7 2 4T RT A52EU 1999051400412 19990514 00412 SW 1999 5 14 PNSA990501 1 19990509 A 2120 AIR DISTRIBUTION SWRNGN SA227 SA227AC 8780603 SW CABIN SMOKE A PNSA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 AL 03 2708D AC713B DURING LANDING ROLLOUT, CABIN FILLED WITH SMOKE. AIRCRAFT WAS UNLOADED AND TAKEN TO THE GATE. THIS INCIDENT IS STILL U NDER INVESTIGATION. 2 L 7 2 4T RT A8SW 1999051400413 19990514 00413 WP 1999 5 14 CALA9900502 1 19990511 A 2560 MEGAPHONE DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 BOTH MEGAPHONES INOP. ONE MEGAPHONE MOUTH RUBBER LOOSE. FWD AND AFT MEGAPHONES BATTERIES REPLACED. IN ONE MEGAPHONE T HE MOUTH RUBBER WAS SECURED PER MM 25-60-00. 2 L 7 3 4F A22WE 1999051400414 19990514 00414 WP 1999 5 14 CALA9900503 1 19990511 A 3350 BR964411 LIGHT DOUG DC10 DC1030 3023501 WP ROW 5,9,21,29 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17087 47928 EMERGENCY LIGHT PARTLY INOP ON SEATS 5K, 9B, 21B, AND 29K. REPLACED LIGHT ASSEMBLIES ON SEATS PER MM 33-50-00. 2 L 7 3 4F A22WE 1999051400415 19990514 00415 WP 1999 5 14 CALA9900504 1 19990510 A 3350 00059338898 LIGHT DOUG DC9 DC932 3022066 WP CABIN MISSING A CALA K NONE L NO TEST CR CRUISE 1 SW 09 18513 48112 AISLE PATH LIGHTING FLOOR TRIM IS MISSING IN FIRST CLASS. REPLACED AND RESECURED AISLE PATH LIGHTING IN FIRST CLASS. 2 L 7 2 4F A6WE 1999051400416 19990514 00416 NM 1999 5 14 CALA9900505 1 19990510 A 5530 SHIELD PLATE BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 VERTICAL STABILIZER INNER COMPARTMENT SHIELD PLATE AT I/B 1 AND LEFT HAND STRINGER NR 7 AREA HAS A SMALL CRACK (.25). R EMOVED FASTENERS, FABRICATED ANGLE PER SRM 55-30-6. TREATED, PRIMED AND INSTALLED DOUBLER PER SRM 51-10-2 AND 55-30-6 P G 2A. 2 L 7 3 4F A3WE 1999051400417 19990514 00417 NM 1999 5 14 CALA9900506 1 19990510 A 5315 BAC150529222 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 FLOORBEAM FS 344 HAS CORROSION TOP FLANGE BOTH SIDES RBL 24 TO LBL 60. REPAIRED AREA PER SRM 53-40-8 PAGE 51. 2 L 7 3 4F A3WE 1999051400418 19990514 00418 NM 1999 5 14 CALA9900507 1 19990510 A 5530 STRINGER BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 VERTICAL STABILIZER INNER COMPARTMENT NR 8 RIB RT STRINGER NR 8 CRACKED AT ATTACH BOLT (2). STOP DRILLED CRACK, FABRICA TED ANGLE AND FILLER REPAIR, TREATED AND PRIMED REPAIR PARTS, INSTALLED PER SRM 55-30-4, 55-30-9 AND 51-30-2. 2 L 7 3 4F A3WE 1999051400419 19990514 00419 NM 1999 5 14 CALA9900508 1 19990510 A 5320 CHORD BOEING 727 727224 1384076 NM BS 306-348 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 CHORD CORROSION INBOARD OF LEFT CUTOUT AT FS 306 TO 348. REMOVED OLD ANGLE, FABRICATED, TREATED, PRIMED AND INSTALLED N EW ANGLE PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999051400420 19990514 00420 WP 1999 5 14 CALA9900509 1 19990510 A 5220 ROD DOUG DC10 DC1030 3023501 WP L3 DOOR DISCONNECTED A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 14079 46927 UNABLE TO ARM L3 DOOR AT DEPARTURE. FOUND ROD AT LOCKING MECHANISM OUT OF PLACE. REINSTALLED ROD AND TIGHTENED HARDWAR E. 2 L 7 3 4F A22WE 1999051400421 19990514 00421 NM 1999 5 14 CALA9900510 1 19990510 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INTERCOSTAL CRACK AT 3 EACH TOP FLANGE HOLES BETWEEN FLOORBEAMS 760 TO 740 0 BL (1). REMOVED, FABRICATED, TREATED, PRIM ED AND INSTALLED PER SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999051400422 19990514 00422 NM 1999 5 14 CALA9900511 1 19990510 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 RIGHT ELEVATOR LOWER SKIN JUST FORWARD OF CONTROL TAB AREA CRACKED (3). STOP DRILLED CRACK. FABRICATED, TREATED, PRIME D AND INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 51-10-1, AND 55-20-3. 2 L 7 3 4F A3WE 1999051400423 19990514 00423 NM 1999 5 14 CALA9900512 1 19990510 A 5320 BAC150643 INTERCOSTAL BOEING 727 727224 1384076 NM BS 400-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INTERCOSTAL CORROSION FS 400 TO 420 RBL 12. REMOVED INTERCOSTAL, FABRICATED, TREATED, PRIMED AND INSTALLED NEW INTERCOS TAL PER SRM 51-10-6, 51-10-1, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999051400424 19990514 00424 NM 1999 5 14 CALA9900513 1 19990510 A 5320 BAC150643 BEAM BOEING 727 727224 1384076 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 CABIN STA 328 TO 344 LBL 30 J BEAM CORRODED. REMOVED J BEAM, RECEIVED EXTRUSION, DRILLED, TREATED, PRIMED AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999051400425 19990514 00425 NM 1999 5 14 CALA9900514 1 19990510 A 5520 CHANNEL BOEING 727 727224 1384076 NM RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 RIGHT ELEVATOR LOWER SKIN FORWARD OF CONTROL TAB INNER CHANNEL CRACKED (.5). STOP DRILLED CRACK, INSTALLED DOUBLER REPA IR PER SRM 55-20-3, 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1999051400426 19990514 00426 NM 1999 5 14 CALA9900515 1 19990510 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1050-1070 BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 FUSELAGE LOWER SKIN BETWEEN STATIONS 1050 TO 1070 AND STRINGER 30 AREA BULGED. REMOVED FASTENERS FROM FUSELAGE SKIN, NO CORROSION WAS FOUND. FABRICATED DOUBLER USING 2024 T3 .080 TREATED, PRIMED AND INSTALLED PER SRM 51-30-2 AND 53-30-3. 2 L 7 3 4F A3WE 1999051400427 19990514 00427 NM 1999 5 14 CALA9900516 1 19990510 A 5754 BAC15141559 CHORD BOEING 727 727224 1384076 NM NR 7 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 APPROX 2.25 INCH CRACK BELOW OUTBOARD UP STOP PAD AT LOWER CHORD RIGHT WING NR 8 SLAT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-4, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999051400428 19990514 00428 NM 1999 5 14 CALA9900517 1 19990510 A 5320 WEB BOEING 727 727224 1384076 NM BS 1178 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 FLOOR LEVEL WEB CORRODED WHERE FS 1178 CHORD ANGLE REMOVED AT RBL 34. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTA LLED PER SRM 53-41-2. 2 L 7 3 4F A3WE 1999051400429 19990514 00429 NM 1999 5 14 CALA9900518 1 19990510 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 FLOORBEAM FS 312 HAS 2 HOLES WITH CORROSION AT LBL 20 AND 3. CUT OUT DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INST ALLED REPAIR PER SRM 53-10-9 FIG 8. 2 L 7 3 4F A3WE 1999051400430 19990514 00430 NM 1999 5 14 CALA9900519 1 19990510 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 700-720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 CORROSION AT STA 28R INBOARD BETWEEN STATION 700 AND 720. REMOVED FAIRING RIBS STA 700 TO 710 RIGHT. CUT OUT DAMAGED A REA, REMOVED INTERCOSTAL STA 700 TO 720 STR 28 RIGHT. ACCOMPLISHED HFEC, NO CKACK FOUND. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PER SRM 53-30-3, 51-10-6 AND 51-30-2. 2 L 7 3 4F A3WE 1999051400431 19990514 00431 NM 1999 5 14 CALA9900520 1 19990510 A 5210 MECHANISM BOEING 727 727224 1384076 NM PASSENGER DOOR HUNG UP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 AFT ENTRY DOOR DOES NOT OPEN SMOOTHLY, HANGS UP AT BOTTOM. ADJUSTED AFT DOOR UPPER LATCH FITTING PER MM 52-13-0 PAGE 40 5. 2 L 7 3 4F A3WE 1999051400432 19990514 00432 NM 1999 5 14 CALA9900521 1 19990510 A 5542 SKIN BOEING 727 727224 1384076 NM RUDDER GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 UPPER RUDDER TRAILING EDGE JUST BELOW NR 2 CONTROL TAB ATTACH HINGE (FROM BOTTOM) AREA GOUGED. REMOVED DAMAGED AREA BY ROUTING, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PER SRM 51-10-2 AND 51-40-2. 2 L 7 3 4F A3WE 1999051400433 19990514 00433 NM 1999 5 14 CALA9900522 1 19990510 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 700-720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 STATION 700 TO 720 STRINGER 28R OUTBOARD INTERCOSTAL FLANGE CORRODED. CUT OUT DAMAGED AREA. FABRICATED, ALODINED, PRIM ED AND INSTALLED REPAIR PER SRM 51-40-3, 51-10-6 AND 51-30-2. 2 L 7 3 4F A3WE 1999051400434 19990514 00434 NM 1999 5 14 9901652702 1 19990501 A 2121 FAN BOEING 727 727225 1384077 NM CABIN FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 8877Z 21450 IN CRUISE FLIGHT, CREW REPORTED SMOKE IN CABIN. CREW DIVERTED FLIGHT TO SLC WITHOUT INCIDENT. MAINTENANCE FOUND GASPER FAN HAD FAILED. REPLACED GASPER FAN, OPERATIONAL CHECK OK. (P/N 07-2120-9-0001) 2 L 7 3 4F A3WE 1999051400435 19990514 00435 EA 1999 5 14 COMA9960187 1 19990510 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 719CA 6728 7253 FLAPS FAILED ON APPROACH AT 19 DEGREES. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 1999051400436 19990514 00436 EA 1999 5 14 COMA9960188 1 19990510 A 2752 853D10012 FLAP CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 719CA 6683 7253 FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED RT OUTBOARD FLAP INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 1999051400437 19990514 00437 EA 1999 5 14 COMA9960189 1 19990510 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 719CA 7253 FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED FLAP CONTROL HANDLE. 2 L 7 2 4F RT A21EA 1999051400438 19990514 00438 EA 1999 5 14 COMA9930190 1 19990510 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FLAP FAIL A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 719CA 6891 7253 FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU). 2 L 7 2 4F RT A21EA 1999051400439 19990514 00439 EA 1999 5 14 COMA9960191 1 19990510 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 719CA 1744 7253 FLAP FAIL ON APPROACH AT 19 DEGREES. REMOVED AND RELACED LT OUTBOARD FLAP INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 1999051400440 19990514 00440 EA 1999 5 14 COMA9960192 1 19990509 A 2750 601R930043 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 946CA 3316 7292 AFTER LANDING RETRACTED FLAPS TO 30 DEGREES, FLAPS INDICATED 30 DEGREES BUT FLAP CAUTION MESSAGE APPEARED. COMPLIED WIT H EO 27-045 AD EO 27-046 AD. REMOVED AND REPLACED FLAP HANDLE. 2 L 7 2 4F RT A21EA 1999051400441 19990514 00441 EA 1999 5 14 COMA9960193 1 19990509 A 5270 SENSOR CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF ADJUST A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 929CA 7035 AFTER TAKEOFF, PASSENGER OUTER DOOR HANDLE STOW AND OVERBOARD COOL CAUTION MESSAGE CAME ON. ADJUSTED PROX SENSOR. 2 L 7 2 4F RT A21EA 1999051400442 19990514 00442 EA 1999 5 14 COMA9960194 1 19990507 A 5210 PUSH RODS CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 721CA 7259 RECEIVED DOOR WARNING MESSAGE AFTER TAKEOFF. ADJUSTED PUSH ROD ON PULL IN LEVER AND ADJUSTED PUSH ROD ON LOWER PIVOT AS SEMBLY. 2 L 7 2 4F RT A21EA 1999051400443 19990514 00443 EA 1999 5 14 COMA9960195 1 19990509 A 2910 HYD SYST CNDAIR CL600 CL6002B19 EA NR 3 OVERSERVICED A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 954CA 7100 ON TAKEOFF, CONTINUOUS THUMP FROM LEFT RUDDER PEDAL AND FLOORBOARDS BELOW RUDDER BELOW RUDDER PEDAL. THUMP WENT AWAY WH EN LANDING GEAR WAS EXTENDED. FOUND NR 3 HYDRAULIC SYSTEM OVERSERVICED. DRAIN EXCESS FLUID PERFORMED GEAR SWINGS. ALS O, PERFORMED OVERWEIGHT LANDING INSPECTION. 2 L 7 2 4F RT A21EA 1999051400444 19990514 00444 EA 1999 5 14 COMA9960196 1 19990510 A 2750 601R57115107 WIRE HARNESS CNDAIR CL600 CL6002B19 EA LT TE FLAP DAMAGED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 719CA 7253 WHEN FLAPS WERE SELECTED TO 45 DEGREES FLAP FAIL CAUTION MESSAGE ILLUMINATED AT 32 DEGREES. REMOVED AND REPLACED LEFT W ING BPSU WIRING HARNESS. CHECKED TORQUE OF FLAP SYSTEM RIGGED FLAP SYSTEM. 2 L 7 2 4F RT A21EA 1999051400445 19990514 00445 SO 1999 5 14 COMA9910074 1 19990510 A 2133 2091G010800 OUTFLOW VALVE EMB 120 EMB120RT SO CABIN FAILED A COMA O OTHER O OTHER UK UNKNOWN 1 SO 01 269CA 16074 1263 AUTO PRESSURIZATION INOPERATIVE. REMOVED AND REPLACED PRESS OUTFLOW VALVE. 2 L 7 2 4T RT A31SO 1999051400446 19990514 00446 SO 1999 5 14 COMA9910075 1 19990510 A 7931 310795501 CHECK VALVE EMB 120 EMB120RT SO LT ENG OIL PRESS FAILED A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 269CA 1263 SMOKE FLOWED HEAVILY FROM COCKPIT GASPERS DURING DESCENT THRU 14,000 FT. TORQUE REDUCED TO 20 PERCENT. REMOVED AND REP LACED LEFT ENGINE OIL PRESSURE CHECK VALVE. GROUND RAN A/C, NO SMOKE OR SMELL NOTED. 2 L 7 2 4T RT A31SO 1999051400447 19990514 00447 SO 1999 5 14 COMA9910076 1 19990508 A 3230 922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 168CA 1168 GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE LANDING GEAR A SYSTEM PROX SENSOR. 2 L 7 2 4T RT A31SO 1999051400448 19990514 00448 SO 1999 5 14 COMA9910077 1 19990508 A 5246 FASTENER EMB 120 EMB120RT SO FUEL SERVICE DR LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 258CA 1247 SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. FOUND FORWARD QUARTER TURN FASTENER LOOSE ON FUEL SERVICE D OOR. REMOVED AND REPLACED FASTENER. 2 L 7 2 4T RT A31SO 1999051400449 19990514 00449 NM 1999 5 14 UPS99229549 1 19990327 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C53-111-01.05-01) ON STIFFENER ATTACH ANGLE BS 320 LBL 15 WL 170. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-20-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999051400450 19990514 00450 NM 1999 5 14 UPS99229550 1 19990327 A 5753 FITTING BOEING 727 72731C 1384011 NM TE FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581.06.00-04) ON NR 7 FLAP TRACK FWD FITTING. REPAIRED PER ER 99-5216. 2 L 7 3 4F A3WE 1999051400451 19990514 00451 NM 1999 5 14 UPS99229551 1 19990510 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION ON STRAP ON FLOORBEAM UPPER CHORD LOWER SIDE BS 312, BL 0, WL 208. REPAIR TO BE ACCOMPLIS HED ON CUSTOMER ID 888989. 2 L 7 3 4F A3WE 1999051400452 19990514 00452 NM 1999 5 14 UPS99229552 1 19990325 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 740-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C53-224-01.00-02) MAIN DECK STR 2R BS 740 TO 870 ALONG BOTH FLANGES ON BOTH SURFACES. RE PAIR ON NRC 888518 AND 888519. 2 L 7 3 4F A3WE 1999051400453 19990514 00453 NM 1999 5 14 UPS99229553 1 19990326 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM BS 846-842 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-02) ON FLOORBEAM UPPER CHORD BS 846 THRU 842, LBL 44, WL 208. REPAIRED ER 99-5239. 2 L 7 3 4F A3WE 1999051400454 19990514 00454 NM 1999 5 14 UPS99229554 1 19990327 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581.06.00-04) ON NR 8 FLAP TRACK FWD ATTACH FITTING. REPAIRED PER ER 99-5226. 2 L 7 3 4F A3WE 1999051400455 19990514 00455 NM 1999 5 14 UPS99229555 1 19990325 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK AT FWD ATTACH LUG AND INSIDE BARREL NUT HOLE. REPAI RED ON CUSTOMER ID 888950. 2 L 7 3 4F A3WE 1999051400456 19990514 00456 NM 1999 5 14 UPS99229556 1 19990325 A 5753 65216518 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 5 FLAP TRACK FWD ATTACH FITTING. REMOVED AND REPLACED SUPPORT AS SY. 2 L 7 3 4F A3WE 1999051400457 19990514 00457 NM 1999 5 14 UPS99229557 1 19990325 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK AT FWD ATTACH LUG AND INSIDE BARREL NUT HOLE. REPAI RED PER ER 99-5243. 2 L 7 3 4F A3WE 1999051400458 19990514 00458 NM 1999 5 14 UPS99229558 1 19990325 A 5753 652920219 CARRIAGE BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-581-04.00-04) ON NR 7 FLAP CARRIAGE UPPER SURFACE O/B SIDE. REMOVED AND REPLACED CAR RIAGE INSTALLATION ON TC C57-581-04-4D. 2 L 7 3 4F A3WE 1999051400459 19990514 00459 NM 1999 5 14 UPS99229559 1 19990427 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C57-174-01-1B) ON INTERNAL 870 SKIN AT UPPER SPAR CHORD BS 870, RBL 61-64. REMOVED CORRO SION PER SRM 57-30-1, FLAP PEENED AREA PER ER NR 99-5258, ALODINED AND PRIMED PER ER NR 99-5258. 2 L 7 3 4F A3WE 1999051400460 19990514 00460 NM 1999 5 14 UPS99229560 1 19990330 A 5320 STIFFENER BOEING 727 72731C 1384011 NM BS 336 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION (C53-111-01.05-01) ON STIFFENER ATTACH ANGLE BS 336 LBL 15 WL 170. REMOVED ATTACH ANGLE, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED PER SRM 51-20-1, INSTALLED ATTACH ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999051400461 19990514 00461 NM 1999 5 14 UPS99229561 1 19990507 A 5753 65327332 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION ON NR 7 FLAP TRACK FWD ATTACH FITTING. FITTING WAS REWORKED ON NRC NR 888956 AND REINSTAL LED ON NRC NR 888744. 2 L 7 3 4F A3WE 1999051400462 19990514 00462 NM 1999 5 14 UPS99229562 1 19990506 A 5753 65327342 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, CORROSION ON NR 8 FLAP TRACK FWD ATTACH FITTING. REWORKED FITTING PER ER 99-5226. 2 L 7 3 4F A3WE 1999051400463 19990514 00463 NM 1999 5 14 99FDEA00173 1 19990510 A 2612 FIRE DET BOX BOEING 727 7272S2F 1384O81 NM ENGINE INOPERATIVE A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 205FE 22927 FIRE BELL CHIMED INTERMITTENTLY WITH ILLUM OF BOTH MASTER FIRE WARNING LIGHT ON GLARESHIELD. INSTALLED SERVICEABLE ENGI NE FIRE DETECTION BOX AND ENG ELEMENT SUPPORT ASSY, SYS OPER CK NORM IN MM 26-11-01. 2 L 7 3 4F A3WE 1999051400464 19990514 00464 NM 1999 5 14 99FDEA00174 1 19990511 A 2612 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM FIRE DET SYST FAILED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 205FE 22927 NR 1 ENG FIRE WARNING LIGHT AND BELL SOUND INTERMITTENTLY. WARNING SILENCED BY OPEN NR 1 ENG SYS A DETECTION CIRCUIT BR EAKER, BOTH FIRE SYS TEST SAT. *S/D* INSTALLED STUB WING PNLS. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT, ALL CK OK MM 26-11. 2 L 7 3 4F A3WE 1999051400465 19990514 00465 NE 1999 5 14 99FDEA00164 2 19990504 A 7200 ENGINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 2 FAILED A FDEA E ENGINE SHUTDOWN Y ENGINE STOPPAGE TO TAKEOFF 1 SO 25 269FE 21675 ON T/O FROM MEM, 18L WINDS 160118625 NR 2 ENG FAILED WITH LOUD BANG. *S/D* NR 2 ENG CHANGE ACCOMPLISHED PER WC 70T0002 . LEAK AND OPS CK GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 1999051400466 19990514 00466 NM 1999 5 14 SCNA99066 1 19990503 A 3350 900835A BATTERY PACK BOEING 727 7272A1 138407F NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 DURING A LINE MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE ASSOCIATED BATTERY PACK AND ALL EMERGENCY LIGHTS CHECK GOOD. 2 L 7 3 4F A3WE 1999051400467 19990514 00467 SO 1999 5 14 SWIA971471 1 19990409 A 2422 INVERTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 233SW 120307 NUMBER TWO INVERTER FAILED IN FLIGHT. DIVERTED FROM YUM TO PSP. REMOVED AND REPLACED NUMBER TWO INVERTER, OPS CHECK NO RMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1999051400468 19990514 00468 1999 5 14 SWIA971472 4 19990403 A 3452 TRANSPONDER EMB 120 EMB120RT SO PWA 118 PW118A NE E & E COMPT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 289YV 120289 ATC REPORTS NO MODE C ON TRANSPONDER. RETURNED TO FIELD. SWAPPED TDR 94 BOXES AND PERFORMED GROUND CHECK. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999051400469 19990514 00469 EA 1999 5 14 SWIA971473 1 19990408 A 5610 WINDOW CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 403SW 7028 LEFT SIDE WINDOW CRACKED IN FLIGHT. DIVERTED FROM ABQ TO FMN. NO LOSS OF PRESSURIZATION OR OTHER DIFFICULTIES ENCOUNTE RED. REMOVED AND REPLACED LEFT SIDE WINDOW IAW MM 56-12-01. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999051400470 19990514 00470 SO 1999 5 14 SWIA971474 1 19990409 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 197SW 120186 ON DEPARTURE OUT OF SLC, RIGHT RUDDER PEDAL STUCK AT APPROX ONE-HALF TRAVEL. RUDDER WOULD CENTER BUT WOULD NOT GO PAST ONE-HALF TRAVEL. FOLLOWED QRH AND UPON SELECTION OF BLUE RUDDER SYSTEM TO OFF, RUDDER TRAVEL WAS NORMAL. RETURNED TO S LC. REMOVED AND REPLACED RUDDER ACTUATOR FOR BLUE SYSTEM. LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999051400471 19990514 00471 SO 1999 5 14 SWIA971475 1 19990509 A 3260 UPLOCK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 190SW 120050 RIGHT RED A LIGHT STAYS ON AFTER RETRACTION. RETURNED TO SLC. ADJUSTED RIGHT MLG UPLOCK ROLLER AND UPLOCK PROXIMITY S ENSORS IAW EMB 120 MM 32-61-01. OPS CHECK GOOD UPON RETRACTION. 2 L 7 2 4T 4 T RT A31SO E20NE 1999051400472 19990514 00472 1999 5 14 SWIA971476 4 19990509 A 3425 AHRS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E & E COMPT TRIPPED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 580SW 120348 INFLIGHT RECEIVED A PIT FLAG ON BOTH EADI'S WITH THE FO'S EADI SHOWING 10 DEGREES LOWER. RESET BOTH AHRS NR 2 CIRCUIT B REAKERS WITHOUT ANY CHANGE. QRH PROCEDURES WERE FOLLOWED WITHOUT ANY RESULTS. RETURNED TO SBA. PERFORMED AHRS INITIAL IZATION AND ORIENTATION TEST PER AND AHRS OPERATES NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1999051400473 19990514 00473 SO 1999 5 14 SWIA971477 1 19990509 A 3230 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 579SW 120347 AFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT AND INTRANSIT LIGHTS WERE ILLUMINATED. RETURNED TO LAX. REPLACED LAND ING GEAR CONTROL BOX. RETRACTED GEAR A DOZEN TIMES, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999051400474 19990514 00474 SO 1999 5 14 SWIA971478 1 19990509 A 3020 TIMER EMB 120 EMB120RT SO PWA 118 PW118A NE RT ENG DEICE FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 284YV 120284 RIGHT ENGINE INLET DEICE FAILED INFLIGHT. RETURNED TO SEA. REMOVED AND REPLACED RIGHT ENGINE INLET DEICE TIMER. GROUN D RUN, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999051400485 19990514 00485 NE 1999 5 14 99ZZZX2005 2 19990324 A 7310 600625333 VALVE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE LEFT MALFUNCTIONED A N9WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 11 733EY 3601 5113 SFO - AIRCRAFT DEPARTED AND HAD LEVELED OFF AT CRUISE SPEED (.80/330) WHEN CREW NOTICED THE LT FUEL QUANTITY DECREASING AT AN ACCELERATED RATE. CREW STARTED IMMEDIATE TRANSFER TO BALANCE THE FUEL LOAD AND DECIDED TO DIVERT TO OAKLAND, CA W HERE THEY MADE AN UNEVENTFUL LANDING, BUT DID LAND OVERWEIGHT. THERE WERE 4 PASSENGERS ON BOARD AND NO EMERGENCY WAS DE CLARED. CAREFUL TROUBLESHOOTING DETERMINED THE TRANSFER EJECTOR SYSTEM WAS AT FAULT AND WAS DEFERRED. AFTER FURTHER TE STING, CHANGED FOLLOWING COMPONENTS: LT AND RT 93 PERCENT VALVES, RT COLLECTOR TANK PUMP CARTRIGE, LT TRANSFER EJECTOR, LT MT1EB FUEL PROBE AND RT MT10EB FUEL PROBE. ALL SYSTEMS TESTED AND FOUND ACCEPTABLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999051400486 19990514 00486 NE 1999 5 14 99ZZZX2006 2 19990324 A 7310 600625333 VALVE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE RIGHT MALFUNCTIONED A N9WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 11 733EY 3616 5113 SFO - AIRCRAFT DEPARTED AND HAD LEVELED OFF AT CRUISE SPEED (.80/330) WHEN CREW NOTICED THE LT FUEL QUANTITY DECREASING AT AN ACCELERATED RATE. CREW STARTED IMMEDIATE TRANSFER TO BALANCE THE FUEL LOAD AND DECIDED TO DIVERT TO OAKLAND, CA W HERE THEY MADE AN UNEVENTFUL LANDING, BUT DID LAND OVERWEIGHT. THERE WERE 4 PASSENGERS ON BOARD AND NO EMERGENCY WAS DE CLARED. CAREFUL TROUBLESHOOTING DETERMINED THE TRANSFER EJECTOR SYSTEM WAS AT FAULT AND WAS DEFERRED. AFTER FURTHER TE STING, CHANGED FOLLOWING COMPONENTS: LT AND RT 93 PERCENT VALVES, RT COLLECTOR TANK PUMP CARTRIGE, LT TRANSFER EJECTOR, LT MT1EB FUEL PROBE AND RT MT10EB FUEL PROBE. ALL SYSTEMS TESTED AND FOUND ACCEPTABLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999051400487 19990514 00487 NE 1999 5 14 99ZZZX2007 2 19990324 A 7310 600628915 CARTRIDGE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE RIGHT COLLECTOR MALFUNCTIONED A N9WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 11 733EY 3601 5113 SFO - AIRCRAFT DEPARTED AND HAD LEVELED OFF AT CRUISE SPEED (.80/330) WHEN CREW NOTICED THE LT FUEL QUANTITY DECREASING AT AN ACCELERATED RATE. CREW STARTED IMMEDIATE TRANSFER TO BALANCE THE FUEL LOAD AND DECIDED TO DIVERT TO OAKLAND, CA W HERE THEY MADE AN UNEVENTFUL LANDING, BUT DID LAND OVERWEIGHT. THERE WERE 4 PASSENGERS ON BOARD AND NO EMERGENCY WAS DE CLARED. CAREFUL TROUBLESHOOTING DETERMINED THE TRANSFER EJECTOR SYSTEM WAS AT FAULT AND WAS DEFERRED. AFTER FURTHER TE STING, CHANGED FOLLOWING COMPONENTS: LT AND RT 93 PERCENT VALVES, RT COLLECTOR TANK PUMP CARTRIGE, LT TRANSFER EJECTOR, LT MT1EB FUEL PROBE AND RT MT10EB FUEL PROBE. ALL SYSTEMS TESTED AND FOUND ACCEPTABLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999051400488 19990514 00488 NE 1999 5 14 99ZZZX2008 2 19990324 A 7310 2780473105 EJECTOR CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE LEFT MALFUNCTIONED A N9WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 11 733EY 3616 5113 SFO - AIRCRAFT DEPARTED AND HAD LEVELED OFF AT CRUISE SPEED (.80/330) WHEN CREW NOTICED THE LT FUEL QUANTITY DECREASING AT AN ACCELERATED RATE. CREW STARTED IMMEDIATE TRANSFER TO BALANCE THE FUEL LOAD AND DECIDED TO DIVERT TO OAKLAND, CA W HERE THEY MADE AN UNEVENTFUL LANDING, BUT DID LAND OVERWEIGHT. THERE WERE 4 PASSENGERS ON BOARD AND NO EMERGENCY WAS DE CLARED. CAREFUL TROUBLESHOOTING DETERMINED THE TRANSFER EJECTOR SYSTEM WAS AT FAULT AND WAS DEFERRED. AFTER FURTHER TE STING, CHANGED FOLLOWING COMPONENTS: LT AND RT 93 PERCENT VALVES, RT COLLECTOR TANK PUMP CARTRIGE, LT TRANSFER EJECTOR, LT MT1EB FUEL PROBE AND RT MT10EB FUEL PROBE. ALL SYSTEMS TESTED AND FOUND ACCEPTABLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999051400489 19990514 00489 NE 1999 5 14 99ZZZX2009 2 19990324 A 7310 391002334 PROBE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A 30015 NE LEFT AND RIGHT MALFUNCTIONED A N9WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 11 733EY 3616 5113 SFO - AIRCRAFT DEPARTED AND HAD LEVELED OFF AT CRUISE SPEED (.80/330) WHEN CREW NOTICED THE LT FUEL QUANTITY DECREASING AT AN ACCELERATED RATE. CREW STARTED IMMEDIATE TRANSFER TO BALANCE THE FUEL LOAD AND DECIDED TO DIVERT TO OAKLAND, CA W HERE THEY MADE AN UNEVENTFUL LANDING, BUT DID LAND OVERWEIGHT. THERE WERE 4 PASSENGERS ON BOARD AND NO EMERGENCY WAS DE CLARED. CAREFUL TROUBLESHOOTING DETERMINED THE TRANSFER EJECTOR SYSTEM WAS AT FAULT AND WAS DEFERRED. AFTER FURTHER TE STING, CHANGED FOLLOWING COMPONENTS: LT AND RT 93 PERCENT VALVES, RT COLLECTOR TANK PUMP CARTRIGE, LT TRANSFER EJECTOR, LT MT1EB FUEL PROBE AND RT MT10EB FUEL PROBE. ALL SYSTEMS TESTED AND FOUND ACCEPTABLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999051400517 19990514 00517 CE 1999 5 14 99ZZZX1912 1 19990427 A 7720 1313503 INDICATOR LEAR 35 35A 5170602 CE COCKPIT MALFUNCTIONED A KKFA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 23 72CK 10 1081946 165 LEFT ENGINE EGT ERRATIC. ENGINE SHUT DOWN AND UNEVENTFUL LANDING ACCOMPLISHED. INSPECTION REVEALED TEMPERATURE INDICAT ING SYSTEM MALFUNCTION. REPLACED TURBINE TEMP GAUGE WITH SERVICEABLE UNIT, SYSTEM OPERATIONALLY CHECKS GOOD. NO RECOMM ENDATION FOR PREVENTION KNOWN. 2 L 7 2 4F A10CE 1999051400521 19990514 00521 CE 1999 5 14 99ZZZX1916 1 19990412 A 2612 9957011 FIRE DETECTOR PYROTECTOR BEECH 99 99A 1154003 CE LT ENG NACELLE CONTAMINATED A KCQA O OTHER O OTHER NR NOT REPORTED 1 GL 13 499CZ U81 FOUND FIREWALL CONNECTOR TO BE WET WITH WATER. PILOT REPORTED FLYING THROUGH SOME INTENSE SHOWERS EN ROUTE TO MILWAUKEE , WI FROM STEVENS POINT, WI. CONNECTOR WAS DRIED OUT, RE-ASSEMBLED, AND FUNCTION TESTED SATISFACTORY. 1 L 7 2 3T A14CE 1999051400530 19990514 00530 1999 5 14 99ZZZM279 4 19990104 A 2565 SLIDE LKHEED 1011 10113851 5265010 WP L2 DOOR MALFUNCTIONED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 196AT 193B1076 AIRCRAFT PARKED AT GATE, NO PASSENGERS, THE L-2 SLIDE CAME PARTIALLY OUT OF THE DOOR. FOUND CLEVIS PIN FOR DETACH HANDL E AT FLOOR LINE, WITH BROKEN SAFETY. SLIDE WAS REPLACED. (M) 2 L 7 3 4F A23WE 1999051400531 19990514 00531 WP 1999 5 14 99ZZZM280 1 19990106 A 3350 P4010014F110 BATTERY AIRCRUISERS T30170539 LKHEED 1011 10113853 5265020 WP R1 SLIDE DISCHARGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 163AT 1229 DURING A PARTIAL EVACUATION DEMONSTRATION, SLIDE NR R1 WAS DEPLOYED, BUT THE EMERGENCY LIGHTS DID NOT ILLUMINATE. BATTE RY WAS CHECKED AND FOUND CONNECTED. THE FINAL TEARDOWN OF THE SLIDE REVEALED THAT THE BATTERY AND LAMP HARNESS PASSED A LL REQUIRED TESTS PER CMM. (M) 2 L 7 3 4F A23WE 1999051400532 19990514 00532 EU 1999 5 14 FJT99039401 1 19990325 A 2910 1379305A77 LINE BAG JETSTM JETSTM3201 1500217 EU RT NACELLE FAILED A FJTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 03 940AE 940 BNA - FLT 402 - A/C WAS AT CRUISE, EN ROUTE TO ALT FROM BNA, APPROX 35 MINUTES INTO THE FLIGHT BOTH HYDRAULIC PRESSURE G AUGES STARTED TO FLUCTUATE AND THEN WENT OT ZERO PRESSURE. THE A/C INCURRED A HYD SYSTEM FAILURE. THE A/C RETURNED TO BNA. AN EMERGENCY LANDING WAS DECLARED AN THE LANDING GEAR AND FLAPS WERE ACTIVATED BY MEANS OF THE EMERGENCY HYD SYSTE M. THE A/C LANDED AND RETURNED SAFELY TO THE GATE. THE RIGHT HYD PUMP RETURN LINE HAD RUPTURED AS A RESULT OF CHAFING THE COMPRESSOR DRAIN LINE. THE LINE WAS REPLACED AND ALL ALSO NR 1 AND NR 2 ENGINE DRIVEN HYD PUMPS. THE SYSTEM FILTER S WERE INSPECTED AND REPLACED. NO EVIDENCE OF METAL NOTED. THE ENTIRE A/C HYD SYSTEM WAS BLED IAW THE A/C MM. GEAR, F 2 L 7 2 4T RT A56EU 1999051400533 19990514 00533 WP 1999 5 14 FJT99049361 2 19990409 A 7320 1379287L405 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE CRACKED A FJTA K NONE N FALSE WARNING CR CRUISE 1 SO 03 936AE 936 P66285C RDU - FLT 7936 - RIGHT ENGINE P3 BLEED LINE CRACKED AT MOUNTING FLANGE TO ENINE. CAUSING LOSS OF BLEED AIR AND ANTI-ICI NG FOR THE RIGHT ENGINE. THE LINE WAS THE PREMOD TYPE AND SHOULD NOT HAVE VEEN INSTALLED ON THE ENGINE. THE LINE WAS R EPLACED WITH POSTMOD LINE P/N 13711543L401. AN INSPECTION IS IN PROGRESS ON ALL ENGINES AND EFFECTED LINES. WILL REPLA CE ANY PREMOD LINES WITH POSTMOD LINES AS REQUIRED A STOCK SWEEP WAS PERFORMED, NO PREMOD LINES FOUND. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999051400534 19990514 00534 EU 1999 5 14 PLGA990328A 1 19990328 A 6120 SCREW SAAB SF340 340B 7860101 EU LT POWER LEVER LOOSE A PLGA K NONE O OTHER LD LANDING 1 NE 05 353BE 340B242 BOS - FLT 6398 - UPON LANDING, CREW WAS UNABLE TO GET REVERSE PITCH ON THE LEFT PROP. CREW WAS ABLE TO MAINTAIN CONTROL OF THE AIRCRAFT AND TAXIED TO THE GATE WITHOUT INCIDENT. BOS MAINTENANCE FOUND A SET SCREW THAT HAD BACKED OUT OF THE CONTROL QUADRANT BY THE LEFT POWER LEVER ROD THAT PREVENTED THE POWER LEVER FROM GOING INTO REVERSE PITCH. MAINTENANCE REPLACED THE CONTROL QUADRANT, PERFORMED THE REQUIRED OPERATIONAL CHECKS, AND RETURNED TO THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999051400535 19990514 00535 EU 1999 5 14 PLGA990312A 1 19990312 A 3240 50104882 BRAKE ASSEMBLY SAAB SF340 SF340A 7850100 EU NR 4 DRAGGING A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NE 05 747BA APR972120 340A148 BOS - FLT 6263 - TAKEOFF ABORTED WHEN THE AIRCRAFT PULLED TO THE RIGHT ON TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND THE NR 4 BRAKE TO BE DRAGGING. THE BRAKE ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. FURTHER INVESTIGATION REVEALED THE BRAKE WAS WITHIN WEAR LIMITS AND THE ANOMOLY COULD NOT BE DUPLICATED DURING AN AS R ECEIVED INSPECTION OF THE BRAKE. (M) 2 L 7 2 4T RT A52EU 1999051400536 19990514 00536 EU 1999 5 14 PLGA990318 1 19990318 A 3097 WIRE SAAB SF340 SF340A 7850100 EU LEFT ENGINE BROKEN A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 342BE 340A096 BOS - FLT 6386 - DURING FLIGHT, THE LEFT INTAKEO HEAT FAILED AND DUE TO WEATHER IN SYR, THE AIRCRAFT RETURNED TO BOS. B OS MAINTENANCE FOUND A BROKEN WIRE ON THE EXHAUST NOZZLE. THE WIRE WAS REPLACED OPERATIONAL CHECKS PERFORMED, AND AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999051400537 19990514 00537 NM 1999 5 14 MZZA99058 1 19990314 A 5713 STRINGER BOEING 727 727264 138408M NM WS 656.5 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRFT AT AIR ASIA, .4375 INCH LONG CRACK WAS FOUND ON LEFT WING UPPER S-9 STRING ER/RIB ATTACH HOLE AT WS 656.5. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA 5762-01050 PART 3 (SB 727-57A159 FIG URE 18). 2 L 7 3 4F A3WE 1999051400538 19990514 00538 NM 1999 5 14 MZZA99057 1 19990312 A 5320 6517510255 WEB BOEING 727 727264 138408M NM BS 1273 WORN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, WORN WAS FOUND ON LEFT SIDE AFTER AIRSTAIR TORQUE BOX HORIZO NTAL WEB AT BS 1273. THE DAMGED WEB OF AFTER AIRSTAIR TORQUE BOX HORIZONTAL WEB WAS REPAIRED PER B727 SRM 51-40-2 FIGUR E 1. (M) 2 L 7 3 4F A3WE 1999051400539 19990514 00539 NM 1999 5 14 MZZA99056 1 19990315 A 5320 6517510256 WEB BOEING 727 727264 138408M NM BS 1320 WORN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, WORN WAS FOUND ON RIGHT SIDE AFTER AIRSTAIR TORQUE BOX HORIZ ONTAL WEB AT BS 1320. THE DAMAGED WEB OF AFTER AIRSTAIR TORQUE BOX HORIZONTAL WEB WAS REPAIRED PER B727 SRM 51-40-2 FIG URE 1. (M) 2 L 7 3 4F A3WE 1999051400540 19990514 00540 NE 1999 5 14 ARWA990307 2 19990325 A 7261 769792 OIL PUMP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE FAILED A ARWA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 1804 A629 45896 MIA - NR 4 ENGINE OIL PRESSURE DROPPED TO 32 PSI. SHUTDOWN ENGINE AS PER ABNORMAL CHECKLIST. WINDMILL SPEEDS WERE N1, 13.5 PERCENT, N2 21 PERCENT, OIL PRESS 3 PSI. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 E NGINE OIL PUMP ASSY IAW MM 72-60-00. OPS CHECK OK ON ENGINE RUN IAW ARROW AIR J/C 6527. (M) 2 L 7 4 4F 4 F 4A25 1E8 1999051400541 19990514 00541 NE 1999 5 14 ARWA990305 2 19990318 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 1 FAILED A ARWA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 307GB 193U131 FLT 507 - ENGINE VIBRATION ON NR 1. VIBRATION METER AT 2 UNITS, ALL OTHER PARAMETERS NORMAL, THROTTLE ON NR 1 ENGINE WA S IMMEDIATELY REDUCED, WHERE NR 1 VIBRATION METER WENT OT 1 UNIT. AFTER PHONE PATH WITH FLIGHT CONTROL, THE FLIGHT WAS DIVERTED TO SJU. THE NR 1 ENGINE WAS LEFT AT IDLE FOR REMAINDER OF FLIGHT, WHICH LANDED NORMALLY IN SJU. ENGINE WILL B E REPLACED. (M) 2 L 7 3 4F 4 F A23WE E12EU 1999051400543 19990514 00543 NE 1999 5 14 F3LA99017 2 19990221 A 7250 HOUSING BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 6 BEARING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PHX - DURING C-CHECK INSPECTION, REPORTED 9 INCH CRACK ON NR 6 TURBINE BEARING EXHAUST CASE HOUSING BETWEEN 9-12 O'CLOCK POSITION ON NR 1 ENIGNE. MAINTENANCE REPAIRED PER JT8D MM 72-54, PARAGRAPH 4. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999051400544 19990514 00544 WP 1999 5 14 RAIA990214 2 19990211 A 7310 1379305A73 FUEL LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 426AM 874 FLT 7424 - STL - RIGHT ENGINE FUEL PUMP LIGHT ILLUMINATED. MAINTENANCE REPLACED MAIN FUEL LINE ON RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999051400545 19990514 00545 NE 1999 5 14 ORJA9904 2 19990105 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RIGHT MALFUNCTIONED A ORJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 752RA 49780 AT LAS ON TAKEOFF FROM LAS, RIGHT ENGINE WOULD NOT PRODUCE TAKEOFF POWER. COULD ONLY GET 1.6 EPR. ABORTED TAKEOFF. RE TURNED TO GATE. INSPECTED NR 2 ENGINE INLETS AND EXHAUST, NO DEFECTS NOTED. INSPECTED AND CLEANED MOISTURE TRAPS. PER FORMED PER MM 71-00-00, PPS 533 AND 534. ALL PARAMETERS MET. SECURED LOOSE 'B' NUTS ON PT2 LINES. AIRCRAFT OK TO RETU RN TO SERVICE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1999051400546 19990514 00546 NE 1999 5 14 ARWA990402 2 19990416 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 1 FAILED A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 306GB 14580 193U1138 MIA - FLT 508 - NR 1 ENGINE SHUT DOWN AT 5:44 GMT, DUE LOW OIL PRESSURE AND TOTAL LOSS OF OIL, OIL PRESS 5 TO 6 PSI INDI CATED ON WINDMILLED. ZERO QTY IND LOW OIL PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED ENGINE IAW ARROW AIL FOR L- 1011-7104A. (M) 2 L 7 3 4F 4 F A23WE E12EU 1999051400547 19990514 00547 NE 1999 5 14 AALA990427 2 19990325 A 7321 7635241 RETAINER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE FUEL CONTROL SHEARED A AALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 07 271AA 49293 718256 DFW - FLT 1010 - DURING DESCENT, LT ENGINE ACCELERATED ABOVE RED LINE ON ALL PARAMETERS WITH THROTTLE AT IDLE. ENGINE W AS SHUT DOWN USING FIRE HANDLE AND WINDMILLED FOR APPROXIMATELY 10 MINUTES. A/C AIR INTERRUPTED AND LANDED DFW W/O FURT HER INCIDENT. LEFT ENGINE WAS REPLACED DUE TO OVERSPEED AND HIGH TEMPERATURE. REQUIRED LEAK, OPERATIONAL, TRIM CHECKS WERE ACCOMPLISHED WITH NO ABNORMALITIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. ENGINE FUEL CONTROL SPEED SET C AM FOLLOWER RETAINER SHEARED OFF CREATING INCORRECT DEMAND FOR ADDITIONAL SPEED. THIS RESULTED IN ENG N1 AND N2 ROTORS TO OVERSPEED. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999051400548 19990514 00548 NE 1999 5 14 HALA9900079 2 19990319 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE NR 3 FAILED A HALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 13 171AA 46906 GEN 3 OFF AND GEN FAIL LIGHTS BOTH ILLUMINATED AND NR 3 AC LOAD INDICATED ZERO. NR 3 CSD OIL PRESS LOW LIGHT ILLUMINATE D CSD OIL OUTLET TEMP NORMAL AND RISE TEMP NORMAL FOLLOWED BY INCREASE IN OUTLET TEMP AFTER SEVERAL MINUTES. OUTLET TEM P REDUCED AFTER CSD DISCONNECT. CSD NR 3 DISCONNECTED AS PER FCOM. NR 3 ENGINE OIL PRESS IN YELLOW BAND JUST AFTER GEN OFF. 20 PSI PRECAUTIONARY SHUT DOWN ENGINE NR 3 AS PER THE FCOM. ENGINE NR 3 OIL QTY INDICATES ZERO AFTER GEN FAILURE . OIL PRESS 15 PSI AFTER SHUTDOWN. CHANGED ENGINE PER DR719401 CARD AND ACCOMPLISHED POWER ASSURANCE CHECK PER DR 7195 1 CARD. (M) 2 L 7 3 4F 4 F A22WE E23EA 1999051400550 19990514 00550 NE 1999 5 14 ORJA99116 2 19990319 A 7200 TAIL PIPE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE ENGINE FIRE A ORJA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 WP 11 755RA 49727 AT SJC, MAINTENANCE ASKED FLIGHT 101 TO RETURN TO GATE AFTER OBSERVING ABNORMAL START. ENGINE START PARAMETERS DID APPE AR WITHIN NORMAL LIMITS. UPON TAXI OUT SAW EVIDENCE OF A TIAL PIPE FIRE. PERFORMED INSPECTION OF ENGINE PER MM, CHAP 7 2-00-00, PAGE 813. ALL ENGINE COMPONENTS CHECKED GOOD. DRY MOTORED FOR ONE MINUTE TO BLOW OUT EXCESSIVE FUEL. EGT REP ORT FROM CREW WAS 430 ON START PER MM. ONLY VISUAL INSPECTION REQUIRED. THIRD START ATTEMPT NORMAL. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1999051400551 19990514 00551 NM 1999 5 14 99ZZZM282 1 19990202 A 5310 STRUCTURE BOEING 727 727251 138408H NM BS 1180 CORRODED A P9RA K NONE O OTHER IN INSP/MAINT 1 SW 09 280US 21159 AEX - WHILE PERFORMING ADS, CPCP AND C2 INSPECTIONS LEVEL 2 CORROSION WAS DISCOVERED AT BS 1180 JUST FORWARD OF THE AFT AIRSTAIR DOOR AND PRESSURE BULKHEAD. REPLACED CHORD OR ANGLE JUST FORWARD OF BS 1183, RUNS FULL WIDTH OF AIRCRAFT. CLE AN AND TREATED ALL CORROSION PER SRM. STILL IN WORK AT THIS TIME. GALLEYS AND LAVS REMOVED, FLOOR PANELS REMOVED AND A LSO PULLED BINS OPEN. (M) 2 L 7 3 4F A3WE 1999051400553 19990514 00553 GL 1999 5 14 C2XA99BT006 2 19990324 A 7230 23067007 SEAL EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 09 16951 145063 SEVERAL AIR RETURNS WITH SMOKE ODOR AND 'LAV SMOKE' LIGHT ON EICAS. FINAL FIX WAS REMOVED AND REPLACED NR 2 ENGINE FAN DRIVE SEAL AND CARBON SEAL ASSY. NO FURTHER ODORS OR 'LAV SMOKE LIGHTS' ON EICAS. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 1999051400556 19990514 00556 NE 1999 5 14 99ZZZM284 2 19990208 A 7320 FUEL FLOW REG LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENGINE INOPERATIVE A AMTA K NONE O OTHER TO TAKEOFF 1 GL 11 196AT B382 193B1076 DURING TAKEOFF, NR 2 EPR DROPPED TO 460 AFTER V1, N1 88 PERCENT, TGT 650, N2 99 PERCENT, FF 2000 LBS/HR LOW THROTTLE AT FULL FORWARD POSITION, TARGET EPR 535, N1 95 PERCENT. REMOVED AND REPLACED NR 2 ENGINE FFR IAW MM CHAPTER 73-21-01, OPS AND LEAK CHECK GOOD. (M) 2 L 7 3 4F 4 F A23WE E12EU 1999051400557 19990514 00557 NE 1999 5 14 99ZZZM285 2 19990210 A 7314 FUEL PUMP LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENGINE FAILED A AMTA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 11 196AT B341 193B1076 DURING TAKEOFF ROLL EPR ON NR 2 ENGINE DECREASED FROM .530 TO .490. REMOVED AND REPLACED NR 2 ENGINE MAIN FUEL PUMP PER MM 73-11-01. LEAK CHECK GOOD ALL PARAMETERS NORMAL FOR TESTS 2, 9 AND 13. (M) 2 L 7 3 4F 4 F A23WE E12EU 1999051400559 19990514 00559 NE 1999 5 14 USAASB99078 2 19990320 A 7314 378200 FUEL PUMP BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A USAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 EA 19 263AU 22869 PHL - FLT 637 - CAPTAIN REPORTED THAT THE NR 2 ENGINE FLAMED OUT AT FL120 ON DESCENT INTO PHL. RESTART WAS ATTEMPTED, B UT UNSUCCESSFUL. APU FAILED TO START ALSO. EMERGENCY WAS DECLARED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT PHL. TO TAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP PER MM 73-11-1. ALSO , REPLACED THE FUEL CONTROL (P/N 743602-4 ON THE NR 2 ENGINE AS PRECAUTIONARY. PERFORMED ENGINE RUN. OPERATIONAL CHECK AND LEAKD CHECK GOOD. STARTED APU SEVERAL TIMES WITH NO PROBLEM. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999051400560 19990514 00560 NM 1999 5 14 USAA039916 1 19990324 A 3240 713005009 VALVE BOEING 727 727227 1384078 NM RT MLG BYPASSING A USAA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 926TS 20774 FLT 6121 - BOS-LGA - NR 3 BRAKE OVERHEATED DURING TAXI-OUT. RETURNED TO GATE. AIRCRAFT WAS DIFFICULT TO PUSHBACK. TOO L EXCESSIVE POWER TO TAXI AND PULLED TO RIGHT. AS SOON AS POWER WAS REMOVED ON TAXI AIRCRAFT CAME TO A STOP ON ITS OWN ACCORD. FOUND NR 3 BRAKE DEBOOST VALVE BYPASSING CAUSING BRAKE TO LOCKUP. REPLACED BRAKE PER MM 32-71-32, NR 3 TIRE PE R MM 32-45-1. NR 3 DEBOOSTER VALVE PER MM 32-41-21. BLED NR 3 BRAKE. REPLCED NR 4 TIRE PER MM 32-45-1. (M) 2 L 7 3 4F A3WE 1999051400561 19990514 00561 NM 1999 5 14 CLCA9903 1 19990319 A 2450 CIRCUIT BREAKER BOEING 757 75723APF 1384966 NM COCKPIT TRIPPED A CLCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 572CA 24868 FLT 33 - MIA-SAP - AIR TURN BACK, CLIMBOUT OF FL240 THE FOLLOWING OCCURED. THE LEFT IRS DISPLAYED ON DC AND EICAS MESSA GE. THE CTR AUTOPILOT DISENGAGED AND AUTO THROTTLES DISCONNECTED. SUBSEQUENTLY IT WAS OBSERVED THAT WX RADAR AND LEFT VOR/DME WERE INOPERATIVE. STATUS MESSAGES DISPLAYED WERE, FLT DATA RECORDER, GROUND PROX BITE, FLP/SLAT ELECTRIC. WARNI NG ELEC AND CAPTAIN INSTR XFER. ADDITIONALLY AFTER RETURNING TO MIA AND LANDING DURING TAXI, RUDDER PCU, RT ELEV AND LT ELEV PCU STATUS MESSAGES DISPLAYED. NORMAL LANDING. RESET ALL LEFT BUS POWER BREAKERS. RESET MAIN POWER. ALL RELATE D EICAS MESSAGES WERE ERASED. PERFORMED MCDP TEST 30. ALL CURRENT FAULT TESTS IAW BOEING MM 22-00-02. NO DEFECTS NOTE 2 L 7 2 4F RT A2NM 1999051400562 19990514 00562 NE 1999 5 14 PLGA990301A 2 19990301 A 7510 0058T80P03 BLEED VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE MALFUNCTIONED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 334BE COMD0506 340A158 BOS-PHL - FLT 6433 - AFTER TAKEOFF, LEFT AIRVALVE LIGHT ILLUMINATED. AIRCRAFT DIVERTED BACK TO BOS AND LANDED WITHOUT I NCIDENT. MAINTENANCE REPLACED THE LEFT ANTI-ICE START BLEED VALVE (P/N 0058T80P03, S/N COMD0506) AND THE BLEED AIR SHUT OFF VLV (P/N 5056T88P01, S/N AFX10598). AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999051400563 19990514 00563 NE 1999 5 14 PLGA990228 2 19990228 A 7510 6058T8P03 BLEED VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE MALFUNCTIONED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 746BA COMD0314 340A138 LGA-PWM - FLT 6556 - DIVERTED TO LGA DUE TO RIGHT AIR VALVE LIGHT ILLUMINATING. AIRCRAFT LANDED WITHOUT INCIDENT. MAIN TENANCE REPLACED THE ANTI-ICE START/BLEED VALVE AND THE BLEED AIR SHUTOFF VALVE, PERFORMED THE REQUIRED OPERATIONAL CHEC KS AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999051400564 19990514 00564 NE 1999 5 14 PLGA990124D 2 19990124 A 7321 7086M60G11 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE MALFUNCTIONED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 745BA 340A111 BOS - FLT 6408 - CREW REPORTED LEFT ENGINE OPERATION ERRATIC. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED THE ECU. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999051400565 19990514 00565 NE 1999 5 14 PLGA990301C 2 19990301 A 7597 WIRE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE AIRFRAME BROKEN A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 744BA 340A105 BOS - FLT 6394 - AFTER DEPARTURE FROM BOS, THE CREW GOT A RIGHT AIR VALVE LIGHT. CREW DIVERTED BACK TO BOS AND LANDED W ITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND FOUND A BROKEN WIRE AT THE AIRFRAME CANNON PLUG. REPAIRED THE WIRE A ND THE SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999051400566 19990514 00566 NE 1999 5 14 PLGA990109 2 19990109 A 7260 CHIP LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE ILLUMINATED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 344BE 340A104 LGA - FLT 6553 - AFTER TAKEOFF, THE LEFT ENGINE CHP DETECTOR LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED REQUIRED CHIP DETECTOR AND SCAVENGE SCREEN INSPECTIONS PER GE MM AN D FOUND NO DEBRIS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999051400567 19990514 00567 NM 1999 5 14 99ZZZM287 1 19990331 A 2597 WIRE DOUG MD11 MD11F 3023600 NM BS 1681 CHAFED A P WRLA O OTHER A FLAME/FIRE NR NOT REPORTED 1 EA 27 274WA 48633 DURING ACCOMPLISHMENT OF A 4C CHECK MAINTENANCE PERSONNEL, FOUND INSULATION BLANKET BURNED AT STATION 1661-1681, BILGE A REA FROM KEEL UP APPROXIMATELY 40 INCHES (ZONE 183). FURTHER INVESTIGATION FOUND THAT WIRE BUNDLE FROM CARGO COMPARMENT LOADING SYSTEM LOAD CONTROLLER TO CARGO SYSTEM POWER ROLLER MOTORS HAD CHAFED AGAINST FUSELAGE FRAME AT STATION 1681 WI TH EVIDENCE OF ARCHING, WIRE BURNED THROUGH. (M) 2 L 7 3 4F RT A22WE 1999051400568 19990514 00568 EU 1999 5 14 VTZA9907723 1 19990326 A 3010 297D524337 DE-ICE BOOT JETAIR JETSTM JETSTM4101 1500501 EU LT HORIZ STAB TORN A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 27 316UE 41055 FLT 7295 - BUF-IAD - DURING CRUISE, AIRCRAFT DIVERTED TO MDT DUE TO CREW HEAD AND FELT VIBRATION. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND LEFT HORIZONTAL DE-ICE BOOT LOOSE AND RIPPED. MAINTENANCE R EMOVED AND REPLACED LEFT HORIZONTAL DE-ICE BOOT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A41NM 1999051400569 19990514 00569 WP 1999 5 14 VTZA9907722 2 19990318 A 7310 8975131 FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE DIRTY A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 322UE 41058 IAD-EWR - BEFORE TAKEOFF, RETURNED TO GATE DUE TO FUEL FILTER LIGHT. MAINTENANCE REMOVED AND REPLACED LEFT FUEL FILTER. OPS AND LEAK CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999051400570 19990514 00570 EU 1999 5 14 VTZA9907719 1 19990318 A 2150 ACM JETAIR JETSTM JETSTM4101 1500501 EU RIGHT MALFUNCTIONED A VTZA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 309UE 41022 FLT 7253 - IAD-RIC - DURING TAXI, RETURNED TO GATE DUE TO RIGHT DUCT TEMP. MAINTENANCE FREED RIGHT ACM, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999051400571 19990514 00571 1999 5 14 99ZZZM288 4 19990317 A 6122 89741016 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 477UE 890 FLT 7652 - IAD-PHL - DURING TAKEOFF, AIRCRAFT RETURNED FROM FLIGHT DUE TO NR 2 ENGINE ONLY PRODUCING 98.5 PERCENT. MAIN TENANCE REMOVED AND REPLACED RT ENGINE PROP GOVERNOR, OPS AND LEAK CHECK GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A56EU 1999051400572 19990514 00572 1999 5 14 VTZA9907707 4 19990314 A 3420 7012100811 RMU JETAIR JETSTM JETSTM4101 1500501 EU LEFT/RIGHT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 306UE 41020 FLT 7306 - IAD-BUF - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT IAD DUE TO BOTH RMUS INOPERATIVE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT AND LEFT RMU OPS CHECK GOOD. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999051400573 19990514 00573 EU 1999 5 14 VTZA9907381 1 19990311 A 6120 31055863 MONOPOLE JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 317UE 41031 FLT 7522 - IAD-EWR - DURING CLIMB, RETURNED FROM FLIGHT DUE TO RIGHT PROP RPM IND FLUX. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SPEED MONOPOLE, OPS CHECK OK. AIRCRAFT WAS RELEASE D AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999051400574 19990514 00574 EU 1999 5 14 REXA99010 1 19990411 A 3241 LIGHT SAAB SF340 SF340A 7850100 EU ANTI-SKID SYSTEM ILLUMINATED A REXA C ABORTED TAKEOFF O OTHER DE DESCENT 1 SO 25 403BH 340A060 ANTI-SKID LIGHT CAME ON DURING FLIGHT. INSPECTED SYSTEM WIRING AND COMPONENTS. CLEANED ALL WEIGHT ON WHEELS SWITCHES A ND HARNESS CONNECTORS. (M) 2 L 7 2 4T RT A52EU 1999051400575 19990514 00575 EU 1999 5 14 REXA99009 1 19990407 A 5610 7256100503 WINDSHIELD SAAB SF340 340B 7860101 EU LT COCKPIT CRACKED A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 369PX 340B295 LEFT FORWARD WINDSHIELD DEVELOPED CRACK INFLIGHT. REMOVED AND REPLACED LEFT FORWARD WINDSHIELD. (M) 2 L 7 2 4T RT A52EU 1999051400576 19990514 00576 EU 1999 5 14 REXA99008 1 19990412 A 2710 MS2764116 BEARING SAAB SF340 SF340A 7850100 EU AILERON CORRODED A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 401BH 340A057 AILERONS HARD TO TURN TO THE LEFT. REMOVED AND REPLACED LEFT AND RIGHT TOWER MOUNT BEARINGS. (M) 2 L 7 2 4T RT A52EU 1999051400577 19990514 00577 EU 1999 5 14 REXA99012 1 19990419 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU MLG BROKEN A REXA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 935MA 340A073 HYDRAULIC LEAK RIGHT GEAR BAY. REMOVED AND REPLACED BROKEN DOWNLOCK SWIVEL ON RIGHT MAIN GEAR. (M) 2 L 7 2 4T RT A52EU 1999051400578 19990514 00578 EU 1999 5 14 REXA99011 1 19990416 A 2450 A2042C PDU SAAB SF340 SF340A 7850100 EU LEFT FAILED A REXA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 SO 25 326PX CG93815 340A054 LOST LEFT MAIN BUSS, LEFT ESSENTIAL BUS AND MAIN INVERTER ON APPROACH. REMOVED AND REPLACED LEFT POWER DISTRIBUTION UNI T. (M) 2 L 7 2 4T RT A52EU 1999051400579 19990514 00579 NM 1999 5 14 USAASB99095 1 19990410 A 3230 RETRACT MECH BOEING 737 7372B7 1384560 NM LANDING GEAR LACK OF LUBE A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 270AU 22882 ATL - FLT 2751 - AFTER TAKEOFF FROM IAD, THE LANDING GEAR FREE FELL (EXTENDED) WITH THE LANDNG GEAR HANDLE IN THE 'OFF' POSITION. CREW WAS ABLE TO RETRACT GEAR AND THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE LUBR ICATED THE NOSE AND MAIN LANDING GEAR UPLOCKS AND ROLLERS. CYCLED GEAR SEVERAL TIMES. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999051400580 19990514 00580 WP 1999 5 14 USAA990351 1 19990407 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 912VJ 74381 47020 PIT - DURING C-6 CHECK, FOUND TWO 1 INCH CRACKS IN BELLFRAME STATION 1076 LONGERON 14L. STOP DRILLED CRACKS AND INSTALL ED A DOUBLER PER EA 51889. (M) 2 L 7 2 4F A6WE 1999051400581 19990514 00581 WP 1999 5 14 USAA990352 1 19990407 A 5311 FRME DOUG DC9 DC931 3022065 WP BS 1074 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 912VJ 74381 47020 PIT - DURING C-6 CHECK, FOUND 2 INCH CRACK IN BELLFRAME AT STATION 1074 LONGERON 14R. INSTALLED A REPAIR DOUBLER PER SR M 53-03 FIG 30. (M) 2 L 7 2 4F A6WE 1999051400582 19990514 00582 EU 1999 5 14 GAIA9944A 2 19990413 A 7200 ENGINE CVAC 240 240D 2422660 WP RROYCE DART DART5424 54522 EU NR 2 FAILED A GAIA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 07 94205 10 40135 FLT 574 - MEM - AFTER DEPARTURE, THE NR 2 ENGINE FAILED SHORTLY AFTER LEVELING OFF AT 11,000. POWER WAS SET AT 14,200 T EMP 770. ENGINE RPM DECREASED RAPIDLY WITH NO WARNING. TEMP PEAKED A 920 BEFORE CONDITION LEVER WAS PLACED IN FEATHER. POWERPLANT WAS OPERATING NORMAL PRIOR TO FAILURE. EMERGENCY DECLARED AIRCRAFT RETURNED TO MEM AND UNEVENTFUL LANDING MADE. ENGINE FAILURE UNDER INVESTIGATION. ENGINE S/N 40135 WAS REMOVED AND REPLACED WITH A SERVICEABLE ENGINE AND THE AIRCRAFT RETURNED TO SERVICE. THE DAMAGED ENGINE AT THIS TIME IS BEYOND ECONOMICAL REPAIR. (M) 2 L 7 2 4R 4 T RT A793 E5EU 1999051400583 19990514 00583 NM 1999 5 14 GAIA9946 1 19990408 A 2613 OVERHEAT LIGHT BOEING 727 727223 1384074 NM NR 1 STRUT ILLUMINATED A GAIA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 6806 19481 AFTER DEPARTING SEA, NR 1 OVERHEAT STRUT LIGHT CAME ON IN CLIMB. ANTI-ICE WAS CLOSED. AIRCRAFT MADE AN UNEVENTFUL LAND ING AT DFW. RAN NR 1 ENGINE AND COULD NOT DUPLICATE THE PROBLEM ON GROUND. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SER VICE WITH NO FURTHER PROBLEMS NOTED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT DFW. (M) 2 L 7 3 4F A3WE 1999051400584 19990514 00584 NM 1999 5 14 GAIA9948 1 19990409 A 3260 656021138 ACCESSORY BOX BOEING 727 727224 1384076 NM LANDING GEAR MALFUNCTION A GAIA K NONE N FALSE WARNING AP APPROACH 1 SW 07 69739 20667 ON FINAL APPROACH TO TOL, PUT GEAR DOWN AND 3 RED LIGHTS, AND 3 GREEN LIGHTS AND TAIL SKID LIGHT. RECYCLED GEAR AND GOT 3 GREEN LIGHTS, NORMAL INDICATIONS. AIRCRAFT MADE AN UNEVENTFUL LANDING AT TOL. REMOVED AND REPLACED LANDING GEAR ACC ESSORY BOX. OPERATIONALLY CHECKS GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE WITH NO ADDITIONAL PROBLEMS NOTED. (M) 2 L 7 3 4F A3WE 1999051400585 19990514 00585 NM 1999 5 14 GAIA9949 1 19990420 A 3260 H1010153 SWITCH BOEING 727 727251 138408H NM NLG FAILED A GAIA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 278US 21157 AFTER TAKEOFF FROM BRO, THE GEAR WAS RETRACTED AND THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. WHEN GEAR POSITIONED T O DOWN RED NOSE GEAR UNSAFE LIGHT REMAINED ON. MANUALLY EXTENDED NOSE GEAR AND NOSE GEAR DOWN LIGHT REMAINED EXTINGUISH ED. THE AIRCRAFT LANDED SAFELY IN BSM WITHOUT FURTHER DIFFICULTY. MAINTENANCE FERRIED THE AIRCRAFT TO DFW WHERE THERE IS AVAILABILITY OF JACKS. FOUND NLG LOCK SWITCH AND NLG POSITION SWITCH BAD. PERFORMED NLG SWING PER BOEING MM 32-33-0 . OPERATIONALLY CHECKS GOOD. THE AIRCRAFT IS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999051400586 19990514 00586 NM 1999 5 14 99ZZZM289 1 19990420 A 3260 H1010154 SWITCH BOEING 727 727251 138408H NM NLG FAILED A GAIA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 278US 21157 AFTER TAKEOFF FROM BRO, THE GEAR WAS RETRACTED AND THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. WHEN GEAR POSITIONED T O DOWN RED NOSE GEAR UNSAFE LIGHT REMAINED ON. MANUALLY EXTENDED NOSE GEAR AND NOSE GEAR DOWN LIGHT REMAINED EXTINGUISH ED. THE AIRCRAFT LANDED SAFELY IN BSM WITHOUT FURTHER DIFFICULTY. MAINTENANCE FERRIED THE AIRCRAFT TO DFW WHERE THERE IS AVAILABILITY OF JACKS. FOUND NLG LOCK SWITCH AND NLG POSITION SWITCH BAD. PERFORMED NLG SWING PER BOEING MM 32-33-0 . OPERATIONALLY CHECKS GOOD. THE AIRCRAFT IS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999051400587 19990514 00587 NM 1999 5 14 GAIA9950 1 19990419 A 3350 BATTERIES BOEING 727 727224 1384076 NM CABIN DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 69739 20667 DURING ROUTINE 'B' CHECK MAINTENANCE, FOUND TWO, EACH FORWARD EMERGENCY EXIT LIGHTS WITH DEAD BATTERIES. REMOVED AND RE PLACED TWO FORWARD ENTRY AREA "EMERGENCY EXIT' LIGHTS. NO ADDITIONAL PROBLEMS WERE NOTED. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 3 4F A3WE 1999051400588 19990514 00588 NE 1999 5 14 MASA99052 2 19990327 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 FAILED A MASA C D ABORTED TAKEOFF RETURN TO BLOCK T ENGINE CASE PENETRATION TO TAKEOFF 1 SW 07 93ZV UE93 FLT 6217 - PHX-FLG - CREW NOTED A LOUD NOISE AND THE NR 2 ENGINE ITT FLUCTUATED ON TAKEOFF ROLL. TAKEOFF WAS ABORTED AN D THE AIRCRAFT WAS RETURNED TO THE GATE. PIECES OF SOME OF THE BLADES WERE FOUND IN THE EXHAUST STACK. THE ENGINE IS B EING REMOVED AND REPLACED AND FURTHER INFORMATION WILL BE FORTHCOMING WHEN THE TEARDOWN REPORT IS RECEIVED. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999051400589 19990514 00589 NM 1999 5 14 MASA99031 1 19990221 A 5210 85210180001 SPRING DHAV DHC8 DHC8202 2809007 NM PAX DOOR BENT A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 448YV 448 FLT 6330 - PRIOR TO DEPARTURE, CREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE D OOR AND FOUND THAT THE CABLE PULLEY HAD TOO MUCH SLACK AND WAS BINDING AT THE DOOR HINGE. MAINTENANCE REMOVED THE CABLE . MAINTENANCE CONTROL DEFERRED THE DISCREPANCY AND PLACARDED BOTH SIDES OF THE DOOR. IN SUBSEQUENT MAINTENANCE REMOVED AND REPLACED THE GAS SPRINGS AND STRUT CABLE. (M) 2 H 7 2 4T RT A13NM 1999051400590 19990514 00590 NM 1999 5 14 99ZZZM290 1 19990221 A 5210 85210263101 CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR FRAYED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 448YV 448 FLT 6330 - PRIOR TO DEPARTURE, CREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE D OOR AND FOUND THAT THE CABLE PULLEY HAD TOO MUCH SLACK AND WAS BINDING AT THE DOOR HINGE. MAINTENANCE REMOVED THE CABLE . MAINTENANCE CONTROL DEFERRED THE DISCREPANCY AND PLACARDED BOTH SIDES OF THE DOOR. IN SUBSEQUENT MAINTENANCE REMOVED AND REPLACED THE GAS SPRINGS AND STRUT CABLE. (M) 2 H 7 2 4T RT A13NM 1999051400591 19990514 00591 NM 1999 5 14 MASA99055 1 19990403 A 5210 85210240005 HANDRAIL DHAV DHC8 DHC8202 2809007 NM PAX DOOR BENT A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 446YV 446 FLT 6325 - GJT-PHX - UPON ARRIVAL IN PHX, WHEN OPENING THE PASSENGER DOOR, THE DOOR FREE FELL. SUBMITTER STATES, IT IS FELT THAT IN GJT, THE RAMP AGEN CLOSED THE DOOR TOO FAST, BENDING THE HANDRAIL MECHANISM. THE SUPPORTING STRUTS HAD TO BE DISCONNECTED IN ORDER TO CLOSE THE DOOR. THE AIRCRAFT WAS FERRIED TO GJT WHERE MAINTENANCE REMOVED AND REPLACED A HA NDRAIL MECHANISM UPPER STRUT ASSEMBLY, TWO GAS SPRINGS AND A DOOR CABLE. OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A13NM 1999051400592 19990514 00592 NM 1999 5 14 99ZZZM291 1 19990403 A 5210 STRUT ASSY DHAV DHC8 DHC8202 2809007 NM PAX DOOR DAMAGED A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 446YV 446 FLT 6325 - GJT-PHX - UPON ARRIVAL IN PHX, WHEN OPENING THE PASSENGER DOOR, THE DOOR FREE FELL. SUBMITTER STATES, IT IS FELT THAT IN GJT, THE RAMP AGEN CLOSED THE DOOR TOO FAST, BENDING THE HANDRAIL MECHANISM. THE SUPPORTING STRUTS HAD TO BE DISCONNECTED IN ORDER TO CLOSE THE DOOR. THE AIRCRAFT WAS FERRIED TO GJT WHERE MAINTENANCE REMOVED AND REPLACED A HA NDRAIL MECHANISM UPPER STRUT ASSEMBLY, TWO GAS SPRINGS AND A DOOR CABLE. OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A13NM 1999051400593 19990514 00593 NM 1999 5 14 99ZZZM292 1 19990403 A 5210 85210263101 GAS SPRING DHAV DHC8 DHC8202 2809007 NM PAX DOOR BENT A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 446YV 446 FLT 6325 - GJT-PHX - UPON ARRIVAL IN PHX, WHEN OPENING THE PASSENGER DOOR, THE DOOR FREE FELL. SUBMITTER STATES, IT IS FELT THAT IN GJT, THE RAMP AGEN CLOSED THE DOOR TOO FAST, BENDING THE HANDRAIL MECHANISM. THE SUPPORTING STRUTS HAD TO BE DISCONNECTED IN ORDER TO CLOSE THE DOOR. THE AIRCRAFT WAS FERRIED TO GJT WHERE MAINTENANCE REMOVED AND REPLACED A HA NDRAIL MECHANISM UPPER STRUT ASSEMBLY, TWO GAS SPRINGS AND A DOOR CABLE. OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A13NM 1999051400594 19990514 00594 NM 1999 5 14 99ZZZM293 1 19990403 A 5210 85210368001 DOOR CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR FRAYED A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 446YV 446 FLT 6325 - GJT-PHX - UPON ARRIVAL IN PHX, WHEN OPENING THE PASSENGER DOOR, THE DOOR FREE FELL. SUBMITTER STATES, IT IS FELT THAT IN GJT, THE RAMP AGEN CLOSED THE DOOR TOO FAST, BENDING THE HANDRAIL MECHANISM. THE SUPPORTING STRUTS HAD TO BE DISCONNECTED IN ORDER TO CLOSE THE DOOR. THE AIRCRAFT WAS FERRIED TO GJT WHERE MAINTENANCE REMOVED AND REPLACED A HA NDRAIL MECHANISM UPPER STRUT ASSEMBLY, TWO GAS SPRINGS AND A DOOR CABLE. OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A13NM 1999051400595 19990514 00595 EA 1999 5 14 MASA99060 1 19990419 A 3350 1317 BULB BRUCE BM10020004 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7219 CLT/YYZ - FLT 5774 - CREW REPORTED THE AFT CEILING EMERGENCY LIGHT WAS INOPERABLE. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (X) 2 L 7 2 4F RT A21EA 1999051400596 19990514 00596 EU 1999 5 14 AALA990502 1 19990411 A 3350 321440 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 8067A 510 JFK - DURING MAINTENANCE CHECK, UNABLE TO TURN OFF OVERHEAD EMERGENCY LIGHTS. MAINTENANCE REPLACED EMERGENCY POWER SUPP LY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999051400597 19990514 00597 WP 1999 5 14 AALA990469 1 19990406 A 3350 A3060722 BULB DOUG DC10 DC1030 3023501 WP ROW 21H FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 164AA 46950 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT ROW 21H INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT ASSEMBLY AT SEAT ROW 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999051400598 19990514 00598 WP 1999 5 14 AALA990400 1 19990316 A 3350 P2010031302 LIGHT DOUG DC10 DC1030 3023501 WP ROW 12H INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 137AA 47847 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 12H INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T ASSEMBLY AT SEAT 12H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999051400600 19990514 00600 NM 1999 5 14 AALA990303 1 19990304 A 3397 WIRE DOUG MD11 MD11 3023602 NM 2R DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT 2R DOOR HAS ONE BULB INOPERATIVE. REPLACED EMERG ENCY EXIT FLOOR PATH FLAT WIRE AT 2R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400601 19990514 00601 NM 1999 5 14 AALA990430 1 19990329 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM ROW 27C LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 27C AND 28C WERE INOPERATIVE. RESEATE D EMERGENCY FLOOR PATH LIGHT WIRE CONNECTOR IN FLOOR TRACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400602 19990514 00602 NM 1999 5 14 AALA990403 1 19990318 A 3397 WIRE DOUG MD11 MD11 3023602 NM R2 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT MAINTENANCE, DOOR MOUNTED EMERGENCY EXIT IDENTIFIER AT R2 DOOR IS INOPERATIVE. RESEATED DOOR MOU NTED EMERGENCY EXIT IDENTIFIER TERMINAL WIRE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400603 19990514 00603 NM 1999 5 14 AALA990404 1 19990318 A 3350 LIGHT DOUG MD11 MD11 3023602 NM ROW 20G DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 20G WERE INOPERATIVE. REPLACED EMERGENCY FLO OR PATH LIGHT STRIP AT SEAT ROW 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400604 19990514 00604 NM 1999 5 14 AALA990405 1 19990318 A 3350 LIGHT DOUG MD11 MD11 3023602 NM ROW 15G DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 15G WERE INOPERATIVE. REPLACED EMERGENCY FLO OR PATH LIGHT STRIP AT SEAT ROW 15G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400605 19990514 00605 NM 1999 5 14 AALA990014 1 19990106 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING WAS INOPERATIVE BETWEEN 3R AND 4R DOORS. FOUND E MERGENCY EXIT FLOOR PATH LIGHT WIRE SHORTED. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE AT SIDEWALL AFT OF R-3 LAVAT ORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400606 19990514 00606 NM 1999 5 14 AALA990463 1 19990406 A 7930 1163P182 SWITCH BOEING 727 727223 1384074 NM NR 1 ENGINE DEFECTIVE A AALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 07 875AA 1146N 21387 MIA - FLT 808 - EN ROUTE POP, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. CREW FOLLOWED CHECKLIST AND SH UTDOWN NR 1 ENGINE. ENGINE WINDMILL TIME WAS 1 HOUR AND 15 MINUTES. FLIGHT CONTINUED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED SCREENS AND CHIP DETECTOR. NO DEBRIS NOTED. REPLACED OIL FILTER ELEMENT AND OIL BYPASS SWITCH. GROUND RAN ENGINE WITH ALL INDICATIONS NORMAL. LEAK CHECK WAS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 3 4F A3WE 1999051400607 19990514 00607 NM 1999 5 14 AALA990456 1 19990331 A 3260 849704 PROX ELECT UNIT ELDEC BOEING 767 767323 1385205 NM E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 7375A 586 25202 MIA - FLT 2101 - ON TAKEOFF UPON RAISING THE GEAR, THE GEAR DOOR AMBER WARNING LIGHT REMAINED ILLUMINATED. EICAS MESSAG E ILLUMINATED WHEN GEAR HANDLE WAS PLACED TO OFF POSITION AND THE LEFT GEAR EXTENDED AND LOCKED IN THE DOWN POSITION. A IRCRAFT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED REQUIRED CHEC KS OF DOOR AND LOCK MECHANISMS WITH NO FAULTS NOTED. MAINTENANCE REPLACED GROUND PROXIMITY ELECTRONIC UNIT. ACCOMPLISH ED LANDING GEAR CONTROL ADJUSTMENT AND SWUNG GEAR WITH NO MESSAGES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999051400608 19990514 00608 NM 1999 5 14 AALA990018 1 19990104 A 3397 WIRE DOUG MD11 MD11 3023602 NM ROW 21C DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 21C INOPERATIVE. REPLACED EMERGENCY EX IT FLOOR PATH FLAT JUMPER WIRE AT SEAT ROW 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400609 19990514 00609 WP 1999 5 14 AALA990476 1 19990407 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 3E DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 233AA 49180 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 3E TO BULKHEAD INOPERATIVE. REPLACED EMERGENCY F LOOR PATH LIGHT STRIP AT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999051400610 19990514 00610 WP 1999 5 14 AALA990485 1 19990409 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP TAILCONE DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7546A 53028 DFW - DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT TAIL CONE EMERGENCY EX IT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999051400611 19990514 00611 WP 1999 5 14 AALA990484 1 19990410 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 583AA 53160 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD CABIN INOPERATIVE. RESEATED EMERGENCY E XIT FLOOR PATH LIGHT WIRE CONNECTOR IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999051400612 19990514 00612 WP 1999 5 14 AALA990478 1 19990408 A 3350 LIGHT DOUG DC9 DC982 3022082 WP GALLEY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7537A 49991 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOO R PATH LIGHT STRIP AT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999051400613 19990514 00613 NM 1999 5 14 AALA990017 1 19990104 A 3397 WIRE DOUG MD11 MD11 3023602 NM ROW 20C DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 20C INOPERATIVE. REPLACED EMERGENCY EX IT FLOOR PATH FLAT JUMPER WIRE AT SEAT ROW 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400618 19990514 00618 1999 5 14 AALA990135 4 19990131 A 2330 6000040007 CONTROL UNIT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1765B 00025577 48596 SEA - FLT 27 - DURING CRUISE A LOUD BUSS HEAD OVER COCKPIT SPEAKER AND WAS SILENCED BY PUSHING THE PA SELECTOR. NR 1 FL T ATTENDANT REPORTED SMOKE FROM THE VIDEO SYSTEM. 1ST OFFICER INVESTIGATED AND DISHARGED THE HALON FIRE EXTINGUISHER IN TO THE AREA. C/B'S WERE PULLED WITH NO FURTHER SMOKE. A/C AIR INTERRUPTED AND RETURNED TO SEA WITHOUT FURTHER INCIDENT . THE SYSTEM WAS DEACTIVATED AND THE VIDEO SYSTEM CONTROL UNIT WAS SENT TO THE SUPPLIER. TECHS FOUND THE UNIT HAD A LO W RESISTANCE FAULT FROM DC GROUND THE VIDEO 3 HI SIGNAL. THIS PATH PROVIDED THE ENERGY AND VOLTAGE NECESSARY TO CAUSE S MOKE TO APPEAR IN THE CABIN. THIS FAILURE IS AN ISOLATED INCIDENT. (M) 2 L 7 3 4F RT A22WE 1999051400619 19990514 00619 WP 1999 5 14 AALA990175 1 19990213 A 3350 CONNECTOR DOUG DC10 DC1010 3022110 WP ROW 15H BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130AA 46989 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROW 15H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CO NNECTOR AT SEAT ROW 15H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999051400623 19990514 00623 EU 1999 5 14 AALA990428 1 19990328 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROW 12 DEFECTIVE A AALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 14056 463 MIA - FLT 882 - DURING PASSENGER DEPLANING, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 12B WERE TORN OUT AND INOPERATI VE. REPLACED EMERGENCY FLOOR PATH LIGHT STRIP AT SEAT ROW 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999051400624 19990514 00624 EU 1999 5 14 AALA990435 1 19990330 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU ROW 14-25 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80057 465 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 14 THROUGHT 25 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT FLAP JUMPER WIRE AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999051400625 19990514 00625 EU 1999 5 14 AALA990275 1 19990224 A 2421 IDG AIRBUS 300 A300B4605R 3930308 EU NR 1 ENGINE MALFUNCTIONED A AALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 07 14068 K0336 511 ENGINE NR 1 GENERATOR PUTTING OUT HIGH FREQUENCY, IDG DISCONNECTED. LEFT IDG REPLACED IAW A300 MM. LEFT IDG SERVICED. SEE PIREP 37 FOR OPERATIONAL CHECK AND LEAK CHECK. MAINTENANCE ENTRY, REF PIREP 34. LEFT IDG REQUIRES FULL OPERATIONA L CHECK AND LEAK CHECK AFTER REPLACEMENT. ACCOMPLISHED LEFT ENGINE RUN, IDG OPS AND IND NORMAL. LEAK CHECKS OK. (M) 2 L 7 2 4F RT A35EU 1999051400626 19990514 00626 NE 1999 5 14 AALA990479 2 19990406 A 7230 815754 CARBON SEAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENGINE FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 430AA 11030 49342 SMF - FLT 752 - DURING CLIMB-OUT, RIGHT ENGINE EXPERIENCED OIL QTY LOSS, RISE IN OIL TEMP, AND LOSS OF OIL PRESSURE. EN G WAS SECURED, THE CREW DECLARED AN EMERGENCY AND DIVERTED TO SMF. A/C LANDED SMF WITHOUT FURTHER INCIDENT. RIGHT ENGI NE WAS REPLACED DUE TO OIL LOSS AND HIGH OIL TEMPERATURE. REQUIRED LEAK, OPERATIONAL, TRIM CHECKS WERE ACCOMPLISHED WIT H NO ABNORMALITIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. THE NR 6 CARBON SEAL WAS BROKEN IN PIECES AND FOUND IN THE BOTTOM OF THE NR 6 BEARING HOUSING. THE PIECES PARTIALLY BLOCKED THE NR 6 SCAVENGE PUMP INLET SCREEN. THE BROKE N NUMBER 6 CARBON SEAL AND SCAVENGE PUMP INLET SCREEN BLOCKAGE CAUSED THE LOSS OF OIL. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999051400627 19990514 00627 WP 1999 5 14 AALA990482 1 19990409 A 2932 SS092900037001 TRANSMITTER DOUG DC9 DC982 3022082 WP LT HYD SYSTEM DEFECTIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 241AA 8550BA 49254 DFW - FLT 1322 - DURING CRUISE, LEFT HYDRAULIC QTY AND PRESSURE DECREASED TO ZERO. FLIGHT AIR INTERRUPTED AND RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEFT PRESSURE TRANSMITTER CASE SPLIT AND LEAKING. REPLACED LEFT PRESSURE TRANSMITTER AND SYSTEM LEAK CHECKED WITH NO LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999051400628 19990514 00628 NM 1999 5 14 AALA990491 1 19990412 A 3350 487191 CONNECTOR BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 22335 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT AFT GALLEY CROSS AISLE INOPERATIVE. REPLACED EMERGENCY EXI T LIGHT CONNECTOR AT AFT GALLEY CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999051400629 19990514 00629 NM 1999 5 14 AALA990483 1 19990409 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661AA 25295 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED CONNECTOR ON EMERGENCY EXIT LIGHTS. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999051400630 19990514 00630 NM 1999 5 14 AALA990490 1 19990310 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 623AA 12294 24581 SJU - FLT 1894 - DURING FLIGHT, EMERGENCY EXIT PATH LIGHTS ILLUMINATED INTERMITTENTLY. RECONNECTED END CONNECTOR ON AFT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999051400633 19990514 00633 NM 1999 5 14 AALA990517 1 19990414 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1050-1055 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND CORROSION IN STRINGER. CUT OUT SECTION OF CORROSION AND INSTALLED REPAIR PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999051400634 19990514 00634 NM 1999 5 14 AALA990516 1 19990414 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1165 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND CORROSION ON SHEAR TIE. CUT OUT CORROSION AND INSTALLED DOUBLER PER 53-10-4. (M) 2 L 7 3 4F A3WE 1999051400635 19990514 00635 NM 1999 5 14 AALA990515 1 19990414 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND WHILE ON CUTTING OUT CORROSION ON SHEAR TIE SKIN WAS DAMAGED. GROUND OUT DAMAGE AND INSTALLED DOUBLER ON EX IT SKIN PER SRM 53-30-3 FIG AND AARD 53-30-03-3 .071 2024T3. (M) 2 L 7 3 4F A3WE 1999051400636 19990514 00636 NM 1999 5 14 AALA990514 1 19990514 A 5330 SKIN BOEING 727 727223 1384074 NM BS 416 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND SKIN CRACKED AT LOWR AFT CORNER OF RIGHT SERVICE DOOR CUTOUT, FORWARD GALLEY DOOR. REMOVED DAMAGED AREA. I NSTALLED DOUBLER REPAIR PER SB 727-53-0188 FIG 2. (M) 2 L 7 3 4F A3WE 1999051400637 19990514 00637 NM 1999 5 14 AALA990513 1 19990414 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680-688 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND CORROSION ON SKIN STATION 680-688, STRINGER 27R. REMOVED CORROSION AND INSTALLED DOUBLER PER 53-30-3 FIG 3A . (M) 2 L 7 3 4F A3WE 1999051400638 19990514 00638 NM 1999 5 14 AALA990512 1 19990408 A 5330 SKIN BOEING 727 727223 1384074 NM BS 684-688 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FUSELAGE SKIN CORROSION AT SKIN LAP 26R OUTBOARD SIDE STATION 684-688. FUSELAGE SKIN CORROSION AT OUTBOARD SIDE O F 27R STATION 685. REMOVED SECTION OF SKIN LAP 2 INCH BY 3 INCH, INSTALLED EXTERNAL DOUBLE OVER BOTH AREAS 680-680 PLUS 18. OVERALL DIMENSION 10 INCH BY 17 INCH 2024T3 .071 THICKNESS PER SRM 53-30-3 FIG 3A. (M) 2 L 7 3 4F A3WE 1999051400639 19990514 00639 NM 1999 5 14 AALA990511 1 19990511 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1050-1055 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND CORROSION ON SKIN. CORROSION ON SKIN CUTOUT AND DOUBLER INSTALLED PER 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1999051400640 19990514 00640 NM 1999 5 14 AALA990510 1 19990414 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND CORROSION ON SHEAR TIE AFT SIDE 11130 FRAME STRINGER 28-29L. REMOVED SHEAR TIE CLEANED CORROSION IN AREA IA W INSTALLED NEW SHEAR TIE PER SRM. (M) 2 L 7 3 4F A3WE 1999051400641 19990514 00641 NM 1999 5 14 AALA990509 1 19990414 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND HOLE IN BELL FRAME FROM SIDEWALL SCREW. INSTALLED DOUBLER PER 51-40-3. (M) 2 L 7 3 4F A3WE 1999051400642 19990514 00642 NM 1999 5 14 AALA990508 1 19990414 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND CRACK IN BELL FRAME. CUTOUT DAMAGED AREA AND INSTALLED REPAIR PER 51-40-3. (M) 2 L 7 3 4F A3WE 1999051400643 19990514 00643 NM 1999 5 14 AALA990507 1 19990407 A 5720 ANGLE BOEING 727 727223 1384074 NM WS 519 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND UPPER SURFACE OF LOWER CHORD ON RIGHT WING L/E BELOW NR 6 SLAT ACT HAS HEAVY CORROSION. REPAIRED PER AARD 5 7-30-00-2 PAGE 1. (M) 2 L 7 3 4F A3WE 1999051400644 19990514 00644 WP 1999 5 14 AALA990329 1 19990311 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1894 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND GALLEY/LAVATORY SUPPORT AFT END STATION 1899 HAS CORROSION, STATION 36L. REMOVED CORRODED SUPPORT AND FABRI CATED NEW PART PER AARD 51-01-00-05 AND REINSTALLED. (M) 2 L 7 3 4F A22WE 1999051400645 19990514 00645 WP 1999 5 14 AALA990330 1 19990311 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1894 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - GALLEY/FLOORBOARD SUPPORT BETWEEN STATION 0 AND STATION 36L AT STATION 1890 HAS CORROSION IN SEVERAL PLACES. REMO VED CORRODED PARTS AND INSTALLED NEW FLOORBOARD SUPPORT PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1999051400646 19990514 00646 WP 1999 5 14 AALA990328 1 19990311 A 5312 BULKHEAD FITTING DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - BULKHEAD TEE FITTING STATION 2007 HAS NUMEROUS AREAS OF CORROSION FROM LONGERON 27L TO LONGERON 27R. REMOVED 2007 BULKHEAD TEE ANGLE AND INSTALLED SERVICEABLE TEE ANGLE PER AARD 51-01-00-05 PAGE 1. (M) 2 L 7 3 4F A22WE 1999051400647 19990514 00647 WP 1999 5 14 AALA990341 1 19990312 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1902-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - GALLEY SUPPORT FROM 2007 AND 1902 RIGHT SIDE HAS NUMEROUS AREAS OF CORROSION. REMOVED CORRODED PART AND FABRICATE D NEW PART AND REINSTALLED PER AARD 51-10-00-01. (M) 2 L 7 3 4F A22WE 1999051400648 19990514 00648 WP 1999 5 14 AALA990340 1 19990312 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 1959-1962 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON NR 8 SEAT TRACK STATION 1959 TO 1962. REMOVED CORRODED SEAT TRACK AND INSTALLED A NEW SECTION PER AARD 51-10-00-1 PAGE 1. (M) 2 L 7 3 4F A22WE 1999051400649 19990514 00649 WP 1999 5 14 AALA990339 1 19990312 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1962-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - GALLEY TIEDOWN/FITTINGS CORRODED FROM 2007 TO 1902, STATION 25R. REMOVED CORRODED SUPPORT AND FABRICATED NEW SUPP ORT AND REINSTALLED PER AARD 51-10-00-01. (M) 2 L 7 3 4F A22WE 1999051400650 19990514 00650 WP 1999 5 14 AALA990410 1 19990319 A 5320 WALL DOUG DC10 DC1030 3023501 WP BS 1510-1519 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON AFT OF OUTBOARD UPPER SLANT WALL OF RIGHT WHEEL WELL, APPROX 30 INCH FROM TOP OF WHEEL WELL. I NSTALL REPAIR DOUBLERS PER ESO 7349 AS A REVISION OF CUP 53-30-00 OF SRM, WORK REF E58-3. (M) 2 L 7 3 4F A22WE 1999051400651 19990514 00651 WP 1999 5 14 AALA990421 1 19990322 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 2000-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSIN ON NR 8 SEAT TRACK AT AFT ATTACH AREA STATION 2000-2007. REPAIRED NR 8 SEAT TRACK AT AFT ATTACH AR EA PER DC10 SRM CHAPTER 53-70-00 VOL 1 FIG 18 AND ESO 7349 DATED 19 MAR 99. (M) 2 L 7 3 4F A22WE 1999051400652 19990514 00652 EU 1999 5 14 AALA990460 1 19990330 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 27-30 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70072 515 FOUND CORROSION IN SEAT TRACK NR 10 FRME 27 TO FRAME 30 AND TIE DOWN FOR LAV 'M'. REMOVED AND REPLACED SECTION OF SEAT TRACK NR 10 PER SRM 51-72-10-0 FROM FRAME 26 TO 30. (M) 2 L 7 2 4F RT A35EU 1999051400653 19990514 00653 EU 1999 5 14 AALA990459 1 19990331 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1764-1817 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70072 515 TUL - NR 9 SEAT TRACK IN 'A' ZONE CABIN CORRODED. INSTALLED NEW SEAT TRACK NR 9 BETWEEN FRAME 26 - FRME 30. INSTALLED 1ST OVER SIZE .25 HLT 4268 AND 4266, SEALED TRACK WITH 870 SEALANT. REF SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999051400654 19990514 00654 EU 1999 5 14 AALA990458 1 19990401 A 5320 MOUNT AIRBUS 300 A300B4605R 3930308 EU LAVATORY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70072 515 TUL - FOUND OUTBOARD FORWARD MOUNT CORRODED LEV U. REPAIRED IN SHOP ON SHOP ORDER NR YFT4. (M) 2 L 7 2 4F RT A35EU 1999051400655 19990514 00655 EU 1999 5 14 AALA990446 1 19990330 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70072 515 TUL - FOUND CORROSION ON TOP OF FLOORBOARD SUPPORT AFT OF FRAME 74, BETWEEN FLOORBOARD SUPPORT 5A AND TRACK NR 6. REPLA CED FLOORBOARD SUPPORT ANGLE PER SRM 51-71-10. (M) 2 L 7 2 4F RT A35EU 1999051400656 19990514 00656 EU 1999 5 14 AALA990445 1 19990330 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAM 71-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70072 515 TUL - FOUND CORROSION ON TOP OF FLOORBOARD SUPPORT TRACK NR 6. REPLACED FLOORBOARD SUPPORT FRAME 71-74 PER SRM 51-71-10 . (M) 2 L 7 2 4F RT A35EU 1999051400657 19990514 00657 WP 1999 5 14 AALA990487 1 19990410 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 765 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION ON SKIN SPLICE DOUBLER. INSTALLED REPAIR DOUBLERS PER ESO 7349 DATED 08 APR 99. (M) 2 L 7 3 4F A22WE 1999051400658 19990514 00658 NM 1999 5 14 AALA990488 1 19990407 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 1967-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - UNDERSIDE OUTBOARD FLANGE HAS CORROSION AT FASTENERS OF FLOORBOARD SUPPORT. FIRST SUPPORT FROM RIGHT SIDE FUSELAG E, FROM STATION 1967-2007, VIEWED FROM BOTTOM WASTE TANK. REPLACED SUPPORT FIRST FROM RIGHT SIDE PER SRM 51-21-01 VOL I I. (M) 2 L 7 3 4F RT A22WE 1999051400659 19990514 00659 NM 1999 5 14 AALA990489 1 19990409 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1967 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - FOUND NR 8 SEAT TRACK CORRODED STATION 1967. REMOVED CORROSION FROM NR 8 TRACK PER SRM 53-70-00 VOL I AND 51-21-0 1 VOL II ACCOMPLISHED REPAIR PER ESO 41000 DATED 4-9-99. (M) 2 L 7 3 4F RT A22WE 1999051400660 19990514 00660 WP 1999 5 14 AALA990496 1 19990412 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP BS 1731 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION AROUND ANTENNA HOLE BETWEEN STRINGER 52 AND 51R. REMOVED CORROSION PER SRM 51-21-01 VOL II. INST ALLED NEW ANTENNA BAY PER AARD 51-01-00-5. (M) 2 L 7 3 4F A22WE 1999051400661 19990514 00661 WP 1999 5 14 AALA990497 1 19990407 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 FOUND STRINGER CORRODED HEAVILY ALONG RIGHT SIDE AND UNDERNEATH FLANGE AT STATION 879, STRINGER 52. CORROSION WAS REMOV ED IAW DC1010 MM SRM 52-21-01 VOL II. REPLACED CORROSION SECTION OF STRINGER 52 WITH NEW STRINGER SECTION AND SPLICE PE R AARD 51-01-00-05, ALODINED AND PAINTED SRM 51-21-01 VOL II. (M) 2 L 7 3 4F A22WE 1999051400662 19990514 00662 WP 1999 5 14 AALA990498 1 19990407 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND LONGERON 51L CORRODED INSIDE AT STATION 1100. REMOVED CORROSION IAW SRM 51-21-01 VOL II. REMOVED AND REPLA CED CORRODED, STRINGER 51L, SECTION WITH NEW SECTION PER AARD 51-01-00-05. ALODINED PRIMED AND PAINTED PER SRM 51-21-01 VOL II. REINSTALLED INTERCOSTAL AND STRINGER END CAP. (M) 2 L 7 3 4F A22WE 1999051400663 19990514 00663 WP 1999 5 14 AALA990499 1 19990412 A 5320 JAMB DOUG DC10 DC1010 3022110 WP BS 879-899 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FORWARD LOWER CORNER OF FORWARD CX DOOR JAMB CORRODED AT RADIUS BETWEEN STATION 879-899. BLENDED CORROSION IAW DC 1010 SRM 51-21-01/ESO 7349. (M) 2 L 7 3 4F A22WE 1999051400664 19990514 00664 WP 1999 5 14 AALA990500 1 19990407 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1741 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION ON BOTTOM OF LONGERON 49L AT STATION 1741. FABRICATE REPLACEMENT STRINGER AND AFT SPLICE INSTALLE D STRINGER SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1999051400665 19990514 00665 WP 1999 5 14 AALA990501 1 19990412 A 5743 TRUNNION DOUG DC10 DC1010 3022110 WP WS 231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND MLG AFT TRUNNION FORWARD FITTING INSIDE BORE CORRODED AND AFT FACE OF FITTING CORRODED. INSTALLED SERVICEAB LE BUSHING AND SPACER PER SRM 57-20-00. (M) 2 L 7 3 4F A22WE 1999051400666 19990514 00666 WP 1999 5 14 AALA990480 1 19990409 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION ON FUSE SKIN UNDER TEMPORARY SKIN DOUBLER IN AREA OF STATION 879 FROM STRINGER 43L TO 47L. REPAIR ED PER ESO 7349 DATED 04-08-99. (M) 2 L 7 3 4F A22WE 1999051400667 19990514 00667 WP 1999 5 14 AALA990295 1 19990226 A 5320 TRAP PANEL DOUG DC10 DC1010 3022110 WP BS 1401 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 116AA 46516 TUL - FOUND CORROSION INSIDE SIDE STRUT BLOCK ATTACHMENT HOLES. AREA LOCAL BLENDED AND TREATED PER AA ESO 7349 DAGED 2- 26-99. (M) 2 L 7 3 4F A22WE 1999051400668 19990514 00668 EU 1999 5 14 AALA990342 1 19990309 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 26-28 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 33069 512 TUL - FOUND CORROSION BETWEEN FRAME 26 AND FRAME 28. REPLACED NR 9 TRACK SECTION WITH NEW PER SRM 51-72-00. (M) 2 L 7 2 4F RT A35EU 1999051400669 19990514 00669 EU 1999 5 14 AALA990311 1 19990308 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU COCKPIT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 33069 512 TUL - FRAME 11 'Z' ANGLE CORRODED AT COCKPIT ENTRY. REMOVED AND REPLACED Z ANGLE AT FRAME 11 (SPLICED IN NEW PIECE AT M IDDLE OF Z ANGLE) PER SRM 51-71-40-2. (M) 2 L 7 2 4F RT A35EU 1999051400670 19990514 00670 EU 1999 5 14 AALA990327 1 19990311 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 28 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 33069 512 TUL - FOUND TRACK NR 8 AT FRAME 28 HAS CORROSION ON IT. INSTALLED TRACK PER SRM 51-72-10 AND ESO 30595, DATED 3/10/99. (M) 2 L 7 2 4F RT A35EU 1999051400671 19990514 00671 EU 1999 5 14 AALA990326 1 19990311 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 73-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 33069 512 TUL - LAV SUPPORT SEAT TRACK NR 1 AT FORWARD CORNER OF L-4 DOOR AFT OF FRAME HAS HEAVY CORROSION. INSTALLED NEW LAV SUP PORT SEAT TRACK NR 1 FORWARD FRAME 73 PER SRM 51-10-00. (M) 2 L 7 2 4F RT A35EU 1999051400672 19990514 00672 EU 1999 5 14 AALA990343 1 19990309 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 26-28 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 33069 512 TUL - FOUND CORROSION BETWEEN FRAME 26 AND FRAME 28. REPLACED NR 10 TRACK SECTION WITH NEW PER SRM 51-72-00. (M) 2 L 7 2 4F RT A35EU 1999051400673 19990514 00673 WP 1999 5 14 AALA990439 1 19990324 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 672 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - FOUND CORROSION ON SEAT TRACK NR 6 DEEP PITTING CENTER OF TRACK. REPLACED SECTION OF TRACK STATION 218-798 REFERE NCE SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1999051400674 19990514 00674 WP 1999 5 14 AALA990438 1 19990326 A 5320 993061291 BRACKET DOUG DC9 DC982 3022082 WP BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - FOUND AFT GIRT BAR MOUNT BRACKET HAS CORROSION BEYOND LIMITS ON TOP OF MOUNT, AFT SERVICE DOOR AREA. INSTALLED NE W GIRT BAR FITTING MOUNT BRACKET 51-10-3. (M) 2 L 7 2 4F A6WE 1999051400675 19990514 00675 WP 1999 5 14 AALA990437 1 19990326 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - FOUND CORROSION ALONG HORIZONTAL AND VERTICAL LEGS OF DOOR OPENING BEAM. INSTALLED FULL LENGTH DOUBLER PER AARD 5 3-10-00-3. (M) 2 L 7 2 4F A6WE 1999051400676 19990514 00676 WP 1999 5 14 AALA990436 1 19990326 A 5320 9936534177 CUSP DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - FOUND CORROSION ON CUSP BELOW G2 AFT INBOARD MONT PAD. CUT OUT DAMAGED AND INSTALLED DOUBLER REPAIR PER AARD 53-0 0-00-02. (M) 2 L 7 2 4F A6WE 1999051400677 19990514 00677 WP 1999 5 14 AALA990447 1 19990401 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 1307-1313 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - FOUND CRACK IN INTERNAL DOUBLER. INSTALLED INTERNAL DOUBLER FILLER AND SPLICE PER ESO 80559 DATED 3/26/99. (M) 2 L 7 2 4F A6WE 1999051400678 19990514 00678 WP 1999 5 14 AALA990448 1 19990331 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP BS 1309 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - OUTFLOW VALVE STIFFENER CASTING HAD CORROSION AND CRACK. REPLACED OUTFLOW VALVE STIFFENER PER SRM 51-10 AND 51-30 . (M) 2 L 7 2 4F A6WE 1999051400679 19990514 00679 WP 1999 5 14 AALA990423 1 19990324 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 380 ROUGH A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 493AA 49731 TUL - FOUND SKIN ROUGH UNDER ANTENNA. SMOOTH SKIN PER SRM 51-50-1, TREATED. (M) 2 L 7 2 4F A6WE 1999051400680 19990514 00680 NM 1999 5 14 AALA990442 1 19990326 A 5311 FRAME BOEING 727 727223 1384074 NM BS 312 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 TUL - FOUND OUTBOARD FLANGE CRACKED OF BELLFRAME STATION 312 AND STRINGER 13. INSTALLED DOUBLER PER SRM 51-40-3 USING . 071 MATERIAL AND .875 HI-LOCKS 3 ON TOP FLANGE AND 4 ON BOTTOM FLANGE AND 2 ROWS ON WEB TOTAL 26 FASTENERS. (M) 2 L 7 3 4F A3WE 1999051400681 19990514 00681 NM 1999 5 14 AALA990451 1 19990330 A 5320 STRAP BOEING 727 727227 1384078 NM BS 416 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND CRACK IN STRAP AT FORWARD DOOR LOWER AFT CORNER. STOP DRILLED AND INSTALLED DOUBLER PER BOEING S/B 727-53-1 88 FIG 3. (M) 2 L 7 3 4F A3WE 1999051400682 19990514 00682 NM 1999 5 14 AALA990450 1 19990329 A 5330 SKIN BOEING 727 727227 1384078 NM BS 742 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND CORROSION ON OUTERSKIN OF A/C AT HI-LOCK FS 742 STRINGER 9L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A, WITH NO CUTOUT PER AARD 53-30-03-3. (M) 2 L 7 3 4F A3WE 1999051400683 19990514 00683 NM 1999 5 14 P2EA99178 1 19990427 A 5330 SKIN BOEING 737 737222 1384473 NM BS 986.5-1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FUSELAGE SKIN BETWEEN BS 986.5 AND BS 1016, FROM STRINGER 10L, TO STRINGER 14L WAS FOUND WITH CORROSION. REPLACED FUSELAGE SKIN PANEL FROM BS 986.5 AND BS 1016 BETWEEN STRINGER 10L AND 14L DUE TO CORROSION PER COO PESA EO COO-3-53-243-99 DATED APR 16, 1999 AND BOEING FAX COO-SJO-99-0504RR DATED APRIL 16, 1999. (M) 2 L 7 2 4F A16WE 1999051400684 19990514 00684 NM 1999 5 14 P2EA99179 1 19990423 A 5330 SKIN BOEING 737 737222 1384473 NM BS 995-1010 MISREPAIRED A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK A REPAIR WAS FOUND NOT PER SRM ON THE FUSELAGE BETWEEN BS 995 AND BS 1010, STRINGER 14 RIGHT. REPA IRED FUSELAGE SKIN SECTION BETWEEN BS 993 AND BS 1013 FROM STRINGER 13 TO STRINGER 15 RIGHT SIDE PER SRM 53-30-3 FIGURE 16. (M) 2 L 7 2 4F A16WE 1999051400685 19990514 00685 NM 1999 5 14 P2EA99180 1 19990419 A 5330 SKIN BOEING 737 737222 1384473 NM BS 907-1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK AT THE FUSELAGE, BETWEEN BS 907 AND BS 1016, FROM STRINGER 14L TO 20L, SKIN PANEL WAS FOUND WITH CO RROSION OUT OF LIMITS. REPLACED FUSELAGE SKIN PANEL FROM BS 908 TO BS 1016, BETWEEN STRINGER 14 TO STRINGER 20 LEFT SID E DUE TO CORROSION PER COOPESA EO COO-3-53-247-99, DATED APR 21, 1999 AND BOEING FAX COO-SJO-99-0524RR, DATED APR 20, 19 99. (M) 2 L 7 2 4F A16WE 1999051400686 19990514 00686 NM 1999 5 14 TSAA9933223 1 19990419 A 3350 6013211 BATTERY BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT POWER SUPPLY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4U RT A16WE 1999051400687 19990514 00687 NM 1999 5 14 TSAA9933224 1 19990425 A 3350 8731002511 LIGHT BOEING 737 7372M6C 1384708 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED AFT SERVICE DOOR EMERGENCY SLIDE LIGHT ASSY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999051400688 19990514 00688 NM 1999 5 14 TSAA9933225 1 19990425 A 3350 9221009 LIGHT BOEING 737 737297 1384480 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED AFT SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999051400689 19990514 00689 NM 1999 5 14 TSAA9933226 1 19990425 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 1 AND NR 2, NR 3, NR 4, NR 5 AND POSITION EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999051400690 19990514 00690 NM 1999 5 14 TSAA9933222 1 19990419 A 3350 86210066 BATTERY BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 4 FLOOR EMERGENCY BATTERY PACK FOR HAVING LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1999051400691 19990514 00691 NM 1999 5 14 TWRA9916 1 19990416 A 3397 WIRE BOEING 747 747136 1384883 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 EGRESS LIGHTS 'A' ZONE LEFT SIDE BOTTOM OF CIRCULAR STAIRWAY AND STAIRWAY WALL DOES NOT ILLUMINATE. REPAIRED BROKEN WIR E AT LIGHT. (M) 2 L 7 4 4F A20WE 1999051400692 19990514 00692 EU 1999 5 14 REXA99005 1 19990228 A 5712 RIB SAAB SF340 SF340A 7850100 EU WS 42.3 CORRODED A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 347AM 340A039 FOUND CORROSION ON RIGHT INBOARD FUEL TANK. REPAIRED CORROSION ON SUMP BAY AREA BY BLENDING SMOOTH, ALODINING AND PRIMI NG. REPAIRED RIB STATION 42.30 FLANGE BETWEEN SL13 AND 14 BY BLENDING. REPAIRED FLANGE AT 42.30 BETWEEN 14 AND 15 BY C UTTING OUT DAMAGE. APPLIED DOUBLER ANGLE IAW SAAB DOC 72SDS1414. (M) 2 L 7 2 4T RT A52EU 1999051400693 19990514 00693 1999 5 14 MZZA99055 4 19990318 A 3425 WIRE BOEING 727 727212 138407G NM RT ADI LOOSE A MZZA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 86425 21459 FLT 992 - GUM - AIR RETURN DUE TO FIRSTI OFFICER ADI INOPERATIVE, DOES NOT RESPOND IN ROLL AND DOES NOT INDICATE A BANK. MAINTENANCE TROUBLESHOOT SYSTEM FOUND FAULTY WIRES. FOUND WIRES NR 27 AND NR 28 GROUNDING OUT AT VG CANNON PLUG. RES PLICED WIRES IAW WDM 34-22-03 PAGE 901. PERFORMED MANUAL VG 'ROLL', FO'S ADI CHECKS GOOD. AIRCRAFT BACK IN SERVICE. ( M) 2 L 7 3 4F A3WE 1999051400694 19990514 00694 EA 1999 5 14 MASA99063 1 19990426 A 3350 OL3071BPEFGPL BULBS CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27172 7172 FLT 5780 - CLT - CREW REPORTED THAT THE FIRST TWO EMERGENCY FLOOR PATH LIGHTS ON THE LEFT SIDE WERE INOPERATIVE. MAINTE NANCE REPLACED BOTH OF THE BULBS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999051400695 19990514 00695 EA 1999 5 14 MASA99062 1 19990421 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 FLT 5757 - SWF-RDU - AFTER ARRIVAL IN RDU, THE CREW REPORTED THAT THE AFT CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BULBS, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999051400696 19990514 00696 NM 1999 5 14 GAIA9952 1 19990419 A 3350 GE307 BULB BOEING 727 727223 1384074 NM PAX DOOR FAILED A GAIA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 6831 20184 DURING PILOT WALK AROUND THE FLIGHT CREW FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REP LACED ONE EACH FORWARD ENTRY AREA ' EMERGENCY EXIT' LIGHT BULB. OPERATIONAL CHECK CARRIED OUT WITH NO ADDITIONAL PROBLE M. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999051400697 19990514 00697 NM 1999 5 14 CALA9900460 1 19990430 A 5315 6545812 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 HOU - FLOORBEAM WEB CRACKED .35 INCH AT STATION 328 LBL 1. INSTALLED REPAIR PER EC/RA 5310-03847. (M) 2 L 7 2 4F RT A16WE 1999051400698 19990514 00698 WP 1999 5 14 CALA9900461 1 19990501 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN BROKEN A CALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 18513 48112 ATL - FLT 715 - EMERGENCY AISLE PATH LIGHTING STRIP IN FIRST CLASS BROKEN, WIRES EXPOSED. INSTALLED NEW SECTIO NOF TRAC K AND COVER. LIGHTING OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999051400699 19990514 00699 WP 1999 5 14 CALA9900462 1 19990428 A 7430 SWITCH DOUG DC9 DC932 3022066 WP COCKPIT FAILED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 18544 47219 IAH - FLT 612 - IMMEDIATELY AFTER TAKEOFF NOTICED ELECTRICAL SMELL IN COCKPIT. SMELL WENT AWAY IN A FEW MINUTES. DURIN G CLIMB-OUT NOTICED LEFT IGNITION C/B TRIPPED. RESET C/B PER QRH, WOULD NOT RESET. GOT A BEEP NOISE AND SPARKS CAME OU T OF OVERHEAD PANEL NEAR IGNITION SWITCH. REPLACED IGNITION SWITCH. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1999051400700 19990514 00700 WP 1999 5 14 CALA9900465 1 19990430 A 5530 591218836 ANGLE DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 HOU - RIGHT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999051400701 19990514 00701 WP 1999 5 14 CALA9900464 1 19990430 A 5530 591218835 ANGLE DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 HOU - LEFT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999051400702 19990514 00702 WP 1999 5 14 CALA9900466 1 19990430 A 5210 995575219N BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 HOU - MAIN CABIN DOOR NR 1 BEAM IS CRACKED AT BOTH ENDS .625 INCH FORWARD AND 1 INCH AFT. REMOVED AND REPLACED BEAM PER SRM 51-30-0. (M) 2 L 7 2 4F A6WE 1999051400703 19990514 00703 WP 1999 5 14 CALA9900467 1 19990430 A 5240 991158221 BEAM DOUG DC9 DC982 3022082 WP FWD SERV DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 HOU - FORWARD SERVICE DOOR NR 4 BEAM IS CRACKED AT FORWARD END 1.5 INCH. INSTALLED NEW BEAM PER SRM 51-30-2 AND 51-30-1 . (M) 2 L 7 2 4F A6WE 1999051400704 19990514 00704 NM 1999 5 14 ASAA9940097 1 19990421 A 5315 6545807 FLOORBEAM BOEING 737 737490 1384715 NM BS 294.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 SEA - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM, BS 294.5, RBL 18 TO 50 CORRODED ON UPPER CHORD. REPAIRED PER SRM 53- 10-51, FIG 205. (M) 2 L 7 2 4F RT A16WE 1999051400705 19990514 00705 NM 1999 5 14 ASAA9940098 1 19990421 A 5315 FLOORBEAM BOEING 737 737490 1384715 NM BS 360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 SEA - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM, BS 360, RLB 20.5 AND 25.5 CORRODED ON UPPER CHORD. REPAIRED PER SRM 53-00-51, FIG 201. (M) 2 L 7 2 4F RT A16WE 1999051400706 19990514 00706 NM 1999 5 14 ASAA9940099 1 19990421 A 5315 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 SEA - DURING SI CHECK, FOUND CORROSION AROUND SCREW HOLES ON MAIN CABIN FLOORBEAM T-CP AT STATION 986 AND LBL 17 THROUGH 33. REPAIRED PER SRM 53-60-51, FIG 203. (M) 2 L 7 2 4F RT A16WE 1999051400707 19990514 00707 WP 1999 5 14 ASAA9980078 1 19990407 A 5347 6019943 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1092-1183 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK FROM FS 1092 TO 1183. REMOVED DAMAGED TRACK AND INS TALLED NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M) 2 L 7 2 4F A6WE 1999051400708 19990514 00708 WP 1999 5 14 ASAA9980077 1 19990407 A 5320 5956034561 FITTING DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CRACK AND CORROSION ON LEFT FLOOR TRACK LOWER SUPPORT ANGLE FITTING BETWEEN LONGERONS 27L AND 28L AT FS 1287. REPLACED FITTING IAW DC9 SRM 51-30-00. (M) 2 L 7 2 4F A6WE 1999051400709 19990514 00709 WP 1999 5 14 ASAA9980076 1 19990407 A 5313 S1242886 LONGERON DOUG DC9 DC982 3022082 WP BS 1231-1251 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 1231 TO 1251. REMOVED DAMAGED AREA AND SPLICED IN NEW SE CTION IAW DC9 SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 1999051400710 19990514 00710 WP 1999 5 14 ASAA9980079 1 19990409 A 5240 MECHANISM DOUG DC9 DC982 3022082 WP R1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 OAK - DURING C-CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. RERIGGED THE R1 DOOR IAW DC9 MM AND OPERATED NORMALLY. ( M) 2 L 7 2 4F A6WE 1999051400711 19990514 00711 WP 1999 5 14 ASAA9980085 1 19990418 A 5610 WINDOW DOUG DC9 DC983 3022083 WP RT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 969AS 53063 SEA - AFTER ARRIVAL OF FLIGHT 472, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED U PPER LOCK BAR LINKAGE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999051400712 19990514 00712 1999 5 14 ASAA9980075 4 19990407 A 2565 D37013103 BOTTLE DOUG DC9 DC982 3022082 WP TAILCONE EXIT LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 6810 49387 PDX - DURING MAINTENANCE CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. R EPLACED THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1999051400713 19990514 00713 NM 1999 5 14 ASAA9940090 1 19990415 A 5220 65C807351 BEAM BOEING 737 737490 1384715 NM BS 947.5-967.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 767AS 27081 SEA - DURING SI CHECK, FOUND THE R-2 DOOR CREASE BEAM CORRODED FROM STATION 947.5 TO 967.5, RBL 62. REPLACED BEAM PER S RM 51-10-02 AND 53-60-15. (M) 2 L 7 2 4F RT A16WE 1999051400714 19990514 00714 NM 1999 5 14 ASAA9940091 1 19990416 A 5210 GUIDE ARM BOEING 737 7374Q8 NM L-1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 776AS 25109 PDX - FLT 343 - L-1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999051400715 19990514 00715 NM 1999 5 14 ASAA9940092 1 19990417 A 5240 MECHANISM BOEING 737 7374Q8 NM L-2 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 785AS 27628 ANC - FLT 88 - L-2 DOOR DIFFICULT TO OPEN AND CLOSE, MAKES METAL GRINDING NOISE. LUBED DOOR ARMS AND ROLLER TRACKS, AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999051400716 19990514 00716 WP 1999 5 14 ASAA9980080 1 19990410 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 962AS 53076 SAN - PRIOR TO DEPARTURE OF FLIGHT 463, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERTED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999051400717 19990514 00717 NM 1999 5 14 ASAA9940089 1 19990412 A 3350 1060091102 LIGHT GRIMES BOEING 737 7374Q8 NM R-2 DOOR BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING MAINTENANCE CHECK, THE R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND BROKEN. REPLACED R-2 DOOR EXIT IDE NTIFIER LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999051400718 19990514 00718 NM 1999 5 14 ASAA9940088 1 19990411 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 PDX - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS/ WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999051400719 19990514 00719 NM 1999 5 14 ASAA9940087 1 19990409 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 PDX - DURING MAINTENANCE CHECK, THE FORWARD 3 AND AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECON NECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999051400720 19990514 00720 NM 1999 5 14 ASAA9910078 1 19990411 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPL ACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999051400721 19990514 00721 NM 1999 5 14 ASAA9910077 1 19990408 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, THE FORWARD AND AFT CABIN EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REP LACED FORWARD AND AFT BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999051400722 19990514 00722 1999 5 14 RAIA990445 4 19990428 A 3425 501156616 ADI JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 570HK 5769 41089 FLT 7784 - DCA - STANDBY ATTITUDE INDICATOR WILL NOT STAY ERECT. MAINTENANCE REPLACED STANDBY ATTITUDE INDICATOR. (M) 2 L 7 2 4T RT A41NM 1999051400723 19990514 00723 EU 1999 5 14 RAIA990444 1 19990427 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU LEFT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 430AM 880 FLT 7301 - DEC - LEFT ENGINE FIRE LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT ENGINE FIRE LOOP. (M) 2 L 7 2 4T RT A56EU 1999051400724 19990514 00724 1999 5 14 RAIA990443 4 19990425 A 3418 103650004 STICK PUSHER JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 551HK 41040 FLT 7546 - STL - STICK PUSHER TEST FAILED. MAINTENANCE REPLACED STICK PUSHER. (M) 2 L 7 2 4T RT A41NM 1999051400725 19990514 00725 1999 5 14 RAIA990442 4 19990415 A 2350 ACP2531 AUDIO PANEL AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 426TE 15345 228 FLT 7156 - STL - NR 1 COMM TRANSMITTS CONTINUOUSLY. MAINTENANCE REPLACED AUDIO PANEL IN THE ACM POSITION. (M) 2 H 7 2 4T RT A53EU 1999051400726 19990514 00726 EU 1999 5 14 RAIA990441 1 19990426 A 6123 300480000006 AUTO FEATHER AEROSP ATR72 ATR72202 8680940 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 723TE 14336 283 FLT 7011 - STL - NR 1 EEC KEEPS FAULTING. MAINTENANCE REPLACED LEFT AUTO FEATHER UNIT. (M) 2 H 7 2 4T RT A53EU 1999051400727 19990514 00727 NE 1999 5 14 RAIA990440 2 19990425 A 7321 8058131005 EEC AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 723TE 3936 283 124437 FLT 7326 - STL - LEFT TORQUE GAUGE STICKS AT 90 PERCENT. MAINTENANCE REPLACED LEFT EEC. (M) 2 H 7 2 4T 4 T RT A53EU E2ONE 1999051400728 19990514 00728 NM 1999 5 14 SWAA990761 1 19990426 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND 3 EA CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 6.7 - RBL 6.7. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999051400729 19990514 00729 NM 1999 5 14 SWAA990762 1 19990426 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 EMERGENCY EXIT SIGN LENS BROKEN AT FWD SERVICE DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999051400730 19990514 00730 NM 1999 5 14 SWAA990763 1 19990426 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 524 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 524, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999051400731 19990514 00731 NM 1999 5 14 SWAA990764 1 19990427 A 5511 6552298 SPAR WEB BOEING 737 7372H4 138448C NM LT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C4 CHECK, FOUND A 1.125 INCH LONG CRACK AT LH HORIZONTAL STABILIZER CENTER SECTION AFT SPAR WEB, APPROX BL 10.878. REPAIRED SPAR WEB PER SWA RA NR 1-255-0292. 2 L 7 2 4F A16WE 1999051400732 19990514 00732 NM 1999 5 14 SWAA990766 1 19990427 A 2761 6549580 ACTUATOR BOEING 737 7372H4 138448C NM RT SPOILER LEAKING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 AIR TURNBACK, MASTER CAUTION HYDRAULIC, AND BOTH ENGINE DRIVEN PUMPS LOW PRESSURE LIGHTS CAME ON AT ROTATION. BRAKE ENE RGY APPROX 18 FOOT POUNDS AFTER LANDING. FOUND NR 6 FLIGHT SPOILER ACTUATOR LEAKING (BLOWN SEAL). REMOVED AND REPLACED ACTUATOR PER MM. 2 L 7 2 4F A16WE 1999051400733 19990514 00733 NM 1999 5 14 SWAA990767 1 19990427 A 2133 6552290 OUTFLOW VALVE BOEING 737 7373H4 1384600 NM CABIN OBSTRUCTION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 AIR TURNBACK, DURING TAKEOFF, PRESSURIZATION AUTO FAIL LIGHT CAME ON, NO PRESSURIZATION CAPABILITY AT ALL. DISCOVERED A PLASTIC TUBING DEBRIS OBSTRUCTING THE OUTFLOW VALVE TRAVEL. REMOVED OBSTRUCTION, PRESSURIZED AIRCRAFT, OPS CHECKED GOO D PER MM. 2 L 7 2 4F RT A16WE 1999051400734 19990514 00734 NM 1999 5 14 SWAA990753 1 19990426 A 3350 D31354 LENS BOEING 737 7373H4 1384600 NM LT PAX DOOR MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 337SW 23959 PLASTIC COVER LENS MISSING FOR LH AFT ESCAPE SLIDE ASSY. REMOVED AND REPLACED PLASTIC LENS PER MM. 2 L 7 2 4F RT A16WE 1999051400735 19990514 00735 NM 1999 5 14 SWAA990754 1 19990426 A 3350 1146801 BULB BOEING 737 7373H4 1384600 NM RT SERVICE DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND RH AFT SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999051400736 19990514 00736 NM 1999 5 14 SWAA990755 1 19990426 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EMERGENCY ESCAPE FLOOR TRACK LIGHT, FWD COVER MISSING. REPLACED COVER, ALSO FOUND WIRES DISCONNECTED. RECONNECTED WIRE S PER MM. 2 L 7 2 4F RT A16WE 1999051400737 19990514 00737 NM 1999 5 14 SWAA990756 1 19990426 A 3350 BR2013 SOCKET BOEING 737 7373H4 1384600 NM CABIN SHORTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED A1 CHECK, FOUND CENTER SECTION OF FLOOR TRACK LIGHTS INOP. FOUND SHORTED SOCKET. REMOVED AND REPLACED TRACK ASSY PER MM. 2 L 7 2 4F RT A16WE 1999051400738 19990514 00738 NM 1999 5 14 SWAA990757 1 19990426 A 5330 SKIN BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND CUT OUT FOR LH NOSE WHEEL WELL ACCESS PANEL CRACKED AT INBD CORNER. REPAIRED SKIN PE R SWA RA NR 1-353-2068. 2 L 7 2 4F RT A16WE 1999051400739 19990514 00739 NM 1999 5 14 SWAA990758 1 19990426 A 5240 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT NR 3 AND NR 4 STOP CUT-OUTS. REPAIRED FRAME PE R SRM. 2 L 7 2 4F RT A16WE 1999051400740 19990514 00740 NM 1999 5 14 SWAA990759 1 19990426 A 5240 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT LOWER CORNER OF FRAME CRACKED. REPAIRED FRAME PER MM. 2 L 7 2 4F RT A16WE 1999051400741 19990514 00741 NM 1999 5 14 SWAA990760 1 19990426 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND 4 EA CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 10 - RBL 13. REPAIRED CRACKS PER SRM. 2 L 7 2 4F RT A16WE 1999051400742 19990514 00742 NM 1999 5 14 SWAA990768 1 19990427 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388SW 26591 EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT MID CABIN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999051400743 19990514 00743 NM 1999 5 14 SWAA990769 1 19990427 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED AT BS 500A, STRINGER 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999051400744 19990514 00744 NM 1999 5 14 SWAA990770 1 19990428 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 717 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM LOWER SKIN CUT OUT AT BS 717 CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999051400745 19990514 00745 NM 1999 5 14 SWAA990771 1 19990428 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 312,LBL 14 - RBL 14, INSIDE CABIN. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999051400746 19990514 00746 NM 1999 5 14 SWAA990772 1 19990428 A 5230 6924284 BUNGEE CORD BOEING 737 7375H4 138449D NM CARGO DOOR OUT OF POSITION A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 523SW 26565 ABORTED TAKEOFF BELOW 80 KNOTS BECAUSE OF FWD CARGO LIGHT ON COCKPIT. FOUND BUNGEE CORD TOUCHING CARGO DOOR PROX SWITCH . REPOSITIONED CORD PER MM. 2 L 7 2 4F RT A16WE 1999051400747 19990514 00747 NM 1999 5 14 SWAA990773 1 19990428 A 3150 6545756 TO WARNING BOEING 737 7373H4 1384600 NM COCKPIT. ACTIVATED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 357SW 26594 ABORTED TAKEOFF WHEN MASTER CAUTION, AND ENG ANNUNCIATOR LIGHTS STAYED OUT ON RECALL FOR TAKEOFF, TAKE OFF WARNING HORN SOUNDED. PERFORMED TAKEOFF WARNING CHECK PER MM OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999051400748 19990514 00748 NM 1999 5 14 SWAA990774 1 19990429 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FRAME AT BS 986 , WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999051400749 19990514 00749 NM 1999 5 14 SWAA990775 1 19990429 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FRAME AT BS 328 , WL 184. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999051400750 19990514 00750 NM 1999 5 14 SWAA990776 1 19990429 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR RED LIGHTS INOP AT OVERWING EXIT. INSTALLED NEW SOCKET PER MM. 2 L 7 2 4F RT A16WE 1999051400751 19990514 00751 NM 1999 5 14 SWAA990777 1 19990429 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN HAS A 2.5 INCH LONG CRACK AT BS 727B, STRINGER 26L. REPAIRED SKIN PER SRM . 2 L 7 2 4F A16WE 1999051400752 19990514 00752 NM 1999 5 14 SWAA990778 1 19990429 A 3350 90052 POWER SUPPLY BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT CONTROL BREAKER POPPED ON ENGINE RUN. REMOVED AND REPLACED BATT ERY POWER SUPPLY PER MM. 2 L 7 2 4F A16WE 1999051400753 19990514 00753 NM 1999 5 14 SWAA990779 1 19990429 A 3350 100031 LIGHT BOEING 737 737301 1384611 NM ROW 23 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 660SW 23230 EMERGENCY OVERHEAD EXIT LIGHT AT ROW 23 CAME LOOSE. RESECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999051400754 19990514 00754 NM 1999 5 14 SWAA990744 1 19990425 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EMERGENCY ESCAPE TRACK LIGHT LOOSE IN AFT CABIN. SECURED TRACK LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999051400755 19990514 00755 NM 1999 5 14 SWAA990745 1 19990424 A 3350 101073 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY P ER MM. 2 L 7 2 4F A16WE 1999051400756 19990514 00756 NM 1999 5 14 SWAA990746 1 19990423 A 3350 101076 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 623SW 27933 DURING SCHEDULED C1 CHECK, FOUND FWD CABIN CEILING EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 1999051400757 19990514 00757 NM 1999 5 14 SWAA990747 1 19990423 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178. CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND 9 EA CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 17.5-RBL 17.5. REPAIRED BULKHEAD PER SWA RA NR 1-353-2067. 2 L 7 2 4F RT A16WE 1999051400758 19990514 00758 NM 1999 5 14 SWAA990748 1 19990423 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAMS, BS 772, RBL 3, AND BS 857, LBL 12, AFT CARGO BIN. REPAIRED BEAMS PER SRM AND SWA RA NR 1-A53-2021. 2 L 7 2 4F RT A16WE 1999051400759 19990514 00759 NM 1999 5 14 SWAA990749 1 19990423 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM, BS 772, LBL 17. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999051400760 19990514 00760 NM 1999 5 14 SWAA990750 1 19990424 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY GIRT BAR ATTACH BRACKET CORRODED AT FLOOR. REMOVED AND REPLACED BRACKET PE R MM. 2 L 7 2 4F RT A16WE 1999051400761 19990514 00761 NM 1999 5 14 SWAA990751 1 19990424 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 294.5, LBL 14-RBL 11. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999051400762 19990514 00762 NM 1999 5 14 SWAA990752 1 19990424 A 5320 BAC1508 T CAP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND UPPER T CAP CRACKED AT BS 663, BL 0. REPAIRED T CAP PER ACO NR 658-57. 2 L 7 2 4F RT A16WE 1999051400763 19990514 00763 NM 1999 5 14 SWAA990742 1 19990423 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 22 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EMERGENCY ESCAPE TRACK LIGHTING LOOSE AT ROW 22. SECURED TRACK LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999051400764 19990514 00764 NM 1999 5 14 SWAA990743 1 19990423 A 3350 P2070001 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 618WN 28034 AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASH LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999051400765 19990514 00765 WP 1999 5 14 TWAA9906301 1 19990430 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 15-20 LOOSE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9622A 53593 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 15 TO 20, AND 24 TO 26. RECONNECTED LOOSE WIRING AT BOTH LOCATIO NS. 2 L 7 2 4F RT A6WE 1999051400766 19990514 00766 WP 1999 5 14 TWAA9906302 1 19990428 A 5751 RIB DOUG DC9 DC931 3022065 WP RT AILERON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND RT AILERON RIB WITH DENT AND .25 INCH IN LONG CRACK, APPROX 10 IN FROM OTBD END AND 5 IN FROM LE. ACCOMPLISHED HFEC TO LOCATE ENDS OF CRACK. REPAIRED PER SRM 53-01, PAGE 10 FIG 2 SHEET 4. 2 L 7 2 4F A6WE 1999051400767 19990514 00767 WP 1999 5 14 TWAA9906303 1 19990426 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CORROSION IN SKIN AT STA 965, LONGERON 22L, LOWER AFT CABIN AIR OUTFLOW VALVE NOZZLE. R EMOVED OLD CORRODED PART, INSTALLED NEW INTERNAL DOUBLER. CUTOUT DAMAGED EXTERNAL SKIN AND INSTALLED FILLER AND DOUBLER PER ARA 13509 AND SRM 53-04. 2 L 7 2 4F A6WE 1999051400768 19990514 00768 WP 1999 5 14 TWAA9906304 1 19990426 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND A FIELD REPAIR ON THE FUSELAGE SKIN AT FWD CARGO OPENING, FWD CORNER OF REPAIR NOT ACCEP TABLE. REMOVED OLD REPAIR AND INSTALLED RECOMMENDED REPAIR PER SRM 53-05, FIG 1 AND ARA 13508. 2 L 7 2 4F A6WE 1999051400769 19990514 00769 WP 1999 5 14 TWAA9906305 1 19990427 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 200-237 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED ON BOTH SIDES OF FLOOR TRACK AT STA 200, RBL 44 IN. MEMBRA NE WAS REPAIRED PER SRM 53-01, FIG 4 SHEET 3, FROM STA 200 TO 237. 2 L 7 2 4F A6WE 1999051400770 19990514 00770 WP 1999 5 14 TWAA9906306 1 19990427 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 980 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT FLOOR SUPPORT INTERCOSTAL CORRODED APPROX STRINGER 27L, STA 980. REPLAC ED INTERCOSTAL FROM STA 980 TO 996 PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999051400771 19990514 00771 WP 1999 5 14 TWAA9906307 1 19990402 A 5530 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT, FOUND INSIDE ANGLE AT STA 1421 WAS CRACKED ON RT SIDE. INSTALLED NEW ANGLE AT STA 1421, PER SRM 5 1-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1999051400772 19990514 00772 WP 1999 5 14 TWAA9906308 1 19990404 A 5520 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT, FOUND INSIDE ANGLE AT STA 1421, LT SIDE, WAS CRACKED. INSTALLED NEW ANGLE PER SRM 51-30-2 AND 51- 30-5. 2 L 7 2 4F A6WE 1999051400773 19990514 00773 WP 1999 5 14 TWAA9906309 1 19990404 A 5530 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT, FOUND .1875 IN CRACK AT THE LT DORSAL FIN ATTACH ANGLE AT STA 1421. INSTALLED NEW ATTACH ANGLE PE R SERVICE BULLETIN 53-223 AND SR09530162. 2 L 7 2 4F A6WE 1999051400774 19990514 00774 WP 1999 5 14 TWAA9906310 1 19990405 A 5530 ANGLE DOUG DC9 DC982 3022082 WP BS 1421 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 953U 49267 DURING CHECK-C MAINT, FOUND A .1875 IN CRACK AT THE RT FWD DORSAL FIN ATTACH ANGLE AT STA 1421. REMOVED AND REPLACED AT TACH ANGLE PER SERVICE BULLETIN 53-223 PER MD9-AD-13. 2 L 7 2 4F A6WE 1999051400775 19990514 00775 WP 1999 5 14 TWAA9906311 1 19990415 A 5312 BULKHEAD DOUG DC9 DC983 3022083 WP AFT PRESS BLKHD DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 FOUND A 7 INCH SLICE AFT OF PRESSURE BULKHEAD IN FUSELAGE SKIN AT LONGERON 9R. SECTION OF LONGERON SPLICED AND DOUBLER INSTALLED PER ARA 16004, AND SRM 63-03, FIG 6, AND SRM 53-01, FIG 4. CHECK-C 10-3-98 MCI. 2 L 7 2 4F RT A6WE 1999051400776 19990514 00776 WP 1999 5 14 AT9900339 1 19990223 A 5311 99196181N FRAME DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, A CRACK ABOVE A REPAIR DOUBLER WAS FOUND IN THE LEFT WHEEL WELL OUTBOARD SIDE STR AP PANEL AT THE BS 718 FRAME. REMOVED AND REPLACED THE FRAME AT BS 718 IAW DC9 SRM 51-30-2, 51-10-0, 51-10-2, 51-10-5, 51-20-0, 51-30-5, AND SB 53-131 REV 4, DATED 11/93. 2 L 7 2 4F A6WE 1999051400777 19990514 00777 WP 1999 5 14 AT9900340 1 19990223 A 5711 SPAR WEB DOUG DC9 DC932 3022066 WP WS 58 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, DURING ACCOMPLISHMENT OF SB 57-200, FOUND A CRACK AT THE LOWER EDGE SPAR WEB OUTB OARD OF XCW 58 FITTING. REPAIRED AFT SPAR WEB LEFT SIDE AT XCW 58, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SB 57-200 AND DRAWING NR 5935248. 2 L 7 2 4F A6WE 1999051400778 19990514 00778 WP 1999 5 14 AT9900341 1 19990219 A 5320 RETAINER DOUG DC9 DC932 3022066 WP BS 218-332 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THREE RETAINER RINGS CARGO TIE DOWN IN FORWARD PIT LEFT SIDE AT BS 218-332 CORRODED. REMOVED CORROSION, FABRICATED REPAIR RETAINER, TREATED, AND PRIMED IAW DC9 SRM 53-01 FIG 1, 51-10-2, AND 51-1 0-4. 2 L 7 2 4F A6WE 1999051400779 19990514 00779 WP 1999 5 14 AT9900342 1 19990221 A 5347 2195051 TIE DOWN DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE G-2 GALLEY FLOOR MOUNTED TIE DOWNS AT BS 980 CORRODED. REMOVED AND REP LACED THE G-2 GALLEY FLOOR MOUNTS TIE DOWNS (4 EA) IAW DC9 MM 25-32-0. 2 L 7 2 4F A6WE 1999051400780 19990514 00780 WP 1999 5 14 AT9900343 1 19990221 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 775 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT CARGO COMPARTMENT FLOOR SUPPORT ON AFT SIDE OF FRAME AT BS 775 BETW EEN L27-28R CRACKED. REMOVED FLOOR SUPPORT, WELDED REPAIR BY USING AMS 4951 FILLER WIRE AND REINSTALLED SUPPORT IAW DC9 SRM 51-30-2, 51-30-5, AND EA 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999051400781 19990514 00781 WP 1999 5 14 AT9900344 1 19990218 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 296 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, NOTED ON EXTERIOR OF SKIN AND FASTENERS AT BS 296 FORWARD OF EXISTING REPAIR CORR ODED. DRILLED OUT FASTENERS AND REMOVED EXISTING REPAIR. CUT OUT SECTION OF SKIN AND REMOVED SHEAR TIE, FABRICATED REP AIR FILLER AND FINGER DOUBLER. DRILLED, TRIMMED, DEBURRED, AND REINSTALLED SHEAR TIE AND REPAIR IAW DC9 SRM 51-30-2, 51 -10-4, 53-04 FIG.35 PG 189, AND 51-10-3. 2 L 7 2 4F A6WE 1999051400782 19990514 00782 WP 1999 5 14 AT9900345 1 19990427 A 5320 1A444641 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE CABIN FLOOR SUPPORT AT BS 200 BL 0-20R CORRODED. REMOVED FLOOR SUPPORT , REPLACED WITH A FABRICATED SUPPORT IAW DC9 SRM 51-10-3, 53-01 FIG.1, 53-11-1, AND 51-10-4. 2 L 7 2 4F A6WE 1999051400783 19990514 00783 WP 1999 5 14 AT9900346 1 19990218 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 218-294 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THREE ACCESS PANEL STRAPS IN THE FORWARD PIT AT BS 218-294 CORRODED. REPLA CED STRAPS, FABRICATED, DRILLED, DEBURRED, TRIMMED TO FIT, INSTALLED CAMLOCKS, ALODINED, AND PRIMED IAW DC9 SRM 51-10-3, 51-10-4, 51-10-2, 51-30-0, AND MM 20-15-0. 2 L 7 2 4F A6WE 1999051400784 19990514 00784 WP 1999 5 14 AT9900347 1 19990219 A 5320 3955999501 BRACKET DOUG DC9 DC932 3022066 WP BS 69 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND PULLEYS AND ATTACH BRACKET ON THE NOSE LANDING GEAR WHEEL WELL AT BS 69 LBL 28 CORRODED. REMOVED AND REPLACED BRACKET FOR GROUND SENSE ASSEMBLY WITH NEW HARDWARE AND TWO PULLEYS IAW DC9 20-16-0. RIGGED AND OPS CHECKED NOSE LANDING GEAR STEERING CONTROL SYSTEM IAW DC9 MM 32-50-0, AND 32-51-0. 2 L 7 2 4F A6WE 1999051400785 19990514 00785 WP 1999 5 14 AT9900348 1 19990223 A 5320 39559971 BRACKET DOUG DC9 DC932 3022066 WP BS 110 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE BRACKET AND PULLEYS BEARING ON THE NOSE LANDING GEAR WHEEL WELL AT BS 110 LBL17 CORRODED. REMOVED AND REPLACED FORWARD BRACKET AND PULLEYS, RIGGED AND OPS CHECKED GOOD IAW DC9 MM 20-16-0, A ND 32-23-1. 2 L 7 2 4F A6WE 1999051400786 19990514 00786 SO 1999 5 14 COMA9910068 1 19990430 A 2750 WARNING EMB 120 EMB120RT SO TE FLAPS ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 152CA 120152 FLAP CONTROL FAULT WARNING. COULD NOT DUPLICATE, NO DEFECTS FOUND. 2 L 7 2 4T RT A31SO 1999051400787 19990514 00787 SO 1999 5 14 COMA9910069 1 19990502 A 3260 922AA2YA66Z72 SENSOR EMB 120 EMB120RT SO NLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 257CA 120248 WHEN LANDING GEAR SELECTED UP, THE NLG INTRANSIT LIGHT REMAINED ON. REPLACED THE NLG UPLOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1999051400788 19990514 00788 EA 1999 5 14 COMA9960178 1 19990501 A 2750 7805013 LEVER CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA K NONE O OTHER AP APPROACH 1 SO 01 712CA 2172 7244 FLAPS FAIL MESSAGE. REPLACED FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 1999051400789 19990514 00789 NM 1999 5 14 UPS99229477 1 19990430 A 5270 SWITCH BOEING 727 72730C 1384009 NM CARGO DOOR OUT OF ADJUST A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 919UP 19012 CARGO DOOR ANNUNCIATOR ILLUMINATED INLIGHT. AIRCRAFT PRESSURIZATION NORMAL. ATB 0245Z DOOR WARNING SYSTEM DEFERRED . CONTROL NR M171685, MEL 5-2-4. DOOR VISUALLY CHECKED BY RFD MX. AT SDF, ADJUSTED FWD CARGO DOOR SWITCH PER M/M 52-7 0-01. OPS CHECK NORMAL. DEFFERAL CLOSED. 2 L 7 3 4F A3WE 1999051400790 19990514 00790 NM 1999 5 14 UPS99629475 1 19990501 A 3240 BRAKE BOEING 767 76734AF 1385212 NM MLG DAMAGED A IPXA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 SO 01 317UP 27745 UPON INSPECTION BY MECHANIC AFTER ARRIVAL INTO SJU, FOUND EVIDENCE OF A MINOR FIRE ON THE NR 6 BRAKE. BRAKE TEMP ONLY R OSE TO 6. PER MM CHAP 05, NO HEAT DAMAGE INSPECTED WAS REQUIRED. VISUALLY INSPECTED BRAKE AND SURROUND AREA FOR DAMAG E, NONE FOUND. EVIDENCE OF CLEANING FLUID, BELIEVE THIS WAS THE CAUSE OF THE MINOR FIRE. DE-ACTIVATED NR 6 BRAKE PER M EL 32-41-1-1 FOR REMOVED AND REPLACED AT A LATER DATE. SEE AMB 06-32-99-013 FOR DESCRIPTION OF RELATED PROBLEMS WITH BR AKE FIRES. 2 L 7 2 4F RT A1NM 1999051400791 19990514 00791 NM 1999 5 14 UPS99629479 1 19990501 A 3350 BULB BOEING 767 76734AF 1385212 NM CREW DOOR FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 326UP 27752 EXTERIOR EMERGENCY ESCAPE LIGHT BELOW CREW ENTRY DOOR INOP. RELAMPED EXTERIOR ESCAPE LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1999051400792 19990514 00792 WP 1999 5 14 UPS99829466 1 19990406 A 5320 57500201 STRAP DOUG DC8 DC873F 302199F WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 902 FRAME STRAP AT LONGERON 18L HAS HEAVY CORROSION. REMOVED, FABRIACTED, AND INSTALLED STRAP IAW DWG 5750020 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999051400793 19990514 00793 WP 1999 5 14 UPS99829467 1 19990405 A 5347 4929127 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, RBL 48 AT FS 1220 IS CRACKED AND CORRODED. CUT OUT SEAT TRACK, FS 1170 TO 127 0, FABRICATED AND SPLICED IN A NEW SECTION IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999051400794 19990514 00794 WP 1999 5 14 UPS99829468 1 19990405 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 675-683 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK IS CORRODED AT FS 675 TO 683, RBL 48. REMOVED DAMAGED SEAT TRACK, FS 480 TO 72 7, INSTALLED NEW SECTION IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999051400795 19990514 00795 WP 1999 5 14 UPS99829469 1 19990422 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 347.75-370 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LT WING UPPER L/E SKIN AT XFS 347.75 TO 370 IS CORRODED BEYOND LIMITS, AT THE T/E. CUT OUT DAMAGED A REA AND REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1999051400796 19990514 00796 WP 1999 5 14 UPS99829470 1 19990426 A 5320 57503227 DOUBLER DOUG DC8 DC873F 302199F WP BS 1350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FINGER DOUBLER, FS 1350, LONGERON 35L TO 35R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INS TALLED FINGER DOUBLER IAW DWG 5750322 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999051400797 19990514 00797 WP 1999 5 14 UPS99829471 1 19990418 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 761.695 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XW 761.695 IS CRACKED AT 1 SCREW HOLE. REPAIRED SKIN IAW EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 1999051400798 19990514 00798 WP 1999 5 14 UPS99829472 1 19990426 A 5320 9755821507 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 1360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 SHEAR TIE AT FS 1360, BETWEEN LONGERON 31R AND 33R IS CRACKED. REMOVED, FABRICATED, AND INSTALLED SH EAR TIE IAW DWG 9755821-507 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999051400799 19990514 00799 WP 1999 5 14 UPS99829473 1 19990418 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 708 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 RT WING L/E, LWR SKIN AT XFS 708 IS CORRODED OUT OF LIMITS AT 1 EA SCREW HOLE. REPAIRED SKIN IAW EO DC8-5720-7787. 2 L 7 4 4F RT 4A25 1999051400800 19990514 00800 WP 1999 5 14 UPS99829474 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 691.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 RT WING L/E RIB AT XFS 691.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED RIB I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999051400801 19990514 00801 WP 1999 5 14 UPS99829476 1 19990430 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 EMERGENCY EXIT LIGHTS INOPERATIVE ON BATTERY POWER. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK. OPS CHECK GOOD P/N ON 60-1223-5, S/N 356, P/N OFF 5708458-503, S/N 488. 2 L 7 4 4F RT 4A25 1999051400802 19990514 00802 EU 1999 5 14 QXEA9900880 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME CONNECTION ANGLE IS CRACKED AT FRAME 17565 AND STRINGER 51. REPAIRED IAW FOKKER SRM 51-31-1 AND F-28 MM 53- 10-5, PAGE 601A, PARAGRAPH 2B3. 2 L 7 2 4F RT A20EU 1999051400803 19990514 00803 EU 1999 5 14 QXEA9900881 1 19990324 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU RT CONSOLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - HORIZONTAL BEAM 1 HAS APPROXIMATELY A 2 CRACK IN RADIUS OF BULKHEAD WEB TO BEAM ATTACH FLANGE ANGLE, UNDER BOTH UP PER AND LOWER RIGHT-HAND CONSOLE FITTINGS. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 13. 2 L 7 2 4F RT A20EU 1999051400804 19990514 00804 EU 1999 5 14 QXEA9900882 1 19990331 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 58-50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 58-5-2 HAS A CRACK IN CONNECTION ANGLE AT STRINGER 36. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400805 19990514 00805 EU 1999 5 14 QXEA9900883 1 19990329 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 54-5-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 54-5-2 HAS A CRACK IN CONNECTION ANGLE AT STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND F-28 MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999051400806 19990514 00806 EU 1999 5 14 QXEA9900884 1 19990327 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 50-2 HAS A CRACK IN CONNECTION ANGLE AT STRINGER 21A. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601, PARAGRAPH 1 AND 2. 2 L 7 2 4F RT A20EU 1999051400807 19990514 00807 EU 1999 5 14 QXEA9900885 1 19990402 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 22293 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 22293 IS CRACKED BETWEEN STRINGER 21 AND 21A. REPAIRED IAW HORIZON AIR EA 4-53-740. 2 L 7 2 4F RT A20EU 1999051400808 19990514 00808 EU 1999 5 14 QXEA9900886 1 19990330 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD DEBONDED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - HORIZONTAL STIFFENER BETWEEN HORIZONTAL BEAMS VIII AND IX IS DISBONDED FROM BULKHEAD BETWEEN 1050L AND 425L. REPA IRED IAW HORIZON AIR EA 4-53-731. 2 L 7 2 4F RT A20EU 1999051400809 19990514 00809 EU 1999 5 14 QXEA9900887 1 19990330 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD DEBONDED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - HORIZONTAL STIFFENER BETWEEN HORIZONTAL BEAM XI AND XII IS DISBONDED FROM BULKHEAD. REPAIRED IAW HORIZON AIR EA 4 -53-731. 2 L 7 2 4F RT A20EU 1999051400810 19990514 00810 EU 1999 5 14 QXEA9900888 1 19990426 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU ROW 9 BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 PDX - EMERGENCY EVACUATION LIGHTS ON AIRCRAFT SEATS ARE NOT IN SYNC WITH EACH OTHER. FOUND WIRE FOR DISARM OF ROW 9, LE FT-HAND POWER SUPPLY BROKEN AT PIN. RE-INSTALLED WIRE WITH NEW PIN IAW FOKKER MM 33-50-00, PAGE 501, STEP 3. 2 L 7 2 4F RT A20EU 1999051400811 19990514 00811 EU 1999 5 14 QXEA9900889 1 19990425 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THE CENTER SECTION OF THE EMERGENCY ESCAPE PATH LIGHTING WILL NOT TURN OFF. REPAIRED IAW F-28 MM 33-50-00, PAGE 5 01. 2 L 7 2 4F RT A20EU 1999051400812 19990514 00812 EU 1999 5 14 QXEA9900890 1 19990417 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 3820 MISDRILLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - MISDRILLED HOLE THROUGH RADIUS OF DIAPHRAGM IN FRAME 3820, RIGHT-HAND SIDE. REPAIRED IAW HORIZON AIR EA 4-53-785. 2 L 7 2 4F RT A20EU 1999051400813 19990514 00813 EU 1999 5 14 QXEA9900891 1 19990413 A 5320 RECEPTACLE FOKKER F28 F28MK4000 4990810 EU PANEL 37AB MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - CAMLOC RECEPTACLE MISSING UNDER PANEL 37AB. REPAIRED IAW HORIZON AIR EA 4-53-744. 2 L 7 2 4F RT A20EU 1999051400814 19990514 00814 EU 1999 5 14 QXEA9900892 1 19990419 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 3820 MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 475AU 11222 PDX - FRAME 3820/3870 HAS 11 HOLES DRILLED THROUGH AFT FACE FROM STRINGER 47 TO 52. REPAIRED IAW HORIZON AIR EA 4-53-76 9. 2 L 7 2 4F RT A20EU 1999051400815 19990514 00815 EU 1999 5 14 QXEA9900893 1 19990327 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE IS A CRACKED CLIP ON FRAME 16660, BETWEEN STRINGER 49 AND 50. REPAIRED ANGLE HAS 2MM GAP BETWEEN ITSELF AND FRAME CASTELLATION. REPAIRED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999051400816 19990514 00816 EU 1999 5 14 QXEA9900894 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT-HAND INBOARD SEAT TRACK BL600L, INBOARD AND OUTBOARD FLANGES HAVE AREAS OF FRETTING CORROSION FROM FRAME 9305 B TO 9305. REPAIRED IAW F-28 MM 53-40-01, PAGE 206, FIGURE 205. 2 L 7 2 4F RT A20EU 1999051400817 19990514 00817 EU 1999 5 14 QXEA9900895 1 19990326 A 5320 FASTENERS FOKKER F28 F28MK4000 4990810 EU BS 9450-10350 MISSING A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE ARE THREE FASTENERS MISSING FROM THE VERTICAL FLANGE OF THE RIGHT OUTBOARD SEAT TRACK BETWEEN STATION 9450 A ND 10350. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400818 19990514 00818 EU 1999 5 14 QXEA9900896 1 19990326 A 5320 FASTENERS FOKKER F28 F28MK4000 4990810 EU BS 11900 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - THERE ARE 6 FASTENERS WITH TOOLING DAMAGE TO HEADS ON THE RIGHT OUTBOARD SEAT TRACK AT STATION 11900. REPAIRED IA W FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400819 19990514 00819 EU 1999 5 14 QXEA9900897 1 19990326 A 5320 FASTENERS FOKKER F28 F28MK4000 4990810 EU FRAME 13345 MISSING A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS MISSING TWO RIVETS, ONE AT FRAME 13345 AND ONE AT FRAME 10346. REPAIRED IAW FOK KER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400820 19990514 00820 EU 1999 5 14 QXEA9900898 1 19990325 A 5320 NUT PLATES FOKKER F28 F28MK4000 4990810 EU FRAME 9805-14285 MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - RIGHT OUTBOARD SEAT TRACK FROM FRAME 9805 TO 14285 IS MISSING FLOOR PANEL ATTACHMENT NUT PLATES. REPAIRED IAW FOK KER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400821 19990514 00821 EU 1999 5 14 QXEA9900899 1 19990325 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - STANDOFF BRACKET ON OUTBOARD SIDE OF RIGHT-HAND INBOARD SEAT TRACK IS CRACKED AT FRAME 6305. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999051400822 19990514 00822 EU 1999 5 14 QXEA9900900 1 19990414 A 5220 FASTENERS FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LOWER AFT CORNER OF SERVICE EMERGENCY DOOR MISSING NINE FASTENERS, REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999051400823 19990514 00823 EU 1999 5 14 QXEA9900901 1 19990325 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY DAMACED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - INSTALL DOUBLER AT LOWER FORWARD CORNER OF FUSELAGE SURROUND FOR THE SERVICE EMERGENCY DOOR. COMPLIED WITH HORIZO N AIR EA 4-53-715. 2 L 7 2 4F RT A20EU 1999051400824 19990514 00824 EU 1999 5 14 QXEA9900902 1 19990414 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - INSTALL DOUBLER AT LOWER AFT CORNER OF FUSELAGE SURROUND FOR THE SERVICE EMERGENCY DOOR. COMPLIED WITH HORIZON AI R EA 4-53-715. 2 L 7 2 4F RT A20EU 1999051400825 19990514 00825 EU 1999 5 14 QXEA9900903 1 19990325 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - INSTALL DOUBLER AT UPPER AFT CORNER OF FUSELAGE SURROUND FOR THE SERVICE EMERGENCY DOOR. COMPLIED WITH HORIZON AI R 4-53-715. 2 L 7 2 4F RT A20EU 1999051400826 19990514 00826 EU 1999 5 14 QXEA9900904 1 19990324 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 475AU 11222 PDX - LEFT-HAND INBOARD SEAT TRACK FROM A POINT APPROXIMATELY 8 AFT OF FRAME 7805, FORWARD TO THE END OF THE SEAT TRACK SECTION NEEDS TO BE REPLACED. REPLACED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999051400827 19990514 00827 WP 1999 5 14 ABXA9900326 1 19990314 A 5751 5763090 FITTING DOUG DOUG DC8 DC863 302198A WP RT AILERON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 RIGHT WING INBOARD AILERON, INBOARD ATTACH FITTING IS BROKEN OFF ON AILERON SIDE. REPLACED FITTING IAW DC8 SRM 27-10-00 . 2 L 7 4 4F 4A25 1999051400828 19990514 00828 WP 1999 5 14 ABXA9900327 1 19990313 A 5730 5611278 SKIN DOUG DOUG DC8 DC863 302198A WP WS 285.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LEFT WING AT LEADING EDGE XFS 285.250 CRACKED AT 3 SCREWS. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999051400829 19990514 00829 WP 1999 5 14 ABXA9900328 1 19990313 A 5712 5769600A RIB DOUG DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LEFT WING LEADING EDGE RIB CRACKED JUST FORWARD OF ACCESS PANEL NR 519A. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999051400830 19990514 00830 WP 1999 5 14 ABXA9900329 1 19990313 A 5730 57695891 SKIN DOUG DOUG DC8 DC863 302198A WP WS 6.225 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 813AX 46136 LEFT WING UPPER SURFACE AT FRONT SPAR BETWEEN STATIONS XOLDI 6.225 AND XFS 379.000 HAD HEAVY INTERNAL CORROSION. REPAIR ED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999051400831 19990514 00831 WP 1999 5 14 ABXA9900330 1 19990418 A 5320 991015527 GUSSET DOUG DOUG DC9 DC931 3022065 WP BS 700 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND RIGHT WHEEL WELL CEILING GUSSET CORRODED AT STATION 700, RBL 32. REPAIRED GUSSET IAW DC9 SRM 53-1 1-3 AND 51-30-3. 2 L 7 2 4F A6WE 1999051400832 19990514 00832 WP 1999 5 14 ABXA9900331 1 19990430 A 3310 5008CW BULB DOUG DC8 DC863 302198A WP COCKPIT FAILED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 828AX 45999 DURING CRUISE, NOTICED ODOR (BURNING SMELL) COMING FROM AREA OF FIRST OFFICER'S GLARESHIELD FLOURESCENT LIGHT. REPLACED LIGHT BULBS AND REMOVED GLUE FROM LIGHT ASSY AREA. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999051400833 19990514 00833 1999 5 14 ABXA9900332 4 19990428 A 3160 SYMBOL GEN DOUG DC8 DC861 3021952 WP RT COCKPIT MALFUNCTIONED A ABXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 852AX 46016 DURING SHORT FINAL, AT 500 FT, LOST ALL NAVIGATIONAL GUIDANCE ON FIRST OFFICER'S SIDE. ALL FLAGS APPEARED. OPENED AND CLOSED NAV CONCENTRATOR AND SYMBOL GENERATOR CIRCUIT BREAKERS, ALL INSTRUMENTS RETURNED TO NORMAL. COULD NOT DUPLICATE DISCREPANCY. ALL EQUIPMENT OPS CHECKED GOOD IAW DC8 MM 34-20-0. 2 L 7 4 4F 4A25 1999051400834 19990514 00834 WP 1999 5 14 MWEA99245 1 19990503 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE GALLEY DOOR SLIDE PRESSURE GAUGE IS LOW AT 2500 PSI. MAINTENANCE REMOVED AND REPLACED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1999051400835 19990514 00835 NM 1999 5 14 MWEA99246 1 19990501 A 2560 100502121 COVER DOUG MD88 MD88 3023688 NM GALLEY DR SLIDE LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 804ME 48030 LOOSE RETAINING PINS ON BOTTOM OF AFT GALLEY SERVICE DOOR SLIDE COVER. ADJUSTED RETAINER PINS AND SLIDE COVER. 2 L 7 2 4F RT A6WE 1999051400836 19990514 00836 WP 1999 5 14 MWEA99247 1 19990429 A 5313 527779221 LONGERON DOUG DC9 DC932 3022066 WP BS 433 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 LONGERON 17L AT STATION 433 IS DENTED. MAINTENANCE FABRICATED AND INSTALLED FILLER AND SPLICES. 2 L 7 2 4F A6WE 1999051400837 19990514 00837 WP 1999 5 14 MWEA99248 1 19990429 A 5320 59122851 DOUBLERS DOUG DC9 DC932 3022066 WP BS 465 DOUBLE DRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 205ME 47601 WINDOW DOUBLERS AT FS 465 503 HAVE SEVERAL DOUBLE DRILLED HOLES. MAINTENANCE FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1999051400838 19990514 00838 NM 1999 5 14 SCNA99703 1 19990413 A 5347 SEAT TRACK BOEING 727 727282 138408T NM BS 1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 1130 WAS FOUND CORRODED OUT OF LIMITS AT THE ATTACH POINT TO THE FLOORBEAM. REMOVED CORROSION IAW B727 SRM 531001. FABRICATED NEW SEAT TRACK FOM BAC 1520792 IAW B727 SRM 511001. TRE ATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED NEW SEAT TRACK IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 1999051400839 19990514 00839 NM 1999 5 14 SCNA99704 1 19990413 A 5315 FLOORBEAM BOEING 727 727282 138408T NM BS 1110 CORRODED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM AT STA 1110 HAS CORRISION OUT OF LIMITS ON THE TOP OF THE FLOORBEAM BETW EEN LT BUTTLINE 24 AND RT BUTTLINE 24. REMOVED CORROSION IAW B727 SRM 531001. FABRICATED NEW FLOORBEAM SUPPORT IAW B72 7 SRM 531008. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 1999051400840 19990514 00840 NM 1999 5 14 DHL99712001 1 19990422 A 2910 82060C08N LINE BOEING 727 72729 1384007 NM NR 2 HYD PUMP RUPTURED A DHLA O OTHER K FLUID LOSS CR CRUISE 1 SO 01 712DH 19401 HYDRAULIC B PUMP NR 2 FAILED AND NR 1 PUMP FAILED INTERMITTENTLY AND PRESSURE DROPPED TO 2000 PSI INTERMITTENTLY. NR 2 PUMP PRESSURE LINE BROKEN. REMOVED AND REPLACED LINE PER MM 29-12-11. INSPECTED AND CHANGED BOTH CASE DRAIN FILTERS AS PRECAUTION. RAN AND LEAK CHECKED OK. 2 L 7 3 4F A3WE 1999051400841 19990514 00841 NE 1999 5 14 TC8A99015 2 19990424 A 7321 FUEL CONTROL DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE MALFUNCTIONED A TC8A O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 23 184SK 45981 669157 TRIP NR 03295 LATI-EINN, NR 1 ENGINE FLAMEOUT AT 22:05 Z, ON DESCENT. ENGINE FLAMEOUT CHECKLIST COMPLETED, 35 PERCENT N 2, OIL PRESSURE 20 PSI AND 25 PERCENT N1. PROCEEDED IN FLIGHT START JT3D CHECKLIST, NO RESPONSE. REMOVED AND REPLACED FUEL CONTROL IAW MM 73-20-1, NO HELP. PREPARED AIRCRAFT FOR THREE ENGINE FERRY. 2 L 7 4 4F 4 F 4A25 1E8 1999051900001 19990519 00001 NM 1999 5 19 CALA9900450 1 19990428 A 5310 146N52932 STRUCTURE BOEING 757 757224 1384958 NM BS 1640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12109 27299 M LAVATORY AFT ATTACHMENT POINTS CORRODED. REPLACED AFT ATTACH POINTS PER SRM 51-40-01. 2 L 7 2 4F RT A2NM 1999052100001 19990521 00001 WP 1999 5 21 TWAA9906901 1 19990504 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 200-206 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND FORMER AND WEB CORRODED AT STA 200 TO 206, LONGERON 18L AND ABOVE. REMOVED CORROSION PE R SPM 6-80-1, PARAGRAPH 3, SECTION A FIG 1. INSTALLED NEW WEB PER SPM 6-70-1. 2 L 7 2 4F A6WE 1999052100002 19990521 00002 WP 1999 5 21 TWAA9906902 1 19990505 A 5744 CASTING DOUG DC9 DC931 3022065 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND RT WING T/E REAR SPAR CENTER FLAP ATTACH CASTING HOLES LINER O/B HOLE AT 6 O'CLOCK POSIT ION WITH CRACK INDICATION. FIFTEEN PERCENT THICKNESS GROUND OUT AND CRACK WAS GONE. REPAIRED REAR SPAR AREA PER DOUGLA S SERVICE REWORK DRAWING J060272. 2 L 7 2 4F A6WE 1999052100003 19990521 00003 WP 1999 5 21 TWAA9906903 1 19990505 A 5320 SPLICE DOUG DC9 DC931 3022065 WP BS 229 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND IN FWD CARGO COMPT THAT LONGERON 30 PRODUCTION SPLICE HAD 2 CRACKS APPROX 1 INCH LONG AT STA 229. REPLACED CRACKED SPLICE PER DOUGLAS INSTALLATION DRAWING 5913508. 2 L 7 2 4F A6WE 1999052100004 19990521 00004 WP 1999 5 21 TWAA9906904 1 19990510 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND STA 965 BULKHEAD CRACKED BETWEEN LONGER 15 AND 16L. REMOVED AND REPLACED WEB PER SPM 6- 70-01. 2 L 7 2 4F A6WE 1999052100005 19990521 00005 WP 1999 5 21 TWAA9907001 1 19990507 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND FLOORBEAM AT STA 160, RBL 48, WITH CORROSION MATERIAL LOSS BEYOND LIMITS TO THE TOP CAP AFT FLANGE. REPAIRED PER SRM 53-05, FIG 20A. 2 L 7 2 4F A6WE 1999052100006 19990521 00006 NM 1999 5 21 HNAA9900058 1 19990512 A 3350 6104791X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 916HA 072 LEFT HAND FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY 3351-PS1. 2 H 7 2 4T RT A13NM 1999052100007 19990521 00007 1999 5 21 MALA976448 4 19990508 A 2565 D31003105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PASSENGER DOOR FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 523XJ E2348 THE MAIN PASSENGER DOOR SLIDE LAYING ON THE JETWAY DIDN'T INFLATE. MAINTENANCE REPLACED SLIDE. ALL WORK DONE PER AVRO MM 25. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999052100008 19990521 00008 NE 1999 5 21 MALA976449 2 19990507 A 7532 7858023 BLEED VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 457XJ 457 LEFT BLEED FAULT LIGHT ILLUMINATED IN FLIGHT. FOLLOWED QRH AND CLOSED LEFT BLEED VALVE, WITH LEFT BLEED VALVE CLOSED, L EFT BLEED FAULT LIGHT ILLUMINATED FOR ABOUT 3 SECONDS, ROUGHLY EVERY 4 MINUTES. MAINTENANCE REPLACED LEFT PRESSURE BLEE D SWITCH. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1999052100009 19990521 00009 WP 1999 5 21 CALA9900538 1 19990513 A 5754 5935801 FAIRING DOUG DC9 DC982 3022082 WP NR 4 LE SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35836 49441 LEFT WING NR 4 SLAT TRACK CAN GOUGED. WELDED CAN PER DRWG 5935801 AND INSTALLED PER MM 27-80-01. 2 L 7 2 4F A6WE 1999052100010 19990521 00010 NM 1999 5 21 CALA9900539 1 19990513 A 5753 652163492 SKIN BOEING 727 727224 1384076 NM RT TE AFT FLAP DEBOND A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 RIGHT INBOARD AFT FLAP AFT SEGMENT UPPER SURFACE HAS 3.25 CHAFED SPOT AND 1.25 X .75 DEBOND AREA 27.5 FROM INBOARD END. REMOVED AND REPLACED FLAP. 2 L 7 3 4F A3WE 1999052100011 19990521 00011 NM 1999 5 21 CALA9900540 1 19990510 A 5210 69765581 TRIGGER BOEING 737 7373T0 1384582 NM PASSENGER DOOR OUT OF POSITION A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 69348 23586 FORWARD ENTRY DOOR WILL NOT OPEN. FOUND RELEASE LATCH MECHANISM DISSASSEMBLED AND TRIGGER OUT OF POSITION. REASSEMBLED AND TESTED PER MM 52-11-00 PAGE 501. 2 L 7 2 4F RT A16WE 1999052100012 19990521 00012 SO 1999 5 21 COMA9910079 1 19990512 A 3350 1011107 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 168CA 1168 EXIT SIGN DETACHED AT SEAT 5A. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999052100013 19990521 00013 SO 1999 5 21 COMA9910080 1 19990511 A 7722 T6 WARNING EMB 120 EMB120RT SO ENGINE ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 179CA 1179 ABORTED TAKEOFF DUE TO T6 WARNING. DOWNLOADED DFDR, FOUND ALL PARAMETERS TO BE WITHIN LIMITS PER PRATT P WHITNEY MAINT MANUAL 02-10-00. NO ACTION REQUIRED. 2 L 7 2 4T RT A31SO 1999052100014 19990521 00014 EA 1999 5 21 COMA9960197 1 19990511 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 963CA 7127 LEFT SIDE WINDOW CRACKED AT 33,000 FT. SHATTERED ON FINAL APPROACH. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 1999052100015 19990521 00015 EA 1999 5 21 COMA9960198 1 19990511 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7689 7131 FLOOR EMERGENCY EXIT LIGHTS WILL NOT COME ON. REPLACED BATTERY AT NR 3 POSITION. 2 L 7 2 4F RT A21EA 1999052100016 19990521 00016 EA 1999 5 21 COMA9960199 1 19990510 A 5270 840534 SWITCH CNDAIR CL600 CL6002B19 EA PASSENGER DOOR CONTAMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 75CA 7267 PAX DOOR OUTER HANDLE MESSAGE THEN PAX DOOR WARNING AT 7,000 FT. CLEANED WATER FROM CONNECTOR BELOW TOP STEP. 2 L 7 2 4F RT A21EA 1999052100017 19990521 00017 EA 1999 5 21 COMA9960200 1 19990507 A 5210 600319463 MECHANISM CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 721CA 7259 AFTER TAKEOFF, DOOR WARNING ILLUMINATED, RETURNED TO AIRPORT. ADJUSTED PUSH ROD ON PULL IN LEVER. 2 L 7 2 4F RT A21EA 1999052100018 19990521 00018 EA 1999 5 21 COMA9960201 1 19990411 A 3520 115083001 MASK CNDAIR CL600 CL6002B19 EA ROW 12CD MALFUNCTIONED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 PASSENGER O2 MASKS AT SEAT 12 CD WOULD NOT AUTO DEPLOY. REPLACED PASSENGER OXYGEN MODULE. 2 L 7 2 4F RT A21EA 1999052100019 19990521 00019 EA 1999 5 21 COMA9960202 1 19990415 A 3350 58731 LIGHT CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912CA 7011 EMERGENCY FLOOR LIGHT (P/N 5873-1) BROKEN. REPLACED EMERGENCY LIGHT TRACK. 2 L 7 2 4F RT A21EA 1999052100020 19990521 00020 EA 1999 5 21 COMA9960203 1 19990413 A 2520 987041 LEG CNDAIR CL600 CL6002B19 EA SEAT 3A & 3B BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 SEAT 3A AND 3B LEG BRACE CRACKED. REPLACED LEG ASSEMBLY. 2 L 7 2 4F RT A21EA 1999052100021 19990521 00021 EA 1999 5 21 COMA9960204 1 19990415 A 3350 58728 LIGHT CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912CA 7011 EMERGENCY FLOOR LIGHT (P/N 5872-8) BROKEN. REPLACED EMERGENCY LIGHT TRACK. 2 L 7 2 4F RT A21EA 1999052100022 19990521 00022 EA 1999 5 21 COMA9960205 1 19990414 A 5210 6006153552 SEAL STRIKER CNDAIR CL600 CL6002B19 EA PASSENGER DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 PREVIOUS REPAIR TO PAX DOOR SEAL STRIKER AT FS 310.00, FILLER IS LOOSE AND DAMAGED. REPLACED FILLER IN PREVIOUS REPAIR. 2 L 7 2 4F RT A21EA 1999052100023 19990521 00023 EA 1999 5 21 COMA9960206 1 19990512 A 3250 16740101 RVDT CNDAIR CL600 CL6002B19 EA RUDDER PEDALS MISINSTALLED A COMA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 01 926CA 7027 RUDDER INPUT TO NOSEWHEEL BACKWARDS, TILLER INPUT CORRECT. FOUND RUDDR PEDAL INPUT RVDT, APPROXIMATELY 180 DEGREES FROM CENTER. INSTALLED RVDT PROPERLY PER TASK 82-51-05-400-801. 2 L 7 2 4F RT A21EA 1999052100024 19990521 00024 NM 1999 5 21 UPS99229565 1 19990506 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, ON EMERGENCY EXIT LIGHT CK FOUND FWD RT OVERWING EXIT LIGHT OUT INSIDE CABIN, BOTH STAIRWELL LIGHTS OUT, BOTH LIGHTS OUT OVERWING UNDER OVERWING EXITS ON LEFT AND RIGHT SIDE OF AIRCRAFT AND LEFT REAR OUTSIDE LIGHT VERY DIM. FWD RIGHT OVERWING EXIT LIGHT REMOVED AND REPLACED, OPS CHECK GOOD. BOTH BATT PACKS REMOVED AND REPLACED, OPS CHE CK GOOD. ALL BATTERIES REMOVED AND REPLACED, OPS CK GOOD. REMOVED AND REPLACED LEFT REAR OUTSIDE BATT, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999052100025 19990521 00025 WP 1999 5 21 UPS99829563 1 19990511 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATT PACK, OPS CHECK GOOD. (P/N 60-1 223-5), (S/N 339) ON, (S/N 337) OFF. 2 L 7 4 4F RT 4A25 1999052100026 19990521 00026 WP 1999 5 21 UPS99829564 1 19990509 A 5314 KEEL BEAM DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:N/A, MAIN LANDING GEAR DOOR SUB KEEL BEAM STRUCTURE HAS SEVERAL CRACKS. 2 L 7 4 4F RT 4A25 1999052100027 19990521 00027 NM 1999 5 21 UPS99229570 1 19990511 A 5730 SKIN BOEING 727 72725C 138400H NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:C, FOUND .30 CRACK RADIATING FROM RIVET ON RIGHT WING TIP UPPER SKIN 18 INCHES AFT OF FORWARD EDGE, 6 IN CHES O/B OF I/B EDGE. STOP DRILLED CRACK AND TRANSFERRED TO NON-ROUTINE CARD 943723. 2 L 7 3 4F A3WE 1999052100028 19990521 00028 WP 1999 5 21 UPS99829566 1 19990414 A 7830 BRACKET DOUG DC8 DC873F 302199F WP NR 4 ENG TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C, NR 4 ENGINE OUTBOARD T/R FWD LOWER CORNER BRACKET CRACKED. DYE PEN AREA IAW MIL-27IF, NO CRACKS NOTE D. 2 L 7 4 4F RT 4A25 1999052100029 19990521 00029 WP 1999 5 21 UPS99829568 1 19990415 A 5320 FITTING DOUG DC8 DC873F 302199F WP CABIN MISDRILLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C2, MAIN CABIN C-3 TORQUE BOX HAS MISDRILLED HOLES L-20R. REMOVED FORWARD SECTION, REMOVED FITTINGS, LO CATED DRILLED FITTINGS, INSTALLED FITTINGS, FABBED INNER AND OUTER IAW DC8 SRM 51-1-20D AND 5 1-3-0. 2 L 7 4 4F RT 4A25 1999052100030 19990521 00030 WP 1999 5 21 UPS99829569 1 19990419 A 5744 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:C2, RT WING FLAP HINGE SUPPORT FITTING I/B SIDE GAVE CRACK INDICATION. REPLACED BRACKET. 2 L 7 4 4F RT 4A25 1999052100031 19990521 00031 WP 1999 5 21 UPS99829571 1 19990513 A 3260 313 BULB DOUG DC8 DC871F 302199D WP RT MLG FAILED A IPXA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 01 797UP 45897 INSPECTION TYPE:N/A, ON FINAL APPROACH LOWERED LANDING GEAR, RT MAIN GREEN LIGHT DID NOT ILLUMINATE. CYCLED GEAR, SAME INDICATION. ALSO, RED NOT LATCHED LIGHTS DID NOT ILLUMINATE. AFTER MISSED APPROACH RAISED GEAR, REPLACED BULBS, LOWERE D GEAR, RT MAIN ILLUMINATED AS NORMAL. SYSTEM OPS CHECKED NORMAL. 2 L 7 4 4F RT 4A25 1999052100032 19990521 00032 NM 1999 5 21 99FDEA00175 1 19990512 A 2613 OVERHEAT LIGHT BOEING 727 72721C 138400M NM LWR AFT BODY MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 144FE 19137 LOWER AFT BODY O/H LIGHT ON. LIGHT WENT OUT WHEN NR 1 BLD AND LT PACK TURN OFF. INSP DUCT IN AFT AIR STAIRS, CEILING, KEEL BEAM AREA AND NO LEAKS FOUND. COULD NOT DUP O/H COND. OK TO CONTINUE SERVICE. 2 L 7 3 4F A3WE 1999052100033 19990521 00033 NM 1999 5 21 99FDEA00176 1 19990512 A 2910 AF2480010H0360 HOSE BOEING 727 727225 1384077 NM LT MLG LEAKED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 468FE 21452 99-110 - UPON RAISING GEAR HANDLE, A SYS HYD PRESSURE AND QUANTITY BOTH WENT TO ZERO. REMOVED AND REPLACED LEFT MAIN LA ND GEAR ACTUATOR HOSE. LEAK AND OPER CK GOOD PER MM 29-11-000-1. 2 L 7 3 4F A3WE 1999052100034 19990521 00034 NM 1999 5 21 99FDEA00177 1 19990512 A 2613 652492 CONTROL UNIT BOEING 727 727233 138408A NM E & E COMPT MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 258FE 20940 LOWER BODY O/H LIGHT ILLUM, WITH BOTH PACKS ON NR 1 ENG BLD CLOSED NR 2 AND 3 ENG BLD OPEN. RAN RED TABS 2-714 WHEN NR 1 BLD AND LT PACK OFF LIGHT WENT OUT. REMOVED AND REPLACED AFT BODY O/H DETECTION DETECTOR AS PER MM 26-14-0, OPER CK N ORM. 2 L 7 3 4F RT A3WE 1999052100035 19990521 00035 WP 1999 5 21 ABXA9900361 1 19990426 A 3297 WIRE DOUG DC9 DC931 3022065 WP NLG BROKEN A ABXA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 23 929AX 45874 NOSE GEAR UNSAFE LIGHT FAILED TO ILLUMINATE DURING GEAR RETRACTION. RECYCLED GEAR, UNSAFE LIGHT FAILED TO ILLUMINATE IN TRANSIT. ALL OTHER INDICATIONS WERE NORMAL. REPAIRED BROKEN WIRE IN CONDUIT JUST AFT OF NOSE GEAR DEPLOYMENT SWITCH (P 1-133). 2 L 7 2 4F A6WE 1999052100036 19990521 00036 WP 1999 5 21 ABXA9900362 1 19990420 A 5712 9919305951 RIB DOUG DOUG DC9 DC941 302207N WP WS 232.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND LEFT WING NR 5 TRACK RIB CRACKED AT STATION XOS 232.5. REPLACED INBOARD WING RIB IAW DC9 SRM. 2 L 7 2 4F A6WE 1999052100037 19990521 00037 WP 1999 5 21 ABXA9900363 1 19990420 A 5751 S391318072 SKIN DOUG DOUG DC9 DC941 302207N WP RT AILERON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND RIGHT AILERON SKIN TRAILING EDGE CRACKED. REPLACED RIGHT AILERON SKIN TRAILING EDGE IAW DC9 SRM 5 1-30-08. 2 L 7 2 4F A6WE 1999052100038 19990521 00038 WP 1999 5 21 ABXA9900364 1 19990420 A 5320 D0489835 WEB DOUG DOUG DC9 DC941 302207N WP BS 984-992 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND CUSP WEB CRACKED STATION 984 TO 992 LEFT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 1999052100039 19990521 00039 WP 1999 5 21 ABXA9900365 1 19990420 A 5320 D0489841 WEB DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 1021 RIGHT. REPLACED CUSP WEB IAW ABX REA D953-28177 MR. 2 L 7 2 4F A6WE 1999052100040 19990521 00040 WP 1999 5 21 MWEA99268 1 19990506 A 5311 5911448517 FRAME DOUG DC9 DC932 3022066 WP BS 503 SPLICED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 THE FORWARD CARGO COMPARTMENT AT FS 503 REQUIRES A SPLICE TO REMOVE LONGERON 30 SECTION. MTC FABRICATED AND INSTALLED F RAME SPLICE AND ANGLE. 2 L 7 2 4F A6WE 1999052100041 19990521 00041 WP 1999 5 21 MWEA99269 1 19990505 A 5313 592031504 LONGERON DOUG DC9 DC932 3022066 WP BS 506 OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 30 AT STATION 506 IS BLENDED OUT OF LIMITS. MTC FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 1999052100042 19990521 00042 WP 1999 5 21 MWEA99270 1 19990507 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT COWL DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 204ME 47680 THE LEFT COWL EMERGENCY LIGHT DID NOT STAY ILLUMINATED FOR THE 10 MINUTE TEST. MTC REMOVED AND REPLACED EMERGENCY BATTE RY PACK. 2 L 7 2 4F A6WE 1999052100043 19990521 00043 NM 1999 5 21 MWEA99271 1 19990506 A 2560 113317 COVER DOUG MD88 MD88 3023688 NM GALLEY DR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 808ME 48070 THE AFT GALLEY SLIDE COVER CAME LOOSE. MTC REINSTALLED GALLEY SLIDE. 2 L 7 2 4F RT A6WE 1999052100044 19990521 00044 WP 1999 5 21 MWEA99272 1 19990507 A 5320 5911448503 SPLICE DOUG DC9 DC932 3022066 WP BS 503 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 THE FORWARD CARGO COMPARTMENT AT FS 503 REQUIRES A SPLICE TO REMOVED LONGERON 30. MTC FABRICATED AND INSTALLED FRAME SP LICE. 2 L 7 2 4F A6WE 1999052100045 19990521 00045 WP 1999 5 21 MWEA99273 1 19990509 A 5311 992361935 FORMER DOUG DC9 DC932 3022066 WP BS 503 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 204ME 47680 FOUND A BAD FASTENER HOLE IN FORMER AT STATION 503 L30. MTC FABRICATED AND INSTALLED FORMER. 2 L 7 2 4F A6WE 1999052100046 19990521 00046 WP 1999 5 21 MWEA99280 1 19990512 A 2560 113311DG COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF WHEN DOOR WAS CLOSED. REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999052100047 19990521 00047 WP 1999 5 21 SCNA99509 1 19990510 A 2134 1194P005005 SWITCH DOUG DC10 DC1015 3022118 WP CABIN FAILED A SCNA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 GL 15 154SY 48259 DURING A HEAVY MAINTENANCE VISIT, DURING COMPLETION OF A CABIN LEAK CHECK THE ALTITUDE WARNING HORN FAILED TO GO OFF WHE N THE CABIN ALTITUDE REACHED 12,000 FT. REMOVED AND REPLACED THE CABIN ALTITUDE SWITCH AND THE SYSTEM OPERATIONALLY CHE CKS GOOD IAW DC10 MM 213303. 2 L 7 3 4F A22WE 1999052100048 19990521 00048 NM 1999 5 21 VNAA9905001 1 19990508 A 3260 OL3092 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG FAILED A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 459PS 3070 THE RIGHT HAND MAIN LANDING GEAR FAILED TO INDICATE A DOWN AND LOCKED CONDITION WHEN SELECTED. THE CREW FOLLOWED QRH PR OCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT CONTINUED THE APPROACH AND A SAFE LANDING WAS MADE. MAINTENANCE INSPE CTED AND REPLACED THE RIGHT HAND MAIN LANDING GEAR DOWNLOCK INDICATOR LIGHT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANU AL 31-14-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999052100071 19990521 00071 CE 1999 5 21 99ZZZX2039 1 19990429 A 3230 BREAKER BEECH 58 58 1152740 CE MLG MALFUNCTIONED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 78DM TH281 BOS - GEAR TRIPPED CIRCUIT BREAKER WHEN GEAR WAS ONLY HALF WAY DOWN. CYCLED GEAR BACK UP, THEN DOWN AGAIN, THEN OK. JA CKED AIRCRAFT, CYCLED GEAR 10 TIMES. OPS CHECKED OK. RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3A16 1999052100079 19990521 00079 WP 1999 5 21 99ZZZX2047 2 19990429 A 7261 CHIP LIGHT CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7313 01518 WP ENGINE ILLUMINATED A DBCA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 13 50DS 6500078 P87267 PILOT NOTED A CHIP DETECTOR LIGHT IN-FLIGHT. PILOT LANDED IN BUFFALO, NY WITHOUT INCIDENT. CLEANED CHIP DETECTOR AND G ROUND RAN. OPERATIONS CHECK OK. PILOT RESUMED TRIP TO MILWAUKEE WITHOUT INCIDENT. SOAP SAMPLE TAKEN AND SENT TO GARRE TT-SPRINGFIELD FOR ANALYSIS. 2 L 7 2 4F 4 F A9NM E6WE 1999052100081 19990521 00081 CE 1999 5 21 99ZZZX2049 1 19990326 A 2150 5055434169 VALVE 574 BEECH 90 F90 1152909 CE CABIN FAILED A PRIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 03 236JS LA90 AIR VALVE STUCK IN OPEN POSITION CAUSING FULL HOT AIR TO CABIN. SMOKE STARTED TO FLOW INTO CABIN AFTER TAKEOFF. AIRCRA FT RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE CLEANED VALVES AND OPS CHECKED OK. BOTH BYPASS VALVES WILL BE REP LACED. 1 L 7 2 4T A31CE 1999052100088 19990521 00088 WP 1999 5 21 TWAA9907101 1 19990511 A 2131 10256862 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A TWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CE 05 976Z 47248 WHILE DESCENDING FROM FL350 TO FL310, LOST CABIN PRESSURIZATION CONTROL. ACCOMPLISHED EMERGENCY DESCENT. REGAINED CONT ROL AT LOWER ALTITUDE. MADE UNSCHEDULED LANDING AT IAH. FOUND AUTO PRESSURIZATION CONTROL INOPERATIVE. PLACARDED AUTO PRESSURIZATION CONTROL PER MEL. THE AUTO PRESSURIZATION CONTROLLER WAS LATER REPLACED. CHECK-C 8-4-98 MCI. 2 L 7 2 4F A6WE 1999052100089 19990521 00089 WP 1999 5 21 TWAA9907102 1 19990512 A 2150 20495054 ACM DOUG DC9 DC983 3022083 WP LEFT FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 05 9619V 53566 ON TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT FROM THE LEFT AIR CONDITIONING PACK. PLACARDED THE PACK INOPERATIVE PER MEL. THE LT AIR CYCLE MACHINE WAS LATER REPLACED DUE TO LEAKAGE. CHECK-C 10-13-98 STL. 2 L 7 2 4F RT A6WE 1999052100090 19990521 00090 WP 1999 5 21 TWAA9907103 1 19990508 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 DURING CHECK-C MAINT, FOUND LOWER RT VERTICAL STABILIZER MOUNT ANGLE CRACKED 2 PLACES AFT END BELOW RUDDER. ACCOMP NDT HFEC FOR CRACK CONTAINMENT AFTER SECTION CUT OUT. TRIMMED OUT CRACK PER SRM 53-05. 2 L 7 2 4F A6WE 1999052100091 19990521 00091 WP 1999 5 21 TWAA9907104 1 19990508 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 DURING OP 16 MAINT CHECK, FOUND LONGERON 4L CRACKED2 EA PLACES APPROX .5 IN LONG AT STA 160. REPLACED FULL SECTION OF L ONGERON 4L STA 150 TO 228 PER SPM 6-70-1. 2 L 7 2 4F A6WE 1999052100092 19990521 00092 NM 1999 5 21 CALA9900541 1 19990514 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 RIGHT LAVATORY FLOOR SUPPORT CORRODED BS 1006-APB RBL18. REPLACED RIGHT AFT LAV FLOOR SUPPORT PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999052100093 19990521 00093 NM 1999 5 21 CALA9900542 1 19990514 A 5320 WEB BOEING 727 727224 1384076 NM BS 1283-1342 CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 AFT AIR STAIR ENTRY WAY LEFT WEB PANEL HAS CHAFE MARKS (6 EA) FROM STA 1283 TO 1342. FABRICATED, TREATED, PRIMED, AND I NSTALLED REPAIR DOUBLER PER SRM 52-01 FIG 61, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1999052100094 19990521 00094 WP 1999 5 21 CALA9900543 1 19990513 A 5315 2921948 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 465 CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 CABIN FS 465 FLOORBEAM UPPER FLANGE IS CHFED BETWEEN RBL 12 AND LDL 12. BLENDED FLOOR BEAM UPPER FLANGE. DIMENSIONS OU T OF LIMITS. REPAIRED FLOORBEAM SUPPORT PER EAC 531155-01055. 2 L 7 2 4F A6WE 1999052100095 19990521 00095 WP 1999 5 21 CALA9900544 1 19990513 A 5315 2777897 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 908 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 AFT CARGO PIT UPPER SIDE OF FLOORBEAM LBL 22 STA 980 IS CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-3, 53-1 0 FIG 10, 53-05 FIG 20A, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 1999052100096 19990521 00096 WP 1999 5 21 CALA9900545 1 19990513 A 5315 2921998 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 408 CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 CABIN FS 408 FLOORBEAM UPPER FLANGE IS CHAFED BETWEEN RBL 12 AND LBL 12. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-30, 53-05, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 1999052100097 19990521 00097 WP 1999 5 21 UPS99829572 1 19990428 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LONG 36 FLANGE AT FS 1360 IS CORRODED BEYOND LIMITS. REPAIRED LONGERON 36 IAW DHC SK880-514. 2 L 7 4 4F RT 4A25 1999052100098 19990521 00098 WP 1999 5 21 UPS99829573 1 19990422 A 5510 4653888502504 FITTING DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LT HORIZ STAB LWR BATHTUB FITTINGS (3 EA.) AT XFS 47 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED 3 EA FITTINGS IAW DWG 4653888, 4653760; AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100099 19990521 00099 WP 1999 5 21 UPS99829574 1 19990430 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FS 1000 FRAME UPPER FLANGE, LWR SURFACE AT LONGERON 36, IS CORRODED BEYOND LIMITS. REPAIRED FRAME IA W SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999052100100 19990521 00100 WP 1999 5 21 UPS99829575 1 19990422 A 5510 4653888504 FITTING DOUG DC8 DC873F 302199F WP RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 RT HORIZ STAB L/E AT XFS 47, THE UPPER BATHTUB FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLE D FITTING IAW DWG 4653888 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100101 19990521 00101 WP 1999 5 21 UPS99829576 1 19990419 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 RT WING L/E, INBD STA XOLDI 6.225 RIB IS CRACKED ABOVE THE PNEU DUCT. STOP DRILLED CRACK AND REPAIRE D IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999052100102 19990521 00102 WP 1999 5 21 UPS99829577 1 19990418 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FS 55 FRAME IS CRACKED AT LONGERON 24L, AROUND THE ROD ATTACHMENT. CUT OUT DAMAGED AREA AND REPAIRED SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999052100103 19990521 00103 WP 1999 5 21 UPS99829578 1 19990419 A 5720 36433192 ANGLE DOUG DC8 DC873F 302199F WP WS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, THE RT STA 98 FLAP ACTUATOR ATTACH FITTING INBD MOUNT ANGLE IS CRACKED AT THE LWR END. REMOVED, FAB RICATED, AND REPLACED THE ANGLE IAW DWG 3643319 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999052100104 19990521 00104 WP 1999 5 21 UPS99829579 1 19990421 A 5320 3755843501 FITTING DOUG DC8 DC873F 302199F WP BS 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FS 1150 TORQUE BOX BATHTUB FITTING BETWEEN LONGERON 35R AND 34R IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999052100105 19990521 00105 WP 1999 5 21 UPS99829580 1 19990420 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LEFT WING INBOARD RIB AT XOLDI 6.225 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999052100106 19990521 00106 WP 1999 5 21 UPS99829581 1 19990504 A 5320 9754002201 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FITTING AT FS 280 AND LONGERON 34L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 5 1-3-0. 2 L 7 4 4F RT 4A25 1999052100107 19990521 00107 WP 1999 5 21 UPS99829582 1 19990427 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 55-80 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 SEAT TRACK FLANGE AT RBL 48, FS 55 TO 80 IS CORRODED BEYOND LIMITS. REMOVED DAMAGED SEAT TRACK FS 55 TO 110, FABRICATED AND REPLACED IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999052100108 19990521 00108 WP 1999 5 21 UPS99829583 1 19990421 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 1834 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FS 1834 SHEAR TIE CRACKED AT LONGERON 3L. REMOVED DAMAGED SHEAR TIE, FABRICATED, AND REPLACED IAW SR M 53-2-0. 2 L 7 4 4F RT 4A25 1999052100109 19990521 00109 WP 1999 5 21 UPS99829584 1 19990418 A 5313 3648666 LONGERON DOUG DC8 DC873F 302199F WP BS 55-70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LONGERON 27R IS CRACKED BETWEEN FS 55 AND 70. REMOVED DAMAGED LONGERON, FABRICATED, AND REPLACED IAW DWG 3648666 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100110 19990521 00110 WP 1999 5 21 UPS99829585 1 19990430 A 5320 3619434503 SPLICE DOUG DC8 DC873F 302199F WP BS 1490 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 LONGERON 35L SPLICE AT FS 1490 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21 . 2 L 7 4 4F RT 4A25 1999052100111 19990521 00111 WP 1999 5 21 UPS99829586 1 19990422 A 5320 3642974502 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FITTING TOP OF CENTER WING BOX AT FS 680 AND LONGERON 22R IS CRACKED. REMOVED, FABRICATED, AND REPLA CED FITTING IAW DWG 3642974 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100112 19990521 00112 WP 1999 5 21 UPS99829587 1 19990427 A 5320 9754002206 FITTING DOUG DC8 DC873F 302199F WP BS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2 FS 340 BETWEEN LONGERON 36 AND 34L, THE FRAME FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED , AND REPLACED FITTING IAW DHC SK880-410 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999052100113 19990521 00113 EU 1999 5 21 QXEA9900464 1 19990305 A 4940 INNITOR FOKKER F28 F28MK4000 4990810 EU APU INOPERATIVE A QXEA H DEACTIVATE SYST/CIRCUITS A J FLAME/FIRE WARNING INDICATION LD LANDING 1 NM 09 478US 27328 372 11227 BIL - DURING LANDING ROLL, BIL TOWER REPORTED FLAMES COMING FROM APU EXHAUST. FIRST OFFICER NOTICED APU TGT 650 DEGRESS AND INCREASING. SHUT DOWN APU. MX DEFERED THE APU. THE FOLLOWING DAY GEG MX GROUND RAN, FOUND AFTER APU WARMED UP IT HAD LOW OIL PRESSURE AND WOULD NOT START. CONTINUED MEL. ON 3/10/99 IN BOI, REPLACED APU. OPS CHECK GOOD. A/C RETUR NED TO SERVICE. THE APU WAS BOROSCOPED AND THE COMBUSTION LINER AND FUEL NOZZLE WERE INSPECTED WITH NO FINDINGS. THIS UNIT WAS DETERMINED TO HAVE A BAD IGNITOR PLUG WHICH WAS REPLACED. IT WAS RUN NUMEROUS TIMES WITHOUT INCIDENT AND HAS B EEN RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999052100114 19990521 00114 EU 1999 5 21 QXEA9901017 1 19990511 A 3350 5515800106 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 SEA - CEILING EXIT SIGN AFT OF MAIN CABIN DOOR NOT ILLUMINATING. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A20EU 1999052100115 19990521 00115 EU 1999 5 21 QXEA9901018 1 19990511 A 4910 38075412 APU FOKKER F28 F28MK4000 4990810 EU APU COMPT INOPERATIVE A QXEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 486US 28080 3795 11237 PDX - LAVATORY SMOKE DETECTOR WENT OFF IN FLIGHT. AIRCRAFT RETURNED TO FIELD. FOUND EVIDENCE OF OIL IN APU DUCT. REMO VED AND REPLACED APU AND COMPLIED WITH THE BLEED AIR SYSTEM BLOWOUT MAINTENANCE TASK CARD. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999052100116 19990521 00116 NM 1999 5 21 99FDEA00178 1 19990513 A 2613 OVERHEAT LOOP BOEING 727 72721C 138400M NM LWR AFT BODY INOPERATIVE A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING UK UNKNOWN 1 SO 25 144FE 19137 99-112 - LWR AFT BODY LIGHT ILLUM. LIGHT EXTINGUISH WHEN RT PACK AND RT BLD TURN OFF. REMOVED AND REPLACED LOOP PER MM 26-14-001-4. OPER CK NORM. 2 L 7 3 4F A3WE 1999052100117 19990521 00117 NM 1999 5 21 99FDEA00179 1 19990514 A 2613 304306B0117 HOSE BOEING 727 72721C 138400M NM AFT AIRSTAIRS LEAKS A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 144FE 19137 99-113 - LWR AFT BODY O/H LIGHT ILLUM. LIGHT WENT OUT AFTER CLOSE NR 1 BLD AND BEFORE TURN OFF NR 1 PACK. 3RD TIME WRI TTEN UP. REMOVED AND REPLACED SENSE LINE. OPER AND LEAK CK NORM. 2 L 7 3 4F A3WE 1999052100118 19990521 00118 NM 1999 5 21 99FDEA00180 1 19990514 A 2613 WIRE BOEING 727 727233 138408A NM LWR AFT BODY OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 258FE 20940 LWR AFT BODY O/H LIGHT. TEST SYS OK PER RED TABS CLOSE BLD. *S/D* REPOSITIONED WIRE REF LOOP POS 26-14-1 PG 203. REM OVED AND REPLACED MODULATING SHUT OFF VALVE PER MM 36-12-042-4. LEAK CK OK. 2 L 7 3 4F RT A3WE 1999052100119 19990521 00119 WP 1999 5 21 ABXA9900366 1 19990512 A 5250 AR2529B1GR41 HANDLE DOUG DC8 DC862 3021970 WP COCKPIT DOOR BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 COCKPIT DOOR HANDLE BROKEN, WOULD NOT OPEN FROM AFT SIDE. REPLACED COCKPIT DOOR HANDLE IAW DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1999052100120 19990521 00120 WP 1999 5 21 ABXA9900367 1 19990510 A 5610 5613217507 WINDOW DOUG DC8 DC863 302198A WP LT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 819AX 45927 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN ALL THE WAY. CLEANED DEBRIS FROM TRACK AND LUBED CLEARVIEW WINDOW. ROLLERS O PS CHECKED OK IAW DC-8 SMM 56-10-3. 2 L 7 4 4F 4A25 1999052100121 19990521 00121 WP 1999 5 21 MWEA99281 1 19990512 A 3397 WIRE DOUG DC9 DC932 3022066 WP TAIL COMPARTMENT BROKEN A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 205ME 47601 THE OVERHEAD EMERGENCY LIGHTS ABOVE TAIL EVACUATION SLIDE ARE VERY DIM. MAINTENANCE REMOVED AND REPLACED TERMINALS AND REPAIRED WIRES. 2 L 7 2 4F A6WE 1999052100122 19990521 00122 WP 1999 5 21 MWEA99282 1 19990513 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 205ME 47601 THE FORWARD GALLEY AREA AISL AND ENTRY WAY OVERHEAD EMERGENCY LIGHTS ARE VERY DIM. MAINTENANCE REMOVED AND REPLACED EME RGENCY LIGHTS BATTERY PACKS. 2 L 7 2 4F A6WE 1999052100123 19990521 00123 WP 1999 5 21 MWEA99285 1 19990512 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT & RT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 205ME 47601 THE LEFT AND RIGHT NACELLE EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1999052100124 19990521 00124 NM 1999 5 21 MWEA99283 1 19990512 A 5330 59360229 SKIN DOUG MD88 MD88 3023688 NM BS 1084 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 803ME 48029 FOUND PREVIOUS REPAIR ON SKIN AT STATION 1084 LONGERON 29R AND 29L. MAINTENANCEC FABRICATED AND INSTALLED DOUBLER REPAI R. 2 L 7 2 4F RT A6WE 1999052100125 19990521 00125 NM 1999 5 21 MWEA99284 1 19990512 A 5320 59568791 WEB DOUG MD88 MD88 3023688 NM BS 207 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FOUND CRACKED WEB AT STATION 207 BETWEEN L14-15. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 1999052100126 19990521 00126 NM 1999 5 21 MWEA99286 1 19990512 A 5754 59362844 SKIN DOUG MD88 MD88 3023688 NM RT TE FLAP OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 THE RIGHT SLAT INBOARD LEADING EDGE SKIN HAS A BLENDOUT EXCEEDING LIMITS. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999052100149 19990521 00149 NM 1999 5 21 SWAA990848 1 19990509 A 5320 141A880 POST BOEING 737 7373H4 1384600 NM RT COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND APPROX A .25 INCH LONG CRACK ON UPPER END OF RT OUTBD SLIDING WINDOW POST. REPAIRED POST PER SRM. 2 L 7 2 4F RT A16WE 1999052100150 19990521 00150 NM 1999 5 21 SWAA990849 1 19990509 A 5312 963820 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 T-CHORD CRACKED AT LBL 5.7 , WL 184. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999052100151 19990521 00151 1999 5 21 SWAA990850 4 19990509 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED BC3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE STRAP DETERIORATED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100152 19990521 00152 1999 5 21 SWAA990851 4 19990510 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM PAX DOOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EVACUATION SLIDE SHOWS LOW PSI. REMOVED AND REPLACEDR SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100153 19990521 00153 NM 1999 5 21 SWAA990852 1 19990510 A 3350 079123 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 EMERGENCY EXIT TRACK LIGHT WIRING EXPOSED ON AFT SECTION. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999052100154 19990521 00154 NM 1999 5 21 SWAA990853 1 19990510 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 500C-500D, STRINGER 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999052100155 19990521 00155 NM 1999 5 21 SWAA990854 1 19990510 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 400 & 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND 2 EA FRAMES CRACKED BETWEEN STRINGERS 8L-9L, BS 400, AND BS 440. REPAIRED FRAMES PER ER 99-5337. 2 L 7 2 4F RT A16WE 1999052100156 19990521 00156 NM 1999 5 21 SWAA990855 1 19990510 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 400, 440, 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND 3 EA FRAMES CRACKED BETWEEN STRINGERS 8R-9R, BS 400, BS 440, AND BS 480. REPAIRED FRAM ES PER ER 99-5337 AND SRM. 2 L 7 2 4F RT A16WE 1999052100157 19990521 00157 NM 1999 5 21 SWAA990856 1 19990510 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM BS 787, 827, 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND 3 EA FRAMES CRACKED BETWEEN STRINGERS 8L-9L, BS 787, BS 827, AND BS 867. REPAIRED FRAME S PER ER 99-5337. 2 L 7 2 4F RT A16WE 1999052100158 19990521 00158 NM 1999 5 21 SWAA990857 1 19990510 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM BS 787,872, 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND 3 EA FRAMES CRACKED BETWEEN STRINGERS 8R-9R, BS 787, BS 827, AND BS 867. REPAIRED FRAME S PER ER 99-5337. 2 L 7 2 4F RT A16WE 1999052100159 19990521 00159 NM 1999 5 21 SWAA990858 1 19990511 A 5712 6545445 RIB BOEING 737 7373H4 1384600 NM WS 135.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND CRACK ON THE RT WING RIB LOWER CHORD AT RADIUS, BETWEEN STRINGERS 2 AND 3, STA 135.5. R EPAIRED RIB PER ER 99-5318. 2 L 7 2 4F RT A16WE 1999052100160 19990521 00160 NM 1999 5 21 SWAA990859 1 19990511 A 5711 6545321 SPAR BOEING 737 7373H4 1384600 NM WS 225 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND CRACK ON THE LT WING REAR SPAR UPPER CHORD AT FASTENER HOLE, STA 225. REPAIRED SPAR PER ER 99-5310. 2 L 7 2 4F RT A16WE 1999052100161 19990521 00161 NM 1999 5 21 SWAA990860 1 19990512 A 2720 450801 PCU BOEING 737 7373H4 1384600 NM RUDDER MALFUNCTIONED A SWAA O OTHER O OTHER CL CLIMB 1 SW 07 645SW 28330 DURING CLIMB, 20000 FEET, 295 KTS, B AUTOPILOT IN USE. AIRCRAFT WAS IN SMOOTH AIR WHEN A SHORT KICK WAS EXPERIENCE. RU DDER KICK WINGS REMAINED LEVEL AT ALL TIMES. NO RUDDER INPUT BY PILOT WAS NOTED. REMOVED AND REPLACED RUDDER PCU ENGAG E SOLENOID PER MM. 2 L 7 2 4F RT A16WE 1999052100162 19990521 00162 NM 1999 5 21 SWAA990845 1 19990509 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 AFT SERVICE DOOR ESCAPE SLIDE PRESS GAUGE NOT VISIBLE. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F A16WE 1999052100163 19990521 00163 1999 5 21 SWAA990846 4 19990509 A 2565 D31591 SLIDE BOEING 737 7373Q8 1384670 NM PAX DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 FWD ENTRY DOOR GIRT VELCRO TORN ON ESCAPE SLIDE ASSY. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100164 19990521 00164 NE 1999 5 21 SWAA990847 2 19990509 A 7320 1853M56P06 HMU BOEING 737 7377H4 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE MALFUNCTIONED A SWAA K NONE E VIBRATION/BUFFET CL CLIMB 1 SW 07 708SW 27842 874174 TRIED TO SET CLIMB POWER, (CDU N1 LIMIT 99.5 PERCENT) NR 1 ENG GOT A STRONG AIRFRAME VIBRATION ANYTIME PWR WAS ADVANCED PAST 93 PERCENT N1, NO MOVEMENT IN EITHER VIBRATION GAUGE. INSPECTED AIRCRAFT, AND NO DEFECTS NOTED. REMOVED AND REPLA CED HMU, LKS AND OPS CHECKED GOOD PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999052100165 19990521 00165 NM 1999 5 21 SWAA990824 1 19990508 A 2560 6557463 HOOK BOEING 737 7373H4 1384600 NM PAX DR GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 AFT ENTRY DOOR EMERGENCY EVACUATION SLIDE GIRT BAR LATCH HOOK HAS BROKEN SCREW. REMOVED AND REPLACED LATCH HOOK ASSY PE R MM. 2 L 7 2 4F RT A16WE 1999052100166 19990521 00166 NM 1999 5 21 SWAA990825 1 19990508 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 FLOOR TRACK EMERGENCY LIGHTING COVER MISSING AT OVERWING EXIT. REMOVED AND REPLACED FLOOR TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999052100167 19990521 00167 NM 1999 5 21 SWAA990826 1 19990507 A 3260 6573762 SWITCH BOEING 737 7373H4 1384600 NM NLG DIRTY A SWAA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 301SW 22941 RED NOSE LANDING GEAR LIGHT ILLUMINATED AND STAYED ON AFTER GEAR RETRACTION. LANDING GEAR CYCLED TO OFF/DOWN/UP. LIGHT EXTINGUISHED AFTER SECOND RETRACTION. NOISE AND VIBRATION ACCOMPANIED RED LIGHT. INSPECTED NOSE GEAR, CLEANED NOSE GE AR POSITION SWITCHES. 2 L 7 2 4F RT A16WE 1999052100168 19990521 00168 NM 1999 5 21 SWAA990827 1 19990507 A 2612 6553874 FIRE DETECTOR BOEING 737 7373H4 1384600 NM CARGO COMPT MALFUNCTIONED A SWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 322SW 23343 AIR TURNBACK, DURING CLIMB, BELL INDICATION OF FIRE IN AFT CARGO COMPT. DISCHARGED BOTH BOTTLES. LIGHT EXTINGUISHED AT GATE RETURN. INSPECTED AFT CARGO BIN, NO EVIDENCE OF FIRE OR EXCESSIVE HEAT. DEACTIVATED FIRE DETECTION SYSTEM PER SI 575, OK FOR CONTINUE. 2 L 7 2 4F RT A16WE 1999052100169 19990521 00169 NM 1999 5 21 SWAA990828 1 19990507 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 602SW 27953 EMERGENCY EXIT SLIDE AT MAIN ENTRY DOOR CAME LOOSE FROM MOUNTING BRACKET. SECURED MOUNTING BRACKET AND REPOSITIONED SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100170 19990521 00170 NM 1999 5 21 SWAA990829 1 19990507 A 2131 6973627 CONTROLLER BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 640SW 27713 AIR DIVERSION, LEVEL AT 35000 FEET, ENGINE AND WING ANTI-ICE ON, THE ALT HORN SOUNDED. CABIN ALT PASSING 10,000 FEET CL IMBING 1000 FPM. OUTFLOW VALVE FULLY CLOSED WITH NO WARNING LIGHTS ILLUMINATED. BEGAN EMERGENCY DESCENT, CYCLED WING A ND ENG ANTI-ICE. 2 L 7 2 4F RT A16WE 1999052100171 19990521 00171 NM 1999 5 21 SWAA990830 1 19990509 A 2910 6937317 MODULE BOEING 737 7373H4 1384600 NM A HYD SYSTEM INOPERATIVE A SWAA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 SW 07 313SW 23335 LOSS OF 'A' SYSTEM HYDRAULICS AFTER TAKEOFF. REMOVED AND REPLACED 'A' SYS HYD MODULE AND BOTH CASE DRAIN FILTERS, SYSTE M OPS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 1999052100172 19990521 00172 NM 1999 5 21 SWAA990831 1 19990507 A 3350 079123 COVER BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 701GS 27836 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING COVER LOOSE AND MISSING LENS. REFASTENED COVER AND REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999052100173 19990521 00173 1999 5 21 SWAA990832 4 19990507 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM GALLEY DOOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY DOOR EVACUATION SLIDE GAUGE READING BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100174 19990521 00174 NM 1999 5 21 SWAA990833 1 19990507 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND BS 360 FRAME CRACKED, BETWEEN STRINGERS 14R-15R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999052100175 19990521 00175 NM 1999 5 21 SWAA990834 1 19990507 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER AT BS 360, STR 14L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999052100176 19990521 00176 NM 1999 5 21 SWAA990835 1 19990507 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND CORROSION AT FASTENER HOLE ON FLOORBEAM, BS 967, RBL 27. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999052100177 19990521 00177 NM 1999 5 21 SWAA990836 1 19990507 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 559 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND BS 559, RT FRAME CRACKED AT RBL 65. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999052100178 19990521 00178 NM 1999 5 21 SWAA990837 1 19990507 A 5315 6516323 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM, BS 328, RBL 57. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999052100179 19990521 00179 NM 1999 5 21 SWAA990838 1 19990507 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM ROW 7 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 327SW 23691 EMERGENCY LIGHT LENS MISSING FROM OVERHEAD BIN BULLNOSE AT ROW 7 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 1999052100180 19990521 00180 NE 1999 5 21 SWAA990839 2 19990511 A 7532 7064004 BLEED VALVE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 371SW 26598 ABORTED TAKEOFF, NR 2 ENGINE SLOW TO ACCELERATE, MAX N1 WAS 76 PERCENT TAKEOFF ABORTED AT 90 KNOTS. REMOVED AND REPLACE D VARIABLE BLEED VALVE MOTOR AND MASTER BLEED VALVE (P/N 10042AV) PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999052100181 19990521 00181 NM 1999 5 21 SWAA990840 1 19990511 A 2560 D31354 SLIDE BOEING 737 7372T4 1384492 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 AFT SERVICE DOOR ESCAPE SLIDE GAUGE OUT VIEW. REPOSITIONED SLIDE ASSY AS REQUIRED PER MM. 2 L 7 2 4F A16WE 1999052100182 19990521 00182 NM 1999 5 21 SWAA990842 1 19990508 A 3350 65C27095 BATTERY CHARGER BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 706SW 28740 DURING SCHEDULED A2 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999052100183 19990521 00183 NM 1999 5 21 SWAA990843 1 19990511 A 3230 65448105 ACTUATOR BOEING 737 7373T5 NM RT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 694SW 23061 AIR TURNBACK, CLIMBING AT 12000 FT, WITH GEAR HANDLE IN OFF POSITION, RT MAIN GEAR EXTENDED, BOTH RED AND GREEN LIGHTS O N, CYCLED GEAR, WITH GEAR DOWN HAD THREE GREEN LIGHTS. REMOVED AND REPLACED UPLOCK ACTUATOR, LEAK AND OPS CKECKED GOOD. 2 L 7 2 4F RT A16WE 1999052100184 19990521 00184 NM 1999 5 21 SWAA990844 1 19990510 A 2560 D31354 SLIDE BOEING 737 7375H4 138449D NM PASSENGER DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 FWD SERVICE DOOR EVACUATION SLIDE DROPPED OUT OF HOLDER. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100185 19990521 00185 NM 1999 5 21 SWAA990811 1 19990505 A 5610 5893543130 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT LEAKING A SWAA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 07 388SW 26591 AIR TURNBACK, AFTER REMOVED AND REPLACED NR 1 F/O WINDOW, TEMPORARY SPEED TAPE CAME LOOSE INFLIGHT (SPEED TAPE OK'D PER MX NOTE TX NR 23483). CLEANED SEALANT, RESEALED AND CURED PER MM. 2 L 7 2 4F RT A16WE 1999052100186 19990521 00186 NM 1999 5 21 SWAA990812 1 19990506 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 440-460 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING WALK AROUND CHECK, FOUND A 4 INCH LONG CRACK AT FUSELAGE EXTERNAL SKIN, APPORX BS 440-460, STRINGER 10R. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999052100187 19990521 00187 NM 1999 5 21 SWAA990813 1 19990505 A 5312 963820 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/2D CHECK, FOUND LT SIDE CHORD AT BS 178 BULKHEAD CRACKED, LBL 26. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999052100188 19990521 00188 NM 1999 5 21 SWAA990814 1 19990505 A 5311 6546804 FRAME BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FRAME AT BS 1016, WL 192, RT SIDE. REPAIRED FRAME PER EO 99-532P. 2 L 7 2 4F RT A16WE 1999052100189 19990521 00189 NM 1999 5 21 SWAA990815 1 19990505 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 987, LBL 40 - 43, INSIDE CABIN. REPAIRED BEAM PER EO 99-5 313. 2 L 7 2 4F RT A16WE 1999052100190 19990521 00190 NM 1999 5 21 SWAA990816 1 19990505 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 771 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, AFT CARGO AREA, BS 771, LBL 12 - RBL2.5. REPAIRED BEAM PER S WA RA NR 1-A53-2021. 2 L 7 2 4F RT A16WE 1999052100191 19990521 00191 NM 1999 5 21 SWAA990817 1 19990505 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 730 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, AFT CARGO AREA, BS 730, RBL 3 - RBL 8. REPAIRED BEAM PER SWA RA NR 1-A53-2021. 2 L 7 2 4F RT A16WE 1999052100192 19990521 00192 NM 1999 5 21 SWAA990818 1 19990505 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, AFT CARGO AREA, BS 860, LBL 17. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999052100193 19990521 00193 NM 1999 5 21 SWAA990820 1 19990506 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND 2 CENTER EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F A16WE 1999052100194 19990521 00194 NM 1999 5 21 SWAA990821 1 19990506 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND 3 EACH STRINGER CLIPS CRACKED AT BS 277, WL 254, 250, AND, 223 RT SIDE. REMOVED AND REP LACED CLIPS PER SRM. 2 L 7 2 4F RT A16WE 1999052100195 19990521 00195 NM 1999 5 21 SWAA990822 1 19990506 A 5313 6852988 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D CHECK, FOUND 2 EACH STRINGER SPLICES CRACKED AT BS 907, STRINGER 4L, AND STRINGER 4R. REPAIRED STRIN GER PER SRM. 2 L 7 2 4F RT A16WE 1999052100196 19990521 00196 NM 1999 5 21 SWAA990823 1 19990506 A 2560 D31354 SLIDE BOEING 737 7373Y0 1384671 NM PASSENGER DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 LT FWD EMERGENCY ESCAPE SLIDE CAME OUT OF THE HOLDER. INSPECTED AND RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100197 19990521 00197 NM 1999 5 21 SWAA990864 1 19990513 A 5315 6546804 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM, BS 328, RBL 37 INSIDE CABIN. REPAIRED BEAM PER SRM. 2 L 7 2 4F A16WE 1999052100198 19990521 00198 NM 1999 5 21 SWAA990865 1 19990513 A 2782 65446579 ACTUATOR BOEING 737 7372H4 138448C NM NR 4 LE SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 60SW 21812 AIR TURNBACK, NR 4 LE SLAT WOULD NOT RETRACT. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 1999052100199 19990521 00199 NM 1999 5 21 SWAA990866 1 19990512 A 5315 6546804 FLOOBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM, BS 986, LBL41-RBL33. REPAIRED BEAM PER SRM, A ND SWA RA NR 1-353-2079. 2 L 7 2 4F RT A16WE 1999052100200 19990521 00200 NM 1999 5 21 SWAA990867 1 19990512 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INNER SIDE OF BELTFRAME AT BS 616, STRINGER 17L. REPAIRED FRAME PER SWA RA N R 1-353-2078. 2 L 7 2 4F RT A16WE 1999052100201 19990521 00201 NM 1999 5 21 SWAA990868 1 19990513 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 15 DETACHED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 EMERGENCY EXIT TRACK LIGHTING PULLED UP AT ROW 15. REPOSITIONED TRACK PER MM. 2 L 7 2 4F RT A16WE 1999052100202 19990521 00202 NM 1999 5 21 SWAA990869 1 19990513 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM PASSENGER DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE GAUGE OUT OF VIEW. REPOSITIONED GAUGE PER MM. 2 L 7 2 4F A16WE 1999052100203 19990521 00203 NM 1999 5 21 SWAA990870 1 19990513 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM LT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED C4 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999052100204 19990521 00204 NM 1999 5 21 SWAA990871 1 19990513 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM SERVICE DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999052100205 19990521 00205 NM 1999 5 21 SWAA990872 1 19990513 A 3350 101073 COVER BOEING 737 7373H4 1384600 NM EMER EXIT DOOR MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 1999052100206 19990521 00206 NM 1999 5 21 SWAA990861 1 19990512 A 5320 65C27314 CLIP BOEING 737 7372T4 1384492 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND 3 STRINGER CLIPS CRACKED AT BS 520, STRINGERS 19L, 19R, AND AT BS 1138, STRINGER 3R. RE MOVED AND REPLACED CLIPS PER SRM. 2 L 7 2 4F A16WE 1999052100207 19990521 00207 NM 1999 5 21 SWAA990862 1 19990512 A 5312 6516300 BULKHEAD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 1O.7, WL 234. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999052100208 19990521 00208 NM 1999 5 21 SWAA990863 1 19990513 A 5311 BAC1490 FRAME BOEING 737 7372T4 1384492 NM BS 956 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND UPPER STUB FRAME CRACKED AT BS 956 RBL 61, WL 262. REMOVED AND REPLACED STUB FRAME PER SRM. 2 L 7 2 4F A16WE 1999052100209 19990521 00209 NM 1999 5 21 SWAA990873 1 19990513 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM ROW 21 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHTS INOP AT ROW 21. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052100210 19990521 00210 NM 1999 5 21 SWAA990874 1 19990513 A 3350 079123 LENS BOEING 737 7375H4 138449D NM ROW 7 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT LENS MISSING AT ROW 7. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 1999052100211 19990521 00211 NM 1999 5 21 TWAA9907201 1 19990514 A 3350 1317 BULB BOEING 767 767231 1385131 NM GALLEY FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 602TW 22565 THE AFT GALLEY CEILING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 2-26-99 LAX. 2 L 7 2 4F RT A1NM 1999052100212 19990521 00212 NM 1999 5 21 TWAA9907202 1 19990514 A 3350 1317 BULB BOEING 767 767231 1385131 NM L4 DOOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 602TW 22565 FOUND EXTERNAL EMERGENCY LIGHT INOPERATIVE AT THE NUMBER 4 DOOR ON LT SIDE OF FUSELAGE. REPLACED THE BULB. CHECK-C 2-2 6-99 LAX. 2 L 7 2 4F RT A1NM 1999052100213 19990521 00213 WP 1999 5 21 TWAA9907203 1 19990514 A 3350 6011779LB POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 405EA 47688 THE CABIN EGRESS LIGHTING IN FWD CABIN CAME ON INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 3-30-99 STL. 2 L 7 2 4F RT A6WE 1999052100214 19990521 00214 WP 1999 5 21 TWAA9907204 1 19990516 A 3397 0105607301 WIRE DOUG DC9 DC983 3022083 WP ROW 11-26 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9405T 53141 ON PREFLIGHT FOUND BROKEN EGRESS LIGHT LENS AND DAMAGED EGRESS WIRING AT SEAT ROW 11. REPLACED COVERS AND REPAIRED 3 WI RE SEGMENTS BETWEEN ROWS 11 AND 26. CHECK-C 11-11-98 MCI. 2 L 7 2 4F RT A6WE 1999052100215 19990521 00215 WP 1999 5 21 AT9900371 1 19990510 A 5315 1A459321 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 196 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO, FL. FOUND THE CABIN FLOORBEAM UPPER FLANGE CORRODED AT BS 196 BL 0. REMOVED FLOORBEAM, CUT, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED NEW FLOORBEAM IAW DC9 SRM 53-01 FIG 1 SHEET 3, 51-30-2, 51-10-3, 53-13-1 AND 53-10-4. 2 L 7 2 4F A6WE 1999052100216 19990521 00216 NM 1999 5 21 AT9900372 1 19990428 A 5312 BULKHEAD ANGLE BOEING 737 7372L9 1384497 NM BS 947 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO, FL. FOUND THE AFT CARGO BULKHEAD UPPER FRAME L ANGLE AT BS 947 CORRODED. REMOVED DAMAGE SECTION, FABRICATED A REPLACEMENT AND ANGLE, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-40-3, 51-30-2, 53-10-1 AND 5 1-10-6. 2 L 7 2 4F RT A16WE 1999052100217 19990521 00217 NM 1999 5 21 AT9900373 1 19990502 A 7110 1A476442 DOUBLER BOEING 737 7372L9 1384497 NM NR1 ENGINE COWL CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL. FOUND CORROSION UNDER THE EXTERNAL TUBE PANEL NR 5102 ENGINE COWLING. R EMOVED DOUBLER, FABRICATED TWO NEW DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED DOUBLERS IAW B737 SRM 51-4 0-2, 51-10-2, AND 51-21-31. DOUBLER (P/N 1A-476-44-1). 2 L 7 2 4F RT A16WE 1999052100218 19990521 00218 NM 1999 5 21 AT9900374 1 19990506 A 5730 SKIN BOEING 737 7372L9 1384497 NM RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION BLISTER ON SURFACE AFT EDGE OF RIGHT WING INBOARD LEADING EDGE INBOARD OF ENGINE CONTROL ACCESS PANEL. REMOVED HYDRAULIC LINES AND PANEL FOR ACCESS TO REPAIR. FABRICATED REPAIR , DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR IAW B737 51-30-2, 51-21-31, AND 51-30-4. LEAKED CHECKED COMP LETED WITH NO DEFECTS NOTED IAW MM 29-11-0. 2 L 7 2 4F RT A16WE 1999052100219 19990521 00219 WP 1999 5 21 AT9900375 1 19990512 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD FLOOR PANEL NR 4691 AT BS 160 TO 200 BL 0-45L CORRODED. FABRICATED NEW FLOOR PANEL, FIT, DRILLED AND INSTALLED NEW SKIN ON HAT CHANNELS AND REINSTALLED FLOOR PANEL IAW DC9 SRM 53-21-0, 51-10-2, AND 53-31-0. 2 L 7 2 4F A6WE 1999052100220 19990521 00220 WP 1999 5 21 AT9900376 1 19990513 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND PASSENGER CABIN FLOORBEAM CHAFED AND CORRODED AT BS 965 BL-30L. FOR MED, FIT, TRIMMED, DRILLED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 53-05 FIG 20A. 2 L 7 2 4F A6WE 1999052100221 19990521 00221 WP 1999 5 21 AT9900377 1 19990516 A 3350 41B004AD0763 BATTERY DOUG DC9 DC932 3022066 WP ROW 20 DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 825AT 47319 THREE OVERHEAD EMEGENCY LIGHTS INOPERATIVE, TWO IN ROW 20 AND ONE IN BETWEEN ROWS 19 AND 20. REMOVED AND REPLACED BATTE RIES IAW MM 33-53-0. 2 L 7 2 4F A6WE 1999052100222 19990521 00222 WP 1999 5 21 AT9900378 1 19990516 A 3350 41B004AD0763 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 825AT 47319 FOUND BOTH AFT OVERHEAD EXIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW MM 33-53-0. 2 L 7 2 4F A6WE 1999052100223 19990521 00223 NM 1999 5 21 AT9900379 1 19990516 A 3350 1000679 BATTERIES BOEING 737 737222 1384473 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 468AT 19074 LEFT HAND OVERWING HATCH EMERGENCY LIGHT ABOVE DOOR HAS DEAD BATTERIES. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY I AW B737 MM 33-51-31. OPS CHECKED OK. 2 L 7 2 4F A16WE 1999052100224 19990521 00224 NM 1999 5 21 UPS99229605 1 19990514 A 7312 DUCT BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE BROKEN A IPXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 01 208UP 21701 687439 INSPECTION TYPE:N/A, FIRE WARNING ON NR 1 ENGINE AFTER TAKEOFF ON CLIMBOUT. SECURED ENGINE IAW PROCEDURE. FIRE WARNING LIGHT/BELL WENT OUT WHEN POWER REDUCED. FOUND FUEL DEICING HEATER DUCT BROKEN. REMOVED AND REPLACED MANIFOLD AND RAN ENGINES. OPS CK AND LK CK GOOD PER MM 71-00-00. 2 L 7 3 4F 4 F A3WE E2EA 1999052100225 19990521 00225 NM 1999 5 21 UPS99229606 1 19990513 A 5753 65192497 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI (CORROSION C57-581-06.00-04) ON NR 6 FLAP TRACK AT SPOILER BEAM PAD. CORROSION ON SPOILER BEAM PAD I S OUT OF LIMITS IAW SRM 57-40-02. FLAP TRACK WAS REPLACED ON CID 888728. 2 L 7 3 4F A3WE 1999052100226 19990521 00226 NM 1999 5 21 UPS99229607 1 19990514 A 5210 AIRSTAIR BOEING 727 72731C 1384011 NM AFT FUSELAGE OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, AFT AIRSTAIR LIGHT ILLUMINATED IN FLT. VISUAL INSPECTION OF STAIR AREA SHOWED FLEXING OF DOOR ARMS INDICATIVE OF UNLOCK CONDITION. DOOR LIGHT WENT OUT WITH INITAIL FLAP SELECTION TO 2 DEGREES (POSSIBLE AIRFLOW CHANGE O N DOOR/STAIR AREA). FOUND AFT AIRSTAIR POSITION PROXIMITY SWITCH TO BE OUT OF ADJUSTMENT. ADJUSTED SWITCH PER MM 52-70 -01 PARA E PAGE 508. FUNCTIONALLY TESTED PER MM 52-70-01 PARA 2 PG 509, NO FURTHER DISCREPANCIES NOTED. 2 L 7 3 4F A3WE 1999052100227 19990521 00227 NM 1999 5 21 UPS99229608 1 19990514 A 2133 OUT FLOW VALVE BOEING 727 72731C 1384011 NM RIGHT STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:SI, AIR TURNBACK AT 1945UTC DUE TO UNSATISFACTORY AIRCRAFT PRESSURIZATION. WHEN CLIMB THRUST SET, CARGO HEAT O'FLOW VALVE CLOSED, FULL MANUAL INCRASE ON MANUAL CONTROLLER. AIRCRAFT WAS ONLY ABLE TO MAINTAIN A CABIN ALTITUD E OF 8,000 AND DIFFERENTIAL OF 7 PSID. HAD FLIGHT CONTINUED, CABIN ALTITUDE WOULD HAVE EXCEEDED 10,000 2-3MTS. TROUBLE SHOT SYSTEM PER MM, FOUND RT OUTFLOW VALVE TO BE STUCK OPEN DUE TO INSULATION BLANKET STUCK IN VALVE. REMOVED BLANKET A ND PERFORMED PRESSURE CONTROL SYSTEM TEST PER MM 21-30-01. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1999052100228 19990521 00228 NM 1999 5 21 UPS99229610 1 19990513 A 3260 CONNECTOR BOEING 727 72731C 1384011 NM NLG DIRTY A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 925UP 19230 INSPECTION TYPE:SI, AIR TURNBACK AT 0100 UTC UPON GEAR RETRACTION, GEAR LEVER WOULD NOT MOVE PAST OFF POSITION. ALSO, I /B ANTISKID RELEASE REMAINED ON IN FLIGHT WITH GEAR HANDLE IN DOWN/IN POSITION. REMOVED, CLEANED CONNECTOR AND RE-INSTA LLED ANTISKID CONTROL BOX. REMOVED AND REPLACED NLG SAFETY SWITCH PER 727 MM 32-09-211. PERFORMED OPERATION CHECK OF A NTISKID SYS CHECK GOOD PER 32-42-00. FUNCTIONAL TESTED GEAR SAFETY SENSOR (SWITCH) GOOD PER 32-21-11. ADJUSTED AND RIG GED NLG PISTON POSITION CABLES PER 727 MM 32-51-00. 2 L 7 3 4F A3WE 1999052100229 19990521 00229 NM 1999 5 21 UPS99229611 1 19990517 A 3610 CLAMP BOEING 727 727247 138408F NM NR 3 ENGINE LOOSE A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 208UP 21701 INSPECTION TYPE:N/A, NR 3 STRUT OVERHEAT LIGHT LIGHT WENT OUT AFTER 15-20 SECONDS. UNABLE TO COMPLETE CHECK LIST DUE TO NR 1 ENGINE SHUTDOWN AND CLOSE PROX TO LANDING. NR 3 PRECOOLER CLAMP LEAKING. TIGHTENED CLAMP, RAN ENGINE NO DEFECTS PER M/M 36-10-10 & 71-00-00. 2 L 7 3 4F A3WE 1999052100230 19990521 00230 WP 1999 5 21 UPS99829588 1 19990411 A 5320 J0602969 CUSP DOUG DC8 DC873F 302199F WP BS 1320-1365 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, RT CUSP FS 1320 TO 1330 & 1340 TO 1365 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICAT ED AND REPLACED CUSP IAW SRM 53-2-5. 2 L 7 4 4F RT 4A25 1999052100231 19990521 00231 WP 1999 5 21 UPS99829589 1 19990420 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3 FS 1060 FRAME AT LONG 35L TO 35R IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPAIRED FRAME IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999052100232 19990521 00232 WP 1999 5 21 UPS99829590 1 19990508 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 70 FLOORBEAM AT RBL 48 IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DHC SK840-349. 2 L 7 4 4F RT 4A25 1999052100233 19990521 00233 WP 1999 5 21 UPS99829591 1 19990427 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1280-1300 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FUSELAGE SKIN AT FS 1280 TO 1300 LONG 25R TO 27R REQUIRES REPAIR. REPAIRED FUSELAGE SKIN IAW DHC SK 840-064. 2 L 7 4 4F RT 4A25 1999052100234 19990521 00234 WP 1999 5 21 UPS99829592 1 19990420 A 5320 9754949111 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 1260-1280 AT LONG 33R, THE INTERCOSTAL UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICAT ED AND REPLACED INTERCOSTAL IAW DWG 9754949 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100235 19990521 00235 WP 1999 5 21 UPS99829593 1 19990427 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1654 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FUSELAGE SKIN AND DOUBLER AT FS 1654 AND LONG 31L ARE CORRODED BEYOND LIMITS. REPAIRED SKIN AND INT ERNAL DOUBLER IAW DHC SK840-923. 2 L 7 4 4F RT 4A25 1999052100236 19990521 00236 WP 1999 5 21 UPS99829594 1 19990411 A 5320 37558451 FITTING DOUG DC8 DC873F 302199F WP BS 1150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, BATHTUB FITTING AT FS 1150 AND LONG 35R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100237 19990521 00237 WP 1999 5 21 UPS99829595 1 19990407 A 5320 J0602969 CUSP DOUG DC8 DC873F 302199F WP BS 1305 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, LT CUSP AT FS 1305 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-5 FIG 15A. 2 L 7 4 4F RT 4A25 1999052100238 19990521 00238 WP 1999 5 21 UPS99829596 1 19990407 A 5320 3754047506 FITTING DOUG DC8 DC873F 302199F WP BS 1347 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, LT FLOORBEAM TO FUSELAGE FRAME FITTING AT FS 1347 HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPL ACED FITTING IAW DWG 3754047 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999052100239 19990521 00239 WP 1999 5 21 UPS99829597 1 19990414 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FUSELAGE FRAME AT FS 1020 AND LONG 34L HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION AND REPAIRED IA W SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999052100240 19990521 00240 WP 1999 5 21 UPS99829598 1 19990405 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, SEAT TRACK RBL 48 AT FS 950 IS CORRODED AND CRACKED. REMOVED DAMAGED SEAT TRACK, FABRICATED AND REP LACED IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999052100241 19990521 00241 WP 1999 5 21 UPS99829599 1 19990406 A 5320 58903141 FITTING DOUG DC8 DC873F 302199F WP BS 55-70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 55 TO 70, LBL 60, THE 9G NET ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5890314 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999052100242 19990521 00242 WP 1999 5 21 UPS99829600 1 19990419 A 5320 37592582 FITTING DOUG DC8 DC873F 302199F WP BS 1270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, LONG 35R SPLICE AT FS 1270 IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100243 19990521 00243 WP 1999 5 21 UPS99829601 1 19990421 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 1000 FRAME AT LBL 32 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53- 2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999052100244 19990521 00244 WP 1999 5 21 UPS99829602 1 19990423 A 5320 46156291 FITTING DOUG DC8 DC873F 302199F WP BS 55 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 55, LBL 54 TO RBL 54, THE FLOOR SUPPORT FITTINGS REQUIRE REPAIR. REPAIRED DAMAGED FLOOR SUPPORT FITTINGS IAW DHC SK840-196 AND DHC SK840-172. 2 L 7 4 4F RT 4A25 1999052100245 19990521 00245 WP 1999 5 21 UPS99829603 1 19990427 A 5313 5646666501 LONGERON DOUG DC8 DC873F 302199F WP BS 1665 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, LONG 23L AT FS 1665 HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION FABRICATED AND REPLACED LONGERON I AW DWG 5646666 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052100246 19990521 00246 WP 1999 5 21 UPS99829604 1 19990405 A 5320 37540251 FITTING DOUG DC8 DC873F 302199F WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 280 AT LONG 27R, IN THE TORQUE BOX, THE SUPPORT CHANNEL ATTACH FITTING IS CRACKED AND CORRODED. R EMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999052100247 19990521 00247 NM 1999 5 21 QXEA9901019 1 19990511 A 2611 473054 DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 364PH 520 YVR- SMOKE WARNING LIGHT ILLUMINATED INTERMITTANTLY. MAINTENANCE PLACED ON MEL. MEL CLEARED BY REPLACING BOTH SMOKE DE TECTORS, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999052100248 19990521 00248 WP 1999 5 21 99FDEA00181 1 19990512 A 5753 VANE DOUG DC10 DC1030F 3023504 WP RT TE FLAP FAILED A FDEA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 SO 25 309FE 48298 BUFFET ENCOUNTERED AS FLAPS SEL TO 35 DEG EXT BUFFET INCREASED WHEN FLAPS 50 DEG EXT SEL. REMOVED AND REPLACED RT I/B A ND O/B FLAP VANE ASSY AND OPS CK NORM PER MM 27-50-03-2. 2 L 7 3 4F RT A22WE 1999052100249 19990521 00249 WP 1999 5 21 ABXA9900368 1 19990514 A 2130 5644698502 DUCT DOUG DC8 DC862 3021970 WP RIGHT RUPTURED A ABXA K NONE O OTHER CR CRUISE 1 GL 23 808AX 45954 ON LEVEL OFF AT 37,000 FEET, CABIN STARTED TO CLIMB AT 3,000 FEET PER MINUTE. COULD NOT CONTROL CABIN RATE. DESCENDED TO 24,000 FEET AND REGAINED CONTROL OF CABIN. MAINTAINED CABIN AT 9,000 FEET. HEARD LOUD NOISE BY THE RIGHT HAND CTC'S AT 37,000. OXYGEN USED IN FLIGHT. FOUND RIGHT HAND HEADER DUCT TO HEAT EXCHANGER RUPTURED. REMOVED AND REPLACED DUCT IAW DC-8 MM 21-54-1, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999052100250 19990521 00250 NM 1999 5 21 MWEA99287 1 19990514 A 2560 11320 BRACKET DOUG MD88 MD88 3023688 NM PAX DOOR SLIDE LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 701ME 49760 THE FORWARD ENTRANCE DOOR FLOOR GIRT BAR BRACKET IS LOOSE. MTC RESECURED FORWARD ENTRANCE DOOR GIRT BAR BRACKET. 2 L 7 2 4F RT A6WE 1999052100251 19990521 00251 WP 1999 5 21 MWEA99288 1 19990514 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE LOW PRESSURE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 602ME 48133 THE MAIN DOOR SLIDE PRESSURE IS NOT IN THE GREEN ARC. MTC FOUND PRESSURE LOW AND REMOVED AND REPLACED DOOR SLIDE. 2 L 7 2 4F A6WE 1999052100252 19990521 00252 WP 1999 5 21 TWAA9907301 1 19990505 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 180 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND CABIN FLOORBEAM REPAIR CRACKED 2 INCHES LONG IN UPPER CAP RADIUS AT FWD SIDE OF STA 180, LBL 15. REPLACED FLOORBEAM TEE UPPER CAP PER SRM 53-11-1, FIG 13 SHEET 1, PAGE 45 AND 47, FIG 13 SHEET 2 AND DAC DRAWI NG 9923484. INSTALLED WEB REPAIR PER SRM 53-01, FIG 2 SHEET 4. 2 L 7 2 4F A6WE 1999052100253 19990521 00253 WP 1999 5 21 TWAA9907302 1 19990512 A 2720 BRACKET DOUG DC9 DC932 3022066 WP RUDDER PEDALS CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 THE CAPTAINS RUDDER PEDAL BRACKET WAS CRACKED AT THE AFT O/B MOUNT LEG, 1.125 INCH LONG. REMOVED AND REPLACED THE RUDDE R BRACKET PER MM 27-20-12. CHECK-C 8-7-98 MCI. 2 L 7 2 4F A6WE 1999052100254 19990521 00254 NM 1999 5 21 PCAA9900012 1 19990516 A 3260 INDICATION DHAV DHC8 DHC8102 2809003 NM NLG MALFUNCTIONED A PCAA O OTHER P NO WARNING INDICATION DE DESCENT 1 EA 13 841EX 249 FLT 3904 - UPON DESCENT INTO ABE WHEN LANDING GEAR WAS SELECTED DOWN, THE NLG FAILED TO ILLUMINATE. NOSE GEAR LIGHT ILL UMINATED ON AND OFF WHEN GEAR WAS EXTENDED. MAINTENANCE INSPECTED NLG INDICATION SYSTEM, CLEANED LIGHT MODULE AND SYSTE M CHECKED OUT NORMAL. 2 H 7 2 4T RT A13NM 1999052100255 19990521 00255 NM 1999 5 21 9901666718 1 19990405 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 281 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING M CHECK, FOUND CRACK IN C3 CLOSURE FRAME ON THE MAIN DECK FS 281, LBL 45. REPAIRED CLOSURE FRAME PER EA 67-16497 7. 2 L 7 4 4F A20WE 1999052100256 19990521 00256 WP 1999 5 21 9901671147 1 19990317 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 147US 46756 DURING M CHECK, FOUND CRACK ON LOWER EDGE OF FRAME AT FS 459 LBL 45. REPAIRED PER EA 11-160402. 2 L 7 3 4F A22WE 1999052100257 19990521 00257 WP 1999 5 21 9901699607 1 19990513 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP TAIL COMPARTMENT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 607NW 47232 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999052100258 19990521 00258 WP 1999 5 21 9901709964 1 19990513 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY P ACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999052100259 19990521 00259 WP 1999 5 21 9901719152 1 19990510 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE MAINTENANCE INSPECTION, FOUND PATHWAY CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999052100260 19990521 00260 NM 1999 5 21 9901726304 1 19990511 A 2910 O RING BOEING 747 747451 1384940 NM NR 4 HYD SYST LEAKING A NWAA O OTHER K FLUID LOSS CR CRUISE 1 GL 01 664US 23819 DURING CRUISE (AMS), THE NR 4 HYDRAULIC SYSTEM LOST FLUID. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. REPL ACED THE O-RING ON THE PLUG FOR THE HYDRAULIC RESERVOIR PRESSURE FILTER MODULE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999052100261 19990521 00261 NM 1999 5 21 UPS99229619 1 19990517 A 3350 BATTERY PACK BOEING 727 72730C 1384009 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHTS ABOVE DOOR INOP, FAILED TO TEST. REMOVED UNIT FROM A/C, PUT BATTERIES ON CHARGE, REINSTALLED BATTS IN A/C AND OPS OK. 2 L 7 3 4F A3WE 1999052100262 19990521 00262 NM 1999 5 21 UPS99629615 1 19990518 A 3310 LIGHT BOEING 767 76734AF 1385212 NM LT MAP LIGHT INOPERATIVE A IPXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 313UP 27764 INSPECTION TYPE:N/A, CAPT MAP LIGHT BEGAN TO EMIT SMOKE ALONG WITH AN ELECTRICAL BURNING SMELL. FLT CREW TURNED OFF LIG HT AND REMOVED BULB. MAINTENANCE DEFERRED MAP LIGHT WITH REF TO MEL 33-11-1-1. RELAMPED, NO HELP. 2 L 7 2 4F RT A1NM 1999052100263 19990521 00263 WP 1999 5 21 UPS99829612 1 19990406 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 560-580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 560 TO 580, LBL 60, THE SEAT TRACK UPPER FLANGE LWR SURFACE HAS HEAVY EXFOLIATION CORROSION UNDER AND AROUND THE CLIP NUTS. CUT OUT DAMAGED SEAT TRACK SECTION, FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM 53-2- 3 FIG 84. 2 L 7 4 4F RT 4A25 1999052100264 19990521 00264 WP 1999 5 21 UPS99829613 1 19990511 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 1300, 1310, 1320 AND 1340, RBL 45 THE SEAT TRACK HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION, F ABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999052100265 19990521 00265 WP 1999 5 21 UPS99829614 1 19990406 A 5347 S2772660 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 275-305 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 275 TO 305, LBL 45, THE SEAT TRACK UPPER FLANGE, LWR SURFACE HAS MODERATE CORROSION AROUND THE CL IP NUTS. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999052100266 19990521 00266 WP 1999 5 21 UPS99829616 1 19990418 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT I/B SLOT VANE I/B END HAS MODERATE CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5720- 7767A. 2 L 7 4 4F RT 4A25 1999052100267 19990521 00267 WP 1999 5 21 UPS99829617 1 19990422 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, FUSELAGE EXTERNAL SKIN AT FS 1620, LONG 20L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REP AIRED IAW DHC SK880-113. 2 L 7 4 4F RT 4A25 1999052100268 19990521 00268 WP 1999 5 21 UPS99829618 1 19990427 A 5320 9754002205 ANGLE DOUG DC8 DC873F 302199F WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, NUT PLATE ANGLE HAS HEAVY CORROSION ON THE UNDERSIDE, FS 280 LONG 34L TO 34R. REMOVED, FABRICATED A ND REPLACED NUT PLATE ANGLE IAW DHC SK880-410 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999052100269 19990521 00269 WP 1999 5 21 UPS99829620 1 19990517 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:N/A, EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK IAW M/M 33-50-01, OPS CHK GOOD. (P/N 5708458-503), (S/N 1132) ON, (P/N 10382) OFF. 2 L 7 4 4F RT 4A25 1999052100270 19990521 00270 EU 1999 5 21 QXEA9901053 1 19990508 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 497US 11173 PDX- EMERGENCY LIGHTS IN CABIN OVERHEAD WILL NOT TEST. AIRCRAFT IN C-CHECK. 2 L 7 2 4F RT A20EU 1999052100271 19990521 00271 EU 1999 5 21 QXEA9901054 1 19990512 A 2170 18084932 COALESCER GARRTT 6837205 FOKKER F28 F28MK4000 4990810 EU CABIN DIRTY A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 497US 124674 11173 PDX- OIL SMELL IN COCKPIT WITH APU AIR OFF. REMOVED AND REPLACED ACM WATER SEPARATOR SOCKS. VERIFIED PROPER ACM OIL SE RVICE. GROUND RUN CHECK GOOD AT VARIOUS SETTINGS. 2 L 7 2 4F RT A20EU 1999052100272 19990521 00272 NM 1999 5 21 99UAL900172 1 19990323 A 2560 284T024210 SENSOR BOEING 284T024210 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMER EXIT SLIDE OUT OF ADJUST A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 656UA 25394 RIGHT WING SLIDE EICAS MESSAGE DISPLAYED INTERMITTENTLY AT CRUISE. *S/D* CHECKED S199 AND S219 PROXIMITY SENSORS FOR T ARGET CLEARANCES, FOUND S219 HAD EXCESSIVE GAP. SHIMMED SENSOR PER MM. REAMED SYSTEM PER MM, ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999052100273 19990521 00273 NM 1999 5 21 99UAL900265 1 19990509 A 3350 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7292U 21570 FWD GALLEY EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY AND BATTERY, OP CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1999052100274 19990521 00274 NM 1999 5 21 99UAL900266 1 19990507 A 5610 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 571UA 26681 DIVERTED TO JAX DUE TO CRACKED F/O WINDOW. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052100275 19990521 00275 NE 1999 5 21 99UAL900267 2 19990510 A 7530 STATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 29 587UA 10925 26713 726646 AFTER CLIMBOUT FROM EWR, RIGHT ENGINE WENT TO IDLE THRUST. FLT DIVERTED TO SYR. *S/D* METAL WAS FOUND IN TAILPIPE. T HE ENGINE WAS REPLACED. SHOP FINDINGS WERE A HPC STATOR FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052100276 19990521 00276 NM 1999 5 21 99UAL900268 1 19990509 A 4920 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAILED A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 557UA 26653 61758 DIVERTED TO BOI DUE TO LOSS OF APU GENERATOR. THE LEFT GENERATOR WAS LOST ON TAKEOFF. *S/D* APU SHUTDOWN WITH 'APU OI L QTY' MSG. FOUND OIL DRIPPING FROM DRAIN MAST INDICATING A CARBON SEAL DEFECTIVE. GENERATOR COULD NOT STAY ON LINE D UE TO AUTO SHUTDOWN FOR LOW OIL QUANTITY. APU WAS REPLACED. DURING SHOP VISIT, DISASSEMBLY REVEALED A DEFECTIVE CARBON SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052100277 19990521 00277 NM 1999 5 21 99UAL900269 1 19990512 A 5230 CONDUIT BOEING 287T43251 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR DISLODGED A UALA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 WP 29 645UA 25280 WHILE EN ROUTE, AIRCRAFT HAD FORWARD CARGO DOOR INDICATION LIGHT ILLUMINATE. DIVERTED JFK. OVERWEIGHT LANDING. *S/D* LARGE FORWARD CARGO DOOR ELECTRICAL CONDUIT PULLED AT LINK ARM PIVOT POINT AT FORWARD BRACKET WHEN DOOR IS CLOSING CAUS ING ELECTRICAL CONNECTOR TO DISLODGE AND GIVE EICAS INDICATIONS. REPLACED DAMAGED CONDUIT ASSEMBLY 287T4325-1. LARGE F ORWARD CARGO DOOR OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999052100278 19990521 00278 NM 1999 5 21 99UAL900270 1 19990503 A 2497 W7860000330 WIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU GEN DAMAGED A UALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 772UA 26930 APU GENERATOR DROPPED OFF LINE AT DEPARTURE. FOUND GENERATOR FEEDER CABLE DAMAGED FROM TERMINAL LUG. *S/D* THE CAUSE OF THE APU GENERATOR DROPPING OFF LINE WAS DAMAGE TO THE PHASE C WIRE (W7860-0003-3/0). THE WIRE WAS REPLACED AND THE A PU GENERATOR SYSTEM OPERATIONAL CHECKED. THE CAUSE OF THE OVERHEAT ON THE TERMINAL COULD NOT BE PRECISELY DETERMINED. C AUSES COULD INCLUDE TERMINATION METHOD FOR THE WIRE ASSEMBLY OR METHOD OF HARDWARE INSTALLATION AT THE TERMINAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999052100279 19990521 00279 NM 1999 5 21 99UAL900271 1 19990513 A 2120 SENSOR ROSEMOUNT 123CH1A BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E & E COMPT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 345UA 24249 EXHAUST FAN INOP. *S/D* EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED EQUIPMENT COOLING LOW FLOW SENSOR, OPS CHE CK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999052100280 19990521 00280 NM 1999 5 21 99UAL900272 1 19990513 A 2120 SENSOR ROSEMOUNT 123CH1A BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E & E COMPT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 323UA 23955 EQUIPMENT COOLING EXHAUST FAN INOP. *S/D* EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED EQUIPMENT COOLING LOW FL OW SENSOR, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999052100281 19990521 00281 NE 1999 5 21 99UAL900273 2 19990513 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FAILED A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 29 534UA 4437 25129 726582 RETURNED TO ORD DUE TO NR 2 ENGINE VIBRATION. *S/D* UPON ARRIVAL ORD, FOUND METAL IN TAILPIPE NR 2 ENGINE. REPLACED E NGINE. FOLLOW UP FINDINGS INDICATED THE LPT 4TH STAGE NGV FAILED DUE TO INTERNAL SULFIDATION. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052100282 19990521 00282 NM 1999 5 21 99UAL900274 1 19990514 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 15-18 DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 119UA 28812 EEL LIGHT INOP UPPER DECK FROM SEAT 15AB TO 18AB. REPLACED BATTERY, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 1999052100283 19990521 00283 NM 1999 5 21 99UAL900275 1 19990514 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE DOOR 1R DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 156UA 20105 EMERGENCY EXIT SIGNS INOP AT DOOR 1R. REPLACED BATTERY PACK, OPS OK. 2 L 7 4 4F 4 F A20WE E20EA 1999052100284 19990521 00284 WP 1999 5 21 ABXA9900369 1 19990513 A 2460 914F5674 RELAY DOUG DC9 DC931 3022065 WP COCKPIT FAILED A ABXA K NONE O OTHER CR CRUISE 1 GL 23 944AX 47550 DURING FLIGHT, CREW REPORTED ELECTRICAL/ BURNING SMELL IN COCKPIT. FOUND LEFT AUX PANEL POWER RELAY FAILED. REPLACED R ELAY IAW DC9 MM 24-20-6. 2 L 7 2 4F A6WE 1999052100285 19990521 00285 WP 1999 5 21 ABXA990371 1 19990503 A 5320 992341929 SLANT PANEL DOUG DOUG DC9 DC941 302207N WP CARGO COMPT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND LEFT SLANT PANEL CORRODED. REPLACED LEFT SLANT PANEL IAW DC9 SRM 51-30-01 AND DWG 9923419-29. 2 L 7 2 4F A6WE 1999052100286 19990521 00286 WP 1999 5 21 ABXA9900372 1 19990503 A 5230 59101577 PAN DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT DOOR OUTER PAN CRACKED. REPAIRED CRACKED IAW DC9 SRM 52-03. 2 L 7 2 4F A6WE 1999052100287 19990521 00287 WP 1999 5 21 ABXA9900373 1 19990503 A 5230 59101575 WEB DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND AFT LOWER CARGO DOOR WEB CRACKED AT AFT HINGE. REPAIRED IAW ABX REA D952-28315. 2 L 7 2 4F A6WE 1999052100288 19990521 00288 WP 1999 5 21 ABXA9900374 1 19990503 A 5320 D0489834 WEB DOUG DOUG DC9 DC941 302207N WP BS 910 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK, FOUND CUSP WEB AT STATION 910, RBL 54-44 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999052100289 19990521 00289 SO 1999 5 21 SWIA971479 1 19990509 A 3610 DRAIN EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PNEU SYST OUT OF POSITION A SWIA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 07 187SW 120037 RIGHT DUCT LEAK LIGHT CAME ON ABOUT 25 MILES OUTSIDE OF TWF. FOLLOWED QRH AND AFTER THREE MINUTES SHUT DOWN RIGHT ENGIN E. THE LIGHT WENT OUT AFTER ENGINE SHUT DOWN. RETURNED TO TWF. REPOSITIONED PNEUMATIC PRESSURE REGULATOR OVERBOARD DR AIN TUBE. ALSO, PERFORMED CHECK OF PNEUMATIC SYSTEM FOR ONE HOUR 45 MINUTES. OPS CHECKS GOOD IAW EMB 120 MM 36-00-00 A ND 36-20-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999052100290 19990521 00290 SO 1999 5 21 SWIA971480 1 19990509 A 5753 ROLLERS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT TE FLAP WORN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 AFTER TAKEOFF, FLAPS WERE RETRACTED AND GOT FLAP DISAGREEMENT. APPLIED QRH PROCEDURE TWICE WITH NO SUCCESS. RETURNED T O FAT. FLAPS RETRACTED NORMALLY ON THE GROUND. REMOVED AND REPLACED LEFT INBOARD FLAP ROLLERS IAW MM 27-50-12. NO OTH ER DISCREPANCIES NOTED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999052100291 19990521 00291 EA 1999 5 21 SWIA971481 1 19990503 A 3250 RVDT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 409SW 7056 NOSE WHEEL STEERING INOP MESSAGE CAME ON IN FLIGHT. RETURNED TO SLC. REMOVED AND REPLACED RIGHT RVDT AT NOSE GEAR, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999052100292 19990521 00292 NM 1999 5 21 TC899019 1 19990518 A 2810 FUEL BOEING 727 7272B6 138407J NM LT WING DISCHARGED A TC8A D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 GL 23 721SK 21298 ON TAXI, NOTIFIED BY TOWER FUEL DISCHARGED FROM LEFT WING. 2 L 7 3 4F A3WE 1999052100293 19990521 00293 NM 1999 5 21 TC8A99018 1 19990513 A 3340 SWITCH BOEING 727 727173C 1384059 NM ROTATING BEACON FAILED A TC8A D RETURN TO BLOCK O OTHER UK UNKNOWN 1 GL 23 704A 19504 ROTATING BEACON INOP. INSTALLED SERVICEABLE SWITCH, OPS CHECKS GOOD IAW MM 33-00. 2 L 7 3 4F A3WE 1999052100294 19990521 00294 NM 1999 5 21 TC8A99020 1 19990518 A 2810 VALVE BOEING 727 7272B6 138407J NM FUEL SYST OUT OF POSITION A TC8A D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 GL 23 721SK 21298 ON TAXI, NOTIFIED BY TOWER FUEL DISCHARGED FROM LEFT WING. RETURN TO RAMP. REPOSITIONED VALVE DEFUEL TO PROPER POSITIO N, OPERATED FUEL PUMPS WITH X FEED VALVE OPEN 1 HOUR. NO FUEL TRANSFERRED TO LEFT WING, NO FUEL FROM VENT PER B727 M/M 28-09-100. 2 L 7 3 4F A3WE 1999052100295 19990521 00295 EU 1999 5 21 RAIA990438 1 19990425 A 7712 31024766 TSCU BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 425AM 870 FLT 7028 - COU - TORQUE FLUCTUATION ON LEFT ENGINE. MAINTENANCE REPLACED TORQUE SIGNAL CONDITIONER FOR LEFT ENGINE. (M ) 2 L 7 2 4T RT A56EU 1999052100296 19990521 00296 EU 1999 5 21 RAIA990436 1 19990422 A 3110 ES300602 CAP PANEL BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 431AM 881 FLT 7367 - PAH - LEFT BETA LIGHT ILLUMINATED. MAINTENANCE REPLACED CAP PANEL. (M) 2 L 7 2 4T RT A56EU 1999052100297 19990521 00297 NE 1999 5 21 ASOA99038 2 19990413 A 7261 OIL SYSTEM EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE REQ'D SERVICE A ASOA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 11 258AS 120131 115498 LFT-DFW - DURING CRUISE AT FL220, RECEIVED ORAL 'OIL' WARNING AND TRIPLE CHIME. LEFT ENGINE OIL PRESSURE INDICATED 50 P SID. FOLLOWED QRH AND POH PROCEDURES AND REDUCED POWER 75 PERCENT NH, FLIGHT IDLE. DECLARED AN EMERGENCY AND DIVERTED TO TXK WHERE LANDING WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE ENGINE WITH 4 QUARTS OF OIL. E NGINE RUNS AND LEAK CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. OIL CONSUMPTION HISTORY OF THE ENGINE WELL WITHI N MM LIMITS. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999052100298 19990521 00298 SO 1999 5 21 ASOA99037 1 19990417 A 6120 PCU EMB 120 EMB120ER 3260203 SO LT PROP LEAKING A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SO 11 639AS 120283 ATL-ILM - CLIMBING OUT OF 22,000 FT RECEIVED AND ORAL 'OIL' WARNING. LEFT ENGIN EOIL PRESURE INDICATION DECREASING. CO MPLETED CHECKLIST. NH WAS DECREASED TO BELOW 75 PERCENT AND PROP FEATHERED. DECLARED AN EMERGENCY AND PERFORMED A PREC AUTIONARY SHUTDOWN OF THE LEFT ENGINE. FLIGHT DIVERTED TO AGS. SINGLE ENGINE APPROACH AND LANDING UNEVENTFUL. MAINTEN ANCE REMOVED AND REPLACED THE PCU AND O-RING AND SERVICED THE ENGINE OIL. ENGINE RUNS AND LEAK CHECKS WERE GOOD AND AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999052100299 19990521 00299 SO 1999 5 21 ASOA99036 1 19990414 A 5411 12003852001 FRAME EMB 120 EMB120RT SO LT/RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 502AS 120274 DURNG C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999052100300 19990521 00300 1999 5 21 RAIA990437 4 19990424 A 3454 6222506004 RMI BAG JETSTM JETSTM3201 1500217 EU NR 2 FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 343TE 956 955 FLT 7440 - STL - NR 1 CDI 30 DEGREES OFF. MAINTENANCE REPLACED NR 2 RMI. (M) 2 L 7 2 4T RT A56EU 1999052100301 19990521 00301 NM 1999 5 21 USAA990216 1 19990401 A 5311 FRAME BOEING 737 737401 1384701 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31080 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 294, WL 208.10 RBBL 55 FRAME. INSTALLED DOUBLER PER S RM 51-70-11 EA 63977. (M) 2 L 7 2 4F RT A16WE 1999052100302 19990521 00302 NM 1999 5 21 USAA990217 1 19990401 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31080 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK BS 294 WL 208.10 RBBL 55 ANGLE STIFFENER. REPAIRED PER S RM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999052100303 19990521 00303 NM 1999 5 21 USAA990225 1 19990401 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31080 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT NUT PLATE HOLES BS 947 LBL 24 - RBL 24 FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLED REPAIR 'T' SECTION AND REPAIR ANGLE PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999052100304 19990521 00304 NM 1999 5 21 USAA990234 1 19990401 A 5320 TIE CLIP BOEING 737 737401 1384701 NM BS 277 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31080 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 277 STRINGER 24L TIE CLIP. REPAIRED PER SRM 51-10-02 . (M) 2 L 7 2 4F RT A16WE 1999052100305 19990521 00305 NM 1999 5 21 USAA990254 1 19990401 A 5311 FRAME BOEING 737 737401 1384701 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31080 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 807 OBL FRAME. INSTALLED REPAIR PLATE AND FILLERS PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999052100306 19990521 00306 NM 1999 5 21 USAA990255 1 19990401 A 5320 FRAME BOEING 737 737401 1384701 NM CARGO DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31080 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .800 INCH CRACK AT FORWARD FRAME OF AFT CARGO DOOR 2 INCH ABOVE FORWAR D LATCH ARM. INSTALLED DOUBLER PER SRM 52-30-02. (M) 2 L 7 2 4F RT A16WE 1999052100307 19990521 00307 NM 1999 5 21 USAA990277 1 19990401 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31078 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AROUND NUT PLATES BS 986 LBL 44 - RBL 30 'T' CAP OF FLOORBEAM. CORROSION TASK NR C53-107-02. REPAIRED PER TR 53-60-01. (M) 2 L 7 2 4F RT A16WE 1999052100308 19990521 00308 NM 1999 5 21 USAA990283 1 19990401 A 5330 SKIN BOEING 737 737401 1384701 NM BS 797 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31078 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .1 INCH BY .4 INCH AREA OF CORROSION AT BS 797 BL 0 SKIN. INSTALLED D OUBLER PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999052100309 19990521 00309 NM 1999 5 21 USAA990284 1 19990401 A 5320 SUPPORT BOEING 737 737401 1384701 NM BS 330 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31078 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT BS 330, WL 208.10 AND RBBL 52 FLOOR SUPPORT. REPLACED FLOOR SUPPORT PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999052100310 19990521 00310 NM 1999 5 21 USAA990288 1 19990401 A 5330 SKIN BOEING 737 737401 1384701 NM BS 757 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31080 23883 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 4 INCH AREA OF CORROSION BS 757 BL 0 SKIN. INSTALLED DOUBLE R PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1999052100311 19990521 00311 NM 1999 5 21 USAA990292 1 19990308 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 321-328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 312 AND 328 LBL 11 FLOOR SUPPORT. REPAIRED PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999052100312 19990521 00312 NM 1999 5 21 USAA99293 1 19990308 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 773 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 773 RBL 3, 1 INCH BY 1 INCH AT NUTPLATE HOLES OF FL OOR SUPPORT. REPAIRED PER TR 53-10-06. (M) 2 L 7 2 4F RT A16WE 1999052100313 19990521 00313 NM 1999 5 21 USAA990294 1 19990308 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 859 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AT BSL 859 LBL 3 FLOORBEAM. INSTALLED DOUBLER PER TR 53-10-06 . (M) 2 L 7 2 4F RT A16WE 1999052100314 19990521 00314 NM 1999 5 21 USAA990295 1 19990308 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 747 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30694 23877 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 8 INCH AREA OF CORROSION AT BS 747 RBBL 13.8 FLOORBEAM. INS TALLED TIE DOWN TRACK PER SRM 53-00-53 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999052100315 19990521 00315 NM 1999 5 21 USAA990135 1 19990218 A 5320 GUSSET BOEING 737 7372B7 1384560 NM NLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AU 44033 22884 CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK IN UPPER RADIUS OF GUSSET AT TOP OF N/G WELL. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999052100316 19990521 00316 NM 1999 5 21 USAA990085 1 19990212 A 5240 6545371523 SKIN BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 49010 22273 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN DOOR SKIN FORWARD SERVICE DOOR UPPER HINGE CUTOUT D OOR EXT SKIN. INSTALLED DOUBLER PER SB 737-32-1016, EA 63767 AND TR 52-40-03A. (M) 2 L 7 2 4F A16WE 1999052100317 19990521 00317 NM 1999 5 21 USAA990086 1 19990212 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 49010 22273 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2.75 INCH CRACK IN EXTERNAL SKIN STATION 727B PLUS 4 INCHES AND STRIN GER 17R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M) 2 L 7 2 4F A16WE 1999052100318 19990521 00318 NM 1999 5 21 USAA990132 1 19990222 A 5330 SKIN BOEING 737 737201 1384454 NM BS 309 HOLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 54051 21665 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A ..125 INCH HOLE IN SKIN STATION 309 BETWEEN S-11 AND S-12. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999052100319 19990521 00319 WP 1999 5 21 USAAD99050 1 19990402 A 2120 71145730016 HOSE DOUG DC9 DC982 3022082 WP AFT FUSELAGE RUPTURED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 829US 49429 DCA-BUF - FLT 8005 - DURING CLIMB POWER SETTINGS THE TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED BUT WOULD EXTINGUISH D URING CRUISE POWER. THE AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLEX COUPLING D OWNSTREAM OF THE RIGHT AIR CONDITIONING TEMP CONTROL VALVE. (M) 2 L 7 2 4F A6WE 1999052100320 19990521 00320 NM 1999 5 21 USAASB99091 1 19990406 A 2824 MA17A2010 VALVE BOEING 737 7374B7 1384702 NM AUX FUEL TANK FAILED A USAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 436US 24558 STL - FLT2074 - ON CLIMB-OUT FROM CLT, AT APPROX 8,000 FT, THE LT 'NO TRANSFER' LIGHT FOR THE AUX FUEL TANK ILLUMINATED. THE AUX FUEL TANK WAS EMPTY. CONTINUING CLIMB, AT APPROX 15,000 FT, THE LT AND RT MLG RED LIGHTS ILLUMINATED WITH RT L/G GREEN LIGHT ON. CREW NOTICED A/C WAS SLUGGISH AND WOULD ONLY CLIMB AT ABOUT 500 FT PER MINUTE. CREW ELECTED TO DIS CONNECT AUTOPILOT AND A/C BEGAN TO BANK TO THE RT. CREW MENTIONED THAT THE F/A'S COMPLAINED ABOUT AN ODOR SIMILAR TO EL ECTRIC SMOKE IN COCKPIT AND FORWARD GALLEY AREA. CAPT DECLARED AN EMERG AND DIVERTED TO STL. FLT LANDED W/O INCIDENT A ND TAXIED TO THE GATE ON ITS OWN POWER. MX R/R'D THE LT AFT TRANSFER VALVE MOTOR IN THE AUX TANK. OPS CHECK GOOD. PER 2 L 7 2 4F RT A16WE 1999052100321 19990521 00321 NM 1999 5 21 USAASB99043 1 19990218 A 3020 655812310 DUCT BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 260AU 22866 CLT - FLT 281 - ON CLIMB-OUT FROM CLT AT 8,000 FT, THE NR 1 ENGINE OVERHEAT LIGHT AND OIL TEMPERATURE LIGHT ILLUMINATED. CAPTAIN REDUCED ENGINE THRUST AND THE OVERHEAT LIGHT EXTINGUISHED. OIL TEMPERATURE CLIMBED TO 130-135 DEGREES. CAPTA IN KEPT THE ENGINE RUNNING AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT, BUT AT THE GATE, TH E NR 1 ENGINE START LEVER WOULD NOT CUTOFF. CAPTAIN SHUT THE NR 1 ENGINE DOWN WITH THE FIRE HANDLE. STIFFNESS IN THROT TLE WAS ALSO NOTED. NO EMERGENCY WAS DECLARED. MX FOUND THE NR 1 ENGINE COWL ANTI-ICE DUCT BLOWN. REMOVED AND REPLACE D DUCT. OPS CHECK AND LEAK CHECK GOOD. REPLACED NR 1 ENGINE FUEL SHUTOFF CABLE AND THRUST CABLE. OPS CHECK GOOD. ALS 2 L 7 2 4F A16WE 1999052100322 19990521 00322 NM 1999 5 21 USAASB99045 1 19990219 A 2170 V1211 COALESCER BOEING 737 737201 1384454 NM LT/RT DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 237US 22353 PHL - FLT 712 - FLIGHT RETURNED TO FIELD AT PHL DUE TO A SMOKE SMELL IN THE COCKPIT. THE SMELL OF SMOKE WAS PRESENT AND TO WORSE ON TAKEOFF ROLL. CAPTAIN DECIDED TO TAKEOFF AND RETURN BACK TO FIELD. NO EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED AIR CONDITIONING SYSTEM OIL CONTAMINATION CHECK PER MM 21-00 -01. REMOVED AND REPLACED BOTH THE RIGHT AND LEFT WATER SEPARATOR BAGS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999052100323 19990521 00323 WP 1999 5 21 USAAD99049 1 19990401 A 2170 V1211 COALESCER DOUG DC9 DC931 3022065 WP RT AIR COND SYS OUT OF POSITION A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 933VJ 47216 ATL-PIT - FLT 1558 - AFTER TAKEOFF THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. AFTER LANDING THE CAPTAIN TALKED FURTHER WITH THE FLIGHT ATTENDANTS AND FOUND THEY WERE N OT SURE IF THERE WAS SMOKE OR WATER VAPOR. MAINTENANCE FOUND THE RIGHT AIR CONDITIONING WATER SEPARATOR BAG DISPLACED A LLOWING HEAVY WATER VAPOR TO BE DISTRIBUTED IN THE CABIN. THE WATER SEPARATOR BAG WAS REPLACED. (M) 2 L 7 2 4F A6WE 1999052100324 19990521 00324 WP 1999 5 21 USAAD99052 1 19990319 A 2910 836SD620 FUSE DOUG DC9 DC982 3022082 WP RT HYD SYST FRACTURED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 825US 49237 LGA-TPA - FLT 2186 - DURING CRUISE, THE RIGHT HYDRAULIC PRESSURE DROPPED TO JUST ABOVE ZERO AND THE RIGHT HYDRAULIC QTY WAS DROPPING. THE A/C DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE R20 HYDRAULIC FUSE. (M) 2 L 7 2 4F A6WE 1999052100325 19990521 00325 WP 1999 5 21 USAA990253 1 19990311 A 5320 FRAME DOUG DC9 DC981 3022081 WP CARGO DOORWAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 827US 47311 48049 PIT - DURIGN C5 CHECK, FOUND 1 INCH AREA OF CORROSION ON AND AROUND FASTENER HOLE AT AFT CARGO DOOR FRAME, FORWARD STRAP FASTENER HOLE IN LINE WITH LONGERON 28R. INSTALLED STRAP ASSEMBLY PER EA NR 51730. (M) 2 L 7 2 4F A6WE 1999052100326 19990521 00326 WP 1999 5 21 USAA990252 1 19990311 A 5320 FRAME DOUG DC9 DC981 3022081 WP CARGO DOORWAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 827US 47311 48049 PIT - DURING C5 CHECK, FOUND 1 INCH AREA OF CORROSION ON AND AROUND FASTENER HOLE AT AFT CARGO DOOR FRAME, AFT STRAP FAS TENER HOLE LONGERON 28R. INSTALLED STRAP ASSEMBLY PER EA NR 51730. (M) 2 L 7 2 4F A6WE 1999052100327 19990521 00327 WP 1999 5 21 USAA990251 1 19990311 A 5753 SKIN DOUG DC9 DC981 3022081 WP RT TE FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 827US 47311 48049 PIT - DURING C5 CHECK, FOUND 1 INCH LONG, 1 INCH WIDE, .011 DENT AND 1 INCH LONG, 1 INCH WIDE, .009 DEEP DENT AT RIGHT W ING INBOARD FLAP, AFT SIDE, MIDDLE OF TOP CENTER SKIN PANEL. CORROSION LEVEL 1. CLEANED AND TREATED CORROSION PER SRM CHAP 51. (M) 2 L 7 2 4F A6WE 1999052100328 19990521 00328 WP 1999 5 21 USAA990266 1 19990326 A 5311 FRAME DOUG DC9 DC982 3022082 WP FRAME 1416 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 815US 47188 48095 PIT - DURING C-06 CHECK, FOUND 1.5 INCH CRACK AT CANTED FRAME 1416 AT LONGERON 6L. STOP DRILLED WITH .25 INCH DRILL (TE MP REPAIR) PER EA 51797. (M) 2 L 7 2 4F A6WE 1999052100329 19990521 00329 WP 1999 5 21 USAA990265 1 19990326 A 5311 FRAME DOUG DC9 DC982 3022082 WP FRAME 1416 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 815US 47188 48095 PIT - DURING C-06 CHECK, FOUND 1.5 INCH CRACK AT CANTED FRAME 1416 AT LONGERON 6R. STOP DRILLED WITH .25 INCH DRILL (TE MP REPAIR) PER EA 51797. (M) 2 L 7 2 4F A6WE 1999052100330 19990521 00330 NM 1999 5 21 USAA990305 1 19990401 A 5311 FRAME BOEING 737 737401 1384701 NM BS 870 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 415US 31078 23883 CLT - DURING VISUAL CHECK INSPECTION, FOUND A 3 INCH CRACK ON FRAME STATION 870 BL 0 BOTTOM FLANGE. REMOVED CRACKED SKI N, FILLER AND REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999052100331 19990521 00331 1999 5 21 USAASB99050 4 19990223 A 3417 CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM NR 2 ADC TRIPPED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 442US 24841 PHL - FL325 - ON CLIMB-OUT FROM PHL, AT 3,000 FEET, THE F/O'S ALTIMETER AND AIRSPEED INDICATION BECAME INOPERATIVE. FLI GHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESET THE NR 2 AIR DATA COMPUTER CIRCUIT BREAKER. SYSTEM OPERATIONAL CHECK GOOD ON GROUND. INSPECTED NR 2 AIR DATA COMPUTER FOR DEF ECTS. NO DEFECTS NOTED. TESTED GOOD. (M) 2 L 7 2 4F RT A16WE 1999052100332 19990521 00332 1999 5 21 RAIA990407 4 19990407 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 7306 41072 FLT 7703 - BOS - AIR DATA FAIL INDICATION ON CAPTAINS SIDE. MAINTENANCE REPLACED CAPTAINS AIR DATA COMPUTOR. (M) 2 L 7 2 4T RT A41NM 1999052100333 19990521 00333 1999 5 21 RAIA990412 4 19990409 A 3425 7012977627 EFIS CONTROLLER JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 551HK 41040 FLT 7330 - STL - CAPTAINS EADI AND EHSI FLASHING ON AND OFF. MAINTENANCE REPLACED EFIS CONTROLLER. (M) 2 L 7 2 4T RT A41NM 1999052100334 19990521 00334 1999 5 21 RAIA990413 4 19990409 A 3425 7002493902 HSI BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 341TE 13230 950 FLT 7410 - STL - FIRST OFFICERS HSI FLAGGED. MAINTENANCE REPLACED HSI INDIATOR. (M) 2 L 7 2 4T RT A56EU 1999052100335 19990521 00335 EU 1999 5 21 RAIA990414 1 19990411 A 3243 ACM26810 MASTER CYLINDER BAG JETSTM JETSTM3201 1500217 EU CAPTAINS RT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 425AM 870 FLT 7360 - STL - RIGHT BRAKE INOPEATIVE ON CAPTAINS SIDE. MAINTENANCE SERVICED CAPTAINS RIGHT MASTER CYLINDER. (M) 2 L 7 2 4T RT A56EU 1999052100336 19990521 00336 EU 1999 5 21 RAIA990408 1 19990408 A 2150 2974A000 PRSOV JETAIR JETSTM JETSTM4101 1500501 EU RT PACK FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 551HK 41040 FLT 7211 - STL - BOTH FLOWS ONLY PUT OUT HOT AIR IN AUTO AND MANUAL MODE. MAINTENANCE REPLACED PRESS REGULATING SHUT-OF F VALVE ON RIGHT SIDE. (M) 2 L 7 2 4T RT A41NM 1999052100337 19990521 00337 1999 5 21 RAIA990426 4 19990418 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 4385 41075 FLT 7516 - STL - NR 2 EADI FAULTED. MAINTENANCE REPLACED NR 2 AIR DATA COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999052100338 19990521 00338 WP 1999 5 21 RAIA990427 2 19990419 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 CE 03 431AM 881 66157 FLT 7075 - STL - LEFT ENGINE FAILED IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999052100339 19990521 00339 EU 1999 5 21 RAIA990421 1 19990414 A 3340 4587 BULB AEROSP ATR42 ATR42300 8680920 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 422TE 106 FLT 7178 - STL - BOTH TAXI LIGHTS INOPERATIVE. MAINTENANCE REPLACED LEFT TAXI LIGHT. (M) 2 H 7 2 4T RT A53EU 1999052100340 19990521 00340 NE 1999 5 21 RAIA990425 2 19990416 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FAILED A RAIA E ENGINE SHUTDOWN X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CE 03 559HK 7339 41075 76115 FLT 7452 - STL - RIGHT ENGINE FLAMED TAXIING BACK INTO GATE. MAINTENANCE RESET IEC COMPUTER AND PERFORMED GROUND RUN. ( M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999052100341 19990521 00341 EU 1999 5 21 RAIA990418 1 19990412 A 2450 A2104F PDU JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 552HK 41057 FLT 7147 - MEM - LEFT BATTERY LIGHT ILLUMINATED. MAINTENANCE REPLACED NR 1 POWER DISTRIBUTION UNIT. (M) 2 L 7 2 4T RT A41NM 1999052100342 19990521 00342 EU 1999 5 21 RAIA990423 1 19990406 A 3241 140149 WHEEL TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU NR 4 WHEEL FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 552HK 41057 FLT 7067 - STL - ANTI-SKID FAULT LIGHT ILLUMINATED. MAINTENANCE REPLACED NR 4 WHEEL TRANSDUCER. (M) 2 L 7 2 4T RT A41NM 1999052100343 19990521 00343 EU 1999 5 21 RAIA990422 1 19990414 A 3340 14626 BULB AEROSP ATR42 ATR42300 8680920 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 422TE 106 FLT 7178 - STL - BOTH TAXI LIGHTS INOPERATIVE. MAINTENANCE REPLACED RIGHT TAXI LIGHT. (M) 2 H 7 2 4T RT A53EU 1999052100344 19990521 00344 EU 1999 5 21 RAIA990420 1 19990413 A 2432 40782 BATTERY AEROSP ATR72 ATR72202 8680940 EU BATTERY COMPT DISCHARGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7417 - STL - MAIN BATTERY DISCHARGE LIGHT ILLUMINATED. MAINTENANCE REPLACED MAIN BATTERY. (M) 2 H 7 2 4T RT A53EU 1999052100345 19990521 00345 EU 1999 5 21 RAIA990419 1 19990412 A 6120 31055863 MONOPOLE JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 03 568HK 41086 FLT 7650 - JFK - LEFT ENGINE OIL CONTAM LIGHT ILLUMINATED, THEN THE LEFT RPM AND TORQUE STARTED FLUCTUATING. MAINTENANC E REPLACED LEFT ENGINE RPM MONOPOLE. INSPECTED LEFT CHIP DETECTOR AND PERFORMED SOAP SAMPLE. (M) 2 L 7 2 4T RT A41NM 1999052100346 19990521 00346 1999 5 21 RAIA990430 3 19990420 A 6140 8659566 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT PROP FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 431AM 13548 881 FLT 7033 - STL - LEFT ENGINE BETA LIGHT ILLUMINATED. MAINTENANCE REPLACED BETA SWITCH ON LEFT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999052100347 19990521 00347 EU 1999 5 21 RAIA990428 1 19990419 A 5720 NAS12213CR3P SCREW BAG JETSTM JETSTM3201 1500217 EU WING TIP INCORRECT PART A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 875JX 875 FLT 7364 - STL - 15 DEGREES HEADING SPLIT. MAINTENANCE REMOVED MAGNETIC SCREWS AND INSTALLED NON-MAGNETIC SCREWS IN BOT H WING TIPS. (M) 2 L 7 2 4T RT A56EU 1999052100348 19990521 00348 EU 1999 5 21 RAIA990429 1 19990420 A 7930 387 BULB BAG JETSTM JETSTM3201 1500217 EU RT OIL COOLER FAILED A RAIA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 425AM 870 FLT 7300 - STL - RIGHT OIL COOLER FLAP LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB. (M) 2 L 7 2 4T RT A56EU 1999052100349 19990521 00349 WP 1999 5 21 GTIA9900045 1 19990317 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 ACY - FLT 286 - OVERHEAD EMERGENCY LIGHT IN COCKPIT INOPERATIVE. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. REMOVED AND REPLACED 2 EACH BATTERIES ON EMERGENCY LIGHT PACK, OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999052100350 19990521 00350 WP 1999 5 21 GTIA9900046 1 19990317 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 FRONT WHITE EMERGENCY FLOOR LIGHT OUT. REPLACED SOCKET AND LENS AND LAMP TO FRONT EPL LIGHT AND REPAIRED BROKEN WIRES. OPERATION CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1999052100351 19990521 00351 WP 1999 5 21 GTIA9900051 1 19990331 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 13512 48111 DTW - FORWARD CABIN EMERGENCY FLOOR LIGHTS OUT. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATION CHECK G OOD ON RAMP AT THIS TIME IAW MM 33-50-0. (M) 2 L 7 2 4F A6WE 1999052100352 19990521 00352 WP 1999 5 21 GTIA9900052 1 19990331 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 13512 48111 DTW - FORWARD EMERGENCY TRACK LIGHTS OUT. RESECURED FORWARD EMERGENCY TRACK LIGHT IAW MM 33-50. (M) 2 L 7 2 4F A6WE 1999052100353 19990521 00353 WP 1999 5 21 GTIA9900054 1 19990403 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947ML 47514 DTW - EMERGENCY EXIT LIGHT INOPERATIVE. MAIN ENTRY DOOR WAY. REMOVED AND REPLACED LIGHT ASSEMBLY. FUNCTIONAL CHECK GO OD DC-9 MM CHAP 33-50-0. (M) 2 L 7 2 4F A6WE 1999052100354 19990521 00354 WP 1999 5 21 GTIA9900055 1 19990408 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 13512 48111 DTW - OVERWING EMERGENCY EXIT LIGHTS (UPPER ONE'S) INOPERATIVE. ALL FOUR OF THEM, FORWARD, AFT AND LEFT AND RIGHT. REM OVED AND REPLACED BATTERY PACK PATTERNS AND OPERATION CHECKED IAW DC-9 MM 33-50-0. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 1999052100355 19990521 00355 CE 1999 5 21 AMWA002467 1 19990118 A 6120 5038912129 SWITCH BEECH 1900 1900D 1154162 CE RT ENGINE MALFUNCTIONED A AMWA O OTHER O OTHER DE DESCENT 1 CE 07 64YV UE64 ON APPROACH TO DSM FROM MCI, THE RT PROP WAS CYCLING IN/OUT OF FEATHER. DSM MAINTENANCE REPLACED THE RT LOW PRESSUER SW ITCH. OPS CHECK NORMAL. THE FOLLOWING DAY, THE PROBLEM REOCCURED IN MCI WHERE THE PEDESTAL SWITCHES WERE ADJUSTED. OP S CHECK NORMAL. NO FURTHER INCIDENTS. (M) 2 L 7 2 4T RT A24CE 1999052100358 19990521 00358 NM 1999 5 21 P2EA99133 1 19990415 A 3230 RETRACT MECH BOEING 737 737247 138448D NM NLG MALFUNCTIONED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 204AU 19603 MCI - FLT 299 - AIR RETURN, NO EMERGENCY DECLARED, LANDING UNEVENTFUL. ON TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. (M ) 2 L 7 2 4F A16WE 1999052100359 19990521 00359 NE 1999 5 21 P2EA99164 2 19990422 A 7532 658385 PRSOV BOEING 737 737244 138448U NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED A P2EA O OTHER J WARNING INDICATION DE DESCENT 1 CE 05 620PC 19708 ATL - FLT 406 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. DESCENDING THROUGH 15,000 FEET, THROTTLES NEAR IDLE, A LOUD BOOM HEARD IN COCKPIT AND CABIN IN THE AIRCONDITIONING SYSTEM. THE LEFT DUCT OVERHEAT LIGHT AND MASTER CAUTION/OVERHEAD LIGHT CAME ON. QRH ITEMS ACCOMPLISHED. EXTINGUISHED OVERHEAT LIGHTS WITH RESET BUTTON. LOUD NOISE CONTINUED WITH LEF T PACK OFF, LEFT ENGINE BLEED OFF, AND ISOLATION VALVE CLOSED UNTIL AFTER LANDING AND SHUT DOWN OF NR 1 ENGINE. INSPECT ED NR 1 ENGINE PNEUMATIC DUCTS, DUCTS IN LEFT WING AREA, LEFT AND RIGHT AIR CONDITIONING PACK AREAS, FORWARD CARGO AFT A REA, E/E AREA. FOUND NO SIGNS OF BLOWN DUCTS. RAN ENGINES PRESSURIZED AIRCRAFT, NO LEAKS FOUND. INSPECTED LEFT AIR CY 2 L 7 2 4F 4 F A16WE E2EA 1999052100360 19990521 00360 WP 1999 5 21 G60A031 1 19990404 A 2730 H21881 LATCHES DOUG DC10 DC1030F 3023504 WP LT ELEVATOR SHEARED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 600GC 46965 ON TRANSIT WALK AROUND, FOUND INBOARD DETACHABLE ELEVATOR IN DETACHED POSITION. LATCH PINS FOUND SHEARED. REMOVED AND REPLACED LEFT DETACHABLE ELEVATOR LATCHES, TWO P/N H2188-1, AND INSTALLED ALL REQUIRED FASTENERS. RELATCHED ELEVATOR AN D CHECKED FOR PROPER MOVEMENT PER MM 27-30-03. REPAIR APPROVED BY MDC, REF FORM 8110-3, 4/5/99, BURCH, DN-DERY-605071-N M. PERMANENT REPAIR REQUIRED WITHIN 4800 FLT HOURS OR NEXT C-CHECK, REF EO 99-2740-007. (M) 2 L 7 3 4F RT A22WE 1999052100361 19990521 00361 NM 1999 5 21 USAA990278 1 19990331 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 39871 23382 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 1 INCH AREA OF CORROSION AT STATION 360 UPPER 'T' CAP FLOORB EAM, CORROSION TASK NR C53-107-02. REPLACED 'T' CAP ON FLOORBEAM PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999052100362 19990521 00362 NM 1999 5 21 USAA990247 1 19990331 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 39871 23382 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT FRAME 480 STRINGER 8L AND 9L. INSTALLED DOUBLER PER EA 64083 . (M) 2 L 7 2 4F RT A16WE 1999052100363 19990521 00363 NM 1999 5 21 USAA990246 1 19990331 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 39871 23382 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AND SHEARED RIVETS AT WL 195 INTERCOSTAL RBL 24, BS 178. FABRICATED REPAIR PER SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999052100364 19990521 00364 NM 1999 5 21 USAA990242 1 19990331 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 39871 23382 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH FLANGE AT INTERCOSTAL BL 0 STATION 344, CORRO SION TASK NR C53-107-02. REMOVED FLANGE AND INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1999052100365 19990521 00365 NM 1999 5 21 USAA990202 1 19990331 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 507AU 39871 23382 DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK BS 178 LBL 24 INTERCOSTAL. INSTALLED FABRICATED DOUBLER PER S RM 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999052100366 19990521 00366 NM 1999 5 21 USAASB99093 1 19990409 A 2910 AS1160800264 LINE BOEING 737 737301 1384611 NM 'B' HYD SYSTEM LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 334US 23231 PIT - FLT 1628 - AFTER CLIMB FROM PHL AT FL330, AIRCRAFT EXPERIENCED A COMPLETE FAILURE OF SYSTEM 'B' HYDRAULICS. CREW REPORTED ZERO PRESSURE AND QUANTITY. THE 'B' SYSTEM PUMPS WERE TURNED OFF WITHIN TWO MINUTES OF LOW PRESSURE LIGHTS. F LIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. AIRCRAFT TAXIED TO THE GATE ON ITS POWER. AN EMERGENCY WAS DECLARED . MAINTENANCE FOUND A HYDRAULIC LINE IN THE MAIN LANDING GEAR WHEEL WELL LEAKING. REPLACE HYDRAULIC LINE. ALSO, REPLA CED NR 2 ENGINE HYDRAULIC PUMP AND ALL HYDRAULIC SYSTEM FILTERS. SERVICED HYDRAULIC TO FULL. RAN ENGINE AND HYDRAULIC SYSTEM. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999052100367 19990521 00367 EU 1999 5 21 USAA990315 1 19990407 A 5310 STRUCTURE FOKKER F28 F28MK0100 4990807 EU BS 27250 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 883US 18810 11337 PIT - DURING C-CHECK, FOUND TWO CRACKS IN FUSELAGE SKIN ( 1 INCH AND 2 INCH LONG CRACKS) AT APU EXHAUST OUTLET AREA FS 2 7250 STRINGERS 46-50. DOUBLER INSTALLED, STRINGERS REPAIRED AND REPLACED PER EA NR 51808 DATED 4/6/99. (M) 2 L 7 2 4F RT 1999052100368 19990521 00368 NM 1999 5 21 USAA049904 1 19990414 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM RT EMER EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 926TS 14042 20774 FLT 6540 - DCA-LGA - FOUND ON L/S CHECK, RIGHT FORWARD EMERGENCY OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK . CHECK OK. (M) 2 L 7 3 4F A3WE 1999052100369 19990521 00369 NM 1999 5 21 USAA049903 1 19990412 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927TS 22857 20837 FLT 6141 - BOS-LGA - FOUND ON L/S CHECK, CABIN CENTER AISLE EMERGENCY LIGHT INOPERATIVE AT ROW 18. REPLACED BATTERY PAC K. (M) 2 L 7 3 4F A3WE 1999052100370 19990521 00370 NM 1999 5 21 USAA049901 1 19990403 A 3350 900542 LIGHT BOEING 727 727225 1384077 NM ROW 3 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 923TS VA5271 20441 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 3. REPLACED EMERGENCY EXIT LIGHT BASE ASSEMBLY, OPERATIONAL CHECK NORM AL. (M) 2 L 7 3 4F A3WE 1999052100371 19990521 00371 NM 1999 5 21 USAA049902 1 19990403 A 3350 1000677 LIGHT BOEING 727 727254 138408L NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913TS 9838 20250 COCKPIT DOOR EMERGENCY EXIT LIGHT WOULD NOT WORK. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1999052100372 19990521 00372 WP 1999 5 21 USAAD99035 1 19990303 A 7722 1245146 INDICATOR DOUG DC9 DC982 3022082 WP RT EGT FLUCTUATION A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 820US 49119 PIT-PBI - FLT 1807 - THE RIGHT ENGINE STARTED TOWARDS EXCEEDING MCP (580) WHEN APPLYING CLIMB POWER WHEN CLEARED TO CLIM B TO 14,000 FT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE EGT INDICATOR AND OPERATED THE ENGINE AT TAKEOFF POWER SEVERAL TIMES. ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1999052100373 19990521 00373 WP 1999 5 21 USAAD99051 1 19990405 A 3350 6011777LB POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959VJ 47352 CMH - THE EMERGENCY EXIT WOULD NOT EXTINGUISH AND THE EMERGENCY LIGHT ARM/CHARGE CIRCUIT BREAKER WILL NOT STAY SET. MAI NTENANCE REPLACED THE LIFT NACELLE LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999052100374 19990521 00374 WP 1999 5 21 USAAD99054 1 19990409 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 985VJ 47208 IND - THE EMERGENCY LIGHTS WERE INOPERATIVE FOR THE FORWARD ENTRY DOOR, SERVICE DOOR, FLIGHT DECK, AND FORWARD AISLE CEI LING. MAINTENANCE REPLACED ALL 10 LIGHT BULBS AND CABIN CEILING POWER SUPPLY AND BATTERIES. (M) 2 L 7 2 4F A6WE 1999052100375 19990521 00375 NM 1999 5 21 99ZZZM295 1 19990406 A 2750 66218291 ECCENTRIC BOEING 727 727225 1384077 NM LT TE FLAP MISSING A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 DURING P/T WALK AROUND LEFT WING INBOARD T/E MID FLAP CARRIAGE MISSING UPPER INBOARD ECCENTRIC, LOCKING TAB WASHER AND N UT ON OUTBOARD CARRIAGE. REPLACED CARRIAGE UPPER ECCENTRIC AND NUT ON LEFT WING INBOARD TRAILING EDGE FLAP IAW 27-51-2. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999052100376 19990521 00376 NM 1999 5 21 99ZZZM296 1 19990409 A 2750 66218291 ECCENTRIC BOEING 727 727225 1384077 NM LT TE FLAP MISSING A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 886MA 21855 DURING P/T WALK AROUND LEFT WING INBOARD T/E MID FLAP CARRIAGE MISSING UPPER INBOARD ECCENTRIC, LOCKING TAB WASHER AND N UT ON OUTBOARD CARRIAGE. REPLACED CARRIAGE UPPER ECCENTRIC AND NUT ON LEFT WING INBOARD TRAILING EDGE FLAP IAW 27-51-2. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999052100377 19990521 00377 NM 1999 5 21 99ZZZM297 1 19990407 A 2750 66218291 ECCENTRIC BOEING 727 727231 1384079 NM LT TE FLAP MISSING A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 808MA 21988 DURING P/T WALK AROUND, FOUND LEFT WING INBOARD T/E MID FLAP CARRIAGE MISSING UPPER INBOARD ECCENTRIC, LOCKING TAB WASHE R AND NUT ON OUTBOARD CARRIAGE. REPLACED CARRIAGE UPPER ECCENTRIC, LOCK TAB WASHER AND NUT ON LEFT WING INBOARD TRAILIN G EDGE FLAP IAW 27-51-2. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999052100378 19990521 00378 NM 1999 5 21 99ZZZM298 1 19990410 A 2750 66218291 ECCENTRIC BOEING 727 727225 1384077 NM RT TE FLAP MISSING A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 804MA 22435 DURING INSPECTION, FOUND RIGHT WING INBOARD AFT FLAP INBOARD ECCENTRIC, LOCK TAB WASHER AND NUT MISSING. REPLACED INBOA RD CARRIAGE ECCENTRIC, LOCK TAB WASHER AND NUT ON RIGHT WING INBOARD AFT FLAP IAW 27-51-2. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999052100379 19990521 00379 NM 1999 5 21 MASA99059 1 19990414 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 FLT 6354 - PHX-FLG - PRIOR TO DEPARTURE, CREW REPORTED THE FORWARD CEILING EMERGENCY LIGHT WAS INOP. MAINTENANCE REPLAC ED THE BULB, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999052100380 19990521 00380 NM 1999 5 21 99ZZZM299 1 19990120 A 3350 5521981 BATTERY PACK BOEING 737 737242 1384477 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 159PL 21186 EMERGENCY TRACK LIGHTING REMAINS ON IN ARM POSITION WITH A/C POWER ON LINE AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. C YCLED SWITCH TO OFF AND REPLACED EMERGENCY LIGHT BATTERY PACKS PER B737 CHAPTER 33 AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999052100381 19990521 00381 NM 1999 5 21 99ZZZM300 1 19990302 A 3350 OL3071BPEGPL BULB BOEING 737 737242 1384477 NM ROW 8 FAILED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 159PL 21186 WHITE FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT BULB AT ROW 8 IAW B737 MM 33-20-0. (M) 2 L 7 2 4F A16WE 1999052100382 19990521 00382 NM 1999 5 21 TSAA9953179 1 19990401 A 5330 SKIN BOEING 737 737230C 1384472 NM BS 867-887 GOUGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 AIRCRAFT SUSTAINED SKIN DAMAGE BETWEEN BS 867 AND BS 887 AT STRINGER 27 RIGHT. THREE GOUGES NOTED. REPAIRED IAW SRM 53 -30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999052100383 19990521 00383 NM 1999 5 21 TSAA9955204 1 19990408 A 5510 6549925506 FITTING BOEING 737 7372Q9 138448M NM RT HORIZ STAB CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 RIGHT UPPER HORIZONTAL STABILIZER ATTACHMENT FITTING (FUSELAGE SIDE) FOUND CRACKED AROUND EAR. REPLACED STABILIZER ATTA CHMENT FITTING. (M) 2 L 7 2 4F A16WE 1999052100384 19990521 00384 NM 1999 5 21 TSAA9933220 1 19990419 A 3350 6013211 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED FORWARD SLIDE LIGHT BATTERY POWER SUPPLY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999052100385 19990521 00385 NM 1999 5 21 TSAA9933221 1 19990419 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999052100386 19990521 00386 NM 1999 5 21 TSAA9933218 1 19990415 A 3350 873100151 LIGHT BOEING 737 7372S5C 1384499 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 4 FLOOR PROXIMITY LIGHT ASSY DUE TO NO 'ALL IS WELL' LED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999052100387 19990521 00387 NM 1999 5 21 TSAA9933219 1 19990415 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 6 FLOOR LIGHT PROXIMITY BATTERY PACK DUE TO NO 'ALL IS WELL' LED. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999052100388 19990521 00388 NM 1999 5 21 GAIA9951 1 19990422 A 3231 INDICATION BOEING 727 727251 138408H NM RT MLG DOOR MALFUNCTIONED A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 279US 21158 ON CLIMB-OUT OF TOL, THE RIGHT GEAR DOOR LIGHT CAME ON IN FORWARD FE'S FORWARD PANEL. SELECTED GEAR TO UP POSITION. TH E LIGHT WENT OUT AND STAYED OUT WHEN GEAR HANDLE WAS SELECTED IN OFF POSITION. AIRCRAFT MADE AN UNEVENTFUL CONTINUATION FLIGHT AND LANDED SAFELY AT BLD. NOT OTHER PROBLEMS WERE NOTED. CONDUCTED A VISUAL INSPECTION OF RIGHT LANDING GEAR S YSTEM AND DOORS. NO DEFECTS WERE FOUND. OPERATIONAL CHECK GOOD ON GROUND. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999052100389 19990521 00389 NM 1999 5 21 F3LA99031 1 19990326 A 5210 65164799 GATE BOEING 737 737317 138447P NM L1 DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-CHECK, INSPECTION REPORTED UPPER DOOR GATE CRACKED AT ACTUATOR EAR ON L-1 DOOR. MAINTENANCE REPLACED UPPER GAT E ASSEMBLY PER MM 52-11-00. RIGGED AND ADJUSTED GATE ASSEMBLY PER MM 52-11-99, PAGES 512-514. (M) 2 L 7 2 4F RT A16WE 1999052100390 19990521 00390 NM 1999 5 21 F3LA99030 1 19990320 A 5320 SUPPORT BOEING 737 737317 138447P NM BS 787 BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DEN - DURING C-CHECK INSPECTION, REPORTED TWO AFT CARGO PIT STANTION CLEATS BROKEN, STATION 787, LEFT FLOOR AREA. MAINT ENANCE REPLACED FLOOR SUPPORT PER SRM 53-00-53 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999052100391 19990521 00391 NM 1999 5 21 F3LA99029 1 19990326 A 5754 SKIN BOEING 737 737317 138447P NM NR 5 LE SLAT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 DURING C-CHECK INSPECTION, REPORTE THREE CRACKS ON THE LOWER SKIN OF THE NR 5 SLAT, OUTBOARD END. MAINTENANCE REPAIRED PER SRM AND EO 57-54-737-002. (M) 2 L 7 2 4F RT A16WE 1999052100392 19990521 00392 NM 1999 5 21 F3LA99028 1 19990404 A 3350 1000679 BATTERY PACK BOEING 737 737201 1384454 NM L1 DOOR DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 20214 DEN - UPON WALK AROUND MAINTENANRE REPORTED EMERGENCY LIGHT ACTIVATION CABLE LOOSE AT SLIDE COVER ON L1 DOOR, EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK. SECURED CABLE ASSY AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1999052100393 19990521 00393 NM 1999 5 21 P2EA99130 1 19990407 A 7797 WIRE BOEING 737 737244 138448U NM NR 1/NR 2 EPR LOOSE A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 05 620PC 19708 PIT - FLT 701 - ON TAKEOFF ROLL, NR 2 ENGINE EPR DID NOT RESPOND WITH ENGINE RUN-UP. FOUND NR 1 ENGINE EPR AND LANDING GEAR WARNING CIRCUIT BREAKERS POPPED. RESET CIRCUIT BREAKERS AND NR 2 EPR CAME UP. FOUND NR 1 AND NR 2 EPR CIRCUIT BRE AKERS REVERSED POSITION AND WIRE LOOSE. REPOSITIONED CIRCUIT BREAKERS PER WIRING DIAGRAM MANUAL 77-13-01. SECURED WIRE , OPERATIONAL CHECK NORMAL PER MM 77. (M) 2 L 7 2 4F A16WE 1999052100394 19990521 00394 NM 1999 5 21 P2EA99131 1 19990411 A 2120 BACC10DU400AB CLAMP BOEING 737 737297 1384480 NM AIR DUCT FAILED A P2EA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 5WM 22629 MCI - FLT 815 - AFTER DEPARTURE, FORWARD LAV SMOKE DETECTOR ALARM SOUNDED. AIRCRAFT RETURNED TO MCI WITH NO EMERGENCY D ECLARED. FOUND BLEED AIR DISTRIBUTION DUCTING CLAMP IN AFT CARGO AREA LEAKING. REPLACED CLAMP. OPERATIONAL CHECK OF E NGINES/APU AND A/C PACKS NORMAL. (M) 2 L 7 2 4F A16WE 1999052100395 19990521 00395 NM 1999 5 21 P2EA99132 1 19990411 A 8012 VALVE BOEING 737 737205 NM NR 1 ENGINE LACK OF LUBE A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 412CE 20412 PIT - FLT 707 - AS POWER WAS APPLIED FOR TAKEOFF, NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. INDICATION WAS ACCOMP ANIED BY A POPPING SOUND. CLEANED AND LUBED NR 1 PRESSURE REGULATING SHUTOFF VALVE. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999052100396 19990521 00396 EU 1999 5 21 VTZA9907708 1 19990314 A 7930 OIL LIGHT BAG JETSTM JETSTM3201 1500217 EU LT/RT ENGINE ILLUMINATED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 475UE 850 FLT 7203 - IAD-ROA - DURING CLIMB, AIRCRAFT RETURNED DUE TO OIL CONTAM LIGHT. PRESSED BOTH LEFT AND RIGHT. LIGHT STAYE D ON. MAINTENANCE CLEANED MOISTURE FROM CAPT SKIRT PANEL DE-ICE FLUID AND CLEANED CAPTAINS DV WINDOW SEAL. OPS CHECK G OOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999052100397 19990521 00397 EU 1999 5 21 VTZA9907709 1 19990315 A 3110 INSTRUMENT PANEL BAG JETSTM JETSTM3201 1500217 EU COCKPIT SMOKING A VTZA D H RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 483UE 898 FLT 7314 - CHO-IAD DURING TAXI, AIRCRAFT EXPERIENCED SMOKE BEHIND PANEL AT CENTER WINDSHIELD. PAX DEPLANED ON TAXIWAY. MAINTENANCE INSPECTED ALL WIRING BEHIND INSTRUMENT PANEL. PERFORMED AVIONICS CHECKS WITH RADAR SCREEN DISCONNECTED. N O BLACK SMOKE EVIDENT. PULLED C/B FOR WX RADAR AND WX RADAR SCREEN BOX SUSPECTED BAD. SUBMITTER STATES, SUSPECTED ALSO FMS. PULLED C/B FOR FMS. PERFORMED ENGINE RUNS WITH AVIONICS ON. NO EVIDENCE OF SMOKE AT ASSOCIATED WX RADAR OR FMS. FOUND WATER AND GLYCOL BEHIND PANEL TO BE SOURCE OF SMOKE. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999052100398 19990521 00398 EU 1999 5 21 VTZA9907732 1 19990331 A 3260 BULB BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A VTZA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 EA 27 480UE 894 FLT 7269 - BWI-IAD - DURING DESCENT, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LEFT GEAR DOWNLOC K LIGHT WOULD NOT ILLUMINATE AND CREW ABORTED APPROACH. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAI NTENANCE INSPECTED AND REMOVED AND REPLACED LIGHT BULB. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A56EU 1999052100399 19990521 00399 EU 1999 5 21 VTZA990730 1 19990228 A 3310 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 315UE 41033 FLT 7686 - LGA-IAD - DURING CRUISE, AIRCRAFT DIVERTED TO ABE DUE TO BURNING ELECTRICAL SMELL ON FLIGHT DECK. AIRCRAFT W ENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND BURNED LIGHT ASSEMBLY ABOVE CAPTAINS OXYGEN MASK. CREW PULLED CIRCUIT BREAKERS H26, H27, D28, J11, AND H7 AND OPENED DMI 05422 MEL 33-1. MAINTENANCE CLOSED DMI05422 ON 3/7/99 BY REMOVING AND REPLACING CAPTAINS CONSOLE LIGHT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999052100400 19990521 00400 EA 1999 5 21 VTZA9907726 1 19990327 A 3260 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR TRIPPED A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 620BR 7179 FLT 7788 - SAV-IAD - DURING TAKEOFF, AIRCRAFT RETURNED TO SAV DUE TO LANDING GEAR DISAGREE MESSAGE. FLIGHT CREW CONTACT ED DISPATCH AND MAINTENANCE CONTROL. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND PSEU FAULT. RESET PSEU AND COULD NOT DUPLICATE AFTER SEVERAL GEAR SWINGS. OPS CHECK OK. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999052100401 19990521 00401 NM 1999 5 21 EIA990085 1 19990207 A 5730 SKIN BOEING 747 747121 1384871 NM BS 1140 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, CENTER WING SECTION UPPER SKIN UPPER SURFACE HAS CORROSION AT BS 1140 LBL 99. REPAIRED IAW RS R-5 7-14-34038, 8110-2 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100402 19990521 00402 NM 1999 5 21 EIA990084 1 19990207 A 5712 RIB BOEING 747 747121 1384871 NM WS 697 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, LEFT WING AT WS 697 INBOARD NACELLE RIB INBOARD STIFFENER CRACKED NRC 7134. REPLACED STIFFENER IA W SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100403 19990521 00403 NM 1999 5 21 EIA990083 1 19990207 A 5400 ANGLE BOEING 747 747121 1384871 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, NR 3 PYLON UNDERWING T/E INBOARD SKIRT FAIRING ANGLE CRACKED NRC 6709. REPLACED SKIRT ANGLE IAW S RM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100404 19990521 00404 NM 1999 5 21 EIA990082 1 19990207 A 5400 FITTING BOEING 747 747121 1384871 NM NR 4 PYLON DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, NR 4 PYLON DIAGONAL BRACE ATTACH FITTING LUG BORE HAS DEEP MACHINE MARK. REPAIRED IAW SB 54-2164. (M) 2 L 7 4 4F A20WE 1999052100405 19990521 00405 NM 1999 5 21 EIA990081 1 19990207 A 5414 SKIN BOEING 747 747121 1384871 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, NR 3 PYLON VALVE ACCESS HOLE AFT LOWER AREA INNER AND OUTER SKIN CRACKED. REPAIRED IAW SRM 54-30- 03. (M) 2 L 7 4 4F A20WE 1999052100406 19990521 00406 NM 1999 5 21 EIA990080 1 19990207 A 5400 FITTING BOEING 747 747121 1384871 NM NR 4 PYLON NOT DRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK NR 4 PYLON DSB AND BACKUP FITTING HOLES NR 1 THROUGH NR 4 LOCATION NEEDS DETERMINED. REPAIRED IAW RS R-57-04-34034, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100407 19990521 00407 NM 1999 5 21 EIA990079 1 19990207 A 5400 FITTING BOEING 747 747121 1384871 NM NR 3 PYLON NOT DRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, NR 3 PYLON DSB AND BACKUP FITTING HOLES NR 1 THROUGH NR 3 LOCATION NEEDS DETERMINED. REPAIRED IAW RS R-57-04-34033, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100408 19990521 00408 NM 1999 5 21 EIA990078 1 19990207 A 5400 FITTING BOEING 747 747121 1384871 NM NR 2 PYLON NOT DRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, NR 2 PYLON DSB AND BACKUP FITTING HOLES NR 1 AND NR 2 LOCATION NEEDS DETERMINED. REPAIRED IAW RS R-57-04-34032, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100409 19990521 00409 NM 1999 5 21 EIA990077 1 19990207 A 5400 FITTING BOEING 747 747121 1384871 NM NR 1 PYLON NOT DRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, NR 1 PYLON DSB AND BACKUP FITTING HOLES NR 1 THROUGH NR 4 LOCATION NEEDS DETERMINED. REPAIRED IAW RS R-57-04-34031, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100410 19990521 00410 NM 1999 5 21 EIA990076 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1959 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 1959 STRINGER 2L, 3L, 3R AND 4R, STRINGER ENDS FOUND CRACKED. NRC 7238, 7239, 7236 A ND 7237 RESPECTIVELY. REPAIRED IAW RS R-53-41-34044, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100411 19990521 00411 NM 1999 5 21 EIAA990075 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1478 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 1478 STRINGER 6L, BS 1485 STRINGER 15R AND 17R, STRINGER ENDS FOUND CRACKED. NRC 723 5, 7230 AND 7231 RESPECTIVELY. REPAIRED IAW RS R-53-41-34003, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100412 19990521 00412 NM 1999 5 21 EIA990074 1 19990207 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 1265 RT FRAME INBOARD CHORD AND WEB CRACKED, NRC 6486. REPAIRED IAW RS R-53-41-34023 , 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100413 19990521 00413 NM 1999 5 21 EIA990073 1 19990207 A 5320 SPLICE BOEING 747 747121 1384871 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 1265, FRAME SPLICE WEB CRACKED AT LBL 120 AND RBL 120. NRC 5711 AND 5712. REPAIRED IAW SRM 53-10-04. (M) 2 L 7 4 4F A20WE 1999052100414 19990521 00414 NM 1999 5 21 EIA990072 1 19990207 A 5330 PANEL BOEING 747 747121 1384871 NM BS 1241 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 1241 AT LB 75 TRIM AIR CLOSE OUT PANEL FOUND CRACKED, NRC 6037. REPLCED CLOSEOUT PAN EL IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100415 19990521 00415 NM 1999 5 21 EIA990071 1 19990227 A 5320 SPLICE BOEING 747 747121 1384871 NM BS 1000 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 1000 STRINGER 7R ATTACH SPLICE FOUND CRACKED, NRC 6958. REPLACED SPLICE FITTING IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100416 19990521 00416 NM 1999 5 21 EIA990070 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 960-980 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 960-980 STRINGER 7R FOUND CRACKED, NRC 6622. REPAIRED IAW SRM 53-10-03. (M) 2 L 7 4 4F A20WE 1999052100417 19990521 00417 NM 1999 5 21 EIA990069 1 19990207 A 5320 FITTING BOEING 747 747121 1384871 NM 3L DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK NR 3L DOOR FORWARD CUTOUT NR 6 STOPPAD FITTING FOUND CRACKED, NRC 7326. REPLACED STOP F ITTING IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100418 19990521 00418 NM 1999 5 21 EIA990068 1 19990207 A 5320 FITTING BOEING 747 747121 1384871 NM 3R DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK NR 3R DOOR FORWARD CUTOUT NR 6 STOP FITTING FOUND CRACKED, NRC 7157. REPLACED STOP FITT ING IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100419 19990521 00419 NM 1999 5 21 EIA990067 1 19990207 A 5320 FITTING BOEING 747 747121 1384871 NM 3L DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK NR 3L DOOR FORWARD CUTOUT NR 8 STOP FITTING FOUND CRACKED, NRC 6487. REPLACED STOP FITT ING IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100420 19990521 00420 NM 1999 5 21 EIA990066 1 19990207 A 5320 STOP BOEING 747 747121 1384871 NM 3R DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK NR 3 R DOOR FORWARD CUTOUT NR 2 STOP FOUND CRACKED, NRC 6813. REPLACED STOP IAW SRM 51- 10-01. (M) 2 L 7 4 4F A20WE 1999052100421 19990521 00421 NM 1999 5 21 EIA990065 1 19990207 A 5320 65B183620 FRAME BOEING 747 747121 1384871 NM 1R DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK NR 1R DOOR FORWARD FRAME BETWEEN NR 1 AND NR 2 STOPS FOUND CRACKED, NRC 6033. REPLACED FRAME IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100422 19990521 00422 NM 1999 5 21 EIA990064 1 19990207 A 5320 BEAM BOEING 747 747121 1384871 NM RT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, RIGHT BLG TRUCK BEAM, CORROSION FOUND AT AFT LUG AND FORWARD ANCHORD POINT AT TILT ACTUATOR, NRC 5 257 AND 5258. REPAIRED IAW OHM 32-10-21. (M) 2 L 7 4 4F A20WE 1999052100423 19990521 00423 NM 1999 5 21 EIA990063 1 19990207 A 5312 BULKHEAD BOEING 747 747121 1384871 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, BS 1480 BULKHEAD AND SKIN INTERFACE AREA AT STRINGER 34L AND 34R, CRACKS WERE FOUND, NRC 6949 AND 6950. REPAIRED IAW RS R-53-61-34047, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100424 19990521 00424 NM 1999 5 21 EIA990062 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 980 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT BS 960-980 STRINGER 47L HAS EXFOLIATION, NRC 6173. REPAIRED STRINGER FR OM BS 950-980 IAW SRM 53-10-03. (M) 2 L 7 4 4F A20WE 1999052100425 19990521 00425 NM 1999 5 21 EIA990061 1 19990207 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 560 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 DURING C-CHECK, FORWARD CARGO COMPARTMENT BS 560 AT STRINGER 38R SUPPORT ANGLE FOUND CORRODED, NRC 6418. REPAIRED IAW S RM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100426 19990521 00426 NM 1999 5 21 EIA990060 1 19990207 A 5320 WEB BOEING 747 747121 1384871 NM BS 560 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT, BS 560 AT STRINGER 34R HORIZONTAL WEB LOWER SURFACE FOUND CRACKED, NRC 6331. REPAIRED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100427 19990521 00427 NM 1999 5 21 EIA990059 1 19990207 A 5330 SKIN BOEING 747 747121 1384871 NM BS 570 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FUSELAGE EXTERNAL SKIN, BS 570 AT EQUIPMENT COOLING DUCT OUTLET CUTOUT, IS CRACKED IN 3 FASTENER H OLES. REPAIRED IAW RS R-53-11-34043, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100428 19990521 00428 NM 1999 5 21 EIA990058 1 19990207 A 5320 CHORD BOEING 747 747121 1384871 NM BS 400 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD E/E BAY BS 400 STRINGER 44R LOWER CHORD HAS CORROSION, NRC 7166. REPAIRED IAW SRM 51-40-0 4. (M) 2 L 7 4 4F A20WE 1999052100429 19990521 00429 NM 1999 5 21 EIA990057 1 19990207 A 5311 FRAME BOEING 747 747121 1384871 NM BS 380 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 380 FRAME CRACKED AT STRINGER 24AL AND 24AR, NRC 6387 AND 6734. REPAIRED IAW RS R-53 -12-34025, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100430 19990521 00430 NM 1999 5 21 EIA990056 1 19990207 A 5312 BULKHEAD WEB BOEING 747 747121 1384871 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, DURING ACCOMP OF EO 53-747-1513-98B AND SB 747-53A2390 PLAN B, BS 1480 BULKHEAD INSPECTION MOD, RI GHT SIDE (4 EACH) FASTENER HOLES FOUND CRACKED, NR 16 AND NR 17 IN WEB SPLICE PLATE, NR 5 OUTER CHORD SPLICE AND NR 9 LO NGERON EXTENSION FITTING, NRC 7281, 7282, 7352 AND 7368. HOLES NR 16, NR 17 AND NR 5, WEB SPLICE PLATE AND OUTER CHORD SPLICE REPLACED IAW SB 53A2390, FOR HOLES NR 14, NR 15, NR 18 AND NR 19, SLEEVED BOLTS INSTALLED IAW SB 53A2390 FOR HOLE NR 9 OF LONGERON EXTENSION FITTING. REPAIR ACCOMPLISHED IAW RS R-53-43-34045, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100431 19990521 00431 NM 1999 5 21 EIA990055 1 19990207 A 5312 BULKHEAD WEB BOEING 747 747121 1384871 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, DURING ACCOMP OF EO 53-747-1513-98B AND SB 747-53A2390 PLAN B, BS 1480 BULKHEAD INSPECTION MOD, LE FT SIDE (3 EACH) FASTENER HOLES FOUND CRACKED, NR 23 AND NR 25 IN WEB SPLICE PLATE AND NR 6 LONGERON EXTENSION FITTING, NRC 7193-7195, 7185 AND 7332. ALL HOLES CLEANED AND CLEARED WITHIN SB LIMITS. (M) 2 L 7 4 4F A20WE 1999052100432 19990521 00432 NM 1999 5 21 EIA990054 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM WS 669.5 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, LEFT WING FUEL TANK AT WS 669.5 RIB UPPER CHORD SHEAR TIE FOUND CRACKED AT STRINGER 26, NRC 6749 A ND 6869. REPAIRED IAW SB 57-2273 REV 2. (M) 2 L 7 4 4F A20WE 1999052100433 19990521 00433 NM 1999 5 21 EIA990053 1 19990207 A 5414 SKIN BOEING 747 747121 1384871 NM NR 3 PYLON CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, NR 3 PYLON LEFT SKIN AT NAC STATION 235 INTERNAL AREA CHAFED AND EXTERNAL DOUBLER CRACKED, NRC 616 9. REPAIRED IAW SRM 54-30-03 FIG 35 AND 36. (M) 2 L 7 4 4F A20WE 1999052100434 19990521 00434 NM 1999 5 21 EIA990052 1 19990207 A 5414 SKIN BOEING 747 747121 1384871 NM NR 2 PYLON DISBONDED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, NR 2 PYLON LEFT SKIN DISBONDED NEAR MIDSPAR FITTING NRC 6678. REPAIRED IAW SRM 54-30-03. (M) 2 L 7 4 4F A20WE 1999052100435 19990521 00435 NM 1999 5 21 EIA990051 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2360 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK BS 2360 STRINGER 25R FOUND CRACKED, NRC 7063. REPAIRED STRINGER IAW SRM 53-10-03. (M) 2 L 7 4 4F A20WE 1999052100436 19990521 00436 NM 1999 5 21 EIA990050 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2360 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, MAIN DECK BS 2360 STRINGER 23R FOUND CRACKED, NRC 7063. REPAIRED STRINGER IAW SRM 53-10-03. (M) 2 L 7 4 4F A20WE 1999052100437 19990521 00437 NM 1999 5 21 EIA990049 1 19990207 A 5320 STRINGER BOEING 747 747121 1384871 NM BS 960 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK, BS 960 STRINGER 10L FOUND CRACKED, NRC 6956. REPAIRED STRINGER FROM 940-980 IAW SRM 53 -10-03. (M) 2 L 7 4 4F A20WE 1999052100438 19990521 00438 NM 1999 5 21 EIA990048 1 19990207 A 5320 TIE BOEING 747 747121 1384871 NM BS 880 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK, BS 880 STRINGER 8L AND 8R TENSION TIE FOUND CRACKED, NRC 6837-6838. REPAIRED IAW SB 53 -2371. (M) 2 L 7 4 4F A20WE 1999052100439 19990521 00439 NM 1999 5 21 EIA990047 1 19990207 A 5320 TIE BOEING 747 747121 1384871 NM BS 780 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK, BS 780 STRINGER 12L AND 12R TENSION TIE FOUND CRACKED, NRC 6776. REPAIRED IAW SB 53-23 71. (M) 2 L 7 4 4F A20WE 1999052100440 19990521 00440 NM 1999 5 21 EIA990046 1 19990207 A 5320 TIE BOEING 747 747121 1384871 NM BS 800 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK, BS 800 STRINGER 11L TENSION TIE FOUND CRACKED, NRC 6775. REPAIRED IAW SB 53-2371. (M) 2 L 7 4 4F A20WE 1999052100441 19990521 00441 NM 1999 5 21 EIA990045 1 19990207 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 460 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK, BS 460 FRAME SUPPORT ANGLE FOUND CRACKED AT STRINGER 15R, NRC 6735. REPAIRED IAW SRM 5 1-10-01. (M) 2 L 7 4 4F A20WE 1999052100442 19990521 00442 NM 1999 5 21 EIA990044 1 19990207 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 440 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK, BS 440 FLOORBEAM UPPER CHORD AND INTERCOSTAL WEB CRACKED AT LBL 66, NRC 5721 AND 5722. REPAIRED FLOORBEAM FROM BL 0 - LBL 75 AND INTERCOSTAL WEB IAW SRM 53-10-07. (M) 2 L 7 4 4F A20WE 1999052100443 19990521 00443 NM 1999 5 21 EIA990043 1 19990207 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2387 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, EMPENNAGE EXTERIOR SKIN DENTED IN 2 SPOTS AT BS 2387 AT STRINGER 38R AND 46R, NRC 6174. REPAIRED PER SRM 53-30-03 FIG 4B. (M) 2 L 7 4 4F A20WE 1999052100444 19990521 00444 NM 1999 5 21 EIA990042 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1900 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1900 SHEAR TIE FOUND CRACKED BETWEEN STRINGER 43L-47L, NRC 6308-6311. R EPAIRED IAW SRM 53-10-04. (M) 2 L 7 4 4F A20WE 1999052100445 19990521 00445 NM 1999 5 21 EIA990041 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1900 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1900 SHEAR TIE FOUND CRACKED BETWEEN STRINGER 49R AND 50R, NRC 6307. RE PAIRED IAW SRM 53-10-04. (M) 2 L 7 4 4F A20WE 1999052100446 19990521 00446 NM 1999 5 21 EIA990040 1 19990207 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1720 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1720 FLOORBEAM WEB CRACKED AT LBL 25, NRC 6060. REPAIRED IAW SRM 51-40- 02. (M) 2 L 7 4 4F A20WE 1999052100447 19990521 00447 NM 1999 5 21 EIA990039 1 19990207 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1720 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1720 FLOORBEAM WEB CRACKED AT LBL 25, NRC 6060. REPAIRED IAW SRM 51-40- 02. (M) 2 L 7 4 4F A20WE 1999052100448 19990521 00448 NM 1999 5 21 EIA990038 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1700 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1700 FRAME SHEAR TIE CRACKED AT STRINGER 51L AND 50R, NRC 6059 AND 6061. REPAIRED IAW SRM 53-10-04 BETWEEN STRINGER 50R AND 51L. (M) 2 L 7 4 4F A20WE 1999052100449 19990521 00449 NM 1999 5 21 EIA990037 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1680 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1680 FRAME SHEAR TIE CRACKED AT STRINGER 50R, NRC 6058. REPAIRED IAW SR M 53-10-04. (M) 2 L 7 4 4F A20WE 1999052100450 19990521 00450 NM 1999 5 21 EIA990036 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1665 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1660 FRAME SHEAR TIE CRACKED AT STRINGER 48R, NRC 6057. REPAIRED IAW SR M 53-10-04 BETWEEN STRINGER 48L-49L. (M) 2 L 7 4 4F A20WE 1999052100451 19990521 00451 NM 1999 5 21 EIA990035 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1640 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, AFT CARGO COMPARTMENT, BS 1640 FRAME SHEAR TIE CRACKED AT STRINGER 51R, NRC 6172. REPAIRED IAW SR M 53-10-04 BETWEEN STRINGER 51L AND 51R. (M) 2 L 7 4 4F A20WE 1999052100452 19990521 00452 NM 1999 5 21 EIA990034 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 820 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT, BS 820 FRAME SHEAR TIE CRACKED AT STRIGNER 38R, NRC 6323. REPAIRED IAW SRM 53-10-04 BETWEEN STRINGER 37R AND 38R. (M) 2 L 7 4 4F A20WE 1999052100453 19990521 00453 NM 1999 5 21 EIA990033 1 19990207 A 5311 FRAME BOEING 747 747121 1384871 NM BS 820 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT, BS 820 FRAME CRACKED AT STRINGER 33R, NRC 6323. REPAIRED IAW SRM 53-10 -04. (M) 2 L 7 4 4F A20WE 1999052100454 19990521 00454 NM 1999 5 21 EIA990032 1 19990207 A 5330 SKIN BOEING 747 747121 1384871 NM BS 240-260 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FUSELAGE SKIN CRACKED FROM BS 240-260 BETWEEN STRINGER 41L AND 42L, NOSE LANDING GEAR WHEEL WELL F ORWARD CORNER, NRC 5728. REPAIRED IAW SB 53-2112 REV 7 AND DRAWING 141U1098. (M) 2 L 7 4 4F A20WE 1999052100455 19990521 00455 NM 1999 5 21 EIA990031 1 19990207 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 2000 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, BULK CARGO COMPARTMENT, BS 2000 FLOORBEAM CRACKED FROM RBL 9 - RBL 19, NRC 6436. REPLACED FLOORBE AM FROM LBL 51 - RBL 35 IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052100456 19990521 00456 NM 1999 5 21 EIA990030 1 19990207 A 5311 FRAME BOEING 747 747121 1384871 NM BS 360 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK AT BS 360 FRAME FOUND CRACKED AT STRINGER 24A LEFT SIDE, NRC 6391. REPAIRED IAW RS R-53 -12-34026, 8110-3, AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100457 19990521 00457 NM 1999 5 21 EIA990029 1 19990207 A 5320 WEB BOEING 747 747121 1384871 NM BS 360 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 DURING C-CHECK, MAIN DECK AT BS 360 SUPPORT WEB FOUND CRACKED AT STRINGER 24R, NRC 6733. REPAIRED IAW SRM 51-40-03. (M ) 2 L 7 4 4F A20WE 1999052100458 19990521 00458 WP 1999 5 21 EIAA990006 1 19990222 A 2910 LINE DOUG DC9 DC933F 302207A WP LT TE FLAP ACT FAILED A EIAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 09 933F 47191 SEA - ON DEPARTURE FROM KSEA NOTED A LOSS OF HYDRAULIC FLUID QUANTITY, LEFT SIDE. CREW RETURNED AIRCRAFT TO KSEA WITHOU T FURTHER INCIDENT. MAINTENANCE PERSONEL FOUND FLAP ACTUATOR LINE CRACKED AND INSTALLED A FLEX LINE PER GP/P AND MB 87- 19. TRANSFERRED FLEX LINE TO CARRY OVER ITEM 870 UNTIL PERMANENT REPAIR. (M) 2 L 7 2 4F A6WE 1999052100459 19990521 00459 WP 1999 5 21 EIAA990004 1 19990227 A 3231 RETRACT MECH DOUG DC9 DC933F 302207A WP NLG DOOR MALFUNCTIONED A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 945F 47279 DEN - ON DEPARTURE FROM DEN, THE FLIGHT CREW, UPON ATTEMPTING TO RAISE THE LANDING GEAR, RECEIVED THE GEAR DOOR OPEN LIG HT ILLUMINATION AND THREE RED GEAR UNSAFE LIGHTS. AFTER RECYCLING THE GEAR HANDLE TO THE DOWN POSITION THE CREW RECEIVE D THREE GREEN LANDING GEAR LIGHTS BUT THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. AIRCRAFT THEN RETURNED TO DEN. SU BSEQUENTLY UPON LANDING, BOTH MAIN GEAR DOORS WERE DAMAGED. CREW REPORTED NO FURTHER INCIDENT. (M) 2 L 7 2 4F A6WE 1999052100460 19990521 00460 WP 1999 5 21 EIA990114 1 19990420 A 3297 G213A24N WIRE DOUG DC9 DC915F 3022037 WP NLG BROKEN A EIAA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 915F 47061 PHX - ON FINAL APPROACH, GEAR DOWN LIGHTS DID NOT FUNCTION. CREW UNABLE TO VERIFY GEAR POSITION, DECLARED EMERGENCY AND REQUESTED EQUIPMENT. REPAIRED BROKEN WIRE AT NOSE GEAR LOCK SWITCH. NOSE GEAR INDICATION OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999052100461 19990521 00461 NM 1999 5 21 EIAA990028 1 19990207 A 5311 FRAME BOEING 747 747121 1384871 NM BS 340 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK AT BS 340 FRAME FOUND CRACKED AT STRINGER 24A LEFT SIDE, NRC 6388. REPAIRED IAW RS R-53 -12-34024, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100462 19990521 00462 NM 1999 5 21 EIAA990027 1 19990207 A 5311 FRAME BOEING 747 747121 1384871 NM BS 340 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, UPPER DECK, BS 340 FRAME UPPER CHORD FOUND CRACKED AT STRINGER 0, NRC 6306. REPAIRED IAW SRM 51-4 0-03. (M) 2 L 7 4 4F A20WE 1999052100463 19990521 00463 NM 1999 5 21 EIA990026 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 280 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, MAIN DECK, BS 280 FRAME CRACKED AT LEFT STRINGER 24A, NRC 6390. REPAIRED IAW HAECO RS R-53-12-340 30, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100464 19990521 00464 NM 1999 5 21 EIA990025 1 19990207 A 5412 BULKHEAD WEB BOEING 747 747121 1384871 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, NR 3 PYLON REAR MOUNT BULKHEAD AFT OUTBOARD LOWER WEB FOUND CRACKED, NRC 6783. REPLACED IAW SRM 5 1-10-01 FWD AND AFT FRAME REPLACED. (M) 2 L 7 4 4F A20WE 1999052100465 19990521 00465 NM 1999 5 21 EIA990024 1 19990207 A 5412 BULKHEAD BOEING 747 747121 1384871 NM NR 3 PYLON MISDRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, NR 3 PYLON AFT VERTICAL BULKHEAD BOTH LEFT AND RIGHT CHORD LOWER PORTION, FOUND 10 MISDRILLED HOLE S, NRC 6339 AND 6340. REPAIRED IAW HAECO RS R-54-53-33997, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100466 19990521 00466 NM 1999 5 21 EIA990023 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 860 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT AT BS 860 SHEAR TIE CRACKED AT STRINGER 29L, NRC 6407. REPAIRED IAW HAE CO RS R-53-22-34022, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100467 19990521 00467 NM 1999 5 21 EIA990022 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 860 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT AT BS 860 SHEAR TIE CRACKED AT STRINGER 28L, NRC 6405. REPAIRED IAW HAE CO RS R-53-22-34022, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100468 19990521 00468 NM 1999 5 21 EIA990021 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 860 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT AT BS 860 SHEAR TIE CRACKED AT STRINGER 29R, NRC 6322. REPAIRED IAW HAE CO RS R-53-22-34022, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100469 19990521 00469 NM 1999 5 21 EIA990020 1 19990207 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 860 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, FORWARD CARGO COMPARTMENT AT BS 860 SHEAR TIE CRACKED AT STRINGER 28R, NRC 6321. REPAIRED IAW HAE CO RS R-53-22-34022, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100470 19990521 00470 NM 1999 5 21 EIAA990019 1 19990207 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 140-160 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURIGN C-CHECK, MAIN DECK FLOOR INTERCOSTAL WEB CRACKED AT LEFT AND RIGHT OUTBOARD CORNERS BS 140-160, NRC 6319 AN D 6318. REPAIRED IAW SRM 51-10-01 COMPLETE REPLACEMENT. (M) 2 L 7 4 4F A20WE 1999052100471 19990521 00471 NM 1999 5 21 EIA990018 1 19990207 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 440 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 HKG - DURING C-CHECK, UPPER DECK FLOORBEAM CRACKED AT BS 440 AT RBL 65, NRC 6431. REPAIRED IAW HAECO RS R-53-15-34037, 8110-3 AND ECRA. (M) 2 L 7 4 4F A20WE 1999052100476 19990521 00476 NM 1999 5 21 EIA990013 1 19990301 A 5313 STRINGER BOEING 747 747131 1384881 NM BS 1805 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 472EV 20320 DURING MODIFICATION AND C-CHECK, MAIN CABIN, STRINGER 8R AT BS 1805 STRINGER IS EXFOLIATED, NRC 13-6522. REPAIRED IAW S RM 53-10-03 FIG 5. (M) 2 L 7 4 4F A20WE 1999052100477 19990521 00477 NM 1999 5 21 EIA990012 1 19990301 A 5313 STRINGER BOEING 747 747131 1384881 NM BS 1960-2160 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 472EV 20320 DURING MODIFICATION AND C-CHECK, MAIN CABIN, STRINGER 2R FROM BS 1960-2160, STRINGER IS EXFOLIATED, NRC 13-6560. REPAIR ED BY REPLACEMENT OF STRINGER SECTION AT PRODUCTION SPLICES IAW SRM 51-30-02. (M) 2 L 7 4 4F A20WE 1999052100478 19990521 00478 NM 1999 5 21 EIA990011 1 19990301 A 5313 STRINGER BOEING 747 747131 1384881 NM BS 2200 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 472EV 20320 DURING MODIFICATION AND C-CHECK, MAIN CABIN, STRINGER 3R AT BS 2200 STRINGER IS EXFOLIATED, NRC 13-6560. REPAIRED IAW S RM 53-10-03. (M) 2 L 7 4 4F A20WE 1999052100479 19990521 00479 NM 1999 5 21 EIA990010 1 19990301 A 5313 STRINGER BOEING 747 747131 1384881 NM BS 630-650 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 472EV 20320 DURING MODIFICATION AND C-CHECK, FORWARD CARGO COMPARTMET AT BS 630 -650 STRINGER 43R CRACKED, NRC 13-6726. REPAIRED IA W ECRA 472-53-513-2. (M) 2 L 7 4 4F A20WE 1999052100480 19990521 00480 NM 1999 5 21 EIA990009 1 19990301 A 5320 FRAME BOEING 747 747131 1384881 NM CARGO DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 472EV 20320 DURING MODIFICATION AND C-CHECK, FORWARD CARGO COMPARTMENT AT BS 600 AND 680 DOOR FRAMES GAUGED, FROM DOOR ACTUATOR MOVE MENT, NRC ZZ-6850. REPAIRED IAW ECRA 472-53-444-2. (M) 2 L 7 4 4F A20WE 1999052100481 19990521 00481 NM 1999 5 21 EIA990008 1 19990301 A 5311 FRAME BOEING 747 747131 1384881 NM BS 570 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 472EV 20320 DURING MODIFICATION AND C-CHECK, FORWARD CARGO COMPARTMENT AT BS 570 LATERAL FRAME IS CRACKED IN SEVERAL PLACES, NRC NR 13-6635. REPAIRED IAW SRM 53-30-21 FIG 5 AND 51-30-02. (M) 2 L 7 4 4F A20WE 1999052100491 19990521 00491 NE 1999 5 21 EIAA990005 2 19990308 A 7200 ENGINE BOEING 747 747SR46 NM PWA JT9 JT9D7AH 52054 NE NR 3 MALFUNCTIONED A EIAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 477EV 20784 662470 JFK - DURING FLIGHT FROM LFPG TO KJFK, FLIGHT CREW REPORTED OIL LOSS FROM THE NR 3 ENGINE. CREW PERFORMED A PRECAUTIONA RY SHUTDOWN OF THE SUBJECT ENGINE AND CONTINUED FLIGHT. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999052100492 19990521 00492 SO 1999 5 21 C2XA99IA235 1 19990321 A 5411 12037467001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT REAR NACELLE FRAME CRACKED ABOVE REAR SPAR. FABRICATED AND IN STALLED REPAIR DOBLERS IAW SRM 51-70-05 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999052100493 19990521 00493 SO 1999 5 21 C2XA99IA236 1 19990321 A 3350 324002102 BATTERY EMB 120 EMB120RT SO ROW 8 DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 57734 120199 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND EMERGENCY LIGHTING INOPERATAIVE FROM ROW 8 TO AFT. REPLACED BATTER Y PACK IN AFT EMERGENCY LIGHTING POWER UNIT IAW AMM 33-50-02 AND CMM 33-51-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999052100494 19990521 00494 SO 1999 5 21 C2XA99IA237 1 19990321 A 5320 12033696003 FIRE WALL EMB 120 EMB120RT SO APU COMPT CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND APU FIRE WALL CRACKED AT FIRE BOTTLE DISCHARGE TUBE. FABRICATED RE PAIR DOUBLER AND INSTALLED IAW EC5330-01102. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999052100495 19990521 00495 SO 1999 5 21 C2XA99IA238 1 19990321 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO FRAME 32-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAME 32 TO 39. REPLACED SEA T TRACK IAW EC25-10-01016. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999052100496 19990521 00496 SO 1999 5 21 C2XA99IA239 1 19990321 A 5320 12004449001 BEAM EMB 120 EMB120RT SO FRAME 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FRAME 40 CROSSBEAMS CORRODED. REMOVED CORROSION FROM LEFT BEAMS. R EMOVED AND INSTALLED NEW RIGHT BEAMS IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999052100497 19990521 00497 SO 1999 5 21 C2XA99IA224 1 19990419 A 3234 12038594001 SELECTOR EMB 120 EMB120RT SO LANDING GEAR INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 31711 120107 IAH - DURING TAKEOFF ON FLIGHT 3660, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE GEAR RETRACTION HANDLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999052100498 19990521 00498 EU 1999 5 21 C2XA99IA222 1 19990420 A 3350 4241601 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING A-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR 42-320 JIC 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1999052100499 19990521 00499 SO 1999 5 21 C2XA99IA221 1 19990411 A 5530 14531597601 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12934 145019 IAH - DURING C-CHECK INSPECTION, FOUND THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE TO BE CRCKED. MAINTENANCE RE MOVED AND REPLACED THE FORWARD SECTION OF THE DRAG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC533 0-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052100500 19990521 00500 SO 1999 5 21 C2XA99IA220 1 19990411 A 5530 14531597602 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12934 145019 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATI ON EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052100501 19990521 00501 SO 1999 5 21 C2XA99IA219 1 19990411 A 5315 14522459001 FLOORBEAM EMB 145 EMB145 SO FRAME 20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12934 145019 IAH - DURING C-CHECK INSPECTION, FOUND THE CENTER FLOORBEAM CORRODED AT FRAME 20 UNDER COMPOSITE FLOOR PANEL SUPPORT. M AINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF FLOORBEAM IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052100502 19990521 00502 SO 1999 5 21 C2XA99IA218 1 19990411 A 3397 7287550505 WIRE EMB 145 EMB145 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12934 145019 IAH - DURING C-CHECK INSPECTION, FOUND THE NR 1 CABIN FLOOR EMERGENCY LIGHTS STRIP TO HAVE A BROKEN WIRE. MAINTENANCE R EMOVED AND REPLACED THE LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052100503 19990521 00503 SO 1999 5 21 C2XA99IA217 1 19990411 A 5315 FLOORBEAM EMB 145 EMB145 SO FRAME 20 CORRODED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12934 145019 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FLOORBEAM CORRODED AT FRAME 20 UNDER COMPOSITE FLOOR PANEL SUPPORT. MAINTEN ANCE REMOVED THE CORROSION, AND INSTALLED A REPAIR DOUBLER ON THE FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/R EPAIR AUTHORIZATION EC5310-01101. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052100504 19990521 00504 SO 1999 5 21 LR7A9942 1 19990515 A 2150 203430 TURBINE LKHEED 382 382G 526414U SO BS 215 FAILED A LR7A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 401LC 4606 FLIGHT DECK AIR CONDITIONING MAKES LOUD WHINE NOISE AND PRODUCED ODOR. REPLACED FLIGHT STATION COOLING TURBINE PER SMP 581 21-50, PG 213-214. LEAK AND OPS CHECK OK. 2 H 7 4 4T A1SO 1999052100505 19990521 00505 NM 1999 5 21 PCAA9900013 1 19990518 A 3230 UPLOCK DHAV DHC8 DHC8102 2809003 NM LT MLG DIRTY A PCAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 13 843EX 335 FLT 3968- BWI-UPON GEAR SELECTION DOWN, THE LEFT MAIN GEAR DID NOT EXTEND. ALTERNATE GEAR EXTENSION WAS PERFORMED SATIS FACTORY. AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED EXTENSION SYSTEM, CLEANED UPLOCK ROLLERS, OPERATED GEAR SEVERAL TIMES. GEAR OPERATED NORMALLY. REMOVED AND REPLACED THE PSEU AS A PRECAUTIONARY MEASURE (NO FAULT CODES). 2 H 7 2 4T RT A13NM 1999052100506 19990521 00506 NM 1999 5 21 CALA9900546 1 19990517 A 5753 652163092 SKIN BOEING 727 727224 1384076 NM RT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND RT WING I/B FOREFLAP BULLNOSE LOWER SIDE ABOVE CENTER HINGE POINT GOUGED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-50-00. 2 L 7 3 4F A3WE 1999052100507 19990521 00507 NM 1999 5 21 CALA9900547 1 19990517 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1035 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND CABIN FLOOR PANEL SUPPORT CORRODED AT STA 1035, RBL 15 TO RBL 62. THE CORROSION WAS REMOVED IAW SRM 51 -6-1. THE SUPPORT WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 1 AND 51-10-1, PAGE 4. 2 L 7 3 4F A3WE 1999052100508 19990521 00508 NM 1999 5 21 CALA9900548 1 19990517 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 1178 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND CABIN FLOOR CHORD ANGLE AT STA 1178, RBL 46 CORRODED AROUND LAV TANK AFT I/B MOUNT BOLT. THE CORRODED AREA WAS REMOVED AND A REINFORCEMENT CHORD REPAIR WAS INSTALLED IAW ECRA 5310-01585. 2 L 7 3 4F A3WE 1999052100509 19990521 00509 NM 1999 5 21 CALA9900549 1 19990517 A 5753 6521630187 SKIN BOEING 727 727224 1384076 NM LT TE FOREFLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND LEFT I/B FOREFLAP UPPER SKIN DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1. 2 L 7 3 4F A3WE 1999052100510 19990521 00510 WP 1999 5 21 CALA9900550 1 19990514 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 37 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 37 AND LONGERON 17. THE DENTED AREA WAS CUT OUT AND A DOUBLER REPAIR WA S INSTALLED IAW SRM 53-04-00, FIGURE 38, PAGE 218J, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999052100511 19990521 00511 WP 1999 5 21 CALA9900551 1 19990514 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .5 INCH CRACK WITH CORROSION IN LOWER FUSELAGE SKIN JUST FORWARD OF BEACON LIGHT. THE CRACKED AREA W AS CUT OUT, THE CORROSION WAS REMOVED IAW SRM 51-10-3. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, PAGE 218A. 2 L 7 2 4F A6WE 1999052100512 19990521 00512 NM 1999 5 21 UPS99229621 1 19990428 A 5311 FRAME BOEING 727 727180C 138406G NM BS 783.95 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, MECHANICAL DAMAGE FOUND ON SECOND FASTENER HOLE ABOVE FLOOR AT BS 783.95 LT. AFTER CLEAN UP, HOLE WA S OUTSIDE LIMITS PER EO B727-5310- 5474 PAGE 9. DAMAGED HOLE TAKEN TO 0.370 AND FREEZE PLUG INSTALLED IAW SRM 51-10- 7 REF SMRO EO 99-12-002 AND UPS EO B727-5310-11383-A. REPAIR TO FRAME RESULTING FROM OVERSIZING OF HOLE, CARRIED OUT IAW EO B727-5310-5474 APPX C. 2 L 7 3 4F A3WE 1999052100513 19990521 00513 NM 1999 5 21 UPS99229623 1 19990428 A 5311 FRAME BOEING 727 727180C 138406G NM BS 848.95 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, MECHANICAL DAMAGE ON SECOND FASTENER HOLE ABOVE FLOOR AT BS 848.95 LT. ON CLEAN UP, HOLE WAS OUTSIDE LIMITS PER PAGE 9 OF EO B727-5310 -5474. REPAIR TO FRAME CARRIED OUT IAW EO B727-5310-5474 APPENDIX C REF SMRO EO 99-1 2-002 AND UPS EO B727-5310-11383 FOR FREEZE PLUG INSTALLATION. 2 L 7 3 4F A3WE 1999052100514 19990521 00514 NM 1999 5 21 UPS99229624 1 19990428 A 5347 SEAT TRACK BOEING 727 727180C 138406G NM BS 770 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, TO FACILITATE REPAIR OF FRAME 783.95 LT, SEAT TRACK MUST BE REMOVED. ON REMOVAL, SEAT TRACK WAS FOUN D TO BE CORRODED AT BS 770 LBL 62.5. NEW SEAT TRACK SECTION SPLICED IAW SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 1999052100515 19990521 00515 NM 1999 5 21 UPS99229625 1 19990510 A 5320 ANGLE BOEING 727 727180C 138406G NM BS 700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, CORROSION ON 'T' ANGLE ON FAIRING UNDER AIR CONDITIONING EQUIPMENT AT BS 700. REPAIRES IAW SRM 51-40 -2 FIG 1. 2 L 7 3 4F A3WE 1999052100516 19990521 00516 NM 1999 5 21 UPS99229626 1 19990507 A 5744 65192609 HINGE BOEING 727 727180C 138406G NM WS 686.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, RIGHT O/B AILERON HINGE CASTING CRACKED AT WS 68605 APPROX (I/B CASTING I/B BALANCE BAY). REPLACED C ASTING IAW DRG 65-19260. 2 L 7 3 4F A3WE 1999052100517 19990521 00517 NM 1999 5 21 UPS99229627 1 19990506 A 5320 FRAME BOEING 727 727180C 138406G NM CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, FRAME CRACKED SECOND FROM AFT AT MID TRACK ATTACH POINT ON AFT CARGO DOOR MOVABLE FAIRING. FRAME REP AIRED IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1999052100518 19990521 00518 NM 1999 5 21 UPS99229628 1 19990505 A 5751 6524646501 HINGE BOEING 727 727180C 138406G NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, RIGHT I/B AILERON CENTER HINGE FITTING CORRODED. REPLACED HINGE FITTING IAW MM 27-10-01. 2 L 7 3 4F A3WE 1999052100519 19990521 00519 NM 1999 5 21 UPS99229631 1 19990519 A 3350 BATTERIES BOEING 727 7272A1 138407F NM EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT OVER MAIN FWD ENTRY DOOR INOP. CHANGED BATTERIES IN BATTERY PACK, OPS CKS GOO D. 2 L 7 3 4F A3WE 1999052100520 19990521 00520 NM 1999 5 21 UPS99229634 1 19990517 A 5280 DOOR BOEING 727 727247 138408F NM RT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:N/A, RIGHT WING GEAR FLYING DOOR, FWD AND AFT OF HINGE PANEL AREA, SKIN CRACKED UNDER AND BEYOND DOUBLER . REMOVED EXISTING DOUBLER, STOP DRILLED CRACKS, INSTALLED DOUBLER PER SRM 52-80-2 FIG 2. 2 L 7 3 4F A3WE 1999052100521 19990521 00521 WP 1999 5 21 UPS99829630 1 19990518 A 2450 50130003 BUS PANEL DOUG DC8 DC871F 302199D WP COCKPIT SMOKED A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 702UP 45902 INSPECTION TYPE:N/A, WHEN GEN RELAY NR 1 CLOSED ON STARTUP, PASSING 45 PERCENT N2, NR 1 BUS PWR FAIL LIGHT ILLUMINATES W ITH SMOKE AND ELECTRICAL BURNING SMELL IN COCKPIT BTB (AC VOLTS AND FREQS NORMAL, NO A/C LOAD) 5/18/99 0420Z. REMOVED A ND REPLACED BUS PROTECTION PANEL (S/N 584) ON, (S/N 815) OFF, (P/N 50130-003 R7R GEN RELAY (P/N 50137-002) (S/N 4662ML) ON, (S/N 3926ML) OFF. REMOVED AND REPLACED REG AND CONTROL PANEL (P/N 51508-000) (S/N 1070BC) ON. RUN ALL ENG, ALL GE N CKS NORMAL. 2 L 7 4 4F RT 4A25 1999052100522 19990521 00522 WP 1999 5 21 UPS99829633 1 19990518 A 2910 FITTING DOUG DC8 DC871F 302199D WP RUDDER LEAKING A IPXA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 707UP 45907 INSPECTION TYPE:N/A, AFTER MORE INVESTIGATION FOUND DURING CRUISE ACFT HAD ERRATIC HYD SYSTEM PRESSURE FOLLOWED BY HYD F LUID LOSS DOWN TO STANDPIPE FLUID. DECLARED EMERGENCY, LANDING IN SDF WAS UNEVENTFUL. OBTAINED FLAPS 3 5 FOR LDG AND N ORMAL GEAR FREE FALL. MX FOUND HYDRAULIC RUDDER PRESSURE SWITCH LEAKING AT 3 FITTINGS. UNION SECURED ALL FITTINGS AND REMOVED AND REPLACED O-RING AT UNION BB08473 2. OPS AND LEAK CHECKS GOOD PER MM 29-30-07. 2 L 7 4 4F RT 4A25 1999052100523 19990521 00523 WP 1999 5 21 UPS99829635 1 19990518 A 5610 WINDOW DOUG DC8 DC873F 302199F WP RT COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE:N/A, F/O SLIDE WINDOW WILL ONY OPEN INTERMITTENTLY. ADJUSTED F/O CLEARVIEW WINDOW PER MM 56-10-03, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999052100524 19990521 00524 WP 1999 5 21 UPS99829636 1 19990510 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 55 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999052100525 19990521 00525 NM 1999 5 21 QXEA9901055 1 19990513 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - CHAFE DAMAGE ON LEADING EDGE OF OUTBOARD FLAP APPROXIMATELY 24 INCHES FROM OUTBOARD END. REPAIRED IAW HORIZON AIR EA 2-57-10. 2 H 7 2 4T RT A13NM 1999052100526 19990521 00526 NM 1999 5 21 QXEA9901056 1 19990513 A 5240 DOOR DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - NR 1 ENGINE SIDE DOOR PANEL 414AR LOWER FLANGE BY DATA PLATE TORN. REPAIRED IAW DASH 8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999052100527 19990521 00527 NM 1999 5 21 QXEA9901057 1 19990507 A 5311 CASTELLATION DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - REAR FUSELAGE INTERNAL FRAME NR 4 CASTELLATION AT 11:00 AND 1:00 POSITION ARE CRACKED. REPAIRED IAW HORIZON AIR E A 2-55-16. 2 H 7 2 4T RT A13NM 1999052100528 19990521 00528 NM 1999 5 21 QXEA9901058 1 19990511 A 5250 BRACKETS DHAV DHC8 DHC8202 2809007 NM COCKPIT DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - COCKPIT DOOR UPPER AND CENTER HINGE BRACKETS ARE WORN BEYOND LIMITS. REPAIRED IAW HORIZON AIR EA 2-52-18. 2 H 7 2 4T RT A13NM 1999052100529 19990521 00529 NM 1999 5 21 QXEA9901059 1 19990510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 240 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - CORROSION ON INBOARD RIGHT-HAND SEAT TRACK AFT OF STATION 240. REPAIRED IAW HORIZON AIR EA 2-53-26. 2 H 7 2 4T RT A13NM 1999052100530 19990521 00530 NM 1999 5 21 QXEA9901060 1 19990510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 222 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - CORROSION ON INBOARD RIGHT-HAND SEAT TRACK FORWARD OF STATION 222. REPAIRED IAW HORIZON AIR EA 2-53-26. 2 H 7 2 4T RT A13NM 1999052100531 19990521 00531 NM 1999 5 21 QXEA9901061 1 19990511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 240 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - CORROSION ON INBOARD LEFT-HAND SEAT TRACK FORWARD OF STATION 240. REPAIRED IAW HORIZON AIR EA 2-53-26. 2 H 7 2 4T RT A13NM 1999052100532 19990521 00532 NM 1999 5 21 QXEA9901062 1 19990510 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 252 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - CORROSION ON INBOARD RIGHT-HAND SEAT TRACK AT STATION 252. REPAIRED IAW HORIZON AIR EA 2-53-26. 2 H 7 2 4T RT A13NM 1999052100533 19990521 00533 NM 1999 5 21 QXEA9901063 1 19990512 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 & 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - RIGHT HAND SEAT TRACK EXTENSION IN BAGGAGE FLOOR HAS CORROSION WHERE O-RINGS MOUNT AT STATION 545 AND STATION 600. REPAIRED IAW DASH 8 RD 8-53-784. 2 H 7 2 4T RT A13NM 1999052100534 19990521 00534 NM 1999 5 21 QXEA9901064 1 19990511 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 & 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 345PH 476 PDX - LEFT-HAND SEAT TRACK EXTENSION IN BAGGAGE FLOOR HAS CORROSION WHERE O-RINGS MOUNT AT STATION 545 AND STATION 600. REPAIRED IAW DASH RD 8-53-784. 2 H 7 2 4T RT A13NM 1999052100535 19990521 00535 NM 1999 5 21 99FDEA00182 1 19990519 A 5311 651634112 FRAME BOEING 727 727247 138408F NM BS 1010 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 FOUND BS 1010 FRAME TO BE CRACKED AT RBL 18, WL 149. *S/D* REMOVED AND REPLACED FRAME PER IAW FEDEX EA 7-5310-45281. 2 L 7 3 4F A3WE 1999052100536 19990521 00536 1999 5 21 DL76L991011 4 19990508 A 2330 ENTERTAIN SYST BOEING 767 767332 1382001 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 177DN 25122 PASSENGER ENTERTAINMENT SYSTEM BEGAN TO SMELL HOT IN FRONT CLOSET AREA. SYSTEM SHUT DOWN BY CREW UTILIZING SAFETY SWITC HES. BUSINESS CLASS MID-CABIN WALL SCREENS REMAINED ILLUMINATED WITH STATIC AND WE WERE UNABLE TO SHUT THEM OFF. ALSO ECONOMY SCREENS REMAINED ILLUMINATED. PULLED J1/J2/J3 C/BS ON PANEL 37, NO HELP. PER ROCKWELL(JFK)-REMOVED AND INSPECT ED ALL LRU'S, NO FAULTS. VIDEO CTL CTR TURNED OFF, OVHD C/B'S PULLED. FWD TO MCO. PER ROCKWELL(ATL)-SYSTEM ACTIVATED, RESET ALL C/B'S. REMOVED ALL BLANKETS AND PILLOWS FROM AREA. SYSTEM OK, REMOVED MCO. 2 L 7 2 4F RT A1NM 1999052100537 19990521 00537 1999 5 21 DL767991014 4 19990508 A 2330 BACR13CC1 RELAY BOEING 767 767232 1385132 NM E/E COMPT FAILED A DALA K NONE M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 101DA 22213 RELAY K459 SHORTED OUT IN P-33 PANEL, CAUSING ELECTRICAL SHORT. REMOVED P33 PANEL. REPLACED K459 RELAY. FOUND HEAT DA MAGE ON TB090. REPLACED ALL HIGH DENSITY BLOCKS AND RE-TERMINATED WIRING. REPLACED NUMEROUS RELAYS FOR POSSIBLE HEAT D AMAGE. PERFORMED CARGO HEAT TEST, T/E SYSTEM TEST, AFT BULK COMPARTMENT TEST, PASSENGER ENTERTAINMENT TEST AND ALL OK. 2 L 7 2 4F RT A1NM 1999052100538 19990521 00538 NM 1999 5 21 DL72S991026 1 19990510 A 7930 102446123S CONNECTOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LOOSE A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 493DA 21062 696580 AFTER TAKEOFF, NR 2 OIL TEMP GAUGE FLUCTUATED FOR 10 SEC AND THEN PEGGED OUT HIGH. RAN CHECKLIST AND SHUT DOWN ENGINE. REPLACED CANNON PLUG AT TEMP BULB. 2 L 7 3 4F 4 F A3WE E2EA 1999052100539 19990521 00539 NE 1999 5 21 DL757991027 2 19990510 A 7230 COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE STALLED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 613DL 42194 22820 716310 COMPRESSOR STALL WITH ENGINE ROLLBACK TO IDLE, NR 1 ENGINE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052100540 19990521 00540 NM 1999 5 21 DL72W991029 1 19990510 A 5755 ANGLE BOEING 727 727247 138408F NM NR 8 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 A 1.5 INCH CRACK IN SUPPORT ANGLE FWD OF NR 8 SPOILER. REPAIRED PER MM 57-20-22 FIG 806. 2 L 7 3 4F A3WE 1999052100541 19990521 00541 NM 1999 5 21 DL72W991030 1 19990510 A 5754 ANGLE BOEING 727 727247 138408F NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 COVE SKIN ATTACH ANGLE CRACKED BELOW I/B STOP PAD NR 8 SLAT. REPAIRED PER MM 57-54-0 FIG 812. 2 L 7 3 4F A3WE 1999052100542 19990521 00542 NM 1999 5 21 DL72S991031 1 19990401 A 5753 652163242 SPAR BOEING 727 727225A 1384077 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 TWO CRACKS AT AFT SPAR RAIL, 34 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F RT A3WE 1999052100543 19990521 00543 NM 1999 5 21 DL72S991032 1 19990401 A 5753 652163242 SPAR BOEING 727 727225A 1384077 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 TEMPORARY REPAIR AFT SPAR RAIL, 47 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F RT A3WE 1999052100544 19990521 00544 NM 1999 5 21 DL72S991033 1 19990401 A 5753 652163242 SPAR BOEING 727 727225A 1384077 NM RT TE FLAP CRACKED A DALA O OTHER K FLUID LOSS IN INSP/MAINT 1 SO 27 8875Z 21293 AFT SPAR RAIL CRACKED, 62 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F RT A3WE 1999052100545 19990521 00545 1999 5 21 DLL14991035 4 19990510 A 2210 COMPUTER LKHEED 1011 1011385115 5265015 WP NR 2 YAW DAMPER MALFUNCTIONED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 1739D 193C1237 PILOT REPORT, IN FLIGHT WHEN USING EITHER 'A' OR 'B' A/P AIRPLANE CONSTANT DUTCH ROLLS. IN CRUISE ON A/P 'A' NR 1 HDG F LAG COMES INTO VIEW AND A/P DISCONNECTS. USING A/P 'B' IN SMOOTH AIR 24,000 GOES INTO DUTCH ROLL. ALSO, OCCURS IN CRUI SE. REPLACED NR 3 YAW RATE GYRO, PER MM AND NR 2 YAW SAS COMPUTER. T/S PER 22-10-33, 22-12-37, AND 22-15-00. PERFORME D A/L AND TABLE 502 CHECKOUT, GOOD. 2 L 7 3 4F A23WE 1999052100546 19990521 00546 NM 1999 5 21 DLM11991037 1 19990510 A 3350 SOCKET DOUG MD11 MD11 3023602 NM ROW 44 & 45 SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 808DE 48479 EMERGENCY LIGHTS FAIL TEST BATTERY 5 AND BATTERY 6 LOW. FOUND SHORTED LIGHT SOCKETS AT SEAT 44 AND 45. REPLACED SAME, GROUND TEST OK. 2 L 7 3 4F RT A22WE 1999052100547 19990521 00547 NM 1999 5 21 DL72S991038 1 19990511 A 7711 EPR INDICATOR BOEING 727 727225A 1384077 NM NR 1 ENGINE FLUCTUATES A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 8875Z 696620 21293 REJECTED TAKEOFF AT DFW DUE TO NR 1 ENGINE EGT FLUCUATION SPEED 70 KTS. TIGHTENED TWO JUNCTIONS AND REPLACED INDICATOR, RAN ENGINE. 2 L 7 3 4F RT A3WE 1999052100548 19990521 00548 NM 1999 5 21 DL72S991039 1 19990511 A 2740 32EN614 SWITCH BOEING 727 727232 1384082 NM STAB TRIM DIRTY A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 516DA 21432 TAKEOFF WARNING HORN SOUNDED DURING POWER UP AND TAKEOFF WAS ABORTED AT 10 KTS. WARNING HORN ITEMS CYCLED AND SOUNDED A GAIN ON SECOND ATTEMPT. FOUND UPPER STAB TRIM SWITCH STICKING. CLEANED AND LUBED SWITCH. TAKEOFF WARNING TEST NORMAL. 2 L 7 3 4F A3WE 1999052100549 19990521 00549 NM 1999 5 21 DLM88991040 1 19990511 A 2121 6054578 FAN DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 944DL 487569 49817 ELECTRICAL ODOR IN CABIN. DIVERTED TO CHS. REPLACED CABIN RECIRC FAN, ALL CKS NORMAL. 2 L 7 2 4F RT A6WE 1999052100550 19990521 00550 NE 1999 5 21 DL72S991041 2 19990511 A 7200 ENGINE 89812621 BOEING 727 727225A 1384077 NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 8875Z 2733 21293 NR 3 ENGINE BLEED TRIP IN FLIGHT. AIRCRAFT RETURNED TO DFW. REPLACED NR 3 ENGINE 13 STAGE PRESSURE REGULATOR. TIGHTEN ED 2 LINES, LEAK CHECKS GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 1999052100551 19990521 00551 NM 1999 5 21 DL76G991042 1 19990511 A 5240 MECHANISM BOEING 767 7673P6 1385105 NM 1R DOOR LACK OF LUBE A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 154DL 25241 DOOR 1R DOOR ARMING LEVER HARD TO OPERATE. SLIDE LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A1NM 1999052100552 19990521 00552 NM 1999 5 21 DL72S991043 1 19990512 A 7603 THROTTLE ROD BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LOOSE A DALA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 27 494DA 21074 696489 AT 10,000 FEET ON DESCENT, THE NR 3 ENGINE WENT TO 95 PERCENT N1 AND EGT TO 610 ENGINE SHUTDOWN WITH THE PRECAUTIONARY E NGINE SHUTDOWN CHECKLIST. FOUND THROTTLE ROD OFF OF THRU SHAFT AT GEARBOX. REINSTALLED SAME ENGINE CHECKS NORMAL ON RU N UP ALL PARAMETERS WITHIN M/M LIMITS. 2 L 7 3 4F 4 F A3WE E2EA 1999052100553 19990521 00553 NM 1999 5 21 DL72W991044 1 19990512 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 NR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999052100554 19990521 00554 NM 1999 5 21 DL72W991045 1 19990512 A 5754 BRACKET BOEING 727 727247 138408F NM NR 1 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 NR 1 L/E FLAP ACT O/B AND I/B MOUNT BRACKETS CRACKED AT UPPER AND LOWER MOUNT BOLTS. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999052100555 19990521 00555 NM 1999 5 21 DL72W991046 1 19990512 A 5755 659892421 ANGLE BOEING 727 727247 138408F NM NR 3 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 TPA - LTR CHK D-1, NR 3 SPOILER I/B ACTUATOR ATTACH ANGLE CRACKED AT LWR BOLT. REPLACED ANGLE PER MM 57-42-0. 2 L 7 3 4F A3WE 1999052100556 19990521 00556 NM 1999 5 21 DL76L991050 1 19990513 A 2420 SWITCH 233N320928 BOEING 767 767332 1382001 NM NR 2 ENGINE FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 188DN D01502 27583 STRONG ELECTRICAL SMELL IN AREA OF FWD COAT CLOSET WITH VIDEO ENTERTAINMENT GEAR. FOUND FAULTY RT GENERATOR DRIVE LIGHT SWITCH. REPLACED GENERATOR POWER PANEL. SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999052100557 19990521 00557 NM 1999 5 21 DL72S991051 1 19990409 A 5753 652163241 SKIN BOEING 727 727225A 1384077 NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 DURING SHOP INSPECTION THE COVE SKIN WAS FOUND CRACKED 32 INCHES FROM THE I/B END OF MIDFLAP. THE COVE SKIN WAS REPAIRE D BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 809. 2 L 7 3 4F RT A3WE 1999052100558 19990521 00558 NM 1999 5 21 DL72S991052 1 19990513 A 5712 651622172 RIB BOEING 727 727225A 1384077 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 INNER SKIN CUT TO GAIN ACCESS TO RIBS. SKIN REPAIRED PER M/M 57-54-0 FIG 801. 2 L 7 3 4F RT A3WE 1999052100559 19990521 00559 NM 1999 5 21 DL72S991053 1 19990513 A 5511 RIB BOEING 727 727232 1384082 NM HORZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 LT ELEV HINGE SUPPORT RIB CRACKED BETWEEN NR 3 AND 4 BAL BOARDS AT LOWER END. REPAIRED PER MM 55-10-31. 2 L 7 3 4F A3WE 1999052100560 19990521 00560 NM 1999 5 21 DL757991055 1 19990513 A 5330 146N34303 SKIN BOEING 757 757232 1384965 NM BS 1550 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 609DL 22816 THE UPPER SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND GOUGED AT FS 1150. THE DAMAGED AREA OF UPPER SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. INSTALLED PER ER/A 367340-14. 2 L 7 2 4F RT A2NM 1999052100561 19990521 00561 NM 1999 5 21 DL76L991070 1 19990516 A 2520 PSU BOEING 767 767332 1382001 NM SEAT 3A FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 180DN 25985 CREW REPORTED ELEC SMELL FROM SEAT 3A. CREW DISCONNECTED CANNON PLUGS FROM SEAT. 2 L 7 2 4F RT A1NM 1999052100562 19990521 00562 NM 1999 5 21 DL76S991075 1 19990516 A 3230 RETRACT MECH BOEING 767 767332 1382001 NM RT MLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 119DL 23278 RT MAIN GEAR REMAINED EXTENDED AFTER T/O, ALT GEAR EXTENSION WORKED OK. MTC IN WORK ON GEAR RETRACTION AT TOC. NO NOTI CEABLE DAMAGE TO GEAR. GEAR PINS INSTALLED FOR MTC. 2 L 7 2 4F RT A1NM 1999052100563 19990521 00563 NM 1999 5 21 DLM88991080 1 19990517 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 MTC FOUND A CRACK AT L2L AND L2R ON THE STA 1418 FRAME. THESE CRACKS ARE TYPICALLY COVERED BY EO 9-63538-3, BUT THE EO AND RELATED SB DO NOT COVER THIS AC. REPAIRED PER ERA 333164-14. 2 L 7 2 4F RT A6WE 1999052100564 19990521 00564 NM 1999 5 21 DL72S991081 1 19990517 A 5330 655456816 SKIN BOEING 727 727225A 1384077 NM R1 DOORWAY TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 THE FUSELAGE SKIN WAS FOUND TORN AT THE LWR HINGE CUTOUT FOR THE R1 DOOR. REPAIRED PER ERA 333131-14, REV A. 2 L 7 3 4F RT A3WE 1999052100565 19990521 00565 NM 1999 5 21 DL76L991086 1 19990517 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM ROW 6-22 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 186DN 27962 FLOOR PATH LIGHTING INOP BETWEEN ROWS 6 AND 22. REPLACED FLOOR LIGHTING POWER SUPPLY. 2 L 7 2 4F RT A1NM 1999052100566 19990521 00566 NM 1999 5 21 DL72W991088 1 19990515 A 5330 65604477 SKIN BOEING 727 727247 138408F NM BS 1130-1166 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 THE FUSELAGE SKIN WAS DENTED BETWEEN FS 1130 AND 1166 BETWEEN STRINGERS 23R AND 24R. THE SKIN DENT WAS CUT OUT WITH A 2 2.5 INCH X 6.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 367383-14, REV A. 2 L 7 3 4F A3WE 1999052100567 19990521 00567 NM 1999 5 21 DL76L991089 1 19990517 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM ROW 6-20 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 186DN 5785 27962 EMERGENCY FLOOR E PATH LIGHTING INOP, BETWEEN SEAT ROW 6 AND 20. REPLACED POWER SUPPLY AND OPS CK OK. 2 L 7 2 4F RT A1NM 1999052100568 19990521 00568 NM 1999 5 21 DL72S991095 1 19990517 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 420-440 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 INTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 420 AND 440. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EX TERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 367400-14AD. 2 L 7 3 4F A3WE 1999052100569 19990521 00569 NM 1999 5 21 DL72S991096 1 19990517 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 INTERNAL HFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 360 AND 380. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN E XTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 367401-14AD. 2 L 7 3 4F A3WE 1999052100570 19990521 00570 WP 1999 5 21 DLL14991097 1 19990517 A 5330 1503140 SKIN LKHEED 1011 1011385115 5265015 WP BS 798 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 THE FUSELAGE SKIN WAS FOUND WITH AREAS OF CORROSION BETWEEN FS 789 AND 809 AND BETWEEN STRINGERS 33 AND 35. THE CORROSI ON WAS REMOVED WITH TWO CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 367367-14, REV A. 2 L 7 3 4F A23WE 1999052100571 19990521 00571 NM 1999 5 21 SCNA99707 1 19990409 A 5330 SKIN BOEING 727 727282 138408T NM EMER EXIT DRWAY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING A HEAVY MAINTENANCE CHECK, FOUND CORROSION IN THE MAIN CABIN LEFT HAND AFT EMERGENCY EXIT HATCH AT THE LOWER FORW ARD CORNER OF CUTOUT. REMOVED CORROSION IAW SRM B727 511006. CORROSION WAS FOUND OUT OF LIMITS PER SRM B727 531001. F ABRICATED DOUBLER FROM 301 1/2 HARD STEEL .125 IAW SRM 533003. ALODINED AND PRIMED IAW B727 SRM 511002 AND MM 512002. I NSTALLED IAW B727 SRM 533003. 2 L 7 3 4F RT A3WE 1999052100572 19990521 00572 NM 1999 5 21 P5CA9900568 1 19990516 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT WING TOP FIXED T/E PANEL BETWEEN I/B AILERON AND SPOILER NR 5 TOP SURFACE FOUND DELAMINATED. REMOVED OLD REPAIR AN D WATER. REPLACED DAMAGED CORE, FILLERS AND OVERLAYS PER SRM 51-40-12. 2 L 7 4 4F A20WE 1999052100573 19990521 00573 NM 1999 5 21 P5CA9900569 1 19990514 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT WING T/E UPPER FIXED PANEL AT WING STA 1190 LOWER SURFACE FOUND DELAMINATED. SANDED CLEANED AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR, APPLIED PARTS UNDER VACCUUM AND CURED REPAIR PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999052100574 19990521 00574 WP 1999 5 21 RRXA99897 1 19990515 A 2830 5252541 ACTUATOR DOUG DC8 DC862F 3021972 WP FUEL DUMP FAILED A RRXA K NONE J WARNING INDICATION CR CRUISE 1 WP 15 997CF 46154 ON TEST OF FUEL DUMP SYSTEM, WHEN DUMP SWITCH WAS PLACED TO DRAIN THE CHUTES WOULD NOT MOVE TO DRAIN. TRIED MANUAL DRAI N, NO HELP. FUEL CONTINUED TO DUMP TO STAND PIPES. REMOVED AND REPLACED DUMP CHUTE ACTUATOR IAW DC8 MM 28-30-2, OPS CK GOOD AT THIS TIME. 2 L 7 4 4F 4A25 1999052100575 19990521 00575 WP 1999 5 21 RRXA99917 1 19990513 A 5320 JAMB DOUG DC8 DC862 3021970 WP CARGO DOORWAY TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 994CF 45956 PER FAA RAMP INSP, METAL TORN AT UPPER SECTION OF MAIN CARGO DOOR JAMB. AIRCRAFT FERRIED TO KMQY FOR REPAIRS. 2 L 7 4 4F 4A25 1999052100576 19990521 00576 NM 1999 5 21 VNAA9905002 1 19990506 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BS 564 DAMAGED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 433JS 3047 A GASH IN THE FUSELAGE, STATION 564, WAS FOUND BY THE CREW DURING THE POST FLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPAIRED THE DAMAGE IN ACCORDANCE WITH DORNIER SRM 53-00-11 AND 53-22-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999052100577 19990521 00577 NM 1999 5 21 VNAA9905003 1 19990510 A 2150 PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 440JS 3058 A RIGHT HAND PAC FAIL AND PAC OVERHEAT WARNING MESSAGE ILLUMINATED DURING THE TAXI OUT FOR TAKEOFF. THE CREW REPORTED A SMALL AMOUNT OF SMOKE IN THE COCKPIT AND RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND PERFORMED AN OPERA TIONAL CHECK OF THE AIR CONDITIONING SYSTEM, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-21-00. THE OPERATIONAL CH ECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999052100578 19990521 00578 NM 1999 5 21 VNAA9905004 1 19990512 A 2913 42086 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MAIN HYD SYST FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 430JS 9571 2810 3044 DURING THE APPROACH, A FLAP CONTROL FAILURE WARNING MESSAGE ILLUMINATED, WITH FLAPS 12 DEGREES SELECTED. A MAIN HYDRAUL IC PUMP WARNING MESSAGE ALSO ILLUMINATED FOR ABOUT ONE SECOND. THE CREW DECLARED AN EMERGENCY, AND CONTINUED THE APPROA CH AND LANDED WITHOUT INCIDENT. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT F OR REPAIR. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE MAIN A/C HYDRA ULIC PUMP, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-11-00. OPERATIONAL AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999052100579 19990521 00579 NM 1999 5 21 TC8A99019 1 19990518 A 2810 FUEL BOEING 727 7272B6 138407J NM LT WING DISCHARGED A TC8A D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 GL 23 721SK 21298 ON TAXI, NOTIFIED BY TOWER FUEL DISCHARGED FROM LEFT WING. SUMPED LEFT WING SURGE TANK AS REQUIRED IAW MM 28-11-0. TRA NSFERRED TO DMI LIST ITEM 9204 IAW TCA MEL 28-1-1, PLACARD INSTALLED. 2 L 7 3 4F A3WE 1999052800012 19990528 00012 SO 1999 5 28 CA990115012 1 19990104 A 3230 10035002B ACCUMULATOR EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA NLG STEERING LEAKING W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 567 PCE51708 (CAN) WHEN GEAR SELECTED UP AFTER TAKEOFF, ALL BUT THE NOSE GEAR INDICATED UP AND LOCKED. DOWN SELECTION MADE AND ALL G REENS. CREW RETURNED AND LANDING OK. THE NOSE LANDING GEAR CENTERING ACCUMULATOR FOUND LOW IN NITROGEN BECAUSE OF A LE AKING SCHRAEDER VALVE. VALVE CLEANED AND ACCUMULATOR TOPPED UP. 1 L 7 2 4T 4 T A21SO E4EA 1999052800014 19990528 00014 CE 1999 5 28 CA990119003 1 19990107 A 5520 505242403 BRACKET BEECH 90 B90 1152912 CE PWA PT6 PT6A20 52043 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE21649 (CAN) CRACK FOUND ON THE LEFT INBOARD ELEVATOR SUPPORT BRACKET. THE CRACK RADIATED FROM THE LOWER RIGHT BOLT HOLE TO TH E WEB OPENING. 1 L 7 2 3T 3 T 3A20 E4EA 1999052800020 19990528 00020 NM 1999 5 28 CA990119025 1 19990111 A 2910 82970010537 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120795 (CAN) HYDRAULIC LINE FOUND LEAKING AT THE 'B' NUT FOR SPOILER. LINE IN THE RIGHT HAND NACELLE BETWEEN THE T-FITTING AND RESERVOIR. 2 H 7 2 4T 4 T RT A13NM E20NE 1999052800023 19990528 00023 EU 1999 5 28 CA990125009 1 19990118 A 2435 23085014 GENERATOR PILATS PC12 PC12 7090550 EU START/GENERATOR FAILED W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 131 97107 (CAN) AT CRUISE ALTITUDE, NR 1 STARTER/GENERATOR VOLTMETER INDICATED ERRATIC INDICATIONS THEN WENT TO ZERO. GENERATOR S ELECTED OFF. ON RETURN LEG, GENERATOR FAILED. COMMUTATOR SEGMENT FOUND BROKEN OFF AND HAD DESTROYED ALL BRUSH ASSEMBLI ES. 1 L 7 1 3T RT A78EU 1999052800025 19990528 00025 EA 1999 5 28 CA990125011 1 19990120 A 5753 C6WF110067 RIBS C6WF10023 DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA TE FLAP LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 34073 310 PCE42181 (CAN) EXCESSIVE LOOSENESS BETWEEN THE 2 HALVES OF THE PLAP AT THE CENTER HINGE ARM POSITION. RIBS ON EITHER SIDE OF THE HINGE ARM ARE ASSEMBLED TO THE ARM BY THE USE OF LONG MS20470AD5 SOLID RIVETS. IT APPEARS THAT THERE HAD BEEN SOME WOR KING BETWEEN RIVET HEADS AND THE OUTBOARD RIB. 1 H 7 2 3T 4 T RT A9EA E4EA 1999052800044 19990528 00044 EA 1999 5 28 CA990203021 1 19990111 A 2752 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE TE FLAP FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 9571 807157 (CAN) FLAP FAIL MESSAGE ON DESCENT. RIGHT WING OUTBOARD FLAP ACTUATORS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999052800045 19990528 00045 EA 1999 5 28 CA990203022 1 19990120 A 5330 PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LH EXHAUST MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 6552 807373 (CAN) DURING WALK-AROUND , FOUND THE LEFT HAND ENGINE EXHAUST PIPE A PANEL MISSING. 2 L 7 2 4F 4 F RT A21EA E15NE 1999052800056 19990528 00056 CE 1999 5 28 CA990209021 1 19990129 A 3260 44EN496 SWITCH 1143610441 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 199 GGMPS0025 (CAN) DURING INSPECTION, AURAL LANDING GEAR WARNING COULD NOT BE CANCELLED. BAD INSULATION BETWEEN PIN NR 8 AND GROUND (SWITCH CASE). 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800057 19990528 00057 CE 1999 5 28 CA990209022 1 19990201 A 5610 1143840205 WINDSHIELD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 5951 95203H2165 GGMPS0123 (CAN) WINDSHIELD FOUND DELAMINATED. CAUSED BY WATER INFILTRATION. ALSO, SOME CORROSION. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800058 19990528 00058 CE 1999 5 28 CA990209023 1 19990203 A 2510 1005304427 ARM REST BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA GGM114452 (CAN) WHEN COPILOT SEAT IN FULL FORWARD POSITION, THE RIGHT HAND ARM REST BLOCKS THE CIRCUIT BREAKERS FROM TRIPPING. AR M RESTS REMOVED AS A TEMPORARY MEASURE. PROBLEM COMMON TO ALL OF SUBMITTER'S FLEET. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800061 19990528 00061 CE 1999 5 28 CA990210006 1 19990203 A 5620 1294300411 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7121 GGMPS0025 (CAN) BOTH FRONT CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. FLIGHT INITIALLY RESTRICTED TO UNPRESSUR IZED UNTIL WINDOW REPLACEMENT AND LATER ALLOWED PRESSURIZED FLIGHT IF WINDOWS WERE REVERSED 180 DEGREES AND PASSED 'OUT OF CONTOUR' TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800062 19990528 00062 CE 1999 5 28 CA990210007 1 19990203 A 5620 1294300561 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7121 GGMPS0025 (CAN) ALL CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED BY RAYTHEON IF WINDOW S WERE REVERSED 180 DEGREES AND UNTIL REPLACEMENT AND THEY PASS OUT OF CONTOUR TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800063 19990528 00063 CE 1999 5 28 CA990210008 1 19990203 A 5620 1294300411 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7414 GGMPS0123 (CAN) BOTH FRONT CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. OPERATION APPROVED PRESSURIZED FLIGHT AS LONG AS THE WINDOWS WERE REVERSED. THIS ALLOWED UNTIL WINDOWS ARE REPLACED AND AS LONG AS THEY PASS OUT OF CONTOUR TES T. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800064 19990528 00064 CE 1999 5 28 CA990210009 1 19990203 A 5620 1294300561 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7414 GGMPS0123 (CAN) 11 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR THE 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED AS LONG AS W INDOWS ARE REVERSED, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800065 19990528 00065 CE 1999 5 28 CA990210010 1 19990203 A 5620 1294300411 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7496 GGM114476 (CAN) BOTH FRONT CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED IF WINDOWS ARE REVERSED 180 DEGREES, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800066 19990528 00066 CE 1999 5 28 CA990210011 1 19990203 A 5620 1294300561 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7496 GGM114476 (CAN) 11 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED IF WINDOWS ARE REVERSED 180 DEGREES, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800067 19990528 00067 CE 1999 5 28 CA990210012 1 19990203 A 5620 1294300411 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 6893 GGMPS0054 (CAN) BOTH FRONT CABIN WINDOWS WERE FOUND OUT OF LIMITS FOR THE 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED IF WI NDOWS ARE REVERSED 180 DEGREES, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800068 19990528 00068 CE 1999 5 28 CA990210013 1 19990203 A 5620 1294300561 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 6893 GGMPS0054 (CAN) 10 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED AS LONG AS WIND OWS ARE REVERSED 180 DEGREES AND PASS TEST. THIS ALLOWED UNTIL REPLACEMENT AVAILABLE. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800069 19990528 00069 CE 1999 5 28 CA990210014 1 19990203 A 5620 1294300411 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7408 GGM114452 (CAN) BOTH FRONT CABIN WINDOWS REPLACED AS THEY WERE FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSUIRZED FLIGHT A LLOWED IF WINDOWS ARE REVERSED 180 DEGREES AND UNTIL REPLACEMENT AND THEY ARE PASSED FOR OUT OF CONTOUR TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800070 19990528 00070 CE 1999 5 28 CA990210015 1 19990203 A 5620 1294300561 WINDOW BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 7408 GGM114452 (CAN) 7 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED AS LONG AS WINDOW S ARE REVERSED 180 DEGREES AND UNTIL REPLACEMENT AND ARE OK FOR OUT OF CONTOUR TEST. 2 L 7 2 4T 4 T RT A24CE E26NE 1999052800085 19990528 00085 EA 1999 5 28 CA990219021 1 19990122 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE COCKPIT SHATTERED W O OTHER O OTHER NR NOT REPORTED 1 CA 9614 807157 (CAN) CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED DURING CLIMB. 2 L 7 2 4F 4 F RT A21EA E15NE 1999052800095 19990528 00095 NE 1999 5 28 CA990416024 2 19990405 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 120189 (CAN) ON DEPARTURE, NR 1 ENGINE OIL PRESSURE GAUGE FLUCTUATED, CONFIRMED BY OIL PRESSURE AND MASTER CAUTION WARNING LIG HTS. PRECAUTIONARY SHUTDOWN OF ENG CARRIED OUT AND AIRCRAFT RETURNED TO ITS DEPARTURE POINT. INVESTIGATION FOUND THIS ENG WAS REMOVED FROM SERVICE IN ANOTHER DASH-8 FOR THE SAME PROBLEM. THE ENG HAD BEEN SENT TO PWC FOR REPAIR. THE ENG WAS REPAIRED AND RAN SERVICEABLE IN THE PWC TEST CELL AND WAS RETURNED TO THE OPERATOR. THE UNIT WAS INSTALLED IN THIS AIRCRAFT, 7.6 FLIGHT HOURS AND 10 FLIGHT CYCLES PREVIOUS TO THIS FAULT AND RAN SERVICEABLE. THE ENG HAS BEEN QUARANTINE D PENDING ARRIVAL OF PWC REP FOR EVALUATION. 2 H 7 2 4T 4 T RT A13NM E20NE 1999052800100 19990528 00100 NE 1999 5 28 CA990430049 2 19990425 A 7200 ENGINE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 1 MALFUNCTIONED W E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 CA 10432 (CAN) ON CLIMB-OUT, THE NR 1 ENGINE VIBRATION WENT FROM 2 TO 5 UNITS ON BOTH CHANNELS. THE THROTTLE WAS RETARDED AND TH E VIBS STILL REMAINED AT 3 UNITS. THE NR 1 ENGINE WAS SHUTDOWN. THE OIL LEVEL WAS 18 LITRES ON SHUTDOWN AND WENT DOWN TO 3 LITRES AT LANDING. MAINTENANCE FOUND OIL AND METAL PARTICLES IN THE EXHAUST. THE ENGINE IS UNDER INVESTIGATION. 2 L 7 3 4F 4 F A23WE E12EU 1999052800109 19990528 00109 WP 1999 5 28 AT9900380 1 19990425 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THREE FLOORBOARD SUPPORT BRACKETS AT BS 160 TO 218 LBL 1 TO 55 CORRO DED. FABRICATED REPAIR FLOOR SUPPORTS, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1999052800110 19990528 00110 WP 1999 5 28 AT9900381 1 19990428 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND FLOORBOARD SUPPORT BRACKET AT BS 160 RBL 0 TO 52 CORRODED. FABRICAT ED FLOOR SUPPORT ANGLE, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1999052800111 19990528 00111 WP 1999 5 28 AT9900382 1 19990504 A 5320 1A4717423 ANGLE DOUG DC9 DC932 3022066 WP BS 170-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CUSP ANGLE AT R-1 DOOR JAMB CORRODED AT BS 170 TO 200. FABRICATED R EPAIR PARTS, DRILLED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 53-05 FIG 55, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999052800112 19990528 00112 WP 1999 5 28 AT9900383 1 19990512 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-389 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND RIGHT HAND FUSELAGE SKIN WITH DENTS AND CREASES AT BS 229 TO 389 L18 -27R. FABRICATED REPAIR SKIN AND SPLICE DOUBLER AND INSTALLED IAW AIRTRAN RES NR 991034. 2 L 7 2 4F A6WE 1999052800113 19990528 00113 WP 1999 5 28 AT9900384 1 19990503 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 148-160 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A CRACK RIGHT HAND FUSELAGE AT BS 148 TO 160 FORTY FIVE INCHES ABOVE CUSP (L13R) IN INTERCOSTAL. ROUTED OUT CRACK AND INSTALLED GUSSET AND L ANGLE REPAIR IAW TIMCO EO NR 99-1139. 2 L 7 2 4F A6WE 1999052800114 19990528 00114 WP 1999 5 28 AT9900385 1 19990507 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 148-160 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A CRACK IN INTERCOSTAL RIGHT HAND FUSELAGE AT BS 148 TO 160 (L10R) F IFTY FOUR INCHES ABOVE CUSP. ROUTED OUT CRACK AND INSTALLED GUSSET AND L ANGLE REPAIR IAW TIMCO EO NR 99-1140. 2 L 7 2 4F A6WE 1999052800115 19990528 00115 WP 1999 5 28 AT9900387 1 19990414 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-197 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE R-1 FLOOR DOOR ENTRANCE AT BS 160 TO 197 RBL 54 CORRODED. REMOV ED R-1 DOOR ENTRANCE PANEL, FABRICATED, PRIMED, PAINTED AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-3 AND 51-30-0. 2 L 7 2 4F A6WE 1999052800116 19990528 00116 WP 1999 5 28 AT9900388 1 19990513 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND SUB FLOORBOARD AT BS 160 TO 200 OUTBOARD RIGHT HAND TOP SIDE CORRODE D. MECHANICALLY REMOVED CORROSION, FABRICATED, TRIMMED, DRILLED, DEBURRED, COUNTERSUNK PANEL, TREATED, PRIMED AND INSTA LLED HAT SECTION IAW B737 SRM 51-10-3, 53-22-0 FIG 3 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1999052800117 19990528 00117 WP 1999 5 28 CALA9900552 1 19990517 A 3411 4024130901 INDICATOR DOUG DC9 DC932 3022066 WP CENTER INST PNL INOPERATIVE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 12508 18269 47797 THE CREW OBSERVED A BURNING ODOR IN THE COCKPIT FOLLOWED BY LIGHT SMOKE WHILE ON APPROACH TO SDF. RED FLAGS WERE OBSERV ED ON TRI, CAPTAIN'S SIDE. THE SMOKE DISSIPATED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RAT/TR I INDICATOR AT FAULT. THE RAT/TRI INDICATOR WAS REMOVED AND REPLACED IAW MM 34-15-2. THE PACKS WERE RUN AND NO ODORS W ERE NOTED. 2 L 7 2 4F A6WE 1999052800118 19990528 00118 WP 1999 5 28 CALA9900553 1 19990517 A 5230 DOUBLER DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO COMPARTMENT DOOR REPAIR DOUBLER AT UPLOCK GUIDE PIN. THE DOUBLER WAS REMOV ED IAW SRM 51-10-2, PAGE 1. A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-2, PAGE 1 AND 51-10-3, PAGE 1. 2 L 7 2 4F A6WE 1999052800119 19990528 00119 WP 1999 5 28 CALA9900554 1 19990517 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 229 ABOVE LONGERON 17. THE DENTED AREA WAS CUT OUT IAW SRM 53-04-00, PA GE 203. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04-00, PAGE 203 AND 51-10-3. 2 L 7 2 4F A6WE 1999052800120 19990528 00120 NM 1999 5 28 CALA9900555 1 19990517 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70330 23460 INSPECTION FOUND A .5 INCH CRACK IN NR 2 ENGINE PYLON SKIN AT PANEL NR 5824 AND A .5 INCH CRACK WAS FOUND IN PANEL NR 58 28. REPAIRS WERE INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 1999052800121 19990528 00121 NM 1999 5 28 CALA9900556 1 19990518 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND FLOOR SUPPORT J-ANGLE CORRODED AROUND SCREW HOLES AT BS 1070 BETWEEN RBL 45 AND 62. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, 51-10-2, PAGE 1 AND 51-20-2, PAGE 1. 2 L 7 3 4F A3WE 1999052800122 19990528 00122 NM 1999 5 28 CALA9900557 1 19990518 A 5311 FRAME BOEING 727 727224 1384076 NM BS 620 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO FRAME AT STA 620, RBL 27-28. THE CRACKED AREA WAS CUT OUT, A SPLICE R EPAIR WAS INSTALLED IAW SRM 51-40-3, 51-10-6 AND 51-30-2. 2 L 7 3 4F A3WE 1999052800123 19990528 00123 NM 1999 5 28 CALA9900558 1 19990518 A 5753 FLAP BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND A .125 INCH CRACK WITH DENT IN THE RIGHT I/B MIDFLAP TRAILING EDGE INBOARD MOST END. THE FLAP WAS REPA IRED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1999052800124 19990528 00124 NM 1999 5 28 UPS99229639 1 19990519 A 3350 S106 BATTERY BOEING 727 72751C 1384015 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:N/A, DURING SECURE CHECK FOUND EMERGENCY EXIT LIGHTS (BOTH) DID NOT WORK. REPLACED BATTS IN BOTH EMERGE NCY EXIT LIGHT ASSY, OPS CK'S NORMAL PER MM 33-50-101. 2 L 7 3 4F A3WE 1999052800125 19990528 00125 NE 1999 5 28 UPS99229640 2 19990517 A 7230 COMPRESSOR BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE STALLED A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 208UP 21701 INSPECTION TYPE:N/A, JUST AFTER T/O PASSING 4,800 FT, NR 1 ENG HAD SEVERE VIBRATION AND EGT CLIMBED IMMEDIATELY TO 800 C WITH THRUST LEVER RETARDED TO FLT IDLE AND EGT CONTINUED TO CLIMB. LOUD BANG (COMPRESSOR STALL) ACCOMPANIED LOSS OF TH RUST. REMOVED AND REPLACED NR 1 ENG. 2 L 7 3 4F 4 F A3WE E2EA 1999052800126 19990528 00126 NM 1999 5 28 UPS99229641 1 19990426 A 5320 FITTING BOEING 727 727180C 138406G NM BS 480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, SUSPECT CRACK ON FWD FLANGE OF BS 480 FITTING LT SIDE AT STR 17. REPAIR CARRIED OUT IAW SMRO EO 99-1 2-003R1 AND UPS ENGINEERING FILE NUMBER 727-53-2125. 2 L 7 3 4F A3WE 1999052800127 19990528 00127 NM 1999 5 28 UPS99229642 1 19990428 A 5311 FRAME BOEING 727 727180C 138406G NM BS 825.95 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, MECHANICAL DAMAGE FOUND ON FIRST FASTENER HOLE BELOW FLOOR AT BS 825 .95 RT. AFTER CLEAN UP THIS HOL E IS OUTSIDE LIMITS PER EO B727-5310-5 474 PAGE 9. FRAME REPAIRED IAW B727-5310-5474 APPENDIX C REF SMRO EO 99-12-002 A ND UPS EO B727-5310-11383. 2 L 7 3 4F A3WE 1999052800128 19990528 00128 NM 1999 5 28 UPS99229643 1 19990428 A 5520 65191441 BRACKET BOEING 727 727180C 138406G NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, SUSPECT CRACK ON LT ELEVATOR REAR SPAR ON BRACKET AT TAB ROD CUTOUT. CRACKED BRACKET REPLACED IAW DR AWING 65-25635. 2 L 7 3 4F A3WE 1999052800129 19990528 00129 NM 1999 5 28 UPS99229644 1 19990426 A 5312 BULKHEAD BOEING 727 727180C 138406G NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, CRACK ON RT KEEL BEAM BULK HEAD BS 930 WL 158. REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999052800130 19990528 00130 NM 1999 5 28 UPS99229645 1 19990430 A 7830 06453010059 BRACKET BOEING 727 727180C 138406G NM NR 3 ENGINE TR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, ENG NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-30-02 AND M M 78-30-00. 2 L 7 3 4F A3WE 1999052800131 19990528 00131 NM 1999 5 28 UPS99229646 1 19990508 A 5313 STRINGER BOEING 727 727180C 138406G NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, DURING ACCOMPLISHMENT OF RT 870 PARTIAL REPLACEMENT CRACK DISCOVERED AT FASTENER HOLE, LWR TANG, STR 13 AFT OF FITTING FLANGE. RT 870 FITTING REPLACED IAW UPS EO B727-5310-3056-B APPD E. 2 L 7 3 4F A3WE 1999052800132 19990528 00132 NM 1999 5 28 UPS99229647 1 19990505 A 5751 CASTING BOEING 727 727180C 138406G NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, RIGHT O/B AILERON TAB ROD HINGE CASTING CORRODED. HINGE CASTINGS REMOVED AND REPLACED IAW MM 27-10-4 1. 2 L 7 3 4F A3WE 1999052800133 19990528 00133 NM 1999 5 28 UPS99229648 1 19990505 A 5752 HINGE BOEING 727 727180C 138406G NM RT AILERON TAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, RIGHT O/B AILERON TAB HINGES CORRODED. RIGHT O/B AILERON TAB HINGES REMOVED AND REPLACED IAW MM 27-1 0-41. 2 L 7 3 4F A3WE 1999052800134 19990528 00134 NM 1999 5 28 UPS99229649 1 19990505 A 5543 SKIN BOEING 727 727180C 138406G NM RUDDER TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, UPPER RUDDER TAB RT SIDE HAS EVIDENCE OF DELAMINATION T/E AREA, AFT OF CENTER HINGE FITTINGS. REPAIR ED IAW SRM 51-40-10 FIG 1. 2 L 7 3 4F A3WE 1999052800135 19990528 00135 NM 1999 5 28 UPS99229650 1 19990429 A 5320 BRACKET BOEING 727 727180C 138406G NM CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, ON INSPECTION OF THE FWD CARGO BAY CEILING, CARGO DOOR UPLOCK RETAINING BRACKET FOUND CRACKED. REPLA CED BRACKET IAW SRM 51-20-1 FIG 3. 2 L 7 3 4F A3WE 1999052800136 19990528 00136 NM 1999 5 28 UPS99229651 1 19990505 A 5532 SKIN BOEING 727 727180C 138406G NM VERT STAB LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, VERTICAL STAB LT SIDE, SKIN LOOSE ADJACENT FASTENERS STR 57 AREA BELOW STAB GEARBOX FWD CUTOUT. REPA IR CARRIED OUT IAW SRM 55-30-5 FIG 4. 2 L 7 3 4F A3WE 1999052800137 19990528 00137 NM 1999 5 28 UPS99229652 1 19990428 A 7830 06453010059 BRACKET BOEING 727 727180C 138406G NM NR 1 ENGINE TR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:C, ENG NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-30-02 AND M M 78-30-00. 2 L 7 3 4F A3WE 1999052800138 19990528 00138 WP 1999 5 28 UPS99829637 1 19990409 A 5313 37585931 LONGERON DOUG DC8 DC873F 302199F WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, LONG 35L IS CRACKED AT FS 1270. REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052800139 19990528 00139 WP 1999 5 28 UPS99829638 1 19990412 A 5320 3773159501 SPLICE DOUG DC8 DC873F 302199F WP BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:C3, FS 1100 FRAME UPPER LIP AT LONG 27R HAS HEAVY CORROSION. REMOVED DAMAGED SPLICE, FABRICATED AND REP LACED IAW DWG 3773159 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052800140 19990528 00140 WP 1999 5 28 UPS99829653 1 19990430 A 5313 37585931 LONGERON DOUG DC8 DC873F 302199F WP BS 1350 - 1347 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LONGERON 36 IS CRACKED BETWEEN FS 1350 AND 1347. REPAIRED LONGERON IAW DH SK880-592. 2 L 7 4 4F RT 4A25 1999052800141 19990528 00141 WP 1999 5 28 UPS99829654 1 19990503 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1160 - 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LONG 28L FS 1160 TO 1180 IS CORRODED BEYOND LIMITS. REPAIRED IAW DH SK880-651. 2 L 7 4 4F RT 4A25 1999052800142 19990528 00142 WP 1999 5 28 UPS99829655 1 19990520 A 2560 SLIDE DOUG DC8 DC873F 302199F WP EMER EXIT DOOR MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A, EMERGENCY SLIDE WOULD NOT CONNECT TO LATCHES, PACKED INCORRECTLY. REPACKED ESCAPE SLIDE, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999052800143 19990528 00143 WP 1999 5 28 UPS99829656 1 19990422 A 5320 561385725 ANGLE DOUG DC8 DC873F 302199F WP BS 62 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, FS -62, LBL 60, THE CUSP TEE ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED THE TEE ANGLE IAW DWG 5613857 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052800144 19990528 00144 WP 1999 5 28 UPS99829657 1 19990420 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 603.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, LT WING L/E RIB AT FS 603.75 IS CRACKED AT THE AFT LOWER FASTENER. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999052800145 19990528 00145 WP 1999 5 28 UPS99829658 1 19990418 A 5320 46455172 ANGLE DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:C2, CABIN FLOORBEAM SUPPORT ATTACH ANGLE IS CRACKED FS 680, RBL 24. REMOVED, FABRICATED AND REPLACED AN GLE IAW DWG 4645517 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999052800146 19990528 00146 WP 1999 5 28 UPS99829660 1 19990420 A 5313 STRINGER DOUG DC8 DC873F 302199F WP BS 1667 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A, STR 24 AT STA 1667 HEAVLY CORRODED. REMOVED SECTION OF STRINGER SPLICED IN NEW SECTION PER 53-2-2. 2 L 7 4 4F RT 4A25 1999052800147 19990528 00147 WP 1999 5 28 UPS99829661 1 19990422 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A, FLOORBEAM AT FS 1680 HAS ELONGATED HOLES FOR CENTER FASTENER OF SEAT TRACK AFT END. CLEANED UP HOL ES TO .5 PER EO DC8-5310-11039-A. 2 L 7 4 4F RT 4A25 1999052800148 19990528 00148 NM 1999 5 28 QXEA9901065 1 19990515 A 3220 88321 AXLE DHAV DHC8 DHC8102 2809003 NM NLG DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 30311 11135 213 PDX- NOSE GEAR TRAILING ARM HAS SEVERAL GOUGES. MAINTENANCE REPLACED TRAILING ARM ASSEMBLY. GEAR SWINGS AND OPERATIONA L CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999052800149 19990528 00149 NM 1999 5 28 QXEA9901066 1 19990518 A 3260 858601 PSEU DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 366PH 520 PDX- GEAR DOOR LIGHTS ILLUMINATED AT 24,000 FEET, A THUMP WAS HEARD IN THE COCKPIT FLOOR AREA. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE PSEU AND PERFORMED GEAR SWINGS, OPERATIONAL CHECKS GOOD. BITE CHECK OF PSEU ALSO CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999052800150 19990528 00150 NM 1999 5 28 99FDEA00183 1 19990516 A 2820 VENT BOX DOUG MD11 MD11F 3023600 NM WING FUEL SYS FUEL A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 590FE 48505 TANK WING OVER FILL ALERT. A/C FUELING AC VENT FUEL OVERHBD NUM TIMES ALERT BOTH IN AUTO AND MANUAL. FUEL IN VENT BOX. DRAINED FUEL FROM BOTH VENT BOXES. ALL TEST PASSED, NO FAULTS FOUND. 2 L 7 3 4F RT A22WE 1999052800151 19990528 00151 WP 1999 5 28 99FDEA00184 1 19990519 A 7933 SENSOR DOUG DC10 DC1010F 3022111 WP NR 1 ENGINE MALFUNCTIONED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 056FE 47810 NR 1 ENGINE OIL TEMP GAUGE ABOVE RED LINE FLUCTUATING. REMOVED AND REPLACED NR 1 ENGINE OIL TEMP SENSOR PER MM 79-32-01 -2. LEAK/OPS CK NORM. 2 L 7 3 4F A22WE 1999052800152 19990528 00152 WP 1999 5 28 ABXA9900375 1 19990519 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN LOOSE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942AX 47552 EMERGENCY LIGHTS WERE DIM AND INTERMITTENT. FOUND GROUND WIRE AT EMERGENCY BATTERY PACK LOOSE AND CORRODED. CLEANED AN D REINSTALLED GROUND WIRE, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999052800153 19990528 00153 WP 1999 5 28 ABXA9900376 1 19990519 A 2460 92057802 RELAY DOUG DC9 DC932 3022066 WP COCKPIT FAILED A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 980AX 47176 EMERGENCY DC BUS OFF LIGHT ILLUMINATED ON GENERATOR INOP CROSS-TIE CHECK. FOUND CONTACTS BETWEEN TERMINALS B1 AND B2 OP EN ON RELAY R2-19. REPLACED RELAY IAW DC9 MM, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999052800154 19990528 00154 WP 1999 5 28 MWEA99289 1 19990519 A 2560 1113317 COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR SLID DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 207ME 47794 GALLEY DOOR SLIDE APPEARS LOOSE. REINSTALLED GALLEY DOOR EMERGENCY SLIDE COVER. 2 L 7 2 4F A6WE 1999052800155 19990528 00155 NM 1999 5 28 MWEA99290 1 19990519 A 3350 6011777 BATTERY PACK DOUG MD88 MD88 3023688 NM EMER EXIT DOOR DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 804ME 48030 LEFT AND RIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT BATTERY PACK. 2 L 7 2 4F RT A6WE 1999052800156 19990528 00156 NM 1999 5 28 DHL99727003 1 19990518 A 5230 SEAL BOEING 727 727228 NM CARGO DOOR DIRTY A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 727DH 20204 AIRCRAFT FAILED TO PRESSURIZE. TROUBLESHOOT SYSTEM, FOUND DEBRIS IN LOWER CARGO DOOR SEAL. REMOVED DEBRIS AND AIRCRAFT PRESSURIZED NORMAL PER MM 21-50-0. 2 L 7 3 4F A3WE 1999052800173 19990528 00173 NM 1999 5 28 HNAA9900059 1 19990520 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 910HA 14526 14526 022 DURING OVERNIGHT, MAINTENANCE IT WAS FOUND THAT THE LT OUTSIDE EMERGENCY LIGHT DID NOT ILLUMINATE. THE PS3 BATTERY PACK WAS REPLACED. 2 H 7 2 4T RT A13NM 1999052800174 19990528 00174 WP 1999 5 28 AT9900389 1 19990519 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD ENTRY FLOOR PANEL NR 4692 AT BS 200 BL 0-65R CORRODED. F ABRICATED PARTS AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 53-21-0 FIG 2D, 51-70-2, 53-05-0, AND 51-30-2. 2 L 7 2 4F A6WE 1999052800175 19990528 00175 WP 1999 5 28 AT9900390 1 19990514 A 5315 S291275812000 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO, FL, FOUND PASSENGER CABIN FLOORBEAM RIGHT SIDE AFT LAVATORY AT BS 996 RBL 17-54R CORRODED . REMOVED UPPER CAP, LOCATED, DRILLED, AND INSTALLED UPPER CAP IAW DC9 SRM 53-11-3 FIG 11, 51-30-5, 51-10-4, AND 51-10- 2. 2 L 7 2 4F A6WE 1999052800176 19990528 00176 WP 1999 5 28 AT9900391 1 19990515 A 5412 BLKHD FRAME DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND ON THE CABIN LEFT FORWARD PYLON BULKHEAD AFT SIDE LOWER FRAME/FLOOR A T BS 965 CORRODED. CUT, DRILLED, AND DEBURRED NEW ANGLE (SUPPORT). LOCATED, CUT, DRILLED, TRIMMED NEW ANGLE REPAIR, AL ODINED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999052800177 19990528 00177 WP 1999 5 28 AT9900392 1 19990509 A 5414 PANEL DOUG DC9 DC932 3022066 WP RT PYLON CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT PYLON PANEL NR 8204 CORRODED AROUND CAMLOCKS AND ON THE BAC K SIDE. FABRICATED, LOCATED, DRILLED, DEBURRED THREE EACH REPAIRS, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 54-01 FIG 1, 54-30-0. 2 L 7 2 4F A6WE 1999052800178 19990528 00178 WP 1999 5 28 AT9900393 1 19990513 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FLOORBOARD SUBFLOOR BOTTOM SIDE CORRODED ON EDGES AND AROUND SCRE W HOLES AT BS 160-200 LEFT SIDE. REMOVED CORROSION, FABRICATED REPAIR SKIN, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PR IMED, AND INSTALLED HAT CHANNELS IAW DC9 SRM 53-21-0, 51-10-4, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999052800179 19990528 00179 WP 1999 5 28 AT9900394 1 19990518 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE CABIN FLOORBOARD PANEL AT BS 200-218 CORRODED ON TOP SIDE AND ARO UND EDGES. REMOVED CORROSION, DISSASEMBLED FLOOR PANEL, FABRICATED REPAIR AND REPLACEMENT SKIN, TRIMMED, DRILLED, DEBUR RED, TREATED, PRIMED, AND ASSEMBLED REPAIR COMPONENTS IAW DC9 SRM 51-30-2, 53-01 FIG. 1, 51-30-3, AND 51-10-3. 2 L 7 2 4F A6WE 1999052800180 19990528 00180 WP 1999 5 28 AT9900395 1 19990518 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT OUTBOARD FORWARD ENTRY FLOOR PANEL AT BS 160-200 CORRODED. FABRICATED FLOOR PANEL, TREATED, AND PRIMED IAW DC9 SRM 51-10-3, 53-01 FIG.1, 51-10-3, AND 53-21-0. 2 L 7 2 4F A6WE 1999052800181 19990528 00181 WP 1999 5 28 AT9900396 1 19990518 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 389 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND IN THE FORWARD CARGO FLOOR FRAME AT BS 389 RBL 3 CORROSION. REMOVED CORROSION AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 86, 51-30-5, AND 51-10-3. 2 L 7 2 4F A6WE 1999052800182 19990528 00182 WP 1999 5 28 AT9900397 1 19990518 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 180-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD ENTRY FLOOR PANEL CORRODED AT BS 180-200 CENTER RIGHT HAN D SIDE. FABRICATED, TRIMMED, DRILLED, FLOOR PANEL AND HAT SECTIONS, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 53-01 FIG.1, AND 51-30-1. 2 L 7 2 4F A6WE 1999052800200 19990528 00200 EU 1999 5 28 MALA976467 1 19990518 A 2560 31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DEPLOYED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 509XJ E2321 DURING PREFLIGHT, LEFT FORWARD PASSENGER DOOR SLIDE PARTIALLY DEPLOYED. MAINTENANCE REPLACED LEFT FORWARD EVACUATION SL IDE. WORK DONE IAW AVRP AMM 25-60-11. 2 H 7 4 4F RT A49EU 1999052800201 19990528 00201 EU 1999 5 28 MALA976468 1 19990509 A 5210 HC521H0709000 CONTROL BOSS BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 AFTER BOARDING, THE LEFT FORWARD CABIN DOOR WILL NOT CLOSE. MAINTENANCE REPLACED DOOR ROLLER INSIDE CONTROL BOS. ALL C HECKS GOOD. 2 H 7 4 4F RT A49EU 1999052800202 19990528 00202 EU 1999 5 28 MALA976469 1 19990511 A 2930 MS24142D1 RELAY SAAB SF340 SF340A 7850100 EU HYD IND SYST FAILED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 27XJ 027 WHILE TAXING HYDRAULIC LIGHT ILLUMINATED, PER QRH, NO HELP. CREW STOPPED AIRCRAFT ON TAXI WAY AND REQUESTED TOW, SINCE MAIN PUMP WAS LOW, COULDN'T GET BRAKES. MAINTENANCE REPLACED RELAY 7ML. ALL WORK DONE IAW SAAB 340 MM, SEC CHECKS GOOD , OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999052800203 19990528 00203 EU 1999 5 28 MALA976470 1 19990510 A 2560 COVER BAC 146 AVRO146RJ85A 1500097 EU EMER EXIT DOOR LOOSE A MALA O OTHER O OTHER IN INSP/MAINT 1 GL 15 510XJ E2325 FORWARD RIGHT DOOR ESCAPE SLIDE COVER IS LOOSE. MAINTENANCE REINSTALLED EMERGENCY SLIDE COVER IAW AMM 25-60-11-10, STEP NR 16. COVER IS SECURE. 2 H 7 4 4F RT A49EU 1999052800204 19990528 00204 EU 1999 5 28 MALA976471 1 19990515 A 3320 BALLAST SAAB SF340 340B 7860101 EU ROW 10B FAILED A MALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 413XJ 413 AFTER PUSH BACK IN GATE WITH BOTH ENGINES RUNNING, CARGO SMOKE LIGHT CAME ON AND OFF TWICE. PASSENGER REPORTED TO FA SE EING SOMETHING WHILE COMING OUT OF ROW 10B AIR GASPER. RETURNED TO GATE. MAINTENANCE INSPECTED CARGO SMOKE DETECTOR WI RING AND AFT FLIGHT RECORDER BAY AND OVERHEAD PSU 9CD, 10CD, AND 11CE, FOUND BALLAST OVER SEAT 10CD HAS BURNING SMELL, V ERIFIED THE WINDOW LIGHTS INOP. MAINTENANCE REPLACED BALLAST. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999052800205 19990528 00205 EU 1999 5 28 MALA976472 1 19990517 A 3310 BALLAST SAAB SF340 340B 7860101 EU RT GLARESHIELD SMOKING A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 417XJ 340B417 FO'S GLARESHIELD SMOKING. MAINTENANCE DETERMINED TO BE EMINATING FROM FO'S GLARESHIELD FLOURESCENT LAMP INBOARD BALLAST . VERIFIED SWITCH AND CB REMOVED POWER FROM CIRCUIT. PULLED AND COLLARED CB L21 FO'S CB PANEL. DEFERRED FO'S GLARESHI ELD FLOURSCENT LIGHT IAW MEL 33-10-1 (C). 2 L 7 2 4T RT A52EU 1999052800206 19990528 00206 NM 1999 5 28 CALA9900559 1 19990514 A 4920 360452445 COMBUSTOR GARRETT 380428101 BOEING 737 737524 1384721 NM APU INOPERATIVE A CALA F ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 SW 09 17620 9889 P100947 27333 THE APU FIRE INDICATION LIGHT AND BELL ACTIVATED APPROXIMATELY TWO MINUTES AFTER STARTING APU WHILE DESCENDING INTO DFW. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT AND BELL WENT OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANC E FOUND WIRES BURNT AT APU THERMOSTAT AND EVIDENCE OF A FUEL STREAM. THE APU WAS RUN AND MAINTENANCE FOUND TORCHING BEI NG CAUSED BY A FAULTY COMBUSTION CAN. THE APU COMBUSTION CAN WAS REMOVED AND REPLACED. THE APU WIRE HARNESS WAS ALSO R EMOVED AND REPLACED. APU LEAK AND OPERATIONAL CHECKS WERE GOOD. IN ADDITION, THE APU FIRE BOTTLE WAS REMOVED AND REPLA CED. 2 L 7 2 4F RT A16WE 1999052800207 19990528 00207 WP 1999 5 28 CALA9900560 1 19990519 A 2560 4953611501 ESCAPE LINE DOUG DC9 DC982 3022082 WP LT EMER EXIT FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND THE LEFT OVERWING EXIT ESCAPE LINE FRAYED AT ATTACH HOOK. THE ESCAPE LINE WAS REMOVED AND REPLACED IAW MM 25-61-00, PAGE 204-205. 2 L 7 2 4F A6WE 1999052800208 19990528 00208 WP 1999 5 28 CALA9900561 1 19990520 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1212-1222 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND LEFT INBOARD SEAT TRACK CORRODED AT STA 1212-1222. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51- 30-01. 2 L 7 2 4F A6WE 1999052800209 19990528 00209 WP 1999 5 28 CALA9900562 1 19990520 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND CORROSION ON FORWARD BAG BIN DOOR JAMB PAN AT STA 370-427. A NEW PAN AND DOUBLERS WERE INSTALLED IAW S RM 53-05. 2 L 7 2 4F A6WE 1999052800210 19990528 00210 WP 1999 5 28 CALA9900563 1 19990520 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1128-1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND LEFT OUTBOARD SEAT TRACK CORRODED AT STA 1136-1128. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999052800211 19990528 00211 WP 1999 5 28 CALA9900564 1 19990520 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 484 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 484, LONGERONS 19 AND 20. THE SKIN WAS REPAIRED IAW SRM 53-04-04, FIGUR E 38. 2 L 7 2 4F A6WE 1999052800212 19990528 00212 NM 1999 5 28 CALA9900565 1 19990520 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1110 FROM RBL 25-45. A REPAIR WAS INSTALLED IAW SRM 51-10-8, PAGE 18. 2 L 7 3 4F A3WE 1999052800213 19990528 00213 NM 1999 5 28 CALA9900566 1 19990520 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 620 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND STRINGER 27R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 620. THE CORRODED SECTION OF STRINGER WAS CU T OUT. A STRINGER REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-6. 2 L 7 3 4F A3WE 1999052800214 19990528 00214 WP 1999 5 28 CALA9900567 1 19990520 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 218-237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 218-237. A NEW SECTION OF SEAT TRACK WAS SPLICED IN IAW SRM 53-05 , FIGURE 4F. 2 L 7 2 4F A6WE 1999052800215 19990528 00215 NM 1999 5 28 UPS99429662 1 19990519 A 3150 WARNING SYST BOEING 747 747SR46 NM COCKPIT MALFUNCTIONED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 680UP 20923 ON SEVERAL OCCASIONS INFLIGHT MASTER WARNING BRIEFLY FLASHED AND FIRE BELL BRIEFLY SOUNDED. ALL OTHER INDICATIONS NORMA L. FUNCTION TEST APU FIRE TEST OPS TEST NORMAL PER MM26-22-00. 2 L 7 4 4F A20WE 1999052800216 19990528 00216 NM 1999 5 28 UPS99429663 1 19990512 A 2612 FIRE CARD BOEING 747 747SR46 NM APU NOT SEATED A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 680UP 20923 1.5 HRS INTO FLT THE APU FIRE WARNING LIGHT ILLUMINATED VERY DIMLY AND THE FIRE BELL SOUNDED, BUT SILENTLY FOR 10 SECOND S. THIS SITUATION DID NOT HAPPEN THE REST OF FLT. RESEATED THE A-5 AND A-8 CONTROL CARDS. APU FIRE TEST GOOD PER M/M 26-10-00. 2 L 7 4 4F A20WE 1999052800217 19990528 00217 EU 1999 5 28 QXEA9901067 1 19990516 A 3350 5515800106 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 496US 11169 PDX - EXIT LIGHT IN CABIN OVER COCKPIT DOOR HAD BULBS INOP. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999052800218 19990528 00218 NM 1999 5 28 99FDEA00185 1 19990521 A 5320 FITTING BOEING 727 72722 1384002 NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 0056 - AFT CARGO BS 1183 CENTER SUPT FORGING/CASTING FOR JACK PAD IS CRACKED FORE AND AFT. INSTALLED BS 1183 CENTER SUPT FORGING FOR JACK PAD PER SRM 51-10-1 AND BOEING DRW 65-16350. 2 L 7 3 4F A3WE 1999052800219 19990528 00219 NM 1999 5 28 99FDEA00186 1 19990409 A 5751 HINGE BOEING 727 72722 1384002 NM RT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 415, RT, WING OTBD AILERON 2ND HINGE O/B HINGE CASTING HAS DEEP PITTIED CORROSION TO MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW TYPE SANDCASTING ALUMINUM IAW BOEING INSTALL DRW NR 65-19260 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICES. 2 L 7 3 4F A3WE 1999052800220 19990528 00220 NM 1999 5 28 99FDEA00187 1 19990409 A 5751 HINGE BOEING 727 72722 1384002 NM RT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 417 RT WING, OTBD AILERON HINGE CASTING HAS DEEP PITTED CORROSION IN MAGNESIUM CASTING. REMOVED AND REPLACED CASTING WITH NEW SAND CASTED ALUM CAST PER DRW BOEING NR 65-15959 AND FASTENERS IAW SRM 51-30-2 AND STANDARD PRACTICES. 2 L 7 3 4F A3WE 1999052800221 19990528 00221 NM 1999 5 28 99FDEA00188 1 19990409 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 0063 - HEAVY CORROSION ON SHEAR TIE AT BS 990 FWD SIDE OF LWR BILGE AREA AT OTBD SIDE OF STR 29 RT. REMOVED AND REPL ACED SHEAR TIE. SEALED AREA AGAINST MOISTURE PER SRM 51-20-4. 2 L 7 3 4F A3WE 1999052800222 19990528 00222 NM 1999 5 28 99FDEA00189 1 19990519 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 680 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 NR 0166 - FWD CARGO LWR FLANGE OF FLOORBEAM DAMAGED BY TOO LONG FASTENERS. INSTALLED CTR SNAKE PIT PNL BS 680, LBL 24, RBL 24. INSTALLED FLOORBEAM LWR CHORD REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999052800223 19990528 00223 NM 1999 5 28 99FDEA00190 1 19990519 A 5530 SUPPORT BOEING 727 72722 1384002 NM VERT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 NR 924 - ANGLE RIB SUPPORT CRACKED IN VERTICAL STAB LEFT CORNER. INSTALLED DOUBLER PER SRM 51-40-3 AND 53-10-9 PG 11. F ABRICATED, PRIMED AND SEALED ACCESS HOLE DOUBLER PER SRM 51-40-2, OPS CK PER ON CARD 70C027-00. 2 L 7 3 4F A3WE 1999052800224 19990528 00224 1999 5 28 MWEA99291 4 19990519 A 3425 4056510903 EFIS DOUG MD88 MD88 3023688 NM LT COCKPIT INOP A MWEA D RETURN TO BLOCK I FLT. ATTITUDE INST. CL CLIMB 1 GL 31 804ME 48030 THE CAPTAINS NAVIGATION DISPLAY IS BLANK ON BOTH ON 1 AND BOTH ON 2. MAINTENANCE REMOVED AND REPLACED CAPTAINS EFIS DIS PLAY UNIT. 2 L 7 2 4F RT A6WE 1999052800225 19990528 00225 WP 1999 5 28 MWEA99292 1 19990518 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP PAX DOOR LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 THE PASSENGER ENTRANCE DOOR GIRT BAR IS DIFFICULT TO INSTALL AND REMOVE. MAINTENANCE COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4F A6WE 1999052800226 19990528 00226 WP 1999 5 28 MWEA99293 1 19990518 A 2560 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR DISENGAGED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 MAIN ENTRY DOOR ESCAPE SLIDE FELL OFF. SECURED PER 25-62-00. 2 L 7 2 4F A6WE 1999052800227 19990528 00227 WP 1999 5 28 MWEA99295 1 19990518 A 5313 27779227 LONGERON DOUG DC9 DC932 3022066 WP BS 979 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND HEAVY CORROSION UNDER LONGERON 23R AT FS 979. MAINTENANCE REMOVED CORROSION, FABRICATED AND INSTALLED ON LONGERON . 2 L 7 2 4F A6WE 1999052800245 19990528 00245 NM 1999 5 28 AT9900398 1 19990423 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 277 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FLOORBEAM AT BS 277 LBL 30-32 UPPER FORWARD WEB CORRODED. CUT O UT CORRODED AREA, FABRICATED REPAIR FILLER AND DOUBLER, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51-10-1, 51-10-6, 53- 10-1, 51-40-2, 51-21-31 AND RES NR 05008. 2 L 7 2 4F RT A16WE 1999052800246 19990528 00246 NM 1999 5 28 AT9900399 1 19990520 A 5320 INTERCOSTAL BOEING 737 7372L9 1384497 NM BS 1006-1016 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE INTERCOSTAL AT BS 1006 TO 1016 LBL 4 CORRODED. REMOVED INTERCOS TAL, FABRICATED REPAIR ANGLE, HEAT TREATED, TRIMMED, DRILLED UP, DEBURRED, TREATED, PRIMED AND INSTALLED IAW B737 SRM 51 -10-6, 51-40-3, 51-10-2, 51-30-2, 51-20-11. 2 L 7 2 4F RT A16WE 1999052800247 19990528 00247 WP 1999 5 28 AT9900400 1 19990419 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-238 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE RIGHT HAND OUTBOARD SEAT TRACK AT BS 200 TO 238 CORRODED. REMOV ED CORRODED SECTION, FABRICATED NEW SEAT TRACK, DRILLED, DEBURRED, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 53-05-0, 51-10-4, 51-30-1 AND 53-21-0 FIG 3. 2 L 7 2 4F A6WE 1999052800248 19990528 00248 WP 1999 5 28 AT9900401 1 19990521 A 3397 WIRE DOUG DC9 DC932 3022066 WP BS 1194 BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 831AT 47674 AFT VENTRAL STAIRWAY AFT LEFT EMERGENCY LIGHT FLICKERS (LOOSE WIRING). REPAIRED BROKEN WIRE IAW MM 20-50-1 AND OPS CHEC K GOOD IAW MM 33-51-0. 2 L 7 2 4F A6WE 1999052800249 19990528 00249 NM 1999 5 28 RAAA99B1003 1 19990521 A 3610 652673822 Y DUCT BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE 13TH STAGE CRACKED A RAAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 AL 03 831RV 19093 653555 UHPP - NR 2 ENGINE FIRE WARNING LIGHT ON AFTER TAKEOFF. SHUT DOWN ENGINE PER ENGINE FIRE CHECK LIST THEN LANDED AT UHPP . REMOVED AND REPLACED 13TH STAGE Y-DUCT PER 75-10-12 AND 75-22-01 (DUE CRACKED). LEAK CHECKED AND NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1999052800250 19990528 00250 NM 1999 5 28 CALA9900568 1 19990523 A 3230 SENSOR BOEING 737 737524 1384721 NM LANDING GEAR OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 14609 27322 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. WHEN RETRACTING FLAPS THE TAKEOFF WARNING HORN SOUNDED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR SAFETY SENSOR GAP OUT OF TOLERANCE. T HE SENSOR WAS ADJUSTED IAW MM 32-09-01. GEAR RETRACTION OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A16WE 1999052800251 19990528 00251 WP 1999 5 28 CALA9900569 1 19990522 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 218-256 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 218 TO 256. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-3 0. 2 L 7 2 4F A6WE 1999052800252 19990528 00252 WP 1999 5 28 CALA9900570 1 19990523 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 218 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND LT FUSELAGE SKIN DENTED BELOW CUSP LINE AT STA 218. THE DENTED AREA WAS ROUTED OUT AND A REPAIR DOUBLE R WAS INSTALLED IAW SRM 53-04, FIGURE 25. 2 L 7 2 4F A6WE 1999052800253 19990528 00253 WP 1999 5 28 9901739754 1 19990517 A 3260 SENSOR DOUG DC9 DC941 302207N WP LT MLG WW INOPERATIVE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 754NW 47178 AFTER TAKEOFF, THE LANDING GEAR DOOR OPEN AND LEFT MAIN LANDING GEAR RED UNSAFE LIGHTS REMAINED ILLUMINATED. THE FLIGHT CREW PERFORMED COM PROCEDURES AND RECYCLED LANDING GEAR. LIGHTS REMAINED ILLUMINATED. FLIGHT RETURNED TO STL AND LAND ED WITHOUT INCIDENT. UPON EXTENSION OF LANDING GEAR, ALL THREE DOWN AND LOCKED GREEN INDICATOR LIGHTS ILLUMINATED. MAI NTENANCE REPLACED THE LEFT MAIN LANDING GEAR UPLOCK SENSOR AND CHECKED WIRING FROM THE PROXIMITY SENSOR ELECTRONICS UNIT AND THE LEFT MAIN LANDING GEAR UPLOCK SENSOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999052800254 19990528 00254 WP 1999 5 28 9901749964 1 19990515 A 3397 WIRE DOUG DC9 DC931 3022065 WP CATWALK CHAFED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING MAINTENANCE INSPECTION, FOUND CATWALK VENTRAL STAIRS AND INTERIOR TAIL CONE RELEASE HANDLE EMERGENCY LIGHTS INOPE RATIVE. MAINTENANCE REPAIRED CHAFED WIRES AT CATWALK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999052800255 19990528 00255 WP 1999 5 28 9901759140 1 19990519 A 3350 BATTERY DOUG DC9 DC914 3022034 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 DURING LINE CHECK, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN POW ER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999052800256 19990528 00256 WP 1999 5 28 9901769154 1 19990519 A 3350 BATTERY DOUG DC9 DC914 3022034 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND TAIL CONE EMERGENCY LIGHTS ON CATWALK INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999052800257 19990528 00257 NM 1999 5 28 UPS99229664 1 19990521 A 7931 626447 VALVE BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A IPXA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 01 208UP 21701 696529 INSPECTION TYPE:N/A ON TAKEOFF ABOVE 80 KTS T6 NR 1 ENGINE OIL PRESSURE WENT ABOVE THE RED LINE TO 65 PSI. WHEN THRUST WAS REDUCED TO CLIMB POWER, T6 OIL PRESS REMAINED ABOVE THE RED LINE UNTIL POWER WAS REDUCED BELOW 1.5 EPR. OIL PRESS R EMAINED BELOW THE THE RED LINE UNTIL BLOCK TURN BACK WAS ACCOMPLISHED. REPLACED THE OIL PRESSURE TRANSMITTER AND OIL PR ESSURE RELIEF VALVE PER MM 79-30-86 AND 79-33-00. RAN NR 1 ENGINE T/O POWER PER MM 71-00-86 OIL PRESS REMAINED WITHIN O IL PRESS LIMITS OF 45-55 PSI. 2 L 7 3 4F 4 F A3WE E2EA 1999052800258 19990528 00258 EU 1999 5 28 QXEA9901068 1 19990521 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 1497 11156 BOI - EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. OPERATIONALLY TESTED, N O DEFECTS NOTED. 2 L 7 2 4F RT A20EU 1999052800259 19990528 00259 WP 1999 5 28 ABXA9900377 1 19990521 A 5752 5910051 SKIN DOUG DOUG DC9 DC941 302207N WP RT AILERON TAB DELAMIINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 DURING C-CHECK, FOUND RIGHT AILERON TRIM TAB DELAMINATED. REPLACED TRIM TAB IAW DC9 MM 27-10-5 AND ABX REA D927-31543. 2 L 7 2 4F A6WE 1999052800260 19990528 00260 WP 1999 5 28 ABXA9900378 1 19990521 A 5720 5910041504 VANE DOUG DOUG DC9 DC941 302207N WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 DURING C-CHECK, FOUND RIGHT INBOARD FLAP FIXED VANE DELAMINATED. REPLACED FLAP FIXED VANE IAW DC9 MM 27-50. 2 L 7 2 4F A6WE 1999052800261 19990528 00261 WP 1999 5 28 ABXA9900379 1 19990521 A 5230 5910157 PAN DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 963AX 47780 DURING C-CHECK, FOUND AFT LOWER CARGO DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-31557. 2 L 7 2 4F A6WE 1999052800262 19990528 00262 WP 1999 5 28 ABXA9900380 1 19990520 A 7931 779606 VALVE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE MALFUNCTIONED A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 852AX 46016 669523 NR 4 ENGINE WAS SHUT DOWN DUE TO OIL QUANTITY GOING TO 0 AND OIL PRESS FLUCTUATING. AT SHUTDOWN OIL PRESS WAS 15 PSI, T HEN WENT TO 0. CLEANED AND INSPECTED NR 4 ENGINE OIL FILTER AND OIL SCAVENGE FILTER. NO METAL CONTAMINATION FOUND. RE PLACED NR 4 ENGINE OIL PRESSURE RELIEF VALVE IAW DC8 MM 79-20-5. 2 L 7 4 4F 4 F 4A25 1E8 1999052800263 19990528 00263 WP 1999 5 28 MWEA99298 1 19990520 A 3260 801801 SENSOR DOUG DC9 DC932 3022066 WP NLG FAILED A MWEA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 GL 31 212ME 47701 AFTER GEAR RETRACTION ON TAKEOFF LEFT GEAR UNSAFE LIGHT WOULD NOT GO OUT. MTC REMOVED AND REPLACED NOSE UP AND DOWNLOCK SENSORS AND CONDUIT. 2 L 7 2 4F A6WE 1999052800264 19990528 00264 WP 1999 5 28 MWEA99299 1 19990524 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 215ME 47744 THE GALLEY SERVICE DOOR EVACUATION SLIDE FELL OFF. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999052800265 19990528 00265 WP 1999 5 28 MWEA99300 1 19990521 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 207ME 47794 THE GALLEY DOOR SLIDE NEEDED TO BE REINSTALLED.MTC REINSTALLED GALLEY DOOR SLI DE. 2 L 7 2 4F A6WE 1999052800266 19990528 00266 NM 1999 5 28 DL72W991047 1 19990512 A 2910 LINE 651784961D BOEING 727 727247 138408F NM B HYD SYST CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 293WA 22111 B-SYS QTY FELL TO ZERO. FOUND HYD LINE CRACKED AT B-SYS HYD FILTER MODULE. REPLACED SAME, SERVICED QTY TO FULL. LEAK CHECK NORMAL. 2 L 7 3 4F A3WE 1999052800267 19990528 00267 NM 1999 5 28 DL73E991054 1 19990513 A 2613 OVERHEAT DET BOEING 737 7372J8 1384489 NM APU INOPERATIVE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 235WA 41642 34486 22859 APU LIGHT ILLUMINATED ON T/O. PULLED HANDLE, LIGHT CONTINUED TO ILLUMINATE ON TAXI BACK. REJECTED TAKEOFF. REPLACED A PU TAILPIPE OVERHEAT DET CONNECTOR D1878 AND WIRE W765-451-18R DUE TO HIGH RESISTANCE SHORT. OPS TEST AND RUN TEST CHEC K GOOD. CONNECTOR (P/N 878581-01). 2 L 7 2 4F RT A16WE 1999052800268 19990528 00268 NM 1999 5 28 DLM88991057 1 19990513 A 3244 TIRE MD88M DOUG MD88 MD88 3023688 NM RT MLG FAILED A DALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 27 925DL 49712 AT ROTATION LOUD BANG, RT ENGINE COMPRESSOR STALLS. FOUND NR 4 TIRE THREW RECAP AND PIECES OF TIRE DAMAGED 6 FAN BLADED . REPLACED FAN. RT I/B FLAP DAMAGED. 2 L 7 2 4F RT A6WE 1999052800269 19990528 00269 NE 1999 5 28 DLM88991058 2 19990514 A 7261 FILTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE DIRTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 913DE 21926 49956 725793 RT ENGINE OIL STRAINER CLOGGED LIGHT ON IN FLT. ENGINE SHUT DOWN. REPLACED MAIN OIL FILTER DUE TO BEING CLOGGED WITH C ARBON. 2 L 7 2 4F 4 F RT A6WE E9NE 1999052800270 19990528 00270 NM 1999 5 28 DL72K991059 1 19990514 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 FOUND ON C1 LETTER CK, LOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 5 SLAT I/B STOP. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999052800271 19990528 00271 NM 1999 5 28 DL72W991066 1 19990513 A 5330 65504477 SKIN BOEING 727 727247 138408F NM BS 1148 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 37447 20648 GOUGE ON THE OUTER SKIN FS 1148 STRINGER 24R. REPAIRED PER ERA 367383-14. 2 L 7 3 4F A3WE 1999052800272 19990528 00272 WP 1999 5 28 DLL10991068 1 19990515 A 3350 BULB OL3071BPEGPL LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 721DA 193C1139 TWO EMERGENCY LIGHTS INOP FIRST CLASS LT TRACK. REPLACED BULBS AND HOLDER. 2 L 7 3 4F A23WE 1999052800273 19990528 00273 NM 1999 5 28 DLM11991069 1 19990515 A 3350 P2070003001 LIGHT DOUG MD11 MD11 3023602 NM DOOR 4R INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 810DE 48565 DURING CABIN CK, FOUND EMERGENCY FLASHLIGHT AT DOOR 4R DISCHARGED AND LENS ASSY CRACKED. EMERGENCY FLASHLIGHT AND BATTE RY ASSY REPLACED, ALL OPS NORMAL. 2 L 7 3 4F RT A22WE 1999052800274 19990528 00274 NM 1999 5 28 DL757991072 1 19990516 A 5350 RADOME 141N782013 BOEING 757 757232 1384965 NM FWD FUSELAGE BROKEN A DALA K NONE O OTHER CL CLIMB 1 SO 27 645DL 2438 24216 ON CLIMBOUT ABOUT 13,000 FT, HEARD TWO LOUD BANGING NOISE FOLLOWED BY LOUD AIR NOISE IN NOSE GEAR AREA. FOUND RADOME AN D RADAR ANTENNA DAMAGED. MAINT IN PROGRESS. 2 L 7 2 4F RT A2NM 1999052800275 19990528 00275 NM 1999 5 28 DL72L991073 1 19990515 A 2760 RETURN LINE 6517840492 BOEING 727 727232 1384082 NM NR 2 SPOILER CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 507DA 21309 SYS A HYD QTY IND DROPPED TO ZERO QTY APPROX ONE HR AND 20 MINS INTO FLT. NR 1 ENG HYD LOW PRESS LIGHT ILLUMINATED. C HECKLIST PROCEDURE INITIATED LANDING UNEVENTFUL. GROUND INVESTIGATION LEAKING HALF WAY POINT LEFT WING. FOUND NR 2 SPO IL-ER RETURN LINE CRACKED BELOW NR 3 SPOILER. REPLACED LINE WITH TEMP FLEX LINE. CYCLED FLAPS AND SLATS SEVERAL TIMES, NO LEAKS FOUND. NO CLEARANCE PROBLEMS FOUND. THIS WAS AN EMERGENCY LANDING INTO PDX. A/C CALLED 20 MINS OUT BEFORE L ANDING IN PDX. 2 L 7 3 4F A3WE 1999052800276 19990528 00276 NM 1999 5 28 DLM11991076 1 19990516 A 2611 SMOKE DETECTOR 7213000012 DOUG MD11 MD11 3023602 NM NR 2 MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 27 813DE 0095 48600 NUMBER 2 SMOKE DETECTOR C/B PULLED DUE TO ERRONEOUS LAV SMOKE INDICATIONS. ERRONEOUS LAV SMOKE INDICATIONS DID NOT REOC CUR. C/B NOT RESET, NO FURTHER DIAGNOSIS ATTEMPTED BY FLIGHT CREW. INSPECTED SMOKE DETECTOR AND FOUND NO DEFECTS. REP LACED NR 2 LAV SMOKE DETECTOR CAPTS SIDE F/C AS PRECAUTIONARY, PERFORMED SATISFACTORY OPERATIONAL TEST ALL OK. 2 L 7 3 4F RT A22WE 1999052800277 19990528 00277 NM 1999 5 28 DL76G991077 1 19990516 A 2910 LINE BOEING 767 7673P6 1385105 NM LT HYD SYST LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 155DL 25269 LEFT HYDRAULIC QUANTITY DECREASING .01/10 MIN, PRESS 3000, TEMP 14, QTY .55. REPLACED NR 1 ENGINE SUPPLY LINE IN STRUT AREA. LEAK CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999052800278 19990528 00278 NM 1999 5 28 DL72S991082 1 19990517 A 5330 SKIN BOEING 727 727225 1384077 NM BS 950-1070 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 MULTIPLE SKIN REPAIRS HAVE BEEN ACCOMPLISHED ON THE LOWER FUSE SKIN BETWEEN BS 950 TO 1070. DUE TO THIS, THE LWR SKIN W ILL BE REPLACED AT THIS VISIT. REPLACED AND SPLICE SKIN PER ERA 333076-14. 2 L 7 3 4F A3WE 1999052800279 19990528 00279 NM 1999 5 28 DL72S991083 1 19990516 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM PASSENGER DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 476DA 20753 AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. 2 L 7 3 4F A3WE 1999052800280 19990528 00280 WP 1999 5 28 DLL10991085 1 19990517 A 3320 78047201 BALLAST LKHEED 1011 10113851 5265010 WP ROW 5E FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 730DA 193C1199 F/A'S REPORTED SMOKE IN THE CABIN IN THE VICINITY OF SEAT 5E, BELIEVED TO BE COMING FROM LIGHTING BALLAST. DEACTIVATED SYSTEM, CONDITION IMPROVED. REPLACED OVERHEAD MODULE AT SEAT 5E/F, REACTIVATED LIGHTING SYS AND ALL CK NORMAL. 2 L 7 3 4F A23WE 1999052800281 19990528 00281 NM 1999 5 28 DLM11991091 1 19990517 A 5230 DOOR DOUG MD11 MD11 3023602 NM CARGO COMPT DAMMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 811DE 48566 AFT OF CNTR CARGO DOOR LOWER AFT CORNER DAMAGED. REPAIRED PER SRM 53-50-00-0-7. 2 L 7 3 4F RT A22WE 1999052800282 19990528 00282 NM 1999 5 28 DL757991098 1 19990518 A 2432 BATTERY CHARGER 425404 BOEING 757 757232 1384965 NM BATTERY COMPT INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 661DN 2357 24972 MAIN BATTERY CHARGER STATUS MSG RECEIVED. REPLACED MAIN BATTERY AND BATTERY CHARGER. 2 L 7 2 4F RT A2NM 1999052800283 19990528 00283 NM 1999 5 28 DL72S991099 1 19990518 A 3350 SIGN 900542 BOEING 727 727225 1384077 NM 2R DOOR INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 8882Z 11034 21579 EMERGENCY EXIT SIGN OVER 2R SERVICE DOOR FLICKERS FROM DIM TO BRIGHT WITH EMERGENCY LIGHT SYSTEM OFF. 2 L 7 3 4F A3WE 1999052800284 19990528 00284 WP 1999 5 28 DLL10991100 1 19990518 A 2612 47226001 FIRE LOOP LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE INOPERATIVE A DALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 27 718DA 51292 0247 193C1097 010573 NR 1 ENG LOOP A ON MCO, LOOP B FLICKERED THEN CAME ON STEADY. CREW SHUTDOWN NR 1 ENG PER POM. REPLACED UPPER GEARBOX L OOP. 2 L 7 3 4F 4 F A23WE E12EU 1999052800285 19990528 00285 NM 1999 5 28 DL76G991101 1 19990519 A 2560 SLIDE 101651303 BOEING 767 7673P6 1385105 NM L1 DOOR PARTIAL DEPLOY A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 153DL 24985 L1 DOOR SLIDE FELL OFF DOOR AND STARTED TO UNLACE. SWAPPED DOOR SLIDE L3 TO L1, PLACED L3 SLIDE ON MCO/PLA PER MEL 52-1 1-04. 2 L 7 2 4F RT A1NM 1999052800286 19990528 00286 NM 1999 5 28 DLM11991103 1 19990519 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM TAIL DAMAGED A DALA K NONE O OTHER LD LANDING 1 SO 27 813DE 48600 TAIL STRIKE ON LANDING CBG. FUSELAGE/PRESSURE BULKHEAD DAMAGE. SKIN AND STRUCTURAL DAMAGE TO BE REPAIRED PER ERAS AND SRM AS APPLICABLE. 2 L 7 3 4F RT A22WE 1999052800287 19990528 00287 NM 1999 5 28 DL76L991105 1 19990519 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 192DN 28449 BUSINESS CLASS EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 1999052800288 19990528 00288 NM 1999 5 28 DL76L991106 1 19990519 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 172DN 24775 BY MTC E-PATH LIGHTS INOP FROM SEAT 31 BACK ON BOTH SIDES OF THE A/C. FOUND FUSES AT POWER SUPPLY BLOWN SUPPLY M9010. R EPLACED SAME, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999052800289 19990528 00289 NM 1999 5 28 DL73K991108 1 19990519 A 2150 69497901 DUCT BOEING 737 737247 138448D NM LT WING CRACKED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 237WA 23185 PRIOR TO T/O, LT WING BODY OVERHEAT LIGHT CAME ON. LIGHT WENT OUT WHEN APU BLEED SECURED. NO PROBLEM UNTIL SHORTLY AFT ER T/O, WHEN F/A REPORTED STRONG SMOKE SMELL. PROBABLY ELECTRICAL, ALL OVER CABIN. CAPT IMMEDIATEDLY ELECTED TO RETURN AND LANDED 3 MIN AFTER T/O. REPLACED CRACKED TURBO FAN DUCT. 2 L 7 2 4F A16WE 1999052800290 19990528 00290 NM 1999 5 28 DL76L991109 1 19990519 A 2530 811150417 COFFEEMAKER BOEING 767 767332 1382001 NM FWD GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 189DN 25990 FAS NOTICED ELECTRICAL SMELL ASSOCIATED W/ FWD GALLEY C/MS. SMELL DISSIPATED WHEN THE C/MS WERE SHUT OFF. REMOVED BOTH COFFEEMAKERS AND INSPECTED WIRING. WIRING OK. OPERATED BOTH C/MS, CKD OK. REMOVED REMNANTS OF PLASTIC ON C/M 1 HOT PLATE, OPS OK. 2 L 7 2 4F RT A1NM 1999052800291 19990528 00291 NM 1999 5 28 DLM88991110 1 19990519 A 3233 593703605507 ACTUATOR DOUG MD88 MD88 3023688 NM LT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 905DL 49536 LT MAIN LANDING GEAR UNSAFE INDICATION WITH GEAR HANDLE UP. CYCLED GEAR DOWN, INDICATION OK. UP UNSAFE AGAIN. GEAR DO OR LIGHT OUT TILL FL270 THEN INTERMITTENT. ALSO, AUTOSPOILER FAIL MSG ON EOAP. DIVERTED TO DFW. REPLACED LEFT MAIN LA NDING GEAR ACT, SWUNG GEAR. OPERATION NORMAL AND ALL INDICATION NORMAL. 2 L 7 2 4F RT A6WE 1999052800292 19990528 00292 NM 1999 5 28 DL72K991111 1 19990519 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 410DA DL7 21222 L2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999052800293 19990528 00293 NM 1999 5 28 DLM11991112 1 19990519 A 5230 DOOR DOUG MD11 MD11 3023602 NM CARGO COMPT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 802DE 48473 AFT OF FWD CARGO DOOR LOWER AFT CORNER DAMAGED. REPAIRED PER SRM. 2 L 7 3 4F RT A22WE 1999052800294 19990528 00294 NM 1999 5 28 DLM11991113 1 19990513 A 5751 NRC6741403 SKIN DOUG MD11 MD11 3023602 NM LT AILERON DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 809DE 48480 LEFT O/B AILERON / FRONT SPAR / LWR FLANGE / XDA 928: TOOLING DAMAGE TO LOWER SPAR FLANGE. SPAR IS M/F SOLID GRAPHITE LAMINATE, APPROX .208 THICK. LOWER FLANGE IS DELAMINATED THROUGH THICKNESS OVER APPROX 1 INCH DEPTH (CHORD-WISE) X 2 W IDTH (SPAN-WISE). REPAIR CONSISTS OF SCARFING OUT DAMAGE AND INSTALLING PRECURED GRAPHITE REPAIR DOUBLER. 2 L 7 3 4F RT A22WE 1999052800295 19990528 00295 NM 1999 5 28 DL76L991114 1 19990519 A 2612 285T03855 CARD BOEING 767 767332 1382001 NM E/E COMPT FAILED A DALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 199DN 28456 FIRE BELL ON TOUCHDOWN THAT COULD NOT BE SILENCED. NO OTHER INDICATIONS. RESET A/C POWER, SYSTEM CHECKED OK. FAULT RE T ON PUSHBACK. REPLACED M1000 CARD IN P51 FILE, SYSTEM CKS OK. 2 L 7 2 4F RT A1NM 1999052800296 19990528 00296 NM 1999 5 28 DL72L991116 1 19990520 A 2781 SWITCH BOEING 727 727232 1384082 NM NR 1 LE FLAP OUT OF ADJUST A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 513DA 21315 UNSAFE (AMBER LIGHT) INDICATION EXT AT FLAPS 5 POSITION. AFTER EXAMINATION IT WAS DETERMINED THAT L/E FLAP NR 1 FAILED TO EXTEND PROPERLY. AFTER TOUCHDOWN, L/E FLAPS LIGHT TURNED GREEN AND POS IND APPEARED NORMAL. ADJUSTED NR 1 L/E FLAP SWITCH PER MM, CHECKS NORMAL. 2 L 7 3 4F A3WE 1999052800297 19990528 00297 NM 1999 5 28 DL76L991117 1 19990519 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM BS 654 INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 174DN 42492 24802 ON L/O, FOUND EMERGENCY LIGHTS INOP SEATS 6, 10, 11 AND 20 FIG. FOUND AFT LIGHT OF SEAT 11FG BLOWING FUSE ON POWER SUPP LY. REPLACED POWER SUPPLY AND FORWARD AFT LIGHT OF 11FG TO MCO AND PLACARD. 2 L 7 2 4F RT A1NM 1999052800298 19990528 00298 NM 1999 5 28 DL76L991119 1 19990520 A 3350 LIGHT BOEING 767 767332 1382001 NM ROW 5AB INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 192DN 28449 SEAT MOUNTED EMERGENCY TRACK LIGHT INOPERATIVE. RELAMPED SAME AT SEAT ROW 5AB, LIGHT OPERATION CHECKS GOOD. 2 L 7 2 4F RT A1NM 1999052800299 19990528 00299 NM 1999 5 28 DL757991120 1 19990520 A 2913 3508807 PUMP BOEING 757 757232 1384965 NM LT ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 675DL 25980 SLOW HYD LEAK IN LT SYS. REPLACED LT ENG HYD PUMP. CHECKED CASE DRAIN AND SUPPLY FILTERS, NO METAL FOUND. OPS AND LEA K CK OK. 2 L 7 2 4F RT A2NM 1999052800300 19990528 00300 1999 5 28 DL76L991121 4 19990520 A 2330 ENTERTAIN SYS BOEING 767 767332 1382001 NM E/E COMPT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 180DN 25985 STRONG ELECTRICAL ODOR COMING FROM FLOOR VENT IN COCKPIT. FOUND SMELL COMING FROM THE CABIN FILE SERVER IN THE FWD E & E COMPT. DISABLED ROCKWELL ENTERTAINMENT SYS ON NEXT LOG ITEM B777659002. NO FURTHER SMELL NOTED. C/B P-37K6 YCC-PAT VMOD PESC-VPTR WAS POPPING WHEN SMELL WAS FIRST NOTICED. ITEM B777659002 DISABLED THE ROCKWELL SYSTEM C/BS CLAMP-ED AS FOLLOWED. C/BS P--37 VC VCC FANS 4 VDU C/BS PANEL 36 ADV 1 AND 2 CLAMPED. FWD SYS TO MCO. 2 L 7 2 4F RT A1NM 1999052800301 19990528 00301 NM 1999 5 28 DL72S991122 1 19990520 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 FOUND AT B-2 LETTER CHECK, LT AFT ENTRYWAY DOOR FRAME HAS .375 INCH VISIBLE CRACK. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999052800302 19990528 00302 NM 1999 5 28 DL72S991123 1 19990507 A 5530 STRINGER BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND DURING MV2 CORROSION VISIT NRC 210, STR 9 CRACKED AT FIN STA 157.2 INSIDE VERT STAB CRAWLWAY (3RD STR FROM BOTTOM, 3RD BAY UP FROM DOOR). REPAIRED PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1999052800303 19990528 00303 NM 1999 5 28 DL72S991124 1 19990520 A 5320 WEB BOEING 727 727232 1384082 NM BS 1226 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 TPA LTR CHK B-2, LT VERT TORQUE BOX WEB CRACKED .25 INCH AT UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0 PG 828, LT VERT TORQUE BOX WEB LWR LIGHTENING HOLE .375 INCH CRACK AT UPPER END AND A .625 INCH CRACK ON LWR END STA 122 6. REPAIRED PER MM 53-11-0 PG 832. 2 L 7 3 4F A3WE 1999052800304 19990528 00304 NM 1999 5 28 DL72S991125 1 19990520 A 3350 20131A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 483DA 20863 FIRST CLASS EMERGENCY LIGHTS DIM. 2 L 7 3 4F A3WE 1999052800305 19990528 00305 NM 1999 5 28 DL72S991128 1 19990521 A 3231 CONTROL CABLE 3240202582 BOEING 727 727232 1384082 NM NLG DOOR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 400DA 21144 AFTER TAKEOFF, PILOT HEARD LOUD NOISE FROM NOSE WHEEL AREA AND NOTICED NLG LIGHT INDICATION. AIRCRAFT RETURNED AND LAND ED WITHOUT INCIDENT. FOUND LOWER NLG DOOR CABLE WITH SEVERAL STRANDS BROKEN AND BIRD CAGED, NLG DOORS WERE NOT FULLY CL OSED. REPLACED CABLE ASSY, TENSIONED AND RIGGED SYSTEM AND PERFORMED GEAR SWING PER MM. 2 L 7 3 4F A3WE 1999052800306 19990528 00306 NM 1999 5 28 DLM11991131 1 19990521 A 3320 LIGHT DOUG MD11 MD11 3023602 NM DOOR 4L OVERHEATED A DALA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 SO 27 810DE 48565 CREW REPORTED WALL AT 4L PASSENGER DOOR HOT. FOUND 4L WORK LIGHT OVERHEATED. REPLACED SAME. 2 L 7 3 4F RT A22WE 1999052800307 19990528 00307 NM 1999 5 28 DL72S991132 1 19990521 A 2782 ACTUATOR 269002917 BOEING 727 727232 1384082 NM NR 4 LE SLAT FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 497DA DL635X 21077 ON APP FLAP EXT 2 TO 5 AMBER L/E FLAP LIGHT REMAINED ILLUM. POSITION TEST SHOWED NO LIGHT FOR LEFT NR 4 SLAT RETRACTED. PERFORMED APP PER POM. C/W PROCS FOR LANDING. TAXIING AFTER LAND UPON FLAP RETRACTION, LOST A HYD SYS FLUID. PERFOR MED PROCS AS PER POM. STOPPED A/C AND TOWED IN. REPLACED LT WING NR 4 SLAT ACT PER MM, LEAK CHECK OK. HYD SERVICED, L IGHTS AND OPN CKS NORMAL. SECURED ACCESS PANELS RII C/W PER CVG QA. 2 L 7 3 4F A3WE 1999052800308 19990528 00308 WP 1999 5 28 DLL14991133 1 19990522 A 3350 BATTERY PACK 516574 LKHEED 1011 1011385115 5265015 WP L4 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 736DY 60834 193C1227 L-4 OUTSIDE EMERGENCY LIGHT STAYED ON. REPLACED EMERGENCY LIGHT BATTERY PACK, CKS OK. 2 L 7 3 4F A23WE 1999052800309 19990528 00309 WP 1999 5 28 DLL10991136 1 19990521 A 5730 PANEL LKHEED 1011 10113851 5265010 WP LT WING CRACKED A DALA K NONE O OTHER DE DESCENT 1 SO 27 718DA 193C1097 CRACK IN SHEET METAL ON TOP OF LEFT WING SECOND CANOE FITTING OUTBOARD FROM WING ROOT. REPAIRED PER ERA OR SRM AS APPLI CABLE. 2 L 7 3 4F A23WE 1999052800310 19990528 00310 NM 1999 5 28 DLM88991137 1 19990522 A 2432 BATTERY 203BC1011 DOUG MD88 MD88 3023688 NM BATTERY COMPT OVERHEAT A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 912DE 8110755 49997 DURING WALKAROUND NOTICED ACRID BURNING SMELL NEAR EXT POWER HOOK UP RECEPTACLE. REPLACED AIRCRAFT BATTERIES AND CHARGE R. 2 L 7 2 4F RT A6WE 1999052800311 19990528 00311 NM 1999 5 28 DLM88991138 1 19990522 A 4900 38005041 APU DOUG MD88 MD88 3023688 NM CABIN LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 919DE 6615 53422 AFTER T/O, MID CABIN TO AFT SMELL OF SMOKE. RETURNED ATL. F/A VERIFIED ODORS 3 TIMES DURING APPROACH. AN UNUSUAL VIBR ATION AFT END WAS ACCOMPANYING THE SMELL. FOUND APU LEAKING INTERNALLY. REMOVED AND REPLACED APU, PERFORMED DUCT BURNO UT PER M/M. REMOVED AND REPLACED H2O SEPARATOR BAGS, A/C CKS OK. 2 L 7 2 4F RT A6WE 1999052800312 19990528 00312 NM 1999 5 28 DL72S991139 1 19990523 A 3350 900542 POWER SUPPLY BOEING 727 727232 1384082 NM ROW 3 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 545DA 22494 ON PREFLIGHT, EMERGENCY EXIT SIGN INOP ROW 3. REPLACED RACK AND BATTERIES, OPN NORMAL. 2 L 7 3 4F A3WE 1999052800313 19990528 00313 NM 1999 5 28 DL72S991140 1 19990523 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 545DA 22494 ON PREFLIGHT, EMERG EXIT SIGN AT ROW 3 INOP. REPLACED RACK AND BATTERIES, OPN NORMAL. 2 L 7 3 4F A3WE 1999052800314 19990528 00314 NM 1999 5 28 DL76L991142 1 19990523 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM ROW 6 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 173DN 24800 EMERGENCY PATH LIGHTS LT SIDE BUSINESS CLASS FROM ROW 6 TO FIRST ROW T/C INOP. REPLACED BATTERY PACK AT 6 A/B, CKS OK. 2 L 7 2 4F RT A1NM 1999052800315 19990528 00315 NM 1999 5 28 DL72S991143 1 19990523 A 3350 3114981 LIGHT BOEING 727 727232 1384082 NM L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 483DA 20863 L2 SLIDE LIGHT INOP. REPLACED SAME. 2 L 7 3 4F A3WE 1999052800316 19990528 00316 NM 1999 5 28 DLM11991144 1 19990523 A 3350 02019243006 LIGHT DOUG MD11 MD11 3023602 NM GALLEY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 803DE 48474 EMERGENCY LIGHTS INOP AT GALLEY 8A. FOUND DURING LAYOVER MTC CHECK. REPLACED LIGHT ASSY, CHECKS OK. 2 L 7 3 4F RT A22WE 1999052800322 19990528 00322 CE 1999 5 28 99ZZZX2078 1 19990323 A 2730 81400010 BRACKET CESSNA 310 310Q 2074242 CE ELEVATOR DAMAGED A A CZUA K NONE O OTHER IN INSP/MAINT 1 EA 25 1312G 4446 310Q1153 BOLT HOLES THROUGH BRACKETS, WHICH SUPPORT ELEVATOR BELLCRANK, ELONGATED FORWARD. NOTED DURING ANNUAL INSPECTION. POSS IBLE CAUSE IS TENSION EXERTED ON BRACKETS BY CABLE TENSION AND CONSTANT FORWARD STRESS CAUSED BY USE OF THE ELEVATORS. 1 L 7 2 3O 3A10 1999052800323 19990528 00323 CE 1999 5 28 99ZZZX2079 1 19990323 A 2730 81400011 BRACKET CESSNA 310 310Q 2074242 CE ELEVATOR DAMAGED A CZUA K NONE O OTHER IN INSP/MAINT 1 EA 25 1312G 4446 310Q1153 BOLT HOLES THROUGH BRACKETS, WHICH SUPPORT ELEVATOR BELLCRANK, ELONGATED FORWARD. NOTED DURING ANNUAL INSPECTION. POSS IBLE CAUSE IS TENSION EXERTED ON BRACKETS BY CABLE TENSION AND CONSTANT FORWARD STRESS CAUSED BY USE OF THE ELEVATORS. 1 L 7 2 3O 3A10 1999052800324 19990528 00324 CE 1999 5 28 99ZZZX2080 1 19990324 A 2730 081400011 BRACKET CESSNA 310 310R 2074245 CE ELEVATOR DAMAGED A CZUA K NONE O OTHER IN INSP/MAINT 1 EA 25 1921G 4387 310R0062 DURING ANNUAL INSPECTION, NOTED EXCESSIVE FORE AND AFT PLAY OF ELEVATOR BELLCRANK. INVESTIGATION REVEALED ELEVATOR BELL CRANK SUPPORT BRACKETS LEFT AND RIGHT TO HAVE SEVERELY ELONGATED BOLT HOLES. 1 L 7 2 3O 3A10 1999052800325 19990528 00325 CE 1999 5 28 99ZZZX2081 1 19990324 A 2730 081400010 BRACKET CESSNA 310 310R 2074245 CE ELEVATOR DAMAGED A CZUA K NONE O OTHER IN INSP/MAINT 1 EA 25 1921G 4387 310R0062 DURING ANNUAL INSPECTION, NOTED EXCESSIVE FORE AND AFT PLAY OF ELEVATOR BELLCRANK. INVESTIGATION REVEALED ELEVATOR BELL CRANK SUPPORT BRACKETS LEFT AND RIGHT TO HAVE SEVERELY ELONGATED BOLT HOLES. 1 L 7 2 3O 3A10 1999052800326 19990528 00326 CE 1999 5 28 99ZZZX2082 1 19990324 A 2730 081A00011 BRACKET CESSNA 310 310R 2074245 CE ELEVATOR DAMAGED A CZUA K NONE O OTHER IN INSP/MAINT 1 EA 25 69610 8903 310R0102 DURING 100-HOUR INSPECTION, NOTED EXCESSIVE FORE AND AFT PLAY OF ELEVATOR. INVESTIGATION REVEALED ELEVATOR BELLCRANK SU PPORT BRACKET BOLT HOLES SEVERELY WORN. DETAILED DESCRIPTION OF DAMAGE AS WELL AS RECOMMENDATIONS FOR DETECTION AND PRE VENTION CAN BE FOUND ON SIMILAR REPORTS ISSUED BY THIS CARRIER ON CESSNA 310Q, SN 1153 (3-23-99) AND CESSNA 310R, SN 006 2 (3-24-99). THIS WAS THE FIRST OF THREE SUCH OCCURRENCES NOTED OUT OF THE FOUR 310 SERIES AIRCRAFT MAINTAINED BY THIS SHOP. 1 L 7 2 3O 3A10 1999052800327 19990528 00327 CE 1999 5 28 99ZZZX2083 1 19990324 A 2730 081A00010 BRACKET CESSNA 310 310R 2074245 CE ELEVATOR DAMAGED A CZUA K NONE O OTHER IN INSP/MAINT 1 EA 25 69610 8903 310R0102 DURING 100-HOUR INSPECTION, NOTED EXCESSIVE FORE AND AFT PLAY OF ELEVATOR. INVESTIGATION REVEALED ELEVATOR BELLCRANK SU PPORT BRACKET BOLT HOLES SEVERELY WORN. DETAILED DESCRIPTION OF DAMAGE AS WELL AS RECOMMENDATIONS FOR DETECTION AND PRE VENTION CAN BE FOUND ON SIMILAR REPORTS ISSUED BY THIS CARRIER ON CESSNA 310Q, SN 1153 (3-23-99) AND CESSNA 310R, SN 006 2 (3-24-99). THIS WAS THE FIRST OF THREE SUCH OCCURRENCES NOTED OUT OF THE FOUR 310 SERIES AIRCRAFT MAINTAINED BY THIS SHOP. 1 L 7 2 3O 3A10 1999052800342 19990528 00342 SO 1999 5 28 99ZZZX2098 2 19990511 A 8530 646277 TAPPET CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO ENGINE CHIPPED A YAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 755AB 462 20700622 814923R CAMSHAFT AND LIFTER FOUND CHIPPED OR SPAWLED DURING C/W CSB 99-3A. 1 H 7 1 3O 3 O A16CE E5CE 1999052800343 19990528 00343 SO 1999 5 28 99ZZZX2099 1 19990505 A 6120 30929005 CONTROL CABLE PIPER PA23 PA23250 7102308 SO PROPELLER FAILED A IAWA K NONE O OTHER IN INSP/MAINT 1 EA 17 6913A 1795 277954108 DURING MAINTENANCE FOUND CABLE FAILED BETWEEN QUADRANT AND FIRST PHENOLIC CLAMP. 1 L 7 2 3O 1A10 1999052800352 19990528 00352 EA 1999 5 28 99ZZZX2108 2 19990324 A 7250 310682001 DUCT BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA LT ENGINE FAILED A P HSRA K NONE O OTHER IN INSP/MAINT 1 NM 05 900DN 2595 B170 PCE92382 THE DEFECT WAS FOUND DURING A REGULAR INSPECTION. UPON VISUAL INSPECTION THROUGH THE EXHAUST DUCTS, NOTED THE INNER SEC TION DUCT ASSY PN 3106820-01 HAD SPLIT, BROKE UP AND CURLED UP. THE END OF THIS CURLED UP METAL PIECE OF THE DUCT HAD C OME IN CONTACT WITH THE POWER TURBINE, THEREFORE, DESTROYING ALL THE POWER TURBINE BLADES. THE BLADES WERE CUT THROUGH EXACTLY THE SAME WAY. THE DEEPEST CUT ON EACH BLADE WAS ALMOST ONE-THIRD OF THE WAY THROUGH. THE LENGTH OF THE DAMAGE ON EACH BLADE WAS ALMOST 1.50 INCHES LONG. SUBMITTER STATED CATASTROPHIC ENGINE FAILURE WAS POSSIBLE. 1 L 7 2 3T 4 T A14CE E4EA 1999052800353 19990528 00353 CE 1999 5 28 99ZZZX2109 1 19990426 A 5720 CAP BEECH 99 99 1154002 CE LT MLG WW CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 95WA U6 CRACK FOUND IN LEFT GEAR WELL AFT OF MAIN SPAR ON INBOARD SIDE OF THE CAP IN THE VICINITY OF THE NACELLE SPLICE PLATE. 1 L 7 2 3T A14CE 1999052800355 19990528 00355 EA 1999 5 28 99ZZZX2111 2 19990324 A 7250 310682001 DUCT BEECH 100 B100 1152919 CE PWA PT6 PT6A28 EA LT ENGINE FAILED A P HSRA K NONE O OTHER IN INSP/MAINT 1 NM 05 53MD 2036 B86 PCE50122 DEFECT WAS FOUND DURING A REGULAR INSPECTION. UPON VISUAL INSPECTION THROUGH EXHAUST DUCTS, NOTICED THE 'SKI SLOPE' IN NER SECTION DUCT ASSY PN 31068200-01 MISSING THE AFT PORTION OF ITS TAPERED CONE. NOTED THE POWER TUBE DAMAGED AND ALL BLADES DESTROYED. APPARENTLY, A PIECE OF IT HAD CURLED UP AND ENGAGED ITSELF WITH THE POWER TURBINE, THEREFORE, GRINDIN G OUT THE CENTER OF EACH POWER TURBINE BLADE EQUALLY. THE AFT PART OF THE CONE IS MISSING. THE BLADES WERE CUT THROUGH EXACTLY THE SAME WAY. THE DEEPEST CUT ON EACH BLADE WAS ALMOST ONE-THIRD OF THE WAY THROUGH. THE LENGTH OF THE DAMAGE ON EACH BLADE WAS ALMOST 1 INCH. SUBMITTER STATED CATASTROPHIC ENGINE FAILURE WAS POSSIBLE. 1 L 7 2 4T 4 T A14CE E4EA 1999052800357 19990528 00357 NE 1999 5 28 R7MA0000613 2 19990414 A 7321 0164348300 FCU AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1 60030 NE NR 2 ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 2730 C370B 10018 16016 NR 2 ENGINE IDLE AND TORQUE CHANGES IRREGULARLY. UPON REMOVAL, FOUND FUEL IN P2 LINE AT FCU. 1 G 7 2 3U 3 U RT H7EU E19EU 1999052800358 19990528 00358 EU 1999 5 28 R7MA0000612 1 19990413 A 7332 109072924113 TRANSDUCER AGUSTA A109 A109K2 0260502 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 726 10016 PRESSURE TRANSDUCER FAILED; WENT BELOW ZERO PSI DURING FIRST FLIGHT. (X) 1 G 7 2 3U RT H7EU 1999052800361 19990528 00361 NM 1999 5 28 99ZZZX2115 1 19990401 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1148 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 76753 21249 DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT STA 1148 BETWEEN BILGE AND STR 29R. 2 L 7 3 4F A3WE 1999052800363 19990528 00363 NM 1999 5 28 99ZZZX2117 1 19990325 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 1010 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 76753 21249 DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR TIE STA 1010 - STR 28R. 2 L 7 3 4F A3WE 1999052800366 19990528 00366 EU 1999 5 28 99ZZZX2120 1 19990226 A 2822 P94B12209 PUMP SNIAS 350 AS350BA 8680817 EU BOOST PUMP MALFUNCTIONED A M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 92MH 301 20940 2898 MOTOR WORKS, BUT UNIT HAS NO PRESSURE OUTPUT, LOOSE INTERNALLY. 1 G 7 1 3U NC H9EU 1999052800367 19990528 00367 EA 1999 5 28 ASOA99016 1 19990202 A 3350 20131A POWER SUPPLY CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 826AS 7210 ATL - FLT 4674 - PRE-FLIGHT - CREW REPORTED THE FORWARD FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. ATL MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR F URTHER SERVICE. (X) 2 L 7 2 4F RT A21EA 1999052800368 19990528 00368 EA 1999 5 28 ASOA99006 1 19990112 A 7931 601509197 TRANSDUCER CNDAIR CL600 CL6002B19 EA LT ENGINE FAILED A ASOA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 11 828AS 7213 ATL/CHA - FLT 4621 - EN ROUTE, LEFT ENGINE OIL PRESSURE WENT TO ZERO PSI. CREW SHUT DOWN THE LEFT ENGINE PER QRH SINGLE ENGINE PROCEDURE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED AT CHA UNEVENTFULLY. ASA MECHANIC SWAPPED THE PRESSURE TR ANSDUCERS AND CONFIRMED INDICATION ONLY. AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT TO MCN. MCN MAINTENA NCE REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE TRANSDUCER. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAF T WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4F RT A21EA 1999052800369 19990528 00369 EA 1999 5 28 ASOA99015 1 19990128 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA EXTERIOR FAILED A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 828AS 7213 OUTSTATION ROA - FLT 4714 - CREW REPORTED THE 2 EXTERIOR EMERGENCY EXIT LIGHTS ON THE RT REAR OF THE AIRCRAFT WERE INOPE RATIVE. LOCAL MAINTENANCE SWAPPED AN OPERABLE BULB FROM THE LEFT SIDE TO THE RIGHT IAW MEL 33-51-2 AND FLIGHT CONTINUED TO ATL. ATL MAINTENANCE REMOVED AND REPLACED BURNED OUT LIGHT BULBS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WA S RELEASED FOR FURTHER SERVICE (X) 2 L 7 2 4F RT A21EA 1999052800370 19990528 00370 EA 1999 5 28 ASOA99018 1 19990203 A 5610 602R330339 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A ASOA O OTHER O OTHER DE DESCENT 1 SO 11 830AS 7236 DTW/ATL - FLT 4630 - DURING DESCENT AT 12,800 FEET AND 280 KNOTS, THE LEFT WINDSHIELD CRACKED. CREW DECLARED AN EMERGEN CY AND LANDED IN ATL WITHOUT FURTHER INCIDENT. ATL MAINTENANCE REMOVED AND REPLACED THE LEFT WINDSHIELD. OPERATIONAL A ND PRESSURE CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4F RT A21EA 1999052800371 19990528 00371 EA 1999 5 28 ASOA99002 1 19990104 A 2750 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER N FALSE WARNING AP APPROACH 1 SO 11 833AS 7246 ATL/DTW - FLT 4626 - EXPERIENCED 'FLAP FAIL' MESSAGE ON EICAS DURING VISUAL APPROACH TO DTW. CREW PERFORMED GO-AROUND, DECLARED AN EMERGENCY AND LANDED ZERO FLAPS WITH NO FURTHER PROBLEMS. MTC CNTL INSTRUCTED CREW TO RESET CIRCUIT BREAKER S AND UPON RESET, MESSAGE CLEARED. AIRCRAFT POSITIONED TO MCN FOR A FLAP RIGGING CHECK. MCN MAINTENANCE PERFORMED A D IAGONISTIC CHECK OF THE FECU AND FOUND 5 FAULT CODES AND 3 LRU CODES. MAINT COMPLETED AN OPERATIONAL CHECK OF THE FECU, RIGGING CHECK OF THE BPSU, AND INSPECTED THE FLAPS FOR TWISTING, SKEWING OR ABNORMAL DEFORMATION. C/W AD98-20-1. ALL OPERATIONAL CHECKS WERE COMPLETED SATISFACTORILY, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4F RT A21EA 1999052800372 19990528 00372 EA 1999 5 28 ASOA99030 1 19990307 A 3350 BR9279232 LENS CNDAIR CL600 CL6002B19 EA EXTERIOR MISSING A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 835AS 7258 OUTSTATION GPT - FLT 4672 - CREW REPORTED THE EXTERIOR EMERGENCY FLOOD LIGHT LENS IS MISSING. AIRCRAFT WAS FERRIED TO A TL FOR REPAIR. ATL MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4F RT A21EA 1999052800373 19990528 00373 EA 1999 5 28 ASOA99031 1 19990309 A 5610 601R330339 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 836AS 7263 ATL/PFN - FLT 4706 - CLIMBING THROUGH 6,000 FEET, LEFT WINDSHIELD SHATTERED. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. (X) 2 L 7 2 4F RT A21EA 1999052800374 19990528 00374 CE 1999 5 28 MASA99061 1 19990420 A 3260 1003810061 SWITCH 5082020517 BEECH 1900 1900D 1154162 CE NLG DEFECTIVE A MASA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 07 138YV UE138 PIT/JHW - FLT 5991 - UPON APPROACH INTO JHW, CREW REPORTED UPON GEAR EXTENSION, THE NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. THE CREW MANUALLY EXTENDED THE GEAR, BUT STILL DID NOT RECEIVE DOWN AND LOCKED INDICATION. AN EMERGENC Y WAS DECLARED, THE JHW ATC TOWER OBSERVED THE NOSE GEAR WAS EXTENDED. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. M AINTENANCE REPLACED THE NOSE GEAR DOWN AND LOCKED SWITCH, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999052800375 19990528 00375 NE 1999 5 28 PLGA990330 2 19990330 A 7261 CHIP LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE ILLLUMINATED A PLGA K NONE N FALSE WARNING AP APPROACH 1 NE 05 338BE 340A034 LGA - FLT 6554 - ON APPROACH TO LA, THE LEFT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. ALL ENGINE PARAMETERS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO PIECES OF ACCEPTABLE METAL ON THE CHIP DETECTOR. THE CHIP DE TECTOR WAS CLEANED AND PENALTY RUNS PERFORMED WITH NO RECURRENCE OF THE CHIP LIGHT. THE AIRCRAFT WAS RETURNED TO SERVIC E. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1999052800376 19990528 00376 EA 1999 5 28 UHLA6401 1 19990412 A 3350 6104789 BATTERY PACK 82410191009 DHAV DHC8 DHC8311 1386006 EA CABIN DISCHARGED A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 802SA 250 UHLA - BUF/TTN - FLT 127 - DURING PRE-FLIGHT CHECKS, MAINTENANCE CONTROL WAS NOTIFIED THE FORWARD OVERHEAD EMERGENCY LI GHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY BATTERY PACK PS2. OPS CHECK GOOD. AIRCRAFT CONTINUED WITHOUT FURTHER INCIDENT. (X) 2 H 7 2 4T RT A13NM 1999052800377 19990528 00377 EA 1999 5 28 VTZA9907382 1 19990314 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PASSENGER DOOR NOT ENGAGED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 635BR 7295 IAD/DAY - FLT 7711 - DURING CRUISE AT 1850 HOURS ON 3-14-99, AIRCRAFT RETURNED TO IAD DUE TO PASSENGER DOOR HANDLE STOW MASTER CAUTION LIGHT COMING ON DURING FLIGHT. FLIGHT CREW CONTACTED DISPATCH AND MAINTENANCE CONTROL. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AL ASSOCIATED LATCHES AND LOCKING FEATURES AND FOUND THE DOOR HANDLE WAS NOT FULLY SEATED. SEATED DOOR HANDLE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999052800378 19990528 00378 CE 1999 5 28 99ZZZX2121 1 19990320 A 3610 66002021 VALVE LEAR 35 35A 5170602 CE ENGINE MALFUNCTIONED A YHPA A B UNSCHED LANDING EMER. DESCENT P NO WARNING INDICATION CR CRUISE 1 NM 03 292ME 1147 292 SDL/IND - WHILE EN ROUTE AFTER CLIMB-OUT TO 40,000 FEET MSL, FLIGHT CREW NOTICED CABIN PRESSURIZATION CLIMBING. FLIGHT CREW MADE A PRECAUTIONARY EMERGENCY DESCENT AND DIVERTED TO GUP. MAINTENANCE REMOVED AND REPLACED BLEED AIR REGULATING V ALVES. AIRCRAFT RETURNED TO SERIVCE. 2 L 7 2 4F A10CE 1999052800379 19990528 00379 NE 1999 5 28 USAASA99001 2 19990329 A 7261 OIL CAP AIRBUS A319 A319112 EU CFMINT CFM56 CFM565B6 13802 NE RT ENGINE LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 703UW 0904 PHX - FLT 17 - EN ROUTE PHL/LAX, THE RIGHT ENGINE OIL QUANTITY BEGAN DROPPING ONE-HALF QUART EVERY 15 MINUTES. AS A PR ECAUTION, THE FLIGHT DIVERTED TO PHX AND LANDED WTIHOUT FURTHER INCIDENT. CONTRACT MAINTENANCE FOUND THE OIL COMING FRO M THE FILL CAP AREA. THEY SERVICED THE RIGHT ENGINE OIL AND TIGHTENED THE FILL CAP. THEY PERFORMED AN ENGINE RUN WITH NO LEAKS NOTED. (X) 2 L 7 2 4F 4 F RT A28NM E37NE 1999052800380 19990528 00380 NM 1999 5 28 UIEA9912 1 19990227 A 2840 285U0143201 LOGIC CARD BOEING 747 74747UF 1384949 NM FUEL SYSTEM FAILED A UIEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 15 493MC 29254 ATO - FLT CV7746/27 - TAKEOFF ABORTED AT 70 KNOTS DUE NR 4 FUEL SPAR VALVE STATUS MESSAGE EICAS AND CIRCUIT BREAKERS TRI PPED. RETURNED TO RAMP. DURING TROUBLESHOOTING. MAINTENANCE DETERMINED THAT FUEL SPAR VALVE POSITION LOGIC CARD NR 12 , PN 285U0143-201, WAS DEFECTIVE. REPLACED LOGIC CARD AND OPERATION NOW NORMAL. (X) 2 L 7 4 4F RT 1384945 1999052800381 19990528 00381 SO 1999 5 28 AD6A99001 1 19990412 A 6120 582855 VALVE HOUSING HAMSTD LKHEED 382 382G 526414U SO PROPELLER DEFECTIVE A AD6A H DEACTIVATE SYST/CIRCUITS P NO WARNING INDICATION CR CRUISE 1 SO 03 82178 238858 5048 NR 4 PROPELLER FLUCTUATED 1 TO 1.5 PERCENT, WENT TO MECK AND RPM DROPPED TO 97 PERCENT WITH MOVEMENT OF THROTTLE. SHUT ENGINE DOWN PRECAUTIONARY. MAINTENANCE FOUND A FAULTY PROPELLER VALVE HOUSING PN 582855 AND REPLACED SAME. (X) 2 H 7 4 4T A1SO 1999052800382 19990528 00382 WP 1999 5 28 99ZZZX2122 1 19990506 A 5350 595591368 FAIRING DOUG DC9 DC932 3022066 WP RT WING/FUS CRACKED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 35 930BB 47521 DURING POST FLIGHT WALK-AROUND, THE RT UPPER WING-TO-FUSELAGE FAIRING (SECOND FROM FORWARD) WAS FOUND BENT BACK AT THE L EADING EDGE, AND CRACKED IN THE AFT CENTER AREA. THE FAIRING ATTACHING HARDWARE WAS STILL INSTALLED. PART REPLACED. IN SPECTION OF THE AIRCRAFT AND RT ENGINE REVEALED NO MATERIAL SEPARATION OR ADDITIONAL DAMAGE. REF: IPC 53-50-00/FIGURE 4/ITEM 25. REF: AIRCRAFT TT: 77,810.6 AND TC: 58.315. 2 L 7 2 4F A6WE 1999052800383 19990528 00383 NM 1999 5 28 99ZZZM301 1 19990101 A 4920 380029812 APU BOEING 757 75723N 1384973 NM APU COMPT FAILED A AMTA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 11 516AT 27972 WHILE PERFORMING PREFLIGHT, THE APUT HAD OIL PRESSURE SHUT DOWN (HIGH OIL CONSUMPTION). REMOVED AND REPLACED APU PER MM , OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 1999052800384 19990528 00384 NM 1999 5 28 99ZZZM302 1 19990203 A 3350 110049 BATTERY CHARGER BOEING 727 727264 138408M NM ROW 1-10 INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 764AT 22984 DURING PREFLIGHT, FOUND THE FIRST TEN ROWS OF EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD BATTERY CHARGER P ER MM 33-50. (M) 2 L 7 3 4F A3WE 1999052800385 19990528 00385 WP 1999 5 28 99ZZZM303 1 19990213 A 3350 CONNECTOR LKHEED 1011 10113851 5265010 WP CABIN DAMAGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 191AT 193C1084 DURING PREFLIGHT, FOUND EXTERIOR ESCAPE LIGHT INOPERATIVE AT R2 POSITION. REPAIRED TERMINALS AT GROUNDING STUDS FOR R2 EMERGENCY LIGHTS POWER PACK. EXTERIOR AND INTERIOR EMERGENCY LIGHTS CHECKED NORMAL. (M) 2 L 7 3 4F A23WE 1999052800386 19990528 00386 NM 1999 5 28 99ZZZM304 1 19990214 A 3350 BATTERY CHARGER BOEING 757 75723N 1384973 NM BS 1324 FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 518AT 27974 DURING PREFLIGHT, FOUND EMERGENCY EGRESS TRACK LIGHTING AT 28 DEF TO END OF RIGHT MID LAVATORY INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER AT LOCATION STATION 1324. OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 1999052800387 19990528 00387 NM 1999 5 28 99ZZZM305 1 19990221 A 3350 POWER SUPPLY BOEING 757 75723N 1384973 NM ROW 27 INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 DURING PREFLIGHT, FOUND EGRESS LIGHT AT ROW 27 TO AFT LAVATORY LIGHTS INOPERATIVE. REMOVED AND REPAIRED BATTERY POWER S UPPLY AT ROW 27-28, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 1999052800388 19990528 00388 1999 5 28 99ZZZM306 4 19990224 A 2565 D30654122 SLIDE BOEING 757 75723N 1384973 NM 1R DOOR DRAGGING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 518AT 27974 BOTTOM OF SLIDE COVER DRAGS ON DOOR FRAME WHEN 1R ENTRY DOOR IS OPENED. REMOVED AND REPLACED R1 DOOR SLIDE IAW MM 25-66 -01, DOOR OPENS AND CLOSES FINE, OK DOOR SERVICE. (M) 2 L 7 2 4F RT A2NM 1999052800389 19990528 00389 NM 1999 5 28 99ZZZM307 1 19990321 A 3397 WIRE BOEING 727 727290 138408W NM CABIN SHORTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 774AT 21510 DURING PREFLIGHT, FOUND AFT SECTION EGRESS TRACK LIGHTING INOPERATIVE. FOUND SHORTED WIRE (WIRING DIAGRAM 33-51-03, WIR E REF NR L7030A22) SPLICED WIRE. (M) 2 L 7 3 4F A3WE 1999052800390 19990528 00390 NM 1999 5 28 99ZZZM308 1 19990329 A 3397 WIRE BOEING 727 727208 138407W NM GALLEY SHORTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 780AT 22295 DURING PREFLIGHT, FOUND FORWARD FLOOR EGRESS LIGHTING INOPERATIVE. REPAIRED SHORTED WIRE AT 1R GALLEY DOOR EXIT IDENTIF IER. (M) 2 L 7 3 4F RT A3WE 1999052800391 19990528 00391 NM 1999 5 28 99ZZZM309 1 19990408 A 3350 100865 POWER SUPPLY BOEING 727 727208 138407W NM ROW 1-5 INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 780AT 22295 DURING PREFLIGHT, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE FIRST 5 ROWS. REMOVED AND REPLACED POWER SUPPLY PER MM 33-50 -00, OPS CHECKED GOOD. (M) 2 L 7 3 4F RT A3WE 1999052800392 19990528 00392 NM 1999 5 28 99ZZZM310 1 19990411 A 3350 FUSE BOEING 757 75723N 1384973 NM ROW 22 FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 DURING PREFLIGHT, FOUND THE FLOOR EGRESS LIGHTS FROM ROW 22 THROUGH AFT LAVATORY INOPERATIVE. REMOVED AND REPLACED FUSE ON BATTERY CHARGER FOR ROWS 22 THROUGH AFT LAV, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 1999052800393 19990528 00393 NM 1999 5 28 99ZZZM311 1 19990414 A 3350 S106 BATTERY BOEING 727 727290 138408W NM L1 DOOR DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 775AT 21511 DURING PREFLIGHT, FOUND L1 DOOR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED L1 DOOR OVERHEAD EMERGENCY LIGHT BATTERY, OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999052800394 19990528 00394 NM 1999 5 28 99ZZZM312 1 19990426 A 3397 WIRE BOEING 727 727208 138407W NM R1 DOOR CHAFED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 780AT 22295 DURING PREFLIGHT, FOUND FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPAIRED CHAFED WIRE AT R1 DOOR F LOOR EMERGENCY EXIT LIGHT IAW WIRING DIAGRAM 33-51-03. OPS CHECKED GOOD. (M) 2 L 7 3 4F RT A3WE 1999052800395 19990528 00395 NM 1999 5 28 99ZZZM313 1 19990505 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM RT EMER EXIT DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 769AT 21998 DURING PREFLIGHT, FOUND RIGHT AFT EMERGENCY EXIT OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED PACK IAW MM 33-50-22, OPS CHECKED NORMAL, OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 1999052800396 19990528 00396 WP 1999 5 28 USAA990388 1 19990417 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 814US 46796 48094 PIT - DURING C3 CHECK, FOUND 1 INCH CRACK IN SKIN AT STATION 200 LONGERON 15L. REPAIRED WITH EXTERNAL DOUBLER PER SRM 5 3-05 FIG 57A. (M) 2 L 7 2 4F A6WE 1999052800397 19990528 00397 WP 1999 5 28 USAA990340 1 19990330 A 5320 CEILING DOUG DC9 DC931 3022065 WP BS 154/158 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 926VJ 42127 48146 PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AND 1 INCH CRACK AT CABIN FLOOR CEILING AT STATION 154 AND 158 ABOVE RIGHT OUTBOARD PULLEY CABLE AROUND 2 CREWS. REMOVED AND REPLACED DEFECTIVE PART. (M) 2 L 7 2 4F A6WE 1999052800398 19990528 00398 WP 1999 5 28 USAA990383 1 19990414 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 64730 47352 PIT - DURING C-2 CHECK, FOUND TWO CRACKS IN FUSELAGE SKIN .5 INCH AND 1.125 INCH AT STATION 1087 LONGERONS 3 AND 4 RIGHT . INSTALLED FILLERS AND DOUBLERS PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1999052800399 19990528 00399 WP 1999 5 28 USAA990384 1 19990414 A 5330 SKIN DOUG DC9 DC931 3022065 WP CARGO DOORWAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 64730 47352 PIT - DURING C-2 CHECK, FOUND 20 INCH OF CORROSION ON SKIN BELOW FORWARD CARGO DOOR UNDER SCUFF PLATE, CORROSION LEVEL 1 . CUT OUT CORRODED AREA AND INSTALLED FILLER AND DOUBLERS PER SRM 53-05 FIG 105. (M) 2 L 7 2 4F A6WE 1999052800400 19990528 00400 WP 1999 5 28 USAA990385 1 19990414 A 5230 59101415 PAN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 64730 47352 PIT - DURING C-2 CHECK, FOUND CARD 001, .75 INCH CRACK TOP FORWARD STOP AND CARD 002, 3 INCH LONG CRACK UPPER HINGE OUTT ER PAN AT UPPER FORWARD SECTION OF PAN OF FORWARD CARGO DOOR. INSTALLED ONE EXTERNAL DOUBLER PER SRM 53-03 FIG 8. (M) 2 L 7 2 4F A6WE 1999052800401 19990528 00401 WP 1999 5 28 USAA990386 1 19990414 A 5230 59101415 PAN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 64730 47352 PIT - DURING C-2 CHECK, FOUND .625 INCH CRACK IN AFT CARGO DOOR PAN IN TOP DOOR STOP PAN, AFT DOOR. INSTALLED EXTERNAL DOUBLER PER SRM 52-03 FIG 7. (M) 2 L 7 2 4F A6WE 1999052800402 19990528 00402 WP 1999 5 28 USAA990387 1 19990415 A 5311 99118433 FRAME DOUG DC9 DC931 3022065 WP BS 1169 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 983VJ 41856 48159 PIT - DURING RON, FOUND 2.5 INCH CRACK ACROSS AFT CANTED FRAME AT UPPER RIGHT SECTION STATION 1169. CUT OUT SECTION OF FRAME, USED PRODUCTION SPLICE TYPE REPAIR AT UPPER END AND ORIGINAL PRODUCTION SPLICE AT LOWER END PER EA 51933. (M) 2 L 7 2 4F A6WE 1999052800403 19990528 00403 WP 1999 5 28 USAA990389 1 19990418 A 5400 STRUCTURE DOUG DC9 DC931 3022065 WP LT PYLON DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 970VJ 81691 47050 PIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT ENGINE FAILURE, DETROIT FOUND 22 INCH BY 8 INCH SECTION OF LT UPPER P YLON SKIN (SKIN, WEB PANEL AND ANGLES) TORN AT STATION 1038, DETECTED IN FLIGHT, PASSENGERS HEARD LOUD NOISE. INSTALLED DOUBLER OVER CUT OUT AREA ON SKIN. REPLACED WEB PANEL AND ANGLES AT STATION 1038. WEB PANEL MANUFACTURED FROM TITANIU M SHEET. REPAIRED PER EA 51786, SRM 53-04-12B. (M) 2 L 7 2 4F A6WE 1999052800404 19990528 00404 WP 1999 5 28 USAA990400 1 19990422 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 4 INCH CORROSION GALLEY AREA NR 49 FLOORBEAM TOP AND LOWER SURFACES, CORROSION L EVEL 1. MANUFACTURED FLOOR SUPPORT AND INSTALLED SAME PER SRM 53-11-1 TYPE A1 AND A2 FIG 11 SHEET 2, ITEM 10. (M) 2 L 7 2 4F A6WE 1999052800405 19990528 00405 WP 1999 5 28 USAA990401 1 19990422 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 5 INCH CORROSION AT STATION 218-237 FLOORBEAM CAP AT CENTER, CORROSION LEVEL 1. FABRICATED AND INSTALLED NEW SECTION BY SPLICING PER TYPICAL REPAIR 53-11-21A. (M) 2 L 7 2 4F A6WE 1999052800406 19990528 00406 WP 1999 5 28 USAA990402 1 19990422 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 8 INCH CORROSION AT GALLEY AREA FLOORBEAM NR 44 TOP AND LOWER SURFACE, CORROSION LEVEL 1. FABRICATED FLOORBEAM AND INSTALLED PER SRM 53-11-1. (M) 2 L 7 2 4F A6WE 1999052800407 19990528 00407 WP 1999 5 28 USAA990403 1 19990422 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 207 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN WEB FINGER AT STATION 207 LONGERON 15L. CUT OUT CRACK SECTION OF WEB, INS TALLED A FILLER AND A DOUBLER PER EA 51868. (M) 2 L 7 2 4F A6WE 1999052800408 19990528 00408 WP 1999 5 28 USAA990404 1 19990422 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200-237 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 6 INCH CORROSION IN FLOOR SUPPORT JUST INBOARD OF SEAT TRACK 19 AT STATION 200-2 37, CORROSION LEVEL 1. FABRICATED NEW FLOOR SUPPORT FROM EXTRUSION AND INSTALLED SAME PER SRM 53-11-1. (M) 2 L 7 2 4F A6WE 1999052800409 19990528 00409 WP 1999 5 28 USAA990405 1 19990422 A 5320 SUBFLOOR DOUG DC9 DC931 3022065 WP BS 218 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 3 INCH BY 3 INCH CORROSION IN SUBFLOOR AT STATION 218, OUTBOARD OF SEAT TRACK 18, CORROSI ON LEVEL 1. CUT OUT DAMAGE AND SPLICED IN A NEW SECTION PER EA 51977. (M) 2 L 7 2 4F A6WE 1999052800410 19990528 00410 WP 1999 5 28 USAA990406 1 19990422 A 5320 59122850806 FRAME DOUG DC9 DC931 3022065 WP LT WINDOW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND .25 INCH CRACK IN SKIN FRAME AT LEFT WINDOW NR 23 LOWER AFT FRAME SECTION AROUND HUCK BOLT . STOP DRILLED CRACK AND INSTALLED A REPAIR ANGLE PER TYPICAL REPAIR 53-30-06A. (M) 2 L 7 2 4F A6WE 1999052800411 19990528 00411 WP 1999 5 28 USAA990407 1 19990422 A 5320 BEAM DOUG DC9 DC931 3022065 WP FRAME 897 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND CORROSION 1 INCH BY .5 INCH FIVE EACH AREAS INSIDE AND OUTSIDE SURFACE (SEVERAL PLACES) AT FRAME 897 LONGERON 29R AND INTERCOSTAL BEAM, AFT CARGO. CORROSION LEVEL 1. REMOVED TIE DOWN, MANUFACTURED NEW STRAP F OR TOP OF INTERCOSTAL FROM 7075T6 .040 INCH AND INSTALLED A NEW TIE DOWN BRACKET PER SRM 51-10-03. (M) 2 L 7 2 4F A6WE 1999052800412 19990528 00412 WP 1999 5 28 USAA990408 1 19990422 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK IN FUSELAGE SKIN AT STATION 1095 LEFT, BELOW LONGERON 3. REPAIRED WITH FIL LER AND DOUBLER PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1999052800413 19990528 00413 WP 1999 5 28 USAA990409 1 19990422 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND TWO EACH 1.5 INCH CRACKS IN FUSELAGE SKIN AT STATION 1095 RIGHT, BETWEEN LONGERON 3 AND 4 RIGHT. INSTALLED EXTERNAL DOUBLER PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1999052800414 19990528 00414 WP 1999 5 28 USAA990410 1 19990422 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 1140 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK ON RIGHT VERTICAL STAB DRAG ANGLE AT STATION 1140 RIGHT VERTICAL STAB ATTAC H ANGLE. REMOVED CRACKED VERTICAL LEG, INSTALLED REPAIR SPLICE PER SRM 53-05 FIG 23A. (M) 2 L 7 2 4F A6WE 1999052800415 19990528 00415 WP 1999 5 28 USAA990411 1 19990422 A 5230 OUTER PAN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 42285 48144 PIT - DURING Q-4 CHECK, FOUND 3 INCH CRACK IN FORWARD CARGO DOOR OUTER PAN AT UPPER HINGE OF FORWARD CARGO DOOR. INSTAL LED EXTERNAL DOUBLER (A-286) PER SRM 52-03 FIG 8. (M) 2 L 7 2 4F A6WE 1999052800416 19990528 00416 WP 1999 5 28 USAA990432 1 19990428 A 5330 SKIN DOUG DC9 DC982 3022082 WP AIRSTAIR DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 35358 49443 PIT - DURING C-4 CHECK, FOUND 1 INCH LONG CRACK IN SKIN AT LOWER AFT CORNER OF FORWARD AIRSTAIR DOOR CUTOUT. INSTALLED DOUBLER PER SRM 53-05 FIG 57A. (M) 2 L 7 2 4F A6WE 1999052800417 19990528 00417 WP 1999 5 28 USAAD99059 1 19990427 A 2170 17946081 WATER SEPARATOR DOUG DC9 DC982 3022082 WP RT PACK BLOWN A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 825US 49237 CLT - FL 1646 - AFTER TAKEOFF, CREW REPORTED THAT THERE WAS SMOKE IN THE CABIN. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF A FIRE. A BLOWN WATER SEPARATOR ON THE RIGHT PACK WAS FOUND AND REPLACED. (M) 2 L 7 2 4F A6WE 1999052800418 19990528 00418 WP 1999 5 28 USAAD99060 1 19990429 A 3260 INDICATION DOUG DC9 DC931 3022065 WP LANDING GEAR MALFUNCTIONED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 977VJ 48155 CLT - FLT 980 - ON APPROACH TO CLT, CREW DID NOT GET ANY LIGHT INDICATION (RED OR GREEN) WHEN THE GEAR WAS SELECTED DOWN , BUT DID GET THE WARNING HORN. THE CREW DID A GO-AROUND AND RECYCLED THE GEAR. CREW THEN RECEIVED ALL GREEN LIGHTS FO R THE GEAR AND NO WARNING HORN. MAINTENANCE CHECKED OUT THE LANDING GEAR SYSTEM AND DID NOT FIND A PROBLEM. THE LANDIN G GEAR LEVER RELAY WAS REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F A6WE 1999052800419 19990528 00419 NM 1999 5 28 USAABB99020 1 19990425 A 2530 OVEN BOEING 757 7572B7 1384964 NM GALLEY FIRE A USAA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 EA 19 614AU 27145 LAX - FLT 41 - EN ROUTE CLT-LAX, FOOD IN THE NR 2 OVEN CAUGHT ON FIRE. THE FLIGHT ATTENDANTS EXTINGUISHED THE FIRE WITH THE FORWARD HALON FIRE BOTTLE. MAINTENANCE REPLACED THE OVEN. (M) 2 L 7 2 4F RT A2NM 1999052800420 19990528 00420 WP 1999 5 28 ASAA9980099 1 19990501 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND INOPERATIVE. REPLACE D THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800421 19990528 00421 WP 1999 5 28 ASAA9980098 1 19990430 A 3397 WIRE DOUG DC9 DC983 3022083 WP L2 DOOR DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 SEA - DURING MAINTENANCE CHECK, BOTH RED EMERGENCY FLOOR TRACK LIGHTS AT L2 DOOR WERE FOUND INOPERATIVE. REPLACED WIRIN G IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800422 19990528 00422 WP 1999 5 28 ASAA9980097 1 19990430 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES I N THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999052800423 19990528 00423 WP 1999 5 28 ASAA9980095 1 19990427 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS BETWEEN THE AFT LAVATORIES WERE FOUND INOPERATIVES. REPLA CED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800424 19990528 00424 WP 1999 5 28 ASAA9980086 1 19990421 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 973AS 53449 SEA - PRIOR TO DEPARTURE OF FLIGHT 187, CREW REPORTED THE OVERHEAD EMERGENCY LIGHT IN THE FLIGHT COMPARTMENT WAS INOPERA TIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800425 19990528 00425 WP 1999 5 28 ASAA9980084 1 19990416 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 15/28 LOOSE A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 976AS 53452 ANC - PRIOR TO DEPARTURE OF FLIGHT 190, CREW REPORTED SECTIONS OF THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID AND AFT CA BIN WERE INOPERATIVE. SECURED WIRING IN FLOOR TRACK AT ROW 15 AND ROW 28 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800426 19990528 00426 WP 1999 5 28 ASAA9980083 1 19990416 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 0662 49234 PDX - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999052800427 19990528 00427 WP 1999 5 28 ASAA9980082 1 19990415 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 2 DEFECTIVE A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 962AS 53076 PDX - PRIOR TO DEPARTURE OF FLIGHT 590, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. REPLACED WIRE SEGMENT IN FLOOR TRACK AT ROW 2 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800428 19990528 00428 WP 1999 5 28 ASAA9980081 1 19990415 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800429 19990528 00429 NM 1999 5 28 ASAA9940102 1 19990503 A 3350 FUSE BOEING 737 737490 1384715 NM R-2 DOOR FAILED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 791AS 28886 YVR - FLT 688 - THE R-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. FERRIED AIRCRAFT TO LAX. REPLACED FUSE AND EX IT LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800430 19990528 00430 NM 1999 5 28 ASAA9940101 1 19990430 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 19 DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 754AS 25095 OAK - FLT 389 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 19 WERE FOUND INOPERATIVE. RECONNECTED BROKEN WIRING AT RO W 19 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800431 19990528 00431 NM 1999 5 28 ASAA9940096 1 19990423 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PDX - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIR ING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800432 19990528 00432 NM 1999 5 28 ASAA9940095 1 19990422 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 14-17 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 792AS 28887 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14-17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800433 19990528 00433 NM 1999 5 28 ASAA9940094 1 19990422 A 3350 LENS BOEING 737 7374Q8 NM L-2 EXIT SIGN MISSING A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 776AS 25109 SEA - FLT 215 - PRIOR TO DEPARTURE, THE PLASTIC 'EXIT SALIDA' LENS WAS FOUND MISSING FROM THE EXIT SIGN ADJACENT TO THE L-2 DOOR. REPLACED 'EXIT' SIGN LENS ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1999052800434 19990528 00434 NM 1999 5 28 ASAA9940093 1 19990421 A 3350 LENS BOEING 737 7374Q8 NM R2 EXIT SIGN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 PDX - DURING MAINTENANCE CHECK, THE EXIT SIGN LENS AT THE R-2 DOOR WAS FOUND MISSING. REPLACED 'EXIT' SIGN LENS ASSEMBL Y. (M) 2 L 7 2 4F RT A16WE 1999052800435 19990528 00435 NM 1999 5 28 ASAA9910091 1 19990430 A 3350 BATTERY GRIMES BOEING 737 737298C 1384490 NM ROW 6, 8, 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 6, 8 AND 16 WOULD NOT TEST. REPLACED BATT ERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800436 19990528 00436 NM 1999 5 28 ASAA9910090 1 19990429 A 3350 6104781 BATTERY BOEING 737 737210C 1384459 NM ROW 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WERE FOUND INOPERATIVE. REPLACED BATTER Y AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800437 19990528 00437 NM 1999 5 28 ASAA9910089 1 19990426 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM NR 3 PALLET DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS ON THE NR 3 PALLET WERE FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800438 19990528 00438 NM 1999 5 28 ASAA9910088 1 19990425 A 3397 WIRE BOEING 737 737210C 1384459 NM ROW 8-11 BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 ANC - DURING MAINTENANCE CHECK, THE TWO FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ON SEAT PALLET 8-11. REPAIRED BROKEN WIRE AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800439 19990528 00439 NM 1999 5 28 ASAA9910087 1 19990425 A 3350 BATTERY PACK BOEING 737 737210C 1384459 NM ROW 8-10 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 8821004 21822 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WILL NOT TURN ON OR OFF ON SEAT PALLET 8-10. REPL ACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800440 19990528 00440 NM 1999 5 28 ASAA9910086 1 19990424 A 3350 88320012 RECEIVER BOEING 737 737290C 138448V NM ROW 8 FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 8 WAS FOUND INOPERATIVE. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800441 19990528 00441 NM 1999 5 28 99ZZZM314 1 19990424 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM ROW 8 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 8 WAS FOUND INOPERATIVE. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800442 19990528 00442 NM 1999 5 28 ASAA9910085 1 19990424 A 3350 883200312 BATTERY BOEING 737 737210C 1384459 NM PALLET 6-1 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE ON SEAT PALLET 6-1. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800443 19990528 00443 NM 1999 5 28 ASAA9910084 1 19990423 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGH TS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800444 19990528 00444 NM 1999 5 28 ASAA9910083 1 19990422 A 3350 6104781 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS TRANSMITTER WAS FOUND TO BE INOPERATIVE. R EPLACED BATTERY IN TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800445 19990528 00445 NM 1999 5 28 ASAA9910082 1 19990418 A 3397 WIRE BOEING 737 7372X6C 1384552 NM PALLET 6-1 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEAT PALLET 6-1 WERE FOUND TO BE INTERMITTENT. REPLACED SEAT PALLET DURING RECON AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800446 19990528 00446 NM 1999 5 28 ASAA9910081 1 19990415 A 3350 6104781 BATTERY GRIMES BOEING 737 737290C 138448V NM ROW 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WOULD NOT SHUTOFF. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800447 19990528 00447 NM 1999 5 28 ASAA9910080 1 19990415 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM ROW 11 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT PACK AT ROW 11 IS ONLY SHOWING ONE OF THREE TRANSMITTER LED'S FLASHIN G. REPLACED BATTERY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800448 19990528 00448 NM 1999 5 28 ASAA9910079 1 19990415 A 3350 6050401 BATTERY GRIMES BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT SIGN ON REMOVABLE BULKHEAD WOULD NOT TEST PROPERLY. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999052800449 19990528 00449 WP 1999 5 28 ASAA9980088 1 19990424 A 5210 ROTATION ROD DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 957AS 49126 SEA - AFTER ARRIVAL OF FLIGHT 376 - CREW REPORTED THE L1 DOOR WAS DIFFICULT TO LOCK AND UNLOCK. ADJUSTED L1 DOOR ROTATI ON ROD IAW DC9 MM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999052800450 19990528 00450 WP 1999 5 28 ASAA9980087 1 19990424 A 5610 PIN DOUG DC9 DC983 3022083 WP RT COCKPIT LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED AND SECURED UPPER HINGE PIN ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999052800451 19990528 00451 WP 1999 5 28 ASAA9980089 1 19990425 A 5240 49157401 HOOK DOUG DC9 DC982 3022082 WP R1 DOOR WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 955AS 48080 PDX - DURING MAINTENANCE CHECK, THE R1 DOR HOLD OPEN HOOK WOLD NOT ENGAGE. REPLACED R1 DOOR HOLD OPEN HOOK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999052800452 19990528 00452 WP 1999 5 28 ASAA9980090 1 19990425 A 5320 5936038501 FRAME DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT LOWER FRAME ON INBOARD SIDE. REPLACED BEAM IAW DC9 SRM 51-30-05 AND 53-05, FIG 63. (M) 2 L 7 2 4F A6WE 1999052800453 19990528 00453 WP 1999 5 28 ASAA9980091 1 19990425 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON LONGERON 29L AT FS 1309. REMOVED DAMAGED AREA AND SPLICED IN NEW SECTION IAW DC9 SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 1999052800454 19990528 00454 WP 1999 5 28 ASAA9980092 1 19990425 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON FLOORBEAM CAP, LBL 42 AT FS 1338. BLENDED DAMAGED AREA AND INSTALLED DOUBLER ANGLE AND WEAR STRIP IAW DC9 SRM 53-05, FIG 20A. (M) 2 L 7 2 4F A6WE 1999052800455 19990528 00455 WP 1999 5 28 ASAA9980093 1 19990425 A 5320 491141131 FITTING DOUG DC9 DC982 3022082 WP BS 208-218 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON LEFT LOWER FRAME FITTINGS AT FS 208 AND 218. REMOVED DAMAGED FITTINGS AND IN STALLED NEW FITTINGS IAW DC9 SRM 51-30-01 AND 51-30-05. (M) 2 L 7 2 4F A6WE 1999052800456 19990528 00456 WP 1999 5 28 ASAA9980094 1 19990425 A 5320 991007815 ANGLE DOUG DC9 DC982 3022082 WP BS 208 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON R1 DOOR LOWER CUSP ANGLE AT FS 208. REPAIRED IAW ASA EA 5310-01675 AND DC9 S RM 53-05, FIG 55. (M) 2 L 7 2 4F A6WE 1999052800457 19990528 00457 WP 1999 5 28 ASAA9980096 1 19990424 A 5754 59358012 TUBE DOUG DC9 DC983 3022083 WP RT LE FLAP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 OAK - DURING C-CHECK, FOUND GOUGE IN RIGHT WING NR 4 LEADING EDGE SLAT TRACK RETRACT TUBE. INSPECTED IAW ASA EA 5740-01 167, NO CRACK NOTED. BLENDED GOUGED AREA IAW DC9 SRM 57-01, PAGE 4 FIG 1. (M) 2 L 7 2 4F RT A6WE 1999052800458 19990528 00458 NM 1999 5 28 ASAA9940100 1 19990425 A 5210 6523464 SNUBBER BOEING 737 7374Q8 NM L-1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 779AS 25111 SEA - FLT 399 - L-1 DOOR DIFFICULT TO CLOSE. REPLACED L-1 DOOR SNUBBER ASSEMBLY AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999052800459 19990528 00459 NE 1999 5 28 PLGA990427 2 19990427 A 7532 6058T80P03 BLEED VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE STICKING A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 748BA COMD0173 340A149 BOS - FLT 6429 - AFTER DEPARTURE FROM BOS, CREW GOT A RIGHT AIR VALVE FAIL LIGHT. AIRCRAFT DIVERTED BACK TO BOS AND LAN DED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ANTI-ICE START BLEED VALVE WHICH WAS STICKING, AND THE AIR VALVE FOR PRE CAUTIONARY REASONS. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1999052800460 19990528 00460 1999 5 28 PLGA990426 4 19990426 A 3417 6224401001 ADC SAAB SF340 340B 7860101 EU E/E COMPT DEFECTIVE A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 359BE 8059 340B285 BOS - FLT 6439 - AFTER DEPARTURE CREW LOST BOTH TRANSPONDERS, TCAS, AUTO-PILOT, YAW DAMPENERS, AND FLIGHT DIRECTORS. AI RCRAFT DIVERTED BACK TO BOSTON AND LANDED WITHOUT INCIDENT. MAINTENANCE FUOND THE AIR DATA COMPUTER (ADC) TO BE DEFECTI VE. THE ADC WAS REPLACED, REQUIRED OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999052800461 19990528 00461 NE 1999 5 28 PLGA990428 2 19990428 A 7321 7239060502 ECU SAAB SF340 340B 7860101 EU GE CT7TP CT75A2 30030 NE RT ENGINE MALFUNCTIONED A PLGA O OTHER J WARNING INDICATION DE DESCENT 1 NE 05 355BE 0185 340B209 GEC067384 BOS - FLT 6307 - ON FIGHT 6307- PHL-BOS, THE CREW NOTED THE RIGHT ENGINE INCREASING IN POWER AFTER THE 64 DEGREE SWITCH. CREW WENT TO TORQUE MOTOR LOCKOUT AND CONTROL OF THE RIGHT ENGINE WAS REGAINED. AIRCRAFT LANDED WITHOUT INCIDENT IN B OS. MAINTENANCE REPLACED THE ECU AND THE CTOT PANEL, PERFORMED THE REQUIRED OPERATIONAL TEST AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1999052800462 19990528 00462 EU 1999 5 28 PLGA990422 1 19990422 A 3260 ATG130902 SWITCH SAAB SF340 340B 7860101 EU RT MLG FAILED A PLGA O OTHER N FALSE WARNING DE DESCENT 1 NE 05 348BE 340B190 BOS-PHL - FLT 6301 - THE CREW FAILED TO GET A RIGHT GREEN DOWN AND LOCKED LIGHT WHEN GEAR HANDLE WAS LOWERED. CREW FOLL OWED THE CHECKLIST AND THE AIRCRAFT LANDED SAFELY IN PHL. THE LANDING GEAR WAS PINNED AND THE AIRCRAFT MOVED TO A MX BA SE FOR REPAIR. MAINTENANCE COULD NOT DUPLICATE THE ANOMALY AND REPLACED THE RIGHT MLG DOWNLOCK SWITCH AND LANDING GEAR HANDLE AS A PRECAUTION. REQUIRED OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999052800495 19990528 00495 NM 1999 5 28 EIA990086 1 19990207 A 5312 BULKHEAD ANGLE BOEING 747 747121 1384871 NM BS 1335 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 97499 20348 DURING C-CHECK, RIGHT WHEEL WELL, BS 1335 UPPER BULKHEAD ATTACHMENT FOUND CORRODED, NRC 5900. REPLACED T-ANGLE IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999052800496 19990528 00496 NM 1999 5 28 MZZA99083 1 19990402 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 720 CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON STRINGER 26L AT BS 720A. THE CORRODED A REA WAS REMOVED AND REPAIRED PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1999052800497 19990528 00497 NM 1999 5 28 MZZA99081 1 19990309 A 5753 651926913 TRACK BOEING 727 727224 1384076 NM TE FLAPS RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, RUST WAS FOUND ON NR 4 FLAP TRACK FORWARD MOUNTING PAD A UPPER SURFACE AND HOLES. THE RUSTED TRACK, P/N 65-19269-20 WAS REMOVED AND REPLACED WITH P/N 65-19269-13 PER B727 MM 27-51-31 AND OPERATIONAL CHECK FOUND SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999052800498 19990528 00498 NM 1999 5 28 MZZA99080 1 19990407 A 5752 651926013 FITTING BOEING 727 727224 1384076 NM LT AILERON TAB BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A BROKEN LUG WAS FOUND ON LEFT WING OUTBOARD AILERON TAB ROD AT TACHING FITTING. THE BROKEN LUG P/N 65-19620-13 WAS REMOVED AND REPLACED PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1999052800499 19990528 00499 NM 1999 5 28 MZZA99079 1 19990408 A 5313 655848825 STRINGER BOEING 727 727224 1384076 NM BS 940-945 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO PLACES CRACKS WERE FOUND ON STRINGER 18A BETWEEN BS 940 AND BS 945. THE CRACKED STRINGER WAS CUT OFF AND REPAIRED PER ECRA 5310-03842. (M) 2 L 7 3 4F A3WE 1999052800500 19990528 00500 NM 1999 5 28 MZZA99078 1 19990402 A 5753 652163261 REAR SPAR BOEING 727 727224 1384076 NM LT TE MID FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CORROSION ON LEFT INBOARD WING MID FLAP REAR SPAR LOWER C HORD AT WBL 115. THE CORRODED AREA WAS CLEANED UP AND REPAIRED PER EC/RA 5750-03182. (M) 2 L 7 3 4F A3WE 1999052800501 19990528 00501 NM 1999 5 28 MZZA99077 1 19990305 A 2760 BACP30J4 PULLEY BOEING 727 727224 1384076 NM NR 4 SPOILER FROZEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FROZEN BEARING WAS FOUND ON NR 4 SPOILER ACTUATOR PULLEY. TH E DAMAGED PULLEY P/N BACP3QJ4 WAS REMOVED AND REPLACED WITH A NEW ONE PER MM 27-61-41. (M) 2 L 7 3 4F A3WE 1999052800502 19990528 00502 NM 1999 5 28 MZZA99076 1 19990309 A 5753 652163396 REAR SPAR BOEING 727 727224 1384076 NM RT TE MIDFLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY 5 INCH AREA CORROSION WAS FOUND ON RIGHT OUTBOARD M IDFLAP REAR SPAR LOWER CHORD FORWARD FLANGE AT WBL 431. THE CORROSION WAS REMOVED AND REPAIRED PER ECRA 5750-03184 DATE D ON APR 6, 1999. (M) 2 L 7 3 4F A3WE 1999052800503 19990528 00503 NM 1999 5 28 MZZA99075 1 19990310 A 5753 PLATE BOEING 727 727224 1384076 NM RT TE MIDFLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH DIAMETER CORROSION WAS FOUND ON RIGHT INBOARD MIDFLAP INNER SPLICE PLATE AT WBL 242. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 51-30-02, 51-10-02. (M) 2 L 7 3 4F A3WE 1999052800504 19990528 00504 NM 1999 5 28 MZZA99074 1 19990309 A 5753 ANGLE BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .25 INCH LONG CRACK WAS FUOND ON RIGHT INBOARD MIDFLAP T/E LO WER CLOSURE ANGLE AT WBL 108. THE CRACKED AREA WAS CUT OFF AND REPAIRED PER SRM 51-40-04, 51-30-02. (M) 2 L 7 3 4F A3WE 1999052800505 19990528 00505 NM 1999 5 28 MZZA99073 1 19990303 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1184 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH LONG CRACK WAS FOUND ON AFT BILGE SKIN AT BS 1184. TH E CRACK AREA WAS CUT OFF AND REPAIRED PER SRM 53-30-03. (M) 2 L 7 3 4F A3WE 1999052800506 19990528 00506 NM 1999 5 28 MZZA99072 1 19990309 A 5315 BAC14902785 FLOORBEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON NR 6A GALLEY FLOORBEAM BETWEEN RBL 32 AND RBL 44 AT BS 1130. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 53-10-08 AND 51-10-02. (M) 2 L 7 3 4F A3WE 1999052800507 19990528 00507 NM 1999 5 28 MZZA99071 1 19990309 A 5320 BAC1510335 SUPPORT BOEING 727 727224 1384076 NM BS 1138 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AN IG CORROSION WAS FOUND ON LEFT AFT LAVATORY FORWARD SUPPORT HAT CHANNEL BETWEEN LBL 28 AND LBL 34 AT BS 1138. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 53-10-02 AND 51-40-04. (M) 2 L 7 3 4F A3WE 1999052800508 19990528 00508 NM 1999 5 28 MZZA99070 1 19990305 A 5330 SKIN BOEING 727 727224 1384076 NM BS 798 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH BY .5 INCH AREA IG CORROSION WAS FOUND ON FUSELAGE SKI N BETWEEN BS 798 AND STRINGER 10L. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 53-30-03 FIG 15A 51-10-02. (M) 2 L 7 3 4F A3WE 1999052800509 19990528 00509 NM 1999 5 28 MZZA99069 1 19990304 A 2760 BACP30K2D PULLEY BOEING 727 727224 1384076 NM NR 12 SPOILER FROZEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FROZEN PULLEY WAS FOUND ON NR 12 SPOILER. THE FROZEN PULLEY P/N BACP30K-2D WAS REMOVED AND REPLACED PER B727 MM 27-61-00 AND OPERATIONAL CHECK FOUND NORMAL. (M) 2 L 7 3 4F A3WE 1999052800510 19990528 00510 EU 1999 5 28 SIMA991232 1 19990503 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 425MJ 425 SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 CORRODED. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999052800511 19990528 00511 EU 1999 5 28 SIMA991233 1 19990503 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 425MJ 425 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT INBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EO E9-5 300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999052800512 19990528 00512 EA 1999 5 28 MASA99069 1 19990508 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 FLT 5776 - LIT-CLT - CREW REPORTED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE ACTION WAS D EFERRED PER MEL 33-51-2. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REP LACED. (M) 2 L 7 2 4F RT A21EA 1999052800513 19990528 00513 EA 1999 5 28 MASA99068 1 19990507 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA ROW 5 FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 FLT 5805 - PHL-MKE - CREW REPORTED THAT THE CEILING EMERGENCY FLOOD LIGHT AT ROW 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999052800514 19990528 00514 WP 1999 5 28 HALA9900110 1 19990505 A 2131 CON5037 CONTROLLER DOUG DC10 DC1030 3023501 WP CABIN FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 141AA 46713 LAX - AIRCRAFT FAILED TO PRESSURIZE DURNG CLIMB-OUT. GOT ALT WARNING HORN AT 10,000 FT. SHORTLY AFTER ATTENDANTS ADVIS ED SOME CABIN MASKS HAD DEPLOYED. ATTEMPTED, BUT WAS UNABLE TO REGAIN CONTROL OF SYSTEM IN SEMI-AUTO AND STANDBY MODES. REMOVED AND REPLACED AUTO CABIN PRESSURE CONTROLLER, STANDBY CABIN PRESSURE CONTROLLER AND TWO EACH OUTFLOW VALVE ACTU ATORS. BITE CHECK NORMAL. GROUND OPERATION CHECK GOOD. (M) 2 L 7 3 4F A22WE 1999052800515 19990528 00515 NM 1999 5 28 GAIA9955 1 19990505 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 DURING ROUTINE SCHEDULED MAINTENANCE, THE FLOORBEAM AT STATION 1130, RBL 45 TO 60 WAS FOUND TO HAVE CORROSION AND OUT OF SRM REPAIR TOLERANCE. REPAIRED DAMAGED FLOORBEAM IAW AMERICAN INTERNATIONAL ENGINEERING INSTRUCTIONS. REF AIA/E/2948, DATED 4/5/99. THIS REPAIR WAS SUBMITTED TO, ACCEPTED AND APPROVED BY THE CHICAGO AIRCRAFT CERTIFICATION OFFICE. THIS AIRCRAFT WAS REPAIRED IAW WITH THE ABOVE APPROVED INSTRUCTIONS AND RETURNED TO SERVICE WITH NO ADDITIONAL DISCREPANCIES NOTED. (M) 2 L 7 3 4F A3WE 1999052800516 19990528 00516 NM 1999 5 28 GAIA99057 1 19990511 A 3350 LIGHT BOEING 727 727223 1384074 NM EMERGENCY EXIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6807 19482 DURING A ROUTINE 'A' CHECK BEING PERFORMED AT OSC, MAINTENANCE FOUND THE EMERGENCY EXIT UNARMED LIGHT INOPERATIVE. THE EMERGENCY EXIT TLIGHT UNARMED LIGHT WAS RELAMPED AND OPERATIONALLY CHECKED GOOD IAW B727 MM 33-50-1. THE AIRCRAFT WAR R ETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999052800517 19990528 00517 NM 1999 5 28 GAIA9956 1 19990507 A 3350 1000679 BATTERY BOEING 727 7272J0 138407E NM COCKPIT DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 281KH 21105 DURING ROUTINE MAINTENANCE WALK AROUND IN TOL, FOUND COCKPIT 'EMERGENCY EXIT' LIGHT BATTERY DEAD. REMOVED AND REPLACED COCKPIT 'EMERGENCY EXIT' LIGHT. OPERATIONAL CHECK GOOD. NO ADDITIONAL PROBLEMS WERE NOTED. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 3 4F RT A3WE 1999052800518 19990528 00518 NM 1999 5 28 99ZZZM316 1 19990504 A 2910 6517844239 LINE BOEING 727 727225 1384077 NM 'A' HYD MODULE LEAKING A MYWA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 19 887MA 21857 AT CRUISE ALTITUDE FROM MYR TO BFD HAD 'A' SYSTEM DECREASED TO '0' SYSTEM LIGHTS CAME 'ON'. CONDUCTED EMERGENCY PROCEDU RES. LOWERED GEAR BY MANUAL PROCEDURES. DIVERTED TO BOS. LANDED WITHOUT INCIDENT. FOUND HYD LINE TO 'A' SYSTEM MODUL E LEAKING. REPLACED LINE WITH FLEX LINE PER 20-10-5, PAGE 855 ITEM 10. REPLACED NR 1 AND NR 2 ENGINE 'A' SYSTEM FILTER S. RAN ALL SYSTEMS, NO LEAKS. SERVICED HYD OK FOR SERVICE. HYD LINE REPLACED AT BOS IS TEMP REPAIR, TRANSFERRED TO DM I NR 7002. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999052800519 19990528 00519 NM 1999 5 28 99ZZZM317 1 19990505 A 3230 CRANK BOEING 727 727225 1384077 NM LANDING GEAR OUT OF POSITION A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 887MA 21857 AFTER TAKEOFF FROM BOS, NOSE GEAR WOULD NOT RETRACT. VISUAL INSPECTION OK. CYCLED GEAR NO HELP. RETURNED TO BOS, LAND ED WITHOUT INCIDENT. FOUND MANUAL EXTENSION CRANK WAS NOT SET TO NEUTRAL POSITION, PREVENTING NOSE GEAR FROM GOING UP D URING NORMAL RETRACTION. PLACED CRANK IN NEUTRAL POSITION IAW 32-34-00 PAGE 11. PERFORMED NORMAL EXTENSION/RETRACTION TEST IW 32-30-00 PAGE 501-503. VISUALLY INSPECTED NLG MANUAL EXTENSION SYSTEM IAW 32-34-11, 32-34-51 AND 32-34-71. NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 1999052800520 19990528 00520 NM 1999 5 28 ASAA9910092 1 19990429 A 3230 BACB10A554 BEARING BOEING 737 737290C 138448V NM NLG FROZEN A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 740AS 22578 ANC - AIR TURN BACK OF FLT 55, CREW REPORTED NOSE LANDING GEAR WARNING LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN TH E UP POSITION. WHEN GEAR HANDLE WAS MOVED TO THE OFF POSITION, THE NOSE GEAR EXTENDED. FOUND EMERGENCY EXTENSION CAM S TUCK IN THE EXTENDED MODE. REPLACED FROZEN BEARING IN MANUAL EXTENSION RELEASE MECHANISM. SYSTEM OPERATED NORMALLY ON MANUAL EXTENSION TEST. (M) 2 L 7 2 4F A16WE 1999052800521 19990528 00521 NM 1999 5 28 ASAA9940104 1 19990506 A 5330 SKIN BOEING 737 737490 1384715 NM BS 1050 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 797AS 28892 OAK - DURING SC WALKAROUND, FOUND LARGE DENT AT STATION 1050, AFT OF L2 DOOR APPROXIMATELY 24 INCHES ABOVE WL. INSTALLE D DOUBLER REPAIR PER SRM 53-00-01 AND 53-00-03. (M) 2 L 7 2 4F RT A16WE 1999052800522 19990528 00522 EU 1999 5 28 AALA990541 1 19990417 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU 4L DOOR CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTING SYSTEM PRESS TO TEST INOPERATIVE. REPAIRED EMERGENCY LIGHTING SY STEM PRESS TO TEST WIRING AT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999052800523 19990528 00523 EU 1999 5 28 AALA990533 1 19990418 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 19 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70074 517 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19G INOPERATIVE. RESEATED CONNECTOR EMERGENCY EXIT LIG HT CONNECTOR AT SEAT 19G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999052800524 19990528 00524 EU 1999 5 28 AALA990532 1 19990418 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROW 28 DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70074 517 JFK - DURING MAINTENANCE CHECK, EMERGENCY EXIT PATH LIGHT STRIP AT SEAT ROW 28C INOPERATIVE. REPLACED EMERGENCY EXIT PA TH LGHT STRIP AT SEAT ROW 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999052800525 19990528 00525 EU 1999 5 28 AALA990519 1 19990411 A 2842 0210KTU01 PROBE FOKKER F28 F28MK0100 4990807 EU RT MAIN TANK DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 1439A TU51917 11434 BNA - FLT 1451 - DURING CRUISE, WITHIN 5 MINUTES OF NORMAL FUEL CHECK A FUEL ASYMMETRY BETWEEN RIGHT AND LEFT MAIN TANKS WAS NOTED. CREW DECLARED AN EMERGENCY AND DIVERTED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. BNA MAINTENANCE DEFERR ED RIGHT MAIN FUEL TANK QTY AND TOTALIZER PER MEL PROCEDURES. AIRCRAFT OVERNIGHTED DFW AND THE FUEL SYSTEM WAS TROUBLES HOT. MAINTENANCE FOUND RIGHT MAIN TANK FUEL PROBE TO BE THE FAULT CAUSE. REPLACED RIGHT MAIN TANK FUEL PROBES. SYSTEM OPERATED NORMAL WITH NO LEAKS. PLACARD REMOVED FROM SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999052800526 19990528 00526 WP 1999 5 28 AALA990546 1 19990420 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 246AA 49238 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHT SRIP AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800527 19990528 00527 WP 1999 5 28 AALA990538 1 19990416 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 482AA 49675 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPAI RED EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800528 19990528 00528 WP 1999 5 28 AALA990539 1 19990416 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN NEEDED REPAIRING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 435AA 49453 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT SECTION OF COACH CABIN INOPERATIVE. R EPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEXT TO RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800529 19990528 00529 WP 1999 5 28 AALA990504 1 19990411 A 3350 SWITCH DOUG DC9 DC982 3022082 WP CABIN OUT OF SEQUENCE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 516AM 49893 DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERWING EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE FOUND SWITCHES T O BE OUT OF SEQUENCE. MAINTENANCE RESEQUENCED SWITCHES AND LIGHTS WENT OUT. SYSTEM GROUND CHECKED NORMAL OPERATIONS. ( M) 2 L 7 2 4F A6WE 1999052800530 19990528 00530 WP 1999 5 28 AALA990530 1 19990418 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 552AA 53034 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800531 19990528 00531 WP 1999 5 28 AALA990534 1 19990417 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 223AA 49173 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE IN FORWARD CABIN. REPAIRED EMERGENCY E XIT FLOOR PATH LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800532 19990528 00532 WP 1999 5 28 AALA990535 1 19990417 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 244AA 49256 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT COACH CABIN INOPERATIVE. MAINTENANCE FOUND A BROKEN CO NNECTOR. REPLACED CONNECTOR TO EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800533 19990528 00533 WP 1999 5 28 AALA990612 1 19990421 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN MISWIRED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 7532A 49924 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT RIGHT AFT OVERWING EXIT INOPERATIVE. REVERSED POLARITY OF EMERGEN CY EXIT FLOOR TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800534 19990528 00534 NM 1999 5 28 AALA990432 1 19990329 A 3340 233T321741 PANEL BOEING 757 757223 1384957 NM COCKPIT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 646AA D00695 24604 MIA - FLT 787 - DURING CLIMB-OUT, ELECTRICAL SMELL WITH SMOKE WAS DETECTED IN THE COCKPIT. CREW ACCOMPLISHED ELECTRICAL SMOKE PROCEDURES AND LANDED MIA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT WING LANDNIG LIGHT SWITCH BURNED. R EPLACED RIGHT WING LANDING LIGHT SWITCH CONTROL PANEL SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999052800535 19990528 00535 NM 1999 5 28 AALA990542 1 19990417 A 2120 AIR DIST BOEING 767 767223 1385123 NM CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 301AA 22307 ORD - FLT 0003 - EN ROUTE JFK-LAX, A SMOKE SMELL IN CABIN THAT POSSIBLE SMELLED LIKE ELECTRICAL. AIRCRAFT AIR INTERRUPT ED AND LANDED ORD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND GROUND RAN ENGINES WITH PACKS BEING CYCL ED. UNABLE TO DUPLICATE SMELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999052800536 19990528 00536 NM 1999 5 28 AALA990527 1 19990415 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 12-14 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 613AA 24489 JFK - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 12D THROUGH 14D WERE INOPERATIVE. REPLACED EMER GENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROWS 12D THROUGH 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999052800537 19990528 00537 NM 1999 5 28 AALA990627 1 19990427 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 685AA 25342 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT IN FORWARD CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT PAT H LIGHT JUMPER WIRE IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999052800538 19990528 00538 NM 1999 5 28 AALA990626 1 19990427 A 3397 WIRE BOEING 767 767223 1385123 NM ROW 26H BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 319AA 22320 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT PASSENGER SEAT ROW 26H INOPERATIVE. REPAIRED BROKEN WIRE A T EMERGENCY EXIT LIGHT CONNECTOR PASSENGER SEAT ROWS 26H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999052800539 19990528 00539 NM 1999 5 28 AALA990641 1 19990429 A 3350 44MY232796 SWITCH BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388AA 27448 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT IN CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONTROL SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999052800540 19990528 00540 NM 1999 5 28 AALA990640 1 19990429 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 38B DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386AA 27060 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT ROW 38B INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT SEAT ROW 38B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999052800541 19990528 00541 NM 1999 5 28 AALA990505 1 19990413 A 3350 S283N00219 LIGHT BOEING 757 757223 1384957 NM LT EMER EXIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 692AA 26972 SFO - DURING OVERNIGHT MAINTENANCE, AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLA CED AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A2NM 1999052800542 19990528 00542 NM 1999 5 28 AALA990540 1 19990416 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 34H LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387AM 27184 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 34H INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR. RESECURED LOOSE CONNECTOR TO EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A1NM 1999052800543 19990528 00543 NM 1999 5 28 AALA990536 1 19990415 A 3350 0201922001 SOCKET BOEING 767 767323 1385205 NM ROW 11AB DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351AA 24032 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 11AB INOPERATIVE. REPLACED EMERGENCY EXIT PATH LI GHT SOCKET AT SEAT 11AB. SYSTEM CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999052800544 19990528 00544 NM 1999 5 28 AALA990531 1 19990418 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 691AA 25697 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT NOPERATIVE IN FORWARD CABIN. REPLACED EMERGENCY EXIT FLOOR PA TH CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999052800545 19990528 00545 EU 1999 5 28 AALA990645 1 19990430 A 2930 O-RING FOKKER F28 F28MK0100 4990807 EU NR 1 HYD PUMP LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 1461C 11481 DFW - FLT 544 - DURING FINAL APPROACH, THE NR 1 HYDRAULIC SYSTEM LOW LIGHT ILLUMINATED ON THE MULTIFUNCTION DISPLAY UNIT (MFDU). CREW ACCOMPLISHED CHECKLIST FOR HYDRAULIC SYSTEM LOW QUANTITY AND ALTERNATE FLAP EXTENSION AND GEAR EXTENSION WAS USED. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 1 ENGINE HYDRAULIC PUMP PRESSURE LINE FIT TING LEAKING. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE FITTING O-RING AND SERVICED HYDRAULIC SYSTEM. S YSTEM WAS CHECKED UNDER PRESSURE WITH NO FURTHER LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999052800546 19990528 00546 EU 1999 5 28 AALA990648 1 19990503 A 2120 AIR DIST FOKKER F28 F28MK0100 4990807 EU CABIN SMOKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1440A 11435 DFW - AFTER TAKEOFF DFW, CABIN FILLED WITH SMOKE FROM AIR CONDITIONING DUCTS. FLIGHT AIR INTERRUPTED, RETURNED DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED OPERATIONS CHECK OF AIR CONDITIONING SYSTEM UNABLE TO DUPLICATE SMOKE. PERFORMED OVERWEIGHT INSPECTION WITH NO FINDINGS. OPERATED PACKS WITH ENGINES AND APU, NO OIL LEA KS OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999052800547 19990528 00547 NM 1999 5 28 AALA990481 1 19990408 A 2497 WIRE BOEING 767 767323 1385205 NM ROW 2-4 SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 372AA 25199 MIA - FLT 995 - AFTER TAKEOFF, SEAT WIRING HARNESS AT ROW 2AB SHORTED OUT CAUSING AN ARC AND SMOKE IN FIRST CLASS CABIN. FLIGHT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SEVERAL WIRES SHORT ED TO GROUND ADJACENT TO PASSENGER SEAT 3A FOOT REST. MAINTENANCE INSTALLED A GROUND GROMMET AND REPAIRED SHORTED WIRIN G TO POWER FOOT RESTS AT SEAT ROWS 2AB THROUGH 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999052800548 19990528 00548 WP 1999 5 28 AALA990642 1 19990429 A 2810 MS29513244 PACKING DOUG DC10 DC1030 3023501 WP LT WING LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 144AA 47848 HNL - FLT 72 - AFTER TAKEOFF HNL, A FLUID LEAK WAS REPROTED COMING FROM THE LEFT WING. FLIGHT AIR INTERRUPTED AND RETUR NED HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND FUEL LEAKING FROM UPPER WING 5TH PANEL FRO M WING TIP. REPLACED JUNCTION PROBE PANEL O-RING AND PANEL SEAL. AIRCRAFT WAS REINSPECTED WITH NO LEAKS DETECTED. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999052800549 19990528 00549 WP 1999 5 28 AALA990615 1 19990422 A 4990 2651 GASKET DOUG DC9 DC983 3022083 WP APU DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 589AA 53252 DFW - FLT 334 - AFTER TAKEOFF DFW, A RUBBER ODOR AND A LIGHT SMOKEY HAZE WAS NOTED BY FLIGHT CREW. FLIGHT AIR INTERRUPT ED AND RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU OIL CAP SEAL DAMAGED. REPLACED APU OIL CAP SEAL AND LEAK CHECKED OK. MAINTENANCE PERFORMED PACK BURNOUT. AFTER BURNOUT WAS ACCOMPLISHED, COALESCER BAGS W ERE REPLACED AS A PRECAUTIONARY. PACKS WERE OPERATED WITH NO LEAKS, ODOR, OR SMOKE NOTED. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999052800550 19990528 00550 WP 1999 5 28 AALA990618 1 19990424 A 4990 38761864 SWITCH DOUG DC9 DC982 3022082 WP APU DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 402A 49313 LAX - FLT 1482 - AFTER TAKEOFF LAX, CABIN FILLED WITH SMOKE. FLIGHT AIR INTERRUPTED AND RETURNED LAX AND LANDED OVERWEI GHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU OIL PRESSURE SWITCH LEAKING. REPLACED APU OIL PRESSURE SWITCH. PERFORMED OVERWEIGHT INSPECTION WITH NO FINDINGS. OPERATED APU WITH NO IL LEAKS OR SMOKE NOTED. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800551 19990528 00551 NE 1999 5 28 AALA990503 2 19990412 A 7230 808904 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 2 ENGINE BROKEN A AALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 07 412AA 49323 717808 SYR - FLT 303 - DURING CRUISE AT 31,000 FEET, FLIGHT CREW HEARD A LOUD NOISE LIKE A COMPRESSOR STALL. CAPTAIN NOTICED N R 1 ENGINE N2 DROPPED TO IDLE POWER. FLIGHT CREW DECLARED AN EMERGENCY, SECURED NR 1 ENGINE AND DIVERTED TO SYR. AIRCR AFT LANDED SYR WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE TURBINE FAILED. REPLACED NR 1 ENGINE, PERFO RMEDENGINE RUN UP. SYSTEM GROUND CHECKED NORMAL OPERATION.A 4TH STAGE TURBINE BLADE FAILED JUST ABOVE THE ROOT PLATFOR M DUE TO HIGH CYCLE FATIGUE. THE LIBERATION OF THE BLADE CAUSED EXTENSIVE DAMAGE TO THE 3RD AND 4TH STAGE AND SUBSEQUE NTLY CA USED COMPRESSOR STALL. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999052800552 19990528 00552 WP 1999 5 28 AALA990630 1 19990427 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 410AA 49321 DFW - FLT 1418 - DURING CRUISE, NOSE GEAR RED UNSAFE LIGHT ILLUMINATED WITH NO OTHER ABNORMALITIES NOTE. FLIGHT CONTINU ED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR LOCK SENSOR FAULTY. REPLACED NOSE L ANDING GEAR LOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800553 19990528 00553 WP 1999 5 28 AALA990638 1 19990429 A 2841 372001001 INDICATOR DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 242AA 568 49255 LAX - FLT 896 - EN ROUTE SJC-DFW - CENTER TANK BOOST PUMP CIRCUIT BREAKERS POPPED WHEN TURNED ON. AIRCRAFT AIR INTERRUP TED AND LANDED LAX WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND FUEL QTY INDICATION SYSTEM AT FAU LT. MAINTENANCE REPLACED COCKPIT FUEL QTY INDICATOR. AS A PRECAUTIONARY, BOTH CENTER BOOST PUMPS WERE REPLACED. REQUI RED FUEL QTY AND TRANSFER CHECKS WERE ACCOMPLISHED WITH NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800554 19990528 00554 WP 1999 5 28 AALA990637 1 19990425 A 2130 WARNING LIGHT DOUG DC9 DC982 3022082 WP CABIN ILLUMINATED A AALA G O2 MASK DEPLOYED N FALSE WARNING DE DESCENT 1 SW 07 73444 49470 DFW - FLT 499 - DURING DESCENT AT FL330, CABIN ALTITUDE LIGHT ILLUMINATED. CREW EXPEDITED DESCENT AND AT FL12 ALL OXYGE N MASKS DEPLOYED. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED RATE CHECK AND GROUND PRESSUR IZED AIRCRAFT IN AUTOMATIC/MANUAL MODE WITH NO ABNORMAL CONDITIONS NOTED. ALL REQUIRED CHECKS WERE PERFORMED WITH NORMA L OPERATION. UNABLE TO DUPLICATE FAULT. REPLACED OXYGEN GENERATORS AND REPACKED MASKS. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F A6WE 1999052800555 19990528 00555 WP 1999 5 28 AALA990647 1 19990502 A 3231 39567851 SNUBBER DOUG DC9 DC982 3022082 WP NLG DOOR DEFECTIVE A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 513AA EFS16358 49890 DFW - FLT 1850 - AFTER TAKEOFF DFW, UPON GEAR RETRACTION A LOUD NOISE AND VIBRATION WAS FELT FROM NOSE GEAR. AIRCRAFT A IR INTERRUPTED AND RETURNED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT NOSE GEAR DOOR SNUBBER FAILED TO LOCK DOOR IN PLACE. MAINTENANCE INSTALLED NEW DOOR SNUBBER. ACCOMPLISHED REQUIRED CHECKS AND SWUNG NOSE GEAR WITH NO FAULT S NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800556 19990528 00556 WP 1999 5 28 AALA990651 1 19990503 A 2120 AIR DIST DOUG DC9 DC982 3022082 WP CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 462AA 49592 MEX - FLT 884 - AFTER TAKEOFF, ELECTRICAL SMELL AND SMOKE WAS NOTED IN CABIN BY FLIGHT CREW. AIRCRAFT AIR INTERRUPTED, RETURNED MEX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED OPERATIONS CHECK OF ELECTRICAL EQUIPMENT. U NABLE TO DUPLCIATE ELECTRICAL SMOKE SMELL. AS A PRECAUTIONARY, CHANGED COALESCER BAGS. OPERATED PACKS WITH ENGINES AND APU WITH NO SMOKE OR ELECTRICAL SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800557 19990528 00557 WP 1999 5 28 AALA990622 1 19990426 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 564AA 49346 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EM ERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999052800558 19990528 00558 WP 1999 5 28 AALA990670 1 19990505 A 3350 LIGHT DOUG DC9 DC982 3022082 WP EMER EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 283AA 49296 DFW - DURING MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED EMERGENCY PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800559 19990528 00559 WP 1999 5 28 AALA990674 1 19990507 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 458AA 49563 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EM ERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999052800560 19990528 00560 WP 1999 5 28 AALA990649 1 19990501 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 1242 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 236AA 49251 TUL - FOUND CORROSION ON LOWER DOOR JAMB BEAM OUTBOARD SIDE AT STATION 1242 BELOW RIGHT TIE DOWN TRACK. TREATED AND PRI MED BLENDED AREA. INSTALLED DOUBLER PER ESO 80559, DATED 4-29-99. (M) 2 L 7 2 4F A6WE 1999052800561 19990528 00561 WP 1999 5 28 AALA990650 1 19990430 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1307 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 236AA 49251 TUL - FOUND CORROSION ON SEAT TRACK NR 3. REPLACED SECTION OF SEAT TRACK FROM STATION 1222-1309 PER SRM 53-05 FIG 4F. ( M) 2 L 7 2 4F A6WE 1999052800562 19990528 00562 WP 1999 5 28 AALA990520 1 19990520 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1278 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND FUSELAGE SKIN CORRODED AT FUSE STATION 127B. INSTALLED DOUBLER PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1999052800563 19990528 00563 WP 1999 5 28 AALA990521 1 19990521 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1216 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND FUSELAGE SKIN CORRODED AT BS 1216. INSTALLED DOUBLER PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1999052800564 19990528 00564 WP 1999 5 28 AALA990522 1 19990414 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1721-1741 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION ON DOUBLER UNDER ANTENNA ATTACH POINTS, AND 16 INCH LONG CRACK IN BELLY SKIN DISCOVERED DURING DOU BLER REMOVAL AREA BETWEEN LONGERON 51L AND 51R STATION 1721-1741. REPAIRED SKIN AND DOUBLER REF SRM 53-20-00 AND ESO 73 49, DATED 4-13-99. (M) 2 L 7 3 4F A22WE 1999052800565 19990528 00565 WP 1999 5 28 AALA990523 1 19990408 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1781 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION UNDER FRAME, INBOARD OF RIGHT LOADING TRAY. BLENDED CORROSION IAW SRM 51-21-01 VOL II. REPAIRED FRAME AT STATION 1781 IAW DC1010 SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1999052800566 19990528 00566 WP 1999 5 28 AALA990524 1 19990414 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1738-1750 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION ON BOTTOM SIDE OF LONGERON 50R. REPAIRED LONGERON PER ONE TIME ESO 7349 DATED 4/13/99. (M) 2 L 7 3 4F A22WE 1999052800567 19990528 00567 WP 1999 5 28 AALA990525 1 19990414 A 5730 SKIN DOUG DC10 DC1010 3022110 WP WING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - LEADING EDGE DAMAGED INBOARD SIDE OF NR 1 SLAT TRACK ICE DOOR. REMOVED DAMAGE AND NECESSARY FASTENERS, INSTALLED AND SECURED DOUBLER WET IAW SRM 57-10-00 PAGE 216. (M) 2 L 7 3 4F A22WE 1999052800568 19990528 00568 WP 1999 5 28 AALA990543 1 19990416 A 5320 BRACKET DOUG DC10 DC1010 3022110 WP BS 1787 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND BRACKET INSIDE LONGERON AT 45R STATION 1787 CORRODED. REPAIRED AND INSTALLED DOUBLER PER ESO 7349, DATED 4/ 16/99. (M) 2 L 7 3 4F A22WE 1999052800569 19990528 00569 NM 1999 5 28 P2EA99183 1 19990502 A 8012 16386 SWITCH BOEING 737 737205 NM NR 1 ENGINE FAILED A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 412CE 084558 20412 ATL - FLT 301 - NR 1 ENGINE START LIGHT ILLUMINATED ON TAKEOFF. REJECTED TAKEOFF. LIGHT WENT OUT WHEN ENGINES CAME TO IDLE. REPLACED NR 1 ENGINE START VALVE AND START VALVE PRESSURE SWITCH. START VALVE LIGHT OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1999052800570 19990528 00570 NM 1999 5 28 P2EA99182 1 19990329 A 5330 SKIN BOEING 737 737222 1384473 NM BS 908-1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE EXTERIOR FUSELAGE FROM BS 947 TO BS 967 AND BETWEEN STRINGER 20 RIGHT AND STRINGER 19 RIGHT WA S FOUND WITH BULGED SKIN. REPLACED AND FABRICATED FUSELAGE SKIN PANEL FROM BS 908 TO BS 1016, BETWEEN STRINGER 14 RIGHT AND STRINGER 20 RIGHT PER COOPESA EO COO-3-53-240-99, DATED APR 29, 1999 AND BOEING FAX COO-SJO-0555RR, DATED APR 29, 1 999. (M) 2 L 7 2 4F A16WE 1999052800571 19990528 00571 NM 1999 5 28 P2EA99181 1 19990327 A 5330 SKIN BOEING 737 737222 1384473 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, CRACKS WERE FOUND ON THE FUSELAGE OUTER SKIN AT BS 219.8, WL 218 AND AT BS 211.8, WL 228 RIGHT SID E. REPAIRED FUSELAGE SKIN SECTIONS FROM BS 216.8 TO BS 223, BETWEEN WL212 AND WL 224 RIGHT SIDE, AND FROM BS 207L8 TO B S 215.8 BETWEEN WL 215 AND WL 228 RIGHT SIDE DUE TO CRACKS PER COOPESA EO COO-3-53-209-00, DATED APR 15, 1999 AND BOEING FAXES NUMBER COO-SJO-99-0437RR DATED APR 2, 199 AND COO-SJO-99-0496RR, DATED APR 14, 1999. (M) 2 L 7 2 4F A16WE 1999052800576 19990528 00576 SW 1999 5 28 99ZZZM318 1 19990430 A 7712 2719158007 TORQUE INDICATOR SWRNGN SA227 SA227AC 8780603 SW RT ENGINE INOPERATIVE A MEJA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 17 3114G 215 AC583 DURING TAKEOFF ROLL AT LCH, THERE WAS NO RIGHT TORQUE INDICATION AND THE TAKEOFF WAS ABORTED. MAINTENANCE REMOVED AND R EPLACED THE RIGHT TORQUE INDICATOR AND COMPLIED WITH AN OPERATIONS CHECK. THE CHECK WAS SATISFACTORY AND THE AIRCRAFT W AS RETURNED TO SERVICE (M) 2 L 7 2 4T RT A8SW 1999052800577 19990528 00577 EA 1999 5 28 MASA99064 1 19990503 A 3350 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA LT WING FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 FLT 5782 - PHL-CRW - CREW REPORTED A LEFT WING EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BULB, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999052800578 19990528 00578 EU 1999 5 28 RAIA990447 1 19990426 A 2130 2648A000 SAFETY VALVE BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 426AM 12513 874 FLT 7312 - STL - AIRCRAFT IS PRESSURIZING ON THE GROUND. MAINTENANCE REPLACED SAFETY VALVE. (M) 2 L 7 2 4T RT A56EU 1999052800579 19990528 00579 SO 1999 5 28 RAIA990501 1 19990503 A 2460 KN4D RELAY EMB 145 EMB145 SO COCKPIT FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 801HK 2368 145053 FLT 5790 - ORD- ELECTRICAL ODOR IN COCKPIT JUST PRIOR TO TAKEOFF. MAINTENANCE REPLACED NR 1 POWER AUXILLARY RELAY (SUSP ECTED FOR OVERHEATING CAUSING ODOR). (M) 2 L 7 2 4F RT T00011AT 1999052800580 19990528 00580 EU 1999 5 28 RAIA990448 1 19990427 A 3610 S2L226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LT PACK FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 558HK 41071 FLT 7282 - STL - DUCT FAIL LIGHT ILLUMINATED FOR LEFT PACK. MAINTENANCE REPLACED SEAL IN BLEED LINE UNDER LEFT INBOARD LEADING EDGE. (M) 2 L 7 2 4T RT A41NM 1999052800581 19990528 00581 1999 5 28 RAIA990502 4 19990503 A 3418 M30204A RELAY BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 864AE 864 FLT 4717 - SMF - DURING STALL TEST, NO STICK PUSHER OR STALL IDENT LIGHTS ILLUMINATE. MAINTENANCE REPLACED LEFT STICK P USHER ISOLATION RELAY. (M) 2 L 7 2 4T RT A56EU 1999052800582 19990528 00582 EU 1999 5 28 RAIA990446 1 19990430 A 7810 141780015 BRACKET JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 551HK 41040 FLT 7518 - STL - RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED. MAINTENANCE REPLACED JET PIPE ATTACH POINT BRACKET ON RIGHT E NGINE. (M) 2 L 7 2 4T RT A41NM 1999052800583 19990528 00583 SO 1999 5 28 RAIA990439 1 19990425 A 2611 FDS765A2A SMOKE DETECTOR EMB 145 EMB145 SO LAVATORY ILLUMINATED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 803HK 145077 FLT 5786 - ORD - LAV SMOKE LIGHT ILLUMINATED, THEN SMOKE APPEARED IN COCKPIT AND CABIN. MAINTENANCE REPLACED LAV SMOKE DETECTOR AND PERFORMED ENGINE RUNS. (M) 2 L 7 2 4F RT T00011AT 1999052800584 19990528 00584 1999 5 28 RAIA990505 4 19990504 A 3422 7000622901 DIRECTIONAL GYRO BAG JETSTM JETSTM3201 1500217 EU NR 1 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 435AM 11878 889 FLT 7286 - STL - NR 1 ATTITUDE INDICATOR FLAGGED. MAINTENANCE REPLACED NR 1 DIRECTIONAL GYRO. (M) 2 L 7 2 4T RT A56EU 1999052800585 19990528 00585 1999 5 28 RAIA990504 4 19990504 A 3425 MS210423 NUT BAG JETSTM JETSTM3201 1500217 EU RT WING MISINSTALLED A RAIA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 CE 03 435AM 889 FLT 7061 - STL - 30 DEGREE SPLIT BETWEEN HSI'S. MAINTENANCE REPLACED MAGNETIC NUT ON RIGHT WING TIP. (M) 2 L 7 2 4T RT A56EU 1999052800586 19990528 00586 EU 1999 5 28 RAIA990506 1 19990505 A 2120 BAEREFJ10049 DUCT BAG JETSTM JETSTM3201 1500217 EU LT PACK FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 425AM 870 FLT 7498 - STL - LEFT FLOW INOPERATIVE, RIGHT SIDE ALREADY DEFERRED. MAINTENANCE REPLACED DUCT ASSEMBLY TO LEFT PACK. ( M) 2 L 7 2 4T RT A56EU 1999052800587 19990528 00587 EU 1999 5 28 RAIA990507 1 19990505 A 7922 L8523427 VERNATHERM BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA E ENGINE SHUTDOWN M OVER TEMP TX TAXI/GRND HDL 1 CE 03 422AM 15325 856 FLT 7422 - STL - RIGHT ENGINE OIL TEMP WENT TO 130 DEGREES, SHUT RIGHT ENGINE DOWN. MAINTENANCE REPLACED OIL COOLER VER NATHERM. (M) 2 L 7 2 4T RT A56EU 1999052800588 19990528 00588 EU 1999 5 28 RAIA990508 1 19990509 A 2434 23095002 GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 559HK 4423 41075 FLT 7494 - STL - NR 2 GENERATOR INOPERATIVE. MAINTENANCE REPLACED NR 2 GENERATOR. (M) 2 L 7 2 4T RT A41NM 1999052800589 19990528 00589 NM 1999 5 28 GAIA9954 1 19990429 A 3260 SWITCH BOEING 727 727223 1384074 NM NLG DOOR OUT OF ADJUST A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 855AA 20996 DURING APPROACH INTO MDT FROM TOL, THE LANDING GEAR HAD TO BE RECYCLED IN ORDER TO PUT THE NOSE GEAR DOOR LIGHT OUT. TH E AIRCRAFT LANDED WITHOUT ANY FURTHER PROBLEMS. CHECKED NOSE WHEEL WELL AND FOUND THE O2 SWITCH JAM NUT LOOSE. TIGHTEN ED THE SAME PER BOEING MAINTENANCE MANUAL AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999052800590 19990528 00590 WP 1999 5 28 HALA9900108 1 19990503 A 3350 SPLICE DOUG DC10 DC1010 3022110 WP SEAT 1B FAILED A HALA K NONE L NO TEST CR CRUISE 1 WP 13 119AA 46519 IN FLIGHT, DOOR 1L, 2L, 3L, EMERGENCY LIGHTS DIMLY AND INTERMITTENTLY ILLUMINATED. OCCASSIONALLY BRIGHT. SEAT LIGHT ON LEFT AND RIGHT SIDE OF LEFT AISLE IN 'A' AND 'B' CABINS ALSO. REPAIRED EMERGENCY LIGHT WIRE AT SEAT 1B. OPERATIONAL C HECK OK. (M) 2 L 7 3 4F A22WE 1999052800591 19990528 00591 WP 1999 5 28 HALA9900109 1 19990504 A 3241 424431 CONTROL BOX DOUG DC9 DC951 3022051 WP ANTI-SKID SYSTEM MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 660HA 48122 HNL - FLT 388 - ANTI-SKID WOULD NOT ARM PRIOR TO TAKEOFF. CONDITION CLEARED AFTER ENGINE SHUTDOWN. REPLACED ANTI-SKID CONTROL BOX. BITE TEST OK. (M) 2 L 7 2 4F RT A6WE 1999052800592 19990528 00592 WP 1999 5 28 HALA9900102 1 19990413 A 5754 DOUBLER DOUG DC9 DC951 3022051 WP NR 1 LE SLAT GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 673MC 47726 RIGHT WING LEADING EDGE AT MOST INBOARD EXISTING REPAIR DOUBLER, HAS DEEP. GOUGES INBOARD OR NR 1 SLAT TELESCOPIC DUCT. REMOVED DOUBLER, FABRICATED NEW DOUBLER PER SRM 57-06A FIG 3, TREAT, PRIMED PER SRM. (M) 2 L 7 2 4F RT A6WE 1999052800593 19990528 00593 WP 1999 5 28 HALA9900101 1 19990406 A 5713 STRINGER DOUG DC9 DC951 3022051 WP WS 280-300 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 673MC 47726 FOUND CORROSION ON STRINGER UNDER SPOILER XRS 280-300. FABRICATED ANGLE, LOWER INTERCOSTAL SUPPORT ANGLE, SPLICE ANGLE 2 EACH SHIMS, PER SRM 57-01 FIG 3. TREATED AND PRIMED PER SRM 51-10-3 AND INSTALLED PER 51-30-2. (M) 2 L 7 2 4F RT A6WE 1999052800594 19990528 00594 WP 1999 5 28 HALA9900100 1 19990403 A 5320 SPLICE DOUG DC9 DC951 3022051 WP BS 1079 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 673MC 47726 AFT CARGO DOOR JAMB PAN SPLICE ANGLE AT STATION 1079 HAS LEVEL 2 CORROSION. FABRICATED AND LOCATED 2 DOUBLERS AND INSTA LLED IAW SRM 51-30-1, 51-10-3, 53-05. (M) 2 L 7 2 4F RT A6WE 1999052800595 19990528 00595 WP 1999 5 28 HALA9900099 1 19990414 A 5320 INTERCOSTAL DOUG DC9 DC951 3022051 WP BS 1293 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 673MC 47726 AFT ACCESSORY COMPARTMENT FUSELAGE STATION 1293, STRINGER 12R INTERCOSTAL HAS ABOUT .5625 INCH LONG CRACK AND LIGHT SURF ACE CORROSION LEVEL 1. REMOVED AND REPLACED FABRICATED INTERCOSTAL IAW SRM 51-10-3, SRM 51-10-2, SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 1999052800596 19990528 00596 1999 5 28 HALA9900106 4 19990502 A 3416 ALTIMETER DOUG DC9 DC951 3022051 WP RT COCKPIT MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 672MC 47661 HNL - DURING CLIMB, EXPERIENCED LARGER AND LARGER A/S DEVIATIONS FROM RIGHT AND LEFT A/S INDICATORS, TCAS FAIL FLAG AND ALTITUDE VARIATIONS, LOSS OF MODE C AND R ALTIMETER WENT INTO BARO MODE. REPLACED FIRST OFFICERS ALTIMETER FOR EXCESSIV E LEAK STATIC SYSTEM. LEAK CHECKED AND OPS CHECKED OK. (M) 2 L 7 2 4F RT A6WE 1999052800597 19990528 00597 WP 1999 5 28 HALA9900107 1 19990501 A 2425 GENERATOR LIGHT DOUG DC10 DC1030 3023501 WP NR 2 ILLUMINATED A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 140AA 46712 KOA - NR 2 ENGINE GEN FAIL LIGHT ON. DEFERRED PER MEL 24-01, PLACARD 5-08C-B, 5/2/99 LAX. REMOVED AND REPLACED NR 2 GE NERATOR, OPS CHECK OK. (M) 2 L 7 3 4F A22WE 1999052800598 19990528 00598 WP 1999 5 28 HALA9900103 1 19990422 A 3244 TIRE DOUG DC10 DC1010 3022110 WP NLG FAILED A HALA K NONE O OTHER LD LANDING 1 WP 13 148AA 46703 SEA - AIRCRAFT ARRIVED SEATTLE LEFT NOSE GEAR TIRE BLOWN. FOUND WHEEL BEARING SEIZED TO AXLE SLEEVE. REMOVED BEARING R ACE INSPECTED SLEEVE. DAMAGE WITHIN LIMITS PER 32-42-01. AIRCRAFT CYCLE LIMITED TO 10 CYCLES. (M) 2 L 7 3 4F A22WE 1999052800599 19990528 00599 WP 1999 5 28 HALA9900104 1 19990429 A 2913 AS66411LS666 PUMP DOUG DC9 DC951 3022051 WP NR 1 ENGINE FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 660HA 5875 MX157566U 48122 HNL - LEFT ENGINE HYD PUMP FAILED. REPLACED LEFT ENGINE HYD PUMP PER MM 29-20-5 ENGINE RUN. OPS AND SECURITY CHECK OK AND LEAK CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999052800600 19990528 00600 WP 1999 5 28 HALA9900105 1 19990429 A 2911 976J2544 GCU DOUG DC10 DC1030 3023501 WP NR 3 ENGINE FAILED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 140AA 46712 SFO - FLT 11 - BLOCK RETURN, NR 3 GEN OFF LIGHT ILLUMINATED, BEFORE TAKEOFF. ISSUED MEL 24-1 AUT NR 4-214C-B, GENERATOR CONTROL UNIT REPLACED APR 29, 99 HNL. (M) 2 L 7 3 4F A22WE 1999052800601 19990528 00601 NM 1999 5 28 TSAA9933228 1 19990430 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 3, NR 4, NR 5 FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A16WE 1999052800602 19990528 00602 NM 1999 5 28 TSAA9933229 1 19990430 A 3350 9221009 BATTERY PACK BOEING 737 7372S2C 138448G NM PAX DOORWAY DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999052800603 19990528 00603 NM 1999 5 28 TSAA9933227 1 19990426 A 3350 86210151 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED AFT CONTROL MODUEL BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999052800604 19990528 00604 NM 1999 5 28 EIA990115 1 19990426 A 2931 60B002017 MODULE BOEING 747 747121 1384871 NM NR 2 PRESS SYS BROKEN A EIAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 480EV 20348 SYD - NR 2 HYD QTY 1 GALLON, ACCOMPLISHED ABNORMAL PROCEDURE HYD SYSTEM LEAK/LOSS JETTISON 40K FUEL, LANDING WT 604.9. F OUND BROKEN CHECK VALVE, HOUSING NR 2 HYD PRESS MODULE SERVICE MODULE INSTALLED PER RMM 29-51-23 AND LEAK CHECKED OK. NR 2 HYD RES SERVICED TO NORMAL OPS LEVEL. (M) 2 L 7 4 4F A20WE 1999052800605 19990528 00605 SO 1999 5 28 C2XA99IA212 1 19990401 A 5330 14522382001 SKIN EMB 145 EMB145 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE DENTED ADJACENT TO PANEL 272DR. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01099, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052800606 19990528 00606 SO 1999 5 28 C2XA99IA211 1 19990401 A 5320 73210303 FITTING EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE INBOARD FORWARD GALLEY ATTACH FITTINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMO VED AND REPLACED THE AFFECTED FITTINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052800607 19990528 00607 SO 1999 5 28 C2XA99IA210 1 19990401 A 5320 STRAP EMB 145 EMB145 SO FRAME 13-18 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 13 TO 18. MAINTENANCE REPAIRED THE AFFECTED BUTT STRAP IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01031, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999052800608 19990528 00608 1999 5 28 JBXA9900086 4 19990525 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 580ML 7289 STALL FAIL AT 6000 FT ON CLIMBOUT. COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CL6 5 MM 27-35-01. FUNCTIONAL TEST FLIGHT REQUIRED. PERFORMED FUNCTIONAL TEST FLIGHT, ALL FLIGHT PHASES GOOD, NO FAULT NOTE D. 2 L 7 2 4F RT A21EA 1999052800609 19990528 00609 NM 1999 5 28 RAAA99B2031 1 19990421 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 344 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND BS 344 FLOORBEAM UPPER CHORD AT LBL 25 THRU LBL 60 CORRODED. REPLACED FLOORBEAM UPPER C HORD BS 344 LBL 25 THRU LBL 68 IAW SRM 53-10-08 PG 9. 2 L 7 3 4F A3WE 1999052800610 19990528 00610 NM 1999 5 28 RAAA99B2032 1 19990421 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 312 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND BS 312 FLOORBEAM UPPER CHORD CORRODED AT LBL 3 THRU LBL 30. REMOVED UPPER CHORD, FABRIC ATED NEW UPPER CHORD 7075T6 .094 AND REPAIRED SPLICE IAW SRM 53-10-08 FIG 9. TREATED, PRIMED, PAINTED IAW SRM 51-10-06. INSTALLED UPPER CHORD SPLICE IAW SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 1999052800611 19990528 00611 NM 1999 5 28 RAAA99B2033 1 19990421 A 5320 CHANNEL BOEING 727 72722C 138400F NM BS 328 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND FLOOR SUPPORT CHANNEL CRACKED AT FORWARD ATTACH HOLE AND FLOORBEAM ATTACH HOLE ELONGATED AT BS 328 RBL 44. REMOVED FLOOR SUPPORT CHANNEL, FABRICATED NEW CHANNEL 7075T6 .094 IAW 51-10-02. TREATED AND PRIMED IAW 51-10-06. INSTALLED CHANNEL IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1999052800612 19990528 00612 NM 1999 5 28 RAAA99B2034 1 19990421 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 740 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND SEAT TRACK AT BS 740 AND RBL 28 CORRODED OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SEAT TRACK FROM BS 700-740 LBL 25 PER SRM 53-10-5-MATERIAL ID FOR REPAIR SECTION IS BAC1520-1264 PER SRM 53-10-02-FABRICATED REPAIR SECTION PER SRM 53-10-05 FIG 7. INSTALLED PER SRM 53-10-05-FIG 7. 2 L 7 3 4F A3WE 1999052800613 19990528 00613 NM 1999 5 28 RAAA99B2035 1 19990421 A 5320 FITTING BOEING 727 72722C 138400F NM BS 870 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION IAW AD91-24-11 OF BS 870 FITTING FOUND CRACK INDICATION TOP SIDE OF HOLE IN ROW NR 3, BOTTOM HOLE IN SPLICE PLATE AND FITTING BELOW STR 9R. NO CRACK DETECTED AFTER REAMING. INSTALLED EXTERNAL DOUBLER IAW SB 727 -53-0194 DWG 65C25277. 2 L 7 3 4F A3WE 1999052800614 19990528 00614 NM 1999 5 28 RAAA99B2036 1 19990421 A 5330 SKIN BOEING 727 72722C 138400F NM BS 338-372 GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND SEVERAL AREAS OF GOUGED SKIN BS 338-372 BELOW AND AFT FWD ENTRANCE DOOR. REPAIRED GOUGE IAW SRM 53-30-3 FIG 13. OTHER GOUGES ALLOWABLE LIMITS IAW 53-30-01 FIG 1. ALODINED AND PRIMED IAW 51-10-02. 2 L 7 3 4F A3WE 1999052800615 19990528 00615 NM 1999 5 28 RAAA99B2037 1 19990421 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 450 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION IAW AD 99 04 22, FOUND STR 21L CORRODED AT BS 450. REPAIRED IAW 53-10-3 FIG 1 DETAIL 2. 2 L 7 3 4F A3WE 1999052800616 19990528 00616 NM 1999 5 28 RAAA99B2038 1 19990421 A 5312 BULKHEAD FITTING BOEING 727 72722C 138400F NM BS 1183 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND S-3AR STRINGER BULKHEAD FITTING CRACKED IN INBOARD FITTING BS 1183 BULKHEAD. REMOVED AN D REPLACED BULKHEAD FITTING STRINGER S-3A IAW SRM 51-10-01. INSTALLED AND TORQUED NEW BOLTS IAW SB 727-53-0178. 2 L 7 3 4F A3WE 1999052800617 19990528 00617 NM 1999 5 28 RAAA99B2039 1 19990421 A 5312 BULKHEAD FITTING BOEING 727 72722C 138400F NM BS 1183 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND S-3AL STRINGER BULKHEAD FITTING CRACKED IN INBOARD FITTING BS 1183 BULKHEAD. REMOVED AN D REPLACED STRINGER BULKHEAD FITTING S-3AL IAW SRM 51-10-01. REPLACED AND TORQUED BOLTS AQS PER SB 727-53-0178. 2 L 7 3 4F A3WE 1999052800618 19990528 00618 NM 1999 5 28 RAAA99B2040 1 19990421 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1080-1183 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION PER CARD S1 14101, FOUND FUSELAGE SKIN CORRODED STR 3R TO STR 4R BS 1135 TO 1183 AND STR 4L BS 1130 TO 1148. REPLACED FUSELAGE SKIN PER BOEING MSG RVV-SEA-99-0004RR STR 1 TO STR 5R AND BS 1080 TO 1183. 2 L 7 3 4F A3WE 1999052800619 19990528 00619 NM 1999 5 28 RAAA99B2041 1 19990421 A 7120 MOUNT BOEING 727 72722C 138400F NM NR 2 ENGINE CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND NR 2 ENGINE AFT MOUNT ATTACH FITTING AND T CHORDS RUSTY AND PITTED. REMOVED AND REPLACE D AFT ENG MOUNT FITTING IAW SRM 54-40-01 AND SRM 51-10-01. 2 L 7 3 4F A3WE 1999052800620 19990528 00620 NM 1999 5 28 RAAA99B2042 1 19990421 A 5530 WEB BOEING 727 72722C 138400F NM VERT STAB CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED C-CHECK, FOUND VERTICAL STABILIZER CLOSURE WEB CORRODED INSIDE LOWER END AT ATTACH ANGLE INSIDE AND AFT NR 2 PYLON ACCESS PANEL AND AT LOWER END FASTENERS ABOVE NR 2 ENGINE MOUNT. REPAIRED IAW RAA ECO 99-4 REFERENCE DWG 6 5-22913 65-17551 M54 NR 761 AND NR 762. 2 L 7 3 4F A3WE 1999052800621 19990528 00621 1999 5 28 COMA9910083 4 19990523 A 3414 39948E2903 INDICATOR EMB 120 EMB120RT SO RT COCKPIT MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 159A 18805 2000 20159 COPILOTS AIR SPEED INDICATOR STUCK AT 100 KTS. REPLACED AIRSPEED INDICATOR. 2 L 7 2 4T RT A31SO 1999052800622 19990528 00622 EA 1999 5 28 COMA9960232 1 19990523 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 915CA 7130 7013 FLAPS FAILED AT 30 DEGREES. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999052800623 19990528 00623 EU 1999 5 28 QXEA9901069 1 19990521 A 3350 XB864041 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 12 BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 BOI - EMERGENCY LIGHT AT ROW 12 HAS A BROKEN COVER. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND OPERATIONALLY TESTED, T EST RESULT IS NORMAL. 2 L 7 2 4F RT A20EU 1999052800624 19990528 00624 EU 1999 5 28 QXEA9901070 1 19990523 A 3350 5515800106 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 GEG - FORWARD CABIN EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE SIGN. OPERATIONAL TEST PERFORMED, RES ULT WAS NORMAL. 2 L 7 2 4F RT A20EU 1999052800625 19990528 00625 NM 1999 5 28 99FDEA00192 1 19990525 A 2612 FIRE LOOP BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE INOPERATIVE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 205FE 22927 99-119 - NR 1 FIRE WARN ILLUM. BELL SOUND INTERMITTENT. THIS IS A REPEAT OCCURRENCE, FIRE WARNING SYS CK PER CKLIST OP ER NORM. INSTALL NR 1 ENG FIREWALL DETECTOR LOOP PER MM 26-11-012-4. RAN HIGH PWR ENG RUN ON NR 1 ENG, NO DEFECTS NOTE D. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999052800626 19990528 00626 NM 1999 5 28 99FDEA00193 1 19990525 A 3260 SWITCH BOEING 727 72722 1384002 NM NLG DOOR FAILED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 181FE 18868 NOSE GEAR DOOR LIGHT STAY ON 2ND OFF PANEL WITH RED DOOR WARNING ON FRONT PANEL. *S/D* REMOVED AND REPLACED RIGHT NOSE GEAR DOOR MICRO SWITCH PLUNGER ASSY PER MM 32-62-011-4 AND ADJUSTED AND TESTED PER MM 32-62-011-5. OPERATION TEST GOOD . 2 L 7 3 4F A3WE 1999052800627 19990528 00627 NM 1999 5 28 99FDEA00191 1 19990521 A 2612 FIRE WARNING BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE ACTIVATED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 205FE 22927 NR 1 ENGINE FIRE WARN LIGHT AND BELL SOUND INTERMITTENT DURING CRUISE FLT. 2 L 7 3 4F A3WE 1999052800628 19990528 00628 NM 1999 5 28 SCNA99074 1 19990524 A 3610 CLAMP BOEING 727 727227 1384078 NM NR 1 STRUT LOOSE A SCNA K NONE J WARNING INDICATION CL CLIMB 1 GL 15 275AF 22092 DURING CLIMB, THE NUMBER ONE ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. UPON INSPECTION OF THE NUMBER ONE STRUT FOUND A L OOSE CLAMP. REMOVED AND REPLACED CLAMP AS REQUIRED. OPERATIONALLY CHECKS GOOD, NO FURTHER DISAGREEMENT NOTED. 2 L 7 3 4F A3WE 1999052800629 19990528 00629 1999 5 28 JBXA9900083 4 19990524 A 3418 45150340 VANE CNDAIR CL600 CL6002B19 EA GE NR 2 AOA BENT A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 580ML 7289 AT ROTATION STALL FAIL, STICK SHAKER WINDSHEAR WARNING. FIRST OFFICERS RED LINE 250 KNTS. REMOVED AND REPLACED RIGHT A OA VANE IAW CRJ MM 27-35-05, OPS CK GOOD IAW CRJ MM 27-35-05 . 2 L 7 2 4F RT A21EA 1999052800630 19990528 00630 1999 5 28 JBXA9900084 4 19990524 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 EA GE STALL WARNING FAILED TEST A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 05 580ML 7289 STALL FAIL ON TAKEOFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER, OPS CK GOOD AT THIS TIME IAW CRJ MM 27-35-01. 2 L 7 2 4F RT A21EA 1999052800631 19990528 00631 1999 5 28 JBXA9900085 4 19990524 A 3418 ACTUATOR CNDAIR CL600 CL6002B19 EA STICK PUSHER FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 580ML 7289 RDU - ON TAKEOFF STALL FAIL WAS INTERMITTEN,THEN STAYED ON. REMOVED AND REPLACED STICK PUSHER ACTUATOR IAW CL65 MM 27-3 5-15 . 2 L 7 2 4F RT A21EA 1999052800632 19990528 00632 SO 1999 5 28 COMA9910082 1 19990522 A 3411 PITOT LINE EMB 120 EMB120RT SO RIGHT CONTAMINATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 159CA 120159 COPILOTS AIRSPEED INDICATOR INOPERABLE. PURGED PITOT LINE, SYSTEM TEST NORMAL. 2 L 7 2 4T RT A31SO 1999052800633 19990528 00633 EA 1999 5 28 COMA9960228 1 19990521 A 2752 854D1001 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 716CA 2032 7250 FLAPS FAILED AT 42 DEGREES. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 1999052800634 19990528 00634 EA 1999 5 28 COMA9960229 1 19990520 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PASSENGER DOOR CONTAMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 940CA 7048 CABIN DOOR OUTER HANDLE WARNING. REMOVED EXCESS GREASE FROM HANDLE MECHANISM, DOOR OPERATES NORMAL. 2 L 7 2 4F RT A21EA 1999052800635 19990528 00635 WP 1999 5 28 AT9900402 1 19990514 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE CABIN FLOOR PANEL NR 90 CORRODED AROUND THE EDGES. REMOVED, FIT , TRIMMED, DRILLED, TREATED, AND PRIMED REPLACEMENT SKIN PANEL AND INSTALLED IAW DC9 SRM 53-21-0, 51-10-2, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1999052800636 19990528 00636 NM 1999 5 28 AT9900404 1 19990523 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 330 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A DENT AT FUSELAGE STATION BS 330 STR 21L. REMOVED EXISTING DOUBLER , TRIMMED OUT DENT, AND FABRICATED A -20 DOUBLER AND -21 TRIPLER. DRILLED, DEBURRED, ALODINED AND INSTALLED REPAIR PARTS IAW B737 51-30-8, 51-20-11, 51-10-2, AND EO 99-1151 SHEET 2 OF 4 STEPS 1-8. 2 L 7 2 4F RT A16WE 1999052800637 19990528 00637 WP 1999 5 28 AT9900405 1 19990513 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 221.5 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A DENT ON THE FORWARD FUSELAGE AT BS 221.5 (1.5) ABOVE L-18L. FABRI CATED TITANIUM FINGER DOUBLER, CUT OUT CREASES, FABRICATED FILLER, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED REP AIR IAW DC9 SRM 53-04-0 AND 51-10-0, 51-30-2 AND RES NR 99-1089. 2 L 7 2 4F A6WE 1999052800638 19990528 00638 WP 1999 5 28 AT9900406 1 19990504 A 3250 5645105509 MECHANISM DOUG DC9 DC932 3022066 WP NLG CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT NOSE STEERING FOLLOW UP DIFFERENTIAL MECHANISM ARM CORRODED . REMOVED AND REPLACED THE NOSE WHEEL STEERING FOLLOW UP DIFFERENTIAL ARM IAW DC9 MM 32-51-2 AND RIGGED CHECK GOOD IAW MM 32-50-0. 2 L 7 2 4F A6WE 1999052800639 19990528 00639 WP 1999 5 28 AT9900407 1 19990511 A 5312 99155665 BULKHEAD PANEL DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE AFT PIT AFT BULKHEAD ACCESS PANEL AT BS 996 CORRODED ON THE BACK SIDE AROUND FASTENER HOLES. REMOVED AND REPLACED PANEL AND REINSTALLED CAMLOCKS IN THE NEW PANEL IAW DC9 SRM 53-01-0, 51-10-3, 51-30-0, AND DINITROL AFT PIT IAW MM 20-15-0 PG 201. 2 L 7 2 4F A6WE 1999052800640 19990528 00640 WP 1999 5 28 AT9900408 1 19990514 A 5320 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LOWER FORWARD CARGO COMPARTMENT DOOR JAMB CORNER CRACKED. CUT O UT CRACKED AREA OF SKIN, NDT VERIFIED REMOVAL. FABRICATED, TREATED, PRIMED, DRILLED, DEBURRED, COUNTERSUNK, AND INSTALL ED IAW DC9 SRM 51-10-3, 51-30-2, 51-30-5, 53-05 FIG 105, AND RES NR 99-1106. 2 L 7 2 4F A6WE 1999052800641 19990528 00641 WP 1999 5 28 AY9900409 1 19990513 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 943-1000 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A DENT AT FUSELAGE SKIN BS 943-1000 L-20R. GAIN ACCESS TO AREA, REM OVED SECTION OF SKIN, DRILLED NEW SECTION AND SKIN SPLICE. INSTALLED NEW SKIN SECTION AND SPLICE DOUBLER IAW DC9 SRM 51 -30-2, 51-10-3, 51-10-2, 51-10-4, AND RES NR 99-995. 2 L 7 2 4F A6WE 1999052800642 19990528 00642 NM 1999 5 28 99UAL900145 1 19990302 A 3610 04P238 SOLENOID BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE WORN A UALA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 29 768UA 5480 5480 26919 222007 FLIGHT CREW REPORTED, NR 2 ENGINE SURGED AT TOP OF DESCENT. *S/D* ENGINE SURGED AND RECOVERED. FLIGHT RECORDER DATA I NDICATED DELAYED OPENING OF 2.9 STABILITY BLEED VALVE. REPLACED 2.9 BLEED SOLENOID (P/N: 04P23-8), PNEUMATIC RELAY VALV E AND 2.9 STABILITY BLEED VALVE. PNEUMATIC RELAY VALVE AND 2.9 STABILITY BLEED VALVE PASSED AS-RECEIVED TEST. FOUND 2. 9 BLEED SOLENOID FAILED DROP-OUT VOLTAGE TEST, VALVE SEAT WORN. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999052800643 19990528 00643 NM 1999 5 28 99UAL900212 1 19990414 A 5753 CARRIAGE ASSY 654648195 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RT TE FLAP BROKEN A UALA K NONE F FLT CONT AFFECTED DE DESCENT 1 WP 29 976UA 2309WG 21598 STEERING YOKE COCKED LEFT AND REQUIRED A GOOD DEAL OF LEFT AILERON TRIM ONCE FLAPS 1 AND BELOW STARTED COMING DOWN. NO CHANGE THROUGH FLAP CONFIGURATIONS TO 30 DEGREE. *S/D* THE RIGHT WING OUTBOARD FLAP INBOARD CARRIAGE ASSEMBLY WAS FOUN D WITH A BROKEN SPINDLE. BOTH CARRIAGE ASSEMBLIES ON THE RIGHT WING OUTBOARD FLAP WERE REPLACED, OPS CHECK OK. 2 L 7 2 4F 4 F A16WE E2EA 1999052800644 19990528 00644 NM 1999 5 28 99UAL900277 1 19990515 A 2130 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAILED A UALA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 WP 29 657UA 27112 FL330 CABIN RATE BEGAN TO CLIMB AT MORE THAT 2,000 FEET PER MINUTE. ATTEMPTED AUTO MODE TO NR 2 MANUAL CABIN, STILL CLI MBING WITH OUTFLOW FULLY CLOSED. THE O2 MASKS DEPLOYED. DIVERTED TO RNO. *S/D* UPPER PRESSURE RELIEF VALVE (MR21313, SN OR DASH 2690) REPLACED AT SFO ON 16MAY99. THE PRESSURE RELIEF VALVE WAS SENT TO ALLIED SIGNAL FOR TESTING. PRELIMI NARY TESTS SHOW THE VALVE FAILED OPEN AND WOULD NOT RESEAT. THE OUTFLOW VALVE (MR21314 DASH 10) WAS ALSO REMOVED AT SFO . BOTH THE OUTFLOW VALVE AND THE OUTFLOW VALVE ACTUATOR WERE FOUND WITHIN LIMITS BY THEIR RESPECTIVE COMPONENT SHOP. 2 L 7 2 4F 4 F RT A1NM E24NE 1999052800645 19990528 00645 NM 1999 5 28 99UAL900278 1 19990514 A 2913 271N10586 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT HYD SYS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 573UA 26685 LANDED AT PDX UNDER AN AMBER ALERT DUE TO LEFT HYDRAULIC SYSTEM LOSING FLUID. FOUND LEFT ACMP LEAKING. REPLACED PUMP. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052800646 19990528 00646 NM 1999 5 28 99UAL900279 1 19990515 A 3241 161T100083 TRANSDUCER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ANTISKID SYS SHORTED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 563UA 26665 DIVERTED TO LAX DUE TO ANTI-SKID INDICATION. *S/D* NR 1 ANTISKID TRANSDUCER FAILED. REPLACED TRANSDUCER. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052800647 19990528 00647 1999 5 28 99UAL900280 4 19990516 A 3160 AIMS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LEFT TRIPPED A UALA K NONE O OTHER CR CRUISE 1 WP 29 786UA 26938 ENGINE BLEED EICAS: BOTH PACKS WORKING OFF OF LEFT BLEED. REPLACED RT PRSOV (PRESSURE REGULATING SHUTOFF VALVE) BUT CO NDITION REMAINS. *S/D* CAUSE WAS A DISCRETE LATCHED FAULT IN INPUT/OUTPUT MODUEL IOM M004 IN LEFT AIMS (AIRPLANE INFOR MATION MANAGEMENT SYSTEM). A RESET OF THE IOM M004 IN LEFT AIMS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999052800648 19990528 00648 NM 1999 5 28 99UAL900281 1 19990515 A 3246 27684 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG FAILED A UALA O OTHER A FLAME/FIRE LD LANDING 1 WP 29 570UA 26678 NOSE WHEEL BEARING FAILURE ON LANDING CAUSED A NOSE GEAR FIRE, WHICH THE AIRPORT FIRE DEPARTMENT EXTINGUISHED. *S/D* L EFT O/B NLG WHEEL BEARING FAILED. POSSIBLE CAGE FAILURE. REPLACED BEARING. 2 L 7 2 4F 4 F RT A2NM E17NE 1999052800649 19990528 00649 NM 1999 5 28 99UAL900282 1 19990517 A 2421 976J49812 GENERATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A UALA H DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 WP 29 7454U 21908 NR 1 AND NR 2 BUS TIE TRIPPED WITH PHASE UNBALANCE UPON FLAP EXTENSION, STARTED SHEDDING CB S, EQUIPMENT COOLING, COOLIN G FANS, BOOST PUMPS AND A & B SYSTEM PUMP. DID NOT LOOSE GENERATORS. *S/D* NR 3 GENERATOR FIELD WINDING OUT OF LIM ITS. FOUND A PHASE WOULD NOT CARRY HEAVY LOAD. REPLACED NR 3 GENERATOR. 2 L 7 3 4F 4 F A3WE E2EA 1999052800650 19990528 00650 NM 1999 5 28 99UAL900283 1 19990518 A 3260 15000323 RELAY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LANDING GEAR INOPERATIVE A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 904UA 25004 UNSAFE GEAR DOWN INDICATION. *S/D* NO GEAR DOWN INDICATION WITH GEAR EXTENDED. REPLACED THE LANDING GEAR AIR/GROUND R ELAY AND LIGHTS CIRCUIT BREAKER ITEM C404 ON THE P6-3 PANEL, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999052800651 19990528 00651 NM 1999 5 28 99UAL900285 1 19990519 A 2150 CONTROL PANEL ALLIEDSIGNAL 5483881 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT & RT PACK MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 302UA 23643 UNABLE TO MAINTAIN PRESSURIZATION. *S/D* LEFT AIR CONDITIONING PACK TRIPPED OFF FOLLOWED BY THE RIGHT PACK TRIPPED OFF AND WOULD NOT RESET. ADJUSTED LEFT RAM AIR EXHAUST LOUVERS. REPLACED AIR CONDITIONING ACCESSORY UNIT, OVERHEAD CONTRO L PANEL AND CABIN TEMPERATURE SENSOR, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999052800652 19990528 00652 1999 5 28 99UAL900287 4 19990519 A 3442 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RADAR SYS FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 657UA 27112 WEATHER RADAR FAILED AFTER DEPARTING JFK. DIVERTED TO IAD DUE TO THUNDERSTORMS EN ROUTE. *S/D* THE WEATHER RADAR TRAN SCEIVER (P/N 622-5122-103, MR43114 - 2032) WAS REPLACED AT IAD. THE SYSTEM OPS CHECKED NORMAL. UPDATE: 7/12/99 THE C OAX CONTACT INSERT ON THE TRANSCEIVER BENCH CONNECTOR D391A WAS DAMAGED AND WOULD NOT MAINTAIN CONTACT. REPLACED CONNEC TOR INSERT, SYSTEM OPERATIONALLY CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1999052800653 19990528 00653 WP 1999 5 28 ABXA9900381 1 19990524 A 5610 5613217507 WINDOW DOUG DC8 DC861 3021952 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 853AX 46037 UNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW (EMERGENCY EXIT). LUBRICATED CAPTAIN'S CLEARVIEW WINDOW LINKAGE, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999052800654 19990528 00654 NM 1999 5 28 SCNA99067 1 19990515 A 3350 1102833 POWER SUPPLY BOEING 727 7272A1 138407F NM AFT AIRSTAIR SHORTED A SCNA K NONE L NO TEST CR CRUISE 1 GL 15 287SC 21345 DURING FLIGHT, THE BATTERY CHARGER 28 VDC CIRCUIT BREAKER POPPED IN FLIGHT. FOLLOWED COM PROCEDURES, TRIED 1 RESET AND BREAKER POPPED AGAIN. FOUND AFT AIRSTAIR BATTERY PACK FOR POWER SUPPLY TO BE SHORTED INTERNALLY. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACKS. OPERATIONS CHECK GOOD IAW 335101. 2 L 7 3 4F A3WE 1999052800655 19990528 00655 NM 1999 5 28 SCNA99068 1 19990516 A 2150 COOLING DOOR BOEING 727 7272J4 1384006 NM LT PACK OPEN A SCNA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 284SC 21438 DURING TAXIING, TURNED LEFT PACK ON AND THE COMPRESSOR DISCHARGE AND SUPPLY TEMPERATURES RISED RAPIDLY, ACCOMPANIED WITH SMOKE IN THE CABIN. RETURNED TO GATE. FOUND LEFT HAND PACK COOLING DOOR CHECK VALVE STUCK OPEN. OPERATIONS CHECK VAL VE PER MM 215500. 2 L 7 3 4F RT A3WE 1999052800656 19990528 00656 NM 1999 5 28 SCNA99070 1 19990521 A 3350 SIGN BOEING 727 727282 138408T NM R1 DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED WIRI NG AT THE R1 DOOR EXIT SIGN, FUNCTIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999052800657 19990528 00657 NM 1999 5 28 SCNA99071 1 19990521 A 3350 900542 BATTERY PACK 900835A BOEING 727 727282 138408T NM LT EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 23375 21949 DURING A LINE MAINTENANCE CHECK, THE LEFT MIDDLE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BOTH THE BATTERY PACK AND POWER SUPPLY, OPERATIONALLY CHECKS GOOD IAW MM 335100. 2 L 7 3 4F RT A3WE 1999052800658 19990528 00658 NM 1999 5 28 SCNA99072 1 19990521 A 3350 900835A BATTERY PACK BOEING 727 727282 138408T NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE FORWARD CABIN OVER AISLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK, OPERATIONALLY CHECKS GOOD IAW MM 335100. 2 L 7 3 4F RT A3WE 1999052800659 19990528 00659 NM 1999 5 28 SCNA99073 1 19990520 A 3350 900542 POWER SUPPLY BOEING 727 727282 138408T NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE CENTER CABIN OVER AISLE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKS GOOD IAW MM 335100. 2 L 7 3 4F RT A3WE 1999052800660 19990528 00660 NE 1999 5 28 P5CA9900571 2 19990522 A 7321 FUEL CONTROL BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE MALFUNCTIONED A P5CA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 WP 23 856FT 19897 662518 DURING DESCENT LEAVING FL350 APPROACHING FL330 FUEL HEAT WAS ON NR 3 ENGINE, WOULD NOT RESPOND BEYOND 65 PERCENT TO THRO TTLE MOVEMENT. NO LOUD NOISES, NO EGT INCREASES. ENGINE WAS SHUTDOWN AND RESTARTED PER AOM. NO FUEL FLOW WITH START L EVER IN IDLE. PLACED START LEVER TO RICH AND ENGINE STARTED OK. PLACED START LEVER TO IDLE AND ENGINE APPEARED NORMAL. REMOVED AND INSPECTED FUEL CONTROL PRESSURE FILTER AND REINSTALLED. NO FOREIGN OBJECTS FOUND, OP CHECK GOOD PER MM 71 -21-03. OP CHECK OF FUEL DEICING SYSTEM GOOD PER MM 73-14-00. GROUND TEST AT IDLE ENGINE APPEARED NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1999052800661 19990528 00661 NM 1999 5 28 P5CA9900572 1 19990517 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 1759 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FUSELAGE DAMAGE FOUND AT FWD OF AFT CARGO DOOR TO EXTERIOR SKIN AT BS 1759 STRINGER 36 TO 37 RIGHT. CUT OUT DAMAGED ARE A AND REPAIRED PER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 1999052800662 19990528 00662 NM 1999 5 28 P5CA9900573 1 19990522 A 2910 LINE BOEING 747 747123 1384873 NM NR 4 HYD SYST CRACKED A P5CA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 23 858FT 20109 FOUND HYDRAULIC LEAK FROM NR 4 SYSTEM RETURN LINE AT TOP OF LOWER AFT CARGO COMPARTMENT NEAR DOOR ACTUATOR. PERMANENT R EPAIRED LINE (1 INCH DIAMETER) BY DEUTSCH PERMASWAGE REPAIR KIT. LEAK CHECKED OK. SERVICED NR 4 SYSTEM PER MM 29-11-00 . 2 L 7 4 4F A20WE 1999052800663 19990528 00663 NM 1999 5 28 SWAA990875 1 19990515 A 2560 6546570 BEAM BOEING 737 7373H4 1384600 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED 1/2D CHECK, FOUND BS 986.5, LBL 43.5 GIRT BAR ATTACH HOLE HAS HEAVY CORROSION AT BEAM. REPAIRED BEAM P ER SWA RA NR 1-353-2079. 2 L 7 2 4F RT A16WE 1999052800664 19990528 00664 NM 1999 5 28 SWAA990876 1 19990516 A 5313 6549892 STRINGER BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND THRU EDDY CURRENT INSPECTION 2 CRACKS AT STRINGER 6L BS 1016. REPAIRED STRINGER P ER SRM. 2 L 7 2 4F A16WE 1999052800665 19990528 00665 NM 1999 5 28 SWAA990878 1 19990515 A 5230 BAC1505 CHORD BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR LOWER T-CHORD CRACKED ON AFT END. REMOVED AND REPLACED DOOR ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052800666 19990528 00666 NM 1999 5 28 SWAA990879 1 19990515 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE BS 178 BULKHEAD CRACKED LBL 26, WL 207. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999052800667 19990528 00667 NM 1999 5 28 SWAA990880 1 19990514 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND LOWER KEEL BEAM CRACKED AT BS 706. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999052800668 19990528 00668 NM 1999 5 28 SWAA990881 1 19990514 A 2131 763101 CONTROLLER BOEING 737 7375H4 138449D NM E & E COMP ERRATIC A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 507SW 24184 AIR TURNBACK, PRESSURIZATION CONTROLLER FAILED TO RETURN TO FIELD (EVEN WITH BOTH PACKS OFF). UPON RETURN TO LAS, MANUA L A/C WAS REQUIRED TO DUMP THE CABIN. REMOVED AND REPLACED PRESSURE CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 1999052800669 19990528 00669 NM 1999 5 28 SWAA990882 1 19990514 A 3350 65C27093 SIGN BOEING 737 7373H4 1384600 NM PASSENGER DOOR BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 622SW 27932 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 1999052800670 19990528 00670 NM 1999 5 28 SWAA990883 1 19990516 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 780 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND 2 INCH LONG CRACK AT FUSELAGE SKIN, BS 780, BELOW SRINGER 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999052800671 19990528 00671 NM 1999 5 28 SWAA990884 1 19990516 A 3350 100885 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FWD END OF EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999052800672 19990528 00672 NM 1999 5 28 SWAA990885 1 19990515 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 20 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED D-CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT BROKEN AT ROW 20. REMOVED AND REPLACED TRACK SECTION PER MM. 2 L 7 2 4F RT A16WE 1999052800673 19990528 00673 NM 1999 5 28 SWAA990886 1 19990517 A 5320 6936642 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, LBL 26, WL 207. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999052800674 19990528 00674 NM 1999 5 28 SWAA990887 1 19990517 A 3350 BR2013 BULB BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED C4 CHECK, FOUND AFT EMERGENCY EVACUATION FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 1999052800675 19990528 00675 NM 1999 5 28 SWAA990888 1 19990517 A 3350 07912 LENS BOEING 737 7375H4 138449D NM EMERGENCY EXIT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED C4 CHECK, FOUND FWD AND AFT EMERGENCY EVACUATION FLOOR TRACK LIGHTING MISSING RED LENSES. INSTALLED RE D LENSES PER MM. 2 L 7 2 4F RT A16WE 1999052800676 19990528 00676 NM 1999 5 28 SWAA990889 1 19990518 A 5220 65C35019 STOP BOEING 737 7373T5 NM RT EMER EXIT DR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C3 CHECK, FOUND SEVERAL WORN STOPS AT RT EMERGENCY OVERWING EXIT HATCH. REMOVED AND REPLACED STOPS PER MM. 2 L 7 2 4F RT A16WE 1999052800677 19990528 00677 NM 1999 5 28 SWAA990890 1 19990518 A 3350 BR2013 CAP BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED C4 CHECK, FOUND END CAP MISSING AT FWD END OF EMERGENCY EVACUATION FLOOR TRACK LIGHTING. INSTALLED TRA CK SECTION PER MM. 2 L 7 2 4F RT A16WE 1999052800678 19990528 00678 NM 1999 5 28 SWAA990891 1 19990518 A 3350 07912 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED C4 CHECK, FOUND MISSING RED LENSES AT FWD AND AFT EMERGENCY EVACUATION FLOOR TRACK LIGHTING. INSTALLED LENSES PER MM. 2 L 7 2 4F RT A16WE 1999052800679 19990528 00679 NM 1999 5 28 SWAA990892 1 19990519 A 3246 26078251 WHEEL BOEING 737 7373H4 1384600 NM NLG VIBRATION A SWAA K NONE E VIBRATION/BUFFET TO TAKEOFF 1 SW 07 394SW 27380 ON TAKEOFF ROLL FROM PHX AT APPROXIMATELY 130-165 KNTS, SIGNIFICANT LATERAL MOVEMENT FROM CENTER LINE WAS ENCOUNTERED. N O SHIMMY BUT DIRECTIONAL CONTROL WAS VERY DIFFICULT, RAPID AND EXTREME RUDDER INPUTS WERE NECESSARY FOR CONTROL. REMOVE D AND REPLACED NOSE TIRE/WHEEL ASSY PER MM. 2 L 7 2 4F RT A16WE 1999052800680 19990528 00680 NM 1999 5 28 SWAA990893 1 19990519 A 3350 OL3071BPEGPL BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EVACUATION FLOOR TRACK LIGHTING INOP AT OVERWING EXIT. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 1999052800681 19990528 00681 NM 1999 5 28 SWAA990896 1 19990520 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STRINGER 10R. REMOVED AND REPLACED STRINGER CLIP PE R SRM. 2 L 7 2 4F A16WE 1999052800682 19990528 00682 NM 1999 5 28 SWAA990897 1 19990520 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED TRANSITION CHECK, FOUND CRACKS AT BULKHEAD WEB, BS 178, RBL 1-LBL 1, WL 188. REPAIRED BULKHEAD PER SRM . 2 L 7 2 4F RT A16WE 1999052800683 19990528 00683 NM 1999 5 28 SWAA990898 1 19990520 A 5220 65C35019 STOPS BOEING 737 7373Q8 1384670 NM LT, RT EMER EXIT WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED TRANSITION CHECK, FOUND WORN STOP PADS AT LT AND RT OVERWING EMERGENCY EXIT DOORS. REMOVED AND REPLACE D STOPS PER MM. 2 L 7 2 4F RT A16WE 1999052800684 19990528 00684 NM 1999 5 28 SWAA990899 1 19990520 A 3350 OL307BPEGPL BULB BOEING 737 7375H4 138449D NM EMERGENCY EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED C3 CHECK, FOUND AFT EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999052800685 19990528 00685 NM 1999 5 28 SWAA990894 1 19990520 A 3222 6573762 STRUT BOEING 737 7373H4 1384600 NM NLG OVERSERVICED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 07 616SW 27699 REJECTED TAKEOFF AT APPROX 70 KNTS AFTER 2 OR 3 SIGNIFICANT YAWS TO LEFT AND RIGHT, ACCOMPANIED BY LOUD BANGS/BUMPS. AP PEARED TO COME FROM NOSE WHEEL WELL AREA. INSPECTED ALL TIRES, BRAKES AND STRUTS AND FOUND NOSE STRUT OVERSERVICED. S ERVICED STRUT PER MM. HIGH SPEED TAXI CKD OK. 2 L 7 2 4F RT A16WE 1999052800686 19990528 00686 NM 1999 5 28 SWAA990895 1 19990520 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 15 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 627SW 27935 EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT ROW 15. RESECURED WIRES AT TRACK LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999052800687 19990528 00687 WP 1999 5 28 TWAA9907501 1 19990521 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 CE 05 993Z 47082 DURING TAXI, FORWARD CABIN EGRESS LIGHTS CAME ON. AIRCRAFT RETURNED TO THE GATE. THE POWER SUPPLY WAS WORN OUT. POWER SUPPLY WAS REPLACED. CHECKS MADE TO ASSURE NORMAL OPERATION. CHECK -C 12-07-98 STL. 2 L 7 2 4F A6WE 1999052800688 19990528 00688 WP 1999 5 28 TWAA9907502 1 19990520 A 3350 3350003611 BATTERY PACK DOUG DC9 DC934 302207E WP ROW 8-20 DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 936L 47711 DURING PREFLIGHT CHECK, ROW 8-20 EGRESS LIGHTS WERE FOUND INOP. THE PROBLEM WAS LOW BATTERY PACKS. TWO PACKS WERE CHAN GED. CHECK -C 06-17-98 STL. 2 L 7 2 4F RT A6WE 1999052800689 19990528 00689 WP 1999 5 28 TWAA9907503 1 19990522 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 905TW 49157 DURING PREFLIGHT CHECKS, FIRST CLASS EGRESS LIGHTS WERE FOUND INOPERATIVE. MOISTURE WAS FOUND IN THE LIGHTING TRACK. M OISTURE WAS DRIED FROM THE TRACK AND CONNECTORS AND LIGHTS OPERATED NORMALLY. CHECKS WERE MADE FOR NORMAL OPERATION. C HECK-C 12-15-98 STL. 2 L 7 2 4F A6WE 1999052800690 19990528 00690 WP 1999 5 28 TWAA9907504 1 19990523 A 3350 SWITCH DOUG DC9 DC983 3022083 WP ROW 7-9 OUT OF POSITION A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9407R 49400 FOUND EGRESS LIGHTS STAYED ON AT ROWS 7 TO 9 AFTER ENGINE SHUT DOWN. RESET THE EMERGENCY LIGHT SWITCH AND OPERATION NOR MAL. CHECK-C 5-1-99 STL. 2 L 7 2 4F RT A6WE 1999052800691 19990528 00691 NM 1999 5 28 TWAA9907505 1 19990523 A 3350 CONNECTOR BOEING 767 767231 1385131 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 603TW 22566 FOUND EGRESS LIGHTS INOPERATIVE IN B ZONE, LEFT SIDE OF CABIN. SECURED CONNECTORS ON POWER FLEX CABLE, B ZONE. CHECK-C 3-27-99 LAX. 2 L 7 2 4F RT A1NM 1999052800692 19990528 00692 WP 1999 5 28 TWAA9907506 1 19990518 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 996 BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND ON RT SIDE OF AIRCRAFT AT CUSP LINE STA 996, THE FWD EDGE OF THE FLANGE WAS BLENDED AND REPAIRED. INSTALLED TEE CAP PER SRM 53-03, FIG 37. 2 L 7 2 4F A6WE 1999052800693 19990528 00693 WP 1999 5 28 TWAA9907507 1 19990515 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 188-193 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 DURING CHECK-C MAINT, FOUND MATERIAL REMOVED BEYOND LIMITS FOR CORROSION REMOVAL ON FLOOR SUPPORT, STA 188 TO 193, RBL 4 4. REPLACED FLOOR SUPPORT AT STA 160 TO 200, RBL 44. 2 L 7 2 4F A6WE 1999052800694 19990528 00694 WP 1999 5 28 TWAA9907508 1 19990511 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 826 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 DURING CHECK-C MAINT, FOUND CABIN FRONT SPAR UPPER CAP TIE ANGLE WAS CRACKED APPROX 6 INCHES LONG, STA 826, RBL 58 INCHE S. REPLACED TIE ANGLE WITH NEW PART PER SRM 6-70-01. 2 L 7 2 4F A6WE 1999052800695 19990528 00695 WP 1999 5 28 TWAA9907509 1 19990513 A 5510 SPAR DOUG DC9 DC931 3022065 WP HORIZ STAB CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND THE HORIZ STABILIZER UPPER SPAR CAP BARREL NUT HOLES, RT SIDE AFT HOLE, AND LT SIDE AFT HOLE, WERE CORRODED. REPAIRED PER ARA 16167. 2 L 7 2 4F A6WE 1999052800696 19990528 00696 WP 1999 5 28 TWAA9907510 1 19990511 A 5744 CASTING DOUG DC9 DC931 3022065 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND LT WING REAR SPAR I/B FLAP ATTACH CASTING HAD CRACK INDICATION AT LOWER O/B HOLE AT 8 O' CLOCK AND LOWER I/B HOLE AT 5:30 AND 6:00 O'CLOCK POSITIONS. REPAIRED PER MC8-AD-34 AND DRAWING JO60271M. 2 L 7 2 4F A6WE 1999052800697 19990528 00697 WP 1999 5 28 TWAA9907511 1 19990522 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 775 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 412EA 47733 FOUND .5 INCH CRACKS IN LONGERON 5L AND 3L, STA 775. SPLICED LONGERON SECTIONS PER SRM 53-02, FIG 18. CHECK-C 10-17-98 STL. 2 L 7 2 4F RT A6WE 1999052800698 19990528 00698 WP 1999 5 28 TWAA9907512 1 19990522 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 775 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 412EA 47733 FOUND .5 INCH CRACK IN LONGERON 2L, STA 775. REPAIRED CRACKED LONGERON 2L AT STA 775 PER SRM 53-02, FIG 18. CHECK-C 10 -17-98 STL. 2 L 7 2 4F RT A6WE 1999052800699 19990528 00699 NM 1999 5 28 TWAA9907513 1 19990519 A 5330 SKIN BOEING 757 757231 1384950 NM FUSELAGE PUNCTURED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 717TW 28485 PUNCTURE IN FUSELAGE, 3 IN BY 5 IN, LOCATED 3 FT FWD OF THE NUMBER 4 DOOR ON LT SIDE, AND 6 IN BELOW THE DOOR. REPAIRED PER SRM 53-00-01, FIG 204, SHEET 3. 2 L 7 2 4F RT A2NM 1999052800700 19990528 00700 EU 1999 5 28 MALA976473 1 19990516 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297.5-564 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK INSPECTION, SEAT TRACK CORROSION. SEAT TRACK WEB AND FLANGES AT BL 0 RIGHT I/B FROM STA 297.5 TO STA 564 .0 HAS CORROSION AND PITTING. MAINTENANCE BLENDED OUT CORROSION AND PITTING IAW SRM 51-70-40 AND IAW SAAB DOC NR 72SDS1 546. FABRICATED REINFORCEMENT ANGLES FROM 7075-T7 IAW SAAB NR 72SDS1546 REV A AND SURFACE TREATED, INSTALLED ANGLES IAW SAAB 72SDS1546 REV A. 2 L 7 2 4T RT A52EU 1999052800701 19990528 00701 EU 1999 5 28 MALA976474 1 19990515 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297.5-525 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 429 DURING C-CHECK INSPECTION, SEAT TRACK WEB AND FLANGES AT BL 18.3 LEFT I/B FROM STA 297.5 TO STA 525.0 HAS CORROSION AND PITTING. MAINTENANCE BLENDED OUT CORROSION AND PITTING IAW SRM 51-70-40 AND IAW SAAB DOC NR 72SDS1546 REV A, FABRICATED REINFORCEMENT ANGLE FROM 7070-T7 IAW SAAB NR 72SDS1546 REV A, SURFACE TREATED, AND INSTALLED ANGLE IAW SAAB NR 72SDS15 45 REV A. 2 L 7 2 4T RT A52EU 1999052800702 19990528 00702 EU 1999 5 28 MALA976475 1 19990523 A 2560 COVER BAC 146 AVRO146RJ85A 1500097 EU PASSENGER DOOR DETACHED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 509XJ E2321 DURING PREFLIGHT, FA NOTED MAIN DOOR SLIDE DRAGS ON FLOOR. MAINTENANCE REMOVED DOOR SLIDE COVER, INSPECTED LEFT FORWARD DOOR SLIDE AND SLIDE FOUND TO BE IN SERVICEABLE CONDITION. 2 H 7 4 4F RT A49EU 1999052800703 19990528 00703 EU 1999 5 28 MALA976476 1 19990521 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 417XJ 340B417 CARGO SMOKE WARNING LIGHT ILLUMINATED DURING FLIGHT. CREW COMPLETED MEMORY ITEMS AND LIGHT WENT OUT. AIRCRAFT CONTINUE D WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 CARGO FIRE EXTINGUISHER IAW 26-23-10-4 IN AMM AND PERFORMED OPS CHECK IAW 26-23-00-5 IN AMM. REPLACED BOTH CARGO SMOKE DETECTORS AND PERFORMED OPS CHECK. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999052800704 19990528 00704 EU 1999 5 28 MALA976477 1 19990521 A 3320 65111 BALLAST SAAB SF340 340B 7860101 EU CABIN FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 417XJ 340B417 A STRONG ELECTRIC SMOKE ODOR WAS DETECTED. MAINTENANCE REPLACED BAD BALLAST FOR SIDEWALL LIGHTING, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999052800705 19990528 00705 EU 1999 5 28 MALA976478 1 19990520 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 412XJ 340B412 ON TAKEOFF OUT OF MSP, HYD PUMP WOULD NOT WORK IN OVERRIDE MODE. AFTER GOING THROUGH QRH IT OPERATED AGAIN. ON LANDING IN MSP, OVERRIDE MODE WOULD NOT WORK UNTIL JUST REACHING THE GATE. MAINTENANCE REPLACED HYD PUMP PER SF340 AMM 29-10-1 0. PERFORMED FUNCTIONAL CHECKS OF HYD PUMP. OPS AND LEAK CHECKS GOOD. SERVICED HYD. 2 L 7 2 4T RT A52EU 1999052800706 19990528 00706 EU 1999 5 28 MALA976479 1 19990519 A 2913 4018502 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM FAILED A MALA O OTHER O OTHER CL CLIMB 1 GL 15 412XJ 340B412 GEAR DID NOT RETRACT UNTIL HYD PUMP SWITCH WAS SELECTED TO OVERRIDE, PUMP WORKS PROPERLY IN THE OVERRIDE POSITION. MAIN TENANCE CONTROL DEFERRED AUTO PUMP CONTROL SYSTEM. MAINTENANCE REPLACED HYD PUMP PER SR340 AMM 29-10-10. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999052800707 19990528 00707 EU 1999 5 28 MALA976480 1 19990520 A 7712 CONNECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 98XJ 098 DURING TAKEOFF, LEFT TORQUE INDICATOR WAS ERRATIC, APPROX 60 TO 110 PERCENT. ALL OTHER ENGINE INDICATIONS NORMAL. ACTU AL POWER APPEARED NORMAL, NO SURGING. AIRCRAFT RETURNED TO CVG. MAINTENANCE INSPECTED LEFT ENGINE AND FOUND CANNON PLU G ON PCU LOOSE. CLEANED AND RESECURED CANNON PLUG. RAN ENGINES WITH AND WITHOUT CTOT, ALL PARAMETERS NORMAL. TQ INDIC ATIONS SOLID OVER THE ENTIRE TORQUE RANGE. 2 L 7 2 4T RT A52EU 1999052800708 19990528 00708 WP 1999 5 28 CALA9900571 1 19990524 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1079-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED FROM STA 1079 TO 1231. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999052800709 19990528 00709 WP 1999 5 28 CALA9900572 1 19990524 A 5240 BEAM DOUG DC9 DC982 3022082 WP FWD SERV DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-02 AND 51-30- 05. 2 L 7 2 4F A6WE 1999052800710 19990528 00710 WP 1999 5 28 CALA9900573 1 19990524 A 5210 BEAM DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A 1 INCH CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51 -30-1. 2 L 7 2 4F A6WE 1999052800711 19990528 00711 WP 1999 5 28 CALA9900574 1 19990525 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A 1 CRACK IN LONGERON 2R AND FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1418. THE CRACKED SECTIONS OF LONGERON WERE REMOVED, NEW SECTIONS AND SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1999052800712 19990528 00712 WP 1999 5 28 CALA9900575 1 19990525 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A .5 INCH CRACK IN LT INNER ATTACH ANGLE AT FORWARD LOWER ATTACH POINT FOR VERTICAL STABILIZER, FUSELAG E STA 1418. A 1.5 INCH CRACK WAS FOUND IN RT INNER ATTACH ANGLE AT FORWARD LOWER ATTACH POINT FOR VERTICAL STABILIZER, FUSELAGE STA 1418. THE ATTACH ANGLES WERE REMOVED AND NEW ONES WERE INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999052800713 19990528 00713 WP 1999 5 28 ABXA9900382 1 19990524 A 5250 AR25291GR41 LATCH DOUG DC8 DC861 3021952 WP COCKPIT MALFUNCTIONED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 COCKPIT DOOR WOULD NOT UNLOCK. REPLACED COCKPIT DOOR LATCH ASSEMBLY IAW DC8 MM 51-30. 2 L 7 4 4F 4A25 1999052800714 19990528 00714 WP 1999 5 28 MWEA99301 1 19990522 A 5210 59347961N FITTING DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACKED FORWARD PASSENGER DOOR NUMBER 1 BEAM AFT END FITTING. MTC FABRICATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999052800715 19990528 00715 WP 1999 5 28 MWEA99302 1 19990522 A 5320 49149541N CLIP DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND HEAVY CORROSION UNDER LONGERON END CLIP AT 22L AND FS 996. MTC FABRICATED AND INSTALLED NEW SHOVEL CLIP. 2 L 7 2 4F A6WE 1999052800716 19990528 00716 WP 1999 5 28 MWEA99303 1 19990522 A 5311 99582391 FRAME DOUG DC9 DC932 3022066 WP BS 1019 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND TWO HOLES IN RADIUS BELOW LONGERON 14R AT STATION 1019. MTC FABRICATED AND INSTALLED FILLER ANGLE AND PLATE. 2 L 7 2 4F A6WE 1999052800717 19990528 00717 WP 1999 5 28 MWEA99304 1 19990522 A 5210 99557521 BEAM DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 THE FORWARD PASSENGER DOOR NUMBER 1 BEAM AFT END IS CRACKED. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999052800718 19990528 00718 WP 1999 5 28 MWEA99305 1 19990524 A 5230 995766411 INTERCOSTAL DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 THE FORWARD CARGO DOOR UPPER STOP SUPPORT INTERCOSTAL IS CRACKED. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999052800719 19990528 00719 NM 1999 5 28 MWEA99306 1 19990525 A 5313 291272712000 LONGERON DOUG MD88 MD88 3023688 NM BS 1361 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FOUND HEAVY CORROSION ON LONGERON 24R AT STATION 1361. MTC FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F RT A6WE 1999060400001 19990604 00001 WP 1999 6 4 AT9900403 1 19990522 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE PASSENGER CABIN FLOORBEAM IN AFT LAVATORY AREA CHAFED AND CORROD ED AT BS 980 BL 0-44L. FORMED NEW FLOORBEAM, LOCATED, DRILLED AND DEBURRED. FABRICATED REPAIR DOUBLER, ALODINED, PRIME D AND INSTALLED REPAIR PARTS IAW DC9 SRM 53-05 FIG 79, 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1999060400002 19990604 00002 WP 1999 6 4 AT9900409 1 19990513 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 943-1000 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 809AT 47322 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A DENT AT FUSELAGE SKIN BS 943-1000 L-20R. GAINED ACCESS TO AREA, R EMOVED SECTION OF SKIN, DRILLED NEW SECTION AND SKIN SPLICE. INSTALLED NEW SKIN SECTION AND SPLICE DOUBLER IAW DC9 SRM 51-30-2, 51-10-3, 51-10-2, 51-10-4, AND RES NR 99-995. 2 L 7 2 4F A6WE 1999060400003 19990604 00003 WP 1999 6 4 CALA9900576 1 19990526 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A .25 INCH CRACK WITH BEND AT LOCKING HANDLE IN FORWARD CARGO DOOR EXTERIOR SKIN. A DOUBLER WAS INSTAL LED IAW SRM 52-05, FIGURE 30. 2 L 7 2 4F A6WE 1999060400004 19990604 00004 WP 1999 6 4 CALA9900577 1 19990526 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 200. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEC TION WAS SPLICED IN IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999060400005 19990604 00005 WP 1999 6 4 CALA9900578 1 19990526 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 389 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 389, LONGERON 30. A DOUBLER WAS INSTALLED IAW SRM 53-04 AND ECR A 5330-02812. 2 L 7 2 4F A6WE 1999060400006 19990604 00006 WP 1999 6 4 CALA9900579 1 19990527 A 5210 BEAM DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A .375 INCH CRACK IN MAIN CABIN DOOR NR 7 BEAM. THE DOOR BEAM WAS REPAIRED IAW SRM 52-05, FIGURE 31. 2 L 7 2 4F A6WE 1999060400007 19990604 00007 WP 1999 6 4 9901779867 1 19990523 A 5753 HINGE DOUG DC9 DC951 3022051 WP LT TE FLAP BROKEN A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 776NC 47786 AFTER CONFIGURING FOR LANDING, A THUMP WAS FELT/HEARD AND A SPLIT FLAP INDICATION WAS NOTICED BY FLIGHT CREW AT APPROXIM ATELY 8 DEGREES RIGHT FLAP AND 40 DEGREES LEFT FLAP. THE FLAP/SLAT HANDLE WAS SPLIT DURING COM PROCEDURES AT WHICH TIME THE FLIGHT CREW REPORTED THERE DID NOT APPEAR TO BE CONTROL OF EITHER FLAP WITH THE FLAP LEVER. THE FLIGHT CREW INITIA TED A GO-AROUND PROCEDURE, DECLARED A YELLOW EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT INBOARD AFT NR 2 FLAP HINGE BROKEN. REPLACED BROKEN PART AND ADJUSTED PER MAINTENANCE MANUAL AND CITEXT PROCEDURES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999060400008 19990604 00008 WP 1999 6 4 9901789602 1 19990521 A 3260 UNSAFE LIGHT DOUG DC9 DC932 3022066 WP NLG ILLUMINATED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 602NW 47046 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS RETURNED TO YEG AND LANDED WITHOUT INCIDEN T. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. MAINTENANCE CYCLED GEAR SEVERAL TIMES. PROBLEM WOULD NOT BE DUPLICATED ON GROUND. 2 L 7 2 4F A6WE 1999060400009 19990604 00009 NE 1999 6 4 9901793221 2 19990524 A 7200 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 FLAMED OUT A NWAA E ENGINE SHUTDOWN J X WARNING INDICATION ENGINE FLAMEOUT AP APPROACH 1 GL 01 321US 262 731728 DURING APPROACH, THE NR 1 EGT EXCEEDANCE OCCURRED AND ENGINE FLAMED OUT AT 2000 FEET. FLIGHT CREW RESTARTED ENGINE AT 4 00 FEET AND PERFORMED AN UNEVENTFUL LANDING. BORESCOPE, FUEL FILTER, MAG PLUG, AND VBV SYSTEM INSPECTIONS REVEALED NO D ISCREPANCIES. AIRCRAFT TO BE FERRIED TO MSP FOR ENGINE CHANGE. 2 L 7 2 4F 4 F RT A28NM E29NE 1999060400010 19990604 00010 NM 1999 6 4 9901806302 1 19990523 A 3350 LIGHT BOEING 747 747451 1384940 NM ROW 51-65 INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51A - 65A. RECONNECTED LIGHTS, OPERATIONAL C HECK GOOD. 2 L 7 4 4F RT A20WE 1999060400011 19990604 00011 NM 1999 6 4 9901816310 1 19990521 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM ROW 51-66 DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND DOOR 4R EMERGENCY EXIT SIGN AND ROWS 51HJK - 66HJK FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RE PLACED BATTERY PACK AND RECONNECTED CONTACTS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999060400012 19990604 00012 WP 1999 6 4 9901829154 1 19990524 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS IN TAIL CATWALK INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN PO WER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999060400013 19990604 00013 NM 1999 6 4 UPS99229674 1 19990526 A 3350 BATTERY PACK BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 907UP 19118 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS LEFT ON FROM LAST FLIGHT. RELAMPED AND REPLACED BATTERY, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999060400014 19990604 00014 NM 1999 6 4 UPS99429673 1 19990505 A 5320 SHEAR TIE BOEING 747 747283B 1384867 NM BS 1241 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 INSPECTION TYPE:C, CORROSION ON UNDERSIDE OF SHEAR TIE BETWEEN STA 1241 AND KEEL BEAM FWD OF SPEED BRAKE MECHANISM. NEW SHEAR TIE FABRICATED AND FITTED IAW 51-30-02. 2 L 7 4 4F A20WE 1999060400015 19990604 00015 EU 1999 6 4 99FDEA00194 1 19990525 A 3222 C231091109 STRUT AIRBUS 310 A310222 3930315 EU NLG BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 420FE 339 BROKEN NOSE LANDING GEAR GROUND LOCK PIN. REMOVED AND REPLACED TELESCOPIC STRUT, TEST SAISFACTORY. GROUND LOCK WAS INS ERTED AND REMOVED EASILY WITH A/C ON GROUND. 2 L 7 2 4F RT A35EU 1999060400016 19990604 00016 WP 1999 6 4 ABXA9900383 1 19990524 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 984AX 47258 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 MM, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999060400017 19990604 00017 NM 1999 6 4 SCNA99075 1 19990525 A 3610 SENSE LINE BOEING 727 727227 1384078 NM NR 1 STRUT DAMAGED A SCNA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 275AF 22092 DURING CLIMB WITH TAKEOFF POWER GOT MOMENTARY ILLUMINATION OF THE NUMBER ONE ENGINE STRUT OVERHEAT LIGHT. ALL OTHER IND ICATIONS NORMAL. REPLACED DAMAGED SENSE LINE ON THE NUMBER ONE ENGINE 13TH STAGE MODULATING AND SHUTOFF VALVE PER BMM C HAPTER 75-30-00. RAN NUMBER ONE ENGINE TO TAKEOFF EPR FOR FOUR MINUTES WITH NO OVERHEAT NOTED. 2 L 7 3 4F A3WE 1999060400018 19990604 00018 NM 1999 6 4 VNAA9905006 1 19990517 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 437JS 2966 957 3055 DURING THE PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS TOWARDS THE REAR OF THE AIRCRAFT, FAILED TO ILLUMINATE. OUTSTATIO N MAINTENANCE INSPECTED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FLIGHT WAS COMPLETED WITH NO PROBLEMS. P IT MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY PACK 7LK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-5 1-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400019 19990604 00019 NM 1999 6 4 SWAA990900 1 19990521 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM ROW 1ABC DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 718SW 27852 EMERGENCY ESCAPE FLOOR TRACK LIGHTING KICKED OUT OF PLACE AND DAMAGED AT ROW 1 ABC. REMOVED AND REPLACED TRACK ASSY PER MM. 2 L 7 2 4F RT A16WE 1999060400020 19990604 00020 NM 1999 6 4 SWAA990901 1 19990523 A 5210 699262 COVER BOEING 737 7373H4 1384600 NM PASSENGER DOOR FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 307SW 22947 AIR TURNBACK, VERY LOUD NOISE AT FWD ENTRY DOOR DURING FLIGHT. REMOVED AND REPLACED UPPER HINGE COVER ON FWD ENTRY DOOR . 2 L 7 2 4F RT A16WE 1999060400021 19990604 00021 NM 1999 6 4 SWAA990902 1 19990521 A 3350 6113211 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999060400022 19990604 00022 NM 1999 6 4 SWAA990903 1 19990521 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND APPROX A 3 INCH LONG CRACK AT FUSELAGE SKIN, BS 727E, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999060400023 19990604 00023 NM 1999 6 4 SWAA990904 1 19990522 A 5330 6545974 SKIN BOEING 737 7372H4 138448C NM BS 785 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND APPROX A 1.25 INCH LONG CRACK AT FUSELAGE SKIN, BS 785 STRINGER 24L. 2 L 7 2 4F A16WE 1999060400024 19990604 00024 NM 1999 6 4 SWAA990905 1 19990522 A 5314 6545866 KEEL BEAM BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULE 1/4D CHECK, FOUND CORROSION AT KEEL BEAM RT SIDE, JUST AFT OF BS 727 BULKHEAD. REPAIRED BEAM PER SRM. 2 L 7 2 4F A16WE 1999060400025 19990604 00025 NM 1999 6 4 SWAA990906 1 19990524 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 EMERGENCY ESCAPE FLOOR TACK LIGHT COVER LOOSE AT ROW 7. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 1999060400026 19990604 00026 NM 1999 6 4 SWAA990907 1 19990523 A 3350 100885 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 309SW 22948 EMERGENCY ESCAPE FLOOR TRACK LIGHT AT FRONT OF PAX CABIN INOP. REMOVED AND REPLACED BATTERY PACK AND GROUND WIRE SECTIO N PER MM. 2 L 7 2 4F RT A16WE 1999060400027 19990604 00027 NM 1999 6 4 SWAA990908 1 19990523 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 18ABC INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 EMERGENCY EXIT LIGHT INOP AT ROW 18 ABC. REPAIRED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 1999060400028 19990604 00028 NM 1999 6 4 SWAA990910 1 19990523 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 937-940 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937-940, STRINGER 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999060400029 19990604 00029 NM 1999 6 4 SWAA990911 1 19990525 A 5330 6545772 SKIN BOEING 737 7372H4 138448C NM BS 727-737 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND THRU EDDY CURRENT INSPECTION 4 EA CRACK INDICATIONS AT BS 727A+10, STRINGERS 4L, 4 R AND AT BS 757, STRINGERS 10L,10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999060400030 19990604 00030 NM 1999 6 4 SWAA990912 1 19990525 A 2560 65657933 BRACKET BOEING 737 7373L9 1384470 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 AFT GIRT BAR BRACKET LOOSE AT RT AFT SERVICE DOOR. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 1999060400031 19990604 00031 NM 1999 6 4 SWAA990913 1 19990522 A 5330 6545772 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING WALKAROUND INSPECTION, FOUND 4 INCH LONG CRACK ON FUSELAGE SKIN BS 727A-727B, STRINGER 10R. REPAIRED SKIN PER SR M. 2 L 7 2 4F A16WE 1999060400032 19990604 00032 NM 1999 6 4 SWAA990914 1 19990525 A 2782 654465111 ACTUATOR BOEING 737 7372H4 138448C NM NR 1 LE SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 055SW 21593 AIR TURNBACK, NR 1 LE SLAT WOULD NOT FULLY RETRACT DURING FLIGHT. REMOVED AND REPLACED NR 1 SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 1999060400033 19990604 00033 NM 1999 6 4 SWAA990916 1 19990524 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 318 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT STRINGER 26L AND SPLICE, BS 318. REPAIRED STRINGER AND SPLICE PER SRM. 2 L 7 2 4F A16WE 1999060400034 19990604 00034 NM 1999 6 4 SWAA990917 1 19990526 A 2782 65446519 ACTUATOR BOEING 737 7372H4 138448C NM NR 3 LE SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 094SW 23053 AIR TURNBACK AFTER TAKEOFF, NR 3 LE SLAT INTRANSIT LIGHT CAME ON, RECYCLED SLATS AND LIGHT REMAINED ON WITH FLAPS IN FUL L UP POSITION. REMOVED AND REPLACED NR 3 SLAT ACTUATOR PER MM. 2 L 7 2 4F A16WE 1999060400035 19990604 00035 NM 1999 6 4 SWAA990918 1 19990524 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTING IN AFT CABIN BROKEN. REPAIRED TRACK LIGHTING P ER MM. 2 L 7 2 4F RT A16WE 1999060400036 19990604 00036 NM 1999 6 4 SWAA990919 1 19990524 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND A 4 INCH LONG CRACK AT FUSELAGE SKIN, BS 727D, STRINGER 24R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 1999060400037 19990604 00037 1999 6 4 SWAA990920 4 19990525 A 2565 61620468 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 FWD SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999060400038 19990604 00038 NM 1999 6 4 SWAA990921 1 19990525 A 5312 963820 BULKHEAD CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, RBL 26, WL 207. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F A16WE 1999060400039 19990604 00039 NM 1999 6 4 SWAA990922 1 19990525 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602SW 27953 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT LENS COMING LOOSE. RESECURED LENS PER MM. 2 L 7 2 4F RT A16WE 1999060400040 19990604 00040 1999 6 4 SWAA990923 4 19990525 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999060400041 19990604 00041 NM 1999 6 4 SWAA990924 1 19990525 A 3350 BR2013 LIGHT BOEING 737 7373T0 1384582 NM ROW 1-6 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP AT ROWS 1 THRU 6. REPAIRED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999060400042 19990604 00042 NM 1999 6 4 HNAA9900060 1 19990527 A 3350 1155591 LIGHT GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 923HA 30238 099 RT FWD SIDEWALL EXIT SIGN FELL DOWN. REMOVED AND REPLACED EXIT SIGN OPS. CHECK GOOD. 2 H 7 2 4T RT A13NM 1999060400043 19990604 00043 WP 1999 6 4 AT9900411 1 19990520 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 236-308 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE CABIN FLOOR PANEL NR 29 AT BS 236-308 RBL 1-24 CORRODED ON MOST OF FACE AND SPOTS ON BACKSIDE OF HAT SECTION REINFORCEMENTS. CUT OUT NEW SKIN AND HAT REINFORCEMENT SECTIONS. DRILL, T RIMMED, ASSEMBLED, TREATED, PRIMED, INSTALLED NEW INSULATION AND EDGE STRIPS IAW DC9 SRM 51-10-3, 51-30-2, 51-70-0 AND 5 3-21-0. 2 L 7 2 4F A6WE 1999060400044 19990604 00044 WP 1999 6 4 AT9900412 1 19990521 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 196 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD HORIZONTAL FLANGE OF LATERAL FLOOR SUPPORT AT BS 196 LBL 0-22 CORRODED. REMOVED FLOOR SUPPORT, TRIMMED NEW FLOOR SUPPORT, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-10-3, 51-10-2, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999060400045 19990604 00045 WP 1999 6 4 AT9900413 1 19990522 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 351 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD CARGO COMPARTMENT FLOORBEAM TO CUSP LINE AT BS 351 CORRO DED AROUND RIVETS, ASSOCIATED HARDWARE AND STAND OFFS. REMOVED CORROSION, FABRICATED REPAIR DOUBLER, DEBURRED, COUNTERS UNK, TREATED, PRIMED AND INSTALLED DOUBLER ON THE UPPER FLANGE IAW DC9 SRM 53-05 FIG 20A, 51-30-0, 51-30-2 AND 51-10-0. 2 L 7 2 4F A6WE 1999060400046 19990604 00046 WP 1999 6 4 AT9900414 1 19990522 A 5320 4911363504N FITTING DOUG DC9 DC932 3022066 WP BS 903 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT SIDE CUSP AT BS 903 FLOOR FRAME FITTING CORRODED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999060400047 19990604 00047 WP 1999 6 4 AT9900415 1 19990525 A 3350 4593 BULB DOUG DC9 DC932 3022066 WP LT NACELLE DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 806AT 47379 FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. RELAMPED LEFT HAND NACELLE EMERGENCY LIGHT IAW MM 33-53-0, OPS CHEC K GOOD. 2 L 7 2 4F A6WE 1999060400048 19990604 00048 WP 1999 6 4 AT9900416 1 19990526 A 5320 RIVET DOUG DC9 DC932 3022066 WP INSTRUMENT PANEL LOOSE A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 821AT 47284 NINETY SECONDS AFTER TAKEOFF A PUFF OF SMOKE CAME OUT NEXT TO THE ALTITUDE REPEATER. RETURNED FOR IMMEDIATE LANDING. R EMOVED LOOSE RIVET THAT WAS TOUCHING THE NOSE TAXI SWITCH. RIVET WAS NOT PART OF THE INTEGRAL GLARESHIELD. 2 L 7 2 4F A6WE 1999060400049 19990604 00049 NM 1999 6 4 CALA9900580 1 19990527 A 3260 CONNECTOR BOEING 727 727232 1384082 NM RT MLG FAILED A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 27783 20638 THE RT MLG RED UNSAFE LIGHT ILLUMINATED STEADILY AT FIRST, AND THEN FLASHED ON AND OFF INTERMITTENTLY WHEN GEAR WAS EXTE NDED ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE TARGETS, SENSORS, AND WIRING WERE VISUALLY INSPECTE D AND CHECKED GOOD. TROUBLESHOOTING THE WIRING IAW MM 32-64-01 AND 32-64-02 FOUND THE D4656P WIRING CONNECTOR AT FAULT. THE D4656P CONNECTOR WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1999060400050 19990604 00050 WP 1999 6 4 CALA9900581 1 19990528 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 120 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 120 ABOVE LONGERON 18L. AN INTERNAL DOUBLER REPAIR WAS INSTALLED IAW SRM 5 3-04, FIGURE 38. 2 L 7 2 4F A6WE 1999060400051 19990604 00051 NM 1999 6 4 UPS99229675 1 19990526 A 5320 69204086 INTERCOSTAL BOEING 727 72725C 138400H NM BS 259-276 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI FLOOR SUPPORT UPPER CHORD CORRODED AT BS 259-276, LBL 8, WL 208. REPLACED INTERCOSTAL IAW SRM 51-30- 2. 2 L 7 3 4F A3WE 1999060400052 19990604 00052 NM 1999 6 4 UPS99229676 1 19990526 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI CORROSION IN SEVERAL PLACES ON FLOORBEAM BS 344, RBL 20 TO LBL 55, WL 208. REMOVED AND REPLACED FLOO RBEAM UPPER CHORD PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999060400053 19990604 00053 NM 1999 6 4 UPS99229677 1 19990526 A 5712 651624925 RIB BOEING 727 72725C 138400H NM WS 491 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI L/W FUEL TANK RIB UPPER CHORD AT WS 491, STR 15 IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED RI B UPPER CHORD PER BAC DWG 65-16249. 2 L 7 3 4F A3WE 1999060400054 19990604 00054 NM 1999 6 4 UPS99229678 1 19990525 A 5520 65242907 FITTING BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI RT ELEVATOR TAB CRANK O/B RIG PIN HOLE LUG IS CRACKED. REMOVED AND REPLACED FITTING IAW OVERHAUL MAN UAL 55-20-01. 2 L 7 3 4F A3WE 1999060400055 19990604 00055 NM 1999 6 4 UPS99229679 1 19990525 A 5713 STRINGER BOEING 727 72725C 138400H NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI CRACKED TAB ON LEFT WING STRINGER 14. REPAIRED PER SRM 57-10-4 FIGURE 8, SHEET 2. 2 L 7 3 4F A3WE 1999060400056 19990604 00056 NM 1999 6 4 UPS99229680 1 19990525 A 5520 69191441 STIFFENER BOEING 727 72725C 138400H NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI RT ELEVATOR T/E DOUBLER (STIFFENER) AT TAB ROD CUTOUT IS CRACKED. REMOVED AND REPLACED DOUBLER (STIF FENER) IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999060400057 19990604 00057 NM 1999 6 4 UPS99229681 1 19990525 A 5311 FRAME BOEING 727 72725C 138400H NM BS 277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI CRACK ON FRAME AT STA 277 ABOVE STR 16R. REPAIRED STA 277 FRAME AT STR 15R AND 16R IAW SRM 51-40-02. 2 L 7 3 4F A3WE 1999060400058 19990604 00058 NM 1999 6 4 UPS99229683 1 19990527 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM PASSENGER DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 210UP 21697 MAIN ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, P/N ON AND OFF 10-00 67-9 S/N OFF 5200 S/N ON 27025. OPS CHECK GOOD PER MM 33-50-01. 2 L 7 3 4F A3WE 1999060400059 19990604 00059 NM 1999 6 4 UPS99229684 1 19990527 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 210UP 21697 COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD PER MM 33-50-01, P/N ON AND OFF 10-0067-9 S/N OFF 28158 S/N ON 28163. 2 L 7 3 4F A3WE 1999060400060 19990604 00060 WP 1999 6 4 UPS99829685 1 19990528 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 LOWER PIT DOOR 33 CRACKED AT LOWER END OF REPAIR BELOW HANDLE. REPAIRED CRACKED DOOR SIN OF NR 3 PIT DOOR IAW SRM 52-2- 0. 2 L 7 4 4F RT 4A25 1999060400061 19990604 00061 NM 1999 6 4 QXEA9901071 1 19990521 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 4026 496 SEA - COCKPIT OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE OVERHEAD LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999060400062 19990604 00062 NM 1999 6 4 QXEA9901072 1 19990521 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 361PH 516 SEA - TWO FLOOR EMERGENCY PATH LIGHTS INOP. MAINTENANCE REPLACED TWO EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999060400063 19990604 00063 NM 1999 6 4 QXEA9901073 1 19990522 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PASSENGER DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 GEG - THE MAIN CABIN DOOR OPERATION HANDLE IS HARD TO MOVE, HANGS UP DURING OPERATION. MAINTENANCE CLEANED AND LUBRICAT ED THE DOOR STOPS AND PIVOT POINTS. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999060400064 19990604 00064 NM 1999 6 4 QXEA9901074 1 19990526 A 3241 427911A CONTROL BOX DHAV DHC8 DHC8102 2809003 NM ANTISKID SYST MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 815PH 50 PDT- NR 1 MAIN WHEEL LOST BRAKING WHILE PARKING. STOPPED AIRCRAFT WITH THE PARKING BRAKE. AIRCRAFT WAS FERRIED FROM PD T-PDX FOR REPAIRS. IN PDX, MAINTENANCE REPLACED THE ANTI-SKID CONTROL BOX. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999060400065 19990604 00065 NM 1999 6 4 QXEA9901075 1 19990524 A 3234 5352011 SELECTOR DHAV 574205 DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTION A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 351PH 490 SEA - AFTER TAKEOFF MAIN LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. AIRCRAFT WAS FERRIED FROM SEA-PDX, WHERE THE COCKPIT SELECTOR PANEL AND SELECTOR VALVE WERE REPLACED. OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999060400066 19990604 00066 NM 1999 6 4 99FDEA00195 1 19990528 A 5312 6517508211 BULKHEAD WEB BOEING 727 727247 138408F NM BS 1342 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 WHILE WORKING W/C 7-5430-7-2303L1 PT 6 DISCOVERED CRACK IN THE BS 1342 BULKHEAD WEB AT WL 252, LBL 17. *S/D* REMOVED A ND REPLACED BULKHEAD WEB PER IAW FEDEX EA 7-5310-45235. 2 L 7 3 4F A3WE 1999060400067 19990604 00067 NM 1999 6 4 99FDEA00196 1 19990528 A 5311 6516349134 FRAME BOEING 727 727247 138408F NM BS 1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-111-01,3) ON I/B FRAME FLANGE AT BS 1166, STR 17R. *S/D* REMOVED AND REPLACED FRAME PER FEDEX EA 7-5310 -45249. 2 L 7 3 4F A3WE 1999060400068 19990604 00068 NM 1999 6 4 99FDEA00197 1 19990528 A 5311 6516348137 FRAME BOEING 727 727247 138408F NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-111-01,3) ON FRAME AT BS 1148, LBL 24 AND LBL 29, WL 161. *S/D* REMOVED AND REPLACED DAMAGE FROM FRAME, ACCOMPLISH SSI INSP AND FAB AND INSTALLED PARTS IAW FEDEX EA 7-5310-45290. 2 L 7 3 4F A3WE 1999060400069 19990604 00069 NM 1999 6 4 99FDEA00198 1 19990529 A 2751 25141D TRANSMITTER BOEING 727 72722 1384002 NM RT TE FLAP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 189FE 19082 99-121 - ON ROTATION, STICK SHAKER ACTUATED, 2ND REPEAT WRITE UP. REMOVED AND REPLACED RIGHT INBD FLAP TRANSMITTER PER MM 27-52-001 OPER CK GOOD. 2 L 7 3 4F A3WE 1999060400070 19990604 00070 WP 1999 6 4 99FDEA00199 1 19990529 A 3260 TARGET DOUG DC10 DC1010F 3022111 WP LT MLG MISSING A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 385FE 46619 99-122 - AFT T/O DFW LEFT GEAR UNSAFE LIGHTS REMAIN ON BOTH PNLS, RAN RED TABS RETURN DFW. FOUND TARGET MISSING. REPLA CED TARGET AND CHECKED REF MM 32-34-03-2 AND EA 8-3260-45056. OPS TEST GOOD. OK FOR SERVICE. 2 L 7 3 4F A22WE 1999060400071 19990604 00071 WP 1999 6 4 ABXA9900384 1 19990526 A 3230 113965650 VALVE DOUG DC8 DC861 3021952 WP LT MLG LEAKING A ABXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 846AX 373 46158 APPROXIMATELY 30 MINUTES INTO FLIGHT, AT CRUISE FLT LEVEL, LOST FLUID FROM HYDRAULIC SYSTEM TO JUST ABOVE STAND-PIPE LE VEL. INITIATED EMERGENCY HYDRAULIC PROCEDURES. REPLACED LEFT MAIN GEAR BOGIE TRIM CYLINDER IAW DC8 MM. OPS CHECKED GO OD. 2 L 7 4 4F 4A25 1999060400072 19990604 00072 NE 1999 6 4 SCNA99077 2 19990523 A 7200 SEAL BOEING 727 727225 1384077 NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE FAILED A SCNA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 282SC 42018 1078 22558 707177 ENGINE NUMBER ONE SHUTDOWN DUE TO LOW OIL PRESSURE AND QUANTITY. LOSS OF OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE A ND RISE OF OIL TEMPERATURE. ENGINE REDUCED TO IDLE PRIOR TO SHUTDOWN. FOUND ENGINE BEARING SEAL LEAKING AND EVIDENCE O F OIL FOUND IN THE EXHAUST SECTION. 2 L 7 3 4F 4 F A3WE E2EA 1999060400073 19990604 00073 NM 1999 6 4 SCNA99076 1 19990521 A 2611 SMOKE DETECTOR BOEING 727 7272J4 1384006 NM LAVATORY INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE AFT RIGHT LAVATORY SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACE D THE SMOKE DETECTOR. OPERATIONALLY CHECK GOOD. 2 L 7 3 4F RT A3WE 1999060400074 19990604 00074 SO 1999 6 4 SWIA971482 1 19990506 A 3260 BULB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 578SW 120346 RIGHT AB AND LEFT A SYSTEM LIGHTS OUT. WOULD NOT TEST. RETURNED TO SFO. REPLACED LAMPS IN GREEN INDICATOR. LIGHTS CH ECK OK ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999060400075 19990604 00075 SO 1999 6 4 SWIA971483 1 19990508 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 288SW 120316 CABIN ALTITUDE CLIMBS IN AUTO, OK IN MANUAL. RETURNED TO SFO. REPLACED AUTO CONTROLLER. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999060400076 19990604 00076 SO 1999 6 4 SWIA971484 1 19990509 A 2750 ROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT TE FLAP SEIZED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 AFTER TAKEOFF FROM SUN, OUTBOARD PAIR OF FLAPS DISAGREED WITH OTHERS. SLIGHT CONTROLABILITY PROBLEM. AFTER RUNNING QR H PROCEDURES, FLAPS WERE STILL DOWN. DIVERTED TO TWF. INSPECTED RIGHT OUTBOARD FLAP. FOUND OUTBOARD UPPER ROLLER SEIZ ED. SPRAYED PENETRATING FLUID ON ROLLER AND WORKED ROLLER FREE. CYCLED FLAPS FIVE TIMES WITH NO FAULTS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999060400077 19990604 00077 1999 6 4 SWIA971485 4 19990505 A 3442 6222504001 ANTENNA EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RADAR SYST FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 204SW 120243 WEATHER RADAR FAILED EN ROUTE TO EKO. CONTINUED TO SLC DUE TO WEATHER IN EKO. UNIT TESTS OK BUT DISPLAYS NO WEATHER ON GROUND. RADAR RETURNED ON DESCENT INTO SLC AND STARTED PAINTING WEATHER AGAIN. REPLACED RADAR ANTENNA ASSEMBLY. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999060400078 19990604 00078 WP 1999 6 4 RRXA99802 1 19990525 A 3231 MECHANISM DOUG DC8 DC873F 302199F WP MLG DOOR LACK OF LUBE A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 961R 46133 AFTER T/O MAIN CARGO DOORS FAILED UPLATCH CK RAN CHECKLIST WITH NO HELP RETURN TO DAY AS PER OPS AND MX CONTROL. PERFOR MED OP CK OF MLG DOOR FLT LOCKS, LUBED FLT LOCK, MLG DOOR UPLATCH CK OPS CKS NORMAL AT THIS TIME COULD NOT DUPLICATE ON GROUND NO LEAKS OR DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999060400079 19990604 00079 WP 1999 6 4 RRXA99803 1 19990520 A 3230 CONTROL CABLE DOUG DC8 DC863F 302198F WP LANDING GEAR UNSECURE A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 921R 46145 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. NO ATTEMPT AT HANDLE LATCH FLIGHT RELEASE. FOUND LANDING GEAR ANTI RETRA CTION CABLE NOT SECURE, SECURED SAME LDG GEAR HANDLE AND GEAR OPS NORMAL ON GRD CK. 2 L 7 4 4F 4A25 1999060400080 19990604 00080 WP 1999 6 4 RRXA99804 1 19990519 A 2910 PACKING DOUG DC8 DC862F 3021972 WP HYDRAULIC LINE MISSING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 997CF 46154 HYDRAULIC OIL LOW LIGHT CAME ON HYDRAULIC QUANTITY DECREASING, RESERVOIR LOW PRESSURE LIGHT ON. EMERGENCY PROCEDURE INI TIATED. EMERGENCY DECLARED. FOUND HYD LINE MISSING PACKING REPLACED PACKING RAN ENGINES AND AUX PUMP. NO LEAKS NOTED , OPS NORMAL. 2 L 7 4 4F 4A25 1999060400081 19990604 00081 SO 1999 6 4 C2XA99IA209 1 19990401 A 5320 BEAM EMB 145 EMB145 SO FRAME 20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED THE AFF ECTED OMEGA BEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999060400082 19990604 00082 SO 1999 6 4 C2XA99IA208 1 19990401 A 5320 14522459001 SUPPORT EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED SUPPORT IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999060400083 19990604 00083 SO 1999 6 4 C2XA99IA207 1 19990401 A 5530 14531597602 ANGLE EMB 145 EMB145 SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL FIN TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SECTION OF DRAG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC533 0-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999060400084 19990604 00084 SO 1999 6 4 C2XA99IA206 1 19990401 A 5530 14531597601 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL FIN TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMO VED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999060400085 19990604 00085 SO 1999 6 4 C2XA99IA205 1 19990401 A 5230 14522493001 SKIN EMB 145 EMB145 SO CARGO DOOR CREASED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13935 145022 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR SKIN WAS FOUND TO CREASED. MAINTENANCE REPAIRED THE DOOR SKIN AND APPLI ED A DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5230-01056, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999060400086 19990604 00086 EU 1999 6 4 C2XA99IA204 1 19990402 A 3397 3351108CF24 WIRE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14825 170 IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER STAIR WAS FOUND TO BE INOPERATIVE. MAINTENANC E REPAIRED A BROKE WIRE ON THE TOP STEP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400087 19990604 00087 EU 1999 6 4 C2XA99BT024 1 19990409 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU ROW 18 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 11835 194 BTV - DURING WEEKLY CHECK ON RON, FOUND AFT REAR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT LOCATION 18WL AND OPS CHECKED EMERGENCY LIGHTS GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400088 19990604 00088 SO 1999 6 4 C2XA99BT026 1 19990415 A 3350 BULB EMB 145 EMB145 SO LT EXTERIOR LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15926 145005 BTV - DURING 4A INSPECTION, FOUND LEFT OUTSIDE EMERGENCY LIGHT INOPERATIVE, FORWARD OF THE WING. MAINTENANCE RESECURED LIGHT BULB IN LEFT, FORWARD OUTSIDE EMERGENCY LIGHT SOCKET. OPS CHECKED LIGHTS GOOD. (M) 2 L 7 2 4F RT T00011AT 1999060400089 19990604 00089 CE 1999 6 4 C2XA99CL029 1 19990412 A 7120 1149800218 TRUSS BEECH 1900 1900D 1154162 CE RT ENGINE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 81536 UE152 CLE - THE ORIGINAL SDR FILED ON 3/3/99, REPORTED THAT THE RIGHT ENGINE TRUSS ASSEMBLY ATTACHMENT BOLT WAS MISSING, CAUSI NG CHAFED DAMAGE TO THE TRUSS TO WING ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD UPPER KEEL IAW B 1900 SRM 51-40-02 AND 51-40-04. THE TRUSS ASSEMBLY WAS REMOVED AND REPLACED FOR PRECAUTIONARY MEASURES IAW B1900 MM 71- 20-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1999060400090 19990604 00090 SO 1999 6 4 C2XA99CL033 1 19990417 A 3230 RETRACT MECH EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12715 120125 CLE - FLT 3052 - CREW REPORTED THAT AFTER TAKEOFF THEY WERE UNABLE TO RETRACT THE LANDING, QRH ITEMS WERE PERFORMED BUT THE LANDING GEAR STILL FAILED TO RETRACT. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECT ED AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS IAW EMB-120 MM 32-30-00 WITH NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400091 19990604 00091 SO 1999 6 4 C2XA99BT027 1 19990420 A 3350 110049 BATTERY CHARGER EMB 145 EMB145ER SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 09 15948 145056 EWR - FLT CO 4090 - CREW REPORTED LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED NR 4 BATTERY CHARGER ASSY. OPS CHECKED, SYSTEM GOOD. ACFT TT: 2,213.2 HOURS. ACFT CYCLES: 1,817. (X) 2 L 7 2 4F RT T00011AT 1999060400092 19990604 00092 SO 1999 6 4 C2XA99CL030 1 19990401 A 3234 12038594001 SELECTOR EMB 120 EMB120RT SO LANDING GEAR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 17728 12086 120179 120182 CLE - FLT 3349 - CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR GREEN 'A' LIGHT REMAINED ILLUMINATED AFTER TAKEOFF, HAD TO USE ELECTRICAL OVERRIDE TO EXTEND THE GEAR. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW EMB-120 MM 32-31-03, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB -120 MM 32-30-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400093 19990604 00093 SO 1999 6 4 C2XA99CL031 1 19990401 A 2150 17185613 HOSE EMB 120 EMB120RT SO RIGHT PACK TORN A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 34712 120111 CLE - FLT 3176 - CREW REPORTED THAT DURING THE BEFORE ENGINE START CHECK LIST THE CAIBN PRESSURE BUMPED UP AND DOWN ASSO CIATED WITH A LOUD SQUEAL FROM THE RIGHT PACK, AND THEN THE CABIN FILLED WITH SMOKE. MAINTENANCE REMOVED AND REPLACED A HOSE ON THE RIGHT PACK IAW SB 120-210048, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-120 MM 21-50-00 AND 21-60-00. A IRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400094 19990604 00094 EU 1999 6 4 C2XA99IA225 1 19990404 A 5311 S53372411202 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 29 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON FRAME 29 BELOW PANEL NR 241DF. REMOVED CORROSION, FAB RICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-25-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400095 19990604 00095 EU 1999 6 4 C2XA99IA226 1 19990404 A 5311 S53672106200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON FRAME 36 AT SERVICE DOOR. REMOVED CORROSION, FABRICAT ED AND INSTALLED REPAIR DOUBLER IAW SRM 53-61-40. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400096 19990604 00096 EU 1999 6 4 C2XA99IA227 1 19990404 A 5320 S53971402260 WEB AEROSP ATR42 ATR42320 8680930 EU FRAME 27 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON WEB AT FRAME 27A BETWEEN LBL 16 AND RBL 16. REPAIRED IAW SRM 53- 91-43. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400097 19990604 00097 EU 1999 6 4 C2XA99IA228 1 19990404 A 5330 S5337300020000 PLATE AEROSP ATR42 ATR42320 8680930 EU FRAME 36-37 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON PLATE BETWEEN FRAMES 36 AND 37 AT STRINGER 14R. REPLA CED THRESHOLD PLATE IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400098 19990604 00098 EU 1999 6 4 C2XA99IA229 1 19990404 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON RIGHT INBOARD SEAT TRACK FROM FRAME 36 TO 39. REPLACE D SEAT TRACK IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400099 19990604 00099 EU 1999 6 4 C2XA99IA230 1 19990404 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON LEFT INBOARD SEAT TRACK FROM FRAME 36 TO 39. REPLACED SEAT TRACK IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400100 19990604 00100 EU 1999 6 4 C2XA99IA231 1 19990404 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 31-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON SEAT TRACK RBL 38 AT FRAME 31 TO 36. REMOVED AND REPL ACED SEAT TRACK IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400101 19990604 00101 EU 1999 6 4 C2XA99IA232 1 19990404 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 33 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON SEAT TRACK LBL 13 AT FRAME 33. REPLACED DAMAGED SECTI ON OF SEAT TRACK IAW SRM 53-53-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400102 19990604 00102 EU 1999 6 4 C2XA99IA233 1 19990404 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 39-41 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND CORROSION ON SEAT TRACK LBL 6 BETWEEN FRAMES 39 AND 41. REMOVED AN D REPLACED SEAT TRACK IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400103 19990604 00103 SO 1999 6 4 C2XA99IA234 1 19990321 A 5330 12019229001 SKIN EMB 120 EMB120RT SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED FOUR PLACES UNDER PANEL NR 198. BLENDED GOUGE S AND INSTALLED RIVETS IAW EC5330-01042 AND DER REPORT NR 99-045. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400104 19990604 00104 EU 1999 6 4 C2XA99IA216 1 19990410 A 3234 F96GA0102 SELECTOR AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 86842 286 IAH - FLT 3254 - THE CREW REPORTED THAT THE MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE CREW RETURNED THE AI RCRAFT TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR CONTROL LEVER IAW ATR -42-320 MM 32-31-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 1999060400105 19990604 00105 SO 1999 6 4 C2XA99IA215 1 19990408 A 3260 922AAZYA6PZ722 SWITCH EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 09 17728 120182 IAH - FLT 3649 - THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR SYSTEM 'B' RED INDICATION LIGHT CAME ON INTERMITTENTL Y DURING FLIGHT. MAINTENANCE PLACED THE 'B' SYSTEM INDICATION ON MEL AND ON 4-10-99 ADJUSTED THE LEFT MAIN GEAR 'B' SYS TEM UPLOCK PROX SWITCH IAW EMB-120-ER MM 32-01-01. THE 'B' SYSTEM INDICATION WAS REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400106 19990604 00106 SO 1999 6 4 C2XA99IA214 1 19990407 A 3260 922AAZYA6PZ722 SWITCH EMB 120 EMB120RT SO RT MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 17728 120182 LRD - FLT 3668 - THE CREW REPORTED THAT DURING LANDING GEAR RETRACTION THE SYSTEM 'A' GREEN LIGHT INDICATION FOR THE RIG HT MAIN LANDING GEAR REMAINED ON AND ALL GEAR WOULD NOT EXTEND AFTER ATTEMPTING TO RECYCLE THEM. THE CREW MANUALLY EXTE NDED THE GEAR AND RETURNED TO LRD WITHOUT INCIDENT. AFTER FERRYING THE AIRCRAFT TO IAH. MAINTENANCE REMOVED AND REPLAC ED THE RIGHT MLG DOWNLOCK SYSTEM 'A' PROX SWITCH IAW EMB-120-ER MM 32-61-01, 32-30-00. THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400107 19990604 00107 SO 1999 6 4 C2XA99IA213 1 19990407 A 3350 12030712509 LIGHT EMB 120 EMB120RT SO ROW 10 OUT OF POSITION A C2XA K NONE O OTHER UK UNKNOWN 1 SW 09 27716 120128 IAH - FLT 202A, THE CREW REPORTED THAT THE RIGHT AFT EMEGENCY EXIT AT ROW 10 WOULD NOT OPEN PROPERLY DUE TO THE OVERHEAD TRIM BLOCKING THE DOOR. MAINTENANCE RESECURED THE OVERHEAD LIGHTING CHANNEL TRIM AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400108 19990604 00108 SO 1999 6 4 C2XA99BT029 1 19990422 A 3350 3025101 LIGHT EMB 145 EMB145ER SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12946 145052 BTV - DURING 2A INSPECTION, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT OVER LEFT HAND WING INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY OVER THYE LEFT HAND WING AND OPS CHECKED, SYSTEM GOOD. (X) 2 L 7 2 4F RT T00011AT 1999060400109 19990604 00109 EU 1999 6 4 C2XA99BT028 1 19990422 A 3260 141FL01D3 SWITCH AEROSP ATR42 ATR42320 8680930 EU RIGHT MLG FAILED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 18814 103 EWR - FLT CO3487 - CREW REPORTED RIGHT MAIN LANDING GEAR UNLOCK LIGHT ILLUMINATED ON RETRACTION. MAINTENANCE REMOVED AN D REPLACED RIGHT LANDING GEAR LIMIT SWITCH IAW 32-61-00-RAI-10010-002. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400110 19990604 00110 SO 1999 6 4 C2XA99CL036 1 19990423 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16724 15871 0893 120171 CLE - FLT 3611 - CREW REPORTED THAT THEY RECEIVED A FLAP CONTROL FAULT THAT WOULD NOT RESET AFTER TAKEOFF. AIRCRAFT RET URNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP ACTUATOR IAW EMB- 120 MM 27-50-09, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999060400111 19990604 00111 GL 1999 6 4 C2XA99CL035 2 19990422 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15932 2684 145015 CAE310095 CLE - DURING A SCHEDULED BORESCOPE INSPECTION THE RIGHT ENGINE HIGH PRESSURE TURBINE BLADE TRACK WAS FOUND TO HAVE SEVER AL BURN HOLE THAT WERE BEYOND MANUFACTURE LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXP RESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999060400112 19990604 00112 CE 1999 6 4 C2XA99CL034 1 19990421 A 7120 MS2000618 BOLTS BEECH 1900 1900D 1154162 CE LT ENGINE LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 87550 UE205 AZO - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE LOWER TRUSS ATTACHMENT BOLTS WERE FOUND TO BE LOOSE. MAINTENANCE R EMOVED AND REPLACED THE LEFT ENGINE LOWER TRUSS ATTACHMENT BOLTS IAW CONTINENTAL EXPRESS ENGINEERING AUTHORIZATION NR 71 20-01018. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1999060400113 19990604 00113 EU 1999 6 4 C2XA99BT033 1 19990427 A 3350 CONNECTOR AEROSP ATR72 ATR72212 EU CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69902 385 BTV - DURING LINE CHECK MAINTENANCE, FOUND EMERGENCY LIGHTS DID NOT PASS CHECK. RESECURED CANNON PLUG AT LOCATION 73WL POWER SUPPLY. OPS CHECKED EMERGENCY LIGHT SYSTEM, GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400114 19990604 00114 SO 1999 6 4 C2XA99BT030 1 19990427 A 3350 7287103507 CONTROL MODULE EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 14939 145030 BTV - CREW REPORTED EMERGENCY LIGHTS WOULD NOT TEST FROM FLIGHT ATTENDANTS PANEL. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL MODULE AND OPS CHECK EMERGENCY LIGHTS GOOD. (M) 2 L 7 2 4F RT T00011AT 1999060400115 19990604 00115 EU 1999 6 4 C2XA99BT031 1 19990427 A 3350 44 BULBS AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 BTV - DURING WEEKLY CHECK, FOUND GROUND ILLUMINATION LIGHTS UNDER LEFT AND RIGHT FORWARD EMERGENCY EXITS AND IN PASSENGE R DOOR INOPERATIVE. REMOVED AND REPLACED BULBS AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400116 19990604 00116 EU 1999 6 4 C2XA99BT032 1 19990425 A 3350 BULB AEROSP ATR72 ATR72212 EU EXTERIOR LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69902 385 BTV - DURING LINE CHECK, MAINTENANCE FOUND AFT RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RESECURED BULB IN RIGHT AFT EXTERIOR EMERGENCY LIGHT. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400117 19990604 00117 EU 1999 6 4 C2XA99BT025 1 19990411 A 3320 LIGHT AEROSP ATR42 ATR42320 8680930 EU ROW 2AB FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 17831 185 EWI - FL CO3549 - CREW REPORTED DURING TAXI STRON BURNING ODOR NOTICED THROUGH OUT CABIN AND COCKPIT. SMELL INTENSITY I NCREASED THROUGHOUT TAXI AND RETURN TO GATE. FOUND SIDEWALL LIGHT SOCKET AT SEAT ROW 2AB BURNED. REMOVED AND REPLACED SOCKET WITH SERVICEABLE UNIT OPS CHECKED LIGHTING GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400118 19990604 00118 SO 1999 6 4 C2XA99CL032 1 19990404 A 3234 12038594001 SELECTOR EMB 120 EMB120RT SO LANDING GEAR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 17728 120067 120182 CLE - FLT 3141 - CREW REPORTED THAT THE LANDING GEAR INDICATION WITH GEAR UP WAS 1 GREEN, ELECTRICAL OVERRIDE PROCEDURES USED TO EXTEND THE GEAR. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED TH E LANDING GEAR CONTROL HANDLE IAW EMB-120 MM 32-31-03, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERV ICE. (M) 2 L 7 2 4T RT A31SO 1999060400119 19990604 00119 NE 1999 6 4 USAAD99056 2 19990416 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RIGHT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 830US 39462 49443 708454 RSW-PIT - FLT 352 - WHILE CLIMBING THROUGH 15,000 FEET THE RIGHT ENGINE EGT WAS 80 DEGREES HIGHER THAN THE LEFT AND THE FUEL FLOW WAS 1,000 LBS PER HOUR HIGHER. THE AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. AN OVERWEIGHT LAND INSPECTION WAS PERFORMED. THE RIGHT ENGINE FUEL CONTROL WAS REPLACED BUT DID NOT CURE THE PROBLEM. THE AIRCRAFT WAS FE RRIED TO THE MAINTENANCE BASE FOR TROUBLESHOOTING. THE RIGHT ENGINE WAS REPLACED. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999060400120 19990604 00120 NM 1999 6 4 USAASB99108 1 19990423 A 7722 EGT INDICATION BOEING 737 737401 1384701 NM NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 407US 23877 SDF - FLT 1266 - EN ROUTE FROM MCI-DCA, AT FL330, THE NR 1 ENGINE EGT WAS ON THE RISE AND WENT TO FULL SCALE WITH RED EG T OVERTEMP LIGHT ILLUMINATING. FUEL FLOW, OIL PRESSURE AND OIL TEMPERATURE WERE ALL NORMAL. DIGITAL TEMPERATURE INDICA TOR WENT BLANK. CREW ACCOMPLISHED CHECKLIST AND DECIDED TO DIVERT TO SDF. NO EMERGENCY WAS DECLARED AS EGT GAUGE BECAM E NORMAL WHILE DESCENDING TO SDF. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED INTERFACE T ERMINAL BLOCK. INSPECTED ENGINE AND WIRING AND RAN ENGINE. COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 2 4F RT A16WE 1999060400121 19990604 00121 NE 1999 6 4 USAAD99057 2 19990416 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LEFT FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 970VJ 47050 654986 DTW - PILOT RECORDED IN LOG BOOK THAT THE CABIN CREW HEARD A LOUD NOISE FROM THE LEFT SIDE OF THE AIRCRAFT. NO IRREGULA RITIES WERE REPORTED FOR ENGINE READINGS. MAINTENANCE FOUND PARTS OF THE COWLING SKIN BLOW OUT NEAR THE 12 O'CLOCK POSI TION. A 3 FT BY 6 INCH HOLE IN THE FAN DISCHARGE FRONT OUTER DUCT AT THE 2 TO 5 O'CLOCK POSITION WAS FOUND. THE ENGINE WAS REPLACED. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999060400122 19990604 00122 WP 1999 6 4 USAA990333 1 19990330 A 5320 CUSP DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922VJ 42939 48142 PIT - DURING Q-1 CHECK, FOUND 2 INCH CRACK AT STATION 965 LT CUSP MEMBRANE. ROUTED OUT CRACK AND INSTALLED DOUBLER PER EA (PENDING) 51752. (M) 2 L 7 2 4F A6WE 1999060400123 19990604 00123 NM 1999 6 4 USAABB99019 1 19990329 A 3350 20131ALP BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 LAX - FOUND INTERIOR AFT LEFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 1999060400124 19990604 00124 NM 1999 6 4 USAASB99098 1 19990409 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM ROW 20 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 560AU 23514 CLT - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROW 20, BULLNOSE AND AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999060400125 19990604 00125 NM 1999 6 4 USAA990310 1 19990414 A 5320 6517688125 ANGLE BOEING 737 737201 1384454 NM BS 344-350 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 45150 22752 CLT - DURING VISUAL CHECK INSPECTION, FOUND A 6 INCH BY 2 INCH AREA OF CORROSION AT BS 344 - BS 350, LBBL 60, WL 208.10 ANGLE BEAM CHORD. REPAIRED DOUBLER PER EA 64341 AND SRM 53-40-3. (M) 2 L 7 2 4F A16WE 1999060400126 19990604 00126 NM 1999 6 4 USAA990311 1 19990413 A 5210 65C27257 DOUBLER BOEING 737 737201 1384454 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 226US 52337 21815 TPA - DURING HFEC CHECK INSPECTION, FOUND A .25 INCH CRACK IN MED REPAIR DOUBLER AFT LOWER CORNER OF MAIN ENTRY DOOR CUT OUT. INSTALLED NEW DOUBLER PER EO 5391G694 AND DRAWING 65C27257. (M) 2 L 7 2 4F A16WE 1999060400127 19990604 00127 NM 1999 6 4 MZZA99067 1 19990410 A 5752 SKIN BOEING 727 727264 138408M NM RT AILERON TAB DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RIGHT WING INBOARD AILERON TAB UPPER SKIN NEAR CENTER HINGE. THE DAMAGED SKIN 2 INCHES BY 2 INCHE IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6 . (M) 2 L 7 3 4F A3WE 1999060400128 19990604 00128 NM 1999 6 4 MZZA99066 1 19990409 A 5753 652163254 SKIN BOEING 727 727264 138408M NM RT TE MID FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BULGED WAS FOUND ON RIGHT WING INBOARD MID FLAP UPPER SKIN AT W BL 140. THE DAMAGED SKIN 2 INCH BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 57-50-04 FIGURE 8. (M) 2 L 7 3 4F A3WE 1999060400129 19990604 00129 NM 1999 6 4 MZZA99065 1 19990409 A 5753 652163254 SKIN BOEING 727 727264 138408M NM RT TE MIDFLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BULGED WAS FOUND ON RIGHT WING INBOARD MID FLAP UPPER SKIN AT W BL 87. THE DAMAGED SKIN 2 INCH BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 57-50-4 FIGURE 8. (M) 2 L 7 3 4F A3WE 1999060400130 19990604 00130 NM 1999 6 4 MZZA99064 1 19990413 A 2750 652469538 DRUM BOEING 727 727264 138408M NM LT TE FLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AIR ASIA, CRACK WAS FOUND ON LEFT WING TE INBOARD AFT FLAP INBOARD CABLE DRU M BRACKET. THE DAMAGED DRUM ASSEMBLY, P/N 65-24695-38 WAS REMOVER AND REPLACED PER MM 27-51-2 AND OPERATIONAL CHECK FOU ND SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999060400131 19990604 00131 NM 1999 6 4 MZZA99063 1 19990409 A 5320 SHEAR TIE BOEING 727 727264 138408M NM BS 950E CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FUSELAGE BS 950E FRAME SHEAR TIE AT S26L . THE CORRODED SHEAR TIE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGURE 13. (M) 2 L 7 3 4F A3WE 1999060400132 19990604 00132 NM 1999 6 4 MZZA99062 1 19990408 A 5330 SKIN BOEING 727 727264 138408M NM BS 970-1010 BUCKLED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BUCKLED WAS FOUND ON AFT FUSELAGE SKIN EXTERNAL SURFACE FROM BS 970 TO BS 1010 AND BETWEEN STRINGER 24L AND STRINGER 25L. THE OIL CANNING SKIN WAS INSTALLED TWO STIFFENER ANGLE PER E C/RA NR 5330-01973. (M) 2 L 7 3 4F A3WE 1999060400133 19990604 00133 NE 1999 6 4 REXA99013 2 19990501 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A REXA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 25 402BH 22668 340A058 GEE367158DK CHIPS LIGHT WARNING WITH ASSOCIATED RISE IN OIL TEMPERATURE ON RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1999060400134 19990604 00134 1999 6 4 GAIA9953 4 19990426 A 2210 2588880901 COUPLER BOEING 727 727223 1384074 NM E/E BAY FAILED A GAIA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 SW 07 855AA 20996 EN ROUTE MCO-MEM - AT FL350, THE LOWER YAW DAMPNER INDUCED A DUTCH ROLL AT .80M. THE CAPTAIN DECLARED AN EMERGENCY AND WAS CLEARED TO FL240. CAPTAIN THEN DISENGAGED THE LOWER YAW DAMPNER AND THE DUTCH ROLL STOPPED. THE CAPTAIN CONTACTED ATC AND INDICATED THAT THE EMERGENCY WAS OVER. THE AIRCRAFT WAS CLEARED TO MEM AND LANDED WITHOUT FURTHER DIFFICULTIES. ON LOGPAGE 1375-18, THE LOWER YAW DAMPNER WAS DEFERRED PER MEL 22-6. THE AIRCRAFT WAS RETURNED TO SERVICE. ON LOGPAG E 1375-21, THE DEFERRED ITEM WAS CLEARED BY REPLACING THE LOWER YAW CHANNEL COUPLER. AN OPERATIONAL CHECK WAS PERFORMED AND WAS FOUND TO BE NORMAL. THE AIRCRAFT WAS AGAIN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999060400135 19990604 00135 NM 1999 6 4 99ZZZM319 1 19990426 A 3350 82510162003 CONTROL BOX DHAV DHC8 DHC8103 1386005 NM CABIN INOPERATIVE A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 803WP 22917 141 FLT 1521 - HNL - EMERGENCY LIGHTS FLICKERED ON AND OFF DURING TAXI. REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL BO X, AND PERFORMED AND OPERATIONAL CHECK OF THE SYSTEM, IAW DASH 8 MM, 33-51-00, PAGE 201-202. SYSTEM CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1999060400136 19990604 00136 EU 1999 6 4 PLGA990416 1 19990416 A 2421 31342001 GENERATOR SAAB SF340 340B 7860101 EU RT ENGINE FAILED A PLGA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 NE 05 348BE 509 340B190 BOS - FLT 6559 - EN ROUTE FROM PWM TO LGA, HAD A/C GEN LIGHT ILLUMINATE SHORTLY AFTER DEPARTURE. FLIGHT COULD NOT CONTI NUE DUE TO WEATHER EN ROUTE AND AIRCRAFT WAS DIVERTED BACK TO BOS. MAINTENANCE FOUND THE RIGHT ENGINE A/C GEN AT FAULT. A/C GENERATOR WAS REPLACED, PERFORMED REQUIRED OPERATIONAL CHECKS AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999060400137 19990604 00137 WP 1999 6 4 ORJA99130 1 19990331 A 3350 6011779 POWER SUPPLY DOUG DC9 DC987 3022087 WP ROW 18 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY SEAT LIGHTING IS OFF AT 18 DEF. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY IAW MM 33. OPS CHECK GOOD . (M) 2 L 7 2 4F RT A6WE 1999060400138 19990604 00138 WP 1999 6 4 ORJA99134 1 19990408 A 3350 BR9661105 CHARGER DOUG DC9 DC982 3022082 WP ROW 8-12 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 LAS - EMERGENCY EXIT LIGHTS AT ROWS 8-12 CAME ON JUST PRIOR TO PUSH BACK. REMOVED AND REPLACED FORWARD RIGHT BATTERY CH ARGER. OPS CHECK OK PER MM 23-11-00. (M) 2 L 7 2 4F A6WE 1999060400139 19990604 00139 WP 1999 6 4 ORJA99132 1 19990325 A 3260 DC6320W27PW CONNECTOR DOUG DC9 DC982 3022082 WP LT MLG FAILED A ORJA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 11 823RA 49889 IN RNO, ABORTED TAKEOFF AT 70 KNOTS, WHEEL NOT TURNING LIGHT ILLUMINATED ON TAKEOFF ROLL. FOUND CANNON PLUG P1-1159 WIT H PIN G BROKEN. REPINNED G. PERFORMED BITE TEST WITH PROX BOX FOR LEFT MAIN WOW SWITCH. OPS NORMAL. (M) 2 L 7 2 4F A6WE 1999060400140 19990604 00140 WP 1999 6 4 ORJA99133 1 19990331 A 3350 6011779 POWER PACK DOUG DC9 DC987 3022087 WP ROW 18 DEF INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY SEAT LIGHTING IS OFF AT 18 DEF. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY IAW MM 33, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400141 19990604 00141 WP 1999 6 4 ORJA99135 1 19990405 A 3350 59306431 BATTERY DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, FORWARD SECTION OF EMERGENCY LIGHTS CAME ON DURING FLIGHT. REMOVED AND REPLACED FORWARD BATTERY AT EMERGENCY LI GHT MODULE IAW MM 33-53-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400142 19990604 00142 WP 1999 6 4 ORJA99136 1 19990407 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC987 3022087 WP GALLEY DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, FORWARD GALLEY EMERGENCY EXIT BATTERY PACK INOPERABLE. REMOVED AND REPLACED GALLEY EMERGENCY EXIT BATTERY PACK IAW 33-21-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400143 19990604 00143 WP 1999 6 4 ORJA99137 1 19990408 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 1-9 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT LAX, EMERGENCY ROW LIGHTS, AIRCRAFT RIGHT, ROWS 1 THROUGH 9, ARE ON WITH SWITCH IN ARM AND OFF. REPLACED BATTERY PAC K LIGHT ASSEMBLY, CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 1999060400144 19990604 00144 WP 1999 6 4 ORJA99138 1 19990409 A 2120 AIR DISTR DOUG DC9 DC987 3022087 WP CABIN SMOKE A ORJA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 11 753RA 49587 AT LAX, CABIN FILLED WITH OIL SMOKE AFTER TAKEOFF, TURNED OFF BOTH PACKS AT 5000 FT, OPENED OUTFLOW VALVE. SMOKE SUBSID ED, LANDED AT LAX. REPLACED SET OF COALESCER BAGS, CLEANED WATER SEPARATORS AND PEFORMED BURNOUT OF HIGH PRESSURE PNEUM ATIC DUCTING AS OUTLINED IN MM 21-20-02, PAGES 209-216. RAN PACKS, NO SMOKE NOTED. (M) 2 L 7 2 4F RT A6WE 1999060400145 19990604 00145 WP 1999 6 4 ORJA99139 1 19990406 A 3350 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY LIGHTING LAST ROW FLOOR LAMP INOPERABLE. REPAIRED EMERGENCY LIGHTING AT LAST ROW SEAT LIGHT IAW MM 20 -50-04. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400146 19990604 00146 WP 1999 6 4 ORJA99140 1 19990415 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 12-16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 SJC - EMERGENCY EXIT LIGHTS ROWS 12-16 INOPERATIVE. REMOVED AND REPLACED LIGHT MODULE EMERGENCY BATTERY PACK IAW MM 33- 53-01. (M) 2 L 7 2 4F RT A6WE 1999060400147 19990604 00147 WP 1999 6 4 ORJA99141 1 19990415 A 3397 00105606003 WIRE DOUG DC9 DC983 3022083 WP ROW 11 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 IN RNO - ESCAPE PATH LIGHT AT ROW 11 IS INOPERATIVE. REPAIRED BROKEN WIRE IAW MM 20-50-01. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400148 19990604 00148 WP 1999 6 4 ORJA99142 1 19990416 A 3350 BR9687100 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 7-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 IN RNO, EMERGENCY LIGHTS INOPERATIVE ROW 7-11. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT EMERGENCY EXIT 20 DEF, SYSTEM OPS CHECK NORMAL PER 33-53-01. (M) 2 L 7 2 4F RT A6WE 1999060400149 19990604 00149 WP 1999 6 4 ORJA99143 1 19990408 A 3350 2AG FUSE DOUG DC9 DC987 3022087 WP ROWS 1-9 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT PDX, FIRST ROWS 1 THROUGH 9, AIRCRAFT RIGHT, EMERGENCY LIGHTS CAME ON IN 'ARM' AND 'OFF' POSITION OF SWITCH. REMOVED AND REPLACED FUSE AT RIGHT EMERGENCY LIGHTS. OPS CHECK NORMAL PER BRUCE INDUSTRIES MM 400-883 AND MM 33-0. (M) 2 L 7 2 4F RT A6WE 1999060400150 19990604 00150 WP 1999 6 4 ORJA99144 1 19990409 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 1/2/3/8 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, EMERGENCY LIGHTS AT ROWS 1, 2, 3, 8, RIGHT SIDE ONLY, ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED FORWARD B ATTERY PACK NEXT TO FORWARD GALLEY DOOR. OPS CHECK NORMAL PER MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 1999060400151 19990604 00151 WP 1999 6 4 ORJA99145 1 19990410 A 3397 WIRE DOUG DC9 DC987 3022087 WP ROWS 1-5 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, EMERGENCY LIGHTS AT ROWS 1 THROUGH 5 ARE ON, WILL NOT TURN OFF. TROUBLESHOT EMERGENCY EXIT LIGHTING SYSTEM FORW ARD GALLEY. RIGHT LIGHT WIRING TO SEATS AT ROW 8 DEF, GROUNDING OUT ON SEAT TRACK AND AIR GRILL. REPAIRED WIRING IAW 2 0-50-01 MM. OPS CHECK GOOD. OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 1999060400152 19990604 00152 WP 1999 6 4 ORJA99146 1 19990410 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 1-5 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AT SJC, EMERGENCY LIGHT AT ROWS 1 THROUGH 5, RIGHT SIDE, ILLUMINATED WILL NOT TURN OFF. REMOVED AND REPLACED FORWARD BA TTERY PACK PER MM 33-53-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999060400153 19990604 00153 WP 1999 6 4 ORJA99149 1 19990415 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 1-9 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, AT SEATS AT ROWS 1 THROUGH 9 EMERGENCY EXIT LIGHTS NOPERATIVE. REMOVED AND REPLACED EMERGENCY PACK, LOCATED IN FORWARD GALLEY AS PER MM 33-24-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400154 19990604 00154 WP 1999 6 4 ORJA99150 1 19990417 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC987 3022087 WP ROW 8D FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT RNO, EMERGENCY LIGHTS AT SEAT 8D INOPERATIVE, SEAT AND CEILING. RELAMPED CEILING LAMPS AND REPLACED FORWARD GALLEY E XIT EMERGENCY LIGHT CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400155 19990604 00155 WP 1999 6 4 ORJA99151 1 19990418 A 3350 BR9661105 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, FIRST EMERGENCY EXIT LIGHTS ON. REMOVED AND REPLACED BATTERY PACK FROM FORWARD GALLEY. OPS CHECK GOOD AS PER 3 3-53-00. (M) 2 L 7 2 4F RT A6WE 1999060400156 19990604 00156 WP 1999 6 4 ORJA99152 1 19990413 A 3350 BR9687100 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 8-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 IN SJC, EMERGENCY LIGHT ROWS 8-11 ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD IAW 3 3-53-00. (M) 2 L 7 2 4F RT A6WE 1999060400157 19990604 00157 WP 1999 6 4 ORJA99153 1 19990415 A 3350 BR9661105 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 6-10 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 IN LAS, EMERGENCY LIGHTS ROWS 6-10 ON. REMOVED AND REPLACED EXIT BATTERY PACK AT FORWARD RIGHT O/W EMERGENCY EXIT PER M M 33-53-00. LIGHTS OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999060400158 19990604 00158 WP 1999 6 4 ORJA99154 1 19990416 A 3350 00105606003 WIRE DOUG DC9 DC983 3022083 WP ROW 8/9 DISCONNECTED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 IN SJC, EMERGENCY PATH LAMP INOPERATIVE AT ROWS 8 AND 9. RECONNECTED BROKEN WIRE AT ROWS 8 AND 9 EMERGENCY PATH LIGHTS IAW 33-24-00, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999060400159 19990604 00159 1999 6 4 ORJA99156 4 19990412 A 3197 WIRE DOUG DC9 DC982 3022082 WP LT MASTER WARN LOOSE A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 821RA 49931 LAS - CAPTAIN MASTER WARNING LIGHT INOPERATIVE. SECURED LOOSE WIRE ON CAPTAIN MASTER WARNING LIGHT OPS CHECK NORMAL PER MM 20-50-04. (M) 2 L 7 2 4F A6WE 1999060400160 19990604 00160 NM 1999 6 4 P2EA99134 1 19990331 A 5230 SKIN BOEING 737 737222 1384473 NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR OUTER SKIN, HANDLE CUTOUT WAS FOUND WITH A CRACK. REPAIRED FCC DOOR OUTER SKIN HANDLE CUTOUT SECTION BETWEEN BS 461 AND BS 474 FROM NR 3 BEAM TO NR 4 BEAM DUE TO CRACK IAW SRM 52-00- 3, FIG 6. (M) 2 L 7 2 4F A16WE 1999060400161 19990604 00161 NM 1999 6 4 P2EA99135 1 19990328 A 5330 SKIN BOEING 737 737222 1384473 NM BS 1008-1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FUSELAGE FROM BS 996 TO BS 1016 ON STRINGERS 6 RT AND 7 RT OUTER SKIN WAS FOUND BULGED. REPAI RED FUSELAGE SKIN BUTT JOINT EXTERNAL SKIN FROM BS 1008 TO BS 1016, BETWEEN STRINGERS 5 RT AND 4RT PER SRM 53-30-3, FIGU RE 28, SHEETS 1, 2, 3, 10 AND 11. CORROSION REMOVED FROM BS 996 TO BS 1008 BETWEEN STRINGERS 5 RT AND 7 RT PER SRM 51-1 0-6. WITHIN LIMITS PER SRM 53-30-1, FIGURE 1. ORIGINAL THICKNESS .072 INCH REMAINING .068 INCH. TREATMENT APPLIED PER SRM 51-10-2. RIVETS REPLACED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999060400162 19990604 00162 NM 1999 6 4 P2EA99136 1 19990327 A 5280 DOOR BOEING 737 737222 1384473 NM LT MLG CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE LEFT MAIN LANDING DOOR SHOCK STRUTS DOOR WS FOUND WITH A CRACK. REPAIRED LEFT MLG SHOCK STRUT DOOR BETWEEN BS 698.80 AND BS 694.80 DUE TO CRACK IAW COOPESA EO C00-3057-219-99 DATED APR 6, 1999 AND BOEING FAX C00-S JO-99-0447RR DATED APR 6, 1999. (M) 2 L 7 2 4F A16WE 1999060400163 19990604 00163 NM 1999 6 4 P2EA99137 1 19990327 A 5313 STIFFENER BOEING 737 737222 1384473 NM BS 540 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, A/C DISTRIBUTION BAY, BS 540, RBL 23, WL 208, STIFFENER WAS FOUND WITH A CRACK. REPLACED FUSELAGE STIFFENER AT BS 540, RBL 23 BETWEEN WL 208 AND WL 152 DUE TO CRACK PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999060400164 19990604 00164 NM 1999 6 4 P2EA99138 1 19990328 A 2750 BELLCRANK BOEING 737 737222 1384473 NM LT TE FLAP WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE LEFT WING OUTBOARD FLAP INBOARD TRACK MOVABLE FAIRING SUPPORT WAS FOUND WITH PLAY AND THE LINK WAS FOUND WITH WEAR. PERFORMED BLENDOUT REPAIR AT LEFT WING OUTBOARD FLAP INBOARD TRACK BELLCRANK SECTION DUE TO WEAR PER COOPESA EO COO-3-57-217-99, DATED APR 7, 1999 AND BOEING FAX COO-SJO-99-0442RR, DATED APR 5, 1999. (M) 2 L 7 2 4F A16WE 1999060400165 19990604 00165 NM 1999 6 4 P2EA99139 1 19990331 A 5730 6550826142 SKIN BOEING 737 737222 1384473 NM WS 114-157 DELAMINATION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE RIGHT WING TRAILING EDGE FIXED PANEL BETWEEN WBL 114 AND WBL 157 WAS FOUND WITH DELAMINATION. REPAIRED WING FIXED PANEL P/N 65-50826-142 PER EO COO-CMP-3-57-215-99, DATED 4-6-99. (M) 2 L 7 2 4F A16WE 1999060400166 19990604 00166 NM 1999 6 4 P2EA99140 1 19990331 A 5755 654645125 SKIN BOEING 737 737222 1384473 NM NR 1 SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE LEFT WING NR 1 SPOILER WAS FOUND WITH DELAMINATION. REPAIRED SPOILER P/N 65-46451-25 PER EO C OO-CMP-3-57-213-99, DATED APR 5, 1999. ASSIGNED SERIAL NUMBER VAG-6 TO SPOILER PART NR 65-46451-25. REPLACED UPPER AND LOWER SKIN AND HONEYCOMB. (M) 2 L 7 2 4F A16WE 1999060400167 19990604 00167 NM 1999 6 4 P2EA99141 1 19990303 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 294.5 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN, FORWARD LAVATORY AREA BS 294.5, LBL 55, FLOORBEAM WAS FOUND CORRODED. REP AIRED FLOORBEAM UPPER CHORD BS 294.5 BETWEEN LBL 59 AND RBL 59 DUE TO CORROSION PER SRM 51-10-1 FIGURE 5, AND UPPER CHOR D SPLICED AT RBL 24 PER SRM 53-10-9, FIGURE 5. (M) 2 L 7 2 4F A16WE 1999060400168 19990604 00168 NM 1999 6 4 P2EA99142 1 19990402 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 986-1016 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FUSELAGE BETWEEN BS 986 AND BS 1016, STRINGER 23L WAS FOUND WITH SEVERAL SMALL CRACKS. REPAIR ED FUSELAGE STRINGER 23 LEFT BETWEEN BS 970 AND BS 1016 DUE TO CRACKS PER SRM 53-10-3, FIGURE 1. FABRICATED STRINGER AN D SPLICE PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999060400169 19990604 00169 NM 1999 6 4 P2EA99143 1 19990403 A 5320 DOUBLER BOEING 737 737222 1384473 NM BS 947-967 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FUSELAGE BETWEEN BS 947 AND BS 967, BETWEEN STRINGERS 24L AND 27L, DOUBLER WAS FOUND WITH CORR OSION. REPLACED FUSELAGE SKIN INTERNAL DOUBLER BETWEEN BS 947 AND BS 967 FROM STRINGER 24 TO 27 LEFT SIDE DUE TO CORROS ION PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999060400170 19990604 00170 NM 1999 6 4 P2EA99144 1 19990327 A 5210 BEAM BOEING 737 737222 1384473 NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FORWARD CARGO DOOR NR 5 BEAM WEB WAS FOUND WITH A CRACK. REPAIRED FORWARD CARGO COMPARTMENT D OOR NR 5 BEAM WEB AFT SECTION DUE TO CRACK PER SB 737-52-1100, SECTION III, FIGURE 6, REVISION 2, DATED MAR 31, 1994. ( M) 2 L 7 2 4F A16WE 1999060400171 19990604 00171 NM 1999 6 4 P2EA99145 1 19990331 A 5730 6550820141 SKIN BOEING 737 737222 1384473 NM WBL 100-180 DELAMINATION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE LEFT WING UPPER SURFACE TRAILING EDGE FIXED PANEL BETWEEN WBL 100 AND WBL 180 WAS FOUND WITH D ELAMINATION. REPAIRED WING FIXED PANEL P/N 65-50820-141 PER EO COO-CMP-3-57-216-99, DATED APR 7, 1999. (M) 2 L 7 2 4F A16WE 1999060400172 19990604 00172 NM 1999 6 4 P2EA99149 1 19990403 A 5320 TEE BOEING 737 737222 1384473 NM BS 927 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE EXTERNAL FUSELAGE, BS 927, BETWEEN STRINGERS 24L AND 25L, 'T' WAS FOUND WITH A CRACK. REPLACE D 'T' AT BS 927 BETWEEN STRINGERS 24 LEFT AND 25 LEFT PER SRM 51-10-1 PAGE 5. RIVETS REPLACED PER SRM 51-30-2. FABRICA TED 'T' PER COOPESA EO COO-3-53-211-99, DATED APR 5, 1999. (M) 2 L 7 2 4F A16WE 1999060400173 19990604 00173 NM 1999 6 4 P2EA99150 1 19990402 A 5320 TEE BOEING 737 737222 1384473 NM BS 947 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE EXTERNAL FUSELAGE BETWEEN STRINGERS 23L AND 24L, BS 947, 'T' WAS FOUND WITH A CRACK. REPLACED 'T' AT BS 947 BETWEEN STRINGERS 23 LEFT AND 24 LEFT PER SRM 51-10-1 PAGE 5, SRM 51-30-2. FABRICATED 'T' PER COOPESA EO COO-3-53-212-99, DATED APR 5, 1999. (M) 2 L 7 2 4F A16WE 1999060400174 19990604 00174 NM 1999 6 4 P2EA99148 1 19990327 A 5330 SKIN BOEING 737 737222 1384473 NM BS 178 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FUSELAGE BS 178 UPPER SECTION LBL 8 OUTER SKIN WAS FOUND WITH MISSING MATERIAL. REPAIRED FUSE LAGE UPPER SKIN SECTION BS 178, LBL 8 PER COOPESA EO COO-3-53-210-99, DATED APR 5, 1999. (M) 2 L 7 2 4F A16WE 1999060400175 19990604 00175 NM 1999 6 4 P2EA99147 1 19990405 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 957-1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, ON THE EXTERNAL FUSELAGE FROM BS 957 TO BS 1016, STRINGER 22L WAS FOUND WITH CORROSION. REPAIRED FUSELAGE NR 22 LEFT STRINGER SECTION BETWEEN BS 952 AND BS 1016 DUE TO CORROSION PER SRM 53-10-03 FIGURE 1. (M) 2 L 7 2 4F A16WE 1999060400176 19990604 00176 NM 1999 6 4 P2EA99146 1 19990402 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 986-1016 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, ON THE EXTERIOR FUSELAGE BETWEEN BS 986 AND BS 1016, STRINGER 21L WAS FOUND WITH SEVERAL SMALL CRA CKS. REPAIRED FUSELAGE NR 21 LEFT STRINGER SECTION BETWEEN BS 973 AND BS 1016 DUE TO CRACKS PER SRM 53-10-3, FIGURE 1. (M) 2 L 7 2 4F A16WE 1999060400177 19990604 00177 WP 1999 6 4 USAAD99053 1 19990408 A 2121 5007025211 FAN DOUG DC9 DC981 3022081 WP CARGO COMPT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 805US 33433 48053 RDU - FLT 1506, AFTER TAKEOFF FROM RDU, THE CREW NOTICED A STRONG ELECTRICAL ODOR. THE FLIGHT RETURNED TO RDU AND LANDE D WITHOUT FURTHER INCIDENT. THE SMELL HAD DISSIPATED PIRO TO LANDING AT RDU. MAINTENANCE FOUND THE CARGO HEAT FAN CIRC UIT BREAKER HAD POPPED. THEY REPLACED THE MID CARGO HEAT FAN. (M) 2 L 7 2 4F A6WE 1999060400178 19990604 00178 NM 1999 6 4 P2EA99151 1 19990403 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 967-1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, STRINGER 25L WAS FOUND WITH CORROSION BETWEEN BS 967 AND BS 1016 AND A CRACK BETWEEN BS 1006 AND B S 1016. REPLACED FUSELAGE STRINGER 25 LEFT BETWEEN BS 967 AND BS 1016 PER SRM 51-10-1 PAGE 5 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1999060400179 19990604 00179 NM 1999 6 4 P2EA99152 1 19990331 A 5753 65719301 SKIN BOEING 737 737222 1384473 NM LT TE FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE LEFT WING OUTBOARD TE FLAP SKIN WAS FOUND WITH DELAMINATION. REPAIRED OUTBOARD FLIPPER FLAP P /N 65-71930-1 PER EO COO-CMP-3-57-214-99 DATED APR 5, 1999. (M) 2 L 7 2 4F A16WE 1999060400180 19990604 00180 NM 1999 6 4 P2EA99153 1 19990407 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 727 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, STRINGER 18 LEFT, AFT CARGO COMPARTMENT, BS 727B PLUS 12, WAS FOUND WITH CORROSION. REPAIRED FUSE LAGE STRINGER 18 LEFT BETWEEN BS 727B PLUS 5 INCHES AND BS 752 DUE TO CORROSION PER SRM 53-10-3 FIGURE 1. FABRICATED AN GLES AND SPLICE PER SRM 51-20-1 AND 51-10-1, PROTECTIVE TREATMENT PER SRM 51-10-2. REMOVED AND REINSTALLED HI-LOCKS AND RIVETS PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999060400181 19990604 00181 NM 1999 6 4 P2EA99154 1 19990327 A 5230 1036541 CASTING BOEING 737 737222 1384473 NM CARGO DOOR DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR OUTER HANDLE CASTING WAS FOUND WITH A HOLE IN IT. REPLACED THE FORWARD CARGO COMPARTMENT DOOR OUTER HANDLE CASTING PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. PERFORMED REMOVAL AND INST ALLATION OF THE CARGO DOOR HANDLE PER MM 52-31-0. (M) 2 L 7 2 4F A16WE 1999060400182 19990604 00182 NM 1999 6 4 P2EA99155 1 19990328 A 5230 BEAM BOEING 737 737222 1384473 NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE AFT CARGO COMPARTMENT DOOR LOWER CROSSBEAM WEB AND OUTER CHORD WAS FOUND CRACKED AT THE AFT LO WER SECTION, DISCOVERED DURING COMPLIANCE WITH VANGUARD EO 993752A002. REPAIRED LOWER CROSSBEAM AND OUTER CHORD IN THE AFT LOWER SECTION OF THE AFT CARGO COMPARTMENT DOOR PER SB 737-52-10-79 SECTION III, PART II, REVISION 5, DATED MAY 16, 1996 AND PART II OF EO 993752A002. (M) 2 L 7 2 4F A16WE 1999060400183 19990604 00183 NM 1999 6 4 P2EA99156 1 19990407 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 344 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN, BS 344, BETWEEN LBL 60 AND RBL 60 FLOORBEAM UPPER CHORD WAS FOUND WITH COR ROSION. REPAIRED FLOORBEAM UPPER CHORD AT BS 344, BETWEEN LBL 65 AND RBL 65 DUE TO CORROSION PER SRM 53-10-9 FIGURE 5. (M) 2 L 7 2 4F A16WE 1999060400184 19990604 00184 NM 1999 6 4 P2EA99157 1 19990407 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 360 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN, BS 360, RBL 13, THE FLOORBEAM UPPER CHORD WAS FOUND WITH CORROSION. REPAI RED FLOORBEAM UPPER CHORD AT BS 360 BETWEEN RBL 5 AND RBL 21 DUE TO CORROSION PER SRM 53-10-9 FIGURE 1. (M) 2 L 7 2 4F A16WE 1999060400185 19990604 00185 NM 1999 6 4 P2EA99158 1 19990327 A 5230 BEAM BOEING 737 737222 1384473 NM CARGO DOOR CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE AFT CARGO COMPARTMENT DOOR, FORWARD NR 5 STOP SECTION AND WEB WERE FOUND CRACKED. REPAIRED AF T CARGO COMPARTMENT DOOR LOWER CROSSBEAM FORWARD SECTION DUE TO CRACK PER SB 737-52-1079, SECTION III, PAR II, REVISION 5 DATED MAY 16, 1996 AND REPLACED THE FORWARD LOWER CORNER DUE TO CORROSION PER SECTION III, PART III OF THE SAME SERVIC E BULLETIN. (M) 2 L 7 2 4F A16WE 1999060400186 19990604 00186 NM 1999 6 4 P2EA99159 1 19990327 A 5730 SKIN BOEING 737 737222 1384473 NM RT WING DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE RIGHT WING UPPER SKIN AT WBL 157 WAS FOUND WITH SPOTFACE DAMAGE. REPAIRED THE RIGHT WING UPPE R SKIN SURFACE AT WBL 157, BETWEEN STRINGER 4 AND STRINGER 6 DUE TO EXISTING SPOTFACES PER COOPESA EO COO-3-57-208-99, D ATED APR 2, 1999 AND BOEING FAX COO-SJO-99-0433RR, DATED APR 1, 1999. (M) 2 L 7 2 4F A16WE 1999060400187 19990604 00187 NM 1999 6 4 P2EA99160 1 19990404 A 5230 FRAME BOEING 737 737222 1384473 NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR FORWARD AND AFT LOWER CORNERS FRAMES WERE FOUND WITH CRACKS. R EPAIRED THE FORWARD CARGO COMPARTMENT DOOR FORWARD AND AFT LOWER CORNERS DUE TO CRACKS PER SB 737-52-1100, SECTION III, FIGURE 3 AND 4, REVISION 2, DATED MARCH 31, 1994. (M) 2 L 7 2 4F A16WE 1999060400188 19990604 00188 NM 1999 6 4 P2EA99161 1 19990405 A 5321 FLOOR BOEING 737 737222 1384473 NM BS 1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN AFT LAVATORY AREA, BETWEEN BS 1016 AND BS 1016 PLUS 11 INCHES, FROM BL 0 TO RBL 36, FLOOR WEB WAS FOUND WITH CORROSION INCLUDING THE SUPPORT ANGLE. REPLACED FLOOR WEB BETWEEN BS 1016 TO BS 1032. 5 FROM BL 0 TO RBL 38 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. SUPPORT ANGLE CORROSION WAS REMOVED, TREATED AND WITHIN L IMITS PER SRM 51-10-6, SRM 51-10-2, AND SRM 53-10-1 FIGURE 1, BETWEEN BS 1016 AND BS 1030, BL 0. ORIGINAL THICKNESS .06 3 INCH, AVERAGE REMOVED .003 INCH. (M) 2 L 7 2 4F A16WE 1999060400189 19990604 00189 NM 1999 6 4 P2EA99162 1 19990405 A 5315 BOEING 737 737222 1384473 NM UNKNOWN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN, AFT LAVATORY AREA, BS 967, BETWEEN RBL 54 AND LBL 54, FLOORBEAM WAS FOUND CORRODED. REPAIRED FLOORBEAM UPPER CHORD BS 967, BETWEEN LBL 12 AND RBL 12 PER SRM 53-10-9 FIGURE 7. CORROSION REMOVED , TREATED, AND WITHIN LIMITS PER SRM 51-10-6, 51-10-2, AND 53-10-1 FIGURE 1 AT BS 967, BETWEEN LBL 12 AND LBL 54, AND BE TWEEN RBL 12 AND RBL 54. ORIGINAL THICKNESS .12 5INCH AVERAGE REMOVED .005 INCH. (M) 2 L 7 2 4F A16WE 1999060400190 19990604 00190 NM 1999 6 4 P2EA99163 1 19990414 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 1016-1024 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, ON THE FUSELAGE AT BS 1016, STRINGER 27L WAS FOUND WITH A CRACK. REPAIRED STRINGER 27L FROM BS 10 16 TO BS 1024 PER SRM 53-10-3, FIGURE 1. (M) 2 L 7 2 4F A16WE 1999060400191 19990604 00191 NM 1999 6 4 P2EA99166 1 19990405 A 5320 INTERCOSTAL BOEING 737 737222 1384473 NM BS 967-987 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN AFT LAVATORY AREA, BETWEEN BS 967 AND BS 987, WL 208.1, RBL 17 INCH, FLOOR SUPPORT (INTERCOSTAL) WAS FOUND WITH CORROSION. REPAIRED FLOOR SUPPORT CHANNEL BETWEEN BS 967 AND BS 987, RBL 17 INCH P ER COOPESA EO COO-3-53-231-99 DATED APR 7, 1999. (M) 2 L 7 2 4F A16WE 1999060400192 19990604 00192 NM 1999 6 4 P2EA99167 1 19990327 A 5320 FRAME BOEING 737 737222 1384473 NM CARGO DOORWAY CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR CUTOUT, STRINGER 20 RIGHT, DOORWAY FRAME WAS FOUND WITH A CRACK AT BS 440. REPLACED THE FORWARD CARGO COMPARTMENT DOOR CUTOUT FRAME AT BS 440, BETWEEN STRINGERS 17 RIGHT AND 28 RIGHT PER SB 737-53-1051, REVISION 5, SECTION III, PART IV DATED FEBRUARY 8, 1990 AND BOEING FAX COO-SJO-99-0440RR, DATED APR 5, 1999. (M) 2 L 7 2 4F A16WE 1999060400193 19990604 00193 NM 1999 6 4 P2EA99168 1 19990402 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 907-1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, AT THE FUSELAGE, BETWEEN BS 967 AND BS 1016, STRINGER 20L WAS FOUND WITH CORROSION. REPLACED STRI NGER 20 LEFT, BETWEEN BS 907 AND BS 1016 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999060400194 19990604 00194 NM 1999 6 4 P2EA99169 1 19990405 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN, AFT LAVATORY AREA, BS 1016, BETWEEN RBL 38 INCH AND LBL 38 INCH, FLOORBEAM WAS FOUND CORRODED. REPAIRED FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN LBL 41 INCH AND RBL 41 INCH PER COOPESA EO COO- 3-53-224-99, DATED APR 8, 1999. (M) 2 L 7 2 4F A16WE 1999060400195 19990604 00195 NM 1999 6 4 P2EA99170 1 19990405 A 5320 INTERCOSTAL BOEING 737 737222 1384473 NM BS 987 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK IN THE PASSENGER CABIN, AFT LAVATORY AREA, BETWEEN BS 987 AND BSL 1016, FROM BL 0 TO LBL 19 INCH, W L 208.1, FLOOR SUPPORTS (INTERCOSTALS) WERE FOUND WITH CORROSION. REPAIRED FLOOR SUPPORT CHANNEL BETWEEN BS 987 AND BS 1006, BL 0 PER COOPESA EO COO-3-53-232-99, DATED APR 9, 1999. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 987 AND BS 1006 , LBL 20 INCH TO LBL 5 INCH PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. REMOVED CORROSION IN FLOOR SUPPORT CHANNEL, TREATE D AND WITHIN LIMITS PER SRM 51-10-6, 51-10-2, AND 53-10-1, FIGURE 1 BETWEEN BS 1006 AND BS 1016, LBL 5 INCH TO BL 0. OR IGINAL THICKNESS .125 INCH AVERAGE REMOVED .004 INCH. (M) 2 L 7 2 4F A16WE 1999060400196 19990604 00196 NM 1999 6 4 P2EA99171 1 19990405 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 987 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN THE PASSENGER CABIN, AFT LAVATORY AREA, BS 987, BETWEEN RBL 47 INCH AND LBL 47 INCH, FLOORBEAM WAS FOUND CORRODED. REPAIRED UPPER CHORD OF FLOORBEAM, BS 987, BETWEEN LBL 51.250 AND RBL 51.250 PER COOPESA EO COO-3-5 3-223-99, DATED APR 8, 1999. (M) 2 L 7 2 4F A16WE 1999060400197 19990604 00197 NM 1999 6 4 P2EA99172 1 19990328 A 5312 BULKHEAD WEB BOEING 737 737222 1384473 NM BS 1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, AT THE AFT CARGO COMPARTMENT AFT PRESSURE BULKHEAD, BS 1016, BETWEEN STRINGERS 26R AND 27R, PRESSU RE BULKHEAD WEB SECTION WAS FOUND WITH CORROSION. REPAIRED PRESSURE BULKHEAD WEB SECTION AT BS 1016, BETWEEN STRINGER 2 6 LEFT AND STRINGER 26 RIGHT DUE TO CORROSION PER COOPESA COO-3-53-234-99, DATED APR 17, 1999 AND BOEING FAX COO-SJO-99- 0469RR, DATED APR 8, 1999. TO PERFORM THE BULKHEAD WEB REPAIR IT WAS NECESSARY TO CUT AND REPAIR THE FUSELAGE SKIN SECT ION BETWEEN BS 1016 AND BS 1035, FROM STRINGER 27 LEFT AND STRINGER 27 RIGHT PER SB 737-53A1075, SECTION III, FIGURE 1, STEP 6, REVISION 2 DATED JULY 13, 1984. (M) 2 L 7 2 4F A16WE 1999060400198 19990604 00198 NM 1999 6 4 P2EA99173 1 19990327 A 5330 SKIN BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE EXTERIOR FUSELAGE SKIN WAS FOUND WITH CRACKS BETWEEN STRINGER 14 LEFT AND STRINGER 16 LEFT AT BS 727A. REPAIRED THE FUSELAGE SKIN SECTION BETWEEN BS 727 AND BS 727B PLUS 15 INCH, FROM STRINGER 14 TO STRINGER 20 LE FT SIDE DUE TO CRACKS PER COOPESA EO COO-3-53-218-99, DATED APR 6, 1999, AND BOEING FAXES COO-SJO-99-0443RR, DATED APR 5 , 1999 AND BOEING FAX COO-SJO-99-0515RR, DATED APR 19, 1999. (M) 2 L 7 2 4F A16WE 1999060400199 19990604 00199 NM 1999 6 4 P2EA99174 1 19990329 A 5330 SKIN BOEING 737 737222 1384473 NM BS 1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, THE FUSELAGE SKIN AT BS 907 AFT WAS FOUND WITH CORROSION, MATERIAL LOSS MORE THAN 15 PERCENT BETWE EN STRINGER 21 LEFT AND 22 LEFT. REPLACED FUSELAGE SKIN PANEL BETWEEN BS 907 AND BS 1016, FROM STRINGER 20 TO STRINGER 25 LEFT SIDE DUE TO CORROSION PER SRM 51-10-1, PAGE 5, AND SRM 51-30-7. (M) 2 L 7 2 4F A16WE 1999060400200 19990604 00200 NM 1999 6 4 P2EA99175 1 19990327 A 5320 BEAM BOEING 737 737222 1384473 NM BS 663.75 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, RIGHT WHEEL WELL, BS 663.75, RBL 68, STRINGER 18A SHEAR BEAM SECTION WAS FOUND WITH A CRACK. REPA IRED RIGHT FUSELAGE STRINGER 18A SHEAR BEAM SECTION AT BS 663.75, RBL 68, WL 200 DUE TO CRACK PER SB 737-53-1066, SECTIO N III, PART III, REVISION 3, DATED FEB 25, 1993. (M) 2 L 7 2 4F A16WE 1999060400201 19990604 00201 NM 1999 6 4 P2EA99176 1 19990327 A 5320 BEAM BOEING 737 737222 1384473 NM BS 663.75 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, LEFT WHEEL WELL, BS 663.75, LBL 68, STRINGER 18A SHEAR BEAM SECTION WAS FOUND WITH A CRACK. REPAI RED LEFT FUSELAGE STRINGER 18A SHEAR BEAM SECTION AT BS 663.75, BL 68, WL 200 DUE TO CRACK PER 737-53-1066, SECTION III, PART II, REVISION 3, DATED FEBRUARY 25, 1993. (M) 2 L 7 2 4F A16WE 1999060400202 19990604 00202 NM 1999 6 4 P2EA99177 1 19990406 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 947 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, IN PASSENGER CABIN AFT LAVATORY AREA, BS 947, BETWEEN RBL 54 INCH AND LBL 54 INCH, FLOORBEAM WAS F OUND WITH CORROSION. REPAIRED FLOORBEAM UPPER CHORD AT BS 947, BETWEEN LBL 59 AND RBL 59 PER COOPESA EO COO-3-53-222-99 , DATED APR 8, 1999. (M) 2 L 7 2 4F A16WE 1999060400203 19990604 00203 WP 1999 6 4 AALA990697 1 19990512 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456AA 49561 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FRONT HALF OF COACH CABIN WERE INOPERATIVE. REPAIRE D EMERGENCY FLOOR PATH LIGHTING WIRE IN COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999060400204 19990604 00204 WP 1999 6 4 AALA990704 1 19990513 A 3350 SOCKET DOUG DC9 DC982 3022082 WP LT EMER EXIT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 555AN 53085 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT LIGHT AT LEFT FORWARD OVERWING EXIT INOPERATIVE. REPAIRED LIGHT ASSEMBLY SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999060400205 19990604 00205 WP 1999 6 4 AALA990703 1 19990513 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENCY FL OOR PATH LIGHTING WIRE SPLICE THAT WAS SHORTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999060400206 19990604 00206 WP 1999 6 4 AALA990718 1 19990517 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7521A 49898 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH FLAT JUMPER WIRE AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999060400207 19990604 00207 WP 1999 6 4 AALA990716 1 19990516 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 17 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 DFW - DURING GROUND OPERATIONS, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 17 INOPERATIVE. REPLACED EMERGENCY FLOOR PA TH LIGHT WIRE CONNECTOR AT SET ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999060400208 19990604 00208 WP 1999 6 4 AALA990712 1 19990514 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP LT EMER EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 210AA 49161 ORD - DURING OVERNIGHT MAINTENANCE, LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE LIGH T ASSEMBLY AT FAULT. REPLACED LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F A6WE 1999060400209 19990604 00209 WP 1999 6 4 AALA990713 1 19990514 A 3350 LAMP DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 483A 49676 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY HANDLE RELEASE FLOOR LIGHT WOULD NOT ILLUMINATE. CLEANED CONTAC TS ON LAMPS. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999060400210 19990604 00210 WP 1999 6 4 AALA990710 1 19990514 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 483A 49676 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE IN FORWARD CABIN. REPAIRED EMERGENCY EXIT FLO OR PATH CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999060400211 19990604 00211 NM 1999 6 4 USAA059901 1 19990509 A 2611 824PY SMOKE DETECTOR BOEING 727 727225 1384077 NM AFT LAV INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS TS970 20445 FLT 6140 - LGA-BOS - REPLACED AFT LAV SMOKE DETECTOR. AFT LAV SMOKE DETECTOR WON'T TEST. (M) 2 L 7 3 4F A3WE 1999060400212 19990604 00212 NM 1999 6 4 USAA059902 1 19990511 A 2611 CONNECTOR BOEING 727 727225 1384077 NM LAV SMOKE DET LOOSE A USAA O OTHER N FALSE WARNING TO TAKEOFF 1 EA 19 923TS 127A 20441 DCA-LGA - FLT 6540 - DCA-LGA - FORWARD LAVATORY SMOKE DETECTOR ALARM WENT OFF DURING TAKEOFF CLIMB. THEN WENT OFF AFTE R F/A PLAYED WITH IT. RESEATED CONNECTOR ON DETECTOR, CHECKS OK. (M) 2 L 7 3 4F A3WE 1999060400213 19990604 00213 EU 1999 6 4 C2XA99IA251 1 19990421 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE INSPECTION, THREE AISLE PATH EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK IAW ATR42-500 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400214 19990604 00214 SO 1999 6 4 C2XA99IA250 1 19990428 A 3350 GE1317 BULB EMB 145 EMB145 SO LT EMER EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 IAH - DURING A-CHECK INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999060400215 19990604 00215 EU 1999 6 4 C2XA99IA249 1 19990418 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 33-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 33 TO 36. MAINTENANC E REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR424-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400216 19990604 00216 EU 1999 6 4 C2XA99IA248 1 19990418 A 5320 S52571401208 DOUBLER AEROSP ATR42 ATR42320 8680930 EU LT MLG WW CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING C-CHECK INSPECTION, THE LEFT WHEEL WELL FORWARD OUTBOARD CORNER RADIUS DOUBLER WAS FOUND TO BE CRACKED JUST AFT OF THE MAIN LANDING GEAR SIDE BRACE INBOARD ATTACH FITTING. MAINTENANCE REPAIRED THE DAMAGED DOUBLER IAW ATR 42 RE PAIR DRAWING 15S535R0045, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400217 19990604 00217 EU 1999 6 4 C2XA99IA247 1 19990418 A 5320 S53970004254 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING C-CHECK INSPECTION, THE CENTER SUPPORT FOR THE BELLY FAIRING BETWEEN THE MAIN LANDING GEAR WAS FOUND TO BE CORRODED AT THE LOWER ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400218 19990604 00218 EU 1999 6 4 C2XA99IA246 1 19990418 A 5311 S53671311200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 37 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING C-CHECK INSPECTION, FRAME 37 RIGHT WAS FOUND TO HAVE CORROSION AT FLOOR LEVEL. MAINTENANCE REPAIRED THE FR AME IAW ATR 42 REPAIR DRAWING 16S536R0054, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400219 19990604 00219 EU 1999 6 4 C2XA99IA245 1 19990418 A 5210 S52176404206 STEP AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR STEP 834Z WAS FOUND TO BE CRACKED AT THE FORWARD OUTBOARD CORNER. M AINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400220 19990604 00220 EU 1999 6 4 C2XA99IA244 1 19990418 A 5313 S53671407232 STRINGER AEROSP ATR42 ATR42320 8680930 EU FRAME 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING C-CHECK INSPECTION, THE LEFT OUTBOARD STRINGER 21 WAS FOUND TO BE CORRODED FORWARD OF FRAME 40. MAINTENANC E REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR IAW ATR42-320 SRM 53-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400221 19990604 00221 EU 1999 6 4 C2XA99IA243 1 19990427 A 3350 3012701 LIGHT AEROSP ATR42 ATR42500 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING MAINTENANCE VISIT INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-500 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400222 19990604 00222 EU 1999 6 4 C2XA99IA242 1 19990428 A 3350 3012701 LIGHT AEROSP ATR42 ATR42500 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14451 512 IAH - DURING MAINTENANCE VISIT INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-500 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400223 19990604 00223 SO 1999 6 4 C2XA99IA241 1 19990419 A 3350 3025101 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING MODIFICATION, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145MM 33-50-07 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4F RT T00011AT 1999060400224 19990604 00224 EU 1999 6 4 C2XA99IA240 1 19990417 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15827 175 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON SEAT TRACK AT LBL 7 FRAME 36 TO 38. REMOVED AND REPLACED SEAT TR ACK IAW SRM 51-25-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400225 19990604 00225 NE 1999 6 4 C2XA99CL040 2 19990510 A 7230 COMPRESSOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 87551 UE206 PCEPS0005 CLE - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE COMPRESSOR BLADES WERE FOUND TO BE DAMAGED BEYOND MANUFACTURES LIMI TS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW B1900 MM 71-00-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTO RY IAW B1900 MM 71-10-00 AND CONTINENTAL EXPRESS TASK CARD NR 4361001. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999060400226 19990604 00226 EU 1999 6 4 C2XA99IA262 1 19990506 A 3397 3351212CF24 WIRE AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14825 170 IAH - FLT 4177 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIV E. MAINTENANCE REPAIRED A BROKEN WIRE FOR THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999060400227 19990604 00227 EU 1999 6 4 C2XA99IA261 1 19990506 A 3350 3011160 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14825 170 IAH - FLT 4199 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LOWER SERVICE DOOR EMERGENCY EXIT SIGN WAS INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999060400228 19990604 00228 EU 1999 6 4 C2XA99IA263 1 19990505 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 EFD - DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR24-500 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE (M) 2 H 7 2 4T RT A53EU 1999060400229 19990604 00229 EU 1999 6 4 C2XA99BT034 1 19990503 A 3397 3011210 WIRE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14813 100 BTV - DURING RON MAINTENANCE, FOUND EMERGENCY LIGHT CHECK FAILED. REPAIRED BROKEN WIRE AND REMOVED AND REPLACED EMERGEN CY LIGHT IN PASSENGER DOOR. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400230 19990604 00230 EU 1999 6 4 C2XA99BT035 1 19990502 A 3350 1670 BULB AEROSP ATR72 ATR72212 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69902 385 BTV - DURING 4A INSPECTION, FUOND LEFT AISLE PATH EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED TRACK LIGHTING BUL B AT END OF AISLE. OPS CHECKED OF EMERGENCY LIGHTS GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400231 19990604 00231 EU 1999 6 4 C2XA99BT036 1 19990502 A 3350 AQS1000 BATTERY PACK AEROSP ATR72 ATR72212 EU SVC DOOR DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69902 385 BTV - DURING 4A INSPECTION, FOUND SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE ON BATTERY PACK. MAINTENANCE REMOVE D AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK. OPS CHECKED OF EMERGENCY LIGHTING GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400232 19990604 00232 SO 1999 6 4 C2XA99BT037 1 19990503 A 3350 1317 BULB EMB 145 EMB145 SO ROW 11 FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15932 145015 BTV - DURING ROUTINE, FOUND EMERGENCY LIGHT IN CEILING TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB IN EMER GENCY EXIT LIGHTS. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1999060400233 19990604 00233 EU 1999 6 4 C2XA99BT038 1 19990505 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 BTV - DURING LINE CHECK MAINTENANCE, FOUND EMERGENCY LIGHTS FAILED CHECK. RELAMPED PASSENGER STAIR DOOR GROUND ILLUMINA TION LIGHT, OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400234 19990604 00234 EU 1999 6 4 C2XA99BT039 1 19990506 A 3350 301180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU ROW 6-9 INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 11835 194 EWR - CREW REPORTS EMERGENCY AISLE PATH LIGHTS ROWS 6, 7, 8 AND 9 STAY ON AFTER AIRCRAFT IS DE-ENERGIZED. REMOVED AND R EPLACED NR 3 EMERGENCY POWER SUPPLY. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400235 19990604 00235 EU 1999 6 4 C2XA99BT040 1 19990505 A 3397 WIRE AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR BROKEN A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 11835 194 EWR - CREW REPORTED SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING ON SERVICE DOOR L IGHT AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999060400236 19990604 00236 SO 1999 6 4 C2XA99BT041 1 19990505 A 3297 WIRE EMB 145 EMB145LR SO LT MLG INOPERATIVE A C2XA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 09 13949 145057 EWR - DURING OVERNIGHT MAINTENANCE, FOUND LEFT DOWN LOCKED INDICATION ON SYSTEM ONE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT SP1422. OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4T RT T00011AT 1999060400237 19990604 00237 EU 1999 6 4 C2XA99IA257 1 19990505 A 3230 1002383Y00 VALVE AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 86842 286 IAH - FLT 3988 - THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WH ERE MAINTENANCE CLEANED THE PROXIMITY SWITCH CANNON PLUG AND OPERATIONALLY CHECKED GOOD IAW ATR42-320 JIC 32-31-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 3467. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE IAW ATR42-320 JIC 32-31-00, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO FURTHER INCIDENTS HAVE BEEN REPORTED TO DATE. (M) 2 H 7 2 4T RT A53EU 1999060400238 19990604 00238 SO 1999 6 4 C2XA99IA259 1 19990505 A 3350 3025101 LIGHT EMB 145 EMB145 SO RT EMER EXIT CORRODED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27962 145110 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAI NTENANCE CLEANED CORROSION FROM THE LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999060400239 19990604 00239 EU 1999 6 4 C2XA99IA258 1 19990504 A 3350 301180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 IAH - DURING MAINTENANCE INSPECTION, THE MIDDLE AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVD AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400240 19990604 00240 EU 1999 6 4 C2XA99IA252 1 19990429 A 3350 167006 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING 'A' CHECK INSPECTION, THE EMERGENCY AISLE PATH LIGHTS AT SEATS 3A/4A WRE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999060400241 19990604 00241 EU 1999 6 4 C2XA99IA253 1 19990428 A 3230 RETRACT MECH AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 86842 286 IAH - FLT 3464 - ON TAKEOFF, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE JACKED THE AIRCRAFT AND PERFORMED GEAR SWINGS WITH NO DEFECTS NOTED. THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE WITH NO FURTHER INCIDENTS REPORTED AT THIS TIME. (M) 2 H 7 2 4T RT A53EU 1999060400242 19990604 00242 NM 1999 6 4 TSAA9933231 1 19990510 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 831-838 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 FOUND CRACK NOTED ON STRINGER 10R LAP JOINT AT BS 831 THROUGH 838. THE LAP JOINT WAS REPAIRED IAW 737 SRM 53-30-03 FIG 42. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999060400243 19990604 00243 NM 1999 6 4 TSAA9933232 1 19990515 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED POWER PACK FOR POSITION NR 6 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999060400244 19990604 00244 EA 1999 6 4 MASA99070 1 19990508 A 3350 OL3071BPEGPL BULB CNDAIR CL600 CL6002B19 EA AIRSTAIR DOOR FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5803 - MKE-PHL - CREW FOUND THE EMERGENCY EXIT SIGN ABOVE THE AIRSTAIR DOOR INOPERATIVE. MAINTENANCE REPLACED THE B ULB, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999060400245 19990604 00245 EA 1999 6 4 MASA99072 1 19990511 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37178 7178 FLT 5408 - CMH-MDW - CREW REPORTED THAT THE FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTING ORANGE OVERLAY AT THE SERVICE DOOR WOULD NOT ILLUMINATE. MAINTENANCE FOUND THE CONNECTOR TO BE LOOSE AND RESECURED THE CONNECTOR. NO DEFECTS WERE F OUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999060400246 19990604 00246 EA 1999 6 4 MASA99071 1 19990511 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA EXTERNAL FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37178 7178 FLT 5361 - DCA-CMH - CRWE REPORTED THE LEFT MIDDLE OVERWING EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE ACT ION AWS DEFERRED PER MEL 33-51-2 AND THE AIRCRAFT WAS RETURNED TO SERVICE. INSUBSEQUENT MAINTENANCE, THE BULB WAS REMOV ED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1999060400247 19990604 00247 EA 1999 6 4 MASA99076 1 19990519 A 3350 MS220793 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA COCKPIT TRIPPED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 FLT 5760 - PHL-BHM - AFTER ARRIVAL IN PHL, CREW REPORTED THAT THE EMERGENCY LIGHTS WERE ILLUMINATING WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE RESET THE CIRCUIT BREAKER, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999060400248 19990604 00248 NM 1999 6 4 UPS99229686 1 19990528 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION, BULGING SKIN AND SHEARED FASTENER HEAD ON SKIN AT BS 1040 RBL 70, WL 208. REMOVED AND RE PLACED SKIN FROM BS 1016 TO 1080, STR 14R-20R. 2 L 7 3 4F A3WE 1999060400249 19990604 00249 NM 1999 6 4 UPS99229687 1 19990527 A 5753 TRACK BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON NR 6 FLAP TRACK AT SPOILER BEAM MOUNT PAD. REMOVED AND REPLACED WITH NEW FLAP TRACK BE AM PER OHM 27-51-21 PG 502. 2 L 7 3 4F A3WE 1999060400250 19990604 00250 NM 1999 6 4 UPS99229688 1 19990513 A 5744 65327331 FITTING BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 2 FLAP TRACK FWD ATTACH WING FITTING. REWORK OUT OF LIMITS PER B OEING DWG 65-32733. REPLACED WITH NEW ITEM. 2 L 7 3 4F A3WE 1999060400251 19990604 00251 NM 1999 6 4 UPS99229689 1 19990528 A 5753 BOLT BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, NR 6 FLAP TRACK AFT MOUNT BOLTS CORRODED. CLEANED AND TREATED BOLT HOLES AND REPLACED BOLTS. 2 L 7 3 4F A3WE 1999060400252 19990604 00252 NM 1999 6 4 UPS99229690 1 19990523 A 5753 651427010 TRACK BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON NR 4 FLAP TRACK AT SPOILER BEAM ATTACH POINT. REPLACED TRACK PER MM 27-51-31. 2 L 7 3 4F A3WE 1999060400253 19990604 00253 WP 1999 6 4 UPS99829691 1 19990528 A 5320 JAMB DOUG DC8 DC873F 302199F WP LT MLG DOORWAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A, LEFT MAIN GEAR DOOR CUTOUT AT REAR SIDE INNER CORNER HAS CURLED SHEET METAL AND A .5 INCH LONG TEAR . *S/D* REPAIRED AREA IAW SRM 51-1-20 AND SRM 53-4 -1. 2 L 7 4 4F RT 4A25 1999060400254 19990604 00254 NM 1999 6 4 DL76L991127 1 19990521 A 2612 CONNECTOR BOEING 767 767332 1382001 NM FIRE WARNING LOOSE A DALA K NONE N FALSE WARNING TO TAKEOFF 1 SO 27 199DN 28456 MOMENTARY FIRE BELL ON TAKEOFF, NO OTHER INDICATIONS. DUPLICATED FAULT BY SHAKING D813 CONNECTOR ON WEU PWR SUPPLY B. F OUND CONNECTOR NOT FULLY SEATED. RESEATED POWER SUPPLY. CONNECTOR NOW ENGAGED, WARNING CHECKS GOOD. 2 L 7 2 4F RT A1NM 1999060400255 19990604 00255 NM 1999 6 4 DL76G991130 1 19990521 A 2820 VALVE BOEING 767 767324 NM RT WING LEAKING A DALA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 394DL 27394 ON TAXI OUT, FOUND FUEL LEAKING ON RT WING. FOUND SURGE BOX RELIEF VALVE LEAKING. RESEATED, LEAK CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999060400256 19990604 00256 NM 1999 6 4 DL757991134 1 19990522 A 2622 EXTINGUISHER BOEING 757 757232 1384965 NM AFT LAV DEPLETED A DALA K NONE O OTHER CR CRUISE 1 SO 27 604DL 22811 LAV AFT LEFT H2O EXTINGUISHER USED, CONT NR C05229076. REPORTED VIA ACARS AND DISPATCHER TO MTC. F/A SUSPECTED PASSENG ER SMOKING IN AFT LEFT LAVATORY AND USED H2O BOTTLE. REPLACED H2O EXTINGUISHER AND SMOKE DETECTOR. 2 L 7 2 4F RT A2NM 1999060400257 19990604 00257 NM 1999 6 4 DL76G991145 1 19990523 A 3350 BPS73 POWER SUPPLY BOEING 767 7673P6 1385105 NM EMER EXIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 24984 RIGHT HAND AFT TWO WING SLIDE EMERGENCY LIGHTS ARE INOP AND R3 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED POWER SU PPLY. 2 L 7 2 4F RT A1NM 1999060400258 19990604 00258 NM 1999 6 4 DL76S991147 1 19990520 A 5315 146T51471 FLOORBEAM BOEING 767 767332 1382001 NM BS 1329 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 DURING REPLACEMENT OF AN OVERHEAD CEILING PANEL IN THE AFT BAG BIN DAMAGE WAS FOUND ON THE BS 1329 FLOORBEAM AT LBL 11 A ND RBL 11. REPAIRED PER ERA 333177-14, REV A. 2 L 7 2 4F RT A1NM 1999060400259 19990604 00259 NM 1999 6 4 DLM11991148 1 19990524 A 5347 AFA774014 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1879 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 809DE 48480 RIGHT AFT O/B SEAT TRACK WAS FOUND WITH EXTENSIVE CORROSION. THE REPLACEMENT SECTION OBTAINED FROM OEM DID NOT MEET B/P SPECS. REWORKED PER ERA 333185-14. 2 L 7 3 4F RT A22WE 1999060400260 19990604 00260 NM 1999 6 4 DL72S991149 1 19990524 A 5713 STRINGER BOEING 727 727225A 1384077 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 THE AFT RIB TO STRINGER ATTACH TAB AT WS 171.5 S18 OF THE RT WING WAS FOUND CRACKED. REPAIRED PER ERA 333161-14, REV B. 2 L 7 3 4F RT A3WE 1999060400261 19990604 00261 NM 1999 6 4 DLM88991154 1 19990524 A 5330 29524401 SKIN DOUG MD88 MD88 3023688 NM BS 297 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 TWO DENTS WERE FOUND AT FS 297 BETWEEN L18L AND L20L. REPAIRED PER ERA 333179-14, REV A. 2 L 7 2 4F RT A6WE 1999060400262 19990604 00262 NM 1999 6 4 DLM88991155 1 19990524 A 5330 595305077 SKIN DOUG MD88 MD88 3023688 NM BS 229-237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 A FUSELAGE SKIN DENT WAS FOUND BETWEEN FS 229 AND FS 237, BETWEEN L18L AND 20L. REPAIRED PER ERA 333159-14, REV A. 2 L 7 2 4F RT A6WE 1999060400263 19990604 00263 NM 1999 6 4 DLM88991156 1 19990524 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM BS 465 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 A DENT WAS FOUND AT APPROX FS 465 AND L20R IN THE FUSELAGE SKIN. REPAIRED PER ERA 333158-14, REV A. 2 L 7 2 4F RT A6WE 1999060400264 19990604 00264 1999 6 4 DL76G991157 4 19990524 A 3442 RADAR 20412222456 BOEING 767 767332 1382001 NM COCKPIT INOPERATIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 1603 4897 29695 WX RADAR SYSTEM INOP. BAD WEATHER, JFK DIVERTED TO BOS. REPLACED CTL/DISPLAY, OPS CK NORMAL. 2 L 7 2 4F RT A1NM 1999060400265 19990604 00265 NM 1999 6 4 DL72K991158 1 19990523 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 580-600 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 417DA 21259 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 360 AND 640 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED ONLY 2 CRACKS BETWEEN FS 580 AND 600. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367428-14AD, REV A. 2 L 7 3 4F A3WE 1999060400266 19990604 00266 NM 1999 6 4 DL72S991159 1 19990522 A 5330 65545826 SKIN BOEING 727 727232 1384082 NM BS 1009-1120 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERN AL HFEC INSPECTION REVEALED 2 CRACKS BETWEEN FS 1030 AND 1050, AND 3 CRACKS BETWEEN FS 1050 AND 1070. THE SKIN LAP WAS CUT OUT BETWEEN FS 1009 AND FS 1120 AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367421-14AD. 2 L 7 3 4F A3WE 1999060400267 19990604 00267 NM 1999 6 4 DLM11991161 1 19990524 A 2560 MEGAPHONE TALBOT DOUG MD11 MD11 3023602 NM CABIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 814DE 48769 ON PREFLIGHT F/C MEGAPHONE FOUND WITH TRIGGER BROKEN. REPLACED SAME. 2 L 7 3 4F RT A22WE 1999060400268 19990604 00268 NM 1999 6 4 DLM11991162 1 19990524 A 2121 FAN 60545708 DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 48474 ELECTRICAL SMELL IN FORWARD PART OF PLANE, FAIRLY NOTICEABLY. TURNED OFF CABIN BUSS AND SITUATION IMPROVED. ISOLATED S OURCE TO NR 1 RECIRC FAN. REPLACED SAME. 2 L 7 3 4F RT A22WE 1999060400269 19990604 00269 NM 1999 6 4 DL76P991163 1 19990524 A 2750 285TOO4953 FSEU BOEING 767 767332 1382001 NM TE FLAPS MALFUNCTIONED A DALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 1402A 25989 DURING APPROACH INTO RSW WITH FLAPS 30 SELECTED, FLAP GOT TO 27 DEG THEN STARTED RETRACTING AUTOMATICALLY TO 20 DEG. AI RSPEED WAS AT 155 KTS. RECEIVED FLAP DISAGREE MESSAGE WHEN THIS HAPPENED. DID NOT GET -FLAP LOAD RELIEF- EICAS MESSAGE . ABORTED APPROACH. PERFORMED GO-AROUND AND ALTERNATELY EXTENDED THE FLAPS. MTC FOUND NO RELATED FSEU FAULTS. REPLAC ED FSEU AND RT ADC AS PRECAUTION. 2 L 7 2 4F RT A1NM 1999060400270 19990604 00270 NM 1999 6 4 DL76L991165 1 19990524 A 2910 HYD SYST BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE REQUIRED SERVICE A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 173DN 24800 724165 RIGHT HYD SYS RSVR LIGHT AND RIGHT HYD QUANT EICAS MESSAGE. SECURED RT PRIM PUMP AND DEMAND PUMP AS PER ABN PROC QTY CO NT TO DROP. LEFT BOTH PUMPS OFF QTY STAB AT .43. SERVICED RT HYD SYSTEM TO FULL. PRESSURIZED SYSTEM FOR APPROX 2 HRS, VISUALLY INSPECTED EXTERIOR OF A/C AND AFT COMPARTMENTS, NO LEAKS FOUND. NO INDICATION OF REDUCTION IN HYD FLUID QTY. RAN ALL FLIGHT CTLS AND BRAKES ASSOCIATED WITH RT SYSTEM, ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999060400271 19990604 00271 NM 1999 6 4 DL76L991168 1 19990525 A 3240 VALVE 705072 BOEING 767 767332 1382001 NM BRAKE SYSTEM LEAKING A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 181DN 25986 ACFT RETURNED TO BLOCKS, RT HYD SYS FAILURE. MTC FOUND RT BRAKE METERING VALVE LEAKING. REPLACED METERING VALVE, OPS C HECKS NORMAL. 2 L 7 2 4F RT A1NM 1999060400272 19990604 00272 NM 1999 6 4 DL76L991169 1 19990525 A 2910 O RING BOEING 767 767332 1382001 NM RT PYLON DAMAGED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 177DN 25122 ACFT DIVERTED TO FRA WITH LOSS OF RT HYD SYS. FOUND O-RING DAMAGED AT RT HYD MODULE PRESS FILL CONNECTOR. REPLACED O-R ING ON ENG R/U, LEAKS CKS OK. 2 L 7 2 4F RT A1NM 1999060400273 19990604 00273 NM 1999 6 4 DL72S991170 1 19990524 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A CRACK BETWEEN FS 360 AND 380. THE CRACK WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-03 FIG 5 AND PER ER/A 367439-14AD. 2 L 7 3 4F A3WE 1999060400274 19990604 00274 NM 1999 6 4 DL72S991171 1 19990524 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 420-440 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 2 CRACKS BETWEEN FS 420 AND 440. THE CRACKS WERE CUT OUT OF THE SKI N LAP AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-03, FIG 5 AND ER/A 367440-14AD. 2 L 7 3 4F A3WE 1999060400275 19990604 00275 WP 1999 6 4 DLL14991172 1 19990523 A 5330 1503541217 SKIN LKHEED 1011 1011385115 5265015 WP BS 1545 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 THE FUSELAGE SKIN ASSY WAS FOUND WITH CORROSION AT FS 1545 AND STRINGER 26. THE CORROSION WAS THROUGH THE C2 DOOR SURR OUND TRIPLER AND SURROUND DOUBLERS AND INTO THE SKIN. THE CORROSION WAS REMOVED WITH A 6 CUTOUT THROUGH THE ENTIRE SKIN ASSY. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL DOUBLERS PER ER/A 367391-14, REV A. 2 L 7 3 4F A23WE 1999060400276 19990604 00276 WP 1999 6 4 DLL14991173 1 19990523 A 5330 1503140 SKIN LKHEED 1011 1011385115 5265015 WP BS 703 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 THE FUSELAGE SKIN WAS CORRODED AT FS 703 BETWEEN STRINGERS 33 AND 34. THE CORROSION WAS CUT OUT OF THE SKIN WITH A 4 X 8 CUTOUT. THE DAMAGE WAS ADJACENT TO AN EXISTING REPAIR DOUBLER INSTALLED TO REPAIR A SIMILAR CUTOUT. THE EXISTING REPAIR WAS REMOVED AND BOTH SKIN CUTOUTS REPAIRED WITH A SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 367407-14, REV B. 2 L 7 3 4F A23WE 1999060400277 19990604 00277 NM 1999 6 4 DL72S991174 1 19990507 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND DURING MV2 MID VISIT NRC 209, 2 CRACKS AT LT SIDE OF VERTICAL WEB STA 1303 INSIDE VERTICAL STAB CRAWLWAY. REPAIRE D PER SRM 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1999060400278 19990604 00278 NM 1999 6 4 DL72S991175 1 19990507 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND DURING MV2 CORROSION VISIT NRC 208, 2 CRACKS AT RT SIDE OF VERTICAL WEB STA 1303 INSIDE VERTICAL STAB CRAWLWAY. R EPAIRED PER SRM 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1999060400279 19990604 00279 NM 1999 6 4 DL73K991176 1 19990525 A 2613 3530310 CONNECTOR BOEING 737 737232 1384475 NM LT WING/BODY CHAFED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 326DL 23098 DURING CLIMBOUT HAD RAPID FLICKERING OF LT WING BODY OVERHEAT LIGHT. TURNED OFF LEFT BLEED, LIGHT STILL ON. PULLED BAC K THROTTLE LIGHT EXTINGUISHED. RETURNED TO GATE. FOUND AND REPAIRED CONN (276) AT APU COMPT BULKHEAD. 2 L 7 2 4F RT A16WE 1999060400280 19990604 00280 NM 1999 6 4 DL72S991177 1 19990525 A 5240 6556150137 FRAME BOEING 727 727232 1384082 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 A .5 INCH CRACK IN R-1 DOOR FWD FRAME EXTENDING FROM LOWER FWD STOP FITTING. REPAIRED PER MM 52-12-0. 2 L 7 3 4F A3WE 1999060400281 19990604 00281 NM 1999 6 4 DL72S991178 1 19990525 A 2410 CSD BOEING 727 727232 1384082 NM NR 2 ENGINE REQUIRED SERVICE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 407DA 21151 CSD LOW PRESSURE LIGHT FLICKERED AND THEN STAYED ON, LOST MAIN AC NR 2. FOUND CSD LOW. SERVICED CSD, RAN ENG AND NO LE AKS NOTED. 2 L 7 3 4F A3WE 1999060400282 19990604 00282 NM 1999 6 4 DL733991180 1 19990525 A 3397 WIRE BOEING 737 737347 1384647 NM ROW 15 20 22 23 LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 312WA 23598 IN-SEAT EMERGENCY PATH LIGHTS INOP IN SEATS 15, 20, 22, 23. FOUND WIRES PULLED FROM CONNECTOR AT EACH LOCATION UNDER SE AT NEXT TO LIGHT ASSY. SECURED SAME, CHECKS OK. 2 L 7 2 4F RT A16WE 1999060400283 19990604 00283 NM 1999 6 4 DLM11991181 1 19990525 A 3350 BATTERY PACK 6044113 DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 803DE 6441040 48474 ON LAYOVER CHECK, EMERGENCY LIGHTS BATTERY PACK 3 AND 4 FAILED TEST. REPLACED SAME. 2 L 7 3 4F RT A22WE 1999060400284 19990604 00284 NM 1999 6 4 DL76L991182 1 19990526 A 3350 0201720001 LIGHT BOEING 767 767332 1382001 NM ROW 35 AB INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 SEAT MOUNTED PROXIMITY LIGHT INOP (1 WHITE) AT SEAT ROW 35AB FWD TO MCO AND PLACARD PER MEL 33-51-03B. RELAMPED SAME, N O HELP. 2 L 7 2 4F RT A1NM 1999060400285 19990604 00285 NM 1999 6 4 DL76L991183 1 19990526 A 3350 0201720001 LIGHT BOEING 767 767332 1382001 NM ROW 30 FG INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 SEAT MOUNTED PROXIMITY LIGHTING INOP AT SEAT ROW 30FG. FWD TO MCO AND PLACARD PER MEL 33-51-03B. RELAMPED SAME, NO HEL P. 2 L 7 2 4F RT A1NM 1999060400286 19990604 00286 NM 1999 6 4 DL76L991184 1 19990526 A 3350 0201720001 LIGHT BOEING 767 767332 1382001 NM ROW 3-10 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 SEAT MOUNTED PROXIMITY LIGHTING INOP AT SEATS 3AB AND 10AB. ALSO, LIGHT LENS COVERS MISSING. RELAMPED PROXIMITY LIGHTI NG AT SEAT ROWS 3AB AND 10AB. REPLACED MISSING LENS COVERS, LIGHTING OPS CKS OK. 2 L 7 2 4F RT A1NM 1999060400287 19990604 00287 NM 1999 6 4 DL72S991185 1 19990522 A 5311 652368721 FRAME BOEING 727 727232 1384082 NM BS 1352 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND DURING MV2 CORROSION VISIT NR 266, T-ANGLE WORN THROUGH THREE PLACES FROM .75 TO 4.25 INCHES LONG AT FWD FLANGE O F T-ANGLE, NR 2 ENG CUTOUT 4 O'CLOCK POS TO 6 O'CLOCK POS STA 1453. NRC 267 NR 2 ENG CUTOUT FWD COWL STRIKER T-ANGLE WO RN THROUGH/THIN 3 O'CLOCK POS TO 5 O'CLOCK POS. SPLICED IN SECTION OF FRAME PER M/M 53-11-0, (P/N 65-23687). 2 L 7 3 4F A3WE 1999060400288 19990604 00288 NM 1999 6 4 DL72S991186 1 19990526 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 541DA 22387 FOUND ON D2 LETTER CK, LOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 2 SLAT I/B STOP PAD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999060400289 19990604 00289 WP 1999 6 4 DLL13991188 1 19990526 A 2910 000AE5616T0250 LINE LKHEED 1011 10113851 5265010 WP NR 2 ENGINE LEAKING A DALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 790DL 193A1143 10574 B-SYSTEM LOW QTY LIGHT ILLUMINATED WITH THE QTY SHOWING SLIGHTLY LESS THAN ONE-QUARTER FULL, PRESS WAS NORMAL. SHUTOFF B-SYSTEM ENG PUMP AND TURNED OFF B2 ATM PER POM. COMPLETED NORMAL DESCENT AND LANDED WITH B-SYSTEM DEPRESSURIZED. FOU ND NR 2 ENG B-SYSTEM HYD PUMP OUTLET LINE LEAKING. REPLACED LINE, LEAK CKS GOOD. 2 L 7 3 4F A23WE 1999060400290 19990604 00290 NM 1999 6 4 DL72S991190 1 19990526 A 2120 AIR DIST BOEING 727 727232 1384082 NM CABIN SMOKE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 546DA 22677 SMOKE HAZE IN CABIN, LT PACK UNCONTROLLABLE OVERHEAT. CHECKED LT PACK SYS AND CONTROLLER, ACM CKS OK. RAN PACK CK OK. UNABLE TO DUPLICATE HAZE. 2 L 7 3 4F A3WE 1999060400291 19990604 00291 NM 1999 6 4 DL76G991191 1 19990526 A 2120 AIR DIST BOEING 767 767332 1382001 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 1604R 30180 F/A IN FWD CABIN REPORTED SMELL OF BURNED PLASTIC AFTER LANDING. ODOR WAS CONCENTRATED IN CTR OF AREA BETWEEN AISLES AN D OCCURED SHORTLY AFTER TOUCHDOWN FOR ABOUT 2 MINS. UNABLE TO TRACE EVIDENTS. 2 L 7 2 4F RT A1NM 1999060400292 19990604 00292 NM 1999 6 4 DL72S991192 1 19990524 A 5330 65545974 SKIN BOEING 727 727225A 1384077 NM BS 950 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 SEVERAL GOUGES WERE FOUND IN THE FUSELAGE SKIN AT BS 950E ABOVE S19R. REPAIRED PER ERA 333124-14, REV B. 2 L 7 3 4F RT A3WE 1999060400293 19990604 00293 NM 1999 6 4 DLM88991193 1 19990527 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM BS 244 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 DENT WAS FOUND IN THE FUSELAGE SKIN AT APPROX FS 242 BETWEEN L17L AND L18L. REPAIRED PER ERA 333169-14, REV B. 2 L 7 2 4F RT A6WE 1999060400294 19990604 00294 NM 1999 6 4 DLM88991194 1 19990527 A 5330 29525581 SKIN DOUG MD88 MD88 3023688 NM BS 617 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 A GOUGE WAS FOUND IN THE FUSE SKIN UNDER THE C2 CARGO DOOR CUTOUT, LOCATED APPROX AT FS 617, BETWEEN L30 AND L28L. REPA IRED PER ERA 333157-14, REV B. 2 L 7 2 4F RT A6WE 1999060400295 19990604 00295 NM 1999 6 4 DL72W991196 1 19990527 A 2910 LINE BOEING 727 727247 138408F NM HYD BAY CHAFED A DALA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 2807W 20579 CLIMBING THROUGH 13,000 FEET B-HYD SYSTEM FLUID QTY DECREASE TO ZERO AND BOTH B-SYSTEM PUMP LIGHTS ILLUMINATED. CHECKLI ST PERFORMED SAFETY WIRE CUT ON GPWS AND THE PNEUMATIC BRAKE HANDLE. REPLACED CHAFED HYDRAULIC LINE IN HYD BAY. 2 L 7 3 4F A3WE 1999060400296 19990604 00296 NE 1999 6 4 DL72W991199 2 19990529 A 7200 ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 3 FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 2820W 59711 21058 696486 NR 3 ENG POPPED AND SHUDDERED DURING APPLICATION OF T/O PWR, APPROX 1.6 EPR PRIOR TO INDICATION OF AIRSPEED. REPLACED E NGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999060400297 19990604 00297 NM 1999 6 4 DL76L991200 1 19990529 A 3350 FUSE BOEING 767 767332 1382001 NM ROW 10F SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 185DN 27961 EMERGENCY PATH LIGHTS INOP IN RT FWD CABIN. DISCONNECTED LIGHT AT SEAT 10F THAT WAS SHORTED. REPLACED FUSE IN BATTERY PACK. FWD TO MCO PER MEL 33-51-03A. 2 L 7 2 4F RT A1NM 1999060400298 19990604 00298 NM 1999 6 4 DL767991201 1 19990529 A 3230 ACTUATOR 273T62004 BOEING 767 767232 1385132 NM RT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 107DL 55 22219 ON T/O FROM MCO, RT LANDING GEAR DID NOT RETRACT. DIVERTED TO ATL WITH ALL GEAR DOWN. REPLACED RT MLG SIDE BRACE LOCK ACTUATOR. 2 L 7 2 4F RT A1NM 1999060400299 19990604 00299 NM 1999 6 4 DL76P991203 1 19990529 A 3234 SELECTOR 257T110315 BOEING 767 767332 1382001 NM LANDING GEAR MALFUNCTIONED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 140LL D00304 25988 DURING GEAR EXT HAD 3 GREEN DOWNLOCK LIGHTS WITH GEAR DISAGREE AND TAIL SKID LIGHTS. EXECUTED MISSED APPROACH REVIEWED POM PROCEDURES. ON SECOND APPROACH SHORT FINAL INDICATIONS RETURNED TO NORMAL. NORMAL LANDING AND ROLLOUT. REPLACED T HE LANDING GEAR SELECTOR HANDLE ASSY PER M/M, ALL INDICATIONS CHECK GOOD. 2 L 7 2 4F RT A1NM 1999060400300 19990604 00300 NM 1999 6 4 DL72S991204 1 19990529 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM PASSENGER DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 420DA 21273 AFT CABIN DOOR EMERGENCY EXCAPE LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999060400301 19990604 00301 NM 1999 6 4 DL72S991206 1 19990530 A 7930 BY PASS LIGHT BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE ILLUMINATED A DALA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 537DA 58885 22073 695228 NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED IN FLT. POM FOLLOWED, ENGINE SHUT DOWN. CHECKED OIL FILTER, ALL OK. RA N ENG, ALL PARAMETERS NORMAL. FWD OIL PRESS BY-PASS LIGHT TO MCO/PLA. 2 L 7 3 4F 4 F A3WE E2EA 1999060400302 19990604 00302 NM 1999 6 4 DLM88991207 1 19990530 A 4910 INLET DOUG MD88 MD88 3023688 NM APU CONTAMINATED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 966DL 53115 AFTER TAKEOFF AT ABOUT 4,000 FEET, EXPERIENCED SMOKE IN THE CABIN. ALL 3 LAV SMOKE DETECTORS WENT OFF, RETURNED TO ATL. CLEANED APU INLET, PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1999060400303 19990604 00303 WP 1999 6 4 DLL10991208 1 19990529 A 2720 CONTROL CABLE LKHEED 1011 10113851 5265010 WP RUDDER PEDALS OUT OF ADJ A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 735D 193C1226 DURING CONTROL CHECK, THE RIGHT RUDDER DISPLACEMENT WAS SIGNIFICANTLY RESTRICTED WHEN FULL PHYSICAL EFFORT WAS PLACED ON THE RIGHT RUDDER IT BROKE FREE WITH A LOAD NOISE FROM UNDER THE F/O'S PANEL. RETURNED TO GATE. MTC INSPECTED RUDDER P EDALS CONTROL AND PEDAL ADJUSTMNT SYS. FOUND COPILOTS PEDAL ADJUSTMENT TELEFLEX CABLE MAY HAVE RUBBED. REPOSITIONED TE LEFLEX ALL RUDDER PEDAL, OPRN CHECKS NORMAL. 2 L 7 3 4F A23WE 1999060400304 19990604 00304 WP 1999 6 4 DLL10991209 1 19990531 A 3230 1523153119 ACTUATOR LKHEED 1011 10113851 5265010 WP RT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 728DA 193C1173 ATB, AFTER T/O MAIN LANDING GEAR TRUCK LIGHT ILLUMINATED. TROUBLESHOT PER FIM 32-30-00 PG 120. REPLACED RT LEVEL CYL, OPS AND LEAK CK NORMAL AND OK. 2 L 7 3 4F A23WE 1999060400305 19990604 00305 WP 1999 6 4 DLL19991210 1 19990531 A 3350 BATTERY PACK 20131A LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 6699 193H1216 FOUND ON LAYOVER CHECK, ESCAPE PATH EMERGENCY LIGHTS PARTIALLY INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1999060400306 19990604 00306 NM 1999 6 4 DL72S991212 1 19990531 A 2820 VALVE 6568 BOEING 727 727225A 1384077 NM RT WING INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 805EA 2252 22436 WHILE DEPARTING ATL, CENTER FUEL GAUAGE WAS READING 2500 LBS LOWER, WHILE RT WING GAUGE WAS READING HIGHER BY THE SAME. TWO UNITS TRIM REQUIRED FOR LEVEL FLT. AFTER RETURNING TO GATE, FOUND NR 3 TANK VALVE SWITCH IN THEOPEN POSITION DUE T O A BROKEN GUARD COVER ON THE WING REFUELING STATION. ALSO FOUND THE DEFUEL VALVE DEFECTIVE. TRANSFERRED FUEL ON THE G ROUND WITH THE DEFUEL VALVE IN THE CLOSED POSTION. REPLACED DEFUEL VALVE. 2 L 7 3 4F RT A3WE 1999060400307 19990604 00307 NM 1999 6 4 DLM88991213 1 19990531 A 2150 20495061 ACM 20495061 DOUG MD88 MD88 3023688 NM LEFT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 956DL 6030912 49887 UNABLE TO MAINTAIN CABIN PRESSURE AT FL350 WITH ENG ANTI-ICE ON. OUTFLOW VALVE INDICATED FULL CLOSED AND FLOW LIGHT ILL UMINATED. INCREASED POWER ON BOTH ENGS AND LOWERED AIRCRAFT ALTITUDE BUT CABIN ALTITUDE CONTINUED TO CLIMB. WHEN CABIN ALT REACHED 10600 FT CREW DIVERTED TO AMA. FERRIED A/C TO DFW. FOUND LEFT ACM SEIZED. REPLACED ACM. PRESSURIZED AIR CRAFT, ALL OPERATION CHECKS GOOD. CHECKED RIGHT PACK, OPERATION GOOD. 2 L 7 2 4F RT A6WE 1999060400308 19990604 00308 NM 1999 6 4 VNAA9905007 1 19990523 A 2913 42086 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MAIN HYD SYST FAILED A VNAA K NONE J WARNING INDICATION AP APPROACH 1 GL 07 437JS 6945 5408 3055 A MAIN HYDRAULIC PUMP FAIL WARNING MESSAGE ILLUMINATED 30 MIN INTO THE FLIGHT. THE CREW FOLLOWED THE QRH, AND CONTINUED ON TO PIT. DURING THE APPROACH INTO PIT, THE LEFT HAND MAIN LANDING GEAR FAILED TO INDICATE A DOWN AND LOCKED CONDITIO N. THE CREW DECLARED AN EMERGENCY, AND FOLLOWED THE QUICK REFERENCE HANDBOOK ONCE MORE. THE AIRCRAFT CONTINUED THE APP ROACH AND LANDED SAFELY IN PIT. MAINTENANCE INSPECTED AND REPLACED THE MAIN HYDRAULIC PUMP, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-11-04. OPERATIONAL AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400309 19990604 00309 NM 1999 6 4 VNAA9905008 1 19990524 A 3260 OL3092 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 432JS 3045 THE LEFT MAIN GEAR GREEN INDICATION LAMPS WERE NOTED TO BE INOPERATIVE, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT R ETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR DOWN AND LOCKED INDICATION LAMPS, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-11-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURN ED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400310 19990604 00310 NM 1999 6 4 VNAA9905009 1 19990525 A 3350 LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN MALFUNCTIONED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 440JS 3058 THE EMERGENCY LIGHTS LOCATED AT THE FORWARD END OF THE CABIN, FAILED TO OPERATE DURING THE PREFLIGHT INSPECTION. MAINTE NANCE INSPECTED AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUA L 33-51-01. THE DISCREPANCY COULD NOT BE DUPLICATED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400311 19990604 00311 NM 1999 6 4 VNAA9905010 1 19990526 A 3260 329630 CONTROL BOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LANDING GEAR INOPERATIVE A VNAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 07 441JS 87999 3059 THE LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED WHEN SELECTED ON FINAL APPROACH. THE CREW FOLLOWED QRH PROCEDURES A ND DECLARED AN EMERGENCY. THE AIRCRAFT MADE A TOWER FLY BY, AND HAD THE TOWER VERIFY THE GEAR POSITION. AFTER THE GEA R WAS VERIFIED DOWN BY THE TOWER, THE AIRCRAFT SHOT ANOTHER APPROACH AND LANDED SAFELY. OUTSTATION MAINTENANCE INSPECTE D AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FLIGHT WAS EXECUTED WITHOUT ANY PROBLEMS. PIT MA INTENANCE INSPECTED AND REPLACED THE DIMMER CONTROL BOX, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-13-11. OPERATI ONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400312 19990604 00312 NM 1999 6 4 VNAA9905011 1 19990528 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 24K DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 437JS 62595 1035 3055 THE EMERGENCY LIGHT 24LK WAS NOTED TO BE INOPERATIVE BY PIT MAINTENANCE, DURING A LINE CHECK ONE INSPECTION. MAINTENANC E INSPECTED AND REPLACED THE 6LK EMERGENCY LIGHT BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. O PERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400313 19990604 00313 NM 1999 6 4 VNAA9905013 1 19990530 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 4, 5 & 6 DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 460PS 75716 38 3061 DURING THE POST FLIGHT INSPECTION, THE EMERGENCY LIGHTS AT ROWS 4, 5, AND 6 WERE NOTED TO BE INOPERATIVE. MAINTENANCE I NSPECTED AND REPLACED THE 5LK EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400314 19990604 00314 NM 1999 6 4 VNAA9905014 1 19990531 A 2150 5729C000 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PACK FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 459PS 7169 31449 3070 A LEFT HAND AIR CONDITIONING PACK OVERHEAT MESSAGE ILLUMINATED DURING THE TAXI OUT FOR TAKEOFF. THE CABIN FILLED WITH SMOKE. THE PACK WAS TURNED OFF AND THE SMOKE CLEARED THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT FOR A FERRY FLIGHT TO DAY FOR REPAIR. THE FERRY FLIGHT WAS CARRIED OUT WITHOUT ANY PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE LEFT HA ND AIR CONDITIONING ENVIROMENTAL CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-51-10. OPERATIONAL CHEC KS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999060400320 19990604 00320 CE 1999 6 4 CA990223013 1 19990217 A 3233 993880081 ACTUATOR BEECH 99 99A 1154003 CE PWA PT6 PT6A27 52043 EA LT MLG LEAKING W A UNSCHED LANDING K FLUID LOSS AP APPROACH 1 CA 0888 PCE40055 (CAN) NOSE GEAR DOWN AND LOCKED GREEN LIGHT DID NOT COME ON WHEN GEAR DOWN SELECTED. LANDING GEAR HAD TO BE LOWERED MAN UALLY. LEFT HAND MAIN GEAR ACTUATOR FOUND LEAKING. HYDRAULIC RESERVOIR LOW. 1 L 7 2 3T 4 T A14CE E4EA 1999060400322 19990604 00322 EA 1999 6 4 CA990223017 1 19990120 A 5753 C6WF110068 RIB C6WF10023 DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA TE FLAP LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 34073 310 PCE42181 (CAN) EXCESSIVE LOOSENESS NOTED BETWEEN THE TWO HALVES OF THE FLAP AT THE CENTER HINGE ARM POSITION. THE RIBS ON EITHER SIDE OF THE HINGE ARM ARE ASSEMBLED TO THE ARM BY THE USE OF LONG MS20470AD5 SOLID RIVETS. IT WOULD APPEAR THAT THERE HAS BEEN SOME WORKING BETWEEN THE RIVET HEADS AND THE OUTBOARD RIB WHICH HAD CAUSED WEARING OF THE RIB AROUND THE RIVET HOLES. 1 H 7 2 3T 4 T RT A9EA E4EA 1999060400324 19990604 00324 EA 1999 6 4 CA990223019 1 19990216 A 7410 MS250242 RELAY AGF26 DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 34088 PCE42181 (CAN) SUBMITTER STATED IT APPEARED THAT A HIGH NUMBER OF GLOW PLUGS WERE BEING USED OVER A SHORT TIME FRAME. ONE PARTIC ULAR SET WAS REPLACED IN OCTOBER AND CHECKED IN FEBRUARY. ONE ELEMENT WAS NOTED AS COMPLETELY MISSING. ENGINE CHECKED AND METAL BUILD-UP FOUND ON TURBINE, STATOR AND SHROUD. IT WAS FINALLY DETERMINED THE GLOW PLUGS MUST BE STAYING ON THR OUGH RELAY K7. RELAY REPLACED AND EVERYTHING NOW NORMAL. IT APPEARS THAT RELAY WAS CAUSING AN INTERMITTENT PROBLEM. 1 H 7 2 3T 4 T RT A9EA E4EA 1999060400426 19990604 00426 NE 1999 6 4 TWAA9907601 2 19990527 A 7260 7T0074 GEARBOX BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE LT ENGINE FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 715TW 28483 4901 THE LEFT ENGINE OIL PRESSURE DROPPED TO ZERO. OIL CONSUMPTION WAS NORMAL. SHUT THE ENGINE DOWN AND RETURNED TO STL. F OUND METAL IN THE OIL SYSTEM. REPLACED THE ENGINE. CHECK-C 4-24-99 LAX. *S/D* FAILURE WAS CAUSED BY THE ANGLE GEARBO X ASSEMBLY BEARING OPTION PART NUMBER 7T0074 AND/OR 7T0121. THIS WAS THE ONLY TWA ENGINE NOT INCORPORATING P&W PW2000 S ERVICE BULLETIN 72-561 WHICH REPLACES THIS BEARING OPTION BECAUSE OF INDUSTRY PROBLEMS. THE SB WILL BE INCORPORATED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999060400427 19990604 00427 WP 1999 6 4 TWAA9907603 1 19990528 A 3350 0105606005 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9401W 53137 DURING PREFLIGHT INSPECTION FOUND EGRESS LIGHT SEGEMENT BROKEN. REPLACED LIGHT SEGMENT. CC-02D 12-15-98 MCI. 2 L 7 2 4F RT A6WE 1999060400428 19990604 00428 NM 1999 6 4 TWAA9907604 1 19990527 A 3350 38931002 BATTERY PACK BOEING 727 727231 1384079 NM GALLEY DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54349 21968 DURING ROUTINE MAINTENANCE FOUND AFT GALLEY EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. CC-03 10-18-98 MCI. 2 L 7 3 4F A3WE 1999060400429 19990604 00429 WP 1999 6 4 TWAA9907605 1 19990529 A 3350 105607011 COVER DOUG DC9 DC983 3022083 WP CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9624T 53594 DURING ROUTINE MAINTENANCE FOUND ESCAPE PATH LIGHT COVERS MISSING. REPLACED MISSING LIGHT COVERS. 2 L 7 2 4F RT A6WE 1999060400430 19990604 00430 WP 1999 6 4 TWAA9907606 1 19990531 A 3350 105607011 COVER DOUG DC9 DC983 3022083 WP CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9413T 53188 DURING PREFLIGHT INSPECTION FOUND ESCAPE PATH LIGHTING COVER MISSING. REPLACED COVER. CC-01 9-1-98 STL. 2 L 7 2 4F RT A6WE 1999060400431 19990604 00431 NM 1999 6 4 HNAA9900061 1 19990530 A 3350 6013211X BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 908HA 5985 633 015 AFT OVERHEAD EMERGENCY LIGHT AND LT AFT EGRESS LIGHT INOP. RELAMPED, NO FIX. REMOVED AND REPLACED EMERGENCY LIGHT BATT ERY PS 3, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999060400432 19990604 00432 NM 1999 6 4 HNAA9900062 1 19990530 A 3150 T/O WARNING DHAV DHC8 DHC8102 2809003 NM COCKPIT ACTIVATED A HNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 07 921HA 089 WARNING HORN SOUNDED ON TAKE-OFF ROLL. FOUND FLAP NEEDLE AT BOTTOM OF ARC BUT STILL IN WHITE AERA. CYCLED FLAPS 5-15-5 , OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999060400433 19990604 00433 SO 1999 6 4 LR7A9943 1 19990412 A 5311 FRAME LKHEED 382 382G 526414U SO BS 817 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND FS 817E LT LOWER RING SEGMENT CRACKED AT WL 156. REPAIRED IAW SMP 583 53-40-3 8, 39. 2 H 7 4 4T A1SO 1999060400434 19990604 00434 SO 1999 6 4 LR7A9944 1 19990412 A 5311 FRAME LKHEED 382 382G 526414U SO BS 817 UNSERVICEABLE A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND FS 817E RT LOWER RING SEGMENT PREVIOUS REPAIR AT WL 156 NOT PER SRM. REPAIRED IAW SMP 583 53-40-38, 39. 2 H 7 4 4T A1SO 1999060400435 19990604 00435 SO 1999 6 4 LR7A9945 1 19990529 A 5320 34319321 STRUT LKHEED 382 382G 526414U SO BS 792 & 814 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 4590 DURING CARGO OFF LOADING AT PATP, WINCH CABLE BROKE AND CARGO SHIFTED RESULTING IN IMPACT DAMAGE TO RT STRUTS AT FS 792 AND 814. FERRIED UNPRESSURIZED WITH NO CARGO ABOARD TO ANC. REPLACED FS 792 AND 814 STRUTS PER SRM 51-10, PG 4. 2 H 7 4 4T A1SO 1999060400436 19990604 00436 SO 1999 6 4 LR7A9946 1 19990530 A 5230 3724053 RAMP LKHEED 382 382G 526414U SO BS 802 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING CONSTRUCTION EQUIPMENT LOADING AT FAI, CARGO RAMP ASSY TAIL SKID AND T/E SECTION DAMAGED. FERRIED UNPRESSURIZED WITH NO CARGO LOAD TO ANC. CARGO RAMP ASSY REMOVED FOR REPAIR. 2 H 7 4 4T A1SO 1999060400437 19990604 00437 WP 1999 6 4 PNSA990502 2 19990531 A 7200 31032021 GASKET SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE RUPTURED A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 640PA AC759B P44691 DURING CLIMBOUT, RT ENGINE FIRE LIGHTS ILLUMINATED. ENGINE WAS SECURED AND AIRCRAFT RETURNED FOR AN UNEVENTFUL LANDING. P-3 GASKET AT THE 4 O'CLOCK (FACING FORWARD) PRIMARY NOZZLE BLANK OUT PLUG WAS FOUND BLOWN OUT. REPLACED GASKET, FLI GHT CHECK WAS SATISFACTORY. 2 L 7 2 4T 4 T RT A8SW E4WE 1999060400438 19990604 00438 SW 1999 6 4 PNSA990503 1 19990508 A 7722 8974691 HARNESS SWRNGN SA227 SA227AC 8780603 SW LT EGT FAILED A PNSA K NONE O OTHER CR CRUISE 1 AL 03 41NE AC741B LT EGT STARTED TO FLICKER DURING CRUISE. COULD NOT DUPLICATE PROBLEM ON GROUND. REPLACED EGT HARNESS FOR TROUBLESHOOT ING. 2 L 7 2 4T RT A8SW 1999060400439 19990604 00439 WP 1999 6 4 PNSA990504 2 19990510 A 7322 2719149003 INDICATOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE EGT MALFUNCTIONED A PNSA O OTHER N FALSE WARNING CR CRUISE 1 AL 03 41NE 3821 AC741B LT ENGINE POWER FLUCTUATING DURING CRUISE. AIRCRAFT WAS FERRIED BACK TO ANC FOR MAINTENANCE. REPLACED EGT INDICATOR, O PERATIONAL CHECK OK. AIRCRAFT EXPERIENCED NO FURTHER PROBLEMS. 2 L 7 2 4T 4 T RT A8SW E4WE 1999060400440 19990604 00440 WP 1999 6 4 PNSA990505 2 19990519 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RIGHT SURGED A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 AL 03 41NE AC741B RT ENGINE SURGED ON TAKEOFF. TAKEOFF WAS ABORTED. PILOT DETERMINED THE ENGINE HAD SURGED DUE TO TEMP LIMITER BYPASS. S ECOND TAKEOFF WAS NORMAL NO FURTHER PROBLEMS NOTED. 2 L 7 2 4T 4 T RT A8SW E4WE 1999060400441 19990604 00441 NM 1999 6 4 RAAA99B1004 1 19990529 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 14 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PASSENGER ROW 14 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999060400442 19990604 00442 NM 1999 6 4 RAAA99B1005 1 19990529 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 10 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PASSENGER ROW 10 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999060400443 19990604 00443 NM 1999 6 4 RAAA99B1006 1 19990529 A 3530 4566M37B042NM PBE BOEING 727 72722C 138400F NM ROW 22 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 FOUND PASSENGER ROW 22 PBE POUCH SOFT AND SEAL BROKEN DURING SERVICE CHECK. CHANGED PBE DUE POUCH VACUUM LOST. 2 L 7 3 4F A3WE 1999060400444 19990604 00444 NM 1999 6 4 RAAA99B2043 1 19990526 A 3350 873100212 LIGHT BOEING 727 72722C 138400F NM RT EMER EXIT BROKEN A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 DURING DAILY SERVICE CHECK, FOUND FORWARD RIGHT HAND OVER WING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT TO HAVE A BROKEN S CREW AND CASE. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1999060400445 19990604 00445 GL 1999 6 4 CALA9900582 2 19990526 A 7260 SEAL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL ACCY GEARBOX LEAKING A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 12080 47981 F/A REPORTED SMOKE WITH AN OILY SMELL IN THE CABIN APPROX 30 MIN AFTER TAKEOFF. THE SMOKE CHECKLIST WAS ACCOMPLISHED WI TH THE SMOKE AND ODOR DISSIPATING AFTER THE NR 2 ENGINE BLEED WAS SHUTOFF AND THE NR 2 PACK WAS SUPPLIED BY THE 1-2 ISOL VALVE. THE FLT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT PROBLEM. MX FOUND OIL RUNNING LEAK FROM PORT B NR 2 ENGIN E DRAIN MAST, FUEL PUMP PORT. THE ACCESSORY GEARBOX CARBON SEAL FOR FUEL PUMP PAD WAS REMOVED AND REPLACED IAW MM 72-65 -00, PAGE 803-805. THE FUEL PUMP CONTROL PACKAGE WAS REMOVED AND REPLACED IAW MM 73-12-01 PG 202A-215. LEAK AND OPERAT IONAL CHECKS WERE PERFORMED IAW MM 71-00-00 AND ALL CHECKS WERE GOOD. 2 L 7 3 4F 4 F A22WE A23EA 1999060400446 19990604 00446 NM 1999 6 4 CALA9900583 1 19990530 A 3230 SPACER BOEING 737 7373T0 1384582 NM LANDING GEAR JAMMED A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 13331 23569 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE OVERRIDE TRIGGER WAS PULLED AND THE GEAR THEN RETRACTED NORMALLY. THE FLIGHT WAS CONTINUED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR LOCK LEVER SYSTEM AND TROUBLESHOT PER MM 32-31-21. MAINTENANCE FOUND TELEFLEX CABLE BINDING DUE TO SISSOR LINK SPACER JAMME D. THE SPACER WAS REMOVED AND REPLACED, THE CABLE WAS LUBRICATED. THE LEVER LOCK SYSTEM OPERATED NORMALLY IAW MM 32-31 -11. 2 L 7 2 4F RT A16WE 1999060400447 19990604 00447 NM 1999 6 4 CALA9900584 1 19990528 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 344-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND SEAT TRACK CORRODED AT STA 344-360, LBL 40. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-52 , FIGURE 202. 2 L 7 2 4F RT A16WE 1999060400448 19990604 00448 NM 1999 6 4 CALA9900585 1 19990528 A 3350 3004321 LIGHT GRIMES BOEING 737 7373T0 1384582 NM R2 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND THE R-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED IAW MM 33-51-22. 2 L 7 2 4F RT A16WE 1999060400449 19990604 00449 NM 1999 6 4 CALA9900586 1 19990529 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10323 23374 INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 344, LBL 36 TO RBL 12. A NEW SECTION OF FLOORBEAM AND DOUBLERS WERE INST ALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999060400450 19990604 00450 NM 1999 6 4 CALA9900587 1 19990531 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 50 TO LBL 30. REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999060400451 19990604 00451 WP 1999 6 4 CALA9900588 1 19990531 A 3350 CANAC4A LIGHT SELFPOWERED DOUG DC9 DC932 3022066 WP ROW 15-16 & 25 DIM A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND THREE SELF ILLUMINATING EXIT SIGNS WITH LOW LIGHT LEVEL AT ROW 15-16 AND ROW 25. THE SIGNS WERE REPLAC ED IAW MM 25-63-0. 2 L 7 2 4F A6WE 1999060400452 19990604 00452 WP 1999 6 4 CALA9900589 1 19990531 A 5320 RIB DOUG DC9 DC932 3022066 WP LT MLG WW GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT MLG WELL CLOSURE RIB GOUGED JUST ABOVE LOCK DOT NR 2. A NEW PLATE AND SPLICES WERE INSTALLED IAW SR M 51-10-2. 2 L 7 2 4F A6WE 1999060400453 19990604 00453 WP 1999 6 4 CALA9900590 1 19990531 A 5753 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT FLAP LOWER TRAILING EDGE AREA DENTED INBOARD OF INBOARD ACTUATOR AREA. A DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 51-30-00. 2 L 7 2 4F A6WE 1999060400454 19990604 00454 NM 1999 6 4 CALA9900591 1 19990531 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 FROM BL 0 TO RBL 70. REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999060400455 19990604 00455 WP 1999 6 4 CALA9900592 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1876-1810 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1876 TO 1810 AT POSITION X = 0.36L AND X = 0.36R. TH E BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400456 19990604 00456 WP 1999 6 4 CALA9900593 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1887-1839 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1887 TO 1839 AT POSITION X = 0.03L AND X + 0.03R. TH E BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400457 19990604 00457 WP 1999 6 4 CALA9900594 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1866 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1866, POSITION X = 0.03L TO X = 0.28L AND POSITION X = 0.03R TO X = 0.28R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00 FIGURE 10. 2 L 7 3 4F A22WE 1999060400458 19990604 00458 WP 1999 6 4 CALA9900595 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.27R TO X = 0.53R. THE BEAM SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400459 19990604 00459 WP 1999 6 4 CALA9900596 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.60R TO 0.90R. THE CORRODED SECTION OF BEAM WAS REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400460 19990604 00460 WP 1999 6 4 CALA9900597 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1996-1903 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1996 TO 1903 AT POSITION X = 0.20R AND X = 0.20L. TH E CORRODED BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400461 19990604 00461 WP 1999 6 4 CALA9900598 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 2007-1876 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1876 AT POSITION X = 0.25R AND X = 0.25L. TH E CORRODED SECTIONS OF BEAM WERE REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400462 19990604 00462 WP 1999 6 4 CALA9900599 1 19990601 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 2007-1893 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1893 AT POSITION X = 0.60L AND X = 0.60R. TH E CORRODED BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400463 19990604 00463 WP 1999 6 4 CALA9900600 1 19990601 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1876 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27L TO X = 0.38L. THE FLOORBEAM CAP PING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400464 19990604 00464 WP 1999 6 4 CALA9900601 1 19990601 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1876 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.04L TO X = 0.22L. THE FLOORBEAM CAP PING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400465 19990604 00465 WP 1999 6 4 CALA9900602 1 19990601 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1876 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.60R TO X = 0.90R AND POSITION X = 0 .60L TO X = 0.90L. THE FLOORBEAM CAPPING SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400466 19990604 00466 WP 1999 6 4 CALA9900603 1 19990601 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1876 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X =0.04R TO X = 0.22R. THE FLOORBEAM CAPP ING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400467 19990604 00467 WP 1999 6 4 CALA9900604 1 19990601 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1876 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27R TO X = 0.33R AND POSITION X = 0. 38R TO X = 0.56R. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400468 19990604 00468 WP 1999 6 4 CALA9900605 1 19990601 A 5312 BULKHEAD TEE DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND T-SECTION ON FORWARD FACE OF REAR PRESSURE BULKHEAD AT STA 2007 FROM POSITION X = 0.55L TO X = 0.65L CO RRODED. THE CORRODED SECTION WAS REMOVED AND A SPLICE REPAIR WAS INSTALLED IAW SRM 53-40-00, FIGURE 16. 2 L 7 3 4F A22WE 1999060400469 19990604 00469 WP 1999 6 4 CALA9900606 1 19990601 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 1866-1856 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74R. THE CORRODED SECTION FOR SEAT TRAC K WAS REPLACED IAW SRM 53-70-00, FIGURE 6. 2 L 7 3 4F A22WE 1999060400470 19990604 00470 WP 1999 6 4 CALA9900607 1 19990601 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 1876-1866 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1876-1866 AT POSITION X = 0.60R AND X = 0.60L. THE SEAT TRACK SECTIONS WERE REPAIRED IAW SRM 53-70-00, FIGURE 6. 2 L 7 3 4F A22WE 1999060400471 19990604 00471 NM 1999 6 4 CALA9900608 1 19990601 A 5755 651734781A SKIN BOEING 727 727224 1384076 NM NR 1 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND NR 1 SPOILER PANEL UPPER SKIN DELAMINATED. THE SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-61-81. 2 L 7 3 4F A3WE 1999060400472 19990604 00472 WP 1999 6 4 CALA9900609 1 19990601 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 218 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 AT LONGERON 18L. THE DENTED AREA WAS REPAIRED IAW ECRA 5330-02817. 2 L 7 2 4F A6WE 1999060400473 19990604 00473 WP 1999 6 4 CALA9900610 1 19990602 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1903 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1903 FROM POSITION X = 0.25L TO X = 0.25R. THE FLOOR SUPPOR T BEAM WAS REPLACED IAW 53-16-00, FIGURE 10. 2 L 7 3 4F A22WE 1999060400474 19990604 00474 WP 1999 6 4 CALA9900611 1 19990602 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 1866-1856 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74L. THE SECTION OF SEAT TRACK WAS REPA IRED IAW SRM 53-70-00, FIGURE 6. 2 L 7 3 4F A22WE 1999060400475 19990604 00475 WP 1999 6 4 CALA9900612 1 19990602 A 5712 RIB DOUG DC9 DC932 3022066 WP LT MLG WW GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND TWO GOUGES IN RIB AT LEFT MLG WELL JUST FORWARD OF GEAR DIAGONAL BRACE. THE GOUGED AREA WAS CUT OUT IA W SRM 51-00-00 AND A NEW ANGLE AND SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999060400476 19990604 00476 WP 1999 6 4 CALA9900613 1 19990602 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 437 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FUSELAGE SKIN DENTED BELOW WINDOW NR 12 (STA 437) AT STRINGER 15R. A DOUBLER AND FINGER DOUBLER REPAIR WAS INSTALLED IAW DOUGLAS DRAWING J060109, SRM 51-10-3 AND ECRA 5330-02815. 2 L 7 2 4F A6WE 1999060400477 19990604 00477 NM 1999 6 4 CALA9900614 1 19990602 A 5720 ANGLE BOEING 727 727224 1384076 NM WS 92 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND A .3125 INCH CRACK IN DOUBLER ANGLE AT RT WING FRONT SPAR WBL 92. THE ANGLE AND STIFFENER WERE REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, FIGURE 4. 2 L 7 3 4F A3WE 1999060400478 19990604 00478 NM 1999 6 4 UPS99429692 1 19990601 A 5400 FITTING BOEING 747 747123 1384873 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A, NR 3 PYLON STRUCTURE FWD OF DIAGONAL BRACE FITTING IS CRACKED AROUND HI-LOK. *S/D* STOP DRILLED C RACK ENDS TO .250 IAW SRM 54-10-05 FIG 2 SHT 2. INSTALLED WEB REPAIR IAW SRM 54-10-03 FIG 2. 2 L 7 4 4F A20WE 1999060400479 19990604 00479 NM 1999 6 4 UPS99429693 1 19990601 A 5411 65B90411604 FRAME BOEING 747 747123 1384873 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A, NR 3 PYLON FRAME CRACKED FWD END OF DIAG BRACE FWD ATTACH FITTING, I/B SIDE APPROX PYLON STA 292, A PPROX 2 INCH LONG, FROM BOTTOM END OF FRAME. *S/D* REMOVED DAMAGED RIB (P/N 65B90411-604) AND REPLACED WITH RIB (P/N 6 5B90411-604) AND BONDING ADHESIVE IAW SRM 51-30-02. HOT BOND OF RIB ACCOMPLISHED IAW B747 SRM 51-40-06. 2 L 7 4 4F A20WE 1999060400480 19990604 00480 NM 1999 6 4 UPS99429694 1 19990601 A 5411 FRAME BOEING 747 747123 1384873 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE:N/A, NR 3 PYLON FRAME CRACKED, FWD END OF DIAG BRACE FWD ATTACH FITTING, O TB SIDE, APPROX PYLON STA 292 . THE CRACK IS APPROX 1.5 INCH LONG, FROM BOTTOM END OF FRAME. 2 L 7 4 4F A20WE 1999060400481 19990604 00481 NM 1999 6 4 UPS99629695 1 19990601 A 3030 PITOT HEAT BOEING 767 76734AF 1385212 NM LT FUSELAGE INOPERATIVE A IPXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 307UP 27760 INSPECTION TYPE:ETOP EICAS MESSAGE CAPT PITOT DISPLAYED AND CAPT PITOT PROBE HEAT LIGHT ILLUMINATED AFTER ENGINE START. REPLACED CAPT PITOT PROBE IAW MM 34-11-01. 2 L 7 2 4F RT A1NM 1999060400482 19990604 00482 EU 1999 6 4 QXEA9901077 1 19990527 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 496US 11169 SEA- FORWARD SEAT MOUNTED EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CARTRIDGE, LIGHT OPERATION CHECKS GOO D. 2 L 7 2 4F RT A20EU 1999060400483 19990604 00483 EU 1999 6 4 QXEA9901078 1 19990529 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU EXTERIOR DIRTY A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 497US 11173 PDX- RIGHT HAND AFT WING/BELLY FAIRING EVACUATION LIGHT INOPERATIVE. CLEANED CONTACTS FOR RIGHT HAND AFT WING/BELLY FAI RING LAMP SOCKET. NO PARTS REPLACED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999060400484 19990604 00484 NM 1999 6 4 99FDEA00200 1 19990519 A 5530 SUPPORT BOEING 727 72722 1384002 NM VERT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 ANGLE RIB SUPPORT CRACKED IN VERTICAL STAB LT CORNER. INSTALLED DOUBLER PER SRM 51-40-3 AND 53-10-9 PG 11. FABRICATED, DRILLED, PRIMED AND SEALED ACCESS HOLE DOUBLER PER SRM 51-40-2. OPS CHECK PERF ON CARD 70C027-00. 2 L 7 3 4F A3WE 1999060400485 19990604 00485 NM 1999 6 4 99FDEA00201 1 19990601 A 5720 CHORD BOEING 727 72722 1384002 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 NR 3 FUEL CELL (NR 2 TANK) BULGED WEB AND POPPED FASTENERS UPPER CHORD BS 870. REMOVED AND REPLACED PER EA 7-5710-43038 A, DATED 5/24/99. 2 L 7 3 4F A3WE 1999060400486 19990604 00486 NM 1999 6 4 99FDEA00202 1 19990601 A 5315 652083430 FLOORBEAM BOEING 727 727247 138408F NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-224-01,3) ON UPPER SURFACE OF UPPER CHORD BS 1130, RBL 47-49, WL 208. *S/D* REMOVED AND REPLACED CORROS ION, FLAP PEENED AREA AND INSTALLED REPAIR STRAP PER FEDEX EA 7-5310-45275. 2 L 7 3 4F A3WE 1999060400487 19990604 00487 NM 1999 6 4 99UAL900288 1 19990521 A 2497 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT CHAFED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 349UA 24253 ACCUMULATION OF SMOKE IN THE FLIGHT DECK. *S/D* WIRE W276-090-14 WAS FOUND CHAFED AGAINST BRACKET 65-55704-4, LOCATED ABOVE THE P6-1 LOAD CONTROL PANEL. DAMAGE THE RESULT OF INADEQUATE BUNDLE CLEARANCE FOLLOWING PREVIOUS SHEET METAL REPA IR. WIRE REPAIRED AND BUNDLE RELOCATED TO PROVIDE CLEARANCE. CIRCUIT BREAKERS C824 AND C755 REPLACED PRECAUTIONARY. S UPPORT BRACKET BLENDED TO REMOVE MINOR ARCHING DAMAGE. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999060400488 19990604 00488 NM 1999 6 4 99UAL900289 1 19990521 A 2612 1061096115 FIRE SENSOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE MALFUNCTIONED A UALA A F E UNSCHED LANDING ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 WP 29 991UA 2106 21981 NR 2 ENGINE FIRE WARNING. *S/D* THE SENSOR ON THE BOTTOM OF NR 2 ENGINE WAS BAD. REPLACED SENSOR PER MM 26-11-02, OPE RATES NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1999060400489 19990604 00489 NM 1999 6 4 99UAL900290 1 19990521 A 5270 SENSOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE PASSENGER DOOR OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 920UA 25387 FORWARD ENTRY DOOR WARNING LIGHT ILLUMINATED. *S/D* PROXIMITY SENSOR TARGET OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SEN SOR TARGET, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999060400490 19990604 00490 NM 1999 6 4 99UAL900292 1 19990522 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 600-660 DAMAGED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 503UA 24624 DURING THE HEAVY MAINTENANCE VISIT, THE FUSELAGE CROWN SKIN AREA BETWEEN BS 600 AND BS 660 AND BETWEEN S-4L AND S-4R WA S FOUND TO HAVE DAMAGE. A MAJOR REPAIR IS REQUIRED TO CORRECT DAMAGED AREA. *S/D* CAUSE NOT IDENTIFIED. REPAIRED CRO WN WITH EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 1999060400491 19990604 00491 NM 1999 6 4 99UAL900293 1 19990512 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1692 DAMAGED A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 595UA 28748 FUSELAGE SKIN AT BS 1692, STR 20L RECEIVED DAMAGE FROM A SERVICE TRUCK. THE RESULTING DAMAGE IS ELEVEN INCHES LONG INCL UDING A 2.75 INCH TEAR IN THE SKIN. THERE WAS NO DAMAGE TO THE UNDERLYING STRUCTURE. *S/D* DAMAGE CAUSED BY CONTACT F ROM SERVICE TRUCK. DAMAGED AREA WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED BASED ON 757 SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 1999060400492 19990604 00492 NM 1999 6 4 99UAL900294 1 19990526 A 2150 ACM AIR RESEARCH AR2040751 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AC COMPT FAILED A UALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 WP 29 7299U 21894 UNABLE TO CONTROL CABIN PRESSUSE. RETURNED TO PHX. DUMPED FUEL. *S/D* CAUSE NOT DETERMINED. REPLACED AIR CYCLE MACH INE AND ACCOMPLISHED PRESSURIZATION CHECK. 2 L 7 3 4F 4 F A3WE E2EA 1999060800001 19990608 00001 NM 1999 6 8 TSAA9933236 1 19990425 A 3350 8731002511 LIGHT BOEING 737 7372M6C 1384708 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED AFT SERVICE DOOR EMERGENCY SLIDE LIGHT ASSY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999060800002 19990608 00002 EA 1999 6 8 COMA9960155 1 19990413 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA K NONE O OTHER LD LANDING 1 SO 01 965CA 4368 1076 7131 FLAPS FAILED AFTER LANDING. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999060800003 19990608 00003 SO 1999 6 8 COMA9910078 1 19990510 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 01 152CA 9257 1152 FLAP CONTROL FAULT AT 80 KTS ON TAKEOFF. REPLACED RIGHT INBOARD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1999060900001 19990609 00001 NM 1999 6 9 SWAA990841 1 19990508 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM ROW 14 EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 EMERGENCY EXIT TRACK LIGHTING HAS WIRES EXPOSED AT ROW 14. REMOVED AND REPLACED FLOOR TRACK LIGHTING ASSY PER MM. 2 L 7 2 4F RT A16WE 1999060900002 19990609 00002 NM 1999 6 9 SWAA990819 1 19990505 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACKED CENTER FLOORBEAM AT BS 663, BL O. REPAIRED BEAM PER SWA RA 1-357-06 79, AND ACO 658-57. 2 L 7 2 4F RT A16WE 1999060900003 19990609 00003 WP 1999 6 9 ABXA9900370 1 19990422 A 5753 9957578508 SKIN DOUG DOUG DC9 DC931 3022065 WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK, FOUND LEFT WING UPPER FLAP SKIN CORRODED. REPLACED UPPER FLAP SKIN IAW DC9 SRM 51-30-2 AND 51-30-4. 2 L 7 2 4F A6WE 1999060900004 19990609 00004 EU 1999 6 9 RAIA990424 1 19990416 A 2421 23095002 GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 574HK 41093 FLT 7452 - STL - RIGHT GENERATOR FAILED. MAINTENANCE REPLACED GENERATOR ON RIGHT ENGINE. (M) 2 L 7 2 4T RT A41NM 1999060900005 19990609 00005 NM 1999 6 9 DL72E991078 1 19990517 A 5330 SKIN BOEING 727 727247 138408F NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 GOUGES WERE FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE WAS LOCATED BETWEEN S24 AND S 24+5 INCHES. REPAIRED PER ERA 333109-14, REV A. 2 L 7 3 4F A3WE 1999060900006 19990609 00006 NM 1999 6 9 DL72E991079 1 19990517 A 5314 65571987 KEEL BEAM BOEING 727 727247 138408F NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING INSPECTION OF THE LWR KEEL BEAM PER EO 4-64433-3, A CRACK WAS FOUND IN THE WEB (ONLY) JUST ABOVE THE VERT FLANGE OF THE LT SIDE BEAM. REPAIRED PER ERA 333113-14, REV B. 2 L 7 3 4F A3WE 1999060900008 19990609 00008 WP 1999 6 9 AT9900386 1 19990415 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 313-389 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 823AT 47529 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION UNDER FASTENERS ON BOTH SIDES OF PANEL NR 5851 AT BS 313 T O 389. FABRICATED NEW PANEL WEB AND FIVE SECTIONS HAT CHANNELS, TRIMMED, DRILLED, DEBURRED, COUNTERSUNK, ASSEMBLED, TRE ATED AND PRIMED IAW DC9 SRM 51-10-2, 51-30-2, 51-10-3, 53-21-0, 53-10-3 AND 53-21-0 FIG 3. 2 L 7 2 4F A6WE 1999060900010 19990609 00010 EA 1999 6 9 COMA9960233 1 19990521 A 2120 DUCT CNDAIR CL600 CL6002B19 EA E & E COMPT LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 986CA 7174 DISPLAY COOL CAUTION MESSAGE. CONNECTED LOOSE AVIONICS COOLING DUCT. 2 L 7 2 4F RT A21EA 1999060900011 19990609 00011 1999 6 9 COMA9960234 4 19990523 A 2210 AUTO PILOT CNDAIR CL600 CL6002B19 EA E & E COMPT MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 975CA 7150 WHEN AUTO PILOT WAS DISCONNECTED FOR APPROACH, THE ELEVATORS WERE STUCK BETWEEN +1 DEGREES AND -1 DEGREES OF TRAVEL. AF TER FORCING 3 TIMES THE ELEVATORS RELEASED. DEFERRED AUTO PILOT SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 1999060900012 19990609 00012 NE 1999 6 9 SWAA990877 2 19990515 A 7320 1853M56P06 HMU BOEING 737 7377H4 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 07 704SW 27838 AIR TURNBACK, LEVEL FLIGHT 11,000 FT, THROTTLE REDUCED TO CRUISE SETTING. SEVERE VIBRATION IN NR 2 ENGINE. POWER RETAR DED AND ENGINE VIBRATION STOPPED. REMOVED AND REPLACED NR 2 ENGINE HMU PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 1999060900013 19990609 00013 NE 1999 6 9 SWAA990915 2 19990524 A 7320 1853M56P06 HMU BOEING 737 7377H4 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 07 745SW 29491 WHEN REDUCING POWER LEVERS FROM CLIMB TO CRUISE THRUST, ENGINES DEVELOPED A HARMONIC RESISTANCE RESULTING IN AIRCRAFT SH AKING AGGRESSIVELY. SHAKING STOPPED WHEN POWER WAS PULLED BACK DOWN TO 85 PERCENT N1. REMOVED AND REPLACED NR 2 ENGINE HMU AND AIRCRAFT VIBRATION MONITOR, (P/N 6672M213), (S/N DA72) PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 1999060900014 19990609 00014 NM 1999 6 9 SWAA990909 1 19990524 A 2560 655743 BRACKET BOEING 737 7373H4 1384600 NM PASSENGER DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FWD AND AFT GIRT BAR ATTACH BRACKETS AT FWD ENTRY DOOR FLOOR. REMOVED A ND REPLACED BRACKET ASSYS PER MM. 2 L 7 2 4F RT A16WE 1999060900015 19990609 00015 NM 1999 6 9 DL72E991150 1 19990521 A 5330 65545906 SKIN BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 FUSELAGE SKIN FOUND WITH CORROSION AT BS 720E AND S26R. ONLY THE LOWER (OVERLAPPED) SKIN WAS DAMAGED. REPAIRED PER ERA 333122-14, REV B. 2 L 7 3 4F A3WE 1999060900016 19990609 00016 NM 1999 6 9 DL72E991151 1 19990521 A 5330 65C139131 SKIN BOEING 727 727247 138408F NM BS 950 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 LOWER SKIN BELOW THE WING TO BODY FAIRING AT BS 950D BETWEEN S26R AND S27R WAS FOUND DAMAGED DUE TO A LOOSE FASTENER. R EPAIRED PER ERA 333123-14, REV A. 2 L 7 3 4F A3WE 1999060900017 19990609 00017 NM 1999 6 9 DL72E991152 1 19990521 A 5330 65182195 SKIN BOEING 727 727247 138408F NM BS 380 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING HMV, A T/L REPAIR WAS REMOVED AND ADDITIONAL DAMAGE WAS NOTED (BELOW AND AFT OF ORIGINAL DAMAGE). BOTH DAMAGES W ILL BE REPAIRED VIA ONE REPAIR SCHEME. REPAIRED PER ERA 300413-14, REV D. 2 L 7 3 4F A3WE 1999060900018 19990609 00018 NM 1999 6 9 DL72E991153 1 19990521 A 5311 651632678 FRAME BOEING 727 727247 138408F NM BS 784 MISDRILLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 WHILE PERFORMING REPETITIVE INSP PER OPN 5865 REQD BY AD 94-02-04 (REF 4-61904-3AD/-12AD) AN OVERSIZED FASTENER HOLE WAS FOUND IN THE RT BS 784 FRAME, I/B CHORD. THE SUBJECT HOLE IS THE 2ND BELOW THE FLOOR LINE. NO CRACKS WERE FOUND. REW ORKED PER ERA 333135-14AD, REV A. 2 L 7 3 4F A3WE 1999060900019 19990609 00019 NM 1999 6 9 DLM90991197 1 19990527 A 2170 V1211 COALESCER BAG V1211 DOUG MD90 MD9030 3023690 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 908DA 53388 OILY SMELL FROM AIR CONDITION SYSTEM AFTER TAKEOFF. REMOVED ACCESS PANEL AND INSULATION BARRIER FOR H2O SEPARATOR BAGS. REPLACED H2O SEPARATOR BAGS, RUN LEAK CK AND OPERATIONAL NORMAL. REINSTALLED PANELS. CHECKED A/C AND APU FOR LEAKS, CHECKED OK. CLEANED APU INLET AND DOOR ASSY, PERFORMED DUCT BURN OUT, RAN PACKS AND NO ODORS. 2 L 7 2 4F RT A6WE 1999060900020 19990609 00020 NM 1999 6 9 DL72E991198 1 19990513 A 5753 652163241 SPAR BOEING 727 727247 138408F NM NR 2 TE MIDFLAP MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 830WA 21482 NR 2 MIDFLAP / UPPER SPAR CHORD / WBL 124 / ALT FAST INSTL. DURING ACCOMPLISHMENT OF EO 4-58705-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED COLLAR AT ONE OF THE MOD FASTENER HOLES DUE TO PROXIMITY OF HOLE TO SPAR FILLET RADIUS. AUTHORIZED USE OF MINI-NUT AND RADIUS BLOCK TO FACILITATE FASTENER INSTL. 2 L 7 3 4F A3WE 1999060900021 19990609 00021 WP 1999 6 9 TWAA9907602 1 19990520 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1003 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 DURING CHECK-C MAINT, FOUND FUSELAGE LONGERON 20R CRACKED AT FASTENER, UPPER O/B CORNER OF THE WHEEL WELL AT STA 1003. S TOP DRILLED CRACK PER SRM 51-00-03 AND REPAIRED PER ARA 16170. 2 L 7 2 4F A6WE 1999061000001 19990610 00001 WP 1999 6 10 AT9900272 1 19990330 A 7603 MS244665151 HARDWARE DOUG DC9 DC932 3022066 WP NR 2 ENGINE FCU MISSING A ZZDA E ENGINE SHUTDOWN F FLT CONT AFFECTED CL CLIMB 1 SW 07 813AT 47318 ON CLIMBOUT, NR 2 ENGINE AT POWER BACK UNABLE TO REDUCE POWER BELOW MAXIMUM CLIMB. THROTTLE MOVEMENT NORMAL BUT POWER R EMAINS AT MAXIMUM CLIMB AFTER BEING RETARDED, NO RESPONSE. DIVERTED TO CHICAGO O'HARE AND DECLARED EMERGENCY. OPENED N R 2 ENGINE COWLING AND FOUND POWER LEVER CONTROL TO FCU WITH HARDWARE DETACHED. REINSTALLED BOLT, WASHER, NUT AND COTTE R KEY IAW DC9 MM 73-20-1. NO PROBLEM ENCOUNTERED DURING ENGINE RUN, ALL INSTRUCTIONS AND READINGS ON BOTH ENGINE THE SA ME. 2 L 7 2 4F A6WE 1999061000002 19990610 00002 NM 1999 6 10 99UAL900169 1 19990318 A 3397 WIRE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 163UA 21353 E-ZONE EMERGENCY FLOOR LIGHT INOP AND 1L CROSS AISLE EMERGENCY LIGHT INOP. REPAIRED WIRES AND CHECKED OK. 2 L 7 4 4F 4 F A20WE E20EA 1999061000005 19990610 00005 WP 1999 6 10 DLL14990670 1 19990326 A 2612 FIRE WIRE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 2 ENGINE CHAFED A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 741DA 193C1245 014707 INTERMITTENT FIRE WARNING A LOOP NR 2 ENG OCCURRED AFTER T/O AT 1500 FT AGL, EPR 1.631 OAT 11 DEG C. NR 2 IDG DISCONNEC TED, HYD PUMPS B1 C1 UNLATCHED, NO FIRE. REPAIRED WIRES FROM SPLITTER TO LOOP. 2 L 7 3 4F 4 F A23WE E12EU 1999061000006 19990610 00006 NM 1999 6 10 DL72S990672 1 19990326 A 7910 LINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LOOSE A DALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SO 27 540DA 22386 687335 NR 1 GEN ON MCO. ON T/O FROM FLL LOST NR 2 GEN, WAS ABLE TO GET NR 2 GEN BACK ON LINE BUT LOW PRESS LIGHT WAS FLICKERIN G AND OIL TEMP WAS HIGH. FOUND OIL LEAK AT COOLER, TIGHTENED LINE. 2 L 7 3 4F 4 F A3WE E2EA 1999061000009 19990610 00009 NE 1999 6 10 RAIA990405 2 19990401 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FLAMED OUT A RAIA E ENGINE SHUTDOWN O OTHER LD LANDING 1 CE 03 574HK 7223 41093 76115 FLT 7460 - STL - RIGHT ENGINE FLAMED OUT AFTER LANDING. MAINTENANCE PERFORMED MAINTENANCE ENGINE RUN, NO DEFECTS NOTED. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999061000010 19990610 00010 NE 1999 6 10 RAIA990341 2 19990301 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FLAMED OUT A RAIA E ENGINE SHUTDOWN X ENGINE FLAMEOUT LD LANDING 1 CE 03 574HK 7157 41093 76115 FLT 7458 - STL - RIGHT ENGINE FLAMED OUT ON LANDING. MAINTENANCE PERFORMED GROUND RUN, NO DEFECTS NOTED. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999061000012 19990610 00012 1999 6 10 CA950929008 4 19990509 A 2565 18307523 VALVE AIRCRUISERS D17862101 BAG BAE146 BAE146200A 1500266 EU ESCAPE SLIDE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) INFLATION CYLINDER AND VALVE ASSY SENT OUT FOR OVERHAUL AND INCORPORATION OF SB 210-25-13. VALVE REINSTALLED AND RECHARGED. DURING RECHARGE, THE VALVE BLEW APART AT 2,000 PSI, CREATING A LIFE THREATENING SITUATION. THE FAILURE OCCU RRED AT THE THREADED PORTION OF THE BOTTLE FITTING ON THE VALVE SIDE OF THE FITTING. VALVE RETURNED TO MANUFACTURER FOR INVESTIGATION. INVESTIGATION COULD NOT DETERMINE THE EXACT CAUSE OF THE FAILURE. POSSIBLY AN OVERTORQUE OF THE BOTTLE FITTING BY PUTTING A WRENCH ON THE VALVE BODY INSTEAD OF THE FITTING HEX, ALONG WITH A POSSIBLE MATERIAL FLAW. HOWEVER , THE FITTING PASSED ALL THE COMPANY TESTS. IT COULD ALSO HAVE BEEN AN UNKNOWN SHOCK LOAD ON THE VALVE BODY. 2 H 7 4 4F RT A49EU 1999061000015 19990610 00015 NM 1999 6 10 CALA9900433 1 19990401 A 3397 BR964412 WIRE BOEING 737 7373T0 1384582 NM ROW 16 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12319 23370 EMERGENCY EXIT AISLE PATH LIGHT AT ROW 16 INOP. REMOVED AND REPLACED LIGHT SOCKET FOR AISLE PATH EMERGENCY EXIT LIGHT A T ROW 16. LIGHT OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1999061100001 19990611 00001 NM 1999 6 11 TWAA9907701 1 19990528 A 3397 0202175007 WIRE BOEING 767 7673Q8 1385142 NM ROW 16-22 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 FOUND CABIN EGRESS LIGHTS ON RT SIDE OF AIRCRAFT WERE INOPERATIVE FROM ROW 16 TO ROW 22, AND BETWEEN THE A AND B BULKHEA D. REPLACED BOTH LIGHT ASSEMBLIES DUE TO BROKEN WIRES. CHECK-C 5-1-99 LAX. 2 L 7 2 4F RT A1NM 1999061100002 19990611 00002 NM 1999 6 11 TWAA9907702 1 19990602 A 3350 LIGHT BOEING 727 727231 1384079 NM ROW 27 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54345 21632 FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE AT RT SIDE AND LEFT SIDE NUMBER ONE DOORS, AND THE EGRESS FLOOR STRIP INOPER ATIVE AT ROW 27. REPLACED THE BATTERY PACK AND THE BULB AT RT SIDE. BATTERY PACK (P/N 61-0478-3) AND BULB (P/N 1619). EGRESS LIGHT REPOSITIONED FLOOR STRIP AT ROW 27. CHECK-C 6-12-98 MCI. 2 L 7 3 4F A3WE 1999061100003 19990611 00003 WP 1999 6 11 TWAA9907703 1 19990528 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 639 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 LONGERON 5L FS 639 WAS CRACKED .25 INCH. REPLACED SECTION ON LONG 5L AND INSTALLED SPLICE SECTION PER SRM 53-02, FIG 18 AND SRO9530128 DRAWING. CHECK-C 11-13-98 STL. 2 L 7 2 4F A6WE 1999061100004 19990611 00004 WP 1999 6 11 TWAA9907704 1 19990527 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 658 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 LONGERON 6L AT FS 658 WAS CRACKED .25 INCH LONG. REPAIRED PER SRM 53-02, FIG 18 AND STANDARD PRACTICES. CHECK-C 11-13- 98 STL. 2 L 7 2 4F A6WE 1999061100005 19990611 00005 WP 1999 6 11 TWAA9907705 1 19990527 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 737 & 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 FOUND .25 INCH CRACKS AT LONGERON 6L AT FS 737 AND 756, AND LONGERON 7R AT FS 680. REPAIRED EACH PER SRM 53-02 FIG 18, AND SRO 9530128. CHECK-C 11-13-98 STL. 2 L 7 2 4F A6WE 1999061100006 19990611 00006 WP 1999 6 11 TWAA9907706 1 19990528 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 LONGERON 6R AT FS 756 WAS CRACKED .25 INCH. REPAIRED LONGERON 6R AT FS 756 PER SRM 53-02 FIG 18 SHEET 1. CHECK-C 11-13 -98 STL. 2 L 7 2 4F A6WE 1999061100007 19990611 00007 WP 1999 6 11 TWAA9907707 1 19990528 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 FOUND LONGERON 4R AT FS 756 CRACKED .25 INCH. CUT OUT DAMAGED SECTION AND REPAIRED LONGERON PER SRM 53-02 FIG 18 SHEET 1. CHECK-C 11-13-98 STL. 2 L 7 2 4F A6WE 1999061100008 19990611 00008 WP 1999 6 11 TWAA9907708 1 19990528 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 FOUND LONGERON 5L AT FS 699 CRACKED .25 INCH. FABRICATED AND INSTALLED LONGERON AND SPLICES IN LONGERON 5L AT FS 699 PE R SRM 53-02 FIG 18 SHEET 1. CHECK-C 11-13-98 STL. 2 L 7 2 4F A6WE 1999061100009 19990611 00009 SO 1999 6 11 LR7A9940 1 19990412 A 5330 SKIN LKHEED 382 382G 526414U SO BS 577-617 WRINKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C-CHECK/BRIDGING INSPECTION PER HC5303, FOUND FS 577 TO 617 BELLY SKIN WRINKLED BEYOND LIMITS. REPLACED SKIN PAN EL IAW SMP 583-40-06. 2 H 7 4 4T A1SO 1999061100010 19990611 00010 SO 1999 6 11 LR7A9941 1 19990412 A 5311 FRAME LKHEED 382 382G 526414U SO BS 817 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C-CHECK/BRIDGING INSPECTION, FOUND LT LOWER RING SEGMENT CRACKED AT FS 817E, WL 156. REPAIRED RING SEGMENT IAW S MP 583 53-40-38, 39. 2 H 7 4 4T A1SO 1999061100011 19990611 00011 WP 1999 6 11 CALA9900615 1 19990520 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 859-879 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND FLOORBEAM CORRODED BETWEEN STA 859 AND 879, RT SIDE. THE BEAM WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999061100012 19990611 00012 WP 1999 6 11 CALA9900616 1 19990524 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1821-1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED ON LT AND RT SIDES AT STA 1821-1887. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999061100013 19990611 00013 WP 1999 6 11 CALA9900617 1 19990524 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1905-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT RT SIDE BETWEEN STA 1905 AND 2007. THE FLOORBEAM WAS REPLACED IAW SRM 51-3 1-01. 2 L 7 3 4F A22WE 1999061100014 19990611 00014 WP 1999 6 11 CALA9900618 1 19990525 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1841-1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CENTRAL FLOORBEAM (NR 2) CORRODED BETWEEN STA 1841 AND 1887. THE FLOORBEAM WAS REPLACED IAW SRM 51-31- 01. 2 L 7 3 4F A22WE 1999061100015 19990611 00015 WP 1999 6 11 CALA9900619 1 19990525 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1902-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1902 AND 2007, RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-31- 01. 2 L 7 3 4F A22WE 1999061100016 19990611 00016 WP 1999 6 11 CALA9900620 1 19990528 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 449.250 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 449.250 ON RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999061100017 19990611 00017 NM 1999 6 11 CALA9900621 1 19990602 A 3260 656021132 ACCESSORY UNIT BOEING 727 727232 1384082 NM LANDING GEAR INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 10791 57701 20645 WHEN GEAR WAS RETRACTED AFTER DEPARTURE A LOUD THUMP WAS HEARD WHEN NOSE GEAR RETRACTED. A LIGHT TEST WAS DONE AND THE NOSE GEAR GREEN LIGHT DID NOT COME ON. PRESS TO TEST AND NEW BULBS HAD NO EFFECT. FLIGHT MANUAL PROCEDURE WAS ACCOMPLI SHED. THE LIGHT TEST WAS CHECKED AGAIN AND NEITHER THE NOSE GEAR GREEN OR RT MAIN GEAR GREEN LIGHTS WOULD TEST. WHEN G EAR WAS EXTENDED FOR LANDING AT IAH 3 GREEN GEAR LIGHTS WERE INDICATED. WHEN FLAPS WERE PUT TO 30 DEGREES THE GEAR WARN ING HORN SOUNDED AND STAYED ON. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. THE LANDING GEAR ACCESSORY UNIT WAS REPLA CED. A LANDING GEAR AND FLIGHT CONTROL POSITION AND WARNING CHECK WAS PERFORMED AND SYSTEM CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1999061100018 19990611 00018 WP 1999 6 11 CALA9900622 1 19990602 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMER EXIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND THE EXTERIOR EMERGENCY EXIT LIGHTS ON BOTH THE RT AND LT SIDE OF AIRCRAFT INOPERATIVE. THE POWER SUPPL Y WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A6WE 1999061100019 19990611 00019 WP 1999 6 11 CALA9900623 1 19990528 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 450.162 & 515 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 AND 515, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30- 00. 2 L 7 3 4F A22WE 1999061100020 19990611 00020 WP 1999 6 11 CALA9900624 1 19990528 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 450.162 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 IN CENTER AND ON RT SIDE. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999061100021 19990611 00021 WP 1999 6 11 CALA9900625 1 19990528 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 427-450 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 427.668 AND 450.162 ON LT SIDE. THE BEAM WAS REPLACED IAW SRM 51- 30-00. 2 L 7 3 4F A22WE 1999061100022 19990611 00022 WP 1999 6 11 CALA9900626 1 19990528 A 5321 FLOOR DOUG DC10 DC1030 3023501 WP BS 1099 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND FORWARD CARGO RT SUPPORT FLOOR PANEL CORRODED AT STA 1099. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30- 00. 2 L 7 3 4F A22WE 1999061100023 19990611 00023 WP 1999 6 11 CALA9900627 1 19990528 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1887-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1887 AND 2007 ON LT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-3 1-01. 2 L 7 3 4F A22WE 1999061100024 19990611 00024 WP 1999 6 11 CALA9900628 1 19990602 A 5230 RETAINER DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72829 49489 INSPECTION FOUND A 2 INCH CRACK ON FORWARD CARGO DOOR LOWER LEFT PAN SEAL RETAINER UNDER DOOR LATCH MECHANISM. A REPAIR WAS INSTALLED IAW ECRA 5210-01343. 2 L 7 2 4F A6WE 1999061100025 19990611 00025 NM 1999 6 11 CALA9900629 1 19990602 A 5330 SKIN BOEING 727 727232 1384082 NM CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND THE NR 3 CARGO DOOR CUTOUT SKIN CORRODED AT AFT LOWER CORNER. REPAIRED IAW ECRA 5330-02818. 2 L 7 3 4F A3WE 1999061100026 19990611 00026 WP 1999 6 11 CALA9900630 1 19990603 A 5320 MOUNTING DOUG DC10 DC1030 3023501 WP BS 1876-1886 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND MOUNTING PLATE ASSEMBLY CORRODED AT STA 1876-1886 FROM POSITION X = 0.02L TO X = 0.10L. THE MOUNTING P LATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 53-16-01. 2 L 7 3 4F A22WE 1999061100027 19990611 00027 NM 1999 6 11 9901846729 1 19990526 A 2913 PUMP BOEING 747 747251F 1384898 NM NR 4 HYD SYST MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 629US 22388 DURING CLIMB, THE NR 4 HYDRAULIC QUANTITY INDICATED ZERO. AIRCRAFT RETURNED TO MNL AND LANDED WITHOUT INCIDENT. REPLAC ED THE HYDRAULIC QUANTITY TRANSMITTER AND ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999061100028 19990611 00028 WP 1999 6 11 9901859874 1 19990601 A 3610 SEAL DOUG DC9 DC951 3022051 WP TAIL COMPARTMENT LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 783NC 48108 AFTER TAKEOFF, THE TAIL COMPARTMENT HIGH TEMPERATURE INDICATOR LIGHT ILLUMINATED WITH POWER SET AT CLIMB AND AT TAKEOFF EPR. INDICATION EXTINGUISHED AT LOWER POWER SETTING. FLIGHT CREW DECLARED YELLOW EMERGENCY, RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PERI SEALS AT RIGHT HEAT EXCHANGER AND TAIL COMPARTMENT TEMPERATURE SENSORS. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999061100029 19990611 00029 WP 1999 6 11 9901869154 1 19990601 A 3350 BATTERY DOUG DC9 DC914 3022034 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND TAIL COMPARTMENT INTERIOR CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999061100030 19990611 00030 NM 1999 6 11 9901876303 1 19990531 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE BETWEEN DOOR 2L AND 3L. REPAIRED LOOSE WIRE, OPERATION AL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999061100031 19990611 00031 1999 6 11 9901886623 4 19990524 A 2565 4A305611 SLIDE BFGOODRICH 7A123858 BOEING 747 747251B 1384892 NM DOOR 2R MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US G1928 21705 DURING SCHEDULED CHECK, DOOR 2R SLIDE DEPLOYED BUT DID NOT INFLATE. REPLACED SLIDE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999061100032 19990611 00032 NM 1999 6 11 9901895504 1 19990430 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM ROW 34-38 DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 504US 23193 DURING SCHEDULED MAINTENANCE CHECKS, ESCAPE PATH LIGHTING AT ROWS 34 AND 38 WERE FOUND INOPERATIVE. MAINTENANCE REPLACE D THE ASSOCIATED BATTERY/CHARGER PACK WITH SERVICEABLE UNIT. 2 L 7 2 4F RT A2NM 1999061100033 19990611 00033 WP 1999 6 11 9901901154 1 19990506 A 3260 INDICATION DOUG DC10 DC1040 3023508 WP LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 154US 46763 ON SELECTING GEAR DOWN DURING APPROACH TO HNL, ALL FOUR LIGHTS REMAINED RED AND ANTISKID WOULD NOT TEST. RECYCLED GEAR AND ALL OPERATED NORMALLY WITH NORMAL ANTI-SKID INDICATIONS. FLIGHT LANDED WITHOUT INCIDENT. OPERATIONAL CHECK OK. AI RCRAFT APPROVED FOR FURTHER SERVICE. 2 L 7 3 4F A22WE 1999061100034 19990611 00034 SO 1999 6 11 COMA9910089 1 19990602 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 120262 EMERGENCY EXIT SIGN IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999061100035 19990611 00035 EA 1999 6 11 COMA9960244 1 19990602 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 924CA 7026 GEAR DISAGREE WARNING, NLG DID NOT RETRACT. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999061100036 19990611 00036 EA 1999 6 11 COMA9960245 1 19990531 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 952CA 7092 FORWARD SECTION OF EMERGENCY FLOOR LIGHTING INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 1999061100037 19990611 00037 EA 1999 6 11 COMA9960246 1 19990531 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTION A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 987CA 7199 PROXIMITY SYSTEM FAULT MESSAGE. LANDING GEAR WAS LOWERED USING EMERGENCY SYSTEM. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1999061100038 19990611 00038 EA 1999 6 11 COMA9960247 1 19990601 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 914CA 10092 7012 FLAPS FAILED. REPLACED FECU. 2 L 7 2 4F RT A21EA 1999061100039 19990611 00039 EA 1999 6 11 COMA9960248 1 19990601 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB FAILED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 981CA 1377 1377 7163 AP PITCH TRIM CAUTION MESSAGE CAME ON DURING FLIGHT. STAB TRIM CH 1 WOULD NOT ALLOW TRIM PAST FOUR UNITS. STAB TRIM CH 2 WOULD ALLOW TRIM PAST FOUR UNITS. REMOVED HSTA AND MCU, INSTALLED SERVICEABLE HSTA AND MCU. 2 L 7 2 4F RT A21EA 1999061100040 19990611 00040 EA 1999 6 11 COMA9960249 1 19990601 A 2740 70623 MCU CNDAIR CL600 CL6002B19 EA HORIZ STAB FAILED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 981CA 10355 10355 7163 AP PITCH TRIM CAUTION MESSAGE CAME ON DURING FLIGHT. STAB TRIM CH 1 WOULD NOT ALLOW TRIM PAST FOUR UNITS. STAB TRIM CH 2 WOULD ALLOW TRIM PAST FOUR UNITS. REMOVED HSTA AND MCU, INSTALLED SERVICEABLE HSTA AND MCU. 2 L 7 2 4F RT A21EA 1999061100041 19990611 00041 NM 1999 6 11 UPS99229696 1 19990527 A 5311 FRAME BOEING 727 727247 138408F NM BS 939 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON 940 FRAME WL 207.5 LBL 67 AT BS 939. REMOVED CORROSION AND TREATED AREA PER SRM 51-20 -00. 2 L 7 3 4F A3WE 1999061100042 19990611 00042 NM 1999 6 11 UPS99229697 1 19990526 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 848, WL 208, LBL 26. REMOVED CORROSION TREATED AND PAINTED AREA P ER MM 51-20-00. 2 L 7 3 4F A3WE 1999061100043 19990611 00043 NM 1999 6 11 UPS99229698 1 19990526 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 826 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 826, LBL 26, WL 208. REMOVED CORROSION 2 X 4 X 0.001 WITHIN LIMIT S PER SRM 53-10-1, ALODINED AND PRIMED. 2 L 7 3 4F A3WE 1999061100044 19990611 00044 NM 1999 6 11 UPS99229699 1 19990527 A 5311 FRAME BOEING 727 727247 138408F NM BS 930 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON FRAME BS 930, WL 207.5, LBL 66. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00. 2 L 7 3 4F A3WE 1999061100045 19990611 00045 NM 1999 6 11 UPS99229700 1 19990527 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON FRAME BS 950, WL 207.5, LBL 55. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00. 2 L 7 3 4F A3WE 1999061100046 19990611 00046 NM 1999 6 11 UPS99229701 1 19990526 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 806 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 806, LBL 26, WL 208. REMOVED CORROSION AND TREATED AREA PER MM 51 -20-00. 2 L 7 3 4F A3WE 1999061100047 19990611 00047 NM 1999 6 11 UPS99229702 1 19990513 A 5315 BAC1505101167 FLOORBEAM BOEING 727 72725C 138400H NM BS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON BS 380 FLOORBEAM LBL 55 TO LBL 46 WL 208. CUT OUT DAMAGED FLOORBEAM , FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1999061100048 19990611 00048 NM 1999 6 11 UPS99229703 1 19990601 A 5720 651620252 STIFFENER BOEING 727 72725C 138400H NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION AND POPPED FASTENER ON BS 870, BL 0 STIFFENER WING CENTER SECTION. REMOVED AND REPLACED S TIFFENER PER SRM 51-30-02. 2 L 7 3 4F A3WE 1999061100049 19990611 00049 NM 1999 6 11 UPS99229704 1 19990601 A 5753 651859929 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON NR 4 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE WITH SERVICEABLE UNIT. 2 L 7 3 4F A3WE 1999061100050 19990611 00050 NM 1999 6 11 UPS99229705 1 19990601 A 5753 651859928 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON NR 3 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE WITH SERVICEABLE UNIT. 2 L 7 3 4F A3WE 1999061100051 19990611 00051 NM 1999 6 11 UPS99229706 1 19990602 A 5753 65192086 FLAP TRACK BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON NR 8 FLAP TRACK INSIDE REAR SPAR MAIN BOLT HOLE AND AROUND FWD LUG. REPLACED FLAP TRAC K. 2 L 7 3 4F A3WE 1999061100052 19990611 00052 NM 1999 6 11 UPS99229707 1 19990602 A 5753 65192086 FLAP TRACK BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON NR 7 FLAP TRACK AROUND FWD LUG. REPLACED FLAP TRACK. 2 L 7 3 4F A3WE 1999061100053 19990611 00053 EU 1999 6 11 QXEA9901079 1 19990530 A 3350 606008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 488US 11240 BOI- AFT FIVE, SEAT EVACUATION LIGHTS ILLUMINATED WHEN BATTERY SWITCH TURNED OFF. REMOVED AND REPLACED BATTERY CARTRIDG E, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999061100054 19990611 00054 1999 6 11 ABXA9900385 4 19990528 A 2210 258668911ABX1 CONTROLLER DOUG DC9 DC931 3022065 WP COCKPIT DEFECTIVE A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 943AX 1841 47528 DURING CRUISE FLIGHT AT 310, A STRONG ACRID SMOKE ODOR AND WHIPSY SMOKE CAME FROM THE AUTOPILOT VERTICAL SPEED WHEEL. D ECLARED EMERGENCY AND PERFORMED EMERGENCY CHECK LISTS. LANDED AT CLEVELAND HOPKINS AIRPORT WITHOUT INCIDENT. REPLACED THE AUTOPILOT CONTROLLER. 2 L 7 2 4F A6WE 1999061100055 19990611 00055 WP 1999 6 11 ABXA9900386 1 19990528 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 904AX 47040 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. CLEANED AND SECURED THE LOOSE/CORRODED GROUND STUD. 2 L 7 2 4F A6WE 1999061100056 19990611 00056 WP 1999 6 11 ABXA9900387 1 19990528 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 904AX 47040 EMERGENCY EVACUATION LIGHTS WERE INOPERATIVE. REPLACED NICAD BATTERIES. 2 L 7 2 4F A6WE 1999061100057 19990611 00057 NM 1999 6 11 MWEA99307 1 19990602 A 5330 5911406 SKIN DOUG MD88 MD88 3023688 NM BS 220 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 DENT AT STATION 220 BETWEEN LONGERONS 17L AND 18L. FORMED DENT BACK INTO SURFACE CONTOUR FABRICATE AND INSTALL DOUBLER. 2 L 7 2 4F RT A6WE 1999061100058 19990611 00058 WP 1999 6 11 MWEA99308 1 19990602 A 5210 591412161N PAN DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 CABIN DOOR PAN JUST NEXT TO BOTTOM HINGE HAS A CRACK PROPAGATING FROM 2ND STOP DRILL HOLE. INSTALLED NEW DOOR PANEL SEG MENT. 2 L 7 2 4F A6WE 1999061100059 19990611 00059 WP 1999 6 11 MWEA99311 1 19990602 A 5313 5914579502 LONGERON DOUG DC9 DC932 3022066 WP BS 1089-1104 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 AFT ACCESS LONGEORN 17R HAS LIGHT CORROSION AND TOOL MARKS ON LOWER SIDE OF LOWER LEG BETWEEN FRAME 1089-1104. REMOVED CORROSION BLENDED TOOL MARKS, FABRICATED NEW SECTION OF THE LONGERON. 2 L 7 2 4F A6WE 1999061100060 19990611 00060 WP 1999 6 11 MWEA99312 1 19990602 A 5320 3912337502 SPLICE DOUG DC9 DC914 3022034 WP BS 604 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LEFT CABIN STATION 604 FRAME AFT SPLICE HAS TOOLING DAMAGE. FABRICATED AND INSTALLED NEW SPLICE. 2 L 7 2 4F A6WE 1999061100061 19990611 00061 NM 1999 6 11 MWEA99313 1 19990602 A 5320 99115937 BEAM DOUG MD88 MD88 3023688 NM BS 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 E AND E COMPARTMENT SUBFLOOR TEE SECTION AT STATION 160, 12 INCHES RIGHT OF AIRCRAFT CENTERLINE HAS A ONE INCH AREA OF H EAVY CORROSION. FABRICATED AND INSTALLED FLOORBEAM CAP SPLICE PER BOEING TELEX. 2 L 7 2 4F RT A6WE 1999061100062 19990611 00062 NM 1999 6 11 DL757991214 1 19990528 A 5414 311N3400 SKIN BOEING 757 757232 1384965 NM NR 1 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 625DL 22915 THE NR 1 ENG NACELLE STRUT SKIN WAS PREVIOUSLY FOUND CRACKED AND REPAIRED. ADDITIONAL CRACKING WAS FOUND DURING THE CUR RENT VISIT. THE NEW CRACK WAS APPROX 1 INCH IN LENGTH. REPAIRED PER ERA 333162-14, REV A. 2 L 7 2 4F RT A2NM 1999061100063 19990611 00063 NM 1999 6 11 DL757991215 1 19990528 A 5330 144N31201 SKIN BOEING 757 757232 1384965 NM BS 970 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 625DL 22915 DAMAGE FOUND IN THE FUSELAGE SKIN AT BS 970, S3R. DAMAGE CUTOUT MEASURES APPROX 4 BY 4. REPAIRED PER ERA 333189-14. 2 L 7 2 4F RT A2NM 1999061100064 19990611 00064 NM 1999 6 11 DL757991216 1 19990528 A 5330 144N31201 SKIN BOEING 757 757232 1384965 NM BS 920 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 625DL 22915 DAMAGE FOUND TO FUSELAGE SKIN AT BS 920, S3R. DAMAGE CUTOUT WAS APPROX 4 BY 4. REPAIRED PER ERA 333190-14. 2 L 7 2 4F RT A2NM 1999061100065 19990611 00065 NM 1999 6 11 DL757991217 1 19990528 A 5320 146N853017 STRAP BOEING 757 757232 1384965 NM BS 1440 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 625DL 22915 CORROSION WAS FOUND IN THE LWR AFT CORNER OF THE INNER STRAP FOR THE C2 DOOR. REPAIRED PER ERA 333195-14, REV A. 2 L 7 2 4F RT A2NM 1999061100066 19990611 00066 NM 1999 6 11 DL757991218 1 19990528 A 5414 311N3450 SKIN BOEING 757 757232 1384965 NM NR 2 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 625DL 22915 THE NR 2 ENG NACELLE STRUT SKIN WAS FOUND WITH MULTIPLE CRACKS IN THE RT SIDE SKIN PANEL. REPAIRED PER ERA 333163-14, R EV A. 2 L 7 2 4F RT A2NM 1999061100067 19990611 00067 NM 1999 6 11 DL73K991219 1 19990528 A 5330 6545769 SKIN BOEING 737 737232 1384475 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309DL 23081 A .75 INCH CRACK WAS FOUND EMANATING FROM THE FWD END OF THE AVIONICS EXHAUST CUTOUT IN THE FUSELAGE BELLY SKIN. ANOTHE R 1.25 INCH CRACK WAS EMANATING FROM THE AFT END OF THE CUTOUT. THE CRACKS WERE STOP DRILLED AND AN ALUMINUM DOUBLER I NSTALLED AROUND THE CUTOUT PER ER/A 367484-14, REV A. 2 L 7 2 4F RT A16WE 1999061100068 19990611 00068 NM 1999 6 11 DL73E991220 1 19990528 A 5330 654580027 SKIN BOEING 737 737247 138448D NM BS 332 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 380DL 23607 THE R1 DOOR CUTOUT (FWD GALLEY DOOR) WAS FOUND WITH A .75 INCH TYPICAL CRACK IN THE LOWER AFT CORNER OF THE CUTOUT. THE CRACK WAS IN THE SKIN ASSY AND UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT AND REPAIRED WITH ALUMINUM DOUBLERS P ER B737 SRM 53-30-3, FIG 26 AND ER/A 367476-14, REV A. 2 L 7 2 4F A16WE 1999061100069 19990611 00069 NM 1999 6 11 DL73K991221 1 19990528 A 5343 654654319 FITTING BOEING 737 737232 1384475 NM BS 685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 THE LT AND RT FS 685 MLG SIDE STRUT SUPPORT FITTINGS WERE FOUND WITH CORROSION IN THE STRUT ATTACH LUG BORES. THE LUGS WERE OVERSIZED TO CLEAN UP THE CORROSION, INSPECTED, AND REPAIRED WITH STELL BUSHINGS PER ER/A 367450-14, REV A. 2 L 7 2 4F RT A16WE 1999061100070 19990611 00070 NM 1999 6 11 DL72S991222 1 19990529 A 5330 6554574155 SKIN BOEING 727 727232 1384082 NM BS 480-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 12 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367489-14AD. 2 L 7 3 4F A3WE 1999061100071 19990611 00071 NM 1999 6 11 DL72L991223 1 19990531 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 47 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT A ND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367496-14AD. 2 L 7 3 4F A3WE 1999061100072 19990611 00072 NM 1999 6 11 DL72L991224 1 19990531 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 680-740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED 8 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINU M DOUBLER PER ER/A 367500-14AD. 2 L 7 3 4F A3WE 1999061100073 19990611 00073 NM 1999 6 11 DL72L991225 1 19990531 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 440-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 2 CRACKS BETWEEN FS 440 AND 460. THE CRACKS WERE CUT OUT OF THE SKIN LAP AND REPAIRED WITH AN ALUMINUM DOUBLER PER B72 7 SRM 53-30-3, FIG 5 AND ER/A 367499-14AD. 2 L 7 3 4F A3WE 1999061100074 19990611 00074 NM 1999 6 11 DLM88991226 1 19990601 A 3222 MS288892 SCHRADER VALVE DOUG MD88 MD88 3023688 NM NLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 928DL 49715 AFTER T/O, NOSE GEAR LIGHT REMAINED RED AND NOISE HEARD. GEAR DOOR LIGHT AND NLG PIN INDICATED NORMAL. WITH GEAR HANDL E DOWN ALL INDICATIONS NORMAL. FOUND NOSE STRUT BOTTOMED OUT. REMOVED AND INSPECTED SCHRADER VLV ON NOSE GEAR. FOUND PACKING IN POOR CONDITION. REPLACED VLV AND PACKING. SERVICED STRUT, JACKED A/C AND CYCLED GEAR. ALL INDICATIONS NORM AL. 2 L 7 2 4F RT A6WE 1999061100075 19990611 00075 NM 1999 6 11 DL767991227 1 19990601 A 2530 811150417 COFFEEMAKER BOEING 767 767232 1385132 NM GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 104DA 22216 ELECTRICAL SMELL IN FWD GALLEY AFTER LANDING, STRONG ODOR UTILITY BUSSES TURNED OFF. NO ELECTRICAL ODOR NOTED ON ENTRY. CKD ALL COMPONENTS IN GALLEY, ALL CK NORMAL. NOTED SPILLED AND BURNED COFFEE ON RT FWD COFFEEMAKER. SUSPECT TH IS WAS ODOR REPORTED. CLEANED COFFEEMAKER PAD, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 1999061100076 19990611 00076 NM 1999 6 11 DLM88991228 1 19990601 A 4910 36280 INLET DOUG MD88 MD88 3023688 NM APU DIRTY A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 966DL 9129 53115 RETURNED TO GATE AFTER SMOKE DETECTORS (BOTH AFT LAVS) WENT OFF. LEFT ENG RUNNING, LEFT PACK RUNNING FOR 5 MIN. APU AI R RUNNING, RIGHT PACK RUNNING SINCE PUSHBACK (20 MIN). LIGHT SMOKE (HAZE VISABLE IN REAR OF CABIN). CLEANED APU INLET BOX, PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1999061100077 19990611 00077 NM 1999 6 11 DL76L991229 1 19990601 A 2730 ACTUATOR 2827001011 BOEING 767 767332 1382001 NM RT ELEV LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 173DN 24800 RT HYD QTY DROPPED TO BELOW .5, RT HYD SYSTEM RSVR LIGHT AND RT HYD QTY MESSAGE. SECURED PRI PUMP AND DEMAND PUMP PER P OM AND QTY STABLIZED AT .3. DIVERTED TO JFK. LEAK CHECKED RUDDER AREA AND LANDING GEAR WITH SIMULATED RETRACTION, NO L EAKS FOUND. FOUND RT ELEV AREA WET, FOUND RT ELEV RT SYST PCA LEAKING. PCA NASI JFK. PCA BEING SHIPPED FROM LAX. 2 L 7 2 4F RT A1NM 1999061100078 19990611 00078 NM 1999 6 11 DL76S991231 1 19990601 A 2121 FAN 732591F BOEING 767 767332 1382001 NM COCKPIT INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 133DN 55 24982 AT CRZ FLT FL390, CREW NOTED AN ELECT ODOR. CREW PERFORMED SMOKE IDENTIFICATION/REMOVAL CHECKLIST. ODOR WAS ELIMINATE D, C/B H-21 ON P6-4 PANEL WAS POPPED. FWD EXHAUST EQUIPT FAN. NO OTHER SMELLS NOTED FOR REMAINDER OF FLT. REPLACED FA N. 2 L 7 2 4F RT A1NM 1999061100079 19990611 00079 NM 1999 6 11 DL72S991233 1 19990602 A 5530 SKIN BOEING 727 727232 1384082 NM BS 1340 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 SKIN CRACKED FS 1340 VENTRAL STAB SKIN IS CRACKED RT SIDE. FABRICATED DOUBLER PER M/M 55-30-0 FIG 801. PERFORMED DYE C HECK PER PS 900-6-3 NR 1. NO CRACKS FOUND PAST FASTENER HOLE. OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 PG 801. 2 L 7 3 4F A3WE 1999061100080 19990611 00080 NM 1999 6 11 DL73K991234 1 19990601 A 5753 SKIN BOEING 737 737232 1384475 NM NR 3 TE FOREFLAP CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 NR 3 FOREFLAP CHAFING AND WORN THROUGH AT UPPER SURFACE I/B END. REPAIRED PER SRM 51-40-6, OPS CHECK OK. 2 L 7 2 4F RT A16WE 1999061100081 19990611 00081 NM 1999 6 11 DLM88991235 1 19990602 A 3610 321417611 VALVE DOUG MD88 MD88 3023688 NM NR 1 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 915DL 49546 AIRBORNE RETURN, RIGHT PACK WOULD NOT PRESSURIZE AIRCRAFT. REPLACED RIGHT PNEUMATIC PILOT PRESS REG. PERFORMED HIGH PO WER ENGINE RUN AND CKD OPERATION OF RIGHT PACK, CKS OK. 2 L 7 2 4F RT A6WE 1999061100082 19990611 00082 NM 1999 6 11 DL72S991238 1 19990602 A 5755 ANGLE BOEING 727 727232 1384082 NM NR 2 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 FOUND ON C2 LETTER CK, CRACK AT LOWER BOLT HOLE OF NR 2 SPOILER O/B SPAR ATTACH ANGLE. REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1999061100083 19990611 00083 NM 1999 6 11 DL72S991239 1 19990602 A 7110 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE COWL WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 COWL STRIKER ANGLE WORN LOWER FWD EDGE OF NR 2 ENGINE CUTOUT 5:30 POSITION. REPAIRED PER M/M 53-11-0 PAGE 801. 2 L 7 3 4F A3WE 1999061100084 19990611 00084 NM 1999 6 11 DL757991240 1 19990602 A 3350 LIGHT BOEING 757 757232 1384965 NM ROW 3C & 5C INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 619DL 22909 ON LAYOVER, FOUND EMERGENCY LIGHTS AT SEATS 3C AND 5C INOP. FOUND LIGHT SOCKETS PULLED OUT OF LENS COVERS. REINSTALLED LIGHT SOCKETS IN LENS COVERS AND SECURED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 1999061100085 19990611 00085 NM 1999 6 11 DL76L991241 1 19990601 A 2730 ACTUATOR 2827001011 BOEING 767 767332 1382001 NM RT ELEVATOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 173DN 2021 24800 CENTER SYS HYD QUANTITY DROPPED INFLT TO .38. SHUTOFF PUMPS AND QTY STABILIZED. FOUND RT ELEV PCA LEAKING. REPLACED S AME. 2 L 7 2 4F RT A1NM 1999061100086 19990611 00086 NM 1999 6 11 DL757991242 1 19990602 A 5310 STRUCTURE BOEING 757 757232 1384965 NM BS 400 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 656DL 24396 AIRCRAFT EXPERIENCE EXTREMELY HARD LANDING. VISUAL INSPECTION REVEALED STRUCTURAL DAMAGE TO EXTERIOR AND INTERIOR SKIN. STRUCTURE JUST AFT OF THE NOSE LANDING GEAR ASSY ON BOTH THE LEFT AND RIGHT SIDES OF THE AIRCRAFT TO BE REPAIRED USING APPROPRIATE ENGINEERING AUTHORIZATIONS, MAINTENANCE MANUAL AND SRM AS APPLICABLE. 2 L 7 2 4F RT A2NM 1999061100087 19990611 00087 WP 1999 6 11 CKSA99059 1 19990524 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 649-749 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND STRINGER CORRODED AT ZONE 120, STA 649 TO STA 749. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 827. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), C CHECK CARD 01-53-1016, CPCP CARD C53-120-04-01, GAMCO NON ROUTINE WORK CARD NR 4 078. 2 L 7 3 4F A23WE 1999061100088 19990611 00088 WP 1999 6 11 CKSA99060 1 19990524 A 5313 156352 LONGERON LKHEED 1011 1011385115 5265015 WP BS 270 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND LONGERON CORRODED AT ZONE 110, STA 270. D ETERMINED TO BE OUT OF LIMITS IAW SRM 51-10-01. REPAIR CARRIED OUT IAW SRM 51-50-02 AND 51-40-01/02. FOUND AT GAMCO MA INTENANCE FACILITY (ABBU), C CHECK CARD 01-00-1008, CPCP CARD C53-110-01-00, NON ROUTINE WORK CARD NR 5072. 2 L 7 3 4F A23WE 1999061100089 19990611 00089 WP 1999 6 11 CKSA99061 1 19990524 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 1792 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND SKIN CORRODED AT ZONE 160, STA 1792, STR 3 6 TO 37. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 827. SEALED AND INSTALLED REPAIR PART IAW SRM 51-40-01 AND 51-25-00. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), C CHECK CARD 01-0 0-1000, CPCP CARD C53-160-04-00, NON ROUTINE WORK CARD NR 5004. 2 L 7 3 4F A23WE 1999061100090 19990611 00090 WP 1999 6 11 CKSA99062 1 19990524 A 5312 1554946101 BULKHEAD FITTING LKHEED 1011 1011385115 5265015 WP BS 1792 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND AFT PRESSURE BLKHD TO FUSELAGE ATTACHMENT FITTING CRACKED AT STA 1792, WL 329, RBL .20. REMOVED CRACKED FITTING IAW SRM 53-40-01. REPAIR CARRIED OUT IAW SRM 53- 21-02. INSTALLED REPAIR FITTING IAW SRM 51-40-01. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), DEFECT CARD REF NR 102-5 43, NON ROUTINE WORK CARD NR 4126. 2 L 7 3 4F A23WE 1999061100091 19990611 00091 WP 1999 6 11 CKSA99063 1 19990524 A 5315 DOUBLER LKHEED 1011 1011385115 5265015 WP BS 729 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 2.5 INCHES LONG AT ZONE 100, STA 729, RBL 70.5 TO RBL 73. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-01. REPAIR C ARRIED OUT IAW SRM 53-21-00. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), GAMCO NON ROUTINE JO NR 160856, NON ROUTINE WO RK CARD NR 4151. 2 L 7 3 4F A23WE 1999061100092 19990611 00092 WP 1999 6 11 CKSA99064 1 19990524 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 769 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 2.5 INCHES LONG AT ZONE 100, STA 769, RBL 57 TO RBL 59. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-01. REPAIR CAR RIED OUT IAW SRM 53-21-01, 51-21-02 AND 51-21-00. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), GAMCO NON ROUTINE JO NR 1 60856, NON ROUTINE WORK CARD NR 4150. 2 L 7 3 4F A23WE 1999061100093 19990611 00093 WP 1999 6 11 CKSA99065 1 19990524 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 709 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND SKIN CORRODED AT ZONE 120, STA 709, STR 32 TO 33. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 825, DETAIL A VEIW B (REF NON ROUTINE CARD 4078). SEALED AND INSTALLED REPAIR PART IAW SRM 51-21-02. FOUND AT GAMCO MAINTENANCE FAC ILITY (ABBU), C CHECK CARD 01-53-1016, CPCP CARD C53-120-04-01, NON ROUTINE WORK CARD NR 4060. 2 L 7 3 4F A23WE 1999061100094 19990611 00094 WP 1999 6 11 CKSA99066 1 19990524 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 865-883 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND STRINGER CORRODED AT ZONE 120, STA 865 TO STA 883. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. FABRICATED AND TREATED REPAIR PARTS IAW L1011 SRM 51 -21-02. REPAIR CARRIED OUT IAW SRM 53-31-00 FIG 827. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), C CHECK CARD 01-53-10 16, CPCP CARD C53-120-04-01, GAMCO NON ROUTINE WORK CARD NR 4051. 2 L 7 3 4F A23WE 1999061100095 19990611 00095 WP 1999 6 11 CKSA99067 1 19990524 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 789 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 23 I NCHES LONG AT ZONE 100, STA 789, LBL 34.5 TO LBL 46.5. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-50-02. REPAIR CARRIED OUT IAW SRM 53-21-00, FLOORBEAM REPAIR. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), GAMCO NON ROUTINE JO NR 160 856, NON ROUTINE WORK CARD NR 4153 AND 4137. 2 L 7 3 4F A23WE 1999061100096 19990611 00096 WP 1999 6 11 CKSA99068 1 19990524 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 689 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED AT ZONE 100 , STA 689, RBL 60 TO RBL 77. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-21-02. REPAIR CARRIED OUT IAW SRM 53-21- 00, FLOORBEAM REPAIR. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), GAMCO NON ROUTINE JO NR 160856, NON ROUTINE WORK CARD NR 4137 AND 4149. 2 L 7 3 4F A23WE 1999061100097 19990611 00097 WP 1999 6 11 CKSA99069 1 19990524 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 1443 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED STA 1443, C -2 CARGO COMPT. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-21-00 FIG 802, INSTALLED AS PER SRM 51-40-01. REPAIR CARRIED OUT IAW SRM 53-21-00 FIG 802. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), GAMCO NON ROUTINE JO NR 160856, C CHE CK CARD 01-27-1006, NON ROUTINE WORK CARD NR 4121. 2 L 7 3 4F A23WE 1999061100098 19990611 00098 WP 1999 6 11 CKSA9970 1 19990524 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 709 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 102CK 193N1198 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND FLOORBEAM LOWER CHORD CORRODED APPROX 12IN CHES AT ZONE 100, STA 709, RBL 68 TO RBL 80. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-01. REPAIR CARRIED OU T IAW SRM 53-21-00, FLOORBEAM REPAIR. FOUND AT GAMCO MAINTENANCE FACILITY (ABBU), GAMCO NON ROUTINE JO NR 160856, NON R OUTINE WORK CARD NR 4152 AND 4137. 2 L 7 3 4F A23WE 1999061100101 19990611 00101 SO 1999 6 11 99ZZZX2125 1 19990505 A 6120 STOP PIPER PA23 PA23250 7102308 SO COCKPIT LOOSE A IAWA K NONE O OTHER IN INSP/MAINT 1 EA 17 6913A 1795 277954108 WHEN COVER WAS REMOVED FROM QUADRANT, ALL WASHER TYPE STOPS WERE FOUND LOOSE AND NUTS COMING OFF. NO STOP NUT. 1 L 7 2 3O 1A10 1999061100104 19990611 00104 EA 1999 6 11 99ZZZX2128 2 19990513 A 7414 M3333 IMPULSE COUPLING SLICK PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA MAGNETO WORN A LABA K NONE O OTHER IN INSP/MAINT 1 AL 05 2947N 460 327940225 IMPULSE COUPLING WORN BEYOND AD 99-04-04 LIMIT. 1 L 7 1 3O 3 O A3SO 1E4 1999061100124 19990611 00124 CE 1999 6 11 99ZZZX2148 1 19990505 A 7120 Y123901 MOUNT LORD CESSNA 310 310K 2074228 CE ENGINE WORN A P7SA K NONE O OTHER IN INSP/MAINT 1 EA 21 6942L 150 310K0042 NEW SHOCK MOUNTS BY LORD COMPANY INSTALLED WITH ENGINE. MOUNTS SHOWED WEAR AFTER 150 HOURS (LAST MOUNTS LASTED DURATION OF ENGINE - 1,500 HOURS). 1 L 7 2 3O 3A10 1999061100153 19990611 00153 WP 1999 6 11 99ZZZX2178 2 19990421 A 7200 ENGINE LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP NR 2 FAILED A BSYA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 07 701AS 15980 1142 047 P74356 AIRCRAFT WAS ROUTED FROM MDW TO DSM, DIVERTED TO OHM DUE TO WEATHER. INBOUND TO OHM, PILOT NOTED VIBRATION IN AIRCRAFT, WAS ISOLATED TO THE RIGHT ENGINE. SHUT DOWN RIGHT ENGINE, AIRCRAFT LANDED SAFELY IN OHM. INSPECTED ENGINE, FOUND INTE RNAL FAILURE. SUSPECT HP BLADE FAILURE. REMOVED ENGINE AND INSTALLED RE-MANUFACTURED ENGINE. DAMAGED ENGINE SHIPPED T O GARRETT FOR REPAIR. 2 L 7 2 4F 4 F A10CE E6WE 1999061100161 19990611 00161 SO 1999 6 11 99ZZZX2186 1 19990507 A 7922 53E19600 VALVE PIPER PA31 PA31350 7103110 SO ENGINE OIL LOCKNUT FAILURE A AKVA K NONE O OTHER IN INSP/MAINT 1 CE 05 927TA 1582 318252061 CRIMP NUT FOUND IN OIL COOLER WHEN FLUSHING DURING ENGINE CHANGE. REMOVED THERMOSTATIC BYPASS VALVE ON AFFECTED ENGINE AND FOUND NUT MISSING FROM VALVE. NO OIL TEMPERATURE PROBLEMS REPORTED BEFORE THIS. VALVE S/N IS 54849. LYC SB 518C A DDRESSES THIS PROBLEM ON THESE VALVES WITH SERIAL NUMBERS LOWER THAN 53788. 1 L 7 2 3O A20SO 1999061100164 19990611 00164 NE 1999 6 11 99ZZZX2189 2 19990502 A 8500 ENGINE DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE LEFT FAILED A VLLA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 05 9923S 7575 177 25964 BP435739 AIRCRAFT EN ROUTE FROM MBS/TPA. LEFT ENGINE STARTED TO LOSE POWER AND WOULD NOT MAINTAIN MANIFOLD PRESSURE. AIRCRAFT D IVERTED TO MWO. FOUND REAR CYLINDERS VALVES NOT MOVING . SUBMITTER SUSPECTED REAR CAM RING FAILURE. 2 L 7 2 4R 4 R A669 5E4 1999061100171 19990611 00171 CE 1999 6 11 99ZZZX2196 1 19990518 A 7714 631056A1 COVER BEECH 58 58 1152740 CE TACHOMETER DRIVE CRACKED A FPIA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 15 80AC 84 TH56 FOUND OIL LEAKING REAR OF ENGINE. FOUND RT ANGLE TACHOMETER DRIVE COVER CRACKED. TT SINCE NEW: 84.3 HOURS. 1 L 7 2 3O 3A16 1999061100190 19990611 00190 CE 1999 6 11 99ZZZX2215 1 19990518 A 2720 ARM BEECH 99 B99 1154004 CE RUDDER PEDAL DAMAGED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 991H U155 RUDDER PEDAL ARM PIVOT HOLES FOR PEDAL ELONGATED. FOUND DURING ROUTINE INSPECTION OF INTERIOR (DETAIL). REPLACED RUDDE R PEDAL ARM. 1 L 7 2 3T A14CE 1999061100191 19990611 00191 CE 1999 6 11 99ZZZX2216 1 19990504 A 5210 994200247 HINGE BEECH 99 B99 1154004 CE PASSENGER DOOR CRACKED A A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 991H U155 PILOT'S CREW DOOR REPORTED DIFFICULT TO CLOSE. INSPECTED DOOR LOCK LATCHES AND LUBBED. NO DISCREPANCIES FOUND. INSPEC TED CREW DOOR UPPER HINGES. UPPER FORWARD HINGE FOUND CRACKED ALONG HINGE LINE, ONE INCH INBOARD. REPLACED HINGE WITH NEW AND SECURED. HINGE MAY HAVE CRACKED DUE TO FLEXING OF DOOR, DUE TO EXCESSIVE SEAL THICKNESS. THE SEAL ON THIS PART ICULAR APPLICATION WAS ACCEPTABLE. 1 L 7 2 3T A14CE 1999061100192 19990611 00192 CE 1999 6 11 99ZZZX2217 1 19990520 A 2730 115610010325 TORQUE TUBE BEECH 99 B99 1154004 CE RT ELEVATOR CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA U127 RIGHT ELEVATOR TORQUE TUBE CRACKED WHERE THE PEDAL ATTACHES TO BELLCRANK ASSEMBLY. 1 L 7 2 3T A14CE 1999061100193 19990611 00193 CE 1999 6 11 99ZZZX2218 1 19990520 A 2720 5052432610 RUDDER PEDAL BEECH 99 B99 1154004 CE COCKPIT BROKEN A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA U127 RUDDER PEDAL ARM BROKE WHERE IT ATTACHES TO ARM. 1 L 7 2 3T A14CE 1999061100194 19990611 00194 CE 1999 6 11 99ZZZX2219 1 19990517 A 2752 995240257 MOTOR BEECH 99 99 1154002 CE TE FLAP FAILED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 24BH U67 FLAPS WERE INOPERATIVE. MOTOR WINDINGS COOKED (BRUSHES WORN). REPLACED FLAP MOTOR AND GEARBOX AS AN ASSEMBLY. VERIFIE D RIGGING OK. MOTOR INOPERATIVE DUE TO NORMAL WEAR. 1 L 7 2 3T A14CE 1999061100205 19990611 00205 CE 1999 6 11 99ZZZX2230 1 19990520 A 2913 99141193 PUMP CESSNA 650 650 2076802 CE HYDRAULIC SYSTEM CRACKED A DBCA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 13 16SU 178 124 6500025 PILOT NOTED HYDRAULIC LEAK ON TAIL. TROUBLESHOT TO LEAKING AUXILIARY HYDRAULIC PUMP. REPLACED PUMP P/N 9914119-3, S/N 124 OFF, S/N 0037 ON. OPERATIONS CHECKED OK. 2 L 7 2 4F A9NM 1999061100206 19990611 00206 EA 1999 6 11 99ZZZX2231 2 19990510 A 7321 25244405 FUEL CONTROLLER BEECH 99 99 1154002 CE PWA PT6 PT6A20 52043 EA RT ENGINE FAILED A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 14MV 1894 A7514 U59 FUEL CONTROLLER FAILED IN-FLIGHT AND DROPPED FUEL PRESSURE TO MIN-FLOW. 1 L 7 2 3T 3 T A14CE E4EA 1999061100213 19990611 00213 NM 1999 6 11 SWAA990925 1 19990526 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED RON CHECK, FOUND CORROSION AT FLOORBEAM, BS 986.5, FROM CENTER TO RT END. REMOVED AND REPLACED FLOORBE AM SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999061100214 19990611 00214 NM 1999 6 11 SWAA990926 1 19990526 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 947-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED RON CHECK, FOUND CORROSION AT STRINGER 28L, BETWEEN BS 947-1006. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999061100215 19990611 00215 NM 1999 6 11 SWAA990927 1 19990526 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM BS 947-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED RON CHECK, FOUND CORROSION AT FUSELAGE SKIN, BS 947-1006, STRINGER 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999061100216 19990611 00216 NM 1999 6 11 SWAA990928 1 19990526 A 5313 6546881 STRINGER BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED RON CHECK, FOUND CRACKS THROUGH EDDY CURRENT INSPECTION AT STRINGERS 6L, AND 6R, AT BULKHEAD STA 1016. REPAIRED STRINGERS PER SWA RA NR 1-353-2086. 2 L 7 2 4F RT A16WE 1999061100217 19990611 00217 NM 1999 6 11 SWAA990929 1 19990526 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM PASSENGER DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 FWD ENTRY WAY, EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999061100218 19990611 00218 NM 1999 6 11 SWAA990930 1 19990526 A 3350 65C27093 COVER BOEING 737 7375H4 138449D NM PASSENGER DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999061100219 19990611 00219 1999 6 11 SWAA990931 4 19990527 A 3418 6554792 SENSOR BOEING 737 7373H4 1384600 NM AOA SYST DAMAGED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 387SW 26602 AIR TURNBACK - DURING AIRCRAFT ROTATION AND UP TO 75 KNOTS AFTER LANDING, STALL WARNING INDICATION, (CONTROL COLUMN VIBR ATOR WENT ON). DISCOVERED CAPTAIN'S AOA SENSOR DAMAGED. REMOVED AND REPLACED AOA SENSOR PER MM. 2 L 7 2 4F RT A16WE 1999061100220 19990611 00220 NM 1999 6 11 SWAA990932 1 19990527 A 5311 6546569 FRAME BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND INTERGRANULAR CORROSION AT BS 1016 BULKHEAD BELT FRAME, RBL 12. REPAIRED FRAME PER S WA RA NR 1-253-2087. 2 L 7 2 4F A16WE 1999061100221 19990611 00221 NM 1999 6 11 SWAA990933 1 19990527 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 1016, STRINGER 24R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F A16WE 1999061100222 19990611 00222 NM 1999 6 11 SWAA990934 1 19990527 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 500, RBL 14. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999061100223 19990611 00223 NM 1999 6 11 SWAA990935 1 19990527 A 5720 6552235 BEAM BOEING 737 7373Y0 1384671 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED TRANSITION CHECK, FOUND LT MAIN LANDING GEAR STABILIZER BEAM CORRODED ARROUND LUGS. REMOVED AND REPLAC ED BEAM PER MM. 2 L 7 2 4F RT A16WE 1999061100224 19990611 00224 NM 1999 6 11 SWAA990936 1 19990529 A 2612 896768 FIRE LOOP BOEING 737 7372H4 138448C NM APU MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 054SW 21535 AIR TURNBACK - DURING TAXING, WITH APU OFF, APU FIRE DETECTION INOP LIGHT ILLUMINATED. SHORTLY AFTER TAKEOFF APU FIRE W ARNING CAME ON. APU FIRE HANDLE PULLED AND BOTTLES DISCHARGED. INSPECTED APU COMPARTMENT NO EVIDENCE OF FIRE. REMOVED AND REPLACED APU TAILPIPE FIRE LOOP DETECTOR PER MM. 2 L 7 2 4F A16WE 1999061100225 19990611 00225 NM 1999 6 11 SWAA990937 1 19990528 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON TOP FLANGE OF FLOORBEAM, BS 294 , RBL 23-47. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999061100226 19990611 00226 NM 1999 6 11 SWAA990938 1 19990528 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 294, LBL 7-11. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999061100227 19990611 00227 NM 1999 6 11 SWAA990939 1 19990528 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAMS, BS 312, LBL 6-RBL 8, BS 294, LBL 21-RBL 24, AND BS 328 RBL 1 4. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999061100228 19990611 00228 NM 1999 6 11 SWAA990940 1 19990528 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 EMERGENCY ESCAPE FLOOR TRACK LIGHT, FWD SECTION INOP. RECONNECTED TRACK SECTION, OPS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 1999061100229 19990611 00229 NM 1999 6 11 SWAA990941 1 19990529 A 5320 963820 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD 2 EA CRACKS, BS 178, LBL 26, WL 197 AND WL 207. REPAIRED CHORD PER SRM . 2 L 7 2 4F A16WE 1999061100230 19990611 00230 NM 1999 6 11 SWAA990942 1 19990529 A 5312 BAC1514 BULKHEAD CHORD BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT BS 1016 BULKHEAD LOWER CHORD BETWEEN STRINGERS 25R-26R. REPAIRED CHORD PER SWA RA NR 1-253-2087. 2 L 7 2 4F A16WE 1999061100231 19990611 00231 NM 1999 6 11 SWAA990943 1 19990529 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM ROW 9 & 14 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS LOOSE AT OVERHEAD BIN BULLNOSE, ROWS 9 RT AND 14 LT. RESECURED L IGHTS PER MM. 2 L 7 2 4F RT A16WE 1999061100232 19990611 00232 NM 1999 6 11 SWAA990944 1 19990530 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 897 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 897, STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999061100233 19990611 00233 1999 6 11 SWAA990945 4 19990601 A 3417 6545752 LINE BOEING 737 7373H4 1384600 NM NR 1 ADC LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 325SW 23689 AIR TURNBACK - AFTER TAKEOFF, CAPTAIN'S AIR SPEED, ALTIMETER, AND IVSI GIVING ERRATIC INDICATIONS. FOUND NR 1 ADC PITOT LINE LOOSE. SECURED LINE PER MM. 2 L 7 2 4F RT A16WE 1999061100234 19990611 00234 NM 1999 6 11 SWAA990946 1 19990531 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 AFT EMERGENCY ESCAPE FLOOR TRACK LIGHTING PULLED LOOSE. REPAIRED TRACK LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999061100235 19990611 00235 NM 1999 6 11 SWAA990947 1 19990601 A 5754 BAC1506 CHORD BOEING 737 7373Y0 1384671 NM NR 5 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED TRANSITION CHECK, FOUND NR 5 LE SLAT T-CHORD CRACKED ARROUND ACTUATOR CUTOUT. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999061100236 19990611 00236 NM 1999 6 11 SWAA990948 1 19990601 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 1 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED C4 CHECK, FOUND NR 1 LE SLAT HAS A 6 INCH LONG CRACK ON AFT RIVET ROW, 27 INCHES FROM INBD END. REPAIR ED SKIN PER SWA RA 1-A57-0691. 2 L 7 2 4F RT A16WE 1999061100237 19990611 00237 NM 1999 6 11 SWAA990949 1 19990601 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999061100238 19990611 00238 NM 1999 6 11 SWAA990950 1 19990601 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED C3 CHECK, FOUND 2 MOST FWD EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP. RECONNECTED LEADS TO UNIT PER MM. 2 L 7 2 4F RT A16WE 1999061100239 19990611 00239 NM 1999 6 11 SWAA990951 1 19990601 A 3350 101114 LIGHT BOEING 737 7375H4 138449D NM RT EMER EXIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 519SW 25318 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 1999061100240 19990611 00240 NM 1999 6 11 SWAA990952 1 19990602 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND A 4 INCH LONG CRACK ON FUSELAGE SKIN, BS 947, BETWEEN STRINGERS 24R-25R. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 1999061100241 19990611 00241 NM 1999 6 11 SWAA990953 1 19990602 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 6L CRACKED AT BS 1016. REPAIRED STRINGER PER SWA RA NR 1-353-2088. 2 L 7 2 4F RT A16WE 1999061100242 19990611 00242 1999 6 11 SWAA990954 4 19990602 A 2565 D31591 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 618WN 28034 DURING SCHEDULED A2 CHECK, FOUND FWD ENTRY DOOR ESCAPE SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999061100243 19990611 00243 NM 1999 6 11 SWAA990955 1 19990602 A 5330 6545890 SKIN BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED TRANSITION CHECK, FOUND CORROSION ON SKIN AT FWD ENTRY DOORWAY, BS 312, WL 276. REPAIRED SKIN PER ER 99-5340. 2 L 7 2 4F RT A16WE 1999061100244 19990611 00244 NM 1999 6 11 TWAA9907801 1 19990526 A 5330 SKIN BOEING 767 767330 NM BS 1213 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 691LF 25137 A DENT APPEARED TO BE STRAIGHTENED OR PRESSED OUT AT STA 1213, BETWEEN STRINGER 35L AND 36L. ORIGINAL DENT 6 IN BY 3 IN BY .187 DEEP. REPAIRED PER SRM 53-00-01, FIG 201. FOUND DURING OP 16 MAINT CHECK. 2 L 7 2 4F RT A1NM 1999061100245 19990611 00245 NM 1999 6 11 TWAA9907802 1 19990529 A 5330 SKIN BOEING 767 767330 NM BS 1439 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 691LF 25137 DURING OP 16 MAINT CHECK, FOUND DENT AND GOUGES IN FUSELAGE SKIN AT STA 1439, FROM STRINGER 33L TO 39L, WITH DENT 26 IN LONG BY 2 IN WIDE AND .093 DEEP. CUT OUT DAMAGE AND REPAIRED PER SRM 53-60-01, FIG 202. 2 L 7 2 4F RT A1NM 1999061100246 19990611 00246 NM 1999 6 11 TWAA9907803 1 19990510 A 5313 STRINGER BOEING 767 767330 NM BS 570-580 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 691LF 25137 DURING OP 16 MAINT CHECK, FOUND CORROSION ON STRINGER 39R AT SPLICE PLATE STA 570 TO 580. REMOVED CORROSION ON STRINGER PER SRM 51-10-00. REMOVED AND REPLACED SPLICE ANGLE PER SRM 51-10-00. 2 L 7 2 4F RT A1NM 1999061100247 19990611 00247 NM 1999 6 11 TWAA9907804 1 19990507 A 5754 SKIN BOEING 767 767231 1385131 NM NR 5 LE SLAT TORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DURING OP 16 MAINT CHECK, FOUND NUMBER 5 LE SLAT INSIDE TE INBD OF OTBD TRACK, BOTTOM SKIN TORN 1 IN BY .5 INCH. INSTAL LED 3 IN BY 2.5 IN FIBERGLASS WET LAY PER SRM 51-70-17 AND SRM 57-41-01 PAGE 204. SEALED AND PAINTED. 2 L 7 2 4F RT A1NM 1999061100248 19990611 00248 NM 1999 6 11 TWAA9907805 1 19990509 A 2730 TEE BOEING 767 767231 1385131 NM RT ELEVATOR WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 608TW 22571 DURING CHECK-C MAINT, FOUND MO 72F01 PHASE A, ON THE RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE, CALLING FOR REPLACEME NT OF TEE. REF SERVICE BULLETIN 27A0136, REV 1. INSTALLED TEE PER SERVICE BULLETIN. 2 L 7 2 4F RT A1NM 1999061100249 19990611 00249 NM 1999 6 11 TWAA9907807 1 19990518 A 2730 TEE BOEING 767 767231 1385131 NM RT ELEVATOR WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 DURING CHECK-C MAINT, MO 72F01 PHASE A, RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE, REQUIRED INSTALLATION OF A NEW TEE AS SHOWN IN FIGURE 2 OF SERVICE BULLETIN 27A0136 REV 1. INSTALLED A TEE PER MODIFICATION ORDER. 2 L 7 2 4F RT A1NM 1999061100250 19990611 00250 NM 1999 6 11 TWAA9907808 1 19990517 A 5754 SKIN BOEING 767 767231 1385131 NM NR 12 LE SLAT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 DURING CHECK-C MAINT, FOUND ON RT WING TOP SIDE OF NUMBER 12 LE SLAT, NEAR OTBD END, A REPAIR AT THE TE OF SLAT IS DELAM INATED. INSTALLED A 6.5 IN BY 4.5 IN HOT BOND REPAIR PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1999061100251 19990611 00251 NM 1999 6 11 AT9900426 1 19990520 A 5320 INTERCOSTAL BOEING 737 7372L9 1384497 NM BS 1006-1016 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND AN INTERCOASTAL AT BS 1006-1016 LBL-4 CORRODED. REMOVED INTERCOSTAL, FABRICATED REPAIR ANGLE, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW B737 SRM 51-20-11, 51-30-2, 51-10-2, 51- 10-6, AND 51-40-3. 2 L 7 2 4F RT A16WE 1999061100252 19990611 00252 NM 1999 6 11 AT9900427 1 19990428 A 5320 ANGLE BOEING 737 7372L9 1384497 NM BS 947 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE AFT CARGO BULKHEAD UPPER FRAME L ANGLE AT BS 947 CORRODED. REMO VED CORRODED ANGLE SECTION AND FABRICATED REPLACEMENT. TREATED, PRIMED, AND INSTALLED IAW B737 SRM 51-40-3, 51-30-2, AN D 53-10-1. 2 L 7 2 4F RT A16WE 1999061100253 19990611 00253 NM 1999 6 11 AT9900428 1 19990423 A 5330 1A462061 SKIN BOEING 737 7372L9 1384497 NM BS 847 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE C-2 DOOR CUT OUT UNDER SCUFF PLATE HAS A V SHAPE GOUGED CHAFFED I NTO THE FUSELAGE EXTERIOR SKIN LOWER AFT CORNER AT BS 847 STRINGER 25R. CUT OUT SKIN AND DOUBLER, HFEC NO CRACKS NOTED. FABRICATED DOUBLER AND FILLER, TREATED, PRIMED, SEALED, AND INSTALLED REPAIRED IAW B737 SRM 51-30-2, 51-20-4, 51-21-31 , AND RES NR 99-1035. 2 L 7 2 4F RT A16WE 1999061100254 19990611 00254 1999 6 11 99FDEA00203 4 19990602 A 3417 ADC AIRBUS 310 A310203 EU LT COCKPIT INOPERATIVE A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 414FE 400 99-123 CAPT A/S TAPE ON PFD STOPED AT 50KTS. REMOVED AND REPLACED ADC. PERF FUNCTIONAL TEST PER 34-10-00 AND 34-18-00 SYS OPS TEST OK. NO LEAKS FND, A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999061100255 19990611 00255 NM 1999 6 11 99FDEA00204 1 19990603 A 7722 EGT INDICATION BOEING 727 727247 138408F NM NR 2 ENGINE HIGH A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 233FE 21327 NR 2 EGT HIGH INTO THE YELLOW BAND (640 DEG C) FOR MORE THAN 5 SEC. PULLED BACK TO 90 PERCENT N1. RETURN TO RDU. NR 2 FUEL FLOW WAS AT 3000 LBS PER HR AND EGT WAS STILL 100 DEG HOTTER THAN 1 AND 3. *S/D* INSTALLED BORESCOPE PLUGS AND I GNITER PLUGS. REMOVED AND REPLACED PS4 UPPER TUBE PER MM 75-31-31. ENG CK GOOD. 2 L 7 3 4F A3WE 1999061100256 19990611 00256 NE 1999 6 11 99FDEA00205 2 19990603 A 7321 8063504 MEC AIRBUS 310 A310203 EU GE CF680 CF680A3 30025 NE NR 2 ENGINE MALFUNCTIONED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 25 408FE 257 NR 2 ENG SHUT DOWN DUE TO LOW OIL PRESS, NO RESTART. *S/D* REMOVED AND REPLACED NR 2 ENG MEC AND FUEL PUMP AS PER AIRB US MM. CK GOOD. REMOVED AND REPLACED CIT SENSOR PER MM. 2 L 7 2 4F 4 F RT A35EU E13NE 1999061100257 19990611 00257 1999 6 11 RRXA991012 4 19990525 A 3457 GPS DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 796FT 46104 NR 2 GPS UNRELIABLE. REMOVED AND CLEANED CONTACTS ON NCU AND PERFORMED GROUND CK ON FLT SYST MANAGEMENT. 2 L 7 4 4F RT 4A25 1999061100258 19990611 00258 WP 1999 6 11 RRXA991013 1 19990526 A 2933 SEAL DOUG DC8 DC873F 302199F WP HYD SYSTEM LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 796FT 46104 LOST HYD FLUID DOWN TO STAND PIPE. FOUND O-RING SEAL LEAKING AT T FITTING ON RUDDER ACCUMULATOR. REMOVED AND REPLACED SEAL, SERVICED HYD SYST. OPS CK GOOD, NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 1999061100259 19990611 00259 1999 6 11 RRXA991014 4 19990527 A 3460 CONNECTOR DOUG DC8 DC873F 302199F WP E/E BAY CONTAMINATED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 796FT 46104 NR 1 AND NR 2 FMS BECAME UNRELIABLE AFTER APPROX 2HRS INTO FLIGHT. NR 1 AND NR 2 FMS INOP, PLACARDED AS SUCH PER MEL 34- 37-, CAT D, DMI NR'S NR 1 D7575041-1853 AND NR 2 D7575042-1854, DUE 24 SEP 99 PLACARDS INSTALLED. NR 1 FMS, CLEANED CAN NON PLUG ON DADC. OPS CKS NORMAL AS PER MM 34 ON GROUND FOR 3 HRS THIS CLEARS MEL34-37 NR 2 FMS. CLEANED CANNON PLUG O N DADC. OPS CKS NORMAL ON GROUND FOR 3 HRS AS PER MM 34 THIS CLEARS MEL 34-37 CONT NR 7575042-1854. REMOVED PLACARD. 2 L 7 4 4F RT 4A25 1999061100260 19990611 00260 NM 1999 6 11 SWAA990956 1 19990603 A 3240 26010425 BRAKE BOEING 737 7372T4 1384492 NM RT MLG MALFUNCTIONED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 SW 07 130SW 22699 ABORTED TAKEOFF - ON TAKEOFF ROLL AT 80 KNOTS, THE AIRCRAFT VIBRATED HEAVILY AND BEGAN TO PULL TO THE RIGHT . VIBRATION CONTINUED UNTIL THE AIRCRAFT STOPPED. REMOVED AND REPLACED NR 3 MLG BRAKE ASSY AND NR 3 TIRE/WHEEL ASSY PER MM. 2 L 7 2 4F A16WE 1999061100261 19990611 00261 NM 1999 6 11 SWAA990957 1 19990531 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 15 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 628SW 27703 WIRES LOOSE AT EMERGENCY ESCAPE FLOOR TRACK LIGHTS AT ROW 15. SECURED WIRES PER MM. 2 L 7 2 4F RT A16WE 1999061100262 19990611 00262 NM 1999 6 11 SWAA990958 1 19990603 A 5315 6546804 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED TRANSITION CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM, BS 986.5, RBL 5-BL 0. REPAIRED BEAM PER EO 99-5383. 2 L 7 2 4F RT A16WE 1999061100263 19990611 00263 NM 1999 6 11 SWAA990959 1 19990602 A 5400 310A1050 STRAP BOEING 737 7373H4 1384600 NM NR 2 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED SERVICE CHECK, FOUND A 2.5 INCH LONG CRACK ON NR 2 PYLON STRAP UNDER THE FRAME, NAC STA 236 RT. REMOVE D AND REPLACED STRAP PER SRM. 2 L 7 2 4F RT A16WE 1999061100264 19990611 00264 NM 1999 6 11 SWAA990960 1 19990603 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED 1/2D CHECK, FOUND THROUGH EDDY CURRENT INSPECTION A CRACK AT BULKHEAD, BS 178 , LBL 13. REPAIRED BULKH EAD PER SRM. 2 L 7 2 4F RT A16WE 1999061100265 19990611 00265 1999 6 11 SWAA990961 4 19990603 A 2565 NAS623 FASTENER BOEING 737 7373H4 1384600 NM GIRT BAR SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 655WN 28400 DURING SCHEDULED C3 CHECK, FOUND SHEARED FASTENER AT FWD ENTRY DOOR GIRT BAR ATTACH HANGER. REMOVED AND REPLACED FASTEN ER PER SRM. 2 L 7 2 4F RT A16WE 1999061100266 19990611 00266 1999 6 11 SWAA990962 4 19990603 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM PASSENGER DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS BELOW LIMITS. REMOVED AND REPLACED SLIDE AS SY PER MM. 2 L 7 2 4F RT A16WE 1999061100267 19990611 00267 WP 1999 6 11 TWAA9907402 1 19990524 A 2121 034964 FAN DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923TW 49379 DURING PRE-FLIGHT, A STRONG ODOR WAS NOTED THROUGHOUT THE AIRCRAFT. THE PASSENGERS WERE REMOVED FROM THE AIRCRAFT SAFEL Y. THE RADIO STANDBY COOLING FAN WAS THE PROBLEM. THE STANDBY COOLING FAN WAS PLACARDED. CHECKS WERE MADE TO ASSURE N ORMAL PERFORMANCE. CHECK-C 7-25-98 STL. THE STANDBY RADIO RACK FAN WAS REPLACED AND THERE WERE NO FURTHER PROBLEMS. 2 L 7 2 4F RT A6WE 1999061100268 19990611 00268 WP 1999 6 11 TWAA9907901 1 19990603 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY EXIT DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 955U 49427 FOUND THE OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 2-19-99 STL. 2 L 7 2 4F A6WE 1999061100269 19990611 00269 WP 1999 6 11 TWAA9907902 1 19990525 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 190-210 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND REPAIR ON FLOOR MEMBRANE BETWEEN STA 190 TO 210, LBL O IN TO 22 IN, WAS COMING LOOSE AND HAD POPPED RIVETS INSTALLED. REPLACED MEMBRANE PER SPM 6-70-01, 775T3 30 PER ORIGINAL SAMPLE. 2 L 7 2 4F A6WE 1999061100270 19990611 00270 WP 1999 6 11 TWAA9907903 1 19990525 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 200. NUMBER 1 FLOOR TRACK TO MEMBRANE AREA, LBL 50. C ORROSION WAS REMOVED PER SRM 6-80-01, PAGE 1 AND REPLACED FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999061100271 19990611 00271 WP 1999 6 11 TWAA9907904 1 19990528 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 756-803 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND SKIN CORROSION BEYOND LIMITS AT STA 756 TO 803, RBL 26L TO 26R. REPLACED SKIN PER DOUGL AS DRAWING 5911421 AND 5916154, AND SPM 6-70-01. 2 L 7 2 4F A6WE 1999061100272 19990611 00272 WP 1999 6 11 TWAA9907905 1 19990525 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1060 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 DURING CHECK-C MAINT, FOUND LOWER CHORD ATTACH BOLTS TO STRINGER 30 AND 29L WERE RUSTY AND CORRODED, STA 1060 FRAME. IN STALLED NEW FRAME AT STA 1060 PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999061100273 19990611 00273 NM 1999 6 11 HNAA9900063 1 19990527 A 3350 6013211X BATTERY DHC8 DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 936HA 4940 4940 145 145 SIX FRONT CABIN FLOOR EMERGENCY LIGHTS ARE OUT. REMOVED AND REPLACED PS2 BATTERY. 2 H 7 2 4T RT A13NM 1999061100274 19990611 00274 NM 1999 6 11 HNAA9900064 1 19990603 A 3350 6104791 LIGHT DHC DHAV DHC8 DHC8102 2809003 NM CABIN SHORTED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 910HA 022 FLOOR ESCAPE PATH LIGHTS WENT OFF, APU FAILURE. REMOVED AND REPLACED 3352-P1 BASE, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999061100275 19990611 00275 NM 1999 6 11 HNAA9900065 1 19990603 A 3350 6013211X BATTERY DHC DHAV DHC8 DHC8201 2809001 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 986HA 21661 21661 421 421 NR 1 AND NR 3 OVHD EMERGENCY CEILING AISLE LIGHTS ARE INOP. REMOVED AND REPLACED BATTERIES PS1 AND PS2, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999061100276 19990611 00276 EU 1999 6 11 MALA976481 1 19990530 A 5210 HC521H0399002 MECHANISM BAC 146 AVRO146RJ85A 1500097 EU PASSENGER DOOR MALFUNCTIONED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 516XJ E2334 AIRCRAFT MAIN FORWARD CABIN DOOR WILL NOT OPEN OR CLOSE FROM THE OUTSIDE. MAINTENANCE REPLACE DOOR GUIDE, ROLLER AND ST OP PLATE. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999061100277 19990611 00277 EU 1999 6 11 MALA976482 1 19990603 A 7410 SWITCH SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT & RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 106XJ 106 DURING FLIGHT, THE LEFT IGNITION LIGHT ILLUMINATED WITH BOTH POWER LEVERS FORWARD OF YELLOW TAPE. AS PER MAINTENANCE CO NTROL, ALL ENGINE INDICATIONS NORMAL. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT AND RIGHT AUTO IGNITION PRES SURE SWITCHES. OPS CHECK GOOD. IAW AMM 74. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999061100278 19990611 00278 EU 1999 6 11 MALA976483 1 19990602 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A MALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 GL 15 421XJ 421 CARGO SMOKE LIGHT ILLUMINATED ON APPROACH TO PIT. CREW ACTIVATED NR 1 FIRE BOTTLE, LIGHT WENT OUT. NO OTHER FIRE OR SM OKE INDICATIONS WERE OBSERVED. MAINTENANCE REPLACED NR 1 CARGO FIRE BOTTLE AND BOTH SMOKE DETECTORS AS A PRECAUTION. S ECURITY AND OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999061100279 19990611 00279 EU 1999 6 11 MALA976484 1 19990602 A 3520 5500AIUBF25A OXYGEN BOTTLE BAC 146 AVRO146RJ85A 1500097 EU CABIN DEPLETED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 504XJ E2311 BOTH CABIN PASSENGER O2 BOTTLES USED IN FLIGHT. MAINTENANCE REPLACED BOTH AFT O2 BOTTLES. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999061100280 19990611 00280 EU 1999 6 11 MALA976485 1 19990601 A 2560 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU SERVICE DOOR DEPLOYED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 523XJ E2348 AFT SERVICE DOOR SLIDE PARTIALLY DEPLOYED. MAINTENANCE REPLACED AFT SERVICE SLIDE IAW AMM 25-60-11. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999061100281 19990611 00281 EU 1999 6 11 MALA976486 1 19990527 A 2560 6500112 LIGHT BAC 146 AVRO146RJ85A 1500097 EU CABIN INOPERATIVE A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 501XJ E2208 FWD EMERGENCY FLASHLIGHT RED INDICATOR LIGHT NOT FLASHING. MAINTENANCE REPLACED FLASHLIGHT. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999061100282 19990611 00282 EU 1999 6 11 MALA976487 1 19990602 A 3350 1317 LAMP SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119XJ 119 EMERGENCY LIGHT ON WALL AT 1C/D INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999061100283 19990611 00283 EU 1999 6 11 MALA976488 1 19990528 A 3610 7275031507 BLEED LINE SAAB SF340 340B 7860101 EU LT ENGINE CRACKED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 424XJ 424 DURING TAKEOFF, NOTED FOD ON RUNWAY, AFTER TAKEOFF TEMP INSIDE AIRCRAFT WAS RISING AS WAS ITT ON LEFT ENGINE, FOLLOWED Q RH, RESET BLEEDS YET TEMP WAS RISING. RETURNED TO MSP. MAINTENANCE COMPLETED COLD AND HOT SECTION AND INLET BOROSCOPE INSPECTION PER TASK CARD 723802, 724402, AND 724403. FOUND NO FOD NOR NOTICEABLE DAMAGE TO ENGINE. INSPECTED BLEED DUC TS FOUND HP BLEED LINE FLANGE CRACKED, REPLACED LINE. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999061100284 19990611 00284 EU 1999 6 11 MALA976489 1 19990526 A 2611 CONNECTOR SAAB SF340 340B 7860101 EU LAVATORY DIRTY A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 424XJ 424 EN ROUTE FROM BMI, THE LAV SMOKE ANNUN LIGHT CAME ON, NO SMOKE WAS PRESENT. MAINTENANCE CLEANED DUST FROM AROUND ENTIRE INSIDE AREA OF LAVATORY, AROUND LAV SMOKE DETECTOR, CLEANED OFF CANNON PLUG AND RE-SECURED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999061100285 19990611 00285 NE 1999 6 11 MALA976490 2 19990526 A 7260 CHIP LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 106XJ 106 LEFT CHIP DETECT LIGHT ILLUMINATED AFTER TAKEOFF FROM DTW. RETURNED TO DTW. MAINTENANCE INSPECTED CHIP DETECTOR FOR DE BRIS, DEBRIS WAS MINIMAL AND ALLOWABLE IAW GE MM CHAP 72-00-00 PG 198. INSPECTED CHIP DETECTOR CANNON PLUG, NO DEFECTS NOTED. GROUND RAN ENGINE, NO ILLUMINATION OF LIGHT NOTED. LEAK CHECKS GOOD. ALL WORK DONE IAW GE MM CHAP 72-00-0 TROU BLE 10. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999061100286 19990611 00286 EU 1999 6 11 MALA976491 1 19990530 A 3350 LIGHT BAC 146 AVRO146RJ85A 1500097 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 526XJ E2351 DURING PREFLIGHT, FIRST CLASS SECTION EMERGENCY LIGHT WON'T ILLUMINATE. MAINTENANCE CYCLED AIRCRAFT MASTER SWITCH SEVER AL TIMES. OPS NORMEL PER M/C. 2 H 7 4 4F RT A49EU 1999061100287 19990611 00287 EU 1999 6 11 MALA976492 1 19990530 A 3350 SWITCH BAC 146 AVRO146RJ85A 1500097 EU CABIN OUT OF POSITION A MALA K NONE L W NO TEST INADEQUATE Q C IN INSP/MAINT 1 GL 15 526XJ E2351 FIRST CLASS FLOOR EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE CLEANED CANNON AND FOUND SWITCH IN ARMED POSITION. OPS CH ECK GOOD. 2 H 7 4 4F RT A49EU 1999061100288 19990611 00288 EU 1999 6 11 MALA976493 1 19990529 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO COMPT CONTAMINATED A MALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 110XJ 340A110 CARGO SMOKE ANNUN ILLUMINATED, DURING GROUND OPERATIONS. RETURNED TO GATE. MAINTENANCE REPLACED CARGO SMOKE DETECTOR, SUSPECTED ANTS IN DETECTOR CAUSING FAULT. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999061100289 19990611 00289 EU 1999 6 11 MALA976494 1 19990530 A 2611 005WS00 WEU SAAB SF340 SF340A 7850100 EU CARGO COMPT FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 110XJ 340A110 CARGO SMOKE ANNUN ILLUMINATED SIX MINUTES AFTER TAKEOFF AROUND 6000 FEET. ILLUMINATED INTERMITTENTLY FOUR TIMES THEN RE MAINED OFF FOR THE REMAINING TRIP BACK TO DTW. MAINTENANCE REPLACED WEU. ALL WORK DONE IAW SAAB 340 MM. ALL CHECKS GO OD. 2 L 7 2 4T RT A52EU 1999061100290 19990611 00290 NM 1999 6 11 PCAA9900014 1 19990601 A 2910 LINE DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYST FAILED A PCAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 13 834EX 285 FLT 3640, EN ROUTE TO BWI, THE NR 2 HYDRAULIC SYSTEM INDICATED ZERO QUANTITY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTE NANCE INSPECTED SYSTEM, FOUND THE HYDRAULIC LINE AT THE NR 2 GEAR ACTUATOR AT FAULT. INSTALLED A FLEXIBLE LINE PER MANU AL PROCEDURES. CHECKED SYSTEM PER CHAPTER 05. SUBSEQUENTLY, THE HYDRAULIC FLEXIBLE LINE WAS REPLACED WITH ORIGINAL EQU IPMENT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999061100291 19990611 00291 NM 1999 6 11 9901915526 1 19990602 A 3260 LIGHT BOEING 757 757251 1384970 NM RT MLG INOPERATIVE A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 526US 23620 RIGHT MAIN LANDING GEAR DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE UPON LANDING GEAR EXTENSION. THE LANDING GEAR WAS CYCLED AND THE COM PROCEDURE WAS ACCOMPLISHED. THE CREW WAS STILL UNABLE TO OBTAIN A DOWN AND LOCKED INDICATION. AFTER DECLARING AN EMERGENCY, THE FLIGHT WAS CONCLUDED IN MSP WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR INDICATOR LIGHT ASSEMBLY WITH A SERVICEABLE UNIT. OPERATIONAL TESTS OF THE SYSTEM WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999061100292 19990611 00292 NM 1999 6 11 9901926309 1 19990602 A 3350 LIGHT BOEING 747 747451 1384940 NM ROW 51-66 INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK (PEK), FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-66. RECONNECTED ELECTRICAL CONNECTO R. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999061100293 19990611 00293 EU 1999 6 11 9901933243 1 19990519 A 3242 21600 BRAKE BFGOODRICH AIRBUS 320 A320212 EU LT MLG FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 343NW 17187 1691 387 DURING POST FLIGHT INSPECTION, FOUND SEVERAL CARBON PIECES AROUND THE NR 1 BRAKE AND WHEEL ASSEMBLY. WHEEL REMOVAL REVE ALED THAT THE BRAKE CARBON DISCS (ROTORS AND STATORS) WERE OXIDIZED AND REDUCED TO SEGMENTS. MAINTENANCE REPLACED THE N R 1 BRAKE AND WHEEL ASSEMBLY. 2 L 7 2 4F RT A28NM 1999061100294 19990611 00294 NM 1999 6 11 9901946719 1 19990410 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM BS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING M CHECK, FOUND CRACK IN UPPER DECK FLOORBEAM UPPER CHORD FS 400. PERMANENT REPAIR WAS MADE PER EA 67-155225. 2 L 7 4 4F A20WE 1999061100295 19990611 00295 NM 1999 6 11 9901952769 1 19990402 A 5314 KEEL BEAM BOEING 727 7272M7 138407S NM BS 950-1000 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 729RW 21742 DURING M CHECK, FOUND CORROSION ON KEEL BEAM FS 950 - 1000, RBL 6. REPAIRED PER EA 27-164644. 2 L 7 3 4F A3WE 1999061100296 19990611 00296 WP 1999 6 11 9901961144 1 19990420 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1353-1365 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING M CHECK, FOUND CORROSION ON BELLY SKIN AT FS 1353 - 1365 AND LONGERON 51L - 52L. REPAIRED PER EA 11-166595. 2 L 7 3 4F A22WE 1999061100297 19990611 00297 WP 1999 6 11 MWEA99314 1 19990601 A 2560 113317 SLIDE DOUG DC9 DC915 3022036 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 500ME 45711 THE GALLEY DOOR SLIDE FELL OFF DOOR. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999061100298 19990611 00298 NM 1999 6 11 MWEA99315 1 19990601 A 2560 D29985107 SLIDE DOUG MD88 MD88 3023688 NM SERVICE DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE AFT SERVICE DOOR SLIDE PACK FELLOFF. MAINTENANCE REINSTALLED AFT SERVICE DOOR SLIDE PACK. 2 L 7 2 4F RT A6WE 1999061100299 19990611 00299 WP 1999 6 11 MWEA99316 1 19990601 A 5312 5910186 VENTRAL DOOR DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD NOT SEALED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 300ME 45718 THE AFT CABIN VENTRAL DOOR BEGAN SQUEALING ON CLIMB-OUT. MAINTENANCE FOUND AFT PRESSURE DOOR NOT PROPERLY SEATED IN ITS BOTTOM CLEVIS AND RESEATED. 2 L 7 2 4F A6WE 1999061100300 19990611 00300 WP 1999 6 11 MWEA99317 1 19990601 A 5330 59114192 SKIN DOUG DC9 DC914 3022034 WP BS 737 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME FUSELAGE SKIN IS DENTED AT STATION 737 LONGERON 16R. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061100301 19990611 00301 NM 1999 6 11 MWEA99318 1 19990601 A 5610 5912290501 WINDSHIELD DOUG MD88 MD88 3023688 NM LT COCKPIT CRACKED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 810ME 48072 THE CAPTAINS WINDSHIELD CRACKED DURING CLIMB. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD. 2 L 7 2 4F RT A6WE 1999061100302 19990611 00302 NM 1999 6 11 SCNA99708 1 19990603 A 3350 9008352 BATTERY PACK BOEING 727 727225 1384077 NM L1 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE CHECK, L1 ENTRANCE WAY EMERGENCY EXIT BATTERY PACK FAILS TO HOLD A CHARGE. REMOVED AND REPLACE D EMERGENCY EXIT BATTERY PACK IAW B727 MM 335002. OPERATIONS CHECK GOOD IAW 335000. 2 L 7 3 4F A3WE 1999061100303 19990611 00303 NM 1999 6 11 SCNA99078 1 19990531 A 3350 LIGHT BOEING 727 727259 138408J NM ROW 5BAC INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE FORWARD HALF OF THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. RE PAIRED THE CONNECTION AT SEATS 5ABC FOR FLOOR TRACK EMERGENCY LIGHTING. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999061100304 19990611 00304 SO 1999 6 11 SWIA971486 1 19990503 A 3610 BLEED LINE EMB 120 EMB120RT SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 289YV 120289 OUTBOARD LEFT STABALIZER, VERTICAL FIN, OUTBOARD RIGHT WING, RIGHT ENGINE AIR INLET ANNUNICATOR INOP ON DE-ICE PANEL. R ETURNED TO LAX. REPLACED RIGHT ENGINE BLEED AIR LINE AND ALSO REPAIRED CHAFFED WIRE ON EJECTOR VALVE IN THE BELLY. RAN ENGINE FOR SEVERAL MINUTES IN ALL CONFIGURATIONS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100305 19990611 00305 SO 1999 6 11 SWIA971487 1 19990505 A 2750 WIRE EMB 120 EMB120RT SO PWA 118 PW118A NE LT TE FLAP CHAFED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 250YV 120250 INBOARD FLAPS WOULD NOT RETRACT AND A DISAGREEMENT INBOARD FLAPS. CYCLED 3 TIMES. RETURNED TO LAX. REPAIRED CHAFFED W IRE ON LEFT INBOARD FLAP. CYCLED FLAPS NUMEROUS TIMES. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100306 19990611 00306 SO 1999 6 11 SWIA971488 1 19990506 A 5220 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT EMER EXIT NOT LATCHED A SWIA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 NM 07 187SW 120037 AIRCRAFT WOULD NOT PRESSURIZE IN AUTO. RETURNED TO SLC. FOUND REAR RIGHT EMERGENCY EXIT AUTO HANDLE PANEL OPEN. CLOSE D PANEL. OPS CHECK GOOD DURING GROUND PRESSURIZATION RUN. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100307 19990611 00307 SO 1999 6 11 SWIA971489 1 19990506 A 2912 FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYDRAULIC SYST CONTAMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 209SW 120269 HYDRAULIC FILTER LIGHT ILLUMINATED ALONG WITH HYD LIGHT ON MAP. RETURNED TO SLC. FOUND HYDRAULIC PRESSURE FILTER BYPAS S POPPED. REMOVED AND REPLACED PRESSURE RETURN FILTER. OPS CHECK AND LEAK CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100308 19990611 00308 SO 1999 6 11 SWIA971490 1 19990507 A 2912 FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE BLUE HYD SYST CONTAMINATED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 188SW 120039 HYDRAULIC FILTER BLUE SYSTEM LIGHT ILLUMINATED. RETURNED TO SLC. REPLACED BLUE SYSTEM RETURN FILTERS. OPS AND LEAKS C HECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100309 19990611 00309 SO 1999 6 11 SWIA971491 1 19990509 A 5210 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PASSENGER DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 189SW 120048 LOSS OF CABIN PRESSURIZATION AT 24,000 FT WITH AUTO MODE ACTIVE AT TIME OF LOSS. MANUAL MODE INEFFECTIVE TO REGAIN CONT ROL. RETURNED TO SLC. REMOVED AND REPLACED PASSENGER DOOR SEAL IAW MM 52-10-04. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100310 19990611 00310 NE 1999 6 11 SWIA971492 2 19990501 A 7261 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1 ENGINE FAILED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 297SW 120327 ATC REPORTED BLACK SMOKE COMING FROM NR 1 ENGINE ON INITIAL CLIMB-OUT. REPORTED CONFIRMED BY OTHER PILOTS ON GROUND. R ETURNED FOR LANDING AT SBA. NO COCKPIT INDICATIONS OF ENGINE FIRE ON NR 1. REPLACED GARLOCK SEAL FOR AIR OIL SEPARATOR BLEEDER TUBE. PERFORMED OPS AND LEAK CHECK. OPS CHECK GOOD. NO LEAK NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100311 19990611 00311 NM 1999 6 11 TWAA9908001 1 19990604 A 3350 8100022604 LIGHT BOEING 767 7673Q8 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 FOUND INOPERATIVE EGRESS LIGHT ON RT SIDE OF CABIN, AFT PART OF FIRST CLASS. REPLACED LIGHT ASSEMBLY. CHECK-C 4-9-99 L AX. - 2 L 7 2 4F RT A1NM 1999061100312 19990611 00312 WP 1999 6 11 TWAA9908002 1 19990604 A 3350 SWITCH DOUG DC9 DC982 3022082 WP COCKPIT OUT OF POSITION A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 902TW 49153 THE EGRESS LIGHTING CAME ON WITH EMERGENCY LIGHT SWITCH IN THE OFF POSITION. CHECKS WERE MADE TO VERIFY THE PERFORMANCE OF THE SYSTEM. UNABLE TO DUPLICATE THE REPORTED PROBLEM. CHECK-C 2-9-99 STL. 2 L 7 2 4F A6WE 1999061100313 19990611 00313 NE 1999 6 11 TWAA9908003 2 19990605 A 7250 TURBINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE DAMAGED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 CE 05 925TW 49357 3262 THE RT ENGINE SHUT ITSELF DOWN WHILE EGT INDICATION INCREASED. CREW ACCOMPLISHED THE ENGINE SHUT DOWN PROCEDURE AND MAD E UNSCHEDULED LANDING AT IND. FOUND TURBINE FAILURE AND REPLACED THE ENGINE. CHECK-C 8-24-98 STL. *S/D* FOUND FOD IM PACT TO 1 EACH 7TH STAGE COMPRESSOR BLADE CAUSED THE BLADE TO FRACTURE FROM FATIGUE PROPAGATION. 2 L 7 2 4F 4 F A6WE E9NE 1999061100314 19990611 00314 WP 1999 6 11 TWAA9908004 1 19990604 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROW 22-23 INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9401W 53137 EGRESS LIGHTING EMERGENCY EXIT STRIPS WERE MISSING AT ROW 22 AND 23, AND IN FRONT OF LAVS. REPLACED THE EGRESS LIGHT PO WER SOURCE (P/N 5822-2) AND THE RED LENS AT ROWS 21, 29, 32 AND 33. LENS (P/N 0105607-301). CHECK-C 12-15-98 MCI. 2 L 7 2 4F RT A6WE 1999061100315 19990611 00315 NE 1999 6 11 TWAA9908005 2 19990603 A 7314 3782017 PUMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LT ENGINE WORN A TWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 05 923L 47109 2147 THE LEFT ENG SHUT ITSELF DOWN DURING TAKEOFF AT 800 FEET. CREW ACCOMPLISHED ENGINE SHUT DOWN AND RETURNED TO STL. REPL ACED THE FUEL CONTROL, (P/N 743602-5) AND FUEL PUMP, (P/N 378201-7). CHECK-C 3-26-99 MCI. 2 L 7 2 4F 4 F A6WE E2EA 1999061100316 19990611 00316 NM 1999 6 11 TWAA9908006 1 19990602 A 5520 251T20021 TEE BOEING 767 767231 1385131 NM RT ELEVATOR WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING CHECK-C MAINT MO 72F01 CALLED FOR REPLACING THE RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE TEE. REPLACED TEE P ER SERVICE BULLETIN 27A0136, REV 1. 2 L 7 2 4F RT A1NM 1999061100317 19990611 00317 WP 1999 6 11 AT9900429 1 19990602 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 737-756 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT SUBFLOOR MEMBRANE AT BS 737-756 CORRODED AND CRACKED. FOR MED, TRIMMED, DRILLED, DEBURRED, TREATED AND PRIMED NEW SUBFLOOR MEMBRANE IAW DC9 SRM 51-10-2, 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1999061100318 19990611 00318 WP 1999 6 11 AT9900430 1 19990602 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION UNDER PREVIOUS REPAIR AT THE FLOORBEAM UPPER CHORD AT BS 160 RBL 50. REMOVED FLOORBEAM DAMAGE AREA. FABRICATED REPAIR FLOORBEAM AND ANGLE, DEBURRED, COUNTERSUNK, TREATED, PRIM ED AND INSTALLED REPAIR IAW DC9 SRM 53-11-01, 51-10-00 AND EO NR 99-1153. 2 L 7 2 4F A6WE 1999061100319 19990611 00319 WP 1999 6 11 AT9900431 1 19990602 A 5530 991180832 ANGLE DOUG DC9 DC932 3022066 WP BS 1251 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND A CRACK ON THE RIGHT SIDE VERTICAL STABILIZER ANGLE ADJACENT TO THE ACME SCREW NUT MOUNT AT BS 1251. REMOVED OLD FITTING, FABRICATED REPAIR ANGLE, FORMED, DRILLED AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-6, AND DOUGLAS DRAWING NR 9911808. 2 L 7 2 4F A6WE 1999061100320 19990611 00320 WP 1999 6 11 AT9900432 1 19990603 A 3610 DUCT DOUG DC9 DC932 3022066 WP TAIL COMPT LOOSE A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 834AT 47488 TAIL COMPARTMENT TEMPERATURE CAME ON IN FLIGHT FOR A FEW SECONDS ON CLIMBOUT, PERFORMED STEP IN ORH AND RETURNED TO HOUS TON. GROUND START OPS CHECKED FOR LEAKS IN AFT COMPARTMENT, DISCONNECTED LEFT PACK PER DDP. RECONNECTED LEFT PACK FOR TROUBLESHOOTING, NO DEFECTS FOUND. CHECKED CLAMPS FOR SECURITY, OPS CHECKED NORMAL IAW MM 21-50. 2 L 7 2 4F A6WE 1999061100321 19990611 00321 NM 1999 6 11 AWXA9900210 1 19990527 A 5347 152015427178TC51 SEAT TRACK BOEING 737 7373B7 1384580 NM BS 520-540 MISINSTALLED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 LBL 45, SEAT TRACK SECTIONS AT BS 520 SPLICE AREA ARE MIS-MATCHED. REMOVED BAD SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW SRM 53-30-52, FIG 1. TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-20-01. REINSTALLED NEW SEAT TRAC K IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999061100322 19990611 00322 NM 1999 6 11 AWXA9900211 1 19990527 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373B7 1384580 NM BS 380-520 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 332AW 23384 FS 380-520 RBL 45, SEAT TRACK GOUGED BEYOND LIMITS. REMOVED SEAT TRACK FS 380-520 RBL 45 IAW SRM 51-40-02. FABRICATED REPLACEMENT SEAT TRACKS PER SRM 53-30-52, FIG 1. TREATED AND PRIMED SEAT TRACKS IAW SRM 51-20-01. INSTALLED SEAT TRACK S FS 380-520 RBL IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999061100323 19990611 00323 NM 1999 6 11 AWXA9900212 1 19990603 A 5320 654541041 CHORD BOEING 737 737277 1384570 NM BS 663 CRACKED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 BL 0, BS 663, TRAVERSE FLOORBEAM UPPER T CHORD CRACKED. REPAIRED PER ER 2-15-12-12B AND SB 737-57-1210. 2 L 7 2 4F RT A16WE 1999061100324 19990611 00324 NM 1999 6 11 AWXA9900213 1 19990603 A 5330 SKIN BOEING 737 737277 1384570 NM BS 967 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 R2 DOOR LOWER FORWARD CORNER OF FUSELAGE CUTOUT CRACKED AT BS 967, WL 208. REPAIRED IAW SRM 53-30-3, FIG 24. 2 L 7 2 4F RT A16WE 1999061100325 19990611 00325 NM 1999 6 11 AWXA9900214 1 19990603 A 5320 BAC148951 ANGLE BOEING 737 737277 1384570 NM BS 460 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 FORWARD PIT STATION 460 LT BETWEEN STR 20L AND 21L, INBOARD FRAME FLANGE HAS 3 CRACKS AT 3 RIVETS. REMOVED DAMAGED ARE A, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-40-3, FIGURE 1 AND SRM 53-10-2. 2 L 7 2 4F RT A16WE 1999061100326 19990611 00326 NM 1999 6 11 AWXA9900215 1 19990603 A 5320 654541051 ANGLE BOEING 737 737277 1384570 NM BS 675 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 CRACK, BL 0, BS 675, TRAVERSE FLOORBEAM LOWER T ANGLE CHORD CRACKED IN RADIUS. REPAIRED PER SB 737-57-1106 AND AWA ER 2 -57-12-13. 2 L 7 2 4F RT A16WE 1999061100327 19990611 00327 NM 1999 6 11 AWXA9900216 1 19990603 A 5311 BAC15171147 FRAME BOEING 737 737277 1384570 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 FORWARD PIT STATION 500 LT BETWEEN STR 24L AND 25L, INBOARD FRAME FLANGE HAS CRACK AND CORROSION AT 2 NUT PLATE ATTACH H OLES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-40-3, FIGURE 1. 2 L 7 2 4F RT A16WE 1999061100328 19990611 00328 NM 1999 6 11 AWXA9900217 1 19990603 A 5330 SKIN BOEING 737 737277 1384570 NM R2 DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 APPROXIMATELY .625 INCH CRACK ON THE R2 DOOR CUTOUT, UPPER HINGE EXTENDING FROM UPPER CUTOUT FORWARD. CUT OUT THE DAMAG ED AREA, FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-30-3, FIGURE 21A. 2 L 7 2 4F RT A16WE 1999061100329 19990611 00329 NM 1999 6 11 AWXA9900218 1 19990603 A 5330 SKIN BOEING 737 737277 1384570 NM L1 DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 A .875 INCH CRACK ON THE L1 DOOR CUTOUT, UPPER HINGE EXTENDING FROM FORWARD CENTER OF CUTOUT FORWARD. CUT OUT DAMAGED A REA, FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-30-3, FIGURE 21 AND AWA ER 2-53-32-28. 2 L 7 2 4F RT A16WE 1999061100330 19990611 00330 NM 1999 6 11 AWXA9900219 1 19990603 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 BS 727A+10 BELOW STRINGER 17L, FUSELAGE SKIN CRACKED APPROXIMATELY 3 INCHES. ACCOMPLISHED REPAIR PER AWA ER 2-53-35-30. 2 L 7 2 4F RT A16WE 1999061100331 19990611 00331 EU 1999 6 11 AWXA9900220 1 19990604 A 4910 INLET AIRBUS 320 A320231 3930325 EU APU DIRTY A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 646AW 271 CONDITIONED AIR HAS PUNGENT ODOR (SMELLS LIKE DIRTY SOCKS), NUMEROUS PASSENGER COMPLAINTS. PLACED ON MEL 36-12-01, CONT ROL NUMBER 105131, APU BLEED AIR SYSTEM INOP. CLEANED APU INLET SCOOP / BOX ASSEMBLY. RAN APU, NO SMELL DETECTED. REM OVED MEL 31-12-01. 2 L 7 2 4F RT A28NM 1999061100332 19990611 00332 NM 1999 6 11 CALA9900631 1 19990603 A 3222 654628811 TORSION LINK BOEING 737 7373T0 1384582 NM NLG BROKEN A CALA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 09 60312 23363 ON LANDING ROLL AT APPROXIMATELY 70 KNOTS WITH NORMAL NOSE WHEEL TOUCHDOWN, A VIOLENT SHIMMY WAS FELT ON RUNWAY UNTIL AI RCRAFT MADE A COMPLETE AND SAFE STOP. THERE WAS NO NOSE WHEEL STEERING CAPABILITY. THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND THE UPPER AND LOWER NLG TORSION LINKS BROKEN. BOTH TORSION LINKS AND THE NOSE WHEEL STEERING COLLAR WERE REMOVED AND REPLACED IAW MM 32-21-11 AND 32-51-61. ALSO, BOTH NOSE WHEEL ASSEMBLIES WERE REPLACED. THE NLG INNER CYLINDER WAS REPLACED DUE TO HEAT DAMAGE CAUSED BY EXCESSIVE NOSE GEAR VIBRATION. 2 L 7 2 4F RT A16WE 1999061100333 19990611 00333 NM 1999 6 11 CALA9900632 1 19990603 A 3397 WIRE BOEING 727 727224 1384076 NM ROW 12 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79749 22451 THE EMERGENCY PATH LIGHTING AT SEAT NR 12 WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOUND AT LIGHT ASSE MBLY AND OPERATION CHECKED GOOD IAW MM 33-50-02, PAGE 201. 2 L 7 3 4F A3WE 1999061100334 19990611 00334 WP 1999 6 11 CALA9900633 1 19990603 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 237 BELOW LONGERON 17L. A DOUBLER WAS INSTALLED IAW SRM 53-04, PAGE 218 F. 2 L 7 2 4F A6WE 1999061100335 19990611 00335 NM 1999 6 11 CALA9900634 1 19990601 A 3350 1001141 BATTERY PACK GRIMES BOEING 727 727224 1384076 NM EXTERIOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND LT AFT EXTERNAL EMERGENCY LIGHT ON AFT WING FAIRING WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALL ED IAW MM 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061100336 19990611 00336 NM 1999 6 11 CALA9900635 1 19990601 A 3350 1000677 BATTERY PACK GRIMES BOEING 727 727224 1384076 NM PAX DOORWAY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND AFT ENTRY OVERHEAD EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED I AW MM 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061100337 19990611 00337 NM 1999 6 11 CALA9900636 1 19990601 A 3350 1000677 BATTERY PACK GRIMES BOEING 727 727224 1384076 NM L1 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND L-1 DOOR UPPER EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW M M 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061100338 19990611 00338 NM 1999 6 11 CALA9900637 1 19990601 A 3350 1000679 BATTERY PACK GRIMES BOEING 727 727224 1384076 NM R2 DOORWAY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND R-2 DOOR UPPER EMERGENCY LIGHT BATTERY PACK WEAK. THE BATTERY PACK WAS RECHARGED AND REINSTALLED IAW M M 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061100339 19990611 00339 WP 1999 6 11 CALA9900638 1 19990604 A 5720 SUPPORT DOUG DC10 DC1030 3023501 WP LT & RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND LT AND RT MLG A FRAME SUPPORT BEAM BOLT HOLES CORRODED. THE SUPPORT BEAM WAS REPAIRED IAW SRM 57-20-00 , PAGE 104. 2 L 7 3 4F A22WE 1999061100340 19990611 00340 WP 1999 6 11 CALA9900639 1 19990527 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 824 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND SEAT TRACKS CORRODED AT STA 824, LT AND RT SIDES. THE SEAT TRACKS WERE REPLACED IAW MM 53-20-00. 2 L 7 3 4F A22WE 1999061100341 19990611 00341 WP 1999 6 11 CALA9900640 1 19990528 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD AFT FITTING ANGLE. THE ANGLE WAS REPLACED IAW SRM 51-3 0-00. 2 L 7 3 4F A22WE 1999061100342 19990611 00342 WP 1999 6 11 CALA9900641 1 19990528 A 5730 SKIN DOUG DC10 DC1030 3023501 WP LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE INTERNAL SKIN AT OUTBOARD LOWER CORNER. A REPAIR WAS PERFORMED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1999061100343 19990611 00343 WP 1999 6 11 CALA9900642 1 19990528 A 5522 SKIN DOUG DC10 DC1030 3023501 WP LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A .75 INCH CRACK IN LT OUTBOARD ELEVATOR TRAILING EDGE. THE TRACK SECTION TRAILING EDGE WAS REPLACED I AW SRM 55-30-00. 2 L 7 3 4F A22WE 1999061100344 19990611 00344 WP 1999 6 11 CALA9900643 1 19990528 A 5720 BEAM DOUG DC10 DC1030 3023501 WP WS 299 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 1 INCH CRACK IN RT WING TRAILING EDGE PANEL FITTING BEAM AT STA XORS 299. A REPAIR WAS PERFORMED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1999061100345 19990611 00345 WP 1999 6 11 CALA9900644 1 19990529 A 5730 SKIN DOUG DC10 DC1030 3023501 WP LT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND LT WING LOWER SKIN PANEL OF LANDING GEAR VANE DELAMINATED ON THE UPPER AND LOWER SURFACE. THE UPPER AN D LOWER SKIN WAS REPAIRED IAW SRM 51-71-00, PARAGRAPH 18B. 2 L 7 3 4F A22WE 1999061100346 19990611 00346 WP 1999 6 11 CALA9900645 1 19990601 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 402 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE OUTBOARD LOWER SKIN AT STA XORS 402. A REPAIR WAS PERFORMED IAW SRM 57-10-00, PAGE 216. 2 L 7 3 4F A22WE 1999061100347 19990611 00347 WP 1999 6 11 CALA9900646 1 19990601 A 5711 SPAR DOUG DC10 DC1030 3023501 WP WS 317 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 0.8 INCH CRACK IN RT WING DROOPED LEADING EDGE ON LATERAL SPAR AT STA XORS 317. A REPAIR WAS PERFORM ED IAW ECRA 5720-01738. 2 L 7 3 4F A22WE 1999061100348 19990611 00348 WP 1999 6 11 CALA9900647 1 19990601 A 5711 SPAR DOUG DC10 DC1030 3023501 WP WS 317 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 1.5 INCH CRACK IN RT WING DROOPED LEADING EDGE ON INTERNAL SPAR AT STA XORS 317. A REPAIR WAS PERFOR MED IAW ECRA 5720-01738. 2 L 7 3 4F A22WE 1999061100349 19990611 00349 WP 1999 6 11 CALA9900648 1 19990601 A 5730 PANEL DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A FOUR INCH CRACK IN RT WING PANEL NR 617CT. REPAIRED IAW SRM 57-10-00, PAGE 25. 2 L 7 3 4F A22WE 1999061100350 19990611 00350 WP 1999 6 11 CALA9900649 1 19990601 A 5751 SKIN DOUG DC10 DC1030 3023501 WP RT AILERON CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND RT WING OUTBOARD AILERON LOWER SKIN INTERNALLY CORRODED. THE AILERON SKIN WAS REPLACED IAW SRM 51-31-0 1 AND 51-33-01. 2 L 7 3 4F A22WE 1999061100351 19990611 00351 SO 1999 6 11 COMA9910090 1 19990604 A 2910 HYD SYST EMB 120 EMB120RT SO GREEN HYD SYST REQD SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 263CA 120255 GREEN HYDRAULIC SYSTEM LOW PRESSURE WARNING DURING GEAR RETRACTION. SERVICED HYDRAULIC RESERVOIR TO PROPER LEVEL. 2 L 7 2 4T RT A31SO 1999061100352 19990611 00352 SO 1999 6 11 COMA9910091 1 19990604 A 7332 1103P1892 PRESSURE SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 258CA 6777 120247 LEFT ENGINE LOW FUEL PRESSURE WARNING. REPLACED PRESSURE SWITCH. 2 L 7 2 4T 4 T RT A31SO E20NE 1999061100353 19990611 00353 NE 1999 6 11 COMA9960250 2 19990605 A 7260 M832481241 O RING CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE CUT A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 962CA 7123 RIGHT HAND ENGINE LOW OIL PRESSURE WARNING. REPLACED THE ENGINE DRIVER HYDRAULIC PUMP DRIVE PAD O-RING. 2 L 7 2 4F 4 F RT A21EA E15NE 1999061100354 19990611 00354 EA 1999 6 11 COMA9960251 1 19990606 A 3230 555405 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 924CA 5536 7026 GEAR DISAGREE MESSAGE, NLG DID NOT RETRACT. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 1999061100355 19990611 00355 NM 1999 6 11 UPS99429771 1 19990605 A 5310 STRUCTURE BOEING 747 747SR46 NM BS 2160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE:N/A, 1 FT X 2 FT AREA OF CORROSION FOUND AT STATION 2160. *S/D* REMOVED CORRODED SKIN AND STRINGER DOU BLER. INSTALLED AND TREATED DOUBLER IAW SRM 53-30-03. 2 L 7 4 4F A20WE 1999061100356 19990611 00356 WP 1999 6 11 UPS99829725 1 19990517 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 480 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C1, MAIN CABIN FRAME STA 480 L10R HAS HOLE FABBED REPAIR ANGLE IAW REO-06496. FABBED FILLER IAW REO -06496, ALODINED AND PRIMED REPAIR ANGLE AND FILLER IAW DC8 SRM 51-1-8, INSTALLED REPAIR WITH HI-LOKS IAW DC8 SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 1999061100357 19990611 00357 WP 1999 6 11 ABXA990388 1 19990529 A 5320 995823869N SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT LONGERON 14 LEFT AND STATION 1056. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999061100358 19990611 00358 WP 1999 6 11 ABXA9900389 1 19990529 A 5313 592480215 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 294, 275, 256 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 294, 275 AND 256. REPAIRED LONGERON 17 LEFT IAW DC9 SRM 53-02 . 2 L 7 2 4F A6WE 1999061100359 19990611 00359 WP 1999 6 11 ABXA9900390 1 19990529 A 5320 99577397 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 1021, BETWEEN LONGERONS 15 AND 16 RIGHT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061100360 19990611 00360 WP 1999 6 11 ABXA9900391 1 19990529 A 5280 39259761 HINGE DOUG DOUG DC9 DC941 302207N WP LT MLG DOORS CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND LEFT MAIN LANDING GEAR INBOARD DOOR HINGE LOBES CRACKED AT AFT END. REPLACED HINGE IAW DC9 SRM 51 -30-1. 2 L 7 2 4F A6WE 1999061100361 19990611 00361 WP 1999 6 11 ABXA9900392 1 19990529 A 5280 39259762 HINGE DOUG DOUG DC9 DC941 302207N WP RT MLG DOORS CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND RIGHT MAIN GEAR INBOARD DOOR HINGE LOBES CRACKED AT AFT END. REPLACED HINGE IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999061100362 19990611 00362 WP 1999 6 11 ABXA990393 1 19990419 A 5720 991009177 SPLICE DOUG DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND RIGHT WING LOWER SPAR CAP SPLICE CORRODED. REPLACED SPLICE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999061100363 19990611 00363 WP 1999 6 11 ABXA9900394 1 19990419 A 5720 99193984AX FITTING DOUG DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND SLAT ACTUATOR ASSEMBLY INBOARD MOUNT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999061100364 19990611 00364 WP 1999 6 11 ABXA9900395 1 19990414 A 5755 3923258504 SUPPORT DOUG DOUG DC9 DC941 302207N WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND OUTBOARD SPOILER TORQUE TUBE CENTER SUPPORT CRACKED. REPLACED TORQUE SUPPORT IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999061100365 19990611 00365 WP 1999 6 11 ABXA990396 1 19990506 A 5311 99234051 FRAME DOUG DOUG DC9 DC941 302207N WP BS 655 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND FRAME AT STATION 655 CRACKED. REPLACED FRAME IAW DC9 SRM 51-30-2 AND DACO DWG NR 9923410. 2 L 7 2 4F A6WE 1999061100366 19990611 00366 WP 1999 6 11 ABXA9900397 1 19990506 A 5320 4911383504 FITTING DOUG DOUG DC9 DC941 302207N WP BS 984 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND FRAME FITTING AT STATION 984 CORRODED. REPLACED FRAME FITTING IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1999061100367 19990611 00367 NM 1999 6 11 MWEA99319 1 19990603 A 2560 D29982107 SLIDE DOUG MD88 MD88 3023688 NM PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF. MTC REINSTALLED FORWARD ENTRANCE DOOR SLIDE. 2 L 7 2 4F RT A6WE 1999061100368 19990611 00368 NM 1999 6 11 DLM88991236 1 19990602 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 966DL 53115 ON TAXI OUT IN CVG, FWD LAV SMOKE DETECTOR CAME ON AND AN ODOR WAS DETECTED IN THE FORWARD PORTION OF THE CABIN. ALS O, PASSENGERS REPORTED SMELLING SMOKE. PERFORMED DUCT BURNOUT, REPLACED COALESCERS. 2 L 7 2 4F RT A6WE 1999061100369 19990611 00369 NM 1999 6 11 DL76L991237 1 19990602 A 2121 FAN 6066223 BOEING 767 767332 1382001 NM LEFT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 185DN 1041826 27961 LEFT RECIRCULATION FAN KICKED OFF AT TOP OF DESCENT. DID NOT RESET. REPLACED RECIRC FAN. 2 L 7 2 4F RT A1NM 1999061100370 19990611 00370 NM 1999 6 11 DL72S991243 1 19990603 A 5720 651852213 CHORD BOEING 727 727232 1384082 NM BS 760 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 INSPECTIONS PER 4-58560-12AD, FOUND 4 FASTENER HOLES WITH TOOLING DAMAGE. NO CRACK INDICATIONS WERE NOTED. REPAIRED PE R ERA 333191-14AD, REV A. 2 L 7 3 4F A3WE 1999061100371 19990611 00371 NM 1999 6 11 DLM88991244 1 19990603 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DE 49967 FS 1418 FRAME WAS CRACKED IN TYP LOCATIONS AT L2L AND L2R. REPAIRED PER ERA 333212-14. 2 L 7 2 4F RT A6WE 1999061100372 19990611 00372 NM 1999 6 11 DL76G991245 1 19990603 A 3350 BATTERIES BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 155DL 25269 LT SIDE CABIN EMERGENCY PATH LIGHTS WOULD NOT EXTINGUISH. REPLACED BATTERY RACK ASSY AND BATTERIES FOR FWD LEFT. 2 L 7 2 4F RT A1NM 1999061100373 19990611 00373 NM 1999 6 11 DL76L991246 1 19990602 A 3350 LIGHT BOEING 767 767332 1382001 NM ROW 6FG INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 174DN 24802 EMERGENCY TRACK LIGHTS INOP AT SEATS 6 F/G THRU 20 F/G. REPLACED SHORTED LIGHT ASSY AT SEAT 11G AND REPLACED FUSE IN PO WER SUPLY M9011. EMERGENCY LIGHTS CK GOOD. 2 L 7 2 4F RT A1NM 1999061100374 19990611 00374 NM 1999 6 11 DL76L991247 1 19990602 A 2730 2827001011 ACTUATOR 2827001011 BOEING 767 767332 1382001 NM LT ELEVATOR DAMAGED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 173DN 2020 24800 EICAS C HYD QTY MSG AND CENTER HYD QTY .45. TURNED CENTER ELEC PUMPS OFF, LEAK CONTINUED. TURNED CENTER DEMAND PUMP OF F. FLUID SLOWLY DECREASED .01 PER 20 MINS. FOUND HYD LEAK FROM LEFT ELEVATOR CENTER PCA. TEFLON SEAL CRACKED FROM ROD . REPLACED PCA PER MM 27-31-05-4, LEAK CHECK PERFORMED, NO LEAK 2 L 7 2 4F RT A1NM 1999061100375 19990611 00375 NM 1999 6 11 DL72S991248 1 19990603 A 5753 SKIN BOEING 727 727232 1384082 NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 545DA 22494 NR 2 MID FLAP COVE LWR COVE SKIN CRACKED ABOVE AFT FLAP I/B ROD. REPAIRED PER MM 57-20-0 FIG 809. 2 L 7 3 4F A3WE 1999061100376 19990611 00376 NM 1999 6 11 DL72S991249 1 19990603 A 3350 BATTERIES 900835A BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 21077 LEFT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS NORMAL. 2 L 7 3 4F A3WE 1999061100377 19990611 00377 NM 1999 6 11 DLM88991250 1 19990603 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 130 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 FUSELAGE SKIN AT STA 130L FOR THE HOLD OPEN PIN SURROUND SKIN DAMAGE BY THE JETWAY. ALSO, L-1 DOOR IS DAMAGED. REPAIRE D SKIN PER SRM 53-04 FIG 24. REPLACED THE L-1 DOOR PER M/M. 2 L 7 2 4F RT A6WE 1999061100378 19990611 00378 NM 1999 6 11 DL72L991253 1 19990518 A 2497 BMS1331 WIRE BOEING 727 727232 1384082 NM NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 ON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL CRACKS ON INSULATION IN ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS13-58 DL (P/N 012210733) PER BOEING SER VICE LETTER 727-SL24026A. 2 L 7 3 4F A3WE 1999061100379 19990611 00379 NM 1999 6 11 DL72L991255 1 19990604 A 2150 CONNECTOR BACC45FT147 BOEING 727 727232 1384082 NM LT PACK FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 501DA 21303 AT 31,000 FT CABIN ALT STILL CLIMBED AT 500 FT MIN. DESCENDED TO 18,000 FT, CABIN ALT LEVELED OFF ATL 9500 FT. BOTH PA CKS APPEARED TO WORK. NO OTHER INDICATIONS TO SHOW LEAK. REPLACED LT PACK VALVE CONNECTOR. LT PACK OPS NORMAL, A/ C PRESS NORMAL. 2 L 7 3 4F A3WE 1999061100380 19990611 00380 NM 1999 6 11 DL76G991256 1 19990604 A 3320 0581416 BALLAST 0581416 BOEING 767 767332 1382001 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 176DZ 29697 BURNING RUBBER ODOR REPORTED IN CABIN BY PASSENGER. RAN PACKS AND INSPECTED AREA, PRESSURIZED AC AND INSP B-BIN AREA, P ULLED DOWN CEILING PANELS AND ALL CKS OK. REPLACED 4 LIGHT BALLAST AS PRECAUTION, ALL CKS OK. 2 L 7 2 4F RT A1NM 1999061100381 19990611 00381 NM 1999 6 11 DL76L991257 1 19990604 A 3350 BULB 767 BOEING 767 767332 1382001 NM EXTERIOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 198DN 28455 EXTERIOR EMERGENCY LIGHT, FIRST LIGHT AFT OF WING INOP. RELAMPED, OPS CK GOOD. 2 L 7 2 4F RT A1NM 1999061100382 19990611 00382 NM 1999 6 11 DL73K991260 1 19990604 A 2170 COALESCER BOEING 737 737232 1384475 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 322DL 23094 DIVERSION DUE TO SMOKE IN CABIN. PERFORMED LT AND RT ENG AND APU BLD COMPRESSION CONT SYS TEST WITH OPERATIONAL LT PACK ONLY. CKS GOOD. REPLACED LT PACK COALESER BAG PER MM. PERFORMED VIS INSPECTION OF BOTH AC BAYS, ALL NORMAL. 2 L 7 2 4F RT A16WE 1999061100383 19990611 00383 NM 1999 6 11 DL72W991261 1 19990604 A 5754 SKIN BOEING 727 727247 138408F NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 A 1.125 INCH VISABLE CRACK ON AFT SKIN OF NR 6 SLAT AT O/B TRAILING EDGE. SPLICED SKIN PER M/M 57-54-0, NR 1. 2 L 7 3 4F A3WE 1999061100384 19990611 00384 NM 1999 6 11 DLM90991262 1 19990604 A 3350 8039491 BATTERY PACK DOUG MD90 MD9030 3023690 NM R1 DOORWAY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 903DA 53383 R1 DOOR EMERGENCY EXIT LIGHTS VERY DIM. REPLACED BATT PACK, OPS NOW OK. 2 L 7 2 4F RT A6WE 1999061100385 19990611 00385 1999 6 11 DL76L991263 4 19990604 A 2330 1301281012 ENTERTAIN SYS BOEING 767 767332 1382001 NM ROW 2CE FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 184DN 27111 IN FLIGHT, STRONG ELECTRICAL BURNING SMELL AND SLIGHT HAZE IN BUSINESS ELITE AREA HAD STRONG SMELL, DEPOWERED ENTERTAIN MENT SYSTEM, SMELL WENT AWAY SLIGHTLY. REPOWERED SYSTEM AND SMELL RETURNED STRONG. SHUT SYSTEM DOWN WITH VCC/ADB SWITC HES, NO EFFECT. MAINTENANCE GAVE C/B'S TO PULL IN E AND E COMPT, SMELL AND HAZE DISSIPATED SLOWLY WITH SLIGHT SMELL LIN GERING OVER 1C AND 2C. SUSPECT COMING OUT OF CENTER CEILING, FWD OF PROJECTOR. E AND E COMPARTMENT HAD NO SMELL OR HAZ E WHEN OPENED. TWO HOURS AFTER C/B'S SHUTDOWN, SMELL COMPLETELY GONE. REPLACED AVU AND CABLES AT SEAT 2CE. 2 L 7 2 4F RT A1NM 1999061100386 19990611 00386 NM 1999 6 11 DL733991265 1 19990605 A 2611 SMOKE DETECTOR 7213000100 BOEING 737 737347 1384647 NM LAVATORY FAILED A DALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 27 306WA 2992 23347 LAV SMOKE FALSE ALARM. ACTIVATED TWICE IN FLIGHT. CIRCUIT BREAKER PULLED TO SILENCE ALARM. REPLACED FWD SMOKE DETECTO R. 2 L 7 2 4F RT A16WE 1999061100387 19990611 00387 NM 1999 6 11 DL757991266 1 19990605 A 3260 387 BULB BOEING 757 757232 1384965 NM COCKPIT FAILED A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 641DL 23995 WHEN GEAR EXTENDED LEFT MAIN DID NOT GO GREEN. ALTERNATE GEAR EXTENSION PER POM, NO HELP. RELAMPED INDICATOR. 2 L 7 2 4F RT A2NM 1999061100388 19990611 00388 NM 1999 6 11 DLM88991267 1 19990602 A 3350 CONNECTOR DOUG MD88 MD88 3023688 NM ROW 29DE DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 905DE 53410 SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 29 D/E INOP. RECONNECTED TERMINAL AT FLOOR LIGHT, CKS GOOD. 2 L 7 2 4F RT A6WE 1999061100389 19990611 00389 NM 1999 6 11 DL72K991269 1 19990606 A 7930 BY PASS SWITCH BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 480DA 20860 700701 WHILE FL300, PWR 2.06 EPR ON NR 2 ENG. THE FILTER BY-PASS LIGHT CAME ON DIM. ONCE THROTTLE RETARDED TO IDLE, LT REMAIN ED ON. SHUTDOWN IAW V LIST. ALL OTHER INDICATIONS NORMAL. ENG WINDMILLED FOR 15 MIN. CHECKED MAIN OIL FILTER, FOUND OK. CHECKED CHIP DETECTOR, FOUND OK. REPLACED FILTER ASSY, RUN-UP, LEAK CHECK FOUND OK. PLACARD PER MEL 79-00-02. BY -PASS FILTER LIGHT. 2 L 7 3 4F 4 F A3WE E2EA 1999061100390 19990611 00390 NM 1999 6 11 DLM11991270 1 19990604 A 3350 BATTERY 5519881 DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 803DE 48474 ON S/C, EMERGENCY LIGHTS TEST BATTERY 3 AND 4 LOW MESSAGE ILLUMINATED. REPLACED NR 3 AND NR 4 BATTERIES, EMERGENCY LIGH T TEST PASS. 2 L 7 3 4F RT A22WE 1999061100391 19990611 00391 NM 1999 6 11 DLM88991271 1 19990606 A 3397 0201720001 WIRE DOUG MD88 MD88 3023688 NM ROW 3CD BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 976DL 53257 SEAT 3CD EMERGENCY TRACK LIGHT INOP. REPLACED LIGHT. 2 L 7 2 4F RT A6WE 1999061100392 19990611 00392 1999 6 11 DL733991272 4 19990606 A 3417 CONNECTOR BOEING 737 7373B7 1384580 NM E & E COMPT LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 952WP 23378 AFTER LIFTOFF AIRSPEED INDICATOR ERRACTIC ALONG WITH ALTIMETER, FIRST OFFICERS SIDE. FOUND PIN 38 PUSHED BACK AT NR 2 ADC RACK CONNECTOR D311A. RESEATED PIN, FLAGS DISAPPEARED. NR 2 ADC FUNCTION TEST VALID. FMCS SENSOR DIS CRETE FOR NR 2 ADC OK. 2 L 7 2 4F RT A16WE 1999061100393 19990611 00393 NM 1999 6 11 DLM11991273 1 19990606 A 2910 CONTROLLER 4059021903 DOUG MD11 MD11 3023602 NM HYD SYST FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 812DE 92070335 48601 ENG HYD PUMP CONTROL RIGHT POPPED 45 MIN AFTER T/O. UNABLE TO CONTROL R HYD PUMPS IN MANUAL OR AUTO. RETURNED TO ATL. REPLACED HYD SYS CONTROLLER. 2 L 7 3 4F RT A22WE 1999061100394 19990611 00394 NE 1999 6 11 DLM88991275 2 19990606 A 7311 FUEL/OIL COOLER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 927DA 21039 49714 726053 ENG FAILURE RT ON DEPARTURE AT 17K, RT ENG FLUX FOR APPROX 15 SEC BEFORE FAILURE. F/A REPORTED POPPING NOISES PRIOR TO FLUX OIL TEMP WENT TO 155 DEG. CHECKED INLET AND EXH, NO TROUBLE FOUND. CHECKED OIL FILTER AND REPLACED SAME. FILTER CLEAN, CHECKED CHIP DET, NO METAL. BORESCOPED 6TH, 7TH AND 13TH STAGE COMPRESSOR, NO DAMAGE FOUND. REPLACED FUEL CONTR OL AND FUEL PUMP. PERFORMED OPN5034 HIGH OIL TEMP TEST, ENG PASSED. TRIMMED ENG PER PFHB, NR 2 ENG FUEL/OIL COOLER LEA KING AT WEEP HOLE. REPLACED NR 2 ENG FUEL/OIL COOLER AND OIL TEMP BULB. LK AND OPN CKS NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 1999061100395 19990611 00395 1999 6 11 SWAA990963 4 19990604 A 3417 D4349J CONNECTOR BOEING 737 7373G7 1384595 NM NR 2 ADC LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 691WN 23781 AIR TURNBACK--- UPON TAKE OFF, F/O'S AIR SPEED, ALTIMETER INDICATORS AND TRANSPONDER INSTRUMENTS BECAME INOP. FOUND Q UICK DISCONNECT ON NR 2 ADC LOOSE. SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 1999061100396 19990611 00396 NM 1999 6 11 SWAA990964 1 19990604 A 3350 300432 COVER BOEING 737 7372T4 1384492 NM ROW 19 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 EMERGENCY EGRESS LIGHT TRACK COVER LOOSE AT ROW 19. SECURED COVER PER MM. 2 L 7 2 4F A16WE 1999061100397 19990611 00397 NM 1999 6 11 SWAA990965 1 19990605 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 AFT SERVICE DOOR EVACUATION SLIDE ASSY NOT SECURED TO DOOR. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999061100398 19990611 00398 NM 1999 6 11 SWAA990966 1 19990605 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM PAX DOORWAY BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999061100399 19990611 00399 NM 1999 6 11 SWAA990967 1 19990606 A 3411 0856AE19 PITOT TUBE BOEING 737 7373T5 NM FWD FUSELAGE BIRD STRIKE A SWAA K NONE C F.O.D. IN INSP/MAINT 1 SW 07 694SW 23061 AIR TURNBACK---- DURING TAKEOFF, A MOMENTARY STALL WARNING INDICATED FOLLOWED BY 50 KNOTS DIFFERENCE IN AIR SPEED INDICA TION. DISCOVERED BIRD STRIKE DEBRIS AT RT PITOT TUBE. REMOVED AND REPLACED RT PITOT TUBE ASSY, NO OTHER DAMAGES FOUND. 2 L 7 2 4F RT A16WE 1999061100400 19990611 00400 NM 1999 6 11 SWAA990968 1 19990604 A 3350 20132012 BATTERY PACKS BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND AFT LT AND RT DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 1999061100401 19990611 00401 NM 1999 6 11 SWAA990969 1 19990604 A 5754 6573714 SKIN BOEING 737 7373A4 1384585 NM NR 5 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C1 CHECK, FOUND NR 5 LE SLAT HAS 7 CRACKS AT LOWER SKIN AFT RIVET ROW. REPAIRED SLAT PER SWA RA NR 1-3 57-0312. 2 L 7 2 4F RT A16WE 1999061100402 19990611 00402 NM 1999 6 11 SWAA990970 1 19990605 A 3350 101114 LENS BOEING 737 7373Q8 1384670 NM SERVICE DOORWAY BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED TRANSITION CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS P ER MM. 2 L 7 2 4F RT A16WE 1999061100403 19990611 00403 NM 1999 6 11 SWAA990971 1 19990606 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM ROW 19 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EGRESS LIGHT INOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999061100404 19990611 00404 NM 1999 6 11 SWAA990972 1 19990606 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND 2 BELTFRAMES CRACKED AT BS 616 LT AND RT, WL 208. REPAIRED FRAMES PER SWA TR NR T1-A 53-026. 2 L 7 2 4F RT A16WE 1999061100405 19990611 00405 EU 1999 6 11 MALA976495 1 19990606 A 3620 M835366022L RELAY SAAB SF340 340B 7860101 EU E & E COMPT FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 434XJ 434 AFTER TAKEOFF, THE LEFT BLEED AIR LEAK LIGHT ILLUMINATED. THE RIGHT BLEED WAS DEFERRED, AIRCRAFT RETURNED TO DTW. MAIN TENANCE REPLACED RELAY 16HD. GROUND RAN ENGINE, PERFORMED OP'S CHECK OF RIGHT BLEED AIR SYSTEM, ALL SYSTEMS CHECK GOOD. NO FAULTS OR ABNORMALITIES NOTED. 2 L 7 2 4T RT A52EU 1999061100406 19990611 00406 EU 1999 6 11 MALA976496 1 19990607 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A MALA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 GL 15 428XJ 428 CARGO SMOKE LIGHT ILLUMINATED, BLEW THE CARGO EXTINGUISHER ONE, AS PER QRH. MAINTENANCE REPLACED FIRE BOTTLE AFT RT NR 1 AND NR 2 OH CARGO DETECTOR. OPS CHECK GOOD OF SMOKE DETECT SYSTEM. 2 L 7 2 4T RT A52EU 1999061100407 19990611 00407 EU 1999 6 11 MALA976497 1 19990607 A 3320 65111 BALLAST SAAB SF340 340B 7860101 EU LAVATORY SMOKED A MALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 15 418XJ 418 LAV SMOKE LIGHT COMES ON INTERMITENTLY AND THEN GOES OUT. MAINTENANCE REPLACED BALLAST, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999061100408 19990611 00408 EU 1999 6 11 MALA976498 1 19990606 A 3260 049410001 CONTROL UNIT SAAB SF340 SF340A 7850100 EU LANDING GEAR MALFUNCTIONED A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 119XJ 119 ON APPROACH TO ROA, PUT GEAR HANDLE DOWN, NOSE GEAR LIGHTS DIDN'T COME ON. CYCLED GEAR TWICE, SAME RESULT. THIRS TIME OF CYCLING GEAR, NOSE GEAR LIGHTS ILLUMINATED. ALL HYD NORMAL. MAINTENANCE REPLACED LANDING GEAR CONTROL UNIT AND INDI CATOR. ALL INDICATIONS CHECKS ARE GOOD, NO OTHER DEFECTS NOTED. ALL OTHER SYSTEMS OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999061100409 19990611 00409 NM 1999 6 11 PCAA9900015 1 19990605 A 3260 RELAY DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER N FALSE WARNING DE DESCENT 1 EA 13 819EX 016 LGA-FLT 3881, UPON LANDING GEAR EXTENSION THE GEAR INOP CAUTION LIGHT ILLUMINATED. AIRCRAFT LANDED SAFELY. MAINTENANCE TROUBLESHOT SYSTEM, REPLACED RELAYS 3261-K5, K6, AND K7. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999061100410 19990611 00410 NE 1999 6 11 PCAA9900016 2 19990606 A 7530 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE FAILED A PCAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 13 812EX 312 120538 SYR-FLT 3863, UPON APPROACH AS POWER REDUCED TO IDLE, THE COCKPIT STARTED TO FILL WITH SMOKE. CREW DONNED O2 MASKS, DEC LARED EMERGENCY AND LANDED SAFELY. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE AIR SWITCHING VALVE AT FAULT. REMOV ED, CLEANED AND REINSTALLED VALVE. GROUND ENGINE RUN PROVED SATISFACTORY. 2 H 7 2 4T 4 T RT A13NM E20NE 1999061100411 19990611 00411 NM 1999 6 11 CALA9900650 1 19990604 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 986-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 986 TO 1006, WL 208, LT SIDE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999061100412 19990611 00412 NM 1999 6 11 CALA9900651 1 19990605 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND MAIN CABIN FLOORBEAM CAP CORRODED AT STA 1130 FROM RBL 25-45. THE FLOORBEAM CAP WAS REMOVED AND REPLAC ED IAW ECRA 5310-03861. 2 L 7 3 4F A3WE 1999061100413 19990611 00413 NM 1999 6 11 CALA9900652 1 19990605 A 5330 SKIN BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND FUSELAGE SKIN CORRODED AROUND BELLY DRAIN AT STA 950E BETWEEN STRINGER 29R TO 30. A REPAIR WAS INSTALL ED IAW ECRA 5330-02822. 2 L 7 3 4F A3WE 1999061100414 19990611 00414 NM 1999 6 11 CALA9900653 1 19990605 A 5314 KEEL BEAM BOEING 727 727224 1384076 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND A 4 INCH CRACK IN KEEL BEAM CHORD AT STA 950E, STRINGER 29R. A REPAIR WAS INSTALLED IAW ECRA 5310-0386 2. 2 L 7 3 4F A3WE 1999061100415 19990611 00415 WP 1999 6 11 CALA9900654 1 19990605 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 427-446 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND RT FUSELAGE SKIN DENTED IN SEVERAL PLACES FROM STA 427 TO 446 BETWEEN LONGERONS 21R TO 25R. THE DENTED AREAS WERE CUT OUT, NEW SKIN AND LONGERON SPLICES WERE INSTALLED IAW DOUGLAS DRAWING SR 09530004. 2 L 7 2 4F A6WE 1999061100416 19990611 00416 NM 1999 6 11 CALA9900655 1 19990607 A 5313 STRINGER BOEING 757 757224 1384958 NM BS 1610-1640 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57111 27301 INSPECTION FOUND A CRACK IN STRINGER 22L AT STA 1610-1640. A STRINGER SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03 AND ECRA 5331-01055. 2 L 7 2 4F RT A2NM 1999061100417 19990611 00417 NM 1999 6 11 CALA9900656 1 19990608 A 3350 D71702001 POWER PACK PAGEAEROSPAC BOEING 727 727224 1384076 NM RT EMER EXIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 88712 19803 INSPECTION FOUND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE POWER PACK ASSEMBLY WAS REPLACED AND OPERAT ION CHECKED GOOD. 2 L 7 3 4F A3WE 1999061100418 19990611 00418 SO 1999 6 11 COMA9910092 1 19990606 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 261CA 120254 EXIT SIGN AT ROW 5 IS INOP. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999061100419 19990611 00419 EA 1999 6 11 COMA9960252 1 19990607 A 3411 PITOT TUBE CNDAIR CL600 CL6002B19 EA RIGHT FOD A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 938CA 7046 EFIS COMP MON WARNING - COPILOTS AIRSPEED 20 KTS LOW. REMOVED DEAD BUG FROM RIGHT HAND PITOT TUBE. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1999061100420 19990611 00420 NM 1999 6 11 QXEA9901082 1 19990601 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTIONED A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 369PH 1023 411 520 PDX- SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. NO SMOKE NOTED. MAINTENANCE REPLACED BOTH SMOKE DETECTORS, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999061100421 19990611 00421 EU 1999 6 11 QXEA9901083 1 19990604 A 3350 606008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 481US 1155 11230 PDX- OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN WERE INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999061100422 19990611 00422 NM 1999 6 11 99FDEA00206 1 19990607 A 5311 651766452 FRAME BOEING 727 727247 138408F NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 THREE DENTS ON TOP FLANGE OF FRAME AT BS 660 BETWEEN STRS 23 AND 26R. *S/D* REMOVED DAMAGE FROM INNER FLANGE, FABRICAT ED AND INSTALLED REPAIR PARTS IAW FEDEX EA 7-5310-45287 AND SRM 51-40-2. 2 L 7 3 4F A3WE 1999061100423 19990611 00423 WP 1999 6 11 ABXA9900398 1 19990419 A 2760 3923259501 SUPPORT DOUG DOUG DC9 DC941 302207N WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LEFT WING INBOARD SPOILER TORQUE TUBE SUPPORT FITTING CRACKED. REPLACED SUPPORT FITTING IAW DC9 S RM 51-30-1. 2 L 7 2 4F A6WE 1999061100424 19990611 00424 WP 1999 6 11 ABXA9900399 1 19990414 A 5720 59113581 SPLICE DOUG DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LEFT WING UPPER SPAR CAP SPLICE CORRODED LEVEL 2 CORROSION. REPLACED T-ANGLE IAW DC9 SRM 51-10-4 AND DACO DWG NR 9910010. 2 L 7 2 4F A6WE 1999061100425 19990611 00425 WP 1999 6 11 ABXA9900400 1 19990419 A 2760 3923255504 SUPPORT DOUG DOUG DC9 DC941 302207N WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND RIGHT WING INBOARD SPOILER TORQUE TUBE CENTER SUPPORT FITTING CRACKED. REPLACED SUPPORT FITTING I AW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999061100426 19990611 00426 WP 1999 6 11 ABXA9900401 1 19990419 A 5313 591140617 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LONGERON 4 LEFT CRACKED AT STATION 160. REPLACED LONGERON 4 LEFT IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061100427 19990611 00427 WP 1999 6 11 ABXA9900402 1 19990419 A 2760 3923257501 SUPPORT DOUG DOUG DC9 DC941 302207N WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND RIGHT WING INBOARD SPOILER TORQUE TUBE SUPPORT FITTING CRACKED. REPLACED SUPPORT FITTING IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1999061100428 19990611 00428 WP 1999 6 11 ABXA9900403 1 19990607 A 5313 59197075 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C-CHECK, FOUND LONGERON 26 LEFT CRACKED AT STATION 945. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061100429 19990611 00429 WP 1999 6 11 ABXA9900404 1 19990604 A 3350 60030431 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 987AX 47364 DURING SERVICE CHECK, EMERGENCY LIGHTS REMAINED ILLUMINATED WHEN ALL POWER WAS REMOVED FROM AIRCRAFT. REPLACED EMERGENC Y LIGHTS POWER SUPPLY BATTERIES IAW DC9 MM, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999061100430 19990611 00430 WP 1999 6 11 ABXA9900405 1 19990506 A 5311 99118594 FRAME DOUG DOUG DC9 DC941 302207N WP BS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND FRAME AT STATION 1180 CRACKED AT LONGERON 14 RIGHT. REPLACED FRAME IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061100431 19990611 00431 WP 1999 6 11 ABXA9900406 1 19990506 A 5320 991184192 CLIP DOUG DOUG DC9 DC941 302207N WP BS 1165 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND FORMER CORRODED AND CRACKED AT CANTED FRAME 1165. REPLACED SHEAR CLIP IAW DC9 SRM 51-10-2. 2 L 7 2 4F A6WE 1999061100432 19990611 00432 WP 1999 6 11 ABXA9900407 1 19990506 A 5313 7910781507 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 427 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 427. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999061100433 19990611 00433 WP 1999 6 11 ABXA9900408 1 19990506 A 2760 3923258501 SUPPORT DOUG DOUG DC9 DC941 302207N WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LEFT WING OUTBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING CRACKED. REPLACED TORSION BAR FITTI NG IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999061100434 19990611 00434 WP 1999 6 11 ABXA9900409 1 19990507 A 5320 99236685 SUBFLOOR DOUG DOUG DC9 DC941 302207N WP BS 154 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND COCKPIT SUBFLOOR CRACKED AT STATION 154 AND RBL 6. REPAIRED IAW ABX REA D953-28407. 2 L 7 2 4F A6WE 1999061100435 19990611 00435 WP 1999 6 11 ABXA9900410 1 19990607 A 5610 5613217508 WINDOW DOUG DC9 DC941 302207N WP RT COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 FIRST OFFICER'S CLEARVIEW WINDOW (EMERGENCY EXIT) WOULD NOT OPEN DURING PREFLIGHT. LOCKING MECHANISM WAS STUCK. UNSTUC K, CLEANED AND LUBRICATED LOCKING MECHANISM GUIDE PIN, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999061100436 19990611 00436 NM 1999 6 11 MWEA99325 1 19990607 A 2560 D29985107 SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOOR OUT OF ADJUST A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE AFT GALLEY DOOR SLIDE COVER CATCHES ON DOOR OPENING. MTC REPOSITIONED SLIDE COVER. 2 L 7 2 4F RT A6WE 1999061100437 19990611 00437 NM 1999 6 11 SCNA99709 1 19990603 A 3350 LIGHT BOEING 727 727225 1384077 NM RT EMER EXIT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE CHECK, THE NO SMOKING SWITCH POPS THE DIM EMERGENCY LIGHT CIRCUIT BREAKER. REPLACED RIGHT HAND AFT OVERWING EMERGENCY LIGHT, OPERATIONS CHECK GOOD IAW B727 MM 335002. 2 L 7 3 4F A3WE 1999061100438 19990611 00438 NM 1999 6 11 P5CA9900602 1 19990602 A 5730 PANEL BOEING 747 747283B 1384867 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEFT WING LOWER SURFACE TRAILING EDGE PANEL BELOW NR 3 SPOILER HAS DELAMINATION. FIBERGLASS REPAIR IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1999061100439 19990611 00439 NM 1999 6 11 P5CA9900603 1 19990602 A 5512 SKIN BOEING 747 747283B 1384867 NM LT HORIZ STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEFT HAND HORIZONTAL STABILIZER LEADING EDGE IS DENTED IN 2 PLACES. DENTED AREAS REPAIRED IAW SRM 51-40-01. 2 L 7 4 4F A20WE 1999061100440 19990611 00440 NM 1999 6 11 P5CA9900604 1 19990602 A 5311 FRAME BOEING 747 747283B 1384867 NM BS 440 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 FOUND CRACK AT UPPER CHORD FRAME STA 440 RIGHT SIDE BETWEEN STR 13 AND 14. FABRICATED CHORD IAW SRM 53-10-20 FIG 31 AND INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999061100441 19990611 00441 NM 1999 6 11 P5CA9900605 1 19990602 A 5753 SKIN BOEING 747 747283B 1384867 NM LT TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEFT INBOARD LOWER FLAP LOWER SURFACE FOUND DELAMINATED. FIBERGLASS REPAIR IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1999061100442 19990611 00442 NM 1999 6 11 P5CA9900606 1 19990602 A 5755 SKIN BOEING 747 747283B 1384867 NM NR 5 SPOILER DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 FOUND LEFT WING NR 5 SPOILER UPPER SURFACE DAMAGED. BONDED NEW SKIN AND DOUBLER PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999061100443 19990611 00443 NM 1999 6 11 P5CA9900607 1 19990602 A 5755 SKIN BOEING 747 747283B 1384867 NM NR 8 SPOILER BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 RIGHT WING NR 8 SPOILER LEADING HAS BROKEN PIECE. FIBERGLASS REPAIR IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1999061100444 19990611 00444 NM 1999 6 11 P5CA9900608 1 19990603 A 5230 HINGE BOEING 747 747283B 1384867 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEVEL 1 CORROSION FOUND AFT CARGO DOOR HINGE. AREA CLEANED PER SRM 51-10-01 AND TREATED. 2 L 7 4 4F A20WE 1999061100445 19990611 00445 NM 1999 6 11 P5CA9900609 1 19990603 A 5230 HINGE BOEING 747 747283B 1384867 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEVEL 1 CORROSION FOUND ON FWD CARGO DOOR HINGES. AREA CLEANED AND TREATED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1999061100446 19990611 00446 NM 1999 6 11 P5CA9900610 1 19990603 A 5753 SKIN BOEING 747 747283B 1384867 NM RT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 RIGHT WING RIGHT HAND AFT FLAP UPPER SURFACE O/B SIDE IS BROKEN. FIBERGLASS REPAIR IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1999061100447 19990611 00447 NM 1999 6 11 P5CA9900611 1 19990603 A 5350 FAIRING BOEING 747 747283B 1384867 NM RT WING/BODY BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 RIGHT WING AFT WING TO BODY FAIRING NEAR INBOARD FLAP IS BROKEN. FIBERGLASS REPAIR IAW SRM 51-10-09. 2 L 7 4 4F A20WE 1999061100448 19990611 00448 NM 1999 6 11 P5CA9900612 1 19990603 A 5753 SKIN BOEING 747 747283B 1384867 NM RT TE MIDFLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 RIGHT HAND OUTBOARD MID FLAP UPPER SURFACE INBOARD HAS DAMAGE. FIBERGLASS REPAIR PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999061100449 19990611 00449 NM 1999 6 11 P5CA9900613 1 19990603 A 5350 FAIRING BOEING 747 747283B 1384867 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 FUSELAGE LOWER SIDE LEFT SIDE AIR CONDITIONING FAIRING PANEL NR 192 HAS DELAMINATION. FIBERGLASS REPAIR PER SRM 51-40-0 9. 2 L 7 4 4F A20WE 1999061100450 19990611 00450 NM 1999 6 11 P5CA9900614 1 19990603 A 5320 CLIP BOEING 747 747283B 1384867 NM BS 300-340 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 FOUND CRACKS ON VERTICAL BEAM CLIPS NOSE WHEEL WELL STRUCTURE RIGHT SIDE STA 300-340. CLIPS REPAIRED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1999061100451 19990611 00451 NM 1999 6 11 P5CA9900615 1 19990603 A 5320 CLIP BOEING 747 747283B 1384867 NM BS 320, 280, 340 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 FOUND CRACKS ON VERTICAL BEAM CLIPS NOSE WHEEL WELL STRUCTURE LEFT SIDE AT BS 320, 280, 340. REPAIRED CLIPS PER SRM 51- 30-02. 2 L 7 4 4F A20WE 1999061100452 19990611 00452 NM 1999 6 11 P5CA9900616 1 19990602 A 5101 STRUCTURE BOEING 747 747122 1384872 NM AIRFRAME DAMAGED A P5CA K NONE C F.O.D. DE DESCENT 1 WP 23 853FT 19753 INBOUND TO RMS AIRCRAFT FLEW THRU INBEDDED THUNDERSTORMS AND HAIL CAUSING DAMAGE TO LEADING EDGES, L1 WINDSHIELD, RADOME AND NAV LIGHTS. PERFORMED BIRD STRIKE/HAIL CONDITION INSPECTION PER MM 5-51-13. REPLACED L1 WINDOW PER MM 56-11-01. R EPLACED NAV LIGHT LENSES PER MM 33-43-03. REPLACED RADOME PER MM 53-52-01. REPAIRED DAMAGED LEADING EDGES ON HORIZ STA B PER POLAR MA 5510-07:01. 2 L 7 4 4F A20WE 1999061100453 19990611 00453 NM 1999 6 11 VNAA9906001 1 19990603 A 3240 BRAKE SYST DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT REQD SERVICE A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 430JS 3044 THE CAPTAINS RIGHT HAND BRAKES DID NOT FUNCTION WHEN PEDAL FORCE WAS APPLIED. THE AIRCRAFT RETURNED TO THE GATE. OUTST ATION MAINTENANCE INSPECTED AND BLED THE CAPTAINS RIGHT HAND BRAKES, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42 -00. TAXI CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999061100454 19990611 00454 NM 1999 6 11 VNAA9906002 1 19990604 A 3240 BRAKES DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT REQD SERVICE A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 430JS 3044 THE CAPTAINS RIGHT HAND BRAKES WERE REPORTED BY THE CREW TO BE MUSHY WHEN APPLIED. MAINTENANCE BLED THE CAPTAINS RIGHT HAND BRAKES, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAF T WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999061100455 19990611 00455 NM 1999 6 11 VNAA9906003 1 19990606 A 3240 AC69963 METERING UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BRAKE SYST FAILED A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 430JS 4605 130 3044 THE AIRCRAFT BRAKES WERE REPORTED BY THE CREW TO PULSATE AND WERE UNSAFE WHEN APPLIED AT LOW AND HIGH SPEEDS. MAINTENAN CE INSPECTED AND REPLACED THE BRAKE METERING UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-03. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999061100456 19990611 00456 NM 1999 6 11 GAIA9958 1 19990513 A 2781 H1010262 SWITCH BOEING 727 727214 138407R NM NR 5 LE FLAP FAILED A GAIA K NONE N FALSE WARNING DE DESCENT 1 SW 07 750US 21512 DURING LANDING OF FLT KHA 511 FROM MCI TO TOL, THE NR 5 LEADING EDGE FLAP AMBER LIGHT REMAINED ILLUMINATED ON THE FLIGHT ENGINEER'S AND FORWARD INSTRUMENT PANELS WHEN SELECTED TO 5 DEGREES. THE FLIGHT CREW FOLLOWED KHA ABNORMAL CHECKLIST A ND DECLARED AN EMERGENCY LANDING INTO TOL. THE AIRCRAFT MADE A SAFE LANDING WITH NO FURTHER INCIDENTS. (M) 2 L 7 3 4F A3WE 1999061100457 19990611 00457 NM 1999 6 11 USAA990214 1 19990423 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 10R TIE CLIP. REPLACED PART. (M) 2 L 7 2 4F A16WE 1999061100458 19990611 00458 NM 1999 6 11 USAA990213 1 19990423 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRCK BS 787 STRINGER 10L TIE CLIP. REPLACED PART. (M) 2 L 7 2 4F A16WE 1999061100459 19990611 00459 NM 1999 6 11 USAA990212 1 19990423 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727 STRINGER 8L TIE CLIP. REPLACED PART. (M) 2 L 7 2 4F A16WE 1999061100460 19990611 00460 NM 1999 6 11 USAA990211 1 19990423 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 727A STRINGER 1 TIE CLIP. REPLACED PART. (M) 2 L 7 2 4F A16WE 1999061100461 19990611 00461 NM 1999 6 11 USAA990210 1 19990423 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 8R TIE CIP. REPLACED PART. (M) 2 L 7 2 4F A16WE 1999061100462 19990611 00462 NM 1999 6 11 USAA990209 1 19990423 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 15R TIE CLIP. REMOVED ORIGINAL CLIP A ND HFEC PART AND STRINGER, NO CRACK FOUND. REINSTALLED ORIGINAL PART PER SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1999061100463 19990611 00463 NM 1999 6 11 USAA990433 1 19990502 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 343 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 45252 22883 TPA - DURING CX-4 CHECK VISUAL CONFIRMED BY EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK IN SKIN AT DOOR SILL IN RIV ET HOLE STATION 343. INSTALLED DOUBLER PER EA 64494. (M) 2 L 7 2 4F A16WE 1999061100464 19990611 00464 NM 1999 6 11 USAASB99116 1 19990430 A 2121 5007024620 FAN BOEING 737 737201 1384454 NM CABIN FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 242US 57267 22444 RIC - FLT 517 - EN ROUTE FOR CLT-DCA AT FL250, FLIGHT ATTENDANT REPORTED THAT A PASSENGER SMELLED SMOKE IN THE FIRST THR EE ROWS OF CABIN. CAPTAIN TURNED GALLEY POWER OFF AND THE FLIGHT ATTENDANT WENT BACK AND CONFIRMED SMOKE COMING OUT OF THE AIR CONDITIONING VENTS. AN EMERGENCY WAS DECLARED. FLIGHT DESCENDED TO FL100 AND DEPRESSURIZED. FLIGHT DIVERTED T O RIC AND LANDED NORMALLY USING FLAPS 40. EMERGENCY EQUIPMENT WAS STANDING BY AND FOLLOWED AIRCRAFT ALL THE WAY TO THE GATE. NO EMERGENCY EVACUATION OCCURRED. MAINTENANCE REMOVED AND REPLACED THE GASPER FAN. OPERATIONAL CHECK GOOD. (M ) 2 L 7 2 4F A16WE 1999061100465 19990611 00465 NM 1999 6 11 USAA990394 1 19990422 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 52217 21816 TPA - DURING EDDY CURRENT INSPECTION, FOUND A 1.25 INCH SKIN CRACK AT BS 727A PLUS 6 INCHES AT STRINGER 19L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999061100466 19990611 00466 NM 1999 6 11 USAA990395 1 19990422 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 52217 21816 TPA - DURING EDDY CURRENT INSPECTION, FOUND A 2 INCH SKIN CRACK AT BS 727A PLUS 13 INCHES AT STRINGER 18L. INSTALLED RE PAIRED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999061100467 19990611 00467 NM 1999 6 11 USAA990396 1 19990422 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 52217 21816 TPA - DURING EDDY CURRENT INSPECTION, FOUND A .875 INCH SKIN CRACK AT BS 727B PLUS 9 INCHES AT STRINGER 17L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999061100468 19990611 00468 NM 1999 6 11 UIEA9921 1 19990414 A 2612 FIRE WARNING BOEING 747 747228F 1384895 NM COCKPIT ACTIVATED A UIEA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 EA 15 536MC 21576 FLT GT020 - FIRE WARNING BELL AND LIGHT SOUNDED ON FORWARD COCKPIT LIGHT FOR CARGO AREA, BUT WENT OUT TOO FAST TO CHECK F/E PANEL. CHECK CARGO AREA FIRE TEST AND INDICATION AND NO ABNORMALITIES NOTED. (M) 2 L 7 4 4F A20WE 1999061100469 19990611 00469 NM 1999 6 11 UIEA9922 1 19990430 A 2611 SMOKE DETECTOR BOEING 747 747230B 1384889 NM NR 4 MALFUNTIONED A UIEA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 508MC 21644 FLT CI328 - MAIN DECK SMOKE DETECTOR (NR 1) RED WARNING LIGHT ILLUMINATED AND BELL SOUNDED AND NR 4 SMOKE DETECTOR (A) L IGHT INTERMITTENTLY FLASHED A FEW TIMES DURING THE FIRST THREE HOURS OF FLIGHT. THEY CAN ON AT THE SAME TIME AND WERE O NLY ON FOR A SHORT PERIOD OF TIME. OPERATIONAL CHECK OF SYSTEM REVEALED NO ABNORMALITIES. (M) 2 L 7 4 4F A20WE 1999061100470 19990611 00470 NM 1999 6 11 UIEA9920 1 19990606 A 3310 MAP LIGHT BOEING 747 7472D7B 1384803 NM LT COCKPIT SMOKING A UIEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 526MC 22337 FLT EK9880 - AMS/DXB - APPROXIMATELY 5 HOURS IN CRUISE, CAPTAIN NOTICED SMOKE COMING FROM AREA OF CAPTAINS MAP LIGHT ASS EMBLY. THIS WAS A MOMENTARY CONDITION. THE FLIGHT CONTINUED FOR ANOTHER 4 HOURS UNEVENTFULLY. DXB MAINTENANCE INSPECT ED ALL WIRING BEHIND CAPTAINS MAP LIGHT ASSY AND NO BURNING FOUND. MAP LIGHT ASSY OPERATIONS NORMALLY. (M) 2 L 7 4 4F RT A20WE 1999061100471 19990611 00471 NM 1999 6 11 UIEA9919 1 19990407 A 2611 2156646 SMOKE DETECTOR BOEING 747 747230B 1384889 NM CARGO COMPT DEFECTIVE A UIEA K NONE N FALSE WARNING CR CRUISE 1 EA 15 508MC 21644 FLT CI326 - MAIN DECK SMOKE DETECTOR SECTION 1 GAVE TOW MOMENTARY FIRE WARNINGS. INSPECTED MAIN DECK AND DETERMINED WAR NING TO BE FALSE. MAIN SMOKE DETECTOR REPLACED. OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1999061100472 19990611 00472 NM 1999 6 11 ORJA99159 1 19990427 A 3610 33991062 VALVE DOUG MD90 MD9030 3023690 NM LT ENGINE FAILED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 901RA 53489 SJC - ABORTED TAKEOFF, ON TAKEOFF ROLL, LEFT PNEUMATIC SYSTEM FAULT ON EOAP THROUGH 80 KNOTS. REMOVED AND REPLACED LEFT PRESSURE REGULATING PILOT SHUTOFF VALVE IAW MM 36-12-03. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999061100473 19990611 00473 WP 1999 6 11 ORJA99165 1 19990426 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 8-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 IN RENO, EMERGENCY LIGHTS ON AT ROWS 8-11. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-53-01. (M) 2 L 7 2 4F RT A6WE 1999061100474 19990611 00474 WP 1999 6 11 ORJA99164 1 19990425 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 20 DEF DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 IN SJC, EMERGENCY LIGHTS ON AT ROWS 8-11. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT ROW 20 DEF IAW MM 33-53-01. O PS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999061100475 19990611 00475 WP 1999 6 11 ORJA99163 1 19990426 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 8-11 CHAFED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 IN PDX, EMERGENCY EXIT LIGHT ON ROWS 8-11. FOUND CHAFING WIRE UNDER SEAT 9D PERFORMED. OPS CHECK OK. ALL INDICATIONS NORMAL PER COMPONENT MAINTENANCE MANUAL 400-079. (M) 2 L 7 2 4F RT A6WE 1999061100476 19990611 00476 WP 1999 6 11 ORJA99161 1 19990424 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 20A DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 IN RNO, EMERGENCY LIGHTS AT SEAT 7D, 8D, 9D AND 10D INOPERATIVE. REPLACED BATTERY PACK AT 20A. OPS NORMAL PER 33-53-01 . (M) 2 L 7 2 4F RT A6WE 1999061100477 19990611 00477 WP 1999 6 11 ORJA99160 1 19990415 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC983 3022083 WP RT EMER EXIT DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 IN LAS - EMERGENCY LIGHTS ROW 6-10 ON. REMOVED AND REPLACED EXIT BATTERY PACK AT FORWARD RIGHT O/W EMERGENCY EXIT PER M M 33-53-00 LIGHTS OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999061100478 19990611 00478 WP 1999 6 11 ORJA99167 1 19990425 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC983 3022083 WP EMPENNAGE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 836RA 53046 SJC - EMERGENCY LIGHT AT EMPENNAGE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK LIGHT AT EMPENNAGE IAW MM 33-53-01. O PS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999061100479 19990611 00479 WP 1999 6 11 ORJA99166 1 19990424 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP RT EMER EXIT BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 SJC - EMERGENCY LIGHT INOPERATIVE AT ROW 8 THROUGH 12 AT RIGHT FORWARD WING EXIT. REPAIRED BROKEN WIRE CONNECTION, OPS CHECK GOOD PER MM 33-53-00. (M) 2 L 7 2 4F A6WE 1999061100480 19990611 00480 WP 1999 6 11 ORJA99168 1 19990423 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 15-18 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAX, EMERGENCY LIGHTS CAME ON DURING DESCENT AISLE ROW 15 THROUGH 18. REPLACED LEFT OVERWING BATTERY PACK ASSY. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999061100481 19990611 00481 WP 1999 6 11 ORJA99158 1 19990428 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAX, REAR ROW EMERGENCY LIGHTS CAME ON AND STAYED ON DURING FLIGHT. REMOVED AND REPLACED LEFT AFT EMERGENCY LIGHT BA TTERY CHARGER PER MM 33-00-00. (M) 2 L 7 2 4F RT A6WE 1999061100482 19990611 00482 NE 1999 6 11 99ZZZM320 2 19990427 A 8530 327629 CYLINDER CVAC 240 2405 2422612 WP PWA R2800 R2800* 52026 NE NR 11 POSITION CRACKED A TFAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 15 295M 64 P31580 NR 2 ENGINE BACK FIRING IN CRUISE. FEATHERED ENGINE AND LANDED TJBQN. FOUND NR 11 CYLINDER CRACKED. REPLACED AND AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R 4 R A793 5E8 1999061100483 19990611 00483 EU 1999 6 11 SIMA991221 1 19990502 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 720 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 236AE 340B236 ABI - FOUND DENT ON LOWER FUSELAGE SKIN AT STATION 720 AND BETWEEN SL 1624 AND SL 1528. REMOVED DAMAGED AREA BY MAKING A .75 INCH CUTOUT. PERFORMED EDDY CURRENT INSPECTION TO THE CUT OUT, NO DEFECTS NOTED. FABRICATED FILLER AND INTERNAL DOUBLER .040 THICK WITH FILLER MEASURING .65 INCH DIAMETER AND DOUBLER MEASURING 3.25 INCH DIAMETER. APPLIED CORROSION PROTECTION OF ALODINE AND EPOXY PRIMER TO REPAIR PARTS AND CUT OUT AREA. APPLIED FAY SEALANT TO MATING SURFACES AND WET ASSEMBLED. APPLIED EDGE/FILLET SEALANT, ADDED FINISH PAINT. WORK DONE IAW SAAB SRM 53-80-10 PAGES 217-222 AND SAAB ST ANDARD PRACTICES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100484 19990611 00484 EU 1999 6 11 SIMA991231 1 19990503 A 3350 74332 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AE 340B374 DFW - FLT 3798 - EMERGENCY LIGHT STRIP AT SEAT 9A IS LOOSE. REMOVED AND REPLACED EMERGENCY LIGHT STRIP. OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100485 19990611 00485 EU 1999 6 11 SIMA991211 1 19990501 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 278AE 18325 340B278 SBA - FLT 9733 - ALL EMERGENCY LIGHTS DO NOT ILLUMINATE. CREW FOUND SWITCH WAS LEFT IN THE ARMED POSITION WHICH DISCHAR GED ALL OF THE BATTERIES. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY POWER SUPPLIES. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 1999061100486 19990611 00486 EU 1999 6 11 99ZZZM321 1 19990501 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 278AE 20530 340B278 SBA - FLT 9733 - ALL EMERGENCY LIGHTS DO NOT ILLUMINATE. CREW FOUND SWITCH WAS LEFT IN THE ARMED POSITION WHICH DISCHAR GED ALL OF THE BATTERIES. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY POWER SUPPLIES. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 1999061100487 19990611 00487 EU 1999 6 11 99ZZZM322 1 19990501 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 278AE 17079 340B278 SBA - FLT 9733 - ALL EMERGENCY LIGHTS DO NOT ILLUMINATE. CREW FOUND SWITCH WAS LEFT IN THE ARMED POSITION WHICH DISCHAR GED ALL OF THE BATTERIES. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY POWER SUPPLIES. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 1999061100488 19990611 00488 EU 1999 6 11 99ZZZM323 1 19990501 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 278AE 17199 340B278 SBA - FLT 9733 - ALL EMERGENCY LIGHTS DO NOT ILLUMINATE. CREW FOUND SWITCH WAS LEFT IN THE ARMED POSITION WHICH DISCHAR GED ALL OF THE BATTERIES. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY POWER SUPPLIES. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 1999061100489 19990611 00489 EU 1999 6 11 99ZZZM324 1 19990501 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 278AE 17504 340B278 SBA - FLT 9733 - ALL EMERGENCY LIGHTS DO NOT ILLUMINATE. CREW FOUND SWITCH WAS LEFT IN THE ARMED POSITION WHICH DISCHAR GED ALL OF THE BATTERIES. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY POWER SUPPLIES. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 1999061100490 19990611 00490 EU 1999 6 11 SIMA991241 1 19990504 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU AVIONICS RACK MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 346SB 82937 340B346 ALB - FLT 4858 - AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT. DIVERTED TO ALB. VERIFIED EVENT WAS A FALSE WARNING. REM OVED AND REPLACED AVIONICS RACK SMOKE DETECTOR. AIRRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100491 19990611 00491 EU 1999 6 11 SIMA991192 1 19990429 A 3350 7239410803 LIGHT SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 241AE 340B241 DFW - FLT 5080 - ONE LIGHT BULB IN EMERGENCY EXIT LIGHTED SIGN ADJACENT TO SEAT 3A DOES NOT ILLUMINATE. REMOVED AND REP LACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100492 19990611 00492 EU 1999 6 11 SIMA991181 1 19990428 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 344SB 340B344 DFW - FLT 5059 - OVERHEAD EMERGENCY LGIHT AT SEAT 14A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHEC K GOOD. (M) 2 L 7 2 4T RT A52EU 1999061100493 19990611 00493 EU 1999 6 11 SIMA991178 1 19990427 A 5330 S53872501200 SKIN AEROSP ATR72 ATR72212 EU FRAME 46-47 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 425MJ 425 SAW - DURING MBV-2 INSPECTION CLEARED TDMI NR 425MQ53023 TWO DENTS IN THE LEFT SIDE OF THE FUSELAGE SKIN 18 INCHES FORWA RD OF THE TAILCONE, BETWEEN FRAMES 46 AND 47 AND BETWEEN STRINGERS 13 AND 16. FORWARD DENT MEASURED 1.5 INCHES INBOARD DIAMETER BY .018 DEEP AND AFT DENT MEASURED 1.75 LONG BY .023 DEEP. REPAIRED THE DENTS IAW SRM 53-00-00 FIGURE 403. AI RCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100494 19990611 00494 EU 1999 6 11 SIMA991177 1 19990427 A 5330 S53671205200 SKIN AEROSP ATR72 ATR72212 EU FRAME 31-32 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 425MJ 425 SAW - DURING MBV-2 INSPECTION, FOUND A DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 31 AND 32 AND BETWEEN S TRINGER 10 AND 12, MEASURING 3 INCHES IN DIAMETER BY .038 DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100495 19990611 00495 EU 1999 6 11 SIMA991176 1 19990427 A 5320 S5337129320001 DRAIN TRACK AEROSP ATR42 ATR42300 8680920 EU CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 141AE 141 SAW - DURING CPCP-1 INSPECTION, FOUND THE FORWARD CARGO DOOR SILL DRAIN TRACK, SUPPORT PLATE AND WEB BETWEEN FRAMES 13 A ND 18 CORRODED. REMOVED AND REPLACED ALL THREE PARTS IAW SRM 53-37-80. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100496 19990611 00496 EU 1999 6 11 99ZZZM325 1 19990427 A 5320 S5337129320201 SUPPORT AEROSP ATR42 ATR42300 8680920 EU CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 141AE 141 SAW - DURING CPCP-1 INSPECTION, FOUND THE FORWARD CARGO DOOR SILL DRAIN TRACK, SUPPORT PLATE AND WEB BETWEEN FRAMES 13 A ND 18 CORRODED. REMOVED AND REPLACED ALL THREE PARTS IAW SRM 53-37-80. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100497 19990611 00497 EU 1999 6 11 99ZZZM326 1 19990427 A 5320 S5337122622001 WEB AEROSP ATR42 ATR42300 8680920 EU CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 141AE 141 SAW - DURING CPCP-1 INSPECTION, FOUND THE FORWARD CARGO DOOR SILL DRAIN TRACK, SUPPORT PLATE AND WEB BETWEEN FRAMES 13 A ND 18 CORRODED. REMOVED AND REPLACED ALL THREE PARTS IAW SRM 53-37-80. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100498 19990611 00498 EU 1999 6 11 SIMA991175 1 19990427 A 5313 S5357430020000 STRINGER AEROSP ATR42 ATR42300 8680920 EU FRAME 26-28 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 141AE 141 SAW - DURING CPCP1 INSPECTION, FOUND THE SPECIAL STRINGERS 21L AND 21R BETWEEN FRAMES 26 AND 28 CORRODED. REPAIRED BOTH STRINGERS IAW SRM SPECIAL STRINGER REPAIR SECTION 53-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100499 19990611 00499 EU 1999 6 11 SIMA991174 1 19990427 A 5320 S5307030922401 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME 43-44 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 141AE 141 DURING CPCP-1 INSPECTION, FOUND THE LEFT FLOOR SUPPORT ANGLE BETWEEN FRAMES 43 AND 44 CORRODED. REMOVED AND REPLACED TH E ANGLE IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100500 19990611 00500 EU 1999 6 11 SIMA991173 1 19990427 A 5347 S53070308200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CARGO COMPT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 141AE 141 SAW - DURING CPCP1 INSPECTION, FOUND THE AFT CARGO RIGHT OUTBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TR ACK IAW EO-E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100501 19990611 00501 EU 1999 6 11 SIMA991172 1 19990427 A 5320 S5307020520301 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME 12 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 141AE 141 SAW - DURING CPCP1 INSPECTION, FOUND THE CREASE BEAM RIGHT ANGLE AT FRAME 12 WAS CORRODED. REMOVED AND REPLACED THE ANG LE IAW RM 51-25-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100502 19990611 00502 EU 1999 6 11 SIMA991162 1 19990426 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 271AT 17801 273 SAW - DURING PS-2 INSPECTION, FOUND NUMEROUS FORWARD EMERGENCY LGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 3WL IAW JIC 335121-RAI-10000. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999061100503 19990611 00503 EU 1999 6 11 SIMA991151 1 19990425 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 271AT 18680 273 SAW - DURING PS-2 INSPECTION, FOUND NUMEROUS FORWARD EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENC Y LIGHT BATTERY PACK AT LOCATION 3WL IAW JIC 335121-RAI-10000. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE ( M) 2 H 7 2 4T RT A53EU 1999061100504 19990611 00504 EU 1999 6 11 SIMA9911211 1 19990422 A 5753 S5751004900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND THE CENTER CAM GUIDE ON THE RIGHT INBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100505 19990611 00505 EU 1999 6 11 SIMA9911210 1 19990422 A 5753 S5751013300300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE RIGHT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100506 19990611 00506 EU 1999 6 11 99ZZZM327 1 19990422 A 5753 S5751012900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE RIGHT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100507 19990611 00507 EU 1999 6 11 99ZZZM328 1 19990422 A 5753 S5751013200300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE RIGHT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100508 19990611 00508 EU 1999 6 11 99ZZZM329 1 19990422 A 5753 S5751013000300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE RIGHT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100509 19990611 00509 EU 1999 6 11 99ZZZM330 1 19990422 A 5753 S5751013100300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE RIGHT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100510 19990611 00510 EU 1999 6 11 SIMA991129 1 19990422 A 5753 S5751014800300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE RIGHT OUTBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100511 19990611 00511 EU 1999 6 11 99ZZZM331 1 19990422 A 5753 S5751014900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE RIGHT OUTBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100512 19990611 00512 EU 1999 6 11 99ZZZM332 1 19990422 A 5753 S5751015000300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE RIGHT OUTBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVE D AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100513 19990611 00513 EU 1999 6 11 SIMA991128 1 19990422 A 5753 S5751004900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE RIGHT INBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100514 19990611 00514 EU 1999 6 11 SIMA991127 1 19990422 A 5753 S5751013300200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE LEFT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100515 19990611 00515 EU 1999 6 11 99ZZZM333 1 19990422 A 5753 S5751012900200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE LEFT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100516 19990611 00516 EU 1999 6 11 99ZZZM334 1 19990422 A 5753 S5751013200200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE LEFT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100517 19990611 00517 EU 1999 6 11 99ZZZM335 1 19990422 A 5753 S5751013000200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE LEFT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100518 19990611 00518 EU 1999 6 11 99ZZZM336 1 19990422 A 5753 S5751013100200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL FIVE CAM GUIDES ON THE LEFT OUTBOARD FLAP OUTBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100519 19990611 00519 EU 1999 6 11 SIMA991126 1 19990422 A 5753 S5751014800200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURNG MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE LEFT OUTBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100520 19990611 00520 EU 1999 6 11 99ZZZM337 1 19990422 A 5753 S5751014900200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURNG MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE LEFT OUTBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100521 19990611 00521 EU 1999 6 11 99ZZZM338 1 19990422 A 5753 S5751015000200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURNG MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE LEFT OUTBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100522 19990611 00522 EU 1999 6 11 SIMA991125 1 19990422 A 5753 S5751004900200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND ALL THREE CAM GUIDES ON THE LEFT INBOARD FLAP INBOARD DEFLECTOR CORRODED. REMOVED AND REPLACED THE CAM GUIDES IAW SRM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100523 19990611 00523 EU 1999 6 11 SIMA991124 1 19990422 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 357 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 344SB 340B344 ABI - DURNG MBV INSPECTION, DENTS WERE DISCOVERED ON THE RIGHT FUSELAGE SKIN PANEL AT STATION 357 BETWEEN SL 1615/1616. RECONTOURED DENTS AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED TWO EXTERNAL DOUBLERS .050 THICK. APPLIED PROT ECTIVE TREATMENT TO THE DOUBLERS AND ONE COAT OF ALODINE AND EPOXY PRIMER. APPLIED FAY SEALANT TO THE CONTACT SURFACE O F THE DOUBLERS, REPOSITIONED, AND INSTALLED TO AIRCRAFT. APPLIED FILLET SEALANT AROUND EDGES OF THE DOUBLERS AND RESTOR ED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1506 AND SAAB SRM 53-70-10 PAGE 217 AND STANDARD SRM PRO CEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100524 19990611 00524 NM 1999 6 11 USAA990361 1 19990502 A 5320 WEB BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTIOIN, FOUND A CRACK .5 INCH VERTICAL ON WEB AT STATION 178 RBL 4.5 WL 198 BULKHEAD WEB. INSTALLED DOUBLER AND FILLER PER T/R 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999061100525 19990611 00525 NM 1999 6 11 USAA990369 1 19990502 A 5320 BEAM BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION FS 344 BL 0 TO LBBL 10 BEAM. CORROSION TASK NR C53-10 7-02. INSTALLED T-CHORD PER EA 64363 AND TR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1999061100526 19990611 00526 NM 1999 6 11 USAA990368 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727F CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 727F BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07, SRM 53-30-07, 53-60-07 AND EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061100527 19990611 00527 NM 1999 6 11 USAA990367 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT BS 867 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061100528 19990611 00528 NM 1999 6 11 USAA990366 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07, 53-30-07, 53-60-07 AND EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061100529 19990611 00529 NM 1999 6 11 USAA990428 1 19990502 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN RADIUS AT STATION 294.5 RBL 54.75 WL 208 ANGLE. INSTA LLED DOUBLER ANGLE PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1999061100530 19990611 00530 NM 1999 6 11 USAA990427 1 19990502 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 986.5 ALONG ENTIRE FLOORBEAM CORROSION TASK NR C53- 107-02. INSTALLED NEW T-CAP, STRAPS, AND SPLICE PER TR 53-60-01. (M) 2 L 7 2 4F RT A16WE 1999061100531 19990611 00531 NM 1999 6 11 USAA990426 1 19990502 A 5320 BEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH SPOT OF SURFACE CORROSION AT FS 328 RBL 40 BEAM, CORROSION TASK NR C53-107-02. SPLICED IN NEW SECTION OF T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999061100532 19990611 00532 NM 1999 6 11 USAA990419 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 867 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. IN STALLED DOUBLER PER SRM 53-00-07 FIG 202 AND EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061100533 19990611 00533 NM 1999 6 11 USAA990424 1 19990502 A 5320 STRAP BOEING 737 737401 1384701 NM BS 780-847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 67 INCH AREA OF SPOTTED CORROSION AT RBL 20 STATION 780-847 STRAP. INSTALLED NEW STRAP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999061100534 19990611 00534 NM 1999 6 11 USAA990418 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 907 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. IN STALLED DOUBLER PER SRM 53-00-07 FIG 202 AND EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061100535 19990611 00535 NM 1999 6 11 USAA990417 1 19990502 A 5321 FLOOR BOEING 737 737401 1384701 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK, NDT VISUAL INSPECTION, FOUND A .75 INCH CRACK AT BS 663.75 LBL 32 FLOOR. INSTALLED DOUBLER PER EA 64378. (M) 2 L 7 2 4F RT A16WE 1999061100536 19990611 00536 NM 1999 6 11 USAA990416 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 787 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. IN STALLED DOUBLER PER SRM 53-00-07 FIG 202 AND EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061100537 19990611 00537 NM 1999 6 11 USAA990415 1 19990502 A 5320 WEB BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 178 LBL 4.5 W/L 201 WEB. FABRICATED AND INST ALLED DOUBLER PER EA 6420. (M) 2 L 7 2 4F RT A16WE 1999061100538 19990611 00538 NM 1999 6 11 USAA990414 1 19990502 A 5320 TIE CLIP BOEING 737 737401 1384701 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT TIE CLIP STATION 767 STRINGER 26L. REMOVED AND REPL ACED STRINGER TIE CLIP PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999061100539 19990611 00539 NM 1999 6 11 USAA990413 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 9 INCH CRACK IN FRAME AT BS 747 BETWEEN STRINGER 8L AND STRINGER 9L. I NSTALLED DOUBLER PER EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061100540 19990611 00540 NM 1999 6 11 USAA990412 1 19990502 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947.530767 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 32 INCH AREA OF CORROSION AT STATION 947.5 LT AND RT OF BL 0 FLOORBEAM . REPAIRED 'T' CAP PER TR 53-60-02. (M) 2 L 7 2 4F RT A16WE 1999061100541 19990611 00541 NM 1999 6 11 USAA990399 1 19990502 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 270-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 26 INCH AREA OF CORROSION AT FORWARD ENTRY DOOR THRESHOLD 'Z' ANGLE F/ S 270 TO FS 344 LBBL 55. REMOVED AND REPLACED 'Z' ANGLE PER REPAIR DOCUMENT 51-70-13. (M) 2 L 7 2 4F RT A16WE 1999061100542 19990611 00542 NM 1999 6 11 USAA990398 1 19990502 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 787-847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF SPOTTED CORROSION FROM STATION 787 TO 847 RBL 14 FLOORB EAM. CORROSION TASK NR C53-208-01. REMOVED AND REPLACED PER TR 53-00-53. (M) 2 L 7 2 4F RT A16WE 1999061100543 19990611 00543 NM 1999 6 11 USAA990397 1 19990502 A 5320 WEB BOEING 737 737401 1384701 NM CARGO DOORWAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 14 INCH BY 30 INCH AREA OF SPOTTED CORROSION UNDER AFT CARGO SILL PANE L WEB. CORROSION TASK NR C53-202-07. REMOVED AND REPLACED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999061100544 19990611 00544 NM 1999 6 11 USAA990381 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727A BETWEEN STRINGER 8R AND STRINGER 9R. REPAIRED DOUBLER PER EA 64326 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999061100545 19990611 00545 NM 1999 6 11 USAA990380 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727D BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED DOUBLER PER EA 64326 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999061100546 19990611 00546 NM 1999 6 11 USAA990379 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727F CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727F BETWEEN STRINGER 8R AND 9R. DOUBLER REPAIRED PER SRM 53-00-07 GIF 202. (M) 2 L 7 2 4F RT A16WE 1999061100547 19990611 00547 NM 1999 6 11 USAA990378 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 747 BETWEEN STRINGER 8R AND STRINGER 9R. REPAIRED DOUBLER PER EA 64326 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999061100548 19990611 00548 NM 1999 6 11 USAA990377 1 19990502 A 5320 BEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND AN AREA OF SURFACE CORROSION SPOTS APPROX 1 INCH AT FS 312, LBBL 24 TO R BBL 12. CORROSION TASK NR C53-107-02. SPLICED IN NEW SECTION OF 'T' CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999061100549 19990611 00549 NM 1999 6 11 USAA990370 1 19990502 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 178 RBL .5 WL 188 BULKHEAD WEB. INSTALLED DOUBLE R PER SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999061100550 19990611 00550 NM 1999 6 11 USAA990425 1 19990502 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 5.3 INCH BY 3.5 INCH AREA OF CORROSION AT RBL 3 STATION 1016 PLUS 5 IN CHES BL 0 PRESS BULKHEAD. INSTALLED DOUBLER PER SRM 53-80-08. (M) 2 L 7 2 4F RT A16WE 1999061100551 19990611 00551 NM 1999 6 11 USAA990371 1 19990502 A 5312 BULKHEAD WEB BOEING 737 737401 1384701 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AFT PRESSURE BULKHEAD DOME WEB STIFFENER AT BOTTOM OF BL 0 STA TION 1016. INSTALLED REPAIR STIFFENER AND REPAIR SPLICES PER SRM 53-70-11. (M) 2 L 7 2 4F RT A16WE 1999061100552 19990611 00552 NM 1999 6 11 USAA990372 1 19990502 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT PRESSURE BULKHEAD RT OF BL 0 JUST AFT STAT ION 1016. INSTALLED DOUBLER PER SRM 53-80-08. (M) 2 L 7 2 4F RT A16WE 1999061100553 19990611 00553 NM 1999 6 11 EISA99052 1 19990219 A 5755 FITTING BOEING 727 727223 1384074 NM NR 5 SPOILER CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CRACKED ATTACH FITTING ON NR 5 SPOILER. REMOVED AND REPLACED NR 5 SPOILER WITH SERVICEABLE UNIT. (M) 2 L 7 3 4F A3WE 1999061100554 19990611 00554 NM 1999 6 11 EISA99051 1 19990219 A 5754 692548312 WEB BOEING 727 727223 1384074 NM NR 8 LE SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND WEB CRACKED IN SEVERAL PLACES, NR 8 SLAT. REMOVED WEB PART NR 69-28483-12 AND INSTALLED NEW PAR NR 69-28483-12 WITH SCREWS. (M) 2 L 7 3 4F A3WE 1999061100555 19990611 00555 NM 1999 6 11 EISA99050 1 19990219 A 5754 RIB BOEING 727 727223 1384074 NM NR 5 LE SLAT CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DEEP GOUGES AND CORROSION ON NR 5 SLAT RIB AT OUTBOARD TRACK F ORWARD ATTACH BOLT HOLE. REMOVED GOUGES AND CORROSION, FABRICATED AND INSTALLED RIB DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061100556 19990611 00556 NM 1999 6 11 EISA99049 1 19990219 A 5754 RIB BOEING 727 727223 1384074 NM NR 5 LE FLAP GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DEEP GOUGES IN RIB OF NR 5 SLAT AT INBOARD TRACK FORWARD ATTAC H BOLT HOLE. REMOVED GOUGES, FABRICATED AND INSTALLED RIB DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061100557 19990611 00557 NM 1999 6 11 EISA99048 1 19990219 A 5754 RIB BOEING 727 727223 1384074 NM NR 3 LE FLAP GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND DEEP GOUGES IN RIB AT OUTBOARD TRACK FORWARD ATTACH BOLT HOLE, NR 3 SLAT. REMOVED GOUGES BY REAMING HOLE PER AD 97-07-08 AND SB 57-0134. (M) 2 L 7 3 4F A3WE 1999061100558 19990611 00558 NM 1999 6 11 EISA99047 1 19990219 A 5754 RIB BOEING 727 727223 1384074 NM NR 1 LE SLAT CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CORROSION AND GOUGES IN RIB OF NR 1 SLAT AT OUTBOARD TRACK FOR WARD ATTACH BOLT HOLE. REMOVED CORROSION AND GOUGES. FABRICATED AND INSTALLED RIB DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061100559 19990611 00559 NM 1999 6 11 EISA99046 1 19990219 A 5754 RIB BOEING 727 727223 1384074 NM NR 4 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACK AND GOUGE IN RIB OF NR 4 SLAT AT OUTBOARD TRACK FORWARD ATTACH BOLT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061100560 19990611 00560 NM 1999 6 11 EISA99045 1 19990219 A 5754 RIB BOEING 727 727223 1384074 NM NR 6 LE SLAT GOUGE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND DEEP GOUGE IN RIB OF NR 6 SLAT AT INBOARD TRACK FORWARD ATTACH BOLT-HOLE. FABRICATED AND INSTALLED RIB DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061100561 19990611 00561 NM 1999 6 11 EISA99043 1 19990219 A 5753 SKIN BOEING 727 727223 1384074 NM RT TE MIDFLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND AREA OF DELAMINATION TOP SURFACE OF RIGHT MID-FLAP. REPAIRED DELAMINATION AREA PER SRM 57-50-1, 57-50-2 AND 57-50-4. (M) 2 L 7 3 4F A3WE 1999061100562 19990611 00562 NM 1999 6 11 EISA99044 1 19990219 A 5712 RIB BOEING 727 727223 1384074 NM LEFT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACK IN RIB OF NR 4 SLAT AT INBOARD TRACK FORWARD ATTACH BOLT -HOLE. FABRICATED AND INSTALLED RIB DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061100563 19990611 00563 NM 1999 6 11 EISA99042 1 19990219 A 5320 65191043 ANGLE BOEING 727 727223 1384074 NM BS 1343 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND 1.5 INCH CRACK AT FORWARD LEFT OF FRAME, FS 1343 ABOVE 'S' DUC T. REMOVED CRACKED PART NR 65-19104-3. FIT TRIM AND DRILL NEW PART NR 65-19104-3 AND INSTALLED PER SRM 51-10-1 AND 51- 30-2. (M) 2 L 7 3 4F A3WE 1999061100564 19990611 00564 NM 1999 6 11 EISA99041 1 19990219 A 5753 SKIN BOEING 727 727223 1384074 NM LT TE MIDFLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND LEFT OUTBOARD MID FLAP DELAMINATED AT LOWER SURFACE TRAILING E DGE. REPAIRED TRAILING EDGE PER SRM 57-50-1, L57-50-2 AND 57-50-4. (M) 2 L 7 3 4F A3WE 1999061100565 19990611 00565 NM 1999 6 11 EISA99038 1 19990219 A 5320 6559948502 FITTING BOEING 727 727223 1384074 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND .25 INCH CRACK IN LOWER AFT CORNER OF AFT CARGO DOOR. REMOVED DAMAGED CORNER SECTION, NEW PART 65-59948-502 DRILLED PER SRM 51-10-1 AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999061100566 19990611 00566 NM 1999 6 11 EISA99081 1 19990327 A 5730 SKIN BOEING 727 727223 1384074 NM WS 456 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND 5 INCH CRACK ON RIGHT WING LEADING EDGE AT WS 456 ABOVE FUELIN G BAY. TRIMMED OUT DAMAGED AREA PER SRM 57-30-4. FABRICATED FILLER AND DOUBLER PER SRM 57-30-4. INSTALLED REPAIR PER SRM 57-30-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999061100567 19990611 00567 NM 1999 6 11 EISA99080 1 19990327 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 620-720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND LEFT OUTBOARD SEAT TRACK CRACKED AT BS 620-720. REMOVED DAMAG ED SEAT TRACK FROM BS 620-720. FABRICATED NEW SEAT TRACK FROM 60-13201 EXTRUSION PER SAMPLE AND INSTALLED PER SRM 51-30 -2. (M) 2 L 7 3 4F A3WE 1999061100568 19990611 00568 NM 1999 6 11 EISA99079 1 19990327 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 520 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND RIGHT OUTBOARD SEAT TRACK CRACKED AT BS 520. REMOVED DAMAGED SEAT TRACK FROM BS 480-580. FABRICATED NEW SEAT TRACK FROM 60-13201 PER SAMPLE AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999061100569 19990611 00569 NM 1999 6 11 EISA99077 1 19990327 A 5753 RIB BOEING 727 727223 1384074 NM NR 4 LE SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND NR 4 SLAT OUTBOARD SUPPORT RIB CRACKED. STOP DRILLED CRACK PE R SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061100570 19990611 00570 NM 1999 6 11 EISA99076 1 19990327 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 675/527 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND STRINGER TIE CRACKED AT BS 675, 527L. REMOVED DAMAGED PART, F ABRICATED AND INSTALLED NEW STRINGER TIE PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999061100571 19990611 00571 NM 1999 6 11 EISA99074 1 19990327 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 1342.4 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACKED STIFFENER ON FORWARD SIDE OF NR 2 ENGINE FIREWALL AT B S 1342.4, PREVIOUS REPAIR. REMOVED OLD REPAIR, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999061100572 19990611 00572 NM 1999 6 11 EISA99073 1 19990327 A 5311 FRAME BOEING 727 727223 1384074 NM BS 440 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND FRAME CRACKED AND DEFORMED AT BS 440, WL 210. TRIMMED DAMAGED SECTION PER SRM 51-40-3. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999061100573 19990611 00573 NM 1999 6 11 EISA99070 1 19990327 A 2761 SUPPORT BOEING 727 727223 1384074 NM RT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACK AT NR 13 SPOILER ACTUATOR INBOARD SUPPORT ANGLE ON REAR SPAR. REMOVED CRACKED SUPPORT AND FABRICATED NEW PAR PER SRM 51-10-1. INSTALLED SUPPORT PER SRM 51-10-1 AND 51-30-2. ( M) 2 L 7 3 4F A3WE 1999061100574 19990611 00574 NM 1999 6 11 EISA99068 1 19990327 A 5522 SKIN BOEING 727 727223 1384074 NM LT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND A 2.5 INCH CRACK IN SKIN ON LEFT ELEVATOR LOWER SURFACE, 20 IN CH AFT OF PANEL NR 9308. STOP DRILLED CRACK PER SRM 55-20-3. FABRICATED AND INSTALLED DOUBLER PER SRM 55-20-3. (M) 2 L 7 3 4F A3WE 1999061100575 19990611 00575 NM 1999 6 11 EISA99057 1 19990314 A 7830 65578771 SWITCH BOEING 727 727223 1384074 NM NR 1 TR UNIT OUT OF ADJUST A EISA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 6819 19494 NR 1 REVERSER LIGHT CAME ON WHEN THROTTLES ADVANCED. ADJUSTED SWITCH FOR NR 1 THRUST REVERSER OPERATING LIGHT PER MM 79 -30. RAN NR 1 ENGINE AND FUNCTION CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1999061100576 19990611 00576 WP 1999 6 11 EISA99060 1 19990327 A 3260 7000010101 SWITCH DOUG DC9 DC931 3022065 WP NLG SHORTED A EISA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 945VJ 47066 ON FINAL, AFTER PUTTING GEAR DOWN DID NOT GET A GREEN NOSE GEAR DOWN INDICATION. FOLLOWED PROCEDURES AND CONFIRMED NOSE GEAR DOWN AND LOCKED THROUGH PEEPHOLE. REPLACED NOSE GEAR LOCK SWITCH PER M/LM 32-60-01. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999061100577 19990611 00577 WP 1999 6 11 EISA99062 1 19990331 A 3350 60030951 POWER PACK DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 950VJ 47564 DURING SERVICE CHECK, FOUND NR 1 THROUGH NR 5 CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY FOR NR 1 THROUGH NR 5 CEILING EMERGENCY LIGHTS IAW MM CHAPTER 33-50-0. (M) 2 L 7 2 4F A6WE 1999061100578 19990611 00578 EU 1999 6 11 SIMA991123 1 19990422 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 344SB 340B344 ABI - DURING MBV INSPECTION, SEAT TRACK 18.3L WAS DISCOVERED TO BE CORRODED. REMOVED FASTENERS AND EXISTING SEAT TRACK. DRILLED FASTENER HOLES ON NEW SEAT TRACK EXTRUSION AND TREATED. POSITIONED NEW SEAT TRACK AND SECURED. APPLIED DINIT ROL TO SEAT TRACK AND SUPPORTS. WORK DONE IAW SAAB SRM 53-70-60 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100579 19990611 00579 EU 1999 6 11 SIMA991122 1 19990422 A 5347 7253799381 SEAT TACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 344SB 340B344 DURING MBV INSPECTION, SEAT TRACK BL 0 WAS DISCOVERED TO BE CORRODED. REMOVED FASTENERS AND EXISTING SEAT TRACK. DRILL ED FASTENERS HOLES ON NEW SEAT TRACK EXTRUSION AND TREATED. POSITIONED NEW SEAT TRACK AND SECURED. APPLIED DINITROL TO SEAT TRACK AND SUPPORTS. WORK DONE IAW SAAB SRM 53-70-60 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100580 19990611 00580 EU 1999 6 11 SIMA991121 1 19990422 A 5414 AL7075T6 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 344SB 340B344 ABI - DURING MBV INSPECTION A CHAFE WAS DISCOVERED ON THE LEFT NACELLE INBOARD OUTER SKIN AT FILLET SEAL CONTACT. BLEND ED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. RESTORED PROTECTIVE TREATMENT INCLUDING THE POLYURETHANE T OP COAT. FABRICATED A DOUBLER AND TRIPLER BOTH .050 THICK. FABRICATED A SHIM .020 THICK. APPLIED FAY SEALANT TO THE C ONTACT SURFACES OF THE REPAIR PARTS AND INSTALLED TO AIRCRAFT. APPLIED FILLET SEALANT AROUND THE EDGES OF THE DOUBLER A ND TRIPLER. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1505 AND STAND SRM PROCEDURES. AIRCR AFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100581 19990611 00581 EU 1999 6 11 SIMA991116 1 19990421 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 249AT 251 0249 ORD - FLT 4302 - EMERGENCY FLOOR PROXIMITY LIGHTS IN THE FORWARD CABIN DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENC Y LIGHT POWER SUPPLY IAW ATR MM 33-51-21. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100582 19990611 00582 EU 1999 6 11 SIMA991115 1 19990421 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING CPCP-1 INSPECTION, FOUND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED BOTH S EAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100583 19990611 00583 EU 1999 6 11 SIMA991113 1 19990421 A 5315 S5367240620802 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 DURING CPCP-1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED FLOORBEAMS 36 AND 38 IAW SR M 51-25-02. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-00-00 FIGURE 438. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100584 19990611 00584 EU 1999 6 11 99ZZZM339 1 19990421 A 5315 S5367240720202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 DURING CPCP-1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED FLOORBEAMS 36 AND 38 IAW SR M 51-25-02. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-00-00 FIGURE 438. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100585 19990611 00585 EU 1999 6 11 99ZZZM340 1 19990421 A 5315 S5367240620801 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 DURING CPCP-1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED FLOORBEAMS 36 AND 38 IAW SR M 51-25-02. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-00-00 FIGURE 438. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100586 19990611 00586 EU 1999 6 11 99ZZZM341 1 19990421 A 5315 S5367240921801 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 DURING CPCP-1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED FLOORBEAMS 36 AND 38 IAW SR M 51-25-02. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-00-00 FIGURE 438. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100587 19990611 00587 EU 1999 6 11 SIMA991114 1 19990421 A 5330 S53172101216 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 6 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING CPCP-1 INSPECTION, FOUND A DENT IN THE LEFT FUSELAGE SKIN AT FRAME 6 BETWEEN STRINGERS 14 AND 15M, MEASURIN G 1 INCH IN DIAMETER AND .023 DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 408. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100588 19990611 00588 EU 1999 6 11 SIMA991112 1 19990421 A 2710 S2711009700320 CONTROL LINK AEROSP ATR42 ATR42300 8680920 EU RT AILERON CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND THE RIGHT AILERON TRIM TAB DUAL LOAD PATH CONTROL LINK EXFOLIATED. REMOVED AND REP LACED THE CONTROL LINK IAW JIC 271172-RAI-10000-002. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100589 19990611 00589 EU 1999 6 11 SIMA991111 1 19990421 A 5320 S5367121729402 SILL AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING MBV-1 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE CORRODED. REMOVED AND REPLACED THE SILL PLATE IAW SR M 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100590 19990611 00590 EU 1999 6 11 SIMA991104 1 19990420 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 312AE 312 LAX - FLT 3237 - EMERGENCY OVERHEAD LIGHT AT SEAT 14A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB SEAT 14A. OPERATI ONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100591 19990611 00591 EU 1999 6 11 SIMA991103 1 19990420 A 5320 S5337129320001 DRAIN TRACK AEROSP ATR42 ATR42300 8680920 EU CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 271AT 273 SAW - DURING CPCP-1 INSPECTION, FOUND THE FORWARD CARGO DOOR DRAIN TRACK CORRODED. REMOVED AND REPLACED THE DRAIN TRACK IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061100592 19990611 00592 EU 1999 6 11 SIMA991102 1 19990420 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 ABI - DURING A MBV INSPECTION, A CHAFE WAS DISCOVERED ON RIGHT NACELLE INBOARD INNER SKIN PANEL. BLENDED OUT THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A DOUBLER .025 THICK. APPLIED FAY SEALANT TO THE CONTACT SURFACE OF THE DOUBLER, REPOSITIONED, AND INSTALLED FASTENERS WET. APPLIED FIRE SEAL AROUND DOU BLER WITH DOW CORNING DC 730. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1494. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100593 19990611 00593 EU 1999 6 11 SIMA991101 1 19990420 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 177.65 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 ABI - DURING A MBV INSPECTION, A BULGE WAS DISCOVERED ON THE AFT LOWER FUSELAGE SKIN AT STATION 177.65 ABOVE STRINGER 15 24. CUT OUT DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A SPACER .032 THICK. FABRICATED A REPAIR PLATE .032 THICK. CLEANED AND APPLIED ALODINE, PRIMER, AND FILLET SEALANT TO THE CONTACT SU RFACE OF THE REPAIR PARTS. FILLED GAP BETWEEN THE SPACER AND THE SKIN WITH FILLET SEALANT. APPLIED TOP COAT TO THE INN ER AREA AND APPLIED DINITROL. RESTORED TOP COAT TO THE OUTER SURFACE. WORK DONE IAW SAAB SRM 53-80-10 PAGE 218 AND STA NDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100594 19990611 00594 EU 1999 6 11 SIMA991098 1 19990419 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-307 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 353SB 340B353 ABI - DURING AN MBV INSPECTION, SEAT TRACK BL 18.3L WAS CORRODED BEYOND LIMITS AT STATION 298. REMOVED DAMAGED SECTION OF SEAT TRACK FROM STATION 297-307. PREPARED REPAIR SEAT TRACK SECTION EXTRUSION 4650000-043 SHPAL 7075-T76511 AND CUT TO LENGTH. PREPARED REPAIR U-BEAM PLAL 7075-T7351. APPLIED SURFACE TREATMENT TO ALL BARE SURFACE. INSTALLED REPAIR SE AT TRACK AND REPAIR U-BEAM WITH FAY SEALANT AND INSTALLED FASTENERS. APPLIED SURFACE TREATMENT TO ALL EXPOSED ATTACHMEN T HARDWARE. WORK DONE IAW SAAB SRM STANDARD PROCEDURES AND SAAB SRM 53-70-60 PAGES 204-205. AIRCRAFT OK FOR SERVICE. ( M) 2 L 7 2 4T RT A52EU 1999061100595 19990611 00595 EU 1999 6 11 SIMA991097 1 19990419 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 353SB 340B353 ABI - DURING A MBV INSPECTION A CHAFE WAS DISCOVERED ON THE RIGHT NACELLE INBOARD OUTER SKIN PANEL AT FILLET FAIRING SEA L CONTACT POINT. BLENDED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. CUT OUT AREA AROUND PUNCTURE AND APPLIE D PROTECTIVE TREATMENT AND POLYURETHANE TOP COAT TO THE BLENDED AREA AND CUT OUT EDGES. FABRICATED A DOUBLER AND A TRIP LER .050 THICK. FABRICATED SHIMS .020 THICK. APPLIED PROTECTIVE TREATMENT AND SEALANT TO THE CONTACT SURFACES OF THE R EPAIR PARTS AND INSTALLED ON AIRCRAFT. APPLIED FILLET SEALANT AROUND EDGE STEPS OF THE REPAIR PARTS. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1473 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061100596 19990611 00596 NM 1999 6 11 USAA990438 1 19990507 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AU 44551 22884 TPA - DURING CX-2 CHECK, FOUND .375 INCH LONG SKIN CRACK, LEFT FUSELAGE, 2 INCH AFT OF BS 727B AT LOWER EDGE OF STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. DOUBLER MADE OF 2024T3 - .063 PER BOEING SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999061100597 19990611 00597 NM 1999 6 11 USAA990436 1 19990510 A 5330 SKIN BOEING 737 737201 1384454 NM BS 947 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 44770 22758 TPA - DURING UNSCHEDULED MAINTENANCE, FOUND .125 INCH CRACK IN SKIN AT STATION 947 AND STRINGER 14R. INSTALLED DOUBLER MADE OF .063 INCH STAINLESS STEEL .5 HARD PER SRM 53-30-3 FIG 21A. (M) 2 L 7 2 4F A16WE 1999061100598 19990611 00598 NM 1999 6 11 USAA990437 1 19990514 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 756 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 231US 51129 21976 TPA - DURING CX-6 CHECK, FOUND 2.5 INCH CRACK IN SKIN AT BS 756 AND S17L. INSTALLED DOUBLER MADE OF 2024T3 .071 INCH TH ICK PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999061100599 19990611 00599 NM 1999 6 11 USAA990439 1 19990514 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 231US 51129 21976 TPA - DURIGN CX-6 CHECK, FOUND .125 INCH CRACK IN SKIN AT BS 727A AND S16L. INSTALLED DOUBLER MADE FROM 2024T3 .100 INC H THICK PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999061100600 19990611 00600 NM 1999 6 11 USAA990391 1 19990423 A 5320 654581945 WEB BOEING 737 7372B7 1384560 NM BS 259 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND A 2 INCH CRACK AT STATION 259 BL 0 CEILING ON NWW VERT STIFFENER WEB. REPAIRED PER SRM 51-10-01 PAGE 5. (M) 2 L 7 2 4F A16WE 1999061100601 19990611 00601 NM 1999 6 11 USAA990423 1 19990423 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 540 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT TERMINAL END STRINGER 26R AT STATION 540. INSTALLED NEW END FITTING PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1999061100602 19990611 00602 NM 1999 6 11 USAA990390 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 12 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRAPS PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 1999061100603 19990611 00603 NM 1999 6 11 USAA990382 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 1 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRAPS PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 1999061100604 19990611 00604 NM 1999 6 11 USAA990364 1 19990423 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING A Q-C CHECK, VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 727 LEFT STRINGER 18A OUTER CHORD FRAME. INS TALLED NEW CHORD PER EO 5394G068 AND EO 5394G076. (M) 2 L 7 2 4F A16WE 1999061100605 19990611 00605 NM 1999 6 11 USAA990363 1 19990423 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH CRACKS AT BS 727 BETWEEN STRINGER 24R AND 25R CHORD AN GLE. REPAIRED PER EA 64377, 64403 AND EO 5394G068. (M) 2 L 7 2 4F A16WE 1999061100606 19990611 00606 NM 1999 6 11 USAA990353 1 19990423 A 5313 655586818 STRINGER BOEING 737 7372B7 1384560 NM BS 911 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2.5 INCH CORRODED AREA AT STRINGER 20L AND STATION 911 AFT C ARGO. INSTALLED J ANGLE, U CHANNEL, SHIMS AND CLIP PER SRM 53-10-3 AND SRM 51-20-1. (M) 2 L 7 2 4F A16WE 1999061100607 19990611 00607 NM 1999 6 11 USAA990314 1 19990423 A 5240 SKIN BOEING 737 7372B7 1384560 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR LOWER AFT CORNER SKIN. INSTALLED EXTERNAL DOUBLER PER T/R 53-10-19 REV A AND EA 64244 AND 64167. (M) 2 L 7 2 4F A16WE 1999061100608 19990611 00608 NM 1999 6 11 USAA990313 1 19990423 A 5330 SKIN BOEING 737 7372B7 1384560 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK HFEC INSPECTION, FOUND A .09375 INCH CRACK IN FORWARD ENTRY DOOR LOWER HINGE CUTOUT FUSELAGE SKIN . INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3 FIG 31. (M) 2 L 7 2 4F A16WE 1999061100609 19990611 00609 NM 1999 6 11 USAA990312 1 19990423 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FLOORBEAM TO FUSELAGE ATTACH ANGLE AT BS 597, RBL 70. 85 AND WL 204-208. INSTALLED ANGLE REPAIR PER EA 64287. (M) 2 L 7 2 4F A16WE 1999061100610 19990611 00610 NM 1999 6 11 USAA990309 1 19990423 A 5320 CREASEBEAM BOEING 737 7372B7 1384560 NM BS 270-360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING VISUAL CHECK INSPECTION, FOUND SEVERAL AREAS OF CORROSION AT BS 270 TO BS 360 STRINGER 17L CREASEBEAM INNER CHORD ANGLE. REPAIRED PER BOEING DRAWING 65-17688 AND SRM 51-30-3. (M) 2 L 7 2 4F A16WE 1999061100611 19990611 00611 NM 1999 6 11 USAA990303 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 947 RBL 6 FLOORBEAM. INSTALLED REPAIR ANGLES AND FILLERS PER SRM 53-10-09 PAGE 26 THROUGH PAGE 30. (M) 2 L 7 2 4F A16WE 1999061100612 19990611 00612 NM 1999 6 11 USAA990302 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 986.5. SPLICED IN NEW SECTION OF FLOORBE AM 'T' CAP PER TR 53-60-01 AND EA 64288. (M) 2 L 7 2 4F A16WE 1999061100613 19990611 00613 NM 1999 6 11 USAA990301 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND CORROSION ALONG TOP SURFACE OF FLOORBEAM AT STATION 967, CORROSION TA SK NR C53-107-02. SPLICED IN NEW 'T' CAP AND DOUBLER PER SRM 53-10-9 FIG 2 AND EA 64204. (M) 2 L 7 2 4F A16WE 1999061100614 19990611 00614 NM 1999 6 11 USAA990300 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 328 LBL 12 AND RBL 1. INSTALLED NEW 'T' CAP REPAIR ANGLES AND STRAPS PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 1999061100615 19990611 00615 NM 1999 6 11 USAA990299 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 294.5 BL 0. SPLICED IN NEW 'T' CAP PER T R 53-10-04B. (M) 2 L 7 2 4F A16WE 1999061100616 19990611 00616 NM 1999 6 11 USAA990298 1 19990423 A 5320 CAP BOEING 737 7372B7 1384560 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION AT BS 344 LBL 6 AND LBL 10 FLOOR 'T' CAP, COR ROSION TASK NR C53-107-01. INSTALLED NEW 'T' CAP REPAIR ANGLES AND CAPS PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 1999061100617 19990611 00617 NM 1999 6 11 USAA990297 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH AREAS OF CORROSION AT STATION 967 BETWEEN LBL 10 AND R BL 50 FLOORBEAM. SPLICED IN NEW 'T' CAP PER SRM 53-10-09 AND EA 64202. (M) 2 L 7 2 4F A16WE 1999061100618 19990611 00618 NM 1999 6 11 USAA990296 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON SURFACE TOP OF FLOORBEAM STATION 1006, CORROSION TASK NR C5 3-107-02. SPLICED IN NEW 'T' CAP PER SRM 53-10-09 AND EA 64206, R 53-10-13. (M) 2 L 7 2 4F A16WE 1999061100619 19990611 00619 NM 1999 6 11 USAA990291 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT STATION 947 RBL 6 ON FLOORBEAM , CORROSION TASK NR C53-107-02. INSTALLED ANGLE PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1999061100620 19990611 00620 NM 1999 6 11 USAA990290 1 19990423 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 947-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY 20 INCH AREA OF CORROSION AT STATION 947 TO STATION 1016 LB L 53 INNER CHORD ANGLE, CORROSION TASK NR C53-107-02. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999061100621 19990611 00621 NM 1999 6 11 USAA990289 1 19990423 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION ON FLOORBEAM AT STATION 328 LBL 12 AND RBL 1, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 1999061100622 19990611 00622 NM 1999 6 11 USAA990259 1 19990423 A 5320 CC1127652 TIE CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 16R TIE CLIP. REPAIRED PER SRM 51-10-0 1. (M) 2 L 7 2 4F A16WE 1999061100623 19990611 00623 NM 1999 6 11 USAA990220 1 19990423 A 5320 69353521 TIE CLIP BOEING 737 7372B7 1384560 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 847 STRINGER 1 TIE CLIP. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 1999061100624 19990611 00624 NM 1999 6 11 USAA990430 1 19990426 A 5330 507945178 SKIN BOEING 737 7372B7 1384560 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 44503 22885 TPA - DURING CX-1 EDDY CURRENT CHECK INSPECTION, FOUND A 2 INCH CRACK LOWER FORWARD ENTRY DOOR HINGE CUT OUT SKIN. INST ALLED DOUBLER PER TR 52-10-5. (M) 2 L 7 2 4F A16WE 1999061100625 19990611 00625 NE 1999 6 11 USAAD99064 2 19990513 A 7321 7696067 FUEL CONTROL DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE LT ENGINE FAILED A USAA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 EA 19 802US 12991 48036 PIT-DFW - FLT 1588 - DURING CRUISE, THE CREW ATTEMPTED TO ADJUST THE LEFT ENGINE THRUST SETTING BUT THERE WAS NO RESPONS E TO THE THROTTLE LEVER MOVEMENT. THE ENGINE POWER STAYED ON 90 PERCENT N1. DURING APPROACH FOR LANDING AT THE DESTINA TION THE LEFT ENGINE WAS SHUTDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CON TROL AND ENGINE DRIVEN FUEL PUMP. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999061100626 19990611 00626 WP 1999 6 11 GTIA9900570 1 19990419 A 2560 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DISENGAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 GALLEY SLIDE PACK FELL OFF. REINSTALLED GALLEY SLIDE PACK IAW DC-9 MM 25-00. OPERATION CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999061100627 19990611 00627 WP 1999 6 11 GTIA9900571 1 19990413 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 MYR - CABIN EMERGENCY LIGHTS WILL NOT WORK. FOUND LOOSE WIRE ON BACK OF SWITCH. TIGHTENED AS REQUIRED IAW 33-53-0 DC-9 MM. OPERATION CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999061100628 19990611 00628 WP 1999 6 11 GTIA9900572 1 19990414 A 2560 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR DISENGAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 942ML 47478 L1 SLIDE PACK FELL OFF COMPLETELY CASING AND SLIDE. REINSTALLED L1 SLIDE PACK AND SLIDE COVER IAW DC-9 MM 25-62-0. SLI DE PACK AND COVER SECURED. OPERATION CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999061100629 19990611 00629 WP 1999 6 11 GTIA9900576 1 19990414 A 3350 LIGHT DOUG DC9 DC987 3022087 WP BS 1408 INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 750RA 49777 LGA - TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT AT STATION 1408. BROKEN AND INOPERATIVE AT BULB HOLDER BASE. REPLACED BROKEN BULB HOLDER BASE OF LIGHT L2-637 IAW MM 33-53-00. LIGHT OPERATION CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999061100630 19990611 00630 WP 1999 6 11 GTIA9900756 1 19990419 A 2560 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DISENGAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DTW - GALLEY SLIDE PACK FELL OFF. REINSTALLED GALLEY SLIDE PACK IAW DC-9 MM 25-00. OPERATION CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999061100631 19990611 00631 WP 1999 6 11 GTIA9900573 1 19990414 A 2560 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR DISENGAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DTW - SLIDE PACK FELL OFF GALLEY DOOR. REINSTALLED R1 SLIDE PACK IAW DC-9 MM 25-61-00. (M) 2 L 7 2 4F A6WE 1999061100632 19990611 00632 WP 1999 6 11 GTIA9900574 1 19990413 A 3350 LIGHT DOUG DC9 DC987 3022087 WP LT EMER EXIT INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 750RA 49777 LGA - L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY WITH REPAIRED ASSEMBLY PER MM 33-50-00. OPERATION CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999061100633 19990611 00633 WP 1999 6 11 GTIA9900755 1 19990423 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMER EXIT DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805RA 48087 DTW - OVERWING AFT EMERGENCY EXIT INTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERIES. OPE RATION CHECK GOOD IAW MD-80 MM 33-50-0. (M) 2 L 7 2 4F A6WE 1999061100634 19990611 00634 WP 1999 6 11 GTIA9900636 1 19990401 A 3350 BULB DOUG DC9 DC932 3022066 WP COCKPIT FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941ML 47131 MLB - CO-PILOTS EMERGENCY FLOOR LIGHTS DO NOT COME ON. RELAMPED FIRST OFFICERS EMERGENCY FLOOD LIGHTS. OPERATIONS CHEC K GOOD PER DC-9 MM 33-11-2. NO OTHER DISCREPANCIES NOTED. (M) 2 L 7 2 4F A6WE 1999061100635 19990611 00635 NM 1999 6 11 99ZZZM342 1 19990506 A 3240 BRAKES BOEING 727 727227 1384078 NM RT MLG DIRTY A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 11 783AT 22000 SMOKE WAS NOTED COMING FROM THE RIGHT MAIN LANDING GEAR AFTER LANDING. NO FIRE NOTED BY THE EMERGENCY CREW. RESIDUAL H YDRAULIC WAS NOTICED ON BRAKES AFTER THE BRAKES WERE REPLACED THE PREVIOUS NIGHT. MAINTENANCE ROTATED BRAKES AND NO DRA GGING WAS NOTED. (M) 2 L 7 3 4F A3WE 1999061100636 19990611 00636 NM 1999 6 11 99ZZZM343 1 19990320 A 2752 MS9391130ZE4C MOTOR BOEING 727 727227 1384078 NM TE FLAPS LEAKING A AMTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 769AT 21998 DURING CRUISE, THE 'A' SYSTEM HYDRAULIC QTY DECREASED TO ZERO. FLUID SHUT OFF CLOSED PRIOR TO LOW PRESSURE WARNING LIGH TS ON. FOUND FLAP HYDRAULIC MOTOR LEAKING. REMOVED AND REPLACED FLAP HYDRAULIC MOTOR PER MM. (M) 2 L 7 3 4F A3WE 1999061100637 19990611 00637 NM 1999 6 11 99ZZZM344 1 19990404 A 2750 CONTROL CABLE BOEING 727 727208 138407W NM RT TE FLAP BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 780AT 22295 DURING PREFLIGHT, FOUND RIGHT INBOARD FLAP INBOARD TE FLAP CABLE BROKEN. REMOVED AND REPLACED RIGHT ACTUATING CABLE PER MM 27-51-5, ADJUSTED AND TESTED OK. (M) 2 L 7 3 4F RT A3WE 1999061100638 19990611 00638 NM 1999 6 11 99ZZZM345 1 19990318 A 3241 WIRE BOEING 727 727247 138408F NM ANTI-SKID SYSTEM SHORTED A AMTA K NONE O OTHER LD LANDING 1 GL 11 784AT 21393 THE NR 3 AND NR 4 MAIN TIRES BLEW ON LANDING. REMOVED AND REPLACED TIRES AND BRAKES. FOUND PROBLEM IN THE WIRING TO TH E ANTI-SKID CONTROL BOX. WIRES 034 AND 025 AT CONNECTOR 4656P WERE FOUND EXPOSED AND SHORTED TO GROUND. WIRES WERE RE- SPLICE AND TESTED GOOD. (M) 2 L 7 3 4F A3WE 1999061100639 19990611 00639 SO 1999 6 11 ASOA99041 1 19990428 A 3610 CLAMP EMB 120 EMB120RT SO RT ENGINE LOOSE A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 11 215AS 120010 DURING CLIMB-OUT CSG-ATL, RIGHT ENGINE 'DUCT LEAKAGE' LIGHT ILLUMINATED. LIGHT REMAINED ON FOR 3 MINUTES AFTER CLOSRING RIGHT ENGINE BLEED. DUCT LEAK LIGHT WENT OUT 4 MINUTES AFTER RIGHT ENGINE WAS SHUTDOWN. DECLARED AN EMERGENCY AND RET URNED TO CSG. MAINTENANCE PERSONNEL FOUND THE ENGINE BLEED SOV LINE CLAMP LOOSE. CLAMP WAS TIGHTENED AND OPERATIONAL C HECKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999061100640 19990611 00640 SO 1999 6 11 ASOA99043 1 19990505 A 3610 12024949001 DUCT EMB 120 EMB120RT SO FUSELAGE CRACKED A ASOA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 11 281AS 120224 ON CLIMB-OUT FROM XNA-DFW, THE RIGHT DUCT LEAK WARNING LIGHT ILLUMINATED FOLLOWED BY THE LEFT DUCT LEAK WARNING LIGHT. T HE CREW SMELLED SMOKE BUT DID NOT OBSERVE ANY. EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO XNA. AFTER LANDING, THE ENGINES WERE SHUTDOWN AND PASSENGERS EVACUATED DUE TO THE PERSISTENT SMOKE ODOR AND DUCT LEAK INDICATIONS. THE AIR CRAFT WAS MAINTENANCE FERRIED TO DFW WHERE MAINTENANCE FOUND THE CROSS BLEED DUCT BLOWN. THE DUCT WAS REPLACED AND THE AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999061100641 19990611 00641 SO 1999 6 11 ASOA99042 1 19990503 A 5411 12003852001 FRAME EMB 120 EMB120RT SO LT/RT NACELLES CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 244AS 28297 120073 DURING C-CHECK INSPECTION, FOUND LEFT AND RIGHT ENGINE NACELLE FRAME NR 1 TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRA ME IN LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999061100642 19990611 00642 SO 1999 6 11 ASOA99039 1 19990422 A 6120 78249046 PCU EMB 120 EMB120RT SO RT PROPELLER FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 235AS 5050 120047 ON CLIMB-OUT BETWEEN 3000 AND 4000 FEET, THE RIGHT PROP FLUCTUATED FROM 98.2 PERCENT TO 101.5 PERCENT. FOLLOWED QRH PRO CEDURES PROP SYNC OFF. PROP STABILIZED AT 101.2 PERCENT AFTER 30 SECONDS. CONTINUED WITH QRH PROCEDURES. FLIGHT IDLE S AME RPM. DECLARED AN EMERGENCY, FEATHERED RIGHT PROP AND RETURNED TO DFW. ENGINE WAS NOT SHUT DOWN, JUST FEATHERED. E EC WAS OFF DUE TO PREVIOUS DEFER. MAINTENANCE REMOVED AND REPLACED THE RIGHT PCU. LEAK AND OPS CHECKS WERE GOOD. RIGH T EEC WAS ALSO REPLACED TO CLEAR THE DEFER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999061100643 19990611 00643 NM 1999 6 11 TSAA9933230 1 19990504 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 1, NR 2, AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999061100644 19990611 00644 NE 1999 6 11 99ZZZM346 2 19990417 A 7314 371900 FUEL PUMP BOEING 727 727251 138408H NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A S84A O OTHER Y ENGINE STOPPAGE AP APPROACH 1 EA 21 267US 5271 20289 653971 ON SIX MILE FINAL, NR 2 ENGINE FLAMED OUT. FOUND NR 2 ENGINE FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP PER MM 73-11-1. PERFORMED ENGINE HIGH POWER RUN PER MM 71-00-57. SYSTEM CHECKED GOOD. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999061100645 19990611 00645 NM 1999 6 11 USAASB99099 1 19990417 A 3230 65462057 LINK BOEING 737 7372B7 1384560 NM NLG BROKEN A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 279AU 22891 BOS - FLT 2609 - AFTER GEAR RETRACTION, CREW HEARD A LOUD NOISE AND FELT A VIBRATION FROM THE NOSE GEAR AREA. FLIGHT DI VERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT NOSE LANDING GEAR LINK ASSEMBLY BROKEN. REPLACED LINK ASSEMBLY PER MM 32-33-61. OPERATIONAL CHECK OF NOSE LANDING GEAR NORMAL. (M ) 2 L 7 2 4F A16WE 1999061100646 19990611 00646 NM 1999 6 11 USAASB99104 1 19990419 A 2931 ST107R TRANSMITTER BOEING 737 7372B7 1384560 NM 'B' HYD SYSTEM FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 278AU 29708 22890 BWI - FL2785 - ON CLIMB-OUT FROM IAD, AT FL170, THE 'B' HYDRAULIC SYSTEM BRAKE PRESSURE INDICATOR FAILED AND INDICATED Z ERO. ALL OTHER HYDRAULIC INDICATIONS WERE NORMAL. CAPTAIN ELECTED TO DIVERT TO BWI AND DECLARE EMERGENCY. FLIGHT LAND ED WITHOUT INCIDENT AND TAXIED TO THE GATE ON ITS OWN POWER. PASSENGERS DEPLANED NORMALLY. MAINTENANCE REMOVED AND REP LACED THE 'B' HYDRAULIC SYSTEM BRAKE SYSTEM BRAKE PRESSURE TRANSMITTER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061100647 19990611 00647 NM 1999 6 11 USAA990450 1 19990430 A 5312 BULKHEAD BOEING 737 737401 1384701 NM AFT PRESS BLKHD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK, FOUND 3 INCHES OF CORROSION AT BL 0 AFT OF 1016 ON WEB OF PRESSURE BULKHEAD, CORROSION LEVEL 2. INSTALLED WEB STIFFENER PER SRM 53-80-08. (M) 2 L 7 2 4F RT A16WE 1999061100648 19990611 00648 NM 1999 6 11 USAA990458 1 19990522 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND 1 INCH CRACK AT DRAG ANGLE AT STATION 540 STRINGER 22L. INSTALLED REPAIR ANGLE PER TYPICA L REPAIR 53-50-03. (M) 2 L 7 2 4F RT A16WE 1999061100649 19990611 00649 NM 1999 6 11 USAASB99129 1 19990524 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 226US 21815 GSO - MAINTENANCE FOUND THE AISLE SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A WIRE SPLICE AND TWO BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061100650 19990611 00650 NM 1999 6 11 USAASB99130 1 19990517 A 3350 CONNECTOR BOEING 737 737401 1384701 NM ROW 6A LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 413US 23882 TPA - MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTING AT SEAT ROW 6A AND THE FIRST CLASS CABINET, LEFT SIDE INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG AT THE FIRST CLASS CABINET, LEFT SIDE, DISCONNECTED. RECONNECTED CANNON PLUG. OPERA TIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061100651 19990611 00651 NM 1999 6 11 USAA059905 1 19990521 A 7920 443330 O-RING BOEING 727 727225 1384077 NM NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 923TS 20441 FLT 6470 - DCA-LGA - NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. ON RUNUP, FOUND OIL LINE TO FUEL OIL COOLER LEAKING. REPLACED O-RING SEAL. RAN ENGINE, OPS CHECK OK MM REF 79-33-0. (M) 2 L 7 3 4F A3WE 1999061100652 19990611 00652 WP 1999 6 11 HALA9900117 1 19990520 A 2781 CONNECTOR DOUG DC9 DC951 3022051 WP LE FLAPS FAILED A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 672MC 47661 HNL - FLT 208 - SLAT DISAGREE LIGHT STAYS ON WHEN SLATS ARE EXTENDED. REPLACED NR 6 PIN ON RIGHT EXTEND SWITCH CANNON P LUG. OPS CHECK ON GROUND GOOD. (M) 2 L 7 2 4F RT A6WE 1999061100653 19990611 00653 WP 1999 6 11 HALA9900119 1 19990522 A 4990 SWITCH DOUG DC9 DC951 3022051 WP APU OIL SYSTEM FAILED A HALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 661HA 47796 HNL - FLT 106 - FLIGHT ATTENDANTS REPORT HAZE AND UNUSUAL ODOR IN CABIN AND SMOKE ALARM ACTIVATION. REPLACED APU OIL PR ESSURE SEQUENCE SWITCH, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999061100654 19990611 00654 NE 1999 6 11 HALA9900118 2 19990520 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17A 52049 NE LEFT FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 662HA 47742 688016 HNL - LEFT EPR DOES NOT RESPOND TO PWR LEVER MOVEMENT APPROPRIATELY. TOOK MUCH MORE LEFT POWER LEVER MOVEMENT TO MATCH RIGHT THROTTLE. LEFT FUEL FLOW WAS APPROX 2000 LBS HIGHER TO MATCH EPR SETTINGS ON RIGHT ENGINE. OTHER LEFT ENGINE IND ICATIONS MATCHED RIGHT ENGINE INDICATIONS WHEN EPR WAS MATCHED. EXCEPT FOR THROTTLE POSITION, LEFT WAS MUCH HIGHER AND HIGH LEFT FUEL FLOW. REMOVED AND REPLACED NR 1 ENGINE. ETR APPROX 1000AM LOCAL. DURING TEARDOWN FOUND SECONDARY FUEL MANIFOLD RUPTURED. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 1999061100655 19990611 00655 NM 1999 6 11 ORJA99171 1 19990510 A 3350 8039251 BATTERY PACK DOUG MD90 MD9030 3023690 NM BS 402 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 901RA 53489 SJC - FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IW 33-5117. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999061100656 19990611 00656 WP 1999 6 11 ORJA99177 1 19990516 A 3241 33019 MANIFOLD DOUG DC9 DC983 3022083 WP LT MLG WW FAILED A ORJA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 11 879RA 53185 RNO - THE RIGHT HYDRAULIC BRAKE PRESSURE INDICATOR DROPS TO 1500 PSI WITH ENGINE HYD PUMP IN LOW AND AUXILIAR PUMP OFF. REMOVED AND REPLACED RT ABS LANDING MANIFOLD IAW MM 32-44-03, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999061100657 19990611 00657 WP 1999 6 11 ORJA99176 1 19990518 A 3350 CONNECTOR DOUG DC9 DC987 3022087 WP ROW 9 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 755RA 49727 AT SJC, EMERGENCY LIGHT AT ROW 9 INOPERATIVE. REPAIRED CONNECTION ON EMERGENCY LIGHT AT ROW 9. OPS CHECK GOOD AS PER M M 33-53-00. (M) 2 L 7 2 4F RT A6WE 1999061100658 19990611 00658 WP 1999 6 11 ORJA99175 1 19990518 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP PAX DOOR INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 821RA 49931 RNO - EMERGENCY LIGHT IN FORWARD PASSENGER DOORWAY INOPERATIVE. REMOVED AND REPLACED LIGHT PER MM 33-53-00, OPS CHECK N ORMAL. (M) 2 L 7 2 4F A6WE 1999061100659 19990611 00659 NM 1999 6 11 P2EA99195 1 19990525 A 2913 6502506 PUMP BOEING 737 737281 138448P NM 'A' HYD SYSTEM LEAKING A P2EA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 219US 184007AK 20414 PIT - FLT 588 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. TOTAL LOSS OF SYSTEM 'A' HYDRAULICS. FOUND NR 2 ENGINE SYST EM 'A' HDYRAULIC PUMP SHAFT SEAL BLOWN. REPLACED NR 2 (SYSTEM 'A') ENGINE HYDRAULIC PUMP PER MM 29-11-31A. OPERATION A ND LEAK CHECKS OK. (M) 2 L 7 2 4F A16WE 1999061100660 19990611 00660 NM 1999 6 11 P2EA99192 1 19990512 A 5755 65799507 SKIN BOEING 737 737205 NM NR 8 SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, THE NR 8 SPOILER WAS FOUND DELAMINATED. REPAIRED PER COOPESA EO NR COO-CMP-3-57-299-99 DATED MAY 18, 1999. (M) 2 L 7 2 4F A16WE 1999061100661 19990611 00661 NM 1999 6 11 P2EA99191 1 19990512 A 5755 65799507 SKIN BOEING 737 737205 NM SPOILER DELAMINATION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, THE NR 2 SPOILER, WAS FOUND DELAMINATED. REPAIRED PER COOPESA EO NR COO-CMP-3-57-300-99, DATED MA Y 18, 1999. (M) 2 L 7 2 4F A16WE 1999061100662 19990611 00662 NM 1999 6 11 99ZZZM347 1 19990528 A 2120 AIR DIST BOEING 727 7272B7 138407L NM COCKPIT ODOR A AMTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 11 760AT 21954 DURING DESCENT, THE CREW NOTICED ELECTRICAL FUMES AND SMELL IN COCKPIT. CHECKED FLUORESCENT LIGHT BALLASTS FOR COCKPIT GLARESHIELD AND F/E'S OVERHEAD PANEL CHECKED OK. OPERATED ALL COCKPIT LIGHTS FOR OVER AN HOUR, NO PROBLEMS NOTED. (M) 2 L 7 3 4F A3WE 1999061100663 19990611 00663 CE 1999 6 11 MASA99067 1 19990506 A 5270 WARNING BEECH 1900 1900D 1154162 CE CARGO DOOR ACTIVATED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 110YV UE110 FLT 5344 - PHL-GON - AFTER DEPARTURE FROM PHL, CREW REPORTED THE CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED. CREW DECLARE D AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR AND DEFERRED THE CARGO DOOR ANNUNCIATOR SYSTEM PER MEL 52-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999061100664 19990611 00664 NE 1999 6 11 MASA99074 2 19990512 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 FAILED A MASA C E ABORTED TAKEOFF ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 93ZV UE93 114071GG FLT 6469 - FMN-PHX - PRIOR TO V1, CAPTAIN REPORTED HEARING LOUD NOISES COMING FROM THE NR 2 ENGINE. CAPTAIN ABORTED TAK EOFF AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED THE NR 2 ENGINE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999061100665 19990611 00665 CE 1999 6 11 MASA99075 1 19990110 A 5511 10162000061 SPAR BEECH 1900 1900D 1154162 CE HORIZONTAL STAB CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 6YV UE6 DURING NIGHT MAINTENANCE, FOUND THE HORIZONTAL STABILIZER MAIN SPAR CENTER WEB CRACKED. MAINTENANCE REPAIRED THE CRACKE D WEBBING IAW RO NR B1900D-55-0001. (M) 2 L 7 2 4T RT A24CE 1999061100666 19990611 00666 CE 1999 6 11 MASA99081 1 19990523 A 5270 WARNING BEECH 1900 1900D 1154162 CE CARGO DOOR ACTIVATED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 65YV UE65 FLT 5923 - BFD-PIT - CREW REPORTED THE CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. DECLARED AN EMERGENCY AND DIVERTED TO DUJ, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION WAS DEFERRED PER MEL 52-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999061100667 19990611 00667 CE 1999 6 11 MASA99078 1 19990520 A 1100 12943008521 PLACARD BEECH 1900 1900D 1154162 CE LT/RT EMER EXIT MISSING A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 113YV UE113 FLT 702 - FMN-ABQ - CREW REPORTED THAT THE EMERGENCY EXITS WERE MISSING THE EXTERIOR EMERGENCY EXIT PLACARDS. MAINTENAN CE INSTALLED NEW PLACARDS AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999061100668 19990611 00668 NM 1999 6 11 ASAA9910098 1 19990504 A 5320 6562185504 BEAM BOEING 737 7372Q8C 138448S NM BS 663 CORRDOED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE PASSENGER CABIN FLOOR SUPPORT I BEAM CORRODED ON TOP AND BOTTOM SIDES, BS 663, RBL 45.5 TO 61.0. REPAIRED PER SRM 51-30-2 AND 51-30-3. (M) 2 L 7 2 4F A16WE 1999061100669 19990611 00669 NM 1999 6 11 ASAA9940108 1 19990513 A 5240 GUIDE ARM BOEING 737 7374Q8 NM R1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 PDX - DURING A-CHECK, THE R-1 DOOR HOLD OPEN LEVER WOULD NOT FUNCTION PROPERLY. REPLACED UPPER GUIDE ARM AND DOOR OPERA TED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999061100670 19990611 00670 NM 1999 6 11 ASAA9910097 1 19990504 A 5330 SKIN BOEING 737 7372Q8C 138448S NM BS 422-426 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND EXTERNAL SKIN CENTER LINE BS 422 TO 426 BETWEEN STRINGER 28L AND 28R CRACKED. REPAIRED PER SRM 53-30-3 AND 53-30-4. (M) 2 L 7 2 4F A16WE 1999061100671 19990611 00671 NM 1999 6 11 ASAA9940106 1 19990504 A 5315 65C3394320 FLOORBEAM BOEING 737 737490 1384715 NM BS 344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PHX - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM CORRODED AT STATION 344, LBL 14. REPAIRED PER EA 5310-01682. (M) 2 L 7 2 4F RT A16WE 1999061100672 19990611 00672 NM 1999 6 11 ASAA9940107 1 19990504 A 5347 SEAT TRACK BOEING 737 737490 1384715 NM BS 889 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS BAC1520792 27082 PHX - DURING SI CHECK, FOUND MAIN CABIN LEFT OUTBOARD SEAT TRACK GOUGED AT STATION 889. REPAIRED PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 1999061100673 19990611 00673 WP 1999 6 11 ASAA9980113 1 19990518 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061100674 19990611 00674 WP 1999 6 11 ASAA9980112 1 19990517 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 975AS 53451 SMF - AFTER ARRIVAL OF FLIGHT 384, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED WIRING TO LIGHT SOCKET IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061100675 19990611 00675 WP 1999 6 11 ASAA9980111 1 19990516 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 2604 49232 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061100676 19990611 00676 WP 1999 6 11 ASAA9980110 1 19990514 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061100677 19990611 00677 WP 1999 6 11 ASAA9980109 1 19990513 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP ROW 12 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, ONE WHITE EMERGENCY FLOOR TRACK LIGHT AT ROW 12 WAS FOUND INOPERATIVE. REPLACED LAMP MO DULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061100678 19990611 00678 NE 1999 6 11 TWAA9908101 2 19990607 A 7314 3782017 PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT TO TAKEOFF 1 CE 05 990Z 47136 2104 THE RT ENGINE SHUT ITSELF DOWN DURING TAKEOFF. THE FLIGHT RETURNED TO SDF. REPLACED THE ENGINE FUEL PUMP DUE TO SHEARE D SHAFT. ALSO, REPLACED THE FUEL CONTROL PRECAUTIONARY, (P/N 743602-5). CHECK-C 9-21-98 STL. 2 L 7 2 4F 4 F A6WE E2EA 1999061100679 19990611 00679 NM 1999 6 11 HNAA9900066 1 19990608 A 3231 83231027001 MECHANISM DHC DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR OUT OF ADJUST A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 931HA 132 AFTER GEAR RETRACTION LEFT GEAR DOOR LIGHT AND DOOR OPEN LIGHT. CYCLED GEAR AND LIGHT STILL ON BUT DOOR CLOSED, SLOWLY FELL OPEN AGAIN. ADJUSTED LEFT HAND MAIN LANDING GEAR FORWARD DOOR ROD. 2 H 7 2 4T RT A13NM 1999061100680 19990611 00680 WP 1999 6 11 AT9900433 1 19990604 A 5320 PAN DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE SUB FLOOR PAN AND DOUBLER AT BS 200 RBL 45 CORRODED. GAINED ACC ESS AS REQUIRED, REMOVED SUB FLOOR PAN AND DOUBLER. CUT OUT, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED DOUBLER A ND PAN IAW DC9 SRM 53-01 FIG 3, 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999061100681 19990611 00681 WP 1999 6 11 AT9900434 1 19990530 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 917 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION ON THE MAIN CABIN ATTACHED WEB AT BS 917 L-18L. REMOVED C ORROSION, FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-20-1, 51-10-3 AND 51-30-0. 2 L 7 2 4F A6WE 1999061100682 19990611 00682 WP 1999 6 11 AT9900435 1 19990525 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 823 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 SHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE MAIN CABIN LEFT LONGERON NR 18 AT BS 823 ATTACHED WEB CORRODED. R EMOVED CORROSION, FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-20-1, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999061100683 19990611 00683 WP 1999 6 11 AT9900436 1 19990604 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 180 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FLOOR SUPPORT AT BS 180 CORRODED AND CRACKED. REMOVED FLOOR SUP PORT, FORMED, HEAT TREATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, 51-10-2 AND 5 1-30-2. 2 L 7 2 4F A6WE 1999061100684 19990611 00684 WP 1999 6 11 AT9900437 1 19990526 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-408 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND MULTIPLE SKIN DAMAGE (DENTS) ON THE RIGHT SIDE AT BS 229-408 L-18-26 R. REMOVED AND REPLACED SKIN DAMAGE SECTION. A NEW SPLICE DOUBLER SECTION WAS INSTALLED IAW DC9 SRM 51-20-0, 51-30-1, 51-30-1, 51-30-2, 51-10-4, 51-30-5, 51-10-3 AND TIMCO RES NR 07921 AND EO NR 99-115. 2 L 7 2 4F A6WE 1999061100685 19990611 00685 WP 1999 6 11 AT9900438 1 19990429 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 580 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE INTERNAL DOUBLER AT BS 580 STRINGER 30. REMOVED LEADING EDGE WI NG TO FUSELAGE FILLET PANELS, BLEED AIR DUCTS, END CAPS AND FRAMES FOR ACCESS. REMOVED CORRODED DOUBLER, FABRICATED DOU BLER, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED DOUBLER AND ALL PREVIOUSLY PARTS REMOVED FOR ACCESS IAW DC9 SRM 53-04 FIG 43, 51-10-4, 51-10-3, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999061100686 19990611 00686 NM 1999 6 11 PCAA9900017 1 19990608 A 5542 85540002001 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 809EX 11591 3727 302 BGM-DURING PERFORMANCE OF AN A1 INSPECTION THE TRAILING RUDDER WAS FOUND CRACKED IN TWO PLACES. MAINTENANCE PERFORMED R EPAIRS IAW BOMBARDIER RD8-55-158. 2 H 7 2 4T RT A13NM 1999061100687 19990611 00687 EU 1999 6 11 JBXA9900087 1 19990609 A 2450 POWER SYS FOKKER F28 F28MK0100 4990807 EU ELECTRICAL SYS MALFUNCTIONED A JBXA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 05 108ML 11484 CREW REPORTED, IN FLIGHT LOST LANDING GEAR DOWN INDICATION. ALSO, LIGHTS INOP ON LEFT HAND EFIS CONTROL PANEL, SELECTOR LIGHT INDICATION ON NR 1 COM CONTROL PANEL AND ADF CONTROL PANEL. EVERYTHING RETURNED TO NORMAL WHEN EXTERNAL POWER WA S CONNECTED. RAN BOTH ENGINES CHECKED ELECTRICAL POWER DISTRIBUTION GOOD. TRANSFERRED ELECTRICAL POWER FROM GEN 1 TO G EN 2 AND APU AND EXT POWER. ALL POWER SWITCHING NORMAL. INSPECTED GEAR INDICATION LIGHT SOCKETS, CHECK GOOD. WORK PER FORMED IAW AMM 24-25-00 AND 33-10-00. 2 L 7 2 4F RT 1999061100688 19990611 00688 NM 1999 6 11 RAAA99B1007 1 19990606 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 22 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999061100689 19990611 00689 NM 1999 6 11 RAAA99B1008 1 19990606 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM RT EMER EXIT DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999061100690 19990611 00690 NM 1999 6 11 CALA9900657 1 19990607 A 3350 P4010021 BATTERY DME BOEING 727 727224 1384076 NM PASSENGER DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND BOTH FORWARD ENTRY EMERGENCY FLASHLIGHTS WITH CHARGE LIGHTS NOT BLINKING. THE BATTERIES FOR BOTH FLASH LIGHTS WERE REMOVED AND REPLACED IAW MM 25-60-00. 2 L 7 3 4F A3WE 1999061100691 19990611 00691 WP 1999 6 11 CALA9900658 1 19990608 A 5230 BEAM DOUG DC9 DC982 3022082 WP BS 617-674 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND MID CARGO DOOR BEAM CORRODED AT FS 617-674 LONGERON 28R. THE MID CARGO DOOR BEAM WAS REMOVED AND REPLA CED IAW SRM 51-30-05. 2 L 7 2 4F A6WE 1999061100692 19990611 00692 NM 1999 6 11 UPS99229774 1 19990529 A 5311 FRAME BOEING 727 727247 138408F NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON FRAME BS 560 WL 215 RBL 64. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. COMPLETE STANDARD FORMED SECTION REPAIR PER SRM 51-40-03, SRM 51-10-2 AND SRM 51-40-3. 2 L 7 3 4F A3WE 1999061100693 19990611 00693 NM 1999 6 11 UPS99229776 1 19990607 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SHEAR TIE BS 1130 RBL 5 WL 148. REPLACED PER SRM 51-10-2, SRM 51-10-1. 2 L 7 3 4F A3WE 1999061100694 19990611 00694 NM 1999 6 11 UPS99229778 1 19990607 A 5314 KEEL BEAM BOEING 727 727247 138408F NM BS 760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON KEEL BEAM AT BS 760, RBL 7, LBL 7 WL 148. REPLACED PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999061100695 19990611 00695 NM 1999 6 11 UPS99229781 1 19990607 A 5753 651925012 TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK IN REAR SPAR MAIN BOLT HOLE. REMOVED AND REPLACED N R 7 FLAP TRACK. 2 L 7 3 4F A3WE 1999061100696 19990611 00696 NM 1999 6 11 UPS99229782 1 19990526 A 5320 69436834 SHEAR TIE BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) ON SHEAR TIES FWD AND AFT SIDE BS 720A FRAME BETWEEN STR 25 AND 26 RT CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW PART PER SRM 51-30-2 PG 2 AND 3. 2 L 7 3 4F A3WE 1999061100697 19990611 00697 NM 1999 6 11 UPS99229783 1 19990529 A 5311 FRAME BOEING 727 727247 138408F NM BS 540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, POSSIBLE CRACK AT FASTENER HOLE IN FRAME BS 540 WL 215 RBL 64. REMOVED DAMAGED AREA IN FRAME, FABRI CATED REPAIR PARTS AND INSTALLED PER SRM 51-40-3, 51-30-2, 51-10-2. 2 L 7 3 4F A3WE 1999061100698 19990611 00698 NM 1999 6 11 UPS99229784 1 19990605 A 5230 SKIN BOEING 727 727247 138408F NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION (C53-111-02.00-02) EMINATING FROM UNDER 3 RIVNUTS ON INNER SKIN OF AFT CARGO DOOR 11 FROM BOTTOM OF DOOR AFT OF FWD FRAME 10, 18 AND 35. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS ON INNER SKIN OF AFT CARGO D OOR AT 35 FROM FWD FRAME AND 11 ABOVE BOTTOM OF DOOR. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS, PER SRM 51-10-6, 51-10-2, 51-30-2 AND 52-00-02. 2 L 7 3 4F A3WE 1999061100699 19990611 00699 NM 1999 6 11 UPS99229785 1 19990529 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 444-457 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 444 TO BS 457 LBL 45. SEAT TRACK FLANGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53-10-5. INSTALLED NEW SEAT TRACK PER MM SRM 53-10-5. 2 L 7 3 4F A3WE 1999061100700 19990611 00700 WP 1999 6 11 UPS99829759 1 19990604 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1704-1717 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:N/A, 13.25 INCH CRACK LOCATED AT LONGERON L28 ON SKIN OF AIPLANE FS 1704 TO FS 1717 (FOR AND AFT). *S/D * REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS IAW DC8 SRM 53-2-1 FIG 4. INSTALLED PARTS IAW SRM 53-2-1, 51-1-23 D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999061100701 19990611 00701 WP 1999 6 11 UPS99829772 1 19990607 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:N/A, DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PA CK, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999061100702 19990611 00702 WP 1999 6 11 UPS99829773 1 19990608 A 5270 H206B SWITCH DOUG DC8 DC873F 302199F WP PASSENGER DOOR FAILED A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 813UP 46059 INSPECTION TYPE:ASN, CABIN DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. ACARS SENSORS (MAIN CREW) CONFIRMED DOOR. AIRCRAFT M AINTAINED DIFFERENTIAL PRESSURIZATION. DOOR APPEARS CLOSED AND SECURE. REPLACED LEFT AFT SERVICE DOOR MICROSWITCH AND CHECKED PER 52-70. 2 L 7 4 4F RT 4A25 1999061100703 19990611 00703 WP 1999 6 11 UPS99829775 1 19990513 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C1, FWD PIT FS 600 L36 CORROSION ON SKIN DOT 0441. REMOVED FASTENERS FOR ACCESS, REMOVED CORROSION, ALO DINED AND PRIMED IAW UPS DC8 SRM 51-1-8. FASTENERS TO BE INSTALLED ON UPS N/R 936077. 2 L 7 4 4F RT 4A25 1999061100704 19990611 00704 WP 1999 6 11 UPS99829777 1 19990512 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C1, CORROSION ON LONGERON 31R ACCESSORY COMPARTMENT STA 660. FABRICATED REPAIR ANGLE IAW REO 06502, ALO DINED AND PRIMED IAW DC8 S RM 51-1-8, INSTALLED REPAIRED ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999061100705 19990611 00705 WP 1999 6 11 UPS99829779 1 19990522 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C1, FWD PIT FS 600 L36 CORRODED. FABBED SPLICE SHIMS IAW TIMCO REO-06533, ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8, INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D AND TIMCO REO-06533. 2 L 7 4 4F RT 4A25 1999061100706 19990611 00706 WP 1999 6 11 UPS99829780 1 19990513 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:C1, FWD PIT FS 640 L33L CORROSION ON WALL TO FRAME AND ATTACH ANGLE DOT N 619. CLEANED CORROSION, CORRO SION BEYOND LIMITS, FABRICATED REPAIR ANGLE PER DC8 DWG 56104-16 ANGLE PER DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999061100707 19990611 00707 EU 1999 6 11 99FDEA00207 1 19990606 A 2130 RELAY AIRBUS 310 A310222 3930315 EU LT & RT MLG INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 419FE 345 RECEIVED NR 2 SYS OUTFLOW VALVE FAULT LIGHT. REGULATOR NR 2 OFF SYS NR 1 CK. PROBLEM COULD NOT DUP ON GROUND. PRECAUT IONARY REPLACED RT AND LT MLG RELAY 60GB AND 45GB, TERMINAL BLOCK 158VT NR 1. TEST PER MM 21-31-00 SAT. 2 L 7 2 4F RT A35EU 1999061100708 19990611 00708 EU 1999 6 11 99FDEA00208 1 19990606 A 3411 PITOT SYS AIRBUS 300 A300F4605R 3930327 EU LEFT FOD A FDEA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 25 674FE 781 REJECTED T/O AT ABOUT 110 KTS DUE TO 30 KTS DIFFERENCE IN F/O CALLED 80 KTS DURING T/O ROLL. REMOVED BUG FROM CAPT'S PI TOT SYSTEM. CK GOOD PER MM 34-10-00. 2 L 7 2 4F RT A35EU 1999061100709 19990611 00709 NM 1999 6 11 99UAL900295 1 19990530 A 2150 PACK ALLIEDSIGNAL 8012401 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RIGHT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 302UA 87599218 23643 THE RIGHT SIDE PRESSURIZATION PACK TRIPPED OFF AND THE AIRCRAFT CABIN ALTITUDE RAPIDLY INCREASED. *S/D* FOUND RIGHT PA CK TURBOFAN MAKING LOUD NOISE. REPLACED RIGHT PACK TURBOFAN. REF MRR 99UAL900306 FOR SUBSEQUENT MAINTENANCE ACTIONS. 2 L 7 2 4F 4 F RT A16WE E2GL 1999061100710 19990611 00710 NE 1999 6 11 99UAL900296 2 19990529 A 7321 FUEL CONTROL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE MALFUNCTIONED A UALA O OTHER A FLAME/FIRE TO TAKEOFF 1 WP 29 602UA 21863 707519 RT ENG SURGE ON TAKEOFF WITH FLAMES REPORTED FROM TAILPIPE AND AUDIBLE BANG. REDUCED POWER AND STABILIZED EGT PEAK 774C FOR 13. FLIGHT CONTINUED TO LAX. *S/D* ACCOMPLISHED SURGE CHECKS PER MM 71- 00-39, NO DEFECTS FOUND. REPLACED FUEL CONTROL AND FUEL PUMP PRECAUTIONARY, ACCOMPLISHED EVBC TRIM, NEEDED NO ADJUSTMENT, 3.0 BLEED VALVE ADJUDTED FROM 1.0 TO 1.04 INCHES AT 1.188 EPR. 2 L 7 2 4F 4 F RT A1NM E3NE 1999061100711 19990611 00711 NM 1999 6 11 99UAL900297 1 19990528 A 4940 519858 STARTER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE APU DEFECTIVE A UALA A UNSCHED LANDING H K ELECT. POWER LOSS-50 PC FLUID LOSS TO TAKEOFF 1 WP 29 602UA 21863 62043 DIVERTED TO SLC DUE TO AN APU OIL LEAK. NR 1 GENERATOR WAS PREVIOUSLY DEFERRED. UPON OPENING APU COWLING FOUND A LARGE AMOUNT OF OIL INSIDE. *S/D* FOUND OIL LEAKING THRU STARTER MOTOR. REPLACED STARTER MOTOR WITH UPGRADED DASH 7. ALSO , REPLACED GEARBOX SHUTOFF VALVE AS A PRECAUTION FOR HIGH OIL CONSUMPTION. AFTER STARTER REPLACEMENT, APU LEAK CHECK AN D OPERATIONAL WERE GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 1999061100712 19990611 00712 NE 1999 6 11 99UAL900298 2 19990529 A 7261 OIL TUBES AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE LEAKING A UALA K NONE A K P FLAME/FIRE FLUID LOSS NO WARNING INDICATION IN INSP/MAINT 1 WP 29 430UA 568 V10143 ON ACFT WALK AROUND, FOUND ACTIVE FIRE IN NR 1 ENGINE LOCATED NEAR LAST TURBINE DISK. FIRE SEEMS TO BE FED BY A SMALL O IL LEAK OF ABOUT 20 TO 25 DROPS. AT LOW POWER SETTINGS OIL SCAVENGE PUMP SOMETIMES DOES NOT SCAVENGE ADEQUATELY FROM TH E NUMBER 5 BEARING COMPARTMENT, ALLOWING OIL TO ACCUMULATE AND SPILL INTO EXHAUST CASE AND TAILPIPE. COA BEING PROTOTYP ED TO CHANGE PLUMBING OF NR 5 SCAVENGE OIL LINE TO IMPROVE SCAVENGE CAPACITY. THIS ENGINE WAS REMOVED FOR OTHER CAUSE A ND WILL RECEIVE PLUMBING MOD DURING SHOP VISIT. 2 L 7 2 4F 4 F RT A28NM E40NE 1999061100713 19990611 00713 NM 1999 6 11 99UAL900299 1 19990601 A 5720 65B0818632 BOLTS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT MLG LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 172UA 24363 RIGHT WING LANDING GEAR BEAM OUTBOARD END GATE FITTING SUPPORT ASSEMBLY (P/N 65B08186-30) SHOWED SIGNS OF MOVEMENT DUE T O BROKEN SEALANT. INSPECTION REVEALED TWO UPPER BOLTS (P/N BACB30US10K54) AND LOWER BOLTS (P/N BACB30PE10C45W) WERE LOO SE. THE BOLTS ATTACH THE GATE SUPPORT FITTING TO THE UPPER AND LOWER CHORDS OF THE WING REAR SPAR. CAUSE: LOOSE BOLTS FROM TIME SINCE NEW. VISUALLY INSPECTED AREA, RE-TORQUED BOLTS AND RESEALED AREA. 2 L 7 4 4F 4 F RT A20WE E24NE 1999061100714 19990611 00714 1999 6 11 99UAL900300 4 19990514 A 2565 7A12403 TUBE B F GOODRICH 7A123831 BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE L 1 DOOR SLIDE TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 159UA G149 21140 EVACUATION SLIDE ON DOOR 1 LEFT WAS DEPLOYED DURING LAX MAINTENANCE CHECK. WITHIN TWENTY MINUTES OF DEPLOYMENT SLIDE WE NT FLAT. *S/D* UNIT WAS SENT TO VENDOR FOR EVALUATION AND REPAIR. VENDOR FOUND A .75 INCH PUNCHER IN THE LOWER TUBE T HAT DEVELOPED INTO A 3 INCH TEAR. UNIT IS BEING REPAIRED BY THE VENDOR. 2 L 7 4 4F 4 F A20WE E20EA 1999061100715 19990611 00715 1999 6 11 99UAL900301 4 19990531 A 3442 675230435 CIRCUIT BREAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 7260U 21407 WHEN WEATHER RADAR TURNED ON GYRO AND STEER FLAGS VISIBLE. RETURNED TO ORD. *S/D* REPLACED CIRCUIT BREAKER C833. 2 L 7 3 4F 4 F A3WE E2EA 1999061100716 19990611 00716 NM 1999 6 11 99UAL900302 1 19990601 A 7603 NS67984W LINKAGE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE DISCONNECTED A UALA C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK W INADEQUATE Q C TO TAKEOFF 1 WP 29 7264U 21411 700134 NR 3 ENGINE WENT TO UNCONTROLLABLE HIGH POWER ON TAKEOFF. ABORTED TAKEOFF AT 60 KNOTS. ENGINE SHUT DOWN WITH SHUT OFF LEVER. *S/D* MECHANICAL ERROR. TORQUE AND SAFETY OF NUT AT FUEL CONTROL THROTTLE LEVER WAS NOT ACCOMPLISHED, ALLOWIN G CONTROL LINKAGE TO BE DISCONNECTED. AIRCRAFT WAS RETURNED TO SERVICE AFTER ACCOMPLISHING PROPER INSTALLATION OF HARDW ARE, FUEL CONTROL UNIT TRIM, AND ENGINE FUNCTIONAL RUN. 2 L 7 3 4F 4 F A3WE E2EA 1999061100717 19990611 00717 NM 1999 6 11 99UAL900303 1 19990602 A 2613 1061096217 OVERHEAT DET BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU COMPT SHORTED A UALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 WP 29 947UA 26688 THE FIRE WARNING FOR THE APU ILLUMINATED. *S/D* CLIMBING THROUGH 10,000 FT, APU FIRE LIGHT ILLUMINATED ON P8-1 PANEL. FLT CREW DISCHARGED APU FIRE BOTTLE AND THE A/C LANDED WITHOUT INCIDENT. VISUALLY INSPECTED APU AND FOUND NO SIGNS OF FIRE, FLUID LEAKS, OR OBVIOUS FAULTS. FURTHER TROUBLESHOOTING OF APU FIRE WARNING SYSTEM FOUND APU TAIL PIPE OVERHEAT D ETECTOR M717 SHORTING TO GROUND AND READING HIGH RESISTANCE BETWEEN PIN C TO A AT D4934P. REPLACED M717 DETECTOR AND HA RNESS ASSY FOR M717. APU FIRE WARNING SYS CHECKED GOOD, AND THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999061100718 19990611 00718 WP 1999 6 11 99UAL900304 1 19990603 A 5230 SEAL DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CARGO DOOR POPPED A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 1849U 46939 AIRCRAFT HAD ABNORMAL INFLIGHT NOISE-VIBRATION. SEE AIRCRAFT LOG FOR DETAILS. AIR NOISE ON RIGHT SIDE OF CABIN BETWEEN 28 & 35. *S/D* AREA CHECKED AND FOUND 12 INCHES OF SEAL POPPED ON THE CENTER CARGO COMPARTMENT PIT DOOR. SEAL REINST ALLED AND DOOR OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A22WE E23EA 1999061100719 19990611 00719 NE 1999 6 11 99UAL900305 2 19990502 A 7230 COMPRESSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STALLED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 7257U 21404 700443 ABORTED TAKEOFF AT BETWEEN 80 AND 100 KNOTS DUE TO A COMPRESSOR STALL ON NR 2 ENGINE. FLAMES REPORTED FROM REAR OF ENG INE. CROSS WINDS 27 TO 45 KNOTS. *S/D* STRONG CROSS WIND WAS THE CAUSE OF THE STALL. THE AIRCRAFT RETURNED TO SERVIC E AFTER FINDING NO ABNORMALITIES DURING THE ENGINE INSPECTION REQUIRED BY MM. 2 L 7 3 4F 4 F A3WE E2EA 1999061100720 19990611 00720 WP 1999 6 11 ABXA9900411 1 19990507 A 5312 5910130505 BULKHEAD JAMB DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND CRACK IN UPPER RIGHT CORNER OF AFT PRESSURE BULKHEAD DOOR. REPAIRED IAW ABX REA D953-28299. 2 L 7 2 4F A6WE 1999061100721 19990611 00721 WP 1999 6 11 ABXA9900412 1 19990507 A 5312 5910130505 BULKHEAD JAMB DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND CRACK IN UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD DOOR. REPAIRED IAW ABX REA D953-28299. 2 L 7 2 4F A6WE 1999061100722 19990611 00722 WP 1999 6 11 ABXA9900413 1 19990507 A 5320 49149551 SPLICE DOUG DOUG DC9 DC941 302207N WP BS 939 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LONGERON SPLICE EXFOLIATED AT STATION 939 AND LONGERON 19 LEFT. REPLACED SPLICE IAW DC9 SRM 51-30 -2. 2 L 7 2 4F A6WE 1999061100723 19990611 00723 WP 1999 6 11 ABXA9900414 1 19990507 A 5312 99119923 BULKHEAD WEB DOUG DOUG DC9 DC941 302207N WP BS 1231 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND CANTED BULKHEAD WEB CORRODED AT STATION 1231. REPAIRED IAW ABX REA D953-28154. 2 L 7 2 4F A6WE 1999061100724 19990611 00724 WP 1999 6 11 ABXA9900415 1 19990514 A 5320 D0489835 WEB DOUG DOUG DC9 DC941 302207N WP BS 1013 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 1013. REPLACED CUSP WEB IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061100725 19990611 00725 WP 1999 6 11 ABXA9900416 1 19990608 A 5230 591014167 PAN DOUG DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03 AND 51-30-1. 2 L 7 2 4F A6WE 1999061100726 19990611 00726 WP 1999 6 11 ABXA9900417 1 19990607 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932F 3022067 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 904AX 47040 DURING MAINTENANCE PREFLIGHT, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY IAW DC9 MM, OP S CHECKED GOOD. 2 L 7 2 4F A6WE 1999061100727 19990611 00727 WP 1999 6 11 ABXA9900418 1 19990514 A 5320 3925966501 FITTING DOUG DOUG DC9 DC941 302207N WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND LONGERON 25R SPLICE FITTING CRACKED AT STATION 617. REPLACED SPLICE FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061100728 19990611 00728 WP 1999 6 11 ABXA9900419 1 19990514 A 5311 99196043 FRAME DOUG DOUG DC9 DC941 302207N WP BS 985 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND FUSELAGE FRAME STATION 985 EXFOLIATED AT LONGERON 4 AND 5 LEFT. REPAIRED FRAME IAW DC9 SRM 51-10- 3 AND 53-03. 2 L 7 2 4F A6WE 1999061100729 19990611 00729 WP 1999 6 11 ABXA9900420 1 19990514 A 5311 99115173 FRAME DOUG DOUG DC9 DC941 302207N WP BS 180 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND CORROSION ON FRAME STATION 180 AT LONGERON 30. REPAIRED IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999061100730 19990611 00730 WP 1999 6 11 ABXA9900421 1 19990514 A 5320 39259661 FITTING DOUG DOUG DC9 DC941 302207N WP BS 620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND CRACKED LONGERON SPLICE FITTING AT STATION 620 AND LONGERON 24 RIGHT. REPLACED SPLICE FITTING IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 1999061100731 19990611 00731 WP 1999 6 11 ABXA9900422 1 19990507 A 5311 99196043 FRAME DOUG DOUG DC9 DC941 302207N WP BS 984 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 974AX 47623 DURING D-CHECK, FOUND FRAME AT STATION 984 CRACKED BETWEEN LONGERON 16 LEFT AND 17 LEFT. REPAIRED IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999061100732 19990611 00732 WP 1999 6 11 MWEA99326 1 19990608 A 3350 082084 DIODE DOUG DC9 DC932 3022066 WP CABIN DEFECTIVE A MWEA K NONE L NO TEST LD LANDING 1 GL 31 401ME 47133 CABIN EMERGENCY LIGHTS CAME ON WHILE LANDING, UNABLE TO TURN OFF ARM AND CHARGE CIRCUIT BREAKER UNABLE TO RESET. REPLAC ED PEEPLS FLOOR TRACK LIGHTING FWD DIODE ASSY, REPAIRED GROUND STRAP AT SWITCH IN COCKPIT. 2 L 7 2 4F A6WE 1999061100733 19990611 00733 WP 1999 6 11 MWEA99327 1 19990607 A 3350 4TL1110B SWITCH DOUG DC9 DC932 3022066 WP CABIN INTERMITTENT A MWEA K NONE L NO TEST LD LANDING 1 GL 31 401ME 47133 EMERGENCY LIGHTS ILLUMINATED ON LANDING, UNABLE TO EXTINGUISH ARM AND CHARGE CIRCUIT BREAKER WILL NOT STAY SET. REPLACE D INTERMITTANT CABIN EMERGENCY LIGHTS SWITCH. 2 L 7 2 4F A6WE 1999061100734 19990611 00734 1999 6 11 MWEA99328 4 19990609 A 2565 D29985107 SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOOR OUT OF POSITION A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 AFT GALLEY SERVICE DOOR HARD TO OPEN BECAUSE OF SLIDE CASE HITTING DOOR. REPLACED EVACUATION SLIDE. 2 L 7 2 4F RT A6WE 1999061100735 19990611 00735 WP 1999 6 11 MWEA99329 1 19990602 A 5320 5910539501 JAMB DOUG DC9 DC932 3022066 WP GALLEY DOORWAY CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 THE GALLEY SERVICE DOOR JAMB CUTOUT PAN ON AFT SIDE IS CHAFED. MTC FABRICATED AND INSTALLED REPAIR DOUBLER AND STOP. 2 L 7 2 4F A6WE 1999061100736 19990611 00736 WP 1999 6 11 SCNA99079 1 19990606 A 3350 LIGHT DOUG DC10 DC1015 3022118 WP ROW 37 INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 151SY 48295 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY PATH LIGHTING ON THE RIGHT SIDE AT SEAT ROW 37 WAS FOUND TO BE INOPERATIV E. REMOVED AND REPLACED THE EMERGENCY PATH LIGHTING ASSEMBLY AT SEAT ROW 37 ON THE RIGHT SIDE. OPERATIONALLY CHECKS GO OD. 2 L 7 3 4F A22WE 1999061100737 19990611 00737 WP 1999 6 11 SCNA99080 1 19990601 A 3350 LIGHT DOUG DC10 DC1015 3022118 WP EMER EXIT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 154SY 48259 DURING A LINE MAINTENANCE CHECK THE FORWARD CABIN OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AND FOUND A SHORT IN THE WIRING IN THE RIGHT SIDEWALL MID CABIN. OPERATIONALLY CHECKS GOO D. 2 L 7 3 4F A22WE 1999061100757 19990611 00757 SW 1999 6 11 99ZZZX2257 1 19990511 A 5302 407030801101 SKIN BELL 407 407 SW TAILBOOM CRACKED A ALGA J DUMP FUEL O OTHER IN INSP/MAINT 1 SW 03 497AL 1866 53173 53172 DURING DAILY INSPECTION PER BELL ASB 407-99-26, FOUND CRACK IN SKIN AT LEFT FORWARD HORIZONTAL STABILIZER UPPER MOUNT. C RACK STARTS FROM UNDER RIVETED MOUNT AND EXTENDED TO FIRST RIVET. 1 G 7 1 3U O H2SW 1999061100759 19990611 00759 NE 1999 6 11 99ZZZX2259 1 19990512 A 3243 7625001101102 MASTER CYLINDER SKRSKY S76 S76A 8143006 NE BRAKE SYSTEM FAILED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 741SW 091 760070 UPON TOUCH DOWN ON PAD, THE LEFT WHEEL BRAKE FAILED TO HOLD. AIRCRAFT TURNED 45 DEGREES TO THE RIGHT. PILOT ON CONTROL S PUT IN LEFT PEDAL AND PULLED POWER STOP TURN. AIRCRAFT WAS REPOSITIONED ON THE PAD AND SHUT DOWN. 1 G 7 2 3U H1NE 1999061100769 19990611 00769 CE 1999 6 11 99ZZZX2269 1 19990514 A 3241 1313503 BRAKE HYDROAIRE 40433L LEAR 25 25 5170506 CE ANTI-SKID FAILED A KKFA O OTHER O OTHER NR NOT REPORTED 1 GL 23 39CK 005 ANTI-SKID FAILED TO CYCLE ON TOUCH DOWN. REPLACED ALL MAIN WHEEL AND BRAKE ASSEMBLIES WITH SERVICEABLE UNITS. REPLACED THE ANTI-SKID TRANSDUCERS WITH SERVICEABLE UNITS. PERFORMED FUNCTIONAL CHECK OF ANTI-SKID SYSTEM IAW THE LEAR 25 SM. N O RECOMMENATION FOR PREVENTION KNOWN AT THIS TIME. 2 L 7 2 4J A10CE 1999061100771 19990611 00771 1999 6 11 99ZZZX2271 4 19990526 A 6122 9696001115 LINE BEECH 58 58 1152740 CE PROP GOVERNOR BROKEN A BSYA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 9189Q TH148 ON TAKEOFF OUT OF CMH, RT ENGINE PROPELLER GOVERNOR LINE BROKE AT FLARE, PROPELLER FEATHERED, AND ENGINE SHUT DOWN. RET URNED TO CMH. REMOVED AND REPLACED UNFEATHERING LINE. OPS CHECKED GOOD. 1 L 7 2 3O 3A16 1999061100773 19990611 00773 EA 1999 6 11 99ZZZX2273 2 19990412 A 8500 CRANKCASE BNORM BN2 BN2A26 1520226 EU LYC O540 O540E4C5 41532 EA ENGINE CRACKED A VLIA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 21 907VL 7793 1833 2192 L1807440A DURING NORMAL DAY OPERATION, PILOT REPORTED RIGHT ENGINE OIL LEAK. DURING VISUAL ISPECTION, FOUND CRACKCASE CRACK BETWE EN CLYINDERS 4 AND 6. RIGHT ENGINE CHANGE. 1 H 7 2 3O 3 O A17EU E295 1999061200001 19990612 00001 NM 1999 6 12 DL777990790 1 19990401 A 3350 LIGHT 331202129 BOEING 777 777232 1385232 NM L4 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 861DA 29952 EXTERIOR EMERGENCY EXIT LIGHT AT L4 DOOR INOP. RELAMPED, CKS OK. 2 L 7 2 4F RT T00001SE 1999061200002 19990612 00002 NM 1999 6 12 DL777990792 1 19990401 A 2131 CONTROLLER 285W02181 BOEING 777 777232 1385232 NM COCKPIT INOPERATIVE A DALA I CABIN DEPRESSURIZATION J WARNING INDICATION DE DESCENT 1 SO 27 861DA 29952 FAA SIMULATION, BOTH AUTO CABIN PRESSURE CONTROLLERS INOP. CHANGED CARD A1 (M23117A1) BAD FAA SIMULATION COMPLETE. 2 L 7 2 4F RT T00001SE 1999061200003 19990612 00003 NM 1999 6 12 DL777990794 1 19990401 A 3350 LENSE 3176976 BOEING 777 777232 1385232 NM 3R DOOR MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 861DA 29952 FAA SIMULATION, MCO DOOR 3R EXTERIOR LIGHT LENS MISSING. REPLACED LENS ASSY, MCO REMOVED FAA SIMULATION COMPLETE. 2 L 7 2 4F RT T00001SE 1999061200004 19990612 00004 NE 1999 6 12 99UAL900215 2 19990417 A 7200 ENGINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 2 MALFUNCTIONED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 163UA 21353 685696 ELECTRICAL OVERHEAT SMELL IN COCKPIT DESCENDING THRU 24,000 FT, NO SMOKE. SMELL DISSIPATED, THEN RETURNED ON ADDING POW ER LATER IN DESCENT. *S/D* FOUND OIL RESIDUE ON NR 1 ACM. REPLACED ACM, NO OIL LEAKS FOUND. INVESTIGATION REVEALED ACM INGESTED FOD, NO DAMAGE FOUND, THE OIL SEALS WERE INTACT. A 2ND ACM WAS REMOVED ON 5/3. THE ACM WAS DISASSEMBLED A ND TESTED, NO LEAKS FOUND. ACM'S WERE NOT THE CAUSE OF THE SMELL. THE NR 2 MAIN ENG WAS REPLACED. AFTER REPLACEMENT O F 2 ACMS, 2 PACK BURNOUTS, SMELL STILL EXISTED, AFTER NR 2 ENGINE REPLACEMENT THE OIL SMELL DISAPPEARED. THE NR 2 ENGIN E WAS LIKELY THE CAUSE OF THE OIL SMELL. 2 L 7 4 4F 4 F A20WE E20EA 1999061200005 19990612 00005 NE 1999 6 12 DL76L990830 2 19990401 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 1200K 5310 28457 727775 FOUND METAL ON NR 3 BEARING CHIP DETECTOR. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999061200007 19990612 00007 WP 1999 6 12 RRXA991015 1 19990527 A 7910 O RING DOUG DC8 DC873F 302199F WP OIL CAP LEAKING A RRXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 831AL 46146 NR 4 ENG OIL QTY WENT TO ZERO IN FLT, OIL PRESSURE FLUCTUATED FROM 13 TO 20 PSI. SHUT DOWN ENGINE FOR PRECAUTION. WIND MILLING OIL AT 4PS. REMOVED AND REPLACED O-RING ON CAP. SERVICED OIL, 13 QUARTS. NR 4 ENG OPS CHECKS GOOD PER CFM MM 71-00. 2 L 7 4 4F RT 4A25 1999061200008 19990612 00008 WP 1999 6 12 RRXA991016 1 19990531 A 7910 O RING DOUG DC8 DC873F 302199F WP OIL CAP LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 603AL 46003 DURING CLIMB-OUT, NR 1 ENG OIL QUANTITY DROPPED TO 4 QTS. OIL PRESS FLUCTUATE AT 30-35 PSI, OIL TEMP 80DEG C. PULLED N R 1 THROTTLE TO IDLE, OIL QUANTITY CONTINUED TO 3QTS AND STEADY. DUMPED FUEL TO MAX LANDING WEIGHT AND RETURNED TO KFLL . UPON INSPECTION FOUND CUT OIL CAP O-RING. REPLACED O-RING, SERVICE ENGINE OIL TANK. NO LEAKS ON ENG RUN UP. 2 L 7 4 4F RT 4A25 1999061200009 19990612 00009 WP 1999 6 12 MWEA99320 1 19990604 A 3520 90002207712 PRESS REGULATOR DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A MWEA G O2 MASK DEPLOYED O OTHER DE DESCENT 1 GL 31 502ME 48132 ON DESCENT THE CABIN PRESSURE CLIMBED TO 10,000 FEET AND CREW HAD TO MANUALLY DEPLOY MASKS. MTC REMOVED AND REPLACED RI GHT WATER SEPARATOR SOCK AND OXYGEN BOTTLE PRESSURE REGULATOR. 2 L 7 2 4F A6WE 1999061800006 19990618 00006 1999 6 18 CA990219022 4 19990121 A 2230 COMPUTER AIRBUS A319 A319114 NM AFCS FAILED W H DEACTIVATE SYST/CIRCUITS R PARTIAL RPM/PWR LOSS DE DESCENT 1 CA (CAN) ON DESCENT WITH AUTO THROTTLE DISCONNECTED, THRUST LOCK APPEARED, UNABLE TO REGAIN ANY ENGINE CONTROL WITH THROTT LES. TAKE-OFF GO-AROUND SELECTED TWICE. AFTER 15 SECONDS, THRUST CONTROL REGAINED. BOTH FLIGHT MANAGEMENT AND GUIDAN CE COMPUTERS REPLACED. 2 L 7 2 4F RT A28NM 1999061800007 19990618 00007 EU 1999 6 18 CA990308024 1 19990210 A 2897 WIRE AIRBUS 320 A320211 3930320 EU RT WING SHORTED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) RIGHT WING NR 1 FUEL BOOST PUMP ELECTRICAL SUPPLY WIRES FOUND ARCING AGAINST WING PLANK CAUSING SIGNIFICANT MATERI AL LOSS IN WING STRUCTURE AND DAMAGE TO WIRE INSULATION. 2 L 7 2 4F RT A28NM 1999061800008 19990618 00008 NM 1999 6 18 CA990308028 1 19990216 A 5230 VALVE AIRBUS A319 A319114 NM CARGO DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UPON OPENING C1 CARGO DOOR, DOOR RAPIDLY OPENED DUE TO PRESSURE TRAPPED IN DOOR ACTUATOR EXTENSION CHAMBERS. REPL ACED C1 DOOR SELECTOR VALVE. REFER TO OPERATOR INFO TELEX A320/321, SE-E/999.0048/96/PP APRIL 96. 2 L 7 2 4F RT A28NM 1999061800009 19990618 00009 NM 1999 6 18 CA990310009 1 19990129 A 3230 574205 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 15356 181 PCE120658 (CAN) LANDING GEAR DID NOT EXTEND WHEN SELECTED, ALTERNATE SYSTEM USED. LANDING GEAR SOLENOID VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999061800012 19990618 00012 EA 1999 6 18 CA990318042 1 19990306 A 2120 6411191 COUPLING AIRESRCH 22016004 CNDAIR CL601 CL6012A12 1900303 EA ACU OVERHEATED W E ENGINE SHUTDOWN M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 7432 (CAN) AFTER ENGINE START, RIGHT ACU FAIL LIGHT ILLUMINATED. CABIN AREA FILLED WITH SMOKE, A/C EVACUATED/SECURED. RIGHT FLEX COUPLING FAILED DUE TO OVERTEMP. 400 DEGREE SWITCH FOUND TO TRIP AT 590 DEGREES. SEE SDR CA990318043 FOR NOTES ON INVESTIGATION. 1 L 7 2 4F RT A21AE 1999061800013 19990618 00013 EA 1999 6 18 CA990318043 1 19990312 A 2120 1173T155 SWITCH CNDAIR CL600 CL600* EA ACU FAILED W K NONE M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 6490 (CAN) AIRCRAFT ON RAMP WITH ACU ON, AIRCRAFT FILLED WITH SMOKE. RIGHT ACU 400 DEGREE SWITCH FOUND OUT OF TOLERANCE, 30 0 DEGREES HIGH. NO INSPECTION REQUIREMENT AGAINST SWITCH. SEE SDR CA990318042 FOR SIMILAR ACTION. 2 L 7 2 4F RT A21EA 1999061800014 19990618 00014 EU 1999 6 18 CA990330035 1 19990307 A 2450 2955T1007 PDU AIRBUS 330 A330202 3930316 EU E/E BAY MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 15736 (CAN) PDU UNITS FOUND RUNNING CONTINUOUSLY WITH BURNING SMELL AND SPARKING. PDU DISCONNECTED. 2 L 7 2 4F RT A46NM 1999061800015 19990618 00015 EU 1999 6 18 CA990330036 1 19990218 A 2450 1231003 PDU AIRBUS 330 A330202 3930316 EU E/E BAY FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 22080 (CAN) PDU UNIT FOUND SMOKING, ELECTRICAL CONNECTOR DISCONNECTED, AIRCRAFT FLOWN TO MAINTENANCE BASE UNDER MEL. 2 L 7 2 4F RT A46NM 1999061800017 19990618 00017 WP 1999 6 18 CA990330063 1 19990312 A 4920 APU LKHEED 1011 10113853 5265020 WP APU BAY FAILED W F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 CA (CAN) FLAME OBSERVED COMING FROM APU EXHAUST DUCT, NO INDICATION IN COCKPIT. GROUND CREW ACTIVATED REMOTE FIRE EXTINQUI SHER SWITCH, DISCHARGING BOTTLES. APU AND COMPARTMENT INSPECTED WITH NO EVIDENCE OF FIRE OR DAMAGE. BOTTLES REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A23WE 1999061800021 19990618 00021 SW 1999 6 18 CA990430021 1 19990423 A 3230 2755001175 HINGE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT MLG DOOR DAMAGED W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA P54183 (CAN) RIGHT MLG WOULD NOT EXTEND. AFTER APPROXIMATELY 150 ATTEMPTS, THE GEAR EXTENDED INTO A DOWN AND LOCKED POSITION. INVESTIGATION REVEALED THAT THE MISALIGNMENT OF THE INBOARD GEAR DOOR DUE TO ELONGATED HOLES IN THE HINGE BRACKETS (P/N 27-55 001-213) CAUSED THE DOOR TO BIND AT THE AFT END PREVENTING THE GEAR FROM EXTENDING. 2 L 7 2 4T 4 T RT A8SW E4WE 1999061800022 19990618 00022 EA 1999 6 18 CA990510023 1 19990505 A 2742 6009230165 ACTUATOR LUCAS CNDAIR CL600 CL600* EA HORIZONTAL STAB FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 7766 1225 249E (CAN) UNIT UPGRADED TO PART C OF SB A600-0645. AFTER 20 HOURS, NR 1 CHANNEL CIRCUIT BREAKER TRIPPED TWICE. RETURNED TO CANADAIR. 2 L 7 2 4F RT A21EA 1999061800023 19990618 00023 EA 1999 6 18 CA990510024 1 19990506 A 2742 6009230165 ACTUATOR LUCAS CNDAIR CL600 CL600* EA HORIZONTAL PITCH FAILED W O OTHER W INADEQUATE Q C IN INSP/MAINT 1 CA 3365 407E (CAN) AFTER INSTALLATION, DURING SYSTEM CHECKS, BOTH LIMIT SWITCHES FOUND UNSAFE. PIF RETURNED TO CANADAIR. 2 L 7 2 4F RT A21EA 1999061800024 19990618 00024 EA 1999 6 18 CA990510025 1 19990506 A 2742 6009230165 ACTUATOR LUCAS CNDAIR CL600 CL600* EA HORIZONTAL STAB FAILED W O OTHER W INADEQUATE Q C IN INSP/MAINT 1 CA 4381 720 287E (CAN) DURING SYSTEM CHECK WITH SINGLE CHANNEL OPERATION, NR 2 CIRCUIT BREAKER TRIPPED. UNIT RETURNED TO CANADAIR. PRE- INSTALLATION FAILURE (PIF). 2 L 7 2 4F RT A21EA 1999061800025 19990618 00025 EU 1999 6 18 CA990521004 1 19990409 A 6520 350A330200004 GEARBOX SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR MAKING METAL W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 7178 1016 M1191 4802TEC (CAN) TAIL ROTOR GEARBOX MAKING DOME SHAPED METAL CHIPS. SUSPECT BEARING FAILURE. ONE OTHER SIMILAR OCCURRENCE REPORTE D. 1 G 7 1 3U 3 U H9EU E19EU 1999061800027 19990618 00027 1999 6 18 CA990521019 4 19990504 A 2565 D31022102 SLIDE A52271002009 AIRBUS 310 A310304 EU RT WING MISADJUSTED W K NONE L NO TEST IN INSP/MAINT 1 CA 17120 3178 UD1119 (CAN) RIGHT OVERWING SLIDE FAILED TO OPEN WHEN TESTED. ACTUATING CABLE EITHER TOO LONG OR TOO SHORT, YET TO BE DETERMIN ED. 2 L 7 2 4F RT A35EU 1999061800034 19990618 00034 SW 1999 6 18 CA990521048 1 19990510 A 2910 2781006003 LINE SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE LT MLG WW CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 880393 (CAN) GEAR DOWN LINE FOUND CRACKED COMING FROM POWER PACK. 2 L 7 2 4T RT A8SW 6 C 3PNE 1999061800037 19990618 00037 WP 1999 6 18 CA990521061 1 19990514 A 2530 02530017M OVEN LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 2 GALLEY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 10432 (CAN) NR 2 AFT GALLEY OVEN STARTED SMOKING, OVEN TURNED OFF AND LATER FOUND TO BE AT FAULT. 2 L 7 3 4F 4 F A23WE E12EU 1999061800040 19990618 00040 WP 1999 6 18 TWAA9908201 1 19990529 A 5753 SKIN DOUG DC9 DC932 3022066 WP RT TE FLAP VANE SCRATCHED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 FOUND THE RT WING T/E FLAP AFT OF MOVAEBLE VANE HAD 2 SCRATCHES .020 TO .050 IN DEEP. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-01, FIG 5, AND ENGR CONCURRENCE A3250A. CHECK-C 8-7-98 MCI. 2 L 7 2 4F A6WE 1999061800041 19990618 00041 WP 1999 6 18 TWAA9908202 1 19990602 A 5312 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND CORROSION WITH POPPED RIVETS AND PILLOWING AT AFT PRESSURE BULKHEAD, STA 996 BETWEEN LON GERON 26L AND 28L. REMOVED CORROSION PER SPM 6-80-01 AND INSTALLED DOUBLER PER SRM 53-03, FIG 24. 2 L 7 2 4F A6WE 1999061800042 19990618 00042 SO 1999 6 18 LR7A9947 1 19990603 A 5230 35361224 CHORD LKHEED 382 382G 526414U SO CARGO DOOR BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING CARGO RAMP ASSY INSPECTION FOR LR7A9946 DAMAGE FOUND RAMP STA 10.4 LOWER AFT CHORD BROKEN AT LBL 24. REMOVED AND REPLACED LOWER CHORD PER SMP 583 51-10-01. 2 H 7 4 4T A1SO 1999061800043 19990618 00043 SO 1999 6 18 LR7A9948 1 19990603 A 5230 ANGLE LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING CARGO RAMP ASSY INSPECTION FOR LR7A9946 DAMAGE FOUND RAMP STA 10 LOWER TEE ANGLE 5 INCH CRACK AT RBL 20. REPAIRE D PER SMP 583 51-140-22. 2 H 7 4 4T A1SO 1999061800044 19990618 00044 SO 1999 6 18 LR7A9949 1 19990603 A 5230 WEB LKHEED 382 382G 526414U SO CARGO DOOR BUCKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING CARGO RAMP ASSY INSPECTION FOR LR7A9946 DAMAGE FOUND RAMP STA 10.4 WEB BUCKLED. REMOVED DAMAGED SECTION OF WEB A ND REPAIRED PER SMP 583 51-140-17. 2 H 7 4 4T A1SO 1999061800045 19990618 00045 NM 1999 6 18 PCAA9900018 1 19990609 A 5542 85540002001 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 807EX 19300 1875 292 BGM-DURING THE PERFORMANCE OF AN A1 INSPECTION THE TRAILING RUDDER WAS FOUND CRACKED. MAINTENANCE REPAIRED IAW BOMBARDI ER RD8-55-155. 2 H 7 2 4T RT A13NM 1999061800046 19990618 00046 NM 1999 6 18 CALA9900659 1 19990604 A 5315 FLOORBEAM BOEING 757 757224 1384958 NM BS 324 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57111 27301 INSPECTION FOUND TOP CHORD OF FLOORBEAM CORRODED AT STA 324, RBL 42. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, PAGES 216-219 AND ECRA 5321-01049. 2 L 7 2 4F RT A2NM 1999061800047 19990618 00047 WP 1999 6 18 CALA9900660 1 19990609 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1437 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND FRAME GOUGED AT FS 1437 BETWEEN LONGERON 2L AND 2R. REPAIRED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999061800048 19990618 00048 WP 1999 6 18 CALA9900661 1 19990609 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1212, LBL 60. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-20-3. 2 L 7 2 4F A6WE 1999061800049 19990618 00049 WP 1999 6 18 CALA9900662 1 19990610 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 295 & 310 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND LT WING SKIN PANEL LOWER SIDE CORRODED AT STA XRS 295 AND 310. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-03, FIGURE 24A. 2 L 7 2 4F A6WE 1999061800050 19990618 00050 NE 1999 6 18 9901971149 2 19990601 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 149US 46758 686157 AT 100 KTS DURING TAKEOFF ROLL, THE NR 1 ENGINE COMPRESSOR STALLED. THE CREW REPORTED A LOUD BANG AND OBSERVED FALLING N1 AND EGT OVERTEMPERATURE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE E NGINE AND FOUND METAL DEBRIS IN THE TAILPIPE. THE AIRCRAFT WAS FERRIED ON TWO ENGINES TO MSP FOR AN ENGINE CHANGE. 2 L 7 3 4F 4 F A22WE E20EA 1999061800051 19990618 00051 NM 1999 6 18 9901986729 1 19990604 A 7830 TR UNIT BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 629US 22388 662715 AT 100 KTS ON TAKEOFF ROLL, THE NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE A IRCRAFT RETURNED TO THE GATE, MAINTENANCE DEFERRED THE REVERSER PER MEL 78-1 AND LOCKED OUT THE REVERSER PER DDG. 2 L 7 4 4F 4 F A20WE E20EA 1999061800052 19990618 00052 WP 1999 6 18 9901999301 1 19990608 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP BRAKE MODULE LOOSE A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 301RC 48054 ON TAKEOFF AFTER RAISING THE LANDING GEAR HANDLE, THE RIGHT HYDRAULIC SYSTEM WENT TO ZERO PRESSURE AND FOUR QUARTS INDIC ATED QUANTITY. FLIGHT CREW DECLARED AN EMERGENCY. ACCOMPLISHED COM PROCEDURES, RETURNED TO MSP, AND LANDED WITHOUT INC IDENT. MAINTENANCE TIGHTENED HYDRAULIC LINE GOING TO THE AUTO BRAKE MODULE AND REPLACED HYDRAULIC SYSTEM FILTERS AS A P RECAUTION. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999061800053 19990618 00053 NM 1999 6 18 9902006634 1 19990607 A 3350 POWER SUPPLY BOEING 747 747227B 1384888 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 634US 22234 DURING LINE CHECK, FOUND C ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999061800054 19990618 00054 WP 1999 6 18 9902019621 1 19990605 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 621NW 47544 EMERGENCY LIGHTS IN COCKPIT WOULD NOT TEST. MAINTENANCE REPLACED BATTERY PACK B5-23 IN FORWARD LAVATORY, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1999061800055 19990618 00055 WP 1999 6 18 9902029154 1 19990608 A 3350 POWER SUPPLY DOUG DC9 DC914 3022034 WP TAIL CONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND TAIL CONE CATWALK AND HANDLE EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999061800056 19990618 00056 WP 1999 6 18 9902039956 1 19990607 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 923RW 47183 DURING LINE MAINTENANCE INSPECTION, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999061800057 19990618 00057 EA 1999 6 18 COMA9960253 1 19990603 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA BS 317 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 TASK 002-53-140-505 FLOOR ANGLE AT SERVICE DOOR ENTRANCE, FS 317 TO FS 342 RBL 42, IS CORRODED. REPLACED ANGLE. 2 L 7 2 4F RT A21EA 1999061800058 19990618 00058 EA 1999 6 18 COMA9960254 1 19990603 A 5315 601R311367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 310-409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 TASK 002-53-140-505 FLOORBEAM CAPS BETWEEN FS 310 TO FS 409 LBL 27, LBL 9, RBL 9 AND RBL 27 ARE CORRODED. REPLACED CORR ODED SECTIONS OF FLOORBEAMS. 2 L 7 2 4F RT A21EA 1999061800059 19990618 00059 EA 1999 6 18 COMA9960255 1 19990603 A 5320 601R3867317 PLATE CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 TASK 002-53-140-505 TOP PLATES, FOR RIBS AT FS 349 BETWEEN FLOORBEAMS ARE CORRODED. FABRICATED AND REPLACED PLATES IAW WVAC EO 601R-53-0052. 2 L 7 2 4F RT A21EA 1999061800060 19990618 00060 EU 1999 6 18 QXEA01084 1 19990606 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 SEA - FORWARD EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EXIT SIGN, OPERATIONAL TEST WAS NORMAL. 2 L 7 2 4F RT A20EU 1999061800061 19990618 00061 EU 1999 6 18 QXEA9901085 1 19990606 A 3350 5005515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 SEA - CABIN FORWARD EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE CABIN FORWARD EXIT SIGN, OPERATIONAL TEST WAS NORMA L. 2 L 7 2 4F RT A20EU 1999061800062 19990618 00062 EU 1999 6 18 QXEA9901269 1 19990607 A 5210 CABLE FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF ADJ A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 478US 11227 PDX- MAIN CABIN DOOR WILL NOT WORK IN EMERGENCY MODE. CLEANED AND LUBED DOOR BACK-UP PINS AND EMERGENCY RELEASE CABLE. RERIGGED EMERGENCY CLUTCH RELEASE CABLE IAW MM 52-10-05. DOOR OPERATES NORMAL. 2 L 7 2 4F RT A20EU 1999061800063 19990618 00063 WP 1999 6 18 ABXA9900423 1 19990604 A 5230 591015741 PAN DOUG DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C-CHECK, FOUND AFT LOWER CARGO DOOR PAN CRACKED. REPLACED DOOR PAN IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061800064 19990618 00064 WP 1999 6 18 ABXA9900424 1 19990604 A 5320 5912285509 RETAINER DOUG DOUG DC9 DC931 3022065 WP BS 698 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C-CHECK, FOUND WINDOW RETAINER CRACKED AT STATION 698, LEFT SIDE. REPAIRED IAW ABX REA D953-31670. 2 L 7 2 4F A6WE 1999061800065 19990618 00065 WP 1999 6 18 ABXA9900425 1 19990604 A 5313 2779224 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 980. REPLACED LONGERON 17 LEFT IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999061800066 19990618 00066 WP 1999 6 18 ABXA9900426 1 19990529 A 5313 592480219 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 256 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 256. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999061800067 19990618 00067 WP 1999 6 18 ABXA9900427 1 19990529 A 5712 991707220 RIB DOUG DOUG DC9 DC941 302207N WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND RIB CRACKED, RIGHT WHEEL WELL, FIRST RIB OUTBOARD OF MAIN LANDING GEAR TRUNNION. REPLACED RIB FOR MER IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999061800068 19990618 00068 WP 1999 6 18 ABXA9900428 1 19990529 A 5755 39232591 BRACKET DOUG DOUG DC9 DC941 302207N WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND LEFT OUTBOARD SPOILER OUTBOARD SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM. 2 L 7 2 4F A6WE 1999061800069 19990618 00069 WP 1999 6 18 ABXA9900429 1 19990529 A 5320 39248461 FITTING DOUG DOUG DC9 DC941 302207N WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND THE LEFT SLANT PANEL OUTBOARD ATTACH FITTING EXFOLIATED. REPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999061800070 19990618 00070 WP 1999 6 18 ABXA9900430 1 19990529 A 5755 3923255502 FITTING DOUG DOUG DC9 DC941 302207N WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND THE RIGHT WING INBOARD SPOILER ACTUATOR, OUTBOARD SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999061800071 19990618 00071 WP 1999 6 18 ABXA9900431 1 19990529 A 5320 99105035 CUSP DOUG DOUG DC9 DC941 302207N WP BS 1035 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND CUSP WEB AT STATION 1035 AND LBL 55 CRACKED. REPAIRED IAW ABX REA D953-31525. 2 L 7 2 4F A6WE 1999061800072 19990618 00072 WP 1999 6 18 ABXA9900432 1 19990529 A 5320 9915565155 FITTING DOUG DOUG DC9 DC941 302207N WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING C-CHECK, FOUND VENTRAL DOOR FITTING CRACKED, 19 INCHES ABOVE FLOOR LEVEL ON LEFT SIDE. REPLACED FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061800073 19990618 00073 WP 1999 6 18 ABXA9900433 1 19990609 A 5311 9919617501 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C-CHECK, FOUND LEFT MAIN FRAME STATION 699 CRACKED. REPLACED LEFT MAIN FRAME IAW DC9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1999061800074 19990618 00074 NM 1999 6 18 DHL9970131D 1 19990329 A 5510 65174303 SUPPORT BOEING 727 72730C 1384009 NM HORIZ STAB GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT HORIZONTAL STAB NR 2 SUPPORT ELEVATOR HAS A GOUGE IN IT. REPLACED SUPPORT PER S/B 55-72. 2 L 7 3 4F A3WE 1999061800075 19990618 00075 NM 1999 6 18 DHL9970145D 1 19990325 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 360 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, 9G FITTING RIPPED OUT OF STR L-15 ATTACHMENT POINT BS 360. CUT OUT DAMAGED SECTION, INSTALLED STRINGER REPA IR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999061800076 19990618 00076 NM 1999 6 18 DHL9970146D 1 19990325 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 360 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, 9G FITTING IS TORN OUT OF STRINGER R 15, BS 360. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR PER SRM 53-10 -3. 2 L 7 3 4F A3WE 1999061800077 19990618 00077 NM 1999 6 18 DHL9970147D 1 19990329 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM NR 3 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FWD END OF NR 3 SEAT TRACK HAS INNER GRANULAR CORROSION. REMOVED AND INSTALLED SEAT TRACK PER SRM 53-10-5 20 LONG. 2 L 7 3 4F A3WE 1999061800078 19990618 00078 NM 1999 6 18 DHL9970148D 1 19990329 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 580-720 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, NR 7 CABIN FLOOR TRACK HAS CORROSION SPOTS AT STA 580, 680, 700 AND 720. REMOVED TRACK FROM 670 TO 740 AND REINSTALLED. REMOVED SEAT TRACK FROM 530 TO 590 AND REINSTALLED PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999061800079 19990618 00079 NM 1999 6 18 DHL9970149D 1 19990326 A 5414 PANEL BOEING 727 72730C 1384009 NM NR 2 ENGINE PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, PANEL TOP OF NR 2 ENGINE TORQUE BOX HAS A HOLE PUNCHED THROUGH. FABRICATED NEW PANEL 21 X 7.5 PER SRM 51- 10-2. 2 L 7 3 4F A3WE 1999061800080 19990618 00080 NM 1999 6 18 DHL9970150D 1 19990326 A 5510 ANGLE BOEING 727 72730C 1384009 NM RT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT HORIZ STAB HAS A CRACK SUPPORT ANGLE. HFEC CRACK, INSTALLED ANGLE REPAIRS PER SRM 51-40-4, 1 X 1 X 8 AND 1 X 1 X 9. 2 L 7 3 4F A3WE 1999061800081 19990618 00081 NM 1999 6 18 DHL9970151D 1 19990329 A 5510 CHORD BOEING 727 72730C 1384009 NM LT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT HORIZ STAB REAR LOWER CHORD HAVE HOLES AND TRIM OUTS. REPAIRED LOWER CHORD PER AVITAS EO 99AVHM012R0-1. 2 L 7 3 4F A3WE 1999061800082 19990618 00082 NM 1999 6 18 DHL9970152D 1 19990326 A 5511 RIB BOEING 727 72730C 1384009 NM LT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT HORIZ STAB BALANCE BAY NR 2 HAS CRACK INTERNAL O/B TOP SUPPORT. REPLACED HINGE SUPPORT RIB PER S/B 55- 72. REPLACED I/B WEB PER SRM 556-10-1, 11.5 X 9. 2 L 7 3 4F A3WE 1999061800083 19990618 00083 NM 1999 6 18 DHL9970153D 1 19990416 A 5751 FITTING BOEING 727 72730C 1384009 NM LT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING O/B AILERON O/B HINGE FITTING CRACKED AT AFT UPPER END AT SKIN ATTACH FLANGE. REMOVED O/B HINGE F ITTING AT LEFT WING PER SRM 51-30-2. REPLACED O/B HINGE FITTING PER SRM 57-30-2. 2 L 7 3 4F A3WE 1999061800084 19990618 00084 NM 1999 6 18 DHL9970154D 1 19990328 A 5751 65217767 CASTING BOEING 727 72730C 1384009 NM LT AILERON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT AILERON LOCKOUT SUPPORT CASTING IS PITTED AT ALL THRU BOLT ATTACH POINTS. REMOVED AND REPLACED SUPPORT CASTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800085 19990618 00085 NM 1999 6 18 DHL9970155D 1 19990326 A 5753 SKIN BOEING 727 72730C 1384009 NM RT TE FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT O/B FLAP FOREFLAP DELAMINATED AT I/B TRAILING EDGE. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-040-8 12' X 8'. 2 L 7 3 4F A3WE 1999061800086 19990618 00086 NM 1999 6 18 DHL9970156D 1 19990329 A 5754 RIB BOEING 727 72730C 1384009 NM NR 6 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING NR 6 L/E SLAT I/B TRACK I/B VERTICAL SUPPORT FLANGE CRACKED. REMOVED AND REPLACED VERTICAL RIB PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999061800087 19990618 00087 NM 1999 6 18 DHL9970157D 1 19990329 A 5754 SUPPORT BOEING 727 72730C 1384009 NM NR 6 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING NR 6 L/E SLAT O/B TRACK O/B VERTICAL SUPPORT FLANGE CRACKED. REMOVED O/B TRACK, REMOVED AND REPLACE D VERTICAL SUPPORT RIB PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800088 19990618 00088 NM 1999 6 18 DHL9970158D 1 19990331 A 5754 RIB BOEING 727 72730C 1384009 NM NR 6 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, NR 6 L/E SLAT NR 3 RIB CRACKED AT BOTTOM RADIUS. REMOVED AND REPLACED NR 3 RIB PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800089 19990618 00089 NM 1999 6 18 DHL9970159D 1 19990326 A 5312 BULKHEAD BOEING 727 72730C 1384009 NM BS 870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RIGHT HAND SECTION 46 STA 870 HAS CORROSION BETWEEN APU PNEUMATIC DUCT AND HYD LINES. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 14 X 10. 2 L 7 3 4F A3WE 1999061800090 19990618 00090 NM 1999 6 18 DHL9970160D 1 19990325 A 5320 FITTING BOEING 727 72730C 1384009 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, STA 950 SIDE FITTING HAS A 8 INCH SEPARATION 3 INCHES ABOVE AND 5 INCHES BELOW STRINGER 10. PERFORMED HFEC, REMOVED RT WINDOW, CUT OUT SECTION OF RT FITTING STA 950 BETWEEN STR 9 AND 14. FABRICATED SPLICE ANGLES PER S/B 53-019 6 13 X 5 AND 13 X 6'. FABRICATED FILLERS, 7.8 X 2.2 AND 10.4 X 2 AND SPLICE PLATE 12.5 X 3.2. INSTALLED WINDOW PLUG. I NSTALLED PARTIAL REPLACEMENT FROM STR 9 TO STR 12 PER S/B 53-0196. 2 L 7 3 4F A3WE 1999061800091 19990618 00091 NM 1999 6 18 DHL9970161D 1 19990326 A 5530 FITTING BOEING 727 72730C 1384009 NM VERTICAL STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, VERTICAL FIN LT HORIZONTAL STAB STAINLESS RUB BLOCK STRIP ON VERT FIN BULGED. REMOVED VERTICAL FITTING AND FOUND CORRODED. REPLACED FITTING SUPORT PER SRM 55-30-2. 2 L 7 3 4F A3WE 1999061800092 19990618 00092 NM 1999 6 18 DHL9970162D 1 19990412 A 5320 BRACKET BOEING 727 72730C 1384009 NM CARGO COMPT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, BRACKET SUPPORT FOR AFT CARGO COMPT UP LATCH CRACKED. REMOVED BRACKET SUPPORT, REPLACED SUPPORT PER SRM 51 -10-1, 17 X 7. 2 L 7 3 4F A3WE 1999061800093 19990618 00093 NM 1999 6 18 DHL9970163D 1 19990326 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 460-480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, CORROSION AT STRINGER 18L, BS 460 TO 480. REMOVED SPLICES, CUT OUT DAMAGED STRINGER FROM 440 TO 480. INSTA LLED STRINGER PER SRM 53-40-3, INSTALLED STRINGER SPLICES PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800094 19990618 00094 NM 1999 6 18 DHL9970164D 1 19990326 A 2710 PULLEY BOEING 727 72730C 1384009 NM LT AILERON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING I/B AILERON / TURN AROUND PULLEY CASTING IS PITTED AT THE TOP AND BOTTOM OF CASTING. REMOVED AND REPLACED PULLEY PER MM 57-42-0. 2 L 7 3 4F A3WE 1999061800095 19990618 00095 NM 1999 6 18 DHL9970165D 1 19990412 A 5713 STRINGER BOEING 727 72730C 1384009 NM WS 601 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, EAR CRACKED ON AFT SIDE OF FWD VENT STRINGER WS 601. INSTALLED REPAIR PER S/B 57A159, 11 INCHES LONG. 2 L 7 3 4F A3WE 1999061800096 19990618 00096 NM 1999 6 18 DHL9970166D 1 19990326 A 5330 PANEL BOEING 727 72730C 1384009 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RIGHT WING T/E LOWER COVE PANEL DELAMINATED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 6 X 6. 2 L 7 3 4F A3WE 1999061800097 19990618 00097 NM 1999 6 18 DHL9970167D 1 19990326 A 5320 STIFFENER BOEING 727 72730C 1384009 NM BS 740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT SECTION 46 STA 740, STIFFENER SUPPORT ATTACH FITTING CORRODED. REMOVED AND REPLACED ATTACH FITTING PER S RM 51-30-2. 2 L 7 3 4F A3WE 1999061800098 19990618 00098 NM 1999 6 18 DHL9970168D 1 19990326 A 5530 65174524 FITTING BOEING 727 72730C 1384009 NM VERT STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, VERTICAL FIN RT HORIZ STAB STAINLESS RUB BLOCK STRIP OVER VERTICAL FIN BULGED. REMOVED AND REPLACED VERTICA L FITTING PER SRM 55-30-2. 2 L 7 3 4F A3WE 1999061800099 19990618 00099 NM 1999 6 18 DHL9970169D 1 19990329 A 2761 BRACKET BOEING 727 72730C 1384009 NM NR 8 SPOILER ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING O/B BRACKET CRACKED AT MLG BEAM PANEL AND NR 8 SPOILER ACTUATOR BRACKET. FABRICATED NEW BRACKET SUP PORT PER SRM 57-20-1, 9 X 5. 2 L 7 3 4F A3WE 1999061800100 19990618 00100 NM 1999 6 18 DHL99720003 1 19990608 A 2923 57186 PUMP BOEING 727 727228 NM NR 2 OVERHEATED A DHLA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TO TAKEOFF 1 SO 01 720DH 19544 ON TAKEOFF, NR 2 B-PUMP OVERTEMPED. REMOVED AND REPLACED NR 2 B-PUMP AND CASE DRAIN FILTER PER MM 29-12-11. 2 L 7 3 4F A3WE 1999061800101 19990618 00101 NM 1999 6 18 DHL99721004 1 19990608 A 7933 162BL704 INDICATOR 1020002 BOEING 727 727228 NM NR 1 OIL SYS MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 721DH 59108 19545 AT FL 310, THE NR 1 OIL TEMP NEEDLE INCREASED TO 130 CELSIUS. FOLLOWING A REDUCTION IN THRUST TO 1.5 EPR THE TEMP DROPP ED BELOW 120. HOWEVER, THE NEEDLE CONTINUED TO FLUCTUATE AND GIVE ERRATIC READINGS. TEMP REMAINED BELOW 120. ALL OTH ER INDICATIONS NORMAL. REPLACED OIL TEMP INDICATOR AND OIL TEMP BULB. 2 L 7 3 4F A3WE 1999061800102 19990618 00102 WP 1999 6 18 DHL99807003 1 19990610 A 3240 SRL07 CONNECTOR DOUG DC8 DC873 302199C WP BRAKE SYS LOOSE A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 807DH 45990 HYDRAULIC BRAKE PRESSURE INDICATOR SHOWED 200 PSI DURING FLIGHT. BRAKING WAS NORMAL UPON LANDING. FOUND INDICATOR NOT ATTACHED TO CONNECTOR. 2 L 7 4 4F RT 4A25 1999061800103 19990618 00103 NM 1999 6 18 DHL9970101D 1 19990331 A 5730 SKIN BOEING 727 72730C 1384009 NM LT WING DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT WING LEADING EDGE HAS LARGE DENT JUST AFT OF NR 1 SLAT O/B SIDE. CUT OUT DAMAGED AREA , INSTALLED REPAIR PER SRM 57-30-4, 7 X 12. 2 L 7 3 4F A3WE 1999061800104 19990618 00104 NM 1999 6 18 DHL9970102D 1 19990328 A 5753 FLAP BOEING 727 72730C 1384009 NM LT TE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT HANED O/B FOREFLAP LEADING EDGE I/B OF NR 1 FLAP TRACK IS GOUGED AT PREV REPAIR. REMOVED AND REPLACED REPAIR PER SRM 57-50-4, 6 X 3. 2 L 7 3 4F A3WE 1999061800105 19990618 00105 NM 1999 6 18 DHL9970103D 1 19990329 A 5751 6521733U997 CASTING BOEING 727 72730C 1384009 NM LT AILERON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING I/B AILERON LOWER INPUT CASTING IS CORRODED. REMOVED AND REPLACED CASTING PER SRM 59-50-1. REBAL ANCE NOT REQD PER SRM 51-80-1. RERIGGED PER MM 27-10-0. 2 L 7 3 4F A3WE 1999061800106 19990618 00106 NM 1999 6 18 DHL9970104D 1 19990329 A 5753 65185328 FITTING BOEING 727 72730C 1384009 NM RT TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING NR 5 FLAP CENTER HINGE SUPPORT FITTING O/B FLANGE ATTACH HOLE CORRODED. REMOVED AND REPLACED SUPPOR T FITTING PER SRM 57-50-2. 2 L 7 3 4F A3WE 1999061800107 19990618 00107 NM 1999 6 18 DHL9970105D 1 19990406 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 380 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FUSE FLOORBEAM CORRODED AT STA 380 BL 49L. CUT OUT FLOORBEAM TO LBL 49. CUT FLOORBEAM CAP OUT FROM LBL 12 TO O/B END. FABRICATED NEW FLOORBEAM TOP CAP WITH SPLICED DOUBLERS PER SRM 53-10-8, 59.5 LONG. 2 L 7 3 4F A3WE 1999061800108 19990618 00108 NM 1999 6 18 DHL9970106D 1 19990326 A 5510 STAB BOEING 727 72730C 1384009 NM HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT HORIZ STAB HAS A CRACK AT SUPPORT ANGLE FOR UPPER PANEL. HFEC CRACK, STOP DRILLED FASTENER HOLES, INSTAL LED ANGLE REPAIR PER AVITAS EO 99AVHM 011RO1. 2 L 7 3 4F A3WE 1999061800109 19990618 00109 NM 1999 6 18 DHL9970107D 1 19990326 A 5510 SUPPORT BOEING 727 72730C 1384009 NM LT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT HORIZONTAL STAB I/B WEB SUPPORT HAS CRACK INTERNAL TOP. HFEC CRACK, ENDED AT FASTENERS, INSTALLED ANGLE REPAIR PER AVITAS RO 99AVHM011RO-1. 2 L 7 3 4F A3WE 1999061800110 19990618 00110 NM 1999 6 18 DHL9970108D 1 19990325 A 5311 FRAME BOEING 727 72730C 1384009 NM BS 910 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT MLG WHEEL WELL ABOVE UPLOCK FITTING FWD WEB O/B FLANGE HAS CRACK DOWN INTO RADII STA 910. STOP DRILLED C RACK AT STR 18A, HFEC STOP DRILLED. FOUND 913 WEB CRACKED. STOP DRILLED CRACK. HFEC, NO PROGRESSION NOTED. INSTALLED FRAME MODIFICATION ABOVE STR 18A AT 910 AND 913 PER S/B 53-165. 2 L 7 3 4F A3WE 1999061800111 19990618 00111 NM 1999 6 18 DHL9970109D 1 19990325 A 5312 BULKHEAD BOEING 727 72730C 1384009 NM BS 870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT WHEEL WELL CORROSION ON BULKHEAD 870 JUST FWD OF LANDING GEAR CONTROL VALVE. CUT OUT DAMAGED AREA, INSTA LLED WEB REPAIR PER SRM 53-10-9, DOUBLER 10 X 5. 2 L 7 3 4F A3WE 1999061800112 19990618 00112 NM 1999 6 18 DHL9970110D 1 19990324 A 5320 WEB BOEING 727 72730C 1384009 NM BS 277 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, NLG LT GEAR DOOR CUTOUT AFT SUPPORT WEB HAS CRACK AT L/E BS 277. REPLACED WEB MATERIAL PER SRM 51-40-2, 8 X 4. 2 L 7 3 4F A3WE 1999061800113 19990618 00113 NM 1999 6 18 DHL9970111D 1 19990324 A 5280 SKIN BOEING 727 72730C 1384009 NM LT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT STRUT DOOR INSIDE SKIN CRACKED AT THE TOP FWD CORNER. FABRICATED NEW DOUBLER 19.5 X 6 AND INSTALLED PER SRM 51-10-2. 2 L 7 3 4F A3WE 1999061800114 19990618 00114 NM 1999 6 18 DHL9970112D 1 19990408 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 1343 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FUSELAGE SKIN DENTED AT APPROX STA 1343 FROM STR 21R TO S-20R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPA IR 12 X 8' PER SRM 53-30-3. 2 L 7 3 4F A3WE 1999061800115 19990618 00115 NM 1999 6 18 DHL9970113D 1 19990401 A 5312 651630018 BULKHEAD ANGLE BOEING 727 72730C 1384009 NM BS 178 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FWD BULKHEAD STA 178 LOWER CHORD ANGLE CORRODED. REMOVED AND REPLACED LOWER CHORD ANGLE PER SRM 53-10-2. 2 L 7 3 4F A3WE 1999061800116 19990618 00116 NM 1999 6 18 DHL9970114D 1 19990401 A 5312 BULKHEAD WEB BOEING 727 72730C 1384009 NM BS 178 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FWD BULKHEAD STA 178 CRACKED. CUT OUT DAMAGED AREA, INSTALLED WEB REPAIR PER SRM 53-10-9, 9.5 X 5. 2 L 7 3 4F A3WE 1999061800117 19990618 00117 NM 1999 6 18 DHL9970115D 1 19990330 A 5350 FAIRING BOEING 727 72730C 1384009 NM LT WING/FUS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING FUSE FAIRING HAS CRACK. STOP DRILLED AND INSTALLED DOUBLER REPAIR PER SRM 51-30-2, 6 X 4. 2 L 7 3 4F A3WE 1999061800118 19990618 00118 NM 1999 6 18 DHL9970116D 1 19990327 A 5320 ANGLE BOEING 727 72730C 1384009 NM BS 325 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FWD LAV FLOOR SUPPORT ANGLE AT DOOR FWD LOWER CORNER IS CORRODED ON LOWER SIDE APPROX STA 325 RBL 14. REMOV ED AND REPLACED SUPPORT ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800119 19990618 00119 NM 1999 6 18 DHL9970117D 1 19990327 A 5320 ANGLE BOEING 727 72730C 1384009 NM BS 330-340 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FWD LAV FLOOR SUPPORT CORRODED ON UPPER SURFACE STA 330 TO 340 RBL 15. REMOVED AND REPLACED SUPPORT ANGLE P ER SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800120 19990618 00120 NM 1999 6 18 DHL9970118D 1 19990327 A 5311 FRAME BOEING 727 72730C 1384009 NM BS 580 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, CORROSION ON ANCHOR NUTS AND ATTACH MOUNTS OF DOOR FRAME BS 580 STR 25R TO 26R. CORROSION OUT OF LIMITS, IN STALLED REPAIR PER SRM 51-40-2, 5.5 X 10. 2 L 7 3 4F A3WE 1999061800121 19990618 00121 NM 1999 6 18 DHL9970119D 1 19990326 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 440-460 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, CORROSION AT BS 440-460 STR 18L. REMOVED SPLICE AND REPAIR , INSTALLED NEW SPLICE AND STRINGER FROM STA 440 TO 480 PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999061800122 19990618 00122 NM 1999 6 18 DHL9970120D 1 19990326 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 470 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, CORROSOIN AT S-23L BS 470. INSTALLED STR REPAIR PER SRM 53-10-3,10.5 LONG. 2 L 7 3 4F A3WE 1999061800123 19990618 00123 NM 1999 6 18 DHL9970121D 1 19990326 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, CORROSION AT S-23R FWD SIDE OF BS 480 FRAME. CUT OUT DAMAGED AREA, INSTALLED STRINGER REPAIR PER SRM 53-10- 3. 2 L 7 3 4F A3WE 1999061800124 19990618 00124 NM 1999 6 18 DHL9970122D 1 19990326 A 5320 FITTING BOEING 727 72730C 1384009 NM BS 740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT SECTION 46 STA 740 JUST FWD DELTA KEEL BEAM VERTICAL STIFFENER CORRODED. REPLACED VERTICAL STIFFENER AND SUPPORT ATTACH FITTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800125 19990618 00125 NM 1999 6 18 DHL9970123D 1 19990325 A 5311 FRAME BOEING 727 72730C 1384009 NM CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FWD LOWER CARGO DOOR CUTOUT FWD FRAME CRACKED BELOW SECOND DOOR STOP FROM TOP. STOP DRILLED CRACK, HFEC, IN STALLED ANGLE REPAIR PER EO DHL MIA-99-0006RR, 7 X 1 X 1. 2 L 7 3 4F A3WE 1999061800126 19990618 00126 NM 1999 6 18 DHL9970124D 1 19990326 A 5311 FRAME BOEING 727 72730C 1384009 NM BS 1116 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, EXFOLIATED CORROSION AT AFT CARGO BILGE INT COMPT, FLOOR FRAME BS 1116, LBL 3. CUT OUT DAMAGED AREA, INSTAL LED ANGLE REPAIR PER SRM 51-40-3, 13 X 1. 2 L 7 3 4F A3WE 1999061800127 19990618 00127 NM 1999 6 18 DHL9970125D 1 19990326 A 5311 6518625122 FRAME BOEING 727 72730C 1384009 NM CARGO COMPT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, INDICATION OF CORROSION AT AFT CARGO COMPT AFT LOWER AREA OF DOOR FRAME. REMOVED FRAME AND INSTALLED NEW FR AME PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999061800128 19990618 00128 NM 1999 6 18 DHL9970126D 1 19990324 A 5320 FRAME BOEING 727 72730C 1384009 NM PAX DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, CRACK INDICATION AT FWD ENTRY DOOR CUT OUT FWD UPPER CORNER. INSTALLED REPAIR / PREVENTATIVE MOD PER S/B 53 -0186, 52 X 22. 2 L 7 3 4F A3WE 1999061800129 19990618 00129 NM 1999 6 18 DHL9970127D 1 19990326 A 5314 KEEL BEAM BOEING 727 72730C 1384009 NM BS 740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT SECTION 46 STA 740 DELTA KEEL BEAM HAD CORROSION. CUT OUT DAMAGED WEB, INSTALLED WEB REPAIR PER SRM 51-4 0-2, 10.5 X 8.5. 2 L 7 3 4F A3WE 1999061800130 19990618 00130 NM 1999 6 18 DHL9970128D 1 19990319 A 5330 PLATE BOEING 727 72730C 1384009 NM PAX DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, FWD ENTRY DOOR UPPER HINGE EXTERNAL COVER PLATE HAD CRACK AT SCREW HOLE. REPLACED COVER PLATE PER SRM 52-0 0-2, 14.5' X 1.5'. 2 L 7 3 4F A3WE 1999061800131 19990618 00131 NM 1999 6 18 DHL9970129D 1 19990329 A 5720 ANGLE BOEING 727 72730C 1384009 NM WS 130 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RIGHT WING I/B LEADING EDGE STA 130 I/B LOWER ATTACH ANGLE CRACKED AT ATTACH FASTENER. REMOVED CRACKED ANGL E SUPPORT, REPLACED ANGLE SUPPORT AND INSTALLED ANGLE REPAIR PER SRM 51-30-2, 20 X 8. 2 L 7 3 4F A3WE 1999061800132 19990618 00132 NM 1999 6 18 DHL9970130D 1 19990329 A 5720 ANGLE BOEING 727 72730C 1384009 NM WS 130 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RIGHT I/B LEADING EDGE WEB AT LEADING EDGE STA 130 I/B SIDE UPPER OLD ANGLE REPAIR CRACKED. REMOVED ANGLE R EPAIR, INSTALLED ANGLE REPAIR PER SRM 51-30-2, 12 X 3. 2 L 7 3 4F A3WE 1999061800133 19990618 00133 NM 1999 6 18 DHL9970132D 1 19990319 A 5720 WEB BOEING 727 72730C 1384009 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING L/E WEB AT WBL 92.8 FWD VERTICAL STIFFENER AT TAI DUCT SUPPORT HAD CRACK AT UPPER AND LOWER ATTACH H OLES. STOP DRILLED CRACK, HFEC, FABRICATED AND INSTALLED ANGLE REPAIR DOUBLER ON RT WING PER SRM 51-40-3, 1.5 X 3. CUT OUT CRACKED SECTION ON RT WING L/E STIFFENER ATTACH HOLE AT WBL 92.8, 1 X 1. FABRICATED AND INSTALLED ANGLE REPAIR ON RT WING L/E VERTICAL STIFFENER PER SRM 51-40-3. DOUBLER 6 X 3. 2 L 7 3 4F A3WE 1999061800134 19990618 00134 NM 1999 6 18 DHL9970133D 1 19990325 A 5753 SKIN BOEING 727 72730C 1384009 NM RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING O/B FLAPS AFT FLAP UPPER SURFACE 134 FROM I/B EDGE AREA DELAMINATED. INSTALLED FIBREGLASS OVERLAY R EPAIR PER SRM 51-40-8, 4 X 9. 2 L 7 3 4F A3WE 1999061800135 19990618 00135 NM 1999 6 18 DHL9970134D 1 19990325 A 5753 SKIN BOEING 727 72730C 1384009 NM RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING O/B FLAPS AFT UPPER SURFACE 73 INCHES FROM I/B EDGE SECTION DELAMINATED. INSTALLED OVERLAY REPAIR P ER SRM 51-40-9, 14 X 6. 2 L 7 3 4F A3WE 1999061800136 19990618 00136 NM 1999 6 18 DHL9970135D 1 19990325 A 5753 SKIN BOEING 727 72730C 1384009 NM RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, RT WING O/B FLAPS AFT FLAP UPPER SURFACE 12 INCHES FROM I/B EDGE SECTION DELAMINATED. INSTALLED OVERLAY REP AIR PER SRM 51-40-8, 8 X 6. 2 L 7 3 4F A3WE 1999061800137 19990618 00137 NM 1999 6 18 DHL9970136D 1 19990327 A 5730 PANEL BOEING 727 72730C 1384009 NM LT WING DISBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT C-CHECK, PANEL NR 8342 L/E SEPARATED AND O/B CORNER CRACKED. INSTALLED BONDED REPAIR PER SRM 51-40-6, 20 X 10. 2 L 7 3 4F A3WE 1999061800138 19990618 00138 NM 1999 6 18 DHL9970137D 1 19990330 A 5730 SKIN BOEING 727 72730C 1384009 NM LT WING GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING L/E SKIN GOUGED AT NR 1 SLAT STA 433 I/B OF TIP. CUT OUT DAMAGED AREA, INSTALLED REPAIR PARTS PER SRM 57-30-4, 6 X 3. 2 L 7 3 4F A3WE 1999061800139 19990618 00139 NM 1999 6 18 DHL9970138D 1 19990330 A 5753 FAIRING BOEING 727 72730C 1384009 NM LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, NR 2 FLAP TRACK MOVEABLE FAIRING HAS SKIN CRACKED AT FWD BOTTOM END. CUT OUT DAMAGED AREA, INSTALLED DOUBL ER REPAIR PER SRM 51-40-2, 4 X 2.75. 2 L 7 3 4F A3WE 1999061800140 19990618 00140 NM 1999 6 18 DHL9970139D 1 19990330 A 5754 SKIN BOEING 727 72730C 1384009 NM LT LE SLAT DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEADING EDGE FLAP LOWER SURFACE DELAMINATED. INSTALLED FILLER REPAIRS PER SRM 51-40-1, 30 X 2. 2 L 7 3 4F A3WE 1999061800141 19990618 00141 NM 1999 6 18 DHL9970140D 1 19990325 A 5754 FENCE BOEING 727 72730C 1384009 NM LT LE SLAT DETERIORATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING NR 4 L/E SLAT WING FENCE L/E DETERIORATED. INSTALLED FILLER REPAIR PER SRM 51-40-1, 10 X 4. 2 L 7 3 4F A3WE 1999061800142 19990618 00142 NM 1999 6 18 DHL9970141D 1 19990325 A 5754 RIB BOEING 727 72730C 1384009 NM LT LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT WING L/E SLAT NR 2 RIB NR 19 CRACKED. TRIMMED CRACKED PORTION OF RIB FLANGE, NDT INSPO, INSTALLED RIB R EPAIR PER SRM 51-30-2, 6 X 4. 2 L 7 3 4F A3WE 1999061800143 19990618 00143 NM 1999 6 18 DHL9970142D 1 19990325 A 5754 RIB BOEING 727 72730C 1384009 NM LT LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING L/E SLAT NR 2 RIB NR 16 CRACKED. TRIMMED CRACKED AREA, INSTALLED RIB, REPAIRED PER SRM 57-30-2, 6 X 4. 2 L 7 3 4F A3WE 1999061800144 19990618 00144 NM 1999 6 18 DHL9970143D 1 19990325 A 5754 RIB BOEING 727 72730C 1384009 NM LT LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LT WING L/E SLAT NR 2 RIB NR 15 CRACKED. TRIMMED CRACKED PORTION, INSTALLED RIB REPAIR PER SRM 57-50-3, 6 X 4. 2 L 7 3 4F A3WE 1999061800145 19990618 00145 NM 1999 6 18 DHL9970144D 1 19990325 A 5754 RIB BOEING 727 72730C 1384009 NM LT LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT D-CHECK, LEFT WING NR 2 SLAT NR 14 RIB IS CRACKED. TRIMMED CRACKED PORTION, NDT PER NDT MANUAL, INSTALLED REPAIR PE R SRM 57-50-3, 6 X4. 2 L 7 3 4F A3WE 1999061800166 19990618 00166 NM 1999 6 18 SWAA990973 1 19990607 A 5240 6547952 SKIN BOEING 737 7372H4 138448C NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR SKIN HAS 1 INCH LONG CRACK AT LOWER HINGE ARM CUT OUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999061800167 19990618 00167 NM 1999 6 18 SWAA990974 1 19990607 A 5754 6573714 SKIN BOEING 737 7372H4 138448C NM NR 4 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED C4 CHECK, FOUND NR 4 LE SLAT HAS A .25 INCH LONG CRACK AT INBD AUX TRACK CUT OUT. REPAIRED SLAT PER SW A RA NR 1-257-0703. 2 L 7 2 4F A16WE 1999061800168 19990618 00168 NM 1999 6 18 SWAA990975 1 19990607 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AFT FLANGE, BS 1006, LBL 29. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999061800169 19990618 00169 NM 1999 6 18 SWAA990976 1 19990608 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM BS 663.75 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 663.75, STRINGERS 10L AND 10R. REMOVED AND REPLACE D STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 1999061800170 19990618 00170 NM 1999 6 18 SWAA990977 1 19990608 A 7170 493645 MOISTURE TRAP BOEING 737 7372H4 138448C NM NR 1 ENGINE REQD SERVICE A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 07 086SW 22827 NR 1 ENGINE SURGING PLUS OR MINUS 0.10 EPR AT TAKEOFF POWER. TAKEOFF REJECTED BELOW 60 KNOTS. DRAINED NR 1 ENGINE MOIS TURE TRAP. RAN ENGINE, OPS CHECK GOOD PER MM. 2 L 7 2 4F A16WE 1999061800171 19990618 00171 NM 1999 6 18 SWAA990978 1 19990608 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING WALK AROUND CHECK, FOUND A 4 INCH LONG CRACK ON FUSELAGE SKIN RT SIDE, JUST FWD OF REAR BAG BIN. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 1999061800172 19990618 00172 NM 1999 6 18 SWAA990979 1 19990608 A 3350 20121 BATTERY CHARGER BOEING 737 7373H4 1384600 NM LT EMER EXIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHT ABOVE LT WING INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999061800173 19990618 00173 NM 1999 6 18 SWAA990980 1 19990608 A 3350 079123 COVER BOEING 737 7373T0 1384582 NM ROW 8 & 21 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT COVER BROKEN BETWEEN ROWS 8 AND 21. REMOVED AND RE PLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999061800174 19990618 00174 NM 1999 6 18 SWAA990981 1 19990609 A 2612 894093 FIRE LOOP BOEING 737 7372H4 138448C NM NR 2 ENGINE MALFUNCTIONED A SWAA D E RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 SW 07 080SW 22675 AIR TURNBACK IN FLIGHT SHUT DOWN. FIRE INDICATION FOR NR 2 ENGINE. DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED NR 2 ENGINE LOWER FIRE LOOP AND FIRE CONTROL PANEL. CLEANED ALL FIRE LOOP ENDS AT FIRE WALL. OPS CHECK GOOD PER MM. (CONTR OL PANEL P/N 69-37307-112). 2 L 7 2 4F A16WE 1999061800175 19990618 00175 NM 1999 6 18 SWAA990982 1 19990609 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 EMERGENCY EVACUATION FLOOR TRACK LIGHTING LOOSE AT MID CABIN. SECURED TRACK LIGHTING.PER MM. 2 L 7 2 4F RT A16WE 1999061800176 19990618 00176 NM 1999 6 18 SWAA990983 1 19990609 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM PAX DOORWAY MISALIGNED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 LEFT AFT ENTRY DOOR LATCH WILL NOT ENGAGE GIRT BAR. REPOSITIONED AFT GIRT BAR BRACKET PER MM. 2 L 7 2 4F RT A16WE 1999061800177 19990618 00177 1999 6 18 SWAA990984 4 19990609 A 2565 D31591 SLIDE BOEING 737 7373L9 1384470 NM PASSENGER DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 FWD ENTRY DOOR SLIDE GIRT BAR INNER PLASTIC SLEEVE BROKEN. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999061800178 19990618 00178 NM 1999 6 18 SWAA990985 1 19990609 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 6 & 7 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT ROWS 6 AND 7. RELAMPED 2 EA LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999061800179 19990618 00179 NM 1999 6 18 SWAA990986 1 19990609 A 3350 D71702001 BATTERY PACK BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 EMERGENCY EXIT LIGHTS AT FLOOR AND AT OVERHEAD BIN BULLNOSES INTERMITTENT. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999061800180 19990618 00180 NM 1999 6 18 SWAA990988 1 19990609 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, ABOVE STRINGER 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999061800181 19990618 00181 NM 1999 6 18 SWAA990989 1 19990609 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT BS 639, BETWEEN STRINGERS 16L-17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999061800182 19990618 00182 NM 1999 6 18 SWAA990990 1 19990609 A 5312 6516300 BULHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12, WL 234. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999061800183 19990618 00183 NM 1999 6 18 SWAA990991 1 19990609 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUT OUT OF FWD ENTRY DOOR. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 1999061800184 19990618 00184 NM 1999 6 18 SWAA990992 1 19990609 A 3350 BR2013 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 609SW 27929 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTING, AFT BULB INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999061800185 19990618 00185 NM 1999 6 18 SWAA990993 1 19990609 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM ROW 14 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 609SW 27929 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK COVER CRACKED AT ROW 14. REMOVED AND REPLACED COVER PER M M. 2 L 7 2 4F RT A16WE 1999061800186 19990618 00186 NE 1999 6 18 SWAA990994 2 19990610 A 7320 1853M56P06 HMU BOEING 737 7377H4 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SW 07 701GS 27836 HEAVY AIRFRAME VIBRATION AT 35000 FT FLIGHT LEVEL, 260 KNOTS, 92 PERCENT N1. VIBRATION GOES AWAY WHEN POWER REDUCED. R EMOVED AND REPLACED NR 2 ENGINE HMU PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 1999061800187 19990618 00187 NM 1999 6 18 SWAA990995 1 19990610 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM UPPER T-CAP, BS 312, LBL2. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999061800188 19990618 00188 NM 1999 6 18 SWAA990996 1 19990610 A 5312 963820 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND LT AND RT SIDE CHORDS CRACKED, BS 178, BL 26, WL 207. REMOVED AND REPLACED CHORDS PE R SRM. 2 L 7 2 4F RT A16WE 1999061800189 19990618 00189 NM 1999 6 18 SWAA990997 1 19990610 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND LT AND RT SIDE BULKHEAD CRACKED, BS 178, BL 1, WL 189. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999061800190 19990618 00190 NM 1999 6 18 SWAA990999 1 19990610 A 2560 6557463 BRACKET BOEING 737 7375H4 138449D NM PAX DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR GIRT BAR, AFT FLOOR ATTACH BRACKET LOOSE. TIGHTENED ATTACH BRACKET PER MM. 2 L 7 2 4F RT A16WE 1999061800191 19990618 00191 NM 1999 6 18 CALA9900663 1 19990610 A 3350 BR964411 LIGHT BRUCE BOEING 757 757224 1384958 NM ROW 32 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17105 27295 THE EMERGENCY PATH LIGHTING ON SEATS 11, 32, AND 34 WERE FOUND INOPERATIVE. THE MODULE AT SEAT 11 WAS TIGHTENED. THE C ONNECTOR AT ROW 34 WAS RECONNECTED. THE LIGHT FIXTURE AT ROW 32 WAS REMOVED AND REPLACED. OPERATION OF THE EMERGENCY P ATH LIGHTING CHECKED GOOD. 2 L 7 2 4F RT A2NM 1999061800192 19990618 00192 WP 1999 6 18 CALA9900664 1 19990610 A 3350 FUSE DOUG DC10 DC1030 3023501 WP ROW 35-45 BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12061 47851 THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROWS 35-45 A/B. MAINTENANCE FOUND A FUSE BLOWN FOR THAT SECTION. THE FUSE WAS REPLACED. OPERATION OF THE LIGHTS CHECKED GOOD. 2 L 7 3 4F A22WE 1999061800193 19990618 00193 WP 1999 6 18 CALA9900665 1 19990611 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1030-1305 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED UNDER GALLEY AREAS NUMBER 3 AND 4 AT STA 1030-1305. THE SEAT TRACK WAS RE MOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999061800194 19990618 00194 NM 1999 6 18 UPS99229786 1 19990514 A 5755 BEAM BOEING 727 72725C 138400H NM LT SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI CORROSION (C57-581-07.00-03) L/W SPOILER BEAM PAD, LOWER SURFACE WHERE NR 4 FLAP TRACK ATTACHES. REM OVED AND INSTALLED NEW SPOILER BEAM, FLAP TRACK ATTACHMENT PAD WORK DONE IAW SRM 51-30-5, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 1999061800195 19990618 00195 NM 1999 6 18 UPS99229792 1 19990512 A 5320 69158409 STIFFENER BOEING 727 72725C 138400H NM BS 229 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON LONGITUDINAL STIFFENER TOP OF NOSE WHEEL WELL STN 229 LBL 20 WL 186. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-30-2 AND 53-10-1 PART REPLACED WITH USED ITEM PER SRM 51-30-5, SRM 51-30 -2 PG 2/8 SRM 51-20-151 AND OHM 20-50-03. 2 L 7 3 4F A3WE 1999061800196 19990618 00196 NM 1999 6 18 UPS99229793 1 19990527 A 5753 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI CORROSION ON NR 7 FLAP CARRIAGE AT SPINDLE FWD END. REPLACE FLAP CARRIAGE. 2 L 7 3 4F A3WE 1999061800197 19990618 00197 NM 1999 6 18 UPS99229795 1 19990609 A 3350 BULB BOEING 727 72725C 138400H NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 TWO AFT AIRSTAIR EMERGENCY LIGHTS INOP. RELAMPED, OPS CHECKS GOOD FROM SWITCH AT FLIGHT ATTENDANTS STATION. 2 L 7 3 4F A3WE 1999061800198 19990618 00198 NM 1999 6 18 UPS99229796 1 19990525 A 5753 651920612 FLAP TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI CORROSION (C57-581-06.00-04) ON NR 6 FLAP TRACK AT SPOILER BEAM PAD AND HOLES AND AT FORWARD LUG AND REAR SPAR MOUNT HOLES. REMOVED NR 6 FLAP TRACK, REMOVED HARDWARE, SENT TO OVERHAUL FACILITY. RECEIVED OVERHAULED FLAP TRACK, INSTALLED HARDWARE AND INSTALLED OVERHAULED FLAP TRACK ONTO AIRCRAFT PER SRM 51-30-02, AND OHM 20-50-03. 2 L 7 3 4F A3WE 1999061800199 19990618 00199 NM 1999 6 18 UPS99229797 1 19990525 A 5753 691920612 FLAP TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 3 FLAP TRACK AT SPOILER BEAM MOUNT PAD AND HOLES AND AT REAR SPAR MOUNT HOLES. REMOVED NR 3 FLAP TRACK, REMOVED HARDWARE, SENT FLAP TRACK OUT TO OVERHAUL FACILITY. RECEIVED OVERHAULED FLAP TRACK AND INSTALLED HARDWARE. ALL WORK IAW SRM 51-30-02 AND OHM 57-40-01, OHM 20-50-03 INSTALLED FLAP TRACK ONTO A IRCRAFT. 2 L 7 3 4F A3WE 1999061800200 19990618 00200 NM 1999 6 18 UPS99229798 1 19990526 A 5320 HFAB53ST011 SHEAR TIE BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI CORROSION ON SHEAR TIE FWD SIDE BS 720E FRAME BETWEEN STR 26 AND 27 LEFT CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED SHEAR TIE PER 53-10-4 SRM REPAIRED SHEAR TIE PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999061800201 19990618 00201 NM 1999 6 18 UPS99229799 1 19990526 A 5320 HFAB53ST011 SHEAR TIE BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI CORROSION ON FWD FACE OF FRAME AND SHEAR TIE BS 720F BETWEEN STR 27 AND 28 RT. BLENDED CORROSION ON FRAME, FOUND TO BE IN LIMITS PER SRM 53-10-1. SHEAR TIE FOUND TO BE OUT OF LIMITS PER 53-10-1 SRM. REPAIRED SHEAR TIE PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999061800202 19990618 00202 WP 1999 6 18 UPS99829794 1 19990610 A 3350 5708458503 EMERG BATT DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 1999061800203 19990618 00203 WP 1999 6 18 UPS99829800 1 19990610 A 2560 GIRT BAR DOUG DC8 DC873F 302199F WP CREW DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 CREW ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT BAR INOP. REPOSITIONED GIRT BAR LOCKING CLIPS ON FLOOR, GIRT BAR LOCK CKS G OOD. 2 L 7 4 4F RT 4A25 1999061800204 19990618 00204 EU 1999 6 18 QXEA9901113 1 19990520 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT OUTBOARD SEAT TRACK HAS A GOUGE 9 FORWARD OF FRAME 10346. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAP H 3C4. 2 L 7 2 4F RT A20EU 1999061800205 19990618 00205 EU 1999 6 18 QXEA9901114 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT OUTBOARD SEAT TRACK HAS FRETTING CORROSION ADJACENT TO FRAME 9305B ON INBOARD FLANGE AND AROUND CAMLOC RECEPT ACLE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800206 19990618 00206 EU 1999 6 18 QXEA9901115 1 19990520 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS SMALL NICKS AND LIGHT CHAFE DAMAGE 4 AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-1 0-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800207 19990618 00207 EU 1999 6 18 QXEA9901116 1 19990520 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION AROUND CAMLOC RECEPTACLE 2 FORWARD OF FRAME 11905. REPAIRED IAW FO KKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800208 19990618 00208 EU 1999 6 18 QXEA9901117 1 19990528 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION 2 INCHES AFT OF FRAME 10966. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999061800209 19990618 00209 EU 1999 6 18 QXEA9901118 1 19990528 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON INBOARD FLANGE AND IN CHANNEL AT FRAME 9305C AND EXTENDS 6 AFT OF FRAME 9 305C. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1999061800210 19990618 00210 EU 1999 6 18 QXEA9901119 1 19990520 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE ADJACENT TO FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999061800211 19990618 00211 EU 1999 6 18 QXEA9901120 1 19990601 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9550-9700 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE BETWEEN STATION 9550 AND 9700. REPAIRED IAW FOKKER SRM 5 1-10-04, PAGE 9, PARAGRAPH 4,A,1 AND HORIZON AIR EA 4-53-813. 2 L 7 2 4F RT A20EU 1999061800212 19990618 00212 EU 1999 6 18 QXEA9901121 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON INBOARD FLANGE AT FRAME 9305B AND EXTENDING 6 FORWARD OF 9305B. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800213 19990618 00213 EU 1999 6 18 QXEA9901122 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE 2 FORWARD AND 2 AFT OF FRAME 8305. REPAIRED IAW FOKKER S RM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800214 19990618 00214 EU 1999 6 18 QXEA9901123 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS FRETTING CORROSION ON OUTBOARD FLANGE EXTENDING 3 AFT TO 8 AFT OF FRAME 7805. REPAIRE D IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800215 19990618 00215 EU 1999 6 18 QXEA9901124 1 19990601 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT INBOARD SEAT TRACK HAS CORROSION 5 FORWARD OF FRAME 7805 ON THE OUTBOARD FLANGE. REPAIRED IAW FOKKER SRM 51- 10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800216 19990618 00216 EU 1999 6 18 QXEA9901125 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS A SMALL TOOLING DAMAGE 4 AFT OF FRAME 11905. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800217 19990618 00217 EU 1999 6 18 QXEA9901126 1 19990601 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS FRETTING CORROSION AROUND CAMLOC RECEPTACLE 2 AFT OF FRAME 11905. REPAIRED IAW FOKKE R SRM 51-10-04, PAGE 8, PARAGRAPH 4 BAND HORIZON AIR EA 4-53-813 2 L 7 2 4F RT A20EU 1999061800218 19990618 00218 EU 1999 6 18 QXEA9901127 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS A SMALL AREA OF FRETTING CORROSION ON INBOARD FLANGE 8 FORWARD OF FRAME 7805. REPAIR ED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800219 19990618 00219 EU 1999 6 18 QXEA9901128 1 19990527 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 7800-8000 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS 3 SMALL AREAS OF FRETTING CORROSION BETWEEN STATION 7800 AND 8000 ON INBOARD FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-813 AND FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800220 19990618 00220 EU 1999 6 18 QXEA9901129 1 19990520 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION 2 FORWARD OF FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRA PH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800221 19990618 00221 EU 1999 6 18 QXEA9901130 1 19990527 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS FRETTING CORROSION ON INBOARD FLANGE 4 FORWARD OF FRAME 9305A. REPAIRED IAW FOKKER S RM 51-10-04, PAGE 9, PARAGRAPH 4B AND HORIZON AIR EA 4-53-813. 2 L 7 2 4F RT A20EU 1999061800222 19990618 00222 EU 1999 6 18 QXEA9901131 1 19990528 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION AT FRAME 9305C AND EXTENDS 3 FORWARD OF FRAME 9305C. REPAIRED IAW FOKKER S RM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999061800223 19990618 00223 EU 1999 6 18 QXEA9901132 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS FRETTING CORROSION IN 3 SMALL AREAS JUST FORWARD OF FRAME 9305C. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800224 19990618 00224 EU 1999 6 18 QXEA9901133 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION 9 AFT OF FRAME 9805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3 ,C,4. 2 L 7 2 4F RT A20EU 1999061800225 19990618 00225 EU 1999 6 18 QXEA9901134 1 19990601 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS A SMALL AREA OF FRETTING CORROSION ADJACENT TO FRAME 10966 ON INBOARD FLANGE. REPAIR ED IAW FOKKER SRM 51-10-04 AND HORIZON AIR EA 4-53-813. 2 L 7 2 4F RT A20EU 1999061800226 19990618 00226 EU 1999 6 18 QXEA9901135 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS TOOLING DAMAGE 4 FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PA RAGRAPH 3,C,4. 2 L 7 2 4F RT A20EU 1999061800227 19990618 00227 EU 1999 6 18 QXEA9901136 1 19990527 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 4850 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION ON INBOARD FLANGE AT FRAME 4850. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800228 19990618 00228 EU 1999 6 18 QXEA9901137 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 47 CORROSION/CRACK AT HOLES, 2 CRACKS ONE AT EACH HOLE 6.3 AFT OF FRAME 6805 AND 6.4 FORWARD OF FRAME 730 5. REPAIRED IAW FOKKER SRM 53-02-06. 2 L 7 2 4F RT A20EU 1999061800229 19990618 00229 NM 1999 6 18 99FDEA00211 1 19990610 A 5315 65402746 FLOORBEAM BOEING 727 727247 138408F NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 234FE 21328 CORROSION (C53-111-01,3) ON FLOORBEAM LOWER CHORD AT BS 1070, WL 200, LBL 40 TO RBL 48. *S/D* REMOVED AND REPLACED FLO ORBEAM PER FEDEX EA 7-5310-45262A. 2 L 7 3 4F A3WE 1999061800230 19990618 00230 NM 1999 6 18 99FDEA00209 1 19990609 A 2611 774001 SMOKE DETECTOR BOEING 727 727233 138408A NM E & E COMPT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 274FE 22039 99-128 PER CREW NR 3 MAIN CARGO DETECTOR SMOKE DETECTOR LIGHT FLICKERED ON LANDING. REMOMED AND REPLACED NR 3 SMOKE DE TECTOR PER MM 26-16-011-4. OPER CK NORMAL. 2 L 7 3 4F RT A3WE 1999061800231 19990618 00231 EU 1999 6 18 99FDEA00210 1 19990610 A 2611 SMOKE DETECTOR AIRBUS 310 A310222 3930315 EU E & E COMPT FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 418FE 343 99-129 AT 17,000 MSL, LT ECAM RED/CRC AVIONICS SMOKE NOT NOTICABLE FUMES/ODORS. REMOVED AND REPLACED 13WA SMOKE DETECTO R PER MM 26-15-12. OPS CK GOOD MM A310-26-15-00. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999061800232 19990618 00232 EU 1999 6 18 99FDEA00212 1 19990611 A 5210 MECHANISM AIRBUS 300 A300F4605R 3930327 EU PASSENGER DOOR UNLATCHED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 654FE 738 99-130 - RIGHT PASSENGER DOOR OPEN ECAM AND SHIME SOUNDED. CHECK DOOR PER AMM 52-10-20-5 ALL LATCHES OPER NORM. SUSPEC T DOOR WAS NOT LATCHED ALL THE WAY. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999061800233 19990618 00233 NM 1999 6 18 99FDEA00213 1 19990607 A 3610 DUCT BOEING 727 727233 138408A NM LT ENGINE LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 220FE 20934 99-131 - NR1 ENGINE STRUT OVERHEAT LIGHT CAME ON. REMOVED AND REPLACED LEFT HEAT EXCHANGER DUCT PER MM 36-12-12-042-4. LEAK CK NORM. 2 L 7 3 4F RT A3WE 1999061800234 19990618 00234 NM 1999 6 18 99FDEA00214 1 19990611 A 5720 CHORD BOEING 727 72725 1384006 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 246 CORROSION (C53-132-02(1)) BETWEEN BS 870 UPPER CHORD AND 870 WEB AT LBL 41. 2 L 7 3 4F A3WE 1999061800235 19990618 00235 NM 1999 6 18 99FDEA00215 1 19990611 A 5720 65192921 WEB BOEING 727 72725 1384006 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 634 WHILE WORKING NR 246 FOUND BS 870 WING CTR SECTION AFT VERTICAL WEB TO BE CORRODED BEYOND LIMITS. 2 L 7 3 4F A3WE 1999061800236 19990618 00236 NM 1999 6 18 99FDEA00216 1 19990611 A 5720 65185372 CHORD BOEING 727 72725 1384006 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 799 WHILE WORKING NR 246 FOUND WING CTR SECTION LWR CHORD AT BS 870, RBL 16 TO RBL 55 TO BE CORRODED. 2 L 7 3 4F A3WE 1999061800237 19990618 00237 WP 1999 6 18 ABXA9900434 1 19990423 A 5712 577615333 RIB DOUG DOUG DC8 DC863 302198A WP WS 484.895 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 484.895. REPAIRED IAW DWG K05056. 2 L 7 4 4F 4A25 1999061800238 19990618 00238 WP 1999 6 18 ABXA900435 1 19990423 A 5712 57701533 RIB DOUG DOUG DC8 DC863 302198A WP WS 454.976 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING LEADING EDGE RIB CRACKED AT STATION XFS 454.976. REPAIRED IAW DWG K05056. 2 L 7 4 4F 4A25 1999061800239 19990618 00239 WP 1999 6 18 ABXA9900436 1 19990420 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP WS 660 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 8716A 46093 RIGHT WING LEADING EDGE AFT END CRACKED AT XFS 660.0. REPAIRED IAW DWG K0 5056. 2 L 7 4 4F 4A25 1999061800240 19990618 00240 WP 1999 6 18 ABXA9900437 1 19990420 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP WS 791.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 791.25, UPPER ARM. REPAIRED IAW DWG KO 5056. 2 L 7 4 4F 4A25 1999061800241 19990618 00241 WP 1999 6 18 ABXA9900438 1 19990420 A 5712 9769545 RIB DOUG DOUG DC8 DC863 302198A WP WS 778.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB UPPER ARM CRACKED AT STATION XFS 778.75. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999061800242 19990618 00242 WP 1999 6 18 ABXA9900439 1 19990611 A 5312 5917579237 BULKHEAD JAMB DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB CRACKED AT STATION 1072 LEFT SIDE. REPAIRED IAW ABX REA D 953-31706MR. 2 L 7 2 4F A6WE 1999061800243 19990618 00243 WP 1999 6 18 ABXA9900440 1 19990611 A 5755 3923258504 FITTING DOUG DOUG DC9 DC941 302207N WP RT SPIOLER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND RIGHT OUTBOARD SPOILER TORSION BAR CENTER SUPPORT CRACKED. REPLACED SUPPORT FITTING IAW DC9 SRM 5 1-30-1. 2 L 7 2 4F A6WE 1999061800244 19990618 00244 WP 1999 6 18 ABXA9900441 1 19990611 A 5320 991050111 MEMBRANE DOUG DOUG DC9 DC941 302207N WP BS 389 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND CUSP WEB MEMBRANE CRACKED AT STATION 389 AND RBL 55. REPAIRED CUSP WEB MEMBRANE IAW DC9 SRM 53-01 . 2 L 7 2 4F A6WE 1999061800245 19990618 00245 WP 1999 6 18 ABXA9900442 1 19990611 A 5320 59148659 DOUBLER DOUG DOUG DC9 DC941 302207N WP BS 636 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND BULGES IN LOWER PRESSURE PANEL WITH SHEARED RIVETS, AT STATION 636 BETWEEN LONGERONS 29 AND 30 RIG HT. REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1999061800246 19990618 00246 WP 1999 6 18 ABXA9900443 1 19990611 A 5320 29560321 FITTING DOUG DOUG DC9 DC941 302207N WP BS 484 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND FLOOR SUPPORT FITTING CRACKED AT STATION 484 AND LONGERON 28 LEFT. REPLACED FITTING IAW DC9 SRM 5 1-30-5. 2 L 7 2 4F A6WE 1999061800247 19990618 00247 WP 1999 6 18 ABXA9900444 1 19990611 A 5311 99234092 FRAME DOUG DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND RIGHT MAIN FRAME CRACKED AT STATION 737, FORWARD FLANGE, TOP SURFACE. REPAIRED IAW ABX REA D953-3 1729MR. 2 L 7 2 4F A6WE 1999061800248 19990618 00248 WP 1999 6 18 ABXA9900445 1 19990611 A 5320 591141237N INTERCOSTAL DOUG DOUG DC9 DC941 302207N WP BS 475 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT STATION 475. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999061800249 19990618 00249 WP 1999 6 18 MWEA99330 1 19990607 A 5330 591142379 SKIN DOUG DC9 DC932 3022066 WP BS 990-996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FUSELAGE SKIN IS CRACKED AT FS 990-996 AT LONGERON 22L. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061800250 19990618 00250 1999 6 18 MWEA99331 4 19990609 A 3442 MI585306401 TRANSCEIVER DOUG DC9 DC932 3022066 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 203ME 47673 EN ROUTE TO MCO, THE WEATHER RADAR STOPPED PAINTING WEATHER, AND DISPLAYED A R/T FAIL ON THE SCREEN. REMOVED AND REPLAC ED THE RADAR R/T UNIT. 2 L 7 2 4F A6WE 1999061800251 19990618 00251 WP 1999 6 18 MWEA99332 1 19990609 A 5330 59114015 SKIN DOUG DC9 DC914 3022034 WP BS 154 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FUSELAGE SKIN HAS CRACK AT FS 154 BETWEEN LONGERON 27 AND 28 R. MAINTENANCE TRIMMED OUT CORRODED SKIN AND REMOVED AND R EPLACED DOUBLER. 2 L 7 2 4F A6WE 1999061800252 19990618 00252 WP 1999 6 18 MWEA99333 1 19990609 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN CHAFED A MWEA K NONE L NO TEST CR CRUISE 1 GL 31 401ME 47133 WHILE EN ROUTE, THE EMERGENCY CABIN LIGHTS ILLUMINATED EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER WAS POPPED BUT DI D RESET. REPAIRED CHAFFED WIRE ABOVE RIGHT LAV. 2 L 7 2 4F A6WE 1999061800253 19990618 00253 NM 1999 6 18 MWEA99334 1 19990609 A 2560 D29985107 SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOOR OUT OF POSITION A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE AFT GALLEY SERVICE DOOR IS DIFFICULT TO OPEN AND HANGS UP ON SLIDE COVER. MAINTENANCE REPOSITION DOOR SLIDE PACK. 2 L 7 2 4F RT A6WE 1999061800254 19990618 00254 WP 1999 6 18 MWEA99335 1 19990610 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 401ME 47133 THE FORWARD ENTRANCE EMERGENCY FLASHLIGHT IS NOT SHOWING A CHARGE AND IS INOP. MAINTENANCE REMOVED AND REPLACED LIGHT A SSEMBLY. 2 L 7 2 4F A6WE 1999061800255 19990618 00255 NM 1999 6 18 SCNA99710 1 19990607 A 3350 BATTERY BOEING 727 7272K3 138400D NM L2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 DURING HEAVY MAINTENANCE CHECK, THE L2 DOOR EMERGENCY LIGHT FLICKERS. AFTER BATTERIES CHARGED OPERATIONS CHECK GOOD IAW B727 MM 335001. 2 L 7 3 4F RT A3WE 1999061800256 19990618 00256 NM 1999 6 18 SCNA99711 1 19990607 A 3350 BATTERY BOEING 727 7272K3 138400D NM ROW 5 DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 DURING HEAVY MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHT LOCATED AT ROW 5 FLICKERS. BATTERIES LOW, AFTER CHARG ING OPERATIONS CHECK GOOD IAW B727 335001. 2 L 7 3 4F RT A3WE 1999061800257 19990618 00257 NM 1999 6 18 VNAA9906004 1 19990608 A 7603 LINKAGE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DISCONNECTED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 460PS 3061 LEFT PROPELLER RPM AND TORQUE READINGS REMAINED AT 74 PERCENT REGARDLESS OF CONDITION LEVER INPUTS. NOSE WHEEL STEERIN G WAS ALSO NOTED TO BE INOPERATIVE. THE CREW SHUTDOWN THE LT ENGINE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AN D FOUND THE CONTROL QUADRANT LEFT CONDITION LEVER TO MICROSWITCH LINKAGE TO BE DISCONNECTED. THE LINKAGE WAS RE-CONNECT ED, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-05. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34N 1999061800258 19990618 00258 SW 1999 6 18 99ZZZX2295 1 19990603 A 2910 70010H00012180 LINE BELL 206 206B 1181511 SW HYDRAULIC SYSTEM LEAKING A ILDA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 801H 12344 3186 WHILE FLYING ON TOUR FLIGHT, PILOT NOTICED AIRCRAFT WAS LOSING HYDRAULIC SYSTEM. PILOT IMMEIDATLEY MADE A PRECAUTIONARY LANDING. INSPECTED AIRCRAFT, FOUND THAT HIGH PRESSURE HYDRAULUIC LINE HAD LEAKS. REMOVED AND REPLACED HYDRAULIC LINE AND FUNCTIONALLY CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U H2SW 1999061800275 19990618 00275 NE 1999 6 18 99ZZZX2312 2 19990513 A 7200 ENGINE LEAR 23 23LEAR 5170102 CE GE CJ610 CJ6104 30006 NE LEFT FAILED A KKFA A UNSCHED LANDING E X VIBRATION/BUFFET ENGINE FLAMEOUT NR NOT REPORTED 1 GL 23 96CK 7918 23016 211ZAT203 LEFT ENGINE EXPERIENCED TURBULENCE INDUCED FLAME-OUT AND WOULD NOT RE-LIGHT IN FLIGHT. UNEVENTFUL LANDING ACCOMPLISHED. ENGINE TO BE REMOVED AND REPLACED. ENGINE WAS REPLACED WITH SERVICEABLE UNIT AND AN ALTITUDE ACCELERATION CHECK ACCOM PLISHED. POSSIBLE CAUSE WAS DETERMINED TO BE A STREAKING FUEL NOZZLE WHICH RESULTED IN TURBINE NOZZLE DAMAGE THAT DISRU PTED THE AIR FLOW IN THE ENGINE CAUSING THE FLAME-OUT. 1 L 7 2 4J 4 J A5CE 1E16 1999061800282 19990618 00282 SO 1999 6 18 99ZZZX2319 1 19990528 A 2140 A2300475 REGULATOR PIPER PA31 PA31350 7103110 SO FUEL PRESSURE LEAKING A WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 35270 219 WAV2001 317952141 DURING 100-HOUR INSPECTION, OBSERVED FUEL LEAK FROM PRESSURE REGULATOR CONTAINMENT VESSEL. REMOVED CONTAINMENT VESSEL A ND FOUND FUEL LEAKING FROM PARTING SURFACE AT THE TOP OF THE REGULATOR. PREVIOUS UNIT WAS REPLACED FOR THE SAME PROBLEM . 1 L 7 2 3O A20SO 1999061800283 19990618 00283 EA 1999 6 18 99ZZZX2320 2 19990501 A 8520 LW19340 CAMSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE WORN A WVBA K NONE O OTHER IN INSP/MAINT 1 AL 01 3527U 836 317952141 L515561A AT 100-HOUR INSPECTION, DISCOVERED FERROUS METAL CONTAMINATION IN FILTER ELEMENT. PERFORMED VALVE CLEARANCE CHECK AND F OUND NR 5, NR 6 INTAKE LOBBS WITH EXCESSIVE CLELARANCE BASED ON A SIMILAR CIRCUMSTANCE. IT WAS DECIDED TO REMOVE THE EN GINE FROM SERVICE FOR CAMSHAFT REPLACEMENT. 1 L 7 2 3O 3 O A20SO E14EA 1999061800285 19990618 00285 WP 1999 6 18 TWAA9908301 1 19990611 A 3350 6100928 BULB DOUG DC9 DC983 3022083 WP ROW 4-11 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9407R 49400 THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROWS 4 TO 11. FOUNDS LAMPS BROKEN IN THE SOCKETS. REPLACED THE LAMPS. C HECK-C 5-1-99 STL. 2 L 7 2 4F RT A6WE 1999061800286 19990618 00286 NM 1999 6 18 HNAA9900068 1 19990613 A 3232 82970018013 ACTUATOR DHC DHAV DHC8 DHC8102 2809003 NM NR 2 MLG DOOR LEAKING A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 912HA 040 040 UPON GEAR RETRACTION THE RT MLG DOOR REMAINED OPEN. CYCLED GEAR, DOOR CLOSED NORMALLY. REMOVED AND REPLACED NR 2 MLG D OOR ACTUATOR. 2 H 7 2 4T RT A13NM 1999061800287 19990618 00287 WP 1999 6 18 AT9900439 1 19990515 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD ENTRY FLOOR PANEL NR 4693 AT LBL 45-65 CORRODED. REMOVE D FLOOR PANEL, FABRICATED, COUNTERSUNK, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-2, 53-21-0 F IG 2D. 2 L 7 2 4F A6WE 1999061800288 19990618 00288 WP 1999 6 18 AT9900440 1 19990508 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 196 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE CABIN ENTRY FLOOR SUPPORT UPPER FLANGE AT BS 196 BL 0-10L CORROD ED. REMOVED, FORMED, DRILLED AND INSTALLED SUPPORT IAW DC9 SRM 51-10-4, 51-30-5, 53-11-1 FIG 13, 51-10-2 AND 51-30-2. 2 L 7 2 4F A6WE 1999061800289 19990618 00289 WP 1999 6 18 AT9900441 1 19990530 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 928 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND ON THE LEFT MAIN CABIN AT BS 928 LONGERON NR 18 ATTACHED WEB CORRODE D. MECHANICALLY REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND FILLER, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 53-1 1-3, 51-10-3 AND 53-20-1. 2 L 7 2 4F A6WE 1999061800290 19990618 00290 WP 1999 6 18 AT9900442 1 19990609 A 5711 SPAR DOUG DC9 DC932 3022066 WP XRS 531.7-560 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT WING OUTBOARD TRAILING EDGE AFT UPPER SPAR CAP (TOP AND BOT TOM) AT XRS 531.7-560 CORRODED. REMOVED CORRODED SPAR CAP, SPLICED IN A NEW SECTION IAW DC9 SRM 57-09 FIG 24, 51-10-4, 51-10-3, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999061800291 19990618 00291 WP 1999 6 18 AT9900443 1 19990609 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 332 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD CARGO FLOORBEAM AT BS 332 CORRODED ON THE LEFT HAND SIDE . CUT OUT LOWER SECTION OF FLOORBEAM, FABRICATED REPAIR EXTRUSION, DOUBLERS AND ANGLE. ALODINED, PRIMED AND INSTALLED FABRICATED REPAIR PARTS IAW DC9 SRM 51-10-3, 53-01 FIG 1, AND TIMCO EO NR 99-1154. 2 L 7 2 4F A6WE 1999061800292 19990618 00292 WP 1999 6 18 AT9900444 1 19990609 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 313 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD CARGO FLOOR FRAME AT BS 313 LBL-48 ON THE LEFT SIDE AT S TAND OFF FOR HYDRAULIC LINES CORRODED. REMOVED STAND OFF, FABRICATED TWO REPAIR ANGLES AND INSTALLED REPAIR AND STAND O FF IAW DC9 SRM 51-30-1 AND TIMCO EO NR 99-1157. 2 L 7 2 4F A6WE 1999061800293 19990618 00293 WP 1999 6 18 AT9900445 1 19990605 A 5320 39120752N ANGLE DOUG DC9 DC932 3022066 WP BS 313 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD CARGO FLOOR FRAME AT LEFT HAND CUSP LINE AT BS 313 CORRO DED. REMOVED AND REPLACED ATTACHED ANGLE, ORDERED, DRILLED, DEBURRED AND INSTALLED IAW DC9 SRM 51-10-4, 51-30-1 AND 51- 30-5. 2 L 7 2 4F A6WE 1999061800294 19990618 00294 WP 1999 6 18 AT9900446 1 19990613 A 2560 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR DETACHED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 801AT 47275 ESCAPE SLIDE CAME OFF THE MAIN CABIN L-1 DOOR HOLDER. RESECURED SLIDE PACK PER MM 25-00. 2 L 7 2 4F A6WE 1999061800295 19990618 00295 NM 1999 6 18 CALA9900666 1 19990611 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 178 STRINGER 19L AND A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT ST A 178 STRINGER 19R. THE INTERCOSTALS WERE REMOVED AND REPLACED IAW ECRA 5310-01968. 2 L 7 2 4F RT A16WE 1999061800296 19990618 00296 WP 1999 6 18 CALA9900667 1 19990613 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 120.5 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 120.5 ABOVE LONGERON 19L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12 B. 2 L 7 2 4F A6WE 1999061800297 19990618 00297 NM 1999 6 18 CALA9900668 1 19990614 A 3350 20131A BATTERY PACK RADIANT BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 63305 23356 THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE IN MID CABIN. MAINTENANCE FOUND BATTERY PACK IN MID CABIN NOT TESTING. THE B ATTERY PACK WAS REMOVED AND REPLACED, OPERATION WAS NORMAL. 2 L 7 2 4F RT A16WE 1999061800298 19990618 00298 WP 1999 6 18 CALA9900669 1 19990614 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP L1 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14839 49635 A PREFLIGHT CHECK FOUND THE PORTABLE EMERGENCY LIGHT AT L-1 DOOR INOPERATIVE. THE PORTABLE EMERGENCY LIGHT WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1999061800299 19990618 00299 NM 1999 6 18 UPS99229801 1 19990609 A 5320 WEB BOEING 727 72725C 138400H NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: SI, CORROSION (C53-224-01.05-01) ON WEB BS 560 WL 208 LBL 48-58. CORROSION REMOVAL OUT OF LIMITS IAW S RM 53-10-1. REPAIRED WEB FROM STA 510-590 WL 208 LBL 48-58 IAW BFG ER NR 99-5507 (UPS FILE 727-53-2130). 2 L 7 3 4F A3WE 1999061800300 19990618 00300 NM 1999 6 18 UPS99229802 1 19990512 A 5330 SKIN BOEING 727 72725C 138400H NM BS 670 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, RULLED FASTENER HEAD IN CROWN SKIN AT BS 670 RBL 28 WL 203. REMOVED FASTENER HEAD AND FOUND INTERNA L LAP CORROSION. CUT OUT CORROSION AND REPAIRED LAP PER EO B727-5330-0509Q PP 83. 2 L 7 3 4F A3WE 1999061800301 19990618 00301 NM 1999 6 18 UPS99429804 1 19990612 A 3350 69B4601014 MODULE BOEING 747 747121 1384871 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST UK UNKNOWN 1 SO 01 682UP 20349 INSPECTION TYPE:N/A, EMERGENCY LIGHTS UNARMED ANNUNCIATOR ILLUMINATED WHEN SWITCH PLACED TO ARMED POSITION. REPLACED EM ERGENCY LIGHT CONTROL PANEL PER M/M 33-51-09, OPS CKS OK. 2 L 7 4 4F A20WE 1999061800302 19990618 00302 WP 1999 6 18 ABXA9900446 1 19990421 A 5320 5614160 SHEAR TIE DOUG DOUG DC8 DC863 302198A WP BS 55 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 SHEAR TIE CRACKED AT LONGERON 33 LEFT AND STATION 55. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5614160. 2 L 7 4 4F 4A25 1999061800303 19990618 00303 WP 1999 6 18 ABXA9900447 1 19990427 A 5712 5769700 RIB DOUG DOUG DC8 DC863 302198A WP WS 616.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 616.25 AT LOWER FASTENERS. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K0505 6. 2 L 7 4 4F 4A25 1999061800304 19990618 00304 WP 1999 6 18 ABXA9900448 1 19990427 A 5712 5759545 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 772.5, AFT LOWER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K5056. 2 L 7 4 4F 4A25 1999061800305 19990618 00305 WP 1999 6 18 ABXA9900449 1 19990427 A 5712 5759545 RIB DOUG DOUG DC8 DC863 302198A WP WS 622.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 622.5, AFT LOWER FASTENER. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K0505 6. 2 L 7 4 4F 4A25 1999061800306 19990618 00306 WP 1999 6 18 ABXA9900450 1 19990426 A 5712 576947121 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING OUTBOARD LEADING EDGE, LOWER RIB CRACKED AT STATION XFS 772.5. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056. 2 L 7 4 4F 4A25 1999061800307 19990618 00307 NM 1999 6 18 99ZZZX2322 1 19990511 A 2530 FAN HE61090 BOEING 757 75723N 1384973 NM NR 4 OVEN INOPERATIVE A AMTA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 522AT 134877 29330 DURING CRUISE AT FL 41.0, ODOR WAS NOTICED IN AFT GALLEY, SMELLED LIKE PLASTIC MELTING. DIVERTED TO SALT LAKE CITY, WIT HOUT FURTHER INCIDENT. FOUND THE NR 4 OVEN FAN INOPERATIVE, OVEN WAS REPLACED, OPS CHECKED GOOD. 2 L 7 2 4F RT A2NM 1999061800308 19990618 00308 NM 1999 6 18 99ZZZX2323 1 19990415 A 4950 DUCT BOEING 757 75723N 1384973 NM APU CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 519AT 27975 DURING PRE-FLIGHT, FOUND THE APU TEE DUCT FORWARD OF SURGE VALVE CRACKED. REPLACED TEE DUCT, REPAIRED THREAD INSERTS, O PS CHECKED NORMAL, NO LEAKS NOTED. 2 L 7 2 4F RT A2NM 1999061800309 19990618 00309 NM 1999 6 18 AALA990629 1 19990318 A 3350 TERMINAL BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 181AN 29591 DFW - FLT 9661 - EMERGENCY LIGHTS ILLUMINATED DURING TAKEOFF ROLL. EMERGENCY LIGHTS EXTINGUISHING ON THEIR OWN. AIRCRA FT WAS MAINTENANCE FERRIED TO AFW FOR REPAIRS. MAINTENANCE FOUND TERMINAL LUG LOOSE AT GROUND 3774. SECURED LOSE TERMI NAL LUG AT GROUND 3774. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999061800310 19990618 00310 NM 1999 6 18 AALA990632 1 19990318 A 3350 P4010049 BATTERY BOEING 757 757223 1384957 NM BS 1634 DISCHARGED A AALA K NONE L NO TEST TO TAKEOFF 1 SW 07 181AN 11437 29591 LAX - FLT 1225 - EMERGENCY EXIT LIGHTS FLICKERED DURING TAKEOFF AND CONTINUED TO FLICKER THE REMAINDER OF THE FLIGHT. M AINTENANCE TROUBLESHOT SYSTEM AND FOUND WEAK EMERGENCY BATTERY PACK. REPLACED EMERGENCY BATTERY PACK. SYSTEM GROUND CH ECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999061800311 19990618 00311 NM 1999 6 18 AALA990631 1 19990316 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 181AN 29591 FLT 3116 - EMERGENCY EXIT LIGHTS FLICKERED DURING TAKEOFF AND REMAINED OFF THE REMAINDER OF THE FLIGHT. SYSTEM WAS PLAC ARDED INOPERABLE AND DEFERRED PER MEL. DFW MAINTENANCE TROUBLESHOT SYSTEM AND ACCOMPLISHED REQUIRED TESTS. UNABLE TO D UPLICATE FAULT. REMOVED PLACARD AND CLEARED MIC SHEET. SYSTEM GROUND CHECKED, NORMAL OPERATION. SECURED LOOSE GROUND LUG ON 3-18-99. (X) 2 L 7 2 4F RT A2NM 1999061800312 19990618 00312 NM 1999 6 18 AALA990634 1 19990308 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST TO TAKEOFF 1 SW 07 181AN 29591 GCM - FLT 0828 - EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY DURING TAXI, TAKEOFF ROLL, AND IN-FLIGHT. MAINTENANCE INSP ECTED EMERGENCY LIGHT SYSTEM AND WAS UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999061800313 19990618 00313 NM 1999 6 18 AALA990635 1 19990307 A 3397 WIRE BOEING 757 757223 1384957 NM ROW 16 BROKEN A AALA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 181AN 29591 DFW - FTL 2099 - EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATED INTERMITTENTLY IN AFT COACH CABIN. MAINTENANCE INSPECTED EMERGENCY LIGHT SYSTEM AND FOUND A BREAK IN FLAT WIRE. REPAIRED BREAK IN FLAT WIRE AT PASSENGER SEAT ROW 16. AS A PREC AUTIONARY, BATTERY PACKS WERE REPLACED. SYSTEM GROUND CHECKED, NORMAL OPERATION. SECURED LOOSE GROUND LUG ON 3-18-99. (X) 2 L 7 2 4F RT A2NM 1999061800314 19990618 00314 WP 1999 6 18 AALA990526 1 19990415 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP EMERGENCY EXIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7534A 2676 49988 PHX - FLT 1982 - DURING PRE-FLIGHT, FORWARD EMERGENCY WALK-AROUND LIGHT WOULD NOT TURN OFF. REPLACED FORWARD EMERGENCY DOOR EMERGENCY WALK-AROUND LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999061800315 19990618 00315 SO 1999 6 18 C2XA99IA260 1 19990505 A 3350 GE1317 BULB EMB 145 EMB145 SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14960 145100 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999061800316 19990618 00316 CE 1999 6 18 99ZZZX2324 1 19990504 A 7120 2452064 BOLT BEECH 1900 1900D 1154162 CE RT ENG TRUSS LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17541 UE203 AXO - DURING A SCHEDULED INSPECTION, THE LOWER OUTBOARD TRUSS BOLT WAS FOUND LOOSE ON THE RIGHT HAND ENGINE. MAINTENANC E REMOVED AND REPLACED THE LOWER OUTBOARD TRUSS BOLT NUT AND RETAINER ON THE RIGHT HAND ENGINE IAW B1900 MM 71-20-00, AN D EA NR 7120-01018. AIRCRAFT RELEASED FOR SERVICE. AIRCRAFT TT: 6,847.0 HOURS. TOTAL CYCLES: 8,145. 2 L 7 2 4T RT A24CE 1999061800317 19990618 00317 CE 1999 6 18 99ZZZX2325 1 19990508 A 3260 1013841377 SWITCH BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 69547 1127A UE189 CLE - FLT 3178 - CREW REPORTED THEY HAD A RED GEAR UNSAFE LIGHT THAT WOULD NOT EXTINGUISH UPON GEAR RETRACTION. AIRCRAF T DIVERTED TO CVG WITHOUT FURTHER INCIDENT, THE AIRCRAFT WAS THEN MAINTENANCE FERRIED TO CLE. MAINTENANCE REMOVED AND R EPLACED THE LANDING GEAR CONTROL SWITCH IAW B1900 MM 32-60-00, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. AIRCRAFT TT: 7,282.8 HOURS. TOTAL CYCLES: 9,056. (X) 2 L 7 2 4T RT A24CE 1999061800318 19990618 00318 NM 1999 6 18 99ZZZX2326 1 19990411 A 2740 AJH73781 PIN DOUG DC10 DC1040F 3023507 NM HORIZ STABILIZER SHEARED A CLCA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 19 140WE 46920 SVMI/SKBO - FLT 113 - STABILIZER JAMMED AT 2 UNITS NOSE UP WHILE MAKING APPROACH. FOUND SHEAR PIN SHEARED ON HORIZONTAL STABILIZER DRIVE UNIT. REPLACED HORIZONTAL STABILIZER CHAIN DRIVE UNIT PER AMM 27-44-05. CONDUCTED TEST FLIGHT. ALL SYSTEMS OPERATED SATISFACTORY. (X) 2 L 7 3 4F TR A22WE 1999061800320 19990618 00320 EU 1999 6 18 R7MA0000635 1 19990423 A 6220 1090110821 BUSHING AGUSTA A109 A109K2 0260502 EU M/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 10018 MRH SWASHPLATE FIXED SCISSORS. REPLACED BEARINGS. 1 G 7 2 3U RT H7EU 1999061800321 19990618 00321 EU 1999 6 18 R7MA0000621 1 19990419 A 6220 1090101433 BUSHING AGUSTA A109 A109K2 0260502 EU M/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX A04102 10018 BUSHING WORN AND GROOVED BEYOND LIMITS. (X) 1 G 7 2 3U RT H7EU 1999061800322 19990618 00322 EU 1999 6 18 R7MA0000622 1 19990419 A 6220 1090101433 BUSHING AGUSTA A109 A109K2 0260502 EU M/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 10018 BUSHING WORN AND GROOVED BEYOND LIMITS. (X) 1 G 7 2 3U RT H7EU 1999061800323 19990618 00323 EU 1999 6 18 R7MA0000628 1 19990423 A 6220 709010118105 ROD ENDS AGUSTA A109 A109K2 0260502 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 10018 ROD ENDS WORN. REPLACED FOUR EACH. (X) 1 G 7 2 3U RT H7EU 1999061800324 19990618 00324 EU 1999 6 18 R7MA0000629 1 19990422 A 6220 109011073109 ROD END AGUSTA A109 A109K2 0260502 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 256 C18805 10018 ROD END WORN. (X) 1 G 7 2 3U RT H7EU 1999061800325 19990618 00325 EU 1999 6 18 R7MA0000642 1 19990427 A 2913 807712 DRIVE COUPLING AGUSTA A109 A109K2 0260502 EU HYDRAULIC PUMP WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 10018 SPLINES WORN BEYOND TOLERANCE. (X) 1 G 7 2 3U RT H7EU 1999061800326 19990618 00326 NE 1999 6 18 99ZZZX2328 2 19990328 A 7230 411104059 LABYRINTH SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER WARPED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 1775 7077 LE45111EA LABYRINTH SEAL HAD EXCESSIVE WARPAGE WHICH RESULTED IN COLLATERAL DAMAGE TO THE GP ROTOR AND SHROUD. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999061800327 19990618 00327 NE 1999 6 18 99ZZZX2329 2 19990328 A 7230 411105067 BLADE BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 755 BE9396 7077 LE45111EA SECONDARY DAMAGE TO LAB SEAL FAILURE. EXCESSIVE DAMAGE TO KNIFE EDGES AND GP BLADES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 1,061.9. 1 G 7 2 3U 3 U H13EU E5NE 1999061800328 19990618 00328 NE 1999 6 18 99ZZZX2330 2 19990328 A 7230 411100720 SHROUD BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 755 7077 LE45111EA SECONDARY DAMAGE TO LAB SEAL FAILURE. EXCESSIVE GROOVES RESULTING FROM GP BLADE DAMAGE. REPLACED WITH NEW UNIT, CORREC TED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999061800329 19990618 00329 1999 6 18 F3LA99040 4 19990508 A 2210 158300101 ACTUATOR BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US 34167 387 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT ABOUT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMMANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINE D CONTROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOV ERED/REGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SY S). AUTOPILOT AILERON ACTUATOR CONNECT (A-SYS). REF: OPER CNTRL NR 99ZZZX2331THRU 99ZZZX2337. (X) 2 L 7 2 4F RT A16WE 1999061800330 19990618 00330 1999 6 18 99ZZZX2331 4 19990508 A 2210 DG1035A803 ADAPTER BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US 11530 564 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT ABOUT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMMANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINE D CONTROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOV ERED/REGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SY S). AUTOPILOT AILERON ACTUATOR CONNECT (A-SYS). REF: OPER CNTRL F3LA99040, AND, NR 99ZZZX2332 THRU 99ZZZX2337. 2 L 7 2 4F RT A16WE 1999061800331 19990618 00331 1999 6 18 99ZZZX2332 4 19990508 A 2210 D1827 CONNECTOR BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US 2993 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT ABOUT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMMANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINE D CONTROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOV ERED/REGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SY S). AUTOPILOT AILERON ACTUATOR CONNECT (A-SYS. REF: OPER CNTRL F3LA99040, AND, NR 99ZZZ2331 THRU 99ZZZX2337. 2 L 7 2 4F RT A16WE 1999061800332 19990618 00332 1999 6 18 99ZZZX2333 4 19990508 A 2210 211C233278 SWITCH BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US H00185A 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT ABOUT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMMANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINE D CONTROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOV ERED/REGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SY S). AUTOPILOT AILERON ACTUATOR CONNECT (A-SYS). CYCLES, 1,243. REF: OPER CNTRL F3LA99040, AND, NR 99ZZZX2331 THRU 9 2 L 7 2 4F RT A16WE 1999061800333 19990618 00333 1999 6 18 99ZZZX2334 4 19990508 A 2210 4051600913 COMPUTER BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US 928 91102640 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT ABOUT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMMANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINE D CONTROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOV ERED/REGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SY S). AUTOPILOT AILERON ACTUATOR CONNECT (A-SYS). REF: OPER CNTRL F3LA99040, AND, NR 99ZZZX2331 THRU 99ZZZX2337. 2 L 7 2 4F RT A16WE 1999061800334 19990618 00334 1999 6 18 99ZZZX2335 4 19990508 A 2210 4051600912 COMPUTER BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US 189 88031182 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMM ANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINED CONT ROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOVERED/R EGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SYS). A UTOPILOT AILERON ACT CONNECT (A-SYS). CYCLES: 80. REF: OPER CNTRL F3LA99040, AND, NR 99ZZZX2331 THRU 99ZZZX2337. 2 L 7 2 4F RT A16WE 1999061800335 19990618 00335 1999 6 18 99ZZZX2336 4 19990508 A 2210 65C370539 PCU BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US 598 262 1665ASSC 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT ABOUT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMMANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINE D CONTROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOV ERED/REGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SY S). AUTOPILOT AILERON ACTUATOR CONNECT (A-SYS). REF: OPER CNTRL F3LA99040, AND, NR 99ZZZX2331 THRU 99ZZZX2337. 2 L 7 2 4F RT A16WE 1999061800336 19990618 00336 1999 6 18 99ZZZX2337 4 19990508 A 2210 4030952906 YAW DAMPENER BOEING 737 737301 1384611 NM AFCS MALFUNCTIONED A L F3LA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 03 578US 2259 91023314 23257 DEN - FLT 520 - CREW REPORTED WHILE CLIMBING THROUGH FL 210, ACFT ROLLED 10 DEGREES RT, THEN 20 DEGREES LT, THEN ROLLED WINGS LEVEL. AT ABOUT FL 230, ACFT STARTED TO FLUTTER FROM LT TO RT ON THE RUDDER. 1-2 SECONDS LATER, ACFT STARTED AN UNCOMMANDED ROLL TO THE LT. TURNED AUTOPILOT AND AUTO THROTTLES OFF, TURNED CONTROL YOKE RT, PUSHED RT RUDDER AND GAINE D CONTROL OF ACFT. CREW REPORTED HANDS AND FEET WERE NOT ON CNTRLS UNTIL AUTOPILOT DISENGAGED, THEN CREW MANUALLY RECOV ERED/REGAINED CONTROL. MAINT REPLACED AUTOPILOT AILERON ACTUATOR (B-SYS) AUTOPILOT AILERON ACTUATOR PRESS SWITCH (B-SY S). AUTOPILOT AILERON ACTUATOR CONNECT (A-SYS). REF: OPER CNTRL F3LA99040, AND, NR 99ZZZX2331 THRU 99ZZZX2336. 2 L 7 2 4F RT A16WE 1999061800337 19990618 00337 NM 1999 6 18 SWAA991000 1 19990611 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701GS 27836 FWD SECTION OF EMERGENCY ESCAPE FLOOR TRACK LIGHTING DAMAGED. REPAIRED BROKEN WIRE PER MM. 2 L 7 2 4F RT A16WE 1999061800338 19990618 00338 NM 1999 6 18 SWAA991001 1 19990612 A 3260 65C28034 SENSOR BOEING 737 7373Y0 1384671 NM LT MLG INOPERATIVE A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 682SW 23496 AIR DIVERTION-- AT CRUISE ALTITUDE LT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED AND REMAINED LIT UNTIL THE GEAR WA S LOWERED. REMOVED AND REPLACED LT MAIN GEAR UPLOCK SENSOR AND LOGIC CARD. 2 L 7 2 4F RT A16WE 1999061800339 19990618 00339 1999 6 18 SWAA991003 4 19990613 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 625SW 27701 FWD ENTRY DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY. 2 L 7 2 4F RT A16WE 1999061800340 19990618 00340 NM 1999 6 18 SWAA991004 1 19990611 A 5320 6558280 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 14R-15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999061800341 19990618 00341 NM 1999 6 18 SWAA991005 1 19990611 A 5311 6546569 FRAME BOEING 737 7372T4 1384492 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME BS 967, LBL 1, WL 177. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1999061800342 19990618 00342 NM 1999 6 18 SWAA991006 1 19990611 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM BS 433-436 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER 24R , BS 433-436. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999061800343 19990618 00343 NM 1999 6 18 SWAA991007 1 19990611 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM PASSENGER DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BOTH FWD ENTRY DOOR GIRT BAR FLOOR ATTACH BRACKETS. REMOVED AND REPLAC ED BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 1999061800344 19990618 00344 1999 6 18 SWAA991008 4 19990611 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999061800345 19990618 00345 NM 1999 6 18 SWAA991009 1 19990611 A 3350 6104781 BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED BATT ERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999061800346 19990618 00346 NM 1999 6 18 SWAA991010 1 19990612 A 5241 BAC1505 FRAME BOEING 737 7373H4 1384600 NM GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY DOOR, LOWER FWD FRAME CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999061800347 19990618 00347 NM 1999 6 18 SWAA991011 1 19990613 A 3350 900835A BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED RON CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999061800348 19990618 00348 NE 1999 6 18 SWAA991012 2 19990613 A 7261 494379 FILTER BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE DIRTY A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 080SW 22675 687783 INFLIGHT SHUT DOWN---- NR 1 ENG OIL FILTER BYPASS INDICATOR ILLUMINATED. REMOVED AND REPLACED NR 1 ENG MAIN OIL FILTER PER MM, DUE TO CARBON DEPOSIT. 2 L 7 2 4F 4 F A16WE E2EA 1999061800349 19990618 00349 NM 1999 6 18 SWAA991013 1 19990614 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM BS 980 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN, BS 980 STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999061800350 19990618 00350 NM 1999 6 18 SWAA991002 1 19990615 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 750 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 750, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999061800351 19990618 00351 NM 1999 6 18 HNAA9900067 1 19990613 A 3231 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM RT MLG MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 912HA 040 RT MAIN LANDING GEAR DOOR DID NOT CLOSE AFTER RETRACTION. CYCLED GEAR AND OK. 2 H 7 2 4T RT A13NM 1999061800352 19990618 00352 NM 1999 6 18 HNAA9900069 1 19990614 A 2770 85520147105 BUMPER DHC 85520001002 DHAV DHC8 DHC8102 2809003 NM ELEV GUST LOCK MISSING A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 RT ELEV SPRING TAB HAS SHEET METAL DAMAGE. RT ELEV UPPER GUST LOCK BUMPER IS MISSING RT ELEV I/B CAP IS DAMAGED. REMOV ED AND REPLACED RT SPRING TAB. INSTALLED GUST LOCK BUMPER. REMOVED AND REPLACED RT ELEVATOR I/B END CAP. 2 H 7 2 4T RT A13NM 1999061800353 19990618 00353 SO 1999 6 18 LR7A9950 1 19990612 A 6120 5825855 VALVE HAMSTD 54H60117 LKHEED 382 382G 526414U SO NR 4 PROPELLER DEFECTIVE A LR7A E ENGINE SHUTDOWN O OTHER CL CLIMB 1 AL 03 401LC 2719 233251 4606 DURING CLIMBOUT FROM BET, NR 4 ENGINE SHUTDOWN AT 1455Z DUE RPM UNCONTROLLABLE. AIRCRAFT CONTINUED TO ANC AND LANDED WI THOUT FURTHER INCIDENT. REPLACED DEFECTIVE NR 4 PROPELLER VALVE HOUSING IAW HN61135. RUN-UP OK IAW HN 7101. 2 H 7 4 4T A1SO 1999061800354 19990618 00354 NM 1999 6 18 AWXA9900221 1 19990613 A 2530 416000123 COFFEEMAKER BOEING 737 737301 1384611 NM GALLEY MALFUNCTIONED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 326AW 23258 ON CLIMB 24000 FT, F/A REPORTED BURNING ELECTRICAL SMELL NEAR L1. PRIOR TO AIR TURNBACK, ACFT RETURNED TO GATE BECAUSE OF ELECTRICAL SMELL IN CABIN NEAR DOOR L1. REMOVED AND REPLACED THE NR 1 COFFEEMAKER. PROBLEM WAS AN EXPOSED HEAT ELEM ENT. RAN BOTH ENGINES TO 70 PERCENT N1, SWAPPED BETWEEN BLEED SOURCES FOR 10 MIN, INSPECTED FWD FLT HANDSET ALCOVE, FOR WARD LAV, EE COMPT, FWD BAG PIT, NO SMOKING, FASTEN SEAT BELT SIGNS, BOTH FWD GALLEY COFFEEMAKERS AND FWD GALLEY BREAKER PANEL ABOVE COFFEEMAKERS. DROPPED CEILING PANEL IN FWD GALLEY, COULD NOT DUPLICATE ON GROUND. NEXT, CONDUCTED A TEST FLIGHT AS PRECAUTION TO CONFIRM GROUND FINDING FOR BURNING ELECTRICAL SMELL NEAR L1 DOOR. NO ELECTRICAL SMELL NOTED DUR 2 L 7 2 4F RT A16WE 1999061800355 19990618 00355 NM 1999 6 18 RAAA99B2044 1 19990611 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 22 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999061800356 19990618 00356 SO 1999 6 18 RAAA99E9020 1 19990426 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 920 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 2 CHECK, FOUND FS 920 FRAME CORRODED FROM STR 34 TO 39 ON INSIDE FLANGE BETWEEN FRAMES. CUT OUT COR RODED AREA OF FRAME AND INSTALLED SPLICE IAW SRM 53-2-3, TREATED AND PRIMED. 2 L 7 4 4T 4A22 1999061800357 19990618 00357 SO 1999 6 18 RAAA99E9021 1 19990611 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO PASSENGER DOOR INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FORWARD PAX DOOR PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1999061800358 19990618 00358 SO 1999 6 18 COMA9910093 1 19990612 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT LATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 256CA 120245 DOORS WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT CLOSED PROPERLY. CLOSED AND LATCHED FUEL SERVICE PANEL. 2 L 7 2 4T RT A31SO 1999061800359 19990618 00359 EA 1999 6 18 COMA9960256 1 19990613 A 5320 601R5361117 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 7169 AIRCRAFT CAME IN FOR 24 MONTH CHECK WITH DMI 205443 FLOOR SUPPORT ANGLE AT FS 621.0 LHS CRACKED. REMOVED AND REPLACED F LOOR SUPPORT ANGLE AT FS 621.0 (P/N 601R-53-61-117) IAW CRJ REO 601R53-61-117 ATTACHED. 2 L 7 2 4F RT A21EA 1999061800360 19990618 00360 EA 1999 6 18 COMA9960257 1 19990608 A 5313 STRINGER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 DOUBLER AFT OF FS 718 HAS APPROX 4 INCH CRACK IN RADIUS AT STRINGER 11. REPAIRED PER WVAC EO NR 601R-53-0058. 2 L 7 2 4F RT A21EA 1999061800361 19990618 00361 EA 1999 6 18 COMA9960258 1 19990608 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 FRAME FLANGE AT FS 718 LT HAS A CRACK THROUGH ONE OF THE FASTENER HOLES JUST BELOW STRINGER 11. TEMPORARILY REPAIRED IA W WVAC EO 601R-53-00560. MUST BE PERMANENTLY REPAIRED NO LATER THAN NEXT C-CHECK. 2 L 7 2 4F RT A21EA 1999061800362 19990618 00362 EA 1999 6 18 COMA9960259 1 19990608 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 FRAME FLANGE AT FS 718 RT HAS A CRACK THROUGH ONE OF THE FASTENER HOLES. REPAIRED PER WVAC EO 601R-53-0057. 2 L 7 2 4F RT A21EA 1999061800363 19990618 00363 EA 1999 6 18 COMA9960260 1 19990610 A 5240 H500020641115 MECHANISM CNDAIR CL600 CL6002B19 EA OXYGEN DOOR NOT LATCHED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 956CA 7105 OXYGEN SERVICE DOOR CAME OPEN IN FLIGHT. REPLACED 02 DOOR LATCH. 2 L 7 2 4F RT A21EA 1999061800364 19990618 00364 EA 1999 6 18 COMA9960261 1 19990610 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 769CA 7292 FLAPS FAILED AFTER LANDING. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999061800365 19990618 00365 EA 1999 6 18 COMA9960262 1 19990610 A 3260 864202 PROX SENSOR CNDAIR CL600 CL6002B19 EA NLG DOOR OUT OF ADJUST A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 917CA 7017 NOSE GEAR WOULD NOT COME DOWN ON APPROACH TO CVG. FOLLOWED QRH, CYCLED GEAR, NOSE GEAR INDICATED DOWN AND LOCKED. CHEC KED CLEARANCE ON NLG PROX SENSORS, ADJUSTED P519GA NLG FWD DOOR. C/W FUNCTIONAL TEST OF LANDING GEAR. 2 L 7 2 4F RT A21EA 1999061800366 19990618 00366 EA 1999 6 18 COMA9960263 1 19990607 A 3150 6229810012 DISPLAY CNDAIR CL600 CL6002B19 EA RT COCKPIT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 817 7141 NR 2 ED WENT BLANK DURING TAKE FF. TAKEOFF CONFIG WARNING. COULD NOT DUPLCIATE SPOILER CONFIG WARNING. REPLACED NR 2 ED. 2 L 7 2 4F RT A21EA 1999061800367 19990618 00367 EA 1999 6 18 COMA9960264 1 19990612 A 5270 601R576891103 HARNESS CNDAIR CL600 CL6002B19 EA CARGO DOOR DAMAGED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 958CA 7111 PROXIMITY SYSTEM FAULT MESSAGE. REPLACED THE CARGO DOOR WIRING HARNESS. 2 L 7 2 4F RT A21EA 1999061800368 19990618 00368 EA 1999 6 18 COMA9960265 1 19990611 A 3220 16400103 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 924CA 9563 713 7026 GEAR DISAGREE WARNING, NLG TOOK A LONG TIME TO RETRACT AND MADE A LOT OF NOISE. REPLACED THE NLG DRAG BRACE. 2 L 7 2 4F RT A21EA 1999061800369 19990618 00369 EA 1999 6 18 COMA9960266 1 19990611 A 3220 16400103 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 01 924CA 9563 7026 FLIGHT DIVERTED BACK TO CVG DUE TO NOSE GEAR DISAGREE. REMOVED AND REPLACED NOSE LANDING GEAR DRAG BRACE. 2 L 7 2 4F RT A21EA 1999061800370 19990618 00370 EA 1999 6 18 COMA9960267 1 19990606 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PASSENGER DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 PAX DOOR SEAL STRIKER AT FS 3100 PREVIOUS REPAIR IS DAMAGED. REPAIRED PER REO 601R-52-11-008, REPAIR C. 2 L 7 2 4F RT A21EA 1999061800371 19990618 00371 EA 1999 6 18 COMA9960268 1 19990606 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PASSENGER DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 PAX DOOR SEAL STRIKER AT FS 349 IS DAMAGED. REPAIRED PER REO 601R-52-11-00 REPAIR A. 2 L 7 2 4F RT A21EA 1999061800372 19990618 00372 EA 1999 6 18 COMA9960269 1 19990606 A 5230 600351663 BRACKET CNDAIR CL600 CL6002B19 EA CARGO DOOR MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 CARGO DOOR STOP BRACKET IS MISSING. INSTALLED CARGO DOOR STOP BRACKET. 2 L 7 2 4F RT A21EA 1999061800373 19990618 00373 EA 1999 6 18 COMA9960270 1 19990608 A 4980 601R9720413 SHIELD CNDAIR CL600 CL6002B19 EA APU COMPT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 APU EXHAUST SHIELD HAS A CRACK AT THE 7 O'CLOCK POSITION. REPAIRED PER CANADAIR REO 601R-49-81-003. 2 L 7 2 4F RT A21EA 1999061800374 19990618 00374 EA 1999 6 18 COMA9960271 1 19990607 A 4980 600971083 DUCT CNDAIR CL600 CL6002B19 EA APU EXHAUST BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 APU EXHAUST DUCT HAS SEVERAL BROKEN FINGER CLAMP STOPS. REPLACED EXHAUST DUCT. 2 L 7 2 4F RT A21EA 1999061800375 19990618 00375 EA 1999 6 18 COMA9960272 1 19990607 A 2710 272005 PCU CNDAIR CL600 CL6002B19 EA RT AILERON LEAKING A COMA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 01 945CA 12669 7069 RIGHT AILERON OUTBOARD PCU LEAKING BEYOND LIMITS. REPLACED PCU. 2 L 7 2 4F RT A21EA 1999061800376 19990618 00376 EA 1999 6 18 COMA9960273 1 19990605 A 5753 601R1430342 CAP CNDAIR CL600 CL6002B19 EA RT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 RIGHT INBOARD FLAP MOVABLE CAP IS CHAFED. BLENDED AND TREATED PER WVAC REO 601R-57-0060. REPAIR IS ACCEPTABLE FOR 1000 FLIGHT HOURS. 2 L 7 2 4F RT A21EA 1999061800377 19990618 00377 EA 1999 6 18 COMA9960274 1 19990605 A 5753 601R1430341 CAP CNDAIR CL600 CL6002B19 EA LT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 LEFT INBOARD FLAP MOVABLE CAP IS CHAFED. BLENDED AND TREATED PER WVAC REO 601R-57-0060. REPAIR IS ACCEPTABLE FOR 1000 FLIGHT HOURS. 2 L 7 2 4F RT A21EA 1999061800378 19990618 00378 EA 1999 6 18 COMA9960275 1 19990615 A 4930 69254517 VALVE CNDAIR CL600 CL6002B19 EA APU MALFUNCTIONED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 713CA 7245 RAMP ATTENDANT ADVISED GLOW ILLUMINATING FROM APU EXHAUST 20 MINUTES AFTER IT WAS SHUT DOWN. NO EVIDENCE OF FIRE FOUND. REMOVED AND REPLACED APU FUEL SOLENOID VALVE FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1999061800379 19990618 00379 EA 1999 6 18 COMA9960276 1 19990615 A 3240 HP13332003 VALVE CNDAIR CL600 CL6002B19 EA NR 2 BRAKE MALFUNCTIONED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 975CA 7150 LOUD SQUEAL FROM NOSE AREA WHEN RIGHT BRAKE APPLIED. REMOVED AND REPLACED NR 2 BRAKE CONTROL VALVE. 2 L 7 2 4F RT A21EA 1999061800380 19990618 00380 NM 1999 6 18 UPS99229806 1 19990531 A 2710 FITTING BOEING 727 72731C 1384011 NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, RIGHT I/B AILERON TAB PUSHROD MAST FITTING CORRODED. RIGHT I/B AILERON TAB MAST IS REPLACED IAW S RM 51-30-2. 2 L 7 3 4F A3WE 1999061800381 19990618 00381 NM 1999 6 18 UPS99229807 1 19990531 A 5752 HINGE BOEING 727 72731C 1384011 NM RT AILERON TAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, RIGHT I/B AILERON TAB O/B HINGE CORRODED (CASTING). REPAIR CARRIED OUT IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999061800382 19990618 00382 NM 1999 6 18 UPS99229808 1 19990531 A 5320 SUPPORT BOEING 727 72731C 1384011 NM BS 1010 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, BROKEN DUCTING SUPPORT AT LT BS 1010 LBL 42.5. DUCTING SUPPORT REPLACED, FABRICATED IAW SRM 51-20 -1. 2 L 7 3 4F A3WE 1999061800383 19990618 00383 NM 1999 6 18 UPS99229809 1 19990529 A 5260 ANGLE BOEING 727 72731C 1384011 NM AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, CORROSION ON RISER FACE ABOVE NR 14 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551 -A. 2 L 7 3 4F A3WE 1999061800384 19990618 00384 NM 1999 6 18 UPS99229810 1 19990529 A 5260 ANGLE BOEING 727 72731C 1384011 NM AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, CORROSION EVIDENT ON RISER FACE ABOVE NR 13 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5 260-7551-A. 2 L 7 3 4F A3WE 1999061800385 19990618 00385 NM 1999 6 18 UPS99229811 1 19990529 A 5260 ANGLE BOEING 727 72731C 1384011 NM AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, CORROSION ON FACE OF RISER ABOVE NR 12 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7 551-D. 2 L 7 3 4F A3WE 1999061800386 19990618 00386 NM 1999 6 18 UPS99229812 1 19990529 A 5260 ANGLE BOEING 727 72731C 1384011 NM AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, CORROSION ON FACE OF RISER ABOVE NR 11 FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551-A. 2 L 7 3 4F A3WE 1999061800387 19990618 00387 NM 1999 6 18 UPS99229813 1 19990529 A 5260 ANGLE BOEING 727 72731C 1384011 NM AIRSTAIRS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, RISER SURFACE CORRODED ABOVE NR 10 STAIRTHREAD FWD SUPPORT ANGLE. REPAIRED IAW EO B727-5260-7551- A. 2 L 7 3 4F A3WE 1999061800388 19990618 00388 NM 1999 6 18 UPS99229814 1 19990527 A 5754 SKIN BOEING 727 72731C 1384011 NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C+SI, NR 6 LE SLAT O/B TRACK SKIN TO TRACK ATTACH BRACKETS CRACKED. BRACKETS REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1999061800389 19990618 00389 NM 1999 6 18 UPS99229832 1 19990613 A 3350 LIGHT BOEING 727 72731C 1384011 NM FLIGHT DECK LOOSE A IPXA K NONE L NO TEST TO TAKEOFF 1 SO 01 925UP 19230 INSPECTION TYPE:N/A, DURING TAKEOFF THE FLIGHT DECK EMERGENCY LIGHT FELL OFF MOUNT. REINSTALLED EMERGENCY EXIT LIGHT AS SY, OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 1999061800390 19990618 00390 NM 1999 6 18 UPS99229833 1 19990612 A 3350 1000679 LIGHT BOEING 727 72730C 1384009 NM FLIGHT DECK MISSING A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY LIGHT MISSING. REPLACED EMERGENCY LIGHT PACK IAW MM 33-50-01, OPS CKS GOOD P ER MM 33-50-01. (P/N 10-0067-9), (S/N 10894) INSTALLED. 2 L 7 3 4F A3WE 1999061800391 19990618 00391 WP 1999 6 18 UPS99829815 1 19990526 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 467.323 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT THE AFT END, STA XS467.323. STOP DRILLED CRACK AND REPAIRED I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999061800392 19990618 00392 WP 1999 6 18 UPS99829816 1 19990526 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 360.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT STA XFS 360.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2 -0 FIG 2. 2 L 7 4 4F RT 4A25 1999061800393 19990618 00393 WP 1999 6 18 UPS99829817 1 19990526 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 354 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT STA XFS 354.000. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2 -0 FIG 2. 2 L 7 4 4F RT 4A25 1999061800394 19990618 00394 WP 1999 6 18 UPS99829818 1 19990526 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 422.185 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, LT CENTER L/E UPPER RIB IS CRACKED AT STA XS 422.185. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 1999061800395 19990618 00395 WP 1999 6 18 UPS99829819 1 19990528 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, STA 980 AT LBL 9.5, THE FLOORBEAM FLANGE FWD SIDE HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 705- 484. 2 L 7 4 4F RT 4A25 1999061800396 19990618 00396 WP 1999 6 18 UPS99829820 1 19990524 A 5320 37778742N FITTING DOUG DC8 DC871F 302199D WP BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, LONGERON 19L INTERCOSTAL ATTACH FITTING IS CRACKED AT STA 840. REMOVED AND REPLACED FITTING IAW DWG 3777874 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999061800397 19990618 00397 WP 1999 6 18 UPS99829821 1 19990527 A 5311 5764343507N FRAME DOUG DC8 DC871F 302199D WP BS 1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, FRAME CAP AT STA 1120 STR 31L-31R IS CORRODED AND CRACKED. REMOVED AND REPLACED CAP IAW DWG 5764343 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999061800398 19990618 00398 WP 1999 6 18 UPS99829822 1 19990524 A 5320 37798741 FITTING DOUG DC8 DC871F 302199D WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, FRAME 759 ATTACH FITTING IS CRACKED AT STR 13L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 37 79874. 2 L 7 4 4F RT 4A25 1999061800399 19990618 00399 WP 1999 6 18 UPS99829823 1 19990523 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, RT WING SKIN IS CRACKED AT STA XRS 74.0 AND STR 12. REPAIRED AREA IAW SRM 57-2-1-FIG 10. 2 L 7 4 4F RT 4A25 1999061800400 19990618 00400 WP 1999 6 18 UPS99829824 1 19990524 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 710 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, RT WING O/B LEADING EDGE HAS HEAVY CORROSION AT STA XFS 710.000. REPAIRED AREA IAW SRM 57-2-1 FIG 2 H. 2 L 7 4 4F RT 4A25 1999061800401 19990618 00401 WP 1999 6 18 UPS99829825 1 19990524 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1734 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, STA 1734 AT STR 25R HAS HEAVY CORROSION (FRAME). REPAIRED AREA IAW SRM 53-2-0 FIG 2 AND 53-5-1. 2 L 7 4 4F RT 4A25 1999061800402 19990618 00402 WP 1999 6 18 UPS99829826 1 19990523 A 5320 4646163501N FITTING DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, STA 440-460, STR 29L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4646163 AND SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999061800403 19990618 00403 WP 1999 6 18 UPS99829827 1 19990523 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, STA 480 AT STR 36 THE FRAME HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999061800404 19990618 00404 WP 1999 6 18 UPS99829828 1 19990526 A 5720 97532977 ANGLE DOUG DC8 DC871F 302199D WP WS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, LT CENTER LEADING EDGE O/B VERTICAL ATTACH ANGLE AT I/B SIDE OF NR 1 STUB WING AT STA XS 520.00 IS C RACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297. 2 L 7 4 4F RT 4A25 1999061800405 19990618 00405 WP 1999 6 18 UPS99829829 1 19990523 A 5320 37734792N FITTING DOUG DC8 DC871F 302199D WP BS 580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, FLOORBEAM ATTACH FITTING AT STA 580 AND STR 21R HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLAC ED FITTING IAW DWG 3773479 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999061800406 19990618 00406 WP 1999 6 18 UPS99829830 1 19990524 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, STA 1520 AT RBL 59, THE SEAT TRACK MOUNTING FLANGE HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 705 -154. 2 L 7 4 4F RT 4A25 1999061800407 19990618 00407 WP 1999 6 18 UPS99829831 1 19990524 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 630-640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:C1, STA 630-640 BETWEEN STR 34L-35R, THE EXTERNAL SKIN HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 705 -552. 2 L 7 4 4F RT 4A25 1999061800408 19990618 00408 NE 1999 6 18 QXEA9901271 2 19990608 A 7532 310848501 P2.5 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE MALFUNCTION A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 815PH 50 BOI- STRONG SMELL OF OIL WHEN THE POWER LEVERS RETARDED TO FLIGHT IDLE. MAINTENANCE PERFORMED A BLEED AIR TEST AND FOUN D THE SMELL WAS FROM NR 1 BLEED. REPLACED THE NR 1 P2.5 SWITCHING VALVE, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 1999061800409 19990618 00409 NM 1999 6 18 QXEA9901275 1 19990606 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 345PH 5030 476 SEA- LEFT AFT EXTERIOR EMERGENCY LIGHT IS INOP. MAINTENANCE REPLACED P5 POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHEC KS GOOD. 2 H 7 2 4T RT A13NM 1999061800410 19990618 00410 NM 1999 6 18 QXEA9901277 1 19990607 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 353PH 9740 7751 496 SEA- 2 RED FLOOR EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED THE EMERGENCY BATTERY AT POSITION P5-6, OPERATIONAL CH ECKS GOOD. 2 H 7 2 4T RT A13NM 1999061800411 19990618 00411 EU 1999 6 18 QXEA9901163 1 19990525 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 12414 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ON STRINGER 43 APPROXIMATELY 3 INCHES AFT OF FRAME 12414. REPAIRED IAW FOKKER SRM 53-10-4, PAG E 9, PARAGRAPH 4B AND SRM 53-10-4 PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1999061800412 19990618 00412 EU 1999 6 18 QXEA9901164 1 19990529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 12853 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ON FRAME 12853 AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 3. 2 L 7 2 4F RT A20EU 1999061800413 19990618 00413 EU 1999 6 18 QXEA9901165 1 19990602 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 12853 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ON FRAME 12853 FROM STRINGER 41 TO STRINGER 45. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 53-01- 01. 2 L 7 2 4F RT A20EU 1999061800414 19990618 00414 EU 1999 6 18 QXEA9901166 1 19990523 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ON FRAME 12875 BETWEEN STRINGERS 31 AND 32. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999061800415 19990618 00415 EU 1999 6 18 QXEA9901167 1 19990519 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ALONG LENGTH OF STRINGER 30 BETWEEN FRAME 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-04, P AGE 8 AND 9, PARAGRAPHS 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800416 19990618 00416 EU 1999 6 18 QXEA9901168 1 19990519 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ON STRINGER 29 AT FORWARD END BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-04 , PAGES 8-9 PARAGRAPH 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800417 19990618 00417 EU 1999 6 18 QXEA9901169 1 19990520 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ALONG LENGTH OF STRINGER 31 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800418 19990618 00418 EU 1999 6 18 QXEA9901170 1 19990519 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ALONG STRINGER 32 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-4, PAGES 8-9, PARAGRAPH 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800419 19990618 00419 EU 1999 6 18 QXEA9901171 1 19990519 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ALONG STRINGER 33 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-10-4, PAGES 8-9, PARAGRAPH 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800420 19990618 00420 EU 1999 6 18 QXEA9901172 1 19990522 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ON THE AFT SIDE OF FRAME 15635 AND BOTH SIDE OF STRINGER 34. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9, PARAGRAPH 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800421 19990618 00421 EU 1999 6 18 QXEA9901173 1 19990520 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 15635 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS CORROSION ALONG STRINGER 45 BETWEEN FRAMES 15635 AND 16060. REPAIRED IAW FOKKER SRM 51-31-0, PAGES 1-10 AND SRM 51-10-04, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1999061800422 19990618 00422 EU 1999 6 18 QXEA9901174 1 19990527 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12414 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME CLIP ON FRAME 12414 IS CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800423 19990618 00423 EU 1999 6 18 QXEA9901175 1 19990525 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 34 FORWARD END, 2.5 INCHES AFT OF FRAME 4900 HAS EXFOLIATION CORROSION. REPAIRED IAW FOKKER SRM 53-02-06 . 2 L 7 2 4F RT A20EU 1999061800424 19990618 00424 EU 1999 6 18 QXEA9901176 1 19990531 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 41 FORWARD END, 2.5 INCHES AFT OF FRAME 4900 HAS EXFOLIATION CORROSION. REPAIRED IAW FOKKER SRM 53-02-06 , FIGURE 1E. 2 L 7 2 4F RT A20EU 1999061800425 19990618 00425 EU 1999 6 18 QXEA9901177 1 19990522 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 5805 CORRODED OUTBOARD FLANGE FORWARD SIDE FROM STRINGER 27 TO 29. REPAIRED IAW FOKKER SRM 51-10-04, PAGES 8-9, PARAGRAPHS 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800426 19990618 00426 EU 1999 6 18 QXEA9901178 1 19990517 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 5305 CORRODED ON AFT SIDE OF INBOARD AND OUTBOARD FLANGE FROM STRINGER 32 TO 35. REPAIRED IAW FOKKER SRM 51 -10-04, PAGES 8-9 AND PARAGRAPHS 3C AND 4B. 2 L 7 2 4F RT A20EU 1999061800427 19990618 00427 EU 1999 6 18 QXEA9901179 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 32 HAS CRACK/CORROSION AT HOLE, 9.7 FORWARD OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE . 2 L 7 2 4F RT A20EU 1999061800428 19990618 00428 EU 1999 6 18 QXEA9901180 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 32 HAS CRACK/CORROSION AT HOLE, 2.7 INCHES FORWARD OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06, FIGU RE 1 EE. 2 L 7 2 4F RT A20EU 1999061800429 19990618 00429 EU 1999 6 18 QXEA9901181 1 19990525 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 34 CRACK/CORROSION AT HOLE, 2.6 INCHES AFT OF FRAME 5305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE. 2 L 7 2 4F RT A20EU 1999061800430 19990618 00430 EU 1999 6 18 QXEA9901182 1 19990514 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 7805 CLIP CRACKED AT STRINGER 44 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800431 19990618 00431 EU 1999 6 18 QXEA9901183 1 19990530 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 46 HAS CORROSION/CRACK AT HOLE, 10 INCHES AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3. 2 L 7 2 4F RT A20EU 1999061800432 19990618 00432 EU 1999 6 18 QXEA9901184 1 19990514 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 47 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800433 19990618 00433 EU 1999 6 18 QXEA9901185 1 19990530 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 46 HAS CORROSION/CRACK AT HOLE, 2.8 INCHES AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3. 2 L 7 2 4F RT A20EU 1999061800434 19990618 00434 EU 1999 6 18 QXEA9901186 1 19990529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 11253 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 9805 AT STATION 11253 HAS CORROSION AT DOUBLER BELOW STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999061800435 19990618 00435 EU 1999 6 18 QXEA9901187 1 19990527 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU BS 10753 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - DOME NUT PLATE 4 AFT OF FRAME 9305C AT STATION 10753 ON STRINGER 37 HAS SURFACE CORROSION. REPAIRED IAW FOKKER SR M 51-10-04, PAGE 8, PARAGRAPH 3C, SRM 51-31-01 PAGE 13, PARAGRAPH B. 2 L 7 2 4F RT A20EU 1999061800436 19990618 00436 NM 1999 6 18 99FDEA00217 1 19990614 A 5315 ADA8404U4715 FLOORBEAM DOUG MD11 MD11F 3023600 NM BS 939 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 FWD CARGO DOOR ENTRY MID UPPER FLOORBEAM LWR CHORD AT BS 939, X=78.0, RHS FOUND WITH ABOUT ONE-INCH CRACK AND DENT. *S/ D* CARRIED OUT REPAIR ON FWD CARGO DOOR IN ACCORDANCE WITH FEDEX AUTH NR 1-5310-42383. 2 L 7 3 4F RT A22WE 1999061800437 19990618 00437 NM 1999 6 18 99FDEA00218 1 19990615 A 5311 9052691 FRAME BOEING 727 72725 1384006 NM BS 970 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 CRACK INDICATION AT BS 970 FRAME, BOTTOM HOLE OF FRAME TO STRINGER 9L. 2 L 7 3 4F A3WE 1999061800438 19990618 00438 NM 1999 6 18 99FDEA00219 1 19990615 A 5320 65184156 WEB BOEING 727 72725 1384006 NM BS 309 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 FOUND CORROSION (C53-224-03) AND GOUGE ON VERTICAL WEB NEAR RT TRUNNION BOLT HOLE BS 309, RBL 14, WL 169. 2 L 7 3 4F A3WE 1999061800439 19990618 00439 NM 1999 6 18 99FDEA00220 1 19990615 A 5315 652082724 FLOORBEAM BOEING 727 72725 1384006 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 639 - WHILE WORK NR 284 FOUND CORROSION ON FLOORBEAM, BS 560, RBL 10-12, WL 208. REPAIRED FLOORBEAM IAW FEDEX SRM 53 -10-8 AND 51-30-2. 2 L 7 3 4F A3WE 1999061800440 19990618 00440 NM 1999 6 18 99FDEA00221 1 19990615 A 5320 65198622 CHORD BOEING 727 72725 1384006 NM BS 304-314 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 CORROSION (C53-224-03) PREVIOUS BLEND ON RT MID NOSE, BS 304-314, RBL 20, WL 170. 2 L 7 3 4F A3WE 1999061800441 19990618 00441 WP 1999 6 18 ABXA990451 1 19990611 A 5610 4653608 LATCH DOUG DOUG DC9 DC941 302207N WP RT COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. FOUND UPPER LATCHING BAYONET OUT OF ADJUSTMENT. ADJUSTED LINKAGE, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999061800442 19990618 00442 WP 1999 6 18 ABXA9900452 1 19990423 A 5712 5769589 RIB DOUG DOUG DC8 DC863 302198A WP WS 304 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 304. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999061800443 19990618 00443 WP 1999 6 18 ABXA9900453 1 19990423 A 5712 5769589 RIB DOUG DOUG DC8 DC863 302198A WP WS 360.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING LEADING EDGE RIB CRACKED, UPPER END AT STATION XFS 360.250. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999061800444 19990618 00444 WP 1999 6 18 ABXA9900454 1 19990423 A 5712 5769589 RIB DOUG DOUG DC8 DC863 302198A WP WS 354 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING CENTER LEADING EDGE UPPER RIB CRACKED AT STATION XFS 354. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999061800445 19990618 00445 WP 1999 6 18 ABXA9900455 1 19990423 A 5712 5769589 RIB DOUG DOUG DC8 DC863 302198A WP WS 366.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT CENTER WING LEADING EDGE UPPER RIB CRACKED AT FASTENER END AT STATION XFS 366.5. REPAIRED IAW DWG K05056. 2 L 7 4 4F 4A25 1999061800446 19990618 00446 WP 1999 6 18 ABXA9900456 1 19990429 A 5712 57701533 RIB DOUG DOUG DC8 DC863 302198A WP WS 195 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46093 LEFT WING LEADING EDGE UPPER RIB CRACKED AT FASTENER END AT STATION XFS 195. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999061800447 19990618 00447 WP 1999 6 18 ABXA9900457 1 19990430 A 5512 5654500405 SKIN DOUG DOUG DC8 DC863 302198A WP RT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE CRACKED AT INBOARD END. REPAIRED IAW DC8 SRM 51-1-11 AND 51-1-21A. 2 L 7 4 4F 4A25 1999061800448 19990618 00448 WP 1999 6 18 ABXA9900458 1 19990430 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP WS 603.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 603.75 AT AFT UPPER FASTENER. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999061800449 19990618 00449 WP 1999 6 18 ABXA9900459 1 19990422 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP WS 641.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB AT STATION XFS 641.25 CRACKED AT AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1999061800450 19990618 00450 WP 1999 6 18 ABXA9900460 1 19990430 A 5712 5769589 RIB DOUG DOUG DC8 DC863 302198A WP WS 407 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RT WING CENTER LEADING EDGE HAD CRACKED SUPPORT RIB AT STA XW 407. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056. 2 L 7 4 4F 4A25 1999061800451 19990618 00451 WP 1999 6 18 ABXA9900461 1 19990430 A 5320 2755342505 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 CRACKED FITTING AT LONGERON 27 LEFT AND STATION 1180. REPLACED FITTING IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999061800452 19990618 00452 WP 1999 6 18 TWAA9908401 1 19990615 A 3350 BATTERY DOUG DC9 DC983 3022083 WP ROW 7-10 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9407R 49400 THE EGRESS LIGHTS AT ROW 7 TO 10 STAYED ON WITH THE SWITCH SELECTED TO OFF. RESEATED THE BATTERIES IN THE POWER PACK AN D OPERATION WAS NORMAL. CHECK-C 5-1-99 STL. 2 L 7 2 4F RT A6WE 1999061800453 19990618 00453 NM 1999 6 18 CALA9900670 1 19990614 A 5320 FRAME BOEING 737 7373T0 1384582 NM LT COCKPIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND A .5 INCH CRACK IN CAPTAIN'S WINDOW FRAME. REPAIRED IAW ECRA 5330-02824. 2 L 7 2 4F RT A16WE 1999061800454 19990618 00454 WP 1999 6 18 CALA9900671 1 19990614 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 230 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 230. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999061800455 19990618 00455 NM 1999 6 18 CALA9900672 1 19990615 A 3350 900835A BATTERY PACK AVIALL BOEING 727 727224 1384076 NM RT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND THE RT AFT OVERWING EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED IAW MM 33-50-01. 2 L 7 3 4F A3WE 1999061800456 19990618 00456 WP 1999 6 18 CALA9900673 1 19990615 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1204 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND A 4 INCH CRACK IN LONGERON 29L SPLICE AT STA 1204. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999061800457 19990618 00457 WP 1999 6 18 CALA9900674 1 19990615 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 200-237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND THE LT FUSELAGE SKIN DENTED AT STA 200-237, LONGERON 17L. THE DENTED AREA WAS CUT OUT. A REPAIR WAS I NSTALLED IAW SRM 51-10-2 AND 53-04, FIGURE 47. 2 L 7 2 4F A6WE 1999061800458 19990618 00458 WP 1999 6 18 CALA9900675 1 19990615 A 5712 RIB DOUG DC9 DC932 3022066 WP WS 410 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND A .25 INCH CRACK IN RT WING L/E RIB AT XFS 410 I/B OF NR 4 SLAT O/B HINGE. THE CRACK WAS STOP DRILLED IAW SRM 57-01, PAGE 9. AN ANGLE REPAIR WAS INSTALLED IAW SRM 57-30-2 AND 57-01, PAGE 9. 2 L 7 2 4F A6WE 1999061800459 19990618 00459 WP 1999 6 18 CALA9900676 1 19990615 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 239 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 239 BETWEEN LONGERON 17L AND 18L. A NEW DOUBLER WAS INSTALLED IAW SRM 53-3 0-05. 2 L 7 2 4F A6WE 1999061800460 19990618 00460 WP 1999 6 18 CALA9900677 1 19990615 A 5280 FRAME DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND THE LEFT I/B MLG DOOR CRACKED AT FORWARD AND LOWER FRAME. THE CRACKS WERE .5 ICNH LONG. THE DOOR FRAM E WAS REPAIRED IAW ECRA 5280-01200. 2 L 7 2 4F A6WE 1999061800461 19990618 00461 WP 1999 6 18 CALA9900678 1 19990615 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 1111-1251 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND AFT CARGO COMPARTMENT LOWER DOOR JAMB AT THRESHOLD CORRODED THE ENTIRE LENGTH AT FS 1111-1251, LONGERON 28R. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 1999061800462 19990618 00462 WP 1999 6 18 CALA9900679 1 19990615 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1022-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND AFT CARGO RT FRAME TRACK CORRODED AT FS 1022-1155, LONGERON 27R. THE CARGO TRACK WAS REMOVED AND REPLA CED IAW SRM 53-24-0. 2 L 7 2 4F A6WE 1999061800463 19990618 00463 WP 1999 6 18 CALA9900680 1 19990615 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 598-760 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND THE RIGHT O/B SEAT TRACK CORRODED FROM STA 598-760, RBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IA W SRM 53-05, FIGURE 4, VIEW E. 2 L 7 2 4F A6WE 1999061800464 19990618 00464 WP 1999 6 18 CALA9900681 1 19990615 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1271-1300 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED FROM STA 1271-1300, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW S RM 51-30-1. 2 L 7 2 4F A6WE 1999061800465 19990618 00465 WP 1999 6 18 CALA9900682 1 19990616 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 210 & 229 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED IN TWO PLACES AT STA 210 AND 229, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999061800466 19990618 00466 WP 1999 6 18 CALA9900683 1 19990616 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 210 & 229 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND THE RIGHT O/B SEAT TRACK CORRODED IN TWO PLACES AT STA 210 & 229, RBL 48. THE SEAT TRACK WAS REMOVED A ND REPLACED IAW SRM 51-30-1 AND SRM 53-05, FIGURE 4A. 2 L 7 2 4F A6WE 1999061800467 19990618 00467 WP 1999 6 18 CALA9900684 1 19990616 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1117-1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND THE LEFT I/B SEAT TRACK CORRODED FROM STA 1117-1136, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED I AW SRM 53-30-2. 2 L 7 2 4F A6WE 1999061800468 19990618 00468 WP 1999 6 18 CALA9900685 1 19990616 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1200-1215 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED FROM STA 1200-1215, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IA W SRM 51-30-1. 2 L 7 2 4F A6WE 1999061800469 19990618 00469 WP 1999 6 18 CALA9900686 1 19990616 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174-1202 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57837 49582 INSPECTION FOUND THE LEFT O/B SEAT TRACK CORRODED FROM STA 1174-1202, LBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED I AW SRM 51-30-1 AND 53-05-04. 2 L 7 2 4F A6WE 1999061800470 19990618 00470 NM 1999 6 18 CALA9900687 1 19990616 A 3350 900835A BATTERY PACK AVIALL BOEING 727 727232 1384082 NM RT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND THE R-2 DOOR EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPER ATION CHECKED GOOD IAW MM 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061800471 19990618 00471 NM 1999 6 18 CALA9900688 1 19990616 A 3350 900835A BATTERY PACK AVIALL BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND LT CENTER OVERWING EMERGENCY EXIT LIGHT FLASHING. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTA LLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061800472 19990618 00472 NM 1999 6 18 CALA9900689 1 19990616 A 3350 900835A BATTERY PACK AVIALL BOEING 727 727232 1384082 NM EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND MAIN CABIN EXIT LIGHT AT OVERWING EXIT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINS TALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061800473 19990618 00473 NM 1999 6 18 CALA9900690 1 19990616 A 3350 900835A BATTERY PACK AVIALL BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND THE LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REI NSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-00. 2 L 7 3 4F A3WE 1999061800474 19990618 00474 NM 1999 6 18 CALA9900691 1 19990616 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 19 & 20 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND EMERGENCY PATH LIGHTING AT ROW 19 AND 20 INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061800475 19990618 00475 NM 1999 6 18 CALA9900692 1 19990616 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 28 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND EMERGENCY PATH LIGHTING AT SEAT ROW 28 INOPERATIVE. WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501. 2 L 7 3 4F A3WE 1999061800476 19990618 00476 NM 1999 6 18 CALA9900693 1 19990616 A 5330 SKIN BOEING 727 727232 1384082 NM BS 360 BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND RT FUSELAGE BELLY SKIN BULGED AT FS 360 AFT OF MLG. A REPAIR WAS INSTALLED IAW SRM 51-10-1, 51-10-2, A ND 51-30-2. 2 L 7 3 4F A3WE 1999061800477 19990618 00477 NM 1999 6 18 9902042286 1 19990609 A 2912 FILTER BOEING 727 727251 138408H NM A HYD SYS LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 286US 21325 ON APPROACH, 'A' SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. HOWEVER, PRESSURE ON 'A' SYSTEM REMAINED GOOD. CREW DECLARED AN EMERGENCY AND LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE FOUND A LEAK IN THE ELEVATOR PCU FILTER HOUSING. REPLAC ED FILTER HOUSING, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999061800478 19990618 00478 NM 1999 6 18 9902056311 1 19990611 A 2910 HYD LINE BOEING 747 747451 1384940 NM NR 3 PYLON LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 611US 745 24225 DURING CLIMB, THE NR 3 HYDRAULIC SYSTEM LOST FLUID. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. RETORQUED HY DRAUALIC SUPPLY LINE IN THE NR 3 PYLON, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999061800479 19990618 00479 NM 1999 6 18 9902065527 1 19990613 A 2130 VALVE BOEING 757 757251 1384970 NM PRESSURE SYS FAILED A NWAA B EMER. DESCENT O OTHER DE DESCENT 1 GL 01 527US 23842 DURING DESCENT INTO DTW, THE CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS 10,000 FEET. AN EMERGENCY DESCENT WAS INITIATED FROM FL240 TO 10,000 FEET. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BO TH PRESSURE RELIEF VALVES WITH SERVICEABLE UNITS. 2 L 7 2 4F RT A2NM 1999061800480 19990618 00480 WP 1999 6 18 9902079152 1 19990613 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE CHECK, FOUND CATWALK EMERGENCY EXIT PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATION AL CHECK OK. 2 L 7 2 4F A6WE 1999061800481 19990618 00481 EU 1999 6 18 QXEA9901188 1 19990523 A 5311 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 9305 HAS CRACKED CLIP AT STRINGER 32 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800482 19990618 00482 EU 1999 6 18 QXEA9901189 1 19990529 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 9305 HAS CRACKED CLIP AT STRINGER 28 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800483 19990618 00483 EU 1999 6 18 QXEA9901190 1 19990522 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805, 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND CABIN STRINGER 28 CORRODED BETWEEN FRAMES 8805 AND 9305. REPAIRED IAW FOKKER SRM 53-02-0, FIGURE 1EE. 2 L 7 2 4F RT A20EU 1999061800484 19990618 00484 EU 1999 6 18 QXEA9901191 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND CABIN STRINGER 32 CORRODED AT HOLE, 2.6 FORWARD FRAME 9305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1E E. 2 L 7 2 4F RT A20EU 1999061800485 19990618 00485 EU 1999 6 18 QXEA9901192 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND CABIN STRINGER 32 CORRODED AT HOLE, 9.7 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE. 2 L 7 2 4F RT A20EU 1999061800486 19990618 00486 EU 1999 6 18 QXEA9901193 1 19990523 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND CABIN STRINGER 30 HAS CRACK WITH CORROSION AT HOLE, 9.7 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-0 6, FIGURE 1BB. 2 L 7 2 4F RT A20EU 1999061800487 19990618 00487 EU 1999 6 18 QXEA9901194 1 19990523 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND CABIN STRINGER 31 HAS CRACK WITH CORROSION AT HOLE, 6.3 AFT FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-0 6, FIGURE 1EE. 2 L 7 2 4F RT A20EU 1999061800488 19990618 00488 EU 1999 6 18 QXEA9901195 1 19990522 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND CABIN FRAME 8805 HAS CORROSION ON TOP/OUTBOARD FLANGE AFT SIDE FROM STRINGER 30 TO 34. REPAIRED IAW FOK KER SRM 51-10-04, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999061800489 19990618 00489 EU 1999 6 18 QXEA9901196 1 19990524 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - OVERHEAD BIN OUTBOARD ATTACH AT FRAME 8305 BETWEEN STRINGER 47 AND 48 IS LOOSE. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1, 2, 3, 5. 2 L 7 2 4F RT A20EU 1999061800490 19990618 00490 EU 1999 6 18 QXEA9901197 1 19990530 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 46 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999061800491 19990618 00491 EU 1999 6 18 QXEA9901198 1 19990523 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7305-7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 30 IS CRACKED AT INSULATION FASTENER HOLE MID WAY BETWEEN FRAME 7305 AND 7805. REPAIRED IAW FOKKER SRM 5 3-02-06, FIGURE 1BB. 2 L 7 2 4F RT A20EU 1999061800492 19990618 00492 EU 1999 6 18 QXEA9901199 1 19990604 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND CABIN FRAME 8305 IS CORRODED ON AFT SIDE AT SPLICE NEAR STRINGER 18. REPAIRED IAW HORIZON AIR EA 4-53-8 22. 2 L 7 2 4F RT A20EU 1999061800493 19990618 00493 EU 1999 6 18 QXEA9901200 1 19990522 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 18 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800494 19990618 00494 EU 1999 6 18 QXEA9901201 1 19990522 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 28 IS CORRODED AT CRACKED INSULATION FASTENER HOLE, 2.5 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06 , FIGURE 1EE. 2 L 7 2 4F RT A20EU 1999061800495 19990618 00495 EU 1999 6 18 QXEA9901202 1 19990522 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 28 CORRODED AT CRACKED INSULATION FASTENER HOLE, 2.8 FORWARD FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-0 6, FIGURE 1EE. 2 L 7 2 4F RT A20EU 1999061800496 19990618 00496 EU 1999 6 18 QXEA9901203 1 19990525 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 35 CRACKED AT INSULATION FASTENER HOLE, 6.6 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIG URE 1BB. 2 L 7 2 4F RT A20EU 1999061800497 19990618 00497 EU 1999 6 18 QXEA9901204 1 19990530 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 34 CRACKED A INSULATION FASTENER HOLE, 8.8 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3. 2 L 7 2 4F RT A20EU 1999061800498 19990618 00498 EU 1999 6 18 QXEA9901205 1 19990530 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 34 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3. 2 L 7 2 4F RT A20EU 1999061800499 19990618 00499 EU 1999 6 18 QXEA9901206 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 8.8 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE . 2 L 7 2 4F RT A20EU 1999061800500 19990618 00500 EU 1999 6 18 QXEA9901207 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1EE . 2 L 7 2 4F RT A20EU 1999061800501 19990618 00501 EU 1999 6 18 QXEA9901208 1 19990523 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 32 CRACKED AT INSULATION FASTENER HOLE, 1.8 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIG URE 1EE. 2 L 7 2 4F RT A20EU 1999061800502 19990618 00502 EU 1999 6 18 QXEA9901209 1 19990523 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 31 CRACKED AT INSULATION FASTENER HOLE, 6.3 FORWARD OF FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIG URE 1EE. 2 L 7 2 4F RT A20EU 1999061800503 19990618 00503 EU 1999 6 18 QXEA9901210 1 19990530 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 30 CORROSION AT CRACKED INSULATION FASTENER HOLE, 1.7 AFT FRAME 8305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1BB. 2 L 7 2 4F RT A20EU 1999061800504 19990618 00504 EU 1999 6 18 QXEA9901211 1 19990525 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME HAS SURFACE CORROSION ON TOP/OUTBOARD FLANGE FROM STRINGER 43 TO 44. REPAIRED IAW FOKKER SRM 53-10-4, PAGE 8-9, PARAGRAPHS EC AND 4B. 2 L 7 2 4F RT A20EU 1999061800505 19990618 00505 EU 1999 6 18 QXEA9901212 1 19990514 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 CRACKED CLIP AT STRINGER 45 RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800506 19990618 00506 EU 1999 6 18 QXEA9901213 1 19990524 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 44 AT RIVET. REPAIRED IAW FOKKER SRM 51-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800507 19990618 00507 EU 1999 6 18 QXEA9901214 1 19990514 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 HAS CRACKED CLIP AT STRINGER 43 AT RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800508 19990618 00508 EU 1999 6 18 QXEA9901215 1 19990522 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 28 IS CRACKED AT INSULATION FASTENER HOLE, 2.7 AFT OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGU RE 1EE. 2 L 7 2 4F RT A20EU 1999061800509 19990618 00509 EU 1999 6 18 QXEA9901216 1 19990514 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 7805 HAS CRACKED CLIP AT STRINGER 43 AT RIVET. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999061800510 19990618 00510 EU 1999 6 18 QXEA9901217 1 19990522 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 28 CORRODED AT CRACK 8.7 AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B. 2 L 7 2 4F RT A20EU 1999061800511 19990618 00511 EU 1999 6 18 QXEA9901218 1 19990522 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 28 CRACKED AT INSULATION FASTENER HOLE, 1.7 AFT OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B. 2 L 7 2 4F RT A20EU 1999061800512 19990618 00512 EU 1999 6 18 QXEA9901219 1 19990522 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7305-7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 28 HAS CORROSION WITH CRACKS AT TWO INSULATION FASTENER HOLES BETWEEN FRAMES 7305 AND 7805. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION B-B, FIGURE 1EE. 2 L 7 2 4F RT A20EU 1999061800513 19990618 00513 EU 1999 6 18 QXEA9901220 1 19990525 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - SURFACE CORROSION ON FRAME 7805 ON TOP FLANGE BELOW STRINGER 41 THROUGH 43, 44 AND 45. REPAIRED IAW FOKKER SRM 51 -10-4, PAGE 8-9 AND PARAGRAPHS 4B AND 3C. 2 L 7 2 4F RT A20EU 1999061800514 19990618 00514 EU 1999 6 18 QXEA9901221 1 19990523 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON FRAME 7805 BOTTOM FLANGE JUST BELOW STRINGER 37. REPAIRED IAW FOKKER SRM 51-10-04, PAG E 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999061800515 19990618 00515 EU 1999 6 18 QXEA9901222 1 19990525 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT-HAND CABIN FRAME 7805 HAS CORROSION ON TOP FLANGE BELOW STRINGER 31 THROUGH 33. REPAIRED IAW FOKKER SRM 51- 10-4, PAGE 9, PARAGRAPH A-B, STEPS 1 AND 2. 2 L 7 2 4F RT A20EU 1999061800516 19990618 00516 EU 1999 6 18 QXEA9901223 1 19990525 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND FORWARD CABIN STRINGER 36 HAS ONE CRACK AT INSULATION FASTENER HOLE, 1.7 FORWARD OF FRAME 7805. REPAIRE D IAW FOKKER SRM 53-02-06, FIGURE 1 EE. 2 L 7 2 4F RT A20EU 1999061800517 19990618 00517 EU 1999 6 18 QXEA9901224 1 19990525 A 5310 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7305-7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND FORWARD CABIN STRINGER 35 HAS 2 CRACKS BETWEEN FRAMES 7305 AND 7805. ONE AT THE INSULATION FASTENER HOL E AND ONE 1.3 FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1 EE. 2 L 7 2 4F RT A20EU 1999061800518 19990618 00518 EU 1999 6 18 QXEA9901225 1 19990530 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND FORWARD CABIN STRINGER 34 HAS TWO CRACKS AT INSULATION HOLES, 1.7 FORWARD OF FRAME 7805 AND 3.9 FORWARD OF FRAME 7805. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3. 2 L 7 2 4F RT A20EU 1999061800519 19990618 00519 EU 1999 6 18 QXEA9901226 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT-HAND CABIN STRINGER 41 HAS CORROSION DAMAGE LOCATED JUST ABOVE FRAME 6805 AND 2.9 FORWARD OF EXISTING REPAIR . REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, SECTION A-A, FIGURE 1. 2 L 7 2 4F RT A20EU 1999061800520 19990618 00520 EU 1999 6 18 QXEA9901227 1 19990524 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT-HAND FORWARD CABIN STRINGER 44 HAS TWO CRACKS BETWEEN FRAMES 6805 AND 7305. ONE CRACK AT EACH INSULATION FA STENER HOLE. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3. 2 L 7 2 4F RT A20EU 1999061800521 19990618 00521 EU 1999 6 18 QXEA9901228 1 19990602 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRETTING CORROSION AROUND BOLT HOLES AT PANEL 24B ON INSIDE OF PANEL. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PA RAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999061800522 19990618 00522 EU 1999 6 18 QXEA9901229 1 19990531 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER NAV/COMM 1 ANTENNA PLATE. REPAIRED IAW HORIZON AIR EA 4-53-8 11. 2 L 7 2 4F RT A20EU 1999061800523 19990618 00523 EU 1999 6 18 QXEA9901230 1 19990526 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - CENTER CARGO DOOR APERTURE DOES NOT ALLOW FOR USE OF STANDARD HARDWARE. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999061800524 19990618 00524 EU 1999 6 18 QXEA9901231 1 19990530 A 5230 DOUBLER FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AFT CARGO DOOR HAS A CRACK IN REPAIR DOUBLER AT NUT PLATE HOLE FOR STAY FITTING. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999061800525 19990618 00525 EU 1999 6 18 QXEA9901232 1 19990525 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 53-02-01, PAG E 6, FIGURE 4 AND SRM 53-00-00, PAGE 2. 2 L 7 2 4F RT A20EU 1999061800526 19990618 00526 EU 1999 6 18 QXEA9901233 1 19990521 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER ATC ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAG RAPH 4. 2 L 7 2 4F RT A20EU 1999061800527 19990618 00527 EU 1999 6 18 QXEA9901234 1 19990524 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON FUSELAGE SKIN UNDER LOWER NAV/COMM 1 ANTENNA BLANKING PLATE. REPAIRED IAW FOKKER SRM 5 3-02-01, PAGE 6 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999061800528 19990618 00528 EU 1999 6 18 QXEA9901235 1 19990521 A 5320 MOUNTS FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON FUSELAGE MOUNTS FOR BLANKING PLATES BY RAD ALT ANTENNAS. REPAIRED IAW FOKKER SRM 51-10 -4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999061800529 19990618 00529 EU 1999 6 18 QXEA9901236 1 19990521 A 5320 MOUNTS FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON BOTH RAD ALT FUSELAGE MOUNTING BASES. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRA PH 4. 2 L 7 2 4F RT A20EU 1999061800530 19990618 00530 EU 1999 6 18 QXEA9901237 1 19990524 A 5320 MOUNT FOKKER F28 F28MK4000 4990810 EU CORRODED CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LIGHT SURFACE CORROSION ON LOWER NR 1 DME FUSELAGE MOUNTING BASE. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGR APH 4 B 112 C. 2 L 7 2 4F RT A20EU 1999061800531 19990618 00531 WP 1999 6 18 ABXA9900462 1 19990503 A 5511 56545124 RIB DOUG DOUG DC8 DC863 302198A WP RT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT HORIZONTAL STABILIZER LEADING EDGE HAD CRACKED LOWER RIB AT STATION FS 122. REPAIRED IAW DC8 SRM 55-2-0 AND 51-1- 8. 2 L 7 4 4F 4A25 1999061800532 19990618 00532 WP 1999 6 18 ABXA9900463 1 19990501 A 5730 57699855 SKIN DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT INBOARD SLOT VANE OUTER SKIN CRACKED AT INBOARD END. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999061800533 19990618 00533 WP 1999 6 18 ABXA9900464 1 19990501 A 5730 57696004 SKIN DOUG DOUG DC8 DC863 302198A WP WS 674 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE UPPER SKIN CRACKED AT STATION FS 674. REPAIRED IAW DC8 SRM 57-2-1 AND 51-1-21. 2 L 7 4 4F 4A25 1999061800534 19990618 00534 WP 1999 6 18 ABXA9900465 1 19990424 A 5712 9753297 RIB DOUG DOUG DC8 DC863 302198A WP WS 456 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT CENTER LEADING EDGE OUTBOARD VERTICAL RIB CRACKED AT STATION XRS 456. REPAIRED IAW DC8 SRM 57-3-3 AND DWG 9753297. 2 L 7 4 4F 4A25 1999061800535 19990618 00535 WP 1999 6 18 ABXA9900466 1 19990423 A 5712 5769589 RIB DOUG DOUG DC8 DC863 302198A WP WS 360.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING LEADING EDGE RIB CRACKED AT STATION FS 360.250. REPAIRED IAW DC8 SRM 57-20. 2 L 7 4 4F 4A25 1999061800536 19990618 00536 WP 1999 6 18 ABXA9900467 1 19990421 A 5720 97532938 ANGLE DOUG DOUG DC8 DC863 302198A WP WS 250.089 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING INBOARD SIDE STATION XS250.089 RIB VERTICAL ANGLE CRACKED AT BOTTOM. REPAIRED IAW DC8 SRM 51-1-21 AN D DWG 97532938. 2 L 7 4 4F 4A25 1999061800537 19990618 00537 WP 1999 6 18 ABXA9900468 1 19990423 A 5720 5769857 CLIP DOUG DOUG DC8 DC863 302198A WP WS 6.225 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT CENTER LEADING EDGE INTERCOSTAL ATTACH CLIP CRACKED AT STATION XOLDI 6.225. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 5769857. 2 L 7 4 4F 4A25 1999061800538 19990618 00538 WP 1999 6 18 ABXA9900469 1 19990423 A 5730 5769589 SKIN DOUG DOUG DC8 DC863 302198A WP WS 285 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT CENTER LEADING EDGE LOWER SKIN CRACKED AT INBOARD END STATION FS 285. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999061800539 19990618 00539 WP 1999 6 18 ABXA9900470 1 19990420 A 5730 5769589 SKIN DOUG DOUG DC8 DC863 302198A WP WS 253 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING CENTER LEADING EDGE HAD CRACKED SKIN AT STATION XW 253. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999061800540 19990618 00540 WP 1999 6 18 ABXA9900471 1 19990423 A 5320 37502571 FITTING DOUG DOUG DC8 DC863 302198A WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 31 LEFT HAD CRACKED SPLICE FITTING BETWEEN STATIONS 440 AND 460. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999061800541 19990618 00541 WP 1999 6 18 MWEA99336 1 19990614 A 5241 5913184501N PAN DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 THE GALLEY SERVICE DOOR PAN CRACKED AT UPPER HINGE CUTOUT UPPER RADIUS. MTC INSTALLED NEW UPPER DOOR PAN AND FABRICATED AND INSTALLED DOUBLER AND SPLICE. 2 L 7 2 4F A6WE 1999061800542 19990618 00542 WP 1999 6 18 MWEA99337 1 19990614 A 5730 59305035 SKIN DOUG DC9 DC981 3022081 WP WS 383 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 PREVIOUS BLEND OUT AT LEFT WING LOWER SKIN AFT SPAR AT XRS 383. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061800543 19990618 00543 NM 1999 6 18 MWEA99338 1 19990614 A 2560 D29982107 SLIDE HOLDER DOUG MD88 MD88 3023688 NM GALLEY LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 701ME 49760 FORWARD GALLEY SLIDE HOLDER IS LOOSE. RESECURED SLIDE HOLDER. 2 L 7 2 4F RT A6WE 1999061800544 19990618 00544 WP 1999 6 18 MWEA99339 1 19990614 A 5320 59174637 JAMB DOUG DC9 DC981 3022081 WP BS 1350 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 FOUND CORROSION AT AFT VENT DOOR LOWER JAM AT FS 1350 BEHIND RUBBER SEAL. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061800545 19990618 00545 WP 1999 6 18 MWEA99340 1 19990614 A 5313 5911429159 LONGERON DOUG DC9 DC981 3022081 WP BS 1375 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 LONGERON 24L AT STATION 1375 IS EXFOLIATED. MTC FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 1999061800546 19990618 00546 WP 1999 6 18 MWEA99341 1 19990614 A 5330 593600417 SKIN DOUG DC9 DC981 3022081 WP BS 769 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 803ME 480299 PREVIOUS REPAIRS AT STATION 769 LONGERON 28L AND ON RIGHT SIDE OF FUSELAGE AT STATION 207 LONGERON 7R. MTC FABRICATED A ND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061800547 19990618 00547 WP 1999 6 18 MWEA99342 1 19990614 A 5330 59360311 SKIN DOUG DC9 DC981 3022081 WP BS 984 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 EXTERIOR SKIN HAS BLEND OUT AT STATION 984 LONGERON 15L AND AT STATION 1117 BETWEEN LONGERON 20-21L. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061800548 19990618 00548 WP 1999 6 18 MWEA99343 1 19990614 A 5730 59305035 SKIN DOUG DC9 DC981 3022081 WP WS 200 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 PREVIOUS BLEND OUT AFT OF SLAT TRACK CAN DRAIN NR 17 STRINGER INBOARD OF XRS 200 ON LEFT WING. MTC FABRICATED AND INSTA LLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061800549 19990618 00549 WP 1999 6 18 MWEA99344 1 19990607 A 5313 591140615N LONGERON DOUG DC9 DC914 3022034 WP BS 160 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LONGERON 3L IS CRACKED AT STATION 160. MTC FABRICATED AND INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 1999061800550 19990618 00550 WP 1999 6 18 MWEA99345 1 19990614 A 5330 59360312 SKIN DOUG DC9 DC981 3022081 WP BS 984 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 803ME 48029 FOUND UNAPPROVED REPAIR ON SKIN ON LONGERON 18R TO 17R AT STATION 984. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999061800551 19990618 00551 WP 1999 6 18 MWEA99346 1 19990614 A 5730 SKIN DOUG DC9 DC914 3022034 WP WS 550 DAMAGED A MWEA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 800ME 45842 DURING TAXI INTO GATE LEFT WING LEADING EDGE AT FS 550 STRUCK GROUND EQUIPMENT. MTC REPAIRED LEFT WING LEADING EDGE WIT H A FILL AND FAIR REPAIR. 2 L 7 2 4F A6WE 1999061800552 19990618 00552 WP 1999 6 18 MWEA99347 1 19990614 A 7797 WIRE DOUG DC9 DC915 3022036 WP LT ENGINE EGT BROKEN A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 300ME 45718 DURING TAKEOFF ROLL, THE LEFT ENGINE EGT DROPPED TO 50 DEGREE, DISCONTINUED TAKEOFF. MTC FOUND BROKEN WIRE AT PIN A CON NECTOR R5-11 ON LEFT ENGINE AND RESOLDERED. 2 L 7 2 4F A6WE 1999061800553 19990618 00553 1999 6 18 MWEA99348 4 19990614 A 3454 5224280109 NAV RECEIVER DOUG DC9 DC914 3022034 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 400ME 45727 THE NR 1 AND NR 2 NAV OSCILATES NO FLAGS IN VIEW. MTC REMOVED AND REPLACED NR 1 AND NR 2 NAV RECEIVER. 2 L 7 2 4F A6WE 1999061800554 19990618 00554 WP 1999 6 18 ASAA9980108 1 19990512 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 1 BROKEN A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 965AS 53079 SEA - AFTER ARRIVAL OF FLT 483 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 1 WAS DISLODGED FROM TRACK. RE PLACED BROKEN WIRES IN FLOOR TRACK ASSEMBLY, REINSTALLED LIGHTING INTO TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061800555 19990618 00555 WP 1999 6 18 ASAA9980106 1 19990510 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 SEA - DURING MAINTENANCE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AN D OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061800556 19990618 00556 WP 1999 6 18 ASAA9980105 1 19990509 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERTED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061800557 19990618 00557 WP 1999 6 18 ASAA9980104 1 19990508 A 3350 082084 DIODE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING IMAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE DIODE ASSEMBLY IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061800558 19990618 00558 WP 1999 6 18 ASAA9980102 1 19990507 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING MAINTENANCE CHECK, OVERHEAD EMERGENCY LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERI ES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061800559 20000609 00559 NE 2000 6 9 ASAA9910101 2 19990519 A 7250 turbine BOEING 737 737290C 138448V NM PWA JT8 JT8D17 52049 NE NR 1 engine FAILED A ASAA E a ENGINE SHUTDOWN UNSCHED LANDING j WARNING INDICATION CL CLIMB 1 NM 01 730AS 22577 8175 ANC - ON TAKEOFF OF FLIGHT 7802, JUST AFTER REDUCING POWER FOR CLIMB CREW REPORTED THE NR 1 ENGINE POPPED AND WAS LOST. SHUTDOWN NR 1 ENGINE AND FOUND TURBINE BLADE DAMAGE. REPLACED NR 1 ENGINE. THE ENGINE WAS ROUTED TO AEROTHRUST CORP F OR INSPECTION AND REPAIR. AEROTHRUST DISASSEMBLED AND INSPECTED THE ENGINE. THE C-7, T-1, T-3, AND T-4 DISKS, ALONG WI TH THE N2 SHAFT WERE REPLACED. THE ENGINE WAS THEN REASSEMBLED, TESTED, BOROSCOPE, AND RETURN TO ALASKA AIRLINES. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999061800560 19990618 00560 WP 1999 6 18 ASAA9980101 1 19990507 A 3350 0105606004 LIGHT DOUG DC9 DC983 3022083 WP ROW 22 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, ONE RED EMERGENCY FLOOR TRACK LIGHT AT ROW 22 WAS FOUND INOPERATIVE. REPLACED LAMP MODU LE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061800561 19990618 00561 WP 1999 6 18 ASAA9980100 1 19990504 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP ROW 20/23 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING MAINTENANCE CHECK, ONE EMERGENCY FLOOR TRACK LIGHT AT ROW 20 AND TWO AT ROW 23 WERE FOUND INOPERATIVE. REP LACED LAMP MODULES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061800562 19990618 00562 NM 1999 6 18 ASAA9940109 1 19990516 A 3397 WIRE BOEING 737 737490 1384715 NM ROW 28 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 705AS 29318 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 23 THROUGH 28 WERE FOUND TO BE INOPERATIVE . RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999061800563 19990618 00563 NM 1999 6 18 ASAA9940105 1 19990507 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 16 DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 754AS 25095 ONT - FLT 354 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN ROW 16 AREA WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING A T ROW 16 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999061800565 19990618 00565 NM 1999 6 18 ASAA9910100 1 19990516 A 3350 6005401 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 SEA - PRIOR TO FLIGHT 65, THE R1 EMERGENCY EXIT LIGHT WOULD NOT TEST PROPERLY. REPLACED BATTERY AND LIGHT OPERATED NORM ALLY. (M) 2 L 7 2 4F RT A16WE 1999061800566 19990618 00566 NM 1999 6 18 ASAA9910099 1 19990515 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM ROW 12 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT ROWS 12 AND 14 WERE FOUND TO BE INOPERATIVE. REPLACED BAT TERY AT ROW 12 AND RECEIVER AT ROW 14. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999061800567 19990618 00567 NM 1999 6 18 99ZZZM348 1 19990515 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM ROW 14 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT ROWS 12 AND 14 WERE FOUND TO BE INOPERATIVE. REPLACED BAT TERY AT ROW 12 AND RECEIVER AT ROW 14. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999061800568 19990618 00568 NM 1999 6 18 ASAA9910096 1 19990512 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT ON THE SMOKE BARRIER WAS FOUND INOPERATIVE. REPLAC ED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999061800569 19990618 00569 NM 1999 6 18 ASAA9910095 1 19990511 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM ROW 14 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 WERE FOUND INOPERATIVE. REPLACED BATTE RY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999061800570 19990618 00570 NM 1999 6 18 ASAA9910094 1 19990507 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 ANC - FLT 41 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ON. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999061800571 19990618 00571 NM 1999 6 18 ASAA9910093 1 19990506 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM ROW 11 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 11 WERE FOUND TO BE INOPERATIVE. REPLACED RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999061800572 19990618 00572 1999 6 18 RAIA990521 4 19990516 A 3425 7002493902 HSI BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 433AM 13634 885 FLT 7086 - STL - CAPTAINS HSI/HDG FLAGGED. MAINTENANCE REPLACED CAPTAINS HSI. (M) 2 L 7 2 4T RT A56EU 1999061800573 19990618 00573 EU 1999 6 18 RAIA990520 1 19990515 A 3040 C20HD WIPER JETAIR JETSTM JETSTM4101 1500501 EU LT WINDSHIELD FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 552HK 41057 FLT 7067 - STL - CAPTAINS WIPER BLADE WORN. MAINTENANCE REPLACED CAPTAINS WIPER BLADE. (M) 2 L 7 2 4T RT A41NM 1999061800574 19990618 00574 EU 1999 6 18 RAIA990519 1 19990515 A 3240 S7618010220400 HANDLE AEROSP ATR42 ATR42300 8680920 EU PARKING BRAKE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 421TE 102 FLT 7156 - STL - EMERGENCY/PARKING BRAKE HANDLE BROKE OFF. MAINTENANCE REPLACED EMERGENCY PARK BRAKE HANDLE. (M) 2 H 7 2 4T RT A53EU 1999061800575 19990618 00575 EU 1999 6 18 RAIA990518 1 19990515 A 2432 40782 BATTERY AEROSP ATR72 ATR72202 8680940 EU BATTERY COMPT DISCHARGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7411 - XNA - MAIN BATTERY CHARGE FAULT LIGHT ILLUMINATED. MAINTENANCE REPLACED MAIN BATTERY. (M) 2 H 7 2 4T RT A53EU 1999061800576 19990618 00576 1999 6 18 RAIA990517 4 19990514 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 14212 879 FLT 7429 - EVV - LEFT STALL TEST FAILED. MAINTENANCE REPLACED LEFT LIFT TRANSDUCER. (M) 2 L 7 2 4T RT A56EU 1999061800577 19990618 00577 WP 1999 6 18 USAAD99069 1 19990524 A 3260 H146 SWITCH DOUG DC9 DC931 3022065 WP NLG FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 978VJ 47371 DAY-ROC - FLT 1743 - WHEN THE LANDING GEAR WAS LOWERED ON APPROACH THE NOSE GEAR UNSAFE RED LIGHT REMAINED ILLUMINATED. THE AIRCRAFT EXECUTED A GO-AROUND, AND AFTER SEVERAL MINUTES THE NOSE GEAR GREEN LIGHT ILLUMINATED AND THE RED UNSAFE L IGHT WENT OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THE PROBLEM TO BE INDICATION AND THE AIRCR AFT WAS FERRIED TO PIT FOR REPAIRS. PIT MAINTENANCE REPLACED THE NOSE GEAR LOCK SWITCH AND PERFORMED A GEAR SWING. ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1999061800578 19990618 00578 EU 1999 6 18 RAIA990523 1 19990517 A 3241 140071 TRANSDUCER AEROSP ATR42 ATR42300 8680920 EU NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424TE 124 FLT 7402 - STL - ANTI-SKID FAULTED. MAINTENANCE REPLACED NR 2 WHEEL TRANSDUCER. (M) 2 H 7 2 4T RT A53EU 1999061800579 19990618 00579 EU 1999 6 18 RAIA990527 1 19990517 A 6120 31043351 SPRING JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 572HK 41091 FLT 7733 - JFK - RIGHT OIL CONTAM LIGHT CAME ON. MAINTENANCE REPLACED RIGHT ENGINE PROP SHAFT WAVE SPRING. (M) 2 L 7 2 4T RT A41NM 1999061800580 19990618 00580 EU 1999 6 18 RAIA990526 1 19990517 A 2150 BA202825 BELLOWS AEROSP ATR72 ATR72202 8680940 EU LT PACK FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 723TE 283 FLT 7417 - STL - LEFT PACK NOT COOLING. MAINTENANCE REPLACED LEFT HEAT EXCHANGER BELLOWS. (M) 2 H 7 2 4T RT A53EU 1999061800581 19990618 00581 NM 1999 6 18 GAIA9959 1 19990519 A 3231 65175711 MECHANISM BOEING 727 727223 1384074 NM NLG DOOR OUT OF ADJUST A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6812 19487 REF LOG SHEET 1591-30, DURING CLIMB-OUT OF FLIGHT KHA 717 FROM OKC TO MCI, THE RED GEAR LIGHT ON THE FORWARD INSTRUMENT PANEL, AND THE AMBER NOSE GEAR LIGHT ON THE FLIGHT ENGINEER'S PANEL BOTH ILLUMINATED WHEN THE AIRCRAFT REACHED AND EXCEE DED 250 KNOTS IAS WITH THE GEAR HANDLE IN THE UP POSITION. THE CREW RECYCLED THE GEAR IAW KHA B727 OPERATIONS MANUAL. T HE PROBLEM REMAINED. THE CREW RETURNED TO OKC AND MADE SAFE LANDING WITHOUT FURTHER INCIDENTS. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE FORWARD NOSE GEAR DOOR MECHANISM WAS OUT OF ADJUSTMENT. THE DOOR MECHANISM WAS ADJUSTED IAW A A 727 MM 32-30. AN OPERATIONAL CHECK WAS PERFORMED ON THE SYSTEM WHICH RESULTED IN NO FURTHER PROBLEMS. THE AIRCRAFT 2 L 7 3 4F A3WE 1999061800582 19990618 00582 WP 1999 6 18 ARWA990501 1 19990522 A 3310 BA170 BALLAST DOUG DC8 DC863F 302198F WP COCKPIT FAILED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 19 441J 983 45988 MIA - FLT 501 - UPON DESCENT INTO MIAMI, NOXIOUS ODORS ENTERED COCKPIT. CREW ON OXYGEN AND RAN CHECKLIST. UNABLE TO PI NPOINT SOURCE OF ODOR. MAINTENANCE REMOVED AND REPLACED GLARESHIELD FLOURSCENT LIGHTING BALLAST. OPS CHECKED IAW MM 33 -13-00. (M) 2 L 7 4 4F 4A25 1999061800583 19990618 00583 WP 1999 6 18 ARWA990502 1 19990523 A 5400 5750821501 BRACKET DOUG DC8 DC862 3021970 WP NR 1 ENGINE BROKEN A ARWA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 19 802BN 45909 BOG - FLT 709 - NR 1 ENGINE INBOARD BYPASS AIR CONSTANT DUCT STRAP BRACKET BROKEN. BLOWOUT DOOR LOST IN FLIGHT. REMOVE D AND REPLACED STRAP. REPLACED NR 1 ENGINE. COWL BLOWOUT DOOR. ENGINE IDLE RUN CHECK OK. (M) 2 L 7 4 4F 4A25 1999061800584 19990618 00584 SO 1999 6 18 RAIA990512 1 19990511 A 2424 50545001B GCU EMB 145 EMB145 SO NR 2 ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 1803 145077 FLT 5793 - TRI - DURING NR 1 ENGINE START, SEVERAL ELECTRICAL MESSAGES APPEARED ON EICAS. WHEN NR 2 ENGINE WAS SHUT DOW N, ELECTRICAL SYSTEM WENT TO ELECTRICAL EMERGENCY. MAINTENANCE REPLACED NR 2 ENGINE GCU. (M) 2 L 7 2 4F RT T00011AT 1999061800585 19990618 00585 EU 1999 6 18 RAIA990513 1 19990513 A 2430 171BS1012 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 41086 FLT 7660 - JFK - STANDBY POWER SUPPLY SHOWS NO CHARGE. MAINTENANCE REPLACED STANDBY POWER SUPPLY. (M) 2 L 7 2 4T RT A41NM 1999061800586 19990618 00586 1999 6 18 RAIA990503 4 19990503 A 3418 M30204A RELAY BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 864AE 864 FLT 4717 - SMF - DURING STALL TEST, NO STICK PUSHER OR STALL IDENT LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT STICK PUSHER ISOLATION RELAY. (M) 2 L 7 2 4T RT A56EU 1999061800587 19990618 00587 EU 1999 6 18 RAIA990514 1 19990513 A 3310 18996C INVERTER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 343TE 955 FLT 7394 - STL - ELECTRICAL SMELL IN COCKPIT. MAINTENANCE REPLACED INVERTER FOR ROOF PANEL LIGHTS IN COCKPIT. (M) 2 L 7 2 4T RT A56EU 1999061800588 19990618 00588 EU 1999 6 18 RAIA990515 1 19990513 A 3246 AH52688 WHEEL JETAIR JETSTM JETSTM4101 1500501 EU NLG FAILED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 567HK 41085 FLT 7784 - DCA - UPON GEAR RETRACTION, VIOLENT SHUDDER WAS FELT. MAINTENANCE REPLACED LEFT NOSE WHEEL ASSEMBLY. (M) 2 L 7 2 4T RT A41NM 1999061800589 19990618 00589 EU 1999 6 18 RAIA990516 1 19990513 A 3246 AH52688 WHEEL JETAIR JETSTM JETSTM4101 1500501 EU NLG FAILED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 567HK 41085 FLT 7784 - DCA - UPON GEAR RETRACTION, VIOLENT SHUDDER WAS FELT. MAINTENANCE REPLACED RIGHT NOSE WHEEL ASSEMBLY. (M) 2 L 7 2 4T RT A41NM 1999061800590 19990618 00590 1999 6 18 RAIA990510 4 19990510 A 3421 7003110912 CRT SCREEN AEROSP ATR72 ATR72202 8680940 EU RT COCKPIT FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 723TE 16225 283 FLT 7411 - XNA - FO'S EADI SCREEN SHORTED OUT CAUSING SMOKE IN COCKPIT. MAINTENANCE REPLACED EADI SCREEN. (M) 2 H 7 2 4T RT A53EU 1999061800591 19990618 00591 WP 1999 6 18 RAIA990509 2 19990504 A 7320 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 03 424AM 12879 865 66066 FLT 7042 - COU - TORQUE DROPPED ON RIGHT ENGINE, TURNED TTL OFF, TORQUE CAME BACK UP. MAINTENANCE REPLACED FUEL BYPASS VALVE ON RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999061800592 19990618 00592 EU 1999 6 18 RAIA990511 1 19990511 A 2910 1379305A157 LINE BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A RAIA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 03 875JX 875 FLT 7394 - STL LOSSED HYDRAULIC PRESSURE ON BOTH SIDES, PERFORMED EMERGENCY GEAR EXTENSION. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR ACTUATOR LINE. (M) 2 L 7 2 4T RT A56EU 1999061800593 19990618 00593 EU 1999 6 18 SIMA991312 1 19990511 A 5320 S536771318210 WEB AEROSP ATR42 ATR42300 8680920 EU FRAME 39-40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-1 INSPECTION, FOUND THE RIGHT AFT FLOOR WEB BETWEEN FRAME 39 AND 40 CORRODED. REMOVED AND REPLACED TH E WEB IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800594 19990618 00594 EU 1999 6 18 SIMA991311 1 19990511 A 5315 S53672404218 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 40 CORRODED. REMOVED AND REPLACED FLOORBEAM 40 IAW 53-61-40. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800595 19990618 00595 EU 1999 6 18 SIMA991313 1 19990511 A 5320 S5367800821602 ZEE AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-1 INSPECTION, FOUND RIGHT AFT CARGO ZEE MEMBER BETWEEN FRAME 39 AND 40 CORRODED. REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800596 19990618 00596 NE 1999 6 18 EISA99072 2 19990327 A 7270 589470 EXIT CASE BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 649129 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED RIGHT SIDE AT 2 O'CLOCK POSI TION. REMOVED AND REPLACED FAN EXIT CASE PER 727 OVERHAUL MANUAL 72-00-34. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999061800597 19990618 00597 NE 1999 6 18 EISA99071 2 19990327 A 7270 589470 EXIT CASE BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 649129 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED AROUND STATOR ON LEFT SIDE A T 9 O'CLOCK POSITION JUST ABOVE CASE LINE. REMOVED AND REPLACED FAN EXIT CASE PER 727 OVERHAUL MANUAL 72-00-34. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999061800598 19990618 00598 NM 1999 6 18 EISA99035 1 19990219 A 5520 DOUBLER BOEING 727 727223 1384074 NM RT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, X-RAY REVEALED A CRACK IN TRAILING EDGE OUTBOARD END OF RIGHT ELEVAT OR AS SEEN IN SHOT NR R-35. CRACK EXISTED IN DOUBLER ON LOWR SURFACE. REMOVED DOUBLER, FABRICATED AND INSTALLED NEW DO UBLER PER SRM 55-20-03. (M) 2 L 7 3 4F A3WE 1999061800599 19990618 00599 WP 1999 6 18 EISA99032 1 19990227 A 2810 V92003 CHECK VALVE DOUG DC9 DC931 3022065 WP CENTER TANK DIRTY A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 945VJ 47066 CREW REPORTED LEFT WING FUEL VENTING OUT OF RIGHT WING. LEAK STOPPED WHEN CENTER TANK PUMPS WERE TURNED OFF. TURN BACK TO (ACY). CHECK FUEL SYSTEM PER CROSS FEED AND TRANS TEST ML/M 28-20-00 PAGE 50/2502. OPS CHECK NORMAL AFTER FREEING CENTER TANK PUMP DISCHARGE CHECK VALVE. (M) 2 L 7 2 4F A6WE 1999061800600 19990618 00600 NM 1999 6 18 EISA99029 1 19990218 A 2611 SMK6D SMOKE DETECTOR BOEING 727 72731 1384010 NM FUSELAGE MALFUNCTIONED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 240NE 18906 DURING CRUISE, CARGO SMOKE LIGHT ILLUMINATED WITH NO SECONDARY INDICATIONS OF SMOKE. GROUND TEST OF SYSTEM CHECKS GOOD. FOUND MOISTURE ON WALLS AND TWO VENT TUBES BENT. REPOSITIONED GROUND TEST GOOD. (M) 2 L 7 3 4F A3WE 1999061800601 19990618 00601 NM 1999 6 18 EISA99023 1 19990212 A 2611 SMK6D SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO COMPT MALFUNCTIONED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 300NE 18974 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT NO OTHER INDICATIONS OF SMOKE, LIGHT WENT OUT AFTER 10 MINUTES. PERFORMED FUNCT IONAL CHECK OF CARGO SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 1999061800602 19990618 00602 NM 1999 6 18 99ZZZM349 1 19990121 A 2133 103280511 OUTFLOW VALVE BOEING 727 72725 1384006 NM RIGHT FAILED A EISA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 290NE 18972 CLIMBING THROUGH FLIGHT LEVEL 280, CABIN PRESSURIZATION FAILED IN AUTO MODE AND MANUAL MODE. REMOVED AND REPLACED LEFT AND RIGHT OUTFLOW VALVES. OPS CHECK GOOD PER MM 21-30-51. (M) 2 L 7 3 4F A3WE 1999061800603 19990618 00603 1999 6 18 EISA99014 4 19990127 A 3425 G4578 NAV CONTROL BOEING 727 7272M7 138407S NM COCKPIT SHORTED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 742RW 21952 CAPTAIN CDI OSCILLATES ONE DOT LEFT AND RIGHT ON LOC/VOR FREQUENCY, CAPTAIN RMI PIVOTS 10 DEGREES LEFT AND RIGHT ON VOR/ LOC FREQUENCY. BOTH OCCUR ALSO WHEN CAPTAIN ON AUX. REMOVED AND REPLACED GPS NMC AND NAV CONTROL HEAD OPS CHECK GOOD O N GROUND. TEST FLIGHT CDI OPERATES NORMAL ON CAPTAIN AND F/O'S SIDE IN NORMAL MODE. (M) 2 L 7 3 4F A3WE 1999061800604 19990618 00604 1999 6 18 99ZZZM350 4 19990127 A 3425 4300341300 NMC BOEING 727 7272M7 138407S NM COCKPIT SHORTED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 742RW 21952 CAPTAIN CDI OSCILLATES ONE DOT LEFT AND RIGHT ON LOC/VOR FREQUENCY, CAPTAIN RMI PIVOTS 10 DEGREES LEFT AND RIGHT ON VOR/ LOC FREQUENCY. BOTH OCCUR ALSO WHEN CAPTAIN ON AUX. REMOVED AND REPLACED GPS NMC AND NAV CONTROL HEAD OPS CHECK GOOD O N GROUND. TEST FLIGHT CDI OPERATES NORMAL ON CAPTAIN AND F/O'S SIDE IN NORMAL MODE. (M) 2 L 7 3 4F A3WE 1999061800605 19990618 00605 WP 1999 6 18 EISA99008 1 19990118 A 5347 591014329 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 194-200 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 969VJ 47421 DURING ACCOMPLISHED OR ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON LEFT INBOARD SEAT TRACK AT FS 194 TO 200. CUT OUT DAMAGED SECTION AND INSTALLED NEW SECTION OF TRACK AT FS 194-200 PER SRM 51-30-02 AND 51-10-1. (M) 2 L 7 2 4F A6WE 1999061800606 19990618 00606 NM 1999 6 18 EISA99007 1 19990120 A 3610 132712 PNEUMATIC LINE BOEING 727 727231 1384079 NM EMPENNAGE PUNCTURED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 12305 19562 NR 3 ENGINE STRUT OVERHEATS IN FLIGHT AFTER TAKEOFF. FOUND BRAIDED HP AIR LINE HOLE ENGINE STRUT. REMOVED AND REPLACED LINE IAW MM CHAPTER 36-12. LEAK AND OPS CHECK GOOD ON GROUND IAW MM 26-14. (M) 2 L 7 3 4F A3WE 1999061800607 19990618 00607 NM 1999 6 18 99ZZZM351 1 19990120 A 2130 1310461 PRESS CONTROL BOEING 727 727223 1384074 NM COCKPIT FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 313NE 19702 CLIMBING THROUGH 10,000 FEET, CABIN PRESSURIZATION BECAME UNCONTROLLABLE IN AUTO OR MANUAL. REMOVED AND REPLACED AUTO P RESSURE CONTROL AND MANUAL PRESSURE CONTROL. SYSTEM OPS CHECK GOOD IAW MM 21-30-0. (M) 2 L 7 3 4F A3WE 1999061800608 19990618 00608 NM 1999 6 18 EISA99004 1 19990119 A 2133 7248272 OUTFLOW VALVE BOEING 727 727223 1384074 NM RIGHT INOPERATIVE A EISA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 313NE 19702 THIRTY MINUTES AFTER, PRESSURIZATION BECAME UNCONTROLLABLE CLIMBING THROUGH FL 250 DID NOT WORK IN AUTO MANUAL. REGAINE D CONTROL AT 12000. TRANSFERRED TO PLACARD NR 971 PER MEL 21-18-1. (M) 2 L 7 3 4F A3WE 1999061800609 19990618 00609 EU 1999 6 18 REXA99014 1 19990508 A 2150 7769106 ACM SAAB SF340 SF340A 7850100 EU RIGHT INOPERATIVE A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 403BH 900383 340A060 STRONG SMELL IN COCKPIT AT 17,000 FEET, NO SMOKE OR OTHER NOTICEABLE PROBLEMS FOUND WITH C/B OR AVIONICS. PERFORMED DET AILED VISUAL, FULL SYSTEMS INSPECTIONS, AND ENGINE RUNS. FOUND ACM TO BE INOPERATIVE. DEFERRED RT ACM. (M) 2 L 7 2 4T RT A52EU 1999061800610 19990618 00610 NM 1999 6 18 UIEA9918 1 19990510 A 2612 WIRE BOEING 747 747230B 1384889 NM MLG WW CHAFED A UIEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 15 508MC 21644 FLT CI 346 - DURING COCKPIT PREFLIGHT CHECKS, WHEN MASTER DIM AND TEST SWITCH PLACED TO 'TEST' POSITION, CIRCUIT BREAKER NR 152 POPPED AND SMOKED. TROUBLESHOT SYSTEM AND FOUND WIRING CHAFING IN OVERHEAD P5 PANEL GOING TO 'WHEEL WELL FIRE D ETECTION MODULE'. REPAIRED WIRING AND MASTER DIM AND TEST SYSTEM OPERATION NORMAL. (M) 2 L 7 4 4F A20WE 1999061800611 19990618 00611 NM 1999 6 18 UIEA9917 1 19990508 A 2432 279202 BATTERY CHARGER BOEING 747 747230B 1384889 NM APU FAILED A UIEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 507MC 21380 FLT 9603 - BTB - DURING TAXI APU BATTERY CHARGER SPARKED TWICE, THEN STARTED, FILLING THE MAIN CABIN WITH SMOKE UNTIL C/ B POPPED. AIRCRAFT RETURNED TO GATE. FOUND APU BATTERY CHARGER DEFETIVE. REPLACED APU BATTERY CHARGER, OPERATIONAL CH ECK NORMAL. (M) 2 L 7 4 4F A20WE 1999061800612 19990618 00612 NM 1999 6 18 USAASB99107 1 19990423 A 3260 655825029 CIRCUIT CARD BOEING 737 737201 1384454 NM E/E COMPT MALFUNCTIONED A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 255AU 22797 TPA - FL2707 - CREW DID NOT RECEIVE ANY LANDING GEAR LIGHTS WHEN GEAR HANDLE WAS LOWERED. CIRCUIT BREAKERS WERE CHECKED , GEAR WAS CYCLED AND VISUAL CHECK THAT GEAR WAS DOWN WAS ACCOMPLISHED. CREW DECLARED AN EMERGENCY. FLIGHT LANDED AT T PA WITHOUT INCIDENT AND TAXIED TO THE GATE ON ITS OWN POWER. AT TOUCHDOWN, THE THREE GEAR GREEN LIGHTS DID ILLUMINATE. MAINTENANCE JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES BUT COULD NOT DUPLICATE PROBLEM. REPLACED CIRCUIT CARD A-7, LANDING GEAR INDICATION, AS PRECAUTIONARY. GEAR INDICATION AND SYSTEM CHECKS NORMAL PER MM 32-09-11A. (M) 2 L 7 2 4F A16WE 1999061800613 19990618 00613 NM 1999 6 18 USAASB99109 1 19990423 A 2910 HYDRAULIC LINE BOEING 737 737201 1384454 NM RT MLG LEAKING A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS AP APPROACH 1 EA 19 246US 22753 RDU - FL2604 - AIRCRAFT WAS EN ROUTE FROM FLL TO BWI, WHEN IT WAS DIRECTED TO HOLD SHORT OF RDU DUE TO AIR TRAFFIC CONTR OL AT DCA. WHILE HOLDING AT 2,500 FEET, THE 'A' HYDRAULIC SYSTEM GAUGE READ ZERO AND WHILE TURNING DURING THE HOLD, TH E 'A' SYSTEM LOW PRESSURE LIGHTS ILLUMINATED AND BEGAN TO FLICKER. FLIGHT DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND A SPOILER RETURN LINE IN THE RIGHT MAIN LANDING GEAR WHEELWELL WITH A HOL E IN THE LINE. ACCOMPLISHED INTERIM REPAIR AND INSTALLED A FLEX LINE. SERVICED HYDRAULIC SYSTEM TO FULL. LEAK AND OPE RATIONAL CHECK GOOD. HYDRAULIC LINE IS PROGRAMMED FOR REPLACEMENT. (M) 2 L 7 2 4F A16WE 1999061800614 19990618 00614 EU 1999 6 18 SIMA991096 1 19990419 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 353SB 340B353 ABI - DURING A MBV INSPECTION DENTS WERE DISCOVERED ON RIGHT FUSELAGE SKIN AT STATION 339-363 BETWEEN SL 1616-1620. CUT OUT DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED TWO EXTERNAL DOUBLERS .050 THICK. APPLIED SURFA CE TREATMENT ON THE DOUBLERS AND ONE COAT OF ALODINE AND A COAT OF EPOXY PRIMER AND TREATED CUT OUT EDGES. APPLIED SEAL ANT TO THE CONTACT SURFACE OF THE DOUBLER AND ATTACHED TO AIRCRAFT. APPLIED FILLET SEALANT AROUND EDGES STEPS OF THE DO UBLERS AND RESTORED SURFACE FINISH. WORK DONE SAAB SRM 53-70-10 PAGE 217. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800615 19990618 00615 EU 1999 6 18 SIMA991095 1 19990419 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 150-152 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 347SB 340B347 ABI - A/C ARRIVED FOR REPAIR OF BIRD STRIKE DAMAGE ON RIGHT COCKPIT SKIN PANEL FORWARD AND ABOVE AOA VANE. REMOVED DAMA GED SKIN PANEL AT FS 150. REMOVED STATION 152 FRAME AND INSTALLED NEW FRAME. THE RBL 29 HAS A CRACK WHICH RUNS AFT FRO M THE FASTENER HOLE AT STATION 152.35/WL96.6. MADE CIRCULAR CUT OUT TO REMOVE THE CRACK AND PERFORMED A DYE PEN INSPECT ION. FABRICATED DOUBLERS AND A TRIPLER, DOUBLER .032 THICK AND TRIPLER .025 THICK. APPLIED CORROSION PREVENTIVE TO THE REPAIR PARTS. REMOVED VERTICAL ANGLE CONNECTING THE FRAME STATION 152 TO THE RBL 29. INSTALLED NEW ANGLE. APPLIED CO RROSION PREVENTIVE TO THE ANGLE AND NEW SKIN PANEL. INSTALLED NEW SKIN PANEL. APPLIED FILLET SEALANT AROUND EDGES OF S 2 L 7 2 4T RT A52EU 1999061800616 19990618 00616 EU 1999 6 18 SIMA991094 1 19990419 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-329 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 ABI - DURING A MBV INSPECTION, SEAT TRACK BL 0 WAS FOUND CORRODED BEYOND SRM LIMITS FROM STATION 297-329. CUT OUT 32 IN CH SECTION OF EXISTING SEAT TRACK. FABRICATED A 32 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76511 MATERIAL. FABR ICATED IN 15 INCH LONG U-BEAM OF PLAL 7075-T7351 MATERIAL. POSITIONED REPAIR U-BEAM INSIDE EXISTING SEAT TRACK AND DRIL LED HOLES. INSTALLED IN AIRCRAFT, PRIMED AND PAINTED FASTENERS. WORK DONE IAW SAAB SRM 53-70-60 AND STANDARD SRM PROCE DURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800617 19990618 00617 EU 1999 6 18 SIMA991093 1 19990419 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-329 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 ABI - DURING A MBV INSPECTION, SEAT TRACK 18.3L WAS FOUND CORRODED BEYOND SRM LIMITS FROM STATION 297-329. CUT OUT 32 I NCH SECTION OF EXISTING SEAT TRACK. FABRICATED A 32 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76511 EXTRUDED MATER IAL. FABRICATED A 15 INCH LONG U-BEAM OF PLAL 7075-T7351 MATERIAL. POSITIONED REPAIR U-BEAM INSIDE EXISTING SEAT TRACK AND DRILLED HOLES. INSTALLED IN AIRCRAFT. PRIMED AND PAINTED FASTENES. WORK DONE IAW SAAB SRM 53-70-60 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800618 19990618 00618 EU 1999 6 18 SIMA991092 1 19990419 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 ABI - DURING A MBV INSPECTION A CHAFE WAS DISCOVERED ON THE LEFT NACELLE INBOARD OUTER SKIN PANEL AT THE FILLET FAIRING SEAL CONTACT POINT. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A DOUBLER AND A TRIPL ER .050 THICK. FABRICATED A SHIM .020 THICK. TREATED ALL REPAIR PARTS WITH PROTECTIVE TREATEMENT INCLUDING POLYURETHAN E TOP COAT. APPLIED FILLET SEALANT TO THE CONTACT SURFACE OF THE REPAIR PARTS. ATTACHED TO AIRCRAFT. FILLET SEALANT A ROUND EDGE STEPS OF THE REPAIR PARTS. RESTORED SURFACE FINISH. WORK DONW IAW SAAB REPAIR STATEMENT RN 72SDS1471 AND ST ANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800619 19990618 00619 EU 1999 6 18 SIMA991091 1 19990419 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 343SB 340B343 ABI - DURING A MBV INSPECTION, DENTS WERE DISCOVERED ON LEFT FUSELAGE SKIN STATION 339-363. CUT OUT DAMAGED AREA AND PE RFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR PLATE .050 THICK. APPLIED PROTECTIVE COAT OF ALODINE AND ONE C OAT OF EPOXY PRIMER AND FAY SEALANT TO THE CONTACT SURFACE OF THE DOUBLER AND ATTACHED TO AIRCRAFT APPLIED FILLET SEALAN T AROUND REPAIR PLATE EDGE STEP. RESTORED SURFACE FINISH. WORK DONE IAW SAAB SRM 59-70-10 PAGE 215 AND STANDARD SRM PR OCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800620 19990618 00620 EU 1999 6 18 SIMA991061 1 19990416 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - A/C ARRIVED IN ABI FOR PERMANENT REPAIR TO A DENT IN FUSELAGE SKIN FORWARD AND BELOW THE AOA VANE. PERFORMED A CI RCULAR CUTOUT .75 INCH DIAMETER TO REMOVE AND PERFORMED EDDY CURRENT TO ENSURE NO CRACKS WERE PRESENT. FABRICATED A SPA CER WITH A DIAMETER OF .070 TO OBTAIN A GAP OF .05 INCH FOR THE EXISTING SKIN. FABRICATED A REPAIR PLATE 3 INCH IN DIAM ETER. APPLIED ALODINE AND PRIMER TO BARE METAL SURFACES. ATTACHED REPAIR PLATES TO AIRCRAFT. FILLET SEALED GAP BETWEE N SPACER AND SKIN. APPLIED CORROSION PREVENTIVE COMPOUND DINITROL AV 25 TO THE INNER AREA. RESTORED SURFACE FINISH. W ORK DONE IAW SAAB 340 SRM PRACTICES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800621 19990618 00621 EU 1999 6 18 SIMA991041 1 19990414 A 3350 GE1317 BULB SAAB SF340 340B 7860101 EU ROW 12 FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 905AE 340B319 DFW - FLT 5046 - EMERGENCY LIGHT AT SEAT 12BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB FOR 12BC EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800622 19990618 00622 EU 1999 6 18 SIMA991033 1 19990413 A 2612 00SW00 WEU SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A SIMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 21 350CF 1014 340B350 LAX - FLT 3449 - AFTE DEPARTURE, THE RIGHT ENGINE FIRE WARNING SYSTEM ACTIVATED. CREW DISCHARGED FIRE EXTINGUISHER AND RETURNED TO LAX. AFTER LANDING CREW PERFORMED AN EMERGENCY EVACUATION OF THE AIRCRAFT, NOTING NO VISIBLE SIGNS OF A FIR E. VERIFIED EVENT AS A FALSE WARNING CAUSED BY THE WEU. REMOVED AND REPLACED WEU AND FIRE EXTINGUISHER. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800623 19990618 00623 EU 1999 6 18 SIMA991031 1 19990413 A 5330 S5387210120005 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 43 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING MBV-1 INSPECTION, FOUND A DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN AT FRAME 43 BETWEEN STRINGER 8 AND 9, MEASURING 24MM BY 3MM BY .044 DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 408. AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999061800624 19990618 00624 EU 1999 6 18 SIMA991001 1 19990410 A 2121 011232100 FAN AEROSP ATR72 ATR72212 EU CABIN SMOKED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 410AT 410 NAS - FLT 5775 - ROUTINE FLIGHT AT FL 150 APPROX 50 NM WEST OF NAS SMOKE WAS NOTICED IN THE MAIN CABIN AIR CONDITIONING SYSTEM. DECLARED EMERGENCY AND DESCENDED TO 5000 FT DIRECT TO NAS. FOLLOWED EMERGENCY PROCEDURES FOR COCKPIT AND ELECT RICAL SMOKE. ONCE THE NR 1 RECIRC FAN WAS TURNED OFF, THE SMOKE DISSIPATED. NORMAL LANDING, TAXI AND DEPLANING OF PASS ENGERS. CONTRACT MAINTENANCE FOUND THE NR 1 RECIRC FAN AS THE SOURCE OF THE SMOKE AND IT WAS MEL'D. SUBSEQUENTLY, THE NR 1 RECIRC FAN WAS REMOVED, REPLACED AND OPERATIONAL CHECKED. THE MEL ITEM WAS RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800625 19990618 00625 EU 1999 6 18 SIMA990984 1 19990408 A 2910 P240606040146 LINE SAAB SF340 340B 7860101 EU LT MLG FAILED A SIMA O OTHER K FLUID LOSS AP APPROACH 1 SW 21 201AE 340B201 JFK - FLT 4812 - LEFT MAIN LANDING GEAR WOULD NOT LOCK DOWN. NOTICED LOSS OF HYD FLUID QTY/PERSS ON INDICATOR. MAIN HY DRAULIC ACCUMULATOR PRESSURE ALSO DOWN. REMOVED AND REPLACED FAILED HYDRAULIC FLEX-LINE AT THE MAIN LANDING GEAR DOWNLO CK ACTUATOR. SERVICED HYDRAULIC SYSTEM. PERFORMED EXTENSION, RETRACTION AND LEAK CHECKS AND RETURNED AIRCRAFT TO SERVI CE. (M) 2 L 7 2 4T RT A52EU 1999061800626 19990618 00626 EU 1999 6 18 SIMA991032 1 19990413 A 5347 S53375001212 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, THE RIGHT FORWARD INBOARD AND OUTBOARD, THE LEFT MIDDLE INBOARD AND OUTBOARD, THE RIGHT MIDDLE INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE L EFT AND RIGHT AFT OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800627 19990618 00627 EU 1999 6 18 99ZZZM352 1 19990413 A 5347 S53375001200 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, THE RIGHT FORWARD INBOARD AND OUTBOARD, THE LEFT MIDDLE INBOARD AND OUTBOARD, THE RIGHT MIDDLE INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE L EFT AND RIGHT AFT OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800628 19990618 00628 EU 1999 6 18 99ZZZM353 1 19990413 A 5347 S53570201204 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, THE RIGHT FORWARD INBOARD AND OUTBOARD, THE LEFT MIDDLE INBOARD AND OUTBOARD, THE RIGHT MIDDLE INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE L EFT AND RIGHT AFT OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800629 19990618 00629 EU 1999 6 18 99ZZZM354 1 19990413 A 5347 S53570201200 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, THE RIGHT FORWARD INBOARD AND OUTBOARD, THE LEFT MIDDLE INBOARD AND OUTBOARD, THE RIGHT MIDDLE INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE L EFT AND RIGHT AFT OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800630 19990618 00630 EU 1999 6 18 99ZZZM355 1 19990413 A 5347 S53678001201 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, THE RIGHT FORWARD INBOARD AND OUTBOARD, THE LEFT MIDDLE INBOARD AND OUTBOARD, THE RIGHT MIDDLE INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE L EFT AND RIGHT AFT OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800631 19990618 00631 EU 1999 6 18 99ZZZM356 1 19990413 A 5347 S53678001210 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, THE RIGHT FORWARD INBOARD AND OUTBOARD, THE LEFT MIDDLE INBOARD AND OUTBOARD, THE RIGHT MIDDLE INBOARD AND OUTBOARD, THE LEFT AND RIGHT FLIGHT ATTENDANT, AND THE L EFT AND RIGHT AFT OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800632 19990618 00632 EU 1999 6 18 SIMA990983 1 19990408 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 264AE 340B264 DFW - FLT 3638 - EMERGENCY FLOOR PROXIMITY LIGH TAT SEAT 10 B/C DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800633 19990618 00633 EU 1999 6 18 SIMA990981 1 19990408 A 5210 MECHANISM SAAB SF340 340B 7860101 EU PAX DOOR DIRTY A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 901AE 340B401 LAW - FLT 3500 - MAIN PASSENGER DOOR HANDLE COULD NOT BE MOVED TO UNLOCK THE DOOR FROM INSIDE THE CABIN. DOOR HAD TO BE UNLOCKED FROM THE OUTSIDE. MAINTENANCE FOUND THE PASSENGER DOOR DID OPERATE FROM THE INSIDE, BUT IT WAS STIFF. INSPEC TED DOOR ASSEMBLY AND FOUND THE DOOR SEAL, ALL STOPS AND GUIDE PINS DIRTY. CLEANED ALL OF THESE ITEMS, THEIR MATING SUR FACES, AND LUBED LINKAGE. DOOR OPERATION WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800634 19990618 00634 EU 1999 6 18 SIMA990976 1 19990407 A 5315 S5367240620801 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FRAME 12-13 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 WITH AN OVERSIZED HI-LOCK HOLE. SPLICED IN NEW SECTION OF FLOORBEAM 2 INCH BY 7 INCH BY .067 DEEP DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 12 AND 13 AND STRINGERS 9 AND 13 . MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403 AND 407. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800635 19990618 00635 EU 1999 6 18 SIMA990975 1 19990407 A 5330 S5317150120605 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 12-13 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING MBV-1 INSPECTION, FOUND A 2 INCH BY 7 INCH BY .067 DEEP DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 12 AND 13 AND STRINGERS 9 AND 13. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403 AND 407. AIRCRAFT R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800636 19990618 00636 EU 1999 6 18 SIMA990974 1 19990407 A 5330 S5317150120605 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 1-2 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING MBV-1 INSPECTION, FOUND A 2 INCH BY 1 INCH BY .066 DEEP DENT IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 1 AND 2 AND STRINGERS 10 AND 11. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800637 19990618 00637 EU 1999 6 18 SIMA990972 1 19990407 A 5320 S536710002201 CHORD AEROSP ATR42 ATR42300 8680920 EU FRAME 36-38 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING MBV-1 INSPECTION, FOUND THE RIGHT OUTER CHORD BETWEEN FRAMES 36 AND 38 AT STRINGER 17 CORRODED. MAINTENANC E REMOVED AND REPLACED THE CHORD IAW SRM 53-16-14. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800638 19990618 00638 EU 1999 6 18 SIMA990973 1 19990407 A 5320 S5367125720402 INTERCOSTAL AEROSP ATR42 ATR42300 8680920 EU FRAME 36-38 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURNIG MBV-1 INSPECTION, FOUND THE RIGHT INTERCOSTAL BETWEEN FRAMES 36 AND 38 AT STRINGER 17 CORRODED. MAINTENANC E REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800639 19990618 00639 EU 1999 6 18 SIMA990971 1 19990407 A 5320 S5367800826901 DRAIN TRACK AEROSP ATR42 ATR42300 8680920 EU SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE DRAIN TRACK CORRODED. MAINTENANCE REMOVED AND REPLACE D THE DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800640 19990618 00640 EU 1999 6 18 SIMA990931 1 19990403 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 560-583 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AE 340B380 ABI - DENT FOUND ON THE RIGHT REAR FUSELAGE SKIN BETWEEN STATION 560 AND STATION 583 AND BETWEEN SL 1615 AND SL 1616 WHI CH WAS BELOW LIMITS. PERFORMED CUTOUT OF THE DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION OF THE CUTOUT AREA AND FO UND NO DEFECTS. FABRICATED TWO EXTERNAL DOUBLERS .050 THICK WITH ONE MEASURING 13 BY 11.5 INCHES AND THE OTHER MEASURIN G 12.2 BY 7.5 INCHES. APPLIED SURFACE TREATEMENT OF ALODINE AND WASH PRIMER AND EPOXY PRIMER TO DOUBLERS AND REPAIR ARE AS. ATTACHED TO AIRCRAFT, APPLIED FILLET SEAL TO ALL EDGES OF THE DOUBLERS. APPLIED FINISH PAINT. WORK DONE IAW SAAB 340 SRM 53-70-10, PAGES 227-219 AND SAAB 340 SRM STANDARD PRACTICES. A/C OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999061800641 19990618 00641 NM 1999 6 18 USAA990429 1 19990502 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK IN FRAME AT BS 400 BETWEEN STRINGER 8L AND STRINGER 9. FABRICATED DOUBLER AND INSTALLED PER EA 64326. (M) 2 L 7 2 4F RT A16WE 1999061800642 19990618 00642 NM 1999 6 18 USAA990362 1 19990502 A 5320 WEB BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURNG Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK .5 INCH VERTICAL ON WEB AT STATION 178 RBL 4.5 WL 201 BULKHEAD WE B. INSTALLED DOUBLER AND FILLER PER T/R 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999061800643 19990618 00643 NM 1999 6 18 USAABB99022 1 19990502 A 8011 9798269 STARTER BOEING 767 767201 1385125 NM LT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 650US 23902 PHL - FL126 - CREW RECEIVED EICAS MESSAGE 'L STARTER CUTOUT' ON CLIMB-OUT FROM PHL. FLIGHT RETURNED TO PHL AND LANDED W ITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE STARTER AND START VALVE. (M) 2 L 7 2 4F RT A1NM 1999061800644 19990618 00644 NM 1999 6 18 99ZZZM357 1 19990502 A 8012 350544851 START VALVE BOEING 767 767201 1385125 NM LT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 650US 23902 PHL - FL126 - CREW RECEIVED EICAS MESSAGE 'L STARTER CUTOUT' ON CLIMB-OUT FROM PHL. FLIGHT RETURNED TO PHL AND LANDED W ITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE STARTER AND START VALVE. (M) 2 L 7 2 4F RT A1NM 1999061800645 19990618 00645 NE 1999 6 18 EISA99063 2 19990402 A 7314 371900 FUEL PUMP BOEING 727 727264 138408M NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE FAILED A EISA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 15DF 20710 665416 NR 1 ENGINE FAILED ON TAKEOFF. FOUND NR 1 ENGINE FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED FUEL PUMP. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999061800646 19990618 00646 NE 1999 6 18 EISA99064 2 19990327 A 7270 589470 CASE BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 649129 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND NR 3 ENGINE FAN EXIT CASE CRACKED AROUND STATOR ON LEFT SIDE AT 9 O'CLOCK POSITION AND RIGHT SIDE AT 2 O'CLOCK POSITION JUST ABOVE CASE SPLIT LINE. REMOVED AND REPLACED FAN EXIT CASE PER 727 OVERHAUL MANUAL 72-00-34. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999061800647 19990618 00647 NM 1999 6 18 EISA99065 1 19990327 A 5754 65162293 RIB BOEING 727 727223 1384074 NM NR 4 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND NR 4 SLAT OUTBOARD SUPPORT CRACKED. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1999061800648 19990618 00648 NM 1999 6 18 EISA99066 1 19990327 A 5754 65162241 RIB BOEING 727 727223 1384074 NM NR 1 LE SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND INBOARD RIB AND RIB ATTACH ANGLE CRACKED AT NR 1 SLAT ACTUATOR. REMOVED AND REPLACED SLAT WITH A SERVICEABLE UNIT PER MM 27-81-11. (M) 2 L 7 3 4F A3WE 1999061800649 19990618 00649 NM 1999 6 18 MZZA99084 1 19990304 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 950-979.5 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON STRINGER 27R TEE CHORD AT C2 DOOR CUT OU T OUTBOARD HORIZONTAL FLANGE UPPER SURFACE BETWEEN 950E PLUS 12.5 AND BS 979.5. THE CORRODED AREA WAS REMOVED AND REPAI RED PER EC/RA 5310-03841 DATED 14 APR 1999. (M) 2 L 7 3 4F A3WE 1999061800650 19990618 00650 1999 6 18 RAIA990524 4 19990517 A 3425 7003360944 COMPUTER AEROSP ATR42 ATR42300 8680920 EU NR 2 AHRS FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 424TE 15647 124 FLT 7326 - STL - EFIS COMP FAULTED. MAINTENANCE REPLACED NR 2 AHR'S COMPUTER. (M) 2 H 7 2 4T RT A53EU 1999061800651 19990618 00651 SO 1999 6 18 RAIA990528 1 19990519 A 2430 K0291 CONTACTOR EMB 145 EMB145 SO APU FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 145077 FLT 5780 - ORD - IMMEDIATELY AFTER STARTING ENGINE NR 1, DC BUS NR 1 AND GEN NR 1 AND 3 TRIPPED OFF LINE WITH MULTIPLE E ICAS MESSAGES. MAINTENANCE REPLACED APU LINE CONTACTOR. (M) 2 L 7 2 4F RT T00011AT 1999061800652 19990618 00652 EU 1999 6 18 RAIA990525 1 19990518 A 7922 L8523427 VERNITHERM BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 340TE 939 FLT 7215 - STL - LEFT ENGINE OIL TEMP AT RED LINE. MAINTENANCE REPLACED LEFT ENGINE OIL COOLER VERNITHERM. (M) 2 L 7 2 4T RT A56EU 1999061800653 19990618 00653 1999 6 18 RAIA990522 4 19990517 A 3442 6227337001 RADAR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 343TE 14501 955 FLT 7465 - ALO - WEATHER RADAR INOPERATIVE. MAINTENANCE REPLACED RADAR R/T. (M) 2 L 7 2 4T RT A56EU 1999061800654 19990618 00654 NM 1999 6 18 USAA990431 1 19990502 A 5313 BAC1498156 STRINGER BOEING 737 7372B7 1384560 NM BS 1010 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 45252 22883 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH SECTION OF STRINGER 27L CORRODED AT STAITON 1010. SPLICES STR INGER PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999061800655 19990618 00655 NM 1999 6 18 USAA990208 1 19990423 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 45029 22879 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 5R TIE CLIP. REPLACED PART. (M) 2 L 7 2 4F A16WE 1999061800656 19990618 00656 NM 1999 6 18 USAASB99105 1 19990416 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 558AU 23512 IAH - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE B ATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800657 19990618 00657 NM 1999 6 18 USAASB99115 1 19990429 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 592US 23937 ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE, FORWARD EXIT SIGNS IN FORWARD GALLEY, SEAT ROW 1 LOW LEVEL EVACUATION LIGHT, MAIN ENTRY DOOR EXIT SIGN, ESCAPE SLIDE LIGHT FOR FORWARD SERVICE DOOR, SEAT ROWS 2 AND 3 BULLN OSE LIGHTS, EXTERIOR OVERWING LIGHTS RIGHT SIDE, SEAT ROWS 12 THROUGH 16 LOW LEVEL EVACUATION LIGHTS, SEAT ROWS 11 AND 1 8 BULLNOSE EMERGENCY LIGHTS AND AFT ENTRY DOOR SIDEWALL EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAT TERY PACKS AT THE FORWARD ENTRYWAY CEILING AND AT SEAT ROW 17 CEILING CENTERLINE AND RELAMPED THE AFT ENTRY DOOR SIDEWAL L EXIT SIGN. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800658 19990618 00658 NM 1999 6 18 USAASB99113 1 19990427 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AU 22757 BDL - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE AFT ENTRY DOOR REMAINS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800659 19990618 00659 NM 1999 6 18 USAASB99112 1 19990422 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 779AU 24996 IAH - MAINTENANCE FOUND THE RIGHT AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800660 19990618 00660 NM 1999 6 18 USAASB99111 1 19990421 A 3350 20121 BATTERY CHARGER BOEING 737 737401 1384701 NM BS 747 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 408US 23878 IAH - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY EXIT LIGHTING AT SEAT ROWS 12 THROUGH 19 INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE BATTERY CHARGER AT STATION 747, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800661 19990618 00661 NM 1999 6 18 USAASB99110 1 19990426 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 228US 21817 CLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FO UND THE INTERIOR LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPE RATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800662 19990618 00662 NM 1999 6 18 99ZZZM358 1 19990426 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 228US 21817 CLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FO UND THE INTERIOR LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPE RATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800663 19990618 00663 NM 1999 6 18 USAABB99021 1 19990430 A 3350 20121 BATTERY CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648US 23900 PHL - FOUND LEFT FORWARD EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER. (M) 2 L 7 2 4F RT A1NM 1999061800664 19990618 00664 1999 6 18 USAASB99119 4 19990503 A 3417 HG480B13 ADC BOEING 737 737201 1384454 NM E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 245US 34956 22751 TPA - FLT 2636 - AT ROTATION ON TAKEOFF FROM TPA, CREW RECEIVED THE FOLLWING INDICATIONS, FIRST OFFICER ALTIMETER INDICA TED STANDBY AND COULD NOT BE RESET, FIRST OFFICER MACH INOPERATIVE, FIRST OFFICER VSI FLAG, ACARS INOPERATIVE, MACH TRIM FAIL AND ALTITUDE ALERT INOPERATIVE. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENC Y WAS DECLARED. REINSTALLED DISCONNECTED PITOT AND STATIC LINES TO AIR DATA COMPUTER. CHECKED BOTH BUSSES FOR PROPER O PERATION. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800665 19990618 00665 NM 1999 6 18 USAASB99117 1 19990502 A 3350 S106 BATTERIES BOEING 737 7372B7 1384560 NM COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 280AU 22892 CLE - MAINTENANCE FOUND THE EMERGNCY LIGHT IN THE COCKPIT CEILING WILL NOT ILLUMINATE WHEN TESTED. MAINTENANCE FOUND BA TTERIES CORRODED WHICH IN TURN HAD SPREAD TO THE LIGHT ASSEMBLY. REMOVED AND REPLACED ENTIRE LIGHT ASSEMBLY (P/N 10-006 7-9) INCLUDING BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800666 19990618 00666 NM 1999 6 18 USAASB99120 1 19990503 A 3320 FT1142 TRANSFORMER BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 279AU 22891 IAD - FL2721 - ON DESCENT, CREW NOTICED AN ELECTRICAL SMELL IN THE FORWARD CABIN. FOUND THE CIRCUIT BREAKER FOR THE FOR WARD PASSENGER CABIN CEILING LIGHT TRIPPED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TH E LEFT CABIN CEILING LIGHT BALLAST OVERHEATED AND THE TRANSFORMER BURNED OUT. REMOVED AND REPLACED THE CABIN CEILING LI GHT TRANSFORMER. INSPECTED WIRING AND BALLAST. RESET CABIN CEILING LIGHTS CIRCUIT BREAKER. OPERATIONAL CHECK OF LIGHT ING SYSTEM GOOD. (M) 2 L 7 2 4F A16WE 1999061800667 19990618 00667 NM 1999 6 18 USAASB99126 1 19990516 A 3350 15AT17 SWITCH BOEING 737 7372B7 1384560 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 272AU 22884 BWI - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CO NTROL SWITCH IN THE COCKPIT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800668 19990618 00668 NM 1999 6 18 USAASB99122 1 19990506 A 3397 WIRE BOEING 737 737401 1384701 NM ROW 8 BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 412US 23881 PHL - MAINTENANCE FOUND THE CABIN FLOOR EMERGENCY PROXIMITY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT S EAT ROW 8. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800669 19990618 00669 NM 1999 6 18 USAASB99102 1 19990417 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM ROW 5A/16A DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 226US 21815 EWR - MAINTENANCE FOUND SEVERAL CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY P ACKS AT SEATS 5A AND 16A AND RERACKED REMAINING BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800670 19990618 00670 NM 1999 6 18 USAASB99101 1 19990411 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM LT/RT EXTERIOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 226US 21815 TPA - MAINTENANCE FOUND THE LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE LEFT AND RIGHT BATTERY PACKS IN THE AFT CARGO COMPARTMENT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800671 19990618 00671 NM 1999 6 18 USAASB99103 1 19990419 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM ROW 16 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 226US 21815 BOS - PILOT REPORTED THAT THE AFT BATTERY PACK UNDER SEAT 16 LEFT NEEDS REPLACED DUE TO THE EMERGENCY LIGHTS ILLUMINATIN G DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT SEAT 16, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800672 19990618 00672 1999 6 18 USAASB99106 4 19990420 A 3425 7725005009 ADI BOEING 737 737401 1384701 NM RT COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 424US 28009 23991 CLT - FLT 306 - JUST AT ROTATION, WHILE TAKING OFF FROM CLT, THE FIRST OFFICERS ADI CIRCUIT BREAKER TRIPPED. CREW RESET THE CIRCUIT BREAKER BUT IT TRIPPED AGAIN. CREW ELECTED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS ADI. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800673 19990618 00673 NM 1999 6 18 TSAA9933233 1 19990510 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 831-838 CRACK A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 WHILE PERFORMING THE EXTERIOR LOW FREQUENCY EDDY CURRENT INSPECTION REQUIRED BY AD 97-22-07 (AD 94-25-05 SUPERSEDED AD) A CRACK WAS DISCOVERED ON STRINGER 10R LAP JOINT AT BS 831 THROUGH 838. THE LAP JOINT WAS REPAIRED IAW 737 SRM 53-30-03 FIG 42. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999061800674 19990618 00674 NM 1999 6 18 TSAA9927234 1 19990519 A 5753 654643927 TRACK BOEING 737 73725A 1384481 NM TE FLAP LOOSE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING WALKAROUND INSPECTION, THE NR 1 ENGINE AFT MOUNT INDICATOR MARKINGS WERE NOTED AS BEING MISALIGNED BY THE MECHANI C. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT ON THE NR 3 TRACK ASSY (1) ONE MOUTN BOLT WAS LOOSE AND ALSO THE A FT MOUNT BORE WAS FOUND ELONGATED OUT OF LIMITS DUE TO THE TRACK ASSY BEING LOOSE AND FREE TO MOVE. WORK IN PROGRESS TO REPLACE WORN TRACK ASSY AND ASSOCIATED HARDWARE. (M) 2 L 7 2 4F RT A16WE 1999061800675 19990618 00675 NM 1999 6 18 TSAA9957235 1 19990520 A 5754 65C266031375P SKIN BOEING 737 737282 13844AT NM RT LE SLAT CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 WHILE PERFORMING THE WALKAROUND INSPECTION, A CRACK WAS DISCOVERED ON THE NR 3 SLAT. THE CRACK WAS ON THE LOWER SKIN IN BOARD EDGE, 2 INCH FORWARD FROM THE AFT EDGE. THE CRACK WAS REPAIRED IAW ECO 2976 PART I. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 1999061800676 19990618 00676 NM 1999 6 18 UIEA9925 1 19990508 A 5230 MS20470B524 RIVET BOEING 747 747230B 1384889 NM CARGO DOOR FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 507MC 21380 FLT NR IB9709 - VCP/EZE - ATB - AT 10,000 FEET DISCOVERED AIRCRAFT UNABLE TO PRESSURIZE. ALL DOOR LIGHTS EXTINGUISHED A ND SUFFICIENT AIRFLOW IN THE AIRCRAFT. USE FHB PROCEDURE AND INSPECTED AS MUCH OF AIRCRAFT AS POSSIBLE TO DETERMINE NO HOLES AND PRESSURIZATION CONTROLLER OK. RETURNED TO VCP. AFTER ARRIVAL, MAINTENANCE FOUND AFT LOWER CARGO DOOR HANDLE RIVET SHEARED ALLOWING LOWER PORTION OF HANDLE TO OPEN CAUSING PRESSURE RELIEF DOORS TO OPEN. REPLACED SHEAR PIN AND OP ERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1999061800677 19990618 00677 NM 1999 6 18 UIEA9924 1 19990516 A 3246 TIRE BOEING 747 7472D3B 1384805 NM RT MLG FAILED A UIEA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 EA 15 506MC 21252 FLT EK9990 - AMS/DXB - ATB - DURING TAKEOFF ROLL, AIRFRAME VIBRATION OCCURRED AT 160 KNOTS. VIBRATION INCREASED AS AIRS PEED INCREASED. ALL OTHER INDICATION NORMAL. ON CLIMB-OUT, AMS CONTROL ADVISED THAT PIECES OF RUBBER WERE FOUND ON THE RUNWAY. ATLAS AIR OPERATIONS CONTROL CENTER, JFK ADVISED CREW TO RETURN AMS. MAINTENANCE FOUND NR 11 TIRE SEPARATED A ND DAMAGE TO WHEEL WELL CONDUIT, TE FLAP RODS, BODY GEAR STEERING MODULE, SEVERAL FAIRING PANELS DAMAGED AND LOWER CHORD CRACKED AT STATION 1480. ALL DAMAGED COMPONENTS/EQUIPMENT REPLACED. ALL SYSTEM NOW OPERATIONAL. (M) 2 L 7 4 4F RT A20WE 1999061800678 19990618 00678 1999 6 18 UIEA9923 4 19990516 A 3425 INS BOEING 747 7472D7B 1384803 NM COCKPIT MALFUNCTIONED A UIEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 526MC 22337 FLT AZ9204 - MXP/JFK - ATB - ALL THREE INS SYSTEMS MALFUNCTIONED. ALL PREFLIGHT FUNCTIONS WERE NORMAL, INS ALIGNED AND LOADED PROPERLY. AFTER DEPARTURE FROM MXP, UPDATED NR 1 INS USING LSA (VOR) AND GVA FOR NR 2 INS, UPDATE PROPERLY OBTAI NED. A SECOND UPDATE WAS ATTEMPTED AT LBL (VOR). ALL THREE (3) INS WARNING LIGHTS APPEARED AT THE SAME TIME AND ALL EX HIBITED THE SAME FAULT CODE. ATLAS AIR OPERATIONS CONTROL CENTER. JFK REQUESTED CREW TO RETURN TO MXP, DUMPED FUEL AND RETURNED TO MXP. INS NAVIGATION UNITS REPLACED. OPERATIONS CHECKS NORMAL. NO OTHER ABNORMALITIES OBSERVED. (M) 2 L 7 4 4F RT A20WE 1999061800679 19990618 00679 NM 1999 6 18 P2EA99184 1 19990512 A 3246 TIRE BOEING 737 737222 1384473 NM NR 2 MLG FAILED A P2EA O OTHER O OTHER LD LANDING 1 CE 05 603DJ 19955 MDW - FLT 709 - ON LANDING, NR 2 MAIN TIRE BLEW. LANDING AND ALL OTHER INDICATIONS NORMAL. REPLACED NR 2 MAIN WHEEL AS SEMBLY PER MM 32-45-11. REPLACED NR 1 MAIN TIRE ASSEMBLY PER MM 32-45-11 DUE TO NR 2 MAIN TIRE DISCREPANCY. (M) 2 L 7 2 4F A16WE 1999061800680 19990618 00680 NM 1999 6 18 P2EA99165 1 19990501 A 5350 RADOME BOEING 737 737247 138448D NM BS 178 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 MDW - PUSH BACK TUG HIT AIRCRAFT DAMAGING RADOME AND FUSELAGE SKIN AT BS 178 AT 6 O'CLOCK POSITION. REPLACED RADOME. F USELAGE SKIN AT BS 178 REPAIRED BY TWA PER TWA ENG ARA NR'S 13540, 13541, 13542 DATED 5/3/99. (M) 2 L 7 2 4F A16WE 1999061800681 19990618 00681 NM 1999 6 18 P2EA99185 1 19990514 A 5270 SOCKET 693735211 BOEING 737 737297 1384480 NM EQUIPMENT DOOR INOPERABLE A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 5WM D00090 22629 MCI - FLT 301 - AIR RETURN, NO EMERGENCY DECLARED, LANDING UNEVENTFUL. AT APPROXIMATELY 1,000 FEET AGL, MASTER CAUTION LIGHT CAME ON, EQUIPMENT DOOR LIGHT CAME ON, AND UNABLE TO PRESSURIZE. SECURED E/E DOOR CLOSED. DEFERRED MEL 52-3 C1 NR M005564 PER MAINTENANCE CONTROL 'EQUIP' LIGHT SOCKET BAD. REPLACED DOOR WARNING LIGHT MODULE PER MM 52-71-0, OPS CHE CK NORMAL. THIS CLEARS DEFERRAL M005564. (X) 2 L 7 2 4F A16WE 1999061800682 19990618 00682 NM 1999 6 18 P2EA99186 1 19990516 A 3260 BULB BOEING 737 737247 138448D NM RT MLG FAILED A P2EA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 05 912MP 19607 PIT - 588 - RIGHT MAIN INDICATION LIGHT WOULD NOT COME ON AFTER LOWERING GEAR HANDLE ON FINAL. RAISED GEAR ON GO AROUND . CHANGED BULBS, LOWERED GEAR AGAIN. RIGHT MAIN INDICATION NORMAL, THEN LEFT MAIN INDICATION WAS OUT. CHANGED BULBS I N LEFT MAIN AND ALL INDICATIONS WORKED NORMAL, 3 GREEN. SIMULATED (TARGETED) EXTENSION AD RETRACTION OF LANDING GEAR PE R MM 31-26-0, INDICATION AND AURAL WARNING SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1999061800683 19990618 00683 NM 1999 6 18 P2EA99190 1 19990517 A 5240 BEAM BOEING 737 737205 NM R1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURNG C-CHECK, THE FORWARD SERVICE DOOR (R1) INTERNAL BEAM NR 7 AFT SECTION IS CRACKED. REPAIRED PER SRM 51-10-03 FIGURE 1. (M) 2 L 7 2 4F A16WE 1999061800684 19990618 00684 NM 1999 6 18 P2EA99189 1 19990508 A 5330 SKIN BOEING 737 737205 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, A CRACK WAS FOUND AT THE EXTERNAL FUSELAGE NR 3 WINDOW CUTOUT. REPAIRED PER S/B 737-53-1115 DATED JAN 2, 1988, SECTION II FIG 3. (M) 2 L 7 2 4F A16WE 1999061800685 19990618 00685 NM 1999 6 18 P2EA99188 1 19990507 A 5712 RIB BOEING 737 737205 NM BS 70.85 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURNG C-CHECK, WHILE INSPECTING THE LEFT WING TO BODY RIB CHORD AT BS 665, BBL 70.85, A CRACK WAS NOTED ON THE HOR IZONTAL FLANGE. LENGTH 2 INCH. THAT CRACK ENDED IN A FASTENER HOLE. THIS DAMAGE IS ACCEPTABLE BUT REQUIRES REINSPECTI ON AT 1500 CYCLE INTERVALS. PERMANENT REPAIR REQUIRED WITHIN 2 YEARS PER S/B 737-57-10S7 REV 8. (M) 2 L 7 2 4F A16WE 1999061800686 19990618 00686 NM 1999 6 18 P2EA99187 1 19990508 A 5240 SKIN BOEING 737 737205 NM R1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, A CRACK WAS FOUND ON THE R1 DOOR, EXTERNAL SKIN, NEAR THE LOWER HINGE, LENGTH .5 INCH. REPAIRED P ER SRM 52-00-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999061800687 19990618 00687 NM 1999 6 18 99ZZZM359 1 19990526 A 3350 6104781 BATTERY PACK BOEING 727 727264 138408M NM L2 AND R2 DOOR DISCHARGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 763AT 22983 DURING PREFLIGHT, FOUND AFT EXTERIOR EMERGENCY LIGHTS FOR THE L2 AND R2 SLIDE LIGHTS OUT. BATTERY PACK WAS REPLACED, CH ECKED OPS GOOD. (M) 2 L 7 3 4F A3WE 1999061800688 19990618 00688 NM 1999 6 18 99ZZZM360 1 19990526 A 3350 6013211 POWER SUPPLY BOEING 727 727264 138408M NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 763AT 22983 DURING PREFLIGHT, FOUND THE FORWARD OUTSIDE SLIDE LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY FOR THE OUTSIDE SLI DE LIGHTS, OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999061800689 19990618 00689 SO 1999 6 18 COMA9910088 1 19990528 A 3350 D36604001 BATTERIES EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 726 120152 HTS - FLT 5730 - EMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES. (M) 2 L 7 2 4T RT A31SO 1999061800690 19990618 00690 SO 1999 6 18 COMA9910087 1 19990528 A 3350 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 267CA 120259 GRR - FLT 5024 - EMERGENCY LIGHTS ARE INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHTS OPERATE NORMAL. (M) 2 L 7 2 4T RT A31SO 1999061800691 19990618 00691 SO 1999 6 18 COMA9910086 1 19990525 A 3350 1011107 SIGN EMB 120 EMB120RT SO CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 268CA 120262 MCO - FLT 5143 - EMERGENCY EXIT SIGN AT ROW 5A IS DIM. REPLACED SIGN. (M) 2 L 7 2 4T RT A31SO 1999061800692 19990618 00692 SO 1999 6 18 COMA9910085 1 19990525 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 1063 120152 LAN - FLT 5076 - EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERIES. (M) 2 L 7 2 4T RT A31SO 1999061800693 19990618 00693 SO 1999 6 18 COMA9910084 1 19990525 A 3260 922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO LT MLG FAILED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 247CA 225 LEFT MLG DOWN INDICATOR ON WITH GEAR RETRACTED. LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. FREE FALL SYSTEM USED TO EXTEND GEAR. REPLACED DOWN LOCK PROXIMITY SENSOR. (M) 2 L 7 2 4T RT A31SO 1999061800694 19990618 00694 NM 1999 6 18 USAA990375 1 19990519 A 5753 65C263434 SUPPORT BOEING 737 737401 1384701 NM TE MID FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30855 23877 CLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, INBOARD SUPPORT ARM AT ECCENTRIC BEARING BORE. CORROSION TASK C57-306-04. CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2 L 7 2 4F RT A16WE 1999061800695 19990618 00695 NM 1999 6 18 USAA990376 1 19990519 A 5753 655224617 SUPPORT BOEING 737 737401 1384701 NM TE MID FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30855 23877 CLT - DURING SHOP VISIT, FOUND CORROSION ON CARRIAGES SUPPORT ARM INBOARD MID FLAP, INBOARD CARRIAGE, OUTBOARD ARM AT BE ARING MOUNT HOLE FOR ECCENTRIC BUSHING. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2 L 7 2 4F RT A16WE 1999061800696 19990618 00696 NM 1999 6 18 USAA990373 1 19990519 A 5753 65C263433 SUPPORT BOEING 737 737401 1384701 NM TE MID FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30855 23877 CLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP OUTBOARD CARRIAGE, OUTBOARD SUPPOR T ARM AT ECCENTRIC BEARING BORE. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTIC AL PART NR. (M) 2 L 7 2 4F RT A16WE 1999061800697 19990618 00697 NM 1999 6 18 USAA990374 1 19990519 A 5753 655224615 SUPPORT BOEING 737 737401 1384701 NM TE MID FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 30855 23877 CLT - DURING SHOP VISIT, FOUND CORROSION IN BEARING RETAINER BORE AT INBOARD MID FLAP INBOARD CARRIAGE, INBOARD SUPPORT ARM, AT ECCENTIC BEARING BORE. CORROSION TASK NR C57-306-04, CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M) 2 L 7 2 4F RT A16WE 1999061800698 19990618 00698 NM 1999 6 18 USAA990480 1 19990521 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 28582 24549 CLT - DURING RON, FOUND 1.5 INCH LONG CRACK ON SKIN AT RIGHT FUSELAGE STATION 7270 AT STRINGER 23R. INSTALLED DOUBLER P ER TYPICAL REPAIR 53-60-03. (M) 2 L 7 2 4F RT A16WE 1999061800699 19990618 00699 NM 1999 6 18 USAA990461 1 19990522 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .250 INCH BY .250 INCH AREAS OF CORROSION ON FLOORBEAM AT BS 986.5 AT LBL 45.5-RBL 45.5. C ORROSION LEVEL 2. INSTALLED NEW 'T' CAP PER TR 53-60-01. (M) 2 L 7 2 4F RT A16WE 1999061800700 19990618 00700 NM 1999 6 18 USAA990457 1 19990522 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND 1 INCH BY 1 INCH CORRODED AREA ON FLOORBEAM AT BS 312 RBL 37, WL 208.1. CORROSION LEVEL 2 . CORROSION TASK NR C53-107-02. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999061800701 19990618 00701 NM 1999 6 18 USAASB99092 1 19990407 A 2424 948F4581 GCU BOEING 737 7374B7 1384702 NM NR 2 GEN FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 435US 34179 24557 LGA - FLT 1290 - ON APPROACH TO LGA, DESCENDING THROUGH FL 180, CREW SMELLED A STRONG ELECTRICAL ODOR IN THE FLIGHT COMP ARTMENT. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. IT WAS NOTED THAT THE NR 2 GENERATOR CONTROL BREAKER WAS TRIPPED. MAINTENANCE FOUND THE NR 2 GENERATOR CONTROL UNIT WITH BURNED COMPONENTS. R EMOVED AND REPLACED THE NR 2 GENERATOR CONTROL UNIT. RESET BREAKER AND RAN ENGINES. ACCOMPLISHED OPERATIONAL CHECK PER MM 24-21-81. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800702 19990618 00702 NM 1999 6 18 USAASB99132 1 19990530 A 3320 61362 BALLAST BOEING 737 737201 1384454 NM GALLEY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 233US 22273 ALB - FL 548 - AFTER TAKEOFF, AT APPROXIMATELY 2,000 FEET, CREW NOTICED SMOKE IN THE COCKPIT. CAPTAIN DECLARED AN EMERG ENCY AND RETURNED TO FIELD AT ALB. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TH E BALLAST FOR THE ENTRYWAY FLUORESCENT LIGHTS IN THE FORWARD GALLEY CEILING, JUST AFT OF COCKPIT DOOR BURNED AND LEAKING . REMOVED AND REPLACED BALLAST. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999061800703 19990618 00703 EU 1999 6 18 USAAF99027 1 19990521 A 2913 42047 PUMP FOKKER F28 F28MK0100 4990807 EU RT ENGINE FAILED A USAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 882US 14105 11334 SBN - FLT 1240 EN ROUTE PIT-SBN, CREW EXPERIENCED TOTAL HYDRAULIC FAILURE. FLIGHT PROCEEDED TO SBN. UPON LANDING, THE NR 3 TIRE BLEW, CAUSING LOSS OF DIRECTIONAL CONTROL OF THE AIRCRAFT. THE AIRCRAFT CAME TO A STOP APPROXIMATELY 6000 FEE T DOWN THE RUNWAY AND OFF THE LEFT SIDE OF THE RUNWAY. MAINTENANCE FOUND THE NR 2 ENGINE EDP LEAKING AND THE NR 2 HYDRA ULIC SYSTEM EMPTY. IT IS NOT KNOWN WHY THE NR 1 SYSTEM FAILED. THE LOSS OF DIRECTIONAL CONTROL WAS DUE TO ANTI-SKID OP ERATION ON LANDING, CAUSING THE TIRE TO BLOW. (M) 2 L 7 2 4F RT 1999061800704 19990618 00704 NM 1999 6 18 USAABB99026 1 19990515 A 3350 873100151REV9 LIGHT BOEING 757 7572B7 1384964 NM ROW 29 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 SFO - FOUND FLOOR EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1999061800705 19990618 00705 NM 1999 6 18 USAABB99027 1 19990517 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 PIT - FOUND R1 DOOR EMERGENCY EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1999061800706 19990618 00706 NM 1999 6 18 USAASB99128 1 19990523 A 5210 BAC1521522 SEAL BOEING 737 737201 1384454 NM PAX DOOR FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 223US 21665 RDU FL324 - ON CLIMB-OUT FROM CLT, JUST PRIOR TO PASSING RDU, CAPTAIN REPORTED HEARING TWO LOUD BANGS FROM THE FORWARD C ABIN/MAIN ENTRY DOOR AREA. FLGIHT DIVERTED TO RDU AND LANDED WITHOUT FURTHER INCIDENT. RDU MAINTENANCE HAD DIFFICULTY OPENING THE DOOR, SO THE PASSENGERS HAD TO EXIT FROM THE AFT ENTRY DOOR. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD ENTRY DOOR SEAL HAD BLOWN. REMOVED AND REPLACED DOOR SEAL AND TWO ROLLERS THAT WERE FOUND BROKEN. PRESSURI ZATION CHECK AND OPERATIOAL CHECK OF DOOR NORMAL. (M) 2 L 7 2 4F A16WE 1999061800707 19990618 00707 WP 1999 6 18 USAAD99070 1 19990601 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 814US 48094 IND - FOUR LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHTS BATTERIES. (M) 2 L 7 2 4F A6WE 1999061800708 19990618 00708 NM 1999 6 18 USAA049905 1 19990415 A 3610 652244419 DUCT BOEING 727 727254 138408L NM NR 1 PYLON DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 19 916TS 20437 FLT 6520- DCA-LGA - AIR RETURN TO DCA - NR 1 ENGINE FIRE LIGHT ILLUMINATED ON TAKEOFF, REDUCED THROTTLE TO IDLE, LIGHT E XTINGUISHED MOMENTARILY. RANCID SMELL IN CABIN, NO SECONDARY ENGINE INDICATIONS. REPLACED 8TH STAGE DUCT. (M) 2 L 7 3 4F A3WE 1999061800709 19990618 00709 EU 1999 6 18 SIMA991412 1 19990521 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 293AT 18407 293 SAW - DURING PS-2 INSPECTION, FOUND FORWARD EMERGENCY FLOOR, EXTERIOR AND EMERGENCY EXIT DOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 3WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 1999061800710 19990618 00710 EU 1999 6 18 SIMA991314 1 19990511 A 2530 16707 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU GALLEY FAILED A SIMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 275BC 275 DCA - FLT 4944 - FLIGHT ATTENDANT REPORTED SMOKE SMELL COMING FORM THE GALLEY. CREW PULLED THE HOT CONTAINER CIRCUIT BR EAKERS. UPON LANDING, SMOKE WAS COMING FROM THE GALLEY. REMOVED AND REPLACED BOTH HOT JUG CONNECTORS. AIRCRAFT RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800711 19990618 00711 EU 1999 6 18 SIMA991374 1 19990517 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 3651 017 SAW - DURING PS-2 INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY PACK AT LOCATION 10WL WAS DISCHARGED. REMOVED AND REPLA CED THE BATTERY PACK IAW JIC 33-51-20. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800712 19990618 00712 EU 1999 6 18 SIMA991163 1 19990426 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AT 4183 0249 SAW - DURING PS-2 INSPECTION, NUMEROUS FORWARD EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGH T BATTERY PACK AT LOCATION 3WL IAW JIC 335121-RA1-10000. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800713 19990618 00713 EU 1999 6 18 SIMA991202 1 19990430 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 141AE 14873 141 SAW - DURNG PS-2 INSPECTION, FOUND THE AFT EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 18WL IAW JIC 335000-OPT-10000. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800714 19990618 00714 EU 1999 6 18 SIMA991201 1 19990430 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 4308 135 SAW - DURING PS-2 INSPECTION, FOUND NUMEROUS CABIN EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATION 3WL AND 10WL IAW MIC 335000-OPT-10000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800715 19990618 00715 EU 1999 6 18 99ZZZM361 1 19990430 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 3936 135 SAW - DURING PS-2 INSPECTION, FOUND NUMEROUS CABIN EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATION 3WL AND 10WL IAW MIC 335000-OPT-10000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800716 19990618 00716 EU 1999 6 18 SIMA991234 1 19990503 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 3539 223 SAW - DURING PS-2 INSPECTION, FOUND FORWARD EMERGENCY FLOOR PROXIMITY LIGHTS BATTERY PACK HAD LOW VOLTAGE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT LOCATION 3WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800717 19990618 00717 EU 1999 6 18 SIMA991442 1 19990524 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 11712 223 SAW - DURING PS-2 INSPECTION, FOUND FORWARD UPPER EMERGENCY EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED E MERGENCY LIGHT BATTERY PACK AT LOCATION 3WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800718 19990618 00718 EU 1999 6 18 SIMA991402 1 19990520 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 222NE 340B222 ABI - DURING MBV INSPECTION, FOUND CHAFE ON THE LEFT INBOARD NACELLE OUTER SKIN PANEL. CUTOUT PUNTURE AREA OF CHAFE AND BLENDED THE REMAINING CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE REWORK AREA WITH NO CRACK INDICATIONS N OTED. RESTORED PROTECTIVE TREATMENT TO THE CHAFED AREA INCLUDING THE POLYURETHANE TOP COAT. FABRICATED A DOUBLER AND T RIPLER .050 THICK. FABRICATED A SHIM .020 THICK. APPLIED PROTECTIVE TREATMENT REPARI PARTS INCLUDING POLYURETHANE TOP COAT. APPLIED SEALANT TO THE CONTACT SURFACES OF THE REPAIR PARTS, REPOSITIONED, AND INSTALLED FASTENERS WET. APPLIED FILLET SEALANT AROUND EDGES OF THE REPAIR PARTS. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS 2 L 7 2 4T RT A52EU 1999061800719 19990618 00719 EU 1999 6 18 DKAA99014 1 19990521 A 3230 A23802102 SWITCH AMD FALC20 FALCON20C5 2730107 EU NLG FAILED A DKAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 810RA 284 81 GEAR HANDLE WOULD NOT RAISE (CMH). FERRIED AIRCRAFT CMH TO YIP (PERMIT NR 99-01). REPLACED LANDING GEAR MICROSWITCH (1 2G). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A7EU 1999061800720 19990618 00720 WP 1999 6 18 ASAA9980124 1 19990524 A 5610 HINGE PIN DOUG DC9 DC982 3022082 WP LT COCKPIT LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 PDX - AFTER ARRIVAL OF FLT 711 - CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM CAME APART. REINSER TED THE WINDOW MECHANISM HINGE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061800721 19990618 00721 WP 1999 6 18 ASAA9980122 1 19990523 A 5610 TRACK DOUG DC9 DC982 3022082 WP LT COCKPIT LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 SEA - AFTER ARRIVAL OF FLIGHT 223, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WS DIFFICULT TO OPEN. TIGHT ENED THE UPPER WINDOW TRACK SCREWS AND SECURED THE AFT WINDOW MOLDING AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061800722 19990618 00722 WP 1999 6 18 ASAA9980119 1 19990523 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 1136-1146 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OAK - DURING 30K CHECK, FOUND CORROSION ON LONGERON 28R AT FS 1137. REPAIRED IAW ASA EA 5310-01689. (M) 2 L 7 2 4F RT A6WE 1999061800723 19990618 00723 WP 1999 6 18 ASAA9980118 1 19990425 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 208-218 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 208 TO 218. REPAIRED IAW ASA EA 5310-01679. (M) 2 L 7 2 4F A6WE 1999061800724 19990618 00724 WP 1999 6 18 ASAA9980117 1 19990425 A 5320 99236663 FITTING DOUG DC9 DC982 3022082 WP BS 218 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 PHX - DURING 15K CHECK, FOUND CORROSION ON THE LEFT FRAME SUPPORT FITTING AT FS 218. REMOVED DAMAGED SECTION OF FITTING AND INSTALLED REPAIR ANGLE AND DOUBLER IAW ASA EA 5310-01672. (M) 2 L 7 2 4F A6WE 1999061800725 19990618 00725 WP 1999 6 18 ASAA9980114 1 19990518 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO RUB ON THE FRAME DURING OPENING AND CLOSING. ADJUSTED THE L1 D OOR BAYONET ROD AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061800726 19990618 00726 WP 1999 6 18 ASAA9980115 1 19990518 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 957AS 49126 PDX - AFTER ARRIVAL OF FLIGHT 461, CREW REPORTED THE L1 DOOR WAS FOUND TO RUB ON THE FRAME WHEN CLOSING. ADJUSTED THE L 1 DOOR TORQUE TUBE MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061800727 19990618 00727 WP 1999 6 18 ASAA9980107 1 19990512 A 5210 LATCH DOUG DC9 DC983 3022083 WP R1 DOOR INOPERATIVE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 944AS 53019 SEA - PRIOR TO DEPARTURE OF FLT 566, CREW REPORTED THE R1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. CLEANED SEALANT FR OM THE R1 DOOR HOLD OPEN LATCH AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999061800728 19990618 00728 WP 1999 6 18 ASAA9980103 1 19990506 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 967AS 49103 SEA - PRIOR TO DEPARTURE OF FLIGHT 652, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. RERIGGED THE L1 DOOR IAW DC9 MM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999061800729 19990618 00729 SO 1999 6 18 C2XA99BT047 1 19990529 A 5414 SKIN EMB 145 EMB145LR SO NR 2 NACELLE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13955 145075 BTV - DURING 5A INSPECTION, FOUND FUSELAGE DAMAGE ON RIGHT SIDE UNDER NR 2 ENGINE AS MARKED. MAINTENANCE REPAIRED SKIN AS PER EMB145 SRM NR 53-31-01. PRESSURE CHECKED AIRCRAFT GOOD. (M) 2 L 7 2 4T RT T00011AT 1999061800730 19990618 00730 EU 1999 6 18 C2XA99BT048 1 19990528 A 3233 D227090001 ACTUATOR AEROSP ATR42 ATR42320 8680930 EU NLG WORN A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 09 14813 100 EWR - PERFORMING LINE MAINTENANCE UPON AIRCRAFT, MAINTENANCE NOTED NOSE LANDING GEAR ACTUATOR AFT ROD END BEARING LOOSE IN ACTUATOR FITTING. REMOVED AND REPLACED NOSE GEAR ACTUATOR OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999061800731 19990618 00731 EU 1999 6 18 C2XA99BT049 1 19990523 A 3260 141FL01B3 SWITCH AEROSP ATR42 ATR42320 8680930 EU LT MLG INOPERATIVE A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 18814 103 EWR - CREW REPORTED GEAR SYSTEM 2 SHOWS UNLOCK ON LEFT MAIN GEAR IN FLIGHT. NO CCAS WARNINGS. MAINTENANCE REMOVED AND REPLACED LEFT UPLOCK LIMIT SWITCH. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999061800732 19990618 00732 EU 1999 6 18 C2XA99BT050 1 19990525 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU LT/RT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15823 165 BTV - DURING LINE/WEEKLY CHECK FLOOR TRACK, UPPER CABIN, LEFT AND RIGHT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY PACK FORWARD LOCATION. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999061800733 19990618 00733 EU 1999 6 18 C2XA99BT051 1 19990531 A 3350 44 BULB AEROSP ATR72 ATR72212 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69901 379 EWR - CREW REPORTS STAIR EMERGENCY LIGHT NO WORKING. REMOVED AND REPLACED BULB. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999061800734 19990618 00734 SO 1999 6 18 C2XA99BT052 1 19990531 A 3350 3025101 LIGHT EMB 145 EMB145ER SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12946 145052 EWR - FLT CO4130 - CREW REPORTS RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGEN CY LIGHT ASSY. OPS CHECKED, EMERGENCY LIGHTS GOOD. (X) 2 L 7 2 4F RT T00011AT 1999061800735 19990618 00735 SO 1999 6 18 C2XA99IA295 1 19990521 A 3350 3025101 LIGHT EMB 145 EMB145ER SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15948 145056 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999061800736 19990618 00736 SO 1999 6 18 C2XA99IA294 1 19990521 A 3350 3025101 LIGHT EMB 145 EMB145ER SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15948 145056 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE LEFT HAND OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999061800737 19990618 00737 EU 1999 6 18 C2XA99IA296 1 19990524 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING LINE CHECK INSPECTION, THE FORWARD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800738 19990618 00738 SO 1999 6 18 C2XA99IA297 1 19990526 A 3350 3025101 LIGHT EMB 145 EMB145LR SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14952 145067 IAH - DURING ROUTINE INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999061800739 19990618 00739 EU 1999 6 18 C2XA99IA298 1 19990526 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14821 160 EFD - DURING MAINTENANCE INSPECTION, THE MIDDLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AT THE CENTER CABIN. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999061800740 19990618 00740 SO 1999 6 18 C2XA99IA293 1 19990523 A 3350 1317 BULB EMB 145 EMB145 SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14933 145018 IAH - DURING C-CHECK INSPECTION, FOUR OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999061800741 19990618 00741 SO 1999 6 18 C2XA99IA292 1 19990523 A 5530 14531597601 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14933 145018 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. M AINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5530-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999061800742 19990618 00742 SO 1999 6 18 C2XA99IA291 1 19990523 A 5530 14531597602 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14933 145018 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. M AINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5530-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999061800743 19990618 00743 SO 1999 6 18 C2XA99IA290 1 19990523 A 5320 14521700007 BEAM EMB 145 EMB145 SO FRAME 20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14933 145018 IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20 EXTENDING UNDER THE BUTT STR AP. MAINTENANCE REMOVED THE CORROSION AND INSTALLED REINFORCEMENTS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAI R AUTHORIZATION EC5310-01106, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999061800744 19990618 00744 SO 1999 6 18 C2XA99IA288 1 19990521 A 3350 3025101 LIGHT EMB 145 EMB145 SO RT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14959 145091 EFD - DURING MAINTENANCE INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT ASSEMLBY IAW EMB145 MM 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4F RT T00011AT 1999061800745 19990618 00745 SO 1999 6 18 C2XA99IA287 1 19990521 A 3350 GE1317 BULB EMB 145 EMB145 SO LT EMER EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14959 145091 EFD - DURNG MAINTENANCE INSPECTION, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB145 MM 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4F RT T00011AT 1999061800746 19990618 00746 CE 1999 6 18 MASA99084 1 19990526 A 6121 6014300 SWITCH BEECH 1900 1900D 1154162 CE PROP SYNC SYS LOOSE A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 2YV UE2 FLT 1031 - ABQ-ROW - EN ROUTE TO ROW,THE CREW REPORTED WHEN THE CO-PILOT PUSHED HIS PATCH SYNC SWITCH THE CIRCUIT BREAKE R FOR THE FLIGHT DIRECTOR POPPED AND A SMALL AMOUNT OF SMOKE CAME FROM THE SWITCH. THE AIRCRAFT LANDED IN ROW WITHOUT I NCIDENT. THE AIRCRAFT WAS FERRIED TO FMN WHERE MAINTENANCE RESEATED THE PITCH SYNC SWITCH, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999061800747 19990618 00747 EA 1999 6 18 MASA99085 1 19990526 A 3350 GE1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA ROW 11 FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77181 7181 FLT 6082 - MAF-PHX - PRIOR TO DEPARTURE, THE CREW REPOTED AN EMERGENCY LIGHT IN THE CEILING AT ROW 11 WAS NOT ILLUMINATI NG. MAINTENANCE DEFERRED THE CEILING EMERGENCY LIGHT PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE THE BULB WAS REPLACED. (M) 2 L 7 2 4F RT A21EA 1999061800748 19990618 00748 EU 1999 6 18 REXA99016 1 19990522 A 5610 7256110504 WINDOW SAAB SF340 SF340A 7850100 EU RT COCKPIT SHATTERED A REXA B EMER. DESCENT O OTHER CR CRUISE 1 SO 25 107PX 983142706 340A010 FIRST OFFICER SIDE WINDOW SHATTERED. REMOVED AND REPLACED RT CPT WINDOW. (M) 2 L 7 2 4T RT A52EU 1999061800749 19990618 00749 NM 1999 6 18 USAA990459 1 19990522 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 1142 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38112 23233 CLT - DURING Q-6 CHECK, FOUND 1 INCH CRACK IN RADIUS OF STRINGER AT STRINGER 5 LEFT AT STATION 1142. INSTALLED REPAIR A NGLE PER EA 64489. (M) 2 L 7 2 4F RT A16WE 1999061800750 19990618 00750 NM 1999 6 18 USAA990460 1 19990529 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURNG Q-4 CHECK, FOUND .125 INCH CRACK IN FRAME AT STATION 400 BETWEEN STRINGER 8R - STRINGER 9R (O/HEAD BIN ATTAC H). INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64581. (M) 2 L 7 2 4F RT A16WE 1999061800751 19990618 00751 NM 1999 6 18 USAA990456 1 19990511 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40049 23514 CLT - DURING C-4 CHECK, FOUND .125 INCH CRACK IN FUSELAGE SIN 727D PLUS 3 INCHES AND .5 INCH BELOW STRINGER 23R. CUT OU T DAMAGE APPROX 8 INCH BY 6 INCH AREA. INSTALLED DOUBLER AND FILLER PER TYPICAL REPAIR 53-60-03. DOUBLER MEASURES 17 I NCHES BY 17 INCHES. ADDED WEIGHT FOR REPAIR IS 2 LBS. REPAIRED PER TYPICAL REPAIR 53-60-03. (M) 2 L 7 2 4F RT A16WE 1999061800752 19990618 00752 NM 1999 6 18 USAASB99131 1 19990526 A 2424 915F2125 GCU BOEING 737 737301 1384611 NM NR 1 FAILED A USAA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 577US 31841 23742 ALB - FL1890 - APPROX 40 MILES SOUTH ALB, CREW SMELLED SMOKE IN THE COCKPIT AND NOTICED SMOKE COMING FROM THE NR 1 GENER ATOR CONTROL UNIT. CREW DONNED OXYGEN MASKS, ACCOMPLISHED EMERGENCY CHECKLIST, PULLED NR 1 GENERATOR CONTROL UNIT OFF L INE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT ALB. SOON AFTER THE NR 1 GENERATOR CONTROL UNIT WAS PULLED OFF LINE , THE SMOKE CLEARED AND THE FLIGHT WAS ABLE TO LAND AT ALB WITHOUT INCIDENT AND TAXI TO THE GATE ON ITS OWN POWER. MAIN TENANCE REMOVED AND REPLACED THE NR 1 GENERATOR CONTROL UNIT. RAN NR 1 ENGINE. ALL INDICATIONS NORMAL. OPERATIONAL CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999061800753 19990618 00753 WP 1999 6 18 USAA990440 1 19990515 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 332 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 42539 48145 PIT - DURING Q-4, C-1, QX-19 CHECK FOUND 1 INCH CRACK AT INTERCOSTAL STATION 332 LONGERON 30. STOP DRILLED CRACK AND IN STALLED DOUBLER PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 1999061800754 19990618 00754 WP 1999 6 18 USAA990441 1 19990515 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 42539 48145 PIT - DURING Q-4 CHECK, FOUND .25INCH LONG CRACK AT LOWER RT PYLON ATTACH ANGLE AT STATION 945. INSTALLED DOUBLER PER S RM 54-04 FIG 10. (M) 2 L 7 2 4F A6WE 1999061800755 19990618 00755 WP 1999 6 18 USAA990446 1 19990515 A 5320 1714673 SUPPORT DOUG DC9 DC931 3022065 WP BS 160-237 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 42539 48145 PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 2 INCH CORROSION ON FLOOR SUPPORT BETWEEN STATION 160-237 SUPPORT NR 24. CORROS ION LEVEL 1. CORROSION TASK NR C46-53303. REMOVED AND REPLACED WITH 171-4673. (M) 2 L 7 2 4F A6WE 1999061800756 19990618 00756 WP 1999 6 18 USAA990445 1 19990515 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 965 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 42539 48145 PIT - DURING Q-4 CHECK, FOUND 1 INCH BY 1 INCH CORRODED AREA AT STATION 965 FLOORBEAM RT LAV THRESHOLD ATTACH POINT. CO RROSION LEVEL 1, CORROSION TASK NR C58-53300. SPLICED IN NEW SECTION OF ANGLE PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F A6WE 1999061800757 19990618 00757 WP 1999 6 18 USAA990444 1 19990515 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 42539 48145 PIT - DURING Q-4 CHECK, FOUND 1 INCH LONG CRACK AT LOWER LEFT PYLON ATTACH ANGLE, STATION 945. INSTALLED DOUBLER PER SR M 54-04 FIG 10. (M) 2 L 7 2 4F A6WE 1999061800758 19990618 00758 WP 1999 6 18 USAA990443 1 19990515 A 5210 591412157N1 PAN DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 42539 48145 PIT - DURING Q-4 CHECK, FOUND 3 INCH CRACK IN PRESSURE PAN, FORWARD PAX DOOR, UPPER FORWARD CORNER. REMOVED AND REPLACE D PER SRM 52-05 FIG 47. (M) 2 L 7 2 4F A6WE 1999061800759 19990618 00759 WP 1999 6 18 USAA990442 1 19990515 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 42539 48145 PIT - DURING Q-4 CHECK, FOUND .75 INCH CRACK IN SKIN AT RIGHT FORWARD OVERWING EMERGENCY EXIT AFT LOWER POCKET. INSTALL ED DOUBLER REPAIR PER SRM 54-05 FIG 32. (M) 2 L 7 2 4F A6WE 1999061800760 19990618 00760 WP 1999 6 18 USAAD99058 1 19990425 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 997VJ 47336 THE TAIL CONE ACTIVATED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999061800761 19990618 00761 WP 1999 6 18 USAAD99061 1 19990503 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP ROW 9 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 976VJ 48147 IND - FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 9-13. REPLACED BATTERY. (M) 2 L 7 2 4F A6WE 1999061800762 19990618 00762 WP 1999 6 18 USAAD99062 1 19990504 A 3350 20131ALP BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 973VJ 47099 DTW - FOUND AFT LOW LEVEL EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1999062200001 19990622 00001 NM 1999 6 22 SWAA990987 1 19990609 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 660 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED, BS 660, BL 0. REPAIRED BEAM PER SWA RA NR 1 -357-0705. 2 L 7 2 4F RT A16WE 1999062200002 19990622 00002 NM 1999 6 22 SWAA990998 1 19990610 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 660 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND BEAM UPPER CHORD CRACKED AT BS 660, BL 0. REPAIRED BEAM PER BAC DRAWING. 2 L 7 2 4F RT A16WE 1999062500001 19990625 00001 NM 1999 6 25 AT9900447 1 19990616 A 3350 276005 FUSE BOEING 737 7372L9 1384497 NM CABIN BLOWN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 DURING LAY OVER CHECK, FOUND THE FORWARD SECTION OF EMERGENCY PATH LIGHTING NOT WORKING. REPLACED BAD FUSE IN BATTERY C HARGER IAW MM 33-21-27 PAGE 35. 2 L 7 2 4F RT A16WE 1999062500002 19990625 00002 SO 1999 6 25 COMA9910094 1 19990613 A 3260 922AA2YA6P272 SENSOR EMB 120 EMB120RT SO LT MLG MALFUNCTION A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 263CA 120255 LANDING GEAR DID NOT EXTEND NORMALLY. OVERRIDE SYSTEM WAS USED. REPLACED THE LEFT HAND MLG DOWNLOCK PROX SENSOR SWITCH . 2 L 7 2 4T RT A31SO 1999062500003 19990625 00003 EA 1999 6 25 COMA9960277 1 19990614 A 5330 SKIN CNDAIR CL600 CL6002B19 EA BS 640-654.5 DAMAGED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 940CA 7048 THE FUSELAGE SKIN WAS DAMAGED BETWEEN FS 6400.0 AND FS 654.5. ALSO, THE DOUBLER AND FRAME AT FS 654.5 WERE DAMAGED. RE PAIRED FUSELAGE SKIN, FRAME AND SPLICE REPAIR BETWEEN FS 640 AND FS 654.5 LHS, IAW WEST VIRGINIA AIR CENTER EO 601R-53-0 070. 2 L 7 2 4F RT A21EA 1999062500004 19990625 00004 EA 1999 6 25 COMA9960278 1 19990613 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 FS 718 AND STR 11 (RHS), DISCOVERED DURING 24 MONTH INSPECTION TO HAVE A CRACK IN THE RADIUS EXTENDING BETWEEN THE SECON D AND THIRD FASTENER HOLE ABOVE STR 11 IN THE FLANGE, A CRACK IN THE FLANGE EXTNEDING THROUGH THE FIRST FASTENER HOLE, A ND A CRACK IN THE DOUBLER ON THE AFT SIDE OF THE FRAME. FRAME FLANGE FS 718 REPAIRED IAW WVAC EO 601R-53-0067. DOUBLER ON AFT SIDE OF FRAME FS 718 REPAIRED IAW WVAC EO 601R-53-0069. 2 L 7 2 4F RT A21EA 1999062500005 19990625 00005 EA 1999 6 25 COMA9960279 1 19990613 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 FS 718 AND STR 11 (LHS) HAS A CRACK IN THE RADIUS EXTENDING BETWEEN THE FIRST AND SECOND FASTENER HOLE ABOVE STRINGER 11 IN THE FLANGE ATTACHING TO THE SKIN AND A CRACK IN THE DOUBLER ON THE AFT SIDE OF FRAME. FRAME FLANGE REPAIRED IAW WVA C EO 601R-53-0066. DOUBLER ON AFT SIDE OF FRAME REPAIRED IAW EO 601R-53-0068. 2 L 7 2 4F RT A21EA 1999062500006 19990625 00006 EA 1999 6 25 COMA9960280 1 19990612 A 5320 601R53611173 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 7169 FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. REPLACED LEFT HAND FLOOR SUPPORT ANGLE AT FS 6210 IN ACCORDANCE WITH CRJ REO 601R-53-61-117A. 2 L 7 2 4F RT A21EA 1999062500007 19990625 00007 EA 1999 6 25 COMA9960281 1 19990613 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PASSENGER DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 7169 PASSENGER DOOR SEAL STRIKER AT FS 310.349 DAMAGED. REPAIRED IN ACCORDANCE WITH CRJ REV 601R-52-11-008 ISSUE B REPAIR A. 2 L 7 2 4F RT A21EA 1999062500008 19990625 00008 EA 1999 6 25 COMA9960282 1 19990613 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PASSENGER DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 983CA 7169 PASSENGER DOOR SEAL STRIKER AT FS 310 DAMAGED. REPAIRED IN ACCORDANCE CRJ REO 601R-52-11-008 ISSUE B REPAIR A. 2 L 7 2 4F RT A21EA 1999062500009 19990625 00009 EA 1999 6 25 COMA9960283 1 19990614 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 991CA 7216 FLAPS FAILED DURING LANDING. REPLACED THE PDU. 2 L 7 2 4F RT A21EA 1999062500010 19990625 00010 1999 6 25 COMA9960284 4 19990616 A 3418 AOA HEAT CNDAIR CL600 CL6002B19 EA RIGHT INOPERATIVE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 914CA 7012 RIGHT HAND AOA HEAT CAUTION MESSAGE. RESET CIRCUIT BREAKER, SYSTEM OPERATION NORMAL. 2 L 7 2 4F RT A21EA 1999062500011 19990625 00011 EA 1999 6 25 COMA9960285 1 19990612 A 3230 CONTROL PANEL CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 917CA 7017 GEAR DISAGREE WARNING WHEN LANDING GEAR SELECTED DOWN NLG INDICATED UNSAFE. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LANDING GEAR CONTROL PANEL FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1999062500012 19990625 00012 EA 1999 6 25 COMA9960286 1 19990613 A 3010 32144424 VALVE CNDAIR CL600 CL6002B19 EA RT WING LEAKING A COMA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 01 987CA 7199 RIGHT HAND 14TH STAGE BLEED AIR DUCT LEAK WARNING. FOUND BLEED LEAK AT RIGHT HAND WING ANTI-ICE SHUTOFF VALVE. REMOVED , INSPECTED AND REINSTALLED VALVE, NO LEAKAGE NOTED. 2 L 7 2 4F RT A21EA 1999062500013 19990625 00013 NM 1999 6 25 UPS99229834 1 19990614 A 5320 651986219 CHORD BOEING 727 72725C 138400H NM BS 298 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON LT NOSE WHEEL WELL MID CHORD BS 298 LBL 15 WL 169. REMOVED CORROSION FROM CHORD PER SR M 51-10-6. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED MID CHORD PER SRM 51-30-2. INSTALLED NEW MID CHORD PER SRM 51-30-5 AND 51-30-6. 2 L 7 3 4F A3WE 1999062500014 19990625 00014 NM 1999 6 25 UPS99229835 1 19990614 A 5320 SHEAR WEB BOEING 727 72725C 138400H NM BS 1175 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION ON SHEAR WEB BS 1175 RBL 58 WL 208. MECHANICALLY REMOVED CORROSION FROM SHEAR WEB, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA ON SHEAR WEB PER SRM 51-30-2. PERFORMED WEB REPAIR PER SRM 5 1-40-2. 2 L 7 3 4F A3WE 1999062500015 19990625 00015 NM 1999 6 25 UPS99229836 1 19990526 A 5753 651920612 TRACK BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 3 FLAP TRACK AT REAR SPAR O/B MOUNT HOLE. REMOVED AND REPLACED F LAP TRACK IAW SRM 51-10-1, TO BE INSTALLED ON TC C57-581-04-3D. 2 L 7 3 4F A3WE 1999062500016 19990625 00016 NM 1999 6 25 UPS99229837 1 19990615 A 5230 65207292 STRAP BOEING 727 72725C 138400H NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C53-111-01-03) ON AFT CARGO DOOR BEAR STRAP STA 1110 BETWEEN STR 23R-24R FWD AND AFT OF FRAME. REPAIRED BEAR STRAP PER ER 99-5506, SRM 51-10-7, 51-30-2, SRM 53-10-2, SRM 51-30-5. 2 L 7 3 4F A3WE 1999062500017 19990625 00017 NM 1999 6 25 UPS99229838 1 19990615 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, PULLED FASTENERS BS 1166 STR 22 LT ON EXTERIOR SKIN CORROSION (C53-100-01.07-04). REMOVED AND REPAI RED DAMAGED AREA PER SRM 51-30-02, SRM 53-10-3 SRM 53-30-1, SRM 51-20-1, SRM 53-30-3, MM 51-20-21, SRM 51-30-5. 2 L 7 3 4F A3WE 1999062500018 19990625 00018 NM 1999 6 25 UPS99229839 1 19990615 A 5230 65207292 FRAME BOEING 727 72725C 138400H NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, WHILE WORKING FUSELAGE 117 CUSTOMER NR 943348 DISCOVERED AFT CARGO DOOR AFT FRAME TO BE CORRODED AND FRAME STRAP TO BE CRACKED AT FASTENER HOLE. REMOVED AND REPLACED FRAME PER ER 99-5506, SRM 51-30-2, SRM 51-10-2. 2 L 7 3 4F A3WE 1999062500019 19990625 00019 NM 1999 6 25 UPS99229841 1 19990612 A 5753 651920812 TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-03) ON NR 1 FLAP TRACK IN REAR SPAR MAIN BOLT HOLE. REMOVED NR 1 FLAP TRAC K, ROUTED TO CSD, RECEIVED NEW FLAP TRACK AND INSTALLED IAW 27-51-31. 2 L 7 3 4F A3WE 1999062500020 19990625 00020 NM 1999 6 25 UPS99229842 1 19990613 A 5753 651926920 TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 5 FLAP TRACK AT SPOILER BEAM PAD FWD ATTACH LUG AND INSIDE L/G BE AM ATTACH HOLES. REMOVED NR 5 FLAP TRACK PER MM 27-51-31. REMOVED ATTACH HARDWARE ON NR 5 FLAP TRACK PER SRM 51-30-2. RECEIVED REPLACEMENT FLAP TRACK, INSTALLED ON TC C57-581-04-4D. REINSTALLED ATTACHING HARDWARE ON NR 5 FLAP TRACK PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999062500021 19990625 00021 NM 1999 6 25 UPS99229843 1 19990611 A 5311 FRAME BOEING 727 727247 138408F NM BS 680 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, DENTED I/B FLANGE ON FRAME AT BS 680, LBL 34, STR 24 IN FWD CARGO BAY. THE DENT ON FRAME OUT OF LIM ITS PER SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS, ALODINED AND PRIMED THE REPAIR PARTS. INSTALLED REPAIR PARTS, ALL WORK ACCOMPLISHED PER SRM 51-40-3, 51-20-1 AND MM 51-20-21. 2 L 7 3 4F A3WE 1999062500022 19990625 00022 NM 1999 6 25 UPS99229844 1 19990611 A 5347 BAC1510190 SEAT TRACK BOEING 727 727247 138408F NM BS 1031 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, SEAT TRACK CORRODED AND DAMAGED TSS 1029 TO BS 1031 RBL 24 WL 208. AFTER REMOVAL OF CORROSION, FOUN D THE SEAT TRACK TO GO BEYOND ALLOWABLE LIMITS PER SRM 53-10-1. FABRICATED NEW SEAT TRACK, ALODINED, PRIMED AND PAINTED AND INSTALLED SEAT TRACK, ALL WORK ACCOMPLISHED IAW SRM 53-10-5, 51-30-2, MM 51-20-151. 2 L 7 3 4F A3WE 1999062500023 19990625 00023 NM 1999 6 25 UPS99229845 1 19990614 A 5313 STRINGER BOEING 727 727247 138408F NM BS 720 & 1270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSIN AND TOOLING DAMAGE ON STRINGER 7 LT BS 720B AND 1270+18. REMOVED CORROSION DAMAGE, FOUND T O BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED STRINGER REPAIR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999062500024 19990625 00024 NM 1999 6 25 UPS99229847 1 19990526 A 5400 S DUCT BOEING 727 72731C 1384011 NM BS 1243 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&AI, CRACK ON INTERNAL SKIN OF 'S' DUCT AT BS 1243 AT 9 O'CLOCK POSITION. REPAIR CARRIED OUT IAW SRM 5 4-10-03 FIG 201. 2 L 7 3 4F A3WE 1999062500025 19990625 00025 NM 1999 6 25 UPS99229848 1 19990610 A 5320 WEB BOEING 727 72731C 1384011 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, BS 870 BBL 15 LT SIDE AIR CONDITIONING DOOR SUPPORT WEB STRUCTURE ATTACHED TO LWR END OF BS 870 BL KHD FOUND CRACKED. WEB REPAIRED IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 1999062500026 19990625 00026 NM 1999 6 25 UPS99229849 1 19990605 A 5320 SPLICE BOEING 727 72731C 1384011 NM BS 580 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, DAMAGE TO SPLICE PLATE AT STA 580 BETWEEN STR 25R AND STR 26R. REPLACED IAW SRM 53-10-2 FIG 3. 2 L 7 3 4F A3WE 1999062500027 19990625 00027 NM 1999 6 25 UPS99229850 1 19990602 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 490 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, FWD CARGO BAY BS 490 CORROSION ON STRINGER 21R. REPLACED WITH NEW PIECE IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999062500028 19990625 00028 NM 1999 6 25 UPS99229851 1 19990602 A 5320 T-SECTION BOEING 727 72731C 1384011 NM BS 600 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, FWD CARGO BAY BS 600 CORROSION ON RT CEILING PANEL ATTACH T-SECTION AT VARIOUS ANCHOR NUTS POINTS. T-SECTION REPLACED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1999062500029 19990625 00029 NM 1999 6 25 UPS99229852 1 19990615 A 3510 MASK BOEING 727 72722C 138400F NM FLIGHT DECK LEAKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:N/A, DURING CREW PREFLIGHT-CAPTAINS O2 MASK FAILED NEGATIVE PRESSURE CHECK AND ALTERNATE PREFLIGHT CHECK . REMOVED AND REPLACED CAPTAINS O2 MASK. SYSTEM CHECKS GOOD, LEAK CHECKS GOOD, REGULATORS CHECK GOOD. 2 L 7 3 4F A3WE 1999062500030 19990625 00030 WP 1999 6 25 UPS99829853 1 19990616 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:N/A, DURING CREW PREFLIGHT EMERGENCY EXIT LIGHTS FAILED TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PAC K. LIGHTS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999062500031 19990625 00031 NE 1999 6 25 99UAL900286 2 19990519 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT BIRD STRIKE A UALA A UNSCHED LANDING C F.O.D. NR NOT REPORTED 1 WP 29 551UA 25399 726526 AIRCRAFT RETURNED TO FIELD DUE TO A LEFT ENGINE BIRD STRIKE. *S/D* BORESCOPED HPC 6TH, 11TH, 15TH AND 17TH STAGE, FOUN D NO LIMITING DISTRESS. REPLACED FOUR DAMAGED FAN BLADES AND THEIR PAIRS. ENGINE RUN VIBRATION CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500032 19990625 00032 NM 1999 6 25 99UAL900306 1 19990604 A 2150 CONTROLLER ALLIED SIGNA 6075182 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT PACK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 302UA 97L231 23643 THE RIGHT PRESSURIZATION PACK CIRCUIT BREAKER TRIPPED. *S/D* FAILURE OF THE RIGHT PACK RAM AIR CONTROLLER AND SENSOR. REPLACED BOTH THE RAM AIR TEMPERATURE SENSOR AND RAM AIR CONTROLLER. 2 L 7 2 4F 4 F RT A16WE E2GL 1999062500033 19990625 00033 NM 1999 6 25 99UAL900307 1 19990603 A 2720 PCU PARKER HANNI 65C370539 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 343UA 2293ABC 24247 RUDDER CONTROL BECAME ERRATIC. *S/D* REPLACED THE RUDDER POWER CONTROL UNIT (PCU). ALSO, ACCOMPLISHED A CHECK OF THE FORCES REQUIRED TO MOVE THE STANDBY RUDDER ACTUATOR INPUT FORCES PER MM 27-21-00-101. INPUT FORCES WERE WITHIN LIMITS A ND NO FAULTS WERE FOUND WITH THE PCU WHEN IT WAS TESTED IN THE COMPONENT REPAIR SHOP. 2 L 7 2 4F 4 F RT A16WE E2GL 1999062500034 19990625 00034 NM 1999 6 25 99UAL900308 1 19990605 A 4970 SWITCH SUNDSTRAND 4950488 AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE APU OIL SYS FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 810UA 843 1413 CREW REPORTS SMOKE IN THE CABIN. EXTERNALLY LEAKING LOW OIL PRESSURE (LOP) SWITCH CAUSED OIL TO FLOW OVER LOAD COMPRESS OR CASE WHICH WAS REINJESTED INTO THE APU AND CAUSED ODOR OR SMOKE. THE APU (APS3200 SERIAL NUMBER 1413) WAS REMOVED AN D ROUTED THROUGH SUNDSTRAND WHO CHANGED THE LOP SWITCH AND RETURNED THE UNIT TO SERVICE (CURRENTLY INSTALLED IN AIRCRAFT 4217). 2 L 7 2 4F 4 F RT A28NM E40NE 1999062500035 19990625 00035 EU 1999 6 25 99UAL900309 1 19990607 A 5610 NP1653116 WINDSHIELD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 432UA 587 CREW REPORTS, F/O WINDSHIELD CRACKED. *S/D* CRACK WAS DUE TO BUSBAR ACRHING FROM MOISTURE INGRESS AND CONTACT WITH THE WINDOW HEAT ELEMENT. F/O WINDSHIELD WAS REPLACED PER AMM 56-11-11 ON 6-7-99. 2 L 7 2 4F 4 F RT A28NM E40NE 1999062500036 19990625 00036 NM 1999 6 25 99UAL900310 1 19990604 A 2120 AIR DIST BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 192UA 26881 INBOUND CREW REPORTED BAD SMELL THROUGH THE WHOLE AIRPLANE. 2 L 7 4 4F 4 F RT A20WE E24NE 1999062500037 19990625 00037 1999 6 25 99UAL900311 4 19990607 A 2565 D30660116 SLIDE AIR CRUISERS D30654122 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 0599 25323 SLIDE/RAFT FAILED AIR RETENTION CHECK DURING OVERHAUL BY VENDOR. *S/D* POROSITY, DUE TO EXCESS MOISTURE, WAS THE CAUSE OF THE FAILED SLIDE/RAFT. VENDOR REPLACED THE INFLATABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500038 19990625 00038 NE 1999 6 25 99UAL900312 2 19990606 A 7320 SPEED CARD 285N0200204 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 559UA 123 26657 FLIGHT RETURNED TO ORD DUE TO THE LOSS OF THE NR 2 ENGINE SPEED CARD. REPLACED THE N-2 SPEED CARD AND ENGINE CHECKED OK ON THE CONTINUING FLIGHTS. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500039 19990625 00039 NM 1999 6 25 99UAL900313 1 19990608 A 2613 S555735614255 OVERHEAT LOOP BOEING 655387420 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING/BODY MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 394UA 24669 LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED. *S/D* A/C DESCENDED TO FL240, AND OVERHEAT LIGHT EXTINGUISHED AFTER APPR OX 9 MIN. A/C LANDED WITHOUT INCIDENT. TROUBLESHOOTING WITH M237 COMPARTMENT OVERHEAT MODULE ISOLATED KEEL BEAM OVERHE AT LOOPS M272 AND M273 AS PRIMARY CAUSE. OVERHEAT LOOPS M272 AND M273 WERE REPLACED, AND LOOPS M274 AND M355 WERE REPLA CED AS PRECAUTIONARY. ALSO, REPAIRED PNEUMATIC DUCT CLAMP BROKEN IN KEEL BEAM AREA. AIRCRAFT OVERHEAT SYSTEM AND LEAK CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999062500040 19990625 00040 1999 6 25 99UAL900314 4 19990608 A 3425 4630018130 INS BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE LT COCKPIT MALFUNCTIONED A UALA C E ABORTED TAKEOFF ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 WP 29 161UA 21352 ABORTED TAKEOFF AT 90 KNOTS, ON ACCOUNT OF CAPTAIN'S ATTITUDE FLAG IN VIEW. AFTER REVERSE, NR 4 GREEN LIGHT ON, SHUT EN GINE DOWN. REALIGNED INS AND FLAG WENT AWAY. STARTED NR 4 ENGINE AND GREEN LIGHT WENT OUT. THEN MADE NORMAL TAKEOFF. *S/D* INS OUT OF ALIGNMENT. NO MALFUNCTION OR ACTION CODES NOTED. REALIGNED INS, FLAG WENT AWAY. INS NR 1 SWAPPED W ITH NR 3 AS A PRECAUTIONARY MEASURE. ALL INS SYSTEMS PASSED OPERATIONAL CHECK. 2 L 7 4 4F 4 F A20WE E20EA 1999062500041 19990625 00041 1999 6 25 99UAL900315 4 19990609 A 3444 9650876001B05B04 GPWS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E & E COMPT TRIPPED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7265U 21412 DURING TAKEOFF ROLL, WINDSHEAR INOPERATIVE LIGHT ILLUMINATED AT 120 KNOTS. TAKEOFF WAS ABORTED. *S/D* RESET GPWS, TES T NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999062500042 19990625 00042 NM 1999 6 25 99UAL900316 1 19990609 A 2830 M259881150 PACKING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT JET PUMP LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 660UA 27115 INTENSE FUEL SMELL IN COCKPIT AND CABIN JUST AFTER LIFTOFF. SMELL DISSIPATED IN FIVE MINUTES. *S/D* FUEL SMELL DUE TO LEAK AT LEFT JETTISON PUMP CAUSED BY DAMAGED PACKINGS ON LEFT JETTISON PUMP SHUTOFF SLEEVE. THE TWO M25988-1-150, AND ONE M25988-1-154 PACKINGS WERE REPLACED AND A LEAK CHECK PERFORMED. NO FURTHER LEAKAGE PRESENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999062500043 19990625 00043 NM 1999 6 25 99UAL900317 1 19990610 A 2810 FUEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 PYLON LEAKING A UALA O OTHER K FLUID LOSS LD LANDING 1 WP 29 367UA 24536 FLUID LEAKING FROM NUMBER 2 PYLON AREA, OVER THE LEADING EDGE OF THE WING. FUEL AND HYDRAULIC QUANTITY NORMAL. UPON AR RIVAL, FOUND NO APPARENT FLUID LEAKS. REMOVED PANEL, FOUND NO LEAKS IN PYLON. RAN FLAPS AND ENGINE, NO LEAKS WERE DETE CTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999062500044 19990625 00044 NM 1999 6 25 99UAL900318 1 19990611 A 5400 RIB BOEING 747 747222B 1384904 NM NR 4 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 152UA 23737 DURING ROUTINE MAINTENANCE IN PYLON NR 4 A RIB WAS FOUND WITH A 6 INCH CRACK ON IT'S WEB. THE CRACK IS AT NAC STA 236.5 AND WL 148 ON THE LEFT SIDE OF THE PYLON ADJACENT TO THE PNEUMATIC DUCT FITTING. 2 L 7 4 4F RT A20WE 1999062500045 19990625 00045 WP 1999 6 25 ABXA9900472 1 19990617 A 5313 59114277 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND LONGERON 16 RIGHT CRACKED AT AFT SIDE OF RIGHT FORWARD PYLON BULKHEAD, STATION 1041. REPAIRED LON GERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999062500046 19990625 00046 WP 1999 6 25 ABXA9900473 1 19990617 A 5753 4916865503 BRACKET DOUG DOUG DC9 DC941 302207N WP LT FLAP BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND THE LEFT FLAP MOVABLE VANE SPRING MOUNT BRACKET LUG BROKE OFF. REPLACED BRACKET IAW DC9 MM 27-50- 1. 2 L 7 2 4F A6WE 1999062500047 19990625 00047 WP 1999 6 25 ABXA9900474 1 19990614 A 5280 591078310 PAN DOUG DOUG DC9 DC941 302207N WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND THE LEFT MAIN LANDING GEAR INBOARD DOOR FORWARD DOOR PAN CRACKED. REPLACED DOOR PAN IAW DC9 SRM 5 1-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999062500048 19990625 00048 WP 1999 6 25 ABXA9900475 1 19990615 A 5755 5910055516 PANEL DOUG DOUG DC9 DC941 302207N WP RT SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 DURING C-CHECK, FOUND RIGHT INBOARD SPOILER PANEL LOWER OUTBOARD SURFACE DELAMINATION. REPLACED SPOILER PANEL IAW DC9 M M 27-61-1. 2 L 7 2 4F A6WE 1999062500049 19990625 00049 WP 1999 6 25 ABXA9900476 1 19990421 A 5730 5769589 SKIN DOUG DOUG DC8 DC863 302198A WP WS 391.5-416.5 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT CENTER LEADING EDGE HAS HEAVY CORROSION UNDER SKIN, UPPER AFT END FROM STATION XFS 391.5 TO 416.5. REPAIRED IAW DC 8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999062500050 19990625 00050 WP 1999 6 25 ABXA9900477 1 19990420 A 5320 5615535 FITTING DOUG DOUG DC8 DC863 302198A WP BS 660 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FITTING CRACKED AT STATION 660 ABOVE FRAME AT LONGERON 36. REPAIRED IAW DC9 SRM 51-3-0 AND ABX REA D853-27291. 2 L 7 4 4F 4A25 1999062500051 19990625 00051 WP 1999 6 25 ABXA9900478 1 19990501 A 5313 561537431 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1600 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 36 STATION 1600 CORRODED. REPAIRED IAW DC8 SRM 53-4-1 AND DWG 5615374. 2 L 7 4 4F 4A25 1999062500052 19990625 00052 WP 1999 6 25 ABXA9900479 1 19990515 A 5313 5615374 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1500-1620 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 34 LEFT, STATION 1500-1620 CORRODED. REPAIRED IAW DC8 DWG 5615374. 2 L 7 4 4F 4A25 1999062500053 19990625 00053 WP 1999 6 25 ABXA9900480 1 19990424 A 5320 5894282 FITTING DOUG DOUG DC8 DC863 302198A WP CARGO DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 NR 1 CARGO COMPARTMENT DOOR FRAME NR 6, LOWER LATCH SUPPORT FITTING CRACKED INSIDE TORQUE BOX. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500054 19990625 00054 WP 1999 6 25 ABXA9900481 1 19990501 A 5313 561537429 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1580-1620 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 35 LEFT STATION 1580-1620 CORRODED. REPAIRED IAW DC8 SRM 53-4-1 AND DWG 5615374. 2 L 7 4 4F 4A25 1999062500055 19990625 00055 NM 1999 6 25 DL72S991274 1 19990607 A 3350 0201991007 LIGHT BOEING 727 727232 1384082 NM ROW 20D MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 404DA 21148 ON L/O, FOUND SEAT 20D EMERGENCY LIGHT MISSING. REPLACED LIGHT ASSY, OPS CKS GOOD. 2 L 7 3 4F A3WE 1999062500056 19990625 00056 NM 1999 6 25 DL757991276 1 19990604 A 5754 114N4003153 SKIN BOEING 757 757232 1384965 NM NR 2 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 DURING REPLACEMENT OF THE TE WEDGE PER E.O. 6-71653-3AD, SEVERAL WEDGE-TO-UPPER SKIN ATTACH FASTENERS WERE INSTALLED WIT H TENSION HEAD FLUSH FASTENERS, RESULTING IN OVERSIZED COUNTERSINKS. AUTHORIZED INSTALLATION OF TENSION HEAD HI-LOKS IN DISCREPANT LOCATIONS. 2 L 7 2 4F RT A2NM 1999062500057 19990625 00057 NM 1999 6 25 DLM88991277 1 19990606 A 2421 GENERATOR 947F9453 DOUG MD88 MD88 3023688 NM LEFT FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 986DL RI11522B 53313 APPROX 4 MIN AFTER T/O, CAPT PFD AND ND BEGAN TO FAIL AND BLANK. ABOUT 2 MIN LATER LT GEN FAILED, RT GEN DID NOT PICK U P LOAD. PWR WOULD SHIFT BETWEEN FAILING AND X-TIE. STARTED APU AS BACKUP AND LT GEN WAS OK FOR REMAINDER OF FLT. 2 L 7 2 4F RT A6WE 1999062500058 19990625 00058 NM 1999 6 25 DLM88991279 1 19990607 A 2910 LINE DOUG MD88 MD88 3023688 NM RT MLG WW LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 998DL 53370 AT TOP OF CLIMB FL350, NOTICED RIGHT HYD RESV LOW QTY LIGHT WITH RT HYD QTY AT 4 THEN 3. ACCOMPLISHED HYD QTY LOW CK L IST. WHEN RT HYD PUMP TURNED OFF QTY INCREASED TO 19 AND STEADY. FOUND HYD LINE IN RT W/W ABOVE A/C HYD PUMP CHAFED AN D LEAKING. REPAIRED, LEAK CKS OK. OPERATED FLT CONTROL WITH RT ENG RUNNING, ALL CKS GOOD. 2 L 7 2 4F RT A6WE 1999062500059 19990625 00059 NM 1999 6 25 DL72S991280 1 19990607 A 3350 LIGHT 900542 BOEING 727 727232 1384082 NM EMER EXIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 404DA 10615 21148 LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 3 4F A3WE 1999062500060 19990625 00060 NM 1999 6 25 DL76L991281 1 19990607 A 2530 OVEN BOEING 767 767332 1382001 NM GALLEY DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 191DN 28448 FLIGHT ATTENDANTS REPORTED SMOKE SMELL IN MID GALLEY AFTER ARRIVAL AT GATE. EXAMINED THE OVENS IN MID GALLEY AND CLEANE D ACCORDINGLY. ALSO, CHECKED CEILING PANELS AROUND GALLEY, NO EVIDENCE OF BURNING OR SMOKE SMELL OBSERVED. 2 L 7 2 4F RT A1NM 1999062500061 19990625 00061 NM 1999 6 25 DL76G991282 1 19990607 A 3230 RETRACT MECH BOEING 767 7673P6 1385105 NM LANDING GEAR MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 155DL 25269 ON ATTEMPTED GEAR RETRACTION GEAR HANDLE STUCK AT OFF POSITION,10-15 SEC LATER HEARD A RELAY CLICK AND THEN HANDLE WAS A BLE TO BE MOVED TO THE UP POSITION. GEAR THEN RETRACTED NORMALLY. WHEN GEAR HANDLE LOWERED TO DOWN POSITION, AT 200 KT S, NOSE AND RT EXTENDED NORMALLY. NO LEFT MAIN GREEN DOWN AND GEAR DISAGREE EICAS, 40-50 SEC LATER LEFT MAIN INDICATED DOWN AND GEAR DISAGREE EXTINGUISHED. NORMAL LANDING AT JFK. 2 L 7 2 4F RT A1NM 1999062500062 19990625 00062 NM 1999 6 25 DL72E991283 1 19990607 A 2782 RIB BOEING 727 727247 138408F NM NR 5 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 A-1 LTR CHK, NR 5 SLAT ACT NOSE RIB CRACKED O/B SIDE AT FWD RADIUS. 2 L 7 3 4F A3WE 1999062500063 19990625 00063 NM 1999 6 25 DLM11991285 1 19990607 A 2910 CONTROL 4059021901 DOUG MD11 MD11 3023602 NM NR 3 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 812DE 92060327 48601 OVERHEAD C/B A-3 RT HYD CONTROL C/B POPPED CANNOT CONTROL ALL RIGHT EDP. REPLACED ENG HYD PUMP CONTROL RT CB AND REL AYS. NR 3 DEPRESS SOLENOID NEEDS CANNON PLUG. 2 L 7 3 4F RT A22WE 1999062500064 19990625 00064 NM 1999 6 25 DL72S991287 1 19990608 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 14 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP FOR THE PANEL WAS CUTOUT AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLE R PER ER/A 367553-14AD. 2 L 7 3 4F A3WE 1999062500065 19990625 00065 NM 1999 6 25 DL72S991288 1 19990603 A 5512 SKIN BOEING 727 727232 1384082 NM LT HORIZ STAB DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 BULGE AT LT HORIZONTAL STABILIZER UPPER SKIN 6 IN FWD OF ELEVATOR 2ND FROM O/B HINGE(MARKED). INSTALLED DOUBLER PER SRM 55-20-3. 2 L 7 3 4F A3WE 1999062500066 19990625 00066 NM 1999 6 25 DL72S991289 1 19990602 A 5754 DOUBLER BOEING 727 727232 1384082 NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 A 1 INCH CRACK IN DOUBLER NR 3 SLAT RIB O/B OF ACT. REPLACED DOUBLER PER MM 57-54-0 FIG 804. 2 L 7 3 4F A3WE 1999062500067 19990625 00067 NM 1999 6 25 DL76L991290 1 19990608 A 5330 143T35612 SKIN BOEING 767 767332 1382001 NM BS 654 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 189DN 25990 THE FUSELAGE SKIN, UNDERLYING STRINGER AND UNDERLYING FRAME CHORD WERE PUNCTURED AND DAMAGED BY GROUND SUPPORT EQUI PMENT. A NEW SECTION OF STRINGER WAS SPLICED, THE FRAME CHORD REPAIRED, AND A SKIN DOUBLER INSTALLED PER THE B767 SRM A ND DOCUMENTED PER ER/A 367542-14. 2 L 7 2 4F RT A1NM 1999062500068 19990625 00068 NM 1999 6 25 DL72S991291 1 19990605 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 AN I/B FLAP TRACK WAS FOUND WITH CORROSION IN TWO BOLT HOLES WHICH ARE THE SUBJECT OF AD 90-07-05. THE CORROSION WAS CL EANED UP BY OVERSIZING THE HOLES WITHIN THE LIMITS OF B727, S/B 57-0178, REV 5 AND DOCUMENTED PER ER/A 367543-14AD. 2 L 7 3 4F A3WE 1999062500069 19990625 00069 NM 1999 6 25 DL72E991292 1 19990606 A 5330 65545703 SKIN BOEING 727 727247 138408F NM BS 420-440 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 420 AND 440. THE CRACK WAS ROUTED OUT AND AN EXTERNAL REPAIR DOUBLER INSTALLED PER B727 SRM 53-30-3, FIG 5 AND ER/A 367547-14AD. 2 L 7 3 4F A3WE 1999062500070 19990625 00070 NM 1999 6 25 DL72W991293 1 19990608 A 5320 FRAME BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND AT F-1 LETTER CHECK, AFT ENTRY DOOR CUTOUT RT FRAME HAS .5 INCH VISIBLE CRACK 6 INCHES BELOW UPPER STOP CASTING. R EPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999062500071 19990625 00071 NM 1999 6 25 DL72W991295 1 19990608 A 5522 SKIN BOEING 727 727247 138408F NM LT ELEV CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON F1 LETTER CK, .375 INCH CRACK ON LT ELEVATOR LOWER SKIN. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1999062500072 19990625 00072 NM 1999 6 25 DL72W991296 1 19990608 A 5755 659892432 ANGLE BOEING 727 727247 138408F NM NR 13 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 NR 13 SPOILER ACTUATOR SUPPORT FITTING O/B ATTACH ANGLE CRACKED. REPLACED ANGLE PER M/M 57-42-0 PG 802. 2 L 7 3 4F A3WE 1999062500073 19990625 00073 NM 1999 6 25 DL767991297 1 19990608 A 3230 17014110CR0720S HOSE BOEING 767 767232 1385132 NM RT MLG FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 113DA 22225 RIGHT MAIN GEAR TRUCK TILT HYD HOSE BURST. A/C DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND HYDRAULIC HOSE TO TRUCK TILT ACTUATOR BURST. REPLACED HOSE. SERVICED SYSTEM, LEAK CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999062500074 19990625 00074 NM 1999 6 25 DLM88991298 1 19990609 A 5510 HINGE DOUG MD88 MD88 3023688 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DL 49541 DURING INSPECTION OF THE VERTICAL TO HORIZONTAL STAB HINGE PLATES (REF ERA 373241-14AD) CORROSION WAS FOUND ON THE FACES AND WITHIN THE BORES OF THE HINGE PLATES. DAMAGE WAS WITHIN SRM ALLOWABLE LIMITS. BORE CLEAN UP EXCEEDED SRM ALLOWABL E LIMITS BY 0.003. REWORKED PER ERA 333220-14AD. 2 L 7 2 4F RT A6WE 1999062500075 19990625 00075 NM 1999 6 25 DLM88991299 1 19990609 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM BS 240 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DE 49967 DENT FOUND IN FUSELAGE SKIN AT APPROX FS 240 BETWEEN L18L AND L20L. DAMAGE CUTOUT IS APPROX 20 BY 13. REPAIRED PER ERA 333205-14, REV A. 2 L 7 2 4F RT A6WE 1999062500076 19990625 00076 NM 1999 6 25 DL76L991300 1 19990609 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 199DN 28456 DURING ETOPS TRIP CHECK, BOTH OVERWING SQUIBS FAILED TO TEST. REPLACED BOTH OVERWING ESCAPE SLIDE BATTERY PACK. PERFOR MED GOOD TEST OF SQUIBS. 2 L 7 2 4F RT A1NM 1999062500077 19990625 00077 NM 1999 6 25 DL72S991301 1 19990609 A 5754 RIB BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 A 1 INCH CRACK IN L/E OF NOSE RIB NR 8 SLAT I/B SIDE OF O/B TRACK. REPAIRED PER M/M 57-54-0 PG 813. 2 L 7 3 4F A3WE 1999062500078 19990625 00078 NM 1999 6 25 DL73E991304 1 19990610 A 2421 GENERATOR 948F4583 BOEING 737 737247 138448D NM NR 2 FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 374DL 23521 NR 2 GEN FAILED. SWAPPED GCU WITH APU AND PUT APU GEN ON MCO. MADE SECOND ATTEMPT TO T/O NR 1 GEN FAILED. 2 L 7 2 4F A16WE 1999062500079 19990625 00079 NM 1999 6 25 DLM11991305 1 19990610 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM BS 1862-2047 TAIL STRIKE A DALA K NONE O OTHER LD LANDING 1 SO 27 813DE 48600 UPON LANDING IN CAMBRIDGE, ENGLAND THE AC EXPERIENCED A TAIL STRIKE. DAMAGE EXTENDS FROM FS 1865 TO FS 2039 AND IS BETW EEN APPROX L49R AND JUST O/B OF L50L. BESIDES THE FUSELAGE SKIN ASSEMBLY DAMAGES, THE AFT PRESSURE BLKHD WAS DAMAGED. R EPAIRED PER ERA 367462-14. 2 L 7 3 4F RT A22WE 1999062500080 19990625 00080 WP 1999 6 25 DLL10991306 1 19990610 A 5312 1505220 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP BS 1363 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 DURING HFEC INSPECTION OF FS 1363 BLKHD LT WEB, ONE CRACK WAS FOUND AT LBL 42 AND WL 140. REPAIRED PER ERA 367563-14AD. 2 L 7 3 4F A23WE 1999062500081 19990625 00081 NM 1999 6 25 DL72S991307 1 19990610 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360-480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING LFEC INSPECTION PER SI 4-74176-12AD, NUMEROUS CRACK INDICATIONS WERE FOUND IN THE VARIOUS FRAME BAYS EXTENDING FR OM BS 360-480 ALONG S4R. THERE WAS A PREVIOUS REPAIR PER ERA 332834-14AD, REV B WHICH WILL BE REMOVED AND INCORPORATED INTO THIS REPAIR. REPAIRED PER ERA 367552-14AD, REV A. 2 L 7 3 4F A3WE 1999062500082 19990625 00082 NM 1999 6 25 DL757991308 1 19990610 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM BS 620 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 668DN 25141 WHILE ACCOMPLISHING PERM REPAIR PER ORIGINAL ISSUE OF ERA 362260-14, ADDITION DAMAGE (TOOLING DAMAGE) WAS FOUND, NECESSI TATING A LARGER SKIN CUTOUT. REPAIRED PER ERA 362260-14, REV B. 2 L 7 2 4F RT A2NM 1999062500083 19990625 00083 NM 1999 6 25 DL72W991309 1 19990610 A 5320 6518414 WEB BOEING 727 727247 138408F NM BS 290 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A CRACK BETWEEN BS 294 AND 286 AT APPROX WL 170. REPAIRED PER ERA 367566-14. 2 L 7 3 4F A3WE 1999062500084 19990625 00084 NM 1999 6 25 DLM88991310 1 19990610 A 2170 COALESCER V1211 DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 973DL 53241 REPORT OF SMOKE IN AFT CABIN BY FLIGHT ATTENDANT SHORTLY AFTER FLIGHT CREW ADJUSTED RT PACK TEMPERTURE CONTROL. REPLACE D COALESER BAGS. 2 L 7 2 4F RT A6WE 1999062500085 19990625 00085 NM 1999 6 25 DL72K991311 1 19990610 A 3350 95246508 RELAY BOEING 727 727232 1384082 NM COCKPIT OVERHEATED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 417DA 21259 JUST PRIOR TO PUSHBACK DETECTED SLIGHT ODOR AFTER ENGINE START. CYCLED PACKS AND GASPER FAN ODOR GOT PROGRESSIVELY WORSE, SEEMED CONFINED TO THE COCKPIT. ISOLATED SMELL TO COCKPIT CEILING. FOUND EMERGENCY EXIT SIGN RELAY BAD. REPLA CED SAME, NO OTHER FAULTS FOUND. EMERGENCY EXIT SIGNS CHECK NORMAL. 2 L 7 3 4F A3WE 1999062500086 19990625 00086 NM 1999 6 25 DL76L991312 1 19990610 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM ROW 1-5 INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 186DN 27962 EMERGENCY LIGHTS ROWS 1-5 LT AND RT SIDE INOP. REPLACED POWER SUPPLY, ALL CK NORM. 2 L 7 2 4F RT A1NM 1999062500087 19990625 00087 NM 1999 6 25 DL72S991313 1 19990610 A 5320 WEB BOEING 727 727225A 1384077 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FOUND ON A-2 LETTER CK, .5 INCH CRACK AT LT TORQUE BOX VERTICAL WEB AT THE UPPER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0. 2 L 7 3 4F RT A3WE 1999062500088 19990625 00088 NM 1999 6 25 DL72S991314 1 19990610 A 5320 WEB BOEING 727 727225A 1384077 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FOUND ON A2 LETTER CK. .25 INCH CRACK AT RT TORQUE BOX VERT WEB LOWER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0 . 2 L 7 3 4F RT A3WE 1999062500089 19990625 00089 NM 1999 6 25 DL73E991315 1 19990610 A 2424 948F4583 GCU BOEING 737 737247 138448D NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 374DL 23521 709151 NR 2 GENERATOR TRIPPED OFF LINE AT 1500 FT AND WOULD NOT RESET. 2 L 7 2 4F 4 F A16WE E2EA 1999062500090 19990625 00090 NM 1999 6 25 DL72S991316 1 19990610 A 5320 FRAME BOEING 727 727225A 1384077 NM CARGO DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 LTR CHECK A2, 1 INCH CRACK AT C-2 DOOR CUTOUT FWD FRAME WEB AT LOWER END. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1999062500091 19990625 00091 NM 1999 6 25 DL72S991317 1 19990610 A 5320 ANGLE BOEING 727 727225A 1384077 NM BS 913 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 MLG W/W STA 913 ANGLE CRACKED AT UPPER RADIUS BLOCK ABOVE UPLOCK. REPAIRED PER DAL M/M 53-11-0 PGS 834-837 AND ERA 36 7582-14 ALLOWING USE OF DAL M/M REPAIR ON EX - EAL AIRCRAFT. 2 L 7 3 4F RT A3WE 1999062500092 19990625 00092 NM 1999 6 25 DLM11991318 1 19990610 A 3260 SENSOR DOUG MD11 MD11 3023602 NM LT MLG IND DIRTY A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 801DE 48472 ON APPROACH BELOW 10,000 FT, LEFT LANDING GEAR LIGHT FLASHED RED WITH THE GEAR HANDLE UP. GEAR INDICATIONS NORMAL WITH GEAR HANDLE DOWN. PERFORMED BITE ON PSEU, NO FAULTS NOTED. CHECKED SENSOR AND CLEANED SAME. 2 L 7 3 4F RT A22WE 1999062500093 19990625 00093 NM 1999 6 25 DL76L991319 1 19990611 A 2520 CONTROL BOX PS45222200 BOEING 767 767332 1382001 NM ROW 10 FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 1201P 159682A 28458 SMOKE REPORTED AT THE FLOOR LEVEL SEAT 10. ELECTRICAL ODOR DETECTED IN FLIGHT BY COCKPIT CREW. C/B'S PULLED AT GALLEY NUMBER 2. HEAT NOTED AT FLOOR LEVEL FRONT OF ROW 10. SUSPECT PASSENGER SEATING/CONVENIENCE ITEMS PROBLEM. REPLACED S EAT POWER CONTROL BOX. ALSO, AVU REPLACED BY ROCKWELL COLLINS AFTER PERFORMING CONFIDENCE CHECK. 2 L 7 2 4F RT A1NM 1999062500094 19990625 00094 NM 1999 6 25 DL73E991320 1 19990611 A 2751 INDICATOR 2061141 BOEING 737 737247 138448D NM TE FLAPS INOPERATIVE A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 374DL 1168 23521 DURING APPROCH WHEN THE FLAPS WERE SELECTED FROM 1 DEG TO 5 DEG THE FLAP INDICATION NEEDLES SPILT AND THE FLAPS STOPPED AT 1 DEG. POM PROCEDURES WERE ACCOMPLISHED AND LANDING WAS UNEVENFUL. REPLACED FLAP INDICATOR, RAN FLAPS AND CHECKS OK . 2 L 7 2 4F A16WE 1999062500095 19990625 00095 NM 1999 6 25 DL76S991321 1 19990611 A 5315 143T51062 FLOORBEAM BOEING 767 767332 1382001 NM BS 500 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 136DL 23146 DAMAGE FROM CONTACT WITH A CARGO CONTAINER WAS FOUND ON THE BS 500 FLOORBEAM BETWEEN RBL AND LBL 11. THE DAMAGE NECESSI ATED REMOVAL THE FLOORBEAM SECTION BETWEEN R/LBL 11. REPAIRED PER ERA 333197-14, REV A. 2 L 7 2 4F RT A1NM 1999062500096 19990625 00096 NM 1999 6 25 DL73E991322 1 19990611 A 5240 SKIN BOEING 737 7372S3 NM BS 320 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 DURING THE INSP OF THE R1 DOOR UPPER CORNERS SEVERAL CRACKS WERE FOUND IN THE SKIN ASSY AND BEARSTRAP. REPAIRED PER ERA 367544-14, REV A. 2 L 7 2 4F RT A16WE 1999062500097 19990625 00097 NM 1999 6 25 DL72S991323 1 19990611 A 5311 655613141 FRAME BOEING 727 727232 1384082 NM BS 1090 SEVERED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 C3 DOOR FWD FRAME AT BS 1090 WAS FOUND SEVERED ABOVE S27R. A PARTIAL FRAME REPLACEMENT WAS MADE. NO SKIN CRACKING REPO RTED. REPAIRED PER ERA 367579-14AD. 2 L 7 3 4F A3WE 1999062500098 19990625 00098 WP 1999 6 25 DLL10991324 1 19990611 A 5312 1505220235 BULKHEAD CAP LKHEED 1011 10113851 5265010 WP BS 1363 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 FS 1363 BLKHD CAP WAS FOUND CRACKED IN THE TYPICAL MANNER. REPAIRED PER ERA 367570-14AD. 2 L 7 3 4F A23WE 1999062500099 19990625 00099 NM 1999 6 25 DL757991325 1 19990611 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM BS 1700 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 668DN 25141 TWO DENTS WERE FOUND AT BS 1690 AND BS 1710, EACH BELOW S18L. REPAIRED PER ERA 367505-14. 2 L 7 2 4F RT A2NM 1999062500100 19990625 00100 NM 1999 6 25 DL76L991326 1 19990612 A 3350 BPS73 BATTERY CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 174DN 24802 LEFT AFT EMERGENCY EXIT LIGHT AND AISLE LIGHTS FORWARD AND AFT OF EXIT LIGHT NOT WORKING DURING OPERATIONAL CHECK OF EM ERGENCY EXIT LIGHTS. REPLACED BATTERY CHARGER, SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999062500101 19990625 00101 NM 1999 6 25 DLM11991327 1 19990612 A 5240 CIRCUIT BREAKER DOUG MD11 MD11 3023602 NM 2R DOOR TRIPPED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 812DE 48601 FOUND C/B FOR 2R DOOR ELECTRIC MOTOR POPPED, WOULD NOT RESET. FWD TO MCO AND PLACARD. 2 L 7 3 4F RT A22WE 1999062500102 19990625 00102 NM 1999 6 25 DL76L991328 1 19990611 A 2710 AILERON CONTROLS BOEING 767 767332 1382001 NM RT MLG WW FOD A DALA D RETURN TO BLOCK F C FLT CONT AFFECTED F.O.D. TX TAXI/GRND HDL 1 SO 27 180DN 25985 ON TAXI OUT DURING FLT CONTROL CK, COULD NOT GET FULL LEFT AILERON CONTROL WHEEL TRAVEL AND THE EICAS DISPLAY INDICATION WOULD NOT MOVE FULL SCALE. RETURNED TO GATE. PERFORMED BITE OF STCMS, CHECKED OK AND NO FAULT FOUND. DURING T/S FOUN D A SMALL ROCK PEBBLE JAMMED IN RT WING AILERON CABLE QUADRANT JUST O/B OF RT LCCA LOCATED RT WHEEL WELL. REMOVED PEBBL E, INSPECTED QUADRANT AND CABLE FOUND OK. AILERONS NOW OPS CKS NORMAL. 2 L 7 2 4F RT A1NM 1999062500103 19990625 00103 WP 1999 6 25 DLL10991329 1 19990612 A 2424 GCU 51511003 LKHEED 1011 10113851 5265010 WP NR 2 FAILED A DALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 27 733DS 952C 193C1224 FLIGHT STATION BUS FAILURE NR 2 ON TAKEOFF. NR 2 BUS TIE BREAKER TRIP OPEN AND NR 2 BREAKER FAILED, OPEN NR 2 FIELD REM AINED CLOSED. REPLACED NR 2 GCU, RAN ENGS AND ALL GEN SYS OPS NORMAL. 2 L 7 3 4F A23WE 1999062500104 19990625 00104 NM 1999 6 25 DL73K991330 1 19990612 A 3244 323001095 TIRE BOEING 737 737232 1384475 NM RT NLG TIRE FAILED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 329DL 23101 EXPERIENCE NOSE WHEEL TIRE FAILURE AT ROTATION. CONTINUED TAKEOFF. INSPECTED AIRCRAFT AND FOUND RT NOSE TIRE TREAD CAP MISSING. REPLACED LEFT AND RIGHT NOSE WHEEL ASSYS PER MM. PERFORMED OVERWEIGHT LANDING INSP. NO DAMAGE TO FUSELAGE A ND WINGS. ENGINE INLETS, CK OK. 2 L 7 2 4F RT A16WE 1999062500105 19990625 00105 NM 1999 6 25 DLM88991331 1 19990613 A 2910 B NUT DOUG MD88 MD88 3023688 NM RT HYD SYST LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 909DL 49540 RT SYS HYDRAULIC QUANTITY DROPPED TO -0- IN FLIGHT. FOUND BRAKE CONTROL VALVE -B- NUT LOOSE. SECURED NUT, SERVICED HYD AND NO LEAKS FOUND. 2 L 7 2 4F RT A6WE 1999062500106 19990625 00106 NM 1999 6 25 DLM88991332 1 19990613 A 3350 P2070003001 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 938DL 49811 MID ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT, CKS GOOD. 2 L 7 2 4F RT A6WE 1999062500107 19990625 00107 NM 1999 6 25 DLM88991333 1 19990613 A 3240 26088921 BRAKE DOUG MD88 MD88 3023688 NM MLG FAILED A DALA O OTHER M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 973DL 53241 AT 8,000 FT BRAKE OVERHEAT LIGHT ILLUM, TEMP STARTED AT 350 AND ROSE TO 410F. THIS TEMP ON NR 4 BRAKE. COMPLIED WITH P OM. LOWERED GEAR AT 14,000 FT, TEMP DECREASED, GEAR RAISED TEMP ROSE TO 275F. FOUND NR 4 TIRE BLOWN. REPLACED NR 4 BR AKE AND NR 3 AND 4 TIRE. 2 L 7 2 4F RT A6WE 1999062500108 19990625 00108 WP 1999 6 25 DLL19991334 1 19990613 A 2910 1549211107 MODULE LKHEED 1011 10113853 5265020 WP NR 2 ENG FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 765DA H2270 193H1206 AFTER DROPPING GEAR, 3 GREEN GEAR LIGHTS. C-SYS PRESSURE STARTED DECREASING, FLUID LOSS INDICATED. DOOR LIGHTS FOR MAI N GEAR REMAINED OPEN. WENT THRU CHECK LIST. TURNED ENG /ATM PUMPS ON, C-SYS OFF. 2 L 7 3 4F A23WE 1999062500109 19990625 00109 NM 1999 6 25 DL72S991335 1 19990613 A 3397 WIRE BOEING 727 727225A 1384077 NM ROW 26D BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805EA 22436 EMERGENCY LIGHT AT SEAT 26D INOP. FOUND BROKEN WIRE AT CONNECTOR. SPLICED WIRE, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 1999062500110 19990625 00110 WP 1999 6 25 DLL19991336 1 19990613 A 3350 SOCKET 337201959 LKHEED 1011 10113853 5265020 WP ROW 2C DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 756DR 193Y1185 EMERGENCY ESCAPE PATH LIGHT DID NOT ILLUM WHEN TESTED. REPLACED SOCKET, NOW OPS NORMAL. 2 L 7 3 4F A23WE 1999062500111 19990625 00111 NM 1999 6 25 SCNA99081 1 19990614 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOV ED AND REPLACED THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT BATTERY PACK (M655). OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999062500112 19990625 00112 NM 1999 6 25 SCNA99082 1 19990613 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND RE PLACED THE RIGHT FORWARD EMERGENCY LIGHT BATTERY PACK (M1086). OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999062500113 19990625 00113 NM 1999 6 25 SCNA99083 1 19990615 A 3350 900542 BATTERY PACK BOEING 727 727225 1384077 NM EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD EXTERNAL OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOV ED AND REPLACED THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999062500114 19990625 00114 NM 1999 6 25 AALA990715 1 19990514 A 5210 TRACK DOUG MD11 MD11 3023602 NM PASSENGER DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - R-1 DOOR CRACKED, 5 INCHES, 2 CRACKS EACH. INSTALLED FABRICATED DOUBLER AND TRACK IAW ESO 41000 DATED 5-12-99. T ST: 27,187.53 HOURS. CYCLES: 3,416. (X) 2 L 7 3 4F RT A22WE 1999062500115 19990625 00115 NM 1999 6 25 AALA990701 1 19990511 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - TRACK ALONG STRINGER FLANGE RADIUS CRACKED. SPLICED AND INSTALLED NEW SECTION OF STRINGER AT END PER ESO 4100 DAT ED 5-10-99. TST: 27,187.5 HOURS. CYCLES: 3,416. (X) 2 L 7 3 4F RT A22WE 1999062500116 19990625 00116 NM 1999 6 25 AALA990700 1 19990511 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - CRACK ALONG STRINGER FLANGE RADIUS. SPLICED AND INSTALLED NEW SECTION OF STRINGER AT END PER ESO 4100 DATED 5-10- 99. TST: 27,187.5 HOURS. CYCLES: 3,416. (X) 2 L 7 3 4F RT A22WE 1999062500117 19990625 00117 NM 1999 6 25 AALA990765 1 19990526 A 5712 RIB BOEING 727 727223 1384074 NM WS 761 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 713AA 22469 TUL - HFEC INDICATES CRACK .50 INCH APPROXIMATELY IN LEFT 70.5 WING T-CHORD RADIUS AT FS 751 (MARKED). REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS AND OTHER REPAIR PARTS IAW SB 727-57-112 FIG 4 AND ESO 11697 DATED 5-24-99. TST: 47 ,052 HOURS. CYCLES: 25,402. (X) 2 L 7 3 4F A3WE 1999062500118 19990625 00118 NM 1999 6 25 AALA990764 1 19990520 A 5330 SKIN BOEING 727 727223 1384074 NM BS 410 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 713AA 22469 TUL - SKIN DENTED AND SCRATCHED STA 410 STR 24R. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-30-3 PAGES 12 -14A. TST: 47,052 HOURS. CYCLES: 25,402. (X) 2 L 7 3 4F A3WE 1999062500119 19990625 00119 NM 1999 6 25 AALA990763 1 19990521 A 5320 CHORD BOEING 727 727223 1384074 NM BS 1176 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 713AA 22469 TUL - AFT VAULT DOOR ENTRY WAY, FS 1176 CHORD IS SEVERELY CORRODED BETWEEN CHORD AND WEB AT BL ZERO TO BL 8 RT. REMOVED CORROSION AREA OF CHORD STA 1176 BL ZERO TO BL 8 RT, INSTALLED DOUBLER PER ESO 11697 DATED 5-17-99. TST: 47,052 HOURS . CYCLES: 25,402. (X) 2 L 7 3 4F A3WE 1999062500120 19990625 00120 NM 1999 6 25 AALA990742 1 19990515 A 2133 AAP1032E OUTFLOW VALVE BOEING 727 727223 1384074 NM A/C BAY DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 872AA 17981 21384 SJU - FLT 1938 - EN ROUTE SJU/TPA CLIMBING THROUGH 30,000 FEET, CABIN PRESSURE STARTED CLIMBING AT 2,000 FEET PER MINUTE . PERFORMED RAPID DECOMPRESSION CHECKLIST WITHOUT RESULTS. AS CABIN ALTITUDE APPROACHED 10,000 FEET, PEFORMED EXPLPERF ORMED EXPLOSIVE DECOMPRESSION CHECKLIST. CABIN ALTITUDE NEVER REGAINED. AIR INTERRUPTED AND LANDED SJU WITHOUT FURTHER INCIDENT. REPLACED BOTH THE AUTO AND MANUAL PRESSURE CONTROL PANELS AND RIGHT OUTFLOW VALVE. RESTORED OXYGEN MASKS. PERFORMED FUNCTIONAL CHECK FLIGHT. SYSTEM CHECKED NORMAL. (X) 2 L 7 3 4F A3WE 1999062500121 19990625 00121 NM 1999 6 25 AALA990711 1 19990514 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 32H FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379AA 25448 EZE - DURING MAINTENANCE CHECK, EMERGENCY EXIT PATH LIGHTS FROM PASSENGER SEAT ROW 32H AFT INOPERATIVE. REPAIRED EMERGE NCY EXIT FLOOR PATH CONNECTOR AT SEAT ROW 36H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999062500122 19990625 00122 WP 1999 6 25 AALA990708 1 19990513 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 291AA 49303 LAX - FLT 1261 - ON APPROACH, CREW REPORTED A LIGHT HAZE OR SMOKE IN CABIN THAT SMELLED LIKE AN ELECTRICAL SMELL. FLIGH T LANDED WITHOUT FURTHER INCIDENT. INSPECTED CABIN AND COCKPIT FOR ELECTRICAL SHORTS WITH NO FINDINGS. AS A PRECAUTONA RY, REMOVED AND REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN-OUT. OPERATION CHECK OF PACKS PRODUCED NO ABNORMAL O DORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999062500123 19990625 00123 NM 1999 6 25 AALA990702 1 19990513 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 38H LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 JFK - DURING MAINTENANCE, EMERGENCY EXIT PATH MARKER LIGHT INOPERATIVE AT SEAT 38H. RESEATED CONNECTOR AT SEAT 38H. SY STEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999062500124 19990625 00124 NM 1999 6 25 AALA990756 1 19990524 A 2820 AAP3043A VALVE BOEING 727 727227 1384078 NM RT WING DEFECTIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 716AA 6227 20608 SJU - FLT 0680 - EN ROUTE AUA/MIA, NR 2 CROSSFEED VALVE FAILED TO OPEN. AIR INTERRUPTED AND LANDED SJU WITHOUT INCIDENT . CHECKED AND DEFERRED ACCORDING TO MEL. SECURED VALVE OPEN AND FLEW TO MIA WITHOUT INCIDENT. REPLACED NR 2 FUEL MANI FOLD VALVE AND CONNECTOR VALVE. PERFORMED OPERATIONAL CHECK WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATI ON. (X) 2 L 7 3 4F A3WE 1999062500125 19990625 00125 NM 1999 6 25 AALA990720 1 19990516 A 3260 CONNECTOR BOEING 757 757223 1384957 NM NLG CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 626AA 24584 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL EXTERIOR EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REPAIRED CORRODED PIN ON CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999062500126 19990625 00126 NM 1999 6 25 AALA990730 1 19990519 A 3297 WIRE BOEING 727 727223 1384074 NM RT MLG LOOSE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 862AA 21089 ORD - FLT 1916 - AFTER TAKEOFF DURING CLIMB-OUT AT 12,000 FEET, RT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED. CREW POSITIO NED GEAR HANDLE IN UP POSITION AND THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED WHEN HANDLE PLACED IN OFF POSITION. FLIGHT CONTINUED AND LANDED ORD WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND RT MLG UPLOCK SENSOR WIRE LOOSE AT GROUNDING STUD. RESECURED LOOSE GROUND WIRE TO STUD. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999062500127 19990625 00127 NM 1999 6 25 AALA990728 1 19990520 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 39AB DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 SFO - DURING MAINTENANCE CHECK, EMERGENCY EXIT PATH LIGHT AT PASSENGER SEAT ROW 39AB INOPERATIVE. REPAIRED EMERGENCY EX IT PATH CONNECTOR AT SEAT ROW 39AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999062500128 19990625 00128 1999 6 25 AALA990722 4 19990506 A 2330 6116730001 VIDEO UNIT BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 376AN 86371 25445 MAN - FLT 0054 - EN ROUTE SEAT 3A AND 3B PERSONAL VIDEO UNITS HAD REPORT OF SMOKING. LANDED MAN WITHOUT INCIDENT. REPL ACED PERSONAL VIDEO UNIT AT 3A. ROCKWELL COLLINS PERFORMED VOTLAGE TEST TO POWER SUPPLY OF PERSONAL VIDEO UNIT AND AT I NPUT. VOLTAGES ARE ALL PROPER. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO NOTICE OF SMOKE. (X) 2 L 7 2 4F RT A1NM 1999062500129 19990625 00129 WP 1999 6 25 AALA990721 1 19990518 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP PASSENGR DOORWAY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455AA 49560 DTW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY WALK-AROUND EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED CONNECTOR T O FORWARD ENTRY WALK-AROUND EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999062500130 19990625 00130 EU 1999 6 25 VTZA990118 1 19990526 A 7722 211M6609 SRI COMPUTER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 480UE 894 IAD/GSO - FLT 7169 - DURING TAKEOFF AT 1420 HOURS ON 5-26-99, AIRCRAFT ABORTED TAKEOFF DUE TO LT ENGINE EGT SPIKE ON TAK EOFF ROLL. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER FROM EMS. MAINTENANCE INSPECTED AND OPENED DMI 42398 MEL 76-1 ON SRI. CHRONIC C00915 REPORT SUBMITTED TO MAINTENANCE ON AIRCRAFT. MAINTENANCE CLOSED DMI 42398 ON 5-27-99 BY SWAPPI NG DELTA P/P COMPUTERS AND GROUND RAN AIRCRAFT. COULD NOT DUPLICATE PROBLEM. MAINTENANCE ALSO CLOSED CHRONIC C0000915 BY INSP ZONE 2 CANNON PLUG AND REMOVING AND REPLACING SRI COMPUTER AND SWAPPING TO BRIDGE NR 2 ON TORQUE SIGNAL CONDITIO NER. OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999062500131 19990625 00131 EU 1999 6 25 VTZA990119 1 19990527 A 2913 PU304436 PUMP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 495UE 818 IAD/PHF - FLT 7411 - AT 1130 HOURS ON 5-27-99 DURING LANDING, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHI CH WAS LT HYDRAULIC PUMP PRESSURE DROPPED TO ZERO BEFORE LANDING. AIRCRAFT WENT TO THE GATE WITH NO FURTHER PROBLEMS. M AINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PUMP. OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR R ETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999062500132 19990625 00132 EU 1999 6 25 USAAF99030 1 19990602 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PASSENGER DOORWA DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 852US 11280 IND - FOUND EMERGENCY LIGHTS INOPERATIVE ABOVE MAIN ENTRY AND FORWARD SERVICE DOORS. MAINTENANCE REPLACED THE BATTERY PACK. (X) 2 L 7 2 4F RT 1999062500133 19990625 00133 EU 1999 6 25 USAAF99029 1 19990528 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU PASSENGER DOORWA DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 859US 11293 IND - FOUND FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (X) 2 L 7 2 4F RT 1999062500134 19990625 00134 WP 1999 6 25 USAAD99071 1 19990601 A 3350 P20120014 LIGHT DOUG DC9 DC931 3022065 WP GALLEY DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 912VJ 47020 PHL - THE GALLEY SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE GALLEY SERVICE DOOR EMERGENCY L IGHT ASSEMBLY. (X) 2 L 7 2 4F A6WE 1999062500135 19990625 00135 NM 1999 6 25 USAA059908 1 19990602 A 3350 20131A BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918TS 20445 BOS/LGA - FLT 6181 - FORWARD SECTION OF EPL INOPERATIVE. REPLACED BATTERY PACK. (X) 2 L 7 3 4F A3WE 1999062500136 19990625 00136 NM 1999 6 25 USAA059909 1 19990602 A 3350 OL3071BPEGPL LAMP BOEING 727 727225 1384077 NM ROW 28 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918TS 20445 BOS/LGA - FLT 6181 - EPL LIGHT INOPERABLE, ROW 28. RELAMPED. (X) 2 L 7 3 4F A3WE 1999062500137 19990625 00137 NM 1999 6 25 GAIA9962 1 19990530 A 2613 OVERHEAT LIGHT BOEING 727 727223 1384074 NM AFT BODY ILLUMINATED A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 854AA 20995 AFTER DEPARATING PHTD EN ROUTE TO PHNL - FLT 7723 - JUST AFTER LEVEL OFF, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. LI GHT GOES OUT AFTER ONE MINUTE, WHEN NR 3 THRUST LEVER IS RETARDED. LIGHT ALSO GOES OUT IF NR 3 BLEED IS CLOSED AND NR 2 BLEED IS OPEN. THRUST LEVERS NORMAL. MADE UNEVENTFUL FLIGHT AND LANDING AT PHNL. IN PHNL, RAN NR 3 ENGINE AND OPENED BLEED VALVE AT PART POWER. COULD NOT DUPLICATE DISCREPANCY. SYSTEM OPERATES NORMALLY. NO OTHER DISCREPANCIES NOTED. A IRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999062500138 19990625 00138 NM 1999 6 25 GAIA9961 1 19990528 A 3610 39271612 VALVE BOEING 727 727223 1384074 NM NR 3 ENGINE FAILED A GAIA K NONE J M WARNING INDICATION OVER TEMP CR CRUISE 1 SW 07 6809 19484 YSSY/NZAA - FLT 6148 - DURING FLIGHT, NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON DURING CRUISE. CREW PEFORMED PROCEDURES PER OAM. LIGHT WENT OUT AFTER POWER REDUCTION. THE CREW MADE A ROUTINE LANDING AT NZAA WITHOUT ANY FURTHER INCIDENTS. AIR LEAK SOURCE FROM 13TH STAGE BLEED AIR MODULATING AND SHUT-OFF VALVE. DEFERRED PER KHA BOEING 727 MEL. (X) 2 L 7 3 4F A3WE 1999062500139 19990625 00139 NM 1999 6 25 GAIA9960A 1 19990527 A 3220 65348784 PIN BOEING 727 7272J0 138407E NM NLG MISSING A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 284KH 21108 MCO - FLT 1726 - AFTER TAKEOFF, RETRACTED GEAR AND GEAR DOOR LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. P ROCEEDED TO MEM AND LANDING WAS SMOOTH. BRAKING WAS STARTED AT 80 KIS, RUMBLE WAS NOTICED IN THE AIRCRAFT. UNABLE TO S TEER AIRCRAFT. AIRCRAFT HAD TO BE TOWED FROM THE RUNWAY. UPON INSPECTION, FOUND THE NOSE LANDING GEAR TORQUE LINK APEX PIN MISSING. REMOVED AND REPLACED DAMAGED STEERING ROD ASSEMBLIES, AND THE LEFT AND RIGHT NOSE WHEEL TIRE ASSEMBLES. R EPLACED NOSE LANDING GEAR TORQUE LINK APEX PIN AND PERFORMED GEAR RETRACTION IAW BOEING MM CHAPTER 32. PERFORMED TAXI C HECK AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A3WE 1999062500140 19990625 00140 NM 1999 6 25 GAIA9963 1 19990601 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM L-1 DOORWAY INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6806 19481 'NO FLIGHT' - FOUND DURING A-CHECK IN DFW. DURING ROUTINE MAINTENANCE AT DFW, THE EMERGENCY LIGHT OVER THE L-1 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE 'EMERGENCY EXIT' LIGHT ASSEMBLY AFTER THE L-1 DOOR. SYSTEM OPERATIO NALLY CHECKS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999062500141 19990625 00141 NM 1999 6 25 F3LA99045 1 19990604 A 2130 39606411 VALVE BOEING 737 737201 1384454 NM FUSELAGE FAILED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 217US 6262 P226 20215 DEN - FLT 546 - FLIGHT CREW REPORTED CABIN ALTITUDE HORN SOUNDED AT 10,000 FEET. CLOSED OUTFLOW VALVE USING MANUAL DC A T 32,500 FEET. CABIN CONTINUED TO CLIMB AT 1,000 FPM AND A RAPID DESCENT WAS MADE TO 14,000 FEET. OXYGEN MASKS WERE AU TOMATICALLY DEPLOYED. REPLACED LT FLOW CONTROL VALVE, RESTOWED OXYGEN MASKS, AND PERFORMED PRESSURIZATION TEST, WITH NO DISCREPANCIES NOTED. CYCLES: 4,630. (X) 2 L 7 2 4F A16WE 1999062500142 19990625 00142 NM 1999 6 25 F3LA99043 1 19990604 A 3220 658005111 DRAG BRACE BOEING 737 737201 1384454 NM NLG CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 2018 193 19421 DEN - DURING SERVICE CHECK, INSPECTION REPORTED NOSE LANDING GEAR UPPER DRAG BRACE BEARING MIGRATING AT ACTUATOR ATTACH POINT. UPON FURTHER INSPECTION, FOUND 1 INCH CRACK IN NOSE GEAR UPPER DRAG BRACE A-FRAME ON RT SIDE OF WEB. MAINTENAN CE INSTALLED NEW DRAG BRACE PER MM 32-32-21, PERFORMED RETRACTION TEST OF NLG, AND CHECKED OKAY. CYCLES: 66,483. (X) 2 L 7 2 4F A16WE 1999062500143 19990625 00143 NM 1999 6 25 F3LA99044 1 19990605 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 42904 22734 DEN - DURING C-CHECK, INSPECTION REPORTED .1250 INCH CRACK IN LT FUSELAGE SKIN PANEL AT BS 727, STR 16L. MAINTENANCE FA BRICATED FILLER AND DOUBLER AND INSTALLED USING REQUIRED FASTENERS PER SRM 53-30-3. CYCLES: 25,993. (X) 2 L 7 2 4F RT A16WE 1999062500144 19990625 00144 NM 1999 6 25 F3LA99033 1 19990423 A 7120 65468508 BOLT BOEING 737 737201 1384454 NM NR 2 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 5934 018 20215 DEN - FLT 857 - DURING SERVICE CHECK, EO 71-20-737-002 WAS ACCOMPLISHED WHICH FOUND THE NR 2 ENGINE OUTBOARD LUG BEARING LOOSE AND DISPLACED. AN ULTRA SOUND INSPECTION REVEALED THE FORWARD ENGINE MOUNT BOLT CRACKED. MAINTENANCE REPLACED N R 2 ENGINE MOUNT ASSEMBLY AND CHECKED OKAY. CYCLES: 4,444. (X) 2 L 7 2 4F A16WE 1999062500145 19990625 00145 EU 1999 6 25 F3LA99041 2 19990525 A 7230 COMPRESSOR BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE FAILED A F3LA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 304FL 27633 EN ROUTE TO SEA, NR 1 ENG SPOOLING DOWN AND NR 1 ENG VIB AT 35,000 FT, SPARKS COMING FROM TAILPIPE. NO FIRE WARN OR O/H IND. NR 1 ENG WAS SHUTDOWN AND NR 1 ENG FIRE BOTTLE WAS DISCHARGED AS A PRECAUTION. DECLARED AN EMERG AND LANDED W/O INCIDENT. NO EMERG EQUIP WAS USED. MX FOUND INTERNAL TURBINE FAILURE AND REPLACED NR 1 ENG. THE FAILURE WAS CONTAINED WITHIN THE ENG, NO EXTERNAL DAMAGE. CAUSE OF DAMAGE WAS DUE TO NR 3 BEARING FAILURE (NO EVIDENCE OF OIL STARVATION). RESULTING BLADE TIP RUB WITH CASE CAUSED EXTENSIVE COMPRESSOR BLADE DAMAGE 6TH STAGE AFT. UNIQUE TO THE 8TH STAGE, 20 BLADES WERE MISSING FROM HUB AND TRAVELED AFT AND ENTERED THE HPT. KEEPER HARDWARD WAS INTACT FOR ALL COMPRESSOR STAGES 2 L 7 2 4F 4 F RT A16WE E21EU 1999062500146 19990625 00146 NM 1999 6 25 F3LA99036 1 19990414 A 5320 WEB BOEING 737 737201 1384454 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 73293 20212 DEN - FLT DURING C-CHECK, INSPECTION REPORTED RIGHT A/C BAY VERTICAL WEB CRACKED AT FORWARD END OF RAM AIR DUCT, BBL 41 KEEL BEAM. MAINTENANCE REPAIRED PER EA 737-57-024. CYCLES: 91,351. (X) 2 L 7 2 4F A16WE 1999062500147 19990625 00147 NE 1999 6 25 PLGA990525 2 19990525 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LEFT FAILED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 742BA 340A092 367299 PQI - FLT 6217 - SHORTLY AFTER TAKEOFF, OUT OF PQI, LEFT ENGINE FAILED. CREW SECURED THE ENGINE. AIRCRAFT DIVERTED TO BGR AND LANDED WITHOUT INCIDENT. LEFT ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999062500148 19990625 00148 NM 1999 6 25 F3LA99042 1 19990524 A 5542 65C2584168 SKIN BOEING 737 7373M8 1384615 NM RUDDER LIGHTNING STRIKE A F3LA K NONE C F.O.D. IN INSP/MAINT 1 NM 03 303FL 25039 BOS - FLT 520 - UPON ARRIVAL IN BOS, FLIGHT CREW REPORTED A LIGHTNING STRIKE TO AIRCRAFT. MAINTENANCE PERFORMED A LIGHT INING STRIKE INSPECTION PER MM 05-51-27 AND NOTED DAMAGE TO RUDDER. INSTALLED TEMPORARY REPAIR PER MM 55-40-01 AND FERR IED AIRCRAFT TO DENVER. REMOVED AND REPAIRED RUDDER PER SRM 51-70-04 AND SRM 55-40-01, AND EA 55-737-303. RUDDER WAS R EBALANCED IN FIXTURE PER SRM 51-60-07 AND REINSTALLED ON AIRCRAFT. CYCLES: 10,770. (X) 2 L 7 2 4F RT A16WE 1999062500149 19990625 00149 NM 1999 6 25 F3LA99034 1 19990414 A 5311 FRAME BOEING 737 737201 1384454 NM BS 380 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 73293 20212 DEN - DURING C-CHECK, INSPECTION REPORTED TWO CRACKS ON FRAME AT BS 380 BETWEEN STR 20R AND STR 21R IN THE FORWARD CARGO COMPARTMENT. MAINTENANCE FABRICATED AND INSTALLED CHANNEL SPLICES PER SRM 51-40-3. CYCLES: 91,351. (X) 2 L 7 2 4F A16WE 1999062500150 19990625 00150 NE 1999 6 25 PLGA990518 2 19990518 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 349BE 340B196 785317 BGR - FLT 6415 - AFTER TAKEOFF OUT OF BGR EN ROUTE TO BOS, THE LT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. AIRCRAFT RETU RNED TO BGR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND UNACCEPTABLE METAL ON THE CHIP DETECTOR. THE SUBJECT ENGIN E HAD ONLY 293 HOURS SINCE LAST OVERHAUL. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1999062500151 19990625 00151 EU 1999 6 25 PLGA990540 1 19990504 A 2613 OVERHEAT SENSOR SAAB SF340 340B 7860101 EU RT ENGINE FAILED A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 349BE 340B196 PWM - FLT 6523 - AFTER DEPARTURE FROM PWM, CREW HAD A RT TAIL PIPE HOT LIGHT ILLUMINATE. CREW DIVERTED BACK TO PWN AND LANDED WITHOUT INCIDENT. CREW DID NOT SHUT DOWN THE ENGINE. THERE WERE NO PASSENGERS ON BOARD. MAINTENANCE FOUND A FA ULTY SENSOR WHICH WAS REPLACED. REQUIRED OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999062500152 19990625 00152 1999 6 25 PLGA990515 4 19990515 A 2312 CONNECTOR CESSNA 340 340A 2076405 CE NR 1 COMM DIRTY A PLGA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 NE 05 339BE 340A044 BOS - FLT 6433 - DURING FLIGHT, NR 1 COMM FAILED AND FLIGHT CONTROL HAD THE AIRCRAFT RETURN TO BOS. BOS MAINTENANCE CLE ANED THE CONNECTORS ON THE R/T UNIT AND PERFORMED GROUND CHECKS. ALL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERV ICE. (X) 1 L 7 2 3O 3A25 1999062500153 19990625 00153 NM 1999 6 25 ASAA9910102 1 19990520 A 5312 BULKHEAD CHORD BOEING 737 7372Q8C 138448S NM BS 178 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD, LBL 5.7 AND WL 195, PUNCTURED AND CRACKED. REPAIRED PER SRM 53-10-11, FIG 8. (X) 2 L 7 2 4F A16WE 1999062500154 19990625 00154 NM 1999 6 25 ASAA9910103 1 19990520 A 5313 STRINGER BOEING 737 7372Q8C 138448S NM BS 322-326 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND STR 26R, BS 322 TO BS 326, CORRODED. REPAIRED PER SRM 53-10-3. (X) 2 L 7 2 4F A16WE 1999062500155 19990625 00155 NM 1999 6 25 ASAA9910104 1 19990520 A 5313 STRINGER BOEING 737 7372Q8C 138448S NM BS 294.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND STR 25R, BS 294.5 TO BS 348, CORRODED. REPAIRED PER SRM 53-10-3. (X) 2 L 7 2 4F A16WE 1999062500156 19990625 00156 NM 1999 6 25 ASAA9910105 1 19990520 A 5330 SKIN BOEING 737 7372Q8C 138448S NM BS 907 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING C-CHECK, FOUND EXTERNAL FUSELAGE SKIN AT BS 907, STR 10L, GOUGED. REPAIRED PER SRM 53-30-3, FIG. 16. (X). 2 L 7 2 4F A16WE 1999062500157 19990625 00157 NM 1999 6 25 ASAA9910106 1 19990520 A 5313 BAC1498157 STRINGER BOEING 737 7372Q8C 138448S NM BS 947-987 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING C-CHECK, FOUND AFT CARGO PIT STR 27L CORRODED FROM BS 947 TO BS 987. REPAIRED PER SRM 53-10-2, FIG 9. (X) 2 L 7 2 4F A16WE 1999062500158 19990625 00158 NM 1999 6 25 ASAA9910107 1 19990520 A 5311 6546547107 FRAME BOEING 737 7372Q8C 138448S NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND EXTERNAL FUSELAGE, LOWER SIDE FRAME AT STA 727 FROM STR 26L TO STR 26R CORRODED ON BOTTOM S IDE. REPAIRED PER SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1999062500159 19990625 00159 NM 1999 6 25 ASAA9910108 1 19990520 A 5313 BAC1498163 STRINGER BOEING 737 7372Q8C 138448S NM BS 962 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND AFT CARGO PIT STRINGER 24R, AT APPROXIMATELY BS 962, CORRODED. REPAIRED PER SRM 53-10-3. ( X) 2 L 7 2 4F A16WE 1999062500160 19990625 00160 NM 1999 6 25 ASAA9910109 1 19990520 A 5311 FRAME BOEING 737 7372Q8C 138448S NM BS 987 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND AFT CARGO PIT FRAME AT BS 987 CORRODED FROM STR 18L TO STR 18R. REPAIRED PER SRM 51-30-2. ( X) 2 L 7 2 4F A16WE 1999062500161 19990625 00161 NM 1999 6 25 ASAA9910110 1 19990520 A 5314 65621251 KEEL BEAM BOEING 737 7372Q8C 138448S NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE LOWER SIDE, KEEL BEAM 27R BETWEEN STA 727 - STA 727A CORRODED ON BOTTO M SIDE. REPAIRED PER EA 5310-01687. (X) 2 L 7 2 4F A16WE 1999062500162 19990625 00162 NM 1999 6 25 ASAA9910111 1 19990520 A 5314 65621251 KEEL BEAM BOEING 737 7372Q8C 138448S NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE LOWER SIDE, KEEL BEAM 27L BETWEEN STA 727 - STA 727A CORRODED ON BOTTO M SIDE. REPAIRED PER EA 5310-01687. (X) 2 L 7 2 4F A16WE 1999062500163 19990625 00163 NM 1999 6 25 ASAA9910112 1 19990520 A 5315 6554907501 FLOORBEAM BOEING 737 7372Q8C 138448S NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE MAIN CABIN FLOORBEAM CORRODED ON TOP AND BOTTOM SIDES OF FLANGE AT BS 727B, BL ZERO TO 5 6. REPAIRED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1999062500164 19990625 00164 NM 1999 6 25 ASAA9910113 1 19990520 A 5320 6567140 SUPPORT BOEING 737 7372Q8C 138448S NM BS 580-727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE LONGITUDINAL SEAT TRACK SUPPORTS CORRODED AT BS 580 - BS 727B, LBL 24.5, BL ZERO, RBL 24 .5 AND RBL 45.5. REPAIRED PER EA 5320-01373. (X) 2 L 7 2 4F A16WE 1999062500165 19990625 00165 NM 1999 6 25 ASAA9910114 1 19990520 A 5330 654577553 SKIN BOEING 737 7372Q8C 138448S NM BS 787-907 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PDX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE SKIN FROM BS 787 TO BS 907, STR 20R TO STR 26R LIGHTLY PITTED WITH COR ROSION. REPAIRED PER SRM 51-10-1 AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1999062500166 19990625 00166 NM 1999 6 25 ASAA9910115 1 19990520 A 5315 6546547520 FLOORBEAM BOEING 737 7372Q8C 138448S NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PDX - DURING C-CHECK, FOUND THE PASSENGER CABIN STUB FLOORBEAM CORRODED AROUND FASTENER HOLES ON TOP SIDE, BS 727, RBL 5 4.0. REPAIRED PER DWG 65-46547; SRM 53-10-1. (X) 2 L 7 2 4F A16WE 1999062500167 19990625 00167 NM 1999 6 25 ASAA9910116 1 19990520 A 5347 605013 SEAT TRACK BOEING 737 7372Q8C 138448S NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE PASSENGER CABIN SEAT TRACK CORRODED ON TOP AND BOTTOM SIDES AT BS 727A TO BS 727B, RBL 6 2.5. REPAIRED PER SRM 53-10-5, FIG 7. (X) 2 L 7 2 4F A16WE 1999062500168 19990625 00168 NM 1999 6 25 ASAA9910117 1 19990520 A 5330 SKIN BOEING 737 7372Q8C 138448S NM BS 685 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE FUSELAGE AT STA 685 BETWEEN STR 4L AND STR 5L GOUGED. REPAIRED PER SRM 53-30-3, FIG 2. (X) 2 L 7 2 4F A16WE 1999062500169 19990625 00169 NM 1999 6 25 ASAA9910118 1 19990520 A 5320 69774611 SUPPORT BOEING 737 7372Q8C 138448S NM BS 332-344 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE R-1 SERVICE DOOR FRAME SUPPORT, TOP AFT LOCATION 332 RT CRACKED. REPAIRED PER SB 737-53 -1108, REV 5. (X) 2 L 7 2 4F A16WE 1999062500170 19990625 00170 NM 1999 6 25 ASAA9910119 1 19990520 A 5347 BAC15201430 SEAT TRACK BOEING 737 7372Q8C 138448S NM BS 540 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK CORRODED AT BS 540, LBL65. REPAIRED PER SRM 53-10-5, FIG 7. (X) 2 L 7 2 4F A16WE 1999062500171 19990625 00171 NM 1999 6 25 ASAA9910120 1 19990520 A 5320 654582936 T-CHORD BOEING 737 7372Q8C 138448S NM BS 351.2-360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE E/E COMPARTMENT T-CHORD COMMON TO STR 27R CORRODED FROM STA 351.20 TO STA 360. REPAIRE D PER EA 5310-01691. (X) 2 L 7 2 4F A16WE 1999062500172 19990625 00172 NM 1999 6 25 ASAA9910121 1 19990520 A 5330 654577646 SKIN BOEING 737 7372Q8C 138448S NM BS 727-887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE EXTERNAL FUSELAGE SKIN FROM BS 727 TO BS 887, STR 25L TO STR 25R LIGHTLY PITTED WITH COR ROSION. REPAIRED PER EA 5330-01378. (X) 2 L 7 2 4F A16WE 1999062500173 19990625 00173 1999 6 25 AALA990717 4 19990517 A 2397 WIRE BOEING 767 767223 1385123 NM EMERGENCY EXIT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 22335 SFO - DURING OVERNIGHT MAINTENANCE, MID-GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED OPEN WIRE INTO CONNECTOR. SYS TEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999062500174 19990625 00174 NM 1999 6 25 SWAA991038 1 19990617 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM ROW 3 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP FWD OF ROW 3. RECONNECTED WIRE TO LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999062500175 19990625 00175 NM 1999 6 25 SWAA991039 1 19990617 A 3350 610478 BATTERY CHARGER BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F A16WE 1999062500176 19990625 00176 NM 1999 6 25 SWAA991040 1 19990617 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999062500177 19990625 00177 NM 1999 6 25 SWAA991041 1 19990617 A 5320 6546525 SHEAR TIE BOEING 737 7372H4 138448C NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CRACKED, BS 380, STRINGER 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999062500178 19990625 00178 NM 1999 6 25 SWAA991042 1 19990617 A 5313 6552988 STRINGER BOEING 737 7372H4 138448C NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 4L CRACKED, BS 907. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999062500179 19990625 00179 NM 1999 6 25 SWAA991043 1 19990617 A 5313 BAC1505 STRINGER BOEING 737 7372H4 138448C NM BS 276 & 310 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 19R 2 EACH CRACKS, BS 276, AND BS 310. REPAIRED STRINGER PER SR M. 2 L 7 2 4F A16WE 1999062500180 19990625 00180 NM 1999 6 25 SWAA991044 1 19990617 A 5311 6516323 FRAME BOEING 737 7372T4 1384492 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED, BS 344, LBL 39, WL 165. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999062500181 19990625 00181 NM 1999 6 25 SWAA991045 1 19990617 A 5240 6969854 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED IN AFT LOWER CORNER. REPAIRED FRAME PER BAC DRAWING. 2 L 7 2 4F RT A16WE 1999062500182 19990625 00182 NM 1999 6 25 SWAA991046 1 19990617 A 5320 141A880 POST BOEING 737 7373H4 1384600 NM LT COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND 0.5 INCH LONG CRACK ON UPPER OUTBD CORNER OF CAPTAIN'S NR 1 WINDOW POST. REPAIRED WI NDOW POST PER SWA RA NR 1 A53-1156. 2 L 7 2 4F RT A16WE 1999062500183 19990625 00183 NM 1999 6 25 SWAA991025 1 19990613 A 5523 183A8410 BUSHING BOEING 737 7377H4 NM RT ELEV TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 708SW 27842 DURING SCHEDULED SPECIAL CHECK, RT ELEVATOR TAB FAILED BEARING FREEPLAY CHECK. REMOVED AND REPLACED BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 1999062500184 19990625 00184 NM 1999 6 25 SWAA991026 1 19990615 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 11-12 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP BETWEEN ROWS 11-12. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999062500185 19990625 00185 1999 6 25 SWAA991027 4 19990615 A 2565 D31591 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED RON CHECK, FWD ENTRY DOOR SLIDE WAS ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999062500186 19990625 00186 NM 1999 6 25 SWAA991014 1 19990614 A 2560 6947525 BRACKET BOEING 737 7373H4 1384600 NM PASSENGER DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR FELL FROM STOWAGE ASSY. REPAIRED GIRT BAR STOW BRACKET AND REPOSITIONED SLIDE ASSY. 2 L 7 2 4F RT A16WE 1999062500187 19990625 00187 NM 1999 6 25 SWAA991015 1 19990614 A 5313 6546569 STRINGER BOEING 737 7372T4 1384492 NM BS 374-378 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND CORROSION AT STRINGER 27L, BS 374-378. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999062500188 19990625 00188 NM 1999 6 25 SWAA991016 1 19990614 A 5311 6546569 FRAME BOEING 737 7372T4 1384492 NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 1138, STRINGER 5L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999062500189 19990625 00189 NM 1999 6 25 SWAA991017 1 19990614 A 5320 BAC1498 SPLICE BOEING 737 7372T4 1384492 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 907, STRINGER 4L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F A16WE 1999062500190 19990625 00190 NM 1999 6 25 SWAA991018 1 19990615 A 5311 6546569 FRAME BOEING 737 7372T4 1384492 NM BS 986.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED, BS 986.5, WL 207. LBL 47.5. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999062500191 19990625 00191 NM 1999 6 25 SWAA991019 1 19990615 A 5320 BAC1515 CHORD BOEING 737 7372T4 1384492 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CRACKED, BS 663, LBL63, WL 208. REPAIRED CHORD PER SRM. 2 L 7 2 4F A16WE 1999062500192 19990625 00192 NM 1999 6 25 SWAA991020 1 19990615 A 5754 6573714 SKIN BOEING 737 7372T4 1384492 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND NR 6 L/E SLAT CENTER AUX TRACK SKIN CUTOUT CRACKED ON UPPER FWD EDGE. REPAIRED SKIN PER ER 99-5412. 2 L 7 2 4F A16WE 1999062500193 19990625 00193 NM 1999 6 25 SWAA991021 1 19990615 A 5320 BAC1498 SPLICE BOEING 737 7372T4 1384492 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 360, STRINGER 4R. REPAIRED SPLICE PER SRM. 2 L 7 2 4F A16WE 1999062500194 19990625 00194 NM 1999 6 25 SWAA991022 1 19990615 A 5320 BAC1518 STIFFENER BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND CRACKED VERTICAL STIFFENER, BS 727 BULKHEAD AFT SIDE, LBL 26. REMOVED AND REPLACED STIF FENER PER SRM. 2 L 7 2 4F A16WE 1999062500195 19990625 00195 NM 1999 6 25 SWAA991023 1 19990614 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 1 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C1 CHECK, FOUND NR 1 L/E SLAT AUX TRACK SKIN CUTOUT CRACKED. REPAIRED SKIN PER SWA RA NR 1-A57-0691. 2 L 7 2 4F RT A16WE 1999062500196 19990625 00196 NM 1999 6 25 SWAA991024 1 19990614 A 5523 183A8400 HINGE BOEING 737 7377H4 NM ELEV TAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 707SA 27841 DURING SCHEDULED SPECIAL CHECK, FOUND RT ELEVATOR TAB MAST FITTING HAS A .125 INCH LONG CRACK ON UPPER OUTBD FLANGE RADI US. REMOVED AND REPLACED RT ELEVATOR TAB ASSY. 2 L 7 2 4F RT A16WE 1999062500197 19990625 00197 NM 1999 6 25 SWAA991028 1 19990616 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999062500198 19990625 00198 NM 1999 6 25 SWAA991029 1 19990616 A 5313 6545776 STRINGER BOEING 737 7372H4 138448C NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND CORROSION ON STRINGER 27R, BS 967. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999062500199 19990625 00199 NM 1999 6 25 SWAA991030 1 19990616 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM BS 936 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 936, STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999062500200 19990625 00200 NM 1999 6 25 SWAA991031 1 19990616 A 3230 A42006028305 SOLENOID BOEING 737 7375H4 138449D NM LANDING GEAR MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 523SW 26565 LANDING GEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF FROM SMF. LANDING GEAR OVERRIDE TRIGGER WAS UTILIZED. AFTER DETE RMINING THERE WAS NOT AN AIR/GROUND SENSOR PROBLEM, GEAR RETRACTED NORMALLY. REMOVED AND REPLACED LANDING GEAR SAFETY S OLENOID PER MM. 2 L 7 2 4F RT A16WE 1999062500201 19990625 00201 NM 1999 6 25 SWAA991032 1 19990616 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM BS 767-847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND STRINGER 10R CRACKED AT BS 767, BS 787, BS 807, BS 827, AND BS 847. REPAIRED STRINGER P ER SRM. 2 L 7 2 4F A16WE 1999062500202 19990625 00202 NM 1999 6 25 SWAA991033 1 19990616 A 5330 6547952 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR, UPPER HINGE ARM CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999062500203 19990625 00203 NM 1999 6 25 SWAA991034 1 19990616 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON FWD SERVICE DOOR, LOWER FWD CUTOUT CORNER. REPAIRED SKIN PE R SWA RA NR 1-353-2095. 2 L 7 2 4F RT A16WE 1999062500204 19990625 00204 NM 1999 6 25 SWAA991035 1 19990616 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED BC3 CHECK, FOUND A 1.5 INCH LONG CRACK ON FUSELAGE SKIN, BS 947, ABOVE STRINGER 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999062500205 19990625 00205 NM 1999 6 25 SWAA991036 1 19990616 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 11-12 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTS INOP BETWEEN ROWS 11 AND 12. RECONNECTED WIRE AT R OWS 11-12 PER MM. 2 L 7 2 4F RT A16WE 1999062500206 19990625 00206 NM 1999 6 25 SWAA991037 1 19990616 A 5523 183A81001 TAB BOEING 737 7377H4 NM LT & RT ELEV CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT ELEVATOR TABS WITH NUMEROUS CRACKS AROUND ATTACH POINT CUTOUTS. REMOVED AND REPLACED ELEVATOR TABS PER MM. 2 L 7 2 4F RT A16WE 1999062500207 19990625 00207 NM 1999 6 25 HNAA9900070 1 19990619 A 3350 10126269 SIGN DHC DHAV DHC8 DHC8102 2809003 NM ROW 4DF LOOSE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 916HA 32976 32976 072 072 EMERGENCY LIGHT SIGN AT 4D-F KNOCKED OFF. RESECURED SIGN. 2 H 7 2 4T RT A13NM 1999062500208 19990625 00208 EU 1999 6 25 MALA976499 1 19990607 A 2910 HYD LINE SAAB SF340 SF340A 7850100 EU RT NACELLE CHAFED A MALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 114XJ 340A114 IN FLIGHT EXPERIENCED A LOSS OF HYDRAULIC FLUID AND MAIN ACCUMULATOR PRESSURE DECREASE, PERFORMED EMERGENCY GEAR EXTENTI ON. DURING TROUBLE SHOOTING, MAINTENANCE FOUND DOWNLOCK HYDRAULIC LINE IN RIGHT NACELLE CHAFFED AND LEAKING, REPAIRED B Y PERMASWEDGE METHOD. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999062500209 19990625 00209 EU 1999 6 25 MALA976500 1 19990610 A 3620 51653118 CONTROL UNIT SAAB SF340 SF340A 7850100 EU LT NACELLE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 991XJ 091 LEFT BLEED AIR LEAK CAME ON SHORTLY AFTER TAKEOFF, AT 1000 FT, FOLLOWED THE QRH AND THE LIGHT REMAINED ON. MAINTENANCE REPLACED BLEED AIR DETECT CONTROL UNIT IAW AMM 36. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999062500210 19990625 00210 EU 1999 6 25 MALA976501 1 19990611 A 3350 7239410802 LIGHT SAAB SF340 SF340A 7850100 EU ROW 4CD INOPEATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 106XJ 106 DURING INSPECTION, EMERGENCY FLOOR LIGHTING AT 4CD INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999062500211 19990625 00211 1999 6 25 MALA976502 4 19990613 A 3442 6222504001 RADAR SAAB SF340 340B 7860101 EU FWD FUSELAGE FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 402XJ 340B402 WEATHER RADAR TILT DOES NOT WORK, IT WOULD ONLY PAINT A SOLID RED LINE AT ABOUT 10 DME. THEN RED LINE WOULD INCREASE WI TH ALTITUDE, RESET CB'S TWICE WITH NO EFFECT, STABALIZATION HAD NO EFFECT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLA CED WEATHER RADAR ANTENNA DRIVE. SYSTEM OPS CHECK GOOD IAW SF 340 MM CHAP 34. 2 L 7 2 4T RT A52EU 1999062500212 19990625 00212 EU 1999 6 25 MALA976503 1 19990618 A 5320 SKIN SAAB SF340 SF340A 7850100 EU BS 345.25 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 DURING HEAVY CHECK INSPECTION, FOUND DENT ON RIGHT FORWARD FUSELAGE AT STATION 345.25 WL 94. REPAIRED IAW MAL EO S53009 PERMENANT REPAIR. 2 L 7 2 4T RT A52EU 1999062500213 19990625 00213 NE 1999 6 25 AWXA9900222 2 19990614 A 7230 COMPRESSOR AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE STALLED A AWXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 28 636AW 098 AIR TURNBACK, NR 2 ENGINE COMPRESSOR STALL AND HIGH EGT. NONE RECEIVED. WILL UPDATE WHEN INFORMATION IS AVAILABLE. 2 L 7 2 4F 4 F RT A28NM E311NE 1999062500214 19990625 00214 NM 1999 6 25 RAAA99B2045 1 19990615 A 3350 862104 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 MID CABIN DOOR EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999062500215 19990625 00215 NM 1999 6 25 RAAA99B2046 1 19990617 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 15 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999062500216 19990625 00216 NM 1999 6 25 CALA9900694 1 19990615 A 2612 FIRE LOOP BOEING 737 7373T0 1384582 NM APU MALFUNCTIONED A CALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 47332 23570 THE APU FIRE DETECTION LIGHT ILLUMINATED AT FL 350 WHILE EN ROUTE FROM IAH TO SEA. EMERGENCY PROCEDURES WERE FOLLOWED A ND THE FIRE BOTTLE WAS DISCHARGED. THE AIRCRAFT WAS DIVERTED TO ABQ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUN D NO EVIDENCE OF FIRE. THE APU FIRE DETECTION SYSTEM WAS TROUBLESHOT IAW MM 26-11-00 WITH NO DISCREPANCIES NOTED. MAIN TENANCE INSPECTED FIRELOOPS AND SHOOK WIRES. THE FAILURE COULD NOT BE DUPLICATED AND SELF TEST WAS NORMAL. 2 L 7 2 4F RT A16WE 1999062500217 19990625 00217 NM 1999 6 25 CALA9900695 1 19990615 A 3397 WIRE BOEING 737 737724 NM COCKPIT BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17719 28938 INSPECTION FOUND THE COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT RESISTOR R340 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999062500218 19990625 00218 NM 1999 6 25 CALA9900696 1 19990615 A 3350 0803004 LIGHT BOEING 737 737524 1384721 NM L2 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17614 27327 INSPECTION FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT L-2 DOOR. THE EXIT LIGHT ASSEMBLY WAS REPLACED IAW MM 33-51-11. 2 L 7 2 4F RT A16WE 1999062500219 19990625 00219 NM 1999 6 25 CALA9900697 1 19990617 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND A .75 INCH CRACK IN C-2 DOOR SKIN AT DOOR HANDLE CUTOUT. A REPAIR WAS INSTALLED IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 1999062500220 19990625 00220 NM 1999 6 25 CALA9900698 1 19990617 A 3350 S283W6032 BATTERY PACK BOEING BOEING 737 737724 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16713 28784 INSPECTION FOUND AFT SEATS EMERGENCY LIGHT INOPERATIVE. THE AFT SEATS EMERGENCY LIGHT BATTERY ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999062500221 19990625 00221 NM 1999 6 25 CALA9900699 1 19990617 A 5330 SKIN BOEING 727 727232 1384082 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND FUSELAGE SKIN BULGED AFT OF EXTERNAL POWER RECEPTACLE AT STA 294, WL 160. THE BULGED AREA WAS CUT OUT. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1999062500222 19990625 00222 WP 1999 6 25 CALA9900700 1 19990617 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-250 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 200-250. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-01, FIGU RE 4, SHEET 1. 2 L 7 2 4F A6WE 1999062500223 19990625 00223 WP 1999 6 25 CALA9900701 1 19990617 A 5320 STOP DOUG DC9 DC982 3022082 WP BAGGAGE COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND FORWARD DOOR STOP FLANGE AT MAIN BAGGAGE BIN DOOR JAMB CORRODED. A REPAIR DOUBLER WAS INSTALLED ON FOR WARD STOP PAD LOWER AREA AT MAIN BAG BIN Z-ANGLE IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1999062500224 19990625 00224 WP 1999 6 25 CALA9900702 1 19990617 A 2560 4919021501 DRIVE SHAFT DOUG DC9 DC982 3022082 WP RT EMER EXIT LACK OF LUBE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND RT WING OVERWING EMERGENCY ESCAPE LINE HARD TO PULL FROM REEL. THE DRIVE SHAFT ASSEMBLY WAS CLEANED AN D LUBRICATED IAW MM 25-60-00. 2 L 7 2 4F A6WE 1999062500225 19990625 00225 NM 1999 6 25 CALA9900703 1 19990618 A 2560 ACREM1A MEGAPHONE BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12216 28776 INSPECTION FOUND MEGAPHONE IN AFT PASSENGER COMPARTMENT INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1999062500226 19990625 00226 NM 1999 6 25 CALA9900704 1 19990618 A 2560 10077977 MEGAPHONE BOEING 777 777224 1385225 NM GALLEY INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78003 27579 INSPECTION FOUND AFT MEGAPHONE AT GALLEY NR 6 INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT T00001SE 1999062500227 19990625 00227 WP 1999 6 25 CALA9900705 1 19990618 A 5210 SKIN DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND A .5 CRACK IN L-1 DOOR EXTERIOR SKIN AT FORWARD LOWER CORNER. A REPAIR WAS INSTALLED IAW SRM 52-03-00, FIGURE 37, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999062500228 19990625 00228 WP 1999 6 25 CALA9900706 1 19990618 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND A .375 INCH CRACK AND LOOSE RIVETS IN FUSELAGE SKIN ABOVE LEFT AFT NOSE WHEEL WELL DOOR AFT HINGE AREA. THE CRACKED AREA AND RIVETS WERE REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 53-05-00, PAGE 169 AND 51-1 0-3, PAGE 1. 2 L 7 2 4F A6WE 1999062500229 19990625 00229 WP 1999 6 25 CALA9900707 1 19990618 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1030-1305 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND LT O/B SEAT TRACK CORRODED UNDER GALLEY AREAS NR 3 AND NR 4 AT STA 1030-1305. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999062500230 19990625 00230 WP 1999 6 25 CALA9900708 1 19990618 A 3350 AD4002P BATTERIES AEROQUALITY DOUG DC9 DC932 3022066 WP EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERIES IN BATTERY PACK WERE REPLACED AND EME RGENCY LIGHT OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999062500231 19990625 00231 NM 1999 6 25 CALA9900709 1 19990618 A 3350 MISC062 BATTERY PACK AVIALL BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND EMERGENCY LIGHTS AT SEVEN SEATS IN COACH SECTION OF CABIN INOPERATIVE. THE OVERHEAD BATTERY PACK WAS R EMOVED AND REPLACED AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999062500232 19990625 00232 NM 1999 6 25 UPS99229854 1 19990609 A 7120 CLEVIS BOEING 727 72731C 1384011 NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI SUPPORT STRUT ABOVE NR 2 ENGINE HORIZ FIREWALL LUG CRACKED AT LWR ATTACHMENT POINT. NR 2 ENGINE ST RUCTURE SUPPORT STRUT LWR CLEVIS REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999062500233 19990625 00233 NM 1999 6 25 UPS99229855 1 19990604 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI FWD CARGO BAY BS 720 CORROSION ON FRAME CHORD ANGLE AT STRINGER 27 LT APPROX. CORROSION REMOVED IA W SRM 51-10-6 AND FOUND TO EXCEED LIMITS CORRODED SECTION OF CHORD ANGLE WAS REMOVED IAW SRM 51-40-3 AND ANGLE REPAIR WA S CARRIED OUT IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1999062500234 19990625 00234 NM 1999 6 25 UPS99229856 1 19990601 A 5310 STRUCTURE BOEING 727 72731C 1384011 NM BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI FWD CARGO DOOR CUT-OUT STRUCTURE CRACKED AT BS 520 NEAR STRINGER 21 AT STOP NR 4. REPAIR CARRIED O UT IAW SRM 51-40-2 FIG 1 AND DRAWING 65-18385. 2 L 7 3 4F A3WE 1999062500235 19990625 00235 NM 1999 6 25 UPS99229858 1 19990601 A 5320 INTERCOSTAL BOEING 727 72731C 1384011 NM BS 480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI CRACK IN INTERCOSTAL AT BS 480 STR 27R. REPAIRED IAW SRM 51-30-02, 51-20-01, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999062500236 19990625 00236 NM 1999 6 25 UPS99229859 1 19990530 A 5520 BALANCE PANEL BOEING 727 72731C 1384011 NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI NR 2 BALANCE PANEL AFT HINGE FWD HALF CRACKED RT SIDE. REPLACED NR 2 BALANCE PANEL AFT HINGE FWD H ALF IAW 27-30-21 MM. 2 L 7 3 4F A3WE 1999062500237 19990625 00237 NM 1999 6 25 UPS99229860 1 19990530 A 5320 NUT BOEING 727 72731C 1384011 NM BS 540-560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI SURFACE CORROSION AROUND A/NUTS BS 540 - 560 LT LBL 24.75. REPAIR CARRIED OUT IAW SRM 53-10-1 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 1999062500238 19990625 00238 NM 1999 6 25 UPS99229861 1 19990528 A 5754 RIB BOEING 727 72731C 1384011 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI SUSPECT CRACKS ON SLAT RIBS AT NR 4 SLAT ACTUATOR ATTACH POINT. REPLACED CRACKED RIBS IAW DRAWING NR 65-17276. 2 L 7 3 4F A3WE 1999062500239 19990625 00239 NM 1999 6 25 UPS99229862 1 19990528 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI AFT CARGO BAY CORROSION ON STRINGER 19 R AT BS 1080. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 A ND 51-10-02 AND DRAWING 65-18385. 2 L 7 3 4F A3WE 1999062500240 19990625 00240 NM 1999 6 25 UPS99229863 1 19990527 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI AFT CARGO BAY ANGLE ON FLOOR CHANNEL AT BS 1150 RBL 4 IS CRACKED ANGLE REPLACED IAW SRM 53-10-2 FIG 8. 2 L 7 3 4F A3WE 1999062500241 19990625 00241 NM 1999 6 25 UPS99229864 1 19990527 A 5320 CHANNEL BOEING 727 72731C 1384011 NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI AFT CARGO BAY FLOOR CHANNEL CRACKED AT BS 1070 LBL 3. REPAIRED CHANNEL IAW SRM 53-10-5 AND 53-10-2 FIG 8. 2 L 7 3 4F A3WE 1999062500242 19990625 00242 NM 1999 6 25 UPS99229865 1 19990527 A 5347 CARGO TRACK BOEING 727 72731C 1384011 NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI AFT CARGO BAY CARGO TRACK AT BS 1070 LBL 18 IS CRACKED. REPAIRED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1999062500243 19990625 00243 NM 1999 6 25 UPS99229866 1 19990602 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 380 & 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI STR CRACKED BS 380 AND 400 AT FRAME ATTACH POINTS RT SIDE. REPAIRED IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999062500244 19990625 00244 NM 1999 6 25 UPS99229868 1 19990527 A 5347 CARGO TRACK BOEING 727 72731C 1384011 NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI AFT CARGO BAY CARGO TRACK AT BS 1070 RBL 14 IS CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-5 FIG 5. 2 L 7 3 4F A3WE 1999062500245 19990625 00245 NM 1999 6 25 UPS99229869 1 19990527 A 5347 CARGO TRACK BOEING 727 72731C 1384011 NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI AFT CARGO BAY CARGO TRACK AT BS 1090 RBL 14 IS CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-5 FIG 5. 2 L 7 3 4F A3WE 1999062500246 19990625 00246 NM 1999 6 25 UPS99229870 1 19990525 A 5320 WINDOW FRAME BOEING 727 72731C 1384011 NM BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI MAIN CARGO DECK WINDOW FRAME STRUCTURE CRACKED AT BS 980 LEFT S11 WINDOW FRAME REPLACED IAW DWG NR 65-19851 NES SEAL FITTED REF MM 56-20-00. 2 L 7 3 4F A3WE 1999062500247 19990625 00247 NM 1999 6 25 UPS99229871 1 19990519 A 5320 651758866 CHORD BOEING 727 72725C 138400H NM BS 287 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) ON TOP CHORD OF F/E'S SEAT G-BEAM STA 287, LBL 9, RBL 11, WL 208 MARKED. REMOVED AND REPLACED CHORD ASSY AT STA 287, LBL 9, RBL 11, WL 208 PER SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1999062500248 19990625 00248 NM 1999 6 25 UPS99229872 1 19990617 A 2844 SWITCH BOEING 727 72725C 138400H NM NR1 FUEL TANK LEAKING A IPXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 01 946UP 19721 INSPECTION TYPE:SI, NR 1 FUEL QUANTITY ROLLED BACK AT TAKEOFF FROM 10500 TO 5000 LBS. AIRCRAFT CONTROL WAS DEGRADED. A LTERNATE FUEL FEED ESTABLISHED TO COMPENSATE FOR INBALANCE. FUEL UPLIFT IN GALLONS DID NOT SHOW ANY DISCREPANCIES. IN F LIGHT EMERGENCY DECLARED. NRC 944172 GENERATED. *S/D* TROUBLESHOT FUEL QTY INDICATING SYSTEM FOR NR 1 TANK. FOUND AL L 4 FUEL PRESS SWITCHES ON LEFT L/E LEAKING FUEL. DAMAGED WIRING AT NR 1 TANK BOSSING PLUS CONNECTOR D578P FUEL SOAKED AND WIRE W436-512-22 DAMAGED AT SM17. REPAIRED IAW 28-41-02, 28-43-01 AND MM 28-41-02. NR 1 TANK FUEL QTY INDICATION S YSTEM FUNCTIONAL TESTS GOOD. 2 L 7 3 4F A3WE 1999062500249 19990625 00249 EU 1999 6 25 QXEA9901278 1 19990607 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AIRFRAME SKIN CHAFED FROM FRAME 14285 TO 14755 WHERE PANEL 91BC WAS INSTALLED, AFT EDGE ENTIRE LENGTH. REPAIRED I AW HORIZON AIR EA 4-53-805. 2 L 7 2 4F RT A20EU 1999062500250 19990625 00250 EU 1999 6 25 QXEA9901279 1 19990607 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS A FUSELAGE SKIN CHAFE 18 LONG WHERE PANEL 92BD WAS MARKED. REPAIRED IAW HORIZON AIR EA 4-53-805. 2 L 7 2 4F RT A20EU 1999062500251 19990625 00251 EU 1999 6 25 QXEA9901280 1 19990606 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - OUTBOARD REAR ATTACH BRACKET, PANEL 81CE, HAS WORKING RIVETS AND LOOSE BRACKET. REPAIRED IAW HORIZON AIR EA 4-57-2 78. 2 L 7 2 4F RT A20EU 1999062500252 19990625 00252 EU 1999 6 25 QXEA9901281 1 19990609 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU PANEL WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - PANEL 82CE NEEDS TO BE REMOVED TO DETERMINE THE WEAR TOLERANCES ON ATTACHING HOLES. REPAIRED IAW HORIZON AIR EA 4 -57-279. 2 L 7 2 4F RT A20EU 1999062500253 19990625 00253 EU 1999 6 25 QXEA9901282 1 19990609 A 5720 MOUNT FOKKER F28 F28MK4000 4990810 EU LT WING LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT WING CANOE 81CE FORWARD MOUNT IS LOOSE. REPAIRED IAW HORIZON AIR EA 4-57-278. 2 L 7 2 4F RT A20EU 1999062500254 19990625 00254 EU 1999 6 25 QXEA9901283 1 19990610 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - SKIN CRACKED ACROSS RIVET ON UPPER WING SKIN, INSIDE PANEL 81X. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05 . 2 L 7 2 4F RT A20EU 1999062500255 19990625 00255 EU 1999 6 25 QXEA9901284 1 19990530 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 493US 11161 PDX - QUESTIONABLE REPAIR TO UPPER SURFACE OF RIGHT INBOARD FLAP JUST ABOVE PANEL 81AD. REPAIRED IAW FOKKER SRM 51-70, PARAGRAPH 3E, STEP 3. 2 L 7 2 4F RT A20EU 1999062500256 19990625 00256 EU 1999 6 25 QXEA9901285 1 19990604 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT INBOARD FLAP HAS A DENT IN UPPER SURFACE OF TRAILING EDGE, 30 OUTBOARD OF STATION 1700. REPAIRED IAW FOKKER SRM 51-70-0, PARAGRAPH 7E. 2 L 7 2 4F RT A20EU 1999062500257 19990625 00257 EU 1999 6 25 QXEA9901286 1 19990611 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AFT FUSELAGE FRAME 19976 CRACKED CLIP NEXT TO STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1999062500258 19990625 00258 EU 1999 6 25 QXEA9901287 1 19990529 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - SUPPORT LINK ASSEMBLY FOR LEFT SPEEDBRAKE HAS CHAFE DAMAGE NEAR LOWER ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4 -55-139. 2 L 7 2 4F RT A20EU 1999062500259 19990625 00259 EU 1999 6 25 QXEA9901288 1 19990611 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AFT FUSELAGE BETWEEN FRAMES 19976 AND 20075, ALONG STRINGER 39 SUSPECT CRACK. REPAIRED IAW HORIZON AIR EA 4-53-82 3. 2 L 7 2 4F RT A20EU 1999062500260 19990625 00260 EU 1999 6 25 QXEA9901289 1 19990611 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AFT FUSELAGE FRAME 19976 HAS CRACKED CLIP BETWEEN STRINGER 39-40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 4. 2 L 7 2 4F RT A20EU 1999062500261 19990625 00261 EU 1999 6 25 QXEA9901290 1 19990602 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AFT FUSELAGE OBLIQUE FRAME 16-2 HAS CRACKED CLIP BETWEEN STRINGERS 69-70. REPAIRED IAW MM 20-30-07, PAGE 203. 2 L 7 2 4F RT A20EU 1999062500262 19990625 00262 EU 1999 6 25 QXEA9901291 1 19990605 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - CORROSION ON OUTBOARD FLANGE OF C-CHANNEL OF FRAME 8305 BETWEEN STRINGER 30 AND 36. REPAIRED IAW FOKKER SRM 51-10 -4. 2 L 7 2 4F RT A20EU 1999062500263 19990625 00263 EU 1999 6 25 QXEA9901292 1 19990530 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 16660 CHAFED AT STRINGER 27 INBOARD FLANGE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH E1. 2 L 7 2 4F RT A20EU 1999062500264 19990625 00264 EU 1999 6 25 QXEA9901293 1 19990530 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 16060 CASTELLATION CRACKED AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999062500265 19990625 00265 EU 1999 6 25 QXEA9901294 1 19990611 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900 MISINSTALLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 50, A SECTION FROM FRAME 4900 TO SPLICE BETWEEN FRAMES 5805 AND 6305 IS INCORRECT THICKNESS FOR THIS LOCA TION. REPLACED STRINGER IAW HORIZON AIR EA 4-53-824. 2 L 7 2 4F RT A20EU 1999062500266 19990625 00266 EU 1999 6 25 QXEA9901295 1 19990525 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 12414 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 12414 HAS PIT/DIVOT 4 AFT OF STRINGER 41. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 5B, STEP 3 AN D SRM 51-10-4, PAGE 8, PARAGRAPH 3C, STEPS 1-2-3-4. 2 L 7 2 4F RT A20EU 1999062500267 19990625 00267 EU 1999 6 25 QXEA9901296 1 19990526 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - MID CABIN, STRINGER 38 HAS CORROSION AROUND HOLE, 5.5 AFT OF FRAME 11405 AT STATION 12853. REPAIRED IAW FOKKER SR M 51-10-04, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1999062500268 19990625 00268 EU 1999 6 25 QXEA9901297 1 19990528 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 5805 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - CASTELLATION FLANGE REMOVED TO FACILITATE STRINGER REPAIRED AT STRINGER 34 AND FRAME 5805. FABRICATED REPAIR ANGL E IAW FOKKER SRM 53-02-12, FIGURE 1. 2 L 7 2 4F RT A20EU 1999062500269 19990625 00269 EU 1999 6 25 QXEA9901298 1 19990530 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - CRACK AT INSULATION ATTACH HOLE ON STRINGER 46, FORWARD OF FRAME 7305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3. 2 L 7 2 4F RT A20EU 1999062500270 19990625 00270 EU 1999 6 25 QXEA9901299 1 19990520 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT OUTBOARD SEAT TRACK HAS 3 SMALL NICKS AND GOUGES BETWEEN FRAMES 14755 AND 15205. REPAIRED IAW FOKKER SRM 51- 10-04, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1999062500271 19990625 00271 EU 1999 6 25 QXEA9901300 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT OUTBOARD SEAT TRACK HAS CORROSION 4 AFT OF FRAME 7305 ON INBOARD AND OUTBOARD FLANGES. REPAIRED IAW FOKKER S RM 51-10-04, PAGE 8, PARAGRAPH 3, C4. 2 L 7 2 4F RT A20EU 1999062500272 19990625 00272 EU 1999 6 25 QXEA9901301 1 19990522 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT OUTBOARD SEAT TRACK HAS FRETTING CORROSION 3 AFT OF FRAME 6305, ON OUTBOARD FLANGE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999062500273 19990625 00273 EU 1999 6 25 QXEA9901302 1 19990601 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT OUTBOARD SEAT TRACK HAS A .5 INCH LONG GOUGE 7 FORWARD OF FRAME 6805 ON INBOARD FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-813. 2 L 7 2 4F RT A20EU 1999062500274 19990625 00274 NE 1999 6 25 QXEA9901365 2 19990615 A 7261 OIL SYS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE OVER SERVICED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 815PH 50 SEA - ACRID SMELL DURING LOW POWER DESCENT. MAINTENANCE FOUND EXTRA OIL IN NR 2 ENGINE, REMOVED OIL. OPERATIONAL AND E NGINE RUN CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999062500275 19990625 00275 NE 1999 6 25 QXEA9901366 2 19990615 A 7230 O RING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 COMPRESSOR FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 815PH 50 SEA - ACRID SMELL DURING DESCENT. SMELL STILL PRESENT WITH EITHER BLEED OFF. MAINTENANCE RAN AND FOUND OIL ON NR 1 COM PRESSOR BLADES AND INTAKE. FERRIED TO PDX. IN PDX, REPLACED O-RINGS ON NL PROBE. OPERATIONAL CHECKS GOOD AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999062500276 19990625 00276 NE 1999 6 25 QXEA9901367 2 19990616 A 7532 310848501 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MALFUNCTION A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 815PH 50 SEA - ACRID SMELL DURING LOW TO MODERATE POWER SETTINGS AT DESCENT. REPLACED NR 2 ENGINE P2.5/P3 SWITCHING VALVE. OPER ATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999062500277 19990625 00277 NM 1999 6 25 QXEA9901368 1 19990612 A 6120 M39016 RELAY DHAV DHC8 DHC8202 2809007 NM RELAY PANEL MALFUNCTION A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 361PH 516 SEA - DURING CLIMB WHEN AUTOFEATHER TURNED OFF, AUTOFEATHER ARM LIGHT BLINKED AND FLICKERED FOR 30 SECONDS. MAINTENANCE REPLACED 6121-K5 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999062500278 19990625 00278 NM 1999 6 25 99FDEA00222 1 19990617 A 2822 BOOST PUMP BOEING 727 7272S2F 1384O81 NM NR 2 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 208FE 22930 LEFT AFT TANK NR 2 BOOST PUMP FAILED. POPPED CIRCUT BREAKER WHILE IN FLT. RESET ONCE, FAILED AGAIN. *S/D* DRAINED FU EL BOOST PUMP AND CLEANED CANNON PLUG. OPER NR 2 FUEL TANK LEFT AFT BOOST PUMP PER MM 28-22-21. 2 L 7 3 4F A3WE 1999062500279 19990625 00279 NM 1999 6 25 99FDEA00223 1 19990617 A 3340 BULB BOEING 727 72722 1384002 NM NLG BROKEN A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 149FE 19087 99-133 AT ROTATION, NOSE WHEEL THUMPED, FIRE WARN BELL CAME ON. NO LIGHT ON. SUSPECT LOUD NOISE WAS TAXI BULB EXPLODI NG, REF WORK RELEASE ITEM 33-40/3122. TEST ENGINES, APU, AND WHEEL WELL FIRE ALARM SYS. NO DEFECTS NOTED, REF MM 26-11 -0 AND 26-15-1. 2 L 7 3 4F A3WE 1999062500280 19990625 00280 NM 1999 6 25 99FDEA00224 1 19990617 A 2611 SMOKE DETECTOR BOEING 727 727227 1384078 NM CARGO COMPT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 490FE 21493 CREW REPORTED NR 3 CARGO SMOKE DETECTOR LIGHT ON. MADE A TURN AROUND AND LANDED WITH NO INCIDENT. *S/D* CHANGED NR 3 SMOKE DETECTOR, MAIN CARGO SMOKE PANE AS PRECAUTION. REMOVED AND REPLACED SMOKE DETECTOR MODULE FOR PRECAUTION. CK GOO D PER MM 21-22-00. 2 L 7 3 4F A3WE 1999062500281 19990625 00281 WP 1999 6 25 ABXA9900842 1 19990622 A 5714 59124112 FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO BAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FITTING JUST BELOW CENTER WING TANK FRONT SPAR IN FORWARD LOWER CARGO COMPARTMENT CORRODED. REPLA CED FITTING IAW DC9 SRM 51-30-5 AND 51-20-0. 2 L 7 2 4F A6WE 1999062500282 19990625 00282 WP 1999 6 25 ABXA9900843 1 19990622 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN CORRODED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 953AX 47608 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. CLEANED CONTACTS ON BATTERIES IN POWER SUPPLY UNIT. 2 L 7 2 4F A6WE 1999062500283 19990625 00283 WP 1999 6 25 ABXA9900844 1 19990622 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 901AX 47381 CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH SWITCH IN ON POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES . 2 L 7 2 4F A6WE 1999062500284 19990625 00284 WP 1999 6 25 ABXA9900845 1 19990622 A 5312 991015519 BULKHEAD DOUG DOUG DC9 DC932F 3022067 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND THE FORWARD PRESSURE PANEL, LEFT FORWARD CORNER OF KEEL AREA FINGER DOUBLER CORRODED. REPLACED F INGER DOUBLER IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999062500285 19990625 00285 WP 1999 6 25 ABXA9900846 1 19990622 A 5320 99100787 WEB DOUG DOUG DC9 DC932F 3022067 WP BS 160 - 218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND WIDESPREAD CORROSION ON THE UPPER CARGO COMPARTMENT SUB FLOOR MEMBRANE, FROM STATION 160 TO 218 AN D LBL 54.5 AND RBL 54.5. REPLACED SUB FLOOR MEMBRANE IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999062500286 19990625 00286 WP 1999 6 25 ABXA9900487 1 19990423 A 5320 3754047502N FITTING DOUG DOUG DC8 DC863 302198A WP BS 1160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FITTING CRACKED INSIDE TORQUE BOX AT LONGERON 22 RIGHT AND STATION 1160. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500287 19990625 00287 WP 1999 6 25 ABXA9900488 1 19990423 A 5320 37515142N FITTING DOUG DOUG DC8 DC863 302198A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FLOORBEAM ATTACH FITTING CRACKED AT STATION 980 AND RBL 30. REPLACED FITTING IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1999062500288 19990625 00288 WP 1999 6 25 ABXA9900489 1 19990511 A 5510 56545108 ANGLE DOUG DOUG DC8 DC863 302198A WP RT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STATION XFS 103 LOWER RIB TIE. REPAIRED IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1999062500289 19990625 00289 WP 1999 6 25 ABXA9900490 1 19990511 A 5414 5769859513 SKIN DOUG DOUG DC8 DC863 302198A WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING NR 2 PYLON LEADING EDGE SKIN CRACKED AT STATION XS 250 UNDER THE UPPER SLOT DOOR. REPAIRED IAW DC8 SRM 57-3-3 . 2 L 7 4 4F 4A25 1999062500290 19990625 00290 WP 1999 6 25 ABXA9900491 1 19990511 A 5320 3779498504 FITTING DOUG DOUG DC8 DC863 302198A WP BS 902 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 18 LEFT INTERCOSTAL ATTACH FITTING CRACKED AT STATION 902. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500291 19990625 00291 WP 1999 6 25 ABXA9900492 1 19990515 A 5320 561537436 INTERCOSTAL DOUG DOUG DC8 DC863 302198A WP BS 1540 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 INTERCOSTAL CORRODED AT STRINGER 34 RIGHT, STATION 1540 TO 1560. REPAIRED IAW DWG 561537 AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999062500292 19990625 00292 WP 1999 6 25 ABXA9900493 1 19990515 A 5320 3755854502 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FITTING CRACKED STATION 1180 AND LONGERON 27 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500293 19990625 00293 WP 1999 6 25 ABXA9900494 1 19990515 A 5313 5615374 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1540-1560 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 35 RIGHT CORRODED AT STATION 1540 TO 1560. REPAIRED IAW DC8 SRM 53-4-1. 2 L 7 4 4F 4A25 1999062500294 19990625 00294 WP 1999 6 25 ABXA9900495 1 19990515 A 5313 37587301 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1540 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 33 LEFT CORRODED AT STATION 1540. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500295 19990625 00295 WP 1999 6 25 ABXA9900496 1 19990515 A 5320 57799361 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1510-1530 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FINGER DOUBLER CRACKED AT STATION 1510 TO 1530 AT LONGERON 31 LEFT. REPAIRED IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999062500296 19990625 00296 WP 1999 6 25 MWEA99349 1 19990615 A 5320 59122701 BEAM DOUG DC9 DC915 3022036 WP COCKPIT MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 900ME 45841 THE WEB BEAM AN DOUBLER BETWEEN CAPTAINS AND SLIDING CLEARVIEW WINDOW HAS A FIGURE 8 HOLE THROUGH ON FASTENER. MAINTENA NCE REMOVED AND REPLACED BEAM AND FABRICATED AND INSTALLED DOUBLER TEMPORARY REPAIR. 2 L 7 2 4F A6WE 1999062500297 19990625 00297 WP 1999 6 25 MWEA99350 1 19990618 A 5753 5910134137 SKIN DOUG DC9 DC914 3022034 WP LT TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 THE LEFT FLAP HAS DENT ON UPPER SURFACE AT XFLS 127. MAINTENANCE FABRICATED AND INSTALLED SKIN AND DOUBLER. 2 L 7 2 4F A6WE 1999062500298 19990625 00298 WP 1999 6 25 MWEA99351 1 19990618 A 5240 39536851 BEAM DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 THE GALLEY SERVICE DOOR HAS SEVERAL CRACKS IN BEAM NR 2 FORWARD SIDE. MAINTENANCE FABRICATED AND INSTALLED FITTING AND DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999062500299 19990625 00299 WP 1999 6 25 MWEA99352 1 19990618 A 5210 5910364 SKIN DOUG DC9 DC981 3022081 WP PASSENGER DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 PASSENGER AIRSTAIR COMPARTMENT DOOR HAS A DEEP GOUGE AT UPPER AFT AREA. MAINTENANCE FABRICATED AND INSTLLED NEW SKIN. 2 L 7 2 4F A6WE 1999062500300 19990625 00300 WP 1999 6 25 MWEA99353 1 19990618 A 5330 593600417 SKIN DOUG DC9 DC981 3022081 WP BS 760 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 803ME 48029 PREVIOUS REPAIR AT STATION 760 LONGERON 28R. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999062500301 19990625 00301 WP 1999 6 25 MWEA99354 1 19990618 A 5730 5935822503 SKIN DOUG DC9 DC981 3022081 WP WS 531 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 803ME 48029 PREVIOUS REPAIR ON LEFT WING LOWER SKIN AT XRS 531. MAINTENANCE FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 1999062500302 19990625 00302 NE 1999 6 25 DL757991337 2 19990613 A 7230 COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE TO TAKEOFF 1 SO 27 628DL 24574 22918 716577 NR 1 ENGINE SHUTDOWN DUE TO COMPRESSOR STALL. FOUND 10 STAGE COMPRESSOR DAMAGED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500303 19990625 00303 NM 1999 6 25 DLM88991338 1 19990614 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 900DE 53372 RTO FOR BURNING SMELL IN COCKPIT SPEED 120KTS. REPLACED WATER SEPARATOR BAGS. RAN ENGINES AND APU. ALL CKS OK. 2 L 7 2 4F RT A6WE 1999062500304 19990625 00304 NM 1999 6 25 DL757991339 1 19990513 A 5522 183N200330 SKIN BOEING 757 757232 1384965 NM RT ELEVATOR DELAMINATION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 624DL 22914 RT ELEVATOR LOWER L/E SKIN, FS 52, 112, 136, 160, 170 AND 220: DELAMINATION. MULTIPLE INTER-PLY DELAMINATION AREA S WERE FOUND AT THE ABOVE STATION LOCATIONS TYPICALLY AROUND HINGE-ATTACH BOLT HOLES IN THE LOWER L/E SKIN. AUTHORIZED TIME-LIMITED WET LAYUP REPAIRS. PERMANENT REPAIR TO BE SCHEDULED WITHIN NEXT 12 MONTHS. 2 L 7 2 4F RT A2NM 1999062500305 19990625 00305 NM 1999 6 25 DL72S991340 1 19990603 A 5311 FRAME BOEING 727 727232 1384082 NM BS 990 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FOUND DURING MV2 CORROSION VISIT NRC 213, CUT AND REMOVE FLOOR SUPPORT RAIL ABOVE STRINGER 29 LT STA 980 FOR ACCESS TO FRAME REPAIR (STA 990) REF NRC 128. REPAIRED PER SRM 53-10-5, WORKED WITH NRC 128, 93, 94. 2 L 7 3 4F A3WE 1999062500306 19990625 00306 NM 1999 6 25 DL72S991341 1 19990602 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 990 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FOUND DURING MV2 CORROSION VISIT NRC 128, CUT FRAME STA 990 TO ACCESS REPAIR OF STR 29 LT REF NRC 89. REPAIRED PER M/M 53-12-0 FIG 805. WORKED WITH NRC 93, 94, 213. 2 L 7 3 4F A3WE 1999062500307 19990625 00307 NM 1999 6 25 DL72S991342 1 19990601 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1000 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FOUND DURING MV2 CORROSION VISIT NRC 89, 1 IN CRACK STR 29 LT AT STA 1000. REPLACED STR 29 LT STA 980 TO STA 1007 PER S RM 53-10-11 FIG 3. WORKED WITH NRC 93, 94, 128, 213. 2 L 7 3 4F A3WE 1999062500308 19990625 00308 WP 1999 6 25 DLL10991343 1 19990614 A 3350 POWER SUPPLY 672320101 LKHEED 1011 10113851 5265010 WP R4 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 727DA 37857 193C1167 AFT CABIN EMERGENCY LIGHTS WOULD NOT REMAIN ON LONG ENOUGH DURING TEST. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AT T HE R4 DOOR POSITION AND THE EMERGENCY LIGHTS CHECKED NORMAL. 2 L 7 3 4F A23WE 1999062500309 19990625 00309 NM 1999 6 25 DL76G991345 1 19990614 A 3350 BPS73 POWER SUPPLY BOEING 767 7673P6 1385105 NM ROW 22-30 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1501P 24983 OVERHEAD EMERGENCY LIGHTS DIM FROM 20 AB TO 30 AB. FOUND BAD POWER SUPPLY M737. REMOVED AND REPLACED POWER SUPPLY IAW M/M, OPS CHK GOOD. 2 L 7 2 4F RT A1NM 1999062500310 19990625 00310 NM 1999 6 25 DLM11991346 1 19990614 A 3350 5519881 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 807DE 48478 DURING EMERGENCY LIGHT TEST, GOT NR 2 BAT LOW MESSAGE. 2 L 7 3 4F RT A22WE 1999062500311 19990625 00311 NM 1999 6 25 DLM11991347 1 19990614 A 3350 BATTERY PACK DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 807DE 48478 EMERGENCY LIGHTS TEST SHOWS BAT 2. ALL LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 BATTERY PACK. EMERGENCY LIGHTS TE ST PASS. ALL LIGHTS ILLUMINATED. 2 L 7 3 4F RT A22WE 1999062500312 19990625 00312 NM 1999 6 25 DLM88991348 1 19990614 A 2150 210017014 DUCT DOUG MD88 MD88 3023688 NM RT ACM FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 918DL 49583 ATB - AT FL240, AUTO PRESS INOP, BLUE LIGHT CAME ON. PRESSURE CONTINUED TO CLIMB AT 700 FT/MIN PASSING 5500 CN PRESSURE . INITIATED DESCENT TO 10000. AIRBORNE RETURN TO DFW. FOUND BLOWN DUCT ON RT ACM. REPLACED DUCT. CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1999062500313 19990625 00313 NM 1999 6 25 DL72S991349 1 19990615 A 7830 TR LIGHT BOEING 727 727225A 1384077 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE ILLUMINATED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 8890Z 50877 21859 700332 ON RUNWAY, NR 3 T/R OPERATING LIGHT CAME ON. CYCLED HANDLE LIGHT EXTINGUISHED. TAKEOFF TERMINATED. CHECKED NR 3 T/R. ALL CKS OK RAN NR 3 ENG, OPERATED NR 3 T/R. ALL CKS OK, ALL IND NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 1999062500314 19990625 00314 NM 1999 6 25 DL72S991350 1 19990615 A 5522 657274812 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 RIGHT ELEVATOR UPPER SKIN CRACKED DAMAGED APPROX .5 INCH, 24 INCHES OUTBD OF TAB. RIGHT ELEVATOR UPPER SKIN CRACKED .37 5 INCH APPROX 20 INCHES OUTBD OF TAB. REPAIRED PER ERA367622-14 CODE 4-55-21. 2 L 7 3 4F A3WE 1999062500315 19990625 00315 NM 1999 6 25 DL72S991351 1 19990615 A 2782 BRACKET BOEING 727 727232 1384082 NM LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 FOUND ON D1 LETTER CK, NR 6 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999062500316 19990625 00316 WP 1999 6 25 DLL10991352 1 19990612 A 5711 1503231105 SPAR LKHEED 1011 10113851 5265010 WP CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 FS 1163 CENTER WING INTERMEDIATE UPPER SPAR CAP WAS FOUND CRACKED IN THE RT OUTBOARD END NEAR RBL 116. REPAIRED PER ERA 367554-14, REV.A 2 L 7 3 4F A23WE 1999062500317 19990625 00317 NM 1999 6 25 DLM88991353 1 19990613 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM BS 229-269 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DL 49541 SEVERAL DENTS WERE FOUND IN THE FUSELAGE SKIN FROM STA 229 TO 269 AND BETWEEN L17L AND 18L. REPAIRED PER ERA 333232-14, REV. A. 2 L 7 2 4F RT A6WE 1999062500318 19990625 00318 NM 1999 6 25 DLM88991354 1 19990613 A 5330 595305069 SKIN DOUG MD88 MD88 3023688 NM BS 320 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DL 49541 LIGHTNING STRIKE DAMAGE WAS FOUND NEAR AN EXISTING REPAIR. EVALUATION OF LIGHTNING STRIKE REQUIRED THE FUSELAGE SKIN TO BE CUT OUT. BOTH DAMAGES ARE INCORPORATED INTO A NEW REPAIR. REPAIRED PER ERA 366417-14, REV B. 2 L 7 2 4F RT A6WE 1999062500319 19990625 00319 NM 1999 6 25 DLM88991355 1 19990613 A 5320 5936038501 JAMB DOUG MD88 MD88 3023688 NM BS 1174 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DL 49541 CORROSION FOUND AT THE C3 DOORWAY LWR DOOR JAMB BEAM. MOST BLENDS WERE WITHIN ALLOWABLE LIMITS, EXCEPT AT FS 1174. REP AIRED PER ERA 333204-14, REV A. 2 L 7 2 4F RT A6WE 1999062500320 19990625 00320 NM 1999 6 25 DLM88991356 1 19990614 A 5330 29524621 SKIN DOUG MD88 MD88 3023688 NM BS 408 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DE 49967 C1 DOOR CUTOUT FOUND WITH THREE SEPARATE GOUGES TO THE LWR SKIN. DAMAGE IS DEEP ENOUGH TO REQUIRE SKIN DAMAGE TO BE CUT OUT. REPAIRED PER ERA 333230-14, REV A. 2 L 7 2 4F RT A6WE 1999062500321 19990625 00321 NM 1999 6 25 DL72S991357 1 19990614 A 5330 655456414 SKIN BOEING 727 727232 1384082 NM BS 580 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 LFEC INSPECTIONS PER SI 4-74176-12AD, REV J ON S26L LAP JOINT FROM BS 481-681 YIELDED SEVERAL CRACK INDICATIONS. ACCOMP LISHMENT OF THE HFEC CONFIRMED 4 CRACKS IN THE LOWER LAP ROW IN THE OVERLAPPED (LWR) SKIN. REPAIRED PER ERA 367594-14AD , REV A. 2 L 7 3 4F A3WE 1999062500322 19990625 00322 NM 1999 6 25 DL757991358 1 19990616 A 5330 143N34719 SKIN BOEING 757 757232 1384965 NM BS 500 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 668DN 25141 DENT FOUND IN FUSELAGE SKIN AT BS 500 BELOW S26R. DAMAGE CUTOUT IS APPROX 4 BY 6. REPAIRED PER ERA 367513-14. 2 L 7 2 4F RT A2NM 1999062500323 19990625 00323 NM 1999 6 25 DL72S991359 1 19990616 A 5330 655458045 SKIN BOEING 727 727232 1384082 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 GOUGE FOUND IN FUSELAGE SKIN AT AFT EDGE OF THE C2 DOOR AT BS 990. DAMAGE AREA IS LOCATED AT S24R PLUS 5 AND IN THE SKI N ONLY. REPAIRED PER ERA 333244-14, REV A. 2 L 7 3 4F A3WE 1999062500324 19990625 00324 NM 1999 6 25 DL72S991360 1 19990616 A 5311 651593459 FRAME BOEING 727 727232 1384082 NM BS 620 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 FRAME AT BS 620 WAS FOUND CRACKED REMOVAL OF THE CRACK REQUIRED REMOVAL OF APPROX 5 OF THE UPPER FLANGE FROM THE PRODUCT ION SPLICE AT RBL 11 INBD TO RBL 6. REPAIRED PER ERA 333235-14. 2 L 7 3 4F A3WE 1999062500325 19990625 00325 NM 1999 6 25 DL72S991362 1 19990216 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 AFT SPAR RAIL DAMAGED AT 2ND FROM I/B AFT FLAP TRACK CUT OUT. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1999062500326 19990625 00326 NM 1999 6 25 DLM11991363 1 19990616 A 3520 OXY GENERATOR 80138683 DOUG MD11 MD11 3023602 NM SEAT 2A & 2B ACTIVATED A DALA G O2 MASK DEPLOYED O OTHER LD LANDING 1 SO 27 813DE 48600 MASK AT SEATS 2A AND 2B CAME DOWN ON LANDING GENERATORS ACTIVATED COULD SMELL IT. REPLACED GENERATOR AND REPACKED MASKS . 2 L 7 3 4F RT A22WE 1999062500327 19990625 00327 NM 1999 6 25 DLM88991364 1 19990615 A 4920 38005041 TURBINE DOUG MD88 MD88 3023688 NM APU FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 961DL 9604 49980 AFTER TRANSIT CHECK, THICK SMOKE IN CABIN WITH LT PACK RUNNING. REPLACED APU. CLEANED APU INLET ASSY. REPLACED COALES CER BAGS. PERFORMED DUCT BURNOUT. RAN PACKS, NO SMOKE OR ODORS. 2 L 7 2 4F RT A6WE 1999062500328 19990625 00328 NM 1999 6 25 DL757991365 1 19990616 A 3260 43467410332207 LIGHT BOEING 757 757232 1384965 NM RT MLG FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 652DL 24392 IN FLIGHT EMERGENCY DECLARED FOR RT MLG UNSAFE INDICATION. REPLACED ONE BULB AND MASSAGED THE GREEN GEAR LIGHT AND GOT A GOOD LOCKED INDICATION. DURING PROCEDURE ALTN GEAR EXTENSION WAS ACCOMPLISHED. FOUND RT MLG INDICATION LIGHT INTERMI TTENTLY INOP. REPLACED RT MLG LIGHT ASSY. GEAR GREEN INDICATIONS ALL NORMAL. 2 L 7 2 4F RT A2NM 1999062500329 19990625 00329 NM 1999 6 25 DL72E991366 1 19990616 A 2910 1240386CR0280 LINE BOEING 727 727247 138408F NM NLG WW LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 831WA 21483 ON TAKEOFF IMMEDIATELY AFTER SELECTING FLAPS TO 2 DEGREES FROM 5 DEGREES, EXPERIENCED A SYSTEM HYDRAULIC LOSS QTY AND PR ESSURE DECREASED RAPIDLY TO 0. SYSTEM B NORMAL THROUGHOUT. MAINTENANCE FOUND ACTUATOR LINE IN NLG WHEELWELL LEAKING. REPLACED LINE, SERVICED HYDRAULIC SYSTEM TO FULL, INSPECTED CASE DRAIN FILTERS ON ALL 3 ENGINES ALL OK. RAN ENGINES AND ALL FLIGHT CONTROLS. ALL HYDRAULIC SYSTEMS CHK OK. 2 L 7 3 4F A3WE 1999062500330 19990625 00330 NM 1999 6 25 DL76G991367 1 19990616 A 2121 219001621 FAN 219001621 BOEING 767 767324 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 394DL 1029639 27394 STRONG ELECTRICAL SMELL AROUND SEATS 35-37 F/G. FOUND AFT EQ EXHAUST FAN 1 EMITTING ELECTRICAL ODOR, REPLACED FAN. 2 L 7 2 4F RT A1NM 1999062500331 19990625 00331 NM 1999 6 25 DL72K991370 1 19990120 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED AT 35 FROM THE I/B END. THE COVE SKIN WAS REPAIRED BY INSTALLIN G A DOUBLER PER MM 57-52-0 FIG 809. 2 L 7 3 4F A3WE 1999062500332 19990625 00332 NM 1999 6 25 DL72S991371 1 19990616 A 5210 SKIN BOEING 727 727232 1384082 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 REF NRC 53 TPA LETTER CHECK C-1, .5 INCH CRACK IN R-1 DOOR SKIN AT LWR AFT CORNER. INSTALLED DOUBLER PER M/M 52-11-01, NR 8. 2 L 7 3 4F A3WE 1999062500333 19990625 00333 NM 1999 6 25 DL72S991372 1 19990616 A 5240 SKIN BOEING 727 727232 1384082 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 REF NRC 52 - TPA LETTER CHECK C-1, .5 INCH CRACK IN DOOR SKIN, R-1 DOOR LOWER FWD CORNER. INSTALLED DOUBLER PER M/M 52- 11-01, NR 8. 2 L 7 3 4F A3WE 1999062500334 19990625 00334 WP 1999 6 25 DLL19991373 1 19990616 A 2150 SENSOR LKHEED 1011 10113853 5265020 WP NR 2 PACK FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 754DL 193Y1181 ON DESCENT, SMOKE ODOR IN CABIN. NR 2 PACK COMPRESSOR DISCHARGE TEMP OFF SCALE HIGH. ACM TEMP 40 DEGREES. REPLACED CO MPRESSOR DISCHARGE TEMP SENSOR. 2 L 7 3 4F A23WE 1999062500335 19990625 00335 NM 1999 6 25 DL757991374 1 19990616 A 5330 146N31111 SKIN BOEING 757 757232 1384965 NM BS 1276 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 668DN 25141 FUSELAGE SKIN FS 1276, STRINGER 4R, LIGHTNING STRIKE REPAIR. THE FUSELAGE SKIN WAS STRUCK BY LIGHTNING AT FS 1276 AND S TRINGER 4R. THE DAMAGE WAS REMOVED FROM THE UPPER SKIN WITH AN APPROX 2 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERN AL ALUMINUM DOUBLER PER ER/A 367569-14, REV A. 2 L 7 2 4F RT A2NM 1999062500336 19990625 00336 NM 1999 6 25 DL72L991375 1 19990617 A 2497 BMS1331 WIRE BOEING 727 727232 1384082 NM NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITHNEW TYPE CABLES BMS 13-58 D. P/N 012210733 PER BOEING SER VICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999062500337 19990625 00337 NM 1999 6 25 DL72L991376 1 19990617 A 2497 BMS1331 WIRE BOEING 727 727232 1384082 NM NR 3 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITHNEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERV ICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999062500338 19990625 00338 NM 1999 6 25 DLM88991377 1 19990617 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 987DL 53338 ATB - RIGHT AFT LAV SMOKE ALARM SOUNDED SHORTLY AFTER TAKEOFF F/A REPORTED MUSTY SMELL AND FAINT HAZE IN AFT CABIN FAINT SMELL WAS ALSO PRESENT IN COCKPIT. RAN A/C DUCT BURNOUT PER M/M AND REPLACED BOTH WATER SEPARATOR BAGS. RAN ENG CHECK S GOOD. 2 L 7 2 4F RT A6WE 1999062500339 19990625 00339 NM 1999 6 25 DL72E991379 1 19990617 A 5754 BRACKET BOEING 727 727247 138408F NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON A1 LETTER CK, NR 8 SLAT INBD MOUNT BRACKET CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999062500340 19990625 00340 NM 1999 6 25 DL72K991380 1 19990617 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM R1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA 21232 EMERGENCY EXIT LIGHT AT R1 DOOR INOP. REPLACED EMERGENCY LIGHT ASSEMBLY AT R1 DOOR, OPS NORMAL. 2 L 7 3 4F A3WE 1999062500341 19990625 00341 NM 1999 6 25 DL757991381 1 19990617 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM BS 1690-1700 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 668DN 25141 FUSELAGE SKIN FS 1690-1710, STRINGER18L, DENT REPAIR. THE FUSELAGE SKIN WAS DENTED JUST BELOW STRINGER 18L BETWEEN FS 1 690 AND FS 1710. THE DAMAGE WAS REMOVED WITH TWO SKIN CUTOUTS. THE CUTOUTS WERE REPAIRED WITH AN EXTERNAL ALUMINUM DOU BLER PER ER/A 367505-14, REV C. 2 L 7 2 4F RT A2NM 1999062500342 19990625 00342 NM 1999 6 25 DL72S991382 1 19990617 A 5320 655612910 SILL BOEING 727 727232 1384082 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FUSELAGE C2 DOOR SURROUND LOWER SILL OUTBD CHORD, CORROSION REPAIR. THE OUTBOARD CHORD OF THE C2 DOOR OPENING LOWER SIL L WAS FOUND CORRODED ON THE OUTBD FLANGE BETWEEN FS 950F+11 AND FS 960. THE CORROSION WAS BLENDED AWAY WITH A MAXIMUM D EPTH OF .075. THE DAMAGE WAS REPAIRED WITH AN ALUMINUM STRAP PER ER/A 367596-14, REV A. 2 L 7 3 4F A3WE 1999062500343 19990625 00343 NM 1999 6 25 SCNA99084 1 19990616 A 5610 WINDOW BOEING 727 7272A1 138407F NM RT COCKPIT LEAKING A SCNA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 287SC 21345 DURING CLIMB-OUT, THE FIRST OFFICER'S R2 SLIDING WINDOW DEVELOPED AN AIR LEAK. RETURNED AIRCRAFT TO MKE. FOUND OBSTRUC TION IN THE R2 WINDOW TRACK. REMOVED OBSTRUCTION THAT WAS SEATED IN WINDOW TRACK. PRESSURIZED AIRCRAFT AND OPERATIONAL LY CHECKS GOOD IAW MM 560000. 2 L 7 3 4F A3WE 1999062500355 19990625 00355 SW 1999 6 25 99ZZZX2350 1 19990527 A 7920 31035781 LINE SWRNGN SA227 SA227AC 8780603 SW ENGINE OIL CHAFED A VPOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 27 2728G AC731 DURING FLIGHT FROM ISN TO MOT, PILOT NOTICED FLUCTUATING OIL PRESSURE, THEN OIL PRESSURE DROPPED BELOW THE YELLOW ARC. P ILOT SHUT DOWN THE ENGINE, LANDING WITHOUT INCIDENT. FOUND OIL LINE FROM NTS TEE TO GEARBOX HAD CHAFED THROUGH ON ANOTH ER OIL LINE. SHOULD HAVE BEEN DISCOVERED DURING PHASE INSPECTION. 2 L 7 2 4T RT A8SW 1999062500357 19990625 00357 EU 1999 6 25 99ZZZX2352 1 19990607 A 2497 1P15B6 WIRE ISRAEL 1124 1124 4500102 EU CABIN CHAFED A MCIA O OTHER O OTHER NR NOT REPORTED 1 WP 11 911CU 246 PILOT REPORTED LOSS OF NR 1 GENERATOR. T/S REVEALED NR 1 GCU FAILED. DURING INSP, FOUND NR 1 COMM AND ACC BUSS HAD 28 VOLTS WITH OR WITHOUT NR 1 AVIONICS SWITCH CLOSED. POWER FOUND ON BOTH SIDES OF RCB1-1 REGARDLESS OF SWITCH POSITION. WITH WIRES DISCONNECTED FROM PINS L1 AND T1, 28V WAS STILL PRESENT AT WIRE NR 1P15A6. MOVING TO TERMINAL STRIP 'AC', B OTH WIRES DISCONNECTED, 28V WAS FOUND AT WIRE 1P15B6 AND NR 1 COMM AND ACC BUSS STILL HOT. WITH WIRE NR 1P15B6 DISCONNE CTED FROM T-STRIP 'AC' AND NR 1 COMM AND ACC BOSS, 28V WAS PRESENT AT BOTH ENDS OF WIRE. 2 M 7 2 4F A2SW 1999062500380 19990625 00380 CE 1999 6 25 99ZZZX2375 1 19990601 A 3246 5030001087 WHEEL HALF BFGOODRICH 50300010133 BEECH 90 E90 1152914 CE MLG CRACKED A F2PA K NONE O OTHER IN INSP/MAINT 1 SO 17 701X 2500 LA0568 LW165 PERFORMED DRY PENETRANT INSPECTION ON WHEEL HALVES PER BF GOODRICH MM, PARA 2 PAGE 501 REV 1/86. FOUND CRACK STARTING I NSIDE TIE BOLT-HOLE EXTENDING OUTWARD IN TWO DIRECTIONS PAST THE WHEEL HALF PACKING GROOVE. CRACK WAS FOUND IN ONE TIE- BOLT HOLE ONLY. ALL TIE-BOLT HOLES HAD CORROSION PITS AROUND SURFACE (INSIDE, MATING SURFACE). CRACK MAY HAVE BEEN DUE TO AGE, PERHAPS WHEEL HALVES SHOULD BE LIFE-LIMITED OR MANDATORY NDI AT CERTAIN HOUR INTERVALS. 1 L 7 2 3T 3A20 1999062500400 19990625 00400 CE 1999 6 25 99ZZZX2396 1 19990601 A 3222 12434262 TORQUE LINK CESSNA 210 210L 2073448 CE NLG CRACKED A DFJA K NONE O OTHER IN INSP/MAINT 1 CE 03 50DB 8504 21060107 DURING A ROUTINE INSPECTION, FOUND NOSE GEAR UPPER TORQUE LINK, P/N 1243426-2, CRACKED. PREVIOUS NOSE WHEEL SHIMMY WAS REPORTED AND STEERING COLLAR SHIMMY WAS REPORTED AND STEERING COLLAR SHIMS AND SHIMMY DAMPENER WERE RE-SEALED. 1 H 7 1 3O 3A21 1999062500406 19990625 00406 SO 1999 6 25 LR7A9951 1 19990614 A 5230 SHELF LKHEED 382 382G 526414U SO BS 10.4 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 CARGO RAMP ASSY RAMP STA 10.4 SHELF CRACKED AND DENTED AT LBL 35 TO LBL 37. REPAIRED IAW SMP 583 51-140-12. 2 H 7 4 4T A1SO 1999062500407 19990625 00407 NM 1999 6 25 PCAA9900019 1 19990617 A 2731 82760174005 ACTUATOR DHAV DHC8 DHC8102 2809003 NM LT ELEV TRIM BINDING A PCAA K NONE F FLT CONT AFFECTED CR CRUISE 1 EA 13 806EX 263 FLT 3796-BDL-ROC: MANUAL & STANDBY ELEVATOR TRIM JAMMED ON DESCENT OUT OF FLIGHT LEVEL 18,000 & UNJAMMED AT 11,000. EL EVATOR HORN HEAT ON THE ENTIRE TIME. ON GROUND WHEN RUNNING THROUGH TRIM RANGE, SNAGS AT FORWARD POSITION. MISTRIM NOS E DOWN INDICATION ON ID802 PANEL. MAINTENANCE TROUBLESHOT SYSTEM, FOUND THE LEFT ELEVATOR TRIM TAB ACTUATOR BINDING. R EMOVED AND REPLACED TRIM ACTUATOR, SYSTEM CHECKED GOOD IAW DHC M/M CHAPTER 27. 2 H 7 2 4T RT A13NM 1999062500408 19990625 00408 NM 1999 6 25 PCAA9900020 1 19990618 A 2611 SMOKE LIGHT DHAV DHC8 DHC8102 2809003 NM BAGGAGE COMPT ILLUMINATED A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 839EX 226 FLT 3800 - BDL AFTER TAKEOFF THE BAGGAGE SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOU T INCIDENT. MAINTENANCE INSPECTED BAG BAY, NO EVIDENCE OF SMOKE OR FIRE, CLEANED ELECTRICAL CONNECTORS, RAN AIRCRAFT WI TH ENGINE BLEEDS ON, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 1999062500409 19990625 00409 NE 1999 6 25 CALA9900710 2 19990618 A 7310 9122M12G01 FUEL LINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE BROKEN A CALA A UNSCHED LANDING K X FLUID LOSS ENGINE FLAMEOUT CR CRUISE 1 SW 09 19072 46576 530114 THE NR 3 ENGINE FLAMED OUT DUE TO LOSS OF FUEL FLOW WHILE EN ROUTE FROM GUM TO HNL. ALL OTHER ENGINE PARAMETERS WERE IN NORMAL RANGE AT TIME OF FAILURE. THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE EDUCTOR VALVE SIGNAL BLEED TUBE TO FUEL FLOW TRANSMITTER FUEL LINE BROKEN AT B-NUT TO UNION FITTING. T HE LINE WAS REMOVED AND REPLACED IAW MM 73-14-01, PAGE 205, ITEM 11. LEAK CHECKS WERE GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1999062500410 19990625 00410 WP 1999 6 25 CALA9900711 1 19990620 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 294 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED AT STA 294 ON LT SIDE JUST FORWARD OF CABIN OUTFLOW VALVE, LONGERON 25L. A REPAIR WAS INSTALLED IAW ECRA 5330-02377. 2 L 7 2 4F A6WE 1999062500411 19990625 00411 SO 1999 6 25 COA9910095 1 19990617 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 266CA 120258 EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999062500412 19990625 00412 NM 1999 6 25 UPS99229873 1 19990618 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 705 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 705 TO BS 708 RBL 95 WL 208. REPLACED TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999062500413 19990625 00413 NM 1999 6 25 UPS99229874 1 19990618 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 630-638 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 630 TO BS 638 RBL 45. REPLACED PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999062500414 19990625 00414 NM 1999 6 25 UPS99229875 1 19990616 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 690 LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10 -5 PG 4. 2 L 7 3 4F A3WE 1999062500415 19990625 00415 NM 1999 6 25 UPS99229876 1 19990617 A 5320 69436832 SHEAR TIE BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, SHEAR TIE CORRODED BS 720 FRAME BETWEEN 25 AND 26 RT. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30- 2 PG 2. 2 L 7 3 4F A3WE 1999062500416 19990625 00416 NM 1999 6 25 UPS99229877 1 19990604 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 474 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C & SI, E & E BAY CRACK ON FLOOR SUPPORT ANGLE BS 474 OVER STRINGER 26R. ANGLE REPLACED IAW SRM 53-10-2 FIG 7. 2 L 7 3 4F A3WE 1999062500417 19990625 00417 NM 1999 6 25 UPS99229878 1 19990604 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, E & E BAY CRACK ON FLOOR SUPPORT ANGLES AT BS 380 OVER STRINGER 25R. REPAIRED IAW SRM 51-40-3 FIG 1 AND REPROTECTED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 1999062500418 19990625 00418 NM 1999 6 25 UPS99229879 1 19990604 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 448 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SUSPECT CRACK ON STRINGER 21R NESTING SECTION AT BS 448 APPROX. NESTING SECTION REPLACED IAW S RM 53-10-02. 2 L 7 3 4F A3WE 1999062500419 19990625 00419 NM 1999 6 25 UPS99229880 1 19990604 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 448 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SURFACE CORROSION ON STRINGER 23R NESTING SECTION AT BS 448 APPROX. NESTING SECTION REPLACED I AW SRM 53-10-02 FIG AND SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999062500420 19990625 00420 NM 1999 6 25 UPS99229881 1 19990602 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SUSPECT CRACK AT STR 25 RT BS 420 AT FRAME ATTACH POINT ON STRINGER LWR FASTENER HOLE. STRINGE R REPAIRED IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999062500421 19990625 00421 NM 1999 6 25 UPS99229882 1 19990602 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 380-420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, STRINGER 23 CRACKED BS 380, 400 AND 420 AT FRAME ATTACH POINTS LT SIDE. STRINGER REPAIRED IAW 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999062500422 19990625 00422 NM 1999 6 25 UPS99229884 1 19990601 A 5320 SPLICE BOEING 727 72731C 1384011 NM BS 480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, CRACK ON AFT OF STRINGER SPLICE ON STR 28L BS 480. STRINGER SPLICE REPLACED IAW SRM 53-10-02 F IG 9 AND SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999062500423 19990625 00423 NM 1999 6 25 UPS99229885 1 19990528 A 5320 BEAM BOEING 727 72731C 1384011 NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, CRACK FOUND ON LONGITUDINAL BEAM IN KEEL AREA LT SIDE BS 930 WL 160 APPROX. NEW BEAM FABRICATE D IAW FRG NR 65-28900, BEAM INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999062500424 19990625 00424 NM 1999 6 25 UPS99229886 1 19990528 A 5320 BEAM BOEING 727 72731C 1384011 NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, CRACK FOUND ON LONGITUDINAL BEAM IN KEEL AREA RT SIDE BS 930 WL 160 APPROX. NEW BEAM FABRICATE D IAW DRG NR 65-28900, NEW BEAM INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999062500425 19990625 00425 NM 1999 6 25 UPS99229887 1 19990527 A 5320 CHANNEL BOEING 727 72731C 1384011 NM BS 1130 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, AFT CARGO BAY FLOOR CHANNEL CRACKED AND DENTED AT BS 1130 RBL 9. FLOOR CHANNEL REPAIRED IAW SR M 53-10-05 FIG 4 & SRM 53-10-2. 2 L 7 3 4F A3WE 1999062500426 19990625 00426 NM 1999 6 25 UPS99229888 1 19990601 A 5730 PANEL BOEING 727 72731C 1384011 NM NR 1 FUEL TANK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, RT WING NR 1 FUEL TANK ACCESS PANEL CORRODED AND CRACKED. REPLACED NR 1 FUEL TANK ACCESS PANEL IAW MM 20-8-11. 2 L 7 3 4F A3WE 1999062500427 19990625 00427 NM 1999 6 25 UPS99229889 1 19990525 A 5753 FLAP TRACK BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, PITTING CORROSION ON NR 1 FLAP TRACK O/B FACE ALONG ROLLER MATING SURFACE. REPLACED FLAP TRACK IAW MM 27-51-31. 2 L 7 3 4F A3WE 1999062500428 19990625 00428 NM 1999 6 25 UPS99229897 1 19990619 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT ON FLIGHT DECK INOP. REMOVED AND REPLACED BATT PACK, LIGHT CHECKS GOOD. 2 L 7 3 4F A3WE 1999062500429 19990625 00429 NM 1999 6 25 UPS99229898 1 19990619 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP ON FLIGHT DECK. REMOVED AND REPLACED BATTERY PACK, LIGHT CHECKS GOOD. 2 L 7 3 4F A3WE 1999062500430 19990625 00430 NM 1999 6 25 99FDEA00225 1 19990618 A 3610 VALVE BOEING 727 727247 138408F NM NR 1 ENGINE INOPERATIVE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION UK UNKNOWN 1 SO 25 237FE 21331 NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. NR 1 ENG WAS PROVIDING BLD FOR LEFT DUCT PRESSURE WHICH WAS 20 PSI HIGHER THAN RIGHT DUCT. REMOVED AND REPLACED NR 1 ENGINE HIGH PRESSURE MODULATING AND SHUTOFF VALVE PER MM 36-12-42 PG 401 AN D 402. LEAK AND OPER CHECK NORM. RAN 1 AND 3 ENGINE TOGETHER WITH BOTH PACKS ON AT APPROX 65 TO 70 PERCEN, N2 LT AND R T DUCT PRESSURE WAS EQUAL AND STEADY. 2 L 7 3 4F A3WE 1999062500431 19990625 00431 NM 1999 6 25 99FDEA00226 1 19990619 A 3610 CLAMP BOEING 727 727247 138408F NM NR 1 ENGINE FAILED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 237FE 21331 ENGINE 1 STRUT OVERHEAT LIGHT ILLUM. FOLLOW RED TAB PROCEDURE. REMOVED AND REPLACED FWD (UPSTREAM) CLAMP ON ENGINE BLD AIR SHUTOFF VALVE PER MM 36-10-001-4, MM 20-80-001-2, FIG 209. 2 L 7 3 4F A3WE 1999062500432 19990625 00432 NM 1999 6 25 99FDEA00227 1 19990619 A 7931 ST104Z TRANSMITTER BOEING 727 72725 1384006 NM NR 2 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 504FE 18274 LOSS OF NR 2 OIL PRESSURE IN FLT TO BELOW 20 PSI WITH NR 2 OIL PRESSURE LIGHT. REMOVED AND REPLACED NR 2 ENGINE OIL PRE SSURE TRANSMITTER PER MM 79-32-001-4. 2 L 7 3 4F A3WE 1999062500433 19990625 00433 WP 1999 6 25 ABXA9900497 1 19990519 A 5300 97558847 FRAME DOUG DOUG DC8 DC863 302198A WP BS 1080 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FRAME CAP AT STATION 1080 EXFOLIATED AT LONGERON 34 RIGHT. REPAIRED IAW DC8 SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F 4A25 1999062500434 19990625 00434 WP 1999 6 25 ABXA9900498 1 19990518 A 5320 57577781 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1650 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 33 RIGHT END FITTING BROKEN AT STATION 1650. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F 4A25 1999062500435 19990625 00435 WP 1999 6 25 ABXA9900499 1 19990518 A 5320 9755536501 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT LOWER CUSP TO FRAME FITTING CRACKED AT STATION 1280. REPLACED FITTING IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1999062500436 19990625 00436 WP 1999 6 25 ABXA9900500 1 19990518 A 5414 57547014 SKIN DOUG DOUG DC8 DC863 302198A WP NR 4 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 NR 4 PYLON UPPER SKIN TRAILING EDGE CRACKED AT STATION XFS 532. REPAIRED IAW ABX REA NR D857-27903MR. 2 L 7 4 4F 4A25 1999062500437 19990625 00437 WP 1999 6 25 ABXA9900501 1 19990512 A 5320 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1360 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FINGER DOUBLER CRACKED AT LONGERON 31 LEFT AND STATION 1360. REPAIRED IAW ABX NR REA D853-27314MR. 2 L 7 4 4F 4A25 1999062500438 19990625 00438 WP 1999 6 25 ABXA9900502 1 19990616 A 3260 UPLATCH ROLLERS DOUG DC9 DC941 302207N WP RT MLG OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 954AX 47612 RIGHT MAIN LANDING GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER TAKEOFF. RECYCLED GEAR, LIGHT REMAINED ON. ADJUSTED SH IMS ON RIGHT MAIN LANDING GEAR UPLATCH ROLLERS IAW DC9 MM 32-31-4. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999062500439 19990625 00439 WP 1999 6 25 ABXA9900503 1 19990521 A 5315 575499101 FLOORBEAM DOUG DOUG DC8 DC863 302198A WP BS 1320 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FLOORBEAM CORRODED AT STATION 1320, LBL 24 TO RBL 24. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999062500440 19990625 00440 WP 1999 6 25 ABXA9900504 1 19990521 A 5730 57547013 SKIN DOUG DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING LEADING EDGE ABOVE NR 1 PYLON SKIN CRACKED ON LOWER SIDE. REPAIRED IAW DC8 SRM 57-2-1A. 2 L 7 4 4F 4A25 1999062500441 19990625 00441 WP 1999 6 25 ABXA9900505 1 19990521 A 5320 SR085300931 STRAP DOUG DOUG DC8 DC863 302198A WP BS 1160-1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 HEAVY CORROSION ON STRAP FROM STATION 1160 TO 1220 AT LONGERON 29 LEFT. REPAIRED IAW ABX REA D853-27321MR. 2 L 7 4 4F 4A25 1999062500442 19990625 00442 WP 1999 6 25 ABXA9900506 1 19990521 A 5320 5615377201 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1660-1680 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 INTERNAL FINGER DOUBLER CORRODED, STATION 1660 TO 1680 AT LONGERON 31 LEFT. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 561537 7. 2 L 7 4 4F 4A25 1999062500443 19990625 00443 WP 1999 6 25 ABXA9900507 1 19990521 A 5320 9755584508 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1290 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT LOWER FRAME TO CUSP FITTING CRACKED AT STATION 1290. REPLACED FITTING IAW DC8 SRM 51-1-20D AND SRM 53-1-0. 2 L 7 4 4F 4A25 1999062500445 19990625 00445 CE 1999 6 25 99ZZZX2403 1 19990608 A 3230 084012515 ROD CESSNA 310 310R 2074245 CE RT MLG FAILED A BSYA O OTHER O OTHER LD LANDING 1 GL 07 37575 310R1207 RIGHT GEAR COLLAPSED ON LANDING GOING INTO DES MOINES (DSM). RETRACT/EXTEND ROD END BROKE LETTING GEAR COLLAPSE. 1 L 7 2 3O 3A10 1999062500446 19990625 00446 NM 1999 6 25 99ZZZX2404 1 19990526 A 3231 4000088001 BELLCRANK PIPER PA60 PA60600 7106001 NM MLG DOOR FAILED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 7512S 6000144064 RIGHT MAIN GEAR DOOR BELLCRANK BROKEN NOT LETTING GEAR GO UP. REMOVED AND REPLACED BELLCRANK, CYCLES GEAR SEVERAL TIMES . OPS CHECKS GOOD. 1 M 7 2 3O RT A17WE 1999062500447 19990625 00447 NM 1999 6 25 99ZZZX2405 1 19990511 A 3233 450590001 ACTUATOR PIPER PA60 PA60600 7106001 NM NLG FAILED A BSYA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 6076L 600713796122 CLT - NOSE GEAR COLLAPSED ON LANDING. NOSE GEAR RETRACT CYLINDER NOT LETTING NOSE GEAR COME DOWN AND LOCK. REMOVED AND REPLACED NOSE GEAR ACTUATOR. OPS CHECK GOOD. INSTALLED SERVICEABLE GEARS AND FERRIED TO CMH. 1 M 7 2 3O RT A17WE 1999062500448 19990625 00448 NM 1999 6 25 99ZZZX2406 1 19990520 A 5610 WINDSHIELD PIPER PA60 PA60600 7106001 NM COCKPIT LEAKING A BSYA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 07 6896B 600919816126 AFTER TAKEOFF OUT OF BDL IN HEAVY RAIN, PILOT NOTICED WINDSHIELD LEAKING WATER ON HIS FEET. RETURNED TO BDL. MAINTENAN CE RE-SEALED WINDSHIELD PER MM. 1 M 7 2 3O RT A17WE 1999062500449 19990625 00449 SO 1999 6 25 99ZZZX2407 1 19990519 A 3260 SWITCH PIPER PA31 PA31350 7103110 SO MLG CONTAMINATED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 35551 31052063 RIGHT GEAR NOT SHOWING DOWN AND LOCK INDICATION, LANDED AT CVG. MECHANIC CLEANED AND LUBED SWITCH, FERRIED TO LUK GEAR DOWN. JACKED AIRCRAFT, CYCLED GEAR. OPS CHECKED GOOD. 1 L 7 2 3O A20SO 1999062500450 19990625 00450 CE 1999 6 25 99ZZZX2408 1 19990514 A 7602 5038901223 CONTROL CABLE BEECH 58 58 1152740 CE MIXTURE CONTROL BROKEN A BSYA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 GL 07 4098S TH600 RIGHT ENGINE SHUT DOWN IN-FLIGHT. LANDED IN ZZV, FOUND MIXTURE CABLE BROKEN. SAFTIED MIXTURE FULL RICH, FERRIED TO CMH . REMOVED AND REPLACED CABLE. 1 L 7 2 3O 3A16 1999062500451 19990625 00451 CE 1999 6 25 99ZZZX2409 1 19990511 A 3230 MS25125E3 SWITCH BEECH 58 58 1152740 CE MLG FAILED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 27MT TH1120 CMH - GEAR DID NOT COME DOWN WHEN FIRST SELECTED. RECYCLED, OPS OK. REMOVED AND REPLACED SELECTOR SWITCH. OPS CHECK O OD. 1 L 7 2 3O 3A16 1999062500467 19990625 00467 WP 1999 6 25 TWAA9908501 1 19990618 A 3350 58222 BATTERY PACK DOUG DC9 DC931 3022065 WP ROW 7-14 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 989Z 47135 FOUND CABIN EGRESS LIGHTS INOPERATIVE FROM ROW 7 TO 14, AND ROW 22 TO AFT CABIN. ACCOMPLISHED A SPLICE TO A CUT FEEDER CABLE FOR ROWS 7 TO 9. REPLACED A FLEX FEEDER LINE (P/N 5853-1) FOR ROW 9 TO 14, AND REPLACED THE BATTER PACK FOR THE A FT CABIN. CHECK-C 6-25-98 STL. 2 L 7 2 4F A6WE 1999062500468 19990625 00468 NM 1999 6 25 TWAA9908502 1 19990620 A 3350 582243 BATTERY PACK BOEING 767 767205 1385121 NM ROW 10-15 DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 651TW 23058 THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 10 TO 15. REPLACED THE BATTERY PACK. CHECK-C 4-7-99 LAX. 2 L 7 2 4F RT A1NM 1999062500469 19990625 00469 NE 1999 6 25 TWAA9908503 2 19990620 A 7314 3782017 FUEL PUMP BOEING 727 727231 1384079 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE WORN A TWAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 CE 05 54349 21968 1504 SHORTLY AFTER APPLYING POWER DURING A GO-AROUND AT DTW, THE NUMBER 1 ENGINE FLAMED OUT. ATTEMPTED RESTART WAS NOT SUCCE SSFUL. THE ENGINE WAS SHUT DOWN AND LANDING WAS MADE AT DTW. IT APPEARED THE FUEL PUMP SHAFT WAS SHEARED. THE FUEL PU MP AND FUEL CONTROL (P/N 743602-5), WAS REPLACED. CHECK-C 10-18-98 MCI. 2 L 7 3 4F 4 F A3WE E2EA 1999062500470 19990625 00470 NM 1999 6 25 RAAA99B2047 1 19990620 A 5280 65216361 DOOR BOEING 727 72722C 138400F NM LG MLG MISSING A RAAA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 AL 03 832RV 19098 AFTER LANDING AT UHPP FOUND LT MLG WING DOOR MISSING FROM AIRCRAFT. INSPECTION REVEALED THE FOLLOWING DOOR HINGES SHEAR ED AT HINGE LINE. DOOR ACTUATING ROD NOT DAMAGED, ACT ROD TO WING DOOR ATTACH BOLT MISSING, WING PANEL NR 1 HAD ONE 8 I NCH LONG GOUGE .375 INCH DEEP, WNG PANEL NR 2 HAS ONE 6 INCHES LONG .375 INCH DEEP GOUGE. AIRCRAFT FERRIED TO ANC MAINT ENANCE BASE. DOOR REPLACEMENT AND REPAIRS IN PROGRESS. SUBMITTER STATES, DOOR ACTUATING ROD TO WING DOOR ATTACH BOLT F AILED CAUSING DOOR TO OPEN AND DEPART THE AIRCRAFT. 2 L 7 3 4F A3WE 1999062500471 19990625 00471 SO 1999 6 25 RAAA99E9022 1 19990619 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 12 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1999062500472 19990625 00472 WP 1999 6 25 9902089962 1 19990618 A 3231 MECHANISM DOUG DC9 DC931 3022065 WP NLG DOOR NOT LATCHED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 914RW 47362 VIBRATION FROM NOSE GEAR AREA OCCURRED AFTER GEAR RETRACTION ON TAKEOFF. CREW RECYCLED GEAR WITH SAME RESULTS. FLIGHT WAS RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CREW DECLARED AN EMERGENCY DUE TO OVERWEIGHT LANDING CONDTIONS. MAINT ENANCE FOUND RIGHT NOSE GEAR DOOR NOT PROPERLY LATCHED AT SNUBBER. RESECURED DOOR. 2 L 7 2 4F A6WE 1999062500473 19990625 00473 NM 1999 6 25 9902096625 1 19990616 A 3232 608002304 ACTUATOR BOEING 747 747251B 1384892 NM NLG DOOR FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 625US 28513 1072 21707 DURING APPROACH, THE NOSE LANDING GEAR WOULD NOT EXTEND. RECYCLED THE LANDING GEAR AND GEAR EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999062500474 19990625 00474 WP 1999 6 25 9902109885 1 19990616 A 3350 BATTERY DOUG DC9 DC951 3022051 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 401EA 47682 FLIGHT CREW REPORTED EMERGENCY LIGHTING INOPERATIVE OR DIM IN TAIL CONE AREA. MAINTENANCE REPLACED BATTERIES, OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999062500475 19990625 00475 WP 1999 6 25 9902119155 1 19990617 A 3350 BATTERY DOUG DC9 DC914 3022034 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORM AL. 2 L 7 2 4F A6WE 1999062500476 19990625 00476 SO 1999 6 25 COMA9910096 1 19990621 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 159A 20291 120159 EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES. 2 L 7 2 4T RT A31SO 1999062500477 19990625 00477 SO 1999 6 25 COMA9910097 1 19990621 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 MISSING A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 256CA 120245 EXIT SIGN MISSING AT ROW 5. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999062500478 19990625 00478 1999 6 25 COMA9960287 4 19990621 A 3420 45150340 SENSOR CNDAIR CL600 CL6002B19 EA LEFT AOA MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 01 981CA 7163 STALL FAIL CAUTION DURING TAKEOFF. REPLACED THE LEFT HAND AOA TRANSDUCER. 2 L 7 2 4F RT A21EA 1999062500479 19990625 00479 1999 6 25 COMA9960288 4 19990621 A 3418 39951 COMPUTER CNDAIR CL600 CL6002B19 EA E & E COMPT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 981CA 7231 215 7163 STICK SHAKER AND STALL FAIL WARNINGS AFTER TAKEOFF. REPLACED THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 1999062500480 19990625 00480 NM 1999 6 25 UPS99229900 1 19990526 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 2 FLAP TRACK FWD LUGS (O/B LUG O/B FACE, I/B LUG I/B AND O/B FACES). R EPAIRED IAW SMRO EO 99-14-006 ENGINEERING FILE NR 727-57-2080. 2 L 7 3 4F A3WE 1999062500481 19990625 00481 NM 1999 6 25 UPS99229901 1 19990526 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 8 FLAP TRACK FWD LUGS (O/B LUG I/B 7 O/B FACES I/B LUG I/B AND O/B FACE S). REPAIRED IAW SMRO EO 99-14-010 ENGINEERING FILE NR 727-57-2076. 2 L 7 3 4F A3WE 1999062500482 19990625 00482 NM 1999 6 25 UPS99229902 1 19990526 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 7 FLAP TRACK FWD LUGS (O/B LUG O/B FACE I/B LUG I/B AND O/B FACES). RE PAIRED IAW SMRO EO 99-14-009 ENGINEERING FILE NR 727-57-2077. 2 L 7 3 4F A3WE 1999062500483 19990625 00483 NM 1999 6 25 UPS99229903 1 19990526 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 3 FLAP TRACK FWD LUGS (O/B LUG I/B FACE I/B LUG I/B AND O/B FACES). RE PAIRED IAW SMRO EO 99-14-007 UPS ENGINEERING FILE NR 727-57-2079. 2 L 7 3 4F A3WE 1999062500484 19990625 00484 NM 1999 6 25 UPS99229904 1 19990526 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, NR 3 FLAP TRACK HOLES D AND C CORRODED. REPAIRED CARRIED OUT IAW OHM 57-40-01. 2 L 7 3 4F A3WE 1999062500485 19990625 00485 NM 1999 6 25 UPS99229905 1 19990526 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, NR 3 FLAP TRACK AFT HOLE G CORRODED. REPAIR CARRIED OUT IAW OHM 57-40-01. 2 L 7 3 4F A3WE 1999062500486 19990625 00486 NM 1999 6 25 UPS99229906 1 19990526 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, NR 6 FLAP TRACK CORRODED. REPLACED NR 6 TRACK IAW MM 57-51-31. 2 L 7 3 4F A3WE 1999062500487 19990625 00487 NM 1999 6 25 UPS99229907 1 19990528 A 5753 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, LIGHT SURFACE CORROSION ON NR 1 FLAP TRACK ATTACH FITTING ON I/B AND O/ B FACES. CORROSION REM OVED IAW SRM 51-10-06, REPAIR CARRIED OUT IAW SMRO EO 99-14-002 UPS ENGINEERING NR 727-57-2074. 2 L 7 3 4F A3WE 1999062500488 19990625 00488 NM 1999 6 25 UPS99229908 1 19990528 A 5753 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, LIGHT SURFACE CORROSION ON NR 2 FLAP TRACK ATTACH FITTING ON I/B FACE. REPAIR CARRIED OUT IAW SMRO EO 99-14-002 UPS ENGINEERING FILE NR 727-57-2074. 2 L 7 3 4F A3WE 1999062500489 19990625 00489 NM 1999 6 25 UPS99229909 1 19990527 A 5310 STRUCTURE BOEING 727 72731C 1384011 NM NR 2 ADF ANTENNA CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, CORROSION ON SUPPORT STRUCTURE FOR NR 2 ADF ANTENNA. REPLACED SUPPORT STRUCTURE IAW SRM 53-10- 2 FIG 3. 2 L 7 3 4F A3WE 1999062500490 19990625 00490 NM 1999 6 25 UPS99229910 1 19990524 A 5230 HANDLE CUTOUT BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, AFT CARGO DOOR SUSPECT CRACK IN HANDLE CUTOUT. REPAIRED IAW SRM 51-10-02. 2 L 7 3 4F A3WE 1999062500491 19990625 00491 NM 1999 6 25 UPS99229911 1 19990528 A 5753 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, LIGHT SURFACE CORROSION ON NR 7 FLAP TRACK ATTACH FITTING ON I/B FACE. REPAIRED IAW SMRO EO 99 -14-002 ENGINEERING FILE NR 727-57-2074. 2 L 7 3 4F A3WE 1999062500492 19990625 00492 NM 1999 6 25 UPS99229912 1 19990528 A 5753 FITTING BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 8 FLAP TRACK ATTACH FITTING I/B AND O/B FACE. REPAIR CARRIED OUT IAW S MRO EO 99-14-002 UPS ENGINEERING FILE NR 727-57-2074. 2 L 7 3 4F A3WE 1999062500493 19990625 00493 NM 1999 6 25 UPS99229913 1 19990527 A 5753 PAD BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SURFACE CORROSION ON NR 5 FLAP TRACK FWD PAD. REPAIRED IAW UPS EO B727-5742-0651-J. 2 L 7 3 4F A3WE 1999062500494 19990625 00494 NM 1999 6 25 UPS99229914 1 19990527 A 5753 PAD BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, CORROSION ON NR 5 FLAP TRACK AFT PAD. REPAIR CARRIED OUT IAW OHM 20-20-01 AND UPS EO B727-5742 -0651-J. 2 L 7 3 4F A3WE 1999062500495 19990625 00495 NM 1999 6 25 UPS99229915 1 19990527 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, CORROSION ON NR 5 FLAP TRACK FWD LUGS I/B AND O/B FACES. REPAIR CARRIED OUT IAW SMRO EO 99-14- 008 UPS ENGINEERING FILE NR 727-58-2078. 2 L 7 3 4F A3WE 1999062500496 19990625 00496 WP 1999 6 25 UPS99829890 1 19990609 A 5280 DOUBLER DOUG DC8 DC873F 302199F WP RT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE: C1, RT W/W INBOARD DOOR, AFT CORNER OF TONGUE REPAIR. DOUBLER GOUGED AND CRACKED. REPAIRED BY FABRICA TION AND INSTALLATION OF DOUBLER IAW DC 8 SRM 52- 2-0 AND DC 8 SRM 51-1-21, 51-1-20A, 51-3-0. SEALED REPAIR IAW DC8 SRM 51-1-16. 2 L 7 4 4F RT 4A25 1999062500497 19990625 00497 WP 1999 6 25 UPS99829891 1 19990607 A 5320 3779762501N FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L4L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW F ITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED FITTING. INSTALLED NEW FITTING, TORQUED BOLT. 2 L 7 4 4F RT 4A25 1999062500498 19990625 00498 WP 1999 6 25 UPS99829892 1 19990607 A 5320 3779762501N FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L6L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW F ITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FITTING, TORQUED BOLT. 2 L 7 4 4F RT 4A25 1999062500499 19990625 00499 WP 1999 6 25 UPS99829893 1 19990607 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L-10R FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED, LO CATED AND DRILLED NEW FITTING AT STA 680 AND L-10R IAW DC-8 SRM 51-3-2. INSTALLED FITTING IAW DC- 8 SRM 51-1-20D. TORQ UED BOLT IAW DC-8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 1999062500500 19990625 00500 WP 1999 6 25 UPS99829894 1 19990606 A 5320 4758514521N FITTING DOUG DC8 DC873F 302199F WP BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C1, INTERCOSTAL FITTING FWD SIDE OF FS 1140 FRAME ABOUT I/B HALF OF LONGERON 33 RT IS CRACKED. REMOVED CRACKED FITTING, RECEIVED NEW FITTING (P/N 4758514-521N). LOCATED, DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FIT TING. 2 L 7 4 4F RT 4A25 1999062500501 19990625 00501 WP 1999 6 25 UPS99829895 1 19990605 A 5320 37592221 FITTING DOUG DC8 DC873F 302199F WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C1, LONGERON 36 AT FS 1270 SPLICE FITTING IS CRACKED. RECEIVED, LOCATED AND DRILLED NEW LONGERON SPLICE FITTING (P/N 375922 2-1) IAW DC-8 SRM 51-3-2. INSTALLED NEW FITTING IAW DAC DWG NR 5750322. 2 L 7 4 4F RT 4A25 1999062500502 19990625 00502 WP 1999 6 25 UPS99829896 1 19990605 A 5320 4758514519N FITTING DOUG DC8 DC873F 302199F WP BS 1228 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C, INTERCOSTAL FITTING, AT FS 1228 ABOVE O/B HALF OF LONGERON 33 RT IS CRACKED ON UPPER AFT LEG. REMOVE D INTERCOSTAL FITTING IAW DC-8 SRM 51-1-20D, RECEIVED FITTING NR 4758514-519N PO NR 294625 AND DRILLED UP IAW DC-8 SRM 5 1-1-20D, INSTALLED FITTING IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999062500503 19990625 00503 WP 1999 6 25 UPS99829899 1 19990621 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:PDC, AIRCRAFT EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50- 01, OP CK GOOD. 2 L 7 4 4F RT 4A25 1999062500504 19990625 00504 NE 1999 6 25 QXEA9901369 2 19990617 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA PW121 PW121 52124 NE NR 1 MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 815PH 16959 3005 50 PCE121131 PDX- UPON THROTTLE BACK FOR DESCENT, THERE WAS A STRONG OIL SMELL IN CABIN COMING IN THROUGH THE BLEEDS. MAINTENANCE RE PLACED THE NR 1 ENGINE, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 1999062500505 19990625 00505 NM 1999 6 25 99UAL900284 1 19990518 A 2120 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AC DUCT LOOSE A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 647UA 25284 FL 410, CREW REPORTED AT SMOOTH CRUISE A NOTICEABLE POP NOISE HEARD BY CREW AND FA'S. FA'S REPORTED A VIBRATION AT THE FLOOR LEVEL IN THE MID GALLEY AREA. NOTE ALL ENGINE PARAMETERS, BLEEDS, PACK OPERATIONS WERE NORMAL. RETURNED TO IAD, OVERWEIGHT LANDING. *S/D* BRACKET THAT SUPPORTS EXTERNAL AIR CONDITIONING CONNECTOR WAS NOT SECURED. IAD REMOVED BRA CKET AND RESECURED BRACKET TO DUCT. JFK INSPECTED THE DUCT AND BRACKET AND FOUND IT TO BE SECURED. BOS COMPLETED EG526 8 WHICH CHECK THE CONDITION AND SECURITY OF THE DUCT, BRACKETS, AND RODS. ALL WERE REPORTED TO BE IN GOOD CONDITION. 2 L 7 2 4F 4 F RT A1NM E24NE 1999062500506 19990625 00506 NM 1999 6 25 99UAL900291 1 19990523 A 3810 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WATER SYS NOT CLOSED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 515UA 24840 DIVERTED TO DEN DUE TO ABNORMAL NOISE UNDER AFT GALLEY. *S/D* THIS IS THE FIRST HIT FOR THIS TYPE OF PROBLEM ON THIS A IRCRAFT. MAINTENANCE FOUND THAT THE POTABLE WATER FILL VALVE WAS PARTIALLY OPEN, VENTING AIR PRESSURE OVERBOARD. NO OT HER DESCREPANCIES WERE FOUND. THE PROBLEM HAS NOT OCCURRED SINCE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500507 19990625 00507 NM 1999 6 25 99UAL900319 1 19990612 A 3260 257T11038 CONTROL MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 579UA 26697 DIVERTED TO IAD DUE TO A GEAR UNSAFE LIGHT INDICATION. FOUND INTERNAL OPEN IN LANDING GEAR LEVER CONTROL MODULE BETWEEN PINS 6 AND 7. REPLACED MODULE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500508 19990625 00508 NE 1999 6 25 99UAL900320 2 19990613 A 7261 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 OIL FILTER CUT A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 534UA 25129 726604 DIVERTED TO GEG DUE TO LOSS OF NR 1 ENGINE OIL QUANTITY. AIRCRAFT DIVERTED TO GEG DUE TO FLUCTUATING OIL PRESSURE. AMT FOUND EVIDENCE OF LEAK AROUND OIL FILTER HOUSING. DETERMINED THE MAIN OIL FILTER O-RING WAS CUT. REPLACED O-RING, SCR EEN, AND PERFORMED 5 MINUTE ENGINE IDLE RUN. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500509 19990625 00509 NE 1999 6 25 99UAL900321 2 19990613 A 7530 BLEED CONTROL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 615UA 21876 707523 ON TAKEOFF, NR 2 ENGINE SUSTAINED TWO SHORT COMPRESSOR STALLS. SURGE CHECKS WERE ACCOMPLISHED REFERENCE MAINTENANCE MAN UAL. THE ENGINE VANE BLEED CONTROL WOULD NOT TRIM, AND IT WAS REPLACED. THE STATOR VANE ACTUATOR WAS REPLACED PRECAUTI ONARY. 2 L 7 2 4F 4 F RT A1NM E3NE 1999062500510 19990625 00510 NE 1999 6 25 99UAL900322 2 19990614 A 7314 M832481210 O-RING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE MISSING A UALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7449U 21903 696564 EXPERIENCED LOW OIL PRESSURE INDICATION IN NR 2 ENGINE. SHUT DOWN NR 2 ENGINE. *S/D* DURING REPLACEMENT OF FUEL PUMP FOR TIME, FUEL PUMP DRIVE SHAFT O RING WAS NOT INSTALLED CAUSING OIL LOSS, AND ILLUMINATION OF LOW OIL PRESSURE LIGHT. A IRCRAFT RETURNED TO SERVICE AFTER INSTALLATION OF MISSING O RING, OIL SYSTEM SERVICE AND FUNCTIONAL RUN. 2 L 7 3 4F 4 F A3WE E2EA 1999062500511 19990625 00511 NM 1999 6 25 99UAL900323 1 19990613 A 5270 WARNING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR 1L ACTIVATED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7445U 21899 DOOR 1L WARNING LIGHT DISPLAYED AT LESS THAN 100 KNOTS. ABORTED TAKEOFF AND RETURNED TO BLOCKS. *S/D* VISUALLY CHECKE D DOOR OPERATION AND INDICATOR LIGHT, OPERATIONALLY CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999062500512 19990625 00512 GL 1999 6 25 99UAL900324 2 19990614 A 7230 COMPRESSOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J Y WARNING INDICATION ENGINE STOPPAGE TO TAKEOFF 1 WP 29 1845U 48261 451134 ON TAKEOFF ROLL APPROX 90 KNOTS, NR 2 ENG FAIL LT ON, DECREASING N1 AND RISING EGT, TO 960 DEGREES C. ABORTED TAKEOFF A ND SHUTDOWN ENGINE, TAKEOFF WEIGHT 352.8 NR (NOTED ENGINE STALLED). INCOMING SHOP BORESCOPE FOUND A STAGE 9 HPC BLADE FAILED AT MIDSPAN. MULTIPLE BLADE AND STATOR DAMAGE DOWNSTREAM AS A RESULT OF SECONDARY DAMAGE. HPT BORESCOPE SHOWED A LUMINUM METAL SPLATTED INDICATING HPC SEAL MATERIAL. SUBJECT ENGINE WAS REMOVED FROM SERVICE ON 6/15/99. 2 L 7 3 4F 4 F A22WE E23EA 1999062500513 19990625 00513 NM 1999 6 25 99UAL900325 1 19990612 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN FLICKERED A UALA K NONE L NO TEST CR CRUISE 1 WP 29 160UA 21237 E-ZONE EMERGENCY LIGHTS FLICKER IN FLIGHT. *S/D* THIS PROBLEM COULD NOT BE DUPLICATED ON THE GROUND. A SYSTEM TEST OF THE E-ZONE EMERGENCY LIGHTS AND BATTERY PACKS WAS ACCOMPLISHED PER MM 33-51-00 PG 507. EMERGENCY LIGHTS AND PACKS TEST ED OK PER SEA. 2 L 7 4 4F 4 F A20WE E20EA 1999062500514 19990625 00514 NM 1999 6 25 99UAL900326 1 19990615 A 3231 26702887 SEQUENCE VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG DOOR FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 570UA 26678 LANDED DCA UNDER AMBER ALERT DUE TO A GEAR INDICATION PROBLEM. *S/D* NLG DOOR SEQUENCE VALVE FAILED. REPLACED VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500515 20001010 00515 NE 2000 10 10 99UAL900327 2 19990616 A 7311 TUBE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING CHAFED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 413UA 8966 8966 470 V10019 FUEL FLOW ON LEFT ENGINE 80 LB/HR MORE THAN RIGHT. FUEL WENT OUT OF BALANCE ON 3 SEPARATE OCCASIONS, WITH THE WORST BEI NG 900 LBS, IE LEFT SIDE LOW. FUEL BURN WAS 1500 LBS, MORE THAN PLANNED. *S/D* FUEL LEAK FROM LINE TO ACOC AIR MODULA TING VALVE. CLAMPS HAD CHAFED THRU FUEL LINE. TWO FUEL TUBES (P/N: 5R8128 AND 5R8129) REPLACED. INVESTIGATION REVEA LED THIS FAILURE TO BE AN ISOLATED EVENT. OUR PLAN OF ACTION IS TO CONTINUE TO MONITOR THESE TUBES BY INSTITUTING AN MA INTENANCE PROGRAM INSPECTION REQUIREMENT TO REMOVE CLAMPS AND INSPECT TUBES FOR FRETTING WEAR AND TO REPLACE TUBES AS N ECESSARY. 2 L 7 2 4F 4 F RT A28NM E40NE 1999062500516 19990625 00516 EU 1999 6 25 99UAL900328 1 19990617 A 3350 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMER EXIT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 432UA 587 OVERWING ESCAPE ROUTE LIGHTING INOP. RELAMPED AND OP'S CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999062500517 19990625 00517 WP 1999 6 25 ABXA9900508 1 19990521 A 5320 36194341 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1490 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON SPLICE CRACKED AT LONGERON 32 LEFT AND STATION 1490. REPAIRED IAW DC8 SRM 51-1-11 AND 51-1-20D. 2 L 7 4 4F 4A25 1999062500518 19990625 00518 WP 1999 6 25 ABXA9900509 1 19990519 A 5320 47585721 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1540 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 33 RIGHT END FITTING CORRODED AT STATION 1540. REPLACED END FITTING IAW DWG 4758572. 2 L 7 4 4F 4A25 1999062500519 19990625 00519 WP 1999 6 25 ABXA9900510 1 19990519 A 5313 3648359 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1380-1400 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 HEAVY CORROSION ON LONGERON 36 AT STATION 1380 TO 1400. REPLACED DAMAGED LONGERON IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500520 19990625 00520 WP 1999 6 25 ABXA9900511 1 19990519 A 5313 3648359 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1340-1360 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 HEAVY CORROSION UNDER LONGERON 36, STATION 1340 TO 1360. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500521 19990625 00521 WP 1999 6 25 ABXA9900512 1 19990519 A 5320 SR08510097 SPLICE DOUG DOUG DC8 DC863 302198A WP BS 1630 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON SPLICE FITTING CORRODED AT LONGERON 25 RIGHT, STATION 1630. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1999062500522 19990625 00522 WP 1999 6 25 ABXA9900513 1 19990525 A 5320 5615377199 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1610-1655 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 INTERNAL DOUBLER CORRODED AT LONGERON 31 LEFT TO 33 LEFT AND STATION 1610 TO 1655. REPAIRED IAW DC8 SRM 51-1-21 AND DWG NR 5615377. 2 L 7 4 4F 4A25 1999062500523 19990625 00523 WP 1999 6 25 ABXA9900514 1 19990525 A 5320 570465021 DOUBLER DOUG DOUG DC8 DC863 302198A WP TAIL CONE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 INTERNAL DOUBLER CRACKED AT TAIL CONE, LOWER NAV LIGHT. REPAIRED IAW DC8 SRM 51-1-21 AND DWG NR 5704650. 2 L 7 4 4F 4A25 1999062500524 19990625 00524 WP 1999 6 25 ABXA9900515 1 19990525 A 5320 4641324N FITTING DOUG DOUG DC8 DC863 302198A WP BS 1690 BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 28 RIGHT END FITTING BROKEN AT STATION 1690. REPLACED FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1999062500525 19990625 00525 WP 1999 6 25 ABXA9900516 1 19990524 A 5313 3773091501 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1680 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 22 RIGHT HAD EXFOLIATION CORROSION AT STATION 1680. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1999062500526 19990625 00526 WP 1999 6 25 ABXA9900517 1 19990522 A 5320 4773155501 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 30 RIGHT END FITTING CORRODED AT STATION 1690. REPLACED END FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500527 19990625 00527 NM 1999 6 25 SCNA99085 1 19990622 A 3350 1002833 POWER SUPPLY BOEING 727 7272A1 138407F NM AFT AIRSTAIR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT IN THE AFT AIRSTAIR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLA CED THE POWER SUPPLY FOR THE EMERGENCY LIGHT IN THE AFT AIRSTAIR. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999062500528 19990625 00528 NM 1999 6 25 DHL99727004 1 19990617 A 2824 61183 VALVE BOEING 727 727228 NM NR 3 CROSSFEED FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 727DH 20204 NR 3 FUEL TANK CROSSFEED MANIFOLD VALVE INOP ON CLIMBOUT. REPLACED CONNECTOR AND VALVE PER MM 20-61-00 AND 28-22-17. 2 L 7 3 4F A3WE 1999062500529 19990625 00529 NE 1999 6 25 DHL99741003 2 19990617 A 7200 ENGINE BOEING 727 7272Q9 138448M NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A DHLA A J UNSCHED LANDING DUMP FUEL J Y WARNING INDICATION ENGINE STOPPAGE TO TAKEOFF 1 SO 01 741DH 21931 P689907 AT APPROX 1500 FT NR 2 ENGINE FAILED EGT CLIMBED TO 700 C AND FLIGHT RETURNED TO LAX. REMOVED AND REPLACED ENGINE. 2 L 7 3 4F 4 F RT A3WE E2EA 1999062500530 19990625 00530 1999 6 25 DHL99806002 4 19990617 A 3418 C264064 COMPUTER DOUG DC8 DC873F 302199F WP E & E COMPT MALFUNCTIONED A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 806DH 46002 ON TAKEOFF ROLL, STICK SHAKER CAME ON AND STAYED ON, REJECTED TAKEOFF. REMOVED AND REPLACED LIFT COMPUTER, LIFT TRANSDU CEER, STALL WARNING MOD TRANSFER RELAY. 2 L 7 4 4F RT 4A25 1999062500531 19990625 00531 WP 1999 6 25 RRXA991094 1 19990618 A 3234 LEVER DOUG DC8 DC871F 302199D WP MLG LACK OF LUBE A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 801GP 46039 ANTI-SKID LIGHT ON WHEN ARMED AND LANDING GEAR RETRACTED, RETURNED TO KDAY (DESTINATION BELOW MAX LANDING WEIGHT). LUBE D AND CLEANED LANDING GEAR LEVER SWITCH, OPS CHECKS GOOD IAW DC-8 MM. 2 L 7 4 4F RT 4A25 1999062500532 19990625 00532 WP 1999 6 25 RRXA991095 1 19990619 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 870TV 46086 AT APPROXIMATELY FLT LEVEL 230 CABIN PRESS WENT TO 10,000 FT, LEVEL OFF A FLT 220 TO MAINTAIN CABIN PRESSURIZATION. AIR CRAFT FERRIED TO EDDF FOR REPAIR. AFT PRESURE BULKHEAD REPAIRED PER BOEING ROD SKETCH 99-06-22-001, REF : EWA M/A NR AM -5312-01:00 AND WORK CARD NR 1. 2 L 7 4 4F RT 4A25 1999062500591 19990625 00591 SW 1999 6 25 HEEA062463 1 19990524 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DETERIORATED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 404PH 1352 53188 UPPER RUBBER DETERIORATED ON MAIN ROTOR GEARBOX MOUNT. 1 G 7 1 3U O H2SW 1999062500651 19990625 00651 WP 1999 6 25 TWAA9908601 1 19990622 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND CRACK AT LONGERON TO FRAME FASTENERS AT STA 200, LONGERON 2L. SPLICED IN NEW LONGERON P ER SRM 53-02, PAGES 48 TO 53, FROM STA 190 TO 228. 2 L 7 2 4F A6WE 1999062500652 19990625 00652 NM 1999 6 25 TWAA9908702 1 19990622 A 3350 57761 BATTERY PACK BOEING 767 767205 1385121 NM ROW 11 DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 651TW 23058 THE EGRESS LIGHT AT ROWS 11 TO 16 ON RT SIDE STAYED ON. REPLACED THE BATTERY PACK AND CLEANED MOISTURE FROM THE LIGHT S TRIP. CHECK-C 4-7-99 LAX. 2 L 7 2 4F RT A1NM 1999062500653 19990625 00653 WP 1999 6 25 TWAA9908703 1 19990622 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 20 DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 959U 49704 THE EGRESS LIGHTS AT ROWS 15 TO 21 CAME ON IN FLIGHT AND WOULD NOT RESET. REPLACED THE BATTERY PACK AT ROW 20. CHECK-C 10-10-98 STL. 2 L 7 2 4F A6WE 1999062500654 19990625 00654 NM 1999 6 25 TWAA9908704 1 19990621 A 3350 LIGHT BOEING 767 767205 1385121 NM ROW 11-16 MALFUNCTIONED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 651TW 23058 THE CABIN EGRESS LIGHTS AT ROWS 11 TO16 ON RT SIDE STAYED ON ALL THE TIME. SYSTEM OPERATION CHECKED NORMAL. UNABLE TO DUPLICATE THE PROBLEM. CHECK-C 4-7-99 LAX. 2 L 7 2 4F RT A1NM 1999062500655 19990625 00655 WP 1999 6 25 TWAA9908705 1 19990621 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 15-20 DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 959U 49704 THE CABIN EGRESS LIGHTS AT ROW 15 TO 20 ILLUMINATED INTERMITTENTLY IN FLIGHT. REPLACED THE MID CABIN EGRESS LIGHT BATTE RIES. CHECK-C 10-10-98 STL. 2 L 7 2 4F A6WE 1999062500656 19990625 00656 WP 1999 6 25 TWAA9908707 1 19990622 A 5313 LONGERON DOUG DC9 DC915 3022036 WP BS 642 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 ACCOMPLISHING MC8-AD-AM FOUND THE RT LONGERON FLANGE ON LONGERON 1 CRACKED ONE INCH AT BELT RING STA 642. SPLICED IN NE W LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 4-12-99 STL. 2 L 7 2 4F A6WE 1999062500657 19990625 00657 WP 1999 6 25 IXXA9900011 1 19990621 A 2110 COMPRESSOR DOUG DC8 DC862 3021970 WP NR 3 DEFECTIVE A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 21CX 1920 45955 EN ROUTE FROM WRI TO COF, AN ODOR WAS SENSED IN THE COCKPIT ACCOMPANIED BY A LOUD NOISE EMITTING FROM THE NUMBER THREE T URBO COMPRESSOR. THE FLIGHT CREW SECURED THE TURBO COMPRESSOR AND THE ODOR SUBSIDED. MAINTENANCE PLACED THE TURBO COMP RESSOR ON DEFERRAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999062500658 19990625 00658 EU 1999 6 25 AWXA9900225 1 19990621 A 2120 AIR DIST AIRBUS 320 A320231 3930325 EU CABIN ODOR A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 646AW 19655 3220 271 STRONG OILY SMELL AFTER TAKEOFF, BELIEVE TO BE PACK SMELL. STILL COULD SMELL AT CRUISE. INSPECTED APU INLET FOR SIGNS OF OIL, NONE FOUND. RAN ENGINES ALTERNATING BLEEDS, SMELL STRONGEST WITH APU BLEED. INSTALLED MEL 49-10-01, CONTROL NR 106292. *S/D* APU WASHED, OPS CHECK GOOD AND MEL CLEARED. 2 L 7 2 4F RT A28NM 1999062500659 19990625 00659 EU 1999 6 25 AWXA9900226 1 19990621 A 7921 5U0002 OIL COOLER AIRBUS 320 A320231 3930325 EU NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 620AW 26396 24494 052 DIVERTED TO DFW FOR LEFT-HAND WING FUEL LOSS. PRELIMINARY INFORMATION, O-RING BLEW OUT OF THE FCOC (FUEL COOLED OIL COO LER) FILTER CARTRIDGE HOUSING. FAILED HELICOIL. CANNOT FIX HELICOIL. *S/D* FOUND FCOC LEAKING. REMOVED AND REPLACED SAME PER 79-21-43. OPS LEAK CHECKS OK. 2 L 7 2 4F RT A28NM 1999062500660 19990625 00660 EU 1999 6 25 AWXA9900227 1 19990622 A 2170 20499001 COALESCER AIRBUS 320 A320231 3930325 EU CABIN DIRTY A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 646AW 18875 998 271 ACRID SMELL AFTER TAKEOFF AND INCREASINGLY WORSE THROUGHOUT THE FLIGHT. SMELL INCREASED FROM SMELL ON GROUND. ACCOMPLI SHED TSM 21-00-00-801-810 TO CHECK FOR OIL IN THE APU BLEED AIR SYSTEM, BOTH EXTERNALLY AND INTERNALLY. ALL DUCTING REI NSTALLED AND BAY SECURED PER 49-11-11-400-001. NO EVIDENCE OF OIL OR GREASE FOUND. REMOVED AND REPLACED BOTH L/R OZONE FILTERS PER CARD S2C21301. LEAK CHECK GOOD. REMOVED AND REPLACED RECIRCULATION FILTERS PER CARD S2B21301. RECIRCULAT ION FILTERS (P/N QA06423-01), OZONE FILTER (P/N 20499001), (S/N 0539), TT: 10081, TC: 4633, TSR: 998. 2 L 7 2 4F RT A28NM 1999062500661 19990625 00661 NM 1999 6 25 CALA9900712 1 19990618 A 3260 SWITCH BOEING 727 727224 1384076 NM NLG DOORS INOPERATIVE A CALA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SW 09 69741 22250 THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING IAH. GEAR RECYCLING DID NOT HELP. FUEL W AS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. BOTH NOSE GEAR DOOR SWITCHES WERE REMO VED AND REPLACED IAW MM 32-62-11. OPERATION AND INDICATION CHECKED GOOD. 2 L 7 3 4F A3WE 1999062500662 19990625 00662 WP 1999 6 25 CALA9900713 1 19990621 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 313-350 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 313-350, LONGERON 19L. REPAIRED IAW ECRA 5331-01056. 2 L 7 2 4F A6WE 1999062500663 19990625 00663 WP 1999 6 25 CALA9900714 1 19990622 A 5210 BEAM DOUG DC9 DC982 3022082 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND A .5 INCH CRACK IN AT AFT END OF MAIN CABIN DOOR NR 7 BEAM. REPAIRED IAW SRM 52-05, FIGURE 31, SHEET 1 2. 2 L 7 2 4F A6WE 1999062500664 19990625 00664 WP 1999 6 25 CALA9900715 1 19990622 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 755-899 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND FLOOR SUPPORT UNDER LAV/GALLEY AREA CORRODED AT STA 755-899, LBL 44. THE CORRODED FLOOR SUPPORT SECTIO N WAS REMOVED AND A NEW SECTION WAS INSTALLED AND REINFORCED IAW SRM 53-70-00, FIGURE 13. 2 L 7 3 4F A22WE 1999062500665 19990625 00665 NM 1999 6 25 UPS99229919 1 19990531 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 540-560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, FWD CARGO BAY CORROSION ON STRINGER 23L AT BS 540 TO BS 560. REPAIR CARRIED OUT IAW SRM 51-10- 6 & SRM 53-10-3 FIG 2. 2 L 7 3 4F A3WE 1999062500666 19990625 00666 NM 1999 6 25 UPS99229920 1 19990527 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, CORROSION IN HOLES E & C IN NR 5 FLAP TRACK. REPAIRED IAW UPS EO B727-5742-0651-J. 2 L 7 3 4F A3WE 1999062500667 19990625 00667 NM 1999 6 25 UPS99229921 1 19990526 A 5530 GUSSET BOEING 727 72731C 1384011 NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, VERT STAB MAIN BOX INTERIOR 9TH COMPARTMENT FROM TOP, RIB TO SKIN ATTACH GUSSET CRACKED AT S7 R T. GUSSET REPLACED IAW SRM 51-20-1 FIG 7. 2 L 7 3 4F A3WE 1999062500668 19990625 00668 NM 1999 6 25 UPS99229922 1 19990531 A 3230 HINGE BOEING 727 72731C 1384011 NM MLG MANUAL DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, NLG MANUAL EXT DOOR HINGE STIFF, LT MLB MANUAL EXT DOOR HINGE CRACKED. HINGES REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1999062500669 19990625 00669 NM 1999 6 25 UPS99229923 1 19990524 A 5230 SKIN BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, SUSPECT CRACK ON MCD SKIN LWR EDGE BS 550. REPAIRED IAW SRM 52-20-2. 2 L 7 3 4F A3WE 1999062500670 19990625 00670 NM 1999 6 25 UPS99229924 1 19990524 A 5720 BRACKET BOEING 727 72731C 1384011 NM LT WING TIP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE: C & SI, LT WING TIP LENS ATTACH BRACKET AFT LWR END CRACKED. REPLACED BRACKET IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999062500671 19990625 00671 EU 1999 6 25 QXEA9901370 1 19990618 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 1147 11234 GEG - THREE VOLT EVACUATION LIGHTS ON RIGHT EMERGENCY EXITS ARE DIM. MAINTENANCE REPLACED THE POSITION NR 4 EMERGENCY P OWER SUPPLY, LIGHTS OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1999062500672 19990625 00672 WP 1999 6 25 99FDEA00228 1 19990623 A 3297 WIRE HARNESS DOUG DC10 DC1030 3023501 WP LT MLG OUT OF POSITION A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 313FE 48311 LEFT MAIN GEAR IND (RED) UNSAFE IN THE UP POSITON IN BOTH PILOT AND 2ND OFFICER'S PNL GEAR. *S/D* TENSION OF WIRE BUND LE ATTACHED TO THE UPLOCK SENSOR FOUND TIGHT. WIRING BUNDLE REROUTED AND LANDING GEAR WARN TEST CARRIED OUT IAW AMM 32- 60-00-5. FOUND IND SATISFIED. 2 L 7 3 4F A22WE 1999062500673 19990625 00673 NM 1999 6 25 99FDEA00229 1 19990622 A 3610 123558 CHECK VALVE BOEING 727 727233 138408A NM NR 3 ENGINE LEAKED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 223FE 20935 99-138 - NR 3 ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB-OUT. RED TAB PROC ACCOMPLISHED. REMOVED AND REPLACED BLEED CH ECK VALVE PER MM 36-10-21, PAGE 401, OPER CHECK OK. 2 L 7 3 4F RT A3WE 1999062500674 19990625 00674 1999 6 25 99FDEA00233 4 19990623 A 3417 4045053903 ADC AIRBUS 310 A310221 3930310 EU E & E COMPT INOPERATIVE A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 448FE 260 NO AIRSPEED IND ON TAKEOFF ROLL. ALL PFD SYMBOLS WERE PRESENT BUT CAPT AIRSPEED TRIANGLE NEVER INCREASED FROM 0. REMOV ED AND REPLACED NR 1 ADC IAW M/M 34-11-34, SYSTEM OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999062500675 19990625 00675 1999 6 25 99FDEA00234 4 19990622 A 3414 AIRSPEED IND AIRBUS 310 A310221 3930310 EU LT COCKPIT INOPERATIVE A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 448FE 260 CAPT HAD NO AIRSPEED INDICATION ON PFD DURING T/O. ABORTED AT 70 KNOTS. F/O AND STBY AIRSPEED INDICATE NORMAL. 2 L 7 2 4F RT A35EU 1999062500676 19990625 00676 WP 1999 6 25 99FDEA00235 1 19990623 A 3260 PROX TARGET DOUG DC10 DC1010F 3022111 WP LT MLG INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 388FE 46622 LEFT MAIN GEAR IND UNSAFE UP AFTER T/O WITH HANDLE UP. BOTH PANELS INDICATE UNSAFE. REMOVED AND REPLACED PROX TARGET, OPS CK PER MM 32-61-03. 2 L 7 3 4F A22WE 1999062500677 19990625 00677 NM 1999 6 25 99FDEA00230 1 19990622 A 3212 PILLOW BLOCK DOUG MD11 MD11F 3023600 NM LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 PILLOW BLOCK ASSY ON LT CTR LAND GEAR HAS CORROSION ON A/C STRUCTURE PAD, BOLT HOLES AND ALIGNMENT PIN HOLE. *S/D* REP AIRED LT PILLOW BLOCK MOUNTING PAD SURFACE AND BORES PER SRM 53-40-00 ON CTR GEAR ASSY. 2 L 7 3 4F RT A22WE 1999062500678 19990625 00678 NM 1999 6 25 99FDEA00231 1 19990622 A 3212 PILLOW BLOCK DOUG MD11 MD11F 3023600 NM RT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 PILLOW BLOCK ASSY ON RT CENTER LANDING GEAR HAS CORROSION ON A/C STRUCTURE PAD, BOLT HOLES AND ALIGNMENT PIN HOLE. *S/D * REMOVED CORROSION FROM CENTER LANDING GEAR, SHEAR PIN AND ATTACH BOLT HOLES PER SRM 53-40-00. DIMENSIONS ARE WITHIN SRM 53-40-00 REPAIR LIMITS. 2 L 7 3 4F RT A22WE 1999062500679 19990625 00679 WP 1999 6 25 ABXA9900518 1 19990522 A 5320 4773155501 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 36 END FITTING CORRODED AT STATION 1690. REPLACED END FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999062500680 19990625 00680 WP 1999 6 25 ABXA9900519 1 19990522 A 5320 4641326 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1690 BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 28 LEFT END FITTING BROKEN AT STATION 1690. REPLACED END FITTING IAW ABX REA D853-2731MR. 2 L 7 4 4F 4A25 1999062500681 19990625 00681 WP 1999 6 25 ABXA9900520 1 19990522 A 5320 3619434501M FITTING DOUG DOUG DC8 DC863 302198A WP BS 1480-1500 BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 33 RIGHT SPLICE BROKEN AT STATION 1480 TO 1500. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1999062500682 19990625 00682 WP 1999 6 25 ABXA9900521 1 19990522 A 5720 9750486 FRAME DOUG DOUG DC8 DC863 302198A WP WS 145 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FRAME CRACKED AT STATION XFS 145.00 UPPER TOP CORNER OF AUX TANK, RIGHT WING. REPAIRED IAW DC8 SRM 57-3-3 AND 57-2-0. 2 L 7 4 4F 4A25 1999062500683 19990625 00683 WP 1999 6 25 ABXA9900522 1 19990522 A 5313 1415997 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1760 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 HEAVY CORROSION ON LONGERON 35 LEFT AT STATION 1760. REPAIRED IAW DC8 SRM 53-2-2 AND DWG NR 1415997. 2 L 7 4 4F 4A25 1999062500684 19990625 00684 WP 1999 6 25 ABXA9900523 1 19990622 A 5313 27779224 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK, FOUND LONGERON 13 RIGHT CRACKED AT STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-0. 2 L 7 2 4F A6WE 1999062500685 19990625 00685 WP 1999 6 25 ABXA9900524 1 19990622 A 5240 5913184501 PAN DOUG DOUG DC9 DC931 3022065 WP SERV DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK, FOUND SERVICE DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03-00 AND 51-30-1. 2 L 7 2 4F A6WE 1999062500686 19990625 00686 WP 1999 6 25 ABXA9900525 1 19990621 A 5311 99196171 FRAME DOUG DOUG DC9 DC931 3022065 WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK, FOUND MAIN FRAME CRACKED IN UPPER CARGO COMPARTMENT. REPAIRED IAW DC9 S/B 53-131 AND DWG 5935650-503. 2 L 7 2 4F A6WE 1999062500687 19990625 00687 WP 1999 6 25 ABXA9900526 1 19990621 A 5730 591216148 PANEL DOUG DOUG DC9 DC931 3022065 WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE UPPER HONEYCOMB PANEL DELAMINATED. REPLACED PANEL IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999062500688 19990625 00688 WP 1999 6 25 ABXA9900527 1 19990531 A 5320 57550592 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 668 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 INTERNAL DOUBLER AT STATION 668 UNDER LONGERON 36 CORRODED. REPAIRED IAW DC8 SRM 51-1-20D AND ABX REA D853-27311. 2 L 7 4 4F 4A25 1999062500689 19990625 00689 WP 1999 6 25 ABXA9900528 1 19990528 A 5712 97532995 RIB DOUG DOUG DC8 DC863 302198A WP WS 520.168 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XS 520.168. REPAIRED IAW DWG NR 9753299. 2 L 7 4 4F 4A25 1999062500690 19990625 00690 WP 1999 6 25 ABXA9900529 1 19990528 A 5320 3755822 SPLICE DOUG DOUG DC8 DC863 302198A WP BS 300-340 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 HEAVY CORROSION FOUND ON LONGERON 28 LEFT AT STATION 300 TO 340. REPAIRED IAW DC8 SRM 53-2-0 AND DWG NR 9754913. 2 L 7 4 4F 4A25 1999062500691 19990625 00691 WP 1999 6 25 ABXA9900530 1 19990501 A 5313 5615374 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 1600 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 36 STATION 1600 CORRODED. REPAIRED IAW DC8 SRM 53-4-1 AND DWG 5615374. 2 L 7 4 4F 4A25 1999062500692 19990625 00692 WP 1999 6 25 MWEA99355 1 19990619 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 602ME 48133 THE PASSENGER DOOR SLIDE FELL OFF. MTC REINSTALLED PASSENGER DOOR SLIDE. 2 L 7 2 4F A6WE 1999062500693 19990625 00693 WP 1999 6 25 MWEA99356 1 19990617 A 3260 H146 SWITCH DOUG DC9 DC915 3022036 WP RT MLG DOOR INOPERATIVE A MWEA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 300ME 45718 AFTER LOWERING LANDING GEAR ON APPROACH, THE GEAR DOOR OPEN LIGHT STAYED ON. MTC REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR POSITION SWITCH. 2 L 7 2 4F A6WE 1999062500694 19990625 00694 NM 1999 6 25 DL757991383 1 19990618 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM BS 620 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 668DN 25141 DURING THE CURRENT HMV, ADDITIONAL DAMAGE WAS FOUND LOCATED TO AN EXISTING SKIN REPAIR. THE SUBJECT SKIN REPAIR WILL BE REMOVED AND A LARGER REPAIR ENCOMPASSING BOTH DAMAGES INSTALLED. REPAIRED PER ERA 362260-14, REV C. 2 L 7 2 4F RT A2NM 1999062500695 19990625 00695 NM 1999 6 25 DL72L991384 1 19990618 A 5330 SKIN BOEING 727 727232 1384082 NM BS 450-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 440-460. THE CRAC K WAS FOUND IN FASTENER ROW 12 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333280-14AD. 2 L 7 3 4F A3WE 1999062500696 19990625 00696 NM 1999 6 25 DL72L991385 1 19990618 A 5330 SKIN BOEING 727 727232 1384082 NM BS 610-620 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 600-620. THE CRAC K WAS FOUND IN FASTENER ROW 10 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333281-14AD. 2 L 7 3 4F A3WE 1999062500697 19990625 00697 NM 1999 6 25 DL72L991386 1 19990618 A 5330 SKIN BOEING 727 727232 1384082 NM BS 710-720 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 700-720. THE CRAC K WAS FOUND IN FASTENER ROW 4 AS ID'D IN FIGURE 6 OF THE SU BJECT SI. REPAIRED PER ERA 333284-14AD. 2 L 7 3 4F A3WE 1999062500698 19990625 00698 NM 1999 6 25 DL72L991387 1 19990618 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1070-1090 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP SPLICE BETWEEN BS 1070-1090. THE CR ACK WAS FOUND IN FASTENER ROW 4 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333282-14AD. 2 L 7 3 4F A3WE 1999062500699 19990625 00699 NM 1999 6 25 DL72L991388 1 19990618 A 5330 SKIN BOEING 727 727232 1384082 NM BS 550-560 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S26R LAP SPLICE BETWEEN BS 540-560. THE CRA CK WAS FOUND IN FASTENER ROW 9 AS ID'D IN FIGURE 6 OF THE SUBJECT SI. REPAIRED PER ERA 333288-14AD. 2 L 7 3 4F A3WE 1999062500700 19990625 00700 NM 1999 6 25 DL72L991389 1 19990614 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 502DA 21304 NR 2 MIDFLAP / UPPER SPAR CHORD / WBL 124.2: ALT FASTENER INSTALLATION - AD 94-07-08. DURING ACCOMPLISHMENT OF EO 4 -58708-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED HI-LOK COLLAR DUE TO INTERFERENCE WITH INSIDE SPAR RADIUS. AUTHORIZE D INSTALLATION USING MINI-NUT AND RADIUS BLOCK. 2 L 7 3 4F A3WE 1999062500701 19990625 00701 NM 1999 6 25 DLM88991390 1 19990617 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 987DL 7130 53338 AFTER TAKEOFF, AFT LAV SMOKE DETECTORS STARTED SIGNALING WITH SOME HAZE IN THE CABIN. RETURNED TO CVG. PERFORMED DUC T BURNOUT PER M/M CH 36. CHANGED WATER BAGS, RAN BOTH ENGS TO TAKEOFF AND NO SMOKE OR HAZE NOTED. ENGS STARTED WITH EX T AIR. APU NOT USED. REPLACED APU AND CLEANED DOORS, RAN APU AND NO LEAKS. ALL INDICATIONS NORMAL. RAN SEVERAL HRS, NO SMOKE OR HAZE. 2 L 7 2 4F RT A6WE 1999062500702 19990625 00702 NM 1999 6 25 DL757991392 1 19990618 A 2612 285N002821 CONTROL CARD BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 626DL 25353 22916 716324 FIRE/OVERHEAT EICAS MSG AND SYS FAIL LIGHT. RESET WITH MAINT DIRECTION AND BOTH FAIL LIGHT AND EICAS MSG RETURNED. DIV ERTED TO KMCO WITH DISPATCH DIRECTION. ONLY RT ENG FIRE LP2 STATUS MSG WHICH IS ALREADY ON MCO. T/S PER FIM AND WDM. R EPLACED FIRE/OVERHEAT/LOGIC CARD M10274 SYSTEM TEST AND ENG RUN UP CKS NORMAL. ALSO, REPLACED LOOP, (P/N 266701017). 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500703 19990625 00703 NM 1999 6 25 DL733991393 1 19990618 A 2710 BEARING KP4R16SD610 BOEING 737 737301 1384611 NM LT AILERON FAILED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 948WP 23259 AILERONS BINDING WITH FLAPS AT 5 DEG DURING CONTROL CHECK. FOUND AILERON CENTERING CAM BEARING FROZEN. REPLACED BEARIN G AND SYS OPS NORMAL. 2 L 7 2 4F RT A16WE 1999062500704 19990625 00704 NE 1999 6 25 DLM11991394 2 19990618 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 MALFUNCTIONED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 805DE 19880 48476 723915 LOUD NOISE REPORTED BY FLT ATTENDANTS AND TOWER, SLIGHT VIBRATION NOTED AT ROTATION RWY 9L IN ATL. SUSPECTED COMPRESSOR STALL. ENGINE INDICATIONS NORMAL. REPLACED NR 2 ENGINE. 2 L 7 3 4F 4 F RT A22WE E24NE 1999062500705 19990625 00705 NM 1999 6 25 DL76L991395 1 19990618 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM ROW 10-31 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DN 24759 LEFT AISLE OVERHEAD EMERGENCY LIGHTS FAILED TO TEST FROM ROW 10 TO ROW 31. REPLACED BATTERY PACK, OPS CHECK GOO D. 2 L 7 2 4F RT A1NM 1999062500706 19990625 00706 WP 1999 6 25 DLL19991396 1 19990619 A 2450 HARNESS LKHEED 1011 10113853 5265020 WP CARGO COMPT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 769DL 193H1218 UNABLE TO CLOSE CARGO DOORS. FOUND NUMEROUS C/B'S POPPED WHEN OUT AT A/C. UPON FURTHER INVESTIGATION FOUND LARGE WIRE BUNDLE IN MESC DAMAGED AT CLAMP. APPEARS IT CHAFED THRU AND BURNED UP WIRING 60-70 WIRES DAMAGED. REPAIRED WIRING. 2 L 7 3 4F A23WE 1999062500707 19990625 00707 NM 1999 6 25 DLM88991397 1 19990619 A 2170 COALESCER DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 987DL 53338 AFTER TAKEOFF SMOKE APPEARED IN CABIN FROM TAIL SECTION CAUSING BOTH AFT LAV SMOKE DETECTORS TO SOUND. BORESCOPED B OTH ENGINES, REPLACED BAGS, PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1999062500708 19990625 00708 NM 1999 6 25 DLM88991398 1 19990619 A 2910 FILTER AD7031H12 DOUG MD88 MD88 3023688 NM RT HYD SYS LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 920DL 49644 ATB-RT HYD SYS LOW IN FLT. REPLACED RT HYD SYS ENGINE PRESSURE FILTER ASSY. 2 L 7 2 4F RT A6WE 1999062500709 19990625 00709 WP 1999 6 25 DLL19991399 1 19990619 A 2497 M911M915 WIRE HARNESS LKHEED 1011 10113853 5265020 WP CARGO COMPT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 769DL 193H1218 MID AND AFT CARGO C/B'S POPPED AND WOULD NOT RESET. ALSO, THE ORD LIGHTS C/B AT 3C11. THIS HAPPENED WHEN STARTING TO C LOSE CARGO DOOR FOR DEPT BOS. MTC IN PROGRESS TO REPAIR BURNT WIRING TO 2 WIRE BUNDLES IN MESC LT O/B CEILING AREA BUND LE M911 AND M915. 2 L 7 3 4F A23WE 1999062500710 19990625 00710 NM 1999 6 25 DL73S991400 1 19990520 A 2933 TRANSMITTER B7113 BOEING 737 737232 1384475 NM A HYD SYST FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 323DL BO1328 23095 DURING CLIMBOUT, SYS A HYD QTY WENT TO .25. INSPECTED HYD SYS IN W/W AND BOTH GEARS, NO LEAKS FOUND. HYD RES INDICATE FULL, HYD IN COCKPIT INDICATE ZERO QTY. REPLACED TRANSMITTER. 2 L 7 2 4F RT A16WE 1999062500711 19990625 00711 NM 1999 6 25 DL72L991401 1 19990620 A 2612 874268 CONNECTOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE SHORTED A DALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 27 514DA 21430 695244 CONTINUOUS FIRE WARNING ON NR 3 ENGINE. UNABLE TO SILENCE FIRE WARN. BOTH EXTINGUISHER BOTTLES DISCHARGED WITH NO HELP. NR 3 ENGINE SHUT DOWN. RECEIVED WARNING APPROX 50 MIN INTO FLIGHT. ENG WINDMILLED FOR APPROX 5 MIN AFTER SHUT DOWN. FOUND LWR FIRE LOOP CONNECTOR SHORTED. REPLACED SAME, CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999062500712 19990625 00712 NM 1999 6 25 DL72S991402 1 19990620 A 2150 VALVE 39854021 BOEING 727 727232 1384082 NM RT PACK FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 535DA P3100 22048 ENG RUNNING ESS PWR SEL ON ENG 1, BOTH PACKS ON. APU GEN/FIELD BREAKER OPENED WITH ASSOCIATED AMBER LIGHTS, 1-3 BTBS OP EN WITH LIGHTS. PACKS TRIPPED, SMOKE, HOT PACK SMELL AND LOSS ELECT. RETURNED TO GATE. ELECT FAULT PANEL UNDEREXCITED SYS 1-3. LIGHTS ILLUMINATED, PACK VALVE C/B TRIPPED. REMOVED AND INSTALLED RT PACK VALVE. RAN ENGS. SWAPPED PWR, AL L CKS NORMAL. 2 L 7 3 4F A3WE 1999062500713 19990625 00713 NE 1999 6 25 DL757991403 2 19990620 A 7321 EEC BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 27 602DL 32414 22809 716524 ON DESCENT RT ENGINE ROLLED BACK TO IDLE AND STABILIZED, THEN ENGINE ROLLED BELOW IDG ONLINE SPEED. CREW ELECTED TO SHU TDOWN ENGINE. RT ENG PRI CONTROL STATUS MSG ON AND THE EPCS MESSAGE EEC P/EEC 275-16 275-19 PRESENT. 2 L 7 2 4F 4 F RT A2NM E17NE 1999062500714 19990625 00714 NM 1999 6 25 DL76G991404 1 19990620 A 2560 101651303 SLIDE BOEING 767 767332 1382001 NM R2 DOOR DETACHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1602 29694 R2 DOOR SLIDE PARTIAL DEPLOYMENT. REATTACHED SLIDE, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999062500715 19990625 00715 NM 1999 6 25 DL76L991405 1 19990621 A 2913 291001935 PUMP 731966 BOEING 767 767332 1382001 NM C HYD SYS FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 197DN 508668 28454 FIFTEEN MIN AFTER T/O, LT HYD PUMP PRIM 1 EICAS MSG ILLUM WITH LIGHT. DIVERTED TO FRA. PLACED PUMP ON MCO. ATB TO FRA . REPLACED NR 1 ELEC PUMP AND CASE RETURN FILTER. REMOVED MCO, SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 1999062500716 19990625 00716 NM 1999 6 25 DLM88991406 1 19990619 A 3350 POWER SUPPLY RPS1 DOUG MD88 MD88 3023688 NM ROW 1-12 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 930DL 3797 49717 ON L/O, FOUND BOTH FWD DOOR EMERGENCY EXIT LIGHTS AND SEATS 1-12 INOP. REPLACED POWER SUPPLY, CHECKS GOOD. 2 L 7 2 4F RT A6WE 1999062500717 19990625 00717 NM 1999 6 25 DL72S991407 1 19990621 A 5311 FRAME BOEING 727 727232 1384082 NM BS 784 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 DURING ACCOMPLISHMENT OF INSPECTIONS OF THE OVERWING EXIT FRAMES, UNIDENTIFIED REPAIRS WERE NOTED. THE SUBJECT ERA WILL EVALUATE THE REPAIRS AND ENSURE COMPLIANCE / DOCUMENTATION. REWORKED PER ERA 333213-14AD, REV A. 2 L 7 3 4F A3WE 1999062500718 19990625 00718 NM 1999 6 25 DLM90991408 1 19990320 A 5320 591214185 ANGLE DOUG MD90 MD9030 3023690 NM BS 1520 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 THE LT VERTICAL STABILIZER-TO-FUSELAGE ATTACH ANGLE WAS FOUND WITH A 1.5 INCH LONG CRACK AT FS 1520. THE CRACK IS TYPICAL OF THAT FOUND IN MD-88 SRM 53-05, FIG 23. THE CRACKED HORIZONTAL FLANGE WAS CUTOUT AND REPAIRED WITH A STEEL A NGLE FABRICATED FROM A NEW PART. THE REPAIR WAS ACCOMPLISHED PER ER/A 367626-14. 2 L 7 2 4F RT A6WE 1999062500719 19990625 00719 SO 1999 6 25 SWIA971493 1 19990609 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 187SW 120037 FIRST OFFICERS WINDSHIELD OUTER PANE SHATTERED CLIMBING THROUGH 20,000 FEET. RETURNED TO SLC. REMOVED AND REPLACED RIG HT WINDSHIELD. NO EVIDENCE OF OTHER DAMAGE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500720 19990625 00720 SO 1999 6 25 SWIA971494 1 19990609 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG FAILED A SWIA A UNSCHED LANDING N E FALSE WARNING VIBRATION/BUFFET CL CLIMB 1 NM 07 216SW 120285 WHEN RAISING LANDING GEAR LEFT MAIN A SYSTEM GAVE UNSAFE INDICATION ACCOMPANIED BY BAD VIBRATION. RETURNED TO ACV. REM OVED AND REPLACED LEFT MAIN LANDING GEAR A UPLOCK PROXIMITY SENSOR, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500721 19990625 00721 SO 1999 6 25 SWIA971495 1 19990601 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 193SW 120088 FLAP CONTROL FAULT CAME ON AFTER TAKEOFF AND WOULD NOT RESET. RETURNED TO SLC. CLEANED FLAP ACTUATOR CANNON PLUGS. CO ULD NOT DUPLICATE ON GROUND. OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500722 19990625 00722 SO 1999 6 25 SWIA971496 1 19990601 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 295UX 120295 LEFT WINDSHIELD SHATTERED CLIMBING THROUGH 12000 FT. REMOVED AND REPLACED LEFT WINDSHIELD IAW MM 56-10-01. NO EVIDENC E OF ANY OTHER DAMAGE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500723 19990625 00723 EA 1999 6 25 SWIA971497 1 19990601 A 3260 INDICATION CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 411SW 7067 NOSE GEAR DISAGREE WARNING LIGHT AFTER GEAR RETRACTION. NOSE GEAR LIGHT STAYED GREEN. PERFORMED GEAR SWING IAW MM 32-3 0-00, NO PROBLEMS FOUND. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F 4 F RT A21EA E15NE 1999062500724 19990625 00724 SO 1999 6 25 SWIA971498 1 19990601 A 3697 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT PACK DUCT BROKEN A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 562SW 120336 LEFT DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. APU BLEED ON, ENGINE BLEEDS OFF. STARTED QUICK REFERENCE HANDBOOK PROC EDURE, LIGHT WENT OUT. RETURNED TO AIRPORT. FOUND BROKEN SOLDER JOINT ON LEFT PACK DUCT LEAK SENSOR NEAR BLEED AIR CON TROL VALVE. RESOLDERED WIRE. LEFT PACK OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500725 19990625 00725 1999 6 25 SWIA971499 4 19990605 A 3454 RMI EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 FAILED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 564SW 120339 AFTER TAKEOFF, SMOKE IN THE COCKPIT THAT APPEARED TO COME FROM RMI NUMBER 2. SMOKE STOPPED WHEN RADIO MASTER NORMAL SWI TCH WAS TURNED OFF. AIRCRAFT RETURNED TO SBA. REPLACED NUMBER 2 RMI. ALSO, INSPECTED ALL WIRES AND OTHER INSTRUMENTS. NO DISCREPANCIES OR DEFECTS NOTED. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500726 19990625 00726 WP 1999 6 25 USAAD99063 1 19990507 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913VJ 45846 IND - THE SERVICE DOOR SLIDE LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999062500727 19990625 00727 WP 1999 6 25 USAAD99066 1 19990517 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 985VJ 47208 IND - THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999062500728 19990625 00728 WP 1999 6 25 USAAD99067 1 19990517 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 971VJ 47051 IND - THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY DOOR SLIDE EMERGEN CY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999062500729 19990625 00729 NM 1999 6 25 USAA059904 1 19990518 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 21244 FLT 6141 - BOS-LGA - FOUND ON L/S, CABIN CEILING EMERGENCY EXIT LIGHT AT ROW 18 INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999062500730 19990625 00730 NM 1999 6 25 USAA059903 1 19990516 A 3350 10600911 LIGHT GRIMES 25424 BOEING 727 727225 1384077 NM L1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918TS 20445 FLT 6100 - LGA-BOS - L-1 DOOR EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED L-1 DOOR EMERGENCY EXIT LIGHT. (M) 2 L 7 3 4F A3WE 1999062500731 19990625 00731 NM 1999 6 25 USAA049908 1 19990428 A 3350 1100049 BATTERY CHARGER BOEING 727 727227 1384078 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924TS 21041 FLT 6151 - BOS-LGA - FOUND ON L/S, EPL LIGHTS OUT FROM ROW 8 TO ROW 15. FOUND FUSE BLOW IN FORWARD EPL BATTERY CHARGER. FUSE PIGTAIL BROKEN IN F3 FUSE HOLDER. REPLACED FORWARD EPL LIGHTS BATTERY CHARGER. (M) 2 L 7 3 4F A3WE 1999062500732 19990625 00732 NM 1999 6 25 USAA049906 1 19990415 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 21244 FLT 6181 - BOS-LGA - FOUND ON L/S, EMERGENCY EXIT LIGHT AT MID CABIN AISLE OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999062500733 19990625 00733 NM 1999 6 25 USAA049907 1 19990415 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 4/5 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 21244 FLT 6181 - BOS-LGA, FOUND ON L/S, EMERGENCY EXIT SIGN AT ROW 4/5 AISLE INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999062500734 19990625 00734 WP 1999 6 25 USAAD99055 1 19990415 A 3350 P4010020 BATTERY DOUG DC9 DC982 3022082 WP PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 IND - THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY DOOR SLIDE EMERGEN CY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999062500735 19990625 00735 WP 1999 6 25 USAAD99068 1 19990519 A 3350 86210151 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 IND - THE EMERGENCY LOW LEVEL EMERGENCY LIGHTS WOULD NOT PASS 'A' CHECK REQUIREMENTS. MAINTENANCE REPLACED THE LIGHT AS SEMBLIES AT SEAT ROW 30 AND THE AFT EXIT. THE BATTERIES IN ALL 4 TRANSMITTERS WERE ALSO REPLACED. (M) 2 L 7 2 4F A6WE 1999062500736 19990625 00736 WP 1999 6 25 99ZZZM362 1 19990519 A 3350 9731044 LIGHT ASSY DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 IND - THE EMERGENCY LOW LEVEL EMERGENCY LIGHTS WOULD NOT PASS 'A' CHECK REQUIREMENTS. MAINTENANCE REPLACED THE LIGHT AS SEMBLIES AT SEAT ROW 30 AND THE AFT EXIT. THE BATTERIES IN ALL 4 TRANSMITTERS WERE ALSO REPLACED. (M) 2 L 7 2 4F A6WE 1999062500737 19990625 00737 NE 1999 6 25 SIMA991315 2 19990511 A 7320 6068T7209 HMU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 278AE WYG700091 340B278 SBP - FLT 3309 - AFTER TAKEOFF AT 800 FT, NR 2 ENGINE COMPRESSOR STALLED AND SHUTDOWN, AND THE OVERTEMP LIGHT ILLUMINATE D. CREW DECLARED AN EMERGENCY AND RETURNED TO SBP. MAINTENANCE DOWNLOADED FDAU DATA AND FOUND NO EXCEEDANCE RECORDED F OR FLIGHT 3309. PERFORMED RIGHT ENGINE BORESCOPE INSPECTION WITH NO DISCREPANCIES NOTED. INSPECTED AND CLEANED RIGHT E NGINE CHIP DETECTOR AND SCAVENGE SCREENS WITH NO DEFECTS NOTED. PERFORMED ENGINE COMPRESSOR WASH. REMOVED AND REPLACED RIGHT ENGINE HMU PER GE REQUEST. PERFORMED LEAK CHECK, GPA RUNS, CTOT, AUTOCOARSEN FUNCTIONAL CHECKS. PERFORMED TEST FLIGHT AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999062500738 19990625 00738 EU 1999 6 25 SIMA991401 1 19990520 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 222NE 340B222 ABI - DURING MBV INSPECTION, FOUND A CHAFE ON THE LEFT FUSELAGE AT THE STABILIZER FILLET FAIRING INTERFACE. BLENDED OUT THE CHAFE AREA AND PERFORMED EDDY CURRENT INSPECTION. RESTORED PROTECTIVE TREATMENT TO THE CHAFED AREA INCLUDING THE P OLYURETHANE TOP COAT. FABRICATED AN EXTERNAL DOUBLER .025 THICK. APPLIED SEALANT TO THE CONTACT SURFACE OF THE DOUBLER , REPOSITIONED, AND INSTALLED FASTENER WET. APPLIED FILLET SEALANT AROUND THE EDGES OF THE DOUBLER. INSTALLED CHAFE PR OTECTION PLATE IAW SB 340-53-042. REPAIR DONE IAW SAAB REPAIR STATEMENT 72SDS1525. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500739 19990625 00739 EU 1999 6 25 SIMA991444 1 19990524 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 203NE 340B203 ABI - DURING MBV INSPECTION, FOUND A SMALL PUNCTURE AND A GROUP OF SMALL DENTS ON THE INTERIOR OF THE PAX DOOR. PERFORM ED CUT OUT OF DAMAGE AND DEBURRED. PERFORMED EDDY CURRENT INSPECTION AND SONIC BOND TEST OF CUT OUT AREA WITH NO INDICA TIONSS NOTED. FABRICATED DOUBLER AND TRIPLER PLATES .050 THICK. REMOVED PAINT FROM THE AREA ADJACENT TO CUT OUT AREAS. FILLED HONEYCOMB CORE WITH EPOXY FILLER. FABRICATED FILLER PLATED AND INSTALLED FLUSH WITH SURFACE APPLIED PRESSURE A ND CURED. CLEANED REPAIR AREA AND REPAIR DOUBLER. APPLIED ADHESIVE TO REPAIR DOUBLERS, POSITIONED, APPLIED PRESSURE AN D CURED. APPLIED FILLET SEALANT TO EDGES OF REPAIR. RESTORED PAINT COATING TO SURFACE. WORK DONE IAW SAAB REPAIR STAT 2 L 7 2 4T RT A52EU 1999062500740 19990625 00740 EU 1999 6 25 SIMA991443 1 19990524 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DENT IN LEFT SIDE OF FUSELAGE SKIN FORWARD OF AND BELOW THE CARGO DOOR. PERFORMED AN EDDY CURRENT INSPECTION OF T HE AREA TO BE REPAIRED. NO INDICATIONS OF CRACKS FOUND. PERFORMED A CUTOUT OF THE DAMAGED SKIN AND RE-EDDY CURRENT THE AREA, NO INDICATIONS OF CRACKS WERE NOTED. FABRICATED A REPAIR PLATE 12 INCH BY .5 INCH, .050 THICK. APPLIED ALODINE AND ONE COAT OF EPOXY PRIMER. CLEANED REPAIR AREA AN PLATE, FAY SEALED, REPOSITIONED AND INSTALLED RIVETS WET. EDGE SE ALED REPAIR AND APPLIED ONE COAT OF EPOXY PRIMER AND ONE COAT OF TOP COAT TO EXTERIOR SURFACES. WORK DONE IAW SAAB 340 SRM 53-70-10, PAGE 215 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500741 19990625 00741 NM 1999 6 25 SIMA991441 1 19990524 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 203AE 21098 ABI - DURING MBV INSPECTION, FOUND CHAFE ON THE LEFT AFT FUSEALGE AT THE HORIZONTAL STABILIZER FILLET FAIRING INTERFACE. BLENDED THE CHAFE AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS. APPLIED PROTECTIVE TREATEM ENT TO THE BLENDED AREA INCLUDING POLYURETHANE TOP COAT. FABRICATED A REPAIR DOUBLER .025 THICK. APPLIED PROTECTIVE TR EATENT OT THE DOUBLER INCLUDING POLYURETHANE TOP COAT. APPLIED FAY SEALANT TO THE CONTACT SURFACE OF THE DOUBLER, REPOS ITIONED AND INSTALLED FASTENERS WET. APPLIED FILLET SEALANT ALONG THE EDGE OF THE DOUBLER AND RESTORED SURFACE FINISH. FABRICATED CHAFE PROTECTION PLATES FROM CRES 301 .25 HARD, .020 THICK, INSTALLED IAW SAAB SERVICE BULLETIN 340-53-042. 2 L 7 4 4F RT A20WE 1999062500742 19990625 00742 NE 1999 6 25 SIMA991445 2 19990524 A 7530 32248122 VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAILED A SIMA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 283AE 7143 340B283 SAN - FLT 3212 - LEFT ENGINE COMPRESSOR STALLED AFTER TAKEOFF AND ENGINE SHUTDOWN. PERFORMED BORESCOPE INSPECTION WITH NO DEFECTS NOTED. REMOVED AND REPLACED LEFT ENGINE ANTI-ICE START/BLEED VALVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999062500743 19990625 00743 EU 1999 6 25 SIMA990775 1 19990318 A 3350 EO218UXU120A RELAY AEROSP ATR72 ATR72212A 8680902 EU CABIN INTERMITTENT A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 548AT 548 DFW - FLT 3556 - EXIT SIGNS AT FORWARD AND AFT BULKHEAD TURN OFF AND ON UNCOMMANDED. REMOVED AND REPLACED RELAY 12E IAW ATR 72 STANDARD PRACTICES 20-00-00. OPERATIONAL CHECK OF EMERGENCY LIGHTING WAS GOOD. AIRCRAFT RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999062500744 19990625 00744 NM 1999 6 25 P2EA99199 1 19990601 A 2420 CONNECTOR BOEING 737 737222 1384473 NM NR 1 ENGINE LOOSE A P2EA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 05 208AU 19547 DEN - FLT 305 - EMERGENCY DECLARED (APU PREVIOUSLY DEFERRED) LANDING UNEVENTFUL AT SCHEDULED DESTINATION. LEFT ENGINE D RIVEN GENERATOR DROPPED OFF LINE IN FLIGHT AND WOULD NOT RESET. SWAPPED APU GCU WITH NR 1 ENGINE GCU. RAN NR 1 ENGINE. GENERATOR OPS CHECKS NORMAL PER MM 24-21-00. SAME MALFUNCTION OCCURRED AFTER 2 FLIGHT LEGS DURING TAXI IN TO GATE IN MSP. MAINTENANCE FOUND PIN PUSHED BACK ON FEEDER WIRE OF CANNON PLUG AT NR 1 ENGINE PYLON. REPOSITIONED AND SECURED PI N IN CANNON PLUG. OPS CHECK NORMAL PER MM 24-21-0. (M) 2 L 7 2 4F A16WE 1999062500745 19990625 00745 NM 1999 6 25 P2EA99198 1 19990507 A 5320 BEAM BOEING 737 737205 NM BS 668 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, LEFT WHEEL WELL SHEAR BEAM BS 668, LBL 65, WL 194 WAS FOUND CRACKED. REPAIRED PER BOEING S/B 737- 53-1066 REV 3 DATED 02/25/93, SECTION III AND PART III. (M) 2 L 7 2 4F A16WE 1999062500746 19990625 00746 NM 1999 6 25 P2EA99197 1 19990507 A 5313 STRINGER BOEING 737 737205 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, SKIN AT BS 727 'A' BETWEEN STRINGER 14R AND 16R WAS FOUND CRACKED IN TWO PLACES. REPAIRED PER EO COO-SJO-99-0628RR DATED 05/20/99. (M) 2 L 7 2 4F A16WE 1999062500747 19990625 00747 NM 1999 6 25 P2EA99196 1 19990508 A 5210 BEAM BOEING 737 737205 NM R1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, R1 DOOR, AFT FRAME, LOWER BEAM REINFORCEMENT WAS CRACKED. REPAIRED PER SRM 51-10-01 PAGE 5 AND 51 -30-02. (M) 2 L 7 2 4F A16WE 1999062500748 19990625 00748 NM 1999 6 25 P2EA99194 1 19990508 A 5330 SKIN BOEING 737 737205 NM BS 477-501 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURNIG C-CHECK, THE LOWER AFT CORNER OF THE FORWARD CARGO COMPARTMENT DOOR CUT OUT WAS FOUND WITH MISSING MATERIAL . REPAIRED DOOR CUT OUT SKIN AND BEARSTRAP BETWEEN BS 477 AND BS 501, FROM STRINGER 23 TO 26R IAW COOPESA EO NR COO-3-5 3-286-99 AND BOEING FAX NR COO-SJO-99-0603. (M) 2 L 7 2 4F A16WE 1999062500749 19990625 00749 NM 1999 6 25 P2EA99193 1 19990507 A 5330 SKIN BOEING 737 737205 NM FUSELAGE CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, THE FORWARD LAVATORY SERVICE PANEL CUT OUT SKIN WAS FOUND CORRODED. THE EXTERNAL FUSELAGE SERVICE PANEL DOUBLER WAS REPLACED PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999062500750 19990625 00750 EA 1999 6 25 MASA99049 1 19990325 A 5210 601R31911501 ACTUATOR CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 77181 7181 FLT 6001 - FAT-PHX - PRIOR TO DEPARTURE, MAINTENANCE NOTICED THAT THE DOOR WOULD NOT CLOSE WITH THE POWER ASSIST. MAINT ENANCE REPLACED THE DOOR ASSIST ACTUATORS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500751 19990625 00751 EA 1999 6 25 99ZZZM363 1 19990325 A 5210 601R31911502 ACTUATOR CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 77181 7181 FLT 6001 - FAT-PHX - PRIOR TO DEPARTURE, MAINTENANCE NOTICED THAT THE DOOR WOULD NOT CLOSE WITH THE POWER ASSIST. MAINT ENANCE REPLACED THE DOOR ASSIST ACTUATORS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500752 19990625 00752 EA 1999 6 25 MASA99053 1 19990328 A 5210 H341427 DOOR HANDLE CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 17175 7175 FLT 5816 - BOS-RDU - UPON ARRIVAL IN RDU, THE CREW FOUND THAT THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE TROUBLESH OT AND FOUND THE TOP CAMS WERE NOT ROTATING FAR ENOUGH TO ALLOW THE DOOR TO OPEN EASILY AND READJUSTED THE DOOR HANDLE. OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500753 19990625 00753 EA 1999 6 25 MASA99066 1 19990504 A 5210 SEAL CNDAIR CL600 CL6002B19 EA PAX DOOR DIRTY A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 17175 7175 FLT 5816 - BOS-RDU - CREW REPORTED THAT THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE TROUBLESHOT, AND CHECKED THE L ATCH MECHANISM RIGGING. NO DISCREPANCIES WERE NOTED. THE DOOR SEAL WAS CLEANED, AND THE AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A21EA 1999062500754 19990625 00754 EA 1999 6 25 MASA99077 1 19990520 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A MASA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 SW 07 27185 7185 FLT 6007 - PHX-DSM - JUST BEFORE FINAL INTO DSM, THE CAPTAIN REPORTED A FLAP FAIL MESSAGE ON THE EICAS AND DECLARED AN E MERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH AD 982001 PART A, DEPOWERED AND REPOWERED THE AI RCRAFT, OPS CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500755 19990625 00755 EA 1999 6 25 MASA99079 1 19990521 A 5210 6003168815 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 77181 7181 FLT 6130 - PHX-MRY - CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE LUBED THE DOOR, OPS CHECK GOOD. THE AI RCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500756 19990625 00756 EA 1999 6 25 MASA99080 1 19990523 A 2750 4916405 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 27173 7173 FLT 5005 - CMH-PHL - DURING TAKEOFF, CREW REPORTED THE FLAPS FAILED TO RETRACT. CREW DECLARED AN EMERGENCY, AND RETURNE D TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FECU, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500757 19990625 00757 EA 1999 6 25 MASA99082 1 19990523 A 5210 601R317473 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 77181 7181 FLT 6021 - PHX-FAT - THE CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED, CLEANED, LUBED AND ADJUS TED THE LOCK LATCHES. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500758 19990625 00758 NE 1999 6 25 GTIA9900575 2 19990417 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE LT ENGINE STALLED A GTIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 23 804RA 48048 718266 FLT 675 - RSW - AT 13,500 ON CLIMB-OUT, LEFT ENGINE LOUD BANG, COMPRESSOR STALLS. LEFT ENGINE BACK TO 1.1 EPR. COMPRES SOR STALLS STOP, DESCENT THROUGH 9000 FEET. COMPRESSOR STALLS AGAIN, LEFT ENGINE TO IDLE UNTIL AFTER LANDING. THE SHUT DOWN ENGINE. ENGINE IDLE SMOOTH. REPLACED LEFT ENGINE IAW MD-80 MM 71-00-00, 71-20-00 AND TRIMMED TO -217A POWER. (M ) 2 L 7 2 4F 4 F A6WE E9NE 1999062500759 19990625 00759 NE 1999 6 25 ASOA99045 2 19990515 A 7261 OIL CAP EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LOOSE A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN K Y FLUID LOSS ENGINE STOPPAGE CL CLIMB 1 SO 11 214AS 120009 ATL-BQK - LOST RIGHT ENGINE OIL PRESSURE AFTER TAKEOFF. CREW SHUT DOWN RIGHT ENGINE AND DECLARED AN EMERGENCY INTO ATL. MAINTENANCE FOUND OIL CAP IN BOTTOM OF COWLING. ENGINE OIL WAS SERVICED AND ENGINE CLEANED. LEAK AND OPS CHECKS WERE GOOD. MECHANIC HAD FAILED TO PROPERLY SECURE THE OIL SERVICE CAP AFTER SERVICING THE ENGINE OIL. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500760 19990625 00760 SO 1999 6 25 ASOA99044 1 19990512 A 2150 32144143 VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE FUSELAGE INOPERATIVE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 281AS 120224 AFTER ENGINE START RIGHT PACK FAIL LIGHT ILLUMINATED ADN CABIN FILLED WITH SMOKE. DETERMINED RIGHT PACK TO BE PROBLEM. MOVED TO DEFER LOG PER MEL 21-50-1. DEFER WAS CLEARED BY REMOVING AND REPLACING THE REGULATOR SHUTOFF VALVE. OPS CHEC K GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999062500761 19990625 00761 WP 1999 6 25 ARWA990503 1 19990526 A 2910 O-RING DOUG DC8 DC863F 302198F WP SLOT CONTL VLV FAILED A ARWA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 19 441J 45988 POS - FLT 602 - AT TOP OF DESCENT, AIL AND RUDDER MANUAL REVERSION LIGHTS CAME ON. SYSTEM PRESSURE DROPPED TO ZERO AND FLUID QUANTITY WAS AT STANDPIPE LEVEL. EMERGENCY PROCEDURES WERE FOLLOWED. AIRCRAFT LANDED AT POS WITHOUT INCIDENT. R EMOVED AND REPLACED SLOT CONTROL VALVE O-RING OPS NORMAL IAW MM 27-80-4. (M) 2 L 7 4 4F 4A25 1999062500762 19990625 00762 WP 1999 6 25 USAAD99065 1 19990516 A 2897 WIRE HARNESS DOUG DC9 DC982 3022082 WP E/E COMPT DAMAGED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 822US 49139 LGA-MCO - FLT 259 - EN ROUTE THE AFT LEFT FUEL BOOST PUMP, 'A' PHASE AND THE FORWARD LEFT FUEL BOOST PUMP, 'A' PHASE CIR CUIT BREAKERS TRIPPED. SHORTLY AFTERWARDS BOTH BOOST PUMPS FAILED ON THE LEFT SIDE AS WELL AT THE RIGHT AFT BOOST PUMP. ALL THREE PHASES OF POWER WERE LOST TO THESE PUMPS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT ITS DESTINAT ION WITHOUT INCIDENT. MAINTENANCE REPAIRED A DAMAGED WIRE BUNDLE IN THE E/E COMPARTMENT. (M) 2 L 7 2 4F A6WE 1999062500763 19990625 00763 NM 1999 6 25 USAABB99024 1 19990518 A 7722 60536801 HARNESS BOEING 767 767201 1385125 NM RT EGT FRAYED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 650US 23902 PHL - FLT 126 - AFTER TAKEOFF FROM PHL, CREW NOTED THAT THE RIGHT EGT INDICATION AND STANDBY INDICATION WERE FLUCTUATING . FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE UPPER EGT HARNESS FRAYED AND REPLA CED IT. TEST FLIGHT FLOWN WITH NO PROBLEMS NOTED. (M) 2 L 7 2 4F RT A1NM 1999062500764 19990625 00764 NE 1999 6 25 USAABB99023 2 19990515 A 7261 43293 O-RING BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE LT ENGINE RUPTURED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 648US 23900 695380 PHL - FLT 12 - EN ROUTE PHL-MAD, AT APPROXIMATELY 50W LONGITUDE, THE CREW NOTED THAT THE LEFT ENGINE OIL PRESSURE WAS LO W AND THAT THE QTY WAS FLUCTUATING BETWEEN 13 AND 14. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE FOUND A BAD O-RING ON THE LEFT ENGINE OIL CAP AND REPLACED IT. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 1999062500765 19990625 00765 NM 1999 6 25 USAABB99025 1 19990518 A 7722 CONNECTOR BOEING 767 767201 1385125 NM RT ENGINE LOOSE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 650US 23902 PHL - FLT 126 - AFTER A PREVIOUS RETF DUE TO FLUCTUATING RIGHT EGT AND SUBSEQUENT MAINTENANCE, FLIGHT 126 AGAIN RETURNED TO PHL FOR THE SAME PROBLEM. MAINTENANCE REPLACED THE NR 17 AND 18 PINS AND SOCKETS INPLUG D4208P. (M) 2 L 7 2 4F RT A1NM 1999062500766 19990625 00766 EU 1999 6 25 USAAF99024 1 19990506 A 3350 71050301 BATTERY FOKKER F28 F28MK0100 4990807 EU PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 885US 11345 PIT - DURING AN ANNUAL SLIDE DEPLOYMENT CHECK, THE EMERGENCY LIGHTS ON THE FORWARD ENTRY DOOR DID NOT ILLUMINATE. THE S LIDE SHOP REPLACED THE BATTERY DURING REPACK. (M) 2 L 7 2 4F RT 1999062500767 19990625 00767 EU 1999 6 25 USAAF990025 1 19990513 A 4910 BAS180TWMB25AA SEAL FOKKER F28 F28MK0100 4990807 EU APU LEAKING A USAA F ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 EA 19 885US 11345 ILM - FLT 243 - ON APPROACH TO ILM, WITH THE APU OPERATING, THE CREW RECEIVED APU FIRE WARNING WHEN THE SPEED BRAKES WER E DEPLOYED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE FLIGHT LANDED AT ILM WITHOUT FURTHER I NCIDENT. MAINTENANCE REPLACED THE APU SHROUD SEALS. (M) 2 L 7 2 4F RT 1999062500768 19990625 00768 EU 1999 6 25 99ZZZM364 1 19990513 A 4910 BAS181WMB25AA SEAL FOKKER F28 F28MK0100 4990807 EU APU LEAKING A USAA F ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 EA 19 885US 11345 ILM - FLT 243 - ON APPROACH TO ILM, WITH THE APU OPERATING, THE CREW RECEIVED APU FIRE WARNING WHEN THE SPEED BRAKES WER E DEPLOYED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE FLIGHT LANDED AT ILM WITHOUT FURTHER I NCIDENT. MAINTENANCE REPLACED THE APU SHROUD SEALS. (M) 2 L 7 2 4F RT 1999062500769 19990625 00769 NM 1999 6 25 AALA990680 1 19990509 A 3350 CONNECTOR BOEING 757 757223 1384957 NM ROW 13D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 619AA 24577 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 13D INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR. RESECURED LOOSE CONNECTOR TO EMERGENCY EXIT LIGHTS AT PASSENGER SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A2NM 1999062500770 19990625 00770 NM 1999 6 25 AALA990659 1 19990504 A 3350 CONNECTOR BOEING 767 767223 1385123 NM ROW 20 AB DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325AA 22326 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH MARKER LIGHT INOPERATIVE AT SEAT 20AB. REPLACED CONNECTOR AT SEAT 20 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999062500771 19990625 00771 NM 1999 6 25 AALA990682 1 19990510 A 3397 WIRE BOEING 767 767223 1385123 NM ROW 24B LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 302AA 22308 SFO - DURING MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROW 24B INOPERATIVE. REPAIRED EMERGENCY EXIT WIRING AT SEA T ROW 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999062500772 19990625 00772 1999 6 25 AALA990660 4 19990504 A 2330 6116730001 ISVM BOEING 767 767223 1385123 NM SEAT 4H SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 307AA 22313 PHX - FLT 199 - EN ROUTE JFK-LAX - DURING CRUISE, THE PASSENGER VIDEO UNIT AT SEAT 4H STARTED SMOKING. FLIGHT AIR INTER RUPTED AND LANDED PHX WITHOUT FURTHER INCIDENT. PASSENGER SEAT ROW WAS PLACARDED AND THE FLIGHT REDEPARTED. OVERNIGHT MAINTENANCE LAX DISCOVERED A DOOR THE UNIT WAS TAMPERED WITH CAUSING IT TO SHORT OUT. MAINTENANCE REPLACED INDIVIDUAL S EAT VIDEO MONITOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999062500773 19990625 00773 NE 1999 6 25 REXA99015 2 19990519 A 7210 6044T35P01 GEAR BOX SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE WORN A REXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 403BH 24671 340A060 GEE367242DK DURING CLIMB, LEFT PROPELLER OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY ENGINE RPM DECREASE AS THE PROPELLER BLADE ANGLE INCREASED TOWARD THE FEATHER POSITION. THE ENGINE WAS SHUTDOWN AND THE PROPELLER MANUALLY FEATHERED IAW APPROPRIATE CH ECKLIST. A SINGLE ENGINE LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. FOUND THE GEAR TEETH ON THE PROPELLER GEARBOX OIL LUBE AND PITCH CONTROL PUMP WORN. REMOVED AND REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1999062500774 19990625 00774 EU 1999 6 25 SIMA991161 1 19990426 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 240DS 340B240 ABI - DURING A PS-2 CHECK, FOUND 2 DENTS IN FUSELAGE SKIN AFT OF THE LEFT ICESHIELD. THE FORWARD DENT REQUIRED REPAIR W HILE THE SECOND DENT WAS WITHIN SRM LIMITS WITH NO DEFECTS NOTED DURING THE EDDY CURRENT INSPECTION AND WAS NOT INCORPOR ATED IN THE REPAIR OF THE FORWARD DENT. RECONTOURED THE DAMAGE SKIN AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE REWORKED AREA. NO FURTHER DEFECTS NOTED. FABRICATED TWO EXTERNAL DOUBLERS 13 INCH BY 6 INCH AND 12 INCH BY 6 INCH, BOT H .050 THICK. APPLIED ALODINE AND ONE COAT OF EPOXY PRIMER TO THE REPAIR PIECES. FAY SEALED REPAIR DOUBLERS AND INSTAL LED ON AIRCRAFT. FILLET SEALED ALL EDGES AND RESTORED SURFACE PROTECTION TO REPAIR AREA. WORK DONE IAW SAAB SRM 53-70- 2 L 7 2 4T RT A52EU 1999062500775 19990625 00775 EU 1999 6 25 SIMA991171 1 19990427 A 5311 SKIN AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 540AM 540 ABI - FOUND BIRD STRIKE TO RIGHT SIDE COCKPIT FUSELAGE SKIN AND FRAME 6 JUST AFT OF STATIC PORT. PERFORMED CUT OUT OF S KIN TO REMOVE DAMAGE (3.7 INCH BY 5). CUT OUT FRAME 6 TO REMOVE DAMAGE TO OUTER FLANGE AND SMALLER AREA OF WEB (4.5 INB H BY 1). FABRICATED INTERNAL DOUBLER MEASURING 17 INCH BY 9 INCH. FABRICATED DOUBLER SHIMS SAME THICKNESS OF DOUBLER F ABRICATED FILLER FOR SKIN MEASURING 3.75 INCH BY 5 INCH. FABRICATED TAPERED FRAME TO SKIN SHIMS .010 THICK. FABRICATED FRAME DOUBLER MEASURING 12 INCH BY 2.5 INCH. FABRICATED FRAME FILLER .040 THICK. APPLIED CORROSION PROTECTION OF ALOD INE AND EPOXY PRIMER TO ALL REPAIR PARTS AND CUT OUT AREAS. REPOSTIONED ALL PARTS WITH FAY SEALANT AND INSTALLED ALL RI 2 H 7 2 4T RT A53EU 1999062500776 19990625 00776 EU 1999 6 25 99ZZZM365 1 19990427 A 5311 FRAME AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 540AM 540 ABI - FOUND BIRD STRIKE TO RIGHT SIDE COCKPIT FUSELAGE SKIN AND FRAME 6 JUST AFT OF STATIC PORT. PERFORMED CUT OUT OF S KIN TO REMOVE DAMAGE (3.7 INCH BY 5). CUT OUT FRAME 6 TO REMOVE DAMAGE TO OUTER FLANGE AND SMALLER AREA OF WEB (4.5 INB H BY 1). FABRICATED INTERNAL DOUBLER MEASURING 17 INCH BY 9 INCH. FABRICATED DOUBLER SHIMS SAME THICKNESS OF DOUBLER F ABRICATED FILLER FOR SKIN MEASURING 3.75 INCH BY 5 INCH. FABRICATED TAPERED FRAME TO SKIN SHIMS .010 THICK. FABRICATED FRAME DOUBLER MEASURING 12 INCH BY 2.5 INCH. FABRICATED FRAME FILLER .040 THICK. APPLIED CORROSION PROTECTION OF ALOD INE AND EPOXY PRIMER TO ALL REPAIR PARTS AND CUT OUT AREAS. REPOSTIONED ALL PARTS WITH FAY SEALANT AND INSTALLED ALL RI 2 H 7 2 4T RT A53EU 1999062500777 19990625 00777 1999 6 25 VTZA990066 4 19990505 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 306UE 41020 FLT 7600 - IAD-BGM - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO NR 1 AHRS FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 AHRS. OPS CHECK OK. AIRCRAFT W AS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500778 19990625 00778 EA 1999 6 25 VTZA990065 1 19990504 A 2450 M610628023 RELAY CNDAIR CL600 CL6002B16 1900305 EA E/E COMPT FAILED A VTZA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 27 621BR 7186 FLT 7795 - IAD-RDU - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO A/C ESSENTIAL BUS FAILED IN FLIGHT. AIRC RAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED A/C ESSENTIAL BUS SENSE RELAY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETRN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500779 19990625 00779 EU 1999 6 25 VTZA990064 1 19990504 A 3350 311701 BATTERY BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 483UE 898 FLT 7243 - IAD-RIC - DURING PREFLIGHT, CREW FOUND EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT STAYED AT THE GATE WITH NO FUR THER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EMERGENCY BATTERY PACKS. OPS CHECK OK. AIRCRAFT WAS REL EASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500780 19990625 00780 EU 1999 6 25 VTZA990063 1 19990503 A 3240 320511 VALVE JETAIR JETSTM JETSTM4101 1500501 EU BRAKE SYSTEM FAILED A VTZA O OTHER O OTHER LD LANDING 1 EA 27 309UE 41022 FLT 7344 - TYS-IAD - DURING LANDING, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS BRAKES INOPERATIVE ON LANDI NG. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BRAKE RELAY VALVE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500781 19990625 00781 EU 1999 6 25 VTZA990061 1 19990503 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 491UE 911 FLT 7405 - IAD-CLE - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED . AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 44089, MEL 52-2. MAINT ENANCE CLOSED DMI 44089 ON 5/03/98 BY REMOVING AND REPLACING PASSENGER DOOR MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS REL EASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500782 19990625 00782 EU 1999 6 25 VTZA990060 1 19990502 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU EXTERNAL FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 312UE 41025 DURING MAINTENANCE, MECHANIC FOUND RIGHT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. AIRCRAFT STAYED AT GATE WITH NO FURT HER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND RELAMPED EMERGENCY LIGHT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500783 19990625 00783 EU 1999 6 25 VTZA990059 1 19990502 A 5270 WARNING LIGHTS BAG JETSTM JETSTM3201 1500217 EU PAX DOOR ILLUMINATED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 491UE 911 FLT 7150 - JFK-IAD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 44088, MEL 52-2. MAINTE NANCE CLOSED DMI 44088 ON 5-3-98 CYCLING PASSENGER DOOR SEVERAL TIME AND COULD NOT DUPLICATE AND NO DEFECTS NOTED, OPS C HECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500784 19990625 00784 EU 1999 6 25 VTZA990058 1 19990502 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 313UE 41026 FLT 7614 - RDU-IAD - DURING MAINTENANCE, MECHANIC FOUND AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. AIRC RAFT STAYED AT GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 48554, MEL 33-14. MAINTENANCE CLOSE D DMI 48554 BY REPAIRING WIRE ON FLOOR TRACK LIGHTING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500785 19990625 00785 EU 1999 6 25 VTZA990055 1 19990501 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU CARGO DOOR FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 476UE 884 FLT 7202 - ROA-IAD - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO POD DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETUR END TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED POD DOOR MICROSWITCH, OPS CHEC K OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500786 19990625 00786 EU 1999 6 25 VTZA990054 1 19990501 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 320UE 41043 FLT 7605 - SCE-IAD - DURING MAINTENANCE, MECHANIC FOUND PART OF THE FLOOR EMERGENCY LIGHTING INOPERATIVE. AIRCRAFT STAY ED AT GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPAIRED BROKEN WIRE ON FORWARD TRACK LIGHTING AND REMOV ED AND REPLACED FUSE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500787 19990625 00787 EU 1999 6 25 VTZA990053 1 19990430 A 3350 311701 BATTERY BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 474UE 849 FLT 7223 - IAD-ORF - DURING PREFLIGHT INSPECTION, CREW FOUND EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED AND RE MOVED AND REPLACED EMERGENCY LIGHTS BATTERIES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500788 19990625 00788 EU 1999 6 25 VTZA990052 1 19990429 A 2913 PV304426 PUMP JETAIR JETSTM JETSTM4101 1500501 EU LT/RT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 324UE 41017 FLT 7362 - IAD-JFK - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT IAD DUE TO HYD HIGH TEMP CAP LIGHT ILLUMINATED. MAIN TENANCE REMOVED AND REPLACED LEFT AND RIGHT ENGINE DRIVEN PUMPS. PRESSURE CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500789 19990625 00789 EU 1999 6 25 VTZA990051 1 19990429 A 2131 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 479UE 893 IAD-SYR - FLT 7316 - DURNIG TAXI, AIRCRAFT RETURNED TO IAD AND MADE AN UNSCHEDULED LANDING DUE TO PRESSURIZATION INTERMI TTENT, INOP IN AUTO AND MANUAL. MAINTENANCE REMOVED AND REPLACED CABIN PRESSURE CONTROLLER CHECK VALVE. OPS CHECK OF M ANUAL AND AUTO PRESSURE MODES NO DEFECTS NOTED. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500790 19990625 00790 EU 1999 6 25 VTZA990049 1 19990428 A 3240 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BRAKE SYSTEM DIRTY A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 329UE 41097 FLT 7568 - CHS - DURING TAXI, AIRCRAFT RETURNED TO BLOCKS DUE TO CONFIG WARNING CAPTION. MAINTENANCE CLEANED EMERGENCY BRAKE CONTROL VALVE MICROSWITCH. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500791 19990625 00791 EU 1999 6 25 VTZA990048 1 19990428 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 315UE 41033 FLT 7216 - IAD-HPN - DURING PREFLIGHT, HAD A SECTION OF EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE SECURED CONNE CTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500792 19990625 00792 1999 6 25 VTZA990047 4 19990428 A 3425 4020531574 ADI BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 494UE 810 FLT 7223 - IAD-PHL - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO CAPTAINS ADI INOPERATIVE. MAINT EANCE REMOVED AND REPLACED ADI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500793 19990625 00793 EU 1999 6 25 VTZA990046 1 19990428 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 305UE 41019 FLT 7216 - IAD-HPN - DURING PREFLIGHT, LEFT 3RD STRIP OF EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE SECURED CONNECT OR, AND AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500794 19990625 00794 EU 1999 6 25 VTZA990045 1 19990427 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU ROW 1A BROKEN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 319UE 41042 FLT 7382 - PIT-IAD - DURING POST FLIGHT INSPECTION, HAD EMERGENCY TRACK LIGHTING INTERMITTENT AT FORWARD SECTION FROM MA IN DOOR TO ROW 1A. MAINTENANCE REPLACED BROKEN WIRE ON FORWARD EMERGENCY LIGHTS TRACK. OPS CHECKED GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500795 19990625 00795 EU 1999 6 25 VTZA990043 1 19990426 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 305UE 41019 FLT 7383 - IAD-PIT - DURING PREFLIGHT TEST OF EMERGENCY LIGHTS, EMERGENCY FLOOR LIGHTS INTERMITTENTLY TURNED OFF. MAINT ENANCE REPAIRED CONNECTOR FOR EMERGENCY TRACK LIGHTING. OK FOR SERVICE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500796 19990625 00796 EA 1999 6 25 VTZA990042 1 19990426 A 2740 HSTCU CNDAIR CL600 CL6002B19 EA HORIZ STAB FAILED A VTZA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 EA 27 623BR 7192 FLT 7836 - FAR-ORD - DURING TAKEOFF, AIRCRAFT RETURNED TO FAR AFTER DECLARING AN EMERGENCY DUE TO STAB TRIM AND MACH TRI M EICAS MESSAGE FAILURE ON BOTH CHANNELS. MAINTENANCE RERACKED HSTCU AND CYCLED C/B'S OPS CHECK GOOD. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500797 19990625 00797 EU 1999 6 25 VTZA990041 1 19990424 A 3240 BRAKE SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU MLG REQ'D SERVICE A VTZA O OTHER O OTHER LD LANDING 1 EA 27 309UE 41022 ROC-IAD - FLT 7647 - DURING LANDING, EXPERIENCED MAIN TOE BRAKES FAILURE. MAINTENANCE OPS CHECKED BRAKE SYSTEM. ACCUMU LATORS AND ANTI-SKID BOX. NO DEFECTS NOTED, BLED BRAKES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE (M) 2 L 7 2 4T RT A41NM 1999062500798 19990625 00798 EA 1999 6 25 VTZA990076 1 19990512 A 3260 SENSOR CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 620BR 7179 FLT 7826 - ORD-AVP - DURING TAKEOFF, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO NO GEAR RETRACTION. AIRCRAFT RETURNED T O GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND ADJUSTED NLG PROX SENSOR AND PERFORMED GEAR SWIN GS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500799 19990625 00799 EU 1999 6 25 VTZA990091 1 19990520 A 3350 312111 BATTERY PACK BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 495UE 818 DURING MAINTENANCE, FOUND EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT STAYED AT THE GATE WITH NO FURTHER PROBLEMS. MAINTENA NCE INSPECTED AND REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNE D TO SERVICE (M) 2 L 7 2 4T RT A56EU 1999062500800 19990625 00800 EU 1999 6 25 VTZA990090 1 19990520 A 5270 SENSOR BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 490UE 909 FLT 7214 - IAD-HPN - DURING CLIMB, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SHIMMED LOCK INDICATOR ASSEMBLY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500801 19990625 00801 EU 1999 6 25 VTZA990089 1 19990519 A 5270 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 495UE 818 FLT 7214 - IAD-HPN - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO DOOR WARNING LIGHT ILLUMINATED. AIRCRAF T RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED PASSENGER DOOR MICROSWITCH, OPS CHE CK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500802 19990625 00802 EU 1999 6 25 VTZA990130 1 19990530 A 3222 STRUT BAG JETSTM JETSTM3201 1500217 EU NLG REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 480UE 894 FLT 7441 - IAD-ORF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NOSE GEAR RED WARNING LIGHT STAYED ON IN TRANSIT. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SERVICED NOSE STRUT. MAINT ENANCE PERFORMED GEAR SWING. OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500803 19990625 00803 EU 1999 6 25 VTZA990129 1 19990529 A 3240 S214161K GAUGE BAG JETSTM JETSTM3201 1500217 EU BRAKE SYSTEM FAILED A VTZA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 EA 27 494UE 810 FLT 7307 - AVP-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT BRAKE PSI SHOWS 2000 PSI IN FLIGHT . AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED GAUGE, OPS CH ECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500804 19990625 00804 1999 6 25 VTZA990099 4 19990524 A 3442 6224027001 RADAR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 483UE 898 FLT 7333 - IAD-CLE - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO WEATHER RADAR INOPERATIVE AN ELECTRICAL SMELL IN CABIN. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND RIGHT AIR INLE T PIPE CRACKED AND REMOVED AND REPLACED RADAR SCREEN AND AIR INLET PIPE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPRO VED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500805 19990625 00805 EU 1999 6 25 99ZZZM366 1 19990524 A 2120 137631402 DUCT BAG JETSTM JETSTM3201 1500217 EU BAGG COMPT CRACKED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 483UE 898 FLT 7333 - IAD-CLE - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO WEATHER RADAR INOPERATIVE AN ELECTRICAL SMELL IN CABIN. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND RIGHT AIR INLE T PIPE CRACKED AND REMOVED AND REPLACED RADAR SCREEN AND AIR INLET PIPE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPRO VED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500806 19990625 00806 EU 1999 6 25 VTZA99098 1 19990524 A 2910 HYD LINE BAG JETSTM JETSTM3201 1500217 EU LEFT LOOSE A VTZA D RETURN TO BLOCK J WARNING INDICATION LD LANDING 1 EA 27 474UE 849 FLT 7323 - ROC-IAD - DURING LANDING, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LOST OF LEFT HYDRA ULIC PSI. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND LOOSE LINE AND TIGHT ENED CONNECTION. MAINTENANCE PERFORMED GEAR SWING AND OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500807 19990625 00807 EU 1999 6 25 VTZA990097 1 19990520 A 2612 ENGINE BAG JETSTM JETSTM3201 1500217 EU LEFT SMOKING A VTZA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 472UE 823 FLT 7272 - DURING ACCOMPLISHMENT OF TORQUE AND TEMPERATURE LIMIT TEST, FLIGHT CREW NOTED DROP IN FUEL FLOW AND RPM ON LE FT ENGINE, TEST WAS REPLACED THREE TIMES WITH SAME RESULT. ON THIRD ATTEMPT FLIGHT CREW NOTED SMOKE COMING FROM LEFT EN GINE FLIGHT CREW ELECTED TO SHUTDOWN BOTH ENGINES AND EVACUATE THE AIRCRAFT ENGINES WERE SHUTDOWN AND AIRCRAFT WAS EVACU ATED WITHOUT FURTHER INCIDENT EXCEPT THAT DURING EVACUATION, F/O SUSTAINED A BUMP ON THE HEAD. AIRCRAFT WAS TOWED TO MA INTENANCE REMP FOR MAINTENANCE. AIRCRAFT WAS EXAMINED FOR EVIDENCE OF FIRE, NONE FOUND. MAINTENANCE PERSONNEL PERFORME D TORQUE AND TEMP LIMIT TEST ON BOTH ENGINES. NO FAULT NOTED. ALL PARAMETERS WERE NORMAL. UNABLE TO DUPLICATE AND FAU 2 L 7 2 4T RT A56EU 1999062500808 19990625 00808 EU 1999 6 25 VTZA990096 1 19990523 A 7712 TTL BAG JETSTM JETSTM3201 1500217 EU RT ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 493UE 805 FLT 7207 - IAD-PHF - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE DROPPED 15 PERCENT. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 43804, MEL 76-2 ON TTL. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500809 19990625 00809 EU 1999 6 25 VTZA990094 1 19990522 A 7797 WIRE HARNESS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DAMAGED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 480UE 894 FLT 7190 - IAD-MDT - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGIEN WOULD NOT MAKE TORQUE. AIRCR AFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPAIRED EXPOSED SHIELDING ON LEFT ENGINE SOFT HARNESS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500810 19990625 00810 EU 1999 6 25 VTZA990085 1 19990517 A 3350 BULB BAG JETSTM JETSTM3201 1500217 EU PAX DOOR FAILURE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 471UE 821 FLT 7333 - IAD - DURING PREFLIGHT, CREW FOUNDN OVERHEAD MAIN DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT STAYED AT GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RELAMPED LIGHT BULB, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500811 19990625 00811 EA 1999 6 25 VTZA990084 1 19990516 A 3240 74485617 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA NLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 620BR 7179 FLT 7736 - GSP-IAD - DURING CLIMB, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO GEAR DISAGREEMENT WARNING LIGHT ON RETRACT ING GEAR. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED SYSTEM TESTS AND REM OVED AND REPLACED LANDING GEAR PARKING BRAKE CONTROL HANDLE ASSY. MAINTENANCE PERFORMED GEAR SWINGS. OPS CHECK OK. AI RCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500812 19990625 00812 EA 1999 6 25 VTZA990083 1 19990516 A 3250 16650101 CONTROL MODULE CNDAIR CL600 CL6002B19 EA NLG STEERING FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 625BR 7214 FLT 7763 - IAD-RDU - AIRCRAFT ABORTED TAKEOFF DUE TO AIRCRAFT PULLED HARD RIGHT DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NOSE WHEEL STEERING CONTROL MODULE, OP S CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500813 19990625 00813 EU 1999 6 25 VTZA990082 1 19990515 A 5210 ACTUATOR BAG JETSTM JETSTM3201 1500217 EU PAX DOOR BROKEN A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 490UE 909 FLT 7418 - IAD-SCE - DURING CRUISE, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BROKEN ACTUATO R ON PASSENGER DOOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500814 19990625 00814 EU 1999 6 25 VTZA990081 1 19990514 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 FLT 7625 - IAD - DURING MAINTENANCE, FOUND FORWARD SECTION OF EMERGENCY ROW EXIT AISLE LIGHTS INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED CONNECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A41NM 1999062500815 19990625 00815 EU 1999 6 25 VTZA990080 1 19990514 A 7712 HARNESS WIRE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE BROKEN A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 486UE 905 FLT 7196 - ROA-IAD - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TTL AND EGT FLUCTUATION. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 45562, MEL 76-2. MAINTENANCE CLOSE D DMI 45562 BY REPAIRING WIRE ON SOFT HARNESS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500816 19990625 00816 EU 1999 6 25 VTZA990079 1 19990514 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 470UE 814 FLT 7253 - IAD-RIC - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED . AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED PASSENGER DOOR MI CROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500817 19990625 00817 EA 1999 6 25 VTZA990078 1 19990513 A 2913 MX580026 PUMP CNDAIR CL600 CL6002B19 EA NR 1 HYD SYSTEM FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 620BR 7179 FLT 7747 - IAD-RSW - DURING CRUISE, AIRCRAFT MADE A UNSCHEDULED LANDING AND DIVERTED TO SAV DUE TO NR 1 HYDRAULIC SYSTEM FAILED, QTY WENT TO ZERO. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND R EPLACED NR 1 HYDRAULIC PUMP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999062500818 19990625 00818 EU 1999 6 25 VTZA990101 1 19990524 A 2612 LIGHT BAG JETSTM JETSTM3201 1500217 EU RT FIRE WARN DIRTY A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 475UE 850 FLT 7514 - PHF-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO RIGHT FIRE WARNING LIGHT INOP. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. AIRCRAFT FERRIED TO IAD. MAINTENANCE INSPECTED AND CLEANED LIGHT SOCKET ASSY. OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500819 19990625 00819 EU 1999 6 25 VTZA990100 1 19990524 A 6120 NTS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 480UE 894 FLT 7197 - IAD-ROA - ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE ROLLED BACK ON TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GA TE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED NTS AND PERFORMED MAF ON LEFT ENGINE. OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999062500820 19990625 00820 SO 1999 6 25 C2XA99IA286 1 19990519 A 3230 12041912001 VALVE EMB 120 EMB120RT SO LT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16710 120106 IAH - FLT 3522 - THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHER E IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR SHUTOFF VALVE. THE AIRCRAFT WAS TEST FLOWN SATISFACTORYILY, AND WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999062500821 19990625 00821 SO 1999 6 25 C2XA99IA280 1 19990514 A 3234 12038594001 CONTROL LEVER EMB 120 EMB120RT SO LANDING GEAR INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 16710 120106 IAH - FLT 3730 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER IAW EMB120MM 32-31-03, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999062500822 19990625 00822 SO 1999 6 25 C2XA99IA281 1 19990514 A 3260 12043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR INOPERATIVE A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 16710 120106 IAH - FLT 3441 - THE CREW REPORTED THAT THE LEFT MAIN GEAR RED INDICATION LIGHT REMAINED ILLUMINATED UNTIL THE CONTROL L EVER WAS CYCLED TWICE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING G EAR RELAY BOX IAW EMB 120MM 32-31-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999062500823 19990625 00823 EU 1999 6 25 C2XA99IA282 1 19990517 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHTS IN THE CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR42-320 MM 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500824 19990625 00824 SO 1999 6 25 C2XA99IA283 1 19990514 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 16710 120106 IAH - FLT 3438 - THE CREW REPORTED THAT THE LEFT MAIN GEAR WOULD NOT RETRACT AND HAD A RUMBLING VIBRATION UNTIL THE CONT ROL LEVER WAS CYCLED MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR IAW EMB120MM, THE LAND ING GEAR RELAY BOX IAW EMB120MM 32-31-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999062500825 19990625 00825 SO 1999 6 25 C2XA99IA284 1 19990519 A 3350 3025101 LIGHT EMB 145 EMB145 SO LT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13958 145085 IAH - DURING SERVICE CHECK INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145MM 33-50-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999062500826 19990625 00826 SO 1999 6 25 C2XA99IA285 1 19990519 A 3350 110049 BATTERY CHARGER EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13958 145085 IAH - DURING SERVICE CHECK INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED BATTERY CHARGER IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4F RT T00011AT 1999062500827 19990625 00827 SO 1999 6 25 C2XA99BT042 1 19990515 A 2710 14566181402 BRACKET EMB 145 EMB145LR SO RIGHT AILERON BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16951 145063 DURING SCHEDULED EA 2710-01012 IN NEWARK, MAINTENANCE FOUND RIGHT OUTBOARD AILERON ROD END MOUNT BRACKET BROKEN. MAINTE NANCE REMOVED AND REPLACED MOUNT BRACKET AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999062500828 19990625 00828 EU 1999 6 25 C2XA99BT043 1 19990518 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CORRODED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 DURING 3 A INSPECTION, FOUND THE EMERGENCY LIGHT IN PASSENGER DOOR TO BE INOPERATIVE. MAINTENANCE CLEANED CORROSION FRO M LIGHT ASSY. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999062500829 19990625 00829 SO 1999 6 25 C2XA99BT044 1 19990516 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145ER SO LANDING GEAR MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14945 145049 EWR - 4135 - AFTER DEPARTURE LANDING GEAR DID NOT RETRACT. QRH, TRY CYCLING GEAR. GEAR CYCLED DID NOT WORK. APPEARED NOSE GEAR RETRACTED BUT MAINS DID NOT. RETURNED TO EWR UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED LGEU AND OPS CHECK ED AIRCRAFT GOOD FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999062500830 19990625 00830 SO 1999 6 25 C2XA99BT045 1 19990519 A 3350 1317 BULB EMB 145 EMB145 SO ROW 3 FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16927 145006 BTV - FLT 4218 - EMERGENCY LIGHT IN PASSENGER DOOR AND OVERHEAD ROW 3 INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT IN PASSENGER AND OVERHEAD ROW 3, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1999062500831 19990625 00831 SO 1999 6 25 C2XA99IA256 1 19990501 A 2120 AIR DIST EMB 120 EMB120RT SO CABIN SMOKING A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 12709 120101 IAH - FLT 3643 ON CLIMB-OUT, THE CREW REPORTED THAT THE CABIN FILLED WITH SMOKE AND THE SMOKE LIGHT ON THE MAP ILLUMINAT ED AT 10,000 MSL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT WHERE MAINTENANCE GROUND RAN THE COOLIN G PACKS OFF OF THE APU, RIGHT ENGINE, LEFT ENGINE, AND INSPECTED THE CABIN LIGHTS AND GALLEY EQUIPMENT WITH NO DEFECTS F OUND. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE WITH NO REPEAT INCIDENTS TO DATE. (M) 2 L 7 2 4T RT A31SO 1999062500832 19990625 00832 EU 1999 6 25 C2XA99IA255 1 19990430 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500833 19990625 00833 EU 1999 6 25 C2XA99IA254 1 19990503 A 3350 3012701 LIGHT AEROSP ATR42 ATR42500 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING MAINTENANCE VISIT INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-500 JIC 33-51-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500834 19990625 00834 EU 1999 6 25 C2XA99IA273 1 19990511 A 5320 S5367800821602 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE RIGHT 'Z' CHANNEL BETWEEN FRAMES 39 AND 40 WAS FOUND TO BE CORRODED. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED 'Z' CHANNEL IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1999062500835 19990625 00835 EU 1999 6 25 C2XA99IA272 1 19990511 A 5320 S5367131821002 WEB AEROSP ATR42 ATR42320 8680930 EU FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE WEB ABOVE STRINGER 14 RIGHT AT FRAME 39 TO 40 WAS FOUND TO BE CORRODED. MAINTENANC E REMOVED AND REPLACED THE AFFECTED WEB IN ACCORDANCE WITH ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500836 19990625 00836 EU 1999 6 25 C2XA99IA271 1 19990511 A 5315 S5367240820201 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500837 19990625 00837 EU 1999 6 25 C2XA99IA270 1 19990511 A 5315 S5367240620801 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500838 19990625 00838 EU 1999 6 25 C2XA99IA269 1 19990511 A 5347 S536780012000 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE AFT FLIGHT ATTENDANT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND 51-21-42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500839 19990625 00839 EU 1999 6 25 C2XA99IA268 1 19990511 A 5347 S536780012100 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE FORWARD FLIGHT ATTENDANT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND 51-21-42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500840 19990625 00840 EU 1999 6 25 C2XA99IA267 1 19990511 A 5320 S5367800826900 CHANNEL AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE CHANNEL ON THE PASSENGER DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMO VED AND REPLACED THE AFFECTED CHANNEL IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999062500841 19990625 00841 EU 1999 6 25 C2XA99IA266 1 19990511 A 5320 S5367800821000 CLIP AEROSP ATR42 ATR42320 8680930 EU FRAME 41 CORROED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, ATTACHMENT CLIP FOR THE RIGHT 'Z' CHANNEL AT FRAME 41 WAS FOUND TO BE CORRODED. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1999062500842 19990625 00842 EU 1999 6 25 C2XA99IA265 1 19990511 A 5320 S5367800826801 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FRAME 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE 'U' CHANNEL AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED 'U' CHANNEL IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500843 19990625 00843 EU 1999 6 25 C2XA99IA264 1 19990511 A 5210 S5217600101200 STRUCTURE AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR STRUCTURE WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE RE MOVED AND REPLACED THE DOOR ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500844 19990625 00844 CE 1999 6 25 C2XA99IA278 1 19990512 A 3234 1013841377 HANDLE BEECH 1900 1900D 1154162 CE LANDING GEAR INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 81556 UE239 IAH - FLT 3362 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999062500845 19990625 00845 SO 1999 6 25 C2XA99IA277 1 19990511 A 3350 7287580505 LIGHT EMB 145 EMB145 SO ROW 15, 16, 17 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13958 145085 IAH - DURING 'A' CHECK INSPECTION, THE EMERGENCY AISLE PATH LIGHT STRIP AT SEATS 15, 16, 17 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999062500846 19990625 00846 SO 1999 6 25 C2XA99IA276 1 19990513 A 3350 3071BPE BULB EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING 'A' CHECK INSPECTION, THE LEFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED LIGHT BULB IAW EMB120 ER MM 33-51-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999062500847 19990625 00847 SO 1999 6 25 C2XA99IA275 1 19990513 A 3350 3071BPE BULB EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING 'A' CHECK INSPECTION, THE RIGHT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB120-ER MM 33-51-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999062500848 19990625 00848 SO 1999 6 25 C2XA99IA274 1 19990513 A 3350 1013073 BULB EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING 'A' CHECK INSPECTION, THE AFT AISLE PATH EMERGENCY RED LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED LIGHT BULB IAW EMB120-ER MM 33-51-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999062500849 19990625 00849 EU 1999 6 25 SIMA991302 1 19990510 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 184AE 17177 340B184 DFW - FLT 3697 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROW 4 AND 5 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGH T POWER SUPPLY IAW SAAB AMM 33-50-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500850 19990625 00850 EU 1999 6 25 SIMA991331 1 19990513 A 3260 387 LAMP SAAB SF340 340B 7860101 EU RT MLG FAILED A SIMA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 21 341SB 340B341 JFK - FLT 4817 - RIGHT MAIN LANDING GEAR SAFE LIGHT BULBS NEED REPLACED. CREW WAS UNABLE TO RELAMP IN FLIGHT, DECLARED EMERGENCY. REMOVED AND REPLACED BULBS FOR RIGHT MAIN LANDING GEAR INDICATION IAW SAAB AMM 31-50-10 PROCEDURE 2. OPERAT IONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500851 19990625 00851 EU 1999 6 25 SIMA991351 1 19990515 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 353SB 340B353 DFW - FLT 3906 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 11B DOES NOT ILLUMINATE. REPLACED FLOOR PROXIMITY LIGHT BULB. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999062500852 19990625 00852 EU 1999 6 25 SIMA991301 1 19990510 A 5315 S53672407207 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 38 AND 39 CORRODED. MAINTENANCE REPAIRED THE FLOORBEAMS IAW SRM 53-00-0 0 FIGURE 438 AND 53-61-40 FIGURE 412. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500853 19990625 00853 EU 1999 6 25 SIMA991381 1 19990518 A 5315 S5337241120002 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE ELONGATION A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAM 18 HAD AN ELONGATED HI-LOCK HOLE. REPAIRED FLOORBEAM 18 IAW SRM 53-00-0 0 FIGURE 429. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500854 19990625 00854 EU 1999 6 25 SIMA991382 1 19990518 A 5330 S5317220121005 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE CANNING A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED OIL CANNING OF LEFT FUSELAGE SKIN BETWEEN FRAME 9 AND 10 AND STRINGE R 14 AND 18. MAINTENANCE INSTALLED A SKIN PATCH AND THREE STIFFENERS IAW ATR DRAWING NR 11S531R016 AND SRM 53-00-00 FIG URE 403. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500855 19990625 00855 EU 1999 6 25 SIMA991383 1 19990518 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING MBV-1 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT MIDDLE INBOARD AND OUTBOARD, LEFT AFT INBOA RD AND OUTBOARD, LEFT AND RIGHT FLIGHT ATTENDANT, RIGHT FORWARD AND RIGHT MIDDLE OUTBOARD, AND THE RIGHT AFT AND RIGHT M IDDLE INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500856 19990625 00856 EU 1999 6 25 SIMA991191 1 19990429 A 5330 S5317150120305 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING CPCP-2 INSPECTION, CLEARED TDMI NR 14AMQ53002A, RIGHT FORWARD UPPER LATERAL SKIN TEMPORARY REPAIR. REMOVED AND REPLACED RIGHT FORWARD UPPER LATERAL SKIN BETWEEN FRAME 1 AND 13 IAW 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500857 19990625 00857 EU 1999 6 25 SIMA991203 1 19990430 A 5330 S5317140120005 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 SAW - DURING MBV-1 INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN JUST FORWARD OF THE WINDSHIELD CENTER LINE BETWEEN FRAM E 2 AND 3, MEASURING 2 INCHES BY 1 INCH BY .032 DEEP. REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 408 AND SRAS ASI/E/3539 1/99. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500858 19990625 00858 NE 1999 6 25 SIMA991414 2 19990521 A 7200 ENGINE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE LEFT POWER LOSS A SIMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 288AM 288 MIA - FLT 5714 - DURING CLIMB-OUT, APPROX 2-3 MINUTES AFTER TAKEOFF, THE LEFT ENGINE TORQUE DROPPED TWENTY PERCENT AS IF IT HAD FLAMED OUT. THE ITT DROPPED ABOUT 100 DEGREES AND THEN THE TORQUE SLOWLY ROSE BACK UP TO CLIMB SETTING. THIS O CCURENCE LASTED ABOUT 15 SECONDS. AIRCRAFT RETURNED TO MIAMI WITH NO FURTHER PROBLEMS. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999062500859 19990625 00859 SO 1999 6 25 SIMA991411 1 19990521 A 3350 7287580501 LIGHT EMB 145 EMB145LR SO CABIN BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 615AE 145087 ORD - FLT 4080 - EMERGENCY EXIT ROW FLOOR PROXIMITY LIGHT STRIP IS MISSING ORANGE STRIPE. REMOVED AND REPLACED EMERGENC Y LIGHT STRIP. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 1999062500860 19990625 00860 EU 1999 6 25 SIMA991413 1 19990521 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 218AE 18942 340B218 DFW - FLT 3841 - EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED TWO EMERGENCY LIGHT BATTERY P ACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500861 19990625 00861 EU 1999 6 25 99ZZZM367 1 19990521 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 218AE 16045 340B218 DFW - FLT 3841 - EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED TWO EMERGENCY LIGHT BATTERY P ACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500862 19990625 00862 EU 1999 6 25 SIMA991421 1 19990522 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 389AE 1166 340B389 DFW - FLT 3645 - EMERGENCY LIGHTS AT SOME LOCATIONS DO NOT ILLUMINATE. REMOVED AND REPLACED TWO EMERGENCY LIGHT POWER S UPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 2 4T RT A52EU 1999062500863 19990625 00863 EU 1999 6 25 99ZZZM368 1 19990522 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 389AE 1217 340B389 DFW - FLT 3645 - EMERGENCY LIGHTS AT SOME LOCATIONS DO NOT ILLUMINATE. REMOVED AND REPLACED TWO EMERGENCY LIGHT POWER S UPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 2 4T RT A52EU 1999062500864 19990625 00864 NM 1999 6 25 USAA059907 1 19990524 A 2611 824PY SMOKE DETECTOR BOEING 727 727227 1384078 NM LAVATORY FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924TS 2058 21041 FLT 6181 - BOS-LGA - FOUND ON L/S, FORWARD LAVATORY SMOKE DETECTOR WILL NOT TEST. REPLACED FORWARD LAVATORY SMOKE DETEC TOR. (M) 2 L 7 3 4F A3WE 1999062500865 19990625 00865 NM 1999 6 25 USAA059906 1 19990524 A 3310 T60320D LIGHT BOEING 727 727225 1384077 NM AILERON TRIM FAILED A USAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 19 918TS S50A 20445 ON THE GROUND, SMOKE STARTED COMING OUT OF CENTER CONSOLE AILERON TRIM WHEEL. FOUND ONE LAMP IN AILERON TRIM WHEEL LIGH T PLATE OVERHEATED AND CAUSING SLIGHT SMOKE. REPLACED TRIM WHEEL LIGHT PLATE. OPERATION CHECKS OK. (M) 2 L 7 3 4F A3WE 1999062500866 19990625 00866 NM 1999 6 25 USAA990449 1 19990430 A 5312 BULKHEAD BOEING 737 737401 1384701 NM AFT PRESS BLKHD CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK, FOUND 4INCH BY 10 INCH CORROSION AT STRINGER 27R TO 27L AT BOTTOM OF AFT PRESSURE BULKHEAD. CO RROSION TASK NR C53-202-1. CORROSION LEVEL 2. INSTALLED DOUBLER PER SRM 53-80-08. (M) 2 L 7 2 4F RT A16WE 1999062500867 19990625 00867 EU 1999 6 25 RAIA990411 1 19990409 A 7331 TNAS1024L1182 GAUGE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 435AM 1109 889 FLT 7472 - STL - LEFT FUEL FLOW GAUGE INOPERATIVE. MAINTENANCE REPLACED LEFT FUEL FLOW TRANSMITTER. (M) 2 L 7 2 4T RT A56EU 1999062500868 19990625 00868 WP 1999 6 25 RAIA990410 2 19990408 A 7320 8961153 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CE 03 427AM 876 66184 FLT 7430 - EVV - RIGHT ENGINE TORQUE SURGING. MAINTENANCE REPLACED P-3 GASKET ON RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999062500869 19990625 00869 EU 1999 6 25 C2XA99IA223 1 19990418 A 3350 E0062B1A4AC0A SWITCH AEROSP ATR42 ATR42500 EU CABIN DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE CLEANED THE FLIGHT ATTENDANTS PUSH BUTTON SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999062500870 19990625 00870 EU 1999 6 25 SIMA990902 1 19990331 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 357 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 ABI - DURING MBV INSPECTION, FOUND DENTS ON RIGHT FS 357 BETWEEN SL 1615-1616. CUT OUT DAMAGE AND PERFORMED AN EDDY CUR RENT INSPECTION WITH NO INDICATION OF CRACKS. FABRICATED TWO EXTERNAL DOUBLERS .050 THICK. APPLIED SURFACE TREATEMENT TO THE DOUBLERS AND ONE COAT OF ALODINE AND ALSO TO EDGES OF THE CUT OUT. APPLIED SEALANT TO THE CONTACT SURFACES OF TH E DOUBLERS, REPOSITIONED AND ATTACHED TO AIRCRAFT. APPLIED SEALANT AROUND EDGES OF THE DOUBLERS. RESTORED SURFACE FINI SH. WORK DONE IAW SAAB 340 SRM 53-70-10 PAGE 217 FIG 210 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500871 19990625 00871 EU 1999 6 25 SIMA990901 1 19990331 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 341SB 340B341 ABI - DURING MBV INSPECTION, FOUND CHAFE ON THE RIGHT NACELLE INBOARD OUTER SKIN PANEL BLENDED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. RESTORED PROTECTIVE TREATEMENT TO THE BLENDED AREA INCLUDING POLYURETHANE TOP COAT. FABRICATED AND EXTERNAL DOUBLER .050 THICK, TRIPLER .050 THICK AND SHIMS .020 THICK. APPLIED P ROTECTIVE TREATMENT TO THE REPAIR PARTS INCLUDING POLYURETHANE TOP COAT. APPLIED FAY SEALANT TO THE CONTACT SURFACES OF THE REPAIR PARTS, REPOSITIONED AND INSTALLED ON AIRCRAFT. APPLIED FILLET SEALANT AROUND EDGES OF THE REPAIR. RESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1464 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE 2 L 7 2 4T RT A52EU 1999062500872 19990625 00872 EU 1999 6 25 SIMA990893 1 19990330 A 5400 ANGLE SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 301AE 340B301 ABI - DURING A MBV INSPECTION, FOUND CHAFE ON THE LEFT NACELLE INLET COMPARTMENT LOWER LONGERON. BLENDED THE CHAFED ARE A AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A REINFORCEMENT L ANGLE .090 THICK . APPLIED SURFACE TREATMENT ON THE EDGE OF THE DAMAGE AND THE REINFORCEMENT ANGLE. APPLIED SEALANT TO THE CONTACT SURF ACE OF THE ANGLE REPOSITIONED AND INSTALLED ON AIRCRAFT. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1459 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500873 19990625 00873 EU 1999 6 25 SIMA990892 1 19990330 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 301AE 340B301 ABI - DURING A MBV INSPECTION, FOUND CHAFE ON THE LEFT NACELLE OUTBOARD INNER SKIN. BLENDED THE CHAFE AREA AND PERFORME D AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A REINFORCEMENT DOUBLER .025. APPLIED SEALANT T O THE CONTACT SURFACE OF THE DOUBLER AND INSTALLED ON AIRCRAFT. APPLIED FIRE SEAL AROUND DOUBLER EDGE STEP WITH DOW COR NING DC730 RTV. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1459 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500874 19990625 00874 EU 1999 6 25 SIMA990891 1 19990330 A 5330 SKIN SAAB SF340 340B 7860101 EU FS 327.5 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 301AE 340B301 ABI - DURING A MBV INSPECTION, FOUND DENTS ON RIGHT FUSELAGE SKIN PANEL STATION 327.5 BETWEEN SL 1620 AND 1622. CLEANED AREA, CUT OUT DAMAGE, AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATION OF CRACKS. DEBURRED AND APPLIED ALOD INE TO THE CUT OUT EDGES. FABRICATED A REPAIR DOUBLER .050 THICK. CLEANED THE DOUBLER AND APPLIED A PROTECTIVE COATING OF ALODINE AND ONE COAT OF EPOXY PRIMER. APPLIED SEALANT TO DOUBLER AND ATTACHED TO FUSELAGE. APPLIED SEALANT TO THE DOUBLER EDGE STEP. APPLIED EPOXY PRIMER AND ONE COAT OF TOP COAT TO THE EXTERIOR SURFACE. RESTORED SURFACE FINISH. WO RK DONE IAW SAAB SRM 53-70-10 PAGE 215 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500875 19990625 00875 EU 1999 6 25 SIMA990871 1 19990328 A 3260 INDICATION SAAB SF340 340B 7860101 EU RT MLG MALFUNCTIONED A SIMA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 21 383AE 340B383 DFW - WHEN LANDING GEAR SELECTED DOWN, THE RIGHT GEAR DID NOT INDICATE DOWN AND LOCKED. REPLACED BULBS, TESTED AND RECY CLED LANDING GEAR AND WHILE THE INTRANSIT LIGHT WORKED NORMALLY AND THE INDICATOR TESTED FINE, THE RIGHT GEAR STILL FAIL ED TO INDICATE DOWN AND LOCKED. FOLLOWED GEAR UNSAFE CYCLING PROCEDURES, AND FINALLY GOT A SAFE INDICATION. MAINTENANC E PERFORMED LANDING GEAR EXTENSION AND RETRACTION FUNCTIONAL TESTS IAW AMM 32-30-00, CYCLING GEAR 20 TIMES, BUT COULD NO T DUPLICATE THE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999062500876 19990625 00876 NM 1999 6 25 ASAA9940116 1 19990522 A 5210 MECHANISM BOEING 737 7374Q8 NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 SEA - PRIOR TO DEPARTURE OF FLIGHT 63, CREW REPORTED L-1 DOOR DIFFICULT TO CLOSE. ADUSTED DOOR MECHANISM AND DOOR OPERA TED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999062500877 19990625 00877 NM 1999 6 25 ASAA9910129 1 19990520 A 5320 SUPPORT BOEING 737 737290C 138448V NM BS 344-360 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURIG A-3 CHECK, FOUND E-2 RACK FORWARD UPPER SUPPORT HAD BEEN CUT BY CABLE JUST AFT OF STATION 344 TO 360 AND THE LOWER TIE SUPPORT CRACKED FROM STATION 344 FLOORBEAM FORWARD TO NEXT BEAM. FERRIED A/C TO SEA AND REPAIRED PER EA 5310 -01695. (M) 2 L 7 2 4F A16WE 1999062500878 19990625 00878 NM 1999 6 25 TSAA9933249 1 19990604 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999062500879 19990625 00879 NM 1999 6 25 TSAA9933250 1 19990604 A 3350 873100151 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 6 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999062500880 19990625 00880 NM 1999 6 25 TSAA9933247 1 19990603 A 3350 9221009 BATTERY PACK BOEING 737 737282C 13844AU NM LT EMER EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED LEFT OVERWING EMERGENCY IDENTIFIER BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1999062500881 19990625 00881 NM 1999 6 25 TSAA9933248 1 19990603 A 3350 8731002511 LIGHT BOEING 737 737282C 13844AU NM LT EMER EXIT INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED LEFT OVERWING EXIT IDENTIFIER ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999062500882 19990625 00882 NM 1999 6 25 TSAA9933241 1 19990528 A 3350 9221009 LIGHT BOEING 737 7372Q9 138448M NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD SERVICE DOOR EMERGENCY LGIHT BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999062500883 19990625 00883 NM 1999 6 25 TSAA9933243 1 19990530 A 3350 1000679 LIGHT BOEING 737 7372S5C 1384499 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED AFT SERVICE DOOR EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999062500884 19990625 00884 NM 1999 6 25 TSAA9933244 1 19990531 A 3350 9221009 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999062500885 19990625 00885 NM 1999 6 25 TSAA9933245 1 19990531 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999062500886 19990625 00886 NM 1999 6 25 TSAA9933246 1 19990531 A 3350 86210066 BATTERY BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1999062500887 19990625 00887 NM 1999 6 25 TSAA9933239 1 19990327 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999062500888 19990625 00888 NM 1999 6 25 TSAA9933240 1 19990328 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999062500889 19990625 00889 NM 1999 6 25 TSAA9957242 1 19990528 A 5753 6571909111 FLAP BOEING 737 7372T4 1384492 NM LT TE MID FLAP CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 LEFT OUTBOARD MID FLAP CRACKED AT AFT FLAP INBOARD TRACK ATTACH POSITION. CRACKED AT BOTH INBOARD AND OUTBOARD TRACK AR M POSITION. REMOVED AND REPLACED MID FLAP IAW 27-51-72, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999062500890 19990625 00890 NE 1999 6 25 COEA9901701 2 19990114 A 7200 ENGINE FOKKER F27 F27MK600 4990706 EU RROYCE DART DART5327R 54509 NE NR 1 FAILED A COEA A UNSCHED LANDING R T PARTIAL RPM/PWR LOSS ENGINE CASE PENETRATION NR NOT REPORTED 1 NM 13 701FE 10419 14100 EN ROUTE TO OAK FOM YVR FLT 7525, PILOTS REPORTED HAVING A LOW TORQUE INDICATION ON NR 1 ENGINE. MAINTENANCE WAS ADVISE D UPON ARRIVAL IN OAK. WHEN THE MECHANIC OPENED THE LOWER COWLING ON THE ENGINE A PIECE OF METAL THAT LOOKED LIKE A PIE CE OF HOUSING FELL OUT. THE MECHANICS SENT DETAILED DRAWINGS BACK TO MAINTENANCE CONTROL AND ADVISED THAT THERE WAS A H OLE IN THE LOWER SECTION OF THE ENGINE THROUGH THE HOLE HE COULD SEE COMPRESSOR BLADES. ENGINE S/N 14100 HAS BEEN REMOV ED AND REPLACED WITH ENGINE S/N 16014. ENGINE RUN, LEAKS CHECKS HAVE BEEN COMPLETED, OPS CHECK OK. TEST FLIGHT PERFORM ED 1/18/99. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T A817 E297 1999062500891 19990625 00891 NE 1999 6 25 VTZA990135 2 19990602 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT MALFUNCTIONED A VTZA D RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 302UE 41013 FLT 7315 - BOS-JFK - ABORTED TAKEOFF DUE TO RIGHT ENGINE ONLY MAKING 90 PERCENT TQ. AIRCRAFT RETURNED TO GATE. MAINTEN ANCE OPENED DMI NR 44978, MEL 76-2. TQ WAS VERIFIED WITH TTL OFF. MAINTENANCE CLOSED DMI 44978 ON 6/6/99 BY GROUND RUN S AND COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999062500892 19990625 00892 EU 1999 6 25 VTZA990108 1 19990521 A 2611 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 323UE 41059 FLT 7346 - TYS-IAD - DURING CRUISE, AIRCRAFT DIVERTED TO BRISTOL, DUE TO POD SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 53040 MEL 26-3. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500893 19990625 00893 1999 6 25 VTZA990132 4 19990602 A 3425 7003938907 FLIGHT DIR JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 27 332UE 41100 FLT 7590 - IAD-BTV - DURING PREFLIGHT, SMOKE WAS OBSERVED ON FLIGHT DECK COMING FROM THE FLIGHT DIRECTOR PANEL. MAINTEN ANCE REMOVED AND REPLACED FLIGHT DIRECTOR PANEL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500894 19990625 00894 EU 1999 6 25 VTZA990133 1 19990602 A 2425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 316UE 41055 FLT 7586 - IAD-PVD - DURING CRUISE, MADE UNSCHEDULED LANDING AT IAD AND RETURNED TO GATE DUE TO NR 1 AHRS FAILURE. MAIN TENANCE REMOVED AND REPLACED AHRS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999062500895 19990625 00895 EU 1999 6 25 VTZA990134 1 19990603 A 2611 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE COMPT MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 309UE 41022 FLT 7350 - JFK-IAD - DURING CRUISE, MADE UNSCHEDULED LANDING AT BWI DUE TO POD SMOKE CAP ILLUMINATION IN FLIGHT. MAINTE NANCE INSPECTED POD SMOKE DETECTOR CANNON PLUG AND DETECTOR UNIT, ALONG WITH INSPECTION OF BATTERY COMPARTMENT. PERFORM ED OPS CHECK OF SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE (M) 2 L 7 2 4T RT A41NM 1999062500896 19990625 00896 NM 1999 6 25 99ZZZM369 1 19990527 A 5270 82400033029 SENSOR DHAV DHC8 DHC8103 1386005 NM PAX DOOR OUT OF ADJUST A KPVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 805WP 353 HNL - FLT 1552 - CLIMBING THROUGH 6500-7500 FT, THE AIRCRAFT WAS PRESSURIZED, THE MASTER WARNING LIGHT ILLUMINATED CONCU RRENTLY WITH THE 'PASS DOOR' WARNING LIGHT. NOTIFIED ATC AND DECLARED AN EMERGENCY, RETURNED HNL TO LAND. INSPECTED AF FECTED SYSTEM AND DEFERRED IAW MEL 52-2. DOOR SENSORS WERE CLEANED AND MEL CLEARED. (M) 2 H 7 2 4T RT A13NM 1999062500897 19990625 00897 EU 1999 6 25 FJT99062421 1 19990609 A 3520 K386384 MASK BAG JETSTM JETSTM3201 1500217 EU CABIN DAMAGED A FJTA K NONE O OTHER NR NOT REPORTED 1 SO 03 242BM 902 MQY - AIRCRAFT WAS RECEIVED TO BE PLCED IN OPERATION, MAINTENANCE DISCOVERED THAT 10 OF THE APPROXIMATELY 20 INSTALLED P ASSENGER OXYGEN MASKS WERE IN AN UNSERVICEABLE CONDITION. THE MASK CUPS WERE EITHER FUSED/TORN. THIS AIRCRAFT HAD PREV IOUSLY BEEN IN STORAGE AND THEN PLACED BACK IN OPERATION APPROX 18 MONTH PRIOR TO THIS DATE. THE DEFECTIVE MASK CUPS WE RE REPLACED WITH NEW UNITS. (M) 2 L 7 2 4T RT A56EU 1999062500898 19990625 00898 NM 1999 6 25 AALA990551 1 19990421 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 868AA 21373 TUL - FOUND CORRODED SHEAR TIE STATION 1148 STRIGNER 26L. REPLACED SHEAR TIE. (M) 2 L 7 3 4F A3WE 1999062500899 19990625 00899 NM 1999 6 25 AALA990552 1 19990416 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 525 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 868AA 21373 TUL - FOUND CORROSION ON STRINGER 28L AT BS 525, REMOVED CORROSION MADE STRINGER OUT OF LIMITS. INSTALLED STRINGER REPA IR AS PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999062500900 19990625 00900 NM 1999 6 25 AALA990553 1 19990421 A 5330 PANEL BOEING 727 727223 1384074 NM BS 1166-1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 868AA 21373 TUL - AFT LAVATORY SERVICE PANEL BULGING AT BOTTOM. REPAIRED SECTION OF SKIN DOUBLER PER SRM 53-30-3. INSTALLED NEW LA VATORY PAN TRIPLER. REINSTALLED LAVATORY PAN DUMP LINE, FILL LINES AND CABLES. (M) 2 L 7 3 4F A3WE 1999062500901 19990625 00901 NM 1999 6 25 AALA990554 1 19990413 A 5330 SKIN BOEING 727 727223 1384074 NM BS 196.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - FOUND CRACK IN FUSELAGE SKIN STATION 196.5 WL 223 LEFT SECTION 41. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53 -30-3 FIG 3 PAGES 12-14A. (M) 2 L 7 3 4F A3WE 1999062500902 19990625 00902 NM 1999 6 25 AALA990555 1 19990416 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - SKIN CORRODED AT BUTT JOINT AT BS 680. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND REINSTALLED INTERCO STAL. (M) 2 L 7 3 4F A3WE 1999062500903 19990625 00903 NM 1999 6 25 AALA990556 1 19990419 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 601 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - OUTBOARD TOP FLANGE OF STRINGER 27L LT GOUGED STATION 601. CUT OUT DAMAGED SECTION AND INSTALLED STRINGER, REPAIR SPLICES AND FILLERS PER SRM 53-10-3 FIG 1 AND REINSTALLED INTERCOSTAL REMOVED FOR ACCESS. (M) 2 L 7 3 4F A3WE 1999062500904 19990625 00904 NM 1999 6 25 AALA990557 1 19990416 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 740 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - FOUND FLOORBEAM UPPER FLANGE CRACKED STATION 740 AT RT INBOARD SEAT TRACK RBL 24. STOPPED DRILLED CRACKS AND INST ALLED DOUBLERS PER SRM 53-10-8 PAGES 18-23. (M) 2 L 7 3 4F A3WE 1999062500905 19990625 00905 NM 1999 6 25 AALA990558 1 19990416 A 5320 WEB BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - FOUND BS 1183 WEB CRACKED. INSTALLED DOUBLER REPAIR ON FORWARD SIDE BS 1183 WEB. (M) 2 L 7 3 4F A3WE 1999062500906 19990625 00906 NM 1999 6 25 AALA990559 1 19990419 A 5531 SPAR WEB BOEING 727 727223 1384074 NM VERT STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - FOUND CRACK IN VERTICAL SKIN REAR SPAR RIGHT JUST ABOVE FUSELAGE SKIN. INSTALLED DOUBLER IAW SRM 55-30-3. (M) 2 L 7 3 4F A3WE 1999062500907 19990625 00907 NM 1999 6 25 AALA990560 1 19990416 A 5720 SPLICE BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - FOUNS STRINGER SPLICE CORRODED. INSTALLED NEW STRINGER SPLICE AT STATION 680 STRINGER 27L PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999062500908 19990625 00908 NM 1999 6 25 AALA990561 1 19990419 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - FOUND CRACK INDICATED ON WEB SURFACE EXTENDING FROM BOLT HOLE OT FASTENER, 12 INCHES FROM TOP OF BS 560 FRAME. DY E CHECKED AREA TO CONFIRM CRACK TERMINATED IN BOLT AND FASTENER HOLES. FOUND NO FURTHER CRACK PROGRESSION. INSTALLED D OUBLER PER SRM 51-4-2 PAGE 1 FIG 1. (M) 2 L 7 3 4F A3WE 1999062500909 19990625 00909 NM 1999 6 25 AALA990562 1 19990420 A 5414 SKIN BOEING 727 727223 1384074 NM NR 3 PYLON DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 TUL - FOUND 4 HOLES THROUGH SKIN ELONGATED AND OVERSIZED. INSTALLED DOUBLER PER ESO 11697, DATED 4-8-99. (M) 2 L 7 3 4F A3WE 1999062500910 19990625 00910 NM 1999 6 25 AALA990563 1 19990420 A 7120 MOUNT BOEING 727 727223 1384074 NM NR 3 ENGINE MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 708AA 22465 TUL - TWO HOLES WERE DOUBLE DRILLED ON UPPER AFT FLANGE OF FORWARD NR 3 ENGINE MOUNT. INSTALLED NEW NR 3 ENGINE FORWARD MOUNT PER ESO 11697, DATED 2-11-99, 2-18-99 AND 4-13-99. (M) 2 L 7 3 4F A3WE 1999062500911 19990625 00911 NM 1999 6 25 AALA990564 1 19990329 A 5730 SKIN BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - HEAVY CORROSION ON OUTER SKIN OF NR 2 FUEL CELL AT STATION 847, LBL 28, WING CENTER SECTION. REMOVED 4 FASTENERS, BLENDED CORROSION. REMOVED .051 THICKNESS. REAMED HOLES 2ND OVER, COLD WORKED HOLES. INSTALLED 4 4 EACH 2ND OVERSIZE HI-LOCKS (SEALER) TREATED AND PRIMED. (M) 2 L 7 3 4F A3WE 1999062500912 19990625 00912 NM 1999 6 25 AALA990565 1 19990420 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND CORROSION AROUND INNER SKIN AROUND ICE LIGHT HOUSING LANDING AT BS 720B-720C AND STRINGER 14L-16L. REPAIRED PER SRM 53-30-3 AREA AROUND ICE LIGHT HOUSING, AND ESO 11697 (PAN HEAD HI-LOCKS) 2 EACH, 4-9-99. (M) 2 L 7 3 4F A3WE 1999062500913 19990625 00913 NM 1999 6 25 AALA990566 1 19990419 A 5511 SPAR BOEING 727 727223 1384074 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND LEFT HORIZ STAB REAR SPAR CHORD UPPER END HAS 1 INCH AREA OF CORROSION BETWEEN NR 6 AND NR 7 ELEV HINGE BEAR ING. REPAIRED AREA OF CORROSION REMOVAL PER ESO 11697, DATED 3/30/99. (M) 2 L 7 3 4F A3WE 1999062500914 19990625 00914 NM 1999 6 25 AALA990567 1 19990401 A 5311 FRAME BOEING 727 727223 1384074 NM BS 375 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - REMOVED DAMAGE BY CUTTING OUT. INSTALLED DOBULER AND FILLER SRM 51-40-3 DOUBLER MATERIAL 7075-T6 .063 INCH THICK FILLER .050 INCH 7075-T6 FASTENERS (10 EACH) .1875 PROTRUDING HD HI-LOCKS (4) .1875 100 DEGREES COUNTERSUNK HD HI-LOCKS WITH TOTAL 14 INCH THIN ALUM WASHERS CPN 592217. (M) 2 L 7 3 4F A3WE 1999062500915 19990625 00915 NM 1999 6 25 AALA990568 1 19990331 A 5320 SILL BOEING 727 727223 1384074 NM BS 970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 970 STRINGER 27 RIGHT DOOR CUT OUT CORRODED CHORD ANGLE, SILL PLATE LOWER. BLENDED CORROSION, HFEC FASTENER HOLES. LIGHTLY SPOTFACED FASTENERS HOLES, AND FLAP PEENDED REWORK AREA PER ESO11697, DATED 3/29/99. (M) 2 L 7 3 4F A3WE 1999062500916 19990625 00916 NM 1999 6 25 AALA990569 1 19990330 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - STATION 950A STIRNGER 19R, BELT FRAME HAS DEEP WEAR FROM CEILING PANEL, DAMAGE ON FREE FLANGE. INSTALLED DOUBLER PER 51-40-3. NO CUT OUT REQUIRED. DOUBLER PUT ON TOP OF FREE FLANGE AND WEB WAS .063 7075 MATERIAL 5.5 INCH LONG. 1 R OW OF 6 HI-LOCKS BACB30FN6-4 IN FREE FLANGE. WEB HAD 2 ROWS OF HI-LOCKS 1ST OVERSIZED. 1ST ROW WAS .1875 INCH BACB30FP 6-4, 2ND ROW WAS .1875 INCH BACB30FP6-3. (M) 2 L 7 3 4F A3WE 1999062500917 19990625 00917 NM 1999 6 25 AALA990570 1 19990407 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND CORROSION ON SHEAR TIE FS 1130 AT STRINGER 30. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIGINAL FASTENER LOCATIONS. FASTENERS THROUGH FRAME .1875 INCH HI-LOCKS. FASTENERS THROUGH SKIN ORIGINAL SIZE AND TY PE REF 51-10-1. (M) 2 L 7 3 4F A3WE 1999062500918 19990625 00918 NM 1999 6 25 AALA990571 1 19990407 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND CORROSION ON SHEAR TIE AFT SIDE FS 1130, STRINGER 28 LEFT OUTBOARD. REMOVED CORRODED SHEAR TIE AND INSTALLE D NEW SHEAR TIE USING ORIG FASTENER LOCATIONS. FASTENERS THROUGH FRAME .1875 INCH HI-LOCKS. FASTENERS THROUGH SKIN RIV ET ORIGINAL SIZE AND TYPE. (M) 2 L 7 3 4F A3WE 1999062500919 19990625 00919 NM 1999 6 25 AALA990572 1 19990407 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND CORROSION ON SHEAR TIE AFT OF FS 1130 AT STRINGER 29 LEFT. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHE AR TIE USING ORIGINAL FASTENER LOCATIONS. FASTENER THROUGH FRAME .1875 HI-LOCKS. FASTENERS THROUGH SKIN ORIGINAL SIZE ADN TYPE REF 51-10-1. (M) 2 L 7 3 4F A3WE 1999062500920 19990625 00920 NM 1999 6 25 AALA990573 1 19990412 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND CORROSION AT FASTENER HOLES FOR CEILIG PANEL ATTACHMENT. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 4-9-99 USING 7075T6 .080 1 INCY BY 16.5 INCH OAL. (M) 2 L 7 3 4F A3WE 1999062500921 19990625 00921 NM 1999 6 25 AALA990574 1 19990414 A 5320 STRAP BOEING 727 727223 1384074 NM BS 620 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUD STRINGER 614-619 ABOVE STRINGER 26R UPPER CHORD ANGLE LOWER TAPERED STRAP DOUBLER CORRODED AROUND 3 NUT PLATE S. REMOVED AND REPLACED TAPERED STRAP. (M) 2 L 7 3 4F A3WE 1999062500922 19990625 00922 NM 1999 6 25 AALA990575 1 19990326 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND FRAME 720 DENTED BETWEEN STRINGER 25L AND 24L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51 -40-3. (M) 2 L 7 3 4F A3WE 1999062500923 19990625 00923 NM 1999 6 25 AALA990576 1 19990403 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1177 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STRINGER 30 CORRODED AT STATION 1177. INSTALLED NEW SECTION OF STRINGER STATION 1156-1183 WITH NEW SPLICE B ETWEEN STATION 1148 AND 1166 PER SRM 51-10-3 PAGE 3, NEW END FITTING INSTALLED AT 1183 ALODINED AND PRIMERED ALL PARTS. (M) 2 L 7 3 4F A3WE 1999062500924 19990625 00924 NM 1999 6 25 AALA990577 1 19990401 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STRINGER 29L CORRODED AROUND FASTENER, OUTBOARD LEG AFT OF STATION 950B TO 950B PLUS 1 INCH. REPAIRED PER E SO 11697 DATED 4-1-99 USING GENERAL GUIDE LINES OF SRM 51-40-4. INSTALLED STRAP REPAIR. (M) 2 L 7 3 4F A3WE 1999062500925 19990625 00925 NM 1999 6 25 AALA990578 1 19990329 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 680 BELLFRAME BENT BETWEEN STRINGER 24L AND 23L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999062500926 19990625 00926 NM 1999 6 25 AALA990579 1 19990326 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND BELLFRAME DENTED BETWEEN STRINGERS 24L AND 22L AT STATION 520. REMOVED DAMAGED AREA OF BELTFRAME AT STRIGNE R 23L AND REPAIRED PER SRM 51-40-2 PAGE 1-5 SHEET 3. DENTS AT 22L AND 24L FOUND TO BE WITHIN LIMITS. (M) 2 L 7 3 4F A3WE 1999062500927 19990625 00927 NM 1999 6 25 AALA990580 1 19990331 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 560 BELLFRAME DENTED IN BETWEEN STRINGERS 24L AND 25L. CUT OUT DAMAGE 1 INCH BY 1.25 INCH AND INSTA LLED DOUBLER PER SRM 51-40-3 PAGE 1-5. MATERIAL .063 INCH 7075T-6, 9 INCH LONG USING 27MS20470D, .1875 INCH RIVETS, 3 R OWS PAST DAMAGE, 1 ON TOP. (M) 2 L 7 3 4F A3WE 1999062500928 19990625 00928 NM 1999 6 25 AALA990581 1 19990329 A 5311 FRAME BOEING 727 727223 1384074 NM BS 580 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 580 BELLFRAME DENTED FROM STRINGER 24L TO 22L. REMOVED AND CUTOUT 3 DAMAGED AREAS (SIZES NOTED ABOV E). INSTALLED .063 DOUBLER, 7075-T6, 20 INCH LONG. INSTALLED 55-MS20470D, .1875 RIVETS AND 4 MS20470D, .25 INCH RIVETS , 3 ROWS TOTAL PER SRM 51-40-3, FIG 1. (M) 2 L 7 3 4F A3WE 1999062500929 19990625 00929 NE 1999 6 25 VTZA990131 2 19990602 A 7200 310349015 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FAILED A VTZA C ABORTED TAKEOFF Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 EA 27 322UE 41058 P76036 FLT 7167 - IAD-GSO - ABORTED TAKEOFF AFTER OBSERVING RIGHT ENGINE TQ SPIKE AND RIGHT OIL CONTAMINATION LIGHT. MAINTENAN CE INSPECTED AND REMOVED AND REPLACED RIGHT ENGINE. COMPLIED WITH PERFORMANCE RUNS. ALL PARAMETERS GOOD. OPS CHECK OK . AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999062500930 19990625 00930 EU 1999 6 25 USAAF99023 1 19990423 A 3231 RETRACT MECH FOKKER F28 F28MK0100 4990807 EU LT MLG DOOR OUT OF ADJUST A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 880US 11331 CLT - FLIGHT 1118 - ON APPROACH TO CLT, WHEN THE LANDING GEAR WAS SELECTED DOWN, A 'L MLG UNSAFE' WARNING MESSAGE APPEAR ED. THE L MLG GREEN SAFE INDICATOR DID NOT ILLUMINATED AND THE BLUE HANDLE LIGHT STAYED ILLUMINATED. CREW PERFORMED AL TERNATE GEAR EXTENSION. FLIGHT LANDED CLT WITHOUT FURTHER INCIDENT. HOWEVER, THE GEAR DOORS DRAGGED ON THE GROUND ON R OLLOUT. MAINTENANCE RIGGED THE LEFT MAIN LANDING GEAR SIDE STAY CLEARANCE 'X' PER FOKKER AMM 32-11-02. REPLACED THE LE FT GEAR DOOR SKID PLATE AND THE RIGHT GEAR DOOR ASSEMBLY DUE TO DAMAGE FROM THE DOORS DRAGGING ON ROLLOUT. (M) 2 L 7 2 4F RT 1999062500931 19990625 00931 NM 1999 6 25 ASAA9910122 1 19990520 A 5347 SEAT TRACK BOEING 737 7372Q8C 138448S NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK CORRODED ON TOP AND BOTTOM SIDES, BS 727B-747, BL 0. REPAIRED PER SRM 53-10-1. (M) 2 L 7 2 4F A16WE 1999062500932 19990625 00932 NM 1999 6 25 ASAA9910123 1 19990520 A 5347 SEAT TRACK BOEING 737 7372Q8C 138448S NM BS 864.5 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND THE MAIN CABIN SEAT TRACK GOUGED BS 864.5, LBL 45.5. REPAIRED PER SRM 53-10-5, FIG 8. (M) 2 L 7 2 4F A16WE 1999062500933 19990625 00933 NM 1999 6 25 ASAA9910124 1 19990520 A 5320 DOUBLER BOEING 737 7372Q8C 138448S NM BS 847 MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND DOUBLE HOLES IN AFT CARGO DOOR, AFT FRAME SKIN DOUBLE FROM STRINGER 20 TO 24 RT, BS 847. RE PAIRED PER EA 5330-01377. (M) 2 L 7 2 4F A16WE 1999062500934 19990625 00934 NM 1999 6 25 ASAA9910125 1 19990520 A 5313 STRINGER BOEING 737 7372Q8C 138448S NM BS 927 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND STRINGER 21R CORRODED BEYOND LIMITS AT BS 927. REPAIRED PER SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 1999062500935 19990625 00935 NM 1999 6 25 ASAA9910126 1 19990520 A 5313 STRINGER BOEING 737 7372Q8C 138448S NM BS 365 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING D-CHECK, FOUND STRINGER 27R AND ADJACENT SKIN CORRODED AT BS 365. REPAIRED PER SRM 51-10-3. (M) 2 L 7 2 4F A16WE 1999062500936 19990625 00936 NM 1999 6 25 ASAA9910127 1 19990520 A 5313 65516985 STRINGER BOEING 737 7372Q8C 138448S NM BS 906 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING 'D' CHECK, FOUND OUTBOARD SIDE OF STRINGER 25L AT STATION 906 CORRODED. REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1999062500937 19990625 00937 NM 1999 6 25 ASAA9910128 1 19990520 A 5330 SKIN BOEING 737 7372Q8C 138448S NM BS 827 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 PHX - DURING 'D' CHECK, FOUND EXTERNAL FUSELAGE SKIN AT BS 827, STRINGER 20L DENTED WITH RIPPLES GOING AFT. REPAIRED PE R SRM 53-30-3, FIG 1. (M) 2 L 7 2 4F A16WE 1999062500938 19990625 00938 NM 1999 6 25 ASAA9940110 1 19990503 A 5315 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PHX - DURING SI CHECK, FOUND FLOORBEAM T-CAP AT BS 986, RBL 8 CORRODED ON AFT FLANGE. REPAIRED PER SRM 53-00-51, FIG 20 3. (M) 2 L 7 2 4F RT A16WE 1999062500939 19990625 00939 NM 1999 6 25 ASAA9940111 1 19990503 A 5315 FLOORBEAM BOEING 737 737490 1384715 NM BS 947.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PHX - DURING SI CHECK, FOUND FLOORBEAM T-CAP AT BS 947.5, RBL 48 CORRODED AROUND SCREW HOLES ON FORWARD SIDE. REPAIRED PER SRM 53-60-51, FIG 203. (M) 2 L 7 2 4F RT A16WE 1999062500940 19990625 00940 NM 1999 6 25 ASAA9940112 1 19990503 A 5315 FLOORBEAM BOEING 737 737490 1384715 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PHX - DURING SI CHECK, FOUND MAIN FLOORBEAM T-CAP AT BS 967, LBL 30 CORRODED AROUND SCREW HOLES ON TOP AND BOTTOM SIDES. REPAIRED PER SRM 53-60-51, FIG 203. (M) 2 L 7 2 4F RT A16WE 1999062500941 19990625 00941 NM 1999 6 25 ASAA9940113 1 19990503 A 5315 BAC15052426 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PHX - DURING SI CHECK, FOUND MAIN FLOORBEAM T-CAP AT BS 986, LBL 34 CORRODED AROUND SCREW HOLES. REPAIRED PER SRM 53-60 -51, FIG 203. (M) 2 L 7 2 4F RT A16WE 1999062500942 19990625 00942 NM 1999 6 25 ASAA9940114 1 19990503 A 5320 654587570 ANGLE BOEING 737 737490 1384715 NM BS 297-337 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PHX - DURING SI CHECK, FOUND MAIN CABIN RIGHT CUSP ANGLE AT STATION 279-337 CORRODED ON UPPER SURFACE OF HORIZONTAL FLAN GE. REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1999062500943 19990625 00943 NM 1999 6 25 ASAA9940115 1 19990503 A 5315 65C33941 FLOORBEAM BOEING 737 737490 1384715 NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 PHX - DURING SI CHECK, FOUND MAIN CABIN FLOORBEAM CORRODED AT STATION 312, LBL 1. REPAIRED PER SRM 53-10-51, FIG 205. ( M) 2 L 7 2 4F RT A16WE 1999062500944 19990625 00944 NM 1999 6 25 ASAA9940117 1 19990527 A 5210 MECHANISM BOEING 737 7374Q8 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 754AS 25095 PDX - PRIOR TO FLIGHT 409, CREW REPORTED THAT THE L1 DOOR WAS DIFFICULT TO CLOSE. INSPECTED, CLEANED, AND LUBRICATED DO OR. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999062500945 19990625 00945 NM 1999 6 25 ASAA9940118 1 19990527 A 5610 BOLT BOEING 737 737490 1384715 NM LT COCKPIT LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 791AS 28886 SEA - PRIOR TO FLIGHT 426 - CREW REPORTED THAT THE CAPTAINS WINDOW WAS BINDING. INSPECTED AND FOUND THAT THE LOWER ROLL ER BEARING ATTACH BOLT WAS LOOSE. TIGHTENED BOLT. CLEANED AND LUBRICATED TRACK. WINDOW OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999062500946 19990625 00946 NM 1999 6 25 ASAA9940119 1 19990527 A 2560 61621469 SLIDE BOEING 737 737490 1384715 NM L2 DOOR PRESSURE LOW A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 799AS 1400 29270 PAE - DURING MAINTENANCE CHECK, THE L2 DOOR EVACUATION SLIDE BOTTLE PRESSURE WAS FOUND TO BE LOW. REPLACED EVACUATION S LIDE AND ROUTED TO ASA SLIDE SHOP WHERE THE BOTTLE WAS REPLACED. (M) 2 L 7 2 4F RT A16WE 1999062500947 19990625 00947 NM 1999 6 25 F3LA99051 1 19990603 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 500 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 DEN - DURING C-CHECK, INSPECTION REPORTED EXFOLIATION CORROSION IN FORWARD CARGO COMPARTMENT, ARUOND FLOOR EDGE BEAM NUT PLATE, AT BS 500A, ABOVE S 26R. MAINTENANCE REMOVED FLOOR EDGE BEAM, BURNISHED CORROSION AND REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1999062500948 19990625 00948 NM 1999 6 25 F3LA99052 1 19990603 A 5311 FRAME BOEING 737 7372L9 1384497 NM CARGO COMPT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 DEN - DURNG C-CHECK INSPECTION, REPORTED CORROSION ON UNDER SIDE OF RIGHT FLOOR TO SIDEWALL FRAME. EXTENDING AFT OF FOR WARD CARGO DOOR TO AIR DISTRIBUTION BAY. MAINTENANCE REMOVED FRAME, BURNISHED CORROSION AND REPAIRED PER SRM 51-40-2. ( M) 2 L 7 2 4F RT A16WE 1999062500949 19990625 00949 WP 1999 6 25 HALA9900130 1 19990522 A 5400 RA2300118 BOLT DOUG DC10 DC1010 3022110 WP NR 1 PYLON BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 TUL - FLT 4101 - FUEL LEAK LEFT WING NR 1 ENGINE PYLON AREA. FOUND NR 1 PYLON FOOTSTOOL LOWER INBOARD, OUTBOARD BOLT BR OKEN, NR 4. REPLACED BOLT PER AD96-06-08 WITH (H11 TYPE) INCONEL PER AD. (M) 2 L 7 3 4F A22WE 1999062600001 19990626 00001 NM 1999 6 26 UPS99629765 1 19990605 A 4950 380029817 THERMOCOUPLER BOEING 767 76734AF 1385212 NM APU INOPERATIVE A IPXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 324UP 27750 INSPECTION TYPE:ETOP APU AIR INOP. *S/D* PERFORMED ECU BITE, FOUND NR 2 EGT LRU FAULT. REMOVED AND REPLACED RT SIDE T HERMOCOUPLERS PER B767 MM 49-71-01 PAGE 401. APU CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999062600002 19990626 00002 EU 1999 6 26 QXEA9901238 1 19990605 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - UPPER NAV/COMM ANTENNA HAS MULTIPLE PITS ON FUSELAGE SKIN UNDER ANTENNA. REPAIRED IAW HORIZON AIR EA 4-53-821. 2 L 7 2 4F RT A20EU 1999062600003 19990626 00003 EU 1999 6 26 QXEA9901239 1 19990529 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION AT EDGE OF SKIN CUTOUT AND AROUND RIVETS 6 AFT OF FRAME 9305A, BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-4 PARAGRAPH 3A, STEPS 1-3. 2 L 7 2 4F RT A20EU 1999062600004 19990626 00004 EU 1999 6 26 QXEA9901240 1 19990526 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 74 HAS TOP SURFACE CORROSION BETWEEN FRAMES 9305A AND 9305B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PA RAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999062600005 19990626 00005 EU 1999 6 26 QXEA9901241 1 19990523 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 9305 AT STRINGER 73, 4 WAY TIE-IN FOR FLOOR SUPPORT HAS CORROSION ON TOP SIDE. REPAIRED IAW FOKKER SRM 51-1 0-4, PAGE 9, PARAGRAPH 4 B AND C. 2 L 7 2 4F RT A20EU 1999062600006 19990626 00006 EU 1999 6 26 QXEA9901242 1 19990526 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - STRINGER 74 HAS CORROSION ON TOP SIDE WHERE IT PASSES THROUGH FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 , PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999062600007 19990626 00007 EU 1999 6 26 QXEA9901243 1 19990526 A 5320 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 9305 SHEAR TIE CLIP HAS CORROSION ON FORWARD SIDE OF FRAME WHERE CUTOUT IS FOR STRINGER 74 PASS THROUGH. RE PAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999062600008 19990626 00008 EU 1999 6 26 QXEA9901244 1 19990526 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 AT STRINGER 74 HAS CORROSION AT UNDERSIDE OF TOP FLANGE AROUND NUT PLATES AT 4 WAY TIE-IN. REPAIRED IA W FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999062600009 19990626 00009 EU 1999 6 26 QXEA9901245 1 19990523 A 5320 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8805 SHEAR TIE CLIP HAS CORROSION, ALSO RIVET BUCK TAILS HAVE CORROSION BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND C. 2 L 7 2 4F RT A20EU 1999062600010 19990626 00010 EU 1999 6 26 QXEA9901246 1 19990526 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION AROUND BELLY DRAIN, AFT SIDE OF FRAME 8305 BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999062600011 19990626 00011 EU 1999 6 26 QXEA9901247 1 19990528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 7805-8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION IN AREA BETWEEN FRAMES 7805 AND 8305 AND STRINGERS 1 AND 2. R EPAIRED IAW FOKKER SRM 51-10-04, PAGE9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999062600012 19990626 00012 EU 1999 6 26 QXEA9901248 1 19990523 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 7805-8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FLOOR SUPPORT ANGLE BETWEEN FRAMES 7805 AND 8305 ABOVE STRINGER 3 HAS CORROSION AROUND NUT PLATES. REPAIRED IAW F OKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4BC. 2 L 7 2 4F RT A20EU 1999062600013 19990626 00013 EU 1999 6 26 QXEA9901249 1 19990526 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 7305-7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FORWARD CARGO BAY INTERIOR BELLY SKIN HAS CORROSION BETWEEN FRAME 7305, 7805 AND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999062600014 19990626 00014 EU 1999 6 26 QXEA9901250 1 19990523 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 8305 AT STRINGER 74 HAS CORROSION ON UNDERSIDE OF TOP FLANGE AROUND NUT PLATE HOLES AT 4 WAY TIE-IN. REPAIR ED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B AND C, SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999062600015 19990626 00015 EU 1999 6 26 QXEA9901251 1 19990519 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AFT CARGO BAY AT FRAME 13815 CLIP IS CRACKED BETWEEN STRINGER 73 AND 72. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 1. 2 L 7 2 4F RT A20EU 1999062600016 19990626 00016 EU 1999 6 26 QXEA9901252 1 19990516 A 5280 SKIN FOKKER F28 F28MK4000 4990810 EU RT MLG DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT-HAND INBOARD MAIN LANDING GEAR DOOR HAS IMPACT DAMAGE 6 FROM UNLOCK BRACKET. REPAIRED IAW FOKKER SRM 52-02- 01, PAGE 3, FIGURE 2. 2 L 7 2 4F RT A20EU 1999062600017 19990626 00017 EU 1999 6 26 QXEA9901253 1 19990526 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 7305 AT STRINGER 74 HAS CORROSION AROUND NUT PLATE FOR THE 4 WAY TIE-IN, UNDERSIDE OF TOP FLANGE OF FRAME. R EPAIRED IAW HORIZON AIR EA 4-53-808. 2 L 7 2 4F RT A20EU 1999062600018 19990626 00018 EU 1999 6 26 QXEA9901254 1 19990526 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 7305 AT STRINGER 1 HAS EXFOLIATION CORROSION AROUND NUT PLATE HOLE UNDERSIDE OF TOP FLANGE OF FRAME. REPAIR ED IAW HORIZON AIR EA 4-53-798 AND EA 4-53-808. 2 L 7 2 4F RT A20EU 1999062600019 19990626 00019 EU 1999 6 26 QXEA9901255 1 19990529 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 6805-7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FORWARD CARGO BAY BELLY SKIN HAS SURFACE CORROSION INSIDE BETWEEN FRAMES 6805 AND 7305 BETWEEN STRINGER 1 AND ANTE NNA DOUBLER. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999062600020 19990626 00020 EU 1999 6 26 QXEA9901256 1 19990528 A 5320 SHEAR TIE FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 7305 SHEAR TIE TOP SURFACE HAS CORROSION BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 , PARAGRAPH 4B AND C. 2 L 7 2 4F RT A20EU 1999062600021 19990626 00021 EU 1999 6 26 QXEA9901257 1 19990527 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 6805 AT STRINGER 74 HAS CORROSION UNDERSIDE OF TOP FLANGE OF FRAME AROUND NUT PLATES FOR THE 4 WAY TIE-IN. R EPAIRED IAW HORIZON AIR EA 4-53-799. 2 L 7 2 4F RT A20EU 1999062600022 19990626 00022 EU 1999 6 26 QXEA9901258 1 19990522 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 6805 AT STRINGER 1 HAS CORROSION UNDERSIDE OF TOP FLANGE OF FRAME AROUND NUT PLATES FOR THE 4 WAY TIE-IN. R EPAIRED IAW HORIZON AIR EA 4-53-799. 2 L 7 2 4F RT A20EU 1999062600023 19990626 00023 EU 1999 6 26 QXEA9901259 1 19990522 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 6305 LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - 90 DEGREE FLOOR SUPPORT BRACKET AT FRAME 6305 AND STRINGER 3 HAS LOOSE ATTACH RIVETS FORWARD SIDE OF FRAME. REPAI RED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999062600024 19990626 00024 EU 1999 6 26 QXEA9901260 1 19990519 A 5320 RIVETS FOKKER F28 F28MK4000 4990810 EU FRAME 5805 MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FRAME 5805 HAS 90 DEGREE BRACKET AT AFT SIDE BETWEEN STRINGERS 4 AND 5 WITH 2 MISSING RIVETS. REPAIRED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999062600025 19990626 00025 EU 1999 6 26 QXEA9901261 1 19990522 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - FORWARD CARGO BAY FRAME 5305 HAS CORROSION AROUND 2 NUT PLATES ON UNDERSIDE OF TOP FLANGE OF C-CHANNEL AT STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-800. 2 L 7 2 4F RT A20EU 1999062600026 19990626 00026 EU 1999 6 26 QXEA9901262 1 19990601 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT-HAND INBOARD PASSENGER SEAT TRACK HAS 2 SUPPORT RISERS AT THE INBOARD AND OUTBOARD FLANGES AT FRAME 4610 TIE IN TABS CRACKED, UNDERSIDE OF FLANGES. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, STEPS 1-5. 2 L 7 2 4F RT A20EU 1999062600027 19990626 00027 EU 1999 6 26 QXEA9901263 1 19990519 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT-HAND DIAGONAL C-CHANNEL PORTION OF FRAME 5305 ABOVE STRINGER 65 HAS CORROSION AROUND LOWER NUT PLATE AND THE AFT FACE OF FRAME. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B AND C, SRM 51-31-02 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999062600028 19990626 00028 EU 1999 6 26 QXEA9901264 1 19990528 A 2150 DUCT FOKKER F28 F28MK4000 4990810 EU ACM EXHAUST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - RIGHT-HAND ACM EXHAUST DUCT IS CRACKED AT TOP AFT CORNER. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999062600029 19990626 00029 EU 1999 6 26 QXEA9901265 1 19990605 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU RT MLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - THERE IS A CRACKED STRINGER AT TOP STRUCTURE IN RIGHT-HAND MAIN LANDING GEAR STRUT BAY, DIRECTLY ABOVE THE GEAR ST RUT AFT LUG. REPAIRED IAW FOKKER SRM 51-31-1 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999062600030 19990626 00030 EU 1999 6 26 QXEA9901266 1 19990519 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - AFT CARGO BAY AT FRAME 13815 CLIP IS CRACKED BETWEEN STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 1 . 2 L 7 2 4F RT A20EU 1999062600031 19990626 00031 EU 1999 6 26 QXEA9901267 1 19990519 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - TCAS ANTENNA DOUBLER INSIDE FORWARD CARGO BAY HAS CORROSION, 3 FORWARD OF FRAME 4610 BETWEEN STRINGER 1 AND 74. R EPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4 A, B, C. 2 L 7 2 4F RT A20EU 1999062600032 19990626 00032 EU 1999 6 26 QXEA9901268 1 19990528 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU LT MLG WW DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT-HAND MAIN LANDING GEAR DOOR WHEEL BAY OUTER SKIN HAS A OPENING IN THE SKIN. REPAIRED IAW FOKKER SRM 52-02-01 , PAGE 3, FIGURE 1 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999062600035 19990626 00035 NM 1999 6 26 AWXA9900223 1 19990617 A 2611 824PY SMOKE DETECTOR BOEING 737 737277 1384570 NM LAVATORY SOUNDED A AWXA O OTHER N FALSE WARNING CR CRUISE 1 WP 28 186AW 22653 SMOKE ALARM IN FORWARD LAV SOUNDED FOR A SHORT TIME IN FLIGHT. CHECKED FOR SMOKE OR FIRE AND NONE NOTED. NO OTHER PROB LEMS DURING FLIGHT. FORWARD LAV SMOKE DETECTOR TESTED OK AT THIS TIME. 2 L 7 2 4F RT A16WE 1999062600036 19990626 00036 WP 1999 6 26 TWAA9908701 1 19990622 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 6-16 DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 926TW 49356 THE CABIN EGRESS LIGHTS FROM ROWS 6 TO 16 CAME ON IN FLIGHT. DURING TROUBLESHOOTING FOUND THE FORWARD CABIN EGRESS LIGH TS WERE INOPERATIVE. REPLACED THE NUMBER 2 BATTERY PACK FOR THE LIGHTS ON IN FLIGHT, AND CLEANED MOISTURE FROM THE LIGH T TRACK FOR THE INOPERATIVE FORWARD CABIN MALFUNCTION. CHECK-C 10-18-98 STL. 2 L 7 2 4F A6WE 1999062600037 19990626 00037 WP 1999 6 26 TWAA9908706 1 19990622 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 6-16 MALFUNCTIONED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 926TW 49356 THE CABIN EGRESS LIGHTS AT ROWS 6 TO 16 WERE ILLUMINATED REGARDLESS OF SWITCH POSITION. RECYLED THE EGRESS LIGHT SYSTEM . CHECK-C 10-18-98 STL. 2 L 7 2 4F A6WE 1999063000001 19990630 00001 NM 1999 6 30 MWEA99361 1 19990621 A 2560 D29985107 SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 AFT GALLEY SLIDE PACK CAME OUT OF HOLDER. REINSTALLED SLIDE INTO COVER. 2 L 7 2 4F RT A6WE 1999063000002 19990630 00002 WP 1999 6 30 MWEA99360 1 19990621 A 2560 113317DG SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 FORWARD ENTRANCE DOOR ESCAPE SLIDE COVER POPPED LOOSE AT ITS BOTTOM FITTING. REINSTALLED COVER. 2 L 7 2 4F A6WE 1999063000003 19990630 00003 WP 1999 6 30 MWEA99359 1 19990621 A 5311 99582041 FRAME DOUG DC9 DC914 3022034 WP BS 566 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 THE FRAME AT STATION 566 HAS A CHAFE MARK JUST ABOVE CUSP LINE. MTC FABRICATED REPAIR STRAP AND INSTALLED. 2 L 7 2 4F A6WE 1999063000004 19990630 00004 WP 1999 6 30 MWEA99358 1 19990622 A 5311 9911538507N FRAME DOUG DC9 DC914 3022034 WP BS 604 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 CRACK AT STATION 604 FRAME ON LEFT WHEEL WELL. MTC REMOVED AND REPLACED FRAME. 2 L 7 2 4F A6WE 1999063000005 19990630 00005 WP 1999 6 30 MWEA99357 1 19990620 A 2560 CLIP DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE BROKEN A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 THE FORWARD PASSENGER DOOR SLIDE RETAINING CLIP BROKE. MTC REINSTALLED FORWARD PASSENGER DOOR SLIDE COVER RETAINING CLI P. 2 L 7 2 4F A6WE 1999063000006 19990630 00006 EU 1999 6 30 VTZA990136 1 19990605 A 3240 SWITCHES JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 320UE 41043 FLT 7668 - IAD-BDL - ABORTED TAKEOFF DUE TO TOCWS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INS PECTED AND CLEANED PARKING BRAKE AND CONDITION LEVERS MICROSWITCHES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200001 19990702 00001 NE 1999 7 2 GXPA99002 2 19990529 A 7321 327B459P9 BELLOWS HAMFLU HFB320 HFB320 4071204 EU GE CJ610 CJ6105 30006 NE FUEL CONTROL LOOSE A GXPA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 23 171GA 1039 240B249A LEFT ENGINE FLAME-OUT CLIMBING FROM FL 370 TO FL 390. ENGINE RE-LIGHT AT 5,000 FEET. FOUND 'P2' BELLOWS LOOSE AT FUEL CONTROL ENGINE. GROUND RUN GOOD AFTER RE-SECURING BELLOWS. (X) 2 L 7 2 4J 4 J A14EU 1E16 1999070200003 19990702 00003 CE 1999 7 2 99ZZZX2426 1 19990514 A 3260 CIRCUIT BREAKER CESSNA 310 310R 2074245 CE MLG MALFUNCTIONED A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 5215C 310R1515 GEAR WARNING CIRCUIT BREAKER TRIPPED NOT GIVING ANY GEAR DOWN INDICATION, LANDED IN DSM. MECHANIC JACKED AIRCRAFT, CYCL ED GEAR MANY TIMES. OPS CHECKED GOOD. RETURNED TO SERVICE. 1 L 7 2 3O 3A10 1999070200006 19990702 00006 CE 1999 7 2 99ZZZX2430 1 19990527 A 2460 99104941 TRANSFORMER CESSNA 500 550 2076604 CE LT PYLON CHAFED A L NVIA O OTHER O OTHER NR NOT REPORTED 1 SW 05 100WT 8392 5500858 WITH RT ENGINE RUNNING AND RT GEN ON-LINE, GEN ASSIST START WAS OPERATIONAL. IF LT ENG WAS RUNNING AND LT GEN ON-LINE, ATTEMPTING A RT START WOULD CAUSE LT GEN TO DROP OFF-LINE AND RT ENG WOULD NOT ROTATE. T/S TO A CT3 (LT GROUND FAULT XF ORMER) WHICH HAD CHAFED AGAINST LT ENG COWLING ATTACH BRACKET AND HAD BEEN RENDERED USELESS. REPLACED LT PYLON CT3 GROU ND FAULT XFORMER WITH NEW PART, SAME P/N, AND SYS WORKED PROPERLY. INSPECTED RT GROUND FAULT XFORMER, FOUND SIGNIFICANT CHAFING AGAINST THE RT COWLING ATTACH BRACKET. REPLACED RT PYLON GROUND FAULT XFORMER WITH NEW PART, SAME P/N, OBSERV ED OTHER CHAFING OCCURRING ON BOTH COWLING ATTACH BRACKETS. 1 L 7 2 4F A22CE 1999070200023 19990702 00023 1999 7 2 9902129154 4 19990621 A 3442 RADAR IND DOUG DC9 DC914 3022034 WP COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8913E 45830 AFTER TAKEOFF, THE RADAR WEATHER SPOKED IN ALL MODES. ONLY 20 PERCENT OF SCREEN PAINTED ANY RETURNS AND RETURNS MOVED W ITH EACH SWEEP. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. EMERGENCY DECLARED FOR OVERWEIGHT LANDING. MAINTE NANCE REPLACED THE RADAR INDICATOR AND CONTROL PANEL AND PERFORMED OVERWEIGHT LANDING INSPECTION OF AIRCRAFT. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1999070200024 19990702 00024 NM 1999 7 2 9902135527 1 19990618 A 2710 CONTROL MIXER BOEING 757 757251 1384970 NM RT AILERON MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 527US 23842 EN ROUTE DTW-SFO CLIMBING THROUGH FL180, CREW REPORTED UNCOMMANDED RIGHT AILERON MOVEMENT. AN EMERGENCY WAS DECLARED. T HE FLIGHT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LATERAL CONTROL MIXER AND RIGGED THE AI LERON CONTROL SYSTEM. AILERON SYSTEM TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999070200025 19990702 00025 WP 1999 7 2 9902149614 1 19990621 A 3260 SENSOR DOUG DC9 DC932 3022066 WP NLG INOPERATIVE A NWAA K NONE N FALSE WARNING DE DESCENT 1 GL 01 614NW 47128 DURING DESCENT AND THROTTLES AT IDLE, THE NOSE LANDING GEAR GREEN INDICATION LIGHT ILLUMINATED ALONG WITH THE LANDING GE AR UNSAFE LIGHTS. ON FINAL APPROACH, THE FLIGHT CREW RECYCLED THE LANDING GEAR SYSTEM AND THE CONDITION REMAINED. IN B OTH INSTANCES, THE LANDING GEAR WAS CLEARLY UP AND LOCKED WITH THE GREEN INDICATION LIGHT ILLUMINATED. AIRCRAFT LANDED AT MSP WITHOUT INCIDENT. MAINTENANCE REPLACED THE BASE FOR NOSE LANDING GEAR GREEN INDICATION LIGHT AND THE NOSE LANDIN G GEAR LOCK SENSOR T2-61. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999070200026 19990702 00026 NM 1999 7 2 9902156307 1 19990619 A 3350 LIGHT BOEING 747 747451 1384940 NM ROW 22-43 INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK (PEK), FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 22-43. RECONNECTED LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999070200027 19990702 00027 NM 1999 7 2 9902166306 1 19990621 A 3350 CONNECTOR BOEING 747 747451 1384940 NM ROW 27 BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND C ZONE FLOOR PATH EMERGENCY LIGHT INOPERATIVE. REPAIRED LIGHT ASSEMBLY CONNECTOR AT ROW 27, OP ERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999070200028 19990702 00028 WP 1999 7 2 9902179604 1 19990621 A 3350 PLUG DOUG DC9 DC932 3022066 WP CATWALK INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE CHECK, FOUND EMERGENCY LIGHTING ON CATWALK INOPERATIVE. MAINTENANCE REPAIRED PLUG END ON WIRING HARNESS BR9 608-001. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999070200029 19990702 00029 SO 1999 7 2 COMA9910098 1 19990622 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 179CA 15663 120179 FLAPS FAIL WARNING. REPLACED THE FLAP ANNUNCIATOR UNIT. 2 L 7 2 4T RT A31SO 1999070200030 19990702 00030 EA 1999 7 2 COMA9960289 1 19990621 A 7110 228500205 COWL CF343A1 CNDAIR CL600 CL6002B19 EA RT ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 807412 7062 DURING MAINTENANCE SEVERAL CRACKS WERE FOUND ON INLET COWL AFT BULKHEAD OF RIGHT ENGINE. ENGINE INLET COWL WAS REPLACED . 2 L 7 2 4F RT A21EA 1999070200031 19990702 00031 EA 1999 7 2 COMA9960291 1 19990613 A 4980 601R972033 BLANKET CNDAIR CL600 CL6002B19 EA APU EXHAUST DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 LOWER APU EXHAUST HEAT BRACKET HAS HOLES. REPLACED HEAT BLANKET. 2 L 7 2 4F RT A21EA 1999070200032 19990702 00032 EA 1999 7 2 COMA9960292 1 19990613 A 4980 601R972035 BLANKET CNDAIR CL600 CL6002B19 EA APU EXHAUST DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 UPPER APU EXHAUST HEAT BLANKET HAS HOLES. REPLACED HEAT BLANKET. 2 L 7 2 4F RT A21EA 1999070200033 19990702 00033 EA 1999 7 2 COMA9960293 1 19990613 A 2730 12031007 DAMPENER CNDAIR CL600 CL6002B19 EA LT ELEVATOR LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 946CA 9625 2270 7072 LEFT INBOARD ELEVATOR FLUTTER DAMPENER LEAKING. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999070200034 19990702 00034 EA 1999 7 2 COMA9960294 1 19990612 A 5312 6013501252 BUKKHEAD ANGLE CNDAIR CL600 CL6002B19 EA AFT PRESS BLKHD CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 ANGLE BRACKET ON REAR PRESSURE BULKHEAD RIGHT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET. 2 L 7 2 4F RT A21EA 1999070200035 19990702 00035 EA 1999 7 2 COMA9960295 1 19990612 A 5312 6013501251 BULKHEAD ANGLE CNDAIR CL600 CL6002B19 EA AFT PRESS BLKHD CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 ANGLE BRACKET ON REAR PRESSURE BULKHEAD, LEFT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET. 2 L 7 2 4F RT A21EA 1999070200036 19990702 00036 EA 1999 7 2 COMA9960296 1 19990613 A 3350 58728 COVER CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 FLOOR EMERGENCY LIGHT STRIP TOP COVER BROKEN. REPLACED COVER. 2 L 7 2 4F RT A21EA 1999070200037 19990702 00037 EA 1999 7 2 COMA9960297 1 19990613 A 4980 601R972013 DUCT CNDAIR CL600 CL6002B19 EA APU EXHAUST BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 APU EXHAUST DUCT HAS SEVERAL BROKEN TABS. REPLACED DUCT. 2 L 7 2 4F RT A21EA 1999070200038 19990702 00038 EA 1999 7 2 COMA9960298 1 19990613 A 4980 15A107101 CLAMP CNDAIR CL600 CL6002B19 EA APU EXHAUST BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 APU EXHAUST FINGER CLAMP HAS BROKEN AND CHAFED FINGERS. REPLACED CLAMP. 2 L 7 2 4F RT A21EA 1999070200039 19990702 00039 EA 1999 7 2 COMA9960299 1 19990613 A 4980 601R9720913 DUCT CNDAIR CL600 CL6002B19 EA APU EXHAUST WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 APU EXHAUST SUPPORT DUCT ASSY IS WORN ON INBOARD SIDE. REPLACED DUCT. 2 L 7 2 4F RT A21EA 1999070200040 19990702 00040 EA 1999 7 2 COMA9960300 1 19990620 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 984CA 7171 FORWARD FUSELAGE EMERGENCY LIGHTING STRIP IS BROKEN. REPLACED LIGHTING STRIP. 2 L 7 2 4F RT A21EA 1999070200041 19990702 00041 EA 1999 7 2 COMA9960301 1 19990620 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PAX DOOR DAMAED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 PAX DOOR SEAL STRIKER DAMAGED AT FS 310, LOWER PART OF OPENING. REPAIRED PAX DOOR SEAL STRIKER IN ACCORDANCE WITH REO 6 01-52-11-008 REPAIR A. 2 L 7 2 4F RT A21EA 1999070200042 19990702 00042 EA 1999 7 2 COMA9960302 1 19990620 A 3350 58731 LIGHT CNDAIR CL600 CL6002B19 EA CABIN CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 EMERGENCY LIGHT FLOOR TRACK LIGHT (P/N 5873-1) IS CRACKED AND THE END CAPS ARE MISSING. REPLACED TRACK LIGHT. 2 L 7 2 4F RT A21EA 1999070200043 19990702 00043 EA 1999 7 2 COMA9960303 1 19990620 A 3350 58728 LIGHT CNDAIR CL600 CL6002B19 EA CABIN CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 EMERGENCY FLOOR TRACK LIGHT (P/N 5872-8) HAS SEVERAL BREAKS AND IS MISSING END CAPS. REPLACED TRACK LIGHT. 2 L 7 2 4F RT A21EA 1999070200044 19990702 00044 EA 1999 7 2 COMA9960304 1 19990620 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PASSENGER DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 7174 PAX DOOR SEAL STRIKER DAMAGED AT FS 310.00, LOWER PART OF PAX DOOR OPENING. REPAIRED IN ACCORDANCE WITH REO CRJ601R-52- 11-008 REPAIR A. 2 L 7 2 4F RT A21EA 1999070200045 19990702 00045 EA 1999 7 2 COMA9960305 1 19990620 A 5320 601R53610043 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 7174 CARGO FLOOR SUPPORT ANGLE AT FS 621.00, WL 73, RIGHT SIDE CRACKED. REPAIRED IN ACCORDANCE WITH CANADAIR REO 601R-53-61- 117 REV A. 2 L 7 2 4F RT A21EA 1999070200046 19990702 00046 EA 1999 7 2 COMA9960306 1 19990620 A 5320 601R53610043 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 7174 CARGO FLOOR SUPORT ANGLE AT FS 621.00, WL 73, LEFT SIDE IS CRACKED. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 1999070200047 19990702 00047 EA 1999 7 2 COMA9960307 1 19990620 A 5320 601R53610043 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 CARGO FLOOR SUPPORT ANGLE AT FS 621 WL 73, LEFT SIDE IS CRACKED. REPAIRED PER CANADAIR REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 1999070200048 19990702 00048 EA 1999 7 2 COMA9960308 1 19990620 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 FRAME FLANGE AT FS 718 STRINGER 11 ON RIGHT SIDE CRACKED. REPAIRED IN ACCORDANCE WITH WVAC E 601R-53-0075, SRM 51-42-21 . 2 L 7 2 4F RT A21EA 1999070200049 19990702 00049 EA 1999 7 2 COMA9960309 1 19990620 A 5320 60036030 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 DOUBLER CRACKED AT FS 718 AT STRINGER 11 ON RIGHT SIDE. REPLACED WITH NEW DOUBLER. 2 L 7 2 4F RT A21EA 1999070200050 19990702 00050 EA 1999 7 2 COMA9960310 1 19990620 A 5320 60036030 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 DOUBLER CRACKED AT FS 718 AT STRINGER 11 ON LEFT HAND SIDE. REPLACED WITH NEW DOUBLER. 2 L 7 2 4F RT A21EA 1999070200051 19990702 00051 WP 1999 7 2 ABXA9900531 1 19990623 A 5230 575407512 FITTING DOUG DOUG DC8 DC863F 302198F WP CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 C-3 DOOR LOWER CORNER FITTING CORRODED. REPAIRED IAW ABX REA D852-28107MR. 2 L 7 4 4F 4A25 1999070200052 19990702 00052 WP 1999 7 2 ABXA9900532 1 19990526 A 5311 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 1690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 STATION 1690 FRAME CORRODED AT LONGERON 32 RIGHT TO 32 LEFT. REPAIRED IAW DC8 SRM 53-2-5 AND DWG NR SK35743. 2 L 7 4 4F 4A25 1999070200053 19990702 00053 WP 1999 7 2 ABXA9900533 1 19990526 A 5413 5757504 STRINGER DOUG DOUG DC8 DC863F 302198F WP NR 3 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 CRACK ON BOTTOM SIDE OF NR 3 ENGINE STRINGER. REPAIRED IAW DC8 SRM 78-2-0. 2 L 7 4 4F 4A25 1999070200054 19990702 00054 WP 1999 7 2 ABXA9900534 1 19990526 A 5320 56440132064 DOUBLER DOUG DOUG DC8 DC863F 302198F WP BS 1690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FINGER DOUBLER CORRODED AT LONGERON 28 RIGHT BETWEEN STATION 1690 AND 1710. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999070200055 19990702 00055 WP 1999 7 2 ABXA9900535 1 19990526 A 5320 5644130 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1690-1710 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FINGER DOUBLER CORRODED AT LONGERON 28 LEFT AND STATIONS 1690-1710. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1999070200056 19990702 00056 WP 1999 7 2 ABXA9900536 1 19990525 A 5320 5757779 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1650-1690 BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON END FITTING BROKEN AT STATION 1650-1690 AND LONGERON 29 LEFT. REPLACED FITTING IAW DC8 SRM 53-1-0 AND 51-1-2D. 2 L 7 4 4F 4A25 1999070200057 19990702 00057 EU 1999 7 2 R7MA0000624 1 19990412 A 6230 1090110055 SUPPORT AGUSTA A109 A109K2 0260502 EU SWASHPLATE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 1576 EM0037 10018 COATING FOR SWASHPLATE SUPPORT WORN TO LIMITS. (X) 1 G 7 2 3U RT H7EU 1999070200058 19990702 00058 EU 1999 7 2 R7MA0000637 1 19990423 A 6220 1090101063 DAMPER AGUSTA A109 A109K2 0260502 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 1348 776 10018 BUSHINGS WORN. PAC WOULD NOT SUPPLY BUSHING. (X) 1 G 7 2 3U RT H7EU 1999070200059 19990702 00059 EU 1999 7 2 R7MA0000620 1 19990419 A 6220 1090101433 BUSHING AGUSTA A109 A109K2 0260502 EU M/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX A04080 10018 BUSHING WORN AND GROOVED BEYOND LIMITS. (X) 1 G 7 2 3U RT H7EU 1999070200060 19990702 00060 EU 1999 7 2 R7MA0000619 1 19990419 A 6220 1090101433 BUSHING AGUSTA A109 A109K2 0260502 EU M/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX A4022 10018 BUSHING WORN AND GROOVED BEYOND LIMITS. (X) 1 G 7 2 3U RT H7EU 1999070200061 19990702 00061 1999 7 2 99ZZZX2448 4 19990307 A 6113 SPINNER BOEING 757 75723N 1384973 NM RT ENGINE ICED UP A AMTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 11 522AT 29330 ON CLIMB-OUT, RT ENIGNE N1 VIBS EXCEEDED 4.0 IN AMBER BAND. FOLLOWED FIM 71-05-00, FIG 108, BLK 1 THROUGH BLK 5. PERFO RMED TEST NR 6. ALL PARAMETERS .9 AT TAKEOFF. SUSPECT ICE BUILD-UP ON SPINNER. OPS CHECK NORMAL PER MM. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1999070200062 19990702 00062 NM 1999 7 2 99ZZZX2449 1 19990323 A 2560 BACKPLATE BOEING 757 75723N 1384973 NM 4L DOOR SLIDE BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 DOOR 4L EVACUATION SLIDE ARMING BACKPLATE BROKEN. RE-EPOXIED ROYALITE COVER ONTO DOOR. OPS CHECK OK. 2 L 7 2 4F RT A2NM 1999070200063 19990702 00063 EA 1999 7 2 MASA99083 1 19990523 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA EMER EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7219 FLT 5841 - DCA-TYS - THE CAPATIN REPORTED THE LT AFT OVERWING EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE A CTION WAS DEFERRED PER MEL 33-51-2. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BUBL WAS REMOV ED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1999070200064 19990702 00064 NE 1999 7 2 SI3R99014 2 19990426 A 7210 HOUSING HAMSTD 7758001 SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE GEARBOX CRACKED B SI3R K NONE O OTHER IN INSP/MAINT 1 NE 03 110PX 28928 UDAG0089 340A023 UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED: CRACKED AFT GEARBOX HOUSING, (PN RFN922). CRACKED AFT RIGHTHA ND IDLER ROLLER BEARING, (SN 4257, PN 775761-2). RIGHT IDLER FORWARD TAB WASHER WAS FOUND BROKEN, (PN 789578-1). REF: HSS SO NR 258577SO. CUST: EXPRESS A/L. CMM 72-11-02. REF: OPER CNTRL NR 99ZZZX2450 AND 99ZZZX2451. 2 L 7 2 4T 4 T RT A52EU E8NE 1999070200065 19990702 00065 NE 1999 7 2 99ZZZX2450 2 19990426 A 7210 BEARING HAMSTD 7758001 SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE GEARBOX CRACKED B SI3R K NONE O OTHER IN INSP/MAINT 1 NE 03 110PX 28928 UDAG0089 340A023 UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED: CRACKED AFT GEARBOX HOUSING, (PN RFN922). CRACKED AFT RIGHTHA ND IDLER ROLLER BEARING, (SN 4257, PN 775761-2). RIGHT IDLER FORWARD TAB WASHER WAS FOUND BROKEN, (PN 789578-1). REF: HSS SO NR 258577SO. CUST: EXPRESS A/L. CMM 72-11-02. REF: OPER CNTRL NR SI3R99014, AND 99ZZZX2451. 2 L 7 2 4T 4 T RT A52EU E8NE 1999070200066 19990702 00066 NE 1999 7 2 99ZZZX2451 2 19990426 A 7210 WASHER HAMSTD 7758001 SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A1 30030 NE GEARBOX BROKEN B SI3R K NONE O OTHER IN INSP/MAINT 1 NE 03 110PX 28928 UDAG0089 340A023 UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED: CRACKED AFT GEARBOX HOUSING, (PN RFN922). CRACKED AFT RIGHTHA ND IDLER ROLLER BEARING, (SN 4257, PN 775761-2). RIGHT IDLER FORWARD TAB WASHER WAS FOUND BROKEN, (PN 789578-1). REF: HSS SO NR 258577SO. CUST: EXPRESS A/L. CMM 72-11-02. REF: OPER CNTRL NR SI3R99014, AND 99ZZZX2450. 2 L 7 2 4T 4 T RT A52EU E8NE 1999070200078 19990702 00078 NE 1999 7 2 EISA99059 2 19990324 A 7261 MS9380236 GASKET DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE TORN A EISA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 977ML 47329 657039 ADDED 5 QUARTS OIL TO NR 2 ENGINE IN LAS, TOTAL 13 QUARTS. HALF WAY TO SAN, QUANTITY WAS DOWN TO 4 QUARTS. (KEPT SLOWL Y DECREASING IN-FLIGHT). SHUT DOWN NR 2 ENGINE. TEMPERATURE NEVER EXCEEDED 110 DEGREES EVEN AFTER IDLING AND SHUT DOWN . DETERMINED OIL FILTER HOUSING GASKET BLOWN. REPLACED WITH MS93H-236 O-RING IAW 79-20-00 DC-9-IPC. (X) 2 L 7 2 4F 4 F A6WE E2EA 1999070200094 19990702 00094 NM 1999 7 2 SWAA991056 1 19990620 A 2910 AE246416E0196 LINE BOEING 737 7373A4 1384585 NM RT MLG LEAKING A SWAA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 676SW 23288 DURING CLIMB, HYD A-SYSTEM LOW PRESS LIGHT ILLUMINATED AT NR 1 ENGINE. HYD QTY READS EMPTY. HYD BRAKE PRESSURE AND MAI N SYSTEM PRESSURE OK. FOUND LEAKING HYD LINE. REMOVED AND REPLACED RT MLG DOWN HYD LINE PER MM. 2 L 7 2 4F RT A16WE 1999070200095 19990702 00095 NM 1999 7 2 SWAA991057 1 19990621 A 5313 6552988 STRINGER BOEING 737 7372H4 138448C NM BS 986-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT STRINGER 24R, BS 986-1006. REMOVED AND REPLACED STRINGER SECTION PER SR M. 2 L 7 2 4F A16WE 1999070200096 19990702 00096 NM 1999 7 2 SWAA991058 1 19990621 A 2560 6546546 BRACKET BOEING 737 7373H4 1384600 NM PASSENGER DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FWD ENTRY DOOR AFT GIRT BAR ATTACH FLOOR BRACKET. REMOVED AND REPLACED GIR T ATTACH BRACKET PER MM. 2 L 7 2 4F RT A16WE 1999070200097 19990702 00097 NM 1999 7 2 SWAA991059 1 19990621 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 727D, BETWEEN STRINGERS 8L-9L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999070200098 19990702 00098 NM 1999 7 2 SWAA991053 1 19990621 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999070200099 19990702 00099 NM 1999 7 2 SWAA991054 1 19990621 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 7 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 522SW 26564 EMERGENCY ESCAPE FLOOR TACK LIGHT BULB AND LENS MISSING AT ROW 7. REPLACED LIGHT BULB AND LENS PER MM. 2 L 7 2 4F RT A16WE 1999070200100 19990702 00100 NE 1999 7 2 SWAA991055 2 19990622 A 7200 ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A SWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 091SW 22963 687885 INFLIGHT SHUT DOWN. NR 2 ENGINE, OIL LOSS. NO OIL PRESSURE AND QUANTITY INDICATION. REMOVED AND REPLACED NR 2 ENG PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999070200101 19990702 00101 NM 1999 7 2 SWAA991060 1 19990621 A 5330 6545890 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED, LOWER HINGE CUTOUT OF AFT SERVICE DOOR. REPAIRED SKIN PER SWA R A NR 1- 253-2096. 2 L 7 2 4F A16WE 1999070200102 19990702 00102 NM 1999 7 2 SWAA991061 1 19990623 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 FWD ENTRY SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999070200103 19990702 00103 NM 1999 7 2 SWAA991062 1 19990623 A 3350 610478 BATTERY PACK BOEING 737 7377H4 NM EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED RON CHECK, FOUND RT EMERGENCY OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM. 2 L 7 2 4F RT A16WE 1999070200104 19990702 00104 1999 7 2 SWAA991063 4 19990623 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED A1 CHECK, FWD SERVICE DOOR EVACUATION SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PE R MM. 2 L 7 2 4F RT A16WE 1999070200105 19990702 00105 NM 1999 7 2 SWAA991064 1 19990623 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 859 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMP FLOORBEAM CORRODED, BS 859,LBL 3.5 AND LBL 7.5. REPAIRED FLOORBEAM PER S RM. 2 L 7 2 4F RT A16WE 1999070200106 19990702 00106 NM 1999 7 2 SWAA991065 1 19990623 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 947, LBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999070200107 19990702 00107 NM 1999 7 2 SWAA991066 1 19990623 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 986, LBL 31-RBL 31. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999070200108 19990702 00108 NM 1999 7 2 SWAA991067 1 19990623 A 5752 654645520 TAB BOEING 737 737317 138447P NM RT AILERON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND RT AILERON TAB LOWER SURFACE CRACKED AND DELAMINATED. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 1999070200109 19990702 00109 1999 7 2 SWAA991047 4 19990619 A 3442 6555899 RADAR BOEING 737 7372H4 138448C NM FWD FUSELAGE INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 080SW 22675 AIR TURNBACK, WEATHER RADAR FAILED DURING FLIGHT. REMOVED AND REPLACED WEATHER RADAR T/R UNIT PER MM. 2 L 7 2 4F A16WE 1999070200110 19990702 00110 NM 1999 7 2 SWAA991048 1 19990618 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OUT OF RETAINER. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999070200111 19990702 00111 NM 1999 7 2 SWAA991049 1 19990620 A 2720 65C370539 PCU BOEING 737 7372H4 138448C NM RUDEER FAILED A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 074SW 22674 AIR TURNBACK, IMMEDIATELY AFTER TAKEOFF ROTATION FELT RIGHT YAW. YAW DAMPER INDICATOR DEFLECTED FULL TO THE RIGHT, YAW DAMPER SWITCH TURNED OFF AND CONTROL WAS NORMAL. REMOVED AND REPLACED RUDDER PCU PER MM. 2 L 7 2 4F A16WE 1999070200112 19990702 00112 NM 1999 7 2 SWAA991050 1 19990618 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM ROW 18 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 ROW 18 LT FLOOR PROXIMITY LIGHT INOP AND COVER MISSING. REPAIRED WIRE AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999070200113 19990702 00113 NM 1999 7 2 SWAA991051 1 19990618 A 5320 6547979 WEB BOEING 737 7373H4 1384600 NM BS 747-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D CHECK, FOUND CORROSION ON CREASE WEB, BS 747-767, STRINGER 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 1999070200114 19990702 00114 NM 1999 7 2 SWAA991052 1 19990620 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 9, WL 234. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999070200115 19990702 00115 NM 1999 7 2 SWAA991068 1 19990622 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED C3 CHECK, FOUND AFT END EMERGENCY ESCAPE FLOOR LIGHT END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F A16WE 1999070200116 19990702 00116 NM 1999 7 2 SWAA991069 1 19990622 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT LOOSE NEXT TO AFT GALLEY. RESECURED TRACK LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999070200117 19990702 00117 NM 1999 7 2 SWAA991070 1 19990622 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CLIP CRACKED, BS 380, STRINGER 5L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F A16WE 1999070200118 19990702 00118 NM 1999 7 2 SWAA991071 1 19990624 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 968 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CORROSION AT STRINGER 27R, BS 968. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999070200119 19990702 00119 NM 1999 7 2 SWAA991072 1 19990624 A 5311 6546569 FRAME BOEING 737 7372H4 138448C NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FRAME CRACKED, BS 947, BETWEEN STRINGERS 17R-19R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999070200120 19990702 00120 NM 1999 7 2 SWAA991073 1 19990622 A 5320 6551261 FRAME BOEING 737 7372T4 1384492 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOORWAY, UPPER FWD STUB FRAME CRACKED. REMOVED AND REPLACED STUB FRAME PER SR M. 2 L 7 2 4F A16WE 1999070200121 19990702 00121 NM 1999 7 2 SWAA991074 1 19990622 A 5330 6552988 SKIN BOEING 737 7372T4 1384492 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND SKIN CRACKED, ON LOWER FWD CORNER OF AFT ENTRY AND SERVICE DOORWAY CUTOUTS. REPAIRED SK IN PER SRM. 2 L 7 2 4F A16WE 1999070200122 19990702 00122 NM 1999 7 2 SWAA991075 1 19990622 A 5330 6551625 SKIN BOEING 737 7372T4 1384492 NM BS 982 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND CORROSION ON OUTFLOW VALVE FUSELAGE SKIN CUTOUT, BS 982. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999070200123 19990702 00123 NM 1999 7 2 SWAA991076 1 19990622 A 5347 6941695 FITTING BOEING 737 7372T4 1384492 NM COCKPIT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND CORROSION AT F/O'S FWD AND AFT SEAT ATTACH FITTINGS. REMOVED AND REPLACED FITTINGS PER MM. 2 L 7 2 4F A16WE 1999070200124 19990702 00124 NM 1999 7 2 SWAA991077 1 19990624 A 5320 BAC1515 BEAM BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND CRACKED CREASED BEAM INBD CHORD, BS 727, LBL 64. REPAIRED BEAM PER SRM. 2 L 7 2 4F A16WE 1999070200125 19990702 00125 NM 1999 7 2 SWAA991078 1 19990624 A 3350 100885 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED SERVICE CHECK, FOUND AFT SECTION OF EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP. REMOVED AND REPLACED BATT ERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999070200126 19990702 00126 WP 1999 7 2 TWAA9908801 1 19990622 A 3260 0080004003 SWITCH BOX DOUG DC9 DC932 3022066 WP NLG DOOR WORN A TWAA O OTHER N FALSE WARNING LD LANDING 1 CE 05 920L 47734 THE NOSE LANDING GEAR UNSAFE LIGHT APPEARED AFTER GEAR WAS EXTENDED. MANUAL EXTENSION OF THE NOSE LANDING GEAR WAS NO H ELP. REPLACED THE GEAR DOOR PROXIMITY SWITCH BOX . CHECK-C 6-12-98 MCI. 2 L 7 2 4F A6WE 1999070200127 19990702 00127 NM 1999 7 2 TWAA9908802 1 19990623 A 2530 CART BOEING 767 767231 1385131 NM GALLRY FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 604TW 22567 WIRE ON A GALLEY CART WAS REPORTED BURNING UNTIL THE CART WAS DISCONNECTED ELECTRICALLY. REPLACED THE CART. CHECK-C 4- 18-99 LAX. 2 L 7 2 4F RT A1NM 1999070200128 19990702 00128 WP 1999 7 2 AT9900461 1 19990622 A 3340 SWITCH DOUG DC9 DC932 3022066 WP RT LANDING LIGHT FAILED A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 15 812AT 47359 DURING APPROACH, NOTED SMOKE AFTER TURNING ON LEFT AND RIGHT WING LANDING LIGHTS, SMOKE STOPPED AFTER TURNING LIGHTS OFF . RIGHT WING LANDING LIGHT SWITCH WAS FOUND TO BE AT FAULT AND PLACED ON MEL (DM24543). LEFT WING LANDING LIGHT WAS OK FOR SERVICE. 2 L 7 2 4F A6WE 1999070200129 19990702 00129 WP 1999 7 2 AT9900462 1 19990621 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOORWAY DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 FORWARD GALLEY EVACUATION SLIDE FELL OUT OF HOUSING. RE-INSTALLED EVACUATION SLIDE IAW MM 25-61 AND RII COMPLIED WITH. 2 L 7 2 4F A6WE 1999070200130 19990702 00130 WP 1999 7 2 AT9900463 1 19990616 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 541 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FRAME IN THE FORWARD PIT AT BS 541 L-29L-29R CORRODED. REMOVED CORRO SION, FABRICATED REPAIR PARTS, HEAT TREATED AND INSTALLED IAW DC9 SRM 53-03 FIG 2A, 51-10-4, 51-10-3, AND 51-30-3. 2 L 7 2 4F A6WE 1999070200131 19990702 00131 NM 1999 7 2 CALA9900716 1 19990623 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016. REPAIRED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999070200132 19990702 00132 WP 1999 7 2 CALA9900717 1 19990624 A 3350 AD4002P BATTERIES AEROQUALITY DOUG DC9 DC982 3022082 WP EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE IN FIRST CLASS SECTION OF CABIN. THE BATTERIES WERE REPLACED IN THE BATTERY PACK AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999070200133 19990702 00133 NM 1999 7 2 CALA9900718 1 19990624 A 3350 252005 FUSE BOEING 757 757224 1384958 NM L2 DOORWAY BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND THE EMERGENCY EXIT SIGN OVER L-2 DOOR INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE IN THE BATTERY PA CK AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 1999070200134 19990702 00134 NM 1999 7 2 CALA9900719 1 19990624 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 294, RBL 35. THE CORROSION WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS SPLICED IN IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999070200135 19990702 00135 WP 1999 7 2 9902181223 1 19990517 A 5753 RIB DOUG DC10 DC1040 3023508 WP RT TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 223NW 46580 DURING L CHECK, FOUND CRACK IN RIGHT OUTBOARD FLAP CLOSURE RIB NEAR ROLLER ASSEMBLY REPAIRED PER EA 12-162794. 2 L 7 3 4F A22WE 1999070200136 19990702 00136 WP 1999 7 2 9902191144 1 19990518 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1119-1139 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING M CHECK, FOUND CORROSION ON LONGERON 48R UPPER AND LOWER SURFACE FROM FS 1119 - FS 1139. REPAIRED PER EA 11-1668 80. 2 L 7 3 4F A22WE 1999070200137 19990702 00137 WP 1999 7 2 9902201144 1 19990420 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1356 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING M CHECK, FOUND CORROSION ON BELLY SKIN AT FS 1356 BETWEEN LBL 51 AND LBL 52. REPAIRED PER EA 11-166595. 2 L 7 3 4F A22WE 1999070200138 19990702 00138 WP 1999 7 2 9902211144 1 19990420 A 5315 FLOORBEAM DOUG DC10 DC1040 3023508 WP BS 879 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING M CHECK, FOUND CRACK IN FLOOR I BEAM SUPPORT AT FS 879 AT BL 0. REPAIRED PER EA 11-167434. 2 L 7 3 4F A22WE 1999070200139 19990702 00139 WP 1999 7 2 9902221144 1 19990517 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 1256 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING M CHECK, FOUND CRACK IN TRANSVERSE FRAME BELOW DOOR 3R THRESHOLD AT FS 1256, RBL 110. REPAIRED PER EA 11-166446. 2 L 7 3 4F A22WE 1999070200140 19990702 00140 WP 1999 7 2 9902231144 1 19990514 A 5711 SPAR DOUG DC10 DC1040 3023508 WP BS 1236 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING M CHECK, FOUND CORROSION ON CHORD AT UPPER CENTER TANK FORWARD SPAR AT FS 1236, RBL 70 TO RBL 75. REPAIRED PER E A 11-167439. 2 L 7 3 4F A22WE 1999070200141 19990702 00141 NM 1999 7 2 UPS99229972 1 19990625 A 5610 57176239 WINDOW BOEING 727 7272A1 138407F NM FLIGHT DECK SHATTERED A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 214UP 21342 INSPECTION TYPE:N/A, AIRCRAFT DIVERTED INTO TUL DUE TO L-2 WINDOW SHATTERED IN FLIGHT. *S/D* REMOVED AND REPLACED L-2 WINDOW WITH NEW PER MM 56-12-11 (P/N 5-71762-39) (S/N 1429) OFF. (P/N 5-71762-39) (S/N 84-H -3-5-116) ON. HEAT CONTROL (P/N 1231-2) (S/N 978) OFF. HEAT CONTROL (P/N 231-2) (S/N 4764) ON. 2 L 7 3 4F A3WE 1999070200142 19990702 00142 WP 1999 7 2 UPS99829953 1 19990624 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP RADIO RACK DEAD A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 EMERGENCY LIGHTS INOP. FOUND EMERGENCY LIGHT SWITCH LEFT ON TURNED SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHTS B ATTERY PACK, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999070200143 19990702 00143 WP 1999 7 2 UPS99829955 1 19990609 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP BS 1420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 FLOORBOARD CORRODED AROUND INSERT FS 1420 LBL 10. REMOVED CORROSION IAW DC8 SRM 51-1-8, CUT OUT DAM AGE AND REPAIR IAW DC 8 SRM 53-2-3 ALODINE AND PRIME REPAIR DOUBLER IAW DC8 SRM 51-1-8. INSTALLED ALL REPAIR DOUBLER IA W DC8 SRM 51-1-21A. 2 L 7 4 4F RT 4A25 1999070200144 19990702 00144 WP 1999 7 2 UPS99829956 1 19990609 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP BS 1470 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 FLOOR PANEL FS 1470 LBL 35 HAS CORROSION BULGE AROUND INSERT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, FAB DOUBLER IAW DC8 SRM 53-2-3, INSTALL DOUBLER IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999070200145 19990702 00145 WP 1999 7 2 UPS99829957 1 19990609 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 880-1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 FLOORBOARD CORRODED ROW-C FS880-1000. REMOVED CORROSION IAW DC8 SRM 51-1-8, REPAIR CORRODED AREA IA W DC8 SRM 53-2-3. ALODINE AND PRIME IAW DC8 SRM 51-1-8, INSTALL REPAIR DOUBLER IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999070200146 19990702 00146 WP 1999 7 2 UPS99829958 1 19990605 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1228 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, BANANA FITTING FS 1228 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING, RECEIVED NEW FITTING. D RILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200147 19990702 00147 WP 1999 7 2 UPS99829959 1 19990605 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, BANANA FITTING FS 1220 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING. RECEIVED NEW FITTING, D RILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200148 19990702 00148 WP 1999 7 2 UPS99829960 1 19990615 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 LONGERON END FITTING CRACKED L10L AFT SIDE OF FRAME 902. REMOVED AND REPLACED END FITTING IAW DC8 S RM 51-1-21. 2 L 7 4 4F RT 4A25 1999070200149 19990702 00149 WP 1999 7 2 UPS99829961 1 19990613 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 1700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 STA 1700 LONG 24 LEFT FRAME SPLICE IS CRACKED. REMOVED FABRICATED AND INSTALLED FRAME SPLICE IAW DC 8 SRM 51-1-20D, 53-5-3, DAC DWG 612142, 51-1-8 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200150 19990702 00150 WP 1999 7 2 UPS99829962 1 19990609 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 580-880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 FLOOR PNL 58-880 ROW A IS CRACKED AT ATTACH HOLE, HAS 2 EACH GOUGES, NUMEROUS AREAS OF BARE METAL AN D CORROSION, AND MISSING/DAMAGED NON- SKID. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0 FIG LF. INSTALLED NON-SKID TA PE AS NECESSARY IAW DC8 MM 20-32-0. REMOVED AND FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-3. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999070200151 19990702 00151 WP 1999 7 2 UPS99829963 1 19990611 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, CORROSION ON FLOOR PANEL AT RBL 35 AT FS 350. REMOVED CORROSION, FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-3 AND INSTALLED REPAIR. 2 L 7 4 4F RT 4A25 1999070200152 19990702 00152 WP 1999 7 2 UPS99829964 1 19990609 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, SEAT TRACK AT STA 870, BL O.O CORR DOT E560. REMOVED CORROSION IAW DC8 SRM 51-1-8 NOT WITHIN LIMIT S IAW DC8 SRM 5 3-2-3. REMOVED DAMAGED SECTION OF TRACK STA 850-890 IAW DC8 SRM 53- 2-3. INSTALLED NEW TRACK SECTION I AW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999070200153 19990702 00153 WP 1999 7 2 UPS99829966 1 19990613 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1080-1100 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 INTERCOSTAL CRACKED AT LONGERON 35L BETWEEN FS 1080-1100. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DAC DWG 9758507 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200154 19990702 00154 WP 1999 7 2 UPS99829967 1 19990613 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1 SPLICE FITTING FS 1050 AT LONGERON 35 RT IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SR M 51-3-2 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200155 19990702 00155 WP 1999 7 2 UPS99829968 1 19990615 A 5720 FITTING DOUG DC8 DC873F 302199F WP BS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN IB AT FS 74 REAR SPAR HAS TWO CRACKED FITTINGS. REMOVED AND REPLACED END FIT TING IAW UPS DC8 SRM 51-2-20D AND DWG 3704 841. 2 L 7 4 4F RT 4A25 1999070200156 19990702 00156 WP 1999 7 2 UPS99829969 1 19990615 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN I/B AT W/S 74.000 REAR SPAR HAS FWD AND AFT FITTINGS CRACKED. REMOVED AND RE PLACED FITTINGS W/SERVICABLE PART IAW DAC DWG 5613423 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200157 19990702 00157 WP 1999 7 2 UPS99829970 1 19990615 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, STRINGER 51 NR 2 MAIN O/B AT W/S 74.000 REAR SPAR HAS AFT FITTING CRACKED. REMOVED AND REPLACED EN D FITTING IAW DAC DAW 5613423 AND DC8 SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 1999070200158 19990702 00158 WP 1999 7 2 UPS99829971 1 19990604 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, LONG 24R FITTING AT STA 920 IS CRACKED ON AFT SIDE DOT L122. REMOVED FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, DC8 SRM 51-3-0, 51-1-20D. INSTALLED SPOILER PULLEY BRACKET AND UPLOCK ASSEMBLY IAW DC8 SRM 51-3-0 AND MM 32-31-03. 2 L 7 4 4F RT 4A25 1999070200159 19990702 00159 NE 1999 7 2 QXEA9901371 2 19990621 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 1 MALFUNCTION A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 815PH 21552 1 50 PCE120696 SEA - HAZE APPEARED IN THE CABIN WITH NO SMOKE ODOR. IT SEEMED TO SUBSIDE AFTER TURNING OFF NR 1 BLEED. MAINTENANCE RE PLACED O-RINGS ON THE NR 1 LP PROBE AND SHIMMED, THE NR 1 P2 VALVE TO 4 SPACERS. DURING GROUND RUN, INSPECTED OIL BREAT HER, NO HELP. AIRCRAFT FERRIED FROM SEA TO PDX FOR REPAIRS. IN PDX, REPLACED NR 1 ENGINE. GROUND RUN AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. AWITING TEARDOWN ANALYSIS OF REMOVED ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999070200160 19990702 00160 EU 1999 7 2 99FDEA00236 1 19990624 A 3411 PITOT SYSTEM AIRBUS 310 A310221 3930310 EU RIGHT DIRTY A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 448FE 260 99-143 - NO AIRSPEED IND ON F/O SIDE PFD ON T/O. RTO AT 70 KNOTS. PERF ADC NR 2 OPS CK IAW MM 34-10-00 SYS CK GOOD. F LUSHED NR 2 PITOT SYS IAW 34-10-00, FOUND DEBRIS IN F/O PITOT TUBE, SYS OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999070200161 19990702 00161 NE 1999 7 2 99FDEA00237 2 19990624 A 7532 BLEED VALVE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE NR 2 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 419FE 345 99-144 - BLEED VALVE NR 2 FAULTED IN CRZ AT FL310, UNABLE TO RECOVER FAULTED BLD VALVE. 2 L 7 2 4F 4 F RT A35EU E3NE 1999070200162 19990702 00162 1999 7 2 99FDEA00238 4 19990624 A 2210 837101A ELECT UNIT AIRBUS 310 A310203 EU NR 2 PITCH TRIM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 426FE 245 99-145 NR 2 PITCH TRIM LEVER WILL NOT REMAIN ENGAGED. NR 1 ATS LEVER WILL NOT REMAIN ENGAGED, NR 2 FD INOP. REMOVED AN D REPLACED PROX ELEC UNIT IAW 32-31-71 SYS FND CK GOOD AND AFS TEST NORM IAW 22-00-00. 2 L 7 2 4F RT A35EU 1999070200163 19990702 00163 NM 1999 7 2 99FDEA00239 1 19990624 A 5520 HINGE BOEING 727 72722 1384002 NM LT ELEVATOR LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 99-146 - WHEN LEFT ELEVATOR IS DEFLECTED UP IT MAKES A POPPING SOUND AND BOWS OUT THE LWR ACCESS PNL ON STAB FWD OF ELEV ATOR. REMOVED AND REPLACED BALANCE PANEL AND IDLER HINGES FOR SHEET METAL. FAB NEW BRACKETS PER BOEING DWG NR 69-22295 AND NR 65-22988. 2 L 7 3 4F A3WE 1999070200164 19990702 00164 NM 1999 7 2 99FDEA00240 1 19990623 A 2820 LINE DOUG MD11 MD11F 3023600 NM NR 2 ENGINE LEAKING A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 25 609FE 48549 FUSELAGE NR 2 ENGINE SHROUD DRAIN VALVE FOUND WITH FUEL PRESENT. LEAKAGE TRACED TO 3 LOCATIONS IN CENTER LAND GEAR WHEE L WELL FWD BULKHEAD. *S/D* REMOVED AND REPLACED 1 NR 2 ENG FUEL LINE COUPLING SEAL AS PER MM 28-00-00-4. CARRIED OUT FUEL SHROUD LEAK CK PER MM 28-25-00-5, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 1999070200165 19990702 00165 WP 1999 7 2 ABXA9900537 1 19990623 A 3220 LANDING GEAR DOUG DOUG DC9 DC932 3022066 WP NLG VIBRATION A ABXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 900AX 47380 VIBRATIONS FROM FRONT OF AIRCRAFT OCCURRED WHEN LANDING GEAR RETRACTED ON TAKEOFF. VIBRATIONS CEASED WHEN GEAR WAS EXTE NDED, BUT RESUMED WHEN GEAR WAS RETRACTED. AIRCRAFT RETURNED TO GEG. INSPECTED AND VERIFIED PROPER SECURITY OF NOSE LA NDING GEAR DOORS. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1999070200166 19990702 00166 WP 1999 7 2 ABXA9900538 1 19990323 A 5521 5910411515 SPAR DOUG 9918450503 DOUG DC9 DC941 302207N WP LT ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 TOP OF LEFT ELEVATOR SPAR CRACKED IN 8 PLACES, STATION 204 TO 220. REPLACED ELEVATOR SPAR IAW DC9 DWG 9918450. 2 L 7 2 4F A6WE 1999070200167 19990702 00167 WP 1999 7 2 ABXA9900539 1 19990517 A 5320 3750330527 SPLICE DOUG DOUG DC8 DC863 302198A WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LONGERON 32 LEFT SPLICE CRACKED BETWEEN STATION 600-620. REPAIRED IAW DC8 SRM 51-1-20D AND DWG NR 3750330527. 2 L 7 4 4F 4A25 1999070200168 19990702 00168 WP 1999 7 2 ABXA9900540 1 19990517 A 5320 561537275 DOUBLER DOUG DOUG DC8 DC863 302198A WP BS 1490 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 FINGER DOUBLER CRACKED AT LONGERON 31 LEFT AND 31 RIGHT AT STATION 1490. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5615372. 2 L 7 4 4F 4A25 1999070200169 19990702 00169 WP 1999 7 2 ABXA9900541 1 19990515 A 5730 5611340 SKIN DOUG DOUG DC8 DC863 302198A WP WS 574 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 RIGHT WING UPPER SKIN CRACKED AT STRINGER 10, INBOARD OF STATION XR 574. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1999070200170 19990702 00170 WP 1999 7 2 ABXA9900542 1 19990515 A 5320 561214253 SHEAR TIE DOUG DOUG DC8 DC863 302198A WP BS 1700 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 SHEAR TIE CRACKED AT STATION 1700 BETWEEN LONGERONS 32 LEFT AND 34 LEFT. REPLACED SHEAR TIE IAW DC8 51-1-20D AND 51-1-2 1. 2 L 7 4 4F 4A25 1999070200171 19990702 00171 WP 1999 7 2 ABXA9900543 1 19990515 A 5720 5769985 SLOT VANE DOUG DOUG DC8 DC863 302198A WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 LEFT WING INBOARD SLOT VANE HAD HEAVY CORROSION. REPAIRED IAW DC8 SRM 57-3-1. 2 L 7 4 4F 4A25 1999070200172 19990702 00172 NM 1999 7 2 SCNA99086 1 19990625 A 2761 ACTUATOR 65C163001 BOEING 727 727259 138408J NM NR 2 SPOILER FAILED A SCNA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 15 289SC SC96061 22475 DURING DESCENT, CREW OBSERVED 'A' SYSTEM HYDRAULIC FAILURE. HYDRAULIC QUANTITY AND PRESSURE READ ZERO. ALL COM PROCEDU RES WERE COMPLIED WITH AND LANDING WAS UNREMARKABLE. INSPECTED AND FOUND A BLOWN O-RING ON THE NR 2 ACTUATOR FOR THE SPO ILER. REMOVED AND REPLACED THE SPOILER ACTUATOR O-RING AND SYSTEM CHECKS GOOD IAW MM 276100. 2 L 7 3 4F A3WE 1999070200173 19990702 00173 NM 1999 7 2 DHL9970501C 1 19990525 A 5720 ANGLE BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, RT WING L/E CAVITY FS 115 VERTICAL ANGLE CRACKED. CUT OUT DAMAGE, HFEC, INSTALLED ANGLE REPAIR 9 BY 2 PER S RM 51-40-3, N/R 2058. 2 L 7 3 4F A3WE 1999070200174 19990702 00174 NM 1999 7 2 DHL9970502C 1 19990502 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 599 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, SEAT TRACK DAMAGED STA 599. CUT OUT DAMGED SECTION FROM 531 TO 665. INSTALLED REPAIR PER SRM 53-10-5, N/R 5001. 2 L 7 3 4F A3WE 1999070200175 19990702 00175 NM 1999 7 2 DHL9970503C 1 19990603 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, CENTER SEAT TRACK STA 600 CORRODED. REMOVED DAMAGED AREA AND INSTALLED TRACK FROM BS 550 TO 630 PER SRM 53- 10-5. FABRICATED AND INSTALLED SPLICE AT BS 630 PER AVITAS EO 99AVHM033D1, N/R 5070. 2 L 7 3 4F A3WE 1999070200176 19990702 00176 NM 1999 7 2 DHL9970504C 1 19990603 A 5312 BULKHEAD BEAM BOEING 727 72722C 138400F NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, FWD SIDE OF 1183 BULKHEAD BEAM RADIUS OF AFT I/B FLANGE CRACKED WL 238 BBL 36. STOP DRILLED CRACK, HFEC, IN STALLED S/B REPAIR PER S/B 53-0192, N/R 3369. 2 L 7 3 4F A3WE 1999070200177 19990702 00177 NM 1999 7 2 DHL9970505C 1 19990525 A 5754 ANGLE BOEING 727 72722C 138400F NM LT LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, LT WING L/E SLAT STA 0 L/E STA 349, WEB O/B UPPER FLANGE OLD ANGLE REPAIR CRACKED. REMOVED AND INSTALLED NE W ANGLE PER SRM 51-30-2 18 BY 1.5, N/R 1165. 2 L 7 3 4F A3WE 1999070200178 19990702 00178 NM 1999 7 2 DHL9970506C 1 19990525 A 5753 SKIN BOEING 727 72722C 138400F NM LT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, LEFT WING O/B AFT FLAP HAS DELAMINATION AT UPPER AND LOWER SURFACE WBL 395. INSTALLED OVERLAY REPAIR PER S RM 51-40-8, 20 BY 10, N/R 1199. 2 L 7 3 4F A3WE 1999070200179 19990702 00179 NM 1999 7 2 DHL9970507C 1 19990525 A 5730 SKIN BOEING 727 72722C 138400F NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, LT WING UPPER L/E NR 4 SLAT O/B HOOK CUT OUT. CRACKED AT AFT O/B CORNER WS 171. STOP DRILLED CRACK, HFEC, INSTALLED DOUBLER 8 BY 5.75 PER SRM 57-30-4, N/R 1183. 2 L 7 3 4F A3WE 1999070200180 19990702 00180 NM 1999 7 2 DHL9970508C 1 19990525 A 2752 SUPPORT BOEING 727 72722C 138400F NM NR 1 TE FLAP ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, LT WING NR 1 FLAP ACTUATOR WING I/B ATTACH VERTICAL SUPPORT UPPER AND LOWER FLANGES CRACKED. REMOVED DAMAG ED SUPPORT, REPLACED SUPPORT 6.5 BY 5.5 PER SRM 51-40-3, N/R 1163. 2 L 7 3 4F A3WE 1999070200181 19990702 00181 NM 1999 7 2 DHL9970509C 1 19990525 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 940 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, RT MLG WHEEL WELL STA 940 STR 17R TO 18R HAS CORROSION AT ANGLE FOR FLANGE. REMOVED UPPER WEB STA 940 TO 95 0 STR 17. REMOVED PRESURE WEB ATTACH ANGLE, INSTALLED NEW ATTACH ANGLE PER SRM 53-10-1. INSTALLED WEB PER SRM 51-30-2 , N/R 7164. 2 L 7 3 4F A3WE 1999070200182 19990702 00182 NM 1999 7 2 DHL9970510C 1 19990520 A 7110 SKIN BOEING 727 72722C 138400F NM NR 1 ENG COWL CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, NR 1 LOWER COWL UNDER SKIN BELOW NR 3 U BOLT. REMOVED DAMAGED AREA, INSTALLED REPAIR PER SRM 54-10-3, SKIN 17 BY 21 FT, DOUBLER 25 BY 4 FT, N/R 6210. 2 L 7 3 4F A3WE 1999070200183 19990702 00183 NM 1999 7 2 DHL9970511C 1 19990526 A 7110 RIB BOEING 727 72722C 138400F NM NR 1 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, NR 1 LOWER COWL REPAIR CRACKING, NR 5 RIB. REMOVED AND REPLACED DAMAGED REPAIR PARTS PER SRM 51-30-2, 16 BY 3, N/R 6205. 2 L 7 3 4F A3WE 1999070200184 19990702 00184 NM 1999 7 2 DHL9970512C 1 19990526 A 7110 SKIN BOEING 727 72722C 138400F NM NR 3 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, 33 ENGINE LOWER COWL SKIN DAMAGED AROUND 3RD LATCH. REPLACED DAMAGED SECTIONS PER SRM 51-40-3, 6 BY 24, N/R 6202. 2 L 7 3 4F A3WE 1999070200185 19990702 00185 NM 1999 7 2 DHL9970513C 1 19990526 A 7110 SKIN BOEING 727 72722C 138400F NM NR 3 ENGINE COWL CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, NR 3 ENGINE LOWER COWL OUTER SKIN HAS COROSION HOLES FROM 45-55 FROM AFT END. CUT OUT DAMAGED AREA, FABRICA TED FILER PER SRM 54-10-3. FILLER 4.65 BY 14.375; DOUBLER 8.375 BY 16.375, N/R 6200. 2 L 7 3 4F A3WE 1999070200186 19990702 00186 NM 1999 7 2 DHL9970514C 1 19990526 A 7110 SKIN BOEING 727 72722C 138400F NM NR 3 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C-CHECK, NR 3 ENGINE UPPER COWL CRACKED AND DAMAGED AT AFT OUTBOARD LATCH CUTOUT. REMOVED OLD REPAIR AND REPLACED PER SRM 51-30-2, 17 BY 4, N/R 6196. 2 L 7 3 4F A3WE 1999070200187 19990702 00187 NM 1999 7 2 DHL9970515C 1 19990525 A 7110 SKIN BOEING 727 72722C 138400F NM NR 3 ENGINE COWL SCRATCHED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, NR 2 ENGINE COWL LT FWD HAS SCRATCH ON EXT SKIN. INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 4 BY 6, N/R 6191 . 2 L 7 3 4F A3WE 1999070200188 19990702 00188 NM 1999 7 2 DHL9970516C 1 19990525 A 7110 SKIN BOEING 727 72722C 138400F NM NR 2 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, NR 2 ENGINE COWL LT FWD HAS AFT BOTTOM CORNER WITH CRACK AND PIECE MISSING. CUT OUT CRACKED SECTION, INSTAL LED REPAIR PER SRM 54-10-3. FILLER 3 BY 1, DOUBLER 8 BY 3, N/R 6189. 2 L 7 3 4F A3WE 1999070200189 19990702 00189 NM 1999 7 2 DHL9970517C 1 19990528 A 2510 SEAT BOEING 727 72722C 138400F NM COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, FLIGHT ENGINEER SEAT TRACK FRAME CRACKED. STOP DRILLED CRACK, HFEC, INSTALLED REPAIR PER SRM 51-30-3, 51-30 -2. N/R 5050. 2 L 7 3 4F A3WE 1999070200190 19990702 00190 NM 1999 7 2 DHL9970518C 1 19990527 A 5542 SKIN BOEING 727 72722C 138400F NM RUDDER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, LOWER RUDDER HAS CORNER OF L/E REPAIR DELAMINATING RT SIDE NEAR ACTUATOR. INSTALLED BONDING REPAIR PER SRM 51-20-3, 7 BY 1, N/R 4206. 2 L 7 3 4F A3WE 1999070200191 19990702 00191 NM 1999 7 2 DHL9970519C 1 19990605 A 5312 BULKHEAD BEAM BOEING 727 72722C 138400F NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, FWD SIDE OF BS 1183 BULKHEAD BEAM CRACKED BBL 36.8 LEFT WL 214, JUST ABOVE CABIN FLOOR. STOP DRILL, HFEC, I NSTALLED REPAIR PER S/B 53A0173, 9.75 BY 5.75, N/R 3370. 2 L 7 3 4F A3WE 1999070200192 19990702 00192 NM 1999 7 2 DHL9970520C 1 19990603 A 5347 659927193 SEAT TRACK BOEING 727 72722C 138400F NM BS 599 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 AT C CHECK, NR 2 SEAT TRACK LOCK FLANGES BROKEN OFF AT STA 599 LBL 48. REMOVED SEAT TRACK FROM BS 530 TO 660. INSTALLE D NEW TRACK PER SRM 53-10-5, N/R 5069. 2 L 7 3 4F A3WE 1999070200193 19990702 00193 EA 1999 7 2 COMA9960290 1 19990613 A 5230 601R3505025 SUPPORT CNDAIR CL600 CL6002B19 EA CARGO COMPT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 946CA 7072 CARGO DOOR SLIDE BRACKET SUPPORT CRACKED. REPLACED SUPPORT. 2 L 7 2 4F RT A21EA 1999070200194 19990702 00194 WP 1999 7 2 TWAA9908901 1 19990626 A 3397 58531 WIRE DOUG DC9 DC931 3022065 WP ROW 14 WORN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 977Z 47249 THE FORWARD SECTION OF THE COACH CABIN FLOOR EGRESS LIGHTS WAS INOPERATIVE. FOUND A HOLE IN THE FEEDER CABLE. REPLACED THE FEEDER CABLE FROM THE POWER SUPPLY TO THE LIGHT STRIP AT ROW 14. CHECK-C 11-13-98 STL. 2 L 7 2 4F A6WE 1999070200195 19990702 00195 WP 1999 7 2 TWAA9908902 1 19990625 A 3350 BATTYERY PACK DOUG DC9 DC931 3022065 WP ROW 21-24 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 984Z 47412 THE EGRESS FLOOR LIGHTS WERE INOPERATIVE FROM ROW 21 TO ROW 24, AND THE LEFT AND RIGHT OVERWING EXIT SIGNS WERE INOPERAT IVE AT ROW 15. REPLACED THE BATTERY PACK (P/N 5822-2) FOR THE EGRESS LIGHTS, AND THE BATTERIES (P/N 41B004AD07G3) FOR T HE EXIT SIGNS. CHECK-C 3-5-99 STL. 2 L 7 2 4F A6WE 1999070200196 19990702 00196 WP 1999 7 2 TWAA9908903 1 19990623 A 5320 9911503167 STIFFENER DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND COCKPIT VERTICAL STIFFENER NUMBER 9911503-167 WAS CRACKED IN THE RADIUS APPROXIMATELY 1. 5 INCH LONG, APPROX 2 INCHES BELOW TOP OF STIFFENER AT STA 69.5, AFT SIDE OF BULKHEAD ON X=-12 ON RT SIDE. MADE UP DOUB LER AND INSTALLED PER ARA 13513. 2 L 7 2 4F A6WE 1999070200197 19990702 00197 WP 1999 7 2 TWAA9908904 1 19990623 A 5312 BULKHEAD BRACE DOUG DC9 DC931 3022065 WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND AFT PRESSURE BULKHEAD, FORWARD SIDE DIAGIONAL BRACE ON PRESSURE BULKHEAD AT STA 996, CRA CKED AT UPPER END BETWEEN LONGERON 3L AND 4L. REMOVED, FABRICATED AND REINSTALLED ANGLE AT UPPER DIAGONAL BRACE, STA 99 6 BETWEEN L3L ANG L4L PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999070200198 19990702 00198 WP 1999 7 2 TWAA9908905 1 19990623 A 5320 99115057 ANGLE DOUG DC9 DC931 3022065 WP BS 83.55 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND COCKPIT CENTER FRAME ANGLE 9911505-7 WAS CRACKED APPROXIMATELY 1.5 INCH IN RADIUS AT I/B END STA 83.55, X=10.00, Z=42, ON LT SIDE. INSTALLED NEW FRAME PER ITEM 30 OF EMLR 69590. 2 L 7 2 4F A6WE 1999070200199 19990702 00199 WP 1999 7 2 TWAA9908906 1 19990617 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 200, BETWEEN NUMBER 1 AND 2 SEAT TRACKS. REPLACED FLO OR SUPPORT PER STD PROCESSES MANUAL 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999070200200 19990702 00200 WP 1999 7 2 TWAA9908907 1 19990617 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT NUMBER 2 SEAT TRACK TO CENTERLINE, STA 200. REPLACED FLOO R SUPPORT PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999070200201 19990702 00201 WP 1999 7 2 TWAA9908908 1 19990622 A 5311 99115056 FRAME DOUG DC9 DC931 3022065 WP BS 83.55 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND COCKPIT FRAME CRACKED AT STA 83.55, X=-11 INCHES, APPROXIMATELY 1.5 INCHES LONG ON RT SI DE. REPAIRED PER SRM 53-03, FIG 34 SHEET 1 TO 7. 2 L 7 2 4F A6WE 1999070200202 19990702 00202 WP 1999 7 2 TWAA9908909 1 19990622 A 5311 99115055 FRAME DOUG DC9 DC931 3022065 WP BS 83.55 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND COCKPIT FRAME 5 ON LT SIDE WAS CRACKED IN RADIUS AT X=+10 CONFIRMED WITH EDDY CURRENT. C RACK WAS APPROXIMATELY .75 INCH LONG AT STA 83.55. REPAIRED PER SRM 53-03 FIG 34, SHEETS 1 TO 7. 2 L 7 2 4F A6WE 1999070200203 19990702 00203 WP 1999 7 2 TWAA9908910 1 19990618 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND STA 200 FLOORBEAM CAP CORRODED JUST OUTBOARD OF NUMBER 4 CHAIR TRACK. REPAIRED FLOORBEA M PER SRM 53-05, PAGE 31. 2 L 7 2 4F A6WE 1999070200204 19990702 00204 NM 1999 7 2 TWAA9908911 1 19990623 A 2730 251T20021 TEE BOEING 767 767231 1385131 NM RT ELEVATOR WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 DURING CHECK-C MAINT MO-72F01A, REQUIRED THE RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE HAVE THE TEE REPLACED PER FIG 2 OF SERVICE BULLETIN 767 27A0136. REMOVED AND REPLACED THE TEE PER MO 72F01 PHASE A AND REF BOEING SERVICE BULLETIN 76 7 27A0136. 2 L 7 2 4F RT A1NM 1999070200205 19990702 00205 NM 1999 7 2 HNAA9900071 1 19990616 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 517-520 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 STRINGER 31S HAS PITTS AT TWO RIVETS, LOCATED AT APROX X520 AND X512. RIVETS NEED REMOVED FOR FURTHER EVALUATION. REMO VED FIVE RIVETS AT STRINGER 31S APROX X520 AND X517. FOUND AREA EXCESSIVELY PITTED. TWO AREAS OUT OF LIMITS APROX .015 AND ONE AREA IN RADIUS APROX .020. REMOVED AND REPLACED STRINGER. 2 H 7 2 4T RT A13NM 1999070200206 19990702 00206 NM 1999 7 2 HNAA9900072 1 19990623 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 510 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 FRAME AT STATION X510 HAS CORROSION AND IS SPLIT WHERE IT MEETS THE SKIN. DAMAGES ARE JUST O/B OF STRINGER 31S. MANUFA CTURED REPAIR ANGLE IAW SRM 53-20-21, ALODINED AND PRIMED ANGLE. REMOVED AND REPLACED FRAME LEG. 2 H 7 2 4T RT A13NM 1999070200207 19990702 00207 WP 1999 7 2 AT9900464 1 19990627 A 2560 SLIDE DOUG DC9 DC932 3022066 WP R-1 DOOR DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 R-1 DOOR SLIDE LOOSE. REINSTALLED R-1 DOOR SLIDE IN BIN PER MM 25-61-0, RII COMPLIED WITH. 2 L 7 2 4F A6WE 1999070200208 19990702 00208 NM 1999 7 2 AT9900465 1 19990626 A 7331 8DJ88LWX3 INDICATOR BOEING 737 737284 138448R NM PWA JT8 JT8D9A 52048 NE NR 2 FUEL FLOW DEFECTIVE A ZZDA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 15 470AT 21501 AT FLIGHT LEVEL 250 AT 1.6 ENGINE PRESSURE RATIO AT FUEL FLOW 3000 NR 2 ENGINE ROLLED BACK TO PLUS 500 FUEL FLOW, SHUT E NGINE DOWN AND AIR STARTED NORMALLY. RAN NORMAL TO LAND. REMOVED AND REPLACED NR 2 FUEL FLOW INDICATOR AND OPS CHECKED GOOD IAW MM 28-40. 2 L 7 2 4F 4 F A16WE E2EA 1999070200209 19990702 00209 WP 1999 7 2 AT9900466 1 19990522 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 240 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND FLOOR SUPPORT AT BS 240 BL-0 CORRODED. REMOVED FLOOR SUPPORT, FABRI CATED FOUR REPAIR ANGLES. HEAT TREATED, DRILLED, DEBURRED, COUNTERSUNK AND INSTALLED ANGLES IAW DC9 SRM 51-10-4, 51-30- 2 AND TIMCO EO NR 99-1162. 2 L 7 2 4F A6WE 1999070200210 19990702 00210 WP 1999 7 2 AT9900467 1 19990601 A 5230 49286651 STOP DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD CARGO DOOR STOPS CHAFED AND CORRODED. REMOVED AND REPLA CED 10 NEW PADS IAW DC9 SRM 51-30-2 AND OHM 52-30-1 PG 57. 2 L 7 2 4F A6WE 1999070200211 19990702 00211 WP 1999 7 2 AT9900468 1 19990617 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 218 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND WEB ON CUSP LINE AT BS 218L CRACKED AND CORRODED. FABRICATED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-30-1 AND 53-20-1. 2 L 7 2 4F A6WE 1999070200212 19990702 00212 NM 1999 7 2 AT9900469 1 19990626 A 3350 6013211 BATTERY BOEING 737 7372L9 1384497 NM EMER EXIT DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 737Q 21279 DURING LAYOVER, FOUND R-2 AND L-2 EMEGENCY SLIDE LIGHTS NOT ILLUMINATING. REPLACED OVERWING BATTERY PACK, OPS CHECKED G OOD IAW MM 33-51-31. 2 L 7 2 4F RT A16WE 1999070200213 19990702 00213 WP 1999 7 2 AT9900470 1 19990609 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 828-865 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT HAND FLOOR SUPPORT AT BS 828-865 CORRODED AROUND FASTENER H OLES. REMOVED AND FABRICATED REPLACEMENT IAW DC9 SRM 51-10-2, 53-01 FIG 1, 51-30-2 AND 51-10-2. 2 L 7 2 4F A6WE 1999070200214 19990702 00214 WP 1999 7 2 AT9900471 1 19990618 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT BS 218 CORRODED . FABRICATED SUPPORT ANGLE AND INSTALLED IAW DC9 SRM 51-10-2, 53-01 FIG 2, AND 51-10-4. 2 L 7 2 4F A6WE 1999070200215 19990702 00215 NM 1999 7 2 AWXA9900228 1 19990624 A 2910 15530030237 HOSE BOEING 737 737277 1384570 NM NLG LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 179AW 22646 EN ROUTE ELP-LAS, AFTER TAKEOFF HYDRAULIC OVERHEAD PANEL LIGHTS ILLUMINATED NR 1 AND NR 2 ENGINE A HYD SYSTEM. HYDRAULI C QUANTITY FLUCTUATING TO 0. CAUTION LIGHTS FLICKERING FOR 30 SECONDS, THEN REMAINED ON. A HYDRAULIC QUANTITY REMAINED AT 0 GALLONS. RETURNED TO ELP. FOUND NOSE GEAR MAIN ACTUATOR HYDRAULIC RETURN LINE LEAKING. REPLACED ACTUATOR RETURN LINE, SERVICED SYSTEM, OPS AND LEAK CHECK OK IAW MM 32-33-00. 2 L 7 2 4F RT A16WE 1999070200216 19990702 00216 NM 1999 7 2 CALA9900720 1 19990623 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 907 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A 2 INCH CRACK IN STRINGER 4L AT STA 907. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999070200217 19990702 00217 NM 1999 7 2 CALA9900721 1 19990625 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A 1 INCH CRACK IN BELTFRAME AT STRINGER 16R AFT OF STA 500C. THE CRACKED SECTION OF FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, DETAIL VII. 2 L 7 2 4F RT A16WE 1999070200218 19990702 00218 WP 1999 7 2 CALA9900722 1 19990625 A 5312 BULKHEAD ANGLE DOUG DC9 DC982 3022082 WP AFT PRESS BLKHD WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND ANGLE STIFFENER WORN THREE QUARTERS OF WAY THROUGH FROM STAINLESS LINE ON LT SIDE OF APB AFT FACE. REP AIRED IAW ECRA 5330-02837. 2 L 7 2 4F A6WE 1999070200219 19990702 00219 NM 1999 7 2 CALA9900723 1 19990625 A 5510 69144106 HINGE PIN BOEING 727 727227 1384078 NM HORIZ STAB BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND HORIZONTAL STABILIZER LT HINGE PIN BROKEN. REPAIR ACCOMPLISHED IAW ECRA 5530-01244. 2 L 7 3 4F A3WE 1999070200220 19990702 00220 NM 1999 7 2 CALA9900724 1 19990625 A 5510 HINGE BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND HORIZONTAL STABILIZER LT HINGE HOUSING INTERIOR SCORED AND CORRODED WITH O/B AREA SHOWING SIGNS OF BEAR ING PLAY ON VERTICAL CAP. REPAIRED IAW ECRA 5530-01244. 2 L 7 3 4F A3WE 1999070200221 19990702 00221 NM 1999 7 2 CALA9900725 1 19990625 A 5510 HINGE BOEING 727 727227 1384078 NM HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND HORIZONTAL STABILIZER RT HINGE HOUSING INTERIOR CHIPPED WITH A 3 INCH CRACK ON VERTICAL CAP. REPAIRED IAW ECRA 5530-01244. 2 L 7 3 4F A3WE 1999070200222 19990702 00222 WP 1999 7 2 CALA9900726 1 19990626 A 7830 9007M60G51 TR UNIT DOUG DC10 DC1030 3023501 WP NR 1 ENGINE DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND NR 1 ENGINE O/B TRANSLATING COWL DELAMINATED AT AFT INNER LOWER SECTION. REPAIRED IAW MM 78-32-01. 2 L 7 3 4F A22WE 1999070200223 19990702 00223 NM 1999 7 2 CALA9900727 1 19990626 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L JUST AFT OF STA 500C. THE STRINGER WAS REPAIRED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 1999070200224 19990702 00224 NM 1999 7 2 CALA9900728 1 19990626 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 30 TO RBL 11. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A REP AIR SECTION AND SPLICE WAS INSTALLED IAW SRM 53-00-51, FIGURE 202. 2 L 7 2 4F RT A16WE 1999070200225 19990702 00225 NM 1999 7 2 CALA9900729 1 19990626 A 5400 SUPPORT BOEING 737 7373T0 1384582 NM NR 1 NACELLE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE DIAGONAL FRAME SUPPORT AT NACELLE STA 315 ON RT SIDE. THE DIAGONAL FRAME SUPPORT WAS REPLACED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999070200226 19990702 00226 WP 1999 7 2 CALA9900730 1 19990627 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 THE TAIL CONE RELEASE PULL WAS EXCESSIVE USING THE INTERIOR AND EXTERIOR HANDLES AND AFT ENTRY DOOR. THE TAIL CONE CABL ES WERE ADJUSTED/TESTED IAW MM 53-53-00, PARAGRAPH 3(A)&(B). DROP TEST PULLED WITHIN ALLOWABLE LIMITS. 2 L 7 2 4F A6WE 1999070200227 19990702 00227 NM 1999 7 2 CALA9900731 1 19990627 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A 4 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 500, STRINGER 14R. THE CRACKED SECTION OF FRAME WAS CU T OUT. REPAIR DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-00-07, FIGURE 201. 2 L 7 2 4F RT A16WE 1999070200228 19990702 00228 NM 1999 7 2 CALA9900732 1 19990628 A 5753 113N34004A SKIN BOEING 757 757224 1384958 NM LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14107 27297 INSPECTION FOUND A .75 INCH CRACK IN LEFT O/B TRAILING EDGE FLAP BY NR 3 SPOILER. THE FLAP WAS REPAIRED IAW ECRA 5731-0 1015. 2 L 7 2 4F RT A2NM 1999070200229 19990702 00229 WP 1999 7 2 CALA9900733 1 19990628 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1841 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 2 INCH CRACK ON VERTICAL ANGLE IN CENTER CARGO COMPARTMENT AT STA 1841, LBL 10. THE ANGLE WAS REMOVE D AND A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070200230 19990702 00230 WP 1999 7 2 CALA9900734 1 19990628 A 5320 WALL DOUG DC10 DC1030 3023501 WP BS 1841 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND TEARS ON VERTICAL WALL IN CENTER CARGO COMPARTMENT AT STA 1841 BETWEEN LBL 40 & 60. THE TORN AREAS WER E TRIMMED OUT AND DEBURRED. REINFORCED AREAS WITH DOUBLER IAW SRM 53-00-01, FIGURE 4 AND INSTALLED RIVETS IAW SRM 51-33 -01. 2 L 7 3 4F A22WE 1999070200231 19990702 00231 WP 1999 7 2 CALA9900735 1 19990628 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1741 & 1761 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND CORROSION ON BOTH LOWER SIDES OF FRAME AT STA 1741 AND 1761 BETWEEN STRINGER 47L AND 50R. THE CORRODED AREAS WERE REMOVED, NEW ANGLES WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070200232 19990702 00232 WP 1999 7 2 CALA9900736 1 19990628 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1851-1868 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND STRINGER 50 CORRODED BETWEEN STA 1851 AND 1868. THE CORRODED SECTION WAS REMOVED, A NEW SECTION OF STR INGER WAS INSTALLED WITH REINFORCEMENT IAW SRM 51-31-01 AND 53-10-00, FIGURE 2. 2 L 7 3 4F A22WE 1999070200233 19990702 00233 NM 1999 7 2 CALA9900737 1 19990628 A 5230 SKIN BOEING 757 757224 1384958 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14107 27297 INSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO DOOR SKIN. REPAIRED IAW ECRA 5231-01015. 2 L 7 2 4F RT A2NM 1999070200234 19990702 00234 NM 1999 7 2 CALA9900738 1 19990628 A 5753 SKIN BOEING 757 757224 1384958 NM RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14107 27297 INSPECTION FOUND A .75 INCH CRACK IN RIGHT O/B TRAILING EDGE FLAP BY NR 10 SPOILER. THE FLAP WAS REPAIRED IAW ECRA 5731 -01015. 2 L 7 2 4F RT A2NM 1999070200235 19990702 00235 SO 1999 7 2 COMA9910099 1 19990624 A 3350 SIGN EMB 120 EMB120RT SO ROW 5 DETACHED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 120267 EMERGENCY EXIT SIGN AT ROW 5 FELL OFF. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999070200236 19990702 00236 SO 1999 7 2 COMA9910100 1 19990624 A 3350 SIGN EMB 120 EMB120RT SO PASSENGER DOOR MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 120264 EMERGENCY EXIT SIGN ON BULKHEAD AT CABIN DOOR WAS MISSING. REPLACED EXIT SIGN ASSY. 2 L 7 2 4T RT A31SO 1999070200237 19990702 00237 EA 1999 7 2 COMA9960311 1 19990625 A 2730 BUSHINGS CNDAIR CL600 CL6002B19 EA RT ELEVATOR WORN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947CA 7077 INSPECTION TASK 00227900106 RIGHT HAND ELEVATOR FAILED BACKLASH CHECK. THE ELEVATOR TO PCU ATTACH POINT BUSHING WERE WO RN AND THE ATTACH BOLTS WERE WORN APPROXIMATELY HALFWAY THROUGH. 2 L 7 2 4F RT A21EA 1999070200238 19990702 00238 EA 1999 7 2 COMA9960312 1 19990624 A 2910 HOSE CNDAIR CL600 CL6002B19 EA NR 1 HYD SYST FAILED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 778CA 7297 NR 1 HYDRAULIC SYSTEM CAUTION, ZERO QUANTITY AND ZERO PRESSURE. REPLACED HOSE ASSY IN AFT EQUIP BAY. 2 L 7 2 4F RT A21EA 1999070200239 19990702 00239 EA 1999 7 2 COMA9960313 1 19990619 A 5320 SUPPORT CNDAIR CL600 CL6002B19 EA BS 62100 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 7174 CARGO FLOOR SUPPORT ANGLES AT FS 62100, WL 73, LEFT AND RIGHT SIDE CRACKED. REMOVED CRACKED PART AND REPLACED WITH NEW ANGLE AND DOUBLER IAW CANADAIR REO 601R5361117, REV A. 2 L 7 2 4F RT A21EA 1999070200240 19990702 00240 EA 1999 7 2 COMA9960314 1 19990619 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA BS 62100 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 CARGO FLOOR SUPPORT ANGLE AT FS 62100, WL 73 LEFTHAND SIDE IS CRACKED. REMOVED CRACKED PART AND REPLACED WITH NEW ANGLE AND DOUBLER IAW CANADAIR REO 601R5361117, REV A. 2 L 7 2 4F RT A21EA 1999070200241 19990702 00241 EA 1999 7 2 COMA9960315 1 19990619 A 5311 FRAME CNDAIR CL600 CL6002B19 EA BS 71800 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 FRAME 71800, STR 11 CRACKED AT FLANGE AND AFT SIDE DOUBLER ON RHS FUSELAGE AND AT AFT SIDE DOUBLER ON LHS FUSELAGE STR 1 1, FS 17800. REPLACED FRAME 71800 RHS IAW WVAC EO 601R530075. REPAIRED DOUBLER AT FS 71800 + STR 11 RHS IAW WVAC EO 60 1R530073. REPAIRED DOUBLER AT FS 71800 + STR 11 LHS IAW WVAC EO 601R530072. 2 L 7 2 4F RT A21EA 1999070200242 19990702 00242 NM 1999 7 2 SCNA99087 1 19990623 A 3350 1102833 POWER SUPPLY BOEING 727 7272A1 138407F NM AFT AIRSTAIR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE AFT AIRSTAIR POWER SUPPLY, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999070200243 19990702 00243 NM 1999 7 2 SCNA99712 1 19990607 A 3350 BULB BOEING 727 7272K3 138400D NM ROW 5 FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 DURING HEAVY MAINTENANCE CHECK, THE AISLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE AT ROW 5. RELAMPED AISLE EMERGENCY EXIT LIGHT IAW B727 MM 335001. 2 L 7 3 4F RT A3WE 1999070200244 19990702 00244 NM 1999 7 2 BJNA990501 1 19990427 A 3350 6013211 POWER SUPPLY BOEING 737 737282 13844AT NM EXTERIOR INOPERABLE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 DURING CONFORMITY INSPECTION, FOUND AFT EXTERIOR EMERGENCY ESCAPE SLIDE LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY POWER SUPPLY PER BMM 33-51-71. (X) 2 L 7 2 4F RT A16WE 1999070200245 19990702 00245 NM 1999 7 2 BJNA990502 1 19990429 A 3350 1000679 LIGHT BOEING 737 737282 13844AT NM PASSENGER DOOR INOPERABLE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 DURING CONFORMITY INSPECTION, FOUND FORWARD ENTRY DOOR EXIT LIGHT INOPERABLE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY ON FORWARD ENTRY DOOR PER BMM 33-51-101. (X) 2 L 7 2 4F RT A16WE 1999070200246 19990702 00246 1999 7 2 99ZZZX2465 4 19990507 A 2565 PINS D30311507 LKHEED 1011 10113853 5265020 WP R3 SLIDE BENT A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 162AT 2611 1220 DURING PRE-FLIGHT, FOUND SOME PARACHUTE PINS PULLED AND BENT ON THE NR R3 SLIDE. REMOVED AND REPLACED SLIDE PER MM. (X ) 2 L 7 3 4F A23WE 1999070200247 19990702 00247 EA 1999 7 2 ASOA99040 1 19990422 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 841AS 7300 TAT - FLT 4700 - PILOT REPORTED FLAPS FAILED ON FINAL APPROACH WHEN SELECTED FROM FLAPS 30 DEGREES TO FLAPS 45 DEGREES. FLAPS FAILED AT 42 DEGREES. LEFT OUTBOARD FLAP WAS FOUND TO BE TWISTED. NR 3 ACTUATOR FAILED TO FULLY EXTEND. LEFT O UTBOARD FLAP AND BOTH ACTUATORS WERE REPLACED. FLAPS WERE RE-RIGGED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RELEA SED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200248 19990702 00248 WP 1999 7 2 99ZZZX2466 1 19990508 A 5730 595591368 PANEL DOUG DC9 DC932 3022066 WP RT WING CRACKED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 35 930BB 47521 DURING POST-FLIGHT WALKAROUND, FOUND THE RT UPPER WING-TO-FUSELAGE FAIRING (SECOND FROM FORWARD) BENT BACK AT THE LEADIN G EDGE, AND CRACKED IN THE AFT CENTER AREA. THE FAIRING ATTACHING HARDWARE WAS STILL INSTALLED. PART REPLACED. INSPEC TION OF THE AIRCRAFT AND RT ENGINE REVEALED NO MATERIAL SEPARATION OR ADDITIONAL DAMAGE. REF: IPC 53-50-00/FIGURE 4/IT EM 25. REF: AIRCRAFT TT: 77,810.6 HOURS AND TC: 58,315. (X) 2 L 7 2 4F A6WE 1999070200249 19990702 00249 NM 1999 7 2 99ZZZX2467 1 19990515 A 2910 LLINE BOEING 727 727214 138407R NM A-HYD SYSTEM FAILED A AMTA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 11 788AT 21958 INBOUND TO O-HARE, HYDRAULIC FLUID LOSS DOWN TO ONE GALLON. A-SYSTEM PUMPS DEPRESSURIZED BEFORE LOW PRESSURE LIGHTS ILL UMINATED. LANDED WITHOUT FURTHER INCIDENT. FOUND THE A-SYSTEM HYDRAULIC PRESSURE TRANSMITTER LEAKING. REPLACED THE HY DRAULIC LINE THAT GOES TO TRANSMITTER. CHECKED FOR LEAKS AND NO LEAKS NOTED. 2 L 7 3 4F A3WE 1999070200250 19990702 00250 NM 1999 7 2 BJNA990404 1 19990423 A 3350 CONNECTOR BOEING 737 737282 13844AT NM CABIN DIRTY A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 WITH FLOOR TRACK LIGHTING ON, STANDING AT MID-CABIN, LIGHTS FLICKER. CLEANED AND SECURED CONNECTIONS. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999070200251 19990702 00251 NM 1999 7 2 99ZZZX2468 1 19990422 A 3350 BATTERY PACK 6104789 BOEING 737 737282 13844AT NM CARGO COMPT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 LEFT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND RPELACED AFT PIT EMERGENCY BATTEYR PACK PER BMM 33-51-31. O PS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999070200252 19990702 00252 SO 1999 7 2 99ZZZX2469 1 19990524 A 3350 3025101 LIGHT EMB 145 EMB145 SO RT EMERG EXIT INOPERABLE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13956 145078 IAH - DURING MAINTENANCE INSPECTION, THE RT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERABLE. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999070200253 19990702 00253 EA 1999 7 2 COMA9960239 1 19990524 A 5753 601R1430342 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 RIGHT INBOARD FLAP LEADING EDGE MOVEABLE VANE CHAFED. REPLACED MOVEABLE VANE LEADING EDGE IAW AERODESIGN REPORT NR 1286 -1. (X) 2 L 7 2 4F RT A21EA 1999070200254 19990702 00254 EA 1999 7 2 COMA9960238 1 19990524 A 5753 601R1430341 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7123 CKB - LEFT INBOARD FLAP LEADING EDGE MOVEABLE VANE CHAFED. REPLACED MOVEABLE VANE LEADING EDGE IAW AERODESIGN REPORT NR 1286-1. (X) 2 L 7 2 4F RT A21EA 1999070200255 19990702 00255 EA 1999 7 2 COMA9960237 1 19990525 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 962CA 7570 7123 CKB - FRAME AT FS 718.00 AND STR 11 LHS HAS A .75 INCH CRACK EXTENDING THROUGH ONE FASTENER HOLE. REPAIRED IAW WVAC E.O . NR 601R-53-0048 REVISION A. PART TC: 7,268. (X) 2 L 7 2 4F RT A21EA 1999070200256 19990702 00256 EA 1999 7 2 COMA9960236 1 19990525 A 7830 TR UNIT CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 962CA 7123 TRI - FLT 5592 - RIGHT ENGINE THRUST REVERSER MESSAGE DURING TAKEOFF. DEFERRED T/R SYSTEM AND AIRCRAFT CONTINUED SERVI CE. (X) 2 L 7 2 4F RT A21EA 1999070200257 19990702 00257 EA 1999 7 2 COMA9960235 1 19990525 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 1428 531 7017 MDT - FLT 5396 - FLAPS FAILED AT 20 DEGREES. REPLACED THE FECU. PART TC: 1,518. (X) 2 L 7 2 4F RT A21EA 1999070200258 19990702 00258 EA 1999 7 2 COMA9960240 1 19990528 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 EA LT COCKPIT FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 947CA 9357 7077 CVG - FLT 5749 - LEFT WINDOW HEAT MESSAGE. REPLACED WINDOW. PART TC: 9,088. (X) 2 L 7 2 4F RT A21EA 1999070200259 19990702 00259 EA 1999 7 2 COMA9960231 1 19990524 A 5101 STRUCTURE CNDAIR CL600 CL6002B19 EA AIRFRAME BIRD STRIKE A COMA K NONE C F.O.D. AP APPROACH 1 SO 01 778CA 7297 CHA - FLT 5535 - BIRD STRIKE DURING LANDING APPROACH. C/W BIRD STRIKE INSPECTION. NO DAMAGE FOUND. (X) 2 L 7 2 4F RT A21EA 1999070200260 19990702 00260 EU 1999 7 2 SIMA991131 1 19990423 A 3260 AIR130902 SWITCH SAAB SF340 340B 7860101 EU LT MLG FAILED A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 286AE 340B286 MRY - FLT 3215 - LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. DEFERRED LANDING GEAR AND ROUTED AIRCRAFT INT O SBP WHERE THE LEFT MAIN LANDING GEAR DOWNLOCK SWITCH WAS REMOVED AND REPLACED. FUNCTIONAL CHECK PERFORMED, THE MEL IT EM WAS RESTORED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999070200261 19990702 00261 EU 1999 7 2 SIMA99117 1 19990421 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 349SB 340B349 DFW - FLT 5130 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 11 DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB. OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999070200262 19990702 00262 EU 1999 7 2 SIMA991021 1 19990412 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISDCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 550LL 0973 550 SAW - DURING PS-2 INSPECTION, FOUND THE LEFT FORWARD CABIN EMERGENCY LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACE D THE BATTERY PACK AND OPERATIONAL CHECKED THE EMERGENCY LIGHTS IAW JIC 335121-RA-10000. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999070200263 19990702 00263 SO 1999 7 2 SIMA991011 1 19990411 A 3350 7287580503 LIGHT EMB 145 EMB145 SO ROWS 17-18 BROKEN A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 610AE 145073 DFW - FLT 3675 - EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROWS 17 AND 18 DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGH T STRIP DUE TO A BROKEN CONNECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999070200264 19990702 00264 EU 1999 7 2 SIMA990982 1 19990408 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 10 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AE 340B348 SBP - DURING PS-2 INSPECTION, FOUND EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 10B/C DOES NOT ILLUMINATE. REMOVED AND REPL ACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999070200274 19990702 00274 NM 1999 7 2 TWAA9909001 1 19990627 A 3350 20131A BATTERY PACK BOEING 767 767231 1385131 NM BS 1400 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 605TW 22568 FOUND THE RT OVERWING SLIDE LIGHT AND THE EMERGENCY LIGHT FORWARD OF THE RIGHT AFT CABIN DOOR WERE INOPERATIVE. REPLACE D THE BATTERY PACK. CHECK-C 5-8-99 LAX. 2 L 7 2 4F RT A1NM 1999070200275 19990702 00275 NM 1999 7 2 TWAA9909002 1 19990616 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 412 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 603TW 22566 DURING CHECK-C MAINT FOUND CORROSION AT APPROXIMATELY STA 412, STRINGER 36R. REMOVED 26 INCH LONG DAMAGED SECTION OF ST RINGER 36R AND INSTALLED NEW SECTION PER SRM 53-00-03. 2 L 7 2 4F RT A1NM 1999070200276 19990702 00276 NM 1999 7 2 TWAA9909003 1 19990616 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 412 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 603TW 22566 DURING CHECK-C MAINT FOUND AT STA 412 AND STRINGER 34R THE STRINGER WAS CRACKED DUE TO CORROSION IN TWO PLACES. REMOVED 29 IN DAMAGED SECTION AND INSTALLED NEW SECTION WITH SPLICE REPAIR PER SRM 53-00-03. 2 L 7 2 4F RT A1NM 1999070200277 19990702 00277 NM 1999 7 2 HNAA9900073 1 19990623 A 5510 FASTENERS DHAV DHC8 DHC8102 2809003 NM HORIZ STAB CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 HORIZONTAL STAB ON UNDERSIDE, 4 HI-LOKS CORRODED AT CENTER BOX, CENTER DOUBLER AFT ROW (MARKED). REMOVED AND REPLACED H I-LOKS. 2 H 7 2 4T RT A13NM 1999070200278 19990702 00278 NM 1999 7 2 HNAA9900074 1 19990615 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 771.803 WRINKLED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 SEVERAL WRINKLES ON BOTTOM FUSELAGE SKIN AT FS 771.803, JUST FORWARD OF TAIL BUMPER BETWEEN STRINGER 31P AND 31S. PER E NGINEERING DISPOSITION, NO FURTHER ACTION REQUIRED, APPLIED YELLOW DOT TO AREA. 2 H 7 2 4T RT A13NM 1999070200279 19990702 00279 NM 1999 7 2 HNAA9900075 1 19990616 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 520 & 517 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 STRINGER 31S HAS PITS AT TWO RIVETS, LOCATED AT APPROX X520 & X517. RIVETS NEED REMOVED FOR FURTHER EVALUATION. REMOV ED FIVE RIVETS AT STRINGER 31S APPROX X520 & X517. FOUND AREA EXCESSIVELY PITTED. REMOVED AND REPLACED SECTION OF STRI NGER AND TENSION FITTING. 2 H 7 2 4T RT A13NM 1999070200280 19990702 00280 NM 1999 7 2 HNAA9900076 1 19990623 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 510 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 FRAME AT STATION X510 HAS CORROSION AND IS SPLIT WHERE IT MEETS THE SKIN. DAMAGE IS JUST O/B OF STRINGER 31S. MANUF RE PAIR ANGLE IAW SRM 53-20-21. ALODINED AND PRIMED ANGLE, INSTALLED ANGLE AS REQUIRED. 2 H 7 2 4T RT A13NM 1999070200281 19990702 00281 NM 1999 7 2 HNAA9900077 1 19990613 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 202 & 207 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 RT CENTER SEAT RAIL HAS SEVERE PITTING CORROSION ON I/B WHICH HAS COMPLETELY CORRODED THROUGH THE METAL - OUT OF LIMITS. REMOVED AND REPLACED RAIL SECTION AND SPLICE. 2 H 7 2 4T RT A13NM 1999070200282 19990702 00282 NM 1999 7 2 HNAA9900078 1 19990613 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 130 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 RT CENTER SEAT RAIL AT FS 130.0 (APPROX) HAS PITTING CORROSION ON TOP FLANGE APPROX .015 DEEP. .010 ALLOWABLE - OUT OF L IMITS. REMOVED AND REPLACED RAIL AND SPLICE. 2 H 7 2 4T RT A13NM 1999070200283 19990702 00283 NM 1999 7 2 HNAA9900079 1 19990613 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 134 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 RT CENTER SEAT RAIL AT FS 134 HAS DRILL HOLE DAMAGE. A DRILL HOLE MEASURING .100 DEEP ON TOP FLANGE (APPROX) REMAINING MATERIAL THICKNESS .042- OUT OF LIMITS. REMOVED AND REPLACED SEAT RAIL AND SPLICE. 2 H 7 2 4T RT A13NM 1999070200284 19990702 00284 NM 1999 7 2 HNAA9900080 1 19990615 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 500 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 CORROSION IN BELLY AT STRINGER 30P AT STATION 500 (WILL NEED SPLICE). REMOVED AND REPLACED STRINGER SPLICE. 2 H 7 2 4T RT A13NM 1999070200285 19990702 00285 NM 1999 7 2 HNAA9900081 1 19990617 A 5320 SILL PLATE DHAV DHC8 DHC8102 2809003 NM PASSENGER DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 LOWER PAX DOOR SILL PLATE HAS AREAS OF CORROSION. ALSO ADJOINING STRUCTURE HAS CORROSION ON LOWER SIDE AT TWO RIVETS AN D NUT PLATES. UPPER PLATE NEEDS REMOVED FOR FURTHER EVAL. REMOVED UPPER PLATE THRESHOLD FOR EVAL, REMOVED CORROSION ON LOWER SIDE AT RIVET AND NUT PLATES AND LOWER SILL PLATE. TREATED AND PRIMED SURFACES. INSTALLED NEW SILL PLATE AND SH IMMED AS REQUIRED. 2 H 7 2 4T RT A13NM 1999070200286 19990702 00286 WP 1999 7 2 IXXA9900012 1 19990629 A 2150 2040755 ACM DOUG DC8 DC871F 302199D WP LT PACK DEFECTIVE A IXXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 828BX 912 45993 EN ROUTE FROM PDX TO TOL, THE FLIGHT CREW NOTICE SMOKE EMMITTING INTO THE COCKPIT, ACCOMPANIED WITH LEFT PACK TEMPERATUR E INCREASING. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, SECURED THE LEFT PACK, SMOKE SUBSIDED. THE FLIGHT RETURNED TO PDX FOR AN UNEVENTUL LANDING. MAINTENANCE INSPECTED THE PACK SYSTEM WHICH REVEALED THE LEFT AIR CYCLE MACH INE DEFECTIVE. MAINTENANCE PLACED THE PACK ON DEFERRAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 1999070200287 19990702 00287 NM 1999 7 2 AWXA9900229 1 19990625 A 2740 65C25514 SWITCH BOEING 737 7373G7 1384595 NM STAB TRIM MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION LD LANDING 1 WP 28 158AW 23780 DURING LANDING, FIRST OFFICER'S FLYING PITCH TRIM WENT TO FULL NOSE-UP. PILOT WAS NOT ACTUATING THE SWITCH. REMOVED AN D REPLACED STAB TRIM CONTROL SWITCH, OPS CHECKED GOOD ON GROUND PER MM 27-41-97. 2 L 7 2 4F RT A16WE 1999070200288 19990702 00288 NM 1999 7 2 AWXA9900230 1 19990628 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 332AW 23384 EMERGENCY EVACUATION TRACK LIGHTING INOPERATIVE. CREW REPORTS EMERGENCY TRACK LIGHTING IN AISLE HAS WIRING EXPOSED IN C ENTER CABIN. REPLACED WIRING. REALIGNED AND RESECURED WIRING AND ASSOCIATED TRACK LIGHTS, FUNCTIONAL CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1999070200289 19990702 00289 EU 1999 7 2 AWXA9900231 1 19990628 A 2910 NAS16126 O-RING AIRBUS 320 A320231 3930325 EU GREEN HYD SYS CUT A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 621AW 053 AFTER TAKEOFF AT 11000 AGL, GREEN HYDRAULIC SYSTEM FAILED DUE LOW QUANTITY. EMERGENCY EQUIPMENT WAS DISPATCHED TO RUNWA Y. FOUND SAMPLING VALVE O-RING CUT AT GREEN SYSTEM MANIFOLD ASSEMBLY. REPLACED O-RING, SERVICED SYSTEM, RAN ENGINE, LE AK CHECK GOOD. ALL HYD PUMPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1999070200290 19990702 00290 WP 1999 7 2 CALA9900739 1 19990628 A 5350 CLIP DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 THE CLIP TENSION AT TAIL CONE RELEASE EXTERIOR HANDLE WAS TOO LOW. A NEW HANDLE RETAINING CLIP WAS INSTALLED AND ADJUST ED IAW MM 53-53-00, PAGE 519. 2 L 7 2 4F A6WE 1999070200291 19990702 00291 WP 1999 7 2 CALA9900740 1 19990628 A 5320 FRAME DOUG DC9 DC982 3022082 WP RT MLG DOORWAY WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND FORWARD UPPER CORNER OF RT MLG WHEEL WELL FORWARD DOOR JAMB FRAME WORN. THE FRAME WAS REPLACED AND A S PLICE REPAIR WAS INSTALLED IAW DOUGLAS DRAWING 5930584. 2 L 7 2 4F A6WE 1999070200292 19990702 00292 WP 1999 7 2 CALA9900741 1 19990628 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 48062 INSPECTION FOUND A 3 INCH CRACK IN BELTFRAME AT STA 1418, LONGERON 2R. REPAIR DOUBLERS WERE INSTALLED IAW DRAWING SR095 30003. 2 L 7 2 4F A6WE 1999070200293 19990702 00293 NM 1999 7 2 CALA9900742 1 19990628 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 312, LBL 17 TO RBL 38. INSTALLED REPAIR IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1999070200294 19990702 00294 NM 1999 7 2 CALA9900743 1 19990628 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND TOP SIDE OF FLOORBEAM CORRODED AT STA 967, RBL 20 AND LBL 30. THE CORRODED SECTION OF FLOORBEAM WAS RE MOVED AND A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1999070200295 19990702 00295 NM 1999 7 2 CALA9900744 1 19990628 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 294, LBL 25 TO RBL 15. A NEW FLOORBEAM AND DOUBLERS WERE INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999070200296 19990702 00296 NM 1999 7 2 CALA9900745 1 19990628 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND LOWER SIDE OF FLOORBEAM CORRODED AT NUT PLATE, STA 294.5, LBL 48. THE CORRODED SECTION WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999070200297 19990702 00297 NM 1999 7 2 CALA9900746 1 19990628 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 344-362 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 344 TO 362. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10- 2. 2 L 7 2 4F RT A16WE 1999070200298 19990702 00298 NM 1999 7 2 CALA9900747 1 19990628 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 340-380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 340-380. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 202. 2 L 7 2 4F RT A16WE 1999070200299 19990702 00299 SO 1999 7 2 COMA9910101 1 19990629 A 3240 2025000002 SWIVEL EMB 120 EMB120RT SO LT MLG BRAKE LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 159CA 1159 LEFT MAIN LANDING GEAR MIDDLE BRAKE SWIVEL LEAKING. REMOVED AND REPLACED SWIVEL. 2 L 7 2 4T RT A31SO 1999070200300 19990702 00300 EA 1999 7 2 COMA9960321 1 19990625 A 2910 601R76514719 LINE CNDAIR CL600 CL6002B19 EA NR 1 HYD SYS LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 778CA 663 7297 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING, ZERO PRESSURE AND ZERO QUANTITY. REPLACED HYDRAULIC HOSE ASSY, AIRCRAFT EQU IPMENT BAY. 2 L 7 2 4F RT A21EA 1999070200301 19990702 00301 EA 1999 7 2 COMA9960320 1 19990626 A 2121 3500023000 FAN CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 960CA 7117 SMOKE IN CABIN. REPLACED BROKEN FAN BY PASS CHECK VALVE. 2 L 7 2 4F RT A21EA 1999070200302 19990702 00302 EA 1999 7 2 COMA9960319 1 19990626 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 918CA 6706 7018 FLAPS FAILED. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999070200303 19990702 00303 EA 1999 7 2 COMA9960318 1 19990627 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 716CA 7250 CONFIG TRIM WARNING AND STAB TRIM WARNING. REPLACED THE HSTA. 2 L 7 2 4F RT A21EA 1999070200304 19990702 00304 EA 1999 7 2 COMA9960317 1 19990626 A 3230 848847 HYD PUMP CNDAIR CL600 CL6002B19 EA MLG WW MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 716CA 7250 LANDING GEAR GLOW TO EXTEND, GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 1999070200305 19990702 00305 EA 1999 7 2 COMA9960316 1 19990628 A 3350 601R461011 LIGHT CNDAIR CL600 CL6002B19 EA ROW 8 INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 719CA 7253 FLOOR PATH EMERGENCY LIGHTS ARE INOPERABLE FROM ROW 8 AFT. REPLACED FLOOR LIGHTING. 2 L 7 2 4F RT A21EA 1999070200306 19990702 00306 NM 1999 7 2 UPS99229981 1 19990624 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) ON LOWER CHORD OF BS 1130 FLOORBEAM AT NUT CLIP HOLES BL 0-RBL 50, WL 2 01. REPAIRED FLOORBEAM PER ER NR 99-5650. 2 L 7 3 4F A3WE 1999070200307 19990702 00307 NM 1999 7 2 UPS99229982 1 19990624 A 5330 SKIN BOEING 727 72722C 138400F NM BS 687 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C, CORROSION (C53-113-01.01-01) ON SKIN BS 687 TO 694 LBL 25 JUST ABOVE STR 26 LT SIDE. AFTER REMOVAL O F CORROSION, FOUND THE SKIN TO GO BEYOND ALLOWABLE DAMAGE. REMOVED DAMAGED SECTION. FABRICATED REPAIR DOUBLER, ALODINE D, PRIMED AND INSTALLED REPAIR DOUBLER ALL DONE IAW SRM 51-10-6, 53-10-1, 51-10-2 AND 51-30-2, SRM 53-30-3. 2 L 7 3 4F A3WE 1999070200308 19990702 00308 NM 1999 7 2 UPS99229983 1 19990618 A 5320 651986219 CHORD BOEING 727 72722C 138400F NM BS 349 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON NOSE MID CHORD BS 349, LBL 15, WL 169. REMOVED CHORD, INSTALLED NEW CHORD. REPLACED WEB WITH FABRICATED WEB, WORK DONE IAW SRM 51-30-2, 53-10-2. 2 L 7 3 4F A3WE 1999070200309 19990702 00309 NM 1999 7 2 UPS99229984 1 19990619 A 5330 SKIN BOEING 727 72722C 138400F NM BS 243.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C, CRACK INDICATION NOTED AT BS 243.7 WL 229 AROUND FASTENER HEAD MARKED IN RED (RIGHT HAND SIDE. REMOV ED DAMAGE, FABRICATED DOUBLER AND INSTALLED WORK DONE IAW SRM 53-30-03, 51-30-02 AND MM 51-20-151. 2 L 7 3 4F A3WE 1999070200310 19990702 00310 NM 1999 7 2 UPS99229985 1 19990621 A 5330 SKIN BOEING 727 72722C 138400F NM BS 243.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C, CRACK INDICATED NOTED AROUND 2 FASTENER HEADS AT LT BS 243.7, WL 198.5 AND WL 200. AREAS MARKED IN R ED. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED WORK DONE IAW SRM 53-30-3, SRM 51-30-02 AND MM 51-20-151. 2 L 7 3 4F A3WE 1999070200311 19990702 00311 WP 1999 7 2 UPS99829973 1 19990627 A 3350 338001018 LIGHT DOUG DC8 DC871F 302199D WP PASSENGER DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERG EXIT LIGHT HAS ONE BULB INOP. REMOVED AND REPLACED ASSY PER DC8 MM 33-50-02P2 01, OPS CK GOOD. 2 L 7 4 4F RT 4A25 1999070200312 19990702 00312 WP 1999 7 2 UPS99829975 1 19990625 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP AIRSTART DOORWAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, PERMANENT REPAIR TO AIRSTART CUTOUT (D161352) INCIDENT NR R598473 DATE OF OCCURANCE 10/22/98 ORIGIN AL INCIDENT. AIRCART PULLED AWAY FROM AIRCRAFT WITH CART STILL CONNECTED. ACCOMPLISHED REPAIR IAW UPS EO DC8-5330-0793 AND UPS DC8 SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999070200313 19990702 00313 WP 1999 7 2 UPS99829976 1 19990607 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, CROSS SLIDE RAMP MOUNT ATTACH FIG CRACKED FS 340 ABOVE L 35L. FABRICATED AND INSTALLED REPAIR ANGL E IAW DC8-SRM 53-2-0 & 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200314 19990702 00314 WP 1999 7 2 UPS99829977 1 19990620 A 5540 WEB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, SUPPORT WEB BENEATH 2ND RUDDER DAMPENER CRACKED IN SEVERAL PLACES STA ZR155. REMOVED AND FABBED NE W 5656229-11 WEB IAW DAC DWG 5656229. REINSTALLED RIB, WEB AND SIDE SKIN IAW DC8 SRM 51-1-21 & 51-1-20D. REINSTALLED L /E SECTION IAW DC8 SRM 51-3-0. REINSTALLED RUDDER IAW DC8 MM 27- 21-01. 2 L 7 4 4F RT 4A25 1999070200315 19990702 00315 WP 1999 7 2 UPS99829978 1 19990618 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, STRINGER-51 NR 2 MAIN O/B AT WS 74.00 REAR SPAR HAS FWD FITTING CRACKED. REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999070200316 19990702 00316 WP 1999 7 2 UPS99829979 1 19990621 A 5540 WEB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, RUDDER STIFFENER INSIDE L/E AT STA ZR 110 IS CRACKED. FABRICATED AND INSTALLED NEW STIFFENER (WEB) IAW DAC DWG 5656229, DC 8 SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1999070200317 19990702 00317 EU 1999 7 2 QXEA9901372 1 19990623 A 3232 ACTUATOR FOKKER F28 F28MK4000 4990810 EU LT NLG DOOR BROKEN A QXEA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 09 488US 11240 BOI - AFTER GEAR RETRACTION HEARD AND FELT VIBRATION FROM NOSE GEAR AREA. RETURNED TO FIELD (BOI). MAINTENANCE INSPECT ED AND FOUND LEFT NOSE GEAR DOOR ACTUATOR ROD BROKEN. REMOVED DOOR AND ROD, PLACED ON CDL. AIRCRAFT REPOSITIONED TO PD X. MAINTENANCE INSTALLED NEW LEFT NOSE GEAR DOOR OPERATING ROD ASSEMBLY. ADJUSTED AND PERFORMED OPERATIONAL TEST, CHEC KS GOOD. 2 L 7 2 4F RT A20EU 1999070200318 19990702 00318 EU 1999 7 2 QXEA9901375 1 19990624 A 3350 A42052 SIGN FOKKER F28 F28MK4000 4990810 EU GALLEY FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 490US 11152 GEG-LIGHTS OUT IN EMERGENCY EXIT SIGN AT GALLEY. REMOVED AND REPLACED CABIN ENTRY EXIT SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999070200319 19990702 00319 EU 1999 7 2 QXEA9901376 1 19990624 A 3350 900542 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 492US 744 11159 GEG-EMERGENCY LIGHTS INOP AT ROWS 8A AND 9A. REPLACED BATTERY PACK SUPPLY LOCATED IN OVERHEAD BIN ROW 9A, OPERATIONAL C HECKS NORMAL. 2 L 7 2 4F RT A20EU 1999070200320 19990702 00320 NM 1999 7 2 99FDEA00241 1 19990625 A 2611 774001 SMOKE DETECTOR BOEING 727 727227 1384078 NM E & E COMPT INOPERATIVE A FDEA A F UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 SO 25 490FE 21493 NR 4 POS SMOKE DETECTOR LIGHT ILLUM WITH AN ASSOCIATED FIRE BELL. REMOVED AND REPLACED COCKPIT VOICE RECORDER FOR BENCH READ-OUT PER MM 23-70-012-4, OPS CK GOOD. REMOVED AND REPLACED NR 4 SMOKE DETECTOR PER MM 26-16-11. 2 L 7 3 4F A3WE 1999070200321 19990702 00321 NM 1999 7 2 99FDEA00242 1 19990625 A 7722 152BL801C INDICATOR BOEING 727 727233 138408A NM NR 2 EGT ERRATIC A FDEA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 25 222FE 20933 NR 2 ENGINE EGT GAUGE ERRATIC IN CRUISE, READ BETWEEN 350-100. SHUT DOWN NR 2 ENG. REMOVED AND REPLACED EGT IND PER MM 77-21-02, RAN UP ENGINE, FOUND OK. 2 L 7 3 4F RT A3WE 1999070200322 19990702 00322 NM 1999 7 2 99FDEA00243 1 19990625 A 5315 65208232 FLOORBEAM BOEING 727 7272S2F 1384O81 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 CORROSION (C53-111-01) UNDER NUTPLATE, LOWER SURFACE OF BS 1148 UPPER CHORD, RBL 57, WL 207.5. *S/D* REPAIRED FLOORBEA M IAW FEDEX EA 7-5310-46923. 2 L 7 3 4F A3WE 1999070200323 19990702 00323 NM 1999 7 2 99FDEA00244 1 19990625 A 5330 652368614 SKIN BOEING 727 7272S2F 1384O81 NM BS 1434 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 AFT FUSELAGE, UPPER RIGHT TORQUE BOX, DENT ON SKIN BS 1434, RBL 18, WL 210. *S/D* FAIRING REMOVED FOR ACCESS (5211R) D ENT IAW SRM 51-30-2. RECONTOUR TO FEDEX SRM 53-30-1, 51-40-1 NFEC SHOW NO CRACK, SUB FASTENER INSTALLED IAW FEDEX EA 7- 5410-46934. 2 L 7 3 4F A3WE 1999070200324 19990702 00324 NM 1999 7 2 99FDEA00245 1 19990625 A 5320 65184172 WEB BOEING 727 72725 1384006 NM BS 294-309 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 WHILE WORKING NR 0795 FOUND CORROSION NOSE WHEEL WELL HORIZONTAL WEB AND BONDED DOUBLERS AT BS 294 TO BS 309, RBL 13 TO LBL 13, WL 181. 2 L 7 3 4F A3WE 1999070200325 19990702 00325 WP 1999 7 2 ABXA9900544 1 19990629 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 973AX 47511 EMERGENCY LIGHTS BATTERY WOULD NOT HOLD CHARGE. REPLACED BATTERIES IAW DC9 MM 33-51-00. 2 L 7 2 4F A6WE 1999070200326 19990702 00326 WP 1999 7 2 ABXA9900545 1 19990625 A 5610 5613217508 WINDOW DOUG DOUG DC9 DC941 302207N WP RT COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 FIRST OFFICER'S CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED FIRST OFFICER'S WINDOW MECHANISM, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999070200327 19990702 00327 WP 1999 7 2 ABXA9900546 1 19990527 A 5720 5701110501N SKIN DOUG DOUG DC8 DC861 3021952 WP LT WING VANE DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 LEFT WING VANE, LOWER SURFACE WAS 90 PERCENT DELAMINATED. REPAIRED UNIT IAW DC8 SRM. 2 L 7 4 4F 4A25 1999070200328 19990702 00328 WP 1999 7 2 ABXA9900547 1 19990527 A 5720 5701446502 SKIN DOUG DOUG DC8 DC861 3021952 WP RT WING VANE DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 RIGHT WING VANE, LOWER LEADING EDGE SKIN WAS 20 PERCENT DELAMINATED. REPAIRED UNIT IAW DC8 SRM. 2 L 7 4 4F 4A25 1999070200329 19990702 00329 WP 1999 7 2 ABXA9900548 1 19990628 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND LONGERON 16 RIGHT CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1999070200330 19990702 00330 WP 1999 7 2 ABXA9900549 1 19990628 A 5313 59114279 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 980. REPAIRED LONGERON IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1999070200350 19990702 00350 SW 1999 7 2 99ZZZX2498 1 19990527 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYSTEM FAILED A ERAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 421EH 33067 APPROXIMATELY 15 MINUTES AFTER DEPARTURE, A SMELL OF BURNED WIRE FUMES WAS NOTICED IN THE AIRCRAFT. AIRCRAFT ROUTED TO INTERCOSTAL CITY. UPON LANDING, MECHANICS FROM LAKE CHARLES COMPLETED A TROUBLESHOOTING PROCEDURE. INVERTER WAS FOUND TO HAVE 2 BURNED DIODES. REMOVED AND REPLACED INVERTER WITH SERVICEABLE. MECHANICS INSPECTED ELECTRICAL SYSTEM AND NO DEFECTS NOTED. TEST RUN AND OPS CHECKED SYSTEM WITH NO DEFECTS NOTED. 1 G 7 2 4U H4SW 1999070200351 19990702 00351 1999 7 2 HALA9900127 4 19990528 A 3420 2588533901 AMPLIFIER DOUG DC9 DC951 3022051 WP NR 2 MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 601AP 13631 1020445 47658 FLT 564 - HNL - NR 2 COMPASS SYSTEM BECAME INOPERATIVE WITH GEAR RAISED. STARTED WORKING AGAIN WITH THE GEAR DOWN. REP LACED NR 2 INSTRUMENT AMPLIFIER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999070200352 19990702 00352 EU 1999 7 2 VTZA990117 1 19990525 A 2435 23095002 STARTER/GEN JETAIR JETSTM JETSTM4101 1500501 EU UNKNOWN A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 301UE 41012 FLT 7393 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LEFT GENERATOR FAILED. AIRCRAFT RETURNED TO GATE WITH NO FUR THER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT STARTER/GENERATOR, OPS CHECK OK. AIRCRAFT WAS RELEA SED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200353 19990702 00353 EU 1999 7 2 VTZA990116 1 19990524 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 324UE 41017 FLT 7225 - IAD-ORF - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED AND FOUND LOOSE CONNECTION. MAINTENANCE RESECURED CONNECTION. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200354 19990702 00354 1999 7 2 VTZA990115 3 19990524 A 6140 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 322UE 41058 IAD-ALB - FLT 7180 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT RED BETA WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BETA SWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200355 19990702 00355 EU 1999 7 2 VTZA990114 1 19990524 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU ROW 6 FAILED A VTZA A UNSCHED LANDING N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 313UE 41026 FLT 7590 - IAD-BTV - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO INTERIOR EMERGENCY EXIT LIGHT IN ROW 6 INOPERATIVE. A IRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RELAMPED LIGHT, OPS CHECK OK. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200356 19990702 00356 1999 7 2 VTZA990113 4 19990523 A 3417 7000700966 DADC JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 324UE 41017 FLT 7356 - IAD-JFK - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 2 DADC FAILED. AIRCRAFT RETURNED TO GATE WITH NO FUTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 2 DADC. OPS CHECK OK. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200357 19990702 00357 EU 1999 7 2 VTZA990112 1 19990522 A 3060 P110164160116 PROP HEAT JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 301UE 41012 FLT 7220 - IAD-HPN - DURING CLIM, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT PROP HEAT FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT PROPELLER, OPS CHECK OK. AIRCRA FT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200358 19990702 00358 EU 1999 7 2 VTZA990111 1 19990522 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 305UE 41019 DURING MAINTENANCE, FOUND LEFT AF TEMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND RELAMPED EMERGENCY LIGHT. OP S CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200359 19990702 00359 EU 1999 7 2 VTZA990110 1 19990521 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 302UE 41013 DURING MAINTENANCE, FOUND EMERGENCY LIGHT RIGHT REAR INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BULB, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200360 19990702 00360 EU 1999 7 2 VTZA990109 1 19990521 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 306UE 41020 FLT 7618 - IAD-RDU - DURING POST FLIGHT, CREW FOUND EMERGENCY LIGHTS NEAR REAR AILSE INOPERATIVE. AIRCRAFT STAYED AT GA TE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESEATED CONNECTOR ON EMERGENCY FLOOR LIGHT, OPS CHECK OK. AIRC RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200361 19990702 00361 EU 1999 7 2 VTZA990107 1 19990519 A 3350 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 313UE 41026 FLT 7159 - BOS-IAD - DURING PREFLIGHT, CREW FOUND FORWARD FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. AIRCRAFT STAYED A T GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET LOOSE CONNECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200362 19990702 00362 EU 1999 7 2 VTZA990106 1 19990517 A 3350 BULBS JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT DIRTY A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 321UE 41045 DURING MAINTENANCE, MECHANIC FOUND LEFT EXTERNAL FORWARD EMERGENCY LIGHT INOPERATIVE. AIRCRAFT SYATED AT GATE WITH NO F URTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED BOTH BULBS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200363 19990702 00363 EU 1999 7 2 VTZA990105 1 19990517 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT MISSING A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 307UE 41021 MAINTENANCE FOUND BULB MISSING FROM RIGHT MIDDLE CABIN EMERGENCY EXIT LIGHT. AIRCRAFT STAYED AT GATE WITH NO FURTHER PR OBLEMS. MAINTENANCE INSPECTED AND REPLACED BULB. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A41NM 1999070200364 19990702 00364 EU 1999 7 2 VTZA990104 1 19990514 A 3350 HOLDER JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 308UE 41023 DURING MAINTENANCE, FOUND EMERGENCY TRACK LIGHTING HOLDER LOOSE. AIRCRAFT STAYED AT THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESECURED HOLDER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A41NM 1999070200365 19990702 00365 EU 1999 7 2 VTZA990103 1 19990513 A 3060 950060 DE-ICE TIMER JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 323UE 41059 FLT 7371 - IAD-ILM - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT PROPELLER HEAT INOPERATIVE. AIRC RAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RIGHT PROP DE-ICE TIMER. OP S CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200366 19990702 00366 EU 1999 7 2 VTZA990032 1 19990415 A 3350 6134051 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU ROW 6, 7, 8 DISCHARGED A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 331UE 41099 DURING MAINTENANCE, THE FOLLOWING EMERGENCY LIGHTS WERE INOPERATIVE WHEN A/C WAS NOT POWERED, FLOOR (ROW 6, 7, 8) EXIT S IGN (6A) AND OVERHEAD (9A). TESTED OK WITH A/C POWERED. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200367 19990702 00367 EA 1999 7 2 VTZA990036 1 19990418 A 2910 NAS16128 O-RING CNDAIR CL600 CL6002B19 EA HYD ACCUMULATOR FAILED A VTZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 625BR 7214 FLT 7241 - CMH-IAD - DURING APPROACH, AIRCRAFT NR 3 HYDRAULIC SYSTEM QTY WENT TO ZERO. CREW UTILIZED ABNORMAL PROCEDURE AND LOWERED LANDING GEAR MANUALLY. MAINTENANCE REMOVED AND REPLACED INBOARD SIDE FITTING O-RING OF NR 3 HYDRAULIC SYST EM ACCUMULATOR, AND PERFORMED POST MAINTENANCE GEAR OPERATION NORMALLY AND MANUALLY. OPS CHECK AND LEAK CHECK OK. AIRC RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999070200368 19990702 00368 EU 1999 7 2 VTZA990035 1 19990417 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA O OTHER L NO TEST TX TAXI/GRND HDL 1 EA 27 308UE 41023 FLT 7331- IAD-CHO - DURING PREFLIGHT, FORWARD LEFT EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE RECONNEC TED LOOSE CONNECTOR IN EMERGENCY TRACK LIGHTING. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A41NM 1999070200369 19990702 00369 EU 1999 7 2 VTZA990034 1 19990416 A 3350 LIGHT BAG JETSTM JETSTM3201 1500217 EU COCKPIT INOPERATIVE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 472UE 823 IAD-LYH - FLT 7501 - DURING PREFLIGHT, OVERHEAD EMERGENCY LIGHT CLOSEST TO COCKPIT ON ROOF WAS INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999070200370 19990702 00370 EU 1999 7 2 VTZA99033 1 19990416 A 3320 BC10072001 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU ROW 10 BC FAILED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 320UE 41043 FLT 7349 - JFK-IAD - DURING CRUISE, DECLARED AN INFLGHT EMERGNECY AND MADE AN UNSCHEDULED LANDING DUE TO SMOKE FROM ROOF PANEL AT 10BC. MAINTENANCE INSPECTED AND FOUND WINDOW LIGHT SOCKET AT ROW 10 BC TO BE BURNED AT SOCKET END. BULB WAS REMOVED FROM SOCKET AT 10 BC AND 9 BC. MAINTENANCE CONTROL, OPENED A DEFERRED MAINTENANCE ITEM UTILIZING MEL 33-7. MAI NTENANCE CLOSED DMI NR 47973 O N4-19-99 BY REPLACING LIGHT FIXTURE. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200371 19990702 00371 EU 1999 7 2 VTZA990038 1 19990422 A 7712 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 474UE 849 ABE-IAD - FLT 7157 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT EGT FLUX. AIRCRAFT WAS FERRIED TO IAD. MAINTENANCE CLEANED ZONE 2 CANNON PLUG AND REPAIRED WIRING INSULATION TT2 SENDOR. OPS CHECK OK. AIRCRAFT WAS RE LEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999070200372 19990702 00372 EU 1999 7 2 VTZA990040 1 19990424 A 2761 TY176301D ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU LT SPOILER FAILED A VTZA O OTHER F FLT CONT AFFECTED LD LANDING 1 EA 27 318UE 41041 FLT 7370 - ILM-IAD - DURING LANDING, AIRCRAFT LEFT SPOILER CAP WAS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT S POILER ACTUATOR. OPS CHECK GOOD. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200373 19990702 00373 EU 1999 7 2 VTZA990075 1 19990512 A 3230 1862K RADIUS ROD BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 494UE 810 FLT 7416 - IAD-SCE - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT MAIN LANDING GEAR SLOW TO RETRACT. A IRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RADIUS ROD, OPS C HECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999070200374 19990702 00374 EU 1999 7 2 VTZA990074 1 19990510 A 7714 137912511 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 494UE 810 FLT 7207 - IAD-PHF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE RPM INDICATION FAILED. AIRC RAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TACH GENERATOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVIE. (M) 2 L 7 2 4T RT A56EU 1999070200375 19990702 00375 1999 7 2 VTZA990073 3 19990509 A 6112 660716235 BOOT BAG JETSTM JETSTM3201 1500217 EU RT PROP MISSING A VTZA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 27 478UE 892 FLT 7558 - CRW-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE VIBRATION. AIRCRAFT DIVERT ED TO LOUISBURG. AIRCRAFT WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND RIGHT PROP DE-ICE MAT MISSING. MAINTENANCE REPLACED PROP DE-ICE BOOT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999070200376 19990702 00376 EU 1999 7 2 VTZA990072 1 19990509 A 3350 6047051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU RT EMER EXIT FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 305UE 41019 MAINTENANCE FOUND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE AND CABIN EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1, 2 AND NR 3 POWER SUPPLIES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200377 19990702 00377 EU 1999 7 2 VTZA990070 1 19990507 A 2612 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 320UE 41043 IAD-BUF - FLT 7302 - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO BAGGAGE SMOKE WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SMOKE DETECTOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4T RT A41NM 1999070200378 19990702 00378 EU 1999 7 2 VTZA990069 1 19990507 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 313UE 41026 FLT 7348 - IAD-JFK - DURING PREFLIGHT INSPECTION, THE MIDDLE SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATI VE. MAINTENANCE REPAIRED PATH LIGHTING, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200379 19990702 00379 EU 1999 7 2 VTZA990068 1 19990505 A 3350 BULB BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 474UE 849 DURING PREFLIGHT, CREW FOUND OVERHEAD EMERGENCY CABIN LIGHT INOPERATIVE. AIRCRAFT STAYED AT GATE WITH NO FURTHER PROBLE MS. MAINTENANCE INSPECTED AND RELAMPED EMERGENCY LIGHT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A56EU 1999070200380 19990702 00380 EU 1999 7 2 VTZA990067 1 19990505 A 3350 04133012 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 308UE 41023 FLT 7547 - EWR-IAD - DURING TAXI, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS EMERGENCY LIGHTIN STRIP LOOSE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SECURED EMERGENCY LIGHTING STRIP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070200381 19990702 00381 NM 1999 7 2 99ZZZM370 1 19990423 A 2133 56697 OUTFLOW VALVE BOEING 737 737247 138448D NM E/E BAY WORN A E9WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 309VA 19614 ON TAKEOFF AND CLIMB, AIRCRAFT WOULD NOT PRESSURIZE WITH RT PACK ONLY OPERATING. PILOT INFORMED MAINTENANCE OF PROBLEM AND WAS INSTRUCTED TO RETURN TO STATION. LEFT PACK NOT OPERATING DUE TO PRIOR MEL CONDITION. TROUBLESHOOT TO FORWARD O UTFLOW VAVLE WAS WORKING IMPROPERLY. REMOVED AND REPLACED AUTOMATIC FLOW CONTROL VALVE, P/N 5669-7, S/N OFF 1047, S/N O N 3876 IAW MM 21-58-31, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999070200382 19990702 00382 NM 1999 7 2 USAASB99076 1 19990320 A 2910 BACH8A08NN0164 HOSE BOEING 737 737201 1384454 NM 'A' HYD SYSTEM RUPTURED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 226US 21815 CLT - FLT 462 - ON CLIMB-OUT OF JAX, F/O NOTICED NR 2 ENG HYD PUMP LOW PRESSURE LIGHT ILLUMINATED. ACCOMP QUICK REF HAN DBOOK PROCEDURES. APPROX 1 MIN LATE, THE NR 1 ENG LOW PRESSURE LIGHT CAME ON AND SYSTEM HYD PRESSURE WENT TO 0. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A RUPTURED 'A' SYSTEM HYDRAULIC PRESSURE HOSE I N THE RIGHT MAIN LANDING GEAR WHEELWELL. REPLACED HOSE AND INSPECTED AND REPLACED PRESSURE, RETURN AND CASE DRAIN FILTE RS. REPLACED NR 1 AND NR 2 ENGINE HYDRAULIC PUMPS. SERVICED HYDRAULIC RESERVOIR AND PRESSURIZED 'A' AND 'B' HYDRAULIC SYSTEMS. NO LEAKS NOTED. WASHSED WHEELWELLS. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1999070200383 19990702 00383 NM 1999 7 2 USAASB99068 1 19990311 A 3244 6558256275 TIRE BOEING 737 737201 1384454 NM RT MLG FAILED A USAA O OTHER O OTHER TO TAKEOFF 1 EA 19 223US 12786 21665 CLT - FLT 1657 - SHORTLY AFTER T/O FROM EWR, CAPT REPORTED VIBRATION AFTER T/O AND SUSPECTED A BLOWN TIRE. TOWER IN CLT WAS ADVISED AND CRASH TRUCKS SETUP FOR INBOUND FLT. CAPT DECLARED AN EMERGENCY LANDING. FLT LANDED SAFELY AT CLT, BUT SHEARED OFF THE REST OF THE NR 3 RIGHT MAIN LANDING GEAR TIRE. FLT LOST HYDRAULICS AND HAD TO BE TOWED TO THE GATE. M X REMOVED AND REPLACED THE BLOWN NR 3 MAIN LANDING GEAR TIRE AND WHEEL ASSEMBLY. ALSO, REPLACED THE NR 4 MLG TIRE AND W HEEL ASSY. REMOVED AND REPLACED BENT RIGHT MLG UPPER DOWNLOCK STRUT ASSY AND LOWER DOWNLOCK LINK ASSY PER MM 32-11-131. STRAIGHTENED AND ADJUSTED BENT TARGET FOR RIGHT MLG DOWNLOCK SENSOR. REPAIRED HYDRAULIC SYSTEM AND ANTI-SKID TRANSDUC 2 L 7 2 4F A16WE 1999070200384 19990702 00384 NM 1999 7 2 USAASB99052 1 19990223 A 2720 PCU BOEING 737 7372B7 1384560 NM RUDDER MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 282AU 23115 BWI - FLT 2710 - EN ROUTE FROM MCO-BDL, AT FL330 AND .74 MACH, FLIGHT WAS APPROACH SBY ON 'A' AUTOPILOT WHEN THE A/C STA RTED PITCHING UP AND ROLLING TO RIGHT 80 DEGRES. CAPT USED FULL POWER AND FULL AILERON TO GET THE AIRCRAFT LEVEL. CAPT STATED THAT WHEN HE TURNED OFF THE 'B' HYD PUMP, THE AIRCRAFT SNAPPED BACK TO NORMAL. CAPTAIN DECLARED AN EMERGENCY AN D THE FLIGHT DIVERTED TO BWI. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT FIND ANY FAULT WITH THE AI RCRAFT. REMOVED AND REPLACED AS PRECAUTIONARY THE RUDDER PCU, STANDBY RUDDER PCU, STANDBY HYD PUMP, YAW DAMP COUPLER, N R 6 AND NR 7 FLIGHT SPOILER ACTUATORS ALL HYDRAULIC FILTERS AND ACCOMPLISHED RIGGING. ALL OPERATIONAL CHECKS, LEAKS CHE 2 L 7 2 4F A16WE 1999070200385 19990702 00385 1999 7 2 AALA990495 4 19990409 A 2397 WIRE BOEING 767 767323 1385205 NM ROW 2-3 SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 372AA 25199 ORD - FLT 955 - SEAT 2 A WIRING HARNESS AT FLOOR PANEL SHORTED OUT CAUSING A FLASHING ARC AS HIGH AS THE WINDOW. BOTH S EATS AT 2 A/B AND 3 A/B HAVE LOST ALL AUDIO VISUAL AND SEAT CONTROLS. AT TIME OF SHORTING, SMOKE WAS SMELLED IN FIRST C LASS. INSPECTED AND FOUND SEVERAL WIRES SHORTED TO GROUND ADJACENT TO 3A FOOT REST AT FLOOR/SIDEWALL WIRE RUN. INSTALL ED GROMMET AND REPAIRED POWER FOOT REST WIRING TO SEATS 2 A/B, 3 A/B, 4 A/B. ALL SEAT CONTROLS OPS CHECK NORMAL. AIRCR AFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 1999070200386 19990702 00386 EU 1999 7 2 FJT99059441 1 19990510 A 2910 1379305A155 HOSE BAG JETSTM JETSTM3201 1500217 EU RT MLG RUPTURED A FJTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 03 944AE 12127 200 944 ALT - FLT 1647 - LOST HYDRAULIC PRESSURE ON FINAL APPROACH TO ALT FROM CAE. AN EMERGENCY MANUAL GEAR AND FLAP EXTENSION WAS PERFORMED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. REPLACED BOTH ENGINE DRIVEN HYDRAULIC PUMPS AS A PR ECAUTIONARY MEASURE. REPLACED THE RUPTURED STEEL FLEX LINE TO THE RT MLG RADIUS ROD. THE HYDRAULIC SYSTEM WAS SERVICED AND BLED. THE ARICRAFT RETURNED TO SERVICE. THE FAILED HYDRAULIC LINE SHOWED NO EVIDENCE OF CHAFING. THE RUPTURE OCC URRED WHERE THE STEEL BRAIDED LINE WAS SWAGED TO THE END FITTING. IT APPEARS NORMAL EXTENSION AND RETRACTION ACTION OF THE RADIUS ROD WAS A CONTRIBUTING FACTOR. PART TC: 16,556. (X) 2 L 7 2 4T RT A56EU 1999070200387 19990702 00387 EU 1999 7 2 VTZA990086 1 19990519 A 3350 BAG JETSTM JETSTM3201 1500217 EU UNKNOWN A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 495UE 818 FLT 7233 - IAD-ORF - DURING PREFLIGHT, CREW FOUND EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT STAYED AT THE GATE WITH NO FUR THER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EMERGENCY POWER UNIT SUPPLY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999070200388 19990702 00388 EU 1999 7 2 VTZA990087 1 19990519 A 7712 201042 FILTER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 486UE 905 FLT 7234 - ORF-IAD - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TTL INOPERATIVE. AIRCRAFT RETURNEE TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 45564 MEL 76-2. MAINTENANCE CLOSED DMI 455 64 ON 5-20-99 BY CLEARING TTL FILTER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999070200389 19990702 00389 EA 1999 7 2 VTZA990088 1 19990519 A 2612 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT FALSE WARNING A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 622BR 7187 FLT 7822 - SGF-ORD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CARGO SMOKE WARNING LIGHT ILLUMINATED. C REW BLEW FIRE EXTINGUISHERS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FERRIED AIR CRAFT TO IAD AND REMOVED AND REPLACED SMOKE DETECTOR AND FIRE EXTINGUISHERS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999070200390 19990702 00390 EU 1999 7 2 SIMA990791 1 19990320 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU WING ROOT FAILED A SIMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 391AE 951211 340B391 SJT - FLT 3588 - DURING APPROACH, CREW NOTICED A BURNING SMELL THROUGHOUT THE AIRCRAFT. SHUT DOWN THE RIGHT BLEED AND T HE SMELL WENT AWAY. MAINTENANCE INSPECTED BLEED SYSTEM, THE REST OF THE AIRCRAFT, AND PERFORMED ENGINE RUNS, BUT COULD NOT DUPLICATE THE SMELL. OPENED MEL AGAINST THE RIGHT ACM AND SUBSEQUENTLY. REMOVED AND REPLACED THE ACM, CLEARED THE MEL, AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999070200391 19990702 00391 WP 1999 7 2 USAA990492 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 718 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND TWO .5 INCH CRACKS AT LONGERON ATTACH POINTS, STATION 718 LONGERON 6 LT. SPLICED IN NEW S ECTION OF LONGERON PER SRM 53-02, FIG 18 SHEET 1. (M) 2 L 7 2 4F A6WE 1999070200392 19990702 00392 WP 1999 7 2 USAA990493 1 19990604 A 5311 99122439 FRAME DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND .75 INCH LONG CRACK IN FRAME BETWEEN LONGERON 15 LT AND 16 LT AT STATION 965. DEFECTIVE P ART REPLACED WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F A6WE 1999070200393 19990702 00393 WP 1999 7 2 USAA990495 1 19990604 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND TWO CRACKS 1 INCH LONG ON FRAME AT SKIN CLIP STATION 945, LONGERON 14R TO 16R. MANUFACTUR ED NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 6. (M) 2 L 7 2 4F A6WE 1999070200394 19990702 00394 WP 1999 7 2 USAA990496 1 19990604 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK AT WEB AT STATION 965 BULKHEAD LOWER INBOARD CORNER. INSTALLED DOUBLER REPAI R PER SRM 53-03 FIG 21. (M) 2 L 7 2 4F A6WE 1999070200395 19990702 00395 WP 1999 7 2 USAA990497 1 19990604 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 5 INCH BY 2 INCH CORROSION AT FRAME WEB AT STATION 996 FLOORBEAM WHERE IT ATTACHED TO RIGH T BELL FRAME. CORROSION LEVEL 1, CORROSION TASK NR C-57-533000. INSTALLED WEB AND FITTING AND DOUBLER PER EA 52122 AND SRM 53-05 FIG 72. (M) 2 L 7 2 4F A6WE 1999070200396 19990702 00396 WP 1999 7 2 USAA990498 1 19990604 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 963 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT STATION 963 LONGERON 16R. INSTALLED DOUBLER REPAIR PER S RM 53-04 FIG 31 AND EA 52111. (M) 2 L 7 2 4F A6WE 1999070200397 19990702 00397 WP 1999 7 2 USAA990499 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 965, LONGERON 17 UPPER AND LOWER LEGS. INSTALLED SPLI CE REPAIR PER SRM 53-04 FIG 18. (M) 2 L 7 2 4F A6WE 1999070200398 19990702 00398 WP 1999 7 2 USAA990500 1 19990604 A 5320 RADIAL DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT NR 2 RADIAL, APBH RIGHT SIDE, OUTBOARD END. COMPLETED CLIP REPAIR PER TY PICAL REPAIR 53-10-22. (M) 2 L 7 2 4F A6WE 1999070200399 19990702 00399 WP 1999 7 2 USAA990501 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 1046 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK AT LONGERON 9R CANTED STATION 1046. SPLICED IN LONGERON PER SRM 53-02 FIG 18 . (M) 2 L 7 2 4F A6WE 1999070200400 19990702 00400 WP 1999 7 2 USAA990502 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 980 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 980, LONGERON 17L. SPLICED IN LONGERON PER SRM 53-02. (M) 2 L 7 2 4F A6WE 1999070200401 19990702 00401 WP 1999 7 2 USAA990503 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 965 AT LONGERON 17L. SPLICED IN LONGERON PER SRM 53-2 2. (M) 2 L 7 2 4F A6WE 1999070200402 19990702 00402 WP 1999 7 2 USAA990504 1 19990604 A 5320 CLIP DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND TWO CRACKS APPROX 2 INCHES LONG ON SKIN FORMER CLIP AT STATION 965 RT, BETWEEN LONGERON 14 R AND 16R. INSTALLED DOUBLER PER SRM 53-02 FIG 6 AND EA NR 52111. (M) 2 L 7 2 4F A6WE 1999070200403 19990702 00403 WP 1999 7 2 USAA990505 1 19990604 A 5320 CLIP DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND CRACKED ATTACH CLIP 1 INCH LONG AT STATION 965 LONGERON 17 LEFT. FABRICATED NEW CLIP. (M ) 2 L 7 2 4F A6WE 1999070200404 19990702 00404 NM 1999 7 2 USAASB99135 1 19990603 A 3350 LIGHT BOEING 737 7373B7 1384580 NM ROW 17-21 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 510AU 23385 PHL - PILOT REPORTED THAT THE LOW LEVEL EMERGENCY LIGHTS IN THE AFT SECTION OF THE CABIN, AT ROWS 17-21 ABC, ARE INOPERA TIVE. MAINTENANCE FOUND THE SEAT ASSEMBLY AT ROW 17 ABC SHORTING OUT THE LOW LEVEL EMERGENCY LIGHTS. REPAIRED BROKEN W IRES AND REPLACED THE FORWARD BATTERY CHARGER ASSEMBLY (P/N 2012-1). OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999070200405 19990702 00405 NM 1999 7 2 USAASB99136 1 19990604 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 25021 PHL - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTS AT THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999070200406 19990702 00406 NM 1999 7 2 99ZZZM371 1 19990604 A 3350 20121 BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 782AU 25021 PHL - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTS AT THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999070200407 19990702 00407 NM 1999 7 2 USAA069909 1 19990306 A 5320 WEB BOEING 727 727254 138408L NM NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913TS 20250 NOSE WHEEL WELL PRESSURE WEB CRACKED ONE INCH ABOVE RIGHT AFT ACCESS PANEL. INSTALLED REPAIR AT NOSE WHEEL WELL PRESSUR E WEB, ABOVE RIGHT AFT ACCESS PANEL. MATERIAL USED, 2024-T3, .050 INCH, 11 INCH BY 8 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0145. (M) 2 L 7 3 4F A3WE 1999070200408 19990702 00408 NM 1999 7 2 USAA069908 1 19990306 A 5320 STRAP BOEING 727 727254 138408L NM BS 930 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913TS 20250 CRACKS ON CIRCUMFERENTIAL SPLICE STRAP BS 930, STRINGER 14R. INSTALLED FUSELAGE FRAME REPAIR AT BS 930, STRINGER 14R. M ATERIAL USED, 7075-T6, .125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0162. (M) 2 L 7 3 4F A3WE 1999070200409 19990702 00409 NM 1999 7 2 USAA069907 1 19990306 A 5311 CIRCUMFERENTIAL BOEING 727 727254 138408L NM BS 930 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913TS 20250 CRACK ON CIRCUMFERENTIAL AT BS 930 STRINGER 13L. INSTALLED FUSELAGE FRAME REPAIR AT BS 930 BETWEEN STRINGER 11 AND STRI NGER 12, AND BETWEEN STRINGER 13 AND STRINGER 14 LEFT. MATERIAL USED, 7075-T6, .125 INCH, 14.5 INCH BY 1.25 INCH. REPA IR INSTALLED IAW SB 727-52-0162. (M) 2 L 7 3 4F A3WE 1999070200410 19990702 00410 NM 1999 7 2 USAA069906 1 19990306 A 5330 SKIN BOEING 727 727254 138408L NM BS 720 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913TS 20250 EXTERIOR SKIN HAS POPPED RIVET HEAD (MISSING) STATION 720D AT STRINGER 28L. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR AT BSB 720D, STRINGER 28L. MATERIAL USED 7075-T6, .125 INCH, 17 INCH BY 13.5 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FI G 1. (M) 2 L 7 3 4F A3WE 1999070200411 19990702 00411 NM 1999 7 2 USAA069905 1 19990306 A 5330 SKIN BOEING 727 727254 138408L NM BS 351 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913TS 20250 EVIDENCE OF CORROSION AT BS 351 STRINGER 26R EXTERIOR. INSTALLED FUSEALGE EXTERIOR SKIN REPAIR AT BS 351, STRINGER 26R. MATERIAL USED, 2024-T3, .063 INCH , 19 INCH BY 11 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999070200412 19990702 00412 NM 1999 7 2 USAASB99121 1 19990506 A 2751 2061141 INDICATOR BOEING 737 7373B7 1384580 NM TE FLAPS FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 515AU 33748 23701 LGA - FLT 420, ON APPROACH, TRAILING EDGE FLAPS WOULD NOT EXTEND MORE THAN FLAPS 10. ACCOMPLISHED GO AROUND AND FLAPS E XTENDED TO FLAPS 15 WITH FLAP HANDLE AT 15. FLAPS RETRACTED NORMALLY. DURING SECOND APPROACH, FLAPS EXTENDED NORMALLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FLAP ASYMMETRY LIGHT ON. REMOVED AND REPLACED FLAP POS ITION INDICATOR. OPERATIONAL CHECK NORMAL. FLAP ASYMMETRY TESTS NORMAL. (M) 2 L 7 2 4F RT A16WE 1999070200413 19990702 00413 EU 1999 7 2 SIMA991551 1 19990604 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 340B218 ABI - DURING MBV INSPECTION, FOUND PUNCTURE OF THE INNER PANEL OF THE MAIN CABIN DOOR CLEANED AREA. REMOVED TOPCOAT PAI NT FOR THE PLANNED 1.5 INCH EXTENT OF THE CUTOUT. CUTOUT DAMAGED SKIN AND PERFORMED AN EDDY CURRENT AND BOND TEST OF TH E SURROUNDING AREA. FABRICATED A FILLER PLATE AND DOUBLER .020 THICK. TREATED ALL EXPOSED METAL EDGES OF THE CUTOUT, F ILLER AND DOUBLER PLATE WITH ALODINE. FILLED THE HONEYCOMB CORE WITH EPOXY FILLER LY/HY 5052 AND INSTALLED THE FILLER P LATE. BONDED THE DOUBLER PLATE TO THE SKIN WITH ADHESIVE EA 9330 AND APPLIED A DISTRIBUTED PRESSURE ON THE DOUBLER PLAT E DURING CURING. EDGE SEALED DOUBLER AND APPLIED SURFACE TOPCOAT TO THE REPAIR AREA. REPAIR WAS DONE BY AVCOM TECHNOLO 2 L 7 2 4T RT A52EU 1999070200414 19990702 00414 SO 1999 7 2 SIMA991542 1 19990503 A 3350 3025101 LIGHT EMB 145 EMB145LR SO EMERGENCY EXIT FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 617AE 145093 ORD - FLT 4112 - LEFT AND RIGHT OVERWING EMERGENCY EXITS SIGNS FAIL TO ILLUMINATE. REMOVED AND REPLACED BOTH EMERGENCY EXIT SIGN LIGHT ASSEMBLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999070200415 19990702 00415 EU 1999 7 2 RAIA990529 1 19990522 A 3250 860122 VALVE BAG JETSTM JETSTM3201 1500217 EU NLG STEERING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 341TE 950 FLT 7093 - SPI NOSE WHEEL STEERING STUCK TO RIGHT AND WILL NOT COME BACK. MAINTENANCE REPLACED STEERING SELECTOR VALVE. (M) 2 L 7 2 4T RT A56EU 1999070200416 19990702 00416 EU 1999 7 2 RAIA990530 1 19990516 A 3610 S3611012900000 DUCT AEROSP ATR72 ATR72202 8680940 EU LEFT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7170 - STL - LEFT BLEED LEAK LIGHT ILLUMINATED. MAINTENANCE REPLACED DUCT ASSY FOR LEFT O-TEMP SWITCH. (M) 2 H 7 2 4T RT A53EU 1999070200417 19990702 00417 EU 1999 7 2 RAIA990531 1 19990514 A 5210 1379230C405 HANDLE BAG JETSTM JETSTM3201 1500217 EU PAX DOOR WORN A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 424AM 865 FLT 7439 - CMI - PAX DOOR CAP LIGHT ILLUMINATED. MAINTENANCE REPLACED MOUNT BOLT FOR PAX DOOR HANDLE. (M) 2 L 7 2 4T RT A56EU 1999070200418 19990702 00418 NE 1999 7 2 RAIA990538 2 19990526 A 7530 ASNA213820 GASKET AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 421TE 102 120530 FLT 7404 - STL - RIGHT ENGINE ITT ERRATIC. MAINTENANCE REPLACED HP BLEED GASKET ON RIGHT ENGINE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999070200419 19990702 00419 NE 1999 7 2 RAIA990537 2 19990526 A 7270 S0003007620000 DUCT AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE LEFT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 421TE 102 120651 FLT 7404 - STL - LEFT ENGINE ITT ERRATIC. MAINTENANCE REPLACED H/P PORT DUCT ASSEMBLY ON LEFT ENGINE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999070200420 19990702 00420 EU 1999 7 2 RAIA990536 1 19990527 A 3260 DHE1148 SWITCH AEROSP ATR72 ATR72202 8680940 EU LT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 721TE 217 FLT 7417 - STL - LENDING GEAR WILL NOT RETRACT. MAINTENANCE REPLACED NR 2 WEIGHT ON WHEEL SWITCH ON LEFT GEAR. (M) 2 H 7 2 4T RT A53EU 1999070200421 19990702 00421 EU 1999 7 2 RAIA990535 1 19990521 A 7711 8972605 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 430AM 880 FLT 7058 - STL - LEFT ENGINE EGT SPIKED. MAINTENANCE REPLCED TRANSDUCER FOR LEFT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999070200422 19990702 00422 SO 1999 7 2 RAIA990534 1 19990526 A 2424 51545001B GCU EMB 145 EMB145 SO NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 803HK 145077 FLT 5776 - ORD - WHT NR 1 ENGINE AND APU RUNNING, TRIED TO START NR 2 ENGINE AND HAD A MULTIPLE FAILURE OF MOST ELECTRIC ITEMS. MAINTENANCE REPLACED NR 1 GEN CONTROL UNIT. (M) 2 L 7 2 4F RT T00011AT 1999070200423 19990702 00423 EU 1999 7 2 RAIA990533 1 19990526 A 2150 6411344 SWITCH AEROSP ATR72 ATR72202 8680940 EU LT PACK FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7166 - STL - LEFT PACK FAULT. MAINTENANCE REPLACED LEFT PACK OVERHEAT SWITCH. (M) 2 H 7 2 4T RT A53EU 1999070200424 19990702 00424 EU 1999 7 2 RAIA990532 1 19990526 A 3320 3717 BALLAST AEROSP ATR72 ATR72202 8680940 EU ROW 5A FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7166 - STL - SMOKE IN COCKPIT. MAINTENANCE REPLACED BALLAST FOR OVERHEAD LIGHT AT SEAT 5A. (M) 2 H 7 2 4T RT A53EU 1999070200425 19990702 00425 WP 1999 7 2 RAIA990542 2 19990531 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 860AE 12084 860 66195R FLT 4730 - FAT - LEFT ENGINE TORQUE DROPPED TO 80 PERCENT. MAINTENANCE REPLACED NR 1 ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999070200426 19990702 00426 1999 7 2 RAIA990541 4 19990531 A 6122 89741018 GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT PROP FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 436AM 891 FLT 7466 - STL - RIGHT ENGINE RPM DROPPED TO 97 PERCENT. MAINTENANCE REPLACED PROP GOVERNOR ON RIGHT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999070200427 19990702 00427 EU 1999 7 2 RAIA990540 1 19990530 A 2120 AIR DIST BAG JETSTM JETSTM3201 1500217 EU COCKPIT ODOR A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 422AM 856 FLT 7290 - STL - ELECTRICAL ODOR COMING FROM COCKPIT. MAINTENANCE PERFORMED GROUND RUN OF ENGINES, COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 2 4T RT A56EU 1999070200428 19990702 00428 NE 1999 7 2 RAIA990539 2 19990528 A 7510 30708215 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 41086 FLT 7742 - DCA - RIGHT PROP ENGINE ANTI-ICE LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT ENGINE ANTI-ICE PRESSURE SWIT CH. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999070200429 19990702 00429 NM 1999 7 2 EISA99084 1 19990406 A 3350 1000679 LIGHT GRIMES BOEING 727 727231 1384079 NM PAX DOOR LOOSE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 12305 19562 EMERGENCY EXIT LIGHT FALLS OFF FORWARD ENTRY DOOR AND WILL NOT STAY ATTACHED. ALSO, LIGHT IS DISCHARGED. REMOVED AND R EPLACED FORWARD ENTRY EXIT LIGHT. SECURITY AND OPS CHECK GOOD PE RMM 33-50-0. (M) 2 L 7 3 4F A3WE 1999070200430 19990702 00430 NM 1999 7 2 EISA99110 1 19990517 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 620-720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION OF SEAT TRACK AT FS 620 TO 720 LBL 24. REMOVED DAMAG E TRACK SECTION FROM FS 620 TO 720 AND REPLACED WITH NEW SECTION PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200431 19990702 00431 NM 1999 7 2 EISA99111 1 19990517 A 5522 SKIN BOEING 727 727223 1384074 NM LT ELEVATOR CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF C-CHECK WORKCARD, FOUND CORROSION ON LOWER SKIN OF LEFT ELEVATOR, 42 INCH FROM OUTBOARD END. R EMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER PER SRM 55-20-3. (M) 2 L 7 3 4F A3WE 1999070200432 19990702 00432 NM 1999 7 2 EISA99112 1 19990517 A 5522 SKIN BOEING 727 727223 1384074 NM LT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN LOWER SKIN ON LEFT ELEVATOR. STOP DRILLED CRACK, FABR ICATED AND INSTALLED DOUBLER PER SRM 55-20-3. (M) 2 L 7 3 4F A3WE 1999070200433 19990702 00433 NM 1999 7 2 EISA99113 1 19990517 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 620 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 1 SEAT TRACK AT FS 620. REMOVED SECTION TO TRA CK FROM FS 620 TO 66O AND REPLACED WITH NEW SECTION OF TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200434 19990702 00434 NM 1999 7 2 EISA99115 1 19990517 A 5230 65571463 FRAME BOEING 727 727223 1384074 NM CARGO DOOR DEFORMED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FORWARD LOWER CORNER OF FORWARD CARGO DOOR, GOUGED AND DEFORMED AT FS 620. REMOVED DAMAGED CORNER, POSITION DRILLED NEW PART AND INSTALLED PER SRM 51-10-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999070200435 19990702 00435 NM 1999 7 2 EISA99116 1 19990517 A 5312 BULKHEAD BEAM BOEING 727 727223 1384074 NM BS 1183 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN SUPPORT BEAM ON REAR BULKHEAD AT FS 1183 RBL 27, WL 26 2. REMOVED DAMAGED AREA PER SRM 51-40-4. FABRICATED AND INSTALLED FILLERS AND DOUBLERS PER SRM 51-40-4, FIG 1. (M) 2 L 7 3 4F A3WE 1999070200436 19990702 00436 NM 1999 7 2 EISA99117 1 19990517 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1050 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND STRINGER 27L CRACKED AT FS 1050. REMOVED DAMAGED AREA, FABRICA TED AND INSTALLED REPAIR PER SRM 51-40-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999070200437 19990702 00437 NM 1999 7 2 EISA99118 1 19990517 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FUSELAGE FRAME CRACKED AT FS 1166 LEFT AT WL 232.5. REMOVED DA MAGED AREA, FABRICATED REPAIR PER SRM 51-40-4 AND INSTALLED PER 51-40-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999070200438 19990702 00438 NM 1999 7 2 EISA99119 1 19990517 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 520 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SHEAR TIE BROKEN AT FS 520 19R. REMOVED BROKEN SHEAR TIE, FABR ICATED NEW PART PER SAMPLE AND INSTALLED PER SRM 51-30-2 AND 51-10-1. (M) 2 L 7 3 4F A3WE 1999070200439 19990702 00439 NM 1999 7 2 EISA99092 1 19990408 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 870-950 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHEC WORK-CARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT RIGHT OUTBOARD TACK FROM F S 870 TO FS 950. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200440 19990702 00440 NM 1999 7 2 EISA99091 1 19990408 A 5753 SKIN BOEING 727 727264 138408M NM TE MID FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF BN58 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND LEFT WING INBOARD MIDFLAP DELAMINATED BETWEEN WBL NR 124-203, 2 03-240 AND BETWEEN 70-124. REPAIRED BY OUTSIDE VENDOR. (M) 2 L 7 3 4F A3WE 1999070200441 19990702 00441 NM 1999 7 2 EISA99090 1 19990408 A 5532 SKIN BOEING 727 727264 138408M NM VERT STAB CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND VERTICAL STABILIZER SKIN CRACKED ON LEFT SIDE JUST BELOW SLIDI NG SEAL TRACK. STOP DRILLED CRACK PER SRM 55-30-3. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 55-30-3. (M) 2 L 7 3 4F A3WE 1999070200442 19990702 00442 NM 1999 7 2 EISA99088 1 19990408 A 5543 65727501 SKIN BOEING 727 727264 138408M NM RUDDER TAB DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND UPPER RUDDER TRIM TAB T/E DELAMINATED ON UPPER EDGE. REPAIR PE RFORMED BY OUTSIDE VENDOR. REPAIRED ON AIRCRAFT. (M) 2 L 7 3 4F A3WE 1999070200443 19990702 00443 NM 1999 7 2 EISA99087 1 19990408 A 5522 65727849 SKIN BOEING 727 727264 138408M NM LT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN LEFT ELEVATOR LOWER SKIN AT OUTBOARD END OF TRIM TAB. REPAIR PER FORMED BY OUTSIDE VENDOR. REMOVAL, INSTALLATION WEIGHT AND BALANCE ON NORDAM CARD NR 0083. (M) 2 L 7 3 4F A3WE 1999070200444 19990702 00444 NM 1999 7 2 EISA99086 1 19990408 A 5522 65727849 SKIN BOEING 727 727264 138408M NM LT ELEVATOR DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND LEFT ELEVATORY T/E DELAMINATED. REPAIR PER FORMED BY OUTSIDE V ENDOR. WEIGHT AND BALANCE PERFORMED IAW SRM 51-180-7. (M) 2 L 7 3 4F A3WE 1999070200445 19990702 00445 NM 1999 7 2 EISA99100 1 19990408 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 480-690 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT LEFT 2ND INBOARD TRACK FRO M FS 480 - FS 690. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200446 19990702 00446 NM 1999 7 2 EISA99099 1 19990408 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 480-690 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT RIGHT 2ND INBOARD TRACK FR OM FS 480 TO FS 690. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200447 19990702 00447 NM 1999 7 2 EISA99098 1 19990408 A 5347 BAC1520492 SEAT TRACK BOEING 727 727264 138408M NM BS 690-740 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT RIGHT 2ND INBOARD TRACK FR OM FS 690 FS 740. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200448 19990702 00448 NM 1999 7 2 EISA99095 1 19990408 A 5347 BAC1520429 SEAT TRACK BOEING 727 727264 138408M NM BS 760-848 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT RIGHT 2ND INBOARD TRACK FR OM FS 760- TO FS 848. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200449 19990702 00449 NM 1999 7 2 EISA99083 1 19990408 A 5522 65727841 SKIN BOEING 727 727264 138408M NM LT ELEVATOR DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 79 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LEFT ELEVATOR EDGE DELAMINATED AND HAS SEVERAL DENTS. REPAIRE D IAW BOEING SRM 55-20-3, 51-40-2 AND 51-40-6 WO NR E-1421. (M) 2 L 7 3 4F A3WE 1999070200450 19990702 00450 NM 1999 7 2 EISA99094 1 19990408 A 5347 BAC1520429 SEAT TRACK BOEING 727 727264 138408M NM BS 760-848 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT LEFT OUTBOARD TRACK FROM F S 760 TO FS 848. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200451 19990702 00451 NM 1999 7 2 EISA99093 1 19990408 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 870-950 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT LEFT OUTBOARD TRACK FROM F S 870 TO FS 950. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200452 19990702 00452 NM 1999 7 2 EISA99039 1 19990219 A 5755 SKIN BOEING 727 727223 1384074 NM NR 31 SPOILER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND DELAMINATION ON UPPER SURFACE OF 31 SPOILER OUTBOARD LEADING ED GE. CUT OUT DAMAGED AREA, REPAIRED HONEYCOMB CORE PER SRM 51-40-6 POTTING REPAIR. FABRICATED NEW SKIN SECTION PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-8. (M) 2 L 7 3 4F A3WE 1999070200453 19990702 00453 NM 1999 7 2 EISA99040 1 19990219 A 5755 SKIN BOEING 727 727223 1384074 NM NR 5 SPOILER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND NR 5 SPOILER DELAMINATED AT INBOARD TRAILING EDGE. REPLACED NR 5 SPOILER WITH SERVICEABLE UNIT PER MM 27-61-01. (M) 2 L 7 3 4F A3WE 1999070200454 19990702 00454 NM 1999 7 2 EISA99053 1 19990219 A 5754 RIB BOEING 727 727223 1384074 NM NR 4 LE SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURNIG ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND 2 RIBS CRACKED IN NR 4 SLAT. FABRICATED AND INSTALLED REPAIR D OUBLERS PER SRM 57-50-2 AND 5140-3. (M) 2 L 7 3 4F A3WE 1999070200455 19990702 00455 NE 1999 7 2 EISA99069 2 19990326 A 7314 371900 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE FAILED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 943VJ 47058 RIGHT ENGINE FAILED TO OR ABOUT 500 FT AGL AFTER TAKEOFF IN RDU. CREW HEARD LOUD POP OR BANG AT FAILURE. NORMAL SINGLE ENGINE LANDING AT RDU. EMERGENCY WAS DECLARED. REMOVED AND REPLACED ENGINE FUEL PUMP IAW MM 73-20-1. OPS GOOD PER MM CHAPTER 71-00. RII SIGN OFF. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999070200456 19990702 00456 WP 1999 7 2 EISA99056 1 19990312 A 3350 110049 BATTERY CHARGER DOUG DC9 DC931 3022065 WP ROW 15-18 FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 943VJ 3115 47058 EMERGENCY TRACK LIGHTING INOPERATIVE SEAT ROW 15 TO 18, FOUND SERVICE CHECK. REMOVED AND REPLACED AFT BATTERY CHARGER F OR EMERGENCY LIGHT SYSTEM IAW MM 33-53-0. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999070200457 19990702 00457 WP 1999 7 2 EISA99054 1 19990312 A 5220 5910159501 SEAL DOUG DC9 DC931 3022065 WP EMER EXIT DOOR OUT OF POSITION A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 943VJ 47058 AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE DUE TO FORWARD RIGHT OVERWING EMERGENCY DOOR NOT BEING SEATED. AIR TURN BA CK. REMOVED AND REPOSITIONED DOOR SEAL PROPERLY. OPS CHECK OK IAW 77-52-20. (M) 2 L 7 2 4F A6WE 1999070200458 19990702 00458 1999 7 2 EISA990033 4 19990226 A 3425 258733513 ADI COLLINS DOUG DC9 DC931 3022065 WP LEFT FAILED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 943VJ 47058 CAPTAIN ADI ERRATIC IN FLIGHT AFTER TAKEOFF BANK AND PITCH BOTH SHOW INCORRECT INDICATIONS. AIR TURN BACK BUFFALO. REP LACED CAPTAINS ADI AND VERTICAL GYRO, OPS CHECK GOOD PER MM 34-00. (M) 2 L 7 2 4F A6WE 1999070200459 19990702 00459 NM 1999 7 2 EISA99075 1 19990327 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 720B CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SUPPORT ANGLE CRACKED AT FS 720B, 525L. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-3 AND 53-10-4. (M) 2 L 7 3 4F A3WE 1999070200460 19990702 00460 NM 1999 7 2 EISA99107 1 19990408 A 5753 652163475 SKIN BOEING 727 727264 138408M NM LT TE AFT FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF BN58 20710 DURING C-CHECK INSPECTION, FOUND LEFT WING T/E AFT FLAP DELAMINATED AT WBL 240. REPAIRED AFT FLAP IAW BOEING 727 SRM CH APTER 51-40-05 AND 51-40-06. (M) 2 L 7 3 4F A3WE 1999070200461 19990702 00461 NM 1999 7 2 EISA99106 1 19990408 A 5543 657275051 SKIN BOEING 727 727264 138408M NM RUDDER TAB DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING C-CHECK INSPECTION, FOUND UPPER RUDDER TRIM TAB T/E DELAMINATED ON UPPER EDGE. REPAIRED IAW BOEING SRM CHAPTER 5 1-40-09 FIGURE 7. (M) 2 L 7 3 4F A3WE 1999070200462 19990702 00462 NM 1999 7 2 EISA99105 1 19990408 A 5522 652563933 SKIN BOEING 727 727264 138408M NM LT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING C-CHECK INSPECTION, FOUND CRACK IN LEFT ELEVATOR LOWER SKIN AT OUTBOARD END OF TRIM TAB. REPAIR LEFT ELEVATOR IA W BOEING 727 SRM CHAPTER 55-20-3, 51-40-5, AND 51-40-5. (M) 2 L 7 3 4F A3WE 1999070200463 19990702 00463 NM 1999 7 2 EISA99104 1 19990408 A 5522 652563933 SKIN BOEING 727 727264 138408M NM ELEVATOR DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 79 20710 DURING C-CHECK INSPECTION, FOUND LEFT ELEVATOR T/E DELAMINATED. OUTSIDE VENDOR FOUND CRACK AT OUTBOARD TRIM TAB FITTIN G AND PHENOLIC DOUBLER BROKEN IN 5 PLACES. STOP DRILLED CRACK. BONDED T/E AND APPLIED DOUBLER. REMOVED PHENOLIC DOUBL ER AND REPLACED. REBONDED T/E AND APPLIED DOUBLER IAW 727 SRM CHAPTER 55-20-3, 51-40-5 AMD 51-40-6. (M) 2 L 7 3 4F A3WE 1999070200464 19990702 00464 NM 1999 7 2 99ZZZM372 1 19990408 A 5522 652563933 SKIN BOEING 727 727264 138408M NM ELEVATOR DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 79 20710 DURING C-CHECK INSPECTION, FOUND LEFT ELEVATOR T/E DELAMINATED. OUTSIDE VENDOR FOUND CRACK AT OUTBOARD TRIM TAB FITTIN G AND PHENOLIC DOUBLER BROKEN IN 5 PLACES. STOP DRILLED CRACK. BONDED T/E AND APPLIED DOUBLER. REMOVED PHENOLIC DOUBL ER AND REPLACED. REBONDED T/E AND APPLIED DOUBLER IAW 727 SRM CHAPTER 55-20-3, 51-40-5 AMD 51-40-6. (M) 2 L 7 3 4F A3WE 1999070200465 19990702 00465 NM 1999 7 2 EISA99103 1 19990408 A 5755 65727302 SKIN BOEING 727 727264 138408M NM NR 14 SPOILER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING C-CHECK INSPECTION, FOUND RIGHT WING NR 14 SPOILER DELAMINATED ALONG TRAILING EDGE. REPAIRED IAW BOEING 727 SRM CHAPTER 51-40-4 IN REFERENCE WITH 53-30-3 FIGURE 12 AND 51-40-6 FIGURE 2. (M) 2 L 7 3 4F A3WE 1999070200466 19990702 00466 NM 1999 7 2 EISA99101 1 19990408 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 950-1010 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT LEFT 2ND INBOARD TRACK FRO M FS 950C TO FS 1010. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999070200467 19990702 00467 NM 1999 7 2 EISA99030 1 19990215 A 2612 182502800 FIRE LOOP BOEING 727 727225 1384077 NM NR 3 ENGINE OUT OF POSITION A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 352PA 20616 ENGINE NR 3 FIRE DETECTOR ILLUMINATED INFLIGHT. FOUND FIRE LOOP GROUNDING ON COWLING. REPOSITIONED LOOP AND OPS CHECK GOOD PER MM 26-81-01. (M) 2 L 7 3 4F A3WE 1999070200468 19990702 00468 WP 1999 7 2 EISA99055 1 19990316 A 3350 43 BULB GRIMES 39558811 DOUG DC9 DC931 3022065 WP COCKPIT FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 969VJ 47421 OVERHEAD EMERGENCY LIGHT IN COCKPIT WILL NOT LIGHT. REPLACED LAMP IAW 33-00-00. (M) 2 L 7 2 4F A6WE 1999070200469 19990702 00469 1999 7 2 EISA99034 4 19990302 A 3420 5223120005 INSTRUMENT AMP BENDIX BOEING 727 727231 1384079 NM E/E COMPT C1 SHORTED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 74318 20051 FLIGHT DIRECTOR BANK INDICATOR INCORRECT. AIR TURN BACK TO EAST MIDLANDS. REMOVED AND REPLACED NR 1 INSTRUMENT AMP AND THE NR 1 VERTICAL. OPS CHECK GOOD IAW MM 34-62. (M) 2 L 7 3 4F A3WE 1999070200470 19990702 00470 NM 1999 7 2 EISA99003 1 19990115 A 2611 35143 SMOKE DETECTOR BOEING 727 72731 1384010 NM CARGO COMPT INOPERATIVE A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 240NE 18906 DURING CRUISE CARGO SMOKE DETECTOR ILLUMINATED WITH NO EVIDENCE OF SMOKE, LIGHT REMAINED ON WITH DOOR OPEN ON GROUND. R EMOVED AND REPLACED NR 1 SMOKE DETECTOR. SYSTEM OPS CHECKS GOOD PER MM 26-17-0. (M) 2 L 7 3 4F A3WE 1999070200471 19990702 00471 NM 1999 7 2 EISA99036 1 19990219 A 5330 652165794 SKIN BOEING 727 727223 1384074 NM RT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CRACK IN RIGHT WING UPPER SURFACE AT NR 11 SPOILER OUTBOARD HIN GE POINT. STOP DRILLED CRACK PER SRM 51-10-01. FABRICATED AND INSTALLED DOUBLER PER SRM 57-30-4. (M) 2 L 7 3 4F A3WE 1999070200472 19990702 00472 NM 1999 7 2 EISA99037 1 19990219 A 5330 652165792 SKIN BOEING 727 727223 1384074 NM RT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND RIGHT WING TRAILING EDGE CRACK AT NR 12 SPOILER, CENTER OUTBOAR D HINGE POINT. STOP DRILLED CRACK PER SRM 51-10-01. FABRICATED AND INSTALLED DOUBLER PER SRM 57-30-4. (M) 2 L 7 3 4F A3WE 1999070200473 19990702 00473 EU 1999 7 2 SIMA991242 1 19990504 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 240DS 340B240 OKC - DURING PAINT STRIPPING, A DENT WAS DISCOVERED IN THE LEFT ICE SHIELD AND FUSELAGE AT APPROXIMATLEY STATION 330 JUS T BELOW SL 1510. REMOVED DAMAGED ICE SHIELD. REMOVED DAMAGED AREA OF FUSELAGE SKIN BY CUTOUT. PERFORMED DYE PENATRANT INSPECTION TO CUT OUT AREA AND FOUND NO DEFECTS. FABRICATED A REPAIR DOUBLER .063 THICK, 11 INCH BY 10.5 INCH SHAPED T O CONTOUR OF SKIN. APPLIED SURFACE TREATMENT OF ALODINE AND EPOXY PRIMER TO REPAIR DOUBLER AND CUT OUT AREA. APPLIED F AY SEALANT TO DOUBLER AND ATTACHED TO AIRCRAFT. INSTALLED NEW ICE SHIELD. EDGE SEALED REPAIR DOUBLER AND ICE SHIELD. R ESTORED SURFACE FINISH. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1524 AND SAAB 340 SRM STANDARD PRACTICES. AIRCRAF 2 L 7 2 4T RT A52EU 1999070200474 19990702 00474 EU 1999 7 2 SIMA991541 1 19990603 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 340B218 ABI - DURING MBV INSPECTION, FOUND CHAFING ON THE LEFT REAR FUSELAGE SKIN PANEL AT HORIZONTAL STABILIZER LEADING EDGE SE AL. BLENDED OUT CHAFE DAMAGE. PERFORMED EDDY CURRENT INSPECTION, WITH NO INDICATIONS OF CRACKS. FABRICATED DOUBLER .0 25 THICK. CONTOURED DOUBLER, ALODINED AND APPLIED EPOXY PRIMER TO REPAIR PARTS AND FUSELAGE PANEL. CLEANED REPAIR AREA , APPLIED FAY SEALANT TO REPAIR DOUBLER. POSITIONED DOUBLER AND INSTALLED ALL FASTENERS WET. APPLIED FILLET SEAL TO ED GES OF REPAIR DOUBLER. INSTALLED ANTI-CHAFE PROTECTION PLATE OVER REPAIR DOUBLER. RESTORED POLYURETHANE TOP COAT. WOR K DONE IAW SAAB REPAIR STATEMENT NR 72SDS1580, STANDARD SRM PROCEDURES AND SAAB SB 340-53-042. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4T RT A52EU 1999070200475 19990702 00475 EU 1999 7 2 SIMA991481 1 19990528 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 14 FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 234AE 340B234 JFK - FLT 4985 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 14 DOES NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY LI GHT BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999070200476 19990702 00476 EU 1999 7 2 SIMA991521 1 19990601 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 275BC 275 SAW - DURING CPCP-1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT FLIGHT ATTENDANT SEAT TRACK CORR ODED. REMOVED AND REPLACED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999070200477 19990702 00477 EU 1999 7 2 99ZZZM373 1 19990601 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 275BC 275 SAW - DURING CPCP-1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT FLIGHT ATTENDANT SEAT TRACK CORR ODED. REMOVED AND REPLACED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999070200478 19990702 00478 EU 1999 7 2 99ZZZM374 1 19990601 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 275BC 275 SAW - DURING CPCP-1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT FLIGHT ATTENDANT SEAT TRACK CORR ODED. REMOVED AND REPLACED THE SEAT TRACK IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999070200479 19990702 00479 EU 1999 7 2 SIMA991522 1 19990601 A 5320 S5367800820002 ZEE AEROSP ATR42 ATR42300 8680920 EU FRAME 39-40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 275BC 275 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AFT ZEE MEMBER BETWEEN FRAME 39 AND 40 CORRODED. REMOVED AND REPLACED TH E ZEE MEMBER IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999070200480 19990702 00480 CE 1999 7 2 RU3A99004 1 19990524 A 3610 32138769 VALVE RKWELL NA265 NA26580 7630108 CE RT ENGINE MALFUNCTIONED A RU3A A E UNSCHED LANDING ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 58 1692 38024 OK - STRONG ODOR OF BURNING RUBBER COCKPIT IMMEDIATELY AFTER TAKEOFF. RIGHT ENGINE FIRE WARNING LIGHT ILLUMINATED IMMED IATELY AFTER TAKEOFF. ENGINE SHUT DOWN AND RETURN SAFELY TO LAND. (M) 2 L 7 2 4F A2WE 1999070200481 19990702 00481 CE 1999 7 2 RU3A99005 1 19990602 A 3230 RETRACT MECH BEECH 300 300BEECH 1152930 CE LANDING GEAR MALFUNCTIONED A RU3A O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 75 FF10 OKC - LANDING GEAR FAILED TO EXTEND NORMALLY ON APPROACH TO LANDING AND EMERGENCY EXTENSION PROCEDURE SUCCESSFULLY EMPLO YED. (M) 2 L 7 2 4T A24CE 1999070200482 19990702 00482 CE 1999 7 2 RU3A99006 1 19990607 A 3260 1013646283 SWITCH BEECH 300 300BEECH 1152930 CE LT MLG FAILED A RU3A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 78 FF13 OKC - AFTER TAKEOFF, LANDING GEAR RETRACTED NORMALLY. AFTER APPROXIMATELY 15 MIN INTO FLIGHT, LANDING GEAR INADVERTENTL Y EXTENDED. REPLACED LANDING GEAR SWITCH AND LEFT SQUAT SWITCH. FLIGHT TEST SATISFACTORY. 2 L 7 2 4T A24CE 1999070200483 19990702 00483 NM 1999 7 2 P2EA99209 1 19990525 A 5313 STRINGER BOEING 737 737205 NM BS 727-796 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, STRINGER 17L WAS CRACKED FROM BS 727 TO BS 796. REPAIRED PER EO COO-3-53-334-99 DATED 5/28/99. ( M) 2 L 7 2 4F A16WE 1999070200484 19990702 00484 NM 1999 7 2 P2EA99207 1 19990508 A 5240 FRAME BOEING 737 737205 NM R1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, R1 DOOR FORWARD FRAME LOWER REINFORCEMENT WAS CRACKED. REPAIRED PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1999070200485 19990702 00485 NM 1999 7 2 P2EA99206 1 19990508 A 5755 655126734 HINGE BOEING 737 737205 NM NR 1 SPOILER CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, LEFT WING NR 1 SPOILER CENTER FITTING WAS CRACKED. FABRICATED FITTING PER EO COO-3-57-301-99. RE MOVED AND REPLACED FITTING PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1999070200486 19990702 00486 NM 1999 7 2 P2EA99205 1 19990508 A 5240 BEAM BOEING 737 737205 NM R1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, R1 DOOR BEAM NR 6 BETWEEN AFT FRAME AND AFT INTERCOSTAL WAS CRACKED. REPAIRED PER SRM 51-40-03 FI G 1. (M) 2 L 7 2 4F A16WE 1999070200487 19990702 00487 NM 1999 7 2 P2EA99204 1 19990508 A 5240 6545871140 FRAME BOEING 737 737205 NM R1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, R1 DOOR, AFT FRAME LOWER END WAS CRACKED. REMOVED AND REPLACED FRAME PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1999070200488 19990702 00488 NM 1999 7 2 P2EA99203 1 19990510 A 5320 CHORD BOEING 737 737205 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, A CHORD WAS FOUND CRACKED AT BS 727, STRINGER 18A, LEFT OUTBOARD SIDE. REPAIRED PER SB 737-53-108 8. (M) 2 L 7 2 4F A16WE 1999070200489 19990702 00489 NM 1999 7 2 P2EA99202 1 19990520 A 2130 65512145 DOOR BOEING 737 737205 NM LT RAM AIR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, THE LEFT RAM AIR DOOR WAS FOUND CRACKED. REPAIRED PER EO COO-3-52-316-99. (M) 2 L 7 2 4F A16WE 1999070200490 19990702 00490 NM 1999 7 2 P2EA99201 1 19990508 A 5240 65458714 FRAME BOEING 737 737205 NM R1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, R1 DOOR WAS FOUND CRACKED AT FORWARD FRAME LOWER SECTION. REMOVED AND REPLACED FRAME PER SRM 51-1 0-01. (M) 2 L 7 2 4F A16WE 1999070200491 19990702 00491 NM 1999 7 2 P2EA99200 1 19990521 A 5320 656228515 ANGLES BOEING 737 737205 NM BS 560 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - DURING C-CHECK, THE LOWER FUSELAGE, EXTERNAL SKIN DRAG ANGLES AT BS 560, STRINGER 24L WAS FOUND CRACKED. REPAIRED PER, SB 737-53-1031 SECTION III PART III PART II FIG 3 DATED 5/15/98 BY REPLACEMENT OF DRAG ANGLES. (M) 2 L 7 2 4F A16WE 1999070200492 19990702 00492 WP 1999 7 2 ORJA99190 1 19990604 A 2425 4055900905 SYMBOL GEN DOUG DC9 DC982 3022082 WP E/E BAY FAILED A ORJA O OTHER J WARNING INDICATION CL CLIMB 1 WP 11 823RA 49889 ONE MINUTE AFTER TAKEOFF, THE NR 1 SYMBOL GENERATOR C/B POPPED, IT FAILED TO RESET. REMOVED AND REPLACED SYMBOL GENERAT OR IAW MM 34-22-10. (M) 2 L 7 2 4F A6WE 1999070200493 19990702 00493 SW 1999 7 2 99ZZZM375 1 19990526 A 3260 602EN6026 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT MLG INOPERATIVE A MEJA O OTHER N FALSE WARNING CL CLIMB 1 SW 17 370AE AC506 AFTER TAKEOFF FROM ANU, THE LEFT MAIN LANDING GEAR ANNUNCIATOR INTRANSIT LIGHT ILLUMINATED. THE CREW RECYCLED THE GEAR TWICE WITH THE SAME RESULTS AND THE AIRCRAFT PROCEEDED ON TO BGI WITHOUT INCIDENT. THE AIRCRAFT WAS THEN INSPECTED AND FERRIED TO SJU FOR MAINTENANCE WITH THE LANDING GEAR DOWN. MAINTENANCE REMOVED AND REPLACED THE LEFT LANDING GEAR UPLIM IT SWITCH WITH A NEW UNIT. SEVERAL RETRACTION TESTS WERE PERFORMED, CHECKED GOOD, AND THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 2 4T RT A8SW 1999070200494 19990702 00494 EU 1999 7 2 DKAA99015 1 19990603 A 2170 8323710 COALESCER AMD FALC20 FALCON 2720302 EU CABIN CONTAMINATED A DKAA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 GL 23 950RA 95 LOST CABIN PRESSURE FL250, COULD NOT MAINTAIN CABIN IN EITHER AUTO OR MANUAL AT ALTITUDE. REPLACED THE WATER SEPARATOR SOCK AND ANTI-ICE PRESSURE REDUCING VALVE FILTER. OPERATIONAL CHECKS GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A7EU 1999070200495 19990702 00495 SO 1999 7 2 ASOA99047 1 19990519 A 3610 38E966A REGULATOR EMB 120 EMB120ER 3260203 SO FUSELAGE LEAKING A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 11 639AS 120283 FLT 4253 - LEFT DUCT LEAK LIGHT IN FLIGHT. FOLLOWED CHECKLIST, LIGHT WOULD NOT EXTINGUISH. SHUTDOWN LEFT ENGINE, LIGHT EXTINGUISHED. RETURNED TO ATL. MAINTENANCE UNABLE TO DUPLICATE ON GROUND. RAN ENGINES FOR 35 MINUTES WITH NO DUCT LE AK INDICATION. CHECKED DUCTS FROM ENGINE TO ACM, NO LEAKS FOUND. REPOSITIONED WIRES ON OUTER SENSOR AND RESOLDERED WIR ES ON SENSOR NEXT TO DE-ICE REGULATOR. FOUND DE-ICE PRESSURE REGULATOR LEAKING. REMOVED AND REPLACED DE-ICE PRESSURE R EGULATOR. GROUND CHECKS GOOD. (M) 2 L 7 2 4T RT A31SO 1999070200496 19990702 00496 SO 1999 7 2 ASOA99046 1 19990518 A 2150 22045402 ACM EMB 120 EMB120ER 3260203 SO WING/FUS VIBRATES A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 638AS 120282 SMELL OF SOMETHING HOT IN CABIN AND LIGHT HAZE SEEN BY FLIGHT ATTENDANT. BELIEVED LEFT PACK OVERHEAT. MAINTENANCE FOUN D THE LEFT PACK TO OPERATE NORMALLY. RIGHT PACK VIBRATES AND DOES NOT COOL WELL. REMOVED AND REPLACED RIGHT ACM. (M) 2 L 7 2 4T RT A31SO 1999070200497 19990702 00497 NM 1999 7 2 AALA990441 1 19990330 A 3397 WIRE BOEING 727 727223 1384074 NM ROW 7DEF DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN FIRST AND COACH CABIN INOPERATIVE. REPLA CED EMERGENCY EXIT FLOOR PATH FLAP JUMPER WIRE AT SEAT ROW 7DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070200498 19990702 00498 NM 1999 7 2 AALA990424 1 19990325 A 3397 WIRE BOEING 727 727233 138408A NM SERVICE DOOR GROUNDED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 866AA 21371 ORD - DURING OVERNIGHT MAINTENANCE, FOUND THE LEFT AND RIGHT AFT SERVICE DOOR EMERGENCY SLIDE LIGHTS INOPERATIVE. MAINT ENANCE FOUND THE RIGHT AFT EMERGENCY EXIT LIGHT RECEPTACLE WITH A WIRE GROUNDING. REPOSITIONED WIRE WHAT WAS GROUNDED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A3WE 1999070200499 19990702 00499 NM 1999 7 2 AALA990336 1 19990314 A 3397 WIRE BOEING 727 727223 1384074 NM ROW 4D DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 883AA 21522 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 4D INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH FLAT JUMPER WIRE AT SEAT ROW 4D. SYSTEM GROUND CHCKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070200500 19990702 00500 NM 1999 7 2 AALA990334 1 19990314 A 3397 WIRE BOEING 727 727223 1384074 NM ROW 16 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843AA 20984 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH FLAT JUMPER WIRE AT SEAT ROW 16. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070200501 19990702 00501 NM 1999 7 2 AALA990676 1 19990507 A 3350 LIGHT BOEING 727 727227 1384078 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 723AA 20731 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY E XIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070200502 19990702 00502 NM 1999 7 2 AALA990544 1 19990418 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM 1L DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 716AA 20608 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 1L DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070200503 19990702 00503 NM 1999 7 2 AALA990408 1 19990322 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721AA 20729 DFW - DURING MAINTENANCE, AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LI GHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070200504 19990702 00504 EU 1999 7 2 AALA990694 1 19990511 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN MALFUNCTIONED A AALA K NONE L NO TEST LD LANDING 1 SW 07 1412A 11370 ORD - FLT 2044 - EMERGENCY EXI TLIGHTS DO NOT ILLUMINATE WHEN GEAR IS DOWN. SYSTEM OPERATES NORMAL WHEN SELECTED TO ON POSITION. CABIN STANDBY LIGHTING WAS PLACARDED PER MEL. DURING MAINTENANCE CHECK, CABIN STANDBY LIGHTING WAS CHECKED P ER 0910 CARD. UNABLE TO DUPLICATE FAULT. REMOVED PLACARD AND CLEANRED MIC SHEET. SYSTEM GROUND CHECKED NORMAL OPERATI ON. (M) 2 L 7 2 4F RT 1999070200505 19990702 00505 EU 1999 7 2 AALA990729 1 19990521 A 3350 A3060698101 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1422J 11405 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH LIGHTING IN MID CABIN WOULD NOT ILLUMINATE. MAINTENANCE FOUND EMERGE NCY PATH LIGHTING POWER STRIP SHORTED. REPLACED POWER STRIP FLAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F RT 1999070200506 19990702 00506 WP 1999 7 2 AALA990741 1 19990521 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 24 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 466AA 49596 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 24 INOPERATIVE. REPLACED EMERGENCY EXIT FLO OR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200507 19990702 00507 WP 1999 7 2 AALA990740 1 19990523 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 28-30 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 292AA 49304 DFW - DURING OVERNIGHT MAINTENANCE, EMEREGNCY EXIT FLOOR PATH LIGHTING AT ROWS 28 THROUGH 30 INOPERATIVE. REPLACED EMER GENCY EXIT FLOOR PATH LIGHT STRIP AND CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200508 19990702 00508 WP 1999 7 2 AALA990723 1 19990520 A 3350 SA2076SO CONNECTOR DOUG DC9 DC982 3022082 WP ROW 20 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7517A 49894 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 20 INOPERATIVE. REPLACED SPLICE CONNEC TOR ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200509 19990702 00509 EU 1999 7 2 AALA990769 1 19990526 A 2560 SCI535B5F48X05N HORN AIRBUS 300 A300B4605R 3930308 EU 3L DOOR DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 JFK - DURING OVERNIGHT MAINTENANCE, 3L DOOR EVACUATION HORN INOPERATIVE. REPLACED EVACUATION HORN AT 3L DOOR. SYTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999070200510 19990702 00510 WP 1999 7 2 AALA990767 1 19990525 A 3350 BULB DOUG DC9 DC982 3022082 WP CATWALK LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7534A 49988 DFW - DURING OVERNIGHT MAINTENANCE, CATWALK CEILING EMERGENCY EXIT LIGHT AT AFT POSITION INOPERATIVE. RESEALED BULB. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200511 19990702 00511 WP 1999 7 2 AALA990771 1 19990526 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 19 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 571AA 49353 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT ROW 19 INOPERATIVE. SPLICED WIRE AT ROW 19 ON EMERGENC Y EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999070200512 19990702 00512 WP 1999 7 2 AALA990772 1 19990526 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90511 49805 DFW - DURING OVERNIGHT CHECK EMERGENCY EXIT FLOOR PATH LIGHT AT WINDOW ESCAPE AREA INOPERATIVE. SPLICED WIRE AT WINDOW ESCAPE AREA ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200513 19990702 00513 WP 1999 7 2 AALA990787 1 19990531 A 3350 L201919 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447AA 49473 DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT OVERHEAD LIGHT INOPERATIVE. REPLACED AFT EMERGENCY EXIT OVERHEAD LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200514 19990702 00514 WP 1999 7 2 AALA990786 1 19990531 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 464AA 49594 DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING JUMPER IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200515 19990702 00515 WP 1999 7 2 AALA990780 1 19990530 A 3260 833703 SENSOR DOUG DC9 DC983 3022083 WP LT MLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 564AA 49346 ORD - FLT 1063 - EN ROUTE YYZ-ORD, DURING CLIMB, THE GEAR DOOR LIGHT ILLUMINATED. FOLLOWED CHECKLIST, TURNED ON RIGHT E NGINE HYDRAULICS AND LIGHT REMAINED OFF FOR REST OF THE FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED SENSOR ON LEFT M AIN LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999070200516 19990702 00516 NM 1999 7 2 AALA990842 1 19990608 A 2530 8609010000 OVEN BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 379AA 25448 LHR - FLT 46 - EN ROUTE NR 2 FIRST CLASS OVEN SMOKING. TURNED OVEN OFF AND SMOKE DISSIPATED. LANDED LHR WITHOUT INCIDE NT. PULLED CIRCUIT BREAKERS AND BANDED AND DEFERRED PER PD. ORD REPLACED FIRST CLASS OVEN. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999070200517 19990702 00517 WP 1999 7 2 AALA990825 1 19990604 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 466AA 49596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN CENTER INOPERATIVE. REPAIR EMERGENCY EXIT FLO OR PATH LIGHTING STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200518 19990702 00518 WP 1999 7 2 AALA990841 1 19990608 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP EMER EXIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 255AA 49287 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200519 19990702 00519 WP 1999 7 2 AALA990821 1 19990603 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7520A 49897 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR EMERGENCY WALK AROUND LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOOR EMERGENCY WALK AROUND LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200520 19990702 00520 EU 1999 7 2 AALA990745 1 19990523 A 2841 SIC50773 COMPUTER AIRBUS 300 A300B4605R 3930308 EU E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 70072 0569 515 MIA - FLT 657 - EN ROUTE JFK-PAP, DURING CRUISE, LEFT INNER FUEL QTY INDICATION RAPIDLY DECREASED FROM ABOUT 28,000 TO 1 1,500 LBS. NO FUEL LEAK INDICATION. AIR INTERRUPTED AND LANDED MIA WITHOUT INCIDENT. REPLACED FUEL QTY COMPUTER. PER FORMED ALL REQUIRED TEST CHECKS ACCORDING TO MAINTENANCE MANUAL. SUMPED ALL TANK OF WATER. TRANSFERRED ALL FUEL OUT OF LEFT INNER TANK, HAD FUELER METER FUEL BACK INTO TANK. USED FUEL TANK STICK FOR FUEL VERIFICATION. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999070200521 19990702 00521 WP 1999 7 2 AALA990789 1 19990601 A 3260 368658188101 PANEL DOUG DC10 DC1010 3022110 WP LANDING GEAR MALFUNCTIONED A AALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 167AA 46930 SJU - FLT 678 - ON THE GROUND AT SJU, THE GREEN LIGHT FOR GEAR INDICATION DID NOT PASS PERSON TO TEST, RED LIGHT NORMAL. REPLACED PILOT ANNUNCIATOR PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999070200522 19990702 00522 EU 1999 7 2 AALA990782 1 19990531 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 33069 512 LHR - FLT 108 - DURING CRUISE, EN ROUTE BOS-LHR, FIRST CLASS OVENS WERE SMOKING. LANDED LHR WITHOUT INCIDENT. CLEANED FIRST CLASS OVEN OF FOOD DEBRIS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999070200523 19990702 00523 WP 1999 7 2 AALA990761 1 19990525 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 428AA 49340 DFW - DURING OVERNIGHT CHECK, AFT TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED GROUND ON AFT TAIL CONE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070200524 19990702 00524 NM 1999 7 2 USAA069903 1 19990604 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 3 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS WA7282 21244 FOUND ON L/S, OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 3. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999070200525 19990702 00525 NM 1999 7 2 USAA069904 1 19990604 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM EMER EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 926TS 20774 FLT 6121 - BOS-LGA, FOUND ON L/S, RIGHT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, CHECKS OK. (M ) 2 L 7 3 4F A3WE 1999070200526 19990702 00526 WP 1999 7 2 USAAD99078 1 19990607 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 928VJ 48131 IND- FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F A6WE 1999070200527 19990702 00527 WP 1999 7 2 USAAD99077 1 19990608 A 3350 20131ALP BATTERY CHARGER DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 934VJ 48114 IND - FOUND AFT SECTION OF EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER (INOPERATIVE) AND T HE BATTERY PACK. (M) 2 L 7 2 4F A6WE 1999070200528 19990702 00528 WP 1999 7 2 USAAD99073 1 19990604 A 3350 9721055 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 IND - MAINTENANCE FOUND THREE PASSENGER CABIN SEATS WITH THE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE THREE BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999070200529 19990702 00529 WP 1999 7 2 USAAD99074 1 19990604 A 3350 8732030153 CONTROL MODULE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST CR CRUISE 1 EA 19 805US 48053 CLT - FLT 1516 - AFT EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT CONTROL M ODULE. (M) 2 L 7 2 4F A6WE 1999070200530 19990702 00530 WP 1999 7 2 USAAD99075 1 19990604 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP ROWS 5/11 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 819US 48099 CLT - FLOOR LEVEL EMERGENCY LIGHT AT ROW 11 IS ILLUMINATED. MAINTENANCE REPLACED THE BATTERY. DURING CHECK OF SYSTEM, FOUND LIGHT AT ROW 5 INOPERATIVE. MAINTENANCE REPLACED THAT BATTERY AS WELL. (M) 2 L 7 2 4F A6WE 1999070200531 19990702 00531 WP 1999 7 2 USAAD99076 1 19990607 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP ROW 1,3,11,16,19 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 815US 48095 PIT - FOUND FLOOR LEVEL EMERGNECY LIGHTS IN ROWS 1, 3, 11, 16 AND 19 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. ( M) 2 L 7 2 4F A6WE 1999070200532 19990702 00532 WP 1999 7 2 USAAD99072 1 19990603 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 PIT - PILOT REPORTED THE LOW LEVEL EMERGENCY LIGHTING WAS INOPERATIVE DURING ORIGINATING PREFLIGHT CHECK. MAINTENANCE R EMOVED AND REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999070200533 19990702 00533 NM 1999 7 2 USAA990530 1 19990522 A 5312 BULKHEAD SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, RBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999070200534 19990702 00534 NM 1999 7 2 USAA990529 1 19990522 A 5312 BULKHEAD SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 198, RBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999070200535 19990702 00535 NM 1999 7 2 USAA990528 1 19990522 A 5312 BULKHEAD SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, RBL 7 INCH. INSTALLED DOUBLER T/R 53 -10-07. (M) 2 L 7 2 4F RT A16WE 1999070200536 19990702 00536 NM 1999 7 2 USAA990527 1 19990522 A 5312 BULKHEAD SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 198, LBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999070200537 19990702 00537 NM 1999 7 2 USAA990526 1 19990522 A 5312 BULKHEAD SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, LBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999070200538 19990702 00538 NM 1999 7 2 USAA990525 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 787, BETWEEN STRINGER 8 AND STRIN GER 9R. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070200539 19990702 00539 NM 1999 7 2 USAA990524 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 827, BETWEEN STRINGER 8R/9R. INST ALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070200540 19990702 00540 NM 1999 7 2 USAA990523 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 380, BETWEEN STRINGER 8R/9R. INSTA LLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070200541 19990702 00541 NM 1999 7 2 USAA069945 1 19990616 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS WA7282 21244 FLT 6181 - BOS-LGA - FOUND ON L/S, COCKPIT OVERHEAD EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999070200542 19990702 00542 NM 1999 7 2 USAA069944 1 19990616 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM R-1 DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 4898 21244 FLT 6181 - BOS-LGA - FOUND ON L/S, R-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999070200543 19990702 00543 WP 1999 7 2 USAAD99080 1 19990613 A 3350 14597101 BATTERY PACK DOUG DC9 DC931 3022065 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 926VJ 48146 IND - THE TAILCONE OVERHEAD EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERIES. (M) 2 L 7 2 4F A6WE 1999070200544 19990702 00544 WP 1999 7 2 USAAD99081 1 19990615 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 47336 IND - THE FORWARD ENTRY DOOR EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE BATTERY FOR THE FORWARD ENTRY DOOR EMERG ENCY LIGHT. (M) 2 L 7 2 4F A6WE 1999070200545 19990702 00545 NM 1999 7 2 USAASB99142 1 19990614 A 3350 500000043 CHARGER BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 236US 22352 ORD - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999070200546 19990702 00546 NM 1999 7 2 USAASB99140 1 19990605 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM ROW 10-22 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 335US 23232 ALB - MAINTENANCE FOUND THE BULLNOSE EMERGENCY EVACUATION LIGHTS AT SEAT ROW 10, RIGHT SIDE, AND SEAT ROWS 12 THROUGH 22 , LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999070200547 19990702 00547 NM 1999 7 2 99ZZZM376 1 19990605 A 3350 20121 BATTERY PACK BOEING 737 737301 1384611 NM ROW 10-22 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 335US 23232 ALB - MAINTENANCE FOUND THE BULLNOSE EMERGENCY EVACUATION LIGHTS AT SEAT ROW 10, RIGHT SIDE, AND SEAT ROWS 12 THROUGH 22 , LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999070200548 19990702 00548 NM 1999 7 2 USAASB99138 1 19990605 A 2432 401767 BATTERY BOEING 737 737301 1384611 NM BATTERY COMPT DISCHARGED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 589US 16172 23934 DEN - FLT 621 - EN ROUTE FROM LAS TO PHL, CREW REPORTED A STRONG ODOR OF ELECTRICAL FUMES IN THE CABIN. CREW DECLARED A N EMERGENCY AND DIVERTED TO DEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MAIN AIRCRAFT BATTERY T O HAVE AN INTERNAL SHORT. REMOVED AND REPLACED THE MAIN AIRCRAFT BATTERY AND THE BATTERY CHARGER PER MM 24-31-11. OPER ATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999070200549 19990702 00549 NM 1999 7 2 99ZZZM377 1 19990605 A 2432 279202 BATTERY CHARGER BOEING 737 737301 1384611 NM BATTERY COMPT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 589US 16172 23934 DEN - FLT 621 - EN ROUTE FROM LAS TO PHL, CREW REPORTED A STRONG ODOR OF ELECTRICAL FUMES IN THE CABIN. CREW DECLARED A N EMERGENCY AND DIVERTED TO DEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MAIN AIRCRAFT BATTERY T O HAVE AN INTERNAL SHORT. REMOVED AND REPLACED THE MAIN AIRCRAFT BATTERY AND THE BATTERY CHARGER PER MM 24-31-11. OPER ATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999070200550 19990702 00550 NM 1999 7 2 USAASB99137 1 19990604 A 2410 731753 CSD BOEING 737 737201 1384454 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 262AU 27987 22868 PHL - FLT 711 - ON CLIMB-OUT FROM EWR, AT APPROXIMATELY FL150, THE NR 2 GENERATOR TRIPPED OFF LINE WITH THE NR 2 CSD IND ICATING LOW OIL PRESSURE AND HIGH OIL TEMPERATURE. WITH THE APU BEING INOPERATIVE AND ON MEL, THE CREW WAS DOWN TO ONE SOURCE OF ELECTRICAL POWER AND PER QUICK REFERENCE HANDBOOK PROCEDURES, DIVERTED TO THE NEAREST SUITABLE AIRPORT AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 CSD AND OIL COOLER (P/N 6A47-000). OPERATIONAL CHECK AND LEAK CHECK GOOD. CLEANED MEL ON APU BY CLEANING THE ATOMIZER AND LAT ER REPLACING THE BURNER CAN. (M) 2 L 7 2 4F A16WE 1999070200551 19990702 00551 WP 1999 7 2 USAA990607 1 19990612 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 168 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 811US 48470 48043 PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .750 INCH CRACK AT FORWARD UPPER CORNER OF MED DOOR JAMB STATION 168 S KIN. REPAIRED PER SRM 53-05, FIG 26 CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F A6WE 1999070200552 19990702 00552 WP 1999 7 2 USAA990608 1 19990612 A 5755 5936838505 FITTING DOUG DC9 DC981 3022081 WP LT SPOILER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 811US 48470 48043 PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LEFT GROUND SPOILER SUPPORT FITTING LEG UPPER END. INSTALL ED PART 5936838-505. (M) 2 L 7 2 4F A6WE 1999070200553 19990702 00553 WP 1999 7 2 USAA990609 1 19990612 A 5320 WEB DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 811US 48470 48043 PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK CANTED WEB AT STATION 1463 STRINGER 18R. CUTOUT DAMAGE A ND INSTALLED DOUBLER PER TR 53-10-25. (M) 2 L 7 2 4F A6WE 1999070200554 19990702 00554 WP 1999 7 2 USAA990610 1 19990612 A 5311 BELTFRAME DOUG DC9 DC981 3022081 WP BS 1322 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 811US 48470 48043 PIT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT STATION 1322 STRINGER 27L TO 27 BELTFRAME. REMOVED AND REPLACED BELTFRAME. (M) 2 L 7 2 4F A6WE 1999070200555 19990702 00555 NM 1999 7 2 AALA990582 1 19990224 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FRAME 600 LEFT STRINGER 22L TO STRINGER 24L, 3 EACH DENTS IN UPPER LIP OF FRAME 2 EACH CUT OUT APPROX 2.25 INCH, O NE CUT OUT APPROX 3 INCHES. REPAIRED AREA. (M) 2 L 7 3 4F A3WE 1999070200556 19990702 00556 NM 1999 7 2 AALA990585 1 19990325 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FRAME 680 DENTED BETWEEN STRINGER 23R AND 24R. INSTALLED BELT FRAME DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999070200557 19990702 00557 NM 1999 7 2 AALA990584 1 19990420 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-4 0-3. (M) 2 L 7 3 4F A3WE 1999070200558 19990702 00558 NM 1999 7 2 AALA990583 1 19990326 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND FRAME 660 DENTED FROM STATION 24L TO 23L. REMOVED TWO DAMAGED AREAS, .75 INCH BY 6.5 INCH, .75 INCH BY .75 INCH. INSTALLED DOUBLER (7075 T-6, .063) 18 INCHES LONG, WITH 3 ROWS OF RIVETS, 1 ROW ON TOP, 2 ROWS ON SIDE WITH 41 .1 875 D-RIVETS AND FOUR .25 INCH D-RIVETS. (M) 2 L 7 3 4F A3WE 1999070200559 19990702 00559 NM 1999 7 2 AALA990586 1 19990329 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 990 BELL FRAME FLANGE AND WEB BENT LEFT STRINGER 25-27. CUT OUT 6.75 INCH BY 1.25 INCH DAMAGED AREA S. INSTALLED .071 T-6 DOUBLER PER SRM 51-40-3, 25 MS20470, 25MS 20470 D6-6 (RIVETS), 16 BACR15CE6D6 RIVETS, 3 BACB30FP6 -3 (RIVETS), 3BAC30M6 COLLARS. (M) 2 L 7 3 4F A3WE 1999070200560 19990702 00560 NM 1999 7 2 AALA990587 1 19990325 A 5311 FRAME BOEING 727 727223 1384074 NM BS 970 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - BELLFRAME FLANGE AND WEB BENT STATION 970 BETWEEN 25 AND 26, STRINGER LEFT. CUT OUT DAMAGE 5.75 BY 1.25. REPAIRE D BELL FRAME STATION 970 BETWEEN 25 AND 26 STRINGER LEFT PER 51-40-3, DOUBLER .71 MATERIAL 13BACB30MB6-3 HI-LOCKS, 13 BA CC30M8 COLLARS, 7NAS8603-3 SCREWS, 2 ROWS ON SIDE, 1 ONT TOP. (M) 2 L 7 3 4F A3WE 1999070200561 19990702 00561 NM 1999 7 2 AALA990588 1 19990330 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 1070 BETWEEN STRINGER 26R-25R, BELLFRAME BENT IN WEB. REMOVED 3.5 INCH BY 1.25 INCH DAMAGED AREA. I NSTALLED .071 T6 DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER WITH 11BACB30FP8-4, 11 BACC30M8, 11 BACBB30FP6-3, 19 BACC30 M6, 8 BACB30F06-3 HI-LOCKS. (M) 2 L 7 3 4F A3WE 1999070200562 19990702 00562 NM 1999 7 2 AALA990589 1 19990329 A 5320 651632710 ANGLE BOEING 727 727223 1384074 NM BS 804.3 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND ANGLE ON FRAME CRACKED AT FASTENER HOLE AT ATTACH POINT TO STRINGER 14R. REMOVED CRACKED PART AND INSTALLED NEW PART WITH HI-LOCKS. (M) 2 L 7 3 4F A3WE 1999070200563 19990702 00563 NM 1999 7 2 AALA990590 1 19990420 A 5320 BEAM BOEING 727 727223 1384074 NM BS 786-790 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND CORROSION ON LIGHTENING HOLE ON BOTTOM OF DELTA BEAM AT STATION 786 TO 790. REPAIRED WITH DOUBLER IAW SRM 5 1-40-2 AND 51-20-0. (M) 2 L 7 3 4F A3WE 1999070200564 19990702 00564 NM 1999 7 2 AALA990591 1 19990407 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1030 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND BELL FRAME (SPLICE) STRAP CRACKED STATION 1030 BETWEEN STRINGER 24L AND 25L. REPLACED (SPLICE) STRAP PER 51 -10-1. (M) 2 L 7 3 4F A3WE 1999070200565 19990702 00565 NM 1999 7 2 AALA990592 1 19990408 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1030 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND BELL FRAME BENT FLANGE AND WEB STATION 1030 STRINGER 26R TO STRINGER 25R. CUT OUT DAMAGED AREA AND INSTALLE D DOUBLERS PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999070200566 19990702 00566 NM 1999 7 2 AALA990593 1 19990413 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1030 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 1030 BELL FRAME BENT (FLANGE/WEB) STRINGER 26-25 LEFT. REMOVED DAMGED SECTIONS, 1 INCH BY 2.8125 IN CH BY 1 INCH BY 1.3125 INCH FROM BELL FRAME FLANGE, DYE CHECKED FOR CRACKS, NONE FOUND. INSTALLED DOUBLER PER SRM 51-40 -3. (M) 2 L 7 3 4F A3WE 1999070200567 19990702 00567 NM 1999 7 2 AALA990594 1 19990416 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND BELL FRAME FLANGE DENTED STATION 1110, STRINGER 27 AND 25R. INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999070200568 19990702 00568 NM 1999 7 2 AALA990595 1 19990404 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1010 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND BELL FRAME FLANGE/WEB BENT. INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999070200569 19990702 00569 NM 1999 7 2 AALA990596 1 19990415 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 620 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-4 0-3 DOUBLER 17-7 MATERIAL .063 THICK 2.5 INCH BY 2.5 INCH BY 15 INCH WITH BAC30FQ6 FASTENERS AND 44 BACC30MB COLLARS. ( M) 2 L 7 3 4F A3WE 1999070200570 19990702 00570 SO 1999 7 2 C2XA99IA279 1 19990517 A 2760 14233022405 CONTROL UNIT EMB 145 EMB145 SO SPOILER SYSTEM INOPERATIVE A C2XA H DEACTIVATE SYST/CIRCUITS F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 09 14959 145091 IAH - FLT 4278 - THE CREW REPORTED THAT AT 14,000 FEET AFTER THE SPEED BRAKE LEVER WAS CLOSED, THE AIRCRAFT ROLLED TO TH E RIGHT, AND SPOILER WARNING MESSAGE ON EICAS WAS DISPLAYED. THE CREW DISENGAGED THE AUTOPILOT, AND PULLED THE CIRCUIT BREAKERS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENNACE REMOVED AND REPLACED THE SPOILER CONTORL UNIT IAW E MB145 MM 27-63-02. THE AIRCRAFT WAS TEST FLOWN WITH NO DISCREPANCIES NOTED, AND WAS THEN APPROVED FOR RETURN TO SERVICE . (X) 2 L 7 2 4F RT T00011AT 1999070200571 19990702 00571 NM 1999 7 2 CALA9900463 1 19990501 A 3350 L870 POWER SUPPLY BOEING 727 727232 1384082 NM EMERGENCY EXIT INOPERABLE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 IAH - TWO OVERWING EMERGENCY LIGHTS AND ONE EMERGENCY LIGHT AFT OF FLAPS LEFT SIDE OF FUSELAGE INOPERABLE. FOUND M654, M954, AND M955 POWER SUPPLIES BAD. REPLACED POWER SUPPLIES AND LIGHT ASSEMBLIES L878, L877, AND L822. EMERGENCY LIGHTS OPS CHECK NORMAL. REFERENCE WDM 33-51-02. (X) 2 L 7 3 4F A3WE 1999070200572 19990702 00572 NM 1999 7 2 CALA9900458 1 19990502 A 5315 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 907-947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 HOU - LEFT INBOARD CABIN SEAT TRACK HAS CORROSION AT STA 907 TO STA 947. FABRICATED AND INSTALLED NEW SECTION OF SEAT T RACK PER SRM 53-00-52 FIG 204. (X) 2 L 7 2 4F RT A16WE 1999070200578 19990702 00578 1999 7 2 F3LA99046 4 19990513 A 2565 1061323461 BATTERY BOEING 737 73736Q 1384409 NM L1 DOOR SLIDE DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 305FA 6449 1225A 28662 DEN - DURING C-CHECK, INSPECTION REPORTED L-1 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-1 EMERGENC Y ESCAPE SLIDE. CYCLES: 2,724. (X) 2 L 7 2 4F RT A16WE 1999070200579 19990702 00579 1999 7 2 F3LA99047 4 19990515 A 2565 1061323469 BATTERY BOEING 737 73736Q 1384409 NM L2 DOOR SLIDE DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 305FA 6449 1109A 28662 DEN - DURING C-CHECK INSPECTION REPORTED L-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOTLAGE TEST. REPLACED L-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,724. (X) 2 L 7 2 4F RT A16WE 1999070200580 19990702 00580 1999 7 2 F3LA99049 4 19990519 A 2565 D31354433 BATTERY BOEING 737 73736N 1384408 NM L2 DOOR SLIDE DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 306FL 6261 1627 28563 DEN - DURING C-CHECK INSPECTION REPORTED L-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,660. (X) 2 L 7 2 4F RT A16WE 1999070200581 19990702 00581 1999 7 2 F3LA99048 4 19990519 A 2565 D31591475 BATTERY BOEING 737 73736N 1384408 NM L1 DOOR SLIDE DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 306FL 6261 1268A 28563 DEN - DURING C-CHECK INSPECTION REPORTED L-1 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-1 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X) 2 L 7 2 4F RT A16WE 1999070200582 19990702 00582 1999 7 2 F3LA99050 4 19990519 A 2565 61621469 BATTERY BOEING 737 73736N 1384408 NM R2 DOOR SLIDE DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 306FL 6261 28563 DEN - DURING C-CHECK INSPECTION REPORTED R-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED R-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X) 2 L 7 2 4F RT A16WE 1999070200583 19990702 00583 EA 1999 7 2 MASA99058 1 19990412 A 5210 TRACKS CNDAIR CL600 CL6002B19 EA PASSENGER DOOR DIRTY A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 7291Z 7291 DCA/CMH - FLT 5361 - CREW REPORTED PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE INSPECTED AND CLEANED SOME DEBRIS FROM T HE LOWER TRACK, OPS CHECK GOOD. NO DEFECT WAS FOUND WITH THE DOOR. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200584 19990702 00584 EA 1999 7 2 MASA99073 1 19990512 A 5210 HSP115N094900 ROLL PIN CNDAIR CL600 CL6002B19 EA PASSENGER DOOR BROKEN A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 77302 H341429 7302 PHX/MAF - FLT 6088 - CAPTAIN REPORTED THE PASSENGER DOOR HANDLE WOULD NOT LOCK. MAINTENANCE INSPECTED THE DOOR HANDLE A ND FOUND THE ROLL PIN WAS BROKEN. THE PIN WAS REPLACED, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200585 19990702 00585 EA 1999 7 2 MASA99065 1 19990503 A 2751 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A MASA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 SW 07 77302 7302 BWI-CMH - FLT 5143 - CREW RECEIVED A FLAP FAIL MESSAGE IN-FLIGHT. NO EMERGENCY WAS DECLARED, BUT THE CAPTAIN REQUESTED EMERGENCY VEHICLES TO STAND BY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE C/W AD 982001, NO DISCREPANC IES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200586 19990702 00586 EU 1999 7 2 SIMA991371 1 19990517 A 2611 721111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS RACK MALFUNCTIONED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 286AE 340B286 SAN - FLT 3212 - AVIONICS SMOKE LIGHT ILLUMINATED. VERIFIED EVENT WAS A FALSE WARNING. REMOVED AND REPLACED AVIONICS S MOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999070200587 19990702 00587 EA 1999 7 2 99ZZZX2504 1 19990326 A 3397 WIRE DHAV DHC8 DHC8311 1386006 EA CABIN LOOSE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 803SA 221 DURING RON MAINTENANCE, AFT CEILING EMERGENCY LIGHT DID NOT TEST. FOUND AND REPAIRED GROUND WIRE. EMERGENCY LIGHTS OPS CHECKS GOOD. (X) 2 H 7 2 4T RT A13NM 1999070200588 19990702 00588 EU 1999 7 2 USAASA99002 1 19990518 A 5610 D5311001802901 WINDOW AIRBUS A319 A319112 EU COCKIPT CRACKED A USAA B EMER. DESCENT O OTHER CR CRUISE 1 EA 19 706US 0946 SEA/PHL - FLT 110 - EN ROUTE, THE FIRST OFFICER'S SLIDING WINDOW CRACKED. A RAPID DESCENT WAS INITIATED TO 10,000 FEET TO RELIEVE PRESSURE ON THE WINDOW. THE AIRCRAFT LANDED AT THE DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED THE F IRST OFFICER'S SLIDING WINDOW ASSEMBLY. (X) 2 L 7 2 4F RT A28NM 1999070200589 19990702 00589 EA 1999 7 2 VTZA990044 1 19990427 A 7714 CONNECTOR CNDAIR CL600 CL6002B19 EA NR 2 ENGINE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 633BR 7274 ORD/AVP - FLT 7826 - DURING CLIMB AT 0850 HRS ON 4-24-99, AIRCRAFT RETURNED TO ORD DUE TO NR 2 ENGINE N2 INDICATING DROP PED OFF-LINE. MAINTENANCE CLEANED CANNON PLUGS TO RT ENGINE N2 SPEED SENSING ALTERNATOR AND CONTROL. AMPLIFIER OPS CHE CK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200590 19990702 00590 EA 1999 7 2 VTZA9950 1 19990428 A 2740 CONNECTOR CNDAIR CL600 CL6002B19 EA HORIZ STABILIZER DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 633BR 7274 ORD/SGF - FLT 7821 - DURING TAKEOFF AT 1415 HRS, AIRCRAFT RETURNED TO ORD AND MADE AN UNSCHEDULED LANDING DUE TO MACH AN D STAB TRIM MESSAGE. MAINTENANCE PERFORMED BITE TEST, AND FULL SYSTEM DIAGNOSITC. CLEARED FCC AUTOPILOT FAULTS FOUND IN HSTCU A & B DIAGNOSTIC, PERFORMED A FULL SYSTEM RESET, REMOVED HSTCU, CLEANED AND INSPECTED CONNECTORS, RE-INSTALLED HSTCU. PERFORMED BITE CHECK AND FULL SYSTEM DIAGNOSTICS. NO FURTHER FAULTS OR DEFECTS NOTED. PERFORMED FULL SYSTEM TE ST ON GROUND. OPS CHECK GOOD. AIRCRAFT RELEASED FOR MAF TO CHECK OPERATION OF THE HORIZONTAL STABILIZER TRIM SYSTEM. M AF SATISFACATORY. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200591 19990702 00591 EA 1999 7 2 VTZA990057 1 19990502 A 3520 MASK CNDAIR CL600 CL6002B19 EA CABIN DEPLOYED A VTZA K NONE O OTHER IN INSP/MAINT 1 EA 27 634BR 7287 ORD - FLT 0000 - DURING PRE-FLIGHT AT 303 OHMS ON 5-2-99, CREW FOUND ALL PASSENGER OXYGEN MASKS DEPLOYED. AIRCRAFT STAY ED AT GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET OXYGEN SYSTEM AND RE-STOWED ALL PASSENGER OXYGEN M ASKS. OPS CHECK OK. AIRCRAFT WAS RELASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200592 19990702 00592 EA 1999 7 2 VTZA990062 1 19990503 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 EA PASSENGER DOOR ILLUMINATED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 635BR 635BR IAD/AVP - FLT 7738 - DURING CRUISE AT 2,255 HRS ON 5-3-99, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WA RNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RECYCLED PASSEN GER DOOR THREE TIMES, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999070200593 19990702 00593 NM 1999 7 2 W7NR9900004 1 19990515 A 5330 SKIN BOEING 737 7372Y5 1384554 NM FUSELAGE DAMAGED A W7NA K NONE C F.O.D. NR NOT REPORTED 1 NM 07 921WA 23039 SMF - AFTER BLOCK-IN, A BELT LOADER IMPACTED THE AIRCRAFT BENEATH THE FOWARD BAGGAGE DOOR. GROUND PERSONNEL DID NOT CHO CK THE BELT LOADER AFTER PULLING UP NEXT TO THE AIRCRAFT. WHILE OFF-LOADING BAGGAGE, PARKING BRAKE SLIPPED OFF AND THE LOADER MOVED FORWARD HITTING THE FUSELAGE BENEATH THE FORWARD CARGO DOOR CAUSING TWO DENTS. ONE ABOUT 12 INCHES LONG, A ND THE OTHER APPROXIMATELY 18 INCHES LONG. AIRCRAFT FERRIED TO TUCSON AND REPAIRED BY HAMILTON AVIATION PER BOEING SRM' S 53-30-3 AND 51-30-2. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4U RT A16WE 1999070200594 19990702 00594 NM 1999 7 2 W7NR9900003 1 19990413 A 2612 896768 FIRE LOOP BOEING 737 7372Y5 1384554 NM APU CRUSHED A W7NA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 NM 07 921WA 21 23039 LGB - FLT 717 - ON CLIMB-OUT, CREW TURNED THE APU OFF AND THE FIRE WARNING SYSTEM ACTIVATED. CREW PULLED THE APU FIRE H ANDLE, DISCHARGED THE BOTTLE, AND WENT TO THE OFF POSITION ON THE START SWITCH. AIRCRAFT RETURNED TO LGB AND LANDED WIT HOUT INCIDENT. FOUND FIRE LOOP CRUSHED IN THE APU SHROUD. NO INDICATION OF FIRE OR OVERHEAT CONDITIONS. REPLACED THE APU FIRE BOTTLE AND THE FIRE ELEMENT. SYSTEM CHECK GOOD, AND AIRCRAFT RETURNED TO SERVICE. PART TC: 22. (X) 2 L 7 2 4U RT A16WE 1999070200595 19990702 00595 NM 1999 7 2 99ZZZX2505 1 19990517 A 3220 MECHANISM BOEING 737 7373U3 13844CC NM NLG WORN A P9OA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 360PR 28742 ON TAXI NOTED A CLUNKING SOUND COMING FROM NLG AREA WITH LESS THAN 8,000 POUNDS OF FUEL ONBOARD. ACFT HAS TOTAL OF 1,3 03 HRS FLIGHT TIME. INSP AND TEARDOWN OF UPPER AND LOWER DRAG LINK TRUNNION BEARINGS AND PINS, SHOCK STRUT TRUNNION BEA RINGS AND PINS, FOUND DAMAGE AND PREMATURE WEAR ON DRAG LINK TRUNNION PINS LT AND RT AND BEARINGS. WASHERS ON PINS CRAC KED, LT AND RT. DAMAGE IN THIS LOCATION CONSISTED OF CIRCUMFERENTIAL GOUGES AND WEAR NEAR OTBD SIDE OF PINS AND BEARING S. DAMAGE NOTED AT UPPER AND LOWER BEARING. NOTED SHOCK STRUT TRUNNION PIN JAM NUTS, LT AND RT, WERE SAFETIED, BUT NEV ER TORQUED. NUTS WERE FOUND HAND TIGHT. ALL PARTS REPLACED. 2 L 7 2 4F RT A16WE 1999070200596 19990702 00596 NM 1999 7 2 CALA9900459 1 19990430 A 5315 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 370 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17306 23357 HOU - CABIN SEAT TRACK LEFT OUTBOARD CORRODED AT STA 370. FABRICATED AND INSTALLED SEAT TRACK PER SRM 53-00-52. (X) 2 L 7 2 4F RT A16WE 1999070200597 19990702 00597 WP 1999 7 2 CALA9900455 1 19990503 A 5400 ANGLE DOUG DC10 DC1030 3023501 WP NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 MAN - SUSPECT CRACK RIGHT DRAG ANGLE REPAIR PLATE AT LOWER END OF FIRST BANJO FITTING. AFTER NDT INSPECTION, CRACK CONF IRMED (1 INCH). CRACK STOP-DRILLED PER SRM 55-20-00, FIG 3. REPAIR PLATE REMOVED AND REPLACED PER SRM 55-20-00 FIG 3. (X) 2 L 7 3 4F A22WE 1999070200598 19990702 00598 WP 1999 7 2 CALA9900456 1 19990503 A 5400 ANGLE DOUG DC10 DC1030 3023501 WP NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 MAN - RIGHT HAND DRAG ANGLE AT LOWER END OF THIRD BANJO FITTING. SUBMITTER SUSPECTED CRACK. AFTER NDT, CRACK CONFIRMED (1 INCH). STOP-DRILLED CRACK PER SRM 55-20-00. REPAIR ANGLE MANUFACTURED, HEAT TREATED, AND FITTED PER SRM 55-20-00 F IG 3. (X) 2 L 7 3 4F A22WE 1999070200599 19990702 00599 WP 1999 7 2 CALA9900457 1 19990503 A 5400 ANGLE DOUG DC10 DC1030 3023501 WP NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 MAN - SUSPECT CRACK LT DRAG ANGLE AT LOWER END OF THIRD BANJO FITTING. AFTER NDT INSPECTION, CRACK CONFIRMED (1 INCH). CRACK STOP-DRILLED PER SRM 55-20-00. REPAIR PLATE MANUFACTURED, HEAT TREATED, AND FITTED PER SRM 55-20-00, FIG 3. (X) 2 L 7 3 4F A22WE 1999070200600 19990702 00600 NM 1999 7 2 HNAA9900082 1 19990611 A 5413 85410734102 STRINGER DHC DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 053 NR 2 NAC OUTBOARD STRINGER IS CRACKED IN TWO PLACES AT THE REPAIR. REMOVED AND REPLACED STRINGER. 2 H 7 2 4T RT A13NM 1999070200601 19990702 00601 NM 1999 7 2 HNAA9900083 1 19990611 A 5413 85410734101 STRINGER DHC DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 053 NR 2 NAC INBOARD STRINGER BELOW THE DECK IS CRACKED JUST PRIOR TO PREVIOUS REPAIR. REMOVED AND REPLACED STRINGER. 2 H 7 2 4T RT A13NM 1999070200602 19990702 00602 NM 1999 7 2 HNAA9900084 1 19990611 A 5413 85410733103 STIFFENER DHC DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 053 NR 2 NAC AFT STIFFENER IS CRACKED. REMOVED AND REPLACED STIFFENER. 2 H 7 2 4T RT A13NM 1999070200603 19990702 00603 NM 1999 7 2 HNAA9900085 1 19990611 A 5720 85300011117 ANGLE DHC DHAV DHC8 DHC8102 2809003 NM CENTER WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 053 AFT LEFT CLOSING ANGLE IS CRACKED. REMOVED AND REPLACED CLOSING ANGLE. 2 H 7 2 4T RT A13NM 1999070200604 19990702 00604 NM 1999 7 2 AT9900472 1 19990627 A 3230 A4200602835 SOLENOID BOEING 737 7372T4 1384492 NM LANDING GEAR DEFECTIVE A ZZDA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 15 467AT 22055 GEAR HANDLE WILL NOT RETRACT PAST OFF POSITION. LEVER LATCH CIRCUIT BREAKER REPEATED POPPED WHEN GEAR LEVER WAS CYCLED. DUMPED FUEL, RETURNED TO ATLANTA. REPLACED LEVER LATCH SOLENOID, OPS CHECKED NORMAL IAW MM 32-31-31. 2 L 7 2 4F A16WE 1999070200605 19990702 00605 WP 1999 7 2 AT9900473 1 19990507 A 5320 1A459301 SUBFLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CABIN ENTRY SUBFLOOR AT BS 160 TO 200 RBL 55 CORRODED. FABRICATED A ND INSTALLED REPAIR IAW DC9 SRM 53-21-0, 51-10-3, 51-10-4 AND 51-30-1. 2 L 7 2 4F A6WE 1999070200606 19990702 00606 WP 1999 7 2 AT9900474 1 19990623 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION AT BS 996 ON NR 1 THRUST REVERSER GROUND ACCESS PANEL INTE RNAL DOUBLER. REMOVED CORRODED INTERNAL DOUBLER, CUT, DRILLED, TRIMMED NEW DOUBLER, ALODINED AND PRIMED IAW DC9 SRM 51- 10-4, 51-30-2, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999070200607 19990702 00607 WP 1999 7 2 AT9900475 1 19990624 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 503 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND SKIN BULGING AT BS 503 L-30 ANTENNA COVER PLATE AREA. REMOVED CORRO DED FINGER DOUBLER, FABRICATED AND INSTALLED A NEW ONE IAW DC9 SRM 53-04-0, 51-10-2, 51-10-4, 51-10-3, 51-30-2 AND 51-20 -0. 2 L 7 2 4F A6WE 1999070200608 19990702 00608 WP 1999 7 2 AT9900476 1 19990605 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 240 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND FLOOR SUPPORT AT BS 240 BL-0 CORRODED. CUT OUT AND REMOVED EXISTING FLOOR SUPPORT, FABRICATED REPAIR SUPPORT AND REPAIR ANGLES IAW DC9 SRM 53-11-2 FIG 4, 53-10-1 FIG 22 AND TIMCO EO NR 99 -1162. 2 L 7 2 4F A6WE 1999070200609 19990702 00609 WP 1999 7 2 AT9900477 1 19990613 A 5720 49137471 BRACKET DOUG DC9 DC932 3022066 WP WS 398 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND PULLEY BRACKET ON LEFT WING REAR SPAR AT XRS 398 CORRODED. REMOVED AND REPLACED PULLEY BRACKET, RETENSION TRIM CABLES AND TRAVEL CHECK GOOD IAW DC9 MM 27-10-0. 2 L 7 2 4F A6WE 1999070200610 19990702 00610 WP 1999 7 2 AT9900478 1 19990608 A 5320 2644290515 BRACKET DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND INBOARD AND OUTBOARD PULLEY SUPPORT BRACKET AT BS 965 CORRODED. REMO VED AND REPLACED PULLEY SUPPORT, ADJUST HORIZONTAL TRIM INDICATION SYSTEM AND OPS CHECKED GOOD IAW DC9 MM 27-40-0. 2 L 7 2 4F A6WE 1999070200611 19990702 00611 WP 1999 7 2 AT9900479 1 19990509 A 5414 995821817 PANEL DOUG DC9 DC932 3022066 WP LT PYLON CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT PYLON PANEL NR 8103 CORRODED AROUND CAMLOCKS AND BACK SIDE OF THE PANEL. MECHANICALLY REMOVED CORROSION FROM PANEL, FOUND PANEL BEYOND REPAIR. ORDERED NEW PANEL IAW DC9 SRM 51-1 0-3, AND 54-02 FIG 3. 2 L 7 2 4F A6WE 1999070200612 19990702 00612 WP 1999 7 2 AT9900480 1 19990514 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 870-889 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION AT LONGERON 10R, J ANGLE FRAME TIE BRACKET AND WEBBING FRO M BS 870 TO 889. REMOVED ANGLE, CUT OUT DAMAGE AREA, FABRICATED DOUBLERS AND FILLER, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 53-01 FIG 2, AND 51-10-2. 2 L 7 2 4F A6WE 1999070200613 19990702 00613 EU 1999 7 2 MALA976508 1 19990624 A 2421 31342001 GENERATOR SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A E UNSCHED LANDING ENGINE SHUTDOWN J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 15 454XJ 454 ON CLIMB OUT LT AC GEN LIGHT ILLUMINATED, PERFORMED QRH, SAME RESULTS. UPON RETURN TO MSP NOTICED ENGINE SURGES UNABLE TO GIVE PARAMETERS. F/A NOTICED SMOKE FROM THE EXHAUST, NOTIFIED CREW AND THE ENGINE WAS SHUT DOWN. MAINTENANCE REPLAC ED AC GEN AND V-BAND CLAMP IAW SAAB TASK CARD 24212. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999070200614 19990702 00614 EU 1999 7 2 MALA976509 1 19990625 A 3350 LIGHT SAAB SF340 340B 7860101 EU ROW 3-6 INOPERATIVE A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 430XJ 430 EMERGENCY LIGHT FLOOR STRIP IN THE CABIN IS SEPARATING FROM THE FLOOR, ROW 3 THRU ROW 6. MAINTENANCE RESECURED EMERGENC Y LIGHTING STRIP AS REQUIRED. ALL CHECKS GOOD IAW SAAB AMM CH 33. 2 L 7 2 4T RT A52EU 1999070200615 19990702 00615 EU 1999 7 2 MALA976510 1 19990624 A 2150 MOTOR SAAB SF340 340B 7860101 EU AIR COND SYS FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 424XJ 424 CREWS REPORTED SMOKE IN CABIN 12 MINUTES AFTER SHUTDOWN, SMOKE APPEARED NEAR FLOOR. MAINTENANCE RAN ALL AIRCRAFT SYSTEM S, FOUND SUPPLEMENTAL AIR CONDITION INOP, PULLED CENTER AISLE FLOOR BOARDS. APPEARS SUPPLEMENTAL AIR CONDITIONER MOTOR HAS BURNT SMELL. MAINTENANCE DEFERRED SUPPLEMENTAL AIR CONDITIONER IAW MEL 25-60-5-12. 2 L 7 2 4T RT A52EU 1999070200616 19990702 00616 NM 1999 7 2 RAAA99B2048 1 19990628 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 15 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 15 PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999070200617 19990702 00617 SO 1999 7 2 RAAA99E9023 1 19990627 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 303 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SERVICE CHECK FOUND FUSELAGE SKIN DENTED AND DEEP GOUGE AT FS 303 BETWEEN STRINGERS 49 AND 50 LEFT HAND. SKIN DA MAGE CUT OUT FROM FS 302.5 TO 304 X 1 HEIGHT BETWEEN STRINGERS 49 AND 50 AND INSTALLED AN EXTERNAL DOUBLER IAW SRM 53-2- 1 FIGURE 2 SHEET 3. 2 L 7 4 4T 4A22 1999070200618 19990702 00618 WP 1999 7 2 CALA9900748 1 19990629 A 3260 INDICATION DOUG DC9 DC982 3022082 WP LANDING GEAR MALFUNCTIONED A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 98876 49444 THREE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING ROC. CYCLING THE GEAR WAS NO HELP. T HE AIRCRAFT WAS RETURNED TO ROC WHERE IT LANDED WITHOUT INCIDENT. THE GEAR WAS SWUNG SEVERAL TIMES AND THE PROBLEM COUL D NOT BE DUPLICATED. AN ADJUSTMENT/TEST WAS PERFORMED ON THE GEAR INDICATION IAW MM 32-60-00 AND ALL CHECKED GOOD. 2 L 7 2 4F A6WE 1999070200619 19990702 00619 NM 1999 7 2 CALA9900749 1 19990629 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 346 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 346 FROM RBL 15 TO LEFT SIDEWALL. THE CORRODED SECTION OF FLOORBEAM WA S REMOVED. A NEW SECTION OF FLOORBEAM AND SPLICE WERE INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999070200620 19990702 00620 NM 1999 7 2 CALA9900750 1 19990629 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 328. THE UPPER SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 5 3-10-51. 2 L 7 2 4F RT A16WE 1999070200621 19990702 00621 NM 1999 7 2 CALA9900751 1 19990629 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 914-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND L-2 PASSENGER DOOR THRESHOLD Z-ANGLE CORRODED FROM STA 914 TO 1006. THE ANGLE WAS REMOVED AND A NEW AN GLE WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999070200622 19990702 00622 WP 1999 7 2 CALA9900752 1 19990630 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1884 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND FLOORBOARD SUPPORTS AT STA 1884 CORRODED. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-42-00 AND GMM 1 0-900-01. 2 L 7 3 4F A22WE 1999070200623 19990702 00623 WP 1999 7 2 CALA9900753 1 19990630 A 5320 SUPPORT BEAM DOUG DC10 DC1030 3023501 WP LAVATORY E CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND LAV E INBOARD SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-42-00 AND GMM 10-900- 01. 2 L 7 3 4F A22WE 1999070200624 19990702 00624 WP 1999 7 2 CALA9900754 1 19990630 A 5320 SUPPORT BEAM DOUG DC10 DC1030 3023501 WP LAVATORY F CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND LAV F OUTBOARD SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-42-00 AND GMM 10-900 -01. 2 L 7 3 4F A22WE 1999070200625 19990702 00625 WP 1999 7 2 CALA9900755 1 19990630 A 5320 SUPPORT BEAM DOUG DC10 DC1030 3023501 WP BS 459 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND FLOOR SUPPORT BEAMS AT STA 459 CORRODED BETWEEN FLOORBOARDS 227CF, 226AF AND 232AF. NEW FLOOR SUPPORT BEAMS WERE INSTALLED IAW SRM 51-42-00 AND GMM 10-900-01. 2 L 7 3 4F A22WE 1999070200626 19990702 00626 WP 1999 7 2 CALA9900756 1 19990630 A 5320 SUPPORT BEAM DOUG DC10 DC1030 3023501 WP LAVATORY F CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND LAV F LATERAL SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-42-00 AND GMM 10-900- 01. 2 L 7 3 4F A22WE 1999070200627 19990702 00627 WP 1999 7 2 CALA9900757 1 19990630 A 5320 SUPPORT BEAM DOUG DC10 DC1030 3023501 WP BS 392-450 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED BETWEEN FLOORBOARDS 227CF AND 226AF AT STA 392 TO 450. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-42-00 AND GMM 10-900-01. 2 L 7 3 4F A22WE 1999070200628 19990702 00628 WP 1999 7 2 CALA9900758 1 19990630 A 5320 SUPPORT BEAM DOUG DC10 DC1030 3023501 WP LAVATORY F CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND LAV F INBOARD SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-42-00 AND GMM 10-900- 01. 2 L 7 3 4F A22WE 1999070200629 19990702 00629 WP 1999 7 2 CALA9900759 1 19990630 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1851 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND FRAME CORRODED IN LOWER LOBE AFT CARGO BILGE AREA AT STA 1851 BETWEEN STRINGER 51L AND 51R WITH CORROSI ON ON STRINGERS 52L AND 51L. THE CORRODED AREA ON FRAME WAS CLEANED AND TREATED IAW SRM 51-21-00. THE CORRODED SECTION S OF STRINGERS WERE REMOVED. NEW STRINGER SECTIONS WERE INSTALLED IAW SRM 51-33-01 AND 53-10-00, FIGURE 2. 2 L 7 3 4F A22WE 1999070200630 19990702 00630 NM 1999 7 2 CALA9900760 1 19990630 A 5751 65C2591117A SKIN BOEING 737 7373T0 1384582 NM LT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND UPPER SURFACE OUTBOARD MID AREA OF LT AILERON DELAMINATED. THE AILERON WAS REPAIRED IAW ECRA 5761-0101 7. 2 L 7 2 4F RT A16WE 1999070200631 19990702 00631 WP 1999 7 2 9902249763 1 19990626 A 3350 BATTERY DOUG DC9 DC941 302207N WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 763NW 47396 DURING LINE CHECK, FOUND AFT STAIRWAY AND TAIL CONE EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999070200632 19990702 00632 WP 1999 7 2 9902259156 1 19990629 A 3350 BATTERY DOUG DC9 DC914 3022034 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8915E 45832 DURING LINE CHECK, FOUND CATWALK AND TAIL CONE EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN P OWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999070200633 19990702 00633 EU 1999 7 2 9902263231 1 19990627 A 2913 4205400 PUMP AIRBUS 320 A320211 3930320 EU NR 2 ENGINE FAILED A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 331NW 19934 19934 318 DURING CLIMBOUT FROM LAX, RECEIVED HYD Y ENG PUMP LOW PR MESSAGE. PLACED THE NR 2 ENGINE DRIVEN YELLOW HYDRAULIC PUMP O FF AND THE YELLOW SYSTEM ELECTRIC PUMP ON PER COM PROCEDURES. LATER DURING CRUISE, RECEIVED HYD Y RSVR LOW LVL MESSAGE AND PLACED THE YELLOW SYSTEM ELECTRIC PUMP OFF PER COM PROCEDURES. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, FILTERS AND FLUSHED SYSTEM AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999070200634 19990702 00634 NM 1999 7 2 9902272705 1 19990625 A 2910 INTERCONNECT BOEING 727 727225 1384077 NM B HYD SYST LEAKING A NWAA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 802ER 22433 ON CLIMBOUT OF MKE, CREW NOTICED BOTH HYDRAULIC SYSTEM LIGHTS ILLUMINATED. CREW DETERMINED THAT FLUID LOSS WAS IN 'B' S YSTEM AND CLOSED PUMP SWITCHES. FLIGHT LANDED AT DTW WITHOUT INCIDENT. DTW MAINTENANCE FOUND GROUND INNERCONNECT LEAKI NG AND REPLACED SAME. 2 L 7 3 4F A3WE 1999070200635 19990702 00635 NE 1999 7 2 9902289154 2 19990625 A 7510 DUCT DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7B 52053 NE RT ENG ANTI-ICE BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8913E 45830 DURING CLIMBOUT THROUGH 4000 FT, THE RIGHT ENGINE FIRE WARNING SOUNDED. WITH THE POWER REDUCED, THE LOOP AND FIRE HANDL E LIGHTS WENT OUT. NO FURTHER FIRE INDICATIONS WERE NOTED. FLIGHT CREW DECLARED A YELLOW EMERGENCY, RETURNED TO BTR, A ND LANDED WITHOUT INCIDENT. OVERWEIGHT LANDING WAS MADE AT 83,200 LBS. MAINTENANCE REPLACED A BROKEN NOW COWL ANTI-ICE DUCT, RIGHT ENGINE AND ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1999070200636 19990702 00636 WP 1999 7 2 ABXA9900550 1 19990630 A 5330 2779661 SKIN DOUG DOUG DC8 DC863F 302198F WP BS 1094 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 LOWER EDGE OF LEFT CENTER SERVICE DOOR CORRODED FROM STATION 1094 INTO STATION 1109. REPAIRED IAW ABX REA B831-28121MR. 2 L 7 4 4F 4A25 1999070200637 19990702 00637 WP 1999 7 2 ABXA9900551 1 19990630 A 3210 BOSS DOUG DOUG DC8 DC863F 302198F WP RT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 46126 LEFT AND RIGHT MAIN GEAR RETRACT PIN BOSSES WERE CORRODED. REPAIRED IAW ABX REA B832-28106MR. 2 L 7 4 4F 4A25 1999070200638 19990702 00638 WP 1999 7 2 ABXA9900552 1 19990628 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND LONGERON 16 LEFT CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999070200639 19990702 00639 WP 1999 7 2 ABXA9900553 1 19990628 A 5313 591140617N LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND LONGERON 4 LEFT CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999070200640 19990702 00640 WP 1999 7 2 ABXA9900554 1 19990628 A 5744 9919475501 FITTING DOUG DOUG DC9 DC932 3022066 WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND LEFT WING SPOILER OUTBOARD ATTACH FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-3 0-5. 2 L 7 2 4F A6WE 1999070200641 19990702 00641 WP 1999 7 2 ABXA9900555 1 19990628 A 5400 591326245N ANGLE DOUG DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND NR 1 PYLON LEFT LOWER ATTACH ANGLE CRACKED AT STATION 990. REPAIRED ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1999070200642 19990702 00642 WP 1999 7 2 ABXA9900556 1 19990628 A 5320 991075527 ANGLE DOUG DOUG DC9 DC932 3022066 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND CUSP WEB ANGLE CLIP CRACKED AT LONGERON 18 LEFT AND STATION 996. REPLACED CUSP WEB ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999070200643 19990702 00643 WP 1999 7 2 ABXA9900557 1 19990628 A 5320 99573925 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 14 LEFT AND 16 LEFT. REPLACED SH EAR TIE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999070200644 19990702 00644 WP 1999 7 2 ABXA9900558 1 19990624 A 5730 5912156193 PANEL DOUG DOUG DC9 DC931 3022065 WP WS 111.5 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK, FOUND LEFT WING UPPER TRAILING EDGE PANEL AT STATION XRS 111.500. REPLACED PANEL IAW DC9 SRM 51-30-1 AN D 51-10-4. 2 L 7 2 4F A6WE 1999070200645 19990702 00645 NM 1999 7 2 P5CA9900627 1 19990629 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM BS 400 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FOUND SHEARED RIVETS AT BS 400 ON FLOORBEAM LEFT SIDE. REPLACED RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999070200646 19990702 00646 NM 1999 7 2 P5CA9900628 1 19990629 A 5320 CLIPS BOEING 747 747249F 1384849 NM BS 340 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FOUND CRACKS ON CLIPS AT NOSE WHEEL WELL VERTICAL BEAM WEB AT BS 340 R. REPLACED CLIPS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999070200647 19990702 00647 NM 1999 7 2 P5CA9900629 1 19990629 A 5312 BULKHEAD FLANGE BOEING 747 747249F 1384849 NM BS 140 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FOUND CRACK ON FLANGE OF PRESSURE BULKHEAD AT BS 140 WL 280 BL 10L. TRIMMED DAMAGED AREA AND FABRICATED NEW ANGLE PER S RM 51-40-03 AND 51-10-02. 2 L 7 4 4F A20WE 1999070200648 19990702 00648 NM 1999 7 2 P5CA9900630 1 19990629 A 5312 BULKHEAD BOEING 747 747249F 1384849 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 CRACKS FOUND ON BS 1000 IN THE RADIUS BETWEEN STR 46 AND 47 LEFT AND RIGHT SIDES. STOP DRILLED, EDDY CURRENT PER SB 530 -2316R1 AND SRM 51-10-01 FIG 2. 2 L 7 4 4F A20WE 1999070200649 19990702 00649 NM 1999 7 2 P5CA9900631 1 19990629 A 5320 VERTICAL BEAM BOEING 747 747249F 1384849 NM BS 320 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FOUND INDICATION OF CRACKS AT HOLE ON VERTICAL BEAM AT BS 30L. STOP DRILLED AND FABRICATED REPAIR PER SRM 53-10-04 FIG 94 PG 8 DETAIL 5. 2 L 7 4 4F A20WE 1999070200650 19990702 00650 NM 1999 7 2 P5CA9900632 1 19990629 A 5320 ANGLE BOEING 747 747249F 1384849 NM BS 434 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FOUND 1.6 INCH CRACK ON RADIUS OF ANGLE FWD OF BS 434 UNDER STR 26. FABRICATED PARTS AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1999070200651 19990702 00651 NM 1999 7 2 P5CA9900633 1 19990629 A 5320 WEB BOEING 747 747249F 1384849 NM BS 434 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FOUND WEB CRACKED AT BS 434L NR 1 MED. TRIMMED AREA AND FABRICATED PART FOR REPAIR PER SRM 53-10-04 AND 51-30-02. 2 L 7 4 4F A20WE 1999070900002 19990709 00002 CE 1999 7 9 99ZZZX2507 1 19990616 A 2910 510011199 LINE CESSNA 402 402C 207590R CE HYDRUALIC SYSTEM CRACKED A GNBA O OTHER O OTHER NR NOT REPORTED 1 SW 01 57PB 15072 402C0300 DURING A RETURN FLIGHT, LEFT AND RIGHT HYDRAULIC FLOW LIGHTS BEGAN TO FLICKER ON AND OFF. CYCLED GEAR DOWN AND MADE AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL FOUND HYDRAULIC RESERVOIR EMPTY. PERFORMED HYDRAULIC PRESSURE CHECK AND FOUN D L-H PRESSURE LINE, FROM THE FLOW SWITCH TO ELBOW, CRACKED IN THE BEND OF THE RADIUS. REPLACED WITH SERVICEABLE LINE. PRESSURE CHECKED AND CYCLED GEAR WITH NO FURTHER LEAKS NOTED. 1 L 7 2 3O A7CE 1999070900007 19990709 00007 SO 1999 7 9 99ZZZX2512 2 19990603 A 8500 ENGINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RIGHT FAILED A HYIA O OTHER O OTHER CR CRUISE 1 NE 01 818AN 522 402C0501 816014R IN CRUISE FLIGHT, RIGHT ENGINE HAD A CATASTROPHIC FAILURE. FOR UKNOWN REASONS, CONNECTING RODS, NR 1, NR 2, NR 4, FAILE D. TCM HAS BEEN NOTIFIED AND WILL INSPECT ASAP. AN UNEVENTFUL LANDING WAS MADE. 1 L 7 2 3O 3 O A7CE E8CE 1999070900008 19990709 00008 1999 7 9 99ZZZX2513 4 19990604 A 3400 ANTENNA BEECH 99 99 1154002 CE NAVIGATION MALFUNCTIONED A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 199GL U15 PILOTS REPORTED VERY WEAK NAVIGATION RECEPTION, EVEN AFTER NUMEROUS CHECKS FROM AVIONICS SHOP EQUIPMENT. A DIFFERENT S ET OF ANTENNAS WERE INSTALLED, BUT DID NOT RESOLVE PROBLEM. ONLY AFTER A NEW SET OF ANTENNAS WERE INSTALLED, DID THE PR OBLEM DISAPPEAR. 1 L 7 2 3T A14CE 1999070900011 19990709 00011 CE 1999 7 9 99ZZZX2516 1 19990607 A 3252 508200208 ROD BEECH 99 B99 1154004 CE SHIMMY DAMPENER CORRODED A TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 899CA U104 SHIMMY DAMPENER ROD WAS FOUND TO HAVE CORROSION INSIDE AND OUT CAUSING FLUID TO LEAK BY THE O-RINGS. CORROSION SEEMS TO BE FROM NORMAL OPERATION. ROD WAS REPLACED. 1 L 7 2 3T A14CE 1999070900015 19990709 00015 NE 1999 7 9 SI3R99013 2 19990410 A 7210 7757652 BEARING 5074T51G10 SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE GEARBOX BROKEN B SI3R K NONE O OTHER IN INSP/MAINT 1 NE 03 6798 TBC00261 GEE785250 DURING DISASSEMBLY OF GEARBOX, SLIDER BLOCK BEARING AND RIGHT IDLER FORWARD TAB WASHER WERE FOUND BROKEN. REF: HSS SO NR 251975 SO CUSTOM: MESBA A/L. 2 L 7 2 4T 4 T RT A52EU E8NE 1999070900141 19990709 00141 WP 1999 7 9 TWAA9909102 1 19990513 A 5511 SPAR DOUG DC9 DC931 3022065 WP HORIZ STAB CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK FOUND THE HORIZONTAL STABILIZER UPPER SPAR CAP BARREL NUT HOLE, RIGHT SIDE AFT, THE HOLE WAS CO RRODED. REPAIRED PER ARA 16167. 2 L 7 2 4F A6WE 1999070900142 19990709 00142 WP 1999 7 9 TWAA9909103 1 19990513 A 5511 SPAR DOUG DC9 DC931 3022065 WP HORIZ STAB CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK FOUND THE HORIZONTAL STABILIZER UPPER SPAR CAP BARREL NUT LEFT SIDE AFT HOLE WAS CORRODED. REP AIRED PER ARA 16167. 2 L 7 2 4F A6WE 1999070900143 19990709 00143 WP 1999 7 9 TWAA9909104 1 19990621 A 5230 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 DURING OP 16 MAINT CHECK FOUND THE MID CARGO DOOR WITH A CRACKED FITTING INSIDE THE CUTOUT, FORWARD OF THE AFT HINGE ARM . REMOVED AND REPLACED THE FITTING PER SRM 6-70-01. 2 L 7 2 4F A6WE 1999070900144 19990709 00144 WP 1999 7 9 TWAA9909105 1 19990618 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 223 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 DURING OP 16 MAINT CHECK FOUND A BLIND FASTENER REPAIR AT STA 223, LONGERON 18L. REMOVED THE REPAIR AND CUT OUT DAMAGED SKIN. REPAIRED PER SRM 53-10-107, FIG 201 PAGES 201 AND 202. 2 L 7 2 4F A6WE 1999070900145 19990709 00145 WP 1999 7 9 TWAA9909106 1 19990621 A 5280 SKIN DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 958U 49703 DURING CHECK-C MAINT THE LEFT MAIN GEAR DOOR HAD A STRESS CRACK IN THE SKIN ABOVE THE BUMPER AND AFT OF THE FORWARD EDGE OF THE DOOR. REPLACED THE CRACKED SKIN WITH SAME TYPE MATERIAL AS REMOVED AND INSTALLED FASTENERS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1999070900146 19990709 00146 WP 1999 7 9 TWAA9909107 1 19990621 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 958U 49703 DURING CHECK-C MAINT THE AFT CARGO COMPARTMENT LOWER DOOR JAMB AREA HAD CORROSION AROUND SCREW HOLES. REMOVED CORROSION PER SRM 51-10-3 AND 53-05 FIG 63. 2 L 7 2 4F A6WE 1999070900147 19990709 00147 WP 1999 7 9 TWAA9909108 1 19990621 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 958U 49703 DURING CHECK-C MAINT THE AFT CARGO COMPARTMENT LOWER DOOR THRESHOLD AREA HAD CORROSION AROUND THE RIVETS AND OUTBOARD FL ANGE. REMOVED CORROSION PER STANDARD PROCESSES MANUAL 6-80-01 AND TREATED PER SRM 53-05, FIG 63. 2 L 7 2 4F A6WE 1999070900148 19990709 00148 NM 1999 7 9 HNAA9900086 1 19990619 A 5320 85331432101 LINK DHC DHAV DHC8 DHC8102 2809003 NM BS 545 CRACKED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 914HA 053 053 LINK SUPPORTING RT CHANNEL AND LWR CHANNEL TOGETHER AT STA X545.0 IS CRACKED. REMOVED AND REPLACED LINK. 2 H 7 2 4T RT A13NM 1999070900149 19990709 00149 NM 1999 7 9 HNAA9900087 1 19990618 A 5313 CVR115 STRINGER DHC DHAV DHC8 DHC8102 2809003 NM BS 504 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 053 STRINGER 25S HAS CORROSION AND PITTING AT X504, REMOVAL OF THE RIVET REQUIRED. REMOVED RIVET AT LOCATION, EVALUATED AND BLENDED CORROSION FOUND AREA OUT OF LIMITS APPROX .013. BLENDED AND REMOVED ALL CORROSION, INSTALLED NESTED ANGLE AS S AME TYPE AS STRINGER TO EXTEND 4 FASTENERS EITHER SIDE OF THE DAMAGE AREA. ALODINED, PRIMED AND PAINTED AREA. 2 H 7 2 4T RT A13NM 1999070900150 19990709 00150 NM 1999 7 9 HNAA9900088 1 19990615 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 190 DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 DENT AT STRINGER 23S AT X190 TOTAL DENT IS APPROX 1.5 DIA .025. DEEP PERFORMED HFEC, NO CRACKS DETECTED. DISPOSITION Y ELLOW DOT. 2 H 7 2 4T RT A13NM 1999070900151 19990709 00151 NM 1999 7 9 HNAA9900089 1 19990610 A 5413 85410733103 STRINGER DHC DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 053 NR 1 NAC AFT STRINGER IS CRACKED. REMOVED AND REPLACED AFT STRINGER. 2 H 7 2 4T RT A13NM 1999070900152 19990709 00152 NM 1999 7 9 HNAA9900090 1 19990629 A 5755 SKIN DHAV DHC8 DHC8102 2809003 NM SPOILER DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 053 DENT ON OUTBOARD ROLL SPOILER INBOARD OF CENTER HINGE. EDGE DISTANCE TO FWD FASTENER .625 OUT OF LIMITS OF RTD8-27-014. DENT IS ON UPPER SKIN. COMPLIED WITH EO 8-53-99-240. MARKED DENT WITH YELLOW DOT. 2 H 7 2 4T RT A13NM 1999070900153 19990709 00153 NM 1999 7 9 HNAA9900091 1 19990629 A 5755 SKIN DHAV DHC8 DHC8102 2809003 NM SPOILER DENTED A HNAA O OTHER O OTHER IN INSP/MAINT 1 EA 07 914HA 053 DENT ON INBOARD GROUND SPOILER UPPER SKIN AT INBOARD END. EXCEEDS MAX, CHORDWISE DIMENSION A OF RD8-27-014. COMPLIED W ITH EO 8-53-99-240. MARKED DENT WITH YELLOW DOT. 2 H 7 2 4T RT A13NM 1999070900154 19990709 00154 SO 1999 7 9 COMA9910102 1 19990629 A 7332 1103P1892 PRESSURE SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 256CA 8094 120245 LEFT ENGINE LOW FUEL PRESSURE WARNING. REPLACED THE LOW PRESSURE SWITCH. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900155 19990709 00155 SO 1999 7 9 COMA9910103 1 19990628 A 7603 CIRCUIT BREAKER EMB 120 EMB120RT SO PWA 118 PW118 NE FLIGHT IDLE SYS TRIPPED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 261CA 120254 THE FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKERS ARE TRIPPED. RESET BREAKERS AND FUNCTION CHECK OF SYSTEM NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900156 19990709 00156 EA 1999 7 9 COMA9960322 1 19990630 A 5320 601R3867325 SUPPORT CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 FLOOR SUPPORT PLATES (P/N 601R38673-25) FS 349 BETWEEN RBL AND RT FUSELAGE SKIN AND (P/N 601R38673-17) BETWEEN LBL 27 AN D LT FUSELAGE SKIN WERE DISCOVERED TO HAVE CORROSION BEYOND LIMITS AS SPECIFIED IN CANADAIR REO 601R53-00-005. REPLACED CORRODED FLOOR SUPPORT PLATES WITH NEW FLOOR SUPPORT PLATES IAW WVAC EO 601R-53-0079A. 2 L 7 2 4F RT A21EA 1999070900157 19990709 00157 EA 1999 7 9 COMA9960323 1 19990630 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 319-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 FLOOR SUPPORT BEAMS RBL 27, RBL 9, LBL 9 AND LBL 27 IN AREAS BETWEEN FS 319 AND FS 349 WERE DISCOVERED TO HAVE CORROSION BEYOND LIMITS AS SPECIFIED IN CANADAIR REO 601R53-00-0005. REMOVED AND REPLACED CORRODED SECTIONS OF FLOORBEAMS RBL 9 AND RBL 27 (BETWEEN FS 280 AND FS 355) AND LBL 27 (BETWEEN FS 310 AND FS 355) IAW CANADAIR REO 601R53-00-027. REPAIRED FLOOR SUPPORT BEAM LBL 9 FS 325 IAW WVAC EO 601R-53-0083A. 2 L 7 2 4F RT A21EA 1999070900158 19990709 00158 EA 1999 7 9 COMA9960324 1 19990630 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 SERVICE DOOR ANGLE, (P/N 601R38303-105) BELOW THRESHOLD PLATE DISCOVERED CORRODED. REPLACED ANGLE IAW WVAC EO 601R-53-0 077. 2 L 7 2 4F RT A21EA 1999070900159 19990709 00159 EA 1999 7 9 COMA9960325 1 19990630 A 5320 6003401717 SUPPORT CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 FLOOR SUPPORT MEMBER, (P/N 60034017-17) FS 280 OUTBOARD OF RBL 9 DISCOVERED WITH 2 INCH CRACK ON BOTTOM SIDE. REPAIRED FLOOR SUPPORT MEMBER FS 280 IAW WVAC EO 601R-53-0090A. 2 L 7 2 4F RT A21EA 1999070900160 19990709 00160 EA 1999 7 9 COMA9960326 1 19990629 A 5270 WARNING CNDAIR CL600 CL6002B19 EA CABIN DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 929CA 7035 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. NO DEFECTS FOUND WITH CABIN DOOR. 2 L 7 2 4F RT A21EA 1999070900161 19990709 00161 EA 1999 7 9 COMA9960327 1 19990630 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT BIRD STRIKE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 SO 01 958CA 7111 BIRD STRIKE DURING TAKEOFF. C/W BIRD STRIKE INSPECTION, NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 1999070900162 19990709 00162 NM 1999 7 9 UPS99228572 1 19990130 A 5312 BULKHEAD BOEING 727 72725C 138400H NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:N/A, 2 X 3 INCH CRACK IN PRESSURE BULKHEAD STA 870, LEFT WHEEL WELL FACING FORWARD. *S/D* REMOVED 4 X 8 INCH SECTION IAW SRM 53-10-1, FABRICATED REPAIR IAW 53-10-9. INSTALLED DOUBLERS, FILLERS AND STRAP IAW 53-10-9. 2 L 7 3 4F A3WE 1999070900163 19990709 00163 NM 1999 7 9 UPS99229787 1 19990513 A 5753 651859928 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C57-581-04.00-04) ON NR 6 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE, INSTALLAT ION ON TC C57-581-04-4D. 2 L 7 3 4F A3WE 1999070900164 19990709 00164 NM 1999 7 9 UPS99229788 1 19990513 A 5753 651859929 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C57-581-04.00-04) ON NR 5 FLAP CARRIAGE AT SPINDLE FWD END. REPLACED CARRIAGE, INSTALLAT ION ON TC C57-581-04-4D. 2 L 7 3 4F A3WE 1999070900165 19990709 00165 NM 1999 7 9 UPS99229789 1 19990513 A 5720 65327332 FITTING BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C57-581-06.00-04) ON NR 7 FLAP TRACK FWD ATTACH WING FITTING. CORROSION OUT OF LIMITS PE R BOEING DWG 65-32733, PART REPLACED WITH NEW ITEM PER SRM 51-30-02 AND DWG 65-17357. 2 L 7 3 4F A3WE 1999070900166 19990709 00166 NM 1999 7 9 UPS99229790 1 19990605 A 5320 BEAM BOEING 727 72725C 138400H NM BS 1110-1150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, AFT CARGO BAY TRANSVERSE BEAM BL 0 WL 200, CORROSION BETWEEN STA 1110 TO 1150 MARKED SDN C53-111-01. 00-03. REMOVED AND REPLACED TRANSVERSE BEAM PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999070900167 19990709 00167 NM 1999 7 9 UPS99229791 1 19990605 A 5320 BEAM BOEING 727 72725C 138400H NM BS 592-596 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:SI, CORROSION (C53-111-01-2B) ON TRANSVERSE BEAM LOWER CHORD STA 592 TO 596 LBL 2 WL 199. REMOVED AND R EPLACED TRANSVERSE BEAM AT BS 592 TO 596 LBL 2 WL 199 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999070900168 19990709 00168 NM 1999 7 9 UPS99229857 1 19990527 A 5751 CASTING BOEING 727 72731C 1384011 NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, RIGHT O/B AILERON LOCKOUT CASTING HAS SURFACE CORROSION AROUND QUADRANT PIVOT BOLT. REPAIR CARRIE D OUT IAW SRM 27-10-2 & 51-30-8. 2 L 7 3 4F A3WE 1999070900169 19990709 00169 NM 1999 7 9 UPS99229867 1 19990528 A 7120 MOUNT BOEING 727 72731C 1384011 NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, PITTING CORROSION IN BORE OF HOLES IN NR 1 ENG FWD MOUNT FITTING. REPAIRED IAW SMRO EO 99-14-011 UPS ENGINEERING FILE NR 727-54-011. 2 L 7 3 4F A3WE 1999070900170 19990709 00170 NM 1999 7 9 UPS99229883 1 19990602 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 219.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, FRAME SUPPORT ANGLE CORRODED AT BONDING WIRE ATTACH POINT BS 219.8 RBL 35. FRAME SUPPORT ANGLE RE PLACED IAW SRM 51-30-2 & SRM 53-10-2. 2 L 7 3 4F A3WE 1999070900171 19990709 00171 NM 1999 7 9 UPS99229986 1 19990625 A 5347 BC15201432 SEAT TRACK BOEING 727 72722C 138400F NM BS 590-605 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C, SEAT TRACK FROM BS 590 TO 605 RBL 25 WL 208 HAS CORROSION IN CHANNEL. AFTER THE CORROSION REMOVAL PR OCESS, FOUND THE AREA TO GO BEYOND ALLOWABLE LIMITS. 2 L 7 3 4F A3WE 1999070900172 19990709 00172 NM 1999 7 9 UPS99229987 1 19990613 A 5711 SPAR CHORD BOEING 727 72731C 1384011 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION WEB BS 870 RBL 70.5 TO LBL 70.5 LWR CHORD, REAR SPAR FOUND CORRODED. REPLACEMENT CHORD INSTALLED IAW SNN MRO EO NR 99-14-015 UPS ENGINEERING FILE NR 727-51-2060. 2 L 7 3 4F A3WE 1999070900173 19990709 00173 NM 1999 7 9 UPS99229989 1 19990613 A 5711 SPAR WEB BOEING 727 72731C 1384011 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION UPPER CHORD REAR SPAR BS 870, WEB FOUND CORRODED RBL 70.5 TO LBL 70.5 . WEB REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060. 2 L 7 3 4F A3WE 1999070900174 19990709 00174 NM 1999 7 9 UPS99229990 1 19990607 A 5711 SPAR BOEING 727 72731C 1384011 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT FLANGE UPPER CHORD REAR SPAR BS 870 CENTER SECTION AT RBL 35 APPROX. UPPER CHORD REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060. 2 L 7 3 4F A3WE 1999070900175 19990709 00175 NM 1999 7 9 UPS99229991 1 19990607 A 5720 STIFFENER BOEING 727 72731C 1384011 NM CENTERWING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT STIFFENER BETWEEN UPPER & LWR WING CENTER SECTION SPAR CHORDS RBL 45. STIFFENER REPLACED IAW DRAWING 65-16202. 2 L 7 3 4F A3WE 1999070900176 19990709 00176 NM 1999 7 9 UPS99229992 1 19990531 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, SURFACE CORROSION ON RT 870 FITTING AT CENTER TANK TORQUE SKIN. REPAIR CARRIED OUT IAW SMRO EO 99 -14-03 UPS ENGINEERING FILE NR 727-57-2064. 2 L 7 3 4F A3WE 1999070900177 19990709 00177 NM 1999 7 9 UPS99229993 1 19990618 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, DURING REPAIR OF FLOORBEAM 560 BETWEEN RBL 45.5 & 62.5 ADDITIONAL CORROSION FOUND AT FLANGE DURING INCORPERATION OF REPAIR ANGLES. FLOORBEAM BS 560 REPAIRED IAW SRMO EO 99-14-012 REV 1 UPS ENGINEERING FILE NR 727-53-2 445. 2 L 7 3 4F A3WE 1999070900178 19990709 00178 NM 1999 7 9 UPS99229994 1 19990527 A 5320 STIFFENER BOEING 727 72731C 1384011 NM RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, CORROSION ON UPPER END OF VERT STIFFENER ATTACHED TO FWD BULKHEAD OF RT WHEEL WELL BBL 40 APPROX. VERTICAL STIFFENER AND NESTING REPLACED IAW DRG NR 65-16330. 2 L 7 3 4F A3WE 1999070900179 19990709 00179 NM 1999 7 9 UPS99229995 1 19990529 A 5320 SEAL BOEING 727 72731C 1384011 NM BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, ON REMOVAL OF VAPOR SEAL AT BS 870 RAMP PLATE AT BS 860 LBL 60 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-40-3. 2 L 7 3 4F A3WE 1999070900180 19990709 00180 NM 1999 7 9 UPS99229996 1 19990601 A 5315 FLOORBEAM BOEING 727 72731C 1384011 NM BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, DURING REPLACEMENT OF LT BS 940 FITTING, FLOORBEAM AT BS 940 LBL 7 0 - LBL 45 LWR CHORD, FOUND COR RODED. FLOORBEAM REPAIRED IAW EO SMRO 99-14-005 UPS ENGINEERING FILE NR 727-53-2134. 2 L 7 3 4F A3WE 1999070900181 19990709 00181 NM 1999 7 9 UPS99229997 1 19990529 A 5730 SKIN BOEING 727 72731C 1384011 NM BS 860 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, CORROSION AROUND FASTENER HEADS WING CENTER SECTION UPPER SKIN BS 860 RBL 60. REPAIRED IAW SMRO E O 99-14-014 UPS ENGINEERING FILE NR 727-57-2065. 2 L 7 3 4F A3WE 1999070900182 19990709 00182 NM 1999 7 9 UPS99229998 1 19990529 A 5730 SKIN BOEING 727 72731C 1384011 NM BS 860 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, CORROSION AROUND FASTENER HEAD WING CENTER SECTION UPPER SKIN BS 860 LBL 60. REPAIRED CARRIED OUT IAW SNN MRO EO 99-14-013 UPS ENGINEERING FILE NR 727-57-2061. 2 L 7 3 4F A3WE 1999070900183 19990709 00183 NM 1999 7 9 UPS99230001 1 19990531 A 7120 CONE BOLT BOEING 727 72731C 1384011 NM NR 2 PYLON GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C7SI, NR 2 PYLON GOUGES ON RT CONE BOLT HOUSING. REPAIRED IAW SMRO EO 99-14-017RI & MM 71-21-11 UPS ENG INEERING FILE NR 727-54-0086. 2 L 7 3 4F A3WE 1999070900184 19990709 00184 NM 1999 7 9 UPS99230004 1 19990615 A 5720 FITTING BOEING 727 72731C 1384011 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C&SI, CRACK INDICATION IN WING CENTER SECTION RT WING TERMINAL FITTING, LWR O/B FASTENER HOLE, BS 870. R EPAIRED IAW SMRO EO 99416RI UPS EO NR B727-5710-11557-A. 2 L 7 3 4F A3WE 1999070900185 19990709 00185 1999 7 9 UPS99529918 4 19990622 A 3416 4039892904 ALTIMETER BOEING 757 75724APF 1384969 NM LT COCKPIT INOPERATIVE A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 458UP 25479 INSPECTION TYPE:N/A, AIR TURNBACK 0705Z. REASON FOR AIR TURNBACK IS INOP CAPTAINS ALTIMETER. INSTALLED BORROWED PART I N SERVICEABLE CONDITION IN CAPTAINS ALTIMETER AS PER M/M 34-13-01. OPS CHECKED GOOD. UPS PART OFF (P/N 4039892-904) (S /N 96073867) BORROWED (P/N 4039892-904) (S/N 043582). 2 L 7 2 4F RT A2NM 1999070900186 19990709 00186 NM 1999 7 9 UPS99529980 1 19990620 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 892 & 895 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 420UP 23907 INSPECTION TYPE:C, MAIN DECK SEAT TRACK ON EXPANSION LINK HAS CORROSION ON TOP SURFACE LT FLANGE LBL 46, BS 892 AND BS 8 95. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED OLD SEAT TRACK AND INSTALLED NEW SEAT TRACK AT EXPANSION LINK BS 880 TO BS 900 IAW SRM 53-30-52, 53-00-52, 51-40-02. 2 L 7 2 4F RT A2NM 1999070900187 19990709 00187 WP 1999 7 9 UPS99829928 1 19990609 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, MAIN CABIN RT SIDE FS 1680 BL 24 THRU 34 FLOORBEAM T-CAP CORRODED ON UNDERSIDE OF NUT PLATE. FAB N EW ANGLE IAW DOUGLAS DWG 5892151, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999070900188 19990709 00188 WP 1999 7 9 UPS99829954 1 19990624 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999070900189 19990709 00189 WP 1999 7 9 UPS99829965 1 19990610 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:C-1, CORROSION EMITTING FROM AROUND AND UNDER NUT PLATES ON BOTTOM SIDE OF FRAME FLANGE AT STA 100 BETWE EN LONG 34R TO 36. REMOVED CORRODED MATERIAL OUT OF LIMITS. REPAIRED WITH FILLER/DOUBLER REPAIR IAW DAC DWG 9753784, 5 3-2-0, 51-1-8, 51-1-21 & 51-1-20D OF DC8 SRM. 2 L 7 4 4F RT 4A25 1999070900190 19990709 00190 WP 1999 7 9 UPS99829974 1 19990626 A 5753 FAIRING DOUG DC8 DC871F 302199D WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 10 INCH CRACK; LEFT INBOARD FLAP SURFBOARD FAIRING D/D 174412. REMOVED AND FABRICATED PLATING AND INSTALLED PLATING PER SRM 57-7-1 PAGE 2. THIS CLEARS DEFFERAL 174412. 2 L 7 4 4F RT 4A25 1999070900191 19990709 00191 NE 1999 7 9 99FDEA00246 2 19990629 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 495FE 21669 99-150 - NR 3 ENGINE OIL TEMP CLIMB TO OFF SCALE HIGH, ENGINE WAS SHUT DOWN PER CK LIST. REPLACED NR 3 ENGINE PER WORK CARD 70T001. 2 L 7 3 4F 4 F A3WE E2EA 1999070900192 19990709 00192 WP 1999 7 9 99FDEA00247 1 19990629 A 3260 UPLOCK TARGET DOUG DC10 DC1010F 3022111 WP RT MLG BENT A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 388FE 46622 RIGHT MLG LIGHT REMAINED ILLUMINATED AT GEAR RETRACT, HYD WERE NORMAL. CYCLE LANDING GEAR PER ABNORMAL PROC. FOUND DOO R PROXIMITY TARGET BENT PER EA 8-3230-46724 C/W EO 8-3260-7-3304 PART 2 ONLY. REMOVED AND REPLACED RIGHT UPLOCK TARGET ASSY. 2 L 7 3 4F A22WE 1999070900193 19990709 00193 WP 1999 7 9 99FDEA00248 1 19990629 A 5350 NKC6122505H TAIL CONE DOUG DC10 DC1030F 3023504 WP AFT FUSELAGE DAMAGED A FDEA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SO 25 303FE 46802 IN FLT HAD LOUD BANG FOLLOWED BY AIRFRAME VIBRATIONS. ON POST FLT PATIO DOORS UNDER NR 2 ENGINE HAD OPENED IN FLT. *S/ D* REMOVED AND REPLACED LT AND RT DROOP ELEVATORS AND TAIL CONE ASSY PER MM 27-30-03-4, MM 53-52-00. REPAIRED TAIL MIS MATCH COVER ON EA 8-5310-35203. 2 L 7 3 4F RT A22WE 1999070900194 19990709 00194 NM 1999 7 9 99UAL900329 1 19990619 A 4920 M83241158 0RING M83241145 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU CUT A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 771UA 26932 P1054 FIFTEEN MINUTES INTO FLIGHT PASSING FL260 FLIGHT ATTENDANT REPORTED SMOKE COMING FROM DOOR 2 RIGHT AREA. ACCOMPLISHED SM OKE EVACUATION CHECKLIST. FLIGHT RETURNED TO GRU. NO SMOKE INDICATIONS IN E & E OR CARGO BAYS. *S/D* APU 3800550-1, SERIAL NUMBER P1054, THE LOAD COMPRESSOR DISASSEMBLY YIELDED THE FOLLOWING RESULTS: BEARING HOUSING HAD EVIDENCE OF OIL STREAKING FROM THE PARTING SURFACE TO THE AIR INLET. BEARING HOUSING O-RING (M8324-1-158) WAS ROLLED AND HAD A SECTION CUT (SLICED) FROM THE OD APPROX .25 INCH LONG. BEARING CARRIER O-RING (M8324-1-145) CUT (SLICED) IN 3 DIFFERENT SECTIO NS FOR A TOTAL OF 3 INCHES OF O-RING MATERIAL REMOVED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999070900195 19990709 00195 1999 7 9 99UAL900330 4 19990618 A 3454 SSPD1133 POWER DIVIDER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VOR ANTENNA FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 7260U 21407 OVER EASTERN KANSAS FLIGHT LOST NAV 1 AND 2 AND WAS NO LONGER CAPABLE OF NAVIGATING. REQUESTED VECTORS TO DEN. *S/D* F AULTY NR 2 VOR ANTENNA POWER DIVIDER. REPLACED NR 2 VOR ANTENNA POWER DIVIDER. 2 L 7 3 4F 4 F A3WE E2EA 1999070900196 19990709 00196 NM 1999 7 9 99UAL900331 1 19990620 A 2782 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 559UA 26657 LANDED SFO UNDER AMBER ALERT DUE TO SLAT DISAGREE LIGHT. *S/D* LEADING EDGE SLAT BINDING IN THE NUMBER ONE POSITION. R OTARY ACTUATOR CAUSED THE OVERLOAD INDICATOR ON THE ACTUATOR TO POP AND SHUT DOWN THE SLAT AND FLAP SYSTEM. REPLACED TH E NUMBER ONE POSITION SLAT ROTARY ACTUATOR AND RETURNED TO SERVICE WITHOUT FURTHER OCCURRENCE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999070900197 19990709 00197 NM 1999 7 9 99UAL900332 1 19990628 A 2150 DUCT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT PACK FAILED A UALA K NONE O OTHER CR CRUISE 1 WP 29 766UA 26917 DURING INSPECTION FOR ABNORMAL NOISE FROM LEFT AIR CONDITIONING PACK, FOUND OZONE CONVERTER DUCT FRACTURED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999070900198 19990709 00198 NM 1999 7 9 99UAL900333 1 19990621 A 2782 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT FAILED A UALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 559UA 26657 LANDED IAD UNDER AMBER ALERT DUE TO LEADING EDGE FLAP DISAGREE LIGHT. *S/D* LEADING EDGE SLAT BINDING IN THE NUMBER ON E POSITION. ROTARY ACTUATOR CAUSED THE OVERLOAD INDICATOR ON THE ACTUATOR TO POP AND SHUT DOWN THE SLAT AND FLAP SYSTEM . REPLACED THE NUMBER ONE POSITION SLAT ROTARY ACTUATOR AND RETURNED TO SERVICE WITHOUT FURTHER OCCURRENCE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999070900199 19990709 00199 NM 1999 7 9 99UAL900334 1 19990622 A 2170 COALESCER BAG BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN CONTAMINATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 312UA 23673 EXPERIENCED SMOKE IN CABIN. *S/D* POSSIBLE COALESCER BAG FAILURE. REPLACED BOTH COALESCER BAGS AND CHANGED THE RECIRC ULATION FAN AND EQUIPMENT COOLING FAN BLOWER AS PRECAUTIONARY. EXTENSIVE INSPECTION OF E & E BAY, CABIN LIGHTING, SIDE AND OVERHEAD PANELS AND ENVIRONMENTAL CONTROL SYSTEM FOUND NO DISCREPANCIES. 2 L 7 2 4F 4 F RT A16WE E2GL 1999070900200 19990709 00200 NM 1999 7 9 99UAL900336 1 19990623 A 5101 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AIRFRAME VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 793UA 26946 CREW REPORTED AFTER TAKEOFF AIRFRAME VIBRATION OF UNDETERMINED ORIGIN. AIRCRAFT RETURNED TO LAX. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999070900201 19990709 00201 NM 1999 7 9 99UAL900337 1 19990625 A 2120 AIR DIST BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 613UA 21874 DIVERTED TO ORD FOR BURNING RUBBER SMELL IN CABIN. ODOR ORIGINALLY DETECTED IN AREA OF ROW 7. FADED, THEN RETURNED IN CENTER AND AFT CABIN AREAS. *S/D* ORD INSPECTED AIRCRAFT CABIN, E&E COMPS, ALL CARGO PITS, RAN APU AND PACKS, RAN ENGI NES AND PACKS. REPLACED ALL DARK CABIN FLUORESCENT BULBS. DEBRIEFED CABIN CREW AND PASSENGERS. NO NOTICEABLE SMELLS N OTED AT GATE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999070900202 19990709 00202 EU 1999 7 9 99UAL900338 1 19990623 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 408UA 457 SYSTEM FAILED EMERGENCY LIGHTING TEST. MESSAGE WAS: BATT L. PSU BATTERY WAS REPLACED (PSU P/N IS 565-0038). 2 L 7 2 4F 4 F RT A28NM E40NE 1999070900203 19990709 00203 NM 1999 7 9 99UAL900339 1 19990625 A 5101 STRUCTURE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AIRFRAME VIBRATION A UALA A J UNSCHED LANDING DUMP FUEL E VIBRATION/BUFFET CL CLIMB 1 WP 29 766UA 26917 EN ROUTE CDG-IAD, DURING CLIMBOUT FL190 THRU FL350, MODERATE AIRFRAME VIBRATION THROUGHOUT AIRCRAFT. DIVERTED TO LHR. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999070900204 19990709 00204 WP 1999 7 9 ABXA990559 1 19990630 A 5543 59102571 TAB DOUG DOUG DC9 DC931 3022065 WP RUDDER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK, FOUND RUDDER TRIM TAB DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC9 MM 27-20-2. 2 L 7 2 4F A6WE 1999070900205 19990709 00205 WP 1999 7 9 ABXA9900560 1 19990629 A 2910 6197 FUSE DOUG DC9 DC941 302207N WP RT MLG DEFECTIVE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 960AX 47762 DURING TAXI-OUT, RIGHT BRAKE WAS GRABBING. TIRE APPEARED TO BE FLAT-SPOTTED. WHILE TAXIING BACK TO BLOCKS, RIGHT BRAKE PEDAL WENT ALL THE WAY TO THE FLOOR. PUMPING THE BRAKES BROUGHT THE PEDAL BACK UP. REPLACED NR 3 AND NR 4 MAIN TIRE A ND WHEEL ASSEMBLIES AND NR 3 AND NR 4 BRAKES. ALSO, REPLACED TWO LOWER HYDRAULIC FUSES. ANTISKID SYSTEM OPS CHECKED GO OD. 2 L 7 2 4F A6WE 1999070900206 19990709 00206 WP 1999 7 9 MWEA99362 1 19990629 A 5311 27779305 FRAME DOUG DC9 DC914 3022034 WP BS 680 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 STATION 680 FRAME CRACKED AT LONGERON 17L. FABRICATED AND SPLICED IN 14 INCH SECTION OF FRAME. 2 L 7 2 4F A6WE 1999070900207 19990709 00207 WP 1999 7 9 MWEA99363 1 19990629 A 5330 59114231 SKIN DOUG DC9 DC914 3022034 WP BS 716 OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 BLEND ON SKIN IS OUT OF LIMITS AROUND LEFT FILLET PANEL FASTENER HOLE AT STATION 716 LONGERON 24L. FABRICATED AND INSTA LLED REPAIR. 2 L 7 2 4F A6WE 1999070900208 19990709 00208 WP 1999 7 9 MWEA99364 1 19990629 A 5313 5914258IN LONGERON DOUG DC9 DC914 3022034 WP BS 615 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LEFT LONGERON 20 AT STATION 615 HAS A CRACK FROM HOLE TO HOLE. INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 1999070900209 19990709 00209 WP 1999 7 9 MWEA99365 1 19990629 A 5320 9910078147 WEB DOUG DC9 DC981 3022081 WP BS 168 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 DAMAGED VERTICAL WEB E & E COMPARTMENT JUST FORWARD OF STA 168-750 RIGHT OF CENTER LINE. FABRICATED AND INSTALLED DOUBL ER. 2 L 7 2 4F A6WE 1999070900210 19990709 00210 WP 1999 7 9 MWEA99366 1 19990629 A 5320 5960381 BEAM DOUG DC9 DC981 3022081 WP BS 693 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 ERRANT HOLE DRILLED THRU STA 693 FRAME AND CAP AT LONGERON 28R THRU NUT CLIP HOLE ON FWD SECTION OF FLOORBOARD ATTACH AN GLE. TRIMMED BEAM, FABRICATED AND INSTALLED. REPAIRED BUSHINGS PER BOEING TELEX MWX-ORD-99-0186RR DATED 6-15-99. 2 L 7 2 4F A6WE 1999070900211 19990709 00211 NM 1999 7 9 MWEA99367 1 19990624 A 2560 D29985107 EVAC SLIDE DOUG MD88 MD88 3023688 NM AFT GALLEY DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 AFT GALLEY DOOR SLIDE FELL OUT. REINSTALLED DOOR SLIDE. 2 L 7 2 4F RT A6WE 1999070900212 19990709 00212 NM 1999 7 9 MWEA99368 1 19990625 A 2560 D29985107 EVAC SLIDE DOUG MD88 MD88 3023688 NM AFT GALLEY OUT OF POSITION A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 AFT GALLEY DOOR SLIDE PACK RUBS AGAINST DOOR FRAME. REPOSITIONED SLIDE PACK AND COVER. 2 L 7 2 4F RT A6WE 1999070900213 19990709 00213 WP 1999 7 9 MWEA99369 1 19990626 A 2560 11331 EVAC SLIDE DOUG DC9 DC9 3022002 WP MAIN DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 212ME 47701 MAIN CABIN DOOR EMERGENCY SLIDE PIN IS OUT. REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999070900214 19990709 00214 NM 1999 7 9 MWEA99370 1 19990623 A 2560 D29985107 DOOR SLIDE DOUG MD88 MD88 3023688 NM AFT GALLEY OUT OF POSITION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE AFT EMERGENCY ESCAPE SLIDE PRESSURE GAUGE IS OBSCURED BY SLIDE MATERIAL. MTC REPOSITIONED SLIDE. 2 L 7 2 4F RT A6WE 1999070900215 19990709 00215 WP 1999 7 9 MWEA99371 1 19990627 A 5210 39142181 FITTING DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FORWARD PASSENGER DOOR LOWER HINGE FITTING IS CRACKED. MTC FABRICATED AND INSTALLED BRACKET AND REMOVED AND REPLACED FI TTING. 2 L 7 2 4F A6WE 1999070900216 19990709 00216 WP 1999 7 9 MWEA99372 1 19990627 A 5754 39202724 BRACKET DOUG DC9 DC932 3022066 WP NR 3 LE SLAT LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 RIGHT WING PULLEY BRACKET UPPER FORWARD MOUNT BOLT IS NOT TIGHT AND HAS A GAP BETWEEN PULLEY BRACKET AND RIB. MTC REMOV ED AND REPLACED UPPER FORWARD MOUNT BOLT ON NR 3 SLAT. 2 L 7 2 4F A6WE 1999070900217 19990709 00217 WP 1999 7 9 MWEA99373 1 19990627 A 5230 59101577 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 AFT CARGO DOOR PAN FORWARD EDGE HAS 2 DENTS. MTC FABRICATED AND INSTALLED DOUBLER SHIMS. 2 L 7 2 4F A6WE 1999070900218 19990709 00218 WP 1999 7 9 MWEA99374 1 19990627 A 5312 99118433 BULKHEAD DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 AFT CANTED BULKHEAD HAS A 1.5 INCH CRACK THROUGH GUIDE PIN HOLE. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999070900219 19990709 00219 WP 1999 7 9 MWEA99375 1 19990627 A 5512 59180031 SKIN DOUG DC9 DC932 3022066 WP LT HORIZ STAB DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 SHARP DING IN LEFT HORIZONTAL STABILIZER LOWER SKIN. MTC REPAIRED WITH FASTENER. 2 L 7 2 4F A6WE 1999070900220 19990709 00220 WP 1999 7 9 MWEA99376 1 19990627 A 3520 11504012 MANIFOLD DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 SEAT 12AB OXYGEN MANIFOLD DOES NOT MOVE TO RELEASE OXYGEN DOOR. MTC REMOVED AND REPLACED MANIFOLD. 2 L 7 2 4F A6WE 1999070900221 19990709 00221 NM 1999 7 9 DLM88991391 1 19990617 A 4920 499001341 APU DOUG MD88 MD88 3023688 NM APU COMP MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 987DL 7130 53338 P80526 AFTER T/O, AFT LAV SMOKE DETECTORS STARTED SIGNALING WITH SOME HAZE IN THE CABIN. RETURNED TO CVG. PERFORMED DUCT BURN OUT PER M/M CH 36 AND REPLACED WATER BAGS, RAN BOTH ENGS TO T/O AND NO SMOKE/HAZE NOTED. ENGS STARTED WITH EXT AIR APU NOT USED. REPLACED APU, CLEANED DOORS. RAN APU, NO LEAKS NOTED AND ALL INDS NORMAL. RAN SEVERAL HRS, NO SMOKE. 2 L 7 2 4F RT A6WE 1999070900222 19990709 00222 NM 1999 7 9 DL76L991409 1 19990622 A 3840 COMPRESSOR 288237 BOEING 767 767332 1382001 NM WATER SYS OVERHEATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 197DN 28454 ELECTRICAL SMELL DETECTED CLOSE TO RT AFT ENTRY DOOR. FOUND WATER COMPRESSOR OVERHEATED CAUSING SMELL. DISCONNECTED AN D TIED BACK C/P AT WATER COMPRESSOR AND PULLED AND COLLARED CBMCO AND PLACARD INSTALLED. 2 L 7 2 4F RT A1NM 1999070900223 19990709 00223 WP 1999 7 9 DLL19991410 1 19990622 A 2910 O RING LKHEED 1011 10113853 5265020 WP HYD SYS DAMAGED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 766DA 193H1207 IN CRUISE, C-SYS HYD LO QTY LIGHT ILLUM. FLUID LEVEL AT 1/8 PRESS GOOD. SECURED ENG PUMP AND ATM AND FLUID LOSS STOPPE D. FOR DESCENT AND LANDING TURNED ON ATM, QTY HELD AT 1/4 PRESS GOOD. GEAR, FLAPS, STEERING OPS NORMAL TO GATE. FLUID QTY AT 1/8 AT GATE. FOUND BAD O-RING ON FLOW LIMITER C-HYD SYS. REPLACED O-RING AND LEAK CK NORMAL. 2 L 7 3 4F A23WE 1999070900224 19990709 00224 1999 7 9 DL76G991411 4 19990617 A 3454 285T05545 VOR CONTROL BOEING 767 767332 1382001 NM GLARESHIELD FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 1603 29695 ON APPROACH DETECTED A MILD ELEC SMELL FROM VOR CONTROL HEADPULLED VOR C/B. REPLACED CONTROL PANEL, CHECK OK. 2 L 7 2 4F RT A1NM 1999070900225 19990709 00225 NM 1999 7 9 DL73K991413 1 19990622 A 3350 LIGHT 20121 BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 302DL 6502 23047 ON MTC INSPECTION, FOUND FWD CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH AFTER TEST. REPLACED POWER SUPPLY AND TEST GOO D. 2 L 7 2 4F RT A16WE 1999070900226 19990709 00226 NM 1999 7 9 DL72S991415 1 19990623 A 5530 651680310 FITTING BOEING 727 727232 1384082 NM VERT STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 RHS BOLT HOLES FOR THE VERT FIN FITTING ATTACH TO TENSION TIE RIB WAS FOUND WITH CORROSION. REWORKED PER ERA 333260-14, REV B. 2 L 7 3 4F A3WE 1999070900227 19990709 00227 NM 1999 7 9 DL72S991416 1 19990623 A 5753 65192497 TRACK BOEING 727 727232 1384082 NM RT TE FLAP CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 CORROSION WAS DISCOVERED IN THE TWO BOLT HOLES WHERE THE I/B FLAP O/B FLAP TRACK ATTACHES TO THE SPOILER SUPPORT LWR CHO RD. REWORKED PER ERA 333256-14, REV A. 2 L 7 3 4F A3WE 1999070900228 19990709 00228 NM 1999 7 9 DL757991418 1 19990623 A 2130 212N30167 DUCT 212N30167 BOEING 757 757232 1384965 NM RT AIR COND BAY CRACKED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 616DL 22823 AIRPLANE WOULD NOT PRESSURIZE ON RIGHT PACK. DIVERTED TO LAX. FOUND RT PACK DISTRIBUTION DUCT LEAKING. REPLACED DUCT, LEAK CHECK OK REF IPC 36-1101-07ITEM 165. 2 L 7 2 4F RT A2NM 1999070900229 19990709 00229 NM 1999 7 9 DL76L991420 1 19990623 A 3610 PRSOV 7738555 BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 197DN 9707110 28454 727738 AFTER TAKEOFF, NO BLEED AIR FROM LEFT ENG. ELECTED TO BRING A/C BACK TO ATL FOR REPAIRS. REPLACED PRSOV, SYSTEM CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999070900230 19990709 00230 NM 1999 7 9 DL72S991421 1 19990623 A 3350 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 404DA 21148 EMERGENCY EXIT LIGHT AT THE LEFT SERVICE DOOR INOP. EMERGENCY EXIT LIGHT AT FWD GALLEY NEEDS RELAMPING. RELAMPED LIGHT S. 2 L 7 3 4F A3WE 1999070900231 19990709 00231 WP 1999 7 9 DLL19991423 1 19990624 A 5712 RIB CAP LKHEED 1011 10113853 5265020 WP WS 555 CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 764DA 193H1202 LT WING UPPER RIB CAP AT IWS 555 WAS FOUND CRACKED DURING A RTN INSP OF THE CAPS. REPAIRED PER ERA 333266-14, REV A. 2 L 7 3 4F A23WE 1999070900232 19990709 00232 WP 1999 7 9 DLL19991424 1 19990624 A 5330 SKIN LKHEED 1011 10113853 5265020 WP BS 1745 MISREPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 764DA 193H1202 AN UNIDENTIFIED SKIN REPAIR WAS FOUND AT STA 1745 AND STR 45 AND 46. THE REPAIR WAS PARTIALLY REMOVED, INSPECTIONS ACCO MPLISHED AND IMPROVEMENTS TO THE REPAIR ACCOMPLISHED. REPAIRED PER ERA 333264-14, REV A. 2 L 7 3 4F A23WE 1999070900233 19990709 00233 WP 1999 7 9 DLL19991425 1 19990624 A 5330 SKIN LKHEED 1011 10113853 5265020 WP BS 930 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 764DA 193H1202 CORROSION WAS FOUND ON THE INTERNAL SURFACE OF THE FUSELAGE SKIN CENTERED AT STA 930 BETWEEN S30 AND S31. REPAIRED PER ERA 333238-14, REV A. 2 L 7 3 4F A23WE 1999070900234 19990709 00234 NM 1999 7 9 DL72W991427 1 19990624 A 5320 FRAME BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 FOUND AT B-1 LTR CK, AFT CABIN ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 5 3-10-9. 2 L 7 3 4F A3WE 1999070900235 19990709 00235 NM 1999 7 9 DL72W991428 1 19990624 A 5711 STIFFENER BOEING 727 727247 138408F NM SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 TPA LTR CHK B-1, O/B SPAR STIFFENER CRACKED AT NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21 . 2 L 7 3 4F A3WE 1999070900236 19990709 00236 WP 1999 7 9 DLL10991429 1 19990623 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP L4 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 38241 193C1180 L4 EMERGENCY EXIT SIGNS INOP. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1999070900237 19990709 00237 WP 1999 7 9 DLL19991430 1 19990624 A 3397 WIRE LKHEED 1011 10113853 5265020 WP ROW 10-16 BROKEN A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 753DA 193W1189 EMERGENCY LIGHTS INOP FROM ROW 10G TO ROW 16G. REPAIRED BROKEN WIRE IN TRACK AT 10G. 2 L 7 3 4F A23WE 1999070900238 19990709 00238 NM 1999 7 9 DL72K991431 1 19990624 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM L-2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 3786 21586 L-2 DOOR EXIT EMERGENCY LIGHT OUT. REPLACED BATTERY PACK, CKS GOOD. 2 L 7 3 4F A3WE 1999070900239 19990709 00239 NM 1999 7 9 DL73K991432 1 19990623 A 5330 SKIN BOEING 737 737232 1384475 NM BS 750 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK AT FS 750 AND STRINGER 19R. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER B737 SRM 53-30-3, FIG 6 AND ER/A 36 7661-14. 2 L 7 2 4F RT A16WE 1999070900240 19990709 00240 NM 1999 7 9 DL72S991433 1 19990623 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF T HE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS ALONG THE JOINT. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE P ANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367640-14, REV A. 2 L 7 3 4F A3WE 1999070900241 19990709 00241 WP 1999 7 9 DLL19991434 1 19990623 A 5711 1506811101 STIFFENER LKHEED 1011 10113853 5265020 WP SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 755DL 193Y1184 THE LBL 30 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR WAS FOUND CRACKED AT A LIGHTENING HOLE 12 FROM THE UPPER E ND OF THE STIFFENER. THE UPPER END OF THE STIFFENER WAS TRIMMED OFF AND A NEW SECTION SPLICED IN PER ER/A 367639-14, REV A. 2 L 7 3 4F A23WE 1999070900242 19990709 00242 NM 1999 7 9 DL733991435 1 19990625 A 2530 8606010000A OVEN BOEING 737 7373B7 1384580 NM GALLEY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 947WP 23376 F/A REPORTED SMOKE COMING FROM OVENS IN LT REAR GALLEY. REMOVED OVENS AND COVER. FOUND MELTED WIRES INSIDE BACK OF OVE NS. REPLACED OVENS AND CONTROLLERS. RAN OVENS FOR 20 MIN, OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 1999070900243 19990709 00243 NM 1999 7 9 DL76S991436 1 19990625 A 2424 GCU BOEING 767 767332 1382001 NM GE CF6 CF680A 30025 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 130DL 24080 580396 DURING CLIMBOUT AT APPROX FL 250 PILOTS NOTICED ODOR IN COCKPIT. THE ODOR BECAME STRONGER, SEVERAL MINUTES LATER THE RT GEN OFF LIGHT ILLUMINATED WITH ASSOCIATED EICAS LIGHTS. THE INTENSITY OF ODOR REQUIRED USE OF COCKPIT OXYGEN MASKS. A /C DIVERTED TO JAX. REPLACED GCU, IDG AND PYLON DISCONNECTS D4216P AND D4266J. RAN ENGINE, SYSTEM CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 1999070900244 19990709 00244 NM 1999 7 9 DLM88991437 1 19990625 A 3260 SWITCH DOUG MD88 MD88 3023688 NM NLG OUT OF ADJUST A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 912DL 49543 AFTER T/O GEAR RETRACTED, NOSE GEAR INDICATION UNSAFE LIGHT RED ILLUMINATED ABOUT 12 TO 15 TIMES FOR ONE TO THREE SECO NDS. THIS HAPPENED FOR ABOUT 5 MINUTES AFTER GEAR RETRACTION. ADJUSTED NOSE GEAR LOCK SWITCH. SWUNG NOSE GEAR , OPERATES NORMALLY. 2 L 7 2 4F RT A6WE 1999070900245 19990709 00245 NM 1999 7 9 DL72S991438 1 19990626 A 2420 SWITCH BOEING 727 727232 1384082 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 27 409DA 21153 AFTER TAKEOFF APPROX 3000 FT, GEN NR 2 BKR AND FIELD LIGHT ON. RAN POM PROCEDURES AND RETURNED TO BOS. REPLACED NR 2 E NG GEN RESIDUAL VOLTAGE SWITCH. 2 L 7 3 4F A3WE 1999070900246 19990709 00246 NE 1999 7 9 DLM88991439 2 19990625 A 7261 FILTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE DIRTY A DALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 918DL 49583 FIFTY MILES EAST OF JAN, THE RT OIL FILTER CLOG MSG ILLUM. CREW FOLLOWED POM AND THE MSG DID NOT EXTINGUISH. THE CREW SHUT DOWN THE ENGINE AND DIVERTED TO JAN. JAN MTC REMOVED THE OIL FILTER AND FOUND FULL OF CARBON. MTC REPLACED THE F ILTER AND PERFORMED AN ENG RUN AND HAD NO LEAKS AND THE CLOG MSG DID NOT RETURN. 2 L 7 2 4F 4 F RT A6WE E9NE 1999070900247 19990709 00247 NM 1999 7 9 DL72K991441 1 19990626 A 2150 ACM 2040751 BOEING 727 727232 1384082 NM RIGHT SEIZED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 521DA 281988 21472 PASSENGER REPORTS SMOKE IN CABIN AFTER GEAR AND FLAP EXTENSION. RT PACK IND 40 DEG WHEN IN FULL COLD. FOUND RT ACM SEIZED. REPLACED RT ACM, CKS GOOD. 2 L 7 3 4F A3WE 1999070900248 19990709 00248 WP 1999 7 9 DLL10991442 1 19990626 A 3350 61020 BATTERY LKHEED 1011 10113851 5265010 WP L1 DOOR DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 L1 FLASHLIGHT BATTERY INOP. REPLACED BATTERY. 2 L 7 3 4F A23WE 1999070900249 19990709 00249 NE 1999 7 9 DLL10991443 2 19990627 A 7230 SEAL LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 ENGINE FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 720DA 33401 193C1136 10400 DURING FLT, USUALLY AT REDUCED POWER, CABIN FILLED WITH A BLUE HAZE AND LAV SMOKE DETECTORS IN FWD AND AFT LAVS WENT OFF FOR SEVERAL MINUTES. REPLACED NR 3 ENGINE DUE TO FRONT BEARING OIL LEAK. 2 L 7 3 4F 4 F A23WE E12EU 1999070900250 19990709 00250 NM 1999 7 9 DLM88991444 1 19990627 A 2720 O-RING 012204662 DOUG MD88 MD88 3023688 NM RUDDER FAILED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 903DL 49534 RUDDER HYD SHUTOFF VALVE HAD O-RING DAMAGE. DAMAGE CAUSED WHITE HAZE IN CABIN WHEN FLUID INGESTED. REPLACED O-RING. 2 L 7 2 4F RT A6WE 1999070900251 19990709 00251 NM 1999 7 9 DL73K991445 1 19990627 A 2530 5374AD COFFEEMAKER BOEING 737 737232 1384475 NM AFT GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 316DL 23088 AFT GALLEY NR 2 COFFEEMAKER WHEN TURNED ON CAUSES SMELL OF HOT ELEC WIRES. INSPECTED CANNON PLUG, CKS OK. REPLACED COF FEEMAKER. 2 L 7 2 4F RT A16WE 1999070900252 19990709 00252 NM 1999 7 9 DLM88991446 1 19990627 A 4910 38005041 APU DOUG MD88 MD88 3023688 NM AUX INOPERATIVE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 947DL 49878 36280 AT 24,000 FT ON CLIMBOUT, A SLIGHT HAZE APPEARED IN THE CABIN AND BOTH AFT SMOKE DETECTORS WENT OFF. APU HAD BEEN OFF F OR 10-15 MINS. LEVELED OFF AND RETURNED TO ATL. PERFORMED DUCT BURNOUT. REPLACED COALESCERS, CLEANED APU INLET. 2 L 7 2 4F RT A6WE 1999070900253 19990709 00253 NM 1999 7 9 DLM88991447 1 19990627 A 2150 39613011 VALVE 39613011 DOUG MD88 MD88 3023688 NM RT PACK STICKING A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 920DL 4242 49644 DURING CLIMB AND INITIAL CRUISE, THE RIGHT PACK COULD NOT KEEP A/C COOL (LT PACK MEL INOP). CABIN SUPPLY TEMP WAS 108 D EG AND CABIN TEMP WAS 90 DEG. RAN PACK IN BOTH AUTO AND MANUAL. FOUND RIGHT FLOW CONTROL VALVE NOT OPENING ALL THE WAY . REPLACED VALVE. 2 L 7 2 4F RT A6WE 1999070900254 19990709 00254 NM 1999 7 9 DL73K991448 1 19990626 A 3350 BATTERY PACK BOEING 737 737232 1384475 NM ROW 18DEF NOT SECURED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 324DL 23096 ON L/O, FOUND EMERGENCY OVERHEAD SEAT LIGHT AT 18DEF INOP. RELAMPED, NO HELP. FOUND BATTERY PACK NOT SECURED. REINSTA LLED AND SECURED, OPN NOW CKS NORMAL. 2 L 7 2 4F RT A16WE 1999070900255 19990709 00255 NM 1999 7 9 DLM88991449 1 19990627 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM L 1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DE 53416 R1 AND L1 DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND RELAMPED, OPS NOW OK. 2 L 7 2 4F RT A6WE 1999070900256 19990709 00256 NM 1999 7 9 DL72S991450 1 19990627 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM EMERGENCY EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 21077 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATT PACK, OPS NOW OK. 2 L 7 3 4F A3WE 1999070900257 19990709 00257 NM 1999 7 9 DLM11991451 1 19990628 A 2530 OVEN 327 DOUG MD11 MD11 3023602 NM G-7 GALLEY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 805DE 48476 IN CRUISE, THE NR 327 G-7 GALLEY OVEN HAD AN ELECTRICAL ODOR. CREW HAD TO PULL THE C/B DUE TO IT NOT POPPING. STRONG S MELL AND SMOKE IN AFT AREA. REPLACED OVEN. 2 L 7 3 4F RT A22WE 1999070900258 19990709 00258 NM 1999 7 9 DL767991452 1 19990627 A 3350 BPS73 POWER SUPPLY BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 106DA 22218 AFT CABIN EMERGENCY LIGHTS INOP ON L/O TEST. REPLACED POWER SUPPLY AND CHARGER, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999070900259 19990709 00259 NM 1999 7 9 DL72L991453 1 19990628 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1090 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 A DENT IN THE SKIN AT BS 1090 WAS FOUND BETWEEN S29R AND S29L. DAMAGE REMOVAL REQUIRED A SKIN CUTOUT OF APPROX 5 BY 11. REPAIRED PER ERA 333290-14. 2 L 7 3 4F A3WE 1999070900260 19990709 00260 NM 1999 7 9 DLM88991454 1 19990628 A 5330 591140659 SKIN DOUG MD88 MD88 3023688 NM BS 215 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DL 49540 A DENT WAS FOUND IN THE FUSELAGE SKIN AT FS 225, JUST ABOVE L18L. DAMAGE CUTOUT WAS APPROX 10 BY 30. REPAIRED PER ERA 333294-14, REV A. 2 L 7 2 4F RT A6WE 1999070900261 19990709 00261 WP 1999 7 9 DLL19991455 1 19990628 A 5753 1533443106 SUPPORT LKHEED 1011 10113853 5265020 WP RT TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 764DA 193H1202 DAMAGED FASTENER HOLES WERE NOTED IN THE RT NR 4 O/B TRACK SUPPORT AT WBL 731. THE HOLE WAS OVERSIZED TO A FINAL DIAMET ER OF 0.799 INCH. REWORKED PER ERA 333262-14, REV A. 2 L 7 3 4F A23WE 1999070900262 19990709 00262 NM 1999 7 9 DL72L991457 1 19990628 A 5754 DOUBLER BOEING 727 727232 1384082 NM LE FLAPS DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 REMOVED DOUBLER, FABRICATED NEW DOUBLER PER M/M 57-54-00 FIG 809. 2 L 7 3 4F A3WE 1999070900263 19990709 00263 NM 1999 7 9 DLM11991458 1 19990628 A 2530 831610405 OVEN 831610405 DOUG MD11 MD11 3023602 NM GALLEY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 805DE 0013 48476 SMOKE NOTICED COMING FROM G-8 GALLEY OVEN DURING FLIGHT. OVEN SHUT OFF. FOUND OVEN 327 FAN NOT RUNNING, CAUSING THE MO TOR TO OVERHEAT. REPLACED OVEN. 2 L 7 3 4F RT A22WE 1999070900264 19990709 00264 NM 1999 7 9 DL72L991459 1 19990628 A 3260 ACCESSORY UNIT 656021132 BOEING 727 727232 1384082 NM RT MLG INOPERATIVE A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 505DA 21307 GEAR EXTENSION BUF UNSAFE GEAR WARNING WITH RT MAIN GEAR RED INDICATOR LIGHT ON WITHOUT THE GREEN DOWN AND SAFE LIGHT ON . REPLACED LANDING GEAR ACCESSORY UNIT. 2 L 7 3 4F A3WE 1999070900265 19990709 00265 1999 7 9 DLM90991460 4 19990628 A 2565 SLIDE 100504201 DOUG MD90 MD9030 3023690 NM L1 DOOR UNSERVICEABLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DA D9F02 53382 L1 DOOR SLIDE REMOVED FOR DOOR MTC AND SLIDE COVER LATCH WOULD NOT RELEASE AND AFTER SLIDE COVER OPENED FOUND PIN PUL LED OUT. REPLACED SLIDE PACK. 2 L 7 2 4F RT A6WE 1999070900266 19990709 00266 1999 7 9 DLM11991462 4 19990628 A 2330 MONITOR RDAV707301 DOUG MD11 MD11 3023602 NM ROW 40J FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 806DE 100170 48477 ODOR DETECTED IN AREA OF MONITOR 40J. MONITOR HAD BEEN FLICKERING, NO PICTURE. POWER REMOVED FROM MONITOR, ODOR DISAPP EARED. REPLACED MONITOR AND POWER SUPPLY. 2 L 7 3 4F RT A22WE 1999070900267 19990709 00267 1999 7 9 DL767991464 4 19990629 A 3454 6225220103 VOR BOEING 767 767232 1385132 NM RIGHT MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 108DL 256 22220 AT THE GATE CREW SMELLED ELECTRICAL ODOR AND SOME SMOKE. A/C WAS DEPLANED. MTC INVESTIGATED FOUND NO OBVIOUS PROBLEM B UT DID FIND VOR/MARKER C/B A-1 POPPED. SWAPPED LT VOR TO RT VOR POSTION AND THEN DEACTIVATED RT VOR PER MEL. A/C FLEW TO ATL. MTC REPLACED NR 2 VOR CONTROL PNL AND XCVR. 2 L 7 2 4F RT A1NM 1999070900268 19990709 00268 NM 1999 7 9 DL72L991467 1 19990626 A 5400 65312814 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 ON HUSH-KIT MOD, FOUND RT NR 2 AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ONE OF NEW MFG. 2 L 7 3 4F A3WE 1999070900269 19990709 00269 NM 1999 7 9 DL72S991468 1 19990629 A 5320 WEB BOEING 727 727232 1384082 NM BS 1235 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 TPA LTR CHK E1, .25 INCH CRACK AT UPPER LIGHTENING HOLE AT RT TORQUE BOX VERT WEB STA 1235. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999070900270 19990709 00270 NM 1999 7 9 DL72S991469 1 19990629 A 5720 ANGLE BOEING 727 727232 1384082 NM LT SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 VERTICAL SPAR STIFFENER CRACKED NR 3 L/E SLAT I/B SIDE OF I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1999070900271 19990709 00271 NM 1999 7 9 DL76L991470 1 19990630 A 5220 145T60821 STEP BOEING 767 767332 1382001 NM RT EMER EXIT MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 186DN 27962 ON ARRIVAL, FOUND RT AFT OVERWING EXIT DOOR STEP MISSING. REF IPC 52-21-01-02 ITEM 75. A/C MTC FERRY HAM ATL AFTER INT ERIM REPAIRS MADE. 2 L 7 2 4F RT A1NM 1999070900272 19990709 00272 NM 1999 7 9 DL72W991471 1 19990630 A 2612 CONNECTOR BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE DIRTY A DALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 27 297WA 22534 700091 INTERMITTENT FLASHING LIGHT SYS A FOR NR 1 ENG FIRE DETAT CRUISE, SMOOTH AIR. RAN PROCEDURE AND SHUT DOWN NR 1 ENG. RE PLACED BLOWN FIRE EXT BOTTLE. FOUND OIL SOAKED CONNECTORS ON LOWER LOOP AND PYLON LOOP. CLEANED CONNECTORS, FIRE TEST NOW OPS NORMAL. INSPECTED ENG, NO EVIDENCE OF FIRE. RAN NR 1 ENG, NO TROUBLE FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1999070900273 19990709 00273 NM 1999 7 9 DLM88991472 1 19990630 A 5330 5911407 SKIN DOUG MD88 MD88 3023688 NM R-1 DOORWAY GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DE 49997 SKIN UNDERNEATH R-1 DOOR GOUGED ALONG L-18R. DAMAGE FOUND AT HMV1-ATL. REPAIRED BY BLENDING GOUGES AND INSTALLING REPA IR DOUBLERS. 2 L 7 2 4F RT A6WE 1999070900274 19990709 00274 NM 1999 7 9 DLM88991473 1 19990624 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 237 CREASED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DE 49997 SKIN FWD OF STA 237 HAS 5 INCH CREASE BETWEEN L-18L AND L-17L. REPAIR CONSISTS OF TRIMMING OUT DAMAGE AND INSTALLING RE PAIR DOUBLER. 2 L 7 2 4F RT A6WE 1999070900275 19990709 00275 NM 1999 7 9 DL76G991474 1 19990627 A 2530 251009131 OVEN BOEING 767 767332 1382001 NM GALLEY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 16065 30199 FWD GALLEY NR 1 OVEN SPARKED AND POPPED BREAKER WHEN TURNED ON. REPLACED OVEN. 2 L 7 2 4F RT A1NM 1999070900276 19990709 00276 WP 1999 7 9 DLL14991475 1 19990629 A 3610 LINE LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE LOOSE A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 741DA 193C1245 NR 2 ENG NACELLE PYLON OVERHEAT LOOPS A & B LIGHTS ON AFTER TAKEOFF. BOTH LOOP LIGHTS WENT OUT WHEN THROTTLE/POWER REDU CED AND HIGH PRESSURE BLEED OFF. WHEN POWER INCREASED, LOOP LIGHTS CAME ON WITH HIGH PRESSURE BLEED OFF. INSPECTED DUC TING AND TIGHTENED CLAMPS IN SPLITTER AREA. INSPECTED AND TIGHTENED CLAMPS IN PYLON ABOVE ENGINE. FOUND B-NUT ON PNEUM ATIC DUCT FWD OF EJECTOR VALVE BACKED OFF. TIGHTENED SENSE LINE B-NUT. APPLIED PNEUMATICS, RAN ENG PER PFHB AND CKS G OOD. 2 L 7 3 4F A23WE 1999070900277 19990709 00277 NM 1999 7 9 DLM88991477 1 19990628 A 2170 COALESCER 20495061 DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 928DL 123475 49715 SMOKE IN CABIN AFTER TAKEOFF. AFT LAV SMOKE DETECTOR ACTIVATED. CKD W/W'S FOR LEAKS, CKD HYD SVC BOTTLES, REPLACED AFT SMOKE DETECTORS, REPLACED WATER SEPARATOR BAGS. FOUND LT WATER SEPARATOR INLET OILY. REPLACED LT ACM, CLEANED APU INL ET ASSY AND PLENUM. PERFORMED DUCT BURNOUT. RAN PACKS OFF APU PNEUMATICS AND PERFORMED HIGH POWER RUN. AFTER E NG RUN AND BURNOUT, REPLACED WATER SEPARATOR BAGS AGAIN, PRECAUTIONARY. 2 L 7 2 4F RT A6WE 1999070900278 19990709 00278 NM 1999 7 9 DL767991478 1 19990630 A 2621 349000047 BOTTLE BOEING 767 767232 1385132 NM CARGO COMPT DISCHARGED A DALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 114DL 22226 NR 1 FIRE BOTTLE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED AND CGO BOTTLE 1 EICAS MSG ILLUMINATED. NR 1 CGO BOTTLE FOUND EMPTY. FWD TO MCO. 2 L 7 2 4F RT A1NM 1999070900279 19990709 00279 1999 7 9 DHL99807004 4 19990630 A 2312 VHF DOUG DC8 DC873 302199C WP NR 2 FAILED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 807DH 45990 UNABLE TO RECEIVE TRANSMISSIONS ON COMM NR 1 AS REPORTED BY ATC CENTER. RECEIVED TRANSMISSIONS INTERMITTENTLY. LOST VH F NR 2 AFTER 1+ 20 MINUTES OF FLIGHT. RESEATED NR 1 VHF R/T, RESEATED CAPTS FREQ SELECTOR PANEL, OPS CHECKED GOOD. RE SEATED NR 2 VHF R/T, RESEATED F/O'S FREQ SELECT PANEL. OPS CHECKED GOOD ON SEVERAL FREQS FROM ALL POSITIONS PER MM 23-2 0-0. 2 L 7 4 4F RT 4A25 1999070900280 19990709 00280 NM 1999 7 9 SWAA991120 1 19990701 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM PASSENGER DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D CHECK, FOUND CORROSION AT FWD ENTRY EVACUATION GIRT BAR FLOOR ATTACH BRACKET, BS 344. REMOVED AND RE PLACED ATTACH BRACKET PER SRM. 2 L 7 2 4F RT A16WE 1999070900281 19990709 00281 NM 1999 7 9 SWAA991121 1 19990701 A 5320 6545409 WEB BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND LT WHEEL WELL CEILING CRACKED, BS 663, LBL 30. REPAIRED WEB PER SWA RA NR1 -353-2104 . 2 L 7 2 4F RT A16WE 1999070900282 19990709 00282 NM 1999 7 9 SWAA991122 1 19990701 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA CRACKS, BS 178 BULKHEAD RBL 1 AND LBL1. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999070900283 19990709 00283 NM 1999 7 9 SWAA991123 1 19990630 A 3350 65C27093 SIGN BOEING 737 7373H4 1384600 NM GALLEY BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 1999070900284 19990709 00284 NM 1999 7 9 SWAA991124 1 19990701 A 3350 BR2013 CONNECTOR BOEING 737 7373H4 1384600 NM ROW 11-15 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP BETWEEN ROWS 11-15. REPAIRED WIRING CONNE CTION PER MM. 2 L 7 2 4F RT A16WE 1999070900285 19990709 00285 NM 1999 7 9 SWAA991125 1 19990701 A 2913 849589 PUMP BOEING 737 7377H4 NM NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 720WN 27854 AIR TURNBACK - NR 1 ENG 'A' HYD SYSTEM LOW PRESS LIGHT ILLUMINATED DURING CLIMB-OUT. ALL OTHER INDICATIONS NORMAL. REM OVED AND REPLACED NR 1 ENG HYD PUMP AND FILTERS. 2 L 7 2 4F RT A16WE 1999070900286 19990709 00286 NM 1999 7 9 SWAA991126 1 19990701 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720WN 27854 DURING SCHEDULE C3 CHECK, FOUND EMERGENCY EVACUATION FLOOR LIGHTING MISSING SECTION AT OVERWING EXIT. INSTALLED LIGHTIN G STRIP PER MM. 2 L 7 2 4F RT A16WE 1999070900287 19990709 00287 NM 1999 7 9 SWAA991127 1 19990701 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM NR 3 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED C2 CHECK, FOUND 3 EA CRACKS AT NR 3 L/E SLAT LOWER SKIN AROUND ACTUATOR CUT OUT. REPAIRED SLAT PER SWA RA NR 1-A57-0691. 2 L 7 2 4F RT A16WE 1999070900288 19990709 00288 NM 1999 7 9 SWAA991128 1 19990701 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 328 FLOORBEAM, LBL 34. REPAIRED BEAM PER SWA RA NR 1-353-2108. 2 L 7 2 4F RT A16WE 1999070900289 19990709 00289 NM 1999 7 9 SWAA991118 1 19990630 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM BS 827, 907, 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED BS 827, BS 907,BS 787, BETWEEN STRINGERS 8L-9L. REPAIRED P ER ER NR 99-5584. 2 L 7 2 4F RT A16WE 1999070900290 19990709 00290 NM 1999 7 9 SWAA991119 1 19990630 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM BS 827 & 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED BS 827, BS 867, BETWEEN STRINGERS 8R-9R. REPAIRED PER ER N R 99-5584. 2 L 7 2 4F RT A16WE 1999070900291 19990709 00291 NM 1999 7 9 SWAA991129 1 19990701 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 986 FLOORBEAM, LBL 29. REPAIRED BEAM PER SWA RA NR 1-353-2103. 2 L 7 2 4F RT A16WE 1999070900292 19990709 00292 NM 1999 7 9 SWAA991130 1 19990701 A 5330 AND10133 PRESSURE BLKHD BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CRACK AT NOSE WHEEL WELL CEILING PRESSURE BULKHEAD AROUND AFT INBD ACCESS PANEL. REP AIRED PRESSURE BULKHEAD PER SWA RA NR 1-353-2106. 2 L 7 2 4F RT A16WE 1999070900293 19990709 00293 NM 1999 7 9 SWAA991103 1 19990629 A 3350 P8020003101 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 FWD OUTBOARD EMERGENCY FLASHLIGHT PLASTIC STRAP BROKEN. REMOVED AND REPLACED PLASTIC STRAP PER MM. 2 L 7 2 4F RT A16WE 1999070900294 19990709 00294 NM 1999 7 9 SWAA991104 1 19990629 A 3350 BR2013 LIGHT BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 EMERGENCY ESCAPE FLOOR LIGHT INOP ON AFT SECTION. REMOVED AND REPLACED FLOOR LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999070900295 19990709 00295 NM 1999 7 9 SWAA991105 1 19990629 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED 1/4D CHECK, FOUND CRACK 3 INCHES LONG, BS 1016 BULKHEAD, STRINGER 6L. REPAIRED BULKHEAD PER XEA X2-53- 248. 2 L 7 2 4F A16WE 1999070900296 19990709 00296 NM 1999 7 9 SWAA991106 1 19990629 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND BS 312 FWD ENTRY DOOR FLOOR GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED GIRT BAR FLOOR BRACKET. 2 L 7 2 4F RT A16WE 1999070900297 19990709 00297 NM 1999 7 9 SWAA991107 1 19990629 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP ON AFT END. REMOVED AND REPLACED COVER PLUG AS SY PER MM. 2 L 7 2 4F RT A16WE 1999070900298 19990709 00298 NM 1999 7 9 SWAA991108 1 19990629 A 3397 65C27093 WIRE BOEING 737 7373H4 1384600 NM PASSENGER DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN WIRE AND REMOVED AND REPLAC ED CONTACT. 2 L 7 2 4F RT A16WE 1999070900299 19990709 00299 NM 1999 7 9 SWAA991109 1 19990629 A 5240 6969854 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT LOWER AFT STOP FITTING. REMOVED AND REPLACED DOOR FRAME PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 1999070900300 19990709 00300 1999 7 9 SWAA991110 4 19990629 A 2565 BACB30NT3K11 FASTENER BOEING 737 7373H4 1384600 NM PAX DOORWAY MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR REAR ATTACH BRACKET MISSING FASTENER. INSTALL ED FASTENER PER MM. 2 L 7 2 4F RT A16WE 1999070900301 19990709 00301 NM 1999 7 9 SWAA991111 1 19990630 A 2560 601 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 328SW 23692 FWD UPPER EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999070900302 19990709 00302 NM 1999 7 9 SWAA991112 1 19990630 A 5753 654782124 CARRIAGE BOEING 737 7372H4 138448C NM RT TE MID FLAP BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 AIRCRAFT ROLLS TO THE RT SIDE ON ALL FLAP SETTINGS. REMOVED AND REPLACED RT OUTBD MID FLAP, INBD FLAP CARRIAGE ASSY PER MM. 2 L 7 2 4F A16WE 1999070900303 19990709 00303 NM 1999 7 9 SWAA991113 1 19990630 A 7711 LG80A6 EPR TRANSMITTER BOEING 737 7372H4 138448C NM RT ENGINE ERRATIC A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 ABORTED TAKEOFF AT APPROX 40 KNTS DUE TO NR 1 ENG SURGING RAPIDLY FROM 1.7 TO 2.00 EPR. REMOVED AND REPLACED EPR TRANSM ITTER PER MM. 2 L 7 2 4F A16WE 1999070900304 19990709 00304 1999 7 9 SWAA991114 4 19990630 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM ESCAPE SLIDE DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING RON CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE CABLE LOCK DISCONNECTED. RECONNECTED SLIDE CABLE LOCK. NO DEFE CTS NOTED PER MM. 2 L 7 2 4F A16WE 1999070900305 19990709 00305 NM 1999 7 9 SWAA991115 1 19990630 A 5230 6546921 FRAME BOEING 737 7375H4 138449D NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR, FWD LOWER FRAME CRACKED. REMOVED AND REPLACED FWD CARGO DOOR ASSY. 2 L 7 2 4F RT A16WE 1999070900306 19990709 00306 NM 1999 7 9 SWAA991116 1 19990630 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 500, 480, 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D CHECK, FOUND 4 EA FRAMES CRACKED, BS 500C, BS 480, BS 440, BETWEEN STRINGERS 8R-9R, AND BS 440, BETWE EN STRINGERS 8L-9L. REPAIRED FRAMES PER ER NR 99-5584. 2 L 7 2 4F RT A16WE 1999070900307 19990709 00307 NM 1999 7 9 SWAA991117 1 19990630 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM BS 727 & 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED BC2 CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS APPROX 1.5 INCHES LONG, BS 727E AND 727D, STRINGER 23R, BS 7 27E, STRINGER 21L, AND BS 747, STRINGER 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999070900308 19990709 00308 NM 1999 7 9 SWAA991092 1 19990627 A 3350 610478 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999070900309 19990709 00309 NM 1999 7 9 SWAA991093 1 19990628 A 5311 6546536 FRAME BOEING 737 7372T4 1384492 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND BS 639 FUSELAGE FRAME CRACKED, STRINGER 16R. REPAIRED FRAME PER ER NR 99-5636. 2 L 7 2 4F A16WE 1999070900310 19990709 00310 NM 1999 7 9 SWAA991094 1 19990627 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM LOWER SKIN CRACKED AT LT SIDE, BS 706. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999070900311 19990709 00311 NM 1999 7 9 SWAA991095 1 19990627 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 344, RBL 5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999070900312 19990709 00312 NM 1999 7 9 SWAA991096 1 19990627 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 772, RBL 8-LBL 13. REPAIRED FLOORBEAM PER SWA RA NR 1-A53 -2021. 2 L 7 2 4F RT A16WE 1999070900313 19990709 00313 NM 1999 7 9 SWAA991097 1 19990627 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED, BS 767, RBL 14. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999070900314 19990709 00314 NM 1999 7 9 SWAA991098 1 19990628 A 3350 P4010021 POWER UNIT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 391SW 27378 FWD OUTBD EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FWD OUTBOARD FLASHLIGHT POWER UNIT PER MM. 2 L 7 2 4F RT A16WE 1999070900315 19990709 00315 NM 1999 7 9 SWAA991099 1 19990628 A 3350 07912 COVER BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED C1 CHECK, FOUND AFT END COVER LOOSE FOR EMERGENCY ESCAPE FLOOR LIGHTS. RESECURED COVER PER MM. 2 L 7 2 4F A16WE 1999070900316 19990709 00316 NM 1999 7 9 SWAA991100 1 19990628 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM ROW 10 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP AT ROW 10. REMOVED AND REPLACED AFT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999070900317 19990709 00317 NE 1999 7 9 SWAA991101 2 19990616 A 7250 65737691 TURBINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A SWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 096SW 23055 687864 AIR TURNBACK, IN FLIGHT SHUT DOWN. NR 1 ENG HPT BLADE FAILURE SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999070900318 19990709 00318 NM 1999 7 9 SWAA991102 1 19990629 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE ASSY FELL OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999070900319 19990709 00319 NM 1999 7 9 SWAA991080 1 19990626 A 3230 6558206 SENSOR BOEING 737 7373H4 1384600 NM RT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 319SW 23340 AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT DURING TAKEOFF. HANDLE WOULD NOT MOVE ABOVE OFF POSITON. ADJUSTED MAIN GE AR SAFETY SENSOR AND PERFORMED GEAR SWING CHECK PER MM. 2 L 7 2 4F RT A16WE 1999070900320 19990709 00320 NM 1999 7 9 SWAA991081 1 19990626 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999070900321 19990709 00321 NM 1999 7 9 SWAA991082 1 19990626 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999070900322 19990709 00322 NE 1999 7 9 SWAA991083 2 19990625 A 7320 1853W56D06 HMU BOEING 737 7377H4 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A SWAA K NONE E VIBRATION/BUFFET DE DESCENT 1 SW 07 704SW 27838 ENGINE/AIRFRAME VIBRATION AT 67 PERCENT N1 DURING APPROACH. REMOVED AND REPLACED NR 1 ENG HMU. 2 L 7 2 4F 4 F RT A16WE E2EA 1999070900323 19990709 00323 NM 1999 7 9 SWAA991084 1 19990625 A 5311 6546536 FRAME BOEING 737 7372T4 1384492 NM BS 53 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FASTENER HOLES, BS 539, RBL 73, WL 229. REPAIRED FRAME PER ER NR 99-5468. 2 L 7 2 4F A16WE 1999070900324 19990709 00324 NM 1999 7 9 SWAA991085 1 19990626 A 5312 6546547 BULKHEAD BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND FUSELAGE BULKHEAD CRACKED, BS 727, LBL 16, WL 176. REPAIRED BULKHEAD PER ER NR 99-5455. 2 L 7 2 4F A16WE 1999070900325 19990709 00325 NM 1999 7 9 SWAA991086 1 19990626 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGERS CRACKED, BS 360, STRINGER 14R AND BS 807, STRINGER 5R. REPAIRED STRINGER S PER SRM. 2 L 7 2 4F A16WE 1999070900326 19990709 00326 NM 1999 7 9 SWAA991087 1 19990626 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM AFT SRVC DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 1999070900327 19990709 00327 NM 1999 7 9 SWAA991088 1 19990626 A 5320 141A880 POST BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED COCKPIT WINDOW POST, NR 1 LT OUTBOARD. REPAIRED WINDOW POST PER SWA RA NR 1- 353-2097. 2 L 7 2 4F RT A16WE 1999070900328 19990709 00328 NM 1999 7 9 SWAA991079 1 19990627 A 3230 6558206 SENSOR BOEING 737 7373H4 1384600 NM RT MLG OUT OF ADJUST A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 387SW 26602 AIR TURBACK, LANDING GEAR WOULD NOT RETRACT DURING TAKEOFF. HANDLE WOULD NOT MOVE ABOVE OFF POSITION. ADJUSTED MAIN GE AR SAFETY SENSOR TELEFLEX CABLE AND PERFORMED GEAR SWING CKECK PER MM. 2 L 7 2 4F RT A16WE 1999070900329 19990709 00329 NM 1999 7 9 SWAA991089 1 19990626 A 5320 65C25723 ANGLE BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FRAME ANGLE BS 616, LBL 67. REPAIRED ANGLE PER SWA RA NR 1-353-2099. 2 L 7 2 4F RT A16WE 1999070900330 19990709 00330 NM 1999 7 9 SWAA991090 1 19990626 A 2560 6946203 BRACKET BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND AFT SERVICE DOOR FWD SLIDE ATTACH BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 1999070900331 19990709 00331 NM 1999 7 9 SWAA991091 1 19990626 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 747 & 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FLOORBEAMS CRACKED, BS 747 AND BS 787, RBL 14. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999070900332 19990709 00332 NM 1999 7 9 TWAA9909201 1 19990701 A 3350 BULB BOEING 767 7673Q8 NM L2 DOOR LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE EXTERIOR EMERGENCY LIGHT AT THE NUMBER 2 CABIN DOOR, LT SIDE, WAS INOPERATIVE. THE LAMP WAS FOUND LOOSE AND WAS RES EATED. CHECK-C 5-1-9 LAX. 2 L 7 2 4F RT A1NM 1999070900333 19990709 00333 WP 1999 7 9 AT9900461R1 1 19990622 A 3340 8906K267 SWITCH DOUG DC9 DC932 3022066 WP RT LANDING LIGHT DEFECTIVE A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 15 812AT 47359 DURING APPROACH, NOTED SMOKE AFTER TURNING ON LEFT AND RIGHT WING LANDING LIGHTS, SMOKE STOP AFTER TURNING LIGHTS OFF. R EMOVED AND REPLACED RIGHT WING LANDING LIGHT SWITCH AND OPS CHECKED GOOD PER MM 33-40. 2 L 7 2 4F A6WE 1999070900334 19990709 00334 WP 1999 7 9 AT9900481 1 19990630 A 3350 HPDS40S3825 SOCKET DOUG DC9 DC932 3022066 WP BS 585 LOOSE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 801AT 47275 STANDBY LIGHTING IN CEILING AT BS 585 WORKING INTERMITTENT. TIGHTEN LIGHT SOCKET IN CEILING AT BS 585, OPS CHECK GOOD P ER 33-52-0. 2 L 7 2 4F A6WE 1999070900335 19990709 00335 WP 1999 7 9 AT9900482 1 19990624 A 5512 SKIN DOUG DC9 DC932 3022066 WP RT HORIZ STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CORROSION ON THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AT BS 73. R EMOVED CORROSION, FABRICATED REPAIR DOUBLER, DRILLED, HEAT TREATED, PRIMED, AND INSTALLED DOUBLER IAW DC9 SRM 51-30-2, 5 1-30-5, AND 51-30-8. 2 L 7 2 4F A6WE 1999070900336 19990709 00336 WP 1999 7 9 AT9900483 1 19990629 A 5720 4911499617 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THREE OUTBOARD STRINGER CLIPS CORRODED ON LEFT WING AT XRS 111.5 BETW EEN 11-12, 12-13, AND 13-14 STRINGERS. REMOVED AND REPLACED CLIPS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED NE W CLIPS IAW DC9 SRM 51-10-4, 51-30-5, 51-20-0, AND 51-22-1. 2 L 7 2 4F A6WE 1999070900337 19990709 00337 EA 1999 7 9 JBXA9900088 1 19990704 A 5240 SERVICE PANEL CNDAIR CL600 CL6002B19 EA LT FUSELAGE NOT CLOSED A JBXA A UNSCHED LANDING N W FALSE WARNING INADEQUATE Q C CL CLIMB 1 SO 05 580ML 7289 OUT OF RDU, FLIGHT 930, HAD LOUD NOISE COMING FROM AIRCRAFT. RETURNED TO RDU. FOUND FRONT SERVICE PANEL LEFT OPEN. MA INTENANCE INSPECTED AND CLOSED SERVICE PANEL IAW AMM 52-20-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999070900338 19990709 00338 CE 1999 7 9 PNSA990601 1 19990620 A 2120 AIR DISTR CESSNA 441 441 2076020 CE CABIN SMOKE A PNSA A H I UNSCHED LANDING DEACTIVATE SYST/CIRCUITS CABIN DEPRESSURIZATION B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 03 544AL 4410120 ON CLIMB-OUT, AIRCRAFT FILLED WITH SMOKE. AIRCRAFT WAS DEPRESSURIZED AND BLEED AIR SHUT OFF. LANDING WAS UNEVENTFUL. P ROBLEM COULD NOT BE DUPLICATED UNLESS AIRCONDITIONING SYSTEM WAS INTENTIONALLY OVERHEATED AND ALLOWED TO SATURATE AT WHI CH POINT A HAZE WAS NOTED IN THE CABIN. THE DUCT OVERHEAT LIGHT WAS ON DURING THIS OVERHEAT CONDITION. AFTER INSPECTIN G THE ACM, THE AIRCRAFT WAS TEST FLOWN AND AN ADDITION 6 HOURS OF REVENUE FLIGHT, WITH NO FAULTS FOUND. 1 L 7 2 3T RT A28CE 1999070900339 19990709 00339 SW 1999 7 9 PNSA990602 1 19990627 A 2913 PV304426 PUMP SWRNGN SA227 SA227AC 8780603 SW LT HYD SYS FAILED A PNSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 41NE 64494 AC741B LT HYDRAULIC PRESSURE LIGHT ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO ANC. MAINTENANCE FOUND SPLINES ON PUMP DRI VE SHAFT STRIPPED. PUMP WAS REPLACED AND TESTED OK. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4T RT A8SW 1999070900340 19990709 00340 SO 1999 7 9 PNSA990603 1 19990624 A 2432 RG35XC BATTERY PIPER PA32 PA32301 7103207 SO BATTERY COMPT DISCHARGED A PNSA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AL 03 8305H 10763 328106017 DURING CRUISE, CHARGING SYSTEM WOULD NOT INDICATE POSITIVE CHARGE RATE. RETURNED TO BASE. REPLACED BATTERY, OPS CHECK OK. 1 L 7 1 3O A3SO 1999070900341 19990709 00341 SW 1999 7 9 PNSA990604 1 19990602 A 2432 237561 BATTERY SWRNGN SA227 SA227AC 8780603 SW BATTERY COMPT FAILED A PNSA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 AL 03 175SW 1394 AC621 RT BATTERY INDICATED OVERHEAT CONDITION AFTER TAKEOFF. AIRCRAFT RETURNED TO BASE BATTERY WAS REPLACED. AIRCRAFT RELEAS ED FOR SERVICE. 2 L 7 2 4T RT A8SW 1999070900342 19990709 00342 NM 1999 7 9 RAAA99B2049 1 19990629 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 12 PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999070900343 19990709 00343 NE 1999 7 9 9902296717 2 19990629 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 4 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 01 617US 21123 662706 AT FL120, DURING DESCENT WITH ENGINES AT IDLE POWER, THE NR 4 ENGINE FLAMED OUT. THE ENGINE WAS RESTARTED AND OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE PERFORMED TROUBLESHOOTING PER FIM WITH NO DEFECTS NOTED. 2 L 7 4 4F 4 F A20WE E20EA 1999070900344 19990709 00344 NM 1999 7 9 9902306729 1 19990628 A 2910 6984610835 MODULE BOEING 747 747251B 1384892 NM NR 4 HYD SYSTEM FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 251F 22388 DURING CRUISE, THE NR 4 HYDRAULIC QUANTITY INDICATION SLOWLY DECREASED. AIRCRAFT DIVERTED TO SEA AND LANDED WITHOUT INC IDENT. REPLACED THE AUXILIARY HYDRAULIC CONTROL MODULE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999070900345 19990709 00345 WP 1999 7 9 9902319947 1 19990629 A 3260 SENSOR DOUG DC9 DC931 3022065 WP LT MLG DOOR MALFUNCTIONED A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 8938E 47161 DURING APPROACH INTO DTW, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR EXTENSION. CREW EXECUTED GO-AR OUND PROCEDURES AND TOWER VERIFIED GEAR TO BE DOWN. EMERGENCY WAS DECLARED AND ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT MAIN GEAR DOOR LATCH MECHANISM AND REPLACED LEFT MAIN GEAR DOWNLOCK AND UPLOCK SENSORS. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999070900346 19990709 00346 WP 1999 7 9 9902329928 1 19990624 A 3231 SPRING DOUG DC9 DC931 3022065 WP NLG DOOR BROKEN A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8921E 45836 NOSE LANDING GEAR WOULD NOT EXTEND ON LANDING. FLIGHT CREW PERFORMED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT NOSE GEAR DOOR CABLE SPRING BROKEN. REPLACED SPRING. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999070900347 19990709 00347 WP 1999 7 9 9902339928 1 19990625 A 3230 SPRING DOUG DC9 DC931 3022065 WP NLG BROKEN A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8921E 45836 DURING APPROACH INTO MSP, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR BUNGEE SPRINGS. OPERATIONAL CHECK NORMAL ON GEAR SWING AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999070900348 19990709 00348 WP 1999 7 9 9902349928 1 19990627 A 3230 BOLT DOUG DC9 DC931 3022065 WP NLG LOOSE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8921E 45836 NOSE LANDING GEAR WOULD NOT EXTEND ON LANDING INTO MSP. CREW UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RETIGHTENED BOLT IN OVERCENTER ARM. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999070900349 19990709 00349 NM 1999 7 9 UPS99630000 1 19990630 A 2920 32687929 AIR DRIVEN PUMP BOEING 767 76734AF 1385212 NM HYD SYSTEM LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 322UP 27748 HYDRAULIC FLUID LOSS IN FLIGHT INFLIGHT EMERGENCY DECLARED. MAINTENANCE FINDINGS, ADP BYPASS HAD OPENED AND WAS LEAKING HYDRAULIC FLUID. ISSUED ECA 04892 REPLACED CENTER ADP PER MM 29-11-03 AND LEAK CHECK OK. P/N OFF 3268792-9 S/N OFF 10 11. P/N ON 3268792-9 S/N ON 727. 2 L 7 2 4F RT A1NM 1999070900350 19990709 00350 NM 1999 7 9 UPS99630005 1 19990702 A 2133 OUTFLOW VALVE BOEING 767 76734AF 1385212 NM CABIN INOPERATIVE A IPXA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 319UP 27758 INSPECTION TYPE:ETOP PILOT REPORT PRESSURIZATION AUTO 1 DID NOT INITIATE AT FL 370 DESCENDING INTO ONT. MANUAL PRESSURI ZATION INITIATED AT FL 200. PRESSURIZATION AUTO 2 ON DEFFERAL. REMOVED AND REPLACED OUTFLOW VALVE, VALVE CHECKS GOOD. 2 L 7 2 4F RT A1NM 1999070900351 19990709 00351 NM 1999 7 9 UPS99630006 1 19990701 A 5414 PANEL BOEING 767 76734AF 1385212 NM RT PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 311UP 27741 RT ENG OTBD SIDE PYLON PANEL CRACKED. PANEL IS FIRST FWD OF HYDRAULI C ACCESS DOOR. CRACK IS 2 INCH LONG RADIATING FRO M AFT EDGE. PANEL NUMBER 447ERX REF MM 06-43-00 PG 213. PERFORMED INTERIM REPAIR PER EO B767-5450-11458-A AS ISSUED BY UPS ENGINEERING. ASSIGNED DEFERRAL D174681 BY AMC. 2 L 7 2 4F RT A1NM 1999070900352 19990709 00352 EU 1999 7 9 QXEA9901423 1 19990628 A 2530 90K6001 RECEPTICAL FOKKER F28 F28MK4000 4990810 EU GALLEY FAILED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 497US 11173 PDX - STRONG OR BURNING ODOR COMING FROM AREA OF LOWER COFFEE JUG. MX PULLED AND COLLARED CIRCUIT BREAKER FOR LOWER COF FEE JUG AND PLACED ON MEL. MEL CLEARED ON 7/2/99 BY REPLACING THE PLUG-IN RECEPTICLE FOR THE LOWER COFFEE JUG. OPERATI ONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999070900353 19990709 00353 EU 1999 7 9 QXEA9901424 1 19990629 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 481US 11230 PDX - EMERGENCY EXIT LIGHT OVER COCKPIT DOOR PARTIALLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN. OP ERATIONAL TEST PERFORMED, OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A20EU 1999070900354 19990709 00354 NM 1999 7 9 99FDEA00249 1 19990701 A 5315 6516338180 FLOORBEAM BOEING 727 7272S2F 1384O81 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 CORROSION UNDER NUT PLATES ON FLOORBEAM BS 950, BL 0-RBL 25, WL 208 (C53-224-01, 3). *S/D* REPAIRED FLOORBEAM IAW FEDE X EA NR 7-5310-46929. 2 L 7 3 4F A3WE 1999070900355 19990709 00355 NM 1999 7 9 99FDEA00250 1 19990630 A 5520 ELEVATOR DOUG MD11 MD11F 3023600 NM LEFT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 LEFT O/B ELEVATOR WITH DAMAGE, O/B END BROKEN OFF. ALSO, LT HORIZONTAL STAB RIB CRACKED. *S/D* REPLACED LT AND RT O/B ELEVATOR PER 27-30-30-4. 2 L 7 3 4F RT A22WE 1999070900356 19990709 00356 WP 1999 7 9 ABXA9900561 1 19990630 A 5250 AR25291GR41 LATCH DOUG DOUG DC9 DC932 3022066 WP COCKPIT DOOR OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 COCKPIT DOOR WOULD NOT OPEN. ADJUSTED COCKPIT DOOR LATCH. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999070900357 19990709 00357 SO 1999 7 9 SWIA971500 1 19990608 A 3260 INDICATION EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG MALFUNCTIONED A SWIA O OTHER N FALSE WARNING LD LANDING 1 NM 07 203SW 120240 NOSE GEAR WOULD NOT RETRACT DURING GO AROUND. SHOWED BOTH A/B RED LIGHTS. SELECTED GEAR UP AGAIN WITH SAME PROBLEM. S ELECTED GEAR DOWN WITH 3 GREEN. INSPECTED LANDING GEAR SYSTEM FOR DEFECTS AND PERFORMED SEVERAL GEAR SWINGS, BUT COULD NOT DUPLICATE PROBLEM. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900358 19990709 00358 SO 1999 7 9 SWIA971501 1 19990609 A 3260 SWITCH EMB 120 EMB120RT SO PWA 118 PW118A NE LT MLG FAILED A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 251YV 120251 WHEN GEAR SELECTOR SELECTED DOWN, THREE RED GEAR LIGHTS ILLUMINATED WITH NO GEAR EXTENSION. CYCLED TWICE MORE WITH SOME RESULT. PERFORMED GEAR ELECTRICAL OVERRIDE PROCEDURE IN QUICK REFERENCE HANDBOOK AND GEAR EXTENDED. REPLACED LEFT MAI N GEAR WEIGHT ON WHEELS PROXIMITY SWITCH. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900359 19990709 00359 EA 1999 7 9 SWIA971502 1 19990609 A 5240 SERVICE PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE OXYGEN SYS NOT CLOSED A SWIA A UNSCHED LANDING E W VIBRATION/BUFFET INADEQUATE Q C CL CLIMB 1 NM 07 412SW 7101 ON TAKEOFF, ADC NR 2 FAILED. SHORTLY THEREAFTER A LOUD VIBRATION COULD BE HEARD AND FELT IN THE COCKPIT. RETURNED TO S LC. FOUND OXYGEN SERVICE PANEL UNLATCHED CAUSING A DISTURBANCE IN AIRFLOW TO THE NR 2 PITOT TUBE. PERFORMED INSPECTION OF O2 SERVICE PANEL AND SECURELY LATCHED PANEL. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999070900360 19990709 00360 EA 1999 7 9 SWIA971503 1 19990601 A 3620 OVERHEAT MESSAGE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT 14 STG DUCT MALFUNCTION A SWIA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 NM 07 410SW 7066 RIGHT 14TH STAGE DUCT OVERHEAT MESSAGE EN ROUTE. QUICK REFERENCE HANDBOOK PERFORMED AND MESSAGE PERSISTS. SINGLE ENGIN E PROCEDURE PERFORMED AND DUCT MESSAGE PERSISTS. LEFT BECAME INTERMITTENT JUST PRIOR TO LANDING. FIRE CREWS REPORTED N O SIGN OF FIRE. REMOVED AND REPLACED RIGHT PYLON 14TH STAGE DUCT ELEMENT PER MM 36-11-05. RAN ENGINES AND INSPECTED 14 TH STAGE DUCT AND COWLING ANTI ICE DUCTING FOR LEAKS. NONE NOTED. OPERATIONALLY RAN RIGHT ENGINE FOR 20 MINUTES WITH N O 14TH STAGE DUCT MESSAGE DUCT. MONITOR TEST GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999070900361 19990709 00361 SO 1999 7 9 SWIA971504 1 19990601 A 2430 RCCB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 216SW 120285 LOUD RELAY CYCLING TYPE SOUND EMITTING FROM CAPTAIN'S SIDE CONSOLE. RETURNED TO LAX. REPLACED GASPER FAN RCCB. OPS CH ECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900362 19990709 00362 SO 1999 7 9 SWIA971505 1 19990602 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 CLIMBING THROUGH 17000 FT CABIN LOST PRESSURIZATION. RETURNED TO SLC. INSTALLED SERVICEABLE ELECTRONIC ALTITUDE CONTRO LLER. OPS CHECK GOOD IAW 21-31-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900363 19990709 00363 SO 1999 7 9 SWIA971506 1 19990602 A 7712 TORQUE SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 294SW 120321 RIGHT TORQUE DROPPED AND RIGHT PROPELLER AUTO FEATHERED. RETURNED TO LAX. REPLACED TORQUE SIGNAL CONDITIONER AND REPLA CED TORQUE SENSOR. PERFORMED OPS CHECK OF TORQUE SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900364 19990709 00364 SO 1999 7 9 SWIA971507 1 19990604 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PASSENGER DOOR DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 216SW 120285 FORWARD DOOR LIGHT ILLUMINATED IN FLIGHT. RETURNED TO STS, COULD NOT DUPLICATE. ON GROUND OPS CHECK GOOD. CLEANED MIC ROSWITCHES. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900365 19990709 00365 SO 1999 7 9 SWIA971508 1 19990604 A 3230 CIRCUIT BREAKER EMB 120 EMB120RT SO PWA 118 PW118 NE LANDING GEAR TRIPPED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 162CA 120150 LANDING GEAR WOULD NOT RETRACT. RETURNED TO PDX. RESET UP/DOWN CONTROL AND DOWN CONTROL OVERRIDE CIRCUIT BREAKERS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900366 19990709 00366 SO 1999 7 9 SWIA971509 1 19990605 A 3241 TRANSDUCER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 581SW 120349 RIGHT INBOARD ANTI-SKID LIGHT CAME ON UPON GEAR DOWN. RECYCLED AND LIGHT REMAINED ON. RETURNED TO LAX DUE TO RUNWAY LE NGTH RESTRICTIONS WITH ANTI-SKID INOP. REMOVED AND REPLACED NR 2 WHEEL SPEED TRANSDUCER WITH SERVICEABLE UNIT. OPS CHE CK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900367 19990709 00367 EA 1999 7 9 SWIA971510 1 19990606 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE OXYGEN COMPT NOT CLOSED A SWIA A UNSCHED LANDING N W FALSE WARNING INADEQUATE Q C CL CLIMB 1 NM 07 405SW 7029 AFTER TAKEOFF, A VERY LOUD SQUEAL WAS HEARD ALONG WITH IAS STALL FAIL, MACH TRIM AND EFIS COMP. RETURNED TO SLC. SECUR ED OXYGEN SERVICE DOOR IN FRONT OF RIGHT PITOT TUBE. ALL SYSTEMS FUNCTION NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 1999070900368 19990709 00368 1999 7 9 SWIA971511 4 19990609 A 3425 COMPUTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1 AHRS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 233SW 120307 CAPTAINS AHRS COMPUTER FAILED. DIVERTED FROM LAX. REPLACED NR 1 AHRS COMPUTER. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999070900369 19990709 00369 EU 1999 7 9 CA990219006 1 19990208 A 3233 200497005 ACTUATOR FOKKER F28 F28MK1000 4990808 EU LT MLG INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CA DRG87380 (CAN) ON DESCENT, LT MLG DID NOT SHOW DOWN AND LOCKED. SEVERAL SELECTIONS CARRIED OUT AND STILL NO SAFE INDICATION. AI RCRAFT RETURNED TO BASE AND LANDED SAFELY, GEAR CHECKED ON RUNWAY AND NOT DOWN AND SAFE PINS INSTALLED. LT MLG DOWNLOC K ACTUATOR REPLACED, ACTUATOR SHIPPED FOR INVESTIGATION. SERVICEABLE ACTUATOR INSTALLED. 2 L 7 2 4F RT A20EU 1999070900372 19990709 00372 WP 1999 7 9 CA990323004 1 19990305 A 6220 369D21210501 STRAP PACK 369D21200503 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R HUB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1608 0420 CAE831949 (CAN) STRAP PACK CRACKED IN AREA ADJACENT TO LEAD/LAG LINK ATTACHMENT. NO CRACKS ARE ALLOWED IN THIS AREA. 1 G 7 1 3U 3 U H3WE E4CE 1999070900374 19990709 00374 WP 1999 7 9 CA990401004 1 19990310 A 6210 369A10045 FOLDING PIN HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R BLADE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 3829 CAE832607 (CAN) IT WAS NOTICED ON POST-FLIGHT INSPECTION THAT THE BOTTOM PART OF THE AFT GREEN M/R BLADE FOLDING PIN WAS HANGING D OWN LOWER THAN THE LEAD-LAG LINK. ALL PARTS OF THE PIN WERE STILL IN PLACE AND THE LEVER ARM WAS STILL HOLDING THE SEL F-LOCKING NUT. NO VIBRATIONS OR ABNORMALITIES WERE NOTED DURING PREVIOUS FLIGHT. NO DAMAGE TO M/R BLADE OR LEAD-LAG L INK. 1 G 7 1 3U 3 U H3WE E4CE 1999070900375 19990709 00375 NM 1999 7 9 CA990416006 1 19990324 A 2722 654486112 PCU BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE RUDDER FAILED W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 CA 37534 134 687733 (CAN) CREW REPORTED DEFLECTION OF RUDDER LEFT TO RIGHT, HAPPENED TWICE IN CRUISE. CLIMB-OUT AT 260 NOTICED SHARP YAW MO VEMENT THEN RETURNED TO NORMAL, TOO QUICK TO NOTICE YAW FLUCTUATION. YAW COUPLER REPLACED. IN CRUISE, AT FL 310, YAW O SCILLATION STARTED, YAW DAMPER DISCONNECTED, OSCILLATION STOPPED, YAW DAMPER COUPLER REPLACED, RUDDER POWER CONTROL UNIT REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999070900376 19990709 00376 NM 1999 7 9 CA990416007 1 19990325 A 2722 654486112 PCU BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE RUDDER FAILED W K NONE F FLT CONT AFFECTED CR CRUISE 1 CA 42688 27 688450 (CAN) PILOT REPORTED VIBRATION THROUGHOUT THE AIRCRAFT WITH B-PUMPS ON. RUDDER OBSERVED TO OSCILLATE 1 TO 1.5 INCH RAN GE, RUDDER FUNCTIONED, VIBRATION QUIT. RUDDER PCU REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1999070900377 19990709 00377 NM 1999 7 9 CA990416012 1 19990330 A 3213 65617405 STRUT 654610022 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE LT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 34494 13261 0002 674646 (CAN) LT MLG OUTER CYLINDER TRUNNION CRACKED. LUG CRACKED FROM TOP OF LUG SURFACE CLOSE TO THE CYLINDER AND DOWN THE BU SHING BORE. GEAR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999070900378 19990709 00378 NM 1999 7 9 CA990416013 1 19990330 A 3211 657376188 TRUNNION BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE MLG DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 51739 12636 688450 (CAN) FOUND MLG OUTER TRUNNION ATTACHMENT LINK SHEARED. GEAR REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1999070900379 19990709 00379 NM 1999 7 9 CA990416014 1 19990331 A 2722 654486112 PCU BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE RUDDER FAILED W A UNSCHED LANDING F E FLT CONT AFFECTED VIBRATION/BUFFET CR CRUISE 1 CA 37537 137 707301 (CAN) ON TWO OCCASIONS UNCOMMANDED YAW EXCURSIONS, ON CLIMB AND IN CRUISE. BOTH TIMES THE YAW WAS QUITE PRONOUNCED AND OF SHORT DURATION, YAW TO RIGHT. YAW DAMPER AND AUTOPILOT WERE ENGAGED. RUDDER POWER CONTROL UNIT REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999070900380 19990709 00380 NM 1999 7 9 CA990416052 1 19990330 A 3221 BEARING BOEING 737 73746B NM CFMINT CFM56 CFM563C1 13802 EU NLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA RY038 858472 (CAN) ON WALK-AROUND, FOUND RT NOSE WHEEL OUT OF ALIGNMENT. FOUND OUTER BEARING BROKEN. BOTH NOSE WHEELS REPLACED. 2 L 7 2 4F 4 F RT A16WE E21EU 1999070900381 19990709 00381 SW 1999 7 9 CA990420011 1 19990413 A 6320 70061J000T310A LINE BELL 206 206L 1181522 SW OIL SYSTEM CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING 200-HOUR INSPECTION, TRANSMISSION OIL LINE P/N 70-061J000T310A WAS FOUND CHAFED THROUGH STAINLESS STEEL SLE EVE. 1 G 7 1 3U H2SW 1999070900383 19990709 00383 SW 1999 7 9 CA990423019 1 19990422 A 5302 206033004045A SKIN BELL 206 206L 1181522 SW TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA AOKP01047 (CAN) DURING COMPLIANCE WITH AD CF-98-42R1, FPI OF TAILBOOM SKIN IN AREA (AROUND THE EDGES OF THE HORIZONTAL STABILIZER OPENING), A CRACK OF 3 MM IN LENGTH WAS FOUND. 1 G 7 1 3U H2SW 1999070900385 19990709 00385 NE 1999 7 9 CA990430005 1 19990420 A 6330 7620903001049 FITTING SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL TRANSMISSION CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17677 CAE890556S (CAN) DURING SCHEDULED 100-HOUR INSPECTION, A 3 INCH CRACK WAS DETECTED MID-SPAN, TOP, OUTBOARD SIDE, STARTING AT A FAST ENER HOLE AND THEN THROUGH A SECOND HOLE ENDING AT THE THIRD HOLE. 1 G 7 2 3U 3 U H1NE E1GL 1999070900386 19990709 00386 SW 1999 7 9 CA990430008 1 19990416 A 7810 205060881001 SHIELD 205060800025 BELL 205 205A1 1181414 SW LYC T53 T5317A 41549 NE TAILPIPE FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA LE07669C (CAN) ON SHUTDOWN, FOLLOWING A ONE HOUR LEG OF A 3.5 HOUR FLIGHT, A RUBBING NOISE WAS HEARD FOLLOWING SHUTDOWN WHILE DYN AMIC COMPONENTS WERE STILL ROTATING. ON FURTHER INSPECTION, IT WAS NOTED THAT THE TAILPIPE SHIELD HAD DROPPED OUT OF PO SITION AND HAD CONTACTED THE SHORT TAIL ROTOR DRIVESHAFT SECTION P/N 204-040-620-009. THIS THEN CAUSED A SCORED GROOVE OF .020 INCH IN THE T/R DRIVESHAFT WHICH COULD HAVE HAD SERIOUS CONSEQUENCES IF NOT DISCOVERED. SUBJECT TAILPIPE SHIELD HAD JUST BEEN INSTALLED AND 2 OUT OF THE 3 DZUS FASTENERS WERE NOT POSITIVELY FASTENED. 1 G 7 1 4U 4 U H1SW E17EA 1999070900388 19990709 00388 SW 1999 7 9 CA990430016 1 19990419 A 6510 2040406043 COUPLING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA T/R DRIVESHAFT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA AFS35304 CPPS60497 (CAN) DURING LUBRICATION OF T/R DRIVE SHAFT COUPLINGS (ON SCHEDULED INSPECTION), CHIPPED TEETH WERE FOUND ON THE SPLINES . 1 G 7 1 4U 4 U H4SW E22EA 1999070900389 19990709 00389 NE 1999 7 9 CA990430058 1 19990415 A 6710 7640003005044 CONTROL LEVER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL MAIN ROTOR MISMANUFACTURED W K NONE O OTHER IN INSP/MAINT 1 CA CAE890138S (CAN) ON SCHEDULED INSPECTION, IT WAS NOTED THAT ONE OF THE BEARINGS ON A FLIGHT CONTROL LEVER WAS NEAR ITS LIMITATION (AXIAL). THE LEVER ASSY P/N 76400-03 005-044 WAS ORDERED AND INSTALLED. HOWEVER, WHEN HYD AND ELEC POWER WAS APPLIED, THE LEVER ASSY WOULD NOT CONTACT ITS STOP BECAUSE IT WAS BINDING AGAINST ITS MOUNTING BRACKET. FURTHER INVESTIGATION RE VEALED THAT THE NEW LEVER ASSY WAS SLIGHTLY THICKER AND GOT CAUGHT UP IN THE EARS OF THE MOUNTING BRACKET. A NEW LEVER WAS THEN RE-ORDERED AND INSTALLED WITH NO PROBLEMS. SIKORSKY WAS ADVISED OF THIS DISCREPANCY. 1 G 7 2 3U 3 U H1NE E1GL 1999070900395 19990709 00395 SW 1999 7 9 CA990531002 1 19990506 A 2550 MS245471 SWITCH HS20200106 BELL 205 205A1 1181414 SW LYC T53 T5317A 41549 NE HOIST FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION HO HOVERING 1 CA 106C LEO7636C (CAN) DURING EXTERNAL HOISTING OPERATIONS, THE HOIST FAILED NEAR THE FULL-UP POSITION. A VISUAL INSPECTION FOUND THE PL UNGER FOR THE FULL-IN LIMIT SWITCH JAMMED IN THE CABLE GUIDE HOUSING OF THE HOIST THEREBY CUTTING POWER TO THE HOIST MOT OR NOT ALLOWING THE CABLE IN OR OUT. THE COVER FOR THE UPPER LIMIT SWITCH WAS REMOVED REVEALING THAT THE CIRCLIP WHICH HOLDS SPRING PRESSURE ON THE PLUNGER HAD BECOME DISENGAGED. THIS WAS THE FIRST HOISTING OPERATION SINCE OVERHAUL. 1 G 7 1 4U 4 U H1SW E17EA 1999070900402 19990709 00402 NE 1999 7 9 CA990614018 1 19990603 A 6510 NAS464P4A5 BOLT SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL T/R DRIVESHAFT SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA CAE890556S (CAN) DURING 50-HOUR INSPECTION, SUBJECT BOLT WAS FOUND SHEARED AT BOLT HEAD. PAINT STRIPE ON BOLT HEAD HAD MOVED. BOL T HOLE BORES INSPECTED AND FOUND SERVICEABLE. ALL IDENTICAL BOLTS (3 EACH), NUTS, WASHERS, CHANGED AS PRECAUTIONARY PR OCEDURE. 1 G 7 2 3U 3 U H1NE E1GL 1999070900403 19990709 00403 WP 1999 7 9 TWAA9909301 1 19990630 A 2120 92743642 RELAY DOUG DC9 DC983 3022083 WP RADIO RACK WORN A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 9304C 49530 AT FL330 THERE WAS SMOKE IN THE CABIN AT PASSENGER ROW ONE. CREW FOUND PHASE A CIRCUIT BREAKER FOR THE STANDBY RADIO RA CK FAN HAD POPPED. CREW PULLED REMAINING FAN CIRCUIT BREAKERS. CORRECTIONS WERE DEFERRED PER MEL. MAINTENANCE LATER R EPLACED THE FAN RELAY. CHECK-C 2-1-99 MCI. 2 L 7 2 4F RT A6WE 1999070900404 19990709 00404 WP 1999 7 9 TWAA9909302 1 19990705 A 2830 654233 VALVE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE FUEL DUMP FAILED A TWAA E ENGINE SHUTDOWN X K ENGINE FLAMEOUT FLUID LOSS LD LANDING 1 CE 05 977Z 47249 2112 DURING FINAL APPROACH, THE RIGHT ENGINE FLAMED OUT. FOUND FUEL LEAKING AT THE PRESSURIZATION AND DUMP VALVE FITTING. R EPLACED THE DUMP VALVE, THE SEAL AND THE FITTING. CHECK-C 11-13-98 STL. 2 L 7 2 4F 4 F A6WE E2EA 1999070900405 19990709 00405 WP 1999 7 9 TWAA9909303 1 19990701 A 5320 WEB DOUG DC9 DC982 3022082 WP SERVICE DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 DURING OP 16 MAINT CHECK, FOUND CORROSION ON THE WEB BELOW THE AFT SERVICE DOOR THRESHOLD PLATE AND FLOOR PANEL. REMOVE D CORROSION AND INSTALLED WEB REPAIR PER SRM 53-01, FIG 2. 2 L 7 2 4F A6WE 1999070900406 19990709 00406 NM 1999 7 9 HNAA9900092 1 19990704 A 5400 85410147 ANGLE DHC DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CHAFED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 938HA 152 152 NR 1 ENG HORSE COLLAR CHAFED ON INBOARD SIDE, FWD ANGLE DOUBLER. PART OF MONOCOQUE STRUCTURE OF NAC CAUSE BY BONDING ST RAP DEPTH= .016. BLENDED AREA IAW EO8-54-99-727. 2 H 7 2 4T RT A13NM 1999070900407 19990709 00407 NM 1999 7 9 HNAA9900093 1 19990702 A 6120 PCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MALFUNCTIONED A HNAA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 07 924HA 105 NR 2 ENG EXCEEDED 135 PERCENT TQ FOR LESS THEN 10 SEC. REMOVED AND REPLACED PROP, PCU, HMU, TSCU AND TQ PROB. INSPECTE D OIL FILTERS AND BORESCOPED ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999070900408 19990709 00408 NM 1999 7 9 HNAA9900094 1 19990704 A 6123 INDICATION LIGHT DHAV DHC8 DHC8201 2809001 NM AUTOFEATHER SYS MALFUNCTIONED A HNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 07 996HA 497 ABORTED T/O DUE TO ABSENCE OF A/F ARM LIGHT. TRIMMED ENG, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999070900409 19990709 00409 NE 1999 7 9 PCAA9900021 2 19990701 A 7230 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MALFUNCTIONED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 13 833EX 282 121087 FLT 3635 - BWI, IN FLIGHT AFTER CRUISE POWER LEVERS WERE BROUGHT BACK TO IDLE, AN ELECTRICAL ODOR WAS NOTICED. MAINTENA NCE RAN ACFT AND ISOLATED NR 2 ENGINE. INSPECTED ENGINE, NO LEAKS NOTED. REMOVED AND CLEANED AIR SWITCHING VALVE. REI NSTALLED VALVE IAW P&W M/M 72-30-00. RAN ACFT, OPS CHECK OK. 2 H 7 2 4T 4 T RT A13NM E20NE 1999070900410 19990709 00410 NM 1999 7 9 PCAA9900022 1 19990702 A 3260 SOCKET DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 13 836EX 297 FLT 3733 - ABE, LANDING GEAR INOP AND CAUTION LIGHT ILLUMINATED IN FLIGHT. CREW DIVERTED INTO ABE. MAINTENANCE TROUBLE SHOT AND FOUND RELAY SOCKET AT 32-61-K7 BAD. REPLACED SOCKET, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999070900411 19990709 00411 NM 1999 7 9 PCAA9900023 1 19990702 A 3260 8053519 RELAY DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 13 836EX 9703 297 FLT 3629 - PHL, LANDING GEAR INOP AND CAUTION LIGHT ILLUMINATED. CREW DIVERTED INTO PHL. TROUBLESHOT LANDING GEAR CAUT ION LIGHT SYSTEM. MEGGED AND RAN WIRES FROM COCKPIT TO RELAY PANEL. INSPECTED ALL WIRES FROM COCKPIT TO RELAY PANEL. F OUND COMPUTER ON MASTER CAUTION PANEL BAD. REMOVED AND REPLACED MASTER CAUTION PANEL, FOUND RELAY 3261-K11 BAD. REPLAC ED RELAY. GEAR RETRACTION TEST PERFORMED SATISFACTORY. 2 H 7 2 4T RT A13NM 1999070900412 19990709 00412 NM 1999 7 9 PCAA9900024 1 19990701 A 3260 PSEU DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 13 836EX 297 FLT 3559 - PHL, LANDING GEAR INOP AND CAUTION LIGHT CAME ON DURING CRUISE FLIGHT. CREW DIVERTED INTO PHL. MAINTENANCE TROUBLESHOT SYSTEM, PERFORMED SEVERAL RETRACTION TESTS AND COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLACED PSEU FOR T ROUBLESHOOTING. 2 H 7 2 4T RT A13NM 1999070900413 19990709 00413 NM 1999 7 9 RAAA99B1009 1 19990703 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 7 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 7 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999070900414 19990709 00414 WP 1999 7 9 CALA9900761 1 19990630 A 3350 EMSE299A BATTERY AVIALL DOUG DC10 DC1030 3023501 WP DOOR 3L DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19072 20098 46576 THE EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK AND CHARGER AT DOOR 3L WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-01, PAGE 201. 2 L 7 3 4F A22WE 1999070900415 19990709 00415 NE 1999 7 9 CALA9900762 2 19990702 A 7200 LK76084 BEARING BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE FAILED A CALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 09 19136 29285 31629 SMOKE APPEARED IN THE CABIN WITH THE RT OIL FILTER LIGHT ILLUMINATING WHILE EN ROUTE FROM EWR TO LAX. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 2 ENGINE OIL FILTER. THE NR 2 ENGI NE WAS REMOVED AND REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD IAW MM 71-00-00. THE ENGINE WAS RUN WITH NO SMOKE NO TED IN THE CABIN. *S/D* INVESTIGATION REVEALED FAILURE OF THE RADIAL DRIVE STEADY BEARING. SUBSEQUENTLY, THE RIGID SH ROUD OIL TUBE CRACKED IN THE 03 INTERMEDIATE CASING MODULE CAUSING THE REPORTED SMOKE IN THE CABIN AND OIL LOSS. 2 L 7 2 4F 4 F RT A2NM E12EU 1999070900416 19990709 00416 NM 1999 7 9 CALA9900763 1 19990630 A 5320 ANGLE BOEING 737 7373T0 1384582 NM R-1 DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND R-1 DOOR THRESHOLD FLOOR ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999070900417 19990709 00417 NM 1999 7 9 CALA9900764 1 19990701 A 3350 BR96441112 LIGHT BRUCE BOEING 737 737724 NM ROW 14 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 23708 28769 INSPECTION FOUND BOTH RED AND WHITE EMERGENCY EXIT AND AISLE LOCATOR LIGHTS AT ROW 14 INOPERATIVE. BOTH LIGHT FIXTURES WERE REPLACED. 2 L 7 2 4F RT A16WE 1999070900418 19990709 00418 NM 1999 7 9 CALA9900765 1 19990701 A 5330 SKIN BOEING 757 757224 1384958 NM BS 400-420 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14107 27297 INSPECTION FOUND FUSELAGE DENTED AT STA 400-420, STRINGER 16L. THE DENTED AREA WAS REPAIRED IAW SRM 53-00-01 AND ECRA 5 331-01057. 2 L 7 2 4F RT A2NM 1999070900419 19990709 00419 WP 1999 7 9 CALA9900766 1 19990701 A 5543 TAB DOUG DC9 DC982 3022082 WP RUDDER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND RT SIDE OF RUDDER TAB DENTED. THE TAB WAS REMOVED AND REPAIRED IAW SRM 55-04, PARAGRAPH 2. THE TAB WA S BALANCED AND REINSTALLED IAW MM 27-20-02. 2 L 7 2 4F A6WE 1999070900420 19990709 00420 WP 1999 7 9 CALA9900767 1 19990701 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1155-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED FROM STA 1155 TO 1174. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53 -05, FIGURE 4 AND SRM 51-30-2. 2 L 7 2 4F A6WE 1999070900421 19990709 00421 NM 1999 7 9 CALA9900768 1 19990625 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT UPPER O/B CORNER OF L-1 WINDSHIELD. REPAIRED SKIN IAW ECRA 5330-02 838. 2 L 7 2 4F RT A16WE 1999070900422 19990709 00422 NM 1999 7 9 CALA9900769 1 19990705 A 2560 MEGAPHONE BOEING 737 737524 1384721 NM CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17614 27327 THE AFT MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED. 2 L 7 2 4F RT A16WE 1999070900423 19990709 00423 WP 1999 7 9 CALA9900770 1 19990704 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 1 INCH CRACK IN STIFFENER VERTICAL ANGLE AT RT MLG WHEEL WELL REAR BULKHEAD LOWER O/B CORNER JOINT TO LONGERON TO BULKHEAD. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-35-02 AND 51-33-01, FIGURE 1. 2 L 7 3 4F A22WE 1999070900424 19990709 00424 WP 1999 7 9 CALA9900771 1 19990705 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND TWO VERTICAL STIFFENER ANGLES ON LT WHEEL WELL AFT SIDE WEB CRACKED. THE CRACKS WERE .5 INCH LONG. TH E TWO ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070900425 19990709 00425 WP 1999 7 9 CALA9900772 1 19990705 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 1 INCH CRACK WITH SHEARED RIVETS IN RT WING NR 2 LEADING EDGE SLAT INBOARD SKIN. THE CRACKED AREA WA S TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-00-01, FIGURE 4. THE RIVETS WERE REPLACED WITH NEW RIVETS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070900426 19990709 00426 WP 1999 7 9 CALA9900773 1 19990705 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND FLOOR SUPPORT CORRODED UNDER LAV/GALLEY FLOOR AREA AT STA 420 BETWEEN BL 0 TO LBL 27. THE FLOOR SUPPOR T WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-21-01. 2 L 7 3 4F A22WE 1999070900427 19990709 00427 WP 1999 7 9 CALA9900774 1 19990705 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1920-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED BETWEEN STA 1920 AND 2007, LBL 55. THE FLOOR SUPPORT WAS REMOVED AND A NE W SUPPORT WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070900428 19990709 00428 WP 1999 7 9 CALA9900775 1 19990705 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1841 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 2 INCH CRACK IN FRAME OF CENTER CARGO COMPARTMENT VERTICAL WALL AT STA 1841, RBL 20. THE CRACKED ARE A WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 53-00-01, FIGURE 4 AND 51-31-01. 2 L 7 3 4F A22WE 1999070900429 19990709 00429 WP 1999 7 9 CALA9900776 1 19990705 A 5320 LINER DOUG DC10 DC1030 3023501 WP BS 1841 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 2 INCH TEAR ON VERTICAL WALL IN CENTER CARGO COMPARTMENT AT STA 1841, RBL 10. THE TORN AREA WAS TRIM MED OUT AND REINFORCED WITH DOUBLER IAW SRM 53-00-01, FIGURE 4, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1999070900430 19990709 00430 WP 1999 7 9 CALA9900777 1 19990705 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 755 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 2 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO AREA AT STA 755 BETWEEN RBL 65 AND 85. THE FLOOR SUPP ORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070900431 19990709 00431 WP 1999 7 9 CALA9900778 1 19990705 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 899 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO AREA AT STA 899, RBL 45-65. THE FLOOR SUPPORT WAS REM OVED AND A NEW ONE WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070900432 19990709 00432 WP 1999 7 9 CALA9900779 1 19990705 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1120 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN ATTACH ANGLE AT STA 1120, STRINGER 33-34R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999070900433 19990709 00433 WP 1999 7 9 CALA9900780 1 19990706 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1060 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND HEAT DAMAGE ON LONGERONS 12R AND 13R AT STA 1060. THE DAMAGED LONGERON SECTIONS WERE REMOVED AND NEW L ONGERONS AND SPLICES WERE INSTALLED IAW SRM 53-01, FIGURE 18. 2 L 7 2 4F A6WE 1999070900434 19990709 00434 WP 1999 7 9 CALA9900781 1 19990706 A 5720 SUPPORT DOUG DC9 DC932 3022066 WP WS 171 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND LT FLAP FIXED VANE SUPPORT WORN WITH A .25 INCH CRACK AT STA XFLS 171. THE FIXED SUPPORT WAS REPLACED IAW MM 27-51-3, PAGE 201. 2 L 7 2 4F A6WE 1999070900435 19990709 00435 WP 1999 7 9 CALA9900782 1 19990702 A 5755 NRC6050502 SKIN DOUG DC10 DC1030 3023501 WP NR 4 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND THE UPPER AND LOWER SURFACE OF RT WING NR 4 SPOILER SKIN DELAMINATED. THE SPOILER WAS REMOVED AND REPL ACED IAW MM 27-60-01. 2 L 7 3 4F A22WE 1999070900436 19990709 00436 WP 1999 7 9 CALA9900783 1 19990702 A 5751 SKIN DOUG DC10 DC1030 3023501 WP LT AILERON CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND LT WING O/B AILERON UPPER SKIN CORRODED AT STA 917. THE AILERON WAS REPLACED IAW MM 27-10-02. 2 L 7 3 4F A22WE 1999070900437 19990709 00437 WP 1999 7 9 CALA9900784 1 19990702 A 5414 SKIN DOUG DC10 DC1030 3023501 WP NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 2 INCH CRACK IN NR 2 ENGINE PYLON SKIN WITH LOOSE FASTENERS ON PYLON FIN. THE SKIN WAS REPAIRED IAW SRM 54-20-00, FIGURE 6 AND FASTENERS WERE REPLACED IAW SRM 51-31-00. 2 L 7 3 4F A22WE 1999070900438 19990709 00438 WP 1999 7 9 CALA9900785 1 19990702 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1060 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 1060 AT LONGERON 12R-12R ATTACH POINT. THE CRACKED AREA OF FR AME WAS CUT OUT IAW SRM 53-03. A NEW FRAME AND SPLICES WERE INSTALLED IAW SRM 51-01-8 AND 51-01, PAGE 1. 2 L 7 2 4F A6WE 1999070900439 19990709 00439 SO 1999 7 9 COMA9910104 1 19990701 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 263CA 19201 120255 FORWARD FLOOR EMERGENCY LIGHTING WAS WEAK. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1999070900440 19990709 00440 EA 1999 7 9 COMA9960337 1 19990703 A 2611 47305C SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 982CA 40281 7168 CARGO SMOKE AND OVERHEAT WARNINGS. REPLACED CARGO SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 1999070900441 19990709 00441 EA 1999 7 9 COMA9960335 1 19990702 A 2750 855D009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTIONED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 739CA 7273 FLAPS FAIL MESSAGE. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999070900442 19990709 00442 EA 1999 7 9 COMA9960334 1 19990701 A 5230 601R3505025 BRACKET CNDAIR CL600 CL6002B19 EA CARGO DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7145 BRACKET ON THE BOTTOM OF THE FORWARD CARGO DOOR FOUND TO BE CRACKED. REPLACED BRACKET. 2 L 7 2 4F RT A21EA 1999070900443 19990709 00443 EA 1999 7 9 COMA9960333 1 19990629 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 975CA 6100 7150 GEAR DISAGREE AND PROX SYSTEM FAULT MESSAGE. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1999070900444 19990709 00444 EA 1999 7 9 COMA9960332 1 19990706 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA BS 310-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 PAX DOOR THRESHOLD ANGLE, (P/N 601R31527-181), PAX DOOR FLOOR SUPPORT ANGLE, (P/N 601R315-27-207) AND SERVICE DOOR THRES HOLD ANGLE, (P/N 601R38303-105), ALL DISCOVERED WITH CORROSION BEYOND REPAIRABLE LIMITS. REPLACED PAX DOOR THRESHOLD AN GLE, (P/N 601R31527-207) IAW WVAC EO 601R-53-0085. REPLACED PAX DOOR FLOOR SUPPORT ANGLE (P/N 601R31527-207) IAW WVAC E O 601R-53-0087. REPLACED SERVICE DOOR THRESHOLD ANGLE (P/N 601R38303-105) IAW WVAC EO 601R-53-0084. 2 L 7 2 4F RT A21EA 1999070900445 19990709 00445 EA 1999 7 9 COMA9960331 1 19990706 A 5320 6003401717 SUPPORT CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 FLOOR SUPPORT MEMBER (P/N 60034017-17) AT FS 280 APPROXIMATELY 1 OUTBOARD OF RBL 9 DISCOVERED WITH 2 INCH CRACK. REPAIR ED FLOOR SUPPORT MEMBER FS 280 IAW WVAC EO 601R-53-0088. 2 L 7 2 4F RT A21EA 1999070900446 19990709 00446 EA 1999 7 9 COMA9960330 1 19990706 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280-409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 FLOOR SUPPORT BEAMS RBL 27, RBL 9, LBL 9 AND LBL 27 IN AREAS BETWEEN FS 280 AND FS 409 WERE DISCOVERD TO BE CORRODED BEY OND REPAIRABLE LIMITS. REMOVED AND REPLACED CORRODED SECTIONS OF FLOORBEAMS RBL 9, LBL 9 AND LBL 27 (BETWEEN FS 280 AND FS 409) IAW WVAC EO 601R-53-0089. REMOVED AND REPLACED CORRODED SECTION OF FLOORBEAM RBL 27 BETWEEN FS 280 AND FS 355 IAW CANADAIR REO 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999070900447 19990709 00447 EA 1999 7 9 COMA9960329 1 19990706 A 5320 SUPPORT CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 FLOOR SUPPORT PLATES (P/N 601R38673-17-19-21) AND 25 AT FS 349 BETWEEN LT FUSELAGE SKIN AND LBL 27, LBL 9, RBL 9, RBL 27 AND RT FUSELAGE SKIN DISCOVERED CORRODED BEYOND SERVICEABLE/REPAIRABLE LIMITS. REPLACED FLOOR SUPPORT PLATES WITH NEW FLOOR SUPPORT PLATES IAW WVAC EO 601R-53-0086. 2 L 7 2 4F RT A21EA 1999070900448 19990709 00448 EA 1999 7 9 COMA9960328 1 19990703 A 5330 SKIN CNDAIR CL600 CL6002B19 EA BS 310 NICKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 DURING INCOMING INSPECTION OF AIRCRAFT FOR EXTERNAL DAMAGE NOTICED THAT FUSELAGE SKIN WAS NICKED AT FS 310 STR 16 BY DOO R LATCH PIN. SKIN WAS BLENDED IAW BOMBARDIER REO 601R-53-21-160. 2 L 7 2 4F RT A21EA 1999070900449 19990709 00449 NM 1999 7 9 UPS99230009 1 19990703 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM GALLEY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:IN, GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT ID AND PLATE. REMOVED AND REPLACED BAT TERY PACK. 2 L 7 3 4F A3WE 1999070900450 19990709 00450 NM 1999 7 9 UPS99230010 1 19990703 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:N/A, RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OVERWING CKS GOOD IAW MM 33-5 0-81. 2 L 7 3 4F A3WE 1999070900451 19990709 00451 NM 1999 7 9 UPS99230011 1 19990703 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:N/A, BOTH LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED PACKS, OVERWING CKS GOOD IAW MM 33-50-81. 2 L 7 3 4F A3WE 1999070900452 19990709 00452 NM 1999 7 9 UPS99430008 1 19990705 A 5330 SKIN BOEING 747 747121 1384871 NM FWD OF CARGO DOO DENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE:IN, DENT 3 FOOT FWD OF AFT CARGO DOOR. REMOVED DAMAGE IAW SRM 53-30-03. INSTALLED DOUBLER IAW SRM 53-3 0-03, PAINTED TO MATCH A/C COLOR SCHEME. 2 L 7 4 4F A20WE 1999070900453 19990709 00453 1999 7 9 UPS99630007 4 19990703 A 3442 DRIVE BOEING 767 76734AF 1385212 NM RADAR ANTENNA INOPERATIVE A IPXA K NONE O OTHER CR CRUISE 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP, WEATHER RADAR INOP. REMOVED AND REPLACED WEATHER RADAR ANTENNA DRIVE UNIT IAW 34-43-05, SYSTEM OP CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999070900454 19990709 00454 WP 1999 7 9 ABXA9900562 1 19990702 A 5313 59114279 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 980. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999070900455 19990709 00455 WP 1999 7 9 ABXA9900563 1 19990702 A 5330 59114013 SKIN DOUG DOUG DC9 DC932 3022066 WP BS 192 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND FUSELAGE EXTERIOR SKIN CRACKED AT STATION 192 AND LONGERON 22 LEFT. REPAIRED LONGERON IAW DC9 SRM 53-04. 2 L 7 2 4F A6WE 1999070900456 19990709 00456 WP 1999 7 9 ABXA9900564 1 19990702 A 5320 992348485 INTERCOSTAL DOUG DOUG DC9 DC932 3022066 WP BS 179 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK, FOUND INTERCOSTAL CRACKED IN E & E COMPARTMENT CEILING AT STATION 179 AND BL 20 LEFT. REPAIRED INTERCOS TAL IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 1999070900457 19990709 00457 NM 1999 7 9 DL72W991479 1 19990630 A 2612 65602097W FIRE LOOP BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 297WA 22534 700091 WHEN TESTING SYS, NR 1 DETECTOR SYS A NR 1 FIRE HANDLE LIGHT COMES ON AND STAYS ON AFTER TEST IS COMPLETE. IN FLIGHT SH UTDOWN FOR FIRE WARNING EARLY TODAY. B SYSTEM ALREADY ON MCO. REPLACED LWR A-B FIRE LOOP, DET UNIT AND CONTROL PANEL. 2 L 7 3 4F 4 F A3WE E2EA 1999070900458 19990709 00458 1999 7 9 DLM11991480 4 19990701 A 2330 1301273111 ENTERTAIN SYS DOUG MD11 MD11 3023602 NM ROW 3C FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 802DE 9810000493 48473 STRONG SMELL COMING FROM ENTERTAINMENT SYSTEM AND FROM SEAT 03C. ENTERTAINMENT SYSTEM SHUTDOWN AND PAX MOVED FROM SEAT 3C. SMELL QUIT AFTER SHUTDOWN OF ENTERTAINMENT SYSTEM. REPLACED AUDIO VIDEO UNIT AT 3C. 2 L 7 3 4F RT A22WE 1999070900459 19990709 00459 NE 1999 7 9 DLL14991481 2 19990630 A 7210 RB211524B4I GEARBOX LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 740DA 193C1244 OIL QUANTITY GAUGE WENT TO ZERO, HAD OIL PRESS CONTINUE TO DECREASE. AS PRECAUTIONARY ENG SHUTDOWN POM. REPLACED NR 2 ENGINE GEARBOX FOR LEAKING. 2 L 7 3 4F 4 F A23WE E12EU 1999070900460 19990709 00460 NM 1999 7 9 DL72S991482 1 19990629 A 5330 SKIN BOEING 727 727225 1384077 NM BS 705 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 THE FUSELAGE SKIN WAS FOUND CORRODED AT AN EXISTING SKIN REPAIR AT FS 705 AND STRINGER 28R. THE SKIN REPAIR WAS REMO VED, THE CORROSION CUTOUT, AND A NEW ALUMINUM REPAIR DOUBLER INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 367664- 14AD, REV A. 2 L 7 3 4F A3WE 1999070900461 19990709 00461 NM 1999 7 9 DL76P991483 1 19990629 A 5330 143T35622 SKIN BOEING 767 767332 1382001 NM FS 654-720 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 140LL 25988 THE FUSELAGE SKIN WAS TORN AND GOUGED BY GROUND EQUIPMENT BETWEEN FS 654 + 44 AND FS 654 + 66 AND BETWEEN STRINGERS 34 R AND 35R. THE DAMAGED SKIN WAS REMOVED WITH A 10 X 20 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM D OUBLER PER ER/A 367677-14. 2 L 7 2 4F RT A1NM 1999070900462 19990709 00462 WP 1999 7 9 DLL10991484 1 19990629 A 5312 1503617107 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP AFT PRESS BLKHD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 718DA 193C1097 WHILE ACCOMPLISHING HFEC INSPECTIONS OF THE UPPER GORE WEB OF THE AFT P-DOME, A 2.5 INCH CRACK WAS FOUND IN THE WEB AT L BL 10. THE CRACK IS TYPICAL OF LAC S/B 093-53-258 (MANDATED PER AD 95-17-03). THE CRACK WAS REPAIRED WITH A DOUBLER AN D TRIPLER PER THE S/B AND DOCUMENTED PER ER/A 367681-14AD. 2 L 7 3 4F A23WE 1999070900463 19990709 00463 NM 1999 7 9 DL72S991485 1 19990701 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 FOUND AT B-1 LTR CK, AFT ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9 . 2 L 7 3 4F A3WE 1999070900464 19990709 00464 NM 1999 7 9 DL72S991486 1 19990701 A 5754 65651622292 SKIN BOEING 727 727232 1384082 NM LT LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 LOWER SKIN REPAIRED PER M/M 57-54-0 FIG 801. 2 L 7 3 4F A3WE 1999070900465 19990709 00465 NM 1999 7 9 DL72S991487 1 19990701 A 5320 WEB BOEING 727 727232 1384082 NM BS 1226 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 TPA LTR CHK B1, .375 INCH CRACK TORQUE BOX VERT WEB STA 1226. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999070900466 19990709 00466 NM 1999 7 9 DLM90991491 1 19990701 A 3350 RPS1 POWER SUPPLY DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TO TAKEOFF 1 SO 27 914DN 53394 EMERGENCY LIGHTS CAME ON ROW 38 DURING T/O. REPLACED DEFECTIVE POWER SUPPLY. 2 L 7 2 4F RT A6WE 1999070900467 19990709 00467 NM 1999 7 9 DLM88991492 1 19990702 A 5330 29524001 SKIN DOUG MD88 MD88 3023688 NM BS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DL 49540 DENT FOUND IN THE FUSELAGE SKIN AT FS 218 NEAR L18L AND L19L. CUTOUT SIZE IS APPROX 3 INCH DIA. REPAIRED PER ERA 33329 3-14. 2 L 7 2 4F RT A6WE 1999070900468 19990709 00468 NM 1999 7 9 DLM88991493 1 19990702 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DL 49540 DENT FOUND IN THE FUSELAGE SKIN AT FS 237, BETWEEN L17L AND L18L. CUTOUT SIZE IS APPROX 3 INCH DIA. REPAIRED PER ERA 3 33306-14. 2 L 7 2 4F RT A6WE 1999070900469 19990709 00469 NM 1999 7 9 DL72W991494 1 19990702 A 3320 BALLAST 036405 BOEING 727 727247 138408F NM ROW 19-18 FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 2821W 21059 AT DEPARTURE TIME, BURNING SMELL IN CABIN AND RT AFT CEILING LIGHT CIRCUIT BREAKER POPPED. FOUND CEILING BALLAST BAD AT SEAT 17. REPLACED SAME. . 2 L 7 3 4F A3WE 1999070900470 19990709 00470 NM 1999 7 9 DL757991495 1 19990701 A 5312 141N292064 BULKHEAD BOEING 757 757232 1384965 NM BS 395 DAMAGED A DALA K NONE O OTHER LD LANDING 1 SO 27 656DL 24396 THE SUBJECT AIRCRAFT SUFFERED A HARD LANDING ON THE NOSE GEAR WHICH CAUSED BUCKLING OF THE FS 395 BULKHEAD LOWER CHOR D AND WEB AND WRINKLING OF THE ADJACENT LT AND RT SKIN PANELS. THE SKIN PANELS, BULKHEAD CAP AND WEB WERE REMOVED AND R EPLACED WITH NEW PARTS PER ER/A 367602-14, REV A. 2 L 7 2 4F RT A2NM 1999070900471 19990709 00471 WP 1999 7 9 DLL10991496 1 19990701 A 5512 1524132 SKIN LKHEED 1011 10113851 5265010 WP HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 735D 193C1226 THE UPPER SKIN OF THE LT HORIZONTAL STABILIZER WAS FOUND WITH A .75 INCH LONG CRACK AT FS 80 AT THE RUNOUT OF STRINGER 31. THE CRACK WAS ROUTED OUT OF THE SKIN WITH A 1.5 INCH DIA HOLE AND REPAIRED WITH AN ALUMINUM DOUBLER AND TRIPLE R PER ER/A 367701-14 AND L1011 SRM 55-15-00, FIG 802. 2 L 7 3 4F A23WE 1999070900472 19990709 00472 NE 1999 7 9 DL767991497 2 19990702 A 7200 ENGINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 1 FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 109DL 22221 580124 NR 1 ENG SLOW TO ACCELERATE, SEVERAL RED LINES. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 1999070900473 19990709 00473 NM 1999 7 9 DL72L991498 1 19990618 A 5700 652163262 SKIN BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 36 INCHES FROM I/B END OF FLAP. THE CRACK WAS REPAIRED BY REMOV ING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 809. 2 L 7 3 4F A3WE 1999070900474 19990709 00474 NM 1999 7 9 DL72L991499 1 19990630 A 5753 652163262 SKIN BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 32 INCHES FROM I/B END. THE DAMAGE WAS REMOVED AND A DOUBLER IN STALLED PER MM 57-52-0, FIG 809. 2 L 7 3 4F A3WE 1999070900475 19990709 00475 NM 1999 7 9 DL72L991500 1 19990618 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 36 INCHES FROM I/B END. THE DAMAGE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1999070900476 19990709 00476 NM 1999 7 9 DL757991501 1 19990702 A 3244 TIRE B757M BOEING 757 757232 1384965 NM RT MLG FAILED A DALA O OTHER O OTHER TO TAKEOFF 1 SO 27 619DL DL152A 22909 CREW REPORTED DURING T/O, POSSIBLE BLOWN TIRE. FOUND UPON ARRIVAL NR 7 TIRE CAP BLOWN AND RT I/B TRAILING EDGE FLAP HAD A 6 INCH CRACK. ALSO, FOUND NR 7 BRAKE WEAR PIN DAMAGED. REPLACED NR 7, 8 TIRE AND NR 7 BRAKE. REPAIRED TRAILING EDGE FLAP PER ERA 367723-14. 2 L 7 2 4F RT A2NM 1999070900477 19990709 00477 NM 1999 7 9 DL72W991502 1 19990702 A 3350 900835A BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 22108 EMERGENCY LIGHT FIRST CLASS OVERHEAD INOP. REPLACED BATTERY, OPS NORMAL. 2 L 7 3 4F A3WE 1999070900478 19990709 00478 NM 1999 7 9 DL76S991504 1 19990703 A 2530 OVEN BOEING 767 767332 1382001 NM GALLEY DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 119DL 23278 ACRID FUMES IN COCKPIT AND CABIN COULD NOT ISOLATE. POSSIBLY STRONGER IN FWD GALLEY AND FC AREA. INSPECTED E & E, ALL CARGO COMPARTMENTS, NOTHING FOUND. REMOVED ALL FC GALLEY OVENS AND COFFEEMAKERS, NOTHING FOUND. CHECKED OVERHEAD AREA OF FC CABIN, NOTHING FOUND. RAN BOTH ENGS AT CRZ POWER FOR 20 MINS WITH BOTH PACKS ON, NO TROUBLE FOUND. REMOVED DIRTY FOOD TRAYS FROM FC OVENS. 2 L 7 2 4F RT A1NM 1999070900479 19990709 00479 NM 1999 7 9 DLM90991506 1 19990703 A 3260 BULB 387 DOUG MD90 MD9030 3023690 NM RT MLG FAILED A DALA O OTHER P NO WARNING INDICATION LD LANDING 1 SO 27 908DA 53388 ON LANDING DFW PLACED GEAR HANDLE DOWN AND HAD NO GREEN LIGHT ON RIGHT MAIN. FOLLOWED CHECK LIST PER POM. FOUND BO TH BULBS INOP. RELAMPED SAME. SIMULATED GEAR SWING USING SLUGS, ALL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999070900480 19990709 00480 NM 1999 7 9 DL72W991507 1 19990703 A 2612 FIRE LOOP 894120 BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 297WA 22534 700091 NR 1 ENG B-FIRE LOOP ON MCO. A-LOOP FAULT LIGHT ILLUM, WOULD NOT TEST. CREW SHUT DOWN ENGINE IN FLT AND BLEW THE FIRE BOTTLE PER THE POM. REPLACED LOWER LOOP. 2 L 7 3 4F 4 F A3WE E2EA 1999070900481 19990709 00481 NM 1999 7 9 DL73K991508 1 19990703 A 3350 BATTERY PACK 20131A BOEING 737 737232 1384475 NM ROW 4, 6 & 8 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 316DL 6560 23088 EMERGENCY LIGHTS AT ROWS 4, 6, 8 ABC OVERHEAD FAILED TO LIGHT ON TEST. REPLACED BATTERY PACK. 2 L 7 2 4F RT A16WE 1999070900482 19990709 00482 WP 1999 7 9 DLL19991509 1 19990703 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 760DH 69459 193Y1194 EMERGENCY LIGHTS IN FIRST CLASS ILLUMINATED. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1999070900483 19990709 00483 NM 1999 7 9 DL76L991510 1 19990704 A 3350 FUSE 201201 BOEING 767 767332 1382001 NM ROW 6AB FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 186DN 27962 EMERGENCY PATH LIGHTS FROM SEAT ROW 6AB THROUGH FIRST ROW OF TOURIST CLASS ON LEFT SIDE OF FUSELAGE FAILED TEST. DETERM INED FUSE WAS BLOWN IN POWER SUPPLY LOCATED AT 6AB. REPLACED FUSES, LIGHTS NOW CHECK OK. 2 L 7 2 4F RT A1NM 1999070900484 19990709 00484 NM 1999 7 9 DL733991511 1 19990704 A 3350 LIGHT 1317 BOEING 737 7373L9 1384470 NM ROW 21D INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 231DN 23717 EMERGENCY EXIT BULLNOSE LIGHT AT 21D INOP. RELAMPED, OPS CKS NORMAL. 2 L 7 2 4F RT A16WE 1999070900485 19990709 00485 NM 1999 7 9 DL72S991512 1 19990704 A 3350 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 ON L/O 2 CK, FOUND NO SMOKING LIGHTS INOP AT 4CD, 14DEF, 19DEF, 23DEF. ALSO, FOUND FASTEN SEAT BELT LIGHTS AT 4CD, 2AB, 20DEF INOP. RELAMPED, ALL CHECK GOOD. 2 L 7 3 4F A3WE 1999070900486 19990709 00486 1999 7 9 DL76L991513 4 19990705 A 2565 SLIDE 101651303 BOEING 767 767332 1382001 NM R1 DOOR DEPLOYED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 189DN PA2222 25990 TWENTY MIN AFTER REACHING TOP OF CLIMB FL310, LOUD NOISE HEARD IN R-1 DOOR AREA. AIR LEAK HEARD ON FWD EDGE OF R-1 DOOR . NO PROBLEM WITH PRESSURIZATION OR CABIN ALTITUDE. AFTER LANDING JFK DURING TAXI R-1 DOOR OPENED AND SLIDE DEPLOYED O N TAXI-WAY. REPLACED SLIDE, DOOR OPERATION OK. 2 L 7 2 4F RT A1NM 1999070900487 19990709 00487 NM 1999 7 9 DLM88991515 1 19990705 A 3320 CONNECTOR DOUG MD88 MD88 3023688 NM ROW 18-21 FAILED A DALA K NONE O OTHER CR CRUISE 1 SO 27 904DL 49535 READING LIGHTS FLASHING IN ROWS 18 - 21. FOUND MID CABIN TRANSFORMER GROUND STUD 3491 BURNED. REPLACED TERMINAL END AN D HARDWARE. SECURED WIRES, ALL LIGHTS CK GOOD. 2 L 7 2 4F RT A6WE 1999070900488 19990709 00488 WP 1999 7 9 DLL10991516 1 19990705 A 3244 L1011M TIRE LKHEED 1011 10113851 5265010 WP MLG FAILED A DALA K NONE O OTHER LD LANDING 1 SO 27 1734D 193C1225 NR 3 RT TIRE THREW RECAP ON LANDING. RUPTURING 2 HYD LINES CAUSING A LOSS OF C-SYSTEM HYD FLUID ON TAXI IN. REPLACED T IRE AND LINES. 2 L 7 3 4F A23WE 1999070900489 19990709 00489 WP 1999 7 9 DHL99801002 1 19990705 A 2130 DUCT DOUG DC8 DC873 302199C WP CABIN LOOSE A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 COULD NOT MAINTAIN CABIN BELOW 10,000 FT THROUGH FL 280. HEARD LOUD BANG ON CLIMBOUT. FOUND DUCT LOOSE ON RIGHT AND LE FT WATER SEPARTOR. RESECURED PER MM 21-55-3. 2 L 7 4 4F RT 4A25 1999070900490 19990709 00490 NM 1999 7 9 VNAA9906007 1 19990628 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 6LK DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 425JS 30664 2895 3037 THE 3RD SET OF EMERGENCY FLOOR LIGHTING INOP. REMOVED AND REPLACED 6LK EMERGENCY BATTERY. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999070900491 19990709 00491 NM 1999 7 9 VNAA9906005 1 19990621 A 3241 AC69895 METERING UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ANTISKID SYS FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 328JS 86381 26787 3030 ANTISKID FAILED ON TAXI OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED BRAKE METERING UNIT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999070900492 19990709 00492 NM 1999 7 9 VNAA9906008 1 19990616 A 2121 011389502 FAN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE GROUND COOLING FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 328JS 96224 38498 3030 DURING ENGINE SHUT DOWN, SMOKE WAS NOTED IN THE COCKPIT. MAINTENANCE INSPECTED AND DEFERRED THE GROUND COOLING FAN IN A CCORDANCE WITH THE MINIMUM EQUIPMENT LIST. LATER ON 17 JUNE 99 THE GROUND COOLING FAN WAS REPLACED AND THE DEFERRAL WAS REMOVED FROM THE AIRCRAFT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999070900493 19990709 00493 NM 1999 7 9 VNAA9906009 1 19990623 A 2121 011390500 FAN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 429JS 10477 3043 THE CABIN FILLED WITH SMOKE AFTER NUMBER ONE ENGINE WAS STARTED. A RE-CIRC FAN FAIL WARNING MESSAGE WAS ALSO NOTED. MA INTENANCE INSPECTED AND CYCLED POWER ON THE AIRCRAFT. THE DISCREPANCY COULD NOT BE DUPLICATED, AND THE AIRCRAFT WAS RET URNED TO SERVICE. ON 23JUNE99 THE AFT RECIRC FAN FAIL WARNING OCCURRED AND THE FAN WAS REPLACED, IN ACCORDANCE WITH DO RNIER MAINTENANCE MANUAL 21-22-01. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999070900494 19990709 00494 NE 1999 7 9 MASA99090 2 19990603 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT MALFUNCTIONED A MASA E L ENGINE SHUTDOWN ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 82YV UE82 114429 PHX - DURING TEST FLIGHT, LEFT PROPELLER RPM STARTED TO DROP OFF. RPM'S WENT FROM 1700 RPM TO 1200 RPM AND CONTINUED DO WN INTO FEATHER. THE CREW SHUT DOWN THE LEFT ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLA CED THE PROPELLER AND THE POWER SECTION. TEAR DOWN INFORMATION WILL BE FORTHCOMING. (X) 2 L 7 2 4T 4 T RT A24CE E26NE 1999070900495 19990709 00495 EU 1999 7 9 RAIA990617 1 19990606 A 7722 3037191 HARNESS AEROSP ATR42 ATR42300 8680920 EU NR 1 ENGINE FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 426TE 228 STL - FLT 7011 - NR 1 ENGINE EXCEEDED TAKEOFF ITT LIMITATIONS. MAINTENANCE REPLACED T-6 CABLE ON NR 1 ENGINE. DOWNLOAD ED FDAU AND DETERMINED THE NR 1 ENGINE WAS NOT OVERTEMPED. (X) 2 H 7 2 4T RT A53EU 1999070900496 19990709 00496 1999 7 9 RAIA990615 4 19990610 A 3420 7012100811 RMU JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 564HK 5416 41081 STL - FLT 7260 - NR 2 RMU INOPERABLE. MAINTENANCE REPLACED NR 2 RADIO MANAGEMENT UNIT. (X) 2 L 7 2 4T RT A41NM 1999070900497 19990709 00497 EU 1999 7 9 RAIA990612 1 19990609 A 7922 L8523427 VERNITHERM BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 435AM 889 STL - FLT 7073 - LEFT ENGINE OIL TEMPERATAURE AT RED LINE. MAINTENANCE REPLACED VERNITHERM FOR LEFT OIL COOLER. (X) 2 L 7 2 4T RT A56EU 1999070900498 19990709 00498 EU 1999 7 9 RAIA990613 1 19990609 A 3246 31485 WHEEL BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA O OTHER O OTHER LD LANDING 1 CE 03 423AM 858 STL - FLT 7476 - LEFT MAIN TIRE BLEW ON LANDING ROLL. MAINTENANCE REPLACED LEFT MAIN WHEEL ASSY. (X) 2 L 7 2 4T RT A56EU 1999070900499 19990709 00499 EU 1999 7 9 RAIA990614 1 19990609 A 3240 215221 BRAKE BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA O OTHER O OTHER LD LANDING 1 CE 03 423AM 12269 1851 858 STL - FLT 7476 - LEFT MAIN TIRE BLEW ON LANDING. MAINTENANCE REPLACED LEFT BRAKE. (X) 2 L 7 2 4T RT A56EU 1999070900500 19990709 00500 SO 1999 7 9 RAIA990618 1 19990610 A 7930 23062618 SENSOR EMB 145 EMB145 SO RT ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 802HK 145066 TRI - FLT 8775 - RIGHT ENGINE OIL PRESSURE TOO HIGH. MAINTENANCE REPLACED OIL PRESSURE SENSOR FOR RIGHT ENGINE. (X) 2 L 7 2 4F RT T00011AT 1999070900501 19990709 00501 EU 1999 7 9 RAIA990619 1 19990610 A 6120 31058993 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 7976 41075 STL - FLT 7516 - IEC FAULT ON BOTH ENGINES. MAINTENANCE REPLACED NTS TRANSUDCER ON LEFT ENGINE. (X) 2 L 7 2 4T RT A41NM 1999070900502 19990709 00502 EA 1999 7 9 UHLA99684 1 19990608 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8311 1386006 EA ROW 11 DISCHARGED A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 804SA 375 GALLEY EMERGENCY LIGHT WAS FOUND INOPERABLE DURING ROUTINE MAINTENANCE. SWAPPED GALLEY BATTERY TO ROW 11 POSITION NR 1. OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A13NM 1999070900503 19990709 00503 EU 1999 7 9 RAIA990609 1 19990607 A 2430 23079009 GENERATOR BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 422AM 14589 160 856 STL - FLT 7444 - RIGHT GENERATOR FAULTED. MAINTENANCE REPLACED GENERATOR. (X) 2 L 7 2 4T RT A56EU 1999070900504 19990709 00504 SO 1999 7 9 RAIA990611 1 19990609 A 2913 14531608401 HOSE EMB 145 EMB145 SO HYDRAULIC PUMP FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 145077 ORD - FLT 5790 - HYDRAULIC LOW LEVEL LIGHT ILLUMINATED. MAINTENANCE REPLACED PRESSURE LINE FOR NR 2 ELECTRIC HYDRAULIC PUMP. (X) 2 L 7 2 4F RT T00011AT 1999070900505 19990709 00505 EU 1999 7 9 RAIA990610 1 19990608 A 7920 L8523427 VERNITHERM BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 432AM 883 STL - FLT 7448 - LEFT ENGINE OIL TEMPERATURE AT RED LINE. MAINTENANCE REPLACED VERNITHERM FOR LEFT OIL COOLER. (X) 2 L 7 2 4T RT A56EU 1999070900506 19990709 00506 EU 1999 7 9 RAIA990608 1 19990606 A 7500 31038761 LINE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 426AM 874 FWA - FLT 7533 - LEFT ENGINE NOT MAKING TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE P3 LINE AND ADJUSTED EGT COMPEN SATOR. (X) 2 L 7 2 4T RT A56EU 1999070900507 19990709 00507 NM 1999 7 9 P2EA99211 1 19990615 A 3250 65462027 TORSION LINKS BOEING 737 737297 1384480 NM NLG MALFUNCTIONED A P2EA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 05 5WM 22629 MCI - FLT 402 - DURING TAKEOFF ROLL, AIRCRAFT DISPLAYED SEVERE NOSE WHEEL SHIMMY. AIRCRAFT RETURNED TO BLOCKS WITHOUT I NCIDENT. REMOVED AND REPLACED UPPER AND LOWER TORSION LINKS ON NOSE LANDING GEAR IAW 31-21-31. REF: OPERATOR CONTROL NR 98ZZZX2533. (X) 2 L 7 2 4F A16WE 1999070900508 19990709 00508 NM 1999 7 9 99ZZZX2533 1 19990615 A 3250 65462883 TORSION LINKS BOEING 737 737297 1384480 NM NLG MALFUNCTIONED A P2EA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 05 5WM 22629 MCI - FLT 402 - DURING TAKEOFF ROLL, AIRCRAFT DISPLAYED SEVERE NOSE WHEEL SHIMMY. AIRCRAFT RETURNED TO BLOCKS WITHOUT I NCIDENT. REMOVED AND REPLACED UPPER AND LOWER TORSION LINKS ON NOSE LANDING GEAR IAW 31-21-31. REF: OPERATOR CONTROL NR P2EA99211. 2 L 7 2 4F A16WE 1999070900509 19990709 00509 1999 7 9 VTZA990141 4 19990602 A 3442 6625941001 RADAR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 481UE 895 SYR/IAD - FLT 7283 - DURING CRUISE AT 2130 HOURS ON 6-2-99, AIRCRAFT DIVERTED TO SCE DUE TO WX RADAR FAILURE IN-FLIGHT. MAINTENANCE REMOVED AND REPLACED WX RADAR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999070900510 19990709 00510 EU 1999 7 9 VTZA990137 1 19990521 A 7712 94959411 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 27 480UE 894 IAD/ROA - FLT 7203 - AT 1900 HOURS ON 5-21-99, AIRCRAFT ABORTED TAKEOFF DUE TO LT ENGINE TORQUE ROLLED BACK ON TAKEOFF R OLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 42397, MEI 76-2. MAINTE NANCE CLOSED DMI 42397 ON 5-22-99 BY REMOVING AND REPLACING LT ENGINE TTL CONTROLLER. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999070900511 19990709 00511 EU 1999 7 9 VTZA990138 1 19990523 A 6120 1680640 MONOPOLE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 491UE 911 IAD/CHO - FLT 7325 - DURING TAKEOFF AT 1628 HOURS ON 5-23-99, AIRCRAFT ABORTED TAKEOFF DUE TO SRI WARNING LIGHT ILLUMINA TED. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 44098. MEL 76-1 ON SRI ON LT ENGINE. MAINTENANCE CLOSED DMI 44098 ON 5-26-99 BY REMOVING AND REPLACING LT PROP GOV MONOPOLE. OPS CHECK OK . AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999070900512 19990709 00512 NE 1999 7 9 P2EA99212 2 19990614 A 7200 ENGINE BOEING 737 737222 1384473 NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A P2EA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 CE 05 603DJ 19955 657173 MCI - FLT 819 - DURING A REDUCED THRUST TAKEOFF, NR 2 EGG WAS IN THE YELLOW BAND. AFTER LIFT-OFF, THE EGT ROSE ABOVE TH E RED-LINE, ABOUT 625 FOR 10 TO 15 SECONDS. RETARDING THE THROTTLES TO BRING THE EGT INTO THE GREEN, RESULTED IN AN EPR READING OF 1.72. AN EPR READING OF 1.85 IS NEEDED FOR CLIMB-OUT. AIRCRAFT RETURNED TO MCI WITH NO INCIDENT. REPLACED NR 2 ENGINE. (X) 2 L 7 2 4F 4 F A16WE E2EA 1999070900513 19990709 00513 CE 1999 7 9 MASA99088 1 19990602 A 2600 114300523 PULL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT CHAFED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 161YV UE161 FKL/PIT - FLT 5952 - CREW NOTICED A NOXIOUS SMELL DURING FLIGHT. MAINTENANCE TROUBLESHOT AND FOUND A CHAFED WIRE IN THE FIRE PULL HANDLE. REMOVED AND REPLACED THE FIRE PULL HANDLE, AND THE AIRCRAFT WAS RETURNED TO SERVICE. HOWEVER, THIS PROBLEM RECURRED LATER IN THE DAY. SEE MRR CONTROL NR MASA99089. (X) 2 L 7 2 4T RT A24CE 1999070900514 19990709 00514 EU 1999 7 9 RAIA990616 1 19990610 A 3610 ASNA213804 O-RING AEROSP ATR42 ATR42300 8680920 EU LT BLEED AIR FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 421TE 102 STL - FLT 7166 - LEFT ENGINE BLEED LEAK. MAINTENANCE REPLACED AN O-RING FOR LEFT SHUT-OFF VALVE. (X) 2 H 7 2 4T RT A53EU 1999070900517 19990709 00517 EA 1999 7 9 99ZZZX2536 1 19990615 A 3230 HJ6G BEARING AIRSCIENCES 7490 DHAV DHC3 DHC3 2800202 EA NLG WORN A FYWA O OTHER O OTHER NR NOT REPORTED 1 AL 05 68086 288 BALL END BEARING WORN CAUSING GEAR LOCK ON LEFT NOSE TO LOCK INTERMITTENTLY. UPON LEFT TURN, LEFT NOSE GEAR EXTENDED OU T OF UP AND LOCKED LOCATION. REPLACED BALL END AND ADJUSTED. PERFORMED RETRACT TEST, RESULTS GOOD. UPLOCK INDICATOR A ND GOOD VISUAL ON LOCK FUNCTION. 1 H 7 1 3R A815 1999070900524 19990709 00524 CE 1999 7 9 99ZZZX2544 1 19990622 A 2720 12606311 ROD END CESSNA 206 U206G 2073356 CE RUDDER BAR BROKEN A HYTA K NONE O OTHER IN INSP/MAINT 1 AL 01 46374 9739 U2060517 ROD END BROKE WHERE IT EXITS SPACER ASSY, PN 1260632-3, WHICH IS THE RUDDER TRIM SPROCKET AT THE END OF THE STEERING BUN GEE. SUBMITTER STATED THIS IS THE THIRD ONE KNOWN TO BREAK IN 10 YEARS. NO NOSE WHEEL STEERING, BUT STILL RUDDER STEER ING. 1 H 7 1 3O A4CE 1999070900528 19990709 00528 CE 1999 7 9 99ZZZX2549 1 19990618 A 3213 508103237 TORQUE KNEE BEECH 99 99 1154002 CE LT MLG CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 95WA U6 THE TORQUE KNEES (UPPER AND LOWER) WERE FOUND CRACKED DURING INSPECTION. CRACK NEAR CENTER PIVOT BOLT AREA. 1 L 7 2 3T A14CE 1999070900529 19990709 00529 EA 1999 7 9 99ZZZX2550 1 19990621 A 5753 6001425025 BEAM 60014002805 CNDAIR CL600 CL6002B16 1900305 EA TE FLAP CORRODED A ACNA K NONE O OTHER IN INSP/MAINT 1 WP 01 716RD 5573 5048 DURING INSPECTION OF FLAP COMPONENTS, CORROSION IN THE FLAP BEAM ASSY BORE HOLE WAS DISCOVERED. BOMBARDIER SERVICE ENGI NEERING DETERMINED THAT ANY CORROSION IN THE BORE HOLE IS CAUSE FOR REMOVAL AND SCRAP. ALL 6 BEAM ASSEMBLIES (3 EACH WI NG) WERE REMOVED AND REPLACED WITH UPGRADED PARTS FROM BOMBARDIER. 2 L 7 2 4F RT A21EA 1999070900540 19990709 00540 WP 1999 7 9 TWAA9909401 1 19990706 A 3350 4TL1110B SWITCH DOUG DC9 DC983 3022083 WP COCKPIT WORN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9620D 53591 THE CABIN EMERGENCY LIGHTS WOULD NOT OPERATE FROM THE COCKPIT SWITCH. REPLACED THE S1-177 COCKPIT SWITCH, (P/N 4TL11-10 B) AND THE BATTERY PACK AT CABIN ROW 50, (P/N 60030451LB). CHECK-C 10-26-98 STL. 2 L 7 2 4F RT A6WE 1999070900541 19990709 00541 WP 1999 7 9 AT9900484 1 19990705 A 3610 39245411 REGULATOR DOUG DC9 DC932 3022066 WP TAIL COMPT DEFECTIVE A ZZDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 15 834AT 47488 TAIL COMPARMENT TEMPERATURE HIGH LIGHT CAME ON. REMOVED AND REPLACED TAIL COMPARTMENT TEMPERATURE HIGH SENSORS AND PNEU MATIC PILOT PRESSURE REGULATOR IAW MM 36-20-2 AND 36-10-2. 2 L 7 2 4F A6WE 1999070900542 19990709 00542 WP 1999 7 9 AT9900485 1 19990630 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 927 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND CORROSION ON LONGERON STRAP AT BS 927 L-23L. FABRICATED REPAIR LONG ERON STRAP, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 53-11-3, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999070900543 19990709 00543 WP 1999 7 9 AT9900486 1 19990624 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 383-509.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND LEFT WING UPPER SURFACE FORWARD OF AILERON TRIM TAB AT XRS 383-509.5 WITH SPOTS OF CORROSION. FABRICATED DOUBLER AND FILLER, ALODINED, PRIMED AND COMPLETED REPAIRS ON LEFT WING IAW DC9 SR M 51-30-3, 57-01 FIG 1, PG 5, 51-10-2 AND 51-30-2. 2 L 7 2 4F A6WE 1999070900544 19990709 00544 WP 1999 7 9 AT9900487 1 19990702 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 408 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND WRINKLE ON THE LEFT HAND EXTERNAL FUSELAGE IN LOWER SKIN AT BS 408 L -28L TO 28R. FABRICATED AND INSTALLED SKIN REPAIR IAW DC9 SRM 53-04 FIG 38, 51-10-3 AND TIMCO EO NR 99-1183. 2 L 7 2 4F A6WE 1999070900545 19990709 00545 WP 1999 7 9 AT9900488 1 19990612 A 5347 TIE DOWN DOUG DC9 DC932 3022066 WP BS 889 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE AFT CARGO TIE DOWN CLOSE OUT RING CORRODED AT BS 889. FABRICATE D NEW CLOSE OUT RING IAW DC9 SRM 53-01 FIG 1 AND 51-10-4. 2 L 7 2 4F A6WE 1999070900546 19990709 00546 WP 1999 7 9 AT9900489 1 19990705 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 353-477 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE RIGHT HAND WING TOP SIDE AFT OF THE TRAILING EDGE SKIN FROM XRS 353-477 CORRODED. FABRICATED SKIN DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2, 51-10-3, 51-30-1 A ND 51-70-2. 2 L 7 2 4F A6WE 1999070900547 19990709 00547 WP 1999 7 9 AT9900490 1 19990630 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 458 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THREE DENTS WITH CREASES AT BS 458R L-19R IN CLOSED PROXIMITY TO AN EXISTING REPAIR AND TO EACH OTHER. REPAIRED DENTS AT BS 458 IAW DC9 SRM 51-10-3, 51-30-2, 51-30-5 AND TIMCO EO NR 99-11 82. 2 L 7 2 4F A6WE 1999070900548 19990709 00548 NM 1999 7 9 QXEA9901373 1 19990623 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM ROW 1 FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 357PH 504 SEA- FLOOR EVACUATION LIGHTS INOP. MAINTENANCE REPAIRED A BROKEN CONNECTOR AT ROW 1, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999070900549 19990709 00549 NM 1999 7 9 QXEA9901374 1 19990624 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 824PH 15672 423 157 PDX- COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. MAINTENANCE REPLACED THE OVERHEAD LIGHT ASSEMBLY, OPERATIONAL CHECKS GOO D. 2 H 7 2 4T RT A13NM 1999070900550 19990709 00550 NM 1999 7 9 QXEA9901421 1 19990625 A 3231 MECHANISM DHAV DHC8 DHC8202 2809007 NM LT MLG DOOR OUT OF ADJUST A QXEA K NONE O OTHER CL CLIMB 1 NM 09 830PH 526 PDX- FORWARD LEFT GEAR DOOR HANGS DOWN IN FLIGHT. MAINTENANCE ADJUSTED THE PIVOT FRAME SHIM THICKNESS AND ADDED TEFLON WASHER TO PIVOT FRAME, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999070900551 19990709 00551 NM 1999 7 9 QXEA9901422 1 19990624 A 6120 M39016 RELAY DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTION A QXEA K NONE O OTHER CL CLIMB 1 NM 09 364PH 520 SEA- NO AUTOFEATHER SELECT OR ARM AFTER TAKEOFF. MAINTENANCE RERACKED THE ADVISORY LIGHT CONTROL BOX. REPLACED THE ARM CONTROL RELAY 6121-K5, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999070900552 19990709 00552 NM 1999 7 9 QXEA9901433 1 19990705 A 3150 8006221 CONTROL BOX DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTION A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 364PH 520 PDX- MASTER WARNING AND SMOKE WARNING ILLUMINATED INTERMITTANTLY. MAINTENANCE INSPECTED CANNON PLUGS AT CARGO BAY SMOKE DETECTORS, NO DEFECTS. REPLACED MASTER WARNING CONTROL BOX, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999070900553 19990709 00553 NM 1999 7 9 99UAL900340 1 19990625 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 658UA 27113 FLIGHT DIVERTED TO LHR UNDER AMBER ALERT DUE TO SMOKE AND ELECTRICAL FUMES IN MID GALLEY WITH VARIOUS ITEMS TURNED ON OR OFF. *S/D* LHR FOUND OVEN R41 SMELLING BADLY WHEN TURNED ON. PULLED AND COLLARED C-B FOR OVEN R41. AT COMPLETION ON FLT 953 IN ORD ON 6/25/99, REPLACED OVEN AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 1999070900554 19990709 00554 NM 1999 7 9 99UAL900341 1 19990628 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 504UA 24625 MULTIPLE FUSELAGE DENTS FORWARD OF 2L. CONTACT BY JETWAY. EXTERNAL REPAIR DOUBLER ENCOMPASSING MULTIPLE SITE DAMAGE. M AJOR REPAIR MRA 096 ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999070900555 19990709 00555 NM 1999 7 9 99UAL900342 1 19990625 A 3350 321430 BATTERY AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE LT EMER EXIT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 821UA 944 MID LEFT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT BATTERY INOP. REPLACED BATTERY (PSU P/N IS 565-0038). 2 L 7 2 4F 4 F RT A28NM E40NE 1999070900556 19990709 00556 NM 1999 7 9 99UAL900343 1 19990625 A 2910 BACH6M0150AAN HOSE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TAIL SKID RUPTURED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 7274U 21421 SHORTLY AFTER TAKEOFF THE FLIGHT EXPERIENCED THE LOSS OF FLUID AND PRESSURE FROM THE A HYDRAULIC SYSTEM. RETURNED TO S TL. *S/D* FOUND PRESSURE LINE GOING TO TAIL SKID ACTUATOR RUPTURED. REPLACED LINE, BOTH ENGINE DRIVEN PUMPS AND CASE DRAIN FILTERS PER MAINTENANCE MANUAL. ALSO, SERVICED HYDRAULIC SYSTEM TO FULL. RAN ENGINES, NO OTHER LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1999070900557 19990709 00557 NM 1999 7 9 99UAL900344 1 19990628 A 2150 ACM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ROW 12-13 VIBRATION A UALA A J UNSCHED LANDING DUMP FUEL E VIBRATION/BUFFET CL CLIMB 1 WP 29 766UA 26917 EN ROUTE CDG-IAD, DURING CLIMBOUT AIRFRAME VIBRATION NOTED AT ROWS 12-13. DIVERTED TO LHR. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999070900558 19990709 00558 NM 1999 7 9 99UAL900345 1 19990628 A 2530 OVEN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 791UA 26933 BURNT PLASTIC SMELL IN MID GALLEY. FOUND AND REMOVED MELTED PLASTIC FROM WARMING OVEN AT POSITION W31. SEA CLEANED INS IDE OF WARMING OVEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999070900559 19990709 00559 NM 1999 7 9 99UAL900346 1 19990629 A 2750 65235526 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FLAP CONTROL FAILRF A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7266U 21413 A HYDRAULIC SYSTEM PRESSURE INDICATION ZERO. ENGINE NR 1 AND NR 2 PUMP LOW PRESSURE LIGHTS ON. *S/D* REPLACED FAILED DRAIN PLUG ON FLAP CONTROL VALVE AND SERVICED HYD SYSTEM. OPERATIONALLY CHECKED SYSTEM. NO LEAKS FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1999070900560 19990709 00560 NM 1999 7 9 99UAL900347 1 19990629 A 2530 COFFEE MAKER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 205UA 28714 ELECTRICAL SMELL AND SPARKING IN AFT GALLEY 441 IN THE AREA OF COFFEEMAKERS. RESET ALL BREAKERS AND TURNED POWER BACK O N TO AFT GALLEY, INSPECTED ALL VISABLE WIRES AND REPLACED COFFEE MAKERS FOR PRECAUTIONARY MEASURES; WAITED 45+ MINUTES W ITH POWER ON GALLEY EQUIPMENT AND NO SMELLS OR FLASHES NOTED AS CREW REPORTED. GALLEY AND EQUIPMENT OPERATES NORMALLY. HOME SHOP CHECKED THE REMOVED COFFEE MAKERS AND NO FAULTS WERE FOUND. ACCOMPLISHED VISUAL CHECKS OF THE WIRING ABOVE GA LLEY CEILING PANELS, THE WIRING BEHIND THE GALLEY CONTROL PANEL, THE COFFEE MAKER COMPARTMENT WIRING AND CONNECTORS. FO UND NO DAMAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999070900561 19990709 00561 NM 1999 7 9 99UAL900350 1 19990630 A 2131 CONTROLLER HAMILTON STA 7638101 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 7263U 21410 OVER BVL, AIRCRAFT LOST CABIN PRESSURE. CABIN ALTITUDE CLIMBED ABOUT I000 FEET PER MINUTE TO FL 140. DESCENDED TO FL 1 40. FLIGHT DIVERTED TO SLC. *S/D* REPLACED PRESSURE CONTROLLER AND PERFORMED AN OPERATIONAL CHECK. 2 L 7 3 4F 4 F A3WE E2EA 1999070900562 19990709 00562 NM 1999 7 9 99UAL900351 1 19990630 A 3246 WHEEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG OUT OF BALANCE A UALA A J UNSCHED LANDING DUMP FUEL O OTHER TO TAKEOFF 1 WP 29 7285U 21563 DURING TAKEOFF, THERE WAS A LOUD BANG AND SEVERE VIBRATION. DUMPED FUEL AND RETURNED TO DEN. *S/D* ACCOMPLISHED CHECK OF AIRCRAFT FOR DAMAGE DUE TO EXCESSIVE VIBRATION FROM NOSE GEAR SHIMMY AND CHECK FOR SOURCE OF ABNORMAL NOISE. NO DEF ECTS NOTED ON GROUND. AS PRECAUTION REPLACED BOTH NOSE GEAR TIRE AND WHEEL ASSYS PER MAINTENANCE MANUAL AND LUBED NOSE GEAR. ACCOMPLISHED NOSE GEAR EXTENSION AND RETRACTION TEST PER MAINTENANCE MANUAL. NO DEFECTS NOTED. ENGINEERING NOTE : AS OF JULY 7,1999, 35 FLIGHTS HAVE OCCURRED SINCE THIS INCIDENT WITH NO FURTHER WRITE-UPS FOR ABNORMAL NOISE OR VIBRA TION. 2 L 7 3 4F 4 F A3WE E2EA 1999070900563 19990709 00563 WP 1999 7 9 ABXA9900565 1 19990701 A 5312 577263833 BULKHEAD BEAM DOUG DOUG DC8 DC861 3021952 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 852AX 46016 THE J-BEAM ON AFT SIDE OF AFT PRESSURE BULKHEAD AT STATION 1766 WAS CRACKED. REPAIRED IAW ABX REA D853-28119MR. 2 L 7 4 4F 4A25 1999070900564 19990709 00564 WP 1999 7 9 ABXA9900566 1 19990706 A 5313 5750198 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 870 & 879 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 852AX 46016 LONGERONS 24 LEFT AND 24 RIGHT CRACKED AT STATIONS 870 AND 879. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1999070900565 19990709 00565 NE 1999 7 9 RRXA991168 2 19990701 A 7310 215174 FUEL FILTER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE CONTAMINATED A RRXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 15 8079U 45947 ON CLIMB-OUT LEAVING BNA OUT OF 9.0 NR 1 ENG FLAMED OUT MADE PRECAUTIONARY SHUT DOWN WAITED 2 MINS PERFORMED RELIGHT PRO CEDURE ENG RELIT AND PERFORMED OK IN TO DAY. INSPECTED NR 1 ENG IAW DC-8 MM. NO DEFECTS FOUND, TAXIED ACFT TO RUN UP P AD RAN AT ALL PWR SETTINGS, OPS CKS GOOD. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER PRECAUTIONARY OPS AND LKS CKS GO OD. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999070900566 19990709 00566 WP 1999 7 9 RRXA991169 1 19990703 A 2120 UNKNOWN DOUG DC8 DC863 302198A WP COCKPIT ODOR A RRXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 951R 46092 HAD ELECTRICAL FIRE ODOR IN COCKPIT, ALL AC LOADS HIGH. ODOR STOPPED. LOADS NORMAL AND CENTER RECIRC FAN INOP. DEFERR ED CENTER RECIRC FAN PER MEL 21-16-2, CONT NR C8993221-2369. CAT C. DUE 07-17-99. PLACARD INSTALLED, CURRENT LIMITERS R EMOVED. 2 L 7 4 4F 4A25 1999070900567 19990709 00567 WP 1999 7 9 RRXA991153 1 19990622 A 3230 4771392501 PIN DOUG DC8 DC871F 302199D WP MLG FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 500MH 45812 ON GEAR RETRACTION LOUD BANG FROM REAR OF AIRCRAFT DOORS AND LANDING GEAR UNSAFE LIGHTS ON IN FRONT OF COCKPIT, FE LEFT GEAR DOOR LIGHT ON. AIRCRAFT FERRIED TO KMQY FOR REPAIR. INSTALLED NEW BOSS PIN PER S/B 32-102R5-6/12/72, EWW MA AI32 10-01:03 AND 8110-3, E099417 NR 1420 4671. 2 L 7 4 4F RT 4A25 1999070900568 19990709 00568 NM 1999 7 9 AALA990597 1 19990406 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 1050 BELLFRAME FLANGE 8 WEB BENT STATION 1050, STRINGER 26 AND 25 LEFT. REPAIRED BELLFRAME PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999070900569 19990709 00569 NM 1999 7 9 AALA990598 1 19990406 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND STATION 1070 BELLFRAME FLANGE AND WEB STRINGER 26 AND 25 LEFT. INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999070900570 19990709 00570 NM 1999 7 9 AALA990599 1 19990409 A 5711 SPAR BOEING 727 727223 1384074 NM WS 213-216 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - RIGHT WING FSS 213-216 LOWER CHORD ANGEL LOWER LEFT HAS EXFOLIATING CORROSION, UPPER SURFACE AROUND AND UNDER STRU T ROD MOUNT BRACKET. REMOVED AND BLENDED CORROSION PER SRM 57-10-1. REPAIRED PER AARD 57-30-00-2. (M) 2 L 7 3 4F A3WE 1999070900571 19990709 00571 NM 1999 7 9 AALA990529 1 19990413 A 3250 RETRACT MECH BOEING 727 727223 1384074 NM NLG LACK OF LUBE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 713AA 22469 CUN - FLT 928 - EN ROUTE GUA-MIA, AFTER TAKEOFF AND RETRACTING GEAR, RED NOSE GEAR LIGHT STAYED ILLUMINATED. ALL INDICA TIONS INDICATED THE NOSE GEAR WAS NOT RETRACTED. FLIGHT AIR INTERRUPTED AND LANDED CUN WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND MAINTENANCE FERRY TO MIA. MIA MAINTENANCE INSPECTED NOSE LANDING GEAR FOR DAMAGE AND CONDITION WITH NO IR REGULARITIES NOTED. MAINTENANCE CLEANED AND LUBRICATED RETRACT AND LOCK ACTUATORS. SWUNG NOSE LANDING GEAR SEVERAL TIM ES WITH SYSTEM OPERATING NORMALLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070900572 19990709 00572 NM 1999 7 9 AALA990545 1 19990418 A 2810 1520001CAP CAP BOEING 727 727223 1384074 NM LT WING LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 872AA 21384 DFW - FLT 1840 - AFTER TAKEOFF, A FLUID LEAK WAS REPORTED COMING FROM THE LEFT WING IN THE AREA OF THE OVERWING FUEL CAP . FLIGHT AIR INTERRUPTED AND RETURNED DFW LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND FUEL IN RE AR SPARE AREA. AIRCRAFT WAS TAKEN OUT OF SERVICE AND MOVED TO THE HANGAR FOR FURTHER EVALUATION. INSPECTED LEFT WING U PPER AND LOWER WING SURFACES, SEAMS, AND REAR SPAR WITH NO LEAKS DETECTED. REPLACED O-RING ON LEFT OVERWING FUEL CAP. A IRCRAFT WAS MOVE AND REINSPECTED WITH NO LEAKS DETECTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070900573 19990709 00573 WP 1999 7 9 AALA990695 1 19990512 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP AC BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 431AA 49343 LAX - FLT 1496 - DURING TAKEOFF WITH FULL POWER, FLIGHT ATTENDANT NOTICED A STRONG ODOR IN THE CABIN. FLIGHT CREW NOTIC ED THE SAME SMELL AND DECIDED TO RETURN LAX. FLIGHT AIR INTERRUPTED AND RETURNED LAX WITHOUT FURTHER INCIDENT. MAINTEN ANCE FOUND EVIDENCE OF BIRD INGESTION IN LEFT ENGINE. INSPECTED LEFT ENGINE WITH NO DAMAGE NOTED. REPLACED COALESCER B AGS AND RAN PACKS WITH AN ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070900574 19990709 00574 NM 1999 7 9 AALA990693 1 19990511 A 2612 FBD1553503 HARNESS BOEING 767 767323 1385205 NM LT ENGINE DEFECTIVE A AALA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 371AA 25198 GIG - FLT 904 - DURING CLIMB-OUT AT FL280, NR 1 ENGINE FIRE STATUS MESSAGE ILLUMINATE. CREW RAN CHECKLISTS AND RETARDED NR 1 ENGINE AND STATUS MESSAGE QUIT. STATUS MESSAGE WAS INTERMITTENT WHILE DUMPING FUEL. FLIGHT RETURNED GIG AND LAND ED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED REQUIRED CHECKS AND PLCARDED NR 1 ENGINE FIRE LOOP. DURING OVERN IGHT MAINTENANCE, NR 1 ENGINE FIRE LOOP DETECTION FAULTED DURING TEST. REPLACED NR 1 ENGINE FIRE LOOP HARNESS. REQUIRE D CHECKS PRODUCED NO FAULTS. PLACARD WAS REMOVED AND MIC SHEET CLEARED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999070900575 19990709 00575 WP 1999 7 9 AALA990687 1 19990507 A 3233 SS093200147001 ACTUATOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 581AA CHC513A 53158 PHX - FLT 1538 - AFTR TAKEOFF, GEAR FAILED TO RETRACT. CREW ACCOMPLISHED CHECKLISTS AND RETURNED PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE GEAR OVER CENTER ACTUATOR. ACCOMPLISHED EXTENSION AND RETRACTION CHECKS A ND LEAK CHECKS WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070900576 19990709 00576 WP 1999 7 9 AALA990686 1 19990507 A 3233 39281375001 ACTUATOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 581AA CHC683A 53158 PHX - FLT 1538 - AFTER TAKEOFF, GEAR FAILED TO RETRACT. CREW ACCOMPLISHED CHECKLISTS AND RETURNED PHX AND LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE REPLACED NOSE GEAR RETRACT ACTUATOR. ACCOMPLISHED EXTENSION AND RETRACTION CHECKS AND LEAK CHECKS WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070900577 19990709 00577 WP 1999 7 9 AALA990683 1 19990505 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP A/C BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 426AA 49338 ORD - FLT 366 - DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED A STRONG HOT BURNING METAL SMELL IN AFT COACH CABIN. FLIGHT AIR INTERRUPTED AND RETURNED ORD WITHOUT FURTHER INCIDENT. BURNIG SMELL DISSIPATED WHEN AIRCRAFT LANDED. MAINTENANCE TROUBLE SHOT SYSTEM UNABLE TO DUPLICATE SMELL. AS A PRECAUTIONARY, MAINTENANCE REMOVED AND REPLCED COALESCER BAGS AND P ERFORMED PACK BURN OUT PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999070900578 19990709 00578 WP 1999 7 9 AALA990679 1 19990507 A 2150 20495061 TURBINE DOUG DC9 DC982 3022082 WP LT ACM SEIZED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 70524 311265 49916 DFW - FLT 817 - DURING TAKEOFF, FLT ATTENDANT REPORTED AN UNUSUAL ODOR WITH SMOKE IN THE CABIN. FLIGHT AIR INTERRUPTED, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND THE LEFT ACM SEIZED. MAINTENANCE REPLACED LEFT ACM. SYSTEM OPERATED NORMAL WITH NO LEAKS NOTED DURNG LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F A6WE 1999070900579 19990709 00579 NM 1999 7 9 AALA990671 1 19990505 A 3260 2314143 SWITCH BOEING 727 727223 1384074 NM RT MLG DOOR DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 897AA 22013 DFW - FLT 594 - AFTER TAKEOFF, THE RIGHT MAIN GEAR DOOR OPEN LIGHT STAYED ILLUMINATED AFTER RAISING THE GEAR HANDLE. CR EW RAN CHECKLIST PROCEDURES AND THE RIGHT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDE D OVERWEIGHT WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOOR SWITCH. CYCLED LANDING GEAR SEVERAL TIMES. OVERWEIGHT LA NDING INSPECTION REVEALED NO FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070900580 19990709 00580 NM 1999 7 9 AALA990669 1 19990505 A 3260 LAMP BOEING 727 727227 1384078 NM RT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 728AA 20735 MCO - FLT 478 - AFTER TAKEOFF, RIGHT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED INTERMITTENTLY. LANDED MCO WITHOUT INCIDENT . RELAMPED RIGHT MAIN GEAR INDICATION MODULE. CHECKED TARGET SWITCHES FOR SECURITY AND CLEANED SWITCHES. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999070900581 19990709 00581 NM 1999 7 9 AALA990600 1 19990319 A 5330 SKIN BOEING 727 727223 1384074 NM BS 383-391 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - PREVIOUSLY WORKED GOUGES IN SKIN HAVE CORROSION AT STATION 383 TO 391, STRINGER 7L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 USING .050 2024T3 MATERIAL. (M) 2 L 7 3 4F A3WE 1999070900582 19990709 00582 NM 1999 7 9 AALA990601 1 19990323 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1301 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - DENT IN FUSELAGE AT STATION 1303, STRINGER 23R. FABRICATED DOUBLER 2024T3, .063 THICK 9 INCH BY 7.5 INCH, ATTACHE D WITH (63 EACH) BACR15CE5 RIVETS AND (12 EACH) BACR15CE SIX RIVETS. (M) 2 L 7 3 4F A3WE 1999070900583 19990709 00583 NM 1999 7 9 AALA990602 1 19990329 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND TOP OF FLOORBEAM AT BS 380 IS CORRODED FROM RBL 48 TO 64 RBL. FLOORBEAM REPAIR COMPLETE AFT FLANGE OF UPPER CHORD STATION 380 RBL 48 TO 65 AS PER AARD 53-10-07-02 PAGE 1-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999070900584 19990709 00584 NM 1999 7 9 AALA990603 1 19990323 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND CORROSION ON BELT FRAME AT BS 720B FROM STRINGER 5R-6R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 USING .071 7075T6 MATERIAL AND .1875 '0' HI-LOCKS. (M) 2 L 7 3 4F A3WE 1999070900585 19990709 00585 NM 1999 7 9 AALA990604 1 19990404 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - CUT OUT DAMAGE AT FS 720A PLUS 10 INCHES SPLICED IN NEW STRINGER. MATERIAL PER SRM 53-10-3 FIG 5. FASTENERS THRO UGH SKIN FOUR .1875 HI-LOCKS PER SIDE OF SPLICE ALSO THROUGH LIP OF STRINGER. FOUR .15625 HI-LOCKS THROUGH SIDE OF 'J' CHANNEL PER SIDE, EACH SIDE OF SPLICE. (M) 2 L 7 3 4F A3WE 1999070900586 19990709 00586 NM 1999 7 9 AALA990668 1 19990419 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1243 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CRACK IN STRINGER 11R AROUND FASTENER JUST AFT OF FS 124. REPAIRED PER ESO 11597 DATED 4/19/99. (M) 2 L 7 3 4F A3WE 1999070900587 19990709 00587 NM 1999 7 9 AALA990605 1 19990404 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - CUT OUT CRACK AND REPAIRED STRINGER 15R FORWARD SIDE OF WING SCANNING LIGHT. MATERIAL PER SRM 53-10-3 FIG 5. FAS TENERS SIX .1875 HI-LOCKS THROUGH SKIN AND STRINGER THREE .1875 HI-LOCKS THROUGH SIDE OF U-CHANNEL PER SIDE, TWO .15625 HI-LOCKS THROUGH STRINGER CLIP AND STRINGER PER SIDE. (M) 2 L 7 3 4F A3WE 1999070900588 19990709 00588 NM 1999 7 9 AALA990606 1 19990419 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - REF E58 NR 3150893, STRINGER 15L CRACKED AT BS 720B PLUS 15 INCHES AT AFT EDGE OF ICE LIGHT HOUSING. REPAIR STRIN GER 15L BS 720B PLUS 15 INCHES AT AFT EDGE OF ICE LIGHT PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999070900589 19990709 00589 NM 1999 7 9 AALA990607 1 19990323 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FRAME DENTED BETWEEN STRINGER 25L AND 24L AT FS 700. REMOVED DAMAGED AREA. INSTALLED DOUBLER 7075T6, .063 FIVE I NCHES LONG WITH FOURTEEN MS20470D, .1875 INCH AND FOUR MS20470D .25 INCH RIVETS, THREE ROWS TOTAL. (M) 2 L 7 3 4F A3WE 1999070900590 19990709 00590 EU 1999 7 9 AALA990323 1 19990311 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1471G 11507 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999070900591 19990709 00591 NM 1999 7 9 AALA990609 1 19990330 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - BELT FRAME, BENT FLANGE AND WEB STATION 950F BETWEEN 26L AND 25L. INSTALLED DOUBLER ON BELT FRAME AT STATION 950F BETWEEN STRINGER 25L AND 26L IAW AARD 53-10-07-3. DAMAGED AREA OF FREE FLANGE AT WEB CUT OUT WAS 1 INCH BY 1.5 INCH. D OUBLER USED WAS 2024 T4 .071 THICK. INSTALLED ONE ROW OF .1875 INCH BOEING HEAD SCREWS (NAS 8603-2) IN FREE FLANGE OF D OUBLER. INSTALLED TWO ROWS OF 1ST OVER HI-LOKS IN FRONT SIDE OF DOUBLER WEB. HI-LOKS WERE BACBB30FN6. (M) 2 L 7 3 4F A3WE 1999070900592 19990709 00592 NM 1999 7 9 AALA990610 1 19990117 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1161 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - FOUND BELL FRAME CORRODED, STATION 1166, STRINGER 26L TO 27L. INSTALLED DOUBLER ON BELL FRAME AS PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999070900593 19990709 00593 NM 1999 7 9 AALA990611 1 19990408 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 FOUND BELL FRAME BENT IN WEB STATION 1130, STRINGER 26R TO STRINGER 25R. CUT OUT DAMGED AREA AND INSTALLED DOUBLER REPA IR PER 51-40-5 (AARD 53-10-07-3). (M) 2 L 7 3 4F A3WE 1999070900594 19990709 00594 NM 1999 7 9 AALA990656 1 19990422 A 5312 BULKHEAD ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION AT 'T' ANGLE UPPER SURFACE AT AFT PRESSURE BULKHEAD AT NR 1 SEAT TRACK INTERFACE. REMOVED DAMGED SECTION OF 'T' ANGLE AND INSTALLED NEW SECTION PER AARD 51-10-00-1 PAGE 1. (M) 2 L 7 3 4F RT A22WE 1999070900595 19990709 00595 NM 1999 7 9 AALA990667 1 19990405 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1243 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND CRACKS IN STRINGER 15R AND 17R AT STATION 1243, BOTH CRACKS IN RADIUS, BOTH CRACKS APPROX .75 INCH LONG. IN STALLED STRINGER REPAIR PER SRM 53-10-3 FIG 2. (M) 2 L 7 3 4F A3WE 1999070900596 19990709 00596 NM 1999 7 9 AALA990666 1 19990428 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1130-1136 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND FASTENER HEADS DISHED STATION 1130-1136, STRINGER 27L, STRINGER 27L CORRODED UNDER SKIN. CUT OUT SKIN STATI ON 1130 TO 1140 FOR ACCESS TO STRINGER. REMOVED CORROSION AND REPAIRED STRINGER 27L PER ESO 11697 DATED 4-27-99. REPAI RED SKIN CUT OTU PER SRM 53-30-3 FIG 5. (M) 2 L 7 3 4F A3WE 1999070900597 19990709 00597 NM 1999 7 9 AALA990665 1 19990503 A 5311 FRAME BOEING 727 727227 1384078 NM BS 620 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CRACK FOUND IN OUTER CHORD WEB APPROX .4375 INCH LONG, END OF CRACK MARKED CRACK IS NEAR AFT LOWER CORNER OF DOOR CUTOUT, FORWARD CARGO. STOP DRILLED CRACK. INSTALLED .050 2024-T3, 5.5 BY 4 DOUBLER WITH 4 ROWS OF FASTENERS CON SISTING OF 5 BACB30MC6 HI-LOKS AND 13 MS20470D RIVETS. (M) 2 L 7 3 4F A3WE 1999070900598 19990709 00598 NM 1999 7 9 AALA990646 1 19990626 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND CORROSION ON FLOORBEAM, FS 380, RBL 50 1 INCH BY 4 INCH. CORROSION REMOVED AND PATCH INSTALLED TO REPLACE U PPER FLANGE OF FLOORBEAM PER SRM 53-10-8 FIG 3. (M) 2 L 7 3 4F A3WE 1999070900599 19990709 00599 WP 1999 7 9 AALA990688 1 19990430 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1260 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 575AM 53152 TUL - FOUND SEAT TRACK NR 2 HAS CORROSION ON FLOORBOARD OUTBOARD LANDING STATION 1260. BLENDED AREA, REMOVED CORROSION AND INSTALLED STRAP PER AARD 53-20-00-13 PAGE 1-2. (M) 2 L 7 2 4F A6WE 1999070900600 19990709 00600 NM 1999 7 9 AALA990699 1 19990512 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - FOUND STRINGER NR 10 CRACKED OUTBOARD END. INSTALLED NEW STRINGER END WITH SPLICE PER ESO 4100 DATED 5-10-99 AND SRM 57-20-00. (M) 2 L 7 3 4F RT A22WE 1999070900601 19990709 00601 NM 1999 7 9 AALA990754 1 19990517 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND CORROSION ON INNER SKIN AT STATION 720B PLUS 2 TO 720B TO 10 IN AREA OF RAM AIR DOOR ACT ROD STRINGER 28L. R EMOVED CORROSION AND INSTALLED REPAIR PER 53-30-3 FIG 1 SHEET 4. (M) 2 L 7 3 4F A3WE 1999070900602 19990709 00602 NM 1999 7 9 AALA990753 1 19990521 A 5330 SKIN BOEING 727 727227 1384078 NM BS 685-688 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND FUSELAGE OUTER SKIN CORRODED (BULGING) AT STRINGER 23 STATION 685-688. REMOVED CORROSION ON SKIN TREATED AN D PRIMED CUT OUT CORRODED STRINGER SECTION 680-685. INSTALLED STRINGER SPLICE PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999070900603 19990709 00603 NM 1999 7 9 AALA990752 1 19990521 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 375 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND STRINGER 23 RT DENTED AT STATION 375 ON LOWER WEB. DYE CHECKED, NO CRACKS FOUND. INSTALLED 'U' CHANNEL REP AIR PER SRM 53-10-3 FIGURE NR 2. (M) 2 L 7 3 4F A3WE 1999070900604 19990709 00604 NM 1999 7 9 AALA990751 1 19990517 A 5330 SKIN BOEING 727 727227 1384078 NM BS 692 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND DENT IN SKIN AT STATION 692, STRINGER 7-8L. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-30-3 FIG 13. (M ) 2 L 7 3 4F A3WE 1999070900605 19990709 00605 NM 1999 7 9 AALA990750 1 19990514 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1095 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND CRACK IN SKIN AT STATION 1095 STRINGER 2 UNDER DOGHOUSE. CUT OUT DAMAGED AREA AND INSTALLED .063 DOUBLER PE R SRM 53-30-3 FIGURE 3. (M) 2 L 7 3 4F A3WE 1999070900606 19990709 00606 NM 1999 7 9 AALA990749 1 19990519 A 5330 SKIN BOEING 727 727227 1384078 NM BS 683-685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND STATION 683 - STATION 685 OUTBOARD STRINGER 26L, INNER SKIN CAP CORRODED. CUT OUT DAMAGED AREA OF SKIN AND INSTALLED DOUBLER AND FILLERS PER SRM 53-30-3 FIGURE NR 3. (M) 2 L 7 3 4F A3WE 1999070900607 19990709 00607 NM 1999 7 9 AALA990748 1 19990521 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1090 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - BELL FRAME DENTED STATION 1090 BETWEEN STRINGER 26L AND 27L. REMOVED DAMAGE AND REPAIRED PER SRM 53-10-4 FIGURE 1 PAGES 3, 4, 5. (M) 2 L 7 3 4F A3WE 1999070900608 19990709 00608 NM 1999 7 9 AALA990747 1 19990521 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 700 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND SHEAR TIE CRACKED AT FS 700 RBL 0. INSTALLED NEW SHEAR TIE AT STATION 700 BL 0 . (M) 2 L 7 3 4F A3WE 1999070900609 19990709 00609 NM 1999 7 9 AALA990746 1 19990519 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1243 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FOUND STRINGER IN LEFT GOUGED AND FASTENER HOLE ELONGATED JUST FORWARD OF BS 1243. REMOVED DAMAGE ON NR 14 STRING ER LEFT PER SRM 53-10-03. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4C-4E FIG 1. (M) 2 L 7 3 4F A3WE 1999070900610 19990709 00610 EU 1999 7 9 SIMA991555 1 19990604 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 268AE 340B268 SYR - FLT 4868 - CARGO SMOKE WARNING ILLUMINATED. DISCHARGED FIRE EXTINGUISHER. RETURNED TO FIELD. VERIFIED EVENT AS A FALSE WARNING. DEFERRED CARGO SMOKE WARNING SYSTEM ON 6-4-99. THE WARNING SYSTEM WAS OPERATIONALLY CHECKED WITH NO D ISCREPANCIES NOTED. RESTORED MEL ITEM AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999070900611 19990709 00611 EU 1999 7 9 REXA99019 1 19990609 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A REXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 361PX 340B249 CARGO SMOKE LIGHT CAME ON IN FLIGHT, ACTIVATED FIRE EXTINGUISHER BOTTLE. CLEANED SMOKE DETECTOR, REMOVED AND REPLACED C ARGO FIRE EXTINGUISHER. SYSTEM OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1999070900612 19990709 00612 EU 1999 7 9 REXA99018 1 19990605 A 3320 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 362PX 340B258 CAPTAIN REPORTS A SMELL OF SMOKE IN CABIN. IT WAS DETERMINED TO BE A WINDOW LIGHT. THE ITEM WAS DEFERED (BULB REMOVED) . (M) 2 L 7 2 4T RT A52EU 1999070900613 19990709 00613 EU 1999 7 9 REXA99017 1 19990604 A 2910 AE7064588 LINE SAAB SF340 SF340A 7850100 EU NLG WW LEAKING A REXA O OTHER K FLUID LOSS CR CRUISE 1 SO 25 404BH 340A061 LOST HYD QUANTITY IN FLIGHT. EMERGENCY EXTENDED GEAR, DECLARED EMERGENCY. REMOVED AND REPLACED FLEX LINE IN NOSE GEAR BAY. (M) 2 L 7 2 4T RT A52EU 1999070900614 19990709 00614 SO 1999 7 9 GLBA99018 1 19990607 A 4997 W1012W1008 WIRE EMB 120 EMB120RT SO COCKPIT FAILED A GLBA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 01 267UE 24212 120071 COCKPIT FILLED WITH SMOKE DUE TO AN APU BUS MALFUNCTION FERRIED A/C TO SPW WITHOUT USE OF THE APU. FOUND WIRING W1012-W 1008 TERMINAL END LOOSE, MELTED. REPLACED APU BUS CABLE. (M) 2 L 7 2 4T RT A31SO 1999070900615 19990709 00615 NM 1999 7 9 GAIA99065 1 19990607 A 3230 651781915 ACTUATOR BOEING 727 727223 1384074 NM LT MLG WW LEAKING A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6811 19486 AFTER TAKEOFF OF SCHEDULED FLIGHT NUMBER 302 FROM SEA TO DFW, THE CREW SELECTED THE GEAR UP. THE LEFT GEAR WOULD NOT RE TRACT. THE CREW RECYCLED THE LANDING GEAR, AND THE LEFT MAIN GEAR REMAINED EXTENDED. THE CREW ELECTED TO RETURN TO SEA . THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED THE UPLOCK ACTUATOR. GEAR SWING CARRIED OUT TO T HE LEFT GEAR. OPERATIONAL CHECKED NORMAL IAW B727 MM 32-32-61. AIRCRAFT WAS RELEASED BACK INTO TO SERVICE. (M) 2 L 7 3 4F A3WE 1999070900616 19990709 00616 NM 1999 7 9 GAIA9964A 1 19990607 A 2610 356644400 ELEMENT BOEING 727 727251 138408H NM NR 1 PYLON INOPERATIVE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 252US 19971 CLIMBING OUT OF MPTO, FLT 317, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED PROCEDURES IAW COCKPIT OPERA TING PROCEDURES MANUAL AND LIGHT REMAINED ILLUMINATED. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AND LIGHT EXTINGUISHED. LANDED WITHOUT FURTHER DIFFICULTY. REMOVED AND REPLACED NR 1 OVERHEAT SENSOR. PERFORMED A OPERATIONAL AND BLEED AIR LEAK CHECK AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999070900617 19990709 00617 NM 1999 7 9 GAIA9966 1 19990608 A 5720 65623355 BEAM BOEING 727 727223 1384074 NM RT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. CORROSION ON RIGHT WALKING BEAM FORWARD OF THE NR 8 SPOILER ACTUATOR. REWORKED RIGHT WALKING BEAM IAW, AMERICAN INTERNATIONAL AIRWAYS, ENGINEERING DEVIATION REQUE ST B2-06492. FLAP PEENED WALKING BEAM IAW B727 SOPM 20-10-03. ITEM RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999070900618 19990709 00618 NM 1999 7 9 GAIA9970 1 19990608 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 700 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. CORROSION ON SHEAR TIE AT BODY STATION 700, LBL 12. REMOVED CORROSION ON SHEAR TIE AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1. REMOVED DAMAGED AREA AND I NSTALLED NEW SHEAR TIE REPAIR ANGLE IAW B727 SRM 53-10-4 FIG 14. RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999070900619 19990709 00619 NM 1999 7 9 GAIA9971 1 19990608 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 720 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. CORROSION ON SHEAR TIE AT BODY STATION 720, BETWEEN STRINGERS 25R AND 26R. REMOVED SHEAR TIE IAW B727 SRM 51-30-2. REMOVED DAMAGED AREA AND INSTALLED NEWLY FABRI CATED SHEAR TIE, IAW B727 SRM 51-30-2. ITEM RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999070900620 19990709 00620 NM 1999 7 9 GAIA9969 1 19990608 A 5320 WEB BOEING 727 727223 1384074 NM BS 1170 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. FLOOR WEB AT FRAME STATION 1170 TO 1175, RB L 26 WAS FOUND TO BE CORRODED. REMOVED CORRODED WEB IAW B727 SRM 51-30-2. INSTALLED NEW WEB IAW B727 SRM 51-30-2. ITE M RETURNED TO SERVICEABLE CONDITON. (M) 2 L 7 3 4F A3WE 1999070900621 19990709 00621 NM 1999 7 9 GAIA9968 1 19990608 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 380 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. THE FLOORBEAM AT FRAME STATINO 380, UPPER C HORD AFT FLANGE BETWEEN RBL 14 AND RBL 28, WAS FOUND TO HAVE CORROSION AND OUT OF SRM REPAIR TOLERANCE PER B727 SRM 51-1 0-1 AND SRM 51-10-6. REMOVED CORROSION IAW B 727 SRM 53-10-8. INSTALLED NEW REPAIR ANGLES IAW B727 SRM 53-10-8. RETUR NED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999070900622 19990709 00622 NM 1999 7 9 GAIA9967 1 19990608 A 5720 659892420 ANGLE BOEING 727 727223 1384074 NM WS 525 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 20186 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT THE OSC MAINTENANCE FACILITY. RIGHT WING STATION 525, REAR SPAR STIFFENER ANGLE HAS CORROSION AT NR 12 SPOILER ACTUATOR OUTBOARD FLANGE. REMOVED AND REPLACED STIFFENER ANGLE IAW B727 SRM 51-30 -02. SEALED FASTENERS IAW B727 MM 28-11-0. NO LEAKS NOTED. RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999070900623 19990709 00623 SO 1999 7 9 ASOA99048 1 19990605 A 2120 AIR DIST EMB 120 EMB120RT SO CABIN SMOKE A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 217AS 120011 FLT 4003 - BURNING SMELL IN COCKPIT SHORTLY AFTER TAKEOFF AND SMOKE IN CABIN THROUGH APPROXIMATELY 6,000. NO OTHER ASSO CIATED FAILURE INDICATED OTHER THAN THE LAV SMOKE DETECTOR WENT OFF. ATL MECHANICS FOUND RAM AIR SWITCH IN THE WRONG PO SITION. OPERATIONAL CHECKS WERE RAN ON BOTH PACKS AND WERE FOUND TO BE GOOD. (M) 2 L 7 2 4T RT A31SO 1999070900624 19990709 00624 SO 1999 7 9 ASOA99049 1 19990607 A 2840 10026000001 INDICATOR EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A ASOA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 11 273AS 120222 AT APPROXIMATELY 12 MILES WEST OF ATLANTA, THERE WAS AN AURAL WARNING. THE FUEL LIGH TON THE MAP WAS ILLUMINATED. BOTH RIGHT ELECTRIC FUEL PUMPS WERE CYCLING IN AUTO. THE RIGHT ENGINE LOST POWER. THE PILOT INITIATED THE ENGINE FAILURE I N FLIGHT CHECKLIST, DECLARED AN EMERGENCY, FEATHERED THE PROPELLERS, RETURNED TO ATL, AND MADE A SINGLE ENGINE LANDING S AFELY. MAINTENANCE REMOVED AND REPLACED FUEL QUANTITY INDICATOR IAW MM. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT IS O K FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999070900625 19990709 00625 NM 1999 7 9 MASA99096 1 19990611 A 3350 82410162007 RELAY DHAV DHC8 DHC8202 2809007 NM E/E BAY FAILED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 456YV 456 FLT 6356 - PSP-PHX - ON TAXI IN PHX, THE CREW REPORTED THAT THE EMERGENCY LIGHTS BEGAN TO FLICKER. MAINTENANCE TROUBLES HOT AND REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL RELAY. OPS CHECK GOOD, THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A13NM 1999070900626 19990709 00626 EA 1999 7 9 MASA99091 1 19990604 A 5210 6003189431 STOP ASSY CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 17175 7175 FLT 5772 - CLT-LIT - THE FLIGHT ATTENDANT REPORTED THAT SHE COULD NOT OPEN THE PASSENGER DOOR. MAINTENANCE ADJUSTED THE INTERNAL OPEN HANDLE STOP, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999070900627 19990709 00627 EA 1999 7 9 MASA99092 1 19990607 A 3350 GE1317 BULB CNDAIR CL600 CL6002B19 EA OVERWING FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 DURING ROUTINE MAINTENANCE, FOUND THE LEFT FORWARD EMERGENCY EXIT OVERWING LIGHT INOPERATIVE. THE BULB WAS REMOVED AND REPLACED, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 1999070900629 19990709 00629 NE 1999 7 9 99ZZZM379 2 19990115 A 7414 SB9RU3 MAGNETO BEECH 18 G18S 1151010 CE PWA R985 R985* 52008 NE LT ENGINE FAILED A GGPA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 01 9210 BA472 103770 AFTER TAKEOFF FROM MWH TO BFI, THE LEFT ENGINE STARTED TO RUN ROUGH. PILOT RETURNED TO MWH. MECHANIC FOUND RIGHT MAGNE TO NO GOOD, MAGNETO WAS CHANGED, GROUND RUN CHECKED OK AND AIRCRAFT RETURNED TO SERVICE. (M) 1 L 7 2 3R 3 R A765 5E1 1999070900631 19990709 00631 NM 1999 7 9 MASA99095 1 19990610 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 456YV 456 FLT 6330 - BFL-PHX - AIRCRAFT WAS EN ROUTE WHEN THE EMERGENCY LIGHTS FLICKERED SEVERAL TIMES. AFTER ARRIVAL IN PHX MAIN TENANCE TROUBLESHOT AND COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999070900632 19990709 00632 1999 7 9 MASA99089 4 19990602 A 3418 MS2452330 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT FAILED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 161YV UE161 FLT 5860 - DUJ-PIT - CREW AGAIN NOTED A NOXIOUS SMELL IN FLIGHT. MAINTENANCE COULD NOT FIND ANY EVIDENCE OF SMELL DURIN G GROUND RUN, HOWEVER DURING TEST FLIGHT. THE SMELL RETURNED. MAINTENANCE FURTHER TROUBLESHOT AND FOUND THE STALL WARN ING TEST SWITCH SHORTED. REMOVED AND REPLACED THE SWITCH, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999070900633 19990709 00633 NM 1999 7 9 99ZZZM381 1 19990607 A 3350 362624 LAMP BOEING 727 727225 1384077 NM ROW 17-18 DISCONNECTED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 889MA 21854 ON PREFLIGHT TRANSIT, FOUND EPL TRACK LIGHTS BETWEEN ROW 17-18C INOPERATIVE. RECONNECTED EPL LIGHTS IAW 33-50-0. OPS C HECKED OK. (M) 2 L 7 3 4F A3WE 1999070900634 19990709 00634 EU 1999 7 9 VTZA990140 1 19990602 A 5270 WARNING LIGHT BAG JETSTM JETSTM3201 1500217 EU PAX DOOR ILLUMINATED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 470UE 814 FLT 7490 - IAD-JFK - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING AND RETURNED TO IAD DUE TO PAX DOOR WARNING LI GHT. MAINTENANCE LUBED SHOOT BOLTS AND HANDLE MECHANISM. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A56EU 1999070900635 19990709 00635 EA 1999 7 9 MASA99097 1 19990612 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA EMER EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17175 7175 FLT 5803 - MKE-PHL - CREW REPORTED LEFT FORWARD EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE ACTION WAS DEFE RRED PER MEL 33-51-2. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE REMOVED AND REPLACED THE BULB. O PS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999070900636 19990709 00636 EA 1999 7 9 MASA99099 1 19990616 A 3350 GE1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA RT EXTERIOR FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 FLT 5773 - CLT-LIT - CAPTAIN REPORTED ONE RIGHT EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE ACTION WAS DEFE RRED PER MEL 33-51-2. THE AIRCRAFT WAS RETURNED TO SERVICE. SUSBSEQUENT MAINTENANCE, REMOVED AND REPLACED BULB. OPS C HECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999070900637 19990709 00637 EU 1999 7 9 VTZA990145 1 19990609 A 5240 ACCESS DOOR BAG JETSTM JETSTM3201 1500217 EU GPU OPEN A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 475UE 850 FLT 7436 - ORF-IAD - DURING CLIMB, AIRCRAFT RETURNED TO ORF DUE TO GPE ACCESS PANEL UNSECURE. MAINTENANCE INSPECTED GPU ACCESS DOOR. NO DEFECTS NOTED. DOOR LATCHED PROPERLY. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999070900638 19990709 00638 EU 1999 7 9 VTZA990120 1 19990525 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 321UE 41045 MAINTENANCE FOUND LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND RELAMPED EMERGENCY LIGHT, OPS CH ECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900639 19990709 00639 EU 1999 7 9 VTZA990148 1 19990602 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 318UE 41041 MAINTENANCE FOUND LEFT AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BULB, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900640 19990709 00640 EU 1999 7 9 VTZA990149 1 19990602 A 3350 21A00511500 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU ROWS 7-10 INOPERABLE A VTZA O OTHER L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 DURING MAINTENANCE, FOUND EMERGENCY TRACK LIGHTING ROWS 7, 8, 9, AND 10 INOPERABLE. MAINTENANCE OPENED DMI 47104, MEL 3 3-14. MAINTENANCE CLOSED DMI 47104 ON 6-3-99 BY REMOVING AND REPLACING EMERGENCY FLOOR TRACK LIGHTING. OPS CHECK OK. A IRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999070900641 19990709 00641 EU 1999 7 9 VTZA990150 1 19990604 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 316UE 41055 MAINTENANCE FOUND FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BULB, OP S CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900642 19990709 00642 EU 1999 7 9 VTZA990151 1 19990609 A 3150 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ILLUMINATED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 309UE 41022 FLT 7364 - IAD-JFK - ABORTED TAKEOFF DUE TO CONFIG WARNIGN MAINTENANCE OPS CHECKED CONFIG WARNING. ALL PARAMETERS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900643 19990709 00643 EU 1999 7 9 VTZA990152 1 19990610 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 326UE 41064 FLT 7580 - IAD-PVD - DURING PREFLIGHT, AFT SECTION OF FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE RESECURED LOOSE CONNECTOR, ALL LIGHTS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900644 19990709 00644 EU 1999 7 9 VTZA990122 1 19990526 A 3350 6047051 POWER PACK JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 MAINTENANCE FOUND RIGHT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED POWER PACK, OPS CHE CK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900645 19990709 00645 EU 1999 7 9 VTZA990121 1 19990525 A 3350 6047051 POWER PACK JETAIR JETSTM JETSTM4101 1500501 EU LEFT WING FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 MAINTENANCE FOUND LEFT AND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED P OWER PACK, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900646 19990709 00646 EU 1999 7 9 99ZZZM382 1 19990525 A 3350 6134051 POWER PACK JETAIR JETSTM JETSTM4101 1500501 EU RT WING FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 303UE 41015 MAINTENANCE FOUND LEFT AND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED P OWER PACK, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900647 19990709 00647 EU 1999 7 9 VTZA990123 1 19990526 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ILLUMINATED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 331UE 41099 FLT 7287 - SWF-IAD - DURING TAKEOFF, AIRCRAFT MADE UNSCHEDULED LANDING DUE TO CARGO DOOR WARNING LIGHT ILLUMINATED. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK AND COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900648 19990709 00648 EU 1999 7 9 VTZA990125 1 19990531 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT MALFUNCTIONED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 315UE 41033 FLT 7600 - IAD-BGM - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO EMERGENCY EXIT WARNING LIGHT ILLUMINATE D. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED EMERGENCY EXIT MICROSWITCH AND COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900649 19990709 00649 1999 7 9 VTZA990124 4 19990530 A 3420 7003110901 EFIS JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 328UE 41083 FLT 8004 - ACY-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CAPTAIN TOP EFIS SCREEN WENT BLANK. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EFIS SCREEN. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900650 19990709 00650 EU 1999 7 9 VTZA990154 1 19990613 A 5230 SWITCHES JETAIR JETSTM JETSTM4101 1500501 EU POD DOOR LACK OF LUBE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 309UE 41022 FLT 7631 - IAD-RDU - ABORTED TAKEOFF DUE TO POD DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTH ER PROBLEMS. MAINTENANCE OPENED DMI 44768, MEL 52-4. MAINTENANCE CLOSED DMI 44768 ON 6-14-99 BY LUBING MICROSWITCHES, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999070900651 19990709 00651 NM 1999 7 9 TSAA9933255 1 19990610 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA O OTHER O OTHER NR NOT REPORTED 1 WP 13 816AL 23122 REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999070900652 19990709 00652 NM 1999 7 9 TSAA9933256 1 19990610 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA O OTHER O OTHER NR NOT REPORTED 1 WP 13 809AL 21720 REPLACED POSITIONS 3, 5 AND 6 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999070900653 19990709 00653 NM 1999 7 9 TSAA9933254 1 19990608 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA O OTHER O OTHER NR NOT REPORTED 1 WP 13 806AL 21927 REPLACED NR 6 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999070900654 19990709 00654 NM 1999 7 9 USAA069941 1 19990426 A 5320 WEB BOEING 727 727225 1384077 NM BS 271 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 NOSE WHEEL WELL HAS A CRACK ON THE RIGHT PRESSURE WEB AT STATION 271. INSTALLED DOUBLER REPAIR AT THE NOSE WHEEL WELL R IGHT PRESSURE WEB, IAW SB 727-53-0145. (M) 2 L 7 3 4F A3WE 1999070900655 19990709 00655 NM 1999 7 9 USAA069940 1 19990426 A 5330 SKIN BOEING 727 727225 1384077 NM BS 258 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 NOSE WHEEL WELL HAS A CRACK ON LEFT PRESSURE WEB AT STATION 258. INSTALLED DOUBLER REPAIR AT THE NOSE WHEEL WELL LEFT P RESSURE WEB, STATION 258. MATERIAL USED, 2024-T3, .050 INCH, 10 INCH BY 18 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-014 5. (M) 2 L 7 3 4F A3WE 1999070900656 19990709 00656 NM 1999 7 9 USAA069939 1 19990426 A 5330 SKIN BOEING 727 727225 1384077 NM BS 720 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 AIR CONDITIONING DISTRIBUTION BAY CORROSION AT RIGHT SIDE OF STRINGER 26R BETWEEN STATION 720E AND 720F. INSTALLED FUSE LAGE EXTERIOR SKIN REPAIR AT STRINGER 26R, BETWEEN STATION 720E AND 720F. MATERIAL USED, 2024-T3, .125 INCH, 18 INCH BY 12 INCH. REPAIR ACCOMPLISHED IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM.008R0-1. (M) 2 L 7 3 4F A3WE 1999070900657 19990709 00657 NM 1999 7 9 USAA069938 1 19990426 A 5280 BEAM BOEING 727 727225 1384077 NM RT MLG DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 RIGHT MLG WING DOOR, T/E BEAM HAS EVIDENCE OF CRACK AT LOWER CENTER. INSTALLED ANGLE REPAIR AT THE RIGHT MAIN LANDING G EAR WING DOOR TRAILING EDGE BEAM. MATERIAL USED, 4130 STEEL, .125 INCH, 2 INCH BY 12 INCH. REPAIR ACCOMPLISHED IAW AVI TAS EA 99AVHM.007R0-1. (M) 2 L 7 3 4F A3WE 1999070900658 19990709 00658 NM 1999 7 9 USAA069937 1 19990426 A 5320 WEB BOEING 727 727225 1384077 NM BS 290 MISREPAIRED A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 918TS 20445 NOSE WHEEL WELL PRESSURE DECK BL '0' AT BS 290 HAS AN IMPROPER REPAIR. INSTALLED DOUBLER REPAIR AT NOSE WHEEL WELL PRES SURE DECK, BL '0' AT BS 290. MATERIAL USED, 2024-T3, .050 INCH, 5 INCH BY 5.75 INCH. REPAIR ACCOMPLISHED IAW SB 727-53 -0145. (M) 2 L 7 3 4F A3WE 1999070900659 19990709 00659 NM 1999 7 9 USAA069936 1 19990426 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 294-312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 EVIDENCE OF CORROSION ON LOWER SIDE OF S24L, BS 294.5 TO BS 312. INSTALLED STRINGER REPAIR AT STRINGER 24L FROM BS 294. 5 TO BS 312. MATERIAL USED, BAC 1498-140, 7 INCH BY 2.5 INCH AND BAC 1498-132, 13 INCH BY 2.5 INCH. REPAIR ACCOMPLISHE D IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999070900660 19990709 00660 NM 1999 7 9 USAA069935 1 19990426 A 5330 SKIN BOEING 727 727225 1384077 NM BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 INSTALLED SKIN DOUBLER REPAIR AT BS 1095, STRINGER 1 DUE TO CRACK. MATERIAL USED 2024-T3, .063 INCH, 11 INCH BY 12 INCH . REPAIR ACCOMPLISHED IAW SB 727-53A0204. (M) 2 L 7 3 4F A3WE 1999070900661 19990709 00661 NM 1999 7 9 USAA069934 1 19990426 A 5330 SKIN BOEING 727 727225 1384077 NM BS 277 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 STATION 277 HAS CRACKED HOLES WHERE STRINGER 11 ATTACHES. INSTALLED DOUBLER REPAIR AT BS 277, STRINGER 11 LEFT. MATERI AL USED, 7075-T6 .050 INCH, 4 INCH BY 10 INCH. REPAIR ACCOMPLISHED IAW SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 1999070900662 19990709 00662 NM 1999 7 9 USAA990483 1 19990530 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 967-975 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 41514 22962 TPA - DURING CX-4 CHECK, FOUND 8 INCHES OF STRINGER WEB CORRODED AT STRINGER 27R AT STATION 967 THROUGH 975. REPLACED S TRINGER PER SRM 53-00-03. (M) 2 L 7 2 4F A16WE 1999070900663 19990709 00663 NE 1999 7 9 USAA069942 2 19990609 A 7321 7436024 FUEL CONTROL HAMSTD 44297 BOEING 727 727254 138408L NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE MALFUNCTIONED A USAA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 EA 19 914TS 20251 657305 FLT 6461 - LGA-DCA - AT 10,000 FT CRUISE, PULLED ALL POWER LEVERS TO IDLE. NR 3 WENT TO FULL POWER, NO CONTROL WITH POW ER LEVER. ENGINE LIMITS NOT EXCEEDED. SHUT DOWN ENGINE. 10 MINUTES WINDMILL AT 15 PSI OIL PRESSURE. REPLACED NR 3 EN GINE FUEL CONTROL PER MM 73-21-2. ENGINE RUNUP PERFORMED PER MM 71-00. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999070900664 19990709 00664 NM 1999 7 9 USAA069943 1 19990613 A 2911 1356603399 ACCUMULATOR PARKER 699 BOEING 727 727254 138408L NM LT MLG WW RUPTURED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 19 912TS 20438 SYSTEM 'B FAILURE EN ROUTE TO LGA. AS PER ABNORMAL, SAFETY WIRE BROKEN ON GPWS AND PNEUMATIC BRAKE. FOUND BRAKE ACCUMU LATOR RUPTURED. REPLACED SAME PER MM 29-32-40. RESAFTIED GPWS SWITCH AND PNEUMATIC BRAKE HANDLE. BLED PNEUMATIC BRAKE LINE PER MM 32-43-0. SERVICED PNEUMATIC BRAKES PER MM 32-00. SERVICED SYSTEM 'B' ACCUMULATOR PER MM 29-00. (M) 2 L 7 3 4F A3WE 1999070900665 19990709 00665 WP 1999 7 9 USAAD99079 1 19990612 A 3610 39271012 VALVE DOUG DC9 DC931 3022065 WP AFT FUSELAGE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 997VJ 47336 PIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTL E WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT AUGMENTATION VALVE AND DUCT. (M) 2 L 7 2 4F A6WE 1999070900666 19990709 00666 WP 1999 7 9 99ZZZM383 1 19990612 A 3610 5910245369 DUCT DOUG DC9 DC931 3022065 WP AFT FUSELAGE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 997VJ 47336 PIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTL E WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT AUGMENTATION VALVE AND DUCT. (M) 2 L 7 2 4F A6WE 1999070900667 19990709 00667 NM 1999 7 9 USAA990474 1 19990525 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 976 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 45207 22882 TPA - DURING CX-6 CHECK, FOUND CORROSION IN FUSELAGE SKIN APPROX 3 INCH IN LENGTH LOCATED BELOW STRINGER 27 LEFT AT STAT ION 976. CORROSION LEVEL 1. ACCOMPLISHED FUSELAGE SKIN EXTERNAL DOUBLER REPAIR PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999070900668 19990709 00668 NM 1999 7 9 USAA990477 1 19990525 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 45207 22882 TPA - DURING CX-6 CHECK, FOUND CORRODED ARM AT FLOORBEAM, APPROX 6 INCH AT STATION 1016, CENTER LINE OF AIRCRAFT CENTER WEB. CORROSION LEVEL 1. ACCOMPLISHED REPAIR PER EA 64270, FASTENERS WERE BACB30FP6 EXCEPT 13 EXISTING BACB30FP88, MATE RIAL .050, 301.5 HARD CAD PLATED STAINLESS PER EA NR 64270. (M) 2 L 7 2 4F A16WE 1999070900669 19990709 00669 NM 1999 7 9 USAA990475 1 19990525 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 996-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 45207 22882 TPA - DURING CX-6 CHECK, FOUND CORROSION IN STRINGER 27L APPROX 20 INCH LONG AT STATION 996 TO 1016, CORROSION LEVEL 1. REPLACED CORRODED SECTION OF STRINGER, SPLICED IN NEW STRINGER AT STATION 956 TO 1016 PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999070900670 19990709 00670 NM 1999 7 9 USAABB99029 1 19990608 A 3350 873203193REV4 CONTROL MODULE BOEING 757 757225 1384959 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 SFO - WHEN COCKPIT SWITCH MOVED TO ARMED POSITION, EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT SHUT OFF. MAINTENANCE REP LACED THE EMERGENCY LIGHTING CONTROL MODULE. (M) 2 L 7 2 4F RT A2NM 1999070900671 19990709 00671 NM 1999 7 9 USAA990522 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 380, BETWEEN STRINGER 8 AND STRINGE R 9L. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900672 19990709 00672 NM 1999 7 9 USAA990521 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 400, BETWEEN STRINGER 8, STRINGER 9 L. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900673 19990709 00673 NM 1999 7 9 USAA990520 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 400, BETWEEN STRINGER 8, STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900674 19990709 00674 NM 1999 7 9 USAA990519 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK AT FUSELAGE FRAME AT FASTENER HOLE AT BS 747 BETWEEN STRINGER 8 AND STRINGE R 9R. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900675 19990709 00675 NM 1999 7 9 USAA990518 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 480, BETWEEN STRINGER 8 AND STRINGE R 9L INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900676 19990709 00676 NM 1999 7 9 USAA990517 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .75 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 440, BETWEEN STRINGER 8 STRINGER 9 . INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900677 19990709 00677 NM 1999 7 9 USAA990516 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 500A, BETWEEN STRINGER 87 AND STR INGER 9R. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64536. (M) 2 L 7 2 4F RT A16WE 1999070900678 19990709 00678 NM 1999 7 9 USAA990515 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .125 INCH CRCK AT FUSELAGE FRAME AT FASTENER HOLE AT BS 440 BETWEEN STRINGER 8 AND STRINGE R 9R. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64536. (M) 2 L 7 2 4F RT A16WE 1999070900679 19990709 00679 NM 1999 7 9 USAA990513 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND 1.5 INCH CRACK AT FASTENER HOLE OF INBOARD CHORD OF FUSELAGE FRAME AT BS 597, WL 203, RBL 64. INSTALLED DOUBLER PER EA 64518 AND EA 64594. (M) 2 L 7 2 4F RT A16WE 1999070900680 19990709 00680 NM 1999 7 9 USAA990512 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND 1 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 827, BETWEEN STRINGER 8 AND STRINGER 9L. DOUBLER AND FILLER INSTALLED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900681 19990709 00681 NM 1999 7 9 USAA990511 1 19990522 A 5312 BULKHEAD WEB BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH VERTICAL CRACK ON BULKHEAD WEB AT STATION 178, LBL 4.5, WL 198. DEFECTIVE PART RE PLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999070900682 19990709 00682 NM 1999 7 9 USAA990510 1 19990430 A 5312 BULKHEAD ANGLE BOEING 737 737401 1384701 NM BS 1030 DRILL MARKS A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 413US 30767 23882 CLT - DURING Q-2 CHECK, FOUND 3 PLACES .125 INCH DRILL MARKS AT BS 1030 RBL 23 (UNDER FLOOR ATTACH ANGLE) AT 1016 PRESSU RE BULKHEAD. BLENDED AREAS/DRILLED HOLE AT DAMAGE AND RIVETS INSTALLED PER SRM 53-80-08. (M) 2 L 7 2 4F RT A16WE 1999070900683 19990709 00683 NM 1999 7 9 USAA990509 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 787 BETWEEN STRINGER 8 AND STRING ER 9L. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900684 19990709 00684 NM 1999 7 9 USAA990508 1 19990522 A 5321 FLOOR BOEING 737 737401 1384701 NM BS 6635 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 CLT - DURING Q-2 CHECK, FOUND TWO .75 INCH CRACKS AT FORWARD END OF BEAD IN PRESSURE DECK/FLOOR AT STTION 6635 LBL 33. I NSTALLED DOUBLER PER EA 64506 AND REV EA 64506A. (M) 2 L 7 2 4F RT A16WE 1999070900685 19990709 00685 NM 1999 7 9 USAA990507 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 867 BETWEEN STRINGER 8 AND STRINGER 9L. INSTALLED DOUBLER PER EA 64536. (M) 2 L 7 2 4F RT A16WE 1999070900686 19990709 00686 NM 1999 7 9 USAABB99028 1 19990604 A 5610 SF15141T4871 SEAL BOEING 767 7672B7 1385107 NM LT COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 653US 24894 LGW - FLT 43 - EN ROUTE AMS-PHL, CAPTAINS SLIDING WINDOW BEGAN TO SQUEAL LOUDLY. FLIGHT DIVERTED TO LGW AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED THE WINDOW SEAL. (M) 2 L 7 2 4F RT A1NM 1999070900687 19990709 00687 EU 1999 7 9 USAAF99031 1 19990604 A 3230 715381 VALVE FOKKER F28 F28MK0100 4990807 EU NLG WW FAILED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 865US 11308 BOS - FLT 1010 - ON APPROACH TO MHT, CREW SELECTED GEAR DOWN. AN UNUSUAL NOISE WAS HEARD, THEN THE MAIN GEAR GREEN LGIH TS ILLUMINATED. AFTER APPROXIMATELY 3-5 MINUTES, THE NOSE GEAR GREEN LIGHT ILLUMINATED. FLIGHT DIVERTED TO BOS AND, AF TER TOWER FLY-BY, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. (M) 2 L 7 2 4F RT 1999070900688 19990709 00688 NM 1999 7 9 USAA990467 1 19990517 A 5330 SKIN BOEING 737 737296 1384486 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 48194 22398 CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1.9 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S17R, 5 INCH FORWARD OF STA TION 747 FRAME. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 2 4F RT A16WE 1999070900689 19990709 00689 NM 1999 7 9 USAA990468 1 19990517 A 5330 SKIN BOEING 737 737296 1384486 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 48194 22398 CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S18R, 2 INCH FORWARD OF STATI ON 727B FRAME. CRACK CUT OUT, INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 6 AND FIG 17. (M) 2 L 7 2 4F RT A16WE 1999070900690 19990709 00690 NM 1999 7 9 USAA990469 1 19990517 A 5330 SKIN BOEING 737 737296 1384486 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 48194 22398 CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 2.75 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT STRINGER 17R, 5 INCHES FOR WARD OF STATION 727B FRAME. REMOVED DAMAGED MATERIAL, INSTALLED DOUBLER PER SRM 53-30-03. (M) 2 L 7 2 4F RT A16WE 1999070900691 19990709 00691 NM 1999 7 9 USAA990485 1 19990530 A 5330 SKIN BOEING 737 737201 1384454 NM BS 756 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 44187 22797 TPA - DURING RON, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 756 AND STRINGER 13R. INSTALLED DOUBLER MADE OF 2023T3 - .072 INCH THICK PER SRM 53-30-3, FIG 6. (M) 2 L 7 2 4F A16WE 1999070900692 19990709 00692 NM 1999 7 9 USAA990466 1 19990522 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 1142 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING CX CHECK, FOUND STRINGER 5 LT CRACKED 1 INCH AT STATION 1142. STOP DRILLED, USED .1875 HI-LOCK FOR REAMED HOLES FOR INSTALLED ANGLE PER SRM 51-10-02 AND EA 64489. (M) 2 L 7 2 4F RT A16WE 1999070900693 19990709 00693 NM 1999 7 9 USAA990435 1 19990509 A 5330 SKIN BOEING 737 7373B7 1384580 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 37074 23595 TPA - DURING CX-3 CHECK, FOUND .25 INCH CRACK IN DOOR SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUT OUT AFT LOWER CORNER. I NSTALLED REPAIR DOUBLER PER EA 64557 AND BOEING SB 737-52-1096 FIG 3. (M) 2 L 7 2 4F RT A16WE 1999070900694 19990709 00694 NM 1999 7 9 USAA990434 1 19990512 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 520 LBL 46 FLOORBEAM. FABRICATED REPAIRED PER EA 64448 AND S/B 737-53-1120. (M) 2 L 7 2 4F RT A16WE 1999070900695 19990709 00695 NM 1999 7 9 USAA990421 1 19990512 A 5714 ANGLE BOEING 737 737301 1384611 NM CTR WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT LOWER END OF INBOARD CHORD ANGLE OF FRAME RBL 65 AT T OP OF WING CENTER SECTION FRAME. INSTALLED FILLER, STIFFENING ANGLE AND TAPERED SHIM PER EA 64331 AND TR 53-62-01. (M) 2 L 7 2 4F RT A16WE 1999070900696 19990709 00696 NM 1999 7 9 USAA990420 1 19990512 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AT BS 727 BL 0 SKIN. FABRICATED REPAIR PER SRM 53-00 -01. (M) 2 L 7 2 4F RT A16WE 1999070900697 19990709 00697 NM 1999 7 9 USAA990365 1 19990512 A 5320 CLIP BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25O INCH CRACK AT BS 380 STRINGER 2L TIE CLIP. REPAIRED PER SRM 51-1 0-01. (M) 2 L 7 2 4F RT A16WE 1999070900698 19990709 00698 NM 1999 7 9 USAA990359 1 19990512 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 380-400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BL 0 AT BS 380 PLUS 3 AND BS 400 MINUS INTERCOSTAL WEB ANGLE. REMOVED AND REPLACED ANGLE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999070900699 19990709 00699 NM 1999 7 9 USAA990358 1 19990512 A 5320 CLIP BOEING 737 737301 1384611 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT FASTENER TIE CLIP STRINGER 10R AND FRAME STATION 663. 75. INSTALLED NEW TIE CLIP PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900700 19990709 00700 NM 1999 7 9 USAA990357 1 19990512 A 5320 CLIP BOEING 737 737301 1384611 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK TIE CLIP STATION 663.75 STRINGER 10L FRAME. INSTALLED N EW TIE CLIP PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999070900701 19990709 00701 NM 1999 7 9 USAA990356 1 19990512 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STRINGER TIE CLIP BS 685 STRINGER 7L. REPAIRED PER SR M 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999070900702 19990709 00702 NM 1999 7 9 USAA990354 1 19990512 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STRINGER TIE CLIP BS 685 STRINGER 6L. REPAIRED PER SR M 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999070900703 19990709 00703 NM 1999 7 9 USAA990355 1 19990512 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 705 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 38012 23233 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STRINGER TIE CLIP BS 705 STRINGER 3L. REPAIRED PER SR M 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999070900704 19990709 00704 EU 1999 7 9 C2XA99BT053 1 19990602 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU ROW 7AB FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14825 170 BTV - DURING 4A CHECK MAINTENANCE, FOUND EMERGENCY EXIT SIGN ABOVE F/A'S SEAT. EMERGENCY FLOOR TRACK LIGHT AT 7AB DIM, AND EMERGENCY EXIT SIGN ABOVE CABIN TO CARGO DOOR ON LEFT SIDE BULB INOPERATIVE. REMOVED AND REPLACED BULBS AS NECESSAR Y. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999070900705 19990709 00705 EU 1999 7 9 C2XA99BT054 1 19990602 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15816 105 EWR - CREW REPORTED PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT AT LOCATION 15 WL. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999070900706 19990709 00706 SO 1999 7 9 C2XA99BT056 1 19990602 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145 SO CARGO COMPT FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14939 145030 BTV - DURING SERVIEC CHECK, MAINTENANCE FOUND BAGGAGE SMOKE DETECTOR INOPERATIVE ON THE GROUND. REMOVED AND REPLACED FO RWARD BAGGAGE SMOKE DETECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 1999070900707 19990709 00707 SO 1999 7 9 C2XA99BT055 1 19990601 A 3350 3025101 LIGHT EMB 145 EMB145ER SO LT EXTERIOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14943 145040 EWR - FLT 4296 - CREW REPORTED LEFT WING FAIRING FUSELAGE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1999070900708 19990709 00708 SO 1999 7 9 C2XA99BT046 1 19990526 A 2434 GENERATOR EMB 145 EMB145 SO NR 1 FAILED A C2XA A UNSCHED LANDING J G H WARNING INDICATION MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 09 16927 145006 CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AI R RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M) 2 L 7 2 4F RT T00011AT 1999070900709 19990709 00709 SO 1999 7 9 C2XA99BT060 1 19990630 A 4920 4501968B APU EMB 145 EMB145LR SO TAILCONE SEIZED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 14950 145061 EWR - CREW REPORTED SMOKE IN COCKPIT AND CABIN ON GROUND WITH APU RUNNING, THE APU SHUTDOWN AUTOMATICALLY. MAINTENANCE FOUND APU SEIZED AND WON'T TURN. APU FAILURE. AIRCRAFT RELEASED IAW MEL 49-00-00 PLACARD NR 175634. APU CHANGED RAN A ND OPERATIONALLY CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 1999070900710 19990709 00710 SO 1999 7 9 C2XA99CL046 1 19990609 A 2150 PACK EMB 120 EMB120RT SO CABIN SMOKING A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 16729 120185 CLE - THE CREW REPORTED SMOKE IN THE CABIN AND COMING FROM THE RIGHT PACK, THE AIRCRAFT WAS TAXIING TO THE MAINTENANCE H ANGAR FOR OTHER MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE PACK SYSTEM IAW EMB-120 MM 21-00-00, NO DE FECTS WERE NOTED DURING THE CHECKS AND THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999070900711 19990709 00711 SO 1999 7 9 C2XA99CL045 1 19990609 A 3230 RETRACT MECH EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SW 09 16729 120185 DTW - THE LEFT MAIN LANDING GEAR WOULD NOT EXTEND, CREW USED THE MANUAL GEAR EXTENSION SYSTEM TO GET THE GEAR DOWN AND L OCKED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRY FLIGHTED TO CLEVELAND FOR REPAIRS. MAINTE NANCE PERFORMED SEVERAL GEAR SWINGS IAW EMB-120 MM 32-30-00 AND EMERGENCY FREEFALL SYSTEM TEST IAW EMB-120 MM 32-34-00, ALL CHECKS WERE SATISFACTORY, AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999070900712 19990709 00712 SO 1999 7 9 C2XA99CL044 1 19990609 A 2932 APTE241000500 TRANSDUCER EMB 120 EMB120RT SO GREEN HYD SYSTEM LEAKING A C2XA A UNSCHED LANDING N K FALSE WARNING FLUID LOSS CR CRUISE 1 SW 09 16729 18324 37533112 120185 DTW - DURING FLIGHT THE CREW LOST THE GREEN SYSTEM HYDRAULIC PRESSURE AND QUANTITY INDICATIONS. THE AIRCRAFT DIVERTED T O DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE TRANSDUCER IAW EMB-120 MM 29-30-09. OPER ATIONAL CHECKS OF THE SYSTEM WAS SATISFACTORY IAW EMB-120 MM 29-00-00. AIRCRAFT WAS FERRY FLIGHTED BACK TO CLEVELAND FO R FURTHER MAINTENANCE. (M) 2 L 7 2 4T RT A31SO 1999070900713 19990709 00713 CE 1999 7 9 99ZZZM384 1 19990601 A 2435 23078019 STARTER/GEN BEECH 1900 1900D 1154162 CE LT ENGINE SHORTED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 836CA UE32 LEFT GENERATOR FAILURE. UPON ENGINE START, GENERATOR FAILED TO COME ON LINE. UNIT REPLACED AND SYSTEM OPERATIONAL CHEC KED SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1999070900714 19990709 00714 NM 1999 7 9 F3LA99077 1 19990617 A 5320 WEB BOEING 737 7372L9 1384497 NM BS 1016 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 DEN - DURING C-6 CHECK, INSPECTION REPORTED RIGHT SIDE WEB AT BS 1016 CORRODED AND DAMAGED. MAINTENANCE FABRICATED REPL ACEMENT WEB AND REPAIRED PER SRM 51-40. (M) 2 L 7 2 4F RT A16WE 1999070900715 19990709 00715 NM 1999 7 9 F3LA99079 1 19990617 A 3244 0397812 TIRE BOEING 737 7373M8 1384615 NM MLG FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 SEA - UPON PREFLIGHT WALKAROUND, FLIGHT CREW REPORTED NR 1 MAIN TIRE RECAP MISSING. MAINTENANCE FOUND DAMAGE TO LEFT IN BOARD FORE, MID AND AFT FLAPS, LOWER GEAR DOOR AFT RIB PANEL, AND LEFT LOWER WING PANEL. REPLACED AFT FLAP PER MM 27-51 -11. DENT ON FORE FLAP FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-50-1, FIG 3, PAGE 6A. REPAIRED DAMAGE TO MID FLA P SKIN PER SRM 51-40-01. REMOVED LEFT MLG INNER DOOR FOR REPAIR AND OPERATING PER CDL 32-10-4. REPAIRED LEFT LOWER WIN G PANEL PER EA 57-737-025 AND SRM 57-51-01. REPLACED NR 1 AND NR 2 MLG TIRE AND WHEEL ASSEMBLIES. NR 1 TIRE HAD BEEN R ECAPPED 3 TIMES. (M) 2 L 7 2 4F RT A16WE 1999070900716 19990709 00716 NM 1999 7 9 F3LA99080 1 19990616 A 3211 65C313326 BEARING BOEING 737 737201 1384454 NM RT MLG OUT OF LIMITS A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 0467 20214 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN RIGHT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT .057. MAINTENANCE REPLACED RIGHT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7007. (M) 2 L 7 2 4F A16WE 1999070900717 19990709 00717 NM 1999 7 9 F3LA99078 1 19990616 A 3211 65C313305 BEARING BOEING 737 737201 1384454 NM LT MLG OUT OF LIMITS A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 01068 20214 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN LEFT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT . 052. MAINTENANCE REPLACED LEFT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7006. (M) 2 L 7 2 4F A16WE 1999070900718 19990709 00718 NM 1999 7 9 F3LA99081 1 19990619 A 5320 INTERCOSTAL BOEING 737 7372L9 1384497 NM BS 947-957 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 DEN - DURING C-CHECK INSPECTION, FOUND CORROSION ON INERCOSTAL AT BS 947 TO BS 957, BL 40R, UNDERSIDE AT NUT PLATE HOLE. MAINTENANCE FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-10-10. (M) 2 L 7 2 4F RT A16WE 1999070900719 19990709 00719 NM 1999 7 9 F3LA99083 1 19990621 A 2710 654476114 PCU BOEING 737 7372L9 1384497 NM AILERON FAILED A F3LA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 03 270FL 4409A 22733 DEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, FIRST OFFICER INITIATED A RIGHT TURN TO FINAL COURSE. AILE RON CONTROL BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS O F FORCE. CAPTAIN ASSISTED FIRST OFFICER AND ROLLED AIRCRAFT TO LEVEL FLIGHT. MAINTENANCE REPLACED A AND B SYSTEM AILER ON PCUS AS A PRECAUTION ADN R 2 FLIGHT SPOILER ACTUATOR DUE TO CHATTERING AND INTERNAL BYPASSING. PERFORMED GENERAL VIS UAL INSPECTION OF FLAP TRACKS, CARRIAGES, TOGGLES, SPINDLES AND AILERON CABLES, AND QUADRANTS, WITH NO DISCREPANCIES NOT ED. TWO BEARINGS SEIZED, CADMIUM PLATING MISSING, FILTER DIRTY, IN ADDITION TO VARIOUS OTHER DISCREPANCIES. DUE TO THE 2 L 7 2 4F RT A16WE 1999070900720 19990709 00720 NM 1999 7 9 99ZZZM385 1 19990621 A 2761 6576112 ACTUATOR BOEING 737 7372L9 1384497 NM NR 2 SPOILER MALFUNCTIONED A F3LA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 03 270FL 22733 DEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, F/O INITIATED A RIGHT TURN TO FINAL COURSE. AILERON CONTRO L BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS OF FORCE. C APTAIN ASSISTED F/O AND ROLLED AIRCRAFT TO LEVEL FLT. MX REPLACED 'A' AND 'B' SYSTEM AILERON PCU'S AS A PRECAUTION AND NR 2 FLT SPOILER ACTUATOR DUE TO CHATTERING AND INTERNAL BYPASSING. PERFORMED GENERAL VISUAL INSPECTION OF FLAP TRACKS, CARRIAGES, TOGGLES, SPINDLES AND AILERON CABLES, AND QUADRANTS, WITH NO DISCREPANCIES NOTED. ACCOMPLISHED WORK CARD 7- 0002, FLIGHT CONTROL MOVEMENT CHECK, WITH NO DISCREPANCIES NOTED. PERFORMED TEST FLIGHT, WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 1999070900721 19990709 00721 NM 1999 7 9 AALA990810 1 19990527 A 5730 SKIN BOEING 727 727223 1384074 NM BS 830 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 703AA 22461 TUL - FOUND CORROSION ON CENTER TANK SKIN ABOVE LEFT AFT PLENUM. REMOVED CORROSION AND INSTALLED DOUBLER/TRIPLER REPAIR PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 1999070900722 19990709 00722 NM 1999 7 9 AALA990815 1 19990528 A 5230 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - CRACK IN FORWARD FRAME WEB NR 2 CARGO DOOR FRAME FROM LOWER DOOR STOP TO TOOLING HOLE. NO STOP DRILL REQUIRED. I NSTALLED DOUBLER REPAIR PER S/B 727-53-A0199 DATED AUG 5, 1993 PER CARD 5295 PG A4. (M) 2 L 7 3 4F A3WE 1999070900723 19990709 00723 NM 1999 7 9 AALA990814 1 19990528 A 5314 KEEL BEAM BOEING 727 727223 1384074 NM BS 871 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - FOUND LEFT KEEL BEAM CHORD CRACKED AT FORWARD FASTENER HOLE AT STATION 871 INSIDE KEEL BEAM, CRACK ENDED AT HOLE. INSTALLED DOUBLER REPAIR PER REV 1, S/B 727-53-0208, DATED FEB 29/96. (M) 2 L 7 3 4F A3WE 1999070900724 19990709 00724 NM 1999 7 9 AALA990813 1 19990602 A 5312 BULKHEAD WEB BOEING 727 727223 1384074 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - APPROX 1 INCH CRACK IN STATION 870 BULKHEAD WEB AT APU LOAD CONTROL VALVE CUTOUT. STOP DRILLED CRACK AND INSTALLE D REPAIR AS PER SRM 53-10-2 PAGE 261C. (M) 2 L 7 3 4F A3WE 1999071300001 19990713 00001 NM 1999 7 13 P2EA99108 1 19990217 A 5712 RIB BOEING 737 737222 1384473 NM WS 524 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, THE RIGHT WING LE RIB LOCATED AT WS 524 WAS FOUND CRACKED. THE RIB WAS REPAIRED AS PER COOPESA EO NR COO-3-57-129-99. (M) 2 L 7 2 4F A16WE 1999071300002 19990713 00002 EU 1999 7 13 DKAA99013 1 19990525 A 5343 MY2021010811 TRUNNION AMD FALC20 FALCOND 2720304 EU NLG CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 226R 27403 226 NOSE LANDING GEAR TRUNNION FITTING WAS FOUND CRACKED DURING OVERWEIGHT LANDING INSPECTION. AIRCRAFT HAD EXPERIENCED AN OVERWEIGHT TAKEOFF AND HAD LANDED WITHIN MAXIMUM AIRCRAFT WEIGHT LIMIT. OVERWEIGHT INSPECTION WAS PERFORMED FOR PRECAUT IONARY REASONS. (M) 2 L 7 2 4F A7EU 1999071300003 19990713 00003 EU 1999 7 13 MALA976511 1 19990626 A 2750 676801007 COMPUTER BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 507XJ E2316 ON DEPARTURE FROM MEM FLAP FAULT ILLUMINATED, RETURNED TO MEM, FLAPS OPERATED CORRECTLY. MAINTENANCE REPLACED FLAP COMP UTER AND PULSE GENERATOR (P/N 676101228-1552). PERFORMED FCS TEST IAW AMM 27-50-00-501, CHECKED GOOD. 2 H 7 4 4F RT A49EU 1999071600008 19990716 00008 SO 1999 7 16 99ZZZX2568 1 19990624 A 2140 A2300475 REGULATOR JANITROL PIPER PA31 PA31350 7103110 SO HEATER LEAKING A WVBA O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 01 3527U 67 317952141 PILOT REPORTED A DROP IN RIGHT FUEL PRESSURE WHEN HEATER WAS STARTED. FURTHER INVESTIGATION REVEALED FUEL LEAKAGE FROM HEATER FUEL PRESSURE REGULATOR AT UPPER SEAL. 1 L 7 2 3O A20SO 1999071600024 19990716 00024 WP 1999 7 16 TWAA9909501 1 19990702 A 5320 TRAP FITTING DOUG DC9 DC931 3022065 WP RIGHT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 DURING CHECK-C MAINTENANCE, THE RT SPAR TO TRAP FITTING HAD FLAW INDICATION BEYOND NDT LIMITS. TRAP FITTING WAS INSTALL ED AND SECURED PER SRM 51-30-1. 2 L 7 2 4F A6WE 1999071600025 19990716 00025 WP 1999 7 16 TWAA9909502 1 19990701 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 1243 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 418EA 47676 DURING CHECK-C MAINTENANCE, THE CANTED BELT RING AT STA 1243, LONGERON 4L, HAD ELONGATED HOLES AT THE BELT RING ATTACH P OINTS. INSTALLED A SECTION OF LONGERON PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 1999071600026 19990716 00026 WP 1999 7 16 TWAA9909503 1 19990707 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 1243 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 418EA 47676 DURING CHECK-C MAINTENANCE, THE AFT CANTED BELT RING AT STA 1243, LONGERON 3L, HAD ELONGATED HOLES AT ATTACH POINTS. RE PAIRED LONGERON SECTION PER SRM 53-02, PAGE 53. 2 L 7 2 4F RT A6WE 1999071600027 19990716 00027 EU 1999 7 16 JBXA9900089 1 19990706 A 3241 60042752 TRANSDUCER FOKKER F28 F28MK0100 4990807 EU NR 2 MLG FAILED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 108ML 11484 FLT 118 RDU TO SWF, ON TAKEOFF ROLL HAD LIFT DUMPER FAULT. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 MAIN LANDING GEAR WHEEL SPEED TRANSDUCER IAW F-100 MM 32-45-22. NO DEFECTS NOTED, OKAY FOR SERVICE. 2 L 7 2 4F RT 1999071600029 19990716 00029 NM 1999 7 16 UPS99230014 1 19990619 A 5330 SKIN BOEING 727 72722C 138400F NM BS 235.8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C CRACK INDICATION NOTED AROUND TWO FASTENER HEADS AT RT BS 235.8 WL 228 AND 229, MARKED IN RED. CUT OU T DAMAGE FABRICATED FILLER AND DOUBLER AND INSTALLED. WORK DONE IAW 53-30-03, 51-10-2, AND 51-30-2 2 L 7 3 4F A3WE 1999071600030 19990716 00030 NM 1999 7 16 UPS99230015 1 19990628 A 2710 652177613 SUPPORT BOEING 727 72722C 138400F NM AILERON LOCKOUT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:C CORROSION UNDER AFT AILERON LOCKOUT GEARBOX ATTACH BOLT (NUTSIDE) ON L/W O/B AILERON LOCKOUT FITTING. REPLACED AILERON LOCKOUT FITTING (SUPPORT) PER ER NR 99-5678. 2 L 7 3 4F A3WE 1999071600031 19990716 00031 NM 1999 7 16 UPS99230016 1 19990701 A 5340 SEAT TRACK BOEING 727 727247 138408F NM BS 522 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE:C CRACKED SEAT TRACK AT BS 522, LBL 45, WL 206. REMOVED DAMAGED SECTION, INSTALLED NEW SECTION, FABRICA TED AND INSTALLED FABRICATED ANGLES AND STRAPS WORK DONE IAW SRM'S 53-10-5 51-30-2 AND 51-20-4. 2 L 7 3 4F A3WE 1999071600032 19990716 00032 NM 1999 7 16 UPS99230017 1 19990701 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 522 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE:C CRACKED SEAT TRACK AT BS 522, LBL 25, WL 206. REMOVED DAMAGED SECTION INSTALLED NEW SECTION, FABRICAT ED SPLICES AND REPAIR EXTRUSIONS, WORK DONE IAW SRM 51-30-2, 53-10-5 AND 51-20-4. 2 L 7 3 4F A3WE 1999071600033 19990716 00033 NM 1999 7 16 UPS99230018 1 19990628 A 5320 ANGLE BOEING 727 727247 138408F NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE:C JACK STAND COMPARTMENT SURROUNDING STRUCTURE IS CRACKED AND DENTED LBL 11 TO LBL 17. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE. WORK DONE IAW SRM'S 51-30-2, 53-10-1, 51-30-5 AND 51-10-2. 2 L 7 3 4F A3WE 1999071600034 19990716 00034 NM 1999 7 16 UPS99230019 1 19990629 A 5320 ANGLE BOEING 727 727247 138408F NM BS 304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE:C CORROSION (C53-111-03.00-01) ON L ANGLE AT BS 304, WL 150, RBL 20 (BELOW DOG HOUSE FLOOR). REMOVED, F ABRICATED AND INSTALLED NEW ANGLE, WORK DONE IAW SRM 53-10-2, 51-30-2 AND SRM 51-40-2. 2 L 7 3 4F A3WE 1999071600035 19990716 00035 NM 1999 7 16 UPS99630013 1 19990707 A 5751 1135710042A AILERON BOEING 767 76734AF 1385212 NM RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 DURING UNLOAD, K LOADER DAMAGED RIGHT O/B AILERON. REMOVED AND REPLACED RT OUTBD AILERON PER MM 27-11-62 P/N 11357100-4 2A, S/N OFF 0013 01, S/N ON 1239. 2 L 7 2 4F RT A1NM 1999071600036 19990716 00036 WP 1999 7 16 UPS99830012 1 19990707 A 3510 6350A34CCC OXY BOTTLE DOUG DC8 DC873F 302199F WP COCKPIT LEAKED A IPXA K NONE O OTHER CL CLIMB 1 SO 01 866UP 45966 AT TOP OF CLIMB, NOTICED BOTH O2 BOTTLES WERE AT 0. REPLACED O2 BOTTLES AND LEAK CHECKED PER M/M 35-10-00 AND 35-20-00. CHECKED FOR LEAKS AT ALL REGULATORS, NO LEAKS NOTED PER 35-10-00 AND 35-20-00. 2 L 7 4 4F RT 4A25 1999071600037 19990716 00037 WP 1999 7 16 UPS99830020 1 19990621 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1400 FRAME, AT LONG 35R IS CRACKED. REPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999071600038 19990716 00038 WP 1999 7 16 UPS99830021 1 19990617 A 5755 564340043 RIB DOUG DC8 DC871F 302199D WP NR 4 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LT WING T/E AT XRS 358, THE NR 4 SPOILER OTBD RIB IS CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-1- 20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600039 19990716 00039 WP 1999 7 16 UPS99830022 1 19990703 A 5311 97585433 FRAME DOUG DC8 DC871F 302199D WP BS 60 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 60 FRAME AT LBL 40 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999071600040 19990716 00040 WP 1999 7 16 UPS99830023 1 19990621 A 5320 37558401 FITTING DOUG DC8 DC871F 302199D WP BS 1152 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1152, AT LONG 33R, THE TORQUE BOX BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999071600041 19990716 00041 WP 1999 7 16 UPS99830024 1 19990619 A 5755 36519421 FITTING DOUG DC8 DC871F 302199D WP NR 4 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LT WING T/E, THE NR 4 SPOILER OTBD HINGE FITTING IS CRACKED. REMOVED AND REPLACED THE HINGE FITTING IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999071600042 19990716 00042 WP 1999 7 16 UPS99830025 1 19990621 A 5320 4641324 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 AFT SIDE OF THE FS 1690 FRAME, THE LONG 36 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999071600043 19990716 00043 WP 1999 7 16 UPS99830026 1 19990620 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 600-620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LONGERON 33R IS CRACKED BETWEEN FS 600 AND 620. CUT OUT DAMAGED SECTION AND REPAIRED IAW DH SK750-12 8X. 2 L 7 4 4F RT 4A25 1999071600044 19990716 00044 WP 1999 7 16 UPS99830027 1 19990618 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 379 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 RT WING L/E RIB AT XFS 379.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SR M 57-2-0. 2 L 7 4 4F RT 4A25 1999071600045 19990716 00045 WP 1999 7 16 UPS99830028 1 19990617 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 722.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LT WING L/E SKIN AT XFS 722.5 IS CRACKED BETWEEN 2 FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 1999071600046 19990716 00046 WP 1999 7 16 UPS99830029 1 19990617 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 566.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LT WING L/E LOWER SKIN IS CRACKED AT XFS 566.25. STOP DRILLED CRACK AT REPAIRED IAW EO DC8-5720-7767 A. 2 L 7 4 4F RT 4A25 1999071600047 19990716 00047 WP 1999 7 16 UPS99830030 1 19990617 A 5720 576960039 DOUBLER DOUG DC8 DC871F 302199D WP WS 566.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LT WING L/E LWR SKIN, INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 566.25. REMOVED, FABRICAT ED, AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999071600048 19990716 00048 WP 1999 7 16 UPS99830031 1 19990617 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 485 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LT WING L/E UPPER SKIN AT XW 485 HAS BULGING, POPPED RIVET AND IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999071600049 19990716 00049 WP 1999 7 16 UPS99830032 1 19990616 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 280 BETWEEN LONG 12L AND 16L, THE PREVIOUS REPAIR DOUBLER IS CRACKED. REMOVED, FABRICATED, AND RE PLACED DOUBLER IAW DWG 5772787 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999071600050 19990716 00050 WP 1999 7 16 UPS99830034 1 19990618 A 5720 576560036 DOUBLER DOUG DC8 DC871F 302199D WP WS 598 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 RT WING L/E AT XFS 598, THE INNER DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REP LACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999071600051 19990716 00051 WP 1999 7 16 UPS99830035 1 19990618 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 691.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LT WING L/E UPPER RIB AT XFS 691.25 IS CRACKED AT THE AFT FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999071600052 19990716 00052 WP 1999 7 16 UPS99830036 1 19990617 A 5320 3750727521 FITTING DOUG DC8 DC871F 302199D WP BS 851 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 KEEL BEAM FITTING AT FS 851, RT SIDE, IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600053 19990716 00053 WP 1999 7 16 UPS99830037 1 19990619 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 32 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 COCKPIT SUB-FLOOR INTERCOSTAL VERTICAL SUPPORT FITTING IS CRACKED, FS -32.OO LBL 12. REPAIRED FITTIN G IAW DH SK750-913. 2 L 7 4 4F RT 4A25 1999071600054 19990716 00054 WP 1999 7 16 UPS99830038 1 19990617 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 55 FRAME BETWEEN LONG 24L AND 25L IS CRACKED AT THE DUCT SUPPORT. CUT OUT DAMAGED FRAME AND REPAI RED IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999071600055 19990716 00055 WP 1999 7 16 UPS99830039 1 19990625 A 5720 576958991 DOUBLER DOUG DC8 DC871F 302199D WP WS 372 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 RT WING L/E AT XFS 372, THE LIFT TRANSDUCER DOUBLER IS CRACKED. REMOVED, FABRICATED, AND REPLACED TH E DOUBLER IAW DWG 5769589 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999071600056 19990716 00056 WP 1999 7 16 UPS99830040 1 19990621 A 5320 37558451 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1200 BETWEEN LONG 35L AND 34L, THE BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING I AW SRM 53-2-0 FIG 3D. 2 L 7 4 4F RT 4A25 1999071600057 19990716 00057 WP 1999 7 16 UPS99830041 1 19990621 A 5320 37592201 FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LONGERON 32L BETWEEN FS 1260 AND 1280, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE SPLIC E FITTING IAW SRM 51-1-20D AND 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1999071600058 19990716 00058 WP 1999 7 16 UPS99830042 1 19990628 A 5320 4758514503 FITTING DOUG DC8 DC871F 302199D WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1240 AT LONG 33R, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600059 19990716 00059 WP 1999 7 16 UPS99830043 1 19990624 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 512-520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 512 TO 520, LONG 33R TO 35R, THE TORQUE BOX WEB IS CORRODED BEYOND LIMITS. REPAIRED WEB IAW SRM 5 3-2-0 FIG 23. 2 L 7 4 4F RT 4A25 1999071600060 19990716 00060 WP 1999 7 16 UPS99830044 1 19990621 A 5320 375414501 FITTING DOUG DC8 DC871F 302199D WP BS 1150-1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LONGERON 31R FITTING, FS 1150 TO 1160 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600061 19990716 00061 WP 1999 7 16 UPS99830045 1 19990628 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1480-1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1480 TO 1540, RBL 52, THE SEAT TRACK IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SEAT TRACK FS 147 0 TO 1580, SPLICED IN A NEW TRACK IAW SRM 53-2-3 FIG 8A. 2 L 7 4 4F RT 4A25 1999071600062 19990716 00062 WP 1999 7 16 UPS99830046 1 19990621 A 5320 37592221 FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1260 TO 1280, LONG 34R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D A ND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600063 19990716 00063 WP 1999 7 16 UPS99830047 1 19990621 A 5320 37592221 FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1260 TO 1280, LONG 36 SPLICE IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0 . 2 L 7 4 4F RT 4A25 1999071600064 19990716 00064 WP 1999 7 16 UPS99830048 1 19990620 A 5320 37739062 FITTING DOUG DC8 DC871F 302199D WP BS 717 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 717, RBL 24, THE FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51 -1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600065 19990716 00065 WP 1999 7 16 UPS99830049 1 19990620 A 5320 37502571 FITTING DOUG DC8 DC871F 302199D WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LONGERON 31R SPLICE FITTING AT FS 450 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600066 19990716 00066 WP 1999 7 16 UPS99830050 1 19990622 A 5320 5645332219 ANGLE DOUG DC8 DC871F 302199D WP BS 879-900 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 MAIN CABIN FS 879 TO 900, LBL 61, THE HORZIZONTAL ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICAT ED, AND REPLACED ANGLE IAW DWG 5645332 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999071600067 19990716 00067 WP 1999 7 16 UPS99830051 1 19990621 A 5320 3750257503 FITTING DOUG DC8 DC871F 302199D WP BS 210 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 210, LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999071600068 19990716 00068 WP 1999 7 16 UPS99830052 1 19990621 A 5320 4641324 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 AFT SIDE OF THE FS 1690 FRAME, THE LONGERON 32R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600069 19990716 00069 WP 1999 7 16 UPS99830053 1 19990621 A 5320 4641324 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 AFT SIDE OF THE FS 1690 FRAME, LONGERON 24R END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0. 2 L 7 4 4F RT 4A25 1999071600070 19990716 00070 WP 1999 7 16 UPS99830054 1 19990621 A 5320 3750257503 FITTING DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 LONGERON 31L SPLICE FITTING AT FS 1050 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1999071600071 19990716 00071 WP 1999 7 16 UPS99830055 1 19990621 A 5320 3755841501 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 BATHTUB FITTING IS CRACKED FS 1200 BETWEEN LONGERON 34R AND 33R. REMOVED AND REPLACED THE FITTING IA W SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999071600072 19990716 00072 WP 1999 7 16 UPS99830056 1 19990627 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 425.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 RT WING L/E RIB AT XFS 425.5 IS CRACKED AT THE AFT LWR END. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999071600073 19990716 00073 WP 1999 7 16 UPS99830057 1 19990626 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1440-1460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1440 TO 1460, LBL 8, THE CEILING INTERCOSTAL IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED INTERCOSTAL IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1999071600074 19990716 00074 WP 1999 7 16 UPS99830058 1 19990619 A 5347 6015176 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 50-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 50 TO 70, RBL 48, THE SEAT TRACK HAS HEAVY CORROSION AROUND THE CLIPNUTS. CUT OUT DAMAGED AREA FR OM FS 50 TO 100, FABRICATED REPLACEMENT TRACK AND INSTALLED IAW SRM 53-2-3 FIG 14. 2 L 7 4 4F RT 4A25 1999071600075 19990716 00075 WP 1999 7 16 UPS99830059 1 19990620 A 5347 6015176 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 789-834 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 789 TO 834, RBL 60, THE SEAT TRACK HAS HEAVY CORROSION. CUT OUT DAMAGED SEAT TRACK FROM FS 750 TO 842, FABRICATED AND INSTALLED IAW SRM 53-2-3 AND EO DC8-5320-5167C. 2 L 7 4 4F RT 4A25 1999071600076 19990716 00076 WP 1999 7 16 UPS99830060 1 19990626 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1310-1420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 FS 1310, 1320 TO 1420, BL 0, THE CABIN SEAT TRACK IS CORRODED AT THE CLIPNUTS. CUT OUT DAMAGED SEAT TRACK FS 1310 TO 1430, FABRICATED, AND REPLACED TRACK AND INSTALLED IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999071600077 19990716 00077 WP 1999 7 16 UPS99830061 1 19990621 A 5320 3773157501 ANGLE DOUG DC8 DC871F 302199D WP BS 1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 VERTICAL SUPPORT ANGLE AT FS 1480, LONGERON 27L HAS HEAVY CORROSION. REMOVED, FABRICATED, AND REPLAC ED THE ANGLE IAW DWG 3773157 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999071600078 19990716 00078 EU 1999 7 16 QXEA9901434 1 19990702 A 3350 900542 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 2422 11167 PDX - CABIN FLOOR PROXIMITY LIGHTING SYSTEM FLICKERED, THEN CAME ON STEADY FOR 30 MINUTES, THEN WENT OUT. WENT ON AND O FF A FEW MORE TIMES. MAINTENANCE REPAIRED WIRING HARNESS AND BATTERY PACK AT SEAT 10AB. PERFORMED OPERATIONAL TEST. T HE SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999071600079 19990716 00079 NE 1999 7 16 MWEA99377 2 19990706 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 BIRD STRIKE A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 31 206ME 47791 SMOKE IN CABIN AND COCKPIT DUE TO INGESTION OF A BIRD. MAINTENANCE FOUND BIRD STRIKE ON NR 1 ENGINE AND PERFORMED FOREI GN OBJECT DAMAGE INSPECTION. 2 L 7 2 4F 4 F A6WE E2EA 1999071600080 19990716 00080 NE 1999 7 16 MWEA99378 2 19990702 A 7311 548003 FUEL OIL COOLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE LT ENGINE LEAKING A MWEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 216ME 47740 LEFT ENGINE LOST 9 QUARTS OF OIL. MAINTENANCE FOUND OIL LEAK AT FUEL OIL COOLER AND REPLACED AFT B-NUT SEAL. 2 L 7 2 4F 4 F A6WE E2EA 1999071600081 19990716 00081 WP 1999 7 16 MWEA99379 1 19990629 A 5730 59101349 SKIN DOUG DC9 DC914 3022034 WP LT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LEFT FLAP HAS LARGE DENT OUTBOARD OF PANEL 1553. MAINTENANCE FABRICTED AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 1999071600082 19990716 00082 WP 1999 7 16 MWEA99381 1 19990703 A 2560 113317 SLIDE DOUG DC9 DC981 3022081 WP SERVICE DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 810ME 48072 FORWARD SERVICE DOOR SLIDE COVER NEEDS TO BE REATTACHED. REATTACHED FORWARD GALLEY ESCAPE SLIDE COVER. 2 L 7 2 4F A6WE 1999071600083 19990716 00083 WP 1999 7 16 MWEA99382 1 19990630 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 202ME 47672 FORWARD CABIN DOOR SLIDE OFF. REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999071600084 19990716 00084 1999 7 16 MWEA99380 4 19990705 A 2210 4034237915 SERVO DOUG DC9 DC981 3022081 WP AILERON FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 810ME 48072 ON CLIMB-OUT OF MCI WITH NR 1 DFGC ENGAGED AUTOPILOT AND AUTO THROTTLES DISCONNECTED THE FMA AND DFGC FAILED. SELECTED NR 2 DFGC AND AUTOTHROTTLES WORKED FOR 10 SEC THEN FAILED ALONG WITH PREVIOUS SYSTEMS, NO HELP WITH BOTH DFGC'S ON 1 OR BOTH ON 2 DIVERTED AIRCRAFT TO MKE FOR REPAIR. REMOVED AND REPLACED THE AILERON SERVO DRIVE AIRCRAFT RETURN TO SERVICE TEST GOOD. 2 L 7 2 4F A6WE 1999071600085 19990716 00085 NM 1999 7 16 DHL99701001 1 19990707 A 2752 MS93911302E MOTOR BOEING 727 72730C 1384009 NM TE FLAPS LEAKING A DHLA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 701DH 19011 HAD A SYSTEM HYDRAULIC FAILURE. FOUND OUTBD FLAP POWER UNIT HYDRAULIC MOTOR LEAKING. REMOVED AND REPLACED PER MM 27-51 -62 LEAK CHECK GOOD SERVICED SYSTEM. 2 L 7 3 4F A3WE 1999071600086 19990716 00086 1999 7 16 DHL99807005 4 19990708 A 3442 2067157153 RT UNIT DOUG DC8 DC873 302199C WP RADAR UNSERVICABLE A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 807DH 45990 RADAR WAS SPOKING, DOES NOT GET GROUND RETURN. REMOVED AND REPLACED RADAR R/T. 2 L 7 4 4F RT 4A25 1999071600087 19990716 00087 WP 1999 7 16 RRXA991170 1 19990702 A 5220 EMERGENCY EXIT DOUG DC8 DC871 302199A WP CABIN UNSECURED A RRXA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 15 811AL 46099 CABIN DOOR WARNING LIGHT CAME ON DURING ROTATION TO TAKEOFF ACCOMPANIED BY LOW RUSHING AIR NOISE. FOUND RT FWD OVERWING HATCH UNLOCKED, LOCKED WINDOW. OPS CK'D OK. 2 L 7 4 4F 4A25 1999071600088 19990716 00088 1999 7 16 RRXA991171 4 19990705 A 3442 20412170413 TRANSCEIVER DOUG DC8 DC873F 302199F WP COCKPIT FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 606AL 46044 WX RADAR FAILED IN FLT. REPLACED XCVR AND RADAR SCOPE, OPS CHECKS GOOD ON GROUND, NO DEFECTS NOTED AT THIS TIME. 2 L 7 4 4F RT 4A25 1999071600089 19990716 00089 NM 1999 7 16 VNAA9907001 1 19990706 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 5LK DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 438JS 7881 178 3056 A SECTION OF EMERGENCY LIGHTING WAS NOTED TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WER E COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999071600090 19990716 00090 EU 1999 7 16 SIMA991691 1 19990618 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 8B FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 278AE 340B278 LAX - FLT 3325 - FLOOR PROXIMITY LIGHT AT SEAT 8B DOES NOT ILLUMINATE. REPA REPLACED FLOOR PROXIMITY LIGHT BULB. OPER ATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999071600091 19990716 00091 EU 1999 7 16 SIMA991673 1 19990616 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU ROW 4A INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 904AE 18612 340B314 DFW - FLT 5037 - EMERGENCY OVERHEAD LIGHT AT SEAT 4A DOES NOT ILLUMINATE. REMOVED AND REPLACED ONE EMERGENCY LIGHT POWE R SUPPLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999071600092 19990716 00092 EU 1999 7 16 SIMA991672 1 19990616 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 334AE 1876 340B334 MIA - ALL CABIN EMERGENCY LIGHTING DOES NOT ILLUMINATE. REMOVED AND REPLACED ALL FIVE POWER SUPPLIES. OPERATIONAL CHEC K GOOD. REF: OPERATOR CONTROL NR 99ZZZX2584 THROUGH 99ZZZX2587. (X) 2 L 7 2 4T RT A52EU 1999071600093 19990716 00093 EU 1999 7 16 99ZZZX2584 1 19990616 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 334AE 104 340B334 MIA - ALL CABIN EMERGENCY LIGHTING DOES NOT ILLUMINATE. REMOVED AND REPLACED ALL FIVE POWER SUPPLIES. OPERATIONAL CHEC K GOOD. REF: OPERATOR CONTROL NR SIMA991672, AND, 99ZZZX2585 THROUGH 99ZZZX2587. 2 L 7 2 4T RT A52EU 1999071600094 19990716 00094 EU 1999 7 16 99ZZZX2585 1 19990616 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 334AE 1884 340B334 MIA - ALL CABIN EMERGENCY LIGHTING DOES NOT ILLUMINATE. REMOVED AND REPLACED ALL FIVE POWER SUPPLIES. OPERATIONAL CHEC K GOOD. REF: OPERATOR CONTROL NR SIMA991672, AND, 99ZZZX2584 THROUGH 99ZZZX2587. 2 L 7 2 4T RT A52EU 1999071600095 19990716 00095 EU 1999 7 16 99ZZZX2586 1 19990616 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 334AE 15466 340B334 MIA - ALL CABIN EMERGENCY LIGHTING DOES NOT ILLUMINATE. REMOVED AND REPLACED ALL FIVE POWER SUPPLIES. OPERATIONAL CHEC K GOOD. REF: OPERATOR CONTROL NR SIMA991672, AND, 99ZZZX2584 THROUGH 99ZZZX2587. 2 L 7 2 4T RT A52EU 1999071600096 19990716 00096 EU 1999 7 16 99ZZZX2587 1 19990616 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 334AE 18324 340B334 MIA - ALL CABIN EMERGENCY LIGHTING DOES NOT ILLUMINATE. REMOVED AND REPLACED ALL FIVE POWER SUPPLIES. OPERATIONAL CHEC K GOOD. REF: OPERATOR CONTROL NR SIMA991672, AND, 99ZZZX2584 THROUGH 99ZZZX2586. 2 L 7 2 4T RT A52EU 1999071600097 19990716 00097 EU 1999 7 16 SIMA991671 1 19990616 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU ROWS 3A-5A FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 381AE 340B381 DFW - FLT 5215 - EMERGENCY FLOOR LIGHTS FROM ROWS 3A TO 5A DO NOT ILLUMINATE. REMOVED AND REPLACED FLOOR STRIP LIGHT AS SEMBLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999071600098 19990716 00098 EU 1999 7 16 SIMA991661 1 19990615 A 3350 1317 BULB SAAB SF340 340B 7860101 EU ROW 8A FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 389AE 340B389 DFW - FLT 5013 - EMERGENCY OVERHEAD LIGHT AT SEAT 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BULB. O PERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999071600099 19990716 00099 EU 1999 7 16 SIMA991761 1 19990625 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 7BC FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 323AE 340B323 DFW - FLT 5053 - EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 7BC DOES ONT ILLUMINATE. REMOVED AND REPALCED BULB. OPERATION AL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999071600100 19990716 00100 EU 1999 7 16 SIMA991762 1 19990625 A 3320 65111 BALLAST SAAB SF340 340B 7860101 EU ROW 8A FAILED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 392AE 552 340B392 DFW - FLT 5324 - SMOKE IN THE REAR CABIN AND CARGO SMOKE LIGHT ILLUMINATED. REMOVED AND REPLACED LIGHT BALLAST AT SEAT 8A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999071600101 19990716 00101 EU 1999 7 16 SIMA991763 1 19990625 A 3350 GE81 BULB SAAB SF340 340B 7860101 EU EMERGENCY EXIT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AE 340B234 MIA - FLT 5831 - RIGHT OVERWING EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL C HECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999071600102 19990716 00102 EU 1999 7 16 SIMA991733 1 19990622 A 2120 AIR DIST SAAB SF340 340B 7860101 EU COCKPIT SMOKE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 370AM 340B370 DFW - FLT 5055 - SMELLED FUMES IN COCKPIT IN-FLIGHT. SMELL PERSISTED FOR TWO TO THREE MINUTES. DECLARED AN EMERGENCY A ND RETURNED TO DFW. PERFORMED GROUND RUN FOR 30 MINUTES. FOUND NO SMOKE OR FUMES DURING THIS TIME WITH AIR CONDITIONIN G PACKS AND BLEEDS IN USE. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999071600103 19990716 00103 EU 1999 7 16 SIMA991702 1 19990619 A 3240 AIR124472 HOSE SAAB SF340 340B 7860101 EU LT MLG FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 359SB 340B359 LRD - FLT 5167 - UPON PARKING, BRAKE OUTBOARD PRESSURE AND HYDRAULIC QUANTITY WENT TO ZERO. REMOVED AND REPLACED BROKEN BRAKE SUPPLY LINE AT THE NR 1 BRAKE. SERVICED SYSTEM, PERFORMED LEAK AND OPERATIONS, CHECKED NORMAL. (X) 2 L 7 2 4T RT A52EU 1999071600104 19990716 00104 EU 1999 7 16 SIMA991652 1 19990614 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 710-718 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 ABI - FOUND DAMAGE TO AFT FUSELAGE SKIN BETWEEN FRAMES AT STA 710 AND STA 718 JUST ABOVE SL 1520 WITH MINOR DAMAGE TO IN TERNAL SPLICE PLATE. PERFORMED A CUT-OUT OF DAMAGED SKIN, EDDY CURRENT INSP, NO DEFECTS. FABBED EXT DOUBLER AND TRIPLE R .032 INCH THICK, DOUBLER 9.75 INCHES BY 7.01 INCHES, AND TRIPLER 9.75 INCHES BY 10.0 INCHES. FABBED FILLER .050 INCH THICK TO DIMENSIONS OF CUT-OUT. POSITIONED REPAIR DOUBLER, TRIPLER, FILLER, AND DRILLED, DEBURRED, BROKE ALL SHARP EDGE S. APPLIED COATING OF ALODINE AND EPOXY PRIMERS. FAY SEALED ALL REPAIR PARTS AND WET INSTALLED ALL FASTENERS. EDGE SE ALED REPAIR. RESTORED FINISH. WORK DONE IAW SAAB 72SDS1597 AND SAAB 340 SRM. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999071600105 19990716 00105 EU 1999 7 16 SIMA991651 1 19990614 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 305AE 340B305 ABI - DURING MBV INSPECTION, FOUND SEAT TRACK AT BL ZERO FROM STA 373.0 FWD TO THE END OF THE TRACK AT STA 297 CORRODED. REMOVED THE DAMAGED AREA. CUT SECTION OF REPAIR EXTRUSION, AND INSERTED U-BEAM INTO EXISITNG SEAT TRACK AND EXTRUSION . DRILLED REPAIR PIECES, FAY SEALED AND INSTALLED. DRILLED WEB FOR THE RE-INSTALLATION OF EMERGENCY FLOOR LIGHTS. DEB URRED AND RESTORED SURFACE PROTECTION. INSTALLED LIGHT ASSEMBLIES AND PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYS WITH NO DEFECTS NOTED. APPLIED ONE COAT OF PRIMER AND TOP COAT TO REST OF REPAIR. WORK DONE IAW SAAB 340 SRM 53-7 0-60 PGS 201, 204, AND 205. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999071600106 19990716 00106 EU 1999 7 16 SIMA991621 1 19990611 A 3240 50125893 BRAKE SAAB SF340 340B 7860101 EU RT MLG LEAKING A SIMA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 339SB MAY950074 340B339 LAX - FLT 3253 - WHILE TAXIING FOR TAKEOFF, HYDRAULIC PRESSURE INDICATION WENT TO ZERO. REMOVED AND REPLACED NR 4 BRAKE ASSY FOR LEAKAGE. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999071600107 19990716 00107 EU 1999 7 16 SIMA991592 1 19990608 A 2910 AE706458 HYDRAULIC LINE SAAB SF340 340B 7860101 EU NLG WW FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 298AE 340B298 AEX - FLT 5078 - LOST HYDRAULIC PRESSURE ON MAIN ACCUMULATOR AND LOST HYDRAULIC QUANTITY INDICATION. REMOVED AND REPLAC ED NOSE LANDING GEAR RETRACT ACTUATOR UP LINE. SERVICED HYDRAULIC SYSTEM AND PERFORMED OPERATIONAL AND LEAK CHECKS. AI RCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999071600108 19990716 00108 EU 1999 7 16 VTZA990155 1 19990613 A 3230 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LANDING GEAR OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 312UE 41025 IAD/EWR - FLT 7538 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE LANDING GEAR NOT RETRACTING AFTER TAK EOFF. MAINTENANCE ADJUSTED AOG SWITCH AND PERFORMED GEAR SWINGS, OPS CHECK GOOD. AIRCRAFT RELEASED AND APPROVED FOR R ETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600109 19990716 00109 EU 1999 7 16 VTZA990167 1 19990615 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 319UE 41042 IAD - DURING MAINTENANCE, FOUND LEFT FORWARD EMERGENCY LIGHT INOPERABLE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FORWARD EMERGENCY LIGHT, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600110 19990716 00110 EU 1999 7 16 VTZA990168 1 19990616 A 3060 PROPELLER HEAT JETAIR JETSTM JETSTM4101 1500501 EU LEFT MALFUNCTIONED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 303UE 41015 IAD/ILM - FLT 7375 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT PROPELLER HEAT FAILURE. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PROBLEM . OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600111 19990716 00111 EU 1999 7 16 SIMA990169 1 19990616 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 316UE 41055 DURING MAINTENANCE, FOUND LEFT FORWARD EMERGENCY LIGHT INOPERABLE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FORWA RD EMERGENCY LIGHT. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600112 19990716 00112 EU 1999 7 16 VTZA990170 1 19990618 A 3260 ATG135002 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 317UE 41031 IAD/CHS - FLT 7567 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RED GEAR WARNING LIGHT ILLUMINATED IN GEA R HANDLE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT MAIN GEAR STANDBY UPLOCK MICROSWITCH. MAINTENANCE PERFORMED GEAR SWINGS. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600113 19990716 00113 EU 1999 7 16 VTZA990171 1 19990620 A 2612 FIRE DETECTION JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 312UE 41025 GBM/IAD - FLT 7601 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO POD SMOKE DETECTOR ILLUMINATED. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIR CRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600114 19990716 00114 EU 1999 7 16 VTZA990172 1 19990620 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT INOPERABLE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 315UE 41033 SWF/IAD - FLT 7283 - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO FORWARD EMERGENCY EXIT LIGHT INOPERABLE. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600115 19990716 00115 EU 1999 7 16 VTZA990156 1 19990615 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 305UE 41019 ROC/IAD - FLT 7614 - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO FLOOR TRACK EMERGENCY LIGHTS INOPERABLE. AIRCRAFT RE TURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESECURED CONNECTOR. OPS CHECK OK. AIRCRAFT RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600116 19990716 00116 EU 1999 7 16 VTZA990173 1 19990621 A 2425 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 1 AND 2 TRIPPED A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 312UE 41025 DTW/IAD - FLT 7312 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO AHRS FAILURE. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RE-RACKED NR 1 AND NR 2 SYMBOL GENERATOR. OPS CHECK OK. AIRCRAF T RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600117 19990716 00117 EU 1999 7 16 VTZA990174 1 19990622 A 2435 23095002 STARTER/GEN JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 317UE 41031 IAD/RDU - DURING CRUISE, AIRCRAFT MADE AN UNSCHEUDLED LANDING DUE TO RT GENERATOR WENT OFF LINE. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RIGHT STARTER/GENERATOR. OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600118 19990716 00118 EU 1999 7 16 VTZA990176 1 19990625 A 2425 7011672112 SYMBOL GEN JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA O OTHER O OTHER AP APPROACH 1 EA 27 308UE 41023 IAD/EWR - FLT 7620 - DURING APPROACH, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS NR 1 SYMBOL GENER ATOR FAILED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 SYMBO L GENERATOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600119 19990716 00119 EU 1999 7 16 VTZA990175 1 19990624 A 2425 7011672112 SYMBOL JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 329UE 41097 IAD/CHS - FLT 7293 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 SYMBOL GENERATOR FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 SYMBOL GENERATOR. OPS C HECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600120 19990716 00120 EU 1999 7 16 VTZA990177 1 19990625 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O J OTHER WARNING INDICATION TO TAKEOFF 1 EA 27 309UE 41022 IAD/HPN - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE OPENED DMI 44771. MEL 52-4, MAINTENANCE CLOSED DMI 44771 ON 6-28-99 BY CLEA NING MICROSWITCHES. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600121 19990716 00121 EU 1999 7 16 VTZA000178 1 19990627 A 7722 EGT COMPENSATOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 330UE 41098 IAD - FLT 7372 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE EGT TEMP OUT ON TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED BOTH EGT COMPENSATORS, OPS CHECK OK. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600122 19990716 00122 EU 1999 7 16 VTZA990180 1 19990628 A 2750 SELECTOR JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS OUT OF POSITION A VTZA O OTHER W INADEQUATE Q C AP APPROACH 1 EA 27 309UE 41022 DL/IAD - FLT 7669 - DURING APPROACH, AIRCRAFT FLAPS STUCK AT 25 DEGREES. MAINTENANCE INSPECTED AND FOUND EMERGENCY HYDR AULIC SELECTOR PARTIALLY SELECTED TO THE FLAPS DOWN POSITION CAUSING THE FLAPS DOWN ONLY BYPASS PIN TO POP ON THE FLAP C ONTROL VALVE. RESET EMERGENCY HYDRAULIC SELECTOR TO NORMAL, AND RESET THE BYPASS PIN, SYSTEM OPS CHECK OK WITH NO DEFEC TS NOTED. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600123 19990716 00123 EU 1999 7 16 VTZA990181 1 19990626 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 306UE 41020 ILM/IAD - FLT 7368 - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO AFT EMERGENCY EXIT LIGHT INOPERABLE. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RELAMPED LIGHT. OPS CHECK OK. AIRCRAFT WAS RELEASED AN D APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999071600124 19990716 00124 EU 1999 7 16 VTZA9990157 1 19990602 A 7712 94959411 TTL COMPUTER BAG JETSTM JETSTM3201 1500217 EU LT/RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 493UE 805 IAD/BWI - FLT 7272 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO BOTH ENGINES NOT REACHING SCHEDULED TORQUE. MAINTE NANCE OPENED DMI 43808. MEL 76-2 FOR LEFT TTL LOW POWER AND DMI 43809, MEL 76-2 FOR RT TTL LOW POWER. MAINTENANCE CLOS ED BOTH DMI'S 43809 AND 43808 ON 6-10-99 BY ADJUSTING TTL COMPUTER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED T O SERVICE. (X) 2 L 7 2 4T RT A56EU 1999071600125 19990716 00125 EU 1999 7 16 VTZA990158 1 19990602 A 6120 PROPELLER GOV BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 475UE 850 IAD/ABE - FLT 7158 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE DUE TO LT ENGINE ONLY MAKING 4 PERCEN T TORQUE. MAINTENANCE ADJUSTED MAXIMUM FUEL FLOW AND PROPELLER GOVERNOR. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURN ED TO SERVICE. 2 L 7 2 4T RT A56EU 1999071600126 19990716 00126 EU 1999 7 16 VTZA990159 1 19990611 A 3230 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 475UE 850 IAD/ORF - FLT 7229 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WOULD NOT RETRACT, AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED WOW MICROSWITCHES AND SERVICED NOSE STRUT. MAIN TENANCE PERFORMED GEAR SWINGS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999071600127 19990716 00127 EU 1999 7 16 VTZA990160 1 19990613 A 3230 622800200 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 475UE 850 IAD/CLE - FLT 7451 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WOULD NOT RETRACT. AIRCRAFT RETUR NED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WOW SWITCH. MAINTENANCE PERFORMED GEAR SWINGS AND OPS CHECKED OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999071600128 19990716 00128 EU 1999 7 16 VTZA990161 1 19990614 A 3234 HANDLE BAG JETSTM JETSTM3201 1500217 EU LANDING GEAR DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 493UE 805 IAD/BUF - FLT 7486 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR HANDLE WOULD NOT GO ALL THE WAY UP . AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED FOD FROM GEAR HANDLE. MAINTENANCE PERFORMED GEAR SWINGS. OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999071600129 19990716 00129 EA 1999 7 16 VTZA990162 1 19990615 A 5270 STRAP CNDAIR CL600 CL6002B19 EA PASSENGER DOOR LOOSE A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 625BR 7214 RDU/IAD - FLT 7792 - DURING CRUISE, AIRCRAFT DIVERTED TO RIC DUE TO PASSENGER DOOR WARNING ON EICAS. AIRCRAFT WENT TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RE-SECURED LOOSE BONDING STRAP FROM PROXIMITY SENSOR, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999071600130 19990716 00130 EA 1999 7 16 VTZA990163 1 19990616 A 5210 DOOR CNDAIR CL600 CL6002B19 EA PASSENGER COMPT NOT STOWED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 626BR 7225 IAD/CRW - FLT 7745 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED . AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESTORED DOOR HANDLE. OPS CHECK OK. AIRC RAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999071600131 19990716 00131 1999 7 16 VTZA990164 4 19990622 A 3425 HSI BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT TRIPPED A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 471UE 821 IAD/BUF - FLT 7486 - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO CAPTAIN'S HSI FLAGGED. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RE-RACKED CAPTAIN'S HSI. OPS CHECK OK. AIRCRAFT RELEASED AND RE TURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999071600132 19990716 00132 EU 1999 7 16 VTZA990165 1 19990602 A 2844 1241012 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT FUEL SYSTEM FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 472UE 823 IAD/ABE - FLT 7152 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT FUEL PSI WENT INTO YELLOW. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSEPCTED AND REMOVED AND REPLACED PRESSURE TRANSDUCER AND FUEL TRIPLE INDICATOR. OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. REF: OPER CONTROL NR 99ZZZX2588. (X) 2 L 7 2 4T RT A56EU 1999071600133 19990716 00133 EU 1999 7 16 99ZZZX2588 1 19990602 A 2840 696219 INDICATOR BAG JETSTM JETSTM3201 1500217 EU LT FUEL SYSTEM FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 472UE 823 IAD/ABE - FLT 7152 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT FUEL PSI WENT INTO YELLOW. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSEPCTED AND REMOVED AND REPLACED PRESSURE TRANSDUCER AND FUEL TRIPLE INDICATOR. OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. REF: OPER CONTROL VTZA990165. 2 L 7 2 4T RT A56EU 1999071600134 19990716 00134 NM 1999 7 16 TSAA9953277 1 19990526 A 5510 WASHER BOEING 737 7372T4 1384492 NM HORIZ STABILIZER DEFECTIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 HORIZONTAL STABILIZER AFT ATTACH FITTINGS UPPER AND LOWER BOLTS HAVE MIGRATING WASHERS UNDER THE NUTS. REPAIR IAW ECO 2 975. AIRCRAFT RETURNED TO SERVICE. TAT: 30,874.2 HOURS. TAC: 38,783. (X) 2 L 7 2 4F A16WE 1999071600135 19990716 00135 NM 1999 7 16 TSAA9952275 1 19990526 A 5230 FRAME BOEING 737 7372T4 1384492 NM CARGO DOOR CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 AFT CARGO DOOR FORWARD FRAME SUSPECT 3 CRACKS RADIATING FROM BOLT HOLE IN CENTER OF FORWARD FRAME. REPAIRED IAW ECO 297 1. AIRCRAFT RETURNED TO SERVICE. TAT: 30,874.2 HOURS. TAC: 38,783. (X) 2 L 7 2 4F A16WE 1999071600136 19990716 00136 NM 1999 7 16 TSAA9952273 1 19990526 A 5320 654795220 FRAME BOEING 737 7372T4 1384492 NM CARGO DOORWAY CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 FORWARD CARGO PIT DOOR LOWER AFT CORNER FRAME CRACKED. REPAIRED IAW ECO 1988R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999071600137 19990716 00137 NM 1999 7 16 TSAA9957271 1 19990526 A 5730 PANEL BOEING 737 7372T4 1384492 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 RIGHT WING LOWER ACCESS PANEL CUT-OUT AT PANEL NR 7406 CORRODED. BLENDED OUT CORROSION PER SRM 57-30-3, AND AREA RE-ASS ESSED BEYOND LIMITS PER SRM 57-30-3. FILLER FABRICATED IAW ECO 2869 PT1. AREAS REFINISHED WITH BMS 10-20 TYPE II PER M M 53-42-11. (X) 2 L 7 2 4F A16WE 1999071600138 19990716 00138 NM 1999 7 16 TSAA9953268 1 19990526 A 5553 6937481501 BUSHING BOEING 737 7372T4 1384492 NM VERTICAL FIN CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 VERTICAL FIN AFT SIDE OF RIGHT OUTBOARD AFT SPAR ATTACH FITTING CORRODED UNDER BUSHING FLANGE. REPAIR IAW ECO 2973. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999071600139 19990716 00139 NM 1999 7 16 TSAA9953267 1 19990526 A 5553 6937481501 BUSHINGS BOEING 737 7372T4 1384492 NM VERTICAL FIN CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 FUSELAGE LUGS FOR VERTICAL FIN AFT SPAR ATTACH HAVE HEAVY FRETTING ON FACES ON BUSHINGS. REPAIRED PER ECO 2978. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999071600140 19990716 00140 NM 1999 7 16 P2EA99214 1 19990616 A 3260 655281130 MODULE BOEING 737 737247 138448D NM LANDING GEAR FAILED A P2EA O OTHER P NO WARNING INDICATION CR CRUISE 1 CE 05 912MP M00217 19607 MCI - FLT 408 - DURING FLIGHT, AN EMERGENCY WAS DECLARED BECAUSE THE GREEN NOSE GEAR LIGHT ILLUMINATED. THE LANDING GEA R WAS VISUALLY CHECKED IN THE UP POSITION. THE RED NOSE GEAR LIGHT DID NOT ILLUMINATE WHEN THRUST LEVERS WERE AT IDLE W ITH AIRCRAFT IN DESCENT. THE GEAR WAS VISUALLY CHECKED, DOWN AND LOCKED AND THE AIRCRAFT LANDED AT MCI WITH NO INCIDENT . REMOVED AND REPLACED ELECTRICAL MODULE IAW MM 32-09-100. OPERATIONAL CHECK NORMAL IAW MM 32-09-100. (X) 2 L 7 2 4F A16WE 1999071600141 19990716 00141 NM 1999 7 16 P2EA99216 1 19990629 A 2780 MECHANISM BOEING 737 737222 1384473 NM NR 6 LE SLAT OUT OF ADJUST A P2EA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 208AU 19547 MDW - FLT 586 - NR 6 LEADING EDGE SLAT WOULD NOT EXTEND IN FLIGHT UNTIL FLAPS 30 POSITION WAS SELECTED. ADJUSTED TENSIO N ON NR 6 SLAT DETENT ARMS PER MM 27-81-0. SLATS OPERATE NORMALLY. (X) 2 L 7 2 4F A16WE 1999071600142 19990716 00142 NE 1999 7 16 ORJA99172 2 19990512 A 7261 7584654 OIL FILTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A ORJA O OTHER J WARNING INDICATION CL CLIMB 1 WP 11 832RA 53044 725704 LAS - DURING CLIMB-OUT, RIGHT OIL STRAINER CLOG ANNUNCIATOR CAME ON WITH ENGINE AT IDLE. REMOVED AND REPLACED NR 2 ENGI NE MAIN OIL FILTER PER MM 79-20-06. RAN ENGINE, NO LEAKS NOTED. OIL STRAINER CLOG ANNUNCIATOR DID NOT COME ON. OIL TE MPERATURE NORMAL. (X) 2 L 7 2 4F 4 F RT A6WE E9NE 1999071600143 19990716 00143 WP 1999 7 16 HALA9900145 1 19990627 A 3411 FITTING DOUG DC10 DC1010 3022110 WP PITOT STATIC SYS DAMAGED A HALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 160AA 46710 ON CLIMB-OUT, STANDBY ALTIMETER APPROX 2,500 FEET LOWER THAN CAPT AND F/O. ALTIMETER AND STANDBY AIRSPEED IND INDICATI NG 40 KNOTS LOW DURING CRUISE AND CLIMB. CABIN PRESS RELIEF LIGHT CAME ON AT FL 310, DIF PRESS 8.6 AND CABIN ATL 3,000. FOLLOWED PROCEDURE NR 21 SEC 5 PG 30, AND NR 19 SEC 5 PG 28. (STANDBY MODE). LEAK TEST ALT PITOT AND STATIC SYS COND UCTED IAW 34-11-00. PITOT SYS CHK GOOD. STATIC SYS INDICATED LEAK. VISUAL INSP OF SYS REVEALED DAMAGED FITTING AT AMB IENT CONNECTION ON PRESS CONTROLLER. REMOVED AND REPLACED DAMAGED FITTING. RE-CONNECTED STATIC LINE, LEAK CHECK GOOD. (X) 2 L 7 3 4F A22WE 1999071600144 19990716 00144 NM 1999 7 16 BJNA990601 1 19990608 A 3350 9008358 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 AFT EMERGENCY EXIT LIGHT IS VERY DIM. REPLACED BATTERY PACK, OPS CHECKED OK PER BMM 33-51-88. (X) 2 L 7 2 4F RT A16WE 1999071600154 19990716 00154 SW 1999 7 16 HEEA062741 1 19990708 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DETERIORATED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 404PH 1352 53188 MAIN ROTOR GEARBOX RUBBER MOUNT DETERIORATED. 1 G 7 1 3U O H2SW 1999071600166 19990716 00166 WP 1999 7 16 TWAA9909601 1 19990615 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 679 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND A CRACK IN LONGERON 5R, APPROXIMATELY .75 INCH LONG THROUGH RIVET STA 679. REPAIRED PER DRAWING SR09530128. 2 L 7 2 4F A6WE 1999071600167 19990716 00167 WP 1999 7 16 TWAA9909602 1 19990701 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CRACKED APPROXIMATELY .25 INCH IN BEND RADIUS AT FWD LOWER CORNER JUST AFT O F STA 69.5, LBL 12.5 IN. MANUFACTURED NEW INTERCOSTAL PER DRAWING PO9530268. PRIMED AND INSTALLED. 2 L 7 2 4F A6WE 1999071600168 19990716 00168 WP 1999 7 16 TWAA9909603 1 19990701 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, INTERCOSTAL WAS CRACKED APPROXIMATELY .25 INCH IN BEND RADIUS AT FWD LOWER CORNER JUST AFT OF STA 69.5, RBL 12.5. MANUFACTURED NEW INTERCOSTAL PER DRAWING PO9530268. PRIMED AND INSTALLED. 2 L 7 2 4F A6WE 1999071600169 19990716 00169 WP 1999 7 16 TWAA9909604 1 19990701 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND VERTICAL STIFFENER NUMBER 9957860-5, LT SIDE AT APPROXIMATELY STA 69.5, X=+10, CRACKED I N THE RADIUS. CRACK APPROXIMATELY .5 INCH LONG. REPLACED VERTICAL STIFFENER PER DRAWING PO9530268. 2 L 7 2 4F A6WE 1999071600170 19990716 00170 WP 1999 7 16 TWAA9909605 1 19990629 A 5730 SKIN DOUG DC9 DC931 3022065 WP WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CRACK APPROXIMATELY 1 INCH AT TOP OF WING LEADING EDGE AT APPROXIMATELY 18 IN OTBD OF NR 7 LEADING EDGE SLAT TRACK. REPAIRED PER SRM 57-06A. 2 L 7 2 4F A6WE 1999071600171 19990716 00171 WP 1999 7 16 TWAA9909606 1 19990630 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1474 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 958U 49703 DURING CHECK-C MAINT, FOUND THE SKIN CRACKED AT STA 1474, LBL 10. REPAIRED PER ARA 16172. 2 L 7 2 4F A6WE 1999071600172 19990716 00172 WP 1999 7 16 TWAA9909607 1 19990630 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 1474 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 958U 49703 DURING CHECK-C MAINT, FOUND DOUBLER CRACKED BETWEEN FORMER AND SKIN AT STA 1474, LBL 10. REPAIRED PER ARA 16172. 2 L 7 2 4F A6WE 1999071600173 19990716 00173 NM 1999 7 16 AT9900491 1 19990706 A 2131 7612608 CONTROLLER BOEING 737 7372T4 1384492 NM COCKPIT FAILED A ZZDA B EMER. DESCENT O OTHER DE DESCENT 1 SO 15 467AT 22055 AT FLIGHT LEVEL 250, REDUCED POWER FOR DESCENT, CABIN ALTITUDE STARTED TO CLIMB AT 1500 FEET PER MINUTE. STANDBY MODE W AS SELECTED AND TOTALLY LOST PRESSURIZATION, OXYGEN MASK DROP. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. PERFORM ED PRESSURE DECAY CHECK. RE-PACKED OXYGEN MASK. OPS CHECKS AND LEAK CHECKS NORMAL IAW MM 21-31-21, 21-31-0, 5-51-91, A ND 34-11-0. 2 L 7 2 4F A16WE 1999071600174 19990716 00174 WP 1999 7 16 IXXA9900013 1 19990707 A 3260 INDICATION DOUG DC8 DC863F 302198F WP MLG MALFUNCTIONED A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 867BX 1229 46049 EN ROUTE FROM IAH TO TOL, THE MAIN LANDING GEAR NOT LATCHED LIGHT ILLUMINATED DURING THE UPLATCH CHECK, THE MAIN GEAR DO OR NOT LATCHED LIGHT REMAINED EXTINGUISHED. THE FLIGHT CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINI NG THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DISCREP ANCIES NOTED. MAINTENANCE PLACE THE GEAR UPLATCH SYSTEM CHECK ON DEFERRAL IN ACCORDANCE WITH COMPANY PROCEDURES. THE A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999071600175 19990716 00175 WP 1999 7 16 IXXA9900014 1 19990707 A 3260 INDICATION DOUG DC8 DC863F 302198F WP MLG MALFUNCTIONED A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 786AL 1303 46121 EN ROUTE FROM LERT TO LICZ, THE MAIN LANDING GEAR NOT LATCHED LIGHT ILLUMINATED DURING THE UPLATCH CHECK, THE MAIN GEAR DOORS NOT LATCHED LIGHT REMAINED EXTINGUISHED. THE FLIGHT CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMA INING THE SAME. THE FLIGHT CONTINUED TO LICZ FOR AN UNEVENTFUL LANDING. A COMPANY REPRESENTATIVE (FLIGHT ENGINEER) INS PECTED THE AIRCRAFT WITH NO DISCREPANCIES NOTED. THE GEAR UPLATCH SYSTEM CHECK ON DEFERRAL IN ACCORDANCE WITH COMPANY P ROCEDURES. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999071600176 19990716 00176 EU 1999 7 16 AWXA9900233 1 19990625 A 2913 693335 PUMP AIRBUS 320 A320232 3930326 EU HYDRAULIC SYS MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 638AW 6 6 455 BLUE HYDRAULIC LOW QUANTITY. SAW INDICATOR ON ECAM PAGE GO TO AMBER ABOUT 10 MINUTES BEFORE ACTUAL ECAM WARNING. REMOV ED AND REPLACED BLUE SYSTEM HYDRAULIC PUMP PER MM CHAPTER 29-12-51. LEAK AND OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 1999071600177 19990716 00177 NM 1999 7 16 AWXA9900234 1 19990706 A 2121 6454051 FAN BOEING 737 7373G7 1384595 NM CABIN FAILED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 308AW 30902 30902 24710 NORMAL OPS, ODOR IN CABIN. DURING DESCENT INTO PHOENIX AT APPROXIMATELY 10-12,000 FEET, FLIGHT ATTENDANT NOTIFIED FLIGH T DECK OF STRONG BURNING SMELL OVERWING. SMELL IMMEDIATELY ABATED WHEN RECIRCULATION FAN TURNED OFF. PACKS WERE ON HIG H. REMOVED AND REPLACED RECIRCULATION FAN PER MM 21-21-22. LEAK AND OPS CHECK OK. 2 L 7 2 4F RT A16WE 1999071600178 19990716 00178 NM 1999 7 16 AWXA9900235 1 19990706 A 2810 FUEL SYSTEM BOEING 737 7373Y0 1384671 NM LT WING LEAKING A AWXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 28 329AW 23500 AIR TURN BACK, AFTER DEPARTURE, TOWER ADVISED THAT FUEL WAS FLOWING FROM THE LEFT WING. IT WAS VISUALLY CHECKED BY CAPT TO BE A SOLID STREAM FLOWING FROM THE LEFT OUTBOARD PORTION OF THE WING. OPS CHECKED REFUEL SYSTEM IAW MM 28-21-00. N O FAULTS OBSERVED. SUSPECT FUEL EXPANSION INTO SURGE TANK. 2 L 7 2 4F RT A16WE 1999071600179 19990716 00179 EU 1999 7 16 AWXA9900236 1 19990706 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 622AW 054 NORMAL OPS, EXIT LIGHTS NOT ILLUMINATING. EXIT LIGHT ON BOTH FORWARD DOORS NOT ILLUMINATED. REMOVED AND REPLACED EMERG ENCY BATTERY PACK PER MM 33-00. SYSTEM OPS CHECKED NORMALLY ON THE GROUND. BATTERY IS EXPENDABLE; NO SERIALIZED DATA. 2 L 7 2 4F RT A28NM 1999071600180 19990716 00180 NM 1999 7 16 AWXA9900237 1 19990708 A 5313 BAC1498156 STRINGER BOEING 737 737277 1384570 NM BS 1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 IN MAINTENANCE, FOUND CORRODED STRINGER 27L AT FS 1006. REMOVED DAMAGED SECTION OF STRINGER. FABRICATED AND INSTALLED REPAIR PARTS. STRINGER SECTION AND SPLICE PER SRM 53-10-3, FIG 1. 2 L 7 2 4F RT A16WE 1999071600181 19990716 00181 NM 1999 7 16 AWXA9900238 1 19990708 A 5315 654681143 FLOORBEAM BOEING 737 737277 1384570 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 IN MAINTENANCE, CORRODED FLOOR BEAM. FUSELAGE STATION 986, RBL 5, CORRODED BEYOND LIMITS, FLOOR BEAM UPPER SURFACE. RE MOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-9, 51-10-2, AND 51-30-2. 2 L 7 2 4F RT A16WE 1999071600182 19990716 00182 NM 1999 7 16 AWXA9900239 1 19990708 A 5315 65468101 FLOORBEAM BOEING 737 737277 1384570 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 IN MAINTENANCE, FOUND FLOORBEAM CORROSION. CORROSION ON TOP OF FLOORBEAM 967, RBL 12 TO R2 DOOR DRAIN AT RBL 50. REMOV ED AND FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-9 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1999071600183 19990716 00183 NM 1999 7 16 AWXA9900240 1 19990708 A 5313 654587789 STRINGER BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 IN MAINTENANCE, CRACKED STRINGER, LEFT MAIN LANDING GEAR WHEEL WELL AT STRINGER 18A, STATION 727, INBOARD AFT END HI-LOC HAS FRACTURE AND 1 INCH CRACK PROTRUDING FROM FASTENER HOLE. STOP DRILLED CRACK, NDT NOTED NO FURTHER CRACK, AND INSTA LLED REPAIR DOUBLERS/ANGLES PER BOEING SERVICE BULLETIN 737-53-1066 WITH NEW HYLOCS AND AWA ER 2-53-13-19. 2 L 7 2 4F RT A16WE 1999071600184 19990716 00184 NM 1999 7 16 AWXA9900241 1 19990708 A 5743 6549488 FITTING BOEING 737 737277 1384570 NM RT MLG CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 IN MAINTENANCE, FOUND CRACKED SUPPORT BEAM, RT MAIN LANDING GEAR SUPPORT BEAM, OUTBOARD ATTACH FITTING, CRACKED UPPER SI DE, MID-FASTENER HOLE. REMOVED 4 EACH FASTENERS PER SRM 51-31-2. HFEC INSPECTION 4 EACH FASTENER HOLES. NO CRACKS NOT ED ON REAR SPAR. REINSTALLED NEW FASTENERS PER SRM 51-30-2 AND ER 3-57-43-27. APPLIED SEALANT TO HEAD OF FASTENERS PER SRM 51-20-4. ALL WORK PERFORMED PER SB 737-57-1216 AND ER 3-57-43-27. FITTING OK FOR SERVICE. REPLACEMENT REQUIRED B EFORE ADDITIONAL 12,000 CYCLES. 2 L 7 2 4F RT A16WE 1999071600185 19990716 00185 NM 1999 7 16 CALA9900786 1 19990702 A 5280 113N810752SP DOOR BOEING 757 757224 1384958 NM RT MLG DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14107 27297 INSPECTION FOUND IMPACT DAMAGE TO RT MLG FIXED DOOR. REPAIRED IAW SRM 52-80-02. 2 L 7 2 4F RT A2NM 1999071600186 19990716 00186 WP 1999 7 16 CALA9900787 1 19990619 A 5720 STRAP DOUG DC10 DC1030 3023501 WP WS 405 & 506 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 2 INCH EFTACK IN LEFT WING LEADING EDGE STRIP AT STA XORS 455 AND XORS 506. REPAIRED IAW DRAWING 293 3 AND SRM 51-30-00. 2 L 7 3 4F A22WE 1999071600187 19990716 00187 WP 1999 7 16 CALA9900788 1 19990619 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 4 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A .25 INCH CRACK IN INTERNAL SKIN OF RT WING LEADING EDGE SLAT NR 4. A REPAIR WAS PERFORMED IAW SRM 57 -00-01, PAGE 12, FIGURE 4, SHEET 2. 2 L 7 3 4F A22WE 1999071600188 19990716 00188 WP 1999 7 16 CALA9900789 1 19990619 A 5720 STRAP DOUG DC10 DC1030 3023501 WP WS 433-455 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 1.5 CRACK IN RT WING LOWER SKIN LEADING EDGE STRAP BETWEEN STA XORS 433 AND XORS 455. A NEW STRAP WA S INSTALLED IAW DRAWING ARB2935 AND SRM 51-31-01. 2 L 7 3 4F A22WE 1999071600189 19990716 00189 WP 1999 7 16 CALA9900790 1 19990623 A 5720 RA23001755 BOLT DOUG DC10 DC1030 3023501 WP BS 1370 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND TRAPEZOIDAL PANEL BOLT IN RT MLG WHEEL WELL BROKEN AT STA 1370. THE BOLT WAS REPLACED IAW MM 20-50-02. 2 L 7 3 4F A22WE 1999071600190 19990716 00190 WP 1999 7 16 CALA9900791 1 19990623 A 5730 SKIN DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 1.25 CRACK ON RT WING UPPER SKIN DROOPED LEADING EDGE. A REPAIR WAS INSTALLED IAW SRM 57-10-00. 2 L 7 3 4F A22WE 1999071600191 19990716 00191 WP 1999 7 16 CALA9900792 1 19990624 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 2 CRACK IN LEFT WING NR 2 SLAT SKIN. REPAIRED IAW SRM 57-10-00, FIGURE 31. 2 L 7 3 4F A22WE 1999071600192 19990716 00192 WP 1999 7 16 CALA9900793 1 19990624 A 5730 SKIN DOUG DC10 DC1030 3023501 WP BS 1090 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND LEFT WING LOWER SKIN DENTED AT STA 1090. THE SKIN WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999071600193 19990716 00193 WP 1999 7 16 CALA9900794 1 19990626 A 5753 SKIN DOUG DC10 DC1030 3023501 WP LT I/B TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND LEFT WING INBOARD FLAP UPPER SKIN UNBONDED ON INBOARD SIDE. THE SKIN WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999071600194 19990716 00194 WP 1999 7 16 CALA9900795 1 19990626 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1821 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 3 CRACK IN CENTER CARGO NR 12 FLOOR STRUCTURAL BEAM AT STA 1821. A NEW BEAM WAS INSTALLED IAW SRM 51 -30-00 AND MM 25-50-00. 2 L 7 3 4F A22WE 1999071600195 19990716 00195 WP 1999 7 16 CALA9900796 1 19990626 A 5230 ANGLE DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 1 CRACK IN ANGLE AT UPPER AFT SECTION OF CENTER CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999071600196 19990716 00196 WP 1999 7 16 CALA9900797 1 19990626 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1741-1761 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND ONE EACH 1 CRACK IN CENTER CARGO STRUCTURAL FLOORBEAMS NR 9 AND NR 10 BETWEEN STA 1761 AND 1741. THE B EAMS WERE REPLACED IAW SRM 53-00-00 AND MM 25-52-00. 2 L 7 3 4F A22WE 1999071600197 19990716 00197 WP 1999 7 16 CALA9900798 1 19990626 A 5320 JAMB DOUG DC10 DC1030 3023501 WP BS 1721 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 1 CRACK IN CENTER CARGO DOOR JAMB AT STA 1721. THE JAMB WAS REPLACED IAW SRM 53-10-00. 2 L 7 3 4F A22WE 1999071600198 19990716 00198 WP 1999 7 16 CALA9900799 1 19990626 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1721-1741 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 3 CRACK IN CENTER CARGO STRUCTURAL FLOORBEAM NR 12 BETWEEN STA 1721 AND 1741. A NEW BEAM WAS INSTALL ED IAW MM 53-00-00 AND DRAWING AFT7009. 2 L 7 3 4F A22WE 1999071600199 19990716 00199 WP 1999 7 16 CALA9900800 1 19990629 A 7110 LONGERON DOUG DC10 DC1030 3023501 WP NR 2 ENGINE COWL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 1 CRACK IN LEFT LONGERON AND A 1 CRACK IN RT LONGERON OF NR 2 ENGINE CORE COWL. THE CRACKS WERE LOCAT ED NEAR HINGES. THE LONGERONS WERE REPAIRED IAW ECRA 7110-01496. 2 L 7 3 4F A22WE 1999071600200 19990716 00200 WP 1999 7 16 CALA9900801 1 19990706 A 5755 5910055523 SKIN DOUG DC9 DC982 3022082 WP LT SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LEFT WING NR 1 O/B SPOILER DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-01. 2 L 7 2 4F A6WE 1999071600201 19990716 00201 WP 1999 7 16 CALA9900802 1 19990706 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 256-275 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND FORWARD CARGO COMPARTMENT LONGERON 30 CORRODED BETWEEN STA 256 AND 275. THE LONGERON SECTION WAS REMOV ED AND REPLACED IAW SRM 53-02, FIGURE 14. 2 L 7 2 4F A6WE 1999071600202 19990716 00202 WP 1999 7 16 CALA9900803 1 19990706 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 465-484 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16813 48066 INSPECTION FOUND LONGERON 30 CORRODED ON O/B SIDE IN FORWARD CARGO COMPARTMENT BETWEEN STA 465 AND 484. THE LONGERON SE CTION WAS REPLACED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1999071600203 19990716 00203 WP 1999 7 16 CALA9900804 1 19990707 A 5751 5910046508 SKIN DOUG DC9 DC932 3022066 WP RT AILERON BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND RT AILERON BULGING. THE AILERON WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-10-31. 2 L 7 2 4F A6WE 1999071600204 19990716 00204 NM 1999 7 16 CALA9900805 1 19990707 A 5330 SKIN BOEING 737 7373T0 1384582 NM WINDOW FRAME CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND A .375 INCH CRACK IN OUTBOARD CORNER OF CAPTAIN'S FORWARD WINDOW FRAME. VA DOUBLER WAS INSTALLED IAW EC RA 5330-02841. 2 L 7 2 4F RT A16WE 1999071600205 19990716 00205 WP 1999 7 16 CALA9900806 1 19990708 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1102-1215 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72824 49484 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1102-1215. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 . 2 L 7 2 4F A6WE 1999071600206 19990716 00206 WP 1999 7 16 CALA9900807 1 19990708 A 5711 SPAR CAP DOUG DC10 DC1010 3022110 WP WS 802-895.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LOWER SPAR CAP CORRODED AT RT WING O/B T/E AILERON CAVITY AT STA XW 802.5 TO XW 895.5. THE CORROSION W AS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5710-01962. 2 L 7 3 4F A22WE 1999071600207 19990716 00207 WP 1999 7 16 CALA9900808 1 19990708 A 5711 SPAR DOUG DC10 DC1010 3022110 WP WS 158 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LEFT WING I/B FALSE SPAR UPPER CAP CORRODED O/B OF SPAR INNER MOST END AT XW 158. THE CORROSION WAS RE MOVED AND FALSE SPAR WAS REPAIRED IAW ECRA 5722-01004. 2 L 7 3 4F A22WE 1999071600208 19990716 00208 WP 1999 7 16 CALA9900809 1 19990708 A 5510 STRIP DOUG DC10 DC1010 3022110 WP HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER MOST I/B L/E ACCESS STRIP CORRODED ON O/B EDGE. THE ACCESS STRIP WAS REPAIRED IAW ECRA 5513-01003. 2 L 7 3 4F A22WE 1999071600209 19990716 00209 WP 1999 7 16 CALA9900810 1 19990708 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND THE RT LOWER FUSELAGE SKIN AFT OF NOSE GEAR CRACKED COMPLETELY THROUGH. REMOVED AND INSTALLED LOWER FU SELAGE SKIN IAW SRM 53-05. 2 L 7 2 4F A6WE 1999071600210 19990716 00210 WP 1999 7 16 CALA9900811 1 19990708 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1007-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND AFT CARGO TIE DOWN TRACK CORRODED AT STA 1007-1155. THE TIE DOWN TRACK WAS REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999071600211 19990716 00211 WP 1999 7 16 CALA9900812 1 19990708 A 5543 SKIN DOUG DC9 DC982 3022082 WP RUDDER TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND RUDDER TRIM TAB DELAMINATED ON TRAILING EDGE AT AFT TOP CORNER AND BOTTOM CORNER. THE RUDDER TAB WAS R EMOVED, REPAIRED, AND REINSTALLED IAW MM 27-20-2 AND SRM 51-90-2. 2 L 7 2 4F A6WE 1999071600212 19990716 00212 NM 1999 7 16 CALA9900813 1 19990629 A 5347 TRACK BOEING 737 7373T0 1384582 NM BS 290 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND GALLEY TRACK CORRODED AT STA 290, RBL 45. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999071600213 19990716 00213 NM 1999 7 16 CALA9900814 1 19990708 A 5320 GUSSET BOEING 737 7373T0 1384582 NM BS 1130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A .5 INCH CRACK IN TORQUE BOX GUSSET AT STABILIZER CENTER SECTION, STA 1130. THE TORQUE BOX GUSSET WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999071600214 19990716 00214 WP 1999 7 16 9902351162 1 19990616 A 2410 LINE DOUG DC10 DC1040 3023508 WP NR 3 CSD LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 162US 46771 EN ROUTE TO HNL FROM SEA, NR 2 CSD OIL PRESSURE LOW LIGHT ILLUMINATED, NR 3 CSD ON MEL. FLIGHT RETURNED TO SEA AND LAND ED WITHOUT INCIDENT. FOUND CSD LINE LEAKING. REPAIRED FILL LINE. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999071600215 19990716 00215 WP 1999 7 16 9902361154 1 19990702 A 2130 VALVE DOUG DC10 DC1040 3023508 WP PRESS SYS CONTAMINATED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 154US 46763 DURING CRUISE FROM DTW TO SFO, UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO, STANDBY, OR MANUAL. AFTER DESCENT TO FL140, A BLE TO USE MANUAL CONTROL. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. FOUND INSULATION STUCK IN LOWER PRESSUR E RELIEF VALVE AND UPPER VALVE DOOR STUCK PARTIALLY OPEN. REPLACED BOTH UPPER AND LOWER CABIN PRESSURE RELIEF VALVE. O PERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999071600216 19990716 00216 WP 1999 7 16 9902379852 1 19990702 A 3230 CONTROL BOX DOUG DC9 DC951 3022051 WP NLG FAILED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 761NC 47709 DURING CLIMB-OUT FROM VPS, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS CONTINUED TO DE STINATION (MEM) WITH GEAR DOWN AND LANDED WITHOUT INCIDENT. CREW DECLARED AN EMERGENCY WITH ATC AS A PRECAUTION. MAINT ENANCE REPLACED PROXIMITY CONTROL BOX AND NOSE GEAR UPLOCK SENSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT A6WE 1999071600217 19990716 00217 WP 1999 7 16 9902389602 1 19990704 A 3620 CONNECTOR DOUG DC9 DC932 3022066 WP TAIL COMPT BROKEN A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 602NW 47046 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED T O MSP. MAINTENANCE FOUND LOOSE CLAMPS CAUSING LEAK FROM RIGHT HEAT EXCHANGER AND CANNON PLUG BROKEN OFF OF TEMPERATURE SENSOR. TIGHTENED CLAMPS TO RIGHT HEAT EXCHANGER AND REPLACED CANNON PLUG. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F A6WE 1999071600218 19990716 00218 NE 1999 7 16 9902399610 2 19990702 A 7321 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LT & RT ENGINE OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 610NW 47432 657568 DURING TAKEOFF ROLL AT 100 KNOTS, THE RIGHT ENGINE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETU RNED TO GATE. MAINTENANCE TRIMMED THE FUEL CONTROLS FOR THE LEFT AND RIGHT ENGINES. OPERATIONAL CHECK OK. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1999071600219 19990716 00219 WP 1999 7 16 9902409154 1 19990705 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND THE ESCAPE PATH EMERGENCY LIGHTING ON CATWALK INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999071600220 19990716 00220 WP 1999 7 16 9902419155 1 19990705 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING ON CATWALK INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999071600221 19990716 00221 SO 1999 7 16 COMA9910105 1 19990706 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 256CA 120245 EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999071600222 19990716 00222 SO 1999 7 16 COMA9910106 1 19990706 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN MISSING A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 246CA 120223 EXIT SIGN AT ROW 5 IS MISSING. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999071600223 19990716 00223 EA 1999 7 16 COMA9960339 1 19990707 A 3222 16050103 STRUT CNDAIR CL600 CL6002B19 EA NLG REQD SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 934CA 12426 1 7042 GEAR DISAGREE WARNING NLG DID NOT RETRACT. FOUND NLG SHOCK STRUT REQUIRED SERVICING. SERVICED NLG STRUT AND AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999071600224 19990716 00224 EA 1999 7 16 COMA9960340 1 19990706 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 986CA 7174 EMERGENCY FLOOR LIGHTING AFT OF WING IS INOPERABLE. RECONNECTED LOOSE WIRING CONNECTOR. 2 L 7 2 4F RT A21EA 1999071600225 19990716 00225 EA 1999 7 16 COMA9960341 1 19990707 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA SERVICE DOOR BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912CA 7011 EMERGENCY LIGHT BY SERVICE DOOR BROKEN. REPLACED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 1999071600226 19990716 00226 EA 1999 7 16 COMA9960342 1 19990703 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 937CA 6079 4591 7044 FLAPS FAIL MESSAGE. REPLACED THE LEFT HAND FLAP NR 3 ACTUATOR. 2 L 7 2 4F RT A21EA 1999071600227 19990716 00227 EA 1999 7 16 COMA9960343 1 19990705 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 739CA 8371 9 7273 FLAPS FAIL MESSAGE. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999071600228 19990716 00228 EA 1999 7 16 COMA9960344 1 19990705 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 978CA 1442 7158 FLAPS FAIL MESSAGE. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 1999071600229 19990716 00229 EA 1999 7 16 COMA9960345 1 19990704 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA ROW 9-12 LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 EMERGENCY LIGHTS ROW 9 THROUGH 12 ARE INOPERABLE. SECURED LOOSE ELECTRICAL CONNECTOR. 2 L 7 2 4F RT A21EA 1999071600230 19990716 00230 EA 1999 7 16 COMA9960347 1 19990704 A 5210 DOOR CNDAIR CL600 CL6002B19 EA CABIN NOT SECURED A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 914CA 7012 MAIN CABIN DOOR AIR LEAK IN AREA OF GROUND STRAP. SECURED THE DOOR ELECTRICAL BONDING STRAP. PRESSURIZED AIRCRAFT. NO LEAKS FOUND. 2 L 7 2 4F RT A21EA 1999071600231 19990716 00231 EA 1999 7 16 COMA9960346 1 19990704 A 3230 102255 BRACKET CNDAIR CL600 CL6002B19 EA NLG BENT A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 931CA 7037 LANDING GEAR DISAGREE MESSAGE. NLG DID NOT RETRACT. REPLACED THE NLG CENTERING PROX SWITCH TARGET BRACKET. 2 L 7 2 4F RT A21EA 1999071600232 19990716 00232 EA 1999 7 16 COMA9960348 1 19990627 A 5320 601R311358 ANGLE CNDAIR CL600 CL6002B19 EA BS 2800 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 14988 7014 ANGLE CRACKED AT FS 2800 ON RIGHT SIDE OF BEAM RBL9. INSTALLED NEW ANGLE IAW REO 601R-53-11-136 STEPS 9 AND 10. 2 L 7 2 4F RT A21EA 1999071600233 19990716 00233 EA 1999 7 16 COMA9960349 1 19990627 A 5320 601R311358 ANGLE CNDAIR CL600 CL6002B19 EA BS 2800 CRACKED A COMA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 SO 01 916CA 14988 7014 ANGLE CRACKED AT FS 2800, LEFT SIDE OF FLOORBEAM LBL9. REPLACED ANGLE IAW CRJ SRM 51-42-71. REO 601R 53-11-136 STEPS 9 AND 10. 2 L 7 2 4F RT A21EA 1999071600234 19990716 00234 EA 1999 7 16 COMA9960350 1 19990629 A 5320 601R311357 ANGLE CNDAIR CL600 CL6002B19 EA BS 2800 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 14988 7014 ANGLE CRACKED AT FS 2800 OUTBOARD OF FLOOR SUPPORT BEAM AT LBL9. REPLACED ANGLE IAW REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 1999071600235 19990716 00235 EA 1999 7 16 COMA9960351 1 19990629 A 5315 601R311367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 355 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 14988 7014 FLOOR SUPPORT BEAM LBL27 HAS CORROSION AT FS 330. REPLACED FLOORBEAM BETWEEN FS 310.00 AND FS 355.00 IAW REO 601R-53-00 27. 2 L 7 2 4F RT A21EA 1999071600236 19990716 00236 EA 1999 7 16 COMA9960352 1 19990629 A 5315 601R311367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 319 & 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 14988 7014 FLOOR SUPPORT BEAM RBL 9 IS CORRODED BETWEEN FS 319.0 AND FS 349.0. REMOVED CORRODED SECTION AND INSTALLED A NEW SECTIO N OF FLOORBEAM IAW REO 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999071600237 19990716 00237 EA 1999 7 16 COMA9960353 1 19990629 A 5315 601R311367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 319 & 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 14988 7014 FLOOR SUPPORT BEAM RBL 27 HAS CORROSION BETWEEN FS 319.0 AND FS 349.0. REMOVED CORRODED SECTION OF FLOORBEAM AND INSTAL LED NEW SECTION OF FLOORBEAM IAW REO 601R-53-00-27. 2 L 7 2 4F RT A21EA 1999071600238 19990716 00238 EA 1999 7 16 COMA9960354 1 19990708 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 14729 7017 FLOOR SUPPORT BEAMS HAVE SEVERAL AREAS OF CORROSION BETWEEN FS 280.0 TO FS 409.0. REMOVED AND REPLACED FLOOR SUPPORT BE AMS LBL9, RBL27, RBL9, LBL27. P/N 601R31113-67 IAW ENGINEERING ORDER 601R-53-0089. 2 L 7 2 4F RT A21EA 1999071600239 19990716 00239 WP 1999 7 16 UPS99830033 1 19990618 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 425.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XFS 425, 5 FWD OF THE SPAR IS CRACKED AT A FASTENER HOLE. STOP DRILLED CRACK & REPAIRED IAW E.O. DC8-5720-4087. 2 L 7 4 4F RT 4A25 1999071600240 19990716 00240 WP 1999 7 16 UPS99830062 1 19990708 A 3260 SWITCH DOUG DC8 DC873F 302199F WP LT MLG DOOR LOOSE A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 801UP 46101 GEAR UPLATCH CHECK FAILED. FOLLOWED CHECK LIST. CHECK STILL FAILED. BOTH DOORS NOT LATCHED AND GEAR NOT LATCHED LIGHT S ILLUMINATED. BOTH ALTERNATE GEAR (MAIN) DOOR LIGHTS ALSO ILLUMINATED DURING UPLATCH CHECK. MAIN GEAR DOOR LIGHT SWIT CH MOVED LEFT DOOR NOT LATCHED LIGHT WENT OUT. MOVED RIGHT, LIGHT STAYED ON. 2 L 7 4 4F RT 4A25 1999071600241 19990716 00241 WP 1999 7 16 UPS99830064 1 19990707 A 3397 WIRE DOUG DC8 DC871F 302199D WP COCKPIT SHORTED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 701UP 45938 EMERGENCY EXIT LIGHTS INOP. T/S AND FOUND WIRE LG19DW22 SHORTED TO GROUND AT COCKPIT DOME LIGHT ASSY. REPAIRED WIRE LI GHT, OP CHECKS GOOD. 2 L 7 4 4F RT 4A25 1999071600242 19990716 00242 EU 1999 7 16 QXEA9901435 1 19990706 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 488US 11240 GEG - BOTH OVERHEAD EMERGENCY EXIT SIGNS AT ROW 8 ARE OUT. REMOVED AND REPLACED EXIT SIGNS AT ROW 8. OPERATIONAL TEST ED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999071600243 19990716 00243 NE 1999 7 16 99FDEA00252 2 19990708 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 3 MALFUNCTIONED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 491FE 21529 99-154 - DURING CLIMB-OUT, NR 3 ENG OIL LOW PRESS/FILTER BYPASS LIGHT CAME ON. SHUT DOWN ENGINE IN FLT. 2 L 7 3 4F 4 F A3WE E2EA 1999071600244 19990716 00244 NM 1999 7 16 99FDEA00253 1 19990702 A 7930 1163P182 BYPASS SWITCH BOEING 727 727227 1384078 NM NR 3 ENGINE MALFUNCTIONED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 491FE 21529 99-155 - ON CLIMB-OUT PASS 7000 MSL, NR 3 ENGINE OIL PRESS LOW/FILTER BYPASS LIGHT CAME ON. REPLACED FILTER AND SEALS P ER 79-00-00. REMOVED AND REPLACED OIL BYPASS SWITCH AS PERCAUTION. 2 L 7 3 4F A3WE 1999071600245 19990716 00245 WP 1999 7 16 99FDEA00254 1 19990708 A 3213 STRUT DOUG DC10 DC1010F 3022111 WP LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 061FE 46973 NR 466 - LEFT MLG HAS CORROSION ON EXT INSIDE OF BEAR STRUT AT O-RING GROOVE. REMOVED AND REPLACED MLG EXT AND TORQUED BOLTS AS PER MM 32-11-04. SERV STRUT PER MM 32-11-01. 2 L 7 3 4F A22WE 1999071600246 19990716 00246 WP 1999 7 16 99FDEA00256 1 19990709 A 5270 CONNECTOR DOUG DC10 DC1010F 3022111 WP NR 2 PACK DOOR DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 054FE 47808 99-156 - AIR COND LIGHT CAME ON AT ABOUT 40 MIN INTO THE FLT. REMOVED CANNON PLUG FROM NR 2 PACK (AC) DOOR. CLEANED PL UG AND REINSTALLED CYCLE SW SEV TIMES. OPS CK NORM IAW 52-70-07-2. 2 L 7 3 4F A22WE 1999071600247 19990716 00247 WP 1999 7 16 99FDEA00255 1 19990708 A 3213 STRUT DOUG DC10 DC1010F 3022111 WP LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 061FE 46973 NR 470 - UPPER SURFACE OF LEFT MLG AFT OF PLUG HAS SURFACE CORROSION. REMOVED CORROSION MAIN GEAR STRUT COMPLIED WITH E A 8-3211-40488. 2 L 7 3 4F A22WE 1999071600248 19990716 00248 NM 1999 7 16 DL72L991518 1 19990706 A 5260 STAIRS BOEING 727 727232 1384082 NM TAIL DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 COMPLY WITH SRM 53-30-3 PERMANENT REPAIR. TIME LTD DBLR AT VENTRAL STAIR CUTOUT. REPAIRED PER ERA 333311-14. REF NR 1 83 AND NR 741. FABRICATED REPAIR PIECES PER PER ERA 333311-14. OK TO INSTALL. INSTALLED REPAIR PER ERA 333311-14. 2 L 7 3 4F A3WE 1999071600249 19990716 00249 NM 1999 7 16 DLM88991520 1 19990706 A 2424 REGULATOR DOUG MD88 MD88 3023688 NM APU OUT OF ADJUST A DALA K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 937DL 49810 LT GEN ON MCO, APU WOULD NOT STAY ON LINE. ADJUSTED LEFT ENGINE GEN FREQUENCY. OPS GOOD. 2 L 7 2 4F RT A6WE 1999071600250 19990716 00250 NM 1999 7 16 DL73K991521 1 19990702 A 5312 BULKHEAD BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 320DL 23092 DURING CORROSION VISIT, 3 INCH CRACK IN 178 BULKHEAD WAS REPAIRED PER SRM 53-10-11 FIG 1 REFER TO NR62. 2 L 7 2 4F RT A16WE 1999071600251 19990716 00251 NM 1999 7 16 DL72S991522 1 19990706 A 5720 STIFFENER BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 REF SHIP 497 TPA LTR CHK D-1, NR 7 SLAT I/B TRACK I/B L/E SPAR STIFFENER CRACKED. REPLACED STIFFENER PER MM 57-20-21. 2 L 7 3 4F A3WE 1999071600252 19990716 00252 NM 1999 7 16 DL72S991523 1 19990706 A 5754 STIFFENER BOEING 727 727232 1384082 NM NR 3 SLAT TRACK CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 NR 3 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. NR 3 SLAT I/B TRACK O/B SPAR STIFFENER CRACKED. REPLACED STIFFENERS PE R M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1999071600253 19990716 00253 NM 1999 7 16 DL757991525 1 19990706 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 615DL 22822 FIRST CLASS EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A2NM 1999071600254 19990716 00254 NE 1999 7 16 DL72K991526 2 19990707 A 7314 FUEL PUMP 37820115 BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 27 413DA 5726 21233 NR 1 ENGINE QUIT RIGHT AFTER ROTATION ON TAKEOFF FLIGHT. ATTENDENT REPORTED A POPPING NOISE NO OTHER ABNORMAL IND, FUEL PUMP SHAFT SHEARED. REPLACED SAME AND CONTROL. 2 L 7 3 4F 4 F A3WE E2EA 1999071600255 19990716 00255 NM 1999 7 16 DL72W991528 1 19990707 A 5755 CASTING BOEING 727 7272Q8 138407W NM NR 12 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 DRG TPA LTR CHK E1, NR 12 SPOILER ACTUATOR SUPPORT FITTING O/B MOUNT CASTING LWR MOUNT BOLT LOBE BROKEN OFF. REPLACED C ASTING PER MM 57-42-0. 2 L 7 3 4F A3WE 1999071600256 19990716 00256 NM 1999 7 16 DL73E991529 1 19990707 A 5270 WIRE 693731754 BOEING 737 737247 138448D NM P5 PANEL FAILED A DALA H DEACTIVATE SYST/CIRCUITS P NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 375DL D00359 23602 FOUND WIRING TO DOOR WARNING MODULE ON P5 PANEL SHORTING ON HYD PUMP CONTROL PANEL. REPAIRED WIRING AND REPLACED HYD PU MP CONTROL PANEL. 2 L 7 2 4F A16WE 1999071600257 19990716 00257 NE 1999 7 16 DL757991530 2 19990705 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 FAILED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 636DL 40574 23763 716317 N CRUISE AT 370, LEFT ENG OIL PRESS WENT TO ZERO, STARTED LOOKING FOR QTY, SHOWED ZERO. STARTED TO THROTTLE BACK, LEFT ENG POPPED THEN SHUT ITSELF DOWN. SUDDEN FAILURE, OIL TEMP NEVER ROSE, WINDMILLED ENG AT 25 MIN. 2 L 7 2 4F 4 F RT A2NM E17NE 1999071600258 19990716 00258 NM 1999 7 16 DL757991531 1 19990708 A 2120 AIR DIST BOEING 757 757232 1384965 NM COCKPIT ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 643DL 23997 FAINT ELECTRICAL ODOR IN THE COCKPIT DURING DESCENT. CREW REPORTED FAINT SMELL AT 15000FT AND DISAPPEARED BY 11000 FT. PULLED INST PNLS OUT. CHECKED C/B'S, NONE POPPED, RAN PACKS CHECKED RECIRC FAN. CHECKED OPS OF COCKPIT LTS. CHECKED E AND E COMPT, NO IND OF ELECTRICAL PROBLEMS OR ODORS NOTED. ALL COCKPIT IND NORMAL. 2 L 7 2 4F RT A2NM 1999071600259 19990716 00259 NM 1999 7 16 DL72S991532 1 19990708 A 5330 65545801 SKIN BOEING 727 727232 1384082 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 GOUGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUOUT AT BS 990, LOCATED AT S24R. THE DAMAGE WAS IN THE SKIN , DOUBLER, TRIPLER AND BEAR STRAP. REWORKED PER ERA 333326-14, REV A. 2 L 7 3 4F A3WE 1999071600260 19990716 00260 NM 1999 7 16 DL72L991533 1 19990708 A 5330 6518420762 SKIN BOEING 727 727232 1384082 NM BS 306 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 GOUGE FOUND IN THE FUSELAGE SKIN JUST ABOVE THE THE L1 DOOR LOWER HINGE CUTOUT. REPAIRED PER ERA 333323-14, REV A. 2 L 7 3 4F A3WE 1999071600261 19990716 00261 WP 1999 7 16 DLL19991534 1 19990708 A 5320 1542396 DECK LKHEED 1011 10113853 5265020 WP BS 415 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 764DA 193H1202 THE NOSE LANDING GEAR PRESSURE DECK WAS FOUND CRACKED IN SIX LOCATIONS. THE LOCATIONS ARE FROM FS 395 TO 437, BETWEEN R BL 24 AND LBL 24. REPAIRED PER ERA 333267-14, REV A. 2 L 7 3 4F A23WE 1999071600262 19990716 00262 NM 1999 7 16 DL72L991537 1 19990614 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 RIB CRACKED INSIDE NR 4 L/E SLAT INBD SIDE OF ACTUATOR ATTACH POINT. REMOVED DAMAGED AREA FABRICATED DOUBLER AND REPLAC EMENT CLIP PER M/M 57-54-00 FIG 809. TREAT AND PAINTED. OK TO INSTALL. REPAIRED CRACKED RIB MM 57-40-00 FIG 809. 2 L 7 3 4F A3WE 1999071600263 19990716 00263 NM 1999 7 16 DL72K991538 1 19990709 A 3350 POWER SUPPLY 900835A BOEING 727 727232 1384082 NM ROW 4 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 7290 21583 EMERGENCY EXIT SIGN AT ROW 4 FAILED TO ILLUMINATE DURING TEST BY CREW MEMBER. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 1999071600264 19990716 00264 NM 1999 7 16 SCNA99088 1 19990705 A 2611 SMOKE DETECTOR BOEING 727 727259 138408J NM FWD LAVATORY INOPERATIVE A SCNA K NONE N FALSE WARNING NR NOT REPORTED 1 GL 15 289SC 22475 DURING FLIGHT, THE SMOKE DETECTOR IN THE FORWARD LAV ALARMS CONTINUOUSLY AFTER TESTING. REMOVED AND REPLACED THE SMOKE DETECTOR IN THE FORWARD LAVATORY. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999071600265 19990716 00265 NM 1999 7 16 SWAA991142 1 19990706 A 5312 6546568 BULKHEAD BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STRINGER 6L. REPAIRED BULKHEAD PER SWA RA NR 1-253-2113. 2 L 7 2 4F A16WE 1999071600266 19990716 00266 NM 1999 7 16 SWAA991143 1 19990706 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM ROW 18DEF INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 18 DEF. RELAMPED PER MM. 2 L 7 2 4F A16WE 1999071600267 19990716 00267 NM 1999 7 16 SWAA991144 1 19990703 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387SW 26602 EEPLS LIGHTS PULLED UP AT FWD END. RESECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999071600268 19990716 00268 1999 7 16 SWAA991145 4 19990705 A 2565 031591475 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 FWD ENTRY DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999071600269 19990716 00269 NM 1999 7 16 SWAA991146 1 19990705 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 19 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED RON CHECK, FOUND EEPLS LIGHT INOP AT ROW 19. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999071600270 19990716 00270 NM 1999 7 16 SWAA991147 1 19990706 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F A16WE 1999071600271 19990716 00271 NM 1999 7 16 SWAA991148 1 19990706 A 3350 BR2013 BULB BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS LIGHT INOP. REPLACED LIGHT BULBS PER MM. 2 L 7 2 4F A16WE 1999071600272 19990716 00272 NM 1999 7 16 SWAA991149 1 19990706 A 3350 65C27093 LENS BOEING 737 7372H4 138448C NM SERVICE DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS ASSY PER MM. 2 L 7 2 4F A16WE 1999071600273 19990716 00273 NM 1999 7 16 SWAA991150 1 19990706 A 3350 6227421 POWER SUPPLY BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CEILING EMERGENCY LIGHT POWER SUPPLY INOP. REMOVED AND REPLACED POWER SUPPLY ASSY PER MM. 2 L 7 2 4F A16WE 1999071600274 19990716 00274 NM 1999 7 16 SWAA991151 1 19990706 A 3350 2013 BATTERY PACK BOEING 737 7372H4 138448C NM AFT GALLEY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP ON AFT GALLEY OVERHEAD. REMOVED AND REPLACED BATTERY PA CKS PER MM. 2 L 7 2 4F A16WE 1999071600275 19990716 00275 NM 1999 7 16 SWAA991152 1 19990706 A 3350 622742 BATTERY BOEING 737 7373H4 1384600 NM AFT CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS BATTERY ASSY INOP. RECHARGED BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999071600276 19990716 00276 NM 1999 7 16 SWAA991153 1 19990706 A 5512 6573782 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED IN AFT SPAR, FWD OF NR 1 BALANCE BAY. REPAIRED SK IN PER BFG ER NR 99-5642 AND SRM. 2 L 7 2 4F RT A16WE 1999071600277 19990716 00277 NM 1999 7 16 SWAA991154 1 19990706 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 1141 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D-CHECK, FOUND BS 1141, STRINGERS 5A LT AND 5A RT CRACKED AT LOWER CHORD. REPAIRED STRINGERS PER SRM. 2 L 7 2 4F RT A16WE 1999071600278 19990716 00278 NM 1999 7 16 SWAA991155 1 19990706 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM ROW 9D MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING IN BULLNOSE AT ROW 9D. REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999071600279 19990716 00279 NM 1999 7 16 SWAA991156 1 19990706 A 3350 07912 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT LENS MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999071600280 19990716 00280 NM 1999 7 16 SWAA991157 1 19990706 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 EEPLS LIGHT HAS EXPOSED WIRES AND MISSING LENS. REPAIRED WIRES AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999071600281 19990716 00281 NM 1999 7 16 SWAA991158 1 19990707 A 5620 655670 WINDOW BOEING 737 7373H4 1384600 NM LT EMER EXIT MISSING A SWAA K NONE O OTHER CR CRUISE 1 SW 07 353SW 24889 DURING FLIGHT, A BANG NOISE FOLLOWED BY A LOUD PRESS LEAK COMING OUT OF LT OVERWING EXIT. AFTER LANDING DISCOVERED OUT ER GLASS PANE ON LT OVERWING WINDOW MISSING. REMOVED AND REPLACED LT OVERWING EXIT HATCH OUTER WINDOW ASSY PER MM. 2 L 7 2 4F RT A16WE 1999071600282 19990716 00282 NM 1999 7 16 SWAA991159 1 19990706 A 7933 19801618 CONNECTOR BOEING 737 7372H4 138448C NM NR 1 ENGINE DIRTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 063SW 22061 AIR TURNBACK---- DURING CLIMB, NR 1 ENG OIL TEMP ROSE PAST THE GREEN ARC INTO THE YELLOW AND WOULD NOT DECREASE. CLEAN ED ALL NR 1 ENG CONNECTORS AT GROUND FLANGE ON HARNESS. RAN ENG, OPS CK GOOD. 2 L 7 2 4F A16WE 1999071600283 19990716 00283 NM 1999 7 16 SWAA991160 1 19990707 A 3350 65C37192 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT EVACUATION SLIDES LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM . 2 L 7 2 4F A16WE 1999071600284 19990716 00284 NM 1999 7 16 SWAA991161 1 19990707 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 873 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C1 CHECK, FOUND THRU EDDY CURRENT INSP CRACKED FUSELAGE SKIN, BS 873, STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999071600285 19990716 00285 NM 1999 7 16 SWAA991162 1 19990707 A 2560 65546 HOLDER BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR GIRT BAR HOLDERS ON SLIDE PACK LOOSE. TIGHTENED HOLDERS PER MM. 2 L 7 2 4F A16WE 1999071600286 19990716 00286 NM 1999 7 16 SWAA991163 1 19990707 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 785 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT STRINGER 26L, BS 785. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999071600287 19990716 00287 NM 1999 7 16 SWAA991164 1 19990707 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FWD GALLEY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 294.5, BL 0 - LBL 17. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999071600288 19990716 00288 NM 1999 7 16 SWAA991165 1 19990707 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D-CHECK, FOUND 5 CRACKS AT BS 178 BULKHEAD BETWEEN LBL 6 RBL 6. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999071600289 19990716 00289 NM 1999 7 16 SWAA991166 1 19990707 A 3350 65C27093 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD ENTRY AND SERVICE DOORS. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999071600290 19990716 00290 NM 1999 7 16 SWAA991167 1 19990708 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS LIGHTS COMING APART ON FLOOR. REPAIRED LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999071600291 19990716 00291 NM 1999 7 16 SWAA991168 1 19990708 A 7933 726 CONNECTOR BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A SWAA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SW 07 528SW 26570 721128 IN FLIGHT/ ENGINE SHUT DOWN--- DURING CLIMB NR 2 ENG OIL TEMP INDICATOR READ 150 DEGREES, 12 MINUTES LATER TEMP WENT UP TO 195 DEGREES. ALL OTHER ENG INDICATIONS NORMAL. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB CANNON PLUG AND OIL TEM P BULB AS A PRECAUTION. ENG OPS CKD GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999071600292 19990716 00292 NE 1999 7 16 SWAA991169 2 19990708 A 7530 1216643 VBV DOOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 300SW 22940 726160 ABORTED TAKEOFF---- NR 2 ENG THRUST WOULD NOT ADVANCE ON TAKEOFF ROLL. REMOVED AND REPLACED NR 2 ENG VBV DOOR ASSY AT 5 O'CLOCK POSITION PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999071600293 19990716 00293 NM 1999 7 16 SWAA991170 1 19990708 A 3350 101114 LENS BOEING 737 7372H4 138448C NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 FLIGHT DECK EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F A16WE 1999071600294 19990716 00294 NM 1999 7 16 SWAA991171 1 19990708 A 5320 6545409 WEB BOEING 737 7373A4 1384585 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULE 1/2D CHECK, FOUND CRACK IN PRESSURE WEB, BS 665, LBL 32. REPAIRED WEB PER SWA RA NR 1-353-2112. 2 L 7 2 4F RT A16WE 1999071600295 19990716 00295 NM 1999 7 16 SWAA991137 1 19990703 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 986 RBL 10-43. REPAIRED BEAM PER SWA RA NR 1-353-2103. 2 L 7 2 4F RT A16WE 1999071600296 19990716 00296 NM 1999 7 16 SWAA991138 1 19990703 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT KEEL BEAM, BS 520. REPAIRED BEAM PER SWA RA NR 1-353-2107 AND SRM. 2 L 7 2 4F RT A16WE 1999071600297 19990716 00297 NM 1999 7 16 SWAA991139 1 19990703 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STUB FRAME, BS 294, RBL 53. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999071600298 19990716 00298 NM 1999 7 16 SWAA991140 1 19990704 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD, BS 178, LBL 6.5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999071600299 19990716 00299 NM 1999 7 16 SWAA991141 1 19990703 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D-CHECK, FOUND CRACKED BULKHEAD, BS 178, RBL 1 - LBL 1. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999071600300 19990716 00300 NM 1999 7 16 SWAA991131 1 19990701 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 8 DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 EMERGENCY ESCAPE FLOOR LIGHT PULLED OUT OF TRACK AT ROW 8. REPLACED WITH NEW TRACK LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999071600301 19990716 00301 NM 1999 7 16 SWAA991132 1 19990703 A 2611 PU90499R3 SMOKE DETECTOR BOEING 737 7377H4 NM LAVATORY MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 727SW 27859 AIR TURNBACK---- LOUD NOISE APPEARS TO COME FROM F/O'S WINDOW ABOVE 9000 FEET. FOUND FWD AND AFT LAV SMOKE DETECTORS AL ARMING. REMOVED AND REPLACED SMOKE DETECTORS PER MM, NOISE WENT AWAY. 2 L 7 2 4F RT A16WE 1999071600302 19990716 00302 NM 1999 7 16 SWAA991133 1 19990702 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM ROW 9 DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 350SW 24409 EMERGENCY ESCAPE LIGHT AT BULLNOSE PUSHED THRU, ROW 9. RESECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999071600303 19990716 00303 1999 7 16 SWAA991134 4 19990702 A 2565 D31591 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999071600304 19990716 00304 1999 7 16 SWAA991135 4 19990703 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 640SW 27713 FWD ENTRY DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999071600305 19990716 00305 NM 1999 7 16 SWAA991136 1 19990702 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM, BS 312, AFT AND FWD FLANGES. REPAIRED BEAM PER SWA RA NR 1-3 53-2109. 2 L 7 2 4F RT A16WE 1999071600306 19990716 00306 WP 1999 7 16 TWAA9909701 1 19990709 A 3350 4TL1110B SWITCH DOUG DC9 DC982 3022082 WP COCKPIT WORN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 920TW 49369 THE EMERGENCY LIGHTS FLASHED ON AND OFF WHEN ARMED. REPLACED THE EMERGENCY LIGHT SWITCH. CHECK-C 6-13-99 STL. 2 L 7 2 4F A6WE 1999071600307 19990716 00307 WP 1999 7 16 TWAA9909702 1 19990709 A 3350 58222 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 984Z 47412 THE CABIN EGRESS LIGHTS AT THE FORWARD COACH SECTION WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 3-15-99 STL. 2 L 7 2 4F A6WE 1999071600308 19990716 00308 WP 1999 7 16 TWAA9909703 1 19990711 A 3350 6011779LB POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 987Z 47137 THE LEFT ENGINE NACELLE EMERGENCY LIGHT REMAINED ON ALL THE TIME. REPLACED THE POWER SUPPLY 6011779LB, AND THE BATTERY PACK 418030CF00101. CHECK-C 4-26-99 MCI. 2 L 7 2 4F A6WE 1999071600309 19990716 00309 NM 1999 7 16 TWAA9909704 1 19990710 A 3350 58225 POWER SUPPLY BOEING 727 727231 1384079 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64346 21633 THE EXTERIOR EMERGENCY LIGHT AT THE LT AND RT AFT CABIN DOORS, AND THE AFT CABIN EGRESS LIGHTS, WERE INOPERATIVE. REPLA CED THE POWER SUPPLY. CHECK-C 9-11-98 MCI. 2 L 7 3 4F A3WE 1999071600310 19990716 00310 WP 1999 7 16 TWAA9909706 1 19990707 A 5210 GUST LOCK DOUG DC9 DC982 3022082 WP PASSENGER DOOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 DURING CHECK-C MAINT, FOUND THE FWD LEFT CABIN DOOR GUST LOCK DAMAGED. TRIMMED OUT EDGE DAMAGE, CHECKED FASTENERS AND E DGE MARGINS, AND TREATED. REPAIRED PER SRM 53-04, FIG 24. 2 L 7 2 4F A6WE 1999071600311 19990716 00311 WP 1999 7 16 TWAA9909707 1 19990706 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 212-223 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 DURING CHECK-C MAINT, FOUND DEEP GOUGES IN FUSELAGE SKIN AT APPROXIMATELY STA 212 TO 223, BETWEEN LONGERON 3L AND 4L. R EPAIRED PER SRM 53-04, FIG 12B. 2 L 7 2 4F A6WE 1999071600312 19990716 00312 WP 1999 7 16 TWAA9909708 1 19990707 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9625W 53595 THE FWD LOWER EDGE OF THE OUTER SKIN WAS BENT IN FOUR INCHES WIDE BY 1 IN HIGH AND 0.25 IN DEEP. REPAIRED PER SRM 52-03 , PAGE 1, ITEM 1 PARAGRAPH A. 2 L 7 2 4F RT A6WE 1999071600313 19990716 00313 WP 1999 7 16 TWAA9909709 1 19990706 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 83.5 MISDRILLED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND ONE HOLE DRILLED INTO LATERAL RIB, TWO INTO LONGITUDINAL RIB AT STA 83.5 X=-10. HOLES DUE TO REPAIR IN FUSELAGE SKIN. BLENDED HOLE IN LATERAL RIB AT STA 83 AND SMOOTHED. INSTALLED REPAIR DOUBLE PER SRM 53 -03, FIG 34 AND ARA 13511. INSTALLED NEW LONGITUDINAL RIB PER SRM 51-01. 2 L 7 2 4F A6WE 1999071600314 19990716 00314 WP 1999 7 16 TWAA9909710 1 19990706 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND FRAME CRACKED APPROXIMATELY .75 INCH LONG IN I/B RADIUS AT STA 83.5 X=-10, RT STATION. R EF SRM 53-03, PAGE 143. STOP DRILLED CRACK AND ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 61-00-03. INSTALLED REPAIR DOUBLER PER SRM 53-03, FIG 34 AND ARA 13511. 2 L 7 2 4F A6WE 1999071600315 19990716 00315 WP 1999 7 16 CALA9900815 1 19990708 A 2450 S49169538 BUS BAR DOUG DC10 DC1030 3023501 WP COCKPIT FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 35084 46991 THE CREW OBSERVED SMOKE IN THE AREA OF THE FIRE T HANDLES ON OVERHEAD CIRCUIT BREAKER PANEL AND JUST TO LEFT OF T HANDLE S WHILE EN ROUTE FROM MXP TO EWR. THE EMERGENCY CHECKLIST WAS COMPLETED AND THE AIRCRAFT WAS DIVERTED TO CDG WHERE IT L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT EMERGENCY BUS A PHASE B7-48 BUS BAR TERMINAL AND ELECTRICAL FLAG TERMIN AL X274AA8A BURNED. THE RIGHT EMERGENCY BUS BAR EPR NR 3 & NR 2 C/B WAS REPLACED. ADDED ONE MORE C/B TO OVERHEAD C/B P ANEL F21 AND INSTALLED TWO NEW FLAG TERMINALS TO CONNECT BUS BAR. 2 L 7 3 4F A22WE 1999071600316 19990716 00316 EA 1999 7 16 COMA9960356 1 19990709 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT BIRD STRIKE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 SO 01 912CA 7011 BIRD STRIKE DURING TAKEOFF. COMPLIED WITH BIRD STRIKE INSPECTION. 2 L 7 2 4F RT A21EA 1999071600317 19990716 00317 EA 1999 7 16 COMA9960357 1 19990709 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN CONTAMINATED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 988CA 7204 FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERATIVE. REMOVED WATER FROM WIRING CONNECTOR SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1999071600318 19990716 00318 EA 1999 7 16 COMA9960358 1 19990710 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 946CA 7072 FLAPS FAILED. RESET FLAP SYSTEM, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999071600319 19990716 00319 EA 1999 7 16 COMA9960359 1 19990710 A 5210 HANDLE CNDAIR CL600 CL6002B19 EA PASSENGER DOOR NOT LATCHED A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 929CA 7035 DOOR UNLOCKED WARNING AFTER TAKEOFF. FOUND DOOR HANDLE UNLATCHED. INSPECTED LATCH MECHANISM AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 1999071600320 19990716 00320 NE 1999 7 16 COMA9960360 2 19990711 A 7397 WIRE HARNESS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT FUEL CONTROL LOOSE A COMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 01 943CA 7062 AFTER TAKEOFF, RIGHT ENGINE ROLLED BACK AND THEN SURGED 10 PERCENT. SECURED LOOSE WIRING HARNESS AT FUEL CONTROL UNIT. 2 L 7 2 4F 4 F RT A21EA E15NE 1999071600321 19990716 00321 EA 1999 7 16 COMA9960361 1 19990708 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 FLAPS FAIL MESSAGE. REPLACED THE PDU. 2 L 7 2 4F RT A21EA 1999071600322 19990716 00322 SO 1999 7 16 COMA9910107 1 19990708 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 120152 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPAIRED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999071600323 19990716 00323 SO 1999 7 16 COMA9910108 1 19990708 A 3350 1317 BULB EMB 120 EMB120RT SO ROW 8 FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 248CA 120228 OVERHEAD EMERGENCY LIGHT AT ROW 8 IS INOPERATIVE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 1999071600324 19990716 00324 SO 1999 7 16 COMA9910109 1 19990708 A 3350 CONNECTOR EMB 120 EMB120RT SO ROW 5 LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 256CA 120245 EMERGENCY FLOOR LIGHTS AFT OF ROW 5 ARE INOPERATIVE. SECURED LOOSE WIRING CONNECTOR. 2 L 7 2 4T RT A31SO 1999071600325 19990716 00325 WP 1999 7 16 UPS99830065 1 19990704 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, AFT CARGO PIT CORROSION EMINATING FROM JOINT AT INTERCOSTAL ATTACH CLIP AND FRAME, STA 1260 LONG 35R . REMOVED LITE CORROSION, ALODINED AND PRIMED IAW DC8-SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999071600326 19990716 00326 WP 1999 7 16 UPS99830066 1 19990704 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, FS 857 LOWER WEB HAS CRACK AT NUT PLATE ON LOWER LEFT ACCESS PANEL. FABBED REPAIR IAW DC8 SRM 53-2- 0. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-8. 2 L 7 4 4F RT 4A25 1999071600327 19990716 00327 WP 1999 7 16 UPS99830067 1 19990704 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, FS 857 LOWER WEB HAS CRACK AT NUT PLATE ON LOWER RIGHT ACCESS PANEL. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND FILLER ALODINED AND PRIMED AREA. 2 L 7 4 4F RT 4A25 1999071600328 19990716 00328 WP 1999 7 16 UPS99830068 1 19990705 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, MAIN CABIN SEAT TRACK WAS GOUGED AND CORRODED AT STA 270. REMOVED AND INSTALLED NEW PLUG (P/N DC8 5 3B-007-004) IAW DC8 SRM 53-2- 3, UPS PARTS TAG NR 942460 (S/N 00290311). 2 L 7 4 4F RT 4A25 1999071600329 19990716 00329 WP 1999 7 16 ABXA9900567 1 19990708 A 5250 AR25291GR41 LOCK DOUG DC8 DC861 3021952 WP COCKPIT DOOR DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 DURING PREFLIGHT INSPECTION, THE COCKPIT DOOR LOCK WAS INOPERATIVE. THE DOOR WOULD NOT UNLOCK WHEN CLOSED. INSTALLED N EW LATCH HANDLE AS REQUIRED, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999071600330 19990716 00330 NM 1999 7 16 SCNA99089 1 19990708 A 2612 893851 FIRE LOOP BOEING 727 7272J4 1384006 NM NR 3 ENGINE FAILED A SCNA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 288SC 20765 DURING FLIGHT, THE NUMBER THREE ENGINE FIRE WARNING LIGHT ILLUMINATED. DISCHARGED BOTH ENGINE FIRE BOTTLES AND FIRE LIG HT REMAINED ON. RETURNED AIRCRAFT TO AIRPORT. FOUND FIREWALL LOOP TO BE AT FAULT. REMOVED AND REPLACED FIRE LOOP SYST EM, OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1999071600331 19990716 00331 NE 1999 7 16 SCNA99090 2 19990709 A 7230 COMPRESSOR BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE STALLED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 15 275AF 22092 DURING TAKEOFF ROLL AT ABOUT 40 KNOTS, NUMBER TWO ENGINE COMPRESSOR STALLED THREE TIMES. ABORTED TAKEOFF AND TAXIED BAC K TO RAMP. INSPECTED NUMBER TWO ENGINE INLET AND EXHAUST WITH NO DAMAGE FOUND. RAN ENGINE PER MAINTENANCE MANUAL WITH ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999071600351 19990716 00351 EU 1999 7 16 99ZZZX2608 1 19990615 A 6410 355A12003108 BLADE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR LOOSE A EHAA K NONE O OTHER IN INSP/MAINT 1 AL 03 917JT 1415 86 2759 DELAMINATION OF SS LEADING EDGE BOTH SIDES OF ONE BLADE. SUBMITTER STATED THIS BLADE HAD JUST HAD THE SAME PROBLEM 86.1 HOURS AGO. INSPECTION OF RECORDS REVEALED THIS PARTICULAR SIDE WAS FACTORY ORIGINAL. 1 G 7 1 3U H9EU 1999071600352 19990716 00352 EU 1999 7 16 99ZZZX2609 1 19990519 A 2422 SPC10 INVERTER UROCOP EC135 EC135P1 8680990 EU E/E BAY INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 409 191 EC1350054 INVERTER UNIT INOPERATIVE. REPLACED WITH NEW, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999071600353 19990716 00353 1999 7 16 99ZZZX2610 4 19990518 A 3422 INDICATOR BENDIX UROCOP EC135 EC135P1 8680990 EU COCKPIT INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 408 3376 EC1350054 VERTICAL GYRO OPERATES INTERMITTENTLY. DROPS OFF-LINE DURING FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999071600354 19990716 00354 NM 1999 7 16 99ZZZX2611 1 19990412 A 6720 16549011 ACTUATOR DOUG MD900 MD900 3027375 NM MAIN ROTOR MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1648 0089831016 90000012 ACTUATOR BACK-DRIVES WHEN POWER IS APPLIED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999071600355 19990716 00355 NM 1999 7 16 99ZZZX2612 1 19990412 A 6720 16549011 ACTUATOR DOUG MD900 MD900 3027375 NM MAIN ROTOR MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1746 0089831099 90000012 ACTUATOR BACK-DRIVES WHEN POWER IS APPLIED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999071600364 19990716 00364 WP 1999 7 16 VTZA990147 2 19990609 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT MALFUNCTIONED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 489UE 908 IAD/CLE - FLT 7451 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LT ENGINE NOT MAKING TORQUE. MAINTENANCE PERFORMED MAINTENANCE RUNS WITH NO DEFECTS NOTED. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1999071600365 19990716 00365 WP 1999 7 16 99ZZZX2621 2 19990607 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RIGHT MALFUNCTIONED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 471UE 821 ABE/IAD - FLT 7155 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING REQUIRED TORQUE. AIRCRAFT FER RIED TO IAD. MAINTENANCE REPLACED RT DELTA POWER BOX, ADJUSTED PROP GOVERNOR III, MAX POWER, AND EGT COMP, OPS CHECK AN D MAINTENANCE, RUNS GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1999071600366 19990716 00366 WP 1999 7 16 VTZA990146 2 19990609 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT MALFUNCTIONED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 482UE 897 IAD/ROC - FLT 7292 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LT ENGINE NOT MAKING TORQUE. MAINTENANCE ADJUSTED LT ENGINE MAX FUEL FLOW, GROUND RUN GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1999071600367 19990716 00367 SO 1999 7 16 SIMA991614 1 19990610 A 3350 RPSI13 BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 610AE 1366912342 145073 ORD - FLT 4265 - LEFT WING EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT T00011AT 1999071600368 19990716 00368 EU 1999 7 16 SIMA991701 1 19990619 A 3234 96GA0102 HANDLE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 368PX 429 340B274 DFW - FLT 3649 - AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RETURNED TO FIELD. REMOVED AND REPLACED THE LANDING GEAR HANDLE. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999071600369 19990716 00369 EA 1999 7 16 COMA9960207 1 19990514 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA LT EMERG EXIT LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 941CA 7050 YUL - FLT 5654 - LEFT OVERWING EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. SECURED LOOSE WIRING CONNECTOR. (X) 2 L 7 2 4F RT A21EA 1999071600370 19990716 00370 EA 1999 7 16 COMA9960215 1 19990514 A 5315 601R3111367 FLOOR BEAM CNDAIR CL600 CL6002B19 EA BS 280-409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 14573 7050 FLOOR BEAMS LBL 27, LBL 9, RBL 9, AND RBL 27 FROM BS 280 TO BS 409 HAVE CORROSION DAMAGE. REPLACED DAMAGED SECTIONS OF FLOOR BEAMS. PART TC: 13,942. (X) 2 L 7 2 4F RT A21EA 1999071600371 19990716 00371 EA 1999 7 16 COMA9960210 1 19990415 A 5315 601R3867317 FLOOR BEAM CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 FLOOR BEAM PLATES AT BS 349.0 ARE CORRODED. REPLACED PLATES. PART TC: 13,637. REF: OPERATOR CONTROL NR 99ZZZX2622 T HROUGH 99ZZZX2624. (X) 2 L 7 2 4F RT A21EA 1999071600372 19990716 00372 EA 1999 7 16 99ZZZX2622 1 19990415 A 5315 601R3867319 FLOOR BEAM CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 FLOOR BEAM PLATES AT BS 349.0 ARE CORRODED. REPLACED PLATES. PART TC: 13,637. REF: OPERATOR CONTROL NR COMA9960210, AND 99ZZZX2623 THROUGH 99ZZZX2624. 2 L 7 2 4F RT A21EA 1999071600373 19990716 00373 EA 1999 7 16 99ZZZX2623 1 19990415 A 5315 601R3867321 FLOOR BEAM CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 FLOOR BEAM PLATES AT BS 349.0 ARE CORRODED. REPLACED PLATES. PART TC: 13,637. REF: OPERATOR CONTROL NR COMA9960210, AND 99ZZZX2622 THROUGH 99ZZZX2624. 2 L 7 2 4F RT A21EA 1999071600374 19990716 00374 EA 1999 7 16 99ZZZX2624 1 19990415 A 5315 601R3867325 FLOOR BEAM CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 FLOOR BEAM PLATES AT BS 349.0 ARE CORRODED. REPLACED PLATES. PART TC: 13,637. REF: OPERATOR CONTROL NR COMA9960210, AND 99ZZZX2622 THROUGH 99ZZZX2623. 2 L 7 2 4F RT A21EA 1999071600375 19990716 00375 EA 1999 7 16 COMA9960211 1 19990415 A 5315 601R3111367 FLOOR BEAM CNDAIR CL600 CL6002B19 EA BS 280-409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 CORROSION DAMAGE FOUND ON FLOOR BEAMS LBL 27, LBL 9, RBL 9, AND RBL 27 FROM BS 280.0 TO BS 409.0. REPLACED CORRODED SEC TIONS OF FLOOR BEAM IAW REO 601R-53-00-027. PART TC: 13,637. (X) 2 L 7 2 4F RT A21EA 1999071600376 19990716 00376 EA 1999 7 16 COMA9960212 1 19990415 A 5347 601R3103215 SEAT RAILS CNDAIR CL600 CL6002B19 EA BS 364 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 SEAT RAILS AT RBL 9 AND LBL 9 AT BS 364 HAVE CORROSION DAMAGE. REPLACED SEAT RAILS. PART TC: 13,637. (X) 2 L 7 2 4F RT A21EA 1999071600377 19990716 00377 EA 1999 7 16 COMA9960213 1 19990415 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA BS 317-342 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 FLOOR ANGLE RBL 42 AT BS 317 TO BS 342 HAS CORROSION DAMAGE. REPLACED ANGLE. PART TC: 13,637. (X) 2 L 7 2 4F RT A21EA 1999071600378 19990716 00378 EA 1999 7 16 COMA9960214 1 19990415 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA BS 317-342 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 14567 7011 FLOOR ANGLE LBL 42 TO BS 317 TO BS 342 HAS CORROSION DAMAGE. REPLACED ANGLE. PART TC: 13,637. (X) 2 L 7 2 4F RT A21EA 1999071600379 19990716 00379 NE 1999 7 16 COMA9960209 2 19990517 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE REQ'D SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 965CA 7131 CVG - FLT 9600 - RIGHT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 35 PSI AND 55 PSI. SERVICED OIL TANK TO PROPER LEVEL. ( X) 2 L 7 2 4F 4 F RT A21EA E15NE 1999071600380 19990716 00380 EA 1999 7 16 COMA9960208 1 19990519 A 2611 475052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 01 988CA 922 1079 7204 CVL - FLT 5722 - CARGO SMOKE WARNING ON APPROACH, DISCHARGED CARGO FIRE EXTINGUISHER. REPLACED SMOKE DETECTOR AND BOTTL ES. NO EVIDENCE OF FIRE. PART TC: 954. (X) 2 L 7 2 4F RT A21EA 1999071600381 19990716 00381 EU 1999 7 16 99ZZZX2625 1 19990604 A 2913 65WE10305 HYDRAULIC PUMP BRAERO DH125 HS125700A 4230170 EU LT ENGINE FAILED A N9WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 11 225BJ 1045 NA0231 ON MAINTENANCE FLIGHT CLIMBING OUT OF FL 340 FROM MDW, THE LEFT HYDRAULIC LOW PRESSURE LIGHT CAME ON. CREW WATCHED PRES SURE GAUGE AND IN ABOUT 2-3 MINUTES, THE RIGHT SIDE LOW PRESSURE LIGHT CAME ON. SYSTEM PRESSURE REDUCED TO 2,300 PSI. P ILOTS USED THE EMERG CHECK LIST, AND REQUESTED OF ATC TO RETURN TO MDW. USING THE CHECK LIST, THE FLAPS AND GEAR WERE P UMPED DOWN FOR A NORMAL LANDING. TOWER WAS NOTIFIED AND A TOW WAS READY TO MOVE THE AIRCRAFT AFTER NORMAL STOP AND SHUT DOWN. PART 91 TRIP WITH ONE PASSENGER ONBOARD. FOUND LEFT ENG HYD PUMP FAILED INTERNALLY CAUSING CASE TO SEPARATE AND LEAK HYDRAULIC FLUID UNTIL SYSTEM WAS DEPLETED. LEFT ENG HYD PUMP REPLACED PER MANUFACTURER'S MM. CYCLES: 627. (X) 2 L 7 2 4F A3EU 1999071600382 19990716 00382 NM 1999 7 16 99ZZZX2626 1 19990507 A 3230 65178194 ACTUATOR BOEING 727 727227 1384078 NM RT MLG CRACKED A P4GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 CGKKF DA714 21043 BQN/SJU - FLT PGI NR 1864/27 - UPON GEAR RETRACTION AFTER TAKEOFF BQN, RT MAIN LANDING GEAR RED LIGHT ILLUMINATED AND RE MAINED ILLUMINATED. MANUAL GEAR EXTENSION ACCOMPLISHED, AIRCRAFT LANDED SJU. FOUND RT MLG UPLOCK ACTUATOR ATTACH CRACK ED OFF. REPLACED SAME PER MM. JACKED AIRCRAFT RETRACTION/EXTENSION CHECK ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1999071600383 19990716 00383 SO 1999 7 16 SIMA991235 1 19990503 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 623AE 05551 145109 ISP - FLT 4245 - BAGGAGE SMOKE INDICATION CAME ON IN-FLIGHT. CREW DISCHARGED FIRE EXTINGUISHERS. INSPECTED BAGGAGE COM PARTMENT AND VERIFIED EVENT AS A FALSE WARNING. ISSUED MEL AGAINST THE BAGGAGE SMOKE DETECTION SYSTEM PER MEL 26-15. R EMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. MEL ITEM RESTORED ON 5-13-99. AI RCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR 99ZZZX2627. (X) 2 L 7 2 4T RT T00011AT 1999071600384 19990716 00384 SO 1999 7 16 99ZZZX2627 1 19990503 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 623AE 05561 145109 ISP - FLT 4245 - BAGGAGE SMOKE INDICATION CAME ON IN-FLIGHT. CREW DISCHARGED FIRE EXTINGUISHERS. INSPECTED BAGGAGE COM PARTMENT AND VERIFIED EVENT AS A FALSE WARNING. ISSUED MEL AGAINST THE BAGGAGE SMOKE DETECTION SYSTEM PER MEL 26-15. R EMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. MEL ITEM RESTORED ON 5-13-99. AI RCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SIMA991235. 2 L 7 2 4T RT T00011AT 1999071600385 19990716 00385 EU 1999 7 16 SIMA991531 1 19990602 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 902AE 340B269 ABI - DENT ON LT REAR FUSELAGE ABOVE ELEVATOR (TDMI NR 9025300B8). CUT OUT DAMAGED AREA AND PERFORMED AN EDDY CURRENT I NSPECTION WITH NO CRACK INDICATIONS. FABRICATED A SPACER .025 INCH THICK AND A REPAIR PLATE .025 INCH THICK. APPLIED C HROMATING TO THE BARE METAL SURFACE AND APPLIED FR PRIMER TO THE TREATED SURFACE. APPLIED FAY SELANT TO THE PLATE AND R EPOSITIONED THE REPAIR PLATE AND SPACER AND INSTALLED. APPLIED FILLET SEALANT IN THE GAP BETWEEN THE SPACER AND SKIN. A PPLIED TOP COAT TO THE OUTER SURFACE AND APPLIED DINITROL AV 25. RESTORED TOP COAT TO THE OUTER SURFACE WORK DONE IAW S AAB SRM 53-90-10, PG 204. CLEARED TDMI. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999071600386 19990716 00386 EA 1999 7 16 VTZA990142 1 19990605 A 3610 14459101 DUCT CNDAIR CL600 CL6002B19 EA LT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 637BR 7308 IAD/BNA - FLT 7705 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEUDLED LANDING DUE TO 14TH STAGE DUCT FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LT ENGINE 14TH STAG E PYLON DUCT ASSY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999071600387 19990716 00387 EA 1999 7 16 VTZA990071 1 19990508 A 2910 AE7090412 HOSE CNDAIR CL600 CL6002B19 EA LT PYLON LEAKING A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 638BR 7311 ORD/SGE - FLT 7621 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 HYDRAULIC SYSTEM FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED FLEXIBLE PRESSURE LINE, OPS CHECK OK. AIR CRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999071600388 19990716 00388 EU 1999 7 16 99ZZZX2628 1 19990705 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SW 09 447TM 13055 447 MIA - FLT 522A - L-1 AND L-2 DOOR EMERGENCY LIGHT BATTERIES WEAK. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PACK P ER AMM 33-51-00. 2 L 7 2 4F RT A28NM 1999071600390 19990716 00390 NM 1999 7 16 HNAA9900095 1 19990709 A 5720 COVER DHAV DHC8 DHC8102 2809003 NM BOOST PUMP LEAKING A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 FUEL BOOST PUMP COVER HAS RUNNING LEAK. REPAIRED IAW EO8-57-99-730 & EO8-57-99-732. THIS HA-300 COVERS LEAK CHECK ONLY . 2 H 7 2 4T RT A13NM 1999071600391 19990716 00391 NM 1999 7 16 HNAA9900096 1 19990701 A 5720 RING DHAV DHC8 DHC8102 2809003 NM WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 AREA WHERE ANTI-FRET RING RESTS AGAINST WITH CLAMP RING HAS SIGNS OF CORROSION APPROX DEPTH .005 - .008. REPAIRED IAW E O8-57-99-732. 2 H 7 2 4T RT A13NM 1999071600392 19990716 00392 NM 1999 7 16 HNAA9900097 1 19990711 A 3350 6013211X BATTERY DHAV DHC8 DHC8102 2809003 NM ROW 1DF DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 937HA 15225 33624 148 FIVE EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED EMERGENCY PACK. 2 H 7 2 4T RT A13NM 1999071600393 19990716 00393 NM 1999 7 16 AT9900492 1 19990709 A 3350 110049 BATTERY CHARGER BOEING 737 737297 1384480 NM CABIN DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 462AT 22631 EMERGENCY EVACUATION LIGHTS INOPERATIVE IN FORWARD SECTION OF AIRCRAFT. REMOVED AND REPLACED FORWARD BATTERY PACK CHARG ER IAW MM 33-51-51. 2 L 7 2 4F A16WE 1999071600394 19990716 00394 NM 1999 7 16 AT9900493 1 19990713 A 3350 110049 FUSE BOEING 737 737297 1384480 NM CABIN FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 462AT 22631 DURING LAYOVER, FOUND AN EMERGENCY PATH LIGHTING SEGMENT OUT. REPLACED BATTERY CHARGER FOR BLOWN FUSE (F2), OPS CHECK N ORMAL IAW MM 33-51-00. 2 L 7 2 4F A16WE 1999071600395 19990716 00395 NE 1999 7 16 MALA976512 2 19990706 A 7320 1103P0631 P3 SWITCH SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT NACELLE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 76XJ 076 ON TAKEOFF DURING ROTATION, THE LEFT IGNITION LIGHT ILLUMINATED AND STAYED ON UNTIL ABOUT 5,500 FEET. ALL ENGINE INSTRU MENTS APPEARED NORMAL. CREW RETURNED TO DTW. MAINTENANCE RAN AIRCRAFT FOR 30 MINUTES AND COULD NOT DUPLICATE ON GROUND . MAINTENANCE REPLACED P3 SWITCH IAW SF340 AMM 74-30-20. PERFORMED OPS CHECK, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999071600396 19990716 00396 EU 1999 7 16 MALA976513 1 19990704 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU AVIONICS BAY FAILED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 142XJ 142 AVIONICS SMOKE WARNING ILLUMINATED IN FLIGHT. DIVERTED TO ATW. MAINTENANCE DEFERRED PER MEL 26-13-3B. ON 7/7 MAINTENA NCE REPLACED SMOKE DETECTOR, ALL CHECKS GOOD IAW SF340 AMM. 2 L 7 2 4T RT A52EU 1999071600397 19990716 00397 EU 1999 7 16 MALA976514 1 19990630 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 433 DURING 4K INSPECTION, FOUND SEAT TRACK CORROSION. MAINTENANCE COMPLETED SAAB STATEMENT 72SDS1629 FOR REPAIR OF SEAT TRA CK. 2 L 7 2 4T RT A52EU 1999071600398 19990716 00398 EU 1999 7 16 MALA976515 1 19990628 A 2760 HC921H0478000 CIRCUIT CARD BAC 146 AVRO146RJ85A 1500097 EU E & E COMPT INTERMITTENT A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 527XJ E2352 AFTER TAKEOFF MANUAL SPOILER FAULT ILLUMINATED. QRH PROCEDURES COMPLIED. MAINTENANCE CONTROLS REQUEST RETURNED TO DTW. MANUAL SPOILER FAULT LIGHT EXTINGUISHED AFTER LANDING AND AIRBRAKE/LIFT SPOILER LEVER WAS RETURNED TO POSITION. MAINT ENANCE REPLACED CIRCUIT CARD CH65. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999071600399 19990716 00399 EU 1999 7 16 MALA976516 1 19990711 A 5210 HANDLE BAC 146 AVRO146RJ85A 1500097 EU PASSENGER DOOR NOT LATCHED A MALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 GL 15 527XJ E2352 LEFT FORWARD CABIN DOOR KEPT DISARMING IN FLIGHT. AIRCRAFT RETURNED TO MSP. MAINTENANCE UPON ARRIVING TO AIRCRAFT FOUN D OUTSIDE DOOR HANDLE NOT RECESSED COMPLETELY OUT OF AIRSTREAM. PUSHED HANDLE BACK INTO DOOR RECESS, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1999071600400 19990716 00400 EU 1999 7 16 MALA976518 1 19990709 A 5280 PANEL BAC 146 AVRO146RJ85A 1500097 EU NLG DOOR CRACKED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 506XJ E2314 DURING CLIMBOUT, WHEN ACCELERATING THRU 210 KTS LOUD NOISE AND VIBRATION SEEMED TO ORIGINATE FROM NOSE GEAR DOORS. CYCL ED GEAR, ALL INDICATIONS NORMAL. NOISE CONTINUED, RETURNED TO MSP FOR MAINTENANCE CONSULT. MAINTENANCE REPAIRED CRACK IN LT NOSE GEAR DOOR SIDE PANEL, BY FABRICATED PATCH FOR NOSE GEAR PANEL, IAW STRUCTURAL REPAIR MANUAL 51-71-11-1. 2 H 7 4 4F RT A49EU 1999071600401 19990716 00401 WP 1999 7 16 IXXA9900015 1 19990710 A 2150 PACK DOUG DC8 DC871F 302199D WP RIGHT MALFUNCTIONED A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 822BX 45813 EN ROUTE FROM TOL TO DFW, THE RIGHT AIR CONDITIONING PACK HAD ZERO FLOW, RUNS HOT AND EMITTED A BURNING ODOR WHEN FULL C OLD SELECTED. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE RIGHT PACK SYSTEM IN AC CORDANCE WITH THE MAINTENANCE MANUAL WITH NO DISCREPANCIES NOTED. MAINTENANCE PERFORMED A SYSTEM OPERATIONAL TEST IN AC CORDANCE WITH THE MAINTENANCE MANUAL WITH NO DISCREPANCIES NOTED. 2 L 7 4 4F RT 4A25 1999071600402 19990716 00402 SO 1999 7 16 COMA9910110 1 19990711 A 5320 12034416002 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 249CA 120230 ON PREFLIGHT WALK AROUND, CREW NOTICED ONE RIVET HEAD BROKEN OFF ON THE RIGHT SIDE OF THE FUSELAGE, JUST BELOW THE F/O'S DV WINDOW, AT FRAME 9. INTERNAL INVESTIGATION REVEALED THE SKIN SUPPORT BRACKET AT THAT LOCATION TO BE CRACKED. THE B RACKET WAS REPLACED PER AERODESIGN REPORT NR 660-1, IR DATED 2-16-93. 2 L 7 2 4T RT A31SO 1999071600403 19990716 00403 EA 1999 7 16 COMA9960362 1 19990712 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 948CA 1296 7079 CARGO SMOKE WARNING. REPLACED THE CARGO SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 1999071600404 19990716 00404 EA 1999 7 16 COMA9960363 1 19990706 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA BS 310-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 PAX DOOR THRESHOLD ANGLE (P/N 601R31527-181), PAX DOOR FLOOR SUPPORT ANGLE (P/N 601R315-207) AND SERVICE DOOR THRESHOLD ANGLE (P/N 601R38303-105) ALL DISCOVERED WITH CORROSION BEYOND REPAIRABLE LIMITS. REPLACED PAX DOOR THRESHOLD ANGLE (P/ N 601R31527-181) IAW WVAC EO 601R-53-0085. REPLACED PAX DOOR FLOOR SUPPORT ANGLE (P/N 601R31527-207), IAW WVAC EO 601R- 53-0087. REPLACED SERVICE DOOR THRESHOLD ANGLE (P/N 601R38303-105), IAW WVAC EO 601R-53-0084. 2 L 7 2 4F RT A21EA 1999071600405 19990716 00405 EA 1999 7 16 COMA9960364 1 19990706 A 5320 SUPPORT CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 FLOOR SUPPORT PLATES (P/N 601R38673-17-19,-21 AND -25) AT FS 249 BETWEEN LT FUSELAGE SKIN AND LBL 27, LBL 9, RBL 9, RBL 27 AND RT FUSELAGE SKIN DISCOVERED CORRODED BEYOND SERVICEABLE/REPAIRABLE LIMITS. REPLACED FLOOR SUPPORT PLATES WITH NE W FLOOR SUPPORT PLATES IAW WVAC EO 601R-53-0086. 2 L 7 2 4F RT A21EA 1999071600406 19990716 00406 EA 1999 7 16 COMA9960365 1 19990706 A 5320 6003401717 SUPPORT CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 FLOOR SUPPORT MEMBER (P/N 60034017-17) AT FS 280.00 APPROXIMATELY 1 OUTBOARD OF RBL 9 DISCOVERED WITH 2 INCH CRACK. REP AIRED FLOOR SUPPORT MEMBER AT FS 280 IAW WVAC EO 601R-53-0088. 2 L 7 2 4F RT A21EA 1999071600407 19990716 00407 EA 1999 7 16 COMA9960366 1 19990710 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7131 FS 718 STR 11 RIGHT AND LEFT SIDE DOUBLERS CRACKED. ALSO, FRAME AT FS 718 LT SIDE HAS 2 INCH CRACK. REPAIRED FRAME AT FS 718 LT SIDE AND DOUBLERS ON RT AND LT SIDE IAW WVAC EO 601R-53-0098, 601R-53-0099 AND 601R-53-0100A. 2 L 7 2 4F RT A21EA 1999071600408 19990716 00408 EU 1999 7 16 QXEA9901464 1 19990710 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 491US 11156 SEA- EXIT SIGN OVER COCKPIT DOOR ENTRANCE INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY. ALL EXIT LIGHTS CHECK NORMAL. 2 L 7 2 4F RT A20EU 1999071600409 19990716 00409 EU 1999 7 16 QXEA9901465 1 19990708 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 499US 11182 GEG- EXIT SIGN AT CABIN ENTRANCE INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECK OF EMERGENCY LIGHTS ARE N ORMAL. 2 L 7 2 4F RT A20EU 1999071600410 19990716 00410 NM 1999 7 16 99FDEA00257 1 19990712 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 SNRM 431, 430, 355, 354 CRACK ON SEAT TRACK BS 635, X=8.5 RT, X=47.5 RT, X=27.5 LT, X=47.5 LT. REPAIRED SEAT TRACK IN A CCORD WITH SRM 53-70-00. 2 L 7 3 4F RT A22WE 1999071600411 19990716 00411 NM 1999 7 16 99FDEA00258 1 19990712 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM CARGO COMPT WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 148FE 19086 FWD CARGO CTR CEILING PANEL FASTENERS WEARING INTO BOTTOM FLOORBEAM. BLENDED WORN AREA, INSTALLED FLOORBEAM LOWER CHORD REPAIR PER SRM 53-10-8 FIG 2. 2 L 7 3 4F A3WE 1999071600412 19990716 00412 EU 1999 7 16 99UAL900352 1 19990702 A 2910 NAS161212 O RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE YELLOW HYD SYS FAILED A UALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 437UA 655 AT APPROX 1 HOUR OUT OF LAX, CREW REPORTED LOSING ALL HYDRAULIC FLUID ON YELLOW SYSTEM. SAMC WAS CONTACTED AND SYSTEM W AS SHUT DOWN PER ECAM MESSAGE. CAPTAIN ELECTED TO CONTINUE TO DESTINATION. *S/D* O-RING BETWEEN YELLLOW ACCUM & PRESS . LINE REPLACED - REF IPC 29-13-03-06A. ALSO SERVICED RESERVOIR TO FULL & CLEANED BOTTOM OF AIRCRAFT OF HYD FLUID. 2 L 7 2 4F 4 F RT A28NM E40NE 1999071600413 19990716 00413 NM 1999 7 16 99UAL900354 1 19990704 A 2120 AIR DIST BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 572UA 26682 CREW REPORTS, ELECTRICAL SMELL FROM FORWARD INSTRUMENT PANEL AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 1999071600414 19990716 00414 NM 1999 7 16 99UAL900355 1 19990703 A 2121 S210N70110 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 549UA 25397 CREW NOTICED ODOR IN THE COCKPIT WITH NUMBER 2 AFT EXHAUST COOLING FAN EICAS MESSAGE. *S/D* CAUSE OF THE SMELL WAS FA ILURE OF THE AFT EXHAUST COOLING FAN. THE FAN WAS REPLACED. NO FURTHER REPORTS OF SMELL WERE NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999071600415 19990716 00415 NM 1999 7 16 99UAL900356 1 19990702 A 2560 7002401 PANEL GABLES ENGIN 1002401 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1 L DEFECTIVE A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 551UA 25399 EMERGENCY EVACUATION GOING OFF WITHOUT BEING SELECTED. *S/D* REPLACED PASSENGER COMPARTMENT EMERGENCY EVACUATION SIGNA L PANEL AT DOOR 1L, CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1999071600416 19990716 00416 NM 1999 7 16 99UAL900357 1 19990628 A 5310 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 480-520 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 THE FUSELAGE SKIN, BETWEEN BS 480 AND 520, STR 37R TO 40R WAS DAMAGED DUE TO CONTACT WITH GROUND EQUIPMENT. THE FRAME A T STA 500 ALSO WAS DAMAGED BETWEEN STR 37 AND 39 AT THE SKIN ATTACHMENT AND STRINGERS 38, 39 AND 40 WERE DAMAGED. THE 3 STRINGERS WERE REPLACED FROM PRODUCTION SPLICE TO PRODUCTION SPLICE. THE FRAME WAS REPAIRED PER SRM 51-70-11 AND THE S KIN WAS REPAIRED PER SRM 53-00-01 FIGURE 216. 2 L 7 4 4F 4 F RT A20WE E24NE 1999071600417 19990716 00417 NM 1999 7 16 99UAL900358 1 19990704 A 7722 EIS DISPLAY SMITH INDUST 312EDP11 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE EGT FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 946UA 561 26687 857415 ABORTED TAKEOFF AT 95 KNOTS DUE TO A HIGH EGT INDICATION ON THE NR 1 ENGINE. TROUBLESHOOTING CONFIRMED EGT INDICATION W AS FLUCTUATING BETWEEN 850-970 DEGS. THE PRIMARY EIS DISPLAY UNIT WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER ANOMALIES. DURING EIS COMPONENT OVERHAUL THE EGT BOARD WAS FOUND TO BE OUT OF LIMITS. 2 L 7 2 4F 4 F RT A16WE E2GL 1999071600418 19990716 00418 NM 1999 7 16 99UAL900359 1 19990706 A 7931 GEARBOX ELBOW BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 GEAR BOX BROKEN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 386UA 24661 722285 LANDED SFO UNDER AMBER ALERT DUE TO AN OIL LOSS INDICATION FOR THE NR 2 ENGINE. AFTER INSPECTION, FOUND THE OIL PRESSUR E ELBOW FITTING CRACKED TO THE TRANSFER GEARBOX PRESSURE TRANSMITTER. AFTER REPLACING THE GEARBOX ELBOW, ACCOMPLISHED L EAK CHECK RUN AND RETURNED AIRCRAFT TO SERVICE. NO FURTHER DISCREPANCIES REPORTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999071600419 19990716 00419 NM 1999 7 16 99UAL900360 1 19990707 A 3020 10327423 SEAL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ANTI ICE VALVE WORN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7251U 21398 RETURNED TO SFO DUE TO STRUT OVERHEAT LIGHT CAME ON AFTER TAKEOFF. *S/D* LEAKING SEAL ON UPPER SIDE OF ANTI-ICE VALVE. REPLACED SEAL. 2 L 7 3 4F 4 F A3WE E2EA 1999071600420 19990716 00420 1999 7 16 99UAL900361 4 19990706 A 3414 B070710007 SWITCH LEAR SEIGLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E&E BAY FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7441U 21895 ABORTED TAKEOFF AT 90 KNOTS DUE TO MACH AIRSPEED WARNING. *S/D* MAINTENANCE REPLACED THE NR 1 MACH AIR SPEED WARNING S WITCH. NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1999071600421 19990716 00421 NM 1999 7 16 99UAL900362 1 19990709 A 3240 277371 FUSE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT BRAKE SYS FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 928UA 26651 CREW REPORTS RIGHT BRAKE INEFFECTIVE, IF BOTH BRAKES USED AIRCRAFT PULLS TO THE LEFT. *SD* REPLACED BRAKE FUSE PER APP PLICABLE AIRCRAFT MAINTENANCE MANUAL 32-41-72. BLED BRAKE SYSTEM AFTER FUSE REPLACEMENT. OPERATIONAL CHECK OF SYSTEM O K. 2 L 7 2 4F 4 F RT A16WE E2GL 1999071600422 19990716 00422 WP 1999 7 16 MWEA99383 1 19990709 A 5210 59100817 SKIN DOUG DC9 DC981 3022081 WP CABIN DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 804ME 48030 FORWARD ENTRANCE DOOR SKIN AROUND HOLD OPEN HOOK IS CRACKED AND HAS SCRATCHED SKIN WHERE HOOK ENGAGES. MTC FABRICATED A ND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999071600423 19990716 00423 WP 1999 7 16 MWEA99384 1 19990705 A 5414 9958191 SKIN DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LEFT PYLON UPPER SKIN STIFFENER IS CRACKED ABOVE 13TH STAGE BLEED DUCT INSIDE PANEL 8103A. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999071600424 19990716 00424 WP 1999 7 16 MWEA99385 1 19990708 A 2560 11331 STRAP DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE BROKEN A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 212ME 47701 THE FORWARD EXIT DOOR SLIDE COVER STRAP WAS BROKEN. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999071600425 19990716 00425 WP 1999 7 16 MWEA99386 1 19990708 A 5330 591142379 SKIN DOUG DC9 DC932 3022066 WP BS 935 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FUSELAGE SKIN DAMAGED FROM STATION 935 TO 970 AND BETWEEN L22L TO L24L. MTC FABRICATED AND INSTALLED TEMPORARY EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999071600426 19990716 00426 WP 1999 7 16 MWEA99387 1 19990708 A 5320 995773937 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 945 & 965 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 SHEAR TIES AT STATION 945 AND 965 ARE DAMAGED FROM LONGERON 22L TO 24L. MTC FABRICATED AND INSTALLED SHEAR TIES. 2 L 7 2 4F A6WE 1999071600427 19990716 00427 WP 1999 7 16 MWEA99388 1 19990708 A 5313 591142397 LONGERON DOUG DC9 DC932 3022066 WP BS 955-970 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LONGERON 23L IS BENT FROM STATION 955 TO STATION 970. MTC FABRICATED AND INSTALLED NEW LONGERON SECTION AND SPLICE. 2 L 7 2 4F A6WE 1999071600428 19990716 00428 WP 1999 7 16 MWEA99389 1 19990708 A 5330 591142959 SKIN DOUG DC9 DC932 3022066 WP BS 997 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 THE EXTERIOR SKIN IS GOUGED AT STATION 997JUST BELOW LONGERON 23L. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999071600429 19990716 00429 WP 1999 7 16 MWEA99390 1 19990708 A 5313 27779225 LONGERON DOUG DC9 DC932 3022066 WP BS 945-965 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LONGERON 24L IS DENTED AT STATION 945-965. MTC FABRICATED AND INSTALLED NEW LONGERON SECTION. 2 L 7 2 4F A6WE 1999071600430 19990716 00430 WP 1999 7 16 MWEA99391 1 19990708 A 5311 995773933 FRAME DOUG DC9 DC932 3022066 WP BS 945-965 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 502ME FRAME AT STATION 945 AND 965 IS DENTED AT LONGERON 23L. MTC FABRICATED AND INSTALLED NEW FRAME SECTION. 2 L 7 2 4F A6WE 1999071600431 19990716 00431 WP 1999 7 16 MWEA99392 1 19990708 A 2913 AS66411LS666 PUMP DOUG DC9 DC914 3022034 WP RT ENGINE FAILED A MWEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 80ME 45795 LOST HYDRAULIC PRESSURE FLUID AND RAN QRH HYDRAULIC PRESSURE LOW LIGHT ON PROCEDURE. MTC REMOVED AND REPLACED RIGHT ENG INE DRIVEN PUMP AND AUXILIARY ELECTRIC PUMP. FABRICATED AND INSTALLED LINE IN WHEEL WELL AREA. 2 L 7 2 4F A6WE 1999071600432 19990716 00432 WP 1999 7 16 MWEA99393 1 19990710 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 202ME 47672 PIN ON STRAP OF EMERGENCY SLIDE ON GALLEY SERVICE DOOR WAS LOOSE. MTC RESECURED PIN ON GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1999071600433 19990716 00433 NM 1999 7 16 DL73E991539 1 19990708 A 3350 RPS1 POWER SUPPLY BOEING 737 737247 138448D NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 381DL 23608 WHEN EMERG LIGHTS TURNED OFF F/C EMERG TRACK LIGHTING CAME ON. REPLACED FWD EMERG LIGHT POWER SUPPLY AND BATTERIE S. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A16WE 1999071600434 19990716 00434 NM 1999 7 16 DL73E991540 1 19990709 A 3350 POWER SUPPLY BPS73 BOEING 737 737247 138448D NM ROW 16-21 INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 373DL 5424 23520 WHITE EMERGENCY TRACK LIGHTS OUT ROW 16 TO ROW 21. FOUND MID AND AFT BATTERY PACK AND PWR SUPPLY BAD. REPLACED SAME, O PS NORMAL. 2 L 7 2 4F A16WE 1999071600435 19990716 00435 NM 1999 7 16 DLM88991542 1 19990708 A 5712 RIB DOUG MD88 MD88 3023688 NM WS 112 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 RIB DAMAGED FROM CABLE AT L/E STA FS 123. RIB WORN THRU AT L/E WIND STATION FS 112 FROM CABLE. L/E FITTING DAMAGED FRO M CABLE AT STA FS 135 APPROX .5 INCH. RIB DAMAGED FROM CABLE AT L/E STA FS 129. L/E FITTING DAMAGED FROM CABLE AT STA FS 140 APROX .25 INCH. ALL REPAIRED PER APPROVED MANUALS. 2 L 7 2 4F RT A6WE 1999071600436 19990716 00436 NM 1999 7 16 DL72E991543 1 19990709 A 5330 65545703 SKIN BOEING 727 727247 138408F NM BS 440-460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF T HE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 440 & 460. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER B727 SRM 53-30-3, FIG 5 AND ER/A 367752-14AD. 2 L 7 3 4F A3WE 1999071600437 19990716 00437 NM 1999 7 16 DL73E991544 1 19990709 A 3350 WA339524012 POWER SUPPLY BOEING 737 737247 138448D NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 381DL 23608 WHEN EMERGENCY LIGHTS TURNED OFF, FIRST CLASS EMERGENCY TRACK LIGHTING CAME ON. REPLACED FWD EMERGENCY LIGHT POWER SUPP LY AND BATTERIES, OPERATION NORMAL. 2 L 7 2 4F A16WE 1999071600438 19990716 00438 NM 1999 7 16 DL72L991545 1 19990709 A 5230 6556927102 CHORD BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 LOWER FWD CORNER OUTER T-CHORD CRACKED AT FASTENER HOLE. REPAIRED PER ERA 372131. 2 L 7 3 4F A3WE 1999071600439 19990716 00439 NE 1999 7 16 DLL10991546 2 19990709 A 7261 RB21122B02 OIL PUMP 727706605 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 ENGINE FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 735D LXU676 193C1226 NR 3 ENG LOSING OIL IN CRUISE. BROUGHT NR 3 ENG BACK TO IDLE. DIVERTED TO SLC. INSPECTED SCAVENGE AND MAIN OIL FILTER S, NO METAL FOUND. CKD ALL CHIP DETECTORS, NO METAL FOUND. SERVICED AND RAN ENG TO TAKEOFF PWR. NO LEAKS NOTED, OIL P RESS AND QTY STABLE. REPLACED ENGINE OIL PUMP. 2 L 7 3 4F 4 F A23WE E12EU 1999071600440 19990716 00440 NM 1999 7 16 DL72S991547 1 19990707 A 5720 ANGLE BOEING 727 727225 1384077 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 ANGLE CRACKED APPROX 3 INCHES AND FASTENERS SHEARED AT FWD SIDE OF NR 7 SPOILER ACTUATOR CASTING. REPAIRED ANGLE PER M/ M 57-20-22 PG 809 PER ERA 367745-14 REF NR 64. 2 L 7 3 4F A3WE 1999071600441 19990716 00441 1999 7 16 DL72S991549 4 19990710 A 3416 FITTING 1QF2364C BOEING 727 727232 1384082 NM NR 2 ALTIMETER CRACKED A DALA K NONE O OTHER CR CRUISE 1 SO 27 528DA 21702 AT 33,000 FT, THE CAPTAINS AND F/O ALTIMETERS DIFFER BY 200 FT AND F/O ALT STICKS AT 2999. REPLACED NR 2 ALT. FOUND CR ACKED DISCONNECT FITTING ON NR 2 ALT. REPLACED FITTING AND PERFORMED LEAK CHECK. 2 L 7 3 4F A3WE 1999071600442 19990716 00442 WP 1999 7 16 DLL14991550 1 19990710 A 2612 FIRE WARNING LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE ACTIVATED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 736DY 32993 193C1227 014783 NR 2 ENGINE IFSD DUE TO FIRE WARNING CLIMBING OUT OF ATL. FIRED BOTH BOTTLES. MTC IN WORK. 2 L 7 3 4F A23WE 1999071600443 19990716 00443 NM 1999 7 16 DLM11991551 1 19990710 A 2611 SA308C SMOKE DETECTOR DOUG MD11 MD11 3023602 NM RT LAVATORY MALFUNCTIONED A DALA O OTHER B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CR CRUISE 1 SO 27 806DE 48477 THERE WAS A SMALL FIRE OR SMOLDER IN 4R LAV TRASH BIN, IT WAS PUT OUT PROMPTLY BY THE FLIGHT ATTENDANT. NO DAMAGE VISAB LE IN CAN. THE SMOKE ALARM DID NOT GO OFF. TESTED SMOKE DETECTOR ON ARRIVAL, CHECKED OK. NO EVIDENCE OF FIRE OR BURNE D MATERIAL. TRASH COMPARTMENT AND CONTAINER IN SERVICABLE CONDITION. REPLACED SMOKE DETECTOR PRECAUTIONARY. 2 L 7 3 4F RT A22WE 1999071600444 19990716 00444 NM 1999 7 16 DL76L991552 1 19990710 A 2530 CHILLER BOEING 767 767332 1382001 NM AFT GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 184DN 27111 GALLEY 413 FAULT LIGHT CAME ON. SLIGHT ELECTRIC ODOR AFTER CHILLER SHUTDOWN. INSPECTED GALLEY (413) CHILLER, OPS OK. R AN FOR 45 MIN, NO FAULT AND DETECTED NO ELECTRIC ODOR BURN. 2 L 7 2 4F RT A1NM 1999071600445 19990716 00445 NM 1999 7 16 DLM88991553 1 19990710 A 3350 61020 BATTERY DOUG MD88 MD88 3023688 NM GALLEY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DL 49583 AFT GALLEY FLASHLIGHT INDICATOR WOULD NOT BLINK AND HAD BROKEN STRAP. REPLACED FLASHLIGHT AND BATTERY ASSY, LIGHT T ESTS OK. 2 L 7 2 4F RT A6WE 1999071600446 19990716 00446 NM 1999 7 16 DL72S991554 1 19990710 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM AFT AIRSTAIR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 416DA 21258 AFT AIRSTAIR EMERG EXIT LIGHT INOP. REPLACED BATTERIES, OPS NOW OK. 2 L 7 3 4F A3WE 1999071600447 19990716 00447 NM 1999 7 16 DL72S991555 1 19990710 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM R1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 416DA 21258 R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NOW OK. 2 L 7 3 4F A3WE 1999071600448 19990716 00448 NM 1999 7 16 DL76L991557 1 19990711 A 2560 SLIDE BOEING 767 767332 1382001 NM LT EMER EXIT FAILED TEST A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 182DN 25987 ON ETOPS PDC LT OVERWING EXIT SLIDE SQUIB TEST INOP. CHECKED VOLTS AT PIN A OF SQUIB CONNECTOR, NO VOLTS. CHECKED BATT ERY PACK WIRING AND CONNECTIONS ALL OK. RESET PLUGS AND RESET DISABLED SWITCHES AND ALL OPS NORMAL. TEST OK. 2 L 7 2 4F RT A1NM 1999071600449 19990716 00449 1999 7 16 DL757991558 4 19990711 A 3160 6229436101 SYMBOL GENERATOR 6229436101 BOEING 757 757232 1384965 NM E & E COMPT MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 604DL 22811 DURING T/O ROLL CREW LOST ALL PRIMARY FLIGHT INSTRUMENTS, BOTH EADI'S AND BOTH EHSI'S. FLIGHT CREW ELECTED TO REJECT TA KEOFF AT 90 KTS. ALL INDICATIONS RETURNED TO NORMAL WITHIN 5 SECS. CONTRACT MAINTENANCE INSPECTED AIRCRAFT AND TESTED ALL SYMBOL GENERATORS WITH NO TROUBLE FOUND. 2 L 7 2 4F RT A2NM 1999071600450 19990716 00450 NE 1999 7 16 DL72S991559 2 19990711 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 MALFUNCTIONED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 485DA 58662 695347 20865 695347 DURING THE ROTATION AND INITIAL CLIMBOUT OF THE TAKEOFF FROM FLL, (OAT 32 DEG CELSIUS USING NORMAL PWR/EPR 2.06). ENG N R 3 EGT EXCEEDED THE TAKEOFF LIMIT. A MAXIMUM TEMP OF 640 DEG CELSIUS ON ENG 3 EGT WAS REACHED FOR A PERIOD OF UP TO 1 MINUTE. THRUST WAS REDUCED TO EGT OF 620 DEG CELSIUS, WHERE EPR WAS NOTED AT 1.78. REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999071600451 19990716 00451 NM 1999 7 16 DL733991560 1 19990711 A 3350 LIGHT 0201720001 BOEING 737 7373L9 1384470 NM ROW 11D INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 232DZ 24220 SEAT MOUNT EMERGENCY EXIT LIGHT INOP. REPLACED SEAT MOUNTED LIGHT ASSY. 2 L 7 2 4F RT A16WE 1999071600452 19990716 00452 NM 1999 7 16 DL72S991561 1 19990711 A 3350 LIGHT 1001141 BOEING 727 727232 1384082 NM AFT STAIRWAY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA 2382 22076 EMERGENCY EXIT CONTROL C/B POPPED, WILL NOT RESET. FOUND AFT STAIR LIGHT INOP. REPLACED LIGHT ASSY AND BATTERY. ALSO, FOUND LOSE TERMINAL IN 48 SEC. REPAIRED SAME, OPS CK NORMAL. 2 L 7 3 4F A3WE 1999071600453 19990716 00453 NM 1999 7 16 TC8A99021 1 19990713 A 2421 GENERATOR BOEING 727 72721C 138400M NM NR 2 MALFUNCTIONED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 705A 19134 UNABLE TO PARALLEL NR 2 GENERATOR. TRANSFERRED TO DMI 9233 AS PER TCA B727 MEL 24-1, SPECIAL PROCEDURES 24-1 PLACARDS I NSTALLED. 2 L 7 3 4F A3WE 1999071600454 19990716 00454 NM 1999 7 16 AALA990812 1 19990602 A 5312 BULKHEAD ANGLE BOEING 727 727223 1384074 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - FOUND STATION 870 BULKHEAD TO KEELBEAM ATTACH ANGLE CRACKED RIGHT W/W. REPLACED CRACKED ANGLE WITH NEW. (M) 2 L 7 3 4F A3WE 1999071600455 19990716 00455 NM 1999 7 16 AALA99081 1 19990527 A 5330 SKIN BOEING 727 727223 1384074 NM BS 610 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - FUSELAGE SKIN GOUGED STRINGER 8R STATION 610, RED 'M' AREA. CUTOUT DAMAGED AREA OF SKIN. INSALLED DOUBLER PER SR M 53-30-3. (M) 2 L 7 3 4F A3WE 1999071600456 19990716 00456 NM 1999 7 16 AALA990819 1 19990602 A 5330 SKIN BOEING 727 727223 1384074 NM BS 610-630 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CRACKS AT 2 FASTENER HOLES BETWEEN 600 PLUS 620 STRINGER 4R CRACKS AT 2 FASTENER HOLES BETWEEN 620 AND 640, STRINGER 4R. CUT OUT DAMAGE 610-630, HFEC'D AREA. NO CRACKS BEYOND CUTOUT. INSTALLED .080 2024T3 DOUBLER USING EXISTI NG FASTENER SPACING PER SRM 53-30-03 PAGE 20-23. (M) 2 L 7 3 4F A3WE 1999071600457 19990716 00457 NM 1999 7 16 AALA990818 1 19990602 A 5330 SKIN BOEING 727 727223 1384074 NM BS 640-660 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CRACKS AT 2 FASTENER HOLES BELOW STRINGER 4R AT SKIN LAP BETWEEN 640-660. CUT OUT DAMAGE 653-660. HFEC'D C UT OUT AREA NO FURTHER CRACKS INSTALLED .080 2024T3 DOUBLER USING EXISTING FASTENER SPACING PER SRM 53-30-03 PAGE 2023. (M) 2 L 7 3 4F A3WE 1999071600458 19990716 00458 NM 1999 7 16 AALA990817 1 19990602 A 5330 SKIN BOEING 727 727223 1384074 NM BS 507-512 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CRACKS AT TWO EACH FASTENER HOLES BELOW STRINGER 4R AT SKIN LAP BETWEEN 500-520. CUT OUT DAMAGE 507-512, HF EC'D AREA, NO FURTHER CRACKS. INSTALLED .080 2024 T-3 DOUBLER USING EXISTING FASTENER SPACING PER SRM 53-30-03 PAGE 20- 23. (M) 2 L 7 3 4F A3WE 1999071600459 19990716 00459 NM 1999 7 16 AALA990809 1 19990626 A 5311 FRAME BOEING 727 727233 138408A NM BS 303.9 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND WEB CRACKED STATION 303.9 STRINGER 16 INSIDE OF FRAME. INSTALLED NEW WEB PER SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999071600460 19990716 00460 NM 1999 7 16 AALA990808 1 19990602 A 5330 SKIN BOEING 727 727233 138408A NM BS 593 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION ON INTERIOR BELLY SKIN BELOW INTERCOSTAL. INSTALLED REPAIR AS PER ESO 11697 DATED 5/27/99. (M) 2 L 7 3 4F RT A3WE 1999071600461 19990716 00461 NM 1999 7 16 AALA990807 1 19990601 A 5330 SKIN BOEING 727 727233 138408A NM BS 685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION ON INTERIOR OF BELLY SKIN OF FORWARD CARGO OUTBOARD STRINGER 27L STATION 685. CUT OUT CORRODED SK IN TO SKIN SPLICE AND REPAIRED WITH DOUBLER PER SRM 53-30-3 FIG 12. (M) 2 L 7 3 4F RT A3WE 1999071600462 19990716 00462 NM 1999 7 16 AALA990806 1 19990601 A 5314 KEEL BEAM BOEING 727 727233 138408A NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION AROUND DOM NUT ON KEEL BEAM EXTENSION STATION 720B. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER ESO 11697 DATED 5/27/99. (M) 2 L 7 3 4F RT A3WE 1999071600463 19990716 00463 NM 1999 7 16 AALA990805 1 19990601 A 5100 STRINGER BOEING 727 727233 138408A NM BS 720-735 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION ON STRINGER 28L AT STATION 720 PLUS 15 INCHES. REMOVED CORROSION INSTALLED REPAIR STRAP PER ESO 1 1697 DATED 5-27-99. (M) 2 L 7 3 4F RT A3WE 1999071600464 19990716 00464 NM 1999 7 16 AALA990804 1 19990601 A 5313 SKIN BOEING 727 727233 138408A NM BS 685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION ON FUSE INTERIOR SKIN STATION 685, OUTBOARD STRINGER 27R. CUT OUT CORRODED SKIN TO SPLICE AND REP AIRED WITH DOUBLERS PER SRM 53-30-3. (M) 2 L 7 3 4F RT A3WE 1999071600465 19990716 00465 NM 1999 7 16 AALA99803 1 19990528 A 5313 STRINGER BOEING 727 727233 138408A NM BS 500-520 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION IN STRINGER 27 RIGHT STATION 500-520. INSTALLED STRINGER REPAIR IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F RT A3WE 1999071600466 19990716 00466 NM 1999 7 16 AALA990802 1 19990601 A 5313 STRINGER BOEING 727 727233 138408A NM BS 690 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION IN STRINGER 26 LEFT, STATION 690. CUT OUT DAMAGED SECTION OF STRINGER 2. INSTALLED NEW SECTION P ER SRM 53-10-3 FIGURE 1. (M) 2 L 7 3 4F RT A3WE 1999071600467 19990716 00467 NM 1999 7 16 AALA990801 1 19990531 A 5313 STRINGER BOEING 727 727233 138408A NM BS 660-700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION AROUND RIVETS ALONG BOTTOM OF STRINGER STATION 660-700. REPAIRED PER SRM 51-10-3 FIG 1. (M) 2 L 7 3 4F RT A3WE 1999071600468 19990716 00468 NM 1999 7 16 AALA990800 1 19990601 A 5330 SKIN BOEING 727 727233 138408A NM BS 1060 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND DENT IN SKIN AT SECOND FRAME FROM TOP, 6 INCHES FORWARD OF AFT EDGE OF RIGHT SERVICE DOOR. CUTOUT DAMAGE AN D REPAIRED PER SRM 52-00-3 FIGURE 4 BY INSTALLATION OF DOUBLER. (M) 2 L 7 3 4F RT A3WE 1999071600469 19990716 00469 NM 1999 7 16 AALA990816 1 19990602 A 5330 SKIN BOEING 727 727233 138408A NM BS 593 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 866AA 21371 TUL - FOUND CORROSION ON INTERIOR BELLY SKIN AND ON INTERCOSTAL STATION 593, STRINGER 28R AND STRINGER 27R. INSTALLED N EW INTERCOSTAL AND REPAIR DOUBLER TO SKIN PER ESO 11697 DATED 5-27-99. (M) 2 L 7 3 4F RT A3WE 1999071600470 19990716 00470 WP 1999 7 16 AALA990759 1 19990521 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1161 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 579AA 53156 TUL - FOUND CORROSION ON AFT CARGO CUTOUT LOWER DOOR BEAM HORIZ LEG STATION 1161 TO 1193. REPAIRED HORIZ DOOR BEAM AT A FT CARGO DOOR CUTOUT STATION 1161 PER ESO 80559, DATED 5-21-99. (M) 2 L 7 2 4F A6WE 1999071600471 19990716 00471 WP 1999 7 16 AALA990758 1 19990520 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 380/402 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 403A 49314 TUL - FOUND CORROSION ON A/C FUSELAGE SKIN STAITON 380 AND 402, UNDER ANTENNAS. REMOVED CORROSION PER SRM 51-10-3 AND T REATED AREA. (M) 2 L 7 2 4F A6WE 1999071600472 19990716 00472 WP 1999 7 16 AALA990757 1 19990520 A 5320 5936038501 BEAM DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 451AA 49477 TUL - FOUND CORROSION ON LOWER JAMB BEAM, NUMEROUS AREAS ALONG BEAM STATION 1155-1212. INSTALLED DOUBLER PER AARD 53-10 -00-03 AND ESO 80559 DATED 5-20-99. (M) 2 L 7 2 4F A6WE 1999071600473 19990716 00473 WP 1999 7 16 AALA990755 1 19990524 A 5610 ADK1691 WINDOW DOUG DC9 DC982 3022082 WP LT COCKPIT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 424AA 49336 IAD- FLT 731 - EN ROUTE DCA- ORD SHORTLY AFTER TAKEOFF, NOTED ELECTRICAL/BURING WIRE TYPE FUMES IN THE COCKPIT. FUMES B ECAME STRONGER AFTER APPROXIMATELY TWO MINUTES IN FLIGHT. FLIGHT ATTENDANTS REPORTED FUMES IN REAR OF AIRCRAFT UPON GAT E ARRIVAL. AIR INTERRUPTED AND LANDED IAD WITHOUT INCIDENT. REPLACED CAPTAINS CLEAR VIEW WINDOW, RAN PACKS NO SMELL NO TED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999071600474 19990716 00474 WP 1999 7 16 AALA990743 1 19990521 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP ACM BAY DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 266AA 524098 49291 DFW - FLT 683 - AFTER TAKEOFF DTW EN ROUTE TO DFW, AN ELECTRICAL ODOR WAS DETECTED IN FAR AFT CABIN. REMOVED GALLEY POW ER, OVERHEAD SIDE WALL LIGHTS, AND RECIRCULATING FAN. ALL ELECTRICAL SYSTEMS INDICATED NORMAL. LANDED DFW WITHOUT INCI DENT. REPLACED RECIRCULATING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999071600475 19990716 00475 EU 1999 7 16 AALA990549 1 19990420 A 3260 LAMP FOKKER F28 F28MK0100 4990807 EU LANDING GEAR OUT OF POSITION A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 1433B 11418 ORD - FLT 1803 - EN ROUTE HPN - ORD, NOSE GEAR POSITION LIGHT ILLUMINATES INTERMITTENTLY WITH ALL OTHER INDICATIONS NORM AL. FLIGHT CONTINUED AND LANDED ORD WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND FAULT IN LIGHT CAPSULE . MAINTENANCE REMOVED LIGHT CAPSULE, FOUND A BULB LODGED BEHIND CAPSULE. REMOVED BULB. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F RT 1999071600476 19990716 00476 EU 1999 7 16 AALA990675 1 19990507 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1437B 11427 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999071600477 19990716 00477 EU 1999 7 16 AALA990681 1 19990510 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1444N 11447 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD CABIN INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT FLOOR PATH LIGHT WIRE CONNECTOR IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999071600478 19990716 00478 EU 1999 7 16 AALA990493 1 19990412 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1439A 11434 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT ARROW MARKER INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999071600479 19990716 00479 NM 1999 7 16 AALA990719 1 19990517 A 3350 LIGHT BOEING 727 727223 1384074 NM R2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 862AA 21089 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND R2 DOOR INOPERATIVE. REPAI RED EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999071600480 19990716 00480 NM 1999 7 16 AALA990705 1 19990513 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 2006 21520 DFW - DURING MAINTENANCE CHECK, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999071600481 19990716 00481 NM 1999 7 16 AALA990677 1 19990507 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 859AA AA49 21086 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF COACH CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999071600482 19990716 00482 NM 1999 7 16 AALA990492 1 19990412 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 896AA 22012 TUL - DURING OVERNIGHT MAINTENANCE, CO-PILOTS OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 3 4F A3WE 1999071600483 19990716 00483 NM 1999 7 16 AALA990624 1 19990427 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AIRSTAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 848AA 15542 20989 TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EXIT LIGHT A SSEMLBY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999071600484 19990716 00484 NM 1999 7 16 AALA990625 1 19990426 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT AIRSTAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 712AA 16209 22468 TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EX IT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999071600485 19990716 00485 NM 1999 7 16 AALA990528 1 19990415 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 872AA 21384 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FORWARD LAVATORY AND GALLEY WERE INOPERATIV E. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE AT FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999071600486 19990716 00486 NM 1999 7 16 AALA990547 1 19990420 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. SPLICED EMERGENCY EXIT FLOOR PAT H LIGHTING BROKEN WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999071600487 19990716 00487 WP 1999 7 16 USAA990488 1 19990604 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 180 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND 2 INCH BY 36 INCH CORROSION AT FLOOR SUPPORT MARKED NR 23 FORWARD GALLEY AREA, STATION 180 . CORROSION LEVER 1. CORROSION TASK NR C46-53303. REMOVED, MANUFACTURED NEW FLOOR SUPPORT AND INSTALLED 7075T6 EXTRUS ION C/C 1719673. (M) 2 L 7 2 4F A6WE 1999071600488 19990716 00488 WP 1999 7 16 USAA99089 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 680 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK IN LONGERON 5 LT AT STATION 680. CUT OUT DAMAGED SECTION AND INSTALLED LONG ERON REPAIR SECTION AND SPLICES PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999071600489 19990716 00489 WP 1999 7 16 USAA990490 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT LONGERON 5 LEFT, STATION 699. CUT OUT DAMAGED SECTION AND INSTALLED LONG ERON REPAIR SECTION AND SPLICES PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999071600490 19990716 00490 WP 1999 7 16 USAA990491 1 19990604 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT LONGERON 2L, STATION 756. CUT OUT DAMAGED SECTION AND INSTALLED LONGERON REPAIR SECTION AND SPLICED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999071600491 19990716 00491 WP 1999 7 16 USAA990487 1 19990604 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 980-996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND CORROSION AT CUSP ANGLE (FLOOR SUPPORT) AT STATION 980-996, RT, L18. CORROSION LEVEL 1. C ORROSION TASK NR C-58-53300. INSTALLED REPAIR PER SRM 53-05 FIG 25. (M) 2 L 7 2 4F A6WE 1999071600492 19990716 00492 WP 1999 7 16 USAA990486 1 19990604 A 5320 CAP DOUG DC9 DC931 3022065 WP BS 96 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49008 48114 PIT - DURING Q-4 CHECK, FOUND CORROSION THE WHOLE WAY THROUGH END CAP, AT STATION 996 - LONGERON 19R. CORROSION LEVEL 1 . CORROSION TASK NR C-57-53300. REWORKED AND REPLACED END CAP FITTING. (M) 2 L 7 2 4F A6WE 1999071600493 19990716 00493 NM 1999 7 16 USAA990470 1 19990514 A 5230 SKIN BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 35344 23739 CLT - DURING RON, FOUND ONE CRACK APPROX .5 INCH LONG AND ONE CRACK .125 INCH LONG ON AFT CARGO DOOR EXTERIOR SKIN AT AF T UPPER CORNER AND FORWARD UPPER CORNER OF HANDLE CUTOUT. CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR PER TR 52-30-03. ( M) 2 L 7 2 4F RT A16WE 1999071600494 19990716 00494 NM 1999 7 16 USAA990476 1 19990529 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND 1.5 INCH BY .5 INCH CORRODED AREA ON FLOORBEAM AROUND FLOORBOARD HOLE AT BS 412 BL 0. COR ROSION LEVEL 1. INSTALLED STRAP ON AFT SIDE PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999071600495 19990716 00495 NM 1999 7 16 USAASB99133 1 19990602 A 5210 6990285 HINGE COVER BOEING 737 737301 1384611 NM PAX DOOR BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 300AU 23228 CLT - FLT 1475 - ON CLIMB-OUT FROM CLT, AT APPROXIMATELY 10,000 FT, THE CREW UNABLE TO PRESSURIZE THE AIRCRAFT AND A LOU D AIR NOISE WAS HEARD COMING FROM THE FORWARD MAIN ENTRY DOOR. DECISION WAS MADE TO RETURN TO FIELD AT CLT. FLIGHT LAN DED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR UPPER HINGE COV ER BROKEN WHICH WOULD NOT ALLOW THE DOOR HINGE TO SEAT PROPERLY IN POSITION. REMOVED AND REPLACED BROKEN HINGE COVER. D OOR OPERATIONAL CHECK NORMAL. PRESSURIZATION CHECK OF AIRCRAFT GOOD. (M) 2 L 7 2 4F RT A16WE 1999071600496 19990716 00496 SO 1999 7 16 C2XA99IA330 1 19990601 A 5320 12006159001 ANGLE EMB 120 EMB120RT SO FRAMED 41-44 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RIGHT SIDEWALL/FLOOR ANGLE FROM FRAME 41 TO 44. REMOVED AND REPL ACED ANGLE IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600497 19990716 00497 SO 1999 7 16 C2XA99IA329 1 19990601 A 5320 12004171003 ANGLE EMB 120 EMB120RT SO FRAME 31-35 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT SIDEWALL/FLOOR ANGLE FROM FRAME 31-35. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600498 19990716 00498 SO 1999 7 16 C2XA99IA328 1 19990601 A 5320 12005802001 SILL EMB 120 EMB120RT SO FRAME 15-20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT OUTBOARD BUTT STRAP FROM FRAME 15 TO FRAME 20. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600499 19990716 00499 SO 1999 7 16 C2XA99IA327 1 19990601 A 5320 12046963007 STRAP EMB 120 EMB120RT SO FRAME 14-20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT INBOARD BUTT STRAP FROM FRAME 14 TO FRAME 20. REMOVED AND R EPLACED BUTT STRAP IAW SRM 51-40-02. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600500 19990716 00500 SO 1999 7 16 C2XA99IA326 1 19990601 A 5320 12027928001 STRAP EMB 120 EMB120RT SO FRAME 30-35 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FROM FRAME 30 TO FRAME 35. REMOVED AND REPL ACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600501 19990716 00501 SO 1999 7 16 C2XA99IA325 1 19990106 A 5320 12027929001 STRAP EMB 120 EMB120RT SO FRAME 35-38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT BL 0 FROM FRAME 35 TO FRAME 39. REMOVED AND REPLAC ED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600502 19990716 00502 SO 1999 7 16 C2XA99IA324 1 19990601 A 5320 12027929001 STRAP EMB 120 EMB120RT SO FRAME 33-38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FROM FRAME 35 TO FRAME 38. REMOVED AND REPL ACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600503 19990716 00503 SO 1999 7 16 C2XA99IA323 1 19990601 A 5320 12006158002 STRAP EMB 120 EMB120RT SO FRAME 40-44 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FRAMES 40, 42 AND 44. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600504 19990716 00504 SO 1999 7 16 C2XA99IA322 1 19990601 A 5320 120279001 STRAP EMB 120 EMB120RT SO FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT RBL 19 FROM FRAME 39 TO FRAME 40. REMOVED AND REPL ACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600505 19990716 00505 SO 1999 7 16 C2XA99IA321 1 19990601 A 5320 12027888003 STRAP EMB 120 EMB120RT SO BS 66531 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT INBOARD STRAP FROM STATION 66531.1 TO 87280.0. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600506 19990716 00506 SO 1999 7 16 C2XA99IA320 1 19990601 A 5320 12007053007 STRAP EMB 120 EMB120RT SO BS 87280 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CENTER BUTT STRAP FROM STATION 87280.0 TO 99645.0. REMOVED AND R EPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600507 19990716 00507 SO 1999 7 16 C2XA99IA319 1 19990601 A 5320 12006153001 BEAM EMB 120 EMB120RT SO FRAME 40-44 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON OMEGA BEAM LBL 19 AT FRAMES 40, 42 AND 44. REPAIRED OMEGA BEAM I AW EC5310-01043. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600508 19990716 00508 SO 1999 7 16 C2XA99IA318 1 19990601 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CROSSBEAM FROM RBL 19 TO RBL 31 AT FRAME 38. REMOVED AND REPLACE D CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600509 19990716 00509 SO 1999 7 16 C2XA99IA317 1 19990601 A 5320 12046156601 STRAP EMB 120 EMB120RT SO FRAME 13-20 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16702 120078 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RIGHT INBOARD BUTT STRAP FROM FRAME 13 TO 20. REMOVED AND REPLAC ED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600510 19990716 00510 SO 1999 7 16 C2XA99IA316 1 19990616 A 3350 AD2047 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING MAINTENANCE INSPECTION, THE AFT FIVE AISLE PATH EMERGNECY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600511 19990716 00511 EU 1999 7 16 C2XA99IA315 1 19990615 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR42-420 JIC 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600512 19990716 00512 SO 1999 7 16 C2XA99IA314 1 19990614 A 3350 3025101 LIGHT EMB 145 EMB145LR SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16951 145063 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAIN TENANCE CLEANED THE LIGHT ASSEMBLY SOCKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999071600513 19990716 00513 EU 1999 7 16 C2XA99IA301 1 19990608 A 5330 S53371420238 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE LEFT FUSELAGE SKIN WAS FOUND TO BE DENTED JUST BELOW THE CARGO DOR CUTOUT. MAINTEN ANCE PERFORMED AN INSERTION REPAIR IAW ATR42-320 SRM 53-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600514 19990716 00514 EU 1999 7 16 C2XA99IA302 1 19990608 A 5313 S5367140722902 STRINGER AEROSP ATR42 ATR42320 8680930 EU FRAME 27/29 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 27 AND 30. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600515 19990716 00515 EU 1999 7 16 C2XA99IA303 1 19990608 A 5313 S5367140723100 STRINGER AEROSP ATR42 ATR42320 8680930 EU FRAME 27/29 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, STRINGER 19 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 27 AND 29. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600516 19990716 00516 EU 1999 7 16 C2XA99IA304 1 19990608 A 5313 S5367100020302 STRINGER AEROSP ATR42 ATR42320 8680930 EU FRAME 27/30 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, STRINGER 17 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 27 AND 30. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600517 19990716 00517 SO 1999 7 16 C2XA99IA313 1 19990614 A 2150 AN47A BOLT EMB 120 EMB120RT SO RAM AIR DOOR WORN A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 15730 120187 IAH - FLT 3561 - DURING CLIMB, THE CREW REPORTED SMOKE IN THE AIRCRAFT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WI THOUT INCIDENT. MAINTENANCE REPLACED THE RAM AIR DOOR ACTUATOR ATTACH BOLT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600518 19990716 00518 SO 1999 7 16 C2XA99IA312 1 19990610 A 3350 GE1317 BULB EMB 145 EMB145LR SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14950 145061 IAH - DURING 1A INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999071600519 19990716 00519 EU 1999 7 16 C2XA99IA311 1 19990613 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU ROW 2AB DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 IAH - DURING 4A INSPECTION, THE EMERGENCY EXIT LIGHTS AT SEATS 2AB THROUGH 4AB WERE FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW ATR42-320 JIC 33-51-21, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600520 19990716 00520 EU 1999 7 16 C2XA99IA310 1 19990612 A 3350 LP1670 BULB AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16450 510 IAH - DURING POST FLIGHT INSPECTION, THE AISLE PATH LIGHTING WAS FOUND TO HAVE ONE BULB INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600521 19990716 00521 EU 1999 7 16 C2XA99IA309 1 19990608 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE AND CORRODED. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600522 19990716 00522 EU 1999 7 16 C2XA99IA308 1 19990608 A 5210 S5217640300860 STAIR AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR STAIR ASSEMBLY WAS FOUND TO BE CRACKED IN SEVERAL PLACES. MAINTENAN CE STOP DRILLED THE CRACKS AND INSTALLED REPAIR DOUBLERS IAW ATR42-320 SRM 52-11-00, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600523 19990716 00523 EU 1999 7 16 C2XA99IA307 1 19990608 A 5210 S5217620420200 PAN AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR PAN WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR42-320 SRM 52-11-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600524 19990716 00524 EU 1999 7 16 C2XA99IA306 1 19990608 A 5315 S5367240820201 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600525 19990716 00525 EU 1999 7 16 C2XA99IA305 1 19990608 A 5320 S5367140620201 DOUBLER AEROSP ATR42 ATR42320 8680930 EU FRAME 32-33 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE VHF ANTENNA DOUBLER BETWEEN FRAMES 32 AND 33 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW ATR42-320 SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 1999071600526 19990716 00526 EU 1999 7 16 C2XA99IA299 1 19990605 A 3350 LP1670 LAMP AEROSP ATR42 ATR42500 EU ROW 1-4 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16450 510 IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT LIGHTS AT ROWS 1-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999071600527 19990716 00527 SO 1999 7 16 C2XA99IA300 1 19990606 A 3350 RPS1B BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 3 EMERGENCY BATTERY PACK WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 3-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4F RT T00011AT 1999071600528 19990716 00528 NM 1999 7 16 F3LA99084 1 19990625 A 2910 6544510816 LINE BOEING 737 737201 1384454 NM 'A' HYD SYSTEM FAILED A F3LA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 03 212US 20212 PHX - UPON ARRIVAL, FLIGHT CREW REPORTED 'A' SYSTEM HYDRAULIC LIGHT FLICKERED, THEN LOST AL SYSTEM 'A' HYDRAULICS AT ALT ITUDE. 'B' SYSTEM AND STANDBY SYSTEM REMAINED NORMAL. REPLACED DEFECTIVE 'A' SYSTEM MAIN HYDRAULIC SUPPLY LINE TO ENGI NE DRIVEN HYDRAULIC PUMP AT RIGHT OUTBOARD WALKING BEAM. PERFORMED LEAK CHECK AND SERVICED HYDRAULIC SYSTEM PER MM 29-0 9-121A AND WORK CARD 1-1101A AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1999071600529 19990716 00529 WP 1999 7 16 99ZZZM386 1 19990502 A 3610 2062301 EDC CVAC 440 440 2422902 WP ENGINE FAILED A RENA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 01 73163 AEIO69741 366 SMOKE IN CABIN. DISCONNECTED ENGINE DRIVEN COMPRESSOR. (M) 2 L 7 2 4R 6A6 1999071600530 19990716 00530 EA 1999 7 16 MASA99086 1 19990601 A 3240 74485617 HANDLE CNDAIR CL600 CL6002B19 EA PARKING BRAKE OUT OF ADJUST A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 37228 7228 FLT 5805 - PHL-MKE - THE CRWE COULD NOT SET THE PARKING BRAKE. MAINTENANCE ADJUSTED THE PARKING BRAKE HANDLE SET SCREW. THE AIRCRAFT WAS RETURNED TO SERVICE (M) 2 L 7 2 4F RT A21EA 1999071600531 19990716 00531 EA 1999 7 16 MASA99087 1 19990601 A 8011 35051889 STARTER CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 77195 7195 FLT 5840 - TYS-DCA - THE RIGHT ENGINE WOULD NOT START. MAINTENANCE TROUBLESHOT AND CONCLUDED THE STARTER HAD FAILED, AN D REMOVED AND REPLACED THE STARTER. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999071600532 19990716 00532 EA 1999 7 16 99ZZZM387 1 19990604 A 2612 FIRE WIRE DHAV DHC7 DHC7102 2802708 EA NR 1 ENGINE CHAFED A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 4860J 19 NR 1 ENGINE FIRE HANDLE INDICATING FIRE AT ALL ITEMS UNABLE TO RESET. REPAIRED NR 1 ENGINE FIRE LOOP WIRING HARNESS. ( M) 2 H 7 4 4T A20EA 1999071600533 19990716 00533 SO 1999 7 16 ASOA99051 1 19990612 A 3350 AGCI FUSE EMB 120 EMB120RT SO CABIN BLOWN A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 275AS 120234 EMERGENCY LIGHTING FLOOR LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED BLOWN FUSE. OPERATIONAL CHECKS WERE GOOD AND AIR CRAFT IS OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600534 19990716 00534 SO 1999 7 16 ASOA99050 1 19990611 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 11 225AS 558 120022 EN ROUTE ATL-MEI - EXPERIENCED FLAP CONTROL FAULT. COULD NOT RESET SO DIVERTED TO JAN. DECLARED EMERGENCY AND MADE A 0 DEGREE FLAP LANDING. MAINTENANCE REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND A IRCRAFT IS OK FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600535 19990716 00535 WP 1999 7 16 99ZZZM388 1 19990610 A 5280 340621040213 FITTING CVAC 340 34031 2422704 WP LT MLG DOOR BROKEN A ERAA K NONE J WARNING INDICATION CL CLIMB 1 AL 03 538JA 34 DURING PILOT TRAINING, TRANSIT LIGHT REMAINED ON WITH GEAR UP. MADE UNEVENTFUL LANDING ANC. LEFT MAIN GEAR OUTBOARD GE AR DOOR RETRACT FITTING BROKEN, CAUSING INBOARD WHEEL ASSY CONTACT WITH INBOARD GEAR DOOR. REPAIRED NACELLE LONGERON AN D REPLACED OUTBOARD DOOR RETRACT FITTING AND IDLER ALONG WITH INBOARD GEAR DOOR. (M) 2 L 7 2 4R 6A6 1999071600536 19990716 00536 SO 1999 7 16 C2XA99CL042 1 19990602 A 3297 WIRE EMB 120 EMB120RT SO LANDING GEAR BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 58733 120197 CLE - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF AND THE UP/DOWN CONTROL C/B POPPED. AIRCRAFT RETURNED TO CLEVELA ND WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED A WIRE AT THE LANDING GEAR CONTROL HANDLE IAW EMB120 WM 20-21-00. OP ERATIONAL CHECKS OF THE RETRACTION AND EXTENSION SYSTEM WERE SATISFACTORY IAW EMB-120 MM 32-30-00. AIRCRAFT WAS RELEASE D TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600537 19990716 00537 SO 1999 7 16 C2XA99CL043 1 19990601 A 7720 3034598CL HARNESS EMB 120 EMB120RT SO NR 1 ENGINE FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 16723 20824 120169 CLE - THE NR 1 ENGINE T6 INDICATION FAILED IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAI NTENANCE REPAIRED A BROKEN WIRE ON THE NR 1 T6 WIRE HARNESS IAW EMB-120 WM 20-21-00. OPERATIONAL CHECK OF THE SYSTEM WA S SATISFACTORY IAW EMB-120 MM 77-20-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999071600538 19990716 00538 EU 1999 7 16 C2XA99BT057 1 19990605 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU ROW 3WL INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14834 193 BTV - DURING LINE CHECK ON RON BTV, FOUND FORWARD EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE (EVERY OTHER ONE). REMOVED A ND REPLACED POWER SUPPLY UNIT AT 3 WL, OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999071600539 19990716 00539 SO 1999 7 16 C2XA99BT058 1 19990605 A 3350 LIGHT EMB 145 EMB145 SO ROW 3/6 INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 15926 145005 EWR - FLT 4281 - CREW REPORTED PSU LIGHTS OVER EMERGENCY LIGHTS ROWS 3 AND 6 AS INOPERATIVE. EMERGENCY LIGHTS TESTED GO OD, REPLACED BULBS IN PSU'S AS NECESSARY. NO EMERGENCY LIGHT PROBLEM FOUND. (M) 2 L 7 2 4F RT T00011AT 1999071600540 19990716 00540 NM 1999 7 16 USAA990556 1 19990610 A 3233 654581945 GUSSET BOEING 737 737301 1384611 NM NLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND 3 INCH CRACK IN NOSE GEAR ACT FORWARD ATTACH FITTING GUSSET. REPLACED GUSSET WITH IDENTIC AL PART NUMBER. (M) 2 L 7 2 4F RT A16WE 1999071600541 19990716 00541 WP 1999 7 16 USAA990620 1 19990620 A 5320 9911839210 WEB DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 48544 48026 PIT - LINE MAINTENANCE REPORT INDICATED 6 INCH CRACK AT RIGHT SIDE CANTED WEB SECTION AT STATION 1463. REMOVED AND REPL ACED CRACKED WEB SECTION. (M) 2 L 7 2 4F A6WE 1999071600542 19990716 00542 NM 1999 7 16 USAA990618 1 19990618 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 26772 24549 CLT - DURING RON VISIT, FOUND 3 INCH CRACK AT HORIZONTAL STAB MAIN BOX SKIN. LOCATION IS LOWER SURFACE OF RIGHT HORIZ S TAB, JUST FORWARD OF THE AFT SPAR ABOUT 5 FEET FROM FROM FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 55-10-07 REV A. (M ) 2 L 7 2 4F RT A16WE 1999071600543 19990716 00543 NM 1999 7 16 USAA990613 1 19990621 A 5311 BOEING 737 737401 1384701 NM UNKNOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A . 2 L 7 2 4F RT A16WE 1999071600544 19990716 00544 NM 1999 7 16 USAA990612 1 19990621 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 500D BETWEEN STRINGER 8R AND 9R FRAME. REP AIRED DOUBLER PER EA 64832 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999071600545 19990716 00545 NM 1999 7 16 USAA990611 1 19990621 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACK IN RADIUS INBOARD SUPPORT ANGLE AT STATION 540 RAM AIR DUCT INLE T. REPAIRED DOUBLER AND ANGLE PER TR 53-50-03. (M) 2 L 7 2 4F RT A16WE 1999071600546 19990716 00546 NM 1999 7 16 USAA990603 1 19990621 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 500A BETWEEN STRINGER 8L AND 9L ON FRAME. I NSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999071600547 19990716 00547 NM 1999 7 16 USAA990602 1 19990621 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FUOND A .375 INCH CRACK AT STATION 787 BETWEEN STRINGER 8L AND 9L ON FRAME. I NSTALLED DOUBLER PER EA 64832. (M) 2 L 7 2 4F RT A16WE 1999071600548 19990716 00548 NM 1999 7 16 USAA990594 1 19990621 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK AT STATION 867 BETWEEN STRINGER 8L AND 9L ON FRAME. INS TALLED DOUBLER PER EA 64832. (M) 2 L 7 2 4F RT A16WE 1999071600549 19990716 00549 NM 1999 7 16 USAA990593 1 19990621 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURNG Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 480 BETWEEN STRINGER 8L AND 9L ON FRAME. IN STALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999071600550 19990716 00550 NM 1999 7 16 USAA990592 1 19990621 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 827 BETWEEN STRINGER 8L AND 9L ON FRAME. I NSTALLED DOUBLER PER EA 64832. (M) 2 L 7 2 4F RT A16WE 1999071600551 19990716 00551 NM 1999 7 16 USAA990591 1 19990621 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 500C BETWEEN STRINGER 8L AND 9L ON FRAME. I NSTALLED DOUBLER PER EA 64832. (M) 2 L 7 2 4F RT A16WE 1999071600552 19990716 00552 NM 1999 7 16 USAA990590 1 19990621 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK BY 72 INCH AREA OF SURFACE CORROSION UPPER T-CAP OF FLOOR BEAM AT STATION 986.5. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. INSTALLED NEW FABRICATED T-CAP PER TR 53-60-0 1. (M) 2 L 7 2 4F RT A16WE 1999071600553 19990716 00553 NM 1999 7 16 USAA069962 1 19990624 A 5311 FRAME BOEING 727 727225 1384077 NM BS 870 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 LEFT BS 870 FRAME HAS HFEC CRACK INDICATION AT STRINGER 18A ATTACH BOLT AFT HOLE IN LOWER ROW. ACCOMPLISHED REPAIR AT L EFT BS 870 FRAME DUE TO CRACK INDICATION AT STRINGER 18A ATTACH BOLT HOLE, AFT HOLE IN LOWER ROW, IAW BOEING TELEX TSI-M IA-99-0008RR. (M) 2 L 7 3 4F A3WE 1999071600554 19990716 00554 NM 1999 7 16 USAA069961 1 19990624 A 5312 BULKHEAD BOEING 727 727225 1384077 NM BS 1183 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 AFT AIRSTAIR EXTERNAL ACCESS PANEL 3902, BS 1183 PRESSURE BULKHEAD CRACKED AT EDGE OF RADIUS BLOCK RBL 16, AT 8 INCHES U P FROM BOTTOM, AND FROM 10 INCH ABOVE BOTTOM TO 14 INCH ABOVE BOTTOM. INSTALLED DOUBLER REPAIR AT FS 1183 PRESSURE BULK HEAD AT EDGE OF RADIUS BLOCK RBL 16. MATERIAL USED, 2024-T3, .063 INCH, 31 INCH BY 19 INCH. REPAIR ACCOMPLISHED IAW B OEING TELEX TSI-MIA-99-0004TR, DATED MAY 11, 99 AND SB 727-53-0202. (M) 2 L 7 3 4F A3WE 1999071600555 19990716 00555 NM 1999 7 16 USAA069960 1 19990624 A 5320 BEAM BOEING 727 727225 1384077 NM BS 1183 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 VERTICAL BEAM IS CRACKED IN BOTH RADIUS LOC AT BS 1183, RBL 36, WL 238. INSTALLED DOUBLER REPAIR ON THE VERTICAL BEAM, BS 1183 RBL 36.83 IAW SB 727-53-0192. MATERIAL USED, 7075-T6, .100 INCH, TWO ANGLES, 48 INCH BY 7 INCH. (M) 2 L 7 3 4F A3WE 1999071600556 19990716 00556 NM 1999 7 16 USAA069959 1 19990624 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 STRINGER 21L IS CRACKED AT OUTBOARD FRAME ATTACH POINT STATION 480. INSTALLED STRINGER REPAIR AT STATION 480, STRINGER 21L AT OUTBOARD FRAME ATTACH POINT. MATERIAL USED, PART NR BAC1498-139, 35 INCH LONG. REPAIR ACCOMPLISHED IAW SRM 53-1 0-3, FIG 1. (M) 2 L 7 3 4F A3WE 1999071600557 19990716 00557 NM 1999 7 16 USAA069958 1 19990624 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 STRINGER 25R IS CRACKED AT OUTBOARD FRAME ATTACH POINT STATION 460. INSTALLED STRINGER REPAIR AT STATIN 460, STRINGER 2 5L AT OUTBOARD FRAME ATTACH POINT. MATERIAL USED, PART NR BAC 1498-139, 33 INCHES LONG. REPAIR ACCOMPLISHED IAW SRM 53 -10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1999071600558 19990716 00558 NM 1999 7 16 USAA069955 1 19990624 A 5210 HOUSING BOEING 727 727225 1384077 NM L-1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 FORWARD ENTRY DOOR HANDLE MECHANISM HOUSING HAS BROKEN ACCESS HOLE EDGES WHERE PUSH ROD PASSES THROUGH CASTING TO TORQUE TUBE. ACCOMPLISHED FORWARD ENTRY DOOR MECHANISM HOUSING REPAIR IAW AVITAS ENGINEERING DRAWING 99AVHM.029D-1. (M) 2 L 7 3 4F A3WE 1999071600559 19990716 00559 NM 1999 7 16 USAA069954 1 19990624 A 5522 SKIN BOEING 727 727225 1384077 NM LT ELEVATOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 LEFT ELEVATOR UPPER SURFACE SKIN GOUGED AND FASTENERS BROKEN, ELEV STATION 123.15 TO 132.15. INSTALLED DOUBLER REPAIR A T LEFT ELEVATOR UPPER SKIN, FROM ELEVATOR STATION 123.15 TO STATION 132.15. MATERIAL USED 2024-T3, .032 INCH, 10.5 INCH BY 7.5 INCH. REPAIR ACCOMPLISHED IAW SRM 55-20-3, FIG 1. (M) 2 L 7 3 4F A3WE 1999071600560 19990716 00560 NM 1999 7 16 USAA069953 1 19990624 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 STRINGER 21R IS CRACKED AT FRAME ATTACH POINTS STATION 460. INSTALLED STRINGER REPAIR AT STRINGER 21R AT FRAME ATTACH P OINTS, STATION 460. MATERIAL USED, CHANNEL, PART NR BAC 1493-412, 10 INCHES LONG, ANGLE; PART NR BAC 1493-513, 10 INCH LONG, STRINGER; PART NR BAC 1498-39, 33 INCHES LONG. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999071600561 19990716 00561 NM 1999 7 16 USAA069952 1 19990624 A 5311 FRAME BOEING 727 727225 1384077 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 FORWARD E/E COMPARTMENT FUSELAGE CIRCUMFERENTIAL FRAME CRACKED AT ATTACHING FASTENERS TO NLG TORQUE BOX VERTICAL STIFFEN ER, LBL 18.6, AT BS 344 JUST ABOVE HORIZONTAL WALKWAY BEAM CHORD. INSTALLED DOUBLER REPAIR AT FORWARD E/E COMPARTMENT, FUSELAGE CIRCUMFERENTIAL FRAME BS 344, LBL 18.6. MATERIAL USED, 7075-T6, .063 INCH, 5.5 INCH BY 12 INCH. REPAIR ACCOMP LISHED IAW SRM 51-10-4 FIG 1. (M) 2 L 7 3 4F A3WE 1999071600562 19990716 00562 NM 1999 7 16 USAA069951 1 19990624 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 400 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 STRINGER 16L, BS 400 DAMAGED. REPAIRED STRINGER AT LEFT BS 400, STRINGER 16L IAW SRM 53-10-3. MATERIAL USED BAC 1498-1 40, 19 INCHES LONG, BAC 1498-131 TWO PIECES 12 INCHES LONG. REPAIR ACCOMPLISHED IAW SRM 51-10-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 1999071600563 19990716 00563 NM 1999 7 16 USAA069950 1 19990624 A 5330 SKIN BOEING 727 727225 1384077 NM BS 400 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 FUSELAGE BS 400, STRIGNER 16L HAS DENT. INSTALLED DOUBLER REPAIR AT LEFT BS 400, MATERIAL USED, 7075-T6, .063 INCH, 21 INCH BY 11 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 1999071600564 19990716 00564 NM 1999 7 16 USAA069949 1 19990624 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1010 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 AFT CARGO COMPARTMENT, BS 1010 FRAME IS CRACKED AT UPPER RADIUS LOCATED BETWEEN STRINGER 26L AND 27L. INSTALLED FRAME R EPAIR AT AFT CARGO COMPARTMENT, BS 1010 FRAME AT UPPER RADIUS, BETWEEN STRINGER 26 AND 27 LEFT. MATERIAL USED, 7075-T6, .063 INCH, 11 INCH BY 4 INCH. REPAIR ACCOMPLISHED IAW SRM 51-10-4 FIG 1. (M) 2 L 7 3 4F A3WE 1999071600565 19990716 00565 NM 1999 7 16 USAA069948 1 19990624 A 5330 SKIN BOEING 727 727225 1384077 NM BS 348.2 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919TS 20447 RIVET HEAD MISSING RIGHT SIDE BETWEEN STRINGER 25R AND 26R AT BS 348.2. INSTALLED DOUBLER REPAIR AT RIGHT BS 348.5, BET WEEN STRINGER 25 AND 26R. MATERIAL USED, 2024-T3, .071 INCH, 12 FT BY 14 INCHES. REPAIR ACCOMPLISHED IAW SRM 53-30-3, FIG 3. (M) 2 L 7 3 4F A3WE 1999071600566 19990716 00566 NM 1999 7 16 USAASB99148 1 19990615 A 3260 806007 LOGIC CARD BOEING 737 7374B7 1384702 NM RT MLG FAILED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 783AU 25022 PHL - FLT 320 - AFTER TAKEOFF FROM RIC, THE RT MLG RED LIGHT REMAINED ILLUMINATED WITH THE GEAR UP. CREW RECYCLED GEAR AND LGIHT EXTINGUISHED. FLIGHT CONTINUED ON TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED LOGIC CARDS M981 (P/N 8-060-02) AND M986 (P/N 65-58250-29) IN THE E11 LANDING GEAR LOGIC SHELF LOCATED IN THE LOWER NOSE COMPT , RT SIDE. METERED BOTH UPLOCK AND DOWNLOCK SENSORS FROM LOGIC SHELF PLUG D2596. CHECKS GOOD. TIGHTENED RIGHT MLG DOO R FOR SAGGING. FURTHERMORE, 4 DAYS LATER ON JUN 19 IN PHL, THE SAME PROBLEM OCCURRED WITH THE RIGHT MLG LIGHT ILLUMINAT ING. THIS TIME, MAINTENANCE REMOVED AND REPLACED LOGIC CARDS M981 AND M982 IN THE E11 LANDING GEAR LOGIC SHELF AND ACCO 2 L 7 2 4F RT A16WE 1999071600567 19990716 00567 NM 1999 7 16 99ZZZM389 1 19990615 A 3260 806002 LOGIC CARD BOEING 737 7374B7 1384702 NM RT MLG FAILED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 783AU 25022 PHL - FLT 320 - AFTER TAKEOFF FROM RIC, THE RT MLG RED LIGHT REMAINED ILLUMINATED WITH THE GEAR UP. CREW RECYCLED GEAR AND LGIHT EXTINGUISHED. FLIGHT CONTINUED ON TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED LOGIC CARDS M981 (P/N 8-060-02) AND M986 (P/N 65-58250-29) IN THE E11 LANDING GEAR LOGIC SHELF LOCATED IN THE LOWER NOSE COMPT , RT SIDE. METERED BOTH UPLOCK AND DOWNLOCK SENSORS FROM LOGIC SHELF PLUG D2596. CHECKS GOOD. TIGHTENED RIGHT MLG DOO R FOR SAGGING. FURTHERMORE, 4 DAYS LATER ON JUN 19 IN PHL, THE SAME PROBLEM OCCURRED WITH THE RIGHT MLG LIGHT ILLUMINAT ING. THIS TIME, MAINTENANCE REMOVED AND REPLACED LOGIC CARDS M981 AND M982 IN THE E11 LANDING GEAR LOGIC SHELF AND ACCO 2 L 7 2 4F RT A16WE 1999071600568 19990716 00568 NM 1999 7 16 USAABB99031 1 19990618 A 3610 312N53217 DUCT BOEING 757 7572B7 1384964 NM RT ENGINE LEAKING A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 EA 19 610AU 27122 PIT - FLT 25 - CREW RECEIVED THE EICAS MESSAGE 'RT ENG OVERHEAT' WITH VISUAL AND AURAL WARNING, WHICH EXTINGUISHED WITH POWER REDUCTION ON THE ENGINE. FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE HP 6 SWIVEL DUCT. (M) 2 L 7 2 4F RT A2NM 1999071600569 19990716 00569 WP 1999 7 16 USAAD99086 1 19990624 A 2161 60714621 CONTROLLER DOUG DC9 DC931 3022065 WP E/E COMPT FAILED A USAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 977VJ 28656 48155 LGA-GSO - FLT 1621 - AFTER TAKEOFF, THE RIGHT AIR CONDITIONING PACK DUCT TEMP INCREASED TO AVOVE 150 DEGREES, CAUSING TH E LAVATORY SMOKE DETECTORS TO ACTIVATE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PL ACED THE RIGHT AIR CONDITIONING AUTO TEMP CONTROL SYSTEM ON MEL AND RELEASED THE AIRCRAFT FOR FLIGHT. DURING OVERNIGHT MAINTENANCE THE RIGHT AIR CONDITIONING AUTO TEMP CONTROLLER WAS REPLACED. (M) 2 L 7 2 4F A6WE 1999071600570 19990716 00570 WP 1999 7 16 USAAD99082 1 19990616 A 2130 PRESSURIZATION DOUG DC9 DC981 3022081 WP CABIN MALFUNCTIONED A USAA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 EA 19 800US 48034 PIT-MSY - FLT 1635 - DURING CLIMB TO 31,000 FT, THE AIRCRAFT WOULD NOT PRESSURIZE USING EITHER PRIMARY, STANDBY, OR MANU AL SYSTEMS. THE CABIN OXYGEN MASKS DEPLOYED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A6WE 1999071600571 19990716 00571 NM 1999 7 16 USAABB99030 1 19990613 A 4920 APU BOEING 757 7572B7 1384964 NM APU COMPT MALFUNCTIONED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 632AU 27810 SFO-PIT - FLT 96 - ABOUT 1 HOUR AFTER TAKEOFF THE APU HAD AN AUTO SHUTDOWN ALONG WITH THE FAULT LIGHT ILLUMINATING AND T HE EICAS MESSAGE APU FAULT LIGHT DISPLAYED. DUE TO ONE ENGINE DRIVEN GENERATOR ALREADY ON MEL THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE PERFORMED A BITE CHECK OF THE APU ECU, NO MESSAGE OR FAULTS WERE NOTED. THE APU WAS STARTED AND RUN FOR 4 HOURS WITH NO AUTO SHUT DOWN. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 1999071600572 19990716 00572 CE 1999 7 16 AMWA005384 1 19990616 A 3230 16001260 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE LANDING GEAR TRIPPED A AMWA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 98YV UE98 ON APPROACH INTO LIT, FLIGHT 5687, WHEN GEAR SELECTED DOWN IT WOULD NOT EXTEND. GEAR WAS MANUALLY EXTENDED AND THE CREW LANDED WITHOUT INCIDENT. LIT MAINTENANCE FOUND THE LANDING GEAR MOTOR C/B POPPED. RESET AND CYCLED THE GEAR SEVERAL T IMES. ALSO, CHECKED FOR CHAFED WIRES BUT NONE WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999071600573 19990716 00573 CE 1999 7 16 AMWA004639 1 19990513 A 5220 12943004519 MECHANISM BEECH 1900 1900D 1154162 CE LT EMER EXIT SERVICEABLE A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 07 174YV 9119 UE174 TO CLEAR BURNING SMELL FROM CKPT ICT MAINTENANCE ATTEMPTED TO OPEN THE LT EMERGENCY EXIT DOOR AND IT WOULD NOT OPEN. AI RCRAFT WAS TAKEN TO ICT HANGAR AND THE DOOR LOCKING MECHANISM WAS LUBED AND ADJUSTED. NO FURTHER INCIDENTS REPORTED. ( M) 2 L 7 2 4T RT A24CE 1999071600574 19990716 00574 CE 1999 7 16 AMWA004638 1 19990513 A 2750 1005240731 FLAP MOTOR BEECH 1900 1900D 1154162 CE TE FLAPS FAILED A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 174YV 653 UE174 FLT 5664 - RTF-ICT - WHEN THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT AND CABIN. AIRCRAFT LANDED WITHOUT INCIDENT. I CT MAINTENANCE REPLACED THE FLAP MOTOR AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4T RT A24CE 1999071600575 19990716 00575 CE 1999 7 16 AMWA003513 1 19990315 A 7933 1303800455 INDICATOR BEECH 1900 1900D 1154162 CE LT OIL TEMP ERRATIC A AMWA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 CE 07 99YV 5134 UE99 FLT 3687 - MSY-LIT - 20 MINUTES INTO FLIGHT THE LEFT OIL TEMP INDICATOR STARTED FLUCTUATING BETWEEN 120 AND 140 DEGREES. A/C RTF IN MSY. THE LEFT ENGINE WAS SHUTDOWN IN FLIGHT. EMERGENCY WAS DECLARED. AIRCRAFT LANDED IN MSY WITHOUT INCI DENT. MAINTENANCE IN MSY SWAPPED GAUGES AND COULD NOT DUPLICATE THE PROBLEM. THEN INSPECTED SYSTEM AND WERE UNABLE TO DUPLICATE PROBLEM. AIRCRAFT RAN AT 85 PERCENT FOR 35 MINUTES ON GROUND WITH NO DISCREPANCIES. PROBLEM LATER OCCURRED F LT 5736 JUST PRIOR TO ARRIVAL IN LIT. HOWEVER, THIS TIME IT FLUCTUATED BETWEEN 60 AND 140 DEGREES LIT MAINTENANCE REPLA CED THE OIL TEMP INDICATOR AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4T RT A24CE 1999071600576 19990716 00576 NM 1999 7 16 USAA990599 1 19990616 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 807 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 30321 23989 TPA - DURNIG CX-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM AFT CARGO DOOR THRESHOLD STATION 807 TO 847, RBB L 13.8. INSTALLED DOUBLER PER EA 64280. (M) 2 L 7 2 4F RT A16WE 1999071600577 19990716 00577 EU 1999 7 16 USAAF99032 1 19990612 A 2720 703852 MANIFOLD FOKKER F28 F28MK0100 4990807 EU RUDDER FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 855US 16665 11283 PIT-TOL - FLT 1045 - AFTER TAKEOFF, THE MFDS MESSAGE 1 INDICATED STAB TRIM CANNEL FAULT NR 1, NR 2, NR 3, YAW DAMPER CHA NNEL NR 1, NR 2, AND 3 RUDDER CHANNEL FAULT NR 2. ALL RESET. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INC IDENT. MAINTENANCE REPLACED THE NR 2 RUDDER MANIFOLD. (M) 2 L 7 2 4F RT 1999071600578 19990716 00578 NM 1999 7 16 USAA069947 1 19990616 A 2910 BACH5P0341CCW HOSE BOEING 727 727225 1384077 NM NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 EA 19 923TS 20441 FLT 6540 - DCA-LGA - HYDRAULIC SYSTEM 'A' FLUID DEPLETED TO ZERO. NORMAL LANDING. FOUND NR 1 ENGINE HYDRAULIC PUMP CAS E DRAIN LINE FROM FIREWALL TO CASE DRAIN FILTER LEAKING. REPLACED LINE. REPLACED NR 1 AND NR 2 'A' SYSTEM CASE DRAIN F ILTERS. (M) 2 L 7 3 4F A3WE 1999071600579 19990716 00579 NM 1999 7 16 EISA99137 1 19990615 A 2781 SWITCH BOEING 727 7272A7 138407K NM LE FLAPS DIRTY A EISA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 310NE 20241 LEADING EDGE FLAPS LIGHT WENT FROM GREEN TO AMBER, F/E PANEL LIGHT NORMAL. CLEANED AND RESET L/E SLAT SWITCH. (M) 2 L 7 3 4F A3WE 1999071600580 19990716 00580 NM 1999 7 16 EISA99129 1 19990523 A 2751 1812993 TRANSMITTER BOEING 727 727223 1384074 NM TE FLAPS SERVICEABLE A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 311NE 19703 DURING CLIMB, WHILE RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES THE OUTBOARD FLAPS LOCKED OUT AT 4 DEGREES, THE INBOARD FLAPS WENT TO 0 DEGREES. CHECKED AND CLEANED CANNON PLUGS ON FLAP POSITION TRANSMITTERS, CLEANED AND LUBED JACKSCREWS, OPS CHECK OK MM 27-52-0. (M) 2 L 7 3 4F A3WE 1999071600581 19990716 00581 NM 1999 7 16 EISA99138 1 19990617 A 3231 65224784 BRACKET BOEING 727 727223 1384074 NM NLG DOOR BROKEN A EISA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 311NE 19703 ON POSITION AND HOLD ON RUNWAY, THERE WAS A LOUD POP FOLLOWED BY NOSE GEAR DOOR LIGHT RETURNED TO GATE. REPLACED NOSE G EAR DOOR BRACKET AND ADJUSTED NOSE GEAR DOORS PER MM 32-22-0. (M) 2 L 7 3 4F A3WE 1999071600582 19990716 00582 NM 1999 7 16 EISA99139 1 19990618 A 3260 65253981 SWITCH BOEING 727 727223 1384074 NM NLG DOOR OUT OF ADJUST A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 311NE 19703 LANDING GEAR DOOR WARNING LIGHT AND NOSE GEAR DOOR WARNING LIGHT ILLUMINATED AT 275 ACCOMPLISHED ABNORMAL CHECKLIST. JA CKED NOSE GEAR, SWUNG GEAR AND ADJUSTED GEAR DOORS PER MM 32-22. (M) 2 L 7 3 4F A3WE 1999071600583 19990716 00583 NM 1999 7 16 EISA99132 1 19990606 A 2197 WIRE BOEING 727 727223 1384074 NM PRESSURE SYSTEM BROKEN A EISA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 311NE 19703 A/C LOST PRESSURIZATION CONTROL. DROPPED TO 10,000 FT AND FLEW TO DFW. REPAIRED BROKEN WIRE ON RIGHT FLOW CONTROL VALV E. (M) 2 L 7 3 4F A3WE 1999071600584 19990716 00584 NM 1999 7 16 EISA99067 1 19990327 A 5754 65162222 SKIN BOEING 727 727223 1384074 NM NR 1 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND SKIN CRACKED ON NR 1 SLAT TRAINING EDGE AREA OUTBOARD SIDE AT O UTBOARD TRACK. REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER PER SRM 57-50-3. INSTALLED REPAIR PER SRM 57-50-3 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999071600585 19990716 00585 NM 1999 7 16 EISA99135 1 19990612 A 2730 260582 INDICATOR BOEING 727 72725 1384006 NM RT ELEV UNSERVICEABLE A EISA O OTHER O OTHER IN INSP/MAINT 1 SW 07 290NE 312 18972 DURING FLIGHT CONTROL CHECK, RT ELEV WOULD NOT INDICATE FULL DEFLECTION IN EITHER DIRECTION. REMOVED AND REPLACED ELEV POSITION INDICATOR IAW MM 31-20-0, NO DEFECTS. (M) 2 L 7 3 4F A3WE 1999071600586 19990716 00586 NM 1999 7 16 EISA99109 1 19990509 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM BS 620-720 INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6815 19490 EMERGENCY EXIT LIGHT IN COCKPIT INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT IN COCKPIT IAW BMM 3350. NO DEFECTS N OTED. (M) 2 L 7 3 4F A3WE 1999071600587 19990716 00587 WP 1999 7 16 EISA99061 1 19990327 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP EMPENNAGE INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 950VJ 47564 FOUND LEFT NACELLE SCANNING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT NACELLE SCANNING LIGHT POWR SUPPLY I AW MM CHAPTER 33-53-0. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999071600588 19990716 00588 1999 7 16 EISA99126 4 19990607 A 2565 73621225 SLIDE DOUG DC9 DC931 3022065 WP TAILCONE FAILED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 FOUND TAILCONE SLIDE WILL NOT HOLD CHARGE. REPLACED TAILCONE SLIDE PER MM 25-62. (M) 2 L 7 2 4F A6WE 1999071600589 19990716 00589 WP 1999 7 16 EISA99125 1 19990605 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP GALLEY DOOR DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 943VJ 47058 GALLEY EMERGENCY SLIDE PACK LIGHT INOPERABLE. REMOVED AND REPLACED GALLEY DOOR EMERGENCY SLIDE PACK LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999071600590 19990716 00590 WP 1999 7 16 EISA99058 1 19990315 A 3350 BATT CHARGER DOUG DC9 DC931 3022065 WP ROW 15-18 FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 943VJ 3115 47058 EMERGENCY TRACK LIGHTING INOPERATIVE. SEAT ROWS 15 TO 18. FOUND DURING SERVICE. REMOVED AND REPLACED AFT BATTERY CHAR GER FOR EMERGENCY LIGHT SYSTEM IAW MM 33-53-0. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999071600591 19990716 00591 WP 1999 7 16 EISA99136 1 19990612 A 3350 079123 LIGHT DOUG DC9 DC931 3022065 WP CABIN BROKEN A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 943VJ 47058 FORWARD RED EMERGENCY LIGHT ON FLOOR LIGHTING BROKEN. REINSTALLED HOUSING ON FORWARD RED EMERGENCY LIGHT ON FLOOR IAW M M CHAPTER 33-53-0. OPS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1999071600592 19990716 00592 NM 1999 7 16 EISA99085 1 19990422 A 2910 RESERVOIR BOEING 727 727223 1384074 NM 'A' HYD SYSTEM REQ'D SERVICE A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6839 20192 LEADING EDGE FLAPS LIGHT ON AFTER TAKEOFF, FLAPS SELECTED UP NR 2 SLAT DID NOT RETRACT. HYDRAULIC QUANTITY FLUCTUATES F ROM 4 TO 2.4 GALLONS. AIR TURN BACK TO BRU. SERVICED AND PURGED 'A' SYSTEM, LEADING FLAPS AND SLATS OPERATED, SYSTEM O PS AND LEAK CHECKS GOOD, 727 MM 27-81-0. (M) 2 L 7 3 4F A3WE 1999071600593 19990716 00593 NM 1999 7 16 EISA99127 1 19990609 A 2424 902F2425 GCU BOEING 727 727231 1384079 NM E/E COMPT FAILED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 74318 20051 NR 1 AND NR 2 GENERATOR UNDER EXCITOR LIGHTS ILLUMINATED, TRIPPED BOTH GENERATORS. REMOVED AND REPLACED NR 2 GCU, OPS C HECK NORMAL. (M) 2 L 7 3 4F A3WE 1999071600594 19990716 00594 1999 7 16 TWAA9909801 4 19990711 A 2330 LIGHT BOEING 767 767231 1385131 NM P5 PANEL FAILED A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 606TW 22569 SMOKE WAS COMING FROM THE PILOTS OVERHEAD PANEL UNTIL THE CIRCUIT BREAKER POPPED. SMOKE WAS FROM A LIGHT PANEL LABELED VIDEO ON. MADE AN UNSCHEDULED LANDING AT PHX. MAINTENANCE DEACTIVATED THE SYSTEM AND THE FLIGHT CONTINUED. CHECK-C 6- 13-99 LAX. *S/D* FINAL CORRECTION WAS REPLACEMENT OF THE LIGHT ASSEMBLY (P/N 434-674-1005-1114) FOR THE VIDEO ON INDIC ATOR LIGHT IN THE (P/N 233T3230-1) PANEL ASSEMBLY ON THE P5 PANEL, EQUIPMENT NUMBER M1111. 2 L 7 2 4F RT A1NM 1999071600595 19990716 00595 NM 1999 7 16 TWAA9909802 1 19990712 A 2611 285N0028136 LOGIC CARD BOEING 767 767231 1385131 NM CARGO COMPT WORN A TWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 05 605TW 22568 EICAS MESSAGES FOR AFT CARGO COMPARTMENT SMOKE DETECTOR NUMBER 2 FLASHED CONTINUOUSLY AND NUMBER 1 DETECTOR FLASHED INTE RMITTENTLY. MADE AN UNSCHEDULED LANDING AT JFK. ON THE GROUND THERE WERE NO MESSAGES. REPLACED THE LOGIC CARD (P/N 85 N0028-136) AND THE NUMBER 2 DETECTOR (P/N 2156-604A). CHECK-C 5-8-99 LAX. 2 L 7 2 4F RT A1NM 1999071600596 19990716 00596 NM 1999 7 16 TWAA9909803 1 19990710 A 3246 29685 BEARING BOEING 757 7572Q8 1384972 NM LT NLG FAILED A TWAA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 CE 05 713TW 28173 DURING TAKEOFF FROM STL, THE LEFT NOSE WHEEL ASSEMBLY SEPARATED FROM THE AIRCRAFT. FLIGHT OPERATED AND LANDED AT MCO WI THOUT INCIDENT. CHECK-C 1-20-99 LAX. INVESTIGATION FOUND THE OUTER BEARING OF THE LEFT NOSE GEAR WHEEL FAILED. THIS C OMPROMISED THE RETENTION OF THE WHEEL AND THE WHEEL DEPARTED FROM THE AIRCRAFT. IN ADDITION TO THE WHEEL ASSEMBLY, THE NOSE GEAR PISTON/AXLE ASSEMBLY HAD TO BE REPLACED DUE TO DAMAGE. 2 L 7 2 4F RT A2NM 1999071600597 19990716 00597 WP 1999 7 16 TWAA9909804 1 19990702 A 5754 SLAT DOUG DC9 DC982 3022082 WP RI WING DAMAGED A TWAA K NONE O OTHER LD LANDING 1 CE 05 918TW 49367 THE RT WING NUMBER 5 SLAT O/B 14 INCHES AND THE SLAT IDLER TRACK CASTING WERE DAMAGED DURING A LANDING INCIDENT. INSTAL LED SERVICEABLE SLAT AND CASTING. CHECK-C 6-4-99 STL. 2 L 7 2 4F A6WE 1999071600598 19990716 00598 WP 1999 7 16 TWAA9909805 1 19990702 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING TORN A TWAA K NONE O OTHER LD LANDING 1 CE 05 918TW 49367 THE RT WING LEADING EDGE SKIN WAS TORN AT THE TOP SIDE DURING A LANDING INCIDENT. REPLACED THE DAMAGED SKIN PER SPM 6-7 0-01. CHECK-C 6-4-99 STL. 2 L 7 2 4F A6WE 1999071600599 19990716 00599 NM 1999 7 16 HNAA9900098 1 19990713 A 2611 82425002009 CABLE DHAV DHC8 DHC8201 2809001 NM BAGGAGE BAY DIRTY A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 998HA 509 BAG BAY SMOKE WARNING LIGHT ON INFLIGHT. INSPECTED SMOKE DETECTOR WIRING, CLEANED AND RESEATED DETECTOR C/P OPS CHECK G OOD. 2 H 7 2 4T RT A13NM 1999071600600 19990716 00600 EA 1999 7 16 JBXA9900091 1 19990713 A 3230 4622 PRIORTY VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG INOPERATIVE A JBXA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 05 578ML 7270 GEAR DISAGREE, 2 NOSE OPEN DOOR MESSAGES ON GEAR RETRACTION. REMOVED AND REPLACED HYDRAULIC PRIORTY VALVE IAW CL-65 MM 32-33-15. PERFORMED FUNCTIONAL CHECK ON PRIORTY VALVE IAW CL-65 MM 32-30-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999071600601 19990716 00601 NM 1999 7 16 RAAA99B1010 1 19990712 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999071600602 19990716 00602 NM 1999 7 16 RAAA99B1011 1 19990712 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 LEFT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999071600603 19990716 00603 NM 1999 7 16 RAAA99B1012 1 19990712 A 5311 FRAME BOEING 727 72722C 138400F NM BS 560 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING TURNAROUND CHECK, FOUND FUSELAGE FRAME TORN AT BS 560 RT BETWEEN STRINGERS 15 AND 16 BY UNKNOWN SOURCE. REPAIRED IAW SRM 51-40-03 FIG 1. 2 L 7 3 4F A3WE 1999071600604 19990716 00604 NM 1999 7 16 CALA9900816 1 19990712 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 660-670 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND A .375 INCH CRACK IN THE RT LOWER KEEL BEAM SKIN PANEL BETWEEN STA 660 AND 670. A REPAIR WAS INSTALLED IAW ECRA 5330-02844. 2 L 7 2 4F RT A16WE 1999071600605 19990716 00605 NM 1999 7 16 CALA9900817 1 19990712 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5 310-03851. 2 L 7 2 4F RT A16WE 1999071600606 19990716 00606 NM 1999 7 16 CALA9900818 1 19990712 A 5320 STIFFENER BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 60312 23363 INSPECTION FOUND CORROSION ON CENTERLINE DOUBLE STIFFENER JUST AFT OF BS 1016 AT BOTTOM OF APB FORWARD SIDE. A NEW CHAN NEL SECTION AND DOUBLERS WERE INSTALLED IAW SRM 53-80-08 AND 51-70-11. 2 L 7 2 4F RT A16WE 1999071600607 19990716 00607 WP 1999 7 16 CALA9900819 1 19990713 A 3350 110049 BATTERY CHARGER DOUG DC9 DC982 3022082 WP SERV DOORWAY INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND TAIL CONE EMERGENCY AISLE PATH LIGHTING INOPERATIVE. THE BATTERY CHARGER AT AFT SERVICE DOOR OVERHEAD PANEL WAS REMOVED AND REPLACED IAW MM 33-50. 2 L 7 2 4F A6WE 1999071600608 19990716 00608 WP 1999 7 16 9902429924 1 19990709 A 2612 FIRE LOOP DOUG DC9 DC932 3022066 WP LT ENGINE DIRTY A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 926RC 47473 LEFT ENGINE FIRE DETECTOR LOOP B-LIGHT ILLUMINATED ON SHORT FINAL. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDE D WITHOUT INCIDENT. MAINTENANCE CHECKED ENGINE DUCTS FOR LEAKS AND CHECKED AND CLEANED ENGINE FIRE LOOPS. NO PROBLEMS WERE FOUND, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999071600609 19990716 00609 WP 1999 7 16 9902439859 1 19990709 A 3260 MODULE DOUG DC9 DC951 3022051 WP RT MLG FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 768NC 47729 LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS CONTINUED TO MSP. RED UNSAFE LIGHT ALSO STAY ED ON DURING GEAR EXTENSION ON LANDING. CREW DECLARED YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENAN CE INSPECTED AND FOUND LEFT MAIN GEAR UNSAFE LIGHT MODULE BAD. REPAIRED MODULE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999071600610 19990716 00610 WP 1999 7 16 9902449977 1 19990708 A 2130 CLAMP DOUG DC9 DC931 3022065 WP TEMP CONTROL VLV MISSING A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 9341 47390 LOSS OF CABIN PRESSURE OCCURRED AT 33,000 FEET WITH CABIN PRESSURE WARNING LIGHT ILLUMINATED. CREW EXECUTED EMERGENCY D ESCENT TO 11,000 FEET. OXYGEN MASKS DID NOT DEPLOY. ENGINE AND WING ANTI-ICE WERE TURNED OFF AND CABIN PRESSURE WAS RE GAINED. AIRCRAFT CLIMBED TO 21,000 FEET AND THE FLIGHT CONTINUTED TO DESTINATION AND UNEVENTFUL LANDING WAS ACCOMPLISHE D. MAINTENANCE FOUND LOOSE AND MISSING CLMAPS AT RIGHT AIR CONDITIONING TEMPERATURE CONTROL VALVE. TIGHTENED AND INSTA LLED CLAMPS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999071600611 19990716 00611 WP 1999 7 16 9902459623 1 19990706 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 623NW 47591 COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999071600612 19990716 00612 WP 1999 7 16 9902469975 1 19990707 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9339 47382 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND REPAIRED BAD WIRE TO CONNECTOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999071600613 19990716 00613 WP 1999 7 16 9902479963 1 19990707 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999071600614 19990716 00614 NM 1999 7 16 9902485513 1 19990706 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM DOOR 2R INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 513US 23201 DURING SCHEDULED MAINTENANCE, THE ESCAPE PATH LIGHT GROUP AT DOOR 2R WOULD NOT RESET PROPERLY. MAINTENANCE REPLACED THE POWER SUPPLY WITH A SERVICEABLE UNIT. SYSTEM TEST WAS SATISFACTORY. 2 L 7 2 4F RT A2NM 1999071600615 19990716 00615 NM 1999 7 16 99FDEA00259 1 19990712 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 148FE 19086 STR 16R IS CRACKED AROUND RIVET HEAD UPPER CHANNEL BS 500. REMOVED AND REPLACED DAMAGED SECTION OF STR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999072000003 19990720 00003 NE 1999 7 20 99ZZZX2537 2 19990615 A 7210 SUN GEAR DHAV DHC3 DHC3 2800202 EA PWA R1340 R1340* 52016 NE GEARBOX FAILED A FYWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AL 05 511BW 5745 649 35 16365 UPON TOUCH DOWN RUN, AT TAKEOFF POWER SETTING, ENGINE RUNNING AT FULL POWER FAILED TO POWER PROPELLER. UPON INVESTIGATI ON, SUN GEAR IN REDUCTION GEARBOX WAS FOUND TO BE IN 3 PIECES. FAILURE DUE TO CRACKED GEAR. REASON FOR CRACKS, UNKNOWN . REPLACED NOSE CASE WITH GEAR REDUCTION ASSY. TEST RAN GOOD. 1 H 7 1 3R 3 R A815 5E2 1999072000005 19990720 00005 EU 1999 7 20 AALA990691 1 19990512 A 3240 BRAKE LINE FOKKER F28 F28MK0100 4990807 EU RT MLG DISCONNECTED A AALA O OTHER O OTHER LD LANDING 1 SW 07 1473K 11515 DFW - FLT 411 - DURING LANDING, THE RIGHT INBOARD BRAKE WOULD NOT RELEASE. AIRCRAFT WAS TAXIED CLEAR OF RUNWAY AND MAIN TENANCE MET THE AIRCRAFT. MAINTENANCE FOUND THE RIGHT INBOARD NR 3 BRAKE LINE UNSEATED. MAINTENANCE RESEATED NR 3 RETU RN BRAKE LINE AND AIRCRAFT TAXIED TO GATE. MAINTENANCE CHECKED NR 3 BRAKE AND HYDRAULIC LINE WITH NO OTHER FAULTS NOTED . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999072000006 19990720 00006 WP 1999 7 20 DLL19991417 1 19990623 A 2612 FIRE WARNING LKHEED 1011 10113853 5265020 WP NR 1 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 768DL 193H1216 INFLIGHT SHUT DOWN A/C. RETURNED TO LAX DUE TO A LOOP FIRE WARNING NR 1 ENGINE. B-LOOP ON DEFERRAL. REPLACED LOWER GE ARBOX LOOP. 2 L 7 3 4F A23WE 1999072100001 19990721 00001 NM 1999 7 21 QXEA9901436 1 19990708 A 6120 GOVERNOR DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF* NE NR 2 ENGINE MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 345PH 476 PCEAG0037 970929 EAT - AFTER TAKEOFF AND GEAR RETRACTION, THE NR 2 ENGINE EXPERIENCED A UNCOMMANDED AUTOFEATHER. NR 1 ENGINE UPTRIMMED T O 110 PERCENT AND NR 2 ENGINE INDICATED 155 PERCENT TORQUE. RETURNED TO EAT AND ACCOMPLISHED A UNEVENTFUL LANDING. AIR CRAFT CURRENTLY DOWN IN EAT FOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999072100002 19990721 00002 NM 1999 7 21 DLM90991524 1 19990706 A 3350 8039491 BATTERY DOUG MD90 MD9030 3023690 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916DN 53396 FOUND EMERGENCY OVERHEAD LIGHTS OUT IN F/C. REPLACED BATTERY PACK. OPS NORMAL. 2 L 7 2 4F RT A6WE 1999072100003 19990721 00003 WP 1999 7 21 TWAA9909705 1 19990702 A 5320 CASTING DOUG DC9 DC982 3022082 WP BS 927 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 DURING CHECK-C MAINT, FOUND FLOORBEAM VERTICAL SUPPORT CASTING CRACKED AT STA 927, RBL 44 INCHES. INSTALLED NEW VERTICA L SUPPORT CASTING AT STA 927, RBL 44 IN, PER SRM 51-30-5. 2 L 7 2 4F A6WE 1999072100004 19990721 00004 EU 1999 7 21 AALA990440 1 19990330 A 3350 502A LIGHT FOKKER F28 F28MK1000 4990808 EU RT LAVATORY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1470K 11506 ORD - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT LIGHT IN RIGHT AFT LAVATORY INOPERATIVE. REPLACED EMERGENCY EX IT LIGHT IN RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A20EU 1999072100005 19990721 00005 NM 1999 7 21 QXEA9901437 1 19990629 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT OUTBOARD SEAT TRACK HAS THREE GOUGES AT AFT CABIN BULKHEAD. REPAIRED IAW DHC-8 SRM 51-70-11. 2 H 7 2 4T RT A13NM 1999072100006 19990721 00006 NM 1999 7 21 QXEA9901438 1 19990627 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT AFT CABIN BULKHEAD. REPAIRED IAW DHC SRM 51-20-16 AND SRM 51-20-3 6. 2 H 7 2 4T RT A13NM 1999072100007 19990721 00007 NM 1999 7 21 QXEA9901439 1 19990630 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CARGO COMPT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT INBOARD SEAT TRACK IN CARGO BAY HAS CORROSION AT AFT TIEDOWN. REPAIRED IAW DHC SRM 51-40-00 AND SRM 51-40-1 1. 2 H 7 2 4T RT A13NM 1999072100008 19990721 00008 NM 1999 7 21 QXEA9901440 1 19990704 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 247 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - CORROSION ON FLANGE OF LEFT-HAND INBOARD SEAT TRACK AT X247. REPAIRED IAW DHC SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999072100009 19990721 00009 NM 1999 7 21 QXEA9901441 1 19990704 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 210 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - CORROSION ON TOP OF RIGHT-HAND INBOARD SEAT TRACK AT X210. REPAIRED IAW DHC SRM 51-40-11, PAGE 6. 2 H 7 2 4T RT A13NM 1999072100010 19990721 00010 NM 1999 7 21 QXEA9901442 1 19990705 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 597 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT INBOARD AFT SEAT TRACK HAS CORROSION IN THE RADIUS AT STATION X597. REPAIRED IAW DHC SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999072100011 19990721 00011 NM 1999 7 21 QXEA9901443 1 19990701 A 2710 MECHANISM DHAV DHC8 DHC8202 2809007 NM AILERON CONTROLS OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - WHILE PERFORMING CHECKS OF THE AILERON CONTROL SYSTEM, FREE PLAY WAS NOTED IN FIRST OFFICERS CONTROL WHEEL WHEN RO LLING FROM LEFT TO RIGHT. REPAIRED IAW HORIZON AIR EA 2-27-18. 2 H 7 2 4T RT A13NM 1999072100012 19990721 00012 NM 1999 7 21 QXEA9901444 1 19990705 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM BS 531.5 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - SUBFLOOR SUPPORT FRAME AND ATTACHING ANGLE ARE CRACKED THROUGH WHERE MOST AFT LEFT INBOARD SEAT TRACK ATTACHED AT STATION X531.500. REPAIRED IAW DHC SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999072100013 19990721 00013 NM 1999 7 21 QXEA9901445 1 19990701 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT INBOARD CENTER SECTION OF SEAT TRACK ON TOP PORTION OF LOWER ATTACH FLANGE AT AFT END DAMAGED. REPAIRED IAW HORIZON AIR EA 2-53-39. 2 H 7 2 4T RT A13NM 1999072100014 19990721 00014 NM 1999 7 21 QXEA9901446 1 19990704 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 597.5 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - FITTING CONNECTIONS TO LEFT INBOARD AFT SEAT TRACK AT STATION 597.500 HAS TOOLING DAMAGE. REPAIRED IAW DHC SRM 51 -40-00. 2 H 7 2 4T RT A13NM 1999072100015 19990721 00015 NM 1999 7 21 QXEA9901447 1 19990704 A 5320 HARDWARE DHAV DHC8 DHC8202 2809007 NM BS 387 IMPROPER PART A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - IMPROPER HARDWARE INSTALLED ON RIGHT INBOARD SEAT TRACK TO FRAME CONNECTION AT STATION X387.0. REMOVED IMPROPER H ARDWARE AND INSTALLED PROPER BOLTS. 2 H 7 2 4T RT A13NM 1999072100016 19990721 00016 NM 1999 7 21 QXEA9901448 1 19990704 A 5320 FASTENER DHAV DHC8 DHC8202 2809007 NM BS 424 IMPROPER PART A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - IMPROPER LENGTH HI-LOKS INSTALLED ON LEFT INBOARD SEAT TRACK TO FRAME CONNECTION AT STATION X424.0. REMOVED AND R EPLACED HI-LOKS WITH CORRECT LENGTH IAW DHC SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999072100017 19990721 00017 NM 1999 7 21 QXEA9901449 1 19990628 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG AFT EDGE OF ACCESS PANEL 261GT. REPAIRED IAW DHC RD8-53-3366. 2 H 7 2 4T RT A13NM 1999072100018 19990721 00018 NM 1999 7 21 QXEA9901450 1 19990630 A 5350 FAIRING DHAV DHC8 DHC8202 2809007 NM WING/FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG AFT EDGE OF CUT OUT FOR WING TO FUSELAGE FAIRING PANEL 261GT. REPAIRED IAW HORI ZON AIR EA 2-37-13. 2 H 7 2 4T RT A13NM 1999072100019 19990721 00019 NM 1999 7 21 QXEA9901451 1 19990630 A 5350 FAIRING DHAV DHC8 DHC8202 2809007 NM WING/FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG AFT EDGE OF CUTOUT FOR WING TO FUSELAGE FAIRING PANEL 261JT. REPAIRED IAW HORIZ ON AIR EA 2-37-13. 2 H 7 2 4T RT A13NM 1999072100020 19990721 00020 NM 1999 7 21 QXEA9901452 1 19990628 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG THE AFT EDGE OF ACCESS PANEL 261JT. REPAIRED IAW DHC RD 8-53-3366. 2 H 7 2 4T RT A13NM 1999072100021 19990721 00021 NM 1999 7 21 QXEA9901453 1 19990628 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG FORWARD AND AFT EDGES OF ACCESS PANEL 261DT. REPAIRED IAW DHC RD 8-53-3366. 2 H 7 2 4T RT A13NM 1999072100022 19990721 00022 NM 1999 7 21 QXEA9901454 1 19990628 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG FORWARD AND AFT EDGES OF ACCESS PANEL 261NT. REPAIRED IAW DHC RD 8-53-3366. 2 H 7 2 4T RT A13NM 1999072100023 19990721 00023 NM 1999 7 21 QXEA9901455 1 19990630 A 5350 FAIRING DHAV DHC8 DHC8202 2809007 NM WING/FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG FORWARD AND AFT EDGES OF CUTOUT FOR WING TO FUSELAGE FAIRING PANEL 261NT. REPAI RED IAW HORIZON AIR EA 2-37-13. 2 H 7 2 4T RT A13NM 1999072100024 19990721 00024 NM 1999 7 21 QXEA9901456 1 19990630 A 5350 PANEL DHAV DHC8 DHC8202 2809007 NM WING/FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG FORWARD AND AFT EDGES OF CUTOUT FOR WING TO FUSELAGE PANEL 261DT. REPAIRED IAW HORIZON AIR EA 2-37-13. 2 H 7 2 4T RT A13NM 1999072100025 19990721 00025 NM 1999 7 21 QXEA9901457 1 19990628 A 5330 PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - THERE IS FRETTING CORROSION ALONG FORWARD AND AFT EDGES OF PANEL 262LT. REPAIRED IAW DHC RD 8-53-3366. 2 H 7 2 4T RT A13NM 1999072100026 19990721 00026 NM 1999 7 21 QXEA9901458 1 19990630 A 5330 PLATES DHAV DHC8 DHC8202 2809007 NM FUSELAGE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - LEFT AND RIGHT GUSTLOCK ASSEMBLY PLATES ARE LOOSE. REPAIRED IAW HORIZON AIR EA 2-55-20 AND RD 8-55-112. 2 H 7 2 4T RT A13NM 1999072100027 19990721 00027 NM 1999 7 21 QXEA9901459 1 19990701 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - CARGO DOOR SKIN CHAFED UPPER AFT CORNER. REPAIRED IAW DHC RD 8-52-21. 2 H 7 2 4T RT A13NM 1999072100028 19990721 00028 NM 1999 7 21 QXEA9901460 1 19990707 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 347PH 480 PDX - FLIGHT ATTENDANT FLASHLIGHT DID NOT TURN OFF WHEN INSERTED INTO CRADLE. REMOVED AND REPLACED FLASHLIGHT WITH A SE RVICEABLE UNIT FROM STOCK. 2 H 7 2 4T RT A13NM 1999072100029 19990721 00029 NM 1999 7 21 QXEA9901461 1 19990703 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM EMPENNAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - RIGHT SIDE OF EMPENNAGE HAS A SCRATCH AND DENT 3.47 INCHES LONG BY 2 INCHES WIDE BY .069 DEEP. FABRICATED AND INS TALLED PATCH PER DHC SRM 53-30-24, PAGE 1-3. 2 H 7 2 4T RT A13NM 1999072100030 19990721 00030 NM 1999 7 21 QXEA9901462 1 19990701 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - INBOARD LOWER SPAR FLANGE HAS CHAFE DAMAGE FROM LOOSE LEADING EDGE. REPAIRED IAW HORIZON AIR EA 8-57-811. 2 H 7 2 4T RT A13NM 1999072100031 19990721 00031 NM 1999 7 21 QXEA9901463 1 19990702 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 347PH 480 PDX - OUTBOARD FLAP, UPPER INBOARD SURFACE BY INBOARD EDGE IS CHAFED. REPAIRED IAW HORIZON AIR EA 2-57-15. 2 H 7 2 4T RT A13NM 1999072300002 19990723 00002 CE 1999 7 23 99ZZZX2631 1 19990702 A 2150 EM608 BLOWER LEAR 35 35LEAR 5170600 CE CARGO BAY SEIZED A FEHA O OTHER O OTHER NR NOT REPORTED 1 SO 13 235EA 12225 994 35061 DURING A FLIGHT, THE CREW NOTICED FAILURE OF THE COCKPIT AIR AND THE CABIN BLOWER CIRCUIT BREAKER WAS EXTENDED. MECHAN IC FOUND THE COCKPIT BLOWER MOTOR HAD SEIZED AND CAUSED THE CABIN BLOWER CIRCUIT BREAKER TO EXTEND. A POSSIBLE SOLUTION WOULD BE A RE-DESIGN OF THE COCKPIT BLOWER MOTOR. 2 L 7 2 4F A10CE 1999072300011 19990723 00011 NE 1999 7 23 99ZZZX2640 1 19990601 A 2710 ROD CONAER LA4 LA4250 5110320 NE AILERON CORRODED A LABA K NONE O OTHER IN INSP/MAINT 1 AL 05 8548Y 107 CORROSION LEFT WING AILERON PUSH/PULL ROD AND ROD END. 2-6-90: DATE OF MFG. TT ON AIRCRAFT: 2,400 HOURS. 1 H 7 1 3O 1A13 1999072300012 19990723 00012 EA 1999 7 23 99ZZZX2641 2 19990526 A 7414 PIN SLICK M3333 PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1G5 41532 EA MAGNETO WORN A LABA O OTHER O OTHER NR NOT REPORTED 1 AL 05 2897X 480 327940187 RL1583748A ENGINE HAS NOTHING BUT SPLASH LUB IN ACCESSORY AREA, AND MAG MOUNTS HIGH ON REAR CASE AND RUNS DRY. INSTALLED ON ENGINE : 10-2-98. CHANGED 5-23-99. 777.2 HRS OFF, 297.4 HRS ON = 479.8 HRS TT. 1 L 7 1 3O 3 O A3SO 1E4 1999072300013 19990723 00013 EU 1999 7 23 99ZZZX2642 1 19990601 A 3250 CONTROL CABLE BNORM BN2 BN2A26 1520226 EU NLG BROKEN A LABA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 05 29884 847 CABLE BROKE WHILE TAXIING TO HANGAR. 7,424 HOURS TT ON AIRFRAME. 1 H 7 2 3O A17EU 1999072300017 19990723 00017 WP 1999 7 23 99ZZZX2646 2 19990621 A 7321 FCU WOODWARD BEECH 18 D18S 1151004 CE GARRTT TPE331 TPE331101B 01514 WP LT ENGINE MALFUNCTIONED A KKFA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 23 502CK 41 916670 A366 P91178C LEFT ENGINE EXPERIENCED GRADUAL 100 HORSEPOWER LOSS. REPLACED LEFT HAND FUEL CONTROL UNIT AND FUEL PUMP WITH SERVICEABL E UNITS. PERFORMED GROUND RUN, LEAK AND PERFORMANCE CHECK IAW GARRETT RUN-UP FROM TTF-0052. 1 L 7 2 3R 3 T A765 E3WE 1999072300018 19990723 00018 WP 1999 7 23 99ZZZX2647 2 19990621 A 7314 FUEL PUMP WOODWARD BEECH 18 D18S 1151004 CE GARRTT TPE331 TPE331101B 01514 WP LT ENGINE MALFUNCTIONED A KKFA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 23 502CK 3398 P10175 A366 P91178C LEFT ENGINE EXPERIENCED GRADUAL 100 HORSEPOWER LOSS. REPLACED LEFT HAND FUEL CONTROL UNIT AND FUEL PUMP WITH SERVICEABL E UNITS. PERFORMED GROUND RUN, LEAK AND PERFORMANCE CHECK IAW GARRETT RUN-UP FROM TTF-0052. 1 L 7 2 3R 3 T A765 E3WE 1999072300034 19990723 00034 CE 1999 7 23 99ZZZX2663 1 19990610 A 2820 VENT CESSNA 208 208B 2073701 CE FUEL SYSTEM CONTAMINATED A L A DEMA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 765FE 208B0259 DEPARTED AUS , FLT 8914 TO SJT/HRL. PILOT REPORTED ON LANDING THAT FUEL PRESS LOW LIGHT CAME ON AND WOULD NOT EXTINGUIS H. MECH OPENED PANELS FOR ACCESS TO RESERVOIR. OPENED DRAIN VALVE FOR THE RESERVOIR, A VACUUM SUCKED AIR INTO FUEL SYS TEM. HE THEN LOOKED AT THE TOP OF WING AND SAID THEY WERE OIL CANNED ON TOP. WHEN FUEL CAPS WERE OPENED,THE SKINS POP PED BACK OUT. MAINT INSTRUCTED HIM TO TRY AND BLOW OUT THE VENT LINES WITH AIR PRESS, HE WAS UNABLE TO DO SO. HE GOT A NITROGEN BOTTLE AND WITH HIGH PRESS WAS ABLE TO BLOW OUT THE VENTS. BOTH VENTS WERE PLUGGED UP ABOUT 12 TO 14 INCHES I NTO THE VENTS BY DIRT DAUBERS, THE ACFT WAS THEN REPOSITIONED BACK TO AUS ON A 91 FLIGHT. 1 H 7 1 3T A37CE 1999072300035 19990723 00035 EU 1999 7 23 AALA990947 1 19990625 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU ROWS 11-15 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1402K 11353 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BETWEEN SEAT ROWS 11 THROUGH 15. REPAI RED WIRING AS REQUIRED BETWEEN SEAT ROWS 11 THROUGH 15. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999072300036 19990723 00036 NM 1999 7 23 AALA990950 1 19990625 A 3350 1001141 LIGHT GRIMES BOEING 727 727227 1384078 NM AFT AIR STAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300037 19990723 00037 NM 1999 7 23 AALA990857 1 19990613 A 3397 WIRE BOEING 727 727223 1384074 NM ROWS 16A-18A LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 712AA 22468 SJU - DURING OVERNIGHT MAINTENANCE, LOWER EMERGENCY EXIT SIGN AT L1, R1, 16A, AND 18A INOPERATIVE. SECURED WIRES ON BAT TERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300038 19990723 00038 NM 1999 7 23 AALA990852 1 19990610 A 3350 TERMINAL BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 892AA 22008 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AFT CABIN INOPERATIVE. REPLACED SEVERAL TERMINAL ENDS ON EMERGENCY EXIT PATH LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300039 19990723 00039 NM 1999 7 23 AALA990851 1 19990610 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 880AA 21519 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AFT CABIN INOPERATIVE. REPAIRED CONNECTOR ON EME RGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300040 19990723 00040 NM 1999 7 23 AALA990853 1 19990610 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT STAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 892AA 22008 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AFT STAIR LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GORUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300041 19990723 00041 NM 1999 7 23 AALA990833 1 19990605 A 3350 BATTERY PACK BOEING 727 727227 1384078 NM CABIN OUT OF POSITION A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729AA 20736 DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERHEAD AIR STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPOSITIONED BATTERY PACK CONTACTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300042 19990723 00042 NM 1999 7 23 AALA990799 1 19990602 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT STAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6823 19701 TPA - DURING OVERNIGHT MAINTENANCE, AFT STAIRS EMERGENCY EXIT LIGHTS OVERHEAD INOPERATIVE. REPLACED EMERGENCY EXIT OVER HEAD LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300043 19990723 00043 NM 1999 7 23 AALA990790 1 19990601 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 879AA 21391 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN FIRST CLASS AND COACH INOPERATIVE. REPAI RED EMERGENCY EXIT FLOOR PATH LIGHTING TRACK CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300044 19990723 00044 NM 1999 7 23 AALA990778 1 19990528 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 880AA 21519 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS BROKEN. REPAIRED FLAT WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300045 19990723 00045 NM 1999 7 23 AALA990775 1 19990527 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 MIA - DURING OVERNIGHT MAINTENANCE, MID-CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE FOR MID-CAB IN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300046 19990723 00046 NM 1999 7 23 AALA990725 1 19990519 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 849AA 20990 DFW - OVERNIGHT MAINTENANCE EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED WIRES TO EMERGENCY EXIT SIGN. SYSTEM GROUND CHEC KED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999072300047 19990723 00047 EU 1999 7 23 AALA990739 1 19990522 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1421K 11404 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT CENTER CEILING PANEL LIGHT INOPERATIVE. REPAIRED WIRES O N FIRST CLASS EMERGENCY EXIT CENTER CEILING PANEL LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999072300048 19990723 00048 NM 1999 7 23 UIEA9947 1 19990702 A 3610 906M87G02 MANIFOLD BOEING 747 747243B 1384830 NM NR 4 ENGINE CRACKED A UIEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 15 516MC 22507 ORD/MXP - FLT AZ9163/02 - DURING CLIMB-OUT AT 4,000 FEET, NR 4 ENGINE NACELLE TEMPERATURES INDICATED 7.6 DEGREES ON BOTH 'A' AND 'B' LOOPS. TEMPERATURE DECREASED WHEN THROTTLE WAS RETARDED. CLOSED BLEED VALVE ACCORDING TO FHB PROCEDURE. A S NR 4 THROTTLE WAS ADVANCED, TEMPERATURE STARTED TO CLIMB. JETTISONED 40,000 KGS OF FUEL. RETURNED TO ORD, LANDING WA S UNEVENTFUL. MAINTENANCE INSPECTION OF NR 4 ENGINE REVEALED A FRACTURED 14TH STAGE BLEED MANIFOLD P/N 906M87G02. MANI FOLD REPLACED. ENGINE RUN-UP CHECKS NORMAL. (X) 2 L 7 4 4F A20WE 1999072300049 19990723 00049 NM 1999 7 23 USAA990595 1 19990617 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 40551 23228 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION AT STRINGER TIE ANGLE BETWEEN STRINGERS 28L AND 28 R STATION 360. FABRICATED AND INSTALLED NEW STRINGER TIE ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999072300050 19990723 00050 NM 1999 7 23 USAA990596 1 19990617 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 40551 23228 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION AT STATION 360 CENTERLINE OF FUSELAGE ON LOWER FRA ME ATTACH ANGLE. FABRICATED AND INSTALLED NEW LOWER FRAME ATTACH ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999072300051 19990723 00051 NM 1999 7 23 USAA990560 1 19990610 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 860 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND 6 CORROSION AT SCREW HOLE IN FLOORBEAM JOGGLE AT BS 860 RBL 8. INSTALLED REPAIR ANGLE PE R TYPICAL REPAIR 53-10-06. (M) 2 L 7 2 4F RT A16WE 1999072300052 19990723 00052 NM 1999 7 23 USAA990604 1 19990621 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION APPROXIMATELY 20 INCH BY 2 INCH UPPER T-CAP AT STA 947, LBL 12 TO RBL 12 FLOORBEAM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. INSTALLED REPLACEMENT T-CAP WITH SP LICE ANGLES AND STRAPS PER TR 53-60-02. (X) 2 L 7 2 4F RT A16WE 1999072300053 19990723 00053 NM 1999 7 23 USAA990605 1 19990621 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK, VISUAL INSPECTION FOUND AN AREA OF CORROSION APPROXIMATELY 2 INCHES BY 6 INCHES UPPER T-CAP AT S TA 967, LBL 30, LBL 5, AND RBL 18 FLOORBEAM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. REPAIRED PER TR-53-15-0 1A AND SRM 53-60-51. (X) 2 L 7 2 4F RT A16WE 1999072300054 19990723 00054 NM 1999 7 23 USAA990628 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK, VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 867 BETWEEN STR 8R AND STR 9R FRAME. (X) 2 L 7 2 4F RT A16WE 1999072300055 19990723 00055 NM 1999 7 23 USAA990627 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 907 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300056 19990723 00056 NM 1999 7 23 USAA990640 1 19990630 A 5320 FRAME BOEING 737 737401 1384701 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT FORWARD SERVICE DOOR CUT-OUT FRAME AT UPPER FORWARD STOP FITTING. REPLACED DOOR FRAME SKIN AND STOP FITTING PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999072300057 19990723 00057 NM 1999 7 23 USAA990639 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-T CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 747 BETWEEN STR 8L AND STR 9L FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300058 19990723 00058 NM 1999 7 23 USAA990638 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 747 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300059 19990723 00059 NM 1999 7 23 USAA990637 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 787 BETWEEN STR 8L AND STR 9L FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300060 19990723 00060 NM 1999 7 23 USAA990636 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 787 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300061 19990723 00061 NM 1999 7 23 USAA990635 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION FOUND A .3750 INCH CRACK AT STA 440 BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300062 19990723 00062 NM 1999 7 23 USAA990634 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 440 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300063 19990723 00063 NM 1999 7 23 USAA990633 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 727G BETWEEN STR 8L AND STR 9L FRAME. INSTALL ED DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300064 19990723 00064 NM 1999 7 23 USAA990631 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECITON, FOUND A.3750 INCH CRACK AT STA 500A BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300065 19990723 00065 NM 1999 7 23 USAA990630 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 480 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300066 19990723 00066 NM 1999 7 23 USAA990629 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 827 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300067 19990723 00067 NE 1999 7 23 USAASB99154 2 19990625 A 7510 DC06F16S1S CONNECTOR BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE BROKEN A USAA A UNSCHED LANDING N M FALSE WARNING OVER TEMP CL CLIMB 1 EA 19 265AU 22962 BWI - FL2700 - FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT INCIDENT DUE TO THE NR 2 ENGINE FUEL HEAT VALVE OPEN L IGHT FLICKERING AND THE NR 2 ENGINE OIL TEMPERATURE RISING SLIGHTLY HIGHER THAN THE NR 1 ENGINE INTO THE YELLOW RANGE. N O ENGINE SHUT DOWN OCCURRED AND NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE GROUND WIRE AT THE NR 2 ENGINE FUEL HE AT VALVE CONNECTOR D1004 BROKEN AT THE PIN. REMOVED AND REPLACED CONNECTOR. PERFORMED ENGINE RUN. FOUND OIL TEMPERATU RES IN GREEN RANGE WITH THE NR 2 ENGINE 10 DEGREES HIGHER THROUGHOUT SETTINGS. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F 4 F A16WE E2EA 1999072300068 19990723 00068 NE 1999 7 23 USAAD99087 2 19990630 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LEFT FAILED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 958VJ 47351 667205 ATL/PIT - FLT 7880 - AFTER ROTATION, THE LEFT ENGINE EGT CONTINUED TO CLIMB TO 600 DEGREES CELSIUS BEFORE ROLLING BACK. THE CREW REDUCED POWER WHEN THE ENGINE EXPERIENCED A COMPRESSOR STALL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED W ITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE. (X) 2 L 7 2 4F 4 F A6WE E2EA 1999072300069 19990723 00069 WP 1999 7 23 USAAD99083 1 19990621 A 3350 41B001TD05G1 BATTERY DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 982VJ 48158 DAY - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE LEFT NACELLE EMERGENCY LIGHT. (X) 2 L 7 2 4F A6WE 1999072300070 19990723 00070 NM 1999 7 23 USAA0679966 1 19990630 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM EMERGENCY EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 926TS 10052 20774 RIGHT FORWARD OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, CHECKS OK. (X) 2 L 7 3 4F A3WE 1999072300071 19990723 00071 WP 1999 7 23 USAAD99085 1 19990622 A 3350 9721062 DIODE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 THE LOW LEVEL EMERGENCY LIGHTS REMAIN ON WHEN THE AIRCRAFT POWER IS TURNED OFF. MAINTENANCE RPELACED THE DIODE AT TERMI NAL STRIP S3-389. (X) 2 L 7 2 4F A6WE 1999072300072 19990723 00072 WP 1999 7 23 USAAD99089 1 19990705 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 977VJ 48155 DTW - THE EMERGENCY LIGHTS AT THE AFT FLIGHT ATTENDANT STATION WERE REMAINING ON DURING THE NORMAL AIRCRAFT ELECTRICAL S YSTEM SHUT DOWN. MAINTENANCE REPLACED THE AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT POWER SUPPLY. (X) 2 L 7 2 4F A6WE 1999072300073 19990723 00073 WP 1999 7 23 USAAD99088 1 19990703 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP PASSENGER DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 970VJ 47050 IND - THE MAIN ENTRANCE DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE MAIN ENTRANCE DOOR SLIDE EMERGENCY LIGHT BATTERY. (X) 2 L 7 2 4F A6WE 1999072300074 19990723 00074 WP 1999 7 23 USAAD99084 1 19990621 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 976VJ 48147 THE SERVICE DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE EMERGENCY LIGHT BATTERY. ( X) 2 L 7 2 4F A6WE 1999072300075 19990723 00075 EU 1999 7 23 USAAF99034 1 19990626 A 5610 D20543405 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU LEFT DELAMINATING A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 862US 5935 11300 BUF - FL 1122 - EN ROUTE PIT/EWR - CREW NOTED SMOKE COMING FROM THE GLARE SHIELD. FLIGHT DIVERTED TO BUF AND LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT WINDSHIELD P1 CONTACT DELAMINATING. THE WINDSHIELD AND HEAT CONTROLL ER WERE CHANGED. (X) 2 L 7 2 4F RT 1999072300076 19990723 00076 EU 1999 7 23 USAAF99035 1 19990626 A 3242 50002683 BRAKES FOKKER F28 F28MK0100 4990807 EU NR 1 DELAMINATED A USAA O OTHER A FLAME/FIRE LD LANDING 1 EA 19 867US 11312 ILM - FLT 573 - DURING LANDING, THE NR 1 BRAKE CAUGHT FIRE. CFR RESPONDED AND EXTINGUISHED THE FIRE. PASSENGERS WERE E VACUATED VIA ESCAPE SLIDE. NO MAJOR INJURIES REPORTED. MINOR INJURIES (SCRATCHES) REPORTED DUE TO EVACUATION. MAINTEN ANCE CARRIED OUT AN INSPECTION OF THE MLG, BRAKES AND CONDUITS PER ENGINEERING INSTRUCTIONS. NO STRUCTURAL OR WIRING CO NDUIT DAMAGE WAS FOUND. THE BRAKES WERE REPLACED. (X) 2 L 7 2 4F RT 1999072300077 19990723 00077 EU 1999 7 23 USAAF99033 1 19990625 A 2121 FAN FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 862US 11300 PIT - FL 591 - ON CLIMB-OUT FROM PIT, CREW NOTED SMOKE COMING FROM BEHIND THE GLARESHIELD. FLIGHT RETURNED TO PIT AND L ANDED WTIH NO FURTHER INCIDENT. MAINTENANCE COULD NOT FIND A DEFINITIVE PROBLEM. BLOWER FAN NR 3 WAS NOTED AS HAVING S OME VIBRATION, AND WAS CHANGED AS A PRECAUTION. (X) 2 L 7 2 4F RT 1999072300078 19990723 00078 EU 1999 7 23 USAAF99028 1 19990523 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU PASSENGER DOORWA BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 857US 11289 RDU - FOUND THE PASSENGER DOOR AND FORWARD SERVICE DOOR EMERGENCY EXIT MARKERS AND FLIGHT COMPARTMENT DOME LIGHT REMAIN ILLUMINATED AT ALL TIMES. AIRCRAFT FERRIED TO PIT WHERE MAINTEANCE REPAIRED A BROKEN WIRE AT THE FORWARD EMERGENCY EXIT LIGHT. (X) 2 L 7 2 4F RT 1999072300079 19990723 00079 NM 1999 7 23 USAA990632 1 19990630 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT STA 727G BETWEEN STR 8R AND STR 9R FRAME. INSTALL ED DOUBLER PER EA 64832 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999072300080 19990723 00080 NM 1999 7 23 9902496631 1 19990520 A 5711 SPAR BOEING 747 747251B 1384892 NM RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING M CHECK, FOUND CRACK IN UPPER CHORD AND WEB HOLE OPENING ON RIGHT WING UPPER MID SPAR NR 3 MAIN FUEL TANK HOLE. R EPAIRED PER EA 66-163365. 2 L 7 4 4F A20WE 1999072300081 19990723 00081 NM 1999 7 23 9902502295 1 19990429 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 1175 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 295US 21506 DURING M CHECK, FOUND CORROSION ON NUT PLATE LOCATION ON 1175 FLOORBEAM. REPAIRED PER EA 22-166634. 2 L 7 3 4F A3WE 1999072300082 19990723 00082 NM 1999 7 23 9902516622 1 19990405 A 5330 SKIN BOEING 747 747251B 1384892 NM CARGO DOORWAY CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 622US 21704 DURING M CHECK, FOUND SKIN CRACKED BELOW AFT CARGO DOOR FORWARD HINGE PIN RETAINER ON AFT LOWER BOLT HOLE. REPAIRED PER EA 66-163356. 2 L 7 4 4F A20WE 1999072300083 19990723 00083 NM 1999 7 23 9902522295 1 19990518 A 5713 STRINGER BOEING 727 727251 138408H NM WS 357 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 295US 21506 DURING M CHECK, FOUND CRACK ON UPPER FORWARD STRINGER AT INBOARD SIDE OF RIGHT WING STATION 357. REPAIRED PER EA 22-166 648. 2 L 7 3 4F A3WE 1999072300084 19990723 00084 WP 1999 7 23 9902541145 1 19990523 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 1512-1517 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER SHELF SUPPORT FITTING OUTBOARD LEG AT FS 1512 - 1517 AT LBL 12. REPAIRED PER EA 11-168288. 2 L 7 3 4F A22WE 1999072300085 19990723 00085 WP 1999 7 23 9902551145 1 19990523 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 1512-1518 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER SHELF SUPPORT FITTING OUTBOARD LEG AT FS 1512-1518 AT RBL 12. REPAIRED PER EA 11-168288. 2 L 7 3 4F A22WE 1999072300086 19990723 00086 WP 1999 7 23 9902561145 1 19990628 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1125 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CORROSION ON LONGERON 48R AT FS 1125. REPAIRED PER EA 168621. 2 L 7 3 4F A22WE 1999072300087 19990723 00087 WP 1999 7 23 9902571145 1 19990624 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 1099 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CRACK IN FORWARD CARGO FLOOR FRAME AT FS 1099, RBL 58. REPAIRED PER EA 11-167242. 2 L 7 3 4F A22WE 1999072300088 19990723 00088 WP 1999 7 23 9902581145 1 19990523 A 5320 SUPPORT DOUG DC10 DC1040 3023508 WP BS 1510 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER LEG SUPPORT AT FS 1510 BETWEEN BL 0 AND LBL 5. REPAI RED PER EA 168288. 2 L 7 3 4F A22WE 1999072300089 19990723 00089 WP 1999 7 23 9902591145 1 19990523 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1512-1518 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER SHELF SKIN AT FS 1512-1518, LBL 11 - LBL 27. REPAIRE D PER EA 11-168288. 2 L 7 3 4F A22WE 1999072300090 19990723 00090 WP 1999 7 23 9902531145 1 19990523 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1510 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CRACK ON SKIN AT FS 1510 BETWEEN LONGERON 50R AND 51R. REPAIRED PER EA 168288. 2 L 7 3 4F A22WE 1999072300091 19990723 00091 WP 1999 7 23 UPS99830088 1 19990701 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2 R/W L/E DOUBLER CRACKED JUST ABOVE NR 4 PYLON. FABRICATED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2 -1A AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999072300092 19990723 00092 WP 1999 7 23 UPS99830090 1 19990706 A 5320 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C-2 FLOORBEAM CORRODED UNDERSIDE AT FS 680 BL 33L TO BL 36L. REPAIRED IAW REO-06602. 2 L 7 4 4F RT 4A25 1999072300093 19990723 00093 WP 1999 7 23 UPS99830091 1 19990709 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 580-660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C3 FLOOR BOARD F88 TO F90 HAS LARGE DOUBLER BULBED BY CORROSION AND EX FOLIATION SHOWING ON UNDERSIDE OF PLANK FABBED AND INSTALLED NEW SECTION AND SPLICES IAW DC8 SRM 53-2-3 FIG 9 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999072300094 19990723 00094 WP 1999 7 23 UPS99830092 1 19990709 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C-2 CORROSION ON MAIN CABIN FLOORBOARD SPLICES (3) STA 1040 X10 TO X17. FABRICATED AND INSTALLED NEW SP LICE IAW DC8 SRM 51-3-0. MAT ID 7075-T 6 .063 PO NR 289791 IAW DC8 SRM 53-7-3, DAC DWG 289791. 2 L 7 4 4F RT 4A25 1999072300095 19990723 00095 WP 1999 7 23 UPS99830093 1 19990704 A 5320 FUSELAGE DOUG DC8 DC873F 302199F WP FS1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2 AFT CARGO PIT STA 1300 6 EA FLOORBOARD SPLICES CORRODED X-38 TO X-20 FABBED AND INSTALLED NEW SPL ICES IAW DC8 SRM 58-1-20 AND DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999072300096 19990723 00096 WP 1999 7 23 UPS99830094 1 19990705 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2 STA 1400 TRACK I SCALLOPS GOUGED. FABRICATED AND INSTALLED NEW SECTION OF CARGO TRACK IAW 51-1-20D, 51-3-0, 53-2-3. MAT ID FOR NEW SECTION OF CARGO TRACK S2772660-13500N, SPO429308. 2 L 7 4 4F RT 4A25 1999072300097 19990723 00097 WP 1999 7 23 UPS99830095 1 19990705 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 255 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK I IS GOUGED AT STA 255. FABRICATED AND INSTALLED PLUG AND CHANNEL IAW DC8 SRM 53-2-3 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999072300098 19990723 00098 WP 1999 7 23 UPS99830096 1 19990705 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 300 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK I IS GOUGED AT STA 300. BLENDED GOUGED AREA, FOUND TO EXCEED LIMITS IAW DC8 SR M 53-2-3. REPAIRED IAW DC8 SRM 53-2-3. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3-0 AND 53-2-3. 2 L 7 4 4F RT 4A25 1999072300099 19990723 00099 NM 1999 7 23 99FDEA00260 1 19990715 A 2612 CONNECTOR BOEING 727 7272S2F 1384O81 NM CARGO COMPT DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 204FE 22926 99-157 - AFT T/O CARGO FIRE IND AT POS 4/5. POS 5 LIGHT STEADY 4 WAS INTERMITTENT. BLEW SENSING LINES FROM ALL 6 SMOKE DETECTORS BACK INTO CABIN. CLEANED CANNON PLUGS ON DETECTORS. SMOKE DETECTION TEST NORM IAW MM 26-16-001-5. 2 L 7 3 4F A3WE 1999072300100 19990723 00100 NM 1999 7 23 99FDEA00261 1 19990713 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 587FE 48489 MAIN DECK AREA - CRACK FOUND ON SEAT TRACK AT STA 635 X = 47.5 LT. CRACK LENGTH APPROX 3.85 IN. *S/D* CRACK AREA TRIM MED OUT AT STA 625 & 645. NEW TRACK REWORKED PER DWG NR NCA 6792. SPLICE HATS REWORK AND SPLICE PLATES FAB AND WEB INS TALLED PER SRM 53-70-00. 2 L 7 3 4F RT A22WE 1999072300101 19990723 00101 1999 7 23 DHL99726001 4 19990713 A 3422 25883024 DG SYST BOEING 727 727228 NM NR 1 FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 726DH 20409 NR 1 COMPASS FLAG, HEADING FLAG IN HSI AND COMPASS FLAG IN NR 2 RMI IN VIEW. REPLACED NR 1 DG. OPS CHECK GOOD PER MM 3 4-21-71. 2 L 7 3 4F A3WE 1999072300102 19990723 00102 NM 1999 7 23 P5CA9900653 1 19990711 A 5330 SKIN BOEING 747 747132 1384882 NM BS 740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FOUND ON SKIN BETWEEN STA 740 AND 760 RIGHT SIDE. CLEANED AND REPAIRED PER SRM 51-10-02 AND 53-30-07. 2 L 7 4 4F A20WE 1999072300103 19990723 00103 NM 1999 7 23 P5CA9900654 1 19990702 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON LAP JOINT STR 23 STA 1820-1780 RIGHT SIDE. CORROSION REMOVED AND REPAIRED PER SRM 51-10-02 AND 53- 30-01. 2 L 7 4 4F A20WE 1999072300104 19990723 00104 NM 1999 7 23 P5CA9900655 1 19990711 A 5330 SKIN BOEING 747 747132 1384882 NM BS 2200-2780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FOUND ON SKIN AT STR 14 BETWEEN STA 2780 AND 2200 AND STA 2240 AND 2280 ON RIGHT SIDE. REMOVED CORROS ION PER SRM 51-00-02 AND 53-30-01. 2 L 7 4 4F A20WE 1999072300105 19990723 00105 NM 1999 7 23 P5CA9900656 1 19990711 A 5330 SKIN BOEING 747 747132 1384882 NM BS 180-200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FOUND ON SKIN BETWEEN STA 180-200 STR 44 RIGHT SIDE. CORROSION REMOVED PER SRM 51-10-02 AND 53-30-01. 2 L 7 4 4F A20WE 1999072300106 19990723 00106 NM 1999 7 23 P5CA9900657 1 19990711 A 5330 SKIN BOEING 747 747132 1384882 NM BS 250-260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SKIN BETWEEN STA 250-260 STR 27 AND 28 LEFT. REMOVED CORROSION PER SRM 51-10-02 AND 53-30-01. 2 L 7 4 4F A20WE 1999072300107 19990723 00107 NM 1999 7 23 P5CA9900658 1 19990713 A 5330 SKIN BOEING 747 747132 1384882 NM WS 235 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON PANEL SKIN BEHIND REAR SPAR WBL 235 LEFT WING. REMOVED RIVETS AND REPAIRED CORROSION PER SRM 57-10 -01. 2 L 7 4 4F A20WE 1999072300108 19990723 00108 NM 1999 7 23 P5CA9900659 1 19990713 A 5512 SKIN BOEING 747 747132 1384882 NM LT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT HORIZONTAL STABILIZER NR 3 ACCESS PANEL 334JB DELAMINATED ON INNER SKIN. REBONDED SKIN TO HONEYCOMB PER SRM 51-10- 06. 2 L 7 4 4F A20WE 1999072300109 19990723 00109 NM 1999 7 23 P5CA9900660 1 19990713 A 5512 SKIN BOEING 747 747132 1384882 NM RT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT HORIZONTAL STABILIZER NR 5 ACCESS PANEL HAS SEVERE AREAS OF DELAMINATION. REBONDED SKIN TO THE HONEYCOMB PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999072300110 19990723 00110 NM 1999 7 23 P5CA9900661 1 19990713 A 5753 SKIN BOEING 747 747123 1384873 NM LT TE FLAP DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEFT OUTBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED DELAMINATION PER SRM 51-40-06. 2 L 7 4 4F A20WE 1999072300111 19990723 00111 NM 1999 7 23 P5CA9900662 1 19990713 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999072300112 19990723 00112 NM 1999 7 23 P5CA9900663 1 19990713 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE MIDFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT INBOARD MID FLAP LEADING EDGE HAS DELAMINATION. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999072300113 19990723 00113 NM 1999 7 23 P5CA9900664 1 19990713 A 5753 SKIN BOEING 747 747132 1384882 NM TE AFT FLAP DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 OUTBOARD AFT FLAP LOWER SURFACE FOUND DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999072300114 19990723 00114 NM 1999 7 23 P5CA9900665 1 19990713 A 5753 SKIN BOEING 747 747132 1384882 NM TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 OUTBOARD FWD FLAP TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999072300115 19990723 00115 NM 1999 7 23 P5CA9900666 1 19990713 A 5522 SKIN BOEING 747 747132 1384882 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT INBOARD ELEVATOR TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999072300116 19990723 00116 NM 1999 7 23 P5CA9900667 1 19990713 A 5512 SKIN BOEING 747 747132 1384882 NM LT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT HORIZONTAL STABILIZER LOWER SURFACE OF TRAILING EDGE NEAR OUTBOARD ELEVATOR FOUND DELAMINATION. REPAIRED PER SRM 5 1-40-09. 2 L 7 4 4F A20WE 1999072300117 19990723 00117 NM 1999 7 23 P5CA9900668 1 19990713 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT WING LEADING EDGE FIXED PANEL DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1999072300118 19990723 00118 NE 1999 7 23 VNAA9907002 2 19990707 A 7210 3038480 GEARBOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT LIGHTNING STRIKE A VNAA K NONE O OTHER CR CRUISE 1 GL 07 436JS 8253 2319 3052 WHILE EN ROUTE TO DCA, THE AIRCRAFT WAS STRUCK BY LIGHTNING. THE FLIGHT CONTINUED ON TO DCA AND LANDED WITHOUT ANY FURT HER PROBLEMS. OUTSTATION MAINTENANCE INSPECTED THE AIRCRAFT AND A FERRY FLIGHT WAS APPROVED TO DAY FOR REPAIRS. DAY MA INTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION PER DORNIER MM 05-51-02. LEFT PROPELLER AND ENGINE GEARBOX WAS REPLAC ED DUE TO DAMAGE FROM THE STRIKE. THE LEFT WING TIP WAS REPLACED AND THE LEFT FLAP RECEIVED A REPAIR AS A RESULT OF DAM AGE FROM THE STRIKE. OPERATION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999072300119 19990723 00119 NM 1999 7 23 VNAA9907005 1 19990712 A 3240 AC69963 METERING UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BRAKE SYST FAILED A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 424JS 7261 14104 3033 THE CREW REPORTED THE AIRCRAFT BRAKES WERE PULSATING AND WOULD NOT STOP THE AIRCRAFT ADEQUATELY. MAINTENANCE INSPECTED AND REPLACED THE BRAKE METERING UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-04. OPERATIONAL CHECKS WERE C OMPLETED AND THE AIRCRAFT WAS RETUNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999072300120 19990723 00120 WP 1999 7 23 TWAA9909901 1 19990712 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND FRAME 911505-5 CRACKED APPROXIMATELY .75 INCH IN RADIUS AT INBD END, STA 83.5 X=10 LEFT SIDE. STOP DRILLED CRACK. REPAIRED PER ARA 13512. 2 L 7 2 4F A6WE 1999072300121 19990723 00121 WP 1999 7 23 TWAA9909902 1 19990712 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND FRAME 911505-5 CRACKED AT INBD END THROUGH RIVET HOLE, TOP LIP JUST AFT OF RADIUS STA 83 .5, X=-10 ON LT SIDE. REF SRM 53-03 PAGE 143. STOP DRILLED CRACK AND REPAIRED PER ARA 13512. 2 L 7 2 4F A6WE 1999072300122 19990723 00122 WP 1999 7 23 TWAA9909903 1 19990712 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CENTER FRAME (9911505-7) CRACKED THROUGH RIVET HOLE AT OTBD END STA 83.5, X=10, LT SIDE JUST AFT OF RADIUS REF SRM 53-03 PAGE 143. INSTALLED NEW FRAME PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999072300123 19990723 00123 WP 1999 7 23 TWAA9909904 1 19990712 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CENTER FRAME (9911505-7) CRACKED THROUGH RIVET AT OTBD END OF STA 83.5, X=-10, LT SIDE U PPER FLANGE JUST AFT OF RADIUS REF SPM 53-03 PAGE 143. INSTALLED NEW FRAME PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999072300124 19990723 00124 WP 1999 7 23 TWAA9909905 1 19990712 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CENTER FRAME (9911505-7) CRACKED .75 INCH LONG IN OTBD END STA 83.5, X=-10 ON RT SIDE. R EF SRM 53-03, PAGE 143 IN RADIUS. INSTALLED NEW FRAME PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999072300125 19990723 00125 WP 1999 7 23 TWAA9909906 1 19990712 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING OP 16 MAINT CHECK, FOUND CENTER FRAME (9911505-7) CRACKED APPROXIMATELY .75 INCH LONG IN RADIUS ON OTBD END, STA 83.5, X=10 ON LT SIDE. INSTALLED NEW FRAME PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999072300126 19990723 00126 WP 1999 7 23 TWAA9909907 1 19990712 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND NOSE HAD CRACK IN PART NBR 5912350-19 DOUBLER APPROXIMATELY .5 INCH FORE AND AFT AT INBD END OF FRAME 9911505-5. FORWARD OF LT CENTER WINDSHIELD POST AT STA 83.5 AT X=-10. INSTALLED NEW PART PER SPM 6-70-01 . 2 L 7 2 4F A6WE 1999072300127 19990723 00127 WP 1999 7 23 TWAA9909908 1 19990712 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CRACK IN P/N 5912350-20 DOUBLER APPROXIMATELY 1.75 INCHES FORE AND AFT AT INBD END OF FR AME 9911505-6. FWD OF RT CENTER WINDSHIELD POST AT STA 83.5, X=-10. REMOVED DOUBLER PER SRO9530268 DRAWING. INSTALLED 912350-92 FILLER AND TITANIUM DOUBLER PER DRAWING SRO 950268. 2 L 7 2 4F A6WE 1999072300128 19990723 00128 WP 1999 7 23 TWAA9909909 1 19990711 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 180-200 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND STATIC BURN AT STA 180 TO 200, LONGERON 4L AND 5L, WAS GROUND BEYOND LIMITS. REPAIRED P ER SRM 53-04, FIG 38 SHEET 18 VIEW E. 2 L 7 2 4F A6WE 1999072300129 19990723 00129 WP 1999 7 23 TWAA9909910 1 19990709 A 5531 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND STA ZPS 52 RIB CRACKED LT LOWER CORNER, STA ZFS 52 RIB CRACKED LOWER CORNER, AND STA ZFS 45 RIB CRACKED IN THE LOWER CORNER. REPAIRED PER SSRM 55-30-02. 2 L 7 2 4F A6WE 1999072300130 19990723 00130 WP 1999 7 23 TWAA9909911 1 19990712 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND COCKPIT VERTICAL STIFFENER 9957860-6, RT SIDE AT APPROXIMATELY 69.5, X=-10, CRACKED IN T HE RADIUS. CRACK APPROXIMATELY 1 INCH LONG. REPLACED THE STIFFENER PER SPM 6-70-01, ITEM 4, B(2)A. 2 L 7 2 4F A6WE 1999072300131 19990723 00131 WP 1999 7 23 TWAA9910001 1 19990715 A 3350 20131 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 27 DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 920TW 49369 THE EGRESS LIGHT AT SEAT ROW 27 WAS REPORTED ILLUMINATED AT ALL TIMES. REPLACED THE EGRESS BATTERY PACK. CHECK-C 6-22- 99 STL. 2 L 7 2 4F A6WE 1999072300132 19990723 00132 NM 1999 7 23 HNAA9900099 1 19990718 A 3350 6104791X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 941HA 161 AFT OVERHEAD DOWN, MID CABIN EXIT AND EXTERIOR AFT LT EGRESS EMERGENCY LTS INOP. REMOVED AND REPLACED POWER SUPPLY. 2 H 7 2 4T RT A13NM 1999072300133 19990723 00133 EU 1999 7 23 JBXA9900092 1 19990717 A 2170 1823505 WATER SEPARATOR FOKKER F28 F28MK0100 4990807 EU NR 1 PACK DIRTY A JBXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 105ML 11475 RIGHT (AIR CONDITIONING) PACK BLOWING HOT AIR ONLY ON CLIMB-OUT, AIR RETURNED TO MCO. (LEFT AIRCONDITIONING PACK INOP U NDER MEL 21-51-1). AIRCRAFT REPOSITIONED TO RDU (CREW ONLY) BOTH PACKS INOP UNDER MEL 21-51-1. REMOVED AND REPLACED NR 1 PACK WATER SEPARATOR ASSEMBLY IAW F-100 AMM 21-51-04. PERFORMED FUNCTIONAL TEST OF NR 2 PACK FLOW CONTROL VALVE IAW F-100 AMM 21-21-01, NO DEFECTS NOTED. REMOVED AND REPLACED NR 2 PACK CONDENSOR BAG IAW F-100 AMM 21-51-04. OPERATIONAL TEST OF BOTH AIR CONDITIONING PACKS GOOD IAW F-100 AMM 21-51-00. 2 L 7 2 4F RT 1999072300134 19990723 00134 WP 1999 7 23 CALA9900820 1 19990714 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1485 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72824 49484 INSPECTION FOUND A .75 INCH CRACK IN LT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE AFT OF VERTICAL REAR SPAR AT STA 14 85. THE ANGLE WAS TRIMMED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 23A. 2 L 7 2 4F A6WE 1999072300135 19990723 00135 NM 1999 7 23 CALA9900821 1 19990707 A 2497 WIRE BOEING 757 757224 1384958 NM NR 2 PYLON CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND GENERATOR FEEDER CABLE CHAFED AGAINST ADJACENT CLAMP AT NR 2 ENGINE PYLON AT WING LEADING EDGE. THE CH AFING CAUSED CONTACT OF WIRE CONDUCTOR TO AIRCRAFT FRAME WITH ARCING DAMAGE TO FEEDER CABLE, CLAMP, AND ATTACH HARDWARE. THE FEEDER WIRE, CLAMP, AND HARDWARE WERE REMOVED AND REPLACED AND THE CLAMP WAS REPOSITIONED TO PROVIDE SUFFICIENT CL EARANCE. 2 L 7 2 4F RT A2NM 1999072300136 19990723 00136 SO 1999 7 23 COMA9910111 1 19990714 A 3260 922AA2YA6PZ SENSOR EMB 120 EMB120RT SO LT MLG FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 263CA 120255 LEFT HAND MLG DISAGREEMENT LIGHT REMAINS ON AFTER GEAR RETRACTED. REPLACED THE UPLOCK PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1999072300137 19990723 00137 EA 1999 7 23 COMA9960367 1 19990706 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280-409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 FLOOR SUPPORT BEAMS RBL27, RBL9, LBL9 AND LBL27 IN AREAS BETWEEN FS 280 AND FS 409 WERE DISCOVERED TO BE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED CORRODED SECTIONS OF FLOORBEAMS RBL9, LBL9, AND LBL27 (BETWEEN FS280 AND FS 40 9) IAW WVAC EO 601R-53-0089. REMOVED AND REPLACED CORRODED SECTION OF FLOORBEAM RBL27 BETWEEN FS 280 AND FS 355 IAW CAN ADAIR REO 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999072300138 19990723 00138 EA 1999 7 23 COMA9960368 1 19990711 A 5311 6003630 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7388 7131 FS 718, STR 11 RHS AFT DOUBLER CRACKED. REPAIRED CRACKED DOUBLER AT FS 718.0 STR 11 RHS IAW WVAC EO 601R-53-0099. 2 L 7 2 4F RT A21EA 1999072300139 19990723 00139 EA 1999 7 23 COMA9960369 1 19990711 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 965CA 7388 7131 FS 718.0, STRI 11 LHS FRAME FLANGE CRACKED AND AFT SIDE OF FRAME DOUBLER CRACKED. REPAIRED CRACKED FRAME FLANGE AND CRA CKED DOUBLER AT FS 718.0 STRI 11 LHS IAW WVAC EO 601R-53-0098 AND WVAC EO 601R-53-0100A. 2 L 7 2 4F RT A21EA 1999072300140 19990723 00140 EA 1999 7 23 COMA9960370 1 19990713 A 2750 601R30043 SELECTOR CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA K NONE O OTHER LD LANDING 1 SO 01 914CA 3763 7012 FLAPS FAILED AFTER LANDING. REPLACED THE FLAP SELECTOR LEVER. 2 L 7 2 4F RT A21EA 1999072300141 19990723 00141 EA 1999 7 23 COMA990371 1 19990702 A 5330 600210325 SKIN CNDAIR CL600 CL6002B19 EA BS 755 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 TAIL SECTION AFT OF EQUIPMENT BAY ACCESS DOOR DAMAGED BY TAIL STAND. LOCATED AND INSTALLED FOLLOWING NEW PARTS LEFT AND RIGHT SKIN PANELS. ALSO REMOVED AND REPLACED DOUBLER P/N 600-21032-9, STRINGER P/N 600-21032-67/GUSSETS P/N 600-21111- 12 AND 11/SKIN ANGLE P/N 600-21022-127 IAW CRJSRM 51-42-06. SEE COMAIR W/O 164828 OR REBAIRE W/O H011 2 L 7 2 4F RT A21EA 1999072300142 19990723 00142 NM 1999 7 23 UPS99230086 1 19990715 A 3260 SWITCH BOEING 727 72727C 138400J NM LT MLG INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 908UP 19114 ATB - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR SAFETY SWITCH AND LINK ASSY, OPS CHECKS GOOD IA W MM 32-09-21 2 L 7 3 4F A3WE 1999072300143 19990723 00143 NM 1999 7 23 UPS99230103 1 19990707 A 5754 RIB BOEING 727 72722C 138400F NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, NR 6 SLAT RIB AT IB SIDE OF ACTUATOR HAS SMALL CRACK IN FWD LOWER RADIUS. RIB REPAIRED IAW SRM 57-50 -3. 2 L 7 3 4F A3WE 1999072300144 19990723 00144 NM 1999 7 23 UPS99230104 1 19990706 A 5320 SUPPORT BOEING 727 72722C 138400F NM BS 1174 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, CORROSION FOUND ON AFT LAVATORY SUPPORT PARTITION FLOOR STRUCTURE BS 1174 LBL 24.75. TOP HAT SECTIO N REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1999072300145 19990723 00145 NM 1999 7 23 UPS99230105 1 19990706 A 5320 SUPPORT BOEING 727 72722C 138400F NM BS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, CORROSION FOUND ON AFT LT LAVATORY PARTITION SUPPORT ON FLOOR STRUCTURE BS 1140 LBL 24.75-LBL60. TOP HAT SECTION REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1999072300146 19990723 00146 NM 1999 7 23 UPS99230106 1 19990708 A 5320 WEB BOEING 727 72722C 138400F NM BS 1130-1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, CORROSION ON SHEAR WEB LBL 24.75 STA 1130-1183. WEB REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999072300147 19990723 00147 NM 1999 7 23 UPS99230107 1 19990709 A 5400 69169274 CLEVIS BOEING 727 72722C 138400F NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, ENGINE NR 2 STRUTS ABOVE NR 2 HORIZONTAL FIRE WALL, CLEVIS CRACKED ON LOWER END OF LOWER STRUT. CLEV IS REPLACED IAW DWG 65-17553. 2 L 7 3 4F A3WE 1999072300148 19990723 00148 NM 1999 7 23 UPS99230108 1 19990705 A 7830 06453010059 BRACKET BOEING 727 72722C 138400F NM NR 3 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, ENGINE NR 3 THRUST REVERSER FAIRING MID SUPPORT BRACKED CRACKED. BRACKET REPLACED IAW MM 78-30-00. 2 L 7 3 4F A3WE 1999072300149 19990723 00149 NM 1999 7 23 UPS99230109 1 19990705 A 7830 06453010059 BRACKET BOEING 727 72722C 138400F NM NR 1 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, ENGINE NR 1 THRUST REVERSER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM 78-30-00. 2 L 7 3 4F A3WE 1999072300150 19990723 00150 NM 1999 7 23 UPS99230110 1 19990706 A 5755 65173527 STIFFENER BOEING 727 72722C 138400F NM NR 4 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, NR 4 SPOILER IB ATTACH VERTICAL LEG CRACKED VERTICAL STIFFENER. REPLACED IAW DWG 69-16201. 2 L 7 3 4F A3WE 1999072300151 19990723 00151 NM 1999 7 23 UPS99430085 1 19990714 A 2780 5150906 MOTOR BOEING 747 747121 1384871 NM NR 2 LE FLAP BAD A IPXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 681UP 19661 LT NR 2 L/E FLAP WOULD NOT RETRACT VIA, THE ALTERNATE METHOD. REPLACED LT NR 2 L/E FLAP ALT DRIVE ELECTRIC MOTOR PER MM 27-81-03. OPS CKS OK. 2 L 7 4 4F A20WE 1999072300152 19990723 00152 NM 1999 7 23 UPS99430101 1 19990716 A 3350 S1356B37 BATTERY BOEING 747 747123F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 REF M-175337: UPPER DECK DOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT BY UPPER DECK DOOR. DEFERRAL REMAINS OPEN DUE TO EXIT LIGHT INOP AT UPPER DECK DOOR. 2 L 7 4 4F A20WE 1999072300153 19990723 00153 NM 1999 7 23 UPS99530098 1 19990711 A 5320 BAC15061108 BEAM BOEING 757 75724APF 1384969 NM BS 900-1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C IN THE MAIN CARGO DECK, THE LONGITUDINAL BEAM AT BS 900-1040 RBL 45 HAS AREAS OF CORROSION AROUND NUT PLATES. CORROSION REMOVAL OUT OF LIMITS IAW SRM 53-00-51. REPLACED LONGITUDINAL BEAM FROM 900-1080 IAW SRM 53-40-51, 5 1-40-02, 51-21-01 , 51-40-05. 2 L 7 2 4F RT A2NM 1999072300154 19990723 00154 NM 1999 7 23 UPS99530099 1 19990711 A 5320 BAC15061108 BEAM BOEING 757 75724APF 1384969 NM BS 1040-1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:C, IN THE MAIN CARGO DECK, THE LONGITUDINAL BEAM RBL 45 HAS AREAS OF CORROSION AROUND NUT PLATES BETWEEN BS 1040-1080. REMOVED CORROSION. REWORK OUT OF LIMITS IAW SRM 53-00-51 PG 101-103. REPLACED LONGITUDINAL BEAM IAW SR M 53-40-51 FIG 1 PG 2-3, 51-40-05 PG 1-2 AND 19, 51-20-04 AND 51-40-02. 2 L 7 2 4F RT A2NM 1999072300155 19990723 00155 WP 1999 7 23 UPS99830089 1 19990701 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2 C CARGO PIT RT TUNNEL STA 1120 FLOORBEAM SUPPORT CORRODED AT NUTPLATE 6 ABOVE LONG 27R. FABRICATED A ND INSTALLED NEW STRUT IAW DC8 SRM 51-3-2 AND 51-1-20. 2 L 7 4 4F RT 4A25 1999072300156 19990723 00156 EU 1999 7 23 QXEA9901466 1 19990714 A 3310 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 493US 11161 PDX - PILOT REPORTS LEFT RED FLOOD BALLAST SMELLS HOT OR BURNING. MAINTENANCE INSPECTED COCKPIT LIGHTING. CHANGED TWO DETERIOATED BULBS. RAN LIGHTS FOR TWO HOURS, NO SMELLS NOTED, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A20EU 1999072300157 19990723 00157 EU 1999 7 23 QXEA9901467 1 19990714 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 498US 2115 11181 BOI - MAINTENANCE REPORTS AFT EXTERIOR LIGHTS DO NOT SHUT OFF WITH SWITCH. REPLACED AFT EMERGENCY POWER SUPPLY. CYCLED LIGHTS: OPERATIONAL CHECK IS NORMAL. 2 L 7 2 4F RT A20EU 1999072300158 19990723 00158 NM 1999 7 23 99FDEA00262 1 19990713 A 5610 5893543095 WINDSHIELD BOEING 727 727233 138408A NM LT COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 222FE 20933 99-158 - DURING CLB L1 WIND STARTED ARCING AND A CRACK DEVELOPED. REMOVED AND REPLACED L1 WINDSHIELD AS PER MM 56/11/01 1/04 AND WINDOW HEAT CONTROL UNIT AS PER MM 30/41/042/5. OP CK GOOD. 2 L 7 3 4F RT A3WE 1999072300159 19990723 00159 NM 1999 7 23 99FDEA00263 1 19990716 A 3260 BULB BOEING 727 727247 138408F NM LT MLG FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 236FE 21330 99-159 - WHEN LAND GEAR 1ST LOWER NO DOWN IND ON LEFT MAIN. REMOVED AND REPLACED BULB. CK PROXIMITY SENSORS PER MM 32- 61, OPS CK NORMAL. 2 L 7 3 4F A3WE 1999072300160 19990723 00160 NM 1999 7 23 99FDEA00264 1 19990716 A 2612 65249203 CONTROL UNIT BOEING 727 72722 1384002 NM APU FAILED A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 149FE 19087 99-160 - DURING DESC, FIRE/WHEEL WELL CARGO SMOKE BELL WENT OFF. REMOVED AND REPLACED WHEEL WELL FIRE DETECTION CONTROL UNIT PERCAUTIONARY. OPS CK GOOD PER MM 26-12-0. ALSO REF MM 26-11-0, 26-15-1, AND 26-17-0. 2 L 7 3 4F A3WE 1999072300161 19990723 00161 EU 1999 7 23 99FDEA00265 1 19990718 A 3411 PITOT AIRBUS 310 A310203 EU LEFT CLOGGED A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 410FE 356 99-161 - REJ T/O AT 90KTS DUE TO NO AIRSPEED IND ON CAPT PFD (SPD TAPE). CLEARED PITOT SYS TUBE WITH AIR AND FOUND BUGS . AIRSPD IND NORM PER A310 MM 34-10-00. AC OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999072300162 19990723 00162 WP 1999 7 23 99FDEA00266 1 19990718 A 3230 TRIM CYLINDER DOUG DC10 DC1030F 3023504 WP LANDING GEAR MALFUNCTIONED A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 308FE 48297 99-162 - GEAR HANDLE WOULD NOT RAISE AFT T/O. RED TAB RAN BUT STILL DID NOT WORK. GOOD HYDS ON ALL 3 SYS. NO PINS FND . BLED/RESET TRIM CYLINDER INTERLOCK FUSE PRECAUTIONARY PER DC-10 MM 32-31-06-2. A/C OK FOR RETURN TO SERVICE. 2 L 7 3 4F RT A22WE 1999072300163 19990723 00163 NM 1999 7 23 DL72E991562 1 19990710 A 5330 655457416 SKIN BOEING 727 727247 138408F NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 FUSELAGE SKIN, FS 481-681, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE B ETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 28 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL SKIN DOUBLER PER ER/A 367751-14AD. 2 L 7 3 4F A3WE 1999072300164 19990723 00164 NM 1999 7 23 DL73K991563 1 19990712 A 7120 654685014 SUPPORT BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 717139 DURING INSP PER OPN 5264, FOUND BUSHING MIGRATED RT FWD ENG MOUNT SUPPORT FITTING. REPLACED SUPPORT FITTING PER EO 03-0 73535-12AD ME-04. FWD MOUNT SUPPORT ASSY PN 713701203. 2 L 7 2 4F 4 F RT A16WE E2EA 1999072300165 19990723 00165 NM 1999 7 23 DL72K991564 1 19990712 A 3350 LIGHT 900542 BOEING 727 727232 1384082 NM L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 276 21586 L2 EMER LIGHT INOP. REPLACED BATTERY PACK. NO HELP. REPLACED BASE. OPS OK NOW. 2 L 7 3 4F A3WE 1999072300166 19990723 00166 NM 1999 7 23 DL72S991565 1 19990712 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN CHAFED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA 22076 EMERGENCY EXIT CONTROL RT CIRCUIT BREAKER POPPED AND WILL NOT RESET. REPLACED WIRE W338-176-18 FROM ABOVE PACK FLOW CON TROL VLV TO ASSY L622 AND REPLACED C/B C267, OPS CK NORMAL. 2 L 7 3 4F A3WE 1999072300167 19990723 00167 NM 1999 7 23 DL757991566 1 19990712 A 3350 0201875003 CONNECTOR BOEING 757 757232 1384965 NM ROW 21 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 SEAT ROW 21 SEAT MOUNTED EMERGENCY LIGHT INOP. REPLACED SEAT HARNESS FOR BROKEN CONNECTOR. 2 L 7 2 4F RT A2NM 1999072300168 19990723 00168 NM 1999 7 23 DL72L991567 1 19990713 A 5310 STRUCTURE BOEING 727 727232 1384082 NM VENTRAL STAIR WE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 THE AFT AIRSTAIR MOUNTING STRUCTURE WAS DAMAGED WHEN THE AIRCRAFT MOVED BACKWARDS WHILE THE AIRSTAIR WAS DOWN AND OPEN. DAMAGED WERE THE LT AND RT SIDE TORQUE BOX WEBS, THE LT AND RT SIDE BEARING DOUBLERS, THE LT AND RT TAIL SKID CAVITY BR ACKETS, THE LT AND RT TAIL SKID CAVITY ANGLES AND THE FUSELAGE SKIN BELOW THE HIGNE POINTS. REPAIRED PER ERA 333311-14, REV C. 2 L 7 3 4F A3WE 1999072300169 19990723 00169 NM 1999 7 23 DL72S991568 1 19990713 A 5313 65584415 STRINGER BOEING 727 727232 1384082 NM BS 990-1010 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 STRINGER 29L WAS FOUND WITH CORROSION IN SEVERAL LOCATIONS FROM APPROXIMATELY STATION 990 TO 1010. NEW SECTION SPLICED IN PER ERA 333339-14, REV A. 2 L 7 3 4F A3WE 1999072300170 19990723 00170 NM 1999 7 23 DL72S991569 1 19990713 A 5313 655848826 STRINGER BOEING 727 727232 1384082 NM BS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 A CRACK WAS FOUND IN S18A RT SIDE AT APPROX BS 950. A NEW SECTION WAS SPLICED IN PER ERA 333330-14, REV A. 2 L 7 3 4F A3WE 1999072300171 19990723 00171 NE 1999 7 23 DLL14991570 2 19990713 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 2 FAILED A DALA A J F UNSCHED LANDING DUMP FUEL ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 SO 27 736DY 33035 193C1227 14783 NR 2 ENGINE IFSD DUE TO FIRE WARNING. FIRED BOTTLES/DUMPED FUEL ATB TO ATL. TROUBLESHOT IN WORK. PREVIOUS DIVERSION F 17/10JUL, ATL/DFW DUE TO SAME PROBLEM. REPLACED ENGINE. 2 L 7 3 4F 4 F A23WE E12EU 1999072300172 19990723 00172 NM 1999 7 23 DL72S991571 1 19990706 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 DURING MV1 CORROSION VISIT, NRC 54 CORROSION ON TOP SURFACE OF FLOORBEAM STA 344 FROM LBL 24 TO RBL 12. REPAIRED PER SR M 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1999072300173 19990723 00173 NM 1999 7 23 DL72K991573 1 19990711 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 720 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FUSELAGE SKIN FS 720A-720B, STRG 4R SKIN LAP SPLICE CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BE TWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 720A AND 720B. THE CRACKS WERE CUTOUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG. 5 AND ER/A 367767-14AD. 2 L 7 3 4F A3WE 1999072300174 19990723 00174 NM 1999 7 23 DL72K991574 1 19990711 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 700-720 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FUSELAGE SKIN FS 700-720, STRG 4R, SKIN LAP SPLICE : CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE B ETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 700 AND 720. THE CRACK WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 367766-14AD. 2 L 7 3 4F A3WE 1999072300175 19990723 00175 NM 1999 7 23 DL72K991575 1 19990711 A 5330 655457415 SKIN BOEING 727 727232 1384082 NM BS 480-500 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FUSELAGE SKIN FS 480-500, STRG 4L, SKIN LAP SPLICE, CRACK REPAIR. HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWE R SKIN OF THE STRINGER 4L LAP SPLICE BETWEEN FS 480 AND 680 INDICATED A SINGLE CRACK BETWEEN FS 480 AND 500. THE CRACK WAS CUTOUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 367765-14 AD. 2 L 7 3 4F A3WE 1999072300176 19990723 00176 NM 1999 7 23 DL72K991576 1 19990711 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FUSELAGE SKIN FS 481-681, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BE TWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 2 9 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUTOUT ALONG THE ENTIRE PANEL AND REPAIRED WITH AN EXTERNAL ALUM INUM DOUBLER PER ER/A 367768-14AD. 2 L 7 3 4F A3WE 1999072300177 19990723 00177 NM 1999 7 23 DL72S991579 1 19990714 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 FOUND AT F-1 LETTER CK, AFT ENTRY WALL LT FRAME HAS .5 INCH VISIBLE CRACK APPROX 6 INCHES BELOW UPPER STOP CASTING. REP AIR PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999072300178 19990723 00178 NM 1999 7 23 DL72S991580 1 19990714 A 5754 651622291 RIB BOEING 727 727232 1384082 NM LT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 LOWER SKIN CUT TO FACILITATE REPAIR OF RIBS. REPAIRED SKIN PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999072300179 19990723 00179 NM 1999 7 23 DL76L991581 1 19990714 A 2560 SLIDE XD4L015 BOEING 767 767332 1382001 NM LT EMER EXIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 182DN 25987 LEFT WING SLIDE SQUIB FAILED TEST NR 1. REPLACED K1 RELAY. 2 L 7 2 4F RT A1NM 1999072300180 19990723 00180 NM 1999 7 23 DL72K991582 1 19990714 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM RT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 415DA 1131 21257 ON L/O, FOUND RT OVERWING EXIT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS NML. 2 L 7 3 4F A3WE 1999072300181 19990723 00181 NE 1999 7 23 DL76S991585 2 19990715 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE DIRTY A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 125DL 23812 24075 580402 ACRID SMOKE SMELL WITH SMOKE DETECTORS GOING OFF ON TAKEOFF TO WT 314,000 LAND WEIGHT 310,000, OVERWEIGHT LANDING, DETEC TORS SOUNDED APPROX THIRTY SECONDS THEN OFF. A/C RETURNED TO GATE. NO VISIBLE SMOKE IN CABIN OR COCKPIT. SMELL DETERM INED COMING FROM BOTHS ENGINES DUE TO COMPRESSOR WASHES. RAN BOTH ENGINES TWENTY MINUTES WITH PACKS ON, NO SMELL OR ODO R NOTICED, NO DETECTORS SOUNDED, NO OVERHEAT INDICATIONS, ALL A/C SYSTEMS OPERATE NORMAL 2 L 7 2 4F 4 F RT A1NM E13NE 1999072300182 19990723 00182 NM 1999 7 23 DL72S991586 1 19990714 A 5330 655457416 SKIN BOEING 727 727232 1384082 NM BS 660-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 FUSELAGE SKIN FS 660-680, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BE TWEEN FS 480 AND 680 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 660 AND 680. THE CRACK WAS CUTOUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUB LER PER B727 SRM 53-30-3, FIG. 5 AND ER/A 367800-14AD. 2 L 7 3 4F A3WE 1999072300183 19990723 00183 NM 1999 7 23 DL72S991587 1 19990714 A 5711 65192922 SPAR BOEING 727 727232 1384082 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 WING CENTER SECTION, REAR SPAR, WEB RBL 10.75 AND LBL 14 CRACK REPAIR. THE CENTER WING REAR SPAR WAS FOUND WITH TWO SMA LL TYPICAL CRACKS NEAR THE UPPER SPAR CAP AT RBL 10.75 AND LBL 14.5. THE CRACKS WERE REMOVED WITH A .25 HOLE AND .625 S LOT RESPECTIVELY. THE CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER ER/A 367797-14AD. 2 L 7 3 4F A3WE 1999072300184 19990723 00184 NM 1999 7 23 DLM88991588 1 19990715 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM BS 427 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DE 49957 A DENT WAS FOUND AT STA 427 BETWEEN L29L AND 30. REPAIRED PER ERA 333340-14, REV A. 2 L 7 2 4F RT A6WE 1999072300185 19990723 00185 NE 1999 7 23 DL73K991589 2 19990715 A 7510 VALVE 320115 BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 311DL 19216 23083 709134 ENGINE OIL TEMP WAS IN THE YELLOW ZONE AROUND 150 DEG C FOR 15 MINUTES. WHEN THE ENGINE WAS IN IDLE THE TEMP WENT UP TO THE RED LINE. REPLACED NR 1 ENGINE FUEL HEAT VALVE (FOUND OPEN/CLOSE IND TANG HANGING UP ON VALVE BODY IN BOTH DIRECTI ONS) PER PFHB DRAINED AND REPLENISHED OIL RESERVOIR. REPLACED MAIN OIL SCREEN. OPERATION AND LEAK CHECK GOOD ON ENGINE RUN. 2 L 7 2 4F 4 F RT A16WE E2EA 1999072300186 19990723 00186 NM 1999 7 23 DL72S991590 1 19990715 A 5753 652163367 SKIN BOEING 727 727225 1384077 NM NR 1 TE MID FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 DURING SHOP INSPECTION, THE THE L/E SKIN WAS FOUND WORN ON THE I/B END OF THE FLAP, APP 6 LONG AREA. REPAIRED PER M/M. 2 L 7 3 4F A3WE 1999072300187 19990723 00187 NM 1999 7 23 DLM88991592 1 19990715 A 3150 WARNING UNIT H05A00354 DOUG MD88 MD88 3023688 NM E/E COMP FAILED A DALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 27 920DE 0771 53423 F/W WILL NOT TEST WHEN BUTTONS ARE PUSHED NO AURAL SOUND NO LIGHTS IN MASTER WARNING MASTER CAUTION. NO LOOP LIGHTS, NO ENGINE FIRE LIGHTS. REPLACED CENTRAL AURAL WARNING UNIT. RAN FIRE WARNING TEST FIRE WARNING TEST OK. 2 L 7 2 4F RT A6WE 1999072300188 19990723 00188 NM 1999 7 23 DL72S991594 1 19990715 A 3242 2114730PT3 BRAKE BOEING 727 727232 1384082 NM NR 1 BRAKE FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 519DA 21470 AFTER TAXI TO RUNWAY, A/C REQUIRED APPROX 1.4 EPR TO INITIATE TAXI. WHEN A/C MOVED A VERY LOUD SHUDDER WAS FELT ON LT S IDE OF A/C. MAINT TOW BACK TO GATE. REPLACED NR 1 BRAKE AND TIRE ASSY DUE NR 1 BRAKE FAILUR. 2 L 7 3 4F A3WE 1999072300189 19990723 00189 WP 1999 7 23 DLL14991595 1 19990715 A 3350 POWER PACK 5165741 LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1739D 54019 193C1237 ON L/O CK, FOUND 1ST CLASS EMERGENCY LIGHTS INOP. REPLACED POWER PACK, OPS CKS OK. 2 L 7 3 4F A23WE 1999072300190 19990723 00190 NM 1999 7 23 SCNA99091 1 19990711 A 3350 BATTERIES BOEING 727 727282 138408T NM AFT AIRSTAIRS DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACE D THE AFT AIRSTAIR EMERGENCY EXIT LIGHT BATTERIES. OPERATIONALLY CHECKS GOOD IAW MM 335071. 2 L 7 3 4F RT A3WE 1999072300191 19990723 00191 SO 1999 7 23 SWIA971512 1 19990709 A 2910 FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 207SW 120266 RIGHT HYDRAULIC FILTER LIGHT ILLUMINATED. RETURNED TO SLC. REPLACED HIGH AND LOW PRESSURE FILTERS ON RIGHT PACK. OPS AND LEAKS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999072300192 19990723 00192 SO 1999 7 23 SWIA971513 1 19990709 A 2752 3203001007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT TE FLAP FAILED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 188SW 120039 FLAP ASYMMETRY AFTER TAKEOFF UPON FLAP RETRACTION. RETURNED TO EKO. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. 2 L 7 2 4T 4 T RT A31SO E20NE 1999072300193 19990723 00193 EA 1999 7 23 SWIA971514 1 19990709 A 5210 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 408SW 7055 AFTER DEPARTURE AIRCRAFT MAIN DOOR HAD LOUD SQUEAL AND AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO SLC. REMOVED AND REP LACED CABIN DOOR SEAL IAW SB 601R-52-067. PRESSURIZED AIRCRAFT AND ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999072300194 19990723 00194 EA 1999 7 23 SWIA971515 1 19990709 A 3230 PIN CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LANDING GEAR NOT REMOVED A SWIA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 NM 07 416SW 7089 GEAR DISAGREE ON DEPARTURE FROM SLC. BURNED FUEL DOWN TO LANDING WEIGHT AND RETURNED TO SLC. FOUND GEAR PIN IN NOSE GE AR. REMOVED PIN. 2 L 7 2 4F 4 F RT A21EA E15NE 1999072300195 19990723 00195 EA 1999 7 23 SWIA971516 1 19990709 A 3020 SENSING ELEMENT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE 14 STAGE DUCT LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 407SW 7034 ON CLIMB-OUT RIGHT 14TH DUCT MSG ILLUMINATED. FOLLOWED QUICK REFERENCE HANDBOOK AND LIGHT EXTINGUISHED WHEN RIGHT 14TH BLEED VALVE WAS CLOSED. RETURNED TO SLC. TORQUED RIGHT 14TH STAGE DUCT SENSING ELEMENT IAW MM 36-21-00. OPS CHECKS GOO D AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 1999072300196 19990723 00196 NE 1999 7 23 SWIA971517 2 19990709 A 7261 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE LOOSE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 297SW 120327 LEFT ENGINE TRAILING SMOKE. RETURNED TO SFO. FOUND OIL IN BREATHER TUBE. REPLACED OIL BREATHER CARBON SEAL. LEFT ENG INE RUN UP OPS CHECKS GOOD IAW MM 72-20-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999072300197 19990723 00197 SO 1999 7 23 SWIA971518 1 19990709 A 3260 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG OUT OF ADJUST A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 227SW 120304 LANDING GEAR LEVER WILL NOT GO INTO UP POSITION UNLESS DOWN LOCK RELEASE BUTTON IS PRESSED. RETURNED TO SLC.ADJUSTED AI R/GROUND PROXIMITY SWITCH ON NOSE STRUT IAW ERAM CMM 32-21-01. SERVICED STRUT. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999072300198 19990723 00198 SO 1999 7 23 SWIA971519 1 19990709 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT TE FLAP FAILED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 193SW 120088 ON CLIMB-OUT GOT A NACELLE FLAP DISAGREEMENT. RESET UNSUCCESSFUL. RETURNED TO RDD. REPLACED LEFT NACELLE FLAP ACTUATO R IAW EMB 120 MM 27-50-03. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999072300199 19990723 00199 SO 1999 7 23 SWIA971520 1 19990709 A 3610 FITTING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT PNEUMATIC SYS DAMAGED A SWIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 188SW 120039 AT 11,000 FEET WE GOT A DUCT LEAK LIGHT. AFTER DOING QUICK REFERENCE HANDBOOK AND WAITING 3 MINUTES THE LIGHT REMAINED ON. BEFORE GETTING ENGINE SHUT DOWN THE LIGHT EXTINGUISHED. RETURNED TO SLC. REMOVED AND REPLACED DAMAGED FITTING TO INLET OF LEFT AIR PRESSURE REGULATOR PER EMB 120 MM 20-10-04. ALSO, REMOVED AND REPLACED LEFT PRESSURE REGULATOR VALVE PER EMB 120 MM 30-10-06. RAN LEFT ENGINE FOR 20 MINUTES HIGH POWER SETTING WITH PACKS ON. OPS CHECK GOOD WITH NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999072300200 19990723 00200 SO 1999 7 23 SWIA971521 1 19990703 A 2150 CLAMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PACK LOOSE A SWIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 217SW 120286 INFLIGHT RIGHT DUCT LEAK LIGHT ILLUMINATED. COMPLIED WITH QUICK REFERENCE HANDBOOK AND LIGHT EXTINGUISHED JUST PRIOR TO ENGINE SHUTDOWN. THE RIGHT BLEED WAS NOT IN USE. REPLACED CLAMP TO RIGHT COOLING TURBINE. RAN PACK AND NO LEAKS WERE NOTED. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999072300201 19990723 00201 NM 1999 7 23 SWAA991184 1 19990713 A 5320 6545409 WEB BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED A1 CHECK, FOUND BEADED PRESS WEB CRACKED, BS 663, LBL 33. REPAIRED WEB PER SWA RA NR1-353-2117. 2 L 7 2 4F RT A16WE 1999072300202 19990723 00202 NM 1999 7 23 SWAA991185 1 19990712 A 5312 6546568 BULKHEAD BOEING 737 7372T4 1384492 NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED RON, FOUND BS 1016, STRINGER 6L AFT BULKHEAD CRACKED. REPAIRED BULKHEAD PER SWA RA NR 1-253-2116. 2 L 7 2 4F A16WE 1999072300203 19990723 00203 NM 1999 7 23 SWAA991186 1 19990712 A 3350 079123 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS FWD TRACK LIGHT OUT OF TRACK. INSTALLED NEW TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999072300204 19990723 00204 NM 1999 7 23 SWAA991187 1 19990711 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS CENTER CABIN LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300205 19990723 00205 1999 7 23 SWAA991188 4 19990711 A 2565 1061323 SLIDE BOEING 737 7373T5 NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300206 19990723 00206 NM 1999 7 23 SWAA991189 1 19990712 A 5311 6551261 FRAME BOEING 737 7373H4 1384600 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED 1/2D CHECK, FOUND LOWER STUB FRAME CRACKED, BS 294, RBL54. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999072300207 19990723 00207 NM 1999 7 23 SWAA991190 1 19990712 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMER EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED C2 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED OVERHEAD EM ERGENCY EXIT LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 1999072300208 19990723 00208 NM 1999 7 23 SWAA991182 1 19990710 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED, BS 727E, STRINGER 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999072300209 19990723 00209 NM 1999 7 23 SWAA991179 1 19990711 A 3260 65C28018 SENSOR BOEING 737 7373H4 1384600 NM NLG MALFUNCTIONED A SWAA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SW 07 301SW 22941 DURING LANDING, NLG UNSAFE LIGHT ILLUMINATED (ACFT DID BY-FLY TO VERIFY NLG DOWN). REMOVED AND REPLACED NLG SENSOR PER MM. 2 L 7 2 4F RT A16WE 1999072300210 19990723 00210 NE 1999 7 23 SWAA991183 2 19990713 A 7320 743602 FCU BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE REQD SERVICE A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 089SW 22904 687780 AIR TURNBACK, NR 1 ENG BEGAN A MINOR THRUST SURGE. THRUST SURGE WENT AWAY WITH REDUCTION OF THRUST. CLEANED NR 1 ENG P S3 AND PS4 MOISTURE TRAPS, SERVICED FCU WITH VERALUBE. PERFORMED ENG STATIC RIG AND TRIM RUN PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999072300211 19990723 00211 NM 1999 7 23 SWAA991172 1 19990711 A 5314 6545866 KEEL BEAM BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED SERVICE CHECK, FOUND CORROSION AND CRACKED KEEL BEAM, BS 500A. REPAIRED KEEL BEAM PER SWA RA NR 1-253- 2115. 2 L 7 2 4F A16WE 1999072300212 19990723 00212 NM 1999 7 23 SWAA991173 1 19990709 A 3150 6545756 WARNING HORN BOEING 737 7372T4 1384492 NM COCKPIT SOUNDED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 722WN 22698 ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED AT APPROX 15 KNOTS INTO THE TAKEOFF. RECYCLED SPEED BRAKES AND FLAPS. OP S CK GOOD PER MM. 2 L 7 2 4F A16WE 1999072300213 19990723 00213 NM 1999 7 23 SWAA991174 1 19990710 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS LIGHTS AND WIRING OUT OF TRACKS. REPAIRED LIGHTS AND WIRING PER MM. 2 L 7 2 4F RT A16WE 1999072300214 19990723 00214 NM 1999 7 23 SWAA991175 1 19990709 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 FWD ENTRY DOOR SLIDE CAME OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300215 19990723 00215 NM 1999 7 23 SWAA991176 1 19990709 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 603SW 27954 FWD ENTRY DOOR SLIDE CAME OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300216 19990723 00216 NM 1999 7 23 SWAA991177 1 19990709 A 2560 D31354 SLIDE BOEING 737 7375H4 138449D NM PASSENGER DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 508SW 24185 FWD ENTRY DOOR SLIDE CAME OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300217 19990723 00217 NM 1999 7 23 SWAA991178 1 19990709 A 3350 100031 LIGHT BOEING 737 7373A4 1384585 NM EMER EXIT DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND RT EMERGENCY EXIT LIGHT ASSY DAMAGED AND UNSECURED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300218 19990723 00218 NM 1999 7 23 SWAA991180 1 19990709 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 793 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, BS 793, RBL 3. REPAIRED BEAM PER SWA RA NR 1-A53-2021. 2 L 7 2 4F RT A16WE 1999072300219 19990723 00219 NM 1999 7 23 SWAA991181 1 19990710 A 5320 BAC1517 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 400-440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND 4 EA SHEAR TIES CRACKED, BS 400 AND 440, STRINGER 14R, BS 460, STRINGER 14L, AND BS 3 60, STRINGER 13L. REPAIRED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 1999072300220 19990723 00220 NM 1999 7 23 TWAA9910101 1 19990716 A 2750 MS93911302E MOTOR BOEING 727 727231 1384079 NM T/E FLAP DRIVE LEAKING A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 64347 21634 THE A-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. MANUALLY EXTENDED THE LANDING GEAR AND RETURNED TO STL. REPLACED THE O/B FLAP DRIVE MOTOR DUE TO LEAKAGE. CHECK-C 8-24-98 MCI. 2 L 7 3 4F A3WE 1999072300221 19990723 00221 NM 1999 7 23 TWAA9910102 1 19990716 A 2612 FIRE LOOP BOEING 767 767231 1385131 NM LT ENGINE FAILED A TWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 604TW 22567 EICAS MSG LT ENG FIRE LP2 AND LT ENG FIRE LP1 DISPLAYED. ALSO FIRE PROT SYS FAIL LIGHT ILLUMINATED. FLIGHT RETURNED T O POP. PLACARDED THE NUMBER 2 LOOP INOPERATIVE PER MEL. NUMBER 1 LOOP CHECKED OK, AND NO LEAKS WERE FOUND. CHECK-C 7- 11-99 LAX. 2 L 7 2 4F RT A1NM 1999072300222 19990723 00222 WP 1999 7 23 TWAA9910103 1 19990707 A 5210 SKIN DOUG DC9 DC983 3022083 WP PASSENGER DOOR BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9625W 53595 THE LT FWD PASSENGER ENTRY DOOR, FORWARD LOWER EDGE OF THE OUTER SKIN, WAS BENT IN 4 INCHES WIDE BY 1 INCH HIGH AND 0.25 IN DEEP. REPAIRED PER SRM 52-03, PAGE 1 ITEM 1 PARAGRAPH A. 2 L 7 2 4F RT A6WE 1999072300223 19990723 00223 NM 1999 7 23 HNAA9900100 1 19990716 A 3350 COVER DHAV DHC8 DHC8102 2809003 NM ROW 4 MISSING A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 162 LOW BULKHEAD EMER LIGHT COVER MISSING RT SIDE ROW 4. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. 2 H 7 2 4T RT A13NM 1999072300224 19990723 00224 NM 1999 7 23 HNAA9900101 1 19990718 A 3350 BATTERY PACK DHAV DHC8 DHC8201 2809001 NM ROW 1 DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 995HA 460 FLOOR EMERGENCY LIGHTS, A/S DOOR EMERGENCY LIGHT AND ROW 1 EMERGENCY LIGHT FLASHING IN FLIGHT. REMOVED AND REPLACED 2 B ATTERY PACKS. 2 H 7 2 4T RT A13NM 1999072300225 19990723 00225 WP 1999 7 23 AT9900494 1 19990714 A 3350 41B004AD073 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 836AT 47397 FOUND FORWARD SERVICE DOOR AREA OVERHEAD EMERGENCY LIGHT DIM. REPLACED BATTERIES ON EMERGENCY DOOR LIGHT, OPS CHECK GOO D IAW MM 33-53-0. 2 L 7 2 4F A6WE 1999072300226 19990723 00226 WP 1999 7 23 CALA9900822 1 19990716 A 5730 ARC063331 PANEL DOUG DC10 DC1010 3022110 WP RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND RT WING LOWER PANEL NR 1 DELAMINATED AT TRAILING EDGE. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 51-31-01, 51-71-00 AND WO 99-0645. 2 L 7 3 4F A22WE 1999072300227 19990723 00227 WP 1999 7 23 CALA9900823 1 19990716 A 5730 ARC02512 PANEL DOUG DC10 DC1010 3022110 WP RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND RT WING UPPER NR 7 PANEL DELAMINATED AT I/B EDGE. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-31-01 AND WO 99-0644. 2 L 7 3 4F A22WE 1999072300228 19990723 00228 WP 1999 7 23 CALA9900824 1 19990716 A 5730 ARC0446503 PANEL DOUG DC10 DC1010 3022110 WP LT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LT WING LOWER PANEL NR 2 DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0643. 2 L 7 3 4F A22WE 1999072300229 19990723 00229 WP 1999 7 23 CALA9900825 1 19990716 A 5512 ALC70644515 PANEL DOUG DC10 DC1010 3022110 WP LT HORIZ STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LT HORIZONTAL STABILIZER 4TH T/E PANEL FROM FUSELAGE GOING O/B DELAMINATED. THE PANEL WAS REMOVED, REP AIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0651 AND TRAVELER 105996. 2 L 7 3 4F A22WE 1999072300230 19990723 00230 WP 1999 7 23 CALA9900826 1 19990716 A 5512 ALC7429452 PANEL DOUG DC10 DC1010 3022110 WP RT HORIZ STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND RT UPPER HORIZONTAL STABILIZER 4TH T/E UPPER AFT PANEL FROM FUSELAGE DELAMINATED. THE PANEL WAS REMOVE D, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0648. 2 L 7 3 4F A22WE 1999072300231 19990723 00231 WP 1999 7 23 CALA9900827 1 19990716 A 5512 ALC7430451 PANEL DOUG DC10 DC1010 3022110 WP LT HORIZ STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LT HORIZONTAL STABILIZER THIRD T/E PANEL FROM FUSELAGE GOING OUTBOARD ON LOWER SURFACE DELAMINATED. TH E PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01AND WO 99-0653. 2 L 7 3 4F A22WE 1999072300232 19990723 00232 WP 1999 7 23 CALA9900828 1 19990716 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 959 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND PILLOWING CORROSION AT LONGERON 49L JUST FORWARD OF ADF DOUBLER AT STA 959. REPAIRED LONGERON 49L IAW SRM 53-10-00, FIGURE 2. 2 L 7 3 4F A22WE 1999072300233 19990723 00233 WP 1999 7 23 CALA9900829 1 19990716 A 5730 ARC0288504 PANEL DOUG DC10 DC1010 3022110 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND RT WING UPPER NR 4 PANEL CORRODED AT THE CENTER OF THE PANEL. THE PANEL WAS REMOVED, REPAIRED AND REIN STALLED IAW SRM 51-31-01 AND WO 99-0660. 2 L 7 3 4F A22WE 1999072300234 19990723 00234 WP 1999 7 23 CALA9900830 1 19990716 A 5730 PANEL DOUG DC10 DC1010 3022110 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND RT WING UPPER NR 6 PANEL CORRODED ON L/E MID PORTION. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01, 51-71-00 AND WO 99-0657. 2 L 7 3 4F A22WE 1999072300235 19990723 00235 WP 1999 7 23 CALA9900831 1 19990716 A 5730 ARC02881H9 PANEL DOUG DC10 DC1010 3022110 WP LT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LT WING UPPER NR 4 PANEL DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-31-01 AND WO 99-0659. 2 L 7 3 4F A22WE 1999072300236 19990723 00236 WP 1999 7 23 CALA9900832 1 19990716 A 5512 ALC72738 PANEL DOUG DC10 DC1010 3022110 WP RT HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND RT HORIZONTAL STABILIZER MOST I/B UPPER L/E AFT SECTION CORRODED UNDER SKIN. REMOVED ACCESS PANEL DOUB LER AND SPLICES. DOUBLERS AND PANEL WERE INSTALLED IAW ECRA 5530-01245 AND SRM 51-31-01. 2 L 7 3 4F A22WE 1999072300237 19990723 00237 WP 1999 7 23 CALA9900833 1 19990716 A 5532 NLC60035 PANEL DOUG DC10 DC1010 3022110 WP VERT STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND VERTICAL STABILIZER L/E PANEL THIRD FROM THE BOTTOM CORRODED. THE CORROSION WAS REMOVED IAW EA 10-5533 -2-A0440 AND ECRA 5533-01001. 2 L 7 3 4F A22WE 1999072300238 19990723 00238 WP 1999 7 23 CALA9900834 1 19990717 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 47-68 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND RT FUSELAGE EXTERNAL SKIN DENTED AT FS 47-68, STRINGER 19R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIG URE 38 AND 51-30-2. 2 L 7 2 4F A6WE 1999072300239 19990723 00239 WP 1999 7 23 CALA9900835 1 19990719 A 5753 SKIN DOUG DC9 DC932 3022066 WP LT T/E FOREFLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND LEFT WING LEFT O/B FOREFLAP DENTED ON LEADING EDGE. THE LEFT O/B FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3. 2 L 7 2 4F A6WE 1999072300240 19990723 00240 SO 1999 7 23 COMA9910112 1 19990701 A 2720 3211001003 PCU EMB 120 EMB120RT SO RUDDER LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 179CA 1179 RUDDER POWER CONTROL UNIT LEAKING HYDRAULIC FLUID. CHANGED RUDDER POWER CONTROL UNIT. 2 L 7 2 4T RT A31SO 1999072300241 19990723 00241 SO 1999 7 23 COMA910113 1 19990717 A 3150 WARNING EMB 120 EMB120RT SO COCKPIT ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 261CA 120254 TRIM INOPERABLE WARNING DURING TAKEOFF. COULD NOT DUPLICATE. RESET SYSTEM AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999072300242 19990723 00242 SO 1999 7 23 COMA9910114 1 19990716 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO ROW 5 DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 189CA 19402 230 120189 EMERGENCY EXIT SIGNS AT ROW 5 ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1999072300243 19990723 00243 EA 1999 7 23 COMA9960372 1 19990716 A 5712 601R5751441 RIB CNDAIR CL600 CL6002B19 EA WS 148 OUT OF LIMITS A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 779CA 7306 AIRCRAFT FOUND TO HAVE ROLL CONDITION UNCOMMANDED DUE TO FLAPS OUT OF RIG. REPAIRED TRAILING EDGE RIB ASSY AT WING STA 148.018 RHS IAW CANADAIR REO 601R-57-51-044, REV A AND CANADAIR REO 601R-57-51-045. 2 L 7 2 4F RT A21EA 1999072300244 19990723 00244 EA 1999 7 23 COMA9960373 1 19990718 A 5330 601R31016 SKIN CNDAIR CL600 CL6002B19 EA BS 310 & 349 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 989CA 7215 FUSELAGE SKIN DAMAGED BY IMPACT WITH PASSENGER DOOR BTM LOCKPINS AT FS 310.00 LHS STR 16 AND FS 349.00 LHS STR 16. PERF ORMED A MAJOR REPAIR TO DAMAGED FUSELAGE SKIN AT FS 310.00 LHS STR 16 IAW CRJ REO 601R-53-21-180 REV NC AND FS 349.00 LH S STR 16 IAW REO 601-53-21-183 REV NC. 2 L 7 2 4F RT A21EA 1999072300245 19990723 00245 EA 1999 7 23 COMA9960374 1 19990717 A 5311 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 7129 WHILE PERFORMING A C1/C2 INSPECTION PART 1 A CRACKED FRAME FLANGE AT FS 718.00 STR 11 LEFT HAND SIDE WAS FOUND. FABRICA TED AND INSTALLED AN ANGLE DOUBLER FROM 2024-0, 0.040 AS PER WVAC EO 601R-53-0102. 2 L 7 2 4F RT A21EA 1999072300246 19990723 00246 EA 1999 7 23 COMA9960375 1 19990717 A 5311 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 7129 WHILE PERFORMING A C1/C2 INSPECTION PART 1 A FRAME FLANGE WAS FOUND TO BE CRACKED AT FS 718.00 STR 11 RIGHT HAND SIDE. F ABRICATED AND INSTALLED AN ANGLE DOUBLER MADE FROM 2024.0, 0.040 AS PER WVAC EO NO 601R-53-0103. 2 L 7 2 4F RT A21EA 1999072300247 19990723 00247 EA 1999 7 23 COMA9960378 1 19990716 A 3610 601R80005 DUCT CNDAIR CL600 CL6002B19 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 LEFT 14TH STAGE BLEED AIR DUCT, UNDER FLOOR PANEL 271 CLF, FS 559 + 48 IS CRACKED. REPLACED DUCT. 2 L 7 2 4F RT A21EA 1999072300248 19990723 00248 EA 1999 7 23 COMA9960379 1 19990710 A 3610 601R800045 DUCT CNDAIR CL600 CL6002B19 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 RIGHT 14TH STAGE BLEED AIR DUCT UNDER FLOOR PANEL 272 CLF FS 559 + 48 IS CRACKED. REPLACED DUCT. 2 L 7 2 4F RT A21EA 1999072300249 19990723 00249 EA 1999 7 23 COMA9960380 1 19990711 A 5751 601R130002 AILERON CNDAIR CL600 CL6002B19 EA RIGHT FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 RIGHT AILERON FAILED BACKLAST CHECK. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1999072300250 19990723 00250 EA 1999 7 23 COMA9960381 1 19990710 A 3350 487191 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947CA 7077 EMERGENCY TRACK LIGHTING AFT CONNECTOR IS BROKEN. REPLACED CONNECTOR. 2 L 7 2 4F RT A21EA 1999072300251 19990723 00251 EA 1999 7 23 COMA9960382 1 19990711 A 3350 BF10011101 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 716CA 7250 ONE BULB IN CENTER CABIN EMERGENCY SIGN IS INOPERABLE. REPLACED SIGN. 2 L 7 2 4F RT A21EA 1999072300252 19990723 00252 EA 1999 7 23 COMA9960383 1 19990716 A 5210 HANDLE CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF ADJUST A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 929CA 7035 DOOR OUTER HANDLE WARNING AFTER TAKEOFF. ADJUSTED DOOR HANDLE SPRING TENSION. 2 L 7 2 4F RT A21EA 1999072300253 19990723 00253 EA 1999 7 23 COMA9960384 1 19990718 A 2750 860D10018 FECU CNDAIR CL600 CL6002B19 EA T/E FLAPS MALFUNCTIONED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 785CA 7326 FLAPS FAIL MESSAGE. REPLACED FECU. 2 L 7 2 4F RT A21EA 1999072300254 19990723 00254 EA 1999 7 23 COMA9960385 1 19990715 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 989CA 7215 EMERGENCY FLOOR LIGHT AT CABIN ENTRANCE IS INOPERABLE. REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 1999072300255 19990723 00255 EA 1999 7 23 COMA9960376 1 19990717 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 7640 7129 FRAME AT FS 718 RHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 4 INCHES ABOVE STRINGER 11 IN TH E FLANGE ATTACHING TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING TO THE FIRST FASTENER HOLE BELOW STRINGER 11. A LSO, THE DOUBLER ON THE AFT SIDE OF FRAME FS 718 AND STRINGER 11 IS CRACKED APPROXIMATELY 2 INCHES. PERFORMED A MAJOR R EPAIR TO CRACKS IN FRAME FS 718 RHS STRINGER 11 IAW WVAC EO 601R-53-0103 AND REPLACED CRACKED DOUBLER AT AFT SIDE OF FRA ME FS 718 RHS STRINGER 11 IAW WVAC EO 601R-53-0105. 2 L 7 2 4F RT A21EA 1999072300256 19990723 00256 EA 1999 7 23 COMA9960377 1 19990717 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 964CA 7129 FRAME AT FS 718 LHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 1 INCH ABOVE STRINGER 11 IN THE FLANGE ATTACHING TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING TOWARD THE FIRST FASTENER HOLE BELOW STRINGER 11. ALSO, THE DOUBLER ON THE AFT SIDE OF FRAME FS 718 LHS AT STRINGER 11 IS CRACKED APPROXIMATELY 4 INCHES. PERFORMED A MA JOR REPAIR TO CRACKS IN FRAME FS 718 LHS STRINGER 11 IAW WVAC EO 601R-53-0102 AND REPLACED CRACKED DOUBLER AT AFT SIDE O F FRAME FS 718 LHS STRINGER 11 IAW WVAC EO 601R-53-010. 2 L 7 2 4F RT A21EA 1999072300257 19990723 00257 NM 1999 7 23 UPS99230112 1 19990706 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C, CRACKS NOTED IN BS 1183, LBL 18 DOOR FRAME. ONE CRACK AT NR 7L DOOR STOP CUTOUT AND THE OTHER CRACK AT 2 FWD OF NR 7L DOOR STOP CUTOUT. ACCESSED AREA AT 1183 FRAME AND REPAIRED FRAME IAW SB B727-53-0210. 2 L 7 3 4F A3WE 1999072300258 19990723 00258 NM 1999 7 23 UPS99230113 1 19990713 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 358 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BS 358, LBL 23, WL 208. REMOVED CORROSION IN A 2' X 8 AREA, REMOVED .038 FROM ORIGINAL THICKNESS OF .100 FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA OF SEAT TRACK, FABRICATED NEW SECTION O F TRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-5, SRM 51-30-2. 2 L 7 3 4F A3WE 1999072300259 19990723 00259 NM 1999 7 23 UPS99230116 1 19990709 A 5543 SKIN BOEING 727 72722C 138400F NM RUDDER TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, RUDDER LOWER TAB DELAMINATED AT UPPER T/E LEFT SIDE PREVIOUS REPAIR. REPAIRED IAW SRM 51-40-10 FIG 3 . 2 L 7 3 4F A3WE 1999072300260 19990723 00260 EU 1999 7 23 UPS99230117 2 19990709 A 7510 DUCT BOEING 727 72722C 138400F NM RROYCE TAY TAY65154 EU NR 3 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, ENGINE NR 3 ANTI-ICE DUCT CRACKED AT BRACKET NEAR ANTI-ICE VALVE. DUCT REPAIRED PER SMRO EO 99-17-00 5 (UPS ENGINEERING FILE NR 727-30- 0009). 2 L 7 3 4F 4 F A3WE E25NE 1999072300261 19990723 00261 NM 1999 7 23 UPS99230118 1 19990707 A 7120 MOUNT BOEING 727 72722C 138400F NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, CORROSION FOUND ON NR 3 ENG FWD MOUNT HOLES AT TRUNNION FITTING ATTACH (PITTING CORROSION). REPAIRED IAW SRMO EO 99-17-003 (UPS ENGINEERING FILE NR 727-54-0089). 2 L 7 3 4F A3WE 1999072300262 19990723 00262 NM 1999 7 23 UPS99230119 1 19990707 A 7120 MOUNT BOEING 727 72722C 138400F NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, CORROSION FOUND ON NR 1 ENG, FWD MOUNT HOLE AFT I/B HOLE ONLY (PITTING CORROSION). INVESTIGATED AND REPAIRED IAW SMRO EO 99-17-002 UPS ENGINEERING FILE NR 727-54-0088. 2 L 7 3 4F A3WE 1999072300263 19990723 00263 NM 1999 7 23 UPS99230120 1 19990708 A 5520 BALANCE PANEL BOEING 727 72722C 138400F NM NR 5 ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, NR 5 ELEVATOR BALANCE PANEL RT HAS EVIDENCE OF CORROSION ON PANEL TO HINGE ATTACH RACK. CORROSION RE MOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-6. BALANCE PANEL REPLACED AND INSTALLED IAW MM 27-30-21. 2 L 7 3 4F A3WE 1999072300264 19990723 00264 NM 1999 7 23 UPS99230121 1 19990706 A 5412 FIREWALL WEB BOEING 727 72722C 138400F NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, STRUCTURE OVER NR 2 ENGINE HORIZ FIREWALL LEFT AND RIGHT WEBS AT BS 1376 ARE CRACKED. FABRICATED AND INSTALLED WEBS IAW DRG NR 65-17555. 2 L 7 3 4F A3WE 1999072300265 19990723 00265 NM 1999 7 23 UPS99230123 1 19990705 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 420 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, ON REMOVAL OF DENTED SKIN, STRINGER FOUND DAMAGED. REPLACED DAMAGED STRINGER SECTION IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999072300266 19990723 00266 NM 1999 7 23 UPS99230124 1 19990707 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 850 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:C, FLOOR SUPPORT CRACKED BS 850 LBL 45.5. FLOOR SUPPORT ANGLE REPAIRED IAW SRM 57-20-1. 2 L 7 3 4F A3WE 1999072300267 19990723 00267 NM 1999 7 23 UPS99430122 1 19990719 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM CREW DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:N/A, EMERGENCY LIGHTS AT CREW SERVICE DOORS INOP. REPLACED BATTERY PACK AT M312 CHARGER PER MM 33-51-04 , INCLUDING CHARGING VOLTAGE AND GROUND. 2 L 7 4 4F A20WE 1999072300268 19990723 00268 NM 1999 7 23 99FDEA00267 1 19990715 A 5313 65C197195 STRINGER BOEING 727 7272S2F 1384O81 NM BS 1013 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 GOUGE IN STRINGER CHANNEL AT 23 RT, BS 1013. *S/D* REPAIRED STR IAW FEDEX EA 7-5310-46927. 2 L 7 3 4F A3WE 1999072300269 19990723 00269 WP 1999 7 23 ABXA9900568 1 19990716 A 3350 41B004AD0763 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928AX 47392 EMERGENCY LIGHTS WOULD NOT ARM. CAME ON INITIALLY, THEN FADED. REPLACED BATTERIES, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999072300303 19990723 00303 NE 1999 7 23 99ZZZX2697 2 19990206 A 7230 COMPRESSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE BLADE FAILED A A6WA E ENGINE SHUTDOWN J E WARNING INDICATION VIBRATION/BUFFET NR NOT REPORTED 1 GL 31 607AW E2052 DEN - FLT 595 - NR 1 ENGINE: VIBRATION 2.5 AIR-BORN. ENGINE SHUT DOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLA DES MISSING FROM NR 3 AND NR 4 WHEEL AND DAMAGE TO NR 2 WHEEL AND SUSPECT DAMAGE TO NR 1 WHEEL. AIRCRAFT TO BE FERRIED TO ATW. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. 2 H 7 4 4F 4 F RT A49EU E6NE 1999072300304 19990723 00304 EU 1999 7 23 99ZZZX2698 1 19990123 A 3233 PIN BAG BAE146 BAE146200A 1500266 EU NLG ACTUATOR FAILED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 607AW E2052 UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK, FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR E.O. E98/002/632. REMOVED AND REPLACED THE NLG RETRACTION JACK PIN AS REQUIRED DURING REMOVAL AND REPLACMENT OF JACK ST REET. ACFT TT: 23,562 HOURS. ACFT TC: 33,928. 2 H 7 4 4F RT A49EU 1999072300305 19990723 00305 1999 7 23 99ZZZX2699 4 19990113 A 2565 D31050103 SLIDE BAG BAE146 BAE146300A 1500267 EU PASSENGER DOOR LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 615AW 16754 0576 E3141 MKE - FLT 619 - RIGHT FORWARD EVACUATION SLIDE NEAR DEPLOYMENT. REMOVED AND REPLACED SLIDE. 2 H 7 4 4F RT A49EU 1999072300306 19990723 00306 EU 1999 7 23 99ZZZX2700 1 19990101 A 2560 D31050105 SLIDE BAG BAE146 BAE146100A 1500260 EU PASSENGER DOOR DEPLOYED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP 23503 0238 E1063 ORD - FLT 545 - WHILE INSPECTING GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR, SLIDE PARTIALLY DEPLOYED. REMOVED AND RE PLACED FORWARD PASSENGER DOOR SLIDE IAW MM. 2 H 7 4 4F RT A49EU 1999072300307 19990723 00307 EU 1999 7 23 99ZZZX2701 1 19990106 A 3260 200876314 BRACKET BAG BAE146 BAE146200A 1500266 EU NLG BROKEN A A6WA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 31 181US E2042 ORD - FLT 526 - NOSE GEAR SQUAT SWITCH SENSOR BROKEN OFF FROM ATTACH POINT. REMOVED AND REPLACED NOSE LANDING GEAR SQUA T SWITCH SENSOR HARNESS AND MOUNTING BRACKET IAW MM. 2 H 7 4 4F RT A49EU 1999072300308 19990723 00308 EU 1999 7 23 A6WA9900024 1 19990106 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU FRAME 29 CRACKED A A6WA O OTHER O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FRAME 29 MLG BAY ROOF LONGERONS CRACKED, NR 3 AND NR 15, NEAR FORWARD ENG. REPAIRED PER BAE REPAIR DRAWING HC536H9211. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300309 19990723 00309 EU 1999 7 23 A6WA9900022 1 19990110 A 5210 ANGLE BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FORWARD PASSENGER DOOR HAS 2 EACH CRACKED ANGLES IN THE HANDLE BOX AREA. MFG AND REPLACED PER BAE DRAWINGS HC521H0507 A ND HC521H0508. INSTALLED ANGLES PER SRM AND BAE FAX DJR/RJ0049-97. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300310 19990723 00310 EU 1999 7 23 A6WA9900039 1 19990418 A 2560 GIRT BAR BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR DISENGAGED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 609AW E2070 AFT PASSENGER CABIN DOOR AFTER OPENING, GIRT BAR DISENGAGED FROM DOOR. FOUND NO PARTIAL DEPLOYMENT OF SLIDE, RE-ENGAGED GIRT BAR TO DOOR. RECONNECTED SLIDE AUTODEPLOY LANYARD. OPS CHECKED DOOR AND GIRT BAR. OPS CHECKS SATISFACTORY. A CFT TT: 23,562 HOURS. ACFT TC: 33,928. (X) 2 H 7 4 4F RT A49EU 1999072300311 19990723 00311 EU 1999 7 23 A6WA9900038 1 19990114 A 5310 STRUCTURE BAG BAE146 BAE146200A 1500266 EU FRAME 50 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER BAE FAX JM/RJ0491-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300312 19990723 00312 EU 1999 7 23 A6WA9900037 1 19990114 A 5310 STRUCTURE BAG BAE146 BAE146200A 1500266 EU FRAME 50 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RIGHT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER FAX JM/RJ049-96. A CFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300313 19990723 00313 EU 1999 7 23 A6WA9900036 1 19990114 A 5320 RIVET BAG BAE146 BAE146200A 1500266 EU FRAME 50 SHEARED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RT UPPER AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLAC ED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300314 19990723 00314 EU 1999 7 23 A6WA9900035 1 19990114 A 5320 RIVET BAG BAE146 BAE146200A 1500266 EU FRAME 50 SHEARED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RI VETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300315 19990723 00315 EU 1999 7 23 A6WA9900034 1 19990114 A 5320 GUSSET BAG BAE146 BAE146200A 1500266 EU FRAME 50 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE HAS A FILLER PANEL CRACKED AT THE LIGHTNING HOLE. REPL ACED GUSSET PLATE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300316 19990723 00316 EU 1999 7 23 A6WA9900033 1 19990116 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 RIGHT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD END. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC : 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300317 19990723 00317 EU 1999 7 23 A6WA9900032 1 19990215 A 5230 RIB BAG BAE146 BAE146200A 1500266 EU CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 AFT CARGO DOOR UPPER MOST RIB IS CRACKING LOCATED UNDER UPPER AFT HINGE 'L' BRACKET ON UPPER MOST RIB IAW BAE REPAIR DRA WING REF HC523H9001 AND FOUND SERVICEABLE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300318 19990723 00318 EU 1999 7 23 A6WA9900031 1 19990129 A 5720 BRACKET BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 LEFT WING TE SHROUD LOWER SKIN STIFFENER AFT (TAG) ANGLE BRACKET CRACKED BETWEEN RIB 8 AND RIB 9. REPLACED BRACKET. AC FT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300319 19990723 00319 EU 1999 7 23 A6WA9900030 1 19990129 A 5730 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 LEFT WING TE TOP SHROUD SKIN STIFFENER TO FALSE SPAR (AFT END) BROKEN BETWEEN RIBS 7 AND 8. REPLACED STIFFENER. ACFT T T: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300320 19990723 00320 EU 1999 7 23 A6WA9900029 1 19990127 A 5720 BRACKET BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 LEFT WING TE SHROUD UPPER SKIN STIFFENER TO FALSE SPARE ANGLE BRACKET CRACKED BETWEEN RIBS 7 AND 8. REPLACED BRACKET. A CFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300321 19990723 00321 EU 1999 7 23 A6WA9900028 1 19990120 A 5320 ANGLE BAG BAE146 BAE146200A 1500266 EU FRAME 50 CORRODED A A6WA O OTHER O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 RIGHT WEB CLOSING ANGLE AFT OF FRAME 50 HAS ONE INCH CRACK. REPAIRED IAW BAE SRM 51-71-11 FIG 2. ACFT TT: 19,327 HOUR S. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300322 19990723 00322 EU 1999 7 23 A6WA9900023 1 19990106 A 5720 BOLT BAG BAE146 BAE146200A 1500266 EU WING BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FRAME 29 LEFT AND RIGHT BOTTOM BOLT OF WING ATTACHMENT BRACKET HEAD APPEARS TO BE BROKEN. REMOVED BOLT, CLEANED AND INS PECTED HOLE, PREP, ALODINE, PRIMED AND INSTALLED NEW BOLT AND NUT IAW FAX DJR/RJ0022/96 AND DJR/RJ0721-96. WITCO BOND W ILL BE APPLIED ON WORKCARD 2166. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300323 19990723 00323 EU 1999 7 23 A6WA9900027 1 19990116 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 LEFT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD ENGINE. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300324 19990723 00324 EU 1999 7 23 A6WA9900026 1 19990109 A 5320 GUSSET BAG BAE146 BAE146200A 1500266 EU CABIN CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 SEVERAL GUSSET PLATES ON FLOOR ARE CORRODED (SURFACE CORROSION) AFT VESTIBULE. REPLACED CORRODED GUSSET PLATES, 2 EACH. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300325 19990723 00325 EU 1999 7 23 A6WA9900025 1 19990109 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU CABIN CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 FORWARD F/A SEAT PAN CRACKED. REPLACED PAN. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X) 2 H 7 4 4F RT A49EU 1999072300470 19990723 00470 NM 1999 7 23 TWAA9910201 1 19990717 A 3350 20121 CHARGER BOEING 767 767231 1385131 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 607TW 22570 THE EGRESS LIGHT STRIP BETWEEN THE LEFT FORWARD CABIN DOOR AND THE FWD GALLEY AND THE AFT LEFT EXTERIOR EMERGENCY LIGHT WERE INOPERATIVE. CORRECTED THE EGRESS LIGHT BY RECONNECTING THE JUMPER CABLE (P/N 5912-2) THAT HAD BECOME DISCONNECTED AND REPLACED THE BATTERY CHARGER FOR THE EXTERIOR LIGHT PROBLEM. CHECK-C 5-21-99 LAX. 2 L 7 2 4F RT A1NM 1999072300471 19990723 00471 WP 1999 7 23 TWAA9910202 1 19990719 A 3350 41B030CF00101 BATTERIES DOUG DC9 DC932 3022066 WP EMER EXIT DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 923L 47109 BOTH OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 3-26-99 MCI. 2 L 7 2 4F A6WE 1999072300472 19990723 00472 NM 1999 7 23 HNAA9900103 1 19990719 A 3350 RELAY DHAV DHC8 DHC8201 2809001 NM CABIN FAILED A HNAA K NONE L NO TEST CR CRUISE 1 EA 07 995HA 460 FLOOR EMERGENCY ESCAPE PATH LIGHTS FLICKER IN FLIGHT. REMOVED AND REPLACED RELAY X-D4N AND 3152 PS1-PS2 BASE ASSY AND B ATTERY, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999072300473 19990723 00473 NM 1999 7 23 AWXA9900242 1 19990713 A 2913 HYD PUMP BOEING 757 7572S7 1384962 NM LT ENGINE FAILED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 902AW 23322 LT HYD SYS FAILED, RT MLG DID NOT EXTEND NORM. LT HYD QTY DROPPED TO .11. CYCLED OFF BOTH ELECT AND ENG PUMPS. GEAR G REEN DOWN LIGHT FAILED TO ILLUM WITH GEAR HANDLE DOWN. EICAS MESSAGE, GEAR DISAGREE, GEAR DOOR DISPLAY DOOR AND GEAR AM BER LIGHTS ILLUM. ALTERNATE GEAR EXTENSION ATTEMP. FOUND LT ENG DRIVEN PUMP CASE DRAIN QD OFF AT PUMP. R&R'D LT ENG D RIVEN PUMP AND LT AC MOTOR PUMP. ALSO CHANGED MLG ALTERNATE UPLOCK ACTUATOR AND RT MAIN GEAR DOOR SEQUENCE VALVE. 2 L 7 2 4F RT A2NM 1999072300474 19990723 00474 EU 1999 7 23 AWXA9900243 1 19990714 A 2150 744A000008 PACK AIRBUS 320 A320231 3930325 EU CABIN MALFUNCTIONED A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 646AW 271 NOTICEABLE OFFENSIVE ODOR FROM AIR CONDITIONING SYSTEM DURING CLIMB AND DESCENT. LT PACK PRODUCING SMELL. PLACED ON ME L 21-52-01. 2 L 7 2 4F RT A28NM 1999072300475 19990723 00475 SO 1999 7 23 COMA9910115 1 19990719 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 8 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 261CA 120254 EXIT SIGN AT ROW 8 IS BROKEN. REPLACED SIGN. 2 L 7 2 4T RT A31SO 1999072300476 19990723 00476 WP 1999 7 23 ABXA9900569 1 19990620 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE RIB AT STATION FS 772.50 CRACKED AT AFT LOWER END. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056 . 2 L 7 4 4F 4A25 1999072300477 19990723 00477 WP 1999 7 23 ABXA9900570 1 19990617 A 5712 8121019 RIB DOUG DOUG DC8 DC863 302198A WP WS 616.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT OUTBOARD LEADING EDGE RIB CRACKED AT STATION XFS 616.25. REPAIRED IAW DC8 SRM 51-1-21 AND DWG K05056. 2 L 7 4 4F 4A25 1999072300478 19990723 00478 WP 1999 7 23 ABXA9900571 1 19990616 A 5712 5269545 RIB DOUG DOUG DC8 DC863 302198A WP WS 622.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 622.5. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K05056. 2 L 7 4 4F 4A25 1999072300479 19990723 00479 WP 1999 7 23 ABXA9900572 1 19990616 A 5712 5269545 RIB DOUG DOUG DC8 DC863 302198A WP WS 791.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS 791.25. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056. 2 L 7 4 4F 4A25 1999072300480 19990723 00480 WP 1999 7 23 ABXA9900573 1 19990612 A 5712 5269545 RIB DOUG DOUG DC8 DC863 302198A WP WS 732.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE CRACKED AT STATION XFS 732.5. REPAIRED IAW DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1999072300481 19990723 00481 WP 1999 7 23 MWEA99395 1 19990719 A 2560 113317 COVER DOUG DC9 DC914 3022034 WP SERV DOOR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 400ME 45727 GALLEY SERVICE DOOR EMERGENCY SLIDE COVER FELL OFF. RE-INSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999072300482 19990723 00482 WP 1999 7 23 MWEA99399 1 19990715 A 2432 43B034LB03 BATTERY DOUG DC9 DC932 3022066 WP NOSE SECTION DEFECTIVE A MWEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 602ME 48133 SMOKE COMING OUT OF BATTERY VENT HOLES. MTC REMOVED AND REPLACED BOTH MAIN BATTERIES, BATTERY CHARGER AND TEMP SENSORS. 2 L 7 2 4F A6WE 1999072300483 19990723 00483 WP 1999 7 23 MWEA99398 1 19990719 A 5313 27779485 LONGERON DOUG DC9 DC914 3022034 WP BS 148 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERON AT STATION 148 L27R WAS DAMAGED. MTC REMOVED AND REPLACED LONGERON. 2 L 7 2 4F A6WE 1999072300484 19990723 00484 WP 1999 7 23 MWEA99397 1 19990719 A 5320 991151595 CLIP DOUG DC9 DC914 3022034 WP BS 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SHEAR CLIP BETWEEN L19L AND L18L STATION 160 HAD CORROSION. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999072300485 19990723 00485 WP 1999 7 23 MWEA99410 1 19990719 A 5321 9910078213 FLOOR DOUG DC9 DC914 3022034 WP BS 120-134 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SUB FLOOR PAN CRACKED AT 3 LOCATIONS BETWEEN STATION 120 TO 134. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1999072300486 19990723 00486 WP 1999 7 23 MWEA99409 1 19990719 A 5330 59114015 SKIN DOUG DC9 DC914 3022034 WP BS 207 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SKIN AT STATION 207 L26R HAD CRACK. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999072300487 19990723 00487 WP 1999 7 23 MWEA99408 1 19990719 A 5330 27779221 SKIN DOUG DC9 DC914 3022034 WP BS 148 CUT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SKIN AT L19L BETWEEN STATION 148 TO 134 WAS CUT. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999072300488 19990723 00488 WP 1999 7 23 MWEA99407 1 19990719 A 5320 991159345 STIFFENER DOUG DC9 DC914 3022034 WP BS 160 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 TWO CRACKED STIFFENERS AT FS 160 AT 14 INCHES FROM OUTBOARD END AND 20 INCHES FROM RIGHT CENTER LINE. MTC REMOVED AND R EPLACED STIFFENERS. 2 L 7 2 4F A6WE 1999072300489 19990723 00489 WP 1999 7 23 MWEA99406 1 19990719 A 5320 99115505 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 134-200 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SEVEN INTERCOSTAL DENTED BETWEEN FS 134 TO 200 AND L22R AND L28L. MTC REMOVED AND REPLACED INTERCOSTALS. 2 L 7 2 4F A6WE 1999072300490 19990723 00490 WP 1999 7 23 MWEA99405 1 19990719 A 5320 991151421 SHEAR TIES DOUG DC9 DC914 3022034 WP BS 134-297 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 TWELVE SHEAR TIES DAMAGED BETWEEN STATION 134 TO 297 AT L18R AND L27R. MTC REMOVED AND REPLACED SHEAR TIES. 2 L 7 2 4F A6WE 1999072300491 19990723 00491 WP 1999 7 23 MWEA99404 1 19990719 A 5311 99115126 FRAME DOUG DC9 DC914 3022034 WP BS 120-200 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 EIGHT FRAME SECTIONS DAMAGED AT STATION 120 TO 200 AND BETWEEN L18R-L22L. MTC REMOVED AND REPLACED FRAMES. 2 L 7 2 4F A6WE 1999072300492 19990723 00492 WP 1999 7 23 MWEA99403 1 19990719 A 5320 49125151 CLIPS DOUG DC9 DC914 3022034 WP BS 110 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SEVEN SHOVEL CLIPS AT STATION 110 BETWEEN L19R AND L25R WERE DAMAGED. MTC REMOVED AND REPLACED SHOVEL CLIPS. 2 L 7 2 4F A6WE 1999072300493 19990723 00493 WP 1999 7 23 MWEA99402 1 19990719 A 5313 277779223 LONGERON DOUG DC9 DC914 3022034 WP BS 110-229 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 LONGERONS L19R TO L25R FROM STATION 110 TO 229 WAS DAMAGED. MTC REMOVED AND REPLACED LONGERONS. 2 L 7 2 4F A6WE 1999072300494 19990723 00494 WP 1999 7 23 MWEA99401 1 19990719 A 5330 59114017 SKIN DOUG DC9 DC914 3022034 WP BS 110-229 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 SKIN PANEL BETWEEN STATION 110 TO 229 AND L18R TO 26R IS DAMAGED. MTC REMOVED AND REPLACED SKIN. 2 L 7 2 4F A6WE 1999072300495 19990723 00495 WP 1999 7 23 MWEA99400 1 19990715 A 2560 100502121 COVER DOUG DC9 DC981 3022081 WP DOOR SLIDE LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 804ME 48030 THE AFT GALLEY DOOR SLIDE COVER CAME LOOSE. MTC RESECURED THE AFT GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1999072300496 19990723 00496 NE 1999 7 23 MWEA99394 2 19990711 A 7321 76960615 FUEL CONTROL DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE LT ENGINE MALFUNCTIONED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 808ME 48070 LEFT ENGINE FUEL FLOW FLUCTUATES 700 POUNDS WITH LEFT ENGINE EPR FLUCTUATING FROM 1.95 DOWN TO 1.70. MTC REMOVED AND RE PLACED LEFT ENGINE FUEL CONTROLLER AND FUEL PUMP. 2 L 7 2 4F 4 F A6WE E9NE 1999072300497 19990723 00497 WP 1999 7 23 MWEA99396 1 19990717 A 2560 100502121 SLIDE DOUG DC9 DC981 3022081 WP SERVICE DOOR OUT OF POSITION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 AFT GALLEY SERVICE DOOR EMERGENCY SLIDE PSI GAUGE UNABLE TO BE READ DUE TO SLIDE SHIFTED TO THE SIDE. RE-INSTALLED SLID E SO THAT GAUGE IS READABLE. 2 L 7 2 4F A6WE 1999072300498 19990723 00498 NM 1999 7 23 SCNA99092 1 19990719 A 2910 HYDRAULIC LINE BOEING 727 727227 1384078 NM NR 1 ENGINE FRACTURED A SCNA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 275AF 22092 DURING CLIMB, AIRCRAFT EXPERIENCED A SYSTEM HYDRAULIC LOSS. COMPLIED WITH COM ABNORMAL PROCEDURES AND RETURNED TO THE A IRPORT. UPON INSPECTION FOUND PRESSURE LINE FROM THE NUMBER ONE ENGINE SPLIT. REPLACED LINE AND SERVICED HYDRAULICS. S YSTEM LEAKS AND OPERATIONALLY CHECKS GOOD IAW MM 290000. 2 L 7 3 4F A3WE 1999072300499 19990723 00499 NM 1999 7 23 SWAA991203 1 19990717 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999072300500 19990723 00500 1999 7 23 SWAA991204 4 19990717 A 2565 D31354 SLIDE BOEING 737 7373T5 NM PASSENGER DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 AFT ENTRY EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300501 19990723 00501 NM 1999 7 23 SWAA991205 1 19990716 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 12-14 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT INOP, ROWS 12 TO 14. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 1999072300502 19990723 00502 NM 1999 7 23 SWAA991206 1 19990718 A 2150 655281057 ACCESSORY UNIT BOEING 737 7373H4 1384600 NM E & E BAY MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 620SW 28036 DURING CLIMB, BOTH A/C PACKS FAILED ALTERNATELY. DIVERTED TO ABQ. REMOVED AND REPLACED A/C ACCESSORY UNIT PER MM. 2 L 7 2 4F RT A16WE 1999072300503 19990723 00503 NM 1999 7 23 SWAA991207 1 19990717 A 7930 42D107A1 SWITCH BOEING 737 7372H4 138448C NM NR 1 ENGINE ERRATIC A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 063SW 22061 NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED SEVERAL TIMES. DIVERTED TO DAL. REMOVED AND REPLACED NR 1 ENG OIL PRESS S WITCH PER MM. 2 L 7 2 4F A16WE 1999072300504 19990723 00504 NM 1999 7 23 SWAA991208 1 19990716 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 EEPLS LIGHTS HAS EXPOSED WIRES BY OVERWING EXITS. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999072300505 19990723 00505 NM 1999 7 23 SWAA991209 1 19990717 A 3350 BR2013 COVER BOEING 737 7373H4 1384600 NM ROW 19 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS LIGHT COVER FELL OUT AT ROW 19. REPAIRED WIRING AND REPLACED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 1999072300506 19990723 00506 NE 1999 7 23 SWAA991210 2 19990718 A 7320 709OM98G05 PMC BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 322SW 23343 AFTER TAKEOFF, NR 1 ENG N2, EGT AND FUEL FLOW INDICATIONS INOP DUE TO PMC. ALSO PMC INOP. REMOVED AND REPLACED NR 1 EN G PMC PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999072300507 19990723 00507 NM 1999 7 23 SWAA991192 1 19990714 A 5230 6547952 CHORD BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR NR 2 LOWER T-CHORD CRACKED. REMOVED AND REPLACED T-CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999072300508 19990723 00508 1999 7 23 SWAA991193 4 19990714 A 2565 1061323 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 FWD ENTRY DOOR EVACUATION SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300509 19990723 00509 NM 1999 7 23 SWAA991194 1 19990714 A 3350 079123 LENS BOEING 737 7373H4 1384600 NM ROW 8 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 EEPLS LIGHT LENS MISSING NEXT TO ROW 8. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 1999072300510 19990723 00510 NM 1999 7 23 SWAA991195 1 19990715 A 3350 A170033 STRAP BOEING 737 7372H4 138448C NM PAX DOOR LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 FWD EMERGENCY FLASHLIGHT SECURITY STRAP BROKEN. INSTALLED STRAP PER MM. 2 L 7 2 4F A16WE 1999072300511 19990723 00511 NM 1999 7 23 SWAA991196 1 19990715 A 3350 079123 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 SEVERAL EEPLS LIGHT LENS CAME OUT OF TRACK DURING LANDING. RE-INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 1999072300512 19990723 00512 NM 1999 7 23 SWAA991197 1 19990715 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM PASSENGER DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASS Y PER MM. 2 L 7 2 4F A16WE 1999072300513 19990723 00513 NM 1999 7 23 SWAA991198 1 19990715 A 3350 610478 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP IN AFT END OF CABIN. REMOVED AND REPLACED BATTERY AND CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999072300514 19990723 00514 NM 1999 7 23 SWAA991199 1 19990715 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN OUT OF TRACK A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 504SW 24181 EEPLS LIGHTS PULLED OUT OF TRACK. RE-INSTALLED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999072300515 19990723 00515 NM 1999 7 23 SWAA991200 1 19990715 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PASSENGER DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999072300516 19990723 00516 NM 1999 7 23 SWAA991201 1 19990715 A 3260 162A0001 INDICATION BOEING 737 7377H4 NM NLG MALFUNCTIONED A SWAA O OTHER N FALSE WARNING LD LANDING 1 SW 07 741SA 29277 NLG UNSAFE INDICATION LIGHT REMAINED ILLUMINATED DURING FIRST ATTEMPT TO LOWER THE NLG. CYCLED THE GEAR AND THE LIGHT WENT OUT. PSEU BITE CLEARED FAULT. TEST OF NLG DOWN SENSOR CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999072300517 19990723 00517 NM 1999 7 23 SWAA991202 1 19990715 A 5314 6545866 KEEL BEAM BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C4 CHECK, FOUND CORROSION AT KEEL BEAM, BS 727+3.00, STRINGER 27L. REPAIRED KEEL BEAM PER SWA RA NR 1 253-2120. 2 L 7 2 4F A16WE 1999072300518 19990723 00518 NM 1999 7 23 SWAA991191 1 19990714 A 5230 6546921 CHORD BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR NR 3 LOWER T-CHORD CRACKED. REMOVED AND REPLACED T-CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999072300552 19990723 00552 NM 1999 7 23 EISA99102 1 19990408 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 480-690 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK, WORK-CARD FOUND SEAT TRACK CORRODED BEYOND LIMITS AT RIGHT OUTBOARD TRACK FROM FS 480 TO FS 690. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999072300553 19990723 00553 NM 1999 7 23 EISA99108 1 19990408 A 5752 652172629 TAB BOEING 727 727264 138408M NM LT AILERON DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF BN48 20710 DURING C-CHECK INSPECTION, FOUND LEFT WING OUTBOARD AILERON TAB DELAMINATED AND HAS SEVERAL DENTS. REPAIRED IAW BOEING SRM 727 CHAPTER 51-50-5-5, 51-40-5 AND 51-40-6. (M) 2 L 7 3 4F A3WE 1999072300554 19990723 00554 NM 1999 7 23 EISA99082 1 19990408 A 5753 652163475 SKIN BOEING 727 727264 138408M NM LT TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LEFT WING TRAILING EDGE FLAP DELAMINATED AT WS 240. REPAIRED BY OUTSIDE VENDOR SEE WO 9829 ITEM NR 0098 FOR REPAIRS REMOVED AND REGLASSED IAW BOEING SRM 51-40-99. (M) 2 L 7 3 4F A3WE 1999072300555 19990723 00555 NM 1999 7 23 EISA99130 1 19990522 A 2751 1812993 INDICATOR BOEING 727 7272A7 138407K NM TE FLAPS UNSERVICEABLE A EISA O OTHER N FALSE WARNING LD LANDING 1 SW 07 310NE 20241 CREW HAD SPLIT FLAP INDICATION, DECLARED EMERGENCY AND MADE 'GO AROUND'. CHECKED FLAP OPERATION, REPLACED OUTBOARD FLAP INDICATOR AND OPS CHECKED OK. (M) 2 L 7 3 4F A3WE 1999072300556 19990723 00556 1999 7 23 PLGA990614 4 19990614 A 2200 9121835104 COMPUTER SAAB SF340 340B 7860101 EU E/E COMPT MALFUNCTIONED A PLGA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 NE 05 349BE 1015 340B196 BOS - FLT 6424 - CREW SELECTED AUTO-PILOT OFF AND ENGAGED YAW DAMPENER. ONCE YAW DAMPENER WAS SELECTED THE RUDDER START ED TO DEFLECT TO FULL LEFT ALONG WITH AUTO TRIM LIGHT ON CWP. CREW BROUGHT THE RUDDER BACK TO THE DESIRED POSITION WITH TRIM. CREW THEN USED MAIN TRIM TO PITCH A/C NOSE UP. ONCE THEY DID THIS, MAIN TRIM TAB CAME UP AND THEY GOT A PITCH T RIM LIGHT ON THE CWP. AS THE MAIN TRIM CAME UP, THE STANDBY TRIM WENT DOWN. BROUGHT THE STANDBY TRIM UP TO MATCH THE M AIN TRIM BY USE OF STANDBY PITCH TRIM SWITCH. THE CREW LANDED THE AIRCRAFT WITHOUT INCIDENT. THE FDR HAS BEEN REMOVED AND SENT OUT TO HAVE ITS INFORMATION DOWNLOADED. MAINTENANCE REPLACED THE PITCH SYNCH COMPUTER AND RELAYS 15FD AND 16FD 2 L 7 2 4T RT A52EU 1999072300557 19990723 00557 EU 1999 7 23 PLGA990526 1 19990526 A 3234 D49410001 CONTROL HANDLE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 351BE 3251190 340B237 BOS - FLT 6219 - AFTER DEPARTURE FROM BOS, THE LANDING GEAR INTRANSIT LIGHT DID NOT OPERATE PROPERLY WHEN THE GEAR WAS R ETRACTED. THE GREEN LIGHTS AND INTRANSIT LIGHTS OPERATED NORMALLY WHEN EXTENDING THE GEAR. THE AIRCRAFT RETURNED TO BO S AND LANED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR HANDLE ASSY, PERFORMED THE REQUIRED OPS CHECK AND R ETURNED THE A/C TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999072300558 19990723 00558 EU 1999 7 23 PLGA990527 1 19990527 A 2424 51539007A GCU SAAB SF340 SF340A 7850100 EU E/E COMPT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 742BA 9018 340A092 BGR - FLT 6268 - AFTER TAKEOFF FROM BGR, THE LEFT DC GENERATOR FAILED AND THE AIRCRAFT RETURNED TO BGR WITHOUT INCIDENT. MAINTENANCE FOUND THE GENERATOR CONTROL UNIT TO BE AT FAULT, THE GCU WAS REPLACED, REQUIRED OPERATIONAL CHECKS WERE PE RFORMED, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999072300559 19990723 00559 EU 1999 7 23 PLGA990528 1 19990528 A 6100 MS295513111 O-RING SAAB SF340 SF340A 7850100 EU LT PROP FAILED A PLGA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NE 05 745BA 340A111 LGA - FLT 6582 - AFTER TAKEOFF FROM LGA, LEFT PROP OIL PRESSURE STARTED TO DROP. AIRCRAFT RETURNED TO LGA AND LANDED WI THOUT INCIDENT. MAINTENANCE REPLACED 6 O-RINGS ON THE TRANSFER TUBES TO THE PROP PCU, PERFORMED THE REQUIRED LEAK CHECK S, AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999072300560 19990723 00560 EU 1999 7 23 PLGA990606 1 19990606 A 6120 AUTOCOARSEN SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A PLGA K NONE O OTHER AP APPROACH 1 NE 05 348BE 340B190 BTV - FLT 6406 - AIRCRAFT HAD A POSSIBLE MOMENTARY AUTO COARSEN EVENT ON THE LEFT ENGINE ON SHORT FINAL TO BTV. CREW RE PORTED THAT IT OCCURRED SO FAST THAT THEY WERE UNSURE OF WHAT IT WAS. THE CREW SAID THEY DID NOT THINK IT WAS A POWER I NTERRUPTION, BUT IT DID SOUND LIKE A MOMENTARY AUTO COARSEN. MAINTENANCE COULD NOT DUPLICATE THE ANOMALY. THE FLIGHT D ATA RECORDER WAS REPLACED AND WILL BE DOWNLOADED TO TRY AND DETERMINE WHAT OCCURRED ON THE AIRCRAFT. THE AIRCRAFT HAS B EEN RETURNED TO SERVICE AND HAS OPERATED WITHOUT A REPEAT OF THIS INCIDENT. (M) 2 L 7 2 4T RT A52EU 1999072300561 19990723 00561 EU 1999 7 23 PLGA990609 1 19990609 A 6120 1103P0620 SWITCH SAAB SF340 SF340A 7850100 EU AUTOCOARSEN INOP A PLGA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NE 05 343BE 340A101 BOS - FLT 3143 - AIRCRAFT WAS DOING A FERRY FLIGHT, ABORTED TAKEOFF ROLL WHEN THE AUTOCOARSEN LIGHT ILLUMINATED. MAINTE NANCE MEL'D THE AUTOCOARSEN SYSTEM AND THE AIRCRAFT CONTINUED TO ALBANY. AT ALBANY, MAINTENANCE REPLACED BOTH P3 SWITCH ES, PERFORMED THE REQUIRED OPERATIONAL CHECKS AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999072300562 19990723 00562 NM 1999 7 23 MASA99102 1 19990622 A 3350 SWITCH DHAV DHC8 DHC8202 2809007 NM COCKPIT OUT OF POSITION A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 6343 - PHX-PSP - THE CAPTAIN REPORTED THAT SEVERAL EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE RESET THE COCK PIT ARMING SWITCH, NO FURTHER DISCREPANCIES WERE NOTED. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999072300563 19990723 00563 CE 1999 7 23 MASA99093 1 19990607 A 6123 5038912129 SWITCH BEECH 1900 1900D 1154162 CE RIGHT FAILED A MASA K NONE J WARNING INDICATION LD LANDING 1 SW 07 146ZV UE146 FLT 110 - DEN-COS - ON APPROACH, THE CAPTAIN REPORTED THE RIGHT PORP APPEARED TO FEATHER BRIEFLY. THE AIRCRAFT WAS FERR IED TO FMN, WHERE MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RIGHT ENGINE LOW PRESSURE AUTOFEATHER SWITCH AND THE LEFT ENGINE HIGH PRESSURE AUTOFEATHER SWITCH. OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999072300564 19990723 00564 CE 1999 7 23 99ZZZM390 1 19990607 A 6123 5038912121 SWITCH BEECH 1900 1900D 1154162 CE LEFT FAILED A MASA K NONE J WARNING INDICATION LD LANDING 1 SW 07 146ZV UE146 FLT 110 - DEN-COS - ON APPROACH, THE CAPTAIN REPORTED THE RIGHT PORP APPEARED TO FEATHER BRIEFLY. THE AIRCRAFT WAS FERR IED TO FMN, WHERE MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RIGHT ENGINE LOW PRESSURE AUTOFEATHER SWITCH AND THE LEFT ENGINE HIGH PRESSURE AUTOFEATHER SWITCH. OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999072300565 19990723 00565 NM 1999 7 23 MASA99101 1 19990621 A 2433 CONNECTOR DHAV DHC8 DHC8202 2809007 NM E/E COMPT LOOSE A MASA O OTHER O OTHER CL CLIMB 1 SW 07 456YV 456 FLT 6235 - MTJ-PHX - THE CAPTAIN REPORTED SHORTLY AFTER TAKEOFF, THE EMERGENCY LIGHTS STARTED TO FLICKER. MAINTENANCE F OUND AND RESECURED A LOOSE CONNECTION ON THE RIGHT TRU. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999072300566 19990723 00566 WP 1999 7 23 ARWA990701 1 19990627 A 3246 1542511 WHEEL DOUG DC8 DC862 3021970 WP LT MLG FAILED A ARWA O OTHER J WARNING INDICATION LD LANDING 1 SO 19 1804 7788 45896 CLO - FLT 627 - INBOURND TO CALI, MESSAGE THAT MLG TIRE HAD SEPARATED FROM AIRCRAFT ON TAKEOFF FROM QUITO, ECUADOR. AIR CRAFT LANDED IN CALI WITHOUT INCIDENT. INSPECTION FOUND NR 2 MLG OUTBOARD WHEEL HALF BEAD HAD SEPARATED AND TIRE EJECTE D. INCURRED DAMAGE TO LT INBOARD WHEEL WELL DOOR DAMAGED AND NR 3 ENGINE TAILPIPE CREASED. CAUSE OF WHEEL FAILURE TO B E DETERMINED BY MANUFACTURER. (M) 2 L 7 4 4F 4A25 1999072300567 19990723 00567 1999 7 23 ARWA990702 4 19990703 A 3414 536149 VALVE DOUG DC8 DC862F 3021972 WP LT COCKPIT LEAKING A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 791AL 2420 46150 MIA - FLT 9038 - DURING CLIMB, F/O'S AIRSPEED INDICATOR WAS SHOWING 10 KTS LOWER THAN THE CAPT AND THE DIFFERENCE INCREA SED WITH THE ALTITUDE UP TO 50 KTS LOWER FL230. SELECTED F/O'S STATIC SELECTOR TO ALT FOR LANDING. REMOVED AND REPLACE D KNOB ALT PITOT SELECTOR VALVE. PERFORMED OPS CHECK PITOT STATIC SYSTEM. FIRST OFFICER AND ALTERNATE, FOUND NORMAL IA W MM 34-12-0. (M) 2 L 7 4 4F 4A25 1999072300568 19990723 00568 NM 1999 7 23 GAIA9973 1 19990608 A 2781 CONNECTOR BOEING 727 7272J0 138407E NM NR 5 LE SLAT DIRTY A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 284KH 21108 FLT 504 - DURING CLIMB-OUT FROM TOL, THE NR 5 SLAT INDICATE AS NOT RETRACED WHILE ALL OTHER TRAILING AND LEADING EDGE DE VICES WERE RETRACTED. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANDED WITHOUT FURTHER PROBL EMS. CLEANED NR 5 SLAT SWITCH CANNON PLUG. OPERATIONALLY CHECKED THE FLAP INDICATING SYSTEM AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 1999072300569 19990723 00569 NM 1999 7 23 GAIA9977 1 19990617 A 2120 AIR DIST BOEING 727 727223 1384074 NM COCKPIT ODOR A GAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 6816 19491 FLT 1756 - HUF-CLT - AT FLT LVL 290 SMELLED ODOR FROM CARGO COMPARTMENT. EMERGENCY WAS DECLARED AND CHECKLIST COMPLETED . NORMAL LANDING AT CLT. PERFORMED HAZ MAT INSPECTION FOR POSSIBLE HAZ WASTE SPILLAGE IAW THE KHA GMM CHAPTER 18. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999072300570 19990723 00570 NM 1999 7 23 ASAA9940131 1 19990608 A 5751 654652030 SUPPORT BOEING 737 7374Q8 NM RT AILERON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE RT AILERON INBOARD HINGE SUPPORT WAS FOUND TO BE CRACKED AT THE NUTPLATE, OUTBOARD SIDE. REPAIRED PER EA 5740-01177. (M) 2 L 7 2 4F RT A16WE 1999072300571 19990723 00571 NM 1999 7 23 ASAA9940130 1 19990608 A 5320 65C807351 CHORD BOEING 737 7374Q8 NM BS 947.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE RIGHT INNER CHORD AT THE R2 DOOR STATION 947.5 TO 957.5 WAS FOUND TO BE CORRODED. R EPAIRED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999072300572 19990723 00572 NM 1999 7 23 ASAA9940129 1 19990608 A 5315 FLOORBEAM BOEING 737 7374Q8 NM BS 344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE FLOORBEAM CAP UPPER SURFACE AT STATION 344, LBL 40-56 WAS FOUND TO BE CORRODED. RE PAIRED PER SRM 53-00-51, FIG 203. (M) 2 L 7 2 4F RT A16WE 1999072300573 19990723 00573 NM 1999 7 23 ASAA9940128 1 19990608 A 5330 SKIN BOEING 737 7374Q8 NM BS 360 LIGHTNING STRIKE A ASAA K NONE C F.O.D. IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE EXTERNAL FUSELGE SKIN AT BS 360, STRINGER 17L WAS FOUND TO HAVE 2 LIGHTNING STRIKES . REPAIRED PER SRM 53-00-01, FIG 223. (M) 2 L 7 2 4F RT A16WE 1999072300574 19990723 00574 NM 1999 7 23 ASAA9940127 1 19990608 A 5315 654681179 FLOORBEAM BOEING 737 7374Q8 NM BS 986.5 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE TOP FLANGES OF THE FLOORBEAM AT STATION 986.5, LBL 33 - RBL 30 WERE FOUND TO BE GOU GED AND CORRODED. REPAIRED PER EA 5310-01697. (M) 2 L 7 2 4F RT A16WE 1999072300575 19990723 00575 NM 1999 7 23 ASAA9940126 1 19990608 A 5315 65C339483 FLOORBEAM BOEING 737 7374Q8 NM BS 947.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE FORWARD AND AFT FLANGES OF THE FLOORBEAM AT STATION 947.5, LBL 12-RBL 10 WERE FOUND TO BE CORRODED. REPAIRED PER EA 5310-01702. (M) 2 L 7 2 4F RT A16WE 1999072300576 19990723 00576 NM 1999 7 23 ASAA9940125 1 19990608 A 5311 65C25230 FRAME BOEING 737 7374Q8 NM BS 727 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE AFT CARGO COMPARTMENT TOP OF MAIN FRAME WAS FOUND TO BE DENTED AT BS 727E 30 INCHES BELOW STRINGER 22R AND BS 727F ABOVE STRINGER 25R. REPAIRED PER EA 5310-01701. (M) 2 L 7 2 4F RT A16WE 1999072300577 19990723 00577 NM 1999 7 23 ASAA9940124 1 19990608 A 5315 602671X7050T7651 FLOORBEAM BOEING 737 7374Q8 NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE FLOORBEAM CAP UPPER SURFACE AT STATION 312 LBL 12 TO RBL 12 WAS FOUND TO BE CORRODE D. REPAIRED PER SRM 53-10-01 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999072300578 19990723 00578 NM 1999 7 23 ASAA9940123 1 19990608 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7374Q8 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 760AS 25098 PHX - DURING SCHEDULED SI CHECK, THE FORWARD AND AFT TOP FLANGED OF THE FLOORBEAM AT STATION 967, LBL 14-21 AND 23-33 WA S FOUND TO BE CORRODED. REPAIRED PER SRM 53-00-51 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999072300579 19990723 00579 NE 1999 7 23 99ZZZM391 2 19990615 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 VIBRATION A AMTA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 11 189AT 193C1081 10341 DURING CLIMB ENGINE VIBRATION FILTER PRESSURE LIGHT CAME ON AND CHANNEL 'A' AND 'B' READING 2.5 UNITS. SHUTDOWN ENGINE NR 2 IAW AOM AND CHECKLIST, DUMPED FUEL BELOW MAXIMUM LANDING WEIGHT. RETURN TO IND. RAN ENGINE IAW MM 71-00-00 AND NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A23WE E12EU 1999072300580 19990723 00580 NM 1999 7 23 F3LA99085 1 19990618 A 5210 65537557 FITTING BOEING 737 737201 1384454 NM AIRSTAIR DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-4 CHECK INSPECTION, REPORTED LEFT UPPER FORWARD STOP FITTING ON AFT AIRSTAIR DOOR CRACKED. MAINTENANCE I NSTALLED REPLACEMENT FITTING PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999072300581 19990723 00581 SO 1999 7 23 C2XA99IA334 1 19990618 A 3350 3025101 LIGHT EMB 145 EMB145LR SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14952 145067 IAH - DURING SERVICE CHECK INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED LIGHT ASSY IAW EMB145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT T00011AT 1999072300582 19990723 00582 SO 1999 7 23 C2XA99IA333 1 19990616 A 3350 GE1317 BULB EMB 145 EMB145 SO EMERGENCY EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16961 145103 IAH - DURING 3A INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURNEDTO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999072300583 19990723 00583 EU 1999 7 23 C2XA99IA332 1 19990616 A 3350 7012210 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 EFD - DURING LINE CHECK INSPECTION, THE AIRSTAIR DOOR EMERGENCY LIGHT WAS FOUNDTO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED LGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300584 19990723 00584 SO 1999 7 23 C2XA99IA331 1 19990616 A 2150 22045402 COOLING TURBINE EMB 120 EMB120RT SO FUSELAGE INOPERATIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 09 15730 120187 IAH - FLT 3578 - THE CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. M AINTENANCE REMOVED AND REPLACED THE LEFT COOLING TURBINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999072300585 19990723 00585 EU 1999 7 23 C2XA99IA335 1 19990618 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTS HAD THREE BULBS NOT ILLUMINATI NG. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300586 19990723 00586 WP 1999 7 23 HALA9900143 1 19990624 A 2170 COALESCER DOUG DC10 DC1010 3022110 WP CABIN DIRTY A HALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 13 160AA 46710 FLT 1 - LAX - CLOSE TO TOP OF CLIMB FA CALLED AND SAID SMOKE IN ALL CABINS PERFORMED CHECKLIST AND RETURNED TO LAX. SMO KE CLEARED ON THE WAY BACK TO LAX. REPLACED ALL 3 COALESCER BAGS RAN ENGINES AND APU FOR LEAK CHECK COULD NOT DUPLICATE ON GROUND. OPS NORMAL, NO LEAKS FOUND. (M) 2 L 7 3 4F A22WE 1999072300587 19990723 00587 NM 1999 7 23 AALA990865 1 19990610 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 1918 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - CORROSION ON LEFT CENTER GALLEY SUPPORT (NEAR FORWARD GALLEY TIE DOWN) AT STATION 1918L. REMOVED CORROSION, BLEND ED AREA, TREATED, PRIMED AND PAINTED PER ESO41000 DATED 6-10-99. (M) 2 L 7 3 4F RT A22WE 1999072300588 19990723 00588 NM 1999 7 23 AALA990866 1 19990610 A 5312 BULKHEAD ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - FOUND CORROSION ON AFT BULKHEAD 'T' ANGLE AT FLOORLINE IN AND OF RIGHT GALLEY SUPPORT ATTACH (36 INCH TO 42 INCH O UTBOARD OF CENTERLINE). REPAIRED PER ESO41000, DATED 06/10/99. (M) 2 L 7 3 4F RT A22WE 1999072300589 19990723 00589 WP 1999 7 23 AALA990934 1 19990623 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1003 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 583AA 53160 TUL - EXTERNAL LONGERON CRACKED AT STATINO 1003, LONGERON 26R. REMOVED AND REPLACED WITH EXTERNAL LONGERON FROM STATION 930 TO STATION 1003 PER STANDARD PRACTICES SRM 51-10 (LONGERON 26). (M) 2 L 7 2 4F A6WE 1999072300590 19990723 00590 WP 1999 7 23 AALA990937 1 19990618 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1309 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 583AA 53160 TUL - DEEP GOUGE IN FUSELAGE SKIN STATION 1309 LONGERON 19R APPROX 1 INCH LONG. INSTALLED DOUBLER PER SRM 53-04 FIG 3A. (M) 2 L 7 2 4F A6WE 1999072300591 19990723 00591 WP 1999 7 23 AALA990936 1 19990613 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1300-1304 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 583AA 53160 TUL - SEAT TRACK NR 2 HAS CORROSION, STATION 1300-1304. REPLACED SEAT TRACK SECTION FROM STATION 126 TO 1304 PER SRM 53 -05. (M) 2 L 7 2 4F A6WE 1999072300592 19990723 00592 WP 1999 7 23 AALA990935 1 19990613 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1300-1304 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 583AA 53160 TUL - NR 3 SEAT TRACK CORRODED STATION 1300-1304. INSTALLED NEW SEAT TRACK SECTION FROM STATION 1260 TO 1304 PER SRM 53 -05. (M) 2 L 7 2 4F A6WE 1999072300593 19990723 00593 NM 1999 7 23 AALA990944 1 19990627 A 3350 B973521385 LIGHT BOEING 767 767323 1385205 NM ROW 41B DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39356 24037 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 41B INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIG HT ASSEMBLY AT SEAT 41B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300594 19990723 00594 NM 1999 7 23 AALA990945 1 19990626 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 4 HJ LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH MARKER LIGHT INOPERATIVE AT SEAT 4HJ. RESEATED CONNECTOR AT SEA T 4HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300595 19990723 00595 NM 1999 7 23 AALA990946 1 19990626 A 3350 0201922001 SOCKET BOEING 767 767323 1385205 NM ROW 28 HJ DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 28HJ INOPERATIVE. REPLACED EMERGENCY EXIT PATH LI GHT SOCKET AT SEAT 28HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300596 19990723 00596 NM 1999 7 23 AALA990903 1 19990620 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 685AA 25342 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED WIRING ON EME RGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999072300597 19990723 00597 NM 1999 7 23 AALA990901 1 19990619 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 644AA 24602 MIA - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED RIGHT OVERWING EMERGENCY E XIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999072300598 19990723 00598 NM 1999 7 23 AALA990931 1 19990623 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 27-36 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 360AA 24041 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SEAT PATH LIGHTS AT ROW 27H AND 36H INOPERATIVE. SECURED EMERGENCY EX IT SEAT PATH LIGHT CONNECTOR AT 27H AND 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300599 19990723 00599 NM 1999 7 23 AALA990908 1 19990720 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON FUSELAGE SKIN OUTBOARD SIDE OF STRINGER 26L FROM STATION 720D PLUS 10 INCH TO 720E. INSTALLED NEW FILLER DOUBLER PER ESO 11697, DATED 9-3-99. (M) 2 L 7 3 4F A3WE 1999072300600 19990723 00600 WP 1999 7 23 AALA990941 1 19990622 A 2170 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 578AA 53155 BFL - FLT 1768 - EN ROUTE BFL-DFW, AFTER TAKEOFF FLIGHT, ATTENDANTS REPORTED FUMES AND SMOKE IN AFT CABIN. SMELLED LIKE POSSIBLE BURNING OIL/HYDRAULIC FLUID. DECLARED AN EMERGENCY, RETURNED BFL, AND LANDED WITHOUT INCIDENT. AIRCRAFT HAS BEEN INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM BFL TO LAX FOR FURTHER EVALUATION OF AIR CONDITIO NING SYSTEM. AT LAX, PERFORMED PAC BURNOUT PER MM. NO SMOKE OR FUMES NOTICED. GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999072300601 19990723 00601 WP 1999 7 23 AALA990909 1 19990618 A 3260 5963254501 PISTON DOUG DC9 DC982 3022082 WP NLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 482AA 49675 DFW - FLT 1203 - AFTER TAKEOFF DFW, LANDING GEAR WOULD NOT RETRACT, FLAPS ORAL WARNING, AUTO SPOILER DO NOT USE LIGHT IL LUMINATED, PRESSURIZATION MALFUNCTION. GROUND SHIFT MECHANISM APPEARED NOT TO OPERATE NORMALLY. RETURNED AND LANDED DF W WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR PISTON AND CYLINDER ASSEMBLY. LUBED NOSE LANDING GEAR, SERVICED NOSE LA NDING GEAR STRUT, PERFORMED NOSE LANDING GEAR SWING. CYCLED SEVERAL TIMES. NOSE LANDING GEAR OPERATIONS CHECK AND LEAK CHECKS NORMAL. TAXIED AIRCRAFT FOR GROUND CHECK. AIRCRAFT TAXIED NORMAL. NOSE LANDING GEAR STEERING OPERATIONS CHECK S NORMAL, RUDDER STEERING OPERATIONS CHECK NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999072300602 19990723 00602 WP 1999 7 23 AALA990940 1 19990624 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 467AA 49597 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS BY FIRST CLASS INOPERATIVE. REP AIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP BY FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 1999072300603 19990723 00603 WP 1999 7 23 AALA990907 1 19990619 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 224AA 49174 DFW - DURING OVERNIGHT MAINTENANCE, STAIRWELL EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED LOOSE CONNECTOR ON STAIRWELL E MERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999072300604 19990723 00604 WP 1999 7 23 AALA990902 1 19990620 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70504 49798 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AFT CABIN INOPERATIVE. REPAIRED WIRING ON EMERGENC Y EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999072300605 19990723 00605 NM 1999 7 23 AALA990890 1 19990615 A 2612 80380303 FIRE DETECTION DOUG MD11 MD11 3023602 NM NR 3 ENGINE DEFECTIVE A AALA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 07 1766A 48597 MIA - FLT 901 - EN ROUTE MIA-EZE - AFTER TAKEOFF CREW RECEIVED NR 3 ENGINE FIRE WARNING. SHUT ENGINE DOWN, RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED LOWER CASE LOOP 'A' DETECTOR AND FIRE DETECTION UNIT. NR 3 ENGINE WAS LEAK CHEC KED TO CONFIRM NO DUCT LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999072300606 19990723 00606 EU 1999 7 23 AALA990840 1 19990524 A 2897 WIRE AIRBUS 300 A300B4605R 3930308 EU E/E COMPT LOOSE A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 70072 515 JFK - FLT 1540 - EN ROUTE JFK-PAP - DURING CRUISE LEFT INNER FUEL QTY DROPPED BY 10,000 LBS AND REMAINED LOW THE REMAINE DER OF THE FLIGHT. WHEN LEFT INNER FUEL TANK REACHED ZERO, XX'S WERE DISPLAYED FOR REMAINDER OF FLIGHT. LANDED JFK WIT HOUT INCIDENT. RESECURED LOOSE HI-Z TERMINAL ON NR 4 PROBE. CAPACITY TEST CHECKS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300607 19990723 00607 EU 1999 7 23 AALA990784 1 19990530 A 2560 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EVAC HORN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 JFK - DURING OVERNIGHT MAINTENANCE, L3 EVACUATION SIGNAL PANEL INOPERATIVE. SECURED CONNECTOR ON EVACUATION HORN. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300608 19990723 00608 NM 1999 7 23 AALA990706 1 19990513 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM ROW 21-34 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1756 48491 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PROXIMITY LIGHT INOPERATIVE FROM SEAT ROW 21G THROUGH 34G. REPAIRED EMERGENCY EXIT FLOOR PROXIMITY CONNECTOR AT SEAT ROW 21G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999072300609 19990723 00609 NM 1999 7 23 AALA990779 1 19990529 A 3397 WIRE DOUG MD11 MD11 3023602 NM ROW 6-8 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1767A 48598 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN SEATS 6H AND 8G INOPERATIVE. REPAIRED SP LICES ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP BETWEEN SEATS 6H AND 8G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999072300610 19990723 00610 NM 1999 7 23 AALA990766 1 19990525 A 3397 WIRE DOUG MD11 MD11 3023602 NM 3L DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1758B 48527 DFW - DURING OVERNIGHT CHECK 3L DOOR MOUNTED EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT SIGN AT 3 L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999072300611 19990723 00611 EU 1999 7 23 AALA990658 1 19990504 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 21-24 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14056 463 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 4R SET ROWS 21H THROUGH 24H INOPERATIVE. MAINTENANCE FOUND A FAULTY CONNECTOR. REPLACED STRIP CONNECTOR AT PASSENGER SEAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300612 19990723 00612 EU 1999 7 23 AALA990657 1 19990504 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU 4R DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14056 463 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 4R DOOR INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR. RESECURED LOOSE CONNECTOR AT 4R JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300613 19990723 00613 EU 1999 7 23 AALA990673 1 19990507 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 17A LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70072 515 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17H INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 17H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300614 19990723 00614 EU 1999 7 23 AALA990639 1 19990429 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14068 511 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT ON RIGHT SIDE OF COACH CABIN INOPERATIVE. MAINTENAN CE FOUND A LOOSE CONNECTOR IN ZONE C-SHORTING EMERGENCY EXIT PATH LIGHTS. RESECURED LOOSE CONNECTOR TO EMERGENCY EXIT L IGHTS IN ZONE C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300615 19990723 00615 EU 1999 7 23 AALA990644 1 19990502 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU L2 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80057 465 SJU - EMERGENCY EXIT SIGN AT 2L DOOR INOPERATIVE. MAINTENANCE FOUND CANNON PLUG LOOSE AT BATTERY PACK. RESEAT CANNON P LUG AT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300616 19990723 00616 EU 1999 7 23 AALA990643 1 19990430 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 15-25 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 11060 470 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEAT ROWS 15B THROUGH 25B WERE INOPERATIVE. RESEATED EMERGENCY FLOOR PATH LIGHT WIRE CONNECTOR AT SIDEWALL SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300617 19990723 00617 EU 1999 7 23 AALA990692 1 19990511 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROW 26 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14068 511 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER ROW 26 CENTER SEAT INOPERATIVE. REPLACED EMERGENC Y EXIT LIGHT ASSEMBLY IN SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300618 19990723 00618 EU 1999 7 23 AALA990696 1 19990512 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROW 20-23 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROW 20H THROUGH 23H INOPERATIVE. REPLACED EMERGE NCY EXIT PATH LIGHT STRIP AT SEAT ROW 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300619 19990723 00619 EU 1999 7 23 AALA990768 1 19990526 A 3350 P2010031303 LIGHT ASSY AIRBUS 300 A300B4605R 3930308 EU 2L DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90070 513 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 2L DOOR FAILED EMERGENCY TEST. REPLACED EMERGENCY EXIT LIGH T ASSEMBLY AT 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300620 19990723 00620 EU 1999 7 23 AALA990770 1 19990526 A 3350 P2010031303 LIGHT ASSY AIRBUS 300 A300B4605R 3930308 EU 2L DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90070 513 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT 2L DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300621 19990723 00621 EU 1999 7 23 AALA990832 1 19990605 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 12-15 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 19059 469 JFK - DURING OVERNIGHT MAINTENANCE, LEFT SIDE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 12-15 INOPERATIVE. SECURED EMERGE NCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300622 19990723 00622 EU 1999 7 23 AALA990834 1 19990606 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU 4L DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 4L DOOR INOPERATIVE. REPLACED WIRING FROM SIDEWALL TO EMER GENCY EXIT LIGHT STRIP AT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300623 19990723 00623 EU 1999 7 23 AALA990850 1 19990604 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80052 460 MIA - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE ON RIGHT S IDE OF EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300624 19990723 00624 EU 1999 7 23 AALA990724 1 19990519 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROW 21-23 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7055A 462 JFK - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEATS 21B AND 23B INOPERATIVE. REPLACED EME RGENCY EXIT FLOOR PATH LIGHT STRIP AND CONNECTOR BETWEEN SEATS 21B AND 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F RT A35EU 1999072300625 19990723 00625 EU 1999 7 23 AALA990736 1 19990522 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU L3 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70072 515 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SELF TEST AT L3 DOOR INOPERATIVE. SECURED LOOSE CONNECTOR ON O VERHEAD CEILING LIGHT AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300626 19990723 00626 EU 1999 7 23 AALA990735 1 19990522 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 20AB BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7083A 645 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOR PATH LIGHTS AT 20AB INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH L IGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999072300627 19990723 00627 NM 1999 7 23 AALA990871 1 19990615 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 21-24 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 360AA 24041 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 21A-24B INOPERATIVE. SECURED WIRING ON BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300628 19990723 00628 NM 1999 7 23 AALA990861 1 19990614 A 3350 S417T5003 LIGHT ASSY BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39365 24046 SFO - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT OVERWING EM ERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300629 19990723 00629 NM 1999 7 23 AALA990798 1 19990601 A 3350 0201922001 SOCKET BOEING 767 767223 1385123 NM ROW 8B DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330AA 22330 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING AT 8B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT P ATH LIGHT SOCKET AT SEAT 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300630 19990723 00630 NM 1999 7 23 AALA990776 1 19990527 A 3350 CONNECTOR BOEING 767 767223 1385123 NM ROW 30 A/B DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 335AA 22333 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING INOPERATIVE AT 30 A/B. REPLACED CONNECTOR FOR EME RGENCY EXIT FLOOR PATH LIGHTING AT SEAT 30 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300631 19990723 00631 NM 1999 7 23 AALA990820 1 19990603 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 685AA 25342 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. SPLICED WIRE ON FIRST CLASS EMERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999072300632 19990723 00632 NM 1999 7 23 AALA990835 1 19990606 A 3350 S283N00219 LIGHT ASSY BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 648AA 24606 DFW - DURING OVERNIGHT MAINTENANCE, AFT RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED AFT RIGHT EMERGENCY EX IT LIGHT ASSY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999072300633 19990723 00633 NM 1999 7 23 AALA990843 1 19990608 A 3350 S417T5003 LIGHT BOEING 767 767323 1385205 NM GALLEY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358AA 24039 MIA - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY RIGH T EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999072300634 19990723 00634 NM 1999 7 23 AALA990855 1 19990610 A 3397 WIRE BOEING 757 757223 1384957 NM EMER EXIT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 630AA 24588 DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE ON LEFT SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999072300635 19990723 00635 EU 1999 7 23 FJT99069401 1 19990619 A 3251 618212 ACTUATOR BAG JETSTM JETSTM3201 1500217 EU NLG STEERING FAILED A FJTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 03 940AE 940 AIRCRAFT WAS TAXIING FROM GATE, LOST NOSE WHEEL STREERING. AIRCRAFT TAXIED BACK TO GATE USING DIFFERENTIAL POWER. INSP ECTION REVEALED THAT THE STEERING ACTUATOR SHAFT HAD SHEARED AT THE ROD END. PART SHALL BE RETURNED TO VENDOR FOR EVALU ATION/REPAIR. THE AIRCRAFT WAS FERRIED TO BNA FOR MAINTENANCE. THE ACTUATOR ASSY WAS REPLACED AND THE AIRCRAFT RETURNE D TO SERVICE WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4T RT A56EU 1999072300636 19990723 00636 NM 1999 7 23 USAA990545 1 19990529 A 5320 ANGLE BOEING 737 7373B7 1384580 NM STA 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND 40 INCH CORROSION AT Z-ANGLE AT BS 947 TO 986. CORROSION LEVEL 1, CORROSION TASK NR C53-1 07-02. REPLACED Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999072300637 19990723 00637 NM 1999 7 23 USAA990544 1 19990529 A 5320 ANGLE BOEING 737 7373B7 1384580 NM BS 947-986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND 1 INCH BY 39 INCH CORRODED AREA AT Z-ANGLE AT STATION 947 TO 986. CORROSION LEVEL 1, CORR OSION TASK NR C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999072300638 19990723 00638 NM 1999 7 23 USAA990543 1 19990529 A 5320 MOUNT BOEING 737 7373B7 1384580 NM BS 1012 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q4 CHECK, FOUND 2 INCH DIAMETER CORRODED AREA AT AFT OUTBOARD LAV MOUNT AT STATION 1012, RBL 37, FLOOR LEVE L. CORROSION LEVEL 1, CORROSION TASK NR C53-107-02. REPLACED SUPPORT MOUNT PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999072300639 19990723 00639 NM 1999 7 23 USAA990542 1 19990529 A 5320 T-CAP BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND .5 INCH CORRODED AREA SEVERAL PLACES AT T-CAP AT BS 1016 LBL 28-33. CORROSION LEVEL 1. I NSTALLED T-CAP REPAIR PER SRM 53-00-51 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999072300640 19990723 00640 NM 1999 7 23 USAA990541 1 19990529 A 5320 STRAP BOEING 737 7373B7 1384580 NM BS 1016-1038 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND 2 INCH BY 14 INCH AREA OF CORROSION AT STRAP AT STATION 1016 TO 1038, WL 3 FLOOR LEVEL. C ORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED STRAP WITH IDENTICAL PAR PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1999072300641 19990723 00641 NM 1999 7 23 USAA990540 1 19990529 A 5320 BEAM BOEING 737 7373B7 1384580 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q4 CHECK, FOUND PREVIOUS BLEND OUT TOP OF T-CAP ON BEAM AT STATION 328 LBL 49, WL 208. INSTALLED REPAIR DO UBLERS AND SPLICE OT CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999072300642 19990723 00642 NM 1999 7 23 USAA990615 1 19990616 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 41055 22959 CLT - DURING RON CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK AT STATION 727D PLUS 15 TO 727D PLUS 19 PARALLEL AND JUST ABOVE STRINGER 24R FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999072300643 19990723 00643 NM 1999 7 23 USAA990598 1 19990617 A 5240 6545871523 SKIN BOEING 737 737301 1384611 NM SERVICE DOOR CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 40551 23228 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT FORWARD LOWER RADIUS AND .125 INCH CRACK AT FASTEN ER ABOVE HINGE CUTOUT FORWARD SERVICE DOOR SKIN. INSTALLED DOUBLER PER EA 64745. (M) 2 L 7 2 4F RT A16WE 1999072300644 19990723 00644 NM 1999 7 23 USAA990597 1 19990617 A 5240 6545871523 SKIN BOEING 737 737301 1384611 NM SERVICE DOOR CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 40551 23228 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .281 INCH CRACK AT FORWARD SERVICE DOOR SKIN UPPER AFT CORNER OF UPPE R HINGE CUTOUT ON EXTERIOR DOOR SKIN. INSTALLED REPAIR DOUBLER PER SB 52-1096. (M) 2 L 7 2 4F RT A16WE 1999072300645 19990723 00645 NM 1999 7 23 USAA990600 1 19990617 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 40551 23228 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK IN SKIN FUSELAGE STATION 380 DIRECTLY AFT OF EQUIP CO OLING DUCT CUTOUT. INSTALLED REPAIR DOUBLER PER TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 1999072300646 19990723 00646 NM 1999 7 23 USAASB9918 1 19990502 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 270AU 22882 CLE - MAINTENANCE FOUND THE CENTER CABIN CEILING EMERGENCY EXIT SIGN LIGHT DIM. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999072300647 19990723 00647 NM 1999 7 23 USAASB99153 1 19990623 A 3610 39268631 REGULATOR BOEING 737 737201 1384454 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 243US 50407 22445 TPA - FLT 2636 - ON CLIMB-OUT FROM TPA, CAPT OBSERVED A DUCT PRESSURE OF OVER 100 PSI ON THE RIGHT SIDE AND 40 PSI ON TH E LEFT SIDE. THE NR 5 LEADING EDGE SLAT TRANSIT LIGHT WAS ALSO ILLUMINATED. CREW CYCLED LEADING EDGE SLATS TWICE BUT L IGHT WOULD NOT EXTINGUISH. VISUAL LOOK AT SLATS SHOWED A SLIGHT SPLIT. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITH OUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR PRESSURE R EGULATOR. OPERATIONAL TEST OF BLEED SYSTEM GOOD. ALSO, REMOVED AND REPLACED THE NR 5 LEADING EDGE SLT ROD END ASSY (P/ N 65-44651-12). OPERATIONAL CHECK AND INDICATION CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999072300648 19990723 00648 NM 1999 7 23 USAASB99144 1 19990614 A 4950 32036221 VALVE BOEING 737 737201 1384454 NM APU FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 254AU 22796 BWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUI CK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE AP U FAILED TO START. FLIGHT DIVERTED TO BWI DUE TO THE AIRCRAFT BEING DOWN TO ONE ELECTRICAL POWER SOURCE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU THREE WAY SOLENOID VALV E. OPERATIONAL CHECK NORMAL. ALSO, REMOVED AND REPLACED NR 1 ENGINE CSD (P/N 731753) AND OIL COOLER (P/N 10-61233-1). GROUND RAN ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999072300649 19990723 00649 NM 1999 7 23 99ZZZM392 1 19990614 A 2410 731753 CSD BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 254AU 22796 BWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUI CK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE AP U FAILED TO START. FLIGHT DIVERTED TO BWI DUE TO THE AIRCRAFT BEING DOWN TO ONE ELECTRICAL POWER SOURCE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU THREE WAY SOLENOID VALV E. OPERATIONAL CHECK NORMAL. ALSO, REMOVED AND REPLACED NR 1 ENGINE CSD (P/N 731753) AND OIL COOLER (P/N 10-61233-1). GROUND RAN ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999072300650 19990723 00650 NM 1999 7 23 99ZZZM393 1 19990614 A 7921 10612831 OIL COOLER BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 254AU 22796 BWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUI CK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE AP U FAILED TO START. FLIGHT DIVERTED TO BWI DUE TO THE AIRCRAFT BEING DOWN TO ONE ELECTRICAL POWER SOURCE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU THREE WAY SOLENOID VALV E. OPERATIONAL CHECK NORMAL. ALSO, REMOVED AND REPLACED NR 1 ENGINE CSD (P/N 731753) AND OIL COOLER (P/N 10-61233-1). GROUND RAN ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999072300651 19990723 00651 NM 1999 7 23 USAASB99150 1 19990620 A 2897 CN0940137 WIRE HARNESS BOEING 737 7372B7 1384560 NM WING FUEL TANKS FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 268AU 22880 RDU - FLT 2826 - EN ROUTE FROM MCO TO BOS, DURING CRUISE, CAPT REPORTED PROBLEMS WITH THE NR 2 FUEL GAUGE. GAUGE WAS UN RELIABLE WITH ITS READINGS AND THE NR 1 FUEL GAUGE WAS ALREADY ON MEL. CREW TRIED RESETTING CIRCUIT BREAKER WITH NO HEL P. THE NR 2 FUEL GAUGE DROPPED TO 6,400 LBS AND CAPT DID NOT FEEL COMFORTABLE CONTINUING ON TO BOS. FLIGHT DIVERTED TO RDU AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 WING TANK HARNESS AND BUSSING PLUG ASSEMBLIES PER MM 28-41-101. OPS CHECK OF FUEL QTY SYSTEM CHECKS GOOD. (M) 2 L 7 2 4F A16WE 1999072300652 19990723 00652 NM 1999 7 23 USAA069963 1 19990626 A 3610 652673821 TUBE BOEING 727 727227 1384078 NM NR 2 ENGINE LOOSE A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 19 925TS 21244 FLT 6041 - BOS-LGA - AIR RETURN BOS, NR 2 ENGINE FIRE WARNING IN FLIGHT. SECURED AND RETORQUED LOOSE 13TH STAGE BLEED A IR TUBE AT CSD EJECTOR SHUTOFF VALVE. THROTTLE REDUCED TO IDLE, ENGINE WAS THEN SHUT DOWN. (M) 2 L 7 3 4F A3WE 1999072300653 19990723 00653 NM 1999 7 23 USAASB99149 1 19990618 A 2150 3219421 VALVE BOEING 737 7373B7 1384580 NM RT PACK FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 389US 23311 LGA - FLT 2323, ON CLIMB-OUT FROM LGA, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO FIELD AT LGA AND LANDED WI THOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT PACK 35 DEGREES SHUTOFF VALVE HAD FAILE D CLOSED. REMOVED AND REPLACED RIGHT PACK 35 DEGREE SHUTOFF VALVE AND TEMPERATURE CONTROL BOX. LEAK CHECK AND OPERATIO NAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999072300654 19990723 00654 NM 1999 7 23 99ZZZM394 1 19990618 A 2160 6075102 TEMP CONTROL BOEING 737 7373B7 1384580 NM RT PACK FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 389US 23311 LGA - FLT 2323, ON CLIMB-OUT FROM LGA, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO FIELD AT LGA AND LANDED WI THOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT PACK 35 DEGREES SHUTOFF VALVE HAD FAILE D CLOSED. REMOVED AND REPLACED RIGHT PACK 35 DEGREE SHUTOFF VALVE AND TEMPERATURE CONTROL BOX. LEAK CHECK AND OPERATIO NAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999072300655 19990723 00655 NM 1999 7 23 USAASB99143 1 19990614 A 2613 CONNECTOR BOEING 737 737301 1384611 NM NR 2 ENGINE CORRODED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 590US 23935 JAX - FLT 1469 - DURING CRUISE, AT APPROXIMATELY FL 350, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ELECTED TO DI VERT TO THE NEAREST STATION AT JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO ENGINE SHUTDOWN OCCURRED NOR WAS AN EME RGENCY DECLARED. MAINTENANCE FOUND PIN NR 17 O THE FIREWALL DISCONNECT CONNECTOR D406 (P/N BACC63BR28B42P6L), PARTIALLY PUSHED BACK AND CORRODED. CLEANED AND REPOSITIONED PIN. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999072300656 19990723 00656 NM 1999 7 23 USAA069965 1 19990627 A 2782 1U110322 ACTUATOR RONSON BOEING 727 727225 1384077 NM NR 5 L/E SLAT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 19 923TS 35850DFLMN 20441 FLT 6051 - BOS-LGA - AIR RETURNED TO BOS ON TAKEOFF, INBOARD FLAP ASYMMETRY TRIP. NR 5 L/E SLAT LIGHT SHOWED AMBER. AC COMP ASYMMETRICAL FLAP ABNORMAL CHECKLIST, RETURNED TO BOS. ALL FLAPS EXTENDED ON LANDING. FOUND RIGHT INBOARD FLAP TR ANSMITTER STICKING ON RETRACTION. REPLACED RIGHT INBOARD FLAP POSITION TRANSMITTER. REMOVED AND REPLACED NR 5 L/E SLAT ACTUATOR. OPERATION OF T/E FLAPS AND NR 5 L/E SLAT ACTUATOR CHECKS OK. (M) 2 L 7 3 4F A3WE 1999072300657 19990723 00657 NM 1999 7 23 USAA069964 1 19990625 A 2910 6517844335 TUBE BOEING 727 727225 1384077 NM 'A' HYD SYSTEM BROKE A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 918TS 20445 SYSTEM 'A' SYSTEM HYDRAULIC FAILURE OCCURRED DURING FLAP RETRACTION. FOUND TWO BROKEN HYDRAULIC TUBES IN LEFT AFT STAIR WELL. IPC 29-15-01G, ITEMS NR 375 AND 270. REPLACED SAME AND PERFORMED HYDRAULIC SYSTEM 'A' TROUBLESHOOTING PER MM 29 -11-0, PAGE 101. CHECKED ALL FILTERS PER MM 29-11-62, 29-11-41 AND 29-11-101. NO METAL FOUND. SERVICED RESERVOIR PER GMM 8-13. LEAK AND OPERATIONAL CHECKS OK. (M) 2 L 7 3 4F A3WE 1999072300658 19990723 00658 NM 1999 7 23 99ZZZM395 1 19990625 A 2910 6517844315 TUBE BOEING 727 727225 1384077 NM 'A' HYD SYSTEM BROKE A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 918TS 20445 SYSTEM 'A' SYSTEM HYDRAULIC FAILURE OCCURRED DURING FLAP RETRACTION. FOUND TWO BROKEN HYDRAULIC TUBES IN LEFT AFT STAIR WELL. IPC 29-15-01G, ITEMS NR 375 AND 270. REPLACED SAME AND PERFORMED HYDRAULIC SYSTEM 'A' TROUBLESHOOTING PER MM 29 -11-0, PAGE 101. CHECKED ALL FILTERS PER MM 29-11-62, 29-11-41 AND 29-11-101. NO METAL FOUND. SERVICED RESERVOIR PER GMM 8-13. LEAK AND OPERATIONAL CHECKS OK. (M) 2 L 7 3 4F A3WE 1999072300659 19990723 00659 NM 1999 7 23 EISA99121 1 19990522 A 2751 1812993 INDICATOR BOEING 727 7272A7 138407K NM TE FLAPS FAILED A EISA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 310NE 0081A 20241 CREW HAD SPLIT INDICATOR DECLARED EMERGENCY AND MADE GO AROUND. CHECKED FLAP OPERATION. REPLACED OUTBOARD FLAP INDICAT OR AND OPS CHECKED OK. (M) 2 L 7 3 4F A3WE 1999072300660 19990723 00660 NM 1999 7 23 EISA99123 1 19990524 A 5312 6586350344 BULKHEAD WEB BOEING 727 727223 1384074 NM BS 1183 GOUGED A EISA K NONE O OTHER CL CLIMB 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 1 8.2 TO RBL 18.2 (31 PLACES). REMOVED DAMAGED AREAS AND INSTALLED PERMANENT REPAIR PER ENGINEERING AUTHORIZATION (EA) NR 7-5310-77-C1529 AND FLIGHT VEHICLES ENGINEERING DRAWING NR 53-99260-1. (M) 2 L 7 3 4F A3WE 1999072300661 19990723 00661 NM 1999 7 23 99ZZZM396 1 19990524 A 5312 6586350339 BULKHEAD WEB BOEING 727 727223 1384074 NM BS 1183 GOUGED A EISA K NONE O OTHER CL CLIMB 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 1 8.2 TO RBL 18.2 (31 PLACES). REMOVED DAMAGED AREAS AND INSTALLED PERMANENT REPAIR PER ENGINEERING AUTHORIZATION (EA) NR 7-5310-77-C1529 AND FLIGHT VEHICLES ENGINEERING DRAWING NR 53-99260-1. (M) 2 L 7 3 4F A3WE 1999072300662 19990723 00662 NM 1999 7 23 EISA99114 1 19990501 A 5347 65571463 SEAT TRACK BOEING 727 727223 1384074 NM BS 480-520 DEFORMED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON SEAT TRACK NR 4 AT FS 480. REMOVED SECTION OF SEA T TRACK FROM FS 480-520 AND REPLACED WITH NEW SECTION PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999072300663 19990723 00663 NM 1999 7 23 EISA99097 1 19990401 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 690 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK, WORK CARD, SEAT TRACK CORRODED BEYOND LIMITS AT RIGHT OURBOARD TRACK AT FS 690 . REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999072300664 19990723 00664 NM 1999 7 23 EISA99089 1 19990408 A 5755 65727302 SKIN BOEING 727 727264 138408M NM NR 14 SPOILER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND RIGHT WING NR 14 SPOILER DELAMINATED ALONG TRAILING EDGE. REP AIR PERFORMED BY OUTSIDE VENDOR (THE NORDAM GROUP). REPAIRED ON AIRCRAFT 727 SRM CHAPTER 51-40-5, 53-30-3 FIGURE 12 AND 51-40-6 FIGURE 2. (M) 2 L 7 3 4F A3WE 1999072300665 19990723 00665 NM 1999 7 23 EISA99120 1 19990514 A 2611 5913311 CIRCUIT BREAKER BOEING 727 727223 1384074 NM P6 PANEL FAILED A EISA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 6819 19494 ON APPROACH, SMELLED SMOKE NOTICED NR 1 AFT AND NR 2 RT FORWARD CIRCUIT BREAKERS TRIPPED. VISUAL SMOKE NOTICED ON TAXI IN. INSPECTED ELECTRICAL SYSTEM FOR HEAT AND SMOKE DAMAGE. REPLACED BOTH CIRCUIT BREAKERS IAW MM 24-50-1. OPS CHECK G OOD. (M) 2 L 7 3 4F A3WE 1999072300666 19990723 00666 NE 1999 7 23 EISA99124 2 19990530 A 7230 COMPRESSOR BOEING 727 727223 1384074 NM PWA JT8 JT8D7 52053 NE NR 2 ENGINE STALLED A EISA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 07 6813 19488 653325 NR 2 ENGINE COMPRESSOR STALLS. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK GOOD. REPLACED 13TH STAGE SURGE BLEED VALV E. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999072300667 19990723 00667 NM 1999 7 23 EISA99122 1 19990523 A 2751 CONNECTOR BOEING 727 727223 1384074 NM TE FLAPS DIRTY A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 311NE 19703 DURING CLIMB WHILE RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES THE OUTBOARD FLAPS LOCKED OUT AT 4 DEGREES. THE INBOARD FLAPS WENT TO ZERO. CHECKED AND CLEANED CANNON PLUS ON FLAP POSITION TRANSMITTER, CLEANED AND LUBED JACK SCREWS, OPS C HECKED OK. (M) 2 L 7 3 4F A3WE 1999072300668 19990723 00668 SO 1999 7 23 C2XA99CL047 1 19990621 A 4990 168401201 APU EMB 120 EMB120RT SO AFT FUSELAGE LEAKING A C2XA K NONE K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 09 26714 120118 CLE - THE CREW REPORTED A SMOKE WARNING INDICATION ON THE MAP ALONG WITH SMOKE COMING FROM THE VENTS DURING FLIGHT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE DETERMINED THAT THE APU WAS LEAKING OIL AND RELEASE D THE AIRCRAFT ON MEL NR 49-00-01 PLACARD NR 175955. AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999072300669 19990723 00669 EU 1999 7 23 C2XA99IA344 1 19990624 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU ROW 62WL DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING SCHEDULED MAINTENANCE, THE EMERGENCY LIGHT BATTERY PACK AT POSTION 62WL WAS FOUND TO HAVE LOW VOLTAGE. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999072300670 19990723 00670 EU 1999 7 23 C2XA99IA343 1 19990623 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 IAH - FLIGHT 3315 - THE PILOT REPORTED THAT THE FORWARD EMERGENCY EXIT LIGHTS AND EXIT SIGN WERE INOPERATIVE. MAINTENAN CE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999072300671 19990723 00671 NE 1999 7 23 C2XA99IA342 2 19990623 A 7200 ENGINE AEROSP ATR42 ATR42500 EU PWA PW120 PW127 NE NR 1 FAILED A C2XA E ENGINE SHUTDOWN O OTHER UK UNKNOWN 1 SW 09 19446 504 PCEAM0041 IAH - FLT 3366 - DURING FLIGHT, THE CREW REPORTED A THUMPING NOISE AND, ENGINE SURGES COMING FROM THE NR 1 ENGINE. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED T HE NR 1 ENGINE AND FOUND AN UNACCEPATABLE AMOUNT OF DEBRIS ON THE ENIGNE CHIP DETECTOR. MAINTENANCE REMOVED AND REPLACE D THE NR 1 ENGINE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999072300672 19990723 00672 EU 1999 7 23 C2XA99IA341 1 19990623 A 3350 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING 4A INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300673 19990723 00673 EU 1999 7 23 C2XA99IA340 1 19990623 A 3350 7007552 FUSE AEROSP ATR42 ATR42320 8680930 EU ROW 8WL FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING 4A INSPECTION, THE EMERGENCY LIGHT AT 8WL WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED POWER SUPPLY FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300674 19990723 00674 EU 1999 7 23 C2XA99IA339 1 19990622 A 3350 OL3042BPE BULB AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED BULB AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300675 19990723 00675 SO 1999 7 23 C2XA99IA338 1 19990621 A 3350 GE1317 BULB EMB 145 EMB145LR SO EMERGENCY EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16951 145063 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999072300676 19990723 00676 SO 1999 7 23 C2XA99IA337 1 19990616 A 3350 110049 BATTERY CHARGER EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14937 145026 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVIEC. (M) 2 L 7 2 4F RT T00011AT 1999072300677 19990723 00677 EU 1999 7 23 C2XA99BT064 1 19990628 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU ROW 10WL FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15827 175 BTV - FLT 3680 - DURING 2A INSPECTION, MAINTENANCE FOUND FORWARD LEFT, RIGHT AND REAR RIGHT EXTERIOR EMERGENCY LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY FUSE AT LOCATION 10WL. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999072300678 19990723 00678 SO 1999 7 23 C2XA99BT063 1 19990626 A 3350 APS1B BATTERY CHARGER EMB 145 EMB145LR SO NR 1/4 FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14953 145071 EWR - FLT 4201 - LEFT AND RIGHT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND BOTH NR 1 AND NR 4 BATTERY CHARGER ASSY TO BE FAULTY. REMOVED AND REPLACED WITH SERVICEABLE UNITS, AND OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4T RT T00011AT 1999072300679 19990723 00679 SO 1999 7 23 C2XA99BT061 1 19990629 A 3350 SMOKE DETECTOR EMB 145 EMB145 SO BAGGAGE COMP FOD A C2XA O OTHER N FALSE WARNING LD LANDING 1 SW 09 14933 145018 BTV - MAINTENANCE TROUBLESHOT AND REPAIRED BAGGAGE SMOKE WARNING ON LANDING REPORT FROM CREW. FOUND SCREW STUCK IN BAGG AGE FORWARD SMOKE DETECTOR. REMOVED SCREW, OPS CHECKED SYSTEM GOOD AND RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999072300680 19990723 00680 EU 1999 7 23 SIMA991765 1 19990625 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING MBV-2 INSPECTION, FOUND CORROSION ON FLOORBEAM 36 AROUND NUTCLIPS. REMOVED AND REPLACED FLOORBEAM 36 IAW E O E2-53-00-029. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300681 19990723 00681 EU 1999 7 23 SIMA991764 1 19990625 A 5320 S53671217210 WEB AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT WEB FORWARD OF THE PASSENGER DOOR BETWEEN FRAMES 35 AND 36 ARE CORRODED. R EMOVED AND REPLACED THE WEB IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300682 19990723 00682 EU 1999 7 23 SIMA991731 1 19990622 A 5330 S5367120500605 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING MBV-2 INSPECTION, FOUND TWO DENTS IN THE LEFT SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 39 AND 42 AND STRING ERS 11 AND 12, MEASURING 1.27 BY .060 AND 1.37 BY .78 BY .056 INCHES. REPAIRED THE DENTS IAW SRM 53-00-00 FIGURE 403. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300683 19990723 00683 EU 1999 7 23 SIMA991732 1 19990622 A 5330 S5367140003405 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING MBV-2 INSPECTION, FOUND THREE DENTS IN THE LOWER SIDE OF THE FUSELAGE SKIN BETWEEN FRAMES 41 AND 43 AND STR INGERS 20 AND 21, MEASURING 2.17 BY 1.34 BY .080, AND 1.50 BY .058, AND 1.50 BY .052 INCHES. REPAIRED THE DENTS IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300684 19990723 00684 EU 1999 7 23 SIMA991766 1 19990625 A 5347 S53375001212 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATT ENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300685 19990723 00685 EU 1999 7 23 99ZZZM397 1 19990625 A 5347 S53375001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATT ENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300686 19990723 00686 EU 1999 7 23 99ZZZM398 1 19990625 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATT ENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300687 19990723 00687 EU 1999 7 23 99ZZZM399 1 19990625 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATT ENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300688 19990723 00688 EU 1999 7 23 99ZZZM400 1 19990625 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATT ENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300689 19990723 00689 EU 1999 7 23 99ZZZM401 1 19990625 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, RIGHT FLIGHT ATT ENDANT, AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999072300690 19990723 00690 EU 1999 7 23 SIMA991721 1 19990621 A 3320 6500100 SOCKET SAAB SF340 340B 7860101 EU ROW 14 FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 390AE 340B390 TXO - FLT 5247 - SMOKE IN THE CABIN COMING FROM OVERHEAD LIGHT AT SEAT 14. SMOKE WENT INTO CARGO AREA AND CAUSED CARGO SMOKE DETECTOR TO ILLUMINATE. DISCHARGED RIGHT CARGO FIRE EXTINGUISHER. ALSO, DISCHARGED BOTH CABIN FIRE EXTINGUISHERS . FERRIED AIRCRAFT TO DFW. REMOVED AND REPLACED LAMP HOLDER FOR OVERHEAD LIGHTING AT SEAT 14. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999072300691 19990723 00691 EU 1999 7 23 SIMA991711 1 19990620 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 283AE 340B283 DFW - FLT 3779 - TWO FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT FUSE. OPERATI ONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999072300692 19990723 00692 WP 1999 7 23 GTIA9900908 1 19990201 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-243 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FORWARD PASS CABIN FLOOR AT FS 200-243 RBL 21-42 LIGHT CORROSION AFTER CORROSION WAS REMOVED FOUND AREA TO BE OUT OF LIMITS REF CARD W144. REMOVED AREA MATERIAL ID 7075T6.040 PER SRM 53-10-0. FABRICATED REPAIR PARTS PER SRM 53-01 FI G 4 ALODINED AND PRIMED PER SRM 51-10-3. INSTALLED PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 1999072300693 19990723 00693 WP 1999 7 23 GTIA9900910 1 19990615 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 140 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - STATION 140X=PLUS 35 TO PLUS 52, 9 BY 18 INCH AREA OF CORROSION DEEP POTTING .5 INCH PUNCTURE AND SURFACE CORROSIO N NUMEROUS AREAS TOP SURFACE COCKPIT FLOORBOARD. REMOVED CORRODED WEB FROM LOCATION REMOVING ALL ATTACH FASTENERS FABRI CATED NEW FLOOR WEB WITH 7075-T6.025 MATERIAL REINSTALLED HAT CHANNELS WITH RIVETS ALODINE AND PRIMERED PER SRM 51-10-3 PAGE 16, PAGE 15 21E, 53-21-0 PAGE 4B, 4 4C, 51-20-0 PAGE 1, 51-30-2 PAGE 1. (M) 2 L 7 2 4F A6WE 1999072300694 19990723 00694 WP 1999 7 23 GTIA9900911 1 19990325 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 229 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - CABIN FS 229 LBL 52 SEVERE CORROSION EMANATING FROM BETWEEN MEMBRANE WEB AND T-ANGLE. REMOVED AND REPLACED WEB AS REQ PER SRM DC9 51-30-02, 51-30-0 NEW WEB'S AREAS MANUFACTURED ON WORK CARD NR A066B03 WEB ALODINED AND PRIMED IAW DC9 51-10-3. INSTALLED WEB IAW DC9 SRM 51-30-02 AND 51-30-08. (M) 2 L 7 2 4F A6WE 1999072300695 19990723 00695 WP 1999 7 23 GTIA9900913 1 19990205 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 980 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - AT STATION 980 LBL ONE FASTENER HOLE WAS FOUND TO BE OUT OF LIMITS AFTER CORROSION WAS REMOVED FROM SEAT TRACK REF W/O W195. CUT OUT DAMAGED AREA PER DC9 SRM 53-05 FIG 20A FABRICATED. EXTRUSION FILLER STEEL RUB STRIP TREATED PRIMED AREA PER DC9 SRM 51-10-3. INSTALLED FILLER STEEL RUB STRIP AND EXTRUSION PER DC9 SRM 53-05 FIG 20A AND INSTALLED FASTEN ERS IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1999072300696 19990723 00696 WP 1999 7 23 GTIA9900912 1 19990203 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-240 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FORWARD PASSENGER COMPARTMENT SEAT TRACK FS 200-240 HAS CORROSION AFT CORROSION WAS REMOVED FOUND AREA TO BE OUT O F LIMITS REF W/C 147. REMOVED AND REPLACED SEAT TRACK AS REQUIRED PER SRM 51-30-01 AND MANUFACTURED NEW TRACK IAW DC9 S RM 51-10-02 ALODINED AND PRIMED IAW 51-10-3. INSTALLED NEW TRACK IAW DC9 51-30-5 AND 51-30-1. (M) 2 L 7 2 4F A6WE 1999072300697 19990723 00697 WP 1999 7 23 GTIA9900914 1 19990206 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 211 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FS 211 R61 WEB HAS CORROSION AND BULGING AREA UNDER EXISTING REPAIR. REMOVED WEB AND DOUBLER FABRICATED NEW WEB P ER DC9 SRM 53-11-1 FIGURE 11 SHEET 1 AND 2 LOCATED AND DRILL HOLE TO EXISTING FASTENER HOLES ALODINED PER DC9 SRM 51-10- 3 PAGE 15 (22A) PRIMED PER DC9 SRM 51-10-3 PAGE 16 (24A). 2 L 7 2 4F A6WE 1999072300698 19990723 00698 WP 1999 7 23 GTIA9900915 1 19990208 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 293-313 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 TEMPORARY REPAIRS ON RIGHT SIDE FUSELAGE AT STATION 293 AND STATION 313. REMOVED TEMPORARY REPAIRS FROM RIGHT SIDE FUSE LAGE CUT OUT SECTION OF SKIN AND FABRICATED SKIN SECTION TITANUM DOUBLER AND INSTALLED USING HI-LOCK FASTENER AND SOLID RIVETS IAW ENG DRAWING 53-99034-3 AND CHAPTERS 53-00 51-00 OF THE DC9 SRM. (M) 2 L 7 2 4F A6WE 1999072300699 19990723 00699 WP 1999 7 23 GTIA9900916 1 19990209 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 211 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FS 211 R61 WEB AT 1.5 INCH LIGHTNING HOLE IS CRACKED AND HAS CORROSION THATS OUT OF LIMITS PER N/RW25. CUSP HAS B EEN REPLACED PER SRM 53-05-00 FIG 55 FASTENERS INSTALLATION PER SRM 51-30-2 AND SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1999072300700 19990723 00700 WP 1999 7 23 GTIA9900917 1 19990211 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 420 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - SEAT TRACK RIGHT SIDE OUTBOARD AT STAITON 420 IS CRACKED EXTENDING .250 FROM ONE OF THE TOP SURFACE HOLES. REMOVE D AND REPLACED OF SEAT TRACK FROM STATION 350 TO STATION 470 PER SRM 53-05 FIG 4F PAGE 10K. (M) 2 L 7 2 4F A6WE 1999072300701 19990723 00701 WP 1999 7 23 GTIA9900918 1 19990212 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 200 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - NO REPAIR FOUND IN THE SRM 53-00 FOR CRACK IN FRAME AT STATION 200 R16. CUT OUT DAMAGED AREA REINSTALLED WEB FABR ICATED AND INSTALLED DOUBLER AND TRIPLER BOEING ENGINEERING MSQ NR AVQ-MOJ-99-0005RR AND INSTALLED FASTENERS IAW DC9 SRM 51-30-2, 51-30-5, 51-30-8, REPAIR PARTS WERE FABRICATED IAW DC9 SRM 51-10-2 ALODINED AND PRIMED IAW DC9 SRM 51-10-3. ( M) 2 L 7 2 4F A6WE 1999072300702 19990723 00702 WP 1999 7 23 GTIA9900919 1 19990218 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218-229 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 TEMPORARY SKIN PANEL REPAIR AT STATION 218 TO 229 L-17 TO 18L. REMOVED SKIN AND REPLACED WITH FABRICATED SKIN AND DOUBL ERS IAW DC9 SRM 53-04 FIG 47. ALL PARTS WERE FAY SURFACE SEALED AND INSTALLED WITH WET FASTENERS IAW DC9 SRM 53-04 FIG 47 HI-LOCK WERE INSTALLED PER DC9 SRM 51-30-5 SOLID RIVETS WERE INSTALLED PER SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999072300703 19990723 00703 WP 1999 7 23 GTIA9900920 1 19990226 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 965 GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 REF PO88 - GOUGE ON SHEAR WALL WEB .010 DEEP MATERIAL .032 BEYOND LIMITS STATION 965 SBL. REMOVED DAMAGED WEB AND REPLA CED WITH NEW 991224-3 WEB INSTALLED FASTENERS PER DC9 SRM 51-30-1 FOR BOLTS 51-30-5 FOR HI-LOCKS 51-30-2 RIVETS. (M) 2 L 7 2 4F A6WE 1999072300704 19990723 00704 WP 1999 7 23 GTIA9900921 1 19990215 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 992 MISREPAIRED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 13512 48111 STATION 992 LEFT STRINGER 22-23 THERE IS A CLASS III SKIN REPAIR WITH CHERRY RIVETS INSTALLED ALSO NUMEROUS FASTENERS WI TH SHORT CENTER TO CENTER SPACING. REMOVED TEMP REPAIR FABRICATED DOUBLER TRIPLER AND FILLER TRIMMED OUT ADDITIONAL ARE A ALODINED AND PRIMED ALL AREAS INSTALLED DOUBLER TRIPLER AND FILLER WET WITH SEAL PER DC9 SRMS 51-10-3, 51-30-5, 51-10- 8, 51-10-4, 51-30-2, 51-30-8 AND ENG DRAWING NR 53-990344 REV 1 DATED 3-10-99. (M) 2 L 7 2 4F A6WE 1999072300705 19990723 00705 WP 1999 7 23 TWAA9910301 1 19990713 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 937-950 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL AT LONGERON 28R WITH INTERGRANULAR CORROSION BETWEEN STRINGER 937 AND 950. P ART MADE PER DRAWING 9957723. REPLACED INTERCOSTAL, INSTALLED WITH HI-LOKS, BECAUSE THEY WERE ORIGINAL FASTENER. 2 L 7 2 4F A6WE 1999072300706 19990723 00706 WP 1999 7 23 TWAA9910302 1 19990714 A 5730 SKIN DOUG DC9 DC931 3022065 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND RT WING UPPER WING SKIN CRACKED AT FUEL TANK ACCESS PLATE 1410A. HIGH FREQ EDDY CURRENT ACCOMP PER 51-00-03, PART 6. CRACK WAS CONTAINED AT PLATE ACCESS HOLE. REPAIRED PER SRM 57-03 FIG 23. 2 L 7 2 4F A6WE 1999072300707 19990723 00707 WP 1999 7 23 TWAA9910303 1 19990714 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP 16 MAINT CHECK, FOUND STA 965 LONGERON 17L WAS CRACKED AT LONGERON TO FORMER. CRACK APPROX .75 INCH LONG. RE PLACED LONGERON FROM STA 955 TO 990 PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1999072300708 19990723 00708 WP 1999 7 23 TWAA9910304 1 19990719 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 FOUND LONGERON 5R CRACKED AT STA 699, APPROX .375 INCH. CUT OUT DAMAGED AREA AND SPLICED IN NEW PER SRM 53-02 FIG 18. C HECK-C 1-5-99 STL. 2 L 7 2 4F A6WE 1999072300709 19990723 00709 WP 1999 7 23 TWAA9910305 1 19990719 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 680 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 FOUND LONGERON 5L CRACKED AT STA 680. SPLICED IN NEW LONGERON SECTION PER SRM 53-02 FIG 18. CHECK-C 1-5-99 STL. 2 L 7 2 4F A6WE 1999072300710 19990723 00710 WP 1999 7 23 TWAA9910306 1 19990719 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 FOUND LONGERON 5L CRACKED AT STA 699. SPLICED IN NEW LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 1-5-99 STL. 2 L 7 2 4F A6WE 1999072300711 19990723 00711 WP 1999 7 23 TWAA9910307 1 19990714 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1309-1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 DURING OP 16 MAINT CHECK, FOUND CORROSION ON INTERCOSTAL STA 1309 TO 1322, BETWEEN LONGERONS 27L AND 28L. REPLACED INTE RCOSTAL PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999072300712 19990723 00712 NM 1999 7 23 HNAA9900104 1 19990720 A 2611 82425002009 CONNECTOR DHC DHAV DHC8 DHC8201 2809001 NM CARGO SMOKE DET DIRTY A HNAA K NONE N FALSE WARNING CR CRUISE 1 EA 07 994HA 459 459 BAG SMOKE WARNING LIGHT FLICKERS IN FLIGHT. CLEANED AND RESEATED BOTH SMOKE DETECTORS C/P'S GROUND TEST GOOD. 2 H 7 2 4T RT A13NM 1999072300713 19990723 00713 NM 1999 7 23 RAAA99B1013 1 19990717 A 3350 873100212 SIGN BOEING 727 72722C 138400F NM EMER EXIT INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 LEFT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT WILL NOT TEST, LEDS REMAIN ON, DURING SERVICE CHECK. REPLACED EGRESS IDENTIFIER LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1999072300714 19990723 00714 NM 1999 7 23 RAAA99B1014 1 19990718 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 17 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 17 FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999072300715 19990723 00715 WP 1999 7 23 CALA9900836 1 19990719 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72824 49484 TAIL CONE DROP FAILED USING INTERIOR TAIL COMPARTMENT RELEASE HANDLE. THE TAIL CONE INTERIOR PULL WAS ADJUSTED WITHIN L IMITS IAW MM 53-50-00. 2 L 7 2 4F A6WE 1999072300716 19990723 00716 WP 1999 7 23 CALA9900837 1 19990720 A 5753 SKIN DOUG DC9 DC932 3022066 WP LT T/E FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND LT AFT FLAP DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3 AND 51-10-3. 2 L 7 2 4F A6WE 1999072300717 19990723 00717 WP 1999 7 23 CALA9900838 1 19990720 A 5754 SKIN DOUG DC9 DC932 3022066 WP NR 1 L/E SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17533 47281 INSPECTION FOUND LT WING NR 1 SLAT INNER SKIN GOUGED. THE FASTENERS AND DAMAGED AREA WERE REMOVED IAW SRM 57-09, PAGE 3 5. A NEW DOUBLER, FILLER AND STRAPS WERE INSTALLED IAW SRM 57-09 PAGE 35 AND 51-30-2 PAGE 2. 2 L 7 2 4F A6WE 1999072300718 19990723 00718 NM 1999 7 23 CALA9900839 1 19990720 A 5230 WEB BOEING 727 727224 1384076 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND TWO CRACKED WEBS AT FORWARD CARGO COMPARTMENT DOOR AFT EDGE. THE CRACKS WERE .5 INCH LONG. NEW WEBS W ERE INSTALLED IAW SRM 52-30-1 AND 51-30-2. 2 L 7 3 4F A3WE 1999072300719 19990723 00719 NM 1999 7 23 CALA9900840 1 19990720 A 5330 SKIN BOEING 727 727224 1384076 NM BS 680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A 2 INCH CRACK IN RT LOWER FUSELAGE SKIN AT STA 680, STRINGER 28R. THE CRACKED AREA AND FASTENERS WERE REMOVED IAW SRM 51-30-2, PAGE 2 AND 53-30-3, PAGE 14E. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-30-3, PAGE 14E. 2 L 7 3 4F A3WE 1999072300720 19990723 00720 1999 7 23 CALA9900841 4 19990720 A 2565 61621469 SLIDE BOEING 737 737524 1384721 NM CABIN LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 23657 28918 INSPECTION FOUND RIGHT AFT SLIDE PRESSURE IN THE RED BAND. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35. 2 L 7 2 4F RT A16WE 1999072300721 19990723 00721 WP 1999 7 23 CALA9900842 1 19990720 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND AFT FACE OF CIRCUMFERENTIAL FRAME CORRODED AT FS 1271, LONGERON 27L TO 27R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 5. 2 L 7 2 4F A6WE 1999072300722 19990723 00722 WP 1999 7 23 CALA9900843 1 19990720 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1197 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND RIGHT O/B SEAT TRACK GOUGED AT STA 1197, RBL 54. A NEW SEAT TRACK AND FITTINGS WERE INSTALLED SRM 53-0 5. 2 L 7 2 4F A6WE 1999072300723 19990723 00723 NM 1999 7 23 CALA9900844 1 19990720 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70352 23590 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 . 2 L 7 2 4F RT A16WE 1999072300724 19990723 00724 WP 1999 7 23 CALA9900845 1 19990720 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1193-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LT SEAT TRACK CORRODED FROM STA 1193 TO 1212, LBL 44. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED A ND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4E, 51-10-4, 51-30-1. 2 L 7 2 4F A6WE 1999072300725 19990723 00725 WP 1999 7 23 CALA9900846 1 19990720 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 38 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AND OIL CANNED AT FS 38 BETWEEN LONGERON 18R AND 19R. THE SKIN WAS REPAI RED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1999072300726 19990723 00726 WP 1999 7 23 CALA9900847 1 19990720 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND ATTACH ANGLE ON END OF SEAT TRACK CORRODED AT FS 200, LBL 44. THE ATTACH ANGLE WAS REMOVED AND A NEW A NGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-03 AND 51-30-5. 2 L 7 2 4F A6WE 1999072300727 19990723 00727 WP 1999 7 23 CALA9900848 1 19990720 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1079-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED FROM STA 1079 TO 1231, LBL 24. THE CORROSION WAS REMOVED IAW SRM 51-30-01 . A NEW SEAT TRACK AND SPLICES WERE INSTALLED IAW SRM 53-05, FIGURE 5, 51-30-1, AND 51-30-5. 2 L 7 2 4F A6WE 1999072300728 19990723 00728 WP 1999 7 23 CALA9900849 1 19990720 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1098-1193 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LT CENTER SEAT TRACK CORRODED FROM STA 1098 TO 1193, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICES WERE INSTALLED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999072300729 19990723 00729 NM 1999 7 23 UPS99230129 1 19990720 A 2612 FIRE WARNING BOEING 727 727173C 1384059 NM RT MLG WW ACTIVATED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 938UP 19506 INSPECTION TYPE:N/A ATB-WHEEL WELL FIRE LIGHT AND BELL CAME ON IN FLIGHT. CREW DECLARED EMERGENCY AND PERFORMED A NORMA L LANDING. UPON INSPECTION FOUND NO EVIDENCE OF SMOKE OR FIRE. LIGHT STAYED ON AFTER ENGINE SHUTDOWN. FOUND RIGHT WHE EL WELL SENSE ELEMENT AT FAULT CAUSING WARNING INDICATIONS. REMOVED AND REPLACED ELEMENT IAW MM 26-12-00. 2 L 7 3 4F A3WE 1999072300730 19990723 00730 WP 1999 7 23 UPS99830125 1 19990707 A 5541 RIB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, LEADING EDGE RUDDER RIB CRACKED. FABRICATED AND INSTALLED NEW RIB IAW DC8 SRM 51-1-24, 51-1-22 & 51 -1- 21. 2 L 7 4 4F RT 4A25 1999072300731 19990723 00731 WP 1999 7 23 UPS99830126 1 19990706 A 5540 WEB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, RUDDER CTR DAMPER LOWER CLOSEOUT WEB WAS CRACKED. FABBED, INSTALLED AND HEAT TREATED NEW WEB IAW DA C DWG 5656229 AND DC 8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999072300732 19990723 00732 WP 1999 7 23 UPS99830127 1 19990702 A 5230 DOUBLER DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2 D CARGO PIT DOOR EXTERIOR SKIN HAS .75 INCH VISIBLE CRACK 12 INCHES ABOVE LOWER AFT CORNER. FABBED A ND INSTALLED DOUBLER IAW DC8 SRM 52-2-0, 51-1-21, 51-1-20 & 51-1-15. 2 L 7 4 4F RT 4A25 1999072300733 19990723 00733 NM 1999 7 23 99FDEA00268 1 19990721 A 3260 WARNING SWITCH BOEING 727 72721C 138400M NM RT MLG DOOR INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 144FE 19137 ON DEPART, RT MLG DOOR APPEAR TO REMAIN OPEN EVEN AFTER CYCLING MLG PER RED TAB PROC. REMOVED AND REPLACED RT GEAR DOOR WARN SWITCH PER MM 32-62-011-4 ADJ & TEST PER MM 32-62-011-5. OPS CK GOOD. 2 L 7 3 4F A3WE 1999072300734 19990723 00734 NE 1999 7 23 99UAL900363 2 19990709 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 WP 29 649UA 25286 COMPRESSOR STALL AT 19,000 FEET, 2 ADDITIONAL MOMENTARY COMPRESSOR STALLS ON APPROACH. 2 L 7 2 4F 4 F RT A1NM E24NE 1999072300735 19990723 00735 NM 1999 7 23 99UAL900364 1 19990709 A 2150 8102093 ACM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT PACK SEIZED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 772UA 26930 PACK MODE L LEFT PACK AIR CYCLE MACHINE HAD FAILED MESSAGE RECEIVED AND FLIGHT CREW NOTICED SMOKE IN COCKPIT AT TOP OF D ESCENT. *S/D* PACK MODEL MESSAGE WAS DUE TO AIR CYCLE MACHINE (P/N 810209-3) SEIZING. HAMILTON STANDARD AND BOEING AR E WORKING TO IMPROVE THE ACM RELIABILITY. ACM TEARDOWN SHOWED THAT ACM FAILURE WAS NOT RELATED TO THE SMOKE INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999072300736 19990723 00736 NE 1999 7 23 99UAL900365 2 19990712 A 7250 54L001 T1 BLADE PRATT WHITNE PW4090 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE FRACTURED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 798UA 9260 9260 222027 26928 222027 AFTER TAKEOFF FROM LHR CREW NOTICED EGT RISE WITH LOSS OF POWER ON NR 1 ENGINE. ENGINE WAS SHUT DOWN AND FLIGHT RETURNE D TO LHR. *S/D* NR 1 ENGINE REMOVED. FOUND HIGH PRESSURE TURBINE DAMAGE ORIGINATING AT STAGE 1 BLADE FRACTURED IN AIR FOIL ABOVE THE PLATFORM. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999072300737 19990723 00737 WP 1999 7 23 99UAL900366 1 19990628 A 3233 ACG71041 BOLT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NLG ACTUATOR BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 1839U 46633 HEARD LOUD BANG WHEN GEAR EXTENDED. BELIEVE IT TO BE NOSE GEAR DOOR AS WE HAD 3 GEAR GREEN LIGHTS. NLG RETRACT ACTUATO R MOUNT BOLT FAILED AND MIGRATED OUT OF THE LOWER CLEVIS ALLOWING GEAR TO FREE FALL UNRESTRICTED BY THE ACTUATOR. NLG R T FWD DOOR DRIVE LINK WAS BENT AND LT DOOR DRIVE LINK BROKEN. THE BOLT AND THE RETRACT ACTUATOR WERE REPLACED. RT AND LT DRIVE LINKS WERE REPLACED. SECONDARY DAMAGE TO THE NLG DOORS WAS REPAIRED. MAGNETIC PARTICLE INSPECTION WAS PERFORM ED FOR NLG RETRACT ACTUATOR LOWER ATTACH LUG, NO DEFECT WAS FOUND. INTENSIFIED VISUAL AND HFEC INSPECTION WAS PERFORMED FOR UPPER AND LOWER LOCK LINKS AT ITS UPPER A-FRAME LUG, TRUNNION ATTACH POINTS, NLG DRAG LINK ATTACH POINTS AND NLG AF 2 L 7 3 4F 4 F A22WE E23EA 1999072300738 19990723 00738 EU 1999 7 23 99UAL900367 1 19990711 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 AFT CABIN EMERGENCY LIGHTS FAIL TEST. MESSAGE IS INTERNAL LOADS EMER LT. TEST OF AFT CABIN EMERGENCY LIGHTS FAILED BUT TEST PASTED AT THE NEXT STATION. 2 L 7 2 4F 4 F RT A28NM E40NE 1999072300739 19990723 00739 1999 7 23 99UAL900368 4 19990713 A 2210 2589124902 YAW DAMPER HONEYWELL 106044718 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE AUTOPILOT FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 911UA 1363 89022950 25255 AIRCRAFT DEMONSTRATED INAPPROPRIATE YAW CHARACTERISTICS AT 10,000 FEET. AIRCRAFT RETURNED TO FIELD. *S/D* THE YAW DAM PER COUPLER WAS REPLACED, AND SENT TO THE SHOP. THE COUPLER WAS RECEIVED IN THE SHOP AND DURING INITIAL POWER-UP THE RA TE GYRO WAS FOUND STUCK AND NOT OPERATING. THE GYRO WAS UNSTUCK AND THE GYRO OPERATED NORMALLY FOR THE REMAINDER OF THE TESTS. ANOTHER FAULT WAS FOUND DURING TESTING. THERE WAS NO ENGAGE MODE INTERLOCK SIGNAL BEING OUTPUT FROM THE COUPLE R. AFTER THE COUPLER REPLACEMENT, FLIGHT TEST PILOTS ACCOMPLISHED A TEST FLIGHT OF THE AIRCRAFT WITH NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 1999072300740 19990723 00740 NM 1999 7 23 99UAL900369 1 19990709 A 2433 TRANS RECTIFIER ELDEC 2299 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E & E COMPT FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 956UA 2863 26704 A STRONG ELECTRICAL ODOR IN THE CABIN WAS REPORTED BY A FLIGHT ATTENDANT. *S/D* TRANSFORMER RECTIFIER POWER SUPPLY FAI LED. REPLACED TRANSFORMER RECTIFIER IN NR 2 POSITION. ALSO, R4 RELAY WAS REPLACED DUE TO ZERO VOLTAGE BETWEEN B1 AND B 2. AIRCRAFT CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999072300741 19990723 00741 NM 1999 7 23 99UAL900370 1 19990709 A 5730 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7446U 21900 THE RIGHT HAND FIXED LEADING EDGE SKIN WAS FOUND WITH CRACKS AT SLAT STATION 105 AND 113. THE STANDARD REPAIR MANUAL R EPAIR COULD NOT BE ACCOMPLISHED BECAUSE OF AN ELECTRICAL WIRE BUNDLE IS IN THE WAY. THE DAMAGED SKIN WAS TRIMMED OUT AN D INTERNAL REPAIR DOUBLERS WERE INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH A N 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999072300742 19990723 00742 NM 1999 7 23 99UAL900371 1 19990623 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 208 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7448U 21902 CRACKS WERE FOUND IN THE FUSELAGE BELLY SKIN AT BS 208, LBL 1. THE CRACKS WERE COMMON TO FOUR FASTENER HOLES COMMON TO A DRAIN HOLE FLAPPER VALVE. THE CRACKS WERE CLEANED UP BY OVERSIZING ALL FOUR HOLES TO 0.421 INCH DIAMETER. THE SKIN W AS CUT OUT AROUND THE DISCREPANT HOLES AND AN EXTERNAL DOUBLER INSTALLED. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999072300743 19990723 00743 NE 1999 7 23 99UAL900372 2 19990714 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 BIRD STRIKE A UALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 WP 29 596UA 28749 RETURNED TO ABQ, ACCOUNT OF BIRD STRIKE TO NR 2 ENGINE ON TAKEOFF. *S/D* ACCOMPLISHED BIRD STRIKE INSPECTION. IDENTIF IED DAMAGE TO THE FAN BLADES AND INLET AREA. NO INTERNAL DAMAGE FOUND ON BORESCOPE. REPLACED DAMAGED FAN BLADES AND RE PAIRED FAN INLET. 2 L 7 2 4F 4 F RT A2NM E17NE 1999072300744 19990723 00744 NM 1999 7 23 99UAL900373 1 19990715 A 2910 AS118G107K000 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT HYD SYS FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 585UA 26709 LANDED DEN UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. RT MLG UPLOCK FLEX HOSE WAS LEAKING AT SWAGED FITTIN G AT ACTUATOR. REPLACED FLEX HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999072300745 19990723 00745 NE 1999 7 23 99UAL900374 2 19990715 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAILED A UALA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 WP 29 563UA 3031 26665 718000 DURING DESCENT FROM 10,000 FT, LEFT ENGINE WENT TO 3.2 VIBES ON DESCENT. DURING SHUTDOWN MADE MOANING NOISE AND VIBRATI ON FELT THROUGH AIRFRAME. ENGINE SUFFERED A FAILURE OF A HPT 2ND STAGE BLADE. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999072300746 19990723 00746 NM 1999 7 23 99UAL900375 1 19990715 A 3397 W207800120 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE 1 L DOOR BROKEN A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 175UA 24382 1L MED EMERGENCY SLIDE LIGHT (ON DOOR) ILLUMINATES WHEN POWER IS OFF AIRCRAFT. THIS PROBLEM WAS CAUSED BY A DISCONTINUI TY IN THE CIRCUIT. A GROUND WIRE WAS FOUND BROKEN (ROUTING OF WIRE IS FROM DX317, PIN 1 TO GD6338). WIRE W2078-001-20 WAS REPLACED (REF WDM 33-51-22). 2 L 7 4 4F 4 F RT A20WE E24NE 1999072300747 19990723 00747 WP 1999 7 23 ABXA9900574 1 19990709 A 5320 5597646 JAMB DOUG DOUG DC8 DC861 3021952 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 852AX 46016 LOWER AFT CORNER OF ENTRY DOOR JAMB CRACKED. REPAIRED IAW ABX REA D853-28136MR. 2 L 7 4 4F 4A25 1999072300748 19990723 00748 WP 1999 7 23 ABXA9900575 1 19990713 A 5712 995746524 RIB DOUG DOUG DC9 DC931 3022065 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 DURING C-CHECK, FOUND RIGHT WING RIB INBOARD OF OUTBOARD FLAP HINGE CRACKED. REPAIRED IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999072300749 19990723 00749 WP 1999 7 23 ABXA9900576 1 19990713 A 5320 99577397N SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR-TIE CRACKED AT STATION 945 AND LONGERON 13 RIGHT. REPAIRED IAW DC9 SRM 53-0 3. 2 L 7 2 4F A6WE 1999072300750 19990723 00750 WP 1999 7 23 ABXA9900577 1 19990720 A 5320 995823870 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1052 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1052 AND LONGERON 16 RIGHT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999072300751 19990723 00751 WP 1999 7 23 ABXA9900578 1 19990719 A 5210 591412159 PAN DOUG DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND LEFT FORWARD ENTRY DOOR PAN CRACKED. REPLACED DOOR PAN SEGMENT IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999072300752 19990723 00752 WP 1999 7 23 ABXA9900579 1 19990716 A 3397 WIRE DOUG DOUG DC9 DC931 3022065 WP LT COCKPIT SHORTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 943AX 47528 SHORTLY AFTER ADJUSTING THE CAPTAIN'S MAP LIGHT RHEOSTAT, THE MAP AND BRIEFCASE CIRCUIT BREAKER OPENED. THERE WAS A STR ONG SMELL OF BURNING WIRE FOR A FEW SECONDS AFTER THE CIRCUIT BREAKER OPENED. REPOSITIONED SHORTED WIRE TO THE MAP LIGH T HOUSING. 2 L 7 2 4F A6WE 1999072300753 19990723 00753 WP 1999 7 23 ABXA9900580 1 19990720 A 5610 5613217507 WINDOW DOUG DOUG DC9 DC941 302207N WP LT COCKPIT BINDING A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 974AX 47623 CAPTAIN'S SLIDING WINDOW (EMERG EXIT) JAMMED INTERMITTENTLY. ADJUSTED LOWER LOCK ON WINDOW ASSEMBLY. 2 L 7 2 4F A6WE 1999072300754 19990723 00754 WP 1999 7 23 ABXA9900581 1 19990720 A 5250 AR25291GR41 LATCH DOUG DOUG DC9 DC931 3022065 WP COCKPIT DOOR STUCK A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 941AX 47419 COCKPIT DOOR LATCH WAS STUCK IN LOCKED POSITION. DISASSEMBLED AND REALIGNED THE DOOR LATCH ASSEMBLY. 2 L 7 2 4F A6WE 1999072300755 19990723 00755 NM 1999 7 23 SCNA99093 1 19990721 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE R2 OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE R2 OVERHEAD EMERGENCY LIGHT BATTERY PACK. LIGHT OPERATIONALLY CHECKS GOOD IAW MM 335071. 2 L 7 3 4F RT A3WE 1999072300756 19990723 00756 WP 1999 7 23 SCNA99094 1 19990717 A 2530 3510004407 COFFEEMAKER DOUG DC10 DC1015 3022118 WP NR 3 FAILED A SCNA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 151SY 3666 48295 DURING FLIGHT, NUMBER THREE COFFEEMAKER SPARKED THEN THE GALLEY POWER TRIPPED OFF LINE. GALLEY COFFEEMAKER CIRCUIT BREA KERS THEN PULLED. REMOVED AND REPLACED THE COFFEMAKER AND CHECKED ALL ELECTRICAL TERMINALS. RESET CIRCUIT BREAKER AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1999073000001 19990730 00001 NM 1999 7 30 99ZZZX2737 1 19990627 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT FS 380 AT R-1 DOOR. 2 L 7 3 4F A3WE 1999073000002 19990730 00002 NM 1999 7 30 99ZZZX2738 1 19990627 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 720 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR SUPPORT BS 720 RBL 13.48. 2 L 7 3 4F A3WE 1999073000003 19990730 00003 NM 1999 7 30 99ZZZX2739 1 19990627 A 5320 655611915 SHEAR TIE BOEING 727 727227 1384078 NM BS 950 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR TIE RT KEAL BEAM CHORD AREA BS 950. 2 L 7 3 4F A3WE 1999073000004 19990730 00004 NM 1999 7 30 99ZZZX2740 1 19990627 A 5314 6516338202 KEEL BOEING 727 727227 1384078 NM BS 950 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON KEEL BEAM CHORD BS 950 RT. 2 L 7 3 4F A3WE 1999073000005 19990730 00005 NM 1999 7 30 99ZZZX2741 1 19990627 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 970-1010 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK BS 970 - BSL 1010, RBL 24.75. 2 L 7 3 4F A3WE 1999073000006 19990730 00006 NM 1999 7 30 99ZZZX2742 1 19990627 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 400 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM BS 400. 2 L 7 3 4F A3WE 1999073000007 19990730 00007 NM 1999 7 30 99ZZZX2743 1 19990627 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 950 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON STR 29R, BS 950. 2 L 7 3 4F A3WE 1999073000008 19990730 00008 NM 1999 7 30 99ZZZX2744 1 19990630 A 5347 SEAT TRACK BOEING 737 737201 1384454 NM BS 344-380 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 226US 21815 DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK RT OUTBOARD STA 344 - STA 380. 2 L 7 2 4F A16WE 1999073000009 19990730 00009 NM 1999 7 30 AALA990685 1 19990509 A 2421 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 07 394AN 29431 MIA - FLT 0909 - DURING CRUISE AT FL 330, RIGHT GENERATOR DRIVE LIGHT ILLUMINATED AND RIGHT GENERATOR CONTROL LIGHT DISC ONNECTED GENERATOR DRIVE. REPLACED RIGHT IDG PER MM. CHECKED PER MM. WORKS OK. PLACARD REMOVED, CLEARED MIC 3942403F 4/0155.10MAY.MIA. (X) 2 L 7 2 4F RT A1NM 1999073000010 19990730 00010 SO 1999 7 30 C2XA99BT059 1 19990605 A 5310 STRUCTURE EMB 145 EMB145 SO FUSELAGE DAMAGED A C2XA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 12957 145080 BTV - FLT 4218 - DURING 1A INSPECTION, MAINTENANCE FOUND EVIDENCE OF A LIGHTNING STRIKE. PERFORMED LIGHTNING STRIKE INS PECTION, FOUND AND REPAIRED DAMAGE WITH DOUBLERS, FILLERS, AND PATCHES. PRESSURIZED AIRCRAFT LEAK CHECKED GOOD. LIGHTEN ING STRIKE DAMAGE JUST AFT OF FR 52 ON STR 2L, 3 RIVETS. LIGHTENING STRIKE DAMAGE ON FR 41 STR 2L, 3 RIVETS. LIGHTENIN G STRIKE DAMAGE ON FR 38, STR 2L, 4 RIVETS. LIGHTENING STRIKE DAMAGE IN FRONT OF FR 31, STR 2L. AFTER REPAIR AND CHECK S, ACFT RETURNED TO SERVICE. ACFT TT: 1,853.2. ACFT CYCLES: 1,330. (X) 2 L 7 2 4F RT T00011AT 1999073000013 19990730 00013 EA 1999 7 30 MASA99098 1 19990615 A 3350 BR9279232 LIGHT BRUCE CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17231 7231 FLT 5759 - PHL-BHM - CREW REPORTED THE FORWARD FLOOR LEVEL EMERGENCY FLOOD LIGHT COVER WAS MISSING. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE REMOVED AND REPLACED BUL B. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999073000014 19990730 00014 SO 1999 7 30 SIMA991613 1 19990610 A 3350 3012501 LIGHT EMB 145 EMB145LR SO RT WING INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AE 145079 ORD - FLT 4201 - RIGHT WING EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED RIGHT WING EXXTERIOR EME RGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 1999073000015 19990730 00015 SO 1999 7 30 SIMA991612 1 19990610 A 3350 1317 BULB EMB 145 EMB145LR SO LT WING FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AE 145109 ORD - FLT 4265 - LEFT WING EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 1999073000016 19990730 00016 SO 1999 7 30 SIMA991446 1 19990524 A 2611 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO BAY MALFUNCTIONED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 630AE 145132 HOU - FLT 3544 - BAGGAGE SMOKE WARNING INDICATION CAME ON IN-FLIGHT. DISCHARGED FIRE EXTINGUISHER. RETURNED TO HOUSTON . VERIFIED EVENT AS A FALSE WARNING AND DEFERRED BAGGAGE SMOKE WARNING SYSTEM. ON 5-31-99, THE BAGGAGE SMOKE WARNING S YSTEM WAS OPERATIONALLY CHECKED WITH NO DISCREPANCIES NOTED. THE MEL ITEM WAS RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 1999073000017 19990730 00017 SO 1999 7 30 SIMA991751 1 19990624 A 3350 3025101 LIGHT EMB 145 EMB145LR SO CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 626AE 145117 ORD - FLT 4265 - LEFT OVERWING EMERGENCY LIGHT ASSEMBLY DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPER ATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 1999073000018 19990730 00018 EA 1999 7 30 VTZA990166 1 19990622 A 2750 860D10018 COMPUTER CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 639BR 7313 ORD/CRW - FLT 7804 - DURING CRUISE AT 1,400 HOURS, AIRCRAFT MADE AN UNSCHEDULED LANDING AND DIVERTED TO CVG DUE TO FLAP FAIL MESSAGE ON EICAS. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLAP COMPUTER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999073000019 19990730 00019 EU 1999 7 30 AALA990837 1 19990607 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1456D 11468 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY, EXIT FLOOR PATH LIGHT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PAT H LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999073000020 19990730 00020 CE 1999 7 30 C2XA99CL041 1 19990531 A 3230 1143640681 PC BOARD BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 09 87555 724I96 UE234 CLE - AFTER TAKEOFF, THE LEADING GEAR WOULD NOT RETRACT, AIRCRAFT CONTINUED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAIN TENANCE REMOVED AND REPLACED PCB A316, ALL OPERATIONAL CHECKS WERE SATISFACTORY IAW BEECHCRAFT MM 32-00-00. AIRCRAFT RE LEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1999073000021 19990730 00021 EA 1999 7 30 DW7A9901 2 19990429 A 8520 ROD BOLT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LT ENGINE SEPARATED A DW7A A B E UNSCHED LANDING EMER. DESCENT ENGINE SHUTDOWN O OTHER CR CRUISE 1 WP 09 74CE 893 317305041 RL866561A CRUISE FLIGHT, 1,500 MSL, 31 RPM/NEGATIVE INDICATION OF EMANANT FAILURE ON ENGINE INSTRUMENTS. HEAVY VIBRATION FOR 5-10 SECONDS, FAILURE OF LEFT ENGINE CASE, ENGINE SHUTDOWN, RTB. SUBMITTER SUGGESTED POSSIBLE CASE OF FAILURE AND ROD END B OLT NOT PROPERLY TORQUED. ALL AD'S C/W, NO ANOMALIES NOTED IN PREVIOUS OIL SAMPLE, POSSIBLE ASSEMBLY ERROR. ENGINE DES TROYED DUE TO INTERNAL COMPONENT FAILURE RESULTING IN DESTRUCTION OF ENGINE CASE. (X) 1 L 7 2 3O 3 O A20SO E14EA 1999073000022 19990730 00022 NM 1999 7 30 UIEA9945 1 19990630 A 7810 314U210057 NOZZLE BOEING 747 74747UF 1384949 NM NR 2 ENGINE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 493MC 3259 483 29254 DURING ROUTINE INSPECTION, NR 2 ENGINE S/N 704756 EXHAUST SLEEVE (NOZZLE) CRACKED AT PREVIOUS WELD REPAIRED AREA. CRACK LENGTH, 10 INCHES AT 11 O'CLOCK POSITION APPROXIMATELY 12 INCHES FORWARD FOR THE AFT END. REFERENCE SDR 99-26. UNIT R EMOVED AND REPLACED. (X) 2 L 7 4 4F RT 1384945 1999073000023 19990730 00023 NM 1999 7 30 UIEA99046 1 19990630 A 2572 E42 RACK BOEING 747 74747UF 1384949 NM BS 160 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 493MC 29254 DURING A SCHEDULED VISUAL INSPECTION OF THE SAT-COM RACK ASSEMBLY (E42) PER ATLAS AIR W.O. NR 1121207 (REF EO NR 121207/ 01), CRACKS WERE DISCOVERED ON THE BOTTOM LT FORWARD FRAME CORNER STA 1600 ALONG WITH LOOSE RIVETS ON THE UPPER FORWARD END OF THE DIAGONAL BRACE CHANNEL. REPAIRS ACCOMPLISHED PER ATLAS AIR EO NR 4453A002. (X) 2 L 7 4 4F RT 1384945 1999073000024 19990730 00024 NM 1999 7 30 UIEA9944 1 19990624 A 2612 FIRE WARNING BOEING 747 74747UF 1384949 NM MAIN DECK ACTIVATED A UIEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 15 494MC 29255 RTO/ANC - FLT FX076 - AT APPROX V1, MAIN DECK FIRE WARNING TRIGGERED BOTH AURAL AND VISUAL WARNINGS. REJECTED TAKEOFF, MAINT AT ANC INSPECTED ACFT FOR DAMAGE PER CHAPTER 5 HIGH ENERGY STOP. NO DAMAGE FOUND. NO FAULT MESSAGES ON CMC. RE QUESTED BOEING TO SEND AOG TEAM TO ANC TO ASSIST IN FAULT ISOLATION AND CORRECTION OF THIS DISCREPANCY. AIRCRAFT CURRE NTLY UNDER MAINTENANCE AT ANC WITH ASSISTANCE FROM BOEING TEAM AND ATLAS AIR QUALITY CONTROL INSPECTION. WILL ADVISE FI NDING WHEN THEY BECOME AVAILABLE. WITH BOEING TECHNICAL EXPERTISE, THE MAIN DECK SMOKE DETECTOR SYS WAS THOROUGHLY CLEA NED. ALL AFOLTS (8) CARDS AND 3 DIODE CARDS WERE REPLACED. ACFT TEST FLOWN AND SYS OPERATION NORMAL. (X) 2 L 7 4 4F RT 1384945 1999073000025 19990730 00025 NM 1999 7 30 UIEA9934 1 19990620 A 3610 65B9454414 DUCT BOEING 747 7472D7B 1384803 NM NR 1 ENGINE CRACKED A UIEA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 EA 15 524MC 21784 JFK/MIA - FLT GT870 - NR ENGINE FLAME-OUT AT TOP OF DESCENT. UNABLE TO RE-LIGHT. MAINTENANCE CHECKED THE FOLLOWING AN D NO DISCREPANIES NOTED (INLET AND EXHAUST, VISUAL CHECK UNDER COWL, BLEW OUT CDP LINE. CHECKED CHIP DETECTORS, FUEL FI LTER FOUND CLEAN, SUMPED NR 1 MAIN AND NR 1 RES TANKS AND NO CONTAMINATION FOUND, CONDITION MOTOR AND LINKAGE OK, DRY AN D WET MOTOR OF ENGINE OK, FUEL PRESSURE AND FUEL FLOW OK). RE-RIGGED VSV/VBV. FURTHER TROUBLESHOOTING IDENTIFIED CRACK IN FLANGE OF 8TH STAGE DUCT. REPLACED DUCT ENGINE. RUN-UP SATISFACTORY. (X) 2 L 7 4 4F RT A20WE 1999073000026 19990730 00026 NM 1999 7 30 UIEA9937 1 19990628 A 5330 SKIN BOEING 747 747271C 1384869 NM BS 800 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 DENT IN FUSELAGE SKIN STA 800 BETWEEN STR 13L, STR 14L. DAMAGED AREA 4 INCHES BY 2.8 INCHES. NO FRAME DAMAGE. BOEING: TLS BKK 99-072TE, 0070RE, 0064TE, 0068RE, 0063TE, 0065RE, 0061TE, 8130-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999073000027 19990730 00027 NM 1999 7 30 UIEA9943 1 19990628 A 5320 SPLICE BOEING 747 747271C 1384869 NM BS 1241 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CRACK IN SPLICE PLATE STRAP BS 1241 L/S. REPLACED SPLICE PLATE AT STA 1241 L/S IAW SB 747 53-2283. (X) 2 L 7 4 4F A20WE 1999073000028 19990730 00028 NM 1999 7 30 UIEA9942 1 19990628 A 5330 SKIN BOEING 747 747271C 1384869 NM BS 2252/2259 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 75003 14439 22403 SCRATCHES, DENTS FUSELAGE SKIN BS 2252 TO BS 2259 STR 49R. REPAIRED PER BOEING TLS BKK 99-0095RE, 0088TE, 8130-3 ISSUED . (X) 2 L 7 4 4F A20WE 1999073000029 19990730 00029 NM 1999 7 30 UIEA9935 1 19990628 A 5311 65B12887 FRAME BOEING 747 747271C 1384869 NM BS 281 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 75003 14439 22403 CRACKED PORTAL FRAME BS 281. WL 331.75, RBL 45 NOSE CARGO DOOR. INSTALLED DOUBLER. REF: SRM 53-10-04, FIG 97. FOUND DURING ACCOMPLISHMENT OF SB B747-53A2265. (X) 2 L 7 4 4F A20WE 1999073000030 19990730 00030 NM 1999 7 30 UIEA9940 1 19990628 A 5414 SKIN BOEING 747 747271C 1384869 NM PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 75003 14439 22403 PYLON SKIN CRACKED NAC 235 R/S. EDGE OF PRE-COOLER EXHAUST DUCT OPENING EDGE. STIFFENER NR 3 RT SIDE. REPAIRED PER TL S BKK-99-0069RE, 99-0064RE, 99-0063RE. 8130-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999073000031 19990730 00031 NM 1999 7 30 UIEA9941 1 19990628 A 5311 FRAME BOEING 747 747271C 1384869 NM BS 1700 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 75003 14439 22403 CRACKED FRAME BS 1680 BETWEEN STR 12/13 RS BS 1700 BETWEEN STR 10/11 RS. REPAIRED PER BOEING TELEX TLS-BKK-99-0082RE, 0 079TE. (X) 2 L 7 4 4F A20WE 1999073000032 19990730 00032 NM 1999 7 30 UIEA9939 1 19990628 A 5320 CHORD BOEING 747 747271C 1384869 NM BS 1265 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 75003 14439 22403 CRACKED CHORD BS 1265 L/S. SPLICED FRAME BS 1265 L/S IAW DRW 14400053-317. REF: BOEING TLX TLS 99-0071RE, 0056TE, 0053R E, 0051TE, 0052RE 0048T3. 8130-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999073000033 19990730 00033 NM 1999 7 30 UIEA9938 1 19990628 A 5330 SKIN BOEING 747 747271C 1384869 NM BS 433 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 75003 14439 22403 DENT IN FUSELAGE SKIN BS 433 BETWEEN STR 46L, 47L. DENT AT BS 520 STR 44L, 47L. INSTALLED DOUBLER PER BOEING TELEX TLS BKK 99-0077RE, 0071TE, 0053TE, 0057RE. 8130-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999073000058 19990730 00058 CE 1999 7 30 99ZZZX2771 1 19990625 A 5510 0732601 FITTING CESSNA 210 T210L 2073449 CE HORIZ STABILIZER LOOSE A P GGUA K NONE O OTHER IN INSP/MAINT 1 NM 13 61170 3781 21060602 REINFORCEMENT P/N 1232623-2 NOTED AS CRACKED. THE AIRCRAFT HAD NOT HAD SE84-17 C/W, SO THE NEW BRACKETS ORDERED. IT WA S SUGGESTED CHANGE COULD BE DONE WITHOUT COMPLETELY REMOVING THE HORIZONTAL STABILIZER. SUBMITTER ELECTED TO REMOVE THE STABILIZER AND INSPECT FURTHER ANYWAY. ADDITIONAL DISCREPANCIES: BOTH FORWARD MOUNT FITTINGS P/N 0732601 LOOSE. INVE STIGATION REVEALED ONE OF THE TOP TWO RIVETS SHEARED AND THE OTHER LOOSE ON BOTH SIDES. THE SHEARED RIVET STILL HAD THE MACHINE HEAD AND THE BUCK TAIL IN PLACE. THE BULKHEAD DOUBLER 1212127-3 ON THE LEFT SIDE APPEARED LOOSE. NOTED A SHEA RED TOP RIVET. BOTH HEADS WERE STILL IN PLACE. 1 H 7 1 3O 3A21 1999073000059 19990730 00059 CE 1999 7 30 99ZZZX2772 1 19990625 A 5510 12326232 REINFORCEMENT CESSNA 210 T210L 2073449 CE HORIZ STABILIZER CRACKED A GGUA K NONE O OTHER IN INSP/MAINT 1 NM 13 61170 3781 21060602 REINFORCEMENT P/N 1232623-2 NOTED AS CRACKED. THE AIRCRAFT HAD NOT HAD SE84-17 C/W, SO THE NEW BRACKETS ORDERED. IT WA S SUGGESTED CHANGE COULD BE DONE WITHOUT COMPLETELY REMOVING THE HORIZONTAL STABILIZER. SUBMITTER ELECTED TO REMOVE THE STABILIZER AND INSPECT FURTHER ANYWAY. ADDITIONAL DISCREPANCIES: BOTH FORWARD MOUNT FITTINGS P/N 0732601 LOOSE. INVE STIGATION REVEALED ONE OF THE TOP TWO RIVETS SHEARED AND THE OTHER LOOSE ON BOTH SIDES. THE SHEARED RIVET STILL HAD THE MACHINE HEAD AND THE BUCK TAIL IN PLACE. THE BULKHEAD DOUBLER 1212127-3 ON THE LEFT SIDE APPEARED LOOSE. NOTED A SHEA RED TOP RIVET. BOTH HEADS WERE STILL IN PLACE. 1 H 7 1 3O 3A21 1999073000063 19990730 00063 NE 1999 7 30 99ZZZX2776 2 19990614 A 7200 ENGINE BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE LEFT MALFUNCTIONED W ANCF A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 23 985AN 9477 24618 727522 GOB/LON - FLT 016 - AIR TURN-BACK. DURING LIFT-OFF, LEFT ENGINE STARTED TO STALL. EGT WENT TO 802. LEFT ENGINE WAS RE DUCED AND STALL CONDITION DISAPPEARED. AIRCRAFT RETURNED AND MADE AN OVERWEIGHT LANDING WITH LEFT ENGINE IN IDLE. SUBM ITTER STATED ENGINE NEEDS TO BE REPLACED AND AIRCRAFT INSPECTED FOR HARD LANDING AND OVERWEIGHT LANDING. NOTE: THIS E NGINE WAS RENTED FROM UNITED AIRLINES AND INSTALLED ON JUNE 12, 1999. AFTER INSTALLED, FLEW 35 HOURS. 2 L 7 2 4F 4 F RT A1NM E24NE 1999073000071 19990730 00071 EU 1999 7 30 UF6A990206 1 19990227 A 3350 0L3071BPEGPL BULB MIDLANDROSS BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 ORD - FLT 5759 - FORWARD CEILING EMERGENCY LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000094 19990730 00094 EU 1999 7 30 UF6A990102 1 19990102 A 3350 58785 CABLE ASSY BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 ORD - EMERGENCY LIGHTING STRIP ADJACENT TO ROW 2 INOPERABLE. MAINTENANCE REPLACED FLOOR PROXIMITY LIGHTING STRIP ON ROW 2. (X) 2 L 7 2 4T RT A27NM 1999073000095 19990730 00095 EU 1999 7 30 UF6A990103 1 19990105 A 3230 201087001 UPLOCK ROTOL BAG ATP ATP EU RT MLG FAILED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 859AW 13782 CWDDDRG389 2036 SBN - FLT 5750 - RIGHT MAIN LANDING GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF. MAINTENANCE LUBRICATED RIGHT HAND MAIN LANDING GEAR UPLOCK. PERFORMED SEVERAL EXTENSIONS AND RETRACTIONS WITH NO FAULT FOUND. (X) 2 L 7 2 4T RT A27NM 1999073000096 19990730 00096 EU 1999 7 30 UF6A990104 1 19990109 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - EMERGENCY LIGHTS INOPERABLE IN CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLIES. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000097 19990730 00097 EU 1999 7 30 UF6A990106 1 19990110 A 3350 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - EMERGENCY LIGHTS WILL NOT ILLUMINATE WHEN SELECTED ON. MAINTENANCE PERFORMED OPS CHECK OF SYSTEM. SYSTEM OPS CHE CKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000098 19990730 00098 EU 1999 7 30 UF6A990105 1 19990109 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN- EXTERNAL EMERGENCY LIGHTS OUT AT LEFT WING TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM OPS C HECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000099 19990730 00099 EU 1999 7 30 UF6A990107 1 19990111 A 5542 SKIN BAG ATP ATP EU RUDDER DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 15037 2021 ORD - RUDDER HAS SEVERE IMPACT DAMAGE TO RIGHT SIDE LOWER SECTION. MAINTENANCE REPAIRED DAMAGE IAW DER REPORT NR 99-005 . (X) 2 L 7 2 4T RT A27NM 1999073000100 19990730 00100 EU 1999 7 30 UF6A990109 1 19990112 A 2433 TR202B TRU BAG ATP ATP EU E/E BAY FAILED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 853AW 6562 517 13190 2022 ORD - FLT 5752 - D.C. LOW VOLTS ILLUMINATED. LOW VOLTS PBSI ALSO ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 1 TRANSFORMER RECTIFIER UNIT. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000101 19990730 00101 EU 1999 7 30 UF6A990110 1 19990112 A 3350 58785 CABLE ASSY BAG ATP ATP EU BS 18-234 FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FLT 5722 - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING BLINKS ON AND OFF DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF FLOOR PROXIMITY LIGHTING. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000102 19990730 00102 EU 1999 7 30 UF6A990112 1 19990115 A 3350 LIGHT BAG ATP ATP EU ROWS 1-4 INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 ORD - FLT 5700 - EMERGENCY LIGHTS ARE INOPERABLE FROM ROWS 1 TO 4. MAINTENANCE PERFORMED OPS CHECK OF SYSTEM. NO DEFEC TS NOTED. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000103 19990730 00103 EU 1999 7 30 UF6A990113 1 19990116 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - EMERGENCY LIGHT IN FLIGHT COMPARTMENT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOO D. (X) 2 L 7 2 4T RT A27NM 1999073000104 19990730 00104 EU 1999 7 30 UF6A990114 1 19990118 A 5350 EMPENNAGE BAG ATP ATP EU BS 441 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 2032 ORD - DAMAGE TO RIGHT HAND EMPENNAGE AREA. DAMAGE LOCATED BETWEEN STA 441.5AS TO STA 378AS. MAINTENANCE REPAIRED DAMAG E TO RIGHT HAND EMPENNAGE IAW DER REPORT NR 99-009. ACFT TT: 14,110 HOURS. (X) 2 L 7 2 4T RT A27NM 1999073000105 19990730 00105 EU 1999 7 30 UF6A990116 1 19990118 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU ROWS 9-10 FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 11813 291 17388 2036 ORD - FLOOR PROXIMITY STRIP AT 9CD AND 10CD INOPERABLE. MAINTENANCE REMOVED AND REPLACED NR 4 POWER SUPPLY. SYSTEM OPS CHECK GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000106 19990730 00106 EU 1999 7 30 UF6A990115 1 19990119 A 2560 P2070003001 FLASHLIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - FLIGHT ATTENDANT A, FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT. SYSTEM OPS CHECKED GOOD . (X) 2 L 7 2 4T RT A27NM 1999073000107 19990730 00107 EU 1999 7 30 UF6A990117 1 19990122 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 SBN - EXTERNAL EMERGENCY LIGHTS ON LEFT WING TRAILING EDGE INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM O PS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000108 19990730 00108 EU 1999 7 30 UF6A990120 1 19990124 A 3350 58785 CABLE ASSY BAG ATP ATP EU BS 234 FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 2032 ORD - FLT 5709 - EMERGENCY EXIT LIGHTING STRIP LEADING TO GALLEY IS INOPERABLE. MAINTENANCE REMOVED AND REPLACED FLOOR PROXIMITY LIGHTING STRIP. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000109 19990730 00109 EU 1999 7 30 UF6A990118 1 19990125 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - EXTERNAL EMERGENCY LIGHTS ON LEFT WING TRAILING EDGE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000110 19990730 00110 EU 1999 7 30 UF6A990119 1 19990125 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - EXTERNAL EMERGENCY LIGHTS ON RIGHT WING TRAILING EDGE INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000111 19990730 00111 EU 1999 7 30 UF6A990121 1 19990128 A 2560 P2070003001 FLASHLIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLT 5757 - FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000112 19990730 00112 EU 1999 7 30 UF6A990307 1 19990307 A 3230 201087001 UPLOCK MESSIER BAG ATP ATP EU NLG CONTAMINATED A UF6A K NONE O OTHER UK UNKNOWN 1 GL 31 852AW 2021 YNG - FLT 5712 - GREEN LIGHT ON NOSE GEAR REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED. MAINTENANCE CLEANED THE NOSE GE AR UPLOCK MICROSWITCH. PERFORMED GEAR EXTENSION AND RETRACTION TEST. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000113 19990730 00113 EU 1999 7 30 UF6A990310 1 19990311 A 5270 14XE112 SWITCH HONEYWELL BAG ATP ATP EU LT EMERG EXIT CONTAMINATED A UF6A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 859AW 2036 ORD - FLT 5754 - LEFT EMERGENCY OVERWING PBSI CWP ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE CLEANED LEFT SIDE OVERWING E XIT DOOR INDICATOR SWITCH. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000114 19990730 00114 EU 1999 7 30 UF6A990301 1 19990301 A 3350 10620BAC6 SWITCH BAG ATP ATP EU COCKPIT FAIALED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 ORD - FLT 5717 - CABIN EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT PBSI. SYS TEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000115 19990730 00115 EU 1999 7 30 UF6A990205 1 19990225 A 3060 7901125 DEICE TIMER DUNLOP BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 853AW 833 9610451 2022 ORD - FLT 5748 - NR 2 PROPELLER LEGEND LIGHT ILLUMINATED WITH PROP CWP. MAINTENANCE REMOVED AND REPLACED THE NR 2 PROPE LLER DEICE TIMER. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000116 19990730 00116 EU 1999 7 30 UF6A990316 1 19990325 A 7921 3036064 OIL COOLER STWARNER BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 GL 31 854AW 1728 846 2028 CAK - FLT 5709 - NR 2 ENGINE LOW OIL PRESSURE CWP WARNING AFTER TAKEOFF. SHUT NR 2 ENGINE DOWN. MAINTENANCE REMOVED AN D REPLACED THE FUEL COOLED OIL COOLER. POWER ASSURANCE RUNS WERE PERFORMED AND ALL SYSTEMS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000117 19990730 00117 EU 1999 7 30 UF6A990401 1 19990401 A 3350 1317 BULB BAG ATP ATP EU LT OVERWING FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. ( X) 2 L 7 2 4T RT A27NM 1999073000118 19990730 00118 EU 1999 7 30 UF6A990315 1 19990321 A 3350 1317 BULB BAG ATP ATP EU FUSELAGE FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - LEFT SIDE FUSELAGE EMERGENCY LIGHT BURNED OUT. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 1999073000119 19990730 00119 EU 1999 7 30 UF6A990318 1 19990329 A 2560 P4010021 BATTERY GRIMES BAG ATP ATP EU FLASHLIGHT DISCHARGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FLT 5717 - LED LIGHT ON AFT FLASHLIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY. SYSTEM OPS CHEC KED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000120 19990730 00120 EU 1999 7 30 UF6A990403 1 19990411 A 3350 1317 BULB BAG ATP ATP EU FUSELAGE FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 SBN - LEFT SIDE EMERGENCY LIGHT BULB AT AFT EXTERIOR IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000121 19990730 00121 EU 1999 7 30 UF6A990404 1 19990412 A 3350 1317 BULB BAG ATP ATP EU FUSELAGE FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT SIDE EMERGENCY LIGHT BULB AT AFT EXTERIOR IS INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000124 19990730 00124 EU 1999 7 30 UF6A990111 1 19990113 A 3350 10620BAC6 SWITCH BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 YNG - FLT 5712 - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING BLINKS ON AND OFF DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY ARM/DISARM PBSI. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000167 19990730 00167 NE 1999 7 30 TWAA9910501 2 19990721 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE NR 2 BIRD STRIKE A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN C F.O.D. TO TAKEOFF 1 CE 05 110HM 49787 1213 THE NUMBER TWO ENGINE INJESTED BIRDS DURING TAKEOFF. THE ENGINE WAS SHUTDOWN DUE TO STALLS AND THE FLIGHT RETURNED TO C LE. DAMAGED COMPRESSOR BLADES WERE DRESSED OUT TO FLY BACK LIMITS. CHECK-C 4-17-99 STL. 2 L 7 2 4F 4 F RT A6WE E9NE 1999073000168 19990730 00168 NM 1999 7 30 HNAA9900106 1 19990721 A 7810 SKIN DHAV DHC8 DHC8102 2809003 NM EXHAUST SHROUD CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 915HA 069 EXHAUST OUTLET SHROUD INNER SKIN CRACKED AT FORWARD O/B END. REPAIRED IAW RD8-54-331 AND EO8-54-99-255. 2 H 7 2 4T RT A13NM 1999073000169 19990730 00169 WP 1999 7 30 CALA9900858 1 19990724 A 5752 59554701 TRIM TAB DOUG DC9 DC982 3022082 WP LT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LT WING AILERON TRIM TAB DELAMINATED. THE TRIM TAB WAS REMOVED AND REPLACED IAW MM 27-10-05. 2 L 7 2 4F A6WE 1999073000170 19990730 00170 WP 1999 7 30 CALA9900859 1 19990724 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1203 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 1203, LBL 44. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NE W SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F, 51-10-4 AND 51-30-1. 2 L 7 2 4F A6WE 1999073000171 19990730 00171 WP 1999 7 30 CALA9900860 1 19990724 A 5730 SKIN DOUG DC9 DC982 3022082 WP LT WING CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LT WING LOWER LEADING EDGE CHAFED BY NR 3 SLAT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-3, 51-30- 1 AND ECRA 5730-01661. 2 L 7 2 4F A6WE 1999073000172 19990730 00172 NM 1999 7 30 CALA9900861 1 19990725 A 3350 P2070001205 LIGHT DME BOEING 737 7373Q8 1384670 NM L-1 DOOR INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14384 26313 INSPECTION FOUND THE L-1 DOOR EMERGENCY FLASHLIGHT INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1999073000173 19990730 00173 NM 1999 7 30 CALA9900862 1 19990726 A 5523 183A84003 FITTING BOEING 737 737724 NM LT ELEV TAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 23707 28768 INSPECTION FOUND A .75 INCH CRACK IN LT ELEVATOR TAB MAST ARM FITTING. THE LT ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-31-00 AND 27-31-31. THE TAB WAS RIGGED AND OPERATION WAS NORMAL. 2 L 7 2 4F RT A16WE 1999073000174 19990730 00174 WP 1999 7 30 CALA9900863 1 19990726 A 7110 NSL605111 COWL DOUG DC10 DC1030 3023501 WP NR 3 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12080 47981 INSPECTION FOUND A 2 INCH CRACK ON INNER LIP OF NR 3 ENGINE INTAKE COWL. THE COWL WAS REPAIRED IAW MM 71-11-00 AND SRM 54-11-00. 2 L 7 3 4F A22WE 1999073000175 19990730 00175 NM 1999 7 30 CALA9900864 1 19990726 A 5720 STIFFENER BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A 1 INCH CRACK IN STIFFENER ON I/B SIDE OF FIXED L/E RIB O/B OF RT WING FORWARD BOTTLE PIN (AFT OF ANTI -ICE DUCT, ACCESS CUTOUT 6402). THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 2. A FORMER ANGLE WAS INSTALLED IAW S RM 51-40-3, FIGURE 1 AND 51-10-2, PAGE 2. 2 L 7 3 4F A3WE 1999073000176 19990730 00176 NE 1999 7 30 9902761233 2 19990717 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK M R J OVER TEMP PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 233NW 46640 455756 DURING TAKEOFF ROLL (DEL), CREW OBSERVED THE NR 1 ENGINE WAS NOT PRODUCING TAKEOFF POWER WITH EGT AT REDLINE. THE TAKEO FF WAS ABORTED AT 130 KTS AND THE AIRCRAFT RETURNED TO THE GATE. AFTER A BORESCOPE, FOUND NO DEFECTS AND AND MEC CHANGE DID NOT CORRECT THE PROBLEM. THE AIRCRAFT WAS FERRIED TO AMS TO REPLACE THE ENGINE. 2 L 7 3 4F 4 F A22WE E23EA 1999073000177 19990730 00177 NE 1999 7 30 9902772762 2 19990721 A 7200 ENGINE BOEING 727 7272M7 138407S NM PWA JT8 JT8D17R 52049 NE NR 1 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 01 722RW 21201 689950 THE NR 1 ENGINE FLAMED OUT AT START OF DESCENT. THE FLIGHT CREW ACCOMPLISHED ENGINE SHUTDOWN COM PROCEDURES THEN RESTAR TED THE NR 1 ENGINE WITH NORMAL OPERATION THE REMAINDER OF THE FLIGHT. FLIGHT LANDED AT DESTINATION WITHOUT INCIDENT. M AINTENANCE PERFORMED TWO ENGINE STARTS IN THE GATE AREA WITH ALL INDICATIONS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999073000178 19990730 00178 NM 1999 7 30 9902786631 1 19990717 A 2760 SWITCH BOEING 747 747251B 1384892 NM SPOILER SYS OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 631US 23111 DURING TAKEOFF (KIX), THE TAKEOFF WARNING HORN SOUNDED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCID ENT. ADJUSTED THE SPOILER LIMIT SWITCH. OPERATIONAL CHECK GOOD. EXACT PART CAUSING DISCREPANCY TO BE DETERMINED. 2 L 7 4 4F A20WE 1999073000179 19990730 00179 1999 7 30 9902791235 4 19990717 A 3417 ADC DOUG DC10 DC1030 3023501 WP NR 2 FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 235NW 46915 ON TAKEOFF ROLL, CO-PILOT'S AIRSPEED INDICATOR, HSI, AND ADI SPEED FLAGS APPEARED. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE NR 2 CENTRAL AIR DATA COMPUTER, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999073000180 19990730 00180 WP 1999 7 30 9902809955 1 19990715 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND AFT COMPARTMENT AND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000181 19990730 00181 WP 1999 7 30 9902819154 1 19990719 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWE R SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000182 19990730 00182 WP 1999 7 30 9902829155 1 19990720 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000183 19990730 00183 WP 1999 7 30 9902839997 1 19990716 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 8933E 47142 ONLY EMERGENCY PATHWAY LIGHTS IN FORWARD CABIN AND FORWARD EXIT LIGHTS WOULD ILLUMINATE. REPLACED BATTERY PACK, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000184 19990730 00184 WP 1999 7 30 9902849997 1 19990720 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND SEAT MOUNTED EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT DOOR 1R, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000185 19990730 00185 WP 1999 7 30 9902859876 1 19990714 A 3397 WIRE DOUG DC9 DC951 3022051 WP COCKPIT CROSSED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 785NC 48110 DURING LINE MAINTENANCE INSPECTION, FORWARD COCKPIT AND FORWARD ENTRY CEILING EMERGENCY LIGHTS WOULD NOT SHUT OFF, NO OT HER POWER AVAILABLE. FOUND WIRES CROSSED AT TERMINALS 4 AND 7. REPAIRED WIRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999073000186 19990730 00186 WP 1999 7 30 9902869870 1 19990714 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP TAIL COMPT INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 779NC 48101 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED POWER SUPPLY A ND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999073000187 19990730 00187 WP 1999 7 30 9902879621 1 19990709 A 3350 BATTERY DOUG DC9 DC932 3022066 WP GALLEY DOOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 621NW 47544 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND FUSE AT GA LLEY SERVICE DOOR EXIT SIGN, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000188 19990730 00188 WP 1999 7 30 9902889971 1 19990709 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERIES, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000189 19990730 00189 WP 1999 7 30 9902899140 1 19990712 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 DURING PERIODIC CHECK, TAIL COMPARTMENT CATWALK EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000190 19990730 00190 WP 1999 7 30 9902909950 1 19990717 A 2780 GUIDE PADS DOUG DC9 DC932 3022066 WP T DUCTS BINDING A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 9346 47376 DURING APPROACH INTO GPT, SLAT DISAGREEMENT LIGHT ILLUMINATED AND AIRCRAFT ROLLED LEFT DURING SLAT EXTENSION. FLIGHT CR EW DECLARED A YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT T-DUCT GUIDE P ADS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000191 19990730 00191 WP 1999 7 30 9902919927 1 19990721 A 2910 LINE DOUG DC9 DC931 3022065 WP LT MLG WW LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 8920E 45835 LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY OCCURRED DURING APPROACH INTO DTW. PRESSURE FLUCTUATED BETWEEN 2399 AND 3000 PS I. FLIGHT CREW SHUT DOWN PUMPS AND UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES TO EXTEND GEAR. AIRCRAFT LANDED WITHOU T INCIDENT. MAINTENANCE FOUND B-NUT LOOSE AT LEFT GEAR SWIVEL LINE AND LINE LEAKING IN LEFT WHEEL WELL. TIGHTENED NUT AND REPLACED LINE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000192 19990730 00192 WP 1999 7 30 9902929950 1 19990721 A 2780 T DUCT DOUG DC9 DC932 3022066 WP LT SLAT BINDING A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 9346 47376 DURING APPROACH INTO DAY, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE LEFT. AN UNEVENTFUL LANDING WAS ACCOMPLI SHED USING FLAPS ONLY. MAINTENANCE REPLACED LEFT SLAT ANTI-ICE T-DUCT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999073000193 19990730 00193 SO 1999 7 30 COMA9910116 1 19990725 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT CLOSED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J W WARNING INDICATION INADEQUATE Q C TO TAKEOFF 1 SO 01 259CA 120252 SERVICE DOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT COMPLETELY CLOSED. 2 L 7 2 4T RT A31SO 1999073000194 19990730 00194 SO 1999 7 30 COMA9910117 1 19990722 A 3230 12038594001 CONTROL MODULE EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 256CA 17461 1245 LANDING GEAR WOULD NOT RETRACT. REPLACED CONTROL MODULE. 2 L 7 2 4T RT A31SO 1999073000195 19990730 00195 SO 1999 7 30 COMA9910118 1 19990725 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT CLOSED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J W WARNING INDICATION INADEQUATE Q C TO TAKEOFF 1 SO 01 266CA 120258 SERVICE DOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT COMPLETELY CLOSED. SECURED FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1999073000196 19990730 00196 EA 1999 7 30 COMA9960389 1 19990725 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 920CA 7251 452 7022 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999073000197 19990730 00197 EA 1999 7 30 COMA9960390 1 19990722 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 962CA 6311 3838 7123 FLAPS FAILED AT 8 DEGREES. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999073000198 19990730 00198 EA 1999 7 30 COMA9960391 1 19990724 A 3620 356024310 SENSOR LOOP CNDAIR CL600 CL6002B19 EA RT PYLON CHAFED A COMA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 01 946CA 7072 A 14TH STAGE BLEED AIR DUCT LEAK MESSAGE IFSD. REPLACED THE RT PYLON LEAK SENSOR LOOP. 2 L 7 2 4F RT A21EA 1999073000199 19990730 00199 EA 1999 7 30 COMA9960392 1 19990725 A 3320 BR95005 BALLAST CNDAIR CL600 CL6002B19 EA CABIN OVERHEAD A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 958CA 7111 SMOKE SMELL IN CABIN. REPLACED LIGHT BALLAST. 2 L 7 2 4F RT A21EA 1999073000200 19990730 00200 EA 1999 7 30 COMA9960393 1 19990712 A 5210 HSP115B094900 PIN H341433 CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR SHEARED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 781CA 7312 CREW REPORTED MAIN CABIN DOOR IS VERY HARD TO OPEN AND THAT DOOR HANDLE SEEMS TO GET STUCK WHEN PULLING UPWARD ON HANDLE . WHILE TROUBLESHOOTING THE DOOR HANDLE (P/N 600-31887-11 ITEM NR 5 PAGE 1 FIG 1 RJ IPC CH 52-11-02) FOUND THE PIN (HSP 115BO94-900 ITEM NR 185 IN THE RJ CMM PG 1010 CHAP 52-11-03) FOR THE FLUSH HANDLE LATCH ASSEMBLY TO BE SHEARED, CAUSING THE HANDLE ASSEMBLY TO BIND UP. 2 L 7 2 4F 4 F RT A21EA E15NE 1999073000201 19990730 00201 EA 1999 7 30 COMA9960394 1 19990722 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 EA FWD FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 AIRCRAFT SUSTAINED GROUND DAMAGE ON RIGHT SIDE OF NOSE SECTION BY FUELING VEHICLE WHILE PARKED AT CVG GATE. DAMAGED ARE A OF AIRCRAFT NOSE SECTION WAS CLASSIFIED AS MAJOR AND WAS REPAIRED IN ACCORDANCE WITH APROVED DATA FROM BOMBARDIER. RE PAIRED EO 601-53-11-161 AND DEPT OF TRANSPORT STATMENT OF COMPLIANCE 601R-RE-07220 DATED 7/21/99. 2 L 7 2 4F RT A21EA 1999073000202 19990730 00202 NM 1999 7 30 UPS99230166 1 19990725 A 2560 ACCESS PANEL BOEING 727 727180C 138406G NM COCKPIT SIDE PNL STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:N/A, CAPTAINS EMERGENCY ESCAPE ROPE ACCESS PANEL DOES NOT OPEN WITH PUSH BUTTON. REPOSITIONED SIDEWALL PANEL TO ALLOW FOR PROPER OPERATION OF ROPE ACCESS. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999073000203 19990730 00203 NM 1999 7 30 UPS99430163 1 19990724 A 2120 HEAT DUCT BOEING 747 747121 1384871 NM CARGO COMPT DIRTY A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 683UP 20353 INSPECTION TYPE:N/A, AFT LWR CARGO COMPARTMENT FIRE WARNING ACCOMPLISHED LWR CARGO COMP SMOKE DET TEST, CKD OK. THOROUG HLY INSPECTED LOWER AFT CARGO COMP, NO EVIDENCE OF FIRE FOUND. WHEN INSPECTING CGO COMPT HEAT DUCT, FOUND PLASTIC TRASH STICKING TO THE DUCT. TRASH WAS PARTLY BURNED AND MOLTEN CAUSING FIRE ALARM GOING OFF. DEFERRED AFT LWR CARGO HEAT PE R MEL. 2 L 7 4 4F A20WE 1999073000204 19990730 00204 NM 1999 7 30 UPS99430164 1 19990718 A 5330 SKIN BOEING 747 747121 1384871 NM LAV DUMP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE:N/A, FUSELAGE SKIN LT SIDE OF LAV DUMP HAS CORROSION AND POPPED HI-LOK RIVET HEADS. REMOVED CORROSION A ND ACCOMPLISHED EO B747 5330 11468 A. 2 L 7 4 4F A20WE 1999073000205 19990730 00205 NM 1999 7 30 UPS99430165 1 19990723 A 3350 SIGN BOEING 747 747123 1384873 NM SERVICE DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:IN, EXIT SIGN OVER CREW SERVE DOOR DOES NOT ILLUMINATE. RESET CANNON PLUG, OP CHECKS OK. 2 L 7 4 4F A20WE 1999073000206 19990730 00206 WP 1999 7 30 UPS99830159 1 19990630 A 5230 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, MAIN CARGO DOOR FTG CRACKED UPPER FWD CORNER NEAR ACTUATOR. INSTALLED NEW FITTING, ACTUATOR SUPPORT AND CORNER FITTING IAW UPS DC8 SRM 51-1-21 & 51-3-0, UPS DCI M/M 52-36-03 & 52-36-01. 2 L 7 4 4F RT 4A25 1999073000207 19990730 00207 WP 1999 7 30 UPS99830160 1 19990707 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 889 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, LEFT WING O/B LEADING EDGE, OUTBOARD END TOP SIDE SKIN IS CRACKED STA 889. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1 & 51-1-21. 2 L 7 4 4F RT 4A25 1999073000208 19990730 00208 WP 1999 7 30 UPS99830161 1 19990704 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, C-PIT STA 1160 FLOORBEAM SUPPORT EXFOLIATED L27L. FABRICATED AND INSTALLED NEW FLOORBEAM SUPPORT AN D SHIM IAW REO NR 06609 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999073000209 19990730 00209 WP 1999 7 30 UPS99830162 1 19990701 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, C-PIT GILLINER SUPPORT ANGLE CORRODED STA 1160 LONG 26L-27L. FABRICATED AND INSTALLED WEB, DOUBLER, FILLER IAW DC8 SRM 51-1-20D, 51 -1-21 DAC DWG 9751879 AND EO DC8 5350-7876. 2 L 7 4 4F RT 4A25 1999073000210 19990730 00210 NM 1999 7 30 99FDEA00282 1 19990726 A 5330 655458313 SKIN BOEING 727 7272S2F 1384O81 NM BS 1072-1083 LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 NR 239 - 4 LIGHTNING STRIKES IN EXTERNAL SKIN BETWEEN BS 1072-1083 AT STR 30. REPAIRED DAMAGED SKIN AT BS 1072.5, STR 3 0 PER FEDEX 7-5330-46963. 2 L 7 3 4F A3WE 1999073000211 19990730 00211 NM 1999 7 30 99FDEA00283 1 19990726 A 5330 655458313 SKIN BOEING 727 7272S2F 1384O81 NM BS 1088-1097 LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 201FE 22924 NR 240 - 3 LIGHTNING STRIKES IN EXTERNAL SKIN AT BS 1088-1097, STR 30. INSTALL PATCH AND INSTALL FILLER WITH SOLID RIVE TS IAW FEDEX SRM 53-30-3 AND EA NR 7-5330-46963, BS 1088-1097, STR 30. 2 L 7 3 4F A3WE 1999073000212 19990730 00212 WP 1999 7 30 ABXA9900593 1 19990714 A 5312 9915558242 BULKHEAD ANGLE DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND A CRACKED ANGLE ON THE AFT PRESSURE BULKHEAD AT LONGERON 16 RIGHT. REPLACED ANGLE IAW DC9 SRM 51- 30-5. 2 L 7 2 4F A6WE 1999073000213 19990730 00213 WP 1999 7 30 ABXA9900594 1 19990714 A 5312 9915558230 BULKHEAD ANGLE DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND A CRACKED ANGLE ON THE AFT PRESSURE BULKHEAD AT LONGERON 12 RIGHT. REPLACED ANGLE IAW DC9 SRM 51- 30-5. 2 L 7 2 4F A6WE 1999073000214 19990730 00214 WP 1999 7 30 ABXA9900595 1 19990714 A 5312 9915558236 BULKHEAD ANGLE DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND CRACKED ANGLE ON AFT PRESSURE BULKHEAD AT LONGERON 14 RIGHT. REPLACED ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999073000215 19990730 00215 WP 1999 7 30 ABXA9900596 1 19990714 A 5312 9915558237 BULKHEAD ANGLE DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND CRACKED ANGLE ON AFT PRESSURE BULKHEAD AT LONGERON 15 LEFT. REPLACED ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999073000216 19990730 00216 WP 1999 7 30 ABXA9900597 1 19990714 A 5320 995773925 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1021 AND LONGERON 15 LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999073000217 19990730 00217 NM 1999 7 30 SCNA99095 1 19990723 A 2131 CONTROLLER BOEING 727 727225 1384077 NM CABIN FAILED A SCNA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 283SC 22559 UPON DESCENT CABIN BEGAN TO CLIMB AT 1200 FEET PER MINUTE, CLOSED CABIN OUTFLOW VALVE AND CLIMB DIDN'T CHANGE. WENT TO STANDBY MODE AND THEN MANUAL BUT COULD NOT CONTROL PRESSURIZATION. ALL PASSENGER SERVICE UNIT OXYGEN MASKS DROPPED. PR ESSURIZED AIRCRAFT AND FOUND FLOW AND RATE OF CLIMB TO CHECK NORMAL. NO LEAKS WERE NOTED. PERFORMED OPERATIONAL CHECK OF PRESSURIZATION CONTROLLER. SYSTEM CHECKS GOOD IAW MM 21310. 2 L 7 3 4F A3WE 1999073000218 19990730 00218 NM 1999 7 30 SWAA991224 1 19990721 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM, BS 967, RBL 42. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999073000219 19990730 00219 NM 1999 7 30 SWAA991225 1 19990722 A 5320 6545772 SPLICE BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D-CHECK, FOUND 2 STRINGER SPLICES CRACKED, BS 907, STRINGERS 4L AND 4R. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2 L 7 2 4F RT A16WE 1999073000220 19990730 00220 NM 1999 7 30 SWAA991226 1 19990722 A 5320 6545409 WEB BOEING 737 7373H4 1384600 NM BS 636-639 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED, BS 636-639, RT SIDE. REPAIRED WEB SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999073000221 19990730 00221 NM 1999 7 30 SWAA991227 1 19990722 A 5312 6516300 BULKHEAD BOEING 737 7372T4 1384492 NM BS 178. CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 10, WL 234. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999073000222 19990730 00222 NM 1999 7 30 SWAA991228 1 19990722 A 5320 65C27314 CLIP BOEING 737 7372T4 1384492 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D-CHECK, FOUND 2 STRINGER CLIPS CRACKED, BS 520, STRINGERS 19L AND 19R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F A16WE 1999073000223 19990730 00223 NM 1999 7 30 SWAA991229 1 19990721 A 5320 6567127 WEB BOEING 737 7372H4 138448C NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED C2 CHECK, FOUND CRACKED UPPER PRESS WEB, RT MLG WHEEL WELL BS 716, RBL 16. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 1999073000224 19990730 00224 NM 1999 7 30 SWAA991221 1 19990721 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED C1 CHECK, FOUND EEPLS WIRING EXPOSED AND LENS COVER MISSING. REROUTED WIRES AND REPLACED LENS COVER PE R MM. 2 L 7 2 4F RT A16WE 1999073000225 19990730 00225 NM 1999 7 30 SWAA991222 1 19990721 A 5523 65C2638415A TAB BOEING 737 7373Q8 1384670 NM LT ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED BC4 CHECK, FOUND LT ELEVATOR TAB CRACKED. REMOVED AND REPLACED LT ELEVATOR TAB ASSY PER MM. 2 L 7 2 4F RT A16WE 1999073000226 19990730 00226 NM 1999 7 30 SWAA991223 1 19990721 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED, BS 663, STRINGER 10L. REMOVED AND REPLACED STRINGER CLIP PER MM. 2 L 7 2 4F RT A16WE 1999073000227 19990730 00227 NM 1999 7 30 SWAA991211 1 19990720 A 3230 6558206 SENSOR BOEING 737 7373H4 1384600 NM RT MLG OUT OF ADJUST A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 386SW 26601 AFTER TAKEOFF MLG WOULD NOT RETRACT, HANDLE WOULD NOT GO PAST OFF POSITION. ADJUSTED GROUND SHIFT CABLE AND AIR SAFETY SENSOR PER MM. 2 L 7 2 4F RT A16WE 1999073000228 19990730 00228 NM 1999 7 30 SWAA991212 1 19990720 A 5330 6545791 SKIN BOEING 737 7373A4 1384585 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 DURING RON CHECK, FOUND FUSELAGE SKIN CRACKED APPROX BS 500C+5, STRINGER 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999073000229 19990730 00229 NM 1999 7 30 SWAA991213 1 19990720 A 2913 371380 PUMP BOEING 737 7375H4 138449D NM NR 2 ENGINE INOP A SWAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 07 508SW 24185 NR 2 ENG HYD PUMP FAILED. REMOVED AND REPLACED NR 2 ENG HYD PUMP AND DRAIN FILTER PER MM. 2 L 7 2 4F RT A16WE 1999073000230 19990730 00230 NM 1999 7 30 SWAA991214 1 19990719 A 5312 BAC1490 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND T-CHORD CRACKED, BS 178 BULKHEAD RBL 24 WL 207. REPAIRED T-CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999073000231 19990730 00231 NM 1999 7 30 SWAA991215 1 19990719 A 5320 6545409245 WEB BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND BS 663 PRESS WEB CRACKED, LBL 32. REPAIRED WEB PER SWA RA NR 1-353-2121. 2 L 7 2 4F RT A16WE 1999073000232 19990730 00232 NM 1999 7 30 SWAA991216 1 19990720 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM BS 350 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN, BS 350 ABOVE STRINGER 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999073000233 19990730 00233 NM 1999 7 30 SWAA991217 1 19990720 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 328, RBL 28- RBL 35. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999073000234 19990730 00234 NM 1999 7 30 SWAA991218 1 19990721 A 2760 6978455 SWITCH BOEING 737 7373G7 1384595 NM SPOILER HANDLE OUT OF ADJUST A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 690SW 23783 TAKEOFF WARNING SOUND WENT OFF PRIOR TO 80 KNOTS. RAN ENGS AND OPS CHECKED GOOD. SECOND TAKEOFF ATTEMPT, TAKEOFF WARNI NG SOUND WENT OFF AGAIN PRIOR TO 80 KNOTS. CLEANED AND ADJUSTED SPOILER HANDLE SWITCH ASSY, OPS CHECKED GOOD PER MM. 2 L 7 2 4F RT A16WE 1999073000235 19990730 00235 NM 1999 7 30 SWAA991219 1 19990720 A 3350 079123 COVER BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHT LENS MISSING. INSTALLED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 1999073000236 19990730 00236 NM 1999 7 30 SWAA991220 1 19990721 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND 8 CRACKS FROM 1 TO 4 INCHES LONG AT BS 178 BULKHEAD, LBL 24-RBL 24. REPAIRED BULKHEA D PER SWA RA NR 1-353-2124. 2 L 7 2 4F RT A16WE 1999073000237 19990730 00237 NM 1999 7 30 TWAA9910401 1 19990721 A 2761 8144DL PLUG BOEING 727 727231 1384079 NM NR 5 SPOILER ACT FAILED A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 54348 21967 ABOUT 15 MINUTES INTO FLIGHT LOST B HYDRAULIC SYSTEM FLUID. RETURNED TO STL. THE NUMBER 5 SPOILER PLUG BLEW OUT OF THE ACTUATOR. REPLACED THE PLUG. CHECK-C 12-13-98 MCI. 2 L 7 3 4F A3WE 1999073000238 19990730 00238 NM 1999 7 30 TWAA9910402 1 19990722 A 3350 1317 LAMP BOEING 767 7673Q8 NM ROW 19 & 40 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 FOUND EGRESS LIGHT INOPERATIVE AT ROW 19 LT SIDE OF CABIN, AND ROW 40 LT SIDE OF CABIN. REPLACED THE LAMP AT BOTH LOCAT IONS. CHECK-C 6-27-99 LAX. 2 L 7 2 4F RT A1NM 1999073000239 19990730 00239 NM 1999 7 30 TWAA9910403 1 19990722 A 3350 S417N50912 LIGHT BOEING 767 7673Q8 NM ROW 1 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 FOUND THE EGRESS LIGHTS INOPERATIVE AT ROW 1 ON LEFT SIDE OF CABIN. REPLACED THE LIGHT STRIP. CHECK-C 6-27-99 LAX. 2 L 7 2 4F RT A1NM 1999073000240 19990730 00240 NM 1999 7 30 HNAA9900105 1 19990722 A 2611 3023143 SMOKE DETECTOR 30326E7 DHAV DHC8 DHC8201 2809001 NM CARGO COMPT FAILED A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 994HA 65250 459 SMOKE WARNING LIGHT CAME ON IN FLIGHT WITH ASSOCIATED MASTER WARNING LIGHT. 2 H 7 2 4T RT A13NM 1999073000241 19990730 00241 WP 1999 7 30 AT9900495 1 19990619 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 541 MISDRILLED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND MISDRILLED HOLE IN INTERCOSTAL SUPPORT FITTING AT BS 541 L-24R. REM OVED FITTING, SPOT FACE HOLE, NDT VERIFIED NO CRACKS. PLUG HOLE WITH HL-18 HI-LOK IAW DC9 SRM 51-30-5 AND TIMCO RES NR 07654. 2 L 7 2 4F A6WE 1999073000242 19990730 00242 WP 1999 7 30 AT9900496 1 19990722 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 169 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND FUSELAGE SKIN AT BS 169 L-22L CRACKED. REMOVED DOUBLER AND FABRICAT ED REPAIR AND INSTALLED IAW AIRTRAN RES NR 99-1265 AND EA NR 09-5310-29-A1487. 2 L 7 2 4F A6WE 1999073000243 19990730 00243 WP 1999 7 30 AT9900497 1 19990701 A 5230 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE AFT LOWER CARGO DOOR INNER PAN CRACKED. BLENDED AREA SMOOTH, FA BRICATED REPAIR DOUBLER, DRILLED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, AND EO NR 99-1181. 2 L 7 2 4F A6WE 1999073000244 19990730 00244 WP 1999 7 30 AT9900498 1 19990712 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 FOUND THE TAIL SECTION CANTED FRAME AT BS 1143 RIGHT SIDE CRACKED AT REAR STAIR ACTUATOR MOUNT. FABRICATED REPAIR DOUBL ERS, HEAT TREAT ANGLES, DRILLED, DEBURRED, AND INSTALLED IAW DC9 SRM 51-10-2A, 51-30-2, 51-10-4, 51-10-3, AND TIMCO RES NR 07025 AND TIMCO EO NR 99-1189. 2 L 7 2 4F A6WE 1999073000245 19990730 00245 1999 7 30 MALA976519 4 19990712 A 3444 9650876040B07B GPWS SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 436XJ 436 ON SHORT FINAL GPWS INDICATED TOO LOW GEAR WHEN THE 3 GREEN GEAR LIGHTS INDICATED DOWN AND INTRANSIT LIGHT OUT. MAINTEN ANCE REPLACED GPWS COMPUTER, OPS CHECKS GOOD IAW SF340 MM CHAPTER 34. 2 L 7 2 4T RT A52EU 1999073000246 19990730 00246 EU 1999 7 30 MALA976520 1 19990714 A 3350 END CAP BAC 146 AVRO146RJ85A 1500097 EU CABIN MISSING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 504XJ E2311 REAR CABIN EMERGENCY TRACK LIGHTING MISSING END CAP, EMERGENCY LIGHTS TO EXPOSED. MAINTENANCE REPLACED END CAP FOR EMER GENCY LIGHTS, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999073000247 19990730 00247 EU 1999 7 30 MALA976521 1 19990711 A 3230 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG LEAKAGE A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 15 112XJ 340A112 ON TAKEOFF HYD CAUTION CAME ON, MAIN ACCUMULATOR WAS 0 AND QUANTITY WAS IN YELLOW. GEAR PUMP WAS TURNED OFF, GEAR WAS I N RETRACTION MODE AND ON LEFT MAIN UNLOCKED FROM THE DOWN POSITION. QRH CHECK LIST WAS USED AND LEFT MAIN WAS HAND PUM PED DOWN, 0 FLAP LANDING WAS PERFORMED IN LAN. POST FLIGHT SHOWED HYD FLUID ALL OVER RIGHT MAIN GEAR. MAINTENANCE REPL ACED RIGHT DOWNLOCK SWIVEL ASSEMBLY. CYCLED GEAR SEVERAL TIMES, OPS CHECK GOOD AND LEAK CHECK GOOD IAW SAAB MM 32-00-00 . 2 L 7 2 4T RT A52EU 1999073000248 19990730 00248 EU 1999 7 30 MALA976522 1 19990705 A 2150 MOTOR SAAB SF340 340B 7860101 EU CABIN AIR COND FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 417XJ 340B417 CREW NOTED SMOKE IN CABIN, SUSPECTED SUPPLEMENTAL AIR CONDITIONER. MAINTENANCE REPLACED A/C MOTOR AND RESET MAIN 105A C B IN RT PDU PANEL. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999073000249 19990730 00249 EU 1999 7 30 JBXA9900093 2 19990724 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 2 VIBRATION A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 104ML 11445 17636 AFTER LIFTOFF IN RDU CREW GOT A VIBRATION HIGH ENG. NR 2 INDICATION ON INNER TAPE (N2). OCCURRED WITH VIBRATION SWITCH IN BOTH NORMAL AND ALTERNATE POSITIONS. CREW REDUCED POWER TO CLIMB POWER AND VIBRATION WARNING CLEARED, BUT WAS STILL IN THE HIGH IN THE NORMAL RANGE. INDICATION STAYED WITHIN LIMITS FOR THE REMAINDER OF THE AIR RETURN. PERFORMED GROUN D RUNS FOR 10 MINUTES AND FOUND VIBRATION TO BE WITHIN LIMITS. ALSO, PERFORMED VIBRATION HIGH INSPECTION. ALL FOUND TO BE WITHIN LIMITS IAW F-100 71-00-00. 2 L 7 2 4F 4 F RT 1999073000250 19990730 00250 NM 1999 7 30 CALA9900850 1 19990722 A 3230 RELAY BOEING 737 7373T0 1384582 NM E & E COMPT INOP A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 14342 23580 THE GEAR HANDLE TRIGGER HAD TO BE PULLED TO RAISE LANDING GEAR PAST THE OFF POSITION AFTER TAKEOFF. THE FLIGHT CONTINUE D TO LAX WHERE IT LANDED WITHOUT INCIDENT. THE FAULT WAS DUPLICATED ON THE GROUND. THE LANDING GEAR LEVER REMAINED LOC KED. MAINTENANCE FOUND THE R276 AIR SENSE RELAY AT FAULT. THE R276 RELAY WAS REMOVED AND REPLACED AND GROUND CHECKS WE RE GOOD IAW MM 32-31-21 AND 32-31-31. 2 L 7 2 4F RT A16WE 1999073000251 19990730 00251 NM 1999 7 30 CALA9900851 1 19990722 A 3350 6013211 POWER SUPPLY GRIMES BOEING 727 727224 1384076 NM E & E COMPT INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND THE FORWARD ENTRY AND FORWARD GALLEY ESCAPE SLIDE EMERGENCY LIGHTS INOPERATIVE. THE BATTERY AND POWER SUPPLY IN E&E COMPARTMENT WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1999073000252 19990730 00252 NM 1999 7 30 CALA9900852 1 19990722 A 3350 3114981 LIGHT GRIMES BOEING 737 7373T0 1384582 NM L-2 DOOR INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17328 23458 INSPECTION FOUND THE L-2 DOOR SLIDE EMERGENCY EGRESS LIGHT INOPERATIVE. THE L-2 DOOR SLIDE EMERGENCY EGRESS REFLECTOR A SSEMBLY WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1999073000253 19990730 00253 WP 1999 7 30 CALA9900853 1 19990628 A 5330 SKIN DOUG DC9 DC982 3022082 WP L1 DOORWAY GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND A GOUGE IN FUSELAGE SKIN AT L-1 DOOR AFT CUTOUT. REPAIRED IAW SRM 53-05, FIGURE 26A. 2 L 7 2 4F A6WE 1999073000254 19990730 00254 WP 1999 7 30 CALA9900854 1 19990721 A 5753 SKIN DOUG DC9 DC982 3022082 WP RT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND RT O/B FLAP PANEL O/B LOWER SURFACE DENTED WITH A BULGE ON O/B END. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1999073000255 19990730 00255 WP 1999 7 30 CALA9900855 1 19990721 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 200-207 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND A 1.25 INCH CRACK IN SKIN AT FASTENER HOLE OF STA 200-207, LONGERON 15L. THE SKIN WAS REPAIRED IAW EA PD80-53-006. 2 L 7 2 4F A6WE 1999073000256 19990730 00256 WP 1999 7 30 CALA9900856 1 19990723 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 465 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND ELONGATED BOLT HOLES IN FORWARD BAGGAGE BIN FLOORBOARD SUPPORT BEAM AT STA 465 FROM STRINGER 227R TO 27 L. THE FLOORBOARD SUPPORT BEAM AND FASTENERS WERE REPLACED IAW ECRA 5320-01588. 2 L 7 2 4F A6WE 1999073000257 19990730 00257 WP 1999 7 30 CALA9900857 1 19990723 A 5512 SKIN DOUG DC10 DC1010 3022110 WP RT HORIZ STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND THREE AFT T/E PANELS DELAMINATED FROM I/B HINGE POINT TO HORIZONTAL TIP AT LOWER RIGHT HORIZONTAL STABI LIZER. THE THREE PANELS WERE REMOVED AND REPLACED IAW MM 51-31-01. 2 L 7 3 4F A22WE 1999073000258 19990730 00258 EA 1999 7 30 COMA9960386 1 19990721 A 2613 OVERHEAT WARNING CNDAIR CL600 CL6002B19 EA CARGO FAN ACTIVATED A COMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 785CA 7326 CARGO OVERHEAT WARNING. DEFERRED CARGO FAN. 2 L 7 2 4F RT A21EA 1999073000259 19990730 00259 EA 1999 7 30 COMA9960387 1 19990720 A 5270 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 958CA 9111 CABIN DOOR WARNING. ADJUSTED DOOR PROXIMITY SENSORS. 2 L 7 2 4F RT A21EA 1999073000260 19990730 00260 EA 1999 7 30 COMA9960388 1 19990719 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 710CA 7241 FLAPS FAILED. RESET FLAP SYSTEM. 2 L 7 2 4F RT A21EA 1999073000261 19990730 00261 NM 1999 7 30 UPS99230154 1 19990722 A 5720 658216229 BEAM BOEING 727 72722C 138400F NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C, CORROSION ON LOWER SURFACE OF LT WING LANDING GEAR BEAM AT NR 4 FLAP TRACK MOUNT. REPAIRED LANDING G EAR BEAM AT NR 4 FLAP TRACK IAW ER 99-5716 (UPS FILE 727-57-2091). 2 L 7 3 4F A3WE 1999073000262 19990730 00262 NM 1999 7 30 UPS99230155 1 19990721 A 5312 BULKHEAD BEAM BOEING 727 72722C 138400F NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE:C INSP 1183 BULKHEAD BL 3683 L AND RT VERTICAL BEAMS & BL 26.83 LT AND RT VERTICAL BEAM AT WL 238 FOUND RBL 26.83 CRACKED. REPAIRED RBL 26.83 VERTICAL BEAM PER ESR 0008 AND EO B727-5310-1116 APPENX E. 2 L 7 3 4F A3WE 1999073000263 19990730 00263 NM 1999 7 30 UPS99230156 1 19990723 A 5320 CREASE BEAM BOEING 727 7272A1 138407F NM BS 1166 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C, LEFT I/B CREASE BEAM IS CUT AT BS 116, WL 209, LBL 64. FOUND CREASE BEAM TO BE CRACKED AT BS 1166, W L 209, LBL 64 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF CREASE BEAM FROM BS 1157 TO BS 1177, FABRICATED NE W CREASE BEAM, REPAIR ANGLE AND SPLICE AND FILLER AND INSTALLED REPAIR PARTS AND CREASE BEAM IAW SRM 51-40-3, SRM 51-30- 2 SRM 51-30-8 FIG 8. 2 L 7 3 4F A3WE 1999073000264 19990730 00264 NM 1999 7 30 UPS99230157 1 19990722 A 5320 SPLICE BOEING 727 7272A1 138407F NM BS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C, WHILE WORKING CARD 973519, FOUND CORROSION AND GOUGE ON STRINGER SPLICE BS 1000, STR 29R, RBL 6, WL 1 48. REMOVED AND REPLACED STR SPLICE BS 1000 STR 29R, RBL 6, WL148, WITH NEW STR SPLICE. 2 L 7 3 4F A3WE 1999073000265 19990730 00265 WP 1999 7 30 UPS99830145 1 19990704 A 5230 DOOR TRACK DOUG DC8 DC873F 302199F WP BS 1200-1210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, AFT CARGO PIT CORROSION ON I/B AND O/B FACES OF INTERCOSTAL IN 'C' PIT DOOR TORQUE OBX STA 1200-1210 L29R. FABRICATED AND INSTALLED DOOR TRACK IAW DC8 SRM 51-3-8 DAC DWG 9754947. 2 L 7 4 4F RT 4A25 1999073000266 19990730 00266 WP 1999 7 30 UPS99830146 1 19990701 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, SHEAR THE CRACKED STA 1160 LONG 26L-27L INSIDE C-PIT DOOR TORQUE BOX. FABRICATED AND INSTALLED NEW SHEAR TIE SECTION IAW DAC DWG NR 9754002 & DC8 SRM 51-1-20D, 53-2-0 FIG 2B. 2 L 7 4 4F RT 4A25 1999073000267 19990730 00267 WP 1999 7 30 UPS99830147 1 19990701 A 5320 STANTION DOUG DC8 DC873F 302199F WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, LT FLOORBEAM SUPPORT STA 1180 CORRODED 12 INCHES ABOVE LONG 27L. REMOVED STANTION, LOCATED DRILLED AND DEBURRED NEW STANTION. INSTALL ED NEW STANTION IAW UPS DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999073000268 19990730 00268 WP 1999 7 30 UPS99830148 1 19990713 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, RT HORZ STAB O/B LEADING EDGE, I/B END, HAS CORROSION AROUND SCREW HOLES. FABBED AND INSTALLED REPA IR FILLED AND DOUBLER IAW DC8 SRM 51-1-21, 51-2 -0, & REO 06610. 2 L 7 4 4F RT 4A25 1999073000269 19990730 00269 WP 1999 7 30 UPS99830149 1 19990713 A 5753 WEB DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, LT WING, I/B FLAP, I/B SIDE, CLOSE OUT WEB CRACKED SEVERAL PLACES. FABRICATED AND INSTALLED NEW WEB , DOUBLER AND STIFFENERS IAW REO 06611 AND DC8 SRM 51-1-21 & 51-1-14. 2 L 7 4 4F RT 4A25 1999073000270 19990730 00270 WP 1999 7 30 UPS99830150 1 19990702 A 5753 HINGE DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, LT OUTBOARD FLAP 339 FLAP HINGE SUPPORT FITTING CRACKED. REMOVED AND REPLACED FLAP HINGE FITTING SU PPORT IAW S/B 27-249. 2 L 7 4 4F RT 4A25 1999073000271 19990730 00271 WP 1999 7 30 UPS99830151 1 19990701 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:C2, CARGO PIT CORROSION ON BOTTOM SIDE OF MAIN CABIN FLOORBOARD AND SEAT TRACK STA 1000-1100 X3 TO -3. F ABRICATED AND INSTALLED FLOOR PANELS IAW DC8 SRM 51-1-8 & 51-3-0, 53- 2-3 AND ADDENDUM DC8-53B-003. 2 L 7 4 4F RT 4A25 1999073000272 19990730 00272 WP 1999 7 30 UPS99830158 1 19990721 A 5414 SKIN DOUG DC8 DC871F 302199D WP NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A ON POST FLIGHT, ENGINEER AND MECHANIC VERIFIED A SMALL CRACK ON NR 2 PYLON. ACCOMPLISHED EO DC8-543 0-11626-A APPENDIX B INTERIM REPAIR NR 2 PYLON OUTBOARD RAMP AT THE ENGINE FAN EXHAUST OUTLET. TRANSFERRED TO DMI LIST C/N D-175661 ASSIGNED. 2 L 7 4 4F RT 4A25 1999073000273 19990730 00273 NM 1999 7 30 QXEA9901469 1 19990721 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 358PH 2907 322 506 SEA- SEVERAL EMERGENCY FLOOR LIGHTS ARE INOP. MAINTENANCE REPAIRED THE WIRE CONNECTOR AT 3352-P3, RECONNECTED CONNECTIO N AT 3352-P10 AND REPLACED BATTERY PACK AT PS-1. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999073000274 19990730 00274 NM 1999 7 30 99FDEA00276 1 19990709 A 3220 TORSION LINKS BOEING 727 7272S2F 1384O81 NM NLG SCRATCHED A FDEA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 211FE 22933 A SEVERE VIBRATION OCCURRED WHEN LEFT RUDDER WAS APPLIED TO TURN LEFT OFF THE RUNWAY. A/C WAS STOPPED IMMED AND EMERGEN CY EQUIP WAS CALLED OUT. REMOVED AND REPLACED BOTH UPPER AND LOWER NOSE GEAR TORSION LINKS AS PER MM 32-21-21. INSTALL ED NG ELECTRICAL HARNESS, NOSE WHEEL STEERING CTRL ROD PER MM 32-21-51 PG 401, MM 32-20-01. 2 L 7 3 4F A3WE 1999073000275 19990730 00275 EU 1999 7 30 99FDEA00277 1 19990722 A 3411 PITOT TUBE AIRBUS 310 A310203 EU NR 1ADC DIRTY A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 445FE 297 DURING T/O, CAPT AIRSPEED ON NR 1 PFD WAS 30 KTS SLOWER THAN F/O'S AIRSPEED ON NR 2 PFD. *S/D* CLEANED OUT PITOT LINE ON NR 1 ADC. OPS CK GOOD PER AIRBUS MM 34-10-00. 2 L 7 2 4F RT A35EU 1999073000276 19990730 00276 NM 1999 7 30 99FDEA00278 1 19990723 A 5270 SWITCH BOEING 727 72727C 138400J NM CARGO DOOR STICKS A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 146FE 19110 AFT CARGO DOOR LIGHT ILLUMINATED AFT T/O, LIGHT EXT ON APPROACH, AT APPROACH SPD. FOUND INNER DOOR SWITCH STUCK. LUBED SWITCH, OPS CK NORMAL. 2 L 7 3 4F A3WE 1999073000277 19990730 00277 NM 1999 7 30 99FDEA00279 1 19990722 A 2750 CABLES BOEING 727 727227 1384078 NM TE AFT FLAP LOOSE A FDEA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 25 484FE 21466 A/C STARTED AIRFRAME VIBRATION. FOUND EDGE FLAPS AFT FLAP FOLLOW UP CABLES LOOSE. RIGGED CABLES PER 727 MM 27-51-5-4, OPS CK GOOD. 2 L 7 3 4F A3WE 1999073000278 19990730 00278 NM 1999 7 30 99FDEA00280 1 19990726 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM CARGO COMPT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 606FE 48602 FOUND CRACK ON SEAT TRACK. SEAT TRACK SPLICE CUT AND REWORKED PER SRM 53-42-01. 2 L 7 3 4F RT A22WE 1999073000279 19990730 00279 EU 1999 7 30 99FDEA00281 1 19990723 A 3241 CONTRL AIRBUS 300 A300F4605R 3930327 EU AUTOBRAKE SYS INOP A FDEA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 665FE 769 ON LAND WITHOUT AUTOBRAKES ARMED, MAX BRAKES WERE APPLIED BY AUTOBRAKE SYSTEM. BRAKE APPLIED, GREEN STRIP IN MAX. AUTO BRAKES SWITCH WAS CYCLING ON & OFF. TOE BRAKES USED TO RELEASE BRAKES. REMOVED AND REPLACED AUTOBRAKE SYS CONTROL UNIT AMM 32-42-72-4. REMOVED AND REPLACED AUTOBRAKE MAX ON-OFF SWITCH AMM 33-10-00-4. OPS CK. 2 L 7 2 4F RT A35EU 1999073000280 19990730 00280 WP 1999 7 30 ABXA9900588 1 19990721 A 5250 AR25291 LATCH DOUG DOUG DC8 DC861 3021952 WP COCKPIT DOOR OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 COCKPIT DOOR HANDLE WOULD NOT UNLOCK. ADJUSTED INNER LATCH, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999073000281 19990730 00281 WP 1999 7 30 ABXA9900589 1 19990715 A 5312 99100733 PANEL DOUG DOUG DC9 DC941 302207N WP BS 83 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND HORIZONTAL PRESSURE PANEL CRACKED, OUTBOARD OF LEFT TUNNEL AREA IN NOSE WHEEL WELL AT STATION 83. REPAIRED IAW DC9 S/B 53-187 AND ABX REA D953-32263MR. 2 L 7 2 4F A6WE 1999073000282 19990730 00282 WP 1999 7 30 ABXA9900590 1 19990714 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1999073000283 19990730 00283 WP 1999 7 30 ABXA9900591 1 19990714 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1999073000284 19990730 00284 WP 1999 7 30 ABXA9900592 1 19990723 A 5755 5910055514 PANEL DOUG DOUG DC9 DC931 3022065 WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 DURING C-CHECK, FOUND INBOARD SPOILER PANEL CRACKED IN TWO PLACES AT DRIVE LINK CUTOUT. REPLACED SPOILER PANEL IAW DC9 MM 27-61-01. 2 L 7 2 4F A6WE 1999073000285 19990730 00285 NM 1999 7 30 MWEA99411 1 19990710 A 3350 60030431 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 601ME 49762 AFT OVERWING EMERGENCY EXIT OVERHEAD LIGHTS REMAIN ON WHEN POWER IS REMOVED FROM AIRCRAFT BUSSES. REPLACED EMERGENCY CE ILING BATTERY PACK. 2 L 7 2 4F RT A6WE 1999073000286 19990730 00286 WP 1999 7 30 MWEA99412 1 19990720 A 5320 591015837 WEB DOUG DC9 DC932 3022066 WP BS 937 MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FOUND MULTIPLE HOLES DRILLED IN WEB AFT OF AFT CARGO DOOR AT STATION 937. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999073000287 19990730 00287 WP 1999 7 30 MWEA99413 1 19990723 A 5311 27779305 FRAME DOUG DC9 DC932 3022066 WP BS 389 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FORWARD CARGO COMPARTMENT STATION 389 RIGHT SIDE OF LONGERON 30 HAS A CRACK IN THE FRAME. INSTALLED REPAIR FILLER SPACE R DOUBLER AND ANGLE. 2 L 7 2 4F A6WE 1999073000288 19990730 00288 WP 1999 7 30 MWEA99414 1 19990723 A 5320 9957447 TRAP PANEL DOUG DC9 DC932 3022066 WP LEFT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 LEFT HAND TRAPEZOIDAL PANEL CRACK BETWEEN FASTENERS NR 5 AND NR 4 (AS NUMBERED) FROM AFT FORWARD. CUT OUT DAMAGED AREA INSTALLED FILLER AND RE-FABRICATED 3 ANGLE. 2 L 7 2 4F A6WE 1999073000289 19990730 00289 WP 1999 7 30 MWEA99415 1 19990727 A 5320 9919402 TRAP PANEL DOUG DC9 DC932 3022066 WP RT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 RIGHT TRAPEZOIDAL PANEL CRACK BETWEEN FASTENERS NR 3 AND NR 2, AS NUMBERD FROM AFT FORWARD. CUT OUT AREA OF CRACKS AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 1999073000290 19990730 00290 NM 1999 7 30 MWEA99417 1 19990719 A 3610 39271012 VALVE DOUG MD88 MD88 3023688 NM RT ENGINE LOOSE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 701ME 49760 TAIL COMP TEMP HIGH ANNUNCIATOR CAME ON WITH ENGINE THROTTLE ADVANCEMENT AND GOES OUT WHEN THROTTLES ARE RETARDED. MTC RESECURED AUG VALVE AND REPLACED TURN BOOT ON RT SIDE ABOVE TEMP CONTROL VALVE. 2 L 7 2 4F RT A6WE 1999073000291 19990730 00291 WP 1999 7 30 MWEA99418 1 19990720 A 2560 11331706 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 FORWARD ENTRANCE DOOR ESCAPE SLIDE COVER IS NOT ATTACHED AT BOTTOM. MTC REINSTALLED DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999073000292 19990730 00292 WP 1999 7 30 MWEA99419 1 19990720 A 2560 113317 SLIDE COVER DOUG DC9 DC932 3022066 WP SERVICE DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 GALLEY SERVICE DOOR SLIDE COVER FELL OFF. REINSTALLED GALLEY SERVICE DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999073000293 19990730 00293 WP 1999 7 30 MWEA99420 1 19990723 A 5347 593056540 SEAT TRACK DOUG DC9 DC981 3022081 WP BS 936-1098 WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 SEAT TRACK NR 3 LUGS WORN AT STATIONS 946, 1003, 1060, 1098. INSTALLED NEW SEAT TRACK FROM STATIONS 936-1098. 2 L 7 2 4F A6WE 1999073000294 19990730 00294 WP 1999 7 30 MWEA99421 1 19990719 A 2560 113317 SLIDE COVER DOUG DC9 DC981 3022081 WP SERVICE DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FORWARD SERVICE DOOR EMERGENCY SLIDE GUARD UNATTACHED. RE-ATTACHED SLIDE COVER. 2 L 7 2 4F A6WE 1999073000295 19990730 00295 WP 1999 7 30 MWEA99422 1 19990717 A 2560 113317 GIRT BAR DOUG DC9 DC981 3022081 WP GALLEY DOOR STUCK A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 810ME 48072 FORWARD GALLEY GIRT BAR THE END VERY HARD TO REMOVE. CLEANED AND LUBED LATCH MECHANISM. INSTALLATION AND REMOVAL OF GI RT BAR NORMAL. 2 L 7 2 4F A6WE 1999073000296 19990730 00296 NM 1999 7 30 DL72S991598 1 19990714 A 5754 65162221 SKIN BOEING 727 727225 1384077 NM NR 3 LE SLAT BIRD STRIKE A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 NR 3 L/E SLAT/UPPER SKIN / OSS 170 - 190 DENT REPAIR. AT SHOP VISIT, THE UPPER SKIN WAS FOUND WITH A LARGE DENT. UPPE R SKIN CUTOUT RESULTED IN APPROX 20 X 20 CUTOUT. INCLUDING THE UPPER SKIN AFT OF THE NOSE BEAM AND THE L/E SKIN FWD OF THE NOSE BEAM. EXTENERAL REPAIR INSTALLED USING SOLID FASTENERS AFT OF NOSE BEAM AND BLIND FASTENERS. INSTALLED FWD OF NOSE BEAM IN INACCESSIBLE AREAS. 2 L 7 3 4F A3WE 1999073000297 19990730 00297 NM 1999 7 30 DL72S991599 1 19990716 A 5753 652163261 FASTENERS BOEING 727 727232 1384082 NM NR 2 TE MID FLAP MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 DURING SHOP INSPECTION, FOUND FASTENERS MISSING. THERE WAS NOT ENOUGH ROOM TO ADD FASTENERS, SO THE SPAR RAIL WAS SPLI CED. ON SO 738482, N/R CARD 012493 & 012494. 2 L 7 3 4F A3WE 1999073000298 19990730 00298 NM 1999 7 30 DL72S991600 1 19990624 A 5230 655714014 SKIN BOEING 727 727225 1384077 NM CARGO DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 ON SHOP VISIT, DAMAGE WAS FOUND TO THE TOP HALF OF THE C1 DOOR, OUTER SKIN. THE SKIN WAS TRIMMED BETWEEN THE NR 3 AND N R 4 STOP BEAMS AND REMOVED TO THE UPPER EDGE. A NEW SECTION WAS FABRICATED AND SPLICE INSTALLED. THE SPLICE CONSISTED OF AN EXTERNAL DOUBLER AND TRIPLER. 2 L 7 3 4F A3WE 1999073000299 19990730 00299 NM 1999 7 30 DL757991604 1 19990717 A 2611 SMOKE DETECTOR 2156204A BOEING 757 757232 1384965 NM CARGO COMPT INOP A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 604DL 22811 IMMEDIATELY AFTER TAKEOFF OUT OF RDU, RECEIVED A SMOKE CAUTION LIGHT ON EQUIP COOLING PANEL. STATUS MESSAGE OVERBOARD E XHAUST VALVE OPEN AND LEFT RECIRC FAN INOP LIGHT. CREW ELECTED TO RETURN TO RDU. CONTRACT MTC FOUND BAD SMOKE DETECTOR . REPLACED DETECTOR AND ALL CHECKED GOOD. 2 L 7 2 4F RT A2NM 1999073000300 19990730 00300 NM 1999 7 30 DLM11991605 1 19990717 A 3810 DRAIN VALVE AV24B3155C1 DOUG MD11 MD11 3023602 NM POTABLE WATER LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 807DE 48478 POTABLE WATER SUPPLY DECREASE FROM FULL TO EMPTY IN 4 HOURS. FOUND RT ELECT DRAIN VALVE LEAKING INTERNALLY. CAPPED LIN E AND VALVE. CLEARED WATER AND ICE OUT OF AFT STAB COMP, DEFERRED REPLACEMENT OF VALVE. 2 L 7 3 4F RT A22WE 1999073000301 19990730 00301 NM 1999 7 30 DL72K991607 1 19990717 A 3350 BATTERY 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA 14562 21232 FOUND FWD AISLE EXIT LIGHT INOP, T/S SYSTEM FOUND RACK ASSY AND BATTERY INOP. REPLACED BOTH SYSTEM, OPS NORMAL. 2 L 7 3 4F A3WE 1999073000302 19990730 00302 NM 1999 7 30 DL72W991609 1 19990717 A 3350 BULB BOEING 727 727247 138408F NM RT EMER EXIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2811W 20649 EMERGENCY LIGHT INOP LOCATED ON EXTERIOR OW BETWEEN RT EMERGENCY ESCAPE HATCHES. RELAMPED SAME, CHECKS GOOD. 2 L 7 3 4F A3WE 1999073000303 19990730 00303 NM 1999 7 30 DL76S991610 1 19990718 A 2760 S252T0016 SHUTOFF VALVE BOEING 767 767332 1382001 NM NR 10 SPOILER CRACKED A DALA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 135DL 25145 CENTER HYDRAULIC RESERVIOR NEEDS FLUID. FOUND NR 10 SPOILER ELECTRONIC SHUTOFF VALVE LEAKING. REPLACED SAME. 2 L 7 2 4F RT A1NM 1999073000304 19990730 00304 NM 1999 7 30 DL73K991611 1 19990718 A 3810 10607849 VALVE BOEING 737 737232 1384475 NM POTABLE WATER LEAKING A DALA K NONE K FLUID LOSS CR CRUISE 1 SO 27 322DL 23094 POTABLE WATER SCV VALVE LEAKING IN THE CLOSED POSITION WHEN A/C IS PRESSURIZED. SUSPECTED OF CAUSING ICE BALL THAT DAM AGED HORZ STAB. REPLACED THE VALVE AND L/E OF THE HORIZONTAL STAB. 2 L 7 2 4F RT A16WE 1999073000305 19990730 00305 NM 1999 7 30 DL767991612 1 19990718 A 2560 H205213 LATCH BOEING 767 767232 1385132 NM RT EMER EXIT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 THE RT OVERWING SLIDE DOOR WOULD NOT OPEN MANUALLY DUE TO WORN SPOTS IN THE LATCH CAM PLATE. THE DOOR OPERATED NORMAL LY AFTER REPLACING THE WORN LATCHES. 2 L 7 2 4F RT A1NM 1999073000306 19990730 00306 NM 1999 7 30 DL757991613 1 19990718 A 2120 AIR DIST BOEING 757 757232 1384965 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 667DN 25035 UNK OILY SMELL ON FINAL, IN MID CABIN. ON TAXI IN, STRONG SMELL THROUGH OUT CABIN AND FLT DECK. 2 L 7 2 4F RT A2NM 1999073000307 19990730 00307 NM 1999 7 30 DL72S991614 1 19990718 A 3350 LIGHT 900835A BOEING 727 727232 1384082 NM RT EMER EXIT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 539DA 10310 22385 DURING L/O, FOUND RIGHT OVERWING SLIDE LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999073000308 19990730 00308 NM 1999 7 30 DL72K991616 1 19990719 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM L2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 481DA 20861 L2 EMERGENCY BATTERY PACK FAILED TO ILLUMINATE DURING TEST. REPLACED PACK. 2 L 7 3 4F A3WE 1999073000309 19990730 00309 NM 1999 7 30 DL72S991617 1 19990714 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 NR 2 MIDFLAP/ UPPER SPAR CHORD / WBL 124.2: ALT FASTENER INSTALLED --- AD 94-07-08. DURING PREVENTATIVE MODIFICATIO N OF THE UPPER SPAR CHORD PER EO 4-58705-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED UPPER SPAR CHORD FASTENER COLLAR DU E TO PROXIMITY OF THE FASTENER HOLE TO THE SPAR RADIUS. AUTHORIZED USE OF RADIUS BLOCK PLUS MINI-NUT. 2 L 7 3 4F A3WE 1999073000310 19990730 00310 WP 1999 7 30 DLL19991618 1 19990708 A 5753 1529516119 SKIN LKHEED 1011 10113853 5265020 WP LT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 764DA 193H1202 WING, LT / OUTB'D FLAP / UPPER SKIN: DOUBLER REPAIR. THE UPPER SKIN WAS FOUND WITH MULTIPLE PUNCTURES AND DENTS DUE TO GROUND HANDLING. DAMAGE APPROX 30 SPAN WISE X 20 CHORD WISE. REPAIR CONSISTED OF TRIMMING OUT ENTIRE DAMAGE SECTION OF SKIN AND SPLICING NEW SECTION IN PLACE. 2 L 7 3 4F A23WE 1999073000311 19990730 00311 NM 1999 7 30 DL72L991619 1 19990622 A 5280 65192709 FITTING BOEING 727 727232 1384082 NM MLG DOOR HINGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 NR 4 INB'D FLAP TRACK TYP CORROSION FOUND AT MLG BEAM ATTACH PAD, WEAR AT FWD ATTACH LUGS AND WEAR AT FWD MLG DOOR HINGE FITTING HOLES. MLG BEAM ATTACH PAD MACHINED. FWD ATTACH LUGS OVERSIZED AND BUSHED. FWD MLG DOOR HINGE FITTING HOLES REWORKED PER SB 727-57-0180, REV 1. 2 L 7 3 4F A3WE 1999073000312 19990730 00312 NM 1999 7 30 DL757991620 1 19990719 A 5754 114N300251 SKIN BOEING 757 757232 1384965 NM NR 5 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 625DL 22915 NR 5 LE SLAT / TE WEDGE REPLACEMENT - FASTENER SUB. DURING ACCOMPLISHMENT OF TE WEDGE REPLACEMENT PER B757 SRM 57-54-02 , FIGURE 202, TWO HOLES COMMON TO THE WEDGE AND THE UPPER SKIN WERE ELONGATED. AUTHORIZED USE OF OVERSIZED FASTENERS. 2 L 7 2 4F RT A2NM 1999073000313 19990730 00313 1999 7 30 DL757991621 4 19990717 A 3160 SWITCH L9001 BOEING 757 757232 1384965 NM COCKPIT SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 605DL 22812 WHEN FWD LAV OCCUPIED LIGHT ON PILOT OVRHD PANEL IS PRESS TO TEST, IT CREATES SPARKS. REPLACED LAV OCCUPIED SWITCH LIGH T, CK'S GOOD. 2 L 7 2 4F RT A2NM 1999073000314 19990730 00314 NM 1999 7 30 DL73K991622 1 19990716 A 5320 65465431 FITTING BOEING 737 737232 1384475 NM BS 685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 FUSELAGE / LT MLG SIDE STRUT SUPPORT FITTING / FS 685 : LUG BORE CORROSION. THE LUG BORE OF THE LT MLG SIDE STRUT SUPP ORT FITTING WAS FOUND WITH CORROSION. THE BORE WAS OVERSIZED TO REMOVE THE CORROSION AND AN OVERSIZE BUSHING INSTALLED . THE REPAIR WAS ACCOMPLISHED PER ER/A 367806-14, REV A. 2 L 7 2 4F RT A16WE 1999073000315 19990730 00315 WP 1999 7 30 DLL10991623 1 19990716 A 5312 1503617111 BULKHEAD PANEL LKHEED 1011 10113851 5265010 WP BS 1809 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1732D 193C1213 FUSELAGE / AFT PRESSURE BULKHEAD / GORE PANEL / STRG. 11 : GOUGE REPAIR. THE AFT PRESSURE BULKHEAD WAS GOUGED BY A LOO SE DIAGONAL BRACE. THE GOUGE WAS ON THE AFT SIDE OF THE GORE PANEL AT FS 1809 NEAR STRINGER 11. THE GOUGE WAS CUTOUT W ITH A 1.0 HOLE AND REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 367758- 14, REV B. 2 L 7 3 4F A23WE 1999073000316 19990730 00316 NM 1999 7 30 DL72L991624 1 19990716 A 5521 657078419 SPAR BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 STABILIZER / LT ELEVATOR / REAR SPAR : CRACK REPAIR. THE L/H ELEVATOR WAS FOUND WITH CRACK EXTENDING.125 INCH BEYOND T HE 2ND FROM I/B END HINGE BRACKET. THE CRACK IS TYPICAL OF B727 S/B 55-0089 AND AD 96-06-05. THE CRACK WAS STOP DRILLE D PER ER/A 367822-14AD AND WILL BE INSPECTED WITHIN 1600 FLIGHT HOURS WITH PERMANENT MODIFICATION PER THE S/B WITHIN 320 0 FLIGHT HOURS. 2 L 7 3 4F A3WE 1999073000317 19990730 00317 NM 1999 7 30 DL73K991625 1 19990716 A 5330 654577882 SKIN BOEING 737 737247 138448D NM BS 332 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 FUSELAGE / SKIN ASSY / R1 DOOR CUTOUT / LOWER AFT CORNER / FS 332 : CRACK REPAIR. THE R1 DOOR CUTOUT WAS FOUND WITH A .375 INCH LONG TYPICAL CRACK IN THE LOWER AFT CORNER (FS 332). THE CRACK WAS THROUGH THE SKIN ASSY AND BEAR STRAP. THE CRACK WAS ROUTED OUT AND REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS PER ER/A 367813-14, REV A. 2 L 7 2 4F A16WE 1999073000318 19990730 00318 NM 1999 7 30 DL72S991626 1 19990719 A 5720 ANGLE BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 NR 5 SLAT LOWER COVE ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812. 2 L 7 3 4F A3WE 1999073000319 19990730 00319 1999 7 30 DL76S991627 4 19990719 A 2397 WIRE BOEING 767 767332 1382001 NM ROW 20FG CHAFED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 129DL 24079 A PASS AT SEAT 20E REPORTED ARCING AROUND HIS READING LIGHT THE PASS. READING LIGHTS IN THE AREA FAILED AND THE ENTERT AINMENT AUDIO THROUGH OUT THE AIRCRAFT FAILED. REPAIRED CHAFED POWER WIRES ABOVE SEATS 20 F AND G, OPS CK NORMAL. 2 L 7 2 4F RT A1NM 1999073000320 19990730 00320 NM 1999 7 30 DL75A991628 1 19990719 A 5210 MECHANISM BOEING 757 757212 NM PAX DOOR OUT OF ADJUST A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 757AT 23127 RIGHT FWD ENTRY DOOR HANDLE UNLOCKED AFTER T/O AND COULD NOT BE LOCKED. EICAS MSG R FWD ENT DOOR AND ENTRY DOOR LIGHT O N OVERHEAD PANEL CAME ON. ADJUSTED LOWER GATE AND STOP PINS PER MM. 2 L 7 2 4F RT A2NM 1999073000321 19990730 00321 NM 1999 7 30 DL72S991629 1 19990720 A 5230 65569271 FRAME BOEING 727 727232 1384082 NM CARGO DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 C-3 CARGO DOOR / DOOR STOP FITTING MODIFICATION / OMIT FRAME DOUBLER REPAIR: AD 90-06-09. DURING CURRENT SHOP VISIT, M TC ACCOMPLISHING DOOR STOP FITTING REPLACEMENT PER EO 4-59432-3AD. DAMAGE WAS FOUND TO FWD EDGE FRAME REQUIRING REPLACE MENT. EO REQUIRES TRIM OF FRAME TO FACILITATE FITTING REMOVAL AND SUBSEQUENT DOUBLER INSTALLED TO REPAIR TRIMMED FRAME. DUE TO FRAME REPLACEMENT, NO NEED TO TRIM FRAME. AUTHORIZED ACCOMPLISHMENT OF EO OMITTING FRAME TRIM. 2 L 7 3 4F A3WE 1999073000322 19990730 00322 NM 1999 7 30 DL76L991630 1 19990720 A 3350 BPS73 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM ROW 1-5 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 192DN 28449 FOUND DURING PDC FWD, BUSINESS CLASS EMERGENCY ESCAPE PATH LIGHTS IN SEATS ROW 1 THRU 5 INOP. FOUND AT SEAT 5AB AFT L UMINATOR RECEPTICLE BROKEN AND DAMAGE AND FUSE IN POWER SUPPLY BLOWN. REPLACED POWER SUPPLY AND LUMINATOR, CHECKS OK. 2 L 7 2 4F RT A1NM 1999073000323 19990730 00323 NM 1999 7 30 DL72S991631 1 19990720 A 5712 651622187 RIB BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999073000324 19990730 00324 NM 1999 7 30 DL76L991633 1 19990720 A 3350 POWER SUPPLY 20121 BOEING 767 767332 1382001 NM ROW 5AB INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 192DN 10764 28449 FOUND DURING INTERNATIONAL CHECK, EMERGENCY LIGHTS FROM 1A/B F/G THROUGH 5A/B F/G INOP. FOUND FUSES BLOWN ON POWER SUPP LY AT 2A/B AND LUMINATOR SHORTED AT SEAT 5A/B. REPLACED POWER SUPPLY AND LUMINATOR. LIGHTS TEST NORMAL. 2 L 7 2 4F RT A1NM 1999073000325 19990730 00325 NM 1999 7 30 DLM88991634 1 19990720 A 2170 COALESCER BAG V1211 DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 922DL 49646 NOTED MUSTY ODOR IN CABIN SHORTLY AFTER T/O AT 1000 AGL. F/A REPORTED SMOKE IN CABIN, RETURNED TO CVG. A/I NOT IN USE, OVEN AND SIDEWALL LIGHTS OFF, APU AIR ON PREVIOUS MCO. CHANGED WATER BAGS AND PERFORMED DUCT BURNOUT, ALL CKS OK. 2 L 7 2 4F RT A6WE 1999073000326 19990730 00326 NM 1999 7 30 DL72S991635 1 19990720 A 5753 6521631326K FLAP BOEING 727 727232 1384082 NM RT TE OTBD FLAP BROKE A DALA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 27 543DA 22392 ON APPROACH, RIGHT O/B TRAILING EDGE FOREFLAP BROKE IN HALF. DID NOT LEAVE AIRCRAFT. DID GO-AROUND. A/C LANDED WITHOU T INCIDENT. 2 L 7 3 4F A3WE 1999073000327 19990730 00327 NM 1999 7 30 DL72S991636 1 19990720 A 5210 STRAP 252046500 BOEING 727 727232 1384082 NM 2-L DOOR OUT OF POSITION A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 494DA 21074 DOOR 2L SAFETY WAS REPORTED BY F/A TO BE FLAPPING AGAINST OUTSIDE OF A/C AFTER T/O. INSPECTED AREA, NO APPRECIABLE DAMA GE NOTED. INSPECTED INTAKE NR 1 ENG, A-OK. REPLACED DAMAGED STRAP. 2 L 7 3 4F A3WE 1999073000328 19990730 00328 NM 1999 7 30 DL757991639 1 19990719 A 2810 FUEL TANK BOEING 757 757232 1384965 NM CENTER WING LEAKING A DALA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 676DL 25981 ON T/O GOT 5 SEC OF FUEL SMELL IN COCKPIT. FOUND FUEL LEAKING IN RT A/C BAY FROM CTR TANK. RT FWD SIDE AND AT RT WING ROOT AT TEMP REPAIR. RESEALED TANK AT TEMP REPAIR AND AT FWD LOWER RT CORNER OF CTR TANK. LEAK CKS OK. 2 L 7 2 4F RT A2NM 1999073000329 19990730 00329 NM 1999 7 30 DL76L991640 1 19990721 A 2820 VALVE AV311 BOEING 767 767332 1382001 NM RT ENGINE FAILED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 188DN P73355 27583 AT 10,000 FT, RT ENGINE SPAR VALVE LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. ENGINE DID NOT SHUT DOWN. WHEN A IRCRAFT ARRIVED AT GATE IN JFK THE CAPT SHUT THE ENGINE DOWN WITH THE T-HANDLE, UNABLE TO DUPLICATE. REPLACED VALVE ACT UATOR AS PRECAUTION. 2 L 7 2 4F RT A1NM 1999073000330 19990730 00330 NE 1999 7 30 DL72S991641 2 19990721 A 7320 BUSHING BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 FUEL CONTL WORN A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE DE DESCENT 1 SO 27 528DA 21702 700312 ON DESCENT INTO BHM, NR 2 THROTTLE RETARDED TO IDLE NR 2 ENG WENT TO HIGH POWER SETTING AND DID NOT RESPOND TO THROTTLE MOVEMENT. ACCOM PRECAUTIONARY ENG SHUTDOWN. OPENED NR 2 ENG COWLING AT GATE AND FOUND THE BUSHING ON THE FUEL CONTROL ROD WORN OUT. REPLACED ROD END BUSHING, RAN ENGINE PER PFHB, CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999073000331 19990730 00331 WP 1999 7 30 DLL19991642 1 19990721 A 2150 VALVE LKHEED 1011 10113853 5265020 WP NR 1 PACK INOP A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 760DH 193Y1194 HEARD POP THEN SMOKE CAME IN COCKPIT AIR VENTS. TURNED OFF NR 1 A/C PACK AND SMOKE STOPPED. FWD TO MCO/PLAC PER MEL. L OCKED CLOSED NR 1 PACK FLOW CONTROL VALVE. 2 L 7 3 4F A23WE 1999073000332 19990730 00332 NM 1999 7 30 DL757991643 1 19990721 A 3230 RETRACT MECH BOEING 757 757232 1384965 NM NLG MALFUNCTIONED A DALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 27 685DA 27588 ON APPROACH IAD PUT GEAR HANDLE TO THE DOWN POSITION, NOSE GEAR WOULD NOT EXTEND. TRIED ALTERNATE EXTEND, STILL DID NOT EXTEND. WENT BACK TO NORMAL EXTEND HEARD GEAR EXTEND. EMERGENCY LANDING IN IAD. MTC PINNED ALL GEAR ON RUNWAY. 2 L 7 2 4F RT A2NM 1999073000333 19990730 00333 NM 1999 7 30 DL72S991646 1 19990712 A 7120 65312813 ANGLE BOEING 727 727232 1384082 NM NR 2 ENG MOUNT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 0 ON HUSHKIT MODIFICATION, NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED. REPLACED ANGLE WITH NEW MANUFACTURED PART LEFT SIDE. 2 L 7 3 4F A3WE 1999073000334 19990730 00334 NM 1999 7 30 DL72S991647 1 19990714 A 7120 65312814 MOUNT BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 NA ON HUSHKIT MOD, FOUND NR 2 AFT ENG MOUNT CORRODED. REPLACED MOUNT. 2 L 7 3 4F A3WE 1999073000335 19990730 00335 NM 1999 7 30 DL72S991648 1 19990720 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 481-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 545DA 22494 LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 & 681 INIDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN THE PANEL. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367826-14AD, REV A. 2 L 7 3 4F A3WE 1999073000337 19990730 00337 NM 1999 7 30 DL75A991651 1 19990722 A 2560 SLIDE D30654122 BOEING 757 757212 NM DOOR R-1 DEPLOYED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 750AT 0049 23126 R-1 DOOR SLIDE DEPLOYED AT GATE BY PERSONNEL. 2 L 7 2 4F RT A2NM 1999073000338 19990730 00338 NM 1999 7 30 DL757991652 1 19990723 A 3230 257T110314 CONTL MODULE BOEING 757 757232 1384965 NM LANDING GEAR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 602DL 22809 GEAR FAILED TO RETRACT, GEAR HANDLE RAISED TO OFF POSITION AND WOULD NOT MOVE FURTHER. GEAR LIGHT AND GEAR DISAGREE MSG ILLUMINATED. FOLLWED POM PROCEDURE. RETURNED TO JFK. ON LANDING AIRCRAFT PULLED TO RIGHT. FOUND NR 3 BRAKE DRAGING REPLACED SAME. HAD FAULT CODES 421/422/423/424 ON PSEU. REPLACING LANDING GEAR CONTROL MODULE PER FIM PRIOR TO MTC, FE RRY TO ATL. 2 L 7 2 4F RT A2NM 1999073000339 19990730 00339 WP 1999 7 30 DHL9980202C 1 19990502 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 640 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 AT C-CHECK, RT WING TO FUSELAGE FS 640 & XW 0 CRACKED ANGLE. REMOVED CRACKED ANGLE FROM RT WING LWR TO FUSELAGE STA 640 AND XWO PER SRM. FABRICATED NEW ANGLE SAME MATERIAL AND THICKNESS 2023-T3 0.050. CLEANED ANGLE AREA PER SRM. TREATED , PRIMED AREA AND NEW ANGLE IAW, OK TO INSTALL NEW ANGLE. INSTALLED NEW ANGLE PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999073000340 19990730 00340 WP 1999 7 30 DHL9980203C 1 19990501 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 760 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 AT C-CHECK, CENTER TANK AREA UPPER FUSELAGE STA 760 O/B RT OF SET TRACK NR 6 FITTING CRACKED BETWEEN FASTENERS. REMOVED CRACKED FITTING FROM CENTER TANK AREA UPPER FUSELAGE. DRILLED NEW FITTING PER SRM. CLEANED FITTING AREA PER SRM. OK TO TREAT, PRIME AREA & NEW FITTING PER SRM. INSTALLED NEW FITTING PER SRM 51-1-20. 2 L 7 4 4F RT 4A25 1999073000341 19990730 00341 WP 1999 7 30 DHL9980204C 1 19990525 A 7110 FITTING DOUG DC8 DC873F 302199F WP NR 4 ENG COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK NON-ROUTINE ENG NR 4 RT AT 12 O'CLOCK FWD CORE COWL CLOSE TO PRECOOLER SCOOP AREA HAD CRACK DAMAGE ON SURFACE. T HRUST REVERSER RT HALF NR 4 ENG IAW MM. FACILITY S/M WORK REMOVED CRACKED FITTING FROM FWD CORE COWL IAW DC-8 SRM 51-1- 21 PAR 5, 51-3-0 PAR 1 & 2 PG 1 AND 51-1-24 PG 1. CLEANED FITTING AREA PER SRM 51-1-8 PAR 6A. OK TO TREAT, PRIME AREA AND NEW FITTING TREATED, PRIMED AREA, NEW FITTING JA DC-8 SRM 51-1 PG 13.16. OK TO INSTALL NEW FITTING INSTALLED NEW FI TTING PER SRM. PENDING RIGGING OPS CK PERFORMED NR 4 T//R CK AND RIG FOUND OK IAW DC8 MM 78-30-0. 2 L 7 4 4F RT 4A25 1999073000342 19990730 00342 WP 1999 7 30 DHL9980205C 1 19990430 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR 4 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C CHECK, NONROUTE ENG #4 INSIDE CENTER PYLON SECTION GENERATOR FEEDER CABLE SUPPORT HAD CRACK DAMAGE ON SURFACE. REMOVE D GENERATOR FEEDER CABLE SUPPORT AS PER DC8 MM 20-50-1. CUT OUT CRACKED AREAS FROM PANEL AT NR 4 PYLON CENTER AREA IAW DC8 SRM 3-2-0 FIG 23. FABRICATED DOUBLERS REPAIR FROM 2024. CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A. OK TO TREAT AN D PRIME AREA DOUBLER REPAIR TREATED AND PRIMED ARA & DOUBLERS PER SRM. INSTALLED DOUBLERS PER SRM 51-1-8. INSTALLED NR 4 PYLON GEN FEEDER CABLES SUPPORT AS PER DC8 MM 20-50-1. PENDING OPS OK, PERFORMED OPS CK DURING ENG RUN POWER RUN FOU ND NORMAL IAW DC 8 MM 71-00. 2 L 7 4 4F RT 4A25 1999073000343 19990730 00343 WP 1999 7 30 DHL9980206C 1 19990429 A 5540 STIFFENER DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RUDDER L/E INTERTIOR STIFFENER CRACKED, MARKED STA ZR DOT 3211. REMOVED STIFFENER FROM RUDDER L/E INTERIOR AT STA ZR 105 IAW. CLEANED DAMAGED AREA, NO CRACKS FOUND AFTER DYE PENETRANT TEST IAW NDT SPM PART 8. TREATED & PRIMED ST IFFENER. OK TO INSTALL STIFFENER. INSTALLED STIFFENER PER SRM 51-1-21 PAR 1 FIG 32. 2 L 7 4 4F RT 4A25 1999073000344 19990730 00344 WP 1999 7 30 DHL9980207C 1 19990429 A 5540 FITTING DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RUDDER I/E INTERIOR, FITTING CRACKED. MARKED STA ZR 105 DOT 327. STOP DRILLED END CRACK 1/4 PR DC-8 SRM 55-2-0 PAGE 7 FIG 2. FABRICATED ANGLE REPAIR 063 2024T3 7 X 1 1/2 X 1/2 IAW DC-8 SRM 55-2-0. TREATED & PRIMED PER DC8 SRM 51 -1-8 PAGE 16 AND 13 PARAG 6 & 6F. INSTALLED REPAIR PER DC8 SRM 51-1-71 PG 1P1. 2 L 7 4 4F RT 4A25 1999073000345 19990730 00345 WP 1999 7 30 DHL9980208C 1 19990430 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 880-980 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 1 BETWEEN STA 880-980 TRACK WAS CORRODED. CUT OUT DAMAGED SECTION OF TRACK NR 1 AT STA 920 AND C LEANED AREA OF TRACK BETWEEN STA 880-980 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 & 51-1-8 PARA 6A. OK TO TREAT AND PRIME REW ORKED AREA IAW DC-8 SRM 51-1-8 PAGE 13 & 16. INSTALLED (1) FOUR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 53-2-3 FIG 6D SHE ET 1 THRU 3. 2 L 7 4 4F RT 4A25 1999073000346 19990730 00346 WP 1999 7 30 DHL9980209C 1 19990430 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 980-1080 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 1 STA 980-1080 TRACK IS CORRODED. CUT OUT DAMAGED SECTIONS OF TRACK NR 1 STA 1100 IAW DC-8 SRM 5 3-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1- 8 PG 13 & 16. INSTALLED 1 FOUR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. 2 L 7 4 4F RT 4A25 1999073000347 19990730 00347 WP 1999 7 30 DHL9980210C 1 19990429 A 5400 SPAR DOUG DC8 DC873F 302199F WP NR 1 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, PYLON FAIRED AREA INBOARD NR 1 PYLON FWD SPAR CAP HAD TWO INCHES & PROGRESSING PREVIOIUSLY STOP HOLE. DOT 3828 44. REMOVED 2 FASTENERS FOR ACCESS TO NDT AT PYLON NR 1 FWD SPAR CAP IAW DC-8 SRM 51-3-0 FIG 52A. REMOVED NR 1 DC-8 SR M 51-1-20 PAR 8 MM 20-15-0 PAR 4B. FABRICATED NEW ANGLE IAW ATM C1-PG3-ATM005239A & DRAWING NR 58 0419 FROM STEEL SHEET 17-7 PH. DRILLED ATTACHING HOLES TO DRAG ANGLE IAW DC-8 SRM 51-3-2 PG 1. PRIMED DRAG ANGLE PER SRM 51-1-8 PG 16. INS TALLED DRAG ANGLE IAW DC-8 SRM 51-1-20D PAR 7 & 51-30 PAR 1 & 2. INST. ENG. NR 1 IAW DHL J/C 8-202. 2 L 7 4 4F RT 4A25 1999073000348 19990730 00348 WP 1999 7 30 DHL9980211C 1 19990521 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, UPPER CARGO COMPT AT STA 1600 CIRCUMFERENTIAL FRAME AT CUSP LINE WAS CRACKED RT SIDE. CUT OUT CRACKED SECTION OF FRAME AT FS 1580 RT M CARGO CABIN IAW DC-8 SRM 53-2-0 FIG 2. FABRICATED NEW SECTION OF FRAME: 6 X 2.5 AND 2 SPLICES 10 X 2.5 IAW MHA ENGINEERING NR 3126. HEAT TREATED FRAME & SPLICES 7075-0 TO 7075-T6 IAW DC-8 SRM 51-1-1, PG 1 TO 21, CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A. DRILLED NEW SECTION OF FRAME & SPLICES PER SRM 51-3-2, PG 1, 51-1-4, PG 1. T REATED, PRIMED AREA & PARTS IAW DC-8 SRM 51-1-8, PG 13 & 16. OK TO INSTALL FRAME REPAIR IAW DC-8 SRM 51-1-20D, PAR 7. 2 L 7 4 4F RT 4A25 1999073000349 19990730 00349 WP 1999 7 30 DHL9980212C 1 19990429 A 7830 TR COWL DOUG DC8 DC873F 302199F WP NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, NR 1 ENGINE PYLON LT AFT REVERSER COWL UPPER AFT AREA FOUND CRACK ON U-CHANNEL ANGLE. REMOVED CRACKED U-CHANNE L ANGLE AT ENG NR 1 LT AFT REVERSER COWL IAW DC-8 SRM 51-1-21A PG 1 PARA 1. FABRICATED NEW U ANGLE 5.5 X 1.375. 301 STA INLESS .25 HARD 0.20. IAW DC-8 SRM 51-1-7 PG 1 PARA 1. INSTALLED U-CHANNEL ANGLE PER DC-8 SRM 51-1-21 PG 1 PARA 1. 2 L 7 4 4F RT 4A25 1999073000350 19990730 00350 WP 1999 7 30 DHL9980213C 1 19990429 A 5720 BRACKET DOUG DC8 DC873F 302199F WP WS 880 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, BELOW LT WING ABOUT X 46.000 STA 880 BRACKET CRACKED. REMOVED CRACKED BRACKET FROM LT WING AT STA 880 IAW DC- 8 SRM 51-1-20D & 51-1-21 PAR 1. FABRICATED NEW BRACKET SAME MATERIAL & THICKNESS 2024-T3 0.0063 DC-8 SRM 53-8-3 FIG 2. CLEANED BRACKET AREA PER SRM 51-1-8 PAR 6A. TREATED, PRIMED AREA & BRACKET PER SRM 51-1-8 PAR 13,16. INSTALLED BRACKE T PER SRM 51-1-20D, 51-1-21 PAR 1. 2 L 7 4 4F RT 4A25 1999073000351 19990730 00351 WP 1999 7 30 DHL9980214C 1 19990511 A 5230 BRACKET DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, MAIN CARGO COMPARTMENT MAIN CARGO DOOR INTERIOR CENTER AREA DOOR LATCH ACTUATOR UPPER ATTACH BRACKET MOUNT BOLT S LOOSE AND SMALL ANGLE BRACKET WAS CRACKED D20CD1. REMOVED DAMAGED BRACKET AT MAIN CARGO COMPT CARGO DOOR INTERIOR CEN TER ARA DOOR LATCH ACTUATOR IAW DC-8 SRM 51-3-0 PAG 2 FIG 52A. FABRICATED NEW ANGLE 7075-T6 .063 2 X 1 IAW DC-8 SRM 51- 1-4 PG 1 PARA 1. REMOVED AND REPAIRED LOOSE FASTENER PER SRM 51-3-0 PG 2 FIG 3A. TREATED, PRIMED PER DC8-SRM 51-1-8 PG 18, PAR 6F. INSTALLED PER DC-8 SRM 51-3-0 PAR 2 FIG 52A. 2 L 7 4 4F RT 4A25 1999073000352 19990730 00352 WP 1999 7 30 DHL9980215C 1 19990507 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP AFT PRESS BLKHD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, AFT PRESSURE BULKHEAD, REAR FACE, CENTER SECTION, ATTACHING ANGLE WAS CRACKED AT BEND RADIUS. BEHIND PULLEY BR ACKET ASSY. CLEANED CRACKED AREA AT ANGLE ON PRESSURE BULKHEAD REAR FACE, CENTER SECTION PER SRM 51-1-8, PARA 6A. STOP DRILLED CRACK, DYE PENETRANT TEST TO ASSURE CRACK WAS REMOVED IAW NDT SRM PART 8. FABRICATED ANGLE FROM EXTRUSTION PAR T NR 60-358-1 IAW MHA ENGINEERING NR F99-013. TREATED, PRIMED AREA & REPAIR PART IAW DC-8 SRM 51-1-8 PG 13 & 16. INSTA LLED ANGLE REPAIR IAW MHA ENGINEERING NR F-99-013 & SRM 51-1-20D, PARA 7. 2 L 7 4 4F RT 4A25 1999073000353 19990730 00353 WP 1999 7 30 DHL9980216C 1 19990508 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 151-171 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 4 BETWEEN STA 151-171 2 PLUG REPAIRS NOT PER SRM. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BET WEEN STA 130 TO 170 & PREPAIRED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK AND FABRICATED SPLICES FROM 7075 -T6 IAW DC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED, PRIMED REWORKED AREA A ND PARTS IAW DC-8 SRM 51-1-8 PG 13, 16. INSTALLED NEW SECTION PER SRM 53-2-3 FIG (SHEET 1). 2 L 7 4 4F RT 4A25 1999073000354 19990730 00354 WP 1999 7 30 DHL9980217C 1 19990504 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, AT STA IS 1220, LONGERON, 26L IS CRACKED AT CARGO PIT NR 3 LT SIDE. FABRICATED DOUBLER REPAIR 2024 T3 032 14 X 4 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED AND PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 6F. INSTALLED REPAIR PER DC -8 SRM 51-1-21 PG 1 . 2 L 7 4 4F RT 4A25 1999073000355 19990730 00355 WP 1999 7 30 DHL9980218C 1 19990504 A 5320 SCUFF PLATE DOUG DC8 DC873F 302199F WP CARGO COMPT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, FWD PIT (C-1) CARGO SCUFF HAD A CRACK, 13 FASTENERS DAMAGED AND SPARK BURN AT LOWER LT AREA. DOT 3822. STOP D RILLED CRACK AND REMOVED DAMAGED FASTENERS AT FWD PIT (C1) CARGO SCUFF AT LOWER LT AREA IAW DC-8 SRM 51-1-21 PG 1. TREA TED, PRIMED DOUBLER AND REWORKING AREA AS PER SRM 51-1-8 PG 16 & 13 PAR 6 AND 6F. INSTALLED REPAIRED DOUBLER AS PER SRM 51-1-21 PG 1. 2 L 7 4 4F RT 4A25 1999073000356 19990730 00356 WP 1999 7 30 DHL9980219C 1 19990503 A 5720 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT WING, L/B HINGE, 2 INCH CRACK UNDER FLAP FITTING ATTCH POINT WING STA: XW 5.000. STOP DRILLED END CRACK .25 AT LT WING L/B FLAP L/B HINGE UNDER FLAP FITTING ATTACH POINT IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED ANGLE REPAIR 2024-T3 050. 6 X 3 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED AND PRIMED PER DC-8 SRM 51-1-8 PAG 16,13 PAR 6 & 6F. INSTAL LED REPAIR PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000357 19990730 00357 WP 1999 7 30 DHL9980220C 1 19990504 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 7000 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, MCC LT CUSP LINE AREA AT STA 700.000 LOWER FITTING IS CRACKED. D 20C01. REMOVED CRACKED FITTING FROM MCC LT C USP LINE AREA AT STA 700.000 IAW DC-8 SRM 51-1-20D PAR 8, 51-3-0 PAR 1 & 2. FABRICATED NEW FITTING FROM ALUMINUM PLATE 7075-T6 IAW MHA ENGINEERING INC NR 3135. CLEANED FITTING AREA PER SRM 51-1-8 PAR 6A. TREATED, PRIMED AREA AND NEW FITT ING PER SRM 51-1-8 PG 13 & 16. INSTALLED NEW FITTING PER SRM 51-1-20D, PAR 7, 51-3-0 PAR 1 & 2. 2 L 7 4 4F RT 4A25 1999073000358 19990730 00358 WP 1999 7 30 DHL9980221C 1 19990503 A 5311 CIRCUMFERENTIAL DOUG DC8 DC873F 302199F WP BS 1380 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, AFT LOWER CARGO COMPT CIRCUMFERENTIAL AT FS 1380 BTW LONG 34R IS CRACKED. REF 34403. STOP DRILLED END CRACK A REA AT AFT CARGO COMPT CIRCUMFERENTIAL STA 1380 BETWEEN LONG 34R TO 33R IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. FABRICATED AN GLE REPAIR 301 STAINLESS .25 HARD. 032 5X2 IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. INSTALLED ANGLE REPAIR PER DC-8 SRM 51-1-2 1 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000359 19990730 00359 WP 1999 7 30 DHL9980223C 1 19990503 A 5311 CIRCUMFERENTIAL DOUG DC8 DC873F 302199F WP BS 1420 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, AFT LOWER CARGO COMPT CIRCUMFERENTIAL AT FS 1420 BTW LONG 36 & 33R IS CRACKED. REF 344015. STOP DRILLED END C RACK AREA AT AFT CC FS 1420 BETWEEN LONG 36 & 33R IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. INSTALLED ANGLE REPAIR PER DC-8 SRM 51-1-21 PG 1 PAR A6 1. 2 L 7 4 4F RT 4A25 1999073000360 19990730 00360 WP 1999 7 30 DHL9980224C 1 19990503 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING AT NR 1 HINGE AREA XW 5 & 980 APPROX CRACKED ANGLE DOT 641-59. REMOVED DAMAGED ANGLE AT RT WING NR 1 H INGE AREA XW 5 FS 940 PER DC-8 SRM 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE PER DC-8 SRM 53-8-3 PG 5/6 FIG 1 2024-T3 05 0 14 X 3. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED NEW ANGLE PER DC-8 SRM 51-1-21 PG 1 PA R 1. 2 L 7 4 4F RT 4A25 1999073000361 19990730 00361 WP 1999 7 30 DHL9980225C 1 19990503 A 5311 CIRCUMFERNTIAL DOUG DC8 DC873F 302199F WP BS 1380 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, AFT LOWER CARGO COMPT CIRCUMFERENTIAL AT FS 1380 BTW LONG 33R IS CRACKED. REF 344013. STOP DRILLED END CRACK AREA AT AFT CARGO COMPT CIRCUMFERENTIAL STA 1380 BTWN LONG 34R IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. FABRICATED ANGLE REPAI R 301 STAINLESS .25 HARD .032 5 X 2 IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. INSTALLED ANGLE REPAIR PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000362 19990730 00362 WP 1999 7 30 DHL9980226C 1 19990503 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT WING, I/B FLAP, I/B HINGE, 2 INCH CRACK UNDER FLAP FITTING ATTACH POINT WING STA XW 5.000. STOP DRILLED END CRACK .25 AT LT WING I/B FLAP I/B HINGE UNDER FLAP FITTING ATTACH POINT IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED ANG LE REPAIR 2024-T3 050. 6X3 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16,13 PAR 6 & 6F. I NSTALLED REPAIR PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000363 19990730 00363 WP 1999 7 30 DHL9980227C 1 19990502 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 255 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT WING CENTER I/E I/B AREA AT STA 255.00 LOWER RIB IS CRACKED. DOT 38138. STOP DRILLED END CRACK AT LT WING CENTER SECTION 4E STA 255.000 LOWR RIB IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 8 X 4 063 7075T6 IAW DC- 8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED REPAIR ANGLE PER SRM 5 1-1-21 PG 1. 2 L 7 4 4F RT 4A25 1999073000364 19990730 00364 WP 1999 7 30 DHL9980228C 1 19990503 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 420 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, FWD LOWER CARGO COMPARTMENT LONG 31R STA 420 CIRCUMFERENTIAL HAS ATTACHED ANGLE WITH CRACK ON SURFACE. DOT 139 19. CLEANED CRACKED AREA AT ANGLE AT FWD LOWER CARGO IS 420 LONG 31R IAW DC-8 SRM 53-2-0 FIG 13 (SHEET 3). TREATED & P RIMED REWORKED AREA IAW SRM 51-1-8 PG 13, 16. INSTALLED ANGLE REPAIR PER SRM 51-1-21 PAR 1 FIG 32. 2 L 7 4 4F RT 4A25 1999073000365 19990730 00365 WP 1999 7 30 DHL9980229C 1 19990503 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING AT NR 1 HINGE AREA XW 5 & FS 980 APPROX CRACKED ANGLE. DOT 641.59. REMOVED DAMAGED ANGLE AT RT WING N R 1 HINGE AREA XW 5 FS 940 IAW DC-8 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE PER DC-8 SRM 53-8-3 PG 5/6 FIG 1 2024-T3 0 50 14X3. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED NEW ANGLE PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000366 19990730 00366 WP 1999 7 30 DHL9980230C 1 19990502 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 640 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING LOWER TO FUSELAGE FS 640 & XW 0 CRACKED ANGLE. DOT 64157. REMOVED CRACKED ANGLE FROM RT WING LWR TO F USELAGE STA 640 & XWO PER SRM 51-1-21 PAR 1. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (14 X 1.15 X 1) IAW DC-8 SRM 53-8-3 FIG 1. CLEANED ANGLE AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA, NEW ANGLE IAW DC-8 SRM 51-1-8 PG 13, 16. INSTALLED NEW ANGLE PER SRM 51-1-21 PAR 1 FIG 32. 2 L 7 4 4F RT 4A25 1999073000367 19990730 00367 WP 1999 7 30 DHL9980231C 1 19990501 A 5720 BRACKET DOUG DC8 DC873F 302199F WP WS 693 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT WING STA SRS 693 THRU PLATE DOOR NR 518B BRACKET CRACKED. DOT 381. STOP DRILLED END CRACK AT LT WING I/E R IB STA WRS 693 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3.050 3 X 1 X 4 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 13 & 16 PAR 6 & 6F. INSTALLED PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000368 19990730 00368 WP 1999 7 30 DHL9980232C 1 19990501 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 780 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, UPPER CARGO COMPT CENTER TANK AREA STA 780 FITTING ON FLOORBEAM REFERENCE SEAT TRACK NR 4 & NR 5 IS CRACKED FIT TING NEED MIRROR & FLASHLIGHT. REMOVED CRACKED FITTING AT MCC TANK AREA STA 780 FLOORBEAM IAW DC-8 SRM 51-1-21D PG 1 PA R 1. DRILLED NEW FITTING PER DC-8 SRM 51-3-2 PG 1 PAR 1. INSTALLED FITTING PER DC-8 SRM 51-1-21D PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000369 19990730 00369 WP 1999 7 30 DHL9980233C 1 19990501 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 760 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, CENTER TANK AREA UPPER FUELAGE STA 760 O/B RT OF SEAT TRACK NR 6 FITTING CRACKED BETWEEN FASTENERS. REMOVED CR ACKED FITTING FROM CENTER TANK AREA UPPER FUSELAGE STA 760 IAW DC-8 SRM 51-1-20D, PAR 8, 51-1-21, PAR 1, FIG 32. DRILLE D NEW FITTING PER SRM 51-3-2, PG 1, SRM 51-1-24, PG 1. CLEANED FITTING AREA PER SRM 51-1-8, PAR 6A. TREATED & PRIMED A REA & NEW FITTING PER SRM 51-1-8, PG 13 & 16. INSTALLED NEW FITTING PER SRM 51-1-20D, PAR 8 & 51-1-21, PAR 1. 2 L 7 4 4F RT 4A25 1999073000370 19990730 00370 WP 1999 7 30 DHL9980234C 1 19990430 A 5753 FITTING DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT STA 97 FLAP HINGE SUPPORT FITTING HAS TWO CRACK INDICATION, ONE IN LT SIDE NR 2 HOLE & ONE IN RT SIDE NR 1 H OLE MARKED. ENLARGED CRACKED HOLES TO THE LIMITATIONS CONTAINED ON SR DRAWING 5894377 & CRACK WAS NOT REMOVED. REMOVED O/B FITTING STA 97 OF LT WING I/B FLAP IAW STEPS 9-13 OF FIG 3 OF SB 27-249 & SRM 51-1-21 PAR 1 & 2. FABRICATED DRILL TEMPLATE & DUPLICATED HOLES PATTERN FROM OLD FITTING TO NEW FITTING IAW STEPS 14-16 OF FIG 3 OF SB 27-249 & SRM 51-3-2 P G 1, 51-1-24 PG 1. INSTALLED NEW FITTING. 2 L 7 4 4F RT 4A25 1999073000371 19990730 00371 WP 1999 7 30 DHL9980235C 1 19990430 A 5711 SPAR DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING AT REAR SPAR AREA XW 5 WEB PANEL IS CRACK 3 LONG DOT 64101. STOP DRILLED END CRACK AT RT WING, REAR SP AR ARA XW5 WEB PANEL IAW DC-8 SRM 51-3-2. FABRICATED DOUBLER REPAIR AS PER SRM 57-2-0 PAR 2 E 6 X 6 .090-2024T3. TREAT ED & PRIMED AS PER SR 51-1-8 PG 13 & 16 PAR 6 & 6F. INSTALLED FABRICATED DOUBLER AS PER SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000372 19990730 00372 WP 1999 7 30 DHL9980236C 1 19990430 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 329 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 1 BETWEEN STA 329 TO 380 TRACK HAS CORROSION. CUT OUT DAMAGED SECTION OF TRACK NR 1 AT STA 329 & CLEANED AREA OF SEAT TRACK BETWEEN STA 329 TO 380 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 & 51-1-8 PAR 6A. FOUR HOLES CARGO TRACK REPAIR INSTALLED IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3. 2 L 7 4 4F RT 4A25 1999073000373 19990730 00373 WP 1999 7 30 DHL9980237C 1 19990430 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 480-580 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 1 BETWEEN STA 480-580 TRACK HAS CORRODED SPOTS. CUT OUT DAMAGED SECTIONS OF TRACK NR 1 STA 520 I AW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6. TREATED & PRIMED REWORKED AREA IAW DC -8 SRM 51-1-8 PG 13 & 16. FOUR HOLES CARGO TRACK INSTALLED IAW DC-8 53-2-3 FIG 6D SHEET 1-3. 2 L 7 4 4F RT 4A25 1999073000374 19990730 00374 WP 1999 7 30 DHL9980238C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1280-1380 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 1 BETWEEN STA 1280-1380 TRACK CORRODED. CUT OUT DAMAGED SECTION OF TRACK NR 1 BETWEEN STA 1350 T O 1370 & PREPARED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 X 1 3), 0.125 (1 X 7), 0.160 (1 X 8) IAW DC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORK AREA PER SRM 51-1-8 PAR 6A. TREA TED & PRIMED REWORKED PARTS IAW DC-8 SRM 51-1-8 PG 13, 16. INSTALLED NEW SECTION OF TRACK PER SRM 53-2-3 FIG 14 (SHEET 1). 2 L 7 4 4F RT 4A25 1999073000375 19990730 00375 WP 1999 7 30 DHL9980240C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 415-420 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 6 BTWN STA 415 - 420 TRACK HOLES WORN. REMOVED (2) DAMAGED, FOUR HOLES CARGO TRACK REPAIR FROM N R 6 SEAT TRACK STA 415-420 IAW DC-8 SRM 51-3-0 PAR 1 & 2. CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA IAW DC-8 SRM 51-1-8 PG 13 & 16. INSTALLED NEW FOUR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 51-3-0 PAR 1 & 2. 2 L 7 4 4F RT 4A25 1999073000376 19990730 00376 WP 1999 7 30 DHL9980241C 1 19990429 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, UPPER CARGO COMPT AT STA 1600 CIRCUMFERENTIAL FRAME AT CUSP LINE IS CRACKED RT SIDE. CUT OUT CRACKED SECTION O F FRAME AT FS 1580 RT CARGO CABIN IAW DC-8 SRM 53-2-0 FIG 2. FABRICATED NEW SECTION OF FRAME: 7075-0 0.080' (6 X 2.5) & SPLICE FROM 7075.0 0.080 (10 X 2.5) IAW MHA ENGINEERING NR 3126. HEAT TREATED FRAME & SPLICES 7075-0 TO 7075-T6 IAW DC -8 SRM 51-1-1, PG 1 TO 21. CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A. DRILLED NEW SECTION OF FRAME & SPLICES PER SRM 5 1-3-2 PG 1, 51-1-24, PG 1. TREATED & PRIMED AREA & PARTS IAW DC-8 SRM 51-1-8 PG 13 & 16. INSTALLED FRAME REAPIR IAW DC -8 SRM 51-1-20D, PAR 7. 2 L 7 4 4F RT 4A25 1999073000377 19990730 00377 WP 1999 7 30 DHL9980242C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1560-1600 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, BETWEEN STA 1560-1600 SEAT TRACK NR 5 IS WORN. CUT OUT DAMAGES SECTION OF NR 5 SEAT TRACK AT STA 1563 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC- 8 SRM 51-1-8 PG 13, 16. INSTALLED (1) FOUR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3. 2 L 7 4 4F RT 4A25 1999073000378 19990730 00378 WP 1999 7 30 DHL9980243C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 220-260 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, NONROUTINE SEAT TRACK NR 6 BTWN STA 220-260 TRACK HOLES WORN & SOME ELONGATED. CUT OUT DAMAGED SECTION OF TRAC K NR 6 BETWEEN STA 170 TO 310 & PREPARED NEW SECTION FROM APPROPRIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FRO M 7075-T6 0.100 (1 X 3), 0.125 (1 X 7), 0.160 (1 X 8) IAW DC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORKED AREA PER S RM 51-1-8 PAR 1. TREATED & PRIMED REWORKED AREA & PARTS IAW DC-8 SRM 51-1-8 PG 13, 16. INSTALLED NEW SECTION PER SRM 5 3-2-3 FIG 14 (SHEET 1). 2 L 7 4 4F RT 4A25 1999073000379 19990730 00379 WP 1999 7 30 DHL9980244C 1 19990429 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, NR 1 ENGINE NOSE COWL L/E INTERIOR AT 10 O'CLOCK POSITION INTERNAL LIP FLANGE IS CRACKED D20EN4. ACCOMPLISHED ENG NR 1 NOSE COWL ANTI-ICE DEFLECTOR REPAIR BY TRIMMING CRACKED SECTION IAW SB 71-105 FIG 2. TREATED AREA OF TRIMMED D EFECTOR PER DC-8 SRM 51-1-8 PG 16 6F. APPLIED SEALANT PER SB 71-105 FIG 2. 2 L 7 4 4F RT 4A25 1999073000380 19990730 00380 WP 1999 7 30 DHL9980245C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 200-299 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 7 BETWEEN STA 299.200 CORROSION SPUTS ON TRACK. CUT OUT DAMAGED SECTION OF TRACK NR 7 AT STA 273 & CLEANED AREA OF TRACK BETWEEN STA 299-200 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3, 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREAS IAW DC-8 SRM 51-1-8 PG 13, 16. INSTALLED (1) FOUR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 53-2-3 FIG 6D S HEET 1 THRU 3. 2 L 7 4 4F RT 4A25 1999073000381 19990730 00381 WP 1999 7 30 DHL9980246C 1 19990429 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 6 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, ABOUT XTS 6.000 BELOW LT WING IS A CRACK SEE MARK DOT 38262. REMOVED CRACKED ANGLE FROM WING ABOUT STA XRS 6. 000 IAW DC-8 SRM 51-1-21 PAR 1 FIG 32. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (20 X 11) IAW DC-8 SRM 57-3-1 FIG 25. CLEANED ANGLE AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA & ANGLE PER SRM 51-1-8 PG 13, 16. I NSTALLED NEW ANGLE PER SRM 51-1-21 PAR 1 FIG 32. 2 L 7 4 4F RT 4A25 1999073000382 19990730 00382 WP 1999 7 30 DHL9980248C 1 19990429 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 46 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, ABOUT XCW 46.00 BELOW LT WING IS CRACKED DOT 382627. REMOVED DAMAGED ANGLE AT LT WING XW 46.00 IAW DC-8 SRM 51 -1-21 PG 1 PAR 1. FABRICATED NEW ANGLE .071 2024T3 12 X 6 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED & PRIMED PER DC-8. 2 L 7 4 4F RT 4A25 1999073000383 19990730 00383 WP 1999 7 30 DHL9980249C 1 19990429 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 162 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT WING ABOUT STA 162.263 T/E PANEL BEHIND REAR SPAR HAS A CRACK DOT 382618. STOP DRILLED END CRACK .25 DIAMET ER IAW DER NR MHA-312A. FABRICATED DOUBLER REPAIR 7.5 X 9.5 2024T3 .050IAW DER NR MHA 3124. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13, PAR 6 & 6F. INSTALLED REPAIR PER DER NR MHA 3124. 2 L 7 4 4F RT 4A25 1999073000384 19990730 00384 WP 1999 7 30 DHL9980250C 1 19990429 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT WING I/B AREA PANEL BELOW NR 2 SPOILER IS DELAMINATED. REMOVED DELAMINATED PANEL AT LT WING 8/B AREA LOWER SURFACE BELOW SPOILER NR 2 IAW DC-8 SRM 51-1-21 PG F1 P1. SEND DELAMINATED PANEL OUT TO BE REPAIR DRILLED SERVICEABLE P ANEL PER DC-8 SRM 51-3-2 PG 1 PAR 1. INSTALLED PANEL PER DC-8 SRM 51-3-0 PG 2 FIG 52A. 2 L 7 4 4F RT 4A25 1999073000385 19990730 00385 WP 1999 7 30 DHL9980251C 1 19990521 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP VANE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, FLAP VANE NR 3 DELAMINATED LEFT WING DOT 38255. REMOVED I/W NR 3 VANE IAW DC-8 27-51-14 ROUTE TO STORES TO BE SENT OUT FOR REPAIR. INSTALLED I/H NR 3 FLAP VANE IAW DC-8 MM 27-51-14 PG 201. PENDING RIG & OPS CHK ACCOMP. RIG & OP S CHK NORMAL IAW DC-8 MM 27-50-0. 2 L 7 4 4F RT 4A25 1999073000386 19990730 00386 WP 1999 7 30 DHL9980252C 1 19990430 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1560-1610 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 2 BETWEEN STA 1560-1610 TRACK WORN/CHIPPED. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 2 BETWEEN S TA 1560 TO 1650 & PREPARED NEW SECTION FROM: APPROPPIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM:7075-T6 0.1 00 (1 X 13) 0.125 (1 X 7) 0.160 (1 X 8) IAW DC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORKED AREA PR SRM 51-1-8 PAR 6 A. TREATED & PRIMED REWORKED AREA & PARTS IAW DC-8 SMM 51-1-8 PG 13, 16. INSTALLED NEW SECTION PER SRM 53-2-3 FIG 14 ( SHEET 1). 2 L 7 4 4F RT 4A25 1999073000387 19990730 00387 WP 1999 7 30 DHL9980253C 1 19990429 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, LT WING NR 1 FLAP VANE HAS DELAMINATED AREA DOT 53901. REMOVED NR 1 FLAP VANE FROM I/H WING IAW DC-8 MM 27-51- 14. SENT TO STOCKROOM. INSTALLED NR 1 FLAP VANE I/H WING IAW DC-8 M/M 27-51-14 PG 201, 203 PAR 2B. PENDING OPS CHK PE RFORMED, OPS CHK NORMAL IAW DC-8 MM 27-50-0. 2 L 7 4 4F RT 4A25 1999073000388 19990730 00388 WP 1999 7 30 DHL9980254C 1 19990430 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL S/B CRACKED RIBS AT UPPER END XFS 728 & XFS 747 DOT 64129-64130. STOP DR ILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 728 &747 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024T3 050 .75 X 1.25 X 5 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTA LLED PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000389 19990730 00389 WP 1999 7 30 DHL9980255C 1 19990430 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING O/B L/E INTO THRU ACCESS PANEL 519C CRACKED RIBS TO UPPER END XFS 622 AND XFS 644 DOT 64131-64132. STO P DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 641 & 622 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2 024 T3 050 .75 X 1.25 X 5 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000390 19990730 00390 WP 1999 7 30 DHL9980256C 1 19990430 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING OUTB L/E INT THRU ACCESS PANEL 518B CRACKED RIBS AT UPPER END XFS 766.25 & XFS 760 DOT 64127-64128. ST OPPED DRILLED END CRACK AT RT WING O/B L/E RIB STA XFS 766.250 & 760 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 13 & 16 PAR 6 & 6F. INSTALLED PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000391 19990730 00391 WP 1999 7 30 DHL9980257C 1 19990430 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 240-260 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 2 BETWEEN STA 240-260 PLUG NO GOOD. REMOVED (1) DAMAGED (4) FOUR HOLES CARGO TRACK REPAIR FROM N R 2 SEAT TRACK STA 240-260 IAW DC-8 SRM 51-3-0 PAR 1 & 2 FIG. CLEANED REPAIRED AREA PER SRM 51-1-8 PAR 6A. TREATED & P RIMED AREA IAW DC-8 SRM 51-1-8 PG 13 & 16. INSTALLED NEW (4) FOUR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 51-3-0 PAR 1 & 2. 2 L 7 4 4F RT 4A25 1999073000392 19990730 00392 WP 1999 7 30 DHL9980258C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 300-340 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 4 BETWEEN STA 300-340 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BETWEEN STA 310-370 & PREPARED NEW SECTION FROM APPROPIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 X 13), 0.1 25 (1 X 7) 0.160 (1 X 8) IAW DC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORKED AREA IAW DC-8 SRM 51-1-8 PAR 6. TREATE D REWORKED AREA & PARTS & PRIMED IAW DC-8 SRM 51-1-8 PG 13, 16. INSTALLED NEW SECTION PER SRM 53-2-3 FIG 14 (SHEET 1). 2 L 7 4 4F RT 4A25 1999073000393 19990730 00393 WP 1999 7 30 DHL9980259C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 220-290 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 4 BETWEEN STA 270-290 TRACK WORN. CUT OUT DAMAGED SECTIONS OF TRACK NR 4 STA 280-290 IAW DC-8 SR M 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51 -1-8 PG 13 & 16. INSTALLED (2) FOUR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. 2 L 7 4 4F RT 4A25 1999073000394 19990730 00394 WP 1999 7 30 DHL9980260C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 2210-260 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 4 BETWEEN STA 221-260 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BETWEEN STA 210-250 & PREPARED NEW SECTION FROM APROPRIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 1000 (1 X 13) 0.125 (1 X 7) 0.160 (1 X 8) IAW EC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRI MED REWORKED AREA & PARTS IAW DC-8 SRM 51-1-8 PG 13 &16. INSTALLED NEW SECTION PER SRM 53-2-3 FIG 14 (SHEET 1). 2 L 7 4 4F RT 4A25 1999073000395 19990730 00395 WP 1999 7 30 DHL9980261C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1300-1320 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 4 BETWEEN STA 1300-1320 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NUMBER 4 BETWEEN STA 1 290-1350 & PREPARED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM: 7075-T6 0.100 (1 X 7) 0.160 (1 X 8) IAW DC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA AND PARTS IAW DC-8 51-1-8 PG 13 & 16. INSTALLED NEW SECTION PER SRM 53-2-3 FIG 14 (SHEET). 2 L 7 4 4F RT 4A25 1999073000396 19990730 00396 WP 1999 7 30 DHL9980262C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 320-340 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 3 BETWEEN STA 320-340 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 3 BETWEEN STA 310 TO 370 & PREPARED NEW SECTION FROM APPROPIATED MATCHING SECTION OF TRACK & FABRICATED SPLICE FROM 7075-T6 0.100 (1 X 13) 0. 125 (1 X 7) 0.160 (1 X 8) IAW DC-8 SRM 53-2-3 FIG 14 (SHEET 1). CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA & PARTS IAW DC-8 SRM 51-1-8 PG 13, 6. INSTALLED NEW SECTION PER SRM 53-2-3 FIG 14 (SHEET 1). 2 L 7 4 4F RT 4A25 1999073000397 19990730 00397 WP 1999 7 30 DHL9980263C 1 19990429 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 400-440 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, SEAT TRACK NR 3 BETWEEN STA 400-440 TRACK WORN. REMOVED (2) DAMAGED, FOUR HOLES CARGO TRACK REPAIR FROM NR 3 S EAT TRACK STA 400-440 IAW DC-8 SRM 51-3-0 PAR 1 & 2. CLEANED REPAIRED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED ARE A IAW DC8 SRM 51-1-8 PG 13, 16. INSTALLED (2) NEW FOR HOLES CARGO TRACK REPAIR IAW DC-8 SRM 51-3-0 PAR 1 & 2. 2 L 7 4 4F RT 4A25 1999073000398 19990730 00398 WP 1999 7 30 DHL9980264C 1 19990430 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING O/B L/E INT THRU ACCES PANEL 518B CRACKED RIBS AT THE UPPER END XFS 772; XFS 779 & XFS 785 DOT 64124-64 125-64126. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 772, XFS 779 & XFS 785 IAW DC-8 SRM 51-3-2 PG 1 PAR 1 & SRM 57-2-0 PG 9/10 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.25 X 6 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. TREATE D & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED ANGLE REPAIR PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000399 19990730 00399 WP 1999 7 30 DHL9980265C 1 19990430 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 797 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 518A RIB CRACK AT UPPER END XFS 797 DOT 64123. STOP DRILLED END CRACK AT RT WING O/B L/E RIB STA XFS 797.000 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 .050 .75 X 1.25 X 5 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 13 & 16 PAR 6 & 6F. INSTALLED PER DC-8 SRM 51-1-21 PG PAR 1. 2 L 7 4 4F RT 4A25 1999073000400 19990730 00400 WP 1999 7 30 DHL9980266C 1 19990430 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 518A RIBS CRACKED AT UPPER END 3 XFS 822; XFS 815 & XFS 809 DOT 64120-641 22-64121. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 822 XFS 815 XFS 809 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. S TOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 822 XFS 815 XFS 809 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED AN GLE REPAIR 204 T3 050 .75 X 1.25 X 6 (3 EA) IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED REPAIR PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000401 19990730 00401 WP 1999 7 30 DHL9980267C 1 19990430 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 828 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 517B RIB CRACK AT UPPER END XFS 828 DOT 64119. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 828 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.25 X 4 IA W DC8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED PER DC8 - SRM 51-1 -21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000402 19990730 00402 WP 1999 7 30 DHL9980268C 1 19990430 A 5730 RIB DOUG DC8 DC873F 302199F WP WS 848 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING O/B L/E INT THRU ACCES PANEL 517B RIB CRACK AT UPPER END XFS 848 DOT 64118. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 848 & IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.25 X 5 I AW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED AND PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 & 6F. INSTALLED PER DC8 SRM 51 -1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999073000403 19990730 00403 WP 1999 7 30 DHL9980269C 1 19990430 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 240 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING T/E LOWER PANEL HAS CRACK STA XRS 240 IS ABOUT 4 LONG DOT 64109. CUT OUT CRACKED AREA AT RT WING T/E L WR PANEL ST XRS 240 IAW DC-8 SRM 51-1-9A PG 1 THRU 69, FABRICATED FILLER FROM 2024-T3 0.020 (3 X 6) & DOUBLER REPAIR FRO M 2024-T3 0.020 (7 X 8) IAW DC-8 SRM 51-1-9A PG 1 THRU 69. CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A. TREATED, PRIMED AREA AND PARTS PER SRM 51-1-8 PG 13 & 16. INSTALLED DOUBLER REPAIR PER SRM 51-1-9A PG 1 THRU 9. 2 L 7 4 4F RT 4A25 1999073000404 19990730 00404 1999 7 30 DHL99720004 4 19990720 A 3421 199111C VERT GYRO BOEING 727 727228 NM NR 1 FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 720DH 19544 CAPTS ADI ATTITUDE FLAG CAME INTO VIEW DURING A TURN. REPLACED NR 1, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999073000405 19990730 00405 NM 1999 7 30 DHL99727005 1 19990720 A 2750 MECHANISM BOEING 727 727228 NM RT TE FLAP OUT OF ADJUST A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 727DH 20204 ON CLIMBOUT AT 28,000 FT 320 KTS VIBRATION ONSET, SLOWED TO 295 VIBRATION STOPPED. DID NOT VIBRATE IN CRUISE. INSPECTE D IAW MM 05-51-181. FOUND RT I/B TRAILING EDGE FLAP ECCENTRICS HAVE EXCESSIVE CLEARENCE. ADJUSTED PER MM 27-51-1. 2 L 7 3 4F A3WE 1999073000406 19990730 00406 NM 1999 7 30 DHL99740002 1 19990722 A 3240 AV24E1144 VALVE BOEING 727 7272Q9 138448M NM PARKING BRAKE FAILED A DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 740DH 21930 AFTER DEPARTURE OUT OF PHX, WHEN PLACING GEAR LEVER FROM UP TO OFF, RED PARKING BRAKE ILLUMINATED. SHORTLY THEREAFTER BOTH ANTI SKIN INOP LIGHTS ILLUMINTED. ABOUT 3 MIN LATER FAIL WARNING PARKING BRAKE C/B POPPED. RESET AND POPPED AGAIN . REMOVED AND REPLACED PARKING BRAKE SHUT OFF VALVE. 2 L 7 3 4F RT A3WE 1999073000423 19990730 00423 CE 1999 7 30 99ZZZX2798 1 19990705 A 3320 PWFLL28 POWER SUPPLY BEECH 90 E90 1152914 CE CABIN FAILED A A CUXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 17 662JS LW176 TUL - AIRCRAFT DEPARTED AND HAD JUST LEVELED OUT OF 14,500 FEET WHEN SMOKE WAS DISCOVERED IN THE CABIN. SMOKE WAS COMIN G FROM THE RIGHT WINDOW FRAME NEAR SEAT NR 6. THE PILOT RETURNED TO TVL. WELL BEFORE LANDING, THE SMOKE HAD QUIT AND C LEARED OUT OF THE CABIN. INVESTIGATION OF AIRCRAFT AT TVL BY SKY TREK AVIATION TECHNICIANS DETERMINED THE POWER SUPPLY FOR THE FLUORESCENT LAMP HAD FAILED. THIS CAUSED THE LAMP RESISTOR TO BE VERY HOT AND THE INSULATION SURROUNDING THE RE SISTOR HAD MELTED. NO OTHER DISCREPANCIES WERE NOTED AT THIS TIME. 1 L 7 2 3T 3A20 1999073000435 19990730 00435 WP 1999 7 30 AT9900499 1 19990723 A 2913 AS664115666 PUMP DOUG DC9 DC932 3022066 WP NR 2 ENGINE FAILED A ZZDA O OTHER J WARNING INDICATION CR CRUISE 1 SO 15 835AT 47534 LOSS RIGHT ENGINE HYDRAULIC PUMP INFLT FOLLOWED BY LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY. REMOVED AND REPLACED NR 2 E NGINE DRIVEN HYDRAULIC PUMP PER M/M 29-10-5. RESERVICED RIGHT HYDRAULIC RESERVOIR AND INSTALLED TEMPORARY FLEX LINE ABO VE RIGHT THRUST REVERSER CONTROL VALVE. LEAK CHECKED AND OPS CHECK C/W. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1999073000436 19990730 00436 WP 1999 7 30 AT9900501 1 19990610 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 446 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND TWO CRACKS UNDERSIDE FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 446 AND L28-29L. STOP DRILLED CRACKS, NDT VERIFIED. WELD REPAIR CRACKS AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51- 30-2, AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999073000437 19990730 00437 WP 1999 7 30 AT9900502 1 19990610 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 465 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND THREE CRACKS IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 465 AND L29-30R. REMOVED FLOOR SUPPORT. STOP DRILLED 3 EACH CRACKS IAW EA NR 12-5321-29-C1362 REV IR DATED 1-5-98, OP TION 1, STEP 1. NDT CONFIRMED CRACKS CONTAINED. WELD REPAIRED 3 EACH CRACKS. INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-3 0-2, AND 51-10-3. 2 L 7 2 4F A6WE 1999073000438 19990730 00438 WP 1999 7 30 AT9900503 1 19990623 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 503 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACKED FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AND BL 3L. STOP DRILLED CRACK IAW EA NR 12-5321-29-C1362 OPT 1 STEP 1. NDT PERFORMED, CRACK CONTAINED. WELD REPAIR 1 EAC H CRACK ON FLOOR SUPPORT, TREATED, AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1999073000439 19990730 00439 WP 1999 7 30 AT9900504 1 19990610 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 503 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AN D BL 13R. REMOVED SUPPORT, STOP DRILLED NDT VERIFIED CRACK TERMINATED. WELD REPAIRED 1 EACH CRACK IAW EA NR 12-5321-29 -C1362 OPT 2 STEP 4. TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999073000440 19990730 00440 WP 1999 7 30 AT9900505 1 19990610 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 503 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AN D BL 6R. STOP DRILLED, NDT VERIFED CRACK TERMINATED. WELD REPAIRED 2 EACH CRACK. TREATED, PRIMED, AND INSTALLED IAW D C9 SRM 51-10-3, 51-30-2, AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999073000441 19990730 00441 WP 1999 7 30 AT9900506 1 19990610 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 503 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 503 AN D BL13L. STOP DRILLED, CONFIRMED CRACK CONTAINED. REMOVED FLOOR SUPPORT, WELD REPAIRED 1 EA CRACK. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2 AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999073000442 19990730 00442 WP 1999 7 30 AT9900507 1 19990610 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 522 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 522 AN D BL 6L. STOP DRILLED, FABRICATED DOULBER REPAIR, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 53-01 FIG 2, 51-10 -4 AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999073000443 19990730 00443 WP 1999 7 30 AT9900508 1 19990621 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 541 MISDRILLED A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND MISDRILLED HOLES IN FRAME AND FLOOR SUPPORT AT BS 541 AND LONGERON 24-27 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLES ON FLOOR SUPPORT AND FRAME IAW EA NR 12-5321-29-C1362 AND DC9 SRM 51-10-2, 53-01 FIG 2, AND 51-30-2. 2 L 7 2 4F A6WE 1999073000444 19990730 00444 WP 1999 7 30 AT9900509 1 19990610 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 560 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CRACK IN FLOOR SUPPORT FWD CARGO COMPARTMENT AT BS 560 BL 16R. REMOVED CRACKED FLOOR SUPPORT FITTING, DRILLED, DEBURRED NEW FITTING AND INSTALLED IAW DC9 SRM 51-30-5, 51-10-4, AND TIMCO RES NR 07655. 2 L 7 2 4F A6WE 1999073000445 19990730 00445 WP 1999 7 30 AT9900510 1 19990609 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 832 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND AFT PIT FLOOR SUPPORT FRAME STA 832 CRACKED ABOVE LONGERO N 29L. STOP DRILL CRACK, REMOVED FLOOR SUPPORT FRAME. HFEC VERIFIED CRACK CONTAINED. WELDED REPAIR 2 CRACKS ON FLOOR SUPPORT, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-30-1, AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999073000446 19990730 00446 WP 1999 7 30 AT9900511 1 19990609 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 851 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND AFT PIT FLOOR SUPPORT FRAME STA 851 CRACKED ABOVE LONGERO N 28L. REMOVED FLOOR SUPPORT. INSPECTED CRACK IDENTIFIED AND CONTAINED AFTER STOP DRILLED. FABRICATED REPAIR DOUBLER, PRIMED, AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-3, 51-30-1 AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999073000447 19990730 00447 NM 1999 7 30 AWXA9900250 1 19990727 A 2121 6454051 FAN BOEING 737 7373Y0 1384671 NM CABIN FAILED A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 28 329AW 36218 36218 23500 NORMAL OPS, SMELL IN CABIN. UNIDENTIFIED ELECTRICAL BURNING SMELL IN FORWARD CABIN. REMOVED AND REPLACED CABIN RECIRCU LATION FAN PER MM 21-21-22. RAN ACFT AND SYS CK GOOD. 2 L 7 2 4F RT A16WE 1999073000448 19990730 00448 WP 1999 7 30 CALA9900865 1 19990726 A 5230 CASTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND A 3 CRACK IN FORWARD BAGGAGE BIN DOOR AFT UPPER STOP SUPPORT CASTING. THE STOP SUPPORT CASTING WAS REM OVED AND REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999073000449 19990730 00449 WP 1999 7 30 CALA9900866 1 19990727 A 3350 1113161 BATTERY PACK DOUG DC9 DC982 3022082 WP CARGO COMPT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16893 49392 INSPECTION FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 1999073000450 19990730 00450 NM 1999 7 30 CALA9900867 1 19990727 A 5220 PRESS PANEL BOEING 727 727224 1384076 NM RT EMER EXIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A .5 INCH CRACK IN FORWARD RT OVERWING EXIT LOWER PRESSURE PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 51-40-3, PAGE 1, 51-10-2, PAGE 1, AND 51-30-2, PAGE 1. 2 L 7 3 4F A3WE 1999073000451 19990730 00451 NM 1999 7 30 CALA9900868 1 19990727 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FOREFLAP CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND THE LEFT O/B FOREFLAP CHAFED IN TWO AREAS AT INBOARD END. THE CHAFED AREAS WERE CUT OUT IAW SRM 57-50- 4, PAGE 17. REPAIR PARTS WERE INSTALLED IAW SRM 57-50-4, PAGE 17 AND 51-30-2. 2 L 7 3 4F A3WE 1999073000452 19990730 00452 NM 1999 7 30 CALA9900869 1 19990727 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 400 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT FS 400 BL 0 TO RBL 24. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS ACCO MPLISHED IAW SRM 53-10-8, PAGE 47. 2 L 7 3 4F A3WE 1999073000453 19990730 00453 NM 1999 7 30 UPS99230167 1 19990726 A 3350 38931002 LIGHT BOEING 727 72751C 1384015 NM PAX DOORWAY INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE:W/E FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, EMERGENCY LIG HT OPS CHECKED NORMAL PER MM 33-50-01. 2 L 7 3 4F A3WE 1999073000454 19990730 00454 NM 1999 7 30 UPS99230170 1 19990723 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION ON SEAT TRACK UPPER SURFACE O/B SIDE BS 950, LBL 45. REMOVED AND REPLACED SEAT TRACK FROM B S 870 TO BS 960. 2 L 7 3 4F A3WE 1999073000455 19990730 00455 NM 1999 7 30 UPS99230171 1 19990723 A 5320 SHEAR TIE BOEING 727 7272A1 138407F NM BS 990 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION ON FRAME SHEAR TIE BS 990, RBL 4, WL 148 BETWEEN STR 29-30R. REMOVED DAMAGE SHEAR TIE AND R EPAIRED IAW SRM 53-10-04 FIG 15. 2 L 7 3 4F A3WE 1999073000456 19990730 00456 NM 1999 7 30 UPS99230172 1 19990725 A 5320 SHEAR TIE BOEING 727 7272A1 138407F NM BS 970 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C WHILE WORKING 973519, FOUND CORROSION ON SHEAR TIE AT BS 970 RBL 8, WL 148 BETWEEN STRINGER 28, 29R. R EPAIRED SHEAR TIE AT BS 970 RBL 8 WL 148 PER SRM 53-10-1, 51-30-2, 53-10-4, 51-10-2. 2 L 7 3 4F A3WE 1999073000457 19990730 00457 NM 1999 7 30 UPS99230173 1 19990723 A 2612 FIRE LOOP BOEING 727 72725C 138400H NM NLG WW SHORTED A IPXA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 01 946UP 19721 WHEEL WELL FIRE INDICATION 20 MILES FROM SDF. GEAR EXTENDED AND LIGHT WENT OUT IMMEDIATELY. NORMAL LANDING, TIRES OK. INSPECTED L AND R W/W FIRE LOOP, NO DEFECTS NOTED, TESTED W/W FIRE DETECTION SYSTEM PER MM 26-12-00 PAGE 501 SYSTEM CHE CKS NORMAL. INSPECTED NOSE W/W FIRE LOOP AND REMOVED RUBBER CONTAMINANT FROM FWD LOOP CHECKS NORMAL. 2 L 7 3 4F A3WE 1999073000458 19990730 00458 NM 1999 7 30 UPS99230175 1 19990726 A 3350 LIGHT BOEING 727 72725C 138400H NM ROW 2 INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 EMERGENCY ESCAPE FLOOR PATH LIGHT AT ROW 2 (ABC) REMAINS ILLUMINATED AT ALL TIMES. DEFERRED PER MEL 33-17-2. 2 L 7 3 4F A3WE 1999073000459 19990730 00459 NM 1999 7 30 UPS99230177 1 19990712 A 5320 CREASE BEAM BOEING 727 7272A1 138407F NM BS 1170 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION ON I/B CREASE BEAM BS 1170 WL 208 LBL 64. CORROSION OUT OF LIMITS REPAIRS WILL BE ACCOMPLIS HED ON NRC 973397, WHICH ENCOMPASS THIS AREA. REPAIR GOES FROM BS 1159-1176. 2 L 7 3 4F A3WE 1999073000460 19990730 00460 NM 1999 7 30 UPS99230178 1 19990712 A 5320 CREASE BEAM BOEING 727 7272A1 138407F NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION ON CREASE BEAM I/B BS 1166, WL 209 RBL 64. CORROSION OUT OF LIMITS REPAIR WILL BE ACCOMPLIS HED ON NRC 973389 DO TO OTHER DEFECTS REPAIR WILL COVER FROM 1138-1176.* 2 L 7 3 4F A3WE 1999073000461 19990730 00461 WP 1999 7 30 UPS99830174 1 19990727 A 2613 OVERTEMP LIGHT DOUG DC8 DC871F 302199D WP FLIGHT DECK ILLUMINATED A IPXA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 744UP 45944 MAIN AIR OVERTEMP LIGHT ILLUM WITH MANIFOLD AIR TEMP IN NORMAL RANGE NO WARNING LIGHT. MONITORED LIGHT SUSPECT PRESS TO TEST. SWITCH LIGHT STILL ILLUM AFTER SHUTDOWN. RELAMPED MAN OVERTEMP LIGHT. RAN ALL ENG. NO OVERTEMP NOTED OPS CK O K. 2 L 7 4 4F RT 4A25 1999073000462 19990730 00462 WP 1999 7 30 UPS99830176 1 19990727 A 3350 570858503 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LTS BATTERY PACK IAW MM33-50-01. SYS OPS CHECKS NORMAL P/N ON 60 -1223-5 OFF 5708458-503 S/N ON 219 S/N OFF 2045. 2 L 7 4 4F RT 4A25 1999073000463 19990730 00463 NE 1999 7 30 99FDEA00284 2 19990726 A 7261 OIL LINE BOEING 727 727233 138408A NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE BROKEN A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 282FE 22349 99-171 - LOSS OF OIL ON NR 2 ENG QTY LOW PRESS, AND HIGH OIL TEMP PERFORM PRECAUTIONARY ENG SHUTDOWN. VIB ON DESCENT. F OUND BROKEN PRESS LINE TO NR 6 BEARING. REPLACED LINE PER PW JT8D MM 72-50 MAINT PRACT. RAN NR 2 ENG PER JET RUN HANDB OOK. NO LEAKS NOTED. ALL ENG PARAMETERS AND IND WERE NORM. 2 L 7 3 4F 4 F RT A3WE E2EA 1999073000464 19990730 00464 NM 1999 7 30 99FDEA00285 1 19990727 A 2497 D23390 WIRE DOUG MD11 MD11F 3023600 NM EXTERNAL POWER DAMAGED A FDEA K NONE A FLAME/FIRE IN INSP/MAINT 1 SO 25 606FE 48602 SNRM 322,444,321 - FWD CARGO EXTERNAL PWR CABLE NR C507-3-OC (AL), FOUND INSULATION BREAKDOWN AND OH SIGN (ARCING) AT BS 899, LBL 20 BELOW FLOORBOARD. INSULATION BLANKET AT BILGE AREA BURNT. REMOVED AND REPLACED EXT PWR SYS OPER CK FOUND SATISFACTORY PER 24-40-00-2. SERVICEABLE ITEM ROBBED FROM N590FE. FWD CARGO COMPT AT BILGE REPLACED PER MM 25-85-01-4 AND SUMP PANEL AFT EDGE REPAIRED SRM 53-00-01 VOL 1. 2 L 7 3 4F RT A22WE 1999073000465 19990730 00465 NM 1999 7 30 99FDEA00286 1 19990727 A 3230 RELAY BOEING 727 727233 138408A NM LANDING GEAR INOP A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 219FE 21102 99-172 LANDING GEAR LEVER FAILED TO RAISE AFTER TAKEOFF. WING ANTI-ICE WAS TESTED AND DID NOT OPEN. REMOVED AND REPL ACED R-92 RELAY, OPER CK WAS NORM PER MM 32-31-011-1 THROUGH 5. CLEANED PROXIMITY SWITCHES. 2 L 7 3 4F RT A3WE 1999073000466 19990730 00466 NM 1999 7 30 99FDEA00287 1 19990727 A 3610 INTERCONN LINE BOEING 727 727233 138408A NM THRUST REVR APU CRACKED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 221FE 20932 99-173 - ENGINE 3 STRUT OH LIGHT ILLUM IN FLT. SYSTEM TEST UNSATISFACTORY WITH CRUISE PWR ON ENG 3. FOUND THRUST REVER SER APU INTERCONNECT LINE CRACKED AND LEAKING. REMOVED AND REPLACED LINE IN ACCORD WITH STANDARD MAINTENANCE PRACTICE. LEAK CK GOOD. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1999073000467 19990730 00467 NM 1999 7 30 99FDEA00288 1 19990726 A 5330 655458313 SKIN BOEING 727 7272S2F 1384O81 NM BS 1059-1067 LIGHTNING STRIKE A FDEA K NONE C F.O.D. IN INSP/MAINT 1 SO 25 201FE 22924 NR 238 - 3 LIGHTNING STRIKES BETWEEN BS 1059 AND 1067 AT STR 30. REPAIRED DAMAGED SKIN PER FEDEX EA 7-5330-46963. 2 L 7 3 4F A3WE 1999073000468 19990730 00468 WP 1999 7 30 ABXA9900598 1 19990714 A 5230 9957663501 PAN DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED AT AFT LATCH. REPAIRED IAW DC9 SRM 52-05-00. 2 L 7 2 4F A6WE 1999073000469 19990730 00469 WP 1999 7 30 ABXA9900599 1 19990714 A 5730 591214461 SKIN DOUG DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND LEFT WING LOWER SKIN CRACKED NEAR INBOARD BUTE DOOR. REPLACED LEFT WING LOWER WING SKIN IAW DC9 S RM 51-30-1. 2 L 7 2 4F A6WE 1999073000470 19990730 00470 WP 1999 7 30 ABXA9900600 1 19990715 A 5730 591214462 SKIN DOUG DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND RT WING LOWER SURFACE PANEL FORWARD OF BUTE DOOR 1601A CRACKED. REPLACED PANEL IAW DC9 SRM 57-31- 3. 2 L 7 2 4F A6WE 1999073000471 19990730 00471 WP 1999 7 30 ABXA9900602 1 19990715 A 5313 59114277 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND LONGERON 16 RIGHT CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999073000472 19990730 00472 NM 1999 7 30 DLM88991653 1 19990723 A 2530 OVEN DOUG MD88 MD88 3023688 NM GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 988DL 53339 FIRST CLASS OVEN SMOKING IN CABIN. FOUND PAPER AND SHIPPING DOCUMENTS ON F/C OVEN INSERT. CLEANED OVEN AND REMOVED INS ERT. 2 L 7 2 4F RT A6WE 1999073000473 19990730 00473 NM 1999 7 30 DLM88991654 1 19990722 A 5330 595305069 SKIN DOUG MD88 MD88 3023688 NM BS 541-588 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DL 49546 FUSELAGE SKIN, FS 541-588 STRINGER 26L, GOUGE REPAIR. THE UPPER SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND GOUG ED BETWEEN FS 541 AND 588. THE DAMAGED SECTION OF SKIN WAS CUT AWAY FROM THE UPPER SKIN. AN ALUMINUM FILLER WAS INSTAL LED WITH AN INTERNAL TITANIUM DOULBER TO REPAIR THE DAMAGE PER ER/A 367832-14, REV A. 2 L 7 2 4F RT A6WE 1999073000474 19990730 00474 NM 1999 7 30 DLM88991655 1 19990722 A 5330 59360023 SKIN DOUG MD88 MD88 3023688 NM BS 588-636 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DL 49546 FUSELAGE SKIN FS 588-636, STRINGER 26L, SKIN GOUGE REPAIR. THE UPPER SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUN D BADLY GOUGED FROM FS 588 TO FS 636. THE SKIN PANEL WAS CUT AT FS 645 FROM STRINGER 26L TO STRINGER 18L AND THE DAMAGE D SECTION REMOVED. A NEW SECTION WAS SPLICED IN WITH AN EXTERNAL ALUMINUM SPLICE DOUBLER PER ER/A 367833-14, REV A. 2 L 7 2 4F RT A6WE 1999073000475 19990730 00475 WP 1999 7 30 DLL14991656 1 19990723 A 5512 1524132103 SKIN LKHEED 1011 1011385115 5265015 WP HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 740DA 193C1244 HORIZONTAL STABILIZER LEFT UPPER SKIN, HSS 80, STIFFENER NR 31 SKIN CRACK. REPAIR THE NR 4 UPPER SKIN PANEL OF THE LEFT HORIZONTAL STABILIZER WAS FOUND WITH A 1.25 CRACK AT THE RUNOUT OF STIFFENER NR 31. THE CRACK WAS ROUTED OUT OF THE SK IN AND AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 367841-14, REV A. 2 L 7 3 4F A23WE 1999073000476 19990730 00476 NM 1999 7 30 DL73K991659 1 19990723 A 3350 POWER SUPPLY BPS73 BOEING 737 737232 1384475 NM CABIN INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 318DL 47908 23090 RIGHT FWD OVERHEAD EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY. SYSTEM OPS NML. 2 L 7 2 4F RT A16WE 1999073000477 19990730 00477 NM 1999 7 30 DL73K991660 1 19990723 A 3350 LIGHT BPS73 BOEING 737 737232 1384475 NM ROW 10-16 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 317DL 19843 23089 EMER TRACK LTS INOP SEATS ROW 10-16. REPLACED EMER TRACK LT PACK BATTERY AND CHARGER OPS NML. 2 L 7 2 4F RT A16WE 1999073000478 19990730 00478 NM 1999 7 30 DL733991661 1 19990724 A 2150 24366100 SEAL BOEING 737 7373B7 1384580 NM LT PACK LEAKING A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 952WP 23378 LEFT WING BODY OVERHEAT ON IN FLIGHT. EXTINGUISHED AFTER 5 MIN. LEFT BLEED CLOSED PER POM. OHMED DETECTORS CHECK GOOD . FOUND PNEU LEAK ON LEFT PACK AT BAND CLAMP ABOVE MOISTURE SEPARATOR. REPLACED SEAL ASSY AT TURBO FAN SUPPLY LINE. L EAK CHECKS GOOD. RAN ENGINE, APU AT GATE NO OVERHEAT. 2 L 7 2 4F RT A16WE 1999073000479 19990730 00479 NM 1999 7 30 DLM88991662 1 19990724 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 907DL 49538 ON CLIMB-OUT ATL, WITH ENG ANTI-ICE ON, FLT ATT REPORTED ODOR AND SMOKE IN AFT CABIN. LAV SMOKE DET WENT OFF. ANTI-ICE TURNED OFF AND SMOKE DISSIPATED. DIVERTED TO CHA, CLEANED APU INLET. REPLACED COALESCER BAGS, PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1999073000480 19990730 00480 NM 1999 7 30 DL72S991663 1 19990723 A 3350 LIGHT 0201991007 BOEING 727 727232 1384082 NM ROW 20 DEF DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 21145 ONE EMERGENCY LIGHT AT 20 DEF INOP. REPLACED SEAT ASSY AT ROW 20 DEF. OPS CHECK GOOD. MCO AND PLACARD REMOVED. 2 L 7 3 4F A3WE 1999073000481 19990730 00481 NM 1999 7 30 DL72E991664 1 19990724 A 2910 1121521095 VALVE BOEING 727 727247 138408F NM A HYD SYS LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 830WA 21482 ON SHORT FINAL LOST ALL A HYD QTY AND PRESSURE. REPLACED FLOW REGULATOR VALVE, NR 1 AND 2 CASE DRAIN FILTERS SERVICED A HYD AND RAN ENGS. ALL INDICATIONS AND OPERATION CHECKS OK LEAK CHECKS OK. 2 L 7 3 4F A3WE 1999073000482 19990730 00482 NM 1999 7 30 DL76L991665 1 19990724 A 2560 BATTERY 20131A BOEING 767 767332 1382001 NM EMER EXIT SLIDE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 197DN 20504NY122 28454 DURING PDC OVERWING SLIDE SQUIBS WOULD NOT TEST. REPLACED BOTH OVERWING SQUIB BATTERIES M961 AND M962. TEST OPS NORMAL . 2 L 7 2 4F RT A1NM 1999073000483 19990730 00483 1999 7 30 DL72S991666 4 19990724 A 3442 20671570153 TR UNIT BOEING 727 727225 1384077 NM RADAR SYS INOP A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 8891Z 3350 21860 WEATHER RADAR INOP. REPLACED TRANSCVR. 2 L 7 3 4F A3WE 1999073000484 19990730 00484 NM 1999 7 30 DL757991668 1 19990724 A 3350 0201720001 LIGHT BOEING 757 757232 1384965 NM ROW 39 INOP A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 DURING L/O, FOUND EMERGENCY LIGHT INOP AT SEATROW 39 RT. NEEDS LIGHT ASSY P/N 331202161-NASI. 2 L 7 2 4F RT A2NM 1999073000485 19990730 00485 NM 1999 7 30 DL73K991670 1 19990725 A 2910 UNION BOEING 737 737232 1384475 NM RT WING LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 301DL 23073 LOST ALL 'A' SYSTEM HYDRAULIC FLUID. FOUND B-NUT LOOSE AT RT REV PRESSURE SWITCH, TIGHTENED SAME, CKS GOOD. 2 L 7 2 4F RT A16WE 1999073000486 19990730 00486 NM 1999 7 30 DLM88991672 1 19990726 A 5330 5911401181 SKIN DOUG MD88 MD88 3023688 NM BS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DL 49543 FUSELAGE SKIN WAS FOUND DENTED AT APPROX FS 218 AND L19L. CUTOUT DIMENSIONS ARE APPROX 16 BY 17. REPAIRED PER ERA 3333 66-14, REV A. 2 L 7 2 4F RT A6WE 1999073000487 19990730 00487 NM 1999 7 30 DLM88991673 1 19990726 A 5330 5924802517 SKIN DOUG MD88 MD88 3023688 NM BS 232 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DL 49543 FUSELAGE SKIN DENTED BETWEEN FS 229 AND 234 BETWEEN L17L AND L18L. CUTOUT DIMENSIONS ARE APPROX 5 BY 11. REPAIRED PER ERA 333371-14, REV A. 2 L 7 2 4F RT A6WE 1999073000488 19990730 00488 NM 1999 7 30 DL72S991674 1 19990725 A 5320 ANGLE BOEING 727 727232 1384082 NM PAX DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 T ANGLE SUPPORT DAMAGED AT AFT HINGE OF DOOR 3348. REMOVED DAMAGED PORTION OF T ANGLE. BEGAN FABRICATING T ANGLE PER M /M 53-30-1 FIG 804. FABRICATED REPAIR PIECES PER M/M 53-30-1 FIG 804. INSTALLED ANGLE REPAIR PER M/M 53-30-4 FIG 804. 2 L 7 3 4F A3WE 1999073000489 19990730 00489 NM 1999 7 30 DL767991675 1 19990726 A 5330 146T33212 SKIN BOEING 767 767232 1385132 NM BS 1260 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 GOUGE IN THE LHS SKIN PANEL BETWEEN BS 1241 TO 1285 AND S22L TO S25L REQUIRED REWORK. REWORKED AND REPAIRED PER ERA 333 352-14, REV. A. 2 L 7 2 4F RT A1NM 1999073000490 19990730 00490 NM 1999 7 30 DL72S991676 1 19990725 A 5754 RIB BOEING 727 727232 1384082 NM NR 3 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 LWR AFT EXTERNAL SKIN OPENED UP TO FACILITATE REPAIR OF NR 6 RIB. REPAIRED SKIN PER SRM 57-54-0 FIG 801. 2 L 7 3 4F A3WE 1999073000491 19990730 00491 NM 1999 7 30 DL72W991678 1 19990716 A 2497 BMS1331 INSULATION BOEING 727 727247 138408F NM NR 1 ENGINE SPLIT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 0 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SER VICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999073000492 19990730 00492 NM 1999 7 30 DL72W991679 1 19990716 A 2497 BMS1331 INSULATION BOEING 727 727247 138408F NM NR 3 ENGINE SPLIT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 0 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE L ETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999073000493 19990730 00493 NM 1999 7 30 DL72W991680 1 19990726 A 5754 BRACKET BOEING 727 727247 138408F NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 FOUND ON F-1 LETTER CK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED OUTBOARD END. REPAIRED PER MM 57-20-0. 2 L 7 3 4F A3WE 1999073000494 19990730 00494 NM 1999 7 30 SCNA99096 1 19990722 A 3260 SWITCH BOEING 727 7272A1 138407F NM LANDING GEAR INOP A SCNA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 286SC 21601 UPON GEAR RETRACTION, GEAR WARNING HORN SOUNDED. PULLED AURAL WARNING CIRCUIT BREAKER TO SILENCE HORN. RESET CIRCUIT B REAKER BEFORE GEAR EXTENSION, GEAR WARNING HORN CAME ON AND THEN WENT OUT WHEN ALL GEAR SHOWED DOWN AND LOCKED. REMOVED AND REPLACED FLAP SWITCH S294 IAW MM 312612. LANDING GEAR WARNING SYSTEM OPERATIONALLY CHECKS GOOD PER MM 326101. 2 L 7 3 4F A3WE 1999073000495 19990730 00495 NM 1999 7 30 DHL9970201C 1 19990623 A 5320 651829813 CASTING BOEING 727 72730C 1384009 NM GALLEY DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, GALLEY DOOR CUTOUT LOWER AFT CORNER CASTING HAS CRACK AND GOUGE. REPLACED CASTING AT DOOR CUT OUT LOWER AFT CO RNER IAW B77 SRM 51-30-2, N/R 3121. 2 L 7 3 4F A3WE 1999073000496 19990730 00496 NM 1999 7 30 DHL9970202C 1 19990619 A 3232 SUPPORT BOEING 727 72730C 1384009 NM LT MLG DOOR ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 TWO CRACKS ON LEFT MLG DOOR ACTUATOR LINK SUPPORT MOUNTED AT THE 870 BULKHEAD, LB22. REMOVED CRACKED ANGLES. REPLACED 3 BRACKETS PER SRM 51-40-3, 8.5 BY 5.5 AND 5 BY 9, 4 BY 3.25, N/R 7032. 2 L 7 3 4F A3WE 1999073000497 19990730 00497 NM 1999 7 30 DHL9970203C 1 19990630 A 7110 FRAME BOEING 727 72730C 1384009 NM NR 1 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, NR 1 ENGINE UPPER COWLING NR 14 FRAME HS EVIDENCE OF HEAVY CHAFING UNDER IMPROPER STRAP REPAIR AT 1/B FLANGE, A T O/B AFT CORNER OF COWL. REMOVED REPAIR, INSTALLED REPAIR PER SRM 54-10-3, 6 BY 3 N/R 6095. 2 L 7 3 4F A3WE 1999073000498 19990730 00498 NE 1999 7 30 DHL9970204C 2 19990621 A 7220 INLET BOEING 727 72730C 1384009 NM PWA JT8 JT8D7 52053 NE NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, NR 1 ENG INLET, AFT FLANGE CRACKED, OUTBD AFT SIDE WHILE COWLING MATES TO INLET. CUT OUT DAMAGED AREA, INSTALL ED DOUBLER REPAIR 8 BY 1 BY 1 FT PER SRM 51-40-2, N/R 6019. 2 L 7 3 4F 4 F A3WE E2EA 1999073000499 19990730 00499 NM 1999 7 30 DHL9970205C 1 19990623 A 7110 FRAME BOEING 727 72730C 1384009 NM PWA JT8 JT8D7 52053 NE NR 2 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, NR 2 ENG R4 FWD COWLING FRAME IS CRACKED AT NR 1 GUIDE AREA. CUT OUT DAMAGED SECTION, INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 13 BY 5, N/R 6041. 2 L 7 3 4F 4 F A3WE E2EA 1999073000500 19990730 00500 NM 1999 7 30 DHL9970206C 1 19990623 A 5753 SKIN BOEING 727 72730C 1384009 NM NR 2 TE MIDFLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, LW NR 2 FLAP (1/B) HAS MID FLAP WITH CORROSION AND DELAMINATION ON TOP SKIN ON TOP OF SECOND TRACK FOR AFT FLAP . CUT-OUT SMALL CORROSION AND DELAMINATION AREA AND INSTALLED FIBERGLASS OVERLAY REPAIR AT LW NR 2 FLAP (I/B) MID FLAP PER BOEING 727 SRM 51-40-8 FIG MAT USE AND RES 50-P HARDENER 946 BATCH AT AK9CP8011K PO NR 8315299 PLUS FIBERGLASS CLOTH STYLE 7781 PART 93115056 SIZE 12 BY 6, N/R 1048. 2 L 7 3 4F A3WE 1999073000501 19990730 00501 NM 1999 7 30 DHL9970207C 1 19990623 A 5753 SKIN BOEING 727 72730C 1384009 NM LT TE AFT FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, LW L/B AFT FLAP HAS CORROSION AND DELAMINATION AT I/B SIDE TOP SKIN. CUT-OUT SMALL CORROSION AND DELAMINATION AREA AND INSTALLED FIBERGLASS OVERLAY REPAIR AT LW I/B AFT FLAP AS PER B727 SRV 51-40-8 FIG 1 MATERIAL USED RES 50-A HAR DENER 946 BATCH NR AK9 CP8011 K DO NR 8315299 PLUS FIBERGLASS CLOTH STYLE 7781 RO NR 93115056 SIZE 14 BY4. 2 L 7 3 4F A3WE 1999073000502 19990730 00502 NM 1999 7 30 DHL9970208C 1 19990622 A 5243 DOOR BOEING 727 72730C 1384009 NM HYD COMPT DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK HYD COMPARTMENT B-SYSTEM DOOR IS DELAM. INSTALLED FIBRGLASS OVERLAY REPAIR AT HYD COMPARTMENT B SYSTEM DOOR AS PER B727 SRM 51-40-8 FIG 1 MATERIAL USED RESIR 50-A HARDENER 946 BATCH NR AK9CP8011K PO NR 8315299 PLUS FIBERGLASS CLOTH STYLE 7781 PO NR 93115056 SIZE 22 BY 20 N/R 3092. 2 L 7 3 4F A3WE 1999073000503 19990730 00503 NM 1999 7 30 DHL9970209C 1 19990622 A 5320 SUPPORT BOEING 727 72730C 1384009 NM BS 600 & 610 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, FAIRING SUPPORTS AT B5 600 AND 610 ARE BENT AND CRACKED AT LEFT SIDE STRINGER 281. CUT OUT DAMAGED RIB WEB INS TALLED REPAIR PER B727 SRM 51-40-2 AT BS 600 AND BS610 FAIRING SUPPORT MAT USED .040 2024T3 LOT NR 58599511 PMS PO NR 83 1125 2 PCS APPROX 6 BY 3 COMBINED AND PRIMED PER B727 SRM 51-10-2. N/R 3115. 2 L 7 3 4F A3WE 1999073000504 19990730 00504 NM 1999 7 30 DHL9970210C 1 19990623 A 5230 DOUBLER BOEING 727 72730C 1384009 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, FWD CARGO COMPARTMENT DOOR HAS A CRACKED DOUBLER AT THE AFT BOTTOM INTERIOR OF DOOR. THIS CAN BE SEEN WITH THE DOOR CLOSED AND INSIDE THE CARGO COMPARTMENT AT FS 560. REMOVED AND REPLACED DAMAGE AREA AT FWD CARGO COMP DOOR AFT BOT TOM INTERIOR OF DOOR MAT USED 2024-T3, 0.50 45 BY 5 LOT 335284 PO NR 8314616 AS PER B 727 SRM 53-10-1. N/R 3140. 2 L 7 3 4F A3WE 1999073000505 19990730 00505 NM 1999 7 30 DHL9970211C 1 19990625 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 259 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, PLUS 10 PERCENT MATERIAL LOSS AT STA 259 CIRCUIT BUTT SEAM APPRX S-9L LOCTION. INSTALLED DOUBLER REPAIR AT BS 259 STR 9L PER B727 S/B 727-53-0084 ALODINED AND PRIMED ALL PARTS AND AREA PER B727 SRM 51-10-2 MAT USED. FILLER .050 2 024T3 21 BY 4 APPROX LOT NR 344022 PO 8314930 DOUBLER .063 2024T3, 27 BY 6 LOT NR 364531 PO NR 64178343. N/R3162. 2 L 7 3 4F A3WE 1999073000506 19990730 00506 NM 1999 7 30 DHL9970212C 1 19990621 A 5330 WEB BOEING 727 72730C 1384009 NM BS 290 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, NOSE WW HORIZ WEB CRACKED ABOVE RT GEAR DOOR FWD HINGE BS290R. REMOVED HORIZ WEB AT NOSE WW RT GEAR DOOR FWD H INGE AREA BS 290R AS PER B727 SRM 51-30-2. REPLACED ENTIRE WEB SECTION AT NOSE WW HORIZ WEB AREA ABOVE RT GEARDOOR FWD HINGE ARA BS 290R. TREATED PRIMED AND INSTALLED AS PER B727 SRM 5-40-2 AND 51-10-6. MATERIAL USED 2024 T3 .032 PO NR 8 313301 MFG LOT NR 263413 7W BY 11 1/2 L. ALODINED AND PRIMED AREA AND PARTS PER B727 SRM 51-10-2. N/R 7049. 2 L 7 3 4F A3WE 1999073000507 19990730 00507 NM 1999 7 30 DHL9970213C 1 19990622 A 5755 SKIN BOEING 727 72730C 1384009 NM NR 1 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, LT/W O/B UPPER T/E PANEL O/B OF NR 1 SPOILER, I/B EDGE OLD REPAIR HAS CRACK AT FASTENER HOLE WS620. REPLACED O /D REPAIR STRAP PR B727 SRM 57-30-4 FIG 10 MATL USED 040 2024T3 APPROX 2 BY 10 LOT NR 44044T25 PMS PO NR 8313480. ALODI NED PRIMED TREATED AS PER B727 SM 51-10-2. N/R 1023. 2 L 7 3 4F A3WE 1999073000508 19990730 00508 NM 1999 7 30 DHL9970214C 1 19990625 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, CRACK INDICATION AT FASTENER ONE INCH RIGHT OF (BLO) STA 480. CUT-OUT DAMAGED AREA OF SKIN AT FWD SIDE STA 480 PRODUCTION BREAK BETWEEN BLO AND STR 28R 4.0 BY 2.0 IAW B727 S/B 727-53-0084 DRAWING NO69-62161 SHEET 2. ALODINED AND PRIMED AREA IAW B727 SRM51-10-2. INSTALLED DOUBLER REPAIR 9.5 BY 6.0 2024T3 .063 PO NR 8314831 LOT NR 316067 IAW B727 S /B 727-53-0084 DRAWING NR 69-62161 SHEET 2. SEALED DOUBLER REPAIR IAW B727 SRM 51-20-4, N/R 3160. 2 L 7 3 4F A3WE 1999073000509 19990730 00509 NM 1999 7 30 DHL9970215C 1 19990617 A 5280 HINGE BOEING 727 72730C 1384009 NM RT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, R MLG FUSELAGE DOOR FORWARD HINGE (MOUNTED TO KEEL BEAM) IS CRACKED AT FORWARD LOBE AFT CORNER. CRACK IS CONFI RMED BY NDT (MARKED). REMOVED AND REPLACED ON RT MLG FUS DOOR FWD HINGE AS PER B727 CHAP 51-30-2. N/R 7016. 2 L 7 3 4F A3WE 1999073000510 19990730 00510 NM 1999 7 30 DHL9970216C 1 19990624 A 5400 ANGE BOEING 727 72730C 1384009 NM NR 2 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, NR 2 ENG PYLON, ANGLE CRACKED AT AFT OF ENG-MOUNT. REMOVED ANGLE AT NR 2 ENG PYLON AT AFT OF ENG MOUNT IAW B72 7 SRM 51-30-2. REPLACED ANGLE AT NR 2 ENG PYLON AT AFT OF ENG MOUNT. MAT USES 7075-00. 050. PO NR 8315267 LO NR 219081 SIZED 8 BY 3 IAW B727 SRM 51-30-2 ALODINE AND PRIMED IAW B727 SRM 51-10-3 HEAT TREATED VERIFY HARDNESS IAW B727 SRM 51- 10-2. N/R6084. 2 L 7 3 4F A3WE 1999073000511 19990730 00511 NM 1999 7 30 DHL9970217C 1 19990620 A 5523 WEIGHT BOEING 727 72730C 1384009 NM RT ELEVATOR TAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, RT ELEVATOR TAB HAS BALANCE WEIGHT CRACKED. REPLACED RT ELEVATOR TAB BALANCE WEIGHTS PER B727 SRM 51-10-1 PAR 5 AND B727 SRM 51-30-2 AND S/B 727 55-0040 FIG 1, N/R4005. 2 L 7 3 4F A3WE 1999073000512 19990730 00512 NM 1999 7 30 DHL9970218C 1 19990620 A 5523 WEIGHT BOEING 727 72730C 1384009 NM LT ELEVATOR TAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, LT ELEVATOR TAB HAS BALANCE WEIGHTS CRACKED. REMOVED AND REPLACED LEFT ELEVATOR TAB WEIGHTS BALANCE AS PER S/B 727-55-0040 FIG NR 1, N/R 4004. 2 L 7 3 4F A3WE 1999073000513 19990730 00513 NM 1999 7 30 DHL9970219C 1 19990621 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 440 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, FUS EXTERIOR SKIN BULGED BUTT JOINT 440 S2R. CUT OUT DAMAGED AREA, FROM STR 4L TO 4R, PERFORMED HFEC, VISUAL I NSPECTED. PERFORMED INSURANCE CUT. INSTALLED REPAIR PARTS PER BOEING TELEX 32-9430, 5 BY 60, N/R 3027. 2 L 7 3 4F A3WE 1999073000514 19990730 00514 NM 1999 7 30 DHL9970220C 1 19990622 A 5240 FRAME BOEING 727 72730C 1384009 NM RT SERVICE DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, RIGHT SERVICE DOOR, THE DOOR FRAME HAS .5 INCH CRACK AREA OF FORWARD NR 2 STOP FROM THE BOTTOM. REMOVED RT SER VICE DOOR IAW B727 MM 52-40-0. INSTALLED RT SERVICE DOOR IAW B727 M/M 52-12-0. ADJUSTED RT SERV DOOR PER B727 M/M 52-1 2-0. LEAK OK IAW B727 MM 21-31-0. N/R 3113. 2 L 7 3 4F A3WE 1999073000515 19990730 00515 NM 1999 7 30 DHL9970221C 1 19990624 A 2761 FITTING BOEING 727 72730C 1384009 NM NR 6 SPOILER ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK NR 6 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED AT TOP FLANGE. CUT OUT DAMAGED AREAS I/B AND O/B SIDE OF NR 6 SPOILER ACT FITTING IAW AVITAS ENG. REPAIR ORDER NR 99AVHM .045R0-1 REV 1R SIZE OF CUT OUT 1 BY 1.5. EDDY CURRENT PER B727 NDT MAN. PART 6.51-00-00 FIG 4. NO CRACK INDICATIONS FOUND. INSTALLED DOUBLER REPAIR ON THE I/B AND O/B SIDE'S OF THE NR 6 SPOILER ACT FITTING IAW AVITAS EO NR 99AVHM .045RO-1 REV 1R MAT USED FILLER 2024T3 .090. 1 BY 1.5 INCH LOT NR 44703616 PO NR 8314951 DBLR'S 1 BY 9 301 L/1 HD .050 LOT NR 67569776 PO NR 8314031. ALODINED AND PRIMED ALL PARTS AND A REA PER B727 SRM 51-1002. N/R 1089. 2 L 7 3 4F A3WE 1999073000516 19990730 00516 NM 1999 7 30 DHL9970222C 1 19990623 A 5720 SUPPORT BOEING 727 72730C 1384009 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, RT WING L/E STRUCTURE WBL 92.8 VERT SUPPORT CRACKED AT BOTTOM WITH SEVERAL STOP DRILLED HOLES. CUT OUT DAMAGED SECTON, INSTALLED ANGLE REPAIR 1 BY 1.5 BY 7 PER SRM 51-40-3, N/R 2055. 2 L 7 3 4F A3WE 1999073000517 19990730 00517 NM 1999 7 30 DHL9970223C 1 19990623 A 5230 DOOR BOEING 727 72730C 1384009 NM CARGO COMPT MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, FWD CARGO COMPARTMENT DOOR, IMPROPER REPAIR DOUBLER INSUFFICIENT AMOUNT OF FASTENERS AND IMPROPERLY COVERING AR EA OF DAMAGE. FS 550 AFT BOTTOM SEEN THROUGH THE INSIDE. REMOVED AND REPLACED DAMAGE AREA AT FWD CARGO COMP DOOR AFT B OTTOM INTERIOR OF DOOR MAT USED 2024-T3 0.50 45 BY 5 LOT NR 335284 PO 8314616 AS PER B727 SRM 53-10-1. ALODINE AND PRIM ED AS PER 73.721 SRM 17-10-2. N/R 3141. 2 L 7 3 4F A3WE 1999073000518 19990730 00518 NM 1999 7 30 DHL9970224C 1 19990623 A 5754 FITTING BOEING 727 72730C 1384009 NM NR 6 LE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK RT WING L/E FLAP NR 6, MIDDLE HINGE UPPER FITTING SUPPORT (MAGNESIUM) HAS SEVERAL AREAS OF CORROSION OR EROISION (MRKD). REMOVED UPPER HINGE FITTING AND ATTCH LINK FOR INC NR 6 L/E FLAP PER B727 SRM 51-30-2. INSTALLED UPPER HINGE FITTING AT RT L/E FLAP NR 6 MIDDLE HINGE AS PER B727 SRM 51-30-2. INSTALLED BOLT ON NR 6 LE FLAP IAW B727 MM 20-50-01. N/R 2044. 2 L 7 3 4F A3WE 1999073000519 19990730 00519 NM 1999 7 30 DHL9970225C 1 19990621 A 2782 MOUNT BOEING 727 72730C 1384009 NM NR 1 LE SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, NR 1 SLAT ACTUATOR MOUNTS CRACKED. REMOVED NR 1 SLAT ACTUATOR FOR S/M REPAIR IAW B727 MM 27-81-32. REPLACED N R 1 SLAT ACTUATOR MOUNTS AS PER B727 SRM 51-30-02 AND SB727 57-0130 MATERIAL USED 7075-T6 .063 SIZE 10 BY 5 PO NR 831473 5 LOT NR 64454495. REINSTALLED NR 1 SLAT ACTUATOR IAW 727 MM 27-81-32-1. OP AND LEAK CHECK OK PERFORMED IAW 727 MM27-81 -0. ALODINED AND PRIMED TREATED AS PER B727 SRM 51-10-2. N/R 1003. 2 L 7 3 4F A3WE 1999073000520 19990730 00520 NM 1999 7 30 DHL9970226C 1 19990621 A 2782 SUPPORT BOEING 727 72730C 1384009 NM NR 1 LE SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, LT/W L/E, NR 1 SLAT ACTUATOR FRONT SPAR ATTACH I/B VERTICAL SUPPORT PREVIOUS REPAIR AT BOLT HOLE STH 734. REMO VED LT/W L/E NR 1 SLAT ACTUATOR FOR S/M REPAIR IAW B727 MM 27-81-32. REPLACED LT/W L/E NR 1 SLAT ACTUATOR FRONT STAR I/ B VERTICAL SUPPORT PER 727 SRM 51-30-02 AND SB 727 57-0130. MATERIAL USED 10 BY 5 301 H/D 1/2 .125 PO NR 990527 LOT NR 64216530. INSTALLED LT/W L/E NR 1 SLAT ACTUATOR IAW 727 MM 27-81-32. OPS AND LEAK CHECK FOUND GOOD IAW B727 MM 27-81-0 . N/R 1012. 2 L 7 3 4F A3WE 1999073000521 19990730 00521 NM 1999 7 30 DHL9970227C 1 19990622 A 5730 PANEL BOEING 727 72730C 1384009 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, RT WING LOWER SURFACE ACCESS PANEL NR 8505 T/E DELAMINATED (MRK). REMOVED PANEL NR 8505 RT WING LOWER SURFACE FOR FIBERGLASS REPAIR IAW B727-200 12-30-0. INSTALLED BONDING REPAIR AT RT WING LOWER SURFACE ACCESS PANEL NR 8505 T/E AS PER B727 SRM 51-40-6 FIG 1 MATERIAL USED ADHESIVE FILM AF163-2K WT. 085 PO NR 9018C9 LOT NR 8314718 AND ALUM 2024TE-0 20 LOT NR 269152 PO NR 72170236 SIZE 52 BY 6. RE-INSTALLED PANEL NR 8505 RT WING LOWER SURFACE IAW 727 MM 12-31-00. N/R 2010. 2 L 7 3 4F A3WE 1999073000522 19990730 00522 NM 1999 7 30 DHL9970228C 1 19990621 A 2782 SUPPORT BOEING 727 72730C 1384009 NM NR 1 LE SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, LT/W L/E, NR 1 FLAP ACTUATOR FRONT SPAR ATTACH. O/B VERTICAL SUPPORT LWR FLANGE CRACKED STA 307. REMOVED LT/W , L/E NR 1 FLAP ACTUATOR FOR S/M REPAIR IAW B727 MM 27-81-22. REPLACED DAMAGED (CRKD) ANGLE LT/W AT 1 FLAP ACTUATOR FRO NT SPAR ATTACH O/B SUPPORT AS PER AND IAW B727-SRM 51-30-02 MATERIAL USED 4 BY 8 2024-T3 .071 PO NR 8311936 LOT NR 94956 593. REINSTALLED L/E NR 1 FLAP ACTUATOR IAW 727 MM 27-81-22. OP AND LEAK CHECK PERFORMED OK IAW 727 MM 27-81-0. ALODI NED AND PRIMED TREATED PER B727 SRM 51-10-2. N/R 1007. 2 L 7 3 4F A3WE 1999073000523 19990730 00523 NM 1999 7 30 DHL9970229C 1 19990623 A 5720 SUPPORT BOEING 727 72730C 1384009 NM WS 130.7 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, RT WING L/E STRUCTURE, CEILING CROSS SUPPORT CRACKED AT O/B END, L/E STA 130.7. REMOVED UNSERVICEABLE CROSS SU PPORT AND REPLACED WITH NEW EXTRUSION ANGLE AS PER B727 CHAP 51-30-2 MAT USED 7075-T6 .75 BY3.75 BY X 16 LOT NR 354192 P O NR 831451. ALODINED AND PRIMED PER B727 SRM 51-10-2. N/R2054. 2 L 7 3 4F A3WE 1999073000524 19990730 00524 NM 1999 7 30 DHL9970230C 1 19990621 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 970 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, FUS EXTERIOR BS 970 S7L GOUGED SKIN. CUT OUT DAMAGES AREA OF SKIN AT STA 970 BETWEEN STR 6-72 3.0 BY 4.0 IAW 3 727 SRM 53-30-3 FIG 1. INSTALLED DOUBLER REPAIR 12 BY 20 PER 13727 SRM 53-30-3 FIG 1 2024T3 .080 PO NR 8314392 LOT NR 3 62671. TREATED AND PRIMED PER SRM B727 51-10-2. N/R 3038. 2 L 7 3 4F A3WE 1999073000525 19990730 00525 NM 1999 7 30 DHL9970231C 1 19990622 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, AFT CARGO BIN SEAT TRACK CRACKED STA 970 RT SIDE. CUT AND TRIMMED NEW SECTION OF FLOOR TRACK, MADE SPLICE STRI PS, PICKED UP EXISTING FASTENER HOLES AND ADDED NEW ATTACH FASTENER HOLES, TREATED N/R 3096 AND PRIMED ALL NEW AND EXIS TING PIECES IAW B727 SRM 53-10-5. REPLACED DAMAGED SECTIONS OF SEAT TRACK FROM STA 950 STA 1030 AND INSTALLED REPAIR AT STA 1030 AS PER B727 SRM 53-10-5 FIG 8 NOT USED BAC 1520 843 80 LOT NR 148462-1 PO NR 8314055 REPAIR STRAPS .250 7075-T6 (2 EA) 18 LOT NR 519161 PO NR 92991721. ALODINED AND PRIMED TREATED AS PER B727 SRM 51-10-2. N/R 3097. 2 L 7 3 4F A3WE 1999073000526 19990730 00526 NM 1999 7 30 DHL9970232C 1 19990622 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 1130-1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, AFT CARGO COMPT STA 1166 RT SEAT TRACK CRACKED. CUT OUT DAMAGED SECTION FROM STA 1166 TO 1130 AS PER B727 SRM 53-10-5 FIG 8. INSTALLED NEW SECTION OF SEAT TRACK FROM STA 1130 TO STA 1166 AND INSTALLED REPAIR PER B727 SRM 53-10-5 FIG 8 AT STA 1130 MAT USED BAC 1520-843 42 LT NR 148462-1 PO NR 8314055. REPAIR STRAPS .250 7075-T6 2 EA 18 LOT NR 5191 61 PO NR 92991721. ALODINED AND PRIMED TREATED AS PER B727 SRM 51-10-2. N/R 3097. 2 L 7 3 4F A3WE 1999073000527 19990730 00527 NM 1999 7 30 DHL9970233C 1 19990622 A 5321 FLOOR BOEING 727 72730C 1384009 NM CARGO COMPT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, AFT CARGO COMPARTMENT AFT BULKHEAD AREA BOTTOM OF CABIN FLOOR HAS AREA OF CORROSION AND A CRACK LEFT SIDE. REM OVED FASTENERS AFT CARGO AFT BULKHEAD BOTTOM AREA AS PER 727 SRM 51-30-2. CUT OUT DAMAGE CORRODED AREA AS PER 727 SRM 5 1-40-2 SIZE CUT OUT 14 BY 15. INSTALLED A WLS REPAIR AS PER B727 SRM 51-40-2 FIG 1 51-30-2. MAT USED 050 2024-T3 5 BY 16, 5 BY 17 LOT NR 335204 PO NR 8314616 DOUBLER, FILLER .040 2024-T3 14 BY 15 LOT NR 284281 PO NR 8314115. ALODINED AND PRIMED TREATED PER B727 SRM 51-10-2. N/R 3106. 2 L 7 3 4F A3WE 1999073000528 19990730 00528 NM 1999 7 30 DHL9970234C 1 19990623 A 5730 PANEL BOEING 727 72730C 1384009 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, LW PANEL ON TOP WING HAS I/B SIDE WITH CRACK AND WORN, O/B SIDE OF NR 5 SPOILER. REMOVED CRACKED METAL STRIP O N L/W PANEL O/B OF NR 5 SPOILER PER B727 SRM 51-30-2. REPLACED METAL STRIP ON L/W PANEL O/B OF NR 5 SPOILER PER B727 SR M 51-40-2. TREATED AND PRIMED PER B727 SRM 51-10-2. MAT USED .050 202473 APPROX 2 BY 20 LOT NR 344022 PO 8314932. OPS CK NR 5 SPOILER FOR SEAL CLEARANCE AT METAL STRIP OK PER B727 MM 27-61-1. N/R 1070. 2 L 7 3 4F A3WE 1999073000529 19990730 00529 NM 1999 7 30 DHL9970235C 1 19990624 A 5752 SKIN BOEING 727 72730C 1384009 NM RT AILERON TAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, RT WING O/B AILERON, I/B UPPER SKIN CRACKED AT I/B TAB BOND WIRE ATTACHMENT FASTENER. REMOVED AILERON TAB, CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 5 BY 7 PER SRM 57-50-5. BALANCEED PER SRM 51-80-4. NO WEIGHT REQUIRED. N/R 2103. 2 L 7 3 4F A3WE 1999073000530 19990730 00530 NM 1999 7 30 DHL9970236C 1 19990622 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 1263-1243 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, RT UPPER AIRSTAIRS AREA, TOP TORQUE BOX SKIN IS OIL CAN BS 1263 TO 1243. CUT OUT DAMAGED AREA AT RT UPPER AIRS TAIR AREA TOP TORQUE BOX SKIN MAT CUT OUT 15 BY 4 AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT UPPER AIRSTAIR A REA AT RT UPPER SKIN BS 1263 TO 1243 AS PER B727 SRM 51-40-2 MAT. USED 2024T3 .040 8 BY 17 PO NR 8314554 LOT NR 445911. ALODINED AND PRIMED PER B727 SRM 51-10-2. N/R 4016. 2 L 7 3 4F A3WE 1999073000531 19990730 00531 NM 1999 7 30 DHL9970237C 1 19990622 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 1285 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, AFT UPPER AIRSTAIRS WELL TOP TORQUE BOX SKIN IS OIL CAN BS 1285. CUT OUT DAMAGED AREA AT AFT UPPER AIRSTAIRS W ELL, TOP TORQUE BOX SKIN. MAT CUT OUT 18 BY 20 AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT AFT AIRSTAIR TORQU E BOX AREA TOP HORIZ WEB AT BS 1285 PER B727 SRM 51-40-2. TREATED AND PRIMED PARTS AND AREA PER B727 51-10-2. MAT USED .040 2024T3 22 BY 24 APPROX PO 8314000 LOT NR 229912. N/R 4018. 2 L 7 3 4F A3WE 1999073000532 19990730 00532 NM 1999 7 30 DHL9970238C 1 19990622 A 5320 ANGLE BOEING 727 72730C 1384009 NM BS 3441 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, NLG W/W AFT, SUPPORT ANGLE IS CRACKED AT STA 3441, ABOVE LOCK DOWN MECHANISM. REMOVED ANGLE, FOUND WEB CRACKED . CUT OUT DAMAGED AREA OF WEB, HFEC OF AREA. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 6 BY 7. REPLACED ANGLE PER SRM 51-30-2, 4 BY 12, N/R 7055. 2 L 7 3 4F A3WE 1999073000533 19990730 00533 NM 1999 7 30 DHL9970239C 1 19990621 A 7110 SKIN BOEING 727 72730C 1384009 NM NR 3 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, NR 3 ENG PYLON, UPPER FIXED COWL PANEL I/B OF UPPER MOUNT YOKE, DAMAGED AT UPPER FWD END. REPLACED DAMAGED ANG LE PER B727 SRM 51-40-3 FIG 1 & 54-10-2 ON NR 3 ENG PYLON UPPER FIXED COWL. I/B OF UPPER MOUNT YOKE AT UPPER FWD END. M AT USED 2024-0 .050 24 BY 4 LOT NR 49684612 PO NR 8315638. HEAT TREATED PART PER GPS 99PMSI.247PS-01. REPLACED DAMAGED SKIN PER B727 SRM 51-40-2 AND 54-30-2. MAT USED 2024T3 .040 23 BY 5.25 LOT NR 445911 PO NR 8314554. REPLACED DAMAGED FIRESHIELD PER B727 SRM 51-40-2 AND 54-30-2. MAT USED S/S 301 L/4 HD .012 23 BY 4 LOT NR 461818 PO NR 8314193. TREATED & PRIMED ALL PARTS PER B727 SRM 51-10-2. REINSTALLED NR 3 ENG PYLON UPPER FIXED COWLING PREVIOUSLY REMOVED PER B727 S 2 L 7 3 4F A3WE 1999073000534 19990730 00534 NM 1999 7 30 DHL9970240C 1 19990621 A 5320 ANGLE BOEING 727 72730C 1384009 NM BS 700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, RIGHT SIDE AIR CONDITIONING COMPARTMENT THROUGH GROUND AIR INLET DOOR AT STA 700 SUPPORT ANGLE FOR BODY FAIRING HAS CORROSION. CUT OUT DAMAGED AREA, INSTALLED ANGLE REPAIR, SUPPORT RIB, PER SRM 51-40-3, .75 BY 1.25 BY .75 LENGT H 10 AND DOUBLERS 2 EA, 1.25 BY .75 BY 19, N/R 3078. 2 L 7 3 4F A3WE 1999073000535 19990730 00535 NM 1999 7 30 DHL9970241C 1 19990621 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 1145-1180 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, FUS EXTERIOR SKIN BULGED BS 1045 TO 1180 RT SIDE OF S DUCT. REMOVED PREVIOUS DBLR AT STR 4 RT BS 1100 TO 1180 FOR ACCESS TO BULGED AREA PER B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT FUS EXTERIOR SKIN RT 1145 TO 1180 RT SIDE OF S- DUCT DAMAGED AT 4 BY 11 AS PER SRM 53-30-3. REMOVED STIRUP TIE AS PER B7272 SRM 51-30-2 AND INSTALLED AS B727 SRM 51-30 -1. CUT ANGLE ON DOG HOUSE STA 1183 TO 1173 RT STR 2 FOR DOUBLER ACCESS AS PR B727 53-30-3. TREAT PRIME AND INSTALLED DOUBLER REPEAT FUS EXT SKIN BS 1145 TO 1180 MAT USED 2024T3 .040 AND 2024T3 ON LOT NR 445911 PO NR 8314554 AND LOT NR 23 8484 AND PO NR 8312876 AS PER B727 SRM 51-10-2 AND 53-30-3 DOUBLER IS 58 BY 13 FILLER 60 BY 6. N/R 3032. 2 L 7 3 4F A3WE 1999073000536 19990730 00536 NM 1999 7 30 DHL9970242C 1 19990623 A 5720 BRACKET BOEING 727 72730C 1384009 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, RT WING T/E COVE PNL SUPPORT BRACKET CRACK AT FASTENER HOLE, I/B END OF NR 11 SPOILER PNL AND BELOW. REPLACED BRACKET AT I/B END OR NR 11 SPOILER PNL AS PER B77 SRM 51-10-1 PAR 4 AND 51-30-2. N/R 2083. 2 L 7 3 4F A3WE 1999073000537 19990730 00537 NM 1999 7 30 DHL9970243C 1 19990622 A 7110 SKIN BOEING 727 72730C 1384009 NM NR 1 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, NR 1 ENG INLET COWL CRACKED OUTER SKIN IN POSITION CRACK CONFIRMED BY NDT PART 6-51-00-00 HFEC JRT NDTI58. CUT OUT DAMAGED AREA ON NR 1 ENG NOSE COWL 17 AFT OF L/E AT 12:30 PR B727 SRM 54-30-3, 2.75 BY 8. PERFORMED HFEC INSP PER B7272 HDT MAN PART 6, 51-0-00 FIG 4, NO CRACK IND'S FOUND. CUT OUT SKIN FOR ACCESS 2 PLACES 5.625D OF PER B727 SRM 54-3 0-3 FIG 3. INSTALLED REPAIR AS PER B727 SRM 54-30-3 FIG 3A. NOT USED FILLER .032 2 .875 BY 7875 PO NR 831195 LOT NR 950 53348. DOUBLERS 15.5 BY 2 FT BY 1 (2EA) LOT NR 8314554 PO NR 8314554. OBTAINED AND PRIMED, TREATED PER B7272 SRM 51-10- 2. OK TO CLOSE ACCESS DOOR. INSTALLED ACCESS DOORS 2 AS PER B7272 SRM 54-30-3 FIG 3 MAT USED DOORS 5.625D .032 LOT NR 2 L 7 3 4F A3WE 1999073000538 19990730 00538 NM 1999 7 30 DHL9970244C 1 19990626 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 950-1030 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C CHECK, LWR AFT CARGO COMPARTMENT RT SEAT TRACK CRACK AT BOTH FWD AFT ENDS. REPLACED DAMAGE SECTION OF SEAT TRACK FROM STA 950 TO STA 1030; INSTALLED REPAIR AT STA 1030 AS PER B7272 SRM 53-10-5 FIG 8 MAT USED BAC1520-843 80 LOT NR 148462- 1 PO NR 8314055; REPAIR STRAPS .250 7075T6 (2 EA) 18 LOT NR 519161 PO NR 92991721. REPLACED DAMAGED SECT OF SEAT TRACK FRAME STA 1130 TO STA 1166 AND INSTALLED REPAIR PER B7272 SRM 53-10-5 FIG8 AT STA 1130 MAT USED BAC1520-843 42WT NR 1484 61-1 PO NR 8314055 REPAIRS STRUPS .250 7075T6 (2EA) 18 LOT NR 519161 PONR 92991721. ALODINED AND PRIMED, TREATED ALL PA RTS PER B7272 SRM 51-10-2. N/R 3167. 2 L 7 3 4F A3WE 1999073000539 19990730 00539 NM 1999 7 30 DHL9970245C 1 19990623 A 5320 WEB BOEING 727 72730C 1384009 NM BS 1176 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 C-CHECK, MAIN CABIN SHEAR WEB PLATE HAS CORROSION BELOW THE PLATE BS 1176 LBL 26. REMOVED FASTENERS ON HAT CHANNEL ANGL E AT BS 1176 LBL26 AS PER SRM 51-30-2. CUTOUT DAMAGE CORRODED AREA AS PER 727 SRM 51-40-2 SIZE CUT OUT 14 BY 15. INSTA LLED A WEB REPAIR AS PER B7272 SRM 51-40-2 FIG 1 AND 51-30-2 MAT USED .050 2024T3 5 BY 16 8 BY 17 LOT NR 335284 PO NR 82 14616 (DOUBLER) FILLER .040 2024T3 14 BY 15 LOT NR 28428 PO NR 8314115. ALODINED AND PRIMED TREATED PER B7272 SRM 51-10 -2. N/R 3130. 2 L 7 3 4F A3WE 1999073000540 19990730 00540 WP 1999 7 30 GTIA9900922 1 19990309 A 5321 FLOOR DOUG DC9 DC932 3022066 WP RT COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - CO-PILOT RUDDER FLOOR PANEL HAS CRACKED STRUCTURE FORWARD END BOTTOM. CUT OUT CRACK INSTALLED ANGLE DOUBLER PER D C9 IAW SRM 53-01-0 PAGE 1 AND 10 EXAMPLED FORMED ANGLE DOUBLER PER DC9 SRM 51-10-2 PAGE 1 FIG 2. INSTALLED FASTENER PER DC9 SRN 51-30-2. (M) 2 L 7 2 4F A6WE 1999073000541 19990730 00541 WP 1999 7 30 GTIA9900923 1 19990210 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-243 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FORWARD PASSENGER FLOOR PANEL FOR FS 200-243 LBL 21-42, CORNER CRACKED (TORN). FABRICATED FLOORBOARD IAW DC9 SRM 53-21-0 PAGE 6 INSTALLED STIFFENERS IAW DC9 SRM 51-30-2 PAGE 30. ALODINED AND PRIMED PER IAW DC9 SRM 51-10-3. INSTALLE D RIVETS IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999073000542 19990730 00542 WP 1999 7 30 GTIA9900924 1 19990227 A 5320 SKIN DOUG DC9 DC932 3022066 WP BS 218 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FS 218 264 LONGERON 15-18 SKIN REPAIR DAMAGED LEFT SIDE. REPLACED DAMAGED SKIN AND FINGER DOUBLERS PER DWG 53-990 34 FAX SURFACED SEAL ALL PARTS PER 51-20-0. INSTALLED FASTENERS WET WITH PR1422-B2. INSTALLED HI-LOCKS PER SRM 51-30-5 AND SOLID RIVETS PER 51-30-2. (M) 2 L 7 2 4F A6WE 1999073000543 19990730 00543 WP 1999 7 30 GTIA990925 1 19990304 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 220 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FLOOR SUPPORT AT STATION 220 RBL 48 TO RBL 56 IS SEVERELY CORRODED. REMOVED FLOOR SUPPORT FOR FURTHER INSPECTION FOUND TO BE OUT OF LIMITS PER 51-10-3. FABRICATED NEW SUPPORT PER DC9 SRM 51-10-1 SURFACE TREATMENT AND INSTALLED NEW S UPPORT PER DC9 SRM 51-10-3 AND 51-10-4. (M) 2 L 7 2 4F A6WE 1999073000544 19990730 00544 WP 1999 7 30 GTIA9900926 1 19990615 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 218 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - REF8 W245 FLOOR WEB LBL 61-64 STATION 218 HAS CORROSION BEYOND LIMITS. MANUFACTURED REPLACEMENT PANEL REF TO DC9 SRM 51-10-2 PAGE 2 PAR 2 SOLUTION HEAT TREATED THEN AGE HARDENED PER AMS-H-6088 AND ISSUED TO AIRCRAFT FOR FIT AND LOCAT ION ON W/O A066-C03-W245. (M) 2 L 7 2 4F A6WE 1999073000545 19990730 00545 WP 1999 7 30 GTIA990927 1 19990615 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 225 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 FLOOR WEB IS CRACKED AT FS 225 LBL 26 INSIDE MAIN CABIN 2ND CRACK AT FS 225 LBL 45. REMOVED DAMAGED CRACKED WEB PER DC9 SRM AND REPLACED WITH NEW WEB LOCATED AND DRILLED ALODINE AND PRIMED PER DC9 SRM 53-05 PAGE 1 27, 53-01 PAGE 2 53-21 PA G 6V 53-10-3 PAGE 16 (23) PAGE 18 (30). (M) 2 L 7 2 4F A6WE 1999073000546 19990730 00546 WP 1999 7 30 GTIA9900928 1 19990315 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP LAVATORY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - TWO FLOORBEAM CORROSION REPAIRS REQUIRE REPLACEMENT TO ACCOMMODATE LAV FLOOR STRUCTURE MODERATE. REMOVED TWO EXIS TING REPAIRS FABRICATED REPAIR ANGLE FROM 7075-T6 EXTRUSION NR S415615 CUST ORDER NR 12401 PO 30196 AND FILLERS FROM 707 5T6.125 PO 62571 IAW SRM 53-05 FIG 20A ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED REPAIR WITH PR1422B2 AND HL18 PB6 HI-LOCKS DC9 SRM 51-20 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1999073000547 19990730 00547 WP 1999 7 30 GTIA9900929 1 19990313 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 965 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - AFT CABIN LT BULKHEAD STATION 965 WATER LINE AND BULKHEAD TO FLOORBEAM ANGLE HAS GOUGES OUT OF LIMIT. REMOVED AND REPLACED WITH NEW PART FASTENERS INSTALLED PER SRM 51-30-5 RIVETS 51-30-2. (M) 2 L 7 2 4F A6WE 1999073000548 19990730 00548 WP 1999 7 30 GTIA9900931 1 19990324 A 2612 4915029503 FIRE HANDLE DOUG DC9 DC932 3022066 WP NR 2 ENGINE WORN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 13512 48111 MHV - NR 2 ENGINE FIRE HANDLE SPINS TO LEFT AND RIGHT WHILE PUSHED IN AND DOES'NT CENTER IN DETENT. REMOVED AND REPLACE D ENGINE FIRE HANDLE IAW DC9 MM 76-20-1 PAGE 401 PARA 3, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999073000549 19990730 00549 WP 1999 7 30 GTIA9900932 1 19990324 A 2612 FIRE HANDLE DOUG DC9 DC932 3022066 WP NR 1 ENGINE OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - NR 1 ENGINE FIRE HANDLE WILL NOT PULL BACK TO STOP REF W/O L150. RIGGED NR 1 FIRE HANDLE SYSTEM PER DC9 MM 76-20- 0 PAGE 201-208 ADJUSTED TENSION PER DC9 MM 76-00 PAGE 204 FIG 201. (M) 2 L 7 2 4F A6WE 1999073000550 19990730 00550 EU 1999 7 30 RAIA990631 1 19990620 A 2910 137905A77 LINE BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 426AM 874 FLT 7378 - STL - HYDRAULIC PRESSURE ON BOTH SIDES DROPPED TO ZERO. MAINTENANCE REPLACED RIGHT HYDRAULIC, PUMP PRESS LIN E. (M) 2 L 7 2 4T RT A56EU 1999073000551 19990730 00551 EU 1999 7 30 RAIA990629 1 19990620 A 2150 5595C056 DUCT ASSY AEROSP ATR72 ATR72202 8680940 EU LT PACK FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7400 - STL - LEFT DUCT TEMP TOO HOT. MAINTENANCE REPLACED DUCT ASSY FOR LEFT HEAT EXCHANGER. (M) 2 H 7 2 4T RT A53EU 1999073000552 19990730 00552 EU 1999 7 30 RAIA990630 1 19990620 A 2150 5595C056 DUCT AEROSP ATR72 ATR72202 8680940 EU RT PACK FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7400 - STL - RIGHT DUCT TEMP TOO HOT. MAINTENANCE REPLACED DUCT ASSY FOR RIGHT HEAT EXCHANGER. (M) 2 H 7 2 4T RT A53EU 1999073000553 19990730 00553 EU 1999 7 30 RAIA990625 1 19990618 A 5320 DOUBLER BAG JETSTM JETSTM3201 1500217 EU FUSELAGE FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424AM 865 STL - DAMAGE TO AFT FUSELAGE RESULTED FROM THE TRESTLE NOT BEING REMOVED PRIOR TO LOWERING A/C OFF OF JACKS. MAINTENANC E REPAIRED DAMAGE IAW EO NR J3200-53-014-1. (M) 2 L 7 2 4T RT A56EU 1999073000554 19990730 00554 EU 1999 7 30 RAIA990621 1 19990617 A 5210 137968C141 LEVER BAG JETSTM JETSTM3201 1500217 EU PAX DOOR FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 03 340TE 939 FLT 7364 - STL - PAX DOOR LIGHT ILLUMINATED. MAINTENANCE REPLACED PAX DOOR LOCK CAM LEVER. (M) 2 L 7 2 4T RT A56EU 1999073000555 19990730 00555 WP 1999 7 30 RAIA990622 2 19990617 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 FAILED A RAIA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CE 03 867AE 14837 867 66142 FLT 4778 - PSP - NR 2 ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED NR 2 ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999073000556 19990730 00556 EU 1999 7 30 RAIA990624 1 19990608 A 3610 ASN21414005 SEAL AEROSP ATR72 ATR72202 8680940 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7460 - STL - LEFT ENGINE BLEED LEAK LIGHT ILLUMINATED. MAINTENANCE REPLACED SEAL FOR TEMP SWITCH FOR BLEED AIR SHUT OFF VALVE. (M) 2 H 7 2 4T RT A53EU 1999073000557 19990730 00557 EU 1999 7 30 RAIA990623 1 19990608 A 2750 TY175902B CONTROL UNIT JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 564HK 41081 FLT 7213 - STL - FLAP FAULT LIGHT ILLUMINATED. MAINTENANCE REPLACED FLAP CONTROL UNIT. (M) 2 L 7 2 4T RT A41NM 1999073000558 19990730 00558 EU 1999 7 30 RAIA990620 1 19990614 A 3250 AIR860122 VALVE JETAIR JETSTM JETSTM4101 1500501 EU NLG FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 570HK 7637 41089 FLT 7635 - JFK - NOSE WHEEL STEERING PULLS HARD RIGHT. MAINTENANCE REPLACED STEERING SELECTOR VALVE. (M) 2 L 7 2 4T RT A41NM 1999073000559 19990730 00559 NM 1999 7 30 99ZZZM402 1 19990519 A 2421 GENERATOR BOEING 737 737247 138448D NM NR 1 FAILED A E9WA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 05 309VA 19614 NR 1 GEN DROPS OFF LINE. (M) 2 L 7 2 4F A16WE 1999073000560 19990730 00560 NE 1999 7 30 99ZZZM403 2 19990517 A 7200 ENGINE BOEING 737 7372H5 138448E NM PWA JT8 JT8D9A 52048 NE NR 2 LOST POWER A E9WA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 SO 05 220US 20453 665864 DURING TAKEOFF AT 80-90 KNOTS, NR 2 ENGINE LOST POWER, WAS SHUTDOWN AND TAKEOFF ABORTED. CAUSE UNDER INVESTIGATION AS T O FOD INGESTION OR NOT. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999073000561 19990730 00561 NM 1999 7 30 USAA990624 1 19990621 A 5330 SKIN BOEING 737 737201 1384454 NM BS 378 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 45400 22753 CLT - DURING METRO MOD, FOUND 1 INCH LONG CRACK ON SKIN AT STATION 378 BETWEEN STRINGER 21L AND STRINGER 22L. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-03 AND EA NR 64917. (M) 2 L 7 2 4F A16WE 1999073000562 19990730 00562 NM 1999 7 30 USAA990623 1 19990621 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 45400 22753 CLT - DURING METRO MOD, FOUND 1 INCH BY 2 INCH AREA OF CORROSION ON FLOORBEAM AT BS 294 AT LBL 06- LBL 10. REPAIRED PER T/R 53-10-04B AND EA NR 64946. (M) 2 L 7 2 4F A16WE 1999073000563 19990730 00563 NM 1999 7 30 USAA990622 1 19990621 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 45400 23314 CLT - DURING METRO MOD, FOUND 2 INCH LONG CRACK ON SKIN AT STATION 727B STRINGER 16L. INSTALLED DOUBLER PER SRM 53-30-3 . (M) 2 L 7 2 4F RT A16WE 1999073000564 19990730 00564 NM 1999 7 30 USAA990589 1 19990616 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 52084 21818 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727A, 2 INCH BY STRINGER 15L . INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999073000565 19990730 00565 NM 1999 7 30 USAA990601 1 19990616 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 52084 21818 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STATION 727A, 2 INCH AT STRINGER 18L . INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999073000566 19990730 00566 NM 1999 7 30 USAA990616 1 19990620 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 45835 22755 TPA - DURING CX-4 CHECK, FOUND CORROSION ON STRINGER .5 INCH BY 3 INCH AT STATION 1006 STRINGER 27L. REMOVED AND REPLAC ED STRINGER THAT WAS CORRODED, CLEANED AND TREATED SAME PER SRM 53-10-3 AND EA 64746. (M) 2 L 7 2 4F A16WE 1999073000567 19990730 00567 NM 1999 7 30 USAA990555 1 19990610 A 5320 693535214 CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND .125 INCH CRACK IN TIE CLIP AT STATION 616 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDEN TICAL PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000568 19990730 00568 NM 1999 7 30 USAA990554 1 19990610 A 5320 69353521 CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND .125 INCH CRACK IN TIE CLIP AT STATION 616 STRINGER 8L. DEFECTIVE PART REPLACED WITH IDEN TICAL PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000569 19990730 00569 NM 1999 7 30 USAA990553 1 19990610 A 5320 69353521 CLIP BOEING 737 737301 1384611 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND CRACKED TIE CLIP .125 INCH CRACK AT BS 706 STRINGER 2L. DEFECTIVE PART REPLACED WITH IDEN TICAL PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000570 19990730 00570 NM 1999 7 30 USAA990551 1 19990610 A 5320 69414372 CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND CRACKED TIE CLIP .125 INCH AT BS 663 STRINGER 10 RIGHT. DEFECTIVE PART REPLACED WITH IDEN TICAL PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000571 19990730 00571 NM 1999 7 30 USAA990550 1 19990610 A 5320 69414372 CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND TWO .5 INCH CRACKS IN TIE CLIP AT BS 663 FRAME TO S-10L TIE CLIP. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000572 19990730 00572 NM 1999 7 30 USAA990549 1 19990610 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND 2 INCH CRACK IN STRINGER 4L AT STATION 907 ABOVE TIE CLIP AT STRINGER 4L. INSTALLED SPLIC E ANGLE PER EA 64679 AND SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000573 19990730 00573 NM 1999 7 30 USAA990514 1 19990610 A 5320 693535214 CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND .250 INCH CRACK IN TIE CLIP AT BS 727D STRINGER 5 LEFT. DEFECTIVE PART REPLACED WITH IDEN TICAL PART NUMBER PER SRM PARA 4. (M) 2 L 7 2 4F RT A16WE 1999073000574 19990730 00574 NM 1999 7 30 USAA990539 1 19990529 A 5320 65C578393 MOUNT BOEING 737 7373B7 1384580 NM BS 993 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FUOND 2 INCH DIAMETER CORRODED AREA IN FORWARD INBOARD LAV MOUNT AT STATION 993 RBL 19 FLOOR LEV EL. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10 -02. (M) 2 L 7 2 4F RT A16WE 1999073000575 19990730 00575 NM 1999 7 30 USAA990538 1 19990529 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND SEVERAL 1 INCH DRAIN CORRODED AREAS IN FLOORBEAM AT STATION 986.5 FROM LEFT CREASE BEAM TO RIGHT CREASE BEAM FLOOR LEVEL. CORROSION LEVEL 1, CORROSION TASK NR C53-107-2. REPLACED BEAM 'T' CAP PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999073000576 19990730 00576 NM 1999 7 30 USAA990537 1 19990529 A 5320 656571023 CLIP BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q4 CHECK, FOUND 1 INCH CRACK IN RADIUS OF VERTICAL FLANGES AT ATTACH CLIP/BRACKETS AT LBL 2 AND RBL 2 AT ST ATION 727D. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBERS PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000577 19990730 00577 NM 1999 7 30 99ZZZM404 1 19990529 A 5320 6565710 BRACKETS BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q4 CHECK, FOUND 1 INCH CRACK IN RADIUS OF VERTICAL FLANGES AT ATTACH CLIP/BRACKETS AT LBL 2 AND RBL 2 AT ST ATION 727D. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBERS PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000578 19990730 00578 NM 1999 7 30 USAA990536 1 19990529 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND .125 INCH CRACK AT FRAME STATION 400 BETWEEN STRINGER 8L - STRINGER 9L (OVERHEAD BIN ATTAC H). INSTALLED DOUBLER REPAIR PER SRM 53-00-07 AND EA 64581. (M) 2 L 7 2 4F RT A16WE 1999073000579 19990730 00579 NM 1999 7 30 USAA990535 1 19990529 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURIGN Q-4 CHECK, FOUND .12 5INCH CRACK AT FRAME STATION 440 BETWEEN STRINGER 8L - STRINGER 9L (OVERHEAD BIN ATTAC H). INSTALLED DOUBLER REPAIR PER SRM 53-00-07 AND EA 64581. (M) 2 L 7 2 4F RT A16WE 1999073000580 19990730 00580 NM 1999 7 30 USAA990534 1 19990529 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND FUSELAGE FRAME CRACKED .200 INCH IN LENGTH, THREE (3) HOLES AT CLIP ATTACH ON FRAME. REMO VED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07, AND EA 64581. (M) 2 L 7 2 4F RT A16WE 1999073000581 19990730 00581 NM 1999 7 30 USAA990533 1 19990529 A 5320 69353521 CLIP BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND .125 INCH CRACK IN CLIP AT STATION 380, TOP CENTER CLIP (STRINGER TO FRAME ATTACH CLIP). D EFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10. (M) 2 L 7 2 4F RT A16WE 1999073000582 19990730 00582 NM 1999 7 30 USAA990532 1 19990529 A 5320 65657103 BRACKET BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND .25 INCH CRACK AT ANTENNA BRACKET AT 727 D TO E. INSTALLED NEW PART, IDENTICAL NUMBER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000583 19990730 00583 NM 1999 7 30 USAA990531 1 19990529 A 5320 654653949 ANGLE BOEING 737 7373B7 1384580 NM BS 518 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURIGN Q-4 CHECK, FOUND 2 INCH CRACK (FASTENER HOLE TO HOLE) AT LOWER END OF BS 618 LEFT FRAME INNER CHORD ANGLE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000584 19990730 00584 NM 1999 7 30 USAA990548 1 19990529 A 5314 65621258 KEEL BEAM BOEING 737 7373B7 1384580 NM BS 170-724 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q4 CHECK, FOUND .5 INCH BY 14 INCH CORRODED AREA AT RT KEEL BEAM AT BS 710 - BS 724, RBL 6.3, WL 148.5. CO RROSION LEVEL 1, CORROSION TASK C53-212-01. REMOVED DAMAGE BY BLENDING/SPOT FACING AND INSTALLED DOUBLER PER EA 64676. (M) 2 L 7 2 4F RT A16WE 1999073000585 19990730 00585 NM 1999 7 30 USAA990547 1 19990529 A 5320 BRACKET BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q4 CHECK, FOUND 2 INCH CRACK IN LOWER FLANGE AT ANTENNA SADDLE BRACKET AT STATION 727E - 727D. REPLACED SA DDLE BRACKET. (M) 2 L 7 2 4F RT A16WE 1999073000586 19990730 00586 NM 1999 7 30 USAA990546 1 19990529 A 5321 FLOOR BOEING 737 7373B7 1384580 NM LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 510AU 40289 23385 CLT - DURING Q-4 CHECK, FOUND 3 INCH CORROSION AT LT LAV FLOOR PAN. CORROSION LEVEL 1, CORROSION TASK NR C53-107-02. N EW WEB INSTALLED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999073000587 19990730 00587 NM 1999 7 30 TWRA9924 1 19990630 A 3397 WIRE BOEING 747 747212B 1384886 NM R2 DOOR BROKEN A TWRA K NONE O OTHER CL CLIMB 1 EA 15 616FF 21939 AFTER TAKEOFF, ALL EMERGENCY LIGHTS IN CABIN CAME ON AND REMAINED ON. REPAIRED BROKEN WIRE AT R2 DOOR AS PER WDM 33-51- 00. (M) 2 L 7 4 4F A20WE 1999073000588 19990730 00588 NM 1999 7 30 GAIA9978 1 19990621 A 5312 BULKHEAD BEAM BOEING 727 727251 138408H NM BS 338.5 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. LEFT SUPPORT BEAM FOR 9G BULKHEAD IS GOUGED AND RUBBED 72 INCH ABOVE FLOOR AT LBL 45. BLENDED GOUGE IAW B727 SRM AND FVI DRAWING 63-99094-1. THIS REPAIR HAS BEEN APPROVED BY THE FAA ATL/ACO LETTER NUMBER ACE 117A-99-10. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000589 19990730 00589 NM 1999 7 30 GAIA9979 1 19990621 A 5330 SKIN BOEING 727 727251 138408H NM BS 650 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. FUSELAGE SKIN GOUGED BY AFT CORNER OF MCD C UTOUT ON DOUBLER. BLENDED GOUGE IAW B727 SRM AND FVI DRAWING 53-99094-2. THIS REPAIR HAS BEEN APPROVED BY THE FAA ATL/ ACO LETTER NUMBER ACE 117A-99-10. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000590 19990730 00590 NM 1999 7 30 GAIA9980 1 19990621 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 680 MISDRILLED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. FLOORBEAM AT FUSELAGE STATION 680 HAS TWO E ACH HOLES MISDRILLED. INSTALLED REPAIR IAW FVI DRAWING 53-99094-3. THIS REPAIR HAS BEEN APPROVED BY THE FAA ATL/ACO LE TTER NUMBER ACE117A-99-10. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000591 19990730 00591 NM 1999 7 30 GAIA9981 1 19990621 A 5753 6521795 FAIRING BOEING 727 727251 138408H NM LT TE FLAP CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. LEFT INBOARD TRACK FAIRING CRACKED ON TOP. WELD REPAIR CRACK IAW FVI DRAWING 53-99084-1. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000592 19990730 00592 NM 1999 7 30 GAIA9982 1 19990621 A 5753 6521795 FAIRING BOEING 727 727251 138408H NM LT TE FLAP CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. LEFT OUTBOARD TRACK FAIRING CRACKED ON TOP. WELD REPAIRED IAW FVI DRAWING 53-99084-2. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000593 19990730 00593 NM 1999 7 30 GAIA9983 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 500 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 500R, FOUND FRAME BENT 6 INCHES ABOVE THE FLOOR LEVEL. REMOVED DAMAGE AND REPAIRED IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-3. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000594 19990730 00594 NM 1999 7 30 GAIA9984 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 520 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 520R, FOUND FRAME BENT 6 INCHES ABOVE THE FLOOR LEVEL. REMOVED DAMAGE AND REPAIRED IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-4. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000595 19990730 00595 NM 1999 7 30 GAIA9985 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 540 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 540R, FOUND FRAME BENT 6 INCH AB OVE THE FLOOR LEVEL. REMOVED DAMAGE AND REPAIRED IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-5. THE AIRCRAFT WAS R ETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000596 19990730 00596 NM 1999 7 30 GAIA9986 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 560 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 560R, FOUND FRAME BENT 6 INCH AB OVE THE FLOOR LEVEL. REMOVED DAMGE AND REPAIRED IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-6. THE AIRCRAFT WAS RE TURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000597 19990730 00597 NM 1999 7 30 GAIA9987 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 580 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 580R, FOUND FRAME BENT 6 INCH AB OVE THE FLOOR LEVEL. REMOVED DAMAGE AND REPAIRED IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-7. THE AIRCRAFT WAS R ETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000598 19990730 00598 NM 1999 7 30 GAIA9988 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 600 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 600R, FOUND FRAME BENT 6 INCH AB OVE THE FLOOR LEVEL. REMOVED DAMAGE AND REPAIRED IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-990848-8. THE AIRCRAFT WAS RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000599 19990730 00599 NM 1999 7 30 GAIA9989 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 640 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 640R, FOUND FRAME BENT 6 INCH ABO VE THE FLOOR LEVEL. REMOVED DAMAGE AND REPAIRED IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-9. THE AIRCRAFT WAS RE TURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000600 19990730 00600 NM 1999 7 30 GAIA9990 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 420 MISDRILLED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 420, FOUND A HOLE DRILLED INTO F RAME RADIUS BELOW STRINGER 16R. REPAIRED FRAME IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-10. THE AIRCRAFT WAS RE TURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000601 19990730 00601 NM 1999 7 30 GAIA9991 1 19990621 A 5312 BULKHEAD CHORD BOEING 727 727251 138408H NM BS 351.2 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 351.2, FOUND SKIN BULGING AND RIVETS PUL LING THROUGH AT STRINGER 26L. REPAIRED FRAME IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-11. THE AIRCRAFT WAS RETU RNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000602 19990730 00602 NM 1999 7 30 GAIA9992 1 19990621 A 5753 6521795 FAIRING BOEING 727 727251 138408H NM RT TE FLAP CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 252US 19971 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. RIGHT WING, INBOARD FLAP, INBOARD FAIRING H AS A CRACK AFT OF INBOARD MOUNT SCREW HOLE. WELD REPAIRED IAW FVI DRAWING 53-99084-12. THE AIRCRAFT WAS RETURNED TO SE RVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000603 19990730 00603 NM 1999 7 30 GAIA9997 1 19990607 A 3411 PITOT TUBE BOEING 727 7272J0 138407E NM NOSE SECTION CLOGGED A GAIA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 284KH 21108 AFTER TAKEOFF FROM AUS TO STL, FLIGHT 721, HAD THE CO-PILOTS AIRSPEED INDICATOR DECREASE 40 TO 50 KNOTS FROM THE CAPTAIN S AIRSPEED INDICATOR. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO AUS. THE AIRCRAFT LANDED WITHOUT FURTHER PROBL EMS. FOUND AN OBSTRUCTION AND CLEARED THE SAME FROM CO-PILOTS PITOT TUBE. PERFORMED PITOT SYSTEM TEST IAW BOEING MM 34 -11-0. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 1999073000604 19990730 00604 NM 1999 7 30 GAIA9998 1 19990707 A 5330 SKIN BOEING 727 727223 1384074 NM BS 990 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6834 20187 FOUND DURING PREFLIGHT WALK AROUND AND REPAIRED AT THE OSC MAINTENANCE FACILITY. A CRACK WAS FOUND IN THE FUSELAGE BELL Y SKIN AT THE 6 O'CLOCK POSITION, AT BODY STATION 990. NO ADDITIONAL DISCREPANCIES WERE NOTED. REMOVED DAMAGED SKIN IA W B727 SRM 53-30-3 FIG 3. FABRICATED REPAIRS PARTS IAW B727 SRM 53-30-3 FIG 3. INSTALLED REPAIR IAW B727 SRM 53-30-3. ITEM RETURNED TO SERVICEABLE CONDITION. (M) 2 L 7 3 4F A3WE 1999073000605 19990730 00605 NM 1999 7 30 TWRA9922 1 19990625 A 3350 CHARGER BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND D-ZONE RIGHT SIDE EGRESS LTS INOPERATIVE. REMOVED AND REPLACED CHARGER, OPERATIONAL CHECK NOR MAL, AS PER MM 43-51-00. (M) 2 L 7 4 4F A20WE 1999073000606 19990730 00606 WP 1999 7 30 ORJA99212 1 19990630 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 9DEF LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 RNO - E-LIGHT AT ROW 9 DEF INOPERATIVE. CONNECTED AND SECURED ELEC CONNECTION AT ROW 9 DEF. OPS NOW OK. (M) 2 L 7 2 4F RT A6WE 1999073000607 19990730 00607 WP 1999 7 30 ORJA99213 1 19990629 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 14 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 SJC - EMX - E-PATH LIGHT INOPERATIVE AT 1 ROW 14. REPAIRED BROKEN WIRE PER MM 25 AND WIRING DIAGRAM. (M) 2 L 7 2 4F RT A6WE 1999073000608 19990730 00608 NM 1999 7 30 ORJA99208 1 19990626 A 3350 60030451 BATTERY PACK DOUG MD90 MD9030 3023690 NM PAX DOOR DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 903RA 53551 SJC - FORWARD ENTRY DOOR EXIT E-PATH LIGHTS BATTERY PACK B5-234 HAS BLOWN INTERNAL FUSE. REMOVED AND REPLACED FORWARD E NTRY E-PATH LIGHT BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999073000609 19990730 00609 1999 7 30 G6OA034 4 19990616 A 3418 2568A13 AOA SENSOR DOUG DC10 DC1030F 3023504 WP E/E COMPT BAD A G6OA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 607GC 46978 DURING CLIMB-OUT, AUTO SLAT SYSTEM DEPLOYED. AFTER TROUBLESHOOTING, REMOVED AND REPLACED NR 2 AOA SENSOR IAW 22-31-01. SLAT SYSTEM TESTED OK IAW 22-33-00. (M) 2 L 7 3 4F RT A22WE 1999073000610 19990730 00610 NM 1999 7 30 TSAA9933282 1 19990625 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 1 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999073000611 19990730 00611 NM 1999 7 30 TSAA9933283 1 19990627 A 3350 873100151 LIGHT BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 4 FLOOR PROXIMITY LIGH TASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999073000612 19990730 00612 NM 1999 7 30 TSAA9933284 1 19990628 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 2 AND NR 3 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999073000613 19990730 00613 NM 1999 7 30 TSAA9933279 1 19990621 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED POSITIONS 1 AND 4 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999073000614 19990730 00614 NM 1999 7 30 TSAA9933280 1 19990624 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 AND NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1999073000615 19990730 00615 NM 1999 7 30 TSAA9933285 1 19990608 A 3350 86210066 BATTERY BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4U RT A16WE 1999073000616 19990730 00616 NM 1999 7 30 TSAA9933286 1 19990704 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M 2 L 7 2 4F RT A16WE 1999073000617 19990730 00617 NE 1999 7 30 TSAA9972281 2 19990623 A 7260 BEARING BOEING 737 7372M6C 1384708 NM PWA JT8 JT8D9A 52048 NE NR 1 GEARBOX WORN A TSAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 13 805AL 21809 656020 FLT 63 - OGG-HNL - DURING CLIMB, THE NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE ON NR 1 GAUGE WAS FA LLING RAPIDLY AND OIL TEMPERATURE WAS RISING. ENGINE WAS SHUTDOWN IAW THE CHECKLIST. EMERGENCY WAS DECLARED. UNEVENTF UL LANDING WAS MADE IN HONOLULU. REMOVED AND REPLACED NR 1 ENGINE IAW FORM M-211, M-213, M-212, M-214, M-215, M-209, AN D M-224. GEARBOX JY1963 WAS TORE DOWN AND ROLLER BEARING P/N PWA 446746 (INSTALLED ON OIL PUMP BEVEL GEAR) WAS FOUND WO RN. THE WORN BEARING CAUSED SLIPPAGE OF THE OIL PUMP AND CAUSED IT TO FAIL. ENGINE RUN OK. A/C RETURNED TO SERVICE. ( M) 2 L 7 2 4F 4 F RT A16WE E2EA 1999073000618 19990730 00618 NM 1999 7 30 EISA99078 1 19990327 A 5754 65162241 RIB BOEING 727 727223 1384074 NM LE SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND INBOARD RIB AND RIB ATTACH ANGLE AT NR 1 SLAT ACTUATOR ATTACH POINT CRACKED. REMOVED AND REPLACED SLAT WITH A SERVICEABLE UNIT PER MM 27-81-11. (M) 2 L 7 3 4F A3WE 1999073000619 19990730 00619 NM 1999 7 30 EISA99131 1 19990602 A 5270 65693581 SWITCH BOEING 727 72731 1384010 NM CARGO DOOR OUT OF ADJUST A EISA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 240NE 18906 CABIN PRESSURE CONTROL IN AUTO INOPERABLE. AIR TURN BACK WAS FOR LOWER FORWARD PIT DOOR LIGHT ILLUMINATED. CHECKED MAN UAL SYSTEM AND DEFERRED. ADJUSTED DOOR SWITCH MM CHAPTER 52-70-6. (M) 2 L 7 3 4F A3WE 1999073000626 19990730 00626 NM 1999 7 30 99ZZZM411 1 19990506 A 2910 2005005 LINE BOEING 757 75728A 1384976 NM LT MLG FAILED A AMTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 521AT 24368 DURING CLIMB, THE LEFT HYDRAULIC QUANTITY WAS LOSS TO .03, LEFT ENGINE PUMP PRESSURE LIGHT CAME ON, THEN LEFT ELECTRICAL HYDRAULIC PUMP PRESSURE LIGHT CAME ON. BOTH PUMPS WERE SHUT OFF, HAD TO USE ALTERNATE FLAPS AND ALTERNATE GEAR EXTEND. REPLACED LEFT LANDING GEAR DOWN LOCK ACTUATOR RETURN FLEX LINE, LEAK CHECKE DOPS CHECKED GOOD PER MM. (M) 2 L 7 2 4F RT A2NM 1999073000627 19990730 00627 NM 1999 7 30 99ZZZM412 1 19990531 A 2751 182994 INDICATOR BOEING 727 727227 1384078 NM TE FLAPS INOPERATIVE A AMTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 783AT 22000 DURING APPROACH ON FLAP EXTENSION, 2 DEGREES TO 5 DEGREES, OUTBOARD FLAPS STOPPED HALFWAY BETWEEN SETTINGS WITH AMBER LE D LIGHTS. AFTER SEVERAL MINUTES FLAPS WENT TO 5 DEGREES ON THEIR OWN. REPLACED FLAP INDICATOR AND LUBED OUTBOARD FORWA RD FLAPS WITH MIL H5606. (M) 2 L 7 3 4F A3WE 1999073000628 19990730 00628 NM 1999 7 30 99ZZZM413 1 19990515 A 2750 CONTROL CABLE BOEING 727 727227 1384078 NM TE FLAPS BROKEN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 766AT LTTEFLAP 21999 DURING PREFLIGHT, THE LEFT INBOARD TRAILING EDGE CABLE ASSY WAS FOUND BROKEN. REPLACED LEFT INBOARD TRAILING EDGE FLAP CABLE ASSY IAW MM 27-51-5, OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1999073000629 19990730 00629 NM 1999 7 30 99ZZZM414 1 19990525 A 2750 106081917 SWITCH BOEING 727 727227 1384078 NM NR 4 LE FLAP INOPERATIVE A AMTA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 11 766AT 21999 DURING APPROACH, THE NR 4 LEADING EDGE FLAP WOULD NOT EXTEND ACCORDING TO F/C ANNUNCIATOR. REPLACED LEADING EDGE FLAP S WITCH TO THE NR 4 POSITION PER 27-82-01, GROUND OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999073000630 19990730 00630 NM 1999 7 30 99ZZZM415 1 19990610 A 2750 MOTOR BOEING 727 727227 1384078 NM RT TE FLAP LEAKING A AMTA A UNSCHED LANDING F K FLT CONT AFFECTED FLUID LOSS CL CLIMB 1 GL 11 766AT 21999 FLIGHT 8035 - ATL-MUN - DURING CLIMB-OUT, SYSTEM 'A' PRESSURE STARTED SURGING WITH HYDRAULIC QUANTITY WENT OT ZERO AT AP PROXIMATELY FL240. DIVERTED TO MCO. FOUND FLAP HYDRAULIC MOTOR IN RIGHT WHEEL WELL LEAKING. REPLACED FLAP MOTOR IAW M M 27-51-62, OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1999073000631 19990730 00631 NM 1999 7 30 99ZZZM416 1 19990520 A 2424 902F2425 GCU BOEING 727 727227 1384078 NM NR 1 GENERATOR INOPERATIVE A AMTA D RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 772AT 22003 FLT 545 - MDW-MCO - DURING TAXI, THE NR 1 FIELD LIGHT WOULD NOT RESET CAUSING PACK TO OVERHEAT AND FILL CABIN WITH SMOKE . GATE TURN BACK. REPLACED THE NR 1 GENERATOR CONTROL PANEL, OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999073000632 19990730 00632 WP 1999 7 30 99ZZZM417 1 19990622 A 7930 SWITCH LKHEED 1011 10113851 5265010 WP NR 1 ENGINE SHORTED A AMTA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 196AT 193B1076 DURING CRUISE, THE NR 1 ENGINE FILTER PRESSURE LIGHT ILLUMINATED, ACCOMPLISHED PRECAUTIONARY ENGINE SHUTDOWN. DIVERTED TO IND. DURING TROUBLESHOOTING FOUND SCAVENGE PRESSURE DIFFERENTIAL SWITCH MAKES CONTRACT UNDER VIBRATION. REPLACED MA IN OIL FILTER PRESSURE AND SCAVENGE DIFFERENTIAL/PRESSURE SWITCHES, OPS CHECK GOOD. CANNON PLUG FOR THE NR 1 ENGINE PRE SSURE LIGHT FOUND TO BE BAD. REPLACED CANNON PLUG, OPS CHECK GOOD. (M) 2 L 7 3 4F A23WE 1999073000635 19990730 00635 NE 1999 7 30 ORJA99179 2 19990525 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE FIRE A ORJA F ACTIVATE FIRE EXT. J WARNING INDICATION IN INSP/MAINT 1 WP 11 822RA 49932 728035 RNO - STARTED NR 1 ENGINE DURING PUSH BACK INFORMED BY GROUND NR 1 ENGINE ON FIRE, CUT FUEL AND IGNITION, MOTORED AND DI SCHARGED NR 1 BOTTLE. INSPECTED ENGINE PER MM 70-00-00 PAGE 263. ENGINE NR 1 HAD A TAILPIPE FIRE, FOUND EXHAUST ACOUST IC PANEL DAMAGED 21 INCH BY 14 INCH. REMOVED LOOSE DEBRIS, PERFORMED TAKEOFF POWER ASSURANCE CHECK. BOTH NR 1 AND NR 2 ENGINES OPS CHECK NORMAL PER MM 71-00-00 PAGE 533. ENGINE CHANGED IN RENO. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999073000636 19990730 00636 NE 1999 7 30 99ZZZM420 2 19990518 A 8530 327629 CYLINDER CVAC 240 2405 2422612 WP PWA R2800 CB3 52026 NE NR 1 ENGINE CRACKED A TFAA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 15 295M 64 P34229 IN CRUISE, NR 1 ENGINE BEGAN TO BACKFIRE, POWER REDUCED RETURNED TO DEPARTURE AIRPORT AND LANDED. FOUND NR 1 CYLINDER C RACKED AND EXHAUST PUSHROD BROKEN CYLINDER AND PUSHROD REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R 4 R A793 E264 1999073000637 19990730 00637 WP 1999 7 30 99ZZZM421 1 19990511 A 2720 AN202KP33B BEARING CVAC 240 240* 2422601 WP RUDDER FAILED A TFAA O OTHER O OTHER CR CRUISE 1 SO 15 22913 14919 316 DURNIG A MAINTENANCE TEST FLIGHT, REQUIRED MORE THAN USUAL RUDDER TRIM. AFTER LANDING, NOTICED FLIGHT TAB APPEARED TO B E STUCK TO ONE SIDE. REMOVED RUDDER AND RUDDER POST. FOUND RUDDER QUADRANT LOCK BEARING FROZEN. BEARING REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R A793 1999073000638 19990730 00638 SO 1999 7 30 ASOA99054 1 19990624 A 2150 700VR02S3D01AMC INDICATOR EMB 120 EMB120RT SO COCKPIT FAILED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 11 240AS 120060 AFTER LANDING CREW EXPERIENCED SMOKE ALONG WITH AN ELECTRICAL SMELL IN THE COCKPIT, BUT COULD NOT LOCATE CAUSE. OPENED THE COCKPIT DOOR THE SMOKE SET OFF THE LAVATORY SMOKE ALARM. MAINTENANCE REMOVED AND REPLACED LEFT PACK FAIL INDICATOR. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999073000639 19990730 00639 SO 1999 7 30 ASOA99053 1 19990619 A 3350 D36604001 BATTERY PACKS EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 244AS 15555 120073 FLT 4862 - EMERGENCY FLOOR LIGHTS AT EXITS ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 POSITION BAT TERY PACKS. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999073000640 19990730 00640 SO 1999 7 30 ASOA99052S 1 19990616 A 2612 360190450180C35M FIRE LOOP EMB 120 EMB120RT SO APU DEFECTIVE A ASOA B F EMER. DESCENT ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 11 233AS 120031 FLT 4862 - AT TOP OF DESCENT RECEIVED INTERMITTENT APU FIRE WARNING. PROCEEDED WITH APU FIRE CHECKLIST. DECLARED EMERG ENCY AND REQUESTED PRIORITY HANDLING INTO DFW. ALSO, REQUESTED FIRE TRUCKS TO BE STANDING BY UPON ARRIVAL. ARRIVED SAF ELY IN DALLAS WITH NO FIRE. MAINTENANCE LOOKED AT APU AND DEFERRED IT. MAINTENANCE MOVED APU FIRE LOOP TO DEFER LOG NR 11002 OPERATE PER MEL 26-12-1. PLACARD INSTALLED CATC EXPIRES 6/26/99. FOUND APU FIRE LOOP CONNECTOR DAMAGED. REPLAC ED PINS. NEEDS NEW CONNECTOR PART NR MS3456KT14S-5S. REPLACED APU FIRE LOOP AND AS A PRECAUTIONARY MEASURE REPLACED AP U FIRE DETECTION MODULE PER MAINTENANCE. DEFER NR 11002 CLEARED AND PLACARD REMOVED. (M) 2 L 7 2 4T RT A31SO 1999073000641 19990730 00641 EU 1999 7 30 99ZZZM422 1 19990626 A 2613 HOT LIGHT SAAB SF340 SF340A 7850100 EU LT TAIL PIPE ILLUMINATED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 111PX 340A024 LEFT TAIL PIPE HOT LIGHT CAME ON. INVESTIGATED LEFT TAIL PIPE HOT LIGHT ON. CHECKED ENGINE FOR BLEED LEAKS, NONE NOTED . CHECKED WIRING AT TAIL PIPE FOR CHAFFING NONE NOTED. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 1999073000642 19990730 00642 1999 7 30 RAIA990642 4 19990628 A 3140 501156616 DCA INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 567HK 41085 FLT 7784 - DCA - STANDBY ATTITUDE INDICATOR INOPERATIVE. MAINTENANCE REPLACED STANDBY INDICATOR. (M) 2 L 7 2 4T RT A41NM 1999073000643 19990730 00643 EU 1999 7 30 RAIA990641 1 19990626 A 3260 8562BPEGP1 BULB JETAIR JETSTM JETSTM4101 1500501 EU NLG FAILED A RAIA O OTHER P NO WARNING INDICATION LD LANDING 1 CE 03 556HK 41073 FLT 7154 - STL - NOSE GEAR LIGHT AND RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. WHEN GEAR EXTENDED EMERGENCY GEARS LIGHTS SHOWED 3 GREEN. ONCE ON GROUND RT MAIN GEAR LIGHT CAME BACK ON. MAINTENANCE REPLACED LANDING GEAR BULBS ON CAP PANEL. (M) 2 L 7 2 4T RT A41NM 1999073000644 19990730 00644 1999 7 30 RAIA990640 4 19990627 A 3452 6226523201 ATC CONTROLLER AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 423TE 119 FLT 7176 - STL - NR 1 AND NR 2 TRANSPONDER INOPERATIVE. MAINTENANCE REPLACED ATC CONTROL HEAD. (M) 2 H 7 2 4T RT A53EU 1999073000645 19990730 00645 1999 7 30 RAIA990639 3 19990627 A 6140 RPT06F848 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 430AM 880 FLT 7476 - STL - RIGHT BETA WOULD NOT EXTINGUISH. MAINTENANCE REPLACED CANNON PLUG. (M) 2 L 7 2 4T RT A56EU 1999073000646 19990730 00646 EU 1999 7 30 RAIA990638 1 19990627 A 2121 EVAC2423FO FAN AEROSP ATR42 ATR42300 8680920 EU LT PACK FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 421TE 102 FLT 7116 - STL - LEFT PACK FAULTED ON TAXI WOULD NOT RESET. MANUAL DID NOT MAKE A DIFFERENCE. DUCT TEMP AT 50 DEGREE. MAINTENANCE REPLACED GROUND COOLING FAN AND TURBINE. (M) 2 H 7 2 4T RT A53EU 1999073000647 19990730 00647 EU 1999 7 30 RAIA990637 1 19990625 A 3620 2758A000 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 435AM 889 FLT 7308 - STL - LEFT DUCT CAP CAME ON DURING TAKEOFF. MAINTENANCE REPLACED LEFT PRESSURE SWITCH. (M) 2 L 7 2 4T RT A56EU 1999073000648 19990730 00648 EU 1999 7 30 RAIA990636 1 19990624 A 7331 TNAS10244182 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 424AM 865 FLT 7482 - STL - RIGHT FUEL FLOW METER AND TOTALIZER INOPERATIVE. MAINTENANCE REPLACED RT FUEL FLOW TRANSMITTER. (M) 2 L 7 2 4T RT A56EU 1999073000649 19990730 00649 EU 1999 7 30 SIMA991861 1 19990705 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423MQ 19795 030 SAW - DURING PS-2 INSPECTION, FOUND SEVERAL EMERGENCY FLOOR PROXIMITY LIGHTS THAT DID NOT ILLUMINATE. REMOVED AND REPLA CED EMERGENCY LIGHT BATTERY PACK AT LOCATION 10 WL IAW JIC 33-51-21-RAI-10100. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000650 19990730 00650 EU 1999 7 30 SIMA991901 1 19990709 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU LT CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT AND RIGHT AFT INBOARD AND THE LEFT AND RIGHT MIDDLE INBOARD SEAT TRACKS CORRO DED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX281 1 THROUGH NR 99ZZZX2813. (X) 2 H 7 2 4T RT A53EU 1999073000651 19990730 00651 EU 1999 7 30 99ZZZX2811 1 19990709 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU RT CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT AND RIGHT AFT INBOARD AND THE LEFT AND RIGHT MIDDLE INBOARD SEAT TRACKS CORRO DED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REPLACED 2 EACH. REF: OPER CNTRL NR SIMA991901, AND 99ZZZX2812 THROUGH 99ZZZX2813. 2 H 7 2 4T RT A53EU 1999073000652 19990730 00652 EU 1999 7 30 99ZZZX2812 1 19990709 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU LT CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT AND RIGHT AFT INBOARD AND THE LEFT AND RIGHT MIDDLE INBOARD SEAT TRACKS CORRO DED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REPLACED 2 EACH. REF: OPER CNTRL NR SIMA991901, AND 99ZZZX2811 THROUGH 99ZZZX2813. 2 H 7 2 4T RT A53EU 1999073000653 19990730 00653 EU 1999 7 30 99ZZZX2813 1 19990709 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU RT CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND LEFT AND RIGHT AFT INBOARD AND THE LEFT AND RIGHT MIDDLE INBOARD SEAT TRACKS CORRO DED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REPLACED 2 EACH. REF: OPER CNTRL NR SIMA991901, AND 99ZZZX2811 THROUGH 99ZZZX2812. 2 H 7 2 4T RT A53EU 1999073000654 19990730 00654 EU 1999 7 30 SIMA991902 1 19990709 A 5315 S5267240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 38 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000655 19990730 00655 EU 1999 7 30 SIMA991903 1 19990709 A 5320 S5367129034801 FITTING AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND FORWARD T-FITTING ON THE PASSENGER DOOR SILL PLATE BETWEEN FRAMES 36 AND 38 CORROD ED. REMOVED AND REPLACED T-FITTING IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000656 19990730 00656 NE 1999 7 30 SIMA991841 2 19990703 A 7200 ENGINE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE RIGHT FAILED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN B R SMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 274AT 9114 59 274 127129 CRP - FLT 3642 - AT AN ALTITUDE OF APPROXIMATELY 10,000 FEET, THE RIGHT ENGINE OIL PRESSURE BEGAN TO DROP FOLLOWED BY TH E ASSOCIATED OIL PRESSURE CAP ADVISTORY. WHILE THE CREW WAS C/W THE QRH, THE ENGINE SHUT DOWN UNCOMMANDED. FLIGHT ATTE NDANT REPORTED SMOKE WITHIN THE AIRCRAFT CABIN. REMOVED AND REPLACED THE RIGHT ENGINE ASSEMBLY IAW ATR JIC WC 05006-CS- 20000-001. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES: 9,156. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1999073000657 19990730 00657 1999 7 30 SIMA991842 4 19990703 A 2330 4970014012 HANDSET SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 244AE 340B244 MIA - FLT 5668 - FLIGHT ATTENDANT PANEL EMERGENCY LIGHT ARM SWITCH DOES NOT ILLUMINATE. REMOVED AND REPLACED FLIGHT ATT ENDANT HANDSET/CRADLE ASSEMBLY IAW SAAB AMM 23-30-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999073000658 19990730 00658 EU 1999 7 30 SIMA991851 1 19990704 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 3 FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 278AE 340B278 LAX - FLT 3319 - EMERGENCY FLOOR PROXIMITY LIGHT BULB IN FRONT OF SEAT 3 DOES NOT ILLUMINATE. REMOVED AND REPLACED EMER GENCY FLOOR LIGHT BULB. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999073000659 19990730 00659 EU 1999 7 30 SIMA991894 1 19990708 A 5315 S526724062081 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000660 19990730 00660 EU 1999 7 30 SIMA991893 1 19990708 A 5320 S5367121729802 SILL AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED SILL PLATE AND DRAIN RACK IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX2814. (X) 2 H 7 2 4T RT A53EU 1999073000661 19990730 00661 EU 1999 7 30 99ZZZX2814 1 19990708 A 5320 S5367121729801 DRAIN TRACK AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED SILL PLATE AND DRAIN RACK IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA991893. 2 H 7 2 4T RT A53EU 1999073000662 19990730 00662 EU 1999 7 30 SIMA991892 1 19990708 A 5320 S5367800821602 ZEE MEMBER AEROSP ATR72 ATR72212 EU FRAMES 39-41 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000663 19990730 00663 EU 1999 7 30 SIMA991891 1 19990708 A 5320 S5367800826801 SUPPORT AEROSP ATR72 ATR72212 EU FRAMES 38-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND THE LEFT AFT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACE D FLOOR SUPPORT IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000664 19990730 00664 EU 1999 7 30 SIMA991871 1 19990706 A 5330 S5317210122005 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE HOLE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - .50 INCH HOLE IN THE FUSELAGE SKIN 10 INCHES BELOW THE COPILOT'S SIDE WINDOW AND JUST FORWARD OF FRAME 8. REPAIRE D THE HOLE IAW SRM 53-00-00 FIGURE 408. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000665 19990730 00665 EU 1999 7 30 SIMA991832 1 19990702 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERABLE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 905AE 340B319 DFW - FLT 3585 - SOME OF THE EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REPAIRED BROKEN GROUND WIRE ON POWER SUPPLY 22LN P1 CANNON PLUG AND REMOVED AND REPLACED POWER SUPPLY AT LOCATION 22LN IAW AMM 33-50-10. OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4T RT A52EU 1999073000666 19990730 00666 EU 1999 7 30 SIMA991822 1 19990701 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-8 INSPECTION, FOUND THE RT MIDDLE OUTBOARD, THE LEFT AFT OUTBOARD AND THE RIGHT AFT INBOARD SEAT TRACK S CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. OPER CNTRL NR 99ZZ ZX2815 AND 99ZZZX2816. (X) 2 H 7 2 4T RT A53EU 1999073000667 19990730 00667 EU 1999 7 30 99ZZZX2815 1 19990701 A 5347 S53678001250 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-8 INSPECTION, FOUND THE RT MIDDLE OUTBOARD, THE LEFT AFT OUTBOARD AND THE RIGHT AFT INBOARD SEAT TRACK S CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. OPER CNTRL NR SIMA 991822 AND 99ZZZX2816. 2 H 7 2 4T RT A53EU 1999073000668 19990730 00668 EU 1999 7 30 99ZZZX2816 1 19990701 A 5347 S53678001248 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-8 INSPECTION, FOUND THE RT MIDDLE OUTBOARD, THE LEFT AFT OUTBOARD AND THE RIGHT AFT INBOARD SEAT TRACK S CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. OPER CNTRL NR SIMA 991822 AND 99ZZZX2815. 2 H 7 2 4T RT A53EU 1999073000669 19990730 00669 EU 1999 7 30 SIMA991823 1 19990701 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN OVERSIZED HOLE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING MBV-2 INSPECTION, FOUND FLOORBEAM 36 WITH A HILOCK HOLE THAT WAS OVERSIZED BEYOND LIMITS. REPAIRED THE FLO ORBEAM IAW SRM 53-00-00 PAGE 498. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999073000670 19990730 00670 EU 1999 7 30 SIMA991931 1 19990712 A 5315 S5367240102061 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAMS 31, 33, AND 35 WITH ELONGATED HI-LOCK HOLES. REPAIRED THE THREE FLOORB EAMS IAW SRM 53-00-00 FIGURE 429. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX.2817 THRU 99ZZZX2818. (X) 2 H 7 2 4T RT A53EU 1999073000671 19990730 00671 EU 1999 7 30 99ZZZX2817 1 19990712 A 5315 S5367240301861 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAMS 31, 33, AND 35 WITH ELONGATED HI-LOCK HOLES. REPAIRED THE THREE FLOORB EAMS IAW SRM 53-00-00 FIGURE 429. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA991931 AND 99ZZZX2818. 2 H 7 2 4T RT A53EU 1999073000672 19990730 00672 EU 1999 7 30 99ZZZX2818 1 19990712 A 5315 S5367240500661 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 431AT 431 SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAMS 31, 33, AND 35 WITH ELONGATED HI-LOCK HOLES. REPAIRED THE THREE FLOORB EAMS IAW SRM 53-00-00 FIGURE 429. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA991931 AND 99ZZZX2817. 2 H 7 2 4T RT A53EU 1999073000673 19990730 00673 NE 1999 7 30 SIMA991895 2 19990708 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FAILED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 21 312AE 16054 2553 340B312 GEE785282 LAS - FLT 3432 - ON TAKEOFF AT APPROXIMATELY 1,100 FEET AGL, HAD WHAT SEEMED TO BE A COMPRESSOR STALL ON THE LEFT ENGINE . TURNED CTOT OFF AND RETARDED POWER LEVER AND THE LEFT WAS STILL POPPING AND THE OVERTEMP WARNING LIGHT WAS ON AND THE TEMPERATURE INDICATION WAS 1,035 DEGREES. SHUT DOWN THE ENGINE AND RETURNED TO THE FIELD. REMOVED AND REPLACED LEFT E NGINE ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. PART TC: 19,841. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1999073000674 19990730 00674 EU 1999 7 30 SIMA991911 1 19990710 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU CARGO CMPT MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 203NE A3859 340B203 MIA - FLT 5611 - CARGO SMOKE WARNING ILLUMINATED ON CWP. DISCHARGED ONE FIRE EXTINGUISHER. RETURNED TO FIELD. VERIFIE D EVENT AS A FALSE WARNING. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND FIRE EXTINGHISHER. PERFORMED THE WIRIN G CHECK. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX2819. (X) 2 L 7 2 4T RT A52EU 1999073000675 19990730 00675 EU 1999 7 30 99ZZZX2819 1 19990710 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU CARGO CMPT MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 203NE A3355 340B203 MIA - FLT 5611 - CARGO SMOKE WARNING ILLUMINATED ON CWP. DISCHARGED ONE FIRE EXTINGUISHER. RETURNED TO FIELD. VERIFIE D EVENT AS A FALSE WARNING. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND FIRE EXTINGUISHER. PERFORMED THE WIRIN G CHECK. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA991911. 2 L 7 2 4T RT A52EU 1999073000676 19990730 00676 EU 1999 7 30 SIMA991941 1 19990713 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU ROW 7A LOOSE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 306AE 340B306 SBP - EMERGENCY LIGHT ABOVE SEAT 7A DOES NOT ILLUMINATE. FOUND CONNECTOR FOR LAMP DISCONNECTED. RECONNECTED CONNECTOR 425VP AND OPERATIONAL CHECKED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999073000677 19990730 00677 NM 1999 7 30 TSAA9933298 1 19990713 A 3350 6012311 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED RIGHT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (X) 2 L 7 2 4F RT A16WE 1999073000678 19990730 00678 NM 1999 7 30 TSAA9933297 1 19990713 A 3350 6012311 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED LEFT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (X) 2 L 7 2 4F RT A16WE 1999073000679 19990730 00679 NM 1999 7 30 TSAA9933295 1 19990708 A 3350 873100151 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERABLE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED NR 5 FLOOR PATH LIGHT ASSY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999073000680 19990730 00680 NM 1999 7 30 TSAA9933294 1 19990708 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED NR 4 FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999073000681 19990730 00681 NM 1999 7 30 TSAA9978296 1 19990710 A 7830 657360629 ACCESSORY UNIT BOEING 737 7372Q9 138448M NM TR UNIT DEFECTIVE A TSAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 13 809AL 21720 HNL/ITO - FLT 404 - TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. TAKEOFF ABORTED AT ABOUT 30 KNOTS. RETURNED TO GATE. REMOVED AND REPLACED ENGINE ACCESSORY UNIT. OPS CHECK OK IAW MM 78-34-91. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999073000682 19990730 00682 SO 1999 7 30 ASOA99059 1 19990711 A 3240 BRAKE EMB 120 EMB120RT SO MLG SMOKING A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 11 239AS 120057 FLT 4861 - ON TAKEOFF, AIRCRAFT 262 AT HOLD SHORT REPORTED TO CREW JUST PRIOR TO LIFT OFF THAT THE OUTBOARD MAIN WAS PUT TING OUT A BIT OF SMOKE. DECIDED TO RETURN TO DFW TO HAVE IT LOOKED AT, LANDED SAFELY. MAINTENANCE INSPECTED BOTH LEFT AND RIGHT OUTBOARD AND INBOARD MAIN TIRE WHEEL AND BRAKE ASSEMBLIES. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT REUTUNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999073000683 19990730 00683 SO 1999 7 30 ASOA99058 1 19990707 A 5230 12023348001 SEAL EMB 120 EMB120RT SO CARGO DOOR FAILED A ASOA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 11 215AS 120010 FLT 4912 - RAPID DECOMPRESSURIZATION AT 20,000 FEET. MANUAL MODE DID NOT CONTROL RATE AT THIS ALTITUDE. AT 10,000 FEET , MANUAL MODE WAS ABLE TO CONTROL RATE. PASSENGER MASKS DID DEPLOY DURING DEPRESSURIZATION. FLIGHT LANDED SAFELY. MAI NTENANCE FOUND BOTTOM AFT PORTION OF THE CARGO DOOR HAD PULLED AWAY FROM THE DOOR. REPAIRED CARGO DOOR SEAL. OPERATION AL CHECKS GOOD AND NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. TT: 34,260.7 HOURS. (X) 2 L 7 2 4T RT A31SO 1999073000684 19990730 00684 EA 1999 7 30 MASA99114 1 19990702 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37178 7178 FLT 6017 - DSM-PHX - THE CAPTAIN REPORTED A CEILING EMERGENCY EXIT LIGHT THAT WOULD NOT ILLUMINATE. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. THE AIRCRAFT RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, INSPECTED AND CHECKED OPERA TION OF EMERGENCY LIGHT. NO DISCREPANCY NOTED. OPS CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999073000685 19990730 00685 1999 7 30 99ZZZX2820 4 19990622 A 6122 311849603 GOVERNOR WOODWARD BEECH 1900 1900D 1154162 CE RT ENGINE FLUCTUATES A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 856CA 11695 4349 2490687 UE66 RIGHT ENGINE TORQUE FLUCTUATION ON TAKEOFF. GOVERNOR REPLACED WITH NEWLY OVERHAULED UNIT. SYSTEM OPERATIONAL AND LEAK CHECKED SATISFACTORILY IAW PRATT & WHITNEY CANADA MM, CHAPTER 61-20-00. (X) 2 L 7 2 4T RT A24CE 1999073000686 19990730 00686 EU 1999 7 30 PLGA990707 1 19990707 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A PLGA A F UNSCHED LANDING ACTIVATE FIRE EXT. B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CR CRUISE 1 NE 05 347BE A2889 340B187 ALB/BOS - FLT 6685 - CREW NOTED CARGO SMOKE DETECTOR LIGHT ILLUMINATED. CREW DISCHARGED THE CARGO FIRE BOTTLE AS PART O F THEIR CHECK LIST AND RETURNED TO ALB. LANDED WTHOUT INCIDENT. ALB MAINTENANCE REPLACED BOTH FORWARD AND AFT CARGO SM OKE DETECTORS AND THE CARGO FIRE BOTTLE. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX2821. ( X) 2 L 7 2 4T RT A52EU 1999073000687 19990730 00687 EU 1999 7 30 99ZZZX2821 1 19990707 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A PLGA A F UNSCHED LANDING ACTIVATE FIRE EXT. B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CR CRUISE 1 NE 05 347BE 9009 340B187 ALB/BOS - FLT 6685 - CREW NOTED CARGO SMOKE DETECTOR LIGHT ILLUMINATED. CREW DISCHARGED THE CARGO FIRE BOTTLE AS PART O F THEIR CHECK LIST AND RETURNED TO ALB. LANDED WTHOUT INCIDENT. ALB MAINTENANCE REPLACED BOTH FORWARD AND AFT CARGO SM OKE DETECTORS AND THE CARGO FIRE BOTTLE. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. REF: OPER CNTRL NR PLGA990707. 2 L 7 2 4T RT A52EU 1999073000688 19990730 00688 EU 1999 7 30 SIMA991821 1 19990701 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU SEAT 12 BC FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 350CF 340B350 LAX - FLT 3265 - FLOOR PROXIMITY LIGHT AT SEAT 12 B/C DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHEC K GOOD. (X) 2 L 7 2 4T RT A52EU 1999073000689 19990730 00689 EU 1999 7 30 99ZZZX2822 2 19990715 A 7200 ENGINE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 304FL 32493 27633 724893 DEN - DURING A-CHECK, INSPECTION REPORTED MAGNETIC CHIP DETECTOR TEST OF FORWARD SUMP DETECTED LARGE PIECES OF METAL IN GEARBOX. MAINTENANCE REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 1999073000690 19990730 00690 NM 1999 7 30 TSAA9921292 1 19990706 A 2131 CONTROLLER BOEING 737 7372Y5 1384554 NM CABIN FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 810AL 24031 HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED BUT DID NO T CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECK OK. REMOVED AND REPLACED LOWER PRESSURE RELIEF VALVE IAW 21-32-20 FOR PRECAUTI ONARY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4U RT A16WE 1999073000691 19990730 00691 NM 1999 7 30 USAABB99032 1 19990629 A 2422 S282T0044 INVERTER BOEING 757 757225 1384959 NM E/E COMPARTMENT FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 607AU 15989 22203 LAX - FLT 19 - INBOUND TO LAX, CREW NOTED AN ELECTRICAL SMELL THROUGHOUT THE AIRCRAFT. THE SMELL DISSIPATED QUICKLY. F LIGHT CONTINUED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE NOTED THE EICAS MESSAGE 'STBY INVERTER' AND REP LACED IT. (X) 2 L 7 2 4F RT A2NM 1999073000692 19990730 00692 NM 1999 7 30 USAASB99161 1 19990703 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM SERVICE DOOR INOPERABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 22879 BWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE DOORS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT A SSEMBLY AND THE BATTERY PACK FOR THE FORWARD ENTRY DOOR AND SERVICE DOOR ESCAPE SLIDE EMERGENCY LIGHTS. OPERATIONAL CHE CK GOOD. REF: OPER CNTRL NR 99ZZZX2823. (X) 2 L 7 2 4F A16WE 1999073000693 19990730 00693 NM 1999 7 30 99ZZZX2823 1 19990703 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM SERVICE DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 22879 BWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE DOORS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT A SSEMBLY AND THE BATTERY PACK FOR THE FORWARD ENTRY DOOR AND SERVICE DOOR ESCAPE SLIDE EMERGENCY LIGHTS. OPERATIONAL CHE CK GOOD. REF: OPER CNTRL NR USAASB99161. 2 L 7 2 4F A16WE 1999073000694 19990730 00694 WP 1999 7 30 MWEA075 1 19990222 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PASSENGER DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 1885 47672 MCI - FORWARD PASSENGER DOOR SLIDE FELL OFF DOOR. MTC RE-INSTALLED DOOR SLIDE. (X) 2 L 7 2 4F A6WE 1999073000695 19990730 00695 WP 1999 7 30 AT9900512 1 19990721 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 370-427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CORROSION BETWEEN DOUBLER AND TRIPLER AT FWD CARGO DOOR LOWER CUTOUT AT BS 370-427. REMOVED LOWER CARGO DOOR CUTOUT DOUBLER AND TRIPLER. FABRICATED NEW REPAIR DOUBLER AND TRIPLER AND INST ALLED IAW DC9 SRM 51-10-3 AND TIMCO EO 99-1187. 2 L 7 2 4F A6WE 1999073000696 19990730 00696 WP 1999 7 30 AT9900513 1 19990719 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-280 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FLOOR PANEL AT BS 200-280 LEFT CORRODED ALONG EDGE UPPER AND LOWER FL ANGE. CRACKS ON END HOLES IN PANEL. HAT CHANNEL CORRODED ENTIRE LENGTH. UPON FURTHER EVALUATION, FLOOR PANEL HAD EXFO LIATION CORROSION. FABRICATED NEW FLOOR PANEL. ALODINED AND PRIMED IAW DC9 SRM 53-21-0 AND 51-10-3. 2 L 7 2 4F A6WE 1999073000697 19990730 00697 WP 1999 7 30 AT9900514 1 19990714 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229 - 409 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND NUMEROUS DENTS IN RT FUSELAGE SKIN AT BS 229 - 389. REMOVE AND REPLA CE SKIN, FABRICATED SKIN AND SPLICE. DRILLED, COUNTERSUNK AND INSTALLED IAW TIMCO EO 99-1188. 2 L 7 2 4F A6WE 1999073000698 19990730 00698 WP 1999 7 30 AT9900515 1 19990628 A 5347 S29559781200 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD CARGO TRACK FWD PIT CORRODED. REMOVED CORROSION, DRILLED, COUNTE RSUNK, ALODINED, PRIMED NEW PART IAW DC9 SRM 51-10-4, 51-10-3, 53-01 FIG 1. 2 L 7 2 4F A6WE 1999073000699 19990730 00699 WP 1999 7 30 AT9900516 1 19990708 A 5320 59203321 END CAP DOUG DC9 DC932 3022066 WP BS 598 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND END CAP OF BS 598 L-27L CORRODED. REMOVED, RECEIVED NEW END CAP, DRI LLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2, 51-30-1 AND 53-01. 2 L 7 2 4F A6WE 1999073000700 19990730 00700 WP 1999 7 30 AT9900517 1 19990628 A 5347 S29559781200 CARGO TRACK DOUG DC9 DC932 3022066 WP BS 484-590 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND FWD CARGO TRACK FWD PIT AT BS 484-590 CORRODED. REMOVED AND REPLACED , DRILLED, COUNTERSUNK HOLES, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, 53-01 FIG1. 2 L 7 2 4F A6WE 1999073000701 19990730 00701 WP 1999 7 30 AT9900519 1 19990717 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND MAIN FRAME CRACKED AT BS 699L. REMOVED AND REPLACED FRAME IAW AIRTRA N EO 12-5311-29-B1044 FIG 5,6 AND 7. 2 L 7 2 4F A6WE 1999073000702 19990730 00702 WP 1999 7 30 AT9900520 1 19990717 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 737 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FRAME CRACKED AT BS 737L. REMOVED AND REPLACED FRAME IAW AIRTRAN EO 12-5311-29-B1044 FIG 5,6 AND 7. 2 L 7 2 4F A6WE 1999073000703 19990730 00703 NM 1999 7 30 AT9900521 1 19990723 A 3397 0816901 WIRE BOEING 737 7372T4 1384492 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 467AT 22055 EMERGENCY PATH LIGHTING MODULE HAD BROKEN WIRE. REPLACED EMERGENCY PATH LIGHTING MODULE IAW B737 20-0, OPS CHECK GOOD. 2 L 7 2 4F A16WE 1999073000704 19990730 00704 WP 1999 7 30 AT9900522 1 19990724 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP CARGO COMPT INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 811AT 47285 RIGHT ENGINE NACELLE AND EMERGENCY SLIDE LAMPS DO NOT ILLUMINATE WITH EMERGENCY SWITCH. REMOVED AND REPLACED POWER SUPP LY IAW MM 33-53-0. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1999073000705 19990730 00705 WP 1999 7 30 AT9900523 1 19990620 A 2550 TRIM STRIP DOUG DC9 DC932 3022066 WP BS 965-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND AFT PIT CENTER CEILING PANEL ATTACH STRAPS CORRODED AT BS 96 5-996. DRILLED 5 EACH CEILING PANEL CLOSE OUT TRIM STRIPS IAW DC9 SRM 51-10-4, 51-10-3. 2 L 7 2 4F A6WE 1999073000706 19990730 00706 WP 1999 7 30 AT9900524 1 19990520 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD PIT CENTER CEILING PANEL FASTENER STRIPS CORRODED AT BS 218. MATERIAL LOSS 100 PERCENT, OUT OF LIMITS, FABRICATED, TRIMMED AND DRILLED NEW STRAPS FROM 7075-T6 .032 IAW DC9 SRM 57-01, FIG 1, 51-10-2, 51-10-3. 2 L 7 2 4F A6WE 1999073000707 19990730 00707 WP 1999 7 30 AT9900525 1 19990630 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 680 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FIRST FASTENER ON RIGHT SHEAR TIE CRACKED AT BS 680 AND LONG ERON 1 R. CUT OUT CRACKED AREAS. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .025 AND 2024-T3 .063. INSTALLED IAW SERVICE REWORK DRAWING SR09530129 PER EO 99-1179. 2 L 7 2 4F A6WE 1999073000708 19990730 00708 WP 1999 7 30 AT9900526 1 19990629 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 290-350 CREASED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN CREASE 60.0 BY 1.5 BY .030 AT BS 290 - 350 BET WEEN L-22L AND L-23L. REMOVED AND REPLACED SKIN IAW TIMCO RES NR 06046, EO NR 1180 AND SRM 53-40 FIG 15D. 2 L 7 2 4F A6WE 1999073000709 19990730 00709 WP 1999 7 30 AT9900527 1 19990622 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 300 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN DENT 16 BY .5 BY .03. AT BS 300 BETWEEN L-18R AND L-19R DENT EXCEEDS LIMITS PER DC9 SRM 53-04 FIG 38 SHEET 10 FOOT NOTE 2 AND 3. REMOVED AND REPLACED FUSELAGE SKIN F ROM BS 229 TO 389 BELOW CUSP LINE IAW TIMCO EO NR 99-1177 APPROVED BY 8110-3 ISSUED BY MCDONNELL DOUGLAS. 2 L 7 2 4F A6WE 1999073000710 19990730 00710 WP 1999 7 30 AT9900528 1 19990619 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 1090 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND AFT AIRSTAIRS FWD SKIN AT BS 1090 AND L-30R MISSING INTERNAL SHIMS. AFTER OPEN UP FOUND WEB CRACKED AND FITTING CORRODED BEYOND LIMITS. FAB AND INSTALLED SHIM AND REPAIR DOUBLERS ON WEB. REMOVED AND REPLACED CORRODED FITTING IAW DC9 SRM 53-01, 51-30-2, 51-10-2. 2 L 7 2 4F A6WE 1999073000711 19990730 00711 WP 1999 7 30 AT9900529 1 19990610 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 99 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FUSELAGE SKIN CREASE 6 INCHES BELOW CUSP LINE ON LEFT SIDE A T BS 99. DRILLED .025 HOLE, INSTALLED RIVET PER RES NR 07613 AND DC9 SRM 51-10-2, 53-04 FIG 38. 2 L 7 2 4F A6WE 1999073000712 19990730 00712 WP 1999 7 30 AT9900530 1 19990521 A 5720 JAMB DOUG DC9 DC932 3022066 WP REFUELING DOOR GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND MAIN RE-FUELING POINT AT LOWER WING SKIN WORN THROUGH WHERE LATCH FOR FUEL DOOR MATES TO LOWER SKIN. FABRICATED FITTINGS. DRILLED, DEBURRED AND COUNTERSUNK HOLES IN FITTINGS. INS TALLED FITTINGS IAW TIMCO EO NR 99-1171, DC9 SRM 57-06B FIG 10, 51-06B SHT 1 AND 2. 2 L 7 2 4F A6WE 1999073000713 19990730 00713 WP 1999 7 30 AT9900531 1 19990704 A 5730 59127371 PANEL DOUG DC9 DC932 3022066 WP WS 353-414 DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND DELAMINATION AND CORROSION DAMAGE ON THE LT WING UPPER T/E P ANEL P/N 5912737-1. REPAIRED PANEL IAW TIMCO EO NR 99-1184. 2 L 7 2 4F A6WE 1999073000714 19990730 00714 WP 1999 7 30 AT9900532 1 19990625 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP BS 405-484 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD CARGO TRACK AT BS 405-484 CORRODED BEYOND LIMITS. FABRI CATED NEW TRACK IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1999073000715 19990730 00715 WP 1999 7 30 AT9900533 1 19990625 A 5347 S29559781200 CARGO TRACK DOUG DC9 DC932 3022066 WP BS 560-588 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD CARGO TRACK AT BS 560-588 CORRODED BEYOND LIMITS. REMOV ED AND REPLACED CARGO TRACK DRILLED AND COUNTERUNK NEW PART IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1999073000716 19990730 00716 WP 1999 7 30 AT9900534 1 19990721 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FLOOR PANEL NR 4693 AT BS 180-200 CORRODED ON TOP SIDE OF PA NEL AND INSULATION TORN. REMOVED CORROSION, PANEL OUT OF LIMITS. FABRICATED NEW FLOOR PANEL IAW 53-21-0, 51-10-3, 51-3 0-2. 2 L 7 2 4F A6WE 1999073000717 19990730 00717 WP 1999 7 30 AT9900535 1 19990723 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-280 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD ENTRY RT FLOOR PANEL AT BS 200-280 CORRODED. 3 HAT CHAN NELS CRACKED, ELONGATED HOLES AND INSULATION MISSING. FABRICATED NEW FLOOR PANEL AND HAT CHANNELS IAW DC9 SRM 53-21-0, 51-10-4. REINSTALLED MISSING INSULATION. 2 L 7 2 4F A6WE 1999073000718 19990730 00718 WP 1999 7 30 AT9900536 1 19990721 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1074 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CANTED FRAME AT BS 1074 CORRODED ON FWD SURFACE BELOW L-2L. REMOVED OLD WEB. FABRICATED WEB REPAIR. DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED WEB REPAIR IAW DC9 SRM 53-01 FIG 1, 51-30-2, 51-30B, 53-11-4 FIG 5. 2 L 7 2 4F A6WE 1999073000719 19990730 00719 WP 1999 7 30 AT9900537 1 19990724 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP AFT CARGO INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 811AT 47285 DURING SCHEDULE SERVICE CHECK, RT ENGINE NACELLE AND RT EMERGENCY SLIDE LAMPS DO NOT ILLUMINATE WITH EMERGENCY SWITCH. R EMOVED AND REPLACED POWER SUPPLY IAW MM 33-53-0. OPERATIONAL CHECK GOOD. NACELLE AND SLIDE LIGHTS ILLUMINATE. 2 L 7 2 4F A6WE 1999073000720 19990730 00720 WP 1999 7 30 CALA9900870 1 19990727 A 3260 SENSOR DOUG DC9 DC982 3022082 WP NLG INOP A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 14818 49478 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE NLG UP/DOWN LOCK PROXIMITY SENSOR IAW MM 32-60-05 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999073000721 19990730 00721 NM 1999 7 30 CALA9900871 1 19990727 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70352 23590 INSPECTION FOUND A 1 CRACK IN NR 1 ENGINE PYLON SKIN AT PANEL CUTOUT 5727L (NAC STA 213). THE CRACK WAS STOP DRILLED AN D A DOUBLER WAS INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 1999073000722 19990730 00722 WP 1999 7 30 CALA9900872 1 19990727 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 286 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND A 4 CRACK IN RT WING L/E UPPER SKIN AT NR 8 L/E SLAT TRACK, STA XOS 286. AN INTERNAL DOUBLER WAS INSTA LLED AND A DIP WAS ISSUED TO PERFORM A VISUAL INSPECTION EVERY SERVICE CHECK AND PENETRANT EVERY SEVEN DAYS WITH A PERMA NENT REPAIR TO BE INSTALLED AT NEXT 1/4D CHECK PER ECRA 5720-01725. 2 L 7 2 4F A6WE 1999073000723 19990730 00723 WP 1999 7 30 CALA9900873 1 19990727 A 5754 RIB DOUG DC9 DC982 3022082 WP NR 5 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND A 0.085 CRACK AT FASTENER HOLE OF LT O/B NR 5 SLAT SEAL RETAINING RIB. THE RIB WAS REMOVED IAW SRM 51- 30-0. THE RIB WAS REPAIRED AND REINSTALLED IAW SRM 51-30-0, ECRA 5750-03253, AND EA 9-2780-2-AO467. 2 L 7 2 4F A6WE 1999073000724 19990730 00724 WP 1999 7 30 CALA9900874 1 19990727 A 5712 RIB DOUG DC9 DC982 3022082 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16806 49260 INSPECTION FOUND A .5 CRACK IN LT WING L/E RIB APPROXIMATELY 12 INCHES O/B OF NR 8 SLAT TRACK AT TOP AFT ATTACH POINT TO SPAR. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-10-03 AND 51-30-0. 2 L 7 2 4F A6WE 1999073000725 19990730 00725 WP 1999 7 30 CALA9900875 1 19990727 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 69.55 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 69.550 I/B OF F/O'S PITOT TUBE ON AIRCRAFT NOSE. THE DENTED AREA WA S CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1999073000726 19990730 00726 WP 1999 7 30 CALA9900876 1 19990727 A 5210 49139471 FITTING DOUG DC9 DC982 3022082 WP L-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 478AC 48063 INSPECTION FOUND A 1 CRACK IN L-1 DOOR LOWER HINGE FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51-10-4. 2 L 7 2 4F A6WE 1999073000727 19990730 00727 NM 1999 7 30 CALA9900877 1 19990727 A 3350 BR964411 LIGHT BRUCE BOEING 727 727224 1384076 NM ROW 30 INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND THE SEAT MOUNTED EMERGENCY EXIT PATH LIGHT AT ROW 30 INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND R EPLACED. 2 L 7 3 4F A3WE 1999073000728 19990730 00728 NM 1999 7 30 UPS99230192 1 19990727 A 3350 LIGHT BOEING 727 72722C 138400F NM COCKPIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 941UP 19196 EMERGENCY LIGHT AT FWD ENTRY DOOR AND COCKPIT INOP. BATTERIES REPLACED, OP CHECKS OK IAW MM 33-50-00. 2 L 7 3 4F A3WE 1999073000729 19990730 00729 WP 1999 7 30 UPS99830179 1 19990629 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 257.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT WING L/E UPPER SKIN AT XW 257.5, 33 FWD OF THE SPAR, IS CRACKED BETWEEN 2 FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1999073000730 19990730 00730 WP 1999 7 30 UPS99830180 1 19990629 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 330 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123 RT WING L/E UPPER SKIN AT XFS 330, AT THE SPAR, HAS INTERGRANNULAR CORROSION AND IS CRACKED. CUT O UT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999073000731 19990730 00731 WP 1999 7 30 UPS99830181 1 19990629 A 5712 5769857614 RIB DOUG DC8 DC873F 302199F WP WS 453 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT WING OTBD SLOT, UPPER OTBD CLOSURE RIB AT XW 453 IS CRACKED AT THE AFT END. REMOVED AND REPLAC ED RIB IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999073000732 19990730 00732 WP 1999 7 30 UPS99830182 1 19990629 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 422.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 422.75 IS CRACKED AT A FASTENER. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087B. 2 L 7 4 4F RT 4A25 1999073000733 19990730 00733 WP 1999 7 30 UPS99830183 1 19990629 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 761.75 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT WING L/E LWR SKIN, AT THE L/E, STA XW 761.75 HAS INTERGRANNULAR CORROSION AROUND 2 SCREWS. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5720-4087B. 2 L 7 4 4F RT 4A25 1999073000734 19990730 00734 WP 1999 7 30 UPS99830184 1 19990630 A 5753 3751693501 FITTING DOUG DC8 DC873F 302199F WP WS 410 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, THE RT STA 410 FLAP UP STOP FITTING IS CRACKED. REMOVED AND REPLACED STOP FITTING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999073000735 19990730 00735 WP 1999 7 30 UPS99830185 1 19990701 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FS 55 FRAME AT LONGERON 24L IS CRACKED AT THE DUCT SUPPORT BRACKET. CUT OUT DAMAGED SECTION AND R EPAIRED FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000736 19990730 00736 WP 1999 7 30 UPS99830186 1 19990701 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FS 55 FRAME AT LONGERON 24R IS CRACKED AT THE DUCT SUPPORT BRACKET. CUT OUT DAMAGED SECTION AND R EPAIRED IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000737 19990730 00737 WP 1999 7 30 UPS99830187 1 19990701 A 5320 37515141 FITTING DOUG DC8 DC873F 302199F WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FLOORBEAM ATTACH FITTING IS CRACKED AT FS 980 BULKHEAD AT LBL 24. REMOVED, FABRICATED, AND REPLAC ED FITTING IAW DWG 3751514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999073000738 19990730 00738 WP 1999 7 30 UPS99830188 1 19990701 A 5320 37558412 FITTING DOUG DC8 DC873F 302199F WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FS 1160, BETWEEN LONGERON 34R AND 33R, THE BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTI NG IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999073000739 19990730 00739 WP 1999 7 30 UPS99830189 1 19990701 A 5320 9754022503 FITTING DOUG DC8 DC873F 302199F WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FLOORBEAM ATTACH FITTING AT FS 280, RBL 57, IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1 -20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999073000740 19990730 00740 WP 1999 7 30 UPS99830190 1 19990701 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 894 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FS 894, LONGERON 24R IS CRACKED. REPAIRED LONGERON IAW DH SK874-640. 2 L 7 4 4F RT 4A25 1999073000741 19990730 00741 WP 1999 7 30 UPS99830191 1 19990701 A 5320 561306444 FITTING DOUG DC8 DC873F 302199F WP BS 72 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LONGERON 30R AT FS 72 HAS MODERATE CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D A ND 51-3-0. 2 L 7 4 4F RT 4A25 1999073000742 19990730 00742 WP 1999 7 30 UPS99830193 1 19990702 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1225 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LONGERON 32L AT FS 1225 HAS HEAVY CORROSION. REPAIRED IAW EO DC8-5310-11651A AND DH SK874-683. 2 L 7 4 4F RT 4A25 1999073000743 19990730 00743 WP 1999 7 30 UPS99830194 1 19990702 A 5320 564989387 ANGLE DOUG DC8 DC873F 302199F WP BS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, ANGLE CRACKED, LT SIDE LWR CENTER WING AT FS 760, XCW 69. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5649893 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999073000744 19990730 00744 WP 1999 7 30 UPS99830195 1 19990702 A 5320 37799782 FITTING DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FWD SIDE OF THE FS 781 FRAME, AT LONGERON 18R, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999073000745 19990730 00745 WP 1999 7 30 UPS99830196 1 19990702 A 5511 RIB DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT HORIZ STAB L/E RIB AT XFS 141.25 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAI RED IAW SRM 55-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000746 19990730 00746 WP 1999 7 30 UPS99830197 1 19990704 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, NR 3 MAIN TANK INBD AFT ACCESS PANEL LAND IS CRACKED AT 2 FASTENER HOLES, (ACCESS PANEL 505F). CU T OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 36. 2 L 7 4 4F RT 4A25 1999073000747 19990730 00747 WP 1999 7 30 UPS99830198 1 19990704 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, SEVERAL POPPED RIVETS AND BULGING IN FINGER DOUBLER, FS 5, LBL 65. REMOVED, FABRICATED, AND REPLA CED FINGER DOUBLER IAW SRM 53-3-3 FIG 6 AND 51-1-21. 2 L 7 4 4F RT 4A25 1999073000748 19990730 00748 WP 1999 7 30 UPS99830199 1 19990728 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748UP 45948 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01 CHKS GOOD. 2 L 7 4 4F RT 4A25 1999073000749 19990730 00749 WP 1999 7 30 UPS99830200 1 19990704 A 5720 576960036 DOUBLER DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT WING L/E AT XFS 597.5, THE SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRIC ATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999073000750 19990730 00750 WP 1999 7 30 UPS99830201 1 19990705 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT WING L/E HAS RIBS CRACKED AT XFS 672.5, 660.0, 641.25 AT THE UPPER RIB; AND LOWER RIB AT XFS 60 3.75. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000751 19990730 00751 WP 1999 7 30 UPS99830202 1 19990727 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805UP 46117 EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK P/N ON/OFF 5708458-503 S/N ON 2024 S/N OFF 783. 2 L 7 4 4F RT 4A25 1999073000752 19990730 00752 WP 1999 7 30 UPS99830203 1 19990705 A 5720 576960035 DOUBLER DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 597.5, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FA BRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999073000753 19990730 00753 WP 1999 7 30 UPS99830204 1 19990705 A 5720 9753294 CLIP DOUG DC8 DC873F 302199F WP WS 267 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT WING L/E, ABOVE THE NR 3 PYLON, APPROX STA XFS 267, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVE D, FABRICATED, AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999073000754 19990730 00754 WP 1999 7 30 UPS99830205 1 19990705 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT WING L/E LWR RIBS ARE CRACKED AT XFS 822.5, 797.5, 791.25, 785.0, 778.75; UPPER RIBS ARE CRACKE D AT XFS 727.5, 760.0, 766.25, 785.0, AND 828.75. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000755 19990730 00755 WP 1999 7 30 UPS99830206 1 19990705 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT WING L/E UPPER RIBS CRACKED AT XS 484.895 AND 448.58. STOP DRILLED CRACKS AND REPAIRED RIBS IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000756 19990730 00756 WP 1999 7 30 UPS99830207 1 19990705 A 5751 SKIN DOUG DC8 DC873F 302199F WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT INBD AILERON UPPER L/E SKIN IS CRACKED JUST OTBD OF THE POWER CYL ATTACH FITTING. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-7767A. 2 L 7 4 4F RT 4A25 1999073000757 19990730 00757 WP 1999 7 30 UPS99830208 1 19990707 A 5320 4718340508 FITTING DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, FS 1540, AT LONGERON 33L, THE SEAT TRACK ATTACH FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABER ICATED, AND REPLACED FITTING IAW DH SK874-181 AND SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999073000758 19990730 00758 WP 1999 7 30 UPS99830209 1 19990707 A 5711 SPAR CHORD DOUG DC8 DC873F 302199F WP WS 17 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT WING FWD LWR SPAR CAP, LWR TAG IS CRACKED AT THE FASTENER HOLE AT XFS 17. CUT OUT DAMAGED AREA AND REPAIRED IAW SB 57-30 AND DWG SRO8570012. 2 L 7 4 4F RT 4A25 1999073000759 19990730 00759 WP 1999 7 30 UPS99830210 1 19990708 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 428.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT WING L/E RIB AT XFS 428.75 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000760 19990730 00760 WP 1999 7 30 UPS99830211 1 19990712 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 438 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LT WING LWR SKIN AT APPROX XRS 438, AND STRINGER 68, IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRE D IAW EO DC8-5730-9004. 2 L 7 4 4F RT 4A25 1999073000761 19990730 00761 WP 1999 7 30 UPS99830212 1 19990714 A 5313 432232741 LONGERON DOUG DC8 DC873F 302199F WP BS 65 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, LONGERON 23R AT FS 65 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A LONGERO N IAW SRM 53-2-2 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999073000762 19990730 00762 WP 1999 7 30 UPS99830213 1 19990722 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 69 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C123, RT WING L/E RIB AT XCW 69 IS CRACKED AT THE UPPER END. STOP DRILLED CRACK AND REPAIRED IAW 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999073000763 19990730 00763 NM 1999 7 30 99FDEA00289 1 19990728 A 7930 1163P182 SWITCH BOEING 727 72722C 138400F NM NR 3 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 112FE 19890 99-174 - NR 3 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON. ENG SHUTDOWN ACCOMPLISHED. REPLACED NR 3 ENG OIL FILTE R BYPASS SWITCH PER MM 79-33-000-0. REPLACED MAIN OIL STRAINER FILTER. PERF ENG WINDMILLING TEST PER MM 72-00 PG 5100. OPS CK GOOD. 2 L 7 3 4F A3WE 1999073000764 19990730 00764 1999 7 30 99FDEA00290 2 19990728 A 7261 FILTER BOEING 727 727227 1384078 NM NR 3 ENGINE DIRTY A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 25 477FE 21394 99-175 - NR 3 OIL QUANTITY DECREASED STEADY TO 0 GAL. LOST ENG OIL PRESSURE AND SHUTDOWN ENGINE IN ACCORD WITH RED TABS . REMOVED AND REPLACED MAIN ENG OIL FILTER PER MM 79-20-03 CK GOOD. PERF LP6 BOSS THREAD REPAIR. LEAK CK GOOD. A/C O K FOR SERVICE. 2 L 7 3 4F A3WE 1999073000765 19990730 00765 1999 7 30 99UAL900376 4 19990717 A 2330 285W00123 CACP BOEING 285W01293 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FLIGHT DECK OVERHEATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 788UA 26942 EN ROUTE LHR-IAD, ELECTRICAL ODOR REPORTED IN FLIGHT DECK AND MID GALLEY AREA. AIRCRAFT RETURNED TO LHR. *S/D* INSULA TION, (HEAT SHRINK), AT BASE OF LAMPS OVERHEATED. THE OVERHEAT CONDITION IS A KNOWN PROBLEM AND BOEING IS PREPARING A S ERVICE BULLETIN AND SOFTWARE TO CORRECT IT. THE CAUSE OF THE OVERHEAT IS THE RAMPING UP OF FILAMENT HEATER CURRENT WHEN BOTH LAMPS HAVE FAILED AND THE UNIT IS IN THE DIM MODE. THE SOFTWARE WILL PREVENT THE CACP/CSCP (P/N'S 285W0012-3/285W 0129-3) FROM GOING INTO DIM MODE. IT WILL TURN OFF THE HEATER CURRENT TO THE CACP AND WILL SIMULATE DIM MODE ON THE CSC P. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999073000766 19990730 00766 NM 1999 7 30 99UAL900377 1 19990623 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 303.5 MISMANUFACTURED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 7442U 21896 AN OVERSIZED COUNTERSUNK FASTENER WAS FOUND IN THE FUSELAGE SKIN AT BS 303.5 BETWEEN STRINGER 3L AND 4L. THE HOLE IS CO MMON TO THE SKIN, DOUBLER AND BEAR STRAP AND THE FASTENER COUNTERSINK CREATES A KNIFE EDGE CONDITION IN THE SKIN AND BON DED DOUBLER. THE FASTENER HOLE WAS OVERSIZED IN THE SKIN AND DOUBLER IN ORDER TO REMOVE THE KNIFE EDGE CONDITION AND A FREEZE PLUG WAS INSTALLED PER SRM 51-10-7. THIS REPAIR WAS APPROVED BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000767 19990730 00767 NM 1999 7 30 99UAL900378 1 19990701 A 5320 6556129 SILL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 950-990 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7442U 21896 THE AFT CARGO DOOR CUTOUT LOWER SILL CHORD AT BS 950E TO BS 990 WAS FOUND CORRODED AND CRACKED, A REPLACMENT CHORD SEGME NT WAS SPLICED IN. THIS REPAIR AREA IS WITHIN SSID INSPECTION AREA, SUBJECT TO AD98-11-03. STRUCTURAL SUBSTANTIATION O F REPAIR PLAN WAS OBTAINED BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000768 19990730 00768 NM 1999 7 30 99UAL900379 1 19990701 A 7120 MOUNT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7442U 21896 DURING ACCOMPLISHMENT OF BOEING SB 727-54A0019 AS MANDATED BY AD97-05-O8, A CRACK INDICATION WAS FOUND IN HOLE H COMMON TO THE NR 1 ENGINE PYLON FORWARD MOUNT. THE FASTENER HOLE H WAS OVERSIZED TO A DIAMETER OF O,3432-0.3442 INCH TO REMOVE THE CRACK AND AN OVERSIZED FASTENER INSTALLED, THIS REPAIR IS A DEVIATION TO AD 97-05-08 AND THEREFORE AN ALTERNATE MEA NS OF COMPLIANCE WAS OBTAINED FROM THE FAA. 2 L 7 3 4F 4 F A3WE E2EA 1999073000769 19990730 00769 NM 1999 7 30 99UAL900380 1 19990701 A 5312 BULKHEAD FITTING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1183 MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 7442U 21896 TWO PRODUCTION HOLES WERE FOUND MISDRILLED AT S29L END FITTING (P/N 65-60208-1), LOCATED AT BS 1183 BULKHEAD CHORD (P/N 65-16350-5) WL 150,LBL 10. THE INBOARD HOLE WAS REPAIRED WITH A FREEZE PLUG, WHILE THE OUTBOARD HOLE WAS OVERSIZED. TH IS REPAIR WAS APPROVED BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000770 19990730 00770 NM 1999 7 30 99UAL900381 1 19990705 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 950 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7442U 21896 CORROSION DAMAGE WAS FOUND ON STRINGER 29 RT (KEEL BEAM) IN THE RADIUS OF THE LOWER FLANGE AT BS 950E PLUS 8. THE CORRO SION DAMAGE WAS BLENDED OUT AND REPAIR ANGLES INSTALLED TO RESTORE THE STRENGTH TO THE STRINGER. THIS REPAIR WAS APPROV ED BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000771 19990730 00771 NM 1999 7 30 99UAL900382 1 19990709 A 2760 4885500901 CONTROL UNIT LEAR ASTRONI 4885500901 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 5 SPOILER FAILED A UALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 29 766UA 00322 26917 NR 5 SPOILER ON THE LEFT WING DOES NOT FULLY RETRACT. MECHANICS FOUND NO COCKPIT INDICATIONS OF A SYSTEM FAILURE OR FAU LT MESSAGES IN THE CMC. REPLACING NR 5 SPOILER PCU DID NOT CORRECT THE PROBLEM. FURTHER TROUBLESHOOTING FOUND ACTUATOR CONTROL ELECTRONICS UNIT (ACE), P/N 488550-09-01, IN THE L2 POSITION TO BE AT FAULT. ACE L2 WAS REPLACED AND ALL TESTS PASSED PER AMM 27-02-02. UAL NOTES LEAR SERVICE BULLETIN 488550-27-02 HAD NOT YET BEEN ACCOMPLISHED ON THIS UNIT. SHO P TESTING AND ENGINEERING ANALYSIS OF THIS ACE FAILURE MODE WILL BE ACCOMPLISHED BY BOEING AND LEAR ASTRONICS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999073000772 19990730 00772 NM 1999 7 30 99UAL900383 1 19990705 A 2820 VENT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT WING TANK DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 7442U 21896 A FUEL TANK ACCESS PLATE WAS INADVERTENTLY LEFT INSIDE THE LEFT HAND WING FUEL TANK. OVER TIME THE LOOSE PLATE DENTED T HE LT WING FUEL VENT TUBES (P/N 65-16708-4,AND 65-16710-124). THE DENTS WERE BEYOND ALLOWABLE LIMITS AND THE VENT REQUI RED REPLACEMENT. LOOSE ACCESS PLATE IN FUEL TANK. LOOSE ACCESS PLATE REMOVED FROM TANK. THE DAMAGED VENT TUBES WERE C UT INTO SECTIONS TO REMOVE THE DAMAGE. NEW SECTIONS OF TUBES WERE SPLICED IN DUE TO THE LIMITED ACCESS INSIDE THE WING. THIS REPAIR WAS APPROVED BY BOEING'S DER WITH AN8110-. 2 L 7 3 4F 4 F A3WE E2EA 1999073000773 19990730 00773 NM 1999 7 30 99UAL900384 1 19990701 A 5712 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 760 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7442U 21896 A CRACKED FASTENER HOLE WAS FOUND IN THE RBBL 70.5 WING RIB UPPER CHORD AT BS 760,WL 198, DURING ACCOMPLISHMENT OF BOEIN G SB 727-57-112, RBBL 70.5 PLUS CHORD PREVENTATIVE MODIFICATION. A REPAIR WAS ACCOMPLISHED PER A DEVIATION TO BOEING SB 727-57-112. THE AREA IS SUJECT TO AD'S 94-07-08, 90-06-09 AND 98-11-03. THE REPAIR WAS APPROVED AS AN AMOC TO AD'S 94 -07-08, AD90-06-09 AND COMPLIANCE TO AD98-11-03. R1 BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000774 19990730 00774 NM 1999 7 30 99UAL900385 1 19990701 A 5310 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 780.95 ELONGATED HOLES A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7442U 21896 EL0NGATED HOLES WERE FOUND AT APPROXIMATELY LBBL 70,5,WL 208 TO 214, BS 780.95 FUSELAGE SKIN, FRAME (P/N 85-16325-81) AN D FRAME STRAP (P/N 65-16325-103). THE ELONGATED HOLES WERE OVERSIZED TO A CLEAN AND ROUND CONDITION. FREEZE PLUGS WERE THEN INSTALLED AND HOLES CORRECTLY LOCATED. INSTALLATION OF LT 70.5 CHORD PREVENTATIVE MOD KIT PER SB 727-57-0112 WAS THEN COMPLETED. AREA IS SUBJECT TO AD'S 94-07-08, 90-06-09 AND 98-11-03. THE REPAIR WAS APPROVED AS AN AMOC TO AD94-07 -08, AD90-05-09 AND COMPLIANCE T0 AD98-11-03 R1 BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000775 19990730 00775 NM 1999 7 30 99UAL900386 1 19990701 A 5712 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 760 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7447U 21901 TWO CRACKED FASTENER HOLES AT BS 760, WL 200 AT WING LBBL 70.5 RIB UPPER CHORD VERTICAL FLANGE WERE FOUND. ONE FASTENER HOLE WAS TRIMMED OUT AND REPAIRED WITH A FILLER, WHILE THE OTHER HOLE WAS REPAIRED WITH A FREEZE PLUG. INSTALLATION OF LT 70.5 CHORD PREVENTATIVE MOD KIT PER SB 727-57-0112 WAS THEN COMPLETED. AREA IS SUBJECT TO AD'S 94-07-08,90-06-09 AN D 98-11-03. THE REPAIR WAS APPROVED AS AN AMOC TO AD04-07-08,AD-90-06-09 AND COMPLIANCE TO AD98-11-03 R1 BY BOEING'S DE R WITH AN B110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000776 19990730 00776 NM 1999 7 30 99UAL900387 1 19990720 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1050 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7451U 21905 CORROSION DAMAGE WAS FOUND ON THE STATION 1050 FLOORBEAM UPPER FLANGE AT RRL 30. THE RESULTING BLENDOUT WENT BEYOND ALL OWABLE LIMITS FOR MATERIAL REMOVAL. THE CORROSION WAS REMOVED BY BLENDING AND A REPAIR STRAP INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999073000777 19990730 00777 WP 1999 7 30 ABXA9900603 1 19990726 A 5730 57695005 SKIN DOUG DOUG DC8 DC863 302198A WP WS 404 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 RIGHT WING LEADING EDGE LOWER SKIN CRACKED AT STATION XW-404. REPAIRED IAW ABX REA D857-31905MR. 2 L 7 4 4F 4A25 1999073000778 19990730 00778 WP 1999 7 30 ABXA9900604 1 19990726 A 5542 565507769 SKIN DOUG DOUG DC8 DC863 302198A WP RUDDER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 LEFT LOWER RUDDER SKIN CRACKED. REPAIRED IAW ABX REA D827-31901. 2 L 7 4 4F 4A25 1999073000779 19990730 00779 WP 1999 7 30 ABXA9900605 1 19990625 A 5755 5910055515 SKIN DOUG DOUG DC9 DC932 3022066 WP LT SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 80825 47364 DURING C-CHECK, LEFT SPOILER ASSY WAS FOUND DELAMINATED IN AREA 12 BY 8 UPPER AND LOWER SKINS. REPLACED UNIT AND REPAIR ED SPOILER ASSY IAW DC9 SRM. 2 L 7 2 4F A6WE 1999073000780 19990730 00780 WP 1999 7 30 MWEA99423 1 19990726 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP GALLEY DOORWAY DISCONNECTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 GALLEY DOOR SLIDE PACK COVER NEEDS TO BE REINSTALLED. REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999073000781 19990730 00781 WP 1999 7 30 MWEA99424 1 19990722 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP GALLEY DOORWAY DISCONNECTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 GALLEY DOOR SLIDE COVER FELL OFF, REINSTALLED. 2 L 7 2 4F A6WE 1999073000782 19990730 00782 WP 1999 7 30 MWEA99425 1 19990721 A 2560 113317 SLIDE DOUG DC9 DC915 3022036 WP GALLEY DOORWAY DISCONNECTED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 300ME 45718 GALLEY DOOR SLIDE COVER POPPED OFF. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1999073000783 19990730 00783 WP 1999 7 30 MWEA99426 1 19990724 A 2560 113317 GIRT BAR DOUG DC9 DC932 3022066 WP GALLEY DOOR DISCONNECTED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 502ME 48132 GALLEY DOOR EMERGENCY SLIDE GIRT BAR CABLE DISCONNECTED. RECONNECTED GIRT BAR PIN. 2 L 7 2 4F A6WE 1999073000784 19990730 00784 WP 1999 7 30 MWEA99427 1 19990727 A 5330 59114011 SKIN DOUG DC9 DC914 3022034 WP GALLEY DOORWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FUSELAGE SKIN UNDER FORWARD GALLEY DOOR SCUFF PLATE HAS SEVERAL AREAS OF LIGHT CORROSION AROUND FASTENER HOLES. BLENDED CORROSION FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999073000785 19990730 00785 WP 1999 7 30 MWEA99428 1 19990727 A 5330 59114013 SKIN DOUG DC9 DC914 3022034 WP BS 135 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DENT IN FUSELAGE SKIN AT STATION 135, 49L. COLD WORKED DENT FABRICATED AND INSTALLED INTERNAL DOUBLER. 2 L 7 2 4F A6WE 1999073000786 19990730 00786 WP 1999 7 30 MWEA99429 1 19990727 A 5320 591141911 DOUBLER DOUG DC9 DC914 3022034 WP BS 642-661 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FINGER DOUBLER CRACKED ON BOTTOM SIDE OF LONGERON 15L BETWEEN FRAME STATION 642 AND 661 LEFT HAND. REMOVED DAMAGED SECT ION OF DOUBLER FABRICATED AND INSTALLED NEW SECTION OF FINGER DOUBLER. 2 L 7 2 4F A6WE 1999073000787 19990730 00787 WP 1999 7 30 MWEA99430 1 19990727 A 5311 59125251 FRAME DOUG DC9 DC914 3022034 WP BS 737 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 STATION 737 FRAME IS CRACKED AT LONGERON 17L FORWARD SIDE. FABRICATED AND INSTALLED REPAIR SPLICES AND ANGLE. 2 L 7 2 4F A6WE 1999073000788 19990730 00788 WP 1999 7 30 MWEA99431 1 19990727 A 5320 9919402506N TRAP PANEL DOUG DC9 DC914 3022034 WP RT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 RIGHT MAIN LANDING GEAR FORWARD TRAPEZODIAL PANEL IS CRACKED BETWEEN 5TH AND 6TH FASTENER HOLES. REMOVED CRACKED PANEL INSTALLED NEW TRAPEZOIDAL PANEL AND STRAP. 2 L 7 2 4F A6WE 1999073000789 19990730 00789 WP 1999 7 30 MWEA99432 1 19990727 A 5311 9911538508N FRAME DOUG DC9 DC914 3022034 WP BS 604 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 CRACK ON FITTING STATION 604 FRAME IN RIGHT WHEEL WELL. INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 1999073000790 19990730 00790 WP 1999 7 30 MWEA99433 1 19990727 A 5241 5913184501 PAN DOUG DC9 DC914 3022034 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 GALLEY SERVICE DOOR PAN HAS ABOUT A ONE INCH CRACK AT THE LOWER SIDE OF THE LOWER DOOR HINGE GOING INTO THE DOOR STOP MO UNT HOLE. REMOVED CRACKED PAN. INSTALLED NEW PAN. 2 L 7 2 4F A6WE 1999073000791 19990730 00791 WP 1999 7 30 MWEA99434 1 19990727 A 5320 99155763 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 680-699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 CRACKED INTERCOSTAL LONGERON 1 STATION 680-699. FABRICATED AND INSTALLED INTERCOSTAL REPAIR. 2 L 7 2 4F A6WE 1999073000792 19990730 00792 WP 1999 7 30 MWEA99435 1 19990727 A 5511 5918000502 SPAR CAP DOUG DC9 DC914 3022034 WP LT HORIZ STAB ELONGATED HOLES A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 UPPER AFT SPAR CAP ON THE LEFT HORIZONTAL STABILIZER HAS MANY ELONGATED HOLES ON THE INBOARD END. INSTALLED NEW SPAR CA P. 2 L 7 2 4F A6WE 1999073000793 19990730 00793 WP 1999 7 30 MWEA99436 1 19990727 A 5313 59142582N LONGERON DOUG DC9 DC914 3022034 WP BS 615 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 RIGHT LONGERON 20 AT STATION 615 HAS 2 CRACK RUNNING FORE AND AFT. REMOVED CRACKED LONGERON INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 1999073000794 19990730 00794 NM 1999 7 30 MWEA99437 1 19990724 A 2560 D29985107 GIRT BAR DOUG MD88 MD88 3023688 NM SERVICE DOOR STUCK A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 AFT GALLEY SERVICE DOOR GIRT BAR DIFFICULT TO DISARM DUE TO SLIDE MATERIAL STUCK BETWEEN GIRT BAR AND GALLEY FLOOR. REP OSITIONED GIRT BAR AND SLIDE. 2 L 7 2 4F RT A6WE 1999073000795 19990730 00795 NM 1999 7 30 MWEA99438 1 19990719 A 5754 5930496508 VANE DOUG MD88 MD88 3023688 NM RT LE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 THE RIGHT WING LEADING EDGE OF FLAP VANE IS HEAVILY CHAFFE. MAINTENANCE FABRICATED AND INSTALLED REPAIR CORE PLUG. 2 L 7 2 4F RT A6WE 1999073000796 19990730 00796 NM 1999 7 30 MWEA99439 1 19990719 A 5730 5922533504 SKIN DOUG MD88 MD88 3023688 NM RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 RIGHT WING NR 3 SLAT BACK SIDE TOP SHEARED FASTENER HAS 2 CRACKS. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 1999073000797 19990730 00797 WP 1999 7 30 MWEA99440 1 19990723 A 5347 593056675 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1041 & 1060 OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 SEAT TRACK NR 2 AT STATION 1041 AND 1060 ARE BLENDED OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 1999073000798 19990730 00798 WP 1999 7 30 MWEA99441 1 19990723 A 5347 593054768 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 503 OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 SEAT TRACK NR 3 LUG AT STATION 503 IS BLENDED OUT OF LIMITS. MAINTENANCE INSTALLED PLUG REPAIR. 2 L 7 2 4F A6WE 1999073000799 19990730 00799 WP 1999 7 30 MWEA99442 1 19990723 A 5330 591145884 SKIN DOUG DC9 DC982 3022082 WP BS 1350 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 HOLE IN SKIN AT STATION 1350 BETWEEN LONGERON 11R AND 23R. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999073000800 19990730 00800 WP 1999 7 30 MWEA99443 1 19990723 A 5311 991960431 FRAME DOUG DC9 DC982 3022082 WP BS 1250 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 THE AFT PART OF FRAME AT STATION 1250 NEAR LONGERON 30 IS CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 1999073000801 19990730 00801 WP 1999 7 30 MWEA99444 1 19990723 A 5753 99575771 SKIN DOUG DC9 DC982 3022082 WP LT TE FLAP GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 LEFT FLAP UPPER SKIN IS GOUGED ON TRAILING EDGE. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999073000802 19990730 00802 WP 1999 7 30 MWEA99445 1 19990727 A 5101 59360311 STRUCTURE DOUG DC9 DC981 3022081 WP LEFT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 AIRCRAFT SUSTAINED FIRE DAMAGE WHILE IN PAINT SHOP DAMAGE IS ON LEFT SIDE FUSELAGE WINDOW BELT OVER WING AREA. REMOVED AND REPLACED WINDOW BELT PANEL, SKIN PANEL, EMERGENCY EXIT DOOR SKIN PANELS, WING TRAILING EDGE PANEL AND WING TO FUSELA GE FILLET PANEL PER DOUGLAS DRAWINGS. 2 L 7 2 4F A6WE 1999073000803 19990730 00803 1999 7 30 MWEA99446 4 19990728 A 2565 13621224 SLIDE DOUG DC9 DC932 3022066 WP ACCESSORY COMPT NO PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT ACCESSORY COMP EVACUATION SLIDE PRESSURE READS 0. REMOVED AND REPLACED AFT EVACAUTION SLIDE. 2 L 7 2 4F A6WE 1999073000804 19990730 00804 WP 1999 7 30 MWEA99447 1 19990728 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 AFT EMERGENCY EXIT SIGNS ARE INOP. REMOVED AND REPLACED BATTERIES. 2 L 7 2 4F A6WE 1999073000805 19990730 00805 NM 1999 7 30 SCNA99097 1 19990723 A 3350 LIGHT BOEING 727 7272K3 138400D NM LT EMER EXIT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 DURING A LINE MAINTENANCE CHECK, THE AFT LEFT OVERWING INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND INOPERATIVE. A WIRE WAS FOUND DISCONNECTED BEHIND THE INTERIOR DECORATIVE PANEL. THE WIRES WERE RESECURED AND SYSTEM OPERATIONALLY CHE CKS GOOD. 2 L 7 3 4F RT A3WE 1999073000806 19990730 00806 WP 1999 7 30 IXXA9900016 1 19990722 A 3220 DOOR DOUG DC8 DC863F 302198F WP NLG INOP A IXXA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 GL 23 784AL 73152 1968 46135 DURING CLIMB FROM RIC TOTOL, A MINOR VIBRATION WAS FELT IN THE NOSE GEAR AREA. THE FLIGHT CREW PERFORMED A SUCCESSFUL G EAR UPLATCH CHECK, THEN CYCLED THE THE GEAR WITH NO CHANGE IN VIBRATION. THE FLIGHT RETURNED TO RIC FOR AN UNEVENTFUL L ANDING. MAINTENANCE INSPECT THE LANDING GEAR WHICH REVEALED THE RIGHT FORWARD NOSE GEAR DOOR OPEN. MAINTENANCE CLEANED AND LUBRICATED THE LINKAGES AND SECURED THE DOOR. 2 L 7 4 4F 4A25 1999073000807 19990730 00807 WP 1999 7 30 ABXA9900582 1 19990619 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 372.750. REPAIRED IAW SRM 51-1-20D AND 57-2-0. 2 L 7 4 4F 4A25 1999073000808 19990730 00808 WP 1999 7 30 ABXA9900583 1 19990619 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE RIB AT STATION XS 484.895 CRACKED AT AFT END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K05056. 2 L 7 4 4F 4A25 1999073000809 19990730 00809 WP 1999 7 30 ABXA9900584 1 19990619 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE RIB CRACKED AT STATION XS 497.491, UPPER, AFT END. REPAIRED IAW DC8 SRM 57-20-0 AND DWG K05056 . 2 L 7 4 4F 4A25 1999073000810 19990730 00810 WP 1999 7 30 ABXA9900585 1 19990619 A 5313 2184971 FITTING DOUG DOUG DC8 DC863 302198A WP FS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FITTING CRACKED AT STATION 1180 AND LONGERONS 34 LEFT TO 35 LEFT. REPAIRED IAW DC8 SRM 51-1-20D AND 53-2-0. 2 L 7 4 4F 4A25 1999073000811 19990730 00811 WP 1999 7 30 ABXA9900586 1 19990620 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE RIB AT STATION XFS 847.5 CRACKED AT LOWER AFT END. REPAIRED IAW DC8 SRM 57-3-1, 51-1-20D AND D WG 5769545. 2 L 7 4 4F 4A25 1999073000812 19990730 00812 WP 1999 7 30 ABXA9900587 1 19990714 A 5313 59248053 LONGERON DOUG DOUG DC9 DC941 302207N WP FS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 LONGERON 4 LEFT CRACKED AT STATION 737. REPAIRED IAW DC9 SRM 53-02-0. 2 L 7 2 4F A6WE 1999073000813 19990730 00813 WP 1999 7 30 99FDEA00269 1 19990503 A 5314 AEA0161 WEB DOUG DC10 DC1010 3022110 WP KEEL BEAM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 DUR A/C P-F CONV AT AERONAVALI, 3 10' CRACKS WERE FOUND AT Y=1386 COMMON TO KEEL WEB, WEB DOUBLER & AEA0501 KEEL WEB UPP ER SPLICE. REPAIRED KEEL WEB AND WEB DOUBLER PER IAW FEDEX EA NR 8-5314-44061. 2 L 7 3 4F A22WE 1999073000817 19990730 00817 WP 1999 7 30 99FDEA00273 1 19990719 A 5320 CLIP DOUG DC10 DC1030F 3023504 WP BS 1225-1375 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 319FE 47820 SNRM 308,309,310 LT WING TO FUSELAGE UPPER FAIRING SUPPORT RIBS ATTACH CLIP CRACKED AT BS 1225, BS 1289, BS 1300, BS 131 0, BS 1341 AND BS 1375. L/H WING TO SELAGE FARIR BOTTOM SUPT RIBS CRACKED. CARRIED OUT REPAIRS PER AEA 0553, ANB 7140, ANB 7139, AEA 0552, ANB 7101, PER SRM 51-35-01. 2 L 7 3 4F RT A22WE 1999073000818 19990730 00818 NM 1999 7 30 99FDEA00274 1 19990727 A 2120 UNKNOWN BOEING 727 727233 138408A NM COCKPIT ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 285FE 22622 BURNING RUBBER SMELL AND SMOKY HAZE IN COCKPIT. INSPECTED BOTH E/E AND A/C PACK BAYS, AFT AIRSTAIRS, GEAR WELLS, FWD BE LLY SNAKE PIT, CAPT AND F/O INSTRUMENT PANEL, OVERHEAD PEDESTAL, C/B RACKS AND RUDDER PEDAL AREA, CHECKED GASPER FAN OPE RATION. W/APU RUNNING OPERATED BOTH PACKS, RAN ALL 3 ENGINES AND PERFORMED PNEU AND A/C CHECKS. FLT CREW SIMULATED T/O AND CLIMB POWER SETTINGS, NO DEFECTS NOTED. CHECKED AIR PRESSURE FILTER PER M/M. 2 L 7 3 4F RT A3WE 1999073000819 19990730 00819 NM 1999 7 30 99FDEA00275 1 19990721 A 3260 40173 SWITCH BOEING 727 72722 1384002 NM LT MLG FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 167FE 18864 ON APPROACH TO MEM GEAR HANDLE WAS PLACED DOWN BUT ONLY NOSE GEAR AND RT MLG IND DOWN & LOCK. EMERG PROC WERE FOLLOWED, BUT STILL NO DOWN & LOCK ON LEFT MAIN. REMOVED AND REPLACED LT MLG DOWNLOCK SWITCH IAW MM 32-61-021-4. 2 L 7 3 4F A3WE 1999073000820 19990730 00820 SO 1999 7 30 SWIA971522 1 19990707 A 5230 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR LEAKING A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 198SW 120227 LOST CABIN PRESSURIZATION AT APPROXIMATELY 16,000 FT, DEPRESSURIZED TO 10,000. CABIN WOULD NOT PRESSURIZE IN EITHER AUT O OR MANUAL MODE. RETURNED TO SLC. REMOVED AND REPLACED CARGO DOOR SEAL IAW MM 52-30-00. PRESSURIZED AIRCRAFT TO 3 PS ID. LEAK AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999073000821 19990730 00821 1999 7 30 SWIA971523 3 19990705 A 6140 SELOC29DH INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT INOP A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 213SW 120277 RIGHT NP ANALOG GAUGE INOP. RETURNED TO FIELD. REMOVED AND REPLACED NUMBER TWO NP INDICATOR WITH SERVICEABLE UNIT. GR OUND RAN ENGINE AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999073000822 19990730 00822 WP 1999 7 30 9902609750 1 19990709 A 5315 FRAME DOUG DC9 DC941 302207N WP FS 617 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 750NW 47114 DURING PERIODIC CHECK, FOUND FLOORBEAM DAMAGE DUE TO CORRROSION. REPAIRED PER EA 97-164483. 2 L 7 2 4F A6WE 1999073000823 19990730 00823 WP 1999 7 30 9902619984 1 19990630 A 5313 LONGERON 22/23L DOUG DC9 DC932 3022066 WP FS 917 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND LONGERON 22L AND 23L DAMAGED BY CORROSION FS 917. REPAIRED PER EA 99-164450. (P/N 5911473 -99) 2 L 7 2 4F A6WE 1999073000824 19990730 00824 WP 1999 7 30 9902629984 1 19990624 A 5311 T-CAP DOUG DC9 DC932 3022066 WP FS 1046 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND T CAP OF FRAME DAMAGED AT TWO PLACED X=27L AND X=27R. REPAIRED PER EA 99-164428. (P/N 9 911838-5) 2 L 7 2 4F A6WE 1999073000825 19990730 00825 WP 1999 7 30 9902639975 1 19990621 A 5313 INTERCOSTAL DOUG DC9 DC931 3022065 WP FS 154 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 DURING PERIODIC CHECK, FOUND INTERCOSTAL 9911557-3 AT FS 154, LONGERON 14R CRACKED. REPAIRED PER EA 99-164421. 2 L 7 2 4F A6WE 1999073000826 19990730 00826 WP 1999 7 30 9902649984 1 19990618 A 5321 SLANT PANEL DOUG DC9 DC932 3022066 WP FS 700 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND CORROSION AT FS 700 SLANT PANELS. REPAIRED PER EA 99-164419. (P/N 5956065-5) 2 L 7 2 4F A6WE 1999073000827 19990730 00827 WP 1999 7 30 9902659975 1 19990616 A 5210 PAX DOOR DOUG DC9 DC931 3022065 WP FS 160 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 DURING PERIODIC CHECK, FOUND .375 INCH CRACK AT UPPER FORWARD CORNER OF PASSENGER DOOR JAMB, FS 160. REPAIRED PER EA 99 -164408. (P/N 5911406-5). 2 L 7 2 4F A6WE 1999073000828 19990730 00828 WP 1999 7 30 9902669984 1 19990623 A 5713 T/E SKIN DOUG DC9 DC932 3022066 WP RT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND CORROSION DAMAGE TO RIGHT WING TRAILING EDGE UPPER SURFACE STRINGER. REPAIRED PER EA 99-16 4406. (P/N 5912156-164) 2 L 7 2 4F A6WE 1999073000829 19990730 00829 WP 1999 7 30 9902679750 1 19990601 A 5314 KEEL BEAM DOUG DC9 DC941 302207N WP FS 655 - 677 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 750NW 47114 DURING PERIODIC CHECK, FOUND KEEL CORRODED ON LONGERON 30 AT FS 655 - 677. REPAIRED PER EA 97-164365. 2 L 7 2 4F A6WE 1999073000830 19990730 00830 WP 1999 7 30 9902689975 1 19990614 A 5314 INTERCOSTAL DOUG DC9 DC931 3022065 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 DURING PERIODIC CHECK, FOUND .5 INCH CRACK AT INTERCOSTAL 99-15551-11. REPAIRED PER EA 99-164404. 2 L 7 2 4F A6WE 1999073000831 19990730 00831 WP 1999 7 30 9902699750 1 19990630 A 5311 FRAME DOUG DC9 DC941 302207N WP FS 973 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 750NW 47114 DURING PERIODIC CHECK, FOUND HORIZONTAL FLANGE UPPER SECTION OF SUBJECT FRAME DAMAGED AT LONGERON 30. REPAIRED PER EA 9 7-164454. (P/N 9958214-29) 2 L 7 2 4F A6WE 1999073000832 19990730 00832 WP 1999 7 30 9902709984 1 19990702 A 5322 ANGLE DOUG DC9 DC932 3022066 WP BULKHEAD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND CORROSION ON RIGHT LOWER CAP ANGLE 6 INBOARD OF OUTBOARD EDGE OF ANGLE. REPAIRED PER EA 99 -164465. (P/N 5910005-50) 2 L 7 2 4F A6WE 1999073000833 19990730 00833 WP 1999 7 30 9902719913 1 19990706 A 5321 SLAT PRESS PANEL DOUG DC9 DC931 3022065 WP FS 700 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING PERIODIC CHECK, FOUND CORROSION ON LHS SLAT PRESSURE PANEL (P/N 5956065-41) AND RHS (P/N 5956065-43). REPAIRED P ER EA 99-164469. 2 L 7 2 4F A6WE 1999073000834 19990730 00834 WP 1999 7 30 9902729913 1 19990706 A 5320 FASTENER DOUG DC9 DC931 3022065 WP FS 160 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING PERIODIC CHECK, HEAVY CORROSION AND CRACK PROPAGATION AT FASTENER HOLE LOCATIONS APPROXIMATELY 6 SECTION. REPAIR ED PER EA 99-164471. (P/N 9911593-7) 2 L 7 2 4F A6WE 1999073000835 19990730 00835 WP 1999 7 30 9902739984 1 19990616 A 5280 DOOR CHANNEL DOUG DC9 DC932 3022066 WP FS 737 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND MAIN LANDING GEAR DOOR JAMB CHANNEL CRACKED .5 INCH IN THE RADIUS. REPAIRED PER EA PP-1644 01. (P/N 5916154-5) 2 L 7 2 4F A6WE 1999073000836 19990730 00836 NM 1999 7 30 9902742768 1 19990520 A 5312 CHORD BOEING 727 7272M7 138407S NM BULKHEAD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 728RW 21741 DURING M-CHECK, FOUND CORROSION ON THE LOWER CHORD AT AFT PRESSURE BULKHEAD. REPAIRED PER EA 27-166620. 2 L 7 3 4F A3WE 1999073000837 19990730 00837 NM 1999 7 30 9902752768 1 19990520 A 5314 KEEL BEAM BOEING 727 7272M7 138407S NM FS 950 - 1110 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 728RW 21741 DURING M-CHECK, FOUND CORROSION ON THE STRINGERS 29R AND 29L KEEL BEAMS. REPAIRED PER EA 27-166632. (P/N 65-56441) 2 L 7 3 4F A3WE 1999073000838 19990730 00838 NM 1999 7 30 VNAA9907006 1 19990718 A 3240 AC69963 METERING UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BRAKES FAILED A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 425JS 38657 596 3037 CREW REPORTED, DURING TAXI BRAKES PULSATED SO STRONGLY AFTER LANDING THAT THEY WERE USELESS IN STOPPING THE AIRCRAFT. M AINTENANCE INSPECTED AND REPLACED THE BRAKE METERING UNIT. OPERATION CHECKS FAILED AND THE BRAKE METERING UNIT HAD TO B E REPLACED AGAIN. BRAKE METERING UNIT SERIAL NUMBER 0021 WAS BAD FROM STOCK. OPERATION AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999073000839 19990730 00839 NM 1999 7 30 VNAA9907007 1 19990720 A 7900 119B OIL PRESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FLUCTUATES A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 439JS 94544 3057 116123 DURING FLIGHT 4029 TO DCA AN OIL PRESSURE FLUX WAS NOTED BY THE FLIGHT CREW. THE CREW FOLLOWED THE QRH AND FEATHERED TH E RIGHT HAND ENGINE. THE FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. OUTSTATION MAINTENANCE INSPECTED AND SERVICED THE ENGINE OIL, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-11-00. ENGINE RUNS AND LEAK CHECKS WERE C OMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE ENGINE WAS ALSO PLACED ON OUR OIL WATCH PROGRAM. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999081200001 19990812 00001 NE 1999 8 12 ORJA99226 2 19990705 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE STALLED A ORJA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 11 836RA 23102 53046 725596 SFO - RETURN TO SFO DUE TO NR 1 ENGINE COMPRESSOR STALL AT CLIMB POWER AT ABOUT 4,000 FEET. REDUCED POWER AND ENGINE RA N NORMAL EXCEPT FOR HIGHER EGT THAN RIGHT ENGINE FOR GIVEN EPR SETTING. REMOVED AND REPLACED NR 1 ENGINE PER QQ TASK CA RD 0099. OPS AND LEAK CHECK GOOD. PERFORMED HI-POWER TRIM PER MM 71-00-00. ALL PARAMETERS MET. (X) 2 L 7 2 4F 4 F RT A6WE E9NE 1999081200002 19990812 00002 WP 1999 8 12 ORJA99227 1 19990703 A 3244 TIRE 50113361 DOUG DC9 DC983 3022083 WP MLG FAILED A ORJA O OTHER O OTHER TO TAKEOFF 1 WP 11 871RA 49788 LAS - LEFT MAIN TIRES FAILED ON TAKEOFF AT APPROXIMATELY 80 KNOTS. REMOVED AND REPLACED NR 1 AND NR 2 MAIN WHEEL TIRE A SSY PER MM 30-40-01. (X) 2 L 7 2 4F RT A6WE 1999081200003 19990812 00003 WP 1999 8 12 ORJA99215 1 19990702 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 RECHARGE LIGHTS ON FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS NOT BLINKING. REMOVED AND REPLACED BATTERY ASSY. ALL FLIGHT ATTENDANTS FLASHLIGHTS OPS CHECK OK. (X) 2 L 7 2 4F A6WE 1999081200004 19990812 00004 WP 1999 8 12 ORJA99231 1 19990708 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROWS 21-24 OUT OF POSITION A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 SAN - EMERGENCY EXIT LIGHTS ROWS 21-24 CAME ON. CHECKED EMERGENCY LIGHTS AT ROWS 21-24 FOR SECURITY AND CONDITION. REP OSITIONED WIRE AT SEAT 21. OPS CHECKED EMERGENCY LIGHTS, SYS CHECKED NORMAL. (X) 2 L 7 2 4F RT A6WE 1999081200005 19990812 00005 WP 1999 8 12 ORJA99222 1 19990617 A 3350 6011779 POWER PACK DOUG DC9 DC983 3022083 WP ROWS 19,20,21 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 RNO - EMERGENCY LIGHTS ROWS 19, 20, 21 ILLUMINATED. REMOVED AND REPLACED EMERGENCY POWER PACK FOR ROWS 19, 20, 21. OPS CHECK GOOD 33-53-01. (X) 2 L 7 2 4F RT A6WE 1999081200006 19990812 00006 WP 1999 8 12 ORJA99223 1 19990630 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 8-12 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 SJC - EMERGENCY PATH LIGHT ON SEATS 8 THROUGH 12 INOPERABLE. REMOVED AND REPLACED MID-RIGHT HAND BATTERY PACK PER MM 33 -53-01. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999081200007 19990812 00007 WP 1999 8 12 ORJA99224 1 19990707 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP RT EMERG EXIT DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 SJC - FORWARD RIGHT EMERGENCY EXIT LAMP INOPERABLE. REPLACED BATTERY PACK ON FORWARD RIGHT EMERGENCY EXIT. OPS CHECK G OOD. (X) 2 L 7 2 4F RT A6WE 1999081200008 19990812 00008 WP 1999 8 12 ORJA99228 1 19990706 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 21-24 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 LAS - EMERGENCY TRACK LIGHTS AFT SECTION CAME ON INTERMITTENTLY DURING FLIGHT ROWS 21-24. REPLACED BATTERY IAW MM 33-53 -00. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1999081200009 19990812 00009 WP 1999 8 12 ORJA99229 1 19990708 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 21-24 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 RNO - EMERGENCY EXIT LIGHTS ON ROWS 21-24 CAME ON INTERMITTENTLY. REMOVED AND REPLACED LIGHT BATTERY PACK ON AFT RIGHT OVERWING DOOR. OPS CHECK GOOD AT THIS TIME. (X) 2 L 7 2 4F RT A6WE 1999081200010 19990812 00010 WP 1999 8 12 ORJA99221 1 19990627 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 17-20 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 878RA 53184 SNA - EMERGENCY LIGHTS ILLUMINATED ON GROUND AT ROWS 17 THROUGH 20. REMAINED ON FOR APPROXIMATELY 20 MINUTES THEN WENT OFF, CAME ON AGAIN (DIMLY) AFTER LANDING. REPLACED BATTERY PACK AT RIGHT AFT EXIT LIGHT EMERGENCY LIGHTS. OPS CHECK NO RMAL. (X) 2 L 7 2 4F RT A6WE 1999081200011 19990812 00011 WP 1999 8 12 ORJA99220 1 19990608 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 17-21 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 LAX - (ON LANDING LAX) A SEGMENT OF EXIT ROW LIGHTING FROM SEATS 17D TO 21D ILLUMINATED. WILL NOT TURN OFF. REMOVED AN D REPLACED EMERGENCY BATTERY PACK AT 21F IAW MM 33-53-01. (X) 2 L 7 2 4F RT A6WE 1999081200012 19990812 00012 NM 1999 8 12 ORJA99219 1 19990625 A 3350 60030451 BATTERY PACK DOUG MD90 MD9030 3023690 NM CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 903RA 53551 SJC - FIRST CLASS CABIN EMERGENCY EXIT FLOOR LAMP INOPERATIVE. FOUND SHORT BULB AT 4DEF WHICH BLEW A FUSE AT BATTERY PA CK B5-240. REMOVED AND REPLACED BULB AND BATTERY PACK IAW MM 33. E.PAN LIGHTNING OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999081200013 19990812 00013 WP 1999 8 12 ORJA99218 1 19990710 A 3350 60030451 POWER PACK DOUG DC9 DC987 3022087 WP ROWS 19-22 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 E-LIGHTS INOPERABLE, ROWS 19-22. REMOVED AND REPLACED E-POWER PACK FOR ROWS 19-22. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999081200014 19990812 00014 WP 1999 8 12 ORJA99217 1 19990706 A 3350 110049 POWER SUPPLY DOUG DC9 DC987 3022087 WP ROWS 27-29 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY LIGHTS AT ROWS 27-29 ON IN-FLIGHT. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY AT LEFT EMERGENCY EXIT PER MM 25-50-04. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999081200015 19990812 00015 WP 1999 8 12 ORJA99216 1 19990704 A 3350 110049 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 SEVERAL EMERGENCY LIGHTS OUT IN AFT CABIN. CHANGED POWER SUPPLY 33-53-00. OPS CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999081200016 19990812 00016 WP 1999 8 12 ORJA99230 1 19990701 A 3350 110049 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 RNO - SEVERAL EMERGENCY LIGHTS OUT IN AFT CABIN. CHANGED POWER SUPPLY 33-53-00. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1999081200017 19990812 00017 CE 1999 8 12 MASA99118 1 19990712 A 5270 WARNING BEECH 1900 1900D 1154162 CE PASSENGER DOOR ACTIVATED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 93ZV UE93 PHX/YUM - FLT 6389- THE AIRCRAFT IN CRUISE WHEN THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND LANDED IN YUM WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION WAS DEFERRED PER MEL 52-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999081200018 19990812 00018 NE 1999 8 12 MASA99117 2 19990710 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FAILED A MASA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 124YV UE124 114014GG IAD/SYR - FLT 5299 - RIGHT ENGINE OIL PSI DROPPED IN-FLIGHT. THE CREW DECLARED AN EMERGENCY AND DIVERTED ITH. THE AIRC RAFT LANDED WTHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE. OPS CHECK GOOD. THE AIRCRAFT RETU RNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200019 19990812 00019 NE 1999 8 12 MASA99108 2 19990628 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 112ZV UE112 114264 ROW/DFW - FLT 1030 - AIRCRAFT WAS ON CLIMB-OUT WHEN THE RIGHT ENGINE TORQUE AND OIL PRESSURE DECREASED AND THE OIL TEMPE RATURE INCREASED. THE CAPTAIN REDUCED POWER ON THE RIGHT ENGINE, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS RETURNE D TO THE FIELD. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE AND PROPELLER. TEAR-DOWN INFORMATION WILL BE FORTHCO MING. (X) 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200020 19990812 00020 EA 1999 8 12 MASA99106 1 19990627 A 3260 864202 SWITCH 601R8500237 CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJUST A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 77260 7260 PHX/MRY - FLT 6138 - THE AIRCRAFT WAS AIRBORNE WHEN THE GEAR WAS SELECTED UP. THE CREW RECEIVED A NOSE GEAR ASSY AND A NOSE GEAR DOOR DISAGREE MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. MAINTENANCE TROUBLESHOT FOUN D THE NOSE GEAR PROXIMITY SWITCH WAS OUT OF RIG. RE-RIGGED THE SWITCH AND PERFORMED A GEAR SWING. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999081200021 19990812 00021 EA 1999 8 12 MASA99113 1 19990702 A 5210 601R31911302 STRUT 601R31902469 CNDAIR CL600 CL6002B19 EA CABIN DOOR MISALIGNED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 17156 7156 RDU/BOS - FLT 5215 - THE CAPTAIN REPORTED DAMAGE TO CABIN DOOR INNER SKIN, DUE TO MISALIGNED STRUT. MAINTENANCE WAS ABL E TO SECURE DOOR CLOSED AND THE AIRCRAFT FERRIED TO BHM WHERE A PERMANENT REPAIR WAS PERFORMED. OPS CHECK GOOD. THE AI RCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999081200022 19990812 00022 EA 1999 8 12 MASA99112 1 19990701 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA AIRSTAIR DOOR LACK OF LUBE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 47202 7202 PHL/MKE - FLT 5809 - THE CAPTAIN REPORTED A STICKY AIRSTAIR DOOR. MAINTENANCE WAS SENT TO INVESTIGATE AND REPORTED NO D ISCREPANCIES, LUBED THE DOOR. FUNCTION CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999081200023 19990812 00023 NE 1999 8 12 MASA99105 2 19990625 A 7320 324485316 COMPUTER DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 2 ENGINE FAILED A MASA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 07 444YV 444 TM123333 PHX/TEX - FLT 6360 - IN-FLIGHT, THE AIRCRAFT LOST TORQUE IN THE NR 2 ENGINE. THE CREW SHUT THE ENGINE DOWN AND DECLARED AN EMERGENCY. THE AIRCRAFT WAS RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE M FC. OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200024 19990812 00024 NM 1999 8 12 99ZZZX2824 1 19990716 A 5753 6519270XX TRACK BOEING 727 727225 1384077 NM TE FLAP CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 LOG PAGE 25775. DURING INSPECTION OF AREA DUE TO REMOVAL OF FLAP FOR GROUND DAMAGE, FOUND SHIMS MIGRATED ON PAD A. REM OVED TRACK TO REPLACE. REMOVED AND REPLACED SHIMS AND NR 4 FLAP TRACK IAW BOEING SB 727-57-0178 REV 5. (X) 2 L 7 3 4F A3WE 1999081200025 19990812 00025 NE 1999 8 12 GAIA99102 2 19990721 A 7532 12355814 BLEED VALVE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE INOPERATIVE A GAIA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 07 855AA 20996 FLT 721 DURING CLIMB-OUT FROM AUS THROUGH FL 250, THE NR 3 ENGINE STRUT OVERHEAT ILLUMINATED FOLLOWED SHORTLY BY THE NR 3 ENGINE BLEED TRIP AND THE LOWER AFT BODY OVERHEAT LIGHT. THE FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO DFW. T HE AIRCRAFT LANDED SAFELY WITHOUT FURTHER DIFFICULTIES. REPOSITIONED AND RETORQUED SEVERAL 8TH AND 13TH STAGE DUCT CLAM PS. REPLACED THE 8TH STAGE CHECK VALVE AND THE NR 3 BLEED VALVE. OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RETURNED T O SERVICE. REF: OPER CNTRL NR 99ZZZX2825. (X) 2 L 7 3 4F 4 F A3WE E2EA 1999081200026 19990812 00026 NE 1999 8 12 99ZZZX2825 2 19990721 A 7532 32146421 BLEED VALVE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE INOPERATIVE A GAIA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 07 855AA 20996 FLT 721 DURING CLIMB-OUT FROM AUS THROUGH FL 250, THE NR 3 ENGINE STRUT OVERHEAT ILLUMINATED FOLLOWED SHORTLY BY THE NR 3 ENGINE BLEED TRIP AND THE LOWER AFT BODY OVERHEAT LIGHT. THE FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO DFW. T HE AIRCRAFT LANDED SAFELY WITHOUT FURTHER DIFFICULTIES. REPOSITIONED AND RETORQUED SEVERAL 8TH AND 13TH STAGE DUCT CLAM PS. REPLACED THE 8TH STAGE CHECK VALVE AND THE NR 3 BLEED VALVE. OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RETURNED T O SERVICE. REF: OPER CNTRL NR GAIA99102. 2 L 7 3 4F 4 F A3WE E2EA 1999081200027 19990812 00027 NM 1999 8 12 GAIA99105 1 19990722 A 5330 SKIN BOEING 727 727223 1384074 NM NOSE SECTION CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6838 20191 DURING A 'ZERO' LIGHT 'C' INSPECTION BEING PERFORMED IN OSC AT AMERICAN INTERNATIONAL AIRWAYS REPAIR STATION, A CRACK WA S FOUND IN FUSELAGE SKIN AT UPPER AFT CORNER OF R5 WINDOW. REPAIRED IAW AIA EDR B2-06523, BOEING REPAIR SKETCH CKFR9905 07, FIGURES 1 AND 2. DER APPROVED ON 8110-3 DATED MAY 18, 1999. (X) 2 L 7 3 4F A3WE 1999081200028 19990812 00028 NM 1999 8 12 GAIA99107 1 19990722 A 5511 RIB BOEING 727 727223 1384074 NM LT HORIZ STAB CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6838 20191 DURING A 'ZERO' LIGHT 'C' INSPECTION BEING PERFORMED IN OSC AT AMERICAN INTERNATIONAL AIRWAYS REPAIR STATION, A CRACK WA S DETECTED ON THE LEFT HORIZONTAL STABILIZER AFT UPPER CLOSURE RIB CHORD. REPAIRED IAW AIA EDR B2-06525 AND BOEING SB 7 27-55-81. DER APPROVED ON 8110-3 DATED MAY 17, 1999. (X) 2 L 7 3 4F A3WE 1999081200029 19990812 00029 NM 1999 8 12 TSAA9921300 1 19990706 A 2130 7207375 RELIEF VALVE BOEING 737 7372Y5 1384554 NM CABIN FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 810AL 24031 HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED, BUT DIDN' T CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECK OK. REMOVED AND REPLACED LOWER PRESSURE RELIEF VALVE IAW 21-32-20 FOR PRECAUTI ONARY. AIRCRAFT RETURNED TO SERVICE. PRESSURE RELIEF VALVE INSTALLATION SUSPECT. CPC TESTED GOOD. MONITORED A/C, NO PROBLEMS. 2 L 7 2 4U RT A16WE 1999081200030 19990812 00030 NM 1999 8 12 TSAA9933299 1 19990715 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 AND NR 6 FLOOR PROXIMITY LIGHT BATTERY PACK ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO S ERVICE. (X) 2 L 7 2 4F RT A16WE 1999081200031 19990812 00031 NM 1999 8 12 99ZZZX2826 1 19990723 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 45319 23257 DEN - DURING C-CHECK INSPECTION, REPORTED 1 INCH CRACK IN FLOOR INTERCOSTAL WEB, BS 178, WL 207, RBL 19.0. MAINTENANCE FABRICATED DOUBLER AND REPAIRED PER SRM 51-70-13 AND SRM 53-10-08. (X) 2 L 7 2 4F RT A16WE 1999081200032 19990812 00032 WP 1999 8 12 USAA990720 1 19990711 A 5240 49157601 LATCH DOUG DC9 DC981 3022081 WP SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 828US 49635 48028 PIT - LGA MAINTENANCE FOUND .50 INCH CRACK AT SERVICE DOOR (RT SIDE) HOLD OPEN CUP. REPLACED WITH LIKE PART PER EA 5241 8A. (X) 2 L 7 2 4F A6WE 1999081200033 19990812 00033 NM 1999 8 12 USAASB99170 1 19990713 A 7711 LG80A6 EPR TRANSMITTER BOEING 737 7372B7 1384560 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 272AU 35070 22884 CLE - FLT 8027 - APPROXIMATELY 7 MINUTES AFTER TAKEOFF, CREW ENCOUNTERED PROBLEMS WITH THE NR 2 ENGINE EPR AND THE AUTOT HROTTLE DISCONNECTING. WITH FUEL FLOW AT 5.3, NR 1 ENGINE EPR WAS AT 1.78 AND THE NR 2 ENGINE AT 1.41. WHEN AUTOTHROTT LE WAS RE-ENGAGED, THE NR 2 THRUST LEVER GOES TO FIREWALL TO MATCH EPR'S. FLIGHT RETURNED TO FIELD AT CLE AND LANDED WI THOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE EPR TRANSMITTER PE R MM 77-11-21. PERFORMED ENGINE RUN. OPERATIONAL CHECK AND LEAK CHECK GOOD. PERFORMED AUTOTHROTTLE BITE TEST. TESTED NORMAL. (X) 2 L 7 2 4F A16WE 1999081200034 19990812 00034 NE 1999 8 12 USAASB99174 2 19990714 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE RIGHT FAILED A USAA A UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 EA 19 283AU 40522 23116 709061 RDU - FLT 2695 - APPROXIMATELY 60 MILES SOUTH OF ORF AT FL 350, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND START ED TO LOSE POWER. AIRFRAME VIBRATION WAS ALSO NOTED. CREW BROUGHT THROTTLE BACK AND RESTORED PARTIAL ENGINE POWER. FL IGHT DIVERTED TO RDU AND LANDED WITHOUT FURTHER INCIDENT. NO ENGINE SHUT DOWN OCCURRED, BUT AN EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED THE NR 2 ENGINE INTAKE AND EXHAUST. RAN ENGINE TO TAKEOFF POWER. COULD NOT DUPLICATE ON GROUND RUN. AIRCRAFT WAS MAINTENANCE FERRIED TO CLT WHERE THE NR 2 ENGINE ASSY WAS REMOVED AND REPLACED PER JOB CARD. OPERATI ONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F A16WE E2EA 1999081200035 19990812 00035 NM 1999 8 12 USAASB99168 1 19990711 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 278AU 22890 CLE - PILOT REPORTED THE OVERWING AND FORWARD GALLEY EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH SWITCH IN ARMED POSITION . WITH SWITCH OFF, ALL LIGHTS EXTINGUISHED. SWITCHING LIGHTS BACK ON, FORWARD GALLEY EEMERGENCY LIGHTS WOULD NOT ILLUM INATE. MAINTENANCE RESET THE EMERGENCY EXIT LIGHT CONTROL BREAKER AND REMOVED AND REPLACED THE R2 EMERGENCY LIGHT BATTE RY PACK. GROUND OPERATIONAL CHECK NOW NORMAL. (X) 2 L 7 2 4F A16WE 1999081200036 19990812 00036 NM 1999 8 12 USAASB99173 1 19990715 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM EMERGENCY EXIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AU 22795 CLE - PILOT REPORTED THE EMERGENCY EXIT LIGHT OVER THE FORWARD GALLEY DOOR ILLUMINATED WITH THE EMERGENCY EXIT SWITCH OF F AND GROUND SERVICE POWER ON. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY OVER THE FORWARD GALLEY DOOR. OPER ATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1999081200037 19990812 00037 WP 1999 8 12 ARWA990703 1 19990725 A 2133 OUTFLOW VALVE DOUG DC8 DC862 3021970 WP CABIN LACK OF LUBE A ARWA A J UNSCHED LANDING DUMP FUEL O OTHER TO TAKEOFF 1 SO 19 1804 45896 MIA - FLT 627 - UNABLE TO PRESSURIZE AIRCRAFT IN AUTO OR MANUAL DURING TAKEOFF. DUMPED FUEL AND RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT INVESTIGATED FOR DEFECTS. PRESSURIZATION NORMAL IAW MM 21-30-00. LUBED OUTFLOW VALVE AS PRECAUTIO NARY. CHECKED NORMAL PER MM 21-30-00. (X) 2 L 7 4 4F 4A25 1999081200038 19990812 00038 NM 1999 8 12 USAASB99165 1 19990706 A 2131 7638101 CONTROLLER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 426US 24548 DCA - FLT 2055 - UPON CLIMB-OUT FROM DCA AT APPROXIMATELY 12,000 FEET, THE CABIN ALTITUDE WARNING SOUNDED. CABIN WAS CL IMBING 2,000 FEET PER MINUTE CLIMBING THROUGH FL 180 TO FL 190. CREW SWITCHED OVER TO STANDBY SYSTEM AND DESCENDED. OX YGEN MASKS DROPPED AND OXYGEN GENERATORS WERE ACTIVATED. FLIGHT RETURNED TO FIELD AT DCA. NO EMERGENCY DECLARED. MAIN T PERFORMED OPERATION TEST OF PRESSURIZATION SYSTEM PER MM 21-31-00 AND FOUND NO FAULTS. REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER (P/N 763810-1) AND PRESSURIZATION CONTROL PANEL (P/N 711002-5) AS PRECAUTIONARY. ALSO, REMOVED AND REPLACED OXYGEN MASKS AT ALL STATIONS AND OXYGEN GENERATORS THAT WERE ACTIVATED. REF: OPER CNTRL NR 99ZZZX2827. (X) 2 L 7 2 4F RT A16WE 1999081200039 19990812 00039 NM 1999 8 12 99ZZZX2827 1 19990706 A 2130 7110025 CONTROL PANEL BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 426US 24548 DCA - FLT 2055 - UPON CLIMB-OUT FROM DCA AT APPROXIMATELY 12,000 FEET, THE CABIN ALTITUDE WARNING SOUNDED. CABIN WAS CL IMBING 2,000 FEET PER MINUTE CLIMBING THROUGH FL 180 TO FL 190. CREW SWITCHED OVER TO STANDBY SYSTEM AND DESCENDED. OX YGEN MASKS DROPPED AND OXYGEN GENERATORS WERE ACTIVATED. FLIGHT RETURNED TO FIELD AT DCA. NO EMERGENCY DECLARED. MAIN T PERFORMED OPERATION TEST OF PRESSURIZATION SYSTEM PER MM 21-31-00 AND FOUND NO FAULTS. REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER (P/N 763810-1) AND PRESSURIZATION CONTROL PANEL (P/N 711002-5) AS PRECAUTIONARY. ALSO, REMOVED AND REPLACED OXYGEN MASKS AT ALL STATIONS AND OXYGEN GENERATORS THAT WERE ACTIVATED. REF: OPER CNTRL NR USAASB99165. 2 L 7 2 4F RT A16WE 1999081200040 19990812 00040 NM 1999 8 12 USAASB99155 1 19990626 A 2913 6507506 PUMP BOEING 737 737401 1384701 NM NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 406US 35184 13193 23876 PIT - FLT 268 - APPROXIMATELY 30 MILES OUT FROM PIT, THE FLIGHT LOST SYSTEM A-HYDRAULIC QUANTITY. CREW SHUT OFF SYSTEM 'A' ELECTRIC HYDRAULIC PUMP AND FOLLOWED PROCEDURES. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDEN T. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED HYDRAULIC PUMP, FILTERS, AND FLUSHED SYSTEM. SERVICED HYDRAULIC RESERVOIR . OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999081200041 19990812 00041 WP 1999 8 12 USAAD99094 1 19990711 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP RT LAVATORY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 IND - THE TAILCONE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE ACTIVATED EMERGENCY LIG HT BATTERY. (X) 2 L 7 2 4F A6WE 1999081200042 19990812 00042 NE 1999 8 12 USAABB035 2 19990712 A 7200 ENGINE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE RIGHT FAILED A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 617AU 21461 27148 030906 CLT/BOS - FLT 1224 - EN ROUTE, THE RIGHT ENGINE OIL PRESSURE BEGAN DROPPING ALONG WITH A LOSS OF OIL QUANTITY. THE RIGH T ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO RDU. THE AIRCRAFT LANDED WITHOUT INCIDENT. (SET 20 MINUTES). MAINTE NANCE REPLACED THE RIGHT ENGINE. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200043 19990812 00043 NM 1999 8 12 TWRA9926 1 19990713 A 3350 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERABLE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 UPPER DECK EMERGENCY ESCAPE LIGHTS INOPERABLE DURING TEST. REPLACED LIGHT STRIP AT BOTTOM OF STAIRWELL - WDM 33-51-00. (X) 2 L 7 4 4F A20WE 1999081200044 19990812 00044 NM 1999 8 12 TWRA9928 1 19990713 A 5720 FASTENERS BOEING 747 747124 1384874 NM LT WING FAILED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 602FF 19734 LEFT WING UPPER WEB TO CHORD FASTENERS SHEARED (ONE EACH) AT FS 636.84 AND (3 EACH) AT FS 655.75, AND FS 646.07. LOWER W EB TO CHORD FASTENERS SHEARED (23 EACH) FS 618.96 TO FS 661.37. REPLACED RIVETS IAW AD 98-15-21 AND SB 57A22266 REV 5. (X) 2 L 7 4 4F A20WE 1999081200045 19990812 00045 NM 1999 8 12 TWRA9927 1 19990713 A 5720 FASTENERS BOEING 747 747124 1384874 NM RT WING CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 602FF 19734 RIGHT WING WEB TO CHORD UPPER FASTENERS CRACKED (2 EACH) AT FS 636.84 AND FS 646.07. LOWER WEB TO CHORD FASTENERS CRACK ED (ONE EACH) AT FS 636.84 AND FS 646.07. REPLACED RIVETS IAW AD 98-15-21 AND SB 57A22266 REV 5. (X) 2 L 7 4 4F A20WE 1999081200046 19990812 00046 NM 1999 8 12 TWRA9925 1 19990713 A 3397 WIRE BOEING 747 747283B 1384867 NM GALLEY BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 622FF 22496 EGRESS FLOOR LIGHTNING STRIP AT MID-GALLEY INOPERABLE. REPAIRED AND SECURED BROKEN WIRE PER WDM 33-51-00. (X) 2 L 7 4 4F A20WE 1999081200047 19990812 00047 1999 8 12 SIMA991791 4 19990628 A 3421 7003652602 ADU AEROSP ATR72 ATR72212A 8680902 EU COCKPIT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 550LL 88020819 550 DFW - FLT 3505 - ADVISORY DISPLAY UNIT SCREEN WENT BLANK AFTER TAKEOFF FOLLOWED BY ELECTRICAL SMELL IN THE COCKPIT AND C ABIN. REMOVED AND REPLACED ADU. ALSO, REMOVED AND REPLACED ASSOCIATED CONTROL PANEL AS A PRECAUTION. AIRCRAFT RETURNE D TO SERVICE. REF: OPER CNTRL NR 99ZZZX2829. (X) 2 H 7 2 4T RT A53EU 1999081200048 19990812 00048 1999 8 12 99ZZZX2829 4 19990628 A 3421 3975602 PANEL AEROSP ATR72 ATR72212A 8680902 EU COCKPIT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 550LL 97112071 550 DFW - FLT 3505 - ADVISORY DISPLAY UNIT SCREEN WENT BLANK AFTER TAKEOFF FOLLOWED BY ELECTRICAL SMELL IN THE COCKPIT AND C ABIN. REMOVED AND REPLACED ADU. ALSO, REMOVED AND REPLACED ASSOCIATED CONTROL PANEL AS A PRECAUTION. AIRCRAFT REUTRNE D TO SERVICE. REF: OPER CNTRL NR SIMA991791. 2 H 7 2 4T RT A53EU 1999081200049 19990812 00049 EU 1999 8 12 SIMA991781 1 19990627 A 3320 8ES00558800 TRANSFORMER AEROSP ATR42 ATR42300 8680920 EU ROW 10CD FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 327AT 327 JFK - FLT 4921 - SMOKE IN THE CABIN AFTER TAKEOFF FOLLOWED BY AN ODOR IN COCKPIT. RETURNED TO FIELD. REMOVED AND REPLA CED BURNED LIGHT TRANSFORMER AT SEAT 10CD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999081200050 19990812 00050 EU 1999 8 12 SIMA991544 1 19990503 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 538AT 0997 538 DFW - FLT 3726 - SOME EMERGENCY LIGHTS FAIL TO ILLUMINATE. REMOVED AND REPLACED LEFT FORWARD POWER SUPPLY AND BATTERY P ACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX2830. (X) 2 H 7 2 4T RT A53EU 1999081200051 19990812 00051 EU 1999 8 12 99ZZZX2830 1 19990503 A 3350 3023000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN INOPERABLE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 538AT 0484 538 DFW - FLT 3726 - SOME EMERGENCY LIGHTS FAIL TO ILLUMINATE. REMOVED AND REPLACED LEFT FORWARD POWER SUPPLY AND BATTERY P ACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA991544. 2 H 7 2 4T RT A53EU 1999081200052 19990812 00052 EA 1999 8 12 MASA99119 1 19990714 A 3350 GE1683 BULB BRUCE BM1000600Z CNDAIR CL600 CL6002B19 EA LT EMERG EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17217 7217 PHL/RDU - FLT 5837 - THE AIRCRAFT HAD AN EXTERNAL EMERGENCY LIGHT INOPERATIVE ON THE LEFT OVERWING EXIT. MAINTENANCE RE MOVED AND REPLACED THE BULB. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999081200053 19990812 00053 NM 1999 8 12 GAIA99106 1 19990722 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6838 20191 DURING A 'ZERO' LIGHT 'C' INSPECTION BEING PERFORMED IN OSC AT AMERICAN INTERNATIONAL AIRWAYS REPAIR STATION, CORROSION WAS DETECTED AT BS 1130 FLOORBEAM UPPER CAP, RBL 34-38. REPAIRED IAW AIA EDR B2-06516. DER APPROVED ON 8110-3 DATED MA Y 12, 1999. (X) 2 L 7 3 4F A3WE 1999081200054 19990812 00054 NE 1999 8 12 TWAA9910601 2 19990728 A 7230 ENGINE BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE RIGHT BIRD STRIKE A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET TO TAKEOFF 1 CE 05 632TW 24953 4701 DURING TAKEOFF, THE RIGHT ENGINE INJESTED A BIRD. CREW REPORTED A VIBRATION. THE ENGINE WAS SHUT DOWN AND THE FLIGHT R ETURNED TO TLV. ON LANDING OVERWEIGHT ALL EIGHT MAIN GEAR TIRES OVERHEATED AND DEFLATED. THE RT ENGINE HAD NUMEROUS B ROKEN BLADES ATTRIBUTED TO THE BIRD INJESTION, SOME OF WHICH PENETRATED THE NOSE COWL. REPLACED THE ENGINE AND NOSE COW L. CHECK-C 7-14-99 LAX. 2 L 7 2 4F 4 F RT A1NM E24NE 1999081200055 19990812 00055 NE 1999 8 12 HNAA9900107 3 19990727 A 6111 PROP DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 1 ENGINE DAMAGED A HNAA K NONE E VIBRATION/BUFFET CL CLIMB 1 EA 07 931HA 132 WHEN DEPARTING DCA, ACFT VIBRATED BAD. NR 1 PROP, NR 2 BLADE DAMAGED. NR 1 ENG REQUIRES VISUAL INSP OF 1ST STAGE IMPE LLER FOR EVIDENCE OF SOFT OR HARD MATERIAL INGESTION. NR 1 PROP NR 2 BLADE REQUIRES SB14SF-61-118 PERFORMED BEFORE REVE NUE FLIGHT. INSPECTED AND FOUND NICKLE SHEATH MISSING FROM NR 1 PROP NR 4 BLADE. REMOVED AND REPLACED NR 1 PROP NR 2 B LADE, OPS CHECK AND LEAK CHECK GOOD. INSPECTION COMPLETE, NO DEFECTS NOTED. ACFT FERRIED. 2 H 7 2 4T RT A13NM 6 C P7NE 1999081200056 19990812 00056 SO 1999 8 12 COMA9910119 1 19990723 A 2913 PV302229 HYD PUMP EMB 120 EMB120RT SO BLUE HYD SYS LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 267CA 2028 120259 BLUE HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED ENGINE HYDRAULIC PUMP. 2 L 7 2 4T RT A31SO 1999081200057 19990812 00057 1999 8 12 COMA9910121 4 19990726 A 3442 6227337001 RADAR EMB 120 EMB120RT SO FWD COMPT FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 256CA 22303 2815 120245 RADAR STUCK IN MAP MODE. COULD NOT DUPLICATE. REPLACED THE WXT-250B FOR TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1999081200058 19990812 00058 EA 1999 8 12 COMA9960395 1 19990726 A 3350 60205 SIGN CNDAIR CL600 CL6002B19 EA SERVICE DOOR BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947CA 7077 EMERGENCY LIGHT AT SERVICE DOOR IS BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A21EA 1999081200059 19990812 00059 EA 1999 8 12 COMA9960396 1 19990725 A 3260 864807 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 976CA 8401 2569 7151 WOW INPUT AND OUTPUT CAUTION MESSAGE. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1999081200060 19990812 00060 EA 1999 8 12 COMA9960397 1 19990726 A 7920 2810044101 CHECK VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A COMA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 960CA 7117 INFLIGHT SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PRESSURE. REPLACED THE OIL REPLENISH SYSTEM CHECK VALVE. 2 L 7 2 4F RT A21EA 1999081200061 19990812 00061 EA 1999 8 12 COMA9960398 1 19990728 A 5330 PLATE CNDAIR CL600 CL6002B19 EA BS 409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 14910 7018 FLOOR SUPPORT TOP PLATE AT FS 409.00 BETWEEN LBL9 AND RBL9 WL 73.5 IS CORRODED. PERFORMED A MAJOR REPAIR BY REMOVING CO RRODED TOP PLATE AT FS 409.00 BETWEEN LBL9 AND RBL 9 WL 73.5 AND FABBING NEW PLATE PER SAMPLE USING 7075-76 .100 IAW WVA C EO 601R-53-0115. 2 L 7 2 4F RT A21EA 1999081200062 19990812 00062 EA 1999 8 12 COMA9960399 1 19990728 A 5320 601R530113 ANGLE CNDAIR CL600 CL6002B19 EA BS 310-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 14910 7018 PAX DOOR THRESHOLD ANGLE P/N 601R31527-181 CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED PAX DOOR THRESHOLD ANGLE P/N 601R31527-181 IAW WVAC EO 601R-53-0113. 2 L 7 2 4F RT A21EA 1999081200063 19990812 00063 EA 1999 8 12 COMA9960400 1 19990728 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA BS 310-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 14910 7018 SERVICE DOOR THRESHOLD ANGLE P/N 601R38303-105 CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED SERVICE DOOR TH RESHOLD ANGLE P/N 601R3803-105 IAW WVAC EO 601R-53-0112. 2 L 7 2 4F RT A21EA 1999081200064 19990812 00064 EA 1999 8 12 COMA9960401 1 19990728 A 5321 6003401717 FLOOR CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 14910 7018 FLOOR MEMBER P/N 600-34017-17 AT FS 280.00 IS CRACKED 2, APPROXIMATELY 1 TO THE RIGHT OF FLOOR SUPPORT OF RBL 9.0. PERF ORMED A MAJOR REPAIR TO CRACKED FLOOR MEMBER P/N 600-34017-17 AT FS 280.00 IAW WVAC EO 601R-53-0117A. 2 L 7 2 4F RT A21EA 1999081200065 19990812 00065 EA 1999 8 12 COMA9960402 1 19990728 A 5320 601R38673 SUPPORT CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 14910 7018 FLOOR SUPORT TOP PLATES P/N 601R38673-17, 19, 21, AND 25 AT FS 349.0 ARE CORRODED. ALSO, L ANGLE SUPPORT P/N 601R38673- 13 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FLOOR SUPPORT TO PLATES P/N 601R38673-17, 19, 21 AND 25 IAW WVAC EO 601R-53-0114 AND REPLACED SUPPORT L ANGLE P/N 601R38673-13 IAW WVAC EO 601R-53-01308B. 2 L 7 2 4F RT A21EA 1999081200066 19990812 00066 EA 1999 8 12 COMA9960403 1 19990728 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280-409. CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 14910 7018 FLOOR SUPPORT BEAM CAPS P/N 601R31113-67 AT LBL 27 BETWEEN FS 314 TO FS 349, LBL9 BETWEEN FS 310.00 TO 409.00, RBL9 BETW EEN FS 310.00 TO FS 409.00 AND RBL 27 BETWEEN FS 310.00 TO 409.00 ARE CORRODED OUT OF LIMITS IAW CRJ REO 601R-53-00-005. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FLOOR SUPPORT BEAM CAPS P/N 601R3113-67 AT LBL 27 BETWEEN FS 280.00 TO FS 349.00, LBL9 BETWEEN FS 280.00 TO FS 409.00, RBL 9 BETWEEN FS 280.00 TO FS 409.00 AND RBL 27 BETWEEN FS 280.00 TO FS 409.00 IAW CRJ REO 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999081200067 19990812 00067 NM 1999 8 12 UPS99230215 1 19990729 A 3350 9631010 LIGHT BOEING 727 72725C 138400H NM CREW ENTRY INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY EXIT LIGHT AT CREW ENTRY FAIL. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999081200068 19990812 00068 NM 1999 8 12 UPS99230216 1 19990726 A 3350 BATTERY PACK BOEING 727 72751C 1384015 NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 903UP 18945 FWD ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, EMERGENCY LIGHT OPS CHECK GOOD PER MM 33-50-01. 2 L 7 3 4F A3WE 1999081200069 19990812 00069 WP 1999 8 12 UPS99830214 1 19990728 A 3350 5708458503 BATTERY DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 COCKPIT EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW M/M 33-50-01, OP'S CK NORMAL OK FOR SERVICE. 2 L 7 4 4F RT 4A25 1999081200070 19990812 00070 WP 1999 8 12 UPS99830218 1 19990712 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING L/E CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E UPPERSKIN AT XFS 710 IS CRACKED AT THE AFT INBD CORNER. CUT OUT DAMAGED AREA AND REPAIRE D IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999081200071 19990812 00071 WP 1999 8 12 UPS99830219 1 19990712 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E UPPER SKIN AT XFS 635 US CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 3 8. 2 L 7 4 4F RT 4A25 1999081200072 19990812 00072 WP 1999 8 12 UPS99830220 1 19990712 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP VANE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT OTBD SLOT VANE HAS EXFOLIATION CORROSION AT THE INBD END. CUT OUT DAMAGED AREA AND REPAIRED IAW S RM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 1999081200073 19990812 00073 WP 1999 8 12 UPS99830221 1 19990712 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 379 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E UPPER SKIN IS CRACKED AT XFS 379. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 3 8. 2 L 7 4 4F RT 4A25 1999081200074 19990812 00074 WP 1999 8 12 UPS99830222 1 19990713 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E SKIN, ABOVE AT THE FWD END OF THE NR 1 PYLON CUT OUT IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1A. 2 L 7 4 4F RT 4A25 1999081200075 19990812 00075 WP 1999 8 12 UPS99830223 1 19990713 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E SKIN AT THE FWD END OF THE NR 2 PYLON CUT OUT IS CRACKED. STOP DRILLED CRACK AND REPAIRE D IAW SRM 57-2-0A FIG 1. 2 L 7 4 4F RT 4A25 1999081200076 19990812 00076 WP 1999 8 12 UPS99830224 1 19990713 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 RT WING L/E LOWER SKIN IS CRACKED AT THE DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999081200077 19990812 00077 WP 1999 8 12 UPS99830225 1 19990713 A 5730 576960036 DOUBLER DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 RT WING L/E SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED, AN D REPLACED DOUBLER IAW DWG 5679300 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999081200078 19990812 00078 WP 1999 8 12 UPS99830226 1 19990713 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 485 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 RT WING L/E SKIN IS CRACKED AND CORRODED AT XW 485. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0 . 2 L 7 4 4F RT 4A25 1999081200079 19990812 00079 WP 1999 8 12 UPS99830227 1 19990713 A 5320 3758519501 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 EXTERNAL, CENTER SECTION KEEL BEAM FITTING AT FS 759 RT IS CRACKED. REMOVED, FABRICATED, AND REPLACE D FITTING IAW DWG 3758519 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999081200080 19990812 00080 WP 1999 8 12 UPS99830228 1 19990714 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 220, BETWEEN LONGERON 11R AND 12R, THE SHEAR TIE IS CRACKED. CUT OUT DAMAGED LEG, AND REPAIRED TH E SHEAR TIE IAW SRM 53-2-0 FIG 2B. 2 L 7 4 4F RT 4A25 1999081200081 19990812 00081 WP 1999 8 12 UPS99830229 1 19990714 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 THE FUSELAGE SKIN AT FS 1660, AFT ENTRY DOOR, AFT UPPER CORNER, HAS 5 CRACKS EXTENDING FROM FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 1999081200082 19990812 00082 WP 1999 8 12 UPS99830230 1 19990715 A 5320 3755822502 FITTING DOUG DC8 DC873F 302199F WP BS 350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 350 BETWEEN LONGERON 36 AND 35L, THE BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999081200083 19990812 00083 WP 1999 8 12 UPS99830231 1 19990715 A 5320 3755822513 FITTING DOUG DC8 DC873F 302199F WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 300 BETWEEN LONGERON 34R AND 35R, THE BATH TUB FITTING HAS MODERATE CORROSION. REMOVED AND REPLAC ED THE FITTING IAW SRM 53-2-0 FIG 1D. 2 L 7 4 4F RT 4A25 1999081200084 19990812 00084 WP 1999 8 12 UPS99830232 1 19990716 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E LOWER RIB AT XOLDI 6.225 IS CRACKED AT THE AFT FASTENER. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999081200085 19990812 00085 WP 1999 8 12 UPS99830233 1 19990716 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 385.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E RIB AT XFS 385.25 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999081200086 19990812 00086 WP 1999 8 12 UPS99830234 1 19990716 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 461.372 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 LT WING L/E RIB AT XS 461.372 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999081200087 19990812 00087 WP 1999 8 12 UPS99830235 1 19990716 A 5720 576960040 DOUBLER DOUG DC8 DC873F 302199F WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 RT WING L/E LOWER SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 572.5. REMOVED, FABRICAT ED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999081200088 19990812 00088 WP 1999 8 12 UPS99830236 1 19990717 A 5320 37799781 FITTING DOUG DC8 DC873F 302199F WP BS 834 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 834 AT LONGERON 18L, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999081200089 19990812 00089 EU 1999 8 12 QXEA9901470 1 19990721 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - SKIN CHAFFED UNDER PANEL 92BD, FRAMES 14755 AND 15205 AND STRINGER 66. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 6. 2 L 7 2 4F RT A20EU 1999081200090 19990812 00090 EU 1999 8 12 QXEA9901471 1 19990718 A 5720 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - BL245L AND Z STRINGER 2.01 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW HORIZON AIR EA 4-57-298. 2 L 7 2 4F RT A20EU 1999081200091 19990812 00091 EU 1999 8 12 QXEA9901472 1 19990718 A 5720 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - BL245L AND Z STRINGER 2.02 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW EA 4-57-298. 2 L 7 2 4F RT A20EU 1999081200092 19990812 00092 EU 1999 8 12 QXEA9901473 1 19990718 A 5720 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - BL245R AND Z STRINGER 2.01 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW HORIZON AIR EA 4-57-298. 2 L 7 2 4F RT A20EU 1999081200093 19990812 00093 EU 1999 8 12 QXEA9901474 1 19990718 A 5720 WEB FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - BL245R AND Z STRINGER 2.02 WEB PLATE IS CRACKED IN THE RADIUS. REPAIRED IAW HORIZON AIR EA 4-57-298. 2 L 7 2 4F RT A20EU 1999081200094 19990812 00094 EU 1999 8 12 QXEA9901475 1 19990713 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - WING MOD VALVE IS CHAFFING INTO STRUCTURE AT BL425L. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 4, FIGURE 9. 2 L 7 2 4F RT A20EU 1999081200095 19990812 00095 EU 1999 8 12 QXEA9901476 1 19990716 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU LT MLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - SKIN STIFFENER IN LEFT WHEEL WELL ABOVE AFT LUG OF MAIN LANDING GEAR SHOCK STRUT IS CRACKED. REPAIRED IAW FOKKER SRM 51-30-01. 2 L 7 2 4F RT A20EU 1999081200096 19990812 00096 EU 1999 8 12 QXEA9901477 1 19990719 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU FUEL SYS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FRETTING CORROSION AROUND SCREW HOLES ON FUEL PANEL 73G. REPAIRED IAW CPCP CARD 700/23. 2 L 7 2 4F RT A20EU 1999081200097 19990812 00097 EU 1999 8 12 QXEA9901478 1 19990719 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU FUEL SYS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FRETTING CORROSION AROUND SCREW HOLES ON FUEL PANEL 73H. REPAIRED IAW CPCP CARD 700/23. 2 L 7 2 4F RT A20EU 1999081200098 19990812 00098 EU 1999 8 12 QXEA9901479 1 19990719 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU FUEL SYS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FRETTING CORROSION AROUND SCREW HOLES ON FUEL PANEL 73J. REPAIRED IAW CPCP CARD 700/23. 2 L 7 2 4F RT A20EU 1999081200099 19990812 00099 EU 1999 8 12 QXEA9901480 1 19990712 A 5540 PATCH FOKKER F28 F28MK4000 4990810 EU RUDDER LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - RUDDER LEADING EDGE FLUSH PATCH AT RIB 1 IS COMING UP ON LEFT EDGE. REPAIRED IAW FOKKER SRM 51-20-05. 2 L 7 2 4F RT A20EU 1999081200100 19990812 00100 EU 1999 8 12 QXEA9901481 1 19990712 A 5540 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER GAPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - RUDDER LEADING EDGE HAS SKIN GAP AT RIB 4 LEFT SIDE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999081200101 19990812 00101 EU 1999 8 12 QXEA9901483 1 19990712 A 5542 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - RUDDER IS DENTED AT 2 FEET FROM BOTTOM, MID SPAN OF SKIN. REPAIRED IAW FOKKER SRM 51-70-0, PAGE 13, PARAGRAPH 7C. 2 L 7 2 4F RT A20EU 1999081200102 19990812 00102 EU 1999 8 12 QXEA9901484 1 19990712 A 5542 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - RUDDER LEADING EDGE SKIN AT RIB 3 HAS A LOOSE RIVET LEFT SIDE. REPAIRED IAW FOKKER SRM 51-1-01. 2 L 7 2 4F RT A20EU 1999081200103 19990812 00103 EU 1999 8 12 QXEA9901485 1 19990715 A 5531 RIB FOKKER F28 F28MK4000 4990810 EU VERT STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - V STAB AT RIB 5.0 AND INTERMEDIATE SPAR II RIGHT SIDE HAS CHAFE DAMAGE FROM STAB. REPAIRED IAW HORIZON AIR EA 4-5 5-149. 2 L 7 2 4F RT A20EU 1999081200104 19990812 00104 EU 1999 8 12 QXEA9901486 1 19990712 A 5540 STRINGER FOKKER F28 F28MK4000 4990810 EU RUDDER BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - RUDDER HAS A BROKEN STRINGER NEAR RIB 7. LOWER RUDDER FLUTTER COMPARTMENT 2 BY .5 PIECE REMOVED FROM AREA. REPAI RED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999081200105 19990812 00105 EU 1999 8 12 QXEA9901487 1 19990715 A 5510 LUG FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - H STAB JUNCTION FITTINGS UPPER LEFT AND UPPER RIGHT LUGS HAVE PITTING RIGHT SIDE LUG IS DEEPER. REPAIRED IAW HORI ZON AIR EA 4-55-150. 2 L 7 2 4F RT A20EU 1999081200106 19990812 00106 EU 1999 8 12 QXEA9901488 1 19990715 A 5510 LUG FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - H STAB JUNCTION FITTINGS LOWER LEFT AND LOWER RIGHT LUGS HAVE PITTING AND STEP WEAR, LEFT LUG STEP WEAR IS PRONOUN CED. REPAIRED IAW HORIZON AIR EA 4-55-150. 2 L 7 2 4F RT A20EU 1999081200107 19990812 00107 EU 1999 8 12 QXEA9901489 1 19990715 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - H STAB DRIVE FITTINGS HAVE PITTING LEFT AND RIGHT LOWER LUGS HAVE STEP WEAR. REPAIRED IAW HORIZON AIR EA 4-55-150 . 2 L 7 2 4F RT A20EU 1999081200108 19990812 00108 EU 1999 8 12 QXEA9901490 1 19990716 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU LT & RT FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - CHAFE ON BOTH LEFT AND RIGHT SIDE OF AFT SIDE OF SPEED BRAKE SUPPORT BOX. REPAIRED IAW HORIZON AIR EA 4-53-834. 2 L 7 2 4F RT A20EU 1999081200109 19990812 00109 EU 1999 8 12 QXEA9901491 1 19990712 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - CRACKS AT FRAME 20075 BETWEEN STRINGER 39 AND 40. REPAIRED IAW FOKKER SRM 53-10-5, PAGE 601A. 2 L 7 2 4F RT A20EU 1999081200110 19990812 00110 EU 1999 8 12 QXEA9901492 1 19990712 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17665 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - WHERE FRAME 17665 AND STRINGER 57 MEET THERE IS A CRACK. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A AND SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1999081200111 19990812 00111 EU 1999 8 12 QXEA9901493 1 19990707 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - CRACKED FRAME CLIP AT FRAME 16060 AND STRINGER 31. REPAIRED IAW FOKKER SRM 51-31-01, SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1999081200112 19990812 00112 EU 1999 8 12 QXEA9901494 1 19990708 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION INSIDE CHANNEL AND AT CUT OUT NEAR FRAME 9305A. REPAIRED IAW FOKKER SRM 5 1-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999081200113 19990812 00113 NM 1999 8 12 99FDEA00292 1 19990728 A 3260 CONNECTOR BOEING 727 72725C 138400H NM LG DOOR LIGHT DIRTY A FDEA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 25 118FE 19300 99-177 - LEFT LANDING GEAR DOOR LIGHT IND UNSAFE. AFT CYCLING GEAR, RED LIGHT EXTINGUISHED. CK LEFT DOOR SWITCH ADJUST MENT PER MM 32-62-011-4. CLEANED AND SECURED CONNNECTOR. DOOR AND LIGHT CHECK NORMAL. 2 L 7 3 4F A3WE 1999081200114 19990812 00114 NM 1999 8 12 99FDEA00293 1 19990728 A 2612 FIRE WARNING BOEING 727 7272S2F 1384O81 NM COCKPIT ACTIVATED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 213FE 22935 99-178 - AT FLT LEVEL 280, W/THRUST AT CR PWR RECEIVED MULTIPLE INTERMITTENT MASTER FIRE WARN LIGHT AND FIRE BELL. ENG OIL TEMP INCREASED TO 138 DEG, ALL OTHER ENG INSTRUMENT NORM. RETARD NR 3 THROTTLE TO IDLE. START DUCT REALIGNED AND S ECURED PER MM 36-00-001-2. ENG RUNS C/O AT FULL PWR PER JET RUN HDBK 6-15. ALL LIMITS OBSERVED. AC OK FOR SERVICE. 2 L 7 3 4F A3WE 1999081200115 19990812 00115 NM 1999 8 12 99FDEA00294 1 19990728 A 2612 FIRE SENSOR BOEING 727 727227 1384078 NM LWR AFT BODY OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 486FE 21489 99-179 - LWR AFT BODY OH LIGHT ILLUMINATED IN FLIGHT, AFTER THE NR 2 BLEED SWITCHES WERE CLOSED. THE LIGHT WENT OUT. T EST OF THE CIRCUIT WAS SUCCESSFUL. REPOSITIONED SENSOR AND RAN NR 2 ENG PER 727, JET RUN HDBK FOR 30 MIN. NO REPEAT, S ENSOR TESTS NORM. 2 L 7 3 4F A3WE 1999081200116 19990812 00116 NM 1999 8 12 99FDEA00295 1 19990727 A 3230 656021123 ACCESSORY UNIT BOEING 727 727233 138408A NM LANDING GEAR FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 219FE 21102 99-180 - LAND GEAR LEVER UNABLE TO RAISE AFT T/O. LAND GEAR LEVER LATCH LIGHTS CIRCUIT BREAKER WAS CK IN. NO CHG. FLA PS RAISED TO 2 AND NO WARN HORN. WING ANTI-ICE TEST AND DID NOT OPEN. NOSE GEAR STEER HANDLE ALIGNMENT MARKS WERE ALIG NED. REMOVED AND REPLACED LAND GEAR ACCESSORY UNIT PER MM 32-09-121. OPS CK GOOD PER MM 32-09-122. 2 L 7 3 4F RT A3WE 1999081200117 19990812 00117 EU 1999 8 12 99FDEA00296 1 19990728 A 2133 81001C010300 OUTFLOW VALVE AIRBUS 310 A310203 EU CABIN FAILED A FDEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 25 443FE 283 99-181 - AT BEG OF ALERT, CABIN PRESS WAS ABOUT 7.1 PSI CABIN RATE 200 FPM. GOT ECAM ALERT. REMOVED AND REPLACED NR 1 OUTFLOW VALVE AMM 21-31-12. OPS CK NORMAL. NOTE NR 2 SYS ON DEFFERAL, MEL 21-1. MACH ITEM 21-30 1817. 2 L 7 2 4F RT A35EU 1999081200118 19990812 00118 WP 1999 8 12 99FDEA00297 1 19990729 A 2910 61912 FUSE DOUG DC10 DC1030F 3023504 WP HYS SYS CRACKED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 320FE 47835 99-182 - AFT GEAR RETRACTION, HYD QUAN AND PRESSURE ON NR 3 SYS DROPPED TO 0. REPLACED THE CRACKED LOCK OUT FUSE PER MM 32-31-06-2 ALSO NR 3 HYD SYS CASE DRAIN FILTER CK IS OK PER MM 29-12-02-2 AND MM 29-12-17-2. LEAK CK IS OK CLOSED SEC URED AND NR 3 ENG COWLING C/W RII. 2 L 7 3 4F RT A22WE 1999081200119 19990812 00119 1999 8 12 99FDEA00298 2 19990729 A 7261 O RING DOUG DC10 DC1030 3023501 WP NR 2 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 318FE 46837 99-183 - LOST ALL OIL QTY FOR NR 2 ENG WITH ACCOMP. REPLACED O-RING. REINSTALLED CHIP DETECTOR SERVICED ENG, OIL TO FUL L RAN ENG PER JRH CHP 5A. NO LEAKS NOTED. OK FOR SERVICE MM 71-00-00. 2 L 7 3 4F A22WE 1999081200120 19990812 00120 NE 1999 8 12 ABXA9900606 2 19990726 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 DEFECTIVE A ABXA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 816AX 3412 46093 669302 NR 1 ENGINE LOST OIL PRESSURE AFTER DEPARTURE. NO OIL QUANTITY, HIGH OIL TEMP, PRESSURE 20 PSI. SECURED NR 1 ENGINE. R EMOVED AND REPLACED NR 1 ENGINE. 2 L 7 4 4F 4 F 4A25 1E8 1999081200121 19990812 00121 WP 1999 8 12 ABXA9900607 1 19990722 A 5313 5911279502 STRINGER DOUG DOUG DC9 DC932 3022066 WP BS 69 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING C-CHECK, FOUND STRINGER 19 CORRODED AT STATION 69. REPLACED SECTION OF STRINGER NR 19 IAW DC9 SRM 53-30-1. 2 L 7 2 4F A6WE 1999081200122 19990812 00122 WP 1999 8 12 ABXA9900608 1 19990722 A 5753 9957578508 SKIN DOUG DOUG DC9 DC932 3022066 WP RT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING C-CHECK, FOUND RIGHT FLAP UPPER SKIN CORRODED. REPLACED NR 3 TRAILING EDGE UPPER SKIN SEGMENT IAW DC9 SRM 53-30- 2. 2 L 7 2 4F A6WE 1999081200123 19990812 00123 WP 1999 8 12 ABXA9900609 1 19990727 A 2510 59253791ABX1 SEAT DOUG DC9 DC931 3022065 WP LT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 947AX 47004 CAPTAIN'S SEAT MOVED AFT AND DOWN, UNCOMMANDED, ON TAKEOFF. LUBRICATED SEAT ADJUSTMENT MECHANISM AND CHECKED LOCKING PI N ENGAGEMENT. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1999081200124 19990812 00124 WP 1999 8 12 ABXA9900610 1 19990727 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 948AX 47065 DURING PREFLIGHT INSPECTION FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1999081200125 19990812 00125 WP 1999 8 12 MWEA99448 1 19990701 A 2560 100503119 GIRT BAR DOUG DC9 DC982 3022082 WP SERVICE DOOR STUCK A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 203ME 48070 THE AFT SERVICE DOOR GIRT BAR IS STUCK. MAINTENANCE REPOSITONED AFT GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1999081200126 19990812 00126 WP 1999 8 12 MWEA99449 1 19990627 A 5414 99577423 SKIN DOUG DC9 DC914 3022034 WP BS 886 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 THE LEFT ENGINE PYLON UPPER SKIN TRAILING EDGE HAS A CRACK AT STATION 886. MAINTENANCE FABRICATED AND INSTALLED DOUBLER . 2 L 7 2 4F A6WE 1999081200127 19990812 00127 WP 1999 8 12 MWEA99450 1 19990728 A 5320 99582387 SPLICE DOUG DC9 DC914 3022034 WP BS 801 INTERFERING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FRAME SPLICE AT STATION 801 LONGERON L10R-L11R INTERFERES WITH INSTALLATION OF EO 1-53-1100. FABRICATED AND INSTALLED R EPAIR ANGLE AND SPLICES. 2 L 7 2 4F A6WE 1999081200128 19990812 00128 WP 1999 8 12 MWEA99451 1 19990727 A 5320 59114151 DOUBLER DOUG DC9 DC914 3022034 WP BS 661 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 TOOL MARK GOUGE ON FINGER DOUBLER AND FUSELAGE SKIN AT LONGERON 1 AND STATION 661. REMOVED GOUGED FINGER ON DOUBLER AND INSTALLED PLUG IN EXISTING FASTENER HOLE PER BOEING TELEX MUX 99-0015H. 2 L 7 2 4F A6WE 1999081200129 19990812 00129 WP 1999 8 12 RRXA991172 1 19990723 A 2750 O RING DOUG DC8 DC873F 302199F WP SLOT CONTL VALVE FAILED A RRXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 15 792FT 46046 AT TIME 14:13-Z ON BOTH HYD PUMPS WITH RES LOW PRESS LT ON. AUX PUMP WOULD ONY BUILD UP TO 1000 PSI, QUANITY STAYED AT 3/4. FLAPS SHOWED A SPLIT WHEN SYSTEM PRESSURIZED IN THE BYPASS POSS. FOUND BLOWN O-RING ON SLOT CONTROL VALVE. REPLA CED O-RING ON SLOT CONTROL VALVE SERVICED HYD SYS AS REQUIRED PERFORMED ENG RUN ON NR 2 AND NR 3 ENG FOR OPS CK HYD PUMP S, PERFORMED FLT CONTROL CKS AND LEAKS CKS OF NEW O-RING, OPS CK GOOD ON ENG DRIVEN PUMPS, FLT CONTROL LEAKS CK GOOD. N O LEAKS OR DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999081200130 19990812 00130 WP 1999 8 12 RRXA991173 1 19990707 A 2612 899097 FIRELOOP DOUG DC8 DC873F 302199F WP NR 3 ENGINE MALFUNCTIONED A RRXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 15 795FT 46103 APROX 1 HR 20 MINS INTO FLT, FIRE WARNING LT AND BELL WENT OFF. INDICATION OF LTS IN NR 3 FIRE HANDLE ON. ALL ENG INDI CATIONS NORM. NR 3 ENG SHORT CIRCUIT LT CAME ON FIRED 1ST BOTTLE. FIRE INDICATION AND TEST GOOD. AFTER TALKING TO COM PANY, INDICATION ON AGAIN. FIRED 2ND BOTTLE, NO LIGHT IN HANDLE BUT COULD NOT GET FIRE TEST. FOUND NR 3 ENG INBD FAN C OWL FIRE LOOP SHORTED. REMOVED AND REPLACED FIRE LOOP SEGMENT ON GROUND RUN, OPS CKS GOOD. RECONNECTED CSD AND GEN OPS CK GOOD AT THIS TIME, NO OTHER DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999081200131 19990812 00131 WP 1999 8 12 RRXA991174 1 19990723 A 5320 PLATE DOUG DC8 DC862 3021970 WP DOOR JAMB DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 REPAIR MAIN CARGO DOOR UPPER JAMB HANGER PLATE PER COTNEY ENG DRW. REPAIRED MAIN CARGO DOOR UPPER JAMBHEADER PLATE PER COTNEY ENG'G DWG EAH 70-1, EMERY DWG NR 70-R01, STC1802SD. 2 L 7 4 4F 4A25 1999081200132 19990812 00132 WP 1999 8 12 RRXA991175 1 19990726 A 2923 LINE DOUG DC8 DC873F 302199F WP HYD SYSTEM LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 796FT 46104 EN ROUTE TO TJBQ LOSS OF HYDRAULICS, PERFORMED LOSS OF HYD. CHECKLIST PER QRH. FOUND RUDDER PUMP PRESSURE LINE LEAKING , REPLACED LINE. LEAK AND OPS CHECKED NORMAL. SERVICED HYD RESV. 2 L 7 4 4F RT 4A25 1999081200133 19990812 00133 SO 1999 8 12 COMA9910120 1 19990726 A 3350 10130115 EXIT LIGHT EMB 120 EMB120RT SO CABIN INOP A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 249CA 120230 EXIT SIGN AT ROW 5 WAS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999081200134 19990812 00134 WP 1999 8 12 TWAA9910701 1 19990720 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, THE VERTICAL SUPPORT FROM CARGO BIN TO FLOORBEAM WAS CRACKED AT TOP, STA 756 RBL 22 INCHES, AF T SIDE OF BEAM. STOP DRILLED CRACK PER SRM 53-01, PAGE 10. INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 1999081200135 19990812 00135 WP 1999 8 12 TWAA9910702 1 19990722 A 5320 SPLICE DOUG DC9 DC931 3022065 WP BS 237&218 LIGHTNING STRIKE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND STATIC BURN ON RIVET IN PRODUCTION SPLICE, STA 237 AND 218, RL 28 AND 29. REPLACED RIVE T PER SRM 53-04, FIG 38. 2 L 7 2 4F A6WE 1999081200136 19990812 00136 WP 1999 8 12 TWAA9910703 1 19990725 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 680 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT BEAM CRACKED AT LT SIDEWALL STA 680. CONFIRMED BY NDT. REPLACED FLOOR SU PPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999081200137 19990812 00137 WP 1999 8 12 TWAA9910704 1 19990723 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 897 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND ANGLE FROM FLOORBEAM TO INTERCOSTAL CRACKED AT STA 897, RBL 23. REMOVED OLD ANGLE, FABR ICATED NEW ANGLE, REINSTALLED NEW ANGLE AT STA 897, RBL 23, PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999081200138 19990812 00138 WP 1999 8 12 TWAA9910705 1 19990726 A 5320 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND AFT FUSELAGE RT SUPPORT ANGLE CRACKED AT LOWER LOUVER SUPPORT. REPLACED ANGLE PER SPM 6 -70-01. 2 L 7 2 4F A6WE 1999081200139 19990812 00139 WP 1999 8 12 TWAA9910706 1 19990725 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 229-245 MISREPAIRED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 9413T 53188 DURING CHECK-C MAINT, FOUND FUSELAGE SKIN REPAIR INSTALLED WITH BLIND FASTENERS AT STA 229 TO 245, STRINGER 18L. REPAIR ED PER SRM 53-04, FIG 12B, WITH SOLID FASTENERS AND ADDING FINGER DOUBLER. 2 L 7 2 4F RT A6WE 1999081200140 19990812 00140 WP 1999 8 12 TWAA9910707 1 19990726 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 217 GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9413T 53188 DURING CHECK-C MAINT, FOUND FUSELAGE SKIN GOUGED AT STA 217, STRINGER 5L AND 6L. AN INTERIM REPAIR HAD BEEN INSTALLED P ER ARA 15461. REPAIRED PER SRM 53-04, FIG 12B, SHEET 5. 2 L 7 2 4F RT A6WE 1999081200141 19990812 00141 NM 1999 8 12 AT9900538 1 19990728 A 3350 P4010020 BATTERY PACK BOEING 737 737214 138446R NM R2 DOOR DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 R2 DOOR MOUNTED EMERGENCY FLOOD LIGHT (SLIDE) WILL NOT ILLUMINATE. REMOVED AND REPLACED R2 DOOR MOUNTED EMERGENCY FLOOD LIGHT BATTERY PACK IAW B737 MM 33-51-71. 2 L 7 2 4F A16WE 1999081200142 19990812 00142 1999 8 12 ATT9900539 2 19990728 A 7261 814086 PUMP BOEING 737 737297 1384480 NM NR 1 ENGINE LEAKING A ZZDA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 15 462AT 22631 NR 1 ENGINE LOST ALL OIL QUANTITY. ENGINE WAS SHUT DOWN ON SHORT FINAL WITH OIL PRESSURE GOING TOWARDS ZERO. OIL TEMPE RATURE OK. INSPECTION FOUND OIL PUDDLING AROUND NR 6 BEARING AREA AND IN TAILPIPE. REMOVED AND REPLACED NR 6 GARLOCK S EAL AND NR 6 BEARING SCAVENGE PUMP ASSY. LEAK/OPS CHECK COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A16WE 1999081200143 19990812 00143 1999 8 12 CALA9900878 4 19990728 A 2340 RDAX3201 DECODER DOUG DC10 DC1030 3023501 WP ROW 37&38KL SHORTED A CALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 59083 47926 SMOKE APPEARED IN THE AIRCRAFT CABIN NEAR THE VICINITY OF SEATS 37 AND 38KL WHILE ON FINAL APPROACH TO DUS. THE FLIGHT ATTENDANT'S PULLED OVERHEAD PANEL IN THE AREA AND USED HALON TO COOL THE AREA. NO FIRE WAS OBSERVED. THE AIRCRAFT LAND ED AT DUS WITHOUT INCIDENT. THE FAULT WAS TRACED TO OVERHEATED TIMER/DECODER ABOVE SEATS 37 AND 38KL. THE TIMER/DECODE R WAS REMOVED AND REPLACED. NO WIRING DAMAGE WAS FOUND. IN ADDITION, THE HALON FIRE EXTINGUISHER WAS REPLACED. 2 L 7 3 4F A22WE 1999081200144 19990812 00144 NM 1999 8 12 CALA9900879 1 19990729 A 2530 416100129 COFFEEMAKER BOEING 737 7373Q8 1384670 NM GALLEY SHORTED A CALA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14383 26312 SMOKE WAS REPORTED IN THE VICINITY OF THE AFT GALLEY COFFEEMAKER WHILE EN ROUTE TO IAH. THE FLIGHT ATTENDANT DISCHARGED THE HALON FIRE EXTINGUISHER ONTO THE AREA, THE GALLEY POWER WAS TURNED OFF, AND THE SMOKE CEASED. THE FLIGHT WAS CONTI NUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT GALLEY COFFEEMAKER IN THE NR 1 POSITION AT FAUL T. THE COFFEEMAKER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. NO OTHER DAMAGE WAS NOTED. 2 L 7 2 4F RT A16WE 1999081200145 19990812 00145 WP 1999 8 12 CALA9900880 1 19990728 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1821 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12080 47981 INVESTIGATION FOUND FRAME CORRODED AT STA 1821, LONGERON 33R-48R. A NEW FRAME WAS INSTALLED IAW SRM 51-33-01 AND 51-35- 0. 2 L 7 3 4F A22WE 1999081200146 19990812 00146 WP 1999 8 12 CALA9900881 1 19990728 A 5711 SPAR DOUG DC10 DC1030 3023501 WP WS 217 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12080 47981 INSPECTION FOUND A .5 INCH CRACK EMANATING FROM NR 3 TRANSFER PUMP COVER O/B ATTACHMENT HOLE IN REAR SPAR AT STA XORS 21 7, RT WING. THE SPAR WAS REPAIRED IAW SRM 57-10-00. 2 L 7 3 4F A22WE 1999081200147 19990812 00147 WP 1999 8 12 CALA9900882 1 19990728 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1105-1202 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND LEFT I/B SEAT TRACK CORROSION FROM STA 1105-1202. THE SEAT TRACK FROM STA 1050-1300 WAS REMOVED AND RE PLACED IAW SRM 53-05-04. 2 L 7 2 4F A6WE 1999081200148 19990812 00148 WP 1999 8 12 CALA9900883 1 19990729 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 1485 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 2 INCH CRACK ON TAIL CANTED FRAME TOP LEFT BRACKET AT STA 1485. A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 1999081200149 19990812 00149 WP 1999 8 12 CALA9900884 1 19990729 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 984 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 2.5 INCH CRACK IN DOUBLER AT AFT END OF KEEL STRUCTURE AT FS 984, RBL 5. THE DOUBLER WAS REMOVED IAW SRM 51-30-05. A NEW DOUBLER WAS INSTALLED IAW SRM 53-14-3, PAGE 19, 51-10-4, 51-30-5, AND 51-30-02. 2 L 7 2 4F A6WE 1999081200150 19990812 00150 WP 1999 8 12 CALA9900885 1 19990729 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 886-905 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 0.45 CRACK IN CABIN WINDOW FRAME DOUBLER AT UPPER FORWARD CORNER BETWEEN FS 886 AND 905, LONGERON 11R . THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1999081200151 19990812 00151 NM 1999 8 12 CALA9900886 1 19990729 A 5713 STRINGER BOEING 727 727224 1384076 NM WS 656.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A ,25 INCH CRACK AT LEFT WING TANK UPPER STRINGER, FIRST FORWARD FROM REAR SPAR, WS 656.5 AT TANK CUT O UT. A REPAIR WAS INSTALLED IAW ECRA 5762-01050. 2 L 7 3 4F A3WE 1999081200152 19990812 00152 WP 1999 8 12 CALA9900887 1 19990729 A 5230 ANGLE DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A .75 INCH CRACK IN ANGLE ON FORWARD SIDE OF AFT LIGHTENING HOLE ON LOWER AFT END OF FORWARD CARGO DOOR . THE ANGLE WAS REMOVED IAW SRM 51-30-02 AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999081200153 19990812 00153 WP 1999 8 12 CALA9900888 1 19990729 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 964 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A .5 INCH CRACK AT UPPER FORWARD CORNER OF WINDOW FRAME ON RT SIDE AT STA 964, LONGERON 11R. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-10-2. 2 L 7 2 4F A6WE 1999081200154 19990812 00154 WP 1999 8 12 CALA9900889 1 19990729 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 218 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND THREE CRACKS IN CUSP WEB AT FS 218, LONGERON 18L. THE CRACKS WERE 1.5 TO 3 LONG. THE CRACKED AREAS WER E CUT OUT IAW SRM 53-01 AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1999081200155 19990812 00155 WP 1999 8 12 CALA9900890 1 19990729 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 150-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND CABIN SUBFLOOR ATTACH ANGLE CORRODED AT STA 150-200, RBL 136. THE ATTACH ANGLE WAS REMOVED IAW SRM 51- 30-2 AND A NEW ANGLE WAS INSTALLED IAW SRM 53-14-1, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999081200156 19990812 00156 WP 1999 8 12 CALA9900891 1 19990729 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP GEAR DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12080 47981 INSPECTION FOUND A 1 CRACK IN GEAR DOOR JAMB ANGLE. THE ANGLE WAS REPAIRED IAW SRM 51-35-01. 2 L 7 3 4F A22WE 1999081200157 19990812 00157 NM 1999 8 12 CALA9900892 1 19990729 A 3350 20131A BATTERY PACK RADIANT BOEING 737 7373T0 1384582 NM BS 326,629,753 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 63305 23356 THE EMERGENCY LIGHT BATTERY PACKS AT M1133 STA 326L, M1134 STA 629L, AND M1136 STA 753L FAILED 10 MINUTE DURATION TEST. THE BATTERY PACKS WERE REPLACED. 2 L 7 2 4F RT A16WE 1999081200158 19990812 00158 WP 1999 8 12 9902939991 1 19990726 A 2841 INDICATOR DOUG DC9 DC931 3022065 WP RT FUEL SYS MALFUNCTIONED A NWAA O OTHER N FALSE WARNING UK UNKNOWN 1 GL 01 8957E 47215 EN ROUTE, RIGHT FUEL QUANTITY BEGAN DECREASING FASTER THAN LEFT. CREW DECLARED AN EMERGENCY WITH DESTINATION STATION AN D AIRCRAFT LANDED WITHOUT INCIDENT. MAITNENANCE DEFERRED RIGHT FUEL QUANTITY INDICATION PER MEL 28-7A. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F A6WE 1999081200159 19990812 00159 WP 1999 8 12 9902949858 1 19990724 A 2780 DUCT DOUG DC9 DC951 3022051 WP RIGHT DENTED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 767NC 47724 DURING APPROACH INTO DTW, AIRCRAFT ROLLED TO THE LEFT ON SLAT EXTENSION. CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED SAFELY USING FLAPS ONLY. MAINTENANCE FOUND RIGHT TELESCOPE DUCT DENTED. REPLACED DUCT. OPERATIONAL CHECK NORMAL AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1999081200160 19990812 00160 WP 1999 8 12 9902959750 1 19990723 A 3350 BATTERIES DOUG DC9 DC941 302207N WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 750NW 47114 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS IN COCKPIT AND AT FORWARD LOWER CEILING PANEL INOPERATIVE. REPLACED BATTE RIES IN PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999081200161 19990812 00161 NM 1999 8 12 9902965518 1 19990720 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 518US 23206 DURING SCHEDULED MAINTENANCE, FIRST CLASS EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED POWER SU PPLY WITH A SERVICEABLE UNIT. 2 L 7 2 4F RT A2NM 1999081200162 19990812 00162 NM 1999 8 12 9902975648 1 19990720 A 3520 CONNECTOR BOEING 757 757251 1384970 NM ROW 33DEF FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 548US 26495 DURING SCHEDULED MAINTENANCE, THE OXYGEN MASKS FOR SEATS 33DEF WOULD NOT DEPLOY. MAINTENANCE REPAIRED THE ELECTRICAL CO NNECTION AT THE RELEASE SOLENOID. SUBSEQUENT SYSTEM TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999081200163 19990812 00163 NM 1999 8 12 UPS99230238 1 19990726 A 5320 CLIP BOEING 727 7272A1 138407F NM BS 990 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION ON SHEAR TIE T-CLIP AT BS 990, RBL 8, WL 148 BETWEEN STR 29-29 R (WHILE WORKING CARD 973519) . REMOVED CORRODED T-CLIP AND REPLACED WITH NEW T-CLIP IAW 51-10-1 AND 51-30-02. 2 L 7 3 4F A3WE 1999081200164 19990812 00164 NM 1999 8 12 UPS99230239 1 19990728 A 5314 KEEL BEAM BOEING 727 7272A1 138407F NM BS 982 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C CORROSION (C53-113-01.06-02) BS 982 RT KEEL BEAM. REMOVED CORRODED KEEL BEAM SEGMENT AND REPLACED WIT H NEW SEGMENT IAW ER 99-5790. 2 L 7 3 4F A3WE 1999081200165 19990812 00165 NM 1999 8 12 UPS99230240 1 19990727 A 5313 STRINGER BOEING 727 7272A1 138407F NM BS 1153 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C WHILE WORKING CUST CARD NR 973522 FOUND CORROSION ON STR 20R STA 1153. REMOVED CORRODED STRINGER BS 1 153 AND REPLACED WITH NEW STRINGER IAW SRM 51-40-03, 51-10-1, 51-30-02, DRW NR 65-16349. 2 L 7 3 4F A3WE 1999081200166 19990812 00166 NM 1999 8 12 UPS99230241 1 19990728 A 5330 SKIN BOEING 727 7272A1 138407F NM BS 1005 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:C WHILE WORKING CARD 973519, FOUND CORROSION ON INNER SKIN AT BS 1005, RBL 7, WL 148. REMOVED CORRODED SECTION OF SKIN AT BS 1005, RBL 7, WL 148 AND REPAIRED IAW ER NR 99-5802 AND SRM 53-30-03 FIG 3A. 2 L 7 3 4F A3WE 1999081200167 19990812 00167 NM 1999 8 12 UPS99230242 1 19990729 A 3350 LIGHT BOEING 727 72725C 138400H NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY EXIT LIGHT INOP AT ENTRY DOOR. REMOVED AND REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999081200168 19990812 00168 NM 1999 8 12 UPS99230252 1 19990729 A 3240 BRAKE BOEING 727 727180C 138406G NM RT MLG STICKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 RIGHT BRAKE STICKS AND RELEASES ONLY WITH LARGE THRUST APPLICATION FOLLOWING STOPOVERS WITH PARKING BRAKE APPLIED FOR AP PROX 30 MINUTES. BLED BRAKES ON RT SIDE BRAKES RELEASE NORMALLY. 2 L 7 3 4F A3WE 1999081200169 19990812 00169 WP 1999 8 12 UPS99830237 1 19990717 A 5320 57727866 JAMB DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 270, THE MAIN CARGO DOOR LOWER DOOR JAMB IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE JAMB I AW DWG 5772786 AND SRM 51-1-20D AND 51-1-20. 2 L 7 4 4F RT 4A25 1999081200170 19990812 00170 WP 1999 8 12 UPS99830244 1 19990713 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 418 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FUSELAGE SKIN AT FS 418, LONGERON 21L, IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK866-41 7. 2 L 7 4 4F RT 4A25 1999081200171 19990812 00171 WP 1999 8 12 UPS99830245 1 19990719 A 5347 S493245470T6 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 DOUBLE SEAT TRACK AT FS 440, RBL 48, IS CORRODED OUT BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLI CED IN A NEW SECTION OF SEAT TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999081200172 19990812 00172 WP 1999 8 12 UPS99830246 1 19990718 A 5320 37558401 FITTING DOUG DC8 DC873F 302199F WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 1160, BETWEEN LONGERON 32R AND 33R, THE BATH TUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND R EPLACED FITTING IAW SRM 5-1-20D. 2 L 7 4 4F RT 4A25 1999081200173 19990812 00173 WP 1999 8 12 UPS99830247 1 19990718 A 5320 3754914501 FITTING DOUG DC8 DC873F 302199F WP BS 1220-1230 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 1220 TO 1230, LONGERON 31R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IA W SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999081200174 19990812 00174 WP 1999 8 12 UPS99830248 1 19990719 A 5313 3615532 LONGERON DOUG DC8 DC873F 302199F WP BS 8&35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 BETWEEN FS 35 AND 8 LONGERON 36 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED LONGERO N IAW DWG 3615532 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999081200175 19990812 00175 WP 1999 8 12 UPS99830249 1 19990719 A 5320 46401111 FITTING DOUG DC8 DC873F 302199F WP BS 12 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 AT FS -12, LONGERON 33L FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4640111 AND SRM 51-1-20D, 51-1-21, AND 51-3-0. 2 L 7 4 4F RT 4A25 1999081200176 19990812 00176 WP 1999 8 12 UPS99830250 1 19990721 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 1060 BETWEEN LONGERON 35R AND 36, THE SHEAR-TIE IS CRACKED. CUT OUT DAMAGED SECTION AND REPAIRED SHEAR-TIE IAW SRM 53-2-0 FIG 2B. 2 L 7 4 4F RT 4A25 1999081200177 19990812 00177 WP 1999 8 12 UPS99830251 1 19990726 A 5320 5751516227 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1, THE INTERCOSTAL AT FS 1240 AND LONGERON 33L IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTER COSTAL IAW DWG 5751516 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999081200178 19990812 00178 WP 1999 8 12 ABXA9900611 1 19990629 A 5522 565497013 SKIN DOUG DOUG DC8 DC863 302198A WP RT ELEVATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT ELEVATOR SKIN CORROSION AFT OF NR 1 HINGE. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-21A. 2 L 7 4 4F 4A25 1999081200179 19990812 00179 WP 1999 8 12 ABXA9900612 1 19990629 A 5712 57695813 FORMER DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING, LEADING EDGE, STATION XFS 710 FORMER CRACKED. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-8. 2 L 7 4 4F 4A25 1999081200180 19990812 00180 WP 1999 8 12 ABXA9900613 1 19990629 A 5320 5644981 INTERCOSTAL DOUG DOUG DC8 DC863 302198A WP BS 8 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 SKIN BULGED AND FITTING CRACKED AT STATION 8 AND LONGERON 30 LEFT. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 4641704. 2 L 7 4 4F 4A25 1999081200181 19990812 00181 WP 1999 8 12 ABXA9900614 1 19990629 A 5320 4641704 FITTING DOUG DOUG DC8 DC863 302198A WP BS 4 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 SKIN BULGED AND FITTING CRACKED AT STATION 4 LONGERON 30 LEFT. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 4641704. 2 L 7 4 4F 4A25 1999081200182 19990812 00182 WP 1999 8 12 ABXA9900615 1 19990623 A 5730 57610417 PANEL DOUG DOUG DC8 DC863 302198A WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FOUND CORROSION ON PANEL 520J, RIGHT WING FUEL ACCESS PANEL. FABRICATED REPLACEMENT PANEL IAW DWG 5761041. 2 L 7 4 4F 4A25 1999081200183 19990812 00183 NM 1999 8 12 SCNA99098 1 19990727 A 3350 1102833 LIGHT BOEING 727 7272J4 1384006 NM PAX DOORWAY INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE AFT ENTRY AIRSTAIR EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND INOPERATIVE. REMOVED AN D REPLACED BATTERY HOLDER ASSEMBLY. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 1999081200184 19990812 00184 NM 1999 8 12 SWAA991230 1 19990724 A 2560 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY INTO CONTAINER PER MM. 2 L 7 2 4F RT A16WE 1999081200185 19990812 00185 NM 1999 8 12 SWAA991231 1 19990723 A 5330 6545766 SKIN BOEING 737 7372H4 138448C NM BS 480-515 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED IN 3 PLACES BETWEEN BS 480-515, STRINGER 4L. REPAIRED SKIN PER S RM. 2 L 7 2 4F A16WE 1999081200186 19990812 00186 NM 1999 8 12 SWAA991232 1 19990722 A 3240 26066722 BRAKE BOEING 737 7373H4 1384600 NM RT MLG MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED 1/4D CHECK, TAXING ACFT FOUND RT BRAKE PRESS WEAK AND WITH ANTI-SKID SYSTEM ON INOP. REMOVED AND REPLA CED RT BRAKE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999081200187 19990812 00187 1999 8 12 SWAA991233 4 19990723 A 2565 1061323418 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 AFT SERVICE DOOR EVACUATION SLIDE DEPLOYED ACCIDENTALY. REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999081200188 19990812 00188 NM 1999 8 12 SWAA991234 1 19990724 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED A1 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM. 2 L 7 2 4F RT A16WE 1999081200189 19990812 00189 NM 1999 8 12 SWAA991235 1 19990724 A 5752 654645524C SKIN BOEING 737 7373Q8 1384670 NM RT AILERON TAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED C4 CHECK, FOUND RT AILERON TAB DELAMINATED INBD OF PUSHRODS. REMOVED AND REPLACED AILERON TAB PER MM. 2 L 7 2 4F RT A16WE 1999081200190 19990812 00190 NM 1999 8 12 SWAA991236 1 19990725 A 3350 20131A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD CABIN EMERGENCY EXI T LIGHT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999081200191 19990812 00191 NM 1999 8 12 SWAA991237 1 19990725 A 3350 BPS73 BATTERY CHARGER BOEING 737 737301 1384611 NM PAX DOORWAY INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD EN TRY DOOR SLIDE EMERGENCY LIGHT BATTERY CHARGER ASSY PER MM. 2 L 7 2 4F RT A16WE 1999081200192 19990812 00192 NM 1999 8 12 SWAA991238 1 19990725 A 7933 6915935 TRANSMITTER BOEING 737 7372H4 138448C NM NR 1 ENGINE ERRATIC A SWAA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 083SW 22732 AIR TURNBACK, NR 1 ENGINE OIL TEMP INDICATION ABOVE LIMITS. REMOVED AND REPLACED NR 1 ENG OIL TEMP TRANSMITTER AND REPA IRED CANNON PLUG WIRING AT TRANSMITTER. 2 L 7 2 4F A16WE 1999081200193 19990812 00193 NM 1999 8 12 SWAA991240 1 19990723 A 3240 6544566 LINES BOEING 737 7373H4 1384600 NM RT MLG MISINSTALLED A SWAA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 07 325SW 23689 RT BRAKES FEEL SPONGY AND INEFFECTIVE. REMOVED CAPS AND PLUGS LEFT ON BRAKE LINES AT RT MLG SWIVEL INBD AND OUTBD LINES . RECONNECTED LINES, BRAKES LEAK AND OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999081200194 19990812 00194 1999 8 12 SWAA991241 2 19990726 A 7261 3353109040 SEAL BOEING 737 7373H4 1384600 NM NR 1 ENGINE FAILED A SWAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 306SW 22946 AIR TURNBACK, IN FLIGHT SHUTDOWN. NR 1 ENG OIL QTY DECREASED TO LESS THAN .5 GAL, LOW OIL PRESS LIGHT ILLUMINATED. REM OVED AND REPLACED NR 1 ENG STARTER GEAR PAD SEAL PER MM. 2 L 7 2 4F RT A16WE 1999081200195 19990812 00195 NE 1999 8 12 SWAA991242 2 19990726 A 7200 1285M39P01 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 BIRD STRIKE A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 SW 07 320SW 23341 726229 ABORTED TAKEOFF, NR 2 ENG ENCOUNTERED BIRD STRIKE AND ABORTED THE TAKEOFF AT 110 KNOTS DUE TO VIBRATION ON THE ENG. RE MOVED AND REPLACED NR 35 AND NR 36 DAMAGED FAN BLADES ON NR 2 ENG. ALSO, REMOVED AND REPLACED CSD OIL COOLER PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999081200196 19990812 00196 NM 1999 8 12 SWAA991243 1 19990726 A 3350 6556633 LENS BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED AT MID CABIN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999081200197 19990812 00197 NM 1999 8 12 SWAA991244 1 19990726 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 1 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999081200198 19990812 00198 NM 1999 8 12 SWAA991245 1 19990726 A 3350 07912 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LENS MISSING AT FWD AND AFT ENDS. REPLACED LENSES PER MM. 2 L 7 2 4F RT A16WE 1999081200199 19990812 00199 NM 1999 8 12 SWAA991246 1 19990726 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK CAP END MISSING AT FWD END. REPLACED CAP END PER MM. 2 L 7 2 4F RT A16WE 1999081200200 19990812 00200 NM 1999 8 12 SWAA991247 1 19990727 A 3350 07912 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS MISSING AFT LENS. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999081200201 19990812 00201 NM 1999 8 12 SWAA991239 1 19990726 A 2740 BACB10A353 BEARINGS BOEING 737 7372H4 138448C NM STAB TRIM WORN A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 055SW 21593 AIR TURNBACK, STAB TRIM MECHANISM MAKES GRINDING NOISE WHEN MOVED. REMOVED AND REPLACED WORN BEARINGS ON RT SIDE OF STA B TRIM MECHANISM. 2 L 7 2 4F A16WE 1999081200202 19990812 00202 NM 1999 8 12 SWAA991248 1 19990727 A 5712 BAC15201456 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED 1/2D CHECK, FOUND .250 INCH LONG CRACK ON RT WING RIB LOWER CHORD, WBL 135.5. REPAIRED RIB PER SWA RA NR 1-357-0730. 2 L 7 2 4F RT A16WE 1999081200203 19990812 00203 NM 1999 8 12 SWAA991249 1 19990727 A 3350 311500 LENS BOEING 737 7372H4 138448C NM LT EMER EXIT MELTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND LT WING EGRESS LIGHT LENS SECTION MELTED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F A16WE 1999081200204 19990812 00204 NM 1999 8 12 SWAA991250 1 19990728 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 27L, BS 986. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999081200205 19990812 00205 NM 1999 8 12 SWAA991251 1 19990728 A 3350 65C27095 BATT CHARGER BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND FWD CENTER AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM. 2 L 7 2 4F A16WE 1999081200206 19990812 00206 NM 1999 8 12 SWAA991252 1 19990728 A 5751 65C25915 ANGLE BOEING 737 7373H4 1384600 NM RT AILERON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C4 CHECK, FOUND RT WING AILERON 3RD RIB SUPPORT ANGLE CRACKED APPROX 1.5 INCH LONG. REPAIRED RIB SUPPO RT ANGLE PER SWA RA NR 1-357-0729. 2 L 7 2 4F RT A16WE 1999081200207 19990812 00207 NM 1999 8 12 SWAA991253 1 19990728 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 509SW 24186 DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHT STRIPS LOOSE AND WIRES EXPOSED. RESECURED STRIPS, WIRES, AND REPLACED DAMA GED COVERS. 2 L 7 2 4F RT A16WE 1999081200208 19990812 00208 NM 1999 8 12 SWAA991254 1 19990728 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED ON RBL 5.7, WL 213-214. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999081200209 19990812 00209 NM 1999 8 12 SWAA991255 1 19990729 A 7930 42D107A1 SWITCH BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED A SWAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 07 080SW 22675 687783 DIVERTION IN FLIGHT SHUT DOWN. NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED AND WOULD NOT GO OUT. REMOVED AND REPLACED NR 1 ENG MAIN OIL FILTER AND OIL FILTER BYPASS LIGHT SWITCH PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999081200210 19990812 00210 NM 1999 8 12 SWAA991256 1 19990729 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 25L CORRODED ON AFT SIDE OF BS 967. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999081200211 19990812 00211 NM 1999 8 12 SWAA991257 1 19990729 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM MID CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C2 CHECK, FOUND LT EMERGENCY EXIT OVERWING DOOR LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999081200212 19990812 00212 NM 1999 8 12 SWAA991258 1 19990729 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CONTAMINATED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED C2 CHECK, FOUND MOISTURE INSIDE EMERGENCY LIGHT LENS ON AFT ENTRY DOOR AREA. REMOVED, CLEANED, AND RES EALED LENS AT LIGHT. 2 L 7 2 4F RT A16WE 1999081200213 19990812 00213 NM 1999 8 12 SWAA991259 1 19990729 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND THROUGH UT INSPECTION, A 1 INCH LONG CRACK AT BS 178 BULKHEAD RH SIDE, WL 200. REPAI RED PER SRM. 2 L 7 2 4F RT A16WE 1999081200214 19990812 00214 NM 1999 8 12 SWAA991260 1 19990729 A 3350 101073 LENS BOEING 737 7377H4 NM GALLEY MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 700GS 27835 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING ON FWD GALLEY AREA. REMOVED AND REPLACED LENS PER MM . 2 L 7 2 4F RT A16WE 1999081200215 19990812 00215 NM 1999 8 12 TWAA9910801 1 19990801 A 3350 363673 LIGHT BOEING 727 727231 1384079 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 84355 21987 THE AFT SECTION OF THE CABIN EMERGENCY EGRESS LIGHTS FAILED TO ILLUMINATE. REPLACED THE EGRESS LIGHT STRIP. CHECK-C 2- 26-99 MCI. 2 L 7 3 4F A3WE 1999081200216 19990812 00216 WP 1999 8 12 TWAA9910802 1 19990730 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP ROW 29 INOP A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 922TW 48013 THE EGRESS LIGHTS ILLUMINATED IN FLIGHT WITH THE SWITCH IN THE ARM POSITION, FROM ROW 29 TO THE BACK OF THE CABIN. REPL ACED THE POWER SUPPLY. CHECK-C 7-17-99 STL. 2 L 7 2 4F A6WE 1999081200217 19990812 00217 NM 1999 8 12 HNAA9900108 1 19990731 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOP A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 911HA 034 FIRST EMERGENCY LIGHT (FWD) ON FLOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999081200218 19990812 00218 NM 1999 8 12 PCAA9900025 1 19990729 A 3260 SWITCH DHAV DHC8 DHC8102 2809003 NM RT MLG MALFUNCTIONED A PCAA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 EA 13 962HA 331 MVY-LGA, FLT 3690-ON APPROACH INTO LGA, THE RIGHT MAIN GEAR LIGHT ILLUMINATED RED. CREW PERFORMED A GO AROUND, CYCLED T HE GEAR AND THE LIGHT INDICATED DOWN AND LOCKED. MAINTENANCE PERFORMED A PSEU TEST AND FOUND NO FAULTS. CLEANED DRAG S TAY PROXIMITY SWITCH, CHECKED GAPS. CLEANED PROX SWITCH HARNESS CANNON PLUG IN FORWARD NACELLE. OPS CHECK GOOD. A/C R ETURNED TO SERVICE. PROBLEM REOCCURED ON GROUND 31 JULY, MAINTENANCE REPLACED THE DOWN LOCK PROXIMITY SWITCH AT THAT TI ME. TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999081200219 19990812 00219 EA 1999 8 12 JBX9900095 1 19990801 A 7933 MS280343 TEMP BULB CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE RT ENGINE INOP A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 571ML 7209 872260 RIGHT ENGINE OIL TEMP RED LINED AT 163 DEGREES. AT IDLE, TEMP DECREASED TO NORMAL RANGE. ADVANCED THRUST, TEMP REMAINE D IN GREEN THEN CLIMED BACK TO 163 DEGREES. RETURNED ENGINE TO IDLE, AND LANDED BACK AT RDU WITH NORMAL OIL TEMP. REMO VED AND REPLACED NR 2 ENGINE OIL TEMP BULB. NO DEFECTS NOTED. ALL WORK ACCOMPLISHED IAW CL-65 MM 79-31-01. AIRCRAFT R ELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200220 19990812 00220 NM 1999 8 12 RAAA99B1015 1 19990725 A 3350 862104 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM EMER EXIT DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 MID CABIN DOOR EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999081200221 19990812 00221 NM 1999 8 12 RAAA99B1016 1 19990725 A 3350 873100212 SIGN BOEING 727 72722C 138400F NM PAX DOOR FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 FORWARD PAX DOOR EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY DUE FAILED. 2 L 7 3 4F A3WE 1999081200222 19990812 00222 NM 1999 8 12 RAAA99B2050 1 19990725 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 2 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 2 PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999081200223 19990812 00223 SO 1999 8 12 RAAA99E8048 1 19990721 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 69 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SERVICE CHECK, FOUND LEFT WING UPPER SURFACE NR 3 AND 4 PANELS CRACKED AND CORRODED WS 69 AT WING TO FUSELAGE FIL LET ATTACH HOLES FROM RISER 15 THROUGH TO RISER 28. INSTALLED REPAIR TO LT WING UPPER SURFACE PANELS 3 AND 4 BS 65 TO W S 101L PER RAAA ECO 99-06 LUNDBY DESIGN SERVICES DRAWINGS NR 188355 AND 188275. 2 L 7 4 4T 4A22 1999081200224 19990812 00224 SO 1999 8 12 RAAA99E8049 1 19990721 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 70 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING WING REPAIR WORK, FOUND LEFT WING UPPER SURFACE NR 6 WING PANEL CRACKED AND CORRODED WS 70 BETWEEN RISERS 36 AND 37. REPAIRED IAW LOCKHEED CALIFORNIA CALIFORNIA CO DRAWING 841796 (88/SK-678). 2 L 7 4 4T 4A22 1999081200225 19990812 00225 EU 1999 8 12 QXEA901520 1 19990726 A 3350 5515800106 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 477AU 11226 PDX - EXIT LIGHT OVER COCKPIT IS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL TEST PERFORMED, TES TED GOOD. 2 L 7 2 4F RT A20EU 1999081200226 19990812 00226 EU 1999 8 12 QXEA9901519 1 19990725 A 3350 XB864041 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8B DETACHED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 475AU 11222 SEA - PLASTIC AISLE EXIT SIGN DETACHED AT SEAT 8B. MAINTENANCE REPLACED EXIT LIGHT ASSEMBLY. OPERATIONAL TEST PERFORME D, TESTED GOOD. 2 L 7 2 4F RT A20EU 1999081200227 19990812 00227 NM 1999 8 12 99FDEA00299 1 19990730 A 3260 SWITCH BOEING 727 727247 138408F NM LANDING GEAR INOP A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 235FE 21329 99-184 - 1ST ATTEMPT TO LWR MLG RECEIVED LEFT AND NOSE UNSAFE IND, 2ND ATTEMPT ALL 3 MLG IND DOWN AND LOCKED. REMOVED A ND REPLACED NOSE GEAR, LMG DOWN LOCK SENSOR,32-61-91, POSITION SWITCH PER MM 32-61-71. 2 L 7 3 4F A3WE 1999081200228 19990812 00228 NM 1999 8 12 99FDEA00300 1 19990730 A 2612 652492 CONTROL UNIT BOEING 727 727233 138408A NM E&E COMPT FAILED A FDEA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 272FE 22037 99-185 - NR 3 ENG STRUT OH LIGHT ILLUMINATED, RAN RED TABS CKLIST. REMOVED AND REPLACED FIRE AND HEAT DETECTION CONTROL LER, PER MM 26-14-000-1. OPS CK GOOD. 2 L 7 3 4F RT A3WE 1999081200229 19990812 00229 NM 1999 8 12 99FDEA00301 1 19990731 A 2782 ACTUATOR BOEING 727 727247 138408F NM LE SLAT FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 25 235FE 21329 99-186 - 'A' SYSTEM HYDRAULIC QUANTITY FELL TO ZERO. PRESSURE OK AT 3000 PSI. COMPLIED WITH LOSS OF 'A' SYSTEM RED TAB LS. REMOVED AND REPLACED TWO WING PANELS AT LT NR 4 SLAT ACTUATOR. REMOVED AND REPLACED NR 4 LEADING EDGE SLAT ACTUATO R PER BOEING MM 27-81-32-4. 2 L 7 3 4F A3WE 1999081200230 19990812 00230 NM 1999 8 12 99FDEA00302 1 19990731 A 5320 651596914 FITTING BOEING 727 72722 1384002 NM BS 740 CRACKED A FDEA K NONE O OTHER NR NOT REPORTED 1 SO 25 187FE 19079 CRACK IN RIGHT HAND BS 740 FRAME FITTING. CRACK FOUND BEYOND REPAIRABLE LIMITS (EA 7-5310-40339 ISSUED) MAJOR REPAIR. * S/D* REPLACED FRAME (P/N 65C137724-92). 2 L 7 3 4F A3WE 1999081200231 19990812 00231 NE 1999 8 12 DL72S991693 2 19990728 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 485DA 54202 20865 700434 NR 2 ENG OIL PRESS SLOWLY DECREASED TO ZERO WITH ASSOCIATED LOW OIL PRESS LIGHT ON. GOOD QTY AND TEMP. REPLACED ENGINE . 2 L 7 3 4F 4 F A3WE E2EA 1999081200232 19990812 00232 WP 1999 8 12 DLL13991707 1 19990729 A 2612 SENSOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENGINE SHORTED A DALA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 27 790DL 193A1143 010243 ON DESCENT, NR 3 ENG 'A' LOOP FIRE LIGHT AND 'B' LOOP ON MCO. ENGINE SHUTDOWN, FIRED BOTH EXT BOTTLES, STILL HAD A LOOP LIGHT. REPLACED UPPER AND LOWER FAN CASE LOOPS AND GEARBOX LOOP. 2 L 7 3 4F 4 F A23WE E12EU 1999081200233 19990812 00233 NM 1999 8 12 DL72S991708 1 19990730 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM ROW 21 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 421DA 21274 ON SVC CK, FOUND CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN AT ROW 21 INOP. REPLACED BATTERY PACK, OPS NML. 2 L 7 3 4F A3WE 1999081200234 19990812 00234 NE 1999 8 12 DL72S991711 2 19990730 A 7321 FUEL CONTROL 7436025 BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 27 515DA 82343 21431 NR 1 ENGINE STARTED FLUX PLUS OR MINUS .2 EPR WITH ALL OTHER ENGINE INSTRUMENTS ALSO. REPLACED NR 1 ENGINE FUEL CONTROL RAN ENG, OPS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999081200235 19990812 00235 NM 1999 8 12 DL73K991714 1 19990731 A 3350 BATTERY BPS73 BOEING 737 737232 1384475 NM ROW 18 DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 304DL 1110 23076 EMERGENCY LIGHT AT 18D AND 2R DOOR ON. REPLACED CHARGER RACK AND BATTERY. 2 L 7 2 4F RT A16WE 1999081200236 19990812 00236 NM 1999 8 12 DL73K991715 1 19990731 A 2740 W326311 WIRE BOEING 737 737232 1384475 NM BS 1088 FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 319DL 23091 STAB TRIM CONTROL WHEEL SWITCHES INOP. POPS ACTUATOR C/B. AUTOPILOT TRIM IS OK. FOUND WIRES SHORTED TO GROUND AT BULK KHEAD 1088. REPAIRED WIRE WITH SPLICES. WIRE NRS W326-313, W326-312, W326-311 PER BOEING STANDARD WIRING PRACTICES M ANUAL. 2 L 7 2 4F RT A16WE 1999081200237 19990812 00237 NM 1999 8 12 DL767991716 1 19990731 A 2421 IDG BOEING 767 767232 1385132 NM NR 2 ENGINE REQUIRED SERVICE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 27 103DA 22215 RT GEN FIELD TRIPPED ON T/O ROLL, ABORTED T/O AT 80 KNOTS. RAN NR 2 ENG, DISCONNECTED RT IDG. VERIFIED NO VOLTS AND FR EQS. SERVICED IDG WITH OIL. 2 L 7 2 4F RT A1NM 1999081200238 19990812 00238 1999 8 12 DL757991719 4 19990730 A 2565 D30656126 LANYARD BOEING 757 757232 1384965 NM L 4 DOOR SLIDE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 671DN 25332 L-4 SLIDE SAFETY LANYARD FOUND BROKEN DURING ACCOMPLISHMENT OF EO 6-71325-3AD. REPLACED SLIDE ASSY. 2 L 7 2 4F RT A2NM 1999081200239 19990812 00239 1999 8 12 DL73E991724 4 19990801 A 3442 RADAR TR UNIT MI585161 BOEING 737 7372S3 NM E/E COMPT INOP A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 369DL 2664 21776 WX RADAR ANT FLASHING ON SCREEN. NO RADAR AVAILABLE. REPLACED WX RARAR TRANSCEIVER. 2 L 7 2 4F RT A16WE 1999081200240 19990812 00240 SO 1999 8 12 SWIA971524 1 19990703 A 3520 MASK EMB 120 EMB120RT SO PWA 118 PW118 NE ROW 7 MALFUNCTIONED A SWIA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 NM 07 162CA 120150 ROW 7 OXYGEN MASKS FELL DOWN. RETURNED TO SEA. SECURED OXYGEN MASK. EXAMINED LATCHING DEVICE AND FOUND NO DEFECTS. O PS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081200241 19990812 00241 SO 1999 8 12 SWIA971525 1 19990703 A 3260 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 187SW 120037 RED TRANSIT LIGHT A WOULD NOT EXTINGUISH ON RETRACTION. RETURNED TO SLC. CLEANED CORRODED CANNON PLUGS ON LEFT GEAR CA NNON PLUGS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081200242 19990812 00242 SO 1999 8 12 SWIA971526 1 19990704 A 3260 SWITCH EMB 120 EMB120RT SO PWA 118 PW118A NE RT MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 271YV 120271 INFLIGHT UPON GEAR RETRACTION, NEEDED TO USE DN LOCK RELEASE OVERRIDE TO BRING GEAR HANDLE UP. UPON FLAP RETRACTION, TR IPLE CHIME AURAL WARNING FLAP ANNUNCIATED CONTINUIOUSLY. AGAIN WHEN THE AUTO FX SWITCH WAS TURNED OFF, WARNINGS CONTINU ED. RETURNED TO PSP. PERFORMED GEAR SWING. FOUND GEAR WOULD NOT SWING WITHOUT OVERRIDE BUTTON. WITH NLG PROX SENSOR SLAVED IN AND TARGETED, GEAR SWINGS OK. REPLACED SENSOR, BUT SWING CHECKS BAD. CHECKED HARNESS WITH A NEW SENSOR AND C HECK OK. CHECKED TARGET THROUGH PROX SENSOR, TARGET NOT USEABLE. REPLACED RIGHT UPLOCK PROXIMITY SWITCH. OPS CHECKS G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081200243 19990812 00243 SO 1999 8 12 SWIA971527 1 19990706 A 2150 VENTURI EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT PACK FAILED A SWIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 293SW 120320 RED DUCT LEAK LIGHT ILLUMINATED (LEFT SIDE) IN FLIGHT. RETURNED TO AIRPORT. REPLACED FLOW LIMITING VENTURI ON LEFT PAC K ASSY. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081200244 19990812 00244 SO 1999 8 12 SWIA971528 1 19990707 A 2150 CLAMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HEAT EXCHANGER LOOSE A SWIA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 NM 07 293SW 120320 LEFT ENGINE DUCT LIGHT ILLUMINATED DURING CLIMB-OUT. RETURNED TO PSP. REMOVED PANELS, TIGHTENED CLAMP ON HEAT EXCHANGE R. REPLACED BOTH SENSORS IN LEFT PACK AREA. RAN ENGINES AND APU. NO DUCT LEAK LIGHT AT THIS TIME. INSTALLED ALL REMO VED PANELS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081200245 19990812 00245 SO 1999 8 12 SWIA971529 1 19990708 A 3610 32144143 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT FAILED A SWIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 293SW 120320 LEFT DUCT LEAK AFTER TAKEOFF. RETURNED FOR LANDING IN PSP. CHECKED FOR DUCT LEAK IN LEFT WING INBOARD LEADING EDGE TO LEFT AIR-CONDITIONING PACK. FOUND LEFT AIR-CONDITIONING PRESSURE REGULATOR/SHUT-OFF BLEED LEAKING BLEED AIR. REPLACED LEFT PRESSURE REGULATING SHUT-OFF BLEED VALVE. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081200246 19990812 00246 NE 1999 8 12 CKSA99071 2 19990729 A 7200 ENGINE BOEING 747 747269B NM PWA JT9 JT9D7 52054 NE NR 3 MALFUNCTIONED A CKSA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 23 707CK 21541 689476 DURING CLIMB AT ALT 28.0, HEARD LOUD BANG JARRING ACFT. NR 3 ENG FAILURE. TIME 2345Z, 21 MIN INTO CLIMB. CLEAR AIR, N O ICING. AIRSPEED 300 KTS, OIL TEMP 130 DEGREES, EGT NORMAL, ENG IGNITION ON, ANTI-ICE OFF, OIL PRESSURE WENT TO 0 SHOR TLY AFTER SHUTDOWN (NO RESTART ATTEMPT). 2 L 7 4 4F 4 F RT A20WE E20EA 1999081200247 19990812 00247 NM 1999 8 12 TWAA9910901 1 19990802 A 3350 6100928 LAMP BOEING 767 767330 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 FOUND THE EGRESS LIGHT INOPERATIVE AT CABIN ROW 1 LT AND RT SIDES, ROW 24 RT SIDE AND 37 RT SIDE. REPLACED THE LAMP AT EACH LOCATION. CHECK-C 5-2-99 MCI. 2 L 7 2 4F RT A1NM 1999081200248 19990812 00248 WP 1999 8 12 TWAA9910902 1 19990727 A 5330 LONGERON DOUG DC9 DC983 3022083 WP BS 256 MISREPAIRED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9413T 53188 DURING CHECK-C MAINT, A 9 INCH BY 9 INCH CLASS 3 REPAIR, FOUND INSTALLED WITH BLIND FASTENERS AT STA 256, WL 209 AND LON GERON 17L, WAS DAMAGED. REPAIRED LONGERON 17L, STA 256, PER SRM 53-02 PAGE 48, FIG 18. REPAIRED CLASS 3 REPAIR PER SRM 53-04, PAGE 39 FIG 12B AND SHEET 4. 2 L 7 2 4F RT A6WE 1999081200249 19990812 00249 WP 1999 8 12 TWAA9910903 1 19990728 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 1193 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9413T 53188 DURING CHECK-C MAINT, FOUND .5 INCH BY 0.080 DEEP AND .4375 INCH LONG BY 0.076 DEEP DENTS IN SKIN AT STA 1193, LONGERON 20L. TWO DENTS WITHIN .5 INCH OF EACH OTHER. ACCOMP HFEC CHECK PER 51-00-03, PART 6 AND NO CRACKS FOUND. REPAIRED PER SRM 53-04, FIG 38 PAGE 218K. 2 L 7 2 4F RT A6WE 1999081200250 19990812 00250 WP 1999 8 12 TWAA9910904 1 19990726 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 617 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND FLOORBEAM SUPPORT ANGLE CRACKED AT STA 617, RBL 23 INCHES. REPLACED PARTS PER SPM 6-70- 01, PAGE 3. 2 L 7 2 4F A6WE 1999081200251 19990812 00251 WP 1999 8 12 TWAA9910905 1 19990723 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CABIN STRINGER 2L CRACKED AT FORMER STA 200. REPLACED CRACKED SECTIONS AND INSTALLED SP LICE PER SRM 53-02, PAGE 48 FIG 18, STA 188 TO 229. 2 L 7 2 4F A6WE 1999081200252 19990812 00252 WP 1999 8 12 TWAA9910906 1 19990727 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND STRINGER 4L CRACKED AT FORMER STA 200. REPLACED STRINGER FROM APPROX STA 230 TO 170. I NSTALLED REPAIR SPLICE AT STA 170 PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1999081200253 19990812 00253 WP 1999 8 12 TWAA9910907 1 19990728 A 5320 FORMER FOOT DOUG DC9 DC931 3022065 WP BS 1109 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND A CRACK AT THE FORMER FOOT AT THE AFT SIDE OF FORMER STA 1109, EIGHT INCHES RIGHT SIDE O F LONGERON 1. INSTALLED NEW FORMER FOOT PER SRM 51-30-2 AND SRM 51-30-5, AND TWA SPM 6-70-01. 2 L 7 2 4F A6WE 1999081200254 19990812 00254 WP 1999 8 12 TWAA9910908 1 19990728 A 5320 FORMER FOOT DOUG DC9 DC931 3022065 WP BS 1109 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CRACK AT FORMER FOOT AT AFT SIDE OF FORMER STA 1109, 10 INCHES LT SIDE OF LONGERON NUMBE R 1. INSTALLED NEW FORMER FOOT PER SRM 51-30-2 AND SRM 51-30-5, AND TWA SPM 6-70-01. 2 L 7 2 4F A6WE 1999081200255 19990812 00255 WP 1999 8 12 TWAA9910909 1 19990729 A 5320 S128742512000 ANGLE DOUG DC9 DC931 3022065 WP BS 929 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND ANGLE FROM FLOORBEAM TO INTERCOASTAL CRACKED AT STA 929, RBL 23 INCHES. REPLACED EXTRUS ION PER SPM 6-70-01, PAGES 2 AND 3. 2 L 7 2 4F A6WE 1999081200256 19990812 00256 WP 1999 8 12 TWAA9910910 1 19990729 A 5311 99115055 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CRACK IN FRAME NUMBER 9911505-5 ALONG RIVETS APPROXIMATELY 1.25 INCHES IN LENGTH, FWD OF LT CENTER WINDSHIELD POST, STA 83.5 AT X=+10. REPAIRED FRAME PER SRM 53-03, FIG 34. 2 L 7 2 4F A6WE 1999081200257 19990812 00257 WP 1999 8 12 TWAA9910911 1 19990729 A 5311 99115056 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CRACK IN RADIUS OF FRAME 9911505-6 APPROXIMATELY .75 INCH IN LENGTH, FWD OF RT CENTER WI NDSHIELD POST, STA 83.5 AT X=-10. REPAIRED FRAME PER SRM 53-05, FIG 34. 2 L 7 2 4F A6WE 1999081200258 19990812 00258 WP 1999 8 12 AT9900540 1 19990729 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 737-756 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE LEFT CUSP WEB AT BS 737-756 WITH CORROSION AND CRACKS. FABRICATE D NEW CUSP WEB, TRIMMED AND DRILLED TO FIT, ALODINED AND PRIMED IAW DC9 SRM 51-10-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999081200259 19990812 00259 WP 1999 8 12 AT9900541 1 19990729 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 149 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD CABIN GALLEY AREA AT BS 149 L-18R AT CUSP LINE LOWER FRAM E WEB AND ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING, CLEAN CORROSION ON LOWER WEB WITHIN LIMITS, TREATED AN D PRIMED AREAS IAW DC9 SRM 51-10-3, 53-01 FIG. 1, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 1999081200260 19990812 00260 WP 1999 8 12 AT9900542 1 19990718 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 198-205 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD CABIN OUTBOARD SEAT TRACK AT BS 198-205 RBL-44 CORRODED. REMOVED SEAT TRACK, CUT, DRILLED, TRIMMED SECTION, ALODINED, PRIMED AND INSTALLED SPLICE IAW DC9 SRM 53-20-1, 53-05 FIG 4F, 51-10-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999081200261 19990812 00261 WP 1999 8 12 AT9900543 1 19990718 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 198-206 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE CABIN RIGHT INBOARD SEAT TRACK AT 198-206 RBL-22 CORRODED. REMOV ED SEAT TRACK, LOCATED AND DRILLED, TRIMMED, COUNTERSUNK, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-4, 51-30-1, 51-10-3, AND 53-05 FIG 4B. 2 L 7 2 4F A6WE 1999081200262 19990812 00262 WP 1999 8 12 AT9900544 1 19990722 A 5753 SKIN DOUG DC9 DC932 3022066 WP RT TE FLAP CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT WING FLAP 25 AND 27 INCHES OUTBOARD OF INBOARD FLAP ACTUATO R CORRODED. REMOVED FASTENERS, BURNISHED CORROSION, FABRICATED DOUBLER, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 57-03 FIG 7. 2 L 7 2 4F A6WE 1999081200263 19990812 00263 WP 1999 8 12 AT9900545 1 19990727 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 180-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD ENTRY FLOOR PANEL AT BS 180-200 CORRODED. FABRICATED FLO OR BOARD, DRILLED, DEBURRED, COUNTERSUNK, DRILLED AND INSTALLED HAT CHANNELS PARTS, AND INSULATION IAW DC9 SRM 53-01 FI G.1, 51-10-4, 51-30-2, AND 53-21-0. 2 L 7 2 4F A6WE 1999081200264 19990812 00264 WP 1999 8 12 AT9900546 1 19990725 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT WING LEADING EDGE PANEL NR 1219A CORRODED AND ANGLE SUPPORT CHAFFED. REMOVED CORROSION, BLEND OUT GOUGE, FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 5 1-30-2, AND 57-01 FIG 1. 2 L 7 2 4F A6WE 1999081200265 19990812 00265 WP 1999 8 12 AT9900547 1 19990721 A 5347 TIE DOWN TRACK DOUG DC9 DC932 3022066 WP BS 937-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE AFT PIT TIE DOWN TRACK AT BS 937-996 WITH CORROSION. REMOVED COR ROSION, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED, AND INSTALLED NEW SECTION IAW DC9 SRM 51-10-4, 51-30-1, AND 51- 10-3. 2 L 7 2 4F A6WE 1999081200266 19990812 00266 WP 1999 8 12 AT9900548 1 19990721 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE CABIN FLOOR PANEL NR 99 AT BS 200 CORRODED. REMOVED CORROSION, F ABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED DOUBLER IAW DC9 SRM 51-10-3, 51-10-4, AND 53- 01. 2 L 7 2 4F A6WE 1999081200267 19990812 00267 WP 1999 8 12 AT9900549 1 19990725 A 5347 TIE DOWN TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CORROSION ON FOUR OF THE FORWARD CARGO PIT TRACK TIE DOWNS. REMOVED CORROSION, DRILLED, AND COUNTERSUNK STRAPS, TREATED, AND PRIMED IAW DC9 SRM 51-10-3, 53-01, AND 51-10-4. 2 L 7 2 4F A6WE 1999081200268 19990812 00268 WP 1999 8 12 AT9900550 1 19990724 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CABIN FLOOR SUPPORT AT BS 200-237 LBL-15 CORRODED. REMOVED AND REPLA CED FLOOR SUPPORT, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 51-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1999081200269 19990812 00269 EU 1999 8 12 MALA976523 1 19990727 A 3260 BULBS SAAB SF340 340B 7860101 EU LT&RT MLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 428XJ 428 ON APPROACH INTO ABR, BOTH LEFT AND RIGHT MAIN GEAR DOWN INDICATORS FAILED. THE QRH WAS COMPLETED AND IT WAS DETERMINED TO BE ALL FOUR LIGHT BULBS NOT ILLUMINATING. CREW SUBSTITUTED LIGHT BULBS AND LANDED IN ABR. MAINTENANCE CONFIRMED LI GHT BULBS BURNT OUT ON LEFT AND RIGHT INDICATORS, RELAMPED INDICATORS. RETURNED INVERTER LAMPS BACK TO ORIGINAL POSTION . LANDING GEAR LIGHT CHECKS OKAY, AS WELL AS INVERTER LIGHTS. OBSERVED CREW PREFORM FUNCTIONAL CHECK ON INVERTER, LIGH T EXTINGUISHES WHEN ON AND ILLUMINATES WHEN OFF. 2 L 7 2 4T RT A52EU 1999081200270 19990812 00270 EU 1999 8 12 MALA976524 1 19990729 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A MALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 590MA 340B181 CARGO SMOKE WARNING ILLUMINATED ON THE GROUND INTERMITTENTLY. MAINTENANCE REPLACED CARGO SMOKE DETECTOR IAW SAAB AMM 26 -13-15-4. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999081200271 19990812 00271 1999 8 12 MALA976525 4 19990729 A 2210 AUTO PILOT BAC 146 AVRO146RJ85A 1500097 EU E&E COMPT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 503XJ E2310 ON CLIMB-OUT FROM MEM, TRP, FD, YDI AND A/T SHUTDOWN, THEN LOST YDI AND FGC1, GOT YELLOW HI TEMP, THEN GOT BRAKE ACC HI TEMP. RETURNED TO MEM. MAINTENANCE CYCLED A/C AVIONICS MASTERS AND AUTO PILOT MASTER SWITCHES. RAN THROUGH RESET OF M CP, TRP, AND AUTO THROTTLE. ALL TESTS PASS AND LIGHTS EXTINGUISHED. TAXIED AIRCRAFT TO RUN UP AREA AND RAN WITH ALL HY DRAULICS ON FOR 1 HOUR, NO FAULTS NOTED. HYDRAULIC FLUID COLOR AND QUANTITY OK. 2 H 7 4 4F RT A49EU 1999081200272 19990812 00272 EU 1999 8 12 MALA976526 1 19990729 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 414XJ 340B414 EMERGENCY FLOOR LIGHTING IS LOOSE. MAINTENANCE INSTALLED NEW SECTION OF FLOOR TRACK LIGHTING. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999081200273 19990812 00273 EU 1999 8 12 MALA976527 1 19990729 A 3244 50104882 TIRE SAAB SF340 340B 7860101 EU RT MLG FAILED A MALA O OTHER O OTHER LD LANDING 1 GL 15 412XJ 340B412 BLEW RIGHT OUTBOARD TIRE ON LANDING. MAINTENANCE REPLACED RT OUTBOARD AND INBOARD TIRES AND RT OUTBOARD BRAKE ASSEMBLY. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999081200274 19990812 00274 WP 1999 8 12 PNSA990701 2 19990706 A 7261 2719301001 SEAL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE WORN A PNSA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 175SW AC621 P44367C WHILE TAXIING TO RUNWAY WITH LT ENGINE RPM AT LOW, OIL TEMPURATURE CLIMBED TO RED LINE. AIRCRAFT RETURNED TO GATE. REP LACED ASPIRATOR SEAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 1999081200275 19990812 00275 NE 1999 8 12 PNSA990702 2 19990703 A 7322 FUEL CONTROL WOODWARD 6068T72P23 SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A PNSA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 AL 03 685PA WYG92784 212 DURING START SEQUENCE OF RT ENGINE AT 50 PERCENT NG ENGINE FLAMED OUT. REPLACED FUEL CONTROL. 2 L 7 2 4T 4 T RT A52EU E8NE 1999081200276 19990812 00276 WP 1999 8 12 CALA9900920 1 19990731 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LOWER SURFACE OF CUSP WEB CORRODED UNDER AND AROUND GALLEY SUPPORT BRACKET AT FS 218, RBL 12. THE CORR ODED AREA OF CUSP WEB WAS CUT OUT IAW SRM 53-01, FIGURE 4 AND A REPAIR WAS INSTALLED IAW SRM 51-30-05. 2 L 7 2 4F A6WE 1999081200277 19990812 00277 WP 1999 8 12 CALA9900921 1 19990731 A 5320 WINDOW FRAME DOUG DC9 DC982 3022082 WP BS 1022-1041 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A .5 INCH CRACK IN UPPER AFT CORNER OF WINDOW FRAME ON RT SIDE BETWEEN STA 1022 AND 1041. THE CRACK WA S STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1999081200278 19990812 00278 WP 1999 8 12 CALA9900922 1 19990731 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND CORROSION ON SUBFLOOR AT STA 160, LBL 10 TO LBL 18. THE SUBFLOOR AND FLOOR SUPPORT WERE REMOVED AND RE PAIRS WERE INSTALLED IAW SRM 51-30-1, 51-10-03, 51-30-2, 51-30, 51-10-2, 53-11-1, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 1999081200279 19990812 00279 WP 1999 8 12 CALA9900923 1 19990731 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND SUBFLOOR CORRODED AT STA 148, BL 0. THE SUBFLOOR WAS REMOVED IAW SRM 51-30-2 AND A NEW ONE WAS INSTALL ED IAW SRM 51-10-2, 53-11-1, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999081200280 19990812 00280 WP 1999 8 12 CALA9900924 1 19990731 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 150-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND SUBFLOOR AT FORWARD SERVICE DOOR ENTRANCE GIRT BAR ATTACH STRUCTURE CORRODED FROM STA 150 TO 200, LBL 5 8. THE SUBFLOOR WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-1, 51-10-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999081200281 19990812 00281 WP 1999 8 12 CALA9900925 1 19990731 A 5711 SPAR DOUG DC9 DC982 3022082 WP WS 331 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND RT WING REFUELING STA WING FRONT LOWER SPAR WORN IN TWO AREAS WHERE ACCESS DOOR LATCHES AT XRS 331. TH E WORN AREAS WERE CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 57-06, FIGURE 10. 2 L 7 2 4F A6WE 1999081200282 19990812 00282 WP 1999 8 12 CALA9900926 1 19990731 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1291 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 2 CRACK IN LONGERON 14R AT FS 1291. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WA S INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 53-02-18. 2 L 7 2 4F A6WE 1999081200283 19990812 00283 WP 1999 8 12 CALA9900927 1 19990731 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 750-807 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LEFT INBOARD SEAT TRACK CORRODED FROM STA 750-807, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, SHEET 1-2. 2 L 7 2 4F A6WE 1999081200284 19990812 00284 NM 1999 8 12 CALA9900928 1 19990731 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 327 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND FORWARD LAV FLOORBEAM CORRODED AT STA 327, RBL 44-60. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03889. 2 L 7 3 4F RT A3WE 1999081200285 19990812 00285 WP 1999 8 12 CALA9900929 1 19990801 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 150 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 6 INCH CRACK IN SUBFLOOR AT STA 150, LBL 12. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED I AW SRM 51-10-4, 51-30-2, AND 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1999081200286 19990812 00286 WP 1999 8 12 CALA9900930 1 19990801 A 5754 BRACKET DOUG DC9 DC982 3022082 WP NR 10 LE SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A GOUGE IN LT WING SLAT NR 0 O/B END AFT ATTACH BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW OVER HAUL MANUAL 27-80-01. 2 L 7 2 4F A6WE 1999081200287 19990812 00287 WP 1999 8 12 CALA9900931 1 19990801 A 5753 PANEL DOUG DC9 DC982 3022082 WP LT TE FLAP CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LEFT WING FLAP FLEX JOINT ACCESS PANEL NR 1540 LOWER SURFACE CHAFED. A REPAIR WAS INSTALLED IAW SRM 51 -10-4 AND 51-30-1. 2 L 7 2 4F A6WE 1999081200288 19990812 00288 WP 1999 8 12 CALA9900932 1 19990801 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND SUBFLOOR WEB CORRODED AT STA 200, RBL 10-50. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2 AN D 51-30-2. 2 L 7 2 4F A6WE 1999081200289 19990812 00289 WP 1999 8 12 CALA9900933 1 19990801 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND COCKPIT FLOOR PANEL LOCATED AT PILOT'S SEAT POSITION STA 150, LBL 40 CORRODED. A NEW FLOOR PANEL WAS I NSTALLED IAW SRM 51-10-04 AND 51-10-03. 2 L 7 2 4F A6WE 1999081200290 19990812 00290 NM 1999 8 12 CALA9900934 1 19990802 A 5330 SKIN BOEING 757 757224 1384958 NM BS 610 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 610, STRINGER 16-17L. THE SKIN WAS REPAIRED IAW ECRA 5331-01060. 2 L 7 2 4F RT A2NM 1999081200291 19990812 00291 NM 1999 8 12 CALA9900935 1 19990802 A 5330 SKIN BOEING 757 757224 1384958 NM BS 1617 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND LEFT LOWER FUSELAGE SKIN DENTED AT STA 1617, STRINGER 25-26L. REPAIRED IAW ECRA 5331-1061. 2 L 7 2 4F RT A2NM 1999081200292 19990812 00292 NM 1999 8 12 CALA9900936 1 19990802 A 5754 ANGLE BOEING 727 727224 1384076 NM RT NR 7 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A .25 INCH CRACK IN RT WING NR 7 SLAT LOWER CHORD. THE LOWER CHORD ANGLE WAS REMOVED AND A NEW CHORD W AS INSTALLED IAW SRM 51-40-4, 51-30-2, 51-10-2. 2 L 7 3 4F A3WE 1999081200293 19990812 00293 WP 1999 8 12 CALA9900937 1 19990802 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP WS 486 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 2 CRACK IN RT WING TRAILING EDGE ANGLE AT XORS 486. THE ANGLE WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999081200294 19990812 00294 WP 1999 8 12 CALA9900938 1 19990802 A 5753 SKIN DOUG DC9 DC982 3022082 WP RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND THE RT I/B FLAP T/E SECTION NR 1 LOWER SURFACE SKIN CORRODED. THE SKIN WAS REMOVED IAW SRM 51-30-2 AND NEW SKIN WAS INSTALLED IAW SRM 57-50-14, 51-10-04, AND 51-30-2. 2 L 7 2 4F A6WE 1999081200295 19990812 00295 WP 1999 8 12 CALA9900939 1 19990802 A 5330 SKIN DOUG DC9 DC982 3022082 WP RT MLG DOORWAY GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND THE RT MLG DOOR CUTOUT GOUGED AT PREVIOUS DOUBLER. THE DOUBLER WAS REMOVED IAW SRM 51-30-2 AND A NEW D OUBLER WAS INSTALLED IAW SRM 51-10-4, 51-30-5, AND 53-01-02. 2 L 7 2 4F A6WE 1999081200296 19990812 00296 SO 1999 8 12 COMA9910124 1 19990802 A 7110 COWL PANEL EMB 120 EMB120RT SO LT ENGINE LOOSE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 189CA 120189 LEFT COWL ACCESS PANEL LOOSE. SECURED LOOSE ACCESS PANEL. 2 L 7 2 4T RT A31SO 1999081200297 19990812 00297 SO 1999 8 12 COMA9910125 1 19990802 A 2150 CLAMP EMB 120 EMB120RT SO RT ACM LOOSE A COMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 268CA 120262 RIGHT BLEED AIR DUCT LEAK WARNING. SECURED LOOSE HOSE CLAMP ON RIGHT ACM. 2 L 7 2 4T RT A31SO 1999081200298 19990812 00298 EA 1999 8 12 COMA9960412 1 19990802 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 729CA 5255 1600 7265 FLAPS FAILED DURING TAXI OUT. REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 1999081200299 19990812 00299 NM 1999 8 12 UPS99230256 1 19990802 A 2612 65249203 RELAY BOEING 727 72725C 138400H NM LT MLG WW INOP A IPXA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 946UP 19721 IN DESCENT, WHEEL WELL FIRE WARNING ILLUMINATED. ACCOMPLISHED CHECKLIST ITEMS LIGHT EXTINGUISHED. INSPECTED W/W'S FOR EVIDENCE OF FIRE OVERHEAT AND PNEUMATIC LEAKS NO DEFECTS NOTED. INSPECTED FIRE LOOPS. NO EVIDENCE OF DAMAGE. REMOVED FIRE AND OVERHEAT ACCESSORY UNIT ASSY. FOUND ONE RELAY WITH BLACK PINS. REPLACED ACCESSORY UNIT W/W, FIRE TEST GOOD IA W MM 26-12-21. PART ON/OFF 65-24920-3 S/N ON 670604 S/N OFF 66807. SYSTEM CHECKS GOOD IAW. 2 L 7 3 4F A3WE 1999081200300 19990812 00300 WP 1999 8 12 UPS99830254 1 19990731 A 5280 SEAL DOUG DC8 DC871F 302199D WP NLG DOOR LOOSE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 750UP 45950 ON DEPART, (C/O) NOTICED AFTER GEAR RETRACT, THE GEAR NOT LATCH LIGHT FLICKERED. DID UPLATCH CK AND LIGHT EVENTUALLY CA ME ON STEADY. WENT TO GEAR NOT LATCH LIGHT ILLUMINATED. CKLIST AND C/W, THIS INCLUDED CYCLING GEAR AND LOOKING THROUGH PEEPHOLE TO CHECK IF N/G WAS DOWN AND LOCKED, IT WASN'T. ALSO, HEARD A BANGING TYPE NOISE. REMOVED AND REPLACED NOSE GEAR DOOR SEAL PER MM 32-30-00 PG 104 SECT D. LUBED UPLATCH MECHANISM PER MM 12-81-01. JACKED AIRCRAFT, CYCLED GEAR 5 TIMES, NO FAULTS NOTED AND INDICATOR LIGHTS OP'D NORMALLY. 2 L 7 4 4F RT 4A25 1999081200301 19990812 00301 NM 1999 8 12 UPS99230253 1 19990730 A 5752 TAB BOEING 727 72727C 138400J NM LT AILERON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 LEFT OUTBOARD AILERON IE WEDGE OUTBOARD OF TAB HAS CORNER MISSING. REPAIRED PER SRM 57-50-01. 2 L 7 3 4F A3WE 1999081200302 19990812 00302 NM 1999 8 12 UPS99230258 1 19990722 A 5720 65216583132 ANGLE BOEING 727 72722C 138400F NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, RT WING TE PANEL OUTBOARD OF NR 7 FLAP TRACK, ATTACH ANGLE CRACKED. ANGLES REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999081200303 19990812 00303 NM 1999 8 12 UPS99230259 1 19990722 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, CRACKED FRAME ANGLE AT FWD SIDE OF LATCH SUPPORT FITTING AT BS500 FWD CARGO BAY. FRAME ANGLE REPAIRE D IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1999081200304 19990812 00304 NM 1999 8 12 UPS99230260 1 19990725 A 5753 69333281 BRACKET BOEING 727 72722C 138400F NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, NR 1 FLAP TRACK MID FAIRING AFT SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 AND DRAWI NG 65-21796. 2 L 7 3 4F A3WE 1999081200305 19990812 00305 NM 1999 8 12 UPS99230261 1 19990725 A 5753 65291566 FAIRING BOEING 727 72722C 138400F NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, NR 7 FLAP TRACK MID FAIRING OUTBOARD TRACK CRACKED. TRACK REPLACED IAW DRAWING 65-21796. 2 L 7 3 4F A3WE 1999081200306 19990812 00306 NM 1999 8 12 UPS99230262 1 19990725 A 5753 69333281 BRACKET BOEING 727 72722C 138400F NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, NR 7 FLAP TRACK MID FAIRING AFT SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW DRAWING 65-21796. 2 L 7 3 4F A3WE 1999081200307 19990812 00307 NM 1999 8 12 UPS99230263 1 19990725 A 5753 65291565 FAIRING BOEING 727 72722C 138400F NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, NR 8 FLAP TRACK MID FAIRING INBOARD TRACK CRACKED. TRACK REPLACED IAW DRAWING 65-21796. 2 L 7 3 4F A3WE 1999081200308 19990812 00308 NM 1999 8 12 UPS99230264 1 19990723 A 7830 06453010059 BRACKET BOEING 727 72722C 138400F NM NR 3 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:C, NR 3 ENGINE THRUST REVERSER FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-30-02 A ND MM 78-30-00. 2 L 7 3 4F A3WE 1999081200309 19990812 00309 1999 8 12 UPS99430152 2 19990723 A 7200 ENGINE BOEING 747 747SR46 NM NR 4 FAILED A IPXA E ENGINE SHUTDOWN M OVER TEMP DE DESCENT 1 SO 01 680UP 20923 NR 4 ENGINE SHUTDOWN IN FLIGHT ON FINAL APPROACH HAD A COMPRESSOR STALL WITH DESCENT POWER ON WITH A IMMEDIATE RAPID RIS E IN EGT. SHUTDOWN EGT SHOWS MAX 914. FELT COMPRESSOR STALL AND HEARD LOW RUMBLE AFTER THRUST LEVER RETARDED TO FLIGHT IDLE. REMOVED AND REPLACED NR 4 ENGINE PER B747 TC 50 00. 2 L 7 4 4F A20WE 1999081200310 19990812 00310 NM 1999 8 12 UPS99430243 1 19990729 A 2160 HEAT SYSTEM BOEING 747 747123F NM CARGO COMMPT INOP A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 674UP 20100 COMPUTER SHOWS FIRE WARNING, AFT CARGO HEAT SYSTEM WILL NOT TEST DI M1 76126. AFT CARGO HEAT SYSTEM WILL NOT TEST. CHE CKED WIRING TO VALVES AND CHECK EXTENSION OVRD VALVES ACTUATOR AND OPS CHECKED GOOD MM 21-44-00. 2 L 7 4 4F A20WE 1999081200311 19990812 00311 WP 1999 8 12 UPS99830257 1 19990801 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:W/,E EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. EMERGENCY LTS GROUN D OPERATIONAL TEST NORMAL PER MM 33-50-01. 2 L 7 4 4F RT 4A25 1999081200312 19990812 00312 WP 1999 8 12 99FDEA00304 1 19990310 A 5320 3D0031730 BOLT DOUG DC10 DC1010 3022110 WP BS 275 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 N2764, DURING A/C P-F CONV AT AERONAVALI, A SUSPECTED BOLT FAILURE WAS FOUND AT STA Y=275 FOR ATTACH P/N ABA7003-2, ABA7 023-1, NBA6044-15 AND ABA7171. REPAIR WAS ACCOMPLISHED IAW EA NR 8-5311-44057 AND IT WAS APPROVED PER FEDEX 8110-3 DATE D 29 APR 99. THE APPROVAL IS FOR 18 FLTS OR UPON REACHING LONG BEACH WHICHEVER COMES FIRST. 2 L 7 3 4F A22WE 1999081200316 19990812 00316 NM 1999 8 12 99FDEA00308 1 19990803 A 7930 BY PASS SWITCH BOEING 727 72725C 138400H NM NR 3 ENGINE INOP A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 120FE 19356 99-188 - AFT T/O ENG NR 3 LOW OIL PRESSURE OR FILTER BYPASS LIGHT ILLUM AT 500 FT ABOVE GROUND LEVEL. OIL PRESS AND TEM P WERE NORM. SHUTDOWN ENG PER RED TAB. OIL QUANTITY NORM. REMOVED AND REPLACED OIL FILTER BYPASS SW MM 79-33-002, INS P MAIL OIL STRAINER MM 79-00, SOCKET ASSY IAW MM 31-00-021-4, ENG'S OIL PRESS IND SYS OPS CK GOOD IAW JRH. OK FOR SVC. 2 L 7 3 4F A3WE 1999081200326 19990812 00326 EU 1999 8 12 CA990219024 1 19990127 A 3230 SENSOR AIRBUS 320 A320211 3930320 EU LT MLG DOOR FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) LEFT MLG DOOR PROXIMITY SWITCH NR 39GA FAILED. 2 L 7 2 4F RT A28NM 1999081200332 19990812 00332 NM 1999 8 12 CA990223014 1 19990109 A 2530 3510001601 COFFEE MAKER BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE GALLEY BURNT W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 0476 30743 (CAN) CREW REPORTED SMOKE IN GALLEY. FOUND BURNED WIRING ON OUTBOARD COFFEEMAKER, REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200334 19990812 00334 CE 1999 8 12 CA990223021 1 19990208 A 3610 1183800031 CHECK VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BLEED AIR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 3700 PCEPS0103 (CAN) BLEED AIR LINE REMOVED TO ALLOW REPLACEMENT OF AIR FILTER. IT WAS THEN NOTED THAT THE CHECK VALVE WAS NOT INTACT. THE EXHAUST COOLING DUCT WAS REMOVED TO FIND THE REMAINING PARTS OF VALVE. 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200335 19990812 00335 EA 1999 8 12 CA990223022 1 19990211 A 2822 2650157 CHECK VALVE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA BOOST PUMP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) VALVE PURCHASED NEW. INSIDE VALVE THERE IS A FLAPPER DOOR WITH A RUBBER SEAL. FLAPPER DOOR SEAL HAD SWOLLEN KEEP ING THE DOOR OPEN; THUS, DEFEATING THE PURPOSE OF THE CHECK VALVE IN THE BOOSTER PUMP SYSTEM. 1 H 7 2 3T 4 T RT A9EA E4EA 1999081200338 19990812 00338 NM 1999 8 12 CA990224003 1 19990215 A 2820 200072002 TUBE 200073 PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA FUEL TRANSFER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 3471 L1834048A (CAN) FUEL TRANSFER TUBE IN RIGHT HAND WING WHERE FUEL STRAINER ATTACHES FOUND TO HAVE DEEP CORROSION PITTING INSIDE TUB E. OPERATOR WILL DO FLEET CAMPAIGN. 1 M 7 2 3O 3 O RT A17WE 1E4 1999081200349 19990812 00349 NE 1999 8 12 CA990226002 1 19990116 A 7714 9580115900 SENSOR SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE OVERSPEED INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 1238 3920 15538TEC (CAN) THE OVERSPEED SENSOR WAS INOPERATIVE CAUSING THE OVERSPEED CAUTION LIGHT TO ILLUMINATE. 1 G 7 2 3U 3 U H1NE E19EU 1999081200350 19990812 00350 NE 1999 8 12 CA990226003 1 19990124 A 2435 23081043 BRUSHES SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE START/GENERATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 2723 268 15536TEC (CAN) ON INSPECTION, THE STARTER/GENERATOR WAS FOUND TO HAVE EXCESSIVE WEAR ON THE BRUSHES. 1 G 7 2 3U 3 U H1NE E19EU 1999081200351 19990812 00351 NE 1999 8 12 CA990226004 2 19990124 A 7322 0164348730 FCU SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S1 60030 NE ENGINE FAULTY W D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 CA 1247 15536TEC (CAN) FAULTY FUEL CONTROL CAUSED TORQUE FLUCTUATIONS. 1 G 7 2 3U 3 U H1NE E19EU 1999081200360 19990812 00360 SW 1999 8 12 CA990301004 1 19990215 A 6220 206011100025 BUSHING 206011100025 BELL 206 206BELL 1181502 SW MAIN ROTOR MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) PRIOR TO INSTALLATION, BUSHING P/N 206-011-128-101 WAS FOUND TO BE THE WRONG DIMENSIONS. 1 G 7 1 3U H2SW 1999081200361 19990812 00361 1999 8 12 CA990301006 4 19990217 A 2397 RG58RG6 WIRE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA NR 2 COMM SYSTEM SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA PCE50047 (CAN) THE 90 DEGREE HEAT DUCT ON THE RIGHT HAND OF THE COPILOT'S RUDDER PEDALS DIRECTS HOT AIR ONTO THE NR 2 COMM, AND D ME COAXIAL WIRE BUNDLES. OVER TIME , THIS CAUSED CABLE DAMAGE MELTING THE WIRE AND ALLOWING THE CENTER CONDUCTOR TO SHO RT TO THE SHIELD. DAMAGE LIMITED TO A SIX INCH AREA. FLEET CAMPAIGN TO BE CARRIED OUT. 1 L 7 2 3T 4 T A14CE E4EA 1999081200364 19990812 00364 NM 1999 8 12 CA990301010 1 19990203 A 3244 0262020 TIRE MICHELIN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 643 8255P00963 PCE120248 (CAN) MAIN GEAR TIRE LEAKING THROUGH SIDEWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200365 19990812 00365 EU 1999 8 12 CA990301011 1 19990204 A 3246 AHA1489 WHEEL DUNLOP BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13368 MJ157 LF05777A (CAN) DURING MAIN WHEEL CHECK FOR LEAKING AIR, A CRACK AND CORROSION WERE FOUND IN THE INBOARD WHEEL HALF, AT END OF BRA KE DRIVE BLOCK ABUTMENT. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200375 19990812 00375 CE 1999 8 12 CA990303010 1 19990228 A 3010 38E855C GASKET LUCAS 99120432 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE DEICE BOOTS BLOWN W O OTHER K FLUID LOSS CR CRUISE 1 CA 3307 RF1878 71711 (CAN) IN CRUISE , PILOTS TESTED THE DEICE SYSTEM AND WING DEICE BOOTS DID NOT SEEM TO INFLATE. INVESTIGATION FOUND THE LOWER GASKET BLOWN OUT OF THE PRESSURE REGULATING VALVE. IT APPEARS THAT CESSNA MAY HAVE FIXED PROBLEM AS THE NEW VALVE S COME WITH DIFFERENT AND NEW GASKETS. 1 L 7 2 4F 4 F A22CE E1NE 1999081200379 19990812 00379 CE 1999 8 12 CA990303015 1 19990303 A 7600 99524119 CATCH 1005241771 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CONDITION LEVER WORN W K NONE O OTHER IN INSP/MAINT 1 CA 4977 GGM114476 (CAN) FOLLOWING AN ENGINE FAILURE WHEN CONDITION LEVERS WERE MOVED FROM HIGH TO LOW IDLE, CAUSED BY WORN CONDITION LEVER S WHICH DID NOT PREVENT A MOVE TO SHUT OFF POSITION, THE COMPANY DID A FLEET INSPECTION AND FOUND 3 OTHER AIRCRAFT WITH THE SAME WORN CONDITION CATCH GATES. 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200380 19990812 00380 CE 1999 8 12 CA990303016 1 19990303 A 7600 99524119 CATCH 1005241771 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CONDITION LEVER WORN W K NONE O OTHER IN INSP/MAINT 1 CA 4699 GGMPS0025 (CAN) AS A RESULT OF AN ENGINE SHUT DOWN DUE TO A WORN CONDITION LEVER CATCH ,THE FLEET WAS CHECKED AND THIS AIRCRAFT FO UND WITH SIMILAR PROBLEM. 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200381 19990812 00381 CE 1999 8 12 CA990303017 1 19990303 A 7600 99524119 CATCH 1005241771 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CONDITION LEVER WORN W K NONE O OTHER IN INSP/MAINT 1 CA 4509 GGMPS0054 (CAN) AS A RESULT OF ENGINE SHUTDOWN, BECAUSE OF A WORN CONDITION LEVER CATCH, THE FLEET WAS CHECKED. THIS AIRCRAFT LEV ER ALSO FOUND WORN. 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200382 19990812 00382 CE 1999 8 12 CA990303018 1 19990218 A 2752 1003840403 MOTOR ELECTROMECH 1005240731 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TE FLAP SEIZED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 539 1941 PCEPS0103 (CAN) ON FINAL, FLAPS 17 DEGREES SELECTED, THEY TRAVELLED TO 17 DEGREES. ON SELECTION TO FULL, THEY DID NOT MOVE. ON G ROUND,THEY STILL DID NOT MOVE. FLAP MOTOR REPLACED. THIS IS FOURTH MOTOR REPLACEMENT. SUBMITTER SUGGESTS THAT THIS IS AN UNACCEPTABLE FAILURE RATE. 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200385 19990812 00385 1999 8 12 CA990308003 4 19990301 A 2215 6185973002 GUARD 6222733002 BEECH 90 C90 1152913 CE PWA PT6 PT6A21 52043 EA AUTOPILOT SERVO CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 891 729 PCE10416 (CAN) RUDDER AUTOPILOT SERVO CAPSTAN CABLE GUARD ASSEMBLIES FOUND DAMAGED. ONE CABLE GUARD CUT IN HALF AND THE OTHER CU T THROUGH MORE THAN 50 PERCENT BY THE RUDDER TRIM AUTOPILOT SERVO CABLE. INVESTIGATION REVEALED THAT THE INCORRECT CAPS TAN ASSEMBLY HAD BEEN MATED TO THE RUDDER A/P SERVO AT OVERHAUL. THE CAPSTAN CABLE GUARDS ARE REMOVABLE AND POSITIONABLE ON THE -002 CAPSTAN WHILE ON THE CORRECT CAPSTAN, THE -003 THE GUARDS ARE FIXED IN PLACE. 1 L 7 2 3T 4 T 3A20 E4EA 1999081200395 19990812 00395 CE 1999 8 12 CA990308015 1 19990301 A 2897 WIRE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE FUEL INDICATOR CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 71711 (CAN) THE THREADS OF THE UPPER HORIZONTAL PANEL SUPPORT ATTACHMENT SCREW CHAFING ON AN UNPROTECTED WIRE BUNDLE CAUSING T WO WIRES TO ARC BETWEEN EACH OTHER AND MELTING THE INSULATION. SMOKE NOT REPORTED BY PILOT, BUT WAS NOTED DURING TROUBL ESHOOTING. WIRING REPAIRED AND WIRE BUNDLE SPIRAL WRAPPED. SHORTER SCREWS USED TO SECURE PANELING. TWO OTHER AIRCRAFT FOUND WITH SAME PROBLEM. 1 L 7 2 4F 4 F A22CE E1NE 1999081200397 19990812 00397 NM 1999 8 12 CA990308019 1 19990301 A 3260 257T110315 SWITCH BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE MLG FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA 30690 (CAN) ON APPROACH AT 1,500 FEET, WARNING TOO LOW GEAR GO-AROUND INITIATED, GEAR RECYCLED AND GEAR SAFE INDICATIONS BACK TO NORMAL. MICROSWITCH ON LANDING GEAR LEVER MODULE GEAR DOWN NOT MAKING CONTACT. REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200398 19990812 00398 CE 1999 8 12 CA990308020 1 19990301 A 3231 NAS464P4A10 BOLT CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE NLG WW SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 3273 71747 (CAN) NAS BOLT SHEARED IN HALF BETWEEN THE NOSE GEAR KEEP SUPPORT STRUCTURE AND THE TORQUE TUBE ASSY, CAUSING THE NOSE G EAR DOORS NOT TO EXTEND OR RETRACT. 1 L 7 2 4F 4 F A22CE E1NE 1999081200401 19990812 00401 EA 1999 8 12 CA990308025 1 19990221 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 9799 807157 (CAN) ON APPROACH ,THE LANDING GEAR DISAGREE MESSAGE ON. AFTER THREE ATTEMPTS TO LOWER GEAR WITHOUT SUCCESS, AN ALTERN ATE GEAR SELECTION WAS SUCCESSFULLY CARRIED OUT. AIRCRAFT LANDED OK. SELECTOR VALVE REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200402 19990812 00402 EA 1999 8 12 CA990308027 1 19990220 A 3260 PS4GA SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG OUT OF ADJUST W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA 9116 807213 (CAN) SHORTLY AFTER TAKEOFF, STEERING INOP AND LANDING GEAR DISAGREE MESSAGES ON WITH NOSE LANDING GEAR STILL DOWN. NOS E LANDING GEAR PROXIMITY SENSORS ADJUSTED. ALSO SENSOR P/N PS13GA. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200403 19990812 00403 EA 1999 8 12 CA990308029 1 19990217 A 5551 600211341 VISOR PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT STABILIZER MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 7046 807343 (CAN) ON TRIP CHECK FOUND THE RIGHT HAND VISOR PANEL ON THE STABILIZER MISSING. THIS IS A 2 INCH BY 4 INCH FAIRING. IT IS THE LOWER LEFT ONE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200404 19990812 00404 WP 1999 8 12 CA990308030 1 19990215 A 7711 TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE NR 1 ENGINE FAULTY W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA P657506D (CAN) DURING TAKEOFF ROLL,THE NR 1 ENGINE EPR GAUGE JUMPED FROM TAKEOFF SETTING OF 2.07 TO 2.15, FUEL FLOW JUMPED FROM 6 ,000 POUNDS PER HOUR TO 8,500 POUNDS PER HOUR AND BACK AGAIN. TAKEOFF WAS REJECTED. THE ENGINE PRESSURE RATIO TRANSMITTE R WAS REPLACED. THE PS3 FILTER AND THE FUEL CONTROL UNIT WATER TRAP WERE CLEANED AND THE PT2 LINE WAS TIGHTENED. THE ENG INE WAS GROUND RUN SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1999081200405 19990812 00405 EA 1999 8 12 CA990308031 1 19990213 A 5210 LATCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR OUT OF ADJUST W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 6295 807389 (CAN) AFTER TAKEOFF THROUGH 4,000 FEET, PASSENGER DOOR LATCH CAUTION MESSAGE, FOLLOWED BY PASSENGER DOOR WARNING MESSAGE . CABIN PRESSURE AT 2.3. AIRCRAFT RETURNED. DOOR LATCH CAM SPIGOTS ADJUSTED TO LOWER LIMIT, INNER HANDLE FRICTION TENS ION ADJUSTED, AND PULL CHECK CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200406 19990812 00406 EU 1999 8 12 CA990308035 1 19990111 A 5240 DOOR AIRBUS A340 A340313 EU FUEL PANEL NOT SECURED W C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 CA (CAN) FUEL PANEL DOOR OPEN LIGHT ON TAKEOFF ABORTED, NR 4 AND NR 8 BRAKES OVERHEATED. LATCHES ON FUEL PANEL DOOR ADJUST ED. 2 L 7 4 4F RT A197 1999081200407 19990812 00407 EA 1999 8 12 CA990308036 1 19990208 A 5210 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR FAILED W I CABIN DEPRESSURIZATION N FALSE WARNING CL CLIMB 1 CA 6278 807389 (CAN) PASSENGER DOOR LIGHT AND CAUTION MESSAGE IN FLIGHT THROUGH 10,500 FEET FLOWED 5 SECONDS LATER BY PASSENGER DOOR WARNING MESSAGE. AIRCRAFT DEPRESSURIZED AND LANDED OK. PROXIMITY SWITCH ELECTRONIC UNIT INTERROGATED SHOWING SENSORS O UT OF RIG. SENSOR HARNESS REPOSITIONED, DOOR ADJUSTMENT AND RIGGING CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200408 19990812 00408 EA 1999 8 12 CA990308037 1 19990208 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 7286 807337 (CAN) FLAPS FAIL MESSAGE ON APPROACH, AS FLAPS TRAVELLING FROM 8 DEGREES TO 20 DEGREES, STUCK AT 15 DEGREES. LANDING OK . RIGHT HAND OUTBOARD FLAP, INBOARD ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200409 19990812 00409 1999 8 12 CA990308038 4 19990204 A 3460 FMCS BOEING 767 767333 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA P724734 (CAN) SEVERAL TIMES DURING FLIGHT, AUTOTHROTTLE WOULD DISCONNECT, ENGINE INDICATION AND CREW ALERT SYSTEM WOULD ANNUNCIA TE AUTOPILOT DISCONNECT, HOWEVER, AUTOPILOT REMAINED ON, AUTOPILOT DISCONNECT ANNUNCIATION WOULD GO OUT AFTER 5 SECONDS, SNAG OCCURRED DURING COMMAND C OR L. 2 L 7 2 4F 4 F RT A1NM E24NE 1999081200410 19990812 00410 SW 1999 8 12 CA990308039 1 19990130 A 6520 206040402003 DRIVESHAFT 206033004003 BELL 206 206L 1181522 SW T/R GEARBOX MISALIGNED W K NONE O OTHER IN INSP/MAINT 1 CA 10735 3829 (CAN) MISALIGNMENT OF DRIVESHAFT AND TAIL ROTOR GEARBOX CAUSING INPUT GEAR PREMATURE WEAR. 1 G 7 1 3U H2SW 1999081200414 19990812 00414 EU 1999 8 12 CA990310004 1 19990116 A 3241 HC324B0017000 VALVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ANTI SKID SYSTEM LEAKING W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 26089 LF05683A (CAN) ANTI-SKID HYDRAULIC LINE LEAKING. FUMES IN CABIN AFTER LANDING. B-NUT TIGHTENED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200415 19990812 00415 NE 1999 8 12 CA990310005 2 19990119 A 7210 GEARBOX DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 15077 415 123126 (CAN) LEVEL NR 3 METAL CONTAMINATION FOUND IN THE REDUCTION GEARBOX (RGB). THE ENGINE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200417 19990812 00417 NM 1999 8 12 CA990310007 1 19990126 A 5610 NP15790110 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 15837 91302H1208 120083 (CAN) DURING CLIMB THROUGH 13,000 FEET AT 2,000 FPM, COPILOT'S OUTER WINDSHIELD SHATTERED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200418 19990812 00418 NM 1999 8 12 CA990310008 1 19990116 A 3060 KCD4N RELAY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PROP DEICE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA PCE120658 (CAN) RIGHT PROPELLER DE-ICE PHASE A SHOWS LOAD WITH DE-ICE SELECTED OFF. RELAY FAILED IN ON POSITION. RELAY REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200419 19990812 00419 EA 1999 8 12 CA990310010 1 19990110 A 2421 31708001A GENERATOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE AC SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 7214 905 1251 123132 (CAN) NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED, RESET UNSUCCESSFUL. AIRCRAFT RETURNED FOR NORMAL LANDING. AC GENERA TOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200420 19990812 00420 EA 1999 8 12 CA990310011 1 19990124 A 2720 XD4N RELAY DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RUDDER FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 17533 123132 (CAN) ACCELERATING THROUGH 140 KNOTS, RUDDER PRESSURE, RUDDER FULL PRESSURE CAUTION LIGHTS ILLUMINATED. RELAY 27-21 K1 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200423 19990812 00423 NM 1999 8 12 CA990310014 1 19990105 A 5347 85320490125 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CABIN CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 39670 120648 (CAN) SEAT RAIL FOUND CORRODED UNDER LAV/GALLEY AREA. PART REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200424 19990812 00424 NM 1999 8 12 CA990310015 1 19990113 A 2910 AEB2151011 MANIFOLD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYD PRESSURE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 2426 2198 0136A 120648 (CAN) AFTER TAKEOFF, NR 2 STANDBY HYDRAULIC PUMP SEL. OFF, NR 2 ENGINE PUMP, RUDDER PRESS, RUDDER FULL PRESS, NR 2 RUDDE R HYD, ROLL SPOILER CAUTION LIGHTS ON. TURNING NR 2 STANDBY PUMP ON, NORMAL OPERATION. PRESSURE MANIFOLD REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200425 19990812 00425 NM 1999 8 12 CA990310016 1 19990205 A 2913 570347 PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CA 18884 504 MX485707C 120648 (CAN) ON GEAR DOWN EXTENSION, GEAR DOORS OPENED BUT GEAR DID NOT EXTEND, NR 2 HYDRAULIC CAUTION LIGHTS ILLUMINATED. ALT ERNATE GEAR EXTENSION CARRIED OUT, AIRCRAFT LANDED......NR 2 EDP REPLACED, SUSPECT AIR IN SYSTEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200426 19990812 00426 NM 1999 8 12 CA990310017 1 19990205 A 2450 M817142 TERMINAL BLOCK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AC SYSTEM BURNT W O OTHER O OTHER CR CRUISE 1 CA 26014 121165 (CAN) NR 1 AC AUXILIARY FUEL PUMP NOT WORKING, CIRCUIT BREAKER TRIPPED. TERMINAL BLOCK 2821 TBL FOUND BURNT THROUGH. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200428 19990812 00428 NM 1999 8 12 CA990310019 1 19990201 A 2530 180140 CONNECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GALLEY LOOSE W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 72559 120229 (CAN) ELECTRICAL BURNING SMELL NOTED AFTER TAKEOFF. HOT POT CONNECTOR IN GALLEY FOUND LOOSE. CONNECTORS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200429 19990812 00429 NM 1999 8 12 CA990310020 1 19990204 A 2460 85321976101 RETAINER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BS 234 WORN W K NONE O OTHER IN INSP/MAINT 1 CA 15785 120229 (CAN) DURING INSPECTION, CHAFING WAS FOUND BETWEEN OVERHEAD WIRING HARNESS AND SHARP EDGES OF TROUGH RETAINER AT STA X23 4.50, ABOVE FORWARD EMERGENCY EXIT. INSULATION WAS WORN BUT NOT THROUGH TO BARE WIRE. ALL SUPPORT FOR BUNDLE APPEARED TO BE IN PLACE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200430 19990812 00430 NM 1999 8 12 CA990310021 1 19990203 A 3320 1009463 LIGHT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GALLEY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 15785 120229 (CAN) ELECTRICAL SMELL REPORTED IN GALLEY. NO FAULT FOUND, SLIGHT ODOR NOTED AT LAMP ASSY, LAMP ASSY REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200431 19990812 00431 NM 1999 8 12 CA990310022 1 19990205 A 3320 1009463 LIGHT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GALLEY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 120229 (CAN) F/A REPORTED ELECTRICAL SMELL IN FORWARD GALLEY. AIR SUPPLY TUBE FOR GASPER FOUND RESTING ON TOP OF LAMP ASSY. T UBE RE-ROUTED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200435 19990812 00435 EU 1999 8 12 CA990310026 1 19990209 A 2752 676001001 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE TE FLAP CONTAMINATED W A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 CA LF05465A (CAN) FLAP FAULT ON APPROACH, FLAPS STUCK 0-18 DEGREES. INVESTIGATION REVEALED WATER IN BALLNUTS OF ACTUATORS. ACTUA TORS LUBRICATED, A/C RETURNED TO SERVICE. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200436 19990812 00436 EU 1999 8 12 CA990310028 1 19990121 A 5240 NAS62039 BOLT AC67912 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE SERVICE DOOR SNAPPED W K NONE O OTHER IN INSP/MAINT 1 CA 26175 LF05629A (CAN) FORWARD SERVICE DOOR GUST DAMP MOUNTING PLATE BOLTS FAILED. BOLTS REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200437 19990812 00437 EU 1999 8 12 CA990310029 1 19990203 A 5270 MS3470L106SN WIRE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE SERVICE DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 26281 LF05629A (CAN) FORWARD SERVICE DOOR UNLOCKED WARN LIGHT EXTINQUISHED WITH DOOR OPEN. BROKEN WIRE REPLACED AT DOOR CANNON PLUG. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200438 19990812 00438 EU 1999 8 12 CA990310030 1 19990209 A 2160 4372C000 SENSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 PACK FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA LF05629A (CAN) NR 2 PACK GOING FULL HOT IN AUTO MODE. DUCT TEMP SENSOR REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200439 19990812 00439 NM 1999 8 12 CA990310031 1 19990215 A 6120 V319 SWITCH JV5 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CONDITION LEVER CONTAMINATED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 120854 890709 (CAN) TAKEOFF WARNING DUE TO NR 2 CONDITION LEVER SWITCH 3151-S4. CLEANED AND ADJUSTED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999081200453 19990812 00453 NM 1999 8 12 CA990310046 1 19990104 A 7711 JG298A5 INDICATOR HONEYWELL BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAULTY W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 34041 28916 B574 674444 (CAN) AIRCRAFT ABORTED TAKEOFF DUE TO NR 1 ENGINE EPR INDICATOR STUCK AT 1.6. THE EPR INDICATOR WAS REPLACED AND THE AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1999081200454 19990812 00454 NM 1999 8 12 CA990310047 1 19990105 A 2917 72909 REGULATOR ADEL 72909 BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE HYDRAULIC SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 33560 2515 H2924 702661 (CAN) AIR TURN BACK DUE TO LOSS OF A-SYSTEM HYDRAULIC PRESSURE. REPLACED AIR PRESSURE REGULATING VALVE ON HYRAULIC RESE RVOIR. 2 L 7 2 4F 4 F A16WE E2EA 1999081200455 19990812 00455 NM 1999 8 12 CA990310048 1 19990105 A 3220 50A3230884 SEAL 654620048 BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE NLG WORN W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 43192 11444 R7638P635 709378 (CAN) AIR TURNBACK, NLG RED UNSAFE LIGHT ON WHEN GEAR SELECTED UP. SEALS AND BEARING REPLACED. NOSE GEAR WOULD NOT RETR ACT AFTER TAKEOFF, NLG OVERSERVICED ON SEAL CHANGE, NLG SERVICED AND RETRACTION TEST CARRIED OUT. 2 L 7 2 4F 4 F A16WE E2EA 1999081200456 19990812 00456 NM 1999 8 12 CA990310049 1 19990111 A 5610 5893543110 WINDSHIELD 5892543110 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 18082 92112H9341 708805 (CAN) FIRST OFFICER'S WINDSHIELD CRACKED, REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200457 19990812 00457 NM 1999 8 12 CA990310050 1 19990114 A 2120 10613266 ACTUATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE AIR DISTRIBUTION FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 30871 28005 840901 702655 (CAN) ON INSTALLATION, FOUND ACTUATOR RAN IN OPPOSITE DIRECTION AS REQUESTED. REPLACED AND VENDOR ADVISED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200458 19990812 00458 NM 1999 8 12 CA990310051 1 19990116 A 7312 320115 VALVE WHITTAKER BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE FUEL HEATER FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA 5669 46033 19779 687898 (CAN) AIRCRAFT DIVERTED DUE TO NR 2 ENGINE OIL TEMPERATURE BEING BEYOND LIMITS. THE OVERTEMP WAS CAUSED BY A FAILED FUE L HEAT CONTROL VALVE. THE VALVE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1999081200459 19990812 00459 EU 1999 8 12 CA990310052 1 19990117 A 2120 748A000005 VALVE AIRBUS 320 A320211 3930320 EU NR 2 PACK FAILED W H O DEACTIVATE SYST/CIRCUITS OTHER B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION TX TAXI/GRND HDL 1 CA 18811 1004 (CAN) AIRCRAFT DECLARED AN EMERGENCY ON TAXI, DUE TO VAPOR IN THE CABIN. ENGINE RUN AT GATE DUPLICATED THE PROBLEM. FO UND WATER VAPOR COMING FROM NR 2 SYSTEM. THE NR 2 PACK ANTI-ICE VALVE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A28NM 1999081200460 19990812 00460 NE 1999 8 12 CA990310053 2 19990105 A 7250 TURBINE WHEEL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE CRACKED W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CA 63562 455340 (CAN) DURING LANDING ROLL, AFTER THRUST REVERSER CANCELLED, SPARKS WERE SEEN FROM REAR OF NR 1 ENGINE. INSPECTION REVEA LED METAL IN THE EXHAUST. DISASSEMBLY FOUND LP TURBINE ASSEMBLY DAMAGED. DISCOURAGER LEG OF NR 1 AIR SEAL HAD PIECES M ISSING WITH CRACKING AND EROSION, WITH EVIDENCE OF OXIDIZATION AT CRACK LOCATIONS IN TWO PLACES OF THE FILLET WELD AREAS . 2 L 7 3 4F 4 F A22WE E23EA 1999081200461 19990812 00461 WP 1999 8 12 CA990310054 1 19990120 A 5230 ADA7250501 CRANK DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 84220 517819 (CAN) DURING INSPECTION, FOUND CRACK IN FORWARD CARGO DOOR SUPPORT CRANK ASSY CAUSED BY USE OF EXTERNAL POWER SOURCE WHI CH OVERRIDES THE LIMIT SWITCHES. REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1999081200462 19990812 00462 NM 1999 8 12 CA990310055 1 19990114 A 3244 H40X14519 TIRE BENDIX 26066712 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE MLG FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 9808 278 B8254 687708 (CAN) ON TAKEOFF, NR 4 TIRE SHREDDED. TAKEOFF REJECTED. FOUND NR 3 TIRE LOW. WHEELS AND BRAKES REPLACED. FLAP DAMAGE REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200463 19990812 00463 NM 1999 8 12 CA990310056 1 19990129 A 2897 BMST337B WIRE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE LEVEL SWITCH CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 707313 (CAN) DURING AD COMPLIANCE, WIRES FOUND CHAFED IN CENTER TANK FUEL LEVEL SWITCH. CHAFE LOCATED AT FRONT SPAR CONDUIT EX IT POINT AND MEASURED 1.25 INCHES IN LENGTH. STRANDS WERE BROKEN AND PROTUDING, NO VISIBLE SIGNS OF ARCING AT CHAFE PO INT. FUEL WAS DISCOVERED INSIDE CONDUIT IN QUESTION. FLOAT SWITCH AND WIRING REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200464 19990812 00464 NM 1999 8 12 CA990310057 1 19990123 A 5311 6545833453 FRAME BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE BS 245-260 CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 54323 688450 (CAN) DURING INSPECTION OF FUSELAGE DENT, THE FORWARD LEFT LAVATORY WAS REMOVED FOR ACCESS. THE CHORD AT STA 245 AND ST A 260 FOUND CORRODED, REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1999081200465 19990812 00465 1999 8 12 CA990310058 4 19990129 A 3421 258733511 VERTICAL GYRO BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE COCKPIT FAILED W C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 CA 34541 12314 707367 (CAN) AT START OF TAKEOFF ,THE FIRST OFFICER'S ADI PITCHED AND ROLLED. TAKEOFF REJECTED AT 40 KNOTS, REPLACED VERTICAL GYRO. 2 L 7 2 4F 4 F A16WE E2EA 1999081200466 19990812 00466 NM 1999 8 12 CA990310061 1 19990207 A 5320 266T12457 ANGLE BOEING 767 767375 NM BS 246 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 39031 (CAN) ZONAL INSPECTION REVEALED 8 FLOOR SUPPORT ANGLES CRACKED AT FLOORBEAM STA 246. ANGLES REPLACED. 2 L 7 2 4F RT A1NM 1999081200468 19990812 00468 WP 1999 8 12 CA990310063 1 19990214 A 5246 ARB1101 REFUELING DOOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE SEPARATED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA 455337 (CAN) FUEL HANDLER FOUND STARBOARD WING REFUELING PANEL MISSING. NEW PANEL INSTALLED. 2 L 7 3 4F 4 F A22WE E23EA 1999081200469 19990812 00469 CE 1999 8 12 CA990310065 1 19990111 A 3250 50420101 BELLCRANK CESSNA 402 402B 207590P CE CONT O520 TSIO520AE 17040 SO NLG STEERING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20652871E (CAN) THE NOSE STEERING BELLCRANK WAS FOUND CRACKED/BROKEN BETWEEN ATTACH FLANGES. NO OTHER FAULTS FOUND DURING FLEET C HECK. 1 L 7 2 3O 3 O A7CE E8CE 1999081200470 19990812 00470 WP 1999 8 12 CA990310066 1 19990115 A 5310 340311031413 FRAME CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL COCKPIT WINDOW CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 501805 (CAN) LEFT DIRECT VISION WINDOW FRAME FOUND CRACKED, FRAME REPLACED. 2 L 7 2 4R 4 T 6A6 E282 1999081200471 19990812 00471 NM 1999 8 12 CA990310068 1 19990302 A 2782 1U109592 ACTUATOR BOEING 727 727225 1384077 NM PWA JT8 JT8D7B 52053 NE LT WING FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA FE2044D 659586 (CAN) ON CLIMB-OUT, THE NR 2 LE SLAT LEFT WING WOULD NOT RETRACT. SEVERAL ATTEMPTS MADE TO RECTIFY, A/C RETURNED TO BLO CKS. ACTUATOR REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999081200486 19990812 00486 NM 1999 8 12 CA990310084 1 19990515 A 2130 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAILED A UALA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 WP 29 657UA 27112 FL330 CABIN RATE BEGAN TO CLIMB AT MORE THAT 2,000 FEET PER MINUTE. ATTEMPTED AUTO MODE TO NR 2 MANUAL CABIN, STILL CLI MBING WITH OUTFLOW FULLY CLOSED. THE O2 MASKS DEPLOYED. DIVERTED TO RNO. *S/D* UPPER PRESSURE RELIEF VALVE (MR21313, SN OR DASH 2690) REPLACED AT SFO ON 16MAY99. THE PRESSURE RELIEF VALVE WAS SENT TO ALLIED SIGNAL FOR TESTING. PRELIMI NARY TESTS SHOW THE VALVE FAILED OPEN AND WOULD NOT RESEAT. THE OUTFLOW VALVE (MR21314 DASH 10) WAS ALSO REMOVED AT SFO . BOTH THE OUTFLOW VALVE AND THE OUTFLOW VALVE ACTUATOR WERE FOUND WITHIN LIMITS BY THEIR RESPECTIVE COMPONENT SHOP. 2 L 7 2 4F 4 F RT A1NM E24NE 1999081200489 19990812 00489 EU 1999 8 12 CA990310089 1 19990104 A 4920 38075411 APU GARRTT 38075411 FOKKER F28 F28MK1000 4990808 EU APU BAY CONTAMINATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 19525 P37632 (CAN) FLIGHT CREW REPORTED A STRONG OILY SMELL IN COCKPIT AND CABIN. AIRCRAFT FERRIED TO HOME BASE. APU CONTAMINATING AIR SYSTEM, REPLACED. 2 L 7 2 4F RT A20EU 1999081200490 19990812 00490 NM 1999 8 12 CA990310090 1 19990105 A 3230 DSC252B40124 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG LEAKING W C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 CA 120468 (CAN) LOSS OF NR 2 HYDRAULIC SYSTEM AFTER TAKEOFF WITH GEAR UP SELECTION. NLG UP LINE WAS FOUND BLOWN APART. LINE REPL ACED AND SYSTEM CHECKED SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200491 19990812 00491 EU 1999 8 12 CA990310091 1 19990108 A 2932 6607P98 CONNECTOR FOKKER F28 F28MK1000 4990808 EU PRESSURE SWITCH LOOSE W D G RETURN TO BLOCK O2 MASK DEPLOYED B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TX TAXI/GRND HDL 1 CA (CAN) PILOT REPORTED ON LONG TAXI, THAT THE PASSENGER COMPLAINED OF MIST/SMOKE IN THE CABIN. CREW ALSO REPORTED THAT TH EY LOST ALL QUANTITY NR 1 UTILITY HYDRAULIC SYSTEM. AIRCRAFT RETURNED TO GATE, FLIGHT ATTENDANTS PASSED AROUND PORTABL E OXYGEN BOTTLES DUE TO CHOKING AROMA. PASSENGER DEPLANED ASAP. NR 1 UTILITY SWITCH LOOSE IN ITS MANIFOLD AND NOT LOC K WIRED. SWITCH REPLACED. 2 L 7 2 4F RT A20EU 1999081200504 19990812 00504 SW 1999 8 12 CA990311010 1 19990106 A 5610 2719442003 WINDSHIELD SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 317 P03551C (CAN) DURING CRUISE, A CRACK APPEARED IN PILOT'S WINDSCREEN EMANATING FROM LOWER LEFT CORNER. WINDSHIELD HAD BEEN INSPE CTED IAW AD 96-20-08 212 HOURS PREVIOUS. 2 L 7 2 4T 4 T RT A8SW E4WE 1999081200508 19990812 00508 CE 1999 8 12 CA990311014 1 19990108 A 7810 3012290 DUCT BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA EXHAUST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 51331100 (CAN) CRACK FOUND ON THE EXHAUST DUCT BY THE INBOARD FLANGE EAR. NOT IN SEAM OR WELD AREA, JUST OUTSIDE OF SEAM STITCH WELD. 1 L 7 2 3T 4 T A14CE E4EA 1999081200509 19990812 00509 SW 1999 8 12 CA990311015 1 19990108 A 2910 2781032778 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE HYDRAULIC SYSTEM CHAFED W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CA P44720C 931124 (CAN) HYDRAULIC PUMP BYPASS LINE, RT NACELLE AFT OF FIREWALL, CHAFED THROUGH AGAINST PRESSURE HYDRAULIC LINE RESULTING I N TOTAL LOSS OF HYDRAULIC FLUID. BOTH LINES REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999081200510 19990812 00510 SW 1999 8 12 CA990311016 1 19990108 A 3230 602EN6026 SWITCH SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE MLG OUT OF RIG W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA P44205C 930243 (CAN) GEAR FAILED TO FULLY RETRACT WHEN COLD. GEAR UP SWITCHES RIGGED IAW MM SYSTEM SERVICEABLE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999081200511 19990812 00511 SW 1999 8 12 CA990311018 1 19990122 A 2910 2781006003 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE HYDRAULIC SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA P44205C 930243 (CAN) GEAR DOWN LINE FOUND CRACKED COMING FROM POWER PACK. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999081200514 19990812 00514 SW 1999 8 12 CA990311021 1 19990203 A 3260 ML345 SWITCH OSA545319 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE RT MLG INTERMITTENT W K NONE O OTHER IN INSP/MAINT 1 CA 1954 P44663C 881750 (CAN) RIGHT MLG DOWN LIGHT INTERMITTENT. RIGHT MLG SWITCH REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999081200515 19990812 00515 CE 1999 8 12 CA990311022 1 19990210 A 2140 993840337 MOTOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HEATER BLOWER FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 403 403 PCE50747 (CAN) AIRCRAFT RETURNED TO BASE AFTER SMOKE IN THE CABIN DURING CLIMB. COMBUSTION BLOWER REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 1999081200518 19990812 00518 CE 1999 8 12 CA990311025 1 19990216 A 7920 SCETS41685 LINE BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA ENGINE BAY MISALIGNED W A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 CA PCE50392 (CAN) OIL VENT LINE HOSE WAS MISALIGNED SO THAT THE FUEL CONTROL UNIT (FCU) ROD WAS CATCHING ON THE HOSE AND CAUSING THE ENGINE POWER INPUT TO BE STUCK AT 1300 FEET/POUNDS. 1 L 7 2 3T 4 T A14CE E4EA 1999081200522 19990812 00522 CE 1999 8 12 CA990311029 1 19990203 A 3213 998100289 STRUT 1158100006 BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 318 AMA2 PCE40209 (CAN) DURING NDT LEVEL 2 INSPECTION OF GEAR LUGS, CRACKS INDICATIONS WERE DISCOVERED. GEAR REMOVED AND SENT TO THUNDER BAY FOR EVALUATION. NO CRACK INDICATIONS WERE FOUND WITH THE GEAR REMOVED FROM THE ACFT ALTHOUGH BLENDING WAS NOTICED I N THE AREA OF AROUND 0.80 THOUSANDS BY THE LUGS. NO REPAIR SCHEMES WERE FOUND AND BEECH CONTACTED FOR ENGINEERING APPRO VAL. APPROVAL OBTAINED FROM BEECH. GEAR WAS THEN SENT FOR EDDY CURRENT AND REJECTED DUE TO THE CRACKS IN THE BLENDED A REA. THE OVERHAUL AGENCY WAS CONTACTED IN REGARDS TO THE BLENDED AREA AND DISCOVERED IT WAS CERTIFIED BY THEM WITH THE B LENDED AREAS AND WITH NO FIELD REPAIR FROM THE MANUFACTURER. WE DO NOT DEAL WITH THEM ANYMORE. 1 L 7 2 3T 4 T A14CE E4EA 1999081200525 19990812 00525 EA 1999 8 12 CA990311032 2 19990114 A 7250 3013102 BLADE BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA TURBINE SECTION LOOSE W O OTHER O OTHER IN INSP/MAINT 1 CA 2722 50754 (CAN) THE POWER SECTION WAS REMOVED FOR MAINTENANCE AND FOUND THE PT BLADES WERE LOOSE. THE UNIT WAS SHIPPED TO AN OVERH AUL FACILITY FOR REPAIR. 23 BLADES REQUIRED REINSTALLATION AND RIVETING. 1 L 7 2 3T 4 T A14CE E4EA 1999081200559 19990812 00559 WP 1999 8 12 CA990311066 1 19990107 A 2720 1516929115 BELLCRANK LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B NE RUDDER DAMAGED W O OTHER O OTHER NR NOT REPORTED 1 CA 10432 (CAN) AFTER ARRIVAL AT GATE, PILOT REPORTED RUDDER JAMMING OCCURRENCE IN THE RUDDER SYSTEM. MAINT FOUND THAT ONE RUDDE R BELLCRANK HAD AN ELONGATED HOLE AT THE ROD END ATTACHMENT AND A DAMAGED BOLT ON THE RUDDER PEEL ASSY. BOLT AND BELLCR ANK REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200560 19990812 00560 WP 1999 8 12 CA990311067 1 19990113 A 3222 1523460101 TORQUE LINK LKHEED 1523545105 LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10289 (CAN) ON WALKAROUND AT NLG UPPER TORQUE LINK, RT SIDE INNER SLEEVE CRACKED. CRACK STARTED FROM SMALL RADIUS NOTCH AND G OES TO THE OPPOSITE SIDE CAUSING SEPARATION OF PART. WHEN NLG DISCONNECTED, OUTER SLEEVE FOUND CRACKED AND NO GREASE PR ESENT, ZEUS FITTING WOULD NOT TAKE GREASE. ICE FOUND IN SPRING COIL AND SLEEVE. SLEEVE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200562 19990812 00562 WP 1999 8 12 CA990311070 1 19990111 A 2913 AE3506J0244210 LINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B NE HYDRAULIC PUMP CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 10256 (CAN) AIRCRAFT RETURNED DUE TO C-SYSTEM HYDRAULIC QUANTITY DECREASING DURING FLIGHT. FOUND C-HYDRAULIC ELECTRIC PUMP PR ESSURE LINE WITH SMALL PIN HOLE CAUSING LEAK. LINE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200563 19990812 00563 WP 1999 8 12 CA990311071 1 19990112 A 3340 LAC011203D HARNESS LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE STROBE MELTED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 14827 (CAN) ON DEPARTURE, CREW REPORTED THE STROBE LIGHT CIRCUIT BREAKER KEPT TRIPPING. INVESTIGATION REVEALED WIRE CHAFING ON CLAMP CLOSE TO WING LANDING LIGHT. REPAIRED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200564 19990812 00564 WP 1999 8 12 CA990311073 1 19990124 A 2530 CIRCUIT BREAKER LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B NE GALLEY FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 10224 (CAN) AT DEPARTURE, BURN SMELL REPORTED BY FLIGHT ATTENDANT. FOUND SB PANEL NR 4 PASS-SERV MDL NR 1 CIRCUIT BREAKER BUR NED OUT, PASS-SERV MDL NR 2 AND NR 7 CIRCUIT BREAKER DAMAGED BY FIRE AND A WIRE TERMINAL DAMAGE. COFFEE CONTAMINATION INSIDE PANEL. GALLEY DRAIN LEAKING AND RUNNING DOWN INTO PANEL. LEAK REPAIRED, CIRCUIT BREAKER REPLACED, AND WIRES REP AIRED/REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200570 19990812 00570 NM 1999 8 12 CA990311080 1 19990105 A 3230 273N20042 ACTUATOR BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RT MLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 30886 (CAN) DURING WALKAROUND, SMOKE COMING FROM RT GEAR AT BRAKE AREA. RESULT OF TRUCK POSITIONER ACTUATOR LEAKING AT PISTON SEAL. ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200572 19990812 00572 WP 1999 8 12 CA990311083 1 19990114 A 5610 1608087101 WINDSHIELD LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10205 (CAN) CAPTAIN'S WINDSHIELD DELAMINATED AND FAULT LIGHT ALWAYS ON, WINDSHIELD DELAMINATED AT MANY PLACES AROUND CONTOUR O F WINDOW. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200573 19990812 00573 NM 1999 8 12 CA990311084 1 19990130 A 7603 87600520001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE POWER LEVER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 120175 (CAN) RIGHT HAND CONDTION CONTROL CABLE FOUND WITH BROKEN STRANDS. AREA OF DEFECT FORWARD OF PULLEY ON FORWARD SIDE OF ENGINE FIREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200574 19990812 00574 EA 1999 8 12 CA990318003 1 19990305 A 5510 C6TPM104927 BRACKET DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE41343 (CAN) DURING SB 454, CRACKS FOUND AT HORIZONTAL STABILIZER ATTACH BRACKET AND 2 CRACKS IN FORWARD ADAPTER. 1 H 7 2 3T 4 T RT A9EA E4EA 1999081200581 19990812 00581 NM 1999 8 12 CA990318013 1 19990307 A 6120 78249047 PCU DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 INOPERATIVE W L A ABORTED APPROACH UNSCHED LANDING R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 14932 123037 890617 (CAN) ON APPROACH, THE CREW NOTICED A PROGRESSIVE DROP IN NR 2 PROPELLER'S RPM. ATTEMPTS TO CONTROL PROP RPM BY SWITCHI NG EEC TO MANUAL WERE UNSUCCESSFUL. THE CREW ELECTED TO SHUT DOWN THE ENGINE, AND THE AIRCRAFT WAS DIVERTED. POST-FLIGH T INSPECTION FOUND THE PROPELLER CONTROL UNIT FAULTY. THE PROP CONTROL UNIT WAS REPLACED, CHECKED SERVICEABLE, AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999081200583 19990812 00583 EU 1999 8 12 CA990318015 1 19990308 A 6720 704A33657003 BEARING 350A33200401 SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A3 41560 NE TAIL ROTOR BRINNELLED W K NONE O OTHER IN INSP/MAINT 1 CA 1907 ERA202 LE43468CE (CAN) WHEN CARRYING OUT SB 05.00.29, SECTION 2(B), CHECK FOR BRINNELLING/BINDING WHEN ROTATING, A SLIGHT, BUT NOTICEABLE BRINNELLING WAS FELT. 1 G 7 1 3U 3 U H9EU E5NE 1999081200609 19990812 00609 SO 1999 8 12 CA990318051 1 19990226 A 3233 47042000 ARM PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA MLG SHEARED W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 7975 PCE51618 (CAN) DURING CLIMB, PILOTS SELECTED GEAR UP AND HEARD AN UNUSUAL NOISE. IT WAS THEN NOTICED THAT THE LANDING GEAR WOULD NOT RETRACT. GEAR DOWN WAS SELECTED AND THREE GREEN AND NEUTRAL WERE OBSERVED. THE AIRCRAFT WAS SAFELY LANDED WITHOUT INCIDENT. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE ACTUATOR ARM AND ROD END WERE SHEARED OFF, AND NO FURTHER D AMAGE WAS FOUND. 1 L 7 2 3T 4 T A8EA E4EA 1999081200610 19990812 00610 SO 1999 8 12 CA990318052 1 19990302 A 2140 COMBUSTION CAN JANITROL FR10E214EL PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA HEATER CRACKED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 500 A96100038 PCE52025 (CAN) UPON TAXIING FOR TAKEOFF, THE PILOT'S DISCOVERED SMOKE ENTERING THE COCKPIT VIA THE HEATER DUCTS. THE HEATER WAS S UBSEQUENTLY SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FBO. THE AIRCRAFT WAS INSPECTED BY AN A.M.E. AND WAS FLOWN BACK TO BASE WITHOUT HEAT. THE HEATER WAS PRESSURE DECAY TESTED AND FOUND TO BE LEAKING. THE UNIT WAS REPLACED. 1 L 7 2 3T 4 T A8EA E4EA 1999081200612 19990812 00612 NM 1999 8 12 CA990318054 1 19990304 A 3211 85411406101 BUSHING 85410029053 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 20923 0761 120439 (CAN) LEFT NACELLE INBOARD LOWER STRUT TO A FRAME PACKERS. FLANGED BUSHING FOUND SHEARED IN HALF. SB 8-54-19 CW. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200613 19990812 00613 NM 1999 8 12 CA990318055 1 19990305 A 2910 82970410115 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 NACELLE CHAFED W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 11982 120581 (CAN) NR 1 NACELLE-EDP CASE DRAIN LINE AND PRESSURE LINE CHAFING TOGETHER CAUSING A HOLE IN CASE DRAIN LINE. LINE REPLA CED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200614 19990812 00614 NM 1999 8 12 CA990318056 1 19990306 A 3260 83220084101 HINGE 83220082107 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE WOW COVER BROKEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 120803 (CAN) WEIGHT-ON-WHEEL (WOW) CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. NLG WOW SENSOR COVER ROTATED AND DAMAGED BOTH SENS ORS. HINGE FOUND BROKEN AT COVER. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200615 19990812 00615 NM 1999 8 12 CA990318057 1 19990306 A 2910 82970010477 LINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 21435 123039 (CAN) NR 2 EDP LINE TO PRESSURE MANIFOLD LEAKING AT B-NUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200616 19990812 00616 NM 1999 8 12 CA990318058 1 19990305 A 2910 82970010297 LINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 21478 123010 (CAN) NR 2 NACELLE MLG DOWN LINE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200617 19990812 00617 EU 1999 8 12 CA990318059 1 19990305 A 2410 IDG AIRBUS 330 A330202 3930316 EU RT ENGINE FAILED W H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA (CAN) ECAM MSG IDG OVERHEAT, INVESTIGATION REVEALED A LOOSE CANNON CONNECTOR AT UPPER RT PYLON. 2 L 7 2 4F RT A46NM 1999081200620 19990812 00620 SW 1999 8 12 CA990318062 1 19990223 A 6210 269A505071 BEARING 269D63071 HUGHES 269 269C1 8059504 SW FLAPPING HINGE BRINNELLING W K NONE O OTHER IN INSP/MAINT 1 CA 1800 Z024 (CAN) INNER RACE OF FLAPPING HINGE BEARING WAS FOUND BRINNELLED (.001 INCH). 1 G 7 1 3O O 4H12 1999081200625 19990812 00625 SW 1999 8 12 CA990318072 1 19990127 A 5302 206031004111 SKIN BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA BCJN07191 CAE823299 (CAN) DURING 300-HOUR INSPECTION, CRACK WAS FOUND ON TAILBOOM SKIN UNDER THE T/R COVER MOUNTING BRACKET (AFT LT SIDE). CRACK WAS APPROX .1875 INCH LONG. 1 G 7 1 3U 3 U H2SW E4CE 1999081200629 19990812 00629 NE 1999 8 12 CA990323001 1 19990211 A 3211 7620902019044 FITTING 762070200201 SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S 60030 NE LT MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 15111 (CAN) DURING POST-FLIGHT/DI, LT MLG DOOR ATTACHMENT FITTING WAS FOUND BROKEN. 1 G 7 2 3U 3 U H1NE E19EU 1999081200633 19990812 00633 EA 1999 8 12 CA990323006 1 19990310 A 3234 574205 VALVE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE MLG SELECTOR LEAKING W O OTHER K FLUID LOSS AP APPROACH 1 CA 19487 510 123059 (CAN) WHEN SELECTED LANDING GEAR WOULD NOT EXTEND, ALTERNATE GEAR SELECTION MADE. LANDING GEAR SELECTOR VALVE WAS LEAKI NG FROM HOUSING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200636 19990812 00636 SO 1999 8 12 CA990323009 1 19990311 A 3230 4025700 TORQUE LINK 4550402 PIPER PA31 PA31350 7103110 SO LT MLG BROKEN W C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CA 45323 (CAN) THE PILOT REPORTED THAT DURING TAKEOFF, A VIBRATION WAS NOTICED. WHILE IN CLIMB, THE PILOT TRIED TO SELECT 'GEAR U P', BUT THE SELECTOR DETENT KEPT THE SELECTOR IN THE 'DOWN' POSITION. ON INSPECTION, THE REAR LUG ON THE LEFT MLG UPPER TORQUE LINK WAS FOUND BROKEN. BUSHINGS ON STRUT WERE DISTRESSED, BUT LOWER TORQUE LINK HAD NO SIGN OF DAMAGE. ALL BUS HINGS, BOLTS AND LOWER TORQUE LINKS WERE REPLACED. NOTE: GEAR SQUAT SWITCH IS LOCATED ON LEFT UPPER TORQUE LINK. 1 L 7 2 3O A20SO 1999081200641 19990812 00641 CE 1999 8 12 CA990323016 1 19990323 A 2120 CEETS5575 DUCT 9738000033 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA AIR DISTRIBUTION CONTAMINATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) IN CLIMB THROUGH 9,700 FEET, THE CREW NOTICED SMOKE IN THE COCKPIT AND RETURNED TO LAND IMMEDIATELY. SMOKE DISSIP ATED DURING DESCENT. MAINTENANCE FOUND THE RIGHT ENGINE HAD AN ACCUMULATION OF OIL IN THE COWLINGS COUPLED WITH A LOOSE OIL LINE AND AN OIL SATURATED AMBIENT AIR DUCT. THIS DUCT FEEDS THE BLEED AIR CONTROL PACK WITH AMBIENT AIR MIXED WITH ENGINE BLEED AIR WHICH, IN TURN, IS DISTRIBUTED INTO THE AIRCRAFT. THE SYSTEM WAS MONITORED FOR THE NEXT 25 HOURS WITH NO RECURRENCE. 1 L 7 2 3T 4 T A14CE E4EA 1999081200644 19990812 00644 NM 1999 8 12 CA990323019 1 19990313 A 2430 WARNING LIGHT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT ILLUMINATED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 31425 (CAN) AT 90 KNOTS, L GEN DRIVE LIGHT EICAS MSR AND MASTER CAUTION CAME ON, TAKOFF REJECTED. MEL APPLIED IDR DISCONNECTE D. PARTS ON ORDER. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200645 19990812 00645 NE 1999 8 12 CA990323020 2 19990307 A 7320 ESC10304E4 EEC BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE MALFUNCTIONED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA 30827 (CAN) FLIGHT CREW NOTED NR 1 ENGINE COULD NOT REACH SELECTED EPR WITH THROTTLE FULL FORWARD. AT 35 KNOTS, A REJECTED TA KEOFF WAS ACTIONED. MAINTENANCE CARRIED OUT A BITE TEST ON THE LEFT ELECTRONIC ENGINE CONTROL (EEC) AND FOUND AN INTERN AL FAULT. THE EEC WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200654 19990812 00654 CE 1999 8 12 CA990323029 1 19990310 A 2731 NAS302771307 CONTROL CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ELEVATOR TAB BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 6678 GGM114476 (CAN) DURING 6TH 200-HOUR INSPECTION, THE ELEVATOR TAB CABLE WAS FOUND WITH SEVERAL WIRE STRANDS BROKEN. ALSO, THE CABL E WAS FOUND CORRODED IN THE SAME AREA ON A LENGTH OF APPROXIMATELY 1 INCH. DAMAGE WAS VISIBLE FROM ACCESS PANEL 331DL. 2 L 7 2 4T 4 T RT A24CE E26NE 1999081200655 19990812 00655 WP 1999 8 12 CA990323030 1 19990311 A 4920 MS21046C4 APU GARRTT GTCP8590F CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL TUBINE SECTION FOD W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA 380 380 P35235 501130 (CAN) APU SURGING. UNIT REMOVED AND INSPECTED. UPON DISMANTLING THE COMBUSTION SECTION, THE NUT HOLDING THE TURBINE BEA RING HOUSING TO THE MAIN BODY WAS MISSING. WHEN THE NUT CAME LOOSE IT WAS EJECTED THROUGH THE TURBINE NOZZLE AND WHEEL ASSY CAUSING UNREPAIRABLE DAMAGE. APU REPLACED. 2 L 7 2 4R 4 T 6A6 E282 1999081200659 19990812 00659 1999 8 12 CA990330001 4 19990222 A 3432 PIN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GLIDE SLOPE SYS LOOSE W O OTHER I FLT. ATTITUDE INST. AP APPROACH 1 CA 26216 120064 (CAN) AIRCRAFT NOSED OVER ON G/S. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200660 19990812 00660 NM 1999 8 12 CA990330002 1 19990302 A 7603 SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE CONTAMINATED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 26276 120064 (CAN) DURING TAKEOFF, NR 2 ENGINE TORQUE ROLLED BACK TO 70 PERCENT FROM 90 PERCENT. TAKEOFF SENSOR CLEANED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200661 19990812 00661 NE 1999 8 12 CA990330003 2 19990302 A 7321 7898426009 EEC DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE MALFUNCTIONED W O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 CA 16058 85054147 120152 (CAN) ON DESCENT, NR 1 ENGINE HAD AN UNCOMMANDED TORQUE ROLLBACK FROM 55 PERCENT TO 15 PERCENT. TEST OF HARNESS SHOWED SOME FAULTS, CONNECTORS CLEANED, NO HARNESS FAULTS FOUND. ENGINE ELECTRONIC CONTROL REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200662 19990812 00662 1999 8 12 CA990330004 4 19990305 A 3414 2114011342 INDICATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AIRSPEED ERRATIC W C ABORTED TAKEOFF I FLT. ATTITUDE INST. TO TAKEOFF 1 CA 30216 9361 238951 120152 (CAN) TAKEOFF ROLL ,CAPTAIN ASI ERRATIC. REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200663 19990812 00663 EA 1999 8 12 CA990330005 1 19990228 A 3297 3261130A22 WIRE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE MLG CHAFED W B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 18498 123110 (CAN) LEFT GEAR AND DOORS WOULD NOT RETRACT. ALTERNATE EXTENSION CARRIED OUT. WIRE 3261-130A22 SHORTED. RELAY 3261-K1 4 AND PSEU REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200665 19990812 00665 NM 1999 8 12 CA990330007 1 19990311 A 6123 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AUTO FEATHER INTERMITTENT W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 120083 901134 (CAN) AUTOFEATHER LIGHT CAME ON DURING TAKEOFF WITH SWITCH IN THE OFF POSITION. TAKEOFF ABORTED. CONTAMINATED BY COFFE E/POP. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999081200666 19990812 00666 NM 1999 8 12 CA990330008 1 19990304 A 3244 B8525 TIRE BENDIX 26066712 BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 7862 2174 B8525 708808 (CAN) NR 4 TIRE TREAD SEPARATED AND FRAGMENTS DAMAGED. THE RIGHT INBOARD FLAP, REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1999081200667 19990812 00667 1999 8 12 CA990330009 4 19990125 A 2565 D30546105 SLIDE A52175401042 AIRBUS 310 A310304 EU PASSENGER DOOR FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 3492 2910 (CAN) ESCAPE SLIDE FAILED TO DEPLOY, LEFT AFT DOOR. 2 L 7 2 4F RT A35EU 1999081200668 19990812 00668 WP 1999 8 12 CA990330010 1 19990305 A 2612 FIRE LOOP CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL NR 1 ENGINE MALFUNCTIONED W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CA 501345 (CAN) NR 1 ENGINE ZONE 1 FIRE LIGHT AND BELL TRIGGERED. POWER LEVERS PULLED BACK WITH NO RESULT. 'E' HANDLED AND MAIN FIRE BOTTLES DEPLOYED. LIGHT STAYED ON, RESERVE BOTTLE FIRED LIGHT ON. THE FIRE LIGHT WHEN OUT ON APPROACH THROUGH 3,0 00 FEET. INSPECTED AIRCRAFT WIRING, LOOPS AND TAIL PIPE. NO FAULT FOUND. REPLACED THE FIRE WARNING CONTROL RELAY AND ZONE 1 FIRE LOOP. 2 L 7 2 4R 4 T 6A6 E282 1999081200669 19990812 00669 NE 1999 8 12 CA990330011 2 19990318 A 7250 769104 TURBINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED W E C ENGINE SHUTDOWN ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 CA 665763 (CAN) DURING LINE-UP WHEN TAKEOFF POWER WAS APPLIED, AT 1.4 EPR, A LOUD BANG WAS HEARD FOLLOWED BY A RISE IN EGT TO 585 DEGREES CELSIUS, ON NR 2 ENGINE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTIO N FOUND THE T4 TURBINE HAD FAILED. THERE WAS NO VISIBLE BLADE PENETRATION THROUGH THE CASE. THE NR 2 ENGINE WAS REPLACE D AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1999081200670 19990812 00670 NM 1999 8 12 CA990330012 1 19990226 A 5312 6517583504 BULKHEAD BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE BS 178 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 58249 702782 (CAN) WHILE INCORPORATING SB 737-53A1173 PRESSURE BULKHEAD REPLACEMENT STA 178, VERTICAL WEB STA 178 RBL 5.7 IDENTIFIED AS CRACKED 2 CM LONG FROM EDGE OF WEB THROUGH ADJACENT FASTENER HOLE AND THREE CRACKS THROUGH 3 ADJACENT FASTENER HOLES . REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200671 19990812 00671 NM 1999 8 12 CA990330013 1 19990310 A 5312 6517582 BULKHEAD BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE BS 178 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 58249 702782 (CAN) WHILE INCORPORATING SB 737-53A1173 PRESSURE BULKHEAD REPLACEMENT, THE WEB WAS IDENTIFIED AS CRACKED DURING DISASS EMBLY .11 CM LONG Y SHAPED CRACK. WEB REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200672 19990812 00672 SW 1999 8 12 CA990330014 1 19990317 A 5302 206033004011A SKIN BELL 206 206L 1181522 SW TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA AOKP639 (CAN) CRACK IN TAILBOOM SKIN ADJACENT TO HORIZONTAL STABILIZER AREA. CRACK WAS FOUND DURING COMPLIANCE WITH AD CF-98-42 . 1 G 7 1 3U H2SW 1999081200673 19990812 00673 NE 1999 8 12 CA990330016 3 19990316 A 6111 7823011 BEARING DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE PROP BLADE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 9625 910401 (CAN) ON PROPELLER INSPECTION, ONE BLADE WAS NOTICEABLY LOOSE. THE NR 2 BLADE WAS REMOVED AND THE PROP BEARING OUTER RA CE WAS FOUND BROKEN IN TWO PIECES. THE EDGE OF THE SAME RACE WAS CHIPPED AT APPROXIMATELY 180 DEGREES OPPOSITE THE BROK EN AREA. FURTHER INSPECTION OF THE NR 4 BLADE FOUND THE BEARING OUTER RACE EDGE ALSO CHIPPED. 2 H 7 2 4T RT A13NM 6 C P7NE 1999081200678 19990812 00678 SW 1999 8 12 CA990330022 1 19990319 A 2740 MDA3711Q ACTUATOR SWRNGN SA226 SA226AT 8780405 SW GARRTT TPE331 TPE33110UA 01514 WP PITCH TRIM MALFUNCTIONED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA P54098 (CAN) PITCH TRIM FAILED IN-FLIGHT. SUBSEQUENT INVESTIGATION REVEALED THAT BOTH UPLIMIT SWITCH ACTUATORS WERE STICKING. SWITCHES CLEANED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A5SW E4WE 1999081200693 19990812 00693 SO 1999 8 12 CA990330040 1 19990315 A 7160 35515006 AIR BOX 8624531 PIPER PA44 PA44180 7104402 SO LYC O360 O360E1A6 41514 EA ENGINE FOD W A UNSCHED LANDING O OTHER DE DESCENT 1 CA 7780 L30077T (CAN) ON THE CARBURETOR AIR BOX BOTTOM ASSY COVER THERE ARE TWO FELT STRIPS SECURED WITH 6 STAPLES. AS THE FELT WORE, T HE WIRE STAPLES BECAME LOOSE AND FELL OUT AND LODGED IN THE THROTTLE BORE AT THE BUTTERFLY VALVE (P/N 87327003). THIS PR EVENTED THE PILOT FROM REDUCING POWER. AN IN-FLIGHT SHUTDOWN WAS NECESSARY. THE SUBMITTER SUGGESTS SECURING THE FELT S TRIPS BETWEEN RIVITED ALUMINIUM WOULD ELIMINATE THE PROBLEM. 1 L 7 2 3O 3 O A19S0 E286 1999081200698 19990812 00698 CE 1999 8 12 CA990330049 1 19990302 A 3297 WIRE BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA MLG BROKEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA PCE40209 (CAN) AIRCRAFT RETURNED TO BASE AFTER TAKEOFF AS THE GEAR WOULD NOT RETRACT. WIRE FOUND BROKEN ON PRESSURE SWITCH. 1 L 7 2 3T 4 T A14CE E4EA 1999081200699 19990812 00699 WP 1999 8 12 CA990330050 2 19990302 A 7230 310812511 BLADE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE COMPRESSOR FRACTURED W C ABORTED TAKEOFF E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA P44722C 880393 (CAN) NR 1 ENGINE WAS SHUTDOWN ON TAKEOFF DUE TO A LOUD BANG FOLLOWED BY A DROP IN OIL PRESSURE. POST-TAKEOFF INSPECTIO N FOUND 1ST STAGE COMPRESSOR BLADE FAILED DUE TO AN INCLUSION CRACK. EVERYTHING DOWNSTREAM WAS DAMAGED BEYOND REPAIR. T HE ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999081200700 19990812 00700 SW 1999 8 12 CA990330052 1 19990316 A 3411 STATIC SYSTEM SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE PITOT CONTAMINATED W A UNSCHED LANDING I N FLT. ATTITUDE INST. FALSE WARNING CL CLIMB 1 CA 880393 (CAN) AIRCRAFT RETURNED TO BASE AFTER TAKEOFF DUE TO VSI, ASI, AND ALTIMETER READINGS WERE UNRELIABLE. WATER/ICE FOUND IN SYSTEM. 2 L 7 2 4T RT A8SW 6 C 3PNE 1999081200701 19990812 00701 CE 1999 8 12 CA990330054 1 19990322 A 2810 1003810051 CAP BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA FUEL CELL LEAKING W O OTHER K FLUID LOSS CR CRUISE 1 CA PCE50747 (CAN) LEFT NACELLE FUEL CAP LEAKING IN CRUISE. UNIT REPLACED AND RETURNED TO SERVICE. BAD SEAL CONTACT DUE TO IMPROPER FIT. 1 L 7 2 3T 4 T A14CE E4EA 1999081200702 19990812 00702 CE 1999 8 12 CA990330055 1 19990322 A 3232 99810057651 ACTUATOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG OUT OF LIMITS W K NONE O OTHER IN INSP/MAINT 1 CA 639 EAS1864 PCE41799 (CAN) AT FIRST END PLAY CHECK, PINION GEAR WAS FOUND TO BE OUT OF LIMITS. 0.10 THOUSAND PLAY IN PINION. 1 L 7 2 3T 4 T A14CE E4EA 1999081200703 19990812 00703 CE 1999 8 12 CA990330056 1 19990322 A 2140 E10D40 HEATER BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA CABIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2229 8976155 51808 (CAN) JANITROL HEATER REMOVED FROM AIRCRAFT DUE TO FUEL LEAKING OUT OF NOZZLE END. UPON INSPECTION OF TEARDOWN, IT WAS DISCOVERED THAT THE WELD AREA OF THE COMBUSTION CAN AT THE NOZZLE END HAD TWO CRACKS IN THE WELD AREA. 1 L 7 2 3T 4 T A14CE E4EA 1999081200708 19990812 00708 WP 1999 8 12 CA990330061 1 19990304 A 3233 269002119 ACTUATOR LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B NE MLG DOOR MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 10432 (CAN) AFTER TAKEOFF, RIGHT MLG DOOR AND INTRANSIT LIGHT ILLUMINATED. INVESTIGATION REVEALED THAT THE DOOR ACTUATOR P/N 2-690021-19 WAS U/S. 2 L 7 3 4F 4 F A23WE E12EU 1999081200709 19990812 00709 WP 1999 8 12 CA990330062 1 19990305 A 5210 LOCK PIN LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B NE PASSENGER DOOR NOT ENGAGED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 10432 (CAN) L3 WARN LIGHT CAME ON, AIRCRAFT LANDED. INVESTIGATION REVEALED LOCK PIN NOT ENGAGED. PIN LUBRICATED AND CHECKED S ERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 1999081200710 19990812 00710 1999 8 12 CA990330064 4 19990302 A 3418 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE STALL WARNING FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 8752 807380 (CAN) IN CLIMB, STALL CAUTION MESSAGE AFTER 8 DEGREE FLAP. FIRST OFFICER STALL TAPE CAME UP TO 160 KNOTS. QUICK REF HA NDBOOK CARRIED OUT. FIRST OFFICER TAPE 190 KNOTS AT FLAP ZERO DEGREE, 145 KNOTS AT FLAP 45 DEGREE. CHANGED LEFT HAND A NGLE OF ATTACK SENSOR, AND NR 2 MACH TRANSDUCER. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200711 19990812 00711 EA 1999 8 12 CA990330065 1 19990305 A 2750 PDU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 8766 807380 (CAN) FLAP FAIL MESSAGE IN-FLIGHT WITH ZERO FLAP SELECTED. DURING APPROACH, FLAPS DID NOT EXTEND. FLAP POWER DRIVE UN IT CHANGED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200712 19990812 00712 EA 1999 8 12 CA990330066 1 19990309 A 2750 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 8788 807380 (CAN) AFTER LANDING FLAPS LOCKED OUT ON RETRACTION, RIGHT HAND BRAKE POSTION SENSING UNIT AND FLAP ELECTRONIC CONTROL UN IT RESET. RIGHT HAND OUTBOARD FLAPS RERIGGED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200713 19990812 00713 EA 1999 8 12 CA990330067 1 19990313 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT SHATTERED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 8804 807380 (CAN) IN CLIMB THROUGH 10,000 FEET THE FIRST OFFICER'S WINDSHIELD SHATTERED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200714 19990812 00714 NM 1999 8 12 CA990330068 1 19990225 A 2420 GENERATOR BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA P707548 (CAN) DURING CRUISE, RT ENGINE GENERATOR FAULT, CREW DISCONNECTED INTEGRATED DRIVE GENERATOR. A/IRCRAFT RETURNED. RT G ENERATOR OFF DISPLAYED, AUX POWER UNIT GENERATOR LIGHT EXITING BUS TIE RESET NORMAL. SNAG REPEAT. REPLACED RT BUS TIE BREAKER, RT INTEGRATED DRIVE GENERATOR, GENERATOR POWER CONTROL UNIT, DIFFERENTIAL PROTECTION CURRENT TRANSFORMER, AUXIL IARY POWER UNIT AND GENERATOR CONTROL UNIT. 2 L 7 2 4F 4 F RT A1NM E3NE 1999081200715 19990812 00715 EA 1999 8 12 CA990330069 1 19990225 A 2750 TE FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE WING FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 807157 (CAN) ON APPROACH, THE FLAPS FAILED. AIRCRAFT LANDED FLAPLESS OK. SYSTEM RESET. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200716 19990812 00716 WP 1999 8 12 CA990330070 1 19990219 A 2841 INDICATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FUEL QUANTITY FAILED W O OTHER K FLUID LOSS NR NOT REPORTED 1 CA P657239D (CAN) FUEL SPILL FROM RIGHT WING VENT BOX DURING RE-FUELING, PASS AND CREW EVACUATED. LEFT WING FUEL QUANTITY INDICATOR NOT WORKING. REPLACED BOTH LUGS ON FUEL QUANTITY PROBE. 2 L 7 2 4F 4 F A6WE E2EA 1999081200717 19990812 00717 EA 1999 8 12 CA990330071 1 19990312 A 3222 STRUT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG DAMAGED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 7485 807337 (CAN) ON TAKEOFF DURING GEAR RETRACTION, A GEAR DISAGREE ANNUNCIATION. MAIN GEAR UP, BUT NOSE GEAR DOWN. GEAR SELECTED TO DOWN AND AIRCRAFT RETURNED. THE NOSE GEAR OLEO FLOATING PISTON WAS NOT FULLY BOTTOMED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200718 19990812 00718 EA 1999 8 12 CA990330072 1 19990312 A 3520 PSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE SEAT 8 DEPLOYED W O OTHER O OTHER NR NOT REPORTED 1 CA 807389 (CAN) TWO PASSENGER OXYGEN UNITS OPENED IN-FLIGHT AND DROPPED ON PASSENGER SEAT 8D/F. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200719 19990812 00719 NM 1999 8 12 CA990330073 1 19990311 A 2780 SENSOR BOEING 767 767333 NM PWA 4060 PW4060 52119 NE LE FLAP FAILED W C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 CA P724695 (CAN) ON TAKEOFF DURING FLAP RETRACTION LEADING EDGE FLAP ASYMMETRY ANNUNCIATED AND LE FLAP LOCK OUT BETWEEN ZERO AND 1. QRH PROCEDURE CARRIED OUT. AIRCRAFT RETURNED TO BLOCKS. ON FINAL APPROACH, LE FLAP ASYMMETRY AND DISAGREE ANNUNCIAT ED INTERMITTENTLY AFTER MASTER CAUTION CANCELLED FOLLOWED AGAIN BY RANDOM ILLUMINATION. REPLACED NR 9 LE FLAP SLAT POSI TION SENSOR. 2 L 7 2 4F 4 F RT A1NM E24NE 1999081200720 19990812 00720 NM 1999 8 12 CA990330074 1 19990311 A 2710 ACTUATOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE AILERON FAILED W O OTHER N FALSE WARNING CR CRUISE 1 CA P707675 (CAN) AILERON LOCKOUT MESSAGE ON ENGINE INDICATING AND ALERT AND CREW ALERT SYSTEM ON CLIMB AND DESCENT. REPLACED RT AI LERON LOCKOUT ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E3NE 1999081200721 19990812 00721 EA 1999 8 12 CA990330076 1 19990309 A 2750 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 CA 807173 (CAN) FLAP FAIL AT 45 DEGREES AND ONCE AT 41 DEGREES. RIGHT BPSU REPLACED AND RE-RIGGED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200722 19990812 00722 EA 1999 8 12 CA990330077 1 19990308 A 3230 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG SELECTOR FAILED W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 CA 807217 (CAN) GEAR SELECTED UP, UNSAFE INDICATION. VIBRATION. RETURNED TO TORONTO. NOSE GEAR SELECTOR VALVE, DOOR SELECTOR VA LVE REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200723 19990812 00723 NM 1999 8 12 CA990330078 1 19990316 A 2720 SERVO BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE YAW DAMPER LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA P707553 (CAN) DURING FLIGHT, LEFT HYDRAULIC QUANTITY INDICATED .75. IT REDUCED STEADILY TILL LEFT SYSTEM PRESSURE, LEFT QUANTIT Y AND RUDDER RATIO MESSAGE APPEARED. AIRCRAFT DIVERTED. ON APPROACH, INOP LIGHT CAME ON. FOUND LEAK COMING FROM RUDD ER POWERPACK AREA. REPLACED YAW DAMPER SERVO ASSY. 2 L 7 2 4F 4 F RT A1NM E3NE 1999081200727 19990812 00727 NM 1999 8 12 CA990330082 1 19990305 A 3244 0262020 TIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 571 8255P00960 PCE120170 (CAN) 10 INCH SECTION OF THREAD AND SIDEWALL MISSING AFTER LANDING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200728 19990812 00728 EU 1999 8 12 CA990330083 1 19990311 A 5610 NP1701012 WINDSCREEN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT SHATTERED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 10529 91155H2889 LF05653A (CAN) COPILOT'S WIND SCREEN SHATTERED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200732 19990812 00732 WP 1999 8 12 CA990521060 1 19990513 A 3242 21367 BRAKE 313752 LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 2503 10432 (CAN) NR 1 AFT MAIN WHEEL HARD TO REMOVE. INVESTIGATION REVEALED ONE BRAKE DISK RUBBING AGAINST HEATSHIELD ON WHEEL. E XCESSIVE EXPANSION OF THE DISK CAUSED IT TO CONTACT THE HEATSHIELD. BRAKES WILL BE MODIFIED TO BF GOODRICH SL 142 9. 2 L 7 3 4F 4 F A23WE E12EU 1999081200737 19990812 00737 NM 1999 8 12 CA990707001 1 19990615 A 2434 23088002A GENERATOR LUCAS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE START/GENERATOR FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 4919 45 1104 120083 (CAN) DURING CRUISE, NR 2 DC GENERATOR FELL OFF-LINE. GENERATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200738 19990812 00738 NM 1999 8 12 CA990707002 1 19990603 A 2910 82950010277 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT NACELLE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24211 120152 (CAN) HYDRAULIC LEAK IN LT NACELLE. PINHOLE FOUND IN OUTBOARD ROLL SPOILER ACTUATOR LIFT/DUMP LINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200739 19990812 00739 NM 1999 8 12 CA990707003 1 19990616 A 3242 68728 SEAL BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BRAKE ASSY FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 13321 1673 120152 (CAN) INVESTIGATION OF BRAKE UNIT REMOVED FOR LEAKING. REVEALED A DAMAGED PISTON O-RING AND THE BACKUP RING FOLDED OVER THE PISTON IN THE SAME AREA. BREAK WEAR WAS .057 INCH REMAINING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200740 19990812 00740 NM 1999 8 12 CA990707004 1 19990618 A 2120 78279012 ACM HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AIR DISTRIBUTION LEAKING W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 13426 4852 900147 120152 (CAN) UPON INVESTIGATION OF AN AIR QUALITY PROBLEM, THE OUTLET DUCT OF THE AIR CYCLE MACHINE WAS FOUND TO BE CONTAMINATE D WITH LUBRICATION OIL. THE OULET DUCT WAS CLEANED, THE ACM REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200741 19990812 00741 EA 1999 8 12 CA990707005 1 19990604 A 3246 2661942 HOUSING BFGOODRICH 21517 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE BRAKE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11150 0361 123113 (CAN) DURING NDT INSPECTION OF BRAKE HOUSING, A CRACK WAS FOUND AROUND THE MOUNTING HOLE. SCRAPPED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200744 19990812 00744 NM 1999 8 12 CA990707009 1 19990603 A 3232 82910010193 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG DOOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 26825 121165 (CAN) HYDRAULIC LEAK IN NOSE AREA. NOSE DOOR SHUT LINE FOUND TO BE CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200745 19990812 00745 EA 1999 8 12 CA990707010 1 19990610 A 3230 DSC252B40124 LINE AEROQUIP SC252B40124 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 19051 123116 (CAN) NLG DRAG STRUT ACTUATOR RETRACT FLEX LINE FAILED IN THE AREA WHERE THE LINE ENTERS THE SWAGED FITTING AT THE ACTUA TOR END. IN-FLIGHT LOSS OF NR 2 SYSTEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200746 19990812 00746 EA 1999 8 12 CA990707013 1 19990605 A 3230 82910010209 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 18585 123133 (CAN) HYDRAULIC LEAK IN NLG BAY. GEAR DOWN LINE WAS FOUND WITH A PIN HOLE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200749 19990812 00749 EA 1999 8 12 CA990707018 1 19990613 A 3350 5521981 BATTERY PACK GRIMES 6038441 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE CABIN OVERHEATED W K NONE M OVER TEMP IN INSP/MAINT 1 CA 4966 159 0924 123110 (CAN) A SECTION OF EMERGENCY TRACK LIGHTING U/S. BATTERY PACK TESTED SERVICEABLE, HOWEVER, THERE WAS EVIDENCE OF OVERH EATING. PACK WAS IN OPERATION FOR 23 DAYS AND 234 CSN. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200751 19990812 00751 NM 1999 8 12 CA990707020 1 19990618 A 3350 82410162005 CONTROL UNIT DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE EMERGENCY LIGHT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 123124 (CAN) EMERGENCY LIGHTS COME ON WHEN SELECTED OFF FROM ARM POSITION. EMERGENCY LIGHT CONTROL UNIT REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200752 19990812 00752 NM 1999 8 12 CA990707021 1 19990614 A 5531 85530184 FRAME DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE VERTICAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16744 120229 (CAN) DURING SCHEDULED INSPECTION, A CRACK WAS LOCATED AT A RIVET HOLE ON FRAME NR 4 OF VERTICAL STABILIZER. REPAIRED B Y DWG NR 8-55-199. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200753 19990812 00753 NM 1999 8 12 CA990707022 1 19990627 A 3244 265X813 TIRE BFGOODRICH 314353 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG FAILED W O OTHER O OTHER LD LANDING 1 CA 1354 121158 (CAN) NR 4 MAIN WHEELTIRE FAILED ON LANDING TO A 6 RUPTURE IN THE INNER SIDEWALL. TIRE WAS A THOMPSON RECAP ON ITS 3RD CYCLE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200758 19990812 00758 EA 1999 8 12 CA990707045 1 19990624 A 3246 MS2125005018 BOLTS BFGOODRICH 312791 CNDAIR CL215 CL2151A10 EA MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 111 0529 (CAN) DURING DISASSEMBLY FOR ROUTINE NDT INSPECTION AND TIRE CHANGE, TWO TIE BOLTS WERE DISCOVERED SHEARED OFF. TORQUE APPEARED TO BE WITHIN MM SPECS. 2 H 7 2 4R A14EA 1999081200770 19990812 00770 NE 1999 8 12 CA990707066 2 19990605 A 7210 M06569AA GEARBOX LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE ENGINE MAKING METAL W A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 CA 14826 (CAN) ENGINE FLAME-OUT AT 35,000 FEET. NO FUEL FLOW WAS OBSERVED. GEARBOX MCD FERROUS CONTAMINATION OBSERVED. THE PRE LIMINARY CONCLUSION WAS DUE TO THE GEARBOX FAILURE, THE FUEL FLOW REGULATOR STOPPED TURNING CAUSING THE FUEL FLOW TO DRO P TO ZERO CAUSING THE ENGINE TO QUIT. FURTHER INVESTIGATION IS TO BE DONE TO GEARBOX, SN CM 5532. 2 L 7 3 4F 4 F A23WE E12EU 1999081200781 19990812 00781 NM 1999 8 12 CA990715018 1 19990629 A 2611 UNKNOWN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GALLEY SMOKE W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 120843 (CAN) FLIGHT ATTENDANT REPORTED A SMOKY ODOR FROM THE LAV/GALLEY AREA. SMOKE DETECTED IN LAVATORY, DETECTOR WENT OFF SH ORTLY AFTER. THERE WAS A STRONG SMELL OF SMOKE WITH NO VISIBLE SIGNS OF SMOKE. NO ABNORMALITIES FOUND. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200789 19990812 00789 EU 1999 8 12 CA990715037 1 19990626 A 2120 FILTER AIRBUS 320 A320211 3930320 EU AIR DISTRIBUTION FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) CABIN SMOKE/HAZE AND ODOR OCCURRED DURING FLIGHT. WHEN APU SELECTED TO OFF, CONDITION IMPROVED. RECIRCULATION FI LTERS AND RECIRC FAN REPLACED. 2 L 7 2 4F RT A28NM 1999081200790 19990812 00790 EA 1999 8 12 CA990715039 1 19990628 A 2721 TRIM PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RUDDER FAILED W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED NR NOT REPORTED 1 CA 807453 (CAN) RUDDER TRIM RUNAWAY ON OPERATION OF RUDDER TRIM. DRILL COMPLETED/OPERATES NORMAL. TRIM PANEL REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200791 19990812 00791 NM 1999 8 12 CA990715041 1 19990701 A 5610 WINDSHIELD AIRBUS A319 A319114 NM COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PILOTS WINDSHIELD OUTER PLY FAILED IN CRUISE. WINDSHIELD REPLACED. 2 L 7 2 4F RT A28NM 1999081200801 19990812 00801 EA 1999 8 12 CA990719017 1 19990615 A 5210 TORQUE TUBE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR OUT OF RIG W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 807389 (CAN) DOOR WARNING LIGHT ON IN-FLIGHT. TORQUE TUBE UPPER LATCH CAMS FOUND OUT OF RIG. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200802 19990812 00802 EA 1999 8 12 CA990719018 1 19990625 A 5311 FRAME CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BS 718 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 807281 (CAN) FUSELAGE STATION 718.0, STRINGERS 10-12 FOUND CRACKED ON BOTH SIDES OF FUSELAGE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200803 19990812 00803 EA 1999 8 12 CA990719019 1 19990625 A 5311 FRAME CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BS 718 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 807213 (CAN) FUSELAGE STATION 718.0, STRINGERS 10-12 FOUND CRACKED ON BOTH SIDES OF FUSELAGE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200804 19990812 00804 EU 1999 8 12 CA990719020 1 19990607 A 3340 SWITCH AIRBUS 320 A320211 3930320 EU BEACON FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) SPARKS OBSERVED COMING FROM BEACON SWITCH. CIRCUIT BREAKER OPENED, SWITCH REPLACED. 2 L 7 2 4F RT A28NM 1999081200805 19990812 00805 EU 1999 8 12 CA990719021 1 19990607 A 2913 SHAFT AIRBUS 320 A320211 3930320 EU FUEL PUMP SHEARED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) ECAM INDICATED NR 1 HYDRAULIC OVERHEAT. INVESTIGATION REVEALED NR 1 ENGINE DRIVEN PUMP DRIVESHAFT SHEARED. 2 L 7 2 4F RT A28NM 1999081200806 19990812 00806 NM 1999 8 12 CA990719022 1 19990607 A 2750 GEARBOX AIRBUS A319 A319114 NM TE FLAP JAMMED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) FLAPS JAMMED IN POSITION 2. LEFT NR 4 ANGLE GEARBOX FAILED. 2 L 7 2 4F RT A28NM 1999081200807 19990812 00807 NM 1999 8 12 CA990719023 1 19990609 A 3260 25GA SENSOR AIRBUS A319 A319114 NM NLG FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. CENTRAL MONITORING SYSTEM INDICATED SENSOR 25GA FAULT. SENSOR REPL ACED. 2 L 7 2 4F RT A28NM 1999081200808 19990812 00808 EU 1999 8 12 CA990719024 1 19990610 A 2612 WIRE AIRBUS 320 A320211 3930320 EU NR 2 ENGINE DAMAGED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) NR 2 ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ON. INVESTIGATION REVEALED DAMAGE TO CONDUIT INDICATION WIRING CAUS ING WIRES TO SHORT. 2 L 7 2 4F RT A28NM 1999081200809 19990812 00809 EU 1999 8 12 CA990719025 1 19990613 A 3260 136GA SENSOR AIRBUS 320 A320211 3930320 EU NLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) LANDING GEAR FAILED TO SHOW UP AND LOCKED INDICATION, NOSE LANDING GEAR DOOR OPEN SENSOR NR 1 36 GA REPLACED. 2 L 7 2 4F RT A28NM 1999081200810 19990812 00810 EU 1999 8 12 CA990719026 1 19990613 A 2120 VALVE AIRBUS 320 A320211 3930320 EU E/E BAY FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) VENT AVIONICS SYSTEM FAULT MESSAGE ILLUMINATED AFTER TAKEOFF. SKIN AIR OUTLET VALVE FOUND AT FAULT AND REPLACED. 2 L 7 2 4F RT A28NM 1999081200811 19990812 00811 EU 1999 8 12 CA990719027 1 19990613 A 4920 APU AIRBUS 320 A320211 3930320 EU APU BAY FAILED W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA (CAN) OIL SMELL IN COCKPIT AND FORWARD GALLEY AFTER TAKEOFF. APU REPLACED. 2 L 7 2 4F RT A28NM 1999081200812 19990812 00812 1999 8 12 CA990719030 4 19990626 A 2350 RADIO PANEL AIRBUS A319 A319114 NM COCKPIT FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) ODOR COMING FROM RADIO MANAGEMENT PANEL, PANEL U/S. PANEL REPLACED. 2 L 7 2 4F RT A28NM 1999081200813 19990812 00813 NM 1999 8 12 AWXA9900252 1 19990801 A 3397 BMS13131122 WIRE BOEING 737 7373Q8 1384670 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 1ST CLASS AND APPROX 7 FLOOR TRACK EMERGENCY LIGHTS INOP. FOUND AND REPAIRED BROKEN WIRE IN EMERGENCY PATH LIGHTING SYS TEM ROW 3. OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999081200814 19990812 00814 NM 1999 8 12 AWXA9900253 1 19990803 A 3040 6937346123 MODULE BOEING 737 7373G7 1384595 NM COCKPIT WINDOW INOP A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 304AW 16302 68 24011 NML OPS, ELECTRICAL SMELL IN COCKPIT. UNKNOWN ELECTRICAL SMELL IN COCKPIT. INSPECTED COCKPIT, RAN ENGINES ISOLATED ODO R TO P5-9 WINDOW, PITOT HEAT MODULE. REPLACED PER MM 30-09-11. ACFT OK FOR SERVICE (TAG 014234). 2 L 7 2 4F RT A16WE 1999081200815 19990812 00815 NM 1999 8 12 AWXA9900254 1 19990803 A 7110 COWL BOEING 737 737112 1384412 NM NR 1 ENGINE CRACKED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 IN MAINTENANCE, NR 1 ENG OB COWL SKIN CRACKED. REMOVED DAMAGED AREA, FABRICATED DOUBLER OF 2024-T3 .040 AND FILLER 2024 -T3 .032. ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED IAW SRM 51-32-.2 2 L 7 2 4F A16WE 1999081200816 19990812 00816 NM 1999 8 12 AWXA9900255 1 19990803 A 5320 ANGLE BOEING 737 737112 1384412 NM BS 1156 CRACKED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 IN MAINTENANCE, FOUND CRACKED ANGLE AT AFT LOWER CORNER OF APU COMPARTMENT AT BS 1156. FABRICATED ANGLE WITH 7075T-6 .0 63. TREATED, PRIMED, AND INSTALLED IAW SRM 51-10-2 AND SRM 51-30-2. 2 L 7 2 4F A16WE 1999081200817 19990812 00817 NM 1999 8 12 AWXA9900256 1 19990803 A 5720 WEB BOEING 737 737112 1384412 NM RT WING CRACKED A AWXA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 WP 28 708AW 19771 IN MAINTENANCE, FOUND NR 3 WEB RIGHT WING HAS 9 CRACK OUTBD FROM END OF AILERON. REMOVED CRACKED WEB. FABRICATED WEB 2 024-T3 .032. TREATED, PRIMED, AND INSTALLED WEB IAW SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1999081200818 19990812 00818 WP 1999 8 12 CALA9900940 1 19990803 A 3230 49397051 UPLOCK DOUG DC9 DC981 3022081 WP RT MLG BROKEN A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 13881 48045 THE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING EWR. THE LANDING GEAR WAS CYCLED AND THE LIG HT EXTINGUISHED. THE FLIGHT CONTINUED TO BOS WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND A BROKEN SPRING ON UPLOCK AND DOOR LATCH MECHANISM. THE SPRING WAS REPLACED. A PSEU BITE WAS PERFORMED IAW MM 32-60-04 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999081200819 19990812 00819 WP 1999 8 12 CALA9900941 1 19990802 A 5347 SUPPORT TRACK DOUG DC9 DC982 3022082 WP BS 1231-1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND AFT CARGO LT SUPPORT TRACK CORRODED AT FS 1231-1322. A NEW TRACK WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999081200820 19990812 00820 WP 1999 8 12 CALA9900942 1 19990802 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBOARD SUPPORT BETWEEN O/B AND CENTER SEAT TRACK AT FS 1136, BL 0 TO RBL 48 CORRODED. THE FLOOR SU PPORT WAS REMOVED IAW SRM 51-30-2. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-13-3, 51-10-03, AND 51-30-1. 2 L 7 2 4F A6WE 1999081200821 19990812 00821 WP 1999 8 12 CALA9900943 1 19990802 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 200 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND TWO PUNCTURES IN SUBFLOOR AT STA 200, LBL 50. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3 , 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1999081200822 19990812 00822 WP 1999 8 12 CALA9900944 1 19990802 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBOARD SUPPORT BETWEEN O/B AND CENTER SEAT TRACK CORRODED AT STA 1155, RBL 48 TO BL 0. THE FLOOR S UPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. 2 L 7 2 4F A6WE 1999081200823 19990812 00823 WP 1999 8 12 CALA9900945 1 19990802 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1155-1160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1155-1160. A NEW SECTION OF SEAT TRACK AND A SPLICE PLATE WERE INSTA LLED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999081200824 19990812 00824 NM 1999 8 12 CALA9900946 1 19990803 A 5330 SKIN BOEING 757 757224 1384958 NM BS 1880 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1880 BETWEEN STRINGER 3 AND 4L. REPAIRED IAW ECRA 5331-01062. 2 L 7 2 4F RT A2NM 1999081200825 19990812 00825 WP 1999 8 12 CALA9900947 1 19990803 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND RT WING FUEL ACCESS PANEL NR 1410 CHAFED AND CORRODED. THE ACCESS PANEL WAS REMOVED AND REPLACED IAW S RM 51-10-3. 2 L 7 2 4F A6WE 1999081200826 19990812 00826 WP 1999 8 12 CALA9900948 1 19990803 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1117 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBOARD ATTACH ANGLE CRACKED IN AFT CARGO AREA AT FS 1117, LONGERON 28L-28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1999081200827 19990812 00827 WP 1999 8 12 CALA9900949 1 19990803 A 5730 ARB0872515 PANEL DOUG DC9 DC982 3022082 WP LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LT WING FUEL ACCESS PANEL NR 1335 CORRODED AND CHAFED. A NEW PANEL WAS INSTALLED IAW MM 51-10-3. 2 L 7 2 4F A6WE 1999081200828 19990812 00828 WP 1999 8 12 CALA9900950 1 19990803 A 5347 SUPPORT TRACK DOUG DC9 DC982 3022082 WP BS 1212-1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND AFT CARGO RT SUPPORT TRACK CORRODED AT FS 1212-1322, RBL 24. THE SUPPORT TRACK WAS REMOVED AND REPLACE D IAW SRM 51-30-1 AND 51-10-03. 2 L 7 2 4F A6WE 1999081200829 19990812 00829 WP 1999 8 12 CALA9900951 1 19990803 A 5753 ANGLE DOUG DC9 DC982 3022082 WP LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 2 INCH CRACK IN LT FLAP NR 2 HINGE AFT FAIRING INTERNAL L-ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-10-3. 2 L 7 2 4F A6WE 1999081200830 19990812 00830 WP 1999 8 12 CALA9900952 1 19990803 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBOARD/FORWARD ENTRY DOOR THRESHOLD ATTACH ANGLE CORRODED AT STA 200, LBL 63. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 53-10-1. 2 L 7 2 4F A6WE 1999081200831 19990812 00831 WP 1999 8 12 CALA9900953 1 19990803 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND CABIN FLOORBOARD ATTACH ANGLE CORRODED AT STA 180, RBL 6 TO RBL 36. THE ANGLE WAS REMOVED AND NEW ANGL E WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-4. 2 L 7 2 4F A6WE 1999081200832 19990812 00832 WP 1999 8 12 CALA9900954 1 19990803 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 140-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 140-200, LBL 6. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INS TALLED IAW SRM 51-10-3, 51-30-1, AND 51-10-4. 2 L 7 2 4F A6WE 1999081200833 19990812 00833 WP 1999 8 12 CALA9900955 1 19990803 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND CABIN FLOORBOARD ATTACH ANGLE CORRODED AT STA 200, RBL 6 TO RBL 52. THE ANGLE WAS REMOVED AND A NEW AN GLE WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999081200834 19990812 00834 WP 1999 8 12 CALA9900956 1 19990803 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 229 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 229 ABOVE LONGERON 18L. REPAIRED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1999081200835 19990812 00835 WP 1999 8 12 CALA9900957 1 19990803 A 5730 SKIN DOUG DC10 DC1030 3023501 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 2 INCH CRACK IN LT WING DROOPED LEADING EDGE SKIN. A REPAIR WAS PERFORMED IAW SRM 57-10-00. 2 L 7 3 4F A22WE 1999081200836 19990812 00836 WP 1999 8 12 CALA9900958 1 19990803 A 5320 CLIP DOUG DC10 DC1030 3023501 WP BS 1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND CENTER CARGO COMPARTMENT SHEAR CLIP CORRODED AT STA 1721 FROM LONGERON 47-48R. REPLACED SHAER CLIP IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999081200837 19990812 00837 EU 1999 8 12 RAIA990635 1 19990624 A 3220 AIR83586 NOSE GEAR JETAIR JETSTM JETSTM4101 1500501 EU FWD FUSELAGE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 570HK 41089 FLT 7753 - NOSEWHEEL STEERING DOORS NOT WORKING LEFT OR RIGHT. MAINTENANCE REPLACED NOSE GEAR ASSY. (M) 2 L 7 2 4T RT A41NM 1999081200838 19990812 00838 EU 1999 8 12 RAIA990634 1 19990623 A 3250 AIR8601212 SELECTOR JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 570HK 41089 FLT 7635 - JFK - NOSEWHEEL STEERING DOES NOT WORK. TILLER UNEFFECTIVE ONLY WAY TO STEER IS THROUGH USE OF DIFFERENTIAL BRAKING. MAINTENANCE REPLACED NOSE STEERING SELECTOR. (M) 2 L 7 2 4T RT A41NM 1999081200839 19990812 00839 EU 1999 8 12 RAIA990633 1 19990623 A 2422 1B3501B13 INVERTER BAG JETSTM JETSTM3201 1500217 EU NR 1 FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 867AE 867 FLT 4793 - FAT - LEFT RMI, RIGHT HEADING IND AND RIGHT ADI INOPERATIVE. MAINTENANCE REPLACED NR 1 STATIC INVERTER. (M) 2 L 7 2 4T RT A56EU 1999081200840 19990812 00840 NM 1999 8 12 MASA99109 1 19990630 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING ROUTINE MAINTENANCE, FOUND NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT POWER SUPPLY AND 2 BULBS, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1999081200841 19990812 00841 NM 1999 8 12 99ZZZM423 1 19990630 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING ROUTINE MAINTENANCE, FOUND NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT POWER SUPPLY AND 2 BULBS, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1999081200842 19990812 00842 NM 1999 8 12 MASA99110 1 19990630 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM COCKPIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING ROUTINE MAINTENANCE, FOUND F/A EMERGENCY LIGHT PUSH BUTTON SWITCH GREEN 'NORMAL' BACKLIGHTING FAILED TO ILLUMINAT E. REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1999081200843 19990812 00843 NM 1999 8 12 MASA99103 1 19990624 A 3350 6038443 POWER SUPPLIES DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 FLT 6551 - PHX-SBP - THE CAPTAIN NOTED THERE WERE NUMEROUS CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL 6 POWER SUPPLIES. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999081200844 19990812 00844 NM 1999 8 12 F3LA99090 1 19990629 A 5320 SHEAR TIE BOEING 737 737201 1384454 NM BS 294.5 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION REPORTED, CRACK IN SHEAR TIE, LAST RIVET TO EDGE OF TIE, AT BS 294.5 ABOVE STRINGER 13L. MAINTENANCE REPAIRED CRACKED AT SHEAR TIE PER SRM 53-10-4, FIG 8. (M) 2 L 7 2 4F A16WE 1999081200845 19990812 00845 NE 1999 8 12 F3LA99091 2 19990622 A 7230 IGV BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION REPORTED NR 2 ENGINE INLET GUIDE VANE CRACKED AND STOP DRILLED AT 2 O'CLOCK POSITION, AF T WELD. MAINTENANCE WELDED CRACK IAW P/W E/M 72-23-04, REPAIR 14, PAGES 901 AND 902, SUBTASK 1, 2, 3 AND 4 AND STRESS R ELIEVED IAW P/W E/M 72-23-01, REPAIR 14. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999081200846 19990812 00846 NM 1999 8 12 F3LA99088 1 19990629 A 7110 ANGLE BOEING 737 737201 1384454 NM NR 2 COWL CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK, INSPECTION REPORTED CRACK AT NR 2 ENGINE NOSE COWL FAIRING (SUGAR SCOOP) SEAL RETAINER INNER ANGLE . MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1999081200847 19990812 00847 NM 1999 8 12 F3LA99087 1 19990628 A 5414 SKIN BOEING 737 737201 1384454 NM PYLON CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN PYLON INNER SKIN WHERE PANEL 5243 ATTACHES. MAINTENANCE REMOVED AND DAMAGED AREA AND REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1999081200848 19990812 00848 NM 1999 8 12 F3LA99086 1 19990625 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 360 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK, INSPECTION REPORTED STRINGER 7R CRACKED ON AFT SIDE OF CIRCUMFERENTIAL FUSELAGE SPLICE AT BS 360. MAINTENANCE REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED STRINGER PER SRM 51-10-2, 51-30-2 AND 51-20-01. (M) 2 L 7 2 4F A16WE 1999081200849 19990812 00849 NM 1999 8 12 F3LA99100 1 19990708 A 2497 WIRE HARNESS BOEING 737 737201 1384454 NM VERTICAL STAB DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DURNG C-CHECK INSPECTION, REPORTED DAMAGED WIRING IN THE VERTICAL STABILIZER. CAUSE OF DAMAGE APPEARS TO BE SKYDROL HYD RAULIC FLUID. THE DAMAGE BEGAN APPROX 8 INCHES FROM RUDDER PCU ELECTRICAL CONNECTORS D-289 AND D-291 AND CONTINUED FOR APPROX 5 FEET, AFFECTING A TOTAL OF 20 WIRES. (M) 2 L 7 2 4F A16WE 1999081200850 19990812 00850 NM 1999 8 12 F3LA99102 1 19990710 A 5400 FAIRING BOEING 737 737201 1384454 NM NR 1 NACELLE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT AFT INBOARD ATTACH POINT. MA INTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M) 2 L 7 2 4F A16WE 1999081200851 19990812 00851 NM 1999 8 12 F3LA99101 1 19990710 A 5400 FAIRING BOEING 737 737201 1384454 NM NR 1 NACELLE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT FORWARD OUTBOARD ATTACH POINT . MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M) 2 L 7 2 4F A16WE 1999081200852 19990812 00852 NM 1999 8 12 F3LA99099 1 19990630 A 7830 RIB BOEING 737 737201 1384454 NM NR 1 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER AFT END. MAINTEN ANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M) 2 L 7 2 4F A16WE 1999081200853 19990812 00853 NM 1999 8 12 F3LA99098 1 19990630 A 7830 RIB BOEING 737 737201 1384454 NM NR 1 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER LOWER SIDE. MAIN TENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M) 2 L 7 2 4F A16WE 1999081200854 19990812 00854 NM 1999 8 12 F3LA99097 1 19990630 A 5320 CHORD BOEING 737 737201 1384454 NM BS 663.75 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION, REPORTED THREE CRACKS FOUND IN PRESSURE DECK COMPRESSION CHORD AT STATION 663.75, RBL 2 5 AND LBL 25. MAINTENANCE FABRICATED AND REPLACED RIB PER EA 51-737-003 AND SRM 51=40-3. (M) 2 L 7 2 4F A16WE 1999081200855 19990812 00855 NM 1999 8 12 F3LA99094 1 19990625 A 7810 EXHAUST CASE BOEING 737 737201 1384454 NM NR 2 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION, REPORTED NR 2 ENGIEN EXHAUST CASE CRACKED AT 3 O'CLOCK STRUT, TOP SIDE. MAINTENANCE ST OP DRILLED AND WELDED CRACK PER P/W MM 72-54 PAGE 204 AND BAC 5975. (M) 2 L 7 2 4F A16WE 1999081200856 19990812 00856 NM 1999 8 12 F3LA99093 1 19990623 A 7810 EXHAUST CASE BOEING 737 737201 1384454 NM NR 2 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURNG C-CHECK INSPECTION, REPORTED NR 2 ENGINE EXHAUST CASE STRUT CRACKED AT 9 O'CLOCK POSITION AT ROOT. MAINTENA NCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC5975. (M) 2 L 7 2 4F A16WE 1999081200857 19990812 00857 NM 1999 8 12 F3LA99092 1 19990623 A 7810 EXHAUST CASE BOEING 737 737201 1384454 NM NR 2 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION, REPORTED A 3 INCH CRACK IN THE NR 2 ENGINE EXHAUST CASE UNDER 3 O'CLOCK POSITION STRUT, EXTENDING TOWARD CENTER OF CASE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC 5975. ( M) 2 L 7 2 4F A16WE 1999081200858 19990812 00858 WP 1999 8 12 GTIA9900885 1 19990615 A 5720 39120703501 TRAP FITTING DOUG DC9 DC932 3022066 WP LT WING DEFECTIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - ULTRASONIC INPECTION SHOWS AN INDICATION OF A DEFECT ON THE INBOARD SIDE OF THE INBOARD VETICAL BOLT ON THE LEFT R EAR SPAR TO TRAPEZOIDAL FITTING. REPLACED TRAP FITTING PER S/B NR 57-129 JACKED AND SHORED A/C. REMOVED AND REPLACED A ILERON CABLE MIXER FITTINGS RIGGED AILERON BUS CABLE AILERON LATERIAL CONTROL MIXER AND TRIM TAB PER MM DC9 27-10-0 PAGE 17, 9, 10, 12, 13. (M) 2 L 7 2 4F A6WE 1999081200859 19990812 00859 WP 1999 8 12 GTIA9900886 1 19990615 A 5753 5913560155 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 13512 48111 MHV - LEFT WING FLAP LEADING EDGE INBOARD P/N 5913560-455 HAS DELAMINATION AND SURFACE CORROSION PART LOATED ON RACK. R EMOVED FLAP CAP ASSY FOR FURTHER INSPECTION. FOUND TO BE OUT OF LIMITS. CAP ASSY REPLACED WITH NEW PART, BACK DRILLED SEALED AND INSTALLED NEW CAP ASSY PER DC0 SRM 51-10-4 AND SRM 51-30 DC9 SRM 57-00 AND SRM 27-00. SEALED CAP ASSY, INSTA LLED FIXED FLAP VANE DC9 MM 27-51-3. (M) 2 L 7 2 4F A6WE 1999081200860 19990812 00860 WP 1999 8 12 GTIA9900890 1 19990127 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 160-220 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FORWARD PASS COMPARTMENT FS 160-220 BL 0 FLOOR SUPPORT ANGLE HAS MILD TO HEAVY CORROSION ENTIRE LENGTH. FLOOR SUP PORT WAS FABRCIATED ALODINED PRIMED AND INSTALLED COMPLETE IAW DC9 SRM 51-10-3, 51-30-5. (M) 2 L 7 2 4F A6WE 1999081200861 19990812 00861 WP 1999 8 12 GTIA9900891 1 19990201 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 160 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FORWARD PASS COMPARTMENT FS 160 FLOOR SUPPORT ANGLE CORRODED LBL 15 TO 55. REMOVED SUPPORT ANGLE, FABRICATED NEW SUPPORT FROM 60-2576 7075T6 PO NR 81278 ALODINED AND PRIMED IAW DC9 SRM 50-10-3. INSTALLED SUPPORT IAW DC9 SRM 51-30-0. (M) 2 L 7 2 4F A6WE 1999081200862 19990812 00862 WP 1999 8 12 GTIA9900893 1 19990127 A 2560 BRACKET DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - R1 DOOR SLIDE SUPPORT BRACKET IS CRACKED FORWARD EDGE. STOP DRILLED CRACK USING .25 INCH DIAMETER DRILL AND BAB D OUBLER IAW DC9 SRM 53-01 FIG 2 DRILLED AND COUNTER SINK RIVET HOLES IAW SRM DC9 51-10-4 AND 51-30-2 ALODINE AND PRIMED I AW DC9 SRM 51-10-3 EDDY CURRENT TEST AND NO DEFECTS FOUND ATTACHED DOUBLER IAW 53-01 FIG 2 INSTALLED ON A/C. (M) 2 L 7 2 4F A6WE 1999081200863 19990812 00863 WP 1999 8 12 GTIA990892 1 19990130 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 955 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - AFT CARGO FS 955 RBL 24 EVIDENCE OF MODERATE TO HEAVY LOAL CORROSION ON FLOORBEAM UPPER CAP. REMOVED AND REPLACED UPPER CAP FABRICATED NEW CAP FROM 7075T6511 EXTRUSION S912758T PO NR 81788. INSTALLED FASTENER PER DC9 SRM 51-30-1 FOR TORQUE OF BOLTS DC9 SRM 51-30-2 FOR RIVET DC9 SRM 51-30-5 FOR HI-LOCKS PART WAS FABRICATED IAW DC9 SRM 51-10-1. (M) 2 L 7 2 4F A6WE 1999081200864 19990812 00864 WP 1999 8 12 GTIA9900894 1 19990127 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-230 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FORWARD PASS COMPARTMENT FS 200 TO 230 RBL 42 SEAT TRACK HAS EXFOLIATION CORROSION ON UPPER SURFACE. REMOVED DAMA GED SECTION OF SEAT TRACK CUT NEW SECTION OF SEAT TRACK EXTRUSION 52914913 PO 81257. FABRICATED AND DRILLED IAW SRM 53- 05 . TREATED AND PRIMED NEW TRACK SECTION IW SRM 51-10-3. INSTALLED TRACK IAW SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1999081200865 19990812 00865 WP 1999 8 12 GTIA9900895 1 19990127 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 220 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FORWARD PASS COMPARTMENT FS 220 RBL 21 SEAT TRACK HAS EXFOLIATION CORROSION ON TOP SURFACE. REMOVED SEAT TRACK AN D REPLACED NEW SEAT TRACK FOR DC9 SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 1999081200866 19990812 00866 WP 1999 8 12 GTIA9900896 1 19990129 A 5320 STIFFENER DOUG DC9 DC932 3022066 WP BS 484 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - LEFT INBOARD FLOOR STATION 484 HAS RIVETS PULLING THROUGH AND BOTH ENDS OF ALL STIFFENERS ARE CRACKED ON 484 AND 5 20. REMOVED DAMAGED STIFFENERS. FABRICATED NEW STIFFENERS LOCATED AND DRILLED IAW SRM 51-01 TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED STIFFENERS IAW SRM 51-30-2 DC9. (M) 2 L 7 2 4F A6WE 1999081200867 19990812 00867 WP 1999 8 12 GTIA9900897 1 19990203 A 5412 BULKHEAD FRAME DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - LEFT PYLON BULKHEAD FORWARD FACE BULKHEAD FRAME HAS A 3.5 INCH CRACK BETWEEN STRINGERS 15 AND 16. REMOVED ANGLE A ND REPLACED WITH NEW ANGLE 9912243-9 PO NR 8125801 PER DC9 SRM 51-30-2 FOR RIVETS 51-30-5 FOR HI-LOCKS. (M) 2 L 7 2 4F A6WE 1999081200868 19990812 00868 WP 1999 8 12 GTIA9900899 1 19990126 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 120 GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 120 WATER LINE 0 HAS A DENT APPROX 1 INCH BY 1 INCH AND IS GOUGED. CUT OUT AREA DAMAGE, FABRICATED DOUBLER AND FILLER AND INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-04 FIG 38 218 AND INSTAL LED FASTENERS IW SC9 SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1999081200869 19990812 00869 WP 1999 8 12 GTIA9900900 1 19990126 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 148 GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 148 WATER LINE 0 HAS A COUPLE OF GOUGES. CUT OUT AREA DAMAGE, FABRICAT E DOUBLER AND FILLER AND INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-04 FIG 38 PAGE 218 AND IAW DC9 SRM 51-30-02 AND 51- 30-05. INSTALLED FASTENERS. (M) 2 L 7 2 4F A6WE 1999081200870 19990812 00870 WP 1999 8 12 GTIA9900901 1 19990129 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 130 GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 130 WATER LINE 0 HAS A COUPLE OF GOUGES. REMOVED DAMAGED AREA (CUT OUT ) AND REPAIRED IAW DC9 SRM 53-04 FIG 38 SHT 21, 51-30-2 AND 51-30-5 JOB COMPLETE REPAIRED FRAME AT FS 130 PER BOEING MES SAGE AUQ-MQJ-99-004RA DATED 12-MAR-99. (M) 2 L 7 2 4F A6WE 1999081200871 19990812 00871 WP 1999 8 12 GTIA9900902 1 19990202 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 617 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FS 617 RBL 50 RIGHT SIDE FLOOR CHIME PLATE CRACKED ON BOTH SIDES OF LIGHTENING HOLE. REMOVED AND REPLACED FLOOR C HIME PLATE IAW SRM 51-00 AND 51-30-02 JOB COMPLETE. (M) 2 L 7 2 4F A6WE 1999081200872 19990812 00872 WP 1999 8 12 GTIA9900903 1 19990202 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR LIGHTNING STRIKE A GTIA K NONE C F.O.D. IN INSP/MAINT 1 GL 23 13512 48111 MHV - RIGHT ELEVATOR TRAILING EDGE OUTBOARD SIDE HAS EVIDENCE OF LIGHTNING STRIKE. MATERIAL ID 10 DOUBLER 2024T3.020 MA TERIAL ID FOR TRAILING EDGE 2024T3.040 , ALODINED AND PRIMED PER SRM DC9 51-10-3. INSTALLED FABRICATED PARTS PER SRM 55 -20-0 FIG 2. (M) 2 L 7 2 4F A6WE 1999081200873 19990812 00873 WP 1999 8 12 GTIA9900904 1 19990202 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 995 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - AFT CABIN ANGLE FS 995 LBL 0-60 HAS CORROSION BEYOND LIMITS CORROSION. REMOVED TO .035 ONLY ALLOWED .025 OER SRM 53-01 PAGE 6. REMOVED CORRODED ANGLE. REPLACED WITH NEW EXTRUSION 7075-T6511 MATERIAL DRILLED AND LOCATED NEW PART ALO DINE AND PRIMED INSTALLED PER DC9 SRM 51-10-3, 53-05, 51-10-01, 51-01, 53-01, 51-30-2, 51-30-5. (M) 2 L 7 2 4F A6WE 1999081200874 19990812 00874 WP 1999 8 12 GTIA9900907 1 19990129 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - FLOORBOARDS FS 160-200 BL 0 TO LBL 42 CORRODED AND SUPTS CRACKED. FABRICATED A NEW SKIN IAW DC9 SRM 53-21-0, 4B I NST HAT SUPPORTS IAW DC9 SRM 53-21-0. ALODINE AND PAINT IAW DC9 SRM. INSTALLED RIVETS IAW SRM DC9. (M) 2 L 7 2 4F A6WE 1999081200875 19990812 00875 WP 1999 8 12 GTIA9900909 1 19990319 A 2620 FIRE HANDLE DOUG DC9 DC932 3022066 WP NR 2 ENGINE STUCK A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 MHV - NR 2 ENIGNE FIRE HANDLE WILL NOT TURN TO NR 1 FIRE AGENT. REPOSITIONED FUEL SHUTOFF VALVE LEVER PER MM DC9 76-20- 0 PAGE 205. (M) 2 L 7 2 4F A6WE 1999081200876 19990812 00876 NM 1999 8 12 AALA990737 1 19990522 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 19 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366AA 25193 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999081200877 19990812 00877 NM 1999 8 12 AALA990738 1 19990522 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 23 DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366AA 25193 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23 INOPERATIVE. CONNECTED EMERGENCY EXIT LIGHT WIRE AT SEAT 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999081200878 19990812 00878 WP 1999 8 12 AALA990839 1 19990608 A 3230 CDK2146A1 LINK DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 482AA 49675 BOS - FLT 1197 - AFTER TAKEOFF EN ROUTE PVD-ORD, UNABLE TO RETRACT NOSE LANDING GEAR. AIRCRAFT DIVERTED AND LANDED BOS WITHOUT INCIDENT. REPLACED LOWER TORQUE LINK AND HOLLOW PIN FOR LOWER TORQUE LINK. ACCOMPLISHED GEAR SWING. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200879 19990812 00879 WP 1999 8 12 AALA990889 1 19990617 A 3610 CLAMP DOUG DC9 DC982 3022082 WP NR 2 ENGINE LOOSE A AALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 70524 49916 DFW - FLT 1233 - AFTER TAKEOFF TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED WITH MASTER WARNING. ANTI-ICE WAS OFF. ON T HROTTLE BACK, LIGHT EXTINGUISHED, BUT ILLUMINATED AGAIN ON THROTTLE UP. APU WAS OFF AT THE TIME. AIR INTERRUPTED RETUR NED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED TWO CLAMPS ON RIGHT PRESSURE REGULATOR. INSPECTION OF DUCT AND VALVE FOR CRACKS, CHECKED GOOD. ACCOMPLISHED LEAK AND OPERATIONS CHECK AT ENGINE RUN UP. HAD NO OVERHEAT LIGHT. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200880 19990812 00880 WP 1999 8 12 AALA990887 1 19990617 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 7/17 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7530 49922 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 7 AND 17 INOPERATIVE. REPLACED SE AT MOUNTED SEAT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200881 19990812 00881 WP 1999 8 12 AALA990872 1 19990615 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77421 49333 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD SECTION OF COACH INOPERATIVE. REPAIRED WIRING ON EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200882 19990812 00882 WP 1999 8 12 AALA990862 1 19990613 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP RT LAVATORY DISCHARGED A AALA A UNSCHED LANDING L NO TEST CR CRUISE 1 SW 07 579AA 53156 LAS - FLT 2051 - EN ROUTE RNO-DFW - EMERGENCY EXIT LIGHTS ILLUMINATED. AIRCRAFT AIR INTERRUPTED AND LANDED LAS WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO DFW FOR REPAIRS. EMERGENCY EXIT OVERHEAD LIGHTS ILLUMINATED IN FLIGHT, CREW PULLED C IRCUIT BREAKERS AND LANDED DFW WITHOUT INCIDENT. REPLACED EMERGENCY EXIT BATTERY PACK IN RIGHT LAVATORY CEILING. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200883 19990812 00883 WP 1999 8 12 AALA990873 1 19990615 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT AFT LAVATORIES SEVERED. SPLICED IN REPAIR STRIP FOR EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200884 19990812 00884 WP 1999 8 12 AALA990793 1 19990528 A 3260 833703 SENSOR DOUG DC9 DC983 3022083 WP RT MLG DAMAGED A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 564AA 49346 ORD - FLT 2268 - EN ROUTE DFW-ORD, GEAR DOOR OPEN LIGHT FLICKERED AND CAME ON INTERMITTENTLY DURING CLIMB IN LIGHT CHOP. LIGHT CAME ON STEADY AT CRUISE (33,000 FT) HYDRAULIC PUMPS WERE LOW/OFF. ABNORMAL PROCEDURE WAS FOLLOWED AND RIGHT PU MPED PLACED IN HIGH POSITION, LIGHT EXTINGUISHED AND REMAINED OUT FOR REMAINDER OF FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED LIGHT MLG DOOR SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999081200885 19990812 00885 EU 1999 8 12 AALA990860 1 19990609 A 2530 8803010000 OVEN FOKKER F28 F28MK0100 4990807 EU GALLEY DEFECTIVE A AALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1460A 11480 FSD - FLT 1155 - DURING CRUISE EN ROUTE MSP-DFW, FLIGHT ATTENDANT REPORTED SMOKE IN FORWARD GALLEY AREA. NOTED A STRONG SMELL OF ELECTRICAL BURNING AND THIN GRAY SMOKE. VISIBLE SMOKE STOPPED WITHOUT ACTION FROM CREW, GALLEY POWER WAS TURN ED OFF AS A PRECAUTION. DECLARED EMERGENCY, AIR INTERRUPTED AND LANDED FSD WITHOUT INCIDENT. REPLACED FORWARD GALLEY O VEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999081200886 19990812 00886 WP 1999 8 12 AALA990856 1 19990612 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN MISWIRED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 7517A 49894 DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY DOOR EXIT MARKER INOPERATIVE. REVERSED CONNECTOR IN FIRST CLASS SECTION. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200887 19990812 00887 WP 1999 8 12 AALA990858 1 19990613 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERWING SIGN INOPERATIVE. REPAIRED WIRES ON EMERGENCY EXIT OVERWING SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200888 19990812 00888 WP 1999 8 12 AALA990859 1 19990613 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 276AA 49273 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200889 19990812 00889 WP 1999 8 12 AALA990836 1 19990607 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 453AA 2387 49558 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200890 19990812 00890 WP 1999 8 12 AALA990846 1 19990609 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT SECTION OF AIRCRAFT INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHT STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200891 19990812 00891 WP 1999 8 12 AALA990845 1 19990609 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 552AA 53034 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHTS STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200892 19990812 00892 WP 1999 8 12 AALA990794 1 19990530 A 3260 833703 SENSOR DOUG DC9 DC983 3022083 WP RT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 564AA 49346 ORD - FLT 1063 - EN ROUTE YYZ-ORD, GEAR DOOR OPEN LIGHT ILLUMINATED DURING CLIMB AT APPROX 300 KNOTS. ABNORMAL PROCEDUR E WAS FOLLOWED AND RIGHT PUMP PLACED IN HIGH POSITION, LIGHT EXTINGUISHED AND REMAINED OUT FOR REMAINDER OF FLIGHT. LAN DED ORD WITHOUT INCIDENT. REPLACED GEAR DOOR SENSOR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999081200893 19990812 00893 WP 1999 8 12 AALA990795 1 19990601 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 470AA 49600 DFW - FLT 2049 - EN ROUTE ATL-DFW - NOSE GEAR RED LIGHT FLICKERED ON CLIMB-OUT AND DURING CRUISE. LANDED DFW WITHOUT IN CIDENT. REPLACED NOSE LANDING GEAR UPLOCK SENSOR AND PSEU. ACCOMPLISHED PSEU BITE CHECK. ACCOMPLISHED SEVERAL NOSE LA NDING GEAR RETRACTIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200894 19990812 00894 WP 1999 8 12 AALA990797 1 19990425 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7536A 49990 ABQ - FLT 468 - AFTER TAKEOFF ABQ, CREW SMELLED STRONG BURNING SMELL IN COCKPIT AND CABIN. AIR INTERRUPTED AND RETURNED TO ABQ. LANDED WITHOUT INCIDENT. REPLACED COALESCER BAGS DUE TO OIL FROM APU AND PERFORMED PACK BURN OUT. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200895 19990812 00895 WP 1999 8 12 AALA990854 1 19990610 A 3222 GA70363MJG VALVE DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 14551 53033 DFW - FLT 1760 - AFTER TAKEOFF DFW EN ROUTE MCO, NOSE GEAR WOULD NOT RETRACT. AIR INTERRUPTED BACK DFW AND LANDED WITHO UT INCIDENT. REPLACED SHRADER VALVE AND SERVICED NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200896 19990812 00896 WP 1999 8 12 AALA990792 1 19990528 A 2612 CONNECTORS DOUG DC9 DC982 3022082 WP LT ENGINE DEFECTIVE A AALA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 07 248AA 49259 MIA - FLT 1479 - DURING CLIMB-OUT FROM FLL AT APPROX 15,000-18,000 FT, THE MASTER CAUTION AND FIRE DETECTION LIGHTS ILLU MINATED, ALONG WITH LOOP 'B' LIGHT FOR THE LEFT ENGINE. PERFORMED APPROPRIATE CHECKLIST AND THE LEFT ENGINE FIRE LIGHT ILLUMINATED ALONG WITH THE AURAL FIRE WARNING. ALL ENGINE INDICATIONS WERE NORMAL FOR CLIMB SETTINGS. THE FIRE HANDLE WAS PULLED AND BOTH FIRE BOTTLES WERE FIRED. FIRE LIGHT REMAINED ILLUMINATED THROUGHOUT FLIGHT. LANDED MIA WITHOUT FUR THER INCIDENT. REPLACED LOWER LOOP 'A' AND 'B' CONNECTORS, GROUND TERMINAL AND LOWER LOOP SUPPORT ASSEMBLY. ACCOMPLISH ED FULL POWER RUN, FIRE TEST OPERATIONS CHECK NORMAL. NO FIRE DETECTION LIGHT NOTED. NO LEAK NOTED. REPLACED FIRED BO 2 L 7 2 4F A6WE 1999081200897 19990812 00897 WP 1999 8 12 AALA990796 1 19990529 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 380-402 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 587AA 53250 ORD - INSPECTION OF ANTENNA INSTALLED CUTOUTS FOUND TWO DOME NUTS ON BOTH CUTOUTS WITH CORROSION, EXTERIOR FUSELAGE SKIN HAS SCRATCHES AROUND BOTH CUTOUTS. CLEANED DOME AND PRIMED WITH ZINC CHROMATE PRIMER SCRATCHES WITH IN LIMITS PREVIOUS LY BURNISHED OUT. (M) 2 L 7 2 4F A6WE 1999081200898 19990812 00898 NM 1999 8 12 AALA990838 1 19990607 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 684AA 25341 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT FLAT CONNECTOR FORWARD AND AFT IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F RT A2NM 1999081200899 19990812 00899 NM 1999 8 12 AALA990774 1 19990526 A 2497 WIRE BOEING 767 767323 1385205 NM CABIN CHAFED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 353AA 24034 LHR - FLT 57 - AFTER TAKEOFF LHR WHILE EN ROUTE TO MIA, CREW SMELLED SMOKE IN FORWARD GALLEY AREA. FORWARD CABIN TEMPER ATURE LIGHTS ILLUMINATED, PASSENGER 02 LIGHT ILLUMINATED AND DROPPED 02 MASKS, VARIOUS CIRCUIT BREAKERS POPPED. CREW DE CLARED AN EMERGENCY AND AIR INTERRUPTED BACK TO LHR AND LANDED WITHOUT INCIDENT. CHAFED WIRE BUNDLE ABOVE FIRST CLASS C ENTRAL CLOSET AREA WAS REPAIRED ACCORDING TO AIRCRAFT WIRING MANUAL CHAPTER 20. ALL RELEVANT CIRCUITS TESTED NORMAL. O 2 MASKS RESTOWED, AND MANUAL 02 TEST PERFORMED NORMAL. FORWARD TEMPERATURE CONTROL OPERATION CHECKS NORMAL. SYSTEM GRO UND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999081200900 19990812 00900 NM 1999 8 12 AALA990762 1 19990525 A 3340 A31207 LIGHT BOEING 757 757223 1384957 NM COCKPIT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 601AN 27052 CCS - FLT 2133 - WHEN NOSE GEAR LANDING LIGHT IS TURNED ON, SPARKS CAN BE SEEN COMING FROM THE SWITCH AREA. PLACARDED N OSE GEAR LANDING LIGHT INOPERATIVE PER MEL. CIRCUIT BREAKER PULLED AND COLLARED. FLEW FLIGHT TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999081200901 19990812 00901 NM 1999 8 12 AALA990847 1 19990606 A 2613 CONNECTOR BOEING 767 767223 1385123 NM CARGO COMPT LOOSE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 339AA 22336 RDU - FLT 174 - DURING CRUISE, FORWARD CARGO OVERHEAT STATUS MESSAGE AND OVERHEAD LIGHT ILLUMINATED IN FLIGHT. AIR INTE RRUPTED BACK TO RDU AND LANDED WITHOUT INCIDENT. NO SIGN OF SMOKE OR HOT CONDITION. SECURED CANNON PLUG ON TEMPERATURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999081200902 19990812 00902 NM 1999 8 12 AALA990917 1 19990621 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 308AA 22314 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 28B INOPERATIVE. SECURED WIRE CONNECTION ON SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999081200903 19990812 00903 WP 1999 8 12 AALA990916 1 19990621 A 3350 SOCKET DOUG DC9 DC982 3022082 WP PAX DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7506 49800 DFW - DURING OVERNIGHT, FORWARD EMERGENCY EXIT FLOOR LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT F LOOD LIGHT SOCKET AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200904 19990812 00904 WP 1999 8 12 AALA990915 1 19990621 A 3397 WIRE DOUG DC9 DC982 3022082 WP GALLEY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 478AA 49653 DFW - DURING OVERNIGHT, MAINTENANCE FORWARD GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED WIRE TO FORWARD GALLEY EME RGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200905 19990812 00905 WP 1999 8 12 AALA990914 1 19990621 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 9D BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 560AA 53090 DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT STRIP AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081200906 19990812 00906 WP 1999 8 12 AALA990913 1 19990621 A 3350 SOCKET DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70401 49312 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT AFT FLIGHT ATTENDANT POSITION INOPERATIVE. REPLACE D LIGHT SOCKET AT AFT FLIGHT ATTENDANT OVERHEAD EMEGENCY EXIT LIGHT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 1999081200907 19990812 00907 NM 1999 8 12 AALA990912 1 19990621 A 3350 LIGHTS BOEING 757 757223 1384957 NM CABIN TRIPPED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 686AA 25343 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AND FORWARD PART OF AIRCRAFT STAYS ILLUMINATED IN ARMED POSITION. RESET EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999081200908 19990812 00908 WP 1999 8 12 AALA990829 1 19990601 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 581AA 53158 TUL - FOUND HOLE DAMAGED FOR NR 3 ACCESS PLATE BOTTOM OF RT WING (SCREW HOLE). CLEANED UP HOLE (MADE ROUND). INSTALLED PLUG PER ESO 80559. (M) 2 L 7 2 4F A6WE 1999081200909 19990812 00909 WP 1999 8 12 AALA990830 1 19990525 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 581AA 53158 TUL - FOUND CRACK IN LONGERON 2R AFT OF STATION 1418, ROUTED OUT TO .5 BY .25 PER ESO 80559, DATED 4/3/98. INSTALLED RE PAIR PER AARD 53-30-00-2, LONGEORN SPLICE. (M) 2 L 7 2 4F A6WE 1999081200910 19990812 00910 WP 1999 8 12 AALA990826 1 19990527 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1433 PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 581AA 53158 TUL - FOUND HOLE IN FUSELAGE SKIN 18 INCHES UP FROM AFT STAIR CUT OUT RIGHT SIDE STATION 1433. CUT OUT DAMAGE. INSTALL ED FLUSH REPAIR PER SRM 53-40 FIG 1. (M) 2 L 7 2 4F A6WE 1999081200911 19990812 00911 WP 1999 8 12 AALA990827 1 19990809 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 451 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND NR 6 SEAT TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999081200912 19990812 00912 WP 1999 8 12 AALA990828 1 19990526 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 237 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 581AA 53158 TUL - FOUND DENT/CREASE IN SKIN AND FRAME STRUCTURE .39 INCHES AFT OF FORWARD ENTRY, BELOW RED STRIPE, BETWEEN LONGERON 17L AND 18L, STATION 237. REMOVED DAMAGED AREA. INSTALLED FLUSH PLUG AND FINGER DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 1999081200913 19990812 00913 NM 1999 8 12 AALA990824 1 19990425 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1964 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - FOUND TRACK NR 1 IS CORRODED AT STATION 1964. REPAIRED TRACK NR 1 PER ESO 41000, DATED 5-24-00. (M) 2 L 7 3 4F RT A22WE 1999081200914 19990812 00914 NM 1999 8 12 AALA990918 1 19990617 A 5330 SKIN BOEING 727 727227 1384078 NM BS 227.8 LIGHTNING STRIKE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - LIGHTNING STRIKE STATION 227.8 JUST BELOW STRINGER 17R. CUT OUT DAMAGE. INSTALLED DOUBLER PER SRM 53-30-3 FIG 13 A WITH PERMANENT FASTENERS. (M) 2 L 7 3 4F A3WE 1999081200915 19990812 00915 NM 1999 8 12 TSAA9953262 1 19990617 A 5330 SKIN BOEING 737 7372M6C 1384708 NM BS 774 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND .875 INCH SKIN CRACK NOTED AT BS 774 STRINGER 17L. HFEC CONFIRMED ENDS OF CRACK. REPAIRED CRACK PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999081200916 19990812 00916 NM 1999 8 12 TSAA9933257 1 19990609 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED BATTERY PACK FOR NR 1 POSITION FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999081200917 19990812 00917 NM 1999 8 12 TSAA9933258 1 19990611 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED BATTERY PACK FOR NR 4 POSITION FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999081200918 19990812 00918 NM 1999 8 12 TSAA9933259 1 19990612 A 3350 9221009 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED FORWARD SERVICE, FORWARD PASSENGER, RIGHT OVERWING, AND LEFT OVERWING SLIDE LIGHT BATTERY PACKS DUE TO INOP. O PS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999081200919 19990812 00919 NM 1999 8 12 TSAA9933260 1 19990614 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 5 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999081200920 19990812 00920 NM 1999 8 12 TSAA9933261 1 19990617 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999081200921 19990812 00921 NM 1999 8 12 TSAA9933263 1 19990618 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 2 EMERGENCY AISLE LIGH TASSY BATTERY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999081200922 19990812 00922 NM 1999 8 12 TSAA9933264 1 19990620 A 3350 6013211 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED AFT DOOR EMERGENCY SLIDE LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999081200923 19990812 00923 NM 1999 8 12 USAA990448 1 19990511 A 5240 6552873159 SKIN BOEING 737 7373B7 1384580 NM L2 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 42282 22956 PIT - DURING TURN AROUND MAINTENANCE, FOUND 2 INCH BY 2 INCH CRACK, TRIANGLE OF METAL SKIN MISSING AT TOP OF LOWER HINGE CUTOUT FORWARD EDGE L2 DOOR. INSTALLED FILLER AND DOUBLER AND BLIND FASTENERS PER EA 64602. (M) 2 L 7 2 4F RT A16WE 1999081200924 19990812 00924 NM 1999 8 12 USAA990561 1 19990610 A 5321 FLOOR BOEING 737 737301 1384611 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND 1.5 INCH CRACK AND .400 INCH CRACK JUST AFT OF STATION 663.75 BL 32 IN PRESSURE FLOOR PANE L. INSTALLED DOUBLER, FILLER AND ANGLE STIFFENER PER EA 64667. (M) 2 L 7 2 4F RT A16WE 1999081200925 19990812 00925 NM 1999 8 12 USAA990559 1 19990610 A 5320 693535214 CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND .5 INCH CRACK IN TIE CLIP AT STATION 727A FRAME TO STRINGER 6R. DEFECTIVE PART REPLACED W ITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999081200926 19990812 00926 EA 1999 8 12 JBXA9900097 1 19990804 A 7830 TR UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE LT ENGINE MALFUNCTIONED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 571ML 7209 THE LEFT THRUST REVERSER UNLOCK LIGHT ILLUMITNATED AT FL280. NO ADVERSE YAW. COMPLETED QHR AND LANDED AT ATL. ASSIGNE D TO MEL 78-30-1. CONTIUNED FLIGHT AND REMOVED DMI PER RIGGING OF LT T/R STOW MICROSWITCH AND THROTTLE MICROSWITCH ALON G WITH RIG CHECK OF BALLSCREW ACTUATOR AND PDU SYSTEM IAW CRJ AMM 78-32-01-330-801, 78-30-00-720-804, AND 78-30-00-6-830 -802. SYSTEMS OPS CK GOOD ON GROUND RUN. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200927 19990812 00927 NE 1999 8 12 JBXA9900096 2 19990802 A 7261 OIL SYS CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE RT ENGINE OVER FILLED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 571ML 7209 ON CLIMB, RIGHT OIL PRESSURE STARTED TO DROP OUT, OIL TEMP CLIMBED TO 160. DRAINED EXCESSIVE OIL FROM OIL TANK AND ACCE SSORY GEAR BOX, GROUND RAN NR 2 ENGINE AT HIGH POWER SETTINGS. OIL TEMP AND PRESSURE WITHIN LIMITS IAW 79-30-00. REF N ON-ROUTNIE NR 05393 FOR WORK PERFORMED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200928 19990812 00928 WP 1999 8 12 9902989610 1 19990801 A 3620 TEMP LIGHT DOUG DC9 DC932 3022066 WP TAIL COMPT ILLUMINATED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 610NW 47432 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND THE FLIGHT WAS RETURN ED TO BNA. AIRCRAFT LANDED WITHOUT INCIDENT. PROBLEM COULD NOT BE DUPLICATED ON GROUND. NO LEAKS WERE FOUND IN TAIL A REA. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999081200929 19990812 00929 WP 1999 8 12 9902999920 1 19990730 A 3231 FASTENERS DOUG DC9 DC932 3022066 WP RT GEAR DOOR LOOSE A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 942N 47459 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW RECYCLED GEAR WITH SAME RESULTS. EMERGENCY WAS DEC LARED AND ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED LO OSE FASTENERS ON RIGHT GEAR DOOR ROLLER ASSEMBLY. ALSO, INSTALLED NEW SKID PLATE ON GEAR DOOR DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999081200930 19990812 00930 WP 1999 8 12 9903009612 1 19990728 A 3230 LINK DOUG DC9 DC932 3022066 WP NLG OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 612NW 47436 NO GREEN OR RED NOSE GEAR LIGHT ON WHEN GEAR WAS EXTENDED FOR LANDING. CREW VISUALLY INSPECTED GEAR AND CONFIRMED NOSE GEAR TO BE IN UP POSITION. YELLOW EMERGENCY WAS DECLARED AND EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED. GEAR E XTENDED NORMALLY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED SIDE CLEARANCE OF AFT MOUNT POINT OVERCENTE R LINK. ALSO, REPLACED BOTH MAIN GEAR DOORS DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK NORMAL. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F A6WE 1999081200931 19990812 00931 WP 1999 8 12 9903011232 1 19990730 A 3230 RETRACT MECH DOUG DC10 DC1030 3023501 WP LANDING GEAR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 232NW 46961 AFTER TAKEOFF FROM HNL, UNABLE TO RAISE GEAR HANDLE, MOVEMENT OF .25 INCH ONLY. FOLLOWED COCKPIT OPERATING MANUAL PROCE DURE. FLIGHT RETURNED TO HNL AND LANDED WITHOUT INCIDENT. BLED HYDRAULIC SYSTEM AND EXERCISED GROUND SENSING ROD. OPE RATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999081200932 19990812 00932 WP 1999 8 12 9903021145 1 19990630 A 5720 DOUBLER DOUG DC10 DC1040 3023508 WP WS 593-629.3 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CRACK ON RIGHT WING FIXED LEADING EDGE AT XORS 593 TO 629.3. REPAIRED PER EA 11-168615. 2 L 7 3 4F A22WE 1999081200933 19990812 00933 WP 1999 8 12 9903031145 1 19990613 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1509-1531 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING M CHECK, FOUND CRACK AND CORROSION ON FUSELAGE SKIN AT FS 1509 - 1531, LONGERON 47L TO 48R. REPAIRED PER EA 11-1 68288. 2 L 7 3 4F A22WE 1999081200934 19990812 00934 EU 1999 8 12 99FDEA00309 1 19990803 A 2170 18084934 COALESCER BAG AIRBUS 300 A300F4605R 3930327 EU CABIN CONTAMINATED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 652FE 735 99-189 - AFTER T/O, A BURN SMELL BECAME PRESENT AND STAYED FOR 1 MIN WITH VENTS OPEN. REMOVED AND REPLACED WATER SEPARA TOR (COALESCOR BAG) IN BOTH PACKS PER MM 21-51-11-3. RAN ENG AT HI-PWR PER JRH. OPS CK GOOD. OK FOR SERV. PREVIOUS W RITE-UP THAT SAME DAY WAS FOR A BIRD INGESTION IN THE NR 1 ENG. HPC BOROSCOPE E/W PER MM 72-31-00 WITH NO DAMAGE NOTED. 2 L 7 2 4F RT A35EU 1999081200935 19990812 00935 NM 1999 8 12 99FDEA00311 1 19990804 A 5610 WINDSHIELD BOEING 727 727233 138408A NM RT COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 269FE 21675 99-191 - AFT T/O R1 WINDOW HEAT ARCED TOP RIGHT TO TOP LEFT 2 MIN LATER OUTER WINDSCREEN CRACKED FROM UPPER RIGHT TO LWR LEFT. REMOVED AND REPLACED R1 WIND PER 727 MM 56-11-011, WIND HEAT CONTROL PER 727 MM 30-41-013. SEAL WIND, INSTALL W INDSHIELD WIPER. WINDSHIELD CONTROLLER INSTALLED. OPS CK NORM. 2 L 7 3 4F RT A3WE 1999081200936 19990812 00936 WP 1999 8 12 99FDEA00312 1 19990804 A 5711 SPAR DOUG DC10 DC10* WP RT WING GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RIGHT WING AFT SPAR AFT TANG HAS A GOUGE ACROSS THE FLANGE AT XROS 414. COMPLIED WITH EA 8-5710-42395 RT REAR SPAR DEVI ATION FROM EO 8-5710-7-30041. 2 L 7 3 4F A22WE 1999081200937 19990812 00937 NM 1999 8 12 99FDEA00313 1 19990804 A 2613 OVERHEAT LIGHT BOEING 727 727227 1384078 NM LWR AFT BODY ILLUMINAATED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 486FE 21489 99-192 - AT CRUISE, LWR AFT BODY OVERHEAT LIGHT ILLUMINATED. RED TAB PROC INITIATED. RETARDING NR 1 THROTTLE EXITING L IGHT. NR 1 BLD AND LEFT PACK OFF REMAINDER OF FLT. COULD NOT DUPLICATE PROBLEM FOUND NOTHING WRONG. 2 L 7 3 4F A3WE 1999081200938 19990812 00938 WP 1999 8 12 ABXA9900620 1 19990803 A 5311 5911448505 FRAME DOUG DOUG DC9 DC941 302207N WP BS 256 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION 256 AND LONGERON 30 CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999081200939 19990812 00939 WP 1999 8 12 ABXA9900621 1 19990803 A 5312 991224381 BULKHEAD WEB DOUG DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND LEFT FORWARD PYLON BULKHEAD FORWARD SIDE LOWER WEB CRACKED. REPAIRED WEB IAW ABX REA D953-32580MR . 2 L 7 2 4F A6WE 1999081200940 19990812 00940 WP 1999 8 12 ABXA9900622 1 19990626 A 5320 37584951N FITTING DOUG DOUG DC8 DC863 302198A WP BS 1240 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FRAME ATTACH FITTING CRACKED AT STATION 1240 AND LONGERON 35 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999081200941 19990812 00941 WP 1999 8 12 ABXA9900623 1 19990625 A 5320 375582 FITTING DOUG DOUG DC8 DC863 302198A WP BS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 CRACKED FITTING IN TORQUE BOX STATION 1180 AND LONGERON 28 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND 51-1-11. 2 L 7 4 4F 4A25 1999081200942 19990812 00942 WP 1999 8 12 ABXA9900624 1 19990624 A 5320 43196205 FITTING DOUG DOUG DC8 DC863 302198A WP BS 300 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 TORQUE BOX BATHTUB FITTING CORRODED AT STATION 300 AND LONGERONS 34 TO 35 RIGHT. REPAIRED IAW DC8 SRM 51-1-0. 2 L 7 4 4F 4A25 1999081200943 19990812 00943 WP 1999 8 12 ABXA9900625 1 19990714 A 5320 49568801 FITTING DOUG DOUG DC9 DC941 302207N WP BS 69.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND NOSE WHEEL WELL PRESSURE PANEL LOWER 2 INBOARD FITTINGS CRACKED AT STATION 69.550, LEFT AND RIGHT BL 12.0. REPLACED FITTINGS AT STATION 69.550 IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999081200944 19990812 00944 WP 1999 8 12 ABXA9900626 1 19990714 A 5313 27779223 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK, FOUND LONGERON 4 LEFT CRACKED AT STATION 160. REPLACED LONGERON 4 LEFT IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999081200945 19990812 00945 NE 1999 8 12 99ZZZX2831 2 19990626 A 7200 ENGINE BOEING 727 7272Q6 138407V NM PWA JT8 JT8D17 52049 NE NR 2 FAILED A C8GA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 1279E 46332 36607 21971 657667 KDAY/KJAX - FLT 326 - IN CRUISE, THE NR 2 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED ON FORWARD CONTROL PANEL. A CORRESP ONDING DROP IN OIL PRESSURE WAS NOTED. OIL QUANTITY INDICATION WAS NORMAL. PRESSURE CONTINUED TO DROP. FLIGHT CREW SE CURED THE NR 2 ENGINE. THE AIRCRAFT CONTINUED TO KJAX AND LANDED WITHOUT FURTHER INCIDENT. THE NR 2 ENGINE HAS BEEN CH ANGED AND SENT FOR ANALYSIS. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F 4 F RT A3WE E2EA 1999081200946 19990812 00946 NM 1999 8 12 AALA991036 1 19990714 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324AA 22325 LAX - DURING OVERNIGHT MAINTENANCE, BOTH OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. RESEATED CONNECTOR TO BATTERY PACK MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999081200947 19990812 00947 NM 1999 8 12 AALA991020 1 19990709 A 3350 S417T5003 LIGHT BOEING 767 767323 1385205 NM L2 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39356 24037 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L2 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999081200948 19990812 00948 NM 1999 8 12 AALA991041 1 19990714 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 327AA 22327 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON THE RIGHT SIDE OF THE MID-GALLEY INOPERATIVE. REPAIRED WIRI NG BEHIND THE EMERGENCY EXIT LIGHT ON THE RIGHT SIDE OF THE MID-GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999081200949 19990812 00949 NM 1999 8 12 AALA991029 1 19990713 A 3350 SWITCH BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 381AN 25450 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS COULD NOT BE TURNED OFF USING THE SWITCH AT THE FORWARD F LIGHT ATTENDANT'S STATION. REPLACED FORWARD FLIGHT ATTENDANT EMERGENCY EXIT SEAT LIGHT SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999081200950 19990812 00950 WP 1999 8 12 AALA991027 1 19990712 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1355 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 586AA 53249 TUL - STA 1355 LONGERON 19L IS GOUGED/WORN. REPAIRED LONGERON 19L AT STA 1355 PER ESO 80559 DATED 7-1-99. TST: 23,816 .18 HOURS. CYCLES: 12,127. (X) 2 L 7 2 4F A6WE 1999081200951 19990812 00951 WP 1999 8 12 AALA991022 1 19990630 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 218 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 586AA 53249 TUL - BOLT BROKEN IN G-2 AFT INBOARD HOLD-DOWN FITTING FOR GALLEY. REPLACED UPPER AND LOWER HOLD-DOWN CASTINGS FOR GALL EY AND ACCOMPLISHED SUB-FLOOR DOUBLER PER SRM 53-01 FIG 4 REV 133 NOTE C AARD 53-00-00-02. TST: 23,816.18 HOURS. CY CLES: 12,127. (X) 2 L 7 2 4F A6WE 1999081200952 19990812 00952 WP 1999 8 12 AALA991025 1 19990712 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 586AA 53249 TUL - STA 1418, LONGERON NR 2 RIGHT, CRACKED ON AFT OUTBOARD SIDE, LOCATED AFT SIDE OF BELT FRAME, STA 1418. INSTALLED LONGERON REPAIR PER AARD 53-30-00-2. TST: 23,816.18 HOURS. CYCLES: 12,127. (X) 2 L 7 2 4F A6WE 1999081200953 19990812 00953 WP 1999 8 12 AALA991026 1 19990712 A 5311 FRAME DOUG DC9 DC982 3022082 WP BW 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 586AA 53249 TUL - STA 1418, BELT FRAME CRACKED AT NR 2 LONGERON, RIGHT ATTACHMENT. INSTALLED BELT FRAME REPAIR PER SRM 53-03. TS T: 23,816.18 HOURS. CYCLES: 12,127. (X) 2 L 7 2 4F A6WE 1999081200954 19990812 00954 NM 1999 8 12 AALA994011 1 19990625 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 391AA 27451 AFW - FLOORBEAM STA 347 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION AND REFINISHED THE SURFACE PER SR M. TST: 20,342.15 HOURS. CYCLES: 3,174. (X) 2 L 7 2 4F RT A1NM 1999081200955 19990812 00955 NM 1999 8 12 AALA994120 1 19990706 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 764 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 358AA 24039 AFW - FLOORBEAM AT STA 764 HAS CORROSION REMOVAL ON UPPER SURFACE. REMAINING IS BEYOND SRM LIMITS. BLENDED OUT CORROSIO N AND REFINISHED THE SURFACE PER SRM. THE BLEND REPAIR IS SATISFACTORY FOR CONTINUED SER SERVICE AS NOTED CONDITION. T ST: 49,449 HOURS. CYCLES: 5,146. (X) 2 L 7 2 4F RT A1NM 1999081200956 19990812 00956 NM 1999 8 12 AALA994116 1 19990706 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 358AA 24039 AFW - FLOORBEAM AT STA 347 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION AND REFINISHED SURFACE PER SRM . FILLED BLENDED AREA WITH BM55-95. THE BLEND REPAIR IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED. TST: 49,449 H OURS. CYCLES: 5,146. (X) 2 L 7 2 4F RT A1NM 1999081200957 19990812 00957 NM 1999 8 12 AALA994115 1 19990706 A 5347 SEAT TRACK BOEING 767 767323 1385205 NM BS 770 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 358AA 24039 AFW - SEAT TRACK AT STA 770 AND LBL 11 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION AND REFINISHED SUR FACE PER SRM. THE BLENDED REPAIR IS SATISFACTORY FOR CONTINUED SERVICE AS NOTED CONDITION. TST: 49,949 HOURS. CYCLES : 8,146. (X) 2 L 7 2 4F RT A1NM 1999081200958 19990812 00958 NM 1999 8 12 AALA994113 1 19990625 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 391AA 27451 AFW - FLOORBEAM AT STA 764 HAS CORROSION. BLENDED OUT CORROSION AND REFINISHED THE SURFACE PER SRM. BLENDED REPAIR IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION. TST: 20,342.15. CYCLES: 3,174. (X) 2 L 7 2 4F RT A1NM 1999081200959 19990812 00959 WP 1999 8 12 GTIA9900946 1 19990701 A 2560 SLIDE DOUG DC9 DC931 3022065 WP R1 DOOR DETACHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 132NK 47202 DTW - FLT 546 - SLIDE PACK FELL OFF GALLEY SERVICE DOOR (TWICE) R1. RE-INSTALLED ESCAPE SLIDE ON R1 DOOR IAW DC-9 MM 25 -61. (X) 2 L 7 2 4F A6WE 1999081200960 19990812 00960 WP 1999 8 12 GTIA9900944 1 19990602 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP COCKPIT DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FLT 951A - COCKPIT OVERHEAD EMERGENCY LIGHT OUT. TROUBLESHOT SYSTEM, FOUND EMERGENCY BATTERY PACK WITH DEAD BATT ERIES. REPLACED BATTERIES ON JOB CARD. LIGHTS WORK CARD. (X) 2 L 7 2 4F A6WE 1999081200961 19990812 00961 WP 1999 8 12 GTIA9900942 1 19990622 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 8 LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 17535 47111 FORWARD ONE-THIRD OF EMERGENCY FLOOR ESCAPE PATH LIGHTS INOPERATIVE. FOUND WIRE OUT OF FLOOR ROW EIGHT. RESECURED AS N ECESSARY. OPERATION CHECKS GOOD IAW DC-9 MM 33-50. (X) 2 L 7 2 4F A6WE 1999081200962 19990812 00962 WP 1999 8 12 GTIA9900941 1 19990701 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP ROWS 7-12 DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 15243 47113 CABIN OVERHEAD EMERGENCY LIGHTS ROWS 7 TO 12 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-32 IAW MM CHAPTER 33-53- 0. OPERATION CHECKS GOOD. (X) 2 L 7 2 4F A6WE 1999081200963 19990812 00963 WP 1999 8 12 GTIA9900937 1 19990701 A 3350 20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML NK0184 47326 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES POWER PACK ASSEMBLY. OPERATION CHECKS GOOD. (X) 2 L 7 2 4F A6WE 1999081200964 19990812 00964 WP 1999 8 12 ASAA9980150 1 19990703 A 5210 LINER DOUG DC9 DC983 3022083 WP L1 DOOR LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 947AS 53020 PDX - FLT 601 - AFTER ARRIVAL, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. FOUND DOOR INTERIOR LINER LOOSE AND CAT CHING ON FORWARD FLIGHT ATTENDANT JUMP SEAT. INSTALLED MISSING FASTENER IN DOOR LINER AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999081200965 19990812 00965 WP 1999 8 12 ASAA9980138 1 19990616 A 5610 GUIDE PIN DOUG DC9 DC983 3022083 WP RT COCKPIT OUT OF POSITION A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 972AS 53448 SEA - FLT 417 - AFTER ARRIVAL, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED GUIDE PI N ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999081200966 19990812 00966 WP 1999 8 12 ASAA9980126 1 19990525 A 5210 49182591 MECHANISM DOUG DC9 DC983 3022083 WP L-1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 943AS 53018 PDX - FLT 449 - CREW REPORTED L-1 DOOR IS DIFFICULT TO LATCH CLOSED THROUGH THE LAST QUARTER OF THE DOOR HANDLE TRAVEL. FOUND INTERLOCK ARM HITTING LOCKPIN RETAINER. SHIMMED LOCKPIN RETAINER AND ADJUSTED INTERLOCK ARM; DOOR OPERATED NORMA LLY. (X) 2 L 7 2 4F RT A6WE 1999081200967 19990812 00967 WP 1999 8 12 ASAA9980134 1 19990607 A 5753 5912149512 HINGE DOUG DC9 DC983 3022083 WP RT TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OAK - DURING 30K CHECK, DAMAGE WAS FOUND ON RT WING OUTBOARD FLAP INBOARD HINGE INBOARD UPPER ATTACH LUB. REPAIRED IAW ASA EA 5740-01168. (X) 2 L 7 2 4F RT A6WE 1999081200968 19990812 00968 WP 1999 8 12 ASAA9980132 1 19990604 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS DIFFICULT TO CLOSE. RE-RIGGED THE L1 DOOR VERTICAL ADJUSTMENT IAW DC9 M M AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999081200969 19990812 00969 WP 1999 8 12 ASAA9980141 1 19990619 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC983 3022083 WP ROWS 18-23 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 23 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999081200970 19990812 00970 WP 1999 8 12 ASAA9980139 1 19990619 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT ABOVE THE AFT FLIGHT ATTENDANT SEAT FLICKERS ON AND OFF WIT H ELECTRICAL POWER OFF. REPLACED THE BATTERIRES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999081200971 19990812 00971 WP 1999 8 12 ASAA9980140 1 19990619 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROWS 29-32 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 29 TO 32 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999081200972 19990812 00972 WP 1999 8 12 ASAA9980137 1 19990615 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999081200973 19990812 00973 WP 1999 8 12 ASAA9980116 1 19990520 A 3350 014597101 BATTERIES MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 937AS 49364 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999081200974 19990812 00974 NM 1999 8 12 ASAA9940132 1 19990617 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 PDX - DURING MAINTENANCE CHECK, THE FORWARD 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIR ING/LIGHTS AND THE LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999081200975 19990812 00975 NM 1999 8 12 ASAA9940122 1 19990609 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT SEVERAL LOCATIONS. RELA MPED 2 EACH LIGHTS AND REPAIRED WIRING TO FLOOR TRACK LIGHTS, LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999081200976 19990812 00976 NM 1999 8 12 ASAA9940120 1 19990528 A 3350 BPS73 BATTERY CHARGER BOEING 737 7374Q8 NM ROWS 13 & 14 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 13 AND 14. R EPLACED BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999081200977 19990812 00977 NM 1999 8 12 ASAA9910211 1 19990630 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, TWO EACH FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BAT TERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999081200978 19990812 00978 NM 1999 8 12 ASAA9910210 1 19990629 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 7372Q8C 138448S NM ROW 17 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 741AS 21959 ANC - PRIOR TO FLT 147, TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. CHECKED AND RELEASED PER MEL 33-1 9A. SUBSEQUENTLY REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999081200979 19990812 00979 NM 1999 8 12 ASAA9910209 1 19990629 A 3397 WIRE BOEING 737 737290C 138448V NM ROW 12 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, 2 EACH EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 12. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999081200980 19990812 00980 NM 1999 8 12 ASAA9910136 1 19990626 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 7372X6C 1384552 NM ROWS 14 & 15 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 JNU - PRIOR TO FLT 61, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED AT ROWS 14 AND 15. REPLACED BATTERY PACK AND L IGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999081200981 19990812 00981 NM 1999 8 12 ASAA9910135 1 19990625 A 3350 873203041 TRANSMITTER INTVLV BOEING 737 7372X6C 1384552 NM R1 DOOR INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 SEA - PRIOR TO FLT 65, THE R1 AND L2 DOOR EMERGENCY LIGHTS WOULD NOT TEST. REPLACED R1 DOOR TRANSMITTER AND L2 DOOR REC EIVER, LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR 99ZZZX2832. (X) 2 L 7 2 4F RT A16WE 1999081200982 19990812 00982 NM 1999 8 12 99ZZZX2832 1 19990625 A 3350 8731002142 RECEIVER INTVLV BOEING 737 7372X6C 1384552 NM L2 DOOR INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 SEA - PRIOR TO FLT 65, THE R1 AND L2 DOOR EMERGENCY LIGHTS WOULD NOT TEST. REPLACED R1 DOOR TRANSMITTER AND L2 DOOR REC EIVER, LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR ASAA9910135. 2 L 7 2 4F RT A16WE 1999081200983 19990812 00983 NM 1999 8 12 ASAA9910130 1 19990523 A 3350 883200312 RECEIVER GRIMES BOEING 737 7372X6C 1384552 NM ROWS 14 AND 20 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT LIGHT RECEIVERS WOULD NOT TEST PROPERLY. REPLACED RECEIVERS AT R OWS 14 AND 20, AND BATTERY AT ROW 18 AND AT THE R-1 DOOR. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. REF: OPER CNTR L NR 99ZZZX2833. (X) 2 L 7 2 4F RT A16WE 1999081200984 19990812 00984 NM 1999 8 12 99ZZZX2833 1 19990523 A 3350 6104781 BATTERY GRIMES BOEING 737 7372X6C 1384552 NM ROW 18 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT LIGHT RECEIVERS WOULD NOT TEST PROPERLY. REPLACED RECEIVERS AT R OWS 14 AND 20, AND BATTERY AT ROW 18 AND AT THE R-1 DOOR. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. REF: OPER CNTR L NR ASAA9910130. 2 L 7 2 4F RT A16WE 1999081200985 19990812 00985 NM 1999 8 12 ASAA9910131 1 19990527 A 3397 WIRE BOEING 737 737290C 138448V NM ROW 12 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND 2 EACH EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROW 12. REPAIRED WIRING A ND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999081200986 19990812 00986 NM 1999 8 12 ASAA9910132 1 19990527 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK THE L1 DOOR INTERIOR EMERGENCY EXIT LIGHT ABOVE DOOR WAS FOUND INOPERATIVE. REPLACED BAT TERY PACK AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999081200987 19990812 00987 NM 1999 8 12 ASAA9910133 1 19990601 A 3350 883200313 RECEIVER INTVLV BOEING 737 737290C 138448V NM ROW 11 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 11 WERE FOUND INOPERATIVE. REPLACED RECEIV ER AND BATTERY AND LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR 99ZZZX2834. (X) 2 L 7 2 4F A16WE 1999081200988 19990812 00988 NM 1999 8 12 99ZZZX2834 1 19990601 A 3350 6104781 BATTERY GRIMES BOEING 737 737290C 138448V NM ROW 11 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 11 WERE FOUND INOPERATIVE. REPLACED RECEIV ER AND BATTERY AND LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR ASAA9910133. 2 L 7 2 4F A16WE 1999081200989 19990812 00989 NM 1999 8 12 ASAA9910134 1 19990602 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 741AS 21959 ANC - FLT 43 - PRIOR TO FLIGHT, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED WHEN THE LIGHT SWITCH WA S IN THE 'OFF' POSITION. REPLACED BATTERY PACK ON PALLET 7-4, AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999081200990 19990812 00990 EU 1999 8 12 SIMA991961 1 19990715 A 3350 9HB000593312 LIGHT SAAB SF340 340B 7860101 EU ROW 8BC MISSING A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 264AE 340B264 SBP - EMERGENCY LIGHT AT SEAT 8BC IS MISSING. REPLACED EMERGENCY LIGHT PANEL ASSEMBLY. OPERATIONAL CHECKED GOOD. (X) 2 L 7 2 4T RT A52EU 1999081200991 19990812 00991 EU 1999 8 12 SIMA991942 1 19990713 A 3310 2LA00507500 LIGHT SAAB SF340 340B 7860101 EU RT COCKPIT FAILED A SIMA A UNSCHED LANDING A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 347SB 340B347 ERI - FLT 9726 - WHEN FIRST OFFICER ADJUSTED THE OVERHEAD MAP READING LIGHT ON RIGHT PEDESTAL, FLAMES AND SMOKE CAME OUT OF THE LIGHT ASSEMBLY. REMOVED AND REPLACED RIGHT HAND OVERHEAD MAP LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999081200992 19990812 00992 EU 1999 8 12 RAIA990718 1 19990714 A 7922 L8523427 VERNITHERM BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 341TE 950 STL - FLT 7442 - COULD NOT MAINTAIN NORMAL POWER SETTINGS WITHOUT EXCEEDING OIL TEMPERATURE ON LEFT ENGINE. MAINTENANCE REPLACED OIL COOLER VERNITHERM ON LEFT ENGINE. (X) 2 L 7 2 4T RT A56EU 1999081200993 19990812 00993 EU 1999 8 12 RAIA990717 1 19990703 A 7331 TNAS1024L1182 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 432AM 883 STL - FLT 7512 - RIGHT FUEL FLOW INOPERABLE. MAINTENANCE REPLACED RIGHT ENGINE FUEL FLOW TRANSMITTER. (X) 2 L 7 2 4T RT A56EU 1999081200994 19990812 00994 EU 1999 8 12 RAIA990716 1 19990702 A 7331 TNAS1024L1182 TRANSMITER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 422AM 856 CMI - FLT 7433 - LEFT FUEL FLOW METER FAILED. MAINTENANCE REPLACED LEFT ENGINE FUEL FLOW TRANSMITTER. (X) 2 L 7 2 4T RT A56EU 1999081200995 19990812 00995 EU 1999 8 12 RAIA990715 1 19990713 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 433AM 885 STL - FLT 7086 - RIGHT ENGINE FIRE DETECT LIGHT ILLUMINATED WHEN POWER LEVERS ARE ADVANCED. (X) 2 L 7 2 4T RT A56EU 1999081200996 19990812 00996 EU 1999 8 12 RAIA990714 1 19990711 A 2910 1379305A77 LINE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 03 426AM 874 COU - FLT 7030 - LEFT HYDRAULIC PUMP FAILED IN CRUISE, THEN RIGHT HYDRAULIC PUMP FAILED ON SHORT FINAL. MAINTENANCE REP LACED HYDRAULIC LINE FOR LEFT ENGINE HYDRAULIC PUMP. (X) 2 L 7 2 4T RT A56EU 1999081200997 19990812 00997 WP 1999 8 12 RAIA990649 2 19990630 A 7320 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CE 03 875JX 875 66334 BMI - FLT 7313 - RIGHT ENGINE EGT FLUX BETWEEN 700 AND 900 DEGREES. MAINTENANCE REPLACED FUEL BYPASS VALVE ON RIGHT ENG INE. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1999081200998 19990812 00998 WP 1999 8 12 RAIA990648 2 19990627 A 7320 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 428AM 877 66291 BMI - FLT 7325 - LEFT ENGINE BYPASSING FUEL. MAINTENANCE REPLACED LEFT ENGINE FUEL BYPASS VALVE. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1999081200999 19990812 00999 NM 1999 8 12 P2EA99217 1 19990630 A 2410 699647C CSD BOEING 737 737297 1384480 NM NR 1 FAILED A P2EA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 5WM 2187 22629 MCI - FLT 406 - DURING FLIGHT, THE NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED INTERMITTENTLY; TEMPERATURE READS APPROXI MATELY 130 DEGREES, AND APPROXIMATELY 40 DEGREES HIGHER THAN NR 2 ENGINE. AIRCRAFT RETURNED TO MCI WITH NO INCIDENT. R EPLACED NR 1 CSD PER MM 24-11-11, NR 1 CSD OIL COOLER PER MM 24-11-21, AND NR 1 CSD OIL COOLER FILTER PER MM 24-11-31. ( X) 2 L 7 2 4F A16WE 1999081201000 19990812 01000 NM 1999 8 12 P2EA99219 1 19990719 A 2910 BACH8A06NN0263T HYD LINE BOEING 737 737247 138448D NM NLG FAILED A P2EA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 204AU 19603 FLT 707 - PIT - SHORTLY AFTER TAKEOFF, AIRCRAFT EXPERIENCED 'A' SYSTEM HYDRAULIC SYSTEM LOSS. LANDING GEAR WAS MANUALLY EXTENDED AND AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. REPLACED NOSE LANDING GEAR ACTUATOR RETRACT LIE WITH TEMPORAR Y LINE. TEMPORARY LINE INSTALLED. INSTALLED HYDRAULIC LINE ON NOSE GEAR EXTENSION/RETRACTION ACTUATOR IAW MM 20-10-51. (M) 2 L 7 2 4F A16WE 1999081201001 19990812 01001 NM 1999 8 12 P2EA99220 1 19990720 A 5730 65454877 DOOR BOEING 737 737281 138448P NM RT WING MISSING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 NSP - FLT 707 - THIS IS A SUPPLEMENTAL/CLOSING ACTION FOR MRR 99220. ON WALK-AROUND INSPECTION AFTER FLIGHT MAINTENANCE , CREW DISCOVERED THE CENTER BOOST PUMP DOOR P/N 65-45487-7 MISSING. DEFERRED PER CDL 57-30-4. REQUESTED PANEL. REF: DEFERRED ITEM C219980 BOOST PUMP PANEL MISSING. INSTALLED BOOST PUMP COVER PANEL MM 57-30-11. THIS CLEARS DEFERRED IT EM C 219980. (X) 2 L 7 2 4F A16WE 1999081201002 19990812 01002 WP 1999 8 12 ORJA99214 1 19990625 A 2560 D29982121 SLIDE DOUG DC9 DC983 3022083 WP GALLEY DOOR DETACHED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 LANYARD ON RIGHT GALLEY DOOR CAME OFF. TOO TIGHT FOR FLIGHT CREW TO RE-INSTALL. RE-INSTALLED DOOR SLIDE AND OPS CHECKE D DOOR OPERATION. DOOR OPS CHECKED NORMAL. AIRCRAFT IS OK FOR SERVICE. (X) 2 L 7 2 4F RT A6WE 1999081201003 19990812 01003 WP 1999 8 12 ORJA99225 1 19990704 A 2560 D29982107 SLIDE DOUG DC9 DC983 3022083 WP GALLEY DOOR DETACHED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 836RA 53046 SEA - R1 DOOR ESCAPE SLIDE FELL OUT OF DOOR. RE-SECURED FORWARD GALLEY DOOR SLIDE AND COVER SLIDE CHECKS GOOD. (X) 2 L 7 2 4F RT A6WE 1999081400001 19990814 00001 EU 1999 8 14 AALA990537 1 19990416 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1468A 11501 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLA CED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A20EU 1999081400003 19990814 00003 EU 1999 8 14 99ZZZX2836 1 19990715 A 2435 150SG122Q START/GENERATOR SNIAS 350 AS350B2 8680813 EU ENGINE FAILED A L A HCMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 13 992BH 437 52687 2889 DURING A TOUR FLIGHT, PILOT REPORTED A TOTAL ELECTRICAL FAILURE. PILOT PROCEEDED TO LAND AT THE COMPANY HELIPORT WITHOU T INCIDENT. FOUND ALL CAUTION LIGHTS, RADIOS, GAUGES, AND AIR CONDITIONING OPERATED NORMALLY. WHEN DEPRESSING THE STAR T OR 'CRANK' SWITCHES FOUND STARTER WOULD NOT ROTATE. REMOVED AND INSTALLED SERVICEABLE BATTERY AND STARTER/GENERATOR A IRCRAFT WAS OPS CHECKED AND RETURNED TO SERVICE. UPON INSPECTION OF THE STARTER/GENERATOR BRUSHES, FOUND 2 OF THE 4 INSI DE BRUSHES WERE WORN. 1 G 7 1 3U H9EU 1999081400007 19990814 00007 SW 1999 8 14 99ZZZX2840 1 19990715 A 6410 212010750105 BLADE 212011701101 BELL 412 412 1182202 SW TAIL ROTOR CRACKED G A UNSCHED LANDING D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 03 3893S 33022 TAIL ROTOR BLADE FAILED IN-FLIGHT. APPROXIMATELY 14 INCHES OF THE OUTBOARD END OF ONE TAIL ROTOR BLADE SEPARATED CAUSIN G AN IMBALANCE CONDITION WHICH CAUSED THE TAIL ROTOR ASSEMBLY AND TAIL ROTOR GEARBOX TO SEPARATE THE AIRCRAFT. ENGINEER ING EVALUATION FOF THE FAILED BLADE REVEALED THE FAILURE ORIGINATED FROM A STRESS FRACTURE THAT WAS CAUSED BY CORROSION IN THE INSIDE OF THE BLADE SKIN. 1 G 7 2 4U H4SW 1999081400061 19990814 00061 NM 1999 8 14 99UAL900388 1 19990725 A 2421 IDG SUNDSTRAND 729825 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 567UA 770 26673 RIGHT GENERATOR FAILED. RETURNED TO DEN. *S/D* REPLACED RIGHT INTEGRATED DRIVE GENERATOR (P/N 729825 DASH 770), AIR-O IL HEAT EXCHANGER AND FUEL-OIL COOLER. RIGHT INTEGRATED DRIVE GENERATOR DIFFERENTIAL FAILED DUE TO CONTAMINATION. UNIT WAS CONTAMINATED WITH MINERAL OIL. 2 L 7 2 4F 4 F RT A2NM E17NE 1999081400062 19990814 00062 NM 1999 8 14 99UAL900389 1 19990724 A 5230 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 565UA 26669 UPON ARRIVAL AT GATE, UNCOMMANDED FWD CARGO DOOR OPENING WHEN GROUND POWER BUS ENERGIZED. *S/D* FWD CARGO DOOR CONTRO L SWITCH WAS FOUND STUCK IN OPEN POSITION. SWITCH WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999081400063 19990814 00063 NE 1999 8 14 99UAL900390 2 19990723 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WING FAILED A UALA A J UNSCHED LANDING DUMP FUEL Y ENGINE STOPPAGE CL CLIMB 1 WP 29 657UA 27112 ENGINE FAILURE ON TAKEOFF. DUMPED FUEL. AMBER ALERT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999081400064 19990814 00064 NM 1999 8 14 99UAL900391 1 19990724 A 2750 RETRACT MECH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS MALFUNCTIONED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 608UA 21869 TE FLAP ASSY EICAS MSG AND TE FLAP LIGHT ILLUMINATED. FLAPS STOPPED AT ONE DEGREE. TOWER CALLED EQUIPMENT. LANDING UN EVENTFUL. 2 L 7 2 4F 4 F RT A1NM E3NE 1999081400065 19990814 00065 NM 1999 8 14 99UAL900392 1 19990722 A 2822 50086 RELAY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE EE BAY FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7251U 21398 AFTER TAKEOFF, ALL BOOST PUMPS FOR NR 2 FUEL TANK FAILED. CIRCUIT BREAKERS POPPED. AFT FLIGHT REPORTED FUEL FUMES. RE TURNED TO DEN. *S/D* MOST LIKELY CAUSE MAY HAVE BEEN A FAULTY APU BUS CIRCUIT BREAKER. PUMPS WERE TRIPPING THEIR BREA KERS WHEN USING APU POWER. PUMPS REPLACED, SPLICES REPLACED AND ELECTRICAL POWER CHECKED. LAST ITEM TO BE REPLACED WA S THE APU CIRCUIT BREAKER. 2 L 7 3 4F 4 F A3WE E2EA 1999081400066 19990814 00066 NM 1999 8 14 99UAL900393 1 19990725 A 2612 195080037510 FIRE LOOP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE DEFECTIVE A UALA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 WP 29 7446U 21900 696578 NR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO STRUT OVERHEAT. RETURNED TO DEN. *S/D* DEFLECTIVE FIRE LOOP AT STUB WING CAUSE D THE STRUT OVERHEAT LIGHT TO ILLUMINATE. AIRCRAFT RETURNED TO SERVICE AFTER REPLACEMENT OF FIRE LOOP AND ENGINE RUN UP VERIFICATION. 2 L 7 3 4F 4 F A3WE E2EA 1999081400067 19990814 00067 NM 1999 8 14 99UAL900394 1 19990723 A 3610 CLAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 7446U 21900 696578 NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. SHUT OFF BLEED AND ANTI-ICE. LIGHT WILL NOT GO OUT. DIVERTED TO CLE. *S/D* TIGHTENED LOOSE CLAMP ON THE 13TH STAGE VALVE AND ONE CLAMP ON THE CHECK VALVE. RAN ALL THREE ENGINES TO TAKEOFF POWE R WITH NO STRUT OVERHEAT INDICATION. 2 L 7 3 4F 4 F A3WE E2EA 1999081400068 19990814 00068 NM 1999 8 14 99UAL900395 1 19990716 A 5531 SPAR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7446U 21900 THE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWA BLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS CUT OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH AN 8110-3 2 L 7 3 4F 4 F A3WE E2EA 1999081400069 19990814 00069 NM 1999 8 14 99UAL900396 1 19990716 A 5712 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE WS 750.95 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7446U 21900 TWO CRACKS WERE DISCOVERED EMANATING FROM TWO FASTENER HOLES OF THE STATION 750.95 RBL 70.5 RIB CHORD UPPER VERTICAL FL ANGE. THE AFFECTED UPPER VERTICAL FLANGE WAS TRIMMED OUT AND A REPAIR WAS INSTALLED PER TIMCO REO-06583, REVISION A. T HIS REPAIR WHICH IS ACCOMPLISHED PER BOEING SERVICE BULLETIN 727-57-0112, REVISION 5, RECEIVED DER 811O-3 APPROVAL AS AN ALTERNATE MEANS OF COMPLIANCE TO AD94-07-08 AND AD90-06-09. 2 L 7 3 4F 4 F A3WE E2EA 1999081400070 19990814 00070 NM 1999 8 14 99UAL900397 1 19990719 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1130 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7451U 21905 CORROSION DAMAGE WAS FOUND ON THE STATION 1130 FLOORBEAM UPPER FLANGE FROM RBL 15 TO 24. THE RESULTING BLENDOUT WENT BE YOND THE ALLOWABLE LIMITS FOR MATERIAL REMOVAL. THE CORROSION DAMAGE WAS REMOVED BY BLENDING AND A REPAIR STRAP INSTALL ED PERTIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999081400071 19990814 00071 NM 1999 8 14 99UAL900398 1 19990726 A 2612 1061096217 FIRE LOOP BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE APU MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 29 977UA 21508 LANDED UNDER AMBER ALERT. EN ROUTE TO MSP, RECEIVED APU FIRE WARNING INDICATION. EXTINGUISHER USED. *S/D* VISUAL INS PECTION OF APU INDICATED NO SIGNS OF FIRE. VISUAL INSPECTION OF WIRING AND LOOPS IN APU COMPARTMENT AND AREA FORWARD OF BULKHEAD SHOWED NO SIGNS OF DAMAGE, CHAFING, OR BREAKS. WIRING TROUBLESHOOTING ISOLATED CAUSE OF FIRE INDICATION TO M7 17 APU TAILPIPE LOOP (AT CONNECTOR D4934, REF WDM 26-12-11). M717 LOOP AND APU FIRE EXTINGUISHER BOTTLE WERE REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. ALSO REFERENCE MRR 99UAL900399. 2 L 7 2 4F 4 F A16WE E2EA 1999081400072 19990814 00072 NM 1999 8 14 99UAL900399 1 19990727 A 2612 1061096217 FIRE LOOP BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE APU MALFUNCTIONED A UALA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 29 977UA 21508 APU FIRE WARNING. *S/D* VISUAL INSPECTION OF APU INDICATED NO SIGNS OF FIRE. VISUAL INSPECTION OF WIRING AND LOOPS IN APU COMPARTMENT AND AREA FORWARD OF BULKHEAD SHOWED NO SIGNS OF DAMAGE, CHAFING, OR BREAKS. WIRING TROUBLESHOOTING ISO LATED CAUSE OF FIRE INDICATION TO M717 APU TAILPIPE LOOP (AT CONNECTOR D4934, REF WDM 26-12-11). THE M717 LOOP AND APU FIRE EXTINGUISHER BOTTLE WERE REPLACED. REFERENCE MRR 99UAL900398. 2 L 7 2 4F 4 F A16WE E2EA 1999081400073 19990814 00073 NE 1999 8 14 99UAL900400 2 19990427 A 7321 FUEL CONTROL WOODWARD 8063215 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE MALFUNCTIONED A UALA K NONE R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 29 364UA 61 24533 724850 ASYMMETRICAL THRUST PROBLEM. ENGINE NR 1 WOULD NOT PRODUCE THRUST ABOVE 51 PERCENT N1. ATC WAS NOTIFIED OF POSSIBLE PR OBLEM AND FIRE AND RESCUE WAS REQUESTED TO BE ON STANDBY. *S/D* REPLACED THE MAIN ENGINE CONTROL. AIRCRAFT RETURNED T O SERVICE. NO FURTHER ANOMALIES NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999081400074 20001010 00074 NE 2000 10 10 99UAL900401 2 19990727 A 7230 2A1165 BEARING AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE NR 3 FAILED A UALA E ENGINE SHUTDOWN R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 WP 29 802UA 7178 7178 690 V10232 NR 1 ENG IN-FLIGHT SHUTDOWN. CREW REPORTS COMPRESSOR STALL, FOLLOWED BY VIBRATION. RETARDED THROTTLE AND EXPERIENCED A NOTHER COMPRESSOR STALL. *S/D* NR 3 BEARING FAILED, CAUSING SECONDARY DAMAGE TO THE INLET GEARBOX AND HIGH PRESSURE CO MPRESSOR MODULE. INVESTIGATION INDICATES THE FAILURE ORIGINATED IN THE BEARING RACE. THE ENGINE MANUFACTURER CONSIDERS THIS FAILURE AN ISOLATED CASE. HOWEVER, WEAR PATTERNS OF OTHER NR 3 BEARINGS ARE BEING MONITORED THROUGHOUT THE INDUST RY. 2 L 7 2 4F 4 F RT A28NM E40NE 1999081400075 19990814 00075 EU 1999 8 14 99UAL900402 1 19990327 A 5230 HANDLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR OUT OF ADJUST A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 419UA 487 RAMP REPORTED AFT CARGO PIT DOOR HANDLE DIFFICULT TO STOW. FOUND HOUSING ASSY (ITEM 180 IPC 52 31 21 PG3B 0) CRACKED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999081400076 19990814 00076 NM 1999 8 14 99UAL900403 1 19990727 A 2610 W654W89318R FIRE WIRE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE CHAFED A UALA E ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 WP 29 165UA 21658 NR 1 ENGINE 'B' FIRE NEEDLE IN FIRE ZONE: TESTED A NEEDLE AND GOT FAULT LIGHT: SELECTED 'B' LOOP AND NO FIRE WARNING: NO TICED BREATHER TEMP RISING (180): SHUT ENGINE DOWN. THE LWR AFT FIRE LOOP WIRING FOR BOTH A/B SYS CHAFED THROUGH THE IN SULATION. THE CULPRIT WAS FOUND TO BE THE COWLING RIB THAT IS CLOSEST TO THE FWD END OF THE LWR AFT LOOP, RIGHT SIDE AT ABOUT 4 O'CLOCK AND 12 INCHES AFT ON FWD END OF COWLING. THIS RIB, FIRST RIB IN COWL COVER, WAS RUBBING ON WIRING ABOU T 1-2 INCHES FROM THE LOOP CONNECTION. THE WIRE HARNESS WAS REPAIRED USING NEW LUGS AND THE CLAMP WAS REPOSITIONED 180 DEGREES TO CLEAR THE COWLING RIB. THE SYSTEM WAS TESTED AND PASSED. 2 L 7 4 4F 4 F A20WE E20EA 1999081400077 19990814 00077 NM 1999 8 14 99UAL900404 1 19990727 A 5711 SPAR WEB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CENTER WING MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 7268U 21415 DURING ACCOMPLISHMENT OF THE CENTER WING BOX REAR SPAR WEB MODIFICATION AS MANDATED BY AD97-25-15, EIGHTY THREE HOLES WE RE MISDRILLED COMMON TO THE REAR SPAR CENTER WEB ACCESS PLATE AND THE REAR SPAR WEB. OVERSIZED FASTENERS OF THE SAME TY PE WERE INSTALLED. THIS REPAIR WAS APPROVED BY BOEING DER WITH AN 8110-3 AS AN ALTERNATE MEAN OF COMPLIANCE TO AD97-25- 15. 2 L 7 3 4F 4 F A3WE E2EA 1999081400078 19990814 00078 NM 1999 8 14 CALA9900959 1 19990804 A 5230 BEAM BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR AFT CORNER AND EDGE BEAM. THE DOOR AFT CORNER AND EDGE BEAM WERE R EPLACED IAW BOEING DRAWING 143N6618, 143N6621, AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 1999081400079 19990814 00079 NM 1999 8 14 CALA9900960 1 19990804 A 5720 CHORD BOEING 757 757224 1384958 NM WS 730 CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND RT WING/FUSELAGE CHORD CHAFED AT STA 730, WBL 70.5 BY U/C BEAM REAR SPAR. THE CHORD SECTION WAS REPLAC ED IAW BOEING DRAWING 149N7222 AND SRM 51-50-02. 2 L 7 2 4F RT A2NM 1999081400080 19990814 00080 NM 1999 8 14 CALA9900961 1 19990804 A 5751 113N710064H SKIN BOEING 757 757224 1384958 NM RT AILERON SPLIT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND RT AILERON COMPOSITE PLIES SPLIT AT HINGE POINT I/B OF ACTUATOR ATTACHMENT LOWER SURFACE. THE AILERON WAS REMOVED, REPAIRED, AND REFITTED IAW SRM 51-70-17, ECRA 5751-01022, AND MM 27-11-21. 2 L 7 2 4F RT A2NM 1999081400081 19990814 00081 NM 1999 8 14 CALA9900962 1 19990804 A 5720 CHORD BOEING 757 757224 1384958 NM WS 720 CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND LT WING/FUSELAGE CHORD CHAFED BY UNDER CARRIAGE BEAM REAR SPAR AT STA 720, WBL 70.5. THE CHORD WAS REP LACED IAW BOEING DRAWING 149N7222. 2 L 7 2 4F RT A2NM 1999081400082 19990814 00082 WP 1999 8 14 CALA9900963 1 19990804 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1921 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1921 ON RT SIDE UNDER LAV J. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999081400083 19990814 00083 WP 1999 8 14 CALA9900964 1 19990804 A 7110 LONGERON DOUG DC10 DC1030 3023501 WP NR 2 ENG COWL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE LEFT CORE COWL LONGERON. REPAIRED IAW ECRA 7110-01511. 2 L 7 3 4F A22WE 1999081400084 19990814 00084 WP 1999 8 14 CALA9900965 1 19990804 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 1309 BETWEEN LONGERONS 14R AND 15R. THE CRACK WAS STOP DRILLED IAW SR M 53-01, FIGURE 2. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-03. 2 L 7 2 4F A6WE 1999081400085 19990814 00085 WP 1999 8 14 CALA9900966 1 19990804 A 5280 SB93201894 DOOR DOUG DC9 DC982 3022082 WP RT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 3 INCH CRACK IN RT MLG DOOR. THE DOOR WAS REMOVED AND REPLACED IAW MM 32-10-0. 2 L 7 2 4F A6WE 1999081400086 19990814 00086 WP 1999 8 14 CALA9900967 1 19990804 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1144 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND AFT CARGO FRAME FITTING CORRODED AT FS 1144, STRINGER 28R. THE FITTING WAS REMOVED AND REPLACED IAW SR M 51-30-5. 2 L 7 2 4F A6WE 1999081400087 19990814 00087 WP 1999 8 14 CALA9900968 1 19990804 A 5320 SUBFLOOR DOUG DC9 DC982 3022082 WP BS 158 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A HOLE PUNCTURED INTO CABIN SUBFLOOR AT STA 158, RBL 6. THE SUBFLOOR WAS REMOVED AND A NEW SUBFLOOR WA S INSTALLED IAW SRM 51-30-2, 51-10-2, 53-11-1, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999081400088 19990814 00088 WP 1999 8 14 CALA9900969 1 19990804 A 5350 FILLET DOUG DC9 DC982 3022082 WP BS 806 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND CORROSION AROUND FASTENER HOLES FOR RT LOWER FILLET PANELS 2213C AND 2208C, STA 806, LONGERON 26R. A D OUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999081400089 19990814 00089 WP 1999 8 14 CALA9900970 1 19990727 A 5320 SHEAR CLIP DOUG DC10 DC1030 3023501 WP BS 1661 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND CENTER CARGO COMPARTMENT LONGERON SHEAR CLIP CORRODED AT STA 1661, LONGERON 48R. THE SHEAR CLIP WAS RE PLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999081400090 19990814 00090 NM 1999 8 14 CALA9900971 1 19990727 A 5320 SUPPORT BOEING 757 757224 1384958 NM L4 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13110 27300 INSPECTION FOUND THE L-4 DOOR SILL SUPPORT CORRODED BETWEEN STA 1661 AND 1680. THE DOOR SILL SUPPORT WAS REPLACED IAW B OEING DRAWING 146N8722. 2 L 7 2 4F RT A2NM 1999081400091 19990814 00091 WP 1999 8 14 CALA9900972 1 19990727 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 118 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING TRAILING EDGE SKIN IN ZONE 541 STA XW 118. THE SKIN WAS REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999081400092 19990814 00092 WP 1999 8 14 CALA9900973 1 19990727 A 5730 STRIP DOUG DC10 DC1030 3023501 WP WS 506 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE STRIP AT STA XORS 506. THE LEADING EDGE STRIP WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999081400093 19990814 00093 WP 1999 8 14 CALA9900974 1 19990728 A 5320 SHEAR CLIP DOUG DC10 DC1030 3023501 WP BS 1781 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND SHEAR CLIP CORRODED IN CENTER CARGO COMPARTMENT AT STA 1781, LONGERON 48L. THE SHEAR CLIP WAS REPLACED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1999081400094 19990814 00094 WP 1999 8 14 CALA9900975 1 19990728 A 5321 FLOOR DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND CABIN FLOOR CORRODED AT STA 2007. REPAIRED IAW SRM 53-40-00. 2 L 7 3 4F A22WE 1999081400095 19990814 00095 WP 1999 8 14 CALA9900976 1 19990728 A 5330 SKIN DOUG DC10 DC1030 3023501 WP R4 DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND FUSELAGE SKIN CORRODED AT NR 4 RT CABIN DOOR LOWER AFT CORNER UNDER THE THRESHOLD. THE SKIN WAS REPLAC ED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999081400096 19990814 00096 WP 1999 8 14 CALA9900977 1 19990730 A 5753 SKIN DOUG DC10 DC1030 3023501 WP RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 1 INCH CRACK IN RT WING O/B FLAP SECTION NR 1 UPPER SKIN AT STA 458. THE FLAP SECTION WAS REPAIRED I AW SRM 51-31-01 AND 57-10-00. 2 L 7 3 4F A22WE 1999081400097 19990814 00097 WP 1999 8 14 CALA9900978 1 19990730 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 72.5&421 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA Y421 AND X72.50. THE SEAT TRACK WAS REPLACED IAW SRM 51-31-01 AND MM 51-30-00. 2 L 7 3 4F A22WE 1999081400098 19990814 00098 WP 1999 8 14 CALA9900979 1 19990730 A 5720 CHANNEL DOUG DC10 DC1030 3023501 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 1 INCH CRACK IN LEFT WING UPPER FUEL ACCESS DOOR NR 534CT CHANNEL. THE CHANNEL WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999081400099 19990814 00099 WP 1999 8 14 CALA9900980 1 19990802 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 421-459 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND LEFT SEAT TRACK CORRODED AT Y421 TO Y459, X72.50. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999081400100 19990814 00100 WP 1999 8 14 CALA9900981 1 19990802 A 5753 SKIN DOUG DC10 DC1030 3023501 WP RT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND RT WING I/B FLAP UPPER SKIN DENTED. THE SKIN WAS REPAIRED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1999081400101 19990814 00101 WP 1999 8 14 CALA9900982 1 19990802 A 5414 SKIN DOUG DC10 DC1030 3023501 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON SKIN AT UPPER SURFACE OF FORWARD PYLON. A REPAIR WAS INSTALLED IAW ECRA 5 431-01006. 2 L 7 3 4F A22WE 1999081400102 19990814 00102 WP 1999 8 14 CALA9900983 1 19990802 A 5730 SKIN DOUG DC10 DC1030 3023501 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 1 INCH CRACK IN LEFT WING TRAILING EDGE LOWER SKIN NEXT TO O/B HINGE OF O/B FLAP. A REPAIR WAS INSTA LLED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1999081400103 19990814 00103 WP 1999 8 14 CALA9900984 1 19990802 A 5753 SKIN DOUG DC10 DC1030 3023501 WP RT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND THE RT WING O/B FLAP LOWER SKIN DENTED. A REPAIR WAS INSTALLED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1999081400104 19990814 00104 WP 1999 8 14 CALA9900985 1 19990802 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A .25 INCH CRACK IN ANGLE AT LT WING DROOPED LEADING EDGE. REPAIRED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1999081400105 19990814 00105 WP 1999 8 14 CALA9900986 1 19990804 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A CRACK IN RADIUS OF LONGERON 4L AT STA 160. REPAIRED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1999081400106 19990814 00106 WP 1999 8 14 CALA9900987 1 19990804 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND A .5 INCH CRACK IN FORWARD ENTRY DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999081400107 19990814 00107 WP 1999 8 14 CALA9900988 1 19990805 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND A 1.5 INCH CRACK IN BELTFRAME AT STA 1418 UNDER LONGERON 2L. THE BELTFRAME WAS REPAIRED IAW DOUGLAS DR AWING NR SR095300003. 2 L 7 2 4F A6WE 1999081400108 19990814 00108 1999 8 14 COMA9910126 3 19990805 A 6111 RFC11N16A BLADE EMB 120 EMB120RT SO LT PROP DELAMINATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 16764 1262 NR 2 BLADE ON LEFT PROPELLER IS DELAMINATED AT TIP. REMOVED AND REPLACED BLADE. 2 L 7 2 4T RT A31SO 1999081400109 19990814 00109 SO 1999 8 14 COMA9910127 1 19990803 A 5713 12016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 179CA 22745 120179 WHILE PERFORMING A MAINTENANCE SERVICE CHECK, MECHANIC NOTICED SMALL FUEL LEAK ON BOTTOM SKIN OF LEFT WING JUST FORWARD OF AND OUTBOARD OF ACCESS PANEL 522EB. INTERNAL INVESTIGATION REVEALED A CRACK IN STRINGER 10A AT THE RIVET HOLE THAT W AS LEAKING FUEL, SEVEN INCHES OUTBOARD OF RIB NR 8. THE STRINGER WAS REPAIRED PER EMB120 SRM 57-20-03, FIGURE 201, PAGE S 201-204 AND EMBRAER REPAIR NR SST-1849/99. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999081400110 19990814 00110 NE 1999 8 14 COMA9960413 2 19990804 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 933CA 7040 807161 OIL SMELL IN COCKPIT DURING FLIGHT. REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081400111 19990814 00111 EA 1999 8 14 COMA9960414 1 19990804 A 3320 BF50063905 LIGHT CNDAIR CL600 CL6002B19 EA LAVATORY OVERHEATED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 912CA 7011 F/A SMELLED ELECTRICAL ODOR IN LAVATORY. REPLACED OVERHEATED LENS COVER ON RETURN TO SEAT SIGN. 2 L 7 2 4F RT A21EA 1999081400112 19990814 00112 EA 1999 8 14 COMA9960415 1 19990802 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA E&E COMPT MALFUNCTIONED A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 947CA 5240 829 7077 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999081400113 19990814 00113 EA 1999 8 14 COMA9960416 1 19990803 A 3350 60205 SIGN CNDAIR CL600 CL6002B19 EA GALLEY BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 927CA 7031 EMERGENCY EXIT SIGN AT GALLEY DOOR IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4F RT A21EA 1999081400114 19990814 00114 EA 1999 8 14 COMA9960417 1 19990803 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT/RT TE FLAPS OUT OF ADJUST A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 975CA 6952 7150 FLAPS FAIL MESSAGE. C/W RIGGING OF LEFT AND RIGHT BPSU. 2 L 7 2 4F RT A21EA 1999081400115 19990814 00115 NM 1999 8 14 QXEA9901523 1 19990727 A 3350 82410162001 CONTROLLER DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 822PH 106 SEA - EMERGENCY EXIT TRACK LIGHTING ILLUMINATED IN FLIGHT, CYCLED SWITH WITH NO CHANGE. MAINTENANCE REPLACED THE LIGHTI NG CONTROLLER. DURING OPERATIONAL CHECK THE FORWARD EXIT LOCATOR LIGHTS WENT OUT. REPAIRED A BROKEN WIRE UNDER THE FLO OR. 2 H 7 2 4T RT A13NM 1999081400116 19990814 00116 NM 1999 8 14 QXEA9901524 1 19990729 A 5210 BOLT DHAV DHC8 DHC8102 2809003 NM PAX DOOR LOOSE A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 814PH 43 SEA - MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE RESECURED HANDRAIL SUPPORT PIVOT BOLT. OPERATIONAL CHEC KS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999081400117 19990814 00117 NM 1999 8 14 QXEA9901525 1 19990727 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 824PH 157 PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR MECHANISM. FLIGHT ATTENDANT OPERATED DOOR, NO EXCE SSIVE EFFORT REQUIRED TO OPEN DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999081400118 19990814 00118 EU 1999 8 14 QXEA9901526 1 19990801 A 3350 1012721 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 483US 11233 SEA - EMERGENCY EVACUATION LIGHT AT SEAT 12B HAS BECOME LOOSE AND PARTIALLY HANGING. LIGHT SYSTEM WORKS OK. REMOVED AN D REPLACED LIGHT ASSEMBLY ON SEAT 12B. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999081400119 19990814 00119 EU 1999 8 14 QXEA9901527 1 19990801 A 3350 SOCKET FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 491US 11156 YYC - EMERGENCY LIGHT CAUTION LIGHT WILL NOT PRESS TO TEST, BULB SOCKET ASSEMBLY LOOSE. FOUND LIGHT SOCKET LOOSE, RESEC URED AND CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 L 7 2 4F RT A20EU 1999081400120 19990814 00120 EU 1999 8 14 QXEA9901528 1 19990806 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 482US 11231 PDX - LEFT FORWARD EVACUATION LIGHT INOP. SECURED LAMP HOLDER ASSEMBLY IN NR 1 FORWARD EMERGENCY LIGHT ASSEMBLY. OPERA TIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1999081400121 19990814 00121 EU 1999 8 14 QXEA9901529 1 19990802 A 3350 5515900004 LIGHT GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 483US 11233 SEA - FORWARD EMERGENCY EXIT SIGN IN GALLEY INOP. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL TEST CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999081400122 19990814 00122 NM 1999 8 14 99FDEA00310 1 19990804 A 2613 356644400 OVERHEAT SENSOR BOEING 727 727233 138408A NM NR 3 STRUT MALFUNCTIONED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 272FE 22037 99-190 - NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. EMERG PROC ACCOMPLISHED. LIGHT REMAIN ILLUM. ENGINE SHUT DOWN. REMOVED AND REPLACED NR 3 ENGINE STRUT OVERHEAT SENSING ELEMENT PER MM 26-14-001-2, RAN ENG PER JET RUN HANDBOOK OPER CK GOOD. NO PNEUMATIC LEAKS FOUND. 2 L 7 3 4F RT A3WE 1999081400123 19990814 00123 EU 1999 8 14 99FDEA00314 1 19990803 A 2170 COALESCER BAG AIRBUS 300 A300F4605R 3930327 EU CABIN DIRTY A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 651FE 728 99-193 - AFT T/O, BURN SMELL PRESENT FOR 1 MIN WITH VENTS OPEN. REMOVED AND REPLACED WATER SEPARATOR IN BOTH PACKS PER MM 21-51-11-3. RAN ENG AT HI-PWR PER JRH. OPS CK GOOD. NO SMELL OR FUMES. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999081400124 19990814 00124 NM 1999 8 14 99FDEA00315 1 19990805 A 2612 656020916 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM E&E COMPT MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 213FE 22935 99-194 - FIRE WARN BELL AND CAPT AND 1ST OFF FIRE WARNING LIGHTS CAME ON. CHANGED THE ENGINE FIRE DETECTION PANEL PER M M 26-11-001-0. OPS CK GOOD. 2 L 7 3 4F A3WE 1999081400125 19990814 00125 NM 1999 8 14 USAA990647 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND A .25 INCH CRACK AROUND RIVET AT BS 500D BETWEEN STR 8R AND STR 9R FRAME . INSTALLED REPAIR ANGLE PER EA 64815 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999081400126 19990814 00126 NM 1999 8 14 USAA990614 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND A .25 INCH CRACK AT BS 787 BETWEEN STR 8 AND STR 9R FRAME. INSTALLED DO UBLER PER SRM 53-00-07 AND EA 64815. (X) 2 L 7 2 4F RT A16WE 1999081400127 19990814 00127 NM 1999 8 14 USAASB99181 1 19990722 A 3350 30043229 LIGHT BOEING 737 7374B7 1384702 NM SERVICE DOORWAY CORRODED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 RIC - MAINTENANCE FOUND THE EXTERIOR ESCAPE SLIDE EMERGENCY LIGHT FOR THE RIGHT AFT SERVICE DOOR INOPERABLE. MAINTENANC E REMOVED AND REPLACED THE EXTERIOR ESCAPE SLIDE LIGHT ASSEMBLY AT THE RIGHT AFT SERVICE DOOR AND REPAIRED WIRING AT THE POWER PACK CANNON PLUG IN ASSOCIATION WITH MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999081400128 19990814 00128 NM 1999 8 14 USAASB99185 1 19990726 A 3350 LIGHT BOEING 737 7372B7 1384560 NM SERVICE DOOR INOPERABLE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 278AU 22890 ATL - PILOT REPORTED THE EMERGENCY EXIT LIGHTS REMAIN ON IN THE ARMED POSITION. MAINTENANCE FOUND LOOSE HARDWARE AT THE FORWARD SERVICE DOOR EMERGENCY LIGHT POWER SUPPLY CAUSING A SHORT AND TRIPPING THE 'EMERG LIGHTS PWR' CIRCUIT BREAKER. SECURED HARDWARE AT THE FORWARD SERVICE DOOR EMERGENCY LIGHT POWER SUPPLY. RESET CIRCUIT BREAKER. EMERGENCY LIGHTS OP ERATIONALLY CHECKED GOOD. (X) 2 L 7 2 4F A16WE 1999081400129 19990814 00129 NM 1999 8 14 USAASB99184 1 19990725 A 3350 S106 BATTERIES BOEING 737 737201 1384454 NM COCKPIT DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 ROC - DURING OVERNIGHT MAINTENANCE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE COCKPIT DOOR INOPERABLE. MAINT ENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECKED GOOD. (X) 2 L 7 2 4F A16WE 1999081400130 19990814 00130 NM 1999 8 14 USAASB99183 1 19990724 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM ROWS 17-20 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 592US 23937 BDL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 20 INOPERABLE. MAINTENANCE REMOVED AND REPLA CED THE CHARGER ASSEMBLY AT STA 962L. OPERATIONAL CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 1999081400131 19990814 00131 1999 8 14 USAASB99141 4 19990611 A 3441 IRS BOEING 737 737401 1384701 NM COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 411US 23880 ROC - FLT 1886 - AFTER TAKEOFF, CREW REPORTED LOSING HEADING INDICATOR. CREW ACCOMPLISHED SPECIAL PROCEDURES, BUT FAILE D TO REST. CAPTAIN ELECTED TO RETURN TO FIELD AT ROC. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAR ED. MAINTENANCE ALIGNED IRS SYSTEM. OPERATIONAL CHECKED GOOD. NO FURTHER ITEMS. (X) 2 L 7 2 4F RT A16WE 1999081400132 19990814 00132 NM 1999 8 14 USAASB99156 1 19990628 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 385US 22958 LGA - FLT 528 - PILOT REPORTED PRIOR TO DEPARTURE, THE FORWARD ENTRY AND FORWARD SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. BATTERY PACK, P/N 2013-1ALP. CHARGER ASSY, P/N 2012-1. REF: OPERATOR CNTRL NR 99ZZZX2961. (X) 2 L 7 2 4F RT A16WE 1999081400133 19990814 00133 NM 1999 8 14 99ZZZX2961 1 19990628 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERABLE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 385US 22958 LGA - FLT 528 - PILOT REPORTED PRIOR TO DEPARTURE, THE FORWARD ENTRY AND FORWARD SERVICE DOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. BATTERY PACK, P/N 2013-1ALP. CHARGER ASSY, P/N 2012-1. REF: OPERATOR CNTRL NR USAASB99156. 2 L 7 2 4F RT A16WE 1999081400134 19990814 00134 1999 8 14 USAASB99146 4 19990615 A 3460 1689250710 FMC BOEING 737 7374B7 1384702 NM E/E COMPT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 449US 26623 24893 LGA - FLT 950 - AFTER TAKEOFF FROM LGA, FLIGHT EXPERIENCED AN FMC PROBLEM. FAILURE OF NAV AND AIRCRAFT DATA OCCURRED. F LIGHT RETURNED TO FIELD AT LGA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLIGHT MANAGEMENT COMPUTER. LOADED NAV DATA. BITE CHECKED AND OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999081400135 19990814 00135 NM 1999 8 14 USAASB99127 1 19990522 A 3340 3008375 BEACON BOEING 737 7374B7 1384702 NM UPPER FUSELAGE FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 426US 23997 24548 JAX - FLT 1023 - EN ROUTE FROM PHL TO MIA, CREW REPORTED THE RIGHT PACK TEMPERATURE INDICATION READ 200 DEGREES ALL THE TIME. CREW ALSO REPORTED THE UPPER ANTI-COLLISION BEACON CIRCUIT BREAKER WAS FOUND OPEN AND WHEN AN ATTEMPT TO RESET TH E BREAKER WAS ACCOMPLISHED, THE BREAKER RE-OPENED CAUSING SMOKE TO APPEAR IN THE PASSENGER MID-CABIN. FLIGHT DIVERTED T O JAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK TEMPERATURE BULB (P/N MS5280 34-1). OPERATIONAL CHECK OF RIGHT PACK NORMAL. MAINTENANCE DETERMINED THE SMOKE TO COME FROM A FAILED UPPER ANTI-COLLI SION BEACON. OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4F RT A16WE 1999081400136 19990814 00136 NM 1999 8 14 USAABB99036 1 19990712 A 2820 233T323512 FUEL CNTRL PANEL BOEING 767 7672B7 1385107 NM COCKPIT BROKEN A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 655US 31587 25257 PHL - FLT 16 - EN ROUTE PHL/CDG, CREW FOUND THE FUEL CROSS-FEEL SWITCH WOULD NOT GO IN. FLIGHT RETURNED TO PHL AND LAND ED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL PANEL. (X) 2 L 7 2 4F RT A1NM 1999081400137 19990814 00137 NM 1999 8 14 USAABB99037 1 19990721 A 4930 388250017 FUEL CONTROL 38002981 BOEING 767 767201 1385125 NM APU FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 646US 0P171C 23898 LGW - FLT 49 - EN ROUTE CDG/PIT, WITH RIGHT IDG ON MEL AND THE APU OPERATING, THE APU 'FAULT' LIGHT ILLUMINATED AND THE EICAS MESSAGE 'APU FAULT' APPEARED. THE APU WAS SHUT DOWN. THE FLIGHT DIVERTED TO LGW AND LANDED WITH NO FURTHER INCID ENT. MAINTENANCE REPLACED THE APU FUEL CONTROL. (X) 2 L 7 2 4F RT A1NM 1999081400138 19990814 00138 1999 8 14 USAASB99178 4 19990719 A 3442 20412170416 TR UNIT BOEING 737 737301 1384611 NM RADAR SYSTEM MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 563AU 23551 BWI - FLT 0166 - DURING CRUISE, EN ROUTE PHX/PHL, THE WEATHER RADAR BECAME UNRELIABLE. TEST PAGE SHOWED 'R/T FAULT' FOL LOWED BY 'NO WXR'. SYSTEM WORKED FINE INITIALLY. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENA NCE OPERATIONALLY CHECKED SYSTEM AND NOTED NO FAULTS FOUND. REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER (P/N 2041217 -0416) AS PRECAUTIONARY. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999081400139 19990814 00139 NE 1999 8 14 USAABB99034 2 19990711 A 7520 312N53217 DUCT BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LEAKING A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 605AU 22201 30921 SFO - FLT 76 - ON CLIMB-OUT FROM SFO, CREW RECEIVED LEFT ENGINE OVERHEAT WARNING. CREW PERFORMED PROCEDURES AND THE WAR NINGS PERSISTED. THE ENGINE WAS SECURED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. (SET 0:20). MAI NTENANCE REPLACED THE LEFT ENGINE HP6 DUCT. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1999081400140 19990814 00140 1999 8 14 USAASB99180 4 19990722 A 3417 HG480B13 ADC BOEING 737 737201 1384454 NM E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 245US 39611 33545 22751 BWI - FLT 2612 - DURING TAKEOFF AND CLIMB-OUT FROM BWI, CAPTAIN REPORTED HE LOST NR 1 AIR DATA COMPUTER AND WINDSHEAR WA RNING WAS GOING OFF. PRESSURIZATION WAS LOST IN AUTOMODE AND REGAINED BY SWITCHING OVER TO STANDBY MODE. CAPTAIN PLACE D FLIGHT IN HOLDING PATTERN AT 8,000 FEET AND LET FIRST OFFICER FLY ACFT WHILE TRYING TO DETERMINE PROBLEM. CAPT DECLAR ED AN EMERGENCY AND ELECTED TO RETURN TO BWI. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINT REMOVED AND REPLACED THE N R 1 AIR DATA COMPUTER. OPER CHECK NORMAL. RAN ENGINE AND CHECKED ELECTRICAL BUSSES. NO FAULTS NOTED. REPLACED POWER MANAGEMENT SYS COMPUTER (P/N 4050730-921) FOR FAILING TEST. BITE CHECK NORMAL. NO FURTHER DISCREPANCIES REPORTED. (X) 2 L 7 2 4F A16WE 1999081400141 19990814 00141 WP 1999 8 14 USAAD99099 1 19990719 A 2450 HDX9F011 RELAY DOUG DC9 DC982 3022082 WP AC POWER DIST FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 829US 49429 PIT/MSY - FLT 474 - AFTER TAKEOFF IT WAS NOTED THERE WERE NO CABIN LIGHTS OR LAVATORY LIGHTS. THE TOILETS DID NOT FLUSH , THE NR 4 TR INDICATED ZERO, AND THE BATTERY CHARGER WAS INOPERATIVE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WI THOUT INCIDENT. MAINTENANCE REPLACED THE GROUND SERVICE BUSS TRANSFER RELAY (R2-50), AND THE GROUND CONTROL RELAY (R2-4 8). (X) 2 L 7 2 4F A6WE 1999081400142 19990814 00142 WP 1999 8 14 USAAD99100 1 19990722 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 IND - THE CEILING EMERGENCY LIGHTS ADJACENT TO THE AFT SERVICE DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENC Y LIGHT BATTERY POWER SUPPLY. (X) 2 L 7 2 4F A6WE 1999081400143 19990814 00143 WP 1999 8 14 USAAD99096 1 19990717 A 3350 P2010014 LIGHT DOUG DC9 DC931 3022065 WP GALLEY DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 981VJ 48157 IND - THE SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY L IGHT ASSEMBLY BATTERY. (X) 2 L 7 2 4F A6WE 1999081400144 19990814 00144 WP 1999 8 14 USAAD99098 1 19990718 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP ROWS 9-13 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918VJ 48138 IND - THE CEILING EMERGENCY LIGHTS AT ROWS 9 THROUGH 13 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWE R SUPPLY. (X) 2 L 7 2 4F A6WE 1999081400145 19990814 00145 EU 1999 8 14 USAAF99036 1 19990720 A 2150 9785606 MODULATING VALVE FOKKER F28 F28MK0100 4990807 EU RT PACK FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 895US 17631 399 11380 PHL - FLT 681 - FLIGHT RETURNED TO PHL DUE TO THE RIGHT PACK RUNNING FULL HOT AND CREATING A BURNING SMELL IN THE CABIN. THE LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT PACK MODULATING VALVE. (X) 2 L 7 2 4F RT 1999081400146 19990814 00146 NM 1999 8 14 USAASB99176 1 19990719 A 5610 BACC45FT105S CONNECTOR BOEING 737 737401 1384701 NM LT COCKPIT FAILED A USAA A UNSCHED LANDING A FLAME/FIRE TO TAKEOFF 1 EA 19 424US 23991 PHL - FLT 1429 - DURING TAKEOFF, THE CAPTAIN'S SLIDING WINDOW WIRING STARTED SPARKING AND BURNING AT THE CONNECTOR STRAI N RELIEF. CAPTAIN TURNED THE WINDOW HEAT OFF AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S SLIDING WINDOW ELECTRICAL CONNECTOR. WINDOW HEAT OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999081400147 19990814 00147 NM 1999 8 14 USAASB99169 1 19990709 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 349US 23552 IAH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999081400148 19990814 00148 WP 1999 8 14 USAAD99097 1 19990717 A 2170 V1211 COALESCER BAG DOUG DC9 DC981 3022081 WP AFT FUSELAGE CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 814US 48094 ORD/PIT - FLT 1817 - DURING CLIMB-OUT THERE WAS A BURNING SMELL IN THE COCKPIT AND THE CABIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AIR CONDITIONING SYSTEM COALESCER BAGS. (X) 2 L 7 2 4F A6WE 1999081400149 19990814 00149 EU 1999 8 14 AALA991056 1 19990717 A 2740 6227478411 COMPUTER COLLINS FOKKER F28 F28MK0100 4990807 EU E/E COMPARTMENT DEFECTIVE A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 1403M 740 11354 DFW - FLT 1779 - ON TAKEOFF FROM DFW TO AMA, STABILIZER TRIM RUNAWAY DETECTED. STABILIZER TRIM SWITCH TURNED OFF AND AI RCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FLIGHT AUGMENTATION COMPUTER AND BOTH CAPTAIN AND FIRST OF FICER TRIM SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999081400150 19990814 00150 EU 1999 8 14 AALA991028 1 19990711 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 24HJ LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 41063 506 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 24HJ AND 25HJ INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED, NORMAL, OPERATION. (X) 2 L 7 2 4F RT A35EU 1999081400151 19990814 00151 EU 1999 8 14 AALA991039 1 19990714 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 24 HJ LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 41063 506 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN ROWS 24 H/J AND 25 H/J INOPERATIVE. RE-SEC URED CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999081400152 19990814 00152 EU 1999 8 14 AALA991035 1 19990713 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7055A 462 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN DOORS 3R AND 3L INOPERATIVE. REPAIRED EM ERGENCY EXIT FLOOR PATH LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999081400153 19990814 00153 WP 1999 8 14 AALA991023 1 19990711 A 2120 DUCT DOUG DC10 DC1010 3022110 WP ACM COMPARTMENT WORN A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 131AA 46994 HNL - FLT 28 - EN ROUTE HNL/SFO DURING CRUISE, CAUSTIC ODOR WAS NOTED IN THE PASSENGER COMPARTMENT IN THE AREA BETWEEN R OWS 16 AND 19. THE AIRCRAFT RETURNED TO HNL AND LANDED WITHOUT INCIDENT. REMOVED TAPE FORM THE NR 1 PNEUMATIC DUCT INS ULATION IN THE CENTER ACCESSORY COMPARTMENT. ALL THREE AIR CONDITIONING PACKS WERE BURNED OUT PER MM. RAN ENGINES. NO ODOR NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1999081400154 19990814 00154 EU 1999 8 14 AALA991019 1 19990711 A 3260 AAP3273A INDICATOR FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 1405J 11356 ORD - FLT 1487 - DURING APPROACH ORD, NOSE GEAR LIGHT DID NOT ILLUMINATE WITH GEAR DOWN. LANDING GEAR CYCLED AND LIGHT ILLUMINATED NORMALLY WITH GEAR SELECTOR IN THE DOWN POSITION. LANDED ORD WITHOUT INCIDENT. REPLACED GEAR POSITION INDI CATOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999081400155 19990814 00155 EU 1999 8 14 AALA991018 1 19990711 A 3230 10SD8001 SOLENOID FOKKER F28 F28MK0100 4990807 EU COCKPIT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1471G 11507 DFW - FLT 1068 - EN ROUTE DFW/CLT AFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR HANDLE. AIR INTERRUPTED, RETURNED DFW, AN D LANDED WITHOUT INCIDENT. REPLACED ANTI-RETRACT SOLENOID. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999081400156 19990814 00156 EU 1999 8 14 AALA991031 1 19990712 A 2934 920100078 TRANSMITTER FOKKER F28 F28MK0100 4990807 EU NR 1 HYD SYSTEM DEFECTIVE A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 1437B FRTR046AG 11427 DFW - FLT 499 - DURING APPROACH DFW FROM HSV, AIRCRAFT LOST NR 1 HYDRAULIC FLUID. LANDED DFW WITH GEAR DOORS DOWN. REP LACED NR 1 HYDRAULIC SYSTEM QUANTITY TRANSMITTER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999081400157 19990814 00157 WP 1999 8 14 AALA991046 1 19990715 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT STAIRWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90511 49805 LGA - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED WIRE BEHIND RELEASE HANDLE FOR AFT STAIRWAY/TAIL CONE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400158 19990814 00158 WP 1999 8 14 AALA991044 1 19990714 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT STAIRWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7548A 53030 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE AT AFT STAIRWAY EMERGE NCY EXIT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400159 19990814 00159 WP 1999 8 14 AALA991043 1 19990713 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS AND FORWARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHT STRIPS INOPERATIVE. R EPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FORWARD GALLEY AND FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OP ERATION. (X) 2 L 7 2 4F A6WE 1999081400160 19990814 00160 WP 1999 8 14 AALA991038 1 19990713 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445AA 49471 DFW - DURING OVERNIGHT MAINTENANCE, WALK-AROUND EMERGENCY LIGHT ASSEMBLY INOPERATIVE. REPLACED WALK-AROUND EMERGENCY LI GHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400161 19990814 00161 WP 1999 8 14 AALA991037 1 19990713 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 224AA 49174 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY FLOOR EXIT LIGHT INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GRO1111U ND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400162 19990814 00162 WP 1999 8 14 AALA991021 1 19990711 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7537A 49991 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY WALK-AROUND EMERGENCY LIGHT ASSEMBLY INOPERATIVE. REPLACED WALK-AROUN D EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400163 19990814 00163 WP 1999 8 14 AALA991030 1 19990712 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT BURNED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 242AA 49255 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE TO TAIL COMPARTMEN T EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400164 19990814 00164 WP 1999 8 14 AALA991053 1 19990717 A 2150 32185831 VALVE DOUG DC9 DC982 3022082 WP RT ACM DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 7520A 4211 49897 IAH - FLT 616 - ON APPROACH TO IAH FROM DFW, SMOKE DETECTED IN CABIN. RIGHT AIR CONDITIONING PACK WAS SHUT DOWN AND PUL LED J-7 CIRCUIT BREAKER. LANDED IAH WITHOUT INCIDENT. REPLACED RIGHT AIR CONDITIONING PACK TEMPERATURE CONTROL VALVE. ALSO, REPLACED LEFT AND RIGHT COALESCER BAGS. PERFORMED AIR CONDITIONING PACK BURN-OUT PER MM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400165 19990814 00165 CE 1999 8 14 MASA99120 1 19990717 A 5270 WARNING BEECH 1900 1900D 1154162 CE PASSENGER DOOR ACTIVATED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 93ZV UE93 IFP/PHX - FLT 6377 - THE CREW DECLARED AN EMERGENCY DUE TO A CABIN DOOR ANNUNCIATOR ILLUMINATED. THE AIRCRAFT LANDED IN PHX SAFELY. MAINTENANCE ACTION WAS DEFERRED PER MEL 52-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999081400166 19990814 00166 NE 1999 8 14 MASA99116 2 19990707 A 7322 324485316 MFC DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE RT ENGINE FAILED A MASA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 446YV 446 PHX/PSP - FLT 6343 - THE CAPTAIN REPORTED THE RIGHT ENGINE WAS MAKING 88 PERCENT TORQUE. MAINTENANCE REMOVED AND REPLAC ED MFC. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1999081400167 19990814 00167 EA 1999 8 14 MASA99121 1 19990719 A 3350 487190487191 SOCKET CNDAIR CL600 CL6002B19 EA CABIN UNPLUGGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 PHL/CVG - FLT 5753 - THE CAPTAIN REPORTED THE EMERGENCY ESCAPE PATH LIGHT HAD A SMALL FORWARD SECTION INOPERABLE. MAINT ENANCE FOUND THE PIN/SOCKET UNPLUGGED. MAINTENANCE REPLUGGED. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. ( X) 2 L 7 2 4F RT A21EA 1999081400168 19990814 00168 1999 8 14 99ZZZX2962 4 19990713 A 2565 D29835105 SEAM AIRCRUISERS BOEING 727 727200 138407E NM ESCAPE SLIDE FAILED A RIVA K NONE O OTHER IN INSP/MAINT 1 SO 17 20709182 DURING FLIGHT ATTENDANT TRAINING, SLIDE INFLATED FOR APPROXIMATELY 10 MINUTES. SEAM AT UPPER AFT CORNER SPLIT, DEFLATIN G SLIDE. 2 L 7 3 4F RT A3WE 1999081400169 19990814 00169 1999 8 14 99ZZZX2963 4 19990712 A 2564 RA46102 LIFE RAFT EAAEROMARINE BOEING 727 727200 138407E NM CABIN FAILED A RIVA K NONE O OTHER IN INSP/MAINT 1 SO 17 F461047 DURING FLIGHT ATTENDANT TRAINING, LIFE RAFT INFLATED ONLY HALF-WAY. 2 L 7 3 4F RT A3WE 1999081400170 19990814 00170 NM 1999 8 14 TSAA9933306 1 19990722 A 3350 963100211 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERABLE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 5 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999081400171 19990814 00171 NM 1999 8 14 TSAA0033304 1 19990722 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 4 EMERGENCY FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999081400172 19990814 00172 NM 1999 8 14 TSAA9933303 1 19990722 A 3350 873100151 LIGHT BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 4 EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999081400173 19990814 00173 NM 1999 8 14 TSAA933302 1 19990721 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999081400174 19990814 00174 NM 1999 8 14 TSAA9933301 1 19990721 A 3350 86210066 BATTERY BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 3 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999081400175 19990814 00175 EU 1999 8 14 SIMA992022 1 19990721 A 5210 S536780082002 ZEE AEROSP ATR72 ATR72212 EU PASSENGER DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING HMBV-1 INSPECTION, FOUND THE LEFT AFT PASSENGER DOOR ZEE MEMBER CORRODED BETWEEN FRAMES 39 AND 40. REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 52-11-30. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999081400176 19990814 00176 EU 1999 8 14 SIMA992021 1 19990721 A 5230 S52376110214 FRAME AEROSP ATR72 ATR72212 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE THREE FORWARD UPPER FRAMES ON THE CARGO DOOR CRACKED. MAINTENANCE REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX2964 AND 99ZZZX2965. (X) 2 H 7 2 4T RT A53EU 1999081400177 19990814 00177 EU 1999 8 14 99ZZZX2964 1 19990721 A 5230 S52376104204 FRAME AEROSP ATR72 ATR72212 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE THREE FORWARD UPPER FRAMES ON THE CARGO DOOR CRACKED. MAINTENANCE REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA992021 AND 99ZZZX2965. 2 H 7 2 4T RT A53EU 1999081400178 19990814 00178 EU 1999 8 14 99ZZZX2965 1 19990721 A 5230 S52376105208 FRAME AEROSP ATR72 ATR72212 EU CARGO DOOR CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE THREE FORWARD UPPER FRAMES ON THE CARGO DOOR CRACKED. MAINTENANCE REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA992021 AND 99ZZZX2964. 2 H 7 2 4T RT A53EU 1999081400179 19990814 00179 EU 1999 8 14 REXA99022 1 19990711 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A REXA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 369PX 340B295 CARGO SMOKE LIGHT CAME ON IN-FLIGHT. ACTIVATED FIRE EXTINGUISHER BOTTLE. CLEANED SMOKE DETECTOR, REMOVED AND REPLACED CARGO FIRE EXTINGUISHER. SYSTEM CHECKS GOOD. (X) 2 L 7 2 4T RT A52EU 1999081400180 19990814 00180 EU 1999 8 14 RAIA990720 1 19990717 A 3233 6158E ACTUATOR BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 864AE 5571 864 PSP - FLT 4705 - NOSE GEAR DID NOT RETRACT. MAINTENANCE REPLACED RETRACTION JACK ON NOSE GEAR. (X) 2 L 7 2 4T RT A56EU 1999081400181 19990814 00181 EU 1999 8 14 RAIA990723 1 19990720 A 2910 1379305A77 LINE BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 875JX 875 STL - FLT 7504 - BOTH HYDRAULIC PRESSURE GAUGES DROPPED TO ZERO. MAINTENANCE REPLACED LEFT HYDRAULUIC PUMP PRESSURE LIN E. (X) 2 L 7 2 4T RT A56EU 1999081400182 19990814 00182 EU 1999 8 14 RAIA990724 1 19990722 A 5320 SKIN AEROSP ATR72 ATR72202 8680940 EU FUSELAGE DAMAGED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 722TE 220 SUSTAINED DAMAGE AT FRAME 44 ON RIGHT SIDE OF AIRCRAFT DURING RAMP OPERATION. MAINTENANCE REPAIRED DAMAGE IAW EO NR ATR 72-53-008-1. ACFT TT: 16,621.0 HOURS. (X) 2 H 7 2 4T RT A53EU 1999081400183 19990814 00183 WP 1999 8 14 ORJA99235 1 19990717 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 8D-11D DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 LAS - EMERGENCY LIGHTS INOPERABLE ON SEATS 8D THROUGH 11D. REMOVED AND REPLACED BATTERY PACK AT RT FORWARD OVERWING EXI T DOOR IAW MM 33-53-00. (X) 2 L 7 2 4F RT A6WE 1999081400184 19990814 00184 WP 1999 8 14 ORJA99234 1 19990712 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY EXIT DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - BOTH AFT LT AND RT EMERGENCY BATTERY LIGHTING INOPERABLE. REPLACED BOTH LT AND RT EMERGENCY EXIT LIGHT BATTERY PA CKS. (X) 2 L 7 2 4F RT A6WE 1999081400185 19990814 00185 WP 1999 8 14 ORJA99233 1 19990711 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROWS 3-6 INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 SEA - EMERGENCY TRACK LIGHTS CAME ON AT ROWS 3-6 ACFT RIGHT. WOULD NOT EXTINGUISH WITH EMERGENCY LIGHT SWITCH OFF. REM OVED AND REPLACED IN SEAT LIGHTING POWER SUPPLY AT R-1 DOOR. (X) 2 L 7 2 4F RT A6WE 1999081400186 19990814 00186 WP 1999 8 14 ORJA99232 1 19990712 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 2 LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 RNO - ROW 2 EMERGENCY LIGHT INOPERABLE. RE-CONNECTED CONNECTOR, OPS CHECK GOOD IAW 33-53-01. (X) 2 L 7 2 4F RT A6WE 1999081400187 19990814 00187 WP 1999 8 14 EIAA990186 1 19990722 A 2510 SEAT DOUG DC9 DC933F 302207A WP COCKPIT MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 945F 47279 MMV - DURING EVALUATION, FOUND COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25. 561. COURIER SEAT DEACTIVATED PER EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91. REV C. EO APPROVED BY 8110-3 DATED 7-15-99. (X) 2 L 7 2 4F A6WE 1999081400188 19990814 00188 WP 1999 8 14 EIAA990181 1 19990722 A 2510 SEAT DOUG DC9 DC915F 3022037 WP COCKPIT MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 916F 47044 MMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FA R 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-8 05-91, REV C. EO APPROVED BY 8110-3 DATED 7-15-99. (X) 2 L 7 2 4F A6WE 1999081400189 19990814 00189 WP 1999 8 14 EIAA990184 1 19990722 A 2510 SEAT DOUG DC9 DC933F 302207A WP COCKPIT MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 940F 47414 MMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FA R 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-8 05-91, REV C. EO APPROVED BY 8110-3 DATED 7-15-99. (X) 2 L 7 2 4F A6WE 1999081400190 19990814 00190 WP 1999 8 14 EIAA990183 1 19990722 A 2510 SEAT DOUG DC9 DC933F 302207A WP COCKPIT MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 933F 47191 DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA 2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25. 561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO-25-DC9-805-91, REV C. EO APPROVED BY 8110-3 DATED 7-15-99. (X) 2 L 7 2 4F A6WE 1999081400191 19990814 00191 WP 1999 8 14 EIAA990182 1 19990722 A 2510 SEAT DOUG DC9 DC932F 3022067 WP COCKPIT MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 932F 47355 MMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA 2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF F AR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9- 805-91, REV C. EO APPROVED BY 8110-3 DATED 7-15-99. (X) 2 L 7 2 4F A6WE 1999081400192 19990814 00192 WP 1999 8 14 EIAA990185 1 19990722 A 2510 SEAT DOUG DC9 DC933F 302207A WP COCKPIT MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 944F 47194 MMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA 2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF F AR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-8 05-91, REV C. EO APPROVED BY 8110-3 DATED 7-15-99. (X) 2 L 7 2 4F A6WE 1999081400193 19990814 00193 EA 1999 8 14 MASA99126 1 19990728 A 3350 GE1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17231 7231 FLT 5763 - STL-PHL - THE PREFLIGHT INSPECTION, THE CAPTAIN REPORTED THE THIRD AFT CEILING EMERGENCY LIGHT WAS NOT ILLUMI NATED. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENAN CE, THE BULB WAS REPLACED. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999081400194 19990814 00194 EA 1999 8 14 MASA99124 1 19990723 A 3350 GE1317 BULB BRUCE BC10020004 CNDAIR CL600 CL6002B19 EA ROW 5 FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37208 7208 DURING ROUTINE MAINTENANCE, THE EMERGENCY CEILING LIGHT ROW 5 WAS FOUND INOPERABLE. FOUND TWO OF THE FOUR MOUNTING SCRE WS FELL OUT AND BULB WAS LOOSE IN SOCKET. MAINTENANCE RE-INSTALLED MOUNTING SCREW, INSTALLED NEW BULB, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999081400195 19990814 00195 EU 1999 8 14 99ZZZX2894 1 19990716 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAMES 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 399AT 399 SJU - HMV1 INSPECTION CRIC NR 7991 AT LT F/A SEAT TRACK IS CORRODED. BLENDED OUT CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 PAGE 312 THROUGH 314. CAUSE OF DAMAGE, ENVIRONMENTAL. COMPLETED CORROSION REPAIR PER EO NR 9-5300-013R4 B Y REMOVING AND REPLACING SEAT TRACK LT SIDE F/A. (X) 2 H 7 2 4T RT A53EU 1999081400196 19990814 00196 WP 1999 8 14 ARWA990704 1 19990727 A 5310 STRUCTURE DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 MIA - FLT 574 - DURING ROUTINE INSPECTION DURING MAIN CARGO DOOR MAINTENANCE, DETECTED APPROXIMATELY 10 INCH CRACK IN ST C DOUBLER EMANATING LOWER FORWARD CORNER AT CUSP LINE. AFTER GAINING INTERNAL ACCESS TO AREA, FOUND 5 EACH FLOORBEAM TO LOWER SILL FITTINGS CRACKED. WORK CONTINUES ON AERONAUTICAL ENGINEERS STC DOOR INSTALLATION. CAUSE UNKNOWN. REMOVED AND REPLACED DOOR SILL FITTINGS IAW STC HOLDERS INSTRUCTION. CAUSE OF FAILURE REMAINS UNDER INVESTIGATION. (X) 2 L 7 4 4F 4A25 1999081400197 19990814 00197 WP 1999 8 14 ARWA990705 1 19990727 A 3260 PROXIMITY CARD DOUG DC8 DC863 302198A WP GEAR DOOR MALFUNCTIONED A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 345JW 46042 MIA - FLT 9038 - DURING GEAR RETRACTION, GOT DOOR NOT LATCHED LIGHT. FOLLOWED DOOR NOT LATCHED LIGHT CHECKLIST. DID NO T SOLVE PROBLEM. RETURNED TO MIAMI. RERACKED PROXIMITY CARD J-12 AND J-13. INDICATION OF GEAR DOOR WARNING. OPS CHEC KED NORMAL IAW 32-10-00. ACCOMPLISHED GEAR SWING. OPS CHECK NORMAL, VARIOUS TIMES IAW 32-20-0. (X) 2 L 7 4 4F 4A25 1999081400198 19990814 00198 NM 1999 8 14 UIEA99049 1 19990716 A 5311 65B017121119 FRAME BOEING 747 747230B 1384889 NM BS 380 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 BS 380 LT, FOUND TWO CRACKS IN FUSELAGE FRAME AT STR 23 DURING SECTION 41 INSPECTION. CRACK RUNS FROM STRINGER CUT-OUT TO NEAREST FASTENER HOLE, THE OTHER TO THE SKIN FLANGE. REPAIRED FRAME WEB, PER KLM DFX 99-132 REV 2, FORM 8110-3 ISSUE D. (X) 2 L 7 4 4F A20WE 1999081400199 19990814 00199 NM 1999 8 14 UIEA99050 1 19990716 A 5311 65B01714518 FRAME BOEING 747 747230B 1384889 NM BS 420 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 BS 420 LT, FOUND CRACK IN FUSELAGE FRAME AT STR 14E DURING SECT 41 INSPECTION. CRACK RUNS FROM STRINGER CUT-OUT TO INBO ARD. REPAIRED FRAME WEB PER ACC KLM DFX 99-134 REV 2, FORM 8110-3. (X) 2 L 7 4 4F A20WE 1999081400200 19990814 00200 NM 1999 8 14 UIEA99052 1 19990716 A 5311 65B01719509 FRAME BOEING 747 747230B 1384889 NM BS 520 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 BS 520 LT, FOUND CRACK IN FUSELAGE FRAME FLANGE BETWEEN STR 9 AND STR 11. ALSO, SHEAR DOUBLER CRACKED IN CUT-OUT TO NEA REST FASTENER HOLE DURING SECTION 41 INSPECTION. REPAIRED STR 9 PER SRM 53-10-04, FIG 85. REPAIRED FRAME AT STR 10 PER ACC KLM DFX 99-126 REV 1. SHEAR DOUBLER AT STR 11 REPAIRED PER ACC KLM DFX 99-123. FORM 8110-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999081400201 19990814 00201 NM 1999 8 14 UIEA99053 1 19990716 A 5711 SPAR WEB BOEING 747 747230B 1384889 NM CENTER WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 LEFT WING GEAR WHEEL, SPOT CORROSION FOUND ON CENTER TANK REAR SPAR WEB BEHIND THE BS 1241 LT BULKHEAD FITTING. REF: A D 98-26-23 AND SB 747-57-2263R2. CORROSION REMOVED IAW SB 747-57 2263 REV R2 AND FAX KLM TLS 99-0008H. FORM 8110-3 ISS UED. 2 L 7 4 4F A20WE 1999081400202 19990814 00202 NM 1999 8 14 UIEA99048 1 19990716 A 5311 65B01711 FRAME BOEING 747 747230B 1384889 NM BS 360 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 BS 360 LT, FOUND CRACK IN FUSELAGE (MID) FRAME AT STR 14E DURING SECTION 41 INSPECTION. CRACK RUNS FROM CUT-OUT TO NEAR EST FASTENER HOLE BELOW FORMED CHORD. REPAIRED FRAME PER ACC KLM DFX 99-133 REV 1. FORM 8110-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999081400203 19990814 00203 NM 1999 8 14 UIEA99054 1 19990716 A 5311 FRAME WEB BOEING 747 747230B 1384889 NM BS 1265 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 BS 1265 HFEC INSPECTION PERFORMED ON LT NR 3 MAIN ENTRY DOOR FRAME. UNDER FLOOR, LINE FOUND CRACK INDICATION IN WEB. I NTERIM REPAIR ACCOMPLISHED PER ACC KLM DFX 99-119 REV 2. RE-INSPECT AT 2,000 CYCLE INTERVALS. FORM 8110-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999081400204 19990814 00204 NM 1999 8 14 UIEA99055 1 19990716 A 5310 STRUCTURE BOEING 747 747230B 1384889 NM BS 1980 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 BULK CARGO DOOR SKIN, DOUBLER AND TRIPLER CRACKED ON BOTTOM OF CUT-OUT AT BS 1980 RT BETWEEN STR 37 AND STR 38. CRACK I S HORIZONTAL AND MEASURES 0.500 INCHES. CRACK REPAIRED PER ACC KLM DFX 99-120. FORM 8110-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999081400205 19990814 00205 NM 1999 8 14 UIEA99056 1 19990716 A 5311 65B01786312 FRAME BOEING 747 747230B 1384889 NM BS 1840 DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 FRAME DENTED AT STA 1840 RT TWO PLACES, FIRST BETWEEN STR 12 AND STR 13, SECOND BETWEEN STR 10 AND STR 11. FRAME REPAIR ED BETWEEN STR 12/13 PER SRM 53-10-04 FIG 87. FRAME REPAIRED BETWEEN STR 10/11 PER ACC KLM DFX 99-127 REV 2. (X) 2 L 7 4 4F A20WE 1999081400206 19990814 00206 NM 1999 8 14 UIEA99051 1 19990716 A 5311 65B01719502 FRAME BOEING 747 747230B 1384889 NM BS 510 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 507MC 85155 15496 21380 BS 520 RT, FOUND CRACK IN FUSELAGE FRAME AT STR 11 DURING SECTION 41 INSPECTION. CRACK RUNS FROM CUT-OUT TO NEAREST FAS TENER HOLE. REPAIRED FRAME PER ACC KLM DFX 99-124 REV 2. FORM 8110-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999081400207 19990814 00207 1999 8 14 AALA990997 4 19990704 A 2210 2588880901 COUPLER HONEYWELL BOEING 727 727223 1384074 NM AUTOPILOT DEFECTIVE A AALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 07 710AA 81031559 22467 MIA - FLT 0971 - EN ROUTE BNA/MIA, HARD UNCOMMANDED RUDDER KICK TO THE RIGHT, AIRCRAFT ROLLED LEFT AS RESULT, AUTOPILOT DISENGAGED TO RECOVER AIRCRAFT. INCIDENT ONLY OCCURRED ONCE. ALL SUBSEQUENT INDICATIONS NORMAL. FLIGHT 28,000, 300 KN OTS, SMOOTH AIR, KICK RESULTED IN APPROXIMATELY 10 DEGREE ROLL. LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED UPPER AN D LOWER YAW DAMPENER COUPLERS. ACCOMPLISHED ADJUSTMENT TEST OF LOWER AND UPPER RUDDER POWER UNITS. DOWNGRADED TO NOT C AT II. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999081400208 19990814 00208 WP 1999 8 14 AALA991017 1 19990710 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG LACK OF LUBE A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 554AA 53084 DFW - FLT 496 - EN ROUTE ELP/DFW DURING GEAR RETRACTION, CREW HEARD A GRINDING NOISE AND RED NOSE GEAR LIGHT STAYED ILLU MINATED FOR APPROXIMATELY A MINUTE, THEN CYCLED OFF AND ON SEVERAL TIMES BEFORE EXTINGUISHING. CONTINUED ON TO DFW. GE AR EXTENDED NORMALLY. LANDED DFW WITHOUT INCIDENT. LUBED NOSE LANDING GEAR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400209 19990814 00209 WP 1999 8 14 AALA990988 1 19990704 A 3230 39370335503 CYLINDER DOUG DC9 DC982 3022082 WP RT MLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 497AA CPT0325 49735 MIA - FLT 0463 - EN ROUTE PBI/DFW, RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RIGHT GEAR LIGHT ILLUMINATE D WITH YELLOW GEAR DOOR OPEN LIGHT. AIR INTERRUPTED AND LANDED MIA WITHOUT INCIDENT. REPLACED RT MLG BUNGEE CYLINDER P ER MM PROCEDURE. ACCOMPLISHED LANDING GEAR SWING AND LEAK CHECK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400210 19990814 00210 WP 1999 8 14 AALA990996 1 19990706 A 2150 CLAMP DOUG DC9 DC982 3022082 WP ACM BAY DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 223AA 49173 DFW - FLT 0465 - TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON AFER TAKEOFF DFW. REDUCED THRUST ON BOTH ENGINES, LIGH T EXTINGUISHED. RETURNED AND LANDED DFW IWTHOUT INCIDENT. REPLACED TWO BROKEN CLAMPS, ONE ON RIGHT PACK ONE, ON LEFT P ACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400211 19990814 00211 NM 1999 8 14 AALA990962 1 19990628 A 3350 SOCKET GRIMES BOEING 757 757223 1384957 NM EMERGENCY EXIT CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 622AA 24580 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENA NCE FOUND CORROSION ON LIGHT SOCKET. CLEANED CORRODED SOCKET. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400212 19990814 00212 NM 1999 8 14 AALA990961 1 19990628 A 3350 SOCKET GRIMES BOEING 757 757223 1384957 NM R4 DOOR CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 622AA 24580 DFW - DURING OVERNIGHT MAINTENANCE, R4 EXTERIOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTNEANCE FOUND COROSION O N LIGHT SOCKET. CLEANED CORRODED SOCKET AND RELAMPED BULB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400213 19990814 00213 NM 1999 8 14 AALA990977 1 19990701 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 3B LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 3B INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F RT A1NM 1999081400214 19990814 00214 NM 1999 8 14 AALA990978 1 19990701 A 3350 LIGHT BOEING 767 767323 1385205 NM ROWS 25-31 SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AA 25196 DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROWS 25 THROUGH 31 INOPERATIVE. REPLACED SHORTED SEAT MOUNTED LIGHT SOCKET. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999081400215 19990814 00215 NM 1999 8 14 AALA990974 1 19990630 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 647AM 24605 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. RECONNECTED EMERG ENCY EXIT FLOOR PATH LIGHT WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X0 2 L 7 2 4F RT A2NM 1999081400216 19990814 00216 NM 1999 8 14 AALA990981 1 19990702 A 3350 8497934191 LIGHT WEBER BOEING 767 767223 1385123 NM ROW 19AB MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 336AA 22334 LAX - DURING OVERNIGHT MAINTENANCE, SEAT 19AB HAD ONLY ONE RED LIGHT ASSEMBLY FOR EMERGENCY EXIT ESCAPE PATH LIGHTING SY STEM. INSTALLED SECOND EMERGENCY EXIT ESCAPE PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999081400217 19990814 00217 NM 1999 8 14 AALA990979 1 19990630 A 2910 LINE BOEING 767 767223 1385123 NM E/E COMPT LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 301AA 22307 JFK - FLT 0160 - AFTER TAKEOFF, FLIGHT CREW NOTICED AN ELECTRICAL SMELL IN COCKPIT AND FORWARD GALLEY AREA. AIRCRAFT AI R INTERRUPTED AND RETURNED JFK WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC FLUID LEAKING FROM GEAR UP LINE. R EPAIRED HYDRAULIC GEAR UP LINE PER MM PROCEDURES. SYSTEM LEAK AND OPERATIONS CHECKED OK. SYSTEM GROUND CHECKED, NORMAL OPERATIONS. (X) 2 L 7 2 4F RT A1NM 1999081400218 19990814 00218 NM 1999 8 14 AALA990980 1 19990702 A 3350 CONNECTOR BOEING 757 757223 1384957 NM 4L DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 181AN 29591 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT MARKERS AT THE 4L DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PAT H LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400219 19990814 00219 NM 1999 8 14 AALA990982 1 19990702 A 3350 CONNECTOR BOEING 757 757223 1384957 NM 4L DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 181AN 29591 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT MARKERS AT THE 4R DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PAT H LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400220 19990814 00220 NM 1999 8 14 AALA990987 1 19990701 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 606AA 27057 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400221 19990814 00221 NM 1999 8 14 AALA990986 1 19990703 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROWS 20-22 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT ROWS 20 THROUGH 22 INOPERATIVE. REPLACED CONNECTOR AN D BATTERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999081400222 19990814 00222 NM 1999 8 14 AALA991010 1 19990707 A 3350 S283N00219 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 688AA 25730 DFW - DURING OVERNIGHT MAINTENANCE, L2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400223 19990814 00223 NM 1999 8 14 AALA990994 1 19990705 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400224 19990814 00224 EU 1999 8 14 AALA990999 1 19990708 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 90070 513 LHR - DURING OVERNIGHT MAINTENANCE, FIRST CLASS NR 1 OVEN SMOKES AT HIGH TEMPERATURE. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999081400225 19990814 00225 WP 1999 8 14 AALA991000 1 19990707 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 245AA 49257 DFW - DURING OVERNIGHT MAINTENANCE, GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED WIRE ON GALLEY EMERGENCY EXIT SIGN . SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400226 19990814 00226 WP 1999 8 14 AALA991011 1 19990708 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 480AA 49655 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM AFT GALLEY DOOR TO AFT OF AIRCRAFT INOPERATI VE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400227 19990814 00227 WP 1999 8 14 AALA991006 1 19990707 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 418AA 49329 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN TAIL COMPARTMENT CEILING INOPERATIVE. REPAIRED WIRE TO EMER GENCY EXIT LIGHT IN TAIL COMPARTMENT CEILING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400228 19990814 00228 WP 1999 8 14 AALA990989 1 19990704 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 406A 49317 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING UNDER EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GORUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400229 19990814 00229 WP 1999 8 14 AALA990983 1 19990703 A 3350 LIGHT DOUG DC9 DC982 3022082 WP STAIRWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 493AA 49731 ORD - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN VENTRAL STAIRWAY AREA BROKEN. REPLACED EMERGENCY LIGHT IN VENTRAL STAI RWAY AREA. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400230 19990814 00230 NE 1999 8 14 AALA990956 2 19990627 A 7250 5005888021 STATOR VANE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 2 ENGINE FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 218AA 49168 709765 PHL - FLT 317 - DURING CLIMB-OUT AT 33,000 FT, FLT CREW HEARD A LOUD NOISE FROM NR 2 ENG WITH THE EGT PEGGED AT 800 DEGR EES.FLT CREW DECLARED AN EMERGENCY, SECURED NR 2 ENG AND DIVERTED TO PHL. A/C LANDED PHL WITHOUT FURTHER INCIDENT. M X FOUND THE NR 2 ENG TURBINE FAILED. REPLACEDNR 2 ENG, PERFORMED ENG RUN UP. SYSTEM GROUND CHECKED NORMAL OPS. THE 8 TH STAGE STATOR VANE WAS BROKEN AND LIBERATED. THE LIBERATED VANE CAUSED THE DAMAGE TOTHE REST OF THE HPC AND ALL STAGE S OF THE TURBINE. FATIGUE MARKS WERE NOTED ON THE 8TH STAGE STATOR FRACTURE SURFACE BUT DUE TO THE SECONDARY DAMAGE, A N IMPACTINITIATION SITE COULD NOT BE DETERMINED. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999081400231 19990814 00231 NM 1999 8 14 AALA990973 1 19990628 A 2780 114T01151 ROD BOEING 767 767323 1385205 NM RT LE SLAT BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 361AA 24042 DW - FLT 0070 - DURING CLIMB-OUT, SLATS WERE RETRACTED AND A SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. CREW RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE OUTBOARD CONTROL ROD FOR NR 7 SLAT BROKEN. M AINTENANCE REPLACED NR 7 CONTROL ROD AND ADJUSTED/OPERATED SLATS FLAPS SEVERAL TIMES WITH NO MESSAGES OR FAULTS ON FSEU OR PROXIMITY BOX. OVERWEIGHT LANDING WAS ACCOMPLISHED WITH NO ABNORMAL FINDINGS. SYSTEM GROUND CHECKED, NORMAL OPERATI ON. (X) 2 L 7 2 4F RT A1NM 1999081400232 19990814 00232 WP 1999 8 14 AALA990993 1 19990705 A 2131 21171803 CONTROLLER GARRTT 1091109 DOUG DC9 DC982 3022082 WP ACM BAY DEFECTIVE A AALA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 SW 07 234AA 49181 DFW - FLT 0730 - EN ROUTE DFW/LGA CLIMBING THROUGH 28,000 FEET, NO FLOW LIGHT ON WITH CABIN CLIMBING. OXYGEN MASKS WERE DROPPED, AND ACOMPLISHED EMERGENCY DESCENT. RETURNED AND LANDED DFW WITHOUT INCIDENT. ACCOMPLISHED REPLACEMENT OF CAB IN PRESSURE CONTROLLERS AND PERFORMED BITE CHECK. OXYGEN GENERATORS AND MASKS REPLACED. PACK FUNCTION AND LEAK CHECK P ERFORMED WITH START CART. AIR CHECKS GOOD. CHECKED PACK OPERATION WITH ENGINE OPERATING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999081400233 19990814 00233 NM 1999 8 14 AALA991040 1 19990714 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 681AA 25338 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP IN FORWARD CABIN INOPERATIVE. REPLACED EME RGENCY EXIT FLOOR PATH LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999081400241 19990814 00241 WP 1999 8 14 TWAA9911001 1 19990806 A 3397 58541 WIRE DOUG DC9 DC951 3022051 WP ROW 17-21 WORN A TWAA O OTHER L NO TEST CR CRUISE 1 CE 05 405EA 47688 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 3 TO 12, AND ILLUMINATED ALL THE TIME BETWEEN ROWS 17 AND 21. REPLACED THE BROKEN FEEDER MFG 5854-1 FOR THE FORWARD CABIN, AND THE MID CABIN POWER SUPPLY MFG 5822-2 FOR THE MALFUNCTION BETWEEN R OWS 17 AND 21. CHECK-C 3-30-99 STL.- 2 L 7 2 4F RT A6WE 1999081400242 19990814 00242 WP 1999 8 14 TWAA9911002 1 19990808 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP ROW 15-31 INOP A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 922TW 48013 THE EGRESS LIGHTS WERE ON ALL THE TIME FROM CABIN ROWS 15 TO 31. REPLACED THE POWER SUPPLY. CHECK-C 7-17-99 STL. 2 L 7 2 4F A6WE 1999081400243 19990814 00243 EU 1999 8 14 AWXA9900257 1 19990806 A 3260 839902 PROX SENSOR AIRBUS 320 A320231 3930325 EU MLG MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 632AW 81 DECLARED EMERGENCY, LGCIU 1 AND 2 DUAL FAULT AFTER SELECTING LANDING GEAR LEVER DOWN. GEAR INDICATED DOWN AND LOCKED DI D MANUAL GEAR EXTENSION CORRECTIVE ACTION. REMOVED AND REPLACED PROXIMITY SENSOR 32. FOUR WRITE-UPS IN 45 DAYS THIS I S FIRST TIME PARTS CHANGED. 2 L 7 2 4F RT A28NM 1999081400244 19990814 00244 1999 8 14 COMA9960418 2 19990802 A 7261 6010310015 TUBE CNDAIR CL600 CL6002B19 EA RT ENGINE LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 765CA 7131 RIGHT ENGINE OIL PRESSURE WARNING. REPLACED THE OIL SERVICING TUBE ASSY. 2 L 7 2 4F RT A21EA 1999081400245 19990814 00245 1999 8 14 COMA9960419 4 19990805 A 3444 6227209002 RADAR ALT CNDAIR CL600 CL6002B19 EA E&E COMPT MALFUNCTION A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 962CA 8102 7123 RADAR ALTIMETER MESSAGE. REPLACED THE RAC-870 NR 2. 2 L 7 2 4F RT A21EA 1999081400246 19990814 00246 NM 1999 8 14 UPS99230292 1 19990807 A 5320 651986220 CHORD BOEING 727 7271A7C 13840X2 NM BS 303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON NLG MID CHORD BS 303 BS 303 WL 172 RBL 25. CORROSION REMOVED IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. REPLACED NOSE CHORD IAW SRM 51-30-2, 51-30-5 MM 20-20-01 AND SWPM 20-10-11. 2 L 7 3 4F A3WE 1999081400247 19990814 00247 NM 1999 8 14 UPS99230293 1 19990729 A 5320 STIFFENER BOEING 727 7271A7C 13840X2 NM BS 345 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON STIFFENER BS 345 WL 175 RBL 14, HORIZONTAL WALK WAY AREA. CORROSION OUT OF LIMITS SRM 53-10-1. REMOVED AND INSTALLED NEW STIFFENER PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999081400248 19990814 00248 NM 1999 8 14 UPS99230294 1 19990730 A 5711 SPAR CHORD BOEING 727 7271A7C 13840X2 NM WS 510 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C C57-562-02-1B, EXFOLIATION CORROSION ON LW FWD UPPER SPAR CHORD AT WS 510.0 (MARKED), NR 3 SLAT AT TAI TELESCOPING DUCT. CORROSION OUT OF LIMITS PER SRM 57-10-1. REMOVED DAMAGE CHORD FROM FSS 346 TO FSS 642. REPLACEMENT CHORD WILL BE INSTALLED ON NRC 934257. 2 L 7 3 4F A3WE 1999081400249 19990814 00249 NM 1999 8 14 UPS99230295 1 19990802 A 5711 SPAR CHORD BOEING 727 7271A7C 13840X2 NM WS 346-642 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CORROSION C57-562-02-1B, L/W FWD UPPER SPAR CHORD ON HORIZONTAL FLANGE AT NR 4 SLAT ACTUATOR O/B MOUN T ANGLE. CORROSION OUT OF LIMITS PER SRM 57-10-1. REMOVED SECTION FROM FSS 346-FSS 642 FRONT SPAR TO BE REPLACED ON NR C 934257. 2 L 7 3 4F A3WE 1999081400250 19990814 00250 NM 1999 8 14 UPS99230296 1 19990730 A 5315 FLOORBEAM BOEING 727 7271A7C 13840X2 NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, WHILE WORKING CUSTOMER CARD NUMBER 933976 INT 64, FOUND CORROSION ON FLOORBEAM BS 312 LBL 3 WL 208. C ORROSION OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED ALL WORK DONE IAW SRM 51-10-6, 53-10-1, 51-30-5, 51-30-6 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1999081400251 19990814 00251 NM 1999 8 14 UPS99230297 1 19990805 A 5321 FLOOR BOEING 727 7271A7C 13840X2 NM BS 342-351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON DOG HOUSE FLOOR IN A FEW AREAS BS 342 TO 351, WL 169, RBL 14 TO 16. R EMOVED CORRODED FLOOR BS 342 TO 351. FABRICATED NEW FLOOR AND INSTALLED IAW SRM 51-30-05 AND DRG NR 65-18415. 2 L 7 3 4F A3WE 1999081400252 19990814 00252 NM 1999 8 14 UPS99230298 1 19990805 A 5320 STIFFENER BOEING 727 7271A7C 13840X2 NM BS 319 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON STIFFENER BS 319, WL 173 TO 187, RBL 14 HORIZONTAL WALKWAY AREA. REM OVED AND REPLACED STIFFENER IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1999081400253 19990814 00253 NM 1999 8 14 UPS99230299 1 19990805 A 5754 65173807 RIB BOEING 727 7271A7C 13840X2 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CRACKED RIB IN NR 4 SLAT, 2ND RIB I/B OF O/B SLAT TRACK WHERE RIB ATTACHES TO LOWER AFT CHORD. REMOV ED AND REPLACED RIB PER SRM 51-30-7. 2 L 7 3 4F A3WE 1999081400254 19990814 00254 NM 1999 8 14 UPS99230300 1 19990729 A 5320 WEB BOEING 727 7271A7C 13840X2 NM BS 309 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON BONDED DOUBLER ON VERTICAL WEB OF HORIZONTAL WALKWAY BS 309. REMOVED DAMAGED BONDED DOUBLER, FABRICATED NEW BONDED DOUBLER AND INSTALLED IAW SRM 51-10-3, 51-10-6, 51-30-2. 2 L 7 3 4F A3WE 1999081400255 19990814 00255 NM 1999 8 14 UPS99230301 1 19990801 A 5315 FLOORBEAM BOEING 727 7271A7C 13840X2 NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, WHILE WORKING CUSTOMER CARD 933983 INT 71, FOUND CORROSION ON BS 328 FLOORBEAM TOP FLANGE WL 208 AT L BL 7 AND LBL 25. REMOVED DAMAGED AREA ON FLOORBEAM. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-8, 51-10-2, 53 -10-8. 2 L 7 3 4F A3WE 1999081400256 19990814 00256 WP 1999 8 14 UPS99830287 1 19990713 A 5330 561386215 SKIN DOUG DC8 DC873F 302199F WP BS 10 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1, A/C COMPT SKIN AT FS 10 BETWEEN LONGERON 34R AND 33R, HAS A GAP THAT LETS PRESSURIZED AIR ESCAPE AND IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW IAW EO DC8-5330-8942-C. 2 L 7 4 4F RT 4A25 1999081400257 19990814 00257 WP 1999 8 14 UPS99830288 1 19990715 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 140 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 140, LBL 44, THE FLOORBEAM IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK866-902. 2 L 7 4 4F RT 4A25 1999081400258 19990814 00258 WP 1999 8 14 UPS99830289 1 19990716 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 717 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 717, RBL 30, THE FLOORBEAM HAS HEAVY CORROSION. REPAIRED FLOORBEAM IAW DH SK866-291. 2 L 7 4 4F RT 4A25 1999081400259 19990814 00259 WP 1999 8 14 UPS99830290 1 19990716 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C1 FS 879, RBL 12, THE CABIN FLOORBEAM HAS HEAVY CORROSION. REPAIRED FLOORBEAM IAW DH SK866-318. 2 L 7 4 4F RT 4A25 1999081400260 19990814 00260 WP 1999 8 14 UPS99830302 1 19990728 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, FWD LWR FILLET AREA FILLET PNL ATTACH BRACKET CRACKED AT STA 680 LONGERON 31R-32R. FABRICATED AND INSTALLED ANGLE FROM 7075-T6.063. ALUMINUM IAW DC8 S RM 53-8-0, 51-1-20D, AND 53-2-0. 2 L 7 4 4F RT 4A25 1999081400261 19990814 00261 WP 1999 8 14 UPS99830303 1 19990725 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, FWD LWR FILLET AREA, FILLET ATTACH ANGLE CRACKED, STA 680 L31L-L32L. FABRICATED AND INSTALLED ANG LE IAW DC8 SRM 53-2-0, 51-1-20D. 2 L 7 4 4F RT 4A25 1999081400262 19990814 00262 WP 1999 8 14 UPS99830304 1 19990728 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, RIB CRACKED AT FASTENER AND FASTENER WORKING UNDER RT FWD LOWER FILLET PANEL STA 822 X-55. FABRIC ATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-0 AND 51-1-21. 2 L 7 4 4F RT 4A25 1999081400263 19990814 00263 WP 1999 8 14 UPS99830305 1 19990729 A 5240 SKIN DOUG DC8 DC873F 302199F WP RT SERVICE DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, INNER SKIN GOUGED ON RT FWD SERVICE DOOR, AT AFT UPPER CORNER, ADJACENT TO LIGHTENING HOLE. FABRI CATED AND INSTALLED DOUBLER, ATTACH ANGLE AND TWO FILLERS IAW DC8 SRM 52-2-3, 52-3-1 FIG 1, 51-9-0 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999081400264 19990814 00264 WP 1999 8 14 UPS99830306 1 19990729 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 804 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, RW OUTBOARDB LE RIB CRACKED AT LWR AFT END STA XFS 804. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 FIG 2, AND 51-1- 21. 2 L 7 4 4F RT 4A25 1999081400265 19990814 00265 WP 1999 8 14 UPS99830307 1 19990729 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 579 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, R/W O/B CTR L/E STA XFS 579 RIB CRACKED AT UPPER AFT END. FABRICATED AND INSTALLED DOUBLER IAW DC 8 SRM 57-2-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999081400266 19990814 00266 WP 1999 8 14 UPS99830308 1 19990729 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, R/W O/B CTR L/E STA XFS 622 RIB CRACKED AT LWR AFT END. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999081400267 19990814 00267 WP 1999 8 14 UPS99830309 1 19990729 A 5313 LONGERON DOUG DC8 DC873F 302199F WP WS 1340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C123, AFT PIT STA 1340 L27R CORRODED. FABRICATED AND INSTALLED NEW LONGERON SECTION AND NEW SPLICE P/N DC8 -53B-900-3 IAW DC8 SRM 53-2-2, 51-1-24 AND 51-1-21D. 2 L 7 4 4F RT 4A25 1999081400268 19990814 00268 WP 1999 8 14 UPS99830310 1 19990806 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 874UP 46074 EMERGENCY EXIT LIGHT SWITCH WAS FOUND ON, BATTERY FOUND DEAD. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK. OPS CK GOO D. WORK IAW MM 33-50-01 PN ON AND OFF 5708458-503 SN ON 10886 OFF 10382. 2 L 7 4 4F RT 4A25 1999081400269 19990814 00269 EU 1999 8 14 QXEA9901533 1 19990805 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 SEA-MID- CABIN EXIT LIGHT NOT FULLY ILLUMINATED. REPLACED BOTH CIRCUIT BOARDS AT MID CABIN EXIT LIGHT. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999081400270 19990814 00270 EU 1999 8 14 QXEA9901534 1 19990806 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 GEG - EXIT SIGN ABOVE COCKPIT DOOR HAS BURNED OUT LIGHT BULBS. REPLACED EXIT SIGN. OPERATIONAL CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999081400271 19990814 00271 EU 1999 8 14 QXEA9901535 1 19990806 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 GEG - EXIT SIGN OVER COAT CLOSET HAS BURNED OUT BULB. REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 1999081400272 19990814 00272 EU 1999 8 14 99FDEA00316 1 19990805 A 3230 SENSOR AIRBUS 300 A300F4605R 3930327 EU LANDING GEAR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 668FE 772 99-195 - GEAR WOULD NOT RAISE WITH INTERLOCK WARNING SWITCH TO SYS 2, GEAR RAISED, LOST NR 1 PITCH TRIM, AUTO THROTTLES, AUTOPILOT, NR 1 PRESS REG. REMOVED AND REPLACED 64GB SENSOR, 32-00-00-4 AND OPS CK 32-00-00-5 AFS LAND TEST PASSED, 22 -00-00-5. 2 L 7 2 4F RT A35EU 1999081400273 19990814 00273 NM 1999 8 14 99FDEA00317 1 19990806 A 2612 2240153503 FIRE LOOP DOUG MD11 MD11F 3023600 NM NR 2 ENGINE FAILED A FDEA A F E UNSCHED LANDING ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 605FE 48514 99-196- WHILE CLIMB, ENG NR 2 FIRE ALERT WARNING ACTIVATED. ENG SHUTDOWN IAW FLT MANUAL. NR 2 FIRE AGENT DISCHARGED. R EMOVED AND REPLACED UP RT FIRE DET ASSY A, HARNESS OF DH4 TO DH23, DH22 TO DH7, AND DH7 TO DH8 FOR MAINT PREVENTION PER MD-11. RUN ENG WITH HI PWR ALL COND NML. 2 L 7 3 4F RT A22WE 1999081400274 19990814 00274 WP 1999 8 14 99FDEA00318 1 19990808 A 5753 FLAP DOUG DC10 DC1010F 3022111 WP TE FLAPS SEPERATED A FDEA K NONE D F INFLIGHT SEPARATION FLT CONT AFFECTED AP APPROACH 1 SO 25 58FE 46705 99-197 - FINAL APPROACH LOUD JOLT WAS FELT WITH FLAPS SEL AND IND 50 (PF) F/O REPORT SOME CONTROL PROB WILL NEED FOR EXC ESSIVE RT AILERON. A/C S/N 46705, FUS NR 33, REG NR N68058 HAS BEEN REPAIRED. 2 L 7 3 4F A22WE 1999081400275 19990814 00275 WP 1999 8 14 ABXA9900629 1 19990806 A 5330 591142739 SKIN DOUG DOUG DC9 DC941 302207N WP BS 1065 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND SKIN AFT OF STATION 1065 BELOW LONGERON 14 RIGHT CRACKED. REPAIRED SKIN IAW ABX REA D953-32592 MR . 2 L 7 2 4F A6WE 1999081400276 19990814 00276 WP 1999 8 14 ABXA9900630 1 19990803 A 5320 4921787 BRACKET DOUG DOUG DC9 DC933F 302207A WP CARGO DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND MAIN CARGO DOOR LOWER JAMB BRACKET CORRODED. REPLACED BRACKET IAW DC9 SRM 51-10-04. 2 L 7 2 4F A6WE 1999081400277 19990814 00277 WP 1999 8 14 ABXA9900631 1 19990803 A 5320 991073415 WEB DOUG DOUG DC9 DC933F 302207A WP BS 313 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED AT STATION 313 RBL 49. REPAIRED IAW DC9 SRM 53-01-00. 2 L 7 2 4F A6WE 1999081400278 19990814 00278 WP 1999 8 14 ABXA9900632 1 19990804 A 5311 5616734513 FRAME DOUG DOUG DC8 DC862 3021970 WP BS 1114.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 804AX 45987 CHANNEL FRAME CRACKED AT STATION 1114.5 FRAME AT NR 3 CARGO COMPARTMENT DOOR JAMB. REPAIRED IAW ABX REA D853-31931MR. 2 L 7 4 4F 4A25 1999081400279 19990814 00279 WP 1999 8 14 ABXA9900633 1 19990712 A 5320 3755822501 FITTING DOUG DOUG DC8 DC863 302198A WP BS 320 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FITTING CORRODED AT STATION 320 BETWEEN LONGERONS 35 AND 36 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1999081400280 19990814 00280 WP 1999 8 14 ABXA9900634 1 19990628 A 5730 57696005 SKIN DOUG DOUG DC8 DC863 302198A WP WS 710 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE STATION XFS 710, TOP SKIN CRACKED. REPAIRED IAW DC8 SRM 57-2-1 AND DWG 5679600. 2 L 7 4 4F 4A25 1999081400281 19990814 00281 NM 1999 8 14 SCNA99099 1 19990802 A 3350 BULB BOEING 727 727225 1384077 NM EMER EXIT FAILED A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 282SC 22558 DURING LINE MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT LIGHT BULB WAS FOUND BROKEN. REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHT LENS AND BULB. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999081400282 19990814 00282 NM 1999 8 14 VNAA9907008 1 19990727 A 3350 321473 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 4LK FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 460PS 10408 11255 3061 DURING THE PRE-FLIGHT INSPECTION, A SECTION OF EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY POWER SUPPLY, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WE RE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999081400283 19990814 00283 NM 1999 8 14 TC8A99022 1 19990807 A 3411 UNION BOEING 727 72721C 138400M NM RT PITOT SYS FAILED A TC8A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 705A 19134 AFTER TAKEOFF, CAPT AND FIRST OFFICER AIRSPEED INDICATOR DIFFERENCE OF 50 KTS (FIFTY KNOTS). RETURN TO FIELD. INSPECTE D F/O'S PITOT SYSTEM, REMOVED AND REPLACED UNION AT F/O'S PITOT PROBE. PERFORMED FULL RANGE PITOT STATIC LEAK CHECK IN ACCORDANCE WITH B727 MM 36-11-0 AND FAR PART 43 APPENDIX E, NO LEAKS NOTED. F/O'S AIRSPEED INDICATOR OPS CHECKS NORMAL IAW B727 MM 36-11-0. 2 L 7 3 4F A3WE 1999081400284 19990814 00284 NM 1999 8 14 TC8A99023 1 19990807 A 3411 PITOT TUBE BOEING 727 72721C 138400M NM RIGHT OBSTRUCTED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 705A 19134 ON TAKEOFF ROLL, CAPT AIRSPEED ALIVE BY 70 KNTS, FIRST OFFICER 0 KTS. ABORT AT 78 KTS IN ACCORDANCE WITH TRANSCONTINENT AL PROCEDURE. NORMAL TAXI IN. REMOVED PITOT LINE FROM AIRSPEED INDICATOR, CAPPED PITOT LINE AT MACH SPEED SWITCH. PRE SSURIZED F/O'S PITOT FROM COCKPIT TO PITOT TUBE. REMOVED OBSTRUCTION FROM F/O'S PITOT SYSTEM. RECONNECTED LINE AT MACH SPEED SWITCH AND AT AIRSPEED INDICATOR. PERFORMED PITOT STATIC TEST IAW B727 MM 36-11-0 AND FAR PART 43 APPENDIX E. A LL SYSTEMS FUNCTIONALLY CHECK NORMAL. 2 L 7 3 4F A3WE 1999081400285 19990814 00285 NM 1999 8 14 HNAA9900109 1 19990806 A 3350 1013073 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOP A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 917HA 075 FLOOR EMERGENCY LIGHT 5TH LIGHT AFT IS INOP. REMOVED AND REPLACEDD LIGHT ASSY. 2 H 7 2 4T RT A13NM 1999081400286 19990814 00286 WP 1999 8 14 AT9900551 1 19990805 A 5350 CABLE DOUG DC9 DC932 3022066 WP TAIL CONE DISCONNECTED A ZZDA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 15 802AT 47177 TAILCONE UNSAFE LIGHT CAME ON AFTER TAKEOFF. RETURNED TO ATLANTA. RE-INSERTED CABLE BALL END INTO TAILCONE RELEASE HAN DLE IAW MM 52-21. RII ACCOMPLISHED. 2 L 7 2 4F A6WE 1999081400287 19990814 00287 SO 1999 8 14 RAAA99E8050 1 19990802 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO EMER EXIT DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1999081400288 19990814 00288 WP 1999 8 14 CALA9900989 1 19990805 A 3297 WIRE DOUG DC9 DC982 3022082 WP NLG SENSOR LOOSE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14814 49112 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF FROM IAH. THE GEAR HANDLE WAS EXTE NDED, BUT THE LIGHT REMAINED ON WITH THE GEAR DOOR OPEN LIGHT ILLUMINATING INTERMITTENTLY. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WIRE PULLED FROM PIN AT CONNECTOR R5-1156. THE CONNECTOR WAS R EPLACED. THE NOSE GEAR WAS SWUNG AND OPERATION CHECKED GOOD IAW MM 32-60-05. 2 L 7 2 4F A6WE 1999081400289 19990814 00289 WP 1999 8 14 CALA9900990 1 19990805 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND A .25 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN AFT EDGE BETWEEN 2ND AND 3RD STOPS FROM BOTTOM. THE CRAC K WAS ROUTED OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-10-1 AND ECRA 5330-02819. 2 L 7 2 4F A6WE 1999081400290 19990814 00290 NM 1999 8 14 CALA9900991 1 19990805 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLES AND EDGES AT STA 986.5. A NEW SECTION OF FLOORBEAM WAS INSTA LLED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999081400291 19990814 00291 WP 1999 8 14 CALA9900992 1 19990805 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND VERTICAL STIFFENER ATTACHED TO FLOOR PAN AND EPC PANEL CORRODED AT STA 160, LBL 10 TO LBL 40. THE STIF FENER WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999081400292 19990814 00292 WP 1999 8 14 CALA9900993 1 19990805 A 5753 NRC6062512 SKIN DOUG DC10 DC1030 3023501 WP RT TE FLAP VANE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND RT WING I/B FLAP VANE UPPER SKIN WORN. THE FLAP VANE WAS REPLACED IAW MM 27-50-03. 2 L 7 3 4F A22WE 1999081400293 19990814 00293 WP 1999 8 14 CALA9900994 1 19990805 A 5320 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LAV FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 1338, LBL 58 TO RBL 58. THE FLOORBEAM WAS RE MOVED AND REPLACED IAW SRM 51-10-3, 51-30-2, 51-30-5, AND 51-10-4. 2 L 7 2 4F A6WE 1999081400294 19990814 00294 WP 1999 8 14 CALA9900995 1 19990805 A 5753 NRC6062519 SKIN DOUG DC10 DC1030 3023501 WP LT TE FLAP VANE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND LEFT WING I/B FLAP VANE EXTERNAL SKIN DENTED. THE FLAP VANE WAS REMOVED AND REPLACED IAW MM 27-50-03. 2 L 7 3 4F A22WE 1999081400295 19990814 00295 WP 1999 8 14 CALA9900996 1 19990805 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-256 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND SEAT TRACK CORRODED AT STA 200-256, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIG URE 4F, 51-30-01, AND 51-30-05. 2 L 7 2 4F A6WE 1999081400296 19990814 00296 NM 1999 8 14 CALA9900997 1 19990805 A 5320 SHEAR WEB BOEING 727 727224 1384076 NM BS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND AFT CABIN SHEAR WEB CORRODED JUST FORWARD OF BS 1183, LBL 17 TO RBL 17. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-10-7, PAGE 4. 2 L 7 3 4F A3WE 1999081400297 19990814 00297 WP 1999 8 14 CALA9900998 1 19990805 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200-256 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 200-256, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INST ALLED IAW SRM 51-30-2, 51-30-5, AND 53-11-1, FIGURE 14. 2 L 7 2 4F A6WE 1999081400298 19990814 00298 WP 1999 8 14 CALA9900999 1 19990805 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1117 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LOWER LIP OF FRAME CORRODED IN AFT PIT AT STA 1117 FROM LONGERON 28L TO 28R. A REPAIR WAS INSTALLED IA W SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1999081400299 19990814 00299 NM 1999 8 14 CALA9901000 1 19990805 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 44. THE CORRODED AREA WAS CUT OUT. A REPAIR DOUBLER AND FILLER WAS INSTALLED IAW SRM 53-10-8, 51-30-2, AND 51-10-6. 2 L 7 3 4F A3WE 1999081400300 19990814 00300 NM 1999 8 14 CALA9901001 1 19990805 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1138 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1138, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTAL LED IAW SRM 51-10-1, PAGE 4 AND 51-30-2, PAGE 2. 2 L 7 3 4F A3WE 1999081400301 19990814 00301 NM 1999 8 14 CALA9901002 1 19990805 A 5720 ANGLE BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A 4.5INCH CRACK IN UPPER T-ANGLE ABOVE WHERE RT O/B AILERON I/B HINGE BRACKET ATTACHES AT RT WING T/E R IB. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-01, PAGE 401 AND 51-30-2. 2 L 7 3 4F A3WE 1999081400302 19990814 00302 NM 1999 8 14 CALA9901003 1 19990805 A 5320 WEB BOEING 727 727224 1384076 NM BS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND TOP OF WEB CORRODED AT STA 1183, LBL 14. THE CORRODED AREA WAS CUT OUT AND A NEW WEB WAS INSTALLED IAW SRM 51-40-2, PAGE 6, FIGURE 1. 2 L 7 3 4F A3WE 1999081400303 19990814 00303 NM 1999 8 14 CALA9901004 1 19990805 A 5720 ANGLE BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND TWO .5 INCH CRACKS THROUGH BOLT HOLES AT O/B LOWER ANGLE INSIDE RT WING FIXED LEADING EDGE RIB, WBL 92. 0 (AFT OF NR 4 L/E FLAP I/B END). THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 2, 51-40-3, PAGE 1, AND 51-20-2, PAGE 1. 2 L 7 3 4F A3WE 1999081400304 19990814 00304 WP 1999 8 14 CALA9901005 1 19990805 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 215-225 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED FROM STA 215-225, LBL 54. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIGU RE 4F. 2 L 7 2 4F A6WE 1999081400305 19990814 00305 WP 1999 8 14 CALA9901006 1 19990805 A 5512 SKIN DOUG DC9 DC982 3022082 WP LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND TWO 1 INCH CRACKS IN LEFT L/E HORIZONTAL STABILIZER I/B SECTION ON L/E SIDE AT STA XHS 9.652. THE CRAC KS WERE STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND ECRA 5510-01458. 2 L 7 2 4F A6WE 1999081400306 19990814 00306 WP 1999 8 14 CALA9901007 1 19990805 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1332 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LAV FLOORBEAM CORRODED AT STA 1332, LBL 58 TO RBL 58. THE FLOORBEAM WAS REPAIRED IAW SRM 53-08, FIGURE 2. 2 L 7 2 4F A6WE 1999081400307 19990814 00307 NM 1999 8 14 CALA9901008 1 19990805 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 10 TO RBL 25. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999081400308 19990814 00308 NM 1999 8 14 CALA9901009 1 19990805 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AROUND NUT PLATE HOLES AT STA 947.5, LBL 15 TO RBL 8. THE FLOORBEAM WAS R EMOVED AND REPLACED IAW SRM 53-00-51, PAGE 207-209. 2 L 7 2 4F RT A16WE 1999081400309 19990814 00309 WP 1999 8 14 CALA9901010 1 19990805 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 339 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT FORWARD AVIONICS COMPARTMENT DOOR CUTOUT, LEFT FORWARD CORNER AT FRAME 33 9. 2 L 7 3 4F A22WE 1999081400310 19990814 00310 WP 1999 8 14 CALA9901011 1 19990805 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1155-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND AFT CARGO SUPPORT TRACK CORRODED ON UPPER AND LOWER SIDE AT FS 1155-1231, LBL 24. THE TRACK WAS REMOVE D IAW SRM 51-30-1. A NEW TRACK WAS INSTALLED IAW SRM 51-10-1, 51-10-4, 51-10-3, AND 51-30-1. 2 L 7 2 4F A6WE 1999081400311 19990814 00311 WP 1999 8 14 CALA9901012 1 19990805 A 5320 FRAME DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND AFT CARGO CEILING FRAME AND SUPPORT CORRODED AT FS 1174, RBL 1. THE CORROSION WAS REMOVED IAW SRM 51-1 0-3 AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 86. 2 L 7 2 4F A6WE 1999081400312 19990814 00312 WP 1999 8 14 CALA9901013 1 19990805 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND CENTER CARGO DOOR EXTERNAL SKIN CHAFED AT LOWER FORWARD CORNER. THE DOUBLER ON CENTER CARGO DOOR WAS R EMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1999081400313 19990814 00313 WP 1999 8 14 CALA9901014 1 19990805 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND ELECTRONIC WALL SUPPORT CORRODED AT STA 160, LBL 16. THE CORROSION WAS REMOVED IAW SRM 51-10-3. A REP AIR WAS INSTALLED IAW SRM 51-30-2 AND ECRA 5320-01589. 2 L 7 2 4F A6WE 1999081400314 19990814 00314 WP 1999 8 14 CALA9901015 1 19990805 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 140-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 140-200, RBL 6. THE CORROSION WAS REMOVED IAW SRM 51-10-03. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11 AND 51-30-1. 2 L 7 2 4F A6WE 1999081400315 19990814 00315 WP 1999 8 14 CALA9901016 1 19990805 A 5511 RIB DOUG DC9 DC982 3022082 WP HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A 1.2 CRACK IN HORIZONTAL STABILIZER LEFT L/E PANEL I/B RIB AT XFS 77. THE RIB WAS REMOVED AND A NEW R IB WAS INSTALLED IAW SRM 51-30-05. 2 L 7 2 4F A6WE 1999081400316 19990814 00316 WP 1999 8 14 CALA9901017 1 19990805 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBEAM WEB CORRODED AT FS 1338 BETWEEN RBL 45 AND LBL 45. THE CORROSION WAS REMOVED IAW SRM 51-10-3 . A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5310-03888 AND SRM 51-10-3. 2 L 7 2 4F A6WE 1999081400317 19990814 00317 WP 1999 8 14 9903049979 1 19990804 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMPT INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999081400318 19990814 00318 WP 1999 8 14 9903059864 1 19990805 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 773NC 47775 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY ESCAPE PATH AND FORWARD GALLEY EXIT SIGN LIGHTS INOPER ATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999081400319 19990814 00319 WP 1999 8 14 9903069997 1 19990730 A 3397 WIRE DOUG DC9 DC931 3022065 WP ROW 1-2 DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SERVICE DOOR AND FORWARD CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. MAI NTENANCE FOUND WIRES BETWEEN ROWS 1 AND 2 PINCHED IN SEAT TRACK SHORTING OUT. REPAIRED WIRING AND REPLACED BATTERY POWE R SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999081400320 19990814 00320 WP 1999 8 14 9903079997 1 19990731 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP ROW 1-4 DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 8933E 47142 FORWARD CABIN EMERGENCY FLOOR LIGHTING INTERMITTENT. REPLACED BATTERIES IN PACK FOR ESCAPE PATH LIGHTING AT ROWS 1 THRU 4, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999081400321 19990814 00321 NM 1999 8 14 UPS99230277 1 19990805 A 2750 RETRACT MECH BOEING 727 72731C 1384011 NM TE FLAPS INOP A IPXA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 922UP 19231 FLAPS FAILED TO DEPLOY. 2 L 7 3 4F A3WE 1999081400322 19990814 00322 NM 1999 8 14 UPS99530281 1 19990805 A 3230 273N10051 ACTUATOR BOEING 757 75724APF 1384969 NM PW2040 NLG UPLOCK FAILED A IPXA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 01 412UP 23852 AT GEAR EXTENSION, NOSE GEAR NOT DOWN MESSAGE DISPLAYED ON EICAS ALONG WITH GEAR DISAGREE AND GEAR DOOR MSGS. ALSO, GEA R AND DOOR AMBER LIGHTS REMAINED ILLUMINATED. ALTERNATE GEAR EXTENSION RESULTED IN SAME INDICATION. REPLACED NOSE LAN DING GEAR DOWNLOCK ACTUATOR AND TESTED PER M/M. 2 L 7 2 4F RT A2NM 1999081400323 19990814 00323 WP 1999 8 14 UPS99830153 1 19990723 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 MAINTENANCE FOUND LEFT WING LOWER SURFACE, APPROX 16 INCHES INBOARD OF NR 1 PYLON, CRACKED SKIN APPROX 4 INCHES LONG. R OUTED OUT CRACKED AREA IAW REO-06635. FABRICATED FILLER, INTERNAL DOUBLERS AND TRIPLERS, EXTERNAL DOUBLER AND TRIPLER I AW REO-O6635. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 81-1-20D AND REO-O6635. 2 L 7 4 4F RT 4A25 1999081400324 19990814 00324 NM 1999 8 14 QXEA9901532 1 19990804 A 6120 8210286 PROP CONTROL DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTION A QXEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 09 345PH 476 YVR - UPON ADVANCING POWER LEVERS FOR TAKEOFF, NR 2 ENGINE EXPERIENCED A UNSCHEDULED FEATHERING OF THE PROPELLER. ABORT ED TAKEOFF AND RETURNED TO THE GATE. AIRCRAFT WAS FERRIED FROM YVR-PDX FOR REPAIRS. FDR WAS DOWNLOADED AND NR 2 TORQUE CONFIRMED TO BE 150 PERCENT. ADJUSTED ARM OF SWITCH 6141S4, REPLACED BOTH PROP CONTROL UNITS, RIGGED DOWNLOAD SWITCHES 6141S3 AND 6141S4. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999081400325 19990814 00325 WP 1999 8 14 ABXA9900627 1 19990803 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DEPLETED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1999081400326 19990814 00326 NE 1999 8 14 ABXA9900628 2 19990803 A 7200 ENGINE PWA DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 4 DEFECTIVE A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 852AX 46016 669523 DURING CLIMB, NR 4 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 35-50 PSI. OIL QUANTITY DROPPED TO .4 GALLONS. OIL TEMPERATU RE WAS 125 DEGREES C. SHUT NR 4 ENGINE DOWN. AFTER SHUT DOWN, OIL PRESSURE FLUCTUATED BETWEEN 15-20 PSI. REPLACED NR 4 ENGINE IAW ABX WORK CARD DC8 8090507. 2 L 7 4 4F 4 F 4A25 1E8 1999081400327 19990814 00327 WP 1999 8 14 MWEA99453 1 19990801 A 2560 113317 GAUGE DOUG DC9 DC932 3022066 WP GALLEY DOOR OUT OF POSITION A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 203ME 47673 PRESSURE GAUGE ON GALLEY SLIDE VERY DIFFICULT TO SEE. REPOSITIONED GALLEY SLIDE. 2 L 7 2 4F A6WE 1999081400328 19990814 00328 WP 1999 8 14 MWEA99454 1 19990728 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 209ME 47730 THE LEFT EMERGENCY OVERWING EVACUATION LIGHT FAILED 20 MINUTE BURN. MAINTENANCE REMOVED AND REPLACED LEFT EMERGENCY OVE RWING EVACUATION LIGHT BATTERY PACK BATTERIES. 2 L 7 2 4F A6WE 1999081400329 19990814 00329 WP 1999 8 14 MWEA99455 1 19990727 A 5230 3926046501 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INTERCOSTAL T FITTING CRACKED AT LOWER AFT DOOR STOP ON FORWARD CARGO DOOR. MAINTENANCE FABRICATED AND INSTALLED NEW FI TTING. 2 L 7 2 4F A6WE 1999081400330 19990814 00330 WP 1999 8 14 MWEA99456 1 19990728 A 5400 991555517 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 UPPER AND LOWER RIB ANGLES AT STATION XN 61-410 IN LEFT PYLON IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED REPAIR A NGLES. 2 L 7 2 4F A6WE 1999081400331 19990814 00331 WP 1999 8 14 MWEA99457 1 19990729 A 5312 59101303 BULKHEAD SKIN DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LOWER LEFT CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB OPENING IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED D OUBLER REPAIR. 2 L 7 2 4F A6WE 1999081400332 19990814 00332 WP 1999 8 14 MWEA99459 1 19990728 A 2560 113317 GIRT BAR DOUG DC9 DC932 3022066 WP PAX DOOR DIRTY A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 215ME 47744 GIRT BAR FOR THE FORWARD ENTRY DOOR WON'T STAY ARMED. CLEANED GIRT BAR HOLDERS. 2 L 7 2 4F A6WE 1999081400333 19990814 00333 WP 1999 8 14 MWEA99460 1 19990730 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP PAX DOOR DEVECTIVE A MWEA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 215ME 47744 EMERGENCY LIGHT MAIN CABIN DOOR WILL NOT TURN ON BY ITS OWN ON/OFF SWITCH, BUT WILL TURN ON BY COCKPIT OVERHEAD SWITCH. REPLACED EMERGENCY LIGHT. 2 L 7 2 4F A6WE 1999081400334 19990814 00334 WP 1999 8 14 MWEA99461 1 19990731 A 5330 5910228189 SKIN DOUG DC9 DC914 3022034 WP AFT FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 2 INCH CRACK IN LEFT AFT FUSELAGE SKIN AFT OF OUTER EMERGENCY TAILCONE RELEASE HANDLE. MAINTENANCE FABRICATED AND INSTA LLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999081400335 19990814 00335 WP 1999 8 14 MWEA99463 1 19990801 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP EMER EXIT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 BOTH AFT LEFT AND RIGHT OVERWING EXIT EMERGENCY LIGHTING WILL NOT TEST. REPLACED EMERGENCY CEILING BATTERY PACK. 2 L 7 2 4F A6WE 1999081400336 19990814 00336 WP 1999 8 14 MWEA99452 1 19990801 A 5320 9919402505N TRAP PANEL DOUG DC9 DC914 3022034 WP LT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 CRACKED TRAPEZOIDAL PANEL STATION 604 LEFT WHEEL WELL. INSTALLED NEW TRAPEZOIDAL PANEL AND STRAP. 2 L 7 2 4F A6WE 1999081400337 19990814 00337 WP 1999 8 14 MWEA99458 1 19990728 A 5412 99581605 FIREWALL DOUG DC9 DC932 3022066 WP LT PYLON GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 LEFT PYLON FIREWALL UPPER CAP IS GOUGED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999081400338 19990814 00338 SO 1999 8 14 SWIA971530 1 19990707 A 3610 DUCT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE LEAKING A SWIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 563SW 120338 DUCT LEAK LIGHT ILLUMINATED IN FLIGHT. FOLLOWED QRH INSTRUCTIONS AND DUCT LEAK LIGHT EXTINGUISHED. RETURNED TO LAX. R EPOSITIONED CLAMP AT HEAT EXCHANGER INLET. RAN LEFT ENGINE AT MAXIMUM RPM IN AUTO/NORM WITH BLEED AND PACKS ON. OPS CH ECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081400339 19990814 00339 SO 1999 8 14 SWIA971531 1 19990707 A 3610 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 563SW 120338 LEFT BLEED DUCT LEAK LIGHT ILLUMINATED IN FLIGHT. FOLLOWED QRH PROCEDURES BUT DUCT LEAK LIGHT REMAINED ON. SHUT DOWN L EFT ENGINE AS PER QRH. RETURNED TO LAX. DUPLICATED PROBLEM ON GROUND AFTER 5 MINUTES AT CLIMB POWER. REPLACED LT 18 P SI REGULATOR. RAN AT CLIMB POWER FOR 15 MIN. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081400340 19990814 00340 SO 1999 8 14 SWIA971532 1 19990701 A 6120 PCU EMB 120 EMB120RT SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 07 271YV 120271 RIGHT ENGINE AUTO FEATHERED ON CLIMB-OUT. RETURNED TO SFO. REMOVED AND REPLACED PCU IAW MM 61-21-00. ALSO, CHANGED TO RQUE SIGNAL CONDITIONER. CHANGED RIGHT ENGINE DUE TO OVER-TORQUE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081400341 19990814 00341 SO 1999 8 14 SWIA971533 1 19990801 A 2750 FCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 07 294SW 120321 DURING GO-AROUND, FLAPS WERE SELECTED UP. FLAP LIGHT ON MAP AND DISAGREEMENT ON FLAP PANEL. INBOARD FLAPS DID NOT RETR ACT. FOLLOWED QRH PROCEDURE. LEFT FLAPS AT 150. ON GROUND FLAPS WORKED FINE. INSPECTED INBOARD FLAPS FOR DEFECTS. N ONE FOUND. RERACKED FCU. OPERATED FLAPS FOR SEVERAL CYCLES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081400342 19990814 00342 1999 8 14 SWIA971534 4 19990701 A 3442 RADAR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT INOP A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 203SW 120240 WEATHER RADAR INOP IN FLIGHT. PAINTS 2-3 BANDS ACROSS DISPLAY IN 10-25 MILE RANGE. RETURNED TO SLC. TESTED RADAR. WE ATHER AND MAP CHECKS GOOD. NO BANDS IN DISPLAY. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081400343 19990814 00343 NE 1999 8 14 SWIA971535 2 19990801 A 7320 7863904 HMU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 188SW 120039 TORQUE ON LEFT ENGINE FLUCTUATED AND THEN DROPPED OFF TO 26 PERCENT TORQUE ACCOMPANIED BY FUEL FLOW FLUCTUATION. PERFOR MED PRECAUTIONARY ENGINE SHUTDOWN. RETURNED TO SLC. REMOVED AND REPLACED LEFT ENGINE HMU IAW RII 73-301 AND MM 73-21-0 0. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999081400396 19990814 00396 CE 1999 8 14 99ZZZX2959 1 19990714 A 3222 BR1916 BEARING CESSNA 310 310P 2074238 CE NLG LACK OF LUBE A P DKBA K NONE O OTHER IN INSP/MAINT 1 SO 09 5817M 2588 310P0117 BEARING HAD LOST LUBRICANT AND STARTED TO CEASE. ONE STYLE BEARING HAS PROVISION FOR A LUBE FITTING, P/N 408420072, 1.3 1 INCH DIAMETER TRUNNION. THIS DIAMETER BEARING 1.19 INCH REQUIRES REMOVAL OF THE NOSE GEAR TO LUBE. 1 L 7 2 3O 3A10 1999081400397 19990814 00397 WP 1999 8 14 TWAA9911101 1 19990808 A 3350 58531 CABLE DOUG DC9 DC934 302207E WP FWD CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 936L 47711 THE FIRST SECTION OF EGRESS LIGHTS IN THE COACH CABIN WERE INOPERATIVE. REPLACED THE FEEDER STRIP. CHECK-C 6-17-98 STL . 2 L 7 2 4F RT A6WE 1999081400398 19990814 00398 WP 1999 8 14 TWAA9911102 1 19990807 A 3244 446K822 TIRE DOUG DC9 DC983 3022083 WP LT MLG FAILED A TWAA A UNSCHED LANDING D K J INFLIGHT SEPARATION FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 05 9306T 49567 DURING TAKEOFF AT SJC, THE NUMBER 1 TIRE COMPLETELY SEPARATED FROM THE WHEEL, CAUSING FAILURE OF THE RH HYDRAULIC SYSTEM . DURING THE LANDING AT SFO THE NUMBER 2 TIRE SEPARATED FROM THE WHEEL. INSPECTION OF THE AIRCRAFT FOUND OTHER DAMAGE CAUSED BY THE TIRE FAILURES, INCLUDING THE LT ENGINE FAN, NOSE COWL, AND ENGINE CASE. BOTH TIRES WERE REPLACED AND THE DAMAGE CORRECTED. CHECK-C 3-12-99 STL. 2 L 7 2 4F RT A6WE 1999081400399 19990814 00399 NM 1999 8 14 TWAA9911103 1 19990809 A 3297 WIRE BOEING 727 727231 1384079 NM GEAR HANDLE FAILED A TWAA K NONE O OTHER TO TAKEOFF 1 CE 05 54336 20490 UNABLE TO RAISE, THE GEAR HANDLE AFTER TAKEOFF AT JFK WAS NECESSARY TO TO USE THE OVERRIDE LEVER LATCH TO RAISE THE GEAR . FOUND WIRE W31203922 WAS OPEN. SPLICED THE WIRE. REF WDM 32-31-01 PAGE 1. CHECK-C 10-29-98 MCI. 2 L 7 3 4F A3WE 1999081400400 19990814 00400 WP 1999 8 14 TWAA9911104 1 19990730 A 5320 WEB DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINTENANCE CHECK, FOUND RT MLG WHEEL WELL CRACKED AT AFT INBD CORNER OF RT MLG WHEEL WELL, 30 INCHES FROM CABIN FLOOR. STOP DRILLED CRACK AND REPAIRED PER SRM 53-01 PAGE 10. INSTALLED FASTENERS PER SPM 6-30-07. 2 L 7 2 4F A6WE 1999081400401 19990814 00401 WP 1999 8 14 TWAA9911105 1 19990802 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 945 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINTENANCE CHECK, AFT CARGO AREA STATION 945, BETWEEN LEFT LONGERON NR 29 AND NR 30, FRAME ANGLE SPLICE WA S CRACKED AT A RIVET. REPLACED ANGLE WITH NEW PART PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999081400402 19990814 00402 WP 1999 8 14 TWAA9911106 1 19990802 A 5210 WEB DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINTENANCE, AFT PASSENGER DOOR WAS CRACKED AT PAN, FWD SIDE OF DOOR, ABOVE UPPER LATCH FITTING. REMOVED A ND REPLACED WEB PER SRM 6-70-01, PAGE 2, ITEM 4A AND DRAWING NR 9915565. 2 L 7 2 4F A6WE 1999081400403 19990814 00403 WP 1999 8 14 TWAA9911107 1 19990802 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND IN LT SIDE OF CABIN AT STA 965 FORMER TO LONGERON 17L HAD ATTACH ANGLE CRACKED. REPLAC ED ANGLE PART NR 2916078-501, PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999081400404 19990814 00404 WP 1999 8 14 TWAA9911108 1 19990802 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CRACK IN FORMER .5 INCHES IN LENGTH AT STA 965, LT FWD SIDE, AT JUNCTION OF LOWER LEG OF ENG MOUNT. INSTALLED CHORD ANGLE PART NR 9912243-9, AS PART OF MO 72J14 PHASE G, PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999081400405 19990814 00405 WP 1999 8 14 TWAA9911109 1 19990802 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK AT STA 980, BETWEEN LONGERON 28L AND 27L, INTERCOSTAL ATTACH ANGLE WAS CRACKED. REPLACED CRACK ED ANGLE WITH ANGLE OF SAME MATERIAL AS EXISTING, 7075-T6, PER SPM 6-70-01. REPLACED HI-LOCKS PER SRM 51-30-5, PAGE 12. 2 L 7 2 4F A6WE 1999081400406 19990814 00406 WP 1999 8 14 TWAA9911110 1 19990803 A 5320 JAMB DOUG DC9 DC931 3022065 WP CARGO DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK IN THE FWD CARGO DOOR OPENING, FOUND A CRACK IN SUBSURFACE OF FUSELAGE AT LOWER AFT DOOR JAM AR EA. INSTALLED A TWO PIECE DOUBLER. CRACK CONTAINMENT AS PER SRM 53-05, FIG 105, SHEET 1,2,3 AND 4, VIEW 7011C, DRAWING NUMBER 5910142, SHEET 1,2 AND 3. 2 L 7 2 4F A6WE 1999081400407 19990814 00407 EU 1999 8 14 MALA976528 1 19990724 A 2150 BRUSHES SAAB SF340 340B 7860101 EU AC DRIVE MOTOR FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 439XJ 439 UNDER ROW 4 SMOKE FROM VENT AND BURNING PLASTIC SMELL. MAINTENANCE REPLACED SUPPLEMENTAL AC DRIVE MOTOR BRUSHES IAW AAR CMM, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999081400408 19990814 00408 EU 1999 8 14 MALA976529 1 19990803 A 7933 4053T73P0 TEMP BULB SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 103XJ 340A103 DURING FLIGHT, RIGHT PROP OIL TEMP EXCEEDED UPPER LIMITS, COMPLIED WITH QRH. NO ABNORMALITIES WERE NOTED ON RIGHT ENGIN E. MAINTENANCE REPLACED RIGHT ENGINE PROP OIL TEMP BULB. RAN ENGINE FOR SEVERAL MINUTES, ALL CHECKS GOOD IAW GE MM. 2 L 7 2 4T RT A52EU 1999081400409 19990814 00409 1999 8 14 MALA976530 2 19990805 A 7261 OIL SYS SAAB SF340 SF340A 7850100 EU RT ENGINE REQD SERVICE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 991XJ 091 ON TAKEOFF AT V1, RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED THEN WENT OUT (APPROX. 1 SEC) ON CLIMB-OUT CHECKED OIL PRE SSURE GAUGE VERIFIED IN YELLOW AREA (APPROX 10-20 PSI) DID NOT NOTICE ANY ENGINE SURGE OR ABNORMAL NOISES, BROUGHT POWER BACK TO 40 PERCENT TORQUE. RETURNED FOR LANDING. MAINTENANCE ADDED 3 QUARTS OF OIL. OPS CHECK GOOD, RECHECK OIL LEVE L-GOOD. NO LEAKS NOTED. 2 L 7 2 4T RT A52EU 1999081400410 19990814 00410 1999 8 14 MALA976531 2 19990801 A 7200 ENGINE BAC 146 AVRO146RJ85A 1500097 EU NR 3 FAILED A MALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 15 501XJ E2208 AFTER TAKEOFF, NOTED NR 3 ENGINE VIBRATION ROSE TO 0.6 ABT 30 MIN INTO FLT VIB ROSE TO 1.1, RETURNED TO MSP. 20 MINUTES OUT OF MSP VIB WENT TO 1.2 RETARDING POWER LEVER KEPT IT BELOW 1.2, AUDIBLE SOUND HEARD AND VIBRATION FELT IN YOKE. MA INTENANCE REPLACED NR 3 ENGINE. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999081400411 19990814 00411 EU 1999 8 14 MALA976532 1 19990801 A 3241 AE20612 CONTROL BOX BAC 146 AVRO146RJ85A 1500097 EU ANTI SKID SYS MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 510XJ E2325 YELLOW SYSTEM ANTI-SKID INOP LIGHT CAME ON DURING FLIGHT, SELECTED GREEN SYSTEM AND LIGHT WENT OUT AND WORKED NORMALLY. MAINTENANCE REPLACED ANTI SKID CONTROL BOX IAW AMM 32-41-47. PERFORMED OPS CHECK, ALL TESTS PASS. 2 H 7 4 4F RT A49EU 1999081400412 19990814 00412 1999 8 14 MALA976533 4 19990804 A 3442 20412220435 RADAR BAC 146 AVRO146RJ85A 1500097 EU COCKPIT INOP A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 519XJ E2344 WEATHER RADAR INOP EN ROUTE WX. RETURNED TO MSP. MAINTENANCE REPLACED RADAR INDICATOR. 2 H 7 4 4F RT A49EU 1999081400413 19990814 00413 EU 1999 8 14 MALA976534 1 19990802 A 2150 VALVE BAC 146 AVRO146RJ85A 1500097 EU LT&RT PACK ICED UP A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 520XJ E2345 CLIMBING THROUGH 5000 FT, PACK 2 VALVE ON, RAN CHECK LIST NO HELP, 10 MINUTES LATER AT 17000 FT PACK 1 VALVE ILLUMINATES , ABLE TO KEEP ONE PACK ON BY SUPPLEMENTING WITH APU AIR. RETURNED TO DTW. MAINTENANCE FOUND AC IN MANUAL MODE WITH DU CT TEMP AT -20 DEGREES C, GROUND RAN APU AIR AND ENGINE AIR FOR 45 MINUTES, INSPECTED AIR CONDITIONING BAY FOR LEAKS AND DUCTING, NO DEFECTS WERE NOTED. BOTH PACKS RESPOND AS REQUIRED, SUSPECT ICED UP VALVES AT ALTITUDE. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999081400414 19990814 00414 EU 1999 8 14 MALA976535 1 19990803 A 2460 52653025 CIRCUIT BREAKER BAC 146 AVRO146RJ85A 1500097 EU E&E COMPT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 528XJ E2353 FLAP FAULT, WINDSHEAR INOP, NR 4 FUEL BOOST PUMP, NR 2 ALT, AND WARNING LIGHT ILLUMINATED. RETURNED TO MSP. MAINTENANC E REPLACED CIRCUIT BREAKER XD-12. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1999081400415 19990814 00415 NM 1999 8 14 PCAA9900026 1 19990808 A 3230 11300105 ACTUATOR DHAV DHC8 DHC8102 2809003 NM LT MLG UPLOCK FAILED A PCAA K NONE J WARNING INDICATION DE DESCENT 1 EA 13 821EX 10583 173 BTV - UPON DESCENT, THE LEFT MAIN GEAR DID NOT EXTEND WHEN SELECTED. GEAR EXTENDED 45 SECONDS LATER WITH DOWN AND LOCKE D INDICATION. MAINTENANCE REMOVED AND RPELACED THE LEFT MAIN GEAR UPLOCK ACTUATOR IAW CHAPTER 32. CYCLED GEAR SEVERAL TIMES, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999081400416 19990814 00416 EA 1999 8 14 JBXA9900098 1 19990810 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE CABIN CONTAMINATED A JBXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 05 578ML 7270 872391872394 AFTER CHANGE OVER FROM APU TO ENGINE BLEED AIR IN CLIMB, THE CABIN BEGAN TO FILL WITH SMOKE. PERFORMED 20 MIN ENGINE RU N, NO SMOKE NOTED. SMELL OF ENGINE COMPRESSOR WASH SOAP WENT AWAY AFTER ONE MINUTE ONCE 10TH STAGE BLEEDS WERE OPENED. REMOVED AND REPLACED BOTH COALESCER BAGS IAW CL-65 AMM 21-51-00. ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081400417 19990814 00417 NM 1999 8 14 CALA9901037 1 19990808 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM L-1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND L-1 DOOR THRESHOLD Z-CHANNEL CORRODED. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1999081400418 19990814 00418 NM 1999 8 14 CALA9901038 1 19990808 A 5320 ANGLE BOEING 737 7373T0 1384582 NM R-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND Z-ANGLE CORRODED AT R-2 DOOR. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1999081400419 19990814 00419 NM 1999 8 14 CALA9901040 1 19990809 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16R AT BS 500C. REPAIRED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 1999081400420 19990814 00420 WP 1999 8 14 CALA9901041 1 19990809 A 5350 RELEASE MECH DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 937MC 49450 THE FORCE REQUIRED TO RELEASE TAILCONE USING BOTH THE INTERIOR TAILCONE RELEASE HANDLE AND THE AFT PASSENGER DOOR EXCEED ED LIMITS. THE TAILCONE RELEASE MECHANISM WAS RIGGED AND TESTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1999081400421 19990814 00421 SO 1999 8 14 COMA9910128 1 19990806 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO ROW 5 DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 189CA 120189 EMERGENCY EXIT SIGNS AT ROW 5 ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1999081400422 19990814 00422 SO 1999 8 14 COMA9910129 1 19990809 A 3620 M1160140242 SENSOR EMB 120 EMB120RT SO RT BLEED AIR MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 286CA 120262 RIGHT HAND DUCT LEAK WARNING IFSD. REPLACED BLEED AIR LEAK SENSOR. 2 L 7 2 4T RT A31SO 1999081400423 19990814 00423 SO 1999 8 14 COMA9910130 1 19990809 A 3350 10130115 LIGHT EMB 120 EMB120RT SO ROW 5 MISSING A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 267CA 120259 EMERGENCY EXIT LIGHT CONVER MISSING ROW 5. REPLACED LIGHT ASSY. 2 L 7 2 4T RT A31SO 1999081400424 19990814 00424 EA 1999 8 14 COMA9960420 1 19990808 A 2751 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 975CA 7150 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM IAW AD 98 20 01. 2 L 7 2 4F RT A21EA 1999081400425 19990814 00425 EA 1999 8 14 COMA9960421 1 19990808 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA ROW 1 INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 987CA 7199 EMERGENCY FLOOR LIGHT AT ROW 1 IS INOPERABLE. REPLACED LAMP. 2 L 7 2 4F RT A21EA 1999081400426 19990814 00426 EA 1999 8 14 COMA9960422 1 19990807 A 2430 DEPLOY SYS CNDAIR CL600 CL6002B19 EA AIR DRIVEN GEN MALFUNCTIONED A COMA K NONE O OTHER CR CRUISE 1 SO 01 943CA 7062 ADG DEPLOYED DURING FLIGHT. DEFERRED THE ADG AUTO DEPLOY SYSTEM. 2 L 7 2 4F RT A21EA 1999081400427 19990814 00427 EA 1999 8 14 COMA9960423 1 19990808 A 3010 OVERHEAT MESSAGE CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 964CA 7129 WING OVERHEAT MESSAGE. COULD NOT DUPLICATE SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1999081400428 19990814 00428 EA 1999 8 14 COMA9960424 1 19990807 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 729CA 6477 7265 FLAPS FAIL MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999081400429 19990814 00429 EA 1999 8 14 COMA9960425 1 19990806 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947CA 7077 NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE INOP. REPLACED LIGHT BULBS. 2 L 7 2 4F RT A21EA 1999081400430 19990814 00430 EA 1999 8 14 COMA9960426 1 19990809 A 3260 86488 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING DE DESCENT 1 SO 01 949CA 5960 4203 7080 PROX SYSTEM FAULT MESSAGE. LANDING GEAR WOULD NOT EXTEND. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1999081400431 19990814 00431 NM 1999 8 14 99UAL900405 1 19990731 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7273U 21420 MID CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY. 2 L 7 3 4F 4 F A3WE E2EA 1999081400432 19990814 00432 NM 1999 8 14 99UAL900406 1 19990730 A 5531 SPAR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7451U 21905 THE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAI R INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMCO'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999081400433 19990814 00433 NM 1999 8 14 99UAL900407 1 19990801 A 5270 CARD ELDEC 835107 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT EMER EXIT DR FAILED A UALA O OTHER N FALSE WARNING UK UNKNOWN 1 WP 29 656UA 25394 LEFT FORWARD EMERGENCY DOOR EICAS MESSAGE ILLUMINATED IN FLIGHT. *S/D* ACCOMPLISHED CHECK OF FWD LEFT EMERGENCY DOOR P ER MM 52-21-01 AND MM 52-71-00. REPLACED M7 CARD AT PSEU PER MM 32-09-06. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999081400434 19990814 00434 NM 1999 8 14 99UAL900408 1 19990730 A 5712 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE WS 760.5 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7451U 21905 DURING INSPECTION AND INSTALLATION OF THE PREVENTIVE MOD PER SERVICE BULLETIN727-57-0012 AS MANDATED BY AD94-07-08 AND AD90-06-09 ON THE LBL 70.5 RIB CHORD AT STATION 760.5 TWO CRACKED FASTENER HOLES WERE FOUND. FATIGUE. C0RRECTION, BOTH HOLES WERE OVERSIZED UNTIL THE CRACKS WERE ILLUMINATED AND OVERSIZED FASTENERS INSTALLED. THIS REPAIR WAS APPROVED AS AN ALTERNATE MEANS OF COMPLIANCE TO AD94-07-08 AND AD90-06-09 BY BOEING'S DER. 2 L 7 3 4F 4 F A3WE E2EA 1999081400435 19990814 00435 NM 1999 8 14 99UAL900409 1 19990801 A 2432 425404 BATTERY CHARGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BATTERY COMPT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 646UA 25283 MAIN BATTERY CHARGER EICAS MSG DISPLAYED. RETURNED TO MIA. *S/D* REPLACED BATTERY CHARGER, SYSTEM OP CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 1999081400436 19990814 00436 NM 1999 8 14 99UAL900410 1 19990803 A 2751 TRANSMITTER 1817389 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT TE FLAP FAILED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 322UA 3868 23954 TRAILING EDGE FLAPS EXTENDED TO 5 DEGREES RIGHT AND 8 DEGREES LEFT ON APPROACH. *S/D* THE FLAP ASYMMETRY WAS CAUSED BY A INOPERATIVE TRAILING EDGE FLAP TRANSMITTER. THE LEFT HAND FLAP TRANSMITTER WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999081400437 19990814 00437 NM 1999 8 14 99UAL900411 1 19990811 A 4920 M83241158 O-RING M83241145 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU CUT A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 781UA 26945 P1054 TWENTY MINUTES AFTER DEPARTURE, AIRCRAFT EXPERIENCED SMOKE IN COCKPIT AND CABIN. RT AIR CONDITIONING PACK WAS SHUT DOWN AND SMOKE SUBSIDED. AIRCRAFT RETURNED TO EWR. *S/D* APU (P/N 3800550-1), (S/N P1054), THE LOAD COMPRESSOR DISASSEMBL Y YIELDED THE FOLLOWING RESULTS: BEARING HOUSING HAD EVIDENCE OF OIL STREAKING FROM THE PARTING SURFACE TO THE AIR INLE T. BEARING HOUSING O-RING (M8324-1-158) WAS ROLLED AND HAD A SECTION CUT (SLICED) FROM THE OD APPROX .25 INCH LONG. BE ARING CARRIER O-RING (M8324-1-145) CUT (SLICED) IN 3 DIFFERENT SECTIONS FOR A TOTAL OF 3 INCHES OF O-RING MATERIAL REMOV ED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999081400438 19990814 00438 NM 1999 8 14 99UAL900412 1 19990805 A 5610 NP1653116 WINDSHIELD AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE RT COCKPIT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 CRACKED RIGHT WINDSHIELD. *S/D* CAUSE OF CRACKED RIGHT WINDSHIELD WAS FOD AS THERE WAS NUMEROUS HITS ALONG LOWER EDGE. 2 L 7 2 4F 4 F RT A28NM E40NE 1999081400439 19990814 00439 NE 1999 8 14 99UAL900413 2 19990710 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 FAILED A UALA E ENGINE SHUTDOWN E VIBRATION/BUFFET DE DESCENT 1 WP 29 915UA 25382 722217 HEARD A THUNK AND EXPERIENCED VIBRATION IN NR 1 ENGINE. GOT LOW OIL PRESSURE AND EXHAUST GAS TEMPERATURE SHOWED 813 DEG REES CELSIUS. *S/D* REPLACED NR 1 ENGINE. AIRCRAFT OPERATIONAL CHECKS GOOD. SHOP INDICATIONS, SHOW FAILURE OF THE NR 4 BEARING WAS THE ROOT CAUSE FOR THE IN-FLIGHT SHUT DOWN AND N1 ROTOR SEIZURE ON THE GROUND. 2 L 7 2 4F 4 F RT A16WE E2GL 1999081400440 19990814 00440 NM 1999 8 14 DL72S991755 1 19990806 A 5330 65545827 SKIN BOEING 727 727232 1384082 NM BS 1090-1110 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 DURING HMV INSPECTIONS IT WAS NOTED THAT THE FUSELAGE SKIN WAS CRACKED AT STRINGER 1 BETWEEN FS 1090 AND FS 1110. THIS DAMAGED WAS REPAIRED PER ER/A 333417-14 AND APPROVED BY FAA 8110-3 FORM, DER DESIGNATION DERY-635273-NM. 2 L 7 3 4F A3WE 1999081400441 19990814 00441 NM 1999 8 14 DL767991756 1 19990802 A 5330 146T33413 SKIN BOEING 767 767232 1385132 NM BS 1540 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 TWO DENTS FOUND DURING HMV, ON THE LOWER LOBE FUSELAGE SKIN AFT OF THE L2 DOOR OPENING AT STA 1555 AND 1560 BETWEEN STRI NGERS 21L AND 22L. EXTERNAL DOUBLER/TRIPLER INSTALLED PER ER/A 333345-14 REV A. 2 L 7 2 4F RT A1NM 1999081400442 19990814 00442 NM 1999 8 14 DL72S991757 1 19990807 A 3350 FUSE BOEING 727 727225A 1384077 NM ROW 1-11 BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 21291 FOUND E-PATH LIGHTS INOP AT ROWS 1 THROUGH 11. FOUND FUSE IN BATTERY RACK BLOWN. REPLACED FUSE, OPS NORMAL. 2 L 7 3 4F RT A3WE 1999081400443 19990814 00443 NM 1999 8 14 DL72S991758 1 19990806 A 3350 BATTERY 900835A BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 485DA UNK 20865 LT MID OVERWING EMERG LIGHT INOP. REPLACED BATTERY AT RACK M654. OPS CHKS GOO. 2 L 7 3 4F A3WE 1999081400444 19990814 00444 1999 8 14 DL76G991759 4 19990807 A 3460 PDC BATTERY BPS73 BOEING 767 7673P6 1385105 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1501P 24983 ON PDC, FOUND RT SLIDE TEST 1 AND LEFT SPOILER TEST 2 INOP. REPLACED BATTERY PACK ON M961 AND NOW OK. 2 L 7 2 4F RT A1NM 1999081400445 19990814 00445 NM 1999 8 14 DL72S991760 1 19990806 A 2613 OVERHEAT LOOP 355944255 BOEING 727 727232 1384082 NM LWR AFT BODY OUT OF POSITION A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 517DA 00 21433 AT APPROX 100 FEET AFE, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. REPLACED FIRE/OVERHEAT DETECTION MODULE. REPLAC ED KEEL BEAM LOOP M367 REPOSITIONED LOOP M 365 NEAR RT PURGE SHUTOFF VALVE. RAN ALL 3 ENGS AT T/O EPR. AT T/O EPR AFT BODY OVERHEAT CHKS NORMAL. 2 L 7 3 4F A3WE 1999081400446 19990814 00446 NM 1999 8 14 DLM88991764 1 19990808 A 2421 GENERATOR 947F9453 DOUG MD88 MD88 3023688 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 968DL XJ2138B 53161 IN CRUISE FL330, RIGHT GEN TRIPPED OFF AND AC X-TIE LOCKOUT MSG ON EOAP. TRIED ONE RESET NO HELP. DIVERTED TO JFK. RE PLACED GCU. 2 L 7 2 4F RT A6WE 1999081400447 19990814 00447 NM 1999 8 14 DL72K991765 1 19990808 A 3260 SWITCH 63200036 BOEING 727 727232 1384082 NM RT MLG DOOR FAILED A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 466DA NA 20743 AFTER T/O, AFTER GEAR RETRACTION, RED DOORS WARNING LIGHT AND R GEAR DOOR WARNING LIGHTS ILLUMINATE WHEN GEAR. HANDLE P LACED TO OFF. INSPECTION AND REPLACED RT GEAR DOOR SWITCH AND SYS CKS OK. 2 L 7 3 4F A3WE 1999081400448 19990814 00448 NM 1999 8 14 DL72K991766 1 19990808 A 2910 HYD SYS BOEING 727 727232 1384082 NM A HYD SYS REQD SERVICE A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 466DA NA 20743 HYD 'A' FLUID LEVEL DROPPED TO 2.0 GAL DURING FLIGHT AND PASSENGERS REPORTED SMELLING FUMES NEAR/IN SEATS OVERWING AREA . ALT FLAPS AND MANUAL GEAR USED. A/C ARRIVED AT GATE WITH HYD QTY 3.75 GAL. SERVICED HYD TO FULL, 1 GAL ADDED. INSP ECTED NOSE AND MAIN GEAR AND WING SLATS AND FLAPS AND RUDDER. RAN ENGS NR 1 AND NR 2 CKD HYD LINES FOUND OK. WITH NEGS RUNNING, NO SMELL IN CABIN. 2 L 7 3 4F A3WE 1999081400449 19990814 00449 NM 1999 8 14 DL733991767 1 19990808 A 3350 LIGHT 0L3071BPEGPL BOEING 737 7373B7 1384580 NM ROW 1D&14D INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 947WP 23376 EMERGENCY LIGHTS AT SEATS 1D ABD 14D INOP. RELAMPED TEST GOOD. 2 L 7 2 4F RT A16WE 1999081400450 19990814 00450 NM 1999 8 14 DL73K991768 1 19990809 A 3350 BPS73 BATTERY PACK BOEING 737 737232 1384475 NM L1 DOOR DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 306DL 23078 L-1 EMERGENCY SLIDE LT INOP. FOUND M1132 BATTERY PACK BAD. REPLACED M1132 SYS. OPS NML. 2 L 7 2 4F RT A16WE 1999081400451 19990814 00451 NM 1999 8 14 DLM11991769 1 19990809 A 3350 900835A BATTERY PACK DOUG MD11 MD11 3023602 NM LT EXTERIOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 801DE 48472 LEFT EXTERIOR OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F RT A22WE 1999081400452 19990814 00452 NM 1999 8 14 DL73K991770 1 19990808 A 3350 BPS73 LIGHT BOEING 737 737232 1384475 NM DOOR 1R INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 305DL 23077 DOOR 1R EMERGENCY LIGHT FLASHES. 2 L 7 2 4F RT A16WE 1999081400453 19990814 00453 NM 1999 8 14 DL72S991772 1 19990809 A 3350 CONNECTOR BOEING 727 727225A 1384077 NM ROW 4AB LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805EA 22436 FIRST CLASS CABIN EMERGENCY LIGHTS WON'T TEST. RESEATED PIN AT QUICK DISCONNECT AT SEAT 4AB. SYSTEM CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1999081400454 19990814 00454 NM 1999 8 14 DL72S991773 1 19990806 A 5532 651746160 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT THE FRONT SPAR WHERE THE TORQUE BOX ATTACHES ON THE LEFT HAND SIDE. T HE CRACK WAS FOUND AT HMV AND WAS REPAIRED PER ER/A 333420-14. 2 L 7 3 4F A3WE 1999081400455 19990814 00455 NM 1999 8 14 DL767991774 1 19990809 A 5720 112T12171 FITTING BOEING 767 767232 1385132 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 A CRACK WAS FOUND IN THE LHS KICKLOAD FITTING IN THE INBD HOLE ON THE OUTER WING SIDE. THE HOLE WAS REAMED TO REMOVED T HE CRACK INDICATION. FINAL REWORKED HOLE DIAMETER IS 0.947. REF NPRM 98-NM-278-AD. REWORKED PER ERA 333356-14AD. 2 L 7 2 4F RT A1NM 1999081400456 19990814 00456 NM 1999 8 14 DL72S991775 1 19990806 A 5510 65434399 HINGE BOEING 727 727232 1384082 NM HORIZ STAB WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE PIVOT HINGE ON THE REAR SPAR OF THE HORIZONTAL STABILIZER WAS WORN AT RBL 10. THIS DAMAGE WAS REPAIRED PER ER/A 367 854-14 AT HMV. 2 L 7 3 4F A3WE 1999081400457 19990814 00457 NM 1999 8 14 DL72S991776 1 19990806 A 5320 651750565 SHEAR TIE BOEING 727 727232 1384082 NM BS 1283 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE FS 1283 FRAME WAS FOUND CRACKED BETWEEN STR 12L AND STR 13L. THIS DAMAGE WAS REPAIRED PER ERA 367856-14. 2 L 7 3 4F A3WE 1999081400458 19990814 00458 NM 1999 8 14 DL72S991777 1 19990806 A 5532 651746161 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE SKIN ON THE RIGHT SIDE OF THE VERTICAL STABILIZER WAS FOUND CRACKED BETWEEN FS 1203 AND 1211. THIS DAMAGE WAS REPA IRED PER ERA 333422-14. 2 L 7 3 4F A3WE 1999081400459 19990814 00459 NM 1999 8 14 DL72S991778 1 19990806 A 5330 6518219137 SKIN BOEING 727 727232 1384082 NM BS 380 CRACKED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 527DA 21587 THE FUSELAGE SKIN WAS DAMAGED DUE TO CONTACT WITH THE JETWAY AT FS 380 BETWEEN STRINGERS 17L AND 18L ON 9/13/93 AND A TE MPORARY REPAIR WAS INSTALLED. AT THIS HMV A PERMANENT REPAIR WAS INSTALLED PER ER/A 257628-14. 2 L 7 3 4F A3WE 1999081400460 19990814 00460 NM 1999 8 14 DL72S991779 1 19990806 A 5330 65545801 SKIN BOEING 727 727232 1384082 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE FUSELAGE SKIN WAS GOUGED AT FS 990 BETWEEN STRINGERS 24R AND 25R DUE TO GROUND DAMAGE. THE REPAIR WAS ACCOMPLISHED BYERA 333427-14. 2 L 7 3 4F A3WE 1999081400461 19990814 00461 NM 1999 8 14 DLM11991780 1 19990803 A 2520 WIRE DOUG MD11 MD11 3023602 NM ROW 5G FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 801DE 48472 LEG REST 5G ELECTRICALLY INOP. REPLACED LEG REST ACTUATOR. NO HELP SPLICED BURNED WIRE. CKS GOOD. 2 L 7 3 4F RT A22WE 1999081400462 19990814 00462 SO 1999 8 14 LR7A9952 1 19990729 A 2130 10604041 SHUTOFF VALVE LKHEED 382 382G 526414U SO CARGO COMPT FAILED A LR7A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 401LC 1506 4606 AIRCRAFT WOULD NOT PRESSURIZE. REPLACED CARGO COMPARTMENT FLOW CONTROL AND SHUTOFF VALVE IAW SMP581 21-50 PG 206. OPS CHECK AND LEAK CHECK OK. AIRCRAFT PRESSURIZED NORMALLY ON GROUND. 2 H 7 4 4T A1SO 1999081400463 19990814 00463 SO 1999 8 14 LR7A9953 1 19990729 A 2130 672790001 VALVE LKHEED 382 382G 526414U SO CARGO COMPT LEAKING A LR7A A UNSCHED LANDING M OVER TEMP CL CLIMB 1 AL 03 401LC 777 4606 CARGO COMPARTMENT REFRIG OVERHEAT LIGHT ILLUMINATED. FOUND GASKETS LEAKING ON FLOOR HEAT DIVERTER VALVE RESEALED IAW SM P581 CH 21-50. LK CK NORMAL. 2 H 7 4 4T A1SO 1999081400464 19990814 00464 SO 1999 8 14 LR7A9954 1 19990729 A 2150 838321 HEAT EXCHANGER LKHEED 382 382G 526414U SO CARGO COMPT CRACKED A LR7A A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 AL 03 401LC 777 4606 CARGO COMPARTMENT OVERHEAT LIGHT ON IN FLIGHT. DIVIDER VALVE LEAKING AT ALL 3 JOINTS. REPLACED GASKETS AND SEALED PER MAINT MANUAL 36-10 PG 205. REPLACED HEAT EXCHANGER IAW SMP581. OPS CK NORMAL. 2 H 7 4 4T A1SO 1999081400465 19990814 00465 NM 1999 8 14 UPS99530312 1 19990809 A 3150 6226540111 EICAS BOEING 757 75724APF 1384969 NM COCKPIT INOP A IPXA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION DE DESCENT 1 SO 01 410UP 23732 ON DESCENT, MULTIPLE WARNINGS (FALSE) INCLUDING ENG FIRE, CARGO FIRE, GEAR DISAGREE. SELECTING RIGHT EICAS COMPUTER COR RECTED PROBLEM. LEFT EICAS COMPUTER WAS DEFFERED OUT OF SJC ON A ONE DAY TIME LIMIT REPLACED IN DSM ON 08/10/99. NO FU RTHER PROBLEMS EICAS COMPUTER PART NUMBER IS 622-6540-111. 2 L 7 2 4F RT A2NM 1999081400466 19990814 00466 WP 1999 8 14 UPS99830311 1 19990809 A 3350 LIGHT DOUG DC8 DC871F 302199D WP CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 718UP 46018 EMERGENCY LIGHT DISARM CHECK DOES NOT CHECK. RELAMPED EMERGENCY LIGHT SWITCH IND LIGHT CKS GOOD PER MM 33-50-00. 2 L 7 4 4F RT 4A25 1999081400467 19990814 00467 EU 1999 8 14 99FDEA00319 1 19990806 A 2910 O RING AIRBUS 310 A310222 3930315 EU GREEN HYD SYS LEAKS A FDEA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 452FE 313 99-198 - LOST GREEN HYD FLUID LOSS. REPLACED O-RING IN RETURN BOSS PER SMP REQUIRES LEAK CK AND INSP OF GREEN HYD SYS M M 29-00-00 PG 320. 2 L 7 2 4F RT A35EU 1999081400471 19990814 00471 NM 1999 8 14 99FDEA00323 1 19990808 A 2750 RETRACT MECH DOUG MD11 MD11F 3023600 NM TE FLAPS INOP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 615FE 48767 99-199 - AFT T/O NORMAL, FLAP/SLAT RETRACTION DEF AIL ALERT CAME ON. 2 L 7 3 4F RT A22WE 1999081400472 19990814 00472 NM 1999 8 14 99FDEA00325 1 19990811 A 3260 ACCESSORY UNIT BOEING 727 72722C 138400F NM LANDING GEAR INOP A FDEA K NONE N FALSE WARNING CL CLIMB 1 SO 25 112FE 19890 99-201 - AFT RAISING LAND GEAR HANDLE ALL 3 UNSAFE RED LIGHTS REMAIN ON. RERACKED LAND GEAR ACCESSORY UNIT, CYCLED LT M LG DOWNLOCK SWITCH, OPS CK NORM PER 727-100 M/M 32-62-001-4. 2 L 7 3 4F A3WE 1999081400473 19990814 00473 NE 1999 8 14 99FDEA00326 2 19990811 A 7230 COMPRESSOR BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STALLING A FDEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 218FE 21101 AFT NORM T/O NR 2 ENG STARTED COMPRESSOR STALLING. THE ENGINES WERE AT CLIMB PWR WITH 150 EG'S FLAPS. *S/D* REMOVED A ND REPLACED NR 2 ENG PER W/C 70T0002. RAN ENG PER JRH. ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 1999081400474 19990814 00474 NM 1999 8 14 99FDEA00327 1 19990811 A 3260 B273202601 ACCESSORY UNIT BOEING 727 72722C 138400F NM LANDING GEAR INOP A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 112FE 19890 99-203 REPEAT, 3 GEAR RED INTRANSIT LIGHTS WOULD NOT EXTINGUISH AFT RAISING GEAR HANDLE TO UP FLT ENGINE DOOR ANNUNCIAT OR PNL NORM. REMOVED AND REPLACED LANDING GEAR ELECTRICAL MODULE PER MM 32-09-111-4 TEST PER MM 32-09-111-5. OPS CK GO OD. 2 L 7 3 4F A3WE 1999081400475 19990814 00475 NE 1999 8 14 99FDEA00324 2 19990809 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 3 ENGINE BIRD STRIKE A FDEA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 25 618FE 48754 99-200 - ON T/O A LARGE BIRD STRUCK THE RT SIDE OF THE A/C. ENG MADE LOUD NOISE PWR REDUCED, VIB WENT AWAY, AND RETURN FOR LAND. FAN BLADES REPLACED SEE WRI 72-10/4339 AND 72-10/4336. REVERSER TRANSLATING COWL REPLACED PER 78-30/4338. P ERF TRIM BALANCE ON NR 3 ENG PER MD11 MM 72-30-00. PERF BIRD STRIKE INSP IAW MD11 MM 05-52-01-6 AND 72-00-02-200-801. 2 L 7 3 4F 4 F RT A22WE E31N3 1999081400476 19990814 00476 WP 1999 8 14 99FDEA00328 1 19990809 A 5400 716581680 BOLT DOUG DC10 DC1010F 3022111 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 056FE 47810 NR 190 NR 3 PYLON AFT SPHERICAL BEARING, THROUGH BOLT FOUND WITH CRACK IND DURING MAGNAFLUX INSP. INSTALL NEW NR 3 PYLO N AFT BEAR THROUGH BOLT PER EO 8-5410-7-430734 PART 4 STEP 12 AND 13. 2 L 7 3 4F A22WE 1999081400477 19990814 00477 NE 1999 8 14 ABXA9900635 2 19990806 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 DEFECTIVE A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 815AX 46093 671118 DURING CRUISE, NR 4 OIL QUANTITY DROPPED TO ZERO, OIL PRESSURE FLUCTUATED 20-45 PSI. ENGINE WAS SHUT DOWN. AFTER SHUTD OWN, OIL PRESSURE MAINTAINED 0-5 PSI. ENGINE WINDMILLED FOR 48 MINUTES. REPLACED NR 4 ENGINE IAW ABX WORK CARD 8090501 , DC8 A AND B. 2 L 7 4 4F 4 F 4A25 1E8 1999081400478 19990814 00478 NM 1999 8 14 MWEA99473 1 19990809 A 5720 5930494501 FIXED VANE DOUG MD88 MD88 3023688 NM LT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE LEFT WING INBOARD NR 3 FLAP FIXED VANE IS CHAFED. MAINTENANCE INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 1999081400479 19990814 00479 NM 1999 8 14 MWEA99474 1 19990809 A 5720 993758922 CLIP DOUG MD88 MD88 3023688 NM WS 330&338 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND CRACKS IN RIGHT WING LEADING EDGE RIB ATTACH CLIPS AT FRONT SPAR UPPER CAP STATION XRS 330 AND 338. MAINTENANCE F ABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999081400480 19990814 00480 NM 1999 8 14 MWEA99475 1 19990809 A 5712 993758924 RIB DOUG MD88 MD88 3023688 NM WS 338 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 RIGHT WING LEADING EDGE RIB DOUBLER AT STATION XRS 338 IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999081400481 19990814 00481 NM 1999 8 14 MWEA99476 1 19990809 A 5712 993758918 RIB DOUG MD88 MD88 3023688 NM WS 330 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE RIGHT WING LEADING EDGE RIB AT STATION XRS 330 HAS CRACK IN THE RADIUS. MAINTENANCE FABRICATED AND INSTALLED DOUBLE R REPAIR. 2 L 7 2 4F RT A6WE 1999081400482 19990814 00482 NM 1999 8 14 MWEA99477 1 19990809 A 5712 99375867 RIB DOUG MD88 MD88 3023688 NM WS 189 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 LEFT WING NOSE RIB IS CRACKED AT TOP AFT END AT STATION XRS 189. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1999081400483 19990814 00483 1999 8 14 MWEA99478 4 19990807 A 3421 258733513 VERTICAL GYRO DOUG DC9 DC982 3022082 WP LT COCKPIT INOP A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 809ME 48071 THE CAPTAINS MCDU BLANKED WITH NO AUTO THROTTLES NO AUTO PILOT AND INTERMITTENT OFF AN ON VOR'S. MAINTENANCE REMOVED AN D REPLACED BOTH VERTICAL GYRO'S. 2 L 7 2 4F A6WE 1999081400484 19990814 00484 NM 1999 8 14 SCNA99713 1 19990731 A 5712 RIB BOEING 727 7272J4 1384006 NM RT WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, THE RIGHT WING LEADING EDGE CAVITY AT FSS 605, RIB HAS CORROSION AT ADELL CLAMP ATTACH P OINT. REMOVED LEADING EDGE RIB IAW B727 SRM 513002. CORROSION WAS FOUND OUT OF LIMITS IAW SRM B727 571001. FABRICATED NEW RIB PER SAMPLE FROM 2024 T3 .050. TREATED AND PRIMED IAW SRM B727 511002 AND MM 512002. INSTALLED IAW SRM B727 51 3002. 2 L 7 3 4F RT A3WE 1999081400486 19990814 00486 CE 1999 8 14 99ZZZX2967 1 19990722 A 3232 66000852 ACTUATOR RONSON LEAR 25 25 5170506 CE RT MLG DOOR LEAKING A KKFA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 23 28CK 1408 045 AIRCRAFT LOST HYDRAULIC PRESSURE. RIGHT HAND INBOARD GEAR DOOR ACTUATOR LEAKING HYDRAULIC FLUID. REPLACED RIGHT INBOAR D GEAR DOOR ACTUATOR WITH SERVICEABLE UNIT IAW LEARJET MODEL 25 SM. REPLACED BOTH ENGINE DRIVEN HYDRAULIC PUMPS AS A PR ECAUTIONARY MEASURE. OPERATIONAL AND LEAK CHECK OF SYSTEM ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE. NO RECOMMENDATI ON KNOWN TO PREVENT RECURRENCE. 2 L 7 2 4J A10CE 1999081400490 19990814 00490 NE 1999 8 14 99ZZZX2971 2 19990809 A 7200 ENGINE LEAR 35 35A 5170602 CE GE CJ610 CJ6106 30006 NE LEFT FAILED A EGQA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 EA 17 78MC 117 251588A THE AIRCRAFT WAS EN ROUTE TO PICK UP PASSENGERS IN SARASOTA, FL PASSING THROUGH 41,000 FEET HEADING FOR 43,000 FEET, THE LEFT ENGINE FLAMED OUT. PILOT'S DESCENDED TO 25,000 FEET AND RELIT THE ENGINE ACCORDING TO CHECKLIST PROCEDURES. ACFT WAS LANDED WITHOUT INCIDENT. MECHANIC REMOVED COWLINGS AND INSPECTED ENGINE. NO DISCREPANCIES NOTED AND THE ENGINE WA S GROUND RUN TO CHECK PERFORMANCE. FINDING ALL PERFORMANCE PARAMETERS NORMAL, ACFT WAS FLOWN BACK TO HOME BASE AT 33,00 0 FEET WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 J A10CE 1E16 1999081400498 19990814 00498 NE 1999 8 14 99ZZZX2979 2 19990720 A 8530 116733CP CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE NR 1 ENGINE CRACKED A MCCA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 11 5831B 78 AL42100882 351640 AFTER LEVELING OFF, ENGINE STARTED TO RUN ROUGH AND BACKFIRE. SECURED ENGINE AND FEATHERED PROPELLER. MAINTENANCE FOUN D CYLINDER NR 1 CRACKED. REPLACED CYLINDER WITH AN OVERHAULED UNIT. AIRCRAFT GROUND RUN AND CHECKED SATISFACTORY. 2 L 7 2 4R 4 R A669 5E4 1999081400501 19990814 00501 SO 1999 8 14 99ZZZX2982 2 19990618 A 8520 534278 PIN CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO CRANKCASE LOOSE A DYVA O OTHER O OTHER NR NOT REPORTED 1 NM 07 5943M 421B0316 235279R THE IDLER GEAR SUPPORT PIN WAS FOUND LOOSE AND BACKED OUT OF THE CRANKCASE CAUSING THE IDLER GEAR TO BE OUT OF POSITION DISCONNECTING THE DRIVE TRAIN TO THE MAGNETOS WHICH CAUSED AN IMMEDIATE TOTAL LOSS OF POWER. THERE WAS ALSO EXTENSIVE D AMAGE TO THE TEETH ON THE CRANKSHAFT GEAR, STARTER-DRIVE ADAPTER GEAR, AND THE CAMSHAFT GEAR THAT WAS POSSIBLY DONE DURI NG THE THREE MINUTES OF WINDMILLING WHILE THE PILOT ATTEMPTED TO RESTART THE ENGINE. THE POSSIBLE CAUSE IS LOOSE 1/4 - 28 NUTS ON THE MOUNTING STUDS FOR THEIDLER GEAR SUPPORT PIN. 1 L 7 2 3O 3 O A7CE E7CE 1999081400509 19990814 00509 NE 1999 8 14 ORJA99169 2 19990512 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 FAILED A ORJA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 832RA 53044 AT LAS, DURING CLIMB-OUT, RIGHT OIL STRAINERS CLOG ANNUNCIATOR CAME ON. WITH RIGHT ENGINE AT IDLE, LIGHT WOULD NOT GO O UT. MAX OIL TEMPERATURE OBSERVED, 129 CELSIUS. REMOVED AND REPLACED NR 2 ENGINE FOR OIL STRAINER CLOG ANNUNCIATOR PER TASK CARD 0099. LEAK AND OPS CHECKS GOOD. TRIMMED ENGINES PER MM 71-00-00. ALL PARAMETERS NORMAL. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1999081400511 19990814 00511 NE 1999 8 14 ARWA990602 2 19990622 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 FAILED A ARWA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL E VIBRATION/BUFFET CL CLIMB 1 SO 19 802BN 45909 SJU - FLT 601 - CLIMBING-OUT THROUGH 16000 FT AT 1302Z, NR 4 ENGINE LOUD BANG ALL PARAMETERS ERRATIC. COMPLETED APPROPR IATE CHECK LISTS. DUMPED FUEL TO MAX LANDING WEIGHT. RETURNED TO TJSJ WITHOUT INCIDENT. CUASE OF FAILURE CONTINUES. R EMOVAL AND REPLACEMENT OF NR 4 ENGINE IN PROGRESS. CAUSE OF FAILURE TO BE DETERMINED AT SHOP VISIT. (M) 2 L 7 4 4F 4 F 4A25 1E8 1999081400512 19990814 00512 NE 1999 8 14 EISA99134 2 19990612 A 7314 378200 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE FAILED A EISA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 SW 07 945VJ 47066 RIGHT ENGINE FAILED NEAR V2 SPEED 115 KNOTS FOLLOWING NORMAL TAKEOFF. REMOVED AND REPLACED FUEL PUMP, ENGINE DRIVEN IAW MM 73-10-1 AND 73-20-1. LEAK CHECK AND TRIM PER 71-00-0. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999081400513 19990814 00513 NE 1999 8 14 AALA990882 2 19990616 A 7321 8062143 FUEL CONTROL DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE NR 1 ENGINE DEFECTIVE A AALA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SW 07 133AA 47828 LAX - FLT 162 - DURING APPROACH LAX AT APPROX 1,006 FEET, THE NR 1 ENGINE FLAMED OUT. FUEL PRESSURE WAS ZERO. FUEL PUM PS WERE ON, HAD 5200 LBS OF FUEL IN NR 1 TANK. ENGINE RELIT AT ABOUT 100 FEET AGL. LANDED LAX WITHOUT INCIDENT. REPLA CED MAIN ENGINE FUEL CONTROL AND FUEL PMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A22WE E23EA 1999081400514 19990814 00514 NE 1999 8 14 MASA99111 2 19990701 A 7314 FUEL PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 1 ENGINE FAILED A MASA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 173YV UE173 FLT 5906 - PIT-FKL - AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A FUEL PUMP FAILURE ON THE NR 1 ENGINE. THE CREW DECLARED AN EMERGENCY, AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION WAS DEFERRED PER MEL 28-5. THE AI RCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999081400515 19990814 00515 WP 1999 8 14 VTZA990031 2 19990412 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE OUT OF ADJUST A VTZA O OTHER J R WARNING INDICATION PARTIAL RPM/PWR LOSS AP APPROACH 1 EA 27 488UE 907 FLT 7599 - BGM-IAD - DURING APPROACH, LEFT ENGINE FAILED IN FLIGHT 0 PERCENT TQ 50 PERCENT RPM, SRL, FUEL, OIL PRESS CAP TIONS. ENGINE FAILED WITH ANTI-ICE AND IGN ON. MAINTENANCE ADJUSTED FLGHT IDLE FUEL FLOW AND MAX POWER ON LEFT ENGINE AND PERFORMED ENGINE RUNS. ALL ENGINE PARAMETERS WITHIN NORMAL OPERATING LIMITS. ALSO, INSPECTED FUEL SUMP FOR CONTAMI NATION, CHECKED GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400516 19990814 00516 WP 1999 8 14 VTZA990037 2 19990421 A 7321 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE FAILED A VTZA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 EA 27 488UE 907 FLT 7318 - CHO-IAD - DURING APPROACH, AIRCRAFT EXPERIENCED IN FLIGHT SHUTDOWN OF LEFT ENGINE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT FUEL CONTROL FOR ADDITIONAL PRECAUTION, FUEL PUMP P/N 897400-7 AS ALSO REPLACED. AIRCRAFT WA S RELEASED FOR MAINTENANCE ACCEPTANCE FLIGHT, WHICH WAS SATISFACTORY. AIRCRAFT WAS THEN RELEASED AND RETURNED TO SERVIC E. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400517 19990814 00517 WP 1999 8 14 VTZA990126 2 19990523 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RIGHT POWER LOSS A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 493UE 805 FLT 7207 - IAD-PHF - DURING CLIMB, AIRCRAT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE DROP TO APPROX 84 PERC ENT. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 42804, MEL 76-2. OP S CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400518 19990814 00518 WP 1999 8 14 VTZA990127 2 19990528 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 492UE 790 FLT 7193 - IAD-ROA - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE DID NOT MAKE TORQUE WITHIN 10 SECONDS. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED ADJUSTED X-SCREW. OPS CHECKED OK. AIR CRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400519 19990814 00519 WP 1999 8 14 VTZA990128 2 19990528 A 7320 31021591 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE CRACKED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 470UE 814 FLT 7631 - IAD-RDU - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT ENGINE WOULD NOT MAKE MORE THAN 60 PERCENT TO RQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED P3 LINE, OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400520 19990814 00520 WP 1999 8 14 VTZA990421 2 19990421 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT FAILED A VTZA K NONE J WARNING INDICATION AP APPROACH 1 EA 27 488UE 907 FLT 7599 - BGM-IAD- DURING APPROACH, LEFT ENGINE FAILED IN FLIGHT 0 PERCENT TORQUE 50 PERCENT, SRL, FUEL, OIL PRESS CAPT IONS. ENGINE FAILED WITH ANTI-ICE AND IGN ON. MAINTENANCE ADJUSTED FLIGHT IDLE FUEL FLOW AND MAX POWER ON LEFT ENGINE AND PERFORMED ENGINE RUNS. ALL ENGINE PARAMETERS WITHIN NORMAL OPERATING LIMITS. ALSO, INSPECTED FUEL SUMP FOR CONTAMI NATION. CHECKED GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400521 19990814 00521 WP 1999 8 14 VTZA990093 2 19990621 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 480UE 894 FLT 7203 - IAD-ROA - ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE ROLLED BACK ON TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GA TE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 42397, MEL 76-2. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400522 19990814 00522 WP 1999 8 14 VTZA990102 2 19990525 A 7310 M976921 FILTER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP NR 2 DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 477UE 890 FLT 7305 - AVP-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO NR 2 FUEL FILTER WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO T HE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FUEL FILTER, OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400523 19990814 00523 WP 1999 8 14 VTZA990095 2 19990523 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 480UE 894 FLT 7195 - IAD-ROA - AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY PRODUCE 99.2 PERCENT RPM. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED X-SCREW ON LEFT ENGINE, OPS CHECK OK. AIRCRA FT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400524 19990814 00524 WP 1999 8 14 VTZA990077 2 19990512 A 7200 310338024 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT FAILED A VTZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 483UE 898 P66082 FLT 7643 - ROC-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOSS OF OIL PRESSURE. AIRCRAFT DIVERTED TO MDT AND WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND IS THE PROCESS OF REMOVING AND REPLACI NG LEFT ENGINE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RET URN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400525 19990814 00525 WP 1999 8 14 99ZZZM424 2 19990517 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE3311 01514 WP RIGHT FAILED A CX7A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 03 832JS 721 P63082 FLT 8832 - LAN-MDW - RIGHT ENGINE FAILED IN FLIGHT WITH OIL CONTAMINATION LIGHT. AIRCRAFT LANDED IN SBN WITHOUT INCIDEN T. RIGHT ENGINE REMOVED AND SENT TO OVERHAUL FACILITY WHERE A COMPLETE TEARDOWN AND INSPECTION WILL BE PERFORMED WITH F AA PRESENT. (M) 2 L 7 2 4T 3 T RT A21EU E3WE 1999081400526 19990814 00526 WP 1999 8 14 VTZA990056 2 19990502 A 7320 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE OUT OF ADJUST A VTZA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 322UE 41058 FLT 7282 - IAD-ROA - DURING LANDING MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS RIGHT ENGINE FLAMED OUT ON LANDING. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED RIGHT DECELL AND GROUND RA N AIRCRAFT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999081400527 19990814 00527 WP 1999 8 14 VTZA990139 2 19990523 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RIGHT MALFUNCTIONED A VTZA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 27 493UE 805 FLT 7207 - IAD-PHF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE DROP TO APPROX 84 PER CENT. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 438004, MEL 76-2. M AINTENANCE CLOSED DMI 43804 ON 5-25-99 BY ADJUSTING X-SCREW. OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999081400528 19990814 00528 NE 1999 8 14 EIAA990007 2 19990322 A 7230 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 STALLED A EIAA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 481EV 19896 SUU - AT TOP OF DESCENT, NR 3 ENGINE HAD A NON-RECOVERABLE ENGINE STALL, OPERATION NORMAL AFTER SHUTDOWN AND RESTART. I DLE ADJUSTED 26 CLICKS. IDLE PARAMETERS NORMAL. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999081400529 19990814 00529 NE 1999 8 14 USAASB99114 2 19990428 A 7510 1D72230684 CONNECTOR BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE LOOSE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 267AU 22879 BWI - FLT 2681 - DURING CLIMB-OUT FROM BWI, THE NR 2 ENGINE FUEL HEAT LIGHT ILLUMINATED. THE NR 2 ENGIN OIL TEMP BEGAN TO EXCEED LIMITS. CREW TRIED DIFFERENT POWER LEVELS, BUT THE OIL TEMPERATURE REMAINED IN THE YELLOW TO RED BAND. CREW DECIDED TO RETURN TO FIELD AT BWI. APPROX 10 MILES OUT FROM BWI, THE NR 2 OIL TEMPERATURE WENT BACK TO THE GREEN BAND A ND THE CREW DID NOT HAVE TO SHUTDOWN THE ENGINE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. M AINTENANCE SECURED LOOSE CANNON PLUG FOR THE NR 2 ENGINE FUEL HEAD VALVE. OPERATIONAL CHECK OF FUEL HEAT SYSTEM GOOD. ( M) 2 L 7 2 4F 4 F A16WE E2EA 1999081400530 19990814 00530 NE 1999 8 14 EIA990113 2 19990409 A 7230 COMPRESSOR BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE STALLED A EIAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 NM 09 482EV 20713 LAX - ON DESCENT, NR 4 ENGINE COMPRESSOR STALLED, EGT RISING, DID NOT EXCEED 850 DEGREES N1 DECREASING, ACCOMPLISHED ENG INE SHUTDOWN. ATTEMPT RESTART, NO FUEL FLOW INDICATED. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999081400531 19990814 00531 NM 1999 8 14 USAA069946 1 19990616 A 7312 320115 VALVE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE FAILED A USAA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 19 924TS 21041 NR 3 ENGINE OIL TEMP HIGH. PERFORMED ABNORMAL HIGH OIL TEMP PROCEDURE. CYCLED FUEL HEAT SWITCH, NO HELP. SHUT DOWN NR 3 ENGINE BEFORE 15 MINUTES MAXIMUM OIL TEMP IN YELLOW BAND. NR 3 FUEL HEAT BLUE INTRANSIT LIGHT ON AT ALL TIMES WITH F UEL HEAT SWITCH OFF. FOUND NR 3 FUEL HEAT VALVE FAILED. REPLACED SAME PER MM 73-14-1. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999081400532 19990814 00532 NE 1999 8 14 AALA990619 2 19990422 A 7310 6667621 FILTER BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE RESTRICTED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 07 877AA 21389 MEM - FLT 1929 - DURING CRUISE, NR 1 ENGINE SURGED 4 TIMES AT FL330 ON ALL PARAMETERS ACCOMPANIED BY FLICKERING AMBER EN GINE ICE LIGHT. FLIGHT AIR INTERRUPTED AND LANDED MEM WITHOUT FURTHER INCIDENT. MAINTENANCE SUMPED BOTH RIGHT AND LEFT WING TANKS WITH NO WATER NOTED. REPLACED NR 1 ENGINE FUEL FILTER AND O-RING. LEAK CHECK OK. NR 1 ENGINE GROUND RUN A T IDLE AND POWER ACCEPTANCE WITH ALL PARAMETERS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999081400533 19990814 00533 NE 1999 8 14 USAASB99134 2 19990602 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15 52051 NE LEFT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 288AU 23135 708367 PVD - FLT 2663 - JUST AFTER TAKEOFF, AT APPROXIMATELY 600 FEET, THE CREW HEARD A LOUD BANG. INDICATIONS FOR THE NR 1 EN GINE EGT WERE IN THE YELLOW ARC, REACHING 600 DEGREES MAXIMUM. ALL OTHER INDICATIONS WERE NORMAL. AFTER RETARDING THE THROTTLE ON THE NR 1 ENGINE ASSY. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999081400534 19990814 00534 NE 1999 8 14 EISA99128 2 19990520 A 7412 103538751 EXCITOR BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE INOPERATIVE A EISA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 275WC 20549 NR 3 ENGINE WOULD NOT LIGHT OFF. REMOVED AND REPLACED NR 3 ENGINE IGNITION EXCITOR. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 1999081400535 19990814 00535 NE 1999 8 14 GAIA9972 2 19990608 A 7261 80730401 OIL TUBE BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE BROKEN A GAIA A E UNSCHED LANDING ENGINE SHUTDOWN K Y FLUID LOSS ENGINE STOPPAGE CL CLIMB 1 SW 07 281KH 21105 FLT 504 - TOL - DURING CLIMB-OUT, HAD OIL PRESSURE ON NR 1 ENGINE DROP TO 5-10 PSI. PRECAUTIONARY SHUT DOWN NR 1 ENGINE . THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. FOUND NR 1 BEA RING PRESSURE TUBE BROKEN. REMOVED AND REPLACED THE SAME. RAN AND LEAKED CHECKED THE ENGINE AND NO DEFECTS WERE NOTED. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 1999081400536 19990814 00536 NE 1999 8 14 GAIA9974 2 19990616 A 7320 228195 O-RING BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE DETERIORATED A GAIA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 SW 07 284KH 21108 DURING BOS-TOL - FLT 715 - DURING DESCENT AT FL280, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE WOULD ONLY PRODUCE PART IAL POWER. THE FLIGHT CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN ON THE NR 1 ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT CONTINUED TO TOL AND LANDED WITHOUT FURTHER PROBLEMS. FOUND THE P/D VALVE PRESSURE LINE PACKING BLOWN OUT. R EPLACED THE SAME AND MAIN OIL STRAINER IAW JT8DMM. NR 1 ENGINE OPERATIONAL AND LEAK CHECKS GOOD. THE AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 1999081400537 19990814 00537 NE 1999 8 14 F3LA99095 2 19990630 A 7230 IGV BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK, INSPECTION REPORTED NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE AT 2 O'CLOCK POSITI ON. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-2 3-01, REPAIR NR 14, SUBTASK 1, 2, 3 AND 4. STRESS RELIEVED PER P/W E/M 72-23-01, REPAIR 14. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999081400538 19990814 00538 NE 1999 8 14 F3LA99096 2 19990630 A 7230 IGV BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DEN - DURING C-CHECK INSPECTION REPORTED, NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE, 10 O'CLOCK POSITIO N. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-23 -01, PAGES 901 AND 902, SUBTASK 1, 2, 3 AND 4. STRESS RELIEVED PER P/W E/M 72-23-01. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999081400539 19990814 00539 NE 1999 8 14 EIA990119 2 19990614 A 7200 ENGINE BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE NR 2 FLAMED OUT A EIAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 NM 09 470EV 20653 662479 TPE - AT FLIGHT LEVEL 410, AIRCRAFT ENCOUNTERED A THUNDERSTORM WHICH DID NOT SHOW UP ON RADAR. THE NR 2 ENGINE FLAMED O UT. AIRCRAFT THEN DESCENDED TO FLIGHT LEVEL 330 AND ACCOMPLISHED AN INFLIGHT RESTART. INSPECTION AT TPE FOUND NO DISCR EPANCIES. LINE MAINTENANCE PLANNING REQUEST HAS BEEN ISSUED FOR A DETAILED INSPECTION. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999081400540 19990814 00540 NE 1999 8 14 EIA990116 2 19990507 A 7230 771841 BLADE BOEING 747 747SR46 NM PWA JT9 JT9D7AH 52054 NE NR 3 ENGINE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 21033 662248 BIRDSTRIKE ON THE NR 3 ENGINE. UPON INSPECTION FOUND DAMAGE TO NR 33 AND NR 34 BLADES. REPLACED DAMAGED BLADES PER EIA MAINTENANCE 'F' CARD NR F7208. OPS CHECKED PER 71-00-00. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999081400541 19990814 00541 NE 1999 8 14 EIA990120 2 19990621 A 7230 COMPRESSOR BOEING 747 747SR46 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE STALLED A EIAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 09 477EV 20784 ORD - AT FL310 PROCEEDING TO KLAX NEAR HLA 1.3 HOURS AFTER DEPARTURE, NR 1 ENGINE EXPERIENCED COMPRESSOR STALL FOLLOWED BY FLAMEOUT. EGT WENT TO 960 CELCIUS FOR 4-5 SECS ENGINE SHUTDOWN. DESCENDED TO FL240 N1 AT 17 PERCENT, OIL PRESSURE A T 11 PSI. CONTACTED TECH CENTER AT MMV AND ATTEMPTED RELIGHT UPON TECH CENTER REQUEST, UNSUCCESSFUL AS N2<23 PERCENT WH ILE EGT OVER 600 CELSIUS, ADVISED TECH CENTER RETURNING TO KORD. WEATHER AT KORD WAS VFR. ACCOMPLISHED AIR TURN BACK A ND UNEVENTFUL 3 ENGINE LANDING. CONDUCTED EXTERIOR INSPECTION OF ENGINE. DISCOVERED METAL IN THE TAILPIPE. REMOVED AN D REPLACED NR 1 ENGINE AS PER EIA TASK FORM 9724001 AND ACCOMPLISHED HIGH POWER RUNUP AS PER 9724007. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999081400543 19990814 00543 NE 1999 8 14 ASOA99057 2 19990701 A 7320 3038046 P3 LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RT ENGINE BROKEN A ASOA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SO 11 639AS 120283 FLT 4882 - JUST BEFORE LANDING CHECK, FO NOTICED POWER LOSS ON RIGHT ENGINE NP FLUCTUATING 10-20 PERCENT. ENGINE THEN F AILED THE FLIGHT CHECK WAS CALLED FOR AND EXECUTED, FOLLOWED BY SINGLE ENGINE AND LANDING CHECKLIST, WHILE CONTINUING TO APPROACH. TOWER WAS ADVISED ON SHORT FINAL AND EMERGENCY WAS DECLARED. FA WAS NOTIFIED AFTER SAFE LANDING DUE TO TIME CONSTRAINT. MAINTENANCE REPLACED P3 LINE ON THE RIGHT ENGINE. TEST RUNS GOOD ON THE GROUND. OPERATIONAL CHECK NORMAL . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999081400544 19990814 00544 WP 1999 8 14 AALA990791 1 19990527 A 7830 0711346003 MANIFOLD DOUG DC9 DC982 3022082 WP NR 1 TR UNIT LEAKING A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 287AA 49299 DFW - FLT 2217 - EN ROUTE ORD-DFW - CREW NOTED ACRID SMOKE IN FIRST CLASS CABIN. EXTINGUISHED OVERHEAD LIGHT AND SMOKE DISSIPATED. WHEN OVERHEAD LIGHT WERE TURNED BACK ON THE SMOKE AND FUMES RETURNED, IMMEDIATELY TURNED OFF OVERHEAD LIGHT S. LANDED DFW WITHOUT INCIDENT. INSPECTED ALL FIRST CLASS CABIN OVERHEAD LIGHTS. ALL LIGHTS NORMAL WITH NO SMOKE BEIN G NOTED. NR 1 THRUST REVERSER MANIFOLD LEAKING HYDRAULIC FLUID INTO THE APU SUSPECT THIS IS CAUSING THE SMOKE IN THE CA BIN. THE NR 1 THRUST REVERSER MANIFOLD WAS PRECAUTIONARY REPLACED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999081400545 19990814 00545 NM 1999 8 14 USAA990558 1 19990610 A 5320 693535214 CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND .12 5INCH CRACK IN TIE CLIP AT STATION 727C STRINGER 6L. DEFECTIVE PART REPLACED WITH IDE NTICAL PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999081400546 19990814 00546 NM 1999 8 14 USAA990557 1 19990610 A 5320 693535214 CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND .125 INCH CRACKED TIE CLIP AT BS 727A STRINGER 5 RT. DEFECTIVE PART REPLACED WITH IDENTIC AL PART NR PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999081900001 19990819 00001 WP 1999 8 19 DHL9980201C 1 19990502 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CARGO COMPT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 AT C-CHECK, FWD LOWER CARGO COMPARTMENT HAS SECTION OF CHANNEL TRACK WITH EVIDENCE OF CORROSION AND SEVERAL CRACKS ON SU RFACE. REMOVED CRACKED SECT OF TRACK CHANNEL IAW, CLEANED TRACK CHANNEL AREA PER SRM. OK TO TREAT, PRIME AREA AND NEW CHANNEL. TREATED, PRIMED AREA AND NEW SECTION OF CHANNEL. OK TO INSTALL NEW SECT OF CHANNEL. INSTALLED NEW SECT PER S RM. 2 L 7 4 4F RT 4A25 1999081900002 19990819 00002 NM 1999 8 19 GAIA99103 1 19990722 A 5312 BULKHEAD BEAM BOEING 727 727223 1384074 NM BS 1183 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6838 20191 DURING A 'ZERO' LIGHT 'C' INSPECTION BEING PERFORMED IN OSC AT AMERICAN INTERNATIONAL AIRWAYS REPAIR STATION, IT WAS DIS COVERED THAT AT THE 1183 PRESSURE BULKHEAD RBL 46.93, VERTICAL BEAM WAS CRACKED FROM WL 198 TO WL 202. REPAIRED IAW AIA EDR B2-06526, DER APPROVED ON 8110-3 DATED MAY 20, 1999. (X) 2 L 7 3 4F A3WE 1999082000001 19990820 00001 SO 1999 8 20 LR7A9955 1 19990811 A 2150 75024416 GASKET LKHEED 382 382G 526414U SO BS 497 FAILED A LR7A H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CR CRUISE 1 AL 03 401LC 4606 CARGO COMPARTMENT REFRIGERATION OVERHEAT LIGHT CAME ON IN FLIGHT, ANC TO FAI. TURNED CARGO COMPARTMENT PAC OFF AND LIGH T WENT OUT. DEFERRED CARGO COMPARTMENT AIR CONDITIONING PACK PER MEL 21-1 AND COMPLIED WITH SPECIAL PROCEDURE 1. DMI NR 00605. ON RETURN TO ANC CHANGED BLEED AIR GASKET FOR HEAT EXCHANGER INLET DUCT DUE FAILED. SYSTEM OPS CHECK NORMAL PER SMP 581 21-50. CLEARED DMI 00605. 2 H 7 4 4T A1SO 1999082000002 19990820 00002 NM 1999 8 20 AWXA9900258 1 19990811 A 3244 AS11506D0346 LINE BOEING 737 737277 1384570 NM NR 3 BRAKE ASSY LEAKS A AWXA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 WP 28 185AW 22652 GATE RETURN DUE TO NO BRAKES. LOSS OF FLUID, HYDRAULIC SYS 'A' (NO CURRENT RELATED HISTORY). REPLACED NR 3 BRAKE LINE AND SERVICED. OPS CHECK GOOD 2 L 7 2 4F RT A16WE 1999082000003 19990820 00003 NM 1999 8 20 AWXA9900259 1 19990812 A 3350 A31038 BATTERY PACK BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 164AW 23625 EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK, NO CURRENT RELATED HISTORY. 2 L 7 2 4F RT A16WE 1999082000004 19990820 00004 WP 1999 8 20 9903089979 1 19990807 A 3397 WIRE DOUG DC9 DC931 3022065 WP TAIL COMPT BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPAIRED SPLICE IN WIRING HARN ESS TO POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999082000005 19990820 00005 WP 1999 8 20 9903099950 1 19990807 A 5260 HANDLE DOUG DC9 DC932 3022066 WP AIRSTAIR DOOR NOT STOWED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 01 9346 47376 AIRFRAME VIBRATION/OSCILLATION OCCURRED IN FLIGHT. CREW DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO MEM. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FORWARD AIRSTAIR DOOR HANDLE NOT COMPLETELY STOWED AND LOOSE. RESTOWED HAN DLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999082000006 19990820 00006 NM 1999 8 20 9903106740 1 19990805 A 2612 FIRE LOOP BOEING 747 747251F 1384898 NM NR 3 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 64OUS 23888 DURING CLIMB, THE NR 3 ENGINE FIRE WARNING ACTIVATED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED T HE IGNITER PLUG BOSS, HIGH STAGE VALVE, AND HIGH STAGE CONTROLLER. OPERATIONAL CHECK GOOD. EXACT FAULT CAUSING DISCREP ANCY TO BE DETERMINED. 2 L 7 4 4F A20WE 1999082000007 19990820 00007 1999 8 20 9903116615 4 19990809 A 2330 20072 VIDIO PROJECTOR BOEING 747 747251B 1384892 NM CABIN FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 615US 20360 DURING CLIMB, FUMES EMITTED FROM THE FIRST CLASS GALLEY. TURNED OFF GALLEY POWER AND RETURNED TO NRT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST CLASS VIDEO PROJECTOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999082000008 19990820 00008 NE 1999 8 20 9903126608 2 19990805 A 7321 FUEL CONTROL BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 01 608US 19785 662693 AT FL370, THE CREW REPORTED NR 4 ENGINE FLAMED OUT. THE ENGINE WAS SECURED PER THE COM, AND NO RESTART WAS ATTEMPTED. T HE FLIGHT DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND METAL DEBRIS IN THE E NGINE FUEL FILTER. THE FUEL CONTROL UNIT AND FUEL PUMP WERE CHANGED. THE SUBSEQUENT ENGINE RUN WAS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1999082000009 19990820 00009 WP 1999 8 20 9903131162 1 19990806 A 3260 DNLOCK SENSOR DOUG DC10 DC1040 3023508 WP RT MLG FAILED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 162US 46771 ON DESCENT INTO SFO, UPON GEAR EXTENSION, GOT RMG UNSAFE INDICATION. RECYCLED GEAR AND STILL INDICATED UNSAFE. VISUAL CHECK OF GEAR SHOWED DOWN. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED GEAR DOWNLOCK SENSOR. OPERATION C HECKS GOOD. 2 L 7 3 4F A22WE 1999082000010 19990820 00010 NE 1999 8 20 9903141154 2 19990805 A 7532 PRBC VALVE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 GL 01 154US 46763 686166 UPON POWER REDUCTION AT FL330, THE NR 1 ENGINE COMPRESSOR STALLED AND THEN FLAMED OUT. THE ENGINE WAS SECURED, AND REST ARTED NORMALLY AT FL300. ENGINE OPERAITON WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER TAFI WITH NO DEFECTS NOTED. THE PRBC, CONVERTER VALVE AND PS4 RESTRICTOR WERE REPLACED. AN ENGINE RUN WAS PERFORM ED, INCLUDING BLEED CHECKS AND TO TAKEOFF POWER, WITH NO DEFECTS NOTED. 2 L 7 3 4F 4 F A22WE E20EA 1999082000011 19990820 00011 EA 1999 8 20 COMA9960427 1 19990808 A 5720 601R1206245 LEADING EDGE CNDAIR CL600 CL6002B19 EA RT WING DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 RIGHT WING OUTBOARD LEADING EDGE HAS A DENT. REPAIRED RIGHT WING OUTBOARD LEADING EDGE AT FS 279.699 AND 288.641 IAW WV AC EO NR 601R-57-0211. 2 L 7 2 4F RT A21EA 1999082000012 19990820 00012 EA 1999 8 20 COMA9960428 1 19990809 A 3211 601R32054K1A BUSHING CNDAIR CL600 CL6002B19 EA LT & RT MLG MIGRATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 LEFT HAND AND RIGHT HAND MLG AFT TRUNNION BUSHING MIGRATED. PERFORMED SERVICE BULLETIN 601R-32054. REPLACED LEFT HAND AFT AND RIGHT HAND AFT TRUNNION BUSHING. 2 L 7 2 4F RT A21EA 1999082000013 19990820 00013 EA 1999 8 20 COMA9960429 1 19990809 A 5315 601R3867317 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLOOR PLATE AT FS 349 BETWEEN LBL 42 AND LBL 27 CORRODED (P/N 601R38673-17). PERFORMED A MAJOR REPAIR REMOVED CORRODED FLOORBEAM PLATE BETWEEN LBL 42 AND LBL 27 FS 349.00. INSTALLED NEW PLATE (P/N 601R38673-17) IAW WVAC EO 601R-53-02-6. 2 L 7 2 4F RT A21EA 1999082000014 19990820 00014 EA 1999 8 20 COMA9960430 1 19990809 A 5315 601R3867325 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLOOR PLATE AT FS 349.00 BETWEEN RBL 27, AND RBL 42 CORRODED (P/N 601R38673-25). PERFORMED MAJOR REPAIR, REMOVED CORROD ED FLOORBEAM PLATE BETWEEN RBL 27 AND RBL 42 FS 349. INSTALLED NEW PLATE IAW WVAC EO 601R-53-02-6, 707ST6-100. 2 L 7 2 4F RT A21EA 1999082000015 19990820 00015 EA 1999 8 20 COMA9960431 1 19990809 A 5320 601R3111357 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 L ANGLES CRACKED ON INBOARD AND OUTBOARD SIDES OF LBL 9 FLOORBEAM FS 280 (P/N 601R31113-57). PERFORMED MAJOR REPAIR REM OVED CRACKED INBORAD AND OUTBOARD SIDES OF LBL 9 FLOORBEAM FS 280. INSTALLED NEW ANGLES IAW WVAC EO 601R-53-0217. 2 L 7 2 4F RT A21EA 1999082000016 19990820 00016 EA 1999 8 20 COMA9960432 1 19990809 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA BS 315-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 SERVICE DOOR THRESHOLD ANGLE RBL 42 CORRODED BETWEEN FS 315 TO FS 349 (P/N 601R38303-105). PERFORMED A MAJOR REPAIR, RE MOVED CORRODED THRESHOLD ANGLE FOR SERVICE DOOR. REPLACED WITH NEW ANGLE (P/N 601R38303-105) IAW WVAC EO 601R53-0204. 2 L 7 2 4F RT A21EA 1999082000017 19990820 00017 EA 1999 8 20 COMA9960433 1 19990809 A 5315 601R3111357 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 281 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 LBL 9 FLOORBEAM WEB (P/N 601R31113-29) CRACKED APPROXIMATELY 2 INCHES ON OUTBOARD SIDE OF FLOORBEAM FS 281.00 UNDER L AN GLE (P/N 601R31113-57). REMOVED CRACKED WEB FROM OUTBOARD SIDE OF FLOORBEAM LBL 9 BETWEEN FS 280.00 AND 292.00. INSTAL LED NEW WEB IAW WVAC EO 601R-53-0215. 2 L 7 2 4F RT A21EA 1999082000018 19990820 00018 EA 1999 8 20 COMA9960434 1 19990809 A 5753 601R145552 HINGE CNDAIR CL600 CL6002B19 EA RT TE FLAP GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 UPON REPLACEMENT OF RIGHT HAND OUTBOARD, OUTBOARD HINGE ARM DISCOVERED A CHAFE AREA ON HINGE ARM (P/N 601R14555-2). REP AIRED IAW WVAC EO 601R-57-0213. 2 L 7 2 4F RT A21EA 1999082000019 19990820 00019 EA 1999 8 20 COMA9960435 1 19990809 A 5315 601R3867319 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLOOR PLATE AT FS 349 BETWEEN LBL 27 AND LBL 9 CORRODED (P/N 601R38573-19). PERFORMED A MAJOR REPAIR, REMOVED CORRODED FLOORBEAM PLATE BETWEEN LBL 27 AND LBL 9 FS 349.00 AND INSTALLED NEW FLOORBEAM PLATE (P/N 601R38673-19) IAW WVAC EO 601R -53-0206. 2 L 7 2 4F RT A21EA 1999082000020 19990820 00020 EA 1999 8 20 COMA9960436 1 19990809 A 5320 601R31527 ANGLE CNDAIR CL600 CL6002B19 EA BS 310 & 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 ANGLE AT FS 310 TO 349 LBL 42 (PAX DOOR ANGLE) CORRODED (P/N 601R31527-49R). PERFORMED A MAJOR REPAIR, REMOVED CORRODED FLOOR ANGLE AT PAX DOOR ENTRANCE. MANUFACTURED NEW ANGLE FROM (P/N S339ZT), 7075T6511, P/O 5051/2 AND INSTALLED IAW WV AC EO 601R-53-0205. 2 L 7 2 4F RT A21EA 1999082000021 19990820 00021 EA 1999 8 20 COMA9960437 1 19990809 A 5320 601R3111358 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 L ANGLES CRACKED ON INBOARD AND OUTBOARD SIDES OF RBL 9 FLOORBEAM FS 280.00 (P/N 601R31113-58). PERFORMED MAJOR REPAIR REMOVED CRACKED ANGLES ON INBOARD AND OUTBOARD SIDES OF RBL 9 FLOORBEAM FS 280. INSTALLED NEW ANGLES IAW WVAC EO 601R-5 3-0212A. 2 L 7 2 4F RT A21EA 1999082000022 19990820 00022 EA 1999 8 20 COMA9960438 1 19990809 A 5315 6003401717 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FS 280 CRACKED JUST OUTBOARD OF FLOORBEAM AT RBL 9 (P/N 600-34017-17). MAJOR REPAIRED FS 280 CRACK JUST OUTBOARD OF FLO ORBEAM RBL 9 ON FS 780.00 600-34017 IAW WVAC EO 601R-53-0212A. 2 L 7 2 4F RT A21EA 1999082000023 19990820 00023 EA 1999 8 20 COMA9960439 1 19990810 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 975CA 7150 FLAPS FAIL MESSAGE. REPLACED THE PDU. 2 L 7 2 4F RT A21EA 1999082000024 19990820 00024 EA 1999 8 20 COMA9960440 1 19990809 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 310 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLOORBEAM CAP RBL 27 CORRODED BETWEEN FS 310 TO FS 362 (P/N 601R31113-67). ALSO, MINOR CORROSION AT RIVNUTS BETWEEN FS 349 AND FS 409. PERFORMED A MAJOR REPAIR REMOVED CORRODED SECTION OF FLOORBEAM CAP RBL 27 BETWEEN FS 315 TO FS 362 (P/N 601R31113-67) AND SPLICED IN NEW SECTION (P/N 601R31113-67) IAW REO 601R-53-00-027 EV NC DATED 3 NOV 97. 2 L 7 2 4F RT A21EA 1999082000025 19990820 00025 EA 1999 8 20 COMA9960441 1 19990809 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 319 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FLOORBEAM CAP LBL 27 CORRODED BETWEEN FS 319, FS 339 (P/N 601R31113-67) CORRODED BEYOND LIMITS OF REO 601R-53-005 SPLICE IN NEW SECTION IAW REO 601R-53-00-027. REMOVED CORRODED SECTION OF FLOORBEAM LBL 27 BETWEEN FS 319.00 TO FS 339.00 (P/ N 601R31113-67) AND SPLICED IN NEW SECTION OF BEAM CAP (P/N 601R31113-67) PERFORMED THIS MAJOR REPAIR IAW REO-601R-53-00 -027 REV NC DATED 3NOV97. 2 L 7 2 4F RT A21EA 1999082000026 19990820 00026 EA 1999 8 20 COMA9960442 1 19990808 A 5311 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 FRAME AT FS 718 RHS DISCOVERED CRACK 4 INCHES ABOVE STR 11 IN THE FLANGE ATTACHING TO THE SKIN AND CRACKED IN 2 PLACES I N THE RADIUS BELOW STR 11 AND CRACKED IN DOUBLER 2 ON AFT SIDE OF FLAME STR 11. REPAIRED FRAME AT FS 718 STR 11 IAW WVA C EO 601R-53-0207A AND REPAIRED DOUBLER IAW WVAC EO 601R-53-0209. 2 L 7 2 4F RT A21EA 1999082000027 19990820 00027 EA 1999 8 20 COMA9960443 1 19990808 A 5311 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 FRAME AT FS 718 LT DISCOVERED TO BE CRACKED IN THE RADIUS EXTENDING 3 INCHES ABOVE STR 11, IN THE FLANGE BELOW STR 11, A ND IN THE DOUBLER ON AFT SIDE OF FRAME AT STR 11. REPAIRED FRAME AT FS 718 IAW WVAC EO 601R-53-0208A AND REPAIRED DOUBL ER IAW WVAC EO 601R-53-0210. 2 L 7 2 4F RT A21EA 1999082000028 19990820 00028 NM 1999 8 20 QXEA990139 1 19990810 A 3231 MECHANISM DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 829PH 304 MWH- GEAR DOOR LIGHT ILLUMINATED. GEAR DOOR REMAIN OPEN. ADJUSTED RIGGING OF LEFT HAND MAIN LANDING GEAR REAR/CENTER D OOR ACTUATOR, FUNCTIONAL CHECK OF GEAR GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999082000029 19990820 00029 EU 1999 8 20 QXEA9901536 1 19990807 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU COCKPIT DOOR FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 PDX- EXIT LIGHT OVER COCKPIT DOOR HAS LIGHT INOPERATIVE. REPLACED CIRCUIT BOARD, OPERATIONAL TEST GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1999082000030 19990820 00030 EU 1999 8 20 QXEA9901537 1 19990810 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 GEG- BOTH OVERHEAD EXIT SIGNS AT MID CABIN INOPERATIVE. REPLACED CIRCUIT BOARDS, OPERATIONAL TEST GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1999082000031 19990820 00031 NM 1999 8 20 QXEA9901538 1 19990810 A 3350 5515800106 LIGHT GRIMES 10005511 DHAV DHC8 DHC8202 2809007 NM CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 348PH 484 PDX- EMERGENCY LIGHT LANTERN OVER COCKPIT DOOR NOT CHARGED. REPLACED EMERGENCY LIGHT IN OVERHEAD COCKPIT. OPERATIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999082000032 19990820 00032 NM 1999 8 20 99FDEA00329 1 19990811 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 MAIN DOCK UPPER FUSELAGE SEAT TRACK FOUND CRACK AT BS 635 X=8.5 RT. - 3.2 IN, AT BS 635 X 27.5 RT. - 3.5. AT BS 635 X 4 7.5 RT -4.3 IN, AT BS 635 X = 47.5 LH-4.5. *S/D* FASTENERS REMOVED AND SEAT TRACK TRIMMED & REWORKED PER SRM 53-42-01. 2 L 7 3 4F RT A22WE 1999082000033 19990820 00033 NM 1999 8 20 99FDEA00330 1 19990812 A 3260 ACCESSORY UNIT BOEING 727 72722C 138400F NM LANDING GEAR INOP A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 112FE 19890 RETRACTION REPEAT GEAR WARN LIGHT PROBLEMS. SYMPTOMS INDENTICAL TO ARD REPORT ON 8/11/99. REMOVED AND REPLACED LAND GE AR ASSY UNIT PER MM 32-09-111-5 PG 1-5 GROUND TEST GOOD. REMOVED AND REPLACED ANNUNCIATOR PANEL PER MM 32-62-001-4. 2 L 7 3 4F A3WE 1999082000034 19990820 00034 WP 1999 8 20 99FDEA00331 1 19990812 A 2613 D10330021 CONTROLLER DOUG DC10 DC1030F 3023504 WP COCKPIT MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 25 303FE 46802 ON TAKEOFF, PNEUMATIC TEMP HI LIGHT FLICKERED INTERM ON PILOT ANNUNCIATOR PANEL. REMOVED AND REPLACED OVERHEAD WARN AND CAUTION ANNUN, SYS LOGIC CONTROLLER UNIT, UNIT PER MM 33-15-03-2. OPS CK GOOD. 2 L 7 3 4F RT A22WE 1999082000035 19990820 00035 NM 1999 8 20 SCNA99100 1 19990810 A 3397 WIRE BOEING 727 727225 1384077 NM GALLEY BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECK, THE FORWARD FOUR EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED TOP COVER AND BASE AT FORWARD GALLEY. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999082000047 19990820 00047 NE 1999 8 20 99ZZZX3001 2 19990730 A 7311 3039259 COOLER BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE NR 1 ENGINE FAILED A DBCA K NONE R J PARTIAL RPM/PWR LOSS WARNING INDICATION IN INSP/MAINT 1 GL 13 670DF 385 WA11014 BB1631 PCEPJ0208 WHILE PERFORMING RUN-UP CHECKS, NR 1 ENGINE WOULD NOT ACCELERATE. TROUBLESHOT TO BAD FUEL/OIL HEAT EXCHANGE P/N 3039259 , S/N WA11014. INSTALLED NEW FUEL OIL HEAT EXCHANGE P/N 3039259, S/N W11769. OPERATIONS CHECKED OK. 1 L 7 2 4T 4 T A24CE E4EA 1999082000051 19990820 00051 CE 1999 8 20 99ZZZX3005 1 19990715 A 3260 6838 BULB LEAR 35 35A 5170602 CE COCKPIT FAILED A BSYA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 07 39DK 480 CMH - LEFT MAIN GEAR NO DOWN AND LOCK INDICATION. DID A FLY-BY CMH TOWER, LANDING LIGHTS WERE ON. LANDED, NO PROBLEM. REMOVED AND REPLACED BULB. OPS CHECKS OK. 2 L 7 2 4F A10CE 1999082000052 19990820 00052 CE 1999 8 20 99ZZZX3006 1 19990720 A 2810 993800005 FUEL CELL BEECH 99 99 1154002 CE NACELLE LEAKING A TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 24BH U67 PILOT REPORTED FUEL LEAKING FROM AREA OTHER THAN THE FUEL SUMPS IN THE VICINITY OF THE NACELLE. INSPECTION REVEALED VAR IOUS SMALL LEAKS IN THE BLADDER OF THE CELL. THE CELL WAS REPLACED WITH A SERVICEABLE CELL AND AIRCRAFT TANK LINER RE-T APED WITH CHAFE RESISTANT FUEL BAY TAPE. IT WAS DETERMINED THE CAUSE OF THE LEAKS WAS NORMAL WEAR. THE AGE OF THE FUEL CELL WAS UNKNOWN. TANK HANGERS WERE STILL IN PLACE AT TIME OF REMOVAL OF THE DEFECTIVE FUEL CELL. 1 L 7 2 3T A14CE 1999082000065 19990820 00065 1999 8 20 99ZZZX3022 4 19990720 A 3452 066107100 TRANSPONDER ALLIEDCONTRL KXP756 BELL 206 206L3 1182108 SW COCKPIT SHORTED H K NONE O OTHER IN INSP/MAINT 1 SW 03 53702 2251 51249 MOISTURE TRAPPED UNDER HEADER CAUSED A SHORT ON TH THE BOARD AT THE 180VAC LINE. BURNED BOARD AND HEADER. 1 G 7 1 3U H2SW 1999082000066 19990820 00066 EU 1999 8 20 VTZA990197 1 19990628 A 3245 TIRE BAG JETSTM JETSTM3201 1500217 EU NLG LOW A VTZA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 EA 27 471UE 821 IAD/ROA - FLT 7190 - DURING TAKEOFF AT 0920 HOURS, AIRCRAFT ABORTED TAKEOFF DUE TO PULL TO LEFT. MAINTENANCE FOUND NOSE TIRE PRESSURES MISMATCHED. SERVICED NOSE TIRES AND RT MAIN TIRE. ALSO, INSPECTED BOTH BRAKES AND FUNCTION CHECKED FOR PROPER OPERATION, NO DEFECTS NOTED. HIGH SPEED TAXI CHECK SATISFACTORY. AIRCRAFT RELEASED AND RETURNED TO SERVICE. ( X) 2 L 7 2 4T RT A56EU 1999082000067 19990820 00067 EU 1999 8 20 VTZA990196 1 19990628 A 7712 SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE MALFUNCTIONED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 474UE 849 IAD/PIT - FLT 7385 - DURING TAKEOFF AT 1340 HOURS, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE FAILING TO MAKE SCHEDULED T ORQUE. MAINTENANCE CALIBRATED RT TORQUE SIGNAL CONDITIONER AND GROUND RAN ENGINES. ALL PARAMETERS WITHIN LIMITS. AIRC RAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999082000068 19990820 00068 EU 1999 8 20 VTZA990195 1 19990627 A 7722 8974768 RESISTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 476UE 884 IAD/GSO - FLT 7531 - DURING TAKEOFF AT 1115 HOURS, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE LOW TORQUE. AIRCRAFT RETUR NED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED P3 GASKET AND EGT COMPENSATING RES ISTOR. OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999082000069 19990820 00069 EU 1999 8 20 VTZA990217 1 19990718 A 2611 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU CARGO BAY CONTAMINATED A VTZA O OTHER N FALSE WARNING DE DESCENT 1 EA 27 483UE 898 IAD/ABE - FLT 7158 - DURING DESCENT AT 2300 HOURS, MAKE SCHEDULED LANDING WITH ONE DISCREPANY WHICH WAS BAGGAGE BAY SMOK E DETECTOR WARNING LIGHT ILLUMINATED. AIRCRAFT LANDED, WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AN D CLEANED SMOKE DETECTOR, OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999082000070 19990820 00070 NE 1999 8 20 VTZA990219 2 19990712 A 7260 31059291 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 319UE 41042 IAD/ILM - FLT 7371 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AND RETURNED TO IAD DUE TO RT OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RIGHT CHIP DETECTOR ASSY. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082000071 19990820 00071 1999 8 20 VTZA990213 3 19990706 A 6112 B4024555 DEICE BOOT BAG JETSTM JETSTM3201 1500217 EU RT PROPELLER SEPARATED A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 480UE 894 PHL/IAD - FLT 7653 - DURING CLIMB AT 0940 HOURS, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT PROP MAT DEPARTED AIRCRA FT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED DE-ICE BOOT ON RT PROP, OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999082000072 19990820 00072 EU 1999 8 20 VTZA990212 1 19990705 A 6120 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU NR 1 ENGINE OUT OF ADJUST A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 481UE 895 IAD/GSO - FLT 7161 - DURING TAKEOFF AT 0645 HOURS, CREW ABORTED TAKEOFF DUE TO NR 1 ENGINE RPM ROLLED BACK SLOWLY TO 99 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED PROP GOVERNOR. OPS CH ECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999082000073 19990820 00073 EU 1999 8 20 VTZA990211 1 19990609 A 7712 9495411 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE FAILED A VTZA O OTHER X ENGINE FLAMEOUT IN INSP/MAINT 1 EA 27 485UE 901 IAD/PHI - FLT 7652 - DURING TAXI AT 0700, AIRCRAFT LT ENGINE FLAMED OUT DURING MORNING TTL TEST. AIRCRAFT WAS EVACUATED ON THE RUNWAY. MAINTENANCE REMOVED AND REPLACED LT TTL VALVE AND TTL CONTROLLER. RUN-UP OKAY. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1999082000074 19990820 00074 WP 1999 8 20 VTZA990092 2 19990520 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT MALFUNCTIONED A VTZA E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 27 472UE 823 FLT 7272 - PRIOR TO TAKEOFF, DURING TORQUE AND TEMPERATURE LIMIT TEST, FLIGHT CREW NOTED DROP IN FUEL FLOW AND RPM ON LT ENGINE. TEST REPEATED 3 TIMES WITH SAME RESULT. ON THIRD ATTEMPT, FLIGHT CREW NOTED SMOKE COMING FROM LT ENG, FLIGHT CREW ELECTED TO SHUT DOWN BOTH ENGINES AND EVACUATE ACFT. ENGINES WERE SHUT DOWN AND ACFT EVACUATED WITHOUT FURTHER INC IDENT EXCEPT THAT DURING EVACUATION, F/O SUSTAINED A BUMP ON THE HEAD (EXAMINED BY PARAMEDIC ON SCENE, RELEASED) ACFT T OWED TO RAMP FOR MAINT. ACFT EXAMINED FOR EVIDENCE OF FIRE, NONE FOUND. MAINT PERFORMED TORQUE AND TEMP LIMIT TEST ON BOTH ENGINES. NO FAULT NOTED. ALL PARAMETERS NORMAL. UNABLE TO DUPLICATE ANY FAULT. ACFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1999082000075 19990820 00075 EU 1999 8 20 VTZA990210 1 19990420 A 2160 7252C000 VALVE BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 476UE 884 IA/SYR - FLT 7261 - DURING TAKEOFF AT 0830 HOURS, MADE AN UNSCHEDULED LANDING DUE TO LT PACK OVER-TEMP WARNING LIGHT ILL UMINATED. CREW REPORTED FUMES ENTERING THE COCKPIT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE I NSPECTED AND OPENED DMI 47472, MEL 21-5, MAINTENANCE CLOSED DMI 47472 ON 4-20-99 BY REMOVING AND REPLACING LT TEMP CONTR OL VALVE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999082000076 19990820 00076 EU 1999 8 20 VTZA990198 1 19990628 A 2910 137311D1443 LINE BAG JETSTM JETSTM3201 1500217 EU HYD SYSTEM FAILED A VTZA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 27 482UE 897 FLT 7232 - ORF-IAD - DURING APPROACH, AIRCRAFT INDICATED RIGHT HYDRAULIC PUMP LOW, THEN ALL HYDRAULIC PRESSURE LOST. AI RCRAFT LANDED AT IAD AFTER AN EMERGENCY WAS DECLARED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED HYDRAUL IC RETURN LINE. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999082000077 19990820 00077 NE 1999 8 20 UF6A990122 2 19990129 A 7320 EEC BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE MALFUNCTIONED A UF6A C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 859AW 2036 124242 GRB - FLT 5738 - ON TAKEOFF, NR 1 ENGINE TORQUE DECREASED BY APPROXIMATELY 20 PERCENT. FURTHER POWER LEVEL INCREASES HA D NO EFFECT. MAINTENANCE CLEARED THE NR 1 EEC AND PERFORMED NUMEROUS POWER ASSURANCE RUNS IN TAKEOFF CONFIGURATION FOR 3 MINUTES EACH IAW P&W MM 72-00. ALL INDICATIONS NORMAL, WITH NO DEFECTS NOTED. (X) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999082000078 19990820 00078 EU 1999 8 20 UF6A990311 1 19990311 A 3350 58785 LIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 ORD - 5732 - REQUEST INSPECTION OF EMERGENCY EXIT FLOOR LIGHTS. MAINTENANCE REMOVED AND REPLACED THE POWER STRIP ADJAC ENT TO ROW 7. SYSTEM OPSCHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999082000079 19990820 00079 SW 1999 8 20 99ZZZX3023 1 19990522 A 3210 407050202115 CROSSTUBE A290 BELL 407 407 SW MLG SKID CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 497AL 53172 THE CROSSTUBE WAS REMOVED FROM SERVICE DUE TO AN INDICATION OF CORROSION IN THE AREA OF CROSS TUBE TO SKIDTUBE JUNCTURE. FURTHER INVESTIGATION REVEALED EXCESSIVE CORROSION UNDER THE SADDLES. THIS OPERATOR VIEWS THIS AS INADEQUATE MANUFACT URING AND REQUESTS SPECIAL WARRANTY CONSIDERATION. ITEM WAS REPLACED WITH NEW. 1 G 7 1 3U O H2SW 1999082000084 19990820 00084 SW 1999 8 20 99ZZZX3028 1 19990622 A 6510 407340340101 DISC PACK 407040001001 BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL 48 RNFS2124 53284 DURING RECURRING INSPECTION OF AD 97-24-17, ONE OUTBOARD DISC IN THE DISC PACK IS CRACKED. SUBMITTER STATED THIS IS THE SECOND CRACKED NEW STYLE DISC PACK IN 50 HOURS. 1 G 7 1 3U O H2SW 1999082000085 19990820 00085 SW 1999 8 20 99ZZZX3029 1 19990613 A 6510 407340340101 DISC PACK 407040001001 BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL 48 RNFS2099 53284 DURING RECURRING INSPECTION OF AD 97-24-17, BOTH OUTBOARD DISCS IN THE DISC PACK ARE CRACKED. SUBMITTER STATED THIS IS THE FIRST OCCURRENCE WITH THE NEW STYLE DISC PACKS. 1 G 7 1 3U O H2SW 1999082000086 19990820 00086 SW 1999 8 20 99ZZZX3030 1 19990626 A 6510 407340340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL 344 53141 DURING PHASE INSPECTION, DISC PACK CRACKED. 1 G 7 1 3U O H2SW 1999082000087 19990820 00087 SW 1999 8 20 99ZZZX3031 1 19990626 A 6510 407340340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL 344 53141 DURING PHASE INSPECTION, DISC PACK CRACKED. 1 G 7 1 3U O H2SW 1999082000108 19990820 00108 NM 1999 8 20 SWAA991261 1 19990729 A 2120 AIR DIST BOEING 737 7373H4 1384600 NM COCKPIT ODOR A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 661SW 23173 DURING CRUISE AND DESCENT, A STRONG ODOR IN COCKPIT (HOT RUBBER). PERFORMED INSPECTION OF FWD AND AFT E/E COMPARTMENT AND COCKPIT AREA. NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1999082000109 19990820 00109 1999 8 20 SWAA991262 4 19990801 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 FWD SERVICE DOOR EVACUATION SLIDE ACCIDENTALLY DEPLOYED, AND LATER ON FELL OUT OF THE CONTAINER IN SLC. REMOVED AND REP LACED SLIDE ASSY, AND REINSTALLED SLIDE ASSY AT SLC PER MM. 2 L 7 2 4F RT A16WE 1999082000110 19990820 00110 NM 1999 8 20 SWAA991263 1 19990801 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED AFT ENTRY DOOR LIGHT A SSY AND BATTERY PACKS AT BS 330 AND 730 LT PER MM. 2 L 7 2 4F RT A16WE 1999082000111 19990820 00111 NM 1999 8 20 SWAA991264 1 19990801 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 FWD SERVICE DOOR EVACUATON SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000112 19990820 00112 NM 1999 8 20 SWAA991265 1 19990801 A 2560 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 723SW 27855 FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR CAUGHT IN DOOR UPON OPENING. INSPECTED AND REPOSITIONED SLIDE ASSY. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999082000113 19990820 00113 NM 1999 8 20 SWAA991266 1 19990801 A 3320 65C33304 LIGHT BOEING 737 737301 1384611 NM ROW 7 & 8 BURNED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 659SW 23229 AIR TURNBACK, 10 MINS AFTER TAKEOFF F/A REPORTED AN ELECTRICAL ODOR AT MID CABIN. FOUND SIDEWALL LIGHT AT ROW 7 ABC AN D 8 ABC BURNED INTERNALLY. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000114 19990820 00114 NM 1999 8 20 SWAA991267 1 19990731 A 3350 610478 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LEFT BATTERY ASSY PER MM. 2 L 7 2 4F A16WE 1999082000115 19990820 00115 NM 1999 8 20 SWAA991268 1 19990731 A 5532 6547401504 SKIN BOEING 737 7372H4 138448C NM VERT STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STAB CRACKED ON RT SIDE FIN STA 126.3, FWD OF VERTICAL TRAILING EDGE ON REAR SPAR CHORD SKIN. REPAIRED CHORD SKIN PER SWA RA NR 1-255-0306. 2 L 7 2 4F A16WE 1999082000116 19990820 00116 NM 1999 8 20 SWAA991269 1 19990730 A 5330 6552880 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN ON AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999082000117 19990820 00117 NM 1999 8 20 SWAA991270 1 19990730 A 5320 6545409 WEB BOEING 737 7373H4 1384600 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND MLG WHEEL WELL CEILING WEB CRACKED, BS 665, LBL 30.5-33.6. REPAIRED WEB PER ER NR 99-5820. 2 L 7 2 4F RT A16WE 1999082000118 19990820 00118 NM 1999 8 20 SWAA991271 1 19990730 A 5311 6546569 FRAME BOEING 737 7372H4 138448C NM BS 951 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACKED FUSELAGE FRAME, BS 951, STRINGER 19R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999082000119 19990820 00119 NM 1999 8 20 SWAA991272 1 19990801 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000120 19990820 00120 NM 1999 8 20 SWAA991273 1 19990801 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 FWD ENTRY DOOR EVACUATION SLIDE ASSY OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000121 19990820 00121 NM 1999 8 20 SWAA991274 1 19990801 A 5320 65458075 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR UPPER CENTER CUT OUT STUB FRAME CRACKED. REPAIRED STUB FRAME PER SWA RA NR 1-353-2133. 2 L 7 2 4F RT A16WE 1999082000122 19990820 00122 NM 1999 8 20 SWAA991281 1 19990802 A 5311 BAC1503 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER INBOARD FASTENER HOLE, BS 616, LBL64, WL 200. REPAIRED FRAME PER ER NR 99-5743. 2 L 7 2 4F RT A16WE 1999082000123 19990820 00123 NM 1999 8 20 SWAA991282 1 19990802 A 3350 65C34691 LIGHT BOEING 737 7375H4 138449D NM ROW 7, 11 & 19 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C2 CHECK, FOUND 3 EACH BULLNOSE EMERGENCY EGRESS LIGHTS LENSES LOOSE AT ROWS 7 ABC, 11 ABC, AND 19 ABC. SECURED LIGHT LENSES PER MM. 2 L 7 2 4F RT A16WE 1999082000124 19990820 00124 NM 1999 8 20 SWAA991275 1 19990802 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000125 19990820 00125 NM 1999 8 20 SWAA991276 1 19990802 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND TWO MOST AFT OVERHEAD EXIT LIGHTS INOP. REMOVED AND REPLACED AFT OVERHEAD BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999082000126 19990820 00126 NM 1999 8 20 SWAA991277 1 19990802 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 632SW 27707 DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT LOOSE AND BROKEN AT MID CABIN. REMOVED AND REPLACED LIGHT ASSY AND SECURED TRACK PER MM. 2 L 7 2 4F RT A16WE 1999082000127 19990820 00127 NM 1999 8 20 SWAA991278 1 19990802 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 886 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN, BS 886, STRINGER 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999082000128 19990820 00128 NM 1999 8 20 SWAA991279 1 19990802 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 927, BETWEEN STRINGERS 21L-22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999082000129 19990820 00129 NM 1999 8 20 SWAA991280 1 19990802 A 5312 6516300 BULKHEAD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND 3 EACH CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 5- LBL 12. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999082000130 19990820 00130 NM 1999 8 20 SWAA991283 1 19990802 A 4920 APU BOEING 737 7372H4 138448C NM TAIL SMOKING A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 095SW 23054 CONTROL TOWER REPORTED SMOKE COMING OUT OF AFT TAIL SECTION. AIRCRAFT RETURNED TO THE GATE. STARTED APU AND NO DEFECT S NOTED, DEFERRED APU. AT BWI, ADJUSTED APU LOAD STAT. REMOVED AND REPLACED BURNER CAN. RAN APU FOR A WHILE AND HEAVY OIL SMELL AND SMOKE DETECTED WHEN APU HAS LOAD ON IT. REMOVED AND REPLACED APU PER MM. OPS CHECKS GOOD. 2 L 7 2 4F A16WE 1999082000131 19990820 00131 NM 1999 8 20 SWAA991284 1 19990804 A 2560 D31354 SLIDE BOEING 737 7372T4 1384492 NM AFT ENTRY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 AFT ENTRY DOOR EVACUATION SLIDE PRESS GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999082000132 19990820 00132 NM 1999 8 20 SWAA991285 1 19990803 A 3350 BR2013 CONNECTOR BOEING 737 7373H4 1384600 NM ROW 20 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 EEPLS LIGHT DISCONNECTED AT ROW 20. RECONNECTED AND SECURED EEPLS WIRES PER MM. 2 L 7 2 4F RT A16WE 1999082000133 19990820 00133 NM 1999 8 20 SWAA991286 1 19990803 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM BS 929-932 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING OVERNIGHT CHECK, FOUND FUSELAGE SKIN CRACKED, BS 929-932, JUST BELOW STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999082000134 19990820 00134 NM 1999 8 20 SWAA991287 1 19990803 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 EEPLS LIGHT DAMAGED. REPAIRED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000135 19990820 00135 NM 1999 8 20 SWAA991288 1 19990803 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH FWD GALLEYS EMERGENCY EXIT LIGHT BATTERY PACKS PER MM. 2 L 7 2 4F A16WE 1999082000136 19990820 00136 NM 1999 8 20 SWAA991289 1 19990803 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM BS 727 & 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULE SPECIAL VISIT CHECK, FOUND 3 EA STRINGER CLIPS CRACKED, STRINGER 4R, BS 727A,727B, AND 767. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F A16WE 1999082000137 19990820 00137 NM 1999 8 20 SWAA991290 1 19990803 A 5210 6547952 SKIN BOEING 737 7372H4 138448C NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C2 CHECK, FOUND FIVE .25 INCH LONG CRACKS ON LOWER AFT SECTION OF FWD ENTRY DOOR SKIN. REPAIRED PER S RM. 2 L 7 2 4F A16WE 1999082000138 19990820 00138 NM 1999 8 20 SWAA991291 1 19990803 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED SEVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 727C, STRINGER 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999082000139 19990820 00139 NM 1999 8 20 SWAA991292 1 19990803 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED SEVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 927, STRINGER 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999082000140 19990820 00140 NM 1999 8 20 SWAA991293 1 19990803 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED A1 CHECK, FOUND FWD EEPLS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999082000141 19990820 00141 NM 1999 8 20 SWAA991294 1 19990803 A 5315 6545809 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 947.5, LBL 50. REPAIRED BEAM PER SWA RA NR 1-353-2135. 2 L 7 2 4F RT A16WE 1999082000142 19990820 00142 NM 1999 8 20 SWAA991295 1 19990803 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 312, RBL 36. REPAIRED BEAM PER SWA RA NR 1-353-2136. 2 L 7 2 4F RT A16WE 1999082000143 19990820 00143 NM 1999 8 20 SWAA991296 1 19990804 A 2612 6558234 FIRE LOOP BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CHAFED A SWAA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 102SW 23108 707387 DIVERSION IN FLIGHT, ENG SHUT DOWN, NR 2 ENG FIRE WARNING LIGHT ILLUMINATED. ACCOMPLISHED CHECK LIST AND FIRE LIGHT ILL UMINATED AFTER FIRE HANDLE WAS PULLED. DISCHARGED ONE FIRE BOTTLE AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 2 EN G LOWER FIRE LOOP DETECTOR (CHAFING ON COWLING), AND REMOVED AND REPLACED DISCHARGED EXTINGUISHER BOTTLE PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999082000144 19990820 00144 1999 8 20 SWAA991297 4 19990804 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 DURING SCHEDULED OVERNIGHT CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000145 19990820 00145 NM 1999 8 20 SWAA991298 1 19990804 A 3397 BR2013 WIRE BOEING 737 7375H4 138449D NM ROW 6-7 BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 EEPLS WIRE BROKEN AT ROWS 6-7. REMOVED AND REPLACED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000146 19990820 00146 NM 1999 8 20 SWAA991299 1 19990804 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM ROW 3,5,9,20,22 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 617SW 27700 DURING SCHEDULED BC4 CHECK, FOUND EEPLS LIGHT STRIPS COVERS BROKEN AT ROWS 3, 5, 9, 20 AND 22. REMOVED AND REPLACED EEP LS STRIP COVERS PER MM. 2 L 7 2 4F RT A16WE 1999082000147 19990820 00147 NM 1999 8 20 SWAA991300 1 19990804 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM PAX DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR GIRT BAR FWD AND AFT ATTACH BRACKETS CORRODED. REMOVED AND REPLACED A TTACH BRACKETS PER MM. 2 L 7 2 4F RT A16WE 1999082000148 19990820 00148 1999 8 20 SWAA991301 4 19990805 A 3420 6973627 RELAY BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 355SW 25250 AIR TURNBACK, DURING CLIMB, BOTH LEFT AND RIGHT IRS WENT TO DC FAIL C/W QRH PROCEDURES. NO HELP. REMOVED AND REPLACED RELAYS R-1, R-4, R-344. RAN ACFT ENGS AND APU. ALL INDICATIONS NORMAL PER MM. 2 L 7 2 4F RT A16WE 1999082000149 19990820 00149 NM 1999 8 20 SWAA991302 1 19990803 A 3350 SC302 LENS BOEING 737 7372H4 138448C NM EXTERIOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED C3 CHECK, FOUND FASTENER MISSING FROM EMERGENCY EGRESS LIGHT LENS AFT OF LT WING TO BODY FAIRING. REPL ACED FASTENER PER MM. 2 L 7 2 4F A16WE 1999082000150 19990820 00150 NM 1999 8 20 SWAA991303 1 19990805 A 7722 WL202EED EGT IND BOEING 737 7373H4 1384600 NM NR 1 ENGINE MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 ABORTED TAKEOFF, NR 1 ENG EGT OVERTEMP LIGHT ILLUMINATED AT 95 KNOTS, REDUCED ENG THRUST AND LIGHT WENT OUT. INSPECTED NR 1 ENG PER MM 72-00-00-6. PERFORMED ENG RUN TO TAKEOFF LIMITS AND OPS CHECK GOOD. LATER AT PHX ADJUSTED VSV'S DUE TO NR 1 ENG SLOW TO START . 2 L 7 2 4F RT A16WE 1999082000151 19990820 00151 1999 8 20 SWAA991315 4 19990808 A 2210 AUTO PILOT BOEING 737 7373H4 1384600 NM E & E COMPT MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 382SW 26588 AIR TURNBACK, LOST F/O'S ROLL PITCH HEADING AFTER TAKEOFF. PERFORMED POWER CK OF ALL BUSES, APU, STANDBY, ENGS, AND AL L INSTRUMENTS CAME BACK TO NORMAL. POWER DOWN AIRCRAFT FOR SEVERAL MINUTES, POWERED AIRCRAFT BACK UP AGAIN, RAN BOTH EN GS. ALL F/O'S INSTRUMENTS OP CK GOOD. 2 L 7 2 4F RT A16WE 1999082000152 19990820 00152 NM 1999 8 20 SWAA991316 1 19990807 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000153 19990820 00153 NM 1999 8 20 SWAA991317 1 19990807 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FACE, BS 772, LBL 3 - LBL 12. REPAIRED BEAM PER SWA RA NR 1-A53-2021. 2 L 7 2 4F RT A16WE 1999082000154 19990820 00154 NM 1999 8 20 SWAA991318 1 19990807 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L CRACKED, BS 360. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999082000155 19990820 00155 NM 1999 8 20 SWAA991319 1 19990808 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 510 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH CRACKS ON FUSELAGE SKIN BS 510, STRINGER 16R, AND BS 930, STRINGER 23L. 2 L 7 2 4F RT A16WE 1999082000156 19990820 00156 NM 1999 8 20 SWAA991320 1 19990808 A 5220 5079778 DOOR BOEING 737 7375H4 138449D NM RT EMER EXIT GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 DURING SCHEDULED C2 CHECK, FOUND 2 EACH SMALL GOUGES ON RT EMERGENCY OVERWING DOOR AT FWD SKIN. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999082000157 19990820 00157 NM 1999 8 20 SWAA991304 1 19990805 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CORRODED, BS 947, BETWEEN STRINGERS 20R-21R. REPAIRED SKIN PER RA 1-253- 2138. 2 L 7 2 4F A16WE 1999082000158 19990820 00158 NM 1999 8 20 SWAA991305 1 19990805 A 3350 101073 LENS BOEING 737 7372H4 138448C NM PAX DOORWAY FADED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F A16WE 1999082000159 19990820 00159 NM 1999 8 20 SWAA991306 1 19990806 A 2560 D31354 SLIDE BOEING 737 7373G7 1384595 NM GALLEY DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 AFT GALLEY DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000160 19990820 00160 NM 1999 8 20 SWAA991307 1 19990806 A 5312 651633 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999082000161 19990820 00161 NM 1999 8 20 SWAA991308 1 19990806 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND CORROSION AT FLOORBEAM UPPER FACE, BS 986, RBL 43 - LBL 43. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999082000162 19990820 00162 NM 1999 8 20 SWAA991309 1 19990806 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 928 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM FWD FLANGE, BS 328, RBL 49. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999082000163 19990820 00163 NM 1999 8 20 SWAA991310 1 19990806 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 827-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 25L HAS HEAVY CORROSION BETWEEN BS 827-847. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999082000164 19990820 00164 NM 1999 8 20 SWAA991311 1 19990806 A 5754 6573714 SKIN BOEING 737 7375H4 138449D NM NR 5 LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT DELAMINATED ON UPPER AFT INBOARD CORNER. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 1999082000165 19990820 00165 1999 8 20 SWAA991312 4 19990806 A 2565 D31354433 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000166 19990820 00166 NM 1999 8 20 SWAA991313 1 19990806 A 3350 20131 BATTERY PACK BOEING 737 7375H4 138449D NM ROW 8-10 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 8-10. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999082000167 19990820 00167 NM 1999 8 20 SWAA991314 1 19990807 A 7830 315A150020 TR SLEEVE BOEING 737 7373H4 1384600 NM NR 2 ENGINE MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 26588 AFTER LANDING DURING THROUGH FLIGHT INPECTION DISCOVERED NR 2 ENG T/R OUTBOARD SLEEVE MISSING FROM AIRCRAFT. REPLACED N R 2 ENG T/R OUTBOARD SLEEVE ASSY PER MM AND LATER ON THE NR 2 ENG OUTBOARD T/R ASSY WAS REPLACED. 2 L 7 2 4F RT A16WE 1999082000168 19990820 00168 NM 1999 8 20 SWAA991321 1 19990810 A 2782 654465115 ACTUATOR BOEING 737 7372H4 138448C NM NR 1 LE SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 073SW 22673 AIR TURNBACK, NR 1 L/E SLAT WOULD NOT RETRACT. REMOVED AND REPLACED NR 1 L/E SLAT ACTUATOR AND ANTI-ICE DUCT FAIRING PE R MM. 2 L 7 2 4F A16WE 1999082000169 19990820 00169 NM 1999 8 20 SWAA991322 1 19990809 A 5312 6546568 BULKHEAD WEB BOEING 737 7372H4 138448C NM BS 1016 OIL CANNED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULHEAD AFT FACE OIL CANNED AT STRINGER 6L, (DAMAGE IS 5 BY 7). REPAIRED BULKH EAD PER SRM. 2 L 7 2 4F A16WE 1999082000170 19990820 00170 NM 1999 8 20 SWAA991323 1 19990809 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED C3 CHECK, FOUND BOTH AFT EVACUATION SLIDES DRAGGING WHEN CLOSING DOORS. REINSTALLED SLIDE ASSY'S PER M M. 2 L 7 2 4F A16WE 1999082000171 19990820 00171 1999 8 20 SWAA991324 4 19990809 A 2565 6949956 CABLE BOEING 737 7372H4 138448C NM SERVICE DR SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE CABLE ROUTED INCORRECTLY. REROUTED SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 1999082000172 19990820 00172 NM 1999 8 20 SWAA991325 1 19990809 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE AT LOWER FUSELAGE EXTERNAL SKIN, BS 727. REPAIRED SKIN PER XEA X2-53 -251, REVISION 1. 2 L 7 2 4F RT A16WE 1999082000173 19990820 00173 NM 1999 8 20 SWAA991326 1 19990809 A 3350 6042221 POWER SUPPLY BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS LIGHTS DIMMED. REMOVED AND REPLACED AFT EEPLS POWER SUPPLY PER MM. 2 L 7 2 4F RT A16WE 1999082000174 19990820 00174 NM 1999 8 20 SWAA991327 1 19990809 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM RT EMER EXIT CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND RT EMERGENCY EGRESS LIGHT LENS CRACKED, BS 727 PLUS 10. REMOVED AND REPLACED LENS PER M M. 2 L 7 2 4F RT A16WE 1999082000175 19990820 00175 1999 8 20 SWAA991328 4 19990809 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 367SW 26578 DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY. 2 L 7 2 4F RT A16WE 1999082000176 19990820 00176 NM 1999 8 20 SWAA991329 1 19990809 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH EEPLS LIGHTS INOP AT OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM . 2 L 7 2 4F RT A16WE 1999082000177 19990820 00177 NM 1999 8 20 SWAA991330 1 19990809 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 20 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT AT ROW 20 INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000178 19990820 00178 NM 1999 8 20 SWAA991331 1 19990810 A 3350 W014S538 SWITCH BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND AFT ATTENDANT EMERGENCY LIGHTS PANEL SWITCH INOP. REMOVED AND REPLACED SWITCH PER MM, A ND WDM. 2 L 7 2 4F RT A16WE 1999082000179 19990820 00179 NM 1999 8 20 SWAA991332 1 19990811 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 17 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 EEPLS LIGHT LENS MISSING AND LIGHT INOP AT ROW 17. REMOVED AND REPLACED LENS AND BULB PER MM. 2 L 7 2 4F RT A16WE 1999082000180 19990820 00180 NM 1999 8 20 SWAA991333 1 19990810 A 5753 6546435 SKIN BOEING 737 7375H4 138449D NM LT TE AFT FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP P ER MM. 2 L 7 2 4F RT A16WE 1999082000181 19990820 00181 NM 1999 8 20 SWAA991334 1 19990810 A 2761 6551267 CASTING BOEING 737 7375H4 138449D NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED CASTING FOR NR 4 GROUND SPOILER ACTUATOR ATTACH FITTING. REPAIRED CASTING PE R SWA RA NR 1-A57-0571. 2 L 7 2 4F RT A16WE 1999082000182 19990820 00182 NM 1999 8 20 SWAA991335 1 19990810 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND THROUGH ULTRASONIC INSPECTION 3 EACH CRACKS AT BS 178 BULKHEAD, LBL 5 - RBL 5. REPAI RED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999082000183 19990820 00183 NM 1999 8 20 SWAA991336 1 19990810 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 363SW 26574 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED AFT FLAP PER SRM. 2 L 7 2 4F RT A16WE 1999082000184 19990820 00184 NM 1999 8 20 SWAA991337 1 19990810 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 400 & 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND 4 EACH CRACKS ON FUSELAGE FRAMES, BS 400 BETWEEN STRINGERS 8L-9L AND 8R-9R AND BS 440 BE TWEEN STRINGERS 8L-9L AND 8R-9R. REPAIRED FRAMES PER ER 99-5734. 2 L 7 2 4F RT A16WE 1999082000185 19990820 00185 NM 1999 8 20 SWAA991338 1 19990810 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND 6 EACH CRACKS ON FUSELAGE FRAMES BS 827 BETWEEN STRINGERS 8L-9L, BS 787 BETWEEN STRINGER S 8L-9L, BS 867 BETWEEN STRINGERS 8L-9L, BS 747, BETWEEN STRINGERS 8R-9R, BS 727D, BETWEEN STRINGERS 8R-9R AND BS 727B, BETWEEN STRINGERS 8R-9R. REPAIRED FRAMES PER ER 99-5734. 2 L 7 2 4F RT A16WE 1999082000186 19990820 00186 NM 1999 8 20 SWAA991339 1 19990810 A 3397 65C27093 WIRE BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT DOORS EMERGENCY EXIT LIGHTS INOP. REPAIRED BROKEN WIRE BY LEFT AFT ENTRY DOOR. 2 L 7 2 4F A16WE 1999082000187 19990820 00187 NM 1999 8 20 SWAA991340 1 19990811 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607SW 27927 SEVERAL EEPLS WIRES LOOSE AND LENSES MISSING. RESECURED WIRES AND REPLACED LENSES PER MM. 2 L 7 2 4F RT A16WE 1999082000188 19990820 00188 NM 1999 8 20 SWAA991341 1 19990811 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/2D CHECK, FOUND THROUGH ULTRASONIC INSPECTION BS 178 BULKHEAD CRACKED, LBL 4.7. REPAIRED BULKHEAD PE R SRM. 2 L 7 2 4F RT A16WE 1999082000189 19990820 00189 NM 1999 8 20 SWAA991342 1 19990811 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND EMERGENCY AISLE OVERHEAD LIGHT INOP, BS 790. REMOVED AND REPLACED FUSE IN POWER SUPPLY PER MM 2 L 7 2 4F RT A16WE 1999082000190 19990820 00190 NM 1999 8 20 SWAA991343 1 19990811 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 480 & 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAMES, BS 500C ,STR 8L-9L AND STR 8R-9R, BS 500A, STR 8L-9L, BS 480, S TR 8R-9R. REPAIRED FRAMES PER ER NR 99-5734. 2 L 7 2 4F RT A16WE 1999082000191 19990820 00191 NM 1999 8 20 SWAA991344 1 19990811 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM BS 907, 864, 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAMES, BS 907, STR 8L-9L , BS867, STR 8R-9R, BS 827, STR 8R-9R. REPAI RED FRAMES PER ER NR. 2 L 7 2 4F RT A16WE 1999082000192 19990820 00192 NM 1999 8 20 SWAA991345 1 19990811 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 722.8 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND CORROSION AT NUTPLATE HOLE ON KEEL BEAM, BS 722.8, RBL 6.5. REPAIRED KEEL BEAM PER ER N R 99-5733. 2 L 7 2 4F RT A16WE 1999082000193 19990820 00193 NM 1999 8 20 SWAA991346 1 19990811 A 3350 07912 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND EEPLS LIGHT LENS MISSING ON AFT END. REPLACED LENS AND CAP PER MM. 2 L 7 2 4F RT A16WE 1999082000194 19990820 00194 NM 1999 8 20 SWAA991347 1 19990811 A 5240 6545871 GUSSET BOEING 737 7375H4 138449D NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER STUB FRAME GUSSET CRACKED. REMOVED AND REPLACED STUB FRAM E GUSSET PER SRM. 2 L 7 2 4F RT A16WE 1999082000195 19990820 00195 NM 1999 8 20 SWAA991348 1 19990811 A 5312 963820 BULKHEAD CHORD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT CHORD CRACKED, RBL 28.5. REMOVED AND REPLACED RT CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999082000196 19990820 00196 NM 1999 8 20 SWAA991352 1 19990812 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082000197 19990820 00197 NM 1999 8 20 SWAA991354 1 19990812 A 2560 BACN10JC3 NUT PLATE BOEING 737 7373H4 1384600 NM PAX DOOR STRIPPED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 FWD ENTRY DOOR EVACUATION SLIDE ATTACH FASTENER WILL NOT SECURE ASSY. REMOVED AND REPLACED NUTPLATE AND REINSTALLED FAS TENER PER MM. 2 L 7 2 4F RT A16WE 1999082000198 19990820 00198 NM 1999 8 20 SWAA991355 1 19990812 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REPAIRED CHAFED WIRES ON BOTH SIDES. R EMOVED AND REPLACED BATTERY PACKS. 2 L 7 2 4F A16WE 1999082000199 19990820 00199 NM 1999 8 20 SWAA991356 1 19990812 A 5330 6545896 SKIN BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C1 CHECK, FOUND AIR CONDITIONING SERVICE DOORWAY SKIN CUT OUT CRACKED, BS 520, STRINGER 28L. REPAIRED PER SWA RA NR 1-253-2142. 2 L 7 2 4F A16WE 1999082000200 19990820 00200 NM 1999 8 20 SWAA991349 1 19990812 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 700 & 715 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 DURING SCHEDULED C4 CHECK, FOUND 2 EACH CRACKS ON KEEL BEAM SKIN, BS 700, AND BS 715. REPAIRED KEEL BEAM PER SWA RA NR 1-353-2141. 2 L 7 2 4F RT A16WE 1999082000201 19990820 00201 NM 1999 8 20 SWAA991350 1 19990812 A 5512 65C25127 SKIN BOEING 737 7373H4 1384600 NM RT HORZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED, STA 157.10 AT REAR SPAR. REPAIRED SKIN PER ER NR 99-5774. 2 L 7 2 4F RT A16WE 1999082000202 19990820 00202 NM 1999 8 20 SWAA991351 1 19990812 A 3350 6013211 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999082000203 19990820 00203 NM 1999 8 20 PCAA9900027 1 19990810 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 815EX 321 BWI - FLT 3900 - MAIN CABIN DOOR VERY DIFFICULT TO OPEN. MAINTENANCE LUBED AND INSPECTED THE AIRSTAIR DOOR LIFT MECHANI SM IAW CHAPTER 52. CHECKED WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999082000204 19990820 00204 WP 1999 8 20 ABXA9900636 1 19990811 A 5311 2537716 FRAME DOUG DOUG DC8 DC863 302198A WP BS 1140 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 CORROSION ON UNDERSIDE OF FRAME AT STATION 1140 BETWEEN LONGERONS 33 AND 34 RIGHT. REPAIRED IAW ABX REA D853-31948MR. 2 L 7 4 4F 4A25 1999082000205 19990820 00205 WP 1999 8 20 ABXA9900637 1 19990809 A 5730 5611350525 SKIN DOUG DOUG DC8 DC862 3021970 WP LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 804AX 45987 LEFT WING UPPER INBOARD AFT SKIN PANEL HAD CRACK ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW DC8 SRM 57-2-1 AND A BX REA D857-31961MR. 2 L 7 4 4F 4A25 1999082000206 19990820 00206 WP 1999 8 20 ABXA9900638 1 19990809 A 5730 5611350526 SKIN DOUG DOUG DC8 DC862 3021970 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 804AX 45987 RIGHT WING UPPER INBOARD AFT SKIN PANEL CRACKED ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW DC8 SRM 57-2-1 AND AB X REA D857-31961MR. 2 L 7 4 4F 4A25 1999082000207 19990820 00207 WP 1999 8 20 ABXA9900639 1 19990628 A 5710 2757851 SKIN DOUG DOUG DC8 DC863 302198A WP RIGHT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 CORROSION AT RIGHT WING UPPER SKIN AT FORWARD SPAR, STATION XRS 250. INSTALLED REPAIR DOUBLER IAW ABX REA D857-27330MR. 2 L 7 4 4F 4A25 1999082000208 19990820 00208 WP 1999 8 20 ABXA9900640 1 19990627 A 5101 DH431965061 ANGLE DOUG DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 FITTING AT STATION 320 BETWEEN LONGERON 35 LEFT AND 36 LEFT CORRODED. REPLACED FITTING IAW DC8 SRM 51-1-20D AND 53-2-0. 2 L 7 4 4F 4A25 1999082000209 19990820 00209 CE 1999 8 20 CA851022001 1 19990810 A 2140 11C30 IGNITION UNIT JANITROL 5751227 BEECH 99 99 1154002 CE PWA PT6 PT6A20 52043 EA HAMSTD 14SF 14SF* NE HEATER FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 1623 S100 (CAN) PRIMARY IGNITION VIBRATOR FAILED. 1 L 7 2 3T 3 T A14CE E4EA 6 C P7NE 1999082000211 19990820 00211 EU 1999 8 20 CA990630003 1 19990525 A 6210 350A11001007 BLADE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3608 4854 303 (CAN) DURING SCHEDULED MAINTENANCE, A 3 INCH CHORDWISE CRACK WAS FOUND ON THE M/R BLADE. THIS CRACK WAS LOCATED 36 INCH ES OUTWARD FROM THE BLADE ROOT. 1 G 7 1 3U 3 U H9EU E19EU 1999082000213 19990820 00213 GL 1999 8 20 CA990630031 2 19990614 A 7323 252466714 GOVERNOR BENDIX ALAA1 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TURBINE FAILED W O OTHER E VIBRATION/BUFFET HO HOVERING 1 CA 639 25832 CAE830529 (CAN) PT GOVERNOR DROOPS 3 PERCENT TO 5 PERCENT AND OVERSPEEDS 3 PERCENT TO 5 PERCENT. GOVERNOR REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 1999082000216 19990820 00216 EU 1999 8 20 CA990707031 1 19990511 A 6230 704A33651158 BEARING 350A37000304 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE SWASHPLATE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 1317 M1044 544 (CAN) DURING 100 HOUR INSPECTION, SWASHPLATE BEARING ROUGHNESS WAS NOTED DURING ROTATION. MAST ASSEMBLY WAS REMOVED AND SENT FOR FURTHER INSPECTION WHERE SWASHPLATE BEARING WAS REPLACED DUE TO CORROSION AND BRINELLING. 1 G 7 1 3U 3 U H9EU E19EU 1999082000217 19990820 00217 GL 1999 8 20 CA990707032 2 19990622 A 7323 23006259 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TURBINE FAILED W O OTHER E VIBRATION/BUFFET DE DESCENT 1 CA 65 2AAD831 CAE821050 (CAN) POWER TURBINE GOVERNOR OVERSPEEDING IN A DESCENT TO 105 PERCENT N2 WITH NO RECOVERY BACK TO 100 PERCENT N2 (MAXIMU M 5 SECONDS ALLOWED TO RECOVER). AT TSO 42.4 HOURS, DEFECT NO OVERSPEED RECOVERY. AT TSO 46.4 HOURS, GOVERNOR TROUBLES HOOTING. AT TSO 64.5 HOURS, OVERSPEED NO RECOVERY. RIGGING CHECK CARRIED OUT TO CONFIRM PROPER RIGGING WAS FOLLOWED. 1 G 7 1 3U 3 U H2SW E4CE 1999082000219 19990820 00219 EU 1999 8 20 CA990707039 1 19990626 A 6320 S1130021089 SWITCH AEROSP 350A32030004 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R GEARBOX SHORTED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 1040 M2306 4576 (CAN) WHILE IN CRUISE FLIGHT, THE MAIN ROTOR GEARBOX OIL PRESSURE LIGHT CAME ON. THE PILOT LANDED IMMEDIATELY. PRESSUR E SWITCH WAS FOUND TO BE SHORTED. PRESSURE SWITCH REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 1999082000221 19990820 00221 1999 8 20 CA990715001 4 19990629 A 3422 200DC GYRO BELL 204 204B 1181404 SW LYC T53 T5313B 41549 NE COCKPIT DG DAMAGED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 1217 LE07672 (CAN) FOLLOWING INSTALLATION OF NEWLY OVERHAULED DIRECTIONAL GYRO, THE PILOT REPORTED A SMOKE SMELL AND FLAG ON THE DIRE CTIONAL GYRO SWUNG ON/OFF. THE DIRECTIONAL GYRO CIRCUIT BREAKER WAS PULLED WHICH RECTIFIED THE PROBLEM. 1 G 7 1 4U 4 U H1SW E17EA 1999082000223 19990820 00223 EU 1999 8 20 CA990715008 1 19990701 A 7110 350A58010101 COWL SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TRANSMISSION FAILED W A UNSCHED LANDING W D INADEQUATE Q C INFLIGHT SEPARATION CR CRUISE 1 CA 4802TEC (CAN) RIGHT COWL ASSEMBLY DEPARTED THE ROTORCRAFT WHILE IN-FLIGHT. SUSPECT FAILURE OF IMPROPERLY SECURED LATCH P/N 355A 58-3043-00. WHEN THE COWL DEPARTED THE ROTORCRAFT, BRACKET P/N 350A58-1014-22 WAS SHEARED OFF AT THE ENGINE DECK. THER E WAS NO DAMAGE TO THE ROTORCRAFT UPON DEPARTURE OF THE SUBJECT TRANSMISSION COWL. 1 G 7 1 3U 3 U H9EU E19EU 1999082000225 19990820 00225 SW 1999 8 20 CA990715013 1 19990628 A 2435 150SG10095 BRUSH ASSY AIRPRTSCORP 150SG117Q BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL START/GEN DAMAGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 255 5799 CAE820688 (CAN) WHILE PERFORMING 100 HOUR INSPECTION, IT WAS FOUND THAT 2 BRUSH ASSEMBLIES HAD SHEARED THE RIVETS ATTACHING THE SP RING BRACKETS. HOWEVER, THE SPRINGS HELD THE BRACKETS IN PLACE, BUT COULD HAVE VIBRATED OUT POSSIBLY CAUSING SEVERE DAM AGE IN-FLIGHT. BRUSHES REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999082000241 19990820 00241 EU 1999 8 20 CA990728009 1 19990708 A 3242 AHA2174 BRAKE DUNLOP BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG WORN W K NONE O OTHER IN INSP/MAINT 1 CA 5979 62 KY069 LF05629A (CAN) BRAKE WEAR PIN DIAMETER FOUND TO BE GREATER THAN THE CLEARANCE BETWEEN THE ROTOR DRIVE PADS. SUBMITTER REPORTS TH IS IS THE SECOND OCCURRENCE. 2 H 7 4 4F 4 F RT A49EU E6NE 1999082000269 19990820 00269 CE 1999 8 20 CA990728080 1 19990721 A 3230 508103437 PIN 5081033710 BEECH 100 A100 1152915 CE PWA PT6 PT6A34 52043 EA MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 4229 PCE57492 (CAN) DURING THE WASH AND REGREASING OF THE RIGHT MAIN LANDING GEAR, THE PIN THAT ATTACHES THE DOWNLOCK HOOK TO THE DOWN LOCK LINK WAS FOUND PROTRUDING AND BROKEN. THE BREAK WAS LOCATED AT THE HOLE FOR THE ROLL PIN. THE ROLL PIN IS USED TO RETAIN THE HOOK PIN IN PLACE. THE FAILURE OF THIS PIN COULD RESULT IN GEAR COLLAPSE. THE PIN, ROLL PIN, AND DOWNLOCK LINK WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 1999082000271 19990820 00271 WP 1999 8 20 CA990728084 1 19990703 A 2460 SWITCH LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE CABIN MALFUNCTIONED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 10114 (CAN) SPARKS AND FOUL SMELL SEEN COMING FROM THE COAT RACK (L3) ADJACENT TO THE MICROSWITCH. WIRES FOUND BROKEN AND AR CING. WIRES REPAIRED. 2 L 7 3 4F 4 F A23WE E12EU 1999082000272 19990820 00272 WP 1999 8 20 CA990728085 1 19990711 A 3233 1535927101 ACTUATOR LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE RT MLG CRACKED W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA M0492 10459 (CAN) AFTER LOSS OF C-SYSTEM HYDRAULIC FLUID, CREW INITIATED A MANUAL GEAR EXTENSION RESULTING IN A LARGE AUDIBLE BANG F ROM THE RIGHT MLG. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE RIGHT LANDING GEAR ACTUATOR SHEAR ED, JURY DRAG BRACE SHEARED, AND INNER DOOR DAMAGE. DUE TO ACTUATOR DAMAGE, THE GEAR HAD NO SNUBBING ON EXTENSION AND S TRUCK THE DOOR AND UPON REACHING THE END OF TRAVEL, SHEARED THE JURY BRACE BOLT. ACTUATOR AND JURY BRACE BOLT REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999082000273 19990820 00273 NE 1999 8 20 CA990728086 2 19990715 A 7320 LK84958 GASKET LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE FUEL FLOW REG MISINSTALLED W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 10066 (CAN) NR 2 ENGINE OIL QUANTITY DECREASED DURING FLIGHT. AIRCRAFT LANDED. INVESTIGATION REVEALED THAT THE GASKET WAS NO T INSTALLED PROPERLY ON THE GEARBOX. 2 L 7 3 4F 4 F A23WE E12EU 1999082000286 19990820 00286 EU 1999 8 20 CA990729005 1 19990709 A 2620 HC262H0061006 PIPE ASSY BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NOSE COWL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA LF05653A (CAN) FIREX PIPE ASSEMBLY FOUND CRACKED DURING NOSE COWL INSPECTION. CRACK INITIATED WHEN RUBBER ON CLAMP P/N AS46760-2 0 BECAME DISLODGED ALLOWING THE PIPE TO VIBRATE AND WEAR ON THE CLAMP. PARTS REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999082000295 19990820 00295 CE 1999 8 20 CA990804035 1 19990730 A 3020 VANE DOOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA COWL UNHOOKED W A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 CA PCE50392 (CAN) AFTER TAKEOFF, PILOT NOTICED NO ITT/TQ CHANGE WITH THE ICE VANE IN OR OUT. CREW RETURNED TO BASE AND FOUND THE VA NE DOOR WAS UNHOOKED. 1 L 7 2 3T 4 T A14CE E4EA 1999082000296 19990820 00296 WP 1999 8 20 TWAA9911201 1 19990815 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP RT EMER EXIT DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 923TW 49379 GREEN EMERGENCY ESCAPE LIGHT STRIP, MID CABIN, STAYS ILLUMINATED WITHOUT ACTIVATION RIGHT SIDE. REPLACED BATTERY PACK A T OVERWING POSITION. CHECK C 07-26-99 STL. 2 L 7 2 4F RT A6WE 1999082000297 19990820 00297 WP 1999 8 20 TWAA9911202 1 19990814 A 3350 582244 BATTERY PACK DOUG DC9 DC982 3022082 WP EMER EXIT DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 920TW 49369 MID CABIN EMERGENCY ESCAPE PATH LIGHTING STAYS ON WITH SWITCH IN ARM POSITION. WILL NOT RESET. REPLACED FWD OVERWING E MERGENCY BATTERIES. CHECK C 06-22-99 STL. 2 L 7 2 4F A6WE 1999082000298 19990820 00298 WP 1999 8 20 TWAA9911203 1 19990804 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1212-1216 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, FOUND STA 1212 TO 1216 LONGERON 29R INTERCOSTAL CORRODED. REMOVED CORROSION BY REPLACEMENT OF PART PER SRM 51-10-3. 2 L 7 2 4F A6WE 1999082000299 19990820 00299 WP 1999 8 20 TWAA9911204 1 19990805 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 180 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR PANEL SUPPORT AT STA 180, BL 0 TO RBL 45 IN. REPLACED PART PER SPM 6 -70-01. 2 L 7 2 4F A6WE 1999082000300 19990820 00300 WP 1999 8 20 TWAA9911205 1 19990805 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND LONGERON CRACKED AT UPPER TIE POINT, STA 965, LONGERON 16R. REPAIRED PER SRM 53-02, FIG 18 PAGE 52, DRAWING 5911427. 2 L 7 2 4F A6WE 1999082000301 19990820 00301 WP 1999 8 20 TWAA9911206 1 19990809 A 5320 BRACKET DOUG DC9 DC982 3022082 WP TAIL COMPT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 911TW 49182 DURING CHECK C MAINT, FOUND MOUNT BRACKET LEG AND WEB CRACKED AT RUDDER PITOT DRAIN MANIFOLD IN RT TAIL COMPT. REPAIRED BRACKET LEG AS NEC PER DC9 SRM 53-01, PAGE 10. REPAIRED WEB AND STOP DRILLED PER SRM 53-01. 2 L 7 2 4F A6WE 1999082000302 19990820 00302 WP 1999 8 20 TWAA9911207 1 19990810 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK FLANGE AT STA 1212 TO 1250, LBL 44. REPLACED CHAIR TRACK PER S PM 6-70-01. 2 L 7 2 4F A6WE 1999082000303 19990820 00303 WP 1999 8 20 TWAA9911208 1 19990810 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK FLANGE, STA 1271 TO 1307, LBL 44. REPLACED CHAIR TRACK PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999082000304 19990820 00304 WP 1999 8 20 TWAA9911209 1 19990810 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1212-1216 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, FOUND IN AFT CARGO COMPT AT STA 1212 TO 1216, INTERCOSTAL BETWEEN LONGERONS 29R AND 30 WITH CO RROSION ON FOOT. REMOVED AND RELACED FOOT PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999082000305 19990820 00305 WP 1999 8 20 TWAA9911210 1 19990810 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT, STA 200, OTBD OF CHAIR TRACK AT RBL 44. REMOVED AND R EPLACED SUPPORT MEMBER PER SPM 6-70-01, PAGE 2. 2 L 7 2 4F A6WE 1999082000306 19990820 00306 WP 1999 8 20 TWAA9911211 1 19990810 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 148-218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT BEAM AT STA 148 TO 218, WAS CORRODED. REPLACED PART PER SRM 6-70-0 1. 2 L 7 2 4F A6WE 1999082000307 19990820 00307 WP 1999 8 20 TWAA9911212 1 19990815 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 USING LOW FREQ EDDY CURRENT, FOUND CRACK INDICATION AT STA 718, LONGERON 4L. CUT OUT AND REPLACED LONGERON SECTION AND INSTALLED SPLICE SECTION PER SRM 53-02, FIG 18. CHECK C 2-12-99 STL. 2 L 7 2 4F A6WE 1999082000308 19990820 00308 WP 1999 8 20 TWAA9911213 1 19990816 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 FOUND LONGERON 6R CRACKED AT BELT RING STA 699. REPAIRED LONGERON PER SRM 53-02, FIG 18. CHECK-C 2-12-99 STL. 2 L 7 2 4F A6WE 1999082000309 19990820 00309 NM 1999 8 20 HNAA9900110 1 19990811 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM BAGGAGE COMPT MALFUNCTIONED A HNAA O OTHER N FALSE WARNING UK UNKNOWN 1 EA 07 983HA 478 SMOKE WARNING ILLUMINATED IN FLIGHT FOR APPROX 10 SECONDS. REMOVED AND REPLACED NR 2 SMOKE DETECTOR FOR T/S NR 1 AND NR 2 SMOKE DETECTOR TEST GOOD. ADDITIONAL INFO, CREW CONFIRMED NO SMOKE IN BAG COMPARTMENT. 2 H 7 2 4T RT A13NM 1999082000310 19990820 00310 NM 1999 8 20 HNAA9900111 1 19990812 A 3350 6104791X BATTERY 6013211X DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 910HA ORF113 022 NR 3 AND NR 4 RED FLOOR ESCAPE LTS INOP. REMOVED AND REPLACED LEFT AFT EMERGENCY LT BATTERY AND BASE. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999082000311 19990820 00311 WP 1999 8 20 AT9900552 1 19990812 A 2450 914F5655 BUS CONTROL DOUG DC9 DC932 3022066 WP E/E COMPT FAILED A ZZDA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 15 838AT 47442 AFTER TAKEOFF, ELECTRICAL POWER WAS LOST FOR A FEW SECONDS AND THEN CAME BACK ON. THIS HAPPEN TWO MORE TIMES. AIRCRAFT RETURN TO ATLANTA AND LANDED AT A WEIGHT OF 100,503 POUNDS. REMOVED AND REPLACED A/C BUS CONTROL PANEL, OPS CHECK WITH ENGINE RUNS AND NUMEROUS CROSS TIES GOOD IAW MM 24-20. INSPECTED AIRCRAFT AS PER OVERWEIGHT LANDING INSPECTION IAW MM 5-51-0. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1999082000312 19990820 00312 WP 1999 8 20 AT9900553 1 19990728 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 197 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND CORROSION ON UPPER SURFACE OF TOP FLANGE OF CABIN FLOOR SUPPORT AT B S 197 BL 0 TO LBL 15. REMOVED FLOOR SUPPORT, FABRICATED, PRIMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT AND RE INSTALLED FLOOR SUPPORT IAW DC-9 SRM 51-10-3, 51-10-3, 51-10-4, 51-30-1, 53-01-5 AND MM 53-20-1, 25-27-0, 53-20-1. 2 L 7 2 4F A6WE 1999082000313 19990820 00313 WP 1999 8 20 AT9900554 1 19990806 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 850 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND CABIN RT INBOARD SEAT TRACK AT BS 218-965 CORRODED. REMOVED CORROSI ON ON SEAT TRACK. OUT OF LIMITS AT BS 850. REMOVED SEAT TRACK AT BS 850. INSTALLED NEW TRACK IAW DC9 SRM 51-10-3, 53- 05 FIG 4F. 2 L 7 2 4F A6WE 1999082000314 19990820 00314 WP 1999 8 20 AT9900555 1 19990723 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 437-483 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND RT FUSELAGE SKIN AT BS 437-483 L24-25 HAS NUMEROUS DENTS. REMOVED S KIN, FABRICATED NEW SKIN AND SPLICES IAW DC9 SRM 53-04 FIG 15A AND TIMCO RES 07032. 2 L 7 2 4F A6WE 1999082000315 19990820 00315 WP 1999 8 20 AT9900556 1 19990721 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND BRACKET AND CANTED FRAM CRACKED AT BS 1143. REMOVED CRACKED SECTION OF FRAME. FABRICATED 2 FRAME SPLICE DOUBLERS AND HEAT TREATED. FORMED PARTS. DRILLED, TREATED, PRIMED. INSTALLED RE PAIR FRAME, SPLICES AND BRACKET IAW DC9 SRM 51-10-2, 51-10-3, 51-10-2, EO 99-1196. 2 L 7 2 4F A6WE 1999082000316 19990820 00316 WP 1999 8 20 AT9900557 1 19990721 A 5730 PANEL DOUG DC9 DC932 3022066 WP LT WING DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LEFT WING UPPER TRAILING EDGE PANEL DELAMINATED. REMOVED PANEL, REP AIRED DELAMINATED AREAS WITH NEW CORE. SPLICED UPPER SKIN IAW DC9 SRM 51-10-2, RES NR 07217, EO NR 991185. REMOVED AND REPLACED BONDED DOUBLER IAW SRM 51-70-2. REINSTALLED LEFT TRAILING EDGE PANEL IAW SRM 51-30-1, 51-30-2. 2 L 7 2 4F A6WE 1999082000317 19990820 00317 WP 1999 8 20 AT9900558 1 19990714 A 2710 59137502 BRACKET DOUG DC9 DC932 3022066 WP WS 420 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND RT WING AILERON OUTBOARD PULLEY BRACKET CORRODED. REMOVED AND REPLA CED RT WING AILERON OUTBOARD PULLEY BRACKET. RIGGED AILERON BUS CABLES AND OPERATIONAL CHECK GOOD IAW DC9 MM 20-16-0, 2 0-17-0, 27-10-0 PG 310, 511 PAR H, ITEMS 1-7. 2 L 7 2 4F A6WE 1999082000318 19990820 00318 WP 1999 8 20 AT9900559 1 19990722 A 5754 SKIN DOUG DC9 DC932 3022066 WP RT LE SLAT DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND RT WING SLAT AREA XRS 67 HAS FILLER REPAIR WITH A DENT AND GOUGED. R EMOVED FILLER COMPOUND. FOUND DENT WITH GOUGE. BURNISHED AREA. VERIFIED NO CRACKS. FOUND TO BE WITHIN LIMITS PER TIM CO EO 99-1197. ALODINED, PRIMED IAW SRM 51-10-3. 2 L 7 2 4F A6WE 1999082000319 19990820 00319 WP 1999 8 20 AT9900560 1 19990720 A 5320 391488671N FITTING DOUG DC9 DC932 3022066 WP BS 990 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LONGERON END FITTING CORRODED AT BS 990 L24L. OBTAINED NEW END FITT ING. DRILLED AND DEBURRED IAW SRM 51-10-2, 51-10-3, 51-10-4. 2 L 7 2 4F A6WE 1999082000320 19990820 00320 WP 1999 8 20 AT9900561 1 19990729 A 5730 PANEL DOUG DC9 DC932 3022066 WP RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND RT WING LOWER LEADING EDGE PANEL CORRODED. REMOVED CORROSION. FABR ICATED DOUBLERS, TREATED, PRIMED AND INSTALLED IAW SRM 57-01 FIG3, 51-10-03, 51-20-0, 51-30-2. 2 L 7 2 4F A6WE 1999082000321 19990820 00321 WP 1999 8 20 AT9900562 1 19990729 A 5720 FIXED VANE DOUG DC9 DC932 3022066 WP RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND OUTBOARD FIXED VANE ON RT WING CORRODED. FABRICATED FILLER AND DOUB LER. INSTALLED IAW DC9 SRM 57-50-1, 51-70-2, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1999082000322 19990820 00322 WP 1999 8 20 AT9900563 1 19990729 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 280 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND FLOOR PANEL ON RT SIDE AT BS 280 CORRODED. FABRICATED NEW PANEL AND INSTALLED IAW DC9 SRM 51-21-0, 51-30-1. 2 L 7 2 4F A6WE 1999082000323 19990820 00323 WP 1999 8 20 AT9900564 1 19990731 A 5720 FIXED VANE DOUG DC9 DC932 3022066 WP RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND SPOTS OF CORROSION ON UNDERSIDE OF RT WING FLAP FIXED VANE. REMOVED CORROSION. FABRICATED FILLERS AND DOUBLER. BONDED REPAIR. ALODINED AND SEALED IAW DC9 SRM 57-50-9 IG 2, 51-50-2. 2 L 7 2 4F A6WE 1999082000324 19990820 00324 WP 1999 8 20 AT9900565 1 19990724 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 990 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LONGERON END FITTING AT BS 990 L-25L CORRODED. DRILLED NEW LONGERON END FITTING IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4. 2 L 7 2 4F A6WE 1999082000325 19990820 00325 WP 1999 8 20 AT9900566 1 19990513 A 5320 49113832N FITTING DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 867AT 47170 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LEFT FRAME AT BS 935 AT CUSP LINE HAS CORROSION. DRILLED NEW FITTIN G IAW DC9 SRM 51-10-2,AND 51-10-4. 2 L 7 2 4F A6WE 1999082000326 19990820 00326 WP 1999 8 20 AT9900567 1 19990729 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND FWD ENTRY FLOOR PANEL AT BS 160-200 RT CORRODED. FABRICATED NEW PAN EL IAW DC9 SRM 53-20-0, 51-10-4. 2 L 7 2 4F A6WE 1999082000327 19990820 00327 WP 1999 8 20 AT9900568 1 19990811 A 4980 5915793 DUCT DOUG DC9 DC932 3022066 WP APU EXHAUST LEAKING A ZZDA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 15 834AT 47488 TAIL COMPARTMENT HI LIGHT CAME ON AT 140 KNOTS ON TAKEOFF ROLL. LIGHT WENT OFF AFTER QRH PROCEDURE AND 30 SECONDS THEN ON AND OFF FOUR TIMES PRIOR TO LANDING. RESECURED SEALS ON RIGHT HEAT EXCHANGER, SECURED AUGMENTOR VALVE CLAMP. REPLAC ED APU EXHAUST DUCT, RUN ENGINES LEAK CHECK GOOD IAW MM 49-80, AND 21-51-4. 2 L 7 2 4F A6WE 1999082000328 19990820 00328 WP 1999 8 20 IXXA9900019 1 19990811 A 3260 UPLATCH LIGHT DOUG DC8 DC863F 302198F WP MAIN GEAR ILLUMINATED A IXXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 786AL 1556 46121 EN ROUTE FROM BHA TO NSY, THE MAIN LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE GEAR UPLATCH CKECK. THE FLIGHT C REW CYCLED THE GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO NSY FOR AN UNEVENTFUL LANDI NG. A COMPANY REPRESENTATIVE INSPECTED THE LANDING GEAR WITH NO DISCREPANCIES NOTED. THE LANDING GEAR UPLATCH CHECK WA S PLACED ON DEFERRAL IN ACCORDANCE WITH COMPANY PROCEDURES. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999082000329 19990820 00329 EU 1999 8 20 PNSA08001 1 19990812 A 2613 OVERHEAT PROB FENWAL 1734362 SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 685PA 212 DURING CLIMB-OUT, LT TAIL PIPE OVERHEAT LIGHT ILLUMINATED RETURNED TO AIRPORT, LANDING WAS UNEVENTFUL. FURTHER INVESTIG ATION DID NOT REVEAL ANY PHYSICAL OR ELECTRICAL PROBLEMS WITH THE TAIL PIPE HEAT DETECTION SYSTEM. AS A PRECAUTIONARY M EASURE ALL THREE OVERHEAT PROBES WERE CHANGED. NO FURTHER PROBLEMS WERE NOTED. 2 L 7 2 4T RT A52EU 1999082000330 19990820 00330 NM 1999 8 20 CALA9901043 1 19990810 A 2420 WIRE HARNESS BOEING 737 737524 1384721 NM NR 1 ENGINE FAILED A CALA A UNSCHED LANDING B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SW 09 14605 27318 LT GEN TRIPPED OFF LINE ON T/O FROM ORF. QRH PROCEDURE WAS RUN AND GEN RESET NORM. APPROX 3 MINS LATER CREW WAS NOTIFI ED OF LIGHT SMOKE IN FWD PART OF CABIN. THE A/C RETURNED TO ORF. MX FOUND NR 1 TRANSFORMER RECTIFIER C/B POPPED AND NR 1 ENG FIREWALL DISCONNECT PHASE (B) FOR GEN FEEDER BURNT. TRANSFORMER RECTIFIER AND BATTERY/CHARGER WERE REPLACED IAW MM 24-21-31 AND 24-31-21. NR 1 ENG GEN HARNESS WAS R/R'D. NR 1 GEN FEEDER CABLE D3024 RECEPTACLE WAS ALSO REPLACED. R ETERMINATED PYLON HARNESS PER BOEING. NR 1 ENG WAS RUN AND GEN FREQ WAS ADJUSTED IAW MM 24-11-11. OPS OF NR 1 GEN WAS GOOD. TEST FLT EVALUATION WAS PERFORMED AND ALL OPS CHECKED GOOD WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1999082000331 19990820 00331 NM 1999 8 20 CALA9901044 1 19990809 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 328, LBL 15 TO RBL 50. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999082000332 19990820 00332 NM 1999 8 20 CALA9901045 1 19990809 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 344, RBL 10 TO LBL 50. REPAIRED FLOORBEAM IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999082000333 19990820 00333 WP 1999 8 20 9903179613 1 19990810 A 3260 PROX SENSOR DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 613NW 47438 DURING APPROACH INTO DTW, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. FLIGHT CREW DECLARED A YELLOW EMERGENCY AND ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. MAINTENANCE FOUND BROKEN NOSE GEAR PROXIM ITY SENSOR. ALSO, REPLACED LEFT MAIN GEAR DOOR SKID PLATE DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999082000334 19990820 00334 WP 1999 8 20 9903159754 1 19990812 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 754NW 47178 DURING LINE MAINTENANCE INSPECTION, FOUND VENTRAL STAIR AND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PAC K. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999082000335 19990820 00335 SO 1999 8 20 COMA0010131 1 19990811 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 263CA 120255 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN. 2 L 7 2 4T RT A31SO 1999082000336 19990820 00336 NE 1999 8 20 COMA9910132 2 19990812 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT BIRD STRIKE A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 264CA 120256 BIRD STRIKE, LEFT ENGINE. C/W BIRD STRIKE AND BIRD INGESTION CHECKS. NO DAMAGE NOTES. 2 L 7 2 4T 4 T RT A31SO E20NE 1999082000337 19990820 00337 SO 1999 8 20 COMA9910133 1 19990812 A 3610 CLAMP EMB 120 EMB120RT SO RIGHT LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 268CA 120262 RIGHT BLEED AIR DUCT LEAK WARNING. TIGHTENED LOOSE CLAMPS AT LOW PRESSURE BLEED AIR VALVE. 2 L 7 2 4T RT A31SO 1999082000338 19990820 00338 SO 1999 8 20 COMA9910134 1 19990814 A 5713 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 249CA 20842 20842 120230 DURING AN INSPECTION, IT WAS DISCOVERED THAT FUEL WAS LEAKING FROM ONE RIVET THAT WAS JUST FORWARD OF THE FUEL PANEL 622 EB ON THE RIGHT WING. UPON FURTHER INVESTIGATION, IT WAS DISCOVERED THAT STRINGER NR 10 LOCATED BETWEEN WING STATION N R YA-2293 AND YA 2593 WAS CRACKED COMPLETELY IN TWO. THE STRINGER WAS THEN REPAIRED BY USING A FILLER PIECE AND THREE S UPPORT PLATES AS PER INSTRUCTIONS FOUND IN THE AIRCRAFT SRM 57-20-03, PAGES 201 THROUGH 204, AND EMBRAER FAX NR SST-2002 /99. 2 L 7 2 4T RT A31SO 1999082000339 19990820 00339 EA 1999 8 20 COMA9960444 1 19990814 A 5720 60010047801 SCUPPER CNDAIR CL600 CL6002B19 EA RT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 CENTER TANK GRAVITY FILL SCUPPER ASSY HAS SEVERAL DAMAGED HI-LOC PIN HOLES. REPAIRED IN ACCORDANCE WITH REO 601R-57-21- 077. 2 L 7 2 4F RT A21EA 1999082000340 19990820 00340 EA 1999 8 20 COMA9960445 1 19990812 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 319-339 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 14418 7022 FLOORBEAM CAP RBL9 CORRODED BETWEEN FS 319 AND FS 339 P/N 601R31113-67. REMOVED CORROSION FROM FLOORBEAM CAP RBL9 BETWE EN FS 319.00 TO FS 339 IAW REO 601R-53-00-005 SURFACED TREATED IAW SRM 51-25-06, SRM 51-25-16. 2 L 7 2 4F RT A21EA 1999082000341 19990820 00341 EA 1999 8 20 COMA9960446 1 19990809 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 339 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 14418 7022 FLOORBEAM CAP LBL9 CORRODED BETWEEN FS 319 AND FS 339 P/N 601R31113-67. REMOVED CORROSION FROM FLOORBEAM CAP LBL 9 BETW EEN FS 319.00 AND FS 339 IAW REO 601R-53-00-005. ETCHED, ALODINED, PRIMED AND PAINTED IAW SRM 51-25-06, SRM 51-25-16. 2 L 7 2 4F RT A21EA 1999082000342 19990820 00342 EA 1999 8 20 COMA9960447 1 19990813 A 3222 16120 PISTON CNDAIR CL600 CL6002B19 EA NLG LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7706 7127 NLG WILL NOT RETRACT. NLG FOUND LEAKING. REPLACED THE NLG PISTON ASSY. 2 L 7 2 4F RT A21EA 1999082000343 19990820 00343 EA 1999 8 20 COMA9960448 1 19990814 A 3230 555406 VALVE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 10084 450 7026 NLG DID NOT EXTEND. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 1999082000344 19990820 00344 EA 1999 8 20 COMA9960449 1 19990814 A 2421 755469D IDG CNDAIR CL600 CL6002B19 EA NR 1 GEN FAILED A COMA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 01 934CA 7564 265 7042 NR 1 GENERATOR FAILED. REPLACED THE IDG. 2 L 7 2 4F RT A21EA 1999082000345 19990820 00345 EA 1999 8 20 COMA9960450 1 19990811 A 2752 854D10010 ACTUATOR CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 975CA 4598 81 7150 FLAPS FAILED AT 8 DEGREES. REPLACED THE RIGHT OUTBOARD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 1999082000346 19990820 00346 EA 1999 8 20 COMA9960451 1 19990811 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA ROW 2-5 DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 914CA 7012 FLOOR PATH LIGHTING INOPERABLE ROWS 2 TO 5. CLEANED WIRING CONNECTIONS, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1999082000347 19990820 00347 EA 1999 8 20 COMA9960452 1 19990811 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 981CA 7163 FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM IAW AD 98-20-01. 2 L 7 2 4F RT A21EA 1999082000348 19990820 00348 NM 1999 8 20 UPS99230322 1 19990813 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 FWD ENTRY EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999082000349 19990820 00349 NM 1999 8 20 UPS99230323 1 19990813 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY LIGHT INOP ABOVE FLT ATTENDANT FWD SEAT. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD, P/N 96-2-1015. 2 L 7 3 4F A3WE 1999082000350 19990820 00350 NM 1999 8 20 UPS99230324 1 19990813 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 OVERHEAD EMERGENCY LIGHTS ON RT SIDE WILL NOT TEST. REPLACED BATTERY PACKS IN OVERHEAD EMERGENCY LIGHTS ON RT SIDE, OPS CK GOOD. 2 L 7 3 4F A3WE 1999082000351 19990820 00351 NM 1999 8 20 UPS99230325 1 19990813 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 SEAT 19-A EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999082000352 19990820 00352 NM 1999 8 20 UPS99230326 1 19990815 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 FWD ENTRY EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999082000353 19990820 00353 NM 1999 8 20 UPS99230327 1 19990815 A 2560 FIRST AID KIT BOEING 727 72725C 138400H NM CABIN MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 FWD FIRST AID KIT MISSING. REPLACED FIRST AID KIT. 2 L 7 3 4F A3WE 1999082000354 19990820 00354 NE 1999 8 20 99FDEA00333 2 19990811 A 7200 ENGINE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 FAILED A FDEA B EMER. DESCENT O OTHER TO TAKEOFF 1 SO 25 660FE 759 AFTER T/O AT GEAR RETRACT, LOUD BANG THOUGHT TO BE FAILURE OF NOSE GEAR COMPONENT. *S/D* REMOVED AND REPLACED NR 2 ENG IAW WORK CARDS 64T0100-2 & 64T0700-2, FUNCTIONAL CK PRETEST ENG MM 71-00-00 AND JRH ALL CK NORMAL. 2 L 7 2 4F 4 F RT A35EU E13NE 1999082000355 19990820 00355 NM 1999 8 20 99FDEA00332 1 19990813 A 3260 6560021132 ACCESSORY UNIT BOEING 727 727227 1384078 NM E & E COMPT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 481FE 21463 99-206 - RT MLG RED LIGHT INTERMITTENT ON. CYCLED GEAR HANDLE FROM OFF TO UP AND GROUND LIGHT EXT. REMOVED AND REPLACE D LANDING GEAR ELECTRONIC MODULE PER 727-200 MM 32-09-121-5. 2 L 7 3 4F A3WE 1999082000356 19990820 00356 EU 1999 8 20 99FDEA00334 1 19990813 A 2450 NSA93845AA01 RELAY AIRBUS 310 A310203 EU E & E COMPT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 445FE 297 ON CLIMB, ALL PITOT FAULT LIGHTS, NR 1 PITCH TRIM FAILED NR 2 YAW DAMP, NR 1 & 2 ATS. CABIN PRESS FAILED AUTO & MANUAL. ALL SYS WORKED FINE ON LANDING. *S/D* REPLACED RELAY 10KC, REMOVED AND REPLACED RELAY 14XC PER STD PTCS. TEST NORMA L. 2 L 7 2 4F RT A35EU 1999082000357 19990820 00357 WP 1999 8 20 ABXA9900641 1 19990811 A 3230 57156105501 CONTROL VALVE DOUG DC8 DC863 302198A WP LT MLG WW LEAKING A ABXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 819AX 45927 ON FINAL APPROACH, WHEN LANDING GEAR LOWERED, HYDRAULIC PRESSURE WAS DECREASING RAPIDLY. PERFORMED LOSS OF HYDRAULICS CHECK LIST. AIRCRAFT WAS TOWED FROM RUNWAY DUE TO LACK OF BRAKE PRESSURE. REPLACED LANDING GEAR CONTROL VALVE IAW DC8 MM 22-32-7. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999082000358 19990820 00358 WP 1999 8 20 ABXA9900642 1 19990812 A 7931 CONNECTOR DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE UNSECURED A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 824AX 46141 671068 NR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO ILLUMINATION OF OIL PRESSURE LIGHT, OIL TEMPERATURE ERRATIC, THEN OFF SCALE HIGH AND NR 2 GENERATOR FAIL LIGHT ILLUMINATION. AFTER ENGINE SECURED, OIL PRESSURE REMAINED AT 20 PSI. FOUND CANNON PLUG A T NR 2 ENGINE PYLON (PL-819) UNSECURED AND CONTAMINATED WITH GREASE. CLEANED AND RESECURED CANNON PLUG. RAN ENGINE. A LL INDICATIONS WERE NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1999082000359 19990820 00359 NM 1999 8 20 DLM11991782 1 19990810 A 2530 OVEN 72077500 DOUG MD11 MD11 3023602 NM GALLEY SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 803DE 158 48474 OVEN LOC 281 OVERHEATS SMOKES DURING OPERATION. OVEN WIRE HARNESS ELECT GENERAL INSPECTED, NO DAMAGE NOTED. REPLACED O VEN. 2 L 7 3 4F RT A22WE 1999082000360 19990820 00360 NM 1999 8 20 DL767991784 1 19990802 A 5730 111T30001 SKIN BOEING 767 767232 1385132 NM CENTER WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 CORROSION ON CENTER WING SKIN UPPER SURFACE AT SPLICE STRINGER U-17 FROM RBL 74 TO RBL 94, ERA 333346-14 REV A. 2 L 7 2 4F RT A1NM 1999082000361 19990820 00361 NM 1999 8 20 DL72S991785 1 19990810 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 FOUND ON E1 LETTER CK, 2 CRACKS AT L-4 WINDOW CUTOUT LOWER INBD FASTENER HOLES. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1999082000362 19990820 00362 NM 1999 8 20 DL73E991786 1 19990810 A 3350 LIGHT 6013211 BOEING 737 7372S3 NM PAX DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 367DL 6983 21774 EMERGENCY LTS INOP LT AND RT FWD ENTRY DOOR ON OUTSIDE OF AIRCRAFT REF WDM 33-51-01. REPLACED M571. OPS NORMAL. 2 L 7 2 4F RT A16WE 1999082000363 19990820 00363 NM 1999 8 20 DL76S991787 1 19990810 A 3350 LIGHT 1317 BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 131DN 24852 DURING MTC, L/O FOUND SEVERAL EMERGENCY LIGHTS IN OVERHEAD BURNED OUT. 2 L 7 2 4F RT A1NM 1999082000364 19990820 00364 NM 1999 8 20 DL73K991788 1 19990810 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM L1 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 309DL 23081 ON NR 4 SERVICE CHECK, L1 DOOR OVERHEAD EMERGENCY LIGHT EXIT SIGN INOP. REMOVED AND REPLACED POWER SUPPLY M1133, OPN CH ECK NORMAL. 2 L 7 2 4F RT A16WE 1999082000365 19990820 00365 NM 1999 8 20 DLM88991789 1 19990810 A 3350 POWER SUPPLY RPS1 DOUG MD88 MD88 3023688 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 944DL 7191 49817 F/C EMERGENCY LIGHTS WOULD NOT TEST. REPLACED PWR SUPPLY B5-211. LIGHTS CK GOOD. 2 L 7 2 4F RT A6WE 1999082000366 19990820 00366 NM 1999 8 20 DL72W991790 1 19990808 A 5313 65564415 STRINGER BOEING 727 7272Q8 138407W NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 FUSELAGE STRINGER S-29L, FS 950F PLUS 10 CORROSION REPAIR. STRINGER 29L WAS FOUND WITH EXTENSIVE CORROSION AROUND STATI ON 950F. THE CORRODED SECTION OF STRINGER WAS CUT AND REMOVED. A NEW SECTION OF STRINGER WAS SPLICED IN PER ER/A 36787 9-14, REV B. 2 L 7 3 4F A3WE 1999082000367 19990820 00367 NM 1999 8 20 DL72S991791 1 19990809 A 5320 5717703002 WINDOW POST BOEING 727 727232 1384082 NM COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 541DA 22387 FUSELAGE COCKPIT WINDOW FRAME, E-F WINDOW POST, DENT/CRACK REPAIR. THE E-F COCKPIT WINDOW FRAME POST WAS DENTED AT THE LOWER SILL OF THE R3 COCKPIT WINDOW WHEN THE FRONT END OF THE AIRCRAFT WAS BLOWN INTO A FIXED STRUCTURE. INSPECTION OF THE POST REVEALED A CRACK AT THE DENTED LOCATION. THE DAMAGED POST WAS REMOVED AND A NEW POST INSTALLED PER ER/A 36 7851-14, REV A. 2 L 7 3 4F A3WE 1999082000368 19990820 00368 NM 1999 8 20 DL757991792 1 19990708 A 5314 146N35601 KEEL BOEING 757 757232 1384965 NM BS 1390 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 FUSELAGE KEEL CHORD STRINGER 29L, FS 1405, CORROSION REPAIR. THE FUSELAGE STRINGER 29L KEEL CHORD WAS FOUND CORRODED AT FS 1405. THE CHORD WAS CUT AT FS 1390 AND THE AFT END OF THE CHORD REMOVED. A NEW SECTION OF CHORD WAS SPLICED IN PER ER/A 367870-14, REV A. 2 L 7 2 4F RT A2NM 1999082000369 19990820 00369 NM 1999 8 20 DL72S991793 1 19990709 A 5330 SKIN BOEING 727 727232 1384082 NM BS 240 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 541DA 22387 FUSELAGE SKIN FS 230-245, R3 COCKPIT WINDOW SURROUND, DENT/TEAR REPAIR. THE FUSELAGE SKIN JUST BELOW THE R3 COCKPIT WIN DOW BETWEEN FS 230 AND 245 WAS DENTED AND TORN WHEN THE FRONT END OF THE AIRCRAFT STRUCK A FIXED STRUCTURE DURING A WIN D STORM. THE DAMAGED SECTION OF SKIN WAS CUTOUT AND AN ALUMINUM DOUBLER INSTALLED PER ER/A 367840-14, REV B. 2 L 7 3 4F A3WE 1999082000370 19990820 00370 NM 1999 8 20 DL72L991795 1 19990811 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 1 INCH CRACK AT RIGHT TORQUE BOX VERTICAL WEB AT UPPER RIVET ROW STA 1223 (48 SEC). REPAIR PER MM 53-11-0. 2 L 7 3 4F A3WE 1999082000371 19990820 00371 WP 1999 8 20 DLL10991796 1 19990811 A 2612 FIRE LOOP 47226001 LKHEED 1011 10113851 5265010 WP NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 733DS 0468 193C1224 'B' LOOP PREVIOUSLY BAD. NR 2 ENG FIRE HANDLE AND NR 2 'A' LOOP ILLUMINATED IN FLIGHT. NR 2 ENG SHUT DOWN AND BOTH FIR E BOTTLES DISCHARGED POM PROCEDURES COMPLETED. WINDMILL TIME 15 MINUTES. NR 2 IDG DISCONNECTED. REPLACED FIRE LOOP ASSY AND DETECTOR CONTROL UNIT. 2 L 7 3 4F A23WE 1999082000372 19990820 00372 NM 1999 8 20 DL72S991797 1 19990811 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM RT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 492DA 33074 21061 RT OVERWING EMERGENCY LIGHTS WERE INOP. REPLACED BATTERY CHARGER AND BATTERY PACK. OPS NOW NML. 2 L 7 3 4F A3WE 1999082000373 19990820 00373 NM 1999 8 20 DL767991798 1 19990805 A 5730 111T30131 SKIN BOEING 767 767232 1385132 NM BS 955-977 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 CORROSION ON WING CENTER SECTION UPPER SKIN AT FS 955-977 BETWEEN RBL 54-74, ERA 333344-14 REV A. 2 L 7 2 4F RT A1NM 1999082000374 19990820 00374 WP 1999 8 20 DLL14991799 1 19990812 A 2530 COFFEEMAKER 4110001137 LKHEED 1011 1011385115 5265015 WP GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 740DA 65 193C1244 ELECTRIC SMOKE FROM MID GALLEY COFFEEMAKER AREA ON, CAPTAIN'S SIDE. SMOKE STOPPED WHEN COFFEEMAKERS WERE TURNED OFF. R EPLACED BOTH COFFEE MAKERS. 2 L 7 3 4F A23WE 1999082000375 19990820 00375 NM 1999 8 20 DL72L991800 1 19990812 A 5330 655457489 SKIN BOEING 727 727232 1384082 NM BS 480 & 680 CRACKED A DALA I CABIN DEPRESSURIZATION O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 SEVERAL CRACKS WERE FOUND WHILE ACCOMPLISHING SI 4-74176-12 BETWEEN FS 480 AND FS 680 AT STR 4R. THIS DAMAGE WAS REPAIR ED BY ER/A333468-14AD. 2 L 7 3 4F A3WE 1999082000376 19990820 00376 NM 1999 8 20 DL72S991801 1 19990809 A 3350 POWER SUPPLY RPS1 BOEING 727 727225 1384077 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 337701962 21291 DURING FIRST FLT DAY NOTED EMERGENCY EXIT LIGHT ON ALL SEATS IN FIRST CLASS AND TWO ROW IN COACH CLASS INOP. REPLACED P OWER SUPPLY. 2 L 7 3 4F A3WE 1999082000377 19990820 00377 1999 8 20 DL72W991802 4 19990812 A 3417 CADC HG180U279 BOEING 727 727247 138408F NM NR 1 FAILED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 2809W B470174 20581 AFTER T/O CAPTAINS MACH INDICATOR DISPLAYED AN OFF FLAG. ALSO, CAPTAINS ALTIMETER HAD A STANDBY FLAG ALSO NEITHER TRANS PONDER DISPLAYED MODE C TO ATL. REPLACED NR 1 CADC CHECKED NORMAL. 2 L 7 3 4F A3WE 1999082000378 19990820 00378 1999 8 20 DL76P991803 4 19990812 A 2565 SLIDE BOEING 767 767332 1382001 NM LT SERVICE DOOR DETACHED A DALA K NONE O OTHER LD LANDING 1 SO 27 144DA 121698008 27584 LT AFT SERVICE DOOR SLIDE PACK ASSY DROPPED 6 INS OFF DOOR. REMOVED SLIDE AND INSTALL PIN. REPLACED LT AFT SERVICE DOO R SLIDE PACK. CKD OPERATION OF LT AFT DOOR OK. REMOVED AND REPLACED PIN CKD OP OF GIRT/ARM LEVER OK PER M/M. 2 L 7 2 4F RT A1NM 1999082000379 19990820 00379 WP 1999 8 20 DLL10991804 1 19990811 A 5311 FRAME LKHEED 1011 10113851 5265010 WP BS 1645 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 718DA 193C1097 FUSELAGE FRAME FS 1645, STRINGER 14L, CRACK REPAIR. THE FS 1645 FRAME WAS FOUND WITH A TYPICAL CRACK AT WL 280.6 AND A N ADDITIONAL CRACK AT STRINGER 14L ABOVE THE TYPICAL CRACK. THE NEW CRACK WAS APPROX 1 LONG AND RAN LONGITUDI NALLY ACROSS THE FRAME. THE LOCKHEED S/B 093-53-271, REPAIR WAS MODIFIED PER ER/A 367910-14, REV B TO. ENCOMPASS BOTH CRACK AREAS. 2 L 7 3 4F A23WE 1999082000380 19990820 00380 WP 1999 8 20 DLL10991805 1 19990811 A 5311 FRAME LKHEED 1011 10113851 5265010 WP BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 718DA 193C1097 FUSELAGE FRAME FS 1183, WL 280.6, CRACK REPAIR. A TYPICAL CRACK WAS FOUND IN THE FS 1183 FUSELAGE FRAME AT WL 280.6. T HE CRACK WAS STOP DRILLED AND REPAIRED PER LACO S/B 093-53-A271 AND ER/A 367927-14, REV A. 2 L 7 3 4F A23WE 1999082000381 19990820 00381 WP 1999 8 20 DLL10991806 1 19990811 A 5730 1527065101 SKIN LKHEED 1011 10113851 5265010 WP WS 425.7 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 718DA 193C1097 WING RT LOWER AFT SKIN IWS 425.7, STRINGER 3, CRACK REPAIR. THE LOWER AFT SKIN OF THE RT WING WAS FOUND WITH A 4.5 LONG CRACK AT THE STRINGER 3 RUNOUT AT IWS 425.7. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH THREE ALUMINUM DOUBLER S PER ER/A 367909-14, REV A. 2 L 7 3 4F A23WE 1999082000382 19990820 00382 NM 1999 8 20 DL767991807 1 19990813 A 2781 INDICATOR 215016001 BOEING 767 767232 1385132 NM LE FLAPS FAILED A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 114DL 197 22226 ON FLAP EXTENSION THE LEFT INDICATOR SHOWED A SPLIT WITH THE RIGHT. CYCLED BACK TO ZERO. FLAP INDICATOR FOLLOWED L/E D ISAGREE ON EICAS. NORMAL CONTROL OF AIRCRAFT. REPLACED INDICATOR. 2 L 7 2 4F RT A1NM 1999082000383 19990820 00383 WP 1999 8 20 DLL10991808 1 19990811 A 5730 1527084 SKIN LKHEED 1011 10113851 5265010 WP WS 395 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 718DA 193C1097 WING LT UPPER SKIN, IWS 395, CRACK REPAIR. AN EXISTING CRACK IN THE LEFT UPPER WING SKIN AT IWS 395 PROGRESSED BEYOND T HE ALLOWABLE SRM LIMIT. THE CRACK STARTED AT THE AFT EDGE OF THE SKIN AND PROGRESSED FWD. THE CRACK IS TYPICAL OF THE SRM, BUT IS NOW 2.3 LONG. THE CRACK WAS STOP DRILLED AND REPAIRED WITH TWO ALUMINUM EXTERNAL DOUBLERS AND INTERNA L ALUMINUM STRAPS PER ER/A 367904-14, REV B. 2 L 7 3 4F A23WE 1999082000384 19990820 00384 NM 1999 8 20 DL72L991809 1 19990811 A 5320 FRAME BOEING 727 727232 1384082 NM CARGO DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 FUSELAGE C1 DOOR SURROUND FRAME, FS 560, WEB CRACK REPAIR. A INCH 2 CRACK WAS FOUND IN THE WEB OF THE FORWARD JAMB FRAM E OF THE C1 DOOR OPENING. THE CRACK WAS LOCATED AT THE 2ND FROM THE TOP DOOR STOP. THE CRACK WAS ROUTED OUT AND REPA IRED WITH A DOUBLER PER ER/A 368008-14. 2 L 7 3 4F A3WE 1999082000385 19990820 00385 NM 1999 8 20 DL72W991810 1 19990811 A 5312 BULKHEAD BEAM BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 FUSELAGE BULKHEAD FS 1183, RBL 26.83, VERTICAL BEAM, CRACK REPAIR. THE RBL 26.83 VERTICAL BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A TYPICAL CRACK. THE BEAM WAS REPAIRED PER BOEING S/B 727-53-0182, REV 1 AND DOCUMENTED PER ER/A 367994- 14AD. 2 L 7 3 4F A3WE 1999082000386 19990820 00386 NM 1999 8 20 DL72S991811 1 19990813 A 5522 657278411 SKIN BOEING 727 727232 1384082 NM LT & RT ELEVATOR SEPARATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 LEFT ELEVATOR T/E SEPARATING O/B OF TAB. RIGHT ELEVATOR T/E SEPARATING O/B OF TAB. INSTALL T/E FASTENERS REF MM 55-20- 0. 2 L 7 3 4F A3WE 1999082000387 19990820 00387 NM 1999 8 20 DL72S991812 1 19990813 A 5330 SKIN BOEING 727 727232 1384082 NM L1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 FOUND ON F1 LETTER CK, .375 INCH CRACK AT L-1 DOOR UPPER HINGE CUTOUT ON THE FUSELAGE. REPAIRED PER MM 53-30-3. 2 L 7 3 4F A3WE 1999082000388 19990820 00388 NM 1999 8 20 DL72S991813 1 19990813 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM ROW 27 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 522DA 72542 21582 LEFT FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CK OK. 2 L 7 3 4F A3WE 1999082000389 19990820 00389 NM 1999 8 20 DLM11991816 1 19990814 A 5230 DOOR DOUG MD11 MD11 3023602 NM CARGO COMPT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 801DE 48472 ON L/O, FOUND FUSELAGE DAMAGE FWD OF BULK CARGO DOOR. REPAIRED DAMAGE PER ERA 368026-14. 2 L 7 3 4F RT A22WE 1999082000390 19990820 00390 NM 1999 8 20 DL76G991817 1 19990814 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM ROW 1-5 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1605 48150 30198 ROWS 1-5 EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 1999082000391 19990820 00391 NM 1999 8 20 DLM88991819 1 19990814 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM T/R UNIT LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 914DL 49545 LOW HYD QTY ON LEFT SIDE (2 QUARTS) AND ASSOCIATED LEFT LOW HYD PRESSURE MESSAGE OCCURRED ON SHORT FINAL TO LANDING. AF TER LANDING GEAR AND FULL FLAPS EXTENDED. TIGHTENED B-NUT ON THRUST REVERSER MODULE. 2 L 7 2 4F RT A6WE 1999082000392 19990820 00392 WP 1999 8 20 DLL19991821 1 19990814 A 3350 BATTERY PACK LKHEED 1011 10113853 5265020 WP LAVATORY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 753DA 193W1189 ON L/O, FOUND AFT LAV EMERGENCY TRACK LIGHTS INOP. REPLACED RACK FOR AFT A/C E-PATH LIGHTING ON RT AFT B/B. 2 L 7 3 4F A23WE 1999082000393 19990820 00393 NM 1999 8 20 SCNA99101 1 19990808 A 3350 BULB BOEING 727 7272J4 1384006 NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE EXTERIOR EMERGENCY EXIT SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED AND ALL EMERGENCY LIGHTING OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999082000394 19990820 00394 NM 1999 8 20 SCNA99102 1 19990812 A 2550 CARGO NET BOEING 727 727259 138408J NM CARGO DOOR OUT OF POSITION A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 289SC 22475 DURING CLIMB-OUT, UNABLE TO MAINTAIN PRESSURIZATION. TROUBLESHOT PRESSURIZATION SYSTEM AND FOUND THE AFT CARGO DOOR NET AND LATCH WEDGED BETWEEN THE CARGO DOOR AND THE DOOR FRAME. REMOVED AND RESECURED THE CARGO NET. PERFORMED AN OPERATI ONAL TEST OF THE SYSTEM PER MM 21300 AND MM 213100. AIRCRAFT OK FOR SERVICE. 2 L 7 3 4F A3WE 1999082000395 19990820 00395 NM 1999 8 20 SCNA99103 1 19990811 A 3350 900835A BATTERY PACK 10617844 BOEING 727 727282 138408T NM R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC M1924 21949 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS ABOVE THE R2 DOOR WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLA CED THE BATTERY PACK AND POWER SUPPLY AT M1093. ALL EMERGENCY LIGHTING OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999082000396 19990820 00396 NM 1999 8 20 DHL9970301C 1 19990720 A 5311 CIRCUMFERENTIAL BOEING 727 72730C 1384009 NM BS 640 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, FWD CARGO COMPT, CRACK AT CIRCUMFERENTIAL STA 640 STRINGER 26L. REMOVED OLD REPAIR, STOP DRILLED CRACK, HFE C. INSTALLED REPAIR PARTS PER SRM 53-10-4, 12 BY 6, N/R 3121. 2 L 7 3 4F A3WE 1999082000397 19990820 00397 NM 1999 8 20 DHL9970302C 1 19990720 A 5720 ANGLE BOEING 727 72730C 1384009 NM WS 498 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, RT WING TRAILING EDGE COVE PANEL OUTBOARD SUPPORT ANGLE IS CRACKED AT WS 498.08 INBOARD OF THE NR 12 SPOILER ACTUATOR. REPLACED COVER PANEL OUTBRD SUPPORT WS 498.08 PER SRM 51-30-2, 51-10-1 PAR 4 N/R 2045. 2 L 7 3 4F A3WE 1999082000398 19990820 00398 NM 1999 8 20 DHL9970303C 1 19990716 A 5720 FAIRING BOEING 727 72730C 1384009 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LEFT WING NR 1 MOVABLE FAIRING GOUGED AT PREVIOUS REPAIR INNER SECTION. REMOVED PAINT FROM REPAIR AREA, REP LACED PREVIOUS REPAIR (5 BY 12) PER SRM 57-20-2 AND SRM 51-40-2, ALODINED AND REPRIMED PER SRM 51-10-2, N/R 1103. 2 L 7 3 4F A3WE 1999082000399 19990820 00399 NM 1999 8 20 DHL9970304C 1 19990719 A 5752 TAB BOEING 727 72730C 1384009 NM LT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, L/W OUTBOARD AILERON TAB, HAS ON TOP LEADING EDGE A METAL LIFTING UP AT I/B SIDE. REPLACED LEADING EDGE MET AL COVER OF L/W O/B AILERON AT LEADING EDGE INBOARD SIDE OF TAB PER SRM 57-50-2 FIG 8 AND 51-30-2 USING .020 2024-T3 1.5 BY 7, ALODINED PRIMED AND TREATED PER SRM 51-10-2. N/R 1168. 2 L 7 3 4F A3WE 1999082000400 19990820 00400 NM 1999 8 20 DHL9970305C 1 19990721 A 5720 FAIRING BOEING 727 72730C 1384009 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LEFT WING NR 1 MOVABLE FAIRING SKIN CORRODED AT FWD I/B SIDE AT FAIRING ATTACH POINT. REMOVED PAINT FROM SK IN CORRODED AREA PER MM 51-20-0, CUT 6 INCH BY 5 INCH SECTION OF SKIN AWAY AND INSTALLED REPAIR SKIN AND SPLICE PLATE PE R SRM 53-50-1 FIG 1 AND SRM 51-30-2, MATERIAL USED .040 7075T6 APPROXIMATELY 8 BY 12. ALODINED AND PRIMED AREA OF REPAI R PER SRM 51-10-2, N/R 1206. 2 L 7 3 4F A3WE 1999082000401 19990820 00401 NM 1999 8 20 DHL9970306C 1 19990717 A 5720 TIP BOEING 727 72730C 1384009 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LEFT WING TIP AFT O/B EDGE AREA CRACKED IN TWO PLACES. REMOVED LEFT WING TIP OUTBOARD EDGE FOR REPAIR IAW S RM 51-30-2. STOP DRILLED CRACK AT TWO PLACES IAW SRM 51-10-1, PERFORMED HFEC IAW NDT PART 68-00-00 FIG 4. NO CRACKS NO TED BEYOND STOP DRILL, ALODINED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR AT LEFT WING TIP AFT O/B EDGE PER SME 57-2 0-5 FIG 2 USING 7075T6 .050 24 BY 8, N/R 1126. 2 L 7 3 4F A3WE 1999082000402 19990820 00402 NM 1999 8 20 DHL9970307C 1 19990720 A 5720 ANGLE BOEING 727 72730C 1384009 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, RT WING TRAILING EDGE COVER PANEL INBOARD SUPPORT ANGLE IS CRACKED AT WS 447.90 JUST INBOARD OF NR 11 SPOILE R ACTUATOR. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING AT WS 447.90 PER SRM 51-10-1 PAR 4 AND 51-30-2, N/R 2044. 2 L 7 3 4F A3WE 1999082000403 19990820 00403 NM 1999 8 20 DHL9970308C 1 19990721 A 5532 PANEL BOEING 727 72730C 1384009 NM VERT STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, V STAB ACCESS PANEL NR 9774 HAS REPAIRS CRACKING UP L/S. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40- 8 FIG 1 USING RESIN 1304, 6 INCH BY 4 INCH, N/R 4128. 2 L 7 3 4F A3WE 1999082000404 19990820 00404 NM 1999 8 20 DHL9970309C 1 19990720 A 5321 FLOOR BOEING 727 72730C 1384009 NM BS 284 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, NOSE W/W PRESS FLOW HAS CRACK AT BS 284.5. REMOVED FLOOR PANEL AT FWD PER SRM 51-30-2. REMOVED 2 EACH OLD DOUBLERS PER SRM 51-30-2. CUT OUT DAMAGED AREA AT BS 284.5 4 BY 1 PER S/B 53-0145, HFEC INSPECTED CUTOUT IAW 51-00-0 FI G 4. NO CRACKS NOTED. INSTALLED DOUBLER REPAIR USING 2024T3 .050 17 INCH BY 10.5 INCH. ALODINED AND PRIMED PER SRM 51 -10-2. INSTALLED FLOOR PANEL PER SRM 51-30-2, N/R 6159. 2 L 7 3 4F A3WE 1999082000405 19990820 00405 NM 1999 8 20 DHL9970310C 1 19990721 A 5230 DEPRESSOR BOEING 727 72730C 1384009 NM CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, SEAL DEPRESSOR AT MCD AFT OF NR 6 LATCH HAS A SQUARE .25 OF MATERIAL MISSING REQUIRES REPAIR. SMOOTHED DAMA GED SECTION PER SRM 51-40-1. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED L ANGLE REPAIR PER SRM 51-40-3 FIG 1 USIN G .063 2024-0 HEAT TREATED TO 2024T3 1 BY 1 BY 14. INSTALLED ANGLES AT SEAL DEPRESSOR PER SRM 51-30-2, N/R 3155. 2 L 7 3 4F A3WE 1999082000406 19990820 00406 NM 1999 8 20 DHL9970311C 1 19990719 A 5320 RECEPTACLE BOEING 727 72730C 1384009 NM BS 364 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, BARRIER NET ATTACH RECEPTACLE AT BS 364 BETWEEN STRINGERS 5L AND 6L UPPER MOUNT BRACKET MISSING ATTACH RIVET AND CRACKED. REMOVED BRACKET SUPPORT PER SRM 51-30-2. REPLACED BRACKET SUPPORT PER SRM 51-30-2 USED 7075T0 .071 AND 2 024T3 .050, ALODINED AND PRIMED PER SRM 51-10-2. HEAT TREATED 7075-T0 TO 7075T6 PER 99PMSI 247 PG -01, N/R 5041. 2 L 7 3 4F A3WE 1999082000407 19990820 00407 NM 1999 8 20 DHL9970312C 1 19990720 A 5320 LONGITUDINAL BOEING 727 72730C 1384009 NM E & E COMPT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, E3 ELECTRONIC RACK UPPER RT LONGITUDINAL IS CRACKED 2 PLACES. STOP DRILLED CRACKS PER SRM 51-10-1 2 PLACES. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1 USING 2024T3 .050 6 BY 4 2 EA, ALODINED AND PRIMED PER SRM 51-10-2, N/R 3126. 2 L 7 3 4F A3WE 1999082000408 19990820 00408 NM 1999 8 20 DHL9970313C 1 19990721 A 7110 SKIN BOEING 727 72730C 1384009 NM NR 2 ENGINE COWL CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, ENGINE NR 2 FWD RT COWL LOWER FWD INSIDE CORNER DOUBLER CHAFFED THROUGH. REMOVED FASTENER AND DAMAGED DOUBL ER PER SRM 51-30-2, CLEANED AND PRIMED ARE PER SRM 51-10-2. REPLACED DOUBLER PER SRM 51-30-2 USED .040 14 BY 5 2024-0 H EAT TREATED TO 2024T3 PER 98PMSI 247 PG-01, N/R 6230. 2 L 7 3 4F A3WE 1999082000409 19990820 00409 NM 1999 8 20 DHL9970314C 1 19990721 A 5313 COWL BOEING 727 72730C 1384009 NM NR 1 ENGINE CHAFF A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, NR 1 TOP COWL OUTBOARD LONGERON HAS DEEP CHAFED SPOTS AT 46 AND 54 INCHES FROM AFT EDGE. REPLACED COLGERON SECTION PER SRM 51-40-2 AND 54-10-2 ON NR 1 TOP COWL, USED 2024T3 .050 20 BY 4, TREATED AND PRIMED AREA PER SRM 51-10-2, N/R 6206. 2 L 7 3 4F A3WE 1999082000410 19990820 00410 NM 1999 8 20 DHL9970315C 1 19990720 A 5230 PLATE BOEING 727 72730C 1384009 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, MAIN CARGO DOOR INTERIOR LOWER PLATE COVER FWD TO AFT SECTION HAS SEVERAL CRACKS AND DENTS ON SURFACE. REMO VED PLATE AT MAIN CARGO DOOR INTERIOR LOWER PLATE COVER REPAIRED PER SRM 51-30-2 AND 51-10-1. ALODINED AND PRIMED PER S RM 51-10-2 USED 2024T3 .032 86 BY 55 AND INSTALLED PER SRM 51-30-2, N/R 5067. 2 L 7 3 4F A3WE 1999082000411 19990820 00411 NM 1999 8 20 DHL9970316C 1 19990721 A 5530 FAIRING BOEING 727 72730C 1384009 NM VERT STAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, V STABILIZER HAS FAIRING DELAMINATED ON BOTH SIDES BELOW TAIL CONE. INSTALLED BONDING REPAIR AT VERTICAL ST ABILIZER FAIRINGS BELOW TAIL CONE PER SRM 51-20-3 FIG 1, MATERIAL USED EPOCAST 1652 A/B, N/R 4127. 2 L 7 3 4F A3WE 1999082000412 19990820 00412 NM 1999 8 20 DHL9970317C 1 19990722 A 5350 TAIL CONE BOEING 727 72730C 1384009 NM AFT FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, TAIL CONE HAS DELAMINATION AT LEFT TOP AREA. REMOVED VERTICAL STABILIZER TAILCONE PER SRM 51-30-2. INSTAL LED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1, USED RESIN 50-A AND CLOTH STYLE 720 10 INCH BY 6 INCH, PRIMED ALL R EAS PER SRM 51-10-2. INSTALLED TAILCONE PER MM 51-30-02, N/R 4124. 2 L 7 3 4F A3WE 1999082000413 19990820 00413 NM 1999 8 20 DHL9970318C 1 19990721 A 5210 STRUCTURE BOEING 727 72730C 1384009 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, FWD ENTRY DOOR INTERIOR FWD UPPER CORNER IS CRACKED. REMOVED INTERIOR FWD ENTRY DOOR PER SRM 51-30-2, FABRI CATED NEW LINER SUPPORT FWD CORNER PER SRM 52-10-1 FIG 1 USED .050 2024-0 HEAT TREATED TO 2024T3 PER 99PMSI 247 PG-01. A LODINED AND PRIMED PER SRM 51-10-2. INSTALLED UPPER CORNER AT FWD ENTRY DOOR PER SRM 51-30-2, N/R 3137. 2 L 7 3 4F A3WE 1999082000414 19990820 00414 NM 1999 8 20 DHL9970319C 1 19990721 A 5230 BRACKET BOEING 727 72730C 1384009 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, FWD CARGO DOOR UPLOCK SUPPORT BRACKET IS CRACKED. REMOVED FWD CARGO DOOR UP LOCK SUPPORT BRACKET PER SRM 51 -30-2. REPLACED FWD CARGO DOOR UPLOCK SUPPORT BRACKET PER SRM 51-30-2 AND 51-40-2, MATERIAL USED 2024T3 .040 6 BY 3, AL ODINED AND PRIMED PER SRM 51-10-2, N/R 3132. 2 L 7 3 4F A3WE 1999082000415 19990820 00415 NM 1999 8 20 DHL9970320C 1 19990721 A 5730 SKIN BOEING 727 72730C 1384009 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG ROW OF FASTENERS JUST FWD OF THE NR 8 SPOILER PANEL. REMOVED PANEL FO R REAIR, CLEANED MATING SURFACE ON WING, NO CORROSION NOTED, TREATED AND PRIMED AREA PER SRM 51-10-2. INSTALLED BONDED REPAIR AT R/WING UPPER SURFACE PANEL PER SRM 51-40-6 FIG 1 SIZE 10 BY 1. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED PANEL PER SRM 51-30-2, N/R 2067. 2 L 7 3 4F A3WE 1999082000416 19990820 00416 NM 1999 8 20 DHL9970321C 1 19990720 A 5730 SKIN BOEING 727 72730C 1384009 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG PANEL 10 FORWARD OF NR 9 AND NR 10 SPOILER PANEL. REMOVED FASTENERS AT RT WING PANEL PER SRM 51-30-2. FOUND DELAMINATED SKIN IN UPPER PANEL, CLEANED MATING SURFACE ON AIRCRAFT TRATED AND PRIMED. NO CORROSION NOTED PER SRM 51-10-2. INSTALLED BONDED REPAIR AT UPPER SURFACE PER SRM 51-40-6 FIG 1 USING ADHE SIVE FILM AF163-2K AND 2024T3 .032 7X33. INSTALLED PANEL PER B727 SRM 51-30-2, N/R 2063. 2 L 7 3 4F A3WE 1999082000417 19990820 00417 NM 1999 8 20 DHL9970322C 1 19990720 A 5753 SKIN BOEING 727 72730C 1384009 NM RT TE FORE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, RT WING INBOARD FORE FLAP HAS SURFACE CORROSION ON LOWER SKIN APPROXIMATELY 12 FROM OUTBD END. REMOVED CORR OSION AT RT WING PER SRM 51-10-6, OUT OF LIMITS PER SRM 57-50-1 FIG 3 DETAIL 3. INSTALLED FG OVERLAY REPAIR PER SRM 51- 40-8 FIG 1 ON RT WING INBD FORE FLAP ON LOWER SKIN MATERIAL USED RESIN 50A MARDENER 946 12 BY 4, N/R 2055. 2 L 7 3 4F A3WE 1999082000418 19990820 00418 NM 1999 8 20 DHL9970323C 1 19990720 A 2782 BOLT BOEING 727 72730C 1384009 NM NR 3 LE SLAT ACT SHEARED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LT WING NR 3 LE SLAT ACTUATOR TIE DOWN BOLT IB LOWER BOLT SHEARED. REPLACE THE IB LOWER BOLT ON NR 3 LE SL AT ACTUATOR PER MM 20-80-1, N/R 1199. 2 L 7 3 4F A3WE 1999082000419 19990820 00419 NM 1999 8 20 DHL9970324C 1 19990716 A 5751 ATTACHMENT BOEING 727 72730C 1384009 NM LT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LT WING I/B AILERON BALANCE PANEL AFT HINGE ATTACHMENT CRACKED. REMOVED AND REPLACED LT WING I/B AILERON BA LANCE PANEL AFT HINGE ATTACHMENTPER MM 27-10-21, N/R 1107. 2 L 7 3 4F A3WE 1999082000420 19990820 00420 NM 1999 8 20 DHL9970325C 1 19990721 A 7110 LONGERON BOEING 727 72730C 1384009 NM NR 1 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, NR 1 LOWER COWL OUTBOARD LONGERON IS CRACKED UNDER RUB PLATE BY NR 3 LATCH V-BOLT CUTOUT. ALSO, SKIN IS BE NT AND CRACKED AROUND CUTOUT. REWORKED SKIN AT NR 1 ENG LOWER COWL NR 3 LATCH U-BOLT CUT OUT PER SRM 51-10-1. NO SIGNI FICANT MATERIAL LOSS. WITHIN LIMITS PER SRM 54-30-1. REMOVED LONGERON AT NR 1 ENF LOWER COWL PER SRM 51-30-2, CLEANED, ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PARTS PER SRM 51-40-3, USING MATERIAL .050 2024T3 20X4, TREATED ALODINE AREA AT NR 3 LATCH CUT OUT PER SRM 51-10-2, N/R 6214. 2 L 7 3 4F A3WE 1999082000421 19990820 00421 NM 1999 8 20 DHL9970326C 1 19990720 A 5720 STIFFENER BOEING 727 72730C 1384009 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LW VERT STIFFENER IS CRACKED AT LOWER END AT FALSE SPAR BELOW NR 5 SPOILER O/B SIDE. STOP DRILLED 1 CRACK PER SRM 57-50-6. REMOVED APPROX 6 OF FASTENERS PER SRM 57-50-6, MADE NEW L ANGLE DOUBLER PER SRM 57-50-6. PICKED UP EX ISTING FASTENER HOLES ONTO NEW L ANGLE DOUBLER PER SRM 57-50-6. TREATED AND PRIMED NEW DOUBLER PER SRM 57-50-6. INSTAL LED NEW DOUBLER PER SRM 57-50. PERFORMED HFEC INSPECTION PER NDT MANUAL PART 6 51-00-00 FIG 4, CRACK ENDS AT STOP DRILL HOLE. MATERIAL USED 8 INCH BY 1 INCH BY 1 INCH .063 2024 T3, N/R 1149. 2 L 7 3 4F A3WE 1999082000422 19990820 00422 NM 1999 8 20 DHL9970327C 1 19990720 A 5730 SKIN BOEING 727 72730C 1384009 NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LW TOP SKIN PANEL HAS FIBERGLASS REPAIR NOT FINISHED BETWEEN WING AND FUSELAGE. REMOVED LW TOP SKIN PANEL L OCATED BETWEEN WING AND FUSELAGE PER SRM 51-30-2. INSTALLED BONDED REPAIR AT LW TOP PANEL PER SRM 51-40-6 FIG 1 MAT USE D 2024 T3 .020 , 2024T3 .025 AND ADHESIVE FILM AF163-2K SIZE 20X27.5. INSTALLED LW TOP SKIN PANEL PER SRM 51-30-2, N/R 1186. 2 L 7 3 4F A3WE 1999082000423 19990820 00423 NM 1999 8 20 DHL9970328C 1 19990727 A 5754 69139954 BOLTS BOEING 727 72730C 1384009 NM RT LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, 2 EA SLAT ROLLER BOLTS CRACKED AT LUBE HOLE AND 6 EA SLAT ROLLER BOLTS WORN. REPLACED PER MM 27-81-11, N/R 2074. 2 L 7 3 4F A3WE 1999082000424 19990820 00424 NM 1999 8 20 DHL9970329C 1 19990723 A 5730 SKIN BOEING 727 72730C 1384009 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, RT WING FIXED LEADING EDGE CUT OUT FOR THE NR 5 SLAT INBD TRACK IS CRACKED. REMOVED SEALS TO GAIN ACCESS TO BACKSIDE OF LEAD EDGE OF WING PER SRM 57-30-4, MADE EXTERNAL DOUBLER PICKED UP EXISTING HOLES 2 EA NEW HLOES ONTO NEW D OUBLER PER SRM 57-30-4. ROUTED CRACK APPROXIMATELY .375 INCH LONG PER SRM 57-30-4, TREATED AND PRIMED NEW DOUBLER AND L EADING EDGE OF WING PER SRM 57-30-4, MATERIAL USED: 6X10 .063 2024T3, N/R 2009. 2 L 7 3 4F A3WE 1999082000425 19990820 00425 NM 1999 8 20 DHL9970330C 1 19990722 A 5755 HINGE BOEING 727 72730C 1384009 NM NR 7 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LW NR 7 SPOILER PANEL CENTER HINGE CASTING OUTBOARD LEG CRACKED AT AFT HOLE. CUT OUT CRACK FROM HINGE CASTI NG 2 LONG PER SRM 51-10-1, DYE PENETRANT INSPECTED CUTOUT PER MIL 68-66B. NO CRACK NOTED, INSTALLED FILLER AND REINFORC ING STRAP AT LEFT WING NR 7 SPOILER O/B UPPER FLANGE PER 99AVHM.054R0-1 USED 2024T3 .125 9X3/. TREATED AND PRIMED PER S RM 51-10-2, SEALED LEADING EDGE WITH PRC AS PER SRM 51-20-4, N/R 1207. 2 L 7 3 4F A3WE 1999082000426 19990820 00426 NM 1999 8 20 DHL9970331C 1 19990721 A 7120 MOUNT BOEING 727 72730C 1384009 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, ENGINE NR 1 GEARBOX FWD MOUNT CRACKED. REMOVED G/B PER MM-72-00, INSTALLED O/H G/B PER MM-72-0. INSTALLED FUEL LINE FROM FUEL OIL COOLER PER MM 28-40-3, LEAK CHECK, NO LEAK FOUND. OPS CHECKED ENGINE RUN AND TRIM, N/R 6179. 2 L 7 3 4F A3WE 1999082000427 19990820 00427 NM 1999 8 20 DHL9970332C 1 19990721 A 5312 BULKHEAD PANEL BOEING 727 72730C 1384009 NM BS 1183 CRUSHED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, RT BS 1183 BULKHEAD PANEL IS CRUSHED AT LOWER END. REPLACED RT STA 1183 BLKHD PANEL PER 53-20-11 MATERIAL U SED P/N AE4155-81162, APPROXIMATELY 7X4N/R 5118. 2 L 7 3 4F A3WE 1999082000428 19990820 00428 NM 1999 8 20 DHL9970334C 1 19990806 A 5753 652919510 TRACK BOEING 727 72730C 1384009 NM NR 3 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, NR 3 FLAP TRACK MOVABLE FAIRING O/B TRACK CRACKED. REMOVED AND REPLACED TRACK PER SRM 51-30-2, N/R 5107. 2 L 7 3 4F A3WE 1999082000429 19990820 00429 NM 1999 8 20 DHL9970335C 1 19990730 A 5312 BULKHEAD SKIN BOEING 727 72730C 1384009 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 C-CK, CRACK BS 1183 BULKHEAD SKIN, AFT BAG COMPT WL 182 RBL 15. OVERSIZED HOLE BY .015625 TO REMOVE INDAT WL190 RBL 15. 5 AND ACCOMP PER SRM 51-10-1, VERIFIED CRACK NOT VISIBLE NDT PROCEDURE HFEC B727, PER NDT MANUAL PART 6510000 FIG 4. NO CRACK IND. DRILLED OUT, INADVERT DRILL START RBL 16 WL 190 & INSTALLED FREEZE PLUG PER BOEING TELEX DHL-MIA-99-00006H. INSTALLED DOUBLER REPAIR BS 1183 BLKHDWL 182 RBL 15 PER SB 53-0175 & BOEING TELEX DHL-MIA-99-00003H AND DHL, MIA-99-00 006 MATERIAL USED 7075 T6 .063 36X12 1/2. ALODINED & PRIMED PER SRM 51-10-2. INSTALLED SERRATED PLATE AT AFT AIRSTAIR DOOR PER SRM 51-30-2. INSTALLED LT & RT AFT AIRSTAIR ACCESS DOOR PER SRM 51-30-2. OPS CK IAW 52-62-10, N/R 3201. 2 L 7 3 4F A3WE 1999082000430 19990820 00430 NM 1999 8 20 DHL9970336C 1 19990730 A 5312 BULKHEAD SKIN BOEING 727 72730C 1384009 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, CRACK AT BS 1183 BULKHEAD SKIN AFT CARGO COMPT WL 182 LBL 15. REMOVED FASTENERS AND STOP DRILLED CRACK PER SRM 51-30-2, AND 51-10-1 PG NR 7. PERFOMRED HFEC INSPECT. NO CRACK IND PAST STOP DRILLS. CUT OUT DAMAGED AREA PER SB 727-53-0175. REMOVED FASTENERS AT AFT BLKD WEB STA 1183 FROM LBL 20 TO RBL 20 PER SB 53-0175, HFEC INSP EXISTING FASTEN ER HOLES IAW S/B 727-51-0175. FOUND CRACK EXTENDING 4 FROM FASTENER HOLES DOWN OF WL 176 AT LBL 6, CUT AWAY DAMAGED ARE A. VERIFIED NO CRACKS. CLEANED AND PRIMED AREA. INSTALLED DOUBLER REPAIR AT BS 1183 BULKHEAD WL 182 LBL 15. MATERIAL USED 7075 T6 .063 36X113/4, N/R 3074/3200. 2 L 7 3 4F A3WE 1999082000431 19990820 00431 NM 1999 8 20 DHL9970338C 1 19990719 A 5312 BULKHEAD BOEING 727 72730C 1384009 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C-CHECK, CRACK AT 1183 BULKHEAD SKIN AFT CARGO COMPT WL 172 RBL 8. REMOVED FASTENERS AND STOP DRILL CRACK AT 1183 BL KD WL 172 RBL 8. PERFORMED HFEC INSPECTION PER NDT MANUAL PART 6 51-00-00 FIG 4. NO CRACK IND PAST STOP DRILLS, CUT OU T DAMAGED AREA PER SB 727-53-0175. REMOVED STIFFENER AT 1183 RBL 8 AND LBL 8 FOR ACCESS PER SB 727-53-0175. REMOVED FA STENERS AT WEB AFT BLKHD BS 1183 FROM LBL 20 TO RBL 20. HFEC INSPECT EXISTING FASTENER HOLES. NO CRACK INDICATIONS NOT ED IN AREA OF WL 172 TO LOWER END. INSTALLED DOUBLER REPAIR AT BS 1183 BULKHEAD. MATERIAL USED 7075 T6 .063 36X12 1/2 . ALODINED AND PRIMED, REINSTALLED STIFFENER PER SRM 51-30-2, N/R 3073/5108. 2 L 7 3 4F A3WE 1999082000432 19990820 00432 NM 1999 8 20 DHL9970339C 1 19990720 A 5720 ANGLE BOEING 727 72730C 1384009 NM WS 115 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C-CHECK, LEFT WING LEADING EDGE CAVITY AREA FSS 115.0 VERTICAL ANGLE CRACKED LOSER SECTION. CUTOUT DAMAGED SECTION 3 BY 2 PER SRM 51-40-3. FABRICATED NEW VERTICAL ANGLE PER SRM 51-40-3 FIGURE 1, MATERIAL USED 7075-0 .071 3 BY 8, .375 INCH, HEAT TREATED 7075-0 TO 7075 T6 PER PMS I.247PS-01. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED VERTICAL ANGLE REPAIR PER SRM 51-40-3 FIGURE 1. SEALED FASTENERS INSIDE FUEL TANK PER MM 28-11-00. LEAK CHECK FOUND TO BE NORMAL PER MM 28-11-0. N/R 1205. 2 L 7 3 4F A3WE 1999082000433 19990820 00433 NM 1999 8 20 DHL9970340C 1 19990720 A 5753 CARRIAGE BOEING 727 72730C 1384009 NM NR 4 TE FLAP LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 LS NR 4 FLAP CARRIAGE HAS THRUST NUT LOOSE, IT HAS EXCESS CLEARANCE BETWEEN SHIMS AND FLAP FITTING. REMOVED LEFT INBOAR D FLAP ASSY PER MM 27-51-3. FOUND LEFT INBOARD THRUST BEARING CASTING OUT OF LIMITS PER MM 27-51-3. REMOVED CARRIAGES FROM OLD FLAP AND TRANSFERRED TO NEW FLAP ASSY PER B 727 MM 27-51-3. INSTALLED LEFT INBOARD FLAP ASSY PER MM 27-51-3. A DJUSTED TRAILING EDGE FLAP TO ROLLER CLEARANCE AND ADJUSTED DROOP PER MM 27-51-3. OPS CK NORMAL PER MM 27-51-3, N/R 114 4. 2 L 7 3 4F A3WE 1999082000434 19990820 00434 NM 1999 8 20 DHL9970341C 1 19990730 A 3270 652561411 HINGE FITTING BOEING 727 72730C 1384009 NM TAIL SKID DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C-CHECK, LEFT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT TAIL SKID DOOR HINGE FITTING AS PER SR M 51-30-2, N/R 3197. 2 L 7 3 4F A3WE 1999082000435 19990820 00435 NM 1999 8 20 DHL9970342C 1 19990730 A 3270 652561412 HINGE FITTING BOEING 727 72730C 1384009 NM TAIL SKID DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, RT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED RT TAIL SKID DOOR HINGE FITTING PER SRM 51-30 -2, N/R 3198. 2 L 7 3 4F A3WE 1999082000436 19990820 00436 NM 1999 8 20 DHL9970344C 1 19990729 A 5320 ANGLE BOEING 727 72730C 1384009 NM BS 930 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 C-CK, LT WING BS 930 LBL 64 VERT ANG CRACKED. R & R FITTING AT LT STA 930 LBL 64, ALOD & PRIM. INSTALL SPLICES STA 920 STR 15/16 RT. INSTALL REPAIR STR 14 & SUB FLOOR WEBS STA 930-940 & 920-930. REPLACED FLOOR PANEL, INSTALL LT W/W EMER G GEAR EXTEN AND FASTENERS AT SEAT TRACK. REMOVE FLOOR PANEL BS 930 VERIFIED CRACK IN VERT FLANGE CRACK ENDS IN RADIUS & CRACK IN HORIZ FLANGE IN CABIN CRACKED AFT FLANGE AT WEB. REMOVE LT W/W EMERG GEAR EXTEN PULLEY, CUT OUT STR 15/16 BS 920 & Z ANGLE NR 14. REMOVE FASTENERS O/B SEAT TRACK STA 890-950 LBL 6. GEAR SWING & EMERG EXTEN OPS CK FOUND NORM. C UT WINDOW FRAME FLANGE STA LT 935 FOR S/M ACCESS & REPAIR WITH WINDOW FRAME DOUBLER P/N 65L15732-19 PER SB 727-53-11. 2 L 7 3 4F A3WE 1999082000437 19990820 00437 NM 1999 8 20 DHL9970345C 1 19990721 A 5241 DOOR BOEING 727 72730C 1384009 NM GALLEY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, GALLEY DOOR UPPER FLAP HINGE HAS CORROSION. REMOVED GALLEY DOOR UPPPER FLAP PER MM 20-10-1. INSTALLED GALL EY DOOR UPPER FLAP (GATE ASSY) PER MM 52-12-0. REMOVED AND REPLACED PIN STOP ON GALLEY DOOR UPPER FLAP PER 52-12-0. SE ALED OUTSIDE OF DOOR WITH RTV SILICONE SEALANT PER MM 57-30-0, N/R 3142. 2 L 7 3 4F A3WE 1999082000438 19990820 00438 NM 1999 8 20 DHL9970346C 1 19990716 A 2760 LINK BOEING 727 72730C 1384009 NM NR 5 SPOILER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, L/W NR 5 SPOILER ACTUATOR GRAY LINK HAS CORROSION INSIDE WING CAVITY. REMOVED LW NR 5 SPOILER ACTUATOR GREY LINK PER MM 57-55-00. REPLACE ACTUATOR LINK PER MM 27-61-81, OPS CHECKED GOOD IAW 27-61-0 N/R 1153. 2 L 7 3 4F A3WE 1999082000439 19990820 00439 NM 1999 8 20 DHL9970347C 1 19990729 A 5512 SKIN BOEING 727 72730C 1384009 NM LT HORIZ STAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, LT INBD HORIZONTAL STABILIZER LEADING EDGE DAMAGED. REMOVED LEADING EDGE FOR APPROX STA 20 LE TO LE STA 147 .32 PER SRM 51-30-2. REMOVED RIBS TO AID IN MAINTAINING CONTOUR OF LEADING EDGE IAW SRM 51-30-2. CUT OUT DAMAGED AREA AT LT LEADING I/B HORIZONTAL STAB LEADING EDGE 6 BY 2.5 PER SRM 55-10-3 FIG 2. INSTALLED FLUSH REPAIR AT L/E PER SRM 5 5-10-3 FIG 2 MATERIAL USED 7075 T6 .063 10 BY 7 DOUBLER, FILLER 6X2 1/2 2024 T3 .050. ALODINED AND PRIMED PER 51-10-2, REINSTALLED FASTENER PER SRM 51-30-2. REINSTALLED LEFT I/B L/E PER SRM 51-30-2, SEALED PER SRM 51-20-4 N/R 4166. 2 L 7 3 4F A3WE 1999082000440 19990820 00440 NM 1999 8 20 DHL9970348C 1 19990729 A 5312 BULKHEAD BOEING 727 72730C 1384009 NM BS 870 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 703DH 19010 AT C CHECK, REPLACED TEMP REPAIR WITH PERMANENT REPAIR BS 870 BULKHEAD WEB. REF: AVITAS ENG LETTER 98 PMS 1.213D-1. RE MOVED TEMPORARY REPAIR AT BS 870. REMOVED OLD PRIMER AND PRC AROUND DAMAGED AREA. PERFORMED HFEC INSP OF STOP DRILL AT BS 870 AND WEB IAW NDT PART 6 51-00-00 FIG 4, CRACK IS CONTAINED WITH STOP DRILL, TREATED AREA WITH ALODINED AND PRIMED. FABRICATE DOUBLER FOR BULKHEAD WEB REPAIR. FABRICATE DOUBLER FOR BULKHEAD WEB REPAIR. MATERIAL USED 15-5 PH .050 18 3/4 X 13 1/2 AND 13 1/2 X 12 AFT DOUBLER. INSTALLED DOUBLERS. PRIMED DOUBLERS PER SRM 51-10-2, SEALED EDGE WITH PRC PE R B727 SRM 51-20-3. INSTALLED BOLTS AT KEEL BEAM BRACKET ATTACH TO FWD FACE OF BLKD STA 870. 2 L 7 3 4F A3WE 1999082000441 19990820 00441 NM 1999 8 20 DHL99709002 1 19990810 A 5101 STRUCTURE BOEING 727 72782C 1384026 NM PWA JT8 JT8D7 52053 NE AIRFRAME BIRD STRIKE A DHLA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 709DH 19968 ON TAKEOFF AT 100 AGL, HAD MULTIPLE BIRD STRIKES. COMPLIED WITH BIRD STRIKE INSPECT, NO DEFECT NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1999082000442 19990820 00442 1999 8 20 DHL99720005 4 19990803 A 3416 A3811910006 ALTIMETER BOEING 727 727228 NM RT COCKPIT FAILED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 720DH 19544 F/O'S ALTIMETER STUCK FOR 800 FT DURING CLIMB AT FL 30.0. REPLACED F/O'S ALTIMETER, SYSTEM OPS CHECKED GOOD IAW MM 34-1 2-01. 2 L 7 3 4F A3WE 1999082000443 19990820 00443 NM 1999 8 20 DHL99720006 1 19990812 A 7722 EGT INDICATION BOEING 727 727228 NM NR 1 ENGINE EXCEEDED LIMITS A DHLA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 AFTER TAKEOFF ROTATION, NR 1 EGT WAS GOING TO EXCEED TAKEOFF LIMITS NR 1 THRUST LEVER WAS REDUCED IN ORDER TO MAINTAIN A MAX CONTINUOUS EGT LIMIT OF NR 1 ENGINE. EPR AT THIS POINT WAS 1.70. GROUND RAN NR 1 ENG TO TAKEOFF EPR ALL INDICATIO NS WITHIN LIMITS IAW JRH 06-09 OK TO CONTINUE. 2 L 7 3 4F A3WE 1999082000444 19990820 00444 NM 1999 8 20 DHL99724004 1 19990810 A 7711 EPR INDICATION BOEING 727 727228 NM NR 3 ENGINE ABNORMAL A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 724DH 19862 REJECTED T/O DUE TO ABNORMAL EPR NR 3 ENG INICATION. DEFERRED NR 3 ENG EPR INDICATION. 2 L 7 3 4F A3WE 1999082000445 19990820 00445 GL 1999 8 20 DHL99804003 2 19990809 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C5 GL NR 4 OVERTEMP A DHLA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 804DH 46124 NR 4 ENG OVERTEMP ON T/O TO 912 DEG FOR 1 SECOND, ENG POWER WAS REDUCED TO PREVENT FURTHER OVERTEMP. CHECK EGT RES AND IND ACCURACY CHECK OK PERFORMED THROUGH 7 STEPS OF CFM T/S FAULT 48. NO FAULTS NOTED PER MM 72-00-00 PG 612 3(A). EGT OVERTEMP CAN HAVE A MAXIMUM OF 10 EXCEEDANCE THIS HAS BEEN THE SECOND OCCURRANCE. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999082000446 19990820 00446 NM 1999 8 20 TC8A99024 1 19990813 A 3411 PITOT TUBE BOEING 727 72721C 138400M NM LEFT OBSTRUCTED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 705A 19134 AT 80 KTS ON FIRST OFFICER AIRSPEED INDICATOR 0 KTS ON CAPTAINS AIRSPEED INDICATOR, ABORT TAKEOFF. PERFORMED PITOT STAT IC LEAK TEST. FOUND OBSTRUCTION IN CAPTS PITOT TUBE. CLEARED TUBE, LEAK CHECK GOOD IAW MM CHAPT 34-11-0 AND FAR PART 4 3 APPENDIX E. 2 L 7 3 4F A3WE 1999082000865 19990820 00865 WP 1999 8 20 AT9900569 1 19990806 A 5730 PANEL DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND CORROSION ON INNER FLANGE LT PANEL NR 2108A. CLEANED CORROSION ON INNER FLANGE. FABRICATED, TREATED, PRIMED AND INSTALLED STRIPS ON INNER FLANGE IAW DC9 SRM 51-10-3, 51-10-2, 51-10- 4. 2 L 7 2 4F A6WE 1999082000866 19990820 00866 WP 1999 8 20 AT9900570 1 19990809 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING SCHEDULED INSPECTION AT TIMCO, FOUND FLANGE OF LONGERON AT RT BOTTOM OF BS 1076 CHAFED. BLENDED OUT CHAFED AREA. FABRICATED AND INSTALLED EXTERNAL STRAP REPAIR AND FILLER IAW DC9 SRM 51-30-5 AND EO NR 99-1216. 2 L 7 2 4F A6WE 1999082000867 19990820 00867 WP 1999 8 20 AT9900571 1 19990520 A 5312 BULKHEAD PANEL DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING SCHEDULED INSPECTION AT TIMCO, FOUND AFT PIT FWD LT BULKHEAD PANEL HAD SEVERAL SPOTS OF SURFACE CORROSION. MECHA NICALLY CLEANED AREAS, FABRICATED NEW PANEL, LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9 SRM 51-10-4, 51-10-3 . 2 L 7 2 4F A6WE 1999082000868 19990820 00868 WP 1999 8 20 AT9900572 1 19990524 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 408 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 805AT 47378 DURING SCHEDULED INSPECTION AT TIMCO, FOUND FWD CARGO COMPARTMENT HAS BENT AND CRACKED FRAME AT BS 408 L24L. REMOVED CA RGO FRAME FLOOR SUPPORT, FABRICATED REPAIR ANGLE IAW EA NR 12-5321-29-C1362. PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1999082000869 19990820 00869 WP 1999 8 20 AT9900573 1 19990630 A 5320 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 DURING SCHEDULED INSPECTION AT TIMCO, FOUND FWD CARGO DOOR FWD LOWER DOOR JAMB DOUBLER CRACKED. ROUTED OUT CRACK AND FA BRICATED FILLER, DOUBLER AND TRIPLER IAW TIMCO RES NR 07030, DRAWING SR09530117 AND DC9 SRM 51-10-2, 51-10-4, 51-10-3, 53-05 FIG 105. 2 L 7 2 4F A6WE 1999082000870 19990820 00870 WP 1999 8 20 AT9900574 1 19990628 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-408 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 DURING SCHEDULED INSPECTION AT TIMCO, FOUND SEVERAL DENTS IN SKIN FROM BS 229-408 L18R AND L-26R. REMOVED AND REPLACED SKIN FROM BS 229-408 L18R-26R. INSTALLED NEW SPLICE SECTION IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5 AND TIMCO EO NR 99-1178. 2 L 7 2 4F A6WE 1999082000871 19990820 00871 NM 1999 8 20 AT9900575 1 19990813 A 7931 FITTING BOEING 737 737297 1384480 NM NR 1 ENG GEARBOX DAMAGED A ZZDA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 462AT 22631 AT ALTITUDE NR 1 ENGINE OIL QUANTITY WENT TO ZERO AND OIL PRESSURE DROPPED INTO THE AMBER BAND. SHUT DOWN THE ENGINE AN D RETURNED. OIL PRESSURE REMAINED AT 35 PSI FOR 40 MIN WINDMILL. INSPECTED, FOUND FITTING UNSECURED. THREAD DAMAGED. REPAIRED GEARBOX, INSTALLED FITTING AND OPS AND LEAK CHECK GOOD. ALL WORK PERFORMED IAW 737 MM 79-00. 2 L 7 2 4F A16WE 1999082000872 19990820 00872 WP 1999 8 20 AT9900576 1 19990622 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, FOUND AFT CARGO COMPARTMENT DOOR JAMB BS 937 CORRODED BETWEEN L25R-L28R. FORMED R EPAIR INTERCOSTAL, HEAT TREATED. REMOVED AND INSTALLED REPAIR INTERCOSTAL IAW DC9 SRM 51-10-3, 51-30-2, 53-05-10, 53-05 -1. 2 L 7 2 4F A6WE 1999082000873 19990820 00873 WP 1999 8 20 AT9900577 1 19990629 A 5414 985821717 PANEL DOUG DC9 DC932 3022066 WP LT PYLON CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, FOUND PANEL NR 8105A ON THE LEFT LOWER PYLON CORRODED. REMOVED AND REPLACED PANEL NR 8105A IAW DC9 SRM 51-30-1, 54-02, 51-10-3. 2 L 7 2 4F A6WE 1999082000874 19990820 00874 WP 1999 8 20 AT9900578 1 19990730 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 164 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, TERMINATED TEMPORARY REPAIR OF RT WING AFT SPAR AT XRS 164. REMOVED TEMPORARY REP AIR. INSTALLED PERMANENT REPAIR IAW DOUGLAS DRAWING JO6016. 2 L 7 2 4F A6WE 1999082000875 19990820 00875 WP 1999 8 20 AT9900579 1 19990730 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 164 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, TERMINATED TEMPORARY REPAIR OF LT WING AFT SPAR AT XRS 164. REMOVED TEMPORARY REP AIR, INSTALLED PERMANENT REPAIR IAW DOUGLAS DRAWING JO60165. 2 L 7 2 4F A6WE 1999082000876 19990820 00876 WP 1999 8 20 AT9900580 1 19990725 A 5754 SKIN DOUG DC9 DC932 3022066 WP NR 3 LE SLAT PUNCTURE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, FOUND TEMPORARY REPAIR OF POSSIBLE PUNCTURE OF RT WING LEADING EDGE NEAR FUELING D OOR. REMOVED RT NR 3 SLAT. INSPECTED PER DC9 NDT SRM. NO NEW CRACKS FOUND. REMOVED INSIDE SKIN PER SRM 57-09. FABRI CATED REPAIR DOUBLERS AND SPLICES. INSTALLED REPAIR DOUBLERS AND SPLICES. REINSTALLED SLAT, WORK DONE IAW DC9 SRM 51-1 0-3, 51-30-2 AND AIRTRAN RES 982250. 2 L 7 2 4F A6WE 1999082000877 19990820 00877 WP 1999 8 20 AT9900581 1 19990730 A 5754 SKIN DOUG DC9 DC932 3022066 WP RT LE FLAP CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, FOUND RT WING LEADING EDGE INBOARD FLAP SURFACE HAS SURFACE CORROSION. REMOVED CO RROSION, DYE PENETRANT AND HFEC INSPECTION. NO RELEVANT INDICATIONS. ALODINED, PRIMED IAW DC9 SRM 51-10-3 AND TIMCO EO NR 99-1192. 2 L 7 2 4F A6WE 1999082000878 19990820 00878 WP 1999 8 20 AT9900582 1 19990721 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 370-427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, FOUND FWD CARGO DOOR CUTOUT LOWER SKIN CORRODED AT BS 370-427. TRIMMED, DRILL, CO UNTERSUNK REPAIR DOUBLER AND TRIPLER. PRIMED, TREATED, INSTALLED FILLERS, DOUBLER AND TRIPLER IAW EO 99-1187. 2 L 7 2 4F A6WE 1999082000879 19990820 00879 WP 1999 8 20 AT9900583 1 19990625 A 5347 S29559781200 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING SCHEDULED INSPECTION AT TIMCO, FOUND CARGO TRACK CORRODED. FABRICATED NEW TRACK IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1999082000880 19990820 00880 NM 1999 8 20 CALA9901046 1 19990812 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 390 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 390. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 1999082000881 19990820 00881 WP 1999 8 20 CALA9901047 1 19990813 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 826-927 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND FLOORBOARD SUPPORT WORN AT STA 826-927, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30 -8. 2 L 7 2 4F A6WE 1999082000882 19990820 00882 WP 1999 8 20 CALA9901048 1 19990813 A 5753 TRACK DOUG DC9 DC982 3022082 WP RT TE FLAP WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND RT WING NR 1 FLAP TRACK WORN. THE NR 1 FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-1. 2 L 7 2 4F A6WE 1999082000883 19990820 00883 WP 1999 8 20 CALA9901049 1 19990813 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 864 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND LT FORWARD EMERGENCY EXIT DOOR CUTOUT PAN BEHIND UPPER DOOR STOP GOUGED AT FS 864, LONGERON 11L. REPAI RED IAW SRM 53-05, FIGURE 32, 51-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1999082000884 19990820 00884 WP 1999 8 20 CALA9901050 1 19990814 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT Y= 1887, X= 3R TO 70R AND AT Y= 1887, X= 3L TO 70L, J CAPPING ST RIP. THE CORRODED SECTIONS OF CAPPING STRIP WERE REMOVED. NEW SECTIONS OF CAPPING STRIP WERE INSTALLED IAW GMM 10-100- 01. 2 L 7 3 4F A22WE 1999082000885 19990820 00885 WP 1999 8 20 CALA9901051 1 19990814 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1990-1996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND THE LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1990-1996, X= 22R. REPAIRED IAW SRM 53-70-00, F IGURE 13 AND 14. 2 L 7 3 4F A22WE 1999082000886 19990820 00886 WP 1999 8 20 CALA9901052 1 19990814 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1838-1873 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED AT STA Y= 1838-1873, X= 3R. THE CORRODED SECTION OF SUPPORT B EAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-100-01. 2 L 7 3 4F A22WE 1999082000887 19990820 00887 NM 1999 8 20 CALA9901053 1 19990814 A 5230 STRUCTURE BOEING 727 727224 1384076 NM CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR LOWER FORWARD AND AFT CORNERS GOUGED. THE FORWARD AND AFT CORNERS OF DO OR WERE REMOVED IAW SRM 51-10-1, PAGE 4. REPAIRED IAW SRM 51-10-2, PAGE 4, 51-10-1, PAGE 4, AND OVERHAUL MANUAL 52-30-2 3, PAGE 403. 2 L 7 3 4F A3WE 1999082000888 19990820 00888 NM 1999 8 20 CALA9901054 1 19990814 A 5720 ANGLE BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FOUR CRACKS IN RT WING FIXED LEADING EDGE RIB TO SKIN INBOARD SIDE CURVED ATTACH ANGLE AT WBL 92, ACCES S CUTOUT 6401. THE CRACKS MEASURED FROM .5 TO FIVE INCHES IN LENGTH. THE CRACKS WERE STOP DRILLED, A REPAIR DOUBLER, A NGLE AND STIFFENER WERE INSTALLED IAW SRM 57-30-4, 51-40-3, 51-10-2, 51-40-3, AND 51-30-4. 2 L 7 3 4F A3WE 1999082000889 19990820 00889 NM 1999 8 20 CALA9901055 1 19990814 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 320 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 320, BL 0 TO LBL 42. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS IN STALLED IAW SRM 53-10-8, PAGE 51-52. 2 L 7 3 4F A3WE 1999082000890 19990820 00890 NM 1999 8 20 CALA9901056 1 19990814 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312 BETWEEN LBL 10 AND RBL 32. INSTALLED REPAIR IAW SRM 53-10-51, FIGURE 205 . 2 L 7 2 4F RT A16WE 1999082000891 19990820 00891 NM 1999 8 20 CALA9901057 1 19990815 A 3350 20131A BATTERY PACK RADIANT BOEING 737 7373T0 1384582 NM R1 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17328 23458 THE EMERGENCY EXIT LIGHT ABOVE R-1 DOOR ILLUMINATED FOR FIVE SECONDS THEN EXTINGUISHED DURING TEST. THE BATTERY PACK WA S REMOVED AND REPLACED, OPERATION CHECKED GOOD IAW MM 33-51-51, PAGE 203. 2 L 7 2 4F RT A16WE 1999082000892 19990820 00892 NM 1999 8 20 CALA9901058 1 19990815 A 5320 WEB BOEING 727 727224 1384076 NM BS 1110-1130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A 1.5 INCH CRACK AND A BEND IN INTERCOSTAL WEB BETWEEN BS 1110-1130, BL 0. THE INTERCOSTAL WEB WAS REM OVED AND REPLACED IAW SRM 51-10-1, PAGE 2 AND 4. 2 L 7 3 4F A3WE 1999082000893 19990820 00893 NM 1999 8 20 CALA9901059 1 19990815 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND CORROSION ON FLOORBEAM WITH FASTENERS PULLED THROUGH AT STA 328, LBL 11. THE CORRODED SECTION OF FLOOR BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999082000894 19990820 00894 WP 1999 8 20 CALA9901060 1 19990816 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 6 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND EMERGENCY LIGHT AT ROW 6DEF INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT AND OPERATION CHE CKED GOOD. 2 L 7 2 4F A6WE 1999082000895 19990820 00895 NM 1999 8 20 CALA9901061 1 19990816 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 328 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 328, WL 190. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 1999082000896 19990820 00896 NM 1999 8 20 CALA9901062 1 19990815 A 2612 FIRELOOP BOEING 737 7373T0 1384582 NM APU SHORTED A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 47332 23570 THE APU FIRE DETECT LIGHT ILLUMINATED WHILE ON CLIMBOUT OF EWR. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTING UISHED. THE APU FIRE LIGHT CAME BACK ON ABOUT FIVE MINUTES LATER. THE AIRCARFT WAS RETURNED TO EWR WHERE IT LANDED WIT HOUT INCIDENT. THE APU WAS INSPECTED AND NO EVIDENCE OF FIRE WAS FOUND. TROUBLESHOOTING FOUND THE LOWER APU LOOP SHORT ING TO CASE GROUND. THE LOWER APU FIRELOOP WAS REPLACED. OPERATION CHECKED GOOD. IN ADDITION, THE FIRE DETECTION MODU LE AND ENGINE AND APU ASSEMBLY MODULE WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE APU FIRE BOTTLE WAS REMO VED AND REPLACED IAW MM 26-22-11. 2 L 7 2 4F RT A16WE 1999082000897 19990820 00897 EA 1999 8 20 COMA9960453 1 19990815 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAPS FAILED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 710CA 10001 996 7241 FLAPS FAILED. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999082000898 19990820 00898 EA 1999 8 20 COMA9960454 1 19990816 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 988CA 7204 DOOR WARNING AFTER TAKEOFF. INSPECTED DOOR AND DOOR WARNING SYSTEM. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999082000899 19990820 00899 NM 1999 8 20 UPS99230328 1 19990817 A 3350 LIGHT BOEING 727 727108C 1384039 NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOP. REPLACED BATTERIES, OPS CKS OK. 2 L 7 3 4F A3WE 1999082000900 19990820 00900 NM 1999 8 20 UPS99230329 1 19990817 A 3350 LIGHT BOEING 727 727108C 1384039 NM FLIGHT DECK INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:N/A COCKPIT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERIES, LIGHTS OPS CK OK. 2 L 7 3 4F A3WE 1999082000901 19990820 00901 NM 1999 8 20 UPS99230332 1 19990723 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN IS BULGED FROM STR 1 TO STR 4 RT BS 620. REMOVED AND REPLACED UPPER FUS ELAGE EXTERIOR SKIN FROM BS 520 TO BS 740 FROM STR 6 LT TO 4 RT AS PER AVITAS REPAIR ORDER 99 AVHM 048RO- 1. PREVIOUSLY ACCOMPLISHED WITH N/R 985901 AND 985502. 2 L 7 3 4F A3WE 1999082000902 19990820 00902 NM 1999 8 20 UPS99230335 1 19990723 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 477 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR REPAIR DOUBLER IS BULGED AT STR 5 RT BS 477. REMOVED AND REPLACED UPPER FUSE LAGE EXTERIOR SKIN FROM BS 440 TO BS 520 FROM STR 10 LT TO 4 RT AND INSTALLED SKIN REPAIR FROM BS 440 TO BS 540 FROM STR 4 RT TO 5 RT AS PER AVITAS 99 AVM 048 RO-1 PREVIOUSLY ACCOMPLISHED WITH NR'S 985901 AND 985502. 2 L 7 3 4F A3WE 1999082000903 19990820 00903 NM 1999 8 20 UPS99230336 1 19990723 A 5230 SKIN BOEING 727 72730C 1384009 NM CARGO DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C, MAIN CARGO DOOR EXTERIOR SKIN IS DENTED 6 INCHES BELOW THE DOOR HINGE BS 548. REWORKED MAIN CARGO DO OR EXTERIOR SKIN BS 548 AS PER SRM 51-40-1, DENT OUT OF LIMITS. CUT OUT SKIN DAMAGED AREA AS PER B727 SRM 52-00-3, INST ALLED DOUBLER PER B727 SRM 52-00-3 PAGE 1. 2 L 7 3 4F A3WE 1999082000904 19990820 00904 NM 1999 8 20 UPS99230339 1 19990723 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN AT SKIN LAP STR 4 RT BS 620 IS BULGED. REMOVED AND REPLACED UPPER FUSEL AGE EXTERNAL SKIN FROM BS 520 TO BS 740 FROM STR 6 LT TO 4 RT AS PER AVITAS REPAIR ORDER 99 AVNM 048RO-1, PREVIOSLY ACCO MPLISHED WITH N/R 985901 AND 985502. 2 L 7 3 4F A3WE 1999082000905 19990820 00905 NM 1999 8 20 UPS99230341 1 19990723 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN IS BULGED AT STR 4 RT TO STR 5 RT BS 480. REMOVED AND REPLACED SKIN FRO M BS 440 TO BS 520 FROM STR 10 LT TO 4 RT AND INSTALLED SKIN REPAIR FROM BS 440 TO BS 540 AND FROM STR 4 RT TO STR 5 RT AS PER AVITAS REPAIR ORDER 99AVHM049RO-1, PREVIOUSLY ACCOMPLISHED WITH N/R 985901 AND 985502. 2 L 7 3 4F A3WE 1999082000906 19990820 00906 WP 1999 8 20 UPS99830330 1 19990812 A 3350 6012235 LIGHT DOUG DC8 DC873F 302199F WP FLIGHT DECK INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:IN, EMERGENCY EXIT LIGHT IN COCKPIT DOME AND ENTRY INOP. REMOVED AND REPLACED BATTERY PACK, CK OK. ON (P/N 5708458-503) (S/N 10389), OFF (S/N 339) (P/N 60-1223-5). 2 L 7 4 4F RT 4A25 1999082000907 19990820 00907 WP 1999 8 20 UPS99830331 1 19990816 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:IN, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK, ON (P/N 60-12 23 -5) (S/N 321), OFF (P/N 5708458-503) (S/N 001). 2 L 7 4 4F RT 4A25 1999082000908 19990820 00908 NM 1999 8 20 QXEA9901645 1 19990811 A 3350 6038443 POWER SUPPLY GRIMES 6104789 DHAV DHC8 DHC8202 2809007 NM ROW 1 & 7-10 INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 348PH 1963 839 484 SEA- CABIN FLOOR EMERGENCY LIGHTS ROWS 1 & 7-10 WOULD NOT SHUTOFF. REPLACED PS2 POWER SUPPLY AND BATTERY, OPERATIONAL T EST GOOD. 2 H 7 2 4T RT A13NM 1999082000909 19990820 00909 NM 1999 8 20 QXEA9901646 1 19990813 A 3350 10005511 LIGHT GRIMES 1014011 DHAV DHC8 DHC8202 2809007 NM COCKPIT INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 353PH 7596 8 496 SEA- COCKPIT HANDHELD EMERGENCY LIGHT ON INTERMITTANT. REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY. FUNCTIONAL TEST CHEC KS NORMAL. 2 H 7 2 4T RT A13NM 1999082000910 19990820 00910 NE 1999 8 20 99FDEA00335 2 19990814 A 7320 7084M12G10 PMC AIRBUS 310 A310203 EU GE CF680 CF680A3 30025 NE NR 2 ENGINE OVERLIMIT A FDEA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 25 426FE 245 DESTINATION THRU FL310 HAD ECAM MSG ENG 2 OVERLIMIT. IND WERE EVIDENT IN N1, EGT, N2 AND HI FF. PULLED THROTTLE TO IDL E & OVERLIMIT ABATED BUT NR 2 STILL MUCH HIGHER THAN ENG NR 1. DFDR VERIFICATION CONFIRMED OVERLIMIT (EGT, N1, N2). PE RFORMED BORESCOPE PER MM NO LIMITING DEFECTS NOTED. REMOVED AND REPLACED NR 2 ENG PMC, PERFORMED TEST PER MM 73-23-00. 2 L 7 2 4F 4 F RT A35EU E13NE 1999082000911 19990820 00911 NM 1999 8 20 99FDEA00336 1 19990817 A 2612 CONNECTOR BOEING 727 72722 1384002 NM NR 2 ENGINE LOOSE A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 149FE 19087 99-210 - FIRE WARN BELL SOUNDED AT ROTATION WITHOUT ASSOC FIRE LIGHTS. BOTH SYS TEST GOOD. NO OTHER IND OF FIRE. NR 2 ENG OPER PWR UNIT AT P6-3 PNL WAS LOOSE ON CONNECTOR, RESECURED AS REQ. GROUND TEST PER MM 26-12-000, 26-11-000, AND 2 6-17-000 OPER CK GOOD. 2 L 7 3 4F A3WE 1999082000912 19990820 00912 WP 1999 8 20 ABXA9900643 1 19990813 A 5320 591000549 PANEL DOUG DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND CORROSION ON LEFT LOWER SLANT PANEL CAP. REPAIRED IAW ABX REA D953-32811MR. 2 L 7 2 4F A6WE 1999082000913 19990820 00913 WP 1999 8 20 ABXA9900644 1 19990816 A 5320 99101515 WEB DOUG DOUG DC9 DC931 3022065 WP BS 598 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND CUSP WEB CRACKED FORWARD AND AFT OF FRAME AT STATION 598, LEFT SIDE. REPLACED CUSP WEB IAW DC9 S RM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999082000914 19990820 00914 WP 1999 8 20 MWEA99479 1 19990805 A 5314 99155251 KEEL TEE DOUG DC9 DC914 3022034 WP BS 498 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 KEEL TEE AT STATION 498 IS CRACKED IN RADIUS. MTC SPLICED IN A NEW TEE SECTION. 2 L 7 2 4F A6WE 1999082000915 19990820 00915 WP 1999 8 20 MWEA99480 1 19990805 A 2560 100502121 EVAC SLIDE DOUG DC9 DC981 3022081 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 804ME 48030 EMERGENCY SLIDE ON AFT GALLEY DOOR NEEDS TO BE RESECURED TO SLIDE DOOR ASSEMBLY. INSTALLED AFT GALLEY SLIDE DOOR. 2 L 7 2 4F A6WE 1999082000916 19990820 00916 NM 1999 8 20 MWEA99481 1 19990810 A 2560 D29982107 EVAC SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 701ME 49760 FORWARD GALLEY SERVICE DOOR ESCAPE SLIDE PACK NOT SECURED. REINSTALLED SLIDE PACK AND LANYARD. 2 L 7 2 4F RT A6WE 1999082000917 19990820 00917 NM 1999 8 20 MWEA99482 1 19990810 A 2560 D29982107 SLIDE DOUG MD88 MD88 3023688 NM PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 FORWARD ENTRANCE DOOR EMERGENCY SLIDE ATTACHMENT CABLE CAME LOOSE FROM DOOR CONNECTION. REINSTALLED SLIDE COVER AND RET AINING CLIP. 2 L 7 2 4F RT A6WE 1999082000918 19990820 00918 WP 1999 8 20 MWEA99483 1 19990809 A 2560 113317 SLIDE DOUG DC9 DC915 3022036 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 300ME 45718 GALLEY DOOR SLIDE COVER POPPED OFF WHEN DOOR WAS CLOSED. REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999082000919 19990820 00919 WP 1999 8 20 MWEA99484 1 19990812 A 2560 100503119 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 804ME 48030 THE AFT GALLEY SLIDE PACK WAS LOOSE. MTC RESECURED AFT GALLEY SLIDE PACK. 2 L 7 2 4F A6WE 1999082000920 19990820 00920 WP 1999 8 20 MWEA99485 1 19990812 A 5512 5918002502N SKIN DOUG DC9 DC914 3022034 WP LT HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 UPPER LEFT HORIZONTAL STABILIZER SKIN FOUND CRACKED. MTC FABRICATED AND INSTALLED NEW SKIN PANEL. 2 L 7 2 4F A6WE 1999082000921 19990820 00921 WP 1999 8 20 MWEA99486 1 19990812 A 5320 5912528501 JAMB DOUG DC9 DC914 3022034 WP BS 755 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DOOR JAMB AT L28R STATION 755 IS GOUGED. MTC FABRICATED AND INSTALLED DOOR JAMB. 2 L 7 2 4F A6WE 1999082000922 19990820 00922 WP 1999 8 20 MWEA99487 1 19990812 A 5347 S2772660 SEAT TRACK DOUG DC9 DC914 3022034 WP BS 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 SEAT TRACK NR 4 FROM STATION 200 TO 218 HAS NUMEROUS AREAS OF LIGHT CORROSION AND TOOL MARKS. MTC FABRICATED AND INSTAL LED NEW SEAT TRACK. 2 L 7 2 4F A6WE 1999082000923 19990820 00923 WP 1999 8 20 MWEA99488 1 19990812 A 5312 59148653 BULKHEAD PANEL DOUG DC9 DC914 3022034 WP BS 503 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 TOOLING DAMAGE BY 6 RIVETS ON FORWARD BAG PIT AT AFT PRESSURE BULKHEAD BOTTOM BETWEEN LONGERON 28L AND 28R. MTC FABRICA TED AND INSTALLED NEW BULKHEAD PANEL. 2 L 7 2 4F A6WE 1999082000924 19990820 00924 WP 1999 8 20 MWEA99489 1 19990812 A 5720 39373041 SPLICE DOUG DC9 DC982 3022082 WP LT WING SPAR MISINSTALLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 LEFT WING UPPER REAR SPAR SPLICE PLATE REMOVED FOR INCORRECT BUSHING ALIGNMENT. MTC FABRICATED AND INSTALLED NEW SPAR S PLICE. 2 L 7 2 4F A6WE 1999082000925 19990820 00925 WP 1999 8 20 MWEA99490 1 19990812 A 2560 113317 DOOR SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 216ME 47740 THE GALLEY DOOR SLIDE FELL OFF. MTC RESECURED DOOR SLIDE. 2 L 7 2 4F A6WE 1999082000926 19990820 00926 WP 1999 8 20 MWEA99492 1 19990806 A 5311 27779305 FORMER DOUG DC9 DC914 3022034 WP BS 801 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 AFT CARGO COMPARTMENT AT STATION 801 FRAME FORMER CRACKED LEFT SIDE OF LONGERON 30. MTC FABRICATED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 1999082000927 19990820 00927 WP 1999 8 20 MWEA99493 1 19990806 A 5230 59101584 INTERCOSTAL DOUG DC9 DC914 3022034 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 AFT CARGO DOOR INTERCOSTAL AT STATION 730 HAS CORROSION UNDER NUT PLATE. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999082000928 19990820 00928 WP 1999 8 20 MWEA99494 1 19990806 A 5320 59160641 FITTING DOUG DC9 DC914 3022034 WP BS 470 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FORWARD CARGO PIT LONGERON 30 END FITTING CRACKED BETWEEN STATION 470-484. MTC REMOVED AND REPLACED END FITTING. 2 L 7 2 4F A6WE 1999082000929 19990820 00929 WP 1999 8 20 MWEA99495 1 19990806 A 5330 59114185 SKIN DOUG DC9 DC914 3022034 WP BS 484 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 LIGHT CORROSION ON INTERNAL SKIN AREA OF LONGERON 30 AT STATION 484. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999082000930 19990820 00930 WP 1999 8 20 MWEA99496 1 19990806 A 5320 591486529 TEE DOUG DC9 DC914 3022034 WP BS 490 OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 THE TEE AT STATION 490 LONGERON 30 IS BLENDED OUT OF LIMITS. MTC REMOVED AND REPLACED TEE. 2 L 7 2 4F A6WE 1999082000931 19990820 00931 WP 1999 8 20 MWEA99497 1 19990806 A 5320 3915130502N FITTING DOUG DC9 DC914 3022034 WP BS 490-498 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 RIGHT LONGERON 30 END CAP FITTING AT STATION 490-498 IS CORRODED. MTC REMOVED AND REPLACED END CAP FITTING. 2 L 7 2 4F A6WE 1999082000932 19990820 00932 WP 1999 8 20 MWEA99498 1 19990806 A 5320 3915130501 BRACKET DOUG DC9 DC914 3022034 WP BS 490-498 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 LONGERON 30 LEFT END CAP BRACKET AT STATION 490-498 WAS CRACKED. MTC REMOVED AND REPLACED END CAP BRACKET. 2 L 7 2 4F A6WE 1999082000933 19990820 00933 WP 1999 8 20 MWEA99499 1 19990806 A 5330 5914863 SKIN DOUG DC9 DC914 3022034 WP BS 490 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 UNDERWING PRESSURE DOME AT STATION 490 HAS CORROSION AND TOOLMARKS BEYOND LIMITS. MTC FABRICATED AND INSTALLED NEW SKIN . 2 L 7 2 4F A6WE 1999082000934 19990820 00934 WP 1999 8 20 MWEA99500 1 19990806 A 5312 59148657 BULKHEAD FITTING DOUG DC9 DC914 3022034 WP BS 490 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 75795 RIGHT AND LEFT FITTINGS FOR PRESSURE BULKHEAD AT STATION 490 WAS CRACKED. MTC REMOVED AND REPLACED FITTINGS. 2 L 7 2 4F A6WE 1999082000935 19990820 00935 WP 1999 8 20 MWEA99501 1 19990806 A 5320 3913209503 FITTING DOUG DC9 DC914 3022034 WP BS 484 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 LONGERON 24R END FITTING AT STATION 484 WAS CRACKED. MTC REMOVED AND REPLACED END FITTING. 2 L 7 2 4F A6WE 1999082000936 19990820 00936 WP 1999 8 20 MWEA99502 1 19990806 A 5320 5913209501N FITTING DOUG DC9 DC914 3022034 WP BS 484 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 LONGERON 26R END FITTING AT STATION 484 IS CORRODED. MTC REMOVED AND REPLACED END FITTING. 2 L 7 2 4F A6WE 1999082000937 19990820 00937 WP 1999 8 20 MWEA99503 1 19990806 A 5320 59124112 FITTING DOUG DC9 DC914 3022034 WP BS 484 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 RIGHT FITTING AT STATION 484 WAS CRACKED. MTC REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 1999082000938 19990820 00938 WP 1999 8 20 MWEA99504 1 19990806 A 5230 59101575 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 INNER PAN OF AFT CARGO DOOR HAS CRACKS AND CORROSION. MTC FABRICATED AND INSTALLED DOOR PAN. 2 L 7 2 4F A6WE 1999082000939 19990820 00939 WP 1999 8 20 MWEA99505 1 19990806 A 5230 591015725 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 CRACK FOUND ON AFT CARGO DOOR AFT SIDE BELOW TORQUE TUBES. MTC FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 1999082000940 19990820 00940 WP 1999 8 20 SCNA99104 1 19990814 A 7714 N1 SENSOR 8DJ176WAP2 DOUG DC10 DC1015 3022118 WP NR 2 ENGINE INOPERATIVE A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 151SY R1096 48295 AIRCRAFT ABORTED TAKEOFF AT 120 KNOTS AS NUMBER TWO ENGINE DIDN'T MAKE REDUCED N1. OPERATIONALLY CHECKED THE NUMBER TWO ENGINE IAW DC-10 MM 710000. OPERATIONALLY CHECKED AIRCRAFT PER MM 055700 AFTER HIGH ENERGY STOP. REMOVED AND REPLACED THE NUMBER TWO ENGINE N1 INDICATOR PER MM 771000 AND SWITCHED THE NUMBER TWO ENGINE N1 SENSOR TO THE LEFT SIDE SENSOR. 2 L 7 3 4F A22WE 1999082000941 19990820 00941 SO 1999 8 20 SWIA971536 1 19990801 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 NM 07 203SW 120240 RIGHT NP WENT TO 102.3 PERCENT AND STAYED THERE FOR APPROX 2 MINUTES UNTIL PROP SYNC TURNED OFF. RETURNED TO SLC. REMO VED AND REPLACED RIGHT PCU, OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999082000942 19990820 00942 NE 1999 8 20 SWIA971537 2 19990809 A 7510 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA E ENGINE SHUTDOWN M OVER TEMP DE DESCENT 1 NM 07 188SW 120039 RIGHT ENGINE DUCT LEAK LIGHT CAME ON DURING DESCENT. SHUT ENGINE DOWN ACCORDING TO QRH PROCEDURES. REMOVED AND REPLACE D RIGHT DE-ICE PRESSURE REGULATOR. RUN UP CHECKS GOOD ON DUCT LEAK. NO LEAKS FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999082000943 19990820 00943 EU 1999 8 20 RAIA990731 1 19990704 A 2761 TY176301D ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU RT SPOILER FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 573HK 41092 DCA - FLT 7740 - SPOILER WILL NOT DEPLOY. MAINTENANCE REPLACED SPOILER ACTUATOR ON RT SIDE. (X) 2 L 7 2 4T RT A41NM 1999082000944 19990820 00944 EU 1999 8 20 RAIA990730 1 19990725 A 7922 L8523427 VERNITHERM BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 341TE 950 STL - FLT 7061 - LEFT ENGINE OIL TEMP RUNNING HOT. MAINTENANCE REPLACED VERNITHERM FOR OIL COOLER ON RIGHT ENGINE. (X) 2 L 7 2 4T RT A56EU 1999082000945 19990820 00945 NM 1999 8 20 UIEA99059 1 19990723 A 5400 65B9410754 TEE CHORD BOEING 747 747230B 1384889 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 79136 14492 21644 DURING ROUTINE INSPECTION OF NR 1 AND NR 4 PYLONS, CRACKS WERE DISCOVERED IN THE RT UPPER TEE CHORD, FORWARD HORIZONTAL FLANGE, NACELLE STA 270. CRACK LENGTH IN NR 1 PYLON WAS 2.25 INCHES, NR 4 PYLON WAS 1.25 INCHES. REPAIRS ACCOMPLISHED IAW KLM DATA FAX 99-088 AND BOEING TELEX NR TLS-AMS-99-0091TE; TLS-AMS-99-00021H; IN ADDITION TO SB 747-54-2125, AND DLM ENGINEERING AND MAINTENANCE REPORT NR KLM 990714. FORM 8110-3 ISSUED. REF: OPER CNTRL NR 99ZZZX3052. (X) 2 L 7 4 4F A20WE 1999082000946 19990820 00946 NM 1999 8 20 99ZZZX3052 1 19990723 A 5400 65B9410754 TEE CHORD BOEING 747 747230B 1384889 NM NR 4 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 79136 14492 21644 DURING ROUTINE INSPECTION OF NR 1 AND NR 4 PYLONS, CRACKS WERE DISCOVERED IN THE RT UPPER TEE CHORD, FORWARD HORIZONTAL FLANGE, NACELLE STA 270. CRACK LENGTH IN NR 1 PYLON WAS 2.25 INCHES, NR 4 PYLON WAS 1.25 INCHES. REPAIRS ACCOMPLISHED IAW KLM DATA FAX 99-088 AND BOEING TELEX NR TLS-AMS-99-0091TE; TLS-AMS-99-00021H; IN ADDITION TO SB 747-54-2125, AND DLM ENGINEERING AND MAINTENANCE REPORT NR KLM 990714. FORM 8110-3 ISSUED. REF: OPER CNTRL NR UIEA99059. 2 L 7 4 4F A20WE 1999082000947 19990820 00947 NM 1999 8 20 UIEA99058 1 19990723 A 5320 FITTING BOEING 747 747230B 1384889 NM BS 1480 INTERFERENCE A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 79136 14492 21644 DURING ROUTINE IMPLEMENTATION OF SB 747-53A2390, FASTENER INTERFERENCE OCCURRED AT THE NR 7 AND NR 8 HOLES IN BOTH THE L EFT AND RIGHT SPLICE AREAS. THE NUTS IN THE SUBJECT AREA INTERFERE WITH THE FLANGE OF THE SPLICE FITTINGS ABOVE THE FAS TENER HOLES. RESOLVED INTERFERENCE BY ENLARGING HOLES TO 05781 INCHES, INSTALLED BUSHINGS AND SMALLER DIAMETER BOLTS PE R BOEING TELEX NR TLS-AMS-99-0087TE; TLS-AMS-99-0017H; TLS-AMS-99-0089TE, AND IAW KLM DATA FAX 99-87. FORM 8110-3 ISSUE D. (X) 2 L 7 4 4F A20WE 1999082000948 19990820 00948 NM 1999 8 20 UIEA99057 1 19990723 A 5720 65B116145 BEAM BOEING 747 747230B 1384889 NM WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 508MC 79136 14492 21644 DURING ROUTINE INSPECTION OF THE WING TRAILING EDGE AREA, FOUND THE UPPER CHORD SUPPORT BEAM CRACKED IN THE VICINITY OF THE LINK ASSEMBLY. MADE PERMANENT REPAIR BY SPLICING IN A REPLACEMENT SECTION IAW KLM ENGINEERING AND MAINTENANCE REPOR T NR 1H105453 AND BOEING TELEX NR TLS-AMS-99-0085TE. FORM 8110-3 ISSUED. (X) 2 L 7 4 4F A20WE 1999082000949 19990820 00949 EU 1999 8 20 SIMA992091 1 19990728 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU DOOR LOOSE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 223AT 223 ORD - FLT 4358 - LOWER EMERGENCY LIGHT AT RIGHT REAR SERVICE DOOR DOES NOT ILLUMINATE. TIGHTENED LOOSE WIRE CONNECTOR A T LIGHT SOCKET. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1999082000950 19990820 00950 EU 1999 8 20 SIMA992101 1 19990729 A 3350 2LA005985 LIGHT SAAB SF340 340B 7860101 EU ROW 3BC FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 353SB 340B353 LAX - FLT 3424 - OVERHEAD EMERGENCY LIGHT AT SEAT 3BC DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT PANEL A T SEAT 3BC. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999082000951 19990820 00951 EU 1999 8 20 SIMA992092 1 19990728 A 5320 S5367800821602 ZEE MEMBER AEROSP ATR72 ATR72212 EU FRAMES 39-41 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-8 INSPECTION, FOUND THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082000952 19990820 00952 EU 1999 8 20 SIMA992093 1 19990728 A 5315 S5337241123402 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE MISDRILLED A SIMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND FLOORBEAM 29 WITH AN OVERSIZED HI-LOCK HOLE AT THE LEFT INBOARD SEAT TRACK CENTER A TTACH POINT. REPAIRED THE FLOORBEAM IAW SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082000953 19990820 00953 EU 1999 8 20 SIMA992094 1 19990728 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAMS 36 AND 38 WITH CORROSION AROUND THE NUTPLATE HOLES. REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435, AND REMOVED AND REPLACED FLOORBEAM 38 IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX3053. (X) 2 H 7 2 4T RT A53EU 1999082000954 19990820 00954 EU 1999 8 20 99ZZZX3053 1 19990728 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAMS 36 AND 38 WITH CORROSION AROUND THE NUTPLATE HOLES. REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435, AND REMOVED AND REPLACED FLOORBEAM 38 IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA992094. 2 H 7 2 4T RT A53EU 1999082000955 19990820 00955 EU 1999 8 20 SIMA992095 1 19990728 A 5320 S5367121720001 WEB AEROSP ATR72 ATR72212 EU FRAMES 36-38 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT AFT WEB BETWEEN FRAMES 36 AND 38 CORRODED. REMOVED AND REPLACED THE WEB IAW 51-25-02. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082000956 19990820 00956 EU 1999 8 20 SIMA992096 1 19990728 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIG HT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE S EAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL 99ZZZX3054 THROUGH 99ZZZX3058. (X) 2 H 7 2 4T RT A53EU 1999082000957 19990820 00957 EU 1999 8 20 99ZZZX3054 1 19990728 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIG HT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE S EAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3055 THROUGH 99ZZ ZX3058. 2 H 7 2 4T RT A53EU 1999082000958 19990820 00958 EU 1999 8 20 99ZZZX3055 1 19990728 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIG HT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE S EAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZ ZX3058. 2 H 7 2 4T RT A53EU 1999082000959 19990820 00959 EU 1999 8 20 99ZZZX3056 1 19990728 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIG HT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE S EAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZ ZX3058. 2 H 7 2 4T RT A53EU 1999082000960 19990820 00960 EU 1999 8 20 99ZZZX3057 1 19990728 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIG HT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE S EAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZ ZX3058. 2 H 7 2 4T RT A53EU 1999082000961 19990820 00961 EU 1999 8 20 99ZZZX3058 1 19990728 A 5347 S53678001225 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIG HT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE S EAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZ ZX3057. 2 H 7 2 4T RT A53EU 1999082000962 19990820 00962 NE 1999 8 20 P2EA99222 2 19990802 A 7200 ENGINE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE BIRD STRIKE A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK C B F.O.D. SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 05 603DJ 19955 MDW - FLT 938 - ABORTED TAKEOFF AT 110 KNOTS DUE A LOUD BANG FOLLOWED BY A BURNT SMELL IN CABIN AND COCKPIT. DISCOVERED BIRD STRIKE NR 1 ENGINE. PERFORMED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. (X) 2 L 7 2 4F 4 F A16WE E2EA 1999082000964 19990820 00964 EU 1999 8 20 FJT99089401 1 19990803 A 5320 137390D120 EDGE MEMBER 137390C415 BAG JETSTM JETSTM3201 1500217 EU BS 485 CRACKED A FJTA K NONE O OTHER IN INSP/MAINT 1 SO 03 940AE 12392 1865 940 MQY - A 3 INCH CRACK WAS FOUND DURING INSPECTION OF THE RUDDER QUADRANT STRUCTURE P/N 137390C415. THE CRACK WAS IN THE EDGE MEMBER P/N 137390C120 WHICH SECURES THE SKINS AND BULKHEADS TOGETHER. THE CRACK IS CAUSED BY THE P/N 137370E6 D-WA SHER (PACKER) WHICH IS CHAFING AGAINST THE RADIUS OF THE EDGE MEMBER P/N 137390C120. THE D-WASHER IS USED TO ASSIST IN ATTACHING THE RUDDER ARTIFICAL FEEL BUNGEES. THE EDGE MEMBER WAS REPLACED AND THE D-WASHER WAS RE-WORKED TO ENSURE A CO RRECT FIT IN RELATION TO THE EDGE MEMBER RADIUS. THE AIRCRAFT RETURNED TO SERVICE. PART TC: 16,556.(X) 2 L 7 2 4T RT A56EU 1999082000966 19990820 00966 CE 1999 8 20 99ZZZX3059 1 19990723 A 3260 24420107 BRACKET LEAR 25 25 5170506 CE NLG DAMAGED A ECAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 11 25EC 25026 NOSE WHEEL UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR WAS SECURED UP. AIRCRAFT RETURNED TO FRG. LANDING GEAR SELECTED DOWN AND SHOWED SAFE. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NOSE GEAR UP AND LOCKED SWITC H BRACKET WAS BENT AND DEFORMED. INVESTIGATION FOUND AIRCRAFT HAD BEEN MOVED BY FBO LINE PERSONNEL JUST PRIOR TO DEPARTU RE FROM FRG. LINE PERSONNEL HAD USED A STRAP STYLE TOWBAR WHICH WAS PLACED TOO LOW, DAMAGING THE BRACKET. 2 L 7 2 4J A10CE 1999082000967 19990820 00967 WP 1999 8 20 AALA991109 1 19990729 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROWS 17-27 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 246AA 49238 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 17 AND 27 INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 17 AND 27. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000968 19990820 00968 EU 1999 8 20 AALA991112 1 19990126 A 3260 D43121403 SENSOR FOKKER F28 F28MK0100 4990807 EU NLG OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1465K 11491 TUL - FLT 9515 - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT, GEAR GREEN LIGHT WAS ILLUMINATED. CYCLED GEAR TWICE AND GR EEN LIGHT STAYED ILLUMINATED. GEAR HANDLE MOVEMENT FELT NORMAL. RETURNED TUL AND LANDED WITHOUT INCIDENT. ADJUSTED NO SE GEAR DOWNLOCK SENSOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999082000969 19990820 00969 NM 1999 8 20 AALA991095 1 19990726 A 3350 0201820001 LIGHT BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321AA 22322 SFO - DURING OVERNIGHT MAINTENANCE, MID-GALLEY RIGHT SIDE EMERGENCY EXIT FLOOR LIGHTING INOPERATIVE. REPLCED EMERGENCY EXT FLOOR LIGHT ASSEMBLY AT RIGHT SIDE OF MID-GALLEY. SYSTEM GORUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999082000970 19990820 00970 EU 1999 8 20 AALA990888 1 19990616 A 2750 A83235415 SYNCHRONIZER FOKKER F28 F28MK0100 4990807 EU LT TE FLAP FAILED A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 1432A 01529 11417 DSM - FLT 1091 - EN ROUTE DFW/DSM DURING CRUISE, HAD FLAP ASEMBLY ON LEFT AND RIGHT MFDU. FLAPS WOULD NOT EXTEND. TRIE D PULLING AND RESETTING 7H, 7J, 40K, 14K CIRCUIT BREAKERS FOR MFDU. WARNINGS EXTINGUISHED, BUT WHEN FLAPS WERE CALLED F OR ON APPROACH NOTHING HAPPENED. MADE ZERO FLAP APPROACH LANDING AT DFW. DECLARED EMERGENCY AND LANDED WITHOUT INCIDEN T. REPLACED LEFT INBOARD FLAP ASSMELBY TRNASMIEMBLY TRANSMITTER. ACCOMPLISHED ALL REQUIRED CHECKS. SYSTEM GROUND CHECK ED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999082000971 19990820 00971 NE 1999 8 20 AALA991093 2 19990723 A 7320 JR34181A AIR FLOW CONTROL FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE NR 2 ENGINE DEFECTIVE A AALA A UNSCHED LANDING Y ENGINE STOPPAGE TO TAKEOFF 1 SW 07 1407D KK11335 11360 JFK - FLT 763 - DURING TAKEOFF ISP/ORD, NR 2 ENGINE FAILED. ENGINE WAS RESTARTED IN-FLIGHT. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED JFK WITHOUT INCIDENT. REPLACED AIR FLOW CONTROL REGULATOR ON NR 2 ENGINE. ALSO REPLACED NR 2 ENGINE F UEL FLOW REGULATOR AS A PRECAUTIONARY MEASURE. PERFORMED ENGINE RUN-UP, TRIM, AND LEAK CHECK, SYSTEM GROUND CHECKED, N ORMAL OPERATION. (X) 2 L 7 2 4F 4 F RT E25NE 1999082000972 19990820 00972 EU 1999 8 20 AALA991062 1 19990720 A 2750 EAFCD8518411 DATA UNIT FOKKER F28 F28MK0100 4990807 EU TE FLAPS DEFECTIVE A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 1422J FBE0034 11405 MSP - FLT 1446 - AFTER TAKEOFF MSP/DFW - FLAPS WOULD NOT RETRACT FROM EIGHT DEGREE ANGLE. AIRCRAFT RETURNED MSP AND LAN DED WITHOUT INCIDENT. REPLACED FLAP CONTROL DATA UNIT. ACCOMPLISHED ALL REQUIRED CHECKS. SYSTEM GROUND CHECKED, NORMA L OPERATION. (X) 2 L 7 2 4F RT 1999082000973 19990820 00973 EU 1999 8 20 AALA991067 1 19990721 A 2720 703852 MANIFOLD VICKERS FOKKER F28 F28MK0100 4990807 EU RUDDER DEFECTIVE A AALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SW 07 1451N 220A 11460 ORD - FLT 1734 - ON CLIMB-OUT FROM ORD/YUL, RECEIVED FAULT INDICATION FOR RUDDERS 1 AND 2, YAW DAMPERS 1 AND 2, AND STAB ILIZER TRIMS 1 AND 2. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED ACTIVE RUDDER MANIFOLD, REPLACED HIGH PRESSURE SWITCH ON STANDBY RUDDER MANIFOLD, AND REPLACED FLIGHT AUGMENTATION COMPUTER. SYSTEM GROUND CHECKED, NORM AL OPERATION. (X) 2 L 7 2 4F RT 1999082000974 19990820 00974 WP 1999 8 20 AALA991085 1 19990723 A 7930 8DJ130LWA1 INDICATOR AMETEK DOUG DC9 DC982 3022082 WP NR 1 ENG OIL DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 402A Y0057 49313 IAH - FLT 1303 - EN ROUTE DFW/MEX, LEFT ENGINE OIL QUANTITY SHOWED STEADY DECREASE POSSIBLY INDICATING HIGH OIL CONSUMPT ION ON NR 1 ENGINE. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IAH WITHOUT INCIDENT. REPLACED NR 1 ENGINE OIL INDICATO R. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000975 19990820 00975 WP 1999 8 20 AALA991092 1 19990725 A 2810 PANEL DOUG DC9 DC982 3022082 WP LT WING LOOSE A AALA K NONE K FLUID LOSS CR CRUISE 1 SW 07 432AA 49350 BNA - FLT 1195 - DURING FLIGHT FROM LBA/BNA, BOOST PUMP PANEL ON LEFT WING UPPER SURFACE WAS REPORTED TO HAVE A LIQUID S EEPING FROM IT. LEFT WING AFT BOOST FUEL BOOST PUMP PANEL WAS RESEALED AND SECURED. FILLED TANK WITH FUEL AND NO LEAKS WERE NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000976 19990820 00976 WP 1999 8 20 AALA991091 1 19990725 A 2120 SEAL DOUG DC9 DC983 3022083 WP TAIL COMPARTMENT LOOSE A AALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 562AA 49344 DFW - FLT 407 - AFTER TAKEOFF FROM DFW EN ROUTE TO PHX, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AT 9,000 FEE T. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. RESECURED SEAL BETWEEN AIR CONDITIONING PLENUM AND HEAT EXCHA NGER ON LEFT HAND OUTBOARD SIDE OF TAIL COMPARTMENT. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F RT A6WE 1999082000977 19990820 00977 WP 1999 8 20 AALA991077 1 19990722 A 2530 2510000405 OVEN DOUG DC9 DC982 3022082 WP GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 579AA 53156 BFL - FLT 1588 - AFTER TAKEOFF FROM BFL TO DFW, FLIGHT ATTENDANT'S REPORTED SMOKE IN CABIN. DISCONNECTED POWER TO GALLE Y AND DECLARED EMERGENCY. LANDED BFL WITHOUT INCIDENT. CLEANED OVEN. ALSO REPLACED COALESCER BAGS AND RIGHT HAND AIR CONDITIONING PACK AUGMENTATION VALVE. RAN ENGINES AND AIR CONDITINING PACKS FOR 20 MINUTES WITH NO SMOKE OR SMELL NOTED . SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000978 19990820 00978 WP 1999 8 20 AALA991052 1 19990717 A 3350 1003695 LIGHT GRIMES DOUG DC9 DC982 3022082 WP RT EMERG EXIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 583AA 53160 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD RIGHT OVER WING EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000979 19990820 00979 WP 1999 8 20 AALA991066 1 19990721 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7509 49803 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHTING STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000980 19990820 00980 WP 1999 8 20 AALA991065 1 19990721 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 279AA 49295 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING ALONG FIRST CLASS GALLEY INOPERATIVE. REPLACED F LAT WIRE LEAD TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000981 19990820 00981 NM 1999 8 20 AALA991058 1 19990719 A 3397 WIRE BOEING 767 767223 1385123 NM ROWS 8 AND 34 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312AA 22315 LHR - DURING ROUTINE MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT SEATS 8HJ AND 34H INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT SEATS 8HJ AND 34H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999082000982 19990820 00982 NM 1999 8 20 AALA991061 1 19990719 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 323AA 22324 SFO - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FLIGHT ATENDANT JUMP SEATS 3RC AND 3LC INOP ERATIVE. SECURED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999082000983 19990820 00983 NM 1999 8 20 AALA991068 1 19990719 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 323AA 22324 SFO - DURING OVERNIGHT, MAINTENANCE L2 DOORWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT L2 DO ORWAY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999082000984 19990820 00984 NM 1999 8 20 AALA991087 1 19990725 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 687AA 25695 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FIRST CLASS GALLEY INOPERATIVE. RE PLACED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FIRST CLASS GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 2 4F RT A2NM 1999082000985 19990820 00985 NM 1999 8 20 AALA991051 1 19990717 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT SEAT 2AB INOPERATIVE. SECURED EMERGENCY EXIT CONNECTO R AT SEATS 2AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999082000986 19990820 00986 NM 1999 8 20 AALA991050 1 19990716 A 3350 SOCKET BOEING 767 767323 1385205 NM ROW 33H DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388AA 27448 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 33H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999082000987 19990820 00987 1999 8 20 AALA991057 4 19990715 A 2330 AUV BOEING 757 757223 1384957 NM ROWS 16-19 SMOKED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 689AA 25731 ELP - FLT 1280 - EN ROUTE LAX/DFW - A BURNING SMELL WAS NOTED IN CABIN AROUND ROWS 16 - 19. VIDEO ENTERTAINMENT SYSTEM WAS TURNED OFF AND SMELL DISSIPATED. AIRCRAFT AIR INTERRUPTED AND DIVERTED TO ELP. AIRCRAFT LANDED AT ELP WITHOUT INCI DENT. COULD NOT DUPLICATE PROBLEM ON GROUND. AIRCRAFT WAS RELEASED FOR SERVICE AND HAS NOT HAD A REPEAT OCCURRENCE FOR 12 FLIGHT SEGMENTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999082000988 19990820 00988 WP 1999 8 20 AALA991083 1 19990719 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 DOUBLE DRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 587AA 53250 TUL - REF: F58 NR 3049490, TWO EACH FASTENER HOLES IN RECTANGLE FRAME UPPER CHORD ANGLE STA 1418, L2 RT ARE DOUBLE DRIL LED. INSTALLED DOUBLER AND FASTENERS PER AARD 53-10-00-19. TST: 23, 873.21 HOURS. CYCLES: 12,091. (X) 2 L 7 2 4F A6WE 1999082000990 19990820 00990 WP 1999 8 20 ARWA990801 1 19990806 A 7722 EGT INDICATOR DOUG DC8 DC862F 3021972 WP NR 4 ENGINE MALFUNCTIONED A ARWA A J E UNSCHED LANDING DUMP FUEL ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 791AL 46150 MIA - FLT 628 - AIR TURNBACK. DURING CLIMB, NR 4 ENGINE INDICATED 40 DEGREES LOWER THAN OTHER ENGINES, HOWEVER, WHEN LE VELED OFF AND AFTER SETTING CRUISE POWER, EGT CONTINUED DECREASING UNTIL IT INDICATED 100 DEGREES CELSIUS LOWER THAN OTH ER ENGINES. PERFORMED PRECAUTIONARY SHUT DOWN AT THAT TIME (1202 Z) WINDMILLING OIL PRESSURE WAS 43 PSI. DUMPED 23,000 POUNDS OF FUEL AND RETURNED TO MIAMI WITHOUT INCIDENT. REPAIRED COLD SOLDER JOINT AT OUTER END OF BALANCE RESISTOR SPO OL. ALSO, REPLACED EGT INDICATOR AS PRECAUTIONARY. PERFORMED ENGINE RUN-UP. ALL PARAMETERS CHECKED NORMAL IAW DC8 MM 77-20-0 AND 71-00-00. (X) 2 L 7 4 4F 4A25 1999082000991 19990820 00991 WP 1999 8 20 AALA991100 1 19990726 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING TO TAKEOFF 1 SW 07 7528A 49920 PDX - FLT 2091 - EN ROUTE DFW/PDX - NOSE GEAR RED LIGHT STAYED ON WITH GEAR HANDLE UP AFTER TAKEOFF. LIGHT EXTINGUISHED 30 MINUTES INTO FLIGHT. REPLACED NOSE GEAER UPLOCK SENSOR. PERFORMED GEAR RETRACTION CHECK. SYSTEM GROUND CHECKED, N ORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999082000992 19990820 00992 EU 1999 8 20 AALA991124 1 19990801 A 3040 EAWTC8803411 CONTROLLER FOKKER F28 F28MK0100 4990807 EU RT WINDSHIELD DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1410E FBE0273 11368 IAH - FLT 1450 - EN ROUTE AUS/ORD, SMOKE AND SPARKS WERE OBSERVED FROM THE FIRST OFFICER'S WINDOW HEAT TERMINAL BLOCK. W INDOW HEAT WAS DISCONNECTED. AIR INTERRUPTED AND LANDED IAH WITHOUT INCIDENT. REPLACED RIGHT HAND WINDSHIELD HEAT CONT ROLLER AND PRECAUTIONARY REPLACMENT OF RIGHT HAND WINDSHIELD. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999082000994 19990820 00994 EA 1999 8 20 CA990401003 2 19990322 A 7414 74830 GEAR PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA MAGNETO WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1700 L111361 L111361 (CAN) ON INSPECTION, ALUMINUM FLAKES WERE FOUND IN THE OIL FILTER ON THE NR 2 ENGINE. INVESTIGATION FOUND THE LEFT HAND MAGNETO LOOSE DUE TO BEARING SHAFT WEAR. THIS ALLOWED THE DRIVE GEAR TO TILT AND CONTACT THE ENGINE CASE CAUSING ALUMI NUM TO WEAR AWAY AND BE COLLECTED IN THE OIL FILTER. THE MAGNETO DRIVE GEAR WAS REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 1999082001003 19990820 01003 EU 1999 8 20 CA990513004 1 19990421 A 6220 350A31202304 FLANGE 350A31003305 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 916 M1303 4576 (CAN) DURING A SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE RADIUS OF FLANGE OF THE VIBRATION ABSORBER ASSEMBLY. MANU FACTURER WAS CONTACTED AND PART WAS CHANGED. 1 G 7 1 3U 3 U NC H9EU E19EU 1999082001005 19990820 01005 SW 1999 8 20 CA990513013 1 19990422 A 5302 206033004045A SKIN BELL 206 206L 1181522 SW TAIL BOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA ACKPO1047 (CAN) DURING COMPLIANCE WITH AD CF-98--42R1, FPI OF TAILBOOM SKIN REVEALED A 3MM CRACK AROUND THE UPPER EDGES OF THE HOR IZONTAL STABILIZER. 1 G 7 1 3U H2SW 1999082001006 19990820 01006 SW 1999 8 20 CA990630005 1 19990525 A 6220 204011121009 BLADE BOLT BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE MAIN ROTOR SCORED W K NONE O OTHER IN INSP/MAINT 1 CA A4595 CPPS61005 (CAN) ON A BLADE CHANGE 459.0 HRS PREVIOUS, ONE OF THE BLADE BOLTS GOT TIGHT AND STARTED TO TURN ABOUT 1/3 OF ITS TRAVEL OUT. AFTER BLADE BOLT WAS REMOVED, INSPECTION REVEALED THAT THE BOLT AND UPPER BUSHING WAS SCORED. BUSHING WAS DRESS ED OUT I.A.W. BELL MANUAL. NEW BLADE WAS INSTALLED, BUT ON A LATER SCHEDULED OTBD FITTING CHANGE, THE BUSHING WAS INSPE CTED AND WAS FOUND TO HAVE A CRACK WHICH WAS LATER CONFIRMED BY NDT. BUSHING WAS THEN REPLACED. 1 G 7 1 4U 4 U H4SW E22EA 1999082001032 19990820 01032 NM 1999 8 20 USAASB99160 1 19990702 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 263AU 22869 CLT - PILOT REPORTED THAT THE OVERHEAD EMERGENCY LIGHTS AND THE FLOOR LEVEL EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY D URING FLIGHT. MAINTENANCE FOUND A BARE WIRE AT THE CONNECTOR FOR THE BATTERY PACK AT SEAT ROW 5ABC AND A BROKEN WIRE AT THE WIRE PLUG AT SEAT ROW 13. REPAIRED WIRE AT CONNECTOR FOR BATTERY PACK AT SEAT ROW 5ABC AND INSTALLED NEW WIRE PLUG AT SEAT ROW 13. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999082001033 19990820 01033 1999 8 20 USAASB99163 4 19990705 A 2210 4030952906 YAW DAMPER BOEING 737 7373B7 1384580 NM E/E COMPT FAILED A USAA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 EA 19 385US 34533 22958 SDF - FLT 1548 - ON TAKEOFF ROLL FROM SDF, AT APPROX 125 KNOTS, AIRCRAFT EXPERIENCED A BRIEF UNCOMMANDED YAW TO THE RIGH T WITH NO FEEDBACK THROUGH RUDDER PEDALS. AFTER MOMENTARY YAW, REST OF TAKEOFF WAS NORMAL. FLIGHT CONTINUED ON TO PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE YAW DAMPER COUPLER. SYSTEM FUNCTIONAL CHECK PERFORMED A ND FOUND SATISFACTORY. ALSO, REMOVED AND REPLACED THE RUDDER POWER CONTROL UNIT (S/N 801ASS, P/N 65C37053-9C). OPERATI ONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999082001034 19990820 01034 CE 1999 8 20 GLBA99023 1 19990623 A 7712 1303890021 TRANSMITTER BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 01 96UX UE96 RIGHT ENGINE WOULD NOT MAKE TORQUE WORN O-RING ON BLEED VALVE. REPLACED O-RING AND REPLACED TORQUE TRANSMITTER, WOULD N OT CALIBRATE. (M) 2 L 7 2 4T RT A24CE 1999082001035 19990820 01035 SO 1999 8 20 GLBA99022 1 19990621 A 2751 3069001017 ANNUNCIATOR EMB 120 EMB120RT SO TE FLAPS INOPERATIVE A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 267UE 120071 FLAPS UP, AIRCRAFT HAD AN INDICATION OF 15 DEGREES FLAP ASYMMETRY. REPLACED THE FLAP ANNUNCIATOR ASSEMBLY. AIRCRAFT TE ST FLOWN OK. (M) 2 L 7 2 4T RT A31SO 1999082001036 19990820 01036 SO 1999 8 20 GLBA99012 1 19990621 A 2611 CONNECTOR EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR LOOSE A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 299UX 120299 LAV SMOKE DETECTOR ALARM SOUNDED AT GATE. INSTALLED PIN AT SMOKE DETECTOR ELECTRICAL CONNECTOR. (M) 2 L 7 2 4T RT A31SO 1999082001037 19990820 01037 CE 1999 8 20 GLBA99017 1 19990606 A 2150 7756355 ACM BEECH 1900 1900D 1154162 CE RT WING FAILED A GLBA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 01 169GL UE169 SMELL OF SMOKE IN COCKPIT WITH ACM RUNNING. REPLACED ACM. (M) 2 L 7 2 4T RT A24CE 1999082001038 19990820 01038 CE 1999 8 20 GLBA99014 1 19990622 A 2720 MS2770852 BOOST PANEL BEECH 1900 1900D 1154162 CE RUDDER SHORTED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 01 100UX 12906 UE100 AIR RETURN FOR SMOKE SMELL IN COCKPIT, FOUND YAW DAMP RUDDER BOOST PANEL CAUSING BURNING SMELL. DISCONNECTED PANEL AND DEFERRED. REPLACED RUDDER BOOST PANEL. (M) 2 L 7 2 4T RT A24CE 1999082001039 19990820 01039 NM 1999 8 20 A6WA9900008 1 19990306 A 2780 ARM DORNER DO32 DO328100 2996000 NM LT LE FLAP CRACKED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 328PH 3006 DURING A SCHEDULED FLAP CHANGE, MAINTENANCE NOTED THE NR 3 ATTACH ARM CRACKED. CRACK EXTENDS 90-95 PERCENT THROUGH ARM FROM LEADING EDGE TO TRAILING EDGE. REPLACED FLAP, LAST C-CHECK C/W AT SAT ON 12/13/97. TMS ACCUMULATED SINCE LAST C-C HECK ARE 1990 HRS AND 2387 CYCLES. (M) 2 H 7 2 4T RT A45NM 1999082001040 19990820 01040 1999 8 20 99ZZZM548 4 19990101 A 2565 D31050105 SLIDE BAG BAE146 BAE146100A 1500260 EU PAX DOOR OUT OF POSITION A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 WHILE INSPECTIONG GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD P ASSENGER DOOR SLIDE IAW MM. (M) 2 H 7 4 4F RT A49EU 1999082001041 19990820 01041 EU 1999 8 20 99ZZZM549 1 19990106 A 3260 SWITCH BAG BAE146 BAE146200A 1500266 EU NLG BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 NOSE GEAR SQUAT SWITCH SENSOR BROKEN OFF FROM ATTACH POINT. REMOVED AND REPLACED NOSE LANDING GEAR SQUAT SWITCH SENSOR HARNESS AND MOUNTING BRACKET IAW MM. (M) 2 H 7 4 4F RT A49EU 1999082001042 19990820 01042 1999 8 20 99ZZZM550 4 19990113 A 2565 SLIDE BAG BAE146 BAE146300A 1500267 EU RIGHT OUT OF POSITION A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 615AW E3141 RIGHT FORWARD EVAC SLIDE NEAR DEPLOYMENT. REMOVED AND REPLACED SLIDE. (M) 2 H 7 4 4F RT A49EU 1999082001043 19990820 01043 EU 1999 8 20 99ZZZM551 1 19990123 A 3233 ACTUATOR BAG BAE146 BAE146200A 1500266 EU NLG FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 UPON REMOVAL OF NOSE LANDING GEAR RETRACTION JACK FOUND PIN AT GEAR BAY SIDEWALL SHEARED. RETRACTION JACK REMOVED FOR E O E98/002/632. REMOVED AND REPLACED THE NLG RETRACTION JACK PIN AS REQ'D DURING REMOVING AND REPLACING OF JACK STREET. (M) 2 H 7 4 4F RT A49EU 1999082001044 19990820 01044 EU 1999 8 20 C2XA99IA346 1 19990701 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING 2A CHECK, FOUND THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR 42-320 MM 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999082001045 19990820 01045 EU 1999 8 20 C2XA99BT065 1 19990630 A 3350 SWITCH AEROSP ATR42 ATR42320 8680930 EU CABIN OUT OF ADJUST A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 14830 184 EWR - CREW REPORTED EMEREGNCY EXIT LIGHT PUSHBUTTON SWITCH AT FLIGHT ATTENDANT STATION INOPERATIVE. MAINTENANCE ADJUSTE D EMERGENCY EXIT LIGHT SWITCH AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999082001046 19990820 01046 GL 1999 8 20 C2XA99BT066 2 19990630 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 14933 145018 310004 BTV - FLT 4201 - CRWE REPORTED, 'LAV SMOKE INDICATION FOLLOWED BY BAG SMOKE IN INDICATION AFTER TAKEOFF, BOTH INDICATION S EXTINGUISHED ON GROUND AFTER AREA RETURN. CAUSED OVERWEIGHT LANDING'. PRESENTLY MAINTENANCE IS TROUBLESHOOTING CAUSE OF INDICATIONS. PERFORMED OVERWEIGHT LANDING INSPECTION AND NO DEFECTS WERE NOTED. FOUND NR 1 ENGINE FAN SEAL LEAKING MAINTENANCE REMOVED AND REPLACED THE ENGINE OPS CHECKED AND LEAKED CHECKED ENGINE OK. RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999082001047 19990820 01047 EU 1999 8 20 C2XA99BT067 1 19990705 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU ROW 10/15L DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15816 105 BTV - DURING A 3A INSPECTION MAINTENANCE, FOUND EMERGENCY AISLE PATH LIGHT, EVERY OTHER ONE INOPERATIVE AND DOOR AND RIG HT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK AT STATIONS 10WL AND 15 WL. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999082001048 19990820 01048 SO 1999 8 20 C2XA99IA352 1 19990630 A 5320 STRAP EMB 145 EMB145 SO FRAME 15-19 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14939 145030 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP BETWEEN FRAMES 15 AND 19 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED THE CORROSION AND INSTALLED REPAIR DOUBLERS IAW EMBRAER REPAIR DRAWING SST1287/99, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999082001049 19990820 01049 SO 1999 8 20 C2XA99IA351 1 19990630 A 5530 14531597602 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14939 145030 IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER FORWARD RIGHT DRAG ANGLE CRACKED. MAINTENANCE REMOVED AND RE PLACED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999082001050 19990820 01050 SO 1999 8 20 C2XA99IA350 1 19990630 A 5530 14531597601 ANGLE EMB 145 EMB145 SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14939 145030 IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER FORWARD LEFT DRAG ANGLE CRACKED. MAINTENANCE REMOVED AND REP LACED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999082001051 19990820 01051 SO 1999 8 20 C2XA99IA349 1 19990630 A 5347 14518644001 SEAT TRACK EMB 145 EMB145 SO COCKPIT WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14939 145030 IAH - DURING C-CHECK INSPECTION, THE FIRST OFFICERS SIDE INBOARD SEAT TRACK WAS FOUND TO BE WORN AROUND THE LOCKING HOLE S. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB145 MM 53-01-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999082001052 19990820 01052 SO 1999 8 20 C2XA99IA348 1 19990630 A 5320 14522459001 BEAM EMB 145 EMB145 SO FRAME 29 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14939 145030 IAH - DURING C-CHECK INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED UNDER THE COMPOSITE FLOOR PANEL SUPPORT AT FRAME 29. MAINTENANCE REMOVED THE DAMAGED SECTION AND INSTALLED A REPAIR DOUBLER IAW EMB145 REPAIR DRAWING SST-1274/99 AND EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999082001053 19990820 01053 SO 1999 8 20 C2XA99IA347 1 19990630 A 3350 3025101 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14939 145030 IAH - DURING C-CHECK INSPECTIN, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999082001054 19990820 01054 SO 1999 8 20 C2XA99CL052 1 19990705 A 2150 9799901 TEMP CONTL VLV EMB 120 EMB120RT SO LT/RT FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 22727 15608 1423 120177 CLE - FLT 4370 - THE CREW REPORTED SMOKE IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT TEMP CONTROL VALVE AND THE LEFT TCV AND THE COMPRESSOR INLET VALV E IAW EMB-120 MM 21-60-01 AND 21-60-10. THE AIRCRAFT PASSED A TEST FLIGHT AND WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001055 19990820 01055 SO 1999 8 20 99ZZZM552 1 19990705 A 3610 97962641 VALVE EMB 120 EMB120RT SO ENGINE DIRTY A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 22727 19623 1064 120177 CLE - FLT 4370 - THE CREW REPORTED SMOKE IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT TEMP CONTROL VALVE AND THE LEFT TCV AND THE COMPRESSOR INLET VALV E IAW EMB-120 MM 21-60-01 AND 21-60-10. THE AIRCRAFT PASSED A TEST FLIGHT AND WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001056 19990820 01056 SO 1999 8 20 C2XA99CL051 1 19990623 A 3240 21585 BRAKE EMB 120 EMB120RT SO MLG CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26714 16715 667 120118 CLE - FLT 3603 - DURING A NR 1 MWA CHANGE, THE NR 1 BRAKE ASSEMBLY FELL APART. MAINTENANCE REMOVED AND REPLACED THE NR 1 BRAKE ASSEMLBY IAW EMB-120 MM 32-41-04. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001057 19990820 01057 SO 1999 8 20 C2XA99CL050 1 19990627 A 2751 WARNING EMB 120 EMB120RT SO TE FLAPS ACTIVATED A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 09 16731 120190 CLE - FLT 3069 - DURING TAKEOFF ROLL, THE CREW ABORTED TAKEOFF DUE TO A ADVANCE STALL WARNING INDICATION AND A FLAP CONT ROL FAULT. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF T HE FLAP SYSTEM IAW EMB-120 MM 27-50-00, WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001058 19990820 01058 SO 1999 8 20 C2XA99CL049 1 19990625 A 2120 AIR DIST EMB 120 EMB120RT SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 26714 120118 CLE - FLT 3155 - DURING FLIGHT WITH THE PACKS IN LOW, THE CREW REPORTED THE SMELL OF SMOKE THROUGHOUT THE CABIN. THE AI RCRAFT CONTINUED ON TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE RAN BOTH ENGINES FOR SEVERAL MINUTES WITH NO DEF ECTS OR SMELLS NOTED ENGINE RUNS WERE DONE IAW EMB-120 MM 71-00-00. AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001059 19990820 01059 1999 8 20 C2XA99CL048 4 19990623 A 3442 CONNECTOR BEECH 1900 1900D 1154162 CE RADAR CONTAMINATED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 09 87550 UE205 CLE - FLT 3169 - THE CREW REPORTED THE RADAR WAS PAINTING RED AT FULL TILT UP, THE AIRCRAFT DID A AIR RETURN TO CLEVELAN D WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED MOISTURE FROM THE R/T CONNECTOR AND PERFORMED RADAR GROUND CHECKS IAW B EECHCRAFT MM 34-40-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999082001060 19990820 01060 SO 1999 8 20 99ZZZM553 1 19990526 A 2434 GENERATOR EMB 145 EMB145 SO NR 2 FAILED A C2XA A UNSCHED LANDING J G H WARNING INDICATION MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 09 16927 145006 CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AI R RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M) 2 L 7 2 4F RT T00011AT 1999082001061 19990820 01061 SO 1999 8 20 99ZZZM554 1 19990526 A 2434 GENERATOR EMB 145 EMB145 SO NR 3 FAILED A C2XA A UNSCHED LANDING J G H WARNING INDICATION MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 09 16927 145006 CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AI R RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M) 2 L 7 2 4F RT T00011AT 1999082001062 19990820 01062 SO 1999 8 20 99ZZZM555 1 19990526 A 2434 GENERATOR EMB 145 EMB145 SO NR 4 FAILED A C2XA A UNSCHED LANDING J G H WARNING INDICATION MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 09 16927 145006 CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AI R RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M) 2 L 7 2 4F RT T00011AT 1999082001063 19990820 01063 SO 1999 8 20 99ZZZM556 1 19990526 A 2434 GENERATOR EMB 145 EMB145 SO NR 5 FAILED A C2XA A UNSCHED LANDING J G H WARNING INDICATION MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 09 16927 145006 CAE - AFTER TAKEOFF, CREW REPORTED FIVE GENS FAILED IN FLIGHT. APU GEN FAILED, THEN GEN 2, GEN 4, GEN 3, AND GEN 1. AI R RETURNED TO CAE LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOOTING. (M) 2 L 7 2 4F RT T00011AT 1999082001064 19990820 01064 EU 1999 8 20 C2XA99BT068 1 19990712 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 BTV - DURING 4A INSPECTION, FOUND AIRSTAIR AND RIGHT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BULBS, OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999082001065 19990820 01065 EU 1999 8 20 C2XA99BT071 1 19990714 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU ROW 3WL INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14830 184 BTV - DURING LINE/WEEKLY CHECK, FOUND FORWARD FLOOR TRACK LIGHTS, AND UPPER EMERGENCY EXIT LIGHT INOPERATIVE WHEN EMERGE NCY LIGHTS ARE IN ARM AND UNDER BATTERY POWER. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AT 3WL AND OPS CHECKED SYS TEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999082001066 19990820 01066 SO 1999 8 20 C2XA99BT070 1 19990714 A 3350 LIGHT EMB 145 EMB145 SO ROW 16/17 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13958 145085 BTV - MAINTENANCE FOUND EMERGENCY AISLE PATH LIGHTING STRIP INCORRECT AT 16 AND 17A. AIRCRAFT MAINTENANCE FERRIED TO CL E DUE TO LACK OF PARTS AVAILABILITY. (M) 2 L 7 2 4F RT T00011AT 1999082001067 19990820 01067 SO 1999 8 20 C2XA99BT069 1 19990714 A 3350 LIGHT EMB 145 EMB145 SO EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13958 145085 BTV - FLT 4218 - MAINTENANCE FOUND LEFT WING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED BULB AND CLEANED CONTACTS. REIN STALLED BULB. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1999082001068 19990820 01068 EU 1999 8 20 C2XA99IA356 1 19990706 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING MAINTENANCE INSPECTION, THE FORWARD BOTTOM EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED POWER SUPPLY IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 H 7 2 4T RT A53EU 1999082001069 19990820 01069 SO 1999 8 20 C2XA99IA355 1 19990707 A 2121 EVAC2322C FAN EMB 120 EMB120RT SO CABIN FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 09 27716 120128 IAH - FLT 3314 - THE CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE RIGHT GROUND COOLING FAN IA W EMB120 MM 21-51-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001070 19990820 01070 SO 1999 8 20 C2XA99IA354 1 19990712 A 2121 12042000001 FAN MUFFLER EMB 120 EMB120RT SO CABIN DAMAGED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 15730 120187 IAH - FLT 3561 - THE CREW REPORTED SMOKE IN THE CABIN AFTER NR 2 ENGINE START. MAINTENANCE INSPECTED THE AIRCRAFT AND P LACED THE GASPER FAN ON MEL 21-24-1C CONTROL NR 183333, AND THE AIRCRAFT WAS RETURNED TO SERVICE AND THE AIRCRAFT THEN A BORTED ITS TAKEOFF WITH THE SAME DISCREPANCY. MAINTENANCE REMOVED AND REPLACED THE RIGHT RICIRCULATION FAN MUFFLER IAW EMB120MM 21-25-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001071 19990820 01071 SO 1999 8 20 C2XA99CL053 1 19990705 A 3230 ACTUATOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 16723 120169 ROC-CLE - FLT 3117 - THE CREW REPORTED A RIGHT MLG GEAR DISAGREEMENT INDICATION LIGH TDURING FLIGHT, THE CREW CYCLED THE GEAR AND THE LIGHT EXTINGUISHED, THE AIRCRAFT CONTINUED ON TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MLG ACTUATOR ROD END AND PEFORMED OPERATIONAL CHECKS IAW EMB-120 MM 32-32-10. THE AIRCRAFT WAS RELEASED TO S ERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001072 19990820 01072 SO 1999 8 20 C2XA99CL054 1 19990707 A 3260 INDICATION EMB 120 EMB120ER 3260203 SO RT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 16718 120136 CMH - FLT 3040 - THE CREW REPORTED THE RT MLG RED 'B' INDICATION REMAINED ON AFTER GEAR RETRACTION. THE AIRCRAFT RETURN ED TO CMH WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED SEVERAL LANDING GEAR SWINGS WITH NO DEFECTS NOTED THE WORK WA S DONE IAW EMB-120 MM 32-30-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082001073 19990820 01073 WP 1999 8 20 USAA990692 1 19990707 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURING Q2 CHECK, FOUND CORROSION SEVERAL INCHES IN 3 DIFFERENT DIRECTIONS AT STATION 996 LONG 18 AREA AT BULKHEAD/ FLOORBEAM AND BELL FRAME TIE IN. CORROSION LEVEL 1/2, CORROSION TASK NR C57-53300. REMOVED AND REPLACED T-CAP SECTION. (M) 2 L 7 2 4F A6WE 1999082001074 19990820 01074 WP 1999 8 20 USAA990693 1 19990707 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 617 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURIGN Q2, C-1 CHECK, FOUND .75 INCH CRACK AT LONGERON 3L AT STATION 617. REPLACED LONGERON SECTION FROM FACTORY SPLICE TO PREVIOUS REPAIR SPLICE PER SRM 53-02. (M) 2 L 7 2 4F A6WE 1999082001075 19990820 01075 WP 1999 8 20 USAA990694 1 19990707 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 207-210 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURING Q2, C-1 CHECK, FOUND 6 INCH BY 3 INCH CORRODED AREA AT DOUBLER BETWEEN 28R AND 29R AT STATION 207-210. COR ROSION LEVEL 1, CORROSION TASK NR C45-53300. REMOVED, MFG NEW, AND INSTALLED. (M) 2 L 7 2 4F A6WE 1999082001076 19990820 01076 WP 1999 8 20 USAA990695 1 19990707 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURIGN Q2, C-1 CHECK, FOUND 2 INCH BY 19 INCH OF CORROSION AT FLOOR SUPPORT C/L OF A/C AT STATION 218-237. CORROS ION LEVEL 1, CORROSION TASK NR C51-53300. REMOVED SUPPORT, MFG NEW, AND INSTALLED. (M) 2 L 7 2 4F A6WE 1999082001077 19990820 01077 WP 1999 8 20 USAA990696 1 19990707 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURING Q2, C-1 CHECK, FOUND 1 INCH BY 10 INCH OF CORROSION AT INTERCOSTAL NEXT TO H20 DRAIN IN E/E. CORROSION LEV EL 1. REMOVED, MFG NEW, AND INSTALLED. (M) 2 L 7 2 4F A6WE 1999082001078 19990820 01078 WP 1999 8 20 USAA990697 1 19990707 A 5320 BEAM DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURING Q2, C-1 CHECK, FOUND 1 INCH BY 19 INCH BEAM CORRODED AT C/L OF A/C STATION 3218237. CORROSION LEVEL 1. RE MOVED BEAM, MFG NEW, AND INSTALLED. (M) 2 L 7 2 4F A6WE 1999082001079 19990820 01079 WP 1999 8 20 USAA990698 1 19990707 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 980 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURING Q2, C-1 CHECK, FOUND LEVEL 1 AND LEVEL 2 CORROSION AT LEFT FLOORBEAM AT STATION 980 AROUND MISSING NUTPLATE . CORROSION LEVEL 1. INSTALLED REPAIR PER PER US AIRWAYS TYPICAL REPAIR 53-10-19. (M) 2 L 7 2 4F A6WE 1999082001080 19990820 01080 WP 1999 8 20 USAA990699 1 19990707 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 756-996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURING Q2, C-1 CHECK, FOUND 1 INCH BY .75 INCH BY 25 INCH, AREA CORRODED AT FLOOR SUPPORT LONG 28L STATION 756 TO 996. CORROSION LEVEL 1, CORROSION TASK NR C57-53300. REMOVED CORROSION, TREATED, PRIMED AND SPLICED IN NEW SECTION OF RAIL. (M) 2 L 7 2 4F A6WE 1999082001081 19990820 01081 WP 1999 8 20 USAA990700 1 19990707 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 604 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURING Q2, C-1 CHECK, FOUND 1 INCH CRACK AT ATTACH ANGLE AT STATION 604 LONG 22B. TRIMMED ANGLE, INSTALLED REPAIR STRAP PER EA 52302. (M) 2 L 7 2 4F A6WE 1999082001082 19990820 01082 WP 1999 8 20 USAA990701 1 19990707 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 420 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURIGN Q2, C-1 CHECK, FOUND 1 INCH BY 1.5 INCH CORRODED AREA AT SEAT TRACK AT STATION 420 RT OUTBOARD SEAT TRACK. CORROSION LEVEL 1, CORROSION TASK NR C58-53300. (M) 2 L 7 2 4F A6WE 1999082001083 19990820 01083 NM 1999 8 20 USAA990702 1 19990726 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 21244 FORWARD CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1999082001084 19990820 01084 WP 1999 8 20 USAA990703 1 19990707 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 64164 47593 PIT - DURIGN Q2, C-1 CHECK, FOUND 3 INCH BY 3 INCH CORRODED AREA AT FLOORBEAM AND FITTING AT STATION 996 LONG 18R. CORR OSION LEVEL 1, CORROSION TASK NR C57-53300. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLERS. REPLACED FITTING PER EA 52267. (M) 2 L 7 2 4F A6WE 1999082001085 19990820 01085 WP 1999 8 20 USAAD99091 1 19990707 A 3610 18J14350 CLAMP DOUG DC9 DC981 3022081 WP LT ENGINE PYLON FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 812US 48092 PIT-MHT - FLT 2160 - AFTER TAKEOFF, THE LEFT ENGINE FIRE HANDLE AND THE 2 LEFT DETECTOR LOOP LIGHTS ILLUMINATED. THE FI RE BELL ALSO RANG. POWER WAS REDUCED AND THE LIGHTS WENT OUT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED A FAILED CLAMP ON THE 13TH STAGE DUCT THROUGH THE ENGINE PYLON. (M) 2 L 7 2 4F A6WE 1999082001086 19990820 01086 WP 1999 8 20 USAAD99093 1 19990709 A 2530 COFFEEMAKER DOUG DC9 DC931 3022065 WP GALLEY DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 971VJ 47051 PIT-IND - FLT 705 - DURING CLIMB, FUMES AND SMOKE WERE DETECTED AROUND THE COFFEEMAKER AND IN THE COCKPIT CLOSET. THE G ALLEY POWER WAS TURNED OFF AND THE CIRCUIT BREAKERS PULLED. THE SMOKE STOPPED WHEN THE GALLEY POWER WAS TURNED OFF. TH E AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED DEBRIS FROM THE INBOARD COFFEEMAKER. (M) 2 L 7 2 4F A6WE 1999082001087 19990820 01087 WP 1999 8 20 USAAD99095 1 19990713 A 2170 V1211 COALESCER BAG DOUG DC9 DC981 3022081 WP CABIN CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 810US 48042 PHL-PIT - FLT 656 - AFTER TAKEOFF, BOTH AFT LAVATORY SMOKE DETECTORS ACTIVATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH WATER SEPARATOR COALESCER BAGS. (M) 2 L 7 2 4F A6WE 1999082001088 19990820 01088 NE 1999 8 20 USAAD99090 2 19990705 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LEFT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 967VJ 47375 687889 IND-PHL - FLT 2056 - DURING CRUISE, THE LEFT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. THE THROTTLE WAS RETARDED BUT THE LIGHT REMAINED ON. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENA NCE REPLACED THE LEFT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999082001089 19990820 01089 NM 1999 8 20 USAASB99158 1 19990629 A 7722 EGT LIGHT BOEING 737 737401 1384701 NM NR 1 ENGINE ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 407US 23877 CLT - FLT 932 - UPON CLIMB-OUT FROM CLT, AP APPROX 18,000 FT, THE NR 1 ENGINE EGT LIGHT ILLUMINATED AS THE NR 1 ENGINE E XCEEDED LIMITS. CAPTAIN PULLED THE THROTTLE BACK OT IDLE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT. NO ENGINE SHUTDOWN OCCURRED BUT AN EMERGENCY WAS DECLARED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERAT IONALLY CHECKED SYSTEM WITH BARFIELD TEST UNIT. SYSTEM IS WITHIN LIMITS PER MM 77-21-00. RESEATED ELECTRICAL CONNECTOR S. NO EXCEEDANCES NOTED PER ACARS READINGS. ENGINE GROUND RUN ACCOMPLISHED. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1999082001090 19990820 01090 WP 1999 8 20 USAA990686 1 19990706 A 5312 BULKHEAD WEB DOUG DC9 DC931 3022065 WP FWD PRESS BLKHD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49217 48114 PIT - DURNG PILOT REPORT, FOUND 1.5 INCH HORIZONTAL CRACK AT FORWARD PRESSURE BULKHEAD WEB LOWER LEFT BEHIND NLG TRUNNIO N 2 INCHES ABOVE BULKHEAD SKIN CLIP. REMOVED DAMAGE. INSTALLED DOUBLER AND FILLER PER EA 52402. (M) 2 L 7 2 4F A6WE 1999082001091 19990820 01091 EU 1999 8 20 RAIA990703 1 19990702 A 2844 41SG107100G14 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU LT FUEL SYSTEM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424AM 5003 865 FLT 7098 - STL - LEFT FUEL PRESSURE GAUGE INOPERATIVE. MAINTENANCE REPLACED TRANSMITTER. (M) 2 L 7 2 4T RT A56EU 1999082001092 19990820 01092 WP 1999 8 20 RAIA990647 2 19990630 A 7310 8953804 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 433AM 885 66146 FLT 7369 - PAH - LEFT ENGINE EGT FLUX 30 PERCENT. MAINTENANCE REPLACED LEFT ENGINE FUEL BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999082001093 19990820 01093 1999 8 20 RAIA990704 4 19990702 A 3425 7003110901 EFIS TUBE JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 41039 FLT 7667 - JFK - CAPTAINS EHSI WENT BLANK. MAINTENANCE REPLACED CAPTAINS EFIS TUBE FOR EHSI. (M) 2 L 7 2 4T RT A41NM 1999082001094 19990820 01094 1999 8 20 RAIA990705 4 19990703 A 3454 6226521016 CONTROL HEAD BAG JETSTM JETSTM3201 1500217 EU NR 2 NAV FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 425AM 8624 870 FLT 7316 - STL - NR 2 NAV DISPLAY STARTED BLINKING. MAINTENANCE REPLACED NR 2 NAV CONTROL HEAD. (M) 2 L 7 2 4T RT A56EU 1999082001095 19990820 01095 EU 1999 8 20 RAIA990706 1 19990703 A 2841 7485222 QUANTITY GAUGE AEROSP ATR42 ATR42300 8680920 EU LT FUEL SYSTEM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424TE 124 FLT 7170 - STL - LEFT FUEL QUANTITY GAUGE WENT TO ZERO. MAINTENANCE REPLACED LEFT FUEL QUANTITY INDICATOR. (M) 2 H 7 2 4T RT A53EU 1999082001096 19990820 01096 1999 8 20 RAIA990707 4 19990703 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 565HK 7396 41082 FLT 7733 - JFK - AHRS NR 2 ATT/ROLL/PITCH COMPARATOR ERROR DISPLAYED. MAINTENANCE REPLACED NR 2 AHRS. (M) 2 L 7 2 4T RT A41NM 1999082001097 19990820 01097 1999 8 20 RAIA990708 4 19990703 A 3442 7008470822 RADAR JETAIR JETSTM JETSTM4101 1500501 EU FWD FUSELAGE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 565HK 6470 41082 FLT 7733 - JFK - RADAR INOPERATIVE. MAINTENANCE REPLACED RADAR R/T. (M) 2 L 7 2 4T RT A41NM 1999082001098 19990820 01098 EU 1999 8 20 RAIA990710 1 19990704 A 2150 32051204 COOLING TURBINE AEROSP ATR72 ATR72202 8680940 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 723TE 283 FLT 7120 - STL - LEFT PAC BLOWS HOT AIR AUTO AND MANUAL MODE. MAINTENANCE REPLACED LEFT COOLING TURBINE. (M) 2 H 7 2 4T RT A53EU 1999082001099 19990820 01099 EU 1999 8 20 RAIA990711 1 19990705 A 2120 AIR DIST AEROSP ATR72 ATR72202 8680940 EU CABIN SMOKE A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 722TE 220 FLT 7534 - STL - SMOKE IN CABIN. MAINTENANCE PERFORMED GROUND RUN OF AIRCRAFT AND ALL SYSTEMS. NO SMOKE NOTED. (M) 2 H 7 2 4T RT A53EU 1999082001100 19990820 01100 NE 1999 8 20 RAIA990713 2 19990707 A 7321 8058131005 EEC AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 721TE 5066 217 124512 FLT 7391 - XNA - RIGHT ENGINE ITT HIGH. MAINTENANCE REPLACED EEC ON RIGHT ENGINE. (M) 2 H 7 2 4T 4 T RT A53EU E2ONE 1999082001101 19990820 01101 1999 8 20 RAIA990712 3 19990707 A 6140 8659567 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 971JX 16756 971 FLT 4722 - LAX - LEFT ENGINE BETA LIGHT INOPERATIVE. MAINTENANCE REPLACED BETA SWITCH ON LEFT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999082001102 19990820 01102 NM 1999 8 20 TSAA9933290 1 19990707 A 3350 873100151 LIGHT BOEING 737 7372S2C 138448G NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 1 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999082001103 19990820 01103 NM 1999 8 20 TSAA9933291 1 19990707 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 1 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999082001104 19990820 01104 NM 1999 8 20 TSAA9953287 1 19990605 A 5330 SKIN BOEING 737 7372S5C 1384499 NM BS 749 CRACK A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FUSELAGE SKIN CRACK AT BS 749 AT STRINGER 17L. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIR ED PER SRM 53-30-3 PAGE 25. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999082001105 19990820 01105 NM 1999 8 20 TSAA9953288 1 19990605 A 5330 SKIN BOEING 737 7372S5C 1384499 NM BS 749 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FUSELAGE SKIN CRACK AT BS 749 AT STRINGER 15L. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIR ED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999082001106 19990820 01106 NM 1999 8 20 TSAA9953289 1 19990605 A 5330 SKIN BOEING 737 7372S5C 1384499 NM BS 536 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FUSELAGE SKIN CRACK AT BS 536 AT STRINGE R15R. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIR ED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999082001107 19990820 01107 EA 1999 8 20 99ZZZM557 1 19990712 A 5520 C6TEM101529 HINGE FITTING DHAV DHC6 DHC6300 2802606 EA LT ELEVATOR WORN A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 710PV 751 HNL - DURING GROUND MAINTENANCE INSPECTION, FOUND LEFT OUTBOARD ELEVATOR HINGE WORN. REPLACED OUTBOARD HINGE. (M) 1 H 7 2 3T RT A9EA 1999082001108 19990820 01108 WP 1999 8 20 HALA9900151 1 19990706 A 3040 204012 TEMP CONTROLLER DOUG DC9 DC951 3022051 WP RT WINDSHIELD FAILED A HALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 674MC 11523 47735 HNL - FLT 549 - BURNING SMELL IN CABIN. STRONGEST ROW 15 TO ROW 7, NO SMOKE. DEACTIVATED UPPER SIDE WALL LIGHTS FOR FE RRY TO HNL FROM LIH. ON ARRIVAL AT HNL, FOUND RIGHT WINDSHIELD TEMP CONTROLLER NO GOOD. BURNED, REMOVED AND REPLACED R IGHT WINDSHIELD TEMP CONTROLLER. OPS AND TEST CHECK OK. REACTIVATED UPPER SIDEWALL LIGHTING. (M) 2 L 7 2 4F RT A6WE 1999082001109 19990820 01109 NM 1999 8 20 GAIA9996 1 19990621 A 5330 SKIN BOEING 727 727251 138408H NM BS 1090-1140 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AIA/OSC MAINTENANCE FACILITY. FOUND SKIN DAMAGED BELOW C-3 DOOR FROM BS 1 090 TO 1140. INSTALLED PERMANENT REPAIR AT NR 3 LOWER CARGO DOOR CUTOUT AREA IAW EDR NR B2-06458 AND DER APPROVED 8110- 3. (M) 2 L 7 3 4F A3WE 1999082001110 19990820 01110 NM 1999 8 20 GAIA9995 1 19990621 A 5311 FRAME BOEING 727 727251 138408H NM BS 600 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AIA/OSC MAINTENANCE FACILITY. FOUND FRAME CRACKED BS 600 AT FASTENER HOLE BETWEEN STRINGER 25L AND 26L. INSTALLED PERMANENT REPAIR AT FRAME BS 600 BETWEEN STRINGER 25L AND 26L IAW EDR NR B2-06 454 AND DER APPROVED 8110-3. (M) 2 L 7 3 4F A3WE 1999082001111 19990820 01111 NM 1999 8 20 GAIA9994 1 19990621 A 5330 SKIN BOEING 727 727251 138408H NM BS 568/648 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AIA/OSC MAINTENANCE FACILITY. FOUND DENT ON MAIN CARGO DOOR DOUBLER AT ST ATION 568 AND 648. INSTALLED PERMANENT REPAIR AT BS 568 AND 648 IAW EDR NR B2-06438 AND DER APPROVED 8110-3. (M) 2 L 7 3 4F A3WE 1999082001112 19990820 01112 NM 1999 8 20 GAIA9993 1 19990621 A 5753 SKIN BOEING 727 727251 138408H NM NR 4 TE MIDFLAP DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 279US 21158 FOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AIA/OSC MAINTENANCE FACILITY. FOUND DENT ON RIGHT WING NR 4 MIDFLAP LEADI NG EDGE. INSTALLED PERMANENT REPAIR AT RIGHT WING NR 4 MID FLAP LEADING EDGE IAW EDR NR B2-06437 AND DER APPROVED 8110- 3. (M) 2 L 7 3 4F A3WE 1999082001113 19990820 01113 NM 1999 8 20 99ZZZM558 1 19990628 A 7930 RELIEF VALVE BOEING 727 727227 1384078 NM NR 1 ENGINE INOPERATIVE A AMTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 772AT 22003 CLIMBING THROUGH FLIGHT LEVEL 18, THE NR 1 ENGINE OIL PRESSURE DROPPED TO 35 PSI, OIL TEMPERATURE INCREASED TO 120 DEGRE ES. THROTTLE RETARDED, OIL PRESSURE REMAINED AT 35 PSI, OIL PRESSURE BEGAN TO RECOVER ON APPROACH TO INDIANAPOLIS AIRPO RT. REMOVED AND REPLACED THE NR 1 ENGINE OIL PRESSURE RELIEF VALVE IAW PW MM 72-61-0, OPERATIONAL CHECKED NORMAL IAW PW MM 72-00. NO LEAKS NOTED AT THIS TIME, OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 1999082001114 19990820 01114 NM 1999 8 20 99ZZZM559 1 19990712 A 3610 65234941 DUCT BOEING 727 727227 1384078 NM AFT AIRSTAIRS CRACKED A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 772AT 22003 DURING CLIMB-OUT, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON, THEN STANDBY HYDRAULIC SYTEM' ON' LIGHT AND 'OVERHEAT' LIGH T CAME ON. RETURNED TO INDIANAPOLIS. FOUND THE NR 1 ENGINE WING ANTI-ICE DUCT RUPTURED ON BOTTOM SIDE JUST OUTBOARD OF FLANGE. REPLACED THE DUCT AND NO LEAKS NOTED AT THIS TIME, OK FOR SERVICE. A NON-DESTRUCTIVE TEST WAS PERFORMED ON TH E FUSELAGE SECTION AT THE AFT AIRSTAIRS LEFT SIDE AND NO DEFECTS WERE NOTED. (M) 2 L 7 3 4F A3WE 1999082001115 19990820 01115 WP 1999 8 20 ASAA9980136 1 19990613 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 969AS 53063 PHX - PRIOR TO DEPARTURE OF FLT 721 - CREW REPORTED THE EMERGENCY FLOOR TRACK RED LIGHTS IN THE FORWARD CABIN WERE INOPE RATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001116 19990820 01116 WP 1999 8 20 ASAA9980133 1 19990605 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001117 19990820 01117 WP 1999 8 20 ASAA9980131 1 19990604 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS BETWEEN THE AFT LAVATORIES WERE FOUND INOPERATIVE. REPLAC ED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001118 19990820 01118 WP 1999 8 20 ASAA9980129 1 19990530 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001119 19990820 01119 WP 1999 8 20 ASAA9980128 1 19990530 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 948AS 53021 PDX - PRIOR TO DEPARTURE OF FLIGHT 102, CREW REPORTED THE FORWARD 2 EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. SECU RED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001120 19990820 01120 WP 1999 8 20 ASAA9980127 1 19990529 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP ROW 21 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 21 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001121 19990820 01121 WP 1999 8 20 ASAA9980125 1 19990525 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP ROW 13-18 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 18 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001122 19990820 01122 WP 1999 8 20 ASAA9980123 1 19990524 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 7-9 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 7 TO 9 WERE FOUND INOPERATIVE. REPLACED WIRI NG IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999082001123 19990820 01123 WP 1999 8 20 ASAA9980121 1 19990523 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMER EXIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001124 19990820 01124 WP 1999 8 20 ASAA9980120 1 19990523 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP ROW 23-27 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 23 TO 27 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999082001176 19990820 01176 NE 1999 8 20 VTZA990233 2 19990720 A 7510 39702022 ANTI-ICE VALVE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 333UE 41101 IAD/GSO - FLT 7403 - DURING CRUISE, AIRCRAFT DECLARED EMERGENCY AND MADE AN UNSCHEDULED LANDING AT IAD AFTER RT ENGINE C APTION ILLUMINATED WHEN ANTI-ICE SWITCHED ON. MAINTENANCE REMOVED AND REPLACED RT ENGINE ANTI-ICE VALVE. OPS CHECK GOO D WITH ENGINE GROUND RUNS. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082001177 19990820 01177 EU 1999 8 20 VTZA990232 1 19990719 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 302UE 41013 SCE/IAD - FLT 7605 - DURING POST-FLIGHT, CREW FOUND FLOOR EMERGENCY TRACK LIGHTING INOPERABLE. AIRCRAFT STAYED AT GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RE-SECURED CONNECTOR TO TRACK LIGHTING, OPS CHECK OK. AIRCRAFT REL EASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001178 19990820 01178 EU 1999 8 20 VTZA990231 1 19990719 A 3350 BULB JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY EXIT FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 306UE 41020 TYS/IAD - FLT 7342 - DURING POST-FLIGHT, CREW FOUND AFT EMERGENCY EXIT LIGHT INOPERABLE. AIRCRAFT STAYED AT GATE WITH N O FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RELAMPED EMERGENCY EXIT LIGHT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001179 19990820 01179 EU 1999 8 20 VTZA990237 1 19990725 A 7600 31055863 NTS TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT/RT IEC FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 320UE 41043 IAD/ORF - FLT 7481 - DURING TAKEOFF AIRCRAFT ABORTED TAKEOFF DUE TO BOTH IEC FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 NTS TRANSDUCER, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001180 19990820 01180 NE 1999 8 20 VTZA990238 2 19990725 A 7320 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 309UE 41022 IAD/DHS - FLT 7347 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED RT ENGINE MAX FUEL FLOW. OPS CHECK OK. AIRCRAFT REL EASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082001181 19990820 01181 EU 1999 8 20 VTZA990239 1 19990706 A 3350 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERABLE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 303UE 41015 IAD/TVS - FLT 7341 - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO EMERGENCY FLOOR TRACK LIGHTING INOPERABLE AND HAD NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND TRACK LIGHTING GOOD, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FO R RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001182 19990820 01182 EU 1999 8 20 VTZA990240 1 19990726 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 315UE 41033 IAD/RIC - FLT 7245 - DURING TAXI, CREW FOUND THAT EMERGENCY FLOOR TRACK LIGHTS INOPERABLE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RE-SECURED CONNECTION ON LIGHTS, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001183 19990820 01183 EU 1999 8 20 VTZA990241 1 19990726 A 5210 SEAL JETAIR JETSTM JETSTM4101 1500501 EU PASSENGER DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 320UE 41043 PVD/IAD - FLT 7531 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND PASSENGER DOOR SEAL MIS-POSITIONED. MAINT ENANCE RE-POSITIONED SEAL. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001184 19990820 01184 EU 1999 8 20 VTZA990153 1 19990610 A 5280 14152030405 BUSHING JETAIR JETSTM JETSTM4101 1500501 EU RT MLG WORN A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 327UE 41080 IAD/RDU - FLT 7623 - DURING CLIMB, AIRCRAFT RETURNED TO GATE DUE TO RT PROPELLER VIBRATION. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND RT SPADE DOOR BUSHINGS WORN AND CAUSING VIBRATION. MAINTENAN CE REMOVED RT SPADE DOOR AND OPENED DMI 50945. CDT 32-10. MAINTENANCE CLOSED DMI 50945 ON 6-16-99 BY REINSTALLING SPAD E DOOR, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001185 19990820 01185 EU 1999 8 20 VTZA990182 1 19990629 A 3234 877701 SELECTOR JETAIR JETSTM JETSTM4101 1500501 EU LANDING GEAR FAILED A VTZA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 322UE 41058 IAD/SWF - FLT 7388 - DURING APPROACH, CREW ABORTED APPROACH AFTER OBSERVING RT MAIN GEAR, MAIN AND STANDBY GEAR INDICATI ONS INOPERABLE. AIRCRAFT LANDED WITH NO FURTHER PROBLEMS. AIRCRAFT WAS FERRIED TO IAD AFTER GEAR INSPECTION. MAINTENA NCE INSPECTED AGAIN AT IAD AND REMOVED AND REPLACED CONTROL, SELECTOR, AND PERFORMED GEAR SWINGS, OPS CHECK OK. AIRCRAF T RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001186 19990820 01186 EU 1999 8 20 VTZA990184 1 19990628 A 5230 DOOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT NOT SECURE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 303UE 41015 IAD/SWF - FLT 7284 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO CARGO DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESECURED DOOR, OPS CHECKED OK. AIRCRAFT WAS RELEASE D AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001187 19990820 01187 EU 1999 8 20 VTZA990185 1 19990705 A 2435 STARTER/GEN JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 27 325UE 41063 IAD/CHS - FLT 7311 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT GENERATOR DROPPED OFF-LINE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED GROUND RUNS ON LT GENERATOR AND COULD N OT DUPLICATE, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001188 19990820 01188 EU 1999 8 20 VTZA990186 1 19990705 A 2722 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU RUDDER LACK OF LUBE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 318UE 41041 IAD/RDU - FLT 7617 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RUDDER TRIM FROZE AND WOULD NOT MOVE. AI RCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND LUBRICATED RUDDER JACK SCREW TRIM TAIL. OP S CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001189 19990820 01189 EU 1999 8 20 VTZA990187 1 19990705 A 5610 WINDSHIELD JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT BIRD STRIKE A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 332UE 41100 IAD/EWR - FLT 7540 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO BIRD STRIKE TO LT WINDSHIELD. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION OF AIRCRAFT AND NO DAMAGE NOTED, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001190 19990820 01190 NE 1999 8 20 VTZA990188 2 19990702 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RIGHT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 307UE 41021 IAD/CHS - FLT 7569 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE WOULD ONLY MAKE 75 PERCENT TORQUE. AIRCR AFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED GROUND RUN AND COULD NOT DUPLICATE P ROBLEM. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082001191 19990820 01191 NE 1999 8 20 VTZA990189 2 19990704 A 7320 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 305UE 41019 IAD/RDU - FLT 7639 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LT ENGINE WOULD NOT MAKE UNSCHEDULED TORQUE. AIRCR AFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED LT MAX FUEL FLOW, OPS CHECK OK. AIRC RAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082001192 19990820 01192 EU 1999 8 20 VTZA990179 1 19990627 A 7722 EGT INDICATION JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 317UE 41031 BOS/JFK - FLT 7663 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE LOW TORQUE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 45131, MEL 76-2 ON TTL. MAINTENANCE CLOSED DMI 45131 ON 6 -29-99 BY ADJUSTING LT EGT COMPENSATION, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001193 19990820 01193 EU 1999 8 20 VTZA990191 1 19990707 A 2750 RETRACT MECH JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS MALFUNCTIONED A VTZA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 27 312UE 41025 IAD/EWR - FLT 7538 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FLAPS WOULD NOT RETRACT AFTER TAKEOFF. FLAPS WENT TO 25 DEGREES AFTER LANDING WITH FLAP SELECTOR IN THE UP POSITION. AIRCRAFT RETURNED TO GATE WITH NO FURTHE R PROBLEMS. MAINTENANCE INSPECTED AND RESET EMERGENCY SELECT BUTTON, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001194 19990820 01194 EU 1999 8 20 VTZA990190 1 19990707 A 2750 QA3043 FILTER JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 312UE 41025 IAD/EWR - FLT 7544 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FLAPS WOULD NOT RETRACT FROM 9 DEGREES. AIRCRAFT RETURNED TO GATE WITH NO FUTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND BYPASS PIN POPPED ON HYDRAULIC RET URN FILTER. MAINTENANCE REMOVED AND REPLACED RETURN FILTER AND FLUSHED SYSTEM AND RESET PIN AND CYCLED FLAPS THROUGH 40 TIMES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001195 19990820 01195 EU 1999 8 20 VTZA990207 1 19990709 A 3350 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 314UE 41027 SCE/IAD - FLT 7605 - DURING DESCENT, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS EMERGENCY FLOOR TR ACK LIGHTS INOPERABLE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESECURED CONNECTION O N LIGHTS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001196 19990820 01196 EU 1999 8 20 VTZA990205 1 19990707 A 2751 TY176004A TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS FAILED A VTZA A UNSCHED LANDING F N FLT CONT AFFECTED FALSE WARNING CL CLIMB 1 EA 27 311UE 41029 IAD/BDL - FLT 7680 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FLAP ASYM AMBER LIGHT ILLUMINATED. AIRCR AFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLAP TRANSDUCER, OPS CHEC K OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001197 19990820 01197 EU 1999 8 20 VTZA990206 1 19990206 A 3350 6047051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 329UE 41097 IAD/ORF - FLT 7225 - DURING PREFLIGHT, AIRCRAFT STAYED AT GATE DUE TO EMERGENCY LIGHT AT MAIN ENTRANCE DOOR DOES NOT ILL UMINATE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FORWARD BATTERY PACK. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001198 19990820 01198 NE 1999 8 20 VTZA990209 2 19990710 A 7320 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 317UE 41031 IAD/RIC - FLT 7245 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE HAD A DUCT FAIL WARNING LIGHT AND ONLY MADE 93 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVE D AND REPLACED DUCT O-RING AND ADJUSTED LT ENGINE MAX POWER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. REF: OPERATOR CNTRL NR 99ZZZX3060. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082001199 19990820 01199 EU 1999 8 20 99ZZZX3060 1 19990710 A 3610 O-RING JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 317UE 41031 IAD/RIC - FLT 7245 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE HAD A DUCT FAIL WARNING LIGHT AND ONLY MADE 93 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVE D AND REPLACED DUCT O-RING AND ADJUSTED LT ENGINE MAX POWER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. REF: OPERATOR CNTRL NR VTZA990209. 2 L 7 2 4T 4 T RT A41NM E18NE 1999082001200 19990820 01200 EU 1999 8 20 VTZA990220 1 19990220 A 3240 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BRAKE SYSTEM OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 309UE 41022 IAD/CMH - FLT 7452 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO CWS CONTINUOUSLY SOUNDED. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND EMERGENCY BRAKE CONTROL VALVE MICROSWITCH OUT OF ADJUSTMENT . MAINTENANCE ADJUSTED MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001201 19990820 01201 EU 1999 8 20 VTZA990228 1 19990715 A 5230 DOOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT NOT LATCHED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 328UE 41083 IAD/EWR - FLT 7494 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO CARGO DOOR CAP ILLUMINATING ON TAKEOFF ROLL. MAINT ENANCE CYCLED BAGGAGE DOOR. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082001202 19990820 01202 WP 1999 8 20 RAIA990803 2 19990804 A 7261 1379305AL03 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CE 03 338TE 932 CMI - FLT 7449 - RIGHT ENGINE OIL PRESSURE LOW. MAINTENANCE REPLACED OIL RETURN LINE TO OIL TANK. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1999082001203 19990820 01203 SO 1999 8 20 RAIA990802 1 19990803 A 3610 M832481226 GAMMA SEAL EMB 145 EMB145 SO RT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 803HK 145077 ORD - FLT 5792 - NR 2 ENGINE BLEED LEAK. MAINTENANCE REPLACED GAMMA SEAL ON NR 2 ENGINE BLEED LINE. (X) 2 L 7 2 4F RT T00011AT 1999082001204 19990820 01204 NE 1999 8 20 RAIA990801 2 19990802 A 7313 AS3209009 O-RING AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CE 03 422TE 106 120540 FLT 7402 - STL - NR 1 ENGINE LEAKING FUEL. MAINTENANCE REPLACED O-RING FOR FUEL NOZZLE AT 10 O'CLOCK POSITION. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999082001205 19990820 01205 1999 8 20 RAIA990744 4 19990730 A 3418 C850023 STICK SHAKER JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 565HK 41082 DCA - FLT 7784 - RIGHT STICK SHAKER INOPERATIVE. MAINTENANCE REPLACED RIGHT STICK SHAKER. (X) 2 L 7 2 4T RT A41NM 1999082001206 19990820 01206 EU 1999 8 20 RAIA990743 1 19990730 A 2422 559012A INVERTER AEROSP ATR42 ATR42300 8680920 EU NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424TE 124 STL - FLT 7126 - ON TAXI OUT, NR 2 INVERTER FAULTED. MAINTENANCE REPLACED NR 2 INVERER. (X) 2 H 7 2 4T RT A53EU 1999082001207 19990820 01207 EU 1999 8 20 RAIA990742 1 19990731 A 2422 559012A INVERTER AEROSP ATR42 ATR42300 8680920 EU NR 2 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424TE 4529 124 STL - FLT 7003 - NR 2 INVERTER FAULT. MAINTENANCE REPLACED NR 2 STATIC INVERTER. (X) 2 H 7 2 4T RT A53EU 1999082001208 19990820 01208 EU 1999 8 20 RAIA990741 1 19990730 A 3240 S1226142 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU BRAKE SYSTEM FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 427AM 876 STL - FLT 7328 - DURING START, EMERGENCY BRAKE ACCUMULATOR INDICATED 3000 PSI. MAINTENANCE REPLACED EMERGENCY BRAKE PRES SURE TRANSMITTER. (X) 2 L 7 2 4T RT A56EU 1999082001209 19990820 01209 EU 1999 8 20 RAIA990740 1 19990728 A 3610 S2L226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 563HK 41079 STL FLT 7282 - LEFT DUCT FAIL LIGHT ON. MAINTENANCE REPLACED SEAL FOR LEFT DUCT. (X) 2 L 7 2 4T RT A41NM 1999082001210 19990820 01210 EU 1999 8 20 RAIA990739 1 19990728 A 3610 600250 SEAL AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 722TE 220 STL - FLT 7408 - BLEED LEAK LEFT SIDE. MAINTENANCE REPLACED SEAL FOR DUCT UNDERNEATH CABIN FLOOR. (X) 2 H 7 2 4T RT A53EU 1999082001211 19990820 01211 SO 1999 8 20 RAIA990738 1 19990727 A 2720 156221 SWITC H EMB 145 EMB145 SO RUDDER FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 802HK 145066 RUDDER SYSTEM NR 2 FAIL LIGHT ON. MAINTENANCE REPLACED NR 2 RUDDER PRESSURE SWITCH. (X) 2 L 7 2 4F RT T00011AT 1999082001212 19990820 01212 EU 1999 8 20 RAIA990737 1 19990727 A 7603 AN3C12 BOLT JETAIR JETSTM JETSTM4101 1500501 EU LT POWER LEVER FAILED A RAIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CE 03 554HK 41067 BWI - FLT 7681 - LEFT POWER LEVER STUCK IN-FLIGHT. SHUT ENGINE DOWN. MAINTENANCE INSPECTED AND FOUND COTTER PIN AND BO LT HEAD CHAFING AGAINST FUEL CONTROL. INSTALLED NEW COTTER PIN AND BOLT. (X) 2 L 7 2 4T RT A41NM 1999082001213 19990820 01213 EU 1999 8 20 RAIA990726 1 19990722 A 7922 L8523427 VERNITHERM BAG JETSTM JETSTM3201 1500217 EU NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 341TE 950 STL - FLT 7107 - ENGINE OIL TEMPERATURE APPROACHING RED LINE. MAINTENANCE REPLACED VERNITHERM IN OIL COOLER FOR NR 1 EN GINE. (X) 2 L 7 2 4T RT A56EU 1999082001214 19990820 01214 1999 8 20 RAIA990729 4 19990722 A 3425 501156616 ADI JETAIR JETSTM JETSTM4101 1500501 EU STANDBY SYSTEM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 41039 JFK - FLT 7633 - STANDBY ATTITUDE INDICATOR WILL NOT STAY ERECT. MAINTENANCE REPLACED STANDBY ADI. (X) 2 L 7 2 4T RT A41NM 1999082001215 19990820 01215 1999 8 20 RAIA990728 4 19990722 A 3425 501156616 ADI JETAIR JETSTM JETSTM4101 1500501 EU STANDBY SYSTEM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 6547 483 41039 JFK - FLT 7633 - STANDBY ATTITUDE DIRECTION INDICATOR WILL NOT STAY ERECT. MAINTENANCE REPLACED STANDBY ADI. (X) 2 L 7 2 4T RT A41NM 1999082001216 19990820 01216 EU 1999 8 20 RAIA990727 1 19990722 A 3620 218D4 CONTROL UNIT BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 435AM 14058 889 STL - FLT 7306 - LEFT DUCT FAIL LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT DUCT FAIL CONTROL UNIT. (X) 2 L 7 2 4T RT A56EU 1999082001217 19990820 01217 EU 1999 8 20 RAIA990736 1 19990727 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 570HK 41089 JFK - FLT 7724 - POD SMOKE LIGHT ILLUMINATED. MAINTENANCE REPLACED POD SMOKE DETECTOR. () 2 L 7 2 4T RT A41NM 1999082001218 19990820 01218 SO 1999 8 20 RAIA990735 1 19990727 A 2910 15633 SWITCH EMB 145 EMB145 SO NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 803HK 145077 ORD - FLT 5792 - NR 1 ENGINE HYDRAULIC PUMP FAIL MESSAGE. MAINTENANCE REPLACED NR 1 EDP PRESSURE SWITCH. (X) 2 L 7 2 4F RT T00011AT 1999082001219 19990820 01219 NE 1999 8 20 RAIA990734 2 19990726 A 7310 3035681 FILTER AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 426TE 228 120561 STL - FLT 7116 - FUEL CLOG LIGHT CAME ON FOR RIGHT ENGINE. MAINTENANCE REPLACED HP FUEL PUMP OUTLET FILTER FOR RIGHT EN GINE. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1999082001220 19990820 01220 EU 1999 8 20 RAIA990733 1 19990714 A 3620 CA06R10SL3SF80 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 426AM 874 STL - FLT 7366 - WAITING FOR DEPARTURE, RECEIVED A LEFT DUCT LIGHT. MAINTENANCE REPLACED LEFT AIR OFF SWITCH CANNON PLU G. (X) 2 L 7 2 4T RT A56EU 1999082001221 19990820 01221 SO 1999 8 20 RAIA990732 1 19990713 A 2460 860CC01 CONTACTOR EMB 145 EMB145 SO NR 1 ESS BUS FAILED A RAIA D RETURN TO BLOCK J H WARNING INDICATION ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 803HK 145077 ORD - FLT 5787 - WHILE STARTING NR 2 ENGINE, LOST ALL ELECTRICAL POWER. MAINTENANCE REPALCED NR 1 ESS BUS TIE CONTACTOR . (X) 2 L 7 2 4F RT T00011AT 1999082001222 19990820 01222 1999 8 20 PLGA990725 4 19990725 A 3425 6226342022 EFIS TUBE SAAB SF340 SF340A 7850100 EU LT COCKPIT FAILED A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 05 744BA 340A105 ALB - FLT 6685 - ALB/BOX - FLT 6685 - RETURNED TO ALB DUE TO ELECTRICAL BURNING SMELL IN THE FLIGHT DECK. AIRCRAFT LAND ED WITHOUT INCIDENT. MAINTENANCE FOUND THE CAPTAIN'S UPPER EFIS TUBE TO BE AT FAULT. THE EFIS TUBE WAS REPLACED. REQU IRED OPERATIONAL CHECKS WERE PERFORMED AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999082001223 19990820 01223 WP 1999 8 20 99ZZZX3061 1 19990721 A 3350 41B004AD07G3 BATTERY GRIMES 60030431 DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 15 930BB 47521 SERVER CENTER CEILING EMERGENCY LIGHTS INOPERABLE. REF: B-CHECK NON-ROUTINE NR B2-0032. FOUND BATTERIES DISCHARGED, R ECHARGED BATTERIES PER MM 33-53-01. REINSTALLED BATTERIES AND OPERATIONAL CHECK GOOD IAW MM 33-50-0. (X) 2 L 7 2 4F A6WE 1999082001224 19990820 01224 WP 1999 8 20 99ZZZX3062 1 19990620 A 3350 08163000603 LIGHT BRUCE DOUG DC9 DC932 3022066 WP ROW 5 LOOSE A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 15 930BB 47521 REF: LOG PAGE 17635, ITEM 1 ON 6-20-99. TRACK LIGHTS ON FLOOR AT ROW 5 ARE LOOSE. RESECURED TRACK PER MM 33-50-0. OPS NORMAL PER MM 33-50-0. (X) 2 L 7 2 4F A6WE 1999082001225 19990820 01225 WP 1999 8 20 99ZZZX3063 1 19990514 A 3350 08163000603 LIGHT BRUCE DOUG DC9 DC932 3022066 WP ROWS 4 AND 12 LOOSE A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 15 930BB 47521 REF: LOG PAGE 18526, ITEM 3 ON 5-14-99. FLOOR TRACK LIGHTING LOOSE AT ROWS 4 AND 12. RE-INSTALLED FLOOR TRACK LIGHTING AT ROWS 4 AND 12 PER MM 33-53-1. PERFORMED TRACK LIGHT CHECK, OK. FOLLOW-UP MAINTENANCE PERFORMED IN GPT - LOG PAGE 1 8527 ITEM 1 ON 5-14-99. VERIFIED TRACK LIGHTING INSTALLED PER MM 33-53-1. 2 L 7 2 4F A6WE 1999082001226 19990820 01226 NM 1999 8 20 USAA990183 1 19990331 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 1661 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 DURING C-CHECK VISUAL INSPECTION, FOUND CORROSION UPPER SURFACE FLOORBEAM AT STA 1661 FROM RBL 17 TO LBL 17. CORROSION TASK NR C53-251-03/C53-252-03. BLENDED CORROSION PER SRM 53-00-51. (X) 2 L 7 2 4F RT A2NM 1999082001227 19990820 01227 NM 1999 8 20 USAA990240 1 19990331 A 5320 ANGLE BOEING 757 757225 1384959 NM BS 1640-1681.8 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ENTIRE SURFACE R-4 ANGLE SUPPORT BETWEEN STA 1640 TO STA 1681. 8. CORROSION TASK NR C53-251-03/C53-252-03. REPLACED COMPONENTS PER SRM 53-60-15. (X) 2 L 7 2 4F RT A2NM 1999082001228 19990820 01228 NM 1999 8 20 USAA990226 1 19990331 A 5320 ANGLE BOEING 757 757225 1384959 NM BS 859 - BS 879 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 DURING C-2 CHECK VISUAL INPSECTION, FOUND CRACKED ANGLE FOR FLOOR SUPPORT BL ZERO BETWEEN STA 859 AND STA 879. INSTALLE D NEW ANGLE SUPPORT PER SRM 53-30-51. (X) 2 L 7 2 4F RT A2NM 1999082001229 19990820 01229 NM 1999 8 20 USAA990181 1 19990331 A 5315 141N51141 FLOORBEAM BOEING 757 757225 1384959 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 60 INCH CORRODED AREA AT BS 377.7 FLOORBEAM UPPER CHORD LBBL 30 - RBL 30. REPLACED T-CAP PER TR 53-15-01. (X) 2 L 7 2 4F RT A2NM 1999082001230 19990820 01230 NM 1999 8 20 USAA990227 1 19990331 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION TOP OF FLOORBEAM STA 365 LBL 62 TO RBL 62. REPAIRED T-CAP PER SRM 5 3-00-51. (X) 2 L 7 2 4F RT A2NM 1999082001231 19990820 01231 NM 1999 8 20 USAA990188 1 19990331 A 5320 141N51603 INTERCOSTAL BOEING 757 757225 1384959 NM BS 345-365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL STA 345 TO STA 365 RBL 25. REPLACED WITH NEW INTERCOSTA L PER SRM 53-00-51. (X) 2 L 7 2 4F RT A2NM 1999082001232 19990820 01232 NM 1999 8 20 USAA990238 1 19990331 A 5320 WEB BOEING 757 757225 1384959 NM BS 345-365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL STA 345 TO STA 365 AT LBL 24 TOP CAP WEB. INSTALLED T-C AP ON WEB. (X) 2 L 7 2 4F RT A2NM 1999082001233 19990820 01233 EU 1999 8 20 VTZA990183 1 19990629 A 3397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BROKEN A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 EA 27 319UE 41042 CHS/IAD - FLT 7562 - DURING TAXI, CREW FOUND FLOOR EMERGENCY TRACK LIGHTS INOPERABLE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. (X) 2 L 7 2 4T RT A41NM 1999082001234 19990820 01234 NE 1999 8 20 VTZA990208 2 19990709 A 7320 31059005 FCU JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE NR 2 ENGINE FAILED A VTZA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 EA 27 323UE 41059 IAD/ORF - FLT 7325 - DURING APPROACH, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS NR 2 ENGINE FLAME D OUT ON APPROACH. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND RE PLACED FUEL CONTROL UNIT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082001235 19990820 01235 EU 1999 8 20 MALA976536 1 19990815 A 7110 LATCH SAAB SF340 SF340A 7850100 EU ENGINE COWL NOT SECURED A MALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 15 68XJ 068 PASSENGER NOTED COWLING MOVED ON TAKEOFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE FOUND LATCH NOT SECURED. RESECURED LA TCH, NO DAMAGE NOTED. 2 L 7 2 4T RT A52EU 1999082001236 19990820 01236 EU 1999 8 20 MALA976537 1 19990812 A 3230 AIR131330 SPRING SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A MALA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 GL 15 115XJ 340A115 RIGHT MAIN GEAR DID NOT LOCK DOWN ON APPROACH TO MSP. QRH UNSUCCESSFUL IN REMEDY. EMERGENCY LANDING MADE WITH INCIDENT . MAINTENANCE FOUND ASSISTER SPRING BROKEN AND CABLE WEDGED IN DRAG BRACE ASSEMBLY. MX REPLACED SPRING, CABLE AND ATTA CHING HARDWARE. REF AMM 32-11-35, RETOUCHED PAINT IN AFFECTED AREA AND PERFORMED GEAR SWINGS. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999082001237 19990820 01237 EU 1999 8 20 MALA976538 1 19990816 A 2613 CONNECTOR SAAB SF340 340B 7860101 EU LT TAIL PIPE LOOSE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 406XJ 406 LEFT TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF, RETURNED TO ATW. MAINTENANCE REMOVED COWL, CLEANED AND TIGHTENED CA NNON PLUGS, REINSTALLED COWL. GROUND RUN, NO LIGHT CAME ON AFTER 2 MINUTES FULL POWER RUN. 2 L 7 2 4T RT A52EU 1999082001238 19990820 01238 EU 1999 8 20 MALA976539 1 19990812 A 2844 LO PRESS LIGHT BAC 146 AVRO146RJ85A 1500097 EU NR 2 FUEL SYS ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 510XJ E2325 NR 2 FUEL LOW PRESSURE AND LEFT INNER LOW PRESSURE LIGHTS ILLUMINATED DURING CLIMBOUT. FOLLOWED QRH AND RETURNED TO MEM . MAINTENANCE SWAPPED LEFT INNER AND RIGHT OUTER RELAYS 2QG3 AND 1QG3 AND CB 2QG4 AND 4QG4, AFTER INSPECTING WIRING BEH IND OVERHEAD FUEL PANEL IN FLIGHT DECK. PERFORMED 20 MINUTE ENGINE RUN OF ALL 4 ENGINES, NO INDICATION OF FUEL LOW PRES S OR L EFT INNER LOW PRESS AT THIS TIME, RELEASED FOR CONTINUED SERVICE. 2 H 7 4 4F RT A49EU 1999082001239 19990820 01239 EU 1999 8 20 MALA976540 1 19990812 A 2840 52710002 RELAY BAC 146 AVRO146RJ85A 1500097 EU LT FUEL SYS FAILED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 510XJ E2325 EN ROUTE THE LEFT INNER FUEL PUMP LIGHT ILLUMINATED. RETURNED TO MEM. MAINTENANCE REPLACED RELAY XL11, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1999082001240 19990820 01240 EU 1999 8 20 MALA976541 1 19990812 A 2913 521449 HYD PUMP BAC 146 AVRO146RJ85A 1500097 EU YELLOW HYD SYS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 516XJ E2334 EN ROUTE THE YELLOW SYSTEM HYDRAULIC HIGH TEMP LIGHT ILLUMINATED. DIVERTED INTO DTW. MAINTENANCE REPLACED YELLOW ENGIN E DRIVEN HYDRAULIC PUMP IAW AMM 29-10-17, PERFORMED FUNCTION CHECK IAW AMM29-10-17. OPS CHECKED GOOD. 2 H 7 4 4F RT A49EU 1999082001241 19990820 01241 EU 1999 8 20 MALA976542 1 19990809 A 2760 WIRE BAC 146 AVRO146RJ85A 1500097 EU SPOILER SYS CHAFED A MALA K NONE O OTHER LD LANDING 1 GL 15 523XJ E2348 DURING GEAR RETRACTION ALL GEAR LIGHTS WENT OUT AND LIFT SPOILER CAUTION LIGHT ON GLARESHIELD ILLUMINATED. FOUND CB B4 POPPED. RESET ONCE AND TRIED THE ANNUNCIATOR TEST BUTTON, GEAR LIGHTS ILLUMINATED THEN CB B4 POPPED AGAIN. FOLLOWED QR H PROCEDURES FOR LANDING IN DTW, GREEN SPOILERS DID NOT DEPLOY ON LANDING. MAINTENANCE FOUND WH4 WIRE TO PIN E CHAFED. RESPLICED WIRE AND SECURED WIRE BUNDLE. 2 H 7 4 4F RT A49EU 1999082001242 19990820 01242 EU 1999 8 20 MALA976543 1 19990811 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DAMAGED A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 447XJ 447 CARGO SMOKE LIGHT ILLUMINATED. MAINTENANCE TIGHTENED CANNON PLUG ON FORWARD DETECTOR & REPLACED AFT DETECTOR DUE TO DAM AGE, IAW MM 2613-15. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999082001243 19990820 01243 EU 1999 8 20 MALA976544 1 19990728 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 DURING HEAVY CHECK INSPECTION, DENT ON RIGHT SIDE OF FUSELAGE AFT OF ICE SHEILD. MAINTENANCE PERFORMED PERMANENT REPAIR IAW EO S53009. 2 L 7 2 4T RT A52EU 1999082001244 19990820 01244 EU 1999 8 20 MALA976545 1 19990811 A 5414 SKIN SAAB SF340 SF340A 7850100 EU LT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 LEFT ENGINE NACELLE INBOARD SIDE CHAFED AFTER REMOVAL OF THE SB DOUBLER. THIS DISCREPANCY WAS DISCOVERED DURING THE AIR CRAFT'S SCHEDULED HEAVY CHECK. MAINTENANCE REPAIRED IAW PER EO S54019. 2 L 7 2 4T RT A52EU 1999082001245 19990820 01245 EU 1999 8 20 MALA976546 1 19990813 A 5754 STRAP SAAB SF340 SF340A 7850100 EU LE FLAPS BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 DURING HEAVY CHECK INSPECTION FOUND CENTER HINGE FLAP STRAP BROKEN AD 990417-01. MAINTENANCE REMOVED AND REPLACED STRAP IAW EO AD 990417-02. 2 L 7 2 4T RT A52EU 1999082001246 19990820 01246 EU 1999 8 20 MALA976547 1 19990813 A 5711 SPAR SAAB SF340 SF340A 7850100 EU WS 142 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 46XJ 046 DURING HEAVY CHECK INSPECTION AND WHILE PERFORMING EO AD990417-02, NOTED REAR SPAR CRACK AT FLAP WS 142. MAINTENANCE RE PAIRED IAW EO S57007. 2 L 7 2 4T RT A52EU 1999082001247 19990820 01247 WP 1999 8 20 9903169885 1 19990812 A 3260 PROX CONTL BOX DOUG DC9 DC951 3022051 WP LT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 401EA 47682 DURING APPROACH INTO DTW, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. FLIGHT CREW DECLARE D AN EMERGENCY AND ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED GREEN DOWNLOCK LIGHT BULBS AND PROXIMITY CONTROL BOX. ALSO, REPAIRED LEFT AND RIGHT MAIN GEAR DOORS DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1999082001248 19990820 01248 NE 1999 8 20 9903182297 2 19990811 A 7314 378200 FUEL PUMP BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE INOP A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 01 297US 40156 5554 21789 696473 AT FLIGHT LEVEL 6,000 FEET, THE NR 2 ENGINE EXPERIENCED A FLAMEOUT WHEN THE THROTTLES WERE PUSHED FORWARD FROM THE IDLE POSITION. THE FLIGHT CREW PERFORMED COM PROCEDURES, WINDMILLED NR 2 ENGINE, DIVERTED FLIGHT TO ORD, AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE FUEL PUMP SHAFT SHEARED. REPLACED THE NR 2 ENGINE FUEL PUMP AND FUEL CONTR OL UNIT. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999082001249 19990820 01249 NE 1999 8 20 9903196635 2 19990812 A 7200 ENGINE BOEING 747 747227B 1384888 NM PWA JT9 JT9D7Q 52054 NE NR 3 FLAMED OUT A NWAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 GL 01 635US 21682 702179 AFTER ENTERING MODERATE TURBULENCE WITH PRECIPITATION, THE AUTO THROTTLES DISCONNECTED AND THE CREW OBSERVED LOW EGT ON THE NR 3 ENGINE. THE ENGINE FLAMEOUT PROCEDURE WAS FOLLOWED AND THE FIRST RESTART ATTEMPT WAS SUCCESSFUL. ENGINE OPERA TION FOR THE REMAINDER OF THE FLIGHT WAS NORMAL. MAINTENANCE REPLACED THE ENGINE FUEL FILTER AND INSPECTED THE ENGINE P ER FIM WITH NO DEFECTS NOTED. 2 L 7 4 4F 4 F A20WE E3NE 1999082001250 19990820 01250 NM 1999 8 20 9903205646 1 19990815 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM ROW 16-19 INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 546US 26493 DURING SCHEDULED MAINTENANCE, THE SEAT MOUNTED EMERGENCY LIGHTS ON ROWS 16-19 WERE INOPERATIVE. MAINTENANCE REPLACED TH E POWER SUPPLY WITH A SERVICEABLE UNIT. OPERATIONAL TESTS WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999082001251 19990820 01251 NM 1999 8 20 99FDEA00337 1 19990817 A 2750 S4913809CW11202 CONTROL CABLE DOUG MD11 MD11F 3023600 NM RT TE FLAP BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 610FE 48603 WING INBOARD FLAP BUS CABLE ON RT WHEEL WELL FOUND BROKEN AT ONE TERMINAL END DURING SYS NR 2 PRESSURE ON. *S/D* RT I/ B FLAP BUS CABLE REMOVED AND REPLACED PER MM 27-51-10-4. SATISFACTORY PER MM 27-50-00-5. 2 L 7 3 4F RT A22WE 1999082001252 19990820 01252 WP 1999 8 20 99FDEA00338 1 19990817 A 5270 WARNING LIGHT DOUG DC10 DC1010F 3022111 WP AIR DOND DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 054FE 47808 AIR COND DOORS LIGHT IN FLIGHT WENT OUT ON GROUND. C/W PRIOR TO DEPARTURE VISUALLY INSURED THAT THE DOORS WERE CLOSED & HANDLE WAS FLUSH WITH FUSELAGE. 2 L 7 3 4F A22WE 1999082001253 19990820 01253 1999 8 20 99FDEA00339 4 19990818 A 3441 4616000800080 IRU AIRBUS 310 A310203 EU NR 2 INOP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 430FE 394 NR 2 IRU WARNING, NR 3 EUR ALREADY ON DEFERRAL. REMOVED AND REPLACED NR 2 IRU PER MM 34-25-14. ACCOMPLISHED OPER CK PE R 34-25-00. 2 L 7 2 4F RT A35EU 1999082001254 19990820 01254 NM 1999 8 20 99UAL900414 1 19990807 A 2530 35200011 COFFEMAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY SMOKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7449U 21903 LOWER COFFEEMAKER IN AFT GALLEY SMOKING AND SPARKING. *S/D* REPLACED COFFEEMAKER. INSPECTED WIRING, LEFT UNIT ON FOR SEVERAL HOURS, NO DEFECTS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1999082001255 19990820 01255 NM 1999 8 20 99UAL900415 1 19990806 A 2131 CONTROLLER HAMILTON STA 106120910 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 380UA 88071958 24655 LOST CABIN PRESSURE ON TAKEOFF. *S/D* COULD NOT CLOSE AFT OUTFLOW VALVE IN MANUAL AC OR DC. REPLACED CABIN PRESSURE S ELECTOR PANEL AND CABIN PRESSURE CONTROLLER. 2 L 7 2 4F 4 F RT A16WE E2GL 1999082001256 19990820 01256 NM 1999 8 20 99UAL900416 1 19990807 A 3230 1U10851 SEQUENCE VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT MLG LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 7251U 21398 ON GEAR EXTENSION AIRCRAFT LOST HYDRAULIC SYSTEM A. BOTH PUMPS RAN TO ZERO HYDRAULIC FLUID QUANTITY. *S/D* REPLACED N R 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND REPLACED LT MLG LOCK OPERATED SEQUENCE VLV PER MAINTENANCE MANUAL. PERFO RMED NORMAL RETRACTION AND MANUAL EXTENSION TESTS, NO IRREGULARITIES FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1999082001257 19990820 01257 NM 1999 8 20 99UAL900417 1 19990807 A 3241 841602 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ANTI SKID SYS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 522UA 24931 DIVERTED TO JFK DUE TO ANTISKID EICAS MESSAGE. *S/D* PERFORMED BITE TEST AND FOUND CARD 2-6 DISPLAYED. REPLACED ANTIS KID AUTOBRAKE CONTROL UNIT. 2 L 7 2 4F 4 F RT A2NM E17NE 1999082001258 19990820 01258 NM 1999 8 20 99UAL900418 1 19990807 A 2913 3508807 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT HYD SYS BROKEN A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 503UA 24624 LANDED DEN UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. *S/D* ENGINE DRIVEN PUMP SHAFT SHEARED. POSSIBLE B EARING FAILURE. REPLACED PUMP. 2 L 7 2 4F 4 F RT A2NM E17NE 1999082001259 19990820 01259 EU 1999 8 20 99UAL900420 1 19990811 A 5610 WINDOW AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT COCKPIT NOT LATCHED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 416UA 479 ABORTED TAKEOFF AFTER PILOTS WINDOW OPENED AT 80-90 KTS. PILOTS REPORTED WINDOW WAS NOT FULLY LOCKED. *S/D* CAPTAIN'S SLIDING WINDOW WAS NOT FULLY LOCKED. RED-COLORED RELEASE BUTTON ON WINDOW HANDLE POPS UP WHEN THE WINDOW IS LOCKED. T HIS SERVES AS A VISUAL INDICATION. ENSURING THAT WINDOW IS FULLY CLOSED AND LOCKED PRIOR TO TAKEOFF HAS BEEN AND REMAIN S AN ELEMENT OF THE FLIGHT CREW'S PREFLIGHT CHECKLIST. 2 L 7 2 4F 4 F RT A28NM E40NE 1999082001260 19990820 01260 1999 8 20 99UAL900421 4 19990812 A 2210 SC47003 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT YAW DAMPER FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 410UA 18418 463 DIVERTED TO ATL DUE TO LOSS OF HYDRAULIC PRESSURE. *S/D* LT YAW DAMPER ACTUATOR DEVELOPED A PIN HOLE LEAK WHICH CAUSED THE HYD SYSTEM (GREEN) TO BLEED DOWN. ACTUATOR (P/N SC4700-3), (S/N 5030), MR27258-1035. ACTUATOR WAS REPLACED AND AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 1999082001261 19990820 01261 NM 1999 8 20 99UAL900422 1 19990812 A 3240 BRAKES AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE MLG LOCKED UP A UALA K NONE O OTHER LD LANDING 1 WP 29 820UA 898 BRAKES LOCKED UP UPON LANDING. *S/D* AFTER LANDING SHUT DOWN NR 2 ENG ON TAXI HOLDING SHORT OF RUNWAY. BRAKES WERE SE T, BRAKES WOULD NOT RELEASE. BSCU WAS RESET, NO HELP. BRAKES WERE BLED AND TAXI TESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999082001262 19990820 01262 NM 1999 8 20 99UAL900423 1 19990812 A 3350 BULB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR 2L FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7280U 21558 EMERGENCY EXIT LIGHT SIGN AT DOOR 2L INOPERATIVE. RELAMPED EXIT LIGHT, OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999082001263 19990820 01263 NM 1999 8 20 99UAL900424 1 19990802 A 5312 BULKHEAD CHORD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1183 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7451U 21905 THE FORWARD EDGE OF THE CHORD AT STATION 1183 BULKHEAD LBL 24, WL 209 WAS CORRODED BEYOND THE SRM ALLOWABLE LIMIT. DAMA GE WAS TRIMMED OUT AND AREA WAS REPAIRED WITH STRAP AND FILLER PER TIMCO INSTRUCTIONS. THIS REPAIR WAS APPROVED BY TIMC O'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999082001264 19990820 01264 WP 1999 8 20 ABXA9900645 1 19990814 A 5610 5613217508 WINDOW DOUG DC8 DC863F 302198F WP RT COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED WINDOW MECHANISM IAW DC8 MM 56-10-3. 2 L 7 4 4F 4A25 1999082001265 19990820 01265 WP 1999 8 20 ABXA9900646 1 19990817 A 5250 AR25291 LOCK DOUG DC8 DC861 3021952 WP COCKPIT DOOR OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 COCKPIT DOOR LOCK WAS INOPERATIVE, WOULD NOT RELEASE. REPAIRED COCKPIT DOOR IAW DC8 MM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999082001266 19990820 01266 WP 1999 8 20 ABXA9900647 1 19990817 A 5313 591287029 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 1089 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND LONGERON 14 LEFT CORRODED AT STATION 1089. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999082001267 19990820 01267 NE 1999 8 20 MWEA99507 2 19990815 A 7260 PACKING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE LT ENG GEAR BOX FAILED A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 212ME 47701 AFTER TAKEOFF, FLIGHT ATTENDANTS SMELLED UNUSUAL ODOR. MTC REMOVED AND REPLACED FORWARD GEARBOX TRANSFER TUBE PAKCINGS. 2 L 7 2 4F 4 F A6WE E2EA 1999082001268 19990820 01268 WP 1999 8 20 MWEA99506 1 19990811 A 2560 113317 COVER DOUG DC9 DC914 3022034 WP DOOR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 80ME 45795 GALLEY DOOR SLIDE COVER FELL OFF. REPLACED COVER. 2 L 7 2 4F A6WE 1999082001269 19990820 01269 NM 1999 8 20 DHL99724005 1 19990818 A 2751 18129932 INDICATOR BOEING 727 727225 1384077 NM TE FLAPS MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 724DH 19862 ON FLAP RETRACTION, O/B INDICATION NOT IN WHITE ARC, I/B FLAP RETRACTION WELL OUT OF ARC AT 2 DEGREE FLAPS UP. OPS CHEC K FLAPS AT ALL SETTINGS, INDICATOR FAILED COMPLETELY. REMOVED AND REPLACED INDICATOR, I/B FLAPS OPERATED NORMAL PER MM 27-81. 2 L 7 3 4F A3WE 1999082100001 19990821 00001 EU 1999 8 21 UF6A990108 1 19990731 A 5542 SKIN BAG ATP ATP EU RUDDER DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 15037 2021 ORD - RUDDER HAS CRACK ON TRAILING EDGE SKIN ADJACENT TO SPRING TAB. MAINTENANCE REPAIRED DAMAGE IAW DER REPORT NR 99-0 05. (X) 2 L 7 2 4T RT A27NM 1999082100002 19990821 00002 EU 1999 8 21 UF6A990308 1 19990731 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - RIGHT HAND REAR EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999082100003 19990821 00003 NE 1999 8 21 JBXA9900094 2 19990725 A 7261 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE NR 2 OVER SERVICED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 583ML 7327 872392 DURING CLIMBOUT, NR 2 ENGINE OIL TEMP BEGAN CLIMBING. PULLED POWER BACK HALF WAY AND TEMP STABILIZED AT 158 DEG. PULLE D POWER BACK TO IDLE AND TEMP RETURNED TO NORMAL RANGE. ALL OTHER ENGINE INDICATIONS WERE NORMAL. FOUND NR 2 ENGINE WA S OVERSERVICED BY 0.25 QTS AND THE NR 2 ENGINE OIL TEMP BULB CANNON PLUG WAS LOOSE. DRAINED OIL TO PROPER LEVEL, SECURE D OIL TEMP BULB CANNON PLUG, AND PERFORMED OPS CHECK IAW 79-31-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999082100004 19990821 00004 NE 1999 8 21 DL76L991593 2 19990715 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 194DN 9307 28451 727717 AT CRUISE ALTITUDE LT ENGINE EGT WENT TO 710 DEGREES. EGT STAYED AT 710 DURING THROTTLE RETARD DOWN TO IDLE RPM OR ABO UT 15 SECONDS. ENGINE WAS NOT SHUT DOWN. A/C DIVERTED TO YYT (ST.JOHNS). PERFORMED BORESCOPE AND RUN UP INSPECTIONS. RESTRICTED TO 60 HRS FOR REMOVAL PER FIM. 2 L 7 2 4F 4 F RT A1NM E24NE 1999082100005 19990821 00005 NM 1999 8 21 DL72S991603 1 19990717 A 2613 DETECTOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE WORN A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 515DA 64057 21431 695272 NR 1 ENG STRUT OVERHEAT. REPLACED S/O VALVE AND CLAMPS. FOUND OVERHEAT DETECTOR WORN. REPLACED SAME, RAN ENG AND CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999082100006 19990821 00006 NM 1999 8 21 DL757991615 1 19990718 A 4920 380029816 APU BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE AFT FUSELAGE MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 667DN 7217 25035 P1642 OIL SMELL IN CABIN DURING FINAL AND DURING TAXI IN. NR 1 ENG REQUIRED 16 PTS OIL. INSPECTED HPC FOR EVIDENCE OF NR 3 B EARING FAILURE, NO OIL FOUND. ALSO, INSPECTED INLET/ EXHAUST FOR SIGNS OF OIL AND NONE FOUND. INSPECTED APU PNEU, DUCT NONE FOUND. PER FIM 49-11-00 FIG 122 REQUIRES REPLACEMENT, PLACED APU AIR ON MCO. APU TO BE REPLACED AT A LATER DATE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999082100007 19990821 00007 NM 1999 8 21 DL72S991632 1 19990720 A 2752 651622187 SKIN BOEING 727 727232 1384082 NM LT LE SLAT CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 LOWER SKIN CUT TO FACILITATE MAINTENANCE. REPAIRED PER M/M 57-54-0 FIG 801. 2 L 7 3 4F A3WE 1999082100008 19990821 00008 NE 1999 8 21 DL757991637 2 19990720 A 7230 COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE STALLED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 655DL 21910 24395 726701 LEFT ENGINE COMPRESSOR STALL AFTER T/O AT 4000 FT AND 250 KTS. INSPECTED LT ENG PER FIM 71-05-00 FIG 103 AND 104. OIL FILTER, CHIP DETECTOR AND BOROSCOPE CHECKS NORMAL. REPLACED OIL FILTER, RAN ENG AND ALL CKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1999082100009 19990821 00009 WP 1999 8 21 DHL9980239C 1 19990429 A 5753 FAIRING DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 C-CHECK, RT WING FLAP HINGE FAIRING AT STA 340 CRACKED IN 2 PLACES, DOT 450 ON RACK E4. STOP DRILLED END CRACK AT RT WI NG FLAP HINGE FAIRING IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED DOUBLER REPAIR 2024 T3.063 4 X 2.5 IAW DC-8 SR 51-1-4 PG 1 PAR 1. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 13 & 16 PAR 6 6F. INSTALLED PER DC-8 SRM 51-1-21 PG 1 PAR 1. 2 L 7 4 4F RT 4A25 1999082100011 19990821 00011 WP 1999 8 21 AT9900500 1 19990609 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 446 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 830AT 47723 DURING A SCHEDULED INSPECTION AT TIMCO, IN LAKE CITY, FL, FOUND CRACK BEYOND DOUBLER UNDERSIDE FLOOR SUPPORT FWD CARGO C OMPARTMENT AT BS 446 AT LONGERON 30. REMOVED EXISTING SPLICE DOUBLER, STOP DRILLED CRACK, FABRICATED REPAIR AND INSTALL ED REPAIR AND SPLICE DOUBLER IAW DC9 SRM 51-30-2, 51-10-3 AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999082100012 19990821 00012 NM 1999 8 21 DL733991658 1 19990723 A 7830 REVERSE LIGHT BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE ILLUMINATED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 306WA 23347 720673 NR 2 ENG REV LIGHT CAME ON DURING TAKEOFF. ABORTED TAKE OFF JUST UNDER 100 KTS. LOCKED OUT NR 2 ENG REV PER MEL 78-00- 02. MCO - CLEANED CONNECTORS. UNABLE TO DUPLICATE, REMOVED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999082100013 19990821 00013 NE 1999 8 21 DL72K991669 2 19990725 A 7314 724203767 SEAL BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 415DA 21257 700397 DURING CRUISE AT FL290, NR 2 ENG OIL QNTY DECREASED TO ZERO GAL. OIL PRESS LOW LIGHT ILLUMINATED OIL TEMP RAISE TO 130 OIL PRESS 17 PSI ENG SHUTDOWN PER CHECKLIST WINDMILLED FOR 22 MINS. PRIOR TO SHUTDOWN OTHER INSTRUMENTS NORMAL. MAINT ENANCE T/S FOUND FUEL PUMP/GEAR BOX CARBON SEAL LEAKING. MTC IN WORK REPLACING SEAL PER M/M. 2 L 7 3 4F 4 F A3WE E2EA 1999082100014 19990821 00014 WP 1999 8 21 AT9900518 1 19990718 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CRACKS IN MAIN FRAME AT BS 718L. REMOVED AND REPLACED MAIN FRAME BS 718L IAW AIRTRAN EO 12-5311-29-B1044 FIG 5,6 AND 7. 2 L 7 2 4F A6WE 1999082100015 19990821 00015 WP 1999 8 21 USAAD990092 1 19990709 A 3350 P2010014 LIGHT DOUG DC9 DC931 3022065 WP PASSENGER DOOR FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913VJ 45846 IND - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LIGHT AND THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE WERE INOPERATIVE. M AINTENANCE REPLACED THE LIGHT ASSEMBLY FOR THE MAIN ENTRANCE SLIDE LIGHT AND THE BATTERY FOR THE EMERGENCY LIGHT ABOVE T HE TAILCONE SLIDE. REF: OPER CNTRL NR 99ZZZX2828. (X) 2 L 7 2 4F A6WE 1999082100016 19990821 00016 WP 1999 8 21 99ZZZX2828 1 19990709 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP RT LAVATORY DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913VJ 45846 IND - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LIGHT AND THE EMERGENCY LIGHT ABOVE THE TAILCONE SLIDE WERE INOPERATIVE. M AINTENANCE REPLACED THE LIGHT ASSEMBLY FOR THE MAIN ENTRANCE SLIDE LIGHT AND THE BATTERY FOR THE EMERGENCY LIGHT ABOVE T HE TAILCONE SLIDE. REF: OPER CNTRL NR USAAD99092. 2 L 7 2 4F A6WE 1999082100017 19990821 00017 EU 1999 8 21 99FDEA00291 1 19990728 A 3230 RETRACT MECH AIRBUS 310 A310203 EU LANDING GEAR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 429FE 364 99-176 - ON T/O IN NR 2 SYS LAND GEAR WOULD NOT RETRACT, HANDLE WOULD NOT GO ABOVE HALFWAY. SWITCH TO SYS NR 1 HANDLE W ENT UP BUT GEAR STAY DOWN. 2 L 7 2 4F RT A35EU 1999082100018 19990821 00018 EU 1999 8 21 QXEA9901495 1 19990708 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION INSIDE CHANNEL AND AT CHANNEL RADIUS STARTING AT TRACK END AND GOING FORWAR D 11. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999082100019 19990821 00019 EU 1999 8 21 QXEA9901496 1 19990706 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - CLIP CRACKED AFT SIDE OF FRAME 16060 AND STRINGER 26. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999082100020 19990821 00020 EU 1999 8 21 QXEA9901497 1 19990706 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - CLIP CRACKED AFT SIDE OF FRAME 16060 AND STRINGER 28. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999082100021 19990821 00021 EU 1999 8 21 QXEA9901498 1 19990706 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - CLIP CRACKED AFT SIDE OF FRAME 16060 AND STRINGER 30. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999082100022 19990821 00022 EU 1999 8 21 QXEA9901499 1 19990706 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - POSSIBLE CLIP CRACKED AFT OF FRAME 16060 AND STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999082100023 19990821 00023 EU 1999 8 21 QXEA9901500 1 19990706 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - POSSIBLE CLIP CRACKED AFT OF FRAME 16060 AT STRINGER 47. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999082100024 19990821 00024 EU 1999 8 21 QXEA9901501 1 19990720 A 5240 BUSHING FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR SEIZED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - SERVICE/EMERGENCY DOOR LATCH BUSHINGS FORWARD, LOWER AND BOTH AFT ARE NOT FREE WHEN DOOR CLOSED AND LATCHED. REPA IRED IAW FOKKER MM 52-40-1, PAGE 502, PARAGRAPH 3AC17. 2 L 7 2 4F RT A20EU 1999082100025 19990821 00025 EU 1999 8 21 QXEA9901502 1 19990711 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - AFT CARGO BAY AT FRAME 13815A BETWEEN STRINGERS 72 AND 73 CLIP IS CRACKED. REMOVED AND REPLACED COMPLETE REPAIR A NGLE. 2 L 7 2 4F RT A20EU 1999082100026 19990821 00026 EU 1999 8 21 QXEA9901503 1 19990711 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - AFT CARGO BAY AFT FRAME 13815A BETWEEN STRINGER 2 AND 3 CLIP IS CRACKED. REMOVED AND REPLACED COMPLETE REPAIR CLI P ANGLE. 2 L 7 2 4F RT A20EU 1999082100027 19990821 00027 EU 1999 8 21 QXEA9901504 1 19990723 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FORWARD CARGO DOOR APERTURE IS DENTED ON BOTH FORWARD AND AFT LOWER EDGES. REPAIRED IAW HORIZON AIR EA 4-53-844. 2 L 7 2 4F RT A20EU 1999082100028 19990821 00028 EU 1999 8 21 QXEA9901505 1 19990710 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU CARGO COMPT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FLOOR FRAME 9305 TOP ANGLE UNDERSIDE HAS CORROSION AROUND NUT PLATE AT 4 WAY GILLINER SUPPORT AB OVE STRINGER 1. REPAIRED IAW FOKKER SRM 51-11-05 AND 51-10-4. 2 L 7 2 4F RT A20EU 1999082100029 19990821 00029 EU 1999 8 21 QXEA9901506 1 19990710 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FLOOR FRAME 9305 TOP ANGLE, UNDERSIDE HAS CORROSION ON AND AROUND GILLINER NUT PLATE ABOVE STRIN GER 2. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999082100030 19990821 00030 EU 1999 8 21 QXEA9901507 1 19990710 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FLOOR FRAME 9305B TOP ANGLE UNDERSIDE HAS CORROSION AROUND NUT PLATES AND ANGLE AT 4 WAY GILLINE R SUPPORT NEAR STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-05 AND 51-10-4. 2 L 7 2 4F RT A20EU 1999082100031 19990821 00031 EU 1999 8 21 QXEA9901508 1 19990711 A 5321 FLOOR FOKKER F28 F28MK4000 4990810 EU FRAME 9305-9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FLOOR SKIN HAS CORROSION AROUND ANTENNA OPENING BETWEEN FLOOR FRAME 9305C AND 9805 AND BETWEEN S TRINGER 1 AND 74. ALSO, THERE IS CORROSION ON ANTENNA MOUNT NUT PLATES. REPAIRED IAW FOKKER SRM 51-10-4, PAGES 8 AND 9 AND PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999082100032 19990821 00032 EU 1999 8 21 QXEA9901509 1 19990710 A 5320 HOUSING FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FLOOR DRAIN TRAP HOUSING HAS CORROSION ON IT AND UNDER IT NEAR FRAME 9305C AND BETWEEN STRINGER 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999082100033 19990821 00033 EU 1999 8 21 QXEA9901510 1 19990710 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FLOOR FRAME 9305 LOWER FRAME ANGLE HAS CORROSION ON IT BETWEEN STRINGER 2 AND 74. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999082100034 19990821 00034 EU 1999 8 21 QXEA9901511 1 19990710 A 5320 HOUSING FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FLOOR DRAIN TRAP HOUSING HAS CORROSION ON IT NEAR FRAME 9305 AND BETWEEN STRINGER 1 AND 74. REP AIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999082100035 19990821 00035 EU 1999 8 21 QXEA9901512 1 19990709 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY CENTER CARGO DOOR APERTURE IS DENTED ON AFT SIDE OF DOOR APERTURE. REPAIRED IAW FOKKER SRM 53-0 2-16, PAGE 3, SECTION C-C, FIGURE 1. 2 L 7 2 4F RT A20EU 1999082100036 19990821 00036 EU 1999 8 21 QXEA9901513 1 19990716 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO COMPARTMENT FORWARD DOOR INNER SHELL SKIN HAS NUMEROUS DENTS. REPAIRED IAW HORIZON AIR EA 4-52-247. 2 L 7 2 4F RT A20EU 1999082100037 19990821 00037 EU 1999 8 21 QXEA9901514 1 19990720 A 5230 LATCH FOKKER F28 F28MK4000 4990810 EU CARGO DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - FORWARD CARGO BAY FORWARD CARGO DOOR LATCH HOOK ON AFT END HAS APPROXIMATELY .015 RADIAL PLAY AT LEVER TO HOOK PIN . REPAIRED IAW OVERHAUL MANUAL 20-30-14, PAGE 203, PARAGRAPH 4 AND PAGE 205, PARAGRAPH 6. 2 L 7 2 4F RT A20EU 1999082100038 19990821 00038 EU 1999 8 21 QXEA9901515 1 19990715 A 3213 AXEL FOKKER F28 F28MK4000 4990810 EU LT MLG WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - LEFT MAIN LANDING GEAR AXLE LEFT SIDE, OUTER PLATING IS CHIPPED OFF OUTBOARD UPPER FORWARD EDGE. REPAIRED IAW HOR IZON AIR EA 4-32-139. 2 L 7 2 4F RT A20EU 1999082100039 19990821 00039 EU 1999 8 21 QXEA9901516 1 19990713 A 5710 STRUCTURE FOKKER F28 F28MK4000 4990810 EU LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - LEFT LOWER WING MAIN LANDING GEAR OUTBOARD DOOR CUTOUT HAS TWO DEEP CHAFFED AREAS AT AFT SIDE APPROXIMATELY STATIO N 1800. REPAIRED IAW HORIZON AIR EA 4-57-296. 2 L 7 2 4F RT A20EU 1999082100040 19990821 00040 EU 1999 8 21 QXEA9901517 1 19990716 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 169.3 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - SUSPECT CRACK AT FORWARD LEFT FUSELAGE SKIN UNDER MAIN CABIN DOOR APPROXIMATELY STATION 169.3 ALONG STRINGER 8. R EPAIRED IAW HORIZON AIR EA 4-53-833. 2 L 7 2 4F RT A20EU 1999082100041 19990821 00041 EU 1999 8 21 QXEA9901518 1 19990714 A 5720 STRUT FOKKER F28 F28MK4000 4990810 EU LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 490US 11152 PDX - LEFT STUBWING ENGINE THRUST STRUT IS CHAFFED ON TOP ABOUT MID POINT BY THE FORWARD BLEED AIR LINE. REPAIRED IAW H ORIZON AIR EA 4-71-128. 2 L 7 2 4F RT A20EU 1999082100042 19990821 00042 NM 1999 8 21 DLM90991706 1 19990729 A 2420 CONVERTOR 1B1893 DOUG MD90 MD9030 3023690 NM LEFT FAILED A DALA K NONE H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 907DA 2700288 53387 L AC PWR FAULT AND L GEN OFF MSG ON OAP. APU IS ON MCO/PLAC. PER EPCU BITE, REPLACED LEFT A/C CONVERTER. OPS CKS NORM AL. 2 L 7 2 4F RT A6WE 1999082100043 19990821 00043 NM 1999 8 21 DLM90991709 1 19990729 A 3397 WIRE DOUG MD90 MD9030 3023690 NM CEILING BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902DA 53382 EMERGENCY LIGHTING CEILING INOP. FOUND BROKEN WIRES IN CEILING REPAIRED WIRES. OPS NORMAL. 2 L 7 2 4F RT A6WE 1999082100044 19990821 00044 NE 1999 8 21 DL757991717 2 19990731 A 7261 FILTER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 SO 27 665DN 29824 25013 716549 CREW CALLED WITH LEFT ENGINE OIL QTY READING ZERO. APPROX 5 MINUTES LATER, PRESSURE STARTED FLUCTUATING PLUS OR MINUS 1 0 PSI. CREW ELECTED TO SHUT ENGINE DOWN. ENGINE WINDMILLED FOR APPROX 10 MINUTES. MAINTENANCE FOUND THE MAIN ENGINE O IL FILTER O-RING CUT. REPLACED FILTER AND SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1999082100045 19990821 00045 NM 1999 8 21 99FDEA00303 1 19990803 A 2933 B7111 INDICATOR BOEING 727 727233 138408A NM P4 PANEL INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 277FE 22042 99-187 - HYD SYS A QUANTITY WENT TO ZERO WHEN LANDING GEAR HANDLE WAS PLACED TO UP. RAN RED TABS. REPLACED BROKEN INDI CATOR, SYSTEM HYD OIL QUANTITY PER 727 MM 29-33-000. COCKPIT IND NOW MATCHES TANK IND. REMOVED PLACARD. 2 L 7 3 4F RT A3WE 1999082100048 19990821 00048 EU 1999 8 21 RAIA990719 1 19990715 A 7722 31050491 EGT HARNESS JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 574HK 41093 STL - FLT 7176 - RIGHT ENGINE EGT WENT TO 640 DEGREES, VARIABLE RED LINE WAS 563 DEGREES. MAINTENANCE REPLACED EGT HARN ESS ON RIGHT ENGINE. DETERMINED TO BE INDICATION PROBLEM. ENGINE WAS NOT OVER TEMPED. 2 L 7 2 4T RT A41NM 1999082100049 19990821 00049 NM 1999 8 21 TWAA9911003 1 19990809 A 3350 251005 FUSE BOEING 767 7673Y0 NM CABIN BLOWN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 FOUND THE EGRESS LIGHTS INOPERATIVE AFT OF THE NUMBER 1 RT SIDE CABIN DOOR TO THE FIRST SEAT ROW, BETWEEN THE LT NUMBER 1 DOOR AND THE RT NUMBER 1 DOOR, AND ON THE LT SIDE FROM ROWS 32 TO 43. RECONNECTED LOOSE TERMINAL AT LIGHT ASSEMBLY FO R THE RT SIDE ROW ONE MALFUNCTION. REPLACED THE JUMPER CABLE MFG S417N509-1 BETWEEN THE L1 AND R1 CABIN DOORS, AND REPL ACED A BLOWN FUSE FOR THE LT SIDE ROW 32 TO 43. CHECK-C 7-14-99 LAX. 2 L 7 2 4F RT A1NM 1999082100054 19990821 00054 CE 1999 8 21 99ZZZX2960 1 19990727 A 3250 SWITCH CESSNA 650 650 2076802 CE NLG OUT OF ADJUST A DBCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 25SD 6500099 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. PILOT FLEW TO HOME BASE WITHOUT INCIDENT. RAN GEAR RETRACT TEST. ADJUS TED NOSE GEAR CENTERING SWITCH. FLIGHT TEST OK. 2 L 7 2 4F A9NM 1999082100055 19990821 00055 NM 1999 8 21 CALA9901039 1 19990722 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14358 23943 INSPECTION FOUND CABIN FLOORBEAM CORRODED ON UPPER CHORD LOWER SURFACE FORWARD AND AFT OF STA 986.5, RBL 25-35. REPAIRE D IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999082100056 19990821 00056 NM 1999 8 21 DLM90991781 1 19990809 A 2421 GENERATOR 1B1893 DOUG MD90 MD9030 3023690 NM RT ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 27 905DA 036C0164 53385 RT GEN FAILED DURING INITIAL TAKEOFF ROLL AT 70KTS OAP MESSAGE RT ELEC SYSTEM FAIL. EPCU FAULTS CEU. REPLACED CEU RAN ENGINE. A/C POWER SYSTEM CHECK GOOD. 2 L 7 2 4F RT A6WE 1999082100057 19990821 00057 NE 1999 8 21 CALA9901042 2 19990807 A 7200 ENGINE BOEING 777 777224 1385225 NM GE GE90 GE9092B 30036 NE NR 1 FAILED A CALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SW 09 77012 29860 NR 1 ENG FLAME-OUT ON DESCENT, ENG RESTART UNSUCCESSFUL. MX R & R THE HMU & EEC. ENG BOROSCOPE WAS PERFORMED, NO TROUB LE FOUND. FUEL STRAINER & MAIN FUEL FILTER REMOVED & INSPECTED, CHECKED GOOD. A FUEL SAMPLE SUBMITTED TO BOEING. TEST FLIGHT WAS CONDUCTED. FUEL SAMPLE ANALYSIS DID NOT DISCLOSE ANY ABNORMALITIES. HMU WAS TESTED & DISASSEMBLED AT THE V ENDOR FACILITY & NO DISCREPANCIES FOUND. EEC WAS SENT TO THE VENDOR FOR TESTING & RETRIEVAL OF NVM, NO DISCREPANCIES NO TED. THE QAR/ACMF DATA WAS STUDIED IN DETAIL WITH INCONCLUSIVE RESULTS. THE CAUSE FOR DISCREPANCY IS NOT UNDERSTOOD. B OEING IS CONSIDERING ADDING ADDITIONAL SIGNALS TO THE DFDR AND QAR SYSTEMS. 2 L 7 2 4F 4 F RT T00001SE E00049EN 1999082600001 19990826 00001 NM 1999 8 26 UIEA9936 1 19990628 A 5320 SUPPORT BOEING 747 747271C 1384869 NM BS 1920 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 CRACK MAIN DECK RIGHT SIDE SUPPORT POST FRAME AT BS 1920 LENGTH 140 MM. REPAIRED BOEING TLS BKK 99-0075TE. REF: SRM 5 3-10-07, FIG 7. (X) 2 L 7 4 4F A20WE 1999082600002 19990826 00002 WP 1999 8 26 MWEA99416 1 19990723 A 5230 3914025502N FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 AFT CARGO DOOR FITTING CRACKED AT ONE HI-LOK HOLE 2ND BEAM FROM BOTTOM FORWARD END. INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999082700001 19990827 00001 WP 1999 8 27 TWAA9911301 1 19990816 A 2740 95906 MOTOR DOUG DC9 DC941 302207N WP PRIMARY TRIM FAILED A TWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 05 935L 47603 LONGITUDINAL TRIM CONTROL WHEEL AND SUITCASE HANDLES INOP. REMOVED AND REPLACED LONGITUDINAL PRIMARY TRIM MOTOR TWA STK NR 80374. OPERATIONAL CHECK WAS NORMAL. CHECK C 9-28-98 STL. 2 L 7 2 4F A6WE 1999082700002 19990827 00002 WP 1999 8 27 TWAA9911302 1 19990811 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-198 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, THE CABIN O/B FLOOR SUPPORT RAIL WAS CORRODED AT STA 160 TO 198 AT FWD GALLEY DOOR. REMOVED T HE CORROSION BY REPLACEMENT OF THE PART PER SPM 6-70-01, SEALED AND USED 5/32 AD RIVETS. 2 L 7 2 4F A6WE 1999082700003 19990827 00003 WP 1999 8 27 TWAA9911303 1 19990813 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1309 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT TRACK SUPPORT INTERCOSTAL CRACKED AND CORRODED AT STA 1309, LONGERON 27R TO 28R. REMOVED INTERCOSTAL AND REPLACED PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999082700004 19990827 00004 WP 1999 8 27 TWAA9911304 1 19990811 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 198 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 951U 49245 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AT STA 198, RBL 9 TO RBL44. FABRICATED ANGLE FROM 7075 T-6 PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999082700005 19990827 00005 1999 8 27 JBXA9900099 4 19990819 A 3418 COMPUTER FOKKER F28 F28MK0100 4990807 EU E & E COMPT MALFUNCTIONED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 104ML 11445 FLT 79 RDU/LGA- ON CLIMBOUT HAD STALL COMPUTER WARNING ASSOCIATED WITH MULTIPLE FAULTS ON RT MFDU. AIR RETURN TO RDU. PERFORMED OPERATIONAL CHECK OF STALL WARNING SYSTEM IAW 27-35-00. NO FAULTS NOTED. UPON ARRIVAL TO AICRAFT NO FAULTS INDICATIED. 2 L 7 2 4F RT 1999082700006 19990827 00006 WP 1999 8 27 IXXA9900020 1 19990813 A 5730 PLATING DOUG DC8 DC871F 302199D WP WS 323 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 821BX 45811 DURING A SCHEDULED HEAVY MAINTENANCE VISIT, A CRACK WAS DETECTED ON THE RIGHT WING LOWER EXTERNAL PLATING AT WING STATIO N XRS323, BETWEEN STRINGER 62 AND 63. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL REPAIR FILLER, EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING SK99526 AND DOUGLAS STRUCTUR AL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 1999082700007 19990827 00007 NM 1999 8 27 AWXA9900260 1 19990813 A 5751 65C25916 SPAR BOEING 737 737301 1384611 NM RT AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, RT AILERON FRONT SPAR LOWER FLANGE DELAMINATED AT I/B HINGE AND I/B CLOSING RIB. RT AILERON REMOVED PER J/C R3 M27015, REPAIRED PER ER3-57-51-17A, BALANCE CHECKED AND REINSTALLED PER J/C R3M27015. FUNCTIONAL CHECKED GOOD PER J/C R 3M27015. 2 L 7 2 4F RT A16WE 1999082700008 19990827 00008 EU 1999 8 27 AWXA9900261 1 19990816 A 2760 31077111 SERVO CONTROL AIRBUS 320 A320231 3930325 EU RT SPOILER LEAKED A AWXA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 633AW 082 DECLARED EMERGENCY, DURING DESCENT ECAM MSG FLT CTRL/SPLR 2 FAULT. YELLOW SYS HYDRAULIC FLUID LOST REF LOG PGS 7422514 & 515 (NO CURRENT RELATED HISTORY 90 DAYS). REPLACED NR 2 RT SPOILER ACTUATOR / SERVO CONTROL PER AMM 27-64-51-401. SE RVICED, LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 1999082700009 19990827 00009 NM 1999 8 27 AWXA9900262 1 19990816 A 2820 CHECK VALVE BOEING 737 7373Y0 1384671 NM CENTER FUEL TANK FAILED A AWXA J DUMP FUEL K FLUID LOSS CL CLIMB 1 WP 28 329AW 23500 DIVERSION AFTER TAKEOFF, FUEL VENTING WITH IMBALANCE REF LOG PG 7422732 / 735. SJC TOWER ADVISED AFTER DEPARTURE LIQUI D VAPOR COMING FROM LT WING TIP. FUEL IMBAL 1200 LBS WITHIN 10 BALANCED FUEL. REPLACED CENTER TANK SCAVENGE FLOW INDIC ATOR CK VLV AND APU FEED LINE THERMAL RELIEF VALVE. 2 L 7 2 4F RT A16WE 1999082700010 19990827 00010 EU 1999 8 27 AWXA9900263 1 19990816 A 4920 38002784 APU AIRBUS 320 A320231 3930325 EU APU COMPARTMENT FAILED A AWXA O OTHER L NO TEST TX TAXI/GRND HDL 1 WP 28 635AW 24458 24458 092 OIL SMELL IN CABIN VENTS. REPLACED AUX POWER UNIT. 2 L 7 2 4F RT A28NM 1999082700011 19990827 00011 NM 1999 8 27 AWXA9900264 1 19990817 A 3233 6545819 SUPPORT BOEING 737 737301 1384611 NM NLG ACTUATOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, CRACKED NLG ACTUATOR SUPPORT BEAM VERTICAL WEB AT FWD END. REMOVED AND REPLACED WEB PER DWG 65-45819. 2 L 7 2 4F RT A16WE 1999082700012 19990827 00012 NM 1999 8 27 AWXA9900265 1 19990817 A 5754 6546431279 SKIN BOEING 737 737301 1384611 NM LT TE FOREFLAP WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, WEAR MARK IN UPPER SURFACE OF LT O/B FOREFLAP MID SECTION. REMOVED FOREFLAP, REPAIRED PER ER 3-57-52-162, REIN STALLED FOREFLAP AND OPERATIONALLY CHECKED OK PER AWA T/C R3M27002. 2 L 7 2 4F RT A16WE 1999082700013 19990827 00013 NM 1999 8 27 AWXA9900266 1 19990817 A 5751 65C25916 SKIN BOEING 737 737301 1384611 NM LT AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, FWD LOWER SPAR FLANGE DELAMINATED AND DAMAGED IN 3 SPOTS ON LT AILERON. REPAIRED PER AWA ER 3-57-51-17A. 2 L 7 2 4F RT A16WE 1999082700014 19990827 00014 NM 1999 8 27 AWXA9900267 1 19990817 A 5330 SKIN BOEING 737 737301 1384611 NM CARGO DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, FUSELAGE SKIN DOUBLER/TRIPLER CRACKED AT C2 DOOR CUTOUT, FWD LOWER CORNER. FASTENERS REMOVED FOR ACCESS, SUSPE CT AREA INSPECTED WITH HIGH FREQ EDDY CURRENT. NO CRACKS FOUND. NEW DOUBLER REPAIR MANUFACTURED AND INSTALLED AS PER E R 3-53-36-08. PRESSURIZED AT 4 PSIG TO LEAK CHECK. NO LEAKS FOUND. 2 L 7 2 4F RT A16WE 1999082700015 19990827 00015 NM 1999 8 27 QXEA9901647 1 19990816 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 348PH 484 SEA- SEVERAL EMERGENCY AISLE PROXIMITY LIGHTS OUT. REPAIRED BROKEN PIN TO PROXIMITY LIGHT P-4. OPERATIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999082700016 19990827 00016 NM 1999 8 27 QXEA9901648 1 19990812 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 SEA- MAIN CABIN DOOR HARD TO OPEN FROM INSIDE. CLEANED MAIN CABIN DOOR SEAL AND DOOR LOCKING/UNLOCKING LEVERS. OPERATI ONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999082700017 19990827 00017 WP 1999 8 27 99FDEA00340 1 19990818 A 5530 AJC7054501 FITTING DOUG DC10 DC1010F 3022111 WP VERT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 056FE 47810 VERTICAL STAB REAR SPAR (P/N AJC7054-501) BANJO FITTING HAS CRACK IND APPROX 4.5 AFT TANG LWR SURFACE ALONG THE RADIUS. *S/D* REPAIRED IAW EO 8-5430-7-2302 PT 2. 2 L 7 3 4F A22WE 1999082700018 19990827 00018 NM 1999 8 27 99FDEA00341 1 19990819 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 MAIN DECK UPPER FUSELAGE, SEAT TRACK FOUND CRACK AT BS 635 X = 8.5 RT. CRACK LENGTH APPROX 3.4 IN. *S/D* REPAIRED AND INSTALLED PARTS, FABRICATED PER SRM 53-70-00 FIG 1 VOL. 2 L 7 3 4F RT A22WE 1999082700019 19990827 00019 WP 1999 8 27 ABXA9900648 1 19990818 A 5320 991015529 DOUBLER DOUG DOUG DC9 DC931 3022065 WP BS 718 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND DOUBLER FORWARD AND AFT OF STATION 718 CORRODED. REPLACED DOUBLER IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999082700020 19990827 00020 WP 1999 8 27 ABXA9900649 1 19990818 A 5320 991015144 WEB DOUG DOUG DC9 DC931 3022065 WP BS 598 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND CUSP WEB CRACKED FORWARD AND AFT OF FRAME AT STATION 598 RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SR M 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1999082700021 19990827 00021 WP 1999 8 27 ABXA9900650 1 19990818 A 2761 59139005517 ACTUATOR DOUG DC9 DC931 3022065 WP LT SPOILER CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND LEFT OUTBOARD SPOILER ACTUATOR VALVE BODY EXFOLIATED AND VALVE LINK MOUNT AREA CRACKED. REPLACED ACTUATOR IAW ABX EA 2760D019-001. 2 L 7 2 4F A6WE 1999082700022 19990827 00022 NM 1999 8 27 SCNA99714 1 19990727 A 3350 SIGN BOEING 727 7272J4 1384006 NM LT EMER EXIT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, THE LEFT HAND AFT OVERWING EXIT EMERGENCY AND PULL SELF LUMINOUS EXIT SIGNS FAILED INTEN SITY INSPECTION. REMOVED AND REPLACED LEFT HAND AFT OVERWING EMER EXIT AND PULL SELF LUMINOUS EXIT SIGNS IAW MM 335031. 2 L 7 3 4F RT A3WE 1999082700023 19990827 00023 NM 1999 8 27 SCNA99715 1 19990727 A 3350 SIGN BOEING 727 7272J4 1384006 NM RT EMER EXIT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, THE RIGHT HAND FWD OVERWING EXIT PULL SELF LUMINOUS EXIT SIGN FAILED INTENSITY INSPECTIO N. REMOVED AND REPLACED RIGHT HAND FWD OVERWING EMER EXIT PULL SELF LUMINOUS EXIT SIGN IAW MM 335031. 2 L 7 3 4F RT A3WE 1999082700024 19990827 00024 NM 1999 8 27 SCNA99716 1 19990727 A 3350 SIGN BOEING 727 7272J4 1384006 NM RT EMER EXIT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, THE RIGHT HAND AFT OVERWING EXIT EMERGENCY AND PULL SELF LUMINOUS EXIT SIGNS FAILED INTE NSITY INSPECTION. REMOVED AND REPLACED RIGHT HAND AFT OVERWING EXIT EMERGENCY AND PULL SELF LUMINOUS EXIT SIGNS IAW M M 335031. 2 L 7 3 4F RT A3WE 1999082700025 19990827 00025 NM 1999 8 27 SCNA99717 1 19990727 A 3350 SIGN BOEING 727 7272J4 1384006 NM LT EMER EXIT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, THE LEFT HAND FWD OVERWING EXIT EMERGENCY AND PULL SELF LUMINOUS EXIT SIGNS FAILED INTEN SITY INSPECTION. REMOVED AND REPLACED LEFT HAND FWD OVERWING EXIT EMERGENCY AND PULL SELF LUMINOUS EXIT SIGNS IAW MM 335031. 2 L 7 3 4F RT A3WE 1999082700026 19990827 00026 NM 1999 8 27 SCNA99718 1 19990805 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 280 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT STA 280 LEFT HAND AT STR 27L AFT SIDE OF LWR FRAME T IAW B727 SRM 531001. REMOVED T CHORD IAW B727 SRM 513002. TRANSFERRED FASTENER LOCATIONS TO NEW T CHORD IAW SRM 5110 01. FABRICATED STRINGER SPLICE IAW B727 SRM 531003 FROM BAC 1498124 FOR STRINGER 25L. TREATED AND PRIMED IAW B727 SRM 511002. INSTALLED SPLICE IAW B727 SRM 513002. FABRICATED SPLICES FOR STR 26L IAW SRM 514004 FROM BAC 14902734. TREATE D AND PRIMED SPLICE IAW SRM 511002 MM 512002. INSTALLED PER B727 SRM 513002. INSTALLED NEW T 6516312145 IAW 513002 AND 511002 SRM B727. 2 L 7 3 4F RT A3WE 1999082700027 19990827 00027 NM 1999 8 27 SCNA99719 1 19990725 A 5320 SUPPORT BOEING 727 7272J4 1384006 NM BS 294 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS IN THE LOWER NOSE COMPARTMENT STA 294 STR 28R, INSIDE RT FORWARD NOSE LANDING GEAR WALKWAY, FRAME SUPPORT ANGLE ON THE UPPER SURFACE IAW B727 SRM 531001. REMOVED FRAME FORME R IAW B727 SRM 513002. REMOVED CORROSION IAW B727 SRM 511006. CUT STRINGERS 25R AND 26R TO FACILITATE INSTALLATION. F ABRICATED STRINGER SPLICE IAW B727 SRM 531003 FROM BAC 1498124 FOR STRINGER 25R. TREATED AND PRIMED IAW B727 SRM 511002 . INSTALLED SPLICE IAW B727 SRM 513002. FAB SPLICES FOR STR 26R FROM BAC 14902734 IAW SRM 514004. TREATED AND PRIMED SPLICE IAW B727 SRM 511002, MM 512002. INSTALLED NEW T 6516312146 IAW SRM 513002 AND 511013. 2 L 7 3 4F RT A3WE 1999082700028 19990827 00028 NM 1999 8 27 9903212713 1 19990706 A 5320 SPLICE BOEING 727 7272S7 138407Z NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 716RC 22021 DURING M-CHECK, FOUND KEEL BEAM SPLICE COULD NOT MEET ULTIMATE STATIC CAPABILITIES. REPAIRED PER EA 27-167886 (P/N 65-5 6441-6). 2 L 7 3 4F A3WE 1999082700029 19990827 00029 NM 1999 8 27 9903222201 1 19990615 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 380 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 201US 22154 DURING M-CHECK, CORROSION WAS FOUND ON THE UPPER CHORD OF FS 380 FLOORBEAM RBL 22-26 AND RBL 52-70. REPAIRED PER EA 22- 167882 (P/N 65-20826-16). 2 L 7 3 4F A3WE 1999082700030 19990827 00030 NM 1999 8 27 9903232201 1 19990618 A 5314 KEEL BEAM BOEING 727 727251 138408H NM BS 984 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 201US 22154 DURING M-CHECK, CORROSION WAS FOUND ON THE LEFT KEEL BEAM AT FS 984. REPAIRED KEEL BEAM PER EA 22-167879 (P/N 65-56441- 5). 2 L 7 3 4F A3WE 1999082700031 19990827 00031 WP 1999 8 27 9903241152 1 19990722 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 420-460 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING M-CHECK, FOUND CORROSION ON ANGLE FITTING FROM FS 420 - 460. REPAIRED PER EA 11-168628. 2 L 7 3 4F A22WE 1999082700032 19990827 00032 WP 1999 8 27 9903259750 1 19990708 A 5312 BULKHEAD CHANNEL DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 750NW 47114 DURING PERIODIC CHECK, AFT PRESSURE BULKHEAD SILL CHANNEL WAS FOUND WITH 2 INCH CRACK FROM FASTENER TO LIP OF FLANGE AT FLOOR. REPAIRED PER EA 97-164468 (P/N 5910130-37). 2 L 7 2 4F A6WE 1999082700033 19990827 00033 WP 1999 8 27 9903269912 1 19990721 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 237 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING PERIODIC CHECK, A CRACK WAS FOUND IN THE VERTICAL WEB OF FS 237 FLOORBEAM. REPAIRED PER EA 99-164486. 2 L 7 2 4F A6WE 1999082700034 19990827 00034 WP 1999 8 27 9903279913 1 19990720 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 617 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING PERIODIC CHECK, FOUND TWO CRACKS ON SEAT TRACK FITTING FS 617. REPAIRED PER EA 99-164490 (P/N 3916212-502). 2 L 7 2 4F A6WE 1999082700035 19990827 00035 WP 1999 8 27 9903289912 1 19990719 A 5310 STRUCTURE DOUG DC9 DC931 3022065 WP BS 110 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING PERIODIC CHECK, CORROSION WAS FOUND AT T FS 110 STR 26L - 27L LEFT SIDE. REPAIRED PER EA 99-168919. 2 L 7 2 4F A6WE 1999082700036 19990827 00036 WP 1999 8 27 9903299912 1 19990719 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING PERIODIC CHECK, FOUND AFT CARGO BULKHEAD WEB CORRODED BEYOND ACCEPTABLE LIMITS, FS 996 LONGERON 26L TO 26R. REPA IRED PER EA 99-168917. 2 L 7 2 4F A6WE 1999082700037 19990827 00037 WP 1999 8 27 9903309913 1 19990719 A 5312 BULKHEAD JAMB DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING PERIODIC CHECK, CRACK WAS FOUND ON AFT PRESSURE BULKHEAD LEFT UPPER DOOR JAMB. REPAIRED PER EA 99-164509 (P/N 59 17463-503). 2 L 7 2 4F A6WE 1999082700038 19990827 00038 1999 8 27 COMA9910135 4 19990817 A 3418 BULB EMB 120 EMB120RT SO NR 2 STALL IND FAILED A COMA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 01 256CA 120245 STALL WARNING LIGHT ILLUMINATED. REPLACED THE NR 2 STALL PANEL LIGHT BULB. 2 L 7 2 4T RT A31SO 1999082700039 19990827 00039 EA 1999 8 27 COMA9960455 1 19990817 A 2120 AIR DIST CNDAIR CL600 CL6002B19 EA COCKPIT ODOR A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 979CA 7159 STRONG BURNING SMELL IN COCKPIT. CLEANED RESIDUAL, COMPRESSOR WAS HOT FROM AIRCRAFT SYSTEM. 2 L 7 2 4F RT A21EA 1999082700040 19990827 00040 EA 1999 8 27 COMA9960456 1 19990817 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA K NONE J WARNING INDICATION LD LANDING 1 SO 01 965CA 7131 FLAPS FAILED AFTER LANDING. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999082700041 19990827 00041 NM 1999 8 27 UPS99230364 1 19990805 A 5754 65172807 RIB BOEING 727 7271A7C 13840X2 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C WHILE WORKING CUSTOMER CARD #934321 FOUND CRACKED RIB IN NR 4 SLAT, 3RD RIB I/B OF O/B SLAT TRACK WHER E RIB ATTACHES TO LOWER AFT CHORD. REMOVED CRACKED RIB AND INSTALLED NEW RIB PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999082700042 19990827 00042 WP 1999 8 27 UPS99830333 1 19990816 A 5610 5613217519 WINDOW DOUG DC8 DC873F 302199F WP CABIN FAILED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:N/A, CAPTINS CLEARVIEW SIDE WINDOW ARCING. REMOVED AND REPLACED CAPTAINS CLEARVIEW WINDOW IAW MM 56-10- 03. TEST ED PER 56-10-03. SYSTEM OPS CK NORMAL. 2 L 7 4 4F RT 4A25 1999082700043 19990827 00043 WP 1999 8 27 UPS99830334 1 19990813 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1600 & 1620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A, FOUND FLOORBEAM CRACKS AT STA 1600 AND 1620. *S/D* REPAIR COMPLETED ON FLOORBEAM. 2 L 7 4 4F RT 4A25 1999082700044 19990827 00044 WP 1999 8 27 UPS99830337 1 19990803 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 518 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, LT WING L/E UPPER SKIN AT XS 518 IS CRACKED AT 1 SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999082700045 19990827 00045 WP 1999 8 27 UPS99830338 1 19990804 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, RT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 1999082700046 19990827 00046 WP 1999 8 27 UPS99830340 1 19990804 A 5720 576960036 DOUBLER DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, RT WING L/E LWR INTERNAL SKIN DOUBLER AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATE D AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1999082700047 19990827 00047 WP 1999 8 27 UPS99830342 1 19990805 A 5320 37739061 FITTING DOUG DC8 DC873F 302199F WP BS 798 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, FS 798 FLOORBEAM AT RBL 24, THE FLOORBEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTI NG IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999082700048 19990827 00048 WP 1999 8 27 UPS99830343 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 791.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, LT WING L/E RIB AT XFS 791.25 IS CRACKED AT THE AFT LWR END. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700049 19990827 00049 WP 1999 8 27 UPS99830344 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, LT WING L/E RIB AT XFS 785.0 IS CRACKED AT THE AFT LWR FASTENER. REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700050 19990827 00050 WP 1999 8 27 UPS99830345 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, LT WING L/E RIB AT XFS 778.75 IS CRACKED AT THE AFT LWR FASTENER. REPAIRED RIB IAW SRM 57-2-0 FIG 2 . 2 L 7 4 4F RT 4A25 1999082700051 19990827 00051 WP 1999 8 27 UPS99830346 1 19990806 A 5720 576960040 DOUBLER DOUG DC8 DC873F 302199F WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 572.5 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATE D AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1999082700052 19990827 00052 WP 1999 8 27 UPS99830347 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, RT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED AND REPAIRED CRACK I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700053 19990827 00053 WP 1999 8 27 UPS99830348 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C1, RT WING L/E RIB AT 622.5 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700054 19990827 00054 WP 1999 8 27 UPS99830349 1 19990816 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 1620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:SV, CORROSION BETWEEN SKIN AND DOUBLER FS 1620 L26R DOT E253. REMOVED CORROSION, FABRICATED AND INSTALL ED REPAIR IAW UPS DC8 SRM 53-4 -1, 53-2-1 FIG 7, 51-120D. 2 L 7 4 4F RT 4A25 1999082700055 19990827 00055 WP 1999 8 27 UPS99830350 1 19990813 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C123, CORROSION FLOORBEAM FS 1600 RT. REPAIRED IAW REO-06679, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700056 19990827 00056 WP 1999 8 27 UPS99830360 1 19990805 A 5320 37532351 FITTING DOUG DC8 DC873F 302199F WP BS 980-988 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS 980 TO 988, THE LONG 22L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 3753235 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700057 19990827 00057 WP 1999 8 27 UPS99830361 1 19990805 A 5320 3755847501 FITTING DOUG DC8 DC873F 302199F WP BS 1152 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS 1152 BETWEEN LONG 32R AND 33R, THE FRAME TO SKIN TIE FITTING IS CRACKED. REMOVED, FABRICATED A ND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700058 19990827 00058 WP 1999 8 27 UPS99830362 1 19990806 A 5720 37048411 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, STA XRS 74 BULKHEAD, O/B SIDE, THE STR 51 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING SR M 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999082700059 19990827 00059 WP 1999 8 27 UPS99830363 1 19990807 A 5320 561229875 DOUBLER DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS -32 TO -50.6, LBL 16 TO 25, THE FINGER DOUBLER HAS SEVERAL RIVET HEAD SHEARED DUE TO CORROSION. REMOVED, FABRICATED AND REPLACED THE FINGER DOUBLER IAW DWG 5612298 AND SRM 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700060 19990827 00060 WP 1999 8 27 UPS99830366 1 19990810 A 5320 3755847501 FITTING DOUG DC8 DC873F 302199F WP BS 1155 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, FS 1155 AT LONG 32R, THE ANGLE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700061 19990827 00061 WP 1999 8 27 MWEA99508 1 19990817 A 5347 591014323 SEAT TRACK DOUG DC9 DC914 3022034 WP BS 227 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 NR 4 SEAT TRACK AT STATION 227 TO 236 HAS HEABY CORROSION. MTC FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2 L 7 2 4F A6WE 1999082700062 19990827 00062 WP 1999 8 27 MWEA99509 1 19990817 A 5347 59101565 SEAT TRACK DOUG DC9 DC914 3022034 WP BS 601 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 NR 3 SEAT TRACK AT STATION 601 HAS CRACKED TABS. MTC FABRICATED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 1999082700063 19990827 00063 WP 1999 8 27 MWEA99510 1 19990817 A 5320 99576762 INTERCOSTAL DOUG DC9 DC914 3022034 WP FUSELAGE MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 600ME 45725 INTERCOSTAL AT LONGERON 8R STATION 465 TO 484, 389 TO 409, AND 313 TO 332 HAVE HOLES. MTC FABRICATED AND INSTALLED REPA IR DOUBLERS. 2 L 7 2 4F A6WE 1999082700064 19990827 00064 WP 1999 8 27 MWEA99511 1 19990817 A 5347 59101565 SEAT TRACK DOUG DC9 DC914 3022034 WP BS 717 & 721 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 TOOL MARKS ON NR 1 SEAT TRACK AT STATION 717 AND NR 2 SEAT TRACK AT STATION 721. MTC FABRICATED AND INSTALLED REPAIR PL UG. 2 L 7 2 4F A6WE 1999082700065 19990827 00065 WP 1999 8 27 MWEA99512 1 19990817 A 5320 591014249N JAMB DOUG DC9 DC914 3022034 WP CARGO DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FORWARD CARGO DOOR JAMB HAS CRACK BETWEEN TWO FASTENERS AT STATION 324. MTC FABRICATED AND INSTALLED NEW JAMB. 2 L 7 2 4F A6WE 1999082700066 19990827 00066 NM 1999 8 27 MWEA99513 1 19990819 A 2560 D29985107 SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 AFT GALLEY DOOR SLIDE AND COVER LOOSE. REINSTALLED AFT GALLEY DOOR SLIDE. 2 L 7 2 4F RT A6WE 1999082700067 19990827 00067 NM 1999 8 27 DLM88991822 1 19990815 A 2410 CSD 976J2528 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 974DL PK6752 53242 725754 RT GEN DROPPED OFF LINE/AC X-TIE LOCKOUT/SPARKS REPORTED COMING FROM UNDERSIDE OF ENG. REPLACED CSD/GEN AND GCU. 2 L 7 2 4F 4 F RT A6WE E9NE 1999082700068 19990827 00068 NM 1999 8 27 DL72S991824 1 19990713 A 5753 652163362 SKIN BOEING 727 727232 1384082 NM NR 4 TE MIDFLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 DURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END OF THE FLAP. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FILLER PER 727 MM 57-52-0, FOG 803. 2 L 7 3 4F A3WE 1999082700069 19990827 00069 NM 1999 8 27 DL76L991825 1 19990817 A 2781 INDICATOR BOEING 767 767332 1382001 NM LE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 179DN 25144 AIR TURNBACK DUE TO L/E SLAT ASYMMETRY LIGHT AND INDICATOR NEEDLES BETWEEN 0 AND 1. CHECKED FSEU, NO FAULTS. CYCLED FLAPS AND RAN FLAPS ELEC, NO PROBLEMS. 2 L 7 2 4F RT A1NM 1999082700070 19990827 00070 NM 1999 8 27 DLM88991826 1 19990817 A 7830 CONTROL MODULE 0711346003 DOUG MD88 MD88 3023688 NM LT TR UNIT CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 944DL 481A 49817 LEFT HYD QUANTITY FELL TO 2 QTS IN FLIGHT. FOUND LEFT REVERSER CONTROL MODULE HOUSING CRACKED. REPLACED SAME. 2 L 7 2 4F RT A6WE 1999082700071 19990827 00071 NM 1999 8 27 DLM11991827 1 19990816 A 2120 AIR DIST DOUG MD11 MD11 3023602 NM COCKPIT ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 814DE 48769 ON DESCENT, VERY LITE BURNING ELECTRICAL ODOR FILLED COCKPIT AREA. SMELL APPEARS TO BE COMING FROM GLARESHIELD AREA. G LARESHIELD LIGHTS WERE TURNED OFF AND ODOR DISSIPATED BY LANDING. INSPECTED AND OPERATED ALL LIGHTS, FANS, DISPLAYS ETC IN AND AROUND GLARESHIELD AND INSTRUMENT PANEL. UNABLE TO IDENTIFY ODOR SOURCE OR DUPLICATE CONDITION. 2 L 7 3 4F RT A22WE 1999082700072 19990827 00072 WP 1999 8 27 DLL19991828 1 19990812 A 5712 1527033 RIB LKHEED 1011 10113853 5265020 WP WS 555 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 765DA 193H1206 LT AND RT WING UPPER RIB CAP AT IWS 555 FOUND CRACKED DURING ROUTINE INSPECTION ERA 333431-14 REV B. 2 L 7 3 4F A23WE 1999082700073 19990827 00073 NM 1999 8 27 DL72L991829 1 19990616 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE MID FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 NR 2 MID FLAP AFT LWR SPAR CAP, REPAIR CRACKED 36 FROM I /B END. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1999082700074 19990827 00074 NM 1999 8 27 DL733991830 1 19990817 A 5312 65163007 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311WA 23597 DURING HMV, THE FS 178 BULKHEAD WAS FOUND TO HAVE 7 CRACKS IN THE PRESSURE WEB. THIS DAMAGE WAS REPAIRED PER ERA 33345 0-14. 2 L 7 2 4F RT A16WE 1999082700075 19990827 00075 NM 1999 8 27 DL72L991831 1 19990616 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 T/E WEDGE LWR SKIN CRACKED 36 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 809. 2 L 7 3 4F A3WE 1999082700076 19990827 00076 NM 1999 8 27 DL733991832 1 19990817 A 5330 65458001000 SKIN BOEING 737 737347 1384647 NM BS 207 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311WA 23597 DURING HMV, DAMAGE WAS DISCOVERED TO THE FUSELAGE SKIN AT FS 207 BETWEEN STRINGERS 19R AND 24R. THIS DAMAGE WAS REPAIRE D PER ERA 333452-14. 2 L 7 2 4F RT A16WE 1999082700077 19990827 00077 NM 1999 8 27 DL72L991833 1 19990616 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 LWR AFT SPAR CAP PANEL ATTACH HOLE ELONGATED 55 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802 NON SHOP ORDER 791453. 2 L 7 3 4F A3WE 1999082700078 19990827 00078 NM 1999 8 27 DL72W991834 1 19990817 A 5230 6557204520 BEAM BOEING 727 727247 138408F NM CARGO DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 C2 DOOR / UPPER PRESSURE BEAM, THE UPPER PRESSURE BEAM WAS FOUND DAMAGED DUE TO GROUND HANDLING AT THE AFT PRESSURE STOP FITTING ATTACH LOCATION. AUTHORIZED REPAIR TO TRIM AND REMOVE AFT HALF OF PRESSURE BEAM AND SPLICE-IN REPLACEMENT SECT ION. 2 L 7 3 4F A3WE 1999082700079 19990827 00079 NM 1999 8 27 DLM88991835 1 19990816 A 5312 995301567 BULKHEAD CAP DOUG MD88 MD88 3023688 NM BS 1463 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 996DL 53363 THE OUTER CAP ANGLE OF THE FS 1463 CANTED BULKHEAD WAS FOUND WITH A 1 INCH CRACK IN THE HORIZONTAL SKIN ATTACH FLANGE. T HE ADJACENT SKIN WAS ALSO CRACKED. THE CRACK WAS AT THE LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE LOCATION. TH E ATTACH ANGLE AND VERTICAL STAB SKIN WERE CUT FOR ACCESS. THE SKIN AND ANGLE CRACK WERE ROUTED OUT. THE CRACK CUTOUTS AND ACCESS CUTOUTS WERE REPAIRED WITH DOUBLERS. 2 L 7 2 4F RT A6WE 1999082700080 19990827 00080 NM 1999 8 27 DL73K991836 1 19990814 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 THE FS 178 BULKHEAD WEB WAS FOUND WITH TWO SMALL CRACKS AT WL 210, BL 5.7 LT & RT AND TWO SMALL CRACKS AT WL 233.5, BL 5.7 (LT & RT). THE WL 233.5 CRACKS WERE REPAIRED WITH DOUBLERS PER SRM 53-10-11. THE CRACKS AT WL 210 WERE JUST ABOVE A LARGE EXISTING WEB REPAIR DOUBLER. THE EXISTING DOUBLER WAS REMOVED, THE NEW CRACKS CUTOUT, AND A NEW DOUBLER INSTALL ED PER ER/A 361208-14, REV D. 2 L 7 2 4F RT A16WE 1999082700081 19990827 00081 NM 1999 8 27 DL73K991837 1 19990814 A 5312 6546568515 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 1016 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 WHILE ACCOMPLISHING LFEC INSPECTIONS OF THE AFT PRESSURE BULKHEAD WEB, A CRACK INDICATION WAS NOTED NEAR STRINGER 6R. I NTERNAL HFEC INSPECTION CONFIRMED TWO CRACKED FASTENER HOLES AT THE WEB TO CAP INTERFACE AT STRINGER 6R. THE CRACKED AR EA OF WEB WAS CUTOUT AND AN ALUMINUM DOUBLER INSTALLED PER ER/A 368012-14AD. 2 L 7 2 4F RT A16WE 1999082700082 19990827 00082 WP 1999 8 27 DLL19991838 1 19990816 A 5330 SKIN LKHEED 1011 10113853 5265020 WP BS 886 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 THE FUSELAGE BELLY SKIN AT FS 886 BETWEEN STR 33 AND 32 WAS FOUND WITH AN AREA OF CORROSION. THE CORROSION WAS REMOVED WITH A 3.7 X 5 CUTOUT. THE CUTOUT WAS NEAR AN EXISTING BELLY SKIN REPLACEMENT REPAIR. AN ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE CUTOUT AND INCORPORATE THE EXISTING SKIN REPAIR PER ER/A 368027-14, REV A. 2 L 7 3 4F A23WE 1999082700083 19990827 00083 NM 1999 8 27 DLM11991839 1 19990815 A 5330 SKIN DOUG MD11 MD11 3023602 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 813DE 48600 THE C1 DOOR FUSELAGE SURROUND SKIN WAS DAMAGED NEAR THE LOWER AFT CORNER OF THE DOOR CUTOUT. THE DAMAGE WAS TO THE OUTER SKIN ONLY. THE SKIN WAS CUT AWAY WITH A 3 X 4 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLE R INSTALLED PER ER/A 368029-14. 2 L 7 3 4F RT A22WE 1999082700084 19990827 00084 NM 1999 8 27 DLM88991840 1 19990817 A 2130 CONTROL VALVE 700569500 DOUG MD88 MD88 3023688 NM LANDING GEAR LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 961DL 49980 ON T/O FROM PBI, THE FLT CREW REPORTED AN ODOR IN THE CABIN. ODOR DISSIPATED ON POWER REDUCTION. ODOR RETURNED AT FL25 0, RT PACK WAS SHUTDOWN AND THE ODOR WENT AWAY. FLIGHT DIVERTEDTO JAX. MAINTENANCE FOUND THE MAIN LANDING GEAR CONTROL VALVE LINE LEAKING AND FLUID WAS STREAKING DOWN THE SIDE OF THE FUSELAGE. TIGHTENED LINE, PERFORMED DUCT BURNOUT. REP LACED COALESCERS. 2 L 7 2 4F RT A6WE 1999082700085 19990827 00085 NM 1999 8 27 DL73K991841 1 19990817 A 2133 322684003 OUTFLOW VALVE BOEING 737 737232 1384475 NM CABIN FAILED A DALA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 27 309DL 23081 AT LEVEL OFF AT 37,000 ALTITUDE WARNING HORN SOUNDED AND CABIN ALTITUDE CLIMBING TO 10,000. DESCENDED TO MAINTAIN 10 ,000 CABIN ALTITUDE AND SELECTED MANUAL AC & DC WORKED OK NO FAIL LIGHT. FOUND FWD OUTFLOW VALVE STUCK OPEN. REPLACED VALVE. ALSO, OVHD PANEL WOULD NOT TEST PROPERLY. REPLACED PANEL. 2 L 7 2 4F RT A16WE 1999082700086 19990827 00086 NM 1999 8 27 DLM11991842 1 19990817 A 3520 80138682 OXYGEN GEN DOUG MD11 MD11 3023602 NM AFT LAV DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 812DE 48601 4L AFT LAV MASKS WERE DEPLOYED IN FLIGHT. WHILE CHECKING CONDITION OF O2 GENERATOR, MECHANIC DISCHARGED SAME. GENERATO R OPERATED CORRECTLY AND WAS REPLACED BY MECHANIC. 2 L 7 3 4F RT A22WE 1999082700087 19990827 00087 NM 1999 8 27 DL767991843 1 19990815 A 3350 EMER EXIT LIGHT 1000677 BOEING 767 767232 1385132 NM COCKPIT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 106DA 22218 FOUND COCKPIT EMERGENCY LIGHT OVER DOOR INOP. 2 L 7 2 4F RT A1NM 1999082700088 19990827 00088 NM 1999 8 27 DL72S991844 1 19990809 A 5530 STRINGER BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 VERTICAL STAB INTERIOR, STRINGER CRACKED AT TIE TO RIB LEFT SIDE AT FIN STA 1338. INSTALLED REPAIR PER SRM 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1999082700089 19990827 00089 NM 1999 8 27 DL72S991845 1 19990817 A 3350 0201720001 LIGHT BOEING 727 727232 1384082 NM ROW 10D BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 416DA 21258 EMERGENCY LIGHT AT SEAT 10D BROKEN. REPLACED BULBS AND LIGHT COVER ASSY. 2 L 7 3 4F A3WE 1999082700090 19990827 00090 NM 1999 8 27 DLM88991846 1 19990818 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 655 DENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DL 49544 DURING HMV, A DENT WAS FOUND IN THE FUSELAGE SKIN AT FS 655 AND STRINGER 30L. THE DAMAGE WAS REPAIRED PER ERA 333458-1 4. 2 L 7 2 4F RT A6WE 1999082700091 19990827 00091 NM 1999 8 27 DLM88991847 1 19990818 A 5330 5924802517 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DL 49544 DURING HMV, DENTS WERE FOUND IN THE FUSELAGE SKIN AT FS 237 BETWEEN STRINGERS 17L AND 18L. THE DAMAGE WAS REPAIRED BY ERA 333441-14. 2 L 7 2 4F RT A6WE 1999082700092 19990827 00092 WP 1999 8 27 DLL19991849 1 19990818 A 2424 GCU 51511003 LKHEED 1011 10113853 5265020 WP NR 2 ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 27 753DA 1060 193W1189 1060 ON TAKEOFF AT 0915 IN MCO FLT STATION BUS 2 FAIL LIGHT ILLUM. ABORTED TAKEOFF AT 125 KTS. APPLIED MINIMUM BRAKES DUE T O LIGHT WGT 332,000 LBS. C/W REPLACED NR 2 GCU, RAN ENG GENERATOR AND BUS OPN NORMAL. ALSO PERFORMED HIGH ENERGY STOP INSPECTION. 2 L 7 3 4F A23WE 1999082700093 19990827 00093 NM 1999 8 27 DLM11991850 1 19990818 A 3397 WIRE DOUG MD11 MD11 3023602 NM ROW 40 SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 801DE 48472 ON L/O, FOUND EMERGENCY LIGHTS OUT AT ROW 38 - 47. EMERGENCY LIGHTS TEST FAULT NR 5 BATTERY. FOUND WIRING SHORTED AT R OW 40 RT SIDE. CLEARED SHORT, SECURED WIRING AND CKS GOOD. 2 L 7 3 4F RT A22WE 1999082700094 19990827 00094 NM 1999 8 27 DL72K991851 1 19990818 A 2913 PUMP AS19570C BOEING 727 727232 1384082 NM B HYD SYS FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 521DA MX46005582 21472 UPON DEPARTURE FROM BOS, HYD SYS B LOST ALL PRESS AND QTY WENT TO 1.5 GALS, FOLLOWED POM. FOUND OUTBOARD MOTOR PUMP L EAKING. REPLACED SAME. 2 L 7 3 4F A3WE 1999082700095 19990827 00095 NM 1999 8 27 DL72L991852 1 19990809 A 5531 RIB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 AT HMV 2 FOUND VERT STAB INTERIOR-RIB CHORD HAS CRACK AT PREVIOUS STRINGER REPAIR-RT SIDE OF VERT AT STA 110.4 STR 10. S TOP DRILLED CRACK PER MM 55-30-00 FIG 802. MADE REPAIR ANGLE PER SAME, INSTALLED. 2 L 7 3 4F A3WE 1999082700096 19990827 00096 NM 1999 8 27 DL767991853 1 19990818 A 2613 OVERHEAT LOOP BOEING 767 767232 1385132 NM NR 1 ENGINE FAILED A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 104DA 22216 850356 AFTER T/O ENG EICAS MSG LT ENG OVHT LP1/LP2 FIRE OVHT SYS FAIL LIGHT ON. REPLACED M687 AND M688 LEFT OVHT LOOP 1 AND 2 CARDS, INSPECTED LEFT ENG PNEU DUCTS AND CLAMPS. RETORQUED CLAMPS. RAN ENGINES TO T/O POWER FOR SEVERAL MIN, NO OVHT MSG OR CAUTION. INSPECTED OVHT LOOPS 1 AND 2 LEFT ENG AND WIRING, NO TROUBLE FOUND. 2 L 7 2 4F RT A1NM 1999082700097 19990827 00097 NM 1999 8 27 DL72S991854 1 19990818 A 3260 656021132 ACCESSORY UNIT BOEING 727 727232 1384082 NM E & E COMPT MALFUNCTIONED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 531DA 21814 ON SHORT FINAL, THE LANDING GEAR WARNING HORN SOUNDED AS FLAPS WERE SET TO 30 DEG. GEAR DOWN AND INDICATION NORMAL. SPE ED BRAKE STOWED. HORN STOPPED DURING GO-AROUND AS FLAPS WERE RETRACTED PAST 30 DEG. REPLACED LANDING GEAR ACCESS UNIT PER M/M 32-09-121. LANDING GEAR WARNING OPERATES NORMAL. 2 L 7 3 4F A3WE 1999082700098 19990827 00098 NM 1999 8 27 DL72L991855 1 19990818 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 FOUND ON A1 LETTER CK, NR 2 SLAT ACTUATOR O/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1999082700099 19990827 00099 WP 1999 8 27 RRXA991320 1 19990303 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP BS 1260 - 1380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CTR FLOOR ATTACH CHANNEL BETWEEN STA 1260 AND STA 1380 AT LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED CENTER FLOOR ATTACH CHANNEL IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999082700103 19990827 00103 NM 1999 8 27 CA990401014 1 19990323 A 7602 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CONDITION LEVER DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 120368 (CAN) LEFT CONDITION LEVER CONTROL CABLE FOUND DAMAGED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700105 19990827 00105 NM 1999 8 27 CA990401019 1 19990322 A 3244 0262020 TIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 732 8255P00917 PCE120405 (CAN) TIRE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700106 19990827 00106 NM 1999 8 27 CA990401021 1 19990322 A 3244 0262020 TIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 654 8256P00912 PCE121384 (CAN) TIRE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700107 19990827 00107 EU 1999 8 27 CA990401022 1 19990320 A 5610 NP1701011 WINDSCREEN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 6535 85292H7004 LF05653A (CAN) PILOTS A WINDSCREEN CRACKED ON TAXI. 2 H 7 4 4F 4 F RT A49EU E6NE 1999082700116 19990827 00116 NM 1999 8 27 CA990412008 1 19990225 A 2910 82950010273 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 23329 120273 (CAN) HYDRUALIC LEAK AT NR 1 DUMP VALVE PRESSURE LINE. NEW LINE INSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700117 19990827 00117 NM 1999 8 27 CA990412009 1 19990310 A 2910 82970010337 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 20632 120249 (CAN) HYDRAULIC LINE FROM NR 1 SPOILER DUMP VALVE LEAKING. LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700118 19990827 00118 NM 1999 8 27 CA990412010 1 19990317 A 3260 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG DOOR FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 120382 (CAN) RIGHT GEAR DOOR LIGHT CAME ON IN CRUISE. WENT OUT AFTER 20 MINUTES. DOOR PROXIMITY SWITCH REPLACED AND RIGGED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700123 19990827 00123 NM 1999 8 27 CA990728006 1 19990713 A 3241 427911A CONTROL BOX ELDEC 841005 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ANTI SKID SYSTEM SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 22378 085 120152 (CAN) ERROR CODE 54 LEAD TO REPLACEMENT OF ANTI-SKID CONTROL UNIT WHICH WAS SHORTED INTERNALLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700124 19990827 00124 NM 1999 8 27 CA990728007 1 19990701 A 2910 8Z6069179 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 2537 121158 (CAN) FLUID LEAK IN THE NR 2 NACELLE AREA. HYDRAULIC RETURN LINE FROM THE NR 2 ACTUATOR. LINE WAS PART OF MOD 8/2781. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700125 19990827 00125 1999 8 27 CA990728008 4 19990706 A 2350 506012 REU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT FAILED W O OTHER O OTHER AP APPROACH 1 CA 11274 357 121165 (CAN) TOTAL COMM FAILURE ON FINAL APPROACH. REMOTE ELECTRONIC UNIT REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700126 19990827 00126 EA 1999 8 27 CA990728010 1 19990709 A 2841 10013000002 INDICATOR SIMMONDS 1284101 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE FUEL SYSTEM INACCURATE W K NONE O OTHER IN INSP/MAINT 1 CA 18801 228 123132 (CAN) RIGHT WING WAS FILLED TO CAPACITY. THE COCKPIT GAUGE SHOWED 200 POUNDS LOW. ERROR WAS CONFIRMED BY THE REPEATER GAUGE AT SINGLE POINT LOCATION. INDICATOR WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700127 19990827 00127 NM 1999 8 27 CA990728012 1 19990714 A 3010 8SC0029028 DEICE BOOT 85720062006 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT WING DISBONDING W K NONE O OTHER IN INSP/MAINT 1 CA 9518 161 0060030 120064 (CAN) DURING A DAILY INSPECTION, IT WAS NOTED THAT THE RIGHT INBOARD DEICE BOOT WAS DISBONDING FROM THE LEADING EDGE. BOOT INSTALLATION WAS ONLY 161 HOURS. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700128 19990827 00128 NM 1999 8 27 CA990728013 1 19990709 A 2910 82950010349 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 20754 120373 (CAN) DURING INSPECTION, HYDRULIC FLUID FOUND DRIPPING FROM LEFT TRAILING EDGE. PRESSURE LINE TO THE OUTBOARD ROLL SPOI LER WAS FOUND CHAFED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700129 19990827 00129 EA 1999 8 27 CA990728016 1 19990713 A 2910 82970010391 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 19497 123110 (CAN) HYDRAULIC LEAK IN THE NR 1 NACELLE AREA. PRESSURE LINE TO DOOR SEQUENCE VALVE BEHIND WHEEL DEBRIS SHIELD LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700134 19990827 00134 EU 1999 8 27 CA990728060 1 19990715 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE EXHAUST PIPE INTERMITTENT W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA 5853 GEE785590 DAP0070 (CAN) AFTER DEPARTURE, IN HEAVY RAIN, JET PIPE HOT LIGHT STARTED INTERMITTANT INDICATIONS. THE ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. ALL INDICATIONS NORMAL. ALL SYSTEMS INSPECTED AND CHECKED. OVERHAUL SWITCHES REPLACED. S USPECT SYSTEM IS VULNERABLE TO MOISTURE INGRESS AT O/T SENSOR ELECTRICAL TERMINALS. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 1999082700137 19990827 00137 EA 1999 8 27 CA990728072 1 19990720 A 2435 23048004M GENERATOR DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA STARTER/GEN FAILED W O OTHER O OTHER CL CLIMB 1 CA 97 9042 PCE42393 (CAN) BOTH GENERATORS KICKED OFF SHORTLY AFTER TAKEOFF. FOLLOWING LONGER THAN NORMAL RUNNING ON THE GROUND WHILE WAITIN G DEPARTURE. ONE RESET, BUT THE OTHER WOULD NOT. RETURNED TO BASE CARRIED OUT. STARTER/GENERATOR REPLACED. 1 H 7 2 3T 4 T RT A9EA E4EA 1999082700138 19990827 00138 EA 1999 8 27 CA990804004 1 19990728 A 2150 78279012 ACM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE CABIN COOLING LEAKING W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 11917 123133 (CAN) CABIN FILLED WITH SMOKE AFTER START. AIR CYCLE MACHINE INTERNAL FLUID LEAK. ACM REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700139 19990827 00139 NM 1999 8 27 CA990804016 1 19990720 A 5230 85331207103 SUPPORT DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4839 123010 (CAN) FORWARD BAGGAGE DOOR TRACK SUPPPORT FOUND CRACKED IN TWO PLACES. FITTING REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700140 19990827 00140 EA 1999 8 27 CA990804018 1 19990702 A 3251 89881 LINK 8900113 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG STEERING SHEARED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 20938 DCL1938899 123028 (CAN) WHILE PARKED AT GATE, A LOUD BANG WAS HEARD FROM NLG. NLG THEN CASTORED AND WOULD NOT CENTER. NO CAUTION LIGHTS. ONE STEERING LINK FOUND BROKE. TOWING FUSELAGE FOUND INTACT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700141 19990827 00141 NM 1999 8 27 CA990804019 1 19990704 A 2910 82950010269 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24673 120804 (CAN) HYDRAULIC LEAK RIGHT REAR SPAR. LIFT DUMP PRESSURE LINE FOR THE RIGHT SPOILER VALVE WAS CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700142 19990827 00142 NM 1999 8 27 CA990804020 1 19990712 A 3230 841005 PSEU ELDEC DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 17599 149 120804 (CAN) ON APPROACH WITH GEAR DOWN ,THE NLG DOOR AMBER, UNSAFE LIGHT AND HORN MOMENTARILY SOUNDED. PSEU REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700143 19990827 00143 NM 1999 8 27 CA990804021 1 19990712 A 3234 5352011 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 13898 57 120804 (CAN) ON APPROACH WITH GEAR DOWN, THE NLG DOOR AMBER, UNSAFE LIGHT AND HORN MOMENTARILY SOUNDED. PSEU REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700144 19990827 00144 NM 1999 8 27 CA990804022 1 19990712 A 2910 170K0036CR0280 FLEX HOSE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24484 121075 (CAN) PRESSURE LINE FROM NR 1SPU TO PRESSURE MANIFOLD WAS FOUND TO BE LEAKING WHERE THE LINE WAS SECURED. LINE CHAFED W HERE IT RUNS THROUGH THE SECURING BLOCK. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700145 19990827 00145 NM 1999 8 27 CA990804023 1 19990719 A 3411 AE1000307E0236 HOSE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PITOT SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24527 121075 (CAN) PITOT STATIC TEST FOUND A LARGE LEAK AT STANDBY ALT STATIC HOSE. FOUND BADLY DETERIORATED AND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700146 19990827 00146 NM 1999 8 27 CA990804024 1 19990702 A 3230 82910010121 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG WW LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 29764 120338 (CAN) DURING A WALK-A-ROUND, FLUID WAS NOTED COMING FROM THE NOSEWHEEL AREA. AFTER RUNNING THE A/C, A PINHOLE WAS FOUND IN THE NLG DOWN LINE IN THE OXYGEN BOTTLE AREA. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700147 19990827 00147 NM 1999 8 27 CA990804025 1 19990713 A 3230 DSC252840124 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 2987 120329 (CAN) BOTH NLG DRAG STRUT FLEX LINES FOUND WEEPING FLUID. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700148 19990827 00148 NM 1999 8 27 CA990804028 1 19990714 A 7931 APT761000100D TRANSMITTER KULITE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE OIL PRESSURE FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 7572 4834188 120803 (CAN) WHILE IN CLIMB, NR 1 OIL PRESSURE READ APPROXIMATELY 52 PSI AND DROPPED SLOWLY TO 45-48 PSI. OIL PRESSURE STABLIZ ED AT 54 PSI WITH POWER LEVER AT FLIGHT IDLE AND CONDITION LEVER IN FEATHER. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700149 19990827 00149 1999 8 27 CA990804029 4 19990715 A 3417 7000700975 ADC DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 13471 87092322 120843 (CAN) PILOTS ALT FAILED ON TAKEOFF ROLL. NR 1 ADC REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700150 19990827 00150 NM 1999 8 27 CA990804030 1 19990712 A 3350 MS3474L2241P CONNECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CABIN FAILED W C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 CA 21652 120549 (CAN) NR 1 A.C. GENERATOR FAILED ON TAKEOFF ROLL. PIN 'N' OF CONNECTOR 2421 -P5 AND J5 WAS BURNT. CONNECTOR REPAIRED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700151 19990827 00151 NM 1999 8 27 CA990804031 1 19990721 A 3231 82910010175 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG DOOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 21718 120549 (CAN) HYDRAULIC FLUID FROM NLG AREA. NLG DOOR CLOSE LINE WAS LEAKING UNDER PRESSURE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700156 19990827 00156 SO 1999 8 27 CA990812011 1 19990726 A 3232 46357000 BRACKET PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA DOOR ACTUATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11711 L27561A (CAN) LEFT MAIN LANDING GEAR INBOARD GEAR DOOR NOT SITTING FLUSH - HANGING DOWN ABOUT .50 INCH. FURTHER INVESTIGATION R EVEALED THAT THE UPPER ATTACHMENT BRACKETS FOR INBOARD GEAR DOOR ACTUATOR WERE CRACKED THROUGH. NEW BRACKETS INSTALLED . P/N'S 46357-000 AND P/N 46357-001. 1 L 7 2 3O 3 O A20SO E14EA 1999082700158 19990827 00158 CE 1999 8 27 CA990812019 1 19990727 A 3230 508200704 SPROCKET 5082001017 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG WORN W K NONE O OTHER IN INSP/MAINT 1 CA PCE50201 (CAN) DURING THE UNDER FLOOR INSPECTION THE AME NOTICED THE AFT CHAIN FOR THE LANDING GEAR ACTUATION SYSTEM HAD JUMPED O NE SET OF TEETH ON A SPROCKET. FURTHER INVESTIGATION FOUND THAT THE CHAIN TENSION WAS OUT OF TOLERANCE WHICH HAS BEEN D ETERMINED TO BE THE CAUSE OF THE CHAIN JUMPING ONE TOOTH. THE CHAIN AND SPROCKET WERE CHANGED. THE CHAIN WAS WITHIN IT S STRETCH LIMITS. 1 L 7 2 3T 4 T A14CE E4EA 1999082700161 19990827 00161 EA 1999 8 27 CA990812027 1 19990714 A 2750 ECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 807373 (CAN) FLAPS CAUTION LIGHT ON WITH FLAPS AT 30 DEGREES, BUT SELECTED TO 45. FLAP ELECTRONIC UNIT AND FLAP CONTROL LEVER REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999082700162 19990827 00162 EA 1999 8 27 CA990812029 1 19990720 A 2750 ECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 807173 (CAN) FLAP FAILED AT ZERO DEGREES. FLAP ELECTRONIC CONTROL UNIT POTENTIOMETER NR 1 AND NR 8 ADJUSTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999082700163 19990827 00163 EA 1999 8 27 CA990812030 1 19990722 A 4990 APU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE APU BAY LEAKING W E ENGINE SHUTDOWN K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 807380 (CAN) AFTER APU START, STRONG SMELL IN COCKPIT AND SMOKE SMELL IN CABIN. LAVATORY SMOKE DETECTOR WENT OFF ONCE. AIRCR AFT AT GATE. APU OIL LEAKING INTO BLEED AIR SYSTEM. APU CHANGED AND COALESCER BAGS CLEANED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999082700164 19990827 00164 EA 1999 8 27 CA990812031 1 19990722 A 2751 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA 807428 (CAN) FLAPS FAILED AT 20 DEGREES AFTER TAKE-OFF. BPSU CHANGED ON LEFT SYSTEM. 2 L 7 2 4F 4 F RT A21EA E15NE 1999082700165 19990827 00165 EA 1999 8 27 CA990812032 1 19990727 A 5610 WINDOW CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 807194 (CAN) TWO LARGE CRACKS NOTICED AFTER TAKEOFF IN LOWER CORNER OF LEFT WINDOW. 2 L 7 2 4F 4 F RT A21EA E15NE 1999082700170 19990827 00170 NM 1999 8 27 HNAA9900112 1 19990728 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 930HA 126 AFT FUSELAGE, SMALL CRACK IN SKIN APPROX 5 IN FWD OF FRAME 3 AT STR 33. TEMP REPAIRED IAW RD8-53-2181. TEMP REPAIRED P ER ENGINEERING. FWD TO ENGINEERING FOR PERM REPAIR. DEFERED FOR 240HRS. ON 8/20/99, THIS DMT WAS CLEARED PER EO8-53-9 9-290. 2 H 7 2 4T RT A13NM 1999082700171 19990827 00171 NM 1999 8 27 HNAA9900113 1 19990819 A 3350 SIGN 6013211X DHAV DHC8 DHC8102 2809003 NM PAX DOOR FAILED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 975HA SBY10 176 PAX EXIT SIGN AND LEFT FWD EGRESS LT OUT. REMOVED AND REPLACED 3351-P1, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999082700172 19990827 00172 WP 1999 8 27 AT9900584 1 19990812 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND CABIN SEAT TRACK CORRODED AT BS 200 LBL 45. REMOVED SEAT TRACK , CUT, DRILLED, COUNTERSUNK NEW SECTION OF SEAT TRACK AND INSTALLED IAW DC9 SRM 53-05, 51-10-4, 51-10-3, 53-21-0 FIG 3. 2 L 7 2 4F A6WE 1999082700173 19990827 00173 WP 1999 8 27 AT9900585 1 19990812 A 5730 PANEL DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND LEFT WING PANEL NR 1144 CORRODED. REMOVED CORROSION AND INSTAL LED A DOUBLER REPAIR IAW DC9 SRM 57-01 FIG NR 5. 2 L 7 2 4F A6WE 1999082700174 19990827 00174 WP 1999 8 27 AT9900586 1 19990813 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE SKIN OF AFT CARGO DOOR AT BS 935 CORRODED. C UT OUT CORRODED AREA. FORMED, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED AND INSTALLED DOUBLER IAW DC9 SRM 51-10-4 , 51-10-3, 51-20-0, 51-30-0, 53-04 FIG 12B. 2 L 7 2 4F A6WE 1999082700175 19990827 00175 WP 1999 8 27 AT9900587 1 19990814 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 976-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE SKIN HAS BULGE AT BS 990 L25L. REMOVED CORRO SION AT BS 976-996. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS IAW TIMCO EO NR 99-1213 AND DC9 SRM 51-10 -3 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1999082700176 19990827 00176 WP 1999 8 27 AT9900588 1 19990620 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 860-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND AFT CARGO COMPARTMENT FLOOR PANEL AT BS 860-996 CORRODED. CUT OUT AND DRILLED FLOOR PANEL IAW DC9 SRM 51-10-4, 53-21-0. 2 L 7 2 4F A6WE 1999082700177 19990827 00177 WP 1999 8 27 AT9900589 1 19990620 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 351-484 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND FWD CARGO COMPARTMENT FLOOR PANEL AT BS 351-484 CORRODED. CUT OUT AND DRILLED FLOOR PANEL IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1999082700178 19990827 00178 WP 1999 8 27 AT9900590 1 19990620 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP BS 560-588 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND RT FWD CARGO PIT TRACK AT BS 560-588 CORRODED. DRILLED AND COU NTERSUNK NEW TRACK IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1999082700179 19990827 00179 WP 1999 8 27 AT9900591 1 19990623 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 332 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND CRACKED FRAME IN FWD PIT AT BS 332 L29R. REMOVED FLOOR SUPPORT ANGLE, WELDED REPAIR, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-30-5, 51-10-3, 51-10-4, 53-20-0 AND EA NR 1 2-5321-29-4362 STEP 4. 2 L 7 2 4F A6WE 1999082700180 19990827 00180 WP 1999 8 27 AT9900592 1 19990623 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 351 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND FWD PIT FLOOR SUPPORT CRACKED AT BS 351 AND L29R. REMOVED FWD PIT FLOOR SUPPORT. WELDED AND REINSTALLED SUPPORT IAW DC9 SRM 51-30-2 AND EA NR 12-5321-29-C1362. 2 L 7 2 4F A6WE 1999082700181 19990827 00181 WP 1999 8 27 AT9900593 1 19990624 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND INTERCOSTAL ATTACH ANGLE AT BS 996 AND L27R CORRODED. REMOVED INTERCOSTAL ATTACH ANGLE AND REPLACED WITH A REPAIR ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999082700182 19990827 00182 WP 1999 8 27 AT9900594 1 19990626 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 237 - 313 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND CENTER FLOOR PANEL AT BL 0 TO RBL 22 AT BS 237-313 HAS SURFACE CORROSION AND INSULATION DETERIORATED. LOCATED AND DRILLED REPLACEMENT FLOOR PANEL ASSEMBLY IAW DC9 SRM 51-30-4. INSTA LLED INSULATION IAW DPS 3-40-9. 2 L 7 2 4F A6WE 1999082700183 19990827 00183 WP 1999 8 27 AT9900595 1 19990701 A 2741 29177811 SHAFT DOUG DC9 DC932 3022066 WP BS 351 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND CORROSION ON HORIZONTAL STABILIZER TAKEOFF WARNING MECHANISM AT BS 351 L20R. REMOVED AND REPLACED MANUAL OVERRIDE CONTROL BELLCRANK SHAFT, INTERCONNECT BRACKET, P/N 5915830-501, LIMI T SWITCH CONTROL ARM, P/N 4915833-1, IAW DC9 M/M 27-40-5, 27-40-0. 2 L 7 2 4F A6WE 1999082700184 19990827 00184 WP 1999 8 27 AT9900596 1 19990624 A 2720 3914309 BRACKET DOUG DC9 DC932 3022066 WP BS 1089 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND SURFACE CORROSION ON RUDDER PULLEY BRACKET AND HARDWARE AT BS 1 089. REMOVED AND REPLACED PULLEY BRACKET IAW DC9 M/M 27-20-7 AND 20-17-0. RUDDER TRIM CABLE TENSION WAS NOT DISTURBED. CABLE TENSION CHECK GOOD IAW DC9 M/M 27-20-7. 2 L 7 2 4F A6WE 1999082700185 19990827 00185 WP 1999 8 27 AT9900597 1 19990624 A 2730 BRACKET DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND SURFACE CORROSION ON ELEVATOR PULLEY BRACKET AND HARDWARE AT BS 1121. REMOVED AND REPLACED PULLEY BRACKET AND HARDWARE ON LEFT ELEVATOR CABLE SYSTEM IAW DC9 M/M 20-16-0 AND 20-17-0. ADJUSTED CABLE TENSION ON ELEVATOR, OPS CHECK GOOD IAW DC9 MM 27-30-0. 2 L 7 2 4F A6WE 1999082700186 19990827 00186 WP 1999 8 27 AT9900598 1 19990728 A 7603 BRACKET DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE BS 945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND NR 1 ENGINE THROTTLE CABLE SECTOR MOUNT BRACKET IN AFT PIT AT B S 945 CORRODED AT MOUNT LUGS AND AT CABLE GUIDE PIN HOLES. REMOVED LEFT THROTTLE SECTOR MOUNT BRACKET AND REPLACED IAW DC9 SRM 51-10-3. TENSIONED THROTTLE CABLES IAW DC9 M/M 76-11-0. 2 L 7 2 4F 4 F A6WE E2EA 1999082700187 19990827 00187 WP 1999 8 27 AT9900599 1 19990717 A 5330 PANEL DOUG DC9 DC932 3022066 WP BS 237-303 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE LT SIDE AT BS 237-303 HAS SPOTS OF SURFACE CO RROSION AROUND WINDOW FRAME BELT. HFEC AND DYE PENETRANT INSPECTION PERFORMED BEFORE REMOVAL OF PANEL. BLEND OUT CORRO SION, REMOVED AND REPLACED WINDOW BELT PANEL AND INSTALLED IAW DC9 SRM 51-30-3, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999082700188 19990827 00188 WP 1999 8 27 AT9900600 1 19990711 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 224-234 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 DURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND FUSELAGE SKIN HAS SEVERAL GOUGES ALONG LOWER EDGE OF LEFT WINDO W BELT AT BS 224 TO 334. BLENDED CHAFFED AREAS. CUT OUT DAMAGED AREAS. FABRICATED FILLERS AND DOUBLERS. TREATED, PRI MED AND INSTALLED REPAIR PARTS IAW RES 1-07105, EO 99-1214, SRM 51-10-3. 2 L 7 2 4F A6WE 1999082700189 19990827 00189 NM 1999 8 27 AT9900601 1 19990818 A 3244 26015711 TIRE BOEING 737 737297 1384480 NM NR 3 FAILED A ZZDA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 15 462AT 22631 NR 3 TIRE FAILURE CAUSED DAMAGE TO AIRCRAFT WHICH RESULTED IN ALL HYDRAULIC FLUID LOSS. REMOVED AND REPLACED NR 3 TIRE AND A REVISION NR AT9900601R1 WILL FOLLOW AFTER AIRCRAFT WILL COME BACK FOR SERVICE. 2 L 7 2 4F A16WE 1999082700190 19990827 00190 WP 1999 8 27 AT9900602 1 19990817 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1168 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND WEAR (CHAFFING) ON THE FRAME AT BS 1168 AT THE TAIL CONE ATTACH POINT S. FABRICATED REPAIR PLATES, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, DOUGLAS SERVICE BULLETIN NR 53-108, AND TIMCO EO NR 99-1222. 2 L 7 2 4F A6WE 1999082700191 19990827 00191 NM 1999 8 27 PCAA9900028 1 19990815 A 5310 STRUCTURE DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A PCAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 13 807EX 292 BGM - DURING THE ACCOMPLISHMENT OF AN A CHECK, THE NOSE LANDING GEAR UPLOCK ACTUATOR FLOORBEAM FRAME AND THE NOSE GEAR T RUNNION SIDE WALL WEB WAS FOUND TO HAVE SEVERAL CRACKS. DAMAGE WAS REPAIRED IAW BOMBARDIER RD'S 8-53-1336 AND 8-53-458. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999082700192 19990827 00192 EU 1999 8 27 AWXA9900268 1 19990820 A 5610 STA320151 WINDSHIELD AIRBUS 320 A320231 3930325 EU LT COCKPIT CRACKED A AWXA B EMER. DESCENT O OTHER CR CRUISE 1 WP 28 640AW 448 EMERGENCY DESCENT, PILOTS FWD WINDSHIELD CRACKED. REPLACED CAPTAINS FWD WINDSHIELD. 2 L 7 2 4F RT A28NM 1999082700193 19990827 00193 NM 1999 8 27 AWXA9900005 1 19990105 A 2751 0020931 CONNECTOR BOEING 737 73733A 1384673 NM TE FLAP IND DIRTY A AWXA O OTHER N FALSE WARNING DE DESCENT 1 WP 28 174AW 23633 STANDARD OPS: SPLIT FLAP IND, P/N 03-2750-9-0012, S/N 1893. ON ARRIVAL DTW, FLAPS EXTENDED TO 1 THEN SPLIT BETWEEN 1 ON THE LT, 2 ON THE RIGHT. EXTENDED THE LE DEVICES TO FULL EXTEND AND LANDED NORM. ON TURN OFF LT FLAP EXTENDED TO 2 SPO NTANEOUSLY FLAPS RETRACTED NORM. LOWERED FLAPS, CK FOR ICE OR FOREIGN MATTER. ALL CLEAR. VISUALLY CK FLAPS AT ALL DET ENT ALL EVEN IND. CK NORM, COULDN'T FIND ANY FAULT ON GROUND. A/C WAS PUT ON ALERT BY TECH SUPPORT FOR FLAP SPLIT IND. PART RETURN FROM VENDOR, NO FAULT FOUND. LT FLAP POSITION IND X-MITTER CANNON PLUG CLEANED ACFT HAS FLOWN 1,050 HRS N O REPEAT WRITE-UPS TO DATE. 2 L 7 2 4F RT A16WE 1999082700194 19990827 00194 NM 1999 8 27 RAAA99B2051 1 19990817 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 22 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 22 PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999082700195 19990827 00195 WP 1999 8 27 CALA9901063 1 19990818 A 3260 DN LOCK SWITCH DOUG DC9 DC932 3022066 WP NLG INOP A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 27509 47798 THE GREEN NLG LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON FINAL APPROACH TO CLE. THE NLG RED UNSAFE LIGHT EXTING UISHED NORMALLY. A GO AROUND WAS PERFORMED AND THE GEAR WAS RECYCLED. THE NLG GREEN LIGHT CAME ON AND A NORMAL LANDING WAS MADE. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR DOWNLOCK SWITCH AND OPERATION CHECKED GOOD IAW MM 32-60-1. 2 L 7 2 4F A6WE 1999082700196 19990827 00196 NM 1999 8 27 CALA9901064 1 19990817 A 3397 WIRE BOEING 737 7373T0 1384582 NM ROW 7-12 CHAFED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 39340 23578 INSPECTION FOUND EMERGENCY AISLE LIGHTS INOPERATIVE FROM ROW 7-12. REPAIRED CHAFED WIRE AT ROW 10 IAW MM 20-30-12. 2 L 7 2 4F RT A16WE 1999082700197 19990827 00197 WP 1999 8 27 CALA9901065 1 19990817 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 28-30 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND EMERGENCY AISLE LIGHTING AT ROW 28-32 INOPERATIVE. MAINTENANCE FOUND LIGHT FIXTURE AT ROW 30 BLOWING F USE AT THE POWER SUPPLY. REPLACED LAMP AND FUSE. 2 L 7 2 4F A6WE 1999082700198 19990827 00198 NM 1999 8 27 CALA9901066 1 19990818 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 14 TO RBL 12. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10- 51. 2 L 7 2 4F RT A16WE 1999082700199 19990827 00199 WP 1999 8 27 CALA9901067 1 19990819 A 3350 FUSE DOUG DC9 DC932 3022066 WP LAVATORY BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12510 47799 INSPECTION FOUND A SECTION OF EMERGENCY LIGHTS INOPERATIVE IN CENTER OF CABIN. MAINTENANCE FOUND FUSE ON BATTERY PACK A T RT AFT LAV CEILING SECTION AT FAULT. THE FUSE WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1999082700200 19990827 00200 NM 1999 8 27 CALA9901068 1 19990819 A 3350 6104789 BATTERY PACK GRIMES BOEING 727 727224 1384076 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A SECTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATI ON CHECKED GOOD IAW MM 33-50-01. 2 L 7 3 4F A3WE 1999082700201 19990827 00201 NM 1999 8 27 CALA9901069 1 19990819 A 3397 WIRE BOEING 727 727224 1384076 NM R1 DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND THE R-1 DOOR EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE TO CHARGER AND R-1 DOOR EXIT IDENTIFIER, AND RELAMPED. OPERATION CHECKED GOOD IAW SRM 33-51-0. 2 L 7 3 4F A3WE 1999082700202 19990827 00202 NM 1999 8 27 CALA9901070 1 19990819 A 3397 WIRE BOEING 727 727224 1384076 NM L1 DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND THE L-1 DOOR EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AT THE L-1 DOOR EXIT IDENTIFIER. OPERATION CHECKED GOOD IAW MM 33-51-0. 2 L 7 3 4F A3WE 1999082700203 19990827 00203 NM 1999 8 27 UPS99230368 1 19990819 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 948UP 19357 INFLIGHT EMERGENCY EXIT LIGHT CAME ON, TAPPED ON LEN'S COVER, LIGHT WENT OUT. FOUND RIGHT MOUNT LATCH UNSECURED, RESECU RED COCKPIT EMERGENCY LIGHT LATCH, LIGHT OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999082700204 19990827 00204 NM 1999 8 27 UPS99230369 1 19990819 A 3510 REGULATOR BOEING 727 72725C 138400H NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 F/E OXYGEN EMERGENCY SWITCH STICKS IN THE ON POSITION. REMOVED AND REPLACED FLIGHT ENGINEER'S 02 REGULATOR PER MM 35-11 -31. LEAK AND OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999082700205 19990827 00205 NM 1999 8 27 UPS99230370 1 19990817 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 LEFT ENTRY DOOR, FORWARD SIDEWALL EXIT IDENTIFIER INOP. REMOVED AND REPLACD BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999082700206 19990827 00206 NM 1999 8 27 UPS99230371 1 19990817 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 9 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 ROW 9 FLOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999082700207 19990827 00207 NM 1999 8 27 UPS99230372 1 19990817 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 17 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 ROW 17 FLOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CK, GOOD. 2 L 7 3 4F A3WE 1999082700208 19990827 00208 WP 1999 8 27 UPS99830374 1 19990808 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 FS 55 FRAME AT LONGERON 24L IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED FRAME IAW SRM 53-2-0 FIG 2 . 2 L 7 4 4F RT 4A25 1999082700209 19990827 00209 WP 1999 8 27 UPS99830375 1 19990809 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 LT WING L/E SKIN AT XFS 560 IS CRACKED AT 1 FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED SKIN IA W SRM 57-2-1 FIG 24. 2 L 7 4 4F RT 4A25 1999082700210 19990827 00210 WP 1999 8 27 UPS99830376 1 19990819 A 5720 576958927 DOUBLER DOUG DC8 DC873F 302199F WP WS 336 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 336 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999082700211 19990827 00211 WP 1999 8 27 UPS99830377 1 19990809 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 404 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 BULGING CORROSION, LT WING L/E UPPER SKIN AT XFS 404. CUT OUT DAMAGED AREA AND REPAIRED SKIN IAW DH SK813- 334. 2 L 7 4 4F RT 4A25 1999082700212 19990827 00212 WP 1999 8 27 UPS99830378 1 19990809 A 5320 JAMB DOUG DC8 DC873F 302199F WP BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 AFT ENTRY DOOR AFT JAM WEB HAS A RIVNUT PULLED THROUGH AND IS CRACKED AT FS 1660 AND LONGERON 15L. C UT OUT DAMAGED AREA AND REPAIRED THE WEB IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999082700213 19990827 00213 WP 1999 8 27 UPS99830379 1 19990809 A 5320 5755936502 FITTING DOUG DC8 DC873F 302199F WP BS 380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 MAIN CABIN, FS 380, THE LONGERON 16R END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE F ITTING IAW DH SK813-507 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999082700214 19990827 00214 WP 1999 8 27 UPS99830380 1 19990811 A 5313 S1415997T LONGERON DOUG DC8 DC873F 302199F WP BS 104 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 HEAVY CORROSION IN THE CENTER CHANNEL OF LONGERON 34R AT FS 104, AROUND THE FASTENERS. CUT OUT DAMAG ED LONGERON 34R BETWEEN FS 90 AND 110 AND SPLICED IN A NEW SECTION OF LONGERON IAW SRM 53-2-2. 2 L 7 4 4F RT 4A25 1999082700215 19990827 00215 WP 1999 8 27 UPS99830381 1 19990810 A 5720 576960036 DOUBLER DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 597.5 IS CRACKED IN TWO PLACES. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700216 19990827 00216 WP 1999 8 27 UPS99830382 1 19990819 A 5320 3750330505 FITTING DOUG DC8 DC873F 302199F WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 THE LONGERON 32R SPLICE FITTING AT FS 450 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700217 19990827 00217 WP 1999 8 27 UPS99830383 1 19990819 A 5320 47516252 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 680, AT LONGERON 11R. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700218 19990827 00218 WP 1999 8 27 UPS99830384 1 19990810 A 5320 47504232 FITTING DOUG DC8 DC873F 302199F WP BS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 THE INTERCOSTAL TO FRAME ATTACH FITTING AT FS 902, LONGERON 18L IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DWG 4750423 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700219 19990827 00219 WP 1999 8 27 UPS99830385 1 19990811 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 478.897 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT WING L/E RIB AT XS 478.897 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700220 19990827 00220 WP 1999 8 27 UPS99830386 1 19990811 A 5320 5645332111 DOUBLER DOUG DC8 DC873F 302199F WP BS 902-920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 FS 920 TO 902, RBL 68, THE FINGER DOUBLER HAS SEVERAL POPPED RIVET HEADS AND BULGING. REMOVED, FABRI CATED, AND REPLACED THE FINGER DOUBLER IAW DWG 5645332 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700221 19990827 00221 WP 1999 8 27 UPS99830387 1 19990811 A 5720 RIB DOUG DC8 DC873F 302199F WP WS 497.491 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT WING L/E RIB AT XS 497.491 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999082700222 19990827 00222 WP 1999 8 27 UPS99830388 1 19990811 A 5720 576960032 DOUBLER DOUG DC8 DC873F 302199F WP WS 570 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 570 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700223 19990827 00223 WP 1999 8 27 UPS99830389 1 19990815 A 5313 25972422 LONGERON DOUG DC8 DC873F 302199F WP BS 8-12 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2 LONGERON 5R AT FS -12 TO 8 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A NEW L ONGERON IAW SRM 53-2-2. 2 L 7 4 4F RT 4A25 1999082700224 19990827 00224 WP 1999 8 27 UPS99830390 1 19990813 A 5320 37502571 FITTING DOUG DC8 DC873F 302199F WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 LONGERON 31R SPLICE FITTING IS CRACKED AT FS 1040 TO 1060. REMOVED AND REPLACED THE SPLICE FITTING I AW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700225 19990827 00225 WP 1999 8 27 UPS99830391 1 19990812 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 366.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 366.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RI B IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999082700226 19990827 00226 WP 1999 8 27 UPS99830392 1 19990812 A 5720 RIB DOUG DC8 DC873F 302199F WP WS 454.976 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 LT WING L/E RIB AT XS 454.976 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE R IB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999082700227 19990827 00227 WP 1999 8 27 UPS99830393 1 19990812 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 316.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 316.5 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999082700228 19990827 00228 NM 1999 8 27 QXEA9901576 1 19990719 A 5753 MOUNT DHAV DHC8 DHC8102 2809003 NM RT TE FLAP OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT NR 4 FLAP AFT MOUNT GAPS DO NOT MEET MANUFACTURERS GAP SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. 2 H 7 2 4T RT A13NM 1999082700229 19990827 00229 NM 1999 8 27 QXEA9901577 1 19990719 A 5753 FLAP TRACK DHAV DHC8 DHC8102 2809003 NM RT TE FLAP OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT NR 4 FLAP TRACK AFT MOUNT GAPS DO NOT MEET MANUFACTURERS GAP SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. 2 H 7 2 4T RT A13NM 1999082700230 19990827 00230 NM 1999 8 27 QXEA9901578 1 19990714 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - FRETTING CORROSION AT BOTH ENDS OF LADDER PLATE 624BT. REPAIRED IAW RD 8-57-633. 2 H 7 2 4T RT A13NM 1999082700231 19990827 00231 NM 1999 8 27 QXEA9901579 1 19990714 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - FRETTING CORROSION AT BOTH ENDS OF LADDER PLATE 624AT. REPAIRED IAW RD 8-57-611 AND DHC8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999082700232 19990827 00232 NM 1999 8 27 QXEA9901580 1 19990717 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM RT WING/FUS CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999082700233 19990827 00233 NM 1999 8 27 QXEA9901581 1 19990712 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT OUTBOARD FLAP HAS A SMALL CHAFED AREA ON OUTBOARD END OF TOP SURFACE. REPAIRED IAW 57-20-11. 2 H 7 2 4T RT A13NM 1999082700234 19990827 00234 NM 1999 8 27 QXEA9901582 1 19990717 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM LT TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT OUTBOARD FLAP ASSEMBLY INBOARD SIDE HAS COMPOSITE DAMAGE. REPAIRED IAW DHC8 SRM 51-40-00, PAGE 201, FIGURE 2 . 2 H 7 2 4T RT A13NM 1999082700235 19990827 00235 NM 1999 8 27 QXEA9901583 1 19990719 A 5753 FLAP TRACK DHAV DHC8 DHC8102 2809003 NM LT TE FLAP OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT NR 5 FLAP TRACK AFT ATTACH GAPS DO NOT MEET MANUFACTURER SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. 2 H 7 2 4T RT A13NM 1999082700236 19990827 00236 NM 1999 8 27 QXEA9901584 1 19990719 A 5753 FLAP TRACK DHAV DHC8 DHC8102 2809003 NM LT TE FLAP OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX- LEFT NR 4 FLAP TRACK AFT ATTACH GAPS DO NOT MEET MANUFACTURERS SPECS. REPAIRED IAW HORIZON AIR EA 9-57-436. 2 H 7 2 4T RT A13NM 1999082700237 19990827 00237 NM 1999 8 27 QXEA9901585 1 19990724 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM LT WING /FUS CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-00, PAGE 4, TABLE 4. 2 H 7 2 4T RT A13NM 1999082700238 19990827 00238 NM 1999 8 27 QXEA9901586 1 19990716 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM LT WING/FUS CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT AFT WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999082700239 19990827 00239 NM 1999 8 27 QXEA9901587 1 19990714 A 5730 PANEL DHAV DHC8 DHC8102 2809003 NM WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - FUEL PANEL 524CT IS CHAFED AT INBOARD EDGE. REPAIRED IAW RD 8-57-320. 2 H 7 2 4T RT A13NM 1999082700240 19990827 00240 NM 1999 8 27 QXEA9901588 1 19990720 A 5753 HOUSING DHAV DHC8 DHC8102 2809003 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT NR 5 FLAP CARRIAGE HOUSING ASSEMBLY IS CHAFED ON INBOARD SIDE WHERE FAIL/SAFE STRAP MOUNTS. REPAIRED IAW HOR IZON AIR EA 9-57-437. 2 H 7 2 4T RT A13NM 1999082700241 19990827 00241 NM 1999 8 27 QXEA9901589 1 19990719 A 5753 FLAP TRACK DHAV DHC8 DHC8102 2809003 NM LT TE FLAP OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT NR 4 FLAP TRACK ASSEMBLY TO CHECK GAPS. REPAIRED IAW HORIZON AIR EA 9-57-436. 2 H 7 2 4T RT A13NM 1999082700242 19990827 00242 NM 1999 8 27 QXEA9901590 1 19990715 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT NACELLE LOWER INBOARD FORWARD CORNER CUTOUT IS CRACKED. REPAIRED IAW DHC-8 RD 8-54-724. 2 H 7 2 4T RT A13NM 1999082700243 19990827 00243 NM 1999 8 27 QXEA9901591 1 19990728 A 5411 FRAME DHAV DHC8 DHC8102 2809003 NM NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - NACELLE FRAME UNDER MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION. REPAIRED IAW HORIZON AI R EA 9-54-203. 2 H 7 2 4T RT A13NM 1999082700244 19990827 00244 NM 1999 8 27 QXEA9901592 1 19990716 A 5540 HINGE DHAV DHC8 DHC8102 2809003 NM RUDDER CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - FORE RUDDER BOTTOM SAFETY HINGE LUG IS CHAFFED AND HAS FRETTING CORROSION ACROSS ENTIRE LUG TOP SURFACE. REPAIRED IAW RD 8-55-537. 2 H 7 2 4T RT A13NM 1999082700245 19990827 00245 NM 1999 8 27 QXEA9901593 1 19990714 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM RT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - THERE IS A 3.5 INCH SCRATCH IN REAR SPAR AT YW RIGHT. REPAIRED IAW DHC8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 1999082700246 19990827 00246 NM 1999 8 27 QXEA9901594 1 19990720 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 342 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT OUTBOARD SEAT TRACK AT STATION 342 THERE IS CORROSION PITS. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 1999082700247 19990827 00247 NM 1999 8 27 QXEA9901595 1 19990714 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 406 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT OUTBOARD SEAT TRACK HAS PITS IN THE HAT CHANNEL AT X406. REPAIRED IAW DHC8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999082700248 19990827 00248 NM 1999 8 27 QXEA9901596 1 19990720 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 374 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION PITS IN THE HAT CHANNEL AT X374. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 1999082700249 19990827 00249 NM 1999 8 27 QXEA9901597 1 19990720 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 364 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT OUTBOARD SEAT TRACK HAS CORROSION PITS IN THE HAT CHANNEL AT X364. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 1999082700250 19990827 00250 NM 1999 8 27 QXEA9901598 1 19990714 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 346 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT OUTBOARD SEAT TRACK AT X346 HAS A GOUGE. REPAIRED IAW DHC8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999082700251 19990827 00251 NM 1999 8 27 QXEA9901599 1 19990720 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 327 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT OUTBOARD SEAT TRACK AT X327 HAS DEEP CORROSION PITS. REPAIRED IAW DHC8 SRM 51-26-26. 2 H 7 2 4T RT A13NM 1999082700252 19990827 00252 NM 1999 8 27 QXEA9901600 1 19990720 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 312 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - RIGHT OUTBOARD SEAT TRACK AT X312 HAS CORROSION PITS. REPAIRED IAW RD 8-53-1342. 2 H 7 2 4T RT A13NM 1999082700253 19990827 00253 NM 1999 8 27 QXEA9901659 1 19990818 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 816PH 54 SEA - MAIN CABIN DOOR EXCEEDINGLY HARD TO OPEN. INSPECTED DOOR AND FOUND NO DISCREPANCIES. LUBED STOPS. CYCLED DOOR S EVERAL TIMES. OPERATIONAL TEST CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 1999082700254 19990827 00254 NM 1999 8 27 99FDEA00342 1 19990819 A 2730 860405003 POWER CONTROL BOEING 727 727247 138408F NM RT ELEVATOR FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 25 234FE 21328 COMPLETE 'A' SYS HYD LOSS. GEAR CRANKED NORM AND ALT FLAPS OPER NORM. FOUND RT ELEV PWR CONTROL UNIT FIT BUSTED. REMO VED RT PWR CONTROL UNIT PER 727-200 MM 27-30-81. PWR CONTROL UNIT NEEDS INSTALL AND OPER CK. REMOVED AND REPLACED RIGH T ELEV PWR CONTROL PACK PER MM 27-30-081-4, OPER CK. 2 L 7 3 4F A3WE 1999082700255 19990827 00255 NE 1999 8 27 99FDEA00343 2 19990818 A 7200 ENGINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 2 FAILED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION UK UNKNOWN 1 SO 25 218FE 21101 99-214 - OIL TEMP NR 2 ENG, 110 DEG C, PRESS 52. NR 1 AND NR 3 OIL TEMP 95 DEG C, PRESS 45. SHUT DOWN NR 2 ENG FOR PRE CAUTION. REMOVED AND REPLACED NR 2 ENG FUEL HEAT SHUT OFF VALVE ASSY PER MM 73-14-11, AND FUEL OIL COOLER PER MM 79-20- 01. OPER CK GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 1999082700256 19990827 00256 NM 1999 8 27 99FDEA00344 1 19990819 A 5270 SOCKET BOEING 727 727227 1384078 NM CARGO DOOR FAILED A FDEA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SO 25 488FE 21491 99-215 - MAIN CARGO DOOR LIGHT ILLUM 25 MIN INTO FLT AT FLT LEVEL 330. REMOVED AND REPLACED SOCKET ASSY AND OPER CK MAI N CARGO DOOR PER MM 53-34-000-5. OPER CK NORM. 2 L 7 3 4F A3WE 1999082700257 19990827 00257 NM 1999 8 27 99FDEA00345 1 19990821 A 2150 ACM DOUG MD11 MD11 3023602 NM NR 2 INOP A FDEA J DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 583FE 48421 ON CLIMBOUT, RECEIVED SEL AIR SYS MAN. CREW NOTICED NR 1 PACK TEMP INCREASING AND 3 MIN LATER AIR MANF 1 FAIL LEVEL 3 A LERT. ENG 1 BLD SHOWED CLOSED AND 1-2 ISOL & 1-3 ISOL SHOW CLOSED. *S/D* REMOVED AND REPLACED NR 2 ACM PER MM 21-53-2 1-2. OPS CK OK MEL IS CLEARED. 2 L 7 3 4F RT A22WE 1999082700258 19990827 00258 NM 1999 8 27 99FDEA00346 1 19990822 A 5320 TIE BOEING 727 7272S2F 1384O81 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 CORROSION UNDER STRINGER TIE, BS 870, STR 9 LT (C53-224-01-2). *S/D * REPAIRED CORROSION AT BS 870, STR 9L IAW FEDEX EA 7-5310-46946. 2 L 7 3 4F A3WE 1999082700259 19990827 00259 WP 1999 8 27 ABXA9900651 1 19990813 A 5312 9915558237N ANGLE DOUG DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD, OUTBOARD LEFT ATTACH ANGLE, CRACKED AT LONGERON 15 LEFT. R EPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999082700260 19990827 00260 WP 1999 8 27 ABXA9900652 1 19990813 A 5311 99196182N FRAME DOUG DOUG DC9 DC933F 302207A WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND RIGHT MAIN FRAME CRACKED AT STATION 718. REPLACED MAIN FRAME IAW DC9 SERVICE BULLETIN 53-131 AND 53-182. 2 L 7 2 4F A6WE 1999082700261 19990827 00261 WP 1999 8 27 ABXA9900653 1 19990813 A 5320 9911840165 SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 1087 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1087 AND LONGERON LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-10-2 AND 5 1-30-1. 2 L 7 2 4F A6WE 1999082700262 19990827 00262 WP 1999 8 27 ABXA9900654 1 19990813 A 5320 995823869 SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND SHEAR-TIIE CRACKED AT STATION 980 AND LONGERON 14 LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2, 5 1-30-5 AND ABX REA 953-32623. 2 L 7 2 4F A6WE 1999082700263 19990827 00263 WP 1999 8 27 ABXA9900655 1 19990813 A 5330 5910228187 SKIN DOUG DOUG DC9 DC933F 302207A WP BS 1121 & 1132 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND FUSELAGE EXTERIOR SKIN PANEL CRACKED IN TWO LOCATIONS, STATION 1121 AND 1132, AT 9 O'CLOCK POSITIO N. REPLACED SKIN IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 1999082700264 19990827 00264 WP 1999 8 27 ABXA9900656 1 19990817 A 5250 LATCH DOUG DC9 DC932 3022066 WP COCKPIT DOOR LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 COCKPIT DOOR WOULD NOT OPEN FROM OUTSIDE. INTERNAL LATCH TRACK HAD JUMPED TRACK DUE TO LOOSE SCREW. RESET TRACK AND TI GHTENED SCREW. 2 L 7 2 4F A6WE 1999082700265 19990827 00265 NM 1999 8 27 SCNA99105 1 19990819 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM PAX DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE AFT AISLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE AF T ENTRY AISLE ILLUMINATION LIGHT BATTERY PACK. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999082700266 19990827 00266 NM 1999 8 27 SCNA99106 1 19990819 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE R2 OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE R2 OVERHEAD LIGHT BATTERY PACK. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999082700267 19990827 00267 NM 1999 8 27 SCNA99721 1 19990817 A 3350 6013211 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, AFT SECTION OF FORWARD LEFT ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REP LACED LIGHT BATTERY PACK AND CHARGER ASSEMBLY IAW B727 MM 335051. OPS CHECK GOOD IAW B727 MM 335001. 2 L 7 3 4F RT A3WE 1999082700268 19990827 00268 NM 1999 8 27 SCNA99720 1 19990725 A 5320 ANGLE BOEING 727 7272J4 1384006 NM BS 330 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS IN THE LOWER NOSE COMPARTMENT STA 330 S28L, INSIDE LT NOSE LANDING GEAR WALKWAY, FRAME SUPPORT ANGLE PER B727 SRM 531001. REMOVED T CHORD IAW B727 SRM 513002. FIT AND TRANS FERRED HOLES TO NEW CHORD PART NUMBER 65198617. INSTALLED NEW T CHORD IAW B727 SRM 511001 AND 513002. 2 L 7 3 4F RT A3WE 1999082700269 19990827 00269 NM 1999 8 27 SCNA99510 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND AROUND NUT PLATE HOLE ON TOP OF THE FLOORBEAM STATION 344 LBL 45. CORROSION WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER SRM 53101 FIGURE 4. 2 L 7 3 4F RT A3WE 1999082700270 19990827 00270 NM 1999 8 27 SCNA99511 1 19990722 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 344-480 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, SEAT TRACK AT LBL 24 BS 344 480 WAS FOUND FOUND TO HAVE CORROSION AROUND FASTENER HOLE S UPPER SURFACE. SEAT TRACK REMOVED AND REPLACED FROM STATION 344 TO 480 PER SRM 53105. TREATED AND PRIMED PER SRM 512 110. INSTALLED PER SRM 53105. 2 L 7 3 4F RT A3WE 1999082700271 19990827 00271 NM 1999 8 27 SCNA99512 1 19990722 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 480-495 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT LBL 24 BS 480 TO 495 WAS FOUND TO HAVE CORROSION ALONG THE UPPER SUR FACE. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW SECTION OF THE SEAT TRACK IAW SRM 53105 PAGE 20 FIG 7 SHEET 3. TRE ATED AND PRIMED IAW SRM 51204. 2 L 7 3 4F RT A3WE 1999082700272 19990827 00272 NM 1999 8 27 SCNA99513 1 19990722 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 344-480 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK WAS FOUND TO BE SEVERELY CORRODED AT BS 344 LBL 2475. THE SEAT TRACK W AS REMOVED AND FABRICATED PER SRM 53105. TREATED AND PRIMED PER 512101 AND INSTALLED PER SRM 53105. 2 L 7 3 4F RT A3WE 1999082700273 19990827 00273 NM 1999 8 27 SCNA99514 1 19990722 A 5320 CHORD BOEING 727 7272J4 1384006 NM BS 360 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND AROUND NUT PLATE HOLES AT BS 360 FROM LBL 6 TO RBL 14. REMOVED DA MAGED UPPER CHORD AND FABRICATED PARTS AND INSTALLED IAW SRM 53108 FIG 3. TREATED AND PRIMED IAW SRM 51102. 2 L 7 3 4F RT A3WE 1999082700274 19990827 00274 NM 1999 8 27 SCNA99515 1 19990722 A 5320 INTERCOSTAL BOEING 727 7272J4 1384006 NM BS 417 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND AT BS 417 RBL 45 ON INTERCOASTAL REPAIR. CORROSION ON REPAIR CORR ODED ALL THE WAY THROUGH. REMOVED AND REPLACED INTERCOASTAL PER SRM 5130. 2 L 7 3 4F RT A3WE 1999082700275 19990827 00275 NM 1999 8 27 SCNA99516 1 19990722 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 460 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK WAS FOUND TO HAVE CORROSION AT BS 460 RBL 2473. REMOVED AND REPLACED S EAT TRACK FROM FACTORY SPLICE TO THE PRODUCTION END PER SRM 5130. FABRICATED REPLACEMENT SEAT TRACK PER SRM 53105 AND T REATED AND PRIMED PER 512101. 2 L 7 3 4F RT A3WE 1999082700276 19990827 00276 NM 1999 8 27 SCNA99517 1 19990722 A 5320 SUPPORT BOEING 727 7272J4 1384006 NM BS 440-460 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND ON THE FLOORBOARDS SUPPORT UPPER SURFACE BETWEEN BS 440 TO 460 RBL 14. REMOVED FLOORBOARDS SUPPORT AND INSTALLED NEW AND SHIMMED REF SRM 51201. 2 L 7 3 4F RT A3WE 1999082700277 19990827 00277 NM 1999 8 27 SCNA99518 1 19990722 A 5320 FASTENERS BOEING 727 7272J4 1384006 NM BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, HILOCKS WERE FOUND CORRODED AT BS 440 RBL 14 AT FLOORBEAM TO FLOOR SUPPORT ATTACHMENT. FLOORBEAM FOR THIS SECTION WAS REPLACED PER 53108. 2 L 7 3 4F RT A3WE 1999082700278 19990827 00278 NM 1999 8 27 SCNA99519 1 19990722 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 383-480 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND ON SEAT TRACK AT BS 383 TO 480 RBL 43. REMOVED AND REPLACED SEAT TRACK FROM FACTORY SPLICE TO PRODUCTION END PER SRM 5130. 2 L 7 3 4F RT A3WE 1999082700279 19990827 00279 NM 1999 8 27 SCNA99520 1 19990722 A 5320 SUPPORT BOEING 727 7272J4 1384006 NM BS 419 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBOARD SUPPORT AT BS 419 RBL 14 WAS FOUND TO HAVE CORROSION ON THE UPPER SURFA CE. REMOVED THE FLOORBOARD SUPPORT AND INSTALLED NEW PART REF SRM 51302. 2 L 7 3 4F RT A3WE 1999082700280 19990827 00280 NM 1999 8 27 SCNA99521 1 19990722 A 5322 SUPPORT BOEING 727 7272J4 1384006 NM BS 400-420 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBOARD SUPPORT AT BS 400 TO 420 RBL 13 WAS FOUND TO HAVE CORROSION ON THE UPPE R SURFACE. REMOVED FLOOR SUPPORT AND INSTALLED NEW SUPPORT AND SHIMMED REF SRM 51201. 2 L 7 3 4F RT A3WE 1999082700281 19990827 00281 NM 1999 8 27 SCNA99522 1 19990722 A 5320 SUPPORT BOEING 727 7272J4 1384006 NM BS 380-400 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBOARD SUPPORT BETWEEN BS 380 AND 400 RBL 13 WAS FOUND TO BE CORRODED. REMOVE D AND INSTALLED NEW FLOORBOARD SUPPORT, SHIMMED, TREATED, AND PRIMED IAW SRM 51101 51302 51201 51106. 2 L 7 3 4F RT A3WE 1999082700282 19990827 00282 NM 1999 8 27 SCNA99523 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 400 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR BEAM AT BS 400 LBL 24 TO RBL 14 WAS FOUND TO HAVE CORROSION AROUND THE FASTE NER HOLES. REMOVED CORROSION MATERIAL LOSS OUT OF LIMITS PER SRM 53101. FABRICATED UPPER CHORD IAW SRM 53108 FIG 3 AND SUPPORT ANGLES. INSTALLED PARTS 53108. 2 L 7 3 4F RT A3WE 1999082700283 19990827 00283 NM 1999 8 27 SCNA99524 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 380 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM UPPER CHORD AT STA 380 RBL 14 TO 41 WAS FOUND TO HAVE CORROSION DUE TO A N EXISTING REPAIR AT THIS LOCATION EXTENDING FROM LBL 7 TO THE RIGHT HAND FRAME. AN ENGINEERING ORDER WAS ISSUED TO ACC OMPLISH A REPAIR FOR THIS FLOOR BEAM. UTILIZING REF 53108 FIG 3. 2 L 7 3 4F RT A3WE 1999082700284 19990827 00284 NM 1999 8 27 SCNA99525 1 19990722 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 480-500 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT BS 480 TO 500 RBL 24 WAS FOUND TO HAVE CORROSION AROUND THE FASTENER HOLES. REMOVED CORRODED PORTION OF SEAT TRACK, TREATED AND PRIMED NEW SECTION OF THE SEAT TRACK AND INSTALLED REF 5310 5. 2 L 7 3 4F RT A3WE 1999082700285 19990827 00285 NM 1999 8 27 SCNA99526 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 328 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM AT BS 328 LBL 195 WAS FOUND CORRODED AROUND THE FASTENER HOLE. REMOVED DAMAGED AREA AND FABRICATED REPAIRED PARTS PER 53108 FIG 9 AND INSTALLED TREATED AND PRIMED IAW 51102. 2 L 7 3 4F RT A3WE 1999082700286 19990827 00286 NM 1999 8 27 SCNA99527 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 460 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM AT STA 460 RBL 12 WAS FOUND TO HAVE CORROSION. REMOVED CORROSION AND TH E MATERIAL LOSS WAS FOUND TO BE OUT OF LIMITS PER SRM 53101. FABRICATED REPAIR ANGLES AND SHIMMED. TREATED PRIMED AND INSTALLED IAW SRM 53108 AND 51102. 2 L 7 3 4F RT A3WE 1999082700287 19990827 00287 NM 1999 8 27 SCNA99528 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM AT STA 440 RBL 15 HAS CORROSION AROUND NUT PLATE HOLE. CORROSION WAS RE MOVED AND FOUND OUT OF LIMITS PER SRM 53108. REMOVED DAMAGED SECTION AND FABRICATED UPPER CHORD FLOORBEAM REPAIR AND SU PPORT ANGLES AND REINFORCEMENT STRAPS AND INSTALLED PER SRM 53108. 2 L 7 3 4F RT A3WE 1999082700288 19990827 00288 NM 1999 8 27 SCNA99529 1 19990722 A 5321 FLOOR BOEING 727 7272J4 1384006 NM BS 760 CORRODED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBOARD SUPPORT AT STA 760 BBL 0 UNDER FLOORBOARD 3/10 SUPPORT WAS FOUND TO BE CRACKED. FABRICATED AND DRILLED AND TREATED AND PRIMED AND INSTALLED NEW PART WITH ANGLE REPAIRS IAW SRM 51403. 2 L 7 3 4F RT A3WE 1999082700289 19990827 00289 NM 1999 8 27 SCNA99530 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 344-360 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM STABILIZER STRAP WAS FOUND CRACKED AND SEVERED AT LBL 45 BETWEEN FLOORBE AMS AT BSTA 344 AND 360. REMOVED DAMAGED SECTION AND FABRICATED REPAIR SECTION IAW SRM 53108 FIG 6. ALODINED PRIMED AN D INSTALLED IAW SRM 53108 FIG 6. 2 L 7 3 4F RT A3WE 1999082700290 19990827 00290 NM 1999 8 27 SCNA99531 1 19990722 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 360 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM STABILIZER STRAP WAS FOUND CRACKED AT LBL 24 75 FORWARD OF THE FLOORBEAM AT BS 360. REMOVED DAMAGED AREA AND FABRICATED REPAIR PART AND INSTALLED IAW SRM 53108 FIG 6. 2 L 7 3 4F RT A3WE 1999082700291 19990827 00291 NM 1999 8 27 SCNA99532 1 19990722 A 5320 ANGLE BOEING 727 7272J4 1384006 NM BS 720-740 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, STA 720 TO 740 BL 0 UPPER ANGLE ON INTERCOASTAL WAS FOUND CRACKED AT NUT PLATE HOLES. REMOVED AND REPLACED ANGLE PER SRM 51302. 2 L 7 3 4F RT A3WE 1999082700292 19990827 00292 NM 1999 8 27 SCNA99534 1 19990810 A 3520 2250507 CONTROL UNIT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, WHEN THE PASSENGER OXYGEN BOTTLES WERE ACTIVATED THE EMERGENCY OXYGEN MASKS DEPLOYED. THE MANUAL OXYGEN CONTROL CABLE WAS FOUND STUCK IN THE ON POSITION. REMOVED AND REPLACED PNEUMATIC FLOW CONTROL UNIT I AW 352111. OPS AND LEAK CHECK GOOD. 2 L 7 3 4F RT A3WE 1999082700293 19990827 00293 NM 1999 8 27 SCNA99535 1 19990517 A 5313 STRINGER BOEING 727 7272J4 1384006 NM FUSELAGE DENTED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, WHILE REPAIRING THE RIGHT SIDE OF THE FUSELAGE NEAR THE FORWARD LAV SERVICE PANEL THE STRINGER WAS FOUND TO BE DENTED BEYOND LIMITS PER SRM 53101. REMOVED DENTED AREA FROM STRINGER AND FABRICATED STRINGER SPLICE FROM 7075 T6. INSTALLED IAW B727 SRM 53103. 2 L 7 3 4F RT A3WE 1999082700294 19990827 00294 NM 1999 8 27 SCNA99536 1 19990722 A 5730 SKIN BOEING 727 7272J4 1384006 NM CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING BOX RT SIDE UPPER SKIN WAS FOUND TO BE CORRODED OUT OF LIMITS RBL 705 BETWEEN S21C AND S18C. REMOVED CORROSION AND REPAIRED CENTER WING BOX UPPER SKIN IAW AMS AND SCA ENGINEERING ORDERS USI NG ACCEPTED METHODOLOGY. 2 L 7 3 4F RT A3WE 1999082700295 19990827 00295 NM 1999 8 27 SCNA99537 1 19990722 A 5730 SKIN BOEING 727 7272J4 1384006 NM CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 290SC 20764 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING BOX LT SIDE UPPER SKIN WAS FOUND TO BE CORRODED OUT OF LIMITS RBL 705 BETWEEN S21C AND S18C. REMOVED CORROSION AND REPAIRED CENTER WING BOX UPPER SKIN IAW AMS AND SCA ENGINEERING ORDERS USI NG ACCEPTED METHODOLOGY. 2 L 7 3 4F RT A3WE 1999082700296 19990827 00296 WP 1999 8 27 SCNA99107 1 19990819 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 1019-1059 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A SCHEDULED MAINTENANCE CHECK, FUSELAGE SKIN WAS FOUND BULGED BETWEEN STA 1019 AND 1059 ON THE LEFT LOWER FUSELAG E AREA. CUT OUT CORROSION AND FABRICATED A PATCH, DOUBLER AND TRIPLER PER SRM VOLUME 1 532000 FIGURE 6 AND INSTALLED A CLASS II REPAIR. 2 L 7 3 4F A22WE 1999082700297 19990827 00297 NM 1999 8 27 DHL99707002 1 19990819 A 3244 26045611 MLG TIRE ASSY BOEING 727 72722 1384002 NM NR 4 MLG BLOWN A DHLA K NONE O OTHER LD LANDING 1 SO 01 707DH 18321 BLOWN NR 4 MAIN GEAR TIRE ON LANDING. REMOVED AND REPLACED TIRE PER MM. 2 L 7 3 4F A3WE 1999082700298 19990827 00298 1999 8 27 DHL99802001 4 19990818 A 2360 16305 STATIC WICKS S656282DC10A DOUG DC8 DC873F 302199F WP WINGS DAMAGED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 802DH 6115 46076 IN PRECIP BOTH VHF AND HF WILL TRANSMIT BUT NOT RECEIVE. REPLACED 10 STATIC WICKS AND NR 1 VHF ANTENNA PER MM 23-60-0 A ND 23-10-0. 2 L 7 4 4F RT 4A25 1999082700299 19990827 00299 NM 1999 8 27 SWAA991362 1 19990816 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM EMER EXIT EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 610WN 27696 EEPLS LIGHT INOP AND WIRES EXPOSED AT OVERWING DOORS. REPAIRED WIRES AND REMOVED AND REPLACED 2 EACH LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999082700300 19990827 00300 NM 1999 8 27 SWAA991363 1 19990816 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 SEVERAL EEPLS LIGHTS PULLED LOOSE. SECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999082700301 19990827 00301 NM 1999 8 27 SWAA991364 1 19990816 A 3150 WARNING HORN BOEING 737 7373H4 1384600 NM COCKPIT ACTIVATED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 341SW 24091 ABORTED TAKEOFF, AT 20 KNOTS TAKEOFF WARNING HORN ON POWER ADVANCE. OPS CHECKED, TAKEOFF WARNING SYSTEM. NO FAULTS NOT ED. 2 L 7 2 4F RT A16WE 1999082700302 19990827 00302 NM 1999 8 27 SWAA991365 1 19990816 A 5511 6547644 RIB BOEING 737 7372T4 1384492 NM LT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB L/E RIB CRACKED, STA 123.85. REPAIRED RIB PER SRM. 2 L 7 2 4F A16WE 1999082700303 19990827 00303 NM 1999 8 27 SWAA991366 1 19990816 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM BS 1010 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND STRINGER 7L CRACKED, BS 1010. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999082700304 19990827 00304 NM 1999 8 27 SWAA991367 1 19990816 A 5320 6516310 CHORD BOEING 737 7372T4 1384492 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CORROSION ON Z-CHORD, BS 270, LBL 6.5-RBL 3. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F A16WE 1999082700305 19990827 00305 NM 1999 8 27 SWAA991368 1 19990816 A 3350 65C27095 BATTERY PACK BOEING 737 7375H4 138449D NM EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EXTERIOR EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999082700306 19990827 00306 NM 1999 8 27 SWAA991369 1 19990817 A 2910 HTD LINES BOEING 737 7373T5 NM NLG LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 667SW 23063 AIR TURNBACK, NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND NOSE LANDING GEAR LOCK ACTUATOR HYD LINES LEAKIN G. REMOVED AND REPLACED 2 EACH LINES PER MM. OPS CHECKED GOOD. P/N'S BACH8B04NN0166T AND 97934B04EE0207T. 2 L 7 2 4F RT A16WE 1999082700307 19990827 00307 NM 1999 8 27 SWAA991370 1 19990817 A 8011 35059456 STARTER BOEING 737 7377H4 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE CRACKED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 727SW 27859 875696 IN FLIGHT ENG SHUT DOWN, DIVERSION, NR 1 ENG LOW OIL PRESS LIGHT ILUMINATED, OIL QTY INDICATION WAS ZERO. ENGINE WAS SH UT DOWN AND DIVERTED FLIGHT TO COS. FOUND CRACKED STARTER. REMOVED AND REPLACED NR 1 ENG STARTER, SERVICED ENG WITH OI L. LEAK AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999082700308 19990827 00308 NM 1999 8 27 SWAA991372 1 19990817 A 3350 100885 BATTERY PACK BOEING 737 7373H4 1384600 NM ROW 17-12 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS LIGHTS INOP AT ROWS 17-12. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999082700309 19990827 00309 NM 1999 8 27 SWAA991374 1 19990817 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHTS FWD NAD AFT END COVERS MISSING. REMOVED AND REPLACED END COVERS PER MM. 2 L 7 2 4F RT A16WE 1999082700310 19990827 00310 NM 1999 8 27 SWAA991375 1 19990817 A 2560 SCREW BOEING 737 7373H4 1384600 NM SRVC DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE FWD HOOK LOOSE. TIGHTENED LOOSE SCREW PER MM. 2 L 7 2 4F RT A16WE 1999082700311 19990827 00311 NM 1999 8 27 SWAA991376 1 19990817 A 2560 6557463 PLATE BOEING 737 7372T4 1384492 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR, FWD GIRT BAR ATTACH BRACKET MOUNT PLATE CORRODED. REMOVED AND REPLACED MOUNT PLATE PER MM. 2 L 7 2 4F A16WE 1999082700312 19990827 00312 NM 1999 8 27 SWAA991378 1 19990817 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM BS 375 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND STRINGER 5L LOWER FLANGE CRACKED AT BS 375. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999082700313 19990827 00313 NM 1999 8 27 SWAA991379 1 19990818 A 2910 B468E662 LINE BOEING 737 7372H4 138448C NM NR 2 HYD SYS LEAKING A SWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 096SW 23055 LOST ALL 'A' SYSTEM HYD PRESSURE AND FLUID DURING FLIGHT. DISCOVERED HYD FLEX LINE LEAKING AT NR 2 ENG HYD PUMP. REMOV ED AND REPLACED LINE PER MM. 2 L 7 2 4F A16WE 1999082700314 19990827 00314 NM 1999 8 27 SWAA991380 1 19990818 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 510 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 510, ABOVE STRINGER 11L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999082700315 19990827 00315 NM 1999 8 27 SWAA991381 1 19990818 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT SERVICE DOOR EVACUATION SLIDE PRESS GAUGE DIFFICULT TO READ. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999082700316 19990827 00316 NM 1999 8 27 SWAA991371 1 19990818 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR LOWER HINGE FUSELAGE SKIN CUT OUT CRACKED. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 1999082700317 19990827 00317 NM 1999 8 27 SWAA991373 1 19990818 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 17.5. REPAIRED BULKHEAD PER SWA RA NR 1-53-2143. 2 L 7 2 4F RT A16WE 1999082700318 19990827 00318 NM 1999 8 27 SWAA991377 1 19990818 A 5330 6545890 SKIN BOEING 737 7373Q8 1384670 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN AT FWD ENTRY DOOR AFT LOWER CORNER CUT OUT. REPAIRED SKIN PER SWA RA NR 1-353-2144. 2 L 7 2 4F RT A16WE 1999082700319 19990827 00319 NM 1999 8 27 SWAA991384 1 19990819 A 3020 470963 DUCT BOEING 737 7372H4 138448C NM NR 2 ENGINE CRACKED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 085SW 22826 AIR TURNBACK, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB. REMOVED AND REPLACED CRACKED NR 2 ENG RT INLET ANTI- ICE DUCT PER MM. 2 L 7 2 4F A16WE 1999082700320 19990827 00320 NM 1999 8 27 SWAA991385 1 19990819 A 5312 963820 BULKHEAD CHORD BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND LEFT SIDE CHORD CRACKED, BS 178, LBL 29. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 1999082700321 19990827 00321 NM 1999 8 27 SWAA991386 1 19990819 A 5230 6549889 FRAME BOEING 737 7372T4 1384492 NM CARGO DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CORROSION ON FWD CARGO DOOR FRAME, BS 492. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999082700322 19990827 00322 NM 1999 8 27 SWAA991387 1 19990818 A 5330 6552880 SKIN BOEING 737 7373Q8 1384670 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE FUSELGE SKIN CUT OUT CRACKED (VERIFIED WITH HFEC INSP). R EPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999082700323 19990827 00323 NM 1999 8 27 SWAA991388 1 19990818 A 3350 07912 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED C3 CHECK, FOUND FWD END OF EEPLS TRACK LOOSE AND LENS MISSING. SECURED TRACK AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999082700324 19990827 00324 NM 1999 8 27 SWAA991389 1 19990818 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 17 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK SECTION MISSING AT ROW 17. REPLACED SECTION PER MM. 2 L 7 2 4F RT A16WE 1999082700325 19990827 00325 NM 1999 8 27 SWAA991382 1 19990818 A 3350 100885 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED A2 CHECK, FOUND EEPLS BATTERY PACK INOP, RT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999082700326 19990827 00326 NM 1999 8 27 SWAA991383 1 19990819 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 399WN 27693 EEPLS LIGHTING LOOSE. SECURED LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999082700327 19990827 00327 NM 1999 8 27 SWAA991357 1 19990814 A 3230 6558206 SENSOR CABLE BOEING 737 7373H4 1384600 NM RT MLG OUT OF ADJUST A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 613SW 27931 AIR TURNBACK, GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. RIGGED MLG GROUND SHIFT SENSOR CABLE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999082700328 19990827 00328 NM 1999 8 27 SWAA991358 1 19990813 A 5753 6573732 SKIN BOEING 737 7372H4 138448C NM LT TE MIDFLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING REPAIR OVERNIGHT, FOUND LT WING OUTBOARD MIDFLAP, INBOARD TRACK CUT OUT TORN AND CRACKED. REPAIRED PER SWA RA NR 1-257-0736. 2 L 7 2 4F A16WE 1999082700329 19990827 00329 NM 1999 8 27 SWAA991359 1 19990813 A 5320 6546567 FRAME BOEING 737 7373Y0 1384671 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/2D CHECK, FOUND AFT GALLEY DOOR FUSELAGE CUT OUT FWD FRAME CRACKED AT STRINGER 12R. REMOVED AND REPL ACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999082700330 19990827 00330 NM 1999 8 27 SWAA991360 1 19990814 A 3350 A1170033 STRAP BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 EMERGENCY FLASH LIGHT SECURING STRAP BROKEN ON FWD END OF CABIN. REMOVED AND REPLACED STRAP PER MM. 2 L 7 2 4F RT A16WE 1999082700331 19990827 00331 NM 1999 8 27 SWAA991361 1 19990815 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA EMERGENCY EXIT LIGHTS INOP RT CENTER CABIN. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F A16WE 1999082700332 19990827 00332 GL 1999 8 27 99ZZZX3064 1 19990728 A 7930 3014794 WARNING LIGHT BEECH 90 C90 1152913 CE PWA PT6 PT6A20 52043 EA CHIP DETECTOR ILLUMINATED A S2KA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 03 183SA 525 LJ5718 PCE22639 RIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT WAS EN ROUTE TO PICK UP PASSENGERS. AIRCRAFT RETU RNED TO HOME BASE. DOM REMOVED CHIP DETECTOR AND FOUND TINY SLIVERS OF METAL ACROSS CONTACTS. SPECIAL OIL SAMPLE TAKEN AND SENT TO LAB. OPERATIONAL CHECK OF CHIP DETECTOR COMPLETED. ENGINE RUN-UP AND LEAK CHECK FOUND OK. WILL RESMAPLE IN 10 FLIGHT HOURS. 1 L 7 2 3T 3 T 3A20 E4EA 1999082700335 19990827 00335 CE 1999 8 27 99ZZZX3067 1 19990721 A 2820 LINE BEECH 58 58 1152740 CE LT ENGINE LEAKING A BSYA O OTHER K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 33DK TH372 MKE - LEFT ENGINE SHUT DOWN ON ROLL-OUT. FUEL LEAK AT FLOW DIVIDER LINE. REPAIRED FUEL LINE. OPS CHECKS GOOD. 1 L 7 2 3O 3A16 1999082700336 19990827 00336 CE 1999 8 27 99ZZZX3068 1 19990713 A 3246 WHEEL BEECH 58 58 1152740 CE NLG WW FREE TO SPIN A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 400RP TH319 AGC - PILOT REPORTS NOISE AFTER GEAR RETRACTION, RETURNED TO AGC. JACKED AIRCRAFT, FOUND NOSE WHEEL FREE SO AS TO SPIN FOR A LONG PERIOD OF TIME AFTER GEAR RETRACTION. 1 L 7 2 3O 3A16 1999082700337 19990827 00337 EA 1999 8 27 99ZZZX3069 2 19990706 A 7200 ENGINE PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1F5 41532 EA RIGHT MALFUNCTIONED A BSYA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 6076L 7137961221 L1797448A CMH - ON TAKEOFF, RIGHT ENGINE LOST POWER. INSPECTED INDUCTION, IGNITION, AND FUEL SYSTEMS, NO FAULTS FOUND. GROUND RU N, OK. RETURNED TO SERVICE. 1 M 7 2 3O 3 O RT A17WE 1E4 1999082700338 19990827 00338 CE 1999 8 27 99ZZZX3070 1 19990702 A 5620 WINDOW 08911077 CESSNA 310 310R 2074245 CE EMERGENCY EXIT SEPARATED A BSYA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 GL 07 5113J 310R0233 SMX - EMERGENCY EXIT CAME OUT OF AIRCRAFT DURING FLIGHT. TEMPORARILY, INSTALLED EMERGENCY EXIT AND FERRIED AIRCRAFT TO MSY MAINTENANCE BASE FOR PERMENENT REPAIR. 1 L 7 2 3O 3A10 1999082700339 19990827 00339 CE 1999 8 27 99ZZZX3071 1 19990702 A 3260 15E13 SWITCH CESSNA 310 310R 2074245 CE RT MLG FAILED A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 28NT 310R0243 FAT - NO RIGHT GEAR DOWN AND LOCK INDICATION. REMOVED AND REPLACED DEFECTIVE DOWN AND LOCK SWITCH. OPS CHECKS GOOD. 1 L 7 2 3O 3A10 1999082700340 19990827 00340 EA 1999 8 27 99ZZZX3072 2 19990701 A 7322 RSA103D1 FUEL SERVO PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA RT ENGINE MALFUNCTIONED A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 8073J 600596180 L1827748A BOL - RT ENGINE SWAGING ON TAKEOFF. RETURNED TO BOL. REMOVED AND REPAIRED FUEL SERVO. OPS CHECKS GOOD. 1 M 7 2 3O 3 O RT A17WE 1E4 1999082700374 19990827 00374 WP 1999 8 27 99ZZZX3106 1 19990811 A 3350 08163000603 LIGHT BRUCE DOUG DC9 DC932 3022066 WP BS 578 LOOSE A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 35 930BB 47521 EMERGENCY ESCAPE PATH TRACK COVER LOOSE (FORWARD OF FORWARD EMERGENCY OVERWING EXIT DOOR). RE-SECURED EMERGENCY TRACK C OVER IAW BRUCE INDUSTRIES INSTALLATION MANUAL 33-21-27. (X) 2 L 7 2 4F A6WE 1999082700375 19990827 00375 EU 1999 8 27 A6WA9900078 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 3C CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN ON SEAT 3C IS CRACKED. REPLACED SEAT PAN 3C. (X) 2 H 7 4 4F RT A49EU 1999082700376 19990827 00376 EU 1999 8 27 A6WA9900077 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 4A CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PANS 4A AND 4C ARE CRACKED. REPLACED SEAT PANS 4A AND 4C. REF: OPERATOR CONTROL NR 99ZZZX3107. (X) 2 H 7 4 4F RT A49EU 1999082700377 19990827 00377 EU 1999 8 27 99ZZZX3107 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 4C CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PANS 4A AND 4C ARE CRACKED. REPLACED SEAT PANS 4A AND 4C. REF: OPERATOR CONTROL NR A6WA9900077. 2 H 7 4 4F RT A49EU 1999082700378 19990827 00378 1999 8 27 A6WA9900059 4 19990618 A 3432 BRACKET BAG BAE146 BAE146200A 1500266 EU GS ANTENNA CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 LEFT GLIDESLOPE ANTENNA BRACKET IS CRACKED. REPLACED ANTENNA BRACKET. (X) 2 H 7 4 4F RT A49EU 1999082700379 19990827 00379 EU 1999 8 27 A6WA9900060 1 19990617 A 5230 STRUCTURE BAG BAE146 BAE146200A 1500266 EU CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 AFT CARGO DOOR, AFT UPPER HINGE POINT IS CRACKED. REPAIRED CRACKS IAW BAE REPAIR NR HC523H9001. RE-PROFILED AFT BOTTOM SEAL CAGE. (X) 2 H 7 4 4F RT A49EU 1999082700380 19990827 00380 EU 1999 8 27 A6WA9900066 1 19990607 A 5720 FASTENER BAG BAE146 BAE146200A 1500266 EU LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 PERFORMED RIL HC571H9033 LEFT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H9033 TO LEFT RIB 2 JO-BOLT REPLACEMENT. (X) 2 H 7 4 4F RT A49EU 1999082700381 19990827 00381 EU 1999 8 27 A6WA9900067 1 19990607 A 5320 STIFFENER BAG BAE146 BAE146200A 1500266 EU BS 25.94 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 FROM EO E95/003/653 STIFFENERS ON FORWARD SIDE FRA 29 STA 25.94 LEFT AND RIGHT AND 31.13 LEFT AND RIGHT HAVE ONE A-BOLT HOLE CRACKED. EO E95/005/653 NEEDS COMPLIANCE AT CRACKED LOCATIONS. REPAIRED STIFFENERS AT FRA 29 STATIONS LEFT AND RI GHT 25.94 AND 31.13 IAW AWAC EO E95-005-653 REV A. (X) 2 H 7 4 4F RT A49EU 1999082700382 19990827 00382 EU 1999 8 27 A6WA9900068 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 15D CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 15D IS CRACKED. REPLACED SEAT PAN 15D. (X) 2 H 7 4 4F RT A49EU 1999082700383 19990827 00383 EU 1999 8 27 A6WA9900069 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 13D CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 13D IS CRACKED. REPLACED SEAT PAN 13D. (X). 2 H 7 4 4F RT A49EU 1999082700384 19990827 00384 EU 1999 8 27 A6WA9900070 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 10D CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 10D IS CRACKED. REPLACED SEAT PAN 10D. (X) 2 H 7 4 4F RT A49EU 1999082700385 19990827 00385 EU 1999 8 27 A6WA9900071 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 8F CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 8F IS CACKED. REPLACED SEAT PAN 8F. (X) 2 H 7 4 4F RT A49EU 1999082700386 19990827 00386 EU 1999 8 27 A6WA9900072 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 7D CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PANS 7D AND 7F ARE CRACKED. REPLACED SEAT PAN 7D AND 7F. REF: OPERATOR CONTROL NR 99ZZZX3108. (X) 2 H 7 4 4F RT A49EU 1999082700387 19990827 00387 EU 1999 8 27 99ZZZX3108 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 7F CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PANS 7D AND 7F ARE CRACKED. REPLACED SEAT PAN 7D AND 7F. REF: OPERATOR CONTROL NR A6WA9900072. 2 H 7 4 4F RT A49EU 1999082700388 19990827 00388 EU 1999 8 27 A6WA9900073 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 1D CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 1D IS CRACKED. REPLACED SEAT PAN 1D. 2 H 7 4 4F RT A49EU 1999082700389 19990827 00389 EU 1999 8 27 A6WA9900074 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 10A CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 10A AND 10C ARE CRACKED. REPLACED SEAT PANS 10A AND 10C. REF: OPERATOR CONTROL NR 99ZZZX3109. (X) 2 H 7 4 4F RT A49EU 1999082700390 19990827 00390 EU 1999 8 27 99ZZZX3109 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 10C CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 10A AND 10C ARE CRACKED. REPLACED SEAT PANS 10A AND 10C. REF: OPERATOR CONTROL NR A6WA9900074. 2 H 7 4 4F RT A49EU 1999082700391 19990827 00391 EU 1999 8 27 A6WA9900075 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 9A CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 9A IS CRACKED. REPLACED SEAT PAN 9A. (X) 2 H 7 4 4F RT A49EU 1999082700392 19990827 00392 EU 1999 8 27 A6WA9900076 1 19990609 A 2520 SEAT BAG BAE146 BAE146200A 1500266 EU ROW 7C CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 SEAT PAN 7C IS CRACKED. REPLACED SEAT PAN 7C. (X) 2 H 7 4 4F RT A49EU 1999082700393 19990827 00393 EU 1999 8 27 A6WA9900058 1 19990605 A 5240 DOOR BAG BAE146 BAE146200A 1500266 EU LAV SERVICE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 FORWARD LAVATORY SERVICE DOOR CRACKED NEAR HINGE AREA. REPAIRED IAW BAE FAX REF NR BARA/AVR/3589/99. (X) 2 H 7 4 4F RT A49EU 1999082700394 19990827 00394 EU 1999 8 27 A6WA9900057 1 19990623 A 2720 LIGHT BAG BAE146 BAE146200A 1500266 EU RUDDER ILLUMINATED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 608AW E2049 DEN - FLT 5669 - AFTER TAKEOFF, RUDDER LIMITER LIGHT ILLUMINATED ON MWS PANEL. LIGHT EXTINGUISHED ON SHORT FINAL. PERF ORMED OPS CHECK OF AIR SPEED SWITCH IAW BAE AMM 27-21-61. 2 H 7 4 4F RT A49EU 1999082700395 19990827 00395 EU 1999 8 27 A6WA9900045 1 19990523 A 2910 HD51127710 O-RING BAG BAE146 BAE146200A 1500266 EU YELLOW HYD SYS FAILED A A6WA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 156TR E2156 LEX/ORD - FLT 5605 - PARKED AT THE GATE IN ORD, FLIGHT ATTENDANT REPORTED CABIN FILLED WITH SMOKE, CFR AT ORD NOTIFIED. REPLACED O-RING ON YELLOW SYSTEM HYDRAULIC PRESSURE FILTER HOUSING. NOTE: CABIN FILLED WITH HYDRAULIC MIST, NOT SMOKE AS REPORTED BY FLIGHT ATTENDANT. (X) 2 H 7 4 4F RT A49EU 1999082700396 19990827 00396 EU 1999 8 27 A6WA9900061 1 19990607 A 5720 FASTENER BAG BAE146 BAE146200A 1500266 EU RT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 PERFORMED RIL HC571H9033, RT RIB 0 JO BOLTS. C/W RIL - HC571H9033 TO RT CENTER TANK RIB 0 JO-BOLT REPLACEMENT. (X) 2 H 7 4 4F RT A49EU 1999082700397 19990827 00397 EU 1999 8 27 A6WA9900062 1 19990607 A 5720 FASTENER BAG BAE146 BAE146200A 1500266 EU RT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 PERFORMED RIL HC571H9033 ON RT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H0933 RT RIB 2 CENTER TANK SIDE JO-BOLT REPLACEMENT . (X) 2 H 7 4 4F RT A49EU 1999082700398 19990827 00398 EU 1999 8 27 A6WA9900063 1 19990607 A 5720 FASTENERS BAG BAE146 BAE146200A 1500266 EU RT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 PERFORMED RIL HC571H9033 RT RIB 2 OUTBOARD JO-BOLTS. C/W RIL HC571H0933 RT WING SIDE OF RIB 2 JO-BOLT REPLACEMENT. (X) 2 H 7 4 4F RT A49EU 1999082700399 19990827 00399 EU 1999 8 27 A6WA9900064 1 19990607 A 5720 FASTENER BAG BAE146 BAE146200A 1500266 EU LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 PERFORMED RIL HC571H9033 LT CENTER TANK RIB 0 JO-BOLTS. C/W RIL HC571H9033 TO LEFT CENTER TANK RIB 0 JO-BOLT REPLACEMEN T. (X) 2 H 7 4 4F RT A49EU 1999082700400 19990827 00400 EU 1999 8 27 A6WA9900065 1 19990607 A 5720 FASTENER BAG BAE146 BAE146200A 1500266 EU LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 PERFORMED RIL HC571H9033 LEFT RIB 2 INBOARD JO-BOLTS. C/W RIL HC571H9033 TO ABOVE LEFT RIB 2 JO-BOLT REPLACEMENT. (X) 2 H 7 4 4F RT A49EU 1999082700401 19990827 00401 EU 1999 8 27 A6WA9900047 1 19990530 A 3241 AE20556 COMPUTER BAG BAE146 BAE146200A 1500266 EU ANTI SKID SYSTEM FAILED A A6WA O OTHER O OTHER LD LANDING 1 GL 31 181US 7 E2042 DURING LANDING ROLL-OUT, APPLIED GREEN BRAKES, NO BRAKING ON LEFT SIDE, SWITCHED TO YELLOW BRAKES, NO BRAKES UNTIL 15 SE CONDS AFTER WHEEL SPIN-UP. REMOVED AND REPLACED ANTI-SKID COMPUTER. PART TOTAL CYCLES: 10. (X) 2 H 7 4 4F RT A49EU 1999082700402 19990827 00402 EU 1999 8 27 A6WA9900046 1 19990527 A 3246 BEARING BAG BAE146 BAE146200A 1500266 EU LT MLG FAILED A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 607AW E2052 REMOVED NR 1 TIRE ASSY, FOUND NR 1 WHEEL INNER BEARING SEIZED ONTO THE AXEL. REMOVED AND REPLACED LEFT MLG AXEL, WHEELS AND NR 1 HEAT PACK AND BRAKE. NR 1 BRAKE P/N AHA1413, SN HB182 TMS 2861. CYCLES 3,131. NR 1 CARBON HEAT PACK PN AH09 068, SN AWAC170. TMS 478. CYCLES, 544. NR 1 WHEEL PN AHA1489 SN GT145, TMS 342. CYCLES, 412. (X) 2 H 7 4 4F RT A49EU 1999082700403 19990827 00403 EU 1999 8 27 A6WA9900055 1 19990421 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 UPPER WING SKIN TRAILING EDGE STIFFENER IS CRACKED AT FORWARD END LOCATED BETWEEN RIBS 9 AND 10, LEFT WING. REPAIRED LT WING SKIN TRAILING EDGE UPPER WING SKIN STIFFENER BETWEEN RIBS 9 AND 10 IAW BAE FAX DJR/RJ0630-98. (X) 2 H 7 4 4F RT A49EU 1999082700404 19990827 00404 EU 1999 8 27 A6WA9900054 1 19990507 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA O OTHER O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 176 BEWEEN RIBS 7 AND 8 CRACKED, FORWARD END. REPLACED LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8. (X) 2 H 7 4 4F RT A49EU 1999082700405 19990827 00405 EU 1999 8 27 A6WA9900053 1 19990507 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 176 BETWEEN RIBS 7 AND 8, CRACKED FORWARD END. REPAIRED RT WIN G TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8 IAW BAE FAX DJR/RJ0630-98. (X) 2 H 7 4 4F RT A49EU 1999082700406 19990827 00406 EU 1999 8 27 A6WA9900052 1 19990507 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 172 BETWEEN RIBS 3 AND 4, CRACKED FORWARD END. REPLACED RT WIN G TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 3 AND 4. (X) 2 H 7 4 4F RT A49EU 1999082700407 19990827 00407 EU 1999 8 27 A6WA9900051 1 19990507 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 178 BETWEN RIBS 8 AND 9, CRACKED FORWARD END. REPLACED LT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 8 AND 9. (X) 2 H 7 4 4F RT A49EU 1999082700408 19990827 00408 EU 1999 8 27 17WA9900050 1 19990507 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA O OTHER O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 177 BETWEEN RIBS 8 AND 9 CRACKED FORWARD END. REPAIRED LEFT WING SKIN TRAILING EDGE, UPPER WING SKIN TRAILING EDGE STIFFENER BETWEEN RIBS 8 AND 9 IAW BAE FAX DJR/RJ0630-98. (X) 2 H 7 4 4F RT A49EU 1999082700409 19990827 00409 EU 1999 8 27 A6WA9900049 1 19990529 A 5210 ANGLE BAG BAE146 BAE146100A 1500260 EU PASSENGER DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD PASSENGER DOOR, INTERNAL ANGLE CRACKED. REPLACED ANGLE. (X) 2 H 7 4 4F RT A49EU 1999082700410 19990827 00410 EU 1999 8 27 A6WA9900048 1 19990529 A 5330 SKIN BAG BAE146 BAE146100A 1500260 EU FUSELAGE DAMAGED A A6WA O OTHER O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 REPAIR TO RIGHT SIDE OF FUSELAGE AT FRAMES 11-13 AT LAP 'E' AREA. C/W REPAIR IAW BAE 146 SRM AND FAX CW/RJ/0754-99, CW/ RJ/0761-99 AND DRAWING HC537H9411. (X) 2 H 7 4 4F RT A49EU 1999082700411 19990827 00411 EU 1999 8 27 A6WA9900042 1 19990510 A 2620 58111011 FLOW VALVE BAG BAE146 BAE146200A 1500266 EU FIRE EXTINGUISH FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 DURING E.O. INSPECTION, VALVE FAILED STEP 3. FLAP VALVE MOVED COMPLETELY FREE WITH NO DAMPING ACTION ABOUT THE HOLLOW R IVET. REMOVED AND REPLACED VALVE ASSY. (X) 2 H 7 4 4F RT A49EU 1999082700412 19990827 00412 EU 1999 8 27 A6WA9900041 1 19990329 A 2620 58111011 CONTROL VALVE BAG BAE146 BAE146200A 1500266 EU FIRE EXTINGUISH FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US E2042 WHILE C/W EO E94/001/626, FOUND FIRE EXTINGUISHER DIRECTIONAL CONTROL VALVE UNSERVICEABLE DUE TO A FAULTY FLAPPER. REPL ACED DIRECTIONAL CONTROL VALVE. (X) 2 H 7 4 4F RT A49EU 1999082700413 19990827 00413 EU 1999 8 27 A6WA9900080 1 19990720 A 2760 FEEDBACK POT BAG BAE146 BAE146200A 1500266 EU AIRBRAKES FAILED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 183US E2043 DURING TAKEOFF ROLL, AIRBRAKE LIGHT CAME ON WITH CONFIG WARING. CYCLED AIRBRAKE SEVERAL TIMES, AIRBRAKE LIGHT COMES ON INTERMITTENT. REPLACED AIRBRAKE FEEDBACK POT, OPS CHECKED GOOD ON GROUND. (X) 2 H 7 4 4F RT A49EU 1999082700414 19990827 00414 EU 1999 8 27 A6WA9900088 1 19990630 A 5330 SKIN BAG BAE146 BAE146300A 1500267 EU FRAMES 35-36 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW E3132 THERE IS A 2.75 INCH CRACK IN LT FUSELAGE BETWEEN FRAMES 35 AND 36 AT STR 19, 6 INCHES FORWARD OF FRAME 38. CRACK RUNS STRAIGHT ALONG EDGE OF INNER LAP JOINT. REPAIRED SAID CRACK BY CUTTING OUT DAMAGE AND RIVETING PATCH IAW BAE FAX REF BA RA/AVRO/3667/99 DATED JULY 6, 1999. (X) 2 H 7 4 4F RT A49EU 1999082700415 19990827 00415 EU 1999 8 27 A6WA9900087 1 19990702 A 5320 WEB BAG BAE146 BAE146300A 1500267 EU NLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW E3132 NOSE LANDING GEAR SIDEWALL DIAPHRAGM CRACKED AT UPPER PIN BOSS. REPLACED LT NOSE GEAR DIAPHRAGM IAW BARA/AVRO/3677/99. (X) 2 H 7 4 4F RT A49EU 1999082700416 19990827 00416 EU 1999 8 27 A6WA9900086 1 19990721 A 2560 D31050105 COVER BAG BAE146 BAE146300A 1500267 EU DOOR SLIDE MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW 8747 0340 E3132 UPON REMOVAL OF LEFT FORWARD EVACUATION SLIDE, FOUND D-SHACKLE ASSY MISSING. INSTALLED LT FORWARD EVAC SLIDE. C/W COVE R LATCH PULL CHECK AND BATTERY EFFICIENCY CHECK. BOTH CHECKS FOUND WITHIN REQUIRED PARAMETERS. ALL WORK ACOMPLISHED I AW BAE MM AND AIR CRUISERS CMM. CLEVIS AND PIN INSTALLED. SN OFF 0340. PART TC: 10,434. (X) 2 H 7 4 4F RT A49EU 1999082700417 19990827 00417 EU 1999 8 27 A6WA9900085 1 19990707 A 5320 FASTENER BAG BAE146 BAE146300A 1500267 EU RT MLG WW FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW E3132 RIGHT MLG BAY, ON EACH FASTENER BROKEN IN MAIN BEAM TO SIDESTAY AT FRAME 29, FASTENER JUST INBOARD APPEARS TO BE LOOSE. REPLACED ONE EACH BROKEN HI-LOC. REMOVED HI-LOC FASTENER JUST INBOARD OF BROKEN FASTENER. CLEANED AND INSPECTED HOLE, HOLE FOUND OK, REPLACED HI-LOC FASTENER. (X) 2 H 7 4 4F RT A49EU 1999082700418 19990827 00418 EU 1999 8 27 A6WA9900084 1 19990702 A 5400 BOLT BAG BAE146 BAE146300A 1500267 EU NR 3 PYLON FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW E3132 NR 2 ENGINE PYLON TO WING, OUTBOARD LOWER BOLT HAD IS SHEARED OFF. REPLACED LOWER OUTBOARD WING TO PYLON BOLT IAW MM 54 -52-00. (X) 2 H 7 4 4F RT A49EU 1999082700419 19990827 00419 NM 1999 8 27 A6WA9900083 1 19990726 A 5610 SDSD0328221A WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT CRACKED A A6WA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 328PH 3006 DEN - FLT 7143 - CAPTAIN'S WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSCREEN. RETURNED TO DEN. (X) 2 H 7 2 4T RT A45NM 1999082700420 19990827 00420 EU 1999 8 27 A6WA9900082 1 19990724 A 5270 SWITCH BAG BAE146 BAE146200A 1500266 EU LOWER DOORS DIRTY A A6WA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 607AW E2052 LOWER DOOR NOT SHUT ON MWS PANEL, CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF AND VERIFIED ALL DOORS SHUT. CLEANED AN D INSPECTED LOWER DOOR SWITCHES, ALL CHECKED GOOD. (X) 2 H 7 4 4F RT A49EU 1999082700421 19990827 00421 1999 8 27 VTZA99030 4 19990718 A 3442 7008470922 RADAR JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 302UE 41013 IAD/PIT - FLT 7385 - DURINB CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO WX RADAR INOPERABLE. AIRCRAFT RETURNED T O GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EX RWX RADAR R/T. OPS CHECK OK. AIRCR AFAT WAS RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082700422 19990827 00422 EU 1999 8 27 VTZA990229 1 19990718 A 7712 TQ INDICATION JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE MALFUNCTIONED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 323UE 41059 IAD/PIT - FLT 7387 - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SWITCHED RT ENGINE TORQUE BRIDGE FROM NR 1 TO NR 2 AND GROUND RAN AIRCRAFT. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082700423 19990827 00423 EU 1999 8 27 VTZA990236 1 19990724 A 2425 7011672111 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 306UE 41020 IAD/ALB - FLT 7182 - DURING TAKEOFF, CREW ABORTED TAKEOFF DUE TO CAPTAIN'S SYMBOL GENERATOR FAILED. AIRCRAFT RETURNED T O GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND AND REPLACED SYMBOL GENERATOR. OPS CHECK OK. A IRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999082700424 19990827 00424 NE 1999 8 27 VTZA990235 2 19990720 A 7320 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE OUT OF ADJUST A VTZA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 302UE 41013 IAD/CHO - FLT 7327 - DURING TAKEOFF, ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING SCHEDULED TORQUE. MAINTENANCE ADJUSTED RIGHT MAXIMUM FLOW. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082700425 19990827 00425 NE 1999 8 27 VTZA990234 2 19990720 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT FAILIURE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 322UE 41058 DLM/IAD - FLT 7368 - DURING CRUISE, CREW MADE AN UNSCHEDULED LANDING AND RETURNED TO DLM AFTER DECLARING AN EMERGENCY DU E TO LT OIL CONTAMINATION INDICATION AND OIL PRESSURE LOSS INDICATION. MAINTENANCE REMOVED AND REPLACED LT ENGINE. C/W PERFORMANCE RUNS. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999082700426 19990827 00426 NM 1999 8 27 A6WA9900056 1 19990530 A 5220 001A522A0350202 SEAL DORNER DO32 DO328100 2996000 NM COCKPIT FAILED A A6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 31 328PH 3006 DEN - FLT 7075 - SMELL BURNING INSULATION OF ELECTRICAL WIRES INSIDE COCKPIT. FOUND ESCAPE HATCH SEAL LEAKING WATER WHI CH SHORTED SEVERAL OVERHEAD PANELS. REMOVED AND REPLACED OVERHEAD ESCAPE HATCH SEAL AND AFFECTED PANELS. AIR RETURN TO DENVER. (X) 2 H 7 2 4T RT A45NM 1999082700427 19990827 00427 NM 1999 8 27 TWAA9911401 1 19990821 A 2910 BACH8A06NN0300T HYD LINES BOEING 727 727231 1384079 NM RT MLG DOOR LEAKING A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 54341 21628 DURING GEAR RETRACTION AFTER TAKEOFF HAD COMPLETE LOSS OF THE -A- HYDRAULIC SYSTEM. MANUALLY EXTENDED GEAR AND USED ALT ERNATE FLAP EXTENSION. RETURNED TO SAT. FOUND THE RT LANDING GEAR DOOR OPEN AND CLOSE HYD LINES LEAKING. REPLACED THE OPEN LINE BACH8A06NN0300T AND CLOSE LINE BACH30AT08K0310. CHECK-C 1-2-99 MCI. 2 L 7 3 4F A3WE 1999082700428 19990827 00428 NE 1999 8 27 TWAA9911402 2 19990820 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENGINE STALLED A TWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 906TW 49160 1209 THE LEFT ENGINE HAD TWO COMPRESSOR STALLS ON TAKEOFF. RETARDED THROTTLE AND SLOWLY ADVANCED THROTTLE AGAIN, STILL STALL ED. ENG RAN OK AT 1.4 EPR. FLIGHT RETURNED TO SLC. FOUND HONEYCOMB LOOSE IN COLD STREAM, TWO HOLES IN COMPRESSOR CASE AND ONE HOLE IN TURBINE CASE. NO PENETRATION OF ENGINE COWLING. ENGINE WAS REPLACED. CHECK-C 1-28-99 STL. 2 L 7 2 4F 4 F A6WE E9NE 1999082700429 19990827 00429 NM 1999 8 27 TWAA9911403 1 19990822 A 3397 WIRE BOEING 767 7673Q8 1385142 NM ROW 2 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT SEAT ROWS 1 AND 2, LEFT SIDE OF CABIN. ATTACHED LOOSE WIRE TO THE LIGHT SOC KET AT ROW 2, LT SIDE OF CABIN. CHECK-C 6-30-99 LAX. 2 L 7 2 4F RT A1NM 1999082700430 19990827 00430 WP 1999 8 27 TWAA9911404 1 19990820 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 996Z 47028 DURING PREFLIGHT CHECK FOUND THE FIRST CLASS AND FIRST SECTION OF COACH EGRESS LIGHTS WERE INOPERATIVE. DRIED WATER FRO M INSIDE THE TRACK. CHECK-C 11-25-98 STL. 2 L 7 2 4F A6WE 1999082700431 19990827 00431 EU 1999 8 27 MALA976548 1 19990818 A 7931 IPTE1191000200 TRANSDUCER SAAB SF340 340B 7860101 EU RT PROP FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 453XJ 453 AFTER DEPARTING GPZ RECEIVED RIGHT PROP OIL PRESSURE WARNING, VERIFIED GAUGE INDICATING LOW PRESSURE, FLUX BETWEEN 5-30 PSI. AIRCRAFT RETURNED TO GPZ. MAINTENANCE REPLACED RT PGB OIL PRESSURE TRANSDUCER. OPS & LEAKS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999082700432 19990827 00432 EU 1999 8 27 JBXA9900100 1 19990821 A 3246 5011166 WHEEL FOKKER F28 F28MK0100 4990807 EU MLG CRACKED A JBXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 05 105ML 11475 ON TAXI OUT CREW FELT SHIMMY IN TAIL OF AIRCRAFT. MAINTENANCE INSPECTED AND FOUND OUTER WHEEL BEARING JOURNAL ON NR 3 M AIN WHEEL HEAT DAMAGED AS A RESULT OF WHEEL FAILURE. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 MAIN WHEEL ASSY AND REMOVED AND REPLACED NR 3 BRAKE ASSY IAW AMM. AIRCRAFT INSPECTED PER MESSIER LANDING GEAR LETTER AND ISSUED FERRY PERM IT TO MAINTENANCE STATION. 2 L 7 2 4F RT 1999082700433 19990827 00433 EU 1999 8 27 AWXA9900269 1 19990817 A 2120 AIR DIST AIRBUS 320 A320231 3930325 EU CABIN ODOR A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 634AW 091 SMELL OF LACQUER FROM ROW 23. FLIGHT ATTENDANTS COMPLAIN OF LIGHT HEADED, HEADACHE AND NAUSEA. AFT RECIRCULATION FAN S HUTDOWN, SMELL SEEMED TO DISSIPATE. COULD NOT DUPLICATE. RAN RECIRCULATION FANS MORE THAN 1 HOUR. NO UNUSUAL SMELLS, NO EVIDENCE OF SPILLAGE, CARPET AND CUSHIONS DRY. NO HISTORY THE PAST 30 DAYS AND NO HISTORY 7 DAYS AFTER. 2 L 7 2 4F RT A28NM 1999082700434 19990827 00434 WP 1999 8 27 CALA9901071 1 19990819 A 5321 FLOOR DOUG DC10 DC1030 3023501 WP CABIN DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND FLOOR PANEL 283KF DELAMINATED WITH CORRODED FERRULES. A NEW FLOOR PANEL WAS INSTALLED IAW GMM 10-100-0 1. 2 L 7 3 4F A22WE 1999082700435 19990827 00435 NM 1999 8 27 CALA9901072 1 19990819 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND A .75 INCH CRACK IN STRINGER 16R AT BS 500C. THE CRACKED SECTION OF STRINGER WAS REMOVED AND A NEW SEC TION WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 1999082700436 19990827 00436 NM 1999 8 27 CALA9901073 1 19990819 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND MAIN DECK FLOORBEAM IN AFT CARGO COMPARTMENT CORRODED AT STA 1130 FROM BL 0 TO RBL 30. REPAIRED IAW SR M 53-10-8 AND ECRA 5310-03898. 2 L 7 3 4F A3WE 1999082700437 19990827 00437 NM 1999 8 27 CALA9901074 1 19990820 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 344-360 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND FUSELAGE SKIN DENTED FROM STA 344-360, WL 190R. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURES 201, 202, AND 223. 2 L 7 2 4F RT A16WE 1999082700438 19990827 00438 NM 1999 8 27 CALA9901075 1 19990820 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND CABIN FLOORBEAM UPPER SURFACE CORRODED AT STA 294 FROM LBL 20 TO RBL 30. THE CORRODED SECTION OF FLOOR BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED USING SPLICE ANGLES IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999082700439 19990827 00439 WP 1999 8 27 CALA9901076 1 19990820 A 5313 STRINGER DOUG DC9 DC982 3022082 WP BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT BS 500C. A STRINGER SPLICE REPAIR WAS INSTALLED IAW SRM 53-00-03, FI GURE 201. 2 L 7 2 4F A6WE 1999082700440 19990827 00440 NM 1999 8 27 CALA9901077 1 19990822 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND RT I/B SEAT TRACK CORRODED FROM STA 328-344. REPAIRED IAW SRM 53-00-52, FIGURE 202, SHEET 1. 2 L 7 2 4F RT A16WE 1999082700441 19990827 00441 NM 1999 8 27 CALA9901078 1 19990822 A 3397 WIRE BOEING 737 7373Q8 1384670 NM ROW 18 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14381 26310 INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 18 ABC. MAINTENANCE FOUND CONNECTOR END PULLED FROM HARNESS. R EMOVED AND REPLACED WIRE ASSEMBLY AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999082700442 19990827 00442 WP 1999 8 27 CALA9901079 1 19990823 A 5320 END CAP DOUG DC10 DC1030 3023501 WP BS 889 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND FORWARD CARGO BAY STRINGER 44R END CAP CORRODED AT STA 889. THE END CAP WAS REPAIRED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1999082700443 19990827 00443 SO 1999 8 27 COMA9910136 1 19990818 A 7312 10818D FUEL HEATER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A COMA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 269CA 16974 451 120263 FUEL LEAKING FROM LEFT ENGINE. REPLACED THE FUEL HEATER. 2 L 7 2 4T 4 T RT A31SO E20NE 1999082700444 19990827 00444 NE 1999 8 27 COMA9910137 2 19990819 A 7510 38E966A REGULATOR EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT LEAKING A COMA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 268CA 120262 RIGHT HAND BLEED AIR DUCT LEAK WARNING. REPLACED THE DEICE REGULATOR. 2 L 7 2 4T 4 T RT A31SO E20NE 1999082700445 19990827 00445 SO 1999 8 27 COMA9910138 1 19990819 A 2750 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTIONED A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 179CA 373 120179 FLAP CONTROL FAULT. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1999082700446 19990827 00446 NE 1999 8 27 COMA9910139 2 19990821 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT & RT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 463CA 120267 LEFT AND RIGHT ENGINES FAIL TO ACHIEVE CHARTED TORQUE. CND ENGINES PERFORM NORMAL DURING GROUND RUNS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999082700447 19990827 00447 EA 1999 8 27 COMA9960457 1 19990818 A 3020 WARNING CNDAIR CL600 CL6002B19 EA ANTI ICE DUCT ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 785CA 7326 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999082700448 19990827 00448 EA 1999 8 27 COMA9960458 1 19990819 A 3020 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA RT STALL HEAT TRIPPED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 920CA 7022 RIGHT HAND STALL HEAT CAUTION MESSAGE. RESET CIRCUIT BREAKER SYSTEM, TEST NORMAL. 2 L 7 2 4F RT A21EA 1999082700449 19990827 00449 NE 1999 8 27 COMA9960459 2 19990821 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT LEAKING A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 947CA 11650 7077 807070 AFTER ENGINE WAS CHANGED, AN OIL SMELL WAS NOTED IN COCKPIT WITH LEFT 10TH STAGE BLEED OPEN DURING GROUND RUNS. REMOVED ENGINE (LEFT) (S/N 807070) AND INSTALLED (S/N 807255). 2 L 7 2 4F 4 F RT A21EA E15NE 1999082700450 19990827 00450 EA 1999 8 27 COMA9960460 1 19990820 A 3030 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA PITOT HEAT TRIPPED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 739CA 7273 PITOT AOA AND STATIC HEAT MESSAGE. RESET C/B SYSTEM, TEST NORMAL. 2 L 7 2 4F RT A21EA 1999082700451 19990827 00451 EA 1999 8 27 COMA9960461 1 19990823 A 5320 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 THE DOUBLER ON THE AFT SIDE OF FRAME 718.00 LHS, STR 11 FOUND TO BE CRACKED. REPLACED DOUBLER AT FRAME 718.00, STR 11 L HS IAW WVAC EO 601R-53-0264. 2 L 7 2 4F RT A21EA 1999082700452 19990827 00452 EA 1999 8 27 COMA9960462 1 19990823 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 FRAME AT FS 718.00 RHS FOUND CRACKED IN THE RADIUS OF THE FLANGE AND IN THE DOUBLER ON AFT SIDE OF FRAME. REPAIRED FRAM E FLANGE IAW WVAC EO 601R-53-0263 AND REPLACED DOUBLER IAW WVAC EO 601R-53-0267. 2 L 7 2 4F RT A21EA 1999082700453 19990827 00453 EA 1999 8 27 COMA9960463 1 19990823 A 3211 601R850071 BUSHING CNDAIR CL600 CL6002B19 EA RT MLG MIGRATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 RIGHT HAND MLG AFT TRUNNION BUSHING MIGRATED FWD 0.050. APPLIED MARK TO LOCATION OF BUSHING AND FILLED SEAL AROUND BUSH ING FLANGE IAW WVAC EO 601R-57-0269. 2 L 7 2 4F RT A21EA 1999082700454 19990827 00454 EA 1999 8 27 COMA9960464 1 19990722 A 5751 601R1301011 SKIN CNDAIR CL600 CL6002B19 EA LT AILERON CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 LEFT HAND AILERON HAS CHAFE ON TOP LEADING EDGES. PERFORMED A MAJOR REPAIR TO CHAFES ON TOP LEADING EDGE OF LEFT HAND A ILERON IAW WVAC EO 601R-57-0266. 2 L 7 2 4F RT A21EA 1999082700455 19990827 00455 EA 1999 8 27 COMA9960465 1 19990722 A 5751 601R130102 SKIN CNDAIR CL600 CL6002B19 EA RT AILERON CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 RIGHT HAND AILERON HAS 5 CHAFED PLACES ON LEADING EDGE ON TOP WHERE SEAL RIDES. PERFORMED A MAJOR REPAIR TO 5 CHAFED PL ACES ON RIGHT HAND AILERON IAW WVAC EO NR 601R-57-0265. 2 L 7 2 4F RT A21EA 1999082700456 19990827 00456 NM 1999 8 27 UPS99230418 1 19990821 A 3510 OXYGEN BOTTLE BOEING 727 72725C 138400H NM COCKPIT EMPTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, CREW O2 PRESSURE READS ZERO. *S/D* REMOVED AND REPLACED CREW O2 BOTTLE. NO LEAKS FOUND. 2 L 7 3 4F A3WE 1999082700457 19990827 00457 NM 1999 8 27 UPS99430415 1 19990822 A 3230 RETRACT MECH BOEING 747 747123 1384873 NM RT MLG MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 671UP 20323 INSPECTION TYPE:N/A, UPON DEPARTURE RIGHT WING GEAR WOULD NOT TILT. LANDING GEAR LEVER WILL NOT MOVE TO THE UP POSITION . CREW COMPLETED CHECKLIST AND RETURNE D TO KIX. ***REFERENCE UPS99430416 FOR REPEAT WRITE-UP*** INSPECTED ALL LANDIN G GEAR, NO DEFECTS FOUND PER MM 32-21-00, AND 32 -11-00. CHECKED AND RESEATED LOGIC CARDS IN THE M-93 AND M-809 ON RIGH T WING GEAR TILT LOGIC CARDS AND CHECKED PRIM AND ALT TILT. SENSORS FOUND WERE NORMAL PER MM 32-61-04 PAGE 201. 2 L 7 4 4F A20WE 1999082700458 19990827 00458 NM 1999 8 27 UPS99430416 1 19990822 A 3230 RETRACT MECH BOEING 747 747123 1384873 NM RT MLG LACK OF LUBE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 671UP 20323 INSPECTION TYPE:N/A, UPON THE SECOND DEPARTURE THE RIGHT WING GEAR WOULD NOT TILT. LANDING GEAR LEVER WILL NOT MOVE TO THE UP POSITION. COMPLETED CHECKLIST AND RETURNED TO KIX. BOTH PRIMARY AND ALT AGREE. ***REFERENCE UPS99430415 FOR RE PEAT WRITE-UP*** JACKED ACFT AND FOUND RIGHT WING GEAR DID NOT TILT POSITION DUE TO THE GEAR PIVOT POINT LACKED LUBRICA TION. COMPLETED LUBRICATION OF ALL LANDING GEAR COMPONENTS. TILT INDICATION OP'S CHECKED NORMAL AS PER MM 32-61-04. 2 L 7 4 4F A20WE 1999082700459 19990827 00459 NM 1999 8 27 UPS99630413 1 19990822 A 2560 65B4028912 HARNESS BOEING 767 76734AF 1385212 NM FLIGHT DECK MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 313UP 27764 INSPECTION TYPE:ETOP REF EO M 2560-11396A DEMO EMERGENCY DESCENT HARNESS BLACK OVER THE SHOULDER STRAP MISSING. REPLACE D EMERGENCY ESCAPE SAFTEY HARNESS. 2 L 7 2 4F RT A1NM 1999082700460 19990827 00460 WP 1999 8 27 UPS99830394 1 19990803 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE AND ONE RIVET HOLE. STOP DRILLED C RACKS AND REPAIRED SKIN IAW EO DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 1999082700461 19990827 00461 WP 1999 8 27 UPS99830395 1 19990803 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, SEAT TRACK AT FS 280, RBL 45 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SEAT TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999082700462 19990827 00462 WP 1999 8 27 UPS99830396 1 19990805 A 5320 3779762501 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE LONGERON 3R END FITTING AT FS 680 WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1999082700463 19990827 00463 WP 1999 8 27 UPS99830397 1 19990805 A 5320 47504202 FITTNG DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE INTERCOSTAL TO FRAME ATTACH FITTING AT FS 857, LONG 18R WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 4750420 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700464 19990827 00464 WP 1999 8 27 UPS99830398 1 19990805 A 5320 3779498502 FITTING DOUG DC8 DC873F 302199F WP BS 847 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE INTERCOSTAL TO FRAME ATTACH FITTING AT 847, LONG 19R WAS CRACKED. REMOVED, FABRICATED AND REP LACED THE FITTING IAW DWG 3779498 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700465 19990827 00465 WP 1999 8 27 UPS99830399 1 19990805 A 5320 37794981 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE INTERCOSTAL TO FRAME ATTACH FITTING AT FS 857, LONG 18R WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 3779498 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700466 19990827 00466 WP 1999 8 27 UPS99830400 1 19990805 A 5320 37799781 FITTING DOUG DC8 DC873F 302199F WP BS 834 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE INTERCOSTAL TO FRAME ATTACH FITTING AT FS 834, LONG 18L IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700467 19990827 00467 WP 1999 8 27 UPS99830401 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 454.9 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, LT WING L/E RIB AT XS454.976 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED TH E RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999082700468 19990827 00468 WP 1999 8 27 UPS99830402 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 297.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, LT WING L/E RIB AT XS 297.5 WAS CRACKED AT THE AFT UPPER END. REPAIRED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700469 19990827 00469 WP 1999 8 27 UPS99830403 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 566.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, RT WING L/E RIB AT XFS 566.25 WAS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700470 19990827 00470 WP 1999 8 27 UPS99830404 1 19990806 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 566.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, RT WING L/E RIB AT XFS 566.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700471 19990827 00471 WP 1999 8 27 UPS99830405 1 19990807 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 665 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, RT WING L/E RIB AT XFS 665 WAS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700472 19990827 00472 WP 1999 8 27 UPS99830406 1 19990807 A 5720 57698917 DOUBLER DOUG DC8 DC873F 302199F WP WS 418 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, RT WING L/E SKIN UPPER DOUBLER AT XFS 418 WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE DOUBL ER IAW DWG 5769891 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999082700473 19990827 00473 WP 1999 8 27 UPS99830407 1 19990805 A 5320 577327558 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS 680, BL 0, THE FLOORBEAM TO BULKHEAD ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLAC ED THE FITTING IAW DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700474 19990827 00474 WP 1999 8 27 UPS99830408 1 19990808 A 5240 561570013 WEB DOUG DC8 DC873F 302199F WP R1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE RT FWD SERVICE DOOR FRAME FWD WEB WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE WEB IAW D WG 5615700 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700475 19990827 00475 WP 1999 8 27 UPS99830409 1 19990814 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C234, RT WING L/E RIB AT XFS 640 WAS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999082700476 19990827 00476 WP 1999 8 27 UPS99830410 1 19990805 A 5320 37799781 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE INTERCOSTAL TO FRAME ATTACH FITTING AT FS 759, LONG 18L IS CRACKED. REMOVED, FABRICATED AND R EPLACED THE FITTING IAW DWG 3779978 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700477 19990827 00477 WP 1999 8 27 UPS99830411 1 19990805 A 5720 576960039 DOUBLER DOUG DC8 DC873F 302199F WP WS 540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, LT WING L/E UPPER SKIN INTERNAL DOUBLER AT XFS 540 IS CRACKED. REMOVED, FABRICATED AND REPLACED T HE DOUBLER IAW DWG 5769600 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700478 19990827 00478 WP 1999 8 27 UPS99830412 1 19990820 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT'S BATT PACK. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999082700479 19990827 00479 WP 1999 8 27 UPS99830414 1 19990822 A 2560 STRAP DOUG DC8 DC871F 302199D WP CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A, RT ESCAPE TAPE RESTRAINING STRAP BROKEN. REMOVED AND REPLACED STRAP. 2 L 7 4 4F RT 4A25 1999082700480 19990827 00480 WP 1999 8 27 UPS99830417 1 19990808 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 204 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, RT WING L/E UPPER SKIN AT XFS 204, JUST I/B OF THE I/B SLOT WAS CRACKED AT 1 RIVET HOLE. STOP DRILL ED CRACK AND REPAIRED SKIN IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999082700481 19990827 00481 WP 1999 8 27 UPS99830419 1 19990808 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1 RT. WING L/E LWR SKIN @ XFS 597.5, IS CRACKED 2 PLACES, AT THE DRAIN HOLE & AT THE RIVET HOLE JUST FW D OF THE DRAIN. STOP DRILLED CRACK & REPAIRED THE SKIN IAW E.O. DC8-5720-4087-A 2 L 7 4 4F RT 4A25 1999082700482 19990827 00482 WP 1999 8 27 UPS99830420 1 19990810 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, RT WING L/E LWR SKIN AT XFS 340, 17 FWD OF THE SPAR WAS CRACKED AT 1 FASTENER HOLE. STOP DRILLED CR ACK AND REPAIRED THE SKIN IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 1999082700483 19990827 00483 WP 1999 8 27 UPS99830421 1 19990810 A 5320 37592581 FITTING DOUG DC8 DC873F 302199F WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, LONGERON 31L SPLICE FITTING AT FS 1270 WAS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700484 19990827 00484 WP 1999 8 27 UPS99830422 1 19990810 A 5320 37592581 FITTING DOUG DC8 DC873F 302199F WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, LONGERON 35L SPLICE FITTING AT FS 1270 WAS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700485 19990827 00485 WP 1999 8 27 UPS99830423 1 19990810 A 5320 3755822505 FITTING DOUG DC8 DC873F 302199F WP BS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, BATHTUB FITTING HAD HEAVY CORROSION AT FS 340, LONG 28L. REMOVED AND REPLACED THE FITTING IAW SRM 5 3-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999082700486 19990827 00486 WP 1999 8 27 UPS99830424 1 19990811 A 5320 3641125502 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, FS 759, RBL 48, THE FWD FITTING WAS CRACKED AT THE BOTTOM I/B FASTENER. REMOVED AND REPLACED THE FI TTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700487 19990827 00487 WP 1999 8 27 UPS99830425 1 19990810 A 5320 37794981 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 857, LONG 18R. REMOVED, FABRICATED AND REP LACED THE FITTING IAW DWG 3779498 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700488 19990827 00488 WP 1999 8 27 UPS99830426 1 19990810 A 5320 3779658502 FITTING DOUG DC8 DC873F 302199F WP BS 834-857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, THE LONG 10R END FITTING AT FS 834 TO 857 WAS CRACKED. REMOVED AND REPLACED THE END FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700489 19990827 00489 WP 1999 8 27 UPS99830427 1 19990811 A 5320 564533225 STIFFENER DOUG DC8 DC873F 302199F WP BS 869 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, SPOT OF HEAVY CORROSION ON THE HORIZONTAL FITTING AT RBL 35, FS 869. REMOVED AND REPLACED THE FITTI NG IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700490 19990827 00490 WP 1999 8 27 UPS99830428 1 19990813 A 5753 3770281503 FITTING DOUG DC8 DC873F 302199F WP WS 475 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, THE RT O/B SLOT, LWR DOOR, INNER FITTING IS CRACKED AT XS 475. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700491 19990827 00491 WP 1999 8 27 UPS99830429 1 19990813 A 5320 3750257503 FITTING DOUG DC8 DC873F 302199F WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, LONG 31L SPLICE FITTING AT FS 1040 TO 1060 WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 5- 1-20D. 2 L 7 4 4F RT 4A25 1999082700492 19990827 00492 WP 1999 8 27 UPS99830430 1 19990813 A 5320 3750545502 FITTING DOUG DC8 DC873F 302199F WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, LONG 35R SPLICE FITTING AT FS 1040 TO 1060 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1999082700493 19990827 00493 WP 1999 8 27 UPS99830431 1 19990814 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 12-32 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C2, THE FINGER DOUBLER AT FS -12 TO -32 AT LONG 21L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION OF THE FINGER DOUBLER, FABRICATED A REPLACEMENT SECTION AND INSTALLED IAW SRM 53-3-3 FIG 1 & SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700494 19990827 00494 WP 1999 8 27 UPS99830432 1 19990815 A 5320 JAMB DOUG DC8 DC873F 302199F WP BS 192 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, THE RT FWD SERVICE DOOR JAMB AT LONG 19R, AT THE LWR AFT CORNER OF THE JAMB IS CRACKED BEYOND LIMIT S, FS 192. CUT OUT THE DAMAGED AREA AND REPAIRED THE WEB IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999082700495 19990827 00495 WP 1999 8 27 UPS99830433 1 19990821 A 5720 SPLICE DOUG DC8 DC873F 302199F WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, RT WING L/E SPLICE AT XFS 710 WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE SPLICE IAW SRM 57-3 -3 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999082700496 19990827 00496 WP 1999 8 27 UPS99830434 1 19990808 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 798 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS 798 FLOORBEAM AT RBL 48 WAS CORRODED OUT OF LIMITS. CUT OUT DAMAGED AREA AND REPAIRED THE FLOO RBEAM IAW DH SK867-114. 2 L 7 4 4F RT 4A25 1999082700497 19990827 00497 WP 1999 8 27 UPS99830435 1 19990820 A 5753 5769859153 SKIN DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, THE RT I/B UPPER SLOT SKIN WAS CRACKED AT THE SPLICE PAN, UNDER THE UPPER SLOT DOOR. REMOVED, FAB RICATED AND REPLACED THE SLOT SKIN IAW DWG 5769859 AND SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999082700498 19990827 00498 WP 1999 8 27 UPS99830436 1 19990821 A 5320 5772656 CLIP DOUG DC8 DC873F 302199F WP BS 1620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS 1620 AND LONG 14R, THE INTERCOSTAL ATTACH CLIP WAS CRACKED. REMOVED, FABRICATED AND REPLACED T HE CLIP IAW DWG 5772656 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700499 19990827 00499 EU 1999 8 27 QXEA9901660 1 19990822 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 480AU 11229 GEG- FOUND EMERGENCY EXIT SIGN HAD MANY BULBS BURNED OUT. REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999082700500 19990827 00500 EU 1999 8 27 QXEA9901661 1 19990820 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 481US 6224 4286 11230 SEA- NUMEROUS EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AT ENTRANCE WAY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999082700501 19990827 00501 EU 1999 8 27 QXEA9901662 1 19990822 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 498US 11181 PDX- CENTER OVERHEAD FORWARD AND AFT EMERGENCY EXIT SIGNS, 28V BULBS INOPERATIVE. REPLACED BOTH FORWARD AND AFT CENTER AISLE EMERGENCY LIGHT ASSEMBLIES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999082700502 19990827 00502 WP 1999 8 27 ABXA9900657 1 19990819 A 5280 49258842N HINGE DOUG DOUG DC9 DC933F 302207A WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR INBOARD DOOR HINGE CRACKED. REPLACED HINGE IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999082700503 19990827 00503 WP 1999 8 27 ABXA9900658 1 19990813 A 5320 9922050IN FITTING DOUG DOUG DC9 DC933F 302207A WP BS 946 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND FITTING CRACKED AT STATION 946 AND LONGERON 23 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999082700504 19990827 00504 WP 1999 8 27 ABXA9900659 1 19990813 A 5320 992341717 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND CRACKED VERTICAL SUPPORT BRACKET UNDER LBL 44 SEAT TRACK STATION 658. REPLACED FITTING IAW DC9 SR M 51-30-5. 2 L 7 2 4F A6WE 1999082700505 19990827 00505 WP 1999 8 27 ABXA9900660 1 19990818 A 5320 59145581 DOUBLER DOUG DOUG DC9 DC933F 302207A WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND FUSELAGE SKIN AND DOUBLER CORRODED AT STATION 965 AND LONGERON 22 LEFT. REPLACED DOUBLER IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999082700506 19990827 00506 WP 1999 8 27 ABXA9900661 1 19990813 A 5230 39260461 FITTING DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR UPPER AFT STOP FITTING CRACKED. REPLACED FITTING IAW DACO DWG DC9 591014 1. 2 L 7 2 4F A6WE 1999082700507 19990827 00507 NM 1999 8 27 SCNA99722 1 19990725 A 5511 SPAR BOEING 727 7272J4 1384006 NM LT HORZ STAB CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT THE AFT UPPER SPAR CHORD OF THE LEFT HORIZONTAL ST ABILIZER IAW B727 SRM 571001 FIG 2. FABRICATED NEW CHORD FROM 2024 T3511 PER SAMPLE. FABRICATED REPAIR ANGLES AND STRA PS FROM 101381203 7075 T6511 .063 7075 T6 IAW B727 SRM 551005. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. I NSTALLED IAW B727 SRM 551005 AND 513002. 2 L 7 3 4F RT A3WE 1999082700508 19990827 00508 NM 1999 8 27 SCNA99108 1 19990821 A 3350 10617842 BATTERY PACK BOEING 727 7272J4 1384006 NM LT EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE FORWARD LT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND RE PLACED EMERGENCY LIGHT BATTERY CHARGER M654. OPERATIONALLY CHECKS GOOD IAW MM 335022. 2 L 7 3 4F RT A3WE 1999082700509 19990827 00509 NM 1999 8 27 SCNA99109 1 19990821 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE CHECK, THE CENTER AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR THE CENTER AISLE EMERGENCY LIGHT. OPERATIONALLY CHECKS GOOD IAW MM 335022. 2 L 7 3 4F RT A3WE 1999082700510 19990827 00510 NM 1999 8 27 SCNA99110 1 19990821 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM LT EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE FORWARD LT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND RE PLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS GOOD IAW MM 335022. 2 L 7 3 4F RT A3WE 1999082700511 19990827 00511 NM 1999 8 27 SCNA99111 1 19990823 A 2612 69295671 FIRE WARN HORN BOEING 727 7272K3 138400D NM NLG WW APU INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 DURING A LINE MAINTENANCE CHECK, THE APU NOSE WHEEL WELL FIRE WARNING HORN WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE NOSE WHEEL WELL APU FIRE WARNING HORN. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999082700512 19990827 00512 NE 1999 8 27 SCNA99112 2 19990820 A 7260 GEARBOX BOEING 727 7272K3 138400D NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE INOP A SCNA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 GL 15 891DB 22770 702662 DURING FLIGHT A LOSS OF ENGINE OIL PRESSURE WAS NOTED ON NUMBER TWO ENGINE. SECURED NUMBER TWO ENGINE PER COM AND SHUTD OWN. FOUND GEARBOX CASE STUD MISSING. REMOVED AND REPLACED ENGINE GEARBOX PER MM 7260. PERFORMED POWER ASSURANCE CHEC K WITH ALL OPERATIONS NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 1999082700513 19990827 00513 NM 1999 8 27 VNAA9908001 1 19990808 A 5101 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AIRFRAME STRIKE A VNAA O OTHER O OTHER DE DESCENT 1 GL 07 437JS 3055 DURING THE DESCENT INTO PIT, THE AIRCRAFT WAS STRUCK BY LIGHTNING. THE FLIGHT CONTINUED TO PIT AND MADE A NORMAL LANDIN G. MAINTENANCE INSPECTED AND REPAIRED LIGHTNING STRIKE DAMAGE ON THE RIGHT HAND ELEVATOR, LEFT HAND FLAP, RIGHT HAND W ING TIP AND THE VERTICAL DORSAL FIN. DAMAGE WAS REPAIRED USING DORNIER 328 SRM 51-77-10. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999082700514 19990827 00514 NM 1999 8 27 VNAA9908005 1 19990813 A 5310 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE DAMAGED A VNAA K NONE C F.O.D. IN INSP/MAINT 1 GL 07 436JS 3052 THE AIRCRAFT WAS STRUCK BY A PICKUP TRUCK WHILE SITTING STATIC AT THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROV ED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FERRY TOOK PLACE WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AND RETURNED THE AIRCRAFT TO SERVICE PER DORNIER RAS 328-53-817 AND DORNIER SPR 21708. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999082700515 19990827 00515 NM 1999 8 27 VNAA9908003 1 19990805 A 2612 BA231771 FIRE WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LAVATORY ACTIVATED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 434JS 10485 3051 THE AIRCRAFT RETURNED TO THE GATE FOR AN INTERMITTANT LAV FIRE WARNING INDICATION. MAINTENANCE INSPECTED AND REPLACED T HE LAV FIRE BOTTLE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-25-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999082700516 19990827 00516 NM 1999 8 27 VNAA9908004 1 19990814 A 2612 51653151 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE APU FAILED A VNAA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 430JS 3044 DURING TAXI ONTO THE GATE, THE CREW RECEIVED AN INTERMITTANT FIRE WARNING INDICATION ON THE RIGHT HAND ENGINE. THE CREW DECLARED AN EMERGENCY, AND FIRED OFF BOTH RIGHT HAND ENGINE FIRE BOTTLES. THE EMERGENCY FIRE CREWS AND MAINTENANCE FOU ND NO INDICATION OF AN ACTUAL FIRE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND ENGINE FIRE CONTROL UNIT WITH THE APU FIRE CONTROL UNIT, IN ACCORDANCE WITH DORNIER MM 26-12-03. THE APU WAS DEFERRED PER THE DORNIER MINIMUM EQUIPMENT LIST, AND THE AIRCRAFT WAS RETURNED TO SERVICE. ON 15 AUGUST, MAINTENANCE REPLACED THE APU FIRE CONTROL UNIT PER DORNIE R MM 26-12-03. THE DEFERRAL WAS REMOVED FROM THE AIRCRAFT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999082700517 19990827 00517 NM 1999 8 27 VNAA9908006 1 19990817 A 3350 3280100 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 457PS 95097 3048 TESTING THE EMERGENCY LIGHTS WAS REPORTED AS INTEMITTANT FROM THE CREW. MAINTENANCE INSPECTED AND REPLACED THE FLIGHT A TTENDANT PANEL, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-12-15. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999082700518 19990827 00518 NM 1999 8 27 VNAA9908007 1 19990818 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 438JS 80235 1525 3056 THE EMERGENCY FLOOR LIGHTING AT SEAT 4D AND 4F WAS NOTED TO BE INOPERATIVE BY THE CREW ON THE PREFLIGHT INSPECTION. MAI NTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT SEAT 4D AND 4F, IN ACCORDANCE WITH DORNIER MM 33-51- 00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999082700519 19990827 00519 WP 1999 8 27 CKSA99072 1 19990820 A 7830 SEQUENCE VALVE DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 3 TR UNIT FAILED A CKSA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 6161M 45762 644852 ON CLIMB HAD FIRE WARNING ON NR 3 ENGINE. PERFORMED FIRE SEVERE DAMAGE OR SEPARATION CHECKLIST. ENGINE SECURED AT 2324 Z, HAD GOOD OIL PRESS (15 PSI) FUEL DUMP COMPLETED. FOUND NR 3 THRUST REVERSER SEQUENCE VALVE LEAKING HOT AIR ON FIRE S ENSOR. REMOVED AND REPLACED NR 3 T/R SEQUENCE VALVE. LEAK AND OPS CHECK GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1999082700520 19990827 00520 SO 1999 8 27 C2XA99IA372 1 19990719 A 3230 RETRACT MECH EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 27716 120128 IAH - FLT 3718 - THE CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND WTHOUT THE USE OF THE ELECTRICAL OVERRIDE SWITCH. T HE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM I AW EMB120 MM 32-30-00, WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999082700521 19990827 00521 SO 1999 8 27 C2XA99CL064 1 19990801 A 4950 APU EMB 145 EMB145 SO CABIN SMOKING A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 09 15932 145015 CLE - FLT 4233 - THE CREW REPORTED THAT AFTER THEY STARTED THE APU, THEY GOT THE LAV AND BAGGAGE SMOKE WARNING ALONG WIT H SMOKE IN THE REAR OF THE AIRCRAFT. MAINTENANCE INSPECTED THE APU AND PLACED IT ON MEL 49-00-00 CONTROL NR 18372B CAT 'C'. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999082700522 19990827 00522 CE 1999 8 27 C2XA99CL065 1 19990803 A 3230 RETRACT MECH BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 81538 UE199 RIC - FLT 3055 - THE CREW REPORTED THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO RIC WITHOUT FURTH ER INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND PERFORMED OPERATIONAL CHECK OF THE GEAR IAW BEECHCRAFT MM 32-30 -00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999082700523 19990827 00523 EU 1999 8 27 C2XA99IA374 1 19990721 A 3350 3012701 LIGHT AEROSP ATR42 ATR42500 EU PASSENGER DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING MAINTENANCE VISIT INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED EMERGENCY LIGHT ASSEMBLY IAW ATR 42-500 MM 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082700524 19990827 00524 EU 1999 8 27 C2XA99IA376 1 19990721 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE RIGHT FRONT EMERGENCY EXIT FLOOD LIGHT TO BE INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (X) 2 H 7 2 4T RT A53EU 1999082700525 19990827 00525 EU 1999 8 27 C2XA99IA375 1 19990721 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING LINE-CHECK INSPECTION, THE CENTER CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082700526 19990827 00526 EU 1999 8 27 C2XA99IA386 1 19990727 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14451 512 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED NUMEROUS INTERIOR EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR 42-500 MM 33-51-21, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082700527 19990827 00527 EU 1999 8 27 C2XA99IA385 1 19990726 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 EFD - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY AISLE PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR 42-320 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082700528 19990827 00528 SO 1999 8 27 C2XA99IA384 1 19990723 A 3350 AD2047 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 47722 120166 IAH - A-CHECK INSPECTION, THE AFT FOUR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AF FECTED EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999082700529 19990827 00529 SO 1999 8 27 C2XA99IA383 1 19990723 A 5315 FLOORBEAM EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14938 145029 IAH - DURING C-CHECK INSPECTION, THE LEFT FLOORBEAM WAS FOUND CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION A ND REPAIRED THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01109, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,914. 2 HOURS. CYCLES: 2,929. (X) 2 L 7 2 4F RT T00011AT 1999082700530 19990827 00530 SO 1999 8 27 C2XA99IA382 1 19990723 A 5315 FLOORBEAM EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14938 145029 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM WAS FOUND CORRODED FROM FRAME 15 TO FRAME 19. MAINTENANCE REMOVED THE CORROSION AND REPAIRED THE AFFECTED FLOORBEAM IAW EMBRAER FAX SST-1287/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) ACFT TT: 3,914.2 HOURS. CYCLES: 2,929. (X) 2 L 7 2 4F RT T00011AT 1999082700531 19990827 00531 SO 1999 8 27 C2XA99IA381 1 19990723 A 3350 110049 POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14938 145029 IAH - DURING C-CHECK INSPECTION, THE FORWARD SECTION OF EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-01, AND THE AIRCRAFT WAS APPROVEDF FOR RETURN TO SERVICE. ACFT TT: 3,914.2 HOURS. CYCLES: 2,929. (X) 2 L 7 2 4F RT T00011AT 1999082700532 19990827 00532 SO 1999 8 27 C2XA99IA380 1 19990723 A 3350 20131A BATTERY EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14938 145029 IAH - DURING C-CHECK INSPECTION, THE AFT SECTION OF EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED EMERGENCY LIGTH BATTERY PACK IAW EMB145 MM 33-50-01, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999082700533 19990827 00533 SO 1999 8 27 C2XA99IA379 1 19990723 A 5530 14531597601 DRAG ANGLE EMB 145 EMB145 SO LT VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14938 145029 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPRROVED FOR RETURN TO SERVICE. ACFT TT: 3,914.2 HOURS. CYCLES: 2,929. (X) 2 L 7 2 4F RT T00011AT 1999082700534 19990827 00534 SO 1999 8 27 C2XA99IA378 1 19990723 A 5530 14531597602 DRAG ANGLE EMB 145 EMB145 SO RT VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14938 145029 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILZIER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATIO N EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 1999082700535 19990827 00535 SO 1999 8 27 C2XA99IA377 1 19990723 A 3350 110049 POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14938 145029 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. (X) 2 L 7 2 4F RT T00011AT 1999082700536 19990827 00536 GL 1999 8 27 C2XA99IA387 2 19990728 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT HIGH OIL PRESS A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 15926 145005 CAE310127 RDU - FLT 4059- DURING TAKEOFF ROLL, THE PILOT REPORTED HIGH OIL PRESSURE IN THE NR 2 ENGINE. THE PILOT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. (X) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999082700537 19990827 00537 GL 1999 8 27 C2XA99IA373 2 19990722 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 14938 145029 CAE311035 IAH - FLT 4249 - THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY CHECKED THE COOLING PACS IAW EMB145 MM 21-25-01 AND FOUND NO DISC REPANCIES. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY RECURRED ON FLT 4252 FROM IAH/LBB WITH A L AV SMOKE WARNING. THE AIRCRAFT LANDED AT LBB WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOV ED AND REPLACED THE NR 1 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999082700538 19990827 00538 1999 8 27 C2XA99CL056 4 19990716 A 3421 6224565001 VERTICAL GYRO BEECH 1900 1900D 1154162 CE NR 2 MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 87557 4762 UE246 CLE - FLT 3056 - THE CREW REPORTED THE NR 2 EADI DISPLAY WENT BLANK IN-FLIGHT MOMENTARILY. THE AIRCRAFT RETURNED TO CLEV ELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 VERTICAL GYRO IAW COLLINS CMM AND PERFORMED O PERATIONAL CHECKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999082700539 19990827 00539 SO 1999 8 27 C2XA99CL057 1 19990701 A 2130 PRESSURIZATION EMB 120 EMB120RT SO CABIN MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 26714 120118 CLE - FLT 3618 - THE CREW REPORTED AFTER TAKEOFF, THE PRESSURIZATION WAS UNCONTROLLABLE IN BOTH AUTO AND MANUAL MODES. T HE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PRESSURIZAT ION SYSTEM IAW EMB-120 MM 21-30-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999082700540 19990827 00540 SO 1999 8 27 C2XA99CL058 1 19990721 A 3230 12043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR FAILED A C2XA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 09 15725 12282 120111 120173 CLE - FLT 3180 - THE CREW REPORTED THAT DURING GEAR RETRACTION, THEY FELT A STRONG VIBRATION AND HEARD A LOUD RUMBLING N OISE FROM THE NOSE GEAR AREA. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REP LACED THE LANDING GEAR RELAY BOX AND PERFORMED OPERATIONAL CHECKS IAW EMB-120 MM 32-31-02. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999082700541 19990827 00541 SO 1999 8 27 C2XA99CL059 1 19990723 A 2611 SMOKE DETECTOR EMB 145 EMB145 SO LAVATORY ACTIVATED A C2XA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 14947 145054 ATL - FLT 3996 - THE CREW REPORTED A LAV SMOKE WARNING AND DISCHARGED THE FIRE BOTTLE. THE AIRCRAFT RETURNED TO ATL WIT HOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 26-14-00 CONTROL NR 183550. (X) 2 L 7 2 4F RT T00011AT 1999082700542 19990827 00542 CE 1999 8 27 C2XA99CL060 1 19990731 A 6120 PCU BEECH 1900 1900D 1154162 CE NR 1 & NR 2 ENG OUT OF ADJUST A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 87551 UE206 CLE - FLT 3023 - THE CREW REPORTED THE PROPS ONLY REACHED 1,650 RPM AT FULL POWER. THE AIRCRAFT RETURNED TO THE GATE WI THOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NR 1 AND NR 2 ENGINE HIGH PROP RPM IAW BEECH 1900D MM 61-20-00 AND PER FORMED OPERATIONAL CHECKS IAW BEECH 1900D MM 61-00-00, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999082700543 19990827 00543 SO 1999 8 27 C2XA99IA357 1 19990615 A 5320 12006159001 ANGLE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 DURING CONTINENTAL EXPRESS C-CHECK, FLOOR STRUCTURE, RT OUTBOARD SUPPORT ANGLE FOUND CORRODED. FRAME 27 TO FRAME 44. RE MOVED AND REPLACED SUPPORT ANGLE AFT '2' SECTIONS IAW SRM 51-40-02. CLEANED AND TREATED FORWARD '2' SECTIONS. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,015.8 HOURS. TAC: 24,392. (X) 2 L 7 2 4T RT A31SO 1999082700544 19990827 00544 SO 1999 8 27 C2XA99IA361 1 19990615 A 5320 12027929001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RT BUTT STRAP FROM FRAME 27 TO FRAME 44. REMOVED AND REPLACED BU TT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,015.8 HOURS. TAC: 24,392. (X) 2 L 7 2 4T RT A31SO 1999082700545 19990827 00545 SO 1999 8 27 C2XA99IA360 1 19990615 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RT OUTBOARD FLOOR CROSSBEAM AT FRAME 36. REMOVED AND REPLACED CR OSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,015.8 HOURS. TAC: 24,392. (X) 2 L 7 2 4T RT A31SO 1999082700546 19990827 00546 SO 1999 8 27 C2XA99IA359 1 19990315 A 5542 12015250001 SKIN EMB 120 EMB120RT SO RUDDER DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 DURING CONTINENTAL EXPRESS C-CHECK, FOUND DENT IN AFT RUDDER, LOWER RT SIDE. CUT OUT DAMAGE, FABRICATED AND INSTALLED F ILLER AND DOUBLER REPAIR IAW SRM'S 51-10-02, 55-00-01 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18, 015.8 HOURS. TAC: 24.392. (X) 2 L 7 2 4T RT A31SO 1999082700547 19990827 00547 SO 1999 8 27 C2XA99IA358 1 19990615 A 5330 12003803001 SKIN EMB 120 EMB120RT SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT AIR CONDITIONER COMPARTMENT FUSELAGE SKIN AND FASTENER CHAFED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM'S 51-14-02, 53-00-01, AND 51-40-02. (X) 2 L 7 2 4T RT A31SO 1999082700548 19990827 00548 EU 1999 8 27 C2XA99IA366 1 19990702 A 5311 S53672409218 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSS FRAME CORRODED AT FRAME 40. REPAIRED IAW EC 5310-01037. AIRCRAFT APPRO VED FOR RETURN TO SERVICE. TAT: 20,297.2 HOURS. TAC: 23,767. (X) 2 H 7 2 4T RT A53EU 1999082700549 19990827 00549 EU 1999 8 27 C2XA99IA365 1 19990702 A 5311 S53672408202 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSS FRAME CORRODED AT FRAME 39. REPAIRED IAW SRM 51-25-01, 51-24-04, AND EO 5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 20,297.2 HOURS. TAC: 23,767. (X) 2 H 7 2 4T RT A53EU 1999082700550 19990827 00550 EU 1999 8 27 C2XA99IA364 1 19990702 A 5311 S53672406208 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSS FRAME CORRODED AT FRAME 36. REPAIRED IAW EC 5310-01037. AIRCRAFT APPRO VED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999082700551 19990827 00551 EU 1999 8 27 C2XA99IA363 1 19990702 A 5313 S5367120218 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 DURING CONTINENTAL EXPRESS C-CHECK, FOUND STR 16R CORRODED BETWEEN FRAMES 36 AND 39. REMOVED AND SPLICED IN NEW SECTION OF STRINGER IAW SRM 53-61-24. AIRCRAFT APPROVED FOR REUTRN TO SERIVCE. TAT: 20,397.2 HOURS. TAC: 23,767. (X) 2 H 7 2 4T RT A53EU 1999082700552 19990827 00552 EU 1999 8 27 C2XA99IA362 1 19990702 A 5320 S53671318310 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT REAR SERVICE DOOR THRESHOLD PLATE CORRODED. REMOVED AND REPLACED THRESHOLD PLATE IAW SRM 51-25-02. AIRCRAFT APROVED FOR RETURN TO SERVICE. TAT: 20,397.2 HOURS. TAC: 23,767. (X) 2 H 7 2 4T RT A53EU 1999082700553 19990827 00553 SO 1999 8 27 C2XA99IA370 1 19990710 A 5530 14531597601 DRAG ANGLE EMB 145 EMB145 SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13936 145025 IAH - DURING C-CHECK INSPECTION, THE FORWARD LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHO RIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. ( X) 2 L 7 2 4F RT T00011AT 1999082700554 19990827 00554 SO 1999 8 27 C2XA99IA369 1 19990710 A 5530 14531597602 DRAG ANGLE EMB 145 EMB145 SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13936 145025 IAH - DURING C-CHECK INSPECTION, THE FORWARD RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTH ORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. (X) 2 L 7 2 4F RT T00011AT 1999082700555 19990827 00555 SO 1999 8 27 C2XA99IA368 1 19990710 A 5320 14522459001 RAMP EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13936 145025 IAH - DURING C-CHECK INSPECTION, THE RAMP UNDER THE CARBON FIBER FLOOR SUPPORT AT FRAME 20 WAS FOUND CORRODED. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED RAMP IAW EMB145 SRM 51-40-02, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. (X) 2 L 7 2 4F RT T00011AT 1999082700556 19990827 00556 SO 1999 8 27 C2XA99IA367 1 19990710 A 5320 14522459001 BEAM EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13936 145025 IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE REMOVE D THE CORROSION AND INSTALLED REPAIR DOUBLERS IAW EMBRAER REPAIR DRAWING SST-1287/99. THE AIRCRAFT WAS THEN APPROVED FO R RETURN TO SERVICE. ACFT TT: 3,925.2 HOURS. CYCLES: 3,189. (X) 2 L 7 2 4F RT T00011AT 1999082700557 19990827 00557 SO 1999 8 27 C2XA99CL055 1 19990716 A 2611 SMOKE LIGHT EMB 120 EMB120RT SO COCKPIT ILLUMINATED A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 26714 120118 CLE - FLT 3274 - THE CREW REPORTED A SMOKE INDICATION LIGHT ILLUMINATED ON THE MAP AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PACK AND BLEED SYSTEMS ON THE G ROUND IAW EMB-120 MM 21-00-00. NO DEFECTS NOTED. THE AIRCRAFT DID A TEST FLIGHT AND THE TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999082700558 19990827 00558 WP 1999 8 27 GTIA9901033 1 19990803 A 3350 60030431 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 14594 47202 MYR - FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT B5-40 IAW MM CHAPTER 33-53-0, OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A6WE 1999082700559 19990827 00559 WP 1999 8 27 GTIA9901032 1 19990803 A 3350 BULB DOUG DC9 DC932 3022066 WP COCKPIT FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942ML 47478 DTW - FLT 592 - LEFT COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BULB. OPERATIONAL CHECKED GOOD IAW 33-50 DC9 MM. ( X) 2 L 7 2 4F A6WE 1999082700560 19990827 00560 WP 1999 8 27 GTIA9901031 1 19990731 A 3397 WIRE DOUG DC9 DC931 3022065 WP ROWS 5-16 LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 ISP - FLT 113 - EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ROWS 5 TO 16. FOUND TRACK AT ROW 16 OFF AND WIRES PULLED FRO M LIGHTS. RESET WIRES AND TRACKS BACK IN PLACE. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A6WE 1999082700561 19990827 00561 WP 1999 8 27 GTIA9901029 1 19990727 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 13512 2219 48111 MYR - FLT 619 - LEFT EMERGENCY NACELLE FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT EMERGENCY NACELLE FLOOR LIGHT S BATTERY PACK IAW MM CHAPTER 33-50-00, OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A6WE 1999082700562 19990827 00562 WP 1999 8 27 GTIA9901028 1 19990712 A 3350 BULB DOUG DC9 DC982 3022082 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 800NK 49144 DTW - SEVERAL CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BULBS. EMERGENCY AND STANDBY LIGHTS OPERATION CHECK GOOD IAW WITH MD80 MM 3351 AND 33-52. (X) 2 L 7 2 4F A6WE 1999082700563 19990827 00563 WP 1999 8 27 GTIA9901027 1 19990414 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 669 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - CABIN LT SIDE FLOOR PANEL STA 669 TO STA 775 CRACKED AT FASTENER HOLE WITH LIGHT SURFACE CORROSION AROUND FASTENER HOLES. SKIN REPLACEMENT NEEDED. COMPLETION OF WORK ON PANEL TO BE COMPELTED ON W122. (X) 2 L 7 2 4F A6WE 1999082700564 19990827 00564 WP 1999 8 27 GTIA9901026 1 19990522 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 598 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - CABIN CENTER RIGHT FLOOR PANEL STA 598 TO STA 639 HAS (5 EACH) CRACKS (3 EACH AT FASTENER HOLES AND TWO BELOW FAST ENER HOLES). REPAIRED CRACKS INSTALLED DOUBLERS IAW SRM DC9 53-05 FAB DOUBLERS IAW SRM DC9 53-05 ALODINED AND PRIMED IA W SRM DC9 51-10-3. (X) 2 L 7 2 4F A6WE 1999082700565 19990827 00565 WP 1999 8 27 GTIA9901025 1 19990728 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 560 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - PASSENGER CABIN INTERNAL LEFT SIDE AT STA 560 AFT SIDE OF FRAME CRACKED APROXIMATELY 2 INCHES ABOVE FLOOR LINE. R EMOVED FITTING FOR INSPECTION. REPAIRED DAMAGED AREA IAW DC9 SRM 51-01 AND SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-6. REINSTALLED FITTING IAW DC9 SRM 53-01 AND SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1999082700566 19990827 00566 WP 1999 8 27 GTIA9901024 1 19990521 A 5313 27779223 LONGERON DOUG DC9 DC931 3022065 WP BS 560 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - PASSENGER CABIN INTERNAL STA 560 LONGERON L-17 HAS A CRACK. HOLES WERE MIS-DRILLED. REPAIR WILL BE ACCOMPLISHED ON W/C NR A092-S39-W132. W132 - REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STA 531 TO STA 588, PRODUCTION SPL ICE PER ENGINEERING DWG 53-99197-1 (CABIN PRESSURIZATION WILL BE ACCOMPLISHED ON WORK CARD NR 1092A09Z025). (X) 2 L 7 2 4F A6WE 1999082700567 19990827 00567 WP 1999 8 27 GTIA9901023 1 19990521 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 207 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - BS 207 LT, STR 13 WEB IS CRACKED. RECEIVED VERIFICATION OF REPAIR MAT'L ON P.O. NR 80319. TRIMMED CRACKED MEMBER IAW DC9 SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-6. INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 53-01 AND SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1999082700568 19990827 00568 WP 1999 8 27 GTIA9901022 1 19990521 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 617 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - CABIN STA 617 RBL 48, CRACK IN WEB. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. ALODINED AND PRIMED AND INST ALLED DOUBLER IAW SRM 53-01 FIG 2 (SHEET 3). (X) 2 L 7 2 4F A6WE 1999082700569 19990827 00569 WP 1999 8 27 GTIA9901021 1 19990728 A 5241 49124191 SPRING DOUG DC9 DC931 3022065 WP GALLEY DOOR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - FORWARD GALLEY DOOR ROLLER ASSY FOR THE DOOR BAYONET SPRING IS BROKEN ALLOWING THE ROLLER ASSY TO FLOAT WHEN THE D OOR IS BEING CLOSED. PERMITS BAYONET TO JAM BEHIND THE ROLLER ASSY. REMOVED AND REINSTALLED BROKEN SPRING WITH NEW ONE AW DC9 MM 52-41-0, PAGE 506. (X) 2 L 7 2 4F A6WE 1999082700570 19990827 00570 WP 1999 8 27 GTIA9901016 1 19990522 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 996 MISMANUFACTURED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 934ML 47526 MHV - BS 996 FLOORBEAM UPPER CAP ANGLE FROM LBL 12 TO EOP AT LBL 52 REQUIRES NEW SECTION TO ACCOMMODATE LT AFT LAV FLOOR STRUCTURE MOD. C/W ENGINEERING DWG NR 53-99197-2. ALODINED AND PRIMED. (X) 2 L 7 2 4F A6WE 1999082700571 19990827 00571 WP 1999 8 27 GTIA9901019 1 19990524 A 5532 PANEL DOUG DC9 DC931 3022065 WP VERTICAL STAB MISALIGNED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 934ML 47526 MHV - REPLACEMENT VERTICAL UPPER CENTER PANEL PN 9911940-403 ATTACH HOLES DO NOT ALIGN WITH AIRCRAFT STRUCTURE. FABED I N REF TO DC9 SRM 51-10 MANUFACTURED FOLLOWING ITEMS. 2 EACH CHANNELS 1 EA RT. 1 EACH LT. 2 INCH Z-CLIPS, 1 EACH RT, 1 EACH LT. 2 BULKHEAD REPAIR ANGLES, 1 EACH RT. 1 EACH LT. HEAT TREATED AND AGED AS REQUIRED. SUPPLIED TO AIRCRAFT FO R FIT AND INSTALL ON WO A092-B10-N062. (X) 2 L 7 2 4F A6WE 1999082700572 19990827 00572 WP 1999 8 27 GTIA9901018 1 19990524 A 5532 9911940403 PANEL DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - VERTICAL STABILIZER CENTER PANEL UPPER, PN 9911940-403, HAS CRACK RT AFT SIDE APPROXIMATELY 8 INCHES LONG. CENTER PANEL REPAIR AND INSTALLATION TO BE ACCOMPLISHED ON A092-A03-N065. (X) 2 L 7 2 4F A6WE 1999082700573 19990827 00573 WP 1999 8 27 GTIA9901017 1 19990519 A 5540 STIFFENER DOUG DC9 DC931 3022065 WP RUDDER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - RUDDER RIB STIFFENER IS CRACKED, PN 5910256. FABBED NEW STIFFENER AND HEAT TREATED PER AMS-H 6080 AND DC9 SRM 51- 10-2 PURCHASE AYA. PART REPAIR PART NOT REQUIRED. (X) 2 L 7 2 4F A6WE 1999082700574 19990827 00574 WP 1999 8 27 GTIA9901015 1 19990522 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 579-680 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - CABIN CENTER LT FLOOR PANEL STA 579 TO STA 680 (BOTTOM OF FLOOR PANEL SUPPORT 2 AND 4 HAS CRACKS AND PUNCTURE HOLE S). REMOVED SUPPORTS 2 AND 4 IAW SRM DC9 53-05 AND REPLACED SUPPORTS 2 AND 4 IAW SRM DC9 53-05. (X) 2 L 7 2 4F A6WE 1999082700575 19990827 00575 WP 1999 8 27 GTIA9901014 1 19990518 A 5512 PANEL DOUG DC9 DC931 3022065 WP HORIZ STABILIZER WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - HORIZONTAL STABILIZER CENTER SECTION PANEL NR 3804A AFT AND LOWER SECTION WORN TO KNIFE EDGE. FABRICATED REPAIR D OUBLERS REF DC9 SRM 5503. HEATED TREATED AND AGE HARDENED PER AMS H 6088. ASSEMBLED AND ISSUED FOR INSTALLATION ON WO A092107022. (X) 2 L 7 2 4F A6WE 1999082700576 19990827 00576 WP 1999 8 27 ARWA990802 1 19990816 A 2750 472085117 COMPARATOR LKHEED 1011 1011385115 5265015 WP TE FLAPS FAILED A ARWA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 19 308GB 790EK 193U1133 MIA - FLT 558 - FLAPS NOT EXTENDED FOR LANDING, LE SLATS OK. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND FLAP BRAKES LOCKE D OUT. RESET FLAPS. OPS NORMAL IAW MM 27-51-60. REMOVED AND REPLACED FLAP ASSY COMPARATOR. OPS CHECK NORMAL IAW MM 2 7-51-49. (M) 2 L 7 3 4F A23WE 1999082700577 19990827 00577 NM 1999 8 27 TWAA9911501 1 19990816 A 3350 362624 FLEX LAMP BOEING 757 757231 1384950 NM AFT LAVATORY WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 708TW 28480 THE EGRESS LIGHTS WERE INOPERATIVE OUTSIDE THE RT AFT LAVATORY. REPLACED THE FLEX LAMP. CHECK-C 9-5-98 LAX. 2 L 7 2 4F RT A2NM 1999082700578 19990827 00578 NM 1999 8 27 PCAA9900029 1 19990823 A 3231 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM LDG GEAR DOORS MALFUNCTIONED A PCAA K NONE J WARNING INDICATION DE DESCENT 1 EA 13 831EX 160 BOS- UPON DESCENT INTO BOS, ALL THREE GEAR DOORS REMAINED OPEN AFTER GEAR EXTENSION THEN CLOSED AFTER TOUCHDOWN. MAINTE NANCE INSPECTED GEAR DOORS, NO DEFECTS NOTED. PERFORMED PSEU TEST PER DHC MANUAL, NO DEFECTS NOTED. A TEST FLIGHT WAS PERFORMED SATISFACTORY. 2 H 7 2 4T RT A13NM 1999082700579 19990827 00579 NM 1999 8 27 PCAA9900030 1 19990820 A 5320 RIVETS DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 822EX 187 BGM- DURING THE ACCOMPLISHMENT OF AN A CHECK, THE NOSE GEAR WELL RIGHT SIDE WEB TOP AREA RIVETS WERE FOUND TO HAVE CRACK S EMINATING FROM THEM. MAINTENANCE PERFORMED A REPAIR IAW RD8-53-458. 2 H 7 2 4T RT A13NM 1999082700580 19990827 00580 NM 1999 8 27 CALA9901080 1 19990808 A 5312 BLKHD STIFFENER BOEING 737 7373T0 1384582 NM AFT PRESS BLKHD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND BOTTOM CENTER RT STIFFENER CORRODED AT AFT PRESSURE BULKHEAD SIDE. REPAIRED IAW SRM 51-70-11, FIGURE 1 . 2 L 7 2 4F RT A16WE 1999082700581 19990827 00581 NM 1999 8 27 CALA9901081 1 19990823 A 5347 GALLEY TRACK BOEING 737 7373T0 1384582 NM BS 328-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND RT O/B GALLEY MOUNT TRACK CORRODED AT STA 328-360. THE MOUNT TRACK WAS REMOVED AND REPLACED IAW SRM 51 -30-2 AND 51-10-2. 2 L 7 2 4F RT A16WE 1999082700582 19990827 00582 WP 1999 8 27 CALA9901082 1 19990823 A 5754 NRB6237501 SKIN DOUG DC10 DC1030 3023501 WP LT LE SLAT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND LT WING NR 8 SLAT CORRODED ON LEADING EDGE AT TRACK. THE NR 8 SLAT WAS REMOVED AND REPLACED IAW MM 27- 80-01. 2 L 7 3 4F A22WE 1999082700583 19990827 00583 WP 1999 8 27 CALA9901083 1 19990824 A 3350 EMBS1392 CHARGER MATHEWS DOUG DC10 DC1030 3023501 WP L-2 DOOR INOP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND L-2 DOOR EMERGENCY LIGHTS BATTERY CHARGER UNIT BATTERY DISCONNECT PLUG CABLE BROKEN AT PLUG. THE CHARG ER UNIT WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00. 2 L 7 3 4F A22WE 1999082700584 19990827 00584 WP 1999 8 27 CALA9901084 1 19990824 A 3397 WIRE DOUG DC10 DC1030 3023501 WP L-3 DOOR CHAFED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND THE EMERGENCY PATH LIGHTING SYSTEM BATTERY POWER SUPPLY BLOWING FUSES AT L-3 DOOR. MAINTENANCE FOUND C HAFED WIRE AT SIDEWALL FORWARD OF LT OVERWING EXIT. REPAIRED IAW MM 20-00-00 AND OPERATION CHECKED GOOD IAW MM 33-50-00 . 2 L 7 3 4F A22WE 1999082700585 19990827 00585 WP 1999 8 27 CALA9901085 1 19990824 A 3397 WIRE DOUG DC10 DC1030 3023501 WP LAVATORY DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 39081 47861 THE EXIT IDENTIFIER AT LAV C FAILED TO ILLUMINATE. INSPECTION FOUND CABLES DAMAGED. THE CABLES WERE REPAIRED AND OPERA TION CHECKED IAW MM 33-50-00. 2 L 7 3 4F A22WE 1999082700587 19990827 00587 WP 1999 8 27 9903319984 1 19990818 A 2120 AIR DIST DOUG DC9 DC932 3022066 WP CABIN SMOKE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 984US 47383 SMOKE IN AFT CABIN SHORTLY AFTER TAKEOFF. CREW DECLARED A YELLOW EMERGENCY AND FLIGHT WAS RETURNED TO MSP. AIRCRAFT LA NDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. 2 L 7 2 4F A6WE 1999082700588 19990827 00588 WP 1999 8 27 9903339987 1 19990813 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 987US 47458 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN COCKPIT, FORWARD GALLEY, AND ENTRANCE WAY ALL INO PERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999082700589 19990827 00589 WP 1999 8 27 9903349921 1 19990814 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERIES, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999082700590 19990827 00590 WP 1999 8 27 9903359973 1 19990819 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9337 47346 DURING LINE MAINTENANCE INSPECTION, FOUND AFT LOWER CEILING AND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-28 AT POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999082700591 19990827 00591 NM 1999 8 27 9903365635 1 19990819 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM ROW 15 INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 535US 26482 DURING SCHEDULED MAINTENANCE, THE EMERGENCY ESCAPE PATH LIGHTS AT ROWS 15 AND 16 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND SERVICEABLE UNIT. OPERATIONAL TEST WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1999082700592 19990827 00592 NE 1999 8 27 COMA9960466 2 19990823 A 7230 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED A COMA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 947CA 7912 14 7077 807255 CREW REPORTED OIL SMELL FROM LEFT PACK WITH 10TH STAGE BLEED OPEN. CHANGED NR 3 CARBON SEAL ON LEFT ENGINE, PERFORMED C OMPRESSOR WASHES. NO SMELL NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999082700593 19990827 00593 EA 1999 8 27 COMA9960467 1 19990823 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT DAMAGED A COMA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 01 946CA 7072 CARGO SMOKE WARNING. REPLACED DAMAGED SMOKE DETECTOR IN CARGO COMPARTMENT. 2 L 7 2 4F RT A21EA 1999082700594 19990827 00594 NM 1999 8 27 UPS99230437 1 19990805 A 5312 BULKHEAD FORGING BOEING 727 72722C 138400F NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CORROSION ON RT SIDE BS 740 BULKHEAD FORGING BETWEEN STR 23R AND STR 24R. FITTING REPLACED IAW UPS E O B727-5310-7477-E & SRS EO 99-24-003 ENGINEERING FILE NR 727-53-2159. 2 L 7 3 4F A3WE 1999082700595 19990827 00595 NM 1999 8 27 UPS99230438 1 19990805 A 5312 BULKHEAD FORGING BOEING 727 72722C 138400F NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CORROSION ON LT BS 740 BULKHEAD FORGING BETWEEN STR 23L AND STR 24L. FITTING REPLACED IAW EO B727-53 10-7477-E. 2 L 7 3 4F A3WE 1999082700596 19990827 00596 NM 1999 8 27 UPS99230439 1 19990817 A 5320 BRACKET BOEING 727 72722C 138400F NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, AFT CARGO BAY, ANGLE BRACKET CRACKED AT BS 970 LBL 20 ATTACHING INTERCOSTAL TO FRAME. FABRICATED REP AIR ANGLE IAW SRM 51-20-01. RE-INSTALLED BRACKET IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999082700597 19990827 00597 NM 1999 8 27 UPS99230440 1 19990813 A 5320 CHANNEL BOEING 727 72722C 138400F NM BS 570 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, LIGHT SURFACE CORROSION ON FLOOR SUPPORT CHANNEL BS 570 RBL 10. CORROSION REMOVED AND FOUND TO BE BE YOND LIMITS IAW 53-10-1, CHANNEL REPAIRED IAW SRM 53-10-5 FIG 4. 2 L 7 3 4F A3WE 1999082700598 19990827 00598 NM 1999 8 27 UPS99230441 1 19990810 A 5753 SKIN BOEING 727 72722C 138400F NM RT TE FOREFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, RT INBOARD FORE FLAP, CRACK AND CHAFING AT I/B LEADING EDGE, AREA FORWARD OF FOREFLAP INBOARD ATTACHM ENT POINT. REPAIR CARRIED OUT IAW SRM 57-50-4. 2 L 7 3 4F A3WE 1999082700599 19990827 00599 NM 1999 8 27 UPS99230442 1 19990810 A 5522 SKIN BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, RT ELEVATOR CRACK ON SKIN BONDED STIFFENER AT STA 204. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIRED IAW EO 99-24-002 UPS ENGINEERING FILE NR 727-55-0397. 2 L 7 3 4F A3WE 1999082700600 19990827 00600 NM 1999 8 27 UPS99230443 1 19990812 A 5230 65196674 HINGE BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, FWD HINGE ON AFT CARGO DOOR CRACKED. NEW HINGE INSTALLED IAW MM 52-31-101. 2 L 7 3 4F A3WE 1999082700601 19990827 00601 NM 1999 8 27 UPS99230444 1 19990810 A 5754 SKIN BOEING 727 72722C 138400F NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, NR 3 L/E FLAP ANTI-ICE SKIN CRACKED AT UPPER FASTENER 2ND SKIN PANEL I/B OF ACTUATOR. REPAIRED IAW E O B727-5750-3082. 2 L 7 3 4F A3WE 1999082700602 19990827 00602 NM 1999 8 27 UPS99230445 1 19990810 A 5754 SKIN BOEING 727 72722C 138400F NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, NR 3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B FASTENER 2ND SKIN PANEL I/B OF ACTUATOR. REPAIRED I AW EO B727-5750-3082. 2 L 7 3 4F A3WE 1999082700603 19990827 00603 NM 1999 8 27 UPS99230454 1 19990822 A 2780 LINKAGE BOEING 727 727185C 138406N NM NR 4 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:N/A, NR 4 L/E FLAP O/B BULL-NOSE LINKAGE WHERE IT ATTACHES TO WING CRAC KED AND CORRODED. INSTALLED NEW LUG AT NR 4 KRUEGER FLAP BULLNOSE LINKAGE WITH REF TO SRM 51- 30-2. CHECKS GOOD. 2 L 7 3 4F A3WE 1999082700604 19990827 00604 NM 1999 8 27 UPS99230456 1 19990822 A 2780 LINKAGE BOEING 727 727185C 138406N NM NR 5 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:N/A, NR 5 LEADING EDGE I/B FLAP BULL-NOSE LINKAGE WHERE IT ATTACHES TO THE WING CRACKED AND CORRODED. I NSTALLED NEW LUG AT NR 5 KRUEGER FLAP BULLNOSE LINKAGE WITH REF TO SRM 51- 30-2. CHECKS GOOD. 2 L 7 3 4F A3WE 1999082700605 19990827 00605 WP 1999 8 27 UPS99830353 1 19990817 A 2560 GIRT BAR DOUG DC8 DC871F 302199D WP CABIN FAILED A IPXA K NONE O OTHER LD LANDING 1 SO 01 797UP 45897 INSPECTION TYPE:N/A, ESCAPE SLIDE GIRT BAR RETAINER FAILED UPON EGRESS OF A/C, SLIDE SEPARATED FROM A/C. STILL I/W ON L OG PAGE 208929/2. FOLLOW UP ACTION SCHEDULED FOR REMAINDER OF DC-8 FLEET. *S/D* INSTALLED HARDWARE IAW EO DC-8-2560-1 1700, OPS CK NORMAL WITH GIRT BAR. 2 L 7 4 4F RT 4A25 1999082700606 19990827 00606 WP 1999 8 27 UPS99830446 1 19990730 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, MAIN CABIN CARGO SUB FLOOR AT RBL 27 SEAT TRACK CORRODED STA 55 DOT G952. FABRICATED AND INSTALLED SEAT TRACK AND PANEL IAW DC8 DRAWING 588958 8 AND DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999082700607 19990827 00607 WP 1999 8 27 UPS99830447 1 19990731 A 5510 WEB DOUG DC8 DC873F 302199F WP HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, LT HORIZ STAB INTERIOR WEB STA EX 99 CORROSION. FABRICATED AND INSTALLED NEW PANEL ASSY, (P/N 56517 47-59) IAW DAC DWG 5651747 AND DC8 SRM 51-1-24 & 51-1-21. 2 L 7 4 4F RT 4A25 1999082700608 19990827 00608 WP 1999 8 27 UPS99830448 1 19990806 A 5400 DOUBLER DOUG DC8 DC873F 302199F WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, NR 1 PYLON LWR FWD EXTERNAL HORSE SHOE DOUBLER IS CRACKED. FABRICATED AND INSTALLED DOUBLER, MATERI AL ID PO NR 22463 7075-T6.080 IAW DC8 SRM 57-2-1A. 2 L 7 4 4F RT 4A25 1999082700609 19990827 00609 WP 1999 8 27 UPS99830449 1 19990729 A 5320 FRAME DOUG DC8 DC873F 302199F WP CARGO DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 AFT PIT INTERNAL DOOR FRAME CORRODED FABRICATED AND INSTALLED INTERCOSTAL AND 2 EACH PULLET BRACK ET IAW D AC DWG #9754947 & DC8 SRM 51-1-20D & 51-3-0. ***CPCP*** 2 L 7 4 4F RT 4A25 1999082700610 19990827 00610 WP 1999 8 27 UPS99830450 1 19990802 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, FUS-1270 LONGERON 34L HAS AN 8 INCH CRACK. REMOVED LONGERON 34L IAW DC8 SRM 51-1-20D, RECEIVED NEW FITTING (P/N 3758593-1) AND INSTALLED LONGERON 34L IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700611 19990827 00611 WP 1999 8 27 UPS99830451 1 19990804 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 990 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, STATION 990 TRACK I HAS CORROSION DOWN CENTER. FABRICATED AND INSTALLED 2 SEAT TRACK SPLICES IAW DC 8 SRM 53-2-3 AND 51-1-8. 2 L 7 4 4F RT 4A25 1999082700612 19990827 00612 WP 1999 8 27 UPS99830452 1 19990726 A 5240 PAN DOUG DC8 DC873F 302199F WP SERVICE DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, 1 HOLE IN AFT SIDE OF RT FWD SERVICE DOOR PAN AT APPROX LONG 14R DOT S815. FABRICATED AND INSTALLED DOUBLER, FILLER AND SEAL RETAINER IAW DC8 SRM 52-2-0, 51-1-9 & 51-3-0. 2 L 7 4 4F RT 4A25 1999082700613 19990827 00613 WP 1999 8 27 UPS99830453 1 19990725 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, 2 FITTINGS STA 1180 LONG 35 AND LONG 34 RT CORRODED. REMOVED Z FITTINGS IAW DC8 SRM 51-1-20D, INSTA LLED NEW FITTINGS (P/N #3755841-50IN) (P/N 3755843-50) IN IAW DCI SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999082700614 19990827 00614 WP 1999 8 27 UPS99830455 1 19990729 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, RT CUSP AT FRAME STA 540 FRAME TO CUSP FITTING CORRODED DOT G-921. FABRICATED AND INSTALLED FITTING (P/N 4597643-2N), PO 300243 IAW DC8 S RM 51-1-24, 51-3-0 & 51-3-1 PG 1. 2 L 7 4 4F RT 4A25 1999082700615 19990827 00615 WP 1999 8 27 UPS99830457 1 19990810 A 5320 WEB DOUG DC8 DC873F 302199F WP LT MLG WW MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, LT WHEEL WELL FWD LWR BLKHD PREVIOUS REPAIR MISSING RIVETS AT TOP. FABRICATED AND INSTALLED WEB/DOU BLER IAW DC8 SRM 53-2-0 & 51-1-21. 2 L 7 4 4F RT 4A25 1999082700616 19990827 00616 WP 1999 8 27 UPS99830458 1 19990730 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, MAIN CARGO SUB FLOOR AT STA 40 RT SIDE UNDER WEB FLOOR SUPPORT CORRODED DOT G-949. FABRICATED AND I NSTALLED BEAM AND ALL ASSOCIATED FASTENERS IAW DC8 DRAWING 5615180. 2 L 7 4 4F RT 4A25 1999082700617 19990827 00617 WP 1999 8 27 UPS99830459 1 19990801 A 5400 FAIRING DOUG DC8 DC873F 302199F WP NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, NR 4 PYLON NOZZLE FAIRING HAS CRACKED FORMER. FABRICATED AND INSTALLED REPAIR IAW TIMCO REO NR 0667 4, HEAT TREATED REPAIR ANGLE AND CLIP IAW DAC DWG 9756774 GEN NOTE 23 AND TIMCO REO NR 0667 4, DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999082700618 19990827 00618 WP 1999 8 27 UPS99830460 1 19990724 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 879 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, LT WHEEL WELL, STA 879, LONG 24, EXTERIOR FACE HAS 4 INCH CRACK. FABRICATED AND INSTALLED ANGLE IAW TIMCO REO NR 06638. INSTALLED FRAME FITTING FS 879 IAW DC8 SRM 51-1-20D, AND 51-3-0. 2 L 7 4 4F RT 4A25 1999082700620 19990827 00620 WP 1999 8 27 UPS99830462 1 19990824 A 3510 6350A34CCC O2 BOTTLE DOUG DC8 DC873F 302199F WP CABIN LOW A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:N/A, BOTH CREW AND COURIER 02 BOTTLES LOW. REPLACED CREW AND COURIER 02 BOTTLES CREW (P/N 6350A34-CC-C) (S/N 722518) ON (P/N 071977) FOURIER (P/N 176530-95), (S/N 302224) OFF, (S/N 782420) ON. LEAK CHECKS GOOD. 2 L 7 4 4F RT 4A25 1999082700621 19990827 00621 WP 1999 8 27 UPS99830463 1 19990824 A 2560 ARM BAR DOUG DC8 DC873F 302199F WP ESAPE SLIDE NOT ATTACHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:N/A, THE ESCAPE SLIDE ARM BAR WOULD NOT ATTACH TO THE HOLDING BRACKET. RE-PACKED EMERGENCY ESCAPE SLIDE AND INSTALLED. 2 L 7 4 4F RT 4A25 1999082700622 19990827 00622 WP 1999 8 27 UPS99830464 1 19990817 A 3220 LANDING GEAR DOUG DC8 DC871F 302199D WP NLG COLLAPSED A IPXA K NONE O OTHER LD LANDING 1 SO 01 797UP 45897 INSPECTION TYPE:N/A, AFTER LANDING AND COMING TO A STOP ON RUNWAY 32R, THE NOSE GEAR COLLAPSED INTO THE WHEEL WELL. *S/ D* ALL REQUIRED EO'S IE DC8-5300-11498A HAVE BEEN C/W BY TIMCO. PER FERRY FLIGHT PERMIT NR 9086 ALL FERRY FLIGHT PROCE DURES HAVE BEEN ACCOMPLISHED AND AIRCRAFT IS IN SAFE OPERATING CONDITION FOR FERRY FLIGHT. ISSUED DMI. 2 L 7 4 4F RT 4A25 1999082700623 19990827 00623 WP 1999 8 27 UPS99830465 1 19990820 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1570 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:SVC, AFT ACCY COMPARTMENT, SEAT TRACK CORRODED BEYOND LIMITS AT FS L3L10. REMOVED SEAT TRACK FROM FS 15 00-1700 L3L10 AND SPLICED IN NEW SEAT TRACK SECTION, INSTALLED SPLICES AND REINSTALLED FLOORBOARDS AND CARGO SYSTEM IAW DC8 SRM 53-2-3, 51-1-24, 51-1-8 & 51-3-0. 2 L 7 4 4F RT 4A25 1999082700624 19990827 00624 WP 1999 8 27 UPS99830466 1 19990820 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:SVC, AFT ACCY COMPARTMENT, CORROSION AT INTERCOSTAL ATTACH ANGLE AROUND FASTENERS AND ANGLE, FS 1560 LON GERON 26L. REMOVED INTERCOSTAL(P/N 5615377-93) FAB AND INSTALLED NEW INTERCOSTAL IAW TIMCO REO 06698. 2 L 7 4 4F RT 4A25 1999082700625 19990827 00625 NM 1999 8 27 QXEA9901663 1 19990819 A 3350 5515800106 LIGHT GRIMES 10005511 DHAV DHC8 DHC8102 2809003 NM CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 829PH 23570 7820 304 PDX- COCKPIT EMERGENCY LANTERN LIGHT DIM THEN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL TEST CHECK GOOD. 2 H 7 2 4T RT A13NM 1999082700626 19990827 00626 EU 1999 8 27 99FDEA00347 1 19990821 A 2752 ACTUATOR AIRBUS 310 A310203 EU TE FLAPS FAILED A FDEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 443FE 283 FLAPS STUCK AT APPROX 2 DEG WITH THE FLAP SYS NR 1 AND NR 2 FLAP FAULT LIGHTS ILLUM ON O/H PAN'L AND ECAM MSG NR 1 AND N R 2 FLAP FAULT. *S/D* REMOVED AND REPLACED NR 1 AND NR 2 SFCC'S, FLAPS HANDLE CSU, AND NR 4 LEFT FLAP JACKSCREW. OPS CHECK OK. 2 L 7 2 4F RT A35EU 1999082700627 19990827 00627 WP 1999 8 27 ABXA9900662 1 19990817 A 5330 591142125 SKIN DOUG DOUG DC9 DC932 3022066 WP BS 778 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 778 AND LONGERON 2 RIGHT TO LONGERON 30. REPLACED SKIN IAW DC9 SRM. 2 L 7 2 4F A6WE 1999082700628 19990827 00628 WP 1999 8 27 ABXA9900663 1 19990817 A 5730 595606529 PANEL DOUG DOUG DC9 DC932 3022066 WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LEFT SLANT PANEL CORRODED. FABRICATED SLANT PANEL AND INSTALLED IAW DC9 SRM 51-30-1 AND DACO DWG NR 5956065. 2 L 7 2 4F A6WE 1999082700629 19990827 00629 WP 1999 8 27 ABXA9900664 1 19990817 A 5311 9918617 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND STATION 699 LEFT MAIN FRAME CRACKED. REPAIRED CRACK IAW ABX REA D953-32765MR. 2 L 7 2 4F A6WE 1999082700630 19990827 00630 WP 1999 8 27 ABXA9900665 1 19990817 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LONGERON 16 RIGHT STATION 965 CRACKED. REPLACED LONGERON SECTION STATION 950 - 996 IAW DC9 SRM 53 -02-1. 2 L 7 2 4F A6WE 1999082700631 19990827 00631 WP 1999 8 27 ABXA9900666 1 19990803 A 5711 5911301 SPAR CAP DOUG DOUG DC9 DC932 3022066 WP WS 267 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND RIGHT WING LOWER REAR SPAR CAP TANG, STATION XRS 267 CRACKED. REPAIRED IAW DC9 SRM 51-30-10 AND ABX REA 957-32858 MR. 2 L 7 2 4F A6WE 1999082700632 19990827 00632 WP 1999 8 27 MWEA99514 1 19990819 A 2560 100503119 HANGER DOUG DC9 DC982 3022082 WP GALLEY DOORWAY BROKEN A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 810ME 48072 THE AFT GALLEY DOOR EMERGENCY SLIDE HANGER BROKE OFF. MTC REMOVED AND REPLACED GIRT BAR HANGER AND REINSTALLED SLIDE DO OR. 2 L 7 2 4F A6WE 1999082700633 19990827 00633 WP 1999 8 27 MWEA99515 1 19990819 A 3350 100865 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 80ME 45795 WHEN AIRCRAFT BUSSES ARE DEPOWERED THE EMERGENCY FLOOR TRACK LIGHT ILLUMINATES. MTC REMOVED AND REPLACED FORWARD EMERGE NCY FLOOR TRACK BATTERY PACK. 2 L 7 2 4F A6WE 1999082700634 19990827 00634 WP 1999 8 27 MWEA99517 1 19990824 A 2520 SEAT BACK DOUG DC9 DC914 3022034 WP CABIN OUT OF POSITION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LEFT AND RIGHT OVERWING EXITS WILL NOT OPEN BECAUSE THEY HIT THE SEAT BACKS. MTC ADJUSTED LEFT AND RIGHT SEAT BACKS AT EXIT_ ROWS. 2 L 7 2 4F A6WE 1999082700635 19990827 00635 WP 1999 8 27 MWEA99518 1 19990824 A 5313 59114277 LONGERON DOUG DC9 DC914 3022034 WP BS 801 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LONGERON L16R, L16L, L17R, AND L17L AT STATION 801 HAD HOLES. MTC FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 1999082700636 19990827 00636 WP 1999 8 27 MWEA99519 1 19990824 A 5320 99577373 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 817 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 STATION 817 AT LONGERON 3R HAD A CRACKED INTERCOSTAL. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999082700637 19990827 00637 WP 1999 8 27 MWEA99520 1 19990824 A 5320 99118781 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 976 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FRAME 976 IS CRACKED AT INTERCOSTAL. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999082700638 19990827 00638 WP 1999 8 27 MWEA99521 1 19990824 A 5320 591014211 JAMB DOUG DC9 DC914 3022034 WP CARGO DOORWAY OVERSIZED HOLES A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FORWARD CARGO DOOR JAMB WEB AT LONGERON 28R HAS NUMEROUS OVERSIZED HOLES. MTC INSTALLED NEW WEB. 2 L 7 2 4F A6WE 1999082700639 19990827 00639 WP 1999 8 27 MWEA99522 1 19990824 A 5330 59128702 SKIN DOUG DC9 DC914 3022034 WP BS 980 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FUSELAGE EXTERIOR SKIN AT STATION 980 L18R WAS DENTED. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999082700640 19990827 00640 WP 1999 8 27 MWEA99523 1 19990824 A 5230 5911424507 SKIN DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 AFT CARGO DOOR AFT SIDE SKIN CRACKED. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999082700641 19990827 00641 WP 1999 8 27 MWEA99524 1 19990823 A 5311 59114471 FRAME DOUG DC9 DC914 3022034 WP BS 256 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 STATION 256 FRAME HAS 2 FASTENERS WITH INPROPER SPRING AND TOOL MARKS AT LONGERON 5L. MTC FABRICATED AND INSTALLED INTE RCOSTAL. 2 L 7 2 4F A6WE 1999082700642 19990827 00642 WP 1999 8 27 MWEA99525 1 19990824 A 5320 59103433 JAMB DOUG DC9 DC914 3022034 WP E & E COMPT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FS 148 E & E COMPARTMENT DOOR JAMB DOUBLER WAS CRACKED AT L27L. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999082700643 19990827 00643 WP 1999 8 27 MWEA99526 1 19990824 A 5230 59101415 PAN DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FORWARD CARGO DOOR HAS A SMALL CRACK IN PAN. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999082700644 19990827 00644 WP 1999 8 27 MWEA99527 1 19990824 A 5313 59114087 LONGERON DOUG DC9 DC914 3022034 WP BS 230 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LONGERON 5L IS CRACKED AT STATION 230. MTC FABRICATED AND INSTALLED NEW LONGERON SECTION. 2 L 7 2 4F A6WE 1999082700645 19990827 00645 WP 1999 8 27 MWEA99528 1 19990824 A 5311 5911447501 FRAME DOUG DC9 DC914 3022034 WP BS 699 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 STATION 699 FRAME HAS TOOL MARKS AND LIGHT CORROSION AT LONGERON 1-3R AND 7R-10R. MTC FABRICATED AND INSTALLED 6 SPLICE S 1 ANGLE AND FRAME. 2 L 7 2 4F A6WE 1999082700646 19990827 00646 WP 1999 8 27 MWEA99529 1 19990824 A 5311 59114481 FRAME DOUG DC9 DC914 3022034 WP BS 408 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FRAME 408 IS CORRODED BETWEEN LONGERON 30-29L. MTC FABRICATED AND INSTALLED FRAME SPLICES. 2 L 7 2 4F A6WE 1999082700647 19990827 00647 NM 1999 8 27 SCNA99113 1 19990823 A 2121 5007024620 FAN BOEING 727 727225 1384077 NM CABIN SHORTED A SCNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 282SC 7200 22558 DURING LEVEL OFF OUT OF DFW NOTICED A STONG ODOR OF SMOKE PREVALENT THROUGHOUT THE AIRCRAFT. SMOKE ODOR STRONG BUT BARE LY VISIBLE. EMERGENCY DESCENT MADE AND ALL EMERGENCY CHECK LISTS COMPLIED WITH. FOUND GASPER FAN SHORTED. REPLACED GA SPER FAN IAW MM 21231. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999082700648 19990827 00648 EU 1999 8 27 VTZA990039 1 19990423 A 5350 STRUCTURE JETAIR JETSTM JETSTM4101 1500501 EU AIRFRAME LIGHTNING STRIKE A VTZA A UNSCHED LANDING C F.O.D. CR CRUISE 1 EA 27 327UE 41080 FLT 7534 - IAD-EWR - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT PHL DUE TO LIGHTNING STRIKE AT LEFT WING TIP. AIRCRA FT RELEASED FOR FERRY FLIGHT TO IAD. MAINTENANCE REMOVED AND REPLACED LEFT AILERON, RIGHT PROP, RADOME AND PATCHED RT F LAP AFTER C/W LIGHTING STRIKE INSPECTION. MAF SATISFACTORY AND COMPASS SWING COMPLIED WITH NO DEFECTS NOTED. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999082700649 19990827 00649 NM 1999 8 27 GAIA9976 1 19990617 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST CL CLIMB 1 SW 07 6821 19496 FLT 1725 - HUF-MCO - COCKPIT EMERGENCY EXIT LIGHT REMAINS ON. AIRCRAFT CONTINUED ON TO MCO WITH NO ADDITIONAL PROBLEMS NOTED AND MADE AN UNEVENTFUL LANDING IN MCO. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY TEST OF EMER GENCY LIGHTING SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999082700651 19990827 00651 EU 1999 8 27 A6WA9900040 1 19990422 A 7600 21175789 TMS COMPUTER BAG BAE146 BAE146200A 1500266 EU NR 1 ENGINE FAILED A A6WA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 GL 31 608AW 28319 E2049 FLT 5581 - NR 1 ENGINE FAILED IN FLIGHT. ZERO OIL PRESSURE ALONG WITH RELATED MWS ANNUN, 15 MINUTE WINDMILL. N1 22.5 P ERCENT N2 12 PERCENT, OIL TEMP AND QTY AND OTHER RELATED ENGINE INSTRUMENTS APPEARED NORMAL. REMOVED AND REPLACED TMS C OMPUTER, HP FUEL FILTER INSPECTED AND REPLACED PER AMM. (M) 2 H 7 4 4F RT A49EU 1999082700652 19990827 00652 NM 1999 8 27 USAA990666 1 19990630 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND SCREW HOLE AT STATION 344 LB L 28 FLOORBEAM. CORROSION TASK NR C53-107-02 AND LEVEL 2. REPLACED DAMAGED AREA PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999082700653 19990827 00653 NM 1999 8 27 USAA990667 1 19990630 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 30660 23886 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 45 INCH AREA OF CORROSION AROUND SCREW HOLE AT STATION 344 L BL 28 FLOORBEAM. CORROSION TASK NR C53-107-02 AND LEVEL 2. REPLACED DAMAGED AREA PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999082700654 19990827 00654 EU 1999 8 27 AALA990823 1 19990520 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FRAME 69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14077 612 TUL - BULGE IN FUSELAGE SKIN AFT OF FRAME 69 BETWEEN STRINGER 23L-24L. INSTALLED DOUBLER PER SRM 53-10-12. (M) 2 L 7 2 4F RT A35EU 1999082700655 19990827 00655 EU 1999 8 27 AALA990726 1 19990518 A 5311 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 28-33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14077 612 TUL - FOUND CORROSION ON SEAT TRACK C, RIGHT UNDER LAV 'M' FRAME 28 TO 33. REPLACED SECTION OF RIGHT 'C' TRACK FROM FRA ME 28 TO FRAME 33.25 PER SRM 51-72-10-0. TREATED PER SRM 51-21-00-0. SPLICE INSTALLED PER SRM 53-10-16, FIG 204. (M) 2 L 7 2 4F RT A35EU 1999082700656 19990827 00656 EU 1999 8 27 AALA990822 1 19990525 A 5754 FLAP AIRBUS 300 A300B4605R 3930308 EU RT LE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14077 612 TUL - FOUND CORROSION INSIDE CENTER LIGHTENING HOLE ON RIGHT KRUEGER FLAP. REMOVED AND REPLACED KRUEGER FLAP PLATE ASSE MBLY (REF E58 NR 2888261 FOR KRUEGER FLAP REMOVAL. REMOVAL/INST PER MM 27-87-11-4. (M) 2 L 7 2 4F RT A35EU 1999082700657 19990827 00657 EU 1999 8 27 AALA990727 1 19990518 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14077 612 TUL - FOUND CORROSION ON FLOOR SUPPORT 'E' LEFT SIDE BETWEEN FRAME 71 AND 73. REMOVED AND INSTALLED NEW FLOOR SUPPORT ' E' LEFT SIDE BETWEEN FRAME 71-73. (M) 2 L 7 2 4F RT A35EU 1999082700658 19990827 00658 EU 1999 8 27 AALA990655 1 19990423 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - FLOORBOARD SUPPORT CORRODED SEVERAL PLACES BETWEEN FRAMES 71 TO 74, JUST AFT OF TRACK NR 5. INSTALLED NEW FLOORBO ARD SUPPORT PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700659 19990827 00659 EU 1999 8 27 AALA990664 1 19990505 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FRAME 46 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - FOUND BELL FRAME AT STATION 46L IS CRACKED. INSTALLED DOUBLER REPAIR PER AARD 53-00-00-7 AT FRAME 46L. (M) 2 L 7 2 4F RT A35EU 1999082700660 19990827 00660 EU 1999 8 27 AALA990663 1 19990505 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU BS 45 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - FOUND BELL FRAME AT 45L IS CRACKED. INSTALLED DOUBLER REPAIR AT FRAME 45L PER AARD 53-00-00-7. (M) 2 L 7 2 4F RT A35EU 1999082700661 19990827 00661 WP 1999 8 27 AALA990969 1 19990625 A 5755 4936976501 BOLT DOUG DC9 DC982 3022082 WP SPOILER FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 424AA 49336 TUL - FOUND THE GRUOND SPOILER MOUNT BOLT WAS FOUND SHEARED. HALF OF THE BOLT WAS STILL ATTACHED, THE OTHER HALF WAS LA YING ON THE PANEL UNDER ACTUATOR. REPLACED BOLT PER MM 27-62-02-2. (M) 2 L 7 2 4F A6WE 1999082700662 19990827 00662 EU 1999 8 27 AALA990662 1 19990505 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FRAME 46 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - FOUND BELL FRAME AT 46R IS CRACKED. INSTALLED DOUBLER REPAIR AT FRAME 46R PER AARD 53-00-00-7. (M) 2 L 7 2 4F RT A35EU 1999082700663 19990827 00663 EU 1999 8 27 AALA990661 1 19990505 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FRAME 45 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - FOUND BELL FRAME 45R CRACKED. INSTALLED DOUBLER REPAIR PER AARD 53-00-00-7. (M) 2 L 7 2 4F RT A35EU 1999082700664 19990827 00664 EU 1999 8 27 AALA990920 1 19990619 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 75-76 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 75-76 AT AFT END R-4 DOOR. INSTALLED NEW F/B SUPPORT PER SRM 51-72- 10-0. (M) 2 L 7 2 4F RT A35EU 1999082700665 19990827 00665 EU 1999 8 27 AALA990919 1 19990618 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 75-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND FLOORBOARD 'D' LEFT CORRODED SEVERAL AREAS. INSTALLED NEW FLOOR SUPPORT PER SRM 51-70-00. (M) 2 L 7 2 4F RT A35EU 1999082700666 19990827 00666 NM 1999 8 27 AALA990925 1 19990824 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 305 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK IN FUSELAGE FRAME (PARTIALLY SEVERED) AT BS 305 STR 4L. I NSTALLED REPLACEMENT WEB PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999082700667 19990827 00667 EU 1999 8 27 AALA990926 1 19990618 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74-76 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 74-76 AFT NR 3 SEAT TRACK. REPLACED F/B SUPPORT PER SRM 51-72-10-0 FROM FRAME 74 TO 76. (M) 2 L 7 2 4F RT A35EU 1999082700668 19990827 00668 EU 1999 8 27 AALA990927 1 19990618 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 73-76 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 73-76 LEFT CENTER OF CABIN. REPLACED F/B SUPPORT PER SRM 51-72-10-0 . (M) 2 L 7 2 4F RT A35EU 1999082700669 19990827 00669 EU 1999 8 27 AALA990928 1 19990618 A 5320 A53279722200 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 75-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAME 75-80 IN CENTER OF CABIN. REPLACED F/B SUPPORT PER SRM 51-72-10-0. ( M) 2 L 7 2 4F RT A35EU 1999082700670 19990827 00670 EU 1999 8 27 AALA990929 1 19990618 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT OUTBOARD OF LAV V TIE DOWN BETWEEN FRAMES 71-74. INSTALLED F/B SUPPORT OUTBOARD OF LAV V TIE DOWN FROM FRAME 71 TO 74 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999082700671 19990827 00671 EU 1999 8 27 AALA990910 1 19990619 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 57.1 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON LONGERON 58 FORWARD OF FRAME 57.1. REPAIRED PER 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1999082700672 19990827 00672 EU 1999 8 27 AALA990863 1 19990611 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 75 AND 78 RIGHT SIDE. INSTALLED FLOORBOARD SUPPORT PER SRM 51-72-90 -0. (M) 2 L 7 2 4F RT A35EU 1999082700673 19990827 00673 EU 1999 8 27 AALA990864 1 19990611 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT FRAME 71 TO 73 AFT AND OUTBOARD NR 6 SEAT TRACK. INSTALLED NEW F/B SUPPORT PER 51- 72-10. (M) 2 L 7 2 4F RT A35EU 1999082700674 19990827 00674 EU 1999 8 27 AALA990867 1 19990416 A 5347 A53279212201 TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 73-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - LAV 'Z' INBOARD SUPPORT TRACK CORRODED. TRACK REPLACED PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999082700675 19990827 00675 EU 1999 8 27 AALA990868 1 19990614 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 73-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND OUTBOARD SEAT TRACK FOR LAV 'Z' CORRODED. SEAT TRACK WAS REPLACED PER 51-72. (M) 2 L 7 2 4F RT A35EU 1999082700676 19990827 00676 EU 1999 8 27 AALA990869 1 19990614 A 5347 A53279212200 TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 73-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - LAV TIE DOWN TRACK CORRODED BETWEEN FRAME 73-74, LEFT INBOARD SHORT TRACK. TRACK WAS REPLACED PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700677 19990827 00677 EU 1999 8 27 AALA990870 1 19990414 A 5347 A53279000204 TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - ADAPTER TRACK CORRODED JUST INSIDE AND FORWARD OF L4 DOOR. ADAPTER REPLACED PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999082700678 19990827 00678 EU 1999 8 27 AALA990874 1 19990614 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 72-73, INBOARD OF NR 3 SEAT TRACK. REMOVED AND REPLACED PER SRM 51- 72-10. (M) 2 L 7 2 4F RT A35EU 1999082700679 19990827 00679 EU 1999 8 27 AALA990875 1 19990614 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON FLOORBEAM BETWEEN FRAMES 71-74, AFT OF NR 5 SEAT TRACK. REMOVED AND REPLACED PER SRM 51-72. ( M) 2 L 7 2 4F RT A35EU 1999082700680 19990827 00680 EU 1999 8 27 AALA990876 1 19990614 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON SEAT TRACK AT STATION 49 RIGHT. REMOVED AND REPLACED SEAT TRACK PER SRM 51-74. (M) 2 L 7 2 4F RT A35EU 1999082700681 19990827 00681 EU 1999 8 27 AALA990877 1 19990614 A 5347 AIRBUS 300 A300B4605R 3930308 EU UNKNOWN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON SEAT TRACK AT STATION 65 RIGHT. REMOVED AND REPLACED PER SRM 51-74. (M) 2 L 7 2 4F RT A35EU 1999082700682 19990827 00682 EU 1999 8 27 AALA990878 1 19990614 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 71-72 INBOARD SEAT TRACK NR 6. REMOVED AND REPLACED FLOORBOARD SUPP ORT PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700683 19990827 00683 EU 1999 8 27 AALA990879 1 19990614 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 79 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT FROM FRAME 79-80 ON RIGHT SIDE OF CABIN. REMOVED AND REPLACED F/B SUPPORT FROM FRA ME 74 TO 80 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700684 19990827 00684 EU 1999 8 27 AALA990880 1 19990615 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT LEFT FROM FRAME 75 TO 80. INSTALLED LEFT F/B SUPPORT FROM FRAME 74 TO 80, 3RD F/B SUPPORT FROM LEFT SIDE PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700685 19990827 00685 EU 1999 8 27 AALA990892 1 19990615 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 77-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - F/B SUPPORT CORRODED 3 PLACES RIGHT SIDE OF CABIN BETWEEN FRAMES 77-80. INSTALLED SERVICEABLE BEAM P/N A532-79224 -001-0019 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700686 19990827 00686 EU 1999 8 27 AALA990893 1 19990616 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON SEAT TRACK AT STATION 58 LEFT. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-72-10 -0. (M) 2 L 7 2 4F RT A35EU 1999082700687 19990827 00687 EU 1999 8 27 AALA990894 1 19990615 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 75-76 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT 'F' BETWEEN FRAME 75 AND 76. REPLACED FLOORBOARD SUPPORT 'F' BETWEEN FRAME 75 AND 76 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700688 19990827 00688 EU 1999 8 27 AALA990895 1 19990615 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT ON SIDE OF FRAME 74 IN CENTER OF CABIN. REPLACED FLOORBOARD SUPPORT ON AFT SIDE OF FRAME 74 IN CENTER OF CABIN PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700689 19990827 00689 EU 1999 8 27 AALA990896 1 19990616 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74-75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON F/B SUPPORT IN CENTER OF CABIN FROM FRAME 74 TO 75. INSTALLED NEW F/B SUPPORT FROM FRAME 74 TO 75 IN CENTER CABIN PER SRM 51-14-10-2. (M) 2 L 7 2 4F RT A35EU 1999082700690 19990827 00690 EU 1999 8 27 AALA990897 1 19990616 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - F/B SUPPORT CORRODED FROM FRAME 74 TO FRAME 80 ON LEFT SIDE OF CABIN. REMOVED AND REPLACED F/B SUPPORT FROM FRAME 74 TO FRAME 80 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700691 19990827 00691 EU 1999 8 27 AALA990898 1 19990617 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU L4 DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - Z-ANGLE CORRODED AT AFT JAMB OF L-4 DOOR SILL PLATE AT FLOOR LINE. INSTALLED 'Z' ANGLE LEFT DOOR AND AFT OF DOOR FRAME 75A PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999082700692 19990827 00692 EU 1999 8 27 AALA990899 1 19990617 A 5320 TIE DOWN AIRBUS 300 A300B4605R 3930308 EU BS 261 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON LAV TIE DOWN ON AFT SIDE OF FRAME 74 OUTBOARD OF NR 5 SEAT TRACK. REPLACED TIE DOWN AFT SIDE O F FRAME 74 OUTBOARD OF NR 5 SEAT TRACK PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999082700693 19990827 00693 EU 1999 8 27 AALA990900 1 19990617 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 261 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND CORROSION ON SUPPORT ANGLE AT AFT END OF L-4 DOOR OPENING BETWEEN FRAME 75-76. INSTALLED ANGLE AFT END OF L -4 DOOR PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999082700694 19990827 00694 EU 1999 8 27 AALA990971 1 19990628 A 3260 PROX UNIT AIRBUS 300 A300B4605R 3930308 EU LANDING GEAR NOT SEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 TUL - FOUND LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. ON TOUCH DOWN, AUTO BRAKES GRABBED THEN RELEASED BRAKE PEDALS G AVE NO BRAKING FORCE. ALT BRAKE WAS SELECTED TO STOP. (M) 2 L 7 2 4F RT A35EU 1999082700695 19990827 00695 NM 1999 8 27 AALA990690 1 19990505 A 5330 SKIN BOEING 727 727227 1384078 NM BS 380 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND DEEP DENT IN SKIN ADL ITEM NR 46 AT STATION 380, ABOVE STRINGER 17L. INSTALLED EXTERNAL DOUBLER .080 2024T3 , 7 INCH BY 9 INCH PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999082700696 19990827 00696 NM 1999 8 27 AALA990689 1 19990509 A 5310 STRUCTURE BOEING 727 727227 1384078 NM BS 940 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND SKIN CRACKED AT 940 CASTING AT STRINGER 18A AND STRINGER 18A CRACKED AT GEAR BEAM 'H' LINK ATTACH BOLT AND G OING AFT ABOUT 1 INCH. INSTALLED SKIN DOUBLER AND STRINGER 18 SPLICE IAW SB 727-53-0172. (M) 2 L 7 3 4F A3WE 1999082700697 19990827 00697 NM 1999 8 27 AALA990684 1 19990507 A 5730 SKIN BOEING 727 727223 1384074 NM BS 833 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND CORROSION ON LOWER CENTER TANK OUTER SKIN STATION 833 RBL 20-24. REMOVED CORROSION AND REPAIRED AREA PER ES O 11697, DATED 5-7-99 PAGES 1/2. (M) 2 L 7 3 4F A3WE 1999082700698 19990827 00698 NM 1999 8 27 AALA990886 1 19990609 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CABIN FLOORBEAM CORRODED TOP SIDE RBL 52-62. REMOVED CORROSION AND INSTALLED REPAIRED DOUBLER PER AARD 53-10-07-2 . (M) 2 L 7 3 4F A3WE 1999082700699 19990827 00699 NM 1999 8 27 AALA990885 1 19990616 A 5321 FLOOR BOEING 727 727223 1384074 NM BS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - EXFOLIATED CORROSION ON FLOOR PAN EXTRUDING UNDER AND CAUSING BULGING TO FLOOR STRAP ON FORWARD SIDE OF STATION 11 83 BULKHEAD, AT LOWER RIGHT CORNER OF VAULT DOOR FRAME, RBL 14 - RBL 24. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40 -2 AND FLOOR PAN ON FORWARD SIDE OF STATION 1183, LOWER RIGHT CORNER OF VAULT DOOR FRAME RBL 14 - RBL 24. (M) 2 L 7 3 4F A3WE 1999082700700 19990827 00700 NM 1999 8 27 AALA990884 1 19990615 A 5330 SKIN BOEING 727 727223 1384074 NM BS 312 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - HFEC INDICATES CRACK IN FUSE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER BSB 727-53-0198 PAGE 32, FIG 4 DETAIL IV. (M) 2 L 7 3 4F A3WE 1999082700701 19990827 00701 EU 1999 8 27 AALA990959 1 19990628 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU L4 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT L4 DOOR BELOW FLIGHT ATTENDANT SEAT INOPERATIV E. MAINTENANCE FOUND A LOOSE CONNECTOR. RESECURED LOOSE CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUN D CHEKED NORAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999082700702 19990827 00702 EU 1999 8 27 AALA990958 1 19990628 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU ROW 12-14 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 12H THROUGH 14H INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT FLAT JUMPER WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999082700703 19990827 00703 EU 1999 8 27 AALA990976 1 19990702 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU R2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77080 626 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT R2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT STRIPS AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999082700704 19990827 00704 EU 1999 8 27 AALA990939 1 19990624 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 2-24 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77080 626 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 20-24 A/B INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT 21 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999082700705 19990827 00705 EU 1999 8 27 AALA990932 1 19990623 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU L4/R4 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80052 460 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ON FLOOR AT R4 AND L4 INOPERATIVE. REPLACED EMERGENCY EXIT FLOO R PATH LIGHT STRIP AT R4 AND L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999082700706 19990827 00706 EU 1999 8 27 AALA990938 1 19990623 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU L3 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70079 619 MIA - DURING OVERNIGHT MAINTENANCE, AFT L3 EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT AFT L3 DOOR. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999082700707 19990827 00707 EU 1999 8 27 AALA990930 1 19990622 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 24-27 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70079 619 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 24/25B, 27/27G AND 24H INOPERATIVE. RECONNE CTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT 24H AND 27C-G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999082700708 19990827 00708 NM 1999 8 27 AALA990954 1 19990626 A 2780 S256T00510 MODULE BOEING 767 767323 1385205 NM RT LE SLAT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 361AA 24042 DFW - FLT 945 - DURING CLIMB-OUT, SLATS WERE RETRACTED AND A SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. CREW RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT SLAT CONTROL MODULE FAULTY. REPLACED RIGH T SLAT CONTROL MODULE. ACCOMPLISHED REQUIRED OPERATIONAL AND LEAK CHECKS. OVERWEIGHT LANDING WAS ACCOMPLISHED WITH NO ABNORMAL FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999082700709 19990827 00709 WP 1999 8 27 AALA990972 1 19990628 A 3350 1001141 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7522A 49899 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF FIRST CLASS CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. RE PLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700710 19990827 00710 WP 1999 8 27 AALA990970 1 19990628 A 3397 WIRE DOUG DC9 DC982 3022082 WP AIRSTAIR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 418AA 49329 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT AIRSTAIR TAIL SECTION INOPERATIVE. REPAIRED EMERGENCY E XIT LIGHT BROKEN WIRE IN AFT AIRSTAIR TAIL SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700711 19990827 00711 WP 1999 8 27 AALA990960 1 19990628 A 3397 WIRE DOUG DC9 DC982 3022082 WP AIRSTAIR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 249AA 49269 DFW - DURNIG OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT AIRSTAIR TAIL SECTION INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT BROKEN WIRE IN AFT AIRSTAIR TAIL SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700712 19990827 00712 NM 1999 8 27 AALA990955 1 19990706 A 3397 WIRE BOEING 757 757223 1384957 NM R4 DOORWAY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 182AN 29592 DFW - DURING OVERNIGHT MAINTENANCE R4 DOOR AFT EXIT SIGN INOPERATIVE. RECONNECTED WIRE ON EMERGENCY EXIT SIGN WIRE QUIC K DISCONNECT. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999082700713 19990827 00713 WP 1999 8 27 AALA990952 1 19990625 A 3397 WIRE DOUG DC9 DC982 3022082 WP PAX DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 405A 49316 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD PASSENGER DOOR EXIT MARKER INOPERATIVE. REPAIRED WIRING FOR FORWARD PASSENG ER DOOR EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700714 19990827 00714 WP 1999 8 27 AALA990957 1 19990628 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 21 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 416AA 49327 SAT - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT ROW 21 AFT INOPERATIVE. RESEATED LOOSE EMERGENCY EX IT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700715 19990827 00715 WP 1999 8 27 AALA990951 1 19990625 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 1, 9, 13 AND LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 428AA 49340 SFO - DURING OVERNIGHT CHECK, OVERHEAD EMERGENCY EXIT LIGHTS AT SEAT ROWS 1, 9, 13 AND 23 INOPERATIVE. RESEATED PINS 3 AND 5 IN FORWARD CHARGER CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700716 19990827 00716 WP 1999 8 27 AALA990943 1 19990627 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 12 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 236AA 49251 DFW - DURING OVERNIGHT MAINTENANCE SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 12 INOPERATIVE AND MISSING LENS. R EPLACED SEAT MOUNTED LIGHT ASSEMBLY AND LENS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700717 19990827 00717 WP 1999 8 27 AALA990921 1 19990622 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 462AA 49592 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700718 19990827 00718 WP 1999 8 27 AALA990922 1 19990622 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7537A 49991 DFW - DURING OVERNIGHT MAINTENANCE GALLEY DOOR EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REINSTALLED PINS IN QUICK DISCONN ECT CONNECTOR FOR GALLEY DOOR EMERGENCY EXIT LIGHT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999082700719 19990827 00719 WP 1999 8 27 AALA990923 1 19990622 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 214AA 49162 MIA - DURING OVERNIGHT MAINTENANCE FORWARD GALLEY DOOR EMERGENCY EXIT LIGHTS AND FLOOR PATH LIGHTING INOPERATIVE. REPAI RED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP AND REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 1999082700720 19990827 00720 NE 1999 8 27 AALA990949 2 19990625 A 7250 804061 BEARING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 2 ENGINE FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 450AA 49476 725576 SAN - FLT 2090 - DURING T/O, LOST POWER ON NR 2 ENG. AIRCRAFT DIVERTED TO MIRAMAR MARINE AIR BASE (NKX) OVERWEIGHT AND WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENG, PERFORMED ENG RUN UP AND LEAK CHECK. PERFORMED O/W INSPECTION WITH NO DISC REPANCIES. SYSTEM GROUND CHECKED NORMAL OPERATION. THE LONG SHAFT FRACTURED APPROX 25 INCHES BACK FROM THE LPC END. TH E CAUSE FOR THE LONG SHAFT FAILURE WAS DUE TO RUBBING ON THE CENTER TUBE TOGETHER WITH COKING BUILDUP. THE RUBBING IS A TTRIBUTED TO THE FAILURE OF THE NR 3 BEARING. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999082700721 19990827 00721 NM 1999 8 27 AALA990714 1 19990515 A 2133 10328051 OUTFLOW VALVE BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 872AA 21384 SJU - FLT 1938 - DURING CLIMB-OUT AT FL300, CABIN PRESSUER STARTED CLIMBING AT 2000 FPM. CREW PERFORMED RAPID DECOMPRES SION CHECKLIST WITHOUT RESULTS. CABIN ALTITUDE APPROACHED 10,000 FT. CREW PERFORMED EXPLOSIVE DECOMPRESSION CHECKLIST. FLIGHT AIR INTERRUPTED AND RETURNED SJU LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND DETERMIN ED OUTFLOW VALVES FAULTY. REPLACED OUTFLOW VALVES AND AS A PRECAUTIONARY. REPLACED AUTO/MANUAL CONTROL PANELS. SYSTEM LEAK CHECKED OK. FUNCTIONAL CHECK FLIGHT HAD NO REOCCURRING PRESSURIZATION PROBLEMS. AIRCRAFT WAS RELEASE FOR REVENUE SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999082700722 19990827 00722 NM 1999 8 27 AALA990709 1 19990514 A 3230 65931551056 ACTUATOR BOEING 727 727223 1384074 NM NLG LEAKING A AALA K NONE J K WARNING INDICATION FLUID LOSS AP APPROACH 1 SW 07 869AA 21374 DFW - FLT 1654 - DURING APPROACH, UNABLE TO EXTEND NOSE GEAR ON FIRST ATTEMPT BUT, EXTENDED NORMALLY ON SECOND ATTEMPT. FLIGHT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE GEAR UNLOCK ACTUATOR LEAKING. REPLACED NOSE GEAR U NLOCK ACTUATOR. LEAK AND OPERATIONS CHECKS WERE NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 3 4F A3WE 1999082700723 19990827 00723 EU 1999 8 27 UF6A990607 1 19990606 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU ROW 7CD FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 ORD - FLOOR PROXIMITY LIGHT STRIP IS INOPERATIVE AT ROW 7CD. MAINTENANCE REMOVED AND REPLACED NR 3 POWER SUPPLY. SYSTE M OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700724 19990827 00724 EU 1999 8 27 UF6A990605 1 19990604 A 5330 SKIN BAG ATP ATP EU FUSELAGE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 FWA - BAGGAGE CARG HIT AIRCRAFT BY AFT BAGGAGE DOOR. MAINTENANCE INSPECTED DAMAGE BEHIND AFT BAGGAGE DOOR AND WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-10-01. ITEM WAS PLACED ON 250 HOUR CARRY-OVER. (M) 2 L 7 2 4T RT A27NM 1999082700725 19990827 00725 EU 1999 8 27 UF6A990604 1 19990604 A 5400 JD711J0016000 AIR SCOOP BAG ATP ATP EU LT NACELLE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SEN - LEFT ENGINE INBOARD NACA DUCT AIR SCOOP IS DAMAGED. MAINTENANCE REMOVED AND REPLACED MODULAR 6. (M) 2 L 7 2 4T RT A27NM 1999082700726 19990827 00726 EU 1999 8 27 UF6A990416 1 19990429 A 2433 TR202B TRU BAG ATP ATP EU NR 2 FAILED A UF6A A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 31 854AW 11555 2028 ORD - FLT 5715 - NR 2 TRU DROPPED OFF LINE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 2 TRU. SYSTEM OPS CHECKED GO OD. (M) 2 L 7 2 4T RT A27NM 1999082700727 19990827 00727 NE 1999 8 27 UF6A990611 2 19990612 A 7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE NR 1 FAILED A UF6A A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 GL 31 856AW 10484 2032 124414 ORD - FLT 5708 - DURING CLIMB, THERE WAS A LOUD POP FROM THE LEFT SIDE. IMMEDIATELY THE NR 1 ENGINE OIL PRESSURE, ENGIN E CONTROL CWP ILLUMINATED WITH NR 1 ENGINE FROZEN PBSI ILLUMINATING. SHORTLY FOLLOWING THE NR 1 ENGINE ASSOCIATED ELECT RICAL CWP'S ILLUMINATED AND NR 1 TORQUE READ 0. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. PERFORMED POWER ASSU RANCE RUNS WITH NO DEFECTS NOTED. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999082700728 19990827 00728 EU 1999 8 27 UF6A990608 1 19990607 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 ORD - EMERGENCY EXIT LIGHTS AT RIGHT AND LEFT OVERWING EXITS AND FLOOR PROXIMITY LIGHTING INOPERATIVE. MAINTENANCE REMO VED AND REPLACED NR 2 POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700729 19990827 00729 EU 1999 8 27 UF6A990609 1 19990812 A 5400 JD711J0219000 MODULAR 6 BAG ATP ATP EU NR 1 ENGINE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - LEFT MODULAR 6 IS CRACKED AT THE AFT FAIRING. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW BAE ATP SRM. (M ) 2 L 7 2 4T RT A27NM 1999082700730 19990827 00730 EU 1999 8 27 UF6A990610 1 19990606 A 7712 3039242 NH PROBE BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A K NONE O OTHER UK UNKNOWN 1 GL 31 851AW 667 CH10151 2020 ORD - FLT 5750 - NR 2 NH WAS ABOVE LIMITS IN CRUISE POWER. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE NR 1 NH PRO BE. PERFORMED POWER ASSURANCE RUNS WITH NO DEFECTS NOTED. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700731 19990827 00731 EU 1999 8 27 UF6A990612 1 19990617 A 5330 SKIN BAG ATP ATP EU BS 413.9 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 2029 ORD - FLT 5712 - REQUEST INSPECTION OF AFT FUSELAGE BELOW HORIZONTAL STABILIZER ON CENTER LINE. MAINTENANCE FOUND DAMAG E UNDER HORIZONTAL STABILIZER AT FORMER 413.9. DAMAGED AREA WAS REPAIRED IAW BAE ATP SRM 53-30, 53-10, AND 51-60-03. ( M) 2 L 7 2 4T RT A27NM 1999082700732 19990827 00732 EU 1999 8 27 UF6A990614 1 19990616 A 3350 58785 LIGHT BAG ATP ATP EU CABIN LOOSE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 2020 ORD - FLT 5734 - FIRST EMERGENCY LIGHT STRIP NEEDS TO BE SECURED. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP. (M ) 2 L 7 2 4T RT A27NM 1999082700733 19990827 00733 EU 1999 8 27 UF6A990613 1 19990616 A 5330 SKIN BAG ATP ATP EU BS 198 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 ORD - FLT 5701 - REQUEST INSPECTION OF 16 INCH SCRATCH AND SMALL DENT ON RIGHT AFT FUSELAGE. MAINTENANCE INSPECTED AREA AND WAS FOUND TO BE WITHIN LIMITS. DAMAGE IS LOCATED AT 198AS. PLACED ITEM ON TCO FOR 2 YEAR REINSPECTION REQUIREMENT . ALL WORK DONE IAW BAE ATP SRM 51-10-00. (M) 2 L 7 2 4T RT A27NM 1999082700734 19990827 00734 EU 1999 8 27 UF6A990615 1 19990617 A 3350 1317 BULB BAG ATP ATP EU EMER EXIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - AFT EMERGENCY OVERWING LIGHT INOPERATIVE ON RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1999082700735 19990827 00735 EU 1999 8 27 UF6A990521 1 19990506 A 5220 JD536J0011000 STRIKE BAG ATP ATP EU EMER EXIT SCORED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT EMERGENCY DOOR APERTURE AND SEAL STRIKER PLATE HAS SEVERAL SCORED AREAS. MAINTENANCE BURNISHED WORN SPOTS AN D DAMAGE WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700736 19990827 00736 EU 1999 8 27 UF6A990533 1 19990508 A 5320 JD256J0064001 BRACKET BAG ATP ATP EU BS 324 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FORWARD PASSENGER DOOR TOP AFT ESCAPE SLIDE MOUNTING BRACKET IS DAMAGED. MAINTENANCE REMOVED AND REPLACED BRACKET . (M) 2 L 7 2 4T RT A27NM 1999082700737 19990827 00737 EU 1999 8 27 UF6A990534 1 19990511 A 5320 5D11186 INTERCOSTAL BAG ATP ATP EU BS 360/343 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - INTERCOSTAL BETWEEN FLOORBEAM AT STATION 360FS AND 343FS HAS CORROSION AROUND NUTPLATE HOLE. MAINTENANCE REAMED O UT THE NUTPLATE HOLE TO .50 DIAMETER AND FABRICATED A STRAP OF 2024-T3, .063 THICK BY 4.00 LONG BY .75 WIDE. ALL WORK W AS DONE IAW ENGINEERING ORDER NR 99-091. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700738 19990827 00738 EU 1999 8 27 UF6A990535 1 19990511 A 5315 JD533J0104002 FLOORBEAM BAG ATP ATP EU BS 343 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLOORBEAM AT STATION 343FS HAS CORROSION. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED AND ANGLE FROM 2024-T3, .050 THICK BY 19.75 INCHES LONG BY 1 INCH WIDE. ANGLE WAS SPLICED INTO FLOORBEAM BY FABRICATING A STRAP FROM 2024-T3, .050 INCHES THICK. ALL WORK WAS DONE IAW ENGINEERING ORDER NR 99-091. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700739 19990827 00739 EU 1999 8 27 UF6A990536 1 19990511 A 5315 JD533J0003002 FLOORBEAM BAG ATP ATP EU BS 324 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLOORBEAM AT STATION 324FS HAS CORROSION. MAINTENANCE CLEANED CORROSION AND SMOOTHERD SHARP EDGES. AREA WAS ALOD INED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. ALL WORK WAS DONE IAW ENGINEERING ORDER NR 99-091. (M) 2 L 7 2 4T RT A27NM 1999082700740 19990827 00740 EU 1999 8 27 UF6A990537 1 19990510 A 5320 BRACKET BAG ATP ATP EU E/E COMPT CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FORWARD AVIONICS CRATE BRACKETS ON FORWARD RIGHT SIDE IS CRACKED. MAINTENENANCE FABRICATED NEW BRACKET AND INSTAL LED. AREA WAS ALODINED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-13 AND 51-40-01. (M) 2 L 7 2 4T RT A27NM 1999082700741 19990827 00741 EU 1999 8 27 UF6A990538 1 19990510 A 5320 BRACKET BAG ATP ATP EU E/E COMPT CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FORWARD AVIONICS CRATE BRACKETS ON FORWARD AND AFT LEFT SIDE IS CRACKED. MAINTENANCE FABRICATED NEW BRACKET AND I NSTALLED. AREA WAS ALODINED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-1 3 AND 51-40-01. (M) 2 L 7 2 4T RT A27NM 1999082700742 19990827 00742 EU 1999 8 27 UF6A990539 1 19990509 A 5751 JD576J0002000W STRINGER BAG ATP ATP EU RT AILERON CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT AILERON UPPER STRINGER NR 2 AT STATION 342.696 WAS FOUND TO BE CRACKED. MAINTENANCE FABRICATED NEW STRINGER FROM RIB 333.454 TO 359.216. AREA WAS ALODINED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-03 AND 51-40-01. (M) 2 L 7 2 4T RT A27NM 1999082700743 19990827 00743 EU 1999 8 27 UF6A990540 1 19990511 A 5315 JD533J0245000 FLOORBEAM BAG ATP ATP EU BS 270 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLOORBEAM AT STATION 270AS HAS CORROSION IN THREE AREAS ACROSS BEAM. CONCERNED AREAS ARE BY THE AFT BAGGAGE DOOR, IN THE CENTER, AND BY THE AFT PASSENGER DOOR. MAINTENANCE REMOVED CORROSION BY MECHANICAL METHOD. AREA WAS ALODINED, PRIMED. STRAP WAS FABRICATED FROM 2024-T3, .071 INCH THICK, 2 INCH WIDE, AND 72.5 INCH LONG. STRAP WAS INSTALLED TO TH E TOP FLANGE OF THE FLOORBEAM. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-091. (M) 2 L 7 2 4T RT A27NM 1999082700744 19990827 00744 EU 1999 8 27 UF6A990541 1 19990511 A 5320 SUPPORT BAG ATP ATP EU BS 380 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - GALLEY AREA PANEL SUPPORT HAS CORROSION AT STATION 380AS. MAINTENANCE REMOVED AND REPLACED PANEL SUPPORT ANGLE. A REA WAS ALODINED AND PRIMED. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-13. (M) 2 L 7 2 4T RT A27NM 1999082700745 19990827 00745 EU 1999 8 27 UF6A990542 1 19990511 A 5347 JD533J0017000 SEAT TRACK BAG ATP ATP EU BS 252 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - REAR SEAT TRACK ON LEFT AND RIGHT SIDE HAS CORROSION IN GALLEY AREA, APPROXIMATELY STATION 252AS. MAINTENANCE REM OVED AND REPLACED CORRODED SEAT TRACK ON BOTH THE LEFT AND RIGHT SIDE. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-13. (M) 2 L 7 2 4T RT A27NM 1999082700746 19990827 00746 EU 1999 8 27 UF6A990543 1 19990511 A 5312 JD255J0282000 BULKHEAD ANGLE BAG ATP ATP EU BS 308 WORN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - AFT BAGGAGE, FORWARD BULKHEAD, ATTACHMENT ANGLE FOR SURROUND ON THE RIGHT SIDE OF THE FUSELAGE HAS SEVERAL WORN S POTS. MAINTENANCE REPAIRED WORN SPOTS IAW ENGINEERING ORDER 99-091. (M) 2 L 7 2 4T RT A27NM 1999082700747 19990827 00747 EU 1999 8 27 UFTA990544 1 19990511 A 5523 JD552J0001004 SKIN BAG ATP ATP EU ELEV TRIM TAB DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 ORD - DENT FOUND IN TWO LOCATIONS ON RIGHT ELEVATOR TRIM TAB. MAINTENANCE INSPECTED TRIM TAB IAW BAE ATP SRM 55-20-00 A ND 51-10-01, DAMAGE WAS FOUND TO BE WITHIN LIMITS. REPAIR OF DAMAGE IS PENDING IAW BAE ATP SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999082700748 19990827 00748 EU 1999 8 27 UF6A990545 1 19990512 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 10373 2034 SBN - CABIN EMERGENCY LIGHTS ARE WEAK AND INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE NR 4 POWER SUPPLY SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700749 19990827 00749 1999 8 27 UF6A990547 4 19990514 A 2565 2077000 SLIDE BAG ATP ATP EU CARGO DOORWAY FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 1738 2029 SBN - AFT BAGGAGE DOOR SLIDE FAILED FUNCTIONAL TEST. MAINTENANCE MANUALLY DEPLOYED SLIDE AND REMOVED AND REPLACED. (M) 2 L 7 2 4T RT A27NM 1999082700750 19990827 00750 EU 1999 8 27 UF6A990548 1 19990514 A 2560 JD256J0006000 FITTING BAG ATP ATP EU PAX DOORWAY OUT OF ADJUST A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 SBN - FLT 5940 - FORWARD PASSENGER DOOR IS JAMMED. MAINTENANCE FOUND GIRT BAR TO BE MISALIGNED. GIRT BAR WAS RESECURED AND SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700751 19990827 00751 EU 1999 8 27 UF6A990546 1 19990512 A 2560 2077001 SLIDE BAG ATP ATP EU BS 289 OUT OF ADJUST A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 8156 2029 ORD - FLT 5706 - REQUEST INSPECTION OF EVACUATION SLIDE ON THE AFT PASSENGER DOOR. MAINTENANCE FOUND SLIDE MISALIGN AND CATCHING ON DOOR. SLIDE WAS REMOVED AND REPLACED. (M) 2 L 7 2 4T RT A27NM 1999082700752 19990827 00752 EU 1999 8 27 UF6A990511 1 19990504 A 5753 229F10462 SKIN BAG ATP ATP EU RT TE FLAP TAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT FLAP TAB SKIN HAS APPROXIMATELY A .025 INCH CRACK AT STATION 34.071. MAINTENANCE INSTALLED REPAIR TO DAMAGE D AREA IAW BAE ATP SRM 57-50-01. (M) 2 L 7 2 4T RT A27NM 1999082700753 19990827 00753 EU 1999 8 27 UF6A990510 1 19990501 A 5720 JD573J0040004 TIP BAG ATP ATP EU WS 534.83 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT FORWARD WING TIP END CAP HAS A CRACKED RIB ASSEMBLY. MAINTENANCE REPAIRED DAMAGED AREA AND INSTALLED DOUBLER IAW BAE ATP SRM 51-60-04. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700754 19990827 00754 EU 1999 8 27 UF6A990509 1 19990501 A 5720 BAG ATP ATP EU UNKNOWN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT AFT WING TIP END CAP HAS CORROSION AT ATTACHMENT HINGE. MAINTENANCE REPAIRED DAMGED AREA AND FABRICATED DOUB LER IAW BAE ATP SRM 51-60-04. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700755 19990827 00755 EU 1999 8 27 UF6A990508 1 19990503 A 5320 JD574J0001003 ANGLE BAG ATP ATP EU BS 117 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT HORIZONTAL STABILIZER HAS A CRACK ON THE INBOARD LEADING EDGE TOP ATTACHMENT ANGLE AT STATION 117.00. MAINTE NANCE CUT OUT DAMAGED AREA AND FABRICATED DOUBELR IAW BAE ATP SRM 51-60-02 FIGURE 2. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700756 19990827 00756 EU 1999 8 27 UF6A990507 1 19990504 A 5320 106D11186 INTERCOSTAL BAG ATP ATP EU STATION 289/360 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - INTERCOSTAL BETWEEN STATIONS 360AS AND 278AS HAS CORROSION. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE WIT HIN LIMITS IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700757 19990827 00757 EU 1999 8 27 UF6A990506 1 19990504 A 5315 JD533J0244000 FLOORBEAM BAG ATP ATP EU BS 289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLOORBEAM AT STATION 289AS HAS CORROSION ON RIGHT SIDE. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700758 19990827 00758 EU 1999 8 27 UF6A990504 1 19990504 A 5315 1D11905 FLOORBEAM BAG ATP ATP EU BS 325 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLOORBEAM AT STATION 325AS HAS CORROSION ON RIGHT SIDE. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700759 19990827 00759 EU 1999 8 27 UF6A990505 1 19990504 A 5315 JD533J0182000 FLOORBEAM BAG ATP ATP EU BS 343 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLOORBEAM AT STATION 343AS HAS CORROSION ON RIGHT SIDE. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700760 19990827 00760 EU 1999 8 27 UF6A990503 1 19990504 A 5315 1D11904 FLOORBEAM BAG ATP ATP EU BS 308 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FLOORBEAM AT STATION 308AS HAS CORROSION ON RIGHT SIDE. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE WITHIN LIMITS AW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700761 19990827 00761 EU 1999 8 27 UF6A990502 1 19990505 A 3350 362624 LAMP BAG ATP ATP EU BS 234 FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 ORD - FLT 5721 - FLOOR EMERGENCY LIGHT ON LEFT SIDE OF GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYST EM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700762 19990827 00762 EU 1999 8 27 UF6A990516 1 19990509 A 5320 6D11186 INTERCOSTAL BAG ATP ATP EU BS 324/343 CORROSION A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - INTERCOSTAL BETWEEN STATION 342FS AND 343FS HAS CORROSION AROUND THE LAVATORY AREA. MAINTENANCE CLEANED CORROSION AND WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-30-01. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700763 19990827 00763 EU 1999 8 27 UF6A990515 1 19990508 A 5753 JD574J0001003 HINGE BAG ATP ATP EU RT TE FLAP CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT INBOARD LEADING EDGE HINGE IS CRACKED AT OUTBOARD HINGE AREA. MAINTENANCE REPLACED HINGE IAW BAE ATP MM 57- 40-00. (M) 2 L 7 2 4T RT A27NM 1999082700764 19990827 00764 EU 1999 8 27 UF6A990514 1 19990507 A 3350 1317 BULB BAG ATP ATP EU RT EMER EXIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - RIGHT AFT OVERWING EMERGENCY LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700765 19990827 00765 EU 1999 8 27 UF6A990513 1 19990504 A 5414 SKIN BAG ATP ATP EU BS 101.254 CHAFED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT MODULE THREE HAS SEVERAL HOLES CHAFED IN BOTTOM FIRE SKIN. MAINTENANCE REPAIRED DAMAGE BY FABRICATION OF DO UBLER IAW BAE ATP SRM 54-10-03 AND 51-60-01 FIGURE ONE. (M) 2 L 7 2 4T RT A27NM 1999082700766 19990827 00766 EU 1999 8 27 UF6A990512 1 19990501 A 5230 JD523J00010021 SKIN BAG ATP ATP EU CARGO DOOR DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - INNER HANDLE DOOR SURROUND ON FORWARD BAGGAGE DOOR IS DAMAGED. MAINTENANCE FOUND DAMAGE TO BE WITHIN ALLOWABLE LI MITS IAW BAE ATP SRM 51-10-01. AREA WAS CLEANED, ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700767 19990827 00767 EU 1999 8 27 UF6A990519 1 19990506 A 5753 JD275J0036001 STRINGER BAG ATP ATP EU RT TE FLAP CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT FLAP UPPER STRINGER NR 1 AND NR 2 WAS FOUND CRACKED AT STATION 76.16 DURING AND RADIOGRAPHIC EXAMINATION. M AINTENANCE REPAIRED THE NR 1 AND NR 2 STRINGERS IAW BAE ATP SRM 51-60-02 FIGURE 2. (M) 2 L 7 2 4T RT A27NM 1999082700768 19990827 00768 EU 1999 8 27 UF6A990517 1 19990508 A 5311 1D11312 FORMER BAG ATP ATP EU BS 325.5 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FORMER 325.5AS IS CRACKED AT GUSSET BETWEEN STRINGERS 37S AND 38S. MAINTENANCE REPLACED CRACKED FORMER SHEAR ANGL E AND GUSSET CLIP IAW BAE ATP SRM 53-10-00 FIGURE 204. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700769 19990827 00769 EU 1999 8 27 UF6A990518 1 19990505 A 5751 JD57J0002000W SKIN BAG ATP ATP EU RT AILERON TEAR A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT AILERON HAS A SMALL TEAR IN THE OUTER SKIN AT THE RADIUS OF THE CENTER HINGE. MAINTENANCE BURNISHED TEAR AN D WAS FOUND WITHIN IAW BAE ATP SRM 51-10-01. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700770 19990827 00770 EU 1999 8 27 UF6A990407 1 19990416 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 11673 2032 SBN - FLIGHT ATTENDANT SWITCH CAUSES INTERMITTENT LIGHTING OF ALL EMERGENCY LIGHTS. MAINTENANCE REMOVED AND REPLACED PO SITION 6 EMERGENCY POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700771 19990827 00771 EU 1999 8 27 UF6A990501 1 19990502 A 2520 0135571 PSU BAG ATP ATP EU ROW 7CD FAILED A UF6A O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 31 856AW 2032 SBN - FLT 5757 - SMOKE IN PASSENGER COMPARTMENT. MAINTENANCE REMOVED AND REPLACED PSU AND ROW 7CD. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999082700772 19990827 00772 EU 1999 8 27 UF6A990520 1 19990506 A 5320 JF536J0011000 JAMB BAG ATP ATP EU BS 57 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT EMERGENCY DOOR APERTURE AND SEAL STRIKER PLATE HAS SEVERAL SCORED AREAS. MAINTENANCE BURNISHED WORN SPOTS A ND DAMAGE WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700773 19990827 00773 EU 1999 8 27 UF6A990522 1 19990508 A 5320 JD539J0006000 JAMB BAG ATP ATP EU BS 289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - AFT PASSENGER DOOR HAS CORROSION ON THE BOTTOM OF THE DOOR SURROUND. MAINTENANCE REMOVED CORROSION AND DAMAGE WAS FOUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-30-01. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700774 19990827 00774 EU 1999 8 27 UF6A990523 1 19990508 A 5320 JD539J0007000 JAMB BAG ATP ATP EU BS 289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - AFT BAGGAGE DOOR HAS CORROSION ON THE BOTTOM OF THE DOOR SURROUND. MAINTENANCE REMOVED CORROSION AND DAMAGE WAS F OUND TO BE WITHIN LIMITS IAW BAE ATP SRM 51-30-01. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700775 19990827 00775 NE 1999 8 27 UF6A990524 2 19990508 A 7261 FILTER BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE DIRTY A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 31 851AW 2020 124015 PIA - FLT 5745 - NR 1 ENGINE OIL FILTER CWP ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACE THE NR 1 E NGINE MAIN OIL PRESSURE AND SCAVENGE FILTER. SYSTEM OPS AND LEAK CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999082700776 19990827 00776 NE 1999 8 27 UF6A990526 2 19990508 A 7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE NR 1 SMOKING A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 852AW 2021 124403 CWA - FLT 5734 - ON SHUTDOWN, THE NR 1 ENGINE WAS EMITTING BLUE SMOKE FORM SIDES OF COWLING DURING OPERATION OF THE FEAT HER LEVERS. THIS OCCURRED UNTIL ENGINE SHUTDOWN AT WHICH TIME FUEL WAS OBSERVED DRAINING FROM FUEL VENT ON RIGHT SIDE O F COWLING. MAINTENANCE RAN THE NR 1 ENGINE SEVERAL TIMES AT 85 PERCENT, DURING ALL SHUTDOWNS NO SMOKE WAS NOTICED COMIN G FROM COWLINGS NOR WAS ANY FUEL OBSERVED LEAKING OUT OF VENTS. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999082700777 19990827 00777 EU 1999 8 27 UF6A990528 1 19990501 A 5320 JD256J0068000 BRACKET BAG ATP ATP EU BS 289 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - TOP AFT ESCAPE SLIDE SUPPORT BRACKET IS CRACKED ON THE AFT BAGGAGE DOOR. MAINTENANCE REMOVED AND REPLACED BRACKET IAW BAE ATP SRM 52-32-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700778 19990827 00778 EU 1999 8 27 UF6A990529 1 19990504 A 5320 239D11186 INTERCOSTAL BAG ATP ATP EU BS 325.5/343 BENT A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - INTERCOSTAL BETWEEN STATION 325.5AS AND 343AS ON RIGHT SIDE IS BENT. MAINTENANCE REPAIRED INTERCOSTAL IAW BAE ATP SRM 51-10-01. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700779 19990827 00779 EU 1999 8 27 UF6A990530 1 19990501 A 5210 JD521J0064002 GUSSET BAG ATP ATP EU PAX DOOR CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - AFT PASSENGER DOOR TOP FORWARD GUSSET IS CRACKED IN TWO PLACES. MAINTENANCE FABRICATED NEW GUSSET AND INSTALLED I AW BAE ATP SRM 51-60-03. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700780 19990827 00780 EU 1999 8 27 UF6A990531 1 19990504 A 5320 36061786001 BRACKET BAG ATP ATP EU BS 289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT AFT SERVO BRACKET HAS CORROSION ON THE SURFACE. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE WITHIN LIM ITS IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999082700783 19990827 00783 NM 1999 8 27 MZZA99127 1 19990630 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 720/740 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH AREA CORROSION WAS FOUND ON STRINGER 27L BETWEE N BS 720F PLUS 6 AND BS 740. THE CORRODED PART OF STRINGER WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-03 FIG 1. ( M) 2 L 7 3 4F A3WE 1999082700784 19990827 00784 NM 1999 8 27 MZZA99142 1 19990605 A 5320 FRAME BOEING 727 727232 1384082 NM CARGO DOORWAY CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH LONG CRACK WAS FOUND ON C3 DOOR FORWARD FLANGE AT ST RINGER 27R ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FI G 1. (M) 2 L 7 3 4F A3WE 1999082700785 19990827 00785 NM 1999 8 27 MZZA99141 1 19990605 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1148 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 1148 FLOORBEA M UPPER CHORD AT LBL 10. THE CORROED PART OF UPPER WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAP 53-10-08 FIG 3. (M) 2 L 7 3 4F A3WE 1999082700786 19990827 00786 NM 1999 8 27 MZZA99140 1 19990611 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 395 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 4 INCH AREA IG CORROSION WAS FOUND ON PASSENGER FLO OR SEAT TRACK AT BS 395 AND RBL 40. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700787 19990827 00787 NM 1999 8 27 MZZA99139 1 19990601 A 5510 BEAM BOEING 727 727232 1384082 NM HORIZ STAB CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION AT AIR ASIA, A 3 INCH LONG CORROSION WAS FOUND ON LEFT STAB UPPER T/E BEAM AT ELEV STATI ON 119. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-06 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700788 19990827 00788 NM 1999 8 27 MZZA99138 1 19990602 A 5510 BEAM BOEING 727 727232 1384082 NM HORIZ STAB CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON RIGHT STABILIZER UPPER T/E BEAM AT ELEVATOR STATION 190. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. ( M) 2 L 7 3 4F A3WE 1999082700789 19990827 00789 NM 1999 8 27 MZZA99137 1 19990604 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720-733 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN STRINGER 27R AND BS 720D PLUS 13. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M) 2 L 7 3 4F A3WE 1999082700790 19990827 00790 NM 1999 8 27 MZZA99136 1 19990603 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720-724 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .75 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN BETWEEN STRING ER 28R AND BS 720A PLUS 4. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M) 2 L 7 3 4F A3WE 1999082700791 19990827 00791 NM 1999 8 27 MZZA99135 1 19990624 A 5330 SKIN BOEING 727 727232 1384082 NM BS 448/480 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 44 8 AND BS 480, STRINGER 26R. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M) 2 L 7 3 4F A3WE 1999082700792 19990827 00792 NM 1999 8 27 MZZA99134 1 19990610 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 328 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 6 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CAB IN FLOORBEAM UPPER CHORD AT BS 328 FROM LBL 01 TO RBL 05. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CH APTER 51-40-04 FIG 2. (M) 2 L 7 3 4F A3WE 1999082700793 19990827 00793 NM 1999 8 27 MZZA99133 1 19990610 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 360/380 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BE TWEEN BS 360/380 ALONG RBL 18. THE DAMGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700794 19990827 00794 NM 1999 8 27 MZZA99132 1 19990610 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 360/380 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTON ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 20 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CAB IN FLOOR SEAT TRACK BETWEEN BS 360 AND 380 ALONG RBL 22 AND RBL 24. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B 727 SRM CHAPTER 53-10-05 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700795 19990827 00795 NM 1999 8 27 MZZA99131 1 19990601 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON BS 1130 AND LBL 46 SEAT TRACK. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700796 19990827 00796 NM 1999 8 27 MZZA99130 1 19990601 A 5510 BEAM BOEING 727 727232 1384082 NM HORIZ STAB CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON LEFT STABILIZER UPPER T /E BEAM AT ELEVATOR STATION 155. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. ( M) 2 L 7 3 4F A3WE 1999082700797 19990827 00797 NM 1999 8 27 MZZA99129 1 19990604 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 950E SHEAR TI E ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FIG 14. (M ) 2 L 7 3 4F A3WE 1999082700798 19990827 00798 NM 1999 8 27 MZZA99128 1 19990605 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1148 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 DURNIG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON BS 1148 FRAME FORWARD FLANG E ON CARGO COMPARTMENT. THE CORRODED PART OF FRAME WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-04 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700799 19990827 00799 NM 1999 8 27 MZZA99126 1 19990616 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 720/740 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON STRINGER 26R BE TWEEN BS 448 AND BS 480. THE CORRODED PART OF STRINGER WAS TRIMMED AND REPAIRED PER B727 CHAPTER 53-10-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700800 19990827 00800 NM 1999 8 27 MZZA99125 1 19990618 A 5320 SPLICE BOEING 727 727232 1384082 NM BS 1010 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH IG CORROSION WAS FOUND ON STRINGER 30 SPLICE ON CARGO COMPARTMENT AT BS 1010. THE DAMAGED PART WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAPTER 53-10-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700801 19990827 00801 NM 1999 8 27 MZZA99123 1 19990620 A 5320 CHANNEL BOEING 727 727232 1384082 NM BS 1273 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1. 5 INCH LONG CRACK WAS FOUND ON U-CHANNEL ATTACHED TO RIGHT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 CHAPTER 51-40-03 AN D 51-30-02. (M) 2 L 7 3 4F A3WE 1999082700802 19990827 00802 NM 1999 8 27 MZZA99122 1 19990605 A 5531 SPAR CHORD BOEING 727 727232 1384082 NM VERT STAB CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON VERTICAL STABILIZER FRONT SPAR LEFT CHOR D AT FS 54. THE CORRODED AREA IS TRIMMED OUT AND REPAIRED PER ECRA 5530-01250. ISSUE A NEW DIP NR CM 556 TO READ AS FO LLOWS WITHIN 11 MONTHS OF INSTALLATION OF THIS REPAIR, CAL WILL DETERMINE IF ADDITIONAL ARE REQUIRED FOR THIS REPAIR FOR SSID ITEM E-4A. (M) 2 L 7 3 4F A3WE 1999082700803 19990827 00803 NM 1999 8 27 MZZA99121 1 19990601 A 5532 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RIGHT VERTICAL STABILIZER SKIN WAS FOUND CRACKED JUST AFT TO THE BS 1183 BULKHEAD AT APPROX WL 302. NO ADDITIONAL REWORK OF THE CRACK IS NECESSARY DUE TO WITHIN LIMIT. ISSUE A DIP NR CM558 TO INSPECT THE FIN SKIN CRACK LOCATED AFT OF BS 1183 AT RT WL 302 PER ECRA 5310-03881 AND REPEAT THE INSPECTIO N EVERY 3000 FLT CYCLES UNTIL PERMANENTLY REPAIRED. (M) 2 L 7 3 4F A3WE 1999082700804 19990827 00804 NM 1999 8 27 MZZA99116 1 19990531 A 5320 WEB BOEING 727 727232 1384082 NM BS 1275 CRACK A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX HORIZONT AL WEB AT BS 1275. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700805 19990827 00805 NM 1999 8 27 MZZA99115 1 19990531 A 5320 CHANNEL BOEING 727 727232 1384082 NM BS 1273 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.25 INCH LONG CRACK WAS FOUND ON U-CHANNEL WHICH IS ATTACHED LEFT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED ANGLES WERE REMOVED AND REPLACED PER B727 SRM CHAP 51-40- 03. (M) 2 L 7 3 4F A3WE 1999082700806 19990827 00806 NM 1999 8 27 MZZA99114 1 19990531 A 5320 WEB BOEING 727 727232 1384082 NM BS 1238 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO PLACES 1. 5 INCH AND .625 INCH LONG CRACKS WERE FOUND ON L- ANGLES WHICH ARE ATTACHED TO RGHT LOWER TORQUE BOX VERTICAL WEB AT BS 1263. THE DAMAGED ANGLES WERE REMOVED AND REPLACE D PER B727 SRM CHAPTER 51-40-02 AND 51-30-02 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700807 19990827 00807 NM 1999 8 27 MZZA99113 1 19990531 A 5320 WEB BOEING 727 727232 1384082 NM BS 1229 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1229. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700808 19990827 00808 NM 1999 8 27 MZZA99120 1 19990615 A 5310 FRAME BOEING 727 727232 1384082 NM BS 219 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 30 SQUARE INCH AREA IG CORROSION WAS FOUND ON FUSELAGE FRAME AT BS 219 AND RT WL 233. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1999082700809 19990827 00809 NM 1999 8 27 MZZA99119 1 19990608 A 5720 STIFFENER BOEING 727 727232 1384082 NM RT FRONT SPAR CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING FRONT SPAR STIFFENER AT SS 58. THE CORRODED WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M) 2 L 7 3 4F A3WE 1999082700810 19990827 00810 NM 1999 8 27 MZZA99118 1 19990618 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 686.5 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 12 AND WS 686.5 W EB ATTACHMENT. THE CRACKED STRINGER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M) 2 L 7 3 4F A3WE 1999082700811 19990827 00811 NM 1999 8 27 MZZA99117 1 19990618 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 629 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 11 AND WS 629 WEB ATTACHMENT. THE CRACKED STIFFENER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M) 2 L 7 3 4F A3WE 1999082700812 19990827 00812 NM 1999 8 27 MZZA99124 1 19990604 A 5330 SKIN BOEING 727 727232 1384082 NM BS 740 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN AT BS 7 20F PLUS 4 AND STRINGER 28L - STRINGER 26R. THE CORRODED AREA WAS CLEANED UP AND REPAIRED PER EC/RA 5330-02842. (M) 2 L 7 3 4F A3WE 1999082700813 19990827 00813 NM 1999 8 27 MZZA99112 1 19990616 A 5320 WEB BOEING 727 727232 1384082 NM BS 1213 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.625 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERT ICAL WEB AT BS 1213. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M) 2 L 7 3 4F A3WE 1999082700814 19990827 00814 SO 1999 8 27 ASOA99060 1 19990719 A 6120 7847702 PCU EMB 120 EMB120RT SO NR 2 ENGINE INOPERATIVE A ASOA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 11 261AS 120141 FLT 4927 - ON TAKEOFF ROLL, THE NR 2 ENGINE FAILED TO DEVELP MORE THAN 51 PERCENT TORQUE. NP WAS SLOW TO SPOOL UP. ABO RTED TAKEOFF AT INITIAL ROLL. RETURN TO GATE SAFELY AND SWAPPED AIRCRAFT. MAINTENANCE REMOVED AND REPLACED PCU AND CHA NGED P3 AIR LINE. GROUND RUN OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082700815 19990827 00815 SO 1999 8 27 ASOA99061 1 19990720 A 3697 W620000820 WIRE EMB 120 EMB120RT 3260202 SO SENSOR BROKEN A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 11 232AS 120036 DUCT LEAK LIGHT ILLUMINATED IN CRUISE. SHUTDOWN ENGINE IN FIGHT PER CHECKLIST. DECLARED AN EMERGENCY AND DIVERTED TO A GS. LANDED SAFELY IN AGS. MAINTENANCE FOUND A BROKEN WIRE AT SENSOR UNDER AIRCRAFT NEXT TO APU BLEED DUCT AND CROSSBLE ED DUCK. REPAIRED WIRE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082700816 19990827 00816 SO 1999 8 27 ASOA99062 1 19990720 A 3350 10130115 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 243AS 120072 MAINTENANCE NOTICED THAT THE EMERGENCY EXIT LIGHT WAS DAMAGED. TXK MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999082700817 19990827 00817 EU 1999 8 27 99ZZZM614 1 19990724 A 3230 664700500A4C LGCIU AIRBUS 320 A320231 3930325 EU ELECTRONIC BAY FAILED A P9RA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 447TM 1032 447 AIRCRAFT RETURNED TO MIA AFTER TAKEOFF DUE TO AN INDICATION OF BOTH LGCIU FAILURE MANUAL DROP OF GEAR. RESET GEAR FREE FALL SYSTEM IAW MM 32-00-201. REMOVED AND REPLACED LGCIU NR 2. (M) 2 L 7 2 4F RT A28NM 1999082700818 19990827 00818 EU 1999 8 27 PLGA990721 1 19990721 A 2910 AE7064586 FLEX LINE SAAB SF340 340B 7860101 EU NLG FAILED A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 05 358BE 340B279 BTV - FLT 6881 - AFTER TAKEOFF FROM BTV, THE MAIN HYDRAULIC PRESSURE DROPPED AND THE HYDRAULIC PUMP CONTINUED TO RUN. T HE CREW USED THE EMERGENCY GEAR EXTENSION SYSTEM TO LOWER THE GEAR AND THE AIRCRAFT RETURNED TO BTV AND LANDED SAFELY. M AINTENANCE FOUND THE HYDRAULIC UP LINE TO THE RETRACT ACTUATOR TO HAVE FAILED AT THE END OF THE LINE WHERE IT IS SWAGGED TO THE CONNECTOR. THE LINE WAS REPLACED, REQUIRED OPERATIONAL CHECKS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVIC E. THE LINE IS BEING SENT FOR EVALUATION TO DETERMINE THE REASON FOR FAILURE. (M) 2 L 7 2 4T RT A52EU 1999082700819 19990827 00819 NM 1999 8 27 TSAA9957305 1 19990721 A 5730 SKIN BOEING 737 737230C 1384472 NM WS 382 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 FOUND CORROSION ON LEFT WING AT WS 382. CLEANED AND TREATED. MATERIAL REMOVAL EXCEEDED SRM 57-30-1 LIMITS. ACCOMPLISH ED FINAL REPAIR PER ECO 1684R10. (M) 2 L 7 2 4F A16WE 1999082700820 19990827 00820 WP 1999 8 27 USAA990733 1 19990716 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 58.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 49273 48114 PIT - DURING THROUGH CHECK, FOUND 3 INCH CRACK AND .5 INCH CRACK AT STATION 58.750 LONGERON 19L. INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHT 3. (M) 2 L 7 2 4F A6WE 1999082700821 19990827 00821 WP 1999 8 27 USAA990740 1 19990722 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 927VJ 42589 48154 PIT - PHL MAINTENANCE FOUND 3.5 INCH CRACK AT BELT FRAME WEB STATION 1095 LEFT SIDE. INSTALLED TEMPORARY DOUBLER PER EA 52499. (M) 2 L 7 2 4F A6WE 1999082700822 19990827 00822 WP 1999 8 27 USAA990741 1 19990722 A 5720 SR09570003813 DOUBLER DOUG DC9 DC981 3022081 WP WS 196.236 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 806US 48365 48038 PIT - DURING Q5/C2 CHECK FOUND 2 INCH CRACK AT LEFT WING PRODUCTIONS SPLICE DOUBLER STATION XFS 196.236. REPLACED DOUBL ER (SPLICE) AND ADDED STRAPS PER SRM 57-06B (FIGURE 9). (M) 2 L 7 2 4F A6WE 1999082700823 19990827 00823 NM 1999 8 27 USAA079901 1 19990721 A 3350 37067001 BATTERY PACK BOEING 727 727254 138408L NM EMER EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 916TS 20437 RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1999082700824 19990827 00824 NM 1999 8 27 USAA990705 1 19990717 A 5320 65C336551 WEB BOEING 737 737401 1384701 NM BS 380-400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING A Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK IN UPPER CHORD RADIUS AT BS 380-400, BLO WL 208 SHEAR W EB. REPLACED UPPER CHORD PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 1999082700825 19990827 00825 NM 1999 8 27 USAA990710 1 19990717 A 5400 CHANNEL BOEING 737 737401 1384701 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK FORWARD OUTBOARD ACCESS CUTOUT PYLON CHANNEL. INSTALLED DOUBLER PER TR 54-30-07. (M) 2 L 7 2 4F RT A16WE 1999082700826 19990827 00826 NM 1999 8 27 USAA990648 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 727B BETWEEN STRINGER 8R AND 9R FRAM E. INSTALLED REPAIR ANGLE PER SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 1999082700827 19990827 00827 NM 1999 8 27 USAA990649 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 727D BETWEEN STRINGER 8R AND 9R FRAME. INSTA LLED DOUBLER PER EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700828 19990827 00828 NM 1999 8 27 USAA990650 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURIGN Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 867 BETWEEN STRINGER 8R AND 9R FRAME . INSTALLED REPAIRE ANGLE PER EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700829 19990827 00829 NM 1999 8 27 USAA990651 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 867 BETWEEN STRINGER 8L AND 9L FRAME . INSTALLED DOUBLER PER EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700830 19990827 00830 NM 1999 8 27 USAA990652 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 747 BETWEEN STRINGER 8R AND 9R FRAME . INSTALLED DOUBLER PER EA 64815 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999082700831 19990827 00831 NM 1999 8 27 USAA990653 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 747 BETWEEN STRINGER 8L AND 9L FRAME . INSTALLED REPAIR ANGLE PER EA 64815 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999082700832 19990827 00832 NM 1999 8 27 USAA990654 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME . INSTALLED DOUBLER PER EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700833 19990827 00833 NM 1999 8 27 USAA990655 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 827 BETWEEN STRINGER 8R AND 9R FRAME . INSTALLED FRAME REPAIR PER SRM 53-00-07 AND EA 64916 AND EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700834 19990827 00834 NM 1999 8 27 USAA990656 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 360 BETWEEN STRINGER 8R AND 9R FRAME . INSTALLED REPAIR CHANNEL PER SRM 53-00-07 AND EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700835 19990827 00835 NM 1999 8 27 USAA990641 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 727F BETWEEN STRINGER 8R AND 9R FRAM E. INSTALLED REPAIR ANGLE PER SRM 53-00-07 AND EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700836 19990827 00836 NM 1999 8 27 USAA990642 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION FOUND A .25 INCH CRACK AROUND RIVET AT BS 727F BETWEEN STRINGER 8L AND 9L FRAME . INSTALLED REPAIR ANGLE PER SRM 53-00-07 AND EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700837 19990827 00837 NM 1999 8 27 USAA990643 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 907 BETWEEN STRINGER 8L AND 9L FRAME . INSTALLED DOUBLER PER EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700838 19990827 00838 NM 1999 8 27 USAA990644 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 400 BETWEEN STRINGER 8L AND 9L FRAME . INSTALLED FILLER AND REPAIR ANGLE PER EA 64815 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999082700839 19990827 00839 NM 1999 8 27 USAA990645 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 440 BETWEEN STRINGER 8R AND 9R FRAME . INSTALLED REPAIR ANGLE PER EA 64815. (M) 2 L 7 2 4F RT A16WE 1999082700840 19990827 00840 NM 1999 8 27 USAA990646 1 19990717 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 30865 23885 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AROUND RIVET AT BS 500C BETWEEN STRINGER 8R AND 9R FRAM E. INSTALLED REPAIR ANGLE PER EA 64815 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999082700841 19990827 00841 WP 1999 8 27 GTIA9900101 1 19990522 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 484 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - PASSENGER CABIN STATION 484 LONGERON R6 INTERCOSTAL CRACKED. FABRICATED REPLACEMENT ITEM REF DC9 SRM 51-10 HEAT T REAT NOT REQUIRED ISSUED TO AIRCRAFT FOR FIT AND INSTALL ON W/O A092B03W106. (M) 2 L 7 2 4F A6WE 1999082700842 19990827 00842 WP 1999 8 27 GTIA9901011 1 19990524 A 5532 PANEL DOUG DC9 DC931 3022065 WP VERT STAB MISALIGNED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 934ML 47526 MHV - VERTICAL CENTER PANEL UPPER P/N 9911940-403 WHICH WAS REPLACED ON W/C NO062 HAS ATTACHING HOLES MISALIGNING WITH M ATING HOLES ON VERT STRUT. PER ENG DWG NR 9909001 INSTALLATION COMPLETE PARTS FAB ON W/C A092-B10-N067 BRACKETS, CHANNE LS, STRAPS ALL INSTALLED COMPLETE PER DC9 SRM 51-30-0 BANNONS FAIRING INSTALLED COMPLETE PER DC9 MM 55-10-0 AND PANEL 35 21 ADN 3622. (M) 2 L 7 2 4F A6WE 1999082700843 19990827 00843 WP 1999 8 27 GTIA9900100 1 19990522 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 484 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO F ACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 S RM 51-30-5 AND 51-10-4 PAGE 1 AND 4A FIG 3A. (M) 2 L 7 2 4F A6WE 1999082700844 19990827 00844 WP 1999 8 27 GTIA9901008 1 19990519 A 5542 SKIN DOUG DC9 DC931 3022065 WP RUDDER CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - THERE ARE 2 CRACKS ON THE RUDDER RIGHT SIDE AT RIB NR 6 AND RIB NR 8. REMOVED AND REPLACED RUDDER AND SKIN AND 1 STIFFENER IAW DC9 SRM 55-03 AND S/B 55-23R6 CNI AND AD87-08-03 W/B TO BE ACCOMPLISHED ON WO A092A03 N061. PAINT TO BE A CCOMPLISHED ON W/O A092P07F032. (M) 2 L 7 2 4F A6WE 1999082700845 19990827 00845 WP 1999 8 27 GTIA9901007 1 19990518 A 5512 SKIN DOUG DC9 DC931 3022065 WP HORIZ STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - HORIZONTAL STABILIZER CENTER SECTION UPPER RIGHT PANEL NR 3806A CRACKED AT AFT UPPER AREA ALSO WORN TO KNIFE EDGE. FABRICATED DOUBLER AND FILLER TO COVER DAMAGED PANEL, INSTALLED PER DC9 IAW SRM 55-03-0 PAGE 28 VIEW F ALODINE AND PRI MED PER DC9 IAW SRM 51-10-3 PAGE 16, 18 PARAGRAPH 23-30. (M) 2 L 7 2 4F A6WE 1999082700846 19990827 00846 WP 1999 8 27 GTIA9901006 1 19990524 A 5510 STRUCTURE DOUG DC9 DC931 3022065 WP HORIZ STAB DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - REMOVAL OF HORIZONTAL STABILIZER IS REQUIRED TO REPLACE WITH SERVICEABLE UNIT. REMOVED AND REPLACED HORIZONTAL ST AB ASSY PER DC9 MM 55-10-0 PAGE 202. HORIZ STABILIZER ADJUSTMENT AND TEST C/W PER DC9 MM 55-10-0 PAGE 501 HORIZ STAB AC CESS PANELS WILL BE INSTALLED ON CARD A092A01M013. (M) 2 L 7 2 4F A6WE 1999082700847 19990827 00847 WP 1999 8 27 GTIA9901005 1 19990518 A 5510 SEALANT DOUG DC9 DC931 3022065 WP HORIZ STAB DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - LEFT HORIZONTAL STABILIZER LIP EXTERIOR SURFACE THE SEALANT IS DAMAGE. NOT REQUIRED HORIZONTAL STAB REMOVED AND R EPLACED ON W/C A092A03M058. (M) 2 L 7 2 4F A6WE 1999082700848 19990827 00848 WP 1999 8 27 GTIA9901002 1 19990721 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12505 45788 MYR - FORWARD EMERGENCY FLOOR LIGHTING 4 RED LENS INOPERATIVE. FOUND 1 POWER WIRE BROKEN UNDER CARPET. REPAIRED SAME. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999082700849 19990827 00849 WP 1999 8 27 GTIA9901001 1 19990720 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 ACY - FLT 502 - ON DAILY, FOUND EMERGENCY LIGHTING SYSTEM INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY FOR EMERGENCY LIGHTING IN ACCORDANCE WITH DC9 MM 33-50-00, OPERATIONAL CHECK GOOD (BATTERY CHARGER). (M) 2 L 7 2 4F A6WE 1999082700850 19990827 00850 WP 1999 8 27 GTIA9900999 1 19990718 A 3350 BULB DOUG DC9 DC987 3022087 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 750RA 49777 A COUPLE OF LIGHTS OUT ON EMERGENCY FLOOR LIGHTING, ALSO NOTICED A FEW LENSES MISSING. INSTALLED NEW LENSE COVER AND BU LBS, OPERATIONAL CHECK GOOD IAW MM REF 33-00. (M) 2 L 7 2 4F RT A6WE 1999082700851 19990827 00851 WP 1999 8 27 GTIA9900995 1 19990712 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY EXIT INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 13512 48111 MLB - FORWARD OVERWING EXIT EMERGENCY LIGHTS WILL NOT GO OFF AFTER TEST. THEN WOULD NOT TEST AFTER CYCLING C/B. REPLAC ED FORWARD OVERWING EXIT EMERGENCY LIGHT, POWER SUPPLY. OPERATION CHECKS GOOD IAW DC-9 MM 33-51. (M) 2 L 7 2 4F A6WE 1999082700852 19990827 00852 WP 1999 8 27 GTIA9900990 1 19990704 A 3397 WIRE DOUG DC9 DC931 3022065 WP COCKPIT LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 MYR - FLT 538 - EMERGENCY LIGHTS WILL NOT ILLUMINATED. TIGHTENED LOOSE WIRES ON COCKPIT EMERGENCY LIGHT SWITCH IAW 33-5 2-DC-9 MM. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999082700853 19990827 00853 WP 1999 8 27 GTIA9900989 1 19990622 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 8 LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 17535 47111 FORWARD ONE-THIRD OF EMERGENCY FLOOR ESCAPE PATH LIGHTS INOPERATIVE. FOUND WIRES OUT ON FLOOR ROW EIGHT RESECURED AS NE CESSARY. OPERATION CHECK GOOD IAW DC-9 MM 33-50. (M) 2 L 7 2 4F A6WE 1999082700854 19990827 00854 WP 1999 8 27 GTIA9900988 1 19990707 A 2560 SLIDE DOUG DC9 DC931 3022065 WP R1 DOOR DETACHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 DTW - SLIDE PACK ON R-1 DOOR FELL FROM THE DOOR ONTO THE CARPET GALLEY FLOOR DURING CLEANING PROCEDURE. RE-INSTALLED SL IDE PACK ON R-1 DOOR IAW MM 25-61-00. (M) 2 L 7 2 4F A6WE 1999082700855 19990827 00855 WP 1999 8 27 GTIA9900987 1 19990706 A 3350 BULB DOUG DC9 DC982 3022082 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 966AS 49104 DTW - EMERGENCY FLOOR TRACK LIGHTING BULBS 19, 31 ARE INOPERATIVE. REPLACED BULBS AND SOCKETS, OPERATION CHECKED GOOD I AW MD-80 MM 33-50. (M) 2 L 7 2 4F A6WE 1999082700856 19990827 00856 WP 1999 8 27 GTIA9900985 1 19990708 A 3350 BATERY CHARGER DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - CABIN, A NUMBER OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER STAND, CHECK GOOD IAW MM 33-50 -00. (M) 2 L 7 2 4F A6WE 1999082700857 19990827 00857 WP 1999 8 27 GTIA9900984 1 19990708 A 3350 BULB DOUG DC9 DC931 3022065 WP VENTRAL STAIRS FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - AFT VENTRAL STAIRS SIDEWALL LIGHTS HAVE INOPERATIVE EMERGENCY LIGHT PORTION. RELAMPED CHECK GOOD AIW 33-50-00. ( M) 2 L 7 2 4F A6WE 1999082700858 19990827 00858 WP 1999 8 27 GTIA9900983 1 19990708 A 3350 LIGHT DOUG DC9 DC931 3022065 WP ACCESSORY COMPT INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 AFT ACCESSORIES COMPARTMENT CAT WALK MISSING EMERGENCY LIGHT LENSE AND BULB. REPLACED EMERGENCY LIGHT LENSE AND BULB IA W DC-9 MM 33-51-00. (M) 2 L 7 2 4F A6WE 1999082700859 19990827 00859 EU 1999 8 27 SIMA992041 1 19990723 A 3320 6500111 SOCKET SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 400BR 340B400 SAT - FLT 5065 - SMOKE IN THE CABIN SMELLED ELECTRICAL IN NATURE. OCCURRED AT FL 200 OVER SAT. MADE EMERGENCY LANDING INTO SAT. FOUND SEAT 5A OVERHEAD LIGHT SOCKET WAS BAD. DEFERRED LIGHT SOCKET. ON AUGUST 5, RESTORED MEL BY REPLACING THE OVERHEAD LAMP HOLDER AT SEAT 5A. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999082700860 19990827 00860 EU 1999 8 27 SIMA991973 1 19990716 A 2611 72111211000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 339SB A4475 340B339 LAX - FLT 3261 - CARGO SMOKE WARNING LIGHT ILLUMINATED THREE TIMES IN FLIGHT. DISCHARGED FIRE EXTINGUISHERS. VERIFIED EVENT AS FALSE WARNING. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999082700861 19990827 00861 EU 1999 8 27 99ZZZM615 1 19990716 A 2611 72111211000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 339SB A4233 340B339 LAX - FLT 3261 - CARGO SMOKE WARNING LIGHT ILLUMINATED THREE TIMES IN FLIGHT. DISCHARGED FIRE EXTINGUISHERS. VERIFIED EVENT AS FALSE WARNING. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999082700862 19990827 00862 NE 1999 8 27 SIMA992081 2 19990727 A 7261 4068T970P01 SEAL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A SIMA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 21 341SB 340B341 785601 BWI - FLT 4901 - RIGHT ENGINE LOST OIL PRESSURE DURING FLIGHT INTO BWI. CREW DECLARED EMERGENCY AND SHUT DOWN RT ENGINE AND LANDED SAFELY. OIL PRESSURE WAS 30-50 PSI PRIOR TO SHUT DOWN. ALSO NOTED OIL ON RIGHT COWLING AFTER LANDING. REM OVED AND REPLACED RIGHT ENGINE B-B AXIS SEAL. SERVICED ENGINE OIL. PERFORMED LEAK CHECK AND RETURNED AIRCRAFT TO SERVI CE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1999082700863 19990827 00863 EU 1999 8 27 SIMA991622 1 19990611 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AT 434 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT MIDDLE INBOARD, LEFT AFT OUTBOARD, AND THE RIGHT MIDDLE OUTBOARD SEAT TRAC KS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999082700864 19990827 00864 EU 1999 8 27 99ZZZM616 1 19990611 A 5347 S53678001225 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AT 434 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT MIDDLE INBOARD, LEFT AFT OUTBOARD, AND THE RIGHT MIDDLE OUTBOARD SEAT TRAC KS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999082700865 19990827 00865 EU 1999 8 27 99ZZZM617 1 19990611 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AT 434 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT MIDDLE INBOARD, LEFT AFT OUTBOARD, AND THE RIGHT MIDDLE OUTBOARD SEAT TRAC KS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999082700899 19990827 00899 SO 1999 8 27 99ZZZX3143 2 19990707 A 8520 629340 BOLT 646778 CESSNA 210 210L 2073448 CE CONT O520 IO520L 17032 SO ENGINE ROD BROKEN A FPIA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SO 15 29278 1246 21059852 ONE CONNECTING ROD BOLT BROKE ON NR 3 CYLINDER CONNECTING ROD. THE CONNECTING ROD EXITED THE ENGINE THROUGH THE TOP OF THE ENGINE CRANKCASE. THE ENGINE WAS SENT TO THE MANUFACTURER FOR METALURGY STUDY. 1 H 7 1 3O 3 O 3A21 E5CE 1999082700907 19990827 00907 1999 8 27 CA990603025 4 19990504 A 3460 FMGC AIRBUS 320 A320211 3930320 EU E/E BAY FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) ON TAKEOFF ROLL, AUTO THROTTLE FAILED. FURTHER INVESTIGATION REVEALED FINGER TROUBLE BY CREW. 2 L 7 2 4F RT A28NM 1999082700909 19990827 00909 1999 8 27 CA990707063 4 19990603 A 8300 873017 CYLINDER KIDDE 89034607 FRCHLD F27 F27F 3373008 EA RROYCE DART DART5297E 54507 EU GEARBOX FAILED W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 4197 259 57519 13751 (CAN) DURING FLIGHT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING. CREW SECURED ENGINE. INVESTIGATION REVEALED THAT THE CYLINDER CAP ON THE AIR COMPRESSOR ON NR 2 ACCESSORY GEARBOX WAS LEAKING. PUMP REPLACED. 2 H 7 2 4T 4 T 7A1 E297 1999082700910 19990827 00910 EA 1999 8 27 CA990728003 1 19990622 A 3230 82910010209 TUBE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG WW LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123113 (CAN) HYDRAULIC LEAK IN NOSE GEAR BAY AREA RESULTED IN REPLACEMENT OF GEAR DOWN LINE. CRACKED APPROX\IMATELY ONE INCH LONG ON THE OUTSIDE RADIUS OF A FACTORY BEND. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700911 19990827 00911 NE 1999 8 27 CA990728004 2 19990628 A 7320 ELECTRONIC CNTRL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE FAILED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 7748 4251 120229 120229 (CAN) ON TWO OCCASIONS, THE FLIGHT CREW EXPERIENCED A TORQUE ROLLBACK ON NR 1 ENGINE DURING CLIMB-OUT. THE EEC HAD REVE RTED BACK TO MANUAL. CYCLING THE SELECTOR BROUGHT IT BACK ON LINE. EEC REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700912 19990827 00912 1999 8 27 CA990728005 4 19990629 A 2360 DISCHARGE WICKS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE WING OUT OF TOLERANCE W O OTHER O OTHER CR CRUISE 1 CA 24430 120152 (CAN) PILOTS REPORTED BOTH RADIOS WERE UNREADABLE DUE TO STATIC WHILE FLYING IN CLOUD. SEVERAL TRAILING EDGE STATIC DIS CHARGERS WERE TESTED OUT OF TOLERANCE AND REPLACED. REPLACED ALL CONDUCTIVE SEALS ON THE COMPOSITE NOSE COMP. ACCESS DO ORS. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700915 19990827 00915 1999 8 27 CA990728056 4 19990624 A 3442 RTA842 WEATHER RADAR COLLINS RTA842 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RADOME MALFUNCTIONED W O OTHER O OTHER CR CRUISE 1 CA 769 (CAN) AIRCRAFT ENTERED A CLOUD DURING CRUISE FLIGHT AT APPROXIMATELY 16,000 FEET. THE RADAR WAS TURNED ON AND BEING MON ITORED. THE CLOUD WAS NOT SHOWN ON THE INDICATORS FOR EITHER CREW MEMBER. THE CLOUD CONTAINED HAILTHE SIZE OF LARGE PE AS TO THE SIZE OF MARBLES CAUSING MINOR COSMETIC DAMAGE TO THE LEADING EDGES OF THE AIRCRAFT. THE CREW MAINTAINED THE R ADAR WAS NOT PAINTING CELLS IF THERE WAS ANOTHER MOISTURE CONTAINING CLOUD IN THE WAY. SUBMITTER STATED UNSURE IF IT IS MECHANICAL OR OPERATIONAL AT THIS TIME. 2 L 7 2 4T 4 T RT A24CE E26NE 1999082700916 19990827 00916 1999 8 27 CA990728057 4 19990625 A 3442 RTA842 WEATHER RADAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RADAR MALFUNCTIONED W O OTHER O OTHER CR CRUISE 1 CA 672 (CAN) AIRCRAFT ENTERED A CLOUD, DURING CRUISE FLIGHT, THAT WAS NOT SHOWING ON THE RADAR INDICATORS. THIS CLOUD CONTAINE D HAIL WHICH STRUCK THE AIRCRAFT LEADING EDGES CAUSING COSMETIC DAMAGE. THE CREW REPORTED THAT THIS CLOUD WAS NOT SHOWI NG ON THE SCREENS AS THERE SEEMED TO BE NO PENETRATION OF THE RADAR BEAM THROUGH OTHER CLOUDS BETWEEN THE CLOUD CONTAINI NG HAIL AND THE AIRCRAFT. SUBMITTER STATED CONTINUING THE INVESTIGATION TO DECIDE IF THE RADAR IS AT FAULT OR IF OPERAT ING PROCEDURES IS AT FAULT. 2 L 7 2 4T 4 T RT A24CE E26NE 1999082700917 19990827 00917 EU 1999 8 27 CA990804005 1 19990730 A 2751 676801007 COMPUTER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE TE FLAP MALFUNCTIONED W C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 CA 18331 15894 LF05542A (CAN) FLAP FAULT INDICATION ON TAKEOFF. PROBLEM FOUND WITHIN FLAP COMPUTER. 2 H 7 4 4F 4 F RT A49EU E6NE 1999082700918 19990827 00918 EA 1999 8 27 CA990812001 2 19990722 A 8500 ENGINE ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA ENGINE BAY FAILED W A UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION HO HOVERING 1 CA 950 L2499540A (CAN) POWER LOSS EXPERIENCED WITH PART CARBURETOR HEAT APPLIED. A DECAY OF ROTOR RPM WAS EXPERIENCED RESULTING IN THE E MERGENCY LANDING. LYCOMING REP FOUND NO DISCREPANCIES AT INVESTIGATION. SUBMITTER STATED CARBURETOR ICING IS BELIEVED TO BE THE FAULT. 1 G 7 1 3O 3 O H11NM E295 1999082700919 19990827 00919 EU 1999 8 27 CA990812034 1 19990717 A 3230 CONTROL UNIT AIRBUS 320 A320211 3930320 EU MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) GEAR WOULD NOT EXTEND, EMERGENCY EXTENSION USED. LGCIU NR 1 SWAPPED, BRAKE/STEER UNIT, GEAR SELECTOR LEVER, GEAR SELECTOR VALVE, MANIFOLD VALVE, GEAR CONTROL UNIT, AND INTERFACE UNIT REPLACED. OPERATIONAL CHECKS COMPLETED. 2 L 7 2 4F RT A28NM 1999082700920 19990827 00920 SW 1999 8 27 CA990812045 1 19990723 A 7810 41200161 STACK ENSTRM 480 480TH28 SW ALLSN 250C 250C20 03013 GL EXHAUST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2421 CAE845007 CAE845007 (CAN) MIS-ALIGNMENT OF EXHAUST STACKS FROM PREVIOUS INSTALLATION CAUSED PREMATURE CRACKING. 1 G 7 1 3O 3 U 0 H1CE E4CE 1999082700921 19990827 00921 NM 1999 8 27 CA990817001 1 19990713 A 3244 265X8013 TIRE BFGOODRICH 314354 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG DELAMINATING W K NONE O OTHER IN INSP/MAINT 1 CA 73 2975 120854 (CAN) DURING INSPECTION, NR 4 MAIN WHEEL TIRE WAS FOUND DELAMINATING THROUGH APPROXIMATELY 75 PERCENT OF THE INBOARD CIR CUMFERENCE OF THE TIRE TREAD AREA. TIRE WAS A THOMPSON RECAP. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700922 19990827 00922 NM 1999 8 27 CA990817002 1 19990720 A 3242 681295 O-RING BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 BRAKE DETERIORATED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 5023 824 1750 120854 (CAN) DURING INSPECTION, NR 2 BRAKE WAS FOUND LEAKING FROM ONE PISTON. THE BACKUP O-RING WAS FOLDED OVER BETWEEN THE PI STON ASSY AND SLEEVE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700923 19990827 00923 NM 1999 8 27 CA990817003 1 19990728 A 2430 28VS200Y4DH TRU 1243001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE E/E BAY FAILED W H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 CA 18051 17866 812 120854 (CAN) DURING FLIGHT, NR 2 TRU ILLUMINATED AND WOULD NOT ACCEPT A LOAD ON THE GROUND. TRU REPLACED 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700924 19990827 00924 NM 1999 8 27 CA990817004 1 19990825 A 3233 11300105 ACTUATOR 1321012 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT MLG BROKEN W O OTHER J WARNING INDICATION CL CLIMB 1 CA 10539 DCL49494 121165 (CAN) ON INITIAL GEAR RETRACTION AFTER TAKEOFF, GEAR DOOR LIGHTS REMAINED ILLUMINATED AND THE RIGHT GEAR DOOR STAYED OPE N. THE GEAR WAS CYCLED AND FUNCTIONED NORMALLY. INSPECTION REVEALED THE RT MLG UPLOCK LATCH SPRING HAD BROKEN. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700925 19990827 00925 NM 1999 8 27 CA990817005 1 19990807 A 2910 82970010121 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 121165 (CAN) DURING CRUISE FLIGHT, NR 1 HYDRAULIC PRESSURE AND FLUID WERE LOST. LINE BETWEEN THE PRESSURE MANIFOLD AND ANTI-SK ID CONTROL VALVE WAS LEAKING. LINE WAS PRE-MOD ALUMINUM. PUMP AND FILTERS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700926 19990827 00926 NM 1999 8 27 CA990817006 1 19990716 A 2497 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT LOOSE W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 16996 120229 (CAN) AIRCRAFT RETURNED TO GATE AFTER TAKEOFF WITH RT AC BUS, TRU, ELEVATOR HORN, AND STALL WARNING HEAT CAUTION LIGHTS ON. WIRE TB2421A FOUND NOT SECURED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700927 19990827 00927 EA 1999 8 27 CA990817007 1 19990721 A 3010 85720011007 DEICE BOOT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE WING DISBONDING W K NONE O OTHER IN INSP/MAINT 1 CA 8134 123113 (CAN) DURING INSPECTION, LEFT INBOARD LEADING EDGE DEICE BOOT WAS FOUND TO BE DISBONDING FROM L/E. L/E REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700928 19990827 00928 EA 1999 8 27 CA990817008 1 19990803 A 3412 82110032011 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE WING LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 19253 123113 (CAN) WHILE INVESTIGATING A HIGH SAT INDICATION AFTER HAVING CHANGED THE PROBE, AN AIR LEAK WAS DISCOVERED IN THE BLEED AIR DUCTING SYSTEM IN THE WINGBOX AREA. A SHROUDED PIPE ASSY WAS LEAKING FROM THE EXPANSION BELLOWS AT THE FORWARD END OF THE DORSAL FIN AND BEHIND THE REAR WING SPAR. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700929 19990827 00929 EU 1999 8 27 CA990817010 1 19990806 A 3340 HC535B075000 LENS BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE EXTERIOR LIGHT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 27794 LF05683A (CAN) RUNWAY EXIT AND WING INSPECTION LIGHT FOUND CRACKED. SUBMITTER STATED THIS LENS IS AN INTEGRAL PART OF THE WING T O FUSELAGE AERODYNAMIC FAIRING, THE FAILURE OF WHICH COULD COMPROMISE THE ENTIRE SET OF FAIRINGS. 2 H 7 4 4F 4 F RT A49EU E6NE 1999082700931 19990827 00931 NM 1999 8 27 CA990817013 1 19990813 A 2997 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CAUTION LIGHT BROKEN W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA 121158 (CAN) DURING CRUISE, NR 2 HYDRAULIC LOW PRESSURE CAUTION LIGHT ILLUMINATED ALONG WITH PRESSURE FLUCTUATION. PRESSURE I NDICATION WAS CAUSED BY BROKEN WIRE AT THE TRANSDUCER. CAUTION LIGHT MALFUNCTIONED BECAUSE OF FAULTY SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700932 19990827 00932 1999 8 27 CA990817014 4 19990813 A 3418 C809072 TRANSDUCER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE STALL WARNING FAILED W O OTHER N FALSE WARNING DE DESCENT 1 CA 22430 494 121158 (CAN) DURING DESCENT, THE RT STALL WARNING LIGHT ILLUMINATED INTERMITTENTLY. TRANSDUCER REPLACED AND WIRE REPAIRED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700933 19990827 00933 NE 1999 8 27 CA990817019 2 19990807 A 7261 B-NUT AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 ENGINE LOOSE W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 731474 (CAN) NR 1 ENGINE OIL QUANTITY DROPPED TO 3.5 DURING FLIGHT. AIRCRAFT LANDED. INVESTIGATION REVEALED A LOOSE B-NUT ON A LINE ON THE ENGINE. THE NR 1 ENGINE FUEL PUMP HAD BEEN REPLACED PRIOR TO THE FLIGHT AND THE LINE MAY HAVE BEEN DISTUR BED THEN AND NOT CORRECTLY TIGHTENED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999082700934 19990827 00934 EU 1999 8 27 CA990817023 2 19990811 A 7240 BLADE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU LP TURBINE FAILED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA 9007 9007 (CAN) LP TURBINE BLADE FAILURE (1). TEAR-DOWN REPORT TO FOLLOW AS SPECIFIED. 2 L 7 2 4F 4 F RT A20EU E2EU 1999082700939 19990827 00939 NM 1999 8 27 CA990817031 1 19990802 A 2910 82950010277 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 29971 120338 (CAN) CREW NOTICED HYDRAULIC FLUID COMING FROM THE LEFT LOWER WING OUTBOARD SPOILER. SPOILER RETURN LINE HAD A PIN HOLE IN IT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700940 19990827 00940 NM 1999 8 27 CA990817032 1 19990728 A 2421 31708001A GENERATOR LUCAS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AC SYSTEM FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 18013 6383 693 120549 (CAN) NR 2 AC GENERATOR CAUTION LIGHT CAME ON DURING FLIGHT. GENERATOR HAD INTERNAL FAILURE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700941 19990827 00941 NM 1999 8 27 CA990817033 1 19990729 A 3320 BR63031023 LIGHT DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CABIN FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 5389 123010 (CAN) FLIGHT CREW NOTICED A BURNING SMELL IN COCKPIT. INVESTIGATION REVEALED CABIN OVERHEAD LAMP ROW 1 CENTER HAD BURNT LAMPHOLDER SOCKET. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700942 19990827 00942 NM 1999 8 27 CA990817034 1 19990805 A 3230 54C546349 SOLENOID VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG FAILED W H DEACTIVATE SYST/CIRCUITS O OTHER AP APPROACH 1 CA 24649 0273 121075 (CAN) NOSE GEAR FAILED TO EXTEND WHEN GEAR SELECTED DOWN WITH RED LIGHT ILLUMINATED. NOSE LANDING GEAR SOLENOID SEQUENC E VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700943 19990827 00943 NM 1999 8 27 CA990817035 1 19990805 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 26429 5231 249 120816 (CAN) LOWER END CAP WAS FOUND LEAKING WHEN ACCOMPLISHING SB A8-32-145. VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700944 19990827 00944 NM 1999 8 27 CA990817036 1 19990805 A 2121 FYOM337003 MOTOR BYLF51514 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE AIR DISTRIBUTION FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 625 119 123152 (CAN) ARCING OF BRUSHES AND ARMATURE BURNT THROUGH CASING COVER. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700945 19990827 00945 NM 1999 8 27 CA990817037 1 19990809 A 3320 82540061113 RECEPTACLE BOX DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CABIN BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 22200 0804349 123152 (CAN) LAVATORY O/H LIGHTING BOX FOUND BURNED ABOVE INCANDESCENT BULBS AND RECEPTACLES (2). ALSO, BURNED WHERE RECEPTAC LES ARE ATTACHED TO BOX. 2 H 7 2 4T 4 T RT A13NM E20NE 1999082700946 19990827 00946 EA 1999 8 27 CA990817038 1 19990811 A 5753 F35 SEALANT DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL TE FLAP DETERIORATED W K NONE O OTHER IN INSP/MAINT 1 CA 22827 (CAN) CF 86-14 AND CF-87-04 ADDRESS PROBLEMS OF FUEL LEAKING FROM FUEL TANK RIBS AND DRAINS INTO THE NR 4 LEFT AND RIGHT FLAP TRACK CANOE. DURING A CORROSION INSPECTION OF THIS AREA, THE SEALANT APPLIED WAS CHIPPING AND FLAKING OFF ALLOWIN G FUEL TO LEAK BACK INTO THE CANOE. SUBMITTER STATED THIS IS THE SECOND TIME THIS PROBLEM HAS BEEN FOUND. AREA WILL BE RE-TREATED PER THE AD. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 1999082700947 19990827 00947 EA 1999 8 27 CA990817039 1 19990811 A 5753 F35 SEALANT DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL TE FLAP DETERIORATED W K NONE O OTHER IN INSP/MAINT 1 CA 25642 (CAN) CF 86-14 AND CF-87-04 ADDRESS PROBLEMS OF FUEL LEAKING FROM FUEL TANK RIBS AND DRAINS INTO THE NR 4 LEFT AND RIGHT FLAP TRACK CANOE. DURING A CORROSION INSPECTION OF THIS AREA, THE SEALANT APPLIED WAS CHIPPING AND FLAKING OFF ALLOWI NG FUEL TO LEAK BACK INTO THE CANOE. SUBMITTER STATED THIS IS THE SECOND TIME THIS PROBLEM HAS BEEN FOUND. AREA WILL BE RE-TREATED PER THE AD. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 1999082700954 19990827 00954 WP 1999 8 27 TWAA9911601 1 19990823 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 33 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9616G 53563 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT SEAT ROW 33. FOUND AND REPAIRED A BROKEN FEEDER WIRE AT THE EGRESS STRIP, R OW 33. CHECK-C 8-15-99 STL. 2 L 7 2 4F RT A6WE 1999082700955 19990827 00955 WP 1999 8 27 TWAA9911602 1 19990825 A 3350 PR2 LAMP DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9628W 53598 THE PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LAMP. 2 L 7 2 4F RT A6WE 1999082700956 19990827 00956 NM 1999 8 27 TWAA9911603 1 19990825 A 3350 767 LAMP BOEING 757 757231 1384950 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 716TW 28484 THE LEFT OUTSIDE DOOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP. 2 L 7 2 4F RT A2NM 1999082700957 19990827 00957 NM 1999 8 27 9903322714 1 19990813 A 2910 VALVE BOEING 727 7272S7 138407Z NM A HYD SYS FAILED A NWAA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 01 718RC 22344 DURING GEAR EXTENSION, AIRCRAFT LOST A SYSTEM HYDRAULICS (QUANTITY AND PRESSURE). CREW ABORTED LANDING AND PERFORMED CO M PROCEDURE. AFTER GO-AROUND, FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED STEERING VALVE. LEAK AND OPERATION AL CHECK OK. 2 L 7 3 4F A3WE 1999082700958 19990827 00958 NM 1999 8 27 QXEA9901627 1 19990731 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM RT TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - TOP SURFACE OF RIGHT-HAND INBOARD FLAP HAS DAMAGE FROM THE WING TRAILING EDGE. REPAIRED IAW HORIZON AREA. 2 H 7 2 4T RT A13NM 1999082700959 19990827 00959 NM 1999 8 27 QXEA9901628 1 19990731 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM RT TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - THERE IS A SMALL ABRASION ON THE TOP SKIN OF THE RIGHT-HAND OUTBOARD FLAP 2 FROM THE INBOARD EDGE. REPAIRED IAW D HC8 SRM 51-20-11. 2 H 7 2 4T RT A13NM 1999082700960 19990827 00960 NM 1999 8 27 QXEA9901629 1 19990729 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND WING, FLAP TRACK NR 4 HAS NUMEROUS AREAS OF PITTING DAMAGE. REPAIRED IAW DHC-8 SRM 57-50-44, PAGE 601. 2 H 7 2 4T RT A13NM 1999082700961 19990827 00961 NM 1999 8 27 QXEA9901630 1 19990728 A 5532 PANEL DHAV DHC8 DHC8202 2809007 NM VERT STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RECESSED AREA FOR ACCESS PANEL 322FR IS GOUGED ON LOWER FORWARD CORNER. REPAIRED IAW DHC8 SRM 55-30-16. 2 H 7 2 4T RT A13NM 1999082700962 19990827 00962 NM 1999 8 27 QXEA9901631 1 19990805 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 445.5 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - DENT ON RIGHT-HAND SIDE OF FUSELAGE SKIN STA 445.500 BETWEEN STRINGER 18 AND 19. REPAIRED IAW HORIZON AIR EA 2-53 -64. 2 H 7 2 4T RT A13NM 1999082700963 19990827 00963 NM 1999 8 27 QXEA9901632 1 19990805 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 396 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS SMALL DENT IN TOP FLANGE AT APPROXIMATELY STATION X396.150. REPAIRED IAW HORIZO N AIR EA 2-53-65. 2 H 7 2 4T RT A13NM 1999082700964 19990827 00964 NM 1999 8 27 QXEA9901633 1 19990804 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT INBOARD SEAT TRACK HAS MINOR CHAFE/GOUGE AT APPROXIMATELY STATION X545.00 ON BOTTOM OF CHANNEL. REPAIRED IAW HORIZON AIR EA 2-53-59. 2 H 7 2 4T RT A13NM 1999082700965 19990827 00965 NM 1999 8 27 QXEA9901634 1 19990804 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND INBOARD SEAT TRACK HAS SMALL NICK AT FLANGE OPENING AT APPROXIMATELY 7.6 FORWARD STATION X545.00. REPAI RED IAW HORIZON AIR EA 2-53-58. 2 H 7 2 4T RT A13NM 1999082700966 19990827 00966 NM 1999 8 27 QXEA9901635 1 19990804 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 454 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RIGHT-HAND INBOARD SEAT TRACK GOUGED ON BOTTOM CHANNEL APPROXIMATELY 10 FORWARD OF STATION X545.00. REPAIRED IAW HORIZON AIR EA 2-53-61. 2 H 7 2 4T RT A13NM 1999082700967 19990827 00967 NM 1999 8 27 QXEA9901636 1 19990804 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - RIGHT-HAND SEAT TRACK HAS SMALL GOUGE ON TOP FLANGE APPROXIMATELY 7.6 FORWARD OF STATION X545.00. REPAIRED IAW HO RIZON AIR EA 2-53-62. 2 H 7 2 4T RT A13NM 1999082700968 19990827 00968 NM 1999 8 27 QXEA9901637 1 19990807 A 5230 FITTING DHAV DHC8 DHC8202 2809007 NM CARGO DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - CARGO DOOR STOP FITTINGS NR 7 AND 8 ON FUSELAGE ARE WORN. REPAIRED IAW DHC8 MM 52-30-00. 2 H 7 2 4T RT A13NM 1999082700969 19990827 00969 NM 1999 8 27 QXEA9901638 1 19990807 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 445.5 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - DENT ON RIGHT-HAND SIDE FUSELAGE SKIN AT STATION X445.500 BETWEEN STRINGER 18 AND 19. REPAIRED IAW HORIZON AIR EA 2-53-57. 2 H 7 2 4T RT A13NM 1999082700970 19990827 00970 NM 1999 8 27 QXEA9901639 1 19990803 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 597.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - FOUND CORROSION ON RIGHT-HAND INBOARD AFT SEAT TRACK AT STATION X597.500. REPAIRED IAW RD 8-53-1339 AND HORIZON A IR EA 2-53-60. 2 H 7 2 4T RT A13NM 1999082700971 19990827 00971 NM 1999 8 27 QXEA9901640 1 19990803 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION ON OUTBOARD FLANGE UNDER WARDROBE. REPAIRED IAW DHC8 SRM 51-40-11 AND 51-40-00. 2 H 7 2 4T RT A13NM 1999082700972 19990827 00972 NM 1999 8 27 QXEA9901641 1 19990802 A 5320 NUT PLATE DHAV DHC8 DHC8202 2809007 NM SEAT TRACK CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - NUT PLATES FOR PANELS 133AZ AND 133BZ ON RIGHT INBOARD SEAT TRACK ARE CORRODED AND SEAT TRACK UNIT NUT PLATES APPE AR TO BE CORRODED. REPAIRED IAW DHC8SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999082700973 19990827 00973 NM 1999 8 27 QXEA9901642 1 19990728 A 5320 CLIP DHAV DHC8 DHC8202 2809007 NM BS 467 MISINSTALLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - SKIN ATTACH CLIP ON FRAME 467 BETWEEN STRINGERS 25S AND 26S IS NOT RIVETED TO SKIN. REPAIRED IAW DHC8 SRM 51-40-0 0. 2 H 7 2 4T RT A13NM 1999082700974 19990827 00974 NM 1999 8 27 99FDEA00348 1 19990824 A 2612 SMOKE DETECTR BOEING 727 72722 1384002 NM CARGO COMPT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 150FE 19141 FIRE BELL SOUNDED. VISUAL INSP FROM FIRE CHIEF, NO IND OF FIRE OR SMOKE. REMOVED AND REPLACED NR 2 SMOKE DETECTOR PER MM 26-17-1. INSPECTED CARGO COMPT, NO EVIDENCE OF SMOKE OR FIRE. 2 L 7 3 4F A3WE 1999082700975 19990827 00975 NM 1999 8 27 99FDEA00349 1 19990824 A 3232 ACTUATOR BOEING 727 727233 138408A NM LT MLG DOOR INOP A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 262FE 21624 SYS A HYD LOSS. DURING GEAR RETRACTION SYS A HYD QTY AND PRESS WENT TO ZERO. REPLACED BOTH CASE DRAIN FILTERS, LEAK CK GOOD ON GROUND RUN, SERVICE HYD TO FULL. REMOVED AND REPLACED LT MAIN GEAR DOOR ACTUATOR, REF EO 7-3230-7-4323 IAW MM 32-32-0181-4. LEAK CK AND OPS CK GOOD. 2 L 7 3 4F RT A3WE 1999082700976 19990827 00976 NM 1999 8 27 99UAL900425 1 19990812 A 2530 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 605UA 21866 FIRST CLASS GALLEY HAS ELECTRICAL SMELL. SMALL AMOUNT OF SMOKE DETECTED. *S/D* FIRST CLASS OVEN WAS REPLACED IN BOS O N 8/13/99. OP CHECKED GOOD. SHOP FINDINGS ON REMOVED OVEN MR25350-104: OVEN HAD BURNED OIL INSIDE (GREASE). CLEANED, TESTED AND RETURNED OVEN TO SERVICE 8/20/99. 2 L 7 2 4F 4 F RT A1NM E3NE 1999082700977 19990827 00977 NM 1999 8 27 99UAL900426 1 19990814 A 2530 OVEN SELL 8055010001 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GALLEY DIRTY A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 906UA 91010296 25006 CABIN ODOR EXPERIENCED AT FL 280 IN DESCENT. OVENS AND LIGHTS TURNED OFF. ODOR SUBSIDED BUT STILL LINGERED. *S/D* OV EN UPPER BAFFLE WAS CONTAMINATED WITH MELTED PLASTIC. OVEN WAS REMOVED AND SHIPPED TO THE COMPONENT SHOP. UNIT WAS CLE ANED, TESTED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999082700978 19990827 00978 NM 1999 8 27 99UAL900427 1 19990816 A 3350 BATTERY AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 826UA 989 EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. *S/D* AFT CHARGER AND BATTERY WERE REPLACED. (P/N 11-0049) CHARGER, BATTER Y (P/N 3214-30). AIRCRAFT HAS BEEN GOOD SINCE REPLACEMENTS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999082700979 19990827 00979 NM 1999 8 27 99UAL900428 1 19990816 A 2820 6525793 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 VENT SYS CRACKED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7260U 21407 DURING CLIMB, FEEDING FUEL FROM NR 2 TANK, TANK NR 1 DROPPED 1,000 LBS. CONDITION CORRECTED WITH CROSSFEED. *S/D* FOU ND CRACKED ELBOW OF THE NR 1 FUEL VENT SYSTEM. REPLACED ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1999082700980 19990827 00980 NM 1999 8 27 99UAL900429 1 19990816 A 5531 SPAR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7457U 21911 THE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWAB LE THICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPA IR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999082700981 19990827 00981 NM 1999 8 27 99UAL900430 1 19990817 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 950-1010 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7445U 21899 CORROSION DAMAGE WAS FOUND ON STRINGER 29 LEFT BETWEEN STATION 950-1010. CORROSION WAS BEYOND ALLOWABLE LIMITS. THE AD JACENT STRINGER 29 RIGHT HAD BEEN REPLACED AT A PREVIOUS VISIT AND THE REPAIR TO THE SKIN FOR THAT REPLACEMENT ALSO INCO RPORATED DAMAGE TO THE BEAR STRAP AROUND THE AFT CARGO DOORWAY. *S/D* THE EXISTING SKIN REPAIR FOR STRINGER 29 RIGHT W AS REMOVED AND ONE LARGE REPAIR WAS USED TO REPAIR THE SKIN CUTOUTS FOR STRINGER 29 RIGHT AND LEFT AND THE DAMAGED BEAR STRAP. THE REPAIR WAS PER TIMCO'S REPAIR INSTRUCTIONS AND WAS APPROVED BY AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999082700982 19990827 00982 NM 1999 8 27 99UAL900431 1 19990818 A 3350 POWER SUPPLY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 905UA 25005 EMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTING IN THE BACK HALF OF THE AIRPLANE ILLUMINATED INTERMITTENTLY. REPLACED AF T LEFT POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999082700983 19990827 00983 NM 1999 8 27 99UAL900432 1 19990819 A 2150 BACC10KH550R CLAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT PACK BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 788UA 9915 26942 SHORTLY AFTER DEPARTING ORD EN ROUTE LHR, CREW RECEIVED STATUS MESSAGE ON BLEED LOOP NR 1. SUBSEQUENTLY MESSAGE RECEIVE D FOR NR 2 BLEED LOOP. AIRCRAFT DIVERTED TO IAD. *S/D* DUCT CLAMP ON RIGHTHAND AC PACK LOWER FLOW CONTROL VALVE (FCV) BROKE, TRIGGERING A BLEED LEAK DETECTION BY THE DUCT LEAK OVERHEAT DETECTION (DLOD) SYSTEM AND ISOLATION OF THE RT BLEE D SYSTEM. REPLACED BROKEN CLAMP ON FLOW CONTROL VALVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999082700984 19990827 00984 GL 1999 8 27 99UAL900433 2 19990816 A 7260 GEAR BOX DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 ENGINE FAILED A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 1836U 47968 451557 OGG-LAX, NR 1 ENGINE FLAMED OUT FOR NO APPARENT REASON. NO VIBRATION, NO ABNORMAL INDICATIONS PRIOR, 32000 FEET, MACH .850, 370000# +/-. AFTER FLAMEOUT, N1: 27.7, N2: 00.1 OIL PRESSURE. DIVERTED TO HNL. *S/D* AT ENGINE SHOP INDUCTIO N THE GEARBOX WAS PARTIALLY DISASSEMBLED FINDING METAL IN THE AGB ALONG WITH A FAILED IGB BEVEL GEAR. THE ENGINE WAS RE MOVED FROM WING. 2 L 7 3 4F 4 F A22WE E23EA 1999082700985 19990827 00985 NM 1999 8 27 99UAL900434 1 19990819 A 2780 65162241 HOOK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 LE SLAT FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7291U 21569 NR 3 LEADING EDGE SLAT DID NOT RETRACT. VERIFIED BY VISUAL CHECK. *S/D* FOUND SLAT HOOK CRACKED. REPLACED SLAT. 2 L 7 3 4F 4 F A3WE E2EA 1999082700986 19990827 00986 NM 1999 8 27 DL72W991856 1 19990819 A 2121 FAN 215201 BOEING 727 727247 138408F NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 2811W 409 20649 ON DESCENT INTO PHL, FLT ATTENDANTS REPORTED SMOKE IN CABIN. POM PROCEDURES FOLLOWED BUT WERE UNABLE TO DETERMINE SOURC E. FLT ATTENDANTS LATER REPORTED, SUSPECTED AN ELECTRICAL PROBLEM. TROUBLESHOT PACK SYSTEM AND ALL NORMAL. FOUND GASP ER FAN POPPING C/B AND CAUSING SEVERE ELEC SMELL. REPLACED SAME. 2 L 7 3 4F A3WE 1999082700987 19990827 00987 WP 1999 8 27 DLL19991857 1 19990819 A 5312 1542506101 BULKHEAD WEB LKHEED 1011 10113853 5265020 WP BS 416 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 765DA 193H1206 TOOLING DAMAGE WAS FOUND ON THE NLG WHEEL WELL BULKHEAD AT APPROX FS 416, RBL 22 ON THE LWR SURFACE O/B FILLET RADIUS IN SIDE THE RT ECS COMPT (NLG BLKHD WEB CAP). DAMAGE DEPTH IS APPROX 0.060 BY 1 IN LENGTH (FWD/AFT) BY 0.5 (VERT). REPAIR ED PER ERA 333433-14, REV B. 2 L 7 3 4F A23WE 1999082700988 19990827 00988 NM 1999 8 27 DL72W991858 1 19990819 A 2611 SMOKE LIGHT BOEING 727 727247 138408F NM AFT LAV ILLUMINATED A DALA K NONE N FALSE WARNING CR CRUISE 1 SO 27 2811W 20649 LAV SMOKE LIGHT ILLUMINATED. LAVS CHECKED AND NO SMOKE/FIRE/FUMES OBSERVED. POM PROCEDURES FOLLOWED AND LIGHT AND CABI N CHIMES EXTINGUISHED WHEN SWITCH IN STARBOARD AFT LAV WAS PLACED OFF. VERIFIED LAV SMOKE DETECTORS IN ALL LAVS CHECK N ORMAL. NO SIGNS OF SMOKE/FIRE/FUMES. 2 L 7 3 4F A3WE 1999082700989 19990827 00989 1999 8 27 DL757991861 4 19990819 A 3451 DME 6224540001 BOEING 757 757232 1384965 NM AVIONICS COMPT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 614DL 753 22821 FAILURE OF GROUND ELECTRICAL POWER, ACRID SMOKE IN COCKPIT AND GALLEY. LT DME C/B POPPED. REPLACED LT DME RECEIVER, OP S CK OK. 2 L 7 2 4F RT A2NM 1999082700990 19990827 00990 NM 1999 8 27 DL72K991862 1 19990819 A 3350 BATTERY BOEING 727 727232 1384082 NM L1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA 21232 ON L/O, FOUND L1 EMERGENCY LIGHT INOP. REPLACED BATTERIES, CKS GOOD. 2 L 7 3 4F A3WE 1999082700991 19990827 00991 NE 1999 8 27 DLM11991863 2 19990819 A 7261 OIL LINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 ENGINE WORN A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 810DE 30434 48565 723924 NR 2 ENG OIL QTY LOW, INDICATED 10 QTS FOLLOWING ENG START. BURNED APPROXIMATELY 1.5 QTS/HR. FOUND NR 3 SCAVENGE LINE LOOSE WORN SHIM. RESHIMED AND RETORQUED LINE, CKS OK. 2 L 7 3 4F 4 F RT A22WE E24NE 1999082700992 19990827 00992 NM 1999 8 27 DLM88991864 1 19990819 A 3350 BATTERY PACK 61020 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 927DA 49714 ON INSPECTION, FOUND FWD I/B FLIGHT ATTENDANT EMERGENCY FLASHLIGHT NOT TESTING. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 2 4F RT A6WE 1999082700993 19990827 00993 NM 1999 8 27 DL72L991865 1 19990811 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 NR 2 K-FLAP ACTUATOR MOUNT BRACKET IS CRACKED IN RADIUS. STOP DRILLED CRACK IN OUTBOARD BRACKET AND FABRICATED DOUBLER PER M/M 57-20-21 FIG 802. OK TO INSTALL. INSTALLED DOUBLER PER M/M 57-20-21 FIG 807. 2 L 7 3 4F A3WE 1999082700994 19990827 00994 NE 1999 8 27 DL72S991866 2 19990820 A 7532 658385 PRBC BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE INOP A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 419DA 21272 696512 AUTO PACK TRIP ON TAKEOFF. POSSIBLE COMPRESS STALL. OCCURED AFTER BRAKES RELEASE. ABORTED TAKEOFF AT 60 KTS. REPLACE D NR 3 ENGINE PRBC FOR OFF IDLE STALL. RAN ENG PER PHHB, ALL INDICATIONS CKS OK. NO STALLS. 2 L 7 3 4F 4 F A3WE E2EA 1999082700995 19990827 00995 WP 1999 8 27 DLL13991868 1 19990821 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 790DL 37832 193A1143 SMOKE SEEN COMING FROM OVHD BIN ABOVE ROW 45 DURING TAXI IN. SMOKE DISSIPATED WHEN THE BIN WAS OPENED. FOUND LT AFT EM ERGENCY LIGHT CHARGER PWR SUPPLY BAD. REPLACED SAME, CKS OK. 2 L 7 3 4F A23WE 1999082700996 19990827 00996 NM 1999 8 27 DL76S991869 1 19990820 A 3350 BATTERY PACK BPS73 BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 126DL 8602 24076 EMERGENCY LIGHT INOP. REPLACED BATTERY RACK. 2 L 7 2 4F RT A1NM 1999082700997 19990827 00997 NM 1999 8 27 DL73K991870 1 19990821 A 7312 320115 HEAT VALVE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 320DL 23092 709247 NOTICED NR 1 FUEL HEAT VALVE OPEN. COULD NOT CLOSE. OIL TEMP ROSE TO 140 DEG AND STAYED. AFTER 15 MIN NR 1 ENGINE WAS SHUTDOWN. REPLACED NR 1 ENG FUEL HEAT VALVE PER M/M 73-14-11. CHECKED OPERATION OF FUEL HEAT VALVE PER M/M 73-14-0. O PERATION CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 1999082700998 19990827 00998 1999 8 27 DL76K991872 4 19990821 A 2330 PROJECTOR BOEING 767 767332 1382001 NM CABIN FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 172DZ 29691 TAXING OUT FOR T/O, STRONG ELECT SMELL IN FIRST CLASS CABIN AROUND PROJECTOR. FWD PASSENGER ENTERTAINMENT SYSTEM TO MCO AND PLAC. PULLED AND COLLARED C/BS 11T34 ALONG WITH C/BS IN E & E, 3TJ2 VIDEO ONE. 2 L 7 2 4F RT A1NM 1999082700999 19990827 00999 NE 1999 8 27 DLM88991873 2 19990822 A 7230 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 BIRD STRIKE A DALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 27 965DL 20366 726052 49984 726052 FLT ATTENDANT REPORTED LOUD NOISE AND VIBRATION AFTER T/O. AT FL 260 NR 1 ENG COMPRESSOR STALLED. FOUND BIRD REMAINS I N NR 1 ENG INLET AND FOD DAMAGE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999082701000 19990827 01000 NM 1999 8 27 DL757991874 1 19990822 A 2560 SWITCH BOEING 757 757232 1384965 NM EMER EXIT SLIDE BENT A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 634DL 23615 TAKEOFF ABORTED AT 100 KIAS DUE TO RT WING SLIDE LIGHT ON EICAS. FOUND RT OVERWING SLIDE PACK PROX SWITCH TARGET BENT . ADJUSTED SAME AND LIGHT CKS GOOD. 2 L 7 2 4F RT A2NM 1999082701001 19990827 01001 NM 1999 8 27 DL76L991875 1 19990822 A 2560 FUSE BOEING 767 767332 1382001 NM ROW 1-5 BLOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 199DN 28456 ON LAYOVER, FOUND EMERGENCY LIGHTS IN FWD BUSINESS CLASS ROWS 1 THRU 5 AT BOTTOM OF SEATS INOP, BOTH SIDES. REPLACED FU SE AT 1AB, OPS OK. 2 L 7 2 4F RT A1NM 1999082701002 19990827 01002 NM 1999 8 27 DLM88991876 1 19990822 A 2120 AIR DIST DOUG MD88 MD88 3023688 NM LAVATORY ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 951DL 49882 SMELLED HOT SMELL/ELECTRICAL SMELL IN 1ST CLASS LAV AREA AND 1ST CLASS LAV SMOKE DETECTOR ALARM SOUNDING. INSPECTED 1ST CLASS LAV AND ASSOCIATED EQUIPMENT, TRASH CAN AND ALL OK. INSPECTED CABIN LIGHTING AND BAG BINS. INSPECTED E & E COMP T, ALL NORM. 2 L 7 2 4F RT A6WE 1999082701003 19990827 01003 NM 1999 8 27 DL72W991877 1 19990822 A 2611 CONNECTOR 7213000000 BOEING 727 727247 138408F NM SMOKE DETECTOR DIRTY A DALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 27 294WA 22112 LAV SMOKE CAUTION LIGHT ILLUMINATED ON S/O PANEL AND CHIMES IN PAX CABIN. NO FIRE WAS LOCATED AND SYSTEM WAS DEACTIVATE D BY PULLING CIRCUIT BREAKER. FOUND LEFT AFT LAV SMOKE DETECTOR WOULD NOT TEST AFTER RESETTING C/B. CLEANED CONNECTION S AT CANNON PLUG AND SWITCH, OPS CKS GOOD. INSPECTED PLACARDS, EXTINGUISHERS, NO INDICATION OF EXCESS HEAT OR FIRE. 2 L 7 3 4F A3WE 1999082701004 19990827 01004 NM 1999 8 27 DL72K991878 1 19990822 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM L1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 524DA 21584 L1 EMERGENCY EXIT DOOR LIGHT BATTERY WOULD NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999082701005 19990827 01005 NM 1999 8 27 DL733991879 1 19990823 A 5330 SKIN BOEING 737 737347 1384647 NM FUSELAGE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311WA 23597 THE FUSELAGE SKIN WAS FOUND WORN AT THE BASE OF THE VERTICAL STABILIZER AT THE LEADING EDGE. THIS DAMAGE WAS FOUND AT A MAINTENANCE VISIT IN ATLANTA AND WILL BE REPAIRED PER ERA 333448-14. 2 L 7 2 4F RT A16WE 1999082701006 19990827 01006 NM 1999 8 27 DLM88991880 1 19990821 A 5330 29525001 SKIN DOUG MD88 MD88 3023688 NM BS 484 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DL 49544 THE FUSELAGE SKIN HAD A DENT AT FS 484 BELOW STRINGER 20R. THIS DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333456-14. 2 L 7 2 4F RT A6WE 1999082701007 19990827 01007 NM 1999 8 27 DL72L991881 1 19990823 A 5320 651750565 SHEAR TIE BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 DURING HMV, A DAMAGED SHEAR TIE ON THE FUSELAGE FRAME AT FS 1263 WAS FOUND BETWEEN STRINGERS 12L AND 14L. THIS DAMAGE WAS REPAIRED PER ERA 333487-14. 2 L 7 3 4F A3WE 1999082701008 19990827 01008 NM 1999 8 27 DLM88991883 1 19990823 A 2530 OVEN DOUG MD88 MD88 3023688 NM GALLEY ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 985DL 53312 SMOKE IN CABIN. FOUND GALLEY OVEN CAUSING SMELL, CORRECTED. 2 L 7 2 4F RT A6WE 1999082701009 19990827 01009 NM 1999 8 27 DL72L991885 1 19990823 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1234 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND AT A-1 LETTER CK, .5 INCH CRACK IN EMPENNAGE SKIN RT SIDE STA 1234 + STR 22. REPAIRED PER SRM 53-30-3 FIG 25. 2 L 7 3 4F A3WE 1999082701010 19990827 01010 NM 1999 8 27 DL72L991886 1 19990823 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND ON A1 LETTER CK, NR 1 L/E FLAP ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999082701011 19990827 01011 NM 1999 8 27 DL72L991887 1 19990824 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 510DA 21312 ON L/O, FOUND RIGHT EXTERIOR OVERWING EMERGENCY LIGHT FLASHING DURING TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999082701012 19990827 01012 NM 1999 8 27 DL73E991888 1 19990823 A 7711 2045061 EPR INDICATOR BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE INOP A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 382DL 23609 709157 NR 1 EPR IND DID NOT INDICATE ON TAKEOFF ROLL. EPR GAUGE DID INDICATE ON ENG RUN AFTER ABORTED TAKEOFF. REPLACED NR 1 EPR INDICATOR. 2 L 7 2 4F 4 F A16WE E2EA 1999082701013 19990827 01013 WP 1999 8 27 DLL19991890 1 19990824 A 2560 D30311513 SLIDE RAFT LKHEED 1011 10113853 5265020 WP R-3 DOOR DETACHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 R-3 DOOR SLIDE SLIPPED FROM CASE, SAFETY PIN BENT. 2 L 7 3 4F A23WE 1999082701014 19990827 01014 NM 1999 8 27 DL72S991891 1 19990823 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 CEILING EMERGENCY EXIT LIGHT NEAR OVERWING EXIT IS INOP. REPAIRED A BROKEN WIRE AT THE LIGHT ASSY CONNECTOR. 2 L 7 3 4F A3WE 1999082701015 19990827 01015 NM 1999 8 27 DL72L991892 1 19990823 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 500-520 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 LFEC INSPECTIONS OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK. INTERNAL HFEC INSPECTION CO NFIRMED A SINGLE CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN BETWEEN FS 500 & 520. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 368077-14AD. 2 L 7 3 4F A3WE 1999082701016 19990827 01016 NM 1999 8 27 DL72S991893 1 19990820 A 5753 65192705 FLAP TRACK BOEING 727 727232 1384082 NM NR 5 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 INBOARD FLAP NR 5 FLAP TRACK AD 90-07-05, AD 90-06-09, CORROSION FOUND AT MLG BEAM ATTACH PAD AND WEAR AT FWD ATTACH LUG FACES. REPAIRED PER ERA 372299-14AD. 2 L 7 3 4F A3WE 1999090200004 19990902 00004 WP 1999 9 2 MWEA99516 1 19990824 A 5210 59103677 BULKHEAD DOOR DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 CRACKS IN AFT BULKHEAD PLUG DOOR INNER STRUCTURE STAR DOUBLER RADIAL. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999090200005 19990902 00005 NE 1999 9 2 HNAA990102 2 19990719 A 7532 310676001 P2.5 VALVE DHAV DHC8 DHC8201 2809001 NM PWA 120 PW123D 52152 NE NR 1 ENGINE OUT OF ADJUST A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 988HA 426 IN CRUISE FLT, NR 1 P/L RETARDED TO FLIGHT IDLE WITHIN A FEW SECONDS SMELL OF SMOKE. TURNED OFF BLEEDS, SMELL DISSIPATE D. INSPECTED NR 1 ENG P 2.5 SWITCHING VALVE, REMOVED SHIM FROM SAME AND GROUND RUN GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 1999090200007 19990902 00007 NM 1999 9 2 EISA99096 1 19990401 A 5347 BAC1520429 SEAT TRACK BOEING 727 727264 138408M NM BS 760 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 15DF 20710 DURING ACCOMPLISHMENT OF ROUNTINE C-CHECK WORK CARD, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT RIGHT OUTBOARD TRACK FRO M FS 760. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1999090200008 19990902 00008 NM 1999 9 2 UIEA9931 1 19990613 A 5310 STRUCTURE BOEING 747 7472D7B 1384803 NM BS 1920 DAMAGED A UIEA K NONE O OTHER TX TAXI/GRND HDL 1 EA 15 523MC 21782 FLT GT363 - ON ARRIVAL, GROUND OPERATIONS FOUND WHEN THE REAR LOWER LOBE CARGO DOOR WAS OPENED, [ALLET POSITION NR 9 HA S SHIFTED AFT GOING OVER THE END STOPS. THERE WAS STRUCTUAL DAMAGE TO THE BRACE POST ON BOTH SIDES OF THE COMPARTMENT T HAT SEPARATE THE BULK COMPARTMENT FROM THE MAIN SECTION OF THE LOWER AFT CARGO COMPARTMENT AT STA 1920. ON FURTHER INVE STIGATION, MAINTENANCE FOUND THAT PALLET LOCKS FOR AFT END OF PALLET WERE IN DOWN POSITION. OPERATIONAL CHECK OF LOCKS AFTER PALLET WAS REMOVED WERE NORMAL. (M) 2 L 7 4 4F RT A20WE 1999090300001 19990903 00001 NM 1999 9 3 AWXA9900270 1 19990826 A 5315 654582213 FLOORBEAM BOEING 737 73733A 1384673 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 C-CHECK, CORROSION AT FS 328 RBL 28.5 AT FASTENER LOCATION FWD FLANGE WENT OUT OF LIMITS ON NR 5240823. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED PER 53-00-51. MATERIAL 7075T6 .090 R609283, 7075T6 .080 R613726. 2 L 7 2 4F RT A16WE 1999090300002 19990903 00002 NM 1999 9 3 AWXA9900271 1 19990826 A 5320 6977065 SUPPORT BOEING 737 73733A 1384673 NM BS 294-312 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 C-CHECK, T-CAP AT LBL 12 BS 280-306 CORRODED BEYOND LIMITS REF N/R 5240810 ZONE ID/43. REMOVED OLD T-CAP, FABRICATED FL OOR SUPPORT AND FILLER, INSTALLED REPAIR PARTS PER SRM 51-10-2, 51-40-2, 53-10-51. REPAIR INSTALLED FROM STA 294-312. 2 L 7 2 4F RT A16WE 1999090300003 19990903 00003 NM 1999 9 3 AWXA9900272 1 19990826 A 5320 QAA250 SILL BOEING 737 73733A 1384673 NM BS 298-324 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 C-CHECK, CORROSION ON BEAM IN FRONT OF R-1 DOOR FROM BS 324 - 298 RBL 50. REMOVED R-1 MOPSILL PER SRM 51-40-2, FAB DOOR SILL FROM 7075-0 .090, HEAT TREATED TO 7075-T6, INSTALLED MOPSILL IAW SRM 51-40-2, INSTALLED R-1 DOOR DRAIN. 2 L 7 2 4F RT A16WE 1999090300004 19990903 00004 NM 1999 9 3 AWXA9900273 1 19990826 A 5330 65C33756 SKIN BOEING 737 73733A 1384673 NM BS 328 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 C-CHECK, FUSELAGE SKIN AROUND R-1 DOOR, AFT LOWER CORNER, 1 INCH CRACK EXTENDING FROM TOP EDGE DOWN TO AND THRU FASTENER AT STA 328, WL 208-1. REPAIRED PER SRM 53-10-01, CUT DAMAGED AREA OUT, NDT NO CRACKS NOTED. FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS, INSTALLED CONICAL WASHERS AND REPAIRED PARTS. MAT 2024T3 .100 R684203,2024T3 .063, R682091, 2024T3 .040. 2 L 7 2 4F RT A16WE 1999090300005 19990903 00005 NM 1999 9 3 AWXA9900274 1 19990826 A 5230 65469945 CHORD BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 C-CHECK, AFT CARGO DOOR HAS CRACKED T-CHORD / L-ANGLE. REMOVED, FABRICATED REPAIR PARTS AND INSTALLED IAW DWG-65-46994, SRM 52-30-2 AND 51-40-02. 2 L 7 2 4F RT A16WE 1999090300006 19990903 00006 NM 1999 9 3 9903376641 1 19990822 A 2121 6054577 FAN BOEING 747 747212B 1384886 NM CABIN FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 641NW 21941 DURING CRUISE, ELECTRICAL FUMES CIRCULATED IN THE COCKPIT AND CABIN. AIRCRAFT DIVERTED TO ANC AND LANDED WITHOUT INCIDE NT. REPLACED GASPER FAN, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999090300007 19990903 00007 WP 1999 9 3 9903389940 1 19990822 A 3244 A9560892 TIRE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE RT MLG FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 01 3322L 21931 225 47031 667012 ON TAKEOFF APROXIMATELY AT ROTATION SPEED, THE RIGHT ENGINE COMPRESSOR STALLED, EGT AND EPR INDICATIONS FLUCTUATED, AND A BURNING RUBBER SMELL WAS REPORTED IN THE CABIN. AN EMERGENCY WAS DECLARED, COM PROCEDURES FOLLOWED AND THE FLIGHT RET URNED TO DLH AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS 200 LBS BELOW MAXIMUM LANDING WEIGHT. MAINTENANCE DISCOVERED TH E NR 3 MAIN TIRE HAD LOST CAP DURING TAKEOFF RESULTING IN FOD DAMAGE TO THE RIGHT ENGINE AND NR 4 BRAKE FLEX HYDRAULIC L INE. MAINTENANCE REPLACED THE NR 3 AND NR 4 MAIN WHEEL AND TIRE ASSEMBLIES, NR 4 BRAKE FLEX HYDRAULIC LINE AND RIGHT EN GINE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1999090300008 19990903 00008 WP 1999 9 3 9903391158 1 19990809 A 7603 POWER LEVER DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE OUT OF ADJUST A NWAA K NONE O OTHER LD LANDING 1 GL 01 158US 46767 686133 AFTER TOUCHDOWN WHEN REVERSE THRUST WAS APPLIED, THE NR 3 ENGINE DID NOT ACCELERATE. THE NR 2 ENGINE DEVELOPED MAXIMUM REVERSE THRUST WHILE THE NR 1 THRUST REVERSER WAS INOPERATIVE ON MEL. MAXIMUM BRAKING WAS APPLIED BUT THE AIRCRAFT DID NOT STOP UNTIL APPROXIMATELY 200 FEET INTO THE OVERRUN AREA. AIRPORT CFR WAS NOTIFIED AND PERFORMED A HOT BRAKE INSPECT ION AFTER WHICH MAINTENANCE TOWED THE AIRCRAFT TO THE GATE. THE NR 3 ENGINE, ADJUSTMENT OF THE POWER LEVER SYSTEM RIGGI NG PER MM 76-11-00. 2 L 7 3 4F 4 F A22WE E20EA 1999090300009 19990903 00009 EA 1999 9 3 COMA9960468 1 19990825 A 5320 6003153551 SEAL STRIKER CNDAIR CL600 CL6002B19 EA PAX DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 PAX DOOR SEAL NIB DAMAGED AT FS 349.00 NEXT TO LOWER AFT LATCH PIN RECEPTICAL. REPAIRED IAW REO 601R-52-11-008 FROM CAN ADAIR. 2 L 7 2 4F RT A21EA 1999090300010 19990903 00010 EA 1999 9 3 COMA9960469 1 19990825 A 5320 6003153552 SEAL STRIKER CNDAIR CL600 CL6002B19 EA PAX DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 PAX DOOR SEAL NIB DAMAGED AT FS 310.00 NEXT TO LOWER FORWARD LATCH PIN RECEPTICAL. REPAIRED IAW REO 601R-52-11-008 FROM CANADAIR. 2 L 7 2 4F RT A21EA 1999090300011 19990903 00011 NM 1999 9 3 UPS99230467 1 19990808 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1263-1273 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CRACK ON STRUCTURE UNDER AIRSTAIRS ACTUATOR STA 1263 TO STA 1273. CRACK STOP DRILLED IAW 51-10-1. R EPAIRED IAW EOB727-5310-1239E SECTION 3. 2 L 7 3 4F A3WE 1999090300012 19990903 00012 NM 1999 9 3 UPS99230468 1 19990809 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1303 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CRACK ON BOX SKIN, LT SIDE OF AIRSTAIRS AT LIGHTENING HOLE AT STA 1303. REPAIRED IAW 51-40-2. 2 L 7 3 4F A3WE 1999090300013 19990903 00013 NM 1999 9 3 UPS99230470 1 19990810 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, FLOORBEAM LWR CHORD BS 1130 RBL 20-24 HAD CORROSION. CORROSION REMOVED IAW SRM 51-10-6 FIG 3, FOUND OUT OF LIMITS. AREA TRIMMED TO REMOVE CORROSION IAW SRM 51-10-6 FIG 3. REF SMRO EO 99-24-004 R1 UPS ENGINEERING FILE N R 727-53-2161. 2 L 7 3 4F A3WE 1999090300014 19990903 00014 NM 1999 9 3 UPS99230471 1 19990810 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 938 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CRACK AT STRINGER 18A LT BS 938. CARRIED OUT REPAIR TO DAMAGED STR IAW SMRO EO 99-24-006 UPS ENGINEE RING FILE NR 727-53-2161. 2 L 7 3 4F A3WE 1999090300015 19990903 00015 NM 1999 9 3 UPS99530473 1 19990825 A 3231 26702887 SEQUENCE VALVE BOEING 757 75724APF 1384969 NM NLG DOOR FAILED A IPXA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 01 412UP 23852 INSPECTION TYPE:N/A, NOSE GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE GEAR DISAGREE AND GEAR DOORS DISPLAYED DOORS AND GEAR AMBER LIGHTS ILLUMINATED. INDICATIONS NORMAL AFTER ALTN GEAR EXT, EXCEPT DOOR S LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED NOSE GEAR DOOR SEQUENCE VALVE IAW MM 32-34-05. SWUNG GEAR 3 TIMES, SYSTEM OP'S CHECK GOOD. 2 L 7 2 4F RT A2NM 1999090300016 19990903 00016 WP 1999 9 3 UPS99830469 1 19990825 A 3233 FITTING DOUG DC8 DC873F 302199F WP NLG ACTUATOR BROKEN A IPXA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 01 808UP 46008 INSPECTION TYPE:N/A AT FL 310 CRUISE FLIGHT, FELT BUMP ND SHUDDER UNDER OUR FEET. PERFORM ED UPLATCH CHECK NORMAL. LOWE RED GEAR, GOT AN IMMEDIATE NOSE GEAR DOWN INDICATION AND ALOT OF ABNORMAL NOISE AND SHUDDERING UNDER OUR FEET. ALL HYDR AULIC AND GEAR INDICATIONS NORMAL. NORMAL LANDING FOUND NLG ACTUATOR ATTACH FITTING BROKEN OFF OF LEFT BRACE AND AP PROX 3 INCH HOLE IN BULKHEAD. BULKHEAD BEING TEMP REPAIRED AND ACTUATOR & FLEX HYD LINES REMOVED, PREPARING A/C FOR NOS E GEAR DOWN UNPRESSURISED FERRY FLIGHT. REPAIRS CARRIED OUT IAW MM 32-31-03 3B 1-15, SRM 51-01-21, DC8-5330-11499. 2 L 7 4 4F RT 4A25 1999090300017 19990903 00017 EU 1999 9 3 99FDEA00350 1 19990824 A 2612 273902 FIRE CONTROL AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE INOP A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 652FE 735 DESCENT INTO LCK, NR 2 LOOP A LIGHT CAME ON WITH FIRE LIGHT IN FUEL SHUTOFF LEVER. THEN BOTH LOOP LIGHTS CAME ON WITH E CAM WARN. JUST ABOUT TO SHUT DOWN ENG, IT STOPPED. REMOVED AND REPLACED NR 2 ENGINE FIRE CONTROL COMPUTER PER MOCC & M M 26-12. RAN ENGINE, OPS CHECK NORMAL. 2 L 7 2 4F RT A35EU 1999090300018 19990903 00018 EU 1999 9 3 99FDEA00351 1 19990825 A 2720 CONTROLS AIRBUS 310 A310222 3930315 EU RUDDER SLOW RESPONSE A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 SO 25 450FE 162 ON T/O, THE A/C SLOW TO RESPOND TO LEFT RUDDER INPUTS. ABORTED TAKEOFF. NO FAULTS WERE NOTED ON MTP. INSPECTED STEERI NG, RUDDER CONTROLS AND LINKAGE, NO DEFECTS NOTED. STEERING AND RUDDER DEFLECTION CK PER WITH FILLER AND RUDDER PEDAL I NPUTS, NO DEFECTS NOTED PER AMM. 2 L 7 2 4F RT A35EU 1999090300019 19990903 00019 EU 1999 9 3 99FDEA00352 1 19990825 A 2752 537E000003 ACTUATOR AIRBUS 310 A310203 EU TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 443FE 283 FLAPS WOULD NOT FULLY RETRACT AFT T/O. BOTH FLAPS FAULT LIGHTS ILLUM. FLAPS EXTENDED NORM FOR LAND AND RETRACT FULLY A FT LANDING. *S/D* REMOVED AND REPLACED NR 1 JACKSCREW PER A310MM 27-54-21, OPS OK. 2 L 7 2 4F RT A35EU 1999090300020 19990903 00020 EU 1999 9 3 99FDEA00353 1 19990825 A 2130 RELAY AIRBUS 310 A310203 EU NR 2 CABIN PRESS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 413FE 397 NR 2 CABIN PRESS REG FAULT. COULD NOT RESET, CABIN WOULD NOT PRESSURIZE. NOSE RELAY FAILED DURING LAST FLT ON AFS TEST PNL. ATS TRIP OFF. NR 2 CABIN PRESS SYSTEM CHECK OK. REMOVED AND REPLACED PSEU, RELAY 96GB AND 141GB OF FLT/GROUND S YS, OPS OK. 2 L 7 2 4F RT A35EU 1999090300021 19990903 00021 NM 1999 9 3 99FDEA00354 1 19990826 A 2750 RETRACT MECH BOEING 727 727233 138408A NM TE FLAPS MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 270FE 22035 ON FLAP RETRACT AFT T/O, AC EXPERIENCED ASYMMETRIC I/B FLAPS, DAMAGE TO RIGHT I/B FLAP. FLAP APPEAR TO BE JAMMED CAUSIN G DAMAGE TO RIGHT ELEPHANT EAR, RIGHT I/B FLAP ASSY, AND RIGHT AILERON. *S/D* INSTALLED RT I/B FLAP, O/B TRACK PER MM 27-51-031-4, TRANSMISSION ASSY PER MM 27-51-061-4. FLAPS OPER NORMAL. 2 L 7 3 4F RT A3WE 1999090300022 19990903 00022 WP 1999 9 3 ABXA9900667 1 19990824 A 5313 5920319508 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 598 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND LONGERON 30 FLANGE CRACKED UNDER AFT END CAP STATION Y-598. REPAIRED LONGERON IAW DC9 SRM 53-02-0 0. 2 L 7 2 4F A6WE 1999090300023 19990903 00023 WP 1999 9 3 ABXA9900668 1 19990824 A 5320 99105516 WEB DOUG DOUG DC9 DC931 3022065 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 617 RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999090300024 19990903 00024 WP 1999 9 3 ABXA9900669 1 19990825 A 5312 591486529N BULKHEAD T-CAP DOUG DOUG DC9 DC931 3022065 WP BS 617 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND PRESSURE BULKHEAD T-CAP CORRODED AT STATION Y-617. REPAIRED T-CAP IAW ABX REA D953-32890 MR. 2 L 7 2 4F A6WE 1999090300025 19990903 00025 WP 1999 9 3 ABXA9900670 1 19990825 A 5320 991050313 CUSP WEB DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND CUSP WEB RIGHT SIDE CRACKED AT STATION Y-945. REPLACED CUSP WEB IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999090300026 19990903 00026 WP 1999 9 3 MWEA999532 1 19990824 A 3210 LANDING GEAR DOUG DC9 DC982 3022082 WP LT MLG BIRD STRIKE A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 GL 31 810ME 48072 LARGE BIRD STRIKE ON LEFT SIDE OF AIRCRAFT AROUND THE MAIN LANDING GEAR. COMPLETED BIRD STRIKE INSPECTION AND HIGH ENER GY STOP INSPECTION WITH NO DAMAGE NOTED. 2 L 7 2 4F A6WE 1999090300027 19990903 00027 WP 1999 9 3 MWEA99533 1 19990826 A 5330 59114101 SKIN DOUG DC9 DC914 3022034 WP BS 255 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FUSELAGE AT STATION 255 LONGERON 20L HAD A DENT. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999090300028 19990903 00028 WP 1999 9 3 MWEA99534 1 19990826 A 5347 99101545 SEAT TRACK DOUG DC9 DC914 3022034 WP BS 766 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 OUTBOARD SEAT TRACKS AT STATION 766 HAD CRACKS. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1999090300029 19990903 00029 WP 1999 9 3 MWEA99535 1 19990826 A 5512 5918002502 SKIN DOUG DC9 DC914 3022034 WP LT HORIZ STAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 AFT HORIZONTAL STABILIZER LEFT AFT SKIN HAD DIMENSIONAL DISCREPANCIES AT STATION XE 49.720. MTC FABRICATED AND INSTALLE D DOUBLER. 2 L 7 2 4F A6WE 1999090300030 19990903 00030 WP 1999 9 3 MWEA99536 1 19990826 A 5330 99101545 SKIN DOUG DC9 DC914 3022034 WP BS 786 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 SUB FLOOR JUST FORWARD OF STATION 786 AND OUTBOARD OF SEAT TRACK 4 HAD A CRACK. MTC FABRICATED AND INSTALLED DOUBLER RE PAIR. 2 L 7 2 4F A6WE 1999090300031 19990903 00031 WP 1999 9 3 MWEA99537 1 19990826 A 5330 99101513 SKIN DOUG DC9 DC914 3022034 WP BS 642 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 SUB FLOOR JUST INBOARD OF STATION 642 IS CRACKED IN 3 PLACES ON LEFT SIDE. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999090300032 19990903 00032 WP 1999 9 3 MWEA99538 1 19990826 A 5512 59180012 SKIN DOUG DC9 DC914 3022034 WP LT HORIZ STAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LEFT HORIZONTAL STABILIZER UPPER FORWARD, CENTER AND AFT SKIN PANEL HAD MANY ELONGATED HOLES. MTC REAMED HOLES, INSTALL ED FASTENERS, PLY WASHERS, AND BUSHING. 2 L 7 2 4F A6WE 1999090300033 19990903 00033 WP 1999 9 3 MWEA99539 1 19990826 A 5730 99184801 SKIN DOUG DC9 DC914 3022034 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 SKIN DAMAGED AT OUTBOARD UPPER SKIN LEFT AILERON. MTC FABRICATED AND INSTALLED PATCH. 2 L 7 2 4F A6WE 1999090300034 19990903 00034 NM 1999 9 3 VNAA9908008 1 19990824 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 4 & 6 DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 433JS 8102 1148 3047 A SECTION OF EMERGENCY FLOOR LIGHTING AT ROWS FOUR AND SIX WAS NOTED TO BE INOPERATIVE DURING THE PRE-FLIGHT INSPECTION . MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY AT POSITION 5LK, IN ACCORDANCE WITH DORNIER MAINTENANC E MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999090300035 19990903 00035 WP 1999 9 3 ASAA9980135 1 19990608 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE O OTHER CR CRUISE 1 NM 01 972AS 53448 ANC - AFTER ARRIVAL OF FLT 127 - CREW REPORTED THE EMERGENCY LIGHTS FLASHED ON. THEN OFF, DURING CRUISE EN ROUTE SEA/ANC . INSPECTED EMERGENCY LIGHTS SYSTEM AND FOUND EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 11 TO 14 INOPERATIVE. RE-CONNECTE D CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999090300036 19990903 00036 WP 1999 9 3 ASAA9980168 1 19990801 A 5240 HANDLE DOUG DC9 DC982 3022082 WP L2 DOOR ROUGH A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 957AS 49126 PDX - FLT 419 - AFTER ARRIVAL, CREW REPORTED THE L2 DOOR WOULD NOT OPEN. FOUND EXTERIOR HANDLE CATCHING ON DOOR STRUCTU RE. REMOVED BURR FROM HANDLE AND SMOOTHED AREA AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999090300037 19990903 00037 NM 1999 9 3 TWRA9923 1 19990630 A 5313 BULKHEAD CHORD BOEING 747 747131 1384881 NM BS 1480 CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 608FF 19672 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING SB 53A2390, A CRACK WAS DETECTED AT BS 1480 BULKHEAD CHORD. A FITTING WAS FABRICATED BY THAI AIRWAYS IAW BOEING SPECIFICATION. (X) 2 L 7 4 4F A20WE 1999090300038 19990903 00038 NM 1999 9 3 TWRA9931 1 19990808 A 2150 7192387 ACM BOEING 747 747136 1384883 NM AIR COND BAY FAILED A TWRA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 606FF 20273 DURING CRUISE, THE FLIGHT ATTENDANT REPORTED A STRONG SMELL OF SMOKE IN CABIN AND COCKPIT ACCOMPANIED BY A MOTORIZED SOU ND. FOUND THE NR 1 PACK AT FAULT. REPLACED THE ACM. OPS CHECKED OK. (X) 2 L 7 4 4F A20WE 1999090300039 19990903 00039 NM 1999 9 3 TWRA9932 1 19990811 A 3350 S1356B37 LIGHT BOEING 747 747131 1384881 NM L4 DOOR FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 608FF 19672 DURING DOD WALK-AROUND WHEN EMERGENCY EXIT LIGHTS SWITCHED ON, DOOR L4 R4 EXIT SIGNS WOULD NOT ILLUMINATE. REMOVED AND REPLACED BOTH EMERGENCY LIGHT ASSY. (X) 2 L 7 4 4F A20WE 1999090300040 19990903 00040 1999 9 3 TWRA9929 4 19990806 A 2330 110360110 MUX BOX HUGHES BOEING 747 747282B 1384860 NM CABIN FAILED A TWRA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 611FF 20502 AFTER BLOCK-OUT, STRONG ODOR OF SMOKE IN C-ZONE. FOUND MUX BOX AT SEAT 23 AT FAULT. REMOVED AND REPLACED MUX BOX. (X) 2 L 7 4 4F A20WE 1999090300041 19990903 00041 EA 1999 9 3 SMPA99002 1 19990806 A 5711 SPAR DHAV DHC6 DHC6200 EA WS 197.5-222.5 CORRODED A SMPA K NONE O OTHER IN INSP/MAINT 1 WP 13 711AS 202 PPG - DISCOVERED SEVERE CORROSION ON RT WING MAIN SPAR CAPS DURING AD 94-08-10, AND SP NR 57 INSPECTION. CORROSION WAS FOUND ON BOTH LOWER FORWARD AND AFT SPAR CAPS. THE FORWARD SPAR CAP IS CORRODED IN WING BAY STA 197.5 TO 210.0. THE AF T SPAR CAP CORROSION IS CENTERED IN WING BAY STA 210.0 AND 222.5. THE CORROSION IS CONTAINED ONLY ON THE SPAR CAPS WITH IN THESE TWO BAYS. THE HORIZONTAL LEG OF THE CAPS SHOWED EVIDENCE OF EXFOLIATION TO A DEPTH OF AT LEAST HALF THE THICKN ESS OF THE EXTRUSION. 1 H 7 2 3T A9EA 1999090300042 19990903 00042 EU 1999 9 3 REXA99023 1 19990805 A 2150 AIR CONDITIONER SAAB SF340 340B 7860101 EU CABIN FAILED A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 361PX 340B249 FA REPORTED SMOKE IN CABIN ON SHORT FINAL AND SCRAPING NOISE WHEN GEAR WAS EXTENDED. VISUALLY INSPECTED GEAR. NO DEFEC TS NOTED AND INSPECTED CABIN FLOOR AND CIRCULATION FANS IN AREA OF SMOKE NO DEFECTS NOTED. FOUND AFT FREON COMPRESSOR LOCKED UP. (X) 2 L 7 2 4T RT A52EU 1999090300043 19990903 00043 EU 1999 9 3 PLGA990730 1 19990730 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU LEFT FAILED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 349BE 2642 901045 340B196 LGA - FLT 6535 - JUST AFTER TAKEOFF, LEFT AIR CONDITIONING WENT TO FULL HOT. THE FLIGHT ATTENDANT SAID IT WAS UNBEARABL E FOR THE PASSENGERS. THE CREW RETURNED TO LGA WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CYCLE MACHINE IAW T HE SAAB MM. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999090300044 19990903 00044 NM 1999 9 3 MASA99127 1 19990730 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 SBP/PHX - FLT 6550 - THE CAPTAIN FOUND THE EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS FERRIED TO PHX. MAINTENANCE R EPLACED ALL BATTERY PACKS FOR THE LIGHTS. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1999090300045 19990903 00045 WP 1999 9 3 HALA9900157 1 19990803 A 7830 HYDRAULIC LINE DOUG DC9 DC951 3022051 WP NR 1 TR UNIT FAILED A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 699HA 47763 HNL - FLT 362 - FA'S REPORTED A BURNING SMELL THROUGHOUT THE CABIN AND COCKPIT. REMOVED AND REPLACED NR 1 ENGINE T/REV BYPASS VALVE LINE (LEAKING INTO APU INLET). REPLACED BOTH WATER SEPARATORS. CHECKS OK. 2 L 7 2 4F RT A6WE 1999090300046 19990903 00046 WP 1999 9 3 HALA9900158 1 19990806 A 3260 0080004003 PROXIMITY BOX DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A HALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 672MC 47661 HNL - FLT 103 - NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH WITH GEAR UP POSITION. LOCK DOWN OK. LIGHT GOES OUT WITH G EAR DOWN. REPLACED NOSE GEAR SENSOR AND CONDUIT. REPLACED PROXIMITY SWITCH BOX. SWUNG GEAR SEVERAL TIMES. OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1999090300047 19990903 00047 NM 1999 9 3 99ZZZX3150 1 19990712 A 5320 TRIPLER BOEING 727 7272K5 NM FUSELAGE CORRODED A FX7A K NONE O OTHER IN INSP/MAINT 1 SO 19 369FA 21851 DURING A B-CHECK INSPECTION, LEVEL 2 CORROSION FOUND ON INNER SIDE OF FUSELAGE SKIN TRIPLER LOCATED AT THE FORWARD BOTTO M CORNER OF THE AFT LAVATORY SERVICE PANEL CUT-OUT. THE TRIPLER WAS REMOVED AND REPLACED PER DER JOSSIAR DRAWING 72R533 1098. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 1999090300048 19990903 00048 NM 1999 9 3 99ZZZX3151 1 19990711 A 5210 65289254 MECHANISM BOEING 727 7272K5 NM PASSENGER DOOR OUT OF ADJUST A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 369FA 21851 KMEM/KMIA - FAE FLT 114 - AFTER TAKEOFF, UNABLE TO PRESSURIZE CABIN. PURSER ADVISED EXTREMELY LOUD NOISE FROM FORWARD E NTRY DOOR. RETURNED TO KMEM, UNEVENTFUL LANDING. ON THE GROUND, REMOVED LINING. ADJUSTED FORWARD ENTRY DOOR UPPER CON TROL ROD ASSEMBLY RIGGING. INSTALLED LINING, OPS CHECK OK BY MM 52-11-61 AND MM 52-11-01. PRESSURIZATION AND LEAK CHEC K IAW MM 21-31-0. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A3WE 1999090300049 19990903 00049 NM 1999 9 3 99ZZZX3152 1 19990713 A 2750 BRACKET BOEING 727 727259 138408J NM RT TE FLAP CRACKED A FX7A O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 19 203AV 22474 AFTER LANDING, SPEED BRAKE HANDLE WOULD NOT RETRACT. UPON INSPECTION, FOUND OUTBOARD FLAP, FORWARD FLAP MIDDLE FLAP CAR RIAGE ATTACH FITTING BROKEN. PULLEY BRACKET DAMAGED DUE TO FLAP MIS-ALIGNMENT. REMOVED AND REPLACED PULLEY BRACKET. R EMOVED AND REPLACED FORWARD FLAP PN 65-21631-262. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999090300050 19990903 00050 NM 1999 9 3 99ZZZX3153 1 19990716 A 2782 106179210 ACTUATOR 269002910L BOEING 727 727259 138408J NM NFR 3 LE SLAT BROKEN A FX7A H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 203AV 19764 22474 KGSO - ON TAXI TO GATE, A-SYSTEM HYDRAULICS DEPLEATED. ISOLATED A AND B HYDRAULIC SYSTEMS. TAXIED TO GATE UNEVENTFUL, FOUND NR 3 L/E SLAT ACTUATOR END CAP SEPARATED FROM ACTUATOR HOUSING. FATIGUE CRACK SUSPECTED. REMOVED AND REPLACED AC TUATOR. OPS CHECK OK IAW MM 27-81-2. ACTUATOR IS ORIGINAL DELIVERY WITH AIRCRAFT. HISTORICAL RECORDS TO BE SEARCHED F OR OVERHAUL AGENCY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999090300051 19990903 00051 WP 1999 9 3 99ZZZX3154 1 19990804 A 2910 113965650 VALVE DOUG DC8 DC8F55 3021928 WP LT MLG BROKEN A FXLA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 55FB 74681 45678 BOG - ON DEPARTURE, EXPERIENCED LOSS OF HYDRAULIC PRESSURE AND QUANTITY. PROCEEDED TO BAQ AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE LEFT MAIN LANDING GEAR BOGIE SWIVEL UNLOCK CYLINDER RELIEF VALVE WAS BROKEN. REPLACED RELIEF V ALVE AND RETURNED AIRCRAFT TO SERVICE. PART TC: 22,693. (X) 2 L 7 4 4F 4A25 1999090300052 19990903 00052 NM 1999 9 3 BJNA990801 1 19990805 A 3350 1000679 LIGHT BOEING 737 737282 13844AT NM COCKPIT INOPERABLE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 344TM 23044 COCKPIT OVERHEAD EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER BMM 33-51-101, TEST OK. (X) 2 L 7 2 4F RT A16WE 1999090300053 19990903 00053 NM 1999 9 3 F3LA99111 1 19990810 A 3350 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 73245 8 20214 DEN - FLT 317 - FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTS FLICKERED IN-FLIGHT. MAINTENANCE RECHARGED BATTERY PAC KS AND OPERATIONAL CHECKED OKAY. PART TC: 90,740. (X) 2 L 7 2 4F A16WE 1999090300054 19990903 00054 NM 1999 9 3 F3LA99110 1 19990809 A 3350 500000043 BATTERY CHARGER BOEING 737 737201 1384454 NM CABIN FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 73233 4 20214 DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING DID NOT EXTINGUISH WHEN TESTED. MAINT ENANCE REPLACED AFT SEAT BATTERY CHARGING UNIT. TC: 9,073. (X) 2 L 7 2 4F A16WE 1999090300055 19990903 00055 NM 1999 9 3 F3LA99109 1 19990810 A 3520 MASK BOEING 737 737201 1384454 NM CABIN DID NOT DEPLOY A F3LA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 03 217US 71507 3508 20215 DEN - DURING DEMONSTRATION, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DEPLOY. MAINTENANCE PERFORMED AN OPERATIONAL CHEC K OF THE PASSENGER OXYGEN SYSTEM MANUAL ACTIVATION PER MM 35-21-00A AND CHECKED OKAY. TC: 88,247. (X) 2 L 7 2 4F A16WE 1999090300056 19990903 00056 NM 1999 9 3 F3LA99113 1 19990812 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN BROKEN A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 73252 20214 DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE REP AIRED BROKEN GROUND WIRE AFT OF BATTERY PACK CONNECTION. TC: 90,747. (X) 2 L 7 2 4F A16WE 1999090300057 19990903 00057 NM 1999 9 3 F3LA99112 1 19990811 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN BROKEN A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 73250 20214 DEN - FLIGHT CREW REPORTED EMERGENCY EXIT AISLE PATH LIGHTING ILLUMINATED IN-FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE A T D9022P AND CHECKED OKAY. TC: 90,745. (X) 2 L 7 2 4F A16WE 1999090300058 19990903 00058 NM 1999 9 3 F3LA99108 1 19990810 A 3520 MASKS BOEING 737 737201 1384454 NM CABIN DID NOT DEPLOY A F3LA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 03 212US 73913 620 20212 DEN - DURING DEMO FLIGHT, FLIGHT CREW REPORTED OXYGEN MASKS DID NOT DROP IN MANUAL MODE. MAINTENANCE RESET T-HANDLE IN COCKPIT AND PERFORMED AN ANNUAL DROP TEST PER MM 35-21-00A. SYSTEM CHECKED OKAY. TC: 91,843. (X) 2 L 7 2 4F A16WE 1999090300059 19990903 00059 NM 1999 9 3 F3LA99106 1 19990716 A 5412 FIREWALL BOEING 737 737301 1384611 NM LT NACELLE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 45319 2167 23257 DEN - DURING C-CHECK, INSPECTION REPORTED FIREWALL FROM CLAMP 12 O'CLOCK POSITION AT NACELLE STA 204.5 (6 INCHES AFT OF FORWARD ENGINE MOUNT ON NACELLE). MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-13. TC: 27,402. (X) 2 L 7 2 4F RT A16WE 1999090300060 19990903 00060 NM 1999 9 3 F3LA99107 1 19990731 A 5320 65465431 SUPPORT BOEING 737 737301 1384611 NM NR 1 MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 30127 23257 DEN - DURING C-CHECK, INSPECTION REPORTED LEFT MAIN LANDING GEAR FORWARD UPLOCK SUPPORT SHAFT LUG CORRODED, STA 685. MA INTENANCE REPLACED NR 1 MAIN LANDING GEAR PER MM 32-11-00. TC: 15,691. (X) 2 L 7 2 4F RT A16WE 1999090300061 19990903 00061 NM 1999 9 3 F3LA99105 1 19990716 A 5754 65C2660195AK SKIN BOEING 737 737301 1384611 NM NR 1 LE SLAT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 45319 PNS014 23257 DEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN NR 1 LEADING EDGE SLAT LOWER SKIN AT TWO RIVETS, OUTBOARD MAIN RACK. MAINTENANCE FABRICATED, TREATED AND INSTALLED REPAIR PER EA 57-737-027. TC: 27,402. (X) 2 L 7 2 4F RT A16WE 1999090300062 19990903 00062 EU 1999 9 3 C2XA99IA392 1 19990711 A 5347 S5367800121000 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CARGO BAY RT SEAT RAIL CORRODED FROM FRAMES 36 TO 39. REMOVED AND REPLACED SE AT TRACK IAW SRM 51-25-05. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) TAT: 23,946.4 HOURS. TAC: 27,645. (X) 2 H 7 2 4T RT A53EU 1999090300063 19990903 00063 EU 1999 9 3 C2XA99IA391 1 19990617 A 5347 S5367800121400 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 25811 094 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CARGO BAY LT SEAT RAIL CORRODED FROM FRAMES 39 TO 41. REMOVED AND REPLACED SE AT TRACK IAW SRM 51-25-05. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 23,946.4 HOURS. TAC: 27,645. (X) 2 H 7 2 4T RT A53EU 1999090300064 19990903 00064 NE 1999 9 3 REXA99020 2 19990617 A 7311 D157310A FUEL/OIL COOLER HAMSTD 7758001 SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RIGHT CRACKED A REXA O OTHER O OTHER CR CRUISE 1 SO 25 347AM UDAG0332 340A039 RIGHT PROPELLER OIL PRESSURE INOPERABLE IN-FLIGHT. RIGHT PGB OVERSERVICED, FOUND FUEL IN OIL. REMOVED AND REPLACED RIG HT ENGINE FUEL HEATER. DRAINED ALL OIL FORM PGB AND PGB OIL COOLER, FLUSHED PBG OIL SYSTEM, REMOVED AND REPLACED PGB OI L FILTER AND RESERVICED PGB OIL. PERFORMED GROUND RUNS AND MONITORED ENGINE AND PROPELLER OIL PRESSURE AND TEMPERATURES . OPERATIONALLY CHECKED GOOD. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1999090300065 19990903 00065 EU 1999 9 3 C2XA99IA390 1 19990711 A 5347 S5367800121000 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CARGO BAY LEFT SEAT RAIL CORRODED FROM FRAMES 36 TO 39. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-25-05. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 23,946.4 HOURS. TAC: 27,645. (X) 2 H 7 2 4T RT A53EU 1999090300066 19990903 00066 EU 1999 9 3 C2XA99IA389 1 19990711 A 5311 S5367240820200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSS FRAME CORRODED AT FRAME 39. REPAIRED IAW EC 5340-01018. AIRCRAFT APPRO VED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300067 19990903 00067 EU 1999 9 3 C2XA99IA388 1 19990711 A 5311 S5367240620800 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSS FRAME CORRODED AT FRAME 36. REPAIRED IAW EC 5310-01037. AIRCRAFT APPRO VED FOR RETURN TO SERVICE. TAT: 23,946.4 HOURS. TAC: 27,645. (X) 2 H 7 2 4T RT A53EU 1999090300068 19990903 00068 SO 1999 9 3 C2XA99IA415 1 19990726 A 5320 12020530001 BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT OUTBOARD BEAM CORRODED BETWEEN FRAMES 14 AND 17. REMOVED CORROSION, FABR ICATED AND INSTALLED REPAIR DOUBLERS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01043 REV. O RIG. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300069 19990903 00069 SO 1999 9 3 C2XA99IA414 1 19990726 A 5330 12002603017 SKIN EMB 120 EMB120RT SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FUSELAGE SKIN DENTED FORWARD OF RIGHT WINDSHIELD. FABRICATED AND INSTALLED RE PAIR DOUBLER IAW SRM'S 53-00-01 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24 ,388. (X) 2 L 7 2 4T RT A31SO 1999090300070 19990903 00070 SO 1999 9 3 C2XA99IA413 1 19990726 A 5720 1201704014 BRACKET EMB 120 EMB120RT SO RT WING HOLES ELONGATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS CHECK, FOUND TIE ANGLE BRACKET HOLES ELONGATED FOR INTERNAL WING STRINGER AFT OF ACCESS PANEL 622EB. REPLACED BRACKET IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,3 88. (X) 2 L 7 2 4T RT A31SO 1999090300071 19990903 00071 SO 1999 9 3 C2XA99IA412 1 19990726 A 5713 12016079002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND INTERNAL WING STRINGER CRACKED AFT OF ACCESS PANEL 622EB. REMOVED DAMAGED SEC TION OF STRINGER AND SPLICED IN NEW SECTION IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010 REV B. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300072 19990903 00072 SO 1999 9 3 C2XA99IA411 1 19990726 A 5320 12027929001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CENTER BUTT STRAP CORRODED BETWEEN FRAMES 34 AND 38. REMOVED AND REPLACED BUT T STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300073 19990903 00073 SO 1999 9 3 C2XA99IA410 1 19990726 A 5320 12006158001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT BUTT STRAP BL 15 CORRODED BETWEEN FRAMES 39 AND 44. REMOVED AND REPLACE D BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300074 19990903 00074 SO 1999 9 3 CX2A99IA409 1 19990726 A 5320 12027928001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LT BUTT STRAP CORRODED UNDER FLOOR PANEL 251CF BETWEEN FRAMES 33 AND 36. REMO VED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24 ,388. (X) 2 L 7 2 4T RT A31SO 1999090300075 19990903 00075 SO 1999 9 3 C2XA99IA408 1 19990726 A 5320 12027929003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT BUTT STRAP CORRODED UNDER FLOOR PANEL 252BF BETWEEN FRAMES 32 AND 33. REMO VED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24, 388. (X) 2 L 7 2 4T RT A31SO 1999090300076 19990903 00076 SO 1999 9 3 C2XA99IA407 1 19990726 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSSBEAM CORRODED AT FRAME 36 BETWEEN BL ZERO AND LBL 19. REMOVED AND REPLAC ED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300077 19990903 00077 SO 1999 9 3 C2XA99IA406 1 19990726 A 5320 12006667003 BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CENTER BEAM BETWEEN FRAMES 38 AND 39. REMOVED CORROSION, FABRICA TED AND INSTALLED REPAIR DOUBLERS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01043 REV ORIG. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300078 19990903 00078 SO 1999 9 3 C2XA99IA405 1 19990726 A 5320 12025849001 BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CENTER BEAM BETWEEN FRAMES 39 AND 44. REMOVED CORROSION, FABRICA TED AND INSTALLED REPAIR DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01043 REV ORIG. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300079 19990903 00079 SO 1999 9 3 C2XA99IA404 1 19990726 A 5320 12027929001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND BUTT STRAP CORRODED ON LT OUTBOARD BEAM BETWEEN FRAMES 36 AND 38. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. ( X) 2 L 7 2 4T RT A31SO 1999090300080 19990903 00080 SO 1999 9 3 C2XA99IA403 1 19990726 A 5320 12005779001C CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSSBEAM CORRODED AT FRAME 40 BETWEEN RT OUTBOARD BEAM AND RT SILL. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300081 19990903 00081 SO 1999 9 3 C2XA99IA402 1 19990726 A 5320 12006158003D BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND BUTT STRAP CORRODED AT FRAME 42 ON CENTER BEAM. REMOVED AND REPLACED BUTT STR AP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300082 19990903 00082 SO 1999 9 3 C2XA99IA401 1 19990726 A 5320 12004449001A CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOOR CROSSBEAM CORRODED AT FRAME 40 BETWEEN RT OUTBOARD BEAM AND CENTER BEAM. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC : 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300083 19990903 00083 SO 1999 9 3 C2XA99IA400 1 19990726 A 5320 1200449001A CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOOR CROSSBEAM CORRODED AT FRAME 38 BETWEEN RT OUTBOARD BEAM AND CENTER BEAM. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC : 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300084 19990903 00084 SO 1999 9 3 C2XA99IA399 1 19990726 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOOR CROSSBEAM CORRODED AT FRAME 38 BETWEEN RT SILL AND RT OUTBOARD BEAM. RE MOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 2 4,388. (X) 2 L 7 2 4T RT A31SO 1999090300085 19990903 00085 SO 1999 9 3 C2XA99IA398 1 19990726 A 5320 12006159001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT SILL CORRODED BETWEEN FRAMES 41 AND FRAME 45. REMOVED AND REPLACED SILL FR OM FRAME 38 TO FRAME 45 IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. AT: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300086 19990903 00086 SO 1999 9 3 C2XA99IA397 1 19990726 A 5311 12022636501 FRAME EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FRAME 47 CRACKED AT STR R15. REMOVED DAMAGE, FABRICATED AND INSTALLED FILTER AND DOUBLER REPAIR IAW SRM'S 51-70-05 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TA C: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300087 19990903 00087 SO 1999 9 3 C2XA99IA396 1 19990726 A 5320 12027929001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND BUTT STRAP CORRODED ON RT OUTBOARD BEAM AT FRAMES 38 TO 42. REMOVED AND REPLA CED BUTT STRAP FROM FRAME 38 TO FRAME 42 IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOU RS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300088 19990903 00088 SO 1999 9 3 C2XA99IA395 1 19990726 A 5320 12018806002 ANGLE EMB 120 EMB120RT SO PASSENGER DOORWA CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOOR SUPPORT ANGLES AT PASSENGER DOOR ENTRANCE CORRODED AT FRAME 14 AND FRAME 15. REMOVED AND REPLACED ANGLES IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. T AC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300089 19990903 00089 SO 1999 9 3 C2XA99IA394 1 19990726 A 5320 12026671001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND BUTT STRAP CORRODED UNDER FLOOR PANELS 231BF AND 231EF, FROM FRAME 13 TO FRAME 16. REMOVED AND REPLACED DAMAGED PORTION OF BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TA T: 18,416.5 HOURS. TAC: 24,388. (X) 2 L 7 2 4T RT A31SO 1999090300090 19990903 00090 SO 1999 9 3 C2XA99IA393 1 19990726 A 5320 12007089603 SUPPORT EMB 120 EMB120RT 3260202 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 DURING CONTINENTAL EXPRESS C-CHECK, FOUND WEB SUPPORT CORRODED UNDER FLOOR PANEL 231AF FROM FRAME 13 TO FRAME 16. REMOV ED AND REPLACED WEB SUPPORT IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24, 388. (X) 2 L 7 2 4T RT A31SO 1999090300091 19990903 00091 EU 1999 9 3 C2XA99IA371 1 19990718 A 3350 3011160 LIGHT AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR INOPERABLE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300103 19990903 00103 NM 1999 9 3 TWAA9911701 1 19990827 A 3350 LIGHT BOEING 757 7572Q8 1384972 NM LAVATORY INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 713TW 28173 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT THE RT AFT LAVATORY. CLEANED THE EGRESS STRIP. CHECK-C 1-20-99 LAX. 2 L 7 2 4F RT A2NM 1999090300104 19990903 00104 NM 1999 9 3 AT9900601R1 1 19990818 A 3244 26015711 TIRE BOEING 737 737297 1384480 NM NR 3 BLOWN A ZZDA A UNSCHED LANDING G MULTIPLE FAILURE TO TAKEOFF 1 SO 15 462AT 22631 NR 3 TIRE FAILURE CAUSED DAMAGE TO AIRCRAFT WHICH RESULTED IN ALL HYDRAULIC FLUID LOSS. REMOVED AND REPLACED NR 3 AND N R 4 TIRE AND BRAKE, NR 1 AND NR 2 ENGINE HYDRAULIC PUMP DUE TO SYSTEM FAILURE. REPLACED HYDRAULIC TEE FITTING, SUPPLY B SYSTEM TUBE ASSEMBLY, AND HYDRAULIC HOSE FLEX LINE. REPLENISHED HYDRAULIC SYSTEM FLUID AND PURGED A AND B SYSTEM AND L EAK CHECK ALL SYSTEM AND COMPLIED WITH OVERWEIGHT LANDING INSPECTION IAW DC9 MM 29-11-0, 29-00, 32-40, 5-51-291 PHASE 1 STEP 2B, 32-30-00-15A, 32-45-11, AND 32-43-0. 2 L 7 2 4F A16WE 1999090300105 19990903 00105 WP 1999 9 3 AT9900603 1 19990729 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE AFT CARGO DOOR OUTER SKIN CRACK AT FASTENERS ON THE LOWER SIDE. R EMOVED LOWER HALF OF PRESSURE SEAL FOR ACCESS. CUT OUT CRACKED AREA, NDT VERIFIED CRACK TERMINATION. DRILLED DOUBLER, TRIMMED, DEBURRED, PRIMED, AND INSTALLED DOUBLER AND REINSTALLED PRESSURE SEAL IAW DC9 SRM 51-10-3, 51-30-5, 52-05 FIG 3 , AND TIMCO RES NR 07648. 2 L 7 2 4F A6WE 1999090300106 19990903 00106 WP 1999 9 3 AT9900604 1 19990809 A 5320 5957139507 BRACKET DOUG DC9 DC932 3022066 WP LT MLG WW CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CORROSION ON TOP OF CONTROL CABLE AILERON PULLEY TOWER IN FORWARD OUT BOARD OF LEFT WHEEL WELL. REMOVED AND REPLACED PULLEY BRACKET AND HARDWARE IAW DC9 MM 20-16-0, 27-61-10, AND TIMCO EO N R 99-1207. 2 L 7 2 4F A6WE 1999090300107 19990903 00107 WP 1999 9 3 AT9900605 1 19990804 A 5530 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE LEFT LOWER AFT BANANA FAIRING ON THE VERTICAL STABILIZER AND SKIN CHAFFED AT YV 227-247. BLEND CHAFFED AREA ON THE BANANA FAIRING AND FABRICATED NEW SKIN PANEL FOR THE VERTICAL STABILI ZER. HEAT TREATED, DYE PENETRANT, TRIMMED, ALODINED, PRIMED, SEAL AND INSTALLED STABILIZER SKIN IAW DC9 SRM 51-30-2, 51 -10-3, AND TIMCO EO NR 99-1198. 2 L 7 2 4F A6WE 1999090300108 19990903 00108 WP 1999 9 3 AT9900606 1 19990814 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN WEAK A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, UPON INSTALLATION FOUND CABIN FLOORBOARD NR 97 WEAK. FABRICATED A REPLACEM ENT FLOORBOARD PANEL IAW DC9 SRM 53-21-0, DOUGLASS DRAWING NR 9915532 AND TIMCO RES NR 07642. 2 L 7 2 4F A6WE 1999090300109 19990903 00109 WP 1999 9 3 AT9900607 1 19990721 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-180 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND RIGHT FLOOR PANEL AT BS 160-180 CORRODED. FABRICATED FLOORBOARD PANE L, DRILLED, DEBURRED, DIMPLED, ALODINED, PRIMED, AND INSTALLED NUT PLATES IAW DC9 SRM 53-21 FIG D, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999090300110 19990903 00110 WP 1999 9 3 AT9900608 1 19990819 A 5320 ANGLE DOUG DC9 DC932 3022066 WP AFT STAIRS CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE AFT VENTRAL STAIR FIFTH STEP SUPPORT ANGLE CORRODED. REMOVED, RE PLACED AND FABRICATED ANGLE, TREATED, PRIMED AREA IAW DC9 SRM 51-10-3, AND 51-10-2. 2 L 7 2 4F A6WE 1999090300111 19990903 00111 WP 1999 9 3 AT9900609 1 19990825 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 19 BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 846AT 47226 FOUND EMERGENCY PATH LIGHT DIM AT ROW 19. REPAIRED WIRING IAW MM 20-50-1. OPS CHECK GOOD IAW BRUCE INDUSTRIES MM 33-21 -27. 2 L 7 2 4F A6WE 1999090300112 19990903 00112 WP 1999 9 3 CALA9901094 1 19990826 A 3231 CONTROL CABLE DOUG DC9 DC931 3022065 WP NLG DOOR BROKEN A CALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 09 14564 47490 A LOUD BANG WAS HEARD UPON GEAR RETRACTION AND THE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER TAKEOFF FROM IAH. THE AIRCR AFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOOR CABLE BROKEN WITH DAMAGE TO FWD NLG DOOR AND DOOR LOCK MECHANISM. THE CABLE, LOCK MECHANISM, AND DOOR WERE REMOVED AND REPLACED IAW MM 32-22-1. 2 L 7 2 4F A6WE 1999090300113 19990903 00113 NM 1999 9 3 UPS99230475 1 19990826 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 9 & 17 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 EMERGENCY LIGHTS OUT AT SEAT NR 9 AND 17 AND LT UPPER REAR LAV. REMOVE AND REPLACE BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999090300114 19990903 00114 NM 1999 9 3 UPS99430474 1 19990825 A 2160 9617017003 CONTROLLER BOEING 747 747123F NM COCKPIT INOP A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 674UP 20100 ATB - CREW REPORTED STRONG ACRID SMELL IN COCKPIT, COULD NOT LOCATE SMELL. CREW USED O2, RETURNED TO HKG. FOUND LEFT UP PPER DECK HEATER TEMP CONTROL AT FAULT. REMOVED AND REPLACED LEFT CONTROLLER. 2 L 7 4 4F A20WE 1999090300115 19990903 00115 WP 1999 9 3 UPS99830476 1 19990729 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 FWD PIT FS 100 RBL 41 FLOORBEAM CORRODED. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW DC8 SRM 51-7-1 FIG 13 AND DC8 SRM 51-2-0, FIG 50 ORG 125. FABRICATED AND INSTALLED DOUBLER IAW REO- 06665, DC8 SRM 51-1-20. INSTALLED FL OORBOARD SECTIONS IAW DC8 SRM 5 1-3-0. 2 L 7 4 4F RT 4A25 1999090300116 19990903 00116 WP 1999 9 3 UPS99830477 1 19990726 A 5240 FRAME DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 1 EA HOLE DRILLED THROUGH RT FWD SERVICE DOOR INNER SKIN IN CLOSE PROXIMITY TO ADJACENT RIVET LOCATED AT LOWER AFT CORNER OF DOOR. 51-9-0 INSTALLED FASTENERS IN PREVIOUS DOUBLER ON SKIN IAW DC8 SRM 5 1-1-2, SRM 51-1-20D. INSTALLED SEAL RETAINER AND CONNECTED ROD ARM IAW DC8 SRM 51-3-0 AND MM 20-18-00. 2 L 7 4 4F RT 4A25 1999090300117 19990903 00117 WP 1999 9 3 UPS99830478 1 19990804 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 STA 1580 TRACK F CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW D C8 SRM 53-2-3. FABRICATED AND INSTALLED SEAT TRACK, STRAPS AND STRIPS I AW DC8 SRM 53-2-3 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300118 19990903 00118 WP 1999 9 3 UPS99830479 1 19990726 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 STA 680 L10R END FTG CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300119 19990903 00119 WP 1999 9 3 UPS99830480 1 19990726 A 5347 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 STA 680 L6R END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300120 19990903 00120 WP 1999 9 3 UPS99830481 1 19990729 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 RT CUSP AT STA 1360 CUSP TO FRAME FITTING CORRODED DOT G-932. REMOVED CORROSION PER DC8 SRM 51-1-8, 53-2-0, FOUND TO BE OUT OF LIMITS PER DC8 SRM 53-2-0. ROUTED OUT DAMAGED FLANGE TO REMOVE CORROSION DAMAGE IAW DC8 SRM 53-2-0. ROATE OUT OF CORROSION DAMAGE FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0, FIG 1F. 2 L 7 4 4F RT 4A25 1999090300121 19990903 00121 WP 1999 9 3 UPS99830482 1 19990727 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1740-1760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 EXFOLIATION INSIDE THE LONGERON CHANNEL. SPLICED IN A NEW LONGERON IAW DC8 SRM 51-1-20D AND 53-3-2. 2 L 7 4 4F RT 4A25 1999090300122 19990903 00122 WP 1999 9 3 UPS99830483 1 19990730 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 MAIN CARGO SUB FLOOR, FLOOR SUPPORT ANGLE CRACKED AND GOUGED AT STA 8 RBL 6 DOT G-956. REMOVED AND R EPLACED FLOOR SUPPORT ANGLE IAW REO 06672. REPAIRED WEB IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999090300123 19990903 00123 WP 1999 9 3 MWEA99540 1 19990826 A 5412 59369933 BULKHEAD DOUG DC9 DC914 3022034 WP BS 786 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FABRICATED AND INSTALLED DOUBLERS PER SRO 5936993 DRAWING FOR STATION 786 LEFT AND RIGHT PYLON BULKHEAD. 2 L 7 2 4F A6WE 1999090300124 19990903 00124 WP 1999 9 3 MWEA99541 1 19990826 A 5230 59203233 JAMB DOUG DC9 DC914 3022034 WP CARGO DOORWAY MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 TEMPORARY REPAIR INSTALLED ON FORWARD CARGO DOOR JAMB AT STATION 370. MTC FABRICATED AND INSTALLED NEW REPAIR PARTS. 2 L 7 2 4F A6WE 1999090300125 19990903 00125 WP 1999 9 3 MWEA99542 1 19990826 A 5523 5910414501 SKIN DOUG DC9 DC914 3022034 WP LT ELEV TAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LEFT ELEVATOR GEARED TAB CENTER ATTACHMENT BEARING IS EXCESSIVELY WORN. MTC REPLACED BEARING, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR ON TAB SURFACE SKIN. 2 L 7 2 4F A6WE 1999090300126 19990903 00126 WP 1999 9 3 MWEA99543 1 19990826 A 5522 591184020 SKIN DOUG DC9 DC914 3022034 WP LT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 LEFT ELEVATOR HAS A CRACK IN UPPER SKIN AND WAS DAMAGED ON LOWER INBOARD SKIN. MTC FABRICATED AND INSTALLED DOUBLER REP AIR. 2 L 7 2 4F A6WE 1999090300127 19990903 00127 WP 1999 9 3 MWEA99544 1 19990825 A 5400 99581913 STIFFENER DOUG DC9 DC914 3022034 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LEFT PYLON 2 CHANNEL STIFFENER HAS A CRACK ON OUTBOARD END. MTC FABRICATED AND INSTALLED DOUBLER AND TRIPLER. 2 L 7 2 4F A6WE 1999090300128 19990903 00128 WP 1999 9 3 MWEA99545 1 19990825 A 5320 99124525 ANGLE DOUG DC9 DC914 3022034 WP BS 332 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FORWARD PIT FRAME ANGLE CRACKED AT STATION 332 29R. MTC FABRICATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 1999090300129 19990903 00129 WP 1999 9 3 MWEA99546 1 19990825 A 5312 59103675 PAN DOUG DC9 DC914 3022034 WP AFT PRES BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 THE AFT PRESSURE BULKHEAD PLUG DOOR HAS A CRACK ON PAN AT 11 O'CLOCK POSITION. MAINTENANCE FABRICATED AND INSTALLED DOU BLER. 2 L 7 2 4F A6WE 1999090300130 19990903 00130 WP 1999 9 3 MWEA99547 1 19990825 A 5530 59102281 SKIN DOUG DC9 DC914 3022034 WP BS 894-908 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 A 1 INCH SKIN CRACK TO THE LEFT OF THE VERTICAL FIN RAM AIR INTAKE AT STATION 894 - 908 BETWEEN LONGERON 2L AND 3L. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999090300131 19990903 00131 WP 1999 9 3 MWEA99548 1 19990825 A 5751 9957571503 SKIN DOUG DC9 DC914 3022034 WP LT AILERON DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LEFT WING AILERON TOP SKIN HAD A DENT. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999090300132 19990903 00132 WP 1999 9 3 MWEA99549 1 19990827 A 5720 99116001 WEB DOUG DC9 DC914 3022034 WP CENTER WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 CRACK AT CENTERLINE FRAME LEFT SIDE OF FRAME WEB. MTC FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F A6WE 1999090300133 19990903 00133 WP 1999 9 3 MWEA99550 1 19990827 A 5400 99581592 WEB DOUG DC9 DC914 3022034 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 CRACK AT RIGHT PYLON VERTICAL WEB U-CHANNEL OUTBOARD OF STATION 859. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1999090300134 19990903 00134 WP 1999 9 3 MWEA99551 1 19990824 A 2130 27007571 OUTFLOW SHAFT DOUG DC9 DC914 3022034 WP CABIN WORN A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 800ME 45842 CABIN UNABLE TO PRESSURIZE ABOVE 3 PSID. MTC REMOVED AND REPLACED OUTFLOW SHAFT, BEARINGS, SEALS AND SEAT. 2 L 7 2 4F A6WE 1999090300135 19990903 00135 NM 1999 9 3 MWEA99552 1 19990827 A 2560 D29982107 SLIDE DOUG MD88 MD88 3023688 NM PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE FORWARD EMERGENCY SLIDE FELL OUT OF HOLDER. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F RT A6WE 1999090300136 19990903 00136 NM 1999 9 3 DL72S991896 1 19990825 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1237 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 A .875 INCH CRACK ON EMPENNAGE SKIN AT STR 22R AND STA 1237. REPAIRED PER SRM 53-30-3 FIG 25. 2 L 7 3 4F A3WE 1999090300137 19990903 00137 NM 1999 9 3 DL72S991897 1 19990825 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 REF SHIP 400 TPA LTR CHK C-1, NR 2 L/E SLAT ANTI-ICE T-DUCT CUT OUT ANGLE CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999090300138 19990903 00138 NM 1999 9 3 DL73K991899 1 19990825 A 2781 SENSOR 189929 BOEING 737 737232 1384475 NM NR 1 LE FLAP INOP A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 322DL 000000 23094 NR 1 LEADING EDGE DEVICE INDICATED FULL EXTENDED AFTER FLAPSWERE PUT UP. REPLACED NR 1 LEADING EDGE FLAP DOWN SENSOR. 2 L 7 2 4F RT A16WE 1999090300139 19990903 00139 NM 1999 9 3 DL72S991901 1 19990825 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 18929 21074 DURING LAYOVER CHECK, FOUND LEFT OVERWING MID POSITION EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK OPS NORMAL. 2 L 7 3 4F A3WE 1999090300140 19990903 00140 NM 1999 9 3 DL76G991902 1 19990826 A 2510 3A0900078011 SEAT BOEING 767 7673P6 1385105 NM RT COCKPIT SPARKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 153DL 24985 F/O SEAT INOP. WHILE MOVING SEAT ELECTRICALLY AFT A VISIBLE SPARK WAS SEEN COMING FROM RIGHT REAR LOWER PART OF SEAT (N EAR TRACK) AND SEAT JAMMED, ABLE TO MOVE MANUALLY. MAINTENANCE FOUND POWER CHORD DAMAGED. NO SPARE AT ARN FWD TO MCO, AS PER MEL 25-11-01A. PLACARD INSTALLED. PULLED F/O SEAT CB. 2 L 7 2 4F RT A1NM 1999090300141 19990903 00141 NM 1999 9 3 DL76S991903 1 19990819 A 5330 143T35214 SKIN BOEING 767 767332 1382001 NM BS 465 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 DENT IN FUSELAGE SKIN AT STA 465 ABOVE STRINGER 34R. STRINGER DAMAGED AT THIS LOCATION ALSO. REPAIR SKIN AND STRINGER PER ER/A 333462-14, REV A. 2 L 7 2 4F RT A1NM 1999090300142 19990903 00142 NM 1999 9 3 DL73E991904 1 19990826 A 2530 PLUG BOEING 737 737247 138448D NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 381DL 23608 ELECTRICAL BURING SMELL FROM AFT GALLEY COFFEE MARKER. PULLED C/B SMELL STOPPED. REPLACED BOTH AFT COFFEE MARKERS FOUN D CANNON PLUG TO NR 1 AFT COFFEE MARKER BADLEY CORRODED. FWD AFT COFFEE MARKER NR 1 TO MCO AND PLAC PULLED AND COLLARED C/B. NEEDS NEW CANNON PLUG. 2 L 7 2 4F A16WE 1999090300143 19990903 00143 NM 1999 9 3 DL757991905 1 19990823 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM BS 1689 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 FUSELAGE SKIN FS 1689, STRINGER 15L-16L, DENT CUTOUT REPAIR. THE FUSELAGE SKIN AT FS 1689 BETWEEN STRINGERS 15L AND 16L WAS FOUND DENTED. THE DAMAGED AREA OF SKIN WAS CUTOUT SPANNING THE STRINGERS OVER A 9.8 BY 2 AREA. THE CUTOUT WA S REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 368048-14, REV A. 2 L 7 2 4F RT A2NM 1999090300144 19990903 00144 NM 1999 9 3 DL73E991906 1 19990824 A 5330 65458001205 SKIN BOEING 737 737247 138448D NM BS 332 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 FUSELAGE SKIN ASSY R1 DOOR CUTOUT LOWER AFT CORNER CRACK REPAIR. A .25 LONG TYPICAL CRACK WAS FOUND IN THE SKIN AND BON DED DOUBLER AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT. THE UNDERLYING BEAR STRAP WAS NOT DAMAGED. THE CRACK WAS RO UTED OUT OF THE SKIN AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 368091-14, REV A. 2 L 7 2 4F A16WE 1999090300145 19990903 00145 NM 1999 9 3 DL72K991907 1 19990826 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 521DA 21472 EXT EXIT LIGHT INOP. REPLACED BATTERY PACK, EXIT LIGHT CHECKS OK. 2 L 7 3 4F A3WE 1999090300146 19990903 00146 SO 1999 9 3 SWIA971538 1 19990804 A 2130 PRESSURIZATION EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 198SW 120227 BETWEEN 9,000 AND 11,000 FT EXPERIENCED FOUR SEPARATE INCIDENCES OF CABIN PRESSURE RELEASE. CABIN ALTITUDE INDICATOR SP IKED TO GREATER THAN 2,000 FPM CLIMB. RETURNED TO SLC. CHECKED AUTO PRESSURIZATION USING TEST EQUIPMENT. ALL FUNCTION S CHECKED NORMAL. ALSO MANUAL PRESSURIZATION CHECKS GOOD. UNABLE TO DUPLICATE CONDITIONS ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300147 19990903 00147 EA 1999 9 3 SWIA971539 1 19990803 A 3222 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG STRUT LEAKING A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 403SW 7028 UPON DEPARTURE, NOSE GEAR INDICATION DOWN AND LOCKED AFTER SELECTING GEAR UP. COMPLIED WITH CHECK LIST AND LOWERED GEAR . RETURNED TO FAT, MEL 32-30-1. REMOVED AND REPLACED NOSE GEAR STRUT TEE SEAL AND SERVICED NOSE STRUT. LEAK CHECKS O K IAW 32-21-00. SWUNG GEAR SEVERAL TIMES AND ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999090300148 19990903 00148 SO 1999 9 3 SWIA971540 1 19990805 A 3260 INDICATION EMB 120 EMB120RT SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 268UE 120207 AFTER TAKEOFF, RIGHT GEAR B INDICATOR REMAINED GREEN. CYCLED GEAR DOWN, 3 DOWN AND LOCKED. CYCLED UP RIGHT SIDE A AND B INDICATORS BOTH RED AND SHUDDER NOTICED. CYCLED UP AND DOWN AGAIN WITH SAME RESULTS. CYCLED DOWN AND LEFT DOWN. RET URNED TO AIRPORT. PERFORMED GEAR SWING AND CHECKED CLEARANCE ON RIGHT GEAR UPLOCK AND DOOR SEQUENCING VALVES. GEAR SWI NGS CHECKS GOOD WITH NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300149 19990903 00149 1999 9 3 SWIA971541 4 19990807 A 3425 AHRS COMPUTER EMB 120 EMB120RT SO PWA 118 PW118A NE COCKPIT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 284YV 120284 ABOUT 30 MINUTES AFTER FIRST OFFICERS EADI FAILED, PIT YELLOW FLAG ON CAPTAIN AND FIRST OFFICERS AND A/P STARTED PITCHIN G UP AND HAD TO BE DISCONNECTED. FIVE MINUTES LATER, HDG YELLOW FLAG AND WE HAD 10 FT-15 FT DIFFERENCE FROM CAPTAINS TO FIRST OFFICER'S HEADING INDICATORS. DIVERTED FROM SFO TO FAT. REPLACED FIRST OFFICER'S AHRS COMPUTER. FIRST OFFICER' S AND CAPTAIN'S AHRS SYSTEM TESTS NORMALLY PER MM 34-21-00. BOTH A/P AND FD SYSTEMS TEST NORMALLY PER MM 22-11-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300150 19990903 00150 SO 1999 9 3 SWIA971542 1 19990809 A 7110 PANEL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ENGINE LOOSE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 296SW 120325 ENGINE PANEL ON TOP WAS NOT SECURE. RETURNED TO FAT. INSPECTED AREA AROUND ENGINE COWL ACCESS PANEL AND OBSERVED NO DA MAGE. SECURED PANEL. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300151 19990903 00151 1999 9 3 SWIA971543 4 19990808 A 3416 ALTIMETER EMB 120 EMB120RT SO PWA 118 PW118 NE LT COCKPIT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 1110J 120110 CAPTAINS ALTIMETER FAILED CLIMBING THROUGH 13,100. OFF FLAG DISPLAYED. RETURNED TO SEA. REMOVED AND REPLACED CAPTAIN' S ALTIMETER IAW MM 34-12-03. CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300152 19990903 00152 SO 1999 9 3 SWIA971544 1 19990801 A 2133 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN INOP A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 198SW 120227 CLIMBING THROUGH 13,000 FEET CABIN SPIKED TO 10000 FT. FOLLOWED QUICK REFERENCE HANDBOOK AND WAS ABLE TO REGAIN CONTROL WITH MANUAL CONTROLLER. RETURNED TO SLC. REMOVED AND REPLACED ELECTRO PNEUMATIC OUTFLOW VALVE PER MM 21-30-04. RAN A IRCRAFT PRESSURIZATION SYSTEM PER 21-30-00. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300153 19990903 00153 SO 1999 9 3 SWIA971545 1 19990801 A 7931 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 ON CLIMB-OUT OF SLC, HAD AURAL WARNING AND MAP INDICATION OIL PRESS 20. RETURNED TO SLC. OIL PRESSURE GAUGE REMAINED I N GREEN AT ALL TIMES. ADDED 2 QUARTS OIL TO THE RIGHT ENGINE AND REPLACED LOW OIL PRESSURE SWITCH. GROUND RAN AIRCRAFT FOR 15 MINUTES. OPS CHECKS GOOD WITH NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300154 19990903 00154 SO 1999 9 3 SWIA971546 1 19990801 A 2612 FIRE DETECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 199SW 120237 LEFT ENGINE FIRE DETECTOR/WHEEL WELL LIGHT CAME ON IN FLIGHT. DIVERTED FROM EKO TO SLC. REPLACED LEFT ENGINE FIRE DETE CTOR. FIRE DETECTION TEST GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300155 19990903 00155 NM 1999 9 3 SWAA991424 1 19990826 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM ROW 17 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 363SW 26574 EEPLS COVER AT ROW 17 LOOSE. RESECURED COVER PER MM. 2 L 7 2 4F RT A16WE 1999090300156 19990903 00156 NM 1999 9 3 SWAA991425 1 19990825 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP BY OVERWING EXITS. RECONNECTED WIRE PER MM. 2 L 7 2 4F RT A16WE 1999090300157 19990903 00157 NM 1999 9 3 SWAA991426 1 19990825 A 3350 07912 COVER BOEING 737 7373A4 1384585 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED BC1 CHECK, FOUND EEPLS COVER DAMAGED AT FWD SECTION AND MISSING AT CENTER SECTION. REPLACED BOTH COVER S PER MM. 2 L 7 2 4F RT A16WE 1999090300158 19990903 00158 NM 1999 9 3 SWAA991427 1 19990825 A 5320 6546534 SHEAR TIE BOEING 737 7373T5 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND BS 520 SHEAR TIE CRACKED, STRINGER 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 1999090300159 19990903 00159 NM 1999 9 3 SWAA991428 1 19990826 A 5320 6545409245 WEB BOEING 737 737317 138447P NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND BS 663 PRESSURE WEB CRACKED, LBL 32. REPAIRED PER SWA RA NR 1-353-2150. 2 L 7 2 4F RT A16WE 1999090300160 19990903 00160 NM 1999 9 3 SWAA991429 1 19990825 A 3150 32EN614 SWITCH BOEING 737 7373Y0 1384671 NM STAB TRIM MALFUNCTIONED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 308SA 23498 ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. ALL SYSTEMS AND FLIGHT CONTROL POSITIONS NORMAL. CLEANED STAB TRIM POSI TION SWITCH, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999090300161 19990903 00161 NM 1999 9 3 SWAA991430 1 19990825 A 3150 32EN614 SWITCH BOEING 737 7373Y0 1384671 NM STAB TRIM MALFUNCTIONED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 308SA 23498 ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. CYCLED SPEED BRAKE HANDLE AND WARNING HORN SILENCED. REMOVED AND REPLAC ED LOWER STAB TAKEOFF WARNING SWITCH PER MM. 2 L 7 2 4F RT A16WE 1999090300162 19990903 00162 NM 1999 9 3 SWAA991431 1 19990826 A 2520 417N3100114 PSU BOEING 737 7373H4 1384600 NM ROW 18 DEF DEPLOYED A SWAA A G UNSCHED LANDING O2 MASK DEPLOYED O OTHER CR CRUISE 1 SW 07 687SW 23388 DIVERTION, DURING CRUISE, PAX O2 MASKS DEPLOYED AT ROW 18 DEF (DIVERTION FROM LAX). DEFERRED PER MEL AND LATER AT HOU. REMOVED AND REPLACED PSU PER MM. 2 L 7 2 4F RT A16WE 1999090300163 19990903 00163 NM 1999 9 3 SWAA991420 1 19990826 A 5315 6546804 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND BS 1016 FLOORBEAM CORRODED, LBL 28.5-33.5. REPAIRED BEAM PER ER NR 99-5770. 2 L 7 2 4F A16WE 1999090300164 19990903 00164 NM 1999 9 3 SWAA991421 1 19990825 A 5320 6546534 SHEAR TIE BOEING 737 7372T4 1384492 NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND BS 520 SHEAR TIE CORRODED AT STRINGER 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999090300165 19990903 00165 NM 1999 9 3 SWAA991422 1 19990826 A 5320 6546567 SHEAR TIE BOEING 737 7372T4 1384492 NM BS 1040 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND BS 1040 SHEAR TIE CRACKED AT STRINGER 13R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999090300166 19990903 00166 NM 1999 9 3 SWAA991423 1 19990826 A 5311 6546536 FRAME BOEING 737 7372H4 138448C NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C3 CHECK, FOUND BELT FRAME CRACKED, BS 639, STRINGER 71R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F A16WE 1999090300167 19990903 00167 NM 1999 9 3 SWAA991417 1 19990824 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 830 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 830, STRINGER 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999090300168 19990903 00168 NM 1999 9 3 SWAA991418 1 19990824 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999090300169 19990903 00169 NM 1999 9 3 SWAA991419 1 19990824 A 7930 21SN04226A SWITCH BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE MALFUNCTIONED A SWAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SW 07 655WN 28400 721146 ENG INFLIGHT SHUT DOWN, NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENG OIL FILTER BYPASS S WITCH AND FILTER PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999090300170 19990903 00170 NM 1999 9 3 SWAA991409 1 19990825 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED, BS 767, STRINGER 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999090300171 19990903 00171 NM 1999 9 3 SWAA991410 1 19990824 A 5320 6545409 WEB BOEING 737 737317 138447P NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND BS 663 BEADED PRESS WEB CRACKED, LBL 30. REPAIRED WEB PER SWA RA NR 1-353-2150. 2 L 7 2 4F RT A16WE 1999090300172 19990903 00172 NM 1999 9 3 SWAA991411 1 19990824 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 619SW 28035 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS MISSING TRACK COVER AT OVERWING EXIT ROW. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999090300173 19990903 00173 NM 1999 9 3 SWAA991412 1 19990824 A 5311 6546546 FRAME BOEING 737 7372T4 1384492 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 767, LBL 69, WL 236. REPAIRED FRAME PER MM. 2 L 7 2 4F A16WE 1999090300174 19990903 00174 NM 1999 9 3 SWAA991413 1 19990824 A 5320 6558280 SHEAR TIE BOEING 737 7372T4 1384492 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED, BS 360, BELOW STRINGER 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999090300175 19990903 00175 NM 1999 9 3 SWAA991414 1 19990824 A 5315 6546804 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM LOWER SURFACE, BS 794, RBL 64. REPAIRED BEAM PER SRM. 2 L 7 2 4F A16WE 1999090300176 19990903 00176 NM 1999 9 3 SWAA991415 1 19990824 A 5320 BAC1490 CREASE BEAM BOEING 737 7372T4 1384492 NM BS 812 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CORRODED CREASE BEAM, BS 812, RBL 64. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F A16WE 1999090300177 19990903 00177 NM 1999 9 3 SWAA991416 1 19990824 A 5532 6552191 SKIN BOEING 737 7372T4 1384492 NM VERT STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND LT SIDE OF VERTICAL STAB SKIN CRACKED, STA 91, JUST AFT OF FRONT SPAR. REPAIRED SKIN PE R SRM. 2 L 7 2 4F A16WE 1999090300178 19990903 00178 NE 1999 9 3 SWAA991400 2 19990823 A 7261 335261002 OIL SYST BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE CONTAMINATED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 653SW 28398 721116 AIR TURNBACK, DURING CLIMB, NR 2 ENGINE OIL QTY WENT TO ZERO AND OIL PRESS DROPPED TO 20 PSI. REMOVED AND REPLACED NR 2 ENG OIL SUPPLY FILTER AND SCAVANGE FILTER, NO CONTAMINATION ON FILTERS. FOUND POLYMIDE MATERIAL IN FWD SCAVANGE OIL SU MP. REMOVED MATERIAL, DRAINED, FLUSHED AND SERVICED SYSTEM PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999090300179 19990903 00179 1999 9 3 SWAA991401 4 19990823 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 AFT ENTRY DOOR EVACUATION SLIDE PRESS GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999090300180 19990903 00180 NM 1999 9 3 SWAA991402 1 19990823 A 5242 6522216 DOOR BOEING 737 7372H4 138448C NM E & E COMPT AJAR A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 071SW 22358 AIR TURNBACK, NO CONTROL OF CABIN PRESSURE, FWD AIRFLOW VALVE STAYS OPEN AND CAN NOT CONTROL. FOUND E/E DOOR AJAR DUE T O SWITCH INOP, REPAIRED PER MM. OPS CHECK GOOD. 2 L 7 2 4F A16WE 1999090300181 19990903 00181 NM 1999 9 3 SWAA991403 1 19990822 A 5220 65C35006 STOPS BOEING 737 737317 138447P NM EMER EXIT DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND RT EMERGENCY OVERWING EXIT DOOR LOWER STOPS CRACKED. REMOVED AND REPLACED STOPS PER MM. 2 L 7 2 4F RT A16WE 1999090300182 19990903 00182 NM 1999 9 3 SWAA991404 1 19990823 A 3350 07912 COVER BOEING 737 7372H4 138448C NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED C3 CHECK, FOUND EEPLS AFT END CAP MISSING. INSTALLED END CAP PER MM. 2 L 7 2 4F A16WE 1999090300183 19990903 00183 NM 1999 9 3 SWAA991405 1 19990823 A 5315 6546804 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/2D CHECK, FOUND BS 328, RBL 0-49 CABIN FLOORBEAM CORRODED ON UPPER FLANGE. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999090300184 19990903 00184 NM 1999 9 3 SWAA991406 1 19990823 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUT OUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999090300185 19990903 00185 NM 1999 9 3 SWAA991407 1 19990823 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED 1/4D CHECK, UT INSPECTION INDICATES 5 EACH CRACKS ON BS 178 BULK HEAD, RBL 5 - LBL 57. REPAIRED BULKHE AD PER SRM. 2 L 7 2 4F RT A16WE 1999090300186 19990903 00186 NM 1999 9 3 SWAA991408 1 19990822 A 5330 6550570 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR UPPER AND LOWER HINGE CUT OUTS ON FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM AND SWA RA NR 1-253-2147. 2 L 7 2 4F A16WE 1999090300187 19990903 00187 NM 1999 9 3 SWAA991390 1 19990822 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 EEPLS LIGHT ASSY OUT OF TRACK IN MID CABIN. REPOSITIONED LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999090300188 19990903 00188 NM 1999 9 3 SWAA991391 1 19990821 A 5240 6545849 MECHANISM BOEING 737 7373H4 1384600 NM SERVICE DOOR NOT LOCKED A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 675AA 23253 AIR TURNBACK, AFT SERVICE DOOR LIGHT ILLUMINATED DURING CLIMB (DOOR HANDLE WOULD NOT LOCK DOWN). ADJUSTED AND TESTED A FT SERVICE DOOR PER MM. 2 L 7 2 4F RT A16WE 1999090300189 19990903 00189 NM 1999 9 3 SWAA991392 1 19990820 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 FWD SERVICE DOOR EVACUATION SLIDE PRESS GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999090300190 19990903 00190 NM 1999 9 3 SWAA991393 1 19990820 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 363SW 26574 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999090300191 19990903 00191 NM 1999 9 3 SWAA991394 1 19990820 A 5311 6546532 FRAME BOEING 737 7373Y0 1384671 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/2D CHECK, FOUND BS 500, LBL 0.5 BELLY FUSELAGE FRAME CRACKED. REPAIRED FRAME PER ER NR 99-5902. 2 L 7 2 4F RT A16WE 1999090300192 20020702 00192 NM 2002 7 2 SWAA991395 1 19990820 A 5330 6552880 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED, ON AFT ENTRY DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER ER N R 99-5917. 2 L 7 2 4F RT A16WE 1999090300193 19990903 00193 NM 1999 9 3 SWAA991396 1 19990820 A 5753 6546435 SKIN BOEING 737 7373Q8 1384670 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E FLAP INBOARD EDGE DELAMINATED. REMOVED AND REPLACED FLAP ASSY P ER MM. 2 L 7 2 4F RT A16WE 1999090300194 19990903 00194 NM 1999 9 3 SWAA991397 1 19990820 A 5312 6516300 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND THROUGH HFEC INSPECTON A 1.5 INCH LONG CRACK ON BS 178 BULKHEAD AFT SIDE, RBL1. REPA IRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999090300195 19990903 00195 NM 1999 9 3 SWAA991398 1 19990821 A 5330 6552988 SKIN BOEING 737 7372T4 1384492 NM BS 970 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 970, BETWEEN STRINGERS 22L-23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999090300196 19990903 00196 NM 1999 9 3 SWAA991399 1 19990822 A 5320 6545409 WEB BOEING 737 7372H4 138448C NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED C3 CHECK, FOUND BS 663 PRESSURE WEB CRACKED, RBL 39.5. REPAIRED WEB PER SWA RA NR 1-253-2149. 2 L 7 2 4F A16WE 1999090300200 19990903 00200 CE 1999 9 3 99ZZZX3158 1 19990721 A 3210 MLG BEECH 58 58 1152740 CE BELLY MALFUNCTIONED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 6273K TH1369 DSM - GEAR WILL NOT RETRACT ALL THE WAY. MAINTENANCE JACKED AIRCRAFT, CYCLED GEAR MANY TIMES, COULD NOT DUPLICATE PROBL EM. RETURNED TO SERVICE. 1 L 7 2 3O 3A16 1999090300223 19990903 00223 CE 1999 9 3 99ZZZX3181 1 19990802 A 5740 AN825A BOLT CESSNA 182 182S 2072701 CE LT/RT WING MISINSTALLED A A FK9A K NONE O OTHER IN INSP/MAINT 1 NM 07 9539P 18280186 FOUND LEFT AND RIGHT UPPER WING STRUT ATTACH BOLTS INSTALLED BACKWARDS FACING AFT TO FORWARD. IPC SHOWS BOLTS INSTALLED FORE TO AFT. 1 H 7 1 3O NT 3A13 1999090300229 19990903 00229 EA 1999 9 3 99ZZZX3187 1 19990702 A 5330 C6F524161 PANEL DHAV DHC6 DHC6300 2802606 EA FUSELAGE CORRODED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 38535 033775 414 BIL - DISCOVERED CORROSION ON FORWARD, UPPER FUSELAGE PANEL. BONDED PANEL CONSTRUCTION, BLASA WOOD CORE. RIVETED TO ST RINGERS AND FRAMES. PANEL REQUIRED REPLACEMENT. MOISTURE PENETRATED CORE. REF: NR 221355. WAR NR 124679. 1 H 7 2 3T RT A9EA 1999090300230 19990903 00230 CE 1999 9 3 99ZZZX3188 1 19990701 A 2120 AIR DISTRIBUTION CESSNA 208 208B 2073701 CE COCKPIT ODOR A HSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 796FE 208B0212 GFK/BIS, FLT 8563 - EN ROUTE PILOT DETECTED FAINT SMELL OF SMOKE FROM AN ELECTRICAL SOURCE. NO CIRCUIT BREAKERS OPENED , NO EQUIPMENT OR SYSTEM FAILURES. ALL NON-ESSENTIAL ELECTRIC POWER WAS SECURED. AIRCRAFT LANDED WITHOUT INCIDENT. CR ASH, FIRE AND RESCUE MET AIRCRAFT AT RUNWAY. NO CAUSE OF PROBLEM/SOURCE OF SMOKE SMELL IDENTIFIED. AIRCRAFT WAS INSPEC TED, GROUND RUN-UP AND ALL SYSTEMS CHECKED WITH NO DEFECTS NOTED. A TEST FLIGHT PERFORMED WITH NO DEFECTS NOTED. NO FU RTHER SMELL OF SMOKE. AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T A37CE 1999090300239 19990903 00239 WP 1999 9 3 CA990603021 1 19990509 A 5280 591016199 PLATE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE MLG DOOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA P657261D (CAN) ON WALK-AROUND, FOUND SEVERAL SLICES ON SIDEWALL NR 4 TIRE. FOUND LOOSE SCREWS ON RIGHT MLG DOOR PLATE, SCREW RE COUNTERSUNK AND INSTALLED USING LOCKTIGHT. 2 L 7 2 4F 4 F A6WE E2EA 1999090300240 19990903 00240 NM 1999 9 3 CA990603022 1 19990509 A 2751 INDICATOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE TE FLAP FAILED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA P709651 (CAN) TRAILING EDGE FLAPS DISAGREE MESSAGE CAME ON WHEN ATTEMPTING TO SELECT FLAPS AT 25 DEGREES, LANDING ACCOMPLISHED U SING 20 DEGREE FLAPS. FLAP POSITION INDICATOR AND K353 AND K216 RELAYS REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300241 19990903 00241 NM 1999 9 3 CA990603023 1 19990518 A 2720 YAW DAMPER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE RUDDER FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA P709698 (CAN) LEFT YAW DAMPER EICAC MESSAGE DISPLAYED AFTER PUSHBACK, YAW PANEL AND LEFT YAW DAMPER SERVO REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300242 19990903 00242 NM 1999 9 3 CA990603024 1 19990406 A 5230 SKIN BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE PAX DOOR DAMAGED W O OTHER O OTHER LD LANDING 1 CA P709635 (CAN) LIGHTNING STRIKE ON ARRIVAL, DAMAGE FORWARD OF R1 DOOR AND STATIC WICK MISSING. REPAIRED DAMAGE AND REPLACED WIC K. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300243 19990903 00243 NM 1999 9 3 CA990603026 1 19990518 A 2910 CAP BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE HYDRAULIC SYSTEM LOOSE W O OTHER K FLUID LOSS CL CLIMB 1 CA P709699 (CAN) LOST C-HYDRAULIC SYSTEM IN CLIMB-OUT. FOUND PLUG CAP LOOSE AT LEFT INBOARD AILERON INBOARD POWER CONTROL UNIT. P LUG TIGHTENED, SYSTEM SERVICED, AND LEAK CHECK CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300244 19990903 00244 WP 1999 9 3 CA990603027 1 19990518 A 2131 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P657537D (CAN) UNABLE TO PRESSURIZE CABIN DURING TAKEOFF. CLIMBED TO 7,000 FEET, BUT CABIN PRESSURE WAS UNCONTROLLABLE IN AUTOMA TIC MODE, MANUAL CONTROL NOT TRIED. BOTH NR 1 AND NR 2 CONTROLLERS REPLACED AND AIRCRAFT CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1999090300245 19990903 00245 NM 1999 9 3 CA990603034 1 19990520 A 2420 915F3126 GCU BOEING 737 7372E1 138448F NM PWA JT8 JT8D9A 52048 NE NR 2 GENERATOR FAILED W C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 CA UN428 687752 (CAN) NR 2 GENERATOR CAME OFF-LINE DURING TAKEOFF. TAKEOFF ABORTED AT 70 KNOTS. NR 2 GENERATOR CONTROL UNIT REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999090300246 19990903 00246 NM 1999 9 3 CA990614016 1 19990527 A 2610 894093 FIRE LOOP BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE NR 1 ENGINE FAULTY W F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 CA 48982 709491 (CAN) ON APPROACH , NR 1 FIRE WARNING ON, BOTH FIRE BOTTLES DISCHARGED, NR 1 ENGINE CHECKED, NO INDICATION OF FIRE, NR 1 ENGINE LOWER FIRE DETECTOR AT FAULT, DETECTOR SHORTED. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999090300248 19990903 00248 NM 1999 9 3 CA990614046 1 19990109 A 2530 3510001601 WIRE BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE COFFEE MAKER BURNED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 0476 30743 (CAN) AFT GALLEY CREW REPORTED SMOKE FROM OUTBOARD COFFEE MAKER. COFFEE MAKER REPLACED DUE TO BURNED WIRES. 2 L 7 2 4F 4 F RT A2NM E12EU 1999090300250 19990903 00250 NM 1999 9 3 CA990614063 1 19990422 A 5311 65956002598 FRAME BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE BS 1080 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 67550 688128 (CAN) CARGO CONVERSION STC REVEALED CORRODED FITTING AT STN 11835STR20L, CRACK AT R1 DOOR AFT UPPER CORNER, CORRODED FRA ME AT RT FUSELAGE STATION 1070 STR 12R, CRACKED FRAME AT LT FUSELAGE STATION 1070 UPPER STOP, CORRODED REINFORCEMENT STR AP AT LT FUSELAGE STATIONS 1070 TO 1080, AND CORRODED AND CRACKS AT CENTER OF S-DUCT - REPAIRED. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300254 19990903 00254 NM 1999 9 3 CA990614067 1 19990509 A 2781 H1010261 SWITCH BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE LE FLAP FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA 3655 (CAN) NR 1 LE FLAP AMBER LIGHT STAYS ON AFTER LE EXTENDED. NR 1 LE FLAP POSITION SW S20Z US, REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300255 19990903 00255 EU 1999 9 3 CA990614069 1 19990524 A 2550 1231003 PDU AIRBUS 330 A330202 3930316 EU CARGO BAY FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) CARGO PDU FOUND SMOKING. UNIT REPLACED. UNITS ARE MADE BY TELAIRE. SEE TELAI RE SIL 25-100. SEE AIRBUS SB A330 -25-3108. 2 L 7 2 4F RT A46NM 1999090300257 19990903 00257 WP 1999 9 3 CA990614076 1 19990117 A 3213 AXLE LKHEED LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE MLG LEAKING W O OTHER Z G SIGNIFICANT FAILURE REPORT MULTIPLE FAILURE LD LANDING 1 CA 10114 (CAN) AFTER HARD LANDING, FOUND AFT DRAIN MAST SEPARATED FROM FUSE ENG 2. APU FUEL SHROUD BENT, AFT BODY SHROUD AND VHF 3 BENT TAIL SKID AT 150 PSI, FLAT SPOT ON SHOE AND LOCKWIRE BROKEN. ALSO FOUND LT REAR AXLE OF MAIN LANDING GEAR WITH GREASE OUT AND A FUEL LEAK STATIC ON NR 3 ENGINE. TEMPORARY REPAIR FOR FERRY FLIGHT FOR PERMANENT REPAIR. 2 L 7 3 4F 4 F A23WE E12EU 1999090300258 19990903 00258 NM 1999 9 3 CA990614081 1 19990615 A 2710 ACTUATOR BOEING 747 747433 NM PWA 4056 PW4056 NE AILERON FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA P724315 (CAN) AILERON LOCK-OUT ON EICAS STATUS REPORT. LEFT AILERON ACTUATOR REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 1999090300259 19990903 00259 NM 1999 9 3 CA990614082 1 19990601 A 2841 FQIC BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE LT FUEL CELL FAULTY W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA P709662 (CAN) AFTER FLIGHT LEVEL, FUEL CONFIGURATION EICAS MESSAGE ON. FUEL QTYS LT MAIN 8.6 AND RT MAIN 16.9. CROSS-FEEDING S TARTED AND RETURNED TO BLOCKS. CARRIED OUT BIT TEST ON FUEL QTY INDICATION COMPUTER AND SHOWS A7 FAULT. FQIC REPLACED. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300260 19990903 00260 WP 1999 9 3 CA990614086 1 19990524 A 2421 GENERATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA P653878D (CAN) IN CRUISE LT AC BUS LIGHT, GENERATOR OFF LIGHT, AC BUS LIGHT AND AC CROSS-TIE LIGHT ON. AIRCRAFT GROUND RUN CROS S-TIE CHECK TRIED, LOCK-OUT LIGHT ON, GENERATOR WOULD NOT COME ON LINE AND AC CROSS-TIE LOCKOUT LIGHT STAYED ON. AUDIB LE CLACKING FROM OVERHEAD HEARD BEFORE GENERATOR FELL OFF-LINE. APU AND LT ENGINE VOLTAGE REG INTERCHANGED, NO FIX. RE PLACED LT GENERATOR. 2 L 7 2 4F 4 F A6WE E2EA 1999090300261 19990903 00261 NM 1999 9 3 CA990614090 1 19990524 A 2572 S14 SWITCH BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE ICAS OVERHEATED W D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 CA P709635 (CAN) DURING FLT EQUIPMENT COOLING OVERHEAT ON IN ICAS, STANDBY SELECTED AND UNABLE TO CLEAR FAULT, OVERRIDE SELECTED AN D FAULT CLEARED. SYSTEM RESET ANDS AME FAULTS. REPLACED OVERHEAT SWITCH S14 AND FLOW DETECTOR TS/04 IN FORWARD CARGO. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300262 19990903 00262 NM 1999 9 3 CA990614091 1 19990523 A 2121 FAN BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE AIR DISTRIBUTION OVERHEATED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA P709633 (CAN) FORWARD EXHAUST EQUIPMENT COOLING FAN CIRCUIT BREAKER TRIPPED IN-FLIGHT, STRONG ELECTRICAL SMELL, SUBSIDED ONE MIN UTE AFTER CIRCUIT BREAKER TRIPPED. REPLACED FORWARD EXHAUST FAN AND GROUND RUN SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300263 19990903 00263 WP 1999 9 3 CA990614092 1 19990520 A 2530 RECEPTICAL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA P657261D (CAN) ON GROUND, MSY CIRCUIT BREAKER FOR NR 1 GALLEY POSITION OVEN FOUND TRIPPED, WHEN RESET, CIRCUIT BREAKER TRIPPED AN D VISABLE ARCING FROM OUTLET. OUTLET REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1999090300264 19990903 00264 NM 1999 9 3 CA990630006 1 19990527 A 3233 65178194 ACTUATOR BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE MLG CRACKED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 2 DA714 666036 (CAN) ON GEAR RETRACTION AFTER TAKEOFF, RT MLG RED LIGHT CAME ON AND REMAINED ON. MANUAL EXTENSION CARRIED OUT AND AC LANDED OK. FOUND RT MLG UPLOCK ACTUATOR ATTACHMENT C RACRACKED OFF. REPLACED, EXTENSION CARRIED OUT SERVICEABLE. 2 L 7 3 4F 4 F A3WE E2EA 1999090300265 19990903 00265 NM 1999 9 3 CA990630048 1 19990601 A 3510 11442729 O2 MASK BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 33624XX 688128 (CAN) FIRST OFFICER'S OXYGEN MASK WILL NOT ALLOW OCCUPANT TO EXHALE THROUGH THE MASK. MASK REMOVED AND REPAIRED PER MM AND REINSTALLED. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300267 19990903 00267 NM 1999 9 3 CA990630050 1 19990609 A 2611 774001 SMOKE DETECTOR BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE CARGO BAY FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 4347 688128 (CAN) NR 2 SMOKE DETECTOR, MAIN DECK CARGO, LIGHT FLICKERS AND DOES NOT TEST. REPLACED WHITTIER SMOKE DETECTOR. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300268 19990903 00268 NM 1999 9 3 CA990630052 1 19990611 A 3240 VALVE BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE BRAKE MALFUNCTIONED W K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA (CAN) RIGHT BRAKE PEDAL DEPRESSED CAUSES AIRCRAFT TO SHUDDER. ANTI-SKID ON OR OFF. NR 3 AND NR 4 BRAKE BOOSTER VALVE S BLED AND CHECKED SERVICEABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300275 19990903 00275 NM 1999 9 3 CA990707023 1 19990621 A 2750 113T13698 FITTING BOEING 767 767375 NM TE FLAP BROKE W K NONE O OTHER IN INSP/MAINT 1 CA 24371 (CAN) RT TRAILING EDGE FLAP OUTER DEFLECTION CONTROL TRACK SUPPORT FITTING BROKEN AT BOTTOM LUG. REPLACED. 2 L 7 2 4F RT A1NM 1999090300276 19990903 00276 NM 1999 9 3 CA990707024 1 19990609 A 2612 894093 FIRE DETECTOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE NR 1 ENGINE FAILED W E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 709479 (CAN) ON CLIMB-OUT, NR 1 ENGINE OVERHEAT WARNING ILLUMINATED. ENGINE SHUT DOWN, BOTH FIRE BOTTLES DISCHARGED. LIGHT ST ILL ON. AIRCRAFT DIVERTED. REPLACED NR 1 ENGINE LOWER FIRE DETECTOR. 2 L 7 2 4F 4 F A16WE E2EA 1999090300277 19990903 00277 NM 1999 9 3 CA990707025 1 19990611 A 2913 O-RING BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE HYDRAULIC PUMP DAMAGED W O OTHER K FLUID LOSS AP APPROACH 1 CA 687708 (CAN) ON LANDING, FLAPS SELECTED, 1 UNIT LOST A-SYSTEM HYDRAULIC PRESSURE. COMPLETED LANDING. O-RING AT NR 2 ENGINE H YDRAULIC PUMP RIPPLE DAMPER LEAKING. O-RING REPLACED, A/C SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1999090300278 19990903 00278 NM 1999 9 3 CA990707028 1 19990624 A 5230 6546921528 FRAME 6546921528 BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE CARGO DOOR CRACKED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 51380 567 709397 (CAN) FORWARD OUTFLOW VALVE CLOSED, LIGHT ON. AIRFLOW IN CABIN POOR AT CRUISE. DUCT PRESSURE 22 PSI AT 33,000 FEET. FO UND CABIN PRESSURE RELIEF VALVES LEAKING, SEALS ADRIFT, AFT LT/RT CABIN DOORS UPPER GATE SEALS ADRIFT, FORWARD CARGO DO OR FOUND TO HAVE A 10 INCH CRACK IN LOWER AFT CORNER. SEALS REPLACED AND DOOR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999090300279 19990903 00279 NM 1999 9 3 CA990707029 1 19990629 A 2421 976J4981 GENERATOR BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED W A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 CA 35421 4670 687708 (CAN) APPROXIMATELY 8 MINUTES AFTER DEPARTURE, HEARD SEVERAL CIRCUIT BREAKERS TRIP, RESET NR 1 TRU CB, IT TRIPPED AGAIN. 1 MINUTE LATER, LT FORWARD AND RT FORWARD FUEL BOOST PUMP CB'S TRIPPED. A/C RETURNED. AFTER LANDING, RT FORWARD FU EL BOOST PUMP CB TRIPPED. REPLACED NR 1 ENGINE GENERATOR. 2 L 7 2 4F 4 F A16WE E2EA 1999090300281 19990903 00281 WP 1999 9 3 CA990707061 1 19990608 A 5730 264 PANEL CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL AILERON LOOSE W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 501379 (CAN) SHORTLY AFTER TAKEOFF, THE CREW NOTICED A VIBRATION COMING FROM THE AILERONS AND TRANSMITTED THROUGH THE CONTROL W HEELS. SPEED REDUCED AND RETURNED TO BLOCKS. AILERON PANEL LOOSE, ATTACHED WITH WRONG SCREWS, ALL PANELS CHECKED FOR P ROPER SCREWS, SCREWS REPLACED. 2 L 7 2 4R 4 T 6A6 E282 1999090300282 19990903 00282 NM 1999 9 3 CA990707068 1 19990622 A 2121 6067723 FAN BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE AIR DISTRIBUTION SEIZED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 30819 (CAN) SMOKE WAS OBSERVED IN COCKPIT AND CABIN AND AT THE SAME TIME THE RT RECIRCULATION FAN LIGHT CAME ON. FAN SEIZED, REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999090300283 19990903 00283 NM 1999 9 3 CA990707069 1 19990630 A 3260 4346741033220 LENS BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE MLG INDICATOR BROKEN W O OTHER N FALSE WARNING LD LANDING 1 CA 30734 (CAN) ON APPROACH WHEN GEAR LOWERED, NO GREEN LIGHT FOR THE LT MLG, ALT GEAR LOWERING CARRIED OUT AND AC LANDED OK. LT GREEN LENS ASSY BROKEN. REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999090300284 19990903 00284 NM 1999 9 3 CA990707072 1 19990306 A 3320 BV031120333 LAMP HOLDER BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE ROW 37/38 SMOKE W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) DURING CLIMB AT 10,000 FEET, FLIGHT DIRECTOR TURNED ON THE CEILING LIGHTS TO FACILITATE CABIN SERVICE. PASSENGERS REPORTED AT ROWS 37 AND 38 ABC ADVISER, THE FLIGHT ATTENDANT SAID THAT SMOKE WAS COMING FROM OVERHEAD COMPARTMENT. FLI GHT ATTENDANT NOTICED SMOKE AND SPARKS COMING FROM WHERE THE NEON LIGHT CONNECTS TO THE SOCKET. LIGHTS TURNED OFF AND B ULB REMOVED. SOCKET REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999090300285 19990903 00285 NM 1999 9 3 CA990707074 1 19990619 A 7711 2299 TRU BOEING 737 7372E1 138448F NM PWA JT8 JT8D9A 52048 NE NR 2 EPR SHORTED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 665978 665978 (CAN) AIRCRAFT RETURNED TO GATE DUE TO NR 2 EPR INDICATOR STUCK AT 1.60 EPR. NR 2 EPD TRANSFORMER RECTIFIER WAS TRIPPI NG CIRCUIT BREAKER. HAD SMOKE IN AREA. REPLACED TRANSFORMER. 2 L 7 2 4F 4 F A16WE E2EA 1999090300286 19990903 00286 EU 1999 9 3 CA990715010 1 19990705 A 3230 200429232 DOWNLOCK ROTOL 200736001 FOKKER F28 F28MK1000 4990808 EU NLG OUT OF ADJUST W A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 CA DRG53568 (CAN) SHORTLY AFTER TAKEOFF WHEN THE GEAR SELECTED UP, THE NLG WOULD NOT RETRACT. AIRCRAFT RETURNED TO BLOCKS. THE LIN KAGE FOR THE NLG DOWNLOCK WAS IMPROPERLY INSTALLED. HAD BEEN REMOVED FOR LUBRICATION. PROPERLY INSTALLED AND GEAR SWIN GS SERVICEABLE. 2 L 7 2 4F RT A20EU 1999090300287 19990903 00287 NM 1999 9 3 CA990715016 1 19990622 A 2610 285N002821 WARNING LIGHT BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT ILLUMINATED W F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CA 30743 (CAN) DURING CRUISE AT 31,000 FEET ONE HOUR INTO FLIGHT, AFT CARGO FIRE LIGHT CAME ON. NO EICAS WARNING. FIRE BOTTLES DISCHARGED IAW QRH. AFLOTS CARD REPLACED. LOGIC CARD. 2 L 7 2 4F 4 F RT A2NM E12EU 1999090300289 19990903 00289 NM 1999 9 3 CA990715027 1 19990630 A 2612 APU BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE APU FAILED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 688128 (CAN) ON PRE-FLIGHT, APU FIRE DETECT WOULD NOT TEST, STATIC, WILL TEST INTERMITTENTLY WHEN RUNNING. CONNECTORS CLEANED AT SENSOR/RESPONDER AND OPS CHECKED OK. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300290 19990903 00290 NM 1999 9 3 CA990715028 1 19990617 A 2612 FIRE DETECTOR BOEING 727 72727C 138400J NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA 653499 (CAN) NR 2 FIRE DETECTION CIRCUIT GROUND LIGHT ON REAR CIRCUIT PANEL ON. REPOSITIONED TWO FIRE LOOP CLAMP GROMMETS ON THE NR 2 ENGINE, TEST SERVICEABLE. 2 L 7 3 4F 4 F A3WE E2EA 1999090300291 19990903 00291 1999 9 3 CA990715029 4 19990715 A 3416 B006381108 ALTIMETER BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 689961 (CAN) FIRST OFFICER'S ALTIMETER READS 100 FEET HIGHER THAN CAPTAIN'S ALT AT DECISION HEIGHT. FO'S ALTIMETER REPLACED AN D SERVICEABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300292 19990903 00292 WP 1999 9 3 CA990715036 1 19990625 A 2121 CONNECTOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AIR DISTRIBUTION LOOSE W O OTHER O OTHER CR CRUISE 1 CA P657239D (CAN) AT FL 330 AFTER SELECTION OF AIRFOIL ANTI-ICE TAIL ANTI-ICE WITH ENG ANTI-ICE ON, CABIN ALT CLIMBED TO 10,000 FEET . AIRFOIL ANT-ICE SELECTED OFF AND DESCENT INITIATED. AT 29,000 FEET,CABIN STARTED A 500 FOOT CLIMB RATE. FOUND DUCT CONNECTOR ADRIFT AT LT AIRCYCLE MACHINE DISCHARGE AFT SIDE OF HEAT EXCHANGER. CLAMP INSTALLED SYSTEM SERVICED. 2 L 7 2 4F 4 F A6WE E2EA 1999090300293 19990903 00293 NM 1999 9 3 CA990715038 1 19990628 A 3244 TIRE BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE MLG FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA P709694 (CAN) NR EIGHT MAIN WHEEL TIRE BLOWN ON LANDING. NR 7 AND NR 8 MAIN WHEEL ASSYS, ANTI-SKID CONTROL BOX, AUTO BRAKE CONT ROL BOX, AND ANTI-SKID MODULE REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300294 19990903 00294 WP 1999 9 3 CA990715040 1 19990701 A 2720 RUDDER PEDDLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P657261D (CAN) CAPTAIN'S RUDDER PEDAL ATTACH BRACKET CRACKED. FAA AD 89-14-02 REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1999090300295 19990903 00295 WP 1999 9 3 CA990715042 1 19990704 A 3020 THERMOVALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT ENGINE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA P656929D (CAN) ON TAKEOFF, TEMP 8C UNABLE TO ACHIEVE TAKEOFF EPR OF 1.99 ON RT ENGINE EPR 1.94 WITH RT THROTTLE FIRE WALLED. AL L OTHER PARAMETERS MATCHED. EPR PROBLEMS SEEM ASSOCIATED WITH USE OF ENGINE ANTI-ICE. RT NOSE COWL THERMOSTAT VALVE RE PLACED. EPR TP2 AND PT7 LINES BLOWN CLEAR. NOSE BULLET SEALS REPLACED. GROUND RUN SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1999090300296 19990903 00296 NM 1999 9 3 CA990719006 1 19990524 A 2520 C23PU696701 CASE 7441004 BOEING 747 747475 NM SEAT TELEPHONE DEFORMED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SEAT TELEPHONE BOXES 7 WIRE CORD REELS EXCESSIVELY HOT AND CASE DEFORMED. REFER TO ASB 6600-23-04. 2 L 7 4 4F RT A20WE 1999090300298 19990903 00298 WP 1999 9 3 CA990719031 1 19990604 A 2780 LINK DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE SPOILER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P654122D (CAN) LT INBOARD SPOILER PANEL LINK CRACKED AT LOWER OUTBOARD LUBE FITTING HOLE. SPOILER PANEL ALSO CRACKED. EDDY CURR ENT INSPECTION AD 85-01-03. REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1999090300299 19990903 00299 1999 9 3 CA990719032 4 19990609 A 3421 VERTICAL GYRO DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE COCKPIT FAILED W O OTHER O OTHER TO TAKEOFF 1 CA P657374D (CAN) FIRST OFFICER'S AUDIO DIRECTIONAL INDICATOR FAILED DURING TAKEOFF, GYRO FLAG IN VIEW. IT CAME ON LINE THEN DISPLA YED GYRO FLAG ON AND OFF SEVERAL TIMES. LAST TIME FOR 15 MINS. NR 2 VERTICAL GYRO REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1999090300300 19990903 00300 WP 1999 9 3 CA990719033 1 19990613 A 2120 CLAMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE AIR DISTRIBUTION MISINSTALLED W B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 CA P657724D (CAN) WHEN DESCENDING THROUGH FLIGHT LEVEL 330 AND CABIN ALTITUDE AT 10,000 FEET, MASTER WARNING CABIN PRESSURE ON FOLLO WED BY RAPID DEPRESSURIZATION. EMERGENCY DESCENT DRILL CARRIED OUT, CABIN DID NOT EXCEED 10,000 FEET, BUT WAS VERY SLO W TO COME DOWN, PACK PRESSURE VERY SLOW. FOUND ONE CLAMP OFF WATER SEPARATOR RT SYSTEM DUCT AND ONE CLAMP OFF LT AIR CY CLE MACHINE DUCT, CLAMPS INSTALLED AND SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1999090300301 19990903 00301 WP 1999 9 3 CA990719034 1 19990623 A 2710 BRACKET DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RUDDER PEDAL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P657716D (CAN) FIRST OFFICER'S RUDDER PEDAL ATTACH BRACKET CRACKED. REPLACED. REFER TO FAA AD 89-14-02. 2 L 7 2 4F 4 F A6WE E2EA 1999090300302 19990903 00302 1999 9 3 CA990719035 4 19990605 A 3417 COMPUTER BOEING 747 747433 NM PWA 4056 PW4056 NE AIR DATA FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA P724345 (CAN) JUST AFTER TAKEOFF, STICK SHAKER ACTIVATED FOR 3 SECONDS. CONTINUED TO FL 310, ALTIMETER DISAGREE AMBER MESSAGE O N EICAS. QUICK REF PROCEDURE RESULTED IN CAPTAIN'S ADI TO C AND FIRST OFFICER TO L, MESSAGE EXTINGUISHED. TRIED TO CONT INUE BUT ON CLIMB ABOVE FL 310, CONTINUOUS STICK SHAKER WITH NO EICAS OR STATUS MESSAGE. CAPTAIN'S AND FIRST OFFICER'S AIR DATA REPLACED. LEFT ANGLE OF ATTACK SENSOR REPLACED. LT AND RT STALL WARNING CARD REPLACED. FULL RANGE LEAK CHECK CARRIED OUT SERVICEABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 1999090300303 19990903 00303 1999 9 3 CA990719036 4 19990621 A 2565 SLIDE BOEING 767 767275 1385155 NM PWA JT9 JT9D7R4D 52054 NE LT WING DEPLOYED W O OTHER J WARNING INDICATION DE DESCENT 1 CA P709606 (CAN) ON APPROACH, LT WING SLIDE CAUTION WAS ANNUNCIATED, LIGHT WENT OUT AFTER SEVERAL SECONDS, SOME BUFFETING FELT, HAN DLING NORMAL. FLIGHT ATTENDANT REPORTED PASSENGER SAW PIECES OF AIRCRAFT FALL OFF. LT WING SLIDE ASSY, LATCH RELEASE, NITROGEN CYL AND SLIDE DOOR ACTUATORS REPLACED. DOOR LINK CABLES INSPECTED, SYSTEM ARMED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300304 19990903 00304 NM 1999 9 3 CA990719037 1 19990615 A 3211 FITTING BOEING 767 767275 1385155 NM PWA JT9 JT9D7R4D 52054 NE MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA P709606 (CAN) CORROSION FOUND ON THE BUSHING SEATS AND CHAMFERS OF THE RT AND LT MLG SIDE BRACE SWIVEL FITTINGS. CORROSION DETE CTED SPECIAL VISIT. REPAIRED IAW 6-57-40/351-57-0451. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300306 19990903 00306 NM 1999 9 3 CA990728020 1 19990708 A 2912 V-CLAMP BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE HYDRAULIC SYSTEM FAILED W H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 702661 (CAN) CREW REPORTED LOSS OF A-SYSTEM HYDRAULIC QUANTITY. BOTH ENGS LOW PRESSURE LIGHTS ON. TURNED ENG HYD PUMPS OFF WHE N LOW PRESSURE LIGHTS ON. FOUND A-SYSTEM FILTER HOUSING CLAMP FAILED. CLAMP, O-RING AND FILTER REPLACED. LEAK CHECK S ERVICED. 2 L 7 2 4F 4 F A16WE E2EA 1999090300307 19990903 00307 NM 1999 9 3 CA990728021 1 19990715 A 2820 COUPLING BOEING 747 747475 NM FUEL SYSTEM DISCONNECTED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 39427 (CAN) UNABLE TO TRANSFER FUEL FROM 4 MAIN TANK TO 3 MAIN FUEL TANK. FUEL DUMPED AND AC DIVERTED. FOUND RIGID COUPLING FOR 3 RESERVE TRANSFER FUEL LINE TO 3 MAIN TANK ADRIFT. LINE RECONNECTED WITH NEW O-RING, LEAK CHECK SERVICED. 2 L 7 4 4F RT A20WE 1999090300308 19990903 00308 NM 1999 9 3 CA990728022 1 19990720 A 2720 4030952902 YAW DAMPER SPERRY 4030952902 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE RUDDER FAILED W A H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA 40921 81111766 674313 (CAN) REPEAT SNAG OF YAW HARD OVER. AUTOPILOT WAS DISENGAGED, YAW DAMPER CENTERED, THEN YAW DAMPER DID ANOTHER HARD OVE R, REPLACED RUDDER PCU, REPLACED YAW DAMPER COUPLER. PREVIOUS YAW PROBLEMS A/P ENGAGED , A/C YAWED TO RIGHT, A/P DISENG AGED THEN RE-ENGAGED. AIRCRAFT YAWED TO RIGHT AGAIN. A/P OFF, YAW DAMPER SELECTED OFF, NO ADVERSE YAW MOVEMENT. YAW D AMPER COUPLER REPLACED. IN CRUISE A/P YAWED TO RIGHT, A/P SWITCHED OFF, NO FURTHER PROBLEMS. YAW DAMPER REPLACED. INF O SNAG, IN CRUISE REDUCED POWER, A/C YAWED TO RIGHT AND THEN KICKED BACK. A/P AND YD WERE ENGAGED. NO FURTHER PROBLEMS REMAINDER OF FLIGHT. YAW DAMPED CHECK CARRIED OUT. 2 L 7 2 4F 4 F A16WE E2EA 1999090300309 19990903 00309 NM 1999 9 3 CA990728023 1 19990722 A 2910 LINE BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE HYDRAULIC SYSTEM LOOSE W B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA 688478 (CAN) ON DESCENT AS POWER WAS REDUCED, A-SYSTEM PRESSURE FLICKERED THEN WENT TO ZERO, LOW PRESSURE LIGHTS ON. EMERGENCY DECLARED. LEFT ENGINE A-HYDRAULIC PUMP PRESSURIZED SYSTEM. LANDED OK. AFTER SHUT DOWN, AIRCRAFT TOWED TO GATE. FO UND HYDRAULIC TANK PRESSURE LINE FROM PRESSURE REGULATOR TO A-SYSTEM RESERVOIR ADRIFT. LINE SECURED ENG 1 AND 2 FILTER DRAINED, REPLACED. PRESSURE FILTERS REPLACED, LEAK CHECK CARRIED OUT. 2 L 7 2 4F 4 F A16WE E2EA 1999090300312 19990903 00312 1999 9 3 CA990728066 4 19990702 A 3416 WL1103AMMS10 ALTIMETER BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 688128 (CAN) CAPTAIN'S ALT FLUCTUATES BY UP TO 1,000 FEET IN CLIMB AND CRUISE. REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300314 19990903 00314 WP 1999 9 3 CA990804006 1 19990727 A 7722 8901218 CIT SENSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE FAILED W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 52928 26020 517982 (CAN) ON ROLLING TAKEOFF, NR 3 ENGINE APPEARED TO BE SLOW TO SPOOL AND HUNG AT 102 PERCENT. ENGINE FAIL LIGHT ILLUMINAT ED AND TAKEOFF ABORTED. BORESCOPE INSPECTION REVEALED NO FAULTS. REPLACED NR 3 ENGINE FUEL FILTER AND FUEL PUMP DEBRIS FILTER, ENGINE RUN OK. 2 L 7 3 4F 4 F A22WE E23EA 1999090300315 19990903 00315 WP 1999 9 3 CA990804007 1 19990729 A 2612 FIRE DETECTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE LOOSE W O OTHER N FALSE WARNING CL CLIMB 1 CA 455337 (CAN) LEVELING OUT AT 32,000 FEET, FIRE WARNING ACTIVATED FOR NR 3 ENGINE. ENGINE THROTTLED BACK TO IDLE AND FIRE WARNI NG WENT OUT. ALL ENGINE PARAMETERS OK. FOUND BIRD CAGE COOLING MANIFOLD ADRIFT ON NR 3 ENGINE REPAIRED. 2 L 7 3 4F 4 F A22WE E23EA 1999090300319 19990903 00319 EU 1999 9 3 CA990804011 1 19990801 A 3220 NLG ROTOL 200736001 FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NLG WW SHEARED W O OTHER O OTHER LD LANDING 1 CA DRG32169 9292 (CAN) AIRCRAFT SLID 200 FEET PAST END OF RUNWAY SHEARING OFF NLG AND DAMAGING LT WING LEADING EDGE WHEN IN CONTACT WITH LIGHT STANDARD. MORE TO FOLLOW. 2 L 7 2 4F 4 F RT A20EU E2EU 1999090300321 19990903 00321 NE 1999 9 3 CA990804014 2 19990715 A 7230 BLADE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 1 ENGINE BENT W K NONE O OTHER IN INSP/MAINT 1 CA 20026 5092 123021 (CAN) NR 1 ENGINE MAKING HUMMING NOISE AT HIGH POWER SETTINGS. BORESCOPE REVEALED BLOOD STAINS AND ONE OF THE LP BLADES WAS BENT. ENGINE SENT TO P&W. 2 H 7 2 4T 4 T RT A13NM E20NE 1999090300322 19990903 00322 NM 1999 9 3 CA990804038 1 19990722 A 2421 727792G IDG BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE DAMAGED W H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA A0707 30680 (CAN) 45 MINUTES AFTER DEPARTURE, THE LT GENERATOR CAME OFF LINE AND IDG LIGHT CAME ON, POWER GENERATION AND IDG DISCONN ECT CHECKLIST ACCOMPLISHED. NR 1 ENGINE IDG INTEGERATED DRIVE GENERATOR FOUND DAMAGED WITH CASING CRACKED AND LEAKING O IL, BOTH REPLACED. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F RT A2NM E12EU 1999090300324 19990903 00324 EA 1999 9 3 CA990804041 2 19990722 A 8530 LW10925 CYLINDER PARTEN P68 P68C 6780105 EU LYC O360 IO360A1B6 41514 EA ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA L2370951A (CAN) NR 4 CYLINDER COMPRESSION RING BROKEN. 1 H 7 2 3O 3 O A31EU 1E10 1999090300325 19990903 00325 NE 1999 9 3 CA990812002 2 19990727 A 7250 TURBINE VANES BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE TURBINE SECTION BENT W B EMER. DESCENT E VIBRATION/BUFFET TO TAKEOFF 1 CA 943 4572 LE07610 (CAN) THE ENGINE WAS ON ITS SECOND TBO EXTENSION WHEN IT EXPERIENCED A TURBINE FAILURE AT 240 HOURS TIME REMAINING. 1 G 7 1 4U 4 U H1SW E17EA 1999090300331 19990903 00331 NM 1999 9 3 CA990812013 1 19990713 A 2913 5718605 PUMP BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE HYDRAULIC SYSTEM OVERHEATED W O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 CA 80748 688128 (CAN) AFTER LANDING, B-SYSTEM HYDRAULIC OVERHEAT LIGHT ILLUMINATED, ISOLATED NR 2 B-PUMP. PUMP REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1999090300332 19990903 00332 1999 9 3 CA990812015 4 19990730 A 3454 285T05545 VOR PANEL BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE VOR SYSTEM OVERHEATED W A UNSCHED LANDING J WARNING INDICATION TX TAXI/GRND HDL 1 CA D00518 30743 (CAN) AFTER ENGINE START, VARIOUS ANNUNCIATOR LIGHTS ILLUMINATED, BATTERY OFF, APU BATTERY DISCHARGE, STANDBY POWER OFF, LT AND RT WING AND ENGINE. A/C DISAGREE. LT VOR/DME PANEL OVERHEATING, SAME REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999090300333 19990903 00333 NE 1999 9 3 CA990812035 2 19990717 A 7230 SENSOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE COMPRESSOR FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 731532 (CAN) NR 2 COMPRESSOR VANE ECAM STAYED ON FOR 20 MINUTES AFTER TAKEOFF. REPLACED VARIABLE BLEED VANE POSITION SENSOR. 2 L 7 2 4F 4 F RT A28NM E29NE 1999090300337 19990903 00337 GL 1999 9 3 CA990812046 1 19990723 A 7810 41200453 EDUCTOR ENSTRM F28 ENSTROM480 GL ALLSN 250C 250C20 03013 GL EXHAUST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE845007 (CAN) CRACKS WERE DISCOVERED WHEN 50 HR INSP C/O. 1 G 7 1 3O 3 U NC H1CE E4CE 1999090300338 19990903 00338 NM 1999 9 3 CA990817017 1 19990806 A 5312 BACB30MR5K6K BOLTS BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE BS 1016 LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 56957 708827 (CAN) DURING ROUTINE C-CHECK, FOUND SEVERAL PERIMETER BOLTS LOOSE AT THE AFT PRESSURE BULKHEAD TO FUSELAGE BUTT SPLICE S TN 1016. TORQUE CHECK OF ALL 225 BOLTS REVEALED 183 WERE LOOSE AND 11 BOLTS SHANKED. ALL BOLTS WERE REMOVED AND HOLES CHECKED FOR DAMAGE. TWO HOLES CORRODED AND ONE ELONGATED. ALL BOLTS REPLACED, CORROSION REMOVED AND OVERSIZED BOLTS IN STALLED IN REPAIRED HOLES. 2 L 7 2 4F 4 F A16WE E2EA 1999090300340 19990903 00340 NE 1999 9 3 CA990818007 2 19990818 A 8530 304149 STUD CNDAIR CL215 CL2151A10 EA PWA R2800 R2800CA 52026 NE CYLINDER SEPARATED W C ABORTED TAKEOFF A FLAME/FIRE TO TAKEOFF 1 CA 906 P32806 (CAN) TWO STUDS PN 304149 SEPARATED FROM REAR CYLINDER. EXHAUST MELTED THE PUSH ROD COVER CAUSING AN OIL LEAK AND SMALL FIRE. WARNING INDICATION IN COCKPIT RESULTED IN ABORTED TAKEOFF. NEW CYLINDER INSTALLED. 2 H 7 2 4R 4 R A14EA 5E8 1999090300341 19990903 00341 NM 1999 9 3 CA990818013 1 19990807 A 7930 FITTING BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE ENGINE OIL LEAKING W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA 666206 (CAN) O-RING FAILURE AT OIL PRESSURE TRANSMITTER TO MAIN OIL FILTER. 2 L 7 2 4F 4 F A16WE E2EA 1999090300342 19990903 00342 NE 1999 9 3 CA990818015 2 19990811 A 7261 VALVE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE OIL SYSTEM STICKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 120940 120940 881116 (CAN) ENGINE LOOSING OIL OUT BREATHER. RESULT WAS P3- P2.5 PRESSURE SWITCH STICKY IN P3 POSITION. VALVE DISASSEMBLED A ND CLEANED. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999090300357 19990903 00357 WP 1999 9 3 TWAA9911801 1 19990823 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN WORN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9630A 53561 THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 3 TO 6, ROWS 21 TO 24, AND ROW 30. REPLACED THE LIGHT STRIP AT EACH LO CATION, (P/N 0105606-005) FOR ROW 3 TO 6, AND (P/N 0105606-004) AT EACH OF THE OTHER TWO LOCATIONS. CHECK-C 5-6-99 STL . 2 L 7 2 4F RT A6WE 1999090300358 19990903 00358 WP 1999 9 3 TWAA9911802 1 19990827 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 DURING CHECK-C MAINT, LONGERON 2L WAS FOUND CRACKED AT THE END CAP STA 1076, ONE INCH LONG. REPAIRED PER SRM 53-02, FIG 8 AND 18. 2 L 7 2 4F A6WE 1999090300359 19990903 00359 WP 1999 9 3 TWAA9911803 1 19990827 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 DURING CHECK-C MAINT, LONGERON 2R WAS FOUND CRACKED AT END CAP STA 1076, A ONE INCH CRACK. REPAIRED PER SRM 53-02, FIG 8 AND 18. 2 L 7 2 4F A6WE 1999090300360 19990903 00360 WP 1999 9 3 TWAA9911804 1 19990820 A 5755 BUSHING DOUG DC9 DC983 3022083 WP TORQUE TUBE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9412W 53187 DURING CHECK-C MAINT FOUND THE LH SPOILER TORQUE TUBE BUSHINGS CORRODED. REPLACED THE CORRODED BUSHING PER MM 27-61-06 FOR INSTALLATION OF TORSION BAR. 2 L 7 2 4F RT A6WE 1999090300361 19990903 00361 WP 1999 9 3 TWAA9911805 1 19990818 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 313 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9412W 53187 DURING CHECK-C MAINT, FOUND A FUSELAGE EXTERNAL DENT IN THE SKIN AT LONGERON 25L, STA 313 APPROX .1875 IN DEEP BY 3.5 IN CHES LONG. REPAIRED DENT IN SKIN PER SRM 53-04, FIG 38 SHEET 22. 2 L 7 2 4F RT A6WE 1999090300362 19990903 00362 EU 1999 9 3 MALA976549 1 19990823 A 2612 SENSOR SAAB SF340 SF340A 7850100 EU CARGO COMPT DIRTY A MALA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 GL 15 68XJ 068 CARGO FIRE LIGHT ILLUMINATED AND CARGO FIRE EXTINGUISHED DEPLOYED. MAINTENANCE COULD NOT DUPLICATE PROBLEM. INSPECTED DETECTION AND ASSOCIATED WIRING, NO DISCREPANCIES NOTED. COMPLETED OPERATIONAL CHECK OF DETECTOR SYSTEM IAW SAAB MM 26- 13-00 & CLEANED PHOTO ELECTRIC SENSOR IAW SAAB MM 26-13-00. OPS CKECKS ARE GOOD. 2 L 7 2 4T RT A52EU 1999090300363 19990903 00363 NE 1999 9 3 MALA976550 2 19990827 A 7320 7086M60G11 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 991XJ 091 LEFT TORQUE GAUGE INOP, FAILED DURING CLIMB. MAINTENANCE REPLACED ECU PER CT7 MM 74-00-00 PAGES 406-410. COMPLETED OPS CHECKS PER CT7 72-00-00, TEST OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999090300364 19990903 00364 EU 1999 9 3 MALA976551 1 19990825 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A MALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 418XJ 418 CARGO SMOKE INDICATION DURING TAKEOFF, SELF EXTINGUISHED AFTER 5 SECONDS. MAINTENANCE CLEANED AND INSPECTED CARGO SMOKE DETECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999090300365 19990903 00365 EU 1999 9 3 MALA976552 1 19990823 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A MALA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 422XJ 422 CARGO SMOKE LIGHT ILLUMINATED, DID NOT GO OUT. LIGHT WAS ON STEADY FROM THE BEGINNING, COMPLETED MEMORY ITEMS AND AFTER BLOWING BOTTLE 1 LIGHT EXTINGUISHED. MAINTENANCE REPLACED NR 1 FIRE BOTTLE AND BOTH SMOKE DETECTORS, IAW SF340 MM 26-0 0-00. FUNCTIONAL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999090300366 19990903 00366 EU 1999 9 3 MALA976553 1 19990827 A 2435 STARTER GEN SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 425XJ 425 LEFT DC GEN LIGHT ILLUMINATED, RAN QRH, TRIED TO RESET, DIDN'T WORK, BUS TIE DID CLOSE. RETURNED TO MSP. MAINTENANCE R EPLACED LT DC STARTER/GEN (P/N 23080-031) (S/N 97077) & LT DC GCU (P/N 51539-007B) (S/N 97988) PER SF 340MM 24-31-10-2. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999090300367 19990903 00367 EU 1999 9 3 MALA976554 1 19990824 A 2430 M833830211 RCCB SAAB SF340 340B 7860101 EU E & E COMPT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 427XJ 427 LOST RIGHT SIDE VOR, COM, RADAR, AUTOPILOT, YAW DAMPER AND TACS IN FLIGHT. RETURNED TO DTW. MAINTENANCE REPLACED RCCB 499. ALL CHECKS GOOD IAW SF 340 MM CHAP 24. 2 L 7 2 4T RT A52EU 1999090300368 20000616 00368 NM 2000 6 16 CALA9901095 1 19990825 A 2820 BACC63BP22C39P7 GROMMET BOEING 737 737724 NM GE CFM56 CFM567B24 NE SPAR VALVE TORN A CALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 09 14731 28799 874863 THE #1 ENGINE FLAMED OUT WHILE CLIMBING THROUGH 24,000 FEET AFTER TAKEOFF FROM IAH. A RESTART WAS NOT ATTEMPTED DUE TO O IL QUANTITY INDICATIONS AT 86% AND THERE WAS NO OIL PRESSURE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT I NCIDENT. THE #1 ENGINE FUEL SPAR VALVE ACTUATOR WAS REPLACED. A VISUAL INSPECTION OF ALL CONNECTORS WAS PERFORMED WITH C HECKS FOR PROPER VOLTAGE AND GROUNDS. NO FAULTS WERE NOTED. IN ADDITION, THE #1 ENGINE CHIP DETECTORS AND OIL FILTER WER E VISUALLY INSPECTED WITH NO FAULTS NOTED. THE FUEL SPAR VALVE AND INDICATION OPERATED NORMALLY WITH NO FAULTS FOUND. A SUBSEQUENT ENGINE RUN WAS ACCOMPLISHED AND IT OPERATED NORMALLY. AN FCD IS BEING ISSUED TO INSPECT THE B737-700 & -800 F 2 L 7 2 4F 4 F RT A16WE E00055EN 1999090300369 19990903 00369 NM 1999 9 3 CALA9901096 1 19990827 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 985.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND FLOORBEAM CORRODED AT STA 985.5 FROM LBL 18 TO R-2 DOOR JAMB. REPAIRED IAW ECRA 5310-03906. 2 L 7 2 4F RT A16WE 1999090300370 19990903 00370 NM 1999 9 3 CALA9901097 1 19990827 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND RT AND LT AFT LAV FLOORBEAM CORRODED ON NUT PLATE HOLES AT STA 1016, RBL 0 TO RBL 50 AND LBL 0 TO LBL 4 0. REPAIRED IAW ECRA 5310-03906. 2 L 7 2 4F RT A16WE 1999090300371 19990903 00371 NM 1999 9 3 CALA9901098 1 19990827 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND MAIN FRAME CRACKED AT STA 616, S18L AND S18R. THE CRACKS WERE 1 AND .75 INCH LONG. DOUBLERS WERE INST ALLED IAW ECRA 5360-01024. 2 L 7 2 4F RT A16WE 1999090300372 19990903 00372 NM 1999 9 3 CALA9901099 1 19990829 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 0 TO WALL. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLE D IAW ECRA 5310-03893. 2 L 7 3 4F A3WE 1999090300373 19990903 00373 SO 1999 9 3 COMA9910140 1 19990824 A 5610 WINDSHIELD EMB 120 EMB120RT SO COCKPIT BIRD STRIKE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 SO 01 179CA 120179 BIRD STRIKE DURING TAKEOFF. C/W BIRD STRIKE INSPECTION, NO DAMAGE FOUND. 2 L 7 2 4T RT A31SO 1999090300374 19990903 00374 SO 1999 9 3 COMA9910141 1 19990825 A 3260 12038594001 BOX CONTROL EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 01 259CA 22016 11132 120252 LEFT HAND MLG DISAGREEMENT LIGHTS FLASHING DURING TAKEOFF. REPLACED THE LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1999090300375 19990903 00375 SO 1999 9 3 COMA9910142 1 19990828 A 5246 MECHANISM EMB 120 EMB120RT SO FUEL DOOR NOT LATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 264CA 120256 SERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN. SECURED FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1999090300376 19990903 00376 EA 1999 9 3 COMA9960470 1 19990826 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 995CA 4040 2804 7229 FLAPS FAILED MESSAGE. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999090300377 19990903 00377 EA 1999 9 3 COMA9960471 1 19990824 A 2150 PACK CNDAIR CL600 CL6002B19 EA LEFT MALFUNCTIONED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 709CA 7238 STRONG SULFURIC SMELL IN AIRCRAFT. DEFERRED LEFT HAND AIR CONDITIONING SYSTEM. 2 L 7 2 4F RT A21EA 1999090300378 19990903 00378 EA 1999 9 3 COMA9960472 1 19990824 A 5270 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 958CA 7111 CABIN DOOR WARNING AFTER TAKEOFF. ADJUSTED DOOR WARNING PROXIMITY SENSORS. 2 L 7 2 4F RT A21EA 1999090300379 19990903 00379 EA 1999 9 3 COMA9960473 1 19990828 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 EA CARGO COMPT ACTIVATED A COMA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 01 926CA 7027 CARGO SMOKE WARNING MESSAGE; BOTTLES DISCHARGED. CARGO SMOKE MESSAGE WAS A FALSE WARNING. REPLACED FIRE BOTTLES AND AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999090300380 19990903 00380 EA 1999 9 3 COMA9960474 1 19990827 A 3350 60206 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 918CA 7018 EMERGENCY LIGHT AT CABIN DOOR BULKHEAD IS INOPERABLE. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A21EA 1999090300381 19990903 00381 NM 1999 9 3 UPS99230490 1 19990827 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMERG LIGHTS INOP LWR MAIN DOOR. REMOVED AND REPLACED BATT PACK, CKS GOOD. 2 L 7 3 4F A3WE 1999090300382 19990903 00382 WP 1999 9 3 UPS99830484 1 19990805 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1152 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, AFT PIT FUSELAGE STA 1152 Z FITTING AT L36 - L35 R CORRODED. REMOVED Z FITTING STA 1152 IAW DC8 SRM 51-1-20D, RECEIVED NEW FITTING Z (P/N 3755845-1N), DRILLED FITTING IAW DC8 SRM 51-1-20D AND INSTALLED IAW DC8 SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1999090300383 19990903 00383 WP 1999 9 3 UPS99830485 1 19990819 A 5330 SKIN DOUG DC8 DC873F 302199F WP R2 DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, R-2 DOOR CUTOUT FUSELAGE SKIN, UNDER SCUFF PLATE HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1- 8, ORIGINAL MATL .080 REMAINING MATL .049 NOT WITHIN LIMITS IAW DC8 SRM 53-2-0. FABBED DOUBLER, LOCAT ED, DRILLED, COUN TERSUNK, DEBURRED IAW REO 06696. INSTALLED DOUBLER AND SEALED IAW REO 06696 AND DC8 SRM 51-1-20D, 51-1-15. 2 L 7 4 4F RT 4A25 1999090300384 19990903 00384 WP 1999 9 3 UPS99830486 1 19990728 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, FWD PIT STA 320 BETWEEN LONG 34R AND 35R, INSIDE DOOR TORQUE BOX, Z FITTING IS CORRODED. REMOVED Z FITTING IAW DC8 SRM 51-1-20D. FABRICATED REPAIR ANGLES IAW DC8 SRM 53-2-0. INSTALLED REPAIR ANGLES AND Z FITTINGS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300385 19990903 00385 WP 1999 9 3 UPS99830487 1 19990728 A 5330 SKIN DOUG DC8 DC873F 302199F WP L2 DOORWAY MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, L-Z DOOR UPPER AFT CORNER OF SKIN HAS PREVIOUS REPAIR NOT PER SRM. ROUTED OUT AREA IAW DC8 SRM 53-2 -0 FIG 18. FORMED DOUBLERS AND FILLER PER DC8 SRM 53-2-0 FIG 18. LOCATED, DRILLED AND TRIMMED DOUBLERS IAW DC8 SRM 53- 2-0 FIG 18. INSTALLED DOUBLERS AND FILLER IAW DC8 SRM 51-1-20D AND 53-2-0 FIG 18. 2 L 7 4 4F RT 4A25 1999090300386 19990903 00386 WP 1999 9 3 UPS99830488 1 19990802 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, AFT PIT FS 1270 LONGERON 34R HAS AN 8 INCH CRACK. REMOVED CRACKED LONGERON NR 34R STD 1270-1350 IAW DC8 SRM 51-1-20D. RECEIVED NEW LONGERON NR 3758593-1. DRILLED UP IAW DC8 SRM 51-1-20D. INSTALLED IAW DC8 SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 1999090300387 19990903 00387 WP 1999 9 3 UPS99830489 1 19990828 A 7110 COWL DOUG DC8 DC871F 302199D WP NR 3 ENGINE DAMAGED A IPXA K NONE O OTHER LD LANDING 1 SO 01 797UP 45897 INSPECTION TYPE:N/A, NR 3 ENG FAN COWL (O/B) DAMAGED WHEN NOSE GEAR COLLAPSED, SEE LOG PAGE 208929 ITEMS 1 AND 2. OPENE D COWL TRANSFERRED TO UPS NON-ROUTINE 544690. 2 L 7 4 4F RT 4A25 1999090300388 19990903 00388 NM 1999 9 3 DHL99707003 1 19990824 A 3260 CONNECTOR BOEING 727 72722 1384002 NM NLG DIRTY A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 707DH 18321 NOSE GEAR GREEN LIGHT EXTINGUISHED WITH THE LANDING GEAR LEVER DOWN, NO RED LIGHTS. CYCLED GEAR, NOSE GEAR GREEN LIGHT CAME ON. JACKED ACFT NOSE, OPERATED NOSE GEAR THRU 6 EXTENSIONS AND RETRACTIONS. ALL LIGHTS OPERATED PROPERLY. CLEANE D BOTH CANNON PLUGS IAW MM 31-26-11. GROUND CHECK OK. 2 L 7 3 4F A3WE 1999090300389 19990903 00389 WP 1999 9 3 K4HA99073 1 19990818 A 5313 LONGERON LKHEED 1011 1011385115 5265015 WP FUSELAGE CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 LOWER AFT CORNER OF MESC DOOR CUTOUT FRAME CORRODED. REMOVED CORRODED AREA ON FRAME AND KEELSON LONGERON. MANUFACTURED LONGERON REPAIR PARTS IAW L-1011 SRM 53-13-00 FIG 807. INSTALLED REPAIRS TO KEELSON LONGERON AND FRAME IAW L1011 SRM 5 3-13-00 FIG 807 AND 53-12-00, 51-30-01 AND EDR NO L1 06596. NON ROUTINE TASK NUMBER 65318. 2 L 7 3 4F A23WE 1999090300390 19990903 00390 WP 1999 9 3 K4HA99074 1 19990818 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 943 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 STR 29 BS 943 WEB AT STR/SKIN ATTACH CORRODED. REMOVED CORROSION FROM WEB, FOUND TO BE WITHIN LIMITS IAW L1011 SRM 51-2 1-01 AND 53-12-00. FOUND STRINGER OUT OF LIMITS IAW L1011 SRM 53-12-00. FABRICATED REPAIR PARTS IAW L1011 SRM 53-12-00 FIG 804. INSTALLED REPAIR PER L1011 SRM 53-13-00 FIG 804. NON-ROUTINE TASK NUMBER 65319. 2 L 7 3 4F A23WE 1999090300391 19990903 00391 NM 1999 9 3 USAASB99197 1 19990725 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM PASSENGER DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 590US 23935 EWR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOPERABLE OVER THE COCKPIT AND FORWARD ENTRY DOOR. MAINTENANCE REMOV ED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999090300392 19990903 00392 NM 1999 9 3 USAASB99194 1 19990807 A 3350 210310005 FUSE BOEING 737 737301 1384611 NM CABIN BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 337US 23235 PHL - DURING OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM ON OVERNIGHT CHECK, MAINTENANCE FOUND THE FIRST CLASS SEAT EMERG ENCY LIGHTS FAILED TO FULLY ILLUMINATE. MAINTENANCE REPLACED A BLOWN FUSE FOUND IN THE BATTERY CHARGER AND REMOVED AND REPLACED THE BATTERY PACK (PN 2013-1ALP). OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999090300393 19990903 00393 EU 1999 9 3 C2XA99IA423 1 19990806 A 3350 3013017 POWER SUPPLY AEROSP ATR42 ATR42500 EU CABIN INOPERABLE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14451 512 EFD - DURING MAINTENANCE INSPECTION, THE NR 3 EMERGENCY LIGHT POWER SUPPLY WAS FOUND INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300394 19990903 00394 EU 1999 9 3 C2XA99IA422 1 19990730 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE RIGHT FORWARD EXTERIOR EMERGENCY FLOOD LIGHT WAS FOUND INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( X) 2 H 7 2 4T RT A53EU 1999090300395 19990903 00395 SO 1999 9 3 99ZZZX3195 1 19990805 A 5330 12019229001 SKIN EMB 120 EMB120RT SO BS 9964.5 CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 59708 120098 DURING CONTINENTAL EXPRESS 'C' CHECK, FOUND LT FUSELAGE SKIN CHAFED BY A/C HEAT EXCHANGER AT FS 9964.5. BLENDED AREA, F ABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 20,512.5 HOURS . TAC: 27,506. (X) 2 L 7 2 4T RT A31SO 1999090300396 19990903 00396 SO 1999 9 3 99ZZZX3196 1 19990805 A 5400 12009639001 STIFFENER EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 59708 120098 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LT MLG WHEELWELL AFT BULKHEAD, OUTBOARD STIFFENER CRACKED. FABRICATED AND INS TALLED REPAIR DOUBLER IAW SRM 54-20-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 20,512.5 HOURS. TAC: 27,506. (X) 2 L 7 2 4T RT A31SO 1999090300397 19990903 00397 EU 1999 9 3 C2XA99IA424 1 19990811 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300398 19990903 00398 SO 1999 9 3 C2XA99CL073 1 19990810 A 2150 DUCT EMB 145 EMB145 SO LT PACK LOOSE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14933 145018 MSP/CLE - FLT 4012 - THE CREW REPORTED SMOKE FROM THE CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. THE AIR CRAFT DIVERTED TO GRB AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A DUCT HAD BLOWN OFF THE LEFT PACK SYSTEM, THEY RELEASED THE AIRCRAFT IAW MEL 36-11-05, CONTROL NUMBER 184831 DAT 'C'. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999090300399 19990903 00399 SO 1999 9 3 C2XA99IA432 1 19990815 A 5530 14531597602 DRAG ANGLE EMB 145 EMB145 SO EMPENNAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATIO N EC5330-01101; AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X) 2 L 7 2 4F RT T00011AT 1999090300400 19990903 00400 SO 1999 9 3 C2XA99IA431 1 19990815 A 5530 14531597601 DRAG ANGLE EMB 145 EMB145 SO EMPENNAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X) 2 L 7 2 4F RT T00011AT 1999090300401 19990903 00401 SO 1999 9 3 C2XA99IA430 1 19990815 A 3350 MS35478605 BULB EMB 145 EMB145 SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT ON PANEL 8AAXW WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999090300402 19990903 00402 SO 1999 9 3 C2XA99IA429 1 19990815 A 5320 STRAP EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING C-CHECK INSPECTION, THE BUTT CENTER BUTT STRAP WAS FOUND CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE R EPAIRED THE AFFECTED BUTT STRAP IAW EMBRAER FAX SST-1287/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X) 2 L 7 2 4F RT T00011AT 1999090300403 19990903 00403 SO 1999 9 3 C2XA99IA428 1 19990815 A 5320 SUPPORT EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT AT FRAME 20 LEFT WAS FOUND CORRODED. MAINTENANCE REPAIRED THE AFFECT ED FLOOR SUPPORT IAW EMBRAER FAX SST-1274/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HO URS. CYCLES: 2,791. (X) 2 L 7 2 4F RT T00011AT 1999090300404 19990903 00404 SO 1999 9 3 C2XA99IA427 1 19990815 A 3350 110049 CHARGER EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING C-CHECK INSPECTION, THE NR 1 EMERGENCY LIGHT BATTERY CHARGER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERIVCE. (X) 2 L 7 2 4F RT T00011AT 1999090300405 19990903 00405 SO 1999 9 3 C2XA99IA426 1 19990815 A 5720 14573504405 GUSSETT EMB 145 EMB145 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15941 145035 IAH - DURING C-CHECK INSPECTION, THE LEFT WING OUTBOARD LEADING EDGE OUTBOARD ATTACH GUSSETT WAS FOUND CRACKED. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED GUSSETT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,791. (X) 2 L 7 2 4F RT T00011AT 1999090300406 19990903 00406 EU 1999 9 3 C2XA99IA425 1 19990814 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED AN EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300407 19990903 00407 SO 1999 9 3 C2XA99CL074 1 19990810 A 2150 TSS44S40 CLAMP EMB 145 EMB145 SO LT PACK BROKEN A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14933 145018 CLE - FLT 3942 - SMOKE FROM CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. AIRCRAFT RELEASED IAW MEL 36-11-0 5 CONTROL NR 184831. MAINTENANCE REMOVED AND REPLACED THE LT PACK DTV DUCT AND REPLACED THE BROKEN CLAMP IAW EMB-145 M M 36-11-9. OPS AND LEAK CHECKS WERE GOOD. REF: EMB-145 IPC 21-51-00 FIG 25 ITEMS 130, 180, 230, FOR PARTS CHANGED. A IRCRAFT IS RELEASED. REF: OPERATOR CNTRL NR C2XA99CL073 DATED 8-10-99. REF: OPERATOR CNTRL NR 99ZZZX3197. (X) 2 L 7 2 4F RT T00011AT 1999090300408 19990903 00408 SO 1999 9 3 99ZZZX3197 1 19990811 A 2150 81S1133 DUCT EMB 145 EMB145 SO LT PACK WEAK A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14933 145018 CLE - FLT 3942 - SMOKE FROM CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. AIRCRAFT RELEASED IAW MEL 36-11-0 5 CONTROL NR 184831. MAINTENANCE REMOVED AND REPLACED THE LT PACK DTV DUCT AND REPLACED THE BROKEN CLAMP IAW EMB-145 M M 36-11-9. OPS AND LEAK CHECKS WERE GOOD. REF: EMB-145 IPC 21-51-00 FIG 25 ITEMS 130, 180, 230, FOR PARTS CHANGED. A IRCRAFT IS RELEASED. REF: OPERATOR CNTRL NR C2XA99CL073 DATED 8-10-99. REF: OPERATOR CNTRL NR C2XA99CL074. 2 L 7 2 4F RT T00011AT 1999090300409 19990903 00409 SO 1999 9 3 C2XA99CL067 1 19990802 A 2150 PACK EMB 120 EMB120RT SO EFT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 12715 120125 CLE - FLT 3179 - THE CREW REPORTED A BURNING SMELL IN FLIGHT FROM THE LEFT PACK. THE AIRCRAFT LANDED IN CLEVELAND WITHO UT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL NR 21-50-02 CAT 'C' CONTROL NUMBER 183687. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999090300410 19990903 00410 SO 1999 9 3 C2XA99CL066 1 19990726 A 7603 SWITCH EMB 120 EMB120RT SO POWER LEVER DIRTY A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 57734 120199 CLE - FLT 3102 - THE CREW REPORTED AN AURAL WARNING AT 90 KNOTS ON TAKEOFF. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED T O THE GATE WITHOUT FURTHER INCIDENT. (X) 2 L 7 2 4T RT A31SO 1999090300411 19990903 00411 SO 1999 9 3 C2XA999CL07 1 19990806 A 3150 1173T030203 SWITCH EMB 120 EMB120RT SO LT PACK FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17720 31 1260 120142 CLE - FLT 3147 - THE CREW REPORTED THAT AFTER TAKEOFF WHEN THE BLEED WAS OPENED, T6 WENT ABOVE 816C. THE AIRCRAFT RETUR NED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK OVERHEAT SWITCH AND PERFORMED OPERATIONAL CHECKS IAW EMB-120 MM 21-61-00, AND 21-61-02. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999090300412 19990903 00412 EU 1999 9 3 C2XA99IA417 1 19990802 A 3350 167006 LAMP AEROSP ATR42 ATR42500 EU ROW 4AB FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16450 510 IAH - DURING MAINTENANCE VISIT INSPECTION, THE AISLE PATH EMERGENCY LIGHT AT SEAT 4AB WAS FOUND INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BULB IAW ATR 42-500 MM 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300413 19990903 00413 EU 1999 9 3 C2XA99IA419 1 19990726 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PASSENGER DOOR INOPERABLE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14821 160 EFD - DURING MAINTENANCE INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR 42320 MM 33-51-24, AND THE AIRCRAFT WAS APPROVD FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300414 19990903 00414 SO 1999 9 3 C2XA99IA418 1 19990727 A 3350 110049 POWER SUPPLY EMB 145 EMB145 SO EMERGENCY EXIT INOPERABLE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 13936 145025 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE LEFT AND RIGHT HAND EXTERIOR EMERGENCY EXIT LIGHTS TO BE INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW WITH EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999090300415 19990903 00415 CE 1999 9 3 C2XA99CL062 1 19990729 A 3610 BLEED AIR SYSTEM BEECH 1900 1900D 1154162 CE RIGHT MALFUNCTIONED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 69549 UE194 FWA - FLT 120G - THE CREW REPORTED THAT SMOKE ENTERED THE CABIN IN-FLIGHT DURING SINGLE ENGINE SIMULATION, THE AIRCRAFT RETURNED TO FWA WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE RIGHT ENVIRONMENTAL BLEED AIR SYSTEM ON MEL NR 21-14 C ONTROL NR 183678 CAT 'C'. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999090300416 19990903 00416 CE 1999 9 3 C2XA99CL061 1 19990724 A 6120 PROP CONTROL BEECH 1900 1900D 1154162 CE E/E COMPT MALFUNCTIONED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 09 87551 UE206 CLE - FLT 3154 - THE CREW REPORTED ON TAKEOFF ROLL, THE NR 1 PROPELLER ONLY WENT TO 1,650 RPM AND THE NR 2 PROPELLER ONL Y WENT TO 1,670 RPM. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND OPERATIO NAL CHECKS IAW BEECHCRAFT MM 61-20-00, ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999090300417 19990903 00417 CE 1999 9 3 C2XA99CL068 1 19990803 A 6123 SWITCH BEECH 1900 1900D 1154162 CE AUTOFEATHER SYS DIRTY A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 49543 UE181 CAK - FLT 3008 - THE CREW REPORTED THAT ON TAKEOFF ROLL, THE 'AFX DISABLE' ANNUNCIATOR ILLUMINATED AND THE LEFT AUTOFEAT HER SYSTEM UNARMED. THE AIRCRAFT REJECTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CLEAN ED PRESSURE SWITCHES IAW BEECHCRAFT MM 61-21-00, THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999090300418 19990903 00418 CE 1999 9 3 C2XA99CL069 1 19990807 A 6123 I293640919 PC BOARD BEECH 1900 1900D 1154162 CE AUTOFEATHER SYS FAILED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 49543 502I95 UE181 IAD - FLT 3015 - THE CREW REPORTED THAT ON TAKEOFF ROLL, THE 'AFX DISABLE' ANNUNCIATOR ILLUMINATED AT 90 KIAS, THE AIRCR AFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTEANCE REMOVED AND REPLACED PCBA123 AND PERFO RMED OPS CHECKS AND ENGINE RUNS IAW BEECHCRAFT MM 61-21-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE . (X) 2 L 7 2 4T RT A24CE 1999090300419 19990903 00419 CE 1999 9 3 C2XZ99CL072 1 19990808 A 6123 1293640919 PC BOARD BEECH 1900 1900D 1154162 CE AUTOFEATHER SYS FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 49543 4993 782E96 UE181 CLE - FLT 3056 - THE CREW REPORTED THE 'AFX DISABLE' LIGHT REMAINED ILLUMINATED UP TO 15,000 FEET. THE AIRCRAFT RETURNE D TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PC BOARD, AND PERFORMED OPERATIONAL CHECK S OF THE AUTOFEATHER SYSTEM IAW BEECHCRAFT MM 61-21-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999090300420 19990903 00420 EU 1999 9 3 SIMA992272 1 19990815 A 2910 AE7069585 HOSE SAAB SF340 340B 7860101 EU NLG WW FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 390AE 340B390 DFW - FLT 5063 - TOTAL HYDRAULIC SYSTEM PRESSURE AND FLUID LOSS. EXTENDED LANDING GEAR MANUALLY AND RETURNED TO FIELD. REMOVED AND REPLACED TWO HOSES ON NOSE LANDING GEAR AND RETURNED TO FIELD. REMOVED AND REPLACED TWO HOSES ON NOSE LAND ING GEAR ACTUATOR. RESERVICED HYDRAULIC SYSTEM. PERFORMED OPERATIONAL CHECK AND RETURNED AIRCRAFT TO SERVICE. REF: O PER CNTRL NR 99ZZZX3198. (X) 2 L 7 2 4T RT A52EU 1999090300421 19990903 00421 EU 1999 9 3 99ZZZX3198 1 19990815 A 2910 AE7069588 HOSE SAAB SF340 340B 7860101 EU NLG WW FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 390AE 340B390 DFW - FLT 5063 - TOTAL HYDRAULIC SYSTEM PRESSURE AND FLUID LOSS. EXTENDED LANDING GEAR MANUALLY AND RETURNED TO FIELD. REMOVED AND REPLACED TWO HOSES ON NOSE LANDING GEAR AND RETURNED TO FIELD. REMOVED AND REPLACED TWO HOSES ON NOSE LAND ING GEAR ACTUATOR. RESERVICED HYDRAULIC SYSTEM. PERFORMED OPERATIONAL CHECK AND RETURNED AIRCRAFT TO SERVICE. REF: O PER CNTRL NR SIMA992272. 2 L 7 2 4T RT A52EU 1999090300422 19990903 00422 EU 1999 9 3 SIMA992231 1 19990811 A 3240 BRAKES SAAB SF340 340B 7860101 EU BRAKE SYSTEM REQ'D SERVICE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 301AE 340B301 JFK - FLT 4925 - LEFT BRAKE GRABS EXCESSIVELY. RIGHT BRAKE DOES NOT GRAB AT ALL. INSPECTED AND BLED ALL FOUR BRAKES. L EAK AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999090300423 19990903 00423 EU 1999 9 3 SIMA992023 1 19990721 A 3240 AIR124472 HOSE SAAB SF340 340B 7860101 EU LT MLG BROKEN A SIMA O OTHER K FLUID LOSS LD LANDING 1 SW 21 335AE 340B335 LAX - FLT 3256 - UPON LANDING, THE LEFT MLG BRAKE LINE BROKE AND THE AIRCRAFT LOST ALL HYDRAULIC FLUID AND BRAKE PRESSUR E. REMOVED AND REPLACED THE LEFT LOWER BRAKE LINE. RESERVICED HYDRAULIC SYSTEM, PERFORMED OPERATIONAL CHECKS, AND RETU RNED AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999090300424 19990903 00424 EU 1999 9 3 SIMA991802 1 19990629 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 626 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 238AE 340B238 ABI - DENT IN LOWER REAR FUSELAGE AT STA 626.0 BETWEEN STR'S 1528 AND 1524. MADE 1.25 INCH CUT-OUT. PERFORMED EDDY CUR RENT INSP OF CUT-OUT WITH NO DEFECTS NOTED. FABBED A SPACER .040 INCH THICK, WITH MAX DIA .08 INCH LESS THAN THAT OF CU T-OUT. FABBED REPAIR PLATE .040 INCH THICK WITH OVERLAP TO CONTAIN TWO ROWS OF RIVETS TO BE INSTALLED ON THE INSIDE OF THE FUSELAGE. CONTOURED BOTH REPAIR PIECES TO FIT FUSELAGE AT DAMAGED AREA. ALODINED AND APPLIED FR-PRIMER TO ALL HOLE S AND EDGES. FAY SEALED AND APPLIED DINITROL AV 25 TO INSIDE REPAIR AREA. ATTACHED REPAIR PLATES TO ACFT. APPLIED TOP COAT. WORK DONE IAW SAAB 340 SRM 53-80-10 PAGES 218-222 AND STD SRM REPAIR PRACTICES. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999090300425 19990903 00425 EU 1999 9 3 SIMA991801 1 19990629 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 351-363 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AE 340B348 ABI - TWO DENTS FOUND AFT OF RT ICE SHIELD BETWEEN STA'S 363 AND 351, STR LINE 1615 AND 1616. RECONTOURED BOTH DENTS. P ERFORMED EDDY CURRENT INSP OF RECONTOURED AREA. NO DEFECTS NOTED. FABBED 2 REPAIR DOUBLERS .050 INCH THICK. DIMENSION S OF 14 INCH BY 5.5 INCH AND SECOND 12 INCHES BY 4.5 INCHES. CONTOURED TO FIT FUSELAGE. APPLIED ALODINE AND EPOXY PRIM ER TO DOUBLERS. FAY SEALED REPAIR DOUBLERS AND ATTACHED TO ACFT WITH FASTENERS. FILLET SEALED REPAIR EDGES AND APPLIED SURFACE TOPCOAT. WORK DONE IAW SAAB 340 SRM 53-70-10 PG 217 AND STD SRM PRINCIPALS. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1999090300426 19990903 00426 EU 1999 9 3 SIMA991662 1 19990615 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 852 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 227AE 340B227 ABI - FOUND SMALL BURNED AREA OF SKIN AT STA 852.0/WL 110.0. AFTER BLENDING, LIMITS FOR SKIN THICKNESS WERE EXCEEDED. R EMOVED DAMAGE WITH .75 INCH CUT-OUT OF SKIN, DEBURRED AND SMOOTHED EDGES. PERFORMED EDDY CURRENT INSP WITH NO DEFECTS N OTED. FABBED FILLER PLATE .032 INCH, DOUBLER 13.5 INCH BY 5.5 INCH, AND TRIPLER 10 INCH BY 3.5 INCH AND .016 INCH THICK WITH CORNER RADII OF.4 INCH. APPLIED ALODINE AND ONE COAT OF EPOXY PRIMER. FAY SEALED AND INSTALLED EXT REINFORCEMENT AND FILLER PLATE PICKING UP EXISTING RIVET HOLES IN STRINGERS AND FRAME USING ORIG RIVET TYPE, MS20470-4. SEALED AND A PPLIED TOPCOAT. WORK DONE IAW SAAB REPAIR STATEMENT NR 72SDS1604 AND SAAB SRM 53-90-10 PG 201. ACFT OK FOR SERVICE. 2 L 7 2 4T RT A52EU 1999090300427 19990903 00427 EU 1999 9 3 SIMA992273 1 19990815 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 203NE 340B203 GGT - FLT 5823 - CARGO SMOKE WARNING LIGHT ON CWP ACTIVATES INTERMITTENTLY. PERFORMED OPERATIONAL TEST WITH NO DISCREPA NCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999090300428 19990903 00428 EU 1999 9 3 SIMA992271 1 19990815 A 3350 60132211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 309AE 19891 340B309 JFK - FLOOR EMERGENCY LIGHTS AT SEAT 3, 4, 5BC DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT LOCATION 20LN. (X) 2 L 7 2 4T RT A52EU 1999090300429 19990903 00429 EU 1999 9 3 SIMA992261 1 19990814 A 3350 2LA00511500 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 184AE 340B184 DFW - FLT 5004 - EMERGENCY LIGHT ABOVE SEAT 12C DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BULB. OPERAT IONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999090300430 19990903 00430 EU 1999 9 3 SIMA992252 1 19990813 A 2611 72111211100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 383AE A2920 340B383 DFW - FLT 5032 - CARGO SMOKE WARNING ACTIVATED. USED FIRE EXTINGUISHER NR 1. VERIFIED EVENT AS A FALSE WARNING. REMOV ED AND REPLACED FORWARD AND AFT SMOKE DETECTORS AND FIRE EXTINGUISHER. PERFORMED OPERATIONAL TEST AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999090300431 19990903 00431 EU 1999 9 3 SIMA992251 1 19990813 A 3320 BR8300809 LIGHT SAAB SF340 340B 7860101 EU GALLEY FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 261AE 340B261 LAW - FLT 3867 - SMALL AMOUNT OF SMOKE CAME FROM GALLEY STORAGE SPACE ADJACENT TO HOT JUGS. TURNED OFF GALLEY WORK LIGH T AND THE SMOKE CEASED. REMOVED AND REPLACED GALLEY WORK LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999090300432 19990903 00432 EU 1999 9 3 SIMA992241 1 19990812 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 238AE 340B238 DFW - FLT 3892 - TWO FORWARD EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BULBS FOR FLOOR L IGHTS. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999090300433 19990903 00433 NM 1999 9 3 TSAA9977394 1 19990814 A 7711 LG80A6 EPR TRANSMITTER BOEING 737 737297 1384480 NM NR 2 ENGINE DEFECTIVE A TSAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 13 726AL 22426 HNL/ITO - FLT 74 - AFTER TAKEOFF, ROLL WAS STARTED AND POWER WAS SET FOR TAKEOFF. A RED FLAG CAME UPON NR 2 ENGINE EPR. REDUCED POWER TO IDLE. NO RTO, SPEED LESS THAN 60 KIAS. ABORTED TAKEOFF. RETURNED TO GATE. REMOVED AND REPLACED EP R TRANSMITTER AND EPR INDICATOR. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999090300434 19990903 00434 NM 1999 9 3 TSAA9933393 1 19990814 A 3350 86210068 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED BATTERY PACK FOR NR 1 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (X) 2 L 7 2 4F RT A16WE 1999090300435 19990903 00435 NM 1999 9 3 TSAA9933392 1 19990813 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 1 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TOR SERVICE. (X) 2 L 7 2 4F RT A16WE 1999090300436 19990903 00436 NM 1999 9 3 TSAA9933396 1 19990816 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERABLE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999090300437 19990903 00437 NM 1999 9 3 TSAA9933395 1 19990816 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 1 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999090300438 19990903 00438 NM 1999 9 3 TSAA9933387 1 19990811 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999090300439 19990903 00439 NM 1999 9 3 TSAA9933389 1 19990812 A 3350 8731002511 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERABLE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED AFT SERVICE DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4F RT A16WE 1999090300440 19990903 00440 NM 1999 9 3 TSAA9933390 1 19990812 A 3350 86210151 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY PACK IN AFT CONTROL MODULE DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999090300441 19990903 00441 NM 1999 9 3 TSAA9933391 1 19990812 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 1 AND NR 2 FLOOR LIGHT BATTERY PACKS DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1999090300442 19990903 00442 NM 1999 9 3 TSAA9933388 1 19990812 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999090300443 19990903 00443 WP 1999 9 3 GTIA9901067 1 19990803 A 3350 1001191 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERABLE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 601 47526 AFT CABIN DOOR EMERGENCY LIGHT (HAND HELD) INOPERATIVE. REMOVED AND REPLACED AFT CABIN DOOR EMERGENCY LIGHT ASSY IAW DC -9 MM 33-50-00. (X) 2 L 7 2 4F A6WE 1999090300444 19990903 00444 NM 1999 9 3 TWAA9911901 1 19990829 A 2560 GIRT BAR BOEING 757 757231 1384950 NM PAX DOOR DIRTY A TWAA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 CE 05 721TW 29954 THE LEFT FORWARD CABIN DOOR ESCAPE SLIDE DID NOT ARM AFTER THE DOOR WAS CLOSED. FOUND DEBRIS WAS UNDER THE GIRT BAR, BL OCKING GIRT BAR ENGAGEMENT. REMOVED THE DEBRIS. 2 L 7 2 4F RT A2NM 1999090300445 19990903 00445 WP 1999 9 3 TWAA9911902 1 19990819 A 5312 BULKHEAD ANGLE DOUG DC9 DC931 3022065 WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND AFT PRESS BULKHEAD, FWD SIDE DIAGONAL BRACE ATTACH ANGLE ON PRESSURE BULKHEAD, STA 996 A T UPPER END, CRACKED BETWEEN LONGERON 3L AND 4L. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE. PAINTED AND REINSTALL ED IN ACCORDANCE WITH SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999090300446 19990903 00446 WP 1999 9 3 TWAA9911903 1 19990819 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, THE RT BULKHEAD WAS CRACKED 3 INCHES LONG, LOCATED 1 INCH ABOVE FLOOR AND 5 INCHES FROM SIDEWA LL ON FWD SIDE, STA 965. REMOVED AND REPLACED BULKHEAD PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999090300447 19990903 00447 WP 1999 9 3 TWAA9911904 1 19990818 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 938 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND IN CABIN THERE WAS CORROSION ON LONGERON 18 WEB, STA 938R. REPLACED WEB PER SRM 6-70-01 , ITEM 4 B-1. 2 L 7 2 4F A6WE 1999090300448 19990903 00448 WP 1999 9 3 TWAA9911905 1 19990818 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 946 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, FOUND CORROSION IN CABIN AT LONGERON 18R, APPROX STA 946 ON WEB. REPLACED WEB PER SPM 6-70-01 , ITEM 4 B-1. 2 L 7 2 4F A6WE 1999090300449 19990903 00449 WP 1999 9 3 TWAA9911906 1 19990822 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 857-965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK, CHAIR TRACK NUMBER 4 WAS CORRODED AT FLANGE, STA 857 THRU 965. NEW TRACK INSTALLED PER SPM 6- 70-01. SPLICE PER SRM 53-05, FIG 4F SHEET 1. 2 L 7 2 4F A6WE 1999090300450 19990903 00450 WP 1999 9 3 AT9900610 1 19990719 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 570-590 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT OUTBOARD SEAT TRACK AT BS 570 - 590 WITH NICKS, SCRATCHES A ND CORROSION. CUT OUT SECTION OF SEAT TRACK, FABRICATED, DRILLED, DEBURRED, COUNTERSUNK, AND INSTALLED IAW DC9 SRM 51-1 0-3, 53-05-0, 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999090300451 19990903 00451 NM 1999 9 3 AT9900611 1 19990827 A 3350 CONNECTOR BOEING 737 737214 138446R NM CABIN LOOSE A ZZDA K NONE L NO TEST CR CRUISE 1 SO 15 460AT 20158 ONCE IN FLIGHT, EMERGENCY EXIT LIGHTS AND AISLE PATH LIGHTING CAME ON IN FLIGHT WITH SWITCH IN ARMED POSITION. CYCLED A IRCRAFT POWER, TESTED OK. INSPECTED AND FOUND LOOSE CONNECTION ON THE AFT SWITCH, SECURED AND CLEANED CONNECTOR AND TES TED GOOD. 2 L 7 2 4F A16WE 1999090300452 19990903 00452 EA 1999 9 3 JBXA9900101 1 19990825 A 2750 85501007 BPSU 1104SD10050 CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A JBXA K NONE J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 05 572ML 0392 7224 FLAP FAIL MSG AFTER SELECTING 8 DEGREES DURING APPROACH. REMOVED AND REPLACED NR 2 BPSU IAW CRJ MM 27-51-10. REMOVED A ND REPLACED FLEXIBLE DRIVE SHAFT NR 5 IAW CRJ MM 27-51-10, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1999090300453 19990903 00453 1999 9 3 AWXA9900275 4 19990830 A 3442 MI5851641 ANTENNA BOEING 737 737277 1384570 NM RADAR FAILED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 184AW 29705 268 22651 AIR TURNBACK - RADAR UNSTABLE IN LEFT TURN, FALLS OFF AND PAINTS THE GROUND IN RIGHT TURN. FO'S GYRO ON AUX, NO HELP. REPLACED RADAR ANTENNA AND R/T, OPS CHECK GOOD REF LOG 7476120. TWO MINOR DEGRADATION DISCREPANCIES IN LAST 30 DAYS, R/T REPLACED 21 AUG 99. 2 L 7 2 4F RT A16WE 1999090300454 19990903 00454 1999 9 3 PNSA990803 2 19990830 A 7230 31011607 SEAL SWRNGN SA227 SA227AC 8780603 SW ENG COMPRESSOR LEAKED A PNSA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 41NE 14573 AC741B DURING CRUISE, CABIN HEAT SELECTOR WAS PLACED TO THE WARM POSITION. COCKPIT BEGAN TO FILL WITH AN OIL MIST AND SMOKE AN D SMELL. HEAT WAS SELECTED BACK TO COLD AND CABIN CLEARED. THIS OCCURRENCE IS STILL UNDER INVESTIGATION. FOUND ENGINE COMPRESSOR SEAL LEAKING. REPLACED SEAL WITH NEW AND NO FURTHER INDICATIONS OF OIL SMELL IN CABIN HAS BEEN DETECTED. 2 L 7 2 4T RT A8SW 1999090300455 19990903 00455 WP 1999 9 3 CALA9901100 1 19990829 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 43537 47112 INSPECTION FOUND FORWARD SECTION OF EMERGENCY AISLE LIGHTING INOPERATIVE. MAINTENANCE FOUND A BROKEN LIGHT SOCKET WIRE. A NEW SOCKET ASSEMBLY WAS SPLICED IN AND FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 1999090300456 19990903 00456 NM 1999 9 3 CALA9901101 1 19990829 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT FASTENER HOLE, STA 312. A NEW FLOORBEAM UPPER CHORD WAS INSTALLED IA W SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999090300457 19990903 00457 NM 1999 9 3 CALA9901102 1 19990830 A 5753 FITTING BOEING 727 727224 1384076 NM LT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FORWARD END OF LT WING NR 4 FLAP TRACK FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED. THE FL AP TRACK WAS REINSTALLED IAW MM 27-51-72, PAGE 401. 2 L 7 3 4F A3WE 1999090300458 19990903 00458 NM 1999 9 3 CALA9901103 1 19990830 A 3350 BATTERY PACK BOEING 727 727224 1384076 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FORWARD OVERHEAD EMERGENCY LIGHT AT ROW NR 2 INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK AT FAULT. THE BATTERY PACK WAS RECHARGED AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-81, PAGE 403. 2 L 7 3 4F A3WE 1999090300459 19990903 00459 NM 1999 9 3 CALA9901104 1 19990830 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND FLOORBEAM CORRODED AT STA 967 ABOUT 20 INCHES FROM CENTERLINE TO BOTH LT AND RT SIDES. THE CORRODED SE CTION OF FLOORBEAM WAS REPLACED IAW ECRA 5310-03909. 2 L 7 2 4F RT A16WE 1999090300460 19990903 00460 NM 1999 9 3 CALA9901105 1 19990830 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND FORWARD CARGO DOOR EXTERIOR SKIN DENTED. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 1999090300461 19990903 00461 WP 1999 9 3 CALA9901106 1 19990830 A 5523 5910414503 SKIN DOUG DC9 DC982 3022082 WP LT ELEV TRIM TAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69826 49486 INSPECTION FOUND THE LT ELEVATOR GEAR TRIM TAB DENTED AT I/B TRAILING EDGE. THE TRIM TAB WAS REMOVED, REPAIRED AND REIN STALLED IAW MM 27-30-04. 2 L 7 2 4F A6WE 1999090300462 19990903 00462 WP 1999 9 3 CALA9901107 1 19990830 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 229-265 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69826 49486 INSPECTION FOUND DENTS IN FORWARD FUSELAGE SKIN ABOVE CUSP LINE AT FS 229 - 265, LONGERON 15L - 18L. THE DENTED AREA OF SKIN WAS REMOVED, A NEW SECTION OF SKIN, DOUBLER, AND LONGERON STRAP WERE INSTALLED IAW SRM 51-10-03 AND ECRA 5330-0244 5. 2 L 7 2 4F A6WE 1999090300463 19990903 00463 NM 1999 9 3 CALA9901108 1 19990830 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 277 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 6L AT STA 277. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 20 3. 2 L 7 2 4F RT A16WE 1999090300464 19990903 00464 NM 1999 9 3 CALA9901109 1 19990831 A 5320 INTERCOSTAL BOEING 757 757224 1384958 NM BS 680-700 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 680 - 700, RBL 56. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-51, ECRA 532 1-01061, AND BOEING DRAWING 143N5845. 2 L 7 2 4F RT A2NM 1999090300465 19990903 00465 NM 1999 9 3 CALA9901110 1 19990831 A 5320 INTERCOSTAL BOEING 757 757224 1384958 NM BS 324 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 324, RBL 40.75. THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01059. 2 L 7 2 4F RT A2NM 1999090300466 19990903 00466 WP 1999 9 3 9903401162 1 19990826 A 5320 WEB DOUG DC10 DC1040 3023508 WP BS 475 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING M-CHECK, FOUND CRACK IN RIGHT NOSE WHEEL WEB AT FS 475 9 INCHES BELOW UPPER PRESSURE DECK. REPAIRED PER EA 11-17 0427. 2 L 7 3 4F A22WE 1999090300467 19990903 00467 WP 1999 9 3 9903411152 1 19990730 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 879 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING M-CHECK, FOUND CRACK ON VERTICAL LEG OF CARGO FLOOR FRAME AT FS 879, RBL 33. REPAIRED PER EA 11-169416. 2 L 7 3 4F A22WE 1999090300468 19990903 00468 WP 1999 9 3 9903421152 1 19990713 A 5320 BEAM DOUG DC10 DC1040 3023508 WP BS 791 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING M-CHECK, FOUND CRACK IN I-BEAM SUPPORT AT FS 791, BL 0. REPAIRED PER EA 11-168291. 2 L 7 3 4F A22WE 1999090300469 19990903 00469 NM 1999 9 3 9903436632 1 19990707 A 5711 SPAR WEB BOEING 747 747251B 1384892 NM WS 574 582 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 632US 23112 DURING M-CHECK, RIGHT WING MIDSPAR WEB WAS FOUND WITH CRACKS BETWEEN WS 574 AND 582 AT FASTENER LOCATIONS COMMON TO THE UPPER CHORD. REPAIRED PER EA 66-168586 (P/N 65B17246-4). 2 L 7 4 4F A20WE 1999090300470 19990903 00470 NM 1999 9 3 9903446716 1 19990716 A 5320 SUPPORT BOEING 747 747251F 1384898 NM BS 600 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 616US 21120 DURING P-CHECK, FOUND CORROSION UNDER NUT PLATE UPPER CHORD OF FLOOR SUPPORT. REPAIRED PER EA 67-166746 (P/N 65B01723-3 28). 2 L 7 4 4F A20WE 1999090300471 19990903 00471 NM 1999 9 3 9903452285 1 19990726 A 5320 SKIN BOEING 727 727251 138408H NM BS 380-420 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 285US 21324 DURING L-CHECK, FOUND CORROSION ON SKIN UNDER THRESHOLD OF FORWARD GALLEY DOORWAY FROM FS 380 TO 420, RBL 71, WL 208. R EPAIRED PER EA 22-153292. 2 L 7 3 4F A3WE 1999090300472 19990903 00472 NM 1999 9 3 9903466627 1 19990826 A 2780 RETRACT MECH BOEING 747 747251B 1384892 NM LE FLAPS MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 01 627US 21708 DURING CLIMB, THE LEADING EDGE FLAP AMBER LIGHTS ILLUMINATED ACCOMPANIED WITH AIRFRAME VIBRATION. AMBER LGHTS FOR THE N R 1 AND NR 2 LEFT WING LEADING EDGE FLAPS REMAINED ILLUMINATED AFTER USING THE ALTERNATE SYSTEM. AIRCRAFT DIVERTED NRT, DUMPED 120,000 LBS OF FUEL, AND LANDED WITHOUT INCIDENT. REPLACED CIRCUIT CARDS YA3A08 AND YA3A13. OPERATIONAL CHECK GOOD. EXACT CAUSE OF EVENT TO BE DETERMINED. 2 L 7 4 4F A20WE 1999090300473 19990903 00473 WP 1999 9 3 9903479935 1 19990821 A 2730 ROD END DOUG DC9 DC931 3022065 WP ELEVATOR LOOSE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 GL 01 1332U 47404 TAKEOFF WAS ABORTED AT APPROXIMATELY 100 KTS DUE TO ELEVATOR BEING DIFFICULT TO CONTROL. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND ROD END TO ELEVATOR BOOST CYLINDER PULLED FROM ELEVATOR ATTACH POINT JAMMING LEFT ELEVATOR FULL UP. REINSTALLED ROD END. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999090300474 19990903 00474 NM 1999 9 3 9903486615 1 19990815 A 3230 RETRACT MECH BOEING 747 747251B 1384892 NM NLG MALFUNTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 615US 20360 WHILE CHECKING FOR A HYDRAULIC LEAK, THE NOSE LANDING GEAR RETRACTED RESULTING IN DOOR 1L BECOMING DETACHED FROM THE FUS ELAGE BY THE JETWAY. THE BOEING AOG TEAM WILL BEGIN THE REPAIR PROCESS ON 26AUG99. EXACT CAUSE OF EVENT TO BE DETERMIN ED. 2 L 7 4 4F A20WE 1999090300475 19990903 00475 WP 1999 9 3 9903499856 1 19990823 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999090300476 19990903 00476 WP 1999 9 3 9903509902 1 19990820 A 3397 WIRE DOUG DC9 DC931 3022065 WP TAIL COMPARTMENT BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 952N 47073 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPAIRED CORRODED YELLOW ARM WIRE IN TAIL COMPARTMENT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999090300477 19990903 00477 EA 1999 9 3 COMA9960475 1 19990829 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 NOSE GEAR DOORS AND SURROUNDING STRUCTURE DAMAGED BY A COLLISION WITH A TUG. INSTALLED FOLLOWING NEW PARTS LEFT HAND NO SE GEAR DOOR (P/N 600-33043-1007), RIGHT HAND NOSE GEAR DOOR (P/N 600-33043-1008), SIDE ATTACH ANGLE (P/N 600-33042-293) AND AIRCRAFT STRIKER ANGLE 600-33042-270. CW DETAILED INSP OF NLG, AND PERFORMED GEAR SWING IAW 51-42-06, 32-22-01, 32 -30-00, 32-20-00 OF THE CRJ MM & SRM. ENGINEERING REPORT NR 3402-1. 2 L 7 2 4F RT A21EA 1999090300478 19990903 00478 EA 1999 9 3 COMA9960476 1 19990830 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 FRAME AT FS 718 DISCOVERED CRACK IN THE RADIUS EXTENDING 4' ABOVE STR 11 RHS, CRACK IN THE FLANGE EXTENDING TO THE FIRST FASTENER HOLE BELOW STR 11 RHS, AND CRACK IN THE DOUBLER ON AIRCRAFT SIDE OF FRAME AT STR 11 RHS. REPAIRED FRAME AT FS 718, STR 11 RHS IAW WVAC EO 601R-53-0285 AND WVAC EO 601R-53-0286. 2 L 7 2 4F RT A21EA 1999090300479 19990903 00479 EA 1999 9 3 COMA9960477 1 19990829 A 5311 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 FS 718 CRACKED BELOW STRINGER 11 ON LEFT SIDE FUSELAGE .25 INCH LONG. PERFORMED A MAJOR REPAIR, REMOVED CRACKED SECTION OF FRAME, INSTALLED REPAIR DOUBLER PO 23127/1 IAW WVAC EO 601R-53-0288. 2 L 7 2 4F RT A21EA 1999090300480 19990903 00480 EA 1999 9 3 COMA9960478 1 19990829 A 5320 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 DOUBLER ON AFT SIDE FS 718 AT STRINGER 11 CRACKED LEFT SIDE FUSELAGE 4 INCH LONG. PERFORMED A MAJOR REPAIR, REMOVED CRA CKED DOUBLER, INSTALLED NEW DOUBLER PO 23127/1 IAW WVAC EO 601R-53-0287. 2 L 7 2 4F RT A21EA 1999090300481 19990903 00481 NE 1999 9 3 COMA9960479 2 19990829 A 7230 6030T61G09 EXHAUST FRAME CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE CRACKED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 946CA 11915 7072 807142 RIGHT HAND LOW OIL PRESSURE. REPLACED CRACKED EXHAUST FRAME. 2 L 7 2 4F 4 F RT A21EA E15NE 1999090300482 19990903 00482 NM 1999 9 3 UPS99230493 1 19990830 A 7830 SKIN BOEING 727 727172C 1384058 NM NR 1 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:N/A, NR 1 THRUST REVERSER UPPER DOOR ASSY INTERIOR SKIN CRACKED IN TWO PLACES. REMOVED AND REPLACED NR 1 T/R UPPER DOOR ASSY IAW MM 78-30-00. 2 L 7 3 4F A3WE 1999090300483 19990903 00483 NM 1999 9 3 UPS99230510 1 19990828 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, CORROSION ON FRAME HAT SECTION AT BS 720E FRAME ABOVE STR 5R TO STR 15R. CORROSION OUT OF LIMITS, F ABRICATED NEW FRAME, REPLACEMENT PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999090300484 19990903 00484 NM 1999 9 3 UPS99230511 1 19990823 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 950-1010 CORRDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 950F - 1010 LBL 45 AT NUT PLATE HOLES. CORROSION FOUND TO BE OUT OF LIMIT S PER SRM 53-10-1 FIG 3. REMOVED AND REPLACED SEAT TRACK FROM BS 950E BS 1020 LBL 45 PER 53-10-5. 2 L 7 3 4F A3WE 1999090300485 19990903 00485 NM 1999 9 3 UPS99230512 1 19990825 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 580-600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, SEAT TRACK CORRODED BETWEEN 580 - 600 RBL 45 WL 208. REPLACED SEAT TRACK RBL 45 BS 540 TO 610 PER S RM 53-10-5. 2 L 7 3 4F A3WE 1999090300486 19990903 00486 NM 1999 9 3 UPS99230513 1 19990820 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 480-520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, SEAT TRACK CORRODED BETWEEN BS 480 - 520 BL 0, WL 208. CORROSION CLEAN-UP BEYOND ACCEPTABLE LIMITS. FABRICATED AND INSTALLED REPLACEMENT TRACK PER SRM 51-10-8 AND 53-10-5. 2 L 7 3 4F A3WE 1999090300487 19990903 00487 NM 1999 9 3 UPS99230514 1 19990830 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 700 LBL 25 WL 208. REPLACED SEAT TRACK EXTRUSION FROM BS 690 TO BS 720D+1 0 PER 727 SRM 53-10-5. 2 L 7 3 4F A3WE 1999090300488 19990903 00488 NM 1999 9 3 UPS99230516 1 19990830 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, UPPER LEFT EXT EMERG LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999090300489 19990903 00489 NM 1999 9 3 UPS99230517 1 19990830 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, CTR RIGHT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OP CHECKS GOOD. 2 L 7 3 4F A3WE 1999090300490 19990903 00490 NM 1999 9 3 UPS99230518 1 19990830 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, CTR LEFT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999090300491 19990903 00491 NM 1999 9 3 UPS99230519 1 19990830 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, LOWER LEFT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999090300492 19990903 00492 NM 1999 9 3 UPS99230520 1 19990830 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, UPPER RIGHT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATT PACK, CHECK GOOD. 2 L 7 3 4F A3WE 1999090300493 19990903 00493 NM 1999 9 3 UPS99230521 1 19990830 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, LOWER RIGHT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATT PACK, OPS CHECKS OK. 2 L 7 3 4F A3WE 1999090300494 19990903 00494 NM 1999 9 3 UPS99230522 1 19990830 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM ROW 3 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMERG FLOOR LIGHT ROW 3 INOP. REMOVED AND REPLACED BATT PACK, OP CHECKS GOOD. 2 L 7 3 4F A3WE 1999090300495 19990903 00495 NM 1999 9 3 UPS99230523 1 19990830 A 3350 9621033 BATTERY PACK BOEING 727 72725C 138400H NM LT EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, LEFT AFT EMER OVERWING EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999090300496 19990903 00496 NM 1999 9 3 UPS99230525 1 19990830 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM VENTRAL STAIRS DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A,VENTRAL STAIRS EMER LIGHT INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999090300497 19990903 00497 NM 1999 9 3 UPS99430491 1 19990830 A 7830 6SB97904210 SKIN BOEING 747 747123 1384873 NM NR 1 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A, 4 X 3 CRACKED OUT AREA AT NR 1 ENG EXHAUST OUTER SLEEVE SKIN O/B SIDE AT 1130. REMOVED TURBINE EXH AUST SLEEVE FRAME ASSY PER MM 78-1-01, INSTALLED NR 1 ENG THRUST REVERSER SLEEVE ASSY PER MM 78-11-00 (P/N 6SB97904-2 10 ) ON, (P/N 6SB97904-210) OFF, (S/N 000162) ON. 2 L 7 4 4F A20WE 1999090300498 19990903 00498 NM 1999 9 3 UPS99430494 1 19990830 A 5730 PANEL BOEING 747 747212B 1384886 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A, CRACK IN UPPER L/E WING PANEL I/B NR 2 ENGINE. *S/D* INSTALLED NEW PANEL AS REQUIRED. 2 L 7 4 4F A20WE 1999090300499 19990903 00499 WP 1999 9 3 UPS99830495 1 19990804 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 80-100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, HEAVY CORROSION ON THE INTERCOSTAL AND END CLIP AT FS 80 TO 100 AT LONG 25R. REMOVED, FABRICATED AND REPLACED THE INTERCOSTAL AND CLIP IAW SRM 53-4-1 & 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300500 19990903 00500 WP 1999 9 3 UPS99830496 1 19990804 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1638 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, CORROSION FOUND ON FUSELAGE INTERNAL SKIN BETWEEN LONG 32R & 33R AT FS 1638. CUT OUT THE DAMAGED AREA AND REPAIRED THE INTERNAL SKIN IAW DH SK867-507. 2 L 7 4 4F RT 4A25 1999090300501 19990903 00501 WP 1999 9 3 UPS99830497 1 19990809 A 5320 5694309 ANGLE DOUG DC8 DC873F 302199F WP BS 1600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS 1600, THE RT UPPER CUSP FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED TH E FITTING IAW DWG 5694309 AND SRM 51-1-20D & 51-3-0. 2 L 7 4 4F RT 4A25 1999090300502 19990903 00502 WP 1999 9 3 UPS99830498 1 19990811 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, LONGERON 24R IS CRACKED AT FS 940. STOP DRILLED CRACK AND REPAIRED LONGERON IAW SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 1999090300503 19990903 00503 WP 1999 9 3 UPS99830499 1 19990814 A 5311 5764343507 FRAME DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C123, FS 1040 FRAME CAP IS CORRODED BEYOND LIMITS BETWEEN LBL 28 TO RBL 28. REMOVED AND REPLACED THE FR AME CAP IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300504 19990903 00504 WP 1999 9 3 UPS99830500 1 19990808 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 475 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, THE RT O/B SLOT LWR DOOR SKIN AT XS 475, IS DENTED AND CRACKED. CUT THE DAMAGED AREA AND REPAIRED T HE SKIN IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999090300505 19990903 00505 WP 1999 9 3 UPS99830501 1 19990811 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 131 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, FS -131, 8 BELOW THE SUBFLOOR, THE FRAME O/B FLANGE IS CRACKED AND CORRODED. STOP DRILLED THE CRACK , REMOVED THE CORROSION, AND REPAIRED THE FRAME CAP IAW DH SK813-878. FRAME CAP WITHIN LIMITS AFTER CORROSION REMOVAL I AW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999090300506 19990903 00506 WP 1999 9 3 UPS99830502 1 19990811 A 5313 975491349 LONGERON DOUG DC8 DC873F 302199F WP BS 270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, LONGERON 34R IS CORRODED BEYOND LIMITS AT FS 270. CUT OUT DAMAGED SECTION OF LONGERON 34R BETWEEN F S 250 & 290 AND SPLICED IN A NEW SECTION IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1999090300507 19990903 00507 WP 1999 9 3 UPS99830503 1 19990814 A 5320 58004713 SPLICE DOUG DC8 DC873F 302199F WP BS 640-660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, THE LONGERON 30R SPLICE FITTING AT FS 640 TO 660 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW S RM 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300508 19990903 00508 WP 1999 9 3 UPS99830504 1 19990815 A 5320 37558241 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, BATH TUB FITTING FS 280, LONG 33R TO 34R IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FITTIN G IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999090300509 19990903 00509 WP 1999 9 3 UPS99830506 1 19990828 A 7830 SKIN DOUG DC8 DC873F 302199F WP NR 1 TR UNIT DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:N/A, DENT IN NR 1 ENGINE OUTBOARD THRUST REVERSER AT 4 O'CLOCK POSITION REF D175215. INSTALLED REPAIR D OUBLER PER CFM MM 78-30-00. 2 L 7 4 4F RT 4A25 1999090300510 19990903 00510 WP 1999 9 3 UPS99830524 1 19990814 A 5320 58004713 SPLICE DOUG DC8 DC873F 302199F WP BS 640-660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C1, LONGERON 34R SPLICE FITTING AT FS 640 TO 660 IS CRACKED. REMOVED, FABRICATED AND REPLACED THE SPLIC E FITTING IAW SRM 51-3-0 AND DWG 5800471. 2 L 7 4 4F RT 4A25 1999090300511 19990903 00511 WP 1999 9 3 UPS99830526 1 19990830 A 5210 HINGE ROD DOUG DC8 DC873F 302199F WP CREW DOOR OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 CREW ENTRY DOOR WILL NOT OPEN. LWR HINGE ASSY W/N RETRACT WHEN TURNING HANDLE TO OPEN DOOR, CANNOT BE OPENED UNLESS HIN GE IS HELD UP. FWD ENTRY LOWER HINGE CONTROL ROD ASSY PER 52-11-01, OPS CK GOOD PER 52-11-01. 2 L 7 4 4F RT 4A25 1999090300512 19990903 00512 WP 1999 9 3 UPS99830527 1 19990828 A 2710 CYLINDER DOUG DC8 DC871F 302199D WP LT AILERON FAILED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 703UP 45939 INSPECTION TYPE:N/A, LOSS OF MAIN RESERVOIR HYDRAULIC FLUID. AILERON AND RUDDER MAN LIGHT ON, PRESSURE FLUCTUATED. RAN LOSS OF HYDRAULICS CHECKLIST, RECOVERED NORMAL GEAR, FLAPS, BRAKES, NW STEERING. FLT CONT NOTIFIED, DECLARED INFLIGHT E MERGENCY W/ATC. NORMAL LANDING. REMOVED AND REPLACED LEFT AILERON POWER CYLINDER IAW MM 27-11-06, NO LEAKS OR CHECKS N OTED. 2 L 7 4 4F RT 4A25 1999090300513 19990903 00513 EU 1999 9 3 QXEA9901677 1 19990826 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 3045 111 11156 BOI- AFT WING ROOT FAIRING EMERGENCY EVACUATION LIGHTS REMAIN ON AFTER AIRCRAFT POWER REMOVED. REPLACED POWER SUPPLY, O PERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999090300514 19990903 00514 EU 1999 9 3 QXEA9901678 1 19990827 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU RT EMER EXIT MISSING A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 499US 11182 PDX- EMERGENCY EXIT SIGN MISSING BETWEEN RIGHT HAND OVERWING EXITS. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999090300515 19990903 00515 NM 1999 9 3 QXEA9901664 1 19990820 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - CARGO DOOR SKIN SMALL CHAFED AREA NEAR AFT UPPER CORNER. REPAIRED IAW HORIZON AIR EA 2-52-28. 2 H 7 2 4T RT A13NM 1999090300516 19990903 00516 NM 1999 9 3 QXEA9901666 1 19990819 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM LT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LIGHT FRETTING CORROSION AROUND SEVERAL SCREW HOLES AND LIGHT CHAFING DAMAGE ON LOWER LEADING EDGE ATTACH FLANGE O F THE LEFT-HAND WING, FORWARD SPAR. REPAIRED IAW DHC-8 PSM 1-8-3, CHAPTER 51-20-26. 2 H 7 2 4T RT A13NM 1999090300517 19990903 00517 NM 1999 9 3 QXEA9901667 1 19990818 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND WING OUTBOARD FLAP TOP SKIN SURFACE HAS HEAVY CHAFING DAMAGE FROM MAKING CONTACT WITH WING. REPAIRED IA W HORIZON AIR EA 2-57-26. 2 H 7 2 4T RT A13NM 1999090300518 19990903 00518 NM 1999 9 3 QXEA9901668 1 19990813 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - DENT IN REAR FUSELAGE RIGHT-HAND SIDE BETWEEN FRAME 2 AND 3 AND STRINGERS 20 AND 21. REPAIRED IAW DHC-8 SRM 53-30 -24, PAGE 2, FIGURE 1 SHEET 1. 2 H 7 2 4T RT A13NM 1999090300519 19990903 00519 NM 1999 9 3 QXEA9901669 1 19990821 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - SMALL DENT/SCRATCH IN FUSELAGE SKIN 6 INCHES ABOVE AND 1 INCH AFT OF RIGHT-HAND PITOT TUBE. REPAIRED IAW HORIZON AIR EA 2-53-76. 2 H 7 2 4T RT A13NM 1999090300520 19990903 00520 NM 1999 9 3 QXEA9901670 1 19990813 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT-HAND SIDE FUSELAGE AREA FOR PANEL 261NT HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 MM 20-32-02, PAGE 202, PARAGRA PH D1-6. 2 H 7 2 4T RT A13NM 1999090300521 19990903 00521 NM 1999 9 3 QXEA9901671 1 19990813 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND SIDE FUSELAGE AREA FOR PANEL 261DT HAS CHAFE DAMAGE. REPAIRED IAW DHC MM 20-32-02, PAGE 202 PARAGRAPH D 1-6. 2 H 7 2 4T RT A13NM 1999090300522 19990903 00522 NM 1999 9 3 QXEA9901672 1 19990817 A 5230 PADS DHAV DHC8 DHC8202 2809007 NM CARGO DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - BOTH BOTTOM PRESSURE PADS FOR LOWER DOOR STOPS GROOVES WORN IN THEM. REPAIRED IAW 51-20-16 AND RD 8-53-104 AND HO RIZON AIR EA 2-53-70. 2 H 7 2 4T RT A13NM 1999090300523 19990903 00523 NM 1999 9 3 QXEA9901673 1 19990823 A 5320 JAMB DHAV DHC8 DHC8202 2809007 NM CARGO DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - CARGO DOOR UPPER APERTURE JUST BEFORE BOTH TOP PRESSURE PADS HAVE DAMAGE FROM DOOR STOPS. REPAIRED IAW HORIZON AI R EA 2-53-79. 2 H 7 2 4T RT A13NM 1999090300524 19990903 00524 NM 1999 9 3 QXEA9901674 1 19990821 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND FORWARD INBOARD CONNECTION ANGLE AT AFT END HAS DAMAGE ATTACHMENT HOLES. REPAIRED IAW HORIZON AIR EA 2- 53-78. 2 H 7 2 4T RT A13NM 1999090300525 19990903 00525 NM 1999 9 3 99FDEA00355 1 19990827 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 MAIN DECK SEAT TRACK CRACKED AT BS Y=635, INTERSECTION OF X=27.5 APPROX 3 IN & X=47.5 APPROX 3 IN. *S/D* MAIN DECK SEA T TRACK BS Y=635, X=27.5 & X=47.5. REPAIR CARRIED OUT PER SRM 53-70-00 VOL 1. 2 L 7 3 4F RT A22WE 1999090300526 19990903 00526 NM 1999 9 3 99FDEA00356 1 19990828 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 483 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FWD CABIN FLOOR TRACK ASSY FOUND CRACKED. FWD CABIN FLOOR TRACK ASSY FOUND CRACKED. FWD CABIN FLOOR TRACK ASSY FOUND C RACKED. *S/D* REPAIR CARRIED OUT PER SRM 53-70-00. 2 L 7 3 4F RT A22WE 1999090300527 19990903 00527 NM 1999 9 3 99FDEA00357 1 19990830 A 5510 652418911 BEAM BOEING 727 727277 138408S NM LT HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 BULGE ON LT HORIZONTAL STAB LOWER T/E BEAM I/B END (C55-391-20-1). *S/D* REMOVED AND REPLACED LT HORIZONTAL STAB LWR T /E BEAM IAW FEDEX MM 55-30-021-4, 27-30-005-4, 27-30-01, 27-30-05, 27-30-001-4, 27-30-000-5, 27-30-001-5, FEDEX SRM 51-3 0-2, 51-30-5, 51-30-8. 2 L 7 3 4F RT A3WE 1999090300528 19990903 00528 NM 1999 9 3 99FDEA00358 1 19990830 A 2701 CONTROL WHEEL DOUG MD11 MD11F 3023600 NM LT COCKPIT POPPING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 623FE 48794 CAPT'S CONTROL WHEEL HAS POPPING SOUND WITH FWD AND AFT MOVEMENT OF CONTROL WHEEL, WITH NO BINDING. REPAIRED IAW EA 1-2 700-46588B. 2 L 7 3 4F RT A22WE 1999090300529 19990903 00529 WP 1999 9 3 ABXA9900671 1 19990813 A 5313 59114279 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 945. REPAIRED IAW DC9 SRM 51-10-2 1ND 51-10-5. 2 L 7 2 4F A6WE 1999090300530 19990903 00530 WP 1999 9 3 ABXA9900672 1 19990817 A 5313 59114279 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1999090300531 19990903 00531 WP 1999 9 3 ABXA9900673 1 19990819 A 5280 59175331 PAN DOUG DOUG DC9 DC932 3022066 WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LEFT MAIN LANDING GEAR INBOARD DOOR INNER PAN CRACKED. REPLACED DOOR IAW DC9 MM. 2 L 7 2 4F A6WE 1999090300532 19990903 00532 WP 1999 9 3 ABXA9900674 1 19990819 A 5311 9918618 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LEFT MAIN FRAME CRACKED AT STATION 718. REPAIRED IAW ABX REA D953-32765MR. 2 L 7 2 4F A6WE 1999090300533 19990903 00533 WP 1999 9 3 ABXA9900675 1 19990819 A 5311 9918619 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LEFT MAIN FRAME CRACKED AT STATION 737. REPAIRED IAW ABX REA D953-32765MR. 2 L 7 2 4F A6WE 1999090300534 19990903 00534 WP 1999 9 3 ABXA9900676 1 19990813 A 5711 99196182 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK, FOUND LEFT MAIN FRAME AT STATION 718 CRACKED IN THE FORWARD AND AFT POCKETS. INSTALLED DOUBLERS IAW DAC O SERVICE BULLETIN 53-100 AND DACO DWG 5934375. 2 L 7 2 4F A6WE 1999090300535 19990903 00535 WP 1999 9 3 ABXA9900677 1 19990829 A 3260 0080004003 CONTROL BOX DOUG DC9 DC941 302207N WP RT MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 955AX 47619 RIGHT MAIN LANDING GEAR LIGHT ILLUMINATED DURING FLIGHT. COMPLIED WITH ABNORMAL PROCEDURES. RECYCLED GEAR, LIGHT REMAI NED ON. SPEED DECREASED TO LESS THAN 300 KNOTS FOR REMAINDER OF FLIGHT. ON DESCENT LIGHT EXTINGUISHED. REPLACED LANDI NG GEAR PROXIMITY CONTROL BOX IAW DC9 MM 32-50-00. CYCLED GEAR SEVERAL TIMES, ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F A6WE 1999090300536 19990903 00536 NM 1999 9 3 DHL99705002 1 19990825 A 2910 LINE BOEING 727 72722C 138400F NM NR 1 ENGINE CRACKED A DHLA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 705DH 19191 WHILE APPROACHING MIA, A HYDRAULIC LEAK WAS IDENTIFIED IN THE A SYSTEM. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND A LINE CRACKED FROM HYDRAULIC MODULE TO NR 1 ENGINE PUMP. REPLACED LINE, CHECKED BOTH CASE DRAIN FILTERS FOR CO NTAMINATION. SERVICED AND LEAK CHECKED OK PER MM 29-11-61. 2 L 7 3 4F A3WE 1999090300537 19990903 00537 NM 1999 9 3 DHL99705003 1 19990824 A 5311 FRAME BOEING 727 72722C 138400F NM BS 280 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 705DH 19191 FOUND 3 INCH CRACK IN NOSE WHEEL WELL LEFT SIDE APPROX STA 280. STOP DRILLED CRACKS, HFEC. CRACKS STOP AT STOP DRILL. CUT OUT DAMAGED AREA PER S/B 53-145 AND INSTALLED REPAIR PER AVITAS ENGINEERING 99DHLI.030R0-1 AND S/B 53-145R1. 2 L 7 3 4F A3WE 1999090300538 19990903 00538 EU 1999 9 3 SIMA991611 1 19990610 A 5270 EO326 SWITCH AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR OUT OF ADJUST A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 209AT 0209 BOS - FLT 4963 - FORWARD CARGO DOOR WARNING CAME ON AFTER TAKEOFF. DECLARED EMERGENCY. RETURNED TO FIELD. ADJUSTED DO OR PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK WITH NO FURTHER DISCREPANCIES NOTED. (M) 2 H 7 2 4T RT A53EU 1999090300539 19990903 00539 EU 1999 9 3 SIMA992162 1 19990804 A 5330 S536712050051 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING MBV-1 INSPECTION, REPAIRED TWO DENTS IN THE LEFT SIDE OF THE FUSEALGE SKIN. FIRST WAS TDMI 249MQ53004F, DE NT AT FRAME 32 WATER LINE 3000. SECOND WAS AFT OF FRAME 31 AT STRINGER 12, MEASURING .5 BY .75 BY .038 DEEP. WORK DONE IAW SRM 53-00-00 FIGURES 404, 405, AND 427. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999090300540 19990903 00540 EU 1999 9 3 SIMA992151 1 19990803 A 5753 S5751211020400 CAM GUIDE AEROSP ATR72 ATR72212 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT INBOARD FLAP INBOARD DEFLECTOR WITH THREE CAM GUIDES CORRODED, THE LEFT OU TBOARD FLAP INBOARD DEFLECTOR WITH TWO CAM GUIDES CORRODED, AND THE LEFT INBOARD FLAP OUTBOARD DEFLECTOR OUTBOARD CAM GU IDE CORRODED. REMOVED AND REPLACED ALL CAM GUIDES IAW SRM 51-25-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999090300541 19990903 00541 EU 1999 9 3 99ZZZM618 1 19990803 A 5753 S5751204920400 CAM GUIDE AEROSP ATR72 ATR72212 EU LT TE FLAP CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT INBOARD FLAP INBOARD DEFLECTOR WITH THREE CAM GUIDES CORRODED, THE LEFT OU TBOARD FLAP INBOARD DEFLECTOR WITH TWO CAM GUIDES CORRODED, AND THE LEFT INBOARD FLAP OUTBOARD DEFLECTOR OUTBOARD CAM GU IDE CORRODED. REMOVED AND REPLACED ALL CAM GUIDES IAW SRM 51-25-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999090300542 19990903 00542 EU 1999 9 3 SIMA992182 1 19990806 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 330AE 340B330 DFW - FLT 5024 - EMERGENCY LIGHTING OVER SEAT 4A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOO D. (M) 2 L 7 2 4T RT A52EU 1999090300543 19990903 00543 EU 1999 9 3 SIMA992181 1 19990806 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 11836 135 SAW - DURING PS-2 INSPECTION, FOUND THE AFT EMERGENCY LIGHTS REMAINED ON WHEN SWITCH WAS RELEASED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 30 WL IAW JIC 33-51-21-RAI-10010-004. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999090300544 19990903 00544 EU 1999 9 3 SIMA992161 1 19990804 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 305AE 340B305 JFK - FLT 4406 - EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 4B DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONA L CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999090300545 19990903 00545 EU 1999 9 3 SIMA992142 1 19990802 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 214DA 340B214 DFW - FLT 5022 - EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 4B DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999090300546 19990903 00546 EU 1999 9 3 SIMA992141 1 19990802 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AE 340B198 DFW - FLT 5086 - EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 11BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIO NAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999090300547 19990903 00547 1999 9 3 99ZZZM619 4 19990630 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT FAILED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 211UX UE211 PILOT REPORTED THAT THE ALTIMETER INDICATED 100 FEET LOW ON THE GROUND. REMOVED AND REPLACED PILOTS ALTIMETER. BENCH C HECK VERIFIED THAT THE ALTIMETER INDICATED PLUS/MINUS 100 FT AT ALL TEST POINTS. THIS IS THE 5TH REPORTED SUCH FAILURE OF THIS ALTIMETER. (M) 2 L 7 2 4T RT A24CE 1999090300548 19990903 00548 1999 9 3 99ZZZM620 4 19990604 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT MALFUNCTIONED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 118UX UE118 PILOT REPORTED 140' SPLIT IN THE ALTIMETERS AT 14,000 FEET INDICATED ALTITUDE. REMOVED AND REPLACED PILOTS ALTIMETER. S UBSEQUENT BENCH CHECK FOUND ALTIMETER TO BE INDICATIN G135 FEET HIGH AT 12,000 FEET. THIS ALTIMETER HAD FLOWN FOR ONLY 2 FLIGHTS SINCE INSTALLATION. (M) 2 L 7 2 4T RT A24CE 1999090300549 19990903 00549 NM 1999 9 3 TSAA9933375 1 19990727 A 5730 SKIN BOEING 737 7372Q9 138448M NM WS 157 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 EXFOLIATION FOUND ON UNDERSIDE OF RIGHT INBOARD WING LOWER SKIN AT STATION 157 AT REAR SPAR. REPAIRED CORRODED AREA IAW ECO 1684R10. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999090300550 19990903 00550 NM 1999 9 3 TSAA995366 1 19990731 A 5330 SKIN BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FOUND 2 INCH CRACK ON RIGHT FUSELAGE AFT OF WINGS BELOW WINDOW. HFEC AROUND CUT COMPLIED WITH. REPAIRED PER SRM 53-30- 3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999090300551 19990903 00551 NM 1999 9 3 TSAA9933376 1 19990802 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999090300552 19990903 00552 NM 1999 9 3 TSAA9977356 1 19990717 A 7711 511863 PT7 TUBE ASSY BOEING 737 73725A 1384481 NM NR 1 ENGINE FAILED A TSAA C D ABORTED TAKEOFF RETURN TO BLOCK L T NO TEST ENGINE CASE PENETRATION TO TAKEOFF 1 WP 13 819AL 23791 FLT 263 - HNL-LIH - NR 1 ENGINE UNABLE TO GET TAKEOFF POWER (1.73 EPR MAX). ABORTED TAKEOFF AT 60 KNOTS. RETURNED TO G ATE. REMOVED AND REPLACED TUBE ASSY. PERFORMED GROUND RUN PER 71-09-200. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999090300553 19990903 00553 NE 1999 9 3 TSAA9972364 2 19990726 A 7200 ENGINE BOEING 737 737230 NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A TSAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 13 823AL 46624 23154 666847 FLT 112 - OGG-KOA - LOUD 'BANG' WITH HIGHT EGT ON NR 2, 650 PLUS. SHUT DOWN ENGINE. EMERGENCY DECLARED. RETURNED TO O GG. NORMAL LANDING. REMOVED AND REPLACED NR 2 ENGINE ASY IAW FORMS M-211, M-212, M-213, M-214, AND M-215. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1999090300554 19990903 00554 NM 1999 9 3 TSAA9927359 1 19990723 A 2760 CONTROL CABLE BOEING 737 7372Q9 138448M NM GROUND SPOILER OUT OF ADJ A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 804AL 21719 FLT 201 - HNL-LIH - AFTER LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION, ACCOMPLISHED CHECKLIST AND WARNING HORN STA YED ON. LANDING GEAR STAYED DOWN AND THREE GREEN LIGHTS STAYED ON STEADY. CHECK CB. PUT GEAR HANDLE DOWN WITH THREE G REEN LIGHTS. RETURNED TO HNL. UNEVENTFUL LANDING. ADJUSTED GROUND SPOILER INTERLOCK VALVE CABLE IAW MM 27-62-57. TES TED IAW MM 27-62-51. NO DISCREPANCIES NOTED. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999090300555 19990903 00555 NM 1999 9 3 TSAA9979363 1 19990726 A 7930 69726881 PRESSURE SWITCH BOEING 737 737282C 13844AU NM NR 1 ENGINE DEFECTIVE A TSAA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 826AL 23051 FLT 943 - KOA-HNL - DURING CRUISE, NR 1 OIL FILTER BYPASS LIGHT ILLUMINATED. PER SOP, SHUT DOWN NR 1 ENGINE IN FLIGHT. DECLARED EMERGENCY. NORMAL LANDING AT HNL. INSPECTED NR 1 ENGINE FILTER. NO DEFECTS NOTED. REMOVED AND REPLACED OIL FILTER BYPASS SWITCH. GROUND RUNUP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999090300556 19990903 00556 NM 1999 9 3 TSAA9933377 1 19990803 A 3350 8731002511 LIGHT BOEING 737 737297 1384480 NM PAX DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999090300557 19990903 00557 NM 1999 9 3 TSAA9933378 1 19990804 A 3350 87310025111 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED AFT ENTRY DOOR EXIT IDENTIFIER LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999090300558 19990903 00558 NM 1999 9 3 TSAA9928365 1 19990730 A 2840 654651093 CONDUIT BOEING 737 7372S5C 1384499 NM CENTER TANK LEAKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 IN THE PROCESS OF ACCOMPLISHING ECO 2956, CENTER TANK FLOAT SWITCH MOD, SB 737 28A1132, AD 99-05012, MECHANICS FOUND THA T FUEL HAD LEAKED INTO THE ELECTRICAL CONDUIT UPON REMOVAL. FURTHER INVESTIGATION (PRESSURE CHECKED) REVEALED THAT THE LEAK BETWEEN THE FLARELESS SLEEVE AND THE CONDUIT. NO OTHER DEFECTS SUCH AS WIRE CHAFFING OR ARCING WERE EVIDENT. (M) 2 L 7 2 4F RT A16WE 1999090300559 19990903 00559 EU 1999 9 3 USAAF99039 1 19990803 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU EMER EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 887US 11349 IND - FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1999090300560 19990903 00560 EU 1999 9 3 USAAF99037 1 19990728 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU RT WING DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 880US 11331 CLT - FOUND RIGHT WING BODY FAIRING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1999090300561 19990903 00561 NM 1999 9 3 USAASB99191 1 19990805 A 2910 65C268103035 HYD LINE BOEING 737 7374B7 1384702 NM RT MLG WW FAILED A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 EA 19 437US 24559 MCO - FLT 538 - APPROX 5 MINS AFTER T/O, THE 'B' HYD SYS LOW PRESS LIGHT ILLUMINATED FOLLOWED BY A TOTAL LOSS OF 'B' HYD SYS QTY AND SUBSEQUENT ILLUMINATION OF THE 'B' SYSTEM LOW QTY LIGHT. SHORTLY THEREAFTER, THE CREW NOTICED STANDBY HYD SYS LOW PRESSURE LIGHT HAD ILLUMINATED, FOLLOWED BY ILLUMINATION OF STANDBY SYS LOW QTY LIGHT. CAPT CONTACTED AND DIVER TED TO MCO. AN EMERGENCY WAS DECLARED AND THE CABIN WAS PREPPED. THE FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE WITH THE 'A' HYD SYS PRESS AND QTY NORMAL. MX R/R'D TEMPORARY FLEX LINE WITH A RIGID HYD PRESS LINE FOR 'B' SYS SP OILERS IN RT MLG WHEELWELL. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999090300562 19990903 00562 NE 1999 9 3 99ZZZM621 2 19990617 A 7321 7436025 FUEL CONTROL BOEING 727 727281 138408N NM PWA JT8 JT8D17A 52049 NE NR 1 ENGINE LEAKING A P9RA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 09 906PG 50011 20728 P688161 UNSCHEDULED LANDING IN STL DUE TO HIGH FUEL FLOW ON NR 1 ENGINE. FUEL CONTROL WAS FOUND TO BE LEAKING AT MATING SURFACE AFT OF THE MOISTURE TRAP. THE FUEL CONTROL WAS REPLACED, ENGINE TRIMMED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999090300563 19990903 00563 CE 1999 9 3 RU3A99008 1 19990803 A 2121 15238203 BLOWER BEECH 300 300BEECH 1152930 CE E/E COMPT FAILED A RU3A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 74 FF9 THE FLT CREW NOTICED A BURNING ODOR/FUMES AT CRUISE ALTITUDE. NO VISIBLE SMOKE WAS NOTED. DURING THIS TIME THE PANEL T ECH NOTICED THAT THE TEMPERATURE IN THE CABIN AVIONICS EQUIPMENT RACK HAD INCREASED TO ABOUT 33 DEGREES CELSIUS. AIRCRA FT MAD UNSCHEDULED LANDING. SYSTEM OPERATED FOR SEVERAL HOURS IN THE HANGAR WITH NO DISCREPANCIES NOTED. REPLACED THE AUXILIARY AIR CONDITIONER BLOWER IN THE CABIN AVIONICS EQUIPMENT RACK. NO VISIBLE DAMAGE COULD BE FOUND ON THE REMOVED MOTOR. SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4T A24CE 1999090300564 19990903 00564 CE 1999 9 3 COEA9901746 1 19990804 A 5230 K5SN HANDLE CESSNA 208 208B 2073701 CE CARGO DOOR OUT OF ADJUST A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 746FX 208B0498 ANCHORAGE - APPROX .25 MILE OUT FROM ANC PILOT NOTED THE DOOR OPEN WARNING LIGHT CAME ON. THE PILOT TURNED BACK TO ANC. WHILE RETURNING, THE UPPER CARGO DOOR OPENED IN FLIGHT. THE AIRCRAFT LANDED SAFELY AT ANC. MAINTENANCE ADJUSTED THE CARGO DOOR HANDLE DETENT. MAINTENANCE INSPECTED DOOR AND NO DAMAGE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 H 7 1 3T A37CE 1999090300565 19990903 00565 EA 1999 9 3 99ZZZM622 1 19990803 A 5210 C6FSM124627 PLATE ASSY DHAV DHC6 DHC6300 2802606 EA LT CREW DOOR WORN A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 712PV 696 HNL - DURING GROUND MAINTENANCE INSPECTION, FOUND LEFT CREW DOOR UPPER HINGE HOLE ELONGATED AND WORN. REPLACED DEFECTIV E HINGE. (M) 1 H 7 2 3T RT A9EA 1999090300566 19990903 00566 EU 1999 9 3 UF6A990716 1 19990712 A 5330 SKIN BAG ATP ATP EU BS 180 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - DENT ON FUSELAGE BEHIND ICESHIELD AT STATION 180FS AND STRINGER 20. MAINTENANCE REMOVED DENT IAW BAE SRM 51-30-01 AND REPAIRED DENT IAW BAE SRM 51-60-01 FIGURE 4. (M) 2 L 7 2 4T RT A27NM 1999090300567 19990903 00567 EU 1999 9 3 UF6A990713 1 19990712 A 5531 JD553J0048000 RIB BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - RIB AT STATION 351.75 IN VERTICAL FIN CRACKED. MAINTENANCE REPAIRED THE RIB IAW BAE SRM 51-60-03. (M) 2 L 7 2 4T RT A27NM 1999090300568 19990903 00568 EU 1999 9 3 UF6A990715 1 19990712 A 5330 SKIN BAG ATP ATP EU BS 325 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - SHARP DENT LEFT SIDE OF FUSELAGE AFT OF STATION 325AS. MAINTENANCE REPAIRED DENT IAW BAE SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300569 19990903 00569 EU 1999 9 3 UF6A990411 1 19990427 A 2422 INVERTER BAG ATP ATP EU NR 2 FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 31 858AW 2035 ORD - FLT 5733 - THE NR 2 INVERTER FAILED ON TAKEOFF ROLL. THE NR 2 NON-ESSENTIAL FELL OFF LINE. MAINTENANCE PERFORMED OPERATIONAL CHECK OF ENTIRE SYSTEM. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1999090300570 19990903 00570 EU 1999 9 3 UF6A990412 1 19990427 A 3350 362624 LIGHT BAG ATP ATP EU ROW 9 INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 2020 SBN - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 9 IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FLOOR PROXIMITY LIGHTIN G STRIP. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300571 19990903 00571 EU 1999 9 3 UF6A990413 1 19990428 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU EMER EXIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 8086 17410 2021 GRB - FLT 5732 - EMERGENCY FLOOR STRIP LIGHTING IN OVERWING EXIT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 3 POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300572 19990903 00572 EU 1999 9 3 UF6A990414 1 19990428 A 5330 SKIN BAG ATP ATP EU BS 180-234 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 11555 2028 ORD - LEFT SIDE FUSELAGE SKIN IS DAMAGED BETWEEN STATION 180AS AND 234AS BETWEEN STRINGER 35 AND 38. MAINTENANCE REPAIR ED DAMAGE IAW DER REPOT NR 99-081. (M) 2 L 7 2 4T RT A27NM 1999090300573 19990903 00573 EU 1999 9 3 UF6A990415 1 19990429 A 5312 BULKHEAD SKIN BAG ATP ATP EU BS 378 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - FOUND DAMAGE TO SKIN JUST AFT OF THE PRESSURE BULKHEAD AT THE 6 O'CLOCK POSITION. MAINTENANCE REPAIRED DAMAGE IAW DER REPORT NR 99-064 REVE A. (M) 2 L 7 2 4T RT A27NM 1999090300574 19990903 00574 EU 1999 9 3 UF6A990410 1 19990427 A 3350 1317 BULB BAG ATP ATP EU EXTERNAL FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - AFT BAGGAGE EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD . (M) 2 L 7 2 4T RT A27NM 1999090300576 19990903 00576 EU 1999 9 3 UF6A990409 1 19990417 A 7921 3036064 OIL COOLER BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 31 851AW 11315 2020 CAK - FLT 5709 - LOW OIL PRESSURE CWP ILLUMINATED, ON THE NR 2 ENGINE, ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACE D THE OIL COOLER ON THE NR 2 ENGINE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300577 19990903 00577 EU 1999 9 3 UF6A990408 1 19990417 A 3350 00140520600 MODULE BAG ATP ATP EU PAX DOOR FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FLT 5704 - WHITE EMERGENCY EXIT LIGHT IS INOPERATIVE OVER FORWARD PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACE D MODULE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300578 19990903 00578 EU 1999 9 3 UF6A990559 1 19990525 A 5230 SP4YB3 HINGE PIN BAG ATP ATP EU CARGO DOOR BROKEN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 ORD - FLT 5753 - HINGE PIN BROKEN ON AFT BAGGAGE DOOR. MAINTENANCE REMOVED AND REPLACED THE LOWER ALIGNMENT HINGE PIN. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300579 19990903 00579 EU 1999 9 3 UF6A990560 1 19990525 A 3350 1317 BULB BAG ATP ATP EU LT EMER EXIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 SBN - LEFT AFT OVERWING EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300580 19990903 00580 EU 1999 9 3 UF6A990561 1 19990525 A 3350 0L3071BPEGPL BULB BAG ATP ATP EU EMER EXIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 SBN - INTERIOR EMERGENCY OVERWING EXIT LIGHT FILAMENTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300581 19990903 00581 EU 1999 9 3 UF6A990562 1 19990526 A 2730 100G3160 BEARING HINGE BAG ATP ATP EU RT ELEVATOR WORN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 YNG - FLT 5711 - RIGHT ELEVATOR OUTBOARD HINGE POINT IS LOOSE. MAINTENANCE REMOVED AND REPLACED OUTER BEARING. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300582 19990903 00582 EU 1999 9 3 UF6A990551 1 19990515 A 5754 BAEREFJ8724 HINGE BAG ATP ATP EU LT LE FLAP CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - HINGE ON LEFT INBOARD LEADING EDGE IS WORN. MAINTENANCE REMOVED AND REPLACED HINGE. (M) 2 L 7 2 4T RT A27NM 1999090300583 19990903 00583 EU 1999 9 3 UF6A990557 1 19990521 A 3350 1317 BULB BAG ATP ATP EU EMER EXIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 SBN - EMERGENCY LIGHTING ON THE RIGHT SIDE AFT OVERWING IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1999090300584 19990903 00584 EU 1999 9 3 UF6A990558 1 19990519 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU ROW 13 FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 855AW 13650 17399 2029 ORD - EMERGENCY FLOOR STRIP AT ROW 13 IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 6 POWER SUPPLY. SYSTEM OPS C HECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300585 19990903 00585 EU 1999 9 3 UF6A990552 1 19990515 A 5320 JD790J0001002 BRACKET BAG ATP ATP EU BS 101.254 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT OIL COOLER HAT CHANNEL BRACKET IS CRACKED. MAINTENANCE REPAIRED BRACKET IAW BAE ATP SRM 51-10-00. AREA WAS ALODINED AND PRIMED. (M) 2 L 7 2 4T RT A27NM 1999090300586 19990903 00586 EU 1999 9 3 UF6A990553 1 19990515 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU ROW 12 FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 7921 16376 2036 ORD - FLT 5748 - CABIN OVERHEAD EMERGENCY LIGHTS PAST ROW 12 AND AFT EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 6 POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300587 19990903 00587 EU 1999 9 3 UF6A990554 1 19990516 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 SBN - LEFT AFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD . (M) 2 L 7 2 4T RT A27NM 1999090300588 19990903 00588 EU 1999 9 3 UF6A990555 1 19990517 A 3350 JD920J0531206 LIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FLT 5723 - SEVERAL EMERGENCY FLOOR LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FLOOR PROXIM ITY LIGHT STRIP. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300589 19990903 00589 NE 1999 9 3 UF6A990556 2 19990517 A 7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE NR 2 SMOKING A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 855AW 2029 124419 ORD - FLT 5702 - SMOKE EMANATING FROM THE NR 2 ENGINE ON TAXI IN FROM LANDING. MAINTENANCE PERFORMED DRY MOTOR OF ENGIN E AND NORMAL ENGINE RUNS WITH NO DEFECTS NOTED. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999090300590 19990903 00590 EU 1999 9 3 UF6A990550 1 19990515 A 5754 JD574J0099000 HINGE BAG ATP ATP EU LE FLAPS CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - HINGE ON PANEL 522AT IS CRACKED AT BOTH ENDS. MAINTENANCE REMOVED AND REPLACED HINGE. (M) 2 L 7 2 4T RT A27NM 1999090300591 19990903 00591 EU 1999 9 3 UF6A990549 1 19990515 A 5530 JD553J0410000 ANGLE BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT SIDE OF VERTICAL STABILIZER HAS A CRACK LOCATED ON THE TOP FAIRING ANGLE. MAINTENANCE FABRICATED ANGLE TO NE ST IN THE END OF THE FAIRING. ANGLE WAS MADE 2024-T3, .071 INCH THICK. ALL WORK WAS PERFORMED IAW ENGINEERING ORDER NR 99-091. (M) 2 L 7 2 4T RT A27NM 1999090300592 19990903 00592 EU 1999 9 3 UF6A990743 1 19990716 A 5330 SKIN BAG ATP ATP EU BS 325 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - DENT ON FUSELAGE BELOW AND AFT OF REAR BAGGAGE DOOR. MAINTENANCE REPAIRED DENT IAW BAE ATP SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999090300593 19990903 00593 EU 1999 9 3 UF6A990742 1 19990716 A 5330 SKIN BAG ATP ATP EU BS 378 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - DENT ON TOP OF FUSELAGE AT RIGHT WINDSCREEN. MAINTENANCE REPAIRED DENT IAW BAE ATP SRM 51-30-01, 53-30-00. (M) 2 L 7 2 4T RT A27NM 1999090300594 19990903 00594 EU 1999 9 3 UF6A990741 1 19990716 A 5330 SKIN BAG ATP ATP EU FUSELAGE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - SKIN CRACKED ON UPPER RADOME HINGE ON FUSELAGE. MAINTENANCE REPAIRED CRACK IAW BAE ATP SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300595 19990903 00595 EU 1999 9 3 UF6A990740 1 19990716 A 5347 JD533J0016000 SEAT RAIL BAG ATP ATP EU FS 252-270 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - SEAT RAIL CORRODED BETWEEN STATION 252AS AND 270AS. MAINTENANCE REPLACED IAW BAE ATP SRM 53-10-13. (M) 2 L 7 2 4T RT A27NM 1999090300596 19990903 00596 EU 1999 9 3 UF6A990739 1 19990716 A 5315 JD533J0245000 FLOORBEAM BAG ATP ATP EU BS 270 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - FLOORBEAM AT STATION 270AS CORRODED. MAINTENANCE REPAIRED FLOORBEAM IAW DER 99-131 AND BAE ATP SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300597 19990903 00597 EU 1999 9 3 UF6A990738 1 19990716 A 5320 240D11186 INTERCOSTAL BAG ATP ATP EU BS 343-360.5 BENT A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - INTERCOSTAL FROM STATION 343AS TO 360AS IS BENT. MAINTENANCE REPLACED INTERCOSTAL IAW BAE ATP SRM 51-60-04 AND 51 -30-01. (M) 2 L 7 2 4T RT A27NM 1999090300598 19990903 00598 EU 1999 9 3 UF6A990737 1 19990716 A 5320 240D11186 INTERCOSTAL BAG ATP ATP EU BS 308/325.5 BENT A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - RIGHT INTERCOSTAL FROM STATION 308AS TO 325AS IS BENT. MAINTENANCE REPLACED INTERCOSTAL IAW BAE ATP SRM 51-60-04 AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300599 19990903 00599 EU 1999 9 3 UF6A990736 1 19990716 A 5315 1D11905 FLOORBEAM BAG ATP ATP EU BS 325.5 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - FLOORBEAM CAPPING STRIP CORRODED AT STATION 325.5AS. MAINTENANCE REPLACED CAPPING STRIP IAW BAE ATP SRM 51-60-03 AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300600 19990903 00600 EU 1999 9 3 UF6A990745 1 19990716 A 5720 ANGLE BAG ATP ATP EU WS 101.254 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - LEFT MODULE 7 HAS INTERNAL CRACK. MAINTENANCE REPAIRED CRACKED IAW BAE ATP SRM 51-60-01, FIG 2. (M) 2 L 7 2 4T RT A27NM 1999090300601 19990903 00601 EU 1999 9 3 UF6A990746 1 19990716 A 5320 BRACKET BAG ATP ATP EU E/E COMPT CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - RIGHT AND LEFT AFT AVIONICS CRATE FORWARD BRACKETS CRACKED. MAINTENANCE REPLACED BRACKETS IAW BAE ATP SRM 51-60-0 4, 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300602 19990903 00602 EU 1999 9 3 UF6A990748 1 19990716 A 5330 SKIN BAG ATP ATP EU BS 431/398 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - DAMAGE TO RIGHT SIDE OF FUSELAGE AT STATION 408FS TO 422FS AND BETWEEN WINDOW FRAME AND STRINGER 15S. MAINTENANCE REPAIRED DAMAGE IAW DER 99-131 AND BAE ATP SRM 53-30-00. (M) 2 L 7 2 4T RT A27NM 1999090300603 19990903 00603 EU 1999 9 3 UF6A990747 1 19990716 A 5320 BRACKET BAG ATP ATP EU E/E COMPT CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - RIGHT AND LEFT AVIONICS CRATE AFT BRACKETS CRACKED. MAINTENANCE REPLACED BRACKETS IAW BAE ATP SRM 51-60-04, 51-30 -01. (M) 2 L 7 2 4T RT A27NM 1999090300604 19990903 00604 EU 1999 9 3 UF6A990744 1 19990716 A 5414 SKIN BAG ATP ATP EU RT NACELLE BURNED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - LIGHTNING STRIKE DAMAGE OUTBOARD SIDE OF NR 2 NACELLE. MAINTENANCE REPAIRED DAMAGE IAW BAE ATP SRM 51-60-01, FIG 1. (M) 2 L 7 2 4T RT A27NM 1999090300605 19990903 00605 EU 1999 9 3 UF6A990732 1 19990714 A 5330 SKIN BAG ATP ATP EU FS 431.75 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - DENT ON RIGHT SIDE OF FUSELAGE AT STRINGER 24 AND STATION 431.75. MAINTENANCE REPAIRED DAMAGE IAW BAE ATP SRM 53- 30-00 FIG 202. TREATED IAW BAE ATP SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300606 19990903 00606 EU 1999 9 3 UF6A990728 1 19990714 A 5530 JD553J0048000 ANGLE BAG ATP ATP EU VERT STAB RIB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - VERTICAL STAB LOWER ATTACHMENT ANGLE BETWEEN VERTICAL WEB AND HINGE BOX WEB IS CRACKED. MAINTENANCE REPAIRED CRAC KED IAW BAE ATP SRM 55-30-00, 51-10-06 AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300607 19990903 00607 EU 1999 9 3 UF6A990729 1 19990714 A 5530 JD553J0416202 CHANNEL BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - CRACK ON LEFT SIDE CHANNEL OF BOTTOM RUDDER HINGE BOX, AROUND RIB STATION 29.53. MAINTENANCE REPLACED CHANNEL IAW BAE ATP SRM 55-30-00, 51-10-03. TREATED AND PRIMED IAW BAE SRM 51-10-06. (M) 2 L 7 2 4T RT A27NM 1999090300608 19990903 00608 EU 1999 9 3 UF6A990730 1 19990714 A 5530 JD553J0416204 ANGLE BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - LOWER ATTACHMENT ANGLE ON VERTICAL STAB AT RUDDER LOWER HINGE POINT CRACKED AT RIB STATION 29.53. MAINTENANCE REP LACED CHANNEL IAW BAE ATP SRM 55-30-00. TREATED AND PRIMED IAW BAE SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300609 19990903 00609 EU 1999 9 3 UF6A990731 1 19990714 A 5530 21H2664 SHROUD BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - CRACK IN UPPER LEFT CORNER OF SHROUD AT LOWER HINGE POINT AT RIB STATION 29.53. MAINTENANCE REPLACED SHROUD IAW B AE ATP SRM 55-30-00 AND 51-10-03. TREATED AND PRIMED IAW BAE SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300610 19990903 00610 EU 1999 9 3 UF6A990733 1 19990714 A 5350 JD553J0410000 FAIRING BAG ATP ATP EU FUS/VERT STAB CRACK A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - CRACK ON LEFT VERTICAL STAB FAIRING. MAINTENANCE REPAIRED CRACK IAW DER 99-131 AND BAE ATP SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300611 19990903 00611 EU 1999 9 3 UF6A990734 1 19990714 A 5350 JD553J0410001 FAIRING BAG ATP ATP EU FUS/VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - RIGHT VERTICAL STAB TO FUSELAGE ANGLE CRACKED AROUND AFT RIVET. MAINTENANCE REPAIRED CRACK IAW DER 99-131 AND BAE ATP SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999090300612 19990903 00612 EU 1999 9 3 UF6A990735 1 19990716 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU GALLEY FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 11606 17370 2034 SBN - EMERGENCY LIGHTS INOPERATIVE IN AFT GALLEY. MAINTENANCE REPLACED POWER SUPPLY NR 7 BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300613 19990903 00613 EU 1999 9 3 UF6A990727 1 19990714 A 5530 JD553J0312000 ANGLE BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - ANGLE CRACKED ON VERTICAL STAB AT RIB 47.78. MAINTENANCE REPAIRED CRACK IAW BAE ATP SRM 51-30-01 AND 51-10-06. ( M) 2 L 7 2 4T RT A27NM 1999090300614 19990903 00614 EU 1999 9 3 UF6A990726 1 19990712 A 5320 JD537J0005000W CHANNEL BAG ATP ATP EU BS 461 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - CRACK ON 'L' CHANNEL AROUND EDGE AT 7 O'CLOCK POSITION. MAINTENANCE BLENDED OUT DAMAGED AREA, PRIMED AND TREATED IAW BAE SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999090300615 19990903 00615 EU 1999 9 3 UF6A990725 1 19990712 A 5542 SKIN BAG ATP ATP EU RUDDER CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - CRACK IN THE RUDDER SKIN AT LEADING EDGE ABOVE BOTTOM HINGE POINT. MAINTENANCE REPAIRED CRACK IAW BAE SRM 51-60-0 1 AND 55-60-01. (M) 2 L 7 2 4T RT A27NM 1999090300616 19990903 00616 EU 1999 9 3 UF6A990724 1 19990712 A 5414 SKIN BAG ATP ATP EU LEFT NACELLE LOOSE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - SEVERAL WORKING RIVETS ON MOD 4 SKIN OUTBOARD SIDE. MAINTENANCE REPLACED SKIN AND REPAIRED IAW BAE SRM 51-10-03 A ND 51-10-06. (M) 2 L 7 2 4T RT A27NM 1999090300617 19990903 00617 EU 1999 9 3 UF6A990723 1 19990712 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU COCKPIT FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 12238 2021 SBN - FLT 5757 - COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. OPS CHEC K GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300618 19990903 00618 EU 1999 9 3 UF6A990722 1 19990712 A 5330 SKIN BAG ATP ATP EU BS 398, 162/325 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - SEVERAL LIGHTNING STRIKE TRACES ALONG BOTTOM OF FUSELAGE AT STATIONS 398 FS, 162 FS, AND 325.5 AS. MAINTENANCE R EPAIRED DAMAGED AREAS IAW BAE ATP SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999090300619 19990903 00619 EU 1999 9 3 UF6A990720 1 19990712 A 5320 383D11186 INTERCOSTAL BAG ATP ATP EU BS 90 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - NR 2 TEMP CONTROL VALVE BRACKET CRACKED. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-60-04 AND 51-40-01. (M) 2 L 7 2 4T RT A27NM 1999090300620 19990903 00620 EU 1999 9 3 UF6A990721 1 19990712 A 5320 239D11186 INTERCOSTAL BAG ATP ATP EU BS 325.5 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - INTERCOSTAL CRACKED IN REAR BAGGAGE AREA AT STATION 325.5AS. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-60-0 4. (M) 2 L 7 2 4T RT A27NM 1999090300621 19990903 00621 EU 1999 9 3 UF6A990719 1 19990712 A 5320 112D11186 INTERCOSTAL BAG ATP ATP EU BS 270-289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - AFT BAGGAGE DOOR THRESHOLD INTERCOSTAL CORRODED. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-60-04. (M) 2 L 7 2 4T RT A27NM 1999090300622 19990903 00622 EU 1999 9 3 UF6A990717 1 19990712 A 5330 SKIN BAG ATP ATP EU BS 180 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - PUNCTURE ON FUSELAGE BEHIND ICESHIELD AT STATION 180 FS AND STRINGER 20. MAINTENANCE REPAIRED DENT IAW BAE SRM 51 -30-00 FIG 201. (M) 2 L 7 2 4T RT A27NM 1999090300623 19990903 00623 EU 1999 9 3 UF6A990718 1 19990712 A 5320 10D11186 INTERCOSTAL BAG ATP ATP EU BS 270-289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - AFT PASSENGER DOOR THRESHOLD INTERCOSTAL CORRODED. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-60-04. (M) 2 L 7 2 4T RT A27NM 1999090300624 19990903 00624 EU 1999 9 3 UF6A990606 1 19990604 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - EMERGENCY LIGHT ON EXTERIOR OF AIRCRAFT, AFT OF RIGHT SIDE EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1999090300625 19990903 00625 EU 1999 9 3 UF6A990603 1 19990605 A 5330 SKIN BAG ATP ATP EU BS 252 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 SBN - DENT FOUND ON RIGHT SIDE OF AIRCRAFT FORWARD OF AFT BAGGAGE DOOR AT STATION 252AS. MAINTENANCE REPAIRED DENT IAW BAE ATP SRM 51-60-01 AND 51-10-06. (M) 2 L 7 2 4T RT A27NM 1999090300626 19990903 00626 EU 1999 9 3 UF6A990758 1 19990723 A 5320 459SS3075 SUPPORT BAG ATP ATP EU BS 271-343 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - CENTER FLOOR SUPPORT IN AFT BAGGAGE AREA IS HEAVILY CORRODED. MAINTENANCE FABRICATED NEW ANGLE AS PER SAMPLE AND INSTALLED. ALL WORK WAS DONE IAW DER REPORT NR 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300627 19990903 00627 EU 1999 9 3 UF6A990759 1 19990723 A 5414 JD711J0219000 SKIN BAG ATP ATP EU NACELLE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE NR 2 MOD 6 IS CRACKED AT APPROX THE 7 O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PARTIAL SKIN REPLACEMENT. ALL WORK WAS DONE IAW DER REPORT NR 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300628 19990903 00628 EU 1999 9 3 UF6A990757 1 19990720 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU ROW 12CD INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 13230 16867 2022 ORD - EMERGENCY FLOOR STRIP INOPERATIVE AT ROW 12C/D AS WELL AS OVERHEAD BIN. MAINTENANCE REMOVED AND REPLACED THE NR 5 POWER SUPPLY. (M) 2 L 7 2 4T RT A27NM 1999090300629 19990903 00629 NE 1999 9 3 UF6A990756 2 19990721 A 7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE NR 1 FAILED A UF6A K NONE M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 31 854AW 12728 2028 124224 SBN - FLT 5762 - ITT EXCEEDED 800 DEGREES DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. SYSTEM OPS C HECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999090300630 19990903 00630 EU 1999 9 3 UF6A990749 1 19990720 A 5315 JD533J0079000 FLOORBEAM BAG ATP ATP EU BS 378 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - FOUND CORROSION ON ANGLE UNDER FLOOR AT STATION 378FS. MAINTENANCE REMOVED CORROSION BY MECHANICAL METHODS AND FA BRICATED NEW SPLICE PLATE FROM ALCLAD 2024T3 .123. ALL WORK WAS DONE IAW DER REPORT 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300631 19990903 00631 EU 1999 9 3 UF6A990751 1 19990720 A 5512 SKIN BAG ATP ATP EU HORIZ STAB DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - DENT IN TRAILING EDGE OF THE RIGHT HORIZONTAL STABILIZER INBOARD OF THE INBOARD HINGE. MAINTENANCE REPAIRED DENT. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-01. (M) 2 L 7 2 4T RT A27NM 1999090300632 19990903 00632 EU 1999 9 3 UF6A990752 1 19990720 A 5320 890310338 ANGLE BAG ATP ATP EU BS 308 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - HEAVY CORROSION AND CRACKING ON THE AFT BAGGAGE COMPARTMENT BULKHEAD AT THE LOWER CORNER WHERE THE BIFOLD DOOR ATT ACHES. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ANGLE. ALL WORK WAS DONE IAW BAE ATP SRM 51-30-07. (M) 2 L 7 2 4T RT A27NM 1999090300633 19990903 00633 EU 1999 9 3 UF6A990753 1 19990720 A 5230 JD256J0064001 BRACKET BAG ATP ATP EU CARGO DOOR DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - REAR BAGGAGE DOOR EMERGENCY SLIDE FORWARD ATTACHMENT BRACKET IS CRACKED. MAINTENACNE REMOVED AND REPLACED THE BRA CKET. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-06. (M) 2 L 7 2 4T RT A27NM 1999090300634 19990903 00634 EU 1999 9 3 UF6A990754 1 19990720 A 5230 JD256J0064001 BRACKET BAG ATP ATP EU CARGO DOOR DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - REAR BAGGAGE DOOR EMERGENCY SLIDE AFT ATTACHMENT BRACKET IS CRACKED. MAINTENANCE REMOVED AND REPLACED THE BRACKET . ALL WORK WAS DONE IAW BAE ATP SRM 51-10-06. (M) 2 L 7 2 4T RT A27NM 1999090300635 19990903 00635 EU 1999 9 3 UF6A990755 1 19990717 A 3350 LIGHT BAG ATP ATP EU ROW 11-14 INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 ORD - FLT 5730 - FLOOR EMERGENCY LIGHTS IN ROW 11 TO 14 AS WELL AS THE OVERHEAD LIGHTS ARE INOPERATIVE. MAINTENANCE PER FORMED OPS CHECK OF THE SYSTEM WITH NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1999090300636 19990903 00636 EU 1999 9 3 UF6A990750 1 19990720 A 5530 ANGLE BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - UPPER ATTACHMENT ANGLE ON THE VERTICAL STABILIZER AT THE LOWER RUDDER HINGE POINT IS CRACKED AT RIB 29.53. MAINTE NANCE FABRICATED ANGLE PER SAMPLE AND INSTALLED. ALL WORK WAS DONE IAW BAE SRM 55-30-00, 51-30-01, AND 51-10-06. (M) 2 L 7 2 4T RT A27NM 1999090300637 19990903 00637 EU 1999 9 3 UF6A990602 1 19990603 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU ROW 10-12 INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 11663 16879 2035 SBN - FLOOR EMERGENCY EXIT LIGHT IS INOPERATIVE AT ROWS 10 THROUGH 12. MAINTENANCE REMOVED AND REPLACED NR 5 POWER SUPP LY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300638 19990903 00638 EU 1999 9 3 UF6A990601 1 19990603 A 3350 OL1793BAE BULB BAG ATP ATP EU PAX DOORWAY FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 SBN - EMERGENCY EXIT LIGHT AT THE FORWARD PASSENGER DOOR IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300639 19990903 00639 EU 1999 9 3 UF6A990764 1 19990728 A 5753 JD275J0036008 SKIN BAG ATP ATP EU LT TE FLAP CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE LEFT INBOARD FLAP TAB HAS APPROXIMATELY A 3 INCH CRACK LOCATED ON THE VERY OUTBOARD EDGE. MAINTENANCE REMOVED DAMAGED AND REPAIRED. ALL WORK WAS DONE IAW BAE ATP SRM 57-50-01. (M) 2 L 7 2 4T RT A27NM 1999090300640 19990903 00640 EU 1999 9 3 UF6A990763 1 19990728 A 5753 JD275J0036011 SKIN BAG ATP ATP EU RT TE FLAP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE RIGHT OUTBOARD FLAP TAB HAS SKIN MISSING ON TRAILING EDGE. MAINTENANCE REPAIRED FLAP TAB DAMAGE. ALL WORK WA S DONE IW BAE ATP SRM 57-51-01 FIGURE 202. (M) 2 L 7 2 4T RT A27NM 1999090300641 19990903 00641 EU 1999 9 3 UF6A990762 1 19990728 A 5753 JD275J0036011 SKIN BAG ATP ATP EU RT TE FLAP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE RIGHT OUTBOARD FLAP TAB HAS PULLED RIVETS AND DAMAGED SKIN. MAINTENANCE REPAIRED FLAP TAB DAMAGE. ALL WORK W AS DONE IAW BAE ATP SRM 57-50-01 FIGURE 202. (M) 2 L 7 2 4T RT A27NM 1999090300642 19990903 00642 EU 1999 9 3 UF6A990761 1 19990727 A 5540 23H2663 BRACKET BAG ATP ATP EU RUDDER CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE LOWER RUDDER HINGE DAGGER BRACKET ON THE LEFT SIDE IS CRACKED. MAINTENANCE FABRICATED NEW BRACKET PER SAMPLE AND INSTALLED. ALL WORK WAS DONE IAW BAE ATP SRM 55-30-00 AND 51-10-00. (M) 2 L 7 2 4T RT A27NM 1999090300643 19990903 00643 EU 1999 9 3 UF6A990760 1 19990727 A 5753 CON697211 HINGE BAG ATP ATP EU RT TE FLAP CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE RIGHT INBOARD LEADING EDGE HAS A CRACK ON THE BOTTOM OF THE OUTBOARD HINGE. MAINTENANCE REMOVED AND REPLACED HINGE. ALL WORK WAS DONE IAW BAE ATP MM 57-40-00. (M) 2 L 7 2 4T RT A27NM 1999090300644 19990903 00644 EU 1999 9 3 UF6A990770 1 19990728 A 5532 JD553J0001000 SKIN BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE VERTICAL STABILIZER NEAR ACCESS PANEL 321AL IS CRACKED. MAINTENANCE REMOVED DAMAGED AREA AND FABRICATED NEW S KIN WITH 2024T3 .050 AND INSTALLED. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300645 19990903 00645 EU 1999 9 3 UF6A990769 1 19990728 A 5330 SKIN BAG ATP ATP EU BS 431.75 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE RIGHT SIDE OF THE FUSELAGE BELOW THE WATER LINE IS DENTED AT STRINGER 24 AND STATION 431.75FS. MAINTENANCE RE CONTOURED DAMAGED AREA, BLENDED AND REPROTECTED. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999090300646 19990903 00646 EU 1999 9 3 UF6A990768 1 19990728 A 5230 JD523J0063002 PATCH BAG ATP ATP EU CARGO DOOR TORN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE REAR BAGGAGE DOOR REINFORCING PATH IS TORN ON LEFT SIDE, BOTTOM. MAINTENANCE REPAIRED REINFORCING PATH. ALL WORK WAS DONE IAW ENGINEERING ORDER NR 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300647 19990903 00647 EU 1999 9 3 UF6A990767 1 19990728 A 5230 JD523J0063002 SKIN BAG ATP ATP EU CARGO DOOR DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE REAR BAGGAGE DOOR EDGE MEMBER HAS A DENT ON THE UPPER LEFT SIDE. MAINTENANCE REPAIRED DENT. ALL WORK WAS DON E IAW ENGINEERING ORDER NR 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300648 19990903 00648 EU 1999 9 3 UF6A990766 1 19990728 A 5540 JD55420140000 HINGE BAG ATP ATP EU RUDDER CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE BOTTOM RUDDER HINGE, UPPER SIDE OF THE BEARING HOUSING PLATE IS CRACKED ON LEFT SIDE. MAINTENANCE REPAIRED HI NGE. ALL WORK WAS DONE IAW ENGINEERING ORDER NR 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300649 19990903 00649 EU 1999 9 3 UF6A990765 1 19990728 A 5540 JD55420140000 HINGE BAG ATP ATP EU RUDDER CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE BOTTOM RUDDER HINGE, UPPER SIDE OF THE BEARING HOUSING PLATE IS CRACKED ON RIGHT SIDE. MAINTENANCE REPAIRED H INGE. ALL WORK WAS DONE IAW ENGINEERING ORDER NR 99-131. (M) 2 L 7 2 4T RT A27NM 1999090300650 19990903 00650 1999 9 3 UF6A990778 4 19990731 A 3442 071131900 RADAR BAG ATP ATP EU COCKPIT FAILED A UF6A A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 856AW 691 3503 2032 ORD - FLT 5711 - WEATHER RADAR TESTED NORMAL BUT PAINTED NOTHING, TX FLIGHT. MESSAGE DISPLAYED. MAINTENANCE REPLACED W EATHER RADAR TRANSMITTER/RECEIVER. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300651 19990903 00651 EU 1999 9 3 UF6A990771 1 19990726 A 3350 1317 BULB BAG ATP ATP EU LAVATORY FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 ORD - FLT 5705 - EMERGENCY LIGHT IN LAVATORY IS INOPERATIVE. MAINTENANCE REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1999090300652 19990903 00652 EU 1999 9 3 UF6A990711 1 19990710 A 3350 6013211 BATTERY PACK GRIMES BAG ATP ATP EU ROW 14 DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 11453 17369 2034 ORD - FLOOR EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 14. MAINTENANCE REMOVED AND REPLACED NR 7 BATTERY PACK. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300653 19990903 00653 EU 1999 9 3 UF6A990701 1 19990701 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 851AW 10306 ATPCO127 2020 SBN - FLT 5753 - DURING TAKEOFF ROLL, THE RIGHT PROP CWP ILLUMINATED WITH ASSOCIATED CYCLING OF THE RED LOW PITCH LIGHT. RIGHT TORQUE REACHED 128 PERCENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 PCU. PERFORMED 2 HIGH SPEED TAXIES WITH NO CWP OR LOW PITCH LIGHTS ILLUMINATING. PERFORMED DOWNLOAD OF FDR AND DETERMINED THAT TORQUE HAD ONLY REACHED 110 PERC ENT AND BEGAN DECREASING. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300654 19990903 00654 EU 1999 9 3 UF6A990624 1 19990630 A 2150 JD210J0107000 CLAMP BAG ATP ATP EU BS 90 FAILED A UF6A A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 852AW 2021 FWA - FLT 5728 - SMOKE IN COCKPIT AND CABIN WITH THE NR 1 ENGINE RUNNING. MAINTENANCE REMOVED AND REPLACED THE GAMAH CL AMP ON THE NR 1 HEAT EXCHANGER DUCT. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300655 19990903 00655 EU 1999 9 3 UF6A990705 1 19990705 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 13359 13359 2034 ORD - FLOOR PROXIMITY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 6 POWER SUPPLY. SYSTEM OPS CHECKED GO OD. (M) 2 L 7 2 4T RT A27NM 1999090300656 19990903 00656 NE 1999 9 3 UF6A990704 2 19990703 A 7210 3035480 REDUCT GEARBOX BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE CONTAMINATED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 10111 124419 2028 124219 SBN - THE NR 2 REDUCTION GEARBOX OIL ANALYSIS IS SHOWING A HIGH CONCENTRATION OF METAL. MAINTENANCE REMOVED AND REPLACE D THE NR 2 REDUCTION GEARBOX. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999090300657 19990903 00657 EU 1999 9 3 UF6A990703 1 19990702 A 2120 AIR DIST BAG ATP ATP EU GALLEY ODOR A UF6A O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 31 853AW 2022 GRB - FLT 5759 - FLIGHT ATTENDANT B NOTICED A BURNING SMELL IN GALLEY DURING FLIGHT. MAINTENANCE RAN BOTH ENGINES WITH NO SIGN OR SMELL OF SMOKED NOTICED. (M) 2 L 7 2 4T RT A27NM 1999090300658 19990903 00658 EU 1999 9 3 UF6A990702 1 19990701 A 3260 OL6034 BULB BAG ATP ATP EU NLG FAILED A UF6A K NONE P NO WARNING INDICATION LD LANDING 1 GL 31 859AW 2036 FWA - FLT 5728 - DURING GEAR DOWN SELECTION DID NOT GET GREEN NOSE LANDING GEAR INDICATION. PERFORMED LEGEND TEST WITH NO GREEN LIGHT. MAINTENANCE REMOVED AND REPLACED PBSI LAMP. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300659 19990903 00659 EU 1999 9 3 UF6A990707 1 19990831 A 5330 SKIN BAG ATP ATP EU BS 418-431 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - DENT FOUND ON THE LEFT FORWARD PRESSURE FUSELAGE AT STRINGER 27 BETWEEN STATIONS 431FS AND 418FS. MAINTENANCE REC ONTOURED, CLEANED, AND BURNISHED DENT. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-014. (M) 2 L 7 2 4T RT A27NM 1999090300660 19990903 00660 EU 1999 9 3 UF6A990706 1 19990708 A 3250 STEERING BAG ATP ATP EU NLG MALFUNCTIONED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 852AW 2021 ORD - FLT 5703 - DIFFICULTY TO MAINTAIN DIRECTIONAL CONTROL ON TAKEOFF ROLL. MAINTENANCE PERFORMED TWO HIGH SPEED TAXIE S FOR OPERATIONAL CHECK OF NOSE WHEEL STEERING. SYSTEM OPS CHECKED GOOD WITH NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1999090300661 19990903 00661 NE 1999 9 3 UF6A990708 2 19990708 A 7210 3035480 REDUCT GEARBOX BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 11309 124414 2020 124223 SBN - THE NR 2 REDUCTION GEARBOX OIL ANALYSIS IS SHOWING A HIGH CONCENTRATION OF METAL. MAINTENANCE REMOVED AND REPLACE D THE NR 2 REDUCTION GEAR BOX. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999090300662 19990903 00662 EU 1999 9 3 UF6A990709 1 19990706 A 5330 SKIN BAG ATP ATP EU BS 162 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - DENT FOUND ON THE RIGHT OF THE FUSELAGE AT STATIONS 162FS. MAINTENANCE REMOVED DENT IAW BAE ATP SRM 51-10-01 AND INSTALLED ANTI-PAINT STIFFENER IAW BAE ATP SRM 51-60-01. (M) 2 L 7 2 4T RT A27NM 1999090300663 19990903 00663 EU 1999 9 3 UF6A990710 1 19990710 A 3350 6013211 BATTERY PACK GRIMES BAG ATP ATP EU ROW 14 DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 7941 16376 2034 ORD - FLOOR EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 14. MAINTENANCE REMOVED AND REPLACED NR 6 BATTERY PACK. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300664 19990903 00664 EU 1999 9 3 UF6A990618 1 19990624 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 SBN - LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300665 19990903 00665 EU 1999 9 3 UF6A990620 1 19990627 A 5330 JD528J0027002W SKIN BAG ATP ATP EU BS 101.254 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 SBN - LEFT MODULAR 4 OUTBOARD SKIN PANEL IS CRACKED AND THE CHANNEL IS ALSO CRACKED. MAINTENANCE REPAIRED THE LEFT MODU LAR 4 OUTBOARD SKIN PANEL AND CHANNEL IAW BAE ATP SRM 51-60-04 AND 01. (M) 2 L 7 2 4T RT A27NM 1999090300666 19990903 00666 EU 1999 9 3 UF6A990619 1 19990627 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 13284 16924 2034 SBN - FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300667 19990903 00667 EU 1999 9 3 UF6A990622 1 19990629 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 12185 17248 2022 ORD - REAR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 7 EMERGENCY POWER SUPPLY. SYSETM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999090300668 19990903 00668 EU 1999 9 3 UF6A990623 1 19990630 A 6120 8022631 SEALS BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE FAILED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 851AW 12185 2020 124015 GRB - THE NR 2 PROP CWP ILLUMINATED WHEN POWER WAS ADVANCED ON TAKEOFF AND LEFT ENGINE WENT INTO UNCOMMANDED REVERSE DUR ING ABORTED TAKEOFF. MAINTENANCE REMOVED PROP TRANSFER TUBE SEALS. PERFORMED CHECK OF PROP SYNC SYSTEM AND RAN BOTH EN GINES TO 85 PERCENT TORQUE. ALL SYSTEMS OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999090300669 19990903 00669 EU 1999 9 3 UF6A990714 1 19990712 A 5330 SKIN BAG ATP ATP EU BS 324-343 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - DENT ON FUSELAGE BETWEEN STATIONS 324FS AND 343FS BELOW STRINGER 44. MAINTENANCE REPAIRED DENT IAW BAE SRM 51-10- 01, BLENDED DAMAGE, ALODINED, PRIMED AND PAINTED. (M) 2 L 7 2 4T RT A27NM 1999090300670 19990903 00670 EU 1999 9 3 UF6A990712 1 19990712 A 5532 JD553J0015000 SKIN BAG ATP ATP EU VERT STAB DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 14663 2036 SBN - PIN HOLE VERTICAL STABILIZER AT STATION 351.75. MAINTENANCE REPAIRED THE HOLE IAW BAE SRM 51-60-01. (M) 2 L 7 2 4T RT A27NM 1999090300671 19990903 00671 NM 1999 9 3 USAA990455 1 19990509 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 1540-1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 19522 27198 CLT - DURING C-4 CHECK, FOUND AFT END OF SEAT TRACK CORRODED 100 INCHES AT RBL 24.5 BETWEEN STATION 1540 AND STATION 164 0, CORROSION LEVEL 2. REPLACED SEAT TRACK BETWEEN STATION 1540 AND 1640 PER SRM 51-10-00 AND BOEING DRAWING NR 146N210. (M) 2 L 7 2 4F RT A2NM 1999090300672 19990903 00672 NM 1999 9 3 USAA990454 1 19990509 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1660 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 19522 27198 CLT - DURING C-4 CHECK, FOUND CORROSION AROUND NUT PLATE .5 INCH BY .5 INCH AT STATION 1660, RBL 26, SURFACE CORROSION O N TOP OF FLOORBEAM, CORROSION LEVEL 2. CUT OUT 2 INCH BY 2.5 INCH AREA OF FLOORBEAM TOP, TWO DOUBLER ANGLES AND A FILL ER PER SRM 53-00-51, SIG 205. (M) 2 L 7 2 4F RT A2NM 1999090300673 19990903 00673 NM 1999 9 3 USAA990465 1 19990509 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM BS 1650-1660 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 19522 27198 CLT - DURING C-4 CHECK, FOUND 20 INCH OF HEAVY CORROSION ON UPPER SURFACE OF INTERCOSTAL BETWEEN STATION 1640 TO 1660 AT BL 0. CORROSION TASK NR C53-252-03, C53-251-03, CORROSION LEVEL 2. INSTALLED NEW INTERCOSTAL PER 757-200 SRM 51-10-00 . (M) 2 L 7 2 4F RT A2NM 1999090300674 19990903 00674 NM 1999 9 3 USAA990464 1 19990509 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 19522 27198 CLT - DURING C-4 CHECK, FOUND 2 INCH CORROSION ALONG UPPER SURFACE FLOORBEAM AT STATION 1640. CORROSION TASK NR C53-252 -03, C53-251-03, CORROSION LEVEL 2. INSTALLED NEW T-CAP ON FLOORBEAM PER 757-200 TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1999090300675 19990903 00675 NM 1999 9 3 USAA990453 1 19990509 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM BS 365-377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 19522 27198 CLT - DURING C-4 CHECK, FOUND CORROSION 12 INCH IN LENGTH AT INTERCOSTAL AT FORWARD CABIN STATION 365-377 RBL 12, CORROS ION LEVEL 2. INSTALLED NEW INTERCOSTAL (FABRICATED) PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999090300676 19990903 00676 NM 1999 9 3 USAA990451 1 19990509 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 1540 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 27198 CLT - DURING C-4 CHECK, FOUND SEAT TRACK CORRODED 100 INCHES ON AFT END BETWEEN BS 1540 AND BS 1640 OUTBOARD ON LEFT SID E, CORROSION LEVEL 2. REPLACED SEAT TRACK BETWEEN BS 1540 AND BS 1640 PER SRM 51-10-00 AND BOEING DRAWING NR 146N5120. (M) 2 L 7 2 4F RT A2NM 1999090300677 19990903 00677 NM 1999 9 3 USAA990452 1 19990509 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 1540 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 19522 27198 CLT - DURING C-4 CHECK, FOUND 100 INCH OF CORROSION ON SEAT TRACK AFT END AT RBL 45 BETWEEN BS 1540 AND BS 1640, CORROSI ON LEVEL 2. REPLACED SEAT TRACK AT RBL 45 AND BS 1540 AND BS 1640 PER SRM 51-10-00 AND BOEING DRAWING NR 146N5120. (M) 2 L 7 2 4F RT A2NM 1999090300678 19990903 00678 NM 1999 9 3 USAASB99186 1 19990728 A 5270 WARNING BOEING 737 7374B7 1384702 NM PAX DOOR ACTIVATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 431US 24553 DCA - FLT 8027 - AFTER TAKEOFF, THE FORWARD ENTRY DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT DCA AND L ANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M) 2 L 7 2 4F RT A16WE 1999090300679 19990903 00679 NM 1999 9 3 USAASB99188 1 19990731 A 2613 6131508551 WIRE HARNESS BOEING 737 737401 1384701 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 405US 23885 PIT - FLT 8574 - FLIGHT RETURNED TO FIELD AT PIT TWO TIMES FOR A NR 2 ENGINE OVERHEAT LIGHT ILLUMINATING DURING CLIMB-OU T. BOTH TIMES THE LIGHT EXTINGUISHED WHEN POWER WAS REDUCED TO IDLE. BOTH FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH THE NR 2 ENGINE AT IDLE. NO EMERGENCIES WERE DECLARED AND NO ENGINE SHUTDOWNS OCCURRED. MAINTENANCE REMOVED AND REPLAC ED THE NR 2 ENGINE SOFT CORE HARNESS ASSEMBLY. RAN ENGINE AT POWER SETTING. OVERHEAT LIGHT DID NOT ILLUMINATE. OPERAT IONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999090300680 19990903 00680 WP 1999 9 3 GTIA9901069 1 19990810 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP ROW 5-15 FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 MYR - EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROW 5 AND 15 INTERMITTENT. FOUND BAD CONNECTION AT ROW 15. REPAIRED AS NE EDED. OPERATION CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1999090300681 19990903 00681 WP 1999 9 3 GTIA9901070 1 19990810 A 3350 BULBS DOUG DC9 DC931 3022065 WP CABIN MISINSTALLED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 MYR - TWO EACH EMERGENCY LIGHTS INOPERATIVE AT OVERHEAD SERVICE ENTRANCE. FOUND INCORRECT BULBS INSTALLED. REPLACED WI TH CORRECT ML43 BULBS. OPERATION CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1999090300682 19990903 00682 WP 1999 9 3 GTIA9901071 1 19990810 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 AFT FLIGHT ATTENDANT FORWARD JUMPSEAT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT B5-27. FOUND POWER AND G ROUND WIRE NOT HOOKED TO AFT EXIT LIGHTS, REINSTALLED. FOUND BAD CONNECTION ON AFT OVERHEAD AISLE LIGHTS, REPAIRED SAME LIGHTS. OPERATION CHECKS GOOD IAW 33-50-0 AND WIRING DA 33-51-01. (M) 2 L 7 2 4F A6WE 1999090300683 19990903 00683 SO 1999 9 3 ASOA99063 1 19990724 A 2150 1945463 HEAT EXCHANGER EMB 120 EMB120RT SO PACK CRACKED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 11 239AS 120057 FLT 4267 - AFTER TAKEOFF CREW REPORTED DUAL PACK FAILURE AND SMOKE EMITTED FROM VENTS IN THE COCKPIT AND CABIN. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ATL. AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CRACK ED HEAT EXCHANGER. REPLACED HEAT EXCHANGER. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999090300684 19990903 00684 SO 1999 9 3 ASOA99064 1 19990724 A 3260 12022623001 HARNESS EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A ASOA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 11 210AS 120006 FLT 4911 - DURING TAKEOFF IN CLIMB, THE PILOT CALLED FOR GEAR UP. THE F/O TRIED SEVERAL TIMES TO MOVE THE GEAR HANDLE U P, BUT WAS UNABLE. THE PILOT DIRECTED THE F/O TO USE THE DOWNLOCK RELEASE BUTTON AND TRY AGAIN, WHICH WAS STILL UNSUCCE SSFUL. DFW MAINTENANCE HAD THE PILOT REPEAT THE PROCEDURE, ALSO UNSUCCESSFUL. THE AIRCRAFT RETURNED TO DFW AND HAD AN UNEVENTFUL LANDING. DFW MAINTENANCE REMOVED AND REPLACED THE RIGHT PROXIMITY SWITCH HARNESS. OPERATIONAL CHECKS WERE G OOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999090300685 19990903 00685 SO 1999 9 3 ASOA99070 1 19990731 A 3350 FO2A250V1A FUSE EMB 120 EMB120RT SO CABIN BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 266AS 120188 DURING INSPECTION, FOUND CABIN TRACK LIGHTING FUSE BLOWN. TXK MAINTENANCE REPAIRED FAULTY CONNECTION ON THE FORWARD CAB IN TRACK LIGHT. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999090300686 19990903 00686 NE 1999 9 3 ASOA99069 2 19990801 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE NR 2 FAILED A ASOA A F UNSCHED LANDING ACTIVATE FIRE EXT. J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 230AS 27416 120032 115115 FLT 4275 - EN ROUTE FROM OAJ TO ATL, AT APPROX 20 MILES EAST OF FLO THE VOR RECEIVED AN 'OIL PRESSURE NR 2' LIGHT ON MAP . CONFIRMED WITH GAUGE AND RIGHT OIL GAUGE WAS READING ZERO. LOW PRESSURE OIL CHECKLIST WAS COMPLETED AND REDUCED POWE R ON AFFECTED ENGINE. F/A REPORTED A STRONG OIL SMELL IN THE CABIN. CAPTAIN SHUT DOWN THE ENGINE, DECLARED AN EMERGENC Y, AND PROCEEDED TO THE NEAREST AIRPORT WHICH WAS FLO. EMERGENCY EQUIPMENT WAS STANDING BY AND TAXIED SAFELY TO THE TER MINAL UNDER NORMAL POWER. MTC REMOVED AND REPLACED ENGINE. FOUND OIL PRESSURE LINE CLOGGED. GOT HOT START AND CONDITI ON LEVER WAS NOT RESPONDING. CHANGED FUEL CONTROL AND O-RINGS. REPLACED PCU. PLANE RUNS FINE WITH EEC OFF, MTC WILL T 2 L 7 2 4T 4 T RT A31SO E20NE 1999090300687 19990903 00687 SO 1999 9 3 ASOA99066 1 19990725 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 275AS 120234 DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MCN MAINTENANCE REMOVED AND REPLACED THE NR 1 E MERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999090300688 19990903 00688 SO 1999 9 3 ASOA99068 1 19990727 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 284AS 17161 120249 DURING INSPECTION, NR 1 AND NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MCN MAINTENANCE REMOVED AND REPLACED T HE NR 1 AND NR 2 EMERGENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999090300689 19990903 00689 SO 1999 9 3 ASOA99065 1 19990724 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 237AS 16194 120051 DURING INSPECTION, NR 1 AND NR 2 EMERGENCY BATTERY PACKS FOUND TO BE INOPERATIVE. TXK MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 EMERGENCY BATTERY PACK. (M) 2 L 7 2 4T RT A31SO 1999090300690 19990903 00690 WP 1999 9 3 ORJA99246 1 19990802 A 3350 6011777 BATTERY PACK DOUG DC9 DC982 3022082 WP EXTERIOR DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 823RA 49889 SJC - EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4F A6WE 1999090300691 19990903 00691 WP 1999 9 3 ORJA99245 1 19990808 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 24 DEF FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 RNO - EMERGENCY LIGHTS ROW 21 THROUGH 24 INOPERATIVE. FOUND SHORTED WIRE AT SEAT 24 DEF. REPAIRED WIRE AND REMOVED AND REPLACED BATTERY PACK AT ROW 21. EMERGENCY LIGHTS OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999090300692 19990903 00692 WP 1999 9 3 ORJA99244 1 19990806 A 3350 BR9661116 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 25-28 UNSERVICEABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 SJC - EMERGENCY LIGHTS ROW 25 THROUGH 28, AIRCRAFT RIGHT, WILL NOT TURN OFF. REMOVED AND REPLACED PACK AT AFT LEFT EMER GENCY EXIT PER MM 33. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999090300693 19990903 00693 WP 1999 9 3 ORJA99243 1 19990728 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 17DEF LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 RNO - EMERGENCY SEAT LIGHT AT 17 DEF, INOPERATIVE. FOUND LOOSE CONNECTOR RE-ATTACHED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999090300694 19990903 00694 WP 1999 9 3 ORJA99242 1 19990725 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 RNO - CABIN RIGHT FORWARD EMERGENCY EXIT BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT RIGHT CABIN WIN E FORWARD EMERGENCY EXIT PER MM 33-53-01. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999090300695 19990903 00695 NM 1999 9 3 ORJA99241 1 19990726 A 3350 1001191 COVER DOUG MD90 MD9030 3023690 NM ROW 23 MISSING A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 905RA 53573 EMERGENCY LIGHT AND COVER MISSING. REPLACED EMERGENCY LIGHT AND COVER, ROW 23, PER MM 33-53-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999090300696 19990903 00696 WP 1999 9 3 ORJA99240 1 19990802 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 21-24 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 SJC - EMERGENCY LIGHTS INOPERATIVE ROW 21-24. REMOVED AND REPLACED BATTERY PACK LEFT ROW 24 PER MM 33-53-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999090300697 19990903 00697 NM 1999 9 3 ORJA99209 1 19990628 A 3397 WIRE DOUG MD90 MD9030 3023690 NM ROW 31 BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 901RA 53489 RNO - EMERGENCY PATH LIGHT AT ROW 33 IS INOPERATIVE. REPLACED BROKEN WIRE ON ROW 31 EMERGENCY EXIT LIGHT SYSTEM, OPS CH ECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999090300698 19990903 00698 NM 1999 9 3 GAIA99112 1 19990806 A 5314 KEEL BEAM BOEING 727 727222 1384073 NM BS 950 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 90AX 20040 DURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE KEEL BEAM (STRINGER 2 7R) AT STATION 950E HAD EXFOLIATED CORROSION. THIS IN THE AREA OF THE NR 2 LOWER CARGO DOOR FRAME. REPAIRED IAW DRAWIN GS 53-99296-1 AND 53-99296-2. THESE DRAWINGS WERE DER APPROVED ON 8110-3, DATED JUN 3, 1999. (M) 2 L 7 3 4F A3WE 1999090300699 19990903 00699 NM 1999 9 3 GAIA99113 1 19990806 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 670 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 90AX 20040 DURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE FLOORBEAM AT STATION 620 IS CORRODED BETWEEN LBL 24.75 AND RBL 24.75 SEAT TRACKS. REPAIRED IAW ATS DRAWING 2000-0276. THIS DRAWING WAS DER RECOMMENDED AND ACO APPROVED ON 8110-3, DATED JUN 21, 1999. (M) 2 L 7 3 4F A3WE 1999090300700 19990903 00700 NM 1999 9 3 GAIA99114 1 19990806 A 5330 SKIN BOEING 727 727222 1384073 NM BS 610 MISINSTALLED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 90AX 20040 DURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT AT STATION 610 AND STRING ER 3L, A FASTENER IS INSTALLED ON TOP OF A BUCKTAIL. REPAIRED IAW ATS DRAWING 2000-0193. THIS DRAWING WAS DER RECOMMEN DED AND ACO APPROVED ON 8110-3, DATED MAY 25, 1999. (M) 2 L 7 3 4F A3WE 1999090300701 19990903 00701 NM 1999 9 3 GAIA99115 1 19990806 A 5320 HAT SECTION BOEING 727 727222 1384073 NM BS 344-360 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 90AX 20040 DURING AN 'HC' INSPECTION BEING PERFORMED IN OKC AT AAR REPAIR STATION, IT WAS DISCOVERED THAT THE HAT SECTION AT STATIO N 344 TO 360, RBL 19 IS CORRODED. HAT SECTION REMOVED PER ATS DRAWING 2000-0373. FABRICATED A NEW FLOOR PANEL IAW B727 SRM 53-20-2. THIS DRAWING WAS DER RECOMMENDED AND ACO APPROVED MAY 25, 1999. (M) 2 L 7 3 4F A3WE 1999090300702 19990903 00702 WP 1999 9 3 GAIA99116 1 19990310 A 5230 5921162503 SKIN DOUG DC9 DC915F 3022037 WP CARGO DOOR DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING B-CHECK INSPECTION, FOUND A SMALL HOLE IN THE MAIN CARGO DOOR BETWEEN L17L AND L18L AT STATION 370. THE HOLE WAS REPAIRED IAW KITTY HAWK EA D9-52-002 THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999090300703 19990903 00703 NM 1999 9 3 GAIA99117 1 19990811 A 2933 CONNECTOR BOEING 727 727223 1384074 NM 'A' HYD SYSTEM DIRTY A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 856AA 20997 FLT 518 - TOL-ATL - CLEARED FOR SHORT APPROACH BY ATC. CREW PREPARED A/C FOR APPROACH BY EXTENDING THE FLAPS AND GEAR. ATC THEN EXTENDED THE APPROACH, SO THE CREW RETRACTED THE FLAPS AND GEAR TO CLEAN UP THE AIRCRAFT. AT THAT TIME, THE ' A' SYSTEM HYD QTY DROPPED TO LESS THAN 2 GAL AND THE LOW QTY LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY, SO THE FLAP S WERE EXTENDED USING THE ALTERNATE SYS AND THE GEAR WAS EXTENDED MANUALLY. A/C LANDED SAFELY W/O ANY FURTHER DIFFICULT IES. AFTER LANDING, THE HYD QTY RETURNED TO NORMAL AND THE LOW QTY LIGHT EXTINGUISHED. MX PRESSURIZED 'A' AND 'B' SYST EM HYDRAULICS AND PERFORMED A VISUAL INSPECTION OF SYSTEMS FOR LEAKS, AND NO DEFECTS WERE NOTED. REMOVED, CLEANED AND R 2 L 7 3 4F A3WE 1999090300704 19990903 00704 NM 1999 9 3 GAIA99111 1 19990803 A 3260 656021132 ACCESSORY UNIT BOEING 727 727251 138408H NM E/E COMPT INOPERATIVE A GAIA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 07 278US 21157 FLT 725 - MMY-TOL - ON LANDING, EXTENDED THE LANDING GEAR. THE RED TAIL SKID LIGHT, THREE GREEN GEAR LIGHTS, THREE RED GEAR LIGHTS ALL ILLUMINATED. ALSO, THE GPWS WARNING TO LOWER GEAR SOUNDED AS WELL. THE CREW PERFORMED A GO AROUND, REC YCLED THE GEAR, AND ALL LIGHTS WORKED PROPERLY. THE AIRCRAFT LANDED WITHOUT FURTHER DIFFICULTIES. REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999090300705 19990903 00705 NM 1999 9 3 GAIA99101 1 19990719 A 3260 FZH6DE10SL3S CONNECTOR BOEING 727 727223 1384074 NM NLG DISENGAGED A GAIA K NONE N FALSE WARNING AP APPROACH 1 SW 07 6821 19496 FLT 2508 - GEG-IND - ON APPROACH, HAD TO CYCLE GEAR TWICE IN ORDER TO GET A NOSE GEAR DOWN AND LOCKED INDICATION. THE A IRCRAFT LANDED SAFELY IN GEG WITHOUT FURTHER PROBLEMS. MAINTENANCE FERRIED THE AIRCRAFT, GEAR DOWN TO SEA WHERE JACKS W ERE AVAILABLE FOR TROUBLESHOOTING. CLEANED AND LUBED NOSE LANDING GEAR. PERFORMED NOSE LANDING GEAR RETRACTION AND EXT ENSION TEST MULTIPLE TIMES. OPERATIONALLY CHECKS GOOD IAW 32-33-0. LOGBOOK RELEASED. DURING PREFLIGHT OF AIRCRAFT PRI OR TO FLIGHT, THE NLG UNSAFE LIGHT ILLUMINATED AND THE LANDING GEAR WARNING SOUNDED. FOUND PUSHED PIN ON THE LOCK POSIT ION CANNON PLUG. REPAIRED THE SAME AND OPERATIONALLY CHECKED GOOD PER MM 32-61-71. THE AIRCRAFT WAS RETURNED TO SERVIC 2 L 7 3 4F A3WE 1999090300706 19990903 00706 NM 1999 9 3 GAIA99110A 1 19990803 A 3297 WIRE BOEING 727 727223 1384074 NM NLG CHAFED A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 6821 19496 FLT 2508 - IND-GEG - ON FINAL APPROACH, HAD TO CYCLE ITS GEAR FOUR TIMES IN ORDER TO GET A NOSE GEAR DOWN AND LOCKED IND ICATION. THE AIRCRAFT LANDED SAFELY IN GEG WITHOUT FURTHER PROBLEMS. MAINTENANCE FERRIED THE AIRCRAFT, GEAR DOWN TO SE A WHERE JACKS WERE AVAILABLE FOR TROUBLESHOOTING. FOUND CHAFFED WIRE IN THE CONDUIT THAT CONNECTS THE NLG LOCK SWITCH T O THE TERMINAL STRIP IN NOSE WHEEL WELL. REPLACED ENTIRE WIRE. ALSO, REPLACED THE NLG LOCK SWITCH, NLG POSITION SWITCH , AND THE LANDING GEAR ACCESSORY UNIT FOR PRECAUTIONARY PURPOSES. PERFORMED AN EXTENSION AND RETRACTION TEST, AND SYSTE M OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999090300707 19990903 00707 EU 1999 9 3 RAIA990810 1 19990810 A 3610 23061 SEAL AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 721TE 217 FLT 7408 - STL - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED DISCHARGE PIPE SEAL. (M) 2 H 7 2 4T RT A53EU 1999090300708 19990903 00708 NE 1999 9 3 RAIA990809 2 19990808 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT FAILED A RAIA O OTHER O J OTHER WARNING INDICATION CR CRUISE 1 CE 03 563HK 7931 41079 75107 FLT 7515 - GRR - LEFT ENGINE SHUT DOWN BY ITS SELF. MAINTENANCE REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999090300709 19990903 00709 EU 1999 9 3 RAIA990807 1 19990808 A 2432 16566 BATTERY AEROSP ATR72 ATR72202 8680940 EU BATT COMPT DISCHARGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 721TE 13833 217 FLT 7400 - STL - MAIN BATTERY CHARGE FAULT LIGHT. MAINTENANCE REPLACED EMERGENCY/STANDBY BATTERY. (M) 2 H 7 2 4T RT A53EU 1999090300710 19990903 00710 EU 1999 9 3 RAIA990806 1 19990808 A 2432 40782 BATTERY AEROSP ATR72 ATR72202 8680940 EU BATT COMPT DISCHARGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 721TE 13992 217 FLT 7400 - STL - MAIN BATTERY CHARGE FAULT LIGHT. MAINTENANCE REPLACED MAIN BATTERY. (M) 2 H 7 2 4T RT A53EU 1999090300711 19990903 00711 1999 9 3 RAIA990805 4 19990805 A 3140 701700082404 COMPUTER EMB 145 EMB145 SO NR 2 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 801HK 145053 FLT 8775 - SBN - RECEIVED BLU ICAS MESSAGE 'CHECKLIST MISS MATCH'. MAINTENANCE REPLACED NR 2 IC600 COMPUTER. (M) 2 L 7 2 4F RT T00011AT 1999090300712 19990903 00712 1999 9 3 RAIA990804 4 19990805 A 3140 701700082404 COMPUTER EMB 145 EMB145 SO NR 1 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 801HK 145053 FLT 8775 - SBN - RECEIVED BLUE ICAS MESSAGE 'CHECKLIST MISS MATCH'. MAINTENANCE REPLACED NR 1 IC600 COMPUTER. (M) 2 L 7 2 4F RT T00011AT 1999090300713 19990903 00713 WP 1999 9 3 HALA9900161 1 19990806 A 2780 2701791 SWITCH DOUG DC9 DC951 3022051 WP LT LE SLAT FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 674MC 47735 KOA - FLT 63 - SLAT EXTEND LIGHT WON'T COME ON. LIGHT TESTS OK. SLATS VISUALLY VERIFIED EXTENDED. FERRIED A/C TO HNL FOR REPAIRS. REPLACED THE LEFT SLAT EXTEND SWITCH. THE OPERATIONAL CHECK WAS OK. (M) 2 L 7 2 4F RT A6WE 1999090300714 19990903 00714 WP 1999 9 3 HALA9900165 1 19990815 A 3340 SWITCH DOUG DC9 DC951 3022051 WP COCKPIT FAILED A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 603DC 47784 HNL - FLT 528 - SMOKE COMING FROM BEHIND LANDING LIGHT SWITCHES. SMOKE STARTED WHEN LIGHTS SWITCHED OFF AFTER LANDING. PULLED C/B K14, 15, AND L14, 15 SMOKE STOPPED. REMOVED AND REPLACED LEFT LANDING LIGHT TOGGLE SWITCH OPS CHECK GOOD. C ONDTION AND SECURITY CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999090300715 19990903 00715 WP 1999 9 3 HALA9900163 1 19990806 A 3350 P4010051111 MODULE DOUG DC9 DC951 3022051 WP ROW 18 INOPERATIVE A HALA K NONE L NO TEST CR CRUISE 1 WP 13 669HA 47654 HNL - FLT 361 - THE FLIGHT ATTENDANT REPORTS THE EMERGENCY LIGHTS FLICKERING DURING FLIGHT FROM ROW 18 AND BACK TO THE R EAR. REPLACED THE AFT CONTROL MODULE. THE OPERATIONAL CHECK WAS OK. (M) 2 L 7 2 4F RT A6WE 1999090300716 19990903 00716 WP 1999 9 3 ASAA9980152 1 19990707 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 2876 53077 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WOULD NOT TURN OFF. REPLACED THE LIGHT ASSEMBLY AN D OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999090300717 19990903 00717 WP 1999 9 3 ASAA9980151 1 19990705 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 1886 49386 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999090300718 19990903 00718 WP 1999 9 3 ASAA9980149 1 19990702 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP ROW 27-28 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 27 TO 28 WERE FOUND INOPERATIVE. REPLACED LA MP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999090300719 19990903 00719 NM 1999 9 3 ASAA9940140 1 19990804 A 3350 1060091102 LIGHT GRIMES BOEING 737 7374Q8 NM L2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 783AS 25114 SEA - DURING MAINTENANCE CHECK, THE L2 DOOR LOWER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999090300721 19990903 00721 NM 1999 9 3 ASAA9940137 1 19990716 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 JNU - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999090300722 19990903 00722 NM 1999 9 3 ASAA9940135 1 19990708 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PDX - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/ LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999090300723 19990903 00723 NM 1999 9 3 ASAA9940133 1 19990701 A 3350 BPS73 CHARGER BOEING 737 7374Q8 NM ROW 8 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 8 TO THE FIRST OVE RWING EXIT. REPLACED BATTERY PACK, CHARGER, AND REPAIRED WIRING, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999090300724 19990903 00724 NM 1999 9 3 99ZZZM623 1 19990701 A 3350 S283T0143 BATTERY CHARGER BOEING 737 7374Q8 NM ROW 8 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 8 TO THE FIRST OVE RWING EXIT. REPLACED BATTERY PACK, CHARGER, AND REPAIRED WIRING, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999090300725 19990903 00725 NM 1999 9 3 TSAA9951323 1 19990617 A 5320 654795220 FRAME BOEING 737 7372Q9 138448M NM CARGO DOORWAY CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 FORWARD CARGO COMPARTMENT FORWARD DOOR FRAME HAS EXFOLIATED CORROSION. CLEANED, TREATED, FABRICATED, AND COMPLETED IAW SRM 51-40-3 PAGE 1. (M) 2 L 7 2 4F A16WE 1999090300726 19990903 00726 NM 1999 9 3 TSAA9957314 1 19990617 A 5720 6555511 FITTING BOEING 737 7372Q9 138448M NM RT WING CORROSION A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 RIGHT WING FRONT SPAR WEB CORROSION AT FSS 435. REPAIRED IAW ECO 2970. (M) 2 L 7 2 4F A16WE 1999090300727 19990903 00727 NM 1999 9 3 USAA990262 1 19990331 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 334 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT INTERCOSTAL BL 0 TO RBL 25 STATION 334. BURNISHED CORROSIO N AND INSTALLED NEW NUT PLATES PER SRM 53-00-04. (M) 2 L 7 2 4F RT A2NM 1999090300728 19990903 00728 NM 1999 9 3 USAA990203 1 19990331 A 5320 CC1145827 INTERCOSTAL BOEING 757 757225 1384959 NM BS 324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 324 TO STATION 345 LBL 20 INTERCOSTAL. REPLACED IN TERCOSTAL. (M) 2 L 7 2 4F RT A2NM 1999090300729 19990903 00729 NM 1999 9 3 USAA990261 1 19990331 A 5320 141N8422L SILL BOEING 757 757225 1384959 NM BS 324-365.25 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT BS 324-BS 365.25 RBBL LOWER SI LL ASSY CORROSION TASK NR C53-221-03 AND C 53-222-03. REPAIRED PER SRM 53-10-15, BURNISHED AREA TO REMOVE CORROSION. ( M) 2 L 7 2 4F RT A2NM 1999090300730 19990903 00730 NM 1999 9 3 USAA990260 1 19990331 A 5320 141N8422L SILL BOEING 757 757225 1384959 NM BS 310.5-324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT BS 310.5 TO BS 324 AT RBBL LOW ER SILL ASSY, CORROSION TASK NR C53-221-03 AND C53-222-03. REPAIRED PER SRM 53-10-15, BURNISHED AREA TO REMOVE CORROSIO N. (M) 2 L 7 2 4F RT A2NM 1999090300731 19990903 00731 NM 1999 9 3 USAA990306 1 19990331 A 5400 FITTING BOEING 757 757225 1384959 NM NR 1 NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING VISUAL CHECK INSPECTION, FOUND A SUPPORT CASTING CRACK AT ATTACHED BOLT LT SIDE NR 1 ENGINE NACELLE STATION 174.30. INSTALLED DOUBLER PER EA 63980 AND 63994. (M) 2 L 7 2 4F RT A2NM 1999090300732 19990903 00732 NM 1999 9 3 USAA990233 1 19990331 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM TOP SURFACE STATION 1640 ENTIRE LENGTH. CORROSIO N TASK NR C53-251-03 AND C53-252-03. REPLACED WITH NEW FABRICATED T-CAP PER TR 53-15-01 AND EA 63981. (M) 2 L 7 2 4F RT A2NM 1999090300733 19990903 00733 NM 1999 9 3 USAA990219 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1600 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 VISUAL INSPECTION, FOUND CRACK FUSELAGE FRAME STATION 1600 BETWEEN STRINGER 26R AND 27R. INSTALLED DOU BLER PER EA 63977. (M) 2 L 7 2 4F RT A2NM 1999090300734 19990903 00734 NM 1999 9 3 USAA990186 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1480 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION FUSELAGE FRAME STATION 1480 BETWEEN STRIGNER 26L AND STRINGER 27L. CORROSION TASK NR C53-163-02/C53-164-02. INSTALLED REPAIR DOUBLER PER SRM 53-00-07 FIG 201 AND EA 63977. (M) 2 L 7 2 4F RT A2NM 1999090300735 19990903 00735 NM 1999 9 3 USAA990187 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1460 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION FUSELAGE FRAME STATION 1460 BETWEEN STRINGER 26L AND STRINGER 27L, CORROSION TASK NR C53-155-02. INSTALLED REPAIR DOUBLER PER SRM 53-00-07 AND EA 63977. (M) 2 L 7 2 4F RT A2NM 1999090300736 19990903 00736 NM 1999 9 3 USAA990280 1 19990331 A 5313 STRINGER BOEING 757 757225 1384959 NM BS 1451 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 1451 STRINGER 30 BL 0 FORWARD END OF SPLICE. ALSO, FOUND CRACK AT FRAME 1360 STRINGER 26-27R, CORROSION TASK NR C53-155-02. INSTALLED DOUBLER ON FRAME PER EA 63977A. (M ) 2 L 7 2 4F RT A2NM 1999090300737 19990903 00737 NM 1999 9 3 USAA990230 1 19990331 A 5313 STRINGER BOEING 757 757225 1384959 NM BS 1400 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER AT S28R FRAME AT STATION 1400 AND STRINGER 28R. S TRINGER SPLICED PER SRM 53-00-03 FIG 201 AND EA 64000. (M) 2 L 7 2 4F RT A2NM 1999090300738 19990903 00738 NM 1999 9 3 USAA990256 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT FRAME 1380 FASTENER HOLE AT RBL 19 WEB. REMOVED AND INSTALLED NEW WEB PER EA 63976. (M) 2 L 7 2 4F RT A2NM 1999090300739 19990903 00739 NM 1999 9 3 USAA990275 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 1360 STRINGER 26 R FRAME, CORROSION TASK NR C53-155 -02. INSTALLED DOUBLER PER EA 63977. (M) 2 L 7 2 4F RT A2NM 1999090300740 19990903 00740 NM 1999 9 3 USAA990257 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A CRACK AT FRAME STATION 1360 STRINGER 26R AND STRINGER 27R. FABRICATED REPAIR PER EA 63977. (M) 2 L 7 2 4F RT A2NM 1999090300741 19990903 00741 NM 1999 9 3 USAA990232 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FRAME STATION 1360 STRINGER 26R, CORROSION TASK NR C53-155- 02. INSTALLED FILLER AND DOUBLER PER EA 63977. (M) 2 L 7 2 4F RT A2NM 1999090300742 19990903 00742 NM 1999 9 3 USAA990218 1 19990331 A 5315 BAC1518338 FLOORBEAM BOEING 757 757225 1384959 NM BS 345 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION STATION 345 TOP OF FLOORBEAM. INSTALLED 'T' CAP PER SRM 53-00 -51, EA 63948A AND TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1999090300743 19990903 00743 NM 1999 9 3 USAA990229 1 19990331 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 324 RBL 46 TO RBL 62 FLOORBEAM. REPLACED FLOORBEAM PER EA 63950. (M) 2 L 7 2 4F RT A2NM 1999090300744 19990903 00744 NM 1999 9 3 USAA990276 1 19990331 A 5320 WEB BOEING 757 757225 1384959 NM BS 1718 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 1718 AT LBL 62 WEB, CORROSION TASK NR C53-155-02. F ABRICATED NEW WEB PER BOEING DRAWING 146N8722. (M) 2 L 7 2 4F RT A2NM 1999090300745 19990903 00745 NM 1999 9 3 USAA990228 1 19990331 A 5320 FITTING BOEING 757 757225 1384959 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF GALLEY FITTING STATION 377 AT RBBL 10.0. M ANUFACTURED NEW FITTING PER DRAWING 92F5033131 AND 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999090300746 19990903 00746 NM 1999 9 3 USAA990237 1 19990331 A 5320 FLOORPAN BOEING 757 757225 1384959 NM BS 1701 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AFT CABIN GALLEY FLOOR PAN STATION 1701-1720 LEFT ZEE TO RT ZE E, CORROSION TASK NR C53-251-03 AND C53-252-03. REMOVED AND REPLACED FLOOR PAN PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999090300747 19990903 00747 NM 1999 9 3 USAA990184 1 19990331 A 5315 146N5092 FLOORBEAM BOEING 757 757225 1384959 NM BS 1681.8 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION UPPER SURFACE FLOORBEAM AT STATION 1681.8 FROM RBL 17 TO LBL 1 7, CORROSION TASK NR C53-251-03/C53-252-03. REPLACED PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999090300748 19990903 00748 NM 1999 9 3 USAA990239 1 19990331 A 5315 146N5092 FLOORBEAM BOEING 757 757225 1384959 NM BS 1681.8 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION TOP SURFACE FLOORBEAM STATION 1681.8, CORROSION TASK NR C53-25 1-03/C53-252-03. REPLACED FLOORBEAM PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999090300749 19990903 00749 NM 1999 9 3 USAA990258 1 19990331 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A CRACK AT FRAME STATION 1460 STRINGER 26R AND STRINGER 27R. REPLACED P ART PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999090300750 19990903 00750 WP 1999 9 3 99ZZZX3199 2 19990613 A 7261 30743721 CHECK VALVE BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R1H 29001 WP LT ENGINE FAILED A KKYA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NE 03 511KA NA0237 P84124 OXC/BDL - EN ROUTE ON A PRE-POSITIONING FLIGHT, THE CREW REPORTED THE OIL PRESSURE STARTED TO DECLINE ON THE LEFT ENGINE . AT 15 PSI, THE LEFT ENGINE WAS SHUT DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT AT BDL. AN INVESTIGATION REVEALED TH AT OIL WAS LEAKING FROM THE CONNECTION AT THE CHECK VALVE, PN 3074372-1. THE ENGINE WAS REMOVED, DETAILS WILL FOLLOW AS THEY BECOME AVAILABLE. 2 L 7 2 4F 4 F A3EU E6WE 1999090300764 19990903 00764 EU 1999 9 3 USAASA99003 1 19990714 A 5240 MECHANISM AIRBUS A319 A319112 EU L2 DOOR NOT LATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 703UW 0904 SNA/PIT - FLT 148 - AFTER TAKEOFF, THE 2L CABIN DOOR WAS LEAKING AND DOOR ARMED INDICATOR WAS FLASHING. THE AIRCRAFT DI VERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND 2L DOOR NOT PROPERLY CLOSED. THE DOOR WARNING SYSTEM AND THE OPERATION OF 2L DOOR WERE CHECKED AND FOUND TO BE NORMAL. THE DOOR WAS PROPERLY CLOSED AND THE AIRCRAFT DISPATCHED. (X) 2 L 7 2 4F RT A28NM 1999090300765 19990903 00765 SW 1999 9 3 99ZZZX3213 1 19990622 A 6510 406040340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL 53264 DURING 25-HOUR INSPECTION, AD 97-24-17. COUPLING DISC CRACKED. 1 G 7 1 3U O H2SW 1999090300813 19990903 00813 NM 1999 9 3 AALA991047 1 19990716 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 183AN 29593 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 3 AND 12 INOPERATIVE. REPLACED END CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999090300814 19990903 00814 NM 1999 9 3 AALA991096 1 19990726 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 676AN 29426 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 3E AND 6E INOPERATIVE. REPLACED CONN ECTORS TO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS BETWEEN SEATS 3E AND 6E. SYSTEM GROUND CHECK, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999090300815 19990903 00815 NM 1999 9 3 AALA991013 1 19990709 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AN 29590 DFW - DURING OVENRIGHT MAINTENANCE, LEFT AND RIGHT MAINTENANCE LEFT AND RIGHT EMERGENCY EXIT FLOOR PATH LIGHTING INOPERA TIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999090300816 19990903 00816 1999 9 3 99ZZZX3261 4 19990712 A 2397 WIRE COLLINS 6226520008 BEECH 1900 1900D 1154162 CE NR 2 COMM FAILED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 01 122UX UE122 NR 2 COMM CONTROL HEAD STARTED SMOKING ON CLIMB-OUT. REMOVED AND REPLACED NR 2 COMM CONTROL (PN 622-6520-008) AND REPAI RED CHAFED AND BURNED WIRES ON PIN 28 AND PIN 37 OF CONNECTOR J176. WIRING HAD CHAFED AND SHORTED OUT. COMM CONTROL CI RCUIT BOARD WAS BURNED. (X) 2 L 7 2 4T RT A24CE 1999090300817 19990903 00817 SO 1999 9 3 GLBA99040 1 19990718 A 2150 22045402 ACM EMB 120 EMB120ER 3260203 SO LT FUSELAGE FAILED A GLBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 01 71GL 120071 COCKPIT AND CABIN FILLED WITH SMOKE DURING TAXI. SMOKE ALARM ACTIVATED. ALSO, HAD PACK FAIL ILLUMINATION FOR LEFT SIDE AND HOT AIR DISCHARGE IN COCKPIT ON BOTH AUTO AND MANUAL. REPLACED ACM/FOUND UNIT TO BE SEIZED. OPS CHECKED GOOD AFTE R REPLACEMENT. RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999090300818 19990903 00818 CE 1999 9 3 MASA99125 1 19990723 A 7110 B140048 HOOK MECHANISM 129910041601 BEECH 1900 1900D 1154162 CE RT COWL WORN A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 76ZV UE76 PHX/FMN - FLT 6462 - THE CAPTAIN REPORTED A FORWARD UPPER COWL LOOSE. THE AIRCRAFT RETURNED TO PHX. MAINTENANCE PERFOR MED AN INSPECTION OF THE COWL AND FOUND ONE LOCK PARTIALLY LOOSE. THEY RESECURED THE COWL AND DEEMED THE ASSEMBLY AND T HE AIRCRAFT AIRWORTHY. THE AIRCRAFT CONTINUED THE FLIGHT TO FMN. FMN MAINTENANCE RE-INSPECTED THE COWL AND FOUND IT PA RTIALLY LOOSE AGAIN. MAINTENANCE REPLACED HOOK AND ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999090300819 19990903 00819 CE 1999 9 3 MASA99123 1 19990722 A 3620 WARNING BEECH 1900 1900D 1154162 CE RT BLEED AIR ACTIVATED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 120YV UE120 PHL/LEB - FLT 5274 - THE AIRCRAFT HAD A RIGHT BLEED AIR FAIL ANNUNCIATOR LIGHT ILLUMINATE AND THE CREW DECLARED AN EMERG ENCY. MAINTENANCE ACTON WAS DEFERRED PER 21-3-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999090300820 19990903 00820 NM 1999 9 3 P2EA99218 1 19990715 A 2780 MECHANICAL BOEING 737 7372Q8 138448K NM NR 3 LE SLAT OUT OF AJDUST A P2EA O OTHER I FLT. ATTITUDE INST. CL CLIMB 1 CE 05 121NJ 21735 MDW - FLT 738 - LEADING EDGE IN-TRANSIT LIGHT STAYS ON IN FLAP POSITIONS 1-10, SLAT NR 3 SLOWS IN TRANSIT. AIRCRAFT ISS UED A SPECIAL FLIGHT PERMIT TO MCI. RE-ADJUSTED LEADING EDGE NR 3 SLAT AND RE-RIGGED DETENT ARMS. AIRCRAFT FLAPS WERE FUNCTIONAL TESTED IN-FLIGHT AND RETURNED TO SERVICE. (X). 2 L 7 2 4F RT A16WE 1999090300821 19990903 00821 NE 1999 9 3 99ZZZX3262 2 19990706 A 7260 CHIP LIGHT CESSNA 340 340A 2076405 CE GE CT7TP CT75A 30030 NE LT ENGINE ILLUMINATED A PLGA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 337BE 340A047 367165 LGA - FLT 6353 - AIRCRAFT WAS OPERATING FLT 6353 BOX/PHL. EN ROUTE TO PHL, CREW HAD A LEFT ENGINE CHIP LIGHT ILLUMINATE INTERMITTENTLY. CREW DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. THE ENGINE WAS NOT SHUT DOWN. MAINTENANCE INSPECTE D THE ENGINE AND FOUND A SMALL SLIVER OF MATERIAL (WITHIN LIMITS) ON THE CHIP DETECTOR. THE CHIP WAS REMOVED. REQUIRED INSPECTIONS AND OPERATIONAL CHECKS ACCOMPLISHED AND THE AIRCRAFT RETURNED TO SERVICE. (X) 1 L 7 2 3O 4 T 3A25 E8NE 1999090300822 19990903 00822 EU 1999 9 3 99ZZZX3263 1 19990621 A 3233 D23071001 ACTUATOR ERAM AIRBUS 320 A320321 3930325 EU NLG FAILED A P9RA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 347TM L1049 347 ATB/MIA - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF MIA. RECYCLED ACCORDING TO PROCEDURES, STILL WOULD NOT RETRACT. REPLACED NOSE LANDING RETRACT ACTUATOR IAW MM 32-20-00. ACCOMPLISHED RETRACTION PER MM 32-00-501 (TASK). FOUND ALL NO RMAL. RETURNED AIRCRAFT TO SERVICE. (X) 2 L 7 2 4F RT A28NM 1999090300823 19990903 00823 EU 1999 9 3 99ZZZX3264 1 19990724 A 3233 D23071001 ACTUATOR ERAM AIRBUS 320 A320321 3930325 EU NLG MALFUNCTIONED A P9RA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 347TM L1049 347 NOSE LANDING GEAR DID NOT RETRACT. RECYCLED ACCORDING TO PROCEDURE, STILL WOULD NOT CYCLE. REPLACED NOSE LANDING RETRA CT ACTUATOR IAW MM 32-20-00. ACCOMPLISHED RETRACTION TEST PER MM 32-30-00. ALSO ACCOMPLISHED FREE FALL IAW MM 32-33-00 -501 (TASK). FOUND ALL NORMAL, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A28NM 1999090300824 19990903 00824 NM 1999 9 3 99ZZZX3265 1 19990721 A 3397 WIRE BOEING 727 7272J0 138407E NM CABIN FAILED A RIVA K NONE L NO TEST IN INSP/MAINT 1 NE 05 362PA 21106 DURING DAILY CHECK, SECTION OF EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE RESULTING IN A 30-MINUTE DELAY. A STRIPPED WIRE WAS FOUND IN THE EMERGENCY PATH LIGHTING. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECK WAS GOOD. (X) 2 L 7 3 4F RT A3WE 1999090300825 19990903 00825 NM 1999 9 3 99ZZZX3266 1 19990715 A 3350 P4010049 BATTERY BOEING 727 7272J0 138407E NM ROW 5 DISCHARGED A RIVA K NONE L NO TEST IN INSP/MAINT 1 NE 05 362PA 21106 SJU - DELAY RESULTING FROM EMERGENCY TRACK LIGHTING AFT OF ROW 5 VERY DIM. CHARGED EMERGENCY TRACK LIGHTING BATTERY. O PERATIONAL CHECK GOOD. (X) 2 L 7 3 4F RT A3WE 1999090300826 19990903 00826 CE 1999 9 3 99ZZZX3267 1 19990612 A 3220 51470025 DRAG BRACE CESSNA 402 402C 207590R CE NLG CRACKED A RSHA K NONE O OTHER TX TAXI/GRND HDL 1 SO 17 251RS 402C0251 NOSE LANDING GEAR DRAG BRACE CRACKED AT REAR ATTACH POINT CAUSING COLLAPSE OF NOSE GEAR ASSEMBLY DURING TAXI. (X) 1 L 7 2 3O A7CE 1999090300827 19990903 00827 SO 1999 9 3 RAIA990725 1 19990719 A 2497 W147027310 WIRE EMB 145 EMB145 3260210 SO COCKPIT FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 807HK 145119 STL - FLT 9672 - ELECTRICAL ARC FROM AREA AROUND APU FIRE EXTINGUISHER. MAINTENANCE REPAIRED WIRE IN OVERHEAD IN COCKPI T. (X) 2 L 7 2 4F RT T00011AT 1999090300828 19990903 00828 EU 1999 9 3 SIMA991543 1 19990503 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 541AT 1274 541 DFW - FLT 3715 - EMERGENCY EXIT SIGNS OVER SERVICE DOOR AND MAIN CABIN DOOR DO NOT ILLUMINATE. REMOVED AND REPLACED EME RGENCY POWER SUPPLY BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999090300829 19990903 00829 SO 1999 9 3 SIMA991767 1 19990625 A 3350 3025101 LIGHT EMB 145 EMB145LR SO CABIN FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 601GH 145046 ORD - FLT 4112 - LEFT AND RIGHT OVERWING EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEM BLIES. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 1999090300830 19990903 00830 SO 1999 9 3 SIMA991991 1 19990718 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 628AE 12809 145124 JAN - FLT 3683 - EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS IAW EMB 145 AMM 33-50 -04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CNTRL NR 99ZZZX3268 AND 99ZZZX3269. (X) 2 L 7 2 4T RT T00011AT 1999090300831 19990903 00831 SO 1999 9 3 99ZZZX3268 1 19990718 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 628AE 13094 145124 JAN - FLT 3683 - EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS IAW EMB 145 AMM 33-50 -04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CNTRL NR SIMA991991 AND 99ZZZX3269. 2 L 7 2 4T RT T00011AT 1999090300832 19990903 00832 SO 1999 9 3 99ZZZX3269 1 19990718 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 628AE 13112 145124 JAN - FLT 3683 - EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACKS IAW EMB 145 AMM 33-50 -04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CNTRL NR SIMA991991 AND 99ZZZX3268. 2 L 7 2 4T RT T00011AT 1999090300833 19990903 00833 SW 1999 9 3 99ZZZX3270 1 19990711 A 7920 LINE BELL 212 212 1181420 SW ENGINE OIL FAILED A A ERAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 AL 03 511EH 31118 ON LANDING APPROACH, ENGINE OIL PRESSURE DROPPED, OIL PRESSURE LIGHT CAME ON, N1 BEGAN RISING. THROTTLE WAS REDUCED TO FLIGHT IDLE. JUST BEFORE LANDING, A LOUD NOISE WAS HEARD, ENGINE WAS SHUT DOWN AFTER LANDING. NO OIL COULD BE SEEN IN SIGHT GLASS. OIL WAS EVIDENT AROUND ENGINE AND ON DECK. OIL LINE RUNNING UNDER ENGINE FROM FUEL OIL HEATER TO COOLER W AS FOUND BENT AND BLOWN OUT OF FITTING. SUSPECT HIGH OIL PRESSURE PROBLEM. INCIDENT UNDER INVESTIGATION. 1 G 7 1 4U H4SW 1999090300834 19990903 00834 NE 1999 9 3 99ZZZX3271 2 19990720 A 7320 017755240 OVERSPEED BOX SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S 60030 NE NR 1 ENGINE FAILED A ERAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 AL 03 576EH 5371 143B 76212 3032 NR 1 ENGINE FAILED IN-FLIGHT. INVESTIGATION AND TROUBLESHOOTING INDICATED THAT THE OVERSPEED BOX FAILED. 1 G 7 2 3U 3 U H1NE E19EU 1999090300836 19990903 00836 NM 1999 9 3 CALA9901111 1 19990831 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND A .5 INCH CRACK AT O/B FORWARD CORNER OF NR 1 ENGINE PYLON ACCESS PANEL 5727L. THE CRACK WAS STOP DRIL LED AND A DOUBLER WAS INSTALLED IAW ECRA 5340-01230. 2 L 7 2 4F RT A16WE 1999090300837 19990903 00837 NM 1999 9 3 CALA9901112 1 19990831 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14308 23359 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52- 30-01, FIGURE 201. 2 L 7 2 4F RT A16WE 1999090300838 19990903 00838 NM 1999 9 3 CALA9901113 1 19990831 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT FASTENER HOLE LOCATIONS, STA 328. A NEW UPPER CHORD WAS INSTALLED IA W SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999090300839 19990903 00839 WP 1999 9 3 CALA9901114 1 19990901 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1871 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND LT LAV FLOOR SUPPORT CORRODED AT ZONE 290, STA 1871. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT W AS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999090300840 19990903 00840 WP 1999 9 3 CALA9901115 1 19990901 A 5350 SPAR DOUG DC10 DC1030 3023501 WP TAILCONE SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND THE TAIL CONE WORK PLATFORM SPAR SHEARED IN SEVERAL PLACES. THE SHEARED AREAS WERE TRIMMED OUT AND REI NFORCED WITH DOUBLERS IAW SRM 53-00-01, FIGURE 4 AND 51-31-01. 2 L 7 3 4F A22WE 1999090300841 19990903 00841 WP 1999 9 3 CALA9901116 1 19990901 A 5350 RIB DOUG DC10 DC1030 3023501 WP TAILCONE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND A 1 INCH CRACK IN RIB AT LT INNER CAVITY OF TAIL CONE. THE RIB WAS TRIMMED OUT AND THE AREA WAS REINFO RCED WITH AN ANGLE REPAIR IAW SRM 53-00-00, FIGURE 1 AND 51-31-01. 2 L 7 3 4F A22WE 1999090300842 19990903 00842 WP 1999 9 3 CALA9901117 1 19990901 A 5400 WEB DOUG DC10 DC1030 3023501 WP NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND A 5 INCH CRACK AT FORWARD WEB OF NR 2 PYLON AFTER REMOVING VERTICAL FIN. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999090300843 19990903 00843 WP 1999 9 3 CALA9901118 1 19990901 A 3397 WIRE DOUG DC9 DC932 3022066 WP EMER EXIT BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18513 48112 THE EMERGENCY EXIT LIGHT AT LOWER FORWARD CORNER OF AFT RIGHT ESCAPE HATCH DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPAIRED BROKEN WIRE AT EXIT LIGHT. 2 L 7 2 4F A6WE 1999090300844 19990903 00844 NE 1999 9 3 99UAL900435 2 19990820 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 MALFUNCTIONED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 551UA 25399 717940 THE NR 2 ENGINE WAS SHUTDOWN ON CLIMB-OUT DUE TO LOSS OF POWER AND HIGH EGT. AIRCRAFT RETURNED TO ABQ. PROBABLE ROOT C AUSE FOUND TO BE THE DISPATCH OF THE AIRCRAFT PER MEL PROCEDURES WITH EEC MAINTENANCE SWITCH IN THE AUTO POSITION AND TH E SECONDARY CHANNEL IN CONTROL. WHILE GOING THROUGH 22K FEET THE EEC HAD AN IN-RANGE SECONDARY PB SENSE FAILURE. THIS TRIGGERED A SERIES OF EVENTS THAT RESULTED IN AN ENGINE EGT OVERTEMP. THIS WAS JOINTLY INVESTIGATED BY SFOEP AND UA FL IGHT SAFETY, WITH ASSISTANCE FROM PWA AND BOEING. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999090300845 19990903 00845 NM 1999 9 3 99UAL900436 1 19990822 A 2751 834503 PROX SENSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE SLAT CONTAMINATED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 603UA 21864 LEADING EDGE DISAGREE: RTF JFK - THE PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) INITIATED FLAP/SLAT FAILURE PROTECTION SHUT DOWN AFTER SENSING AN ASYMMETRIC DIFFERENCE BETWEEN SLAT SENSORS 299, 287, AND 305. THE SUBJECT SENSORS WERE FOUND TO B E CONTAMINATED WITH EXCESSIVE GREASE AND DIRT. SUBJECT SENSORS WERE CLEANED AND OPERATIONALLY CHECKED PER MM, ALL OPS C HECKS NORMAL. FINAL BITE CHECK OF THE PSEU INDICATED NO FAULTS. 2 L 7 2 4F 4 F RT A1NM E3NE 1999090300846 19990903 00846 NM 1999 9 3 99UAL900438 1 19990820 A 5314 KEEL BEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 950 MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 7445U 21899 A DOUBLE DRILLED HOLE WAS FOUND ON THE LOWER FLANGE OF THE STRINGER 29 RIGHT KEEL BEAM CHORD AT STATION 950C. THE HOLE WAS TRIMMED OUT AND A REPAIR STRAP INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY FAA FORM 8110- 3. 2 L 7 3 4F 4 F A3WE E2EA 1999090300847 19990903 00847 NM 1999 9 3 99UAL900439 1 19990820 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 360 MISDRILLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 7445U 21899 A .1562 INCH DIAMETER HOLE WAS MISDRILLED ON THE UPPER CHORD OF THE STATION 360 FLOORBEAM AT ABOUT RBL 54. THE HOLE GOE S THROUGH THE HORIZONTAL FLANGE AND EXTENDS INTO THE VERTICAL WEB OF THE FLOORBEAM. THE DAMAGE WAS REPAIRED PER THE INS TRUCTIONS GIVEN IN TIMCO REO-06685. THIS REO CALLS FOR THE INSTALLATION OF TWO (2) ANGLES AND ONE (1) STRAP TO LOCALLY REINFORCE THE DISCREPANT AREA. THIS REPAIR HAS BEEN APPROVED BY FAA FORM 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999090300848 19990903 00848 NM 1999 9 3 99UAL900440 1 19990820 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1070 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7445U 21899 CORROSION WAS DISCOVERED ON THE UPPER CHORD OF THE STATION 1070 FLOORBEAM (P/N 65-20821-21), CENTERED ABOUT RBL 26. THE DAMAGE COVERS A SPAN OF SIX (6) FASTENER ROWS LOCATED BETWEEN THE RBL 24.75 SEAT TRACK AND THE GALLEY RAIL INBOARD OF T HIS LOCATION. A REPAIR STRAP WAS INSTALLED ON THE FLOORBEAM UPPER CHORD PER THE INSTRUCTIONS GIVEN IN TIMCO REO-06686. THIS REPAIR WAS APPROVED PER AN FAA FORM 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999090300849 19990903 00849 NM 1999 9 3 99UAL900444 1 19990823 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ROW 7ABC INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 362UA 24455 EMERGENCY EXIT LIGHTS AT 7A, B, AND C FLOOR INOPERABLE. SECURED LIGHT STRIP, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999090300850 19990903 00850 NM 1999 9 3 DHL9970101A 1 19990829 A 5320 WEB BOEING 727 72730C 1384009 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 701DH 19011 AT A CHECK, 3.5 INCH CRACK NOSE WHEEL WELL 15 AFT OF FWD BULKHEAD LEFT SIDE. STOP DRILLED CRACK, FABRICATED REPAIR DOUB LER PER SRM 41-40-2. 2 L 7 3 4F A3WE 1999090300851 19990903 00851 NM 1999 9 3 DHL99702001 1 19990831 A 2780 BOLT BOEING 727 72730C 1384009 NM NR 2 LE FLAP LOOSE A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 702DH 19793 WHEN SELECTING FLAP 2 DEGREE UPON FLAP RETRACTION, AMBER L/E LIGHT FAILED TO EXTINGUSH. NO AMBER L/E LIGHTS ON S/O AUX PANEL WERE ILLUMINATED. FOUND AND SECURED 1 THROUGH BOLT ON FLAP DETENT SWITCH. CHECKED ADJUSTMENT AND OPS CHECK GOO D. 2 L 7 3 4F A3WE 1999090300852 19990903 00852 NM 1999 9 3 VNAA9908009 1 19990827 A 7603 FRICTION LOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT STUCK A VNAA K NONE O OTHER NR NOT REPORTED 1 GL 07 328JS 3030 FLIGHT CREW REPORTED CONDITION LEVER VERY HARD TO MOVE AND FRICTION KNOB STUCK. MAINTENANCE INSPECTED AND LOOSENED THE FRICTION KNOB, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-10-00. FUNCTION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999090900001 19990909 00001 EU 1999 9 9 VTZA990214 1 19990707 A 3250 AIR860020 SELECTOR BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 485UE 901 IA/ROA - FLT 7201 - DURING TAKEOFF, CREW ABORTED TAKEOFF DUE TO AIRCRAFT PULLED LEFT ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED STEERING SELECTOR, OPS CHECK OK. AIR CRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999090900002 19990909 00002 NE 1999 9 9 VTZA990218 2 19990712 A 7260 31059291 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 319UE 41042 IAD/ILM - FLT 7371 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AND RETURNED TO IAD DUE TO RT OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RIGHT CHIP DETECTOR ASSY. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999091000002 19990910 00002 CE 1999 9 10 99ZZZX3274 1 19990816 A 3230 2710969 SELECTOR VALVE PARKERHANFIN CESSNA 500 550 2076604 CE NLG FAILED A A IMJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 25 122G 9679 073B 5500110 THE LANDING GEAR CONTROL VALVE FAILED TO RETRACT GEAR. THIS WAS DISCOVERED WHEN THE CREW SELECTED 'GEAR UP' AFTER TAKEO FF. THIS IS THE ORIGINAL VALVE INSTALLED IN THE AIRCRAFT AT MANUFACTURER (20 YEARS OLD). 1 L 7 2 4F A22CE 1999091000024 19990910 00024 GL 1999 9 10 99ZZZX3296 2 19990606 A 7200 ENGINE BOLKMS 105 BO105LSA3 5626020 EU ALLSN 250C 250C28C 03013 GL ENGINE BAY MALFUNCTIONED A BRMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 93LF 2450 846 2038 CAE280105 FLYING FROM POCATELLO TO TWIN FALLS, PILOT ENCOUNTERED ABNORMAL TORQUE CHANGES IN NR 1 ENGINE. IT HAPPENED TWICE. PILO T NOTED LOW OIL PRESSURE, THEN NO OIL PRESSURE. THE NR 1 ENGINE IS SHUT DOWN IN-FLIGHT AND A LANDING WAS MADE AT BURLEY AIRPORT. NO EXTERNAL OIL LEAKS FOUND. OIL LEVEL ALMOST AT MAXIMUM AT THE DAILY INSPECTION. SUBMITTER SUGGESTED PROBL EM INTERAL TURBINE OR GEARBOX SEAL. 1 G 7 2 3U 3 U H3AU E1GL 1999091000051 19990910 00051 CE 1999 9 10 99ZZZX3325 1 19990805 A 2810 50389035 FUEL CELL BEECH 99 B99 1154004 CE FUSELAGE LEAKING A TIMA K NONE L NO TEST IN INSP/MAINT 1 NM 07 99TH U155 FUEL WAS FOUND LEAKING FROM AREA OTHER THAN FUEL SUMP. TROUBLESHOT PROBLEM TO SMALL HOLE AT UPPER, AFT CORNER. REPLACE D FUEL CELL WITH SERVICEABLE FUEL CELL IAW BEECH 99 MM. THE AGE OF THE OLD FUEL CELL COULD NOT BE DETERMINED BY RELIABLE MEANS, BUT WAS SUSPECTED TO BE PART OF THE PROBLEM. ALL HANGERS WERE IN PLACE AND DID NOT CAUSE THE SOURCE OF THE LEAK . 1 L 7 2 3T A14CE 1999091000056 19990910 00056 CE 1999 9 10 99ZZZX3331 1 19990809 A 5312 BULKHEAD CESSNA 208 208B 2073701 CE CARGO BAY BUCKLED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 948FE 7911 208B0052 DAMAGE TO SUB-FLOOR FRAMES IN AFT CARGO AREA. FIVE BULKHEADS REQUIRED REPLACEMENT DUE TO DAMAGE POSSIBLY RELATED TO MIS HANDLED FREIGHT. THE AREA OF DAMAGE IS AT THE CARGO DOOR ENTRANCE. SUBMITTER STATED THIS IS A RECURRING PROBLEM ON THE SE AIRCRAFT FOR THE PAST YEAR. MANUFACTURER HAS BEEN NOTIFIED. 1 H 7 1 3T A37CE 1999091000058 19990910 00058 NM 1999 9 10 TWAA9912001 1 19990901 A 3350 767 BULB BOEING 767 767330 NM ROW 16-21 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 THE EGRESS LIGHTS WERE INOPERATIVE ON LT SIDE OF CABIN FROM ROW 16 THRU 21 AND ROW 35 THRU 42. THE NUMBER 4 AFT EXTERI OR OVERWING EMERGENCY LIGHT WAS ALSO INOPERATIVE. RESEATED CONNECTOR AT ROW 21 LEFT SIDE, AND ROW 42 LEFT SIDE FOR THE EGRESS MALFUNCTIONS, AND RELAMPED THE EXTERIOR EMERGENCY LIGHT. CHECK-C 6-8-99 MCI. 2 L 7 2 4F RT A1NM 1999091000059 19990910 00059 WP 1999 9 10 AT9900612 1 19990825 A 5321 47089A7 FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CABIN FLOOR PANEL AT BS 200-237 CORRODED. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-2, 51-30-3, 53-21-0. 2 L 7 2 4F A6WE 1999091000060 19990910 00060 WP 1999 9 10 AT9900613 1 19990827 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CABIN FLOOR PANEL AT BS 160-200 CORRODED. REMOVED HAT SEC TIONS, CUT AND DRILLED NEW SKIN PANEL AND INSTALLED HAT SECTIONS IAW DC9 SRM 53-05 PG 1, 51-30-2, 51-10-3. 2 L 7 2 4F A6WE 1999091000061 19990910 00061 WP 1999 9 10 AT9900614 1 19990722 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 955-960 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CUSP WEB CRACKED AT BS 955-960 LBL 48-52. REMOVED CUSP FO UND CORROSION. FORMED, DRILLED AND DEBURRED ONE CUSP SECTION AND FOUR REPAIR STRAPS. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 53-05 FIG 97 AND MM 53-20-1. 2 L 7 2 4F A6WE 1999091000062 19990910 00062 WP 1999 9 10 AT9900615 1 19990722 A 5320 CUSP WEB DOUG DC9 DC932 3022066 WP BS 945-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND RT CUSP WEB CORRODED AT BS 945-965. REMOVED CUSP WEB. FA BRICATED, ALODINED, PRIMED AND INSTALLED REPAIR SECTIONS OF WEB IAW DC9 SRM 53-05 FIG 97 AND MM 53-20-1. 2 L 7 2 4F A6WE 1999091000063 19990910 00063 WP 1999 9 10 AT9900616 1 19990706 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 770 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND LOWER KEEL BEAM SKIN AT BS 770 HAS AN AREA OF BULGING CORR OSION THAT HAS PUSHED OUT AND CRACKED THE SKIN. REMOVED SKIN PANEL AND LONGERONS 29L AND 29R FROM BS 658-756. DRILLED, DEBURRED, COUNTERSUNK, TREATED AND PRIMED. REINSTALLED LONGERONS AND NEW SKIN IAW DC9 SRM 51-10-1, 51-30-2, 51-30-1, 5 3-04 FIG 42, 52-05 FIG 48. 2 L 7 2 4F A6WE 1999091000064 19990910 00064 WP 1999 9 10 AT9900617 1 19990708 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 218-235 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND RT INBOARD SEAT TRACK SCRATCHED AND CORRODED AT BS 218 TO 965. REMOVED SECTION OF SEAT TRACK FROM BS 218-235 AT EXISTING SPLICE. FABRICATED REPAIR SECTION, ALODINED, PRIMED AND INSTALLED SECTION AT EXISTING SPLICE IAW DC9 SRM 51-30-2, 53-05 FIG 1, 53-05 FIG 4, 51-10-3. 2 L 7 2 4F A6WE 1999091000065 19990910 00065 WP 1999 9 10 AT9900618 1 19990714 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 870-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND AFT PIT LONGERON 30 CORRODED AT BS 870-965. CUT LONGERON FROM BS 870-955. REMOVED SHEAR TIES, FLOOR SUPPORT AND CUT FRAME AT BS 917. REMOVED LONGERON, DRILLED, DEBURRED, TREAT ED, PRIMED AND INSTALLED NEW LONGERON. INSTALLED SHEAR TIES AND FLOOR SUPPORT. FABRICATED FRAME REPAIR, TREATED, PRIME D AND INSTALLED FRAME REPAIR IAW DC9 SRM 53-01 FIG1, 51-30-2, 51-10-4, 51-10-2, 51-30-2, 53-03 FIG 2A. 2 L 7 2 4F A6WE 1999091000066 19990910 00066 1999 9 10 AT9900619 4 19990708 A 3455 ADF PANEL DOUG DC9 DC932 3022066 WP LEFT FWD ADF CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND FLAKING PAINT AND FLARE SPRAY ON LEFT FORWARD ADF PANEL. R EMOVED CORROSION AND PEELING FLARE SPRAY FROM ADF PANEL. CLEANED, PREPARED AREA AND APPLIED ASTRO STRIKE. REMOVED AND REPLACED ANTENNA FEED PLATE (P/N 4714051-503). SEALED ASTRO STRIKE. PERFORMED CONTINUITY CHECK BETWEEN ADJACENT CONDUC TIVE COMPONENTS. RESULTS NORMAL. 2 L 7 2 4F A6WE 1999091000067 19990910 00067 WP 1999 9 10 AT9900620 1 19990627 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE MISREPAIRED A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 803AT 47261 DURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FLORIDA, FOUND CLASS III TEMPORARY REPAIR ON FUSELAGE FORWARD OF RIGHT WI NG ROOT PER DC9 SRM 53-40 FIG 12B SHT 15 PAGE 60A. REMOVED BLIND RIVETS AND REPLACED WITH SOLID FASTENERS. CHANGED CLA SS III REPAIR TO CLASS I REPAIR ALL IAW DC9 SRM 51-30-1, 51-30-0, AND TIMCO RES NR 05024. 2 L 7 2 4F A6WE 1999091000068 19990910 00068 NM 1999 9 10 AT9900621 1 19990901 A 3350 BATTERY PACK BOEING 737 7372L9 1384497 NM L2-DOOR DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 466AT 21279 EXTERIOR EMERGENCY LIGHTS AFT OF R2 AND L2 DOOR DID NOT ILLUMINATE DURING ROUTINE CHECK. REMOVED BATTERY PACK. CHECKED VOLTAGE, VOLTAGE OF BATTERY CHECKS GOOD. REMOVED AND RESEATED BATTERY PACK HOUSING. LIGHTS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999091000069 19990910 00069 EU 1999 9 10 AWXA9900276 1 19990830 A 2910 D2727111C00200 HYD LINE AIRBUS 320 A320231 3930325 EU GREEN HYD SYST LOOSE A AWXA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 645AW 238 EMERGENCY DECLARED, HYD GREEN LOW LEVEL RESULTING IN LOSS OF GREEN HYDRAULIC SYSTEM. INSPECTED SYSTEMS, NO LEAKS NOTED. FOUND GREEN SYS 5 QTS LOW. SERVICED QTY, ALL SYSTEMS OPS NML. SUSPECT LOW LEVEL WARNING TRIGGERED AFTER GEAR RET AND TEMP CHANGE. 30 AUG 99- A/C ARRIVED IN SFO WITH LOW GREEN HYD. UAL TECH IN SFO FOUND AND RE-TORQUED LOOSE GREEN RUDDE R SERVO ACTUATOR LINE. RESERVICED, LEAK CHECK GOOD. 2 L 7 2 4F RT A28NM 1999091000070 19990910 00070 NM 1999 9 10 UPS99230530 1 19990821 A 5340 SEAT TRACK BOEING 727 7272A1 138407F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 950B-950C LBL 25 WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-1 0-1. REMOVED AND REPLACED SEAT TACK FROM BS 950+10 TO BS 950F+10 LBL 25 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999091000071 19990910 00071 NM 1999 9 10 UPS99230531 1 19990820 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE: SI, CORROSION ON FLOORBEAM UPPER TEE BS 620 RBL 26 TO 43. CORROSION FOUND TO BE OUT OF LIMITS ON CHORD AT RBL 31-36.5. PERFORMED FLOORBEAM REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999091000072 19990910 00072 NM 1999 9 10 UPS99230532 1 19990825 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, BS 360 FRAME IS CRACKED AT NUT PLATE HOLE, BS 360 WL 218, LBL 68. REMOVED DAMAGE, FABRICATED AND IN STALLED REPAIR PARTS PER SRM 51-40-3 PG 1-6. 2 L 7 3 4F A3WE 1999091000073 19990910 00073 NM 1999 9 10 UPS99230533 1 19990830 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, FRAME IS CRACKED AROUND FASTENER HOLE AT BS 360 LBL 68, WL 303 JUST ABOVE STR 8. DAMAGE WAS OUT OF LIMITS. CUT OUT DAMAGE AREA 2.0' X 2.4 X .050, FABRICATED REPAIR DOUBLER OUT OF 7075.0. 50. SENT TO HEAT TREAT TO-T6 C ONDITION AND INSTALLED REPAIR IAW SRM 51-40-3, SRM 51-30-2. 2 L 7 3 4F A3WE 1999091000074 19990910 00074 NM 1999 9 10 UPS99230534 1 19990814 A 5720 BEAM BOEING 727 7272A1 138407F NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, SPOILER BEAM MOUNT PAD FOR NR 6 FLAP TRACK IS CORRODED (ON WING SIDE). REMOVED AND REPLACED SPOILER BEAM MOUNT PAD PER SRM 51-20-151, 51-30-2. 2 L 7 3 4F A3WE 1999091000075 19990910 00075 NM 1999 9 10 UPS99230536 1 19990826 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 372-377 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK B STA 372 TO 377, LBL 45, WL 208. CORROSION CLEAN-UP BEYOND ACCEPTABLE LIMI TS. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-5 AND 51-30-8. 2 L 7 3 4F A3WE 1999091000076 19990910 00076 NM 1999 9 10 UPS99430528 1 19990831 A 3231 SAFETY VALVE BOEING 747 747121 1384871 NM MLG DOOR FAILED A IPXA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 682UP 20349 RIGHT BODY GEAR DOOR OPENED DURING DESCENT, 3000 FT, 220KTS. BOTH PRIMARY AND ALTERNATE SHOWED DOOR OPENED. THE DOOR D ID CLOSE AFTER LANDING GEAR WAS EXTENDED. FOUND BODY RT BODY GEAR DOOR SAFETY VALVE BYPASSING TOG 36550. REMOVED AND R EPLACED BODY GEAR DOOR SAFETY VALVE IAW B747 MM 32-33 -29, (NO HELP) NEEDS RIGG CHECK, PERFORMED CHECK PER MM 32-53-00, JACKED ACFT. GROUND OPS CHECK GOOD, OK FOR SERVICE. 2 L 7 4 4F A20WE 1999091000077 19990910 00077 NM 1999 9 10 UPS99430529 1 19990831 A 5320 DOUBLER BOEING 747 747123F NM AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE:N/A,TAIL SKID AREA SHOWS 2.25 INCH CRACK. REPAIRED CRACK PER SRM PAGE 53-30-03 PAGE 21 FIC/A SHEET 4 . INSTALLED PERMANENT REPAIR DOUBLER. 2 L 7 4 4F A20WE 1999091000078 19990910 00078 WP 1999 9 10 UPS99830537 1 19990823 A 5720 FITTING DOUG DC8 DC873F 302199F WP BS 693 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, RIGHT WING O/B AILERON ATTACH FITTING CRACKED (VERIFIED BY EDDY CURRENT INSP) AT LOWER MOUNT BOLT HO LES BELOW AILERON DAMPERS STA XW 693. INSTALLED NEW FITTING STA 693 AND TORQUED PER DC8 M/M 20-16-0 & 57-40- 00. REMOV ED R/W O/B AILERON ATTACH FITTING. REMOVED RT I/B LOWER ATTACH FITTING BOLT AT STA 693 REAR SPAR IAW DC8 SRM 51-3-0. I NSTALLED NEW BOLT & TORQUED IAW DC8 M/M 20-16-0, INSTALLED NEW FITTING AT STA 693 IAW DC8 M/M 20-16-0 & 57-40-0. 2 L 7 4 4F RT 4A25 1999091000079 19990910 00079 WP 1999 9 10 UPS99830541 1 19990725 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, FUSELAGE SKIN EXTERIOR BULGED STA 620 L33R-L34R DOT S851. REMOVED CORROSION AND FOUND SKIN TO BE BE YOND ALLOWABLE LIMITS. REMOVED SKIN AND INTERNAL DOUBLERS. FABBED AND INSTALLED NEW SKIN AND DOUBLERS IAW DC8 SRM 53-4 -1, 51-1-8, 51-1-20D, 51-1-21 AND DAW DWG NR 5754992. FABRICATED REPAIR SPLICES. 2 L 7 4 4F RT 4A25 1999091000080 19990910 00080 WP 1999 9 10 UPS99830542 1 19990726 A 5320 JAMB DOUG DC8 DC873F 302199F WP BS 190 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, MAIN CABIN R-1 DOOR JAM IS CRACKED AT STATION 190 L21R. REMOVED DAMAGED WEB, FABBED AND INSTALLED W EB IAW DC8 SRM 51-1-8, 53-2 -0, 51-1-21 & DAC DWG 5615700. 2 L 7 4 4F RT 4A25 1999091000081 19990910 00081 WP 1999 9 10 UPS99830546 1 19990726 A 5312 BULKHEAD ANGLE DOUG DC8 DC873F 302199F WP AFT PRESS BLKHD CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, CORROSION ON AFT PRESS BULKHEAD FLOORBOARD SUPPORT ANGLE ABOVE LONG 32R. EXFOLIATED BEYOND LIMITS I AW DC8 SRM 53-2-0. FABBED NEW ANGLE IAW DWR NR 5753522. LOCATED, DRILLED AND DEBURRED NEW ANGLE, OK TO TREAT IAW DC8 S RM 51-3-2. 2 L 7 4 4F RT 4A25 1999091000082 19990910 00082 WP 1999 9 10 UPS99830547 1 19990818 A 5720 INTERCOSTAL DOUG DC8 DC873F 302199F WP WS 339 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, LEFT WING, TRAILING EDGE STA 339, INTERCOSTAL CRACKED FITTING CHAFED OUT OF LIMITS. REMOVED INTERCO STAL, FABRICATED AND INSTALLED INTERCOSTAL AND NEW SUPPORT FITTING (P/N 5707538-3) IAW DC8 SRM 57-5-1 & 51-1-21. 2 L 7 4 4F RT 4A25 1999091000083 19990910 00083 WP 1999 9 10 UPS99830548 1 19990803 A 5315 FLOOR BEAM DOUG DC8 DC873F 302199F WP BS 920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, CORROSION AND POPPED RIVETS AROUND FASTENERS ON FLOOR SUPPORT BEAM FS 920 LT SIDE OF FUSELAGE. FABB ED ANGLE ON TIMCO OPS 50017, SHOT PEENED IAW DC8 SRM 51-1-4A. DRILLED AND SLOTTED CRACK IN FLOORBEAM IAW REO 06663 REV B. FABBED DOUBLER AND SHIM IAW REO 06663 REV B. DYE PEN ON STOP DRILL IAW DPS 4707-1, NO CRACK NOTED. REMOVED AND REI NSTALLED LT MLG MANUAL FREE FALL PULLEY IAW DC8 SRM 51-3-0. INSTALLED REPAIR IAW DC8 SRM 51-1-20D & 51-3-0. 2 L 7 4 4F RT 4A25 1999091000084 19990910 00084 WP 1999 9 10 UPS99830549 1 19990730 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, STA 70 L36 STANCHION FITTING CRACKED. REPLACED CHANNEL (P/N 5613064-107), FITTING (P/N 4646944-501) . FABBED PLATE IAW DAC DWG 5613064. FABBED LT STANCHION PER DAC DWG 5613064. LOCATED AND DRILLED NEW RT STANCHION & F ITTING. INSTALLED NEW FITTINGS AND STANCHIONS PER DC8 SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1999091000085 19990910 00085 WP 1999 9 10 UPS99830552 1 19990730 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, AFT PIT FS 1040 CORROSION ON LOWER SURFACE OF UPPER FRAME FLANGE AT L31R. REMOVED FLOORBEAM, SUPPOR T, END FITTING, INTERCOSTALS, FRAME ANGLE, FRAME CAP AND FRAME SECTION. LOCATE NEW FRAME SECTION, DRILLED AND REAMED EX ISTING HOLES AND INSTALLED FRAME SECTION. REINSTALLED FLOORBEAM, SUPPORT, END FITTING, INTERCOSTALS, FRAME ANGLE AND FR AME CAP IAW DC8 SRM 51-1-21 & 51-1-20D. 2 L 7 4 4F RT 4A25 1999091000086 19990910 00086 WP 1999 9 10 UPS99830553 1 19990727 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, APB FLOORBOARD SUPPORT ANGLE CRACKED AND EXFOLIATED AT LBL 7. BLENDED SUPPORT ANGLE IAW DC8 SRM 51- 1-8. FOUND OUT OF LIMITS IAW DC 8 SRM 53-2-0. FABBED NEW ANGLE IAW DRW NR 5753522. REMOVED PULLEY BRACKET ASSY AT STA 1766 SYS LTSD. REMOVED PULLEY BRACKET ASSY RUDDER SYS LTSD STA 1766. INSTALLED PULLEY AND BRACKET ASSY AT STA 1766 IA W DC8 MM 27-30-00 & 27-20-00. 2 L 7 4 4F RT 4A25 1999091000087 19990910 00087 WP 1999 9 10 UPS99830555 1 19990726 A 5246 WEB DOUG DC8 DC873F 302199F WP RT FUEL DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, FITTING CRACKED INSIDE RT FWD SERVICE DOOR TORQUE BOX AT LWR FWD CORNER OF DOOR FRAME. REMOVED WEB TO GAIN ACCESS TO FITTING AND FOUND WEB & ANGLE TO BE CORRODED BEYOND LIMITS. REMOVED FITTING, FABBED NEW FITTING, NEW WEB AND ATTACH ANGLE. INSTALLED ALL IAW DWG NR 5615700 2024-T3 & T6, NR 2649 943, & DC8 SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 1999091000088 19990910 00088 EU 1999 9 10 QXEA9901679 1 19990901 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 483US 11233 SEA- FORWARD OVERHEAD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999091000089 19990910 00089 EU 1999 9 10 QXEA9901680 1 19990831 A 2611 0158500781 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 491US 11156 BOI - DURING CLIMB, LAVATORY SMOKE ALARM SOUNDED. NO SMOKE WAS NOTED UPON INVESTIGATION. DEFERRED LAVATORY IAW MEL 26- 7 (A/B). AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 9/2 BY REPLACING THE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999091000090 19990910 00090 NM 1999 9 10 99FDEA00359 1 19990901 A 2120 56697 CONTROL VALVE BOEING 727 72722C 138400F NM E&E COMPT FAILED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 103FE 19199 BURNING SMELL IN COCKPIT AREA AND IN BULKHEAD AREA NEXT TO LAVATORY. REPLACED FLOW CONTROL VALVE PER B727 MM 21-58-021- 4. NO FURTHER SMELLS DETECTED. A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 1999091000091 19990910 00091 NM 1999 9 10 99FDEA00360 1 19990902 A 5530 BUSHING DOUG MD11 MD11F 3023600 NM VERT STAB OVERSIZE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 585FE 48481 RT BANJO NR 4 FITTING AFT LWR FASTENER'S HOLE FOUND INSTALL WITH BUSHING OF DIAMETER 0.593 IN EXCEED MAX REWORK DIAMETER OF HOLE SIZE 0.450. REPAIRED FITTING AS PER EA 1-5530-47413 & EA 1-5530-47414. 2 L 7 3 4F RT A22WE 1999091000092 19990910 00092 NM 1999 9 10 99FDEA00361 1 19990902 A 5320 655624913 SPLICE BOEING 727 727277 138408S NM BS 1005-1012 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 CORROSION ON LT KEEL BEAM STRINGER SPLICE BS 1005-1012 O/B FLANGE (SPEC C53-113-01(2)). *S/D* LT KEEL BEAM STR SPLICE TO BE REPLACED ON NR 252. 2 L 7 3 4F RT A3WE 1999091000093 19990910 00093 NM 1999 9 10 99FDEA00362 1 19990902 A 5313 655623654 STRINGER BOEING 727 727277 138408S NM BS 675 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 WHILE WORKING NR 233 FOUND CORROSION IN STR 27 RT, BS 675 (FWD BAY). *S/D* REPAIRED STR 27 RT, BS 668-680 IAW FEDEX SR M 53-10-3. 2 L 7 3 4F RT A3WE 1999091000094 19990910 00094 WP 1999 9 10 ABXA9900678 1 19990827 A 5250 AR25291 HANDLE DOUG DC8 DC861 3021952 WP COCKPIT DOOR DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 UNABLE TO OPEN COCKPIT DOOR FROM INSIDE COCKPIT. REPAIRED COCKPIT DOOR HANDLE, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999091000095 19990910 00095 NM 1999 9 10 DL72S991910 1 19990826 A 5320 651751737 CHANNEL BOEING 727 727232 1384082 NM BS 1263, CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 THE AFT CHANNEL AT FS 1263 ON THE RT TORQUE BOX OF THE VENTRAL STAIRWAY WAS FOUND WITH A TYPICAL CRACK PER B727 S/B 53-0129. THE CRACK PART WAS REMOVED AND REPLACED WITH A NEW CHANNEL PER ER/A 368109-14AD. 2 L 7 3 4F A3WE 1999091000096 19990910 00096 NM 1999 9 10 DL757991911 1 19990827 A 2570 INSULATION BOEING 757 757232 1384965 NM BS 1440 BURNED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 626DL 22916 FOUND INSULATION BLANKET BEHIND E-6 RACK ADJACENT TO APU GROUND STUD ATTACHMENT TO BE BURNED. NO APPARENT DAMAGE TO SUR ROUNDING STRUCTURE WAS NOTED. IT APPEARS THAT LINT/DEBRIS COVERED THE BLANKET AND THE BLANKET WAS IGNITED. 2 L 7 2 4F RT A2NM 1999091000097 19990910 00097 NM 1999 9 10 DL72L991912 1 19990820 A 5743 65196709 TRACK BOEING 727 727232 1384082 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 NR 4 I/B FLAP TRACK, TYPICAL CORROSION FOUND AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUG. AUTHORIZED MACHINE BLENDING OF PADS AND LUG FACES. 2 L 7 3 4F A3WE 1999091000098 19990910 00098 NM 1999 9 10 DL738991913 1 19990826 A 3397 WIRE BOEING 737 737832 13844CF NM ROW 12DEF LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DA 29623 SEAT 12DEF EEPLS LIGHT INOP. FOUND WIRE PULLED OUT OF QD BEHIND SIDEWALL AT SEAT 12DEF. RECONNECTED LIGHT, CKS GOOD. 2 L 7 2 4F RT A16WE 1999091000099 19990910 00099 NM 1999 9 10 DL738991914 1 19990826 A 3350 SOCKET BOEING 737 737832 13844CF NM L1 DOOR DIRTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 375DA 29623 EXTERIOR EMER LIGHT AT L1 DOOR INOP. CLEANED SOCKET CONTACTS, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999091000100 19990910 00100 NM 1999 9 10 DL73K991915 1 19990827 A 2121 FAN 215201 BOEING 737 737232 1384475 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 324DL AA25283OFF 23096 AT DEPARTURE - WHEN FLT CREW SWITCHED ON GASPER FAN GOT ELECTRICAL SMELL IN COCKPIT AND CABIN. REMOVED BAGS FROM FWD B/ B AND PULLED AFT WALL TO CONFIRM GASPER FAN AT FAULT. REPLACED GASPER FAN, OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 1999091000101 19990910 00101 NM 1999 9 10 DL72K991916 1 19990827 A 2121 215201 FAN BOEING 727 727232 1384082 NM A/C COMPT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 417DA 21259 STRANGE SMELL, STRONG AT TIMES COMING FROM PACKS IN FLT. PACK TEMPS REMAINED NORMAL, SMOKE ID/RMVL CHECLIST WAS RUN TO COMPLETION. NO SMOKE WAS VISIBLE JUST ODOR. REPLACED GASPER FAN. 2 L 7 3 4F A3WE 1999091000102 19990910 00102 NM 1999 9 10 DL73K991917 1 19990827 A 3510 MASK MC1017100 BOEING 737 737247 138448D NM COCKPIT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 14411 23187 OBSERVERS 02 MASK FAILED. REPLACED OBSERVERS 02 MASK. 2 L 7 2 4F A16WE 1999091000103 19990910 00103 NM 1999 9 10 DLM88991918 1 19990828 A 2530 OVEN 50459 DOUG MD88 MD88 3023688 NM FWD GALLEY DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 903DL 49534 EN ROUTE TO MKE ON FLT 1872/28, THE FLT CREW REPORTED BURNING SMELL IN FWD GALLEY. FOUND FOOD BOILED OVER IN OVEN, NO V ISIBLE SMOKE OCCURRED. CLEANED OVEN. 2 L 7 2 4F RT A6WE 1999091000104 19990910 00104 NM 1999 9 10 DL72S991920 1 19990828 A 3244 TIRE B727M232 BOEING 727 727232 1384082 NM NR 1 FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 516DA DL932 21432 NR 1 TIRE BLOWN. REPLACED NR 1 WHEEL AND BRAKE. ALSO REPLACED NR 2 WHEEL. 2 L 7 3 4F A3WE 1999091000105 19990910 00105 WP 1999 9 10 DLL19991921 1 19990828 A 3350 5165741 POWER PACK LKHEED 1011 10113853 5265020 WP L3 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 193H1202 CEILING AND EXTERIOR EMERGENCY LIGHTS AT L3 DOOR INOP. REPLACED EMERGENCY LIGHT POWER PACK AT L3 DOOR. EMERGENCY LIGHT S CHECK GOOD PER MM. 2 L 7 3 4F A23WE 1999091000106 19990910 00106 NM 1999 9 10 DL72K991922 1 19990829 A 3411 ZH83230204 HOSE BOEING 727 727232 1384082 NM RT INSTR PANEL LEAKING A DALA K NONE G MULTIPLE FAILURE CR CRUISE 1 SO 27 417DA 21259 CAPT AND F/O AIRSPEED AND ALTITUDE DISAGREES (30-50 KTS SLOWER ON F/O'S) 2,000 FT LWR ON F/O'S. WHEN F/O WENT TO ALTERN ATE, IT TRIPPED THE CADC OFF LINE. CAPT'S NUMBERS APPEARED CORRECT, F/O'S APPEARED INCORRECT. FOUND STATIC LEAK AT FL EX HOSE TO ALT ALERT IND. REPLACED HOSE AND IND. REPLACED ADC. PUMP-UP PITOT-STATIC LEAK CK OK. 2 L 7 3 4F A3WE 1999091000107 19990910 00107 WP 1999 9 10 DLL19991923 1 19990828 A 3230 2680262M6 RETRACT MECH LKHEED 1011 10113853 5265020 WP LANDING GEAR MALFUNCTIONED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 754DL 193Y1181 ON APPROACH GEAR WOULD NOT EXTEND NORMALLY. NO ABNORMAL INDICATIONS NOTED. EXTENDED GEAR USING MANUAL EXTENSION HANDLE S. INITIAL INDICATIONS INTRANSIT LIGHT AND GEAR DOOR LIGHTS ONLY. 2 L 7 3 4F A23WE 1999091000108 19990910 00108 NM 1999 9 10 DL733991924 1 19990829 A 5270 TARGET BOEING 737 737347 1384647 NM CARGO DOOR BENT A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 313WA 23599 AFT CARGO LIGHT ILLUMINATED AT APPROX 1000 FT MSL. FOUND TARGET BENT, REPOSITIONED SAME. CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1999091000109 19990910 00109 WP 1999 9 10 DLL14991925 1 19990829 A 5720 1556399101 STIFFENER LKHEED 1011 1011385115 5265015 WP BS 983 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 741DA 193C1245 THE RBL 22.5 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR (FS 983) WAS FOUND WITH A TYPICAL CRACK EMANATING FROM A LIGHTENING HOLE IN THE STIFFENER WEB NEAR THE UPPER END. THE STIFFENER WAS REMOVED AND REPLACED WITH A NEW STIFFENER MANUFACTURED WITHOUT LIGHTENING HOLES PER ER/A 368106-14AD. 2 L 7 3 4F A23WE 1999091000110 19990910 00110 NM 1999 9 10 DL72W991926 1 19990829 A 5330 65545901 SKIN BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION BETWEEN FS 720 & 720A AND BETWEEN S-28L & 28R. THE DAMAGE W AS ADJACENT TO AN EXISTING REPAIR CUTOUT. THE EXISTING CUTOUT WAS ENLARGED TO 8.8 X 25 TO REMOVE ALL DAMAGE. THE CUTO UT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 368118-14, REV B. 2 L 7 3 4F A3WE 1999091000111 19990910 00111 NM 1999 9 10 DL75A991927 1 19990830 A 2560 MEGAPHONE MV10 BOEING 757 757212 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752AT 23128 AFT CABIN MEGAPHONE MISSING. INSTALLED NEW MEGAPHONE. 2 L 7 2 4F RT A2NM 1999091000112 19990910 00112 NM 1999 9 10 DL76L991928 1 19990830 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 192DN 28449 ENERG LIGHTS INOP ON FWD BUSINESS ELITE SEATS. REMOVED AND REPLACED LIGHT ASSY FWD SIDE 3 F/G AND POWER SUPPLY. 2 L 7 2 4F RT A1NM 1999091000113 19990910 00113 NM 1999 9 10 DL72L991929 1 19990809 A 5754 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 AT HMV2, FOUND NR 6 L/E SLAT 10TH RIB FROM I/B END IS CRACKED IN TWO PLACES. REMOVED RIB, FABBED NEW PER SRM 51-00 AND INSTALLED. 2 L 7 3 4F A3WE 1999091000114 19990910 00114 WP 1999 9 10 DLL19991930 1 19990830 A 2910 HYD LINE LKHEED 1011 10113853 5265020 WP RT WING CRACKED A DALA O OTHER K FLUID LOSS DE DESCENT 1 SO 27 764DA 193H1202 DURING DESCENT, -B- HYD SYSTEM FLUID LEVEL DROPPED TO 1/4 AND RESERVOIR LOW QTY LIGHT ILLUMINATED. REPLACED -B- SYSTEM RETURN LINE AT RT INBD GROUND SPOILER PER MM. SVCD -B- SYSTEM HYD LK CK AND OPN CK NORMAL. 2 L 7 3 4F A23WE 1999091000115 19990910 00115 NM 1999 9 10 DL72L991931 1 19990831 A 5532 651746160 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 THE VERT STAB LT SKIN WAS FOUND CRACKED WITH A TIME LIMITED REPAIR LOCATED AT BS 1203 WL 295. THE RESULTANT TRIM OUT IS APPROX 1.25 IN DIAMETER. REPAIRED PER ERA 333479-14, REV C. 2 L 7 3 4F A3WE 1999091000116 19990910 00116 NM 1999 9 10 DL72L991932 1 19990831 A 5330 65583855 SKIN BOEING 727 727232 1384082 NM BS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 A CRACK WAS FOUND IN THE FUSE SKIN AT APPROX BS 947 ON THE LT AT S18A AND CUTOUT. REPAIRED PER ERA 333475-14, REV C. 2 L 7 3 4F A3WE 1999091000117 19990910 00117 NM 1999 9 10 DL72L991933 1 19990831 A 5330 655457489 SKIN BOEING 727 727232 1384082 NM BS 580 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 LFEC INSPECTION (PER SI 4-74176-12AD) ON THE S4R LAP JOINT REVEALED CRACK INDICATIONS BETWEEN BS 480 AND 680. INTERNAL HFEC INSPECTIONS CONFIRMED THIRTEEN (13) CRACK INDICATIONS IN THE LOWER ROW OF THE LOWER SKIN. REPAIRED PER ERA 333468- 14AD, REV B. 2 L 7 3 4F A3WE 1999091000118 19990910 00118 NM 1999 9 10 DL733991934 1 19990828 A 5320 6545838 FITTING BOEING 737 7373B7 1384580 NM NLG WW CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947WP 23376 THE LT AND RT NLG DRAG BRACE ATTACH FITTING BORES WERE FOUND WITH CORROSION. THE BORES WERE OVERSIZED TO REMOVE THE CO RROSION AND PERMIT INSTALLATION OF .05 THICK WALL REPAIR BUSHINGS. AL-NI-BR REPAIR BUSHINGS WERE INSTALLED IN THE REWOR KED BORES PER ER/A 368101-14, REV A. 2 L 7 2 4F RT A16WE 1999091000119 19990910 00119 NM 1999 9 10 DL72S991935 1 19990802 A 2497 BMS1331 INSULATION BOEING 727 727232 1384082 NM NR 1 ENGINE SPLIT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 ON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999091000120 19990910 00120 NM 1999 9 10 DL72W991936 1 19990815 A 2497 BMS1331 INSULATION BOEING 727 727247 138408F NM NR 1 ENGINE SPLIT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 ON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISC WITH NEWTYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999091000121 19990910 00121 NM 1999 9 10 DL73K991937 1 19990829 A 5312 65163007 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307DL 23079 THE FS 178 BULKHEAD WEB WAS FOUND WITH A .75 CRACK AT LBL 6.7 WL 208 AND ANOTHER .75 CRACK AT BL 0 WL 190. THERE WAS A N EXISTING DOUBLER REPAIR INSTALLED TO REPAIR OTHER PREVIOUS CRACK CUTOUTS. THE EXISTING DOUBLER WAS REMOVED, THE WEB I NSPECTED, THE NEW CRACKS ROUTED OUT, AND A LARGER ALUMINUM DOUBLER INSTALLED PER ER/A 368119-14, REV B. 2 L 7 2 4F RT A16WE 1999091000122 19990910 00122 NM 1999 9 10 DL72S991938 1 19990830 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 380-400 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & FS 481, CONFIRMED TWO CRACKS BETWEEN FS 380 & 480. THE CRACKED AREA WAS ROUTED OUT OF THE SKIN LAP AND REPAIRE D WITH AND EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 368132-14AD. 2 L 7 3 4F A3WE 1999091000123 19990910 00123 NM 1999 9 10 DLM88991939 1 19990831 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM RT PYLON CHAFED A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 933DL 49720 LOSS OF THE RIGHT HYD SYSTEM. INITIALLY LOST THE RIGHT PRESSURE THEN THE RIGHT HYD QTY WENT TO ZERO WITH THE TRAN SFER AND AUX PUMPS. FOUND FLEXIBLE HYD PRESSURE LINE FROM PYLON TO ENG DISCONNECT WORN THRU AT CLAMP. REPLACED HOSE AN D CLAMP. 2 L 7 2 4F RT A6WE 1999091000124 19990910 00124 NM 1999 9 10 DL72K991940 1 19990831 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM ROW 16 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 4577 21583 EMERGENCY LIGHT BATTERY PACK RACK ROW 16 OVERHEAD TEST BAD. REPLACED BATTERY PACK RACK. 2 L 7 3 4F A3WE 1999091000125 19990910 00125 NM 1999 9 10 DL72W991941 1 19990831 A 7120 FITTING BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LOOSE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 292WA 67205 22110 695215 ON TAKEOFF NR 1 ENG HAD LOW OIL PRESSURE AND LOW OIL PRESSURE LIGHT. ALSO, OIL QTY DROPPED. RTO FOUND BANJO FITTING LO OSE AND TIGHTEND SAME. MTC FERRY ATL FOR ENGINE CHANGE. 2 L 7 3 4F 4 F A3WE E2EA 1999091000126 19990910 00126 NM 1999 9 10 DL73K991943 1 19990901 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM FWD GALLEY INOP A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 322DL 23094 ON TAXI OUT, UNABLE TO EXTINGUISH EMERG FLOOR PATH LIGHTING SYS RT SIDE OF A/C. REPLACED AFT RT EMERGENCY LIGHT PWR PAC K AND BATTERY IN FWD GALLEY CEILING. SYS OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1999091000127 19990910 00127 NM 1999 9 10 DLM11991944 1 19990901 A 3840 CIRCUITE BREAKER 8378M11 DOUG MD11 MD11 3023602 NM WATER PRESS SYS TRIPPED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 814DE 97050014 48769 TWO C/B ARE OUT FOR THE NR 1 H20 PRESSURE SYS. F/A NOTICED ELEC ODOR DURING CRUISE NEAR THIS BREAKER PANEL. REMOVED AN D REPLACED NR 1 H20 COMPRESSOR. 2 L 7 3 4F RT A22WE 1999091000128 19990910 00128 NM 1999 9 10 DL72S991946 1 19990901 A 5320 WEB BOEING 727 727232 1384082 NM BS 1266 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 FOUND ON C2 LETTER CK, .0625 INCH CRACK IN LT TORQUE BOX WEB LT SIDE STA 1266. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999091000129 19990910 00129 NM 1999 9 10 SCNA99115 1 19990826 A 3350 900542 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE FWD CENTER AISLE OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLA CED BATTERY PACK. LIGHT OPERATIONALLY CHECKED GOOD REF MM 335071. 2 L 7 3 4F RT A3WE 1999091000130 19990910 00130 NM 1999 9 10 VNAA9908010 1 19990830 A 7602 250205003 CONTROL CABLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE BENT A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 07 328JS 3030 FLIGHT CREW REPORTED LEFT ENGINE CONDITION LEVER DIFFICULT TO OPERATE. MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FERRY FLIGHT TO CAK. THE LEFT HAND CONDITION LEVER CONTROL CABLE WAS REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL 76- 11-31. FUNCTION CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999091000172 19990910 00172 NM 1999 9 10 TWAA9912101 1 19990902 A 5610 141N485066 WINDOW BOEING 757 757231 1384950 NM LT COCKPIT WORN A TWAA K NONE O OTHER CR CRUISE 1 CE 05 718TW 28486 DURING CRUISE THE R2 WINDOW HEAT TERMINAL SHORTED OUT MELTING THE INSULATION. PLACARD WINDOW HEAT INOPERATIVE PER MEL. *S/D* FOUND THE POWER TERMINAL SHORTED OUT AT THE WINDOW. REPLACED THE WINDOW AND SHORTED TERMINAL. 2 L 7 2 4F RT A2NM 1999091000173 19990910 00173 WP 1999 9 10 TWAA9912102 1 19990903 A 3350 59128 POWER STRIP DOUG DC9 DC982 3022082 WP ROW 7-15&28 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 922TW 48013 DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOP AT ROW 7-15 AND 28 AFT. REPLACED POWER LIGHT STRIP. AC-12 STL 7-17-99. 2 L 7 2 4F A6WE 1999091000174 19990910 00174 1999 9 10 AT9900632 4 19990903 A 2210 25878313 COMPUTER DOUG DC9 DC932 3022066 WP E/E COMPT MALFUNCTIONED A ZZDA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 15 801AT 47275 CREW REPORTED YAW OSCILLATIONS DURING CLIMB-OUT. UNSURE IF IT WAS A YAW DAMPER PROBLEM OR AND ENGINE MALFUNCTION. AFTE R LANDING DETERMINED TO BE A YAW DAMPER PROBLEM. REMOVED AND REPLACED STAB AUGMENTATOR COMPUTER. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999091000175 19990910 00175 EU 1999 9 10 MALA976555 1 19990828 A 2434 23080031 GENERATOR SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 433XJ 433 DURING FLIGHT, RT DC GEN ILLUMINATED, FOLLOWED QRH AND GEN WON'T RESET. RETURNED TO DTW. MAINTENANCE REPLACED RIGHT DC GEN. OPS CHECK GOOD IAW SF340 MM ATA CHAP. 2 L 7 2 4T RT A52EU 1999091000176 19990910 00176 EU 1999 9 10 MALA976556 1 19990816 A 5753 SKIN SAAB SF340 SF340A 7850100 EU RT TE FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 076 DURING HEAVY CHECK, ON THE RIGHT FLAP LOWER SKIN PANEL WS 138, INNER SKIN SURFACE TEARING IS NOTED. MAINTENANCE REPAIRE D IAW EO NR S57023. 2 L 7 2 4T RT A52EU 1999091000177 19990910 00177 EU 1999 9 10 MALA976557 1 19990816 A 5720 ANGLE SAAB SF340 SF340A 7850100 EU WS 142 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 076 DURING HEAVY CHECK, RIGHT FLAP ASSEMBLY HI-LOCKS BROKEN, RIB SUPPORT ANGLE AT WS 142 IS CRACKED. MAINTENANCE COMPLETED AD 99-04-17. 2 L 7 2 4T RT A52EU 1999091000178 19990910 00178 EU 1999 9 10 MALA976558 1 19990816 A 5711 SPAR SAAB SF340 SF340A 7850100 EU WS 142 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 076 DURING HEAVY CHECK INSPECTION, CRACK FOUND AT WS 142 REAR SPAR. MAINTENANCE REPAIRED WITH GENERIC EO NR S57007 IAW SRM 57-80-10. 2 L 7 2 4T RT A52EU 1999091000179 19990910 00179 EU 1999 9 10 MALA976559 1 19990831 A 7712 TQ IND SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 423XJ 423 RIGHT TORQUE GAUGE FLUCTUATES IN CLIMB 2-3 PERCENT, NOTED 84 PERCENT POWER SET, ALL OTHER INDICATIONS NORMAL AND CONSTAN T. AIRCRAFT RETURNED TO DTW. MAINTENANCE GROUND RAN AIRCRAFT, ALL SYSTEMS CHECK GOOD. FOUND 2-3 PERCENT TORQUE FLUCTU ATIONS IN LIMITS PER GE MM 72-00-00 PAGE 516 TABLE 501. 2 L 7 2 4T RT A52EU 1999091000180 19990910 00180 SO 1999 9 10 LR7A9956 1 19990902 A 5320 343493L FITTING LKHEED 382 382G 526414U SO BS 858 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING SCHEDULED A-1 CHECK PER CARD HA 1201, FOUND FS 858 LT FITTING CRACKED AT LOWER AFT SIDE OF SLOPING LONGERON ATTAC H. REPLACED FITTING PER SRM 53-10. 2 H 7 4 4T A1SO 1999091000181 19990910 00181 EU 1999 9 10 JBXA9900102 1 19990902 A 2130 PRSOV FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1&2 FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 105ML 11475 FLT NR 668 RDU/MCO ON CLIMB-OUT HAD BLEED 1 AND 2 FAULT AND PRESS CONTROLLER FAULT ON MFDU. RETURN TO RDU AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 PROSV. OPERATIONAL AND LEAK CHECKS ARE GOOD IAW F-100 MM 36-11-05. AL SO, PERFORMED SELF TEST OF NR 1 AND NR 2 CPC. OPS CHECK GOOD IAW F-100 MM 21-31-01. 2 L 7 2 4F 4 F RT 1999091000182 19990910 00182 NM 1999 9 10 AWXA9900277 1 19990830 A 3397 13131122 WIRE BOEING 737 7373G7 1384595 NM ROW 1-5 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 EMERGENCY LIGHTS INOPERATIVE. ESCAPE PATH LIGHTING INOP ROWS 1-5. REPAIRED WIRING AISLE 3. 2 L 7 2 4F RT A16WE 1999091000183 19990910 00183 NM 1999 9 10 AWXA9900278 1 19990830 A 3397 13131122 WIRE BOEING 737 737277 1384570 NM ROW 15 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 EMERGENCY LIGHT AT ROW 15 INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 15. 2 L 7 2 4F RT A16WE 1999091000184 19990910 00184 NM 1999 9 10 AWXA9900279 1 19990831 A 3397 13131122 WIRE BOEING 737 737277 1384570 NM ROW 11L BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 EMERGENCY LIGHT AT SEAT 11L INOP. REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A16WE 1999091000185 19990910 00185 NM 1999 9 10 AWXA9900280 1 19990830 A 3397 13131122 WIRE BOEING 737 7373G7 1384595 NM ROW 2&16 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 156AW 23778 EMERGENCY LIGHT AT SEATS 16 AND 2D INOPERATIVE. SPLICED BROKEN WIRES AT 16 AND 2D. 2 L 7 2 4F RT A16WE 1999091000186 19990910 00186 NM 1999 9 10 AWXA9900281 1 19990831 A 5320 693535213 CLIP BOEING 737 737277 1384570 NM BS 7273 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 SHEAR TIE CRACKED AT STA 727B, STR 4L DOT NR 087-199. REMOVED AND REPLACED DAMAGED SHEAR TIE CLIP IAW 537 SRM 51-40-2. 2 L 7 2 4F RT A16WE 1999091000187 19990910 00187 NM 1999 9 10 AWXA9900282 1 19990831 A 5311 BAC15048180 FRAME BOEING 737 737277 1384570 NM BS 907 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 CORROSION AFT PIT STA 907 BETW STR 25L AND 26L, FRAME HAS CORROSION ON AFT SIDE WITH CRACKS AT FWD SKIN ATTACH AREA, REF X2D53002. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE AND FILLER IAW 737SRM 53-10-4, 51-10-2, AND 52-30-2. MAT'L .063 SHT 7075-0 QQA 250/13, HEAT TREATED 7075T6 FOR REPAIR ANGLE .050 SHT. 2 L 7 2 4F RT A16WE 1999091000188 19990910 00188 NM 1999 9 10 AWXA9900283 1 19990831 A 5320 BAC14902807 SHEAR TIE BOEING 737 737277 1384570 NM BS 967 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 FRAME TO FUSELAGE CLIP CRACKED, LT SIDE FS 967 STR 8L. REMOVED, FABRICATED, TREATED, PRIMED, AND INSTALLED CLIP IAW SRM 53-10-4, 51-30-2, AND 51-30-2, 7075-T6 .050. 2 L 7 2 4F RT A16WE 1999091000189 19990910 00189 NM 1999 9 10 AWXA9900284 1 19990831 A 5347 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM BS 872-877 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 SEAT TRACK HAS CORROSION STA 872-877, RBL 45. REMOVED AND FABRICATED REPLACEMENT PART BAC1520-792 FROM R659935 AND SPLI CE FROM .030 301 1/2 HARD R679407, TREATED, PRIMED AND INSTALLED IAW SRM 53-00-52, 53-10-5, AND 53-10-2. 2 L 7 2 4F RT A16WE 1999091000190 19990910 00190 WP 1999 9 10 CALA9901119 1 19990901 A 3397 WIRE DOUG DC10 DC1030 3023501 WP ROW 29-35 DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19072 46576 INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE AT SEATS 29AB TO 35AB. MAINTENANCE REPAIRED DAMAGED WIRES AT SEAT 32AB IAW WDM 33-53-03 AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1999091000191 19990910 00191 WP 1999 9 10 CALA9901120 1 19990901 A 5520 BALANCE WT DOUG DC9 DC982 3022082 WP RT ELEVATOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69826 49486 INSPECTION FOUND RT ELEVATOR O/B TIP MASS BALANCE CORRODED. THE RT WEIGHT WAS REMOVED. INSTALLED NEW RIB AND COUNTER W EIGHT IAW SRM 51-30-05. 2 L 7 2 4F A6WE 1999091000192 19990910 00192 NM 1999 9 10 CALA9901121 1 19990901 A 5315 FLOORBEAM BOEING 757 757224 1384958 NM BS 377 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 377, RBL 59-61.5. THE FLOORBEAM UPPER CHORD WAS REPAIRED IAW SRM 53-10-51 AND ECRA 5321-01060. 2 L 7 2 4F RT A2NM 1999091000193 19990910 00193 NM 1999 9 10 CALA9901122 1 19990901 A 5753 113N300319H SKIN BOEING 757 757224 1384958 NM TE FLAPS GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND LT O/B FLAP I/B UPPER PANEL GOUGED BY SPOILER HINGE FITTING BOLTS AT FLAP STA 425.5. THE PANEL WAS REP AIRED IAW ECRA 5731-01017. 2 L 7 2 4F RT A2NM 1999091000194 19990910 00194 NM 1999 9 10 CALA9901123 1 19990902 A 5320 SHEAR WEB BOEING 757 757224 1384958 NM BS 1681 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND SHEAR WEB CORRODED AT STA 1681, LBL 16.4, LBL 40.0, AND BL 0 TO LBL 10.7. THE AREAS WERE REPAIRED IAW ECRA 5321-01062 AND ECRA 5321-01063. 2 L 7 2 4F RT A2NM 1999091000195 19990910 00195 NM 1999 9 10 CALA9901124 1 19990903 A 5330 SKIN BOEING 757 757224 1384958 NM BS 456 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND A GOUGE IN FUSELAGE SKIN PANEL AT STA 456, STRINGER 27-28R. THE SKIN WAS REPAIRED IAW ECRA 5331-01066. 2 L 7 2 4F RT A2NM 1999091000196 19990910 00196 NM 1999 9 10 CALA9901125 1 19990903 A 3350 BR963180 CONNECTOR BOEING 737 7373T0 1384582 NM ROW 17 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND EMERGENCY LIGHT AT SEAT 17ABC INOPERATIVE. MAINTENANCE FOUND CONNECTOR BETWEEN EMERGENCY LIGHT FIXTURE AND SEAT HARNESS BROKEN ON HARNESS SIDE. THE SEAT HARNESS ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD . 2 L 7 2 4F RT A16WE 1999091000197 19990910 00197 NM 1999 9 10 CALA9901126 1 19990903 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 927 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND FLOORBEAM CORRODED AT STA 927, RT O/B SEAT TRACK. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-60 -51. 2 L 7 2 4F RT A16WE 1999091000198 19990910 00198 WP 1999 9 10 CALA9901127 1 19990903 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND RT RUDDER SKIN PUNCTURED APPROXIMATELY 30 INCHES DOWN FROM TOP EDGE. THE DAMAGED AREA WAS CUT OUT IAW SRM 55-03-00. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-03 AND 51-10-3. THE RUDDER WAS REBALANCED IAW SRM 55-40-1, PAG E 42. 2 L 7 2 4F A6WE 1999091000199 19990910 00199 WP 1999 9 10 9903519948 1 19990830 A 3610 DUCT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LT ENGINE BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8929E 45866 666774 AFTER TAKEOFF, THE LEFT ENGINE FIRE WARNING HANDLE AND TWO LOOP INDICATOR LIGHTS ILLUMINATED AND THE FIRE WARNING BELL S OUNDED. FLIGHT CREW NOTED THE FIRE WARNING CEASED WHEN THROTTLES WERE RETARDED TO IDLE POWER. FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARED YELLOW EMERGENCY, RETURNED TO STL, AND LANDED WITHOUT INCIDENT. MAIN BRAKES BECAME LOCKED AFTER L ANDING AND WERE COOLED TO ALLOW FOR TAXI INTO GATE AREA. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND THE 13TH STAGE DUCT CRACKED AND REPLACED SAME. ALSO, FOUND AND REPAIRED ONE BROKEN FUEL FLOW WIRE LOCATED UNDER THE SADDLE DUCT. OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1999091000200 19990910 00200 NM 1999 9 10 9903522702 1 19990825 A 2170 COALESCER BOEING 727 727225 1384077 NM LT&RT DIRTY A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 01 8877Z 21450 ON TAKEOFF, SMOKE FILLED THE CABIN AREA. PERFORMED COM PROCEDURE AND SMOKE DISSIPATED. FLIGHT LANDED IN DTW WITHOUT IN CIDENT. DTW MAINTENANCE REPLACED THE COALESCER SOCKS ON THE LEFT AND RIGHT WATER SEPARATORS. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999091000201 19990910 00201 NM 1999 9 10 9903535513 1 19990831 A 2150 PACK BOEING 757 757251 1384970 NM LEFT INOP A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 513US 23201 IN CRUISE AT FL350, CREW NOTED FUMES IN THE FLIGHT DECK AREA. THE FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. M AINTENANCE FOUND THE LEFT PACK INOPERATIVE. PLACED LEFT PACK ON MEL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1999091000202 19990910 00202 SO 1999 9 10 COMA990143 1 19990901 A 5713 12016079002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 259CA 19458 120252 DURING MAINTENANCE SERVICE CHECK, FUEL WAS FOUND LEAKING FROM RIGHT WING LOWER SKIN RIVET ON AFT OUTBOARD SIDE OF PANEL 622EB. INTERNAL INSPECTION FOUND WING STRINGER NR 8 CRACKED AT THAT LOCATION. THE STRINGER WAS REPAIRED PER EMB120 SRM 57-20-03, PAGE 201-204 AND EMB FAX SST-2243/99 DATED AUGUST 27, 1999. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999091000203 19990910 00203 EA 1999 9 10 COMA9960480 1 19990831 A 3350 CNDAIR CL600 CL6002B19 EA UNKNOWN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 OUTSIDE EMERGENCY LIGHT BY CABIN DOOR IS INOPERABLE. CLEANED LIGHT BULB SOCKET, OPS CHECK OK. 2 L 7 2 4F RT A21EA 1999091000204 19990910 00204 EA 1999 9 10 COMA9960481 1 19990830 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORZ STAB MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 936CA 9564 2453 7043 PITCH TRIM AND NOSE DOWN MESSAGE, CO-PILOT HAD TO USE STRONG FORWARD PRESSURE TO KEEP AIRCRAFT FROM CLIMBING. REPLACED THE PITCH TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 1999091000205 19990910 00205 NM 1999 9 10 UPS99230557 1 19990829 A 5310 FRAME BOEING 727 72725C 138400H NM BS1010 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON FRAME IN AFT CARGO PIT AT BS 1010 RBL 10, WL 140. REPAIRED SHEAR TIE ON FRAME AT BS 101 0, RBL 10, WL 140 PER SRM 53-10-4, 51-20-4. 2 L 7 3 4F A3WE 1999091000206 19990910 00206 NM 1999 9 10 UPS99230558 1 19990827 A 5753 65192702 TRACK BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON NR 5 FLAP TRACK AT MOUNT PAD AND FLANGE RADIUS AS MARKED. REPLACED FLAP TRACK WITH OVER HAULED TRACK P/W 65-19270-2 S/N HYY-4019. 2 L 7 3 4F A3WE 1999091000207 19990910 00207 NM 1999 9 10 UPS99230559 1 19990830 A 5753 65192509 TRACK BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI NR 2 FLAP TRACK I/B FW MOUNTING LUG IS CORRODED. REPLACED NR 2 FLAP TRACK PER 727 MM 27-51-31. 2 L 7 3 4F A3WE 1999091000208 19990910 00208 EU 1999 9 10 99FDEA00363 1 19990903 A 3610 PRESSURE CONTL AIRBUS 310 A310222 3930315 EU NR 2 BLEED AIR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 416FE 288 NR 2 BLEED AIR FAULTED, X BLEED MANIFOLD AND SHORTLY NR 1 BLEED FAULTED. REMOVED AND REPLACED NR 2 PRESSURE CONTROLLER PER MM 36-11-19, ENG RUN PERF OPS CHECK NORM. ENG RUN PER OPS CHECK NORM AT N1 40 PERCENT TEMP WAS 175 AND STABLE, MATC H NR 1 BLEED CHECK GOOD. 2 L 7 2 4F RT A35EU 1999091000209 19990910 00209 WP 1999 9 10 ABXA9900679 1 19990831 A 3230 PIVOT PIN DOUG DC9 DC941 302207N WP NLG OUT OF POSITION A ABXA K NONE J WARNING INDICATION AP APPROACH 1 GL 23 966AX 47510 NOSE GEAR WOULD NOT EXTEND AND GEAR DOORS WOULD NOT OPEN WHEN GEAR WAS EXTENDED. RECYCLED GEAR, SYSTEM FUNCTIONED NORMA L. REMOVED AND REINSTALLED AFT PIVOT PIN ON OVER-CENTER LINK TO OBTAIN 55 DEGREE ANGLE ON IDLER ARM IAW DC9 MM 32-20-00 . OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999091000210 19990910 00210 WP 1999 9 10 ABXA9900680 1 19990901 A 2750 LATCH DOUG DC9 DC941 302207N WP TE FLAPS LACK OF LUBE A ABXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 23 953AX 47608 FLAPS WOULD NOT REMAIN IN POSITION BEYOND THE 5 DEGREE DETENT. WOULD NOT LOCK IN POSITION. DECLARED EMERGENCY. LANDIN G WAS UNEVENTFUL. CLEANED AND LUBRICATED FLAP HANDLE RELEASE LATCH IAW DC9 MM. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999091000211 19990910 00211 WP 1999 9 10 ABXA9900681 1 19990901 A 2120 AIR DIST DOUG DOUG DC8 DC863 302198A WP COCKPIT ODOR A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 812AX 46126 DURING CRUISE, NOTICED LIGHT SMELL COMING FROM BEHIND FLIGHT ENGINEER'S PANEL. SMELLED LIKE BURNING PLASTIC. MAINTENAN CE COULD NOT DUPLICATE. COULD NOT SMELL ANY UNUSUAL ODORS FROM FLIGHT ENGINEER'S PANEL. 2 L 7 4 4F 4A25 1999091000212 19990910 00212 WP 1999 9 10 SCNA99116 1 19990901 A 3350 BULB DOUG DC10 DC1015 3022118 WP ROW 6 FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 154SY 48259 DURING A LINE MAINTENANCE CHECK, AN EMERGENCY TRACK LIGHT BY SEAT ROW 6 WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLAC ED THE LIGHT BULB IN THE EMERGENCY TRACK BY SEAT ROW 6 RIGHT SIDE. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1999091000213 19990910 00213 NM 1999 9 10 DHL99724006 1 19990829 A 3244 49X17 TIRE BOEING 727 727228 NM RT MLG SEPERATED A DHLA O OTHER O OTHER LD LANDING 1 SO 01 724DH 19862 NR 3 MAIN TIRE RECAP CAME OFF ON LANDING DAMAGE TO RT INBD FLAP, AND NR 3 ENGINE. REMOVED AND REPLACED WHEEL AND TIRE, RT INBD FLAP ASSY AND C-1 FAN . 2 L 7 3 4F A3WE 1999091000214 19990910 00214 NM 1999 9 10 VNAA9909001 1 19990902 A 7933 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT OILTEMP LOOSE A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 432JS 3045 AFTER TAKEOFF FROM PIT,THE RIGHT ENGINE OIL TEMPERATURE INDICATION WENT TO 120 DEGREES AND THEN THE DISPLAY WENT BLANK O N THE EICAS DISPLAY. THE AIRCRAFT RETURNED TO THE FIELD AND MAINTENANCE INSPECTED THE RIGHT ENGINE OIL TEMPERATURE SENS OR AND RESECURED CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-32-00. GROUND OPERATIONAL CHECKS WERE COMP LETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999091000215 19990910 00215 NM 1999 9 10 SWAA991459 1 19990902 A 3246 6558256 BEARING BOEING 737 7373Q8 1384670 NM LT MLG FAILED A SWAA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SW 07 670SW 23784 ON DEPARTURE OUT OF BUR, TOWER NOTIFIED ACFT LOST OF NR 1 WHEEL ASSY AND ACFT DIVERTED TO ONT. FOUND NR 1 AXLE NUT STIL L ATTACHED AND TIGHT, THE INNER BEARING STILL ON THE AXLE AND UNDAMAGED. THE OUTER BEARING INNER RACE ON AXLE SEVERELY SCARRED, MUTILATED AND FROZEN IN PLACE. AFTER CLEAN UP OF AREA, FOUND AXLE SLEEVE ROTATED 90 DEGREES BUT STILL FIRMLY I N PLACE. INSPECTION OF INNER AXLE PER MM PROCEDURE FOR WHEEL BEARING FAILURE REVEALED PAINT DISCOLORATION. REMOVED AND REPLACED BOTH NR 1 AND NR 2 TIRE/WHEEL ASSY'S, NR 1 BRAKE ASSY AND MX FERRY ACFT TO PHX FOR AXLE REPAIR. 2 L 7 2 4F RT A16WE 1999091000216 19990910 00216 NE 1999 9 10 SWAA991460 2 19990902 A 7311 692023002 FUEL OIL COOLER BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A SWAA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 305SW 22945 721140 DECLARED EMERGENCY WHEN NR 1 ENG OIL TEMP LIGHT ILLUMINATED WITH ENGINE RETARDED TO IDLE. REMOVED AND REPLACED NR 1 ENG FUEL OIL HEAT EXCHANGER PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999091000217 19990910 00217 NM 1999 9 10 SWAA991461 1 19990901 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 AFT ENTRY EVACUATION SLIDE PRESS GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999091000218 19990910 00218 NM 1999 9 10 SWAA991462 1 19990901 A 3350 07912 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS MISSING LENS AT OVERWING DOOR. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999091000219 19990910 00219 1999 9 10 SWAA991463 4 19990901 A 2565 63551 SLIDE BOEING 737 7377H4 NM AFT ENTRY DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 723SW 27855 DURING SCHEDULED RON, AFT ENTRY EVACUATION SLIDE DEPLOYED ACCIDENTALLY. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999091000220 19990910 00220 NM 1999 9 10 SWAA991464 1 19990901 A 5753 6546430122 SKIN BOEING 737 7373H4 1384600 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C1 CHECK, FOUND RT INBD T/E FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999091000221 19990910 00221 NM 1999 9 10 SWAA991465 1 19990901 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999091000222 19990910 00222 NM 1999 9 10 SWAA991466 1 19990901 A 5523 65C2638423A SKIN BOEING 737 737317 138447P NM LT ELEVATOR TAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND LEFT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 1999091000223 19990910 00223 NM 1999 9 10 SWAA991467 1 19990902 A 5314 65C26493 KEEL BEAM BOEING 737 7373T5 NM BS 610-630 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM STRESS PANEL CORRODED BETWEEN BS 610 TO BS 630. REMOVED AND REPLACED PANEL PER ER 99-6004. 2 L 7 2 4F RT A16WE 1999091000224 19990910 00224 NM 1999 9 10 SWAA991468 1 19990902 A 5314 6545866 KEEL BEAM BOEING 737 7373T5 NM BS 500-727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED ON RT LOWER CHORD. REMOVED AND REPLACED KEEL BEAM RT LOWER CHORD FROM BS 500D TO 727 PER SRM. 2 L 7 2 4F RT A16WE 1999091000225 19990910 00225 NM 1999 9 10 SWAA991469 1 19990902 A 5330 6545890 SKIN BOEING 737 7373T5 NM FUSELAGE. CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUT OUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER ER NR 99-5992. 2 L 7 2 4F RT A16WE 1999091000226 19990910 00226 NM 1999 9 10 SWAA991470 1 19990902 A 5314 6545866 KEEL BEAM BOEING 737 7372T4 1384492 NM BS 727-817 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CORRODED KEEL BEAM, BS 727 TO BS 817 RT SIDE. REMOVED AND REPLACED KEEL BEAM SECTION PE R SRM. 2 L 7 2 4F A16WE 1999091000227 19990910 00227 NM 1999 9 10 SWAA991471 1 19990902 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM UPPER FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING WALK ARROUND INSPECTION, FOUND APPROX A 8 INCH LONG CRACK ON FUSELAGE CROWN 4 FEET FWD OF ANTI COLLITION LIGHT. R EPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999091000228 19990910 00228 NM 1999 9 10 SWAA991472 1 19990902 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM UPPER FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED APPROX BS 500 TO 500A, STRINGER 11R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999091000229 19990910 00229 NM 1999 9 10 SWAA991448 1 19990831 A 5312 6516300 BULKHEAD BOEING 737 737317 138447P NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 8 -RBL 10. REPAIRED BULKHEAD PER SWA RA NR 1-353-2152. 2 L 7 2 4F RT A16WE 1999091000230 19990910 00230 NM 1999 9 10 SWAA991450 1 19990831 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 26R, BS 500D. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999091000231 19990910 00231 NM 1999 9 10 SWAA991449 1 19990830 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 872,500&804 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 25L, BS 827,BS 500B, BS 804. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999091000232 19990910 00232 NM 1999 9 10 SWAA991451 1 19990831 A 3350 07912 COVER BOEING 737 7375H4 138449D NM ROW 10 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 EEPLS COVER MISSING AT ROW 10. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999091000233 19990910 00233 1999 9 10 SWAA991452 4 19990831 A 2565 D31591 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 FWD SERVICE DOOR EVACUATION SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999091000234 19990910 00234 NM 1999 9 10 SWAA991453 1 19990830 A 5320 6937403 ANGLE BOEING 737 7373T5 NM BS 727 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM SUPPORT ANGLE CORRODED, BS 727, LBL 8. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. 2 L 7 2 4F RT A16WE 1999091000235 19990910 00235 NM 1999 9 10 SWAA991454 1 19990830 A 5320 6545866 SPLICE BOEING 737 7373T5 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM INBD TEE SPLICES CRACKED, BS 727, BOTH LT AND RT SIDES. REMOVED AND REPLA CED TEE SPLICES PER SRM. 2 L 7 2 4F RT A16WE 1999091000236 19990910 00236 NM 1999 9 10 SWAA991455 1 19990830 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED 1/2D CHECK, FOUND FWD CABIN EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999091000237 19990910 00237 NM 1999 9 10 SWAA991456 1 19990830 A 5753 6546435236 SKIN BOEING 737 7372H4 138448C NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT OUTBD T/E FLAP DELAMINATED NEAR INBD END. REMOVED AND REPLACED RT WIN G AFT FLAP ASSY PER MM. 2 L 7 2 4F A16WE 1999091000238 19990910 00238 NM 1999 9 10 SWAA991457 1 19990831 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 FUSELAGE SKIN CRACKED 2 INCHES LONG AT APPROX BS, 727A - 727B, STRINGER 11R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999091000239 19990910 00239 NM 1999 9 10 SWAA991458 1 19990901 A 3230 65C16237 CIRCUIT BREAKER BOEING 737 7377H4 NM COCKPIT TRIPPED A SWAA A UNSCHED LANDING P NO WARNING INDICATION TO TAKEOFF 1 SW 07 720WN 27854 AIR TURNBACK, GEAR LEVER WOULD NOT RAISE ON TAKEOFF, RETRACTED FLAPS AND NO TAKEOFF WARNING HORN. FOUND LANDING GEAR LA TCH AND PRESS WARNING CIRCUIT BRAKER TRIPPED. RESET CIRCUIT BRAKER, PERFORMED GEAR HANDLE OPS CHECK, SYSTEM WORKS GOOD PER MM. 2 L 7 2 4F RT A16WE 1999091000240 19990910 00240 NM 1999 9 10 SWAA991432 1 19990828 A 5330 6552988 SKIN BOEING 737 737317 138447P NM BS 907-1106 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT BELLY SKIN, BS 907 TO 1106, STRINGERS 25L-25R. REMOVED AND REPLACED BEL LY SKIN SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999091000241 19990910 00241 NM 1999 9 10 SWAA991433 1 19990828 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 22R, BS 500C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999091000242 19990910 00242 NM 1999 9 10 SWAA991434 1 19990828 A 5315 6546804 FLOORBEAM BOEING 737 737317 138447P NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON BS 727D FLOORBEAM UPPER FLANGE, LBL 17- RBL 3. REPAIRED BEAM PER SWA RA NR 1-A53-2021. 2 L 7 2 4F RT A16WE 1999091000243 19990910 00243 NM 1999 9 10 SWAA991435 1 19990828 A 3350 101114 LENS BOEING 737 7373A4 1384585 NM LT&RT EMER EXIT BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED C2 CHECK, FOUND LT AND RT OVERWING EMERGENCIY EXIT SIGN LENSES BROKEN. REMOVED AND REPLACED BOTH LENSE S PER MM. 2 L 7 2 4F RT A16WE 1999091000244 19990910 00244 NM 1999 9 10 SWAA991436 1 19990828 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 1-4 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 388SW 26591 EEPLS INOP AT ROWS 1-4. RECONNECTED WIRING AND REPLACED LIGHTS AND MOLDING PER MM. 2 L 7 2 4F RT A16WE 1999091000245 19990910 00245 NM 1999 9 10 SWAA991437 1 19990827 A 3350 079123 LENS BOEING 737 737301 1384611 NM ROW 15 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED C4 CHECK, FOUND EEPLS LENS MISSING AT ROW 15. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999091000246 19990910 00246 NM 1999 9 10 SWAA991438 1 19990827 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 4.7. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999091000247 19990910 00247 NM 1999 9 10 SWAA991439 1 19990827 A 5313 6545772 STRINGER BOEING 737 7372T4 1384492 NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE SECTION PE R ER NR 99-5927. 2 L 7 2 4F A16WE 1999091000248 19990910 00248 NM 1999 9 10 SWAA991440 1 19990826 A 5311 6546536 FRAME BOEING 737 7372H4 138448C NM BS 693 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED C3 CHECK, FOUND BELT FRAME CRACKED, BS 693, STRINGER 17R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F A16WE 1999091000249 19990910 00249 NM 1999 9 10 SWAA991441 1 19990828 A 3350 6104781 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DASCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352SW 24888 EEPLS REMAINS ON WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999091000250 19990910 00250 NM 1999 9 10 SWAA991442 1 19990827 A 2910 3810056106 HYD SYS BOEING 737 7373L9 1384470 NM LOWER MID FUSE REQD SERVICE A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 657SW 23331 HYD LOW PRESSURE A-SYSTEM INDICATON, QTY DECREASED TO 1/4 FULL. PREVIOUSLY REMOVED AND REPLACED NR 1 ENG T/R ISOLATION VALVE AND SUSPECT AIR IN SYSTEM. SERVICED HYD A-SYSTEM, ACTUATED FLIGHT CONTROLS AND NR 1 ENG T/R. ALL INDICATIONS CHE CKED GOOD. 2 L 7 2 4F RT A16WE 1999091000251 19990910 00251 NM 1999 9 10 SWAA991443 1 19990827 A 3244 2607825 TIRE BOEING 737 7373H4 1384600 NM NLG WORN A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 07 616SW 27699 ABORTED TAKEOFF, AIRCRAFT VEERED TO THE LEFT DURING TAKEOFF. RUNWAY WAS WET. FOUND NLG TIRES WORN. REMOVED AND REPLAC ED BOTH NLG TIRE/WHEEL ASSY'S. 2 L 7 2 4F RT A16WE 1999091000252 19990910 00252 NM 1999 9 10 SWAA991444 1 19990829 A 2150 BACC10BN550LM COUPLING BOEING 737 7372H4 138448C NM RT ACM LEAKING A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 081SW 22730 ABORTED TAKEOFF, RT WING BODY OVERHEAT LIGHT ILLUMINATED DURING TAKEOFF AT 78 KNOTS. FOUND COUPLING LEAKING AT COMPRESS OR SIDE OF RT AIR CYCLE MACHINE. REMOVED AND REPLACED COUPLING PER MM. 2 L 7 2 4F A16WE 1999091000253 19990910 00253 NM 1999 9 10 SWAA991445 1 19990829 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND 7 EA EEPLS LIGHTS INOP NEAR OVERWING EXIT. RECONNECTED WIRING AND OPS CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999091000254 19990910 00254 NM 1999 9 10 SWAA991446 1 19990829 A 3350 079123 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999091000255 19990910 00255 NM 1999 9 10 SWAA991447 1 19990829 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 515 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 515, STRINGER 12R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999091000256 19990910 00256 WP 1999 9 10 TWAA9912201 1 19990829 A 3350 408822101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 954U 49426 FOUND EMERGENCY CEILING LIGHTS INOPERATIVE AT ROWS 12,15, 17, 19, 21, 23, 24, 26, AND 28. THE EMERGENCY EXIT LIGHTS BY ROW 22 OVER THE WING, AND THE TAIL CONE EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERIES AT STA TIONS 170, 480, 580, 880, 1050, AND 1350. CHECK-C 8-9-99 MCI. 2 L 7 2 4F A6WE 1999091000257 19990910 00257 WP 1999 9 10 TWAA9912202 1 19990903 A 3350 3350002621 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 920TW 49369 THE EGRESS LIGHT STRIP IN REAR OF CABIN WAS ON AND WOULD NOT RESET. REPLACED THE BATTERY PACK. CHECK-C 6-22-99 STL. 2 L 7 2 4F A6WE 1999091000258 19990910 00258 WP 1999 9 10 TWAA9912203 1 19990903 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 617 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 984Z 47412 LONGERON 9L HAD A .25 INCH CRACK ON UPPER FLANGE AT ATTACHMENT TO FUSELAGE FRAME AT STA 617. SPLICED IN NEW LONGERON PE R SRM 53-02, FIG 18. CHECK-C 3-15-99 STL. 2 L 7 2 4F A6WE 1999091000259 19990910 00259 WP 1999 9 10 TWAA9912204 1 19990903 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 984Z 47412 FOUND .5 INCH CRACK IN LONGERON 6R AT STA 756. REPLACED LONGERON SECTION AND SPLICED AS PER SRM 53-02, FIG 18. CHECK-C 3-15-99 STL. 2 L 7 2 4F A6WE 1999091000260 19990910 00260 NM 1999 9 10 HNAA9900118 1 19990907 A 5610 8SC0519009 WINDOW DHAV DHC8 DHC8201 2809001 NM LT COCKPIT CRACKED A HNAA K NONE D INFLIGHT SEPARATION CR CRUISE 1 EA 07 995HA 6964 460 CAPTAIN'S SIDE WINDOW CRACKED IN FLIGHT AND APPROX REAR THIRD OF OUTER LAMINATE SEPARATED FROM A/C. REMOVED AND REPLACE D CAPTAIN'S SIDE WINDOW, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1999091000261 19990910 00261 WP 1999 9 10 CALA9901128 1 19990906 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQD SERVICE A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 16802 49222 THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS RE TURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR STRUT REQUIRED SERVICING. A FULL NOSE STRUT SERVICING WAS PERFORMED IAW MM 32-21-02. A NLG SWING WAS PERFORMED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999091000262 19990910 00262 NM 1999 9 10 CALA9901129 1 19990905 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND STRINGER 29R CORRODED AT STA 1016. THE AREA WAS REPAIRED BY INSTALLING A FORMED CHANNEL SECTION WITH F ASTENERS IAW SRM 51-70-11, FIGURE 1. 2 L 7 2 4F RT A16WE 1999091000263 19990910 00263 NM 1999 9 10 CALA9901130 1 19990905 A 5220 CASTING BOEING 727 727224 1384076 NM RT EMER EXIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A 1 INCH CRACK IN RT FORWARD OVERWING DOOR INNER UPPER CASTING. THE CASTING WAS REMOVED AND A NEW CAST ING WAS INSTALLED IAW SRM 51-30-2, FIGURE 1. 2 L 7 3 4F A3WE 1999091000264 19990910 00264 NM 1999 9 10 CALA9901131 1 19990905 A 5312 BULKHEAD WEB BOEING 737 7373T0 1384582 NM BS 1016 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 23365 INSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD WEB CRACKED IN FOUR PLACES AT FASTENER HOLES AT STA 1016, STRINGE R 6L-7L. ALSO, SEVERAL ELONGATED HOLES WERE FOUND. REPAIRED IAW ECRA 5310-03917. 2 L 7 2 4F RT A16WE 1999091000265 19990910 00265 WP 1999 9 10 CALA9901132 1 19990905 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND STIFFENER CORRODED IN AFT CARGO COMPARTMENT AT STA 2007. REPAIRED IAW ECRA 531-01069. 2 L 7 3 4F A22WE 1999091000266 19990910 00266 NM 1999 9 10 CALA9901133 1 19990906 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 328-344. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 53-00-52, FIGU RE 202. 2 L 7 2 4F RT A16WE 1999091000267 19990910 00267 EA 1999 9 10 COMA9960482 1 19990904 A 4920 38465803 HOUSING CNDAIR CL600 CL6002B19 EA APU TURBINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 6797 1374 7204 AFTER APU REMOVAL FOR MAINTENANCE FOUND TURBINE HOUSING CRACKED NEAR FUEL NOZZLE BOSSES. RETURNED TO ALLIED SIGNAL FOR REPAIR AND -3 MOD. 2 L 7 2 4F RT A21EA 1999091000268 19990910 00268 EA 1999 9 10 COMA9960483 1 19990901 A 4920 38465803 HOUSING CNDAIR CL600 CL6002B19 EA APU TURBINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 8601 7134 AFTER REMOVAL OF APU FOR MAINTENANCE FOUND TURBINE HOUSING CRACKED NEAR FUEL NOZZLE BOSSES. RETURNED TO ALLIED SIGNAL F OR REPAIR AND -3 MODIFICATION. 2 L 7 2 4F RT A21EA 1999091000269 19990910 00269 NE 1999 9 10 COMA9960484 2 19990904 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FAILED A COMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 991CA 7316 807495 LEFT ENGINE ITT 880 DEGREES, VIB 4.0 IFSD. REPLACED LEFT HAND ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999091000270 19990910 00270 NE 1999 9 10 COMA9960485 2 19990902 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 947CA 7077 807255 THICK OILY SMOKE IN COCKPIT FROM THE AIRCRAFT SYSTEM. REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999091000271 19990910 00271 EA 1999 9 10 COMA9960486 1 19990906 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA RICHT BIRD STRIKE A COMA K NONE C F.O.D. UK UNKNOWN 1 SO 01 938CA 7046 BIRD STRIKE RIGHT HAND SIDE OF NOSE. C/W BIRD STRIKE INSPECTION. NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 1999091000272 19990910 00272 EA 1999 9 10 COMA9960487 1 19990901 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 969CA 7141 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. INSPECTED DOOR, NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999091000273 19990910 00273 EA 1999 9 10 COMA9960488 1 19990901 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA ROW 8 LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 932CA 7038 FLOOR EMERGENCY LIGHT IS INOPERABLE AT ROW 8. SECURED LOOSE WIRING CONNECTION. SYSTEM CHECK OK. 2 L 7 2 4F RT A21EA 1999091000274 19990910 00274 EA 1999 9 10 COMA9960489 1 19990902 A 5210 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 963CA 7127 CABIN DOOR OUTER HANDLE MESSAGE. INSPECTED DOOR, NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999091000275 19990910 00275 EA 1999 9 10 COMA9960490 1 19990902 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA SERVICE DOOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951CA 7091 EMERGENCY LIGHT AT SERVICE DOOR IS INOPERABLE. REPLACED BULB. 2 L 7 2 4F RT A21EA 1999091000276 19990910 00276 EA 1999 9 10 COMA9960491 1 19990906 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 946CA 7072 CABIN DOOR LATCH MESSAGE ON EICAS. DEFERRED DOOR WARNING SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 1999091000277 19990910 00277 EA 1999 9 10 COMA9960492 1 19990904 A 2751 WARNING CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 973CA 7146 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999091000278 19990910 00278 NM 1999 9 10 UPS99230561 1 19990901 A 2761 ACTUATOR BOEING 727 72725C 138400H NM FLIGHT SPOILERS FAILED A IPXA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 01 947UP 19722 INSPECTION TYPE:N/A, ON HIGH SPEED CLIMB PROFILE 340 FLTS A/C REQUIRED 10 DEG RIGHT AILERON INPUT. A/C TRIMMED IAW AOM PROCEDURE. LEFT RUDDER TRIM 1/4 TURN AILERON TRIM 1/2 TURN. A/C LANDED FLAPS 30 AT 140 KNOTS WITH 20 DEG RIGHT AILERON REQUIRED TO KEEP WINGS LEVEL. EMERGENCY DECLARED DUE TO INCREASED LANDING SPEED. *S/D* REMOVED AND REPLACED NR 1, 2 AND 3 FLIGHT SPOILER ACT PER MM 27 -61-81, PERFORMED LEAK CHECK AND ADJUSTED ALL CHECKS GOOD. 2 L 7 3 4F A3WE 1999091000279 19990910 00279 NM 1999 9 10 UPS99230568 1 19990904 A 5230 CARGO DOOR BOEING 727 72725C 138400H NM MAIN CARGO CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE:N/A, MAIN CARGO DOOR UPPER AFT STRUCTURE/STRAP HAS CORROSION. 2 L 7 3 4F A3WE 1999091000280 19990910 00280 NM 1999 9 10 UPS99230571 1 19990902 A 5310 INTERCOSTAL BOEING 727 72731C 1384011 NM BS 380 - 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C, INTERCOSTAL CRACKED LT SIDE OF E & E BAY BETWEEN BS 380 - 400 LEVEL WITH FLOOR. REPLACED INTERCOSTAL IAW SRM 51-20-01 FIG 7. 2 L 7 3 4F A3WE 1999091000281 19990910 00281 NM 1999 9 10 UPS99230572 1 19990904 A 5753 SKIN BOEING 727 72727C 138400J NM RT TE FOREFLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:N/A, RIGHT I/B FORE FLAP SKIN PEELED BACK AND CRACKED L/E NEXT TO SPRING DOOR. *S/D* REMOVED NAD REPLA CED RIGHT FOREFLAP PER MM 27-51-05. (P/N 65-21 630-92) ON, (P/N 65-21630-174) OFF, (S/N BN119) ON, (S/N 126) OFF. 2 L 7 3 4F A3WE 1999091000282 19990910 00282 NM 1999 9 10 UPS99230574 1 19990831 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1330 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C, SUSPECT CORROSION ON SKIN BS 1330 S9 LT. DAMAGE REPAIRED IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1999091000283 19990910 00283 NM 1999 9 10 UPS99230575 1 19990906 A 3350 BATTERY BOEING 727 72751C 1384015 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS GREW DIM. REPLACED BATTERIES IN BOTH EMERGENCY EXIT LIGHTS. 2 L 7 3 4F A3WE 1999091000284 19990910 00284 NM 1999 9 10 UPS99530577 1 19990831 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 INSPECTION TYPE:C, AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CRACKED BS 1475 RT. REMOVED DAMAGED SECTION, FABRICATED REPA IR PARTS AND INSTALLED. 2 L 7 2 4F RT A2NM 1999091000285 19990910 00285 NM 1999 9 10 UPS99530578 1 19990831 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 INSPECTION TYPE:C, FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT CRACKED. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AN D INSTALLED. 2 L 7 2 4F RT A2NM 1999091000286 19990910 00286 WP 1999 9 10 UPS99830562 1 19990728 A 5312 RIB DOUG DC8 DC873F 302199F WP WS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, RIB CRACKED AT FASTENER AND FASTENER WORKING UNDER RT FWD FILLET PANEL STA 822 X-55. FABRICATED DOU BLER, STOP DRILLED CRACK, INSTALLED DOUBLER. ALL WORK ACCOMPLISHED IAW DC8 SRM 53-8-3, 51-9-0, 53-2-0, 51-1-8 & 53-2-0 . 2 L 7 4 4F RT 4A25 1999091000287 19990910 00287 WP 1999 9 10 UPS99830564 1 19990727 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3, RT FWD PIT STA 260 FROM LONG 34R TO 35L FRAME IS CORRODED. REMOVED GILLINER SUPPORT L/R SIDE AT LS 260, FOUND FRAME SECTION OUT OF LIMITS. REMOVED INTERCOSTAL, DRILLED NEW FRAME SEGMENT A/C IAW DC8 SRM 51-3-2. FABBED AND INSTALLED FRAME SEGMENT, SKIN CHIP, SPLICES INTERCOSTAL AND GILLINER SUPPORT IAW DC8 SRM 51-1-20D, 51-1-21, 53-2- 0 & 51-3-2. 2 L 7 4 4F RT 4A25 1999091000288 19990910 00288 WP 1999 9 10 UPS99830569 1 19990905 A 2160 SWITCH DOUG DC8 DC873F 302199F WP LT PAC INOP A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 808UP 46008 INSPECTION TYPE:N/A, ATB-LOUD HOWLING NOISE IN THE COCKPIT COMING FROM THE NOSE AREA IMPEDING COMMUNICATIONS. FOUND LEF T FAN INLET DOOR REMAINS OPEN IN FLIGHT. REPAIRED GROUND AT S3-8012. ALSO, REMOVED AND REPLACED R2-25, DOOR NOW CLOSES WITH GROUND TO FLIGHT SHIFT. 2 L 7 4 4F RT 4A25 1999091000289 19990910 00289 WP 1999 9 10 UPS99830570 1 19990907 A 5720 FLAPWELL DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A, RT WING FLAPWELL DAMAGED BY FLAP ACT LINK FAILURE. *S/D* REF DMI D178387 INTERIM REPAIR TO RT WIN G AUX SPAR. TRANSFERRED TO NRC 626624 C/W REPAIR PER EO DC8-5720-11513-A. OK FOR A ONE TIME FLIGHT TO DHC FOR PERMANEN T REPAIR. 2 L 7 4 4F RT 4A25 1999091000290 19990910 00290 WP 1999 9 10 UPS99830576 1 19990904 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A, DURING BISE CHECK THE EMERGENCY EXIT LIGHT DO NOT ILLUMINATE. REMOVED AND REPLACED EMER EXIT LIGHT S BATTERY, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999091000291 19990910 00291 NM 1999 9 10 SCNA99117 1 19990905 A 3350 900542 BATTERY PACK BOEING 727 727227 1384078 NM R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT ABOVE THE R2 DOOR WAS FOUND TO BE DIM. REMOVED AND REPLACED THE BA TTERY PACK IAW MM 345001. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999091000292 19990910 00292 WP 1999 9 10 RRXA991377 1 19990831 A 2720 16000G9 VALVE DOUG DC8 DC862 3021970 WP RUDDER MALFUNCTIONED A RRXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 15 993CF 46028 AFTER TAKEOFF, DURING RIGHT TURN AIRCRAFT HAD STUDDERING, TURNING OUT OF TURN SAME BUFFETING EFFECT IN AIRFRAME. DID NO T FEEL IN YOKE, NO VISIBLE ENGINE INDICATIONS OF MALFUNCTION. NO LEFT TURNS MADE). FOUND RUDDER PRESSURE REDUCER VALVE BYPASSING. REMOVED AND REPLACED RUDDER PRESSURE REDUCER VALVE, LEAK AND OPS CHECK GOOD ON GROUND. 2 L 7 4 4F 4A25 1999091000293 19990910 00293 WP 1999 9 10 RRXA991378 1 19990824 A 2913 6500101 PUMP DOUG DC8 DC871 302199A WP NR 3 ENGINE FAILED A RRXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 15 811AL 46099 HYD OIL TEMP CAME ON WITH TEMP APPROX 80 DEG TURNED LT PUMP OFF, RT PUMP FLUCTUATED PLUS/MINUS 200 PSI TURNED LT ON, RT OFF, TEMP WENT NORM BUT LT PUMP PRESS REACHED 3500 PSI SHUT BOTH OFF FOR FLT. ON APPROACH, ATTEMPTED TO TURN BOTH PUMPS ON, NO PRESS FROM EITHER ENG PUMP HYD QTY NORMAL AT ALL TIMES. FOUND NR 3 ENG HYD PUMP FAILED. REMOVED AND REPLACE D BOTH LEFT AND RIGHT ENG DRIVEN PUMPS. REMOVED AND REPLACED CASE DRAIN FILTERS, DAUL FILTERS, AUX PUMP FILTERS AND MAI N RES FILTER, DRAINED HYD SYSTEM AND RESERVICED. AFTER INITIAL RUN UP 7 SYSTEM CKS, CHANGED ALL FILTERS AGAIN, FILTERS FOUND TO BE CLEAN. 2 L 7 4 4F 4A25 1999091000294 19990910 00294 NM 1999 9 10 USAA990205 1 19990331 A 5320 ANGLE BOEING 757 757225 1384959 NM BS 1400 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE SUPPORT ANGLE STATION 1400 RBL 16-20, CORROSI ON TASK NR C53-155-02. REPLACED SUPPORT ANGLE PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000295 19990910 00295 NM 1999 9 10 USAA990204 1 19990331 A 5320 SHEAR TIE BOEING 757 757225 1384959 NM BS 1320 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF SHEAR TIE STATION 1320 BETWEEN STRINGER 28 R AND 29R, CORROSION TASK NR C53-155-02. REPLACED SHEAR TIE PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000296 19990910 00296 NM 1999 9 10 USAA990207 1 19990331 A 5320 SHEAR TIE BOEING 757 757225 1384959 NM BS 1300 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF SHEAR TIE STATION 1300 BETWEEN STRINGER 28 R AND 29R, CORROSION NR C53-155-02. REPLACED SHEAR TIE PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000297 19990910 00297 NM 1999 9 10 USAA990235 1 19990331 A 5320 ANGLE BOEING 757 757225 1384959 NM BS 1280 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH AREA OF CORROSION STATION 1280 BETWEEN STRINGER 27R AND 28R ANGLE. FABRICATED ANGLE PER REPAIR DOCUMENT 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000298 19990910 00298 NM 1999 9 10 USAA990263 1 19990331 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 345-365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT INERCOSTAL RBL 46 STATION 345 TO STATION 365. INSTALLED NE W INTERCOSTAL PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000299 19990910 00299 NM 1999 9 10 USAA990206 1 19990331 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 410 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL AT STATION 410 TO STATION 365, RBL 46. INSTALLED NEW INTERCOSTAL PER SRM 61-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000300 19990910 00300 NM 1999 9 10 USAA990241 1 19990331 A 5320 BAC1520792 INTERCOSTAL BOEING 757 757225 1384959 NM BS 410 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL RBL 25 STATION 410 TO STATION 365. REPLACED SEAT TRACK PER SRM 51-10-00 AND 53-10-52. (M) 2 L 7 2 4F RT A2NM 1999091000301 19990910 00301 NM 1999 9 10 USAA990185 1 19990331 A 5320 141N5160U102 INTERCOSTAL BOEING 757 757225 1384959 NM BS 334 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORRSION INTERCOSTAL RBL 25 TO RBL 39, STATION 334. REMOVED AND REPLACE D INTERCOSTAL PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000302 19990910 00302 NM 1999 9 10 USAA990236 1 19990331 A 5320 CC1148414 INTERCOSTAL BOEING 757 757225 1384959 NM BS 324-418 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AREA INTERCOSTAL BS 0 STATION 324 TO STATION 418. REPLACED IN TERCOSTAL PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000303 19990910 00303 NM 1999 9 10 USAA990231 1 19990331 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL RBL 62 STATION 324 TO STATION 345. REPAIRED INTER COSTAL PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000304 19990910 00304 NM 1999 9 10 USAA990215 1 19990331 A 5320 1142576 INTERCOSTAL BOEING 757 757225 1384959 NM BS 310-324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 606AU 45836 22202 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 1 INCH INTERCOSTAL LBL 22 BETWEEN STATION 310 AND 324. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091000305 19990910 00305 NM 1999 9 10 USAA990773 1 19990728 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK, FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM T-CAP AT STATION 947 BETWEEN LBL 14 TO RBL 16, COR ROSION LEVEL 2. CORROSION TASK NR C53-107-02. SPLICED T-CAP SECTION/DOUBLERS PER SRM 53-00-51 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999091000306 19990910 00306 NM 1999 9 10 USAA990776 1 19990728 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 397 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK, FOUND 1 INCH CRACK AT STATION 397 B/O 0 INTERCOSTAL UPPER CHORD. REPLACED WITH IDENTICAL PART N UMBER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999091000307 19990910 00307 NM 1999 9 10 USAA990775 1 19990728 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK, FOUND .25 INCH CRACK AT 178 BULKHEAD AFT SIDE RBL 2, 4 INCHES UP FROM BASE OF BULKHEAD. DOUBLER REPAIR PER SRM 53-10-008 FIG 203. (M) 2 L 7 2 4F RT A16WE 1999091000308 19990910 00308 NM 1999 9 10 USAA990774 1 19990728 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 320-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK, FOUND CORROSION ENTIRE UPPER SURFACE OF FORWARD ENTRY DOOR Z-ANGLE STATION 320-344. DEFECTIVE P ART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999091000309 19990910 00309 NM 1999 9 10 USAA990748 1 19990728 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 907 LEFT SIDE STRINGER 8-9 IN FRAME. REPAIRE D DOUBLER PER EA 65076. (M) 2 L 7 2 4F RT A16WE 1999091000310 19990910 00310 NM 1999 9 10 USAA990747 1 19990728 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 727B BETWEEN STRINGER 9L AND STRINGER 8L FRAM E. REPAIRED DOUBLER PER EA 65076. (M) 2 L 7 2 4F RT A16WE 1999091000311 19990910 00311 NM 1999 9 10 USAA990746 1 19990728 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 291 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 291 MINUS 2, 4 INCH BELOW STRINGER 12R AT OUT BOARD FLANGE SHEAR WEB ANGLE. REPAIRED PER SRM 53-10-02. (M) 2 L 7 2 4F RT A16WE 1999091000312 19990910 00312 NM 1999 9 10 USAA990745 1 19990728 A 5320 654580734 ANGLE BOEING 737 737401 1384701 NM BS 291.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 291.5, 4 INCHES ABOVE STRINGER 10R ANGLE. REPAIRE D PER BOEING 737-400 SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999091000313 19990910 00313 NM 1999 9 10 USAA990730 1 19990728 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FRAME AT STATION 867 LEFT BETWEEN STRINGER 8/9. REPAI RED DOUBLER PER EA 65076. (M) 2 L 7 2 4F RT A16WE 1999091000314 19990910 00314 NM 1999 9 10 USAA990777 1 19990728 A 5320 ANGLE BOEING 737 737401 1384701 NM STATION 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK, FOUND CRACK AT STATION 294.5 JUST AHEAD OF Z-ANGLE AT RT ENTRY. REPLACED ANGLE PER SRM 51-10-02 . (M) 2 L 7 2 4F RT A16WE 1999091000315 19990910 00315 NM 1999 9 10 USAA990778 1 19990728 A 5230 SKIN BOEING 737 737401 1384701 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK, FOUND .25 INCH SKIN CRACK IN AFT CARGO DOOR HANDLE FLAP CUT OUT. INSTALLED DOUBLER PER SRM 52-0 0-01. (M) 2 L 7 2 4F RT A16WE 1999091000316 19990910 00316 WP 1999 9 10 USAA990794 1 19990722 A 5730 SKIN DOUG DC9 DC981 3022081 WP WS 343 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 806US 48365 48038 PIT - DURING Q5/C2 CHECK, FOUND 2.375 INCH CRACK AT LOWER LEFT WING FIXED LEADING EDGE XFS 343. INSTALLED DOUBLERS PER EA 52330. (M) 2 L 7 2 4F A6WE 1999091000317 19990910 00317 NM 1999 9 10 USAA990308 1 19990413 A 5320 ANGLE BOEING 767 7672B7 1385107 NM BS 1087 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 655US 34884 25257 CLT - DURING VISUAL CHECK INSPECTION, FOUND A 1 INCH CRACK AT BS 1087 RBL 25 ANGLE SUPPORT. FABRICATED NEW ANGLE PR BOE ING DRAWING 140T0130. (M) 2 L 7 2 4F RT A1NM 1999091000318 19990910 00318 NM 1999 9 10 USAA990307 1 19990413 A 5320 ANGLE BOEING 767 7672B7 1385107 NM BS 1087 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 655US 34884 25257 CLT - DURING VISUAL CHECK INSPECTION, FOUND A 1 INCH CRACK AT BS 1087 LBL 25 ANGLE SUPPORT. FABRICATED NEW ANGLE PER BO EING DRAWING 140T0130. (M) 2 L 7 2 4F RT A1NM 1999091000319 19990910 00319 NE 1999 9 10 USAABB9033A 2 19990706 A 7530 14J981 HP 2 DUCT BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LEAKING A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 608AU 13145 22204 30534 PHL - FLT 1854 - ON CLIMB-OUT FROM PHL, AT APPROX FL180, CREW RECEIVED THE E/M 'LT ENG OVHT' AND ASSOCIATED LIGHT. CREW REDUCED THRUST ON THE ENGINE. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE HP 2 AND HP6 DUCTS FOR LEAKING. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1999091000320 19990910 00320 NE 1999 9 10 USAABB9033B 2 19990706 A 7530 16J081 HP 6 DUCT BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LEAKING A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 608AU 13145 22204 30534 PHL - FLT 1854 - ON CLIMB-OUT FROM PHL, AT APPROX FL180, CREW RECEIVED THE E/M 'L ENG OVHT' AND ASSOCIATED LIGHT. CREW REDUCED THRUST ON THE ENGINE. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE HP2 AND HP6 DUCTS FOR LEAKING. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1999091000321 19990910 00321 NM 1999 9 10 USAA079903 1 19990729 A 2751 BACC45FT18A14S CONNECTOR BOEING 727 727227 1384078 NM TE FLAPS CONTAMINATED A USAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 EA 19 926TS 20774 FLT 6421 - LGA-DCA - DURING APPROACH TO DCA SELECTING FLAPS 2 DEGREES GAVE NORMAL LEADING EDGE DEVICES, 2 DEGREES OUTBOA RD FLAPS AND 0 DEGREES INBOARD FLAPS. AT 15 DEGREES AND HIGHER INBOARD FLAPS CAME DOWN NORMALLY AND FOLLOWED FLAPS SELE CTED ALL THE WAY TO FLAPS 40 DEGREES, LANDED WITH FLAPS AT 40 DEGREES. INBOARD FLAPS UP VERIFIED VISUALLY, COMPLIED WIT H AOM PROCEDURES. PERFORMED TROUBLESHOOTING PER BOEING MM REF 27-51-0, PAGE 102. FOUND CONTAMINATION OF INBOARD FLAP P OSITION INDICATOR CONNECTOR. CLEANED CONNECTOR OPERATIONAL CHECK NORMAL PER MM. (M) 2 L 7 3 4F A3WE 1999091000322 19990910 00322 WP 1999 9 10 USAAD99104 1 19990727 A 3350 41B001TD05G1 BATTERY DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 938VJ 48119 IND - THE RIGHT NACELLE SCAN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE SCAN EMERGENCY LIG HT BATTERY. (M) 2 L 7 2 4F A6WE 1999091000323 19990910 00323 WP 1999 9 10 USAAD99105 1 19990727 A 3350 41B001TD05G1 BATTERY DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 960VJ 47505 DTW - THE LEFT NACELLE SCAN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE SCAN EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999091000324 19990910 00324 WP 1999 9 10 USAAD99101 1 19990724 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 982VJ 48158 IND - THE AFT OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT OVERWING EMERGENCY EXIT LIG HT BATTERIES. (M) 2 L 7 2 4F A6WE 1999091000325 19990910 00325 WP 1999 9 10 USAAD99102 1 19990726 A 3350 201312ALP BATTERY DOUG DC9 DC931 3022065 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918VJ 48138 IND - ONE SECTION OF THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGH T BATTERY. (M) 2 L 7 2 4F A6WE 1999091000326 19990910 00326 WP 1999 9 10 USAAD99103 1 19990726 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925VJ 48145 ROC - THE OVERHEAD AISLE EMERGENCY LIGHTS AT ROWS 10 THROUGH 14 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FO R THE OVERHEAD AISLE EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999091000327 19990910 00327 WP 1999 9 10 USAAD99106 1 19990729 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 936VJ 48116 IND - THE FORWARD CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD CABIN OVERHEAD EME RGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999091000328 19990910 00328 WP 1999 9 10 USAAD99107 1 19990730 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 806US 48038 PHL - THE TAIL AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE TAIL AREA EMERGENCY LIG HTS. (M) 2 L 7 2 4F A6WE 1999091000329 19990910 00329 NM 1999 9 10 TSAA9957315 1 19990617 A 5711 6555511 SPAR WEB BOEING 737 7372Q9 138448M NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 RT WING FRONT SPAR WEB CORROSION FROM FSS 425 - 433. REPAIRED PER ECO 2970. (M) 2 L 7 2 4F A16WE 1999091000330 19990910 00330 NM 1999 9 10 TSAA9951311 1 19990617 A 5511 65499256 SPAR BOEING 737 7372Q9 138448M NM HORIZ STAB CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 HORIZONTAL STAB CENTER SECTION REAR SPAR UPPER CHORD RIGHT FORWARD ATTACH LUG CRACKED. ACCOMPLISHED BY BOEING AOG TEAM PER 6-1171-TA1224R1. (M) 2 L 7 2 4F A16WE 1999091000331 19990910 00331 NM 1999 9 10 TSAA9951310 1 19990617 A 5343 693786762 BUSHINGS BOEING 737 7372Q9 138448M NM RT MLG CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 RIGHT MAIN LANDING GEAR SUPPORT BEAM FITTING (TOP) CORROSION NOTED IN FITTING AT BS 706 RT. COMPLETED IAW ECO 2966. (M ) 2 L 7 2 4F A16WE 1999091000332 19990910 00332 NM 1999 9 10 TSAA9933385 1 19990808 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM PAX CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED NR 4 FLOOR EMERGENCY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091000333 19990910 00333 NM 1999 9 10 TSAA9933384 1 19990806 A 3350 6012311 BATTERY PACK BOEING 737 737230 NM EMER EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED RIGHT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1999091000334 19990910 00334 NM 1999 9 10 TSAA9933383 1 19990806 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED BATTERY PACK IN NR 3 POSITION FLOOR PROX LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 1999091000335 19990910 00335 NM 1999 9 10 TSAA9933382 1 19990806 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED NR 6 FLOOR EMERGENCY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091000336 19990910 00336 NM 1999 9 10 TSAA9933380 1 19990805 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 2 EMERGENCY FLOOR PROX LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999091000337 19990910 00337 NM 1999 9 10 TSAA9933381 1 19990805 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091000338 19990910 00338 NM 1999 9 10 TSAA9933357 1 19990718 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 3 PROXIMITY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091000339 19990910 00339 NM 1999 9 10 TSAA9933358 1 19990718 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED NR 2 FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1999091000340 19990910 00340 NM 1999 9 10 TSAA9933360 1 19990725 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091000341 19990910 00341 NM 1999 9 10 TSAA9933361 1 19990723 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1999091000342 19990910 00342 NM 1999 9 10 TSAA9933362 1 19990725 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 4 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1999091000343 19990910 00343 NM 1999 9 10 TSAA9933386 1 19990810 A 3350 6012311 BATTERY PACK BOEING 737 737230 NM EMER EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED RIGHT OVERWING SLIDE LIGHT BATTERY POWER SUPPLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1999091000344 19990910 00344 NM 1999 9 10 TSAA9933370 1 19990729 A 3350 86210066 BATTERY BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY PACKS FOR NR 3, NR 4, AND NR 6 FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 1999091000345 19990910 00345 NM 1999 9 10 TSAA9933371 1 19990729 A 3350 1102833 LIGHT ASSY BOEING 737 7372M6C 1384708 NM EMER EXIT INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT ASSY DUE INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999091000346 19990910 00346 NM 1999 9 10 TSAA9933367 1 19990730 A 3350 900542 BATTERY BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY PACKS FOR FORWARD AISLE EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1999091000347 19990910 00347 NM 1999 9 10 TSAA9933368 1 19990731 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 5 EMERGENCY FLOOR BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1999091000348 19990910 00348 NM 1999 9 10 TSAA9933369 1 19990801 A 3350 1000679 LIGHT BOEING 737 7372Q9 138448M NM COCKPIT INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A16WE 1999091000349 19990910 00349 NM 1999 9 10 TSAA9933372 1 19990727 A 3350 8731002511 LIGHT BOEING 737 737230 NM EMER EXIT INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED AFT SERVICE DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999091000350 19990910 00350 NM 1999 9 10 TSAA9933373 1 19990727 A 3350 9221009 BATTERY PACK BOEING 737 737230 NM EMER EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED BATTERY PACK FOR AFT SERVICE DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091000351 19990910 00351 NM 1999 9 10 TSAA9933374 1 19990727 A 3350 6012311 BATTERY PACK BOEING 737 737230 NM EMER EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED BATTERY PACK FOR RIGHT OVERWING EMERGENCY SLIDE LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091000352 19990910 00352 NM 1999 9 10 USAA990626 1 19990628 A 5240 6545871523 SKIN BOEING 737 7372B7 1384560 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 43587 22888 TPA - DURING CX-3 VISUAL INSPECTION, FOUND TWO CRACKS, ONE CRACK .125 INCH AND ONE CRACK .25 INCH LOWER HINGE CUTOUT AT FORWARD SERVICE DOOR SKIN. INSTALLED FILLER, DOUBLER AND FASTENERS PER TR 52-10-01A. (M) 2 L 7 2 4F A16WE 1999091000353 19990910 00353 NM 1999 9 10 USAA990625 1 19990627 A 5330 SKIN BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AU 44698 22795 TPA - DURING A RON, VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 380 BETWEEN STRINGER 28L AND 28R AFT EQUIP COOLI NG ACCESS ON SKIN. INSTALLED DOUBLER PER TR 53-30-04/SB 737-53-1117/SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1999091000354 19990910 00354 NM 1999 9 10 USAA990662 1 19990630 A 5330 SKIN BOEING 737 737201 1384454 NM BS 978-980 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 22273 CLT - DURING A PILOTS REPORT VISUAL INSPECTION CHECK, FOUND A 2. 5 FT CRACK JUST BELOW STRINGER 21L FROM STATION 978 TO 980 IN FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-03 FIG 6 AND EA 65015. (M) 2 L 7 2 4F A16WE 1999091000355 19990910 00355 NM 1999 9 10 USAA990665 1 19990627 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 884 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 231US 51384 21976 PHL - DURING RON, FOUND 2.5 INCH CRACK IN SKIN AT STATION 884 AT STRINGER 24 RT. INSTALLED DOUBLER REPAIR AT STRINGER A REA PER SRM 53-30-3, FIG 1 SHT 4. (M) 2 L 7 2 4F A16WE 1999091000356 19990910 00356 NM 1999 9 10 USAA990673 1 19990710 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 54594 21667 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN SKIN AT STATION 727B AND STRINGER 18L, SKIN. INSTALL ED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999091000357 19990910 00357 NM 1999 9 10 USAA990735 1 19990717 A 5330 SKIN BOEING 737 737201 1384454 NM BS 747/767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 48992 22352 PIT - DURING RON CHECK, FOUND A .75 INCH CRACK AT STATION 747 STRINGER 18 RT AND A .75 INCH LONG CRACK AT STATION 767 ST RINGER 19 RT ON SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999091000358 19990910 00358 NM 1999 9 10 USAA990736 1 19990717 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 48992 22352 PIT - DURING RON CHECK, FOUND .5 INCH LONG CRACK AT STATION 727A STRINGER 18 RT ON SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999091000359 19990910 00359 NM 1999 9 10 USAA990744 1 19990724 A 5320 SKIN BOEING 737 737201 1384454 NM BS 420 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 55016 21665 PIT - DURING RON MAINTENANCE, FOUND 5 INCH LONG CRACK AT STATION 420, BODY LINE 0, CENTER LINE UNDERSIDE ON FUSELAGE SKI N. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 1 (SHEET 4). (M) 2 L 7 2 4F A16WE 1999091000360 19990910 00360 NM 1999 9 10 USAA990663 1 19990703 A 5347 BAC1520792 SEAT TRACK BOEING 737 737201 1384454 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 54594 21667 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND MINOR CORROSION AT FORWARD END OF LEFT SEAT TRACK INBOARD AND OUTBOARD, CORROSION LEVEL 1. SPLICED IN AND FABRICATED REPAIR PARTS PER SRM 53-10-5 FIG 2. (M) 2 L 7 2 4F A16WE 1999091000361 19990910 00361 NM 1999 9 10 USAA990664 1 19990702 A 5330 SKIN BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 42705 22868 CLT - DURING RON CHECK VISUAL INSPECTION, FOUND A 75 INCH CRACK AFT SIDE OF EQUIPMENT COOLING EXHAUST AT STATION 380 BET WEEN BL 0 AND STRINGER 28L FUSELAGE SKIN. REPAIRED PER TR 53-30-04. (M) 2 L 7 2 4F A16WE 1999091000362 19990910 00362 NM 1999 9 10 USAA990704 1 19990706 A 5320 654581945 ANGLE BOEING 737 737201 1384454 NM NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 44417 22797 CLT - DURING A RON VISUAL INSPECTION, FOUND A 3 INCH CRACK AT NOSE GEAR GUSSET ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-6. (M) 2 L 7 2 4F A16WE 1999091000363 19990910 00363 NM 1999 9 10 USAA990732 1 19990718 A 5320 69353520 TIE CLIP BOEING 737 737201 1384454 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 50992 22018 CLT - DURING C-CHECK, FOUND .25 INCH CRACK IN TIE CLIP AT STATION 480 STRINGER 24L (TOP LEFT CORNER). REPLACED TIE CLIP PER SRM 51-40-02. (M) 2 L 7 2 4F A16WE 1999091000364 19990910 00364 NM 1999 9 10 USAA990731 1 19990717 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 45144 22885 TPA - DURING RON, FOUND 8 SQUARE INCH OF CORROSION ON FLOORBEAM AT STATION 1016 AND BL 0. SPLICED NEW SECTION OF BEAM P ER SRM 53-10-9 FIG 2. (M) 2 L 7 2 4F A16WE 1999091000365 19990910 00365 NM 1999 9 10 USAA990734 1 19990717 A 5320 WEB BOEING 737 737201 1384454 NM BS 259.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 48992 22352 PIT - DURING RON CHECK, FOUND 6 INCH CRACK AT PRESSURE SIDEWALL WEB, NOSE WHEEL WELL AT BS 259.5, WL 175.6. INSTALLED S HEETMETAL DOUBLERS AND FILLERS PER TYPICAL REPAIR 53-10-12 REV A AND EA 52440. (M) 2 L 7 2 4F A16WE 1999091000366 19990910 00366 NM 1999 9 10 USAA990743 1 19990723 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 985.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 42843 22867 TPA - DURING CX-1 CHECK, FOUND 2 INCH BY 10 INCH CORRODED AREA ON TOP SECTION OF 985.5 FLOORBEAM, RT SIDE AT PREVIOUS RE PAIR. INSTALLED NEW REPAIR AT FLOORBEAM PER TYPICAL REPAIR MANUAL 53-60-01. (M) 2 L 7 2 4F A16WE 1999091000367 19990910 00367 NM 1999 9 10 USAA990742 1 19990723 A 5320 FITTING BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 42843 22867 TPA - DURING CX-1 CHECK, FOUND TWO EACH 1 INCH LONG CRACKS IN FITTING AT BS 727 COMPRESSION CHORD, ONE AT RBL 25 AND ONE AT RBL 45. INSTALLED REPAIR PER TYPICAL REPAIR 53-10-03A. (M) 2 L 7 2 4F A16WE 1999091000368 19990910 00368 NM 1999 9 10 USAA990826 1 19990807 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 44712 22886 TPA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK ABOVE RIVET .125 INCH CRACK BELOW RIV ET STRINGER 17R, WL STATION 344 SKIN. INSTALLED REPAIR DOUBLER PER SB 737-53-1083 FIG 3C. (M) 2 L 7 2 4F A16WE 1999091000369 19990910 00369 NM 1999 9 10 USAASB99159 1 19990630 A 2612 5401 FIRE LOOP BOEING 737 7372B7 1384560 NM APU FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 269AU 22881 MCO-BWI - FLT 2662, AT APPROX FL330, CREW RECEIVED AND APU FIRE DETECTION LIGHT. CREW SHUTDOWN THE APU. WITH A/C BEING DOWN TO ONE SOURCE OF ELECT POWER, CREW DIVERTED FLIGHT TO THE NEAREST SUITABLE AIRPORT AT RDU. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU FIRE DETECTION LOOP M515 AND CON NECTOR D1446. OPS CHECK GOOD. CLEARED MEL ON THE NR 1 CSD. FOUND THE NR 1 CSD OVERSERVICED. CHECKED CHIP DETECTOR AN D FOUND TO BE OK. REPLACED CSD FILTER AND OIL COOLER (P/N 10-61-233-1). SERVICED CSD. LEAK CHECK AND OPERATIONAL CHEC K GOOD. (M) 2 L 7 2 4F A16WE 1999091000370 19990910 00370 NM 1999 9 10 USAASB99166 1 19990707 A 3260 189929 UPLOCK SENSOR BOEING 737 737201 1384454 NM RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 241US 22443 BOS - FLT 2673 - AFTER TAKEOFF, WHEN LANDING GEAR WAS RETRACTED, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AN D STAYED ON. CAPT RECYCLED THE GEAR BUT THE LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WIT HOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR PER BOEING MM 32-61-21. ACCOMPLISHED GEAR SWING. OPERATIONAL CHECK OF GEAR SYSTEM GOOD. (M) 2 L 7 2 4F A16WE 1999091000371 19990910 00371 NM 1999 9 10 USAASB99172 1 19990714 A 2910 O-RING BOEING 737 7372B7 1384560 NM MLG WW DAMAGED A USAA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 EA 19 283AU 23116 PBI-BWI - FLT 2615, DURING CRUISE, THE SYSTEM 'B' HYDRAULIC QUANTITY LIGHT ILLUMINATED FOLLOWED BY LOSS OF PRESSURE ON H YDRAULIC GAUGE. SHORTLY AFTER, THE LOW PRESSURE LIGHTS ON THE 'B' PUMPS ILLUMINATED. CREW SHUT OFF THE 'B' PUMPS AND D ECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT BWI. SYSTEM 'A' HYDRAULIC SYSTEM READ ONE GALLON UPON LANDING. MAINTENANCE FOUND AN O-RING DAMAGED AT THE NR 2 'B' PUMP PRESSURE LINE FITTING. REPLACED O-RING AND SERVICED SYSTEM. LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999091000372 19990910 00372 NM 1999 9 10 USAASB99182 1 19990724 A 5210 69902913 HINGE BOEING 737 737201 1384454 NM FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 259AU 22806 BWI - FLT 2622 - DURING CLIMB-OUT FROM BWI, CREW REPORTED A LOUD UNBEARABLE SQUEAL COMING FROM THE MAIN ENTRY DOOR. FLI GHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND R EPLACED THE MAIN ENTRY DOOR LOWER HINGE FLAP ASSEMBLY. PRESSURIZED AIRCRAFT TO 6.5 PSI. OPERATIONAL CHECK AND PRESSURI ZATION CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999091000373 19990910 00373 NM 1999 9 10 USAASB99193 1 19990805 A 2751 2061141 POSITION IND BOEING 737 737201 1384454 NM TE FLAPS FAILED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 259AU 14717 22806 BWI - FLT 2638 - ON PREPARATION FOR LANDING AT BWI, CREW ENCOUNTERED A SPLIT FLAP INDICATION OF 1 DEGREE. FLAPS WOULD N OT EXTEND BEYOND 2 DEGREES OR RETRACT. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND INSPECTED FLAPS. FLAPS CHECKED GOOD AND OPERATED NORMAL. SYSTEM OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4F A16WE 1999091000374 19990910 00374 NE 1999 9 10 USAASB99189 2 19990731 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE RIGHT BIRD STRIKE A USAA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. TO TAKEOFF 1 EA 19 271AU 42787 22883 709055 BWI - FLT 2704 - ON TAKEOFF ROLL, NR 2 ENGINE INGESTED A BIRD. CREW SHUT DOWN NR 2 ENGINE POWER PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS TEN M INUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSEMBLY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999091000375 19990910 00375 WP 1999 9 10 ASAA9980162 1 19990722 A 5610 PIN DOUG DC9 DC982 3022082 WP SLIDING WINDOW OUT OF POSITION A USAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 19 951AS 49111 SEA - AFTER ARRIVAL OF FLT 471, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. RESEATED HANDL E LATCH ROD ATTACH PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999091000376 19990910 00376 WP 1999 9 10 ASAA9980160 1 19990720 A 5610 PIN DOUG DC9 DC983 3022083 WP SLIDING WINDOW OUT OF POSITION A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 963AS 53077 SFO - AFTER ARRIVAL OF FLIGHT 102, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. REPOSITION ED UPPER GUIDE PIN IN TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000377 19990910 00377 WP 1999 9 10 ASAA9980157 1 19990715 A 5610 PIN DOUG DC9 DC983 3022083 WP SLIDING WINDOW OUT OF POSITION A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 943AS 53018 PDX - PRIOR TO DEPARTURE OF FLIGHT 304, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. REINSERT ED HINGE PIN IN WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000378 19990910 00378 WP 1999 9 10 ASAA9980148 1 19990701 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 958AS 53024 SEA - PRIOR TO DEPARTURE OF FLIGHT 87, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN AND MID CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000379 19990910 00379 WP 1999 9 10 ASAA9980147 1 19990628 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 1976 53023 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000380 19990910 00380 WP 1999 9 10 ASAA9980146 1 19990628 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 2866 48080 SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999091000381 19990910 00381 WP 1999 9 10 ASAA9980145 1 19990625 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 49126 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES I N THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999091000382 19990910 00382 WP 1999 9 10 ASAA9980144 1 19990621 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 1991 49387 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999091000383 19990910 00383 WP 1999 9 10 ASAA9980143 1 19990620 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 962AS 53076 SEA - PRIOR TO DEPARTURE OF FLT 354, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000384 19990910 00384 WP 1999 9 10 ASAA9980142 1 19990620 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP ROW 8-13 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 13 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000385 19990910 00385 SO 1999 9 10 C2XA99CL092 1 19990821 A 3234 12038594001 SELECTOR EMB 120 EMB120RT SO LANDING GEAR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15713 120031R 120114 CAK - FLT 3008 - THE CREW REPORTED THAT THE LEFT MAIN GEAR DISAGREEMENT LIGHT AFTER SELECTING THE GEAR. THE AIRCRAFT LA NDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR HANDLE AND PERFORMED OPERATIO NAL CHECKS IAW EMB120 MM 32-31-01, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000386 19990910 00386 CE 1999 9 10 C2XA99CL085 1 19990818 A 6120 5038912121 SWITCH BEECH 1900 1900D 1154162 CE ENGINE FAILED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 49543 0854 UE181 CLE - FLT 3439 - THE CREW REPORTED THAT ON TAKEOFF THE 'AFX DISABLE' LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE CR EW ABORTED TAKEOFF AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE A/F HIGH PRESSURE SWITCH IAW B1900D MM 61-21-00 AND REMOVED AND REPLACED PC BOARD A123 IAW B1900D MM 31-51- 05. OPS CHECK OF THE SYSTEM WAS GOOD IAW B1900D MM 61-21-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000387 19990910 00387 CE 1999 9 10 99ZZZM624 1 19990818 A 3150 1293640919 PC BOARD BEECH 1900 1900D 1154162 CE CABIN FAILED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 49543 998H94 UE181 CLE - FLT 3439 - THE CREW REPORTED THAT ON TAKEOFF THE 'AFX DISABLE' LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE CR EW ABORTED TAKEOFF AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE A/F HIGH PRESSURE SWITCH IAW B1900D MM 61-21-00 AND REMOVED AND REPLACED PC BOARD A123 IAW B1900D MM 31-51- 05. OPS CHECK OF THE SYSTEM WAS GOOD IAW B1900D MM 61-21-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000388 19990910 00388 SO 1999 9 10 C2XA99CL083 1 19990817 A 7722 ITT INDICATION EMB 145 EMB145 SO NR 1 ENGINE OUT OF RANGE A C2XA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 SW 09 13935 145022 CLE - FLT 4045 - THE CREW REPORTED THEY ABORTED TAKEOFF DUE TO THE NR 1 ITT WENT OVER 924 CELSIUS ON TAKEOFF. THE AIRCR AFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE DOWNLOADED THE CMC AND FOUND NO EXCEEDANCES RECORDED THE Y PERFORMED POWER ASSURANCE RUNS AND FOUND ALL PARAMETERS TO BE NORMAL IAW ALLISON AE3007A MM 72-00-00. THE AIRCRAFT WA S RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999091000389 19990910 00389 CE 1999 9 10 C2XA99CL081 1 19990816 A 3260 SWITCH BEECH 1900 1900D 1154162 CE LT MLG DIRTY A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 87550 UE205 ABE-CLE - FLT 3005 - THE CREW REPORTED THAT AFTER SELECTING THE GEAR DOWN THAT THE LEFT GEAR DOWN INDICATION CAME ON AND THEN WENT OUT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE LEFT LANDING GEAR D OWNLOCK SWITCH AND PERFORMED OPERATIONAL CHECKS IAW B1900D MM 32-00-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEAS ED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000390 19990910 00390 SO 1999 9 10 C2XA99CL080 1 19990812 A 5270 LIGHT EMB 120 EMB120RT SO CARGO DOOR ILLUMINATED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 09 16724 120171 CLE-GRR - FLT 3079 - THE CREW REPORTED THE CARGO DORO WARNING LIGHT CAME ON, DURING TAKEOFF. THE AIRCRAFT ABORTED TAKEO FF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 52-70-1/2 CAT 'C' CONTR OL NUMBER 184689. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000391 19990910 00391 SO 1999 9 10 C2XA99CL089 1 19990818 A 3610 SENSE LINE EMB 120 EMB120RT SO BLEED AIR LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16724 120171 CLE - ORF - FLT 3739 - THE CREW REPORTED THE CROSSBLEED WOULD NOT CLOSE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FUR THER INCIDENT. MAINTENANCE RESECURED THE CROSSBLEED SENSE LINE AND PERFORMED OPERATIONAL CHECKS IAW EMB120 MM 36-10-07, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000392 19990910 00392 CE 1999 9 10 C2XA99CL088 1 19990819 A 3030 HEAT BEECH 1900 1900D 1154162 CE RT PITOT MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 69548 UE193 CLE-MBS - FLT 3251 - THE CREW REPORTED THAT THE RIGHT PITOT HEAT WOULD NOT TURN ON. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE RIGHT PITOT HEAT IAW B1900D MM 30-30-00, NO DE FECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000393 19990910 00393 SO 1999 9 10 C2XA99CL090 1 19990820 A 2150 32144143 VALVE EMB 120 EMB120RT SO LEFT PACK FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 26714 350 120118 CLE-GRR - FLT 3069 - THE CREW REPORTED SMOKE FROM THE F/O'S SIDE PANEL. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURT HER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK VALVE IAW EMB120 MM 21-50-01 AND PERFORMED OPERATIONAL CHE CKS IAW EMB120 MM 21-50-00, NO DEFECTS WERE NOTED. (M) 2 L 7 2 4T RT A31SO 1999091000394 19990910 00394 SO 1999 9 10 C2XA99CL091 1 19990820 A 3260 INDICATION EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 12709 120101 YYZ-CLE - FLT 3609 - THE CREW REPORTED THAT ON FINAL THEY LOST THE NR 2 T6 INDICATION, TQ INDICATOR, THE GEAR INDICATION S, COM NR 2 AND THE AURAL WARNING WAS GOING OFF 'TRIM'. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESE T CB4071, AND JACKED THE AIRCRFAFT AND PERFORMED LANDING GEAR SWINGS IAW EMB120 MM 32-30-00, AND PERFORMED ENGINE RUNS W ITH ALL ELECTRICAL SYSTEMS ON IAW EMB120MM 71-00-00. ALL CHECKS WERE GOOD, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000395 19990910 00395 CE 1999 9 10 C2XA99CL079 1 19990815 A 3260 SWITCH BEECH 1900 1900D 1154162 CE RT MLG DIRTY A C2XA K NONE N FALSE WARNING LD LANDING 1 SW 09 81536 UE152 AZO-CLE - FLT 3032 - THE CREW REPORTED THE LANDING GEAR LIGHTS ON THE RIGHT SIDE DID NOT ILLUMINATE WHEN THE GEAR WAS SE LECTED DOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GEAR SWINGS AND FOUND THE RT DOWNLOCK INDICATOR TO BE VERY DIM, THE CLEANED THE UP AND DOWN LOCK SWITCHES AND OPS CHECKED THE SYSTEM GOOD IAW B1900D MM 32-30 -00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000396 19990910 00396 SO 1999 9 10 C2XA99CL078 1 19990814 A 7830 TR LIGHT EMB 145 EMB145 SO NR 2 ENGINE ILLUMINATED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 09 17928 145007 CLE-MSP - FLT 4059 - THE CREW REPORTED THAT ON TAKEOFF ROLL THE 'ENGINE 2 REV DISAGREE' WARNING APPEARED, THE AIRCRAFT A BORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 78-34-00 CO NTROL NUMBER 184857. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999091000397 19990910 00397 CE 1999 9 10 C2XA99CL077 1 19990812 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG FAILED A C2XA K NONE J WARNING INDICATION LD LANDING 1 SW 09 81533 UE137 LAN - THE CREW REPORTED THAT THE RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE WITH THE GEAR SELECTED DOWN. THE AIRCRAFT LAN DED IN LAN WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR ACTUATOR AND PERFORMED OPERAT IONAL CHECK IAW B1900D MM 32-30-10, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000398 19990910 00398 SO 1999 9 10 C2XA99CL076 1 19990813 A 2750 3635001001 BRAKE EMB 145 EMB145LR SO LT TE FLAP FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14950 00230 145061 CLE - THE CREW REPORTED THAT AFTER TAKEOFF THE FLAP LOW SPEED ADVISORY CAME ON, THE AIRCRAFT RETURNED TO CLEVELAND WITHO UT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT AND RIGHT FLAP TRANSMISSION BRAKES IAW EMB145 MM 27 -51-01, SYSTEM OPERATIONAL CHECK WAS GOOD IAW EMB145 MM 27-51-00-700-801-A. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999091000399 19990910 00399 SO 1999 9 10 99ZZZM625 1 19990813 A 2750 3635001001 BRAKE EMB 145 EMB145LR SO LT TE FLAP FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14950 00235 145061 CLE - THE CREW REPORTED THAT AFTER TAKEOFF THE FLAP LOW SPEED ADVISORY CAME ON, THE AIRCRAFT RETURNED TO CLEVELAND WITHO UT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT AND RIGHT FLAP TRANSMISSION BRAKES IAW EMB145 MM 27 -51-01, SYSTEM OPERATIONAL CHECK WAS GOOD IAW EMB145 MM 27-51-00-700-801-A. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999091000400 19990910 00400 SO 1999 9 10 C2XA99CL075 1 19990813 A 7722 TUBE EMB 145 EMB145 SO NR 2 ITT DISCONNECTED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 09 14925 145004 7722 CLE - THE CREW REPORTED THAT THE NR 2 ENGINE ITT WENT OT RED LINE ON TAKEOFF, THE AIRCRAFT ABORTED TAKEOFF, AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE CABCV INTERCONNECT TUBE DISCONNECTED. MAINTENANCE RECONNE CTED THE TUBE IAW EMB145 75-31-15 AND PERFORMED ENGINE RUNS AT IDLE AND MAX TAKEOFF IAW EMB145 MM 72-00-00. ITT WAS NOR MAL IAW EMB145 MM 77-00-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999091000401 19990910 00401 SO 1999 9 10 C2XA99CL100 1 19990824 A 2120 PIN EMB 145 EMB145 SO NR 1 RAM AIR LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 16927 145006 CLE - FLT 4237 - THE CREW REPORTED THE RAM AIR FAILED DURING FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE SECURED A LOOSE PIN ON THE NR 1 RAM AIR ACTUATOR AND PERFORMED OPERATIONAL CHECKS IAW EMB145 MM 21-25-00, NO DEFECTS WERE NOTED. THE AIRCRAFT RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999091000402 19990910 00402 CE 1999 9 10 C2XA99CL099 1 19990823 A 3260 SWITCH BEECH 1900 1900D 1154162 CE LANDING GEAR DIRTY A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 09 38537 UE158 MBS-CLE - FLT 3240 - THE CREW REPORTED THE RIGHT GEAR LIGHT 'R AND H' ARE INTERMITTENT. THE AIRCRAFT LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE CLEANED THE PRESS/RESET PUSHBUTTON, CLEANED ALL THE SWITCHES AND INSPECTED THE WIRING HARNES SES, AND PERFORMED OPS CHECK IAW B1900D MM32-30-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000403 19990910 00403 CE 1999 9 10 C2XA99CL098 1 19990823 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG FAILED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 09 87550 8741 UE205 MDT-CLE - FLT 3131 - THE CREW REPORTED THE 'L' GEAR LIGHT WOULD NOT ILLUMINATE AFTER GEAR EXTENSION UNTIL ON SHORT FINAL , AT ABOUT 500 FT. THE LIGHT ILLUMINATED WITH THE PRESS TO TEST. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4T RT A24CE 1999091000404 19990910 00404 CE 1999 9 10 C2XA99CL097 1 19990823 A 3260 1293640455 PC BOARD BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 09 87550 504D95 UE205 PIT-CLE - FLT 3037 - THE CREW REPORTED THEY HAD TO CYCLE THE LANDING GEAR THREE TIMES TO GET THE 'L' GREEN LIGHT TO ILLU MINATE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED PC BOARD A319 AND PERFORMED OPE RATIONAL CHECKS IAW B1900D MM 32-60-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000405 19990910 00405 SO 1999 9 10 C2XA99CL096 1 19990823 A 2130 PRESSURIZATION EMB 120 EMB120RT SO CABIN FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 16729 120185 AZO - FLT 3019 - THE CREW REPORTED A BURNING SMELL IN CLIMB BEFORE THE PRESSURIZATION FAILED. THE AIRCRAFT LANDED WITHO UT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE AIRCONDITIONER SYSTEM BOTH PACKS OPERATED NORMAL I AW EMB120MM 21-00-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000406 19990910 00406 CE 1999 9 10 C2XA99CL095 1 19990822 A 3020 DUCT BEECH 1900 1900D 1154162 CE NR 1 ENGINE LOOSE A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 38537 UE158 CLE - FLT 3129 - THE CREW REPORTED THE LEFT FIRE T-HANDLE ILLUMINATED DURING TAXI TO THE RUNWAY, THE LIGHE EXTINGUISHED AFTER PULLING T-HANDLE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESECURED THE NR 1 ENG INE RIGHT INLET DE-ICE DUCT TO THE EXHAUST STACK IAW B1900 MM 78-00-00 AND PERFORMED OPERATIONAL CHECK OF THE FIRE DETEC TION SYSTEM IAW B1900 MM 26-00-00, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000407 19990910 00407 SO 1999 9 10 C2XA99CL094 1 19990822 A 3350 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16729 120185 CLE-SDF - FLT 3285 - THE CREW REPORTED THE LAST FIVE EMERGENCY LIGHT IN THE CABIN AISLE ARE INOPERATIVE. THE AIRCRAFT W AS AT THE GATE, NO FURTHER INCIDENTS REPORTED. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE SYSTEM IAW EMB120MM 33-5 0-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000408 19990910 00408 CE 1999 9 10 C2XA99CL093 1 19990820 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG FAILED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 09 87552 1273 0671A UE216 MBS-CLE - FLT 3250 - THE CREW REPORTED THAT WHEN THE GEAR WAS EXTENDED TO THE LEFT MAIN GEAR DOWN LIGHT WAS DELAYED APPR OX FIVE SECONDS THEN CAME ON. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR ACTUATOR AND PERFORMED OPERATIONAL CHECKS IAW B1900D MM 32-30-10, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS REL EASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091000409 19990910 00409 EU 1999 9 10 C2XA99BT081 1 19990813 A 2120 AIR DISTRIBUTION AEROSP ATR42 ATR42320 8680930 EU COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 17831 185 EWR - FLT C03099 - CREW REPORTED STRONG ODOR IN COCKPIT (POSSIBLE ELECTRICAL ODOR) ON CLIMB-OUT, AIR RETURNED WITHOUT IN CIDENT. MAINTENANCE PERFORMED ENGINE GROUND RUNS, CHECKED CABIN AND FLIGHT COMPARTMENT AIR DISTRIBUTION SYSTEMS AND FOU ND NO DISCREPANCIES. RETURNED AIRCRAFT TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091000410 19990910 00410 SO 1999 9 10 C2XA99BT080 1 19990812 A 3320 SOCKET EMB 145 EMB145ER SO ROW 4A BURNED A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 09 13929 145009 EWR - FLT C04235 - CREW REPORTED SEAT 4A LIGHT SOCKET BURNED AND ELECTRICAL SMOKE MESSAGE REPORTED ON EICAS PERFORMED GA TE RETURN. REMOVED AND REPLACED LIGHT SOCKET AND OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1999091000411 19990910 00411 SO 1999 9 10 C2XA99BT079 1 19990823 A 3350 3025101 LIGHT EMB 145 EMB145LR SO EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13949 145057 BTV - CO4218 - DURNG 4A INSPECTION MAINTENANCE FOUND RIGHT AFT EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS ON LIGHT S OCKET, OPS CHECKED GOOD. (M) 2 L 7 2 4T RT T00011AT 1999091000412 19990910 00412 EU 1999 9 10 C2XA99BT078 1 19990824 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14813 100 BTV - CO3680 - DURING 3A INSPECTION MAINTENANCE, FOUND PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT UNIT ON PASSENGER DOOR AND OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999091000413 19990910 00413 SO 1999 9 10 C2XA99BT077 1 19990822 A 3350 SOCKET EMB 145 EMB145ER SO RT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12946 145052 BTV - DURING A ROUTINE INSPECTION, MAINTENANCE FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHTS NOT WORKING. MAINTENANCE C LEANED RT FORWARD OVERWING EMERGENCY LIGHT SOCKET AND OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999091000414 19990910 00414 SO 1999 9 10 C2XA99BT076 1 19990824 A 3350 3025101 LIGHT EMB 145 EMB145 SO RT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 BTV - CO4218 - DURING ROUTINE INSPECTION, FOUND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT, OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999091000415 19990910 00415 SO 1999 9 10 ASOA99077 1 19990810 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 285AS 14951 120265 DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERG ENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000416 19990910 00416 SO 1999 9 10 ASOA99076 1 19990806 A 5320 12005807007 BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 120060 DURING C-CHECK, FOUND CORROSION IN THE FUSELAGE FLOOR OMEGA BEAM. REPAIRS WERE MADE IAW THE EO 120-53-0114. (M) 2 L 7 2 4T RT A31SO 1999091000417 19990910 00417 SO 1999 9 10 ASOA99075 1 19990806 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 505AS 3229 120279 DURING INSPECTION, NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERG ENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000418 19990910 00418 SO 1999 9 10 ASOA99074 1 19990806 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 236AS 24432 120049 DURING INSPECTION, NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERG ENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000419 19990910 00419 SO 1999 9 10 ASOA99073 1 19990910 A 5313 STRINGER EMB 120 EMB120RT SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 264AS 120165 DURING INSPECTION, FOUND CRACKS ON THE LEFT AND RIGHT NR 10 STRINGER. REPAIRS WERE MADE IAW THE EO 120-57-0081 AND EO 1 20-57-0082. (M) 2 L 7 2 4T RT A31SO 1999091000420 19990910 00420 SO 1999 9 10 ASOA99072 1 19990802 A 3350 1013073 BULB EMB 120 EMB120RT SO CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 258AS 120131 DURING INSPECTION, FOUND CABIN TRACK LIGHTING BULB BROKEN. ATL MAINTENANCE REPAIRED BROKEN BULB. OPERATIONAL CHECKS WE RE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091000421 19990910 00421 WP 1999 9 10 ASAA9980161 1 19990721 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999091000422 19990910 00422 WP 1999 9 10 ASAA9980159 1 19990719 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 957AS 49126 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 16 TO 19 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999091000423 19990910 00423 WP 1999 9 10 ASAA9980158 1 19990715 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 975AS 53451 SEA - PRIOR TO DEPARTURE OF FLT 444, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000424 19990910 00424 WP 1999 9 10 ASAA9980156 1 19990714 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 975AS 53451 ANC - PRIOR TO DEPARTURE OF FLT 188, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE INOPERATIVE. S ECURED CONNECTOR TO LIGHT ASSEMBLY AT ROW 27 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000425 19990910 00425 WP 1999 9 10 ASAA9980154 1 19990712 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 01 947AS 53020 ONT - RETURN TO GATE OF FLIGHT 439, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE . RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000426 19990910 00426 WP 1999 9 10 ASAA9980153 1 19990708 A 3350 0105606004 BULB DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 968AS 53016 PDX - DURING MAINTENANCE CHECK, THREE EMERGENCY FLOOR TRACK RED LIGHTS AT THE OVERWING EXITS WERE FOUND INOPERATIVE. RE PLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999091000427 19990910 00427 NM 1999 9 10 ASAA9910224 1 19990721 A 3397 WIRE BOEING 737 737290C 138448V NM ROW 17 BROKEN A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 742AS 23136 ANC - PRIOR TO FLIGHT 143, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 17 WERE FOUND TO BE INOPERATIVE. REPAIRED BROKE N WIRE AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000428 19990910 00428 NM 1999 9 10 ASAA9910223 1 19990718 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM ROW 5 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 5 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999091000429 19990910 00429 NM 1999 9 10 ASAA9910222 1 19990717 A 3350 6104781 BATTERY GRIMES BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 743AS 21821 ANC - PRIOR TO FLIGHT 152, THE EMERGENCY EXIT TRACK LIGHTS ON SEAT PALLET 2-6 WERE FOUND TO BE INOPERATIVE. REPLACED BA TTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000430 19990910 00430 NM 1999 9 10 99ZZZM626 1 19990717 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 743AS 21821 ANC - PRIOR TO FLIGHT 152, THE EMERGENCY EXIT TRACK LIGHTS ON SEAT PALLET 2-6 WERE FOUND TO BE INOPERATIVE. REPLACED BA TTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000431 19990910 00431 NM 1999 9 10 ASAA9910221 1 19990716 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM ROW 5 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 5 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000432 19990910 00432 NM 1999 9 10 ASAA9910220 1 19990712 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 737298C 1384490 NM LT EMER EXIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WILL NOT TURN OFF. REPLACED BATTERY CHA RGER AND BATTERY PACK. LIGHT WILL NOW TURN OFF. RELEASED PER MEL 33-14, FOR DAY OPERATION ONLY. SUBSEQUENTLY REPLACED BATTERY PACK AND LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSEMBLY, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999091000433 19990910 00433 NM 1999 9 10 99ZZZM627 1 19990712 A 3350 65753421 LIGHT GRIMES BOEING 737 737298C 1384490 NM LT EMER EXIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WILL NOT TURN OFF. REPLACED BATTERY CHA RGER AND BATTERY PACK. LIGHT WILL NOW TURN OFF. RELEASED PER MEL 33-14, FOR DAY OPERATION ONLY. SUBSEQUENTLY REPLACED BATTERY PACK AND LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSEMBLY, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999091000434 19990910 00434 NM 1999 9 10 ASAA9910219 1 19990711 A 3350 6013211 BATERY PACK GRIMES BOEING 737 737298C 1384490 NM EMER EXIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE VERY DIM. REPLACED BATT ERY PACK AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999091000435 19990910 00435 NM 1999 9 10 ASAA9910218 1 19990710 A 3350 8731002142 LIGHT BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE 'EXIT TO REAR' LIGHT ON SMOKE BARRIER NR 12 WAS FOUND TO BE INOPERATIVE. REPLACED ' EXIT TO REAR' LIGHT ASSY, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999091000436 19990910 00436 NM 1999 9 10 ASAA9910217 1 19990709 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 7372X6C 1384552 NM L1 DOOR DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR AND RIGHT OVERWING EXIT LIGHTS WERE FOUND TO BE VERY DIM. REPLACED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999091000437 19990910 00437 NM 1999 9 10 ASAA9910216 1 19990707 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM ROWS 8-11 INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 740AS 22578 SEA - PRIOR TO FLIGHT 63 - THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 8-11 AND 16-19 ILLUMINATED. REPLACED THE RECEIVER AT ROWS 8-11 AND THE BATTERY AT ROWS 16-19, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000438 19990910 00438 NM 1999 9 10 99ZZZM628 1 19990707 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM ROWS 16-19 DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 740AS 22578 SEA - PRIOR TO FLIGHT 63 - THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 8-11 AND 16-19 ILLUMINATED. REPLACED THE RECEIVER AT ROWS 8-11 AND THE BATTERY AT ROWS 16-19, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000439 19990910 00439 NM 1999 9 10 ASAA9910214 1 19990703 A 3350 6104781 BATTERY GRIMES BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 741AS 21959 ANC - PRIOR TO FLIGHT 152, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ON THE 3RD PALLET FROM AFT. REP LACED BATTERY IN AFT TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000440 19990910 00440 NM 1999 9 10 ASAA9910213 1 19990702 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 SEA - PRIOR TO FLIGHT 61, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGH T OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999091000441 19990910 00441 NM 1999 9 10 ASAA9910212 1 19990702 A 3350 RPS1B CHARGER GRIMES BOEING 737 737210C 1384459 NM L2/R2 DOORS INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE L2 AND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACE D BATTERY PACK AND CHARGER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000442 19990910 00442 NM 1999 9 10 99ZZZM629 1 19990702 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 737210C 1384459 NM L2/R2 DOORS DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE L2 AND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACE D BATTERY PACK AND CHARGER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999091000443 19990910 00443 GL 1999 9 10 C2XA99CL082 2 19990816 A 7200 ENGINE EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 14945 145049 CAE310012 YUL-CLE - FLT 3995 - THE CREW REPORTED THE NR 1 ENGINE SMOKES ON SHUTDOWN. THE AIRCRAFT WAS AT THE GATE, NO FURTHER INC IDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW TASK CARD NR 6271001. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999091000444 19990910 00444 NM 1999 9 10 AALA990911 1 19990524 A 5320 DOUG MD11 MD11 3023602 NM UNKNOWN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - THE NR 1 GALLEY FLOOR SUPPORT IS CORRODED. REMOVED GALLEY FLOOR SUPPORT NR 1. MANUFACTURED FLOOR SUPPORT PER AAR D 51-10-001. INSTALLED NR 1 GALLEY FLOOR SUPPORT 2 L 7 3 4F RT A22WE 1999091000445 19990910 00445 WP 1999 9 10 AALA991120 1 19990729 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 457AA 49562 TUL - NR 3 LONG LEFT CRACKED AT STATION 160. REMOVED DAMAGED LONG NR 3 SECTION. INSTALLED LONG SPLICE FITTING PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999091000446 19990910 00446 WP 1999 9 10 AALA991119 1 19990728 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1201 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 457AA 49562 TUL - NR 2 CABIN SEAT TRACK CORRODED IN CTR AND AROUND LUGS AT STATION 1201. ROUTED OUT CORRODED AREA OF TRACK. INSTAL LED REPAIR PLUG PER SRM 53-05 FIG 4B. (M) 2 L 7 2 4F A6WE 1999091000447 19990910 00447 WP 1999 9 10 AALA991118 1 19990728 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 486 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 457AA 49562 TUL - NR 1 SEAT TRACK GOUGED IN CENTER TOP SURFACES AT STATION 486. ROUTED OUT DAMAGED AREA. INSTALLED REPAIR PLUG PER SRM 53-05 FIG 4B. (M) 2 L 7 2 4F A6WE 1999091000448 19990910 00448 WP 1999 9 10 AALA991117 1 19990728 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 703 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 457AA 49562 TUL - NR 1 SEAT TRACK GOUGED IN CENTER TOP SURFACE AT STATION 703. ROUTED OUT DAMAGED AREA OF TRACK. INSTALLED REPAIR PLUG PER SRM 53-05 FIG 4B. (M) 2 L 7 2 4F A6WE 1999091000449 19990910 00449 EU 1999 9 10 AALA991161 1 19990811 A 5720 ANGLE AIRBUS 300 A300B4605R 3930308 EU RT WING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - ACCOMPLISH PERMANENT REPAIR TO RIGHT WING ROOT PICK UP ANGLE. MADE REPAIR TO RT WING ROOT PER ESO 3095, DATED 7-6 -99. (M) 2 L 7 2 4F RT A35EU 1999091000450 19990910 00450 EU 1999 9 10 AALA991009 1 19990707 A 5720 ANGLE AIRBUS 300 A300B4605R 3930308 EU LT WING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - ACCOMPLISH PERMANENT REPAIR TO LEFT WING ROOT PICK UP ANGLE. INSTALLED PERMANENT REPAIR TO LT WING ROOT PICK UP A NGLE PER ESO 3095, DATED 7-6-99. (M) 2 L 7 2 4F RT A35EU 1999091000451 19990910 00451 NM 1999 9 10 AALA990948 1 19990625 A 2820 AAP2043A VALVE H80682 BOEING 727 727223 1384074 NM RT WING DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 886AA 21525 BNA - FLT 1750 - EN ROUTE DFW-PHL, NR 2 CROSSFEED VALVE FAILED TO OPEN. AIR INTERRUPTED AND LANDED BNA WITHOUT INCIDENT . CHECKED AND DEFERRED ACCORDING TO MEL. REPLACED NR 2 FUEL MANIFOLD VALVE. PERFORMED OPERATIONAL CHECK WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999091000452 19990910 00452 NM 1999 9 10 AALA991069 1 19990720 A 2840 421505 TRIM UNIT BOEING 727 727227 1384078 NM COCKPIT DEFECTIVE A AALA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 723AA 404 20731 MIA - FLT 2104 - EN ROUTE BZE-MIA, FUEL QTY GAUGE FOR NR 2 TANK FLUCTUATED AND INDICATED A DECREASING FUEL SUPPLY AT AT GREATER RATE THAN FUEL USAGE FROM TANKS 1 AND 3. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED MIA WITHOUT INCIDENT. N R 2 FUEL TANK AND SUPPLY LINES INSPECTED FOR LEAKS. NONE FOUND. REPLACED NR 2 FUEL SYSTEM DIGITAL CALIBRATION TRIM UNI T. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999091000453 19990910 00453 NM 1999 9 10 AALA991134 1 19990803 A 2612 901905 FIRE LOOP BOEING 767 767323 1385205 NM LT ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 374AA AA79 25201 LAX - FLT 898 - AFTER TAKEOFF LAX, MIA LEFT ENGINE FIRE LOOP NR 2 LIGHT ILLUMINATED FOLLOWED BY LOOP NR 1 LIGHT. AIRCRA FT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE UPPER AFT FIRE DETECTION LOOP. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091000454 19990910 00454 NM 1999 9 10 AALA991089 1 19990724 A 2530 8609010000 OVEN BOEING 767 767223 1385123 NM CABIN DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 303AA 22309 SFO - FLT 177 - EN ROUTE JFK-SFO, NR 2 OVEN IN FIRST CLASS GALLEY PRODUCED SMOKE AND A BURNING ODOR. CLEANED NUMBER 2 F IRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091000455 19990910 00455 WP 1999 9 10 AALA991131 1 19990802 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 407AA 49318 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR EMERGENCY WALK AROUND LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOOR EMERGENCY WALK AROUND LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091000456 19990910 00456 WP 1999 9 10 AALA991143 1 19990805 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 459AA 49564 LAX - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT CONNECTOR AND LIGHT STRIP IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091000457 19990910 00457 EU 1999 9 10 AALA991090 1 19990725 A 2150 20497524 ACM AIRBUS 300 A300B4605R 3930308 EU ACM BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 14053 1182775 420 KIN - FLT 628 - AFTER TAKEOFF KIN EN ROUTE TO MIA, SMOKE AND FUMES WERE NOTED IN COCKPIT. AIRCRAFT RETURNED TO KIN AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AIR CONDITIONING PACK ACM. ALSO, REPLACED NR 1 AIR CONDITIONING PACK FLOW CONTR OL VALVE AS PRECAUTIONARY MEASURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999091000458 19990910 00458 NM 1999 9 10 AALA991098 1 19990726 A 3610 CLAMPS BOEING 727 727223 1384074 NM NR 3 ENGINE LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 702AA 22460 MIA - FLT 275 - AFTER TAKEOFF MIA EN ROUTE TO LRM, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO M IA AND LANDED WITHOUT INCIDENT. RESECURED LOOSE BLEED DUCT CLAMPS IN NR 3 ENGINE STRUT. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 3 4F A3WE 1999091000459 19990910 00459 EU 1999 9 10 AALA991136 1 19990804 A 3260 CONNECTOR FOKKER F28 F28MK0100 4990807 EU COCKPIT LOOSE A AALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 07 1440A 11435 DFW - FLT 1137 - ON APPROACH TO DFW, LANDING GEAR LIGHTS FAILED TO ILLUMINATE ON EXTENSION OF LANDING GEAR. AIRCRAFT LA NDED DFW WITHOUT INCIDENT. RESECURED CONNECTOR TO GEAR ANNUNCIATOR MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F RT 1999091000460 19990910 00460 WP 1999 9 10 AALA991101 1 19990728 A 2810 PANEL DOUG DC9 DC982 3022082 WP RT WING LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 07 459AA 49564 BNA - FLT 712 - EN ROUTE DFW-LGA, FUEL LEAK NOTED FROM INSPECTION PANEL ON UPPER RIGHT WING. AIRCRAFT LANDED BNA WITHOU T INCIDENT. RESEALED INSPECTION PANEL ON UPPER RIGHT WING. FILLED TANK WITH FUEL AND NO LEAKS WERE NOTED. SYSTEM GROU ND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091000461 19990910 00461 WP 1999 9 10 AALA991113 1 19990728 A 2150 20495061 ACM DOUG DC9 DC982 3022082 WP LEFT ACM BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 466AA 542493 49596 MIA - FLT 2024 - EN ROUTE MIA-BOS, SMOKE NOTED IN CABIN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACE D LEFT ACM. ACCOMPLISHED PACK BURNOUT OF BOTH AIR CONDITIONING PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091000462 19990910 00462 NM 1999 9 10 AALA990942 1 19990624 A 2613 3566444000 OVERHEAT LOOP BOEING 727 727223 1384074 NM NR 3 ENGINE DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 874AA 21386 MIA - FLT 625 - AFTER TAEKOFF STRUT OVERHEAT LIGHT FLICKERED AT FL330. FLIGHT CREW PERFORMED EMERGENCY CHECKLIST AND LI GHT EXTINGUISHED. CLOSED NUMBER THREE BLEED VALVE AND DESCENDED TO FL250. OPENED NR 1 BLEED VALVE FOR REMAINDER OF FLI GHT WITH NO OVERHEAT INDICATION. MAINTENANCE FOUND STRUT OVERHEAT LOOP FAULTY. REPLACED STRUT OVERHEAT LOOP. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999091000463 19990910 00463 WP 1999 9 10 AALA991133 1 19990803 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 441AA 49460 DFW - FLT 2374 - AFTER TAKEOFF DFW TO ORD, NOTED HYDRAULIC FLUID ODOR THROUGHOUT CABIN AND LEFT HYDRAULIC FLUID QTY DECR EASING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPAIRED LEAKING HYDRAULIC FLUID LINE CONNECTED TO HYDRAULIC FLUI D TRANSFER PUMP. ACCOMPLISHED AIR CONDITIONING PACK BURN OUT AND REPLACED SEPARATOR BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091000469 19990910 00469 EA 1999 9 10 99ZZZX3380 2 19990824 A 7200 ENGINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA NR 1 ENGINE FAILED A DATA E C ENGINE SHUTDOWN ABORTED TAKEOFF T J ENGINE CASE PENETRATION WARNING INDICATION TO TAKEOFF 1 GL 13 58DD 14919 3846 SH3008 PCE84159 AS POWER WAS ADVANCED FROM FLIGHT IDLE DURING THE TAKEOFF ROLL, A LOUD BANG CAME FROM THE LEFT ENGINE. LEFT NQ BEGAN DE CREASING. ENGINE WAS SHUT DOWN AND TAKEOFF ABORTED. PAST FLIGHT INSPECTION REVEALED HOLES AND DENTS IN BOTH EXHAUST ST ACKS AS WELL AS TWO PUNCTURES IN THE LEFT FUSELAGE SKIN. 2 H 7 2 4T 4 T A41EU E4EA 1999091000470 19990910 00470 CE 1999 9 10 99ZZZX3381 1 19990811 A 7722 414021 INDICATOR BEECH 200 B200 1152922 CE ITT FAILED A DBCA O OTHER N FALSE WARNING AP APPROACH 1 GL 13 670DF 411 483 BB1631 NR 1 ITT GAUGE DROPPED TO ZERO ON APPROACH. TROUBLESHOT TO BAD ITT GAUGE. REPLACED GAUGE, PN 41-402-1, SN 483 OFF, PN 130-380041-7, SN 543 ON. OPERATIONS CHECKED OK. 1 L 7 2 4T A24CE 1999091000472 19990910 00472 CE 1999 9 10 99ZZZX3383 1 19990315 A 3231 66003161 SELECTOR VALVE LEAR 35 35A 5170602 CE MLG DOOR INTERMITTENT A CJPA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 03 925DM 5307 486 LANDING GEAR WOULD NOT RETRACT WHEN 'GEAR UP' SELECTED. SNOW, ICE AND SLUSH WERE SUSPECT. AIRCRAFT WAS JACKED AND CLEA NED OF ALL MOISTURE AND GEAR OPERATED NORMALLY. AFTER TAKEOFF WITH DE-ICED GEAR, LANDING GEAR DID NOT RETRACT AGAIN. A IRCRAFT WAS JACKED AND TROUBLESHOT. AFTER SEVERAL CYCLES, GEAR FAILED TO RETRACT. THE MAIN GEAR DOOR SELECTOR VALVE WA S DETERMINED TO BE INTERMITTENT AND WAS REPLACED. GEAR WAS CYCLED NORMALLY ON JACKS AND TEST FLOWN NORMALLY. 2 L 7 2 4F A10CE 1999091000476 19990910 00476 CE 1999 9 10 99ZZZX3387 1 19990810 A 5210 9942002457 HINGE BEECH 99 99 1154002 CE CREW DOOR BENT A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 24BH U67 CREW DOOR LEAKS AIR IN-FLIGHT DUE TO SLIGHT MIS-ALIGNMENT ON FORWARD EDGE. PROBLEM FOUND TO BE BENT HINGE ON UPPER FORW ARD SIDE. REPLACED HINGE AND INSPECTED AREA FOR HIDDEN DAMAGE. NO OTHER DISCREPANCIES TO REPORT. THE DESIGN OF THE HI NGE IS SUCH THAT THIS PROBLEM COULD RECUR IF DOOR IS HANDLED ROUGHLY OR DOOR SEAL IS NOT PROPERLY SHIMMED. FORTUNATELY, INSPECTIONS ARE FREQUENTLY CONDUCTED TO INCLUDE THIS AREA. THE HINGE SHOWED NO SIGN OF CRACKS THROUGH VISUAL INSPECTIO N. 1 L 7 2 3T A14CE 1999091000534 19990910 00534 NM 1999 9 10 SPA9900005 1 19990820 A 3350 900542 BATTERY CHARGER BOEING 737 7372T4 1384492 NM CABIN INOP A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING ROUTINE CHECK, THE INTERIOR EMERGENCY EXIT LIGHT ABOVE THE LT OVERWING ESCAPE HATCH WAS FOUND INOPERATIVE. THE A SSOCIATED SYSTEM BATTERY CHARGER WAS REPLACED. SUBSEQUENT SYSTEM TEST WAS SATISFACTORY PER MM 33-51-81. 2 L 7 2 4F A16WE 1999091000535 19990910 00535 NM 1999 9 10 SPAA00006 1 19990822 A 5330 SKIN BOEING 737 737236 1384476 NM SERVICE DOORWAY CRACKED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 923WA 21800 DURING THE ACCOMPLISHMENT OF CPCP TASK C53-100-01, PART 10 OF 12, A 3 INCH CRACK WAS NOTED IN THE FUSELAGE SKIN AND DOUB LER AT THE LOWER AFT CORNER OF THE RIGHT FORWARD SERVICE DOOR CUTOUT. DAMAGED MATERIAL WAS REMOVED, REPAIR DOUBLERS AND FILLERS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE B-737 SRM, CHAPTER 53-3-3, FIGURE 26. 2 L 7 2 4F RT A16WE 1999091000536 19990910 00536 NM 1999 9 10 SPAA00007 1 19990904 A 2910 106056342 HYDRAULIC LINE BOEING 737 7372T4 1384492 NM NR 1 ENGINE DAMAGED A SPAA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 703S 22529 RDD - NR 1 ENGINE LOST ALL A SYSTEM HYDRAULIC FLUID DURING ENGINE START. INVESTIGATION REVEALED THAT THE NR 1 ENGINE DR IVEN HYDRAULIC PUMP PRESSURE LINE WAS DAMAGED, CAUSING THE FLUID LOSS. THE HYDRAULIC PRESSURE LINE WAS REPLACED AND LEA K CHECKED PER MM 29-11-0. CASE DRAIN FILTER INSPECTED PER MM 29-11-41. HYDRAULIC SYSTEM SERVICED PER MM 12-12-0. 2 L 7 2 4F A16WE 1999091000537 19990910 00537 NM 1999 9 10 AT9900621R1 1 19990901 A 3350 BATTERY PACK BOEING 737 7372L9 1384497 NM L-2 DOOR DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 737Q 21279 EXTERIOR EMERGENCY LIGHTS AFT OF R2 AND L2 DOOR DID NOT ILLUMINATE DURING ROUTINE CHECK. REMOVED BATTERY PACK. CHECK V OLTAGE, VOLTAGE OF BATTERY CHECKS GOOD. REMOVED AND RESEATED BATTERY PACK HOUSING. LIGHTS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999091000538 19990910 00538 WP 1999 9 10 AT9900633 1 19990901 A 4920 38025611 APU DOUG DC9 DC932 3022066 WP APU COMPT FAILED A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 810AT 47277 AT 5,000 FEET DURING CLIMB, SMOKE FILLED THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO AIRPORT. FOUND CRACK IN TAURUS. R EMOVED AND REPLACED APU. OPS CHECK AND LEAK CHECK GOOD IAW 49-10-0. 2 L 7 2 4F A6WE 1999091000539 19990910 00539 1999 9 10 AT9900634 2 19990903 A 7261 655813530 OIL LINE BOEING 737 737297 1384480 NM NR 2 ENGINE BROKEN A ZZDA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 462AT 22631 NR 2 ENGINE OIL PSI AND QUANTITY WENT TO ZERO, SHUT DOWN ENGINE IN-FLIGHTAND DIVERTED TO JAN. LANDED AIRCRAFT WITHIN TH IRTY MINUTES OF INCIDENT. FOUND BROKEN OIL LINE AT ENGINE MAIN OIL SCREEN, REPLACED OIL LINE. 2 L 7 2 4F A16WE 1999091000540 19990910 00540 EU 1999 9 10 PNSA990801 1 19990812 A 2613 OVERHEAT PROB FENWAL 1734362 SAAB SF340 340B 7860101 EU LT TAIL PIPE FAILED A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 685PA 212 DURING CLIMBOUT, LT TAIL PIPE OVERHEAT LIGHT ILLUMINATED. RETURNED TO AIRPORT, LANDING WAS UNEVENTFUL. FURTHER INVESTI GATION DID NOT REVEAL ANY PHYSCIAL OR ELECTRICAL PROBLEMS WITH THE TAIL PIPE HEAT DETECTION SYSTEM. AS A PRECAUTIONARY MEASURE ALL THREE OVERHEAT PROBES WERE CHANGED. NO FURTHER PROBLEMS WERE NOTED. 2 L 7 2 4T RT A52EU 1999091000541 19990910 00541 NE 1999 9 10 PNSA990802 2 19990825 A 7261 O RING SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE LAEKING A PNSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 685PA 212 785163 RT ENGINE OIL PRESSURE STARTED TO FLUCTUATE BETWEEN 30 TO 80 PSI. AIRCRAFT RETURNED TO BASE, LANDING WAS NORMAL. NO VI SABLE OIL LEAKAGE WAS FOUND. OIL LEVEL WAS LOW. FOUND C SUMP O-RINGS LEAKING. REPLACED O-RINGS. 2 L 7 2 4T 4 T RT A52EU E8NE 1999091000542 19990910 00542 EA 1999 9 10 PNSA990804 2 19990828 A 7414 10349276 CONDENSER PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA LH MAGNETO INTERMITTANT A PNSA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 8429N 8834 328106089 JUST AFTER TAKEOFF AIRCRAFT BEGAN TO VIBRATE. RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. REPLACED SHORTED CONDENSER F OR LT MAGNETO. OPERATIONAL CHECK OK. 1 L 7 1 3O 3 O A3SO 1E4 1999091000543 19990910 00543 EU 1999 9 10 QXEA9901682 1 19990903 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU COCKPIT DOOR INOP A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 481US 11230 BOI- EXIT SIGN OVER COCKPIT DOOR IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLEY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999091000544 19990910 00544 EU 1999 9 10 QXEA9901683 1 19990903 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 481US 11230 GEG- CENTER AISLE ROW 8 EXIT SIGN HAS INOPERATIVE LIGHTS. REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999091000545 19990910 00545 NM 1999 9 10 99FDEA00364 1 19990903 A 2612 FIRE BELL BOEING 727 7272S2F 1384O81 NM CARGO COMPT SOUNDED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 211FE 22933 AT FLT LEVEL 270, ENG FIRE WARNING BELL SOUNDED AND EXT 2 TIMES. FIRE WARNING MAIN CARGO SMOKE AND GROUND FAULT DET SYS CHECKED GOOD. CONNECTORS CHECKED AND CLEANED ON FIRE AND OVHT DET MODULE. ENG FIRE WARNING TEST PER MM 26-11-001-5. S YS CHECKED SERVICEABLE. 2 L 7 3 4F A3WE 1999091000546 19990910 00546 WP 1999 9 10 99FDEA00365 1 19990901 A 5350 ARB7105501 FILLET DOUG DC10 DC1030F 3023504 WP LT WING/FUS MISSING A FDEA K NONE D INFLIGHT SEPARATION CL CLIMB 1 SO 25 311FE 46871 PIECE OF AC LOST ON T/O ROTATION. LEFT SLAT TO FUSELAGE FILLET DEPARTED A/C. INSP FUSELAGE AFT OF MISSING PERFORMANCE FAIRING NO DAMAGE NOTED. ALSO INSPECTED NR 2 ENG INTAKE WITH NO DAMAGE NOTED. REMOVED AND REPLACED CLOSE-OUT STRIP OF I/B 1L SLAT UPON INSPECTION. REPLACED LOWER FAIR MT FITTING IAW DC10 SRM 51-33-01. 2 L 7 3 4F RT A22WE 1999091000547 20000613 00547 NM 2000 6 13 99FDEA00366 1 19990908 A 5347 S4929148 SEAT TRACK DOUG MD11 MD11F 3023600 NM CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 613FE 48749 SNRM 419 MAIN DECK FORWARD CABIN DOOR WAY SEAT TRACK AT BS 655 FOUND CRACKED, X=107-25. CRACK LENGTH APPROX 1 INCH. ** S/D ** AREA SMOOTH AND PROTECTED AS PER SRM 51-21-01 VOL 2. NDT INSP CARRIED OUT. NO CRACK EVIDENT. 2 L 7 3 4F RT A22WE 1999091000548 19990910 00548 EU 1999 9 10 99FDEA00367 1 19990907 A 3232 A5383194420400 FITTING AIRBUS 310 A310222 3930315 EU RT MLG DOOR ACT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 449FE 217 TWO MAIN CROSSBEAMS THAT RUN ACROSS THE LANDING GEAR BAY AND HOLD BOTH MLG DOOR ACTUATORS UPPER ATTACH ARE BROKEN. RT M LG DOOR ACTUATOR ATTACH FITTING WAS PULLED AWAY FROM MAIN CROSSBEAM. *S/D* REPAIRED PER EA 6-5310-42321. 2 L 7 2 4F RT A35EU 1999091000549 19990910 00549 WP 1999 9 10 99FDEA00368 1 19990831 A 5347 S4929147 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 MAIN DECK UPPER FUSELAGE, CRACK FOUND ON SEAT TRACK AT BS 635 X=27.5 LH-687. MAIN DECK UPPER FUSELAGE CRACK ON SEAT TRA CK AT BS 635 X=75.25 RH-688. MAIN DECK CRACK ON SEAT TRACK AT BS 775X=8.5 RH-700. *S/D* REPAIRED SEAT TRACKS 687, 688 , 700 AS PER SRM 53-70-00 FIG 1, VOL 1. 2 L 7 3 4F RT A22WE 1999091000550 19990910 00550 WP 1999 9 10 99FDEA00369 1 19990906 A 7830 TR COWL DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE DEPARTED A FDEA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SO 25 310FE 48299 NR 2 ENGINE THRUST REVERSER TRANSLATING COWL DEPARTED THE A/C ON LANDING. *S/D* REMOVED AND REPLACED NR 2 RT T/R FAN I AW MM 78-32-11-2. 2 L 7 3 4F RT A22WE 1999091000551 19990910 00551 NM 1999 9 10 99FDEA00370 1 19990903 A 5530 FITTING DOUG MD11 MD11F 3023600 NM VERT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 DURING EDDY CURRENT INSP ON RT BANJO NR 4 FOUND INNER FWD FLANGE WITH .5 INCH CRACK AT RADIUS AREA FWD CTR FASTENER HOLE DIA 0.371 IN AND LWR FWD FASTENER HOLE DIA 0.325 IN WITH SHORT EDGE MARGIN AND CRACK=FREE COND-585., FOUND FOR UPPER AN D LWR FASTENER HOLE WITH CRACKS AND ALL 3 FWD HOLES LARGER THAN 0.275 DIA. -600. *S/D* REPAIRED AS PER EA 1-5530-47423 . 2 L 7 3 4F RT A22WE 1999091000552 19990910 00552 NE 1999 9 10 99UAL900442 2 19990828 A 7532 1115V0315 BLEED VALVE JANITROL AER 1115V07004 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 648UA 25285 724671 NR 1 ENGINE NACELLE OVERHEAT. *S/D* ENGINE 2.95 STABILITY BLEED VALVE WAS OPEN ON TAKEOFF. REPLACED 2.95 STABILITY BL EED VALVE, 2.95 BLEED SOLENOID AND 2.95 BLEED PNEUMATIC RELAY VALVE. SOLENOID AND RELAY VALVES TESTED OK. THE 2.95 BLE ED VALVE WAS FOUND LEAKING AT THE PISTON RING SEALS PW75-130, WHICH IS ACCOMPLISHED AT VALVE OVERHAUL IMPROVES VALVE PIS TON RING SEALS. 2 L 7 2 4F 4 F RT A1NM E24NE 1999091000553 19990910 00553 NM 1999 9 10 99UAL900447 1 19990825 A 2120 AIR DIST 5XA00503300 AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE COCKPIT ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 810UA 843 FLIGHT EN ROUTE TO YVR, CREW DISCOVERED A HEATED PANEL AFT OF CB PANEL 49VU. *S/D* ACTUAL ODOR WAS NOT CONFIRMED. AS PRECAUTION, LIGHT BALLAST FIN NR 6LF WAS REPLACED AS WELL AS THE RECIRCULATION FAN FILTERS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999091000554 19990910 00554 1999 9 10 99UAL900448 4 19990826 A 2564 7A147913 TUBE BF GOODRICH 7A14805 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE/RAFT TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 11874 38 G1863 26892 SLIDE/RAFT (P/N 7A1479-13) (S/N G1863) FAILED FLAT FIRE INFLATION TEST. UPPER INFLATION TUBE RUPTURED AT THE TOP RT COR NER. THIS IS THE FIRST UAL SHOP VISIT FOR THIS UNIT. DATE OF MANUFACTURE WAS 4/96 AND LAST OVERHAUL BY VENDOR WAS 5/30 /96. *S/D* PROBABLE CAUSE FOR THE FAILURE IS PACKING DAMAGE BETWEEN TUBE MATERIAL AND THE INFLATE/DEFLATE VALVE. SENT UNIT TO VENDOR FOR WARRANTY REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 1999091000555 19990910 00555 NE 1999 9 10 99UAL900452 2 19990828 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FAILED A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 WP 29 538UA 6026 25222 717947 RETURNED TO LAX DUE TO A NR 2 ENGINE VIBRATION. FOUND METAL IN THE TAIL PIPE AND THE ENGINE WAS REPLACED. SHOP FINDING S WERE A FAILED 4TH STAGE LPT VANE. CAUSE WAS HEAVY SULFIDATION, AND PARTS WERE RETURNED TO PWA FOR INVESTIGATION. 2 L 7 2 4F 4 F RT A2NM E17NE 1999091000556 19990910 00556 1999 9 10 99UAL900453 4 19990829 A 3130 17M303266 FLIGHT RECORDER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 996UA 22456 CREW REPORTS A BURNING SMELL IN THE AFT GALLEY AREA. *S/D* THE SMELL WAS FOUND TO BE COMING FROM THE FLIGHT DATA RECO RDER. REPLACED THE FLIGHT DATA RECORDER. NO DAMAGED WIRING OR SIGNS OF FIRE WERE FOUND IN THE VICINITY OF THE RECORDER . 2 L 7 2 4F 4 F A16WE E2EA 1999091000557 19990910 00557 NM 1999 9 10 99UAL900454 1 19990820 A 2120 AIR DIST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT ODOR A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7466U 21920 RETURNED TO GATE DUE TO ARCING ODOR IN COCKPIT. CLICKING STATIC ON RADIO. WINDSHEAR INOPERATIVE FAILURE LIGHT STARTED TO FLICKER. ON WAY BACK TO GATE SMOKE BEGAN TO COME FROM UNDER THE INSTRUMENT PANEL. RAN ENGINES WITH ALL SYSTEMS OPER ATING, LOOKED BEHIND INSTRUMENT PANEL (FE'S PANEL) AND E/E COMPARTMENT. NO DEFECTS NOTED. UNABLE TO DUPLICATE SMELL ON GRND. TEST FLT TO VERIFY OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1999091000558 19990910 00558 NM 1999 9 10 99UAL900455 1 19990828 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 7 DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7281U 21559 EMERGENCY EXIT LIGHT IN CABIN TO OVERWING IS INOPERATIVE. REPLACED ROW 7 BATTERYS IN EMERGENCY LIGHT. OPERATIONALLY CH ECKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999091000559 19990910 00559 NM 1999 9 10 99UAL900456 1 19990831 A 5210 SEAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE PAX DOOR FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 909UA 25009 DOOR ONE LEFT PRESSURE SEAL FOUND LEAKING AND MAKING NOISE. FOUND LOWER HINGE COVER SEAL DISTORTED. REPLACED LOWER HI NGE SEAL AND PRESSURIZED TO 5 PSI WITH NO LEAKS NOTED ON DOOR. 2 L 7 2 4F 4 F RT A16WE E2GL 1999091000560 19990910 00560 NM 1999 9 10 99UAL900457 1 19990901 A 3350 LIGHT BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE ROW 15 INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 991UA 21981 EMERGENCY EGRESS FLOOR LIGHTING AT ROW 15 THRU 18 INOPERABLE. REPLACED LIGHTING FEEDER STRIP, OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1999091000561 19990910 00561 NM 1999 9 10 99UAL900458 1 19990902 A 2530 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY SMOKING A UALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 603UA 21864 FWD GALLEY OVEN SMOKING WITH ELECT SMELL. 2 L 7 2 4F 4 F RT A1NM E3NE 1999091000562 20001010 00562 NE 2000 10 10 99UAL900459 2 19990902 A 7230 6A4254 BLADE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE STAGE 4 FAILED A UALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 WP 29 818UA 3429 882 V10419 RETURNED TO SFO DUE TO NR 1 ENGINE FAILURE. *S/D* STAGE 4 BLADE FAILED IN FATIGUE IN ROOT ATTACHMENT AREA, LIBERATING AIRFOIL AND PLATFORM AND CAUSING EXTENSIVE DOWNSTREAM DAMAGE. THE MANUFACTURER HAS ISOLATED THE CAUSE TO A VSV SCHEDULE INTRODUCED WITH EEC SOFTWARE CHANGE NR 11. EEC SOFTWARE WILL BE REVISED TO REVERT TO PREVIOUS VSV SCHEDULE. A SERVICE BULLETIN IS EXPECTED IN APRIL OF 2000. 2 L 7 2 4F 4 F RT A28NM E40NE 1999091000563 19990910 00563 NM 1999 9 10 99UAL900460 1 19990903 A 2150 ROLLERS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT PACK OUT OF POSITION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 799UA 26926 EN ROUTE SFO-CDG DURING CLIMB, CREW REPORTED HEAVY VIBRATION COMING FROM LEFT SIDE OF AIRCRAFT AROUND ROW 12. TURNED OF F LEFT PACK AND VIBRATION DECREASED CONSIDERABLY. *S/D* THE LEFTHAND RAM AIR INLET DOOR ROLLERS WERE FOUND OFF THE ROL LER TRACKS. THE ROLLERS WERE PUT BACK ON TRACK ACCORDINGLY AND THE RAM AIR DOOR ASSEMBLY WAS OPERATIONALLY CHECKED. T HE AIRCRAFT WAS RETURNED TO REVENUE SERVICE WITH NO FURTHER INCIDENT REPORTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999091000564 19990910 00564 WP 1999 9 10 ABXA9900682 1 19990820 A 5312 5910130392 BULKHEAD TEE DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND A CRACK INDICATION IN THE AFT PRESSURE BULKHEAD NR 6 TEE CAP. REPAIRED IAW ABX EA 53-120037-006. 2 L 7 2 4F A6WE 1999091000565 19990910 00565 WP 1999 9 10 ABXA9900683 1 19990820 A 5744 5912547501 HINGE DOUG DOUG DC9 DC931 3022065 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND LEFT AILERON INBOARD HINGE FITTING CRACKED AT SPAR MOUNT HOLE. REPLACED HINGE IAW DACO DWG 591051 5. 2 L 7 2 4F A6WE 1999091000566 19990910 00566 WP 1999 9 10 ABXA9900684 1 19990823 A 5320 39570831 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND FITTING CRACKED BELOW LONGERON 16 LEFT ON THE AFT SIDE OF STATION 1076 FRAME. REPLACED FITTING IA W DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999091000567 19990910 00567 WP 1999 9 10 ABXA9900685 1 19990823 A 5311 59135956 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND FRAME CRACKED AT STATION 1076 AND LONGERON 13 RIGHT. REPLACED SECTION OF FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999091000568 19990910 00568 WP 1999 9 10 ABXA9900686 1 19990819 A 5312 9915558239N FRAME DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND OUTBOARD END OF THE AFT PRESSURE BULKHEAD FRAME CRACKED AT LONGERON 15 LEFT. REPAIRED IAW DC9 SRM 51-30-5 AND 51-20-0. 2 L 7 2 4F A6WE 1999091000569 19990910 00569 NM 1999 9 10 SCNA99723 1 19990822 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 315 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS IN THE LOWER NOSE COMPARTMENT, INSIDE THE RT NOSE LAND ING GEAR WALKWAY AT STA 315 BETWEEN STRINGER 26 AND 27R EXTENDING UPWARD TO FRAME WEB. REMOVED CORROSION IAW B727 SRM 5 11006. MATERIAL ID PER B727 SRM 531002 AS 7075 T6 .045C. TRIMMED DAMAGE IAW B727 SRM 531004. FABRICATED REPAIR DOUBLE R FROM 7075 T6. TREATED AND PRIMED IAW B727 SRM 512002 AND MM 511002. INSTALLED IAW B727 SRM 513002 AND 531004. 2 L 7 3 4F RT A3WE 1999091000570 19990910 00570 SO 1999 9 10 SWIA971547 1 19990807 A 3097 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DE ICE SYS CHAFED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 189SW 120048 ICE BOOTS IN TIMERS 1 AND 2 FAILED IN LIGHT MODE. HEAVY MODE WAS OK. RETURNED TO SLC. INSPECTED DEICE SYSTEM. FOUND CHAFED WIRE ON DEICE VALVES. REPAIRED WIRES AS REQUIRED PER STP 20-0-00 AND OPS CHECK SYSTEM PER MM 20-00-00. OPS CHEC KS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999091000571 19990910 00571 1999 9 10 SWIA971548 3 19990807 A 6140 NP PROB EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1 ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 227SW 120304 NUMBER ONE NP GAUGE FLUCTUATED FROM 85 PERCENT NP TO 35 PERCENT NP IN CRUISE FLIGHT (BOTH DIGITAL AND ANALOG INDICATIONS ). NO OTHER ENGINE INSTRUMENTS WERE ABNORMAL. RETURNED TO LAX. REPLACED LEFT ENGINE NP PROBE AND NP INDICATOR. OPS C HECKS GOOD. RAN AT CRUISE POWER SETTING AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999091000572 19990910 00572 SO 1999 9 10 SWIA971549 1 19990801 A 5246 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL SYST NOT LATCHED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 193SW 120088 AIRCRAFT RETURNED TO FIELD FOR SERVICE DOOR LIGHT. SECURED LATCH ON INBOARD FUEL DOOR. NO OTHER APPARENT DAMAGE OR DEF ECTS, OPS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999091000573 19990910 00573 SO 1999 9 10 SWIA971550 1 19990801 A 3411 PITOT TUBE EMB 120 EMB120RT SO PWA 118 PW118A NE NR 3 MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 250YV 120250 CAPTAINS AND FIRST OFFICERS ALTIMETERS OFF BY UP TO 300 FEET. RETURNED TO SEA. REMOVED AND REPLACED FIRST OFFICERS ALT IMETER IAW MM. REMOVED AND REPLACED FIRST OFFICERS NUMBER THREE PITOT TUBE IAW MM 34-11-00. PERFORMED PITOT STATIC TES T IAW MM 34-12-31. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999091000574 19990910 00574 SO 1999 9 10 SWIA971551 1 19990801 A 2750 12042642507 CONTROL HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 298SW 120328 AFTER TAKEOFF, WHEN FLAPS SELECTED UP, INBOARD FLAP PAIRS IN DISAGREEMENT WITH OUTBOARD AND NACELLE. QUICK REFERENCE HA NDBOOK PROCEDURE INEFFECTIVE. OPERATES NORMAL ON GROUND AFTER RETURNING TO SJC. REPLACED FLAP CONTROL HANDLE AND RERAC KED FLAP CONTROL UNIT. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999091000575 19990910 00575 NE 1999 9 10 SWIA971552 2 19990801 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RIGHT FAILED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 ON CLIMB AT 1000 FT, RIGHT ENGINE TORQUE ROSE UNCOMMANDED TO APPROXIMATELY 124 PERCENT. PROP NP WAS APPROXIMATELY 100 P ERCENT, T6 BELOW 800 FT. ALL OTHER PARAMETERS NORMAL AND EEC WARNING ENSUED. CHECK LIST CALLED FOR EEC SWITCH TO MANUAL AT WHICH TIME CONTROL OVER ENGINE WAS RETAINED TO POWER LEVER, TORQUE REMAINED 124 PERCENT FOR 10-15 SECONDS. RETURNED TO SFO. RIGHT ENGINE TORQUE IS WITHIN LIMITS AS PER PRATT AND WHITNEY ENGINE MM 05-10-00, PAGE 8 FIGURE 2. PERFORMED ENGINE RUN. FOUND RIGHT EEC FAILED, WON'T RESET. DEFERRED RIGHT EEC AS PER MEL 73-21-1. 2 L 7 2 4T 4 T RT A31SO E20NE 1999091000576 19990910 00576 SO 1999 9 10 SWIA971553 1 19990909 A 3230 UPLOCK SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG OUT OF POSITION A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 RIGHT MAIN WOULD NOT RETRACT. RETURNED TO WYS. INSPECTED LEFT AND RIGHT MAIN LANDING GEAR RIGGING, FOUND NORMAL. ADJU STED RIGHT UPLOCK SENSOR STRIKER TARGET IN 1/2 TURN. CYCLED GEAR, ALL INDICATION AND OPERATION NORMAL PER MM 32-30-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999091500001 19990915 00001 NE 1999 9 15 99ZZZX3021 2 19990727 A 7320 418186001 PY LINE BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE ENGINE FUEL CRACKED C A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 05 143CF 47506 LE47014AE THIS PY AIR LINE CRACKED AND CAUSED SUDDEN DECELERATION. PILOT MADE NORMAL SINGLE ENGINE LANDING WITHIN PUBLISHED OEI L IMITATIONS. VIBRATIONS WERE RECORDED ON MAIN DRIVESHAFT. THE ENGINE ASSY AND MAIN DRIVE SHAFT WERE REPLACED. 1 G 7 2 3U 3 U H9SW E5NE 1999091500002 19990915 00002 NE 1999 9 15 SWAA991353 2 19990812 A 7320 1853M56P06 HMU BOEING 737 7377H4 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE FAILED A SWAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 07 704SW 27838 874259 DURING CLIMB WITH 99.7 PERCENT N1 POWER EXPERIENCED ENGINE VIBRATION, NR 2 ENG THRUST LEVER ALSO VIBRATED, REDUCED N1 TO 99 PERCENT AND VIBRATION WENT AWAY. REMOVED AND REPLACED NR 2 ENG HMU PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 1999091700001 19990917 00001 EU 1999 9 17 JBXA9900103 1 19990909 A 2720 SWITCH FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU RUDDER FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 105ML 11475 FLT 220 RDU/MCO ON CLIMBOUT HAD A RUDDER NR 2 FAULT. AIR RETURN TO RDU. PERFORMED OPS CHECK OF RLMU IAW 27-23-01, NO F AULTS NOTED ON GROUND. GROUND OPERATED ENGS AND PUT RUDDER IN SEVERAL CONFIGURATION AND NO FAULTS FOUND. REMOVED AND R EPLACED ACTIVE RUDDER MANIFOLD PRESS SWITCHES IAW 27-22-05. 2 L 7 2 4F 4 F RT 1999091700002 19990917 00002 SO 1999 9 17 COMA9910144 1 19990907 A 5713 12016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 120247 DURING COMPLIANCE OF 1C TASK 28-01, THE LEFT WING STRINGER NR 10 WAS FOUND CRACKED AT FASTENER HOLE LOCATION APPROXIMATE LY SIX INCHES INBOARD OF RIB NR 8. THE CRACK WAS REPAIRED PER EMB120 SRM 57-20-03, FIGURE 201 AND EMBRAER REPAIR NR SST -2296/99, DATED SEPTEMBER 7, 1999. 2 L 7 2 4T RT A31SO 1999091700003 19990917 00003 SO 1999 9 17 COMA9910145 1 19990907 A 2751 WARNING EMB 120 EMB120RT SO TE FLAPS ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 159A 120159 FLAP CONTROL FAULT WARNING. COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. 2 L 7 2 4T RT A31SO 1999091700004 19990917 00004 NE 1999 9 17 COMA9960493 2 19990907 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FAILED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 933CA 7040 807077 OILY SMELL FROM LEFT HAND ENGINE BLEED AIR. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999091700005 19990917 00005 EA 1999 9 17 COMA9960494 1 19990907 A 2150 WARNING CNDAIR CL600 CL6002B19 EA LT PACK ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 710CA 7241 LEFT HAND AIRCRAFT PACK HIGH PRESSURE WARNING. COULD NOT DUPLICATE. OPERATIONAL CHECK OF SYSTEM WAS NORMAL. 2 L 7 2 4F RT A21EA 1999091700006 19990917 00006 EA 1999 9 17 COMA9960495 1 19990908 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA ROW 2 FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 975CA 7150 EMERGENCY LIGHT ROW 2 IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999091700007 19990917 00007 EA 1999 9 17 COMA9960496 1 19990908 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 918CA 7018 LANDING GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 1999091700008 19990917 00008 EA 1999 9 17 COMA9960497 1 19990908 A 7830 22850775101 SPRING 2285020013 CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT TR UNIT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 014 7013 807038 WHILE PERFORMING A MAINTENANCE SERVICE CHECK 50 HOUR INSPECTION MECHANIC FOUND A BROKEN BLOCKER DOOR (P/N 228-50219-111) ON THE LEFT ENGINE THRUST REVERSER, VISIBLE FROM THE GROUND. FURTHER INVESTIGATION FOUND PROBABLE CAUSE TO BE TWO BROK EN RETURN SPRINGS (P/N 228-50775-101), WHICH CAUSED DOOR NOT TO RETURN IN PROPER SEQUENCE. REMOVED BROKEN SPRINGS AND D OOR, REPLACED WITH SERV PARTS IAW CANADAIR MMC NR 78-33-11 AND 78-33-21. 2 L 7 2 4F 4 F RT A21EA E15NE 1999091700009 19990917 00009 EA 1999 9 17 COMA9960498 1 19990905 A 5320 601R530312 CLEAT CNDAIR CL600 CL6002B19 EA BS 484 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 7080 CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 HAS AN APPROXIMATELY 0.75 INCH CRACK IN THE RADIUS. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 IAW WVAC EO 601R-53-0312B. 2 L 7 2 4F RT A21EA 1999091700010 19990917 00010 EA 1999 9 17 COMA9960499 1 19990905 A 5320 601R530312 CLEAT CNDAIR CL600 CL6002B19 EA BS 484 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 7080 CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 HAS AN APPROXIMATELY 0.75 INCH CRACK IN THE RADIUS. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 IAW WVAC EO 601R-53-0312A. 2 L 7 2 4F RT A21EA 1999091700011 19990917 00011 EA 1999 9 17 COMA9960500 1 19990905 A 3231 601R751461 VALVE CNDAIR CL600 CL6002B19 EA NLG DOORS MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 988CA 4246 7204 LOUD PULSATING SOUND FROM NLG AREA. REPLACED THE NLG DOORS SELECTOR VALVE. 2 L 7 2 4F RT A21EA 1999091700012 19990917 00012 EA 1999 9 17 COMA9960501 1 19990904 A 3260 864202 SENSOR CNDAIR CL600 CL6002B19 EA LT MLG FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 7014 LEFT HAND MLG DISAGREE WARNING. REPLACED THE LEFT HAND MLG UPLOCK PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 1999091700013 19990917 00013 NM 1999 9 17 QXEA9901681 1 19990902 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 360PH 515 PDX - LIGHT BULBS INOPERATIVE AT FLIGHT ATTENDANT'S EMERGENCY LIGHT SWITCH. RESEATED CONNECTOR FOR FLIGHT ATTENDANT'S E MERGENCY LIGHT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999091700014 19990917 00014 EU 1999 9 17 QXEA9901854 1 19990906 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU ROW 8E INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 GEG - EMERGENCY LIGHT OVERHEAD OF ROW 8E INOPERATIVE. REPLACED CIRCUIT BOARD, OPERATIONAL TEST CHECKS GOOD. 2 L 7 2 4F RT A20EU 1999091700015 19990917 00015 NM 1999 9 17 QXEA9901855 1 19990903 A 6123 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTO FEATHER SYS DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PDX - NO AUTO FEATHER ARM LIGHT ON TAKEOFF ROLL. INSPECTED AND CLEANED POWER LEVEL SWITCHES G121-S6 AND S7. COMPLIED W ITH FUNCTIONAL TEST OF POWER LEVEL SWITCHES AND AUTO FEATHER SYSTEM. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PA RTS REPLACED. 2 H 7 2 4T RT A13NM 1999091700016 19990917 00016 NM 1999 9 17 QXEA9901856 1 19990904 A 6123 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTO FEATHER SYS OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 361PH 516 PSC - AUTO FEATHER DID NOT ARM. CLEANED AND INSPECTED CONTROL QUADRANT SWITCHES. ADJUSTED NR 1 AND NR 2 AUTO FEATHER A RMING POTENTIOMETER. GROUND RUN OK. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999091700017 19990917 00017 NM 1999 9 17 QXEA9901857 1 19990907 A 3350 6104789 BATTERY DHAV 82410162007 DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 357PH 3519 504 SEA- REAR CABIN OVERHEAD EMERGENCY LIGHTS STOP WORKING AFTER 10 SECONDS. REMOVED AND REPLACED BATTERY. OVERHEAD EMERGE NCY LIGHT OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999091700018 19990917 00018 NM 1999 9 17 99FDEA00371 1 19990907 A 3260 DNLOCK SWITCH BOEING 727 72725C 138400H NM NLG INOP A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 116FE 19298 LANDING NOSE GEAR IND DOWN THEN WHEN GEAR DOOR LIGHT EXT NOSE GEAR LIGHT WENT OUT. ALL LANDING DOWNLOCK PINS INSTALLED. REMOVED AND REPLACED LANDING ANNUNCIATOR PNL. REPLACED NOSE GEAR DOWNLOCK SWITCH PER AMM 32-61-021-4 & CONNECTOR D298 PER SMP. SYS OPS CK GOOD. 2 L 7 3 4F A3WE 1999091700019 19990917 00019 NM 1999 9 17 99FDEA00372 1 19990908 A 5243 6556235159 DOOR BOEING 727 727233 138408A NM HYD SERVICE BAY MISSING A FDEA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 25 276FE 22041 AT FLT LEVEL 250, 340 IND AIR SPEED, DEPLOY SPEED BRAKE SLIGHTLY AND CHANGING THROTTLE POSITION HAD NO EFFECT. FOUND HY D SERVICE DOOR MISSING. FAB NEW CVR PNL FOR DOOR AS PER ENG AUTH NR 7-5350-47517. AC OK TO CONTINUE ONE FLT LEG. 2 L 7 3 4F RT A3WE 1999091700020 19990917 00020 WP 1999 9 17 99FDEA00373 1 19990908 A 3260 TARGET DOUG DC10 DC1010F 3022111 WP RT MLG INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 385FE 46619 WHEN GEAR RAISE AFT TO, RMG REMAIN RED. COMPLIED WITH RED TAB CK LIST RECYCLING GEAR STILL HAD BOTH RT MAIN RED LIGHT W ITH GEAR HANDLE UP. REMOVED AND REPLACED TARGET PER MM 32-61-03-2 RF EA 8-3260-47519. AC OK FOR SERVICE. 2 L 7 3 4F A22WE 1999091700021 19990917 00021 WP 1999 9 17 ABXA9900687 1 19990804 A 5311 5616734513 FRAME DOUG DOUG DC8 DC862 3021970 WP BS 1114.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 804AX 95987 CHANNEL FRAME CRACKED AT STATION 1114.5, NR 3 CARGO COMPARTMENT. REPAIRED IAW ABX REA D853-31931MR. 2 L 7 4 4F 4A25 1999091700022 19990917 00022 WP 1999 9 17 ABXA9900688 1 19990809 A 5730 5611350525 SKIN DOUG DOUG DC8 DC862 3021970 WP WS 69.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 804AX 45987 LEFT WING UPPER INBOARD AFT SKIN PANEL HAD A CRACK ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW ABX REA D857-31961 MR. 2 L 7 4 4F 4A25 1999091700023 19990917 00023 WP 1999 9 17 ABXA9900689 1 19990809 A 5730 5611350526 SKIN DOUG DOUG DC8 DC862 3021970 WP WS 69.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 804AX 45987 RIGHT WING UPPER INBOARD AFT SKIN PANEL HAD CRACK ABOVE REAR SPAR AT STATION XCW 69.5. REPAIRED IAW ABX REA D857-31961M R. 2 L 7 4 4F 4A25 1999091700024 19990917 00024 WP 1999 9 17 ABXA9900690 1 19990902 A 5320 3619434505 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 390 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 LONGERON SPLICE FITTING CRACKED AT STATION 390 AND LONGERON 33 -35 RIGHT. REPAIRED IAW ABX REA D853-32693MR. 2 L 7 4 4F 4A25 1999091700025 19990917 00025 WP 1999 9 17 ABXA9900691 1 19990902 A 5330 5644981 SKIN DOUG DOUG DC8 DC862 3021970 WP BS 240 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 SKIN CORRODED AT STATION 240, BELOW LONGERON 3 LEFT. REPAIRED IAW ABX REA D853-32664MR. 2 L 7 4 4F 4A25 1999091700026 19990917 00026 WP 1999 9 17 ABXA9900692 1 19990903 A 5610 WINDOW DOUG DC9 DC914 3022034 WP LT COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 CAPTAIN'S CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEAR VIEW WINDOW TRACK. OPS CHECKED GOO D. 2 L 7 2 4F A6WE 1999091700027 19990917 00027 NM 1999 9 17 ABXA9900693 1 19990909 A 2612 BACR13CE2 RELAY BOEING 767 767281 1385109 NM FIRE WARNING STICKING A ABXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 23 783AX 23016 DISCRETE FIRE LIGHT ILLUMINATED DURING TAKEOFF, WITH NO OTHER INDICATIONS. AIR TURNBACK TO ILN. FOUND RELAY K693 STICK ING ON P37. REPLACED RELAY. SYSTEM OPS CHECKED GOOD IAW B767 AMM. 2 L 7 2 4F RT A1NM 1999091700028 19990917 00028 WP 1999 9 17 MWEA99595 1 19990903 A 5210 995576311 FRAME DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FORWARD PASSENGER DOOR FRAME BETWEEN BEAMS NR 4 AND NR 5 IS CRACKED. MTC REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 1999091700029 19990917 00029 WP 1999 9 17 MWEA99586 1 19990903 A 5230 59101575 PAN DOUG DC9 DC914 3022034 WP CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 AFT CARGO DOOR PAN AFT EDGE IS CHAFED. MTC REPLACED PAN. 2 L 7 2 4F A6WE 1999091700030 19990917 00030 WP 1999 9 17 MWEA99591 1 19990903 A 5320 591140187 DOUBLER DOUG DC9 DC914 3022034 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 CRACK ON FORWARD WATER SERVICE PANEL DOUBLER LOWER AFT CORNER AND UPPER AFT CORNER. MTC INSTALLED REPAIR DOUBLER PER BO EING TELEX MWX-ORD-99-00076H. 2 L 7 2 4F A6WE 1999091700031 19990917 00031 NM 1999 9 17 SCNA99118 1 19990908 A 3350 LIGHT BOEING 727 7272K3 138400D NM R1 DOOR INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 291SC 22770 DURING A LINE MAINTENANCE CHECK, THE R1 DOOR INTERIOR EMERGENCY EXIT SIGN OVER THE DOOR OPENING WOULD NOT ILLUMINATE WHE N TESTED. REMOVED AND REPLACED THE R1 DOOR INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999091700185 19990917 00185 WP 1999 9 17 TWAA9912302 1 19990909 A 2530 50198A82439 COFFEE MAKER DOUG DC9 DC931 3022065 WP NR 2 FAILED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 986Z 47589 DURING CRUISE GOT A BURNING SMELL FROM NUMBER 2 COFFEE MAKER. REPLACED COFFEE MAKER. CC 3-3-99 MCI. 2 L 7 2 4F A6WE 1999091700186 19990917 00186 NM 1999 9 17 TWAA9912303 1 19990910 A 3397 WIRE BOEING 757 7572Q8 1384972 NM ROW 1-6 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 712TW 27624 FOUND SECTION OF EGRESS LIGHTS OUT ROW 1 THROUGH 6. REPAIRED A BROKEN WIRE. CC01 12-11-99 LAX. 2 L 7 2 4F RT A2NM 1999091700187 19990917 00187 WP 1999 9 17 TWAA9912304 1 19990910 A 3350 010560600 LIGHT DOUG DC9 DC983 3022083 WP ROW 7 LOOSE A TWAA K NONE L NO TEST LD LANDING 1 CE 05 9630A 53561 DURING LANDING, SECTION OF EGRESS LIGHTS AT ROW 7 APPEARED TO BE LOOSE. REPLACED LIGHT SECTION. AC07 7-27-99 JFK. 2 L 7 2 4F RT A6WE 1999091700188 19990917 00188 WP 1999 9 17 TWAA9912305 1 19990910 A 3350 362623 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOP A TWAA K NONE L NO TEST LD LANDING 1 CE 05 991Z 47096 DURING LANDING NOTICED A SECTION OF COACH EGRESS LIGHTS INOP. REPLACED LIGHT STRIP AND BATTERY PACK. CC 7-23-99 STL. 2 L 7 2 4F A6WE 1999091700189 19990917 00189 NM 1999 9 17 HNAA9900119 1 19990912 A 5330 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 151-157 DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 922HA 094 REINSPECT AND EVALUATE APPROX 10 DENTS ON STR 30S, BETWEEN STATIONS X151.6 AND X157.0 FOR PERMANENT REPAIR. ALSO, GENER ATE DMT FOR PERM REPAIR. DEFERED PER DISPOSITION ON 8\14\99 SEQ 29. REPAIRED IAW EO8-53-99-316. 2 H 7 2 4T RT A13NM 1999091700190 19990917 00190 NM 1999 9 17 HNAA9900120 1 19990912 A 5311 85320638 FRAME DHAV DHC8 DHC8102 2809003 NM BS 240 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 922HA 094 FRAME CORRODED AT FRAME LEG JOINT STA X240 STR 31R. REPAIRED IAW EO8-53-99-318. 2 H 7 2 4T RT A13NM 1999091700191 19990917 00191 WP 1999 9 17 AT9900635 1 19990907 A 2560 5917690409 COVER DOUG DC9 DC932 3022066 WP R-1 DOOR BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 R-1 GIRT BAR STOW HOOK BROKEN. REMOVED AND REPLACED R-1 DOOR SLIDE COVER IAW MM 25-61 RII COMPLIED WITH. 2 L 7 2 4F A6WE 1999091700192 19990917 00192 1999 9 17 AT9900638 4 19990827 A 3416 51828007206 ALTIMETER DOUG DC9 DC932 3022066 WP COCKPIT DEFECTIVE A ZZDA K NONE O OTHER DE DESCENT 1 SO 15 849AT 47484 ON DESCENT INTO BOSTON, BOTH ALTIMETERS APPEARED TO BE INOPERATIVE. WHILE DESCENDING TO FL 240, TRIED TO LEVEL AT 240 AN D CAPTAIN ALTIMETER CONTINUED TO FL 215 WHILE FIRST OFFICER CLIMBED TO FL 255 WITH BOTH VSI'S SHOWING LEVEL FLIGHT. REM OVED AND REPLACED AIR DATA COMPUTER AND BOTH ALTIMETERS. PERFORMED PITOT STATIC CHECK AND SELF TEST ON THE EQUIPMENT IA W MM 34-10. AIR DATA COMPUTER P/N OFF 2587400-170 S/N OFF 0611993. FIRST OFFICER ALTIMETER P/N OFF 570-24929-004, S/N OFF 2952. 2 L 7 2 4F A6WE 1999091700193 19990917 00193 EU 1999 9 17 MALA976560 1 19990903 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 076 DURING HEAVY CHECK INSPECTION, DENT ON LEFT SIDE OF FUSELAGE AFT OF ICE SHIELD. MAINTENANCE REPAIRED IAW GENERIC EO NR 53009. 2 L 7 2 4T RT A52EU 1999091700194 19990917 00194 EU 1999 9 17 MALA976561 1 19990904 A 2150 SWITCH SAAB SF340 SF340A 7850100 EU RT ACM FAILED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 119XJ 119 RIGHT LP BLEED CYCLES ON AND OFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RIGHT OVER PRESSURE SWITCH PN 211C119 -136A AMM 36-21-00, RIGHT OVER TEMP SWITCH PN M2001-542, RT ACM AND HEAT EXCHANGER. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999091700195 19990917 00195 1999 9 17 MALA976562 4 19990904 A 3442 CONNECTOR SAAB SF340 340B 7860101 EU RADAR LOOSE A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 456XJ 456 DURING FLIGHT, RADAR WENT INTERMITTENT, THEN INOP, SEEMED TO BE STABILIZATION THAT WAS INOP. IT WOULD ONLY PAINT A THIN PINK STRIP FROM NOSE TO TOP OF SCREEN. MAINTENANCE FOUND CANNON PLUG AT PEDESTAL LOOSE. RESECURED WEATHER RADAR SYSTE M. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999091700196 19990917 00196 1999 9 17 MALA976563 4 19990907 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR MALFUNCTIONED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 521XJ E2346 SLIDE FOR FORWARD LEFT DOOR PARTIALLY DEPLOYED. MAINTENANCE REPLACED FWD PAX DOOR SLIDE IAW AMM 25-60-11. SEC CHECK GO OD. 2 H 7 4 4F RT A49EU 1999091700197 19990917 00197 EU 1999 9 17 MALA976564 1 19990905 A 2910 L38710SA SWIVEL FITTING SAAB SF340 SF340A 7850100 EU MLG FAILED A MALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 15 68XJ 068 HYD CAUTION LIGHT ON, MAIN ACC PRESS 0, HYD QUANTITY 0, EMERGENCY ACC 3000, IB/OB BRAKE PRESSURE REMAINED 3000 UNTIL BRA KE USE ON LANDING. USED EMERGENCY EXTENTION FOR GEAR AS PER QRH. MAINTENANCE REPLACED LT/RT SEP BOLT AND SWIVEL FITTIN G PN L38710SA. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999091700198 19990917 00198 EU 1999 9 17 MALA976565 1 19990907 A 7602 CONDITION LEVER SAAB SF340 340B 7860101 EU LT ENGINE OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 590MA 340B181 CREW NOTED PROP RPM ON LT PROPELLER WELL BELOW TAKEOFF SETTING SHORTLY AFTER V1 ROTATION. RETURNED TO DTW AND ACCOMPLIS HED QRH FOR PROP MALFUNCTION. MAINTENANCE INSPECTED LT CONDITION LEVER RIGGING, FOUND OUT OF RIG, RE-RIGED THE LT CONDI TION LEVER IAW 76-10-00-5 SAAB MM. PERFORMED APR AND PROP OVERSPEED AND PCU HOLD CHECK, MAX RUN CTOT RUNS. OPS CHECK G OOD. 2 L 7 2 4T RT A52EU 1999091700199 19990917 00199 EU 1999 9 17 MALA976566 1 19990908 A 2440 GPU PLUG SAAB SF340 340B 7860101 EU FUSELAGE SMOKING A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 412XJ 340B412 GROUND CREW REPORTED SMOKE FROM GPU PLUG AFTER IT WAS DISCONNECTED, SHUT DOWN AND HAD PLUG LOOKED AT. MAINTENANCE INSPE CTED AFT RT ELECTRICAL COMPARTMENT, BATTERY COMPARTMENT, GPU PLUG AREA. STARTED AS AGAIN WITH POWER CART, NO DEFECTS NO TED. STARTED AIRCRAFT AGAIN WITH BATTERY POWER, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1999091700200 19990917 00200 EU 1999 9 17 MALA9765668 1 19990909 A 3350 6122751 BATTERY BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 513XJ E2329 ON WALKAROUND, FOUND 10 FLOOR TRACK EMERGENCY LIGHTS AND 2 OVERHEAD EMERGENCY LIGHTS OUT. MAINTENANCE REPLACED BATTERY PACK AT POSITION LE11 IAW AVRO AMM CH 33. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999091700201 19990917 00201 EU 1999 9 17 MALA976567 1 19990907 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 420XJ 420 AFTER TURNING BLEEDS ON, NOTICED STRONG ODOR, SIMULAR TO A TAR SMELL, ODOR CONTINUED TO STAY IN COCKPIT UNTIL LANDING. S MELL WAS STRONGEST FROM FA'S JUMPSEAT. MAINTENANCE REPLACED RT ACM IAW SAAB MM 21-00-00. RUN AC BLEED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999091700202 19990917 00202 EU 1999 9 17 JBXA9900104 1 19990909 A 4950 BLEED VALVE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU APU FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 105ML 11475 ON CLIMB-OUT FROM RDU ON FLT 859, CREW REPORTED BLEED NR 1 AND 2 AND APU BLEED FAULTS. REMOVED AND REPLACED NR 2 HIGH P RESS BLEED VALVE IAW 36-11-00, OPS CHECK GOOD. ALSO, PERFORMED FUNCTIONAL CHECK FLT, ALL OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT 1999091700203 19990917 00203 WP 1999 9 17 CALA9901134 1 19990907 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 148 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND COCKPIT RT FLOOR SKIN PUNCTURED AT FS 148, RBL 14. THE PUNCTURED AREA WAS REMOVED AND TWO DOUBLERS WER E INSTALLED IAW SRM 53-10-1, FIGURE 12, SHEET 2. 2 L 7 2 4F A6WE 1999091700204 19990917 00204 WP 1999 9 17 CALA9901135 1 19990907 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 484 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND CENTER FLOORBOARD SUPPORT AT STA 484, RBL 10 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-10-14. 2 L 7 2 4F A6WE 1999091700205 19990917 00205 WP 1999 9 17 CALA9901136 1 19990907 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND SEAT TRACKS CORRODED AT STA 200-237, RBL 22 AND STA 218-234, LBL 22. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 51-30-05, 53-24-0, AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999091700206 19990917 00206 WP 1999 9 17 CALA9901137 1 19990907 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A .75 INCH CRACK IN FORWARD ENTRY DOOR INNER SKIN AT STA 207, LONGERON 15L. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5310-03891 AND EA 9-5314-2-A0482. 2 L 7 2 4F A6WE 1999091700207 19990917 00207 WP 1999 9 17 CALA9901138 1 19990907 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1250 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 4 CRACK IN LT CUSP WEB AT STA 1250, LBL 58. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INST ALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2. 2 L 7 2 4F A6WE 1999091700208 19990917 00208 WP 1999 9 17 CALA9901139 1 19990907 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 636-655 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 10 CRACK IN RT CUSP WEB BETWEEN STA 636 AND 655, RBL 44-54.5. THE CRACKED AREA WAS REMOVED AND A REPA IR WAS INSTALLED IAW SRM 53-01, FIGURE 4, SHEET 3. 2 L 7 2 4F A6WE 1999091700209 19990917 00209 WP 1999 9 17 CALA9901140 1 19990907 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOORBEAM WEB CORRODED AT STA 1338, LBL 54.5. THE CORRODED AREA WAS CUT OUT AND A FILLER AND DOUBLER R EPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4. 2 L 7 2 4F A6WE 1999091700210 19990917 00210 WP 1999 9 17 CALA9901141 1 19990907 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 478-1079 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND RT OB SEAT TRACK CORRODED AT STA 478-788, RBL 58 AND LT O/B SEAT TRACK CORRODED AT STA 1060-1079, LBL 5 8. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 53-05, FIGURES 4F AND 16, 51-30-5, AND 51-30-2. 2 L 7 2 4F A6WE 1999091700211 19990917 00211 WP 1999 9 17 CALA9901142 1 19990907 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 1287-1307 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND TWO FLOOR SUPPORT BRACKETS CORRODED AT FS 1287-1307, LBL 22. ONE BRACKET WAS CLEANED OF CORROSION AND THE OTHER BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999091700212 19990917 00212 WP 1999 9 17 CALA9901143 1 19990907 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 157-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 157, BL 0 - LBL 10 AND STA 157-200, LBL 18. THE FLOOR SUPPORTS WERE REM OVED AND REPLACED IAW SRM 53-14-1, 51-30-2, 51-30-5, 51-30-1, AND 51-30-3. 2 L 7 2 4F A6WE 1999091700213 19990917 00213 WP 1999 9 17 CALA9901144 1 19990907 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOORBEAM LT END FITTING CORRODED AT STA 1174. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5 AND 51-10-3. 2 L 7 2 4F A6WE 1999091700214 19990917 00214 WP 1999 9 17 CALA9901145 1 19990907 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 0.7 CRACK IN LONGERON 3L AT STA 160 AND A 0.6 CRACK IN LONGERON 4L AT STA 160. THE LONGERONS WERE RE PLACED IAW SRM 53-02, FIGURE 18, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999091700215 19990917 00215 WP 1999 9 17 CALA9901146 1 19990907 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1338. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999091700216 19990917 00216 WP 1999 9 17 CALA9901147 1 19990907 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SPPORT CORRODED AT FS 1174, LBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLE D IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1999091700217 19990917 00217 WP 1999 9 17 CALA9901148 1 19990907 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1320 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND RT AFT LAV FLOOR PAN CENTER SUPPORT CORRODED AT FS 1320, RBL 40. A NEW SUPPORT WAS INSTALLED IAW SRM 5 1-10-4, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999091700218 19990917 00218 WP 1999 9 17 CALA9901149 1 19990908 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 168 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 168, BL 0 TO RBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPO RT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11 AND 51-30-5. 2 L 7 2 4F A6WE 1999091700219 19990917 00219 WP 1999 9 17 CALA9901150 1 19990908 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 1174, RBL 22. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A N EW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 1 AND 51-10-3. 2 L 7 2 4F A6WE 1999091700220 19990917 00220 WP 1999 9 17 CALA9901151 1 19990908 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND LOWER FLOOR SUPPORT ANGLE CORRODED AT STA 160, LBL 18-44. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPP ORT ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-1. 2 L 7 2 4F A6WE 1999091700221 19990917 00221 WP 1999 9 17 CALA9901152 1 19990908 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2 CRACK IN FORWARD CARGO DOOR PAN ON LOWER SIDE OF DOOR NEAR NR 2 FRAME. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-4, 51-30-02, AND 51-30-7. 2 L 7 2 4F A6WE 1999091700222 19990917 00222 WP 1999 9 17 CALA9901153 1 19990908 A 5720 SUPPORT DOUG DC9 DC982 3022082 WP WS 189 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2 CRACK INCH LT WING REAR SPAR WEB LOWER SUPPORT JUST O/B OF FLAP I/B HINGE, XRS 189. THE ANGLE SUPP ORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999091700223 19990917 00223 WP 1999 9 17 CALA9901154 1 19990908 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1112-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1112-1309, LBL 54. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 5 1-30-1, 51-10-3, AND 53-05, FIGURE 1A. 2 L 7 2 4F A6WE 1999091700224 19990917 00224 WP 1999 9 17 CALA9901155 1 19990908 A 5280 SKIN DOUG DC9 DC982 3022082 WP NLG DOOR CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND RT FORWARD NLG DOOR CREASED ON OUTER FORWARD UPPER CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 4 AND 51-10-3. 2 L 7 2 4F A6WE 1999091700225 19990917 00225 WP 1999 9 17 CALA9901156 1 19990908 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1137-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND RT FORWARD CARGO FLOOR TRACK CORRODED AT STA 1137-1155, RBL 24. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4, 51-30-1, AND 51-30-2. 2 L 7 2 4F A6WE 1999091700226 19990917 00226 NM 1999 9 17 9903546624 1 19990904 A 3610 7371091 VALVE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 624US 60484 21706 702050 DURING TAKEOFF ROLL, THE NR 1 ENGINE WAS UNABLE TO OBTAIN TAKEOFF EPR WITH THE POWER LEVER AT THE MECHANICAL STOP. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 120 KTS. THE AIRCRAFT THEN RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE NR 1 PNEUMATIC SYSTEM HIGH STAGE BLEED VALVE TO BE MALFUNCTIONING. THE NR 1 PNEUMATIC SYSTEM WAS PLACED ON MEL 36-1 WITH THE HIGH STAGE VALVE LOCKED CLOSED PER DDG. 2 L 7 4 4F 4 F A20WE E3NE 1999091700227 19990917 00227 NE 1999 9 17 9903553265 2 19990820 A 7230 7360077370 BLADE AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A3 NE ENGINE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 365NW 1610 964 733159 DURING AN OVERNIGHT LINE INSPECTION, IT WAS DISCOVERED THAT A SECTION OF A FAN BLADE MID SPAN SHROUD HAD LIBERATED. MAI NTENANCE REPLACED FOUR FAN BLADES. 2 L 7 2 4F 4 F RT A28NM E29NE 1999091700228 19990917 00228 NE 1999 9 17 9903563267 2 19990828 A 7230 7360077360 BLADE AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A3 NE NR 2 ENGINE FAILED A NWAA O OTHER O OTHER CL CLIMB 1 GL 01 367NW 1212 988 733169 DURING CLIMB, THE FLIGHT CREW NOTED A HIGHER ENGINE NR 2 VIBRATION READING THAN NR 1 ENGINE. AT DESTINATION, AIRPORT MA INTENANCE INSPECTION OF NR 2 ENGINE REVEALED A SECTION OF A FAN BLADE MIS SPAN SHROUD HAD LIBERATED. MAINTENANCE REPLAC ED TWO FAN BLADES. 2 L 7 2 4F 4 F RT A28NM E29NE 1999091700229 19990917 00229 WP 1999 9 17 9903579945 1 19990903 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8925E 45840 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1999091700230 19990917 00230 WP 1999 9 17 9903589945 1 19990907 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8925E 45840 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1999091700231 19990917 00231 WP 1999 9 17 9903599926 1 19990905 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP COCKPIT INOP A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 926NW 47425 COCKPIT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700232 19990917 00232 WP 1999 9 17 9903609920 1 19990907 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 942N 47459 DURING PERIODIC CHECK, FORWARD CABIN OVERHEAD EMERGENCY LIGHTS EXTINGUISHED AFTER ONE MINUTE. REPLACED BATTERIES. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700233 19990917 00233 WP 1999 9 17 9903619156 1 19990905 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8915E 45832 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700234 19990917 00234 WP 1999 9 17 9903629154 1 19990904 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING PERIODIC CHECK, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700235 19990917 00235 WP 1999 9 17 9903639902 1 19990405 A 5712 RIB DOUG DC9 DC931 3022065 WP WS 187 235 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 925N 47073 DURING PERIODIC CHECK, RIGHT TRAILING EDGE FLAP PANEL 1682 WAS REMOVED FROM AIRCRAFT. SIX RIBS WERE FOUND WITH CRACKS A T WS 187R - 235R. REPAIRED PER EA 99-164060. 2 L 7 2 4F A6WE 1999091700236 19990917 00236 WP 1999 9 17 9903649154 1 19990809 A 5312 BULKHEAD DOUG DC9 DC914 3022034 WP BS 623 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING PERIODIC CHECK, FOUND RIGHT SLANT PRESSURE PANEL ABOVE MAIN LANDING GEAR WHEEL WELL CORRODED FS 623, WL -55. REP AIRED PER EA 91-169010. 2 L 7 2 4F A6WE 1999091700237 19990917 00237 WP 1999 9 17 9903659912 1 19990725 A 5720 DOUBLER DOUG DC9 DC931 3022065 WP BS 996 935 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING PERIODIC CHECK, CORROSION WAS FOUND ON LOWER SECTION OF FUSELAGE SKIN BETWEEN FS 935 AND 996 AT AFT CARGO DOOR JA MB DOUBLER. REPAIRED PER EA 99-164498. 2 L 7 2 4F A6WE 1999091700238 19990917 00238 WP 1999 9 17 9903669154 1 19990810 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 164 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING PERIODIC CHECK, FOUND .125 INCH CRACK EMANATING FROM FASTNER HOLE AT FS 164, LONGERON 4L. REPAIRED PER EA 91-168 955. 2 L 7 2 4F A6WE 1999091700239 19990917 00239 WP 1999 9 17 9903679758 1 19990812 A 5312 BULKHEAD DOUG DC9 DC941 302207N WP BS 737 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING PERIODIC CHECK, CORROSION WAS FOUND IN RIGHT SLANT PRESSURE PANEL FS 737. REPAIRED PER EA 97-168991. 2 L 7 2 4F A6WE 1999091700240 19990917 00240 WP 1999 9 17 9903689912 1 19990727 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING PERIODIC CHECK, .5 INCH AND .375 INCH CRACKS WERE FOUND AT LOWER CARGO HOLD BULKHEAD FS 756. REPAIRED PER EA 99- 168926. 2 L 7 2 4F A6WE 1999091700241 19990917 00241 WP 1999 9 17 9903699758 1 19990824 A 5230 DOUBLER DOUG DC9 DC941 302207N WP CARGO DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING PERIODIC CHECK, FOUND CORROSION BETWEEN SKIN AND DOOR DOUBLER. TRIMMED FORWARD CARGO DOOR DOUBLER BETWEEN LOWER FORWARD AND AFT CORNERS PER EA 169077. 2 L 7 2 4F A6WE 1999091700242 19990917 00242 NM 1999 9 17 9903716743 1 19990618 A 5315 FLOOBEAM BOEING 747 747249F 1384849 NM BS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING COMMISSIONING, FOUND CRACK IN UPPER CHORD UPPER DECK FLOORBEAM FS 400, LEFT SIDE. REPAIRED PER EA 67-166837. 2 L 7 4 4F A20WE 1999091700243 19990917 00243 NM 1999 9 17 9903722713 1 19990707 A 5713 LONGERON BOEING 727 7272S7 138407Z NM WS 686 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 716RC 22021 DURING M CHECK, A CRACK WAS FOUND ON THE STRINGER FLANGE ON THE OUTBOARD SIDE OF THE RIB BOLT HOLE OF THE LEFT WING. RE PAIRED PER EA 27-167908. 2 L 7 3 4F A3WE 1999091700244 19990917 00244 NM 1999 9 17 9903732713 1 19990706 A 5311 FRAME BOEING 727 7272S7 138407Z NM BS 760 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 716RC 22021 DURING M CHECK, A CRACK WAS FOUND IN THE FORWARD UPPER HOLE OF FRAME FS 760, WL 202. RBL 70.5. REPAIRED PER EA 27-16790 9. 2 L 7 3 4F A3WE 1999091700245 19990917 00245 NM 1999 9 17 UPS99230589 1 19990831 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1072 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLERS BS 1072 BETWEEN S 17 AND 16 RT. REPAIR CARRIED I AW SRM 53-30-3 FIG 3 A AND EO 99-26-003 UPS ENGINEERING FILE NR 727-30-0011. 2 L 7 3 4F A3WE 1999091700246 19990917 00246 NM 1999 9 17 UPS99230590 1 19990831 A 5720 BRACKET BOEING 727 72731C 1384011 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C RT WING, LWR FIXED TE PANEL SUPPORT BRACKET CRACKED AREA AT NR 8 SPOILER CENTER HINGE SUPPORT FITTING. BRACKET REMOVED AND REPLACED IAW SRM 51-10-3 SRM 51-20-1 SRM 51-30-2. 2 L 7 3 4F A3WE 1999091700247 19990917 00247 NM 1999 9 17 UPS99230592 1 19990902 A 5754 RIB BOEING 727 72731C 1384011 NM NR 3 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C NR 3 LE SLAT RIB CRACKED O/B SIDE OF I/B SLAT TRACK. RIB REPAIR CARRIED OUT IAW 57-30-3. 2 L 7 3 4F A3WE 1999091700248 19990917 00248 NM 1999 9 17 UPS99230593 1 19990901 A 5320 BRACKET BOEING 727 72731C 1384011 NM BS 950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C ON REMOVAL OF LT MLG PRESSURE WEB DOUBLER AND BRACKETS ONE BRACKET AT BS 950 BL 60 FOUND TO BE CRACKED . REPLACED ANGLE IAW DRAWING NR 65-89360. 2 L 7 3 4F A3WE 1999091700249 19990917 00249 NM 1999 9 17 UPS99230594 1 19990901 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C ON REMOVAL OF LT PRESSURE WEB REPAIRS IN LT MLG CEILING A SUSPECT CRACK DETECTED ON FRAME AT BS 930 BE LOW S-17. NEW FRAME INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999091700250 19990917 00250 NM 1999 9 17 UPS99230595 1 19990830 A 3211 HOUSING BOEING 727 72731C 1384011 NM RT MLG TRUNION CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C SUSPECT CRACK ON RT MLG TRUNNION BEARING HOUSING. REPAIR CARRIED OUT IAW SRM 20-20-01, MM 32-11-51, O HM 32-10-13 AND MM 32-32-00. 2 L 7 3 4F A3WE 1999091700251 19990917 00251 NM 1999 9 17 UPS99230596 1 19990903 A 3020 BRACKET BOEING 727 72731C 1384011 NM NR 1 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C ENGINE NR 1 NACELLE ANTI-ICE DUCT CRACKED AT ATTACH BRACKET. REPAIR CARRIED OUT IAW SMRO EO 99-26-002 UPS ENGINEERING FILE NR 727-53-2165. 2 L 7 3 4F A3WE 1999091700252 19990917 00252 NM 1999 9 17 UPS99230597 1 19990901 A 5753 SKIN BOEING 727 72731C 1384011 NM RT TE MID FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C RT OUTBOARD MID FLAP, EVIDENCE OF CORROSION ON TE SKIN LWR SURFACE AREA AFT OF NR 8 TEARDROP FAIRING. DAMAGED SKIN REPAIRED IAW SRM 51-40-6 FIG 41. 2 L 7 3 4F A3WE 1999091700253 19990917 00253 NM 1999 9 17 UPS99230598 1 19990906 A 5753 651976918 WING BOEING 727 7272A1 138407F NM 84-5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI NR 4 FLAP TRACK CORRODED AT SPOILER BEAM MOUNT BOLT HOLES AREA AND FWD FITTING MOUNT BOLT HOLE. REPL ACED NR 4 FLAP TRACK. INSTALLATION OF NEW NR 4 TRACK WILL ACCOMPLISHED ON TC NR C57-581-04-3D. 2 L 7 3 4F A3WE 1999091700254 19990917 00254 NM 1999 9 17 UPS99230599 1 19990906 A 5753 651920612 FLAP TRACK BOEING 727 7272A1 138407F NM NR 6 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI NR 6 FLAP TRACK IS CORRODED AT FWD ATTACH LUG AND AT SPOILER BEAM ATTACH POINT. REPLACED NR 6 FLAP T RACK. INSTALLATION OF NEW NR 6 FLAP TRACK WILL BE ACCOMPLISHED ON TC NR C57-581-04-4D. 2 L 7 3 4F A3WE 1999091700255 19990917 00255 NM 1999 9 17 UPS99230600 1 19990816 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 680-740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI SEAT TRACK CORRODED AT BS 680-740 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 660-740 PER SRM 51-30-2 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 1999091700256 19990917 00256 NM 1999 9 17 UPS99230601 1 19990905 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION (C53-224-03.00-01) ON HAT CHANNEL BS 344, RBL 36, WL 208. REMOVED CORROSION, FOUND TO BE O UT OF LIMITS PER SRM 53-10-1. PERFORMED REPAIR AND REPLACED HAT CHANNEL PER SRM 51-30-5, SRM 51-30-6, AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999091700257 19990917 00257 NM 1999 9 17 UPS99230602 1 19990826 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1090 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION (C53-224-01.05-03) ON BS 1090 FLOORBEAM ON TOP AND BOTTOM OF UPPER CHORD, LBL 48-LBL55, WL 208. REMOVED UPPER CHORD OF FLOORBEAM FABRICATED REPAIR PART, DRILLED UP, ALODINED, PRIMED, SEALED AND INSTALLED IAW SR M 53-10-8, 53-10-01, 51-30-02. 2 L 7 3 4F A3WE 1999091700258 19990917 00258 NM 1999 9 17 UPS99230603 1 19990824 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI FUSELAGE AFT SIDE SHEAR TIE AT BS 1166 JUST INBD OF STR 26R HAS CORROSION (C53-111-01.00-03) CORROSIO N OUT OF LIMITS. REMOVE, FABRICATED AND INSTALLED SHEAR TIE. ALL WORK DONE PER SRM 51-10-6, 53-10-1, 51-30-5, 51-30-2 A ND 51-10-2. 2 L 7 3 4F A3WE 1999091700259 19990917 00259 NM 1999 9 17 UPS99230604 1 19990904 A 5313 69144925 STRINGER BOEING 727 72725C 138400H NM BS 485 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION (C53-113-01-00-01) ON STRINGER SPLICE 28 RT BS 485 WL 145. REPLACED STRINGER SPLICE AT BS 485, WL 145 PER SRM 53-10-1, 51-30-2, 51-30-5. 2 L 7 3 4F A3WE 1999091700260 19990917 00260 NM 1999 9 17 UPS99230605 1 19990909 A 5320 WEB BOEING 727 72725C 138400H NM BS 255 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION (C53-221-01.03-01) ON WEB AT BS 255, RBL 49, WL 226 IN THE COCKPIT (MARKED). REMOVED CORRO SION AND REPAIRED PER SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 1999091700261 19990917 00261 NM 1999 9 17 UPS99230606 1 19990909 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON FLOORBEAM UPPER AND LOWER SURFACE AROUND ALL FASTENER HOLES BS 344, W L 208 RBL 25 TO LBL 60. FABRICATED FLOORBEAM (CHORD) FROM 7075-T6 EXTRUSION AND REPLACED SECTION FROM LBL 65 TO RBL 65 WL 208 PER SRM 53-10-8 FIG 5. 2 L 7 3 4F A3WE 1999091700262 19990917 00262 NM 1999 9 17 UPS99230607 1 19990910 A 7120 MOUNT BOEING 727 72731C 1384011 NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C ENGINE NR 3 FWD MOUNT, PITTING CORROSION 4 MOUNT HOLES. NR 3 ENGINE MOUNT FWD MOUNT FITTING HOLES REP AIRED IAW EO NR B727-544 0-11592-A. 2 L 7 3 4F A3WE 1999091700263 19990917 00263 NM 1999 9 17 UPS99230608 1 19990909 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON FLOORBEAM AROUND FASTENER HOLES BS 312, WL 208, LBL 20, LBL 45. REMO VED CORROSION AND REPAIRED PER SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 1999091700264 19990917 00264 NM 1999 9 17 UPS99230609 1 19990910 A 7120 MOUNT BOEING 727 72731C 1384011 NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C ENGINE NR 1 FWD MOUNT PITTING CORROSION ON OUTBOARD ENGINE MOUNT HOLES NR 1 ENGINE FWD MOUNT FITTING O UTBOARD HOLES. REPAIRED IAW EO NR B727- 5440-11592-A. 2 L 7 3 4F A3WE 1999091700265 19990917 00265 NM 1999 9 17 UPS99230610 1 19990909 A 5315 EXTBAC150510024 FLOORBEAM BOEING 727 72725C 138400H NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON FLOORBEAM UPPER CHORD AT BSTA 328, WL 208, LBL 3, LBL 20, LBL 30 AND LBL 45 CORROSION WA S 100 PERCENT THROUGH CHORD FLANGES. REMOVED AND REPLACED UPPER CHORD FROM RBL 34-LBL 65 PER SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 1999091700266 19990917 00266 WP 1999 9 17 UPS99830582 1 19990728 A 5330 FITTING DOUG DC8 DC873F 302199F WP BS 1300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 RT AFT TYPE 1 DOOR FWD TORQUE BOX STA 1300 L12R HAS CORROSION/CRACK. PERFORMED HFEC IAW MIL-SID-271F TO VERIFY CRACK. REMOVED FITTING FROM A/C. LOCATED, DRILLED AND REAMED NEW FITTING IAW DC8 SRM 51-3-2 AND D AC DWG NR 3755819. INSTALLED FRAME FITTING IAW DC8 SRM 51-3-0 AND 51-1 -20D. 2 L 7 4 4F RT 4A25 1999091700267 19990917 00267 WP 1999 9 17 UPS99830583 1 19990826 A 5240 SKIN DOUG DC8 DC873F 302199F WP BS 190 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 5 CRACK IN FUSELAGE SKIN STA 190 AT FWD SERVICE DOOR CUTOUT LWR CORNER. ROUTED OUT DAMAGED SECTION O F SKIN AND FABRICATED AND INSTALLED DOUBLER IAW REO-06671. 2 L 7 4 4F RT 4A25 1999091700268 19990917 00268 WP 1999 9 17 UPS99830585 1 19990731 A 3230 MECHANISM DOUG DC8 DC873F 302199F WP LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 LT MLG BOSS CORRODED. REMOVED CORROSION BY REAMING BOSS DIA 1.8134. RESHOP PEEN DIA 1.838 5 IAW DC8 SRM 32-1-1. MANUFACTURED BUSHING IAW DAC SB NR 32-102. INS TALLED BUSHING AND RETRACT PIN IAW REO 801UP-46-21373 AND DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999091700269 19990917 00269 WP 1999 9 17 UPS99830586 1 19990801 A 5520 ELEVATOR DOUG DC8 DC873F 302199F WP RIGHT LIGHTNING STRIKE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:C3 LIGHTNING STRIKE ON RT ELEVATOR T/E AT STA XE290 GEN RFTS. REMOVED DAMAGED MATERIAL AND ID MAT IAW R EO 06684. FABRICATED AND INSTALLED DOUBLER AND FILLER BOND AND SEAL IAW REO 06684 AND SRM 55-4-0, DC8 MM 27-30-02 AND 2 7-30-03. 2 L 7 4 4F RT 4A25 1999091700270 19990917 00270 WP 1999 9 17 UPS99830588 1 19990909 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:N/A, FUSELAGE SKIN DAMAGE JUST AFT OF THE NLG W/W HAS AN 11 INCH CRACK. DUE TO LEFT NOSE TIRE TREAD SEP ARATION. *S/D* DAMAGE REMOVED AS REQ'D RHODES 75705 RSB 0596 1 QC 2, FABRICATED AND DRILLED DOUBLER PER UPS DRAWING UP S-SDF-9900296 F BPT 92716. OK TO INSTALL RSB 05961 QC3. INSTALLED 98 PERCENT OF FASTENERS IN DOUBLER SEATED EXTERIOR O F DOUBLER, COMPLETE D INTERIM REPAIR. 2 L 7 4 4F RT 4A25 1999091700271 19990917 00271 NM 1999 9 17 99FDEA00379 1 19990910 A 2612 FIRE CONTROL BOEING 727 727233 138408A NM LWR AFT BODY INOP A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 218FE 21101 99-236 - DURING CLIMB, LWR AFT BODY OVHT LIGHT ILLUMINATED NR 2 AND 3 BLEED AIR OPEN, NR 1 CLOSED. REMOVED AND REPLACED OVERHEAT AND FIRE DETECTOR CONTROL BOX. OPER CK SYSTEM PER MM 26-14-011. AC OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1999091700272 19990917 00272 NM 1999 9 17 DLM11991947 1 19990901 A 3840 WATER COMP 8378M11 DOUG MD11 MD11 3023602 NM NR 1 FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 806DE OFF109320 48477 PAX AT 3B NOTICED A HOT WIRE SMELL. THE CREW ALSO NOTICED THE SMELL. LATER F/A AND PASSENGER COMPLAINED OF HEADACHES I NSPECTED CEILING FWD CABIN FOR BURNING WIRE CK OK. CHECKED SIDEWALL OF FWD CRAGO COMP FOUND NR 1 WATER COMP BEARING FAI LURE. REPLACED NR 1 WATER COMP. CKS GOOD. 2 L 7 3 4F RT A22WE 1999091700273 19990917 00273 NM 1999 9 17 DL72W991948 1 19990901 A 3411 400061B45 STATIC LINE BOEING 727 727247 138408F NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 2814W 20870 CAPT'S AIRSPEED INDICATOR FROZE AT 210KTS AT ABOUT 2000 FOO ON CLIMB-OUT. ALTIMETER READINGS CONSISTENTLY LOWER THAN F/ O'S. ALTIMETER READINGS. CADC WOULD NOT RESET. SELECTING ALTERNATE SOURCE DID NOT CORRECT PROBLEM. REPLACED CAP'T A/ S AND ALT STATIC LINES. PUMPED UP SYS-CKS GOOD. 2 L 7 3 4F A3WE 1999091700274 19990917 00274 NM 1999 9 17 DL72S991949 1 19990902 A 3350 900835A BATTERY PACK BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z 21858 RIGHT CENTER OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OP CKS GOOD. 2 L 7 3 4F RT A3WE 1999091700275 19990917 00275 NM 1999 9 17 DL72W991951 1 19990902 A 5320 WEB BOEING 727 727247 138408F NM BS 1260 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FOUND ON F1 LETTER C, .25 INCH CRACK LOWER LIGHTENING HOLE RT VERTICAL TORQUE BOX WEB STA 1260. REPAIRED PER MM 53-11-0 . 2 L 7 3 4F A3WE 1999091700276 19990917 00276 NM 1999 9 17 DL72W991953 1 19990902 A 2782 BRACKET BOEING 727 727247 138408F NM NR 8 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 NR 8 SLAT ACTUATOR I/B AND O/B MOUNT BRACKETS CRACKED ON WEBS. REPAIRED PER M/M 57-20-21 PAGE 812. 2 L 7 3 4F A3WE 1999091700277 19990917 00277 NM 1999 9 17 DL72W991954 1 19990902 A 5754 ANGLE BOEING 727 727247 138408F NM NR 6LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 NR 6 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED ANGLE PER M/M 57-20-21 PAGE 813. 2 L 7 3 4F A3WE 1999091700278 19990917 00278 NM 1999 9 17 DL72S991955 1 19990902 A 5330 65182173 SKIN BOEING 727 727232 1384082 NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 FUSELAGE SKIN FS 360-481, STRG 4L SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BET WEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIR MED 14 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUT OUT AND REPLACED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 368137-14AD. 2 L 7 3 4F A3WE 1999091700279 19990917 00279 NM 1999 9 17 DL72S991956 1 19990903 A 3350 LIGHT 1000677 BOEING 727 727225A 1384077 NM L 2 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z 3724 21858 L-2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED L-2 EMERGENCY EXIT LIGHT ASSY CHECKS OK. 2 L 7 3 4F RT A3WE 1999091700280 19990917 00280 NM 1999 9 17 DL72W991957 1 19990903 A 2782 BRACKET BOEING 727 727247 138408F NM NR 5 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 NR 5 L/E FLAP ACTUATOR I/B MOUNT BRACKET CRACKED BELOW LOWER MOUNT BOLT. REPAIRED PER M/M 57-20-21 PAGE 811. 2 L 7 3 4F A3WE 1999091700281 19990917 00281 NM 1999 9 17 DL72W991958 1 19990903 A 5522 SKIN BOEING 727 727247 138408F NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 RT ELEVATOR LOWER SKIN CRACKED. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1999091700282 19990917 00282 NM 1999 9 17 DL72W991959 1 19990903 A 3297 WIRE 656021132 BOEING 727 727247 138408F NM RT MLG IND FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 293WA OFFR00085S 22111 AFTER GEAR RETRACTION RT GEAR RED AND GREEN LIGHTS REMAINED ILLUMINATED. CREW CYCLED GEAR WITH SAME RESULTS GEAR WAS VE RIFIED VISUALLY TO BE UP AND LOCKED. SHORTLY AFTERWARDS BOTH LIGHTS WENT OUT THEN CAME ON INTERMITTENTLY. A/C DIVERTED TO ATL FOR MTC. REPLACED PINS 1 AND 2 IN D4660 CANNON PLUG. REPLACED WIRES FROM PLUG TO SENSOR. REPLACED LANDING G EAR ACCY BOX AS PRECAUTION. GEAR SWING CK GOOD. 2 L 7 3 4F A3WE 1999091700283 19990917 00283 NM 1999 9 17 DL72S991960 1 19990903 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM RT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 406DA 21150 RT AFT 2 OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS M957 AND M956, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999091700284 19990917 00284 WP 1999 9 17 DLL10991965 1 19990904 A 2120 223101 FAN LKHEED 1011 10113851 5265010 WP COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 735D 193C1226 IRREG HEARD STRANGE FAN LIKE NOISE BEHIND SS/O PANEL FOLLOWED BY SMOKE/FUMES IN COCKPIT. FOUND INSTRUMENT COOLING FAN A T FAULT (CB3 A21 TRIPPED) FAN SIEZED UP FWD TO MCO AND PLAC 21-25-21B C/P TIED BACK. 2 L 7 3 4F A23WE 1999091700285 19990917 00285 NM 1999 9 17 DLM88991968 1 19990904 A 3350 100865 POWER SUPPLY DOUG MD88 MD88 3023688 NM ROW 1-4&10-12 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DL 49583 FOUND EMERGENCY LIGHTS AT DOORS 1L, 2L AND SEATROWS 1, 2, 3, 4, 10, 11 AND 12 INOP. FOUND WIRES AT SEATROW 11 BROKEN AN D REPAIRED SAME, NO HELP. REPLACED POWER SUPPLY B5-211, LIGHTS TEST NORMAL P/N 337701962, S/N 5122. 2 L 7 2 4F RT A6WE 1999091700286 19990917 00286 NE 1999 9 17 DLM88991969 2 19990905 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 27 927DA 21736 49714 726053 NR 2 ENGINE OIL TEMP WENT ABOVE 190 DEG'S FOR 15 TO 20 MINUTES AFTER TAKEOFF. WHEN CREW WENT TO SHUT DOWN ENGINE, ENGIN E DID NOT APPEAR TO BE RUNNING. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999091700287 19990917 00287 NM 1999 9 17 DLM88991970 1 19990904 A 2150 PACK DOUG MD88 MD88 3023688 NM RIGHT MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 969DL 53172 DURING CRUISE FLIGHT, FLIGHT ATTENDANT COMPLAINED OF A BURNING ODOR IN CABIN. DESECENDED AND SHUT OFF THE LEFT A/C PACK WITHIN 1 MIN. THE RIGHT PACK TEMP VLV OPENED TO FULL HOT WITH THE RIGHT PACK TEMP CONTROL IN AUTO. TURNED THE LEFT PA CK ON, TURNED OFF THE RT PACK AND WITHIN 3 MINS THE BURNING ODOR DISSIPATED IN THE CABIN. DID DUCT BURN-OUT PER M/M. C KD OPERATION OF BOTH PACKS, PACK OPERATION NORMAL, REPLACED COALESCER BAGS. 2 L 7 2 4F RT A6WE 1999091700288 19990917 00288 NM 1999 9 17 DL72W991972 1 19990905 A 2121 215201 FAN 215201 BOEING 727 727247 138408F NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 2814W OFFAA77796 20870 JUST PRIOR TO DESCENT INTO TUS, A SLIGHT SMELL OF SMOKE WAS SMELLED IN THE COCKPIT AND BY THE FLIGHT ATTENDENTS IN THE V BACK OF THE CABIN. THE ODOR APPEARED TO BE COMING OUT OF THE GASPERS. THE SMELL OF SMOKE DISSIPATED AFTER A COUPLE OF MINUTES. REPLACED GASPER FAN. 2 L 7 3 4F A3WE 1999091700289 19990917 00289 NM 1999 9 17 DL72W991973 1 19990906 A 3350 BATTERY PACK 900542 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2810W 5006 20648 EMERGENCY LIGHTS DO NOT TEST CORRECTLY. REPLACED BATTERY PACKS. 2 L 7 3 4F A3WE 1999091700290 19990917 00290 NM 1999 9 17 DL72W991974 1 19990906 A 3350 BATTERY PACK 900542 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2810W YA8888 20648 EMERGENCY LIGHTS TEST INOP. REPLACED PACK. 2 L 7 3 4F A3WE 1999091700291 19990917 00291 NM 1999 9 17 DL72S991975 1 19990906 A 2913 PUMP AS19570C BOEING 727 727225A 1384077 NM B HYD SYS FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 8890Z OFFMX241515 21859 HYD SYSTEM B NR 2 PUMP LIGHT CAME ON INTERMITTANTLY THEN STEADY B HYD PRESSURE FLUCTUATED THEN WENT TO ZERO AND LOST SYS TEM B NR 1 HYD PUMP AT THE SAME TIME. A HYD SYSTEM GOOD WITH GOOD PRESSURE. 2 L 7 3 4F RT A3WE 1999091700292 19990917 00292 NM 1999 9 17 DL72S991976 1 19990906 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM L2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532DA 22045 L-2 DOOR OVERHEAD EMERGENCY LT WOULD NOT TEST REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999091700293 19990917 00293 NM 1999 9 17 DL72W991977 1 19990906 A 2121 5007024620 FAN BOEING 727 727247 138408F NM COCKPIT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 2814W 20870 SMOKE IN COCKPIT COMING FROM THE GASPER VENTS. REPLACED GASPER FAN PER M/M. OPS NORMAL. 2 L 7 3 4F A3WE 1999091700294 19990917 00294 NM 1999 9 17 DLM11991978 1 19990906 A 2910 HYD SWITCH DOUG MD11 MD11 3023602 NM NR 2 ENGINE LEAKING A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 814DE 48769 DURING CRUISE, SYSTEM NR 2 HYD QTY WENT TO ZERO. FOUND O-RING PACKING ON LOW PRESS SWITCH RT EDP NR 2 SYSTEM DETERIORAT ED. REPLACED PACKING/SVCD NR 2 HYD SYS/LEAK AND OPS CK NORMAL. 2 L 7 3 4F RT A22WE 1999091700295 19990917 00295 NM 1999 9 17 DL72S991979 1 19990906 A 3350 900835A PACK BATTERY BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 485DA 20865 FOUND MID LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPS CKS GOOD. 2 L 7 3 4F A3WE 1999091700296 19990917 00296 NM 1999 9 17 DLM88991980 1 19990907 A 7930 SWITCH DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 962DL 21083 49981 726051 L OIL STRAINER CLOG MSG AFTER T/O WOULD NOT EXTINGUISH L ENG SHUT DOWN IAW POW 140000 LBS LANDING NORMAL. REPLACED DIFF PRESS SWITCH. REMOVED AND REPLACED MAIN OIL SCREEN RAN ENG CKD GOOD. NO MSG AND NO LEAKS. 2 L 7 2 4F 4 F RT A6WE E9NE 1999091700297 19990917 00297 NM 1999 9 17 DL733991981 1 19990907 A 2130 CONTROL PANEL 7110025 BOEING 737 737347 1384647 NM COCKPIT FAILED A DALA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 27 302WA GA49059 23182 ON DESCENT, AUTO PRESS FAIL MADE UNPRESSURIZED LANDING. REPLACED PRESS CONTROL PANEL. CKS NORMAL. 2 L 7 2 4F RT A16WE 1999091700298 19990917 00298 NM 1999 9 17 DLM88991984 1 19990905 A 3397 WIRE DOUG MD88 MD88 3023688 NM R1 GALLEY DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 975DL 53243 EMERGENCY LIGHTS INOP AT FWD GALLEY. FOUND WIRE PULLED FROM SPLICE UNDER CARPET. RETERMINATED WIRE. CKS GOOD. 2 L 7 2 4F RT A6WE 1999091700299 19990917 00299 NM 1999 9 17 DL72S991985 1 19990907 A 3231 ROD 69295273 BOEING 727 727232 1384082 NM NLG DOOR BROKE A DALA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 27 531DA 21814 AFTER T/O, DURING GEAR RETRACTION, GOT A LOUD SNAP WITH A VIBRATION AND A RED GEAR DOOR ON FWD PANEL AND NLG DOOR LIGHT ON S/O PNL. REPLACED NOSE GEAR ACT ROD. SWUNG NOSE GEAR GEAR AND DOORS OPERATE NORMAL. 2 L 7 3 4F A3WE 1999091700300 19990917 00300 NM 1999 9 17 DL733991986 1 19990907 A 2751 2061141 INDICATOR BOEING 737 737347 1384647 NM TE FLAPS INOP A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 303WA 23183 AFTER T/O FROM SLC, WITH THE FLAPS INTRANSIT FROM 5 DEG TO 1 DEG, THE FLAP GAUGE SHOWED A SPLIT WITH RT FLAP SHOWING 2 D EG AND THE LT FLAP SHOWING 1.5 DEG. THIS CAUSED AN ASYMMETRICAL TRIP. AFTER TALKING WITH ATL MTC AND HAVING THE GAUGE FAIRED WE LANDED NML IN SLC. REPLACED INDICATOR. CHECKED FLAPS FOR CONDITION AND OPERATION. FOUND OK. OPERATED FLAPS SEVERAL TIMES. 2 L 7 2 4F RT A16WE 1999091700301 19990917 00301 NM 1999 9 17 DL72K991987 1 19990907 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM ROW 8-9 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 417DA 21259 EMERGENCY CEILING AREA WHITE LIGHT INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999091700302 19990917 00302 NM 1999 9 17 DL72S991988 1 19990907 A 3350 LIGHT 02019241001 BOEING 727 727232 1384082 NM R1 DOOR DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 405DA 21149 R1 DOOR EMERGENCY EXIT LIGHT DAMAGED. REPLACED EMERGENCY LIGHT ASSY. 2 L 7 3 4F A3WE 1999091700303 19990917 00303 NM 1999 9 17 DLM88991994 1 19990908 A 5330 595305069 SKIN DOUG MD88 MD88 3023688 NM BS 256 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DL 49591 A DENT WAS DISCOVERED IN THE FUSELAGE SKIN AT FS 256 BETWEEN LONGERONS 23L AND 24L. THE DAMAGE WAS FOUND AT HMV AND REP AIRED PER ER/A 333520-14. 2 L 7 2 4F RT A6WE 1999091700304 19990917 00304 NM 1999 9 17 DL757992001 1 19990908 A 2913 731966 HYD PUMP 731966 BOEING 757 757232 1384965 NM NR 1 ENGINE FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 614DL NK415706 22821 NK4157 06T CENTER NR 1 HYD PUMP LOW PRESS FOLLOWED BY PUMP OVHEAT BY LOSS OF CENTER HYD QTY. REPLACED NR 1 HYD PUMP, PUMP BORR OWED FROM UAL. LEAK AND OPS CHK GOOD. 2 L 7 2 4F RT A2NM 1999091700305 19990917 00305 WP 1999 9 17 DLL14992003 1 19990908 A 2913 693980 PUMP LKHEED 1011 1011385115 5265015 WP C HYD SYS CRACKED A DALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 737D 193C1228 HYDRAULIC SYS C QUANTITY GAUGE SLOWLY DECREASED BELOW ONE-HALF INDICATOR MARK. SHUTOFF C1 PUMP AND C2 ATM AS PER POM. Q TY CONTINUED TO DECREASE TO .125 AND LOW QTY LIGHT CAME ON. FOUND C SYS A/C PUMP LEAKING FROM CASE. REPLACED WITH BOR ROWED TWA PART S/N 277295. INSPECTED CASE DRAIN PRESSURE AND RETURN FILTERS CKS GOOD. A/C PUMP OPS AND LEAK CKS GOOD. RESET C1 PUMP MOTORED ENG CKS GOOD. 2 L 7 3 4F A23WE 1999091700306 19990917 00306 NM 1999 9 17 DL767992005 1 19990908 A 5330 146T32212 SKIN BOEING 767 767232 1385132 NM BS 1255-1270 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 105DA 22217 FUSELAGE SKIN FS 1255-1270, STRINGER 38L-39L, CRACK REPAIR. WHILE ACCOMPLISHING REPETITIVE HFEC INSPECTION OF EXISTING SKIN DENTS BETWEEN FS 1255 AND 1260 AND BETWEEN S-38L AND 39L, THREE SMALL CRACKS WERE DETECTED. THE CRACKS WERE CUTOUT OF THE SKIN. AN EXSITING DOUBLER REPAIR WAS ADJACENT TO THIS LOCATION AND REMOVED. THE PREVIOUSLY REPAIRED DAMAGE CU TOUT AND THE NEW DAMAGE CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER PER ER/A 368192-14. 2 L 7 2 4F RT A1NM 1999091700307 19990917 00307 NM 1999 9 17 DL767992006 1 19990908 A 5330 146T32212 SKIN BOEING 767 767232 1385132 NM BS 1270 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 105DA 22217 FUSELAGE SKIN FS 1270 STRINGER 38R, CRACK REPAIR. DURING REPETITIVE HFEC INSPECTION OF AN EXISTING DENT AT FS 1270, NEA R STRINGER 38R, A CRACK WAS FOUND. THE CRACK WAS ROUTED OUT OF THE SKIN WITH A CUTOUT. THE SKIN CUTOUT WAS REPAIRED WI TH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 368195-14. 2 L 7 2 4F RT A1NM 1999091700308 19990917 00308 1999 9 17 DHL99804006 4 19990908 A 2211 25878905 ROLL COMPUTER DOUG DC8 DC873F 302199F WP AUTOPILOT MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 804DH 46124 AUTOPILOT INOPERATIVE. REMOVED AND REPLACED ROLL COMPUTER. 2 L 7 4 4F RT 4A25 1999091700309 19990917 00309 1999 9 17 DHL99366001 4 19990907 A 3425 40042555901 ADI AIRBUS 300 A300B4203 3930306 EU NR 2 MALFUNCTIONED A DHLA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 01 366DH 249 NR 2 COMPASS SYSTEM FAILED RUSULTING IN LOSS OR NR 2 COMPASS INDICATION. SWITCHING BOTH TO CAPTAINS POPPED COMPASS 32-2 6 CIRCUIT BREAKER. COULD NOT RESTORE SYSTEM. REPLACED F/O ADI INDICATOR, FUNCTIONAL CHECK OK PER MM. 2 L 7 2 4F RT A35EU 1999091700310 19990917 00310 NE 1999 9 17 DHL99366002 2 19990908 A 7310 9068744G01 FUEL LINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 ENGINE CRACKED A DHLA A B E UNSCHED LANDING EMER. DESCENT ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 366DH 249 AT STABILIZED CRUISE, FL 350, NR 1 ENGINE ROLLED BACK TO APPROX 87 PERCENT N1. THROTTLE RETARDED TO DETERMINE IF RPM W OULD FOLLOW. ENGINE THEN ROLLED BACK TO 38 PERCENT, FUEL FLOW TO 1700 AND ENGINE CEASED TO FOLLOW THROTTLE INPUTS. ENG INE SHUTDOWN PER PROCEDURE. RELIGHT UNSUCESSFUL, DIVERTED TO MCI. REMOVED AND REPLACED NR 1 ENGINE FUEL LINE TO MEC FO R FUEL FLOW INDICATOR. FOUND LINE CRACKED. 2 L 7 2 4F 4 F RT A35EU E23EA 1999091700311 19990917 00311 NM 1999 9 17 SWAA991488 1 19990907 A 2560 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 508SW 24185 AFT SERVICE DOOR SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999091700312 19990917 00312 NM 1999 9 17 SWAA991489 1 19990905 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM ROW 8 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT LOOSE AT ROW 8. RESECURED EEPLS LIGHT PER MM. 2 L 7 2 4F A16WE 1999091700313 19990917 00313 NM 1999 9 17 SWAA991490 1 19990906 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FWD OVERHEAD EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999091700314 19990917 00314 NM 1999 9 17 SWAA991491 1 19990906 A 5753 654653424 TRACK BOEING 737 7372T4 1384492 NM LT TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND NR 2 FLAP TRACK HAS PITTING CORROSION ON AFT MOUNTING SURFACE. REMOVED AND REPLACED NR 2 FLAP TRACK ASSY PER MM. 2 L 7 2 4F A16WE 1999091700315 19990917 00315 NM 1999 9 17 SWAA991492 1 19990907 A 5320 65516989 SPLICE BOEING 737 7372H4 138448C NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED, BS 908, STRINGER 4L. REMOVED AND REPLACED STRIN GER SPLICE PER SRM. 2 L 7 2 4F A16WE 1999091700316 19990917 00316 NM 1999 9 17 SWAA991493 1 19990907 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999091700317 19990917 00317 NM 1999 9 17 SWAA991494 1 19990907 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND 3 INCHES LONG CRACK ON FUSELAGE SKIN, BS 727B, STRINGER 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999091700318 19990917 00318 NM 1999 9 17 SWAA991495 1 19990907 A 2560 D31354 SLIDE GAUGE BOEING 737 7372H4 138448C NM PAX DOORWAY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRES GAUGE OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM . 2 L 7 2 4F A16WE 1999091700319 19990917 00319 NM 1999 9 17 SWAA991496 1 19990908 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOOR BEAM UPPER CHORD CORRODED IN NUMEROUS SCREW HOLES. REPAIRED BEAM PER SW A RA NR 1-353-2160. 2 L 7 2 4F RT A16WE 1999091700320 19990917 00320 1999 9 17 SWAA991486 4 19990906 A 3460 FMCS BOEING 737 7373Q8 1384670 NM COCKPIT MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 695SW 23506 AIR TURNBACK, AFTER TAKEOFF, FIRST OFFICER'S AIR SPEED, ALTIMETER, AND VERTICAL SPEED INDICATORS FAILED. STICK SHAKER C AME ON FOR APPROX 1 MINUTE. PERFORMED DFCS AND FMCS BITE PER MM. INSPECTED AIRCRAFT AND TESTED SYSTEM PER MM. OPS CHE CKED NORMAL. 2 L 7 2 4F RT A16WE 1999091700321 19990917 00321 NM 1999 9 17 SWAA991487 1 19990908 A 2121 65771 FAN BOEING 737 7373H4 1384600 NM E&E COMP OVER HEATED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 391SW 27378 DECLARED EMERGENCY LANDING, DURING FLIGHT A SMOKE/BURNING SMELL IN COCKPIT. DISCOVERED EQUIPMENT COOLING FAN OVERHEATED AND C/B TRIPPED. DEFERRED PER MEL AND DURING RON REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM. 2 L 7 2 4F RT A16WE 1999091700322 19990917 00322 NM 1999 9 17 SWAA991473 1 19990904 A 5320 6558280 FRAME BOEING 737 7373H4 1384600 NM SRVC DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR LOWER CUT OUT FUSELAGE STUB FRAME CRACKED, BS 294. REPAIRED FRAME P ER SRM. 2 L 7 2 4F RT A16WE 1999091700323 19990917 00323 NM 1999 9 17 SWAA991474 1 19990904 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND 2 EACH CRACKS, BS 178 BULKHEAD, BL 0 - RBL 7. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999091700324 19990917 00324 NM 1999 9 17 SWAA991475 1 19990904 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM SRVC DOORWAY CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED ABOVE AFT SERVICE DOOR. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999091700325 19990917 00325 NM 1999 9 17 SWAA991476 1 19990904 A 3350 100031 BATTERY PACK BOEING 737 7372H4 138448C NM ROW 2 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 2. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F A16WE 1999091700326 19990917 00326 NM 1999 9 17 SWAA991477 1 19990904 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM ROW 19 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 19. RELAMPED PER MM. 2 L 7 2 4F A16WE 1999091700327 19990917 00327 NM 1999 9 17 SWAA991478 1 19990904 A 3213 654611646 INNER CYLINDER BOEING 737 7373Q8 1384670 NM NR 1 MLG GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING RON, FOUND NR 1 MLG AXLE SLEEVE ROTATED 90 DEGREES AND HAS SMALL GOUGES WITH PAINT DISCOLORATION ON AXLE. REMOVE D AND REPLACED NR 1 MLG INNER CYLINDER ASSY PER MM. (THIS IS A CONTINUATION OF SDR FORM NR SWAA99-1459, SUBMITTED SEPT 3 , 1999). 2 L 7 2 4F RT A16WE 1999091700328 19990917 00328 NM 1999 9 17 SWAA991479 1 19990903 A 3350 10885 BATTERY PACK BOEING 737 7373H4 1384600 NM ROW 12-17 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP, ROW 12 THROUGH 17. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999091700329 19990917 00329 NM 1999 9 17 SWAA991480 1 19990903 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 751 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 751, STRINGER 18R. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999091700330 19990917 00330 NM 1999 9 17 SWAA991481 1 19990903 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 518 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 518, STRINGER 12L. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999091700331 19990917 00331 NM 1999 9 17 SWAA991482 1 19990903 A 5313 BAC1498 STRINGER BOEING 737 7372T4 1384492 NM AFT FUSELAGE CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND STRINGER 24R CORRODED, BS 986-1016. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F A16WE 1999091700332 19990917 00332 NM 1999 9 17 SWAA991483 1 19990903 A 5320 6547998 BEAM BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CREASE BEAM INBOARD CHORD CRACKED, BS 727, RBL 63. REMOVED AND REPLACED CREASE BEAM INB OARD SECTION, BS 672-727+6 PER SRM. 2 L 7 2 4F A16WE 1999091700333 19990917 00333 NM 1999 9 17 SWAA991484 1 19990903 A 7933 65C469901 TEMP BULB BOEING 737 7375H4 138449D NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A SWAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SW 07 515SW 25154 725924 IN FLIGHT ENGINE SHUTDOWN, NR 1 ENGINE OIL TEMP CLIMBED ABOVE RED BAND DURING FLIGHT. ALL OTHER ENGINE INDICATIONS NORM AL. REMOVED AND REPLACED NR 1 ENG OIL SYSTEM AND SCAVANGE FILTERS, OIL, FUEL/OIL HEAT EXCHANGER AND OIL TEMP BULB. RAN ENGINE, OPS CHECKED GOOD PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999091700334 19990917 00334 NM 1999 9 17 SWAA991485 1 19990903 A 2781 189929 SENSOR BOEING 737 7372H4 138448C NM NR 3 SLAT DAMAGED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 105SW 23249 AIR TURNBACK, NR 3 L/E SLAT EXTEND TRANSIT LIGHT ILLUMINATED WITH SLAT RETRACTED. REMOVED AND REPLACED NR 3 SLAT PROX S ENSOR. 2 L 7 2 4F A16WE 1999091700335 19990917 00335 NM 1999 9 17 SWAA991497 1 19990908 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR DETACHED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 EMERGENCY EXIT LIGHT OVER FWD SERVICE DOOR FELL OUT DURING FLIGHT. REINSTALLED EXIT LIGHT PER MM. 2 L 7 2 4F A16WE 1999091700336 19990917 00336 NM 1999 9 17 SWAA991498 1 19990908 A 5220 651750 HANDLE BOEING 737 7373H4 1384600 NM LT EMER EXIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY DOOR HANDLE COVERPLATE BROKEN. REMOVED AND REPLACED HANDLE PER MM. 2 L 7 2 4F RT A16WE 1999091700337 19990917 00337 NM 1999 9 17 SWAA991499 1 19990908 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999091700338 19990917 00338 NM 1999 9 17 SWAA991500 1 19990908 A 5330 6545890 SKIN BOEING 737 7372T4 1384492 NM BS 317 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND 1.3 INCH LONG CRACK ON FUSELAGE SKIN, BS 317, STRINGER 18R. REPAIRED SKIN PER SRM . 2 L 7 2 4F A16WE 1999091700339 19990917 00339 NM 1999 9 17 SWAA991501 1 19990908 A 5330 6545773 SKIN BOEING 737 7372T4 1384492 NM BS 747&767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS, STRINGER 10R, BS 747 AND BS 767. REPAIRED SKIN PER S RM. 2 L 7 2 4F A16WE 1999091700340 19990917 00340 NM 1999 9 17 SWAA991502 1 19990908 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 767, STRINGER 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999091700341 19990917 00341 NM 1999 9 17 SWAA991503 1 19990909 A 3230 273A12011 ACTUATOR BOEING 737 7377H4 NM NLG DNLOCK INOP A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 704SW 27838 AIR TURNBACK, NLG FAILED TO RETRACT AFTER TAKEOFF (GEAR RECYCLED TWICE). PINNED NLG AND RELEASED FOR FERRY FLIGHT TO DA L. AT DAL, REMOVED AND REPLACED NLG LOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 1999091700342 19990917 00342 NM 1999 9 17 SWAA991504 1 19990909 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 DURING SCHEDULED A2 CHECK, FOUND 3 EACH EEPLS COVERS DAMAGED. REMOVED AND REPLACED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 1999091700343 19990917 00343 NM 1999 9 17 SWAA991505 1 19990909 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED C2 CHECK, FOUND AFT EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999091700344 19990917 00344 NM 1999 9 17 SWAA991506 1 19990909 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED C1 CHECK, FOUND WEAK BATTERY AT EMERGENCY EXIT RT CEILING LIGHT. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999091700345 19990917 00345 NM 1999 9 17 SWAA991507 1 19990909 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL10.5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999091700346 19990917 00346 NM 1999 9 17 SWAA991508 1 19990909 A 5312 963089 BULKHEAD CHORD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD ANGLE CRACKED, LBL26.5. REMOVED AND REPLACED CHORD ANG LE PER SRM. 2 L 7 2 4F RT A16WE 1999091700347 19990917 00347 NM 1999 9 17 TWAA9912301 1 19990909 A 3110 658060021 CLOCK BOEING 767 767330 NM COCKPIT UNKNOWN A TWAA K NONE O OTHER UK UNKNOWN 1 CE 05 691LF 25137 BURNING ODOR COMING FROM COCKPIT CLOCK. REPLACED COCKPIT CLOCK TWA STOCK NR 63078. CC6D 6-8-99 MCI. 2 L 7 2 4F RT A1NM 1999091700348 19990917 00348 WP 1999 9 17 CALA9901158 1 19990908 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1170-1271 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND LT AFT CARGO TRACK CORRODED AT SAT 1170-1271, LBL 24. A NEW CARGO TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05, FIGURE 4C. 2 L 7 2 4F A6WE 1999091700349 19990917 00349 WP 1999 9 17 CALA9901159 1 19990908 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 541 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND LOWER ANGLES CORRODED AT BOTH SIDES OF FALSE BULKHEAD AT FS 541. THE SUPPORT ANGLES WERE REMOVED AND R EPLACED IAW SRM 51-30-2, 51-10-3, 51-01, FIGURE 1, SHEET 3, 53-20-0, AND 53-24-0. 2 L 7 2 4F A6WE 1999091700350 19990917 00350 WP 1999 9 17 CALA9901160 1 19990908 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 257 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2.25 INCH CRACK IN LT WING LOWER LEADING EDGE SKIN AT STA XRS 257(NR 8 SLAT TRACK). A DOUBLER WAS IN STALLED IAW ECRA 5730-01667, SRM 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999091700351 19990917 00351 WP 1999 9 17 CALA9901161 1 19990908 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FORWARD ENTRANCE DOOR CUTOUT CORRODED ON LOWER FORWARD CORNER AT FS 200, LONGERON 18L. A REPAIR DOUBLE R AND FILLER WERE INSTALLED IAW ECRA 5310-03900 AND EA 9-5314-2-A0486. 2 L 7 2 4F A6WE 1999091700352 19990917 00352 WP 1999 9 17 CALA9901162 1 19990908 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 218, LBL 6. A NEW SUPPORT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-1 0-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999091700353 19990917 00353 WP 1999 9 17 CALA9901163 1 19990908 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1009-1079 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AROUND CLIP NUTS AT STA 1009-1079. THE SEAT TRACK WAS REPLACED IAW ECRA 5310-03904. 2 L 7 2 4F A6WE 1999091700354 19990917 00354 WP 1999 9 17 CALA9901164 1 19990908 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT AT FS 446, LONGERON 23L. THE SUPPORT WAS REMOVED AND A NE W SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2. 2 L 7 2 4F A6WE 1999091700355 19990917 00355 WP 1999 9 17 CALA9901165 1 19990908 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM TO FRAME SUPPORT FITTING AT STA 1338, RBL 54.5. THE FITTING WAS REPLACED IAW SRM 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999091700356 19990917 00356 WP 1999 9 17 CALA9901166 1 19990908 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155, LONGERON 28R-29R. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-1 0-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999091700357 19990917 00357 WP 1999 9 17 CALA9901167 1 19990908 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1332 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 1332, LBL 34 TO 42.5. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10 -3 AND 53-05, FIGURE 20A. 2 L 7 2 4F A6WE 1999091700358 19990917 00358 NM 1999 9 17 CALA9901168 1 19990909 A 2560 MEGAPHONE BOEING 727 727224 1384076 NM CABIN INOP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REPLACED. 2 L 7 3 4F A3WE 1999091700359 19990917 00359 NM 1999 9 17 CALA9901169 1 19990909 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 640-720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND FORWARD CARGO STRINGER 27L CORRODED AT FS 660-640, FS 720C-720B, AND 720B-720A. THE CORRODED AREAS WER E CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 51-20-0. 2 L 7 3 4F A3WE 1999091700360 19990917 00360 WP 1999 9 17 CALA9901170 1 19990910 A 3350 900542 POWER SUPPLY GRIMES DOUG DC9 DC982 3022082 WP EMER EXIT INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND EMERGENCY OVERWING AFT LIGHT INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33- 50-22. 2 L 7 2 4F A6WE 1999091700361 19990917 00361 WP 1999 9 17 CALA9901171 1 19990910 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP EMER EXIT INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77827 49487 THE RIGHT AND LEFT AFT OVERWING EMERGENCY EXIT SIGNS WOULD NOT ILLUMINATE DURING TEST. THE BATTERY POWER SUPPLY WAS REM OVED AND REPLACED IAW MM 33-53-00. 2 L 7 2 4F A6WE 1999091700362 19990917 00362 NM 1999 9 17 CALA9901172 1 19990907 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 370 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 370. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202. 2 L 7 2 4F RT A16WE 1999091700363 19990917 00363 NM 1999 9 17 CALA9901173 1 19990908 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 907-930 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 907-930. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52 . 2 L 7 2 4F RT A16WE 1999091700364 19990917 00364 NM 1999 9 17 CALA9901174 1 19990911 A 5320 BRACKET BOEING 737 7373T0 1384582 NM BS 520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 1 INCH CRACK IN EXPANSION JOINT BRACKET AT BS 520, LBL 45.5. A NEW BRACKET WAS INSTALLED IAW SRM 51- 40-02. 2 L 7 2 4F RT A16WE 1999091700365 19990917 00365 WP 1999 9 17 CALA9901175 1 19990912 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP RT COCKPIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2 INCH CRACK IN RT COCKPIT SLIDING WINDOW CUTOUT UPPER AFT CORNER INSIDE DOUBLER. THE DOUBLER WAS RE MOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-1. 2 L 7 2 4F A6WE 1999091700366 19990917 00366 WP 1999 9 17 CALA9901176 1 19990912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1309 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 3 INCH CRACK IN LT CENTER SEAT TRACK AT FS 1309, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-3, AND 53-05, FIGURE 4A. 2 L 7 2 4F A6WE 1999091700367 19990917 00367 WP 1999 9 17 CALA9901177 1 19990912 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1022-1243 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND AFT RIGHT O/B SEAT TRACK CORRODED AT STA 1022-1041, RBL 54.5 AND STA 1092-1243, RBL 54.5. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, AND 53-05, FIGURE 4. 2 L 7 2 4F A6WE 1999091700368 19990917 00368 WP 1999 9 17 CALA9901178 1 19990912 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 157-180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 157-180, RBL 40. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-3 0-2, 51-30-5, AND 51-10-3. 2 L 7 2 4F A6WE 1999091700369 19990917 00369 WP 1999 9 17 CALA9901179 1 19990912 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 157-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 157-200, BL 0 AND STA 200, BL 0 TO RBL 40. THE SUPPORTS WERE REMOVED AN D REPLACED IAW SRM 53-14-1, FIGURE 11, 51-10-4, 51-10-3, 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999091700370 19990917 00370 WP 1999 9 17 CALA9901180 1 19990912 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, BL 0 TO LBL 12 AND LBL 40. THE FLOOR SUPPORTS WERE REMOVED AND REP LACED IAW SRM 51-30-2, 53-14-1, 51-10-3, 51-30-4, AND 51-30-5. 2 L 7 2 4F A6WE 1999091700371 19990917 00371 WP 1999 9 17 CALA9901181 1 19990912 A 5310 SUBFLOOR DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND SUBFLOOR CORRODED AT STA 200, LBL 40 AND LBL 18 TO RBL 30. THE SUBFLOOR AREAS WERE REPAIRED IAW SRM 51 -30-2, 53-05, FIGURE 25, 51-30-5, AND 53-01, FIGURE 4. 2 L 7 2 4F A6WE 1999091700372 19990917 00372 WP 1999 9 17 CALA9901182 1 19990912 A 5310 SUBFLOOR DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND SUBFLOOR CORRODED AT STA 218, LBL 42-44. THE SUBFLOOR WEB AND STIFFENERS WERE REMOVED AND A NEW WEB AN D STIFFENERS WERE INSTALLED IAW SRM 53-10-4, 51-30-2, 51-30-4, AND 51-30-8. 2 L 7 2 4F A6WE 1999091700373 19990917 00373 WP 1999 9 17 CALA9901183 1 19990912 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 148-160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND L-ANGLE ABOVE LONGERON 18R AT STA 148-160 CORRODED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLE D IAW SRM 51-30-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999091700374 19990917 00374 EA 1999 9 17 COMA9960502 1 19990912 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 FRAME AT FS 718.00 LHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 4 ABOVE STRINGER II IN THE FL ANGE ATTACHING TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING TO THE SECOND FASTENER HOLE BELOW STRINGER II. ALSO , DOUBLER ON THE AFT SIDE OF FRAME FS 718.00 RHS IS CRACKED APPROXIMATELY 4. 2 L 7 2 4F RT A21EA 1999091700375 19990917 00375 EA 1999 9 17 COMA9960503 1 19990911 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA BS 310&349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 PAX DOOR THRESHOLD ANGLE CORRODED LBL 42 BETWEEN FS 310 AND FS 349 (P/N 601R31527-181). PERFORMED A MAJOR REPAIR REMOVE D CORRODED THRESHOLD ANGLE (P/N 601R31527-181). INSTALLED A NEW THRESHOLD ANGLE MADE FROM EXTRUSION 3992T-068, MATERIAL 7075 - T65II IAW WVAC EO NR 601K-53-0316. 2 L 7 2 4F RT A21EA 1999091700376 19990917 00376 EA 1999 9 17 COMA9960504 1 19990911 A 5320 601R386731719 PLATE CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 FS 349 FRAME PLATE BETWEEN LBL 42 AND LBL 27 CORRODED BETWEEN LBL 27 AND LBL 9, BETWEEN RBL 9 AND RBL 27 BETWEEN RBL 27 AND RBL 42. ALSO, CORRODED (P/N 601R38673-17,19,21 AND 25). PERFORMED A MAJOR REPAIR REMOVED THE CORRODED PLATES AT F S 349 AND FABRICATED AND INSTALLED NEW PLATES IAW WVAC EO 601R-53-0317. 2 L 7 2 4F RT A21EA 1999091700377 19990917 00377 EA 1999 9 17 COMA9960505 1 19990911 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA SERV DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 SERVICE DOOR THRESHOLD ATTACH SKIN HAS SURFACE CORROSION. PERFORMED A MAJOR REPAIR, REMOVED THE CORRODED THRESHOLD ANGL E (P/N 601R38303-105). INSTALLED A NEW THRESHOLD ANGLE (P/N 601R38303-105) IAW WVAC EO 601R-53-0315. 2 L 7 2 4F RT A21EA 1999091700378 19990917 00378 EA 1999 9 17 COMA9960506 1 19990912 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 FRAME AT FS 718.00 RHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 2 ABOVE STRINGER II IN THE FL ANGE ATTACHING TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING BETWEEN THE FIRST AND SECOND FASTENER HOLE BELOW STR INGER II. ALSO, THE DOUBLER ON THE AFT SIDE OF FRAME FS 718.00 RHS IS CRACKED APPROXIMATELY 4. PERFORMED A MAJOR REPAI R TO CRACKS IN FRAME AT FS 718.00 RHS IAW WVAC EO 601R-53-0319 AND REPLACED DOUBLER AT AFT SIDE OF FRAME FS 718.00 RHS S TR II IAW WVAC EO 601R-53-0320. 2 L 7 2 4F RT A21EA 1999091700379 19990917 00379 EA 1999 9 17 COMA9960507 1 19990912 A 5400 601R3700457 ANGLE CNDAIR CL600 CL6002B19 EA LT PYLON CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 PANEL 411AL CHAFED BY FASTENER MID FRAME OUTBOARD EDGE LEFT HAND ENGINE PYLON. PERFORMED MAJOR REPAIR SMOOTHED CHAFE ON (P/N 601-37004-133) AND FABED NEW SUPPORT ANGLE 601-37004-57 AS PER SAMPLE USING 2024-T3.040 PO NR 4206/1 AND INSTALLED IAW WVAC EO NR 601R-54-0327. 2 L 7 2 4F RT A21EA 1999091700380 19990917 00380 EA 1999 9 17 COMA9960508 1 19990912 A 5210 FILLER CNDAIR CL600 CL6002B19 EA PAX DOOR MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 PAX DOOR SEALING NIB IS DAMAGED AT LOWER FORWARD AREA (FILLER ONLY MISSING). REPAIRED IAW REO'S 601R-52-11-008. REPLAC ED FILLER ONLY. 2 L 7 2 4F RT A21EA 1999091700381 19990917 00381 EA 1999 9 17 COMA9960509 1 19990912 A 5210 FILLER CNDAIR CL600 CL6002B19 EA PAX DOOR MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 PAX DOOR SEALING NIB IS DAMAGED AT LOWER FORWARD AREA (FILLER ONLY MISSING). REPAIRED IAW REOSA 601R-52-11-008. REPLAC ED FILLER ONLY. 2 L 7 2 4F RT A21EA 1999091700382 19990917 00382 NM 1999 9 17 UPS99230611 1 19990828 A 5320 WEB BOEING 727 72731C 1384011 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C, CRACK FOUND LT MLG WHEEL WELL PRESSURE WEB LBL 36 BS 940. REPAIRED PRESSURE WEB ON LT MLG WHEEL WELL IAW DRAWING NR 65 -89360 AND EO B727-5310-0460 APPENDIX C. 2 L 7 3 4F A3WE 1999091700383 19990917 00383 NM 1999 9 17 UPS99230612 1 19990903 A 5720 TE WEDGE BOEING 727 72731C 1384011 NM WS 251-383 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C, DURING REPAIR ON RT INBOARD MID FLAP DELAMINATION, CORROSION FOUND O N T/E WEDGE UPPER SURFACE. REPL ACED MID FLAP IAW MM 27-51-23. 2 L 7 3 4F A3WE 1999091700384 19990917 00384 NM 1999 9 17 UPS99230613 1 19990831 A 7830 BRACKET BOEING 727 72731C 1384011 NM NR 1 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C, ENGINE NR 1 THRUST REV OUTBOARD FAIRING MID AND AFT SUPPORT BRACKETS CRACKED. NR 1 ENGINE THRUST REV ERSER OUTBOARD FAIRING MID AND AFT SUPPORT BRACKETS REPLACED IAW MM 78-30-00. 2 L 7 3 4F A3WE 1999091700385 19990917 00385 NM 1999 9 17 UPS99230615 1 19990830 A 5320 STRAP BOEING 727 72731C 1384011 NM RT COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE:C, ON X-RAY INSP OF E & F WINDOW POST RT SIDE OF COCKPIT CRACK FOUND IN PT F OF STEEL STRAP. REPAIR CAR RIED OUT IAW UPS EO B727-5310-0012 USING KIT (P/N 65C 35282-8). 2 L 7 3 4F A3WE 1999091700386 19990917 00386 NM 1999 9 17 UPS99230618 1 19990910 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 19 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY LIGHT ROW 19 LT SIDE INOP. REMOVED AND REPLACED BATTERY PACK AT SEAT ROW 19 LT SIDE. EM ERGENCY LIGHT OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999091700387 19990917 00387 NM 1999 9 17 UPS99430614 1 19990912 A 5414 PANEL BOEING 747 747123 1384873 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE:N/A, APPROX 11 INCH CRACK ON NR 3 PYLON I/B SIDE FWD OF LOWER ACCESS PANEL. PERFORM CONDUCTIVITY TEST A ND VISUAL INSPECTION PER BOEING LETTER 99-00318H. *S/D* COMPLISHED CONDUCTIVITY TEST AND VISUAL INSPECTION PER BOEING REQUEST LETTER 99-00318H. 2 L 7 4 4F A20WE 1999091700388 19990917 00388 1999 9 17 UPS99430617 4 19990909 A 2211 COMPUTER BOEING 747 747123F NM AUTOPILOT INOP A IPXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 674UP 20100 INSPECTION TYPE:N/A, IN CRUISE AFTER AN ATC REQUIRED SPEED REDUCTION, B AUTOPILOT ABRUPTLY PITCHED A/C NOSE UP (ADDITION AL 2.5 - 3 DEGREES. F/O PUSHED OVER BUT COULD NOT PREVENT AN ALTITUDE DEVIATION OF 300 FT NEITHER A/P OR ALTITUDE HOLD DISENGAGED AUTOMATICALLY. SUBSEQUENT A A/P OPS NORMAL. B A/P DISCREPANCY RECURRED WHEN RE-ENGAGED. *S/D* REMOVED AND REPLACED B SYSTEM PITCH COMPUTER PER MM 22-12-01, PERFORMED OPS CHECK AND AUTOPILOT CHECKS NORMAL. 2 L 7 4 4F A20WE 1999091700389 19990917 00389 NM 1999 9 17 UPS99630616 1 19990911 A 5330 SKIN BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 INSPECTION TYPE:N/A, CRACK ON PIT 34 UPPER AFT CORNER FUSELAGE SKIN 1 INCH LONG. 2 L 7 2 4F RT A1NM 1999091700390 19990917 00390 NM 1999 9 17 99FDEA00380 1 19990910 A 2150 VALVE BOEING 727 727233 138408A NM LT PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 218FE 21101 LWR AFT BODY OVERHEAT LIGHT CAME ON DURING CLIMBOUT. PERFORMED RED TABS AND ISOLATED TO BE LEAK BETWEEN NR 1 BLD VALVE AND LT PACK VALVE. 2 L 7 3 4F RT A3WE 1999091700391 19990917 00391 NM 1999 9 17 99FDEA00381 1 19990911 A 2782 ACTUATOR BOEING 727 727247 138408F NM NR 7 LE SLAT FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 234FE 21328 ON DEPARTURE DURING FLAP RETRACTION FROM 2 DEG TO 0 DEG, NR 7 SLAT WOULD NOT RETRACT. OPERATED SLAT/FLAPS NUMEROUS TIME S, OPS CHECKS GOOD. CHECKED NR 7 SLAT ACTUATOR FOR BYPASSING. CHECK OK, NO PLAY FOUND IN TRACKS OF ACTUATOR. OK FOR S ERVICE. ALL WORK IAW B727 MM 27-80-00. 2 L 7 3 4F A3WE 1999091700392 19990917 00392 NM 1999 9 17 99FDEA00382 1 19990913 A 5320 651634021 FRAME BOEING 727 727277 138408S NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 NR 502 - WHILE WORKING NR 252 FOUND SHEAR TIE CORRODED AT BS 970, STR 29-30R, WL 156. REMOVED AND REPLACED CORROSION FO UND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 GAINED ACCESS IAW FEDEX SRM 53-10-4. 2 L 7 3 4F RT A3WE 1999091700393 19990917 00393 NM 1999 9 17 99FDEA00383 1 19990913 A 5313 STRINGER BOEING 727 727277 138408S NM BS 960-1007 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 NR 252 - CORROSION LEFT KEEL BEAM BS 1000 IN POCKET OR U-SECTION. REMOVED DAMAGED SECTION OF STR 29L FROM BS 1007 TO 96 0 AND SPLICED NEW STR 29L SECTION PER FEDEX EA NR 7-5310-46997. 2 L 7 3 4F RT A3WE 1999091700394 19990917 00394 WP 1999 9 17 99FDEA00384 1 19990910 A 5730 SKIN DOUG DC10 DC1030F 3023504 WP WS 402 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 310FE 48299 RT WING LOWER SURFACE OF LEADING EDGE ALONG XORS 402 FOUND WITH 2 INCH CRACK. *S/D* REPAIR CARRIED OUT PER SRM 57-10-0 0 FIG 68 VOL 1. 2 L 7 3 4F RT A22WE 1999091700395 19990917 00395 WP 1999 9 17 ABXA9900694 1 19990910 A 5230 591014163 PAN DOUG DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INNER AND OUTER PANS TO BE CRACKED. REPAIRED IAW ABX REA D952-33186. 2 L 7 2 4F A6WE 1999091700396 19990917 00396 WP 1999 9 17 ABXA9900695 1 19990910 A 5720 9919398 FITTING DOUG DOUG DC9 DC931 3022065 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND FITTING CRACKED AT LEFT WING SLAT DRIVE. REPLACED FITTING IAW ABX REA D957-33196. 2 L 7 2 4F A6WE 1999091700397 19990917 00397 WP 1999 9 17 ABXA9900696 1 19990910 A 5400 99582216 ANGLE DOUG DOUG DC9 DC931 3022065 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND RIGHT PYLON HAD CRACKED WEB AT LOWER ATTACH ANGLE. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5 . 2 L 7 2 4F A6WE 1999091700398 19990917 00398 WP 1999 9 17 ABXA9900697 1 19990910 A 5320 39203412 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND CRACK IN FUSELAGE FRAME ATTACH FITTING AT STATION 617, BELOW LONGERON 18 RIGHT. REPLACED FITTING IAW DC9 SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1999091700399 19990917 00399 WP 1999 9 17 ABXA9900698 1 19990910 A 5311 592433713 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, INSPECTION FOUND FUSELAGE FRAME STATION 658 CRACKED BELOW LONGERON 18 LEFT. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999091700400 19990917 00400 WP 1999 9 17 ABXA9900699 1 19990910 A 5400 591326210 ANGLE DOUG DOUG DC9 DC931 3022065 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND RIGHT PYLON LEADING EDGE INBOARD LOWER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1999091700401 19990917 00401 WP 1999 9 17 ABXA9900700 1 19990910 A 5230 39132491 FITTING DOUG DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR BEAM END FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30 -5. 2 L 7 2 4F A6WE 1999091700402 19990917 00402 WP 1999 9 17 ABXA9900701 1 19990910 A 5313 27779224 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, INSPECTION FOUND LONGERON 17 RIGHT CRACKED AT STATION 945. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999091700403 19990917 00403 NM 1999 9 17 DHL99724008 1 19990911 A 5754 692951213 BRACKET BOEING 727 727228 NM NR 1 LE FLAP BROKEN A DHLA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 01 724DH 19862 NR 1 KRUEGER FLAP INTRANSIT LIGHT ON DURING RETRACTION AT FLAPS 5 DEGREE. REMOVED AND REPLACED KRUEGER SWITCH ARM BRACK ET PER MM 27-82-1, OPS CHECK OK. 2 L 7 3 4F A3WE 1999091700406 19990917 00406 EU 1999 9 17 CA990630002 1 19990514 A 6210 355A11002011 BLADE SNIAS 350 AS350B1 8680811 EU MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2750 8192 (CAN) DURING SCHEDULED MAINTENANCE, A 6 INCH CHORDWISE CRACK WAS FOUND ON THE LOWER SURFACE OF THE M/R BLADE. THE CRACK STARTED AT APPROXIMATELY 78 INCHES OUTWARD FROM THE BLADE ROOT. 1 G 7 1 3U H9EU 1999091700407 19990917 00407 EU 1999 9 17 CA990630004 1 19990615 A 6210 350A11001007 BLADE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5205 4535 4498 (CAN) DURING SCHEDULED MAINTENANCE, NUMEROUS 10 MM CRACKS WERE NOTED ON THE LOWER INBOARD AREA APPROXIMATELY 1000 MM FRO M THE BLADE ROOT. 1 G 7 1 3U 3 U H9EU E19EU 1999091700408 19990917 00408 SW 1999 9 17 CA990719005 1 19990630 A 6720 204010775003 HOUSING BELL 204 204B 1181404 SW LYC T53 T5311B 41549 NE PITCH CHANGE WORN W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA LE08329 (CAN) PILOT NOTICED BALL WAS OUT OF TURN/SLIP INDICATOR SO THEN PILOT INPUTTED THE RIGHT PEDAL TO CORRECT. HOWEVER, THE ROTORCRAFT DID NOT RESPOND TO RIGHT PEDAL INPUT, BUT DID RESPOND TO LEFT PEDAL INPUT. PILOT THEN LANDED THE ROTORCRAFT . SUBSEQUENT INVESTIGATION REVEALED THAT THE INTERNAL SPLINES OF THE PITCH CHANGE HOUSING WERE WORN ENOUGH SO THAT THE PITCH CHANGE ROD WAS INEFFECTIVE. 1 G 7 1 4U 4 U H1SW E1EA 1999091700410 19990917 00410 CE 1999 9 17 CA990728028 1 19990719 A 3213 250040495 AXLE HELIO 2500404511 HELIO H395 H395 4300202 CE LYC O480 GO480G1A6 41527 EA HARTZL HCB3Z HCB3Z201 GL RT MLG BROKEN W O OTHER O OTHER LD LANDING 1 CA L21637 L217 (CAN) RIGHT MAIN GEAR AXLE BROKE DURING LANDING. FRACTURE OCCURRED NEAR THROUGH-BOLT AND WOULD BE DETECTABLE IF AXLE WA S PRESSED OUT OF STRUT ASSEMBLY. AIRCRAFT WAS SUBSTANTIALLY DAMAGED. 1 H 7 1 3O 3 O 1A8 E275 5 C P907 1999091700411 19990917 00411 WP 1999 9 17 CA990728029 1 19990709 A 5630 369350642 WINDOW HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL REAR DOOR SEPARATED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA CAE830950 (CAN) RIGHT REAR DOOR WINDOW DEPARTED ROTORCRAFT DURING CRUISE. THIS WINDOW HAD A PREVIOUS CRACK AND WAS A RUBBER MOUNT ED WINDOW. 1 G 7 1 3U 3 U H3WE E4CE 1999091700414 19990917 00414 SW 1999 9 17 CA990728048 1 19990629 A 2435 BEARING LUCAS 23031004 BELL 204 204B 1181404 SW LYC T53 T5311B 41549 NE STARTER/GEN WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 617 LEO8130A (CAN) UNIT SENT TO O/H. WHEN SG WAS DISASSEMBLED, IT WAS NOTED THAT THE WRONG BEARINGS WERE INSTALLED (NOT THE MANUFACT URER'S BEARINGS). UNAPPROVED PARTS REPLACED AND RETURNED TO SERVICE. 1 G 7 1 4U 4 U H1SW E1EA 1999091700415 19990917 00415 SW 1999 9 17 CA990812004 1 19990801 A 6710 212010783101 BEARING BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE MAIN ROTOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 73 LE07569X (CAN) DURING SCHEDULED MAINTENANCE, IT WAS DISCOVERED THAT THE BALL LINER WAS MOVING ALLOWING THE BALL TO CONTACT METAL THEREBY CAUSING DAMAGE TO BALL. 1 G 7 1 4U 4 U H1SW E17EA 1999091700417 19990917 00417 EU 1999 9 17 CA990812043 1 19990802 A 2120 355A25201102 DUCT SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE VENTILATION UNIT CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 982 4550 (CAN) DURING FLIGHT IN RAIN CONDITIONS, THE LOW ROTOR/HYDRAULIC PRESSURE WARNING HORN SOUNDED SEVERAL TIMES ALTHOUGH ALL SYSTEMS WERE OPERATING NORMALLY. FURTHER INVESTIGATION REVEALED THAT RAIN WATER WAS MIGRATING THROUGH THE CABIN VENTIL ATION DUCTING VIA THE INSTRUMENT PANEL AND EVENTUALLY ONTO THE AVIONICS SHELF AND ONTO PRINTED CIRCUITS THEREBY CAUSING THIS FALSE WARNING PROBLEM. 1 G 7 1 3U 3 U NC H9EU E19EU 1999091700418 19990917 00418 SO 1999 9 17 CA990812044 1 19990723 A 6220 FN22M624 NUT 41430003 CAMAIR 480 480 1890102 SO ALLSN 250C 250C20 03013 GL MAIN ROTOR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 930 CAE845007 (CAN) DURING ROUTINE INSPECTION, IT WAS NOTED THAT THE BOLT P/N LWB-22-6-58 THAT HOLDS THE END OF THE HYDRAULIC DAMPER W AS PROTRUDING. FURTHER INVESTIGATION REVEALED THE NUT P/N FN22M-624 AND WASHER P/N WP22-6 WERE MISSING. 1 L 7 2 3O 3 U 2A2 E4CE 1999091700419 19990917 00419 NE 1999 9 17 CA990817020 1 19990809 A 6420 S1610330032 HUB S1619311002 SKRSKY S58T S58ET 8141803 NE PWA PT6T PT6T3 52045 EA TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1188 1629 CPPS60191 (CAN) T/R HUB WAS REMOVED AND DISASSEMBLED IN ORDER TO COMPLY WITH SB. DURING OVERHAUL, AN NDT INSPECTION REVEALED A CR ACK IN THE RADIUS OF THE MOUNTING FLANGE (INBD SIDE). IT IS THOUGHT THAT A FAULTY CASTING MAY HAVE CAUSED THE CRACK. 2 G 7 2 4U 4 U 1H11 E22EA 1999091700420 19990917 00420 GL 1999 9 17 CA990817025 2 19990806 A 7421 CH3416B IGNITER ALLSN 250C20R2 BELL 206 206L 1181522 SW ALLSN 250C 250C20R2 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA CAE295288 CAE295288 (CAN) ROTORCRAFT WOULD NOT START. PROBLEM WAS WITH FAULTY IGNITER PLUG. 1 G 7 1 3U 3 U H2SW E4CE 1999091700421 19990917 00421 EA 1999 9 17 CA990818001 1 19990721 A 6230 AO2R25518 LINK 107R25015 BOEING 107 1072 9420604 EA GE CT58 CT581401 30011 NE SWASHPLATE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2481 CH42 280244L (CAN) PART WAS NEW AT PREVIOUS OVERHAUL OF ROTOR HEAD ASSY, HOWEVER, DISASSEMBLY REVEALED THAT A 0.125 INCH CRACK AT THE PIN BORE EDGE FOUND DURING NDT INSPECTION. 2 G 7 2 4U 4 U 1H16 1E3 1999091700422 19990917 00422 EA 1999 9 17 CA990818003 1 19990803 A 6230 414R350510 BEARING BOEING 234 234 1385049 EA LYC AL5512 AL5512 41581 NE SWASHPLATE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 7241 25 A841992 LE60002 (CAN) AFTER SHUTDOWN (FOLLOWING LOGGING OPERATIONS), A LOT OF BLACK GREASE AND METAL HAD BEEN SLUNG FROM THE SWASHPLATE SEAL AND PIECES OF BEARING CAGE WERE FOUND ALL OVER THE AFT SWASHPLATE AREA AND THRUST DECK. SWASHPLATE WAS REMOVED AND BEARINGS WERE EXTREMELY ROUGH TO TURN. 2 G 7 2 4U 4 U H9EA E4NE 1999091700437 19990917 00437 WP 1999 9 17 TWAA9912401 1 19990911 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 25 BROKEN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9403W 53139 THE EGRESS LIGHTS WOULD NOT COME ON FROM CABIN ROW 25 TO THE AFT CABIN DOORS. REPLACED BROKEN POWER WIRES IN THE TRACK. CHECK-C 11-3-98 MCI. 2 L 7 2 4F RT A6WE 1999091700438 19990917 00438 WP 1999 9 17 TWAA9912402 1 19990909 A 3213 5925371501 STRUT DOUG DC9 DC931 3022065 WP LT MLG RUPTURED A TWAA O OTHER O OTHER LD LANDING 1 CE 05 993Z 47082 DURING LANDING THE LT MAIN LANDING GEAR COLLAPSED. AS A RESULT THE AIRCRAFT STOPPED WITH THE LEFT WING TIP IN CONTACT W ITH THE GROUND. CHECK-C 12-7-98 STL. *S/D* FLIGHT CREW REPORTED A HARD LANDING. IT APPEARS THAT THE LT MAIN LANDING GEAR OUTER CYLINDER RUPTURED AT TOUCHDOWN RESULTING IN LOSS OF THE LOWER HALF OF THE GEAR ASSEMBLY. THE AIRCRAFT CAME T O REST ON THE LT WING, RT GEAR AND NOSE GEAR. 2 L 7 2 4F A6WE 1999091700439 19990917 00439 WP 1999 9 17 TWAA9912403 1 19990903 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 69 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND RIVET HOLE 16 INCHES RIGHT OF CENTER, AT STA 69, SHOWING A CRACK USING HIGH FREQ EDDY CU RRENT. REPAIRED PER MD8-AD-DU, AND DRAWING SRO9530239. 2 L 7 2 4F A6WE 1999091700440 19990917 00440 WP 1999 9 17 TWAA9912404 1 19990903 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 69.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND SKIN CRACK AT FASTENER 18 INCHES RIGHT OF CENTER LINE, STA 69.5. REPAIRED PER MC8-AD-DU AND DRAWING SR09530239. 2 L 7 2 4F A6WE 1999091700441 19990917 00441 WP 1999 9 17 TWAA9912405 1 19990908 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND NUMBER 3 CHAIR TRACK CORRODED BETWEEN STA 200 AND 218. REPLACED TRACK PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999091700442 19990917 00442 WP 1999 9 17 TWAA9912406 1 19990908 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND (P/N 9911505-6) FRAME CRACKED AT STA 83.5, X-10. INSTALLED DOUBLER PER SRM 53-03, FIG 3 4 AND TWA SPM 6-70-01 PAGE 3. 2 L 7 2 4F A6WE 1999091700443 19990917 00443 WP 1999 9 17 TWAA9912407 1 19990908 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND (P/N 9911505-5) FRAME CRACKED AT STA 83.5, X+10. INSTALLED DOUBLER PER SRM 53-03, FIG 3 4 AND TWA SPM 6-70-1 PAGE 3. 2 L 7 2 4F A6WE 1999091700444 19990917 00444 WP 1999 9 17 TWAA9912408 1 19990908 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LONGERON 16R WITH A CRACK AT AFT SIDE OF STA 965 BULKHEAD, AT TOP FLANGE OF LONGERON, AP PROX 1.5 INCHES LONG. REPAIRED LONGERON 16R WITH HAT SECTION REPAIR PER SRM 53-02, FIG 18 SHEETS 1-4 AND 5. 2 L 7 2 4F A6WE 1999091700445 19990917 00445 WP 1999 9 17 TWAA9912409 1 19990908 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, LONGERON 17R HAD APPROX .5 IN CRACK AT AFT SIDE OF STA 965 BULKHEAD. INSTALLED LONGERON HAT S ECTION REPAIR PER SRM 53-02, FIG 18, SHEETS 1-4 AND 5. 2 L 7 2 4F A6WE 1999091700446 19990917 00446 WP 1999 9 17 TWAA9912410 1 19990910 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP BS 69 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND AT STA 69, X-10, UPPER END OF VERTICAL STIFFENER WAS CRACKED ABOVE AND BELOW RIVET HOLE. REPLACED PARTS PER SRM 51-01. 2 L 7 2 4F A6WE 1999091700447 19990917 00447 WP 1999 9 17 TWAA9912411 1 19990910 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP BS 69 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND AT STA 69, X-10, UPPER END OF VERTICAL STIFFENER WAS CRACKED AT RIVET HOLE. REPLACED PA RT PER SRM 51-01. 2 L 7 2 4F A6WE 1999091700448 19990917 00448 WP 1999 9 17 TWAA9912501 1 19990914 A 3350 1315 BULB DOUG DC9 DC983 3022083 WP AFT STAIRS FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9303K 49529 EMERGENCY LIGHTS IN AFT STAIRS INOPERATIVE. REPLACED BULB. CHECK C 11/25/98 MCI. 2 L 7 2 4F RT A6WE 1999091700449 19990917 00449 SO 1999 9 17 LR7A9958 1 19990913 A 5313 LONGERON LKHEED 382 382G 526414U SO BS 836 GOUGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING THRU FLIGHT CHECK, FOUND LT SLOPING LONGERON H FLANGE GOUGED APPROX .020 INCH DEPTH AT FS 836. BLENDED, INSPECTE D, PRIMED AND TOP COATED PER COTNEY COMPANY EDJ19-1, REV IR. 2 H 7 4 4T A1SO 1999091700450 19990917 00450 SO 1999 9 17 LR7A9959 1 19990913 A 5320 DOUBLER LKHEED 382 382G 526414U SO BS 203 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING PRE FLIGHT INSPECTION CREW NOTED APPROX. 1 INCH CRACK IN WL 195 CREW DOOR LONGERON FATIGUE PREVENTATIVE MODIFICAT ION DOUBLER AT FS 203. REMOVED DAMAGED DOUBLER. INSPECTED SKIN AND LONGERON. NO OTHER DEFECTS NOTED. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-30-30. 2 H 7 4 4T A1SO 1999091700451 19990917 00451 EU 1999 9 17 JBXA9900105 1 19990907 A 3610 BLEED AIR CONTL FOKKER F28 F28MK0100 4990807 EU NR 1&2 OUT OF ADJUST A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 105ML 11475 BOS- FLIGHT 668 ABORTED TAKEOFF, BLEED 1 AND 2 FAULT. NO RESET. ACCOMPLISHED BLEED AIR SUPPLY AND CONTROL. ADJUSTME NT AND TEST PER FOKKER 100 MM, CK'S OK PER 36-11-00. 2 L 7 2 4F RT 1999091700452 19990917 00452 NM 1999 9 17 AWXA9900285 1 19990831 A 5320 653535214 TIE CLIP BOEING 737 737277 1384570 NM BS 344 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, TIE CLIP CRACKED RT SIDE FUSELAGE STA 344 STR 11R. REMOVED, FABRICATED REPLACEMENT PART, AND INSTALLED IAW SRM 51-30-2, SRM 51-10-3 FIG 2. 2 L 7 2 4F RT A16WE 1999091700453 19990917 00453 NM 1999 9 17 AWXA9900286 1 19990831 A 5315 65C271567 FLOORBEAM BOEING 737 737277 1384570 NM BS 685 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, CABIN FLOORBEAM RBL 27, STA 685 DOUBLER REPAIR IS CRACKED AT UPPER RADIUS. REMOVED, FABRICATED REPLACEMENT PAR T, AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 1999091700454 19990917 00454 NM 1999 9 17 AWXA9900287 1 19990831 A 5312 654687782 BULKHEAD WEB BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, TWO CRACKS ON RT O/B BULKHEAD SHEAR WEB AT BS 727 STR 18A SHEAR BEAM. REMOVED WEB AND ATTCH PARTS IAW SRM 51-3 0-2. INSTALLED NEW WEB AND ATTACH PARTS. REMOVED AND REINSTALLED 3 STIFFENERS FROM 18A WEB. 2 L 7 2 4F RT A16WE 1999091700455 19990917 00455 NM 1999 9 17 AWXA9900288 1 19990831 A 5330 65737421 SKIN BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, CRACK IN FUSELAGE LT SIDE APPROX 9 AFT AND PARALLEL TO WING SCAN LIGHT (TEMP REPAIR INSTALLED) BS 520 BETWEEN S TR 16 & 17 LT. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 53-30-3 FIG 1. 2 L 7 2 4F RT A16WE 1999091700456 19990917 00456 NM 1999 9 17 AWXA9900289 1 19990831 A 5313 6573744 STRINGER BOEING 737 737277 1384570 NM BS 515 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, STRINGER 16 LT CRACKED AT STA 515. REMOVED DAMAGED SECTION, FABRICATED REPAIR PART AND INSTALLED IAW SRM 51-10 -2 AND SRM 53-10-2 FIG 9, BS 515-540. 2 L 7 2 4F RT A16WE 1999091700457 19990917 00457 NM 1999 9 17 AWXA9900290 1 19990831 A 5320 69144691 TIE CLIP BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, STRINGER TIE CLIP CRACKED STA 520 STR 16 LT. REMOVED, FABRICATED, AND INSTALLED IAW 51-10-3 FIG 2 & SRM 51-30- 2. 2 L 7 2 4F RT A16WE 1999091700458 19990917 00458 NM 1999 9 17 AWXA9900291 1 19990831 A 5753 654953223 SKIN BOEING 737 737277 1384570 NM RT TE MID FLAP CHAFFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, RT I/B MID FLAP REPAIR ON I/B SIDE IS CHAFED OUT OF LIMITS. REMOVED DAMAGED SECTION AND FABRICATED REPLACEMENT SKIN SECTION OF 2024T3,QQA 250/5 0.080 DOUBLER AND 2 CORNER TRIPLERS WITH ONE FILLER OF 2024 T-3 .040 IAW 737 SRM 57-5 0-4 FIG 4, INSTALLED IAW SRM 51-30-2 AND SEALED. 2 L 7 2 4F RT A16WE 1999091700459 19990917 00459 NM 1999 9 17 AWXA9900292 1 19990831 A 5330 6573742 SKIN BOEING 737 737277 1384570 NM BS 312 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, EXTERNAL SKIN AROUND L1 DOOR, AT UPPER DOOR HINGE CUTOUT, 1 CRACK EXTENDING FWD FROM FWD EDGE OF CUTOUT. FABR ICATED AND INSTALLED REPAIR PARTS PER SRM 53-30-3 FIG 21. 2 L 7 2 4F RT A16WE 1999091700460 19990917 00460 NM 1999 9 17 AWXA9900293 1 19990831 A 5315 65C25211150 FLOORBEAM BOEING 737 737277 1384570 NM BS 578 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, MAIN CABIN FLOORBEAM FS 578 RBL 65 CRACKED WEB AT WL 207. REMOVED, FABRICATED AND REPAIRED PER ER 2-53-15-86A. 2 L 7 2 4F RT A16WE 1999091700461 19990917 00461 NM 1999 9 17 AWXA9900294 1 19990831 A 5320 65C22320 ANGLE BOEING 737 737277 1384570 NM BS 598 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 C-CHECK, FLOORBEAM ATTACH ANGLE TO FUSELAGE AT STA 598 WL 208 LT CUSP LINE CRACK STR 17L. REMOVED, FABRICATED, AND INST ALLED REPAIR PARTS PER AWA ER 2-53-15-86 + SB 737-53-1061. 2 L 7 2 4F RT A16WE 1999091700462 19990917 00462 EU 1999 9 17 AWXA9900295 1 19990902 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU EMER EXIT DISCHARGED A AWXA K NONE L NO TEST CR CRUISE 1 WP 28 635AW 092 OVERWING EMER EXIT LIGHTS FLICKERING IN FLIGHT--BATT PACK FAILED TEST. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1999091700463 19990917 00463 1999 9 17 AWXA9900296 4 19990905 A 2350 8990850004 RADIO PANEL AIRBUS 320 A320232 3930326 EU COCKPIT UNSERVICABLE A AWXA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 639AW 6445 2403 471 NR 1 RADIO MGT PANEL (RMP) FAILED, FOLLOWED BY SMELL OF SMOKE IN COCKPIT. PULLED VHF-1 AND RMP-1 C/B, SMOKE DISSIPATED. SWAPPED NR 1 AND NR 3 RMP IAW AMM 23-13-13-401 AND MEL'D (C/N 1109370) NR 3 RMP. THEN REMOVED AND REPLACED NR 3 RMP. 2 L 7 2 4F RT A28NM 1999091700464 19990917 00464 1999 9 17 AWXA9900297 4 19990905 A 2210 SC47003 ACTUATOR AIRBUS 320 A320231 3930325 EU YAW DAMPER LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 645AW 238 CREW REPORTED GREEN HYDRAULIC SYSTEM LOW IN FLIGHT. AT CRUISE, LF 370, HYD GREEN LOW LEVEL ECAM MESSAGE. ACCOMPLISHED ECAM ACTIONS AND CONTINUED FLIGHT FOR UNEVENTFUL LANDING IN MIAMI. FOUND YAW DAMPER SYSTEM NR 1 LEAKING AT ACTUATOR. C OMPLIED WITH MEL 22-63-01. 2 L 7 2 4F RT A28NM 1999091700465 19990917 00465 EU 1999 9 17 AWXA9900298 1 19990906 A 2921 MS21924J12 B NUT AIRBUS 320 A320231 3930325 EU YELLOW HYD SYS LOOSE A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 646AW 271 AMBER ECAM MESSAGE, CLASS NR 1. YELLOW HYDRAULIC RESERVOIR LOW QUANTITY. FOUND 'B' NUT LOOSE ON YELLOW HYDRAULIC ACCUM ULATOR. TIGHTENED NUT. SERVICED SYSTEM WITH APPROXIMATELY 4 GALLONS. 2 L 7 2 4F RT A28NM 1999091700466 19990917 00466 EU 1999 9 17 AWXA9900299 1 19990906 A 2910 248016060 FITTING AIRBUS 320 A320231 3930325 EU GREEN HYD SYS LOOSE A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 618AW 304 ON DESCENT INTO ORD, GREEN HYDRAULIC LOW LEVEL FAULT, LOSS OF QUANTITY. FOUND HYDRAULIC PRESSURE AND RETURN FITTINGS TO YAW DAMPER ACTUATOR VERY LOOSE. RESECURED FITTINGS, NO FURTHER LEAKS NOTED. 2 L 7 2 4F RT A28NM 1999091700467 19990917 00467 1999 9 17 AWXA9900300 4 19990907 A 2565 D30664105 SLIDE AIRBUS 320 A320231 3930325 EU L-1 DOOR DEPLOYED A AWXA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 28 631AW 20192 1817 077 ON ARRIVAL AT GATE SLIDE AT L-1 DEPLOYED WHEN DOOR WAS OPENED, DID NOT INFLATE. REMOVED AND REPLACED SLIDE. 2 L 7 2 4F RT A28NM 1999091700468 19990917 00468 EU 1999 9 17 AWXA9900302 1 19990909 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU GALLEY DISCHARGED A AWXA K NONE L NO TEST CR CRUISE 1 WP 28 640AW 448 EMERGENCY EXIT LIGHTS BLINK ON AND OFF DURING CRUISE. REMOVED AND REPLACED AFT GALLEY EMER LIGHT BATT PACK, SYSTEM TEST OK. 2 L 7 2 4F RT A28NM 1999091700469 19990917 00469 NM 1999 9 17 AWXA9900303 1 19990910 A 5754 65C266031 SPAR BOEING 737 737301 1384611 NM NR 3 LE SLAT BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 CONDITION: C-CHECK SLAT DAMAGEDISCREPANCY: #3 SLAT LOWER AFT SPAR BROKEN OUT SECTION AT ACTUATORCORRECTIVE ACTION: RE PAIRED PER AWA ER 3-57-55-38ARECOMMENDATION: CLOSE 2 L 7 2 4F RT A16WE 1999091700470 19990917 00470 NM 1999 9 17 AWXA9900304 1 19990910 A 5320 393535214 CLIP BOEING 737 7373G7 1384595 NM BS 344 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 C-CHECK, STRINGER CLIP 11A CRACKED STA 344. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT PART 7075-T6 .032 PER SRM 51 -40-00 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 1999091700471 19990917 00471 NM 1999 9 17 AWXA9900305 1 19990910 A 5315 6546812 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 947,967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 C-CHECK, CORROSION BETWEEN STA 947 TO 967 BL 42 LT & RT FLOOR SUPPORT BEAMS 2 EA. REMOVED FLOOR SUPPORT BEAM STA 947 TO 967 BL 42, FAB MAT BAC1506-43, 7050 - T7611 AND SHIM MAT 7075 T-6 .0125 IAW SRM 51-30-1, SRM 53-60-5T FIG 1. TREATED, PRIMED AND INSTALLED PARTS IAW SRM 51-20-01 AND 52-40-00. 2 L 7 2 4F RT A16WE 1999091700472 19990917 00472 NM 1999 9 17 AWXA9900306 1 19990910 A 5320 65C80735116 SILL BOEING 737 7373G7 1384595 NM BS 947.5-1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 C-CHECK, CORROSION BETWEEN STA 947.5 AND STA 1016 BL 54L FLOORBEAM. REMOVED AFT L-1 MOP SILL, INSTALLED NEW MOP SILL AT DOOR L-1 FLOOR IAW SRM 51-40-02, 53-60-15. 2 L 7 2 4F RT A16WE 1999091700473 19990917 00473 NM 1999 9 17 AWXA9900307 1 19990910 A 5315 654681143 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, TOP OF FLOORBEAM STA 986.5 FROM RBL 55 TO LBL 55 CORROSION BEYOND LIMITS AT TWO PLACES. CUT OUT DAMAGED SECTIO N, REMOVED INTERCOSTALS, FABRICATED T FROM BAC1505-100617-7075-T-7, INSTALLED T AND INTERCOST ALS IAW SRM 53-00-51 FIG 201 AND 51-40-02. 2 L 7 2 4F RT A16WE 1999091700474 19990917 00474 NM 1999 9 17 AWXA9900308 1 19990910 A 5320 6545855 SILL BOEING 737 737301 1384611 NM BS 947.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, CORROSION FROM STA 947.5 TO 1006 BL 65R MOPSILL R2 DOOR CUTOUT. REMOVED, FABRICATED, HEAT TREATED AND INSTALLE D SILL AND REPAIR ANGLE IAW SRM 51-40-02 AND 53-60-15 FIG 1. 2 L 7 2 4F RT A16WE 1999091700475 19990917 00475 NM 1999 9 17 AWXA9900309 1 19990910 A 5320 65479080 CHORD BOEING 737 737301 1384611 NM BS 847-867 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, CORROSION AFT CABIN AT CREASE BEAM BTWN BS 847 AND BS 867. REMOVED AND FABRICATED REPAIR PARTS AND INSTALLED I AW SRM 53-60-13, SRM 51-70-12, AND SRM 51-40-2. 2 L 7 2 4F RT A16WE 1999091700476 19990917 00476 NM 1999 9 17 AWXA9900310 1 19990910 A 5511 65C25145 RIB BOEING 737 737301 1384611 NM LT HORIZ STAB GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, LT HORIZONTAL STAB STA 295.10 O/B EDGE HAS GOUGE ON FRAME. REMOVED, FABRICATED, TREATED AND INSTALLED FRAME AN D PLATE IAW 55-10-9, 51-40-02, AND 51-20-01. 2 L 7 2 4F RT A16WE 1999091700477 19990917 00477 NM 1999 9 17 AWXA9900311 1 19990910 A 5240 6545877 SKIN BOEING 737 737301 1384611 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 C-CHECK, R1 DOOR AFT LOWER CORNER HAS 3 INCH LONG CRACK. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-01 FIG 202. 2 L 7 2 4F RT A16WE 1999091700478 19990917 00478 NM 1999 9 17 AWXA9900312 1 19990913 A 2120 AIR DIST AIRBUS A319 A319132 NM CABIN ODOR A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 806AW 1056 OBNOXIOUS ODOR LIKE WD-40 COMING FROM AC SYSTEM WHEN PACKS 1 AND 2 ARE RUNNING OFF APU AIR. RAN PACKS OFF NR 1 AND NR 2 ENG AND OFF APU BLEED. NO ABNORMAL ODORS IN CABIN. 2 L 7 2 4F RT A28NM 1999091700479 19990917 00479 EU 1999 9 17 AWXA9900313 1 19990913 A 3350 321454 PWR SUPPLY AIRBUS 320 A320231 3930325 EU RT OVERWING INOP A AWXA O OTHER L NO TEST TX TAXI/GRND HDL 1 WP 28 645AW 5631 985 238 EMERGENCY EXITS OVERWING RIGHT AND AISLE AFT CENTER REMAIN ON. REMOVED AND REPLACED RT OVERWING EMERG LIGHT POWER SUPPL Y. 2 L 7 2 4F RT A28NM 1999091700480 19990917 00480 NM 1999 9 17 AWXA9900314 1 19990913 A 2781 20224B INDICATOR BOEING 737 7373Q8 1384670 NM NR 2 LE SLAT DISCONNECTED A AWXA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 WP 28 327AW 23507 SLAT 2 AND FWD INDICATIONS INOP. AC DIVERTED TO ONT DUE TO RESTRICTIONS AS STATED IN QRH. A/C PLACED ON MEL., TECH FOU ND PIN NR 20 ON L/E FLAP SLAT INDICATOR PUSHED BACK. RESEATED PIN, OPS CHECK NORMAL. MEL CLEARED. 2 L 7 2 4F RT A16WE 1999091700481 19990917 00481 WP 1999 9 17 CALA9901185 1 19990912 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND COCKPIT RT FLOOR SKIN CORRODED AT FS 148, RBL 6. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WER E INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999091700482 19990917 00482 WP 1999 9 17 CALA9901186 1 19990912 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1330-1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND AFT LT SERVICE DOOR LOWER CUTOUT FLOOR LEVEL SUPPORT CORRODED AT FS 1330-1338, LBL 14. A NEW SUPPORT W AS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999091700483 19990917 00483 WP 1999 9 17 CALA9901187 1 19990912 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1183, LBL 42. REMOVED FORWARD AND AFT FRAME FITTINGS TORQUE BOX DOU BLER AND VERTICAL STIFFENER IAW SRM 51-30-1 AND 51-30-5. A REPAIR WEB WAS INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, AND 51-30-5. THE FITTINGS, FRAME AND STRAPS WERE INSTALLED IAW SRM 53-01-2. 2 L 7 2 4F A6WE 1999091700484 19990917 00484 WP 1999 9 17 CALA9901188 1 19990912 A 5320 FLOOR DOUG DC9 DC982 3022082 WP BS 1138 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND CABIN LT FLOOR SKIN CORRODED AT FS 1138, LBL 42. INSTALLED NEW SKIN AND SUPPORTS IAW SRM 51-30-2, 51-3 0-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999091700485 19990917 00485 WP 1999 9 17 CALA9901189 1 19990912 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOORBEAM WEB CORRODED AT STA 1338, RBL 54.5 AND RBL 35-45. THE CORRODED AREAS WERE CUT OUT AND REPAIR S WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3, 51-30-2, 51-30-5 AND ECRA 5310-03899. 2 L 7 2 4F A6WE 1999091700486 19990917 00486 WP 1999 9 17 CALA9901190 1 19990912 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND LT FLOOR SUPPORT CORRODED AT FS 1155, JUST O/B OF I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1999091700487 19990917 00487 WP 1999 9 17 CALA9901191 1 19990912 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 256 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2 INCH CRACK IN LONGERON 27L AT FS 256. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SPLICE AND LONGERON WERE INSTALLED IAW SRM 53-14-02, FIGURE 3, 53-02, FIGURE 18, 51-30-02, AND 51-30-05. 2 L 7 2 4F A6WE 1999091700488 19990917 00488 WP 1999 9 17 CALA9901192 1 19990912 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 195 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2 INCH CRACK IN SUBFLOOR CUSP WEB AT STA 195, RBL 9. THE SUBFLOOR CUSP WEB WAS REPAIRED IAW SRM 53-0 1, FIGURE 4, SHEET 3. 2 L 7 2 4F A6WE 1999091700489 19990917 00489 WP 1999 9 17 CALA9901193 1 19990912 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1269 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FRAME LOWER LOBE AND WEB CORRODED AT FS 1269, LONGERON 28L-28R. THE CORRODED AREA WAS CUT OUT AND A RE PAIR WAS INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 53-05, FIGURE 4A. 2 L 7 2 4F A6WE 1999091700490 19990917 00490 WP 1999 9 17 CALA9901194 1 19990912 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1333 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FALSE BULKHEAD LOWER ATTACH ANGLE CORRODED AT FS 1333, LONGERON 28L-28R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-10-4 AND 53-01, FIGURE 2, SHEET 4. 2 L 7 2 4F A6WE 1999091700491 19990917 00491 WP 1999 9 17 CALA9901195 1 19990912 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1050 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A SMALL HOLE PUNCTURED IN CUSP WEB AT FS 1050, RBL 59. THE PUNCTURED AREA WAS REMOVED AND A DOUBLER WA S INSTALLED IAW SRM 51-30-5, 51-10-2, AND ECRA 5310-03907. 2 L 7 2 4F A6WE 1999091700492 19990917 00492 WP 1999 9 17 CALA9901196 1 19990912 A 5755 SKIN DOUG DC9 DC982 3022082 WP RT SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 2.2 INCH CRACK IN RT I/B SPOILER FIXED SUPPORT PANEL. THE CRACKED AREA OF SKIN WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 51-30-1 AND 51-10-4. 2 L 7 2 4F A6WE 1999091700493 19990917 00493 WP 1999 9 17 CALA9901197 1 19990912 A 5754 FITTING DOUG DC9 DC982 3022082 WP NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A .25 INCH CRACK IN RT WING NR 5 SLAT O/B FITTING. THE FITTING WAS REMOVED, REPAIRED AND REINSTALLED I AW SRM 51-30-2, 51-30-8, AND ECRA 5750-03276. 2 L 7 2 4F A6WE 1999091700494 19990917 00494 WP 1999 9 17 CALA9901198 1 19990912 A 5543 TAB DOUG DC9 DC982 3022082 WP RUDDER DISBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND RUDDER TRIM TAB METAL TAB DISBONDED ON RT SIDE OF TAB. THE RUDDER TAB WAS REMOVED AND THE METAL TAB WA S REMOVED AND REPLACED. THE RUDDER TAB WAS REINSTALLED AND RIGGED IAW MM 27-20-02. 2 L 7 2 4F A6WE 1999091700495 19990917 00495 WP 1999 9 17 CALA9901199 1 19990910 A 5532 SKIN DOUG DC9 DC982 3022082 WP VERT STAB PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A HOLE THROUGH SKIN AND RIB OF VERTICAL STABILIZER AFT UPPER STRINGER TIP FAIRING. THE RIB AND SKIN WE RE REPAIRED IAW SRM 55-01, FIGURES 2 & 4. 2 L 7 2 4F A6WE 1999091700496 19990917 00496 WP 1999 9 17 CALA9901200 1 19990912 A 5532 9911834261 PANEL DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND CRACKS IN VERTICAL STABILIZER PANEL NR 6404. THE CRACKS WERE 1-2 INCHES LONG. THE PANEL WAS REMOVED AN D A NEW PANEL WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999091700497 19990917 00497 1999 9 17 COMA9910146 4 19990910 A 3160 3069001017 ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 159A 11919 1159 TAKEOFF WAS ABORTED DUE TO MULTIPLE ERRATIC WARNINGS ON ANNUNCIATOR. REPLACED THE ANNUNCIATOR PANEL ASSEMBLY. 2 L 7 2 4T RT A31SO 1999091700498 19990917 00498 EA 1999 9 17 COMA9960510 1 19990910 A 3620 355523255 SENSE ELEMENT CNDAIR CL600 CL6002B19 EA BLEED AIR FAILED A COMA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 964CA 7129 ANTI-ICE DUCT WARNING MESSAGE DURING POSITIONING OF AIRCRAFT FOR TAKEOFF. REPLACED BLEED LEAK SENSING ELEMENT A40WK. 2 L 7 2 4F RT A21EA 1999091700499 19990917 00499 NE 1999 9 17 COMA9960511 2 19990910 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT FAILED A COMA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 01 967CA 7134 807416 DURING CRUISE FLIGHT AFTER DEPARTING FROM IAD, THE HOT WARNING ACTIVATED FOR THE RIGHT ENGINE, THE RIGHT ENGINE WAS SHU TDOWN INFLIGHT AND AIRCRAFT CONTINUED DESTINATION FLIGHT TO CVG WHERE AN EMERGENCY WAS DECLARED. FOUND THE RIGHT ENGINE CONTAMINATED WITH METAL CHIPS, REPLACED THE RIGHT ENGINE ASSEMBLY. 2 L 7 2 4F 4 F RT A21EA E15NE 1999091700500 19990917 00500 EA 1999 9 17 COMA9960512 1 19990913 A 2751 FAIL LIGHT CNDAIR CL600 CL6002B19 EA RT TE FLAP ILLUMINATED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 01 729CA 7265 FLAP FAIL CAUTION ACTIVATED AT 20 DEGREES FLAP POSITION. COMPLIED WITH AD98-20-01, PARAGRAPH (B), 3, (D AND E) 4. 2 L 7 2 4F RT A21EA 1999091700501 19990917 00501 EA 1999 9 17 COMA9960513 1 19990913 A 3350 645 LIGHT CNDAIR CL600 CL6002B19 EA ROW 5-8 FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 932CA 7038 DURING PRE-FLIGHT INSPECTION, FOUND KNEE LEVEL EMERGENCY LIGHTING INOPERATIVE BY RIGHT OVERWING EXIT AND FLOOR EMERGENCY LIGHTING ROW 5 THROUGH 8. REPLACED POWER STRIP FOR ROW 5 THROUGH 8. 2 L 7 2 4F RT A21EA 1999091700502 19990917 00502 EA 1999 9 17 COMA9960514 1 19990913 A 2751 FAIL LIGHT CNDAIR CL600 CL6002B19 EA RT TE FLAP ILLUMINATED A COMA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 SO 01 729CA 7265 FLAP FAIL CAUTION ACTIVATED AT 20 DEGREES FLAP POSITION. COMPLIED WITH AD 98-20-01, PARAGRAPH (B) 3, (D AND E) 4. 2 L 7 2 4F RT A21EA 1999091700503 19990917 00503 EA 1999 9 17 COMA9960515 1 19990913 A 2751 FAIL LIGHT CNDAIR CL600 CL6002B19 EA RT TE FLAP ILLUMINATED A COMA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 01 729CA 7265 FLAP FAIL CAUTION ACTIVATED AT 20 DEGREES FLAP POSITION. COMPLIED WITH AD 98-20-01, PARAGRAPH (B) 3, (D AND E) 4. 2 L 7 2 4F RT A21EA 1999091700504 19990917 00504 EA 1999 9 17 COMA9960516 1 19990913 A 3350 64645 LIGHT CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779CA 7306 EMERGENCY LIGHTS AFT OF THE EXIT ROW ARE INOPERATIVE. REPLACED THE AFT FLOOR LIGHTING CARRIER STRIP. 2 L 7 2 4F RT A21EA 1999091700505 19990917 00505 EA 1999 9 17 COMA9960517 1 19990913 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT WING FAILED A COMA D RETURN TO BLOCK N FALSE WARNING AP APPROACH 1 SO 01 729CA 7265 FLAP FAIL CAUTION ACTIVATED AT 22 DEGREES FLAP POSITION. REPLACED THE LEFT BRAKE POSITIONING SENSING UNIT. 2 L 7 2 4F RT A21EA 1999091700506 19990917 00506 EA 1999 9 17 COMA9960518 1 19990913 A 2751 FAIL LIGHT CNDAIR CL600 CL6002B19 EA RT TE FLAP ILLUMINATED A COMA K NONE N FALSE WARNING DE DESCENT 1 SO 01 729CA 7265 FLAP FAIL CAUTION ACTIVATED AT 20 DEGREES FLAP POSITION. COMPLIED WITH AD 98-20-01, PARAGRAPH (B) 3, (D AND E) 4. 2 L 7 2 4F RT A21EA 1999091700507 19990917 00507 EA 1999 9 17 COMA9960519 1 19990913 A 5330 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 139.54 CRACK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 LEFT WING FUEL ACCESS HOLE AT POSITION 540 FB HAS A CRACK O/B HORIZONTAL SURFACE. REPAIRED CRACK IAW BOMBARDIER REO NR 601R-5721-030. 2 L 7 2 4F RT A21EA 1999091700508 19990917 00508 NM 1999 9 17 QXEA9901880 1 19990907 A 3350 6104789 BATTERY DHAV 6038443 DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 357PH 3519 504 SEA - REAR CABIN OVERHEAD EMERGENCY LIGHTS STOP WORKING AFTER 10 SECONDS. REMOVED AND REPLACES BATTERY. OVERHEAD EMERG ENCY LIGHTS OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999091700509 19990917 00509 NM 1999 9 17 QXEA9901881 1 19990910 A 3350 1013079 LIGHT DHAV 825200977011 DHAV DHC8 DHC8202 2809007 NM ROW 8 INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 364PH 524 PDX - EMERGENCY ESCAPE PATH LIGHT AT ROW 8 INOPERATIVE. REPLACED ESCAPE PATH LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999091700510 19990917 00510 EU 1999 9 17 QXEA9901882 1 19990907 A 3242 50040702 BRAKE FOKKER F28 F28MK4000 4990810 EU LT MLG INOP A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 4979 11159 SEA - LEFT BRAKE FEELS AS IF ANTI-SKID IS RELEASING PRESSURE INTERMITTANTLY ON LANDING. CHECKED ANTI-SKID. FOUND NUMBE R TWO BRAKE HOT. REPLACED NUMBER TWO BRAKE ASSEMBLY. TAXI CHECK, ANTI-SKID AND BRAKES OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1999091700511 19990917 00511 EU 1999 9 17 QXEA9901883 1 19990909 A 3350 521271 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 28505 11231 GEG - FORWARD GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPLACED CIRCUIT BOARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1999091700512 19990917 00512 EU 1999 9 17 QXEA9901884 1 19990911 A 3350 900542 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU ROW 4 INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 GEG - OVERHEAD EMERGENCY LIGHT AT ROW FOUR WILL NOT EXTINGUISH. REPLACED BATTERY POWER SUPPLY AT ROW 4. LIGHTS CHECK G OOD. 2 L 7 2 4F RT A20EU 1999091700513 19990917 00513 EU 1999 9 17 QXEA9901885 1 19990910 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 SEA - GASH AND DENT IN FUSELAGE SKIN, JUST AFT OF MAIN CABIN DOOR. DAMAGED NOTED 70 MILLIMETERS IN LENGTH FORMING TWO D ENTS, .1 INCHES AND .045 INCHES IN DEPTH. DAMAGE OUT OF LIMITS. AIRCRAFT SAFE FOR FERRY FLIGHT. REPAIRED AS REQUIRED. 2 L 7 2 4F RT A20EU 1999091700514 19990917 00514 WP 1999 9 17 99FDEA00385 1 19990913 A 3620 SWITCH DOUG DC10 DC1030 3023501 WP NR 1 MANIFOLD FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 318FE 46837 AT LEVEL 290 GOT A NR 1 MANIFOLD FAIL LIGHT. REPLACED MANIFOLD FAILURE DETECTION PRESSURE SWITCH AS PER AMM 36-23-03-4. PERFORMED OPS CHECK PER MM 30-11-00-2, MM 36-23-03. OPS CHECK GOOD. 2 L 7 3 4F A22WE 1999091700515 19990917 00515 NM 1999 9 17 99UAL900461 1 19990906 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOP A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 120UA 29166 EMERGENCY LIGHT IN CEILING NEXT TO DOOR 3 LEFT, INOP. RELAMPED CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 1999091700516 19990917 00516 1999 9 17 99UAL900462 4 19990904 A 2370 RDAX4322 AUDIO BOX DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE ROW 32C FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 1858U 46987 ELECTRICAL SMELL AROUND SEAT 33, 32, 34 LEFT SIDE OF AC. PAX CLAIMS SMELLS WAS STRONG FOR FEW SECONDS THEN DISAPPEARED. PAX 32C LOOSE OVERHEAD LIGHTS AND AUDIO. *S/D* SEAT ELECTRONIC BOX FAILED AT SEAT 32C. REPLACED SEAT ELECTRONIC BOX AT 32C, OPS CHECK NORMAL AND NO ODOR NOTED. 2 L 7 3 4F 4 F A22WE E23EA 1999091700517 19990917 00517 NE 1999 9 17 99UAL900463 2 19990901 A 7200 ENGINE AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE NR 2 FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 802UA 690 V10094 JUST PRIOR TO GEAR EXT, STRONG ODOR (LIKE HOT A-C DUCT) PERMEATED CABIN CAUSING BURNING EYES AND NOSE. AFTER EXTENSIVE TROUBLESHOOTING AND REPLACEMENT OF TWO ENGINES, AN OIL RESIDUE AND FINE WHITE METALLIC POWDER RESIDUE WAS FOUND IN THE N R 2 IAE V2500, ENGINE BLEED DUCTS. THIS ENGINE WAS SENT TO LUFTHANSA FOR TEAR DOWN (ENGINE ORDER NUMBER G452) AND INSPE CTION FINDINGS WILL BE RECORDED OUTLINING THE CAUSE OF THE REMOVAL. NO FINDINGS HAVE BEEN IDENTIFIED TO DATE, HOWEVER T HERE HAS BEEN NO RECURRENCE OF THIS DISCREPANCY (ODOR IN CABIN) SINCE SEPTEMBER 10, 1999 WHEN THE ENGINE WAS REMOVED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999091700518 19990917 00518 1999 9 17 99UAL900464 4 19990906 A 3460 FWC AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E&E COMP MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 419UA 487 F/O PITOT, TAT PROBES AND AUTO THROTTLE APPEAR ON STATUS PAGE ACCOMPANIED BY STALL WARNING AND AUDIBLE OVERSPEED WARNING SPURIOUSLY AT FL 370, MACH .79 TO .80. FOR LAST 40 TO 50 MINS OF FLIGHT STALL WARNING AND OVERSPEED CONTINUOUSLY. *S/D * FAULT COULD NOT BE DUPLICATED ON GROUND TESTS. ALL FLIGHT COMPUTERS WERE RESET AND AIRCRAFT RETURNED TO SERVICE. FW C 2 DID FAULT ON FOLLOWING TRIP. THE FWC WAS RESET AND AIRCRAFT HAS OPERATED NORMALLY WITHOUT FAULTING. 2 L 7 2 4F 4 F RT A28NM E40NE 1999091700519 19990917 00519 NM 1999 9 17 99UAL900465 1 19990905 A 2910 COUPLING AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE YELLOW HYD SYS LOOSE A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 812UA 850 DIVERTED TO DEN DUE TO LOW HYDRAULIC QUANTITY. *S/D* FOUND A COUPLING LOOSE. RETIGHTENED AND REPLACED AN O-RING ON RE TURN LINE. 2 L 7 2 4F 4 F RT A28NM E40NE 1999091700520 19990917 00520 NM 1999 9 17 99UAL900466 1 19990907 A 3244 TIRE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE NLG FAILED A UALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 29 828UA 1031 ON TAKEOFF CREW HEARD A LOUD BANG AND ANOTHER AIRCRAFT OBSERVED DEBRIS DEPARTING AIRCRAFT. SAN AIRPORT RECOVERED TIRE D EBRIS FROM RUNWAY. LEFT NOSE LANDING GEAR TIRE TREAD SEPARATED ON DEPARTURE. FLIGHT DIVERTED TO LAX UNDER AMBER ALERT. *S/D* LT NLG TIRE TREAD SEPARATED ON DEPARTURE. LEFT NOSE TIRE ON ARRIVAL FOUND TREAD MISSING. REPLACED LEFT NOSE A ND RIGHT NOSE TIRE PER MM 32-41-12. 2 L 7 2 4F 4 F RT A28NM E40NE 1999091700521 19990917 00521 NM 1999 9 17 99UAL900467 1 19990904 A 2720 YAW DAMPER HONEYWELL 10622532 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AUTO PILOT MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 357UA 99030753 24378 AIRCRAFT EXPERIENCED A SHARP YAW TO LEFT ON RUNWAY JUST PRIOR TO V1. YAW DAMP WAS ENGAGED AT THE TIME. THE YAW DAMPER COUPLER WAS REPLACED AND SENT TO HONEYWELL IN SEATTLE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999091700522 19990917 00522 1999 9 17 99UAL900468 4 19990909 A 2210 422081100 TRANSDUCER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AUTO PILOT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 29 432UA 587 IN CRUISE WITH AUTOPILOT 2 ENGAGED, AIRCRAFT EXPERIENCED AN UNCOMMANDED PITCH UP AND A SUBSEQUENT ELEVATOR AND AILERON C OMPUTER 2 PITCH FAULT DISPLAY ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING UNIT. AUTOPILOT 1 OPERATES NORMALLY. FLIGHT DIVERTED TO PIT. THE ACTUATOR POSITION TRANSDUCER WAS FAULTY (FAULT WAS ELAC 2 THS 9CE). TRANSDUCER IS NON-STO CK. THE THS ELECTRONIC MODULE AND TRANSDUCER WERE REPLACED. THE AIRCRAFT HAD NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A28NM E40NE 1999091700523 19990917 00523 NM 1999 9 17 99UAL900469 1 19990903 A 5320 SILL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CARGO DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7445U 21899 CORROSION DAMAGE WAS FOUND ON THE OUTBOARD CHORD OF THE AFT CARGO DOOR LOWER SILL. THE DAMAGED AREA WAS CUT OUT AND REP AIRED WITH A STRIP AND ANGLE REPAIR PER TIMCO REO-06703 REPAIR INSTRUCTIONS. THE REPAIR WAS APPROVED BY FAA FORM 8110-3 . 2 L 7 3 4F 4 F A3WE E2EA 1999091700524 19990917 00524 WP 1999 9 17 ABXA9900702 1 19990910 A 5250 AR25291GR41 LATCH DOUG DC9 DC932 3022066 WP COCKPIT DOOR BROKEN A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 900AX 47380 COCKPIT DOOR WOULD NOT OPEN FROM INSIDE COCKPIT. REPLACED COCKPIT DOOR HANDLE ASSY IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999091700525 19990917 00525 WP 1999 9 17 ABXA9900703 1 19990910 A 5313 27779223 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON 13 RIGHT CRACKED AT STATION 945. SPLICED LONGERON 13 RIGHT IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999091700526 19990917 00526 WP 1999 9 17 ABXA9900704 1 19990910 A 5313 591140517 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON 2 LEFT CRACKED AT STATION 200. REPLACED LONGERON 2 LEFT FROM STATION 194 TO 230 IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999091700527 19990917 00527 WP 1999 9 17 ABXA9900705 1 19990910 A 5313 59114277 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPLACED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999091700528 19990917 00528 WP 1999 9 17 ABXA9900706 1 19990910 A 5711 5911301506 SPAR CAP DOUG DOUG DC9 DC931 3022065 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND RIGHT WING LOWER SPAR CRACKED. REPAIRED IAW DC9 DRAWINGS M07181 AND J060173. 2 L 7 2 4F A6WE 1999091700529 19990917 00529 WP 1999 9 17 ABXA9900707 1 19990910 A 5711 5911301506 SPAR CAP DOUG DOUG DC9 DC931 3022065 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND RIGHT WING AFT LOWER SPAR CRACKED AT HOLE NR 4. REPAIRED IAW DC9 SERVICE REWORK DRAWING J060123 A ND ABX DRAWING M07181. 2 L 7 2 4F A6WE 1999091700530 19990917 00530 WP 1999 9 17 ABXA9900708 1 19990914 A 5755 5910055515 PANEL DOUG DOUG DC9 DC941 302207N WP LT SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND LEFT OUTBOARD SPOILER DELAMINATED AT INBOARD FORWARD CORNER. REPLACED SPOILER PANEL IAW DC9 MM 27 -61-1. 2 L 7 2 4F A6WE 1999091700531 19990917 00531 WP 1999 9 17 MWEA99596 1 19990913 A 5210 9955792501 SKIN DOUG DC9 DC914 3022034 WP PAX DOOR MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 FOUR OVERSIZED HOLES IN THE PASSENGER DOOR SKIN JUST ABOVE NR 1 BEAM, AFT SIDE. SPLICED NEW SECTION OF SKIN PER BOEING TELEX NR MWX-ORD-99-00099H. 2 L 7 2 4F A6WE 1999091700532 19990917 00532 WP 1999 9 17 MWEA99597 1 19990913 A 5320 59160641 FITTING DOUG DC9 DC914 3022034 WP BS 466-488 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 500ME 45711 LONGERON 30 END FITTING FROM STATION 466-488 HAS 2 MISDRILLED HOLES. INSTALLED NEW END FITTING. 2 L 7 2 4F A6WE 1999091700533 19990917 00533 WP 1999 9 17 MWEA99598 1 19990913 A 5210 9955752 BEAM DOUG DC9 DC914 3022034 WP PAX DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 TOOL MARKS PASSENGER DOOR, UPPER FORWARD INNER STRUCTURE, BOTTOM SIDE OF NR 1 HORIZONTAL BEAM. FABRICATED AND INSTALLED NEW BEAM. 2 L 7 2 4F A6WE 1999091700534 19990917 00534 WP 1999 9 17 MWEA99599 1 19990912 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP GALLEY DR SLIDE LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 301ME 47190 COVER FOR GALLEY SLIDE PARTIALLY OFF ITS FITTING. REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999091700535 19990917 00535 NM 1999 9 17 DHL99740003 1 19990914 A 2611 SMOKE LIGHT BOEING 727 7272Q9 138448M NM CARGO COMPT LOOSE A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 740DH 21930 CARGO SMOKE LIGHT CAME ON IN FLIGHT. DIVERTED TO GEG. INSPECTED ALL SIX SMOKE DETECTOR LIGHTS, FOUND NR 6 BEACON LOOSE . RESECURED BEACON LIGHT, OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1999091700536 19990917 00536 NM 1999 9 17 VNAA9909002 1 19990911 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7-10 DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 432JS 6757 1870 3045 THE CABIN EMERGENCY LIGHTS FROM ROWS 7 TO 10 AND THE LT EMERGENCY EXIT SIGN WERE FOUND TO OPERATE INTERMITTENTLY BY THE FLIGHT CREW. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY LOCATED AT POSITION 6LK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATION CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999091700538 19990917 00538 EU 1999 9 17 RAIA990632 1 19990622 A 2910 NTA152504 O-RING AEROSP ATR42 ATR42300 8680920 EU HYDRAULIC BAY FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 424TE 124 STL - FLT 7152 - GREEN HYDRAULIC PUMP LOW LEVEL LIGHT ILLUMINATED. MAINTENANCE REPLACED O-RING ON PRESSURE SWITCH. (X) 2 H 7 2 4T RT A53EU 1999091700539 19990917 00539 WP 1999 9 17 VTZA9907733 2 19990421 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT FAILED A VTZA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 EA 27 488UE 907 BGM\IAD - FLT 7599 - DURING APPROACH, LEFT ENGINE FAILED IN-FLIGHT, ZERO PERCENT TO 50 PERCENT RPM, SRL, FUEL OIL PRESSU RE CAPTIONS. ENGINE FAILED WITH ANTI-ICE AND IGN ON. MAINTENANCE ADJUSTED FLIGHT IDLE FUEL FLOW AND MAX POWER ON LT EN GINE AND PERFORMED ENGINE RUNS. ALL ENGINE PARAMETERS WITHIN NORMAL OPERATING LIMITS. ALSO, INSPECTED FUEL SUMP FOR CO NTAMINATION, CHECKED GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1999091700540 19990917 00540 NM 1999 9 17 UIEA9926 1 19990529 A 7810 314U210057 NOZZLE BOEING 747 74747UF 1384949 NM NR 2 ENGINE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 493MC 2776 417 29254 EXHAUST NOZZLE CRACKED AT CIRCUMFERENTIAL SEAM WELD, NR 2 ENGINE 11 O'CLOCK POSTION 8 INCH LENGTH AFT END. REPLACED. ( X) 2 L 7 4 4F RT 1384945 1999091700541 19990917 00541 NM 1999 9 17 UIEA9928 1 19990604 A 2612 FIRE WARNING BOEING 747 74747UF 1384949 NM COCKPIT ACTIVATED A UIEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 15 494MC 29255 FLT FX076 - TAKEOFF ABORTED AT 138 KNOTS DUE FIRE WARNING ALARM (AURAL AND VISUAL). AFTER REJECTED TAKEOFF (THROTTLES I DLE, FULL REVERSE, MAX BRAKING) NO FURTHER INDICATION. WAS UNABLE TO DETERMINE WHICH ENGINE CAUSED WARNING. INSPECTED ALL ENGINES AND NO DAMAGE FOUND. PERFORMED CHAPTER 5 HIGH ENERGY STOP INSPECTION AND CMC GROUND TEST, NO ABNORMALTIES N OTED. PERFORMED ENGINE RUN-UP AND WAS UNABLE TO DUPLICATE DISCREPANCY. NO CMC MESSAGES RECORDED IN PLF (PRESENT LEG FA ULTS) OR EF (EXISTING FAULTS). (X) 2 L 7 4 4F RT 1384945 1999091700542 19990917 00542 NM 1999 9 17 99ZZZX3446 1 19990601 A 7722 15BL801C EGT INDICATOR BOEING 727 7272J0 138407E NM NR 3 ENGINE FAILED A RIVA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 362PA 21106 APPROXIMATELY TEN MINUTES AFTER TAKEOFF FROM EWR, NR 3 EGT GAUGE QUIT WORKING. AIRCRAFT RETURNED TO EWR. REMOVED AND R EPLACED NR 3 EGT INDICATOR. OPERATIONAL CHECK SATISFACTORY. 2 L 7 3 4F RT A3WE 1999091700543 19990917 00543 NM 1999 9 17 99ZZZX3447 1 19990721 A 3397 WIRE BOEING 727 7272J0 138407E NM CABIN STRIPPED A RIVA K NONE L NO TEST IN INSP/MAINT 1 SO 17 362PA 21106 DURING DAILY CHECK, SECTION OF EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE RESULTING IN A 30-MINUTE DELAY. A STRIPPED WIRE WAS FOUND IN THE EMERGENCY PATH LIGHTING. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECK WAS GOOD. 2 L 7 3 4F RT A3WE 1999091700544 19990917 00544 WP 1999 9 17 G6OA033 1 19990624 A 7120 MOUNT DOUG DC10 DC1030F 3023504 WP NR 1 ENGINE LOOSE A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 600GC 46965 DURING C-CHECK INSPECTION, NR 1 ENGINE FORWARD MOUNT WAS FOUND SLIGHTLY SEPARATED. FURTHER INVESTIGATION FOUND NUT/BOLT LOOSENED FROM EACH OTHER WHICH ALLOWED THE MOUNTING BRACKET TO SEPARATE. INSPECTED AND RE-WORKED PER EO 99-5415-026. R E-INSTALLED ENGINE, PERFORMED LEAK CHECKS AND POWER ASSURANCE RUN IAW JC105 AND MM 71-06-00. (X) 2 L 7 3 4F RT A22WE 1999091700545 19990917 00545 SO 1999 9 17 C2XA99IA345 1 19990626 A 3350 GE1317 BULB EMB 145 EMB145 SO EMERGENCY EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14959 145091 IAH - FLT 4173 - THE PILOT REPORTED THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED LIGHT BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999091700546 19990917 00546 NM 1999 9 17 BJNA990602 1 19990623 A 3350 582214 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERABLE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 CENTER SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERABLE. REMOVED AND REPLACED CENTER SECTION FLOOR TRACK LIGHTING P ER LUMINESCENT SYSTEM MANUAL 33-50-01 PAGE 106. (X) 2 L 7 2 4F RT A16WE 1999091700547 19990917 00547 NM 1999 9 17 BJNA990603 1 19990623 A 3350 LIGHT BOEING 737 737282 13844AT NM L1 DOOR INOPERABLE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 L2 DOOR EMERGENCY LIGHT INOPERABLE (EXTERIOR). CLEANED LIGHT SOCKET. LIGHT NOW WORKS IAW 33-51-61. (X) 2 L 7 2 4F RT A16WE 1999091700550 19990917 00550 EA 1999 9 17 ASOA99055 1 19990625 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A ASOA A B F UNSCHED LANDING EMER. DESCENT ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 11 841AS 7300 FLT 4737 - CARGO SMOKE WARNING ISSUED 3 TIMES, THEN AFTER A SHORT INTERVAL, A 4TH CARGO SMOKE WARNING WAS ISSUED. RAN C ARGO SMOKE CHECK LIST, FIRED FIRE EXTINGUISHERS, DECLARED AN EMERGENCY, DIVERTED TO MEM. LANDED SAFELY AND EVACUATED AI RCRAFT ON DE-ICE PAD. THERE WAS NO EVIDENCE OF SMOKE OR FIRE - FALSE INDICATION. MAINTENANCE REPLACED CARGO COMPARTMEN T FORWARD AND AFT SMOKE DETECTORS, FIRE EXTINGUISHERS AND SQUIBS. ALL SYSTEM OPS CHECKED GOOD, AND AIRCRAFT RELEASED FO R SERVICE. THIS MRR REMAINS OPEN PENDING SHOP REPORT ON SMOKE DETECTORS. (X) 2 L 7 2 4F RT A21EA 1999091700556 19990917 00556 NM 1999 9 17 AALA990831 1 19990604 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 184AN 29594 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FORWARD SECTION OF COACH INOPERATIVE. REPLACE D EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999091700557 19990917 00557 NM 1999 9 17 AALA990844 1 19990609 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROWS 26-30 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 396AN 29603 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 25B THROUGH 30B INOPERATIVE. RE-SECURED CONNECTOR AT SEAT 25A. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999091700558 19990917 00558 1999 9 17 AALA990773 4 19990826 A 2397 WIRE COLLINS BOEING 777 777223 1385213 NM ROW 27AB FAILED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 771AN 29579 DFW - FLT T0051 - AFTER TAKEOFF LGW WHILE EN ROUTE TO DFW, CREW SMELLED ELECTRICAL SMOKE AT SEATS 27A AND 27B. ENTERTAI NMENT UNITS AT BOTH SEATS AUTOMATICALLY SHUT DOWN AND SMELL DISSIPATED. LANDED DFW WITHOUT INCIDENT. DE-ACTIVATED SEAT S 27A AND 27B, DEFERRED PER PRIORITY DEFERRAL LIST. REPLACED AUDIO VIDEO UNIT CABLE AT AUDIO VIDEO UNIT SEAT 27. (X) 2 L 7 2 4F RT T00001SE 1999091700559 19990917 00559 NM 1999 9 17 AALA990734 1 19990521 A 3350 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY EXIT PINS UNSEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 775AN 29584 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS INOPERATIVE. RESET PIN IN EMERGENCY EXIT LIGHT CONNECTOR. SY STEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 1999091700560 19990917 00560 NM 1999 9 17 AALA990733 1 19990521 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY EXIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 775AN 29584 DFW - DURING OVERNIGHT EMERGENCY EXIT LIGHT INOPERATIVE. RE-CONNECTED WIRES TO EMERGENCY EXIT LIGHT SYSTEM. SYSTEM GRO UND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 1999091700561 19990917 00561 NM 1999 9 17 AALA990783 1 19990530 A 3350 CONNECTOR BOEING 777 777223 1385213 NM ROW 20CG LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 775AN 29584 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20C AND 20G INOPERATIVE. TIGHTENED EMERGENCY EXIT LIGH T CONNECTOR UNDER SEAT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 1999091700562 19990917 00562 NM 1999 9 17 A6WA9900007 1 19990303 A 2120 AIR DISTRIBUTION DORNER DO32 DO328100 2996000 NM CABIN SMOKE A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 330PH 3008 DEN - FLT 7131 - CABIN FILLED WITH SMOKE AT ENGINE SHUT-DOWN. INSPECTED PACKS, FOUND NO DISCREPANCIES. GROUND RAN AIRC RAFT 15 MINUTES, COULD NOT DUPLICATE. NO CAS MESSAGE, SYSTEM OPS CHECK NORMAL. (X) 2 H 7 2 4T RT A45NM 1999091700564 19990917 00564 NM 1999 9 17 A6WA9900005 1 19990219 A 2421 ALTERNATOR DORNER DO32 DO328100 2996000 NM NR 1 AND 2 FAILED A A6WA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 31 334PH 3012 AFTER SECURING NR 1 ENGINE, EXPERIENCED NR 1 AND NR 2 ALTERNATOR FAILURE. PER CHECKLIST, RESET NR 2 ON-LINE FOR 2-3 MIN UTES. EXPERIENCED SECONDARY FAILURE. GUC - FLT 7133 - RAN AIRCRAFT FOR 10 MINUTES. COULD NOT DUPLICATE. OPS CHECK GO OD. (X) 2 H 7 2 4T RT A45NM 1999091700565 19990917 00565 EA 1999 9 17 A6WA9900006 1 19990304 A 3520 MASK CNDAIR CL600 CL6002B19 EA CABIN DEPLOYED A A6WA G O2 MASK DEPLOYED O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 MEM - FLT 7615 - UPON ARRIVAL AT AIRCRAFT, FOUND ALL PASSENGER OXYGEN MASKS DEPLOYED. RE-STOWED ALL OXYGEN MASKS AND PE FORMED OPERATIONAL CHECK OF OXYGEN MASKS, PERFORMED IAW CRJ MM 35-21-09. NO DEFECTS NOTED. (X) 2 L 7 2 4F RT A21EA 1999091700566 19990917 00566 EA 1999 9 17 A6WA9900090 1 19990729 A 5210 DOOR CNDAIR CL600 CL6002B19 EA PASSENGER COMPT OUT OF ADJUST A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401AW 7280 MEM - FLT 5617 - PASSENGER DOOR CAUTION ILLUMINATED AFTER TAKEOFF, RETURNED TO MEMPHIS. AFTER LANDING, COULD NOT CLOSE DOOR PROPERLY. RE-ADJUSTED REAR SPIGOT TO OBTAIN PROPER GAP PER AMM. (X) 2 L 7 2 4F RT A21EA 1999091700567 19990917 00567 EA 1999 9 17 A6WA9900089 1 19990728 A 3244 26104851 TIRE CNDAIR CL600 CL6002B19 EA NLG FAILED A A6WA K NONE O OTHER LD LANDING 1 GL 31 401AW 7280 JAN - FLT 5520 - ON LANDING, NOSE TIRE BLEW WITH VIBRATION AND CLUNKING NOISE IN WHEELWELL. REMOVED AND REPLACED NOSE T IRE. INSPECTED UNDERSIDE OF AIRCRAFT AND NOSE GEAR WHEELWELL. NO DEFECTS NOTED. (X) 2 L 7 2 4F RT A21EA 1999091700568 19990917 00568 EA 1999 9 17 A6WA9900081 1 19990718 A 5210 LATCH MECH CNDAIR CL600 CL6002B19 EA PASSENGER DOOR NOT LATCHED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401AW 7280 DEN - FLT 5558 - IN CLIMB EDI MSG. DOOR LATCH CAUTION. SHORTLY FOLLOWED BY EDI MSG DOOR LATCH WARNING. F/A CONFIRMED TOP TWO LATCHES NOT ALIGNED. PERFORMED OPS CHECK IAW MM, CHECKS GOOD. WILL PERFORM TEST FLIGHT. TEST FLIGHT SUCCESSFU L. (X) 2 L 7 2 4F RT A21EA 1999091700569 19990917 00569 EA 1999 9 17 A6WA9900079 1 19990701 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF ADJUST A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 401AW 7280 DEN - FLT 5618 - PASSENGER DOOR LATCH CAS MESSAGE. PERFORMED PASSENGER DOOR FUNCTIONAL TEST. MOVED AFT UPPER LATCH DOW N ONE SERRATION. DOOR OPS CHECK GOOD. (X) 2 L 7 2 4F RT A21EA 1999091700570 19990917 00570 EA 1999 9 17 A6WA9900044 1 19990512 A 2750 85501009 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A A6WA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 31 401AW 330 0958A 7280 DEN/MEM - FLT 5616 - 'FLAP FAIL' CAUTION AT 29,000 FEET. CRUISE FLIGHT WITH NO FLAP SELECTION. LANDING MADE WITH ZERO FLAPS AT 174 KNOTS. FERRIED AIRCRAFT TO DEN. REMOVED AND REPLACED LEFT BRAKE POSITION SENSOR UNIT (BPSU). PART TOTAL CYCLES: 230. (X) 2 L 7 2 4F RT A21EA 1999091700571 19990917 00571 EA 1999 9 17 A6WA9900043 1 19990511 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 401AW 7280 MSN/DEN - FLT 5537 - 'FLAP FAIL' MESSAGE IN CRUISE AT 35,000 FEET. NO SELECTION HAD BEEN MADE, LANDING SPEED 167 KNOTS WITH ZERO FLAPS. C/W SUPPLEMENT 98-18. NO TWISTING OF FLAPS EVIDENT. CLEARED FAULT BY DEPOWERING A/C, CYCLED FLAPS NU MEROUS TIMES. NO FURTHER DISCREPANCIES. TEST FLIGHT COMPLETED SATISFACTORILY. (X) 2 L 7 2 4F RT A21EA 1999091700574 19990917 00574 SO 1999 9 17 C2XA99IA353 1 19990702 A 3350 110049 BATTERY CHARGER EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13964 145123 IAH - DURING PRE-FLIGHT INSPECTION, CREW REPORTED THE LEFT AFT EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 MM 33-50-04 AND 33-50-07, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1999091700575 19990917 00575 WP 1999 9 17 EIAA990179 1 19990630 A 3244 9550267 TIRE DOUG DC9 DC933F 302207A WP NLG FAILED A EIAA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 NM 09 944F 47194 ON TAKEOFF ROLL AT APPROXIMATELY 60 - 80 KNOTS, AIRCRAFT EXPERIENCED SEVERE VIBRATION. APPEARED TO BE COMING FROM NOSE WHEEL. TAKEOFF ABORTED AND VIBRATIONS TOPPED AT APPROXIMATELY 25 KNOTS. (X) 2 L 7 2 4F A6WE 1999091700576 19990917 00576 CE 1999 9 17 99ZZZX3457 1 19990716 A 5610 1013840257 WINDSHIELD BEECH 200 B200 1152922 CE LT COCKPIT CRACKED A FFSA K NONE O OTHER CR CRUISE 1 AL 01 575T BB1384 PILOT'S WINDSHIELD CRACKED IN-FLIGHT ON GAL/FAI LEG. LANDED AT FAI. 1 L 7 2 4T A24CE 1999091700577 19990917 00577 CE 1999 9 17 99ZZZX3458 1 19990705 A 5610 12950251 WINDSHIELD BEECH 1900 1900C 1154161 CE LT COCKPIT CRACKED A FFSA K NONE O OTHER CR CRUISE 1 AL 01 575Q UC160 PILOT'S WINDSHIELD CRACKED IN-FLIGHT. LANDED AT GAL. NOT E: WINDSHIELD HUMP SEALS HAD BEEN REPLACED ON 6-23-99. 2 L 7 2 4T RT A24CE 1999091700578 19990917 00578 WP 1999 9 17 GTIA9900882 1 19990607 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY EXIT INOPERABLE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 133NK 14321 48111 MLG - FLT 409 - DURING DAILY, FOUND AFT EMERGENCY EXIT LIGHTS INOPERABLE. REMOVED AND REPLACED OUTBOARD RIGHT AFT IN RI GHT LAVATORY POWER SUPPLY AND BATTERY CHANGE UNIT. OPS CHECK GOOD IAW 33-50-00. (X) 2 L 7 2 4F A6WE 1999091700579 19990917 00579 WP 1999 9 17 GTIA9901034 1 19990804 A 4990 OIL LINE DOUG DC9 DC981 3022081 WP APU LOOSE A GTIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 GL 23 981SB 48058 DTW - FLT 629 - FUMES IN CABIN AFT LAVATORY, SMOKE DETECTORS ALARM ON. INSPECTED, FOUND OIL LINE LOOSE ON THE APU WHIC H WAS FEEDING FUMES INTO THE PACKS. TIGHTENED OIL LINE IAW MD80 MM 49-90-0. INSPECTED, OPERATIONAL CHECK GOOD AT THIS TIME. (X) 2 L 7 2 4F A6WE 1999091700580 19990917 00580 WP 1999 9 17 GTIA9900986 1 19990713 A 3350 LIGHT DOUG DC9 DC983 3022083 WP ROWS 6-16 INOPERABLE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 DTW - EMERGENCY EXPRESS LIGHTS ROWS 6-16 DO NOT ILLUMINATE. PERFORMED OPERATION CHECK, OPERATION CHECKED GOOD IAW MD-80 MM 33-50. (X) 2 L 7 2 4F RT A6WE 1999091700581 19990917 00581 1999 9 17 GLBA99024 4 19990625 A 2210 6229627005 COMPUTER BEECH 1900 1900D 1154162 CE YAW DAMPER INOPERABLE A GLBA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CE 01 192GL 8952 287 UE192 RUDDER HAD FULL DEFLECTION WHEN YAW DAMPER ENGAGED. REPLACED YAW DAMPER COMPUTER. (X) 2 L 7 2 4T RT A24CE 1999091700582 19990917 00582 WP 1999 9 17 HALA9900138 1 19990618 A 3260 PROXIMITY BOX DOUG DC9 DC951 3022051 WP LANDING GEAR FAILED A HALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 649HA 47715 AFTER GEAR-UP, ALL THREE RED UNSAFE LIGHTS STAYED ON. CYCLED GEAR, LIGHTS STAYED ON. REPLACED PROXIMITY BOX. OPERATIO NAL TEST OF GEAR LIGHTS TEST OK. (X) 2 L 7 2 4F RT A6WE 1999091700583 19990917 00583 EA 1999 9 17 MASA99107 1 19990628 A 3350 GE1683 BULB BRUCE CNDAIR CL600 CL6002B19 EA LT EXTERIOR FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77278 7278 FLT 5122- LGA-CMH - THE CAPTAIN REPORTED LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE WAS DEFERRED PE R MEL 33-51-2. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, REMOVED AND REPLACED THE BULB. OPS CH ECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999091700584 19990917 00584 EA 1999 9 17 SMPA99001 1 19990806 A 5711 SPAR DHAV DHC6 DHC6200 EA WS 57 CORRODED A SMPA K NONE O OTHER IN INSP/MAINT 1 WP 13 719AS 33591 139 PPG - RIGHT WING WAS INSPECTED IAW AD 94-08-10 AND EMMA SP NR 57, MAIN SPAR CAP INSP FOR CORROSION. A SPOT OF CORROSION WAS FOUND ON THE LOWER FORWARD SPAR CAP CENTERED AT WS 57. THE DAMAGE MEASURED APPROX 2.5 INCHES IN LENGTH BY 0.2 INCH WIDE AT MAX DEPTH OF .05 INCH. THE DAMAGED SPAR CAP WAS REPLACED WITH A NEW EXTRUSION INSERTED IN AT WS 74.0. THIS IS MADE POSSIBLE BY AN APPROVED DEHAVILLAND REPAIR SCHEME DESIGNED FOR THIS AREA. THERE WERE NO OTHER CORROSION DAMAGES F OUND ON THIS WING. PART TC: 76,112. (X) 1 H 7 2 3T A9EA 1999091700588 19990917 00588 NM 1999 9 17 TWRA9930 1 19990806 A 2560 GIRT BAR BOEING 747 747212B 1384886 NM R2 DOOR OUT OF POSITION A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 624FF 21439 PRIOR TO DEPARTURE, FLIGHT ATTENDANT REPORTED R2 DOOR AUTO SELECT STIFF. FOUND SURVIVAL KIT NOT PROPERLY PACKED. REPAC KED AND PERFORMED OPS CHECK, OK. (X) 2 L 7 4 4F A20WE 1999091700589 19990917 00589 EU 1999 9 17 USAA990691 1 19990707 A 5720 D57541237200 DOUBLER AIRBUS A319 A319112 EU LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 85 1033 PIT - PILOT REPORT INDICATED OUTBOARD LEG COMPLETELY CRACKED OFF. INBOARD LEG 2.50 INCH CRACK AT PANEL ATTACH DOUBLER A T BOTH FORWARD EXTENDING LEGS BETWEEN RIBS 23 AND 24, LT WING. MANUFACTURED NEW DOUBLER 2024-T3 0.063 INCH PER SRM 57-5 1-26 FIG 9. (X) 2 L 7 2 4F RT A28NM 1999091700590 19990917 00590 EU 1999 9 17 99ZZZX3465 1 19990707 A 5720 D57550102202 BEAM AIRBUS A319 A319112 EU LT WING BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 85 1033 PIT - PILOT REPORT INDICATED 12 INCH SECTION BROKEN OFF BEAM ASSEMBLY, TIE, ATTACHED TO PANEL 575AT LEFT WING. DEFECTIV E PART REPLACED WITH IDENTICAL PART NUMBER. (X) 2 L 7 2 4F RT A28NM 1999091700591 19990917 00591 EU 1999 9 17 USAA990688 1 19990707 A 5751 D5764000000800B SKIN AIRBUS A319 A319112 EU LT AILERON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 85 1033 PIT - PILOT REPORT INDICATED ONE EACH 2 INCH LONG CRACK AND 3.50 INCH LONG CRACK AT LEFT AILERON AT INBOARD END LEFT AIL ERON UPPER SURFACE LEADING EDGE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (X) 2 L 7 2 4F RT A28NM 1999091700592 19990917 00592 EU 1999 9 17 USAA990689 1 19990707 A 5720 D57541499208 ANGLE AIRBUS A319 A319112 EU LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 85 1033 PIT - PILOT REPORT INDICATED 3 INCH CRACK, PIECE MISSING AT INBOARD ATTACH ANGLE FOR PANEL 575AT LEFT WING. MANUFACTURE D NEW ANGLE OF 2024-TE 0.063 INCH PER DWG D575-41499. (X) 2 L 7 2 4F RT A28NM 1999091700593 19990917 00593 EU 1999 9 17 USAA990690 1 19990707 A 5730 D5754601401600B PANEL AIRBUS A319 A319112 EU LT WING BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 711UW 85 1033 PIT - PILOT REPORT INDICATED 1.50 INCH BY 3.25 INCH PIECE MISSING INBOARD AFT CORNER, 3 SCREWS PULLED THROUGH UPPER AILE RON INBOARD ACCESS PANEL 575AT LEFT WING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (X) 2 L 7 2 4F RT A28NM 1999091700594 19990917 00594 NM 1999 9 17 UIEA9930 1 19990612 A 2424 GCU BOEING 747 7472D7B 1384803 NM NR 2 ENGINE INOPERATIVE A UIEA A J UNSCHED LANDING DUMP FUEL J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 15 527MC 22471 TPE/ANC - FLT GT386 - AFTER TAKEOFF, NR 2 GENERATOR FIELD AND MAIN BREAKER TRIPPED FOLLOWED BY NR 2 BUS TIE BREAKER TRIP . ONE MINUTE LATER, NR 1 GENERATOR FIELD AND MAIN GEN BREAKER TRIPPED. COULD NOT RESTORE EITHER GENERATOR. RESET NR 2 BTB AND THE NR 1 BTB TRIPPED AND COULD NOT BE RESTORED. 20 MINUTES LATER, NR 3 BTB TRIPPED, DUMPED FUEL RETURNED TO T PE. APPROACH AND LANDING UNEVENTFUL. DURING T/S, TPE MAINT FOUND NR'S 1, 2, AND 3 GENERATOR CONTROL UNITS DEFECTIVE. R EPLACED 3 GCU'S ALL ENG RUN-UP AND NR'S 1 AND 2 GENERATOR CHKS NORMAL. NR 2 GEN INOP, DEFERRED MEL ITEM 24-1. MAINT RE PLACED NR 2 GEN AND NR 2 GCU AGAIN. OPER NORMAL. (X) 2 L 7 4 4F RT A20WE 1999091700595 19990917 00595 NM 1999 9 17 UIEA9933 1 19990621 A 5312 65B152476 BULKHEAD SPLICE BOEING 747 7472F6B 1384807 NM PRESS BULKHEAD CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 534MC 73462 15404 21832 CRACKS FOUND ON WEB SPLICE PLATE HOLES NR 11 RIGHT AND NR 23 RIGHT. HOLE NR 11 RIGHT, INSTALLED SEPRATE BUSHINGS IN EAC H PART PER SB 747-53A2390 FIG 14. HOLE NR 23 RIGHT, REPAIRED OVERSIZE HOLE IN WEB SPLICE PLATE BULKHEAD. CHORD AND WEB PER BUSHING REPAIR PER SB 747-53A2390 FIG 14. (X) 2 L 7 4 4F A20WE 1999091700596 19990917 00596 NM 1999 9 17 99ZZZX3466 1 19990602 A 7810 314U210057 NOZZLE BOEING 747 74747UF 1384949 NM NR 3 ENGINE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 408MC 1777 244 29261 EXHAUST SLEEVE CRACKED AT AFT CIRCUMFERENTIAL SEAM WELD. NR 3 ENGINE, 11 O'CLOCK POSITION 10 INCH LENGTH AND SECOND CRA CK 3 O'CLOCK POSITION 1.50 INCH LENGTH. AFTER REMOVAL, FOUND SMALL 1.50 INCH CRACK INSIDE ON BULKHEAD. ITEM REPLACED. (X) 2 L 7 4 4F RT 1384945 1999091700597 19990917 00597 NM 1999 9 17 UIEA9932 1 19990621 A 5312 65B152471 BUILKHEAD SPLICE BOEING 747 7472F6B 1384807 NM PRESS BULKHEAD CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 534MC 73462 15404 21832 CRACKS FOUND ON WEB SPLICE PLATE HOLES NR 11 LEFT AND NR 21 LEFT. HOLES NR 11 LEFT, INSTALLED SEPARATE BUSHINGS IN EACH PART PER SB 747-53A2390 FIG 14. HOLE NR 21 LEFT, REPAIRED OVERSIZE HOLE IN BULKHEAD. CHORD AND WEB PER BUSHING REPAIR PER SB 747-53A2390 FIG 14. (X) 2 L 7 4 4F A20WE 1999091700598 19990917 00598 NM 1999 9 17 AALA990848 1 19990606 A 3350 0201975005 HARNESS BOEING 777 777223 1385213 NM ROW 34 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 777AN 29585 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 34 INOPERATIVE. REPLACED EMERGENCY EXIT SEAT HARNESS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 1999091700599 19990917 00599 NM 1999 9 17 USAA089903 1 19990818 A 2910 BACH8C08NN0290 HOSE BOEING 727 727227 1384078 NM B HYD PUMP LEAKING A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS UK UNKNOWN 1 EA 19 924TS 21041 HYDRAULIC SYSTEM B ELECTRIC PUMP NR 2 LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. B SYSTEM HYDRAULIC QUANTITY INDICATED Z ERO. EXECUTED APPROPRIATE ABNORMAL PROCEDURES. AFTER LANDING, B SYSTEM RESERVOIR INDICATED AT 1.5 GALLONS LOW. FOUND NR 2 B SYSTEM PUMP PRESSURE LINE LEAKING. REPLACED LINE, CHECKED AND REPLACED NR 1 AND NR 2 B PUMP PRESSURE AND CASE DR AIN FILTERS. CHECKED HYDRAULIC TUBING IN LEFT FAIRING AREA FOR EVIDENCE OF OVERHEATING. CHECKED OK. SERVICED HYDRAULI C SYSTEM A PER GMM 8.13.1. OPERATIONAL AND LEAK CHECKED OK PER MM 29-12-2, 29-12-21 AND 29-12-32. (M) 2 L 7 3 4F A3WE 1999091700600 19990917 00600 NM 1999 9 17 USAA990668 1 19990713 A 5330 SKIN BOEING 757 757225 1384959 NM BS 1420 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 47079 22196 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION AT STATION 1420 LBL 29 BETWEEN STRI NGER 30 AND 29L SKIN, CORROSION LEVEL 2. REPAIRED WITH EXTERNAL DOUBLER PER SRM 53-00-01 FIG 206. (M) 2 L 7 2 4F RT A2NM 1999091700601 19990917 00601 NM 1999 9 17 USAA990669 1 19990713 A 5330 SKIN BOEING 757 757225 1384959 NM BS 1330 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 47079 22196 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2.25 INCH AREA OF CORROSION AT STATION 1330 LBL 29 BETWEEN S TRINGER 27L AND 28L SKIN, CORROSION LEVEL 2. INTERIM REPAIR (DOUBLER) PER EA 65029 AND SRM 53-00-01 FIG 204. (M) 2 L 7 2 4F RT A2NM 1999091700602 19990917 00602 NM 1999 9 17 USAA990670 1 19990713 A 5330 SKIN BOEING 757 757225 1384959 NM BS 1400-1420 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 47079 22196 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AT BS 1400 TO BS 1420 LBL 18 WEB AN D SKIN, CORROSION LEVEL 2. FABRICATED WEB PER SRM 53-60. (M) 2 L 7 2 4F RT A2NM 1999091700603 19990917 00603 NM 1999 9 17 USAA990671 1 19990713 A 5330 SKIN BOEING 757 757225 1384959 NM BS 1300-1320 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AU 47079 22196 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 4 INCH AREA OF CORROSION AT BS 1300 TO BS 1320 RBL 18 WEB AN D SKIN, CORROSION LEVEL 2. INSTALLED NEW WEB PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091700604 19990917 00604 NM 1999 9 17 USAA990749 1 19990722 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AU 19049 27201 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION ON SEAT TRACK AT STATION 377, LBL 24.75, CORROSION LEV EL 2. INSTALLED NEW SEAT TRACK PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091700605 19990917 00605 NM 1999 9 17 USAA990750 1 19990722 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AU 19049 27201 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH BY .75 INCH AREA OF CORROSION AT STATION 377, LBL 43 AROUND S CREW HOLES ON FLOORBEAM, CORROSION LEVEL 2. INSTALLED DOUBLER REPAIR ANGLE PER TR 53-15-02 AND SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091700606 19990917 00606 NM 1999 9 17 USAA990760 1 19990722 A 5313 STRINGER BOEING 757 7572B7 1384964 NM BS 620 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AU 19049 27201 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .875 INCH CRACK AFT OF 620 STRINGER 16. INSTALLED REPAIR PART PER SRM 53-00-03 FIG 201. (M) 2 L 7 2 4F RT A2NM 1999091700607 19990917 00607 NM 1999 9 17 USAA990761 1 19990722 A 5311 FRAME BOEING 757 7572B7 1384964 NM BS 720 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AU 19049 27201 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A CRACK IN RADIUS OF FUSELAGE FRAME STATION 720, BL 0 BELOW ACE LOADER J ACK SCREW ASSY. INSTALLED REPAIR ANGLE PER SRM 51-70-11. (M) 2 L 7 2 4F RT A2NM 1999091700608 19990917 00608 NM 1999 9 17 USAA990587 1 19990616 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 19482 27199 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON END OF SEAT TRACK STATION 377.7 AT LBBL 45.5, CORROSION LEV EL 2. INSTALLED NEW SEAT TRACK PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1999091700609 19990917 00609 NM 1999 9 17 USAA990588 1 19990616 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AU 19482 27199 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE AROUND NUTPLATE 10 INCH AREA AT STATION 1640, LBL 54.9 TO RBL 54.9 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-221-03 AND C53-222-03. REMOVED AND REPLACED UPPER T-CAP PER REPAIR DOCUMENT 53-15-01 FIG 203. (M) 2 L 7 2 4F RT A2NM 1999091700610 19990917 00610 NM 1999 9 17 USAA990481 1 19990520 A 5347 SEAT TRACKS BOEING 757 7572B7 1384964 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AU 19374 27200 CLT - DURING C-4 CHECK, FOUND 2 INCH CORROSION ON ENDS OF SEAT TRACK AT STATION 377 AT LBBL 25 AND LBBL 45, CORROSION LE VEL 2. REPLACED SEAT TRACK SECTIONS PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091700611 19990917 00611 NM 1999 9 17 USAA990482 1 19990520 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AU 19374 27200 CLT - DURING C-4 CHECK, FOUND 1.5 INCH CORROSION ON ENDS OF SEAT TRACK AT STATION 377 AT LBBL 25 AND 45, CORROSION LEVE L 2. REPLACED SEAT TRACK SECTIONS PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999091700612 19990917 00612 NM 1999 9 17 USAA990472 1 19990517 A 5320 BEAM BOEING 767 767201 1385125 NM BS 355 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 46215 23901 CLT - DURING C-4 CHECK, FOUND 3 INCH CORROSION AT SCREW HOLE ON T-CAP AT STATION 355 APPROX RBL 47. CORROSION LEVEL 2. INSTALLED REPAIR ANGLES PER SRM 53-00-51. (M) 2 L 7 2 4F RT A1NM 1999091700613 19990917 00613 NM 1999 9 17 USAA990473 1 19990517 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM BS 287 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 46215 23901 CLT - DURING C-4 CHECK, FOUND 2 INCH CORRODED AREA OF FLOORBEAM AT STATION 287 RBL 79. CORROSION LEVEL 1. SPLICED SECT ION T-CAP, INSTALLED REPAIR ANGLES EPR SRM 51-10. (M) 2 L 7 2 4F RT A1NM 1999091700614 19990917 00614 NM 1999 9 17 USAA990479 1 19990517 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 46215 23901 CLT - DURING C-4 CHECK, FOUND 2 INCH BY 1 INCH CORRODED AREA AT FLOORBEAM STATION 344 RBL 88, CORROSION LEVEL 1. REPLAC ED T-CAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A1NM 1999091700615 19990917 00615 NM 1999 9 17 USAA990471 1 19990517 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM BS 303 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 649US 46215 23901 CLT - DURING C-4 CHECK, FOUND 2 INCH CORROSION ON FLOORBEAM AT STATION 303 RBL 53, CORROSION LEVEL 1. CUT SECTION OF T- CAP, INSTALLED NEW SECTION AND REPAIR ANGLES PER SRM 53-00-51. (M) 2 L 7 2 4F RT A1NM 1999091700616 19990917 00616 NM 1999 9 17 USAA990422 1 19990430 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM BS 346 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 45616 23902 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 4 INCH AREA OF CORROSION AT STATION 346 FLOORBEAM. INSTALLE D REPAIR ANGLE PER EA 64434. (M) 2 L 7 2 4F RT A1NM 1999091700617 19990917 00617 NM 1999 9 17 USAA990463 1 19990430 A 5311 FRAME BOEING 767 767201 1385125 NM BS 287 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 45616 23902 CLT - DURING C-4 CHECK, FOUND 3 INCH CORRODED AREAS AROUND NUTPLATE HOLES AT T-CAP FRAME AT STATION 287 RBL 63, CORROSIO N LEVEL 2. REPAIRED T-CAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A1NM 1999091700618 19990917 00618 NE 1999 9 17 USAA089902 2 19990807 A 7261 7578678 FILTER BOEING 727 727225 1384077 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE DIRTY A USAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 19 923TS 20441 654694 NR 3 ENGINE OIL BYPASS LIGHT ILLUMINATED ON TAKEOFF ROLL. REPLACED NR 3 OIL FILTER. RAN ENGINE PER MM 71-00. LIGHT WE NT OUT, LEAK CHECKS OK. FILLED NR 3 OIL TANK. CHECKS OK. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999091700619 19990917 00619 EU 1999 9 17 USAAF99038 1 19990803 A 5610 D20543401 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU LEFT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 889US 11358 BNA - FLT 793 - EN ROUTE CLT-STL, AT FL310, CREW DETECTED A NOXIOUS SMELL AND THEN SAW SMOKE IN THE COCKPIT. CREW DESEL ECTED WINDOW HEAT AND THE ODOR STOPPED. FLIGHT DIVERTED TO BNA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLAC ED THE WINDSHIELD. (M) 2 L 7 2 4F RT 1999091700620 19990917 00620 WP 1999 9 17 USAAD99110 1 19990808 A 3230 3914738500 ACTUATOR DOUG DC9 DC931 3022065 WP NLG FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 932VJ 47447 47189 ROC-DCA - FLIGHT 887 - DURING LANDING GEAR EXTENSION, ON APPROACH, THE NOSE GEAR DID NOT EXTEND. THE LANDING GEAR WAS C YCLED BUT THE NOSE GEAR REMAINED RETRACTED. THE EMERGENCY GEAR EXTENSION LEVER WAS USED AND THE NOSE GEAR EXTENDED. TH E AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR UNLOCK ACTUATOR AND THE OVERCENTER LINKA GE. (M) 2 L 7 2 4F A6WE 1999091700621 19990917 00621 WP 1999 9 17 USAAD99111 1 19990811 A 2450 947F9463 AC BUSS CONTROL DOUG DC9 DC931 3022065 WP E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 929VJ 48118 PHL-ROC - FLT 275 - DURING CLIMB-OUT, THE CREW NOTICED NUMEROUS 'CLICKS' INDICATING RELAYS CYCLING. IMMEDIATELY THEREAF TER THE ANNUNCIATOR PANEL INDICATED NUMEROUS SYSTEM FAILURES FOLLOWED SHORTLY BY CABIN PRESSURE WARNING. THE AIRCRAFT R ETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AC BUSS CONTROL PANEL AND THE LEFT AUXILIARY POWER RELAY. (M) 2 L 7 2 4F A6WE 1999091700622 19990917 00622 NM 1999 9 17 AALA991108 1 19990729 A 3350 S283N00219 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639AA 24597 DFW - DURING OVERNIGHT MAINTENANCE, AFT GALLEY RIGHT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT AT AFT GALLEY RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999091700623 19990917 00623 NM 1999 9 17 AALA991122 1 19990731 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31H INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY EXIT LIGHT AT SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700624 19990917 00624 NM 1999 9 17 AALA991138 1 19990804 A 3350 1000679 LIGHT GRIMES BOEING 767 767223 1385123 NM COCKPIT DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 1615 22335 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT A SSEMBLY SIGN ABOVE COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700625 19990917 00625 NM 1999 9 17 AALA991146 1 19990809 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366AA 25193 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 26H INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT S EAT LIGHT AT ROW 26H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700626 19990917 00626 NM 1999 9 17 AALA991148 1 19990806 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330AA 22330 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS UNDER FLIGHT ATTENDANT SEATS IN FIRST GALLEY AREA INOPERATIVE. REPAIRED WIRES TO EMERGENCY EXIT LIGHTS UNDER FLIGHT ATTENDANT SEATS IN FIRST GALLEY AREA. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700627 19990917 00627 NM 1999 9 17 AALA991147 1 19990806 A 3397 WIRE BOEING 767 767323 1385205 NM AFT FUSELAGE FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 390AA 27450 SFO - DURING OVERNIGHT MAINTENANCE, RIGHT AFT GROUND ILL EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED SPLICE TO RIGHT AFT GROUND ILL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700628 19990917 00628 NM 1999 9 17 AALA991156 1 19990810 A 3350 S417T5003 LIGHT BOEING 767 767223 1385123 NM L2 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 301AA 22307 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LOWER LEFT OF L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BY LOWER LEFT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700629 19990917 00629 NM 1999 9 17 AALA991155 1 19990810 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39356 24037 LAX - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHTS AT 32AB THROUGH 41AB INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700630 19990917 00630 WP 1999 9 17 AALA991165 1 19990811 A 2130 1304761 SELECTOR DOUG DC9 DC983 3022083 WP COCKPIT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 588AA 115489 53251 DFW - FLT 1110 - AFTER LEVELING OFF AT 33,000 FT FOR ABOUT 2 MINUTES THE MASTER WARNING LIGHT ILLUMINATED FROM THE CABIN ALTIMETER WARNING LIGHT. THE CABIN WAS CLIMBING AT ABOUT 600 FT PER MINUTE. STARTED EMERGENCY DESCENT AND CAUGHT THE CABIN AT ABOUT 12,500 FT. LEVEL AT 10,000 FT. MANUAL WOULD AFFECT THE PRESSURIZATION BUT NOT TO THE EXTENT IT SHOULD H AVE. LANDED DFW WITHOUT INCIDENT. REPLACED PRESSURIZATION SELECTOR PANEL, OUTFLOW VALVE ACTUATOR AND MOTOR, AND NUMBER 1 PRESSURIZATION CONTROLLER. ACCOMPLISHED BITE AND OPERATIONS CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999091700631 19990917 00631 WP 1999 9 17 AALA991128 1 19990801 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 553AA 477035 53083 LIT - FLT 791 - EN ROUTE LGA, DFW SMOKE AND ELECTRICAL SMELL DETECTED. AIRCRAFT AIR INTERRUPTED AND LANDED LIT WITHOUT INCIDENT. REPLACED CABIN AIR RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700632 19990917 00632 WP 1999 9 17 AALA991171 1 19990814 A 2910 LINE DOUG DC9 DC982 3022082 WP MLG LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 205AA 49155 DFW - FLT 2066 - ON APPROACH TO DFW, RIGHT HYDRAULIC QTY SHOWED 1 QT AND PRESSURE VARIED BETWEEN 1,000-1,500 PSI. RAN Q RH PROCEDURES FOR LOSS OF RIGHT HYDRAULIC FLUID AND EXTENDED THE GEAR USING ALTERNATE PROCEDURE. LANDED DFW WITHOUT INC IDENT. REPLACED HYDRAULIC LINE TO RUDDER CONTROL, BOTH MLG DOORS, AND WATER SEPARATOR BAGS. ACCOMPLISHED PACK BURNOUT AND GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700633 19990917 00633 WP 1999 9 17 AALA991176 1 19990815 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 449AA 49475 ORD - FLT 350 - AFTER TAKEOFF ORD-LGA, NOSE GEAR UNSAFE LIGHT ON RETRACTION. GEAR LOWERED AND SAFE LIGHTS ILLUMINATED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR UP PROXIMITY SENSOR, CYCLED LANDING GEAR SEVE RAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700634 19990917 00634 WP 1999 9 17 AALA991201 1 19990817 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 497AA 49735 DFW - FLT 731 - EN ROUTE LGA-DFW, NOSE LANDING GEAR RED LIGHT INTERMITTENT ILLUMINATION WITH GEAR HANDLE IN UP POSITION. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR POSITION SENSOR. CYCLED NOSE LANDING GEAR SEVERAL T IMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700635 19990917 00635 WP 1999 9 17 AALA991183 1 19990815 A 4990 OIL PLUG DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 278AA 49294 LAX - FLT 596 - AFTER TAKEOFF FROM BUR TO DFW, SMOKE REPORTED IN PASSENGER CABIN. EMERGENCY DECLARED AND AIRCRAFT LANDE D LAX WITHOUT INCIDENT. REPLACED APU ENGINE OIL MAIN OIL DRAIN PLUG AND O-RINGS. PERFORMED AIR CONDITIONING PACK BURNO UT PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700636 19990917 00636 WP 1999 9 17 AALA991182 1 19990815 A 7830 FITTING DOUG DC9 DC982 3022082 WP LT TR UNIT LOOSE A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 430AA 49342 DFW - FLT 1873 - ON TAXI OUT FROM GATE, SMOKE AND FUMES NOTED IN PASSENGER CABIN WITH HYDRAULIC QTY DECREASING. PASSENG ERS AND CREW EVACUATED WITHOUT INCIDENT. RETORQUED B-NUT AT LEFT THRUST REVERSER HYDRAULIC VALVE FITTING. PERFORMED AI R CONDITIONING PACK BURNOUT PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700637 19990917 00637 NM 1999 9 17 AALA991097 1 19990724 A 2497 WIRE BOEING 767 767323 1385205 NM ROW 2D CHAFED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 07 373AA 25200 ORD - FLT 99 - DURING LANDING ORD, A FLASH AND SPARKS WERE OBSERVED IN THE AREA OF THE L-1 DOOR AND THE AREA ABOVE THE C REDENZA AT SEAT 2D. AIRCRAFT LANDED WITHOUT INCIDENT. REPAIRED CHAFFED FORWARD GALLEY POWER WIRE, REPAIRED CHAFFED FOR WARD FLIGHT ATTENDANT 02 MODULE WIRE. REPAIRED CHAFFED FORWARD GALLEY BALLAST WIRE. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F RT A1NM 1999091700638 19990917 00638 NM 1999 9 17 AALA991129 1 19990802 A 2450 D25BD RELAY BOEING 767 767323 1385205 NM E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 07 363AA CH60976 24044 MSY - FLT 207 - EN ROUTE MIA-LAX, LEFT FORWARD FUEL BOOST PUMP CAUTION LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. CA BIN SIDEWALL LIGHTS AND FLIGHT ATTENDANT JUMP SEAT WORK LIGHTS INOPERATIVE. ALSO, RECEIVED CARGO DETECTION AIR ADVISORY MESSAGE AND SYSTEM 1, 2 AND 3 HYDRAULIC FLUID QTY INDICATORS WENT TO .02. AIRCRAFT AIR INTERRUPTED TO MSY AND LANDED W ITHOUT INCIDENT. REPLACED ELECTRICAL RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700639 19990917 00639 EU 1999 9 17 AALA991184 1 19990815 A 3520 17408075 OXYGEN MASK FOKKER F28 F28MK0100 4990807 EU CABIN DEPLOYED A AALA O OTHER O OTHER UK UNKNOWN 1 SW 07 1457B 11469 ORD - FLT 879 - OXYGEN MASKS DID NOT DROP AT SEATS 5A, 7A, AND 18A WHEN PASSENGER OXYGEN DEPLOYMENT SWITCH WAS INADVERTE NLY ACTIVATED WITH AIRCRAFT ON THE GROUND. REPACKED ALL MASKS AND SUCCESSFULLY TESTED DROP SYSTEM. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999091700640 19990917 00640 EU 1999 9 17 AALA991181 1 19990816 A 5542 PANEL FOKKER F28 F28MK0100 4990807 EU E/E COMPT LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 1408B 11361 MCI - FLT 1939 - AFTER TAKEOFF MCI-DFW, LOUD NOISE NOTED IN COCKPIT ALONG WITH PRESSURIZATION PROBLEM. AIRCRAFT RETURNE D TO MCI AND LANDED WITHOUT INCIDENT. FORWARD ELECTRONIC EQUIPMENT COMPARTMENT ACCESS PANEL SEAL RESEATED. SYTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999091700641 19990917 00641 EU 1999 9 17 AALA991180 1 19990815 A 5270 D43162401 SWITCH FOKKER F28 F28MK0100 4990807 EU CARGO DOOR OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1464A 11490 DFW-CLT - DURING CLIMB-OUT, FORWARD CARGO DOOR WARNING RECEIVED. AIRCRAFT RETURNED TO DFW AND WARNING EXTINGUISHED DURI NG DESCENT. AIRCRAFT LANDED DFW WITHOUT INCIDENT. ADJUSTED FORWARD CARGO DOOR SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999091700642 19990917 00642 NM 1999 9 17 AALA991167 1 19990814 A 2710 285T0017104 CSEU BOEING 767 767223 1385123 NM E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 320AA 22321 MIA - FLT 973 - EN ROUTE MIA-GIG, AT CRUISE, APPROXIMATELY 2 HOURS INTO FLIGHT, THE EICAS MESSAGE 'SPOILERS' AND 'R YAW DAMPER' ILLUMINATED. AT THE SAME TIME THE EICAS MESSAGE 'AILERON LOCKOUT' WAS FLICKERING AND THEN BECAME A STEADY MESSA GE, MOMENTS LATER THE RUDDER RATION EICAS MESSAGE ILLUMINATED. CIRCUIT BREAKERS WERE NORMAL, AS WELL AS, HYDRAULICS AND ELECTRONICS. RETURNED AND LANDED MIA W/O INCIDENT. REPLACED BOTH RIGHT CSEU UNITS AS A PRECAUTION. LAND 40 TEST PASS ES WITH NO FAULTS. NO FAULTS ON GROUND TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999091700643 19990917 00643 EU 1999 9 17 AALA991166 1 19990813 A 2612 900045 CONTROLLER FOKKER F28 F28MK0100 4990807 EU APU DEFECTIVE A AALA F ACTIVATE FIRE EXT. N FALSE WARNING UK UNKNOWN 1 SW 07 1421K 11404 LGA - FLT 1084 - EN ROUTE YYZ-LGA - APU FIRE AND AUTO SHUTDOWN DISCHARGED AGEN DURING IN FLIGHT. LANDED LGA WITHOUT FUR THER INCIDENT. REPLACED APU FIRE DETECTION CONTROL UNIT FIRE WARNING. REPLACED APU FIRE BOTTLE, APU FUEL SOLENOID IGNI TER BOX, AND BOTH IGNITER PLUGS. ACCOMPLISHED OPERATION AND LEAK CHECK OF APU. CHECKED APU AND TAIL COMPARTMENT WITH B OTH ENGINES AT HIGH POWER. NO LEAKS DETECTED. INSPECTED APU ENCLOSURE, NO FIRE DAMAGE NOTED. SYSTEM GROUND CHECKED NO RMAL OPERATION. (M) 2 L 7 2 4F RT 1999091700644 19990917 00644 WP 1999 9 17 AALA991187 1 19990812 A 5320 FRAME DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 455AA 49560 TUL - FOUND CORROSION ON HORIZONTAL AND VERTICAL SECTIONS OF MID CARGO DOOR FRAME BEAM. REMOVED CORROSION PER SRM 51-10 -03 AND INSTALLED FABRICATED DOUBLER PER AARD 53-10-00-16 IN AFT LOWER DOOR STOP AREA OF BEAM. (M) 2 L 7 2 4F A6WE 1999091700645 19990917 00645 WP 1999 9 17 AALA991186 1 19990813 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1150-1184 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 458AA 49563 TUL - NR 6 TRACK CORRODED, STATION 1150 TO 1184. INSTALLED TWO PLUG REPAIRS AT STATION 1150 AND 1184 PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 1999091700646 19990917 00646 NM 1999 9 17 AALA991078 1 19990720 A 5320 CASTING BOEING 727 727227 1384078 NM BS 940 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 725AA 20732 TUL - FOUND 940 CASTING HAS CORROSION ON FORWARD FACE AND IN BORE. REMOVED CORROSION HFEC'D, REWORKED AREA PER ESO 1169 7 DATED 7-19-99 OR BACK OF E58-3048962. (M) 2 L 7 3 4F A3WE 1999091700647 19990917 00647 NM 1999 9 17 AALA991079 1 19990720 A 5320 CASTING BOEING 727 727227 1384078 NM BS 940 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 725AA 20732 TUL - FOUND LEFT 940 CASTING AFT FACE CORRODED. REMOVED CORROSION HFEC'D, REWORKED AREA PER ESO 11697 DATED 7-19-99 ON BACK OF E58-3048964. (M) 2 L 7 3 4F A3WE 1999091700648 19990917 00648 NM 1999 9 17 AALA991080 1 19990720 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 725AA 20732 TUL - SHEAR TIE CORRODED STATION 720A, STRINGER 28L. INSTALLED REPAIR PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999091700649 19990917 00649 NM 1999 9 17 AALA991081 1 19990721 A 5711 SPAR BOEING 727 727227 1384078 NM WS 546 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 725AA 20732 TUL - FOUND LEFT WING, FORWARD LOWER SPAR CHORD HAS CORROSION AT WS 546 WITH PREVIOUS BLEND. INSTALLED DOUBLER PER AARD 53-30-00-02 AND ESO DATED 7/20/99. (M) 2 L 7 3 4F A3WE 1999091700650 19990917 00650 NM 1999 9 17 AALA991082 1 19990720 A 5711 SPAR BOEING 727 727227 1384078 NM WS 196-199 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 725AA 20732 TUL - LEFT FRONT SPAR HAS CORROSION ON LOWER CHORD ANGLE VERTICAL LEG. INSTALLED SPAR CHORD REPAIR DOUBLERS PER SRM 57- 10-6. (M) 2 L 7 3 4F A3WE 1999091700651 19990917 00651 NM 1999 9 17 AALA991070 1 19990715 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 591 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - STRINGER 28L HAS HEAVY CORROSION AT FS 591. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED SPLICE REPAIR IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999091700652 19990917 00652 NM 1999 9 17 AALA991071 1 19990715 A 5330 SKIN BOEING 727 727223 1384074 NM BS 578-592 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - FUSELAGE SKIN CORRODED FS 587-592 OUTBOARD OF STRINGER 28 LEFT. REMOVED DAMAGED SKIN. INSTALLED DOUBLER REPAIR I AW SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1999091700653 19990917 00653 NM 1999 9 17 AALA991072 1 19990714 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - LOWER FLANGE OF BELLFRAME CORRODED, FORWARD CARGO STATION 720E BETWEEN STRINGER 27L AND 28L. CORRODED SECTION REM OVED, ANGLE REPAIR INSTALLED AT SHEAR TIE PER SRM 53-10-4 PAGES 58-60. (M) 2 L 7 3 4F A3WE 1999091700654 19990917 00654 NM 1999 9 17 AALA991073 1 19990719 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 942 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - RIGHT STRINGER 18A CRACKED IN RADIUS HORIZONTAL OUTBOARD LEG, EXTENDING OUT FROM RADIUS BLOCKS AFT SIDE OF 940 CAS TING. REMOVED DAMAGED SECTION SPLICED IN NEW SECTION OF RT STRINGER 18A PER SB 727-53-0172. (M) 2 L 7 3 4F A3WE 1999091700655 19990917 00655 NM 1999 9 17 AALA991074 1 19990715 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 568 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - FOUND CORROSION ON SHEAR TIE BETWEEN STRINGER 26R-27R, STATION 568. REMOVED CORRODED SHEAR TIE. INSTALLED NEW SH EAR TIE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999091700656 19990917 00656 NM 1999 9 17 AALA991005 1 19990706 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 675 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND STRINGER 28L CORRODED AT PRODUCTION SPLICE, BS 675. REMOVED CORROSION DAMAGED PORTION OF STRINGER 28L AND I NSTALLED STRINGER REPAIR SPLICE PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999091700657 19990917 00657 NM 1999 9 17 AALA991004 1 19990628 A 5311 FRAME BOEING 727 727227 1384078 NM BS 480 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FRAME CRACKED ON WEB AT STRINGER CUTOUT STATION 480, STRINGER 27R. INSTALLED WEB REPAIR PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1999091700658 19990917 00658 NM 1999 9 17 AALA991003 1 19990706 A 5330 SKIN BOEING 727 727227 1384078 NM BS 251.9 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND CRACK IN FUSELAGE SKIN AT RIVET LOCATED BS 251.9 AND STRINGER 22L. REMOVED RIVET, CONFIRMED CRACK WITH HFEC . REMOVED 1 INCH DIAMETER AREA OF SKIN TO REMOVE CRACKED AREA, CONFIRMED CRACK REMOVAL WITH HFEC. INSTALLED DOUBLER PE R SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999091700659 19990917 00659 NM 1999 9 17 AALA991002 1 19990708 A 5320 FRAME BOEING 727 727227 1384078 NM CARGO DOORWAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - HFEC INDICATES CRACK IN NR 2 CARGO DOOR FORWARD FUSELAGE FRAME WEB INBOARD OF LOWER STOP FITTING. STOP DRILLED CR ACK, HFEC AROUND STOP DRILL, NO FURTHER CRACK PROGRESSION. INSTALLED DOUBLER PER SB 727-53A 0199 FIG 2 WITH .080 INCH 7 075-T6. (M) 2 L 7 3 4F A3WE 1999091700660 19990917 00660 EU 1999 9 17 AALA990617 1 19990422 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - FOUND FLOORBOARD SUPPORT CORRODED SEVERAL PLACES FROM FRAME 71 TO FRAME 74 AFT OF TRACK NR 5. REMOVED BEAM AND IN STALLED NEW BEAM (P/N A5327920620800, BETWEEN FRAME 71 TO 74 AFT OF NR 5 TRACK PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999091700661 19990917 00661 EU 1999 9 17 AALA990616 1 19990422 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4630 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - SUPPORT CORRODED UNDER FLOORBOARD AT BS 4630. INSTALLED NEW SUPPORT PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1999091700662 19990917 00662 EU 1999 9 17 AALA990614 1 19990421 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7076A 610 TUL - FLOORBOARD SUPPORT CORRODED UNDER LAV AFT OF TRACK 4 FRAME 71 TO 74. REPLACED BEAM A6327920620800 PER SRM 51-74-1 0-2. (M) 2 L 7 2 4F RT A35EU 1999091700663 19990917 00663 NM 1999 9 17 AALA991015 1 19990706 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND CORROSION ON STRINGER SPLICE AT BS 480. REMOVED CORRODED STRINGER SPLICE AND INSTALLED REPAIR SPLICE PE SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999091700664 19990917 00664 NM 1999 9 17 AALA991016 1 19990702 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND CORROSION ON SHEAR TIE STATION 700 BETWEEN STRINGER 27R AND 28R. INSTALLED DOUBLER ON SHEAR TIE STATION 700 BETWEEN STRINGER 27 AND 28R PER SRM 53-10-4 PAGES 58-60. (M) 2 L 7 3 4F A3WE 1999091700665 19990917 00665 EA 1999 9 17 MASA991122 1 19990721 A 2910 AE2460010H0264 HOSE CNDAIR CL600 CL6002B19 EA NR 1 HYD SYSTEM RUPTURED A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 17217 7217 FLT 5750 - BHM-PHL - THE AIRCRAFT EXPERIENCED A COMPLETE LOSS OF HYDRAULIC FLUID IN THE NR 1 HYDRAULIC SYSTEM. THE AIRC RAFT DIVERTED TO CLT WITHOUT FURTHER INCIDENT THE CREW DECLARED AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED THE RUPT URED LINE. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999091700666 19990917 00666 EA 1999 9 17 MASA99134 1 19990722 A 5210 56244 CAM FOLLOWER CNDAIR CL600 CL6002B19 EA PAX DOOR JAMMED A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 17175 7175 FLT 5772 - CLT-LIT - THE AIRCRAFT HAD A PASSENGER DOOR THAT WAS HARD TO OPEN. MAINTENANCE UNJAMMED A ROLLER ON THE PASS ENGER DOOR. OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999091700667 19990917 00667 EU 1999 9 17 AALA991127 1 19990728 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 26 BELOW CENTER SCISSOR. REPAIRED PER SRM 53-10-15, BY REPLACING S ECTION OF SUPPORT ANGLE. (M) 2 L 7 2 4F RT A35EU 1999091700668 19990917 00668 EU 1999 9 17 AALA991153 1 19990806 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND CORROSION ON STRINGER 48L 2 PLACES BETWEEN FRAME 70 AND 71 BELOW THE WASTE WATER TANK JUNCTION BOX. REMOVED AND REPLACED SECTION OF STRINGER 48L PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999091700669 19990917 00669 EU 1999 9 17 AALA991152 1 19990805 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU E/E COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND CORROSION ON AFT SIDE OF FRAME C-20 ON STRINGER. STRINGER 53L IS CORRODED FROM FRAME 20 FORWARD ABOUT 8 INC HES TO 10 INCHES. REPLACED SECTION OF STRINGER AND SPLICED PER SRM 53-00-00. (M) 2 L 7 2 4F RT A35EU 1999091700670 19990917 00670 EU 1999 9 17 AALA991114 1 19990729 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND CORROSION IN SEAT TRACK AND NR 10 RIGHT SIDE OF AIRCRAFT. REMOVED AND REPLACED RT SIDE NR 10 SEAT TRACK PER SRM 51-72-10-8. (M) 2 L 7 2 4F RT A35EU 1999091700671 19990917 00671 EU 1999 9 17 AALA991140 1 19990803 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND CORROSION ON NUT PLATE AT POWER ROLLER TRAY 4TH FROM AFT, RT SIDE, OUTBOARD OF NR 5 TRAY. REMOVED AND REPLA CED FLOOR ANGLE PER MM 53-10-15-2. (M) 2 L 7 2 4F RT A35EU 1999091700672 19990917 00672 EU 1999 9 17 AALA991116 1 19990728 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND AFT LEFT GALLEY ON TRACK B HAS CORROSION AROUND TWO ATTACH FITTING. REMOVED DAMAGED TRACK SECTION AND INSTA LLED NEW ONE OF SAME P/N USING HI-LOCKS AND PRO BR870 RAF A300 SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999091700673 19990917 00673 EU 1999 9 17 AALA991115 1 19990728 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND CORROSION AT LAV TIE DOWN AF TOF FRAME C79 ON FLOOR SUPPORT 59 INCHES LEFT OF AIRCRAFT CENTER LINE. REMOVED DAMAGE TRACK SECTION AND INSTALLED NEW ONE OF SAME P/N USING HI-LOCKS AND PRO PR870 REF A300 SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999091700674 19990917 00674 EU 1999 9 17 AALA991014 1 19990708 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80084 675 TUL - FOUND CORROSION AT NR 3 SEAT TRACK. REMOVED CORROSION PER SRM 51-74-10. ALODINED, PRIMED PAINTED AREA AND INSTAL LED ALUMINUM PLUG WITH SEALANT, REF A300 SRM 51-21-00 AND ESO 305.75 AARD CHP53 DATED 7 JUL 99. (M) 2 L 7 2 4F RT A35EU 1999091700675 19990917 00675 EU 1999 9 17 AALA991008 1 19990707 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80084 675 TUL - FOUND SEAT TRACK NR 1 CORRODED JUST FORWARD OF THE L-1 DOOR. REMOVED CORROSION PER SRM 51-71-10. INSTALLED STRAP REPAIR PER AARD 53-20-00-2. ALODINED, PRIMED AND PAINTED PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1999091700676 19990917 00676 EU 1999 9 17 AALA991007 1 19990707 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80084 675 TUL - FOUND CORROSION ON FLOOR SUPPORT TOP FLANGE, 3RD FLOOR SUPPORT FROM LEFT SIDE AT FRAME C13. REMOVED CORROSION PER SRM 51-74-10. INSTALLED STRAP PER AARD 53-20-00-2. ALODINED, PRIMED AND PAINTED PER SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1999091700677 19990917 00677 EU 1999 9 17 AALA991034 1 19990710 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80084 675 TUL - FOUND CORROSION ON SEAT TRACK NR 8. REPLACED FLOOR SEAT TRACK FROM FRAME 27-31 PER SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1999091700678 19990917 00678 EU 1999 9 17 AALA991033 1 19990713 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU FRAME 45 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80084 675 TUL - FOUND RIGHT FRAME 45 BASE FITTING CRACKED. INSTALLED DOUBLER PER AARD 53-00-00-7 ON RT FRAME 45. (M) 2 L 7 2 4F RT A35EU 1999091700679 19990917 00679 NM 1999 9 17 TSAA9933399 1 19990819 A 3350 8731002511 LIGHT BOEING 737 737209 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 827AL 23913 REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700680 19990917 00680 NM 1999 9 17 TSAA9933400 1 19990819 A 3350 873100151 LIGHT BOEING 737 737209 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 2 EMERGENCY FLOOR LIGH TASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700681 19990917 00681 NM 1999 9 17 TSAA9953404 1 19990816 A 5350 654577625 SKIN BOEING 737 7372T4 1384492 NM BS 947 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 FOUND 4.125 INCH CRACK 2 INCH FORWARD OF BS 947 AT STRINGER 24L. SKIN REPAIR IAW SRM 53-30-3 FIGURE 6 SHEET 4 PAGE 12B. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091700682 19990917 00682 EU 1999 9 17 SIMA992291 1 19990817 A 5320 S5367800821602 ZEE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 348AE 349 DURING MBV-2 INSPECTION, FOUND RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 42 CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700683 19990917 00683 WP 1999 9 17 ARWA990902 1 19990905 A 2741 575600015 SENSOR DOUG DC8 DC863F 302198F WP HORIZ STAB FAILED A ARWA A UNSCHED LANDING F N FLT CONT AFFECTED FALSE WARNING CL CLIMB 1 SO 19 661AV 2872 45969 MIA - FLT 601 - AFTER ROTATION STAB CONTINUOUSLY RAN NOSE DOWN AND WARNING HORN RAN CONTINUOUSLY. SPLIT SUITCASE HANDLE S AND PULLED 'STAB AND AUTOPILOT' OFF WARNING HORN CIRCUIT BREAKER TO SILENCE HORN. RETURNED TO MIA WITHOUT INCIDENT. R EPLACED STAB MOTION SENSOR. OPS CHECKED NORMAL IAW MM 27-30-0. PERFORMED VISUAL INSPECTION OF HORIZ STAB DRIVE MECHANI SM. NO DEFECTS NOTED. OPS CHECKED NORMAL IAW 27-40-0. (M) 2 L 7 4 4F 4A25 1999091700684 19990917 00684 EU 1999 9 17 99ZZZM630 1 19990813 A 2611 72111211100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 383AE A5035 340B383 DFW - FLT 5032 - CARGO SMOKE WARNING ACTIVATED. USED FIRE EXTINGUISHER NR 1. VERIFIED EVENT AS A FALSE WARNING. REMOV ED AND REPLACED FORWARD AND AFT SMOKE DETECTORS AND FIRE EXTINGUISHER. PERFORMED OPERATIONAL TEST AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999091700685 19990917 00685 SO 1999 9 17 SIMA992192 1 19990807 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145 SO CARGO COMPT FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 611AE 05986 145074 DFW - FLT 3502 - BAGGAGE SMOKE LIGHT CAME ON. USED BOTH FIRE EXTINGUISHERS. VERIFIED EVENT AS A FALSE WARNIGN. REMOVE D AND REPLACED FIRE EXTINGUISHERS. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999091700686 19990917 00686 SO 1999 9 17 99ZZZM631 1 19990807 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145 SO CARGO COMPT FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 611AE 05986 145074 DFW - FLT 3502 - BAGGAGE SMOKE LIGHT CAME ON. USED BOTH FIRE EXTINGUISHERS. VERIFIED EVENT AS A FALSE WARNIGN. REMOVE D AND REPLACED FIRE EXTINGUISHERS. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS. FUNCTIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999091700687 19990917 00687 NM 1999 9 17 GAIA99125 1 19990820 A 2612 65249203 FIRE DETECTOR BOEING 727 727223 1384074 NM LWR AFT BODY FAILED A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 855AA 20996 EN ROUTE FROM STL-TOL, LOWER AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT. PULLED NR 2 THROTTLE TO IDLE. RAN CHECKLIST. L IGHT WENT OUT. RESTORED PARTIAL POWER TO NR 2. NR 2 START VLV LIGHT STARTED TO FLICKER. PULLED NR 2 THROTTLE BACK TO IDLE. THEN LOWER AFT BODY LIGHT CAME BACK ON. REDUCED SOME POWER ON 1 AND 3 THROTTLES AND LIGHT WENT OUT AND STAYED OU T. THE AIRCRAFT LANDED SAFELY. PERFORMED RESISTANCE CHECK ON KEEL BEAM AFT CARGO COMPARTMENT, AND AFT AIRSTAIR OVERHEA T DETECTORS. REMOVED AND REPLACED FIRE AND OVERHEAT DETECTOR. RAN ENGINES TO TAKEOFF POWER. CHECKED ALL DUCTS FOR LEA KS. NO LEAKS NOTED. LOWER AFT BODY OVERHEAT OPERATIONAL CHECKS NORMAL. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED 2 L 7 3 4F A3WE 1999091700688 19990917 00688 WP 1999 9 17 GAIA99121 1 19990813 A 5510 39151571 SUPPORT DOUG DC9 DC915F 3022037 WP HORIZ STABILIZER DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 112PS 47013 DURING C-CHECK INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER FORWARD LOWER FAIRING SUPPORT DAMAGED. THE SUPPORT WAS REPAIRED IAW KITTY HAWK EA D9-53-070 THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999091700689 19990917 00689 WP 1999 9 17 GAIA99122 1 19990813 A 5753 5912146501 SKIN DOUG DC9 DC915F 3022037 WP LT TE FLAP DELAMINATED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 112PS 47013 DURING C-CHECK INSPECTION, FOUND DELAMINATION ON THE LEFT FLAP REMOVABLE PANEL TRAILING EDGE SKIN AT XFLS187. THE SKIN WAS REPLACED IAW KITTY HAWK EA D9-53-073. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999091700690 19990917 00690 WP 1999 9 17 GAIA99124A 1 19990824 A 3297 WIRE DOUG DC9 DC915F 3022037 WP NLG BROKEN A GAIA O OTHER N FALSE WARNING LD LANDING 1 SW 07 564PC 47062 FLT 564 - LRD-FWA - ON APPROACH TO FWA, THE NLG DOWN AND LOCKED GREEN LIGHT FAILED TO ILLUMINATE WHEN THE GEAR WAS PLACE D IN THE DOWN POSITION. ATC WAS NOTIFIED AND EMERGENCY WAS DECLARED, THE FLIGHT CREW MADE A VISUAL CHECK TO CONFIRM THE GEAR WAS DOWN AND LOCKED. AN UNEVENTFUL LANDING WAS MADE. SECURED BROKEN WIRE AT NOSE LANDING GEAR UPLOCK SWITCH CANN ON PLUG AS REQUIRED. OPERATIONAL CHECKED SYSTEM IAW DC-9 MM CHAPTER 32-60-1. NO DEFECTS NOTED. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F A6WE 1999091700691 19990917 00691 NM 1999 9 17 GAIA99126 1 19990827 A 2781 WIRE BOEING 727 727223 1384074 NM LE FLAP IND BROKEN A GAIA K NONE P NO WARNING INDICATION CR CRUISE 1 SW 07 6812 19487 EN ROUTE FROM GEG TO IND, FLT 2507 - NR 3 LEADING EDGE FLAP INDICATOR, ON F/E PANEL, DOES NOT INDICATE GREEN NOR AMBER A FTER SELECTING FLAPS. F/O INDICATOR INDICATES AMBER. AIRCRAFT MADE AN UNEVENTFUL LANDING AT IND. REPAIRED BROKEN WIRE AT LEFT NR 3 LEADING EDGE FLAP POSITION SWITCH. OPERATIONALLY CHECK GOOD IAW BOEING MM 27-00. AIRRAFT RETURNED TO SER VICE WITH NO ADDITIONAL PROBLEMS. (M) 2 L 7 3 4F A3WE 1999091700692 19990917 00692 WP 1999 9 17 GAIA99118 1 19990813 A 5330 59114013 SKIN DOUG DC9 DC915F 3022037 WP BS 200 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 112PS 47013 DURING C-CHECK INSPECTION, FOUND SKIN DAMAGE BY THE MAIN ENTRANCE DOOR AIRSTAIR CUTOUT AT L22L AND STATION 200. THE SKI N WAS REPAIRED IAW KITTY HAWK EA D9-53-069 THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999091700693 19990917 00693 WP 1999 9 17 GAIA99119 1 19990813 A 5330 59183741 SKIN DOUG DC9 DC915F 3022037 WP BS 484-544 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 112PS 47013 DURING C-CHECK INSPECTION, FOUND CORROSION BETWEEN THE LEFT WINDOW BELT AND THE FUSELAGE SKIN FROM STATION 544 TO 484. T HE SKIN WAS REPAIRED IAW KITTY HAWK EA D9-53-071 THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999091700694 19990917 00694 WP 1999 9 17 GAIA99120 1 19990813 A 5753 59135609 SKIN DOUG DC9 DC915F 3022037 WP TE FLAP CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 112PS 47013 DURING C-CHECK INSPECTION, FOUND A CRACK ON THE LT FLAP LEADING EDGE SKIN AT XW250. THE SKIN WAS REPAIRED IAW KITTY HAW K EA D9-53-072. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999091700695 19990917 00695 NM 1999 9 17 GAIA99123 1 19990819 A 8012 CONNECTOR BOEING 727 727223 1384074 NM NR 2 ENGINE LOOSE A GAIA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SW 07 855AA 20996 FLT 514 - BDL-EWR - ON APPROACH, HAD THE NR 2 ENGINE START VALVE COME ON. THE AOM PROCEDURE FOR THE START VALVE LIGHT O N WAS COMPLIED WITH AND THE NR 2 ENGINE WAS SHUTDOWN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT BDL WITHOUT FURTHER DIFFICULTIES. CHECKED NR 2 ENGINE START VALVE WIRING FOR CONDITION AND SECURITY. CLEANED AND RESEATED CANNON P LUGS. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999091700696 19990917 00696 NM 1999 9 17 TSAA9933406 1 19990821 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 2 FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700697 19990917 00697 NM 1999 9 17 TSAA9933407 1 19990821 A 3350 86210151 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED AFT EMERGENCY CONTROL MODULE (INTERVALVE) BATTERY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999091700698 19990917 00698 NM 1999 9 17 TSAA9933408 1 19990821 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 3 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1999091700699 19990917 00699 NM 1999 9 17 TSAA9933409 1 19990821 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700700 19990917 00700 NM 1999 9 17 TSAA9933410 1 19990823 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700701 19990917 00701 NM 1999 9 17 TSAA9933411 1 19990823 A 3350 86210066 BATTERY BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY PACKS FOR NR 2, NR 4 AND NR 5 EMERGENCY FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700702 19990917 00702 NM 1999 9 17 TSAA9933412 1 19990823 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED NR 6 FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1999091700703 19990917 00703 NM 1999 9 17 TSAA9933413 1 19990823 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700704 19990917 00704 NM 1999 9 17 TSAA9933414 1 19990823 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091700705 19990917 00705 EU 1999 9 17 99ZZZM632 1 19990824 A 2700 3945122505 ELAC AIRBUS 320 A320231 3930325 EU E/E COMPT FAILED A P9RA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 304ML 1367 373 ELAC NR 1 FAILED IN FLIGHT. REF MEL 27-93-01 C NR 1146 ELAC INDICATION PER MAINTENANCE CONTROL. (M) 2 L 7 2 4F RT A28NM 1999091700706 19990917 00706 NM 1999 9 17 F3LA99115 1 19990822 A 3397 WIRE BOEING 737 737201 1384454 NM ROW 9 FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 205AU 19421 DEN - DURING C-4 CHECK INSPECTION, REPORTED EMERGENCY EXIT SIGN INOPERATIVE AT ROW 9 LEFT SIDE. MAINTENANCE REPAIRED WI RING AT SEAT 9C FOR EMERGENCY EXIT SIGN. (M) 2 L 7 2 4F A16WE 1999091700707 19990917 00707 NM 1999 9 17 F3LA9914 1 19990821 A 5522 SKIN BOEING 737 7372L9 1384497 NM LT ELEVATOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 22733 DEN - DURING C-6 CHECK INSPECTION REPORTED TWO HOLES IN BOTTOM SIDE OF LT ELEVATOR. MAINTENANCE REPAIRED ELEVATOR DAMAG E PER SRM 51-40-9 AND SRM 55-20-3. PERFORMED WEIGHT AND BALANCE OF ELEVATOR PER SRM 51-80-4. REINSTALLED LEFT ELEVATOR TAB, WHICH WAS REMOVED FOR ELEVATOR BALANCE, PER MM 27-31-31. INSTALLED ELEVATOR PER MM 27-31-11 AND ADJUSTED AND RIG CHECKED PER MM 27-31-0. (M) 2 L 7 2 4F RT A16WE 1999091700708 19990917 00708 WP 1999 9 17 ARWA990901 1 19990830 A 2120 56454131 DUCT DOUG DC8 DC863 302198A WP NOSE WW RUPTURE A ARWA B EMER. DESCENT O OTHER DE DESCENT 1 SO 19 345JW 46042 SJU - FLT 501 - UNABLE TO CONTROL CABIN. NOISE COMING FROM UNDERNEATH COCKPIT FLOOR. EMERGENCY DESCENT PERFORMED. LAN DED WITHOUT INCIDENT. REPLACED DISTRIBUTION DUCT. LEAK CHECKED OK PER MM 21-50-0. (M) 2 L 7 4 4F 4A25 1999091700709 19990917 00709 SO 1999 9 17 ASOA99078 1 19990813 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 503AS 120275 DURING INSPECTION, NR 3 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERG ENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091700710 19990917 00710 SO 1999 9 17 ASOA99079 1 19990813 A 3350 F02A250V1A FUSE EMB 120 EMB120RT SO CABIN BLOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 284AS 120249 DURING INSPECTION, FOUND CABIN TRACK LIGHTING FUSE BLOWN. MAINTENANCE REPAIRED FAULTY CONNECTION ON THE FORWARD CABIN T RACK LIGHT. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091700711 19990917 00711 SO 1999 9 17 ASOA99081 1 19990816 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 229AS 18383 120042 DURING INSPECTION, EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTE RY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999091700712 19990917 00712 SO 1999 9 17 ASOA99082 1 19990816 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 639AS 120283 DURING C-CHECK, FOUND CORROSION AT FRAME 21 BETWEEN STRINGERS 20 LEFT AND 20 RT. REPAIRS WERE MADE IAW THE EO 120-53-01 15. (M) 2 L 7 2 4T RT A31SO 1999091700713 19990917 00713 NM 1999 9 17 99ZZZM633 1 19990715 A 2612 893851 CONNECTOR BOEING 727 7272Q6 138407V NM NR 1 ENGINE DAMAGED A AMTA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 11 782AT 21972 NR 1 ENGINE FIRE WARNING ANNUNCIATOR CAME ON AT 230. ACCOMPLISHED ENGINE FIRE SHUTDOWN PROCEDURE, FIRE HANDLE PULLED AN D FIRED BOTH BOTTLES AND LIGHT REMAINED ON UNTIL AT APPROXIMATELY 3,000 FT. AFTER EXTENSIVE TROUBLESHOOTING CONNECTOR D 400 WAS FOUND WITH AN INTERMITTENT GROUND AT PIN K IN LOOP B WIRE 452-18. REPLACED BAD CONNECTOR AND NEW LOOP WAS INSTA LLED. A/C TESTED AND FOUND OK FOR SERVICE. (M) 2 L 7 3 4F RT A3WE 1999091700714 19990917 00714 NM 1999 9 17 99ZZZM634 1 19990715 A 2170 COELESCER BAG BOEING 727 727227 1384078 NM CABIN DIRTY A AMTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 778AT 22005 AFTER TAKEOFF FLIGHT ATTENDANT REPORTED SMOKE IN THE AFT CABIN. REPLACED LEFT AND RIGHT COELESCER BAGS, ALL OTHER COMPO NENTS IN THE LEFT AND RIGHT ACMS WERE FOUND SPINNING FREELY. OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 1999091700715 19990917 00715 WP 1999 9 17 99ZZZM635 1 19990717 A 5610 1634896102 WINDSHIELD LKHEED 1011 10113851 5265010 WP RIGHT SHORTED A AMTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 191AT 193C1084 DURING CRUISE, FELT STRONG ELECTRICAL ODOR, AFTER APPROXIMATELY 1.5 HOURS CO-PILOTS WINDSHIELD BEGAN TO SMOKE. WINDSHIE LD SYSTEM TURNED OFF. REPLACED RIGHT FORWARD WINDSHIELD, CHECKED FOR OPERATION AND FOUND OK FOR SERVICE. (M) 2 L 7 3 4F A23WE 1999091700716 19990917 00716 WP 1999 9 17 99ZZZM636 1 19990817 A 2910 AE2460001J0165 LINE DOUG DC8 DC861 3021952 WP NR 3 HYD PUMP CHAFED A FXLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 30UA 56829 45888 AFTER TAKEOFF MIA, EXPERIENCED HYDRAULIC QTY LOSS AND PRESSURE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTIO N REVEALED HYDRAULIC PRESSURE LINE CHAFED AT NR 3 ENGIEN HYDRAULIC PUMP. REPLACED LINE, CHECKED FILTERS, SERVICED SYSTE M AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1999091700717 19990917 00717 EU 1999 9 17 C2XA99IA444 1 19990810 A 5320 S53672408223 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FRAME 38-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT C-CHANNEL CORRODED FROM FRAME 38 TO FRAME 39. REMOVED, FABRICATED AND INST ALLED NEW C-CHANNEL IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700718 19990917 00718 EU 1999 9 17 C2XA99IA443 1 19990810 A 5320 S53672408222 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FRAME 38-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT C-CHANNEL CORRODED FROM FRAME 38 TO FRAME 39. REMOVED, FABRICATED AND IN STALLED NEW C-CHANNEL IAW SRM 51-24-01 AND 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700719 19990917 00719 EU 1999 9 17 C2XA99IA442 1 19990810 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOORBEAM AT FRAME NR 38 CORRODED. REMOVED CORROSION AND REPAIRED IAW EC5310- 01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700720 19990917 00720 EU 1999 9 17 C2XA99IA441 1 19990810 A 5315 S53672408202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOORBEAM AT FRAME NR 39 CORRODED. REMOVED CORROSION AND REPAIRED IAW EC5310- 01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700721 19990917 00721 EU 1999 9 17 C2XA99IA440 1 19990810 A 5315 S53672409218 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOORBEAM AT FRAME NR 40 CORRODED. REMOVED CORROSION AND REPAIRED IAW EC5310- 01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700722 19990917 00722 EU 1999 9 17 C2XA99IA439 1 19990810 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 17-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT INBOARD SEAT TRACK CORRODED AND GOUGED FROM FRAME 17 TO FRAME 37. CUT O UT DAMAGED SECTIONS (5 TOTAL), FABRICATED AND INSTALLED REPAIR DOUBLERS IAW EC5340-01018. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700723 19990917 00723 EU 1999 9 17 C2XA99IA438 1 19990810 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT CENTER SEAT TRACK CORRODED FROM FRAME 39 AFT. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-25-04, 51-21-17, 51-21-31, 51-25-02 AND 51-25-03. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700724 19990917 00724 EU 1999 9 17 C2XA99IA437 1 19990810 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 17-37 DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURNG CONTINENTAL EXPRESS C-CHECK, FOUND LEFT OUTBOARD SEAT TRACK CORRODED, GOUGED AND BARE METAL EXPOSED FROM FRAME 17 TO FRAME 37. REPAIRED THREE AREAS FROM FRAME 17 TO FRAME 21 IAW EC5340-01018. REMOVED AND REPLACED SEAT TRACK FROM FRA ME 18 TO FRAME 23 IAW SRM 51-25-04 AND 51-22-02. TREATED EXPOSED METAL ON SEAT TRACK FROM FRAME 23 TO FRAME 37 IAW SRM 51-21-17 AND 51-21-28. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700725 19990917 00725 EU 1999 9 17 C2XA99IA436 1 19990810 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT INBOARD SEAT TRACK CORRODED FROM FRAME 39 TO FRAME 40. REMOVED AND REPL ACED SEAT TRACK IAW SRM 51-25-04, 51-21-17, 51-21-31, 51-25-02 AND 51-25-03. AIRCRAFT APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999091700726 19990917 00726 EU 1999 9 17 C2XA99IA435 1 19990810 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAME 36 TO FRAME 39. REMOVED AND REPLA CED SEAT TRACK IAW SRM 51-25-04, 51-21-17, 51-21-31, 51-25-02 AND 51-25-03. AIRCRAFT APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999091700727 19990917 00727 EU 1999 9 17 C2XA99IA434 1 19990810 A 5320 S5367131831001 PLATE AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND SERVICE DOOR THRESHOLD PLATE CORRODED. REMOVED AND REPLACED THRESHOLD PLATE I AW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700728 19990917 00728 EU 1999 9 17 C2XA99IA433 1 19990810 A 5320 S5367121729402 PLATE AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT ENTRANCE DOOR THRESHOLD PLATE CORRODED. REMOVED AND REPLACED ENTRANCE DO OR THRESHOLD PLATE IAW SRM 51-25-02 AND 51-25-03. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999091700729 19990917 00729 CE 1999 9 17 C2XA99CL086 1 19990819 A 3230 RETRACT MECH BEECH 1900 1900D 1154162 CE LT MLG REQ'D SERVICE A C2XA K NONE J WARNING INDICATION LD LANDING 1 SW 09 49543 UE181 CLE-PIT - FLT 3030 - THE CREW REPORTED THE LEFT MAIN GEAR LIGHT DID NOT ILLUMINATED WHEN THE GEAR WAS SELECTED DOWN. TH E AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE HYDRAULIC RESEVOIR AND PERFORMED OPS CHECK OF THE GEAR IAW B1900D MM 32-30-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999091700730 19990917 00730 NM 1999 9 17 USAASB99198 1 19990728 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 385US 22958 EWR - PILOT REPORTED THAT THE FORWARD ENTRY DOOR EMERGENCY LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE C HARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999091700731 19990917 00731 NM 1999 9 17 TSAA9957379 1 19990805 A 5754 6546421231A SKIN BOEING 737 7372T4 1384492 NM NR 1 LE SLAT INOPERATIVE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 NR 1 LEADING EDGE SLAT L/E SKIN HAS 3 CLOSE DENTS 14.5 INCHES INBOARD OF SLAT OUTBOARD EDGE. HFEC REVEALED NO CRACKS AT DENTS. THREE DENTS LOCALIZED WITHIN 2 INCH AREA WITH DEEPEST POINT .067 INCH DEEP. PER SRM 57-50-1 FIG 2, DENT IS OUT OF LIMITS. REMOVED AND REPLACED NR 1 SLAT IAW MM 27-81-21. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091700732 19990917 00732 WP 1999 9 17 AALA991150 1 19990806 A 2613 S1309 SENSOR DOUG DC9 DC982 3022082 WP TAIL COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 253AA 49286 DFW - FLT 1969 - TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED AFTER TAKEOFF DFW. OCCURRED AFTER GEAR RETRACTION. EMERG ENCY PROCEDURE ACCOMPLISHED AND LIGHT EXTINGUISHED. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED TAIL COMPARTMEN T HIGH TEMPERATURE SENSORS SI-309 AND SI-131. PERFORMED HIGH POWER ENGINE RUN WITH NO LEAKS OR DISCREPANCIES NOTED. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700733 19990917 00733 WP 1999 9 17 AALA991130 1 19990802 A 3230 59104475071 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG LACK OF LUBE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 70401 49312 LGA - FLT 357 - AFTER TAKEOFF LGA FOR ORD, UNABLE TO RETRACT NOSE GEAR. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INC IDENT. LUBED NOSE GEAR AND PERFORMED NOSE GEAR RETRACTION TEST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999091700734 19990917 00734 NM 1999 9 17 TWRA9934 1 19990817 A 3350 S1356B37 LIGHT BOEING 747 747283B 1384867 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 622FF 17089 22496 FOUND 4R CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPS CHECK OK MM 33-52-00. (M) 2 L 7 4 4F A20WE 1999091700735 19990917 00735 NM 1999 9 17 TWRA9933 1 19990817 A 3213 65B012036 STRUT BOEING 747 747130 1384880 NM RT MLG CRACKED A TWRA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 EA 15 603FF 17089 19746 DURING WALK AROUND, FOUND RIGHT BODY GEAR STRUT, OUTER CYLINDER CRACK APPROX .75 INCH IN LENGTH .75 WAY FROM TOP OF CYLI NDER ON FRONT SIDE. REMOVED AND REPLACED STRUT ASSY. (M) 2 L 7 4 4F A20WE 1999091700736 19990917 00736 NM 1999 9 17 TWRA9935 1 19990819 A 3397 WIRE BOEING 747 747283B 1384867 NM L2 DOOR BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 622FF 22496 CROSSOVER STRIP FOR EGRESS LIGHT INOP AT L2 DOOR. REPAIRED BROKEN WIRE. OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1999091700737 19990917 00737 EU 1999 9 17 RAIA990812 1 19990812 A 3150 E83029 CAP PANEL JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 564HK 41081 FLT 7406 - STL - ICE LOOK UP LIGHT ON CAP WILL NOT EXTINGUISH. MAINTENANCE REPLACED CAP PANEL. (M) 2 L 7 2 4T RT A41NM 1999091700738 19990917 00738 1999 9 17 RAIA990818 4 19990814 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 555HK 8465 41072 FLT 7755 - JFK - NR 1 AHRS INOPERATIVE. MAINTENANCE REPLACED NR 1 AHRS. (M) 2 L 7 2 4T RT A41NM 1999091700739 19990917 00739 EU 1999 9 17 RAIA990816 1 19990813 A 2150 1746D000001 PACK JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 562HK 727 41078 FLT 7789 - JFK - RIGHT DUCT OVERTEMP. MAINTENANCE REPLACED RIGHT COLD AIR UNIT. (M) 2 L 7 2 4T RT A41NM 1999091700740 19990917 00740 1999 9 17 RAIA990814 4 19990813 A 3444 6222855001 RADAR ALT BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 431AM 881 FLT 7300 - STL - RADAR ALT INOPERATIVE. MAINTENANCE REPLACED RADAR ALT. (M) 2 L 7 2 4T RT A56EU 1999091700741 19990917 00741 EU 1999 9 17 RAIA990819 1 19990805 A 2120 ASK226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 567HK 41085 FLT 7635 - JFK - RIGHT DUCT FAIL LIGHT ON. MAINTENANCE REPLACED RIGHT INBOARD DUCT SEAL. (M) 2 L 7 2 4T RT A41NM 1999091700742 19990917 00742 NE 1999 9 17 RAIA990822 2 19990816 A 7310 DH8975131 FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 566HK 41084 76109 FLT 7632 - ROC - RIGHT FUEL FILTER LIGHT ON. MAINTENANCE REPLACED FUEL FILTER ON RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999091700743 19990917 00743 WP 1999 9 17 RAIA990821 2 19990816 A 7510 1379287C405 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT ENGINE FAILED A RAIA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 03 435AM 889 66188 FLT 7395 - CGI - EGT FLUCTUATING, OIL PRESSURE GAUGE FLUCTUATING ON LEFT ENGINE. SHUT ENGINE DOWN. MAINTENANCE REPLACE D BLEED LINE FROM ENGINE TO PRECOOLER. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999091700744 19990917 00744 EU 1999 9 17 RAIA990823 1 19990817 A 7921 HTE8600282 ACTUATOR BAG JETSTM JETSTM3201 1500217 EU RT OIL COOLER FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 426AM 874 FLT 7348 - STL - RIGHT OIL COOLER FLAP WILL NOT OPERATE IN MANUAL AND AUTO MODE PREVIOUSLY DEFERRED. MAINTENANCE REPLAC ED RIGHT OIL COOLER FLAP ACTUATOR. (M) 2 L 7 2 4T RT A56EU 1999091700745 19990917 00745 EU 1999 9 17 RAIA990824 1 19990817 A 2731 050287501 LEVER JETAIR JETSTM JETSTM4101 1500501 EU RT ELEVATOR OUT OF POSITION A RAIA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 CE 03 560HK 41076 FLT 7155 - BDL - ELEVATOR CONTROL IS EXTREMELY MUSHY, VERY NON RESPONSIVE. HAD TO USE EXCESSIVE FORCE ON THE TAKEOFF RO LL. MAINTENANCE FOUND RIGHT ELEVATOR CABLE TENSION REGULATOR OUTPUT ARM OFF. REINSTALLED PER CMM 27-10, OPS CHECK GOOD . (M) 2 L 7 2 4T RT A41NM 1999091700746 19990917 00746 SO 1999 9 17 RAIA990825 1 19990818 A 3010 3294453 VALVE EMB 145 EMB145 SO HORIZ STAB FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 803HK 145077 FLT 5794 - ORD - STAB ANTI-ICE FAIL. MAINTENANCE REPLACED HORIZONTAL STAB THERMAL ANTI-ICING VALVE. (M) 2 L 7 2 4F RT T00011AT 1999091700747 19990917 00747 1999 9 17 RAIA990826 3 19990818 A 6140 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT PROP FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 343TE 1318 955 FLT 7030 - COU - RIGHT RPM GAUGE FLUCTUATING. MAINTENANCE REPLACED TACH GENERATOR ON RIGHT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999091700748 19990917 00748 EU 1999 9 17 UF6A990806 1 19990812 A 5320 JF553J0410000 ANGLE BAG ATP ATP EU VERT STAB/FUS CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - CRACK ON LEFT ANGLE WHERE FUSELAGE MEETS THE VERTICAL STABILIZER. MAINTENANCE REPAIRED ANGLE. ALL WORK WAS DONE IAW ENGINEERING REPORT NR 99-149. (M) 2 L 7 2 4T RT A27NM 1999091700749 19990917 00749 EU 1999 9 17 UF6A990803 1 19990810 A 2421 BA03304 GENERATOR BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 GL 31 856AW 10445 1032 2032 ORD - FLT 5748 - THE NR 1 GENERATOR FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 1 GENERATOR. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999091700750 19990917 00750 NE 1999 9 17 UF6A990802 2 19990807 A 7321 324484111 FUEL CONTROL BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE FAILED A UF6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 854AW 9427 B21733N 2028 CWA - FLT 5716 - THE NR 2 ENGIEN WENT TO 120.4 PERCENT AND REMAINED THERE AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLAC ED THE NR 2 MECHANICAL FUEL CONTROL. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999091700751 19990917 00751 EU 1999 9 17 UF6A990772 1 19990730 A 5753 JD275J0036008 FLAP TAB BAG ATP ATP EU LT TE FLAP CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE LEFT INBOARD FLAP TAB IS CRACKED AT STATION 296.366. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW WITH BAE ATP SRM 57-50-01, FIGURE 202. (M) 2 L 7 2 4T RT A27NM 1999091700752 19990917 00752 EU 1999 9 17 UF6A990773 1 19990730 A 5230 JD523J0063002 SKIN BAG ATP ATP EU CARGO DOOR DENT A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE REAR BAGGAGE DOOR HAS A DENT AT THE BOTTOM OF THE RIGHT CORNER. MAINTENANCE REPAIRED DENT. ALL WORK WAS DONE IAW WITH BAE ATP SRM 52-12-01, 51-20-00, 51-10-06, AND 53-30-00. (M) 2 L 7 2 4T RT A27NM 1999091700753 19990917 00753 EU 1999 9 17 UF6A990774 1 19990730 A 5230 JF523J0063002 SKIN BAG ATP ATP EU CARGO DOOR DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE REAR BAGGAGE DOOR HAS A DENT BY THE EXTERNAL DOOR HANDLE. MAINTENANCE REPAIRED DENT. ALL WORK WAS DONE IAW W ITH BAE ATP SRM 52-12-01, 51-20-00, 51-10-06, AND 53-30-00. (M) 2 L 7 2 4T RT A27NM 1999091700754 19990917 00754 EU 1999 9 17 UF6A990775 1 19990730 A 5532 JD553J0001000 SKIN BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE LEFT SIDE OF THE VERTICAL STABILIZER IS CRACKED AT THE TRAILING EDGE ABOVE RIB 29.53. MAINTENANCE FABRICATED NEW SKIN PER SAMPLE WITH 2024T3 .020 INCH AND REPLACED DAMAGED AREA. ALL WORK WAS DONE IAW WITH BAE ATP SRM 55-30-00, 5 1-10-00, AND 51-40-00. (M) 2 L 7 2 4T RT A27NM 1999091700755 19990917 00755 EU 1999 9 17 UF6A990776 1 19990730 A 5532 JD553J0001000 SKIN BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE LEFT SIDE OF THE VERTICAL STABILIZER IS CRACKED AT THE LOWER CORNER NEAR THE RECESS AREA FOR THE RUDDER, LOCAT ED BY THE BOTTOM HINGE. MAINTENANCE FABRICATED NEW SKIN PER SAMPLE WITH 2024T3 .020 INCH AND REPLACED DAMAGED AREA. AL L WORK WAS DONE IAW WITH BAE ATP SRM 55-30-00, 51-10-00, AND 51-40-00. (M) 2 L 7 2 4T RT A27NM 1999091700756 19990917 00756 EU 1999 9 17 UF6A990801 1 19990803 A 7921 10750E OIL COOLER BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 31 852AW 11530 789 2021 ORD - FLT 5721 - NR 1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED IN FLIGHT. ENGINE WAS SHUT DOWN PER EMERGENCY CHECKLI ST. MAINTENANCE REPLACED ENGINE OIL COOLER, DRAINED AND RESERVICED ENGINE OIL. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1999091700757 19990917 00757 EU 1999 9 17 UF6A990777 1 19990730 A 5400 JD711J0291000 MODULE BAG ATP ATP EU LT NACELLE WORN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE MODULAR 6 TITANIUM TUBE HAS A HOLE IN IT AND IS WORN DEEPLY ON BOTH SIDES. MAINTENANCE ROUTED OUT THE HOLE AN D SMOOTHED THE EDGES. THE CHAFFED AREAS WRE BLENDED OUT SMOOTH. ALL WORK WAS DONE IAW WITH ENGINEERING REPORT NR 99-13 1. (M) 2 L 7 2 4T RT A27NM 1999091700758 19990917 00758 EU 1999 9 17 UF6A990816 1 19990818 A 5753 JD275J0036011 FLAP TAB BAG ATP ATP EU TE FLAP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 SBN - LEFT FLAP TAB TRAILING EDGE IS DAMAGED AT STATION 143.366. MAINTENANCE REPAIRED DAMAGE. ALL WORK WAS DONE IAW BA E ATP SRM 57-50-01. (M) 2 L 7 2 4T RT A27NM 1999091700759 19990917 00759 EU 1999 9 17 UF6A990815 1 19990818 A 5400 JD711J0007000 MODULAR 5 BAG ATP ATP EU LT NACELLE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 SBN - RIGHT MODULAR 5 IS PUNCTURED ON TOP AND DELAMINATING. MAINTENANCE REPAIRED DAMAGE. ALL WORK WAS DONE IAW BAE ATP SRM 54-10-01. (M) 2 L 7 2 4T RT A27NM 1999091700760 19990917 00760 EU 1999 9 17 UF6A990813 1 19990818 A 5350 JD553J0410001 FAIRING BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 SBN - RIGHT VERTICAL FAIRING ATTACHMENT TO FUSELAGE IS CRACKED. MAINTENANCE REPAIRED CRACKED. ALL WORK WAS DONE IAW EN GINEERING REPORT NR 99-153. (M) 2 L 7 2 4T RT A27NM 1999091700761 19990917 00761 EU 1999 9 17 UF6A990814 1 19990818 A 5350 JD551J0073000 FAIRING BAG ATP ATP EU HORIZ STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 SBN - LEFT HORIZONTAL FAIRING ATTACHMENT TO FUSELAGE IS CRACKED. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW ENG INEERING REPORT NR 99-153. (M) 2 L 7 2 4T RT A27NM 1999091700762 19990917 00762 EU 1999 9 17 UF6A990817 1 19990819 A 2422 INVERTER BAG ATP ATP EU NR 2 FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 31 858AW 2035 ORD - FLT 5711 - THE NR 2 INVERTER DROPPED OFF LINE DURING TAKEOFF. MAINTENANCE RESET SYSTEM. SYSTEM OPS CHECKED GOOD WITH NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1999091700763 19990917 00763 EU 1999 9 17 UF6A990818 1 19990822 A 3350 GE1317 BULB BAG ATP ATP EU EMER EXIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 15345 2028 SBN - EMERGENCY EXIT LIGHT OVER RIGHT WING INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999091700764 19990917 00764 EU 1999 9 17 UF6A990812 1 19990818 A 5350 JD553J0410000 FAIRING BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 LEFT VERTICAL FAIRING ATTACHMENT TO FUSELAGE IS CRACKED. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW ENGINEERING REPORT NR 99-153. (M) 2 L 7 2 4T RT A27NM 1999091700765 19990917 00765 EU 1999 9 17 UF6A990807 1 19990812 A 5512 JD551J0006000 SKIN BAG ATP ATP EU HORIZ STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - CRACK IN THE LEFT HORIZONTAL STABILIZER TRAILING EDGE AT STATION 45.72. MAINTENANCE REPAIRED DAMAGE. ALL WORK WA S DONE IAW BAE ATP SRM 51-60-01 FIGURE 1. (M) 2 L 7 2 4T RT A27NM 1999091700766 19990917 00766 EU 1999 9 17 UF6A990808 1 19990812 A 3230 JD321J0024001 LEVER BAG ATP ATP EU RT MLG CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - RIGHT MAIN LANDING GEAR LEVER ASSEMBLY HAS A CRACK IN THE ATTACHMENT BRACKET. MAINTENANCE REMOVED AND REPLACED TH E LEVER ASSEMBLY. (M) 2 L 7 2 4T RT A27NM 1999091700767 19990917 00767 EU 1999 9 17 UF6A990811 1 19990810 A 2121 7846261 FAN BAG ATP ATP EU NR 1 FAILED A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 31 859AW 8100 890938 2036 ORD - FLT 5763 - NR 1 RECIRC FAN INOPERATIVE WITH A STRONG BURNING ODOR NOTICED. MAINTENANCE REMOVED AND REPLACED THE N R 1 RECIRCULATION FAN. (M) 2 L 7 2 4T RT A27NM 1999091700768 19990917 00768 EU 1999 9 17 UF6A990805 1 19990810 A 3397 58786 WIRE BAG ATP ATP EU ROW 14-16 FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 ORD - FLOOR PROXIMITY LIGHTING STRIP INOPERATIVE FROM ROW 14CD TO 16CD. MAINTENANCE REMOVED AND REPLACED THE LIGHTING S TRIP. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999091700769 19990917 00769 EA 1999 9 17 VTZA1999025 1 19990726 A 3350 BULB CNDAIR CL600 CL6002B19 EA EXTERIOR FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 623BR 7192 FLT 7730 - GSP-IAD - DURING TAXI, CREW FOUND RT AFT OUTSIDE EMERGENCY LIGHT INOPERATIVE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RELAMPED EMERGENCY LIGHT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999091700770 19990917 00770 EU 1999 9 17 VTZA990251 1 19990724 A 3222 STRUT BAG JETSTM JETSTM3201 1500217 EU NLG REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 474UE 849 FLT 7521 - IAD-PHL - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LANDING GEAR WOULD NOT RETRACT. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPACKED NLG STRUT AND PERFORMED GEAR SWING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999091700771 19990917 00771 EA 1999 9 17 VTZA990250 1 19990722 A 3350 CONNECTOR CNDAIR CL600 CL6002B16 1900305 EA CABIN LOOSE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 621BR 7186 FLT 7776 - IND-IAD - DURING PREFLIGHT, AIRCRAFT STAYED AT GATE DUE TO EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINT ENANCE INSPECTED AND FOUND LOOSE CONNECTOR. MAINTENANCE RESECURED CONNECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999091700772 19990917 00772 EA 1999 9 17 VTZA990249 1 19990721 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT BIRDSTRIKE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK L NO TEST TO TAKEOFF 1 EA 27 631BR 7261 FLT 7776 - IND-IAD - CREW ABORTED TAKEOFF DUE TO BIRDSTRIKE TO LEFT WINDSREEN. AIRCRAFT RETURNED TO GATE WITH NO FURTHE R PROBLEMS. MAINTENANCE INSPECTED FOUND NO DEFECTS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4F RT A21EA 1999091700773 19990917 00773 EU 1999 9 17 VTZA990247 1 19990719 A 7712 TQ SIG COND BAG JETSTM JETSTM3201 1500217 EU LT/RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 474UE 849 FLT 7654 - IAD-PHL - CREW ABORTED TAKEOFF DUE TO BOTH ENGINES TEMPTED OUT BEFORE TARGET TORQUE. AIRCRAFT LANDED AND RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED LEFT AND RT TORQUE SIGNAL CONDITIONS. OPS C HECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999091700775 19990917 00775 EU 1999 9 17 VTZA990244 1 19990718 A 5270 WARNING BAG JETSTM JETSTM3201 1500217 EU PAX DOOR ACTIVATED A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 470UE 814 FLT 7259 - SYR-IAD - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCR AFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CHECKED DOOR AND COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999091700776 19990917 00776 EA 1999 9 17 VTZA990242 1 19990723 A 3340 601R560031 LIGHT CNDAIR CL600 CL6002B19 EA TAIL SECTION FAILURE A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 630BR 7255 FLT 7705 - IAD-BNA - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NAV LIGHT C/B POPPED. AIRCRAFT LANDED A ND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED OPENED DMI 46825, MEL 33-4. MAINTENANCE CLOSED DMI 46825 ON 7/29/99 BY REMOVING AND REPLACING UPPER TAIL NAV LIGHT ASSY. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVE D FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999091700777 19990917 00777 EU 1999 9 17 VTZA990227 1 19990715 A 3350 BATTERY PACK BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 471UE 821 DURING PREFLIGHT CHECK AFTER OVERNIGHT MAINTENANCE, AIRCRAFT EMERGENCY LIGHT TOGGLE SWITCH FOUND IN ON POSITION. MAINTE NANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A56EU 1999091700778 19990917 00778 1999 9 17 VTZA990226 4 19990712 A 2340 B692254 STATION BOX BAG JETSTM JETSTM3201 1500217 EU COCKPIT INOPERATIVE A VTZA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 487UE 906 FLT 7659 - PHL-IAD - DURING TAKEOFF, AIRCRAFT INTERCOM INTERMITTENT AFTER WATER SPILLED FROM DV WINDOW ONTO CAPTAINS LEF T KNEE AND COMM BOX DURING START OF TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE, THEN WAS FERRIED TO IAD. MAINTENANCE REMO VED AND REPLACED STATION BOX, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999091700779 19990917 00779 WP 1999 9 17 USAADD99118 1 19990821 A 3231 39567851 LINK DOUG DC9 DC931 3022065 WP NLG DOOR FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 970VJ 47050 PIT-BNA - FLT 223 - ON GEAR RETRACTION AFTER TAKEOFF THE AIRCRAFT DEVELOPED A SEVERE VIBRATION IN THE NOSE GEAR AREA. T HE VIBRATION INCREASED IN PROPORTION TO AIRSPEED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAIN TENANCE REPLACED THE RIGHT NOSE LANDING GEAR DOOR LINK, INSPECTED THE AREA FOR DAMAGE, AND PERFORMED A NOSE LANDING GEAR RETRACTION AND NOSE LANDING GEAR DOOR FIT CHECK. AN OVERWEIGHT LANDING INSPECTION WAS ALSO PERFORMED. (M) 2 L 7 2 4F A6WE 1999091700780 19990917 00780 WP 1999 9 17 USAAD99119 1 19990822 A 3350 9721050 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822US 49139 BOS - THE EXIT IDENTIFIERS AND ONE SEAT MOUNTED EMERGENCY LIGHT WERE IOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIG HT BATTERIES. (M) 2 L 7 2 4F A6WE 1999091700781 19990917 00781 NM 1999 9 17 TSAA9933402 1 19990816 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K L NONE ABORTED APPROACH L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED FORWARD SERVICE EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F A16WE 1999091700782 19990917 00782 NM 1999 9 17 TSAA9933403 1 19990816 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 1 FLOOR LIGHT EMERGENCY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091700783 19990917 00783 NM 1999 9 17 TSAA9933405 1 19990817 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 AND NR 6 FLOOR PROXIMITY LIGHT BATTERY PACKS DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999091700784 19990917 00784 NM 1999 9 17 TSAA9933397 1 19990819 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED BATTERY PACK FOR NR 5 FLOOR LIGHT ASSY DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700785 19990917 00785 NM 1999 9 17 TSAA9933398 1 19990819 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999091700786 19990917 00786 NM 1999 9 17 AALA991121 1 19990726 A 5320 WEB BOEING 727 727223 1384074 NM BS 950 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - HFEC INDICATES CRACK IN UPPER PRESS DECK AT BEAD FORWARD OF STATION 950, OUTBOARD MOST BEAD. REPAIRED PER ESO 116 97, DATED 7-21-99. (M) 2 L 7 3 4F A3WE 1999091700787 19990917 00787 NM 1999 9 17 AALA991188 1 19990722 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1233 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 712AA 22468 TUL - FOUND STRINGER 16L CRACKED LEFT STATION 1233. CUT OUT DAMAGED SECTION OF STRINGER. INSTALLED DOUBLER REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999091700788 19990917 00788 NM 1999 9 17 AALA991142 1 19990729 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 920 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - STATION 920 STIFFENER AT INBOARD W/W WALL CORRODED AT NUTPLATE LOWER FORWARD CORNER OF APU AIR INTLET SCREEN. REM OVED CORROSION. INSTALLED REPAIR DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999091700789 19990917 00789 NM 1999 9 17 AALA991141 1 19990802 A 5511 SPAR BOEING 727 727223 1384074 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - LEFT HORIZONTAL STAB REAR SPAR UPPER CHORD CORRODED FORWARD OF NR 1 BALANCE PANEL STATION 33-34. BLENDED CORROSIO N PER ESO 11697, PAGES 1 AND 2, DATED 8-2-00. TREATED, PRIMED, SEALED AND PAINTED AREA. (M) 2 L 7 3 4F A3WE 1999091700790 19990917 00790 NM 1999 9 17 AALA991191 1 19990802 A 5720 STIFFENER BOEING 727 727223 1384074 NM WS 265 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 869AA 21374 TUL - FRONT SPAR VERT STIFFENER CORRODED AT TOP JUST OUTBOARD OF FUEL PRESS SWITCHES. REMOVED AND REPLACED STIFFENER WI TH 6 EACH , STEEL HI-LOCKS HL62, 7 EACH STEEL HI-LOCKS HL62 PER SRM 51-10-1 AND SAME PART NR STIFFENER. (M) 2 L 7 3 4F A3WE 1999091700791 19990917 00791 NM 1999 9 17 AALA991190 1 19990809 A 5320 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 869AA 21374 TUL - FOUND BOTTOM OF FRAME CORRODED. REMOVED CORRODED SHEAR TIE AND LEG FROM LOWER FRAME STATION 600, STRINGER 27R-28R PER SRM 53-10-4 FIG 13. FABRICATED AND INSTALLED FRAME REPAIR FOR SHEAR TIE AND LEG PER SRM 53-10-4 FIG 13. (M) 2 L 7 3 4F A3WE 1999091700792 19990917 00792 NM 1999 9 17 AALA991189 1 19990805 A 5320 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 869AA 21374 TUL - FORWARD FROM WEB FOR DOOR CUTOUT HAS CRACK EXTENDING ON BOTH SIDES OF FLUSH RIVET HOLE JUST ABOVE UPPER DOOR STOP CASTING. STOP DRILLED CRACKS IAW SRM 51-10-1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-40-2 FIG 1 . (M) 2 L 7 3 4F A3WE 1999091700793 19990917 00793 NM 1999 9 17 AALA991054 1 19990719 A 5730 SKIN BOEING 727 727223 1384074 NM WS 804 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FOUND CORROSION ON LOWER WING SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER. INSTALLED REPAIR PER SRM 57-30-3 FIG 8 SHE ET 3. (M) 2 L 7 3 4F A3WE 1999091700794 19990917 00794 NM 1999 9 17 AALA991055 1 19990709 A 5320 WEB BOEING 727 727223 1384074 NM BS 1320 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FOUND LEFT HORIZONTAL WEB CRACKED AIRSTAIR TORQUE BOX BELOW ACCESS PLATE STATION 1320. ROUTED OUT CRACK, REPAIRED AS PER B727 SRM CH 51-40-2, TYPICAL WEB REPAIR. (M) 2 L 7 3 4F A3WE 1999091700795 19990917 00795 NM 1999 9 17 AALA990968 1 19990621 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1305 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - SMALL DENT, FORWARD OF EXT POWER PANEL AND CRACK EXTENDING FROM RIVET. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER PER 53-30-3 FIG 5. (M) 2 L 7 3 4F A3WE 1999091700796 19990917 00796 NM 1999 9 17 AALA991001 1 19990702 A 5712 RIB BOEING 727 727227 1384078 NM WS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - LEFT BS 760 RIB CHORD, HFEC SHOWS CRACK INDICATION APPROX .75 INCH AFT OF FLOORBEAM WEB AT LOWER EDGE OF REPAIR DO UBLER. REPAIRED PER SB 727-57-0112 FIG 12 SRM 57-10-5 PAGE 1, E589069177. (M) 2 L 7 3 4F A3WE 1999091700797 19990917 00797 NM 1999 9 17 AALA990967 1 19990622 A 5320 WINDOW FRAME BOEING 727 727223 1384074 NM BS 211.8 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - R-1 WINDOW FRAME CRACKED UPPER RIGHT CORNER. INSTALLED REPAIR DOUBLER UPPER RT CORNER OF R-1 WINDOW FRAME PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999091700798 19990917 00798 WP 1999 9 17 AALA991207 1 19990818 A 5320 SILL DOUG DC9 DC982 3022082 WP BS 1162/1193 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 458AA 49563 TUL - FOUND CORROSION ON SILL BEAM (628R) FROM STATION 1155-1212. REMOVED CORROSION. INSTALLED SRO9520008-15 DOUBLER P ER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 1999091700799 19990917 00799 WP 1999 9 17 AALA991238 1 19990805 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 169 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 285AA 49297 TUL - FOUND LONGERON 4 LEFT SPLICE FS 160 PLUS 9 INCHES TO REPAIR CRACK IN LONGERON AT 4 LEFT FS 160. REPAIR PER SRM 53 -02 FIG 18. (M) 2 L 7 2 4F A6WE 1999091700800 19990917 00800 WP 1999 9 17 AALA991239 1 19990818 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1090 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 285AA 49297 TUL - FUSELAGE SKIN NICK AND GOUGED THROUGH AREA RIGHT OF LONGERON 1 STATION 1070-1110 AFT OF TEAR DROP ANTENNA. BLENDE D DAMAGED AREAS STATION 1070 AND 1110, WITHIN LIMITS. BLENDED GOUGED STATION 1090 OUT OF LIMITS. INSTALLED DOUBLER PER SRM 53-04 PAGE 218F FIG 38. (M) 2 L 7 2 4F A6WE 1999091700801 19990917 00801 EU 1999 9 17 MALA976569 1 19990913 A 3350 6104789 POWER SUPPLY SAAB SF340 SF340A 7850100 EU CABIN INOP A MALA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 15 79XJ 079 EMERGENCY POWER LIGHT ON OVERHEAD ON, FOLLOWED QRH AND CALLED MAINTENANCE CONTROLL. CREW CYCLED ALL EMERGENCY POWER, OF F THEN ON, EMERGENCY POWER LIGHT REMAINED ON. RETURNED TO GATE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY. ALL CHEC KS GOOD. 2 L 7 2 4T RT A52EU 1999091700802 19990917 00802 EU 1999 9 17 MALA976570 1 19990913 A 2611 7211121100 SMOKEDETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 429XJ 429 ON TAXI OUT, CARGO SMOKE WARNING ILLUMINATED, PER QRH NR 1 CARGO EXTINGUISHER ACTIVATED. CARGO SMOKE WARNING EXTINGUISH ED FOR APPROXIMATELY 30 SECONDS AFTER BOTTLE DISCHARGED. RETURNED TO THE GATE. MAINTENANCE REPLACED NR 1 FIRE BOTTLE A ND BOTH SMOKE DETECTOR FOR PRECAUTIONARY REASON. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999091700803 19990917 00803 1999 9 17 MALA976571 4 19990912 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DEPLOYED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 514XJ E2330 FORWARD LEFT CABIN DOOR SLIDE DEPLOYED. MAINTENANCE REPLACED ESCAPE SLIDE IAW 25-60-11. 2 H 7 4 4F RT A49EU 1999091700804 19990917 00804 EU 1999 9 17 MALA976572 1 19990913 A 5240 LATCH BAC 146 AVRO146RJ85A 1500097 EU SERVICE DOOR OUT OF ADJUST A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 515XJ E2333 THE FORWARD RIGHT EXIT DOESN'T STAY LATCHED OPEN. MAINTENANCE TIGHTENED THE HOLO OPEN LATCH TURNBUCKLE ON RIGHT FORWARD EXIT DOOR IAW AVRO DOOR CMM 52-10-13 PG 721. OPS AND SECURITY CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999091700805 19990917 00805 NE 1999 9 17 MALA976573 2 19990912 A 7321 230349306 ECU BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 ENGINE FAILED A MALA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 GL 15 528XJ E2353 AT 31,000 FT, NR 3 ENGINE AIR VALVE LIGHT CAME ON, THEN OIL 3 LOW PRESSURE LIGHT CAME ON, VERIFIED WITH OIL PRESSURE GAU GE IN RED, CREW SHUT DOWN ENGINE. DIVERTED TO STL. MAINTENANCE INVESTIGATED DISCREPANCY, NO LEAK NOTED AND NO FAULT ON ECU. PERFORMED GROUND RUNS PER AMM 71-00-00, PERFORMED OVERSPEED TEST, REPLACED ECU. PERFORMED GROUNDS RUN, OPS CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 1999091700806 19990917 00806 NE 1999 9 17 CALA9901184 2 19990912 A 7250 SEAL BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE CRACKED A CALA C ABORTED TAKEOFF T J ENGINE CASE PENETRATION WARNING INDICATION TO TAKEOFF 1 SW 09 17356 23942 720957 SHORTLY AFTER TAKEOFF FROM PBI, THE NR 1 ENGINE EXPERIENCED AN UNCONTAINED FAILURE AT APPROXIMATELY 1,000 FEET. THE AIR CRAFT WAS RETURNED TO PBI WHERE IT LANDED SAFELY. INITIAL FINDINGS REVEALED DAMAGE TO THE LT SIDE OF THE FUSELAGE AND V ERTICAL STABILIZER. THE AIRCRAFT WAS TAKEN OUT OF SERVICE. THE NR 1 ENGINE WILL BE REMOVED AND REPLACED. INVESTIGATI ON REVEALED THAT THE PRIMARY CAUSE OF FAILURE WAS DUE TO A CRACKED BOLT HOLE FOR THE HPT ROTATING AIR SEAL. SERVICE BUL LETIN 72-9-22 IS BEING ISSUED FOR AN EDDY CURRENT INSPECTION OF THE BOLT HOLE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999091700807 19990917 00807 WP 1999 9 17 9903749918 1 19990912 A 2910 836SD620 FUSE DOUG DC9 DC932 3022066 WP LT HYD SYS BROKEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 940N 66800 66800 47572 LEFT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO DTW. A IRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT HYDRAULIC SYSTEM TOP BRAKE FUSE ON INBOARD SIDE BROKEN OFF. RE PLACED FUSE. ALSO REPLACED ENGINE DRIVEN HYDRAULIC PUMP. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700808 19990917 00808 NM 1999 9 17 9903752714 1 19990910 A 2750 POWER UNIT BOEING 727 7272S7 138407Z NM TE FLAPS FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 718RC 22344 INBOUND TO DTW, AIRCRAFT LOST A SYSTEM HYDRAULICS. CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. DTW MAINTENANCE REPLACED FLAP POWER UNIT AND HYDRAULIC MOTOR. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999091700809 19990917 00809 WP 1999 9 17 9903769878 1 19990911 A 2120 AIR DIST DOUG DC9 DC951 3022051 WP LAVATORY SMOKE A NWAA A F UNSCHED LANDING ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 787NC 48149 DURING CLIMBOUT, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN ALONG WITH AFT LAVATORY SMOKE DETECTOR ACTIVATED. CREW DECLA RED A RED EMERGENCY AND FLIGHT WAS RETURNED TO BUF. AIRCRAFT LANDED WITHOUT INCIDENT. FIRE EXTINGUISHERS IN AFT LAVATO RY WERE UTILIZED TO DAMPEN SMOKE. MAINTENANCE INSPECTED AFT LAVATORIES FOR EVIDENCE OF SMOKE, OVERHEATING, AND/OR ELECT RICAL DAMAGE. NO PROBLEMS WERE FOUND. 2 L 7 2 4F RT A6WE 1999091700810 19990917 00810 EU 1999 9 17 9903773209 1 19990907 A 5310 STRUCTURE AIRBUS 320 A320211 3930320 EU FUSELAGE DAMAGED A NWAA K NONE C F.O.D. IN INSP/MAINT 1 GL 01 309US 118 DURING INSPECTION OF DOOR 1R SLIDE GIRT BAR TRIGGER SPRING PER EO 2561-01223, THE SLIDE DROPPED (UNPACKED) FROM THE DOOR PACKBOARD ASSEMBLY AND THE INFLATION BOTTLE HIT THE GROUND BRAKING AT THE NECK ALLOWING THE BOTTLE TO PROPEL ITSELF INT O THE FORWARD RIGHT UPPER AND LOWER WING TO FUSELAGE FAIRING AREA. FOUR FORMERS WERE DAMAGED ALONG WITH DENTS IN THE FU SELAGE SKIN AND A GOUGE WITH A 1.5 INCH CRACK. REPAIRED SKIN DAMAGE PER A320 SRM. 2 L 7 2 4F RT A28NM 1999091700811 19990917 00811 NM 1999 9 17 9903786615 1 19990911 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 615US 20360 DURING CHECK, E ZONE FLOOR PATH EMERGENCY LIGHTS WOULD NOT TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999091700812 19990917 00812 NM 1999 9 17 9903796626 1 19990912 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 626US 21708 DURING LINE CHECK, FOUND E ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. CHARGED SYSTEM, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999091700813 19990917 00813 NM 1999 9 17 9903806628 1 19990908 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 628US 22389 DURING LINE CHECK, FOUND B AND D ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES AND BATTERIES, O PERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999091700814 19990917 00814 WP 1999 9 17 9903819945 1 19990912 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP TAIL COMPT DIRTY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8925E 45840 DURING PERIODIC CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS ON CATWALK INOPERATIVE. CLEANED CORROSION FROM CATWALK S TRIP CONNECTOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700815 19990917 00815 WP 1999 9 17 9903829156 1 19990911 A 3350 POWER SUPPLY DOUG DC9 DC914 3022034 WP TAIL COMPT INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8915E 45832 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700816 19990917 00816 1999 9 17 9903839150 4 19990907 A 3418 COMPUTER DOUG DC9 DC914 3022034 WP NR 1 STALL WARN MALFUNCTIONED A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 8908E 45749 STALL WARNING SYSTEM ACTIVATED ON APPROACH INTO GSO. CREW ADVANCED THROTTLES TO MECHANICAL STOPS AND EXECUTED GO-AROUND PROCEDURES. NORMAL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT. MAINTENANCE REPLACED NR 1 STALL WARNING TRANSDUCER AND STALL WARNING COMPUTER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999091700817 19990917 00817 NM 1999 9 17 UPS99230623 1 19990914 A 3350 LIGHT BOEING 727 72751C 1384015 NM PAX DOOR DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE:N/A, MAIN ENTRY DOOR EMERGENCY LIGHTS DIM. REMOVED AND CLEANED LENS, CHECKS OK. 2 L 7 3 4F A3WE 1999091700818 19990917 00818 NM 1999 9 17 UPS99430619 1 19990913 A 5414 PANEL BOEING 747 747212B 1384886 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A, NR 4 PYLON PANEL CRACKED. REPAIRED PANEL IAW B747-5430-11517. 2 L 7 4 4F A20WE 1999091700819 19990917 00819 WP 1999 9 17 UPS99830620 1 19990914 A 2560 SLIDE DOUG DC8 DC873F 302199F WP CABIN DETACHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:N/A, ESCAPE SLIDE FELL OUT OF CONTAINER WHEN S/O ATTEMPTED TO ARM. *S/D* REPACKED SLIDE TO FREE UP GIR T BAR. 2 L 7 4 4F RT 4A25 1999091700820 19990917 00820 WP 1999 9 17 UPS99830621 1 19990914 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP NR 6 INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:N/A, NR 6 SMOKE DETECTOR WILL NOT TEST. DEFERRED IAW MEL 26-10-1, PLACARD INSTALLED. 2 L 7 4 4F RT 4A25 1999091700821 19990917 00821 WP 1999 9 17 UPS99830622 1 19990913 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:N/A, 1 INCH CRACK UPPER AFT CORNER FUSELAGE PIT 34. *S/D* REPAIRED CRACK IAW SRM 53-02-00. 2 L 7 4 4F RT 4A25 1999091700822 19990917 00822 NM 1999 9 17 99FDEA00386 1 19990915 A 2612 FIRE LIGHT BOEING 727 7272D4 138407U NM NR 2 ENGINE ILLUMINATED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 287FE 21849 THE 2 FIRE WARN BELL CUTOUT LIGHTS ILLUM. ALL ENG INSTRUMENTS AND IND WERE NORMAL. TESTED ALL ENGINE FIRE LOOPS PER 72 7 MM 26-11-001-0, ALL TEST NORM. RAN ALL ENG PER JET RUN HDBK, NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1999091700823 19990917 00823 NM 1999 9 17 99FDEA00387 1 19990915 A 2120 AIR DIST BOEING 727 72722C 138400F NM CARGO COMPT FUMES A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 113FE 19894 AIRCRAFT NEEDS INSP FOR ODOR. CVG FIRE DEPT FOUND FUMES EMANATING FROM CRATE IN NR 2 CONTAINER. RAMP AGENT REMOVED CRA TE. INSP AC COMP AND FOUND NO CONTAMINATION OR DEFECTS. FUMES FROM SOLID OBJECTS IN CRATE. 2 L 7 3 4F A3WE 1999091700824 19990917 00824 WP 1999 9 17 MWEA99600 1 19990914 A 2740 95906 TRIM MOTOR DOUG DC9 DC932 3022066 WP HORIZ STAB MALFUNCTIONED A MWEA K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 31 301ME 47190 PRIMARY TRIM RAN AWAY RUNNING FORWARD. REPLACED PRIMARY TRIM MOTOR. 2 L 7 2 4F A6WE 1999092100002 19990921 00002 WP 1999 9 21 ASAA9980166 1 19990730 A 5610 WINDOW DOUG DC9 DC982 3022082 WP RT COCKPIT DIRTY A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 951AS 49111 SEA - AFTER ARRIVAL OF FLT 383 - CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. REMOVED DEBRIS FROM WINDOW TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999092100003 19990921 00003 NM 1999 9 21 DL72L991895 1 19990820 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 NR 5 INB'D FLAP TRACK AD 90-07-05 AND 90-06-09 TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUGS. AUTHORIZED MACHINING CORROSION AND WEAR. INSTALLED SPLICE PLATE REPAIR TO MLG BEAM ATTACH PAD AS PER SB 57-0178. 2 L 7 3 4F A3WE 1999092100004 19990921 00004 EU 1999 9 21 C2XA99IA416 1 19990831 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING MAINTENANCE INSPECTION, THE RIGHT FRONT EMERGENCY EXIT FLOOD LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999092100005 19990921 00005 NM 1999 9 21 QXEA9901675 1 19990821 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 202-222 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - LEFT-HAND INBOARD SEAT TRACK FROM STA 202.750 TO 222.700 HAS MINOR SURFACE CORROSION AND LIGHT PITTING. REPAIRED IAW SHC-8 SRM 51-40-11 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999092100006 19990921 00006 NM 1999 9 21 QXEA9901676 1 19990818 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CARGO COMPT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS MINOR CORROSION WHERE CARGO TIE DOWN MOUNTS. REPAIRED IAW HORIZON AIR EA 2-53-7 3. 2 H 7 2 4T RT A13NM 1999092100010 19990921 00010 NM 1999 9 21 HNAA9900117 1 19990903 A 2431 522487 TEMP MONITOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT FAILED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 938HA 28330 152 SMOKE IN COCKPIT AROUND BATTERY TEMP MONITOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1999092400001 19990924 00001 WP 1999 9 24 TWAA9912601 1 19990908 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP TAIL CONE DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 923TW 49379 THE TAIL CONE SLIDE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY. CHECK-C 8-3-99 STL. 2 L 7 2 4F RT A6WE 1999092400002 19990924 00002 NM 1999 9 24 TWAA9912602 1 19990903 A 3350 1313 LAMP BOEING 757 757231 1384950 NM ROW 3 AND 4 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 711ZX 28481 THE OVERHEAD EMERGENCY LIGHTS BETWEEN CABIN ROWS 3 AND 4 WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 11-20-98 LAX. 2 L 7 2 4F RT A2NM 1999092400003 19990924 00003 NM 1999 9 24 9903842285 1 19990721 A 5314 KEEL BEAM BOEING 727 727251 138408H NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 285US 21324 DURING M-CHECK, FOUND CORROSION ON KEEL BEAM IN AFT CARGO BAY FS 950, WL 150, RBL 10. REPAIRED PER EA 22-167932. 2 L 7 3 4F A3WE 1999092400004 19990924 00004 NM 1999 9 24 9903852285 1 19990702 A 5314 KEEL BEAM BOEING 727 727251 138408H NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 285US 21324 DURING M-CHECK, FOUND CORROSION ON THE LOWER OUTBOARD FLANGE OF THE LEFT KEEL BEAM FS 950. REPAIRED PER EA 22-167917. 2 L 7 3 4F A3WE 1999092400005 19990924 00005 NM 1999 9 24 9903862285 1 19990721 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 380 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 285US 21324 DURING M-CHECK, FOUND CORROSION ON THE UPPER FLANGE OF THE FLOORBEAM FS 380, RBL 8. REPAIRED PER EA 22-167934. 2 L 7 3 4F A3WE 1999092400006 19990924 00006 NM 1999 9 24 9903872285 1 19990721 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 285US 21324 DURING M-CHECK, FOUND CORROSION ON THE UPPER FLANGE OF THE FLOORBEAM AT FS 1130, RBL 25 AND RBL 45. REPAIRED PER EA 22- 167937. 2 L 7 3 4F A3WE 1999092400007 19990924 00007 SO 1999 9 24 COMA9910147 1 19990915 A 2460 M61628 RELAY EMB 120 EMB120RT SO ELEC BAY FAILED A COMA K NONE O OTHER CL CLIMB 1 SO 01 263CA 1255 THE EMERGENCY BUS LIGHT ILLUMINATED DURING FLIGHT AND WOULD NOT EXTINGUISH. REPLACED RELAY KO440. 2 L 7 2 4T RT A31SO 1999092400008 19990924 00008 EA 1999 9 24 COMA9960520 1 19990915 A 5320 601R3113 CLIP CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 PERFORMED A MAJOR REPAIR BY REPLACED CRACKED CLIPS AT FS 280 LBL 9 IAW WVAC EO 601R-53-0326A. 2 L 7 2 4F RT A21EA 1999092400009 19990924 00009 EA 1999 9 24 COMA9960521 1 19990915 A 5320 6003106819 DOUBLER CNDAIR CL600 CL6002B19 EA BS 461 DOUBLE DRILLED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 DURING THE REMOVAL OF DOUBLER PLATE (P/N 600-31068-19) THE ATTACHMENT HOLE WAS DOUBLE DRILLED. PERFORMED A MAJOR REPAIR TO DOUBLER PLATE (P/N 600-53-0324B). 2 L 7 2 4F RT A21EA 1999092400010 19990924 00010 EA 1999 9 24 COMA9960523 1 19990905 A 5320 601R530312 CLEAT CNDAIR CL600 CL6002B19 EA BS 484 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 7080 CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 HAS AN APPROXIMATELY 0.75 INCH CRACK IN THE RADIUS. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED CLEAT (P/N 601R3117-009) AT FS 484 RBL 27 IAW WVAC EO 601R-53-0312B. 2 L 7 2 4F RT A21EA 1999092400011 19990924 00011 EA 1999 9 24 COMA9960524 1 19990915 A 3260 TARGET CNDAIR CL600 CL6002B19 EA RT MLG LOOSE A COMA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 SO 01 977CA 7157 GEAR DISAGREE WARNING DURING CLIMBOUT FROM YUL. ADJUSTED THE RIGHT MLG PROXIMITY SENSOR UPLOCK TARGET PER TASK 32-61-05 -400-801. 2 L 7 2 4F RT A21EA 1999092400012 19990924 00012 EA 1999 9 24 COMA9960525 1 19990915 A 5315 601R311367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 310-355 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 FUSELAGE FLOORBEAM CAPS (P/N 601R31113-67) CORRODED OUT OF LIMITS PER CRJ REO 601R-53-00-005 REV AT RBL 27 FS 310 TO FS 355 AND RBL 9 FS 310 TO FS 355. PERFORMED A MAJOR REPAIR BY REPLACING FLOORBEAM CAPS (P/N 601R3113-67) AT RBL 27 FS 280 TO FS 409 AND RBL 9 FS 280 TO FS 355 IAW CRJ REO 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999092400013 19990924 00013 EA 1999 9 24 COMA9960526 1 19990914 A 3320 BR9800001 BULB CNDAIR CL600 CL6002B19 EA ROW 2&3 FAILED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 943CA 7042 ELECTRICAL ODOR IN THE AREA OF CABIN SEATING ROWS 2 AND 3 DURING FLIGHT. AIRCRAFT RETURNED TO CVG. REPLACED CEILING LI GHT BULBS ABOVE SEATS 2 AND 3. 2 L 7 2 4F RT A21EA 1999092400014 19990924 00014 NM 1999 9 24 UPS99230627 1 19990914 A 5320 SUPPORT BOEING 727 72725C 138400H NM BS 259-277 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, FOUND CORROSION OF FLOOR SUPPORT AT LBL 15 FROM BS 259 TO BS 277. REMOVED CORROSION AND REPAIRED PE R BAC DRAWING 65-17593 SH4. 2 L 7 3 4F A3WE 1999092400015 19990924 00015 NM 1999 9 24 UPS99230628 1 19990914 A 5320 SILL BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, FOUND SILL WEB TO HAVE CORROSION ON BOTTOM SIDE OF WEB. REMOVED CORROSION AND REPAIRED PER SRM 51-4 0-2. 2 L 7 3 4F A3WE 1999092400016 19990924 00016 NM 1999 9 24 UPS99230629 1 19990913 A 5320 WEB BOEING 727 72725C 138400H NM BS 219.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-221-01.03-01) ON WEB AT BS 219.8 WL 211-214 AND WL 227-233 LBL 39. REMOVED CORROSION AT WEB, BS 219, LBL 39, WL 211-214 AND WL 227-233, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED WEB REPAIR PER SRM 51-40-2. 2 L 7 3 4F A3WE 1999092400017 19990924 00017 WP 1999 9 24 UPS99830624 1 19990915 A 3231 MECHANISM DOUG DC8 DC871F 302199D WP RT MLG DOOR OUT OF ADJUST A IPXA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 01 713UP 46014 INSPECTION TYPE:N/A, AFTER TAKEOFF DURING GEAR RETRACTION DOOR NOT LATCHED (RIGHT) REMAINED ILLUMINATED. CHECKLIST FOLL OWED, AFTER THREE GEAR RETRACTION CYCLES LIGHT FINALLY EXTINGUISHED. ADJUSTED RIG ON RIGHT HAND MAIN GEAR DOOR ACTUATOR PER M/M 32-32-07. GROUND OPS CHECK, NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999092400018 19990924 00018 WP 1999 9 24 UPS99830631 1 19990915 A 2830 FUEL DUMP DOUG DC8 DC871F 302199D WP FUEL SYSTEM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A, CORROSION AND METAL DISTRESS FOUND ON LEFT FUEL DUMP. ACCOMPLISHED INTERIM REPAIR PER EO DC-8-5720 -1158-A, ITEM DEFERRED PER EO DC8-5720-11858-A. SPEED TAPE APPLIED, OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 1999092400019 19990924 00019 WP 1999 9 24 99FDEA00388 1 19990914 A 5347 S4929147 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 635&755 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 310FE 48299 MAIN DECK UPPER CARGO, SEAT TRACK CRACKED AT BS 635 X=27.5-242. UPPER CARGO SEAT CRACK AT BS Y=755 INTERSECTING X=8.5. *S/D* REPAIRED MDUC PER SRM 53-70-00 VOL 1-242 & UCST PER SRM 53-70-00 VOL 1-243. 2 L 7 3 4F RT A22WE 1999092400020 19990924 00020 WP 1999 9 24 ABXA9900709 1 19990903 A 5312 5910130293 STIFFENER DOUG DOUG DC9 DC941 302207N WP AFT FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD, AFT SIDE STIFFENER CRACKED AT BOTTOM OF VENTRAL DOOR CUTOUT. REPAIRED IAW DC9 SRM DRAWING K05159. 2 L 7 2 4F A6WE 1999092400021 19990924 00021 WP 1999 9 24 ABXA9900710 1 19990903 A 7830 5958775513 TR BUCKET DOUG DOUG DC9 DC941 302207N WP NR 1 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND NR 1 ENGINE UPPER THRUST REVERSER BUCKET INBOARD LOWER SKIN CRACKED AFT OF IDLER LINK ATTACH POINT . REPLACED NR 1 ENGINE UPPER THRUST REVERSER BUCKET. 2 L 7 2 4F A6WE 1999092400022 19990924 00022 WP 1999 9 24 ABXA9900711 1 19990903 A 5400 591326244 ANGLE DOUG DOUG DC9 DC941 302207N WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND THE NR 2 PYLON UPPER ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1999092400023 19990924 00023 WP 1999 9 24 ABXA9900712 1 19990909 A 5320 991224644 SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 1038 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 1038 AND LONGERON 18 RIGHT. REPLACED SHEAR TIE IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999092400024 19990924 00024 WP 1999 9 24 ABXA9900713 1 19990909 A 5320 3912286503 FITTING DOUG DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 DURING C-CHECK, FOUND FRAME ATTACH FITTING CRACKED AT KEEL WEB. REPLACED FRAME FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999092400025 19990924 00025 WP 1999 9 24 ABXA9900714 1 19990909 A 5240 59215061 SKIN DOUG DOUG DC9 DC931 3022065 WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 DURING C-CHECK, FOUND SERVICE DOOR EXTERIOR SKIN CRACKED. REPAIRED SERVICE DOOR IAW DC9 SRM 52-01. 2 L 7 2 4F A6WE 1999092400027 19990924 00027 CE 1999 9 24 99ZZZX3468 1 19990817 A 7120 5038913315 ISOLATOR BEECH 99 99 1154002 CE LT ENGINE DETERIORATED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 24BM U67 LEFT ENGINE VIBRATION ISOLATORS APPEAR TO BE DETERIORATED BEYOND NORMAL WEAR. VIBRATION ISOLATORS WERE REPLACED WITH NE W ISOLATORS. THE CAUSE OF THE DETERIORATION WAS UNKNOWN AND DID NOT APPEAR TO BE AGE RELATED. 1 L 7 2 3T A14CE 1999092400034 19990924 00034 CE 1999 9 24 99ZZZX3475 1 19990813 A 5751 122005312 HINGE ASSY CESSNA 206 U206G 2073356 CE RT WING CRACKED A HXXC K NONE O OTHER IN INSP/MAINT 1 AL 03 733KD 8120 U20604772 BOTH INBOARD AND OUTBOARD AILERON HINGE BRACKET ASSYS ON THE RIGHT WING WERE CRACKED ON THE BOTTOM AND HAD LOOSE OF SHEA RED RIVETS WHERE THEY ATTACH TO THE REAR SPAR. THIS DAMAGE CANNOT BE SEEN WITHOUT REMOVING THE FALSE SPAR, BUT CAN BE D ETECTED BY LOOSENESS OF THE BRACKET UP AND DOWN. 1 H 7 1 3O A4CE 1999092400038 19990924 00038 CE 1999 9 24 99ZZZX3479 1 19990827 A 3230 98810017235M50D7 RELAY BEECH 58 58 1152740 CE GEARBOX FAILED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 78RE TH371 TRB - LANDING GEAR WOULD NOT EXTEND, TRIPPED CIRCUIT BREAKER. LANDING GEAR GEARBOX JAMS AT GEAR UP POSITION, SUSPECT DY NAMIC BREAK RELAY NOT STOPPING GEAR MOTOR SOON ENOUGH. REMOVED AND REPLACED GEARBOX AND RELAY. OPS CHECKS GOOD. 1 L 7 2 3O 3A16 1999092400039 19990924 00039 SO 1999 9 24 99ZZZX3480 2 19990826 A 7322 FUEL SERVO BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO RT ENGINE FAILED A BSYA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 GL 07 2892W TH389 810935A RIGHT ENGINE QUIT ON FINAL APPROACH. ROD CAME OFF FUEL SERVO TO THROTTLE PLATE CAUSING LEAN MIXTURE. REPLACED LEVER, R OD, AND SPRING. OPS CHECKS GOOD. 1 L 7 2 3O 3 O 3A16 E5CE 1999092400040 19990924 00040 SO 1999 9 24 99ZZZX3481 1 19990804 A 7933 53583000 PROBE PIPER PA31 PA31350 7103110 SO RT ENGINE MALFUNCTIONED A BSYA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 525AA 3682 318052111 RIGHT OIL TEMPERATURE WENT TO RED LINE ON TAKEOFF, ABORTED TAKEOFF. 1 L 7 2 3O A20SO 1999092400044 19990924 00044 SO 1999 9 24 99ZZZX3485 1 19990802 A 2140 A23D0475 REGULATOR PIPER PA31 PA31350 7103110 SO HEATER LEAKING A WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3527U 170 317952141 DURING ROUTINE INSPECTION, REGULATOR WAS FOUND LEAKING AT UPPER GASKET. 1 L 7 2 3O A20SO 1999092400055 19990924 00055 CE 1999 9 24 99ZZZX3496 1 19990830 A 2910 2407003466 LINE LEAR 25 25D 5170514 CE HYDRAULIC SYSTEM CRACKED A MXIA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 21 321GL 2117 289 THE LEFT ENGINE HYDRAULIC PRESSURE LINE CRACKED UNDER AN ADEL CLAMP THAT SECURED THE LINE TO THE AIRCRAFT STRUCTURE LOCA TED ABOVE AND AFT OF THE GENERATOR CONTROL UNIT. THE LINE HAD BEEN BADLY WORN BY TWO CLAMPS. ANYTIME AN ACCUMULATION O F BLACK RESIDUE IS NOTED AROUND THESE CLAMPS DURING AN INSPECTION, REMOVE THE CLAMPS AND INSPECT THE TUBING FOR WEAR. 2 L 7 2 4J A10CE 1999092400064 19990924 00064 NM 1999 9 24 99ZZZX3505 1 19990824 A 7500 H610026 LINE AEROCD 100 100 NM BLEED AIR CRACKED A DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 36WH 76 BE26 PILOT NOTED DUAL BLEED AIR FAIL LIGHTS ON MASTER CAUTION PANEL. PILOT FERRIED AIRCRAFT BACK TO HOME BASE WITHOUT INCIDE NT. TROUBLESHOT TO CRACKED BLEED AIR LINES. REPLACED CRACKED LINES. GROUND CHECK OK. 1 L 7 1 3O NT 1A21 1999092400070 19990924 00070 CE 1999 9 24 99ZZZX3511 1 19990823 A 3244 9543991 TIRE LEAR 25 25 5170506 CE MLG FAILED A KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 39CK 49 005 THREE MAIN WHEEL TIRES BLEW ON LANDING. REPLACED ALL MAIN WHEEL AND BRAKE ASSEMBLIES WITH SERVICEABLE UNITS. FUNCTIONA L CHECK OF ANTI-SKID SYSTEM AND PARKING BRAKE SYSTEM RIGGING CHECKED IAW THE LEARJET 25 SM. SYSTEMS CHECKED NORMAL AT T HIS TIME. 2 L 7 2 4J A10CE 1999092400071 19990924 00071 CE 1999 9 24 99ZZZX3512 1 19990809 A 3230 124001GCR0445 HOSE BEECH 99 99A 1154003 CE NLG CHAFED A TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 32GCA U135 NOSE GEAR HYDRAULIC HOSE CHAFED THROUGH 6 INCHES AFT OF FORWARD BULKHEAD AND LEAKED FLUID OUT OF SYSTEM. 1 L 7 2 3T A14CE 1999092400199 19990924 00199 EU 1999 9 24 CA990420008 1 19990408 A 2435 230321423 BELL ASSY AIRCRFTPRDTS 150SG122Q SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE STARTER/GEN WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 7496 7022 (CAN) STARTER/GENERATOR REC'D FOR REPAIR AT 1056 HOURS TSO (1600 HOURS TBO) WITH WORN COMMUTATOR. UPON DISASSY/INSPECTI ON, LUCAS P/N 23032-1423 (A.D.E) END BELL ASSY WAS FOUND. THIS PART IS NOT APPROVED FOR INSTALLATION AND WAS FOUND WORN BEYOND LIMITS AT THE BEARING LINER. THE OWNER'S MAINTENANCE RECORDS ARE COMPLETE TO ZERO HOURS TSN, THUS PREVIOUS OVER HAUL AMO'S WHO PREVIOUSLY WORKED ON SUBJECT STARTER/GENERATOR ARE BEING CONTACTED FOR INFORMATION. THE SUBJECT PART IS IN QUARANTINE. 1 G 7 1 3U 3 U H9EU E19EU 1999092400201 19990924 00201 CE 1999 9 24 CA990907010 1 19990804 A 3222 MS28775335 O-RING 5082019637 BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA NLG ABRADED W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA 35 (CAN) OLEO WENT FLAT, LOST ALL OIL AND NITROGEN AFTER A NORMAL LANDING. AIRCRAFT WAS FUELED AND CREW DEPARTED FOR 7 HOU RS - UPON RETURN, OLEO WAS FLAT. LANDING GEAR HAD BEEN OVERHAULED AND INSPECTED FOR FIVE YEAR REQUIREMENT 07/12/99. UP ON INSPECTION OF ASSY, UPPER SEAL 'O' RING WAS FOUND TO BE ROLLED AND ABRADED ALMOST 1/4 OF CIRCUMFERENCE. NEW SEAL INS TALLED. NOTE: THERE IS A SPECIFIC PROCEDURE FOR INSTALLATION IN COMPONENT MAINTENANCE MANUAL. 1 L 7 2 3T 4 T A14CE E4EA 1999092400203 19990924 00203 SO 1999 9 24 CA990907026 1 19990126 A 3233 BEARING 2185500 PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA MLG ACTUATOR WORN W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION DE DESCENT 1 CA RL350155A (CAN) LANDING GEAR WOULD NOT EXTEND FOR LANDING. PILOT HAD TO USE EMERGENCY MANUAL EXTENSION. AFTER TEARDOWN, FOUND BA LL BEARINGS WORN AND JAMMED IN ACTUATOR HOUSING. 1 L 7 2 3O 3 O A1EA 1E12 1999092400204 19990924 00204 1999 9 24 CA990907035 4 19990810 A 3120 CLOCK MORAVN Z142 Z142 EU COCKPIT INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA 855 (CAN) DUE TO RECENT SHORTING AND MELTING OF CLOCKWIRE IN LIKE MODEL AIRCRAFT (FQUIE) THE CLOCK WAS INSPECTED FOR THE PRE SENCE OF A CIRCUIT PROTECTING DEVICE. NONE WAS FOUND LEAVING THE CLOCK WIRE 'HOT'. AN IN-LINE FUSE WAS INSTALLED AT T HE BATTERY SWITCH. 1 L 7 1 3O NT A76EU 1999092400205 19990924 00205 CE 1999 9 24 CA990907037 1 19990818 A 3320 6900042 BALLAST 6900026 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA CABIN OVERHEATED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA PCE80277 (CAN) CABIN LIGHTING WAS TURNED ON RESULTING IN AN ELECTRICAL BURNING ODOR AND SMOKE. LIGHTING AND ALL ELECTRICS WERE T URNED OFF. MAINTENEANCE FOUND A BURNED LIGHTING BALLAST UNIT. 1 L 7 2 4T 4 T A24CE E4EA 1999092400206 19990924 00206 SO 1999 9 24 CA990907038 1 19990807 A 3233 BRUSHES BOSCH 1711920MO27M PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA MLG MOTOR WORN W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 101477 RL350155A (CAN) GEAR WOULDN'T COME UP. CIRCUIT BREAKER DID NOT TRIP. WARNING HORN WENT OFF WHEN MANIFOLD PRESSURE AT 15. NOTICE D NOSE GEAR PARTIALLY DOWN IN MIRROR. CYCLED GEAR A FEW TIMES, GEAR CAME DOWN AND LOCKED SHOWING GREEN LIGHT. 1 L 7 2 3O 3 O A1EA 1E12 1999092400207 19990924 00207 SO 1999 9 24 CA990907040 1 19990825 A 7331 LINE PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA LT NACELLE BROKEN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA RL350155A (CAN) LOST FUEL FLOW INDICATION ON LEFT ENGINE. FOUND FUEL FLOW SENSE LINE AFT OF ENGINE FIREWALL IN NACELLE BROKEN OFF . CAUSE MOST LIKELY FROM VIBRATION/FLEXING OF LINE. LINE REPAIRED. 1 L 7 2 3O 3 O A1EA 1E12 1999092400208 19990924 00208 SO 1999 9 24 CA990907041 1 19990817 A 2730 71056003 SPRING PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA STABALIZER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA L346161A (CAN) DURING A ROUTINE INSPECTION OBSERVED SOME SMALL MINUTE CRACKING AROUND THE RADIUS OF EACH HOOK END. SPRING AND LI NK CHANGED OUT WITH NEW, OLD SPRING TAGGED AND PLACED IN QUARANTINE. 1 L 7 2 3O 3 O A20SO E14EA 1999092400209 19990924 00209 1999 9 24 99ZZZX3517 4 19990715 A 2215 SERVO COLLINS BEECH 1900 1900D 1154162 CE RUDDER MISMANUFACTURED A GLBA K NONE F W FLT CONT AFFECTED INADEQUATE Q C CR CRUISE 1 CE 01 192GL 137 8210 UE192 AIRCRAFT YAWS LEFT AND RIGHT UNCOMMANDED (SAME CONDITION WITH YAW DAMP 'OFF'). SELECTED RUDDER BOOST TO 'OFF' AND CONTI NUED FLIGHT WITH NO ADDITIONAL PROBLEMS. TROUBLESHOOTING BY MAINTENANCE PERSONNEL FOUND PRIMARY RUDDER SERVO TO BE DRIV ING RUDDER IN WRONG DIRECTION. REMOVED AND REPLACED RUDDER SERVO. POST-INSTALLATION TESTS PERFORMED SATISFACTORILY. T EAR DOWN OF RUDDER SERVO REVEALED IMPROPER ASSEMBLY FOLLOWING REPAIRS BY CERTIFIED REPAIR STATION. COMPONENT P/N SVO656 225734002. 2 L 7 2 4T RT A24CE 1999092400210 19990924 00210 NM 1999 9 24 P2EA99225 1 19990811 A 3260 CONTROL HANDLE BOEING 737 7372Q8 138448K NM LANDING GEAR LACK OF LUBE A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 121NJ 21735 MCI - FLT 402 - AFTER TAKEOFF WHEN THE LANDING GEAR WAS PLACED IN THE UP POSITION, ALL 3 GEAR LIGHTS REMAINED ON (RED). THE SAME INDICATION WAS PRESENT IN THE LANDING GEAR HANDLE. DISCOVERED LANDING GEAR CONTROL HANDLE STICKING. CLEANED AND LUBED HANDLE. PERFORMED GEAR POSITION SENSOR TEST IAW MM 32-61-00. NO DEFECTS NOTED. (X) 2 L 7 2 4F RT A16WE 1999092400211 19990924 00211 NM 1999 9 24 P2EA99224 1 19990809 A 3244 TIRE BOEING 737 7372Q8 138448K NM NLG FAILED A P2EA O OTHER C D F.O.D. INFLIGHT SEPARATION TO TAKEOFF 1 CE 05 121NJ 21735 MDW - FLT 744 - ON TAKEOFF ROLL, PILOT HEARD A LOUD BANG. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. UPON INSPECTION, FOUND NOSE TAXI LIGHT LENS BROKEN, BOTH NLG TIRES WITH MANY CUTS AND NR 3 AND NR 4 MAIN TIRES OUT. REMOVED AND REPLACE D NOSE TAXI LIGHT ASSY IAW MM 33-42-51. REMOVED AND REPLACED BOTH NLG WHEELS IAW MM 32-45-21. REMOVED AND REPLACED NR 3 AND NR 4 MAIN WHEELS IAW 32-45-11. (X) 2 L 7 2 4F RT A16WE 1999092400212 19990924 00212 CE 1999 9 24 COEA9902876 1 19990826 A 2612 4779000B CONTROL UNIT CESSNA 208 208B 2073701 CE FIRE DETECTOR MALFUNCTIONED A COEA O OTHER N FALSE WARNING CR CRUISE 1 NM 13 876FE 3831 8915017 208B0207 FIRE WARNING HORN AND LIGHT ACTIVATE INTERMITTENTLY IN-FLIGHT. MAINTENANCE REPLACED FIRE DETECTOR CONTROL. TESTED OK. AIRCRAFT RETURNED TO SERVICE. (X) 1 H 7 1 3T A37CE 1999092400213 19990924 00213 NE 1999 9 24 99ZZZX3518 1 19990611 A 6410 7615007100053 BLADE 761500904305 SKRSKY S76 S76C 8143008 NE TAIL ROTOR FRACTURED D A A UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CR CRUISE 1 SO 11 110AL A0860192 760385 TIP CAP REMOVED FROM SIKORSKY OTR. INSTALLED ON BLUE BLADE. AIRCRAFT FLOWN ABOUT 1.50 HOURS. CREW HEARD 'BANG' FOLLOW ED BY HEAVY VIBRATION. LANDED, FOUND AFT ONE-THIRD OF TIP CAP MISSING. NO INDICATION OF HAVING STRUCK ANYTHING. SUBMI TTER STATED THIS CAP HAD BEEN TAKEN OFF AND REPLACED AT LEAST THREE TIMES FOR PAINT AND FILLER PROBLEMS. 1 G 7 2 3U NC H1NE 1999092400216 19990924 00216 NM 1999 9 24 99ZZZX3521 1 19990412 A 7933 900D3658007101 THERMAL VALVE DOUG MD900 MD900 3027375 NM OIL COOLER FLUCTUATING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 154 257 90000012 OIL TEMPERATURE FLUCTUATION TO VALVE (NOT SEATING). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999092400217 19990924 00217 NM 1999 9 24 99ZZZX3522 1 19990604 A 6710 900C2010214101 PITCH LINK DOUG MD900 MD900 3027375 NM MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 327 90000012 PITCH LINK WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999092400219 19990924 00219 SW 1999 9 24 99ZZZX3524 1 19990821 A 6510 407340340101 DISC PACK 407040302101 BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL 537 50 RNFS2273 53141 ONE DISC ON AFT SIDE OF THE DISC PACK CRACKED IN HALF. INSTALLED DISC PACK S/N RNFS-2938, FOUND AT AIR LOGISTICS LLC, H OUMA BASE. 1 G 7 1 3U O H2SW 1999092400232 19990924 00232 CE 1999 9 24 99ZZZX3537 1 19990902 A 2120 UNKNOWN LEAR 35 35A 5170602 CE COCKPIT SMOKE A BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 700SJ 082 MKC - AFTER TAKEOFF, GOT SMOKE IN CABIN. RETURNED TO MKC. MAINTENANCE COULD NOT FIND ANY PROBLEMS, TEST FLEW AIRCRAFT HAD NO PROBLEMS. SUSPECT AUXILIARY CABIN HEATER MIGHT HAVE BEEN ON. 2 L 7 2 4F A10CE 1999092400233 19990924 00233 NM 1999 9 24 99ZZZX3538 1 19990819 A 3234 CABLES BOEING 727 727276 138408R NM MLG LEVER MISINSTALLED A S84A O OTHER O OTHER NR NOT REPORTED 1 EA 21 908PG 20951 CANCUN - FLT 301 - GEAR LEVER WILL NOT MOVE TO UP POSITION, USED OVERRIDE TRIGGER TO RAISE GEAR UP. FOUND NOSE GEAR SAF ETY SWITCH CABLES IN WRONG POSITION, RE-POSITIONED CABLES CORRECTLY, ADJUSTED, OPS CHECK AND INSPECTED IAW 32-09-221. 2 L 7 3 4F RT A3WE 1999092400234 19990924 00234 NM 1999 9 24 99ZZZX3539 1 19990827 A 2120 2075621 DUCT BOEING 727 727276 138408R NM RT PACK OVERHEAT A S84A O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 21 908PG 20951 JFK - FLT 301 - AIRCRAFT HAS SMOKE IN CABIN DUE TO DUCT OVERHEAT IN RIGHT PACK. DEFERRED PER MEL 21-5, PLACARD INSTALLE D. BREAKER COLLARED, DDPG 21-5 C/W. TRANSFERRED TO DMI SHEET. NOTE: RIGHT PACK COOLING FAN BURNED OUT, TO BE REPLACE D 8-27-99 AT JFK. 2 L 7 3 4F RT A3WE 1999092400235 19990924 00235 NM 1999 9 24 99ZZZX3540 1 19990829 A 2710 BCREF0400 CONTROL CABLE BOEING 727 727276 138408R NM RT AILERON FAILED A S84A K NONE O OTHER IN INSP/MAINT 1 EA 21 908PG 20951 JFK - FLT 301 - RIGHT INBOARD AILERON CABLE BROKEN, FOUND ON TRANSIT CHECK. REMOVED AND REPLACED CABLE ASSY IAW 27-10-0 . 2 L 7 3 4F RT A3WE 1999092400236 19990924 00236 NM 1999 9 24 SWAA991548 1 19990916 A 5320 6516307 STIFFNER BOEING 737 7372T4 1384492 NM BS 235 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CORRODED STIFFENER CHORD, BS 235, RBL 9, WL 182. REMOVED AND REPLACED CHORD SECTION PER SRM. 2 L 7 2 4F A16WE 1999092400237 19990924 00237 NM 1999 9 24 SWAA991549 1 19990916 A 5315 6546529 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND BS 520 FLOORBEAM CRACKED AT 2 EACH PLACES, LBL 45 AND RBL 45. REPAIRED FLOORBEAM PER SR M. 2 L 7 2 4F A16WE 1999092400238 19990924 00238 NM 1999 9 24 SWAA991550 1 19990916 A 5330 6550570 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUT OUT CRACKED. REPAIRED PER DALFORT XEA X2-52-28. 2 L 7 2 4F A16WE 1999092400239 19990924 00239 NM 1999 9 24 SWAA991551 1 19990916 A 3350 079123 COVER BOEING 737 7373H4 1384600 NM ROW 14 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 616SW 27699 EEPLS TRACK COVER LOOSE AT ROW 14. REINSTALLED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999092400240 19990924 00240 NM 1999 9 24 SWAA991552 1 19990916 A 3240 65447314 VALVE BOEING 737 7372T4 1384492 NM LT MLG INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 LT BRAKE OCCASIONALLY RELEASES DURING BRAKING ACTION BELOW 50 KNOTS. REMOVED AND REPLACED LT GEAR BRAKE AUGMENTATION VA LVE PER MM. 2 L 7 2 4F A16WE 1999092400241 19990924 00241 NM 1999 9 24 SWAA991536 1 19990914 A 5753 6937232 FITTING BOEING 737 7373H4 1384600 NM RT TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND CORROSION ON RT WING NR 8 T/E AFT FLAP TRACK ATTACH FITTING. REMOVED AND REPLACED NR 8 AFT FLAP TRACK ATTACH FITTING PER SRM. 2 L 7 2 4F RT A16WE 1999092400242 19990924 00242 NM 1999 9 24 SWAA991537 1 19990914 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED 1/2D CHECK, FOUND INTERIOR AND EXTERIOR OVERWING EXIT LIGHTS ILLUMINATED WHEN POWER IS TURNED OFF. REM OVED AND REPLACED LT AND RT BATTERY ASSY'S. 2 L 7 2 4F RT A16WE 1999092400243 19990924 00243 NM 1999 9 24 SWAA991538 1 19990914 A 3350 20121 BATTERY CHARGER BOEING 737 7373A4 1384585 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED A2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999092400244 19990924 00244 NM 1999 9 24 SWAA991539 1 19990915 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED RON, FOUND 4 EACH CRACKS ON FUSELAGE SKIN, BS 500A +4, AND BS 500C +6, STRINGER 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999092400245 19990924 00245 NM 1999 9 24 SWAA991540 1 19990915 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM RT LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED AT 3 EACH PLACES. REMOVED AND REPLACED L/E SL AT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999092400246 19990924 00246 NM 1999 9 24 SWAA991541 1 19990915 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED BC2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR ATTACH BRACKETS LOOSE. TIGHTENED HOLDING B RACKETS PER MM. 2 L 7 2 4F RT A16WE 1999092400247 19990924 00247 NM 1999 9 24 SWAA991542 1 19990915 A 5312 6546568 BULKHEAD BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND BS 1016 PRESSURE BULKHEAD CORRODED, LBL 7, WL 192. REPAIRED BULKHEAD PER BS 737-53A1075 AND DRAWING 65C28106. 2 L 7 2 4F A16WE 1999092400248 19990924 00248 NM 1999 9 24 SWAA991543 1 19990915 A 5312 6545409 BULKHEAD WEB BOEING 737 7372T4 1384492 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND BS 663 PRESSURE WEB CRACKED, RBL 39, WL 203. REPAIRED WEB PER ER NR 99-5890. 2 L 7 2 4F A16WE 1999092400249 19990924 00249 NM 1999 9 24 SWAA991544 1 19990915 A 5743 6582770 BEAM BOEING 737 7372T4 1384492 NM LH MLG CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CORROSION ON LT MAIN LANDING GEAR BEAM ATTACH FITTING, FWD OUTBOARD HOLE. REPAIRED BEAM PER ER NR 99-5782. 2 L 7 2 4F A16WE 1999092400250 19990924 00250 NM 1999 9 24 SWAA991533 1 19990914 A 3350 6104781 BATTERY ASSY BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED RON, FOUND EEPLS FWD SECTION INOP. REMOVED AND REPLACED BATTERY ASSY PER MM. 2 L 7 2 4F RT A16WE 1999092400251 19990924 00251 NM 1999 9 24 SWAA991534 1 19990914 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 523SW 26565 EEPLS LOOSE AT MID CABIN. REPOSITIONED WIRES AND REINSTALLED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999092400252 19990924 00252 NM 1999 9 24 SWAA991535 1 19990914 A 5330 6545772 SKIN BOEING 737 7372H4 138448C NM BS 837 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED, BS 837, BETWEEN STRINGERS 9L -10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999092400253 19990924 00253 NM 1999 9 24 SWAA991545 1 19990915 A 5743 6582770 FITTING BOEING 737 7372T4 1384492 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND CRACKED RT MAIN LANDING GEAR BEAM ATTACH FITTING AT SECOND INBOARD HOLE. REPAIRED BEAM ASSY PER ER 99-5833. 2 L 7 2 4F A16WE 1999092400254 19990924 00254 NM 1999 9 24 SWAA991546 1 19990915 A 5311 6546546 FRAME BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SPECIAL VISIT, FOUND BS 727 FUSELAGE FRAME CRACKED AT STRINGER 4R. REPAIRED FRAME PER DALFORT XEA NR X 2-53-253. 2 L 7 2 4F A16WE 1999092400255 19990924 00255 NM 1999 9 24 SWAA991547 1 19990915 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313SW 23335 LOWER AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999092400256 19990924 00256 NM 1999 9 24 SWAA991529 1 19990913 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP 11L CRACKED, BS 706. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 1999092400257 19990924 00257 NM 1999 9 24 SWAA991530 1 19990913 A 3350 284A01061 LENS BOEING 737 7377H4 NM PAX DOORWAY CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 742SW 29278 DURING LINE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999092400258 19990924 00258 NM 1999 9 24 SWAA991531 1 19990914 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE FRAME CRACKED, BS 500, BETWEEN STRINGERS 20L-21L. REMOVED AND REPLACED F RAME SECTION PER SRM. 2 L 7 2 4F A16WE 1999092400259 19990924 00259 NM 1999 9 24 SWAA991532 1 19990914 A 3350 07912 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS LIGHT MISSING RED LENS AT MID CABIN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999092400260 19990924 00260 NM 1999 9 24 SWAA991522 1 19990912 A 2560 A170033 STRAPS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 EMERGENCY FLASHLIGHT STRAPS BROKEN. REMOVED AND REPLACED STRAPS PER MM. 2 L 7 2 4F RT A16WE 1999092400261 19990924 00261 NM 1999 9 24 SWAA991523 1 19990912 A 5330 65457734 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED RON, FOUND 2 EA CRACKS ON FUSELAGE SKIN, BS 827, STRINGER 22L AND BS 727C+ 4, STRINGER 14L. REPAIRED S KIN PER SRM. 2 L 7 2 4F A16WE 1999092400262 19990924 00262 NM 1999 9 24 SWAA991524 1 19990912 A 3350 300432 BATTERY PACK BOEING 737 7372T4 1384492 NM EXTERIOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOORS EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999092400263 19990924 00263 NM 1999 9 24 SWAA991525 1 19990913 A 2560 6567380 COVER BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 AFT ENTRY DOOR EVACUATION SLIDE PRESS GAUGE VIEW LENS CRACKED. REMOVED AND REPLACED SLIDE COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 1999092400264 19990924 00264 NM 1999 9 24 SWAA991526 1 19990913 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313SW 23335 FWD EEPLS LIGHT PULLED UP FROM TRACK. REINSTALLED FWD EEPLS LIGHT SECTION PER MM. 2 L 7 2 4F RT A16WE 1999092400265 19990924 00265 NM 1999 9 24 SWAA991527 1 19990913 A 3350 079123 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED RON, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING NEXT TO ROW 15. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999092400266 19990924 00266 NM 1999 9 24 SWAA991528 1 19990913 A 5320 65C10300 CASTING BOEING 737 7372H4 138448C NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND NLG ACTUATOR BEAM CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM. 2 L 7 2 4F A16WE 1999092400267 19990924 00267 NM 1999 9 24 SWAA991512 1 19990911 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM SERV DOORWAY MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 649SW 27719 DURING SCHEDULED SERVICE CK CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999092400268 19990924 00268 NM 1999 9 24 SWAA991513 1 19990910 A 3350 10114 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 1999092400269 19990924 00269 NM 1999 9 24 SWAA991514 1 19990910 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED 1/2D CHECK, FOUND BS 947.5 UPPER CHORD OF FLOORBEAM CORRODED, LBL 20.75. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999092400270 19990924 00270 NM 1999 9 24 SWAA991515 1 19990910 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT AT CEILING INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999092400271 19990924 00271 NM 1999 9 24 SWAA991516 1 19990911 A 5330 6545819 SKIN BOEING 737 7372H4 138448C NM NOSE W W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND NOSE WHEEL WELL LT CEILING SKIN CRACKED AT BOLT HOLE, AFT INBOARD CORNER REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999092400272 19990924 00272 NM 1999 9 24 SWAA991517 1 19990911 A 5320 AND101392 CHORD BOEING 737 7372H4 138448C NM NOSE W W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND NOSE WHEEL WELL VERTICAL SUPPORT CHORD ANGLE CRACKED, BS 260, LBL O TO 1.6, WL 208. RE PAIRED CHORD PER SWA RA NR 1-253-2161. 2 L 7 2 4F A16WE 1999092400273 19990924 00273 NM 1999 9 24 SWAA991518 1 19990909 A 3610 332A13055 DUCT BOEING 737 7373Y0 1384671 NM NR 1 ENGINE RUPTURED A SWAA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 664WN 23495 NR 1 ENG EGT IND 80 DEGREES HIGHER THAN NR 2 ENG, ALSO SLOW TO ACCELERATE. FOUND 9TH STG DUCT RUPTURED ON ENG. REMOVED AND RELACED 9TH STG DUCT. 2 L 7 2 4F RT A16WE 1999092400274 19990924 00274 NM 1999 9 24 SWAA991519 1 19990910 A 2170 1808494 COALESCER BAG BOEING 737 7373H4 1384600 NM AC BAY DIRTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 620SW 28036 OILY ACRID SULFUR SMELL IN THE CABIN DURING FLIGHT. REMOVED AND REPLACED RT A/C WATER SEPARATOR COALESCER BAG PER MM. O PERATED SYSTEM, ODOR WENT AWAY. 2 L 7 2 4F RT A16WE 1999092400275 19990924 00275 NM 1999 9 24 SWAA991520 1 19990912 A 7722 WL202EED6 EGT INDICATOR BOEING 737 7373H4 1384600 NM NR 2 ENGINE INOP A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 365SW 26576 AIR TURNBACK, DURING FLIGHT, NR 2 ENG EGT INDICATOR INOP. REMOVED AND REPLACED NR 2 ENG EGT INDICATOR PER MM. 2 L 7 2 4F RT A16WE 1999092400276 19990924 00276 NM 1999 9 24 SWAA991509 1 19990911 A 5311 141A880 FRAME BOEING 737 7375H4 138449D NM FWD FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED 1/4D CHECK, FOUND THROUGH HFEC INSPECTION CRACKED L-1 COCKPIT WINDOW FRAME, UPPER OUTBOARD CORNER. REP AIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999092400277 19990924 00277 NM 1999 9 24 SWAA991510 1 19990911 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM RT HORZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED BC1 CHECK, FOUND RT HORIZONTALSTABILIZER LOWER SKIN CRACKED FWD OF 1ST BALANCE PANEL ALONG REAR SPAR. R EPAIRED SKIN PER SWA RA NR 1-555-0313. 2 L 7 2 4F RT A16WE 1999092400278 19990924 00278 NM 1999 9 24 SWAA991511 1 19990911 A 3350 20121 BATTERY PACK BOEING 737 7375H4 138449D NM LT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED BC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999092400279 19990924 00279 NM 1999 9 24 SWAA991521 1 19990912 A 2612 V25693 FIRE LOOP BOEING 737 7373H4 1384600 NM NR 1 ENGINE OUT OF POSITION A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 325SW 23689 ABORTED TAKEOFF, NR 1 ENG OVERHEAT MASTER CAUTION ILLUMINATED DURING TAKEOFF AT APPROX 50 KNOTS. REPOSITIONED NR 1 ENG FIRE DETECTION LOOP AT 6 O'CLOCK POSITION PER MM. OPS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 1999092400280 19990924 00280 WP 1999 9 24 TWAA9912701 1 19990916 A 5320 JAMB DOUG DC9 DC933F 302207A WP PAX DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 DURING CHECK-C MAINT, THE FWD UPPER CORNER OF THE LEFT FORWARD CABIN DOOR OPENING HAD ONE INCH CRACK IN THE INNER SKIN A ND TITANIUM DOUBLER. REPAIRED CRACK PER SRM 53-05, FIG 25A AND EMLR 69463. 2 L 7 2 4F A6WE 1999092400281 19990924 00281 WP 1999 9 24 IXXA9900023 1 19990916 A 3310 BA170MOD BALLAST DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 823BX 80196 2862 46064 EN ROUTE FROM JFK TO TOL, AN ODOR WAS SENSED IN THE COCKPIT WHEN THE GLAIR SHIELD LIGHTING WAS ILLUMINATED. THE CREW TU RNED THE LIGHTS OFF AND THE ODOR SUBSIDED. MAINTENANCE INSPECTED THE LIGHTING SYSTEM, WHICH REVEALED A DEFECTIVE LIGHT BALLAST. MAINTENANCE REPLACED THE BALLAST AND PER A SUCCESSFUL OPERATIONAL TEST. THE AIRCRAFT WAS RETURNED TO SERVICE . 2 L 7 4 4F RT 4A25 1999092400282 19990924 00282 NM 1999 9 24 AWXA9900315 1 19990914 A 3350 20121 CHARGER BOEING 737 73733A 1384673 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 VARIOUS EMERGENCY EXIT SIGNS INOP. FOUND SHORTED WIRE FOR TWO ASSY'S. REPAIRED WIRE AND REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A16WE 1999092400283 19990924 00283 EU 1999 9 24 AWXA9900316 1 19990914 A 4920 38002784 APU AIRBUS 320 A320231 3930325 EU APU DIRTY A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 28 644AW 13968 750 317 STRONG ODOR IN CABIN WHILE RUNNING PACK ON APU. WASHED APU PER CARD Z6D49301 MEL CLEARED. 2 L 7 2 4F RT A28NM 1999092400284 19990924 00284 1999 9 24 AWXA9900317 4 19990915 A 2210 4030952 YAW COUPLER BOEING 737 7373S3 1384711 NM AUTO PILOT FAILED A AWXA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 WP 28 312AW 40038 2664 24060 LATERAL SIDE MOTION WAS NOTICED IN AIRFRAME NO CHANGE WITH AUTO PILOT, PMCS, AND YAW DAMPNER OFF. REMOVED AND REPLACED YAW DAMPNER COUPLER, MEL CLEARED. 2 L 7 2 4F RT A16WE 1999092400285 19990924 00285 NM 1999 9 24 AWXA9900318 1 19990915 A 3350 849029 BATTERY PACK BOEING 737 73733A 1384673 NM ROW 17 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 172AW 23631 EMERGENCY PATH LIGHTING INOP AT ROW 17 AFT TO L2 AND R2. REMOVED AND REPLACED BATTERY PACK. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999092400286 19990924 00286 NM 1999 9 24 AWXA9900319 1 19990916 A 3350 1013101 BATTERY BOEING 737 737112 1384412 NM L2 DOORWAY DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 L2 EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F A16WE 1999092400287 19990924 00287 WP 1999 9 24 CALA9901201 1 19990912 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 875 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND 3 CRACKS IN CENTER WING TO BODY FAIRING SUPPORT ANGLES(3) AT STA 875, BL 0. THE ANGLES WERE REMOVED AN D NEW ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-30-4, AND 51-30-5. 2 L 7 2 4F A6WE 1999092400288 19990924 00288 WP 1999 9 24 CALA9901202 1 19990912 A 5330 PANEL DOUG DC9 DC982 3022082 WP BS 864-870 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND KEEL ACCESS PANEL BETWEEN BOTH MLG DOORS CORRODED ON ONE END AT FS 864-870. A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-00-60. 2 L 7 2 4F A6WE 1999092400289 19990924 00289 WP 1999 9 24 CALA9901203 1 19990912 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP BS 484-503 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND LOWER FUSELAGE EXTERNAL CUTOUT FOR NR 2 AD ANTENNA CORRODED BETWEEN SKIN AND INTERNAL DOUBLER AND MATIN G SURFACE AT FS 484-503, LONGERON 29L AND 30. THE INTERNAL DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5 . 2 L 7 2 4F A6WE 1999092400290 19990924 00290 WP 1999 9 24 CALA9901204 1 19990912 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 140 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 140, LONGERON 19R. REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 22, VIEW I. 2 L 7 2 4F A6WE 1999092400291 19990924 00291 NM 1999 9 24 CALA9901205 1 19990912 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, LBL 2-17. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1999092400292 19990924 00292 WP 1999 9 24 CALA9901206 1 19990909 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS294 & 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, BL 0 TO RBL 50 AND STA 328, BL 0 TO RBL 50. NEW FLOORBEAM SECTIONS WERE INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F A6WE 1999092400293 19990924 00293 NM 1999 9 24 CALA9901207 1 19990911 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 50 TO RBL 12. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A N EW SECTION WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999092400294 19990924 00294 NM 1999 9 24 CALA9901208 1 19990912 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 & 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 8 TO LBL 36 AND STA 986, RBL 15 TO LBL 40. THE CORRODED SECTIONS OF FLOORBEAM WERE REMOVED AND REPLACED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1999092400295 19990924 00295 WP 1999 9 24 CALA9901209 1 19990914 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND AFT CARGO DOOR GOUGED ON PAN AROUND DOOR STOPS. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-03, 51-10-4, 52-03, FIGURE 8 AND EA 5233-2-A0495. 2 L 7 2 4F A6WE 1999092400296 19990924 00296 WP 1999 9 24 CALA9901210 1 19990914 A 5754 SKIN DOUG DC9 DC982 3022082 WP LT LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INPECTION FOUND LEFT WING 0 SLAT DENTED. THE SLAT WAS REPAIRED IAW ECRA 5720-01120. 2 L 7 2 4F A6WE 1999092400297 19990924 00297 WP 1999 9 24 CALA9901211 1 19990914 A 5320 TIE STRAP DOUG DC9 DC982 3022082 WP BS 1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND TIE STRAP CORRODED AT LEFT AFT SERVICE DOOR CUTOUT, FS 1136, LONGERON 27R. THE TIE STRAP WAS REMOVED A ND A NEW TIE STRAP WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4. 2 L 7 2 4F A6WE 1999092400298 19990924 00298 WP 1999 9 24 CALA9901212 1 19990914 A 5512 PANEL DOUG DC9 DC982 3022082 WP RT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 1.5 CRACK IN RT HORIZONTAL STABILIZER PANEL NR 3804 L/E. THE CRACKED AREA WAS REMOVED AND A REPAIR W AS INSTALLED IAW SRM 51-30-2, 55-01, 51-30-2, 55-01, FIGURE 4, AND 55-12. 2 L 7 2 4F A6WE 1999092400299 19990924 00299 WP 1999 9 24 CALA9901213 1 19990914 A 5754 SLAT DOUG DC9 DC982 3022082 WP RT LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND RT WING 0 SLAT DENTED. REPAIRED SLAT IAW ECRA 5720-01170. 2 L 7 2 4F A6WE 1999092400300 19990924 00300 WP 1999 9 24 CALA9901214 1 19990914 A 5280 DOUBLER DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A .75 INCH CRACK IN LT MLG DOOR LOWER LT CORNER DOUBLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28. 2 L 7 2 4F A6WE 1999092400301 19990924 00301 WP 1999 9 24 CALA9901215 1 19990914 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1007 BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND AFT PIT FORWARD BULKHEAD CENTER VERTICAL SUPPORT BENT AT FS 1007, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-10-4, 51-10-2, 51-30-2, 51-30-5, AND 51-10-3. 2 L 7 2 4F A6WE 1999092400302 19990924 00302 WP 1999 9 24 CALA9901216 1 19990914 A 5730 PANEL DOUG DC9 DC982 3022082 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 3 INCH CRACK IN RT WING TRAILING EDGE PANEL NR 1610. THE PANEL WAS REPAIRED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999092400303 19990924 00303 WP 1999 9 24 CALA9901217 1 19990914 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 210 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 210 BETWEEN LONGERON 18 AND 19L. THE DENTED AREA WAS REPAIRED IAW SRM 53-04 , FIGURE 25. 2 L 7 2 4F A6WE 1999092400304 19990924 00304 WP 1999 9 24 CALA9901218 1 19990914 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1100-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RT I/B SEAT TRACK CORRODED AT FS 1100-1130, RBL 22. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INS TALLED IAW SRM 53-05, FIGURE 4. 2 L 7 2 4F A6WE 1999092400305 19990924 00305 NM 1999 9 24 CALA9901219 1 19990915 A 5314 KEEL BEAM BOEING 727 727232 1384082 NM BS 801 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND KEEL BEAM WEB CORRODED AT STA 801, LT SIDE. THE CORRODED WEB AREA WAS REMOVED AND A NEW WEB WAS INSTAL LED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1999092400306 19990924 00306 NM 1999 9 24 CALA9901220 1 19990915 A 5322 SHEAR TIE BOEING 727 727232 1384082 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND SHEAR TIES CORRODED AT STA 990, S29R AND STA 1090, S29R. NEW SHEAR TIES WERE INSTALLED IAW SRM 53-10-4 , 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1999092400307 19990924 00307 NM 1999 9 24 CALA9901221 1 19990915 A 5311 FRAME BOEING 727 727232 1384082 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A 4 INCH CRACK IN FRAME AT STA 500, STRINGER 21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBL ER WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1999092400308 19990924 00308 NM 1999 9 24 CALA9901222 1 19990915 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 660-680 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND STRINGER S28R AND S27L CORRODED AT STA 660-680. THE CORRODED SECTION OF STRINGERS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW 51-30-2, 53-10-3, 51-30-1, 51-10-2, AND 51-10-6. 2 L 7 3 4F A3WE 1999092400309 19990924 00309 NM 1999 9 24 CALA9901223 1 19990915 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 750 & 850 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND KEEL BEAM ANGLES AT STA 750, RT SIDE AND STA 850, RBL 5 TO LBL 5 CORRODED. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999092400310 19990924 00310 NM 1999 9 24 CALA9901224 1 19990915 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 990-1010 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL BETWEEN STA 990 AND 1010 AT S24L. THE CRACK WAS STOP DRILLED AND A REPA IR DOUBLER WAS INSTALLED IAW SRM 51-10-1, 51-40-3, AND 51-30-2. 2 L 7 3 4F A3WE 1999092400311 19990924 00311 NM 1999 9 24 CALA9901225 1 19990915 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 759-824 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND THREE ANGLES CORRODED IN KEEL BEAM AREA FROM STA 759-824. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-4, 51-30-2, AND 51-10-1. 2 L 7 3 4F A3WE 1999092400312 19990924 00312 NM 1999 9 24 CALA9901226 1 19990915 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND SHEAR TIE CORRODED AT STA 1148, STRINGER 24R TO 27R. REPAIRED SHEAR TIE IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1999092400313 19990924 00313 NM 1999 9 24 CALA9901227 1 19990915 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND FRAME SHEAR TIES CORRODED AT STA 720B, STRINGER 28L-28R, STA 720C, S28L-28R, AND STA 720F, S25R-27R. T HE SHEAR TIES WERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-10-6, 53-10-4, 51-30-2. 2 L 7 3 4F A3WE 1999092400314 19990924 00314 NM 1999 9 24 CALA9901228 1 19990915 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 15. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-8 AND 51-30-2. 2 L 7 3 4F A3WE 1999092400315 19990924 00315 NM 1999 9 24 CALA9901229 1 19990915 A 5320 WEB BOEING 727 727232 1384082 NM BS 1142-1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND WEB SKIN CORRODED AT STA 1142-1148, STRINGER 26R TO 20R. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALL ED IAW SRM 51-30-2 AND 51-40-2. 2 L 7 3 4F A3WE 1999092400316 19990924 00316 NM 1999 9 24 CALA9901230 1 19990915 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND STRINGER 29R CORRODED AT STA 344. THE SKIN WAS CUT AND CORRODED STRINGER WAS REMOVED. A FILLER, DOUBL ER, AND STRINGER REPAIR WERE INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1999092400317 19990924 00317 NM 1999 9 24 CALA9901231 1 19990915 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND FRAME AND WEB CORRODED AT STA 1148 FROM STRINGER 27L-27R. THE WEB WAS REMOVED, REPAIRED, AND REINSTALL ED IAW SRM 51-10-6, 53-10-4, FIGURE 45, AND 51-30-2. THE FRAME WAS REPAIRED IAW SRM 53-10-4, FIGURE 15. 2 L 7 3 4F A3WE 1999092400318 19990924 00318 NM 1999 9 24 CALA9901232 1 19990915 A 5311 FRAME BOEING 727 727232 1384082 NM BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND FRAME CORRODED AT STA 580, STRINGER 26R-27R. THE CORRODED AREA WAS REMOVED IAW SRM 53-10-4 AND A REPAI R WAS INSTALLED IAW SRM 51-10-1 AND 53-10-4. 2 L 7 3 4F A3WE 1999092400319 19990924 00319 NM 1999 9 24 CALA9901233 1 19990915 A 5330 SKIN BOEING 737 7373T0 1384582 NM L2 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A .25 INCH CRACK IN SKIN AT L-2 DOOR CUTOUT LOWER HINGE AREA. REPAIRED IAW ECRA 5360-01026. 2 L 7 2 4F RT A16WE 1999092400320 19990924 00320 WP 1999 9 24 CALA9901234 1 19990915 A 5753 SPAR CAP DOUG DC9 DC982 3022082 WP LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND A 3.5 INCH CRACK IN LT WING FLAP TRAILING EDGE CAP JUST O/B OF FLEX JOINT ASSEMBLY. REPAIRED IAW SRM 5 7-03, FIGURE 9 AND MM 51-00-00. 2 L 7 2 4F A6WE 1999092400321 19990924 00321 WP 1999 9 24 CALA9901235 1 19990915 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229 BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND LT FUSELAGE SKIN BULGED AT STA 229 BETWEEN LONGERON 17L AND 18L. THE BULGED AREA OF SKIN WAS REMOVED. NEW SKIN WAS INSTALLED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1999092400322 19990924 00322 WP 1999 9 24 CALA9901236 1 19990915 A 5753 VANE DOUG DC9 DC932 3022066 WP CENTER TE FLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND THE RT FLAP I/B FIXED VANE AND LT FLAP CENTER FIXED VANE DEBONDED. THE FLAP VANES WERE REMOVED AND REP LACED IAW MM 27-51-3, PAGE 201. 2 L 7 2 4F A6WE 1999092400323 19990924 00323 WP 1999 9 24 CALA9901237 1 19990915 A 5730 PANEL DOUG DC9 DC932 3022066 WP RT WING DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND LOWER SURFACE OF RT WING UPPER TRAILING EDGE PANEL DEBONDED. THE PANEL WAS REMOVED AND REPLACED IAW SR M 51-30-2, FIGURE 4. 2 L 7 2 4F A6WE 1999092400324 19990924 00324 NM 1999 9 24 CALA9901238 1 19990915 A 5210 ANGLE BOEING 737 7373T0 1384582 NM L-1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND L-1 DOOR Z-ANGLE CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999092400325 19990924 00325 NM 1999 9 24 UPS99230626 1 19990915 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON FLOORBEAM LOWER SURFACE AROUND SEVERAL FASTENERS HOLES BS 480, WL 208, BL 0- LBL 45. BL ENDED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED FLOORBEAM UPPER CHORD FROM BL 0 - LBL 45, BS 480 PER SRM 53-10-8 F IG 5. 2 L 7 3 4F A3WE 1999092400326 19990924 00326 NM 1999 9 24 UPS99430633 1 19990917 A 5210 SKIN BOEING 747 747283B 1384867 NM PAX DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 SHEET METAL DAMAGE MAIN DOOR NR 3 ACCESS PANEL AND DOUBLER. 2 L 7 4 4F A20WE 1999092400327 19990924 00327 EU 1999 9 24 QXEA9901926 1 19990914 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 GEG - OVERHEAD EXIT ANNUNCIATOR ABOVE COAT CLOSET HAS INOPERATIVE LAMPS. REPLACED CIRCUIT BOARD. CHECKS GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999092400328 19990924 00328 EU 1999 9 24 QXEA9901927 1 19990914 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU ROW 8&9 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 PDX - EXIT SIGN AT ROW 8 AND 9 INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999092400329 19990924 00329 NM 1999 9 24 QXEA9901928 1 19990914 A 3350 61047811 BATTERY DHAV DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 365PH 3065 520 SEA - FORWARD AISLE EMERGENCY FLOOR LIGHTS ARE INOP. REPLACED BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999092400330 19990924 00330 EU 1999 9 24 QXEA9901759 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8305 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRA PH 3 AND SRM 51-11-01. 2 L 7 2 4F RT A20EU 1999092400331 19990924 00331 EU 1999 9 24 QXEA9901760 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8305 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRA PH 3 AND SRM 51-11-01. 2 L 7 2 4F RT A20EU 1999092400332 19990924 00332 EU 1999 9 24 QXEA9901761 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8305 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRA PH 3 AND SRM 51-11-01. 2 L 7 2 4F RT A20EU 1999092400333 19990924 00333 EU 1999 9 24 QXEA9901762 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400334 19990924 00334 EU 1999 9 24 QXEA9901763 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400335 19990924 00335 EU 1999 9 24 QXEA9901764 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400336 19990924 00336 EU 1999 9 24 QXEA9901765 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400337 19990924 00337 EU 1999 9 24 QXEA9901766 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400338 19990924 00338 EU 1999 9 24 QXEA9901767 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 8805 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400339 19990924 00339 EU 1999 9 24 QXEA9901768 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400340 19990924 00340 EU 1999 9 24 QXEA9901769 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400341 19990924 00341 EU 1999 9 24 QXEA9901770 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400342 19990924 00342 EU 1999 9 24 QXEA9901771 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400343 19990924 00343 EU 1999 9 24 QXEA9901772 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400344 19990924 00344 EU 1999 9 24 QXEA9901773 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400345 19990924 00345 EU 1999 9 24 QXEA9901774 1 19990822 A 5310 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-30-01. 2 L 7 2 4F RT A20EU 1999092400346 19990924 00346 EU 1999 9 24 QXEA9901775 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-30-01. 2 L 7 2 4F RT A20EU 1999092400347 19990924 00347 EU 1999 9 24 QXEA9901776 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400348 19990924 00348 EU 1999 9 24 QXEA9901777 1 19990823 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400349 19990924 00349 EU 1999 9 24 QXEA9901778 1 19990823 A 5310 FOKKER F28 F28MK4000 4990810 EU UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT R4QME 9305A AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400350 19990924 00350 EU 1999 9 24 QXEA9901779 1 19990823 A 5310 FOKKER F28 F28MK4000 4990810 EU UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400351 19990924 00351 EU 1999 9 24 QXEA9901780 1 19990820 A 5310 FOKKER F28 F28MK4000 4990810 EU UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 57. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400352 19990924 00352 EU 1999 9 24 QXEA9901781 1 19990827 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305A AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400353 19990924 00353 EU 1999 9 24 QXEA9901782 1 19990820 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305B AND STRINGER 57. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400354 19990924 00354 EU 1999 9 24 QXEA9901783 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305B AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400355 19990924 00355 NM 1999 9 24 99FDEA00389 1 19990916 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 CORROSION (C53-224-09) AT BS 1130, RBL 60-66, WL 208 BOTTOM SIDE OF UPPER CHORD OF FLOORBEAM. *S/D* REMOVED RADIUS FIL LER PER SRM 51-30-2. REMOVED CORROSION, ALODINED, PRIMED & REINSTALLED PER FED 51-30-2. 2 L 7 3 4F RT A3WE 1999092400356 19990924 00356 NM 1999 9 24 99FDEA00390 1 19990916 A 5320 65317731 CHORD BOEING 727 727233 138408A NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 CORROSION (C53-224-08) ON 1176 CHORD, LBL 52-58, WL 208. *S/D* REPAIRED CORROSION IAW FEDEX SRM 53-10-8. REPAIRED LAV SHEAR WEB IAW FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1999092400357 19990924 00357 NM 1999 9 24 99FDEA00391 1 19990916 A 5320 691487112 SHEAR TIE BOEING 727 727233 138408A NM BS 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 SHEAR TIE CRACKED AFT SIDE BS 700, RBL 5, WL 148. *S/D* REMOVED, FABBED, INSTALLED NEW SHEAR TIE IAW FEDEX SRM 51-30-2 & DRAWINGS 65-15938 & 69-14871. 2 L 7 3 4F RT A3WE 1999092400358 19990924 00358 NM 1999 9 24 99FDEA00392 1 19990916 A 5311 651766334 FRAME BOEING 727 727233 138408A NM BS 660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 NR 223 CORROSION (C53-113-01-1) ON FRAME BS 660, BBLO, WL 148. REPAIRED DAMAGED SHEAR TIE IAW FEDEX SRM 53-10-4. 2 L 7 3 4F RT A3WE 1999092400359 19990924 00359 NM 1999 9 24 99FDEA00393 1 19990916 A 5311 65561241 FRAME BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 CORROSION ON 950F FRAME WL 148, LBL 9. *S/D* REPAIR FRAME WITH SHEAR TIE IAW FEDEX SRM 53-10-4, 51-30-2. 2 L 7 3 4F RT A3WE 1999092400360 19990924 00360 WP 1999 9 24 ABXA9900715 1 19990915 A 3260 313 BULB DOUG DC8 DC863 302198A WP COCKPIT CORRODED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 820AX 46155 DID NOT GET RIGHT MAIN GEAR GREEN LIGHT WHEN GEAR HANDLE PLACED IN DOWN POSITION. RECYCLED GEAR, DID NOT CHANGE INDICAT ION. CONTACTS ON BULBS WERE CORRODED. REPLACED BOTH INDICATION BULBS. SYSTEM OPS CHECKED GOOD IAW DC8 MM. 2 L 7 4 4F 4A25 1999092400361 19990924 00361 WP 1999 9 24 ABXA9900716 1 19990915 A 3230 ACTUATOR DOUG DC8 DC863 302198A WP NLG OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 813AX 46136 NOSE LANDING GEAR FAILED UPLATCH CHECK AND FELL OUT OF THE WHEEL WELL. RECYCLED GEAR, NO HELP. PERFORMED ALTERNATE UPL ATCH CHECK AND GEAR REMAINED IN WHEEL WELL. CHECKED ALL NOSE LANDING GEAR COMPONENTS. NO DEFECTS NOTED. ADJUSTED NOSE LANDING GEAR RETRACT ACTUATOR IAW DC8 MM 32-22-2. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999092400362 19990924 00362 NE 1999 9 24 ABXA9900717 2 19990915 A 7321 71128726 FUEL CONTROL DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE MALFUNCTION A ABXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 GL 23 817AX 4845 45928 671384 NR 2 ENGINE FLAMED-OUT AT FL330, FUEL PRESSURE WENT TO ZERO. OIL PRESSURE LIGHT ILLUMINATED. SECURED ENGINE. OIL QUAN TITY WAS 3.2 GALLONS. OIL PRESSURE WAS 25 PSI. ENGINE MOTORED FOR APPROXIMATELY 2 HOURS AND 40 MINUTES. REPLACED NR 2 FUEL CONTROL IAW DC8 MM 73-20-00. TRIMMED ENGINE IAW DC8 MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1999092400363 19990924 00363 NM 1999 9 24 DL757992004 1 19990909 A 2120 AIR DIST 216201018 BOEING 757 757232 1384965 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 634DL 23615 SMOKE SMELL IN CABIN STARTED AT ROW 27 AND STARTED DRIFTING AFT IN CABIN. SMELL ONLY NO VISABLE SMOKE. REPLACED RECIRC FILTERS RT SIDE. LT RECIRC FILTERS FOUND CLEAN. INSP PSU'S AND CABIN LIGHTING COMPONENTS. INSP OVERHEAD BINS. RAN EN GS AND OPERATED PACKS PER PFHB NO ODORS OR VAPORS PRESENT. INSP BAG BINS REVEALED NOTHING. ALSO, INSP PAX BAGS CARRY O N AND IN BINS NO ODORS. THIS IS A DIVERSION W/EMERG UNITS CALLED. 2 L 7 2 4F RT A2NM 1999092400364 19990924 00364 1999 9 24 DL72S992007 2 19990909 A 7532 BLEED VALVE BOEING 727 727232 1384082 NM NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 517DA 21433 AFTER TAKEOFF, (NORMAL POWER) THE ENG 2 APU BLEED HIGH TEMP LIGHT ILLUMINATED. THE NR 2 THROTTLE WAS RETARDED AND THE L IGHT WENT OUT. DISCUSSED WITH ATL/MCC AND FLIGHT RETURNED TO SLC. LIGHT TESTED GOOD. REPLACED NR 2 ENG BLEED VALVE CB , CKS GOOD. 2 L 7 3 4F A3WE 1999092400365 19990924 00365 NM 1999 9 24 DL72S992008 1 19990910 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FOUND ON F1 LETTER CK, 1 INCH CRACK IN STRINGER 18A AT STA 940 IN THE UPPER AND LOWER RADIUS RT. REPAIRED PER MM 53-12- 0. 2 L 7 3 4F A3WE 1999092400366 19990924 00366 NM 1999 9 24 DL72S992009 1 19990910 A 5320 WEB BOEING 727 727232 1384082 NM BS 1290 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 .25 INCH CRACK ON LEFT VERT TORQUE BOX WEB LWR LIGHTING HOLE STA 1290. ROUTE OUT CRACK PER MM 53-11-0. 2 L 7 3 4F A3WE 1999092400367 19990924 00367 NM 1999 9 24 DL72S992010 1 19990910 A 5400 SKIN BOEING 727 727232 1384082 NM S DUCT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 .5 INCH CRACK ON DUCT HOUSING SKIN AT PANEL 9524 RT SIDE. REPAIR PER MM 54-30-0. 2 L 7 3 4F A3WE 1999092400368 19990924 00368 NM 1999 9 24 DL72S992011 1 19990910 A 5754 STIFFENER BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 L/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK O/B SIDE OF TRACK. REPAIR PER MM 57-20-21. 2 L 7 3 4F A3WE 1999092400369 19990924 00369 NM 1999 9 24 DL72S992012 1 19990910 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 2 INCH VISIBLE CRACK IN VERT SPAR STIFFENER I/B SIDE OF O/B TRACK NR 3 L/E SLAT. REPAIRED PER MM 57-20-21 P 813. 2 L 7 3 4F A3WE 1999092400370 19990924 00370 NM 1999 9 24 DL76G992013 1 19990910 A 2121 732591F FAN BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 169DZ 29689 CREW REPORTED SMOKE IN COCKPIT AND FWD CABIN AREA ALONG WITH AN EICAS MESSAGE FWD EQUIPMENT EXHAUST FAN. REPLACED FWD E Q EXHAUST FAN. 2 L 7 2 4F RT A1NM 1999092400371 19990924 00371 NM 1999 9 24 DL72W992014 1 19990909 A 5400 65312813 ANGLE BOEING 727 727247 138408F NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 0 DURING HUSH-KIT MOD, FOUND NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED OLD ANGLE WITH ONE OF NEW MFG. 2 L 7 3 4F A3WE 1999092400372 19990924 00372 WP 1999 9 24 DLL10992016 1 19990910 A 2120 AIR DIST LKHEED 1011 10113851 5265010 WP CABIN ODOR A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 720DA 193C1136 AFTER TAKEOFF ATL, A VERY NOXIOUS ODOR CAME FROM THE AIR CONDITIONING SYSTEM IT SET OFF THE AFT SMOKE DET IN AFT LAVS. O DOR REDUCED AND SEEMED SPENT AS A/C PRESSURIZED AND WE CLIMBED TO HIGHER ALT. RAN PACKS WITH ALL THREE ENGS AT T/O PWR NO DISCREPANCIES NOTED. 2 L 7 3 4F A23WE 1999092400373 19990924 00373 WP 1999 9 24 DLL10992021 1 19990910 A 5230 SEAL 1522480119 LKHEED 1011 10113851 5265010 WP C-1 CARGO DOOR MISSING A DALA O OTHER O OTHER CL CLIMB 1 SO 27 727DA 193C1167 LOUD NOISE (BANGING THUMPING) RIGHT SIDE B ZONE AREA. STARTED ABOUT FL300 IN CLIMB TO FL320. CONTINUED UNTIL DECENT TO FL 240, AND SPEED 300KTS. INSPECTION UPON INSP FOUND C-1 DOOR UPPER AFT SEAL MISSING. REPLACED CORNER SEAL PER M/M. 2 L 7 3 4F A23WE 1999092400374 19990924 00374 NM 1999 9 24 DL76G992022 1 19990912 A 3310 LIGHT CONTROL BDC5 BOEING 767 7673P6 1385105 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 155DL 25269 FIRST OFFICERS INSTRUMENT FLOOD LIGHT GAVE OFF STRONG BURNING ODOR. TURNED OFF SWITCH AND SMELL CEASED. FOUND FLOOD LI GHT CONTROL ON P7 PRODUCING BURNING SMELL. REPLACED DIMMER. 2 L 7 2 4F RT A1NM 1999092400375 19990924 00375 NM 1999 9 24 DL73K992023 1 19990911 A 3350 276005 FUSE BOEING 737 737232 1384475 NM ROW 10-18 BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 314DA 23086 E-PATH LIGHTS INOP ROW 10 TO 18. REPLACED FUSE IN PWR SUPPLY. 2 L 7 2 4F RT A16WE 1999092400376 19990924 00376 NM 1999 9 24 DL72L992025 1 19990912 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM RT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 513DA 24510 21315 RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK OPS CK OK. 2 L 7 3 4F A3WE 1999092400377 19990924 00377 NM 1999 9 24 DL72L992026 1 19990912 A 3350 BATTERY 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 513DA 72375 21315 32 OVERHEAD EXIT LIGHT INOP. REPLACED BATTERY OPS NOW OK. 2 L 7 3 4F A3WE 1999092400378 19990924 00378 NM 1999 9 24 DL72W992028 1 19990912 A 3350 900542 LIGHT BOEING 727 727247 138408F NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2814W 20870 OVERHEAD EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED LIGHT, CKS NML. 2 L 7 3 4F A3WE 1999092400379 19990924 00379 NM 1999 9 24 DL767992029 1 19990815 A 5320 146T20032 BLKHD CHORD BOEING 767 767232 1385132 NM BS 1065 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 THE PN 146T2003-2 CHORD WAS FOUND CORRODED ON THE AFT SIDE OF THE STA 1065 BULKHEAD AT A PRIMARY ATTACH FITTING AT STRIN GER 23R. THE CHORD WAS REPLACED PER DWG 146T2000; NO DAMAGE TO ATTACHING STRUCTURE WAS FOUND. 2 L 7 2 4F RT A1NM 1999092400380 19990924 00380 NM 1999 9 24 DL72L992030 1 19990913 A 5753 65192709 FLAP TRACK BOEING 727 727232 1384082 NM TE FLAPS CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 NR 5 FLAP TRACK, REF AD 90-07-05 AND AD 90-06-09, TYP CORROSION FOUND TO MLG BEAM AND SPOILER BEAM ATTACH PAD SURFACE AN D ATTACH BOLT HOLES. TYPICAL WEAR FOUND AT FWD TRACK ATTACH LUG FACES. ALL CORROSION AND WEAR WAS MACHINED. AUTHORIZE D REWORKED DIMENSIONS AND INSTALLATION OF SPLICE PLATE OVER MLG BEAM ATTACH HOLES. 2 L 7 3 4F A3WE 1999092400381 19990924 00381 NM 1999 9 24 DL72L992031 1 19990913 A 5753 65192702 FLAP TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 NR 4 FLAP TRACK, REF AD 90-07-05, 90-06-09, 91-09-03, 94-05-04, TYPICAL CORROSION FOUND TO MLG BEAM AND SPOILER BEAM ATT ACH PAD AND ATTACH HOLES. WEAR FOUND AT TRACK FWD ATTACH LUG FACES AND FWD MLG HINGE FITTING ATTACH HOLES. AUTHORIZED MACHINING TO OVERSIZED DIMENSIONS AND INSTL OF SPLICE PLATE REPAIR TO MLG BEAM AREA. 2 L 7 3 4F A3WE 1999092400382 19990924 00382 NM 1999 9 24 DL767992032 1 19990815 A 5320 140T011534 SPLICE BOEING 767 767232 1385132 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 STRINGER 32R SPLICE WAS FOUND CORRODED AT STA 434, SPLICE WAS REPLACED PER DWG 140T0110 AND SRM 53-00-3-2-202. 2 L 7 2 4F RT A1NM 1999092400383 19990924 00383 NM 1999 9 24 DL767992033 1 19990815 A 5320 140T011517 SPLICE BOEING 767 767232 1385132 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 STRINGER 33L SPLICE WAS FOUND CORRODED AT STA 434, SPLICE WAS REPLACED PER DWG 140T0110 AND SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999092400384 19990924 00384 NM 1999 9 24 DL767992034 1 19990815 A 5320 140T01154 SPLICE BOEING 767 767232 1385132 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 STRINGER 35L SPLICE WAS FOUND CORRODED AT STA 434 AND WAS REPLACED PER DWG 140T0110 AND SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999092400385 19990924 00385 NM 1999 9 24 DL767992035 1 19990815 A 5320 140T01154 SPLICE BOEING 767 767232 1385132 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 STRINGER 38L SPLICE WAS FOUND CORRODED AT STA. 434 AND WAS REPLACED PER DWG 140T0110 AND SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999092400386 19990924 00386 NM 1999 9 24 DL767992036 1 19990815 A 5320 140T01154 SPLICE BOEING 767 767232 1385132 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 STRINGER 39L SPLICE WAS FOUND CORRODED AT STA 434 AND WAS REPLACED PER DWG 140T0110 AND SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999092400387 19990924 00387 NM 1999 9 24 DL767992037 1 19990815 A 5320 140T01154 SPLICE BOEING 767 767232 1385132 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 STRINGER 37L SPLICE WAS FOUND CORRODED AT STA 434 AND WAS REPLACED PER DWG 140T0110 AND SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999092400388 19990924 00388 NM 1999 9 24 DL72E992039 1 19990428 A 5753 652163245A ANGLE BOEING 727 727247 138408F NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE LOWER AFT CLOSEOUT ANGLE WAS FOUND CRACKED 55 FROM IB END OF THE FLAP. THE ANGLE WAS REPAIR ED BY INSTALLING A DOUBLER PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999092400389 19990924 00389 NM 1999 9 24 DL72E992040 1 19990428 A 5754 652163245A ANGLE BOEING 727 727247 138408F NM LT TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 33 FROM IB END OF THE FLAP. THE ANGLE WAS REPAIR ED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER AND SECTION OF ANGLE. 2 L 7 3 4F A3WE 1999092400390 19990924 00390 NM 1999 9 24 DL72E992041 1 19990428 A 5753 652163245A ANGLE BOEING 727 727247 138408F NM NR 2 TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 FROM THE IB END OF THE FLAP. THE ANGLE WAS RE PAIRED PER MM 57-52-0, FIG 802 BY INSTALL A DOUBER AND SECTION OF ANGLE. 2 L 7 3 4F A3WE 1999092400391 19990924 00391 1999 9 24 DL76G992042 4 19990913 A 2330 1011590001 FAN BOEING 767 7673P6 1385105 NM CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 155DL 25269 ELECTRICAL ODOR APPARENTLY FROM ENTERTAINMENT SYSTEM. STOPPED WHEN UNIT TURNED OFF. REPLACED COOLING FAN. 2 L 7 2 4F RT A1NM 1999092400392 19990924 00392 NM 1999 9 24 DL72E992043 1 19990907 A 5720 ANGLE BOEING 727 727247 138408F NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 AT HMV, FOUND RT WING REAR SPAR LWR CHORD ANGLE IS CRACKED, O/B OF NR 5 FLAP TRACK. REMOVED CRACKED SECTION, FABRICATED NEW PER MM 57-55-0, AND INSTALLED. 2 L 7 3 4F A3WE 1999092400393 19990924 00393 NM 1999 9 24 DL76L992044 1 19990913 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM ROW 4B INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 LT SIDE BUSINESS CLASS EMERGENCY LIGHTS INOP. REPLACED CHARGER, OPS OK. FOUND SEAT 4AB LIGHTS INOP. REPAIRED WIRING H ARNESS OPS OK. 2 L 7 2 4F RT A1NM 1999092400394 19990924 00394 NM 1999 9 24 DL757992045 1 19990913 A 3350 LIGHT GE767 BOEING 757 757232 1384965 NM LT EMER EXIT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 686DA 27589 IR LT AFT EMERGECEY LIGHT OVER WING LIGHT INOP, RELAMPED. 2 L 7 2 4F RT A2NM 1999092400395 19990924 00395 NM 1999 9 24 DL757992046 1 19990913 A 3397 WIRE 0201875003 BOEING 757 757232 1384965 NM ROW 6C BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 686DA 27589 IR 6C EMER LIGHT INOP. REPLACED HARNESS. 2 L 7 2 4F RT A2NM 1999092400396 19990924 00396 NM 1999 9 24 DLM88992047 1 19990914 A 5330 5911406 SKIN DOUG MD88 MD88 3023688 NM BS 228 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 GROUND DAMAGE WAS DISCOVERED TO THE FUSELAGE SKIN AT FS 228 BETWEEN STRINGERS 17L AND 18L. THE DAMAGE WAS REPAIRED AT H MV PER ERA 333535-14. 2 L 7 2 4F RT A6WE 1999092400397 19990924 00397 NM 1999 9 24 DLM88992048 1 19990914 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM BS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 218 AND STRINGER 19L. THE DAMAGE WAS REPAIRED PER ERA 333534-14 AT HMV. 2 L 7 2 4F RT A6WE 1999092400398 19990924 00398 NM 1999 9 24 DL72E992049 1 19990914 A 5311 FRAME BOEING 727 727247 138408F NM BS 784 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 THE OVERWING EXIT FRAME AT FS 784 WAS FOUND CRACKED. THIS DAMAGE WAS REPAIRED AT HMV PER ERA 333610-14. 2 L 7 3 4F A3WE 1999092400399 19990924 00399 NM 1999 9 24 DL767992050 1 19990914 A 2750 MECHANISM BOEING 767 767232 1385132 NM TE FLAPS LACK OF LUBE A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 27 114DL 22226 IN FLT: LOWERED FLAPS TO 1 DEG AND RCVD L /E SLAT DISAGREE LIGHT. SELECT ALT, DID NOT HELP. WHILE LOWERING FLAPS ELECTR ICALLY, RCVD T/E FLAP DISAGREE LIGHT. FLAPS LOCKED AT 16 DEG. WHEN LOWERED ELECTRICALLY, L/E SLAT LIGHT WENT AWAY. T/ E FLAP LIGHT REMAINED. LUBED LE AND TE FLAPS, OPERATED SAME SEVERAL TIMES. ALL CKS GOOD. FSEU CKS NML. 2 L 7 2 4F RT A1NM 1999092400400 19990924 00400 NM 1999 9 24 DL757992052 1 19990914 A 2560 SWITCH BOEING 757 757232 1384965 NM EMER EXIT DOOR DIRTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 677DL 25982 EMERGENCY DOORS STATUS MSG APPEARED ON CLIMB-OUT, LT AND RT WING SLIDE MSG APPEARED INTERMITTENTLY, CONTINUED TO APPEAR UNTIL SHORT FINAL. OPENED DOORS, CLEANED PROX SWITCH SENSORS AND RESEATED DOORS ALL OPNS NORMAL. 2 L 7 2 4F RT A2NM 1999092400401 19990924 00401 NM 1999 9 24 DL72L992053 1 19990915 A 5720 STIFFNER BOEING 727 727232 1384082 NM LE WING SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND ON MV2 CK INBD AND OUTBD SPAR STIFFENERS CRACKED AT THE NUMBER 7 SLAT I/B TRACK ON THE FWD WING SPAR. REPAIRED PE R MM 57-20-21. 2 L 7 3 4F A3WE 1999092400402 19990924 00402 NM 1999 9 24 DL72L992054 1 19990915 A 5720 STIFFNER BOEING 727 727232 1384082 NM LE WING SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND ON MV2 CK, L/E WING SPAR STIFFENER CRACKED AT THE NUMBER 7 SLAT O/B TRACK O/B SIDE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999092400403 19990924 00403 NM 1999 9 24 DL72L992055 1 19990915 A 5754 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND ON MV2 CK, .375 INCH CRACK ON NR 2 L/E SLAT RIB O/B OF ACTUATOR ATTACH BOLT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999092400404 19990924 00404 NM 1999 9 24 DLM88992056 1 19990915 A 3350 LIGHT DOUG MD88 MD88 3023688 NM R1 DOOR BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 922DL 49646 LENS OF R1 DOOR EMERGENCY BROKEN. REPLACED LIGHT ASSY. OPS CKS NML. 2 L 7 2 4F RT A6WE 1999092400405 19990924 00405 NM 1999 9 24 DL72E992057 1 19990915 A 5330 65182175 SKIN BOEING 727 727247 138408F NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 THE FUSELAGE SKIN WAS FOUND CRACKED AT THE STRINGER 4L LAP JOINT FROM FS 360-481. THE DAMAGE WAS REPAIRED PER ERA 33359 9-14AD AT HMV. 2 L 7 3 4F A3WE 1999092400406 19990924 00406 NM 1999 9 24 DL733992058 1 19990915 A 5313 STRINGER BOEING 737 737347 1384647 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 A CRACK WAS FOUND IN THE WEB OF STRINGER 18A AT FS 727. THE DAMAGE WAS REPAIRED PER ERA 333598-14 AT MV. 2 L 7 2 4F RT A16WE 1999092400407 19990924 00407 NM 1999 9 24 DLM88992059 1 19990915 A 5311 591359577 FRAME DOUG MD88 MD88 3023688 NM BS 1418 MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 916DL 49591 THE FS 1418 FRAME WAS FOUND TO HAVE A DOUBLE DRILLED HOLE ATSTRINGER L1. THE DAMAGE WAS REPAIRED PER ERA 333514-14 AT H MV. 2 L 7 2 4F RT A6WE 1999092400408 19990924 00408 NM 1999 9 24 DL76S992060 1 19990908 A 5720 112T700312 FITTING BOEING 767 767332 1382001 NM RT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 RT WING, I/B UNDERWING SIDE LOAD FITTING WAS FOUND WITH CORROSION DAMAGE IN THE BORE. REPAIR PER ER/A 333555-14 REV A. 2 L 7 2 4F RT A1NM 1999092400409 19990924 00409 NM 1999 9 24 DL76S992061 1 19990909 A 5400 311T115117 FITTING BOEING 767 767332 1382001 NM NR 1 PYLON CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 I/B LUG OF THE NR 1 ENGINE PYLON MIDSPAR O/B FITTING FOUND WITH CORROSION AND WEAR DAMAGE. DAMAGE FOUND ON FACE OF LUG AND IN BORE, ERA 333570-14 REV A. 2 L 7 2 4F RT A1NM 1999092400410 19990924 00410 NM 1999 9 24 DLM88992063 1 19990915 A 2150 ACM DOUG MD88 MD88 3023688 NM LEFT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 919DE 53422 ELECTRICAL FUMES DETECTED IN CABIN AND COCKPIT AT FL 350, HAZE DISSIPATED IN COCKPIT WITHIN ONE MINUTE AND WITHIN FOUR M INUTES IN CABIN. FOUND LT ACM SEIZED. REPLACED SAME, RAN PACKS AND ENGS. ALL CK GOOD. 2 L 7 2 4F RT A6WE 1999092400411 19990924 00411 NM 1999 9 24 DL757992064 1 19990915 A 4920 331200 APU BOEING 757 757232 1384965 NM AFT FUSELAGE INOP A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 652DL 19333 24392 1072 USING APU BLEED AIR TO RUN AIRCONDITIONING PACKS, GOT SOME SMOKE FROM AREA OF APU. COCKPIT SMELLED AS IF AIR COND PACKS OVERHEATED. NO PROBLEMS IN FLT WITH PACKS. TROUBLESHOT, PLACED APU ON MCO PER MEL 49-11-01A. 2 L 7 2 4F RT A2NM 1999092400412 19990924 00412 NM 1999 9 24 DL72E992065 1 19990428 A 5753 652163246A ANGLE BOEING 727 727247 138408F NM NR 3 TE MIDFLAP MISREPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 56 FROM IB END. THE ANGLE WAS REPAIRED PER 727 M M 57-52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND A NEW SECTION OF ANGLE. 2 L 7 3 4F A3WE 1999092400413 19990924 00413 NM 1999 9 24 DL72E992066 1 19990428 A 5753 652163246A ANGLE BOEING 727 727247 138408F NM NR 3 TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 34 FROM IB END. THE ANGLE WAS REPAIRED PER MM 57 -52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND NEW SECTION OF ANGLE. 2 L 7 3 4F A3WE 1999092400414 19990924 00414 NM 1999 9 24 DL72E992067 1 19990428 A 5753 652163246A ANGLE BOEING 727 727247 138408F NM NR 3 TE MID FLAP MIS INSTALKLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND WITH FASTENERS MISSING. THE ANGLE WAS REPAIRED PER MM 57 -52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND NEW SECTION OF ANGLE. 2 L 7 3 4F A3WE 1999092400415 19990924 00415 1999 9 24 DL76L992068 2 19990914 A 7320 WIRE BOEING 767 767332 1382001 NM PW4060 NR 1&2 ENGINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 25985 DURING MTC SETUP INSPECTION OF NR 1 ENG S/N 724139 AND NR 2 ENG S/N 724142, FOUND EEC CONTROL WIRING CHAFFED THROUGH INS ULATION ONLY, AT CLAMPS LOCATED AT HYD PRESS LINE MOUNT POINT IN PYLONS UNDER PANELS 432FR AND 442FL. MADE APPROVED REP AIR PER BOEING WIRING STD. PRACTICE MANUAL. 2 L 7 2 4F RT A1NM 1999092400416 19990924 00416 NE 1999 9 24 DL76L992069 2 19990915 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 179DN 25144 DURING MTC SETUP INSPECTION OF NR 1 ENG S/N 727524 AND NR 2 ENG S/N 724314, FOUND EEC CONTROL WIRING CHAFFED THROUGH INS ULATION ONLY, AT CLAMPS LOCATED AT HYD PRESS LINE MOUNT POINT IN PYLONS UNDER PANELS 432FR AND 442FL. MADE APPROVED REP AIR PER BOEING WIRING STD. PRACTICE MANUAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999092400417 19990924 00417 1999 9 24 DL76L992070 2 19990915 A 7320 WIRE BOEING 767 767332 1382001 NM PW4060 LT PYLON CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 194DN 28451 WORKING MSU TO CK FOR DAMAGED/CHAFFING WIRING FOR THE LT/RT ENG EEC CONT WIRES. REFF PYLON ACCESS PNLS 432FR LT AND 442 FL FOR RT. FOUND 1 CHAFFED WIRE IN LT PYLON UNDER CLAMP OF SMALLER BUNDLE. REPAIRED PER BAC WIRING STD PRACTICE MANUAL 20-10-13 PG 8. 2 L 7 2 4F RT A1NM 1999092400418 19990924 00418 NM 1999 9 24 DLM88992071 1 19990914 A 5512 SKIN DOUG MD88 MD88 3023688 NM HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 THE UPPER, AFT SKIN PANEL OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED DURING AN INSPECTION BY EO 9-61905-3AD, (LT AND RT) THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333575-14AD. 2 L 7 2 4F RT A6WE 1999092400419 19990924 00419 NM 1999 9 24 DL733992072 1 19990916 A 5314 STRINGER BOEING 737 737347 1384647 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 STRINGER 18AR WAS FOUND CRACKED AT FS 727. THE DAMAGE WAS REPAIRED PER ERA 333593-14 AT HMV. 2 L 7 2 4F RT A16WE 1999092400420 19990924 00420 NM 1999 9 24 DL72E992073 1 19990916 A 5753 65192709 TRACK BOEING 727 727247 138408F NM TE FLAP CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 INB'D FLAP, NR 4 FLAP TRACK: TYPICAL CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND TYPICAL WEAR AT FWD ATTACH LUGS A ND SPACER BLOCK BOLT HOLES, REF AD 90-07-05 AND 90-06-09. AUTHORIZED MACHINING OF ALL CORROSION AND WEAR. SPLICE P LATE REPAIR INSTALLED OVER MLG BEAM ATTACH HOLES. 2 L 7 3 4F A3WE 1999092400421 19990924 00421 NM 1999 9 24 DL72E992074 1 19990916 A 5753 65192709 TRACK BOEING 727 727247 138408F NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 INB'D FLAP NR 5 FLAP TRACK, TYPICAL CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUGS, REF AD 90 -07-05 AND 90-06-09. AUTHORIZED MACHINING OF ALL CORRODED AND WORN SURFACES. SPLICE PLATE REPAIR INSTALLED OVER OVERSI ZED MLG BEAM ATTACH HOLES. 2 L 7 3 4F A3WE 1999092400422 19990924 00422 NE 1999 9 24 DL76P992075 2 19990915 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 14156 1706 25989 724692 SETUP TO INSPECT EEC WIRING HARNESSES RUNNING THROUGH ENGINE PYLONS FOR ANY CHAFFING OR DAMAGED WIRING. FOUND 3 WIRES C HAFFED IN NR 1 ENGINE PYLON WIRE HARNESS AND COMPLETED TEMPORARY REPAIR OF WIRES PER STANDARD WIRING PRACTICES 20 -10-13 PAR 2. 2 L 7 2 4F 4 F RT A1NM E24NE 1999092400423 19990924 00423 NE 1999 9 24 DL76L992076 2 19990915 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE LT&RT PYLON CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 SETUP TO INSPECT EEC WIRING HARNESSES RUNNING THROUGH ENGINE PYLONS FOR ANY CHAFFING OR DAMAGED WIRING. FOUND 6 WIRES O N LEFT ENGINE WIRE HARNESS AND 1 WIRE ON RIGHT ENGINE HARNESS. COMPLETED TEMPORARY REPAIR TO ALL 7 CHAFFED WIRES PER STANDARD WIRING PRACTICES MANUAL 20-10-13 PAR 2A. 2 L 7 2 4F 4 F RT A1NM E24NE 1999092400424 19990924 00424 NM 1999 9 24 DL72S992077 1 19990916 A 2751 10619261 INDICATOR BOEING 727 727232 1384082 NM TE FLAPS MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 516DA 21432 WHEN FLAPS WERE POSITIONED TO FLAPS 2, THE LEFT AND RIGHT OUTBOARD SHOWED SLIGHT ASYMMETRY (ABOUT 1 NEEDLE WIDTH) RAN CH ECKLIST AND LOWERED FLAPS WITH ALTERNATE FLAP SWITCHES. FLAPS LOWERED TO 30 ON BOTH OUTBOARD, BUT INBOARD NOW SHOWED A SLIGHT SPLIT(ABOUT 5). HOWEVER, THE NEEDLE EVENTUALLY VIBRATED (OR FLICKERED) TO NORMAL(30,30). REPLACED OUTBOARD FLA P INDICATOR. RAN FLAPS. INDICATION AND FLAPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1999092400425 19990924 00425 NE 1999 9 24 DL76L992078 2 19990916 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE PYLON CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 178DN 25143 MSU TO CHECK FOR DAMAGED/CHAFFING WIRING FOR LT/RT ENG EEC CONTROL WIRES. C/W PYLON WIRE INSPECTION OF CHAFFED WIRES, F OUND DAMAGE TO OUTER INSULATION REPAIRED CHAFFED INSULATION BOTH ENGS PER BOEING STD PRACTICE 20-10-13. 2 L 7 2 4F 4 F RT A1NM E24NE 1999092400426 19990924 00426 NM 1999 9 24 DL72S992079 1 19990916 A 7110 SKIN BOEING 727 727232 1384082 NM NR 2 ENG INLET CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 5 INCH CRACK NR 2 ENG INLET OUTER SKIN BELOW DOUBLER AT 3:00 POSITION. REPAIRED PER MM 54-30-0 P 801. 2 L 7 3 4F A3WE 1999092400427 19990924 00427 1999 9 24 DL72S992080 4 19990916 A 3442 ANTENNA 20871790501 BOEING 727 727232 1384082 NM FWD FUSELAGE FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 409DA 3269 21153 WEATHER RADAR INOP, RESET CB, LEFT IN STANDBY FOR 5 MIN. WORKED 10 MIN, THEN INOP AGAIN, REPEAT WRITE-UP. REPLACED RAD AR ANTENNA AND CONTROL PANEL. TRANSMITTED RADAR FOR 20 MIN. RADAR CKS OK. 2 L 7 3 4F A3WE 1999092400428 19990924 00428 NM 1999 9 24 DL72S992081 1 19990916 A 5754 STIFFENER BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 2 INCH CRACK IN VERTICAL SPAR STIFFENER NR 7 SLAT O/B TRACK I/B SIDE. REPLACED SPAR STIFFENER PER MM 57-20-21. 2 L 7 3 4F A3WE 1999092400429 19990924 00429 NM 1999 9 24 DL72S992082 1 19990916 A 3350 BATTERIES S106 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 518DA 21469 ON L/O, FOUND MID CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPERATION NOW NML. 2 L 7 3 4F A3WE 1999092400430 19990924 00430 1999 9 24 SWIA971554 4 19990909 A 2350 519011 REU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E&E COMPT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 295SW 120322 RADIO FAILURE, LOSS OF ABILITY TO TRANSMIT OR RECEIVE. RETURNED TO FAT. REPLACED REU. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400431 19990924 00431 SO 1999 9 24 SWIA971555 1 19990909 A 2930 FILTER LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE GREEN HYD SYS ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 199SW 120237 GREEN SYSTEM FILTER LIGHT ILLUMINATED AFTER DEPARTURE WHEN THE GEAR WAS BROUGHT UP. RETURNED TO SLC. REMOVED AND REPLA CED GREEN HYDRAULIC FILTERS. INSPECTED FILTERS WITH NO CONTAMINATION NOTED. LEAKS CHECKED GOOD IAW MM 29-10-06. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400432 19990924 00432 SO 1999 9 24 SWIA971556 1 19990909 A 2422 INVERTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 1&2 FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 236SW 120312 DUAL INVERTER FAILURE. RETURNED TO PSP. REMOVED AND REPLACED NUMBER 1 AND NUMBER 2 INVERTERS. OPS CHECKS GOOD AT THI S TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400433 19990924 00433 SO 1999 9 24 SWIA971557 1 19990909 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 229SW 120305 AFTER TAKEOFF IN CLIMB, RIGHT RUDDER LOCKED AND RESTRICTED IN FORWARD TRAVEL. RETURNED TO SAN. REPLACED BLUE HYDRAULIC SYSTEM RUDDER ACTUATOR PER MM 27-22-02. NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400434 19990924 00434 SO 1999 9 24 SWIA971558 1 19990909 A 7112 TQ PROB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 301YV 120301 LEFT TORQUE GAUGE INOP TO INTERMITTENT AT 13,000 MSL ON CLIMB-OUT. RETURNED TO SFO. REMOVED AND REPLACED LEFT TORQUE P ROBE SENSOR. RAN LEFT ENGINE THROUGH PARAMETERS. NO INTERMITTENT FLUCTUATION OR FAILURE. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400435 19990924 00435 SO 1999 9 24 SWIA971559 1 19990909 A 3260 WARNING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR ACTIVATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 188SW 120039 ON CLIMB-OUT THROUGH 23,000 FT, AURAL LANDING GEAR WARNING SOUNDED WITH ASSOCIATED LIGHT ON MAP AND REPEATED AURAL WARNI NGS. RETURNED TO SLC. CHECKED ALL LANDING GEAR WARNINGS AND FOUND ALL WORKING NORMAL. BOTH EEC'S WERE DEFERRED AND SU SPECT THAT UPPER POWER LEVER MICROSWITCH WAS BEING TRIGGERED. ALL CHECKS GOOD. UNABLE TO DUPLICATE DISCREPANCY. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400436 19990924 00436 SO 1999 9 24 SWIA971560 1 19990903 A 5210 DOOR EMB 120 EMB120RT SO PWA 118 PW118A NE PAX COMPT NOT SEALED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 250YV 120250 CABIN DOOR LEAKS LOUD SQUEAL AND UNABLE TO MAINTAIN PRESSURE. RETURNED TO SFO. APPLIED RTV TO UPPER FORWARD CORNER OF MAIN CABIN DOOR. PRESSURIZED AIRCRAFT TO 6 PSID AND NO SQUEAL NOTED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400437 19990924 00437 NM 1999 9 24 VNAA9909003 1 19990915 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 5-7 DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 436JS 8385 1339 3052 THE EMERGENCY FLOOR LIGHTING ADJACENT TO CABIN SEAT ROWS 5 THROUGH 7 WAS FOUND TO BE INOPERATIVE BY MAINTENANCE PERSONNE L. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK LOCATED AT POSITION 5LK IN ACCORDANCE WITH DORNI ER MAINTENANCE MANUAL 33-51-00. OPERATION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999092400465 19990924 00465 EA 1999 9 24 99ZZZX3568 1 19990816 A 5610 6003303025 WINDSHIELD CNDAIR CL600 CL6001A11 1900302 EA COCKPIT CRACKED A EXOA O OTHER O OTHER CR CRUISE 1 SO 17 63HJ 1079R 1021 PILOT'S WINDSHIELD CRACKED (OUTER LAYER ONLY) IN CRUISE FLIGHT. 2 L 7 2 4F RT A21EA 1999092400466 19990924 00466 CE 1999 9 24 99ZZZX3569 1 19990826 A 5540 50524327 HORN BEECH 99 B99 1154004 CE RUDDER CORRODED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA U127 BELLCRANK ASSY AT BASE OF RUDDER FOUND LOOSE TO RUDDER TUBE COLLAR ASSY. CORROSION DETERMINED TO BE PROBLEM ON HOLES OF THE BELLCRANK ASSY. BELLCRANK WAS REPLACED WITH SERVICEABLE UNIT. PERIODIC DISASSEMBLY, INSPECTION, AND LUBRICATION O F COMPONENTS WITH STEEL AND MAGNESIUM/ALUMINUM PARTS COMBINED COULD BE ACCOMPLISHED. 1 L 7 2 3T A14CE 1999092400467 19990924 00467 CE 1999 9 24 99ZZZX3570 1 19990825 A 3230 115380002 MOTOR PESCO BEECH 99 99 1154002 CE MLG FAILED A BEMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 125DP 535 U12 PILOT TOOK OFF AND TRIED TO RETRACT LANDING GEAR. CIRCUIT BREAKER TRIPPED FOR LANDING GEAR MOTOR. PILOT USED EMERGENCY BLOW-DOWN TO EXTEND THE GEAR TO THE DOWN AND LOCKED POSITION. PILOT LANDED SAFELY. THIS AIRCRAFT HAD PREVIOUSLY BEEN C ONVERTED FROM A MECHANICAL TO A HYDRAULIC GEAR SYSTEM BY AVIR DESIGN. ELECTRIC MOTOR WAS REMOVED AND DISASSEMBLED. THE GEAR AT THE DRIVE END OF THE ARMATURE WAS FOUND LOCKED UP. BEARING PN 77R14. BEARING WAS REPLACED AND GEAR RETRACTION TESTED NORMALLY. STC SA 4013WE. 1 L 7 2 3T A14CE 1999092400468 19990924 00468 CE 1999 9 24 99ZZZX3571 1 19990828 A 5520 115610010 HINGE 115610010275 BEECH 99 B99 1154004 CE ELEVATOR DAMAGED A A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA U127 INSPECTION REVEALED LEFT ELEVATOR MIDDLE HINGE HOLES WORN. REPLACED BOTH MIDDLE AND OUTBOARD HINGE WITH NEW HINGES. HI NGES POSSIBLY WORN DUE TO PIVOT BOLTS NOT PROPERLY TORQUED TO BUSHINGS BETWEEN HINGE PLATES. SUBMITTER STATED DURING IN SPECTION, BOLTS SHOULD BE CHECKED FOR SECURITY. 1 L 7 2 3T A14CE 1999092400470 19990924 00470 CE 1999 9 24 99ZZZX3573 1 19990907 A 3230 426EN98 SQUAT SWITCH LEAR 25 25D 5170514 CE LT MLG FAILED A MXIA O OTHER O OTHER NR NOT REPORTED 1 EA 21 800RF 281 THE LANDING GEAR RETRACTED, BUT WOULD NOT EXTEND WITH HYDRAULIC PRESSURE, ALTERNATE GEAR EXTENSION WAS USED AND THE GEAR EXTENDED. TROUBLESHOOTING REVEALED THE GEAR UP SOLENOID WAS RECEIVING 28 VOLTS WITH THE GEAR HANDLE IN THE DOWN POSITI ON. FOUND THE LEFT SQUAT SWITCH FAILED INTERNALLY ALLOWING 28 VOLTS FROM THE ANTI-SKID YSTEM AND THE LEFT BLEED AIR SYS TEM TO POWER THE GEAR UP SOLENOID. REPLACED THE SQUAT SWITCH AND FUNCTIONALLY TESTED THE LANDING GEAR SYSTEM. 2 L 7 2 4J A10CE 1999092400472 19990924 00472 EU 1999 9 24 99ZZZX3575 1 19990906 A 5320 SD3113413XB FITTING STBROS SD3 SD330 8100602 EU FUSELAGE CORRODED A AVSA K NONE O OTHER IN INSP/MAINT 1 WP 13 78NF 23749 SH3044 FOUND SOME CORROSION OF JACK POINT FITTING BETWEEN SPAR AND SPAR CAP ON LT STUB WING. CONSULTED WITH MANUFACTURER FOR P OSSIBLE TREATMENT OF REPLACEMENT. THEY RECOMMENDED CLEANING AND TREATMENT IF NOT MORE THAN 5 INCHES LONG. FITTING WAS REPLACED WITH NEW ONLY. OLD FITTING SENT WITH ENGINEER TO FACTORY. 2 H 7 2 4T A41EU 1999092400478 19990924 00478 WP 1999 9 24 TWAA9912801 1 19990913 A 3350 1315 LAMP DOUG DC9 DC983 3022083 WP ROW 33 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9306T 49567 THE AFT STAIR EMERGENCY LIGHT AND THE EGRESS LIGHT AT ROW 33 WERE INOPERATIVE. RELAMPED THE TWO AFT STAIR LIGHTS, AND R ECONNECTED THE EGRESS STRIP AT ROW 33. CHECK-C 3-12-99 STL. 2 L 7 2 4F RT A6WE 1999092400479 19990924 00479 WP 1999 9 24 TWAA9912802 1 19990917 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9406W 53126 THE CABIN EGRESS LIGHTS WERE INOPERATIVE ROWS 2 TO 5, AND DIM FROM ROWS 12 THRU 27. REPLACED THE LAMPS, (P/N 7732), AT ROWS 1 THRU 5, AND REPLACED THE MID CABIN BATTERIES, (P/N 408822-101), FOR THE DIM LIGHTS. CHECK-C 1-18-99. 2 L 7 2 4F RT A6WE 1999092400480 19990924 00480 WP 1999 9 24 TWAA9912803 1 19990917 A 3350 1315 BULB DOUG DC9 DC982 3022082 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 918TW 49367 THE AFT LEFT CABIN EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 6-4-99 STL. 2 L 7 2 4F A6WE 1999092400481 19990924 00481 NE 1999 9 24 TWAA9912804 2 19990919 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE BIRD STRIKE A TWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 CE 05 9405T 53141 1415 ON TAKEOFF JUST AFTER BECOMING AIRBORNE THE AIRCRAFT WAS STRUCK BY A FLOCK OF BIRDS. THE FLIGHT RETURNED TO ABQ. THERE WAS MINOR DAMAGE TO THE NOSE LANDING GEAR AREA, AND THE RT ENGINE HAD TWO FIRST STAGE COMPRESSOR BLADES WITH MINOR DAMA GE. THE ENGINE WAS BORESCOPED. CHECK-C 11-11-98 MCI. 2 L 7 2 4F 4 F RT A6WE E9NE 1999092400482 19990924 00482 NM 1999 9 24 HNAA9900128 1 19990920 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 467-488 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 STRINGER 31S FROM X488 - X467 HAS CORROSION AROUND RIVET HOLES. RIVETS CIRCLED IN RED NEED REMOVED AND CORROSION EVALUA TED. REMOVED RIVETS. SEVERAL AREAS OF CORROSION MEASURES FROM .003 - .022 DEEP. SPLICED STRINGER 31S IAW RD8-53-1834. 2 H 7 2 4T RT A13NM 1999092400483 19990924 00483 NM 1999 9 24 HNAA9900129 1 19990920 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 445-467 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 908HA 015 STRINGER 31S FROM X467 - X445 HAS CORROSION, MOSTLY AROUND RIVET HOLES. RIVETS CIRCLED IN RED NEED REMOVED FOR FURTHER EVALUATION. REMOVED RIVETS. SEVERAL AREAS OF CORROSION MEASURE FROM .003 - .012 DEEP. SPLICED STRINGER IAW RD8-53-183 4. 2 H 7 2 4T RT A13NM 1999092400484 19990924 00484 WP 1999 9 24 AT9900636 1 19990902 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FLOORBEAM LOWER ANGLE AT BS 965 LBL 42 TO RBL 42 CORRODED. FABRICATE D FLOORBEAM REPAIR DOUBLERS, TREATED, PRIMED, REINSTALLED CABLE PULLEY TOWERS, AND RIGGED HORIZONTAL STABILIZER CABLES I AW DC9 MM 27-40-0 PG 214-219 PARAGRAPH J, 53-05 PG 243 FIG 79 AND 51-10-3. 2 L 7 2 4F A6WE 1999092400485 19990924 00485 WP 1999 9 24 AT9900637 1 19990905 A 5754 9919305 RIB DOUG DC9 DC932 3022066 WP NR 3 LE SLAT GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND GOUGED ON THE LEADING EDGE NR 3 SLAT RIB AT XOS 288.193. BLEND OUT G OUGED AREA, TREAT, PRIMED, AND REFINISH IAW DC9 SRM 57-01-0 FIG 1, SHEET 3, 57-21-1 FIG 1, AND TIMCO EO NR 99-1238. 2 L 7 2 4F A6WE 1999092400486 19990924 00486 WP 1999 9 24 AT9900639 1 19990916 A 2842 MS29513232 O RING DOUG DC9 DC932 3022066 WP LT FUEL PROB DAMAGED A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 824AT 47278 ON TAKEOFF, NOTICED STRONG ODOR. FLIGHT ATTENDANT REPORTED FUMES AND SMOKE OR HAZE IN CABIN, AS ODOR DISSIPATED HAZE RE MAINED. FOUND CUT O-RING ON LEFT FUEL PROBE NR 2. REMOVED AND REPLACED O-RING PER MM 2800. LEAK CHECK OK. REMOVED AN D REPLACED BOTH COALESCER BAGS AS PRECAUTIONARY. 2 L 7 2 4F A6WE 1999092400487 19990924 00487 WP 1999 9 24 AT9900640 1 19990717 A 5320 PAN DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 866AT 47168 SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT SIDE AFT CARGO PIT DOOR CUT OUT CORRODED. REPAIRED THE AFT CARGO DOOR FUSELAGE CUT OUT PAN AFT CORNER BY REMOVING CORROSION AND FABRICATING AND INSTALLING REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-10-4, 51-10-2, 53-31-0 FIG. 8, 53-05 FIG 44, AND 51-30-1. 2 L 7 2 4F A6WE 1999092400489 19990924 00489 NM 1999 9 24 9903896624 1 19990915 A 2913 887673 PUMP BOEING 747 747251B 1384892 NM NR 4 ENGINE LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 624US 250 21706 DURING CRUISE, THE NR 4 HYDRAULIC SYSTEM QUANTITY DECREASED. AIRCRAFT DIVERTED TO ANC AND LANDED WITHOUT INCIDENT. REP LACED THE NR 4 ENGINE DRIVEN HYDRAULIC PUMP, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999092400490 19990924 00490 NE 1999 9 24 9903909911 2 19990916 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LEFT FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 961N 77019 1024 47405 657313 AFT LEFT LAVATORY SMOKE DETECTOR SOUNDED WITH PASSENGER REPORTING STRANGE ODOR IN BACK OF CABIN. FLIGHT WAS RETURNED TO BHM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HEAT EXCHANGERS. 2 L 7 2 4F 4 F A6WE E2EA 1999092400491 19990924 00491 WP 1999 9 24 9903911162 1 19990823 A 5315 FLOORBEAM DOUG DC10 DC1040 3023508 WP BS 1099 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING M-CHECK, FOUND CRACK IN FLOORBEAM AT FS 1099, LBL 58. REPAIRED PER EA 11-106300. 2 L 7 3 4F A22WE 1999092400492 19990924 00492 NM 1999 9 24 9903926743 1 19990728 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 2220 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING COMMISSIONING CHECK (XMN), FOUND CRACK ON FRAME AT FS 2220, STR 25R - 26R. REPAIRED PER EA 67-170253. 2 L 7 4 4F A20WE 1999092400493 19990924 00493 NM 1999 9 24 9903936743 1 19990723 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 1800 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING COMMISSIONING CHECK (XMN), FOUND CRACK IN MAIN DECK FRAME AT UPPER FLANGE CORNER FS 1800, STR 11R - 12R. REPAIRE D PER EA 67-170254. 2 L 7 4 4F A20WE 1999092400494 19990924 00494 NM 1999 9 24 9903946743 1 19990722 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 1700 DEFORMED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING COMMISSIONING CHECK (XMN), FOUND DEFORMATION ON MAIN DECK FRAME FS 1700, STR 12R - 13R. REPAIRED PER EA 67-17025 1. 2 L 7 4 4F A20WE 1999092400495 19990924 00495 NM 1999 9 24 9903956743 1 19990722 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 1680 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING COMMISSIONING CHECK (XMN), FOUND MAIN DECK FRAME UPPER FLANGE CRACKED FS 1680, STR 13R. REPAIRED PER EA 67-17024 9. 2 L 7 4 4F A20WE 1999092400496 19990924 00496 EA 1999 9 24 COMA9960527 1 19990914 A 3246 50105842 WHEEL 50105711 CNDAIR CL600 CL6002B19 EA MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 2933 OCT971556 7174 WHEEL WAS REMOVED FOR A BRAKE CHANGE. DURING CLEANING OF THE WHEEL SUB-ASSEMBLY A CRACK WAS DETECTED AT THE SPOKE IN TH E WHEEL. (TOTAL TIRE CHANGES 14). WHEEL HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR EVALUATION. 2 L 7 2 4F RT A21EA 1999092400497 19990924 00497 EA 1999 9 24 COMA9960528 1 19990916 A 2751 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 776CA 7293 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999092400498 19990924 00498 EA 1999 9 24 COMA9960529 1 19990916 A 2933 CONNECTOR CNDAIR CL600 CL6002B19 EA NR 1 HYD SYS LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 956CA 7105 NR 1 HYD SYSTEM QUANTITY INDICATOR IS INOP. TIGHTENED WIRING CONNECTOR FOR QUANTITY GAUGE. 2 L 7 2 4F RT A21EA 1999092400499 19990924 00499 EA 1999 9 24 COMA9960530 1 19990916 A 2710 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 EA COCKPIT INOP A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 983CA 7169 AILERON TRIM IS INOPERABLE. REPLACED TRIM PANEL. 2 L 7 2 4F RT A21EA 1999092400500 19990924 00500 EA 1999 9 24 COMA9960531 1 19990917 A 2910 AE7090052 HYD LINE CNDAIR CL600 CL6002B19 EA LT PYLON FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 986CA 7174 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED LEAKING HIGH PRESSURE LINE IN LEFT HAND PYLON. 2 L 7 2 4F RT A21EA 1999092400501 19990924 00501 NM 1999 9 24 UPS99230634 1 19990910 A 5720 STIFFNER BOEING 727 7271A7C 13840X2 NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C RW VERTICAL STIFFENER ON FWD WEB JUST O/B OF 740 BOTTLE PIN IS CRACKED AT BOTTOM FASTENER. REMOVED ST IFFENER, FABRICATED A NEW ONE, ALODINED AND PRIMED NEW STIFFENER. INSTALLED STIFFENER, ALL WORK ACCOMPLISHED IAW SRM 51 -30-05, BOEING DRAWING NR 69-20117-1, SRM 51-30-2. 2 L 7 3 4F A3WE 1999092400502 19990924 00502 NM 1999 9 24 UPS99230635 1 19990729 A 5531 SPAR BOEING 727 7271A7C 13840X2 NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, LT VERTICAL MID SPAR FRETTING WHERE PANEL 9601 ATTACHES AT AFT END. REPAIRED LT VERTICAL MID SPAR WI TH SPLICE REPAIR IAW ERN 99-5888. 2 L 7 3 4F A3WE 1999092400503 19990924 00503 NM 1999 9 24 UPS99230636 1 19990910 A 5531 SPAR BOEING 727 7271A7C 13840X2 NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, RT VERTICAL MID SPAR FRETTING WHERE PANEL 9602 ATTACHES AT AFT END. REPAIRED LT VERTICAL MID SPAR WI TH SPLICE REPAIR IAW ERN 99-5888. 2 L 7 3 4F A3WE 1999092400504 19990924 00504 NM 1999 9 24 UPS99230638 1 19990919 A 5711 SPAR BOEING 727 72731C 1384011 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE:N/A, LT WING AFT FALSE SPAR LWR. CAP CRACKED BELOW I/B GROUND SPOILER ACTUATOR SUPPORT BRACKET AT TERMI NATING END. DAMAGE APROX 1.25 INCHES IN LENGTH. *S/D* REPAIRED CRACK PER UPS EO B727-5750-11867-A, PARA 6A. CRACK ST OP DRILLED IAW SRM 51-10-1 D-178976 ASSIGNED TO CREATE MPI FOR INSPECTION. 2 L 7 3 4F A3WE 1999092400505 19990924 00505 NM 1999 9 24 UPS99230639 1 19990903 A 5330 SKIN BOEING 727 727185C 138406N NM BS 913 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, UPPER FUSELAGE SKIN HAS BULGE AND SKIN CRACKED AT BS 913 AND STR 4 LT. CUT OUT DAMAGED AREA, REMOVED CORROSION, INSTALLED DOUBLER REPAIR FROM STATION 810 TO 930 STRINGER 4 LT AS PER UPS EO B727-5330-0509 AND B727 SRM 53- 30-3 FIG 5. 2 L 7 3 4F A3WE 1999092400506 19990924 00506 NM 1999 9 24 UPS99230640 1 19990906 A 5753 651920918 FLAP TRACK BOEING 727 7272A1 138407F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, NR 5 FLAP TRACK IS CORRODED AT FWD ATTACH LUG AND AT SPOILER BEAM ATTACH POINT. REPLACED NR 5 FLAP TRACK. REMOVAL AND INSTALLATION ACCOMPLISHED ON TC NR C57-581-04-4A. 2 L 7 3 4F A3WE 1999092400507 19990924 00507 NM 1999 9 24 UPS99230641 1 19990910 A 5320 CHORD BOEING 727 7272A1 138407F NM BS 345-350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI WHILE WORKING CARD NR919297 DISCOVERED GOUGES AND CORROSION ON BS 345-350 RBL 20 WL 148 (DAMAGED RT N OSE GEAR DRAG BRACE SIDE CHORD). REMOVED AND REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999092400508 19990924 00508 NM 1999 9 24 UPS99230642 1 19990915 A 5720 BEAM BOEING 727 7272A1 138407F NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, LT MLG BEAM IS CORRODED AT NR 4 FLAP TRACK MOUNT BOLT HOLES. REMOVED CORROSION AND REPAIRED LG BEAM PER ER NR 99-6038. 2 L 7 3 4F A3WE 1999092400509 19990924 00509 NM 1999 9 24 UPS99230643 1 19990820 A 5713 STRINGER BOEING 727 7272A1 138407F NM WS 251-277.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, CORROSION (C57-571-01.02-02) RW FUEL CELL INTERIOR ON STR 4 AROUND SEVERAL FASTENERS BETWEEN WS 251. 0 AND WS 277.5. REPAIR WORK DONE PER ER 99-6010 FILE NR 727-57-2110. 2 L 7 3 4F A3WE 1999092400510 19990924 00510 NM 1999 9 24 UPS99230644 1 19990820 A 5713 STRINGER BOEING 727 7272A1 138407F NM WS 277.5-304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, CORROSION IN 3 AREAS R/W FUEL CELL INTERIOR, UPPER SURFACE OF LOWER SKIN BETWEEN WS 304 AND WS 277.5 STR 10-11. REMOVED CORROSION PER SRM 51-10-6, REPAIRED STRINGER 10 PER SRM 57-10-4 AND ER 99-6058. 2 L 7 3 4F A3WE 1999092400511 19990924 00511 NM 1999 9 24 UPS99230645 1 19990820 A 5713 STRINGER BOEING 727 7272A1 138407F NM WS 224.5-251 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 213UP 21341 INSPECTION TYPE:SI, CORROSION (C57-571-01.02-02) RW FUEL CELL INTERIOR AROUND FASTENERS ON STR 4 BETWEEN WS 224.5 AND WS 251.0. REPAIRED PER ER 99-6010 FILE NR 727-57-2110. 2 L 7 3 4F A3WE 1999092400512 19990924 00512 NM 1999 9 24 UPS99230646 1 19990903 A 5542 SKIN BOEING 727 727185C 138406N NM RUDDER DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE:C, LOWER RUDDER, RT SIDE, CORNER OF SKIN PANEL DEBONDED WITH CORROSION. INSTALLED FIBERGLASS REPAIR OVE RLAY AT LOWER RUDDER RT SIDE SD PER B727 SRM 51-40-8. 2 L 7 3 4F A3WE 1999092400513 19990924 00513 NM 1999 9 24 UPS99230647 1 19990918 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, FLOOR EMER LIGHTS OUT IN SEAT POS 13 & 15. REPLACED BATTERY PACKS IN POS 13 & 15. 2 L 7 3 4F A3WE 1999092400514 19990924 00514 NM 1999 9 24 UPS99230648 1 19990917 A 3350 BATTERY BOEING 727 72725C 138400H NM GALLEY DOORWAY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERG EXIT LIGHT OVER GALLEY DOOR DOES NOT ILLUMINATE. REPLACED BATT PACK, CKS OK. 2 L 7 3 4F A3WE 1999092400515 19990924 00515 NM 1999 9 24 UPS99230649 1 19990917 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMER LIGHT AT 17ABC INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999092400516 19990924 00516 1999 9 24 UPS99430630 4 19990916 A 3434 MARKER BEACON BOEING 747 747121 1384871 NM COCKPIT INOP A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE:N/A, MARKER BEACON INOP. 2 L 7 4 4F A20WE 1999092400517 19990924 00517 NM 1999 9 24 UPS99430637 1 19990919 A 2612 69B475193 DRIVER CARD BOEING 747 747123 1384873 NM FIRE WARN SYS DEFECTIVE A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 673UP 20325 INSPECTION TYPE:N/A, ON DEPARTURE CLIMBOUT INTERMITTENT FIRE WARNINGS BEGAN. ALL FIRE WARNING SYSTEMS FOR CARGO COMPTS TESTED GOOD. LWR AFT CARGO FIRE WARNING CONTINUED EMERGENCY RETURN WAS INITIATED AND TOUCHDOWN WAS MADE OVERWEIGHT AND VERY SMOOTH AT APPROX 165 KTS AND 685,000 LBS. RESCUE CREWS REPORTED NO EVIDENCE OF FIRE. REMOVED AND REPLACED A-7 DRI VER CARD LWR CARGO (P/N 69B47519-3), (S/N AA27) ON, (S/N 208) OFF. REMOVED AND REPLACED A-8 DRIVER CARD NR 4 ENG AS PRE CAUTION, (P/N 69B47519-3), (S/N FT2-7) ON, (S/N 267) OFF. OPERATIONAL CK OF FIRE WARINING SYSTEM ON LWR CARGO AND NR 4 ENG CKS GOOD PER MM 26-10-01. 2 L 7 4 4F A20WE 1999092400518 19990924 00518 NM 1999 9 24 99FDEA00376 1 19990909 A 5330 6556148 SKIN BOEING 727 727277 138408S NM BS 1070 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 245FE 22016 DENT ON EXTERNAL SKIN AT BS 1070, STR 19L. *S/D* REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1999092400519 19990924 00519 WP 1999 9 24 ABXA9900718 1 19990910 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 1056. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1999092400520 19990924 00520 WP 1999 9 24 ABXA9900719 1 19990910 A 5753 995760014 ANGLE DOUG DOUG DC9 DC941 302207N WP RTTE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999092400521 19990924 00521 WP 1999 9 24 ABXA9900720 1 19990910 A 5312 5910310392 BULKHEAD TEE DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD NR 2 TEE CAP CRACKED AT THIRD RADIAL. REPLACED NR 2 TEE CAP IAW ABX EA 531 -20033-001. 2 L 7 2 4F A6WE 1999092400522 19990924 00522 WP 1999 9 24 ABXA9900721 1 19990910 A 5330 9910073 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 80 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 DURING C-CHECK, FOUND RIVETS SHEARED DUE TO CORROSION AT BL 13 RIGHT AND STATION 80. REPAIRED IAW ABX REA D953-33205 MR AND DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999092400523 19990924 00523 WP 1999 9 24 ABXA9900722 1 19990910 A 5312 591016342 BLKHD RADIAL DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 937AX 47074 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD VERTICAL LEG OF RADIAL NR 14 RIGHT CRACKED. REPAIRED IAW ABX REA D953-3324 5 AND ABX DWG K05159. 2 L 7 2 4F A6WE 1999092400524 19990924 00524 NM 1999 9 24 MWEA99603 1 19990915 A 5241 59114024 SKIN DOUG MD88 MD88 3023688 NM GALLEY DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FORWARD GALLEY SERVICE DOOR, LOWER OUTBOARD SKIN AND HOLD-OPEN HOOK CUP FUSELAGE SKIN IS GOUGED. MTC FABRICATED AND INS TALLED REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 1999092400525 19990924 00525 WP 1999 9 24 MWEA99604 1 19990916 A 5230 59101415 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 FORWARD CARGO DOOR OUTER PAN IS CRACKED AND LOWER FORWARD AREA HAS A DENT. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999092400526 19990924 00526 WP 1999 9 24 MWEA99605 1 19990913 A 3350 6011779 BATTETY PACK DOUG DC9 DC914 3022034 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 500ME 45711 LEFT NACELLE LIGHT DID NOT PASS BURN TEST -- MTC R/R NACELLE LIGHT BATTERY PACK 2 L 7 2 4F A6WE 1999092400527 19990924 00527 WP 1999 9 24 MWEA99606 1 19990913 A 5520 59180432 SHROUD DOUG DC9 DC914 3022034 WP RT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT ELEVATOR INBOARD GEAR TAB PUSH ROD SHROUD IS CRACKED. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999092400528 19990924 00528 WP 1999 9 24 MWEA99607 1 19990913 A 2710 CONTROL CABLE DOUG DC9 DC932 3022066 WP LT AILERON FROZEN A MWEA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 206ME 47791 AILERONS VERY DIFFICULT TO MOVE DURING DESCENT, FEELS FROZEN. MTC FOUND ICE BUILD-UP IN LEFT WHEEL WELL FORWARD TOP OUT BOARD AILERON CABLE/PULLEY STACK. MTC REMOVED OBSTRUCTION AND CLEANED DRAIN. 2 L 7 2 4F A6WE 1999092400529 19990924 00529 WP 1999 9 24 MWEA99608 1 19990917 A 5241 593998825 FRAME DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 GALLEY DOOR NR 1 FRAME IS CRACKED IN RADIUS ON AFT END OF BEAM. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999092400530 19990924 00530 NM 1999 9 24 SCNA99119 1 19990910 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM RT EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECK, THE RIGHT FOWARD OVERWING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVE D AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD REF MM 335071. 2 L 7 3 4F A3WE 1999092400531 19990924 00531 NM 1999 9 24 SCNA99120 1 19990916 A 5230 DOORS BOEING 727 7272J4 1384006 NM CARGO COMPT LEAKING A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 285SC 21676 UNABLE TO CONTROL CABIN PRESSURE DURING CLIMB. STOPPED ASCENT THEN BEGAN DESCENT TO MAINTAIN CABIN ALTITUDE BELOW 10,00 0 FEET. CABIN CONTROLLER DIDN'T HAVE ANY EFFECT IN AUTO, STANDBY OR MANUAL MODES. AIRCRAFT DOORS WERE LEAK CHECKED AND FOUND OVERWING EMERGENCY EXITS AND FORWARD AND AFT CARGO DOORS LEAKING. ALSO, FOUND SUPPLY DUCT GASPER FAN DUCT LEAKIN G. CORRECTED ALL LEAKS AND PRESSURIZED AIRCRAFT. NO LEAKS NOTED AND AIRCRAFT TEST FLOWN TO OPERATIONALLY CHECK SYSTEM. 2 L 7 3 4F RT A3WE 1999092400532 19990924 00532 NM 1999 9 24 SCNA99724 1 19990912 A 5313 STRINGER BOEING 727 7272J4 1384006 NM BS 950 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING A HEAVY MAINTENANCE CHECK, OUT OF LIMITS CORROSION WAS FOUND IN THE AFT CARGO BILGE AREA AT STR 29L BETWEEN STA 9 50E AND 950F. REMOVED AND REPLACED DAMAGED CHORD WITH NEW CHORD IAW B727 SRM 51501. CUT ACCESS HOLE TO ACCESS S29L. F ABBED DOUBLER PER SRM 53303 AND INSTALLED ALL REPAIR PIECES PER B727 SRM 53303 AND 51404. 2 L 7 3 4F RT A3WE 1999092400533 19990924 00533 NM 1999 9 24 SCNA99725 1 19990912 A 5313 65198618 STRINGER BOEING 727 7272J4 1384006 NM BS 310 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING A HEAVY MAINTENANCE CHECK, OUT OF LIMITS CORROSION WAS FOUND IN THE LOWER NOSE COMPARTMENT INSIDE THE RIGHT NOSE LANDING GEAR WALKWAY AT STA 310 RBL 30 ON THE STRUCTURAL CHORD. REMOVED CORRODED CHORD AND REPLACED CHORD WITH A NEW CH ORD IAW B727 SRM 51511 AND 51302. 2 L 7 3 4F RT A3WE 1999092400534 19990924 00534 NM 1999 9 24 SCNA99600 1 19990902 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 760.95 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINTENANCE CHECK, A FLOORBEAM WAS FOUND CRACKED AT RBL 55 FS 760.95. FABRICATED, TREATED AND INSTALLED A REPAIR DOUBLER IAW B727 SRM 51402 AND 51201, 51302. 2 L 7 3 4F A3WE 1999092400535 19990924 00535 NM 1999 9 24 TC8A99025 1 19990918 A 2923 CONNECTOR BOEING 727 72721C 138400M NM NR 2 HYD PUMP WET A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 705A 19134 NR 2 B-PUMP C/B WILL NOT RESET. BMM 29-12-0, OPERATION OF B-PUMP. EXCESSIVE MOISTURE ON PUMP CONNECTION. 2 L 7 3 4F A3WE 1999092400536 19990924 00536 EU 1999 9 24 RAIA9909003 1 19990916 A 2612 51228801 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 570HK 41089 75086 JFK- LEFT ENGINE OVERHEAT CAP ILLUMINATED. MAINTENANCE REPLACED FIRE LOOP ASSY FOR LEFT ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 1999092400537 19990924 00537 EU 1999 9 24 RAIA9909004 1 19990918 A 2421 8260121 GENERATOR AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LT ENGINE FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 722TE 19193 14394 220 124169R STL- NR 1 GENERATOR FELL OFF LINE AND WOULDN'T RESET. MAINTENANCE REPLACED NR 1 GENERATOR. 2 H 7 2 4T 4 T RT A53EU E2ONE 1999092400538 19990924 00538 EU 1999 9 24 RAIA9909005 1 19990919 A 3242 AC69596 MAXARET BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 430AM 437 437 880 STL- LEFT BRAKE DOESN'T WORK. MAINTENANCE REPLACED MAXARET FOR LEFT WHEEL. 2 L 7 2 4T RT A56EU 1999092400539 19990924 00539 WP 1999 9 24 TWAA9912901 1 19990920 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L1 PAX DOORWAY INOP A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 917TW 49366 THE EMERGENCY LIGHT BY THE NUMBER 1 LEFT CABIN DOOR WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. CHECK-C 7-13-99 STL. 2 L 7 2 4F A6WE 1999092400540 19990924 00540 NM 1999 9 24 TWAA9912902 1 19990921 A 5730 SKIN BOEING 757 7572Q8 1384972 NM WS 341.5-425.5 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 703TW 27620 DURING CHECK-C MAINT, FOUND APPROX 200 RIVETS WITH STAGE 2 CORROSION ON TOP OF THE LEFT WING UNDER THE ICE DETECTION STR IPE, STA 341.5 THRU 425.5. *S/D* CORROSION WAS REMOVED BY BLENDING PER SRM 57-30-1 FIG 6, AT A 10:1 REMOVAL RATIO. AL L BLEND OUT AREAS WERE MEASURED AND INFORMATION GIVEN TO BOEING ENGINEERING. A BOEING TEAM ACCOMPLISHED FASTENER REMOVA L AND INSTALLATION OF 120 FASTENERS WITH MATERIAL REMOVED GREATER THAN 0.020 INCHES. THE DAMAGED BACR15FH8* RIVETS WERE REPLACED WITH BACB30NY8K*Y HI-LOKS. TWA MAINTENANCE RESTORED THE AREA TO THE ORIGINAL PROTECTIVE FINISH PER SRM 57-30- 1, FIGURE 6. 2 L 7 2 4F RT A2NM 1999092400541 19990924 00541 WP 1999 9 24 TWAA9912903 1 19990919 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 658 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 921L 47107 FOUND A .25 INCH CRACK IN LONGERON 6L AT STA 658. REPAIRED PER SRM 53-02, FIG 18. CHECK-C 7-14-98 STL. 2 L 7 2 4F A6WE 1999092400542 19990924 00542 WP 1999 9 24 TWAA9912904 1 19990919 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 921L 47107 FOUND A .1875 INCH CRACK AT LONGERON 6L STA 718. REPAIRED PER SRM 53-02, FIG 18. CHECK-C 7-14-98 STL. 2 L 7 2 4F A6WE 1999092400543 19990924 00543 NM 1999 9 24 AWXA9900320 1 19990920 A 8011 7749843 STARTER BOEING 757 7572G7 1384963 NM NR 1 ENGINE FAILED A AWXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 908AW 15094 5536 24233 BOTH ENGINES RUNNING BURNING SMELL NOTICED IN REAR OF A/C AND IN COCKPIT VERIFIED SMELL WITH NR 1 BLEED ON, LT PACK ON, ISO VALVE CLOSED. COULD NOT DUPLICATE IN ANY OTHER CONFIG. FOUND NR 1 STARTER OIL LOW WITH METAL CHIPS. REMOVED AND R EPLACED STARTER, TT 0107843. 2 L 7 2 4F RT A2NM 1999092400544 19990924 00544 NM 1999 9 24 AWXA9900321 1 19990919 A 2910 65446915 HYD MODULE BOEING 737 737301 1384611 NM RT MLG FAILED A AWXA O OTHER L NO TEST AP APPROACH 1 WP 28 326AW 46871 46871 23258 ON FINAL, LOWERED LANDING GEAR, DID NOT GET GREEN LIGHTS BUT RED. CYCLED GEAR WITH SAME RESULTS. MANUALLY EXTENDED RT GEAR AND GOT GREEN LIGHT, LANDED NORMALLY. REMOVED AND REPLACED RT MLG HYDRAULIC MODULE, LK AND OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999092400545 19990924 00545 NM 1999 9 24 AWXA9900322 1 19990919 A 5610 5717623073AW WINDOW BOEING 737 737301 1384611 NM L2 WINDOW CRACKED A AWXA K NONE O OTHER CR CRUISE 1 WP 28 324AW 23261 L2 WINDOW OUTER PANE CRACKED AT ALTITUDE THEN STARTED ARCING, NO PRESS LOSS. REMOVED AND REPLACED CAPT'S SLIDING WINDOW . ALSO, REPLACED WINDOW HEAT CONTROL. 2 L 7 2 4F RT A16WE 1999092400546 19990924 00546 WP 1999 9 24 CALA9901239 1 19990917 A 3222 VALVE DOUG DC9 DC983 3022083 WP NLG FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 938MC 49525 THE NOSE GEAR RED UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. CYCLING THE GEAR PRODUCED NO CHANGE. THE AI RCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT FLAT. THE SHRADER VALVE WAS REPLACED AND THE NLG WAS SERVICED WITH NITROGEN IAW MM 32-21-02. A NOSE GEAR SWING WAS PERFORMED AND OPERATION CHEC KED GOOD. 2 L 7 2 4F RT A6WE 1999092400547 19990924 00547 WP 1999 9 24 CALA9901241 1 19990916 A 5730 PANEL DOUG DC9 DC982 3022082 WP WS 69 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 3 INCH CRACK IN STRESS PANEL AT LT WING SPAR AREA, XRS 69. THE PANEL WAS REMOVED AND REPLACED IAW MM 20-10-01 AND SRM 51-30-05. 2 L 7 2 4F A6WE 1999092400548 19990924 00548 WP 1999 9 24 CALA9901242 1 19990916 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 200 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND AN 8 INCH CRACK IN REPAIR DOUBLER AT L-1 DOOR AREA CUSP WEB, FS 200, LONGERON 18L. THE CRACKED AREA WA S TRIMMED OUT IAW SRM 53-01, FIGURE 1. A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999092400549 19990924 00549 WP 1999 9 24 CALA9901243 1 19990916 A 5542 SKIN DOUG DC9 DC982 3022082 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 2 INCH CRACK IN RUDDER BOTTOM RT SIDE FAIRING SKIN. THE FAIRING SKIN WAS REMOVED IAW SRM 51-30-1. A REPAIR WAS INSTALLED IAW SRM 51-10-4, 51-30-2, 51-10-3, AND 51-30-1. 2 L 7 2 4F A6WE 1999092400550 19990924 00550 WP 1999 9 24 CALA9901244 1 19990916 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1308 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FLOORBEAM CORRODED IN AFT PIT AT CEILING, STA 1308, RBL 24. A FLOORBEAM FILLER REPAIR WAS INSTALLED IA W SRM 53-05, FIGURE 20A. 2 L 7 2 4F A6WE 1999092400551 19990924 00551 WP 1999 9 24 CALA9901245 1 19990916 A 7110 5930645509 COWL DOUG DC9 DC982 3022082 WP NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 12 CRACK IN NR 2 ENGINE INLET HOUSING INTERNAL LOWER AFT WALL. THE NR 2 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01. 2 L 7 2 4F A6WE 1999092400552 19990924 00552 WP 1999 9 24 CALA9901246 1 19990916 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 180 & 200 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 180 BETWEEN LONGERON 22R AND 23R, AND AT STA 200 BETWEEN LONGERONS 19R AND 20R. THE DENTED AREAS OF SKIN WERE REPAIRED IAW SRM 53-04, FIGURE 38 AND MM 51-00-00. 2 L 7 2 4F A6WE 1999092400553 19990924 00553 WP 1999 9 24 CALA9901247 1 19990916 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-210 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 200-210, RBL 54.5. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE PLATE WERE INSTALLED IAW SRM 51-30-1, 51-30-5, 53-05, FIGURE 4F, 51-12-3, AND 51-12-5. 2 L 7 2 4F A6WE 1999092400554 19990924 00554 NM 1999 9 24 CALA9901248 1 19990917 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND FORWARD LAV/GALLEY AREA FLOORBEAM CORRODED AT STA 294, LBL 18 TO RBL 12. A FLOORBEAM UPPER TEE CHORD R EPAIR WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999092400555 19990924 00555 NM 1999 9 24 CALA9901249 1 19990917 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 727, STRINGER 14L. REPAIRED IAW ECRA 5310-03926. 2 L 7 2 4F RT A16WE 1999092400556 19990924 00556 NM 1999 9 24 CALA9901250 1 19990917 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 990 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 990, STRINGER 23L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOS TAL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1999092400557 19990924 00557 NM 1999 9 24 CALA9901251 1 19990917 A 3397 WIRE BOEING 727 727232 1384082 NM ROW 11 DISCONNECTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 THE EMERGENCY EXIT LIGHT WIRING WAS FOUND PULLED OUT OF CONDUIT AND DISCONNECTED AT ROW 11. THE WIRING WAS RECONNECTED AND PLACED BACK INTO CONDUIT IAW MM 20-00-00. 2 L 7 3 4F A3WE 1999092400558 19990924 00558 WP 1999 9 24 CALA9901252 1 19990918 A 3350 20131A BATTERY PACK RADIANT DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND FORWARD CABIN EMERGENCY PATH LIGHTING INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERA TION CHECKED GOOD IAW MM 33-50-00. 2 L 7 2 4F A6WE 1999092400559 19990924 00559 WP 1999 9 24 CALA9901253 1 19990918 A 5753 SKIN DOUG DC9 DC932 3022066 WP RT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND A DENT ON BOTTOM OF RT WING FLAP APPROXIMATELY 13 O/B OF I/B FOLDING VANES AREA. THE DENTED AREA WAS C UT OUT AND A REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 5 AND 51-10-2, PAGE 1. 2 L 7 2 4F A6WE 1999092400560 19990924 00560 WP 1999 9 24 CALA9901254 1 19990918 A 5310 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND CORROSION AT FORWARD BAGGAGE COMPARTMENT LOWER CUTOUT WHERE THRESHOLD MOUNTS. THE FORWARD LOWER CUTOUT WAS REMOVED. THE LOWER CARGO DOOR JAMB PAN WAS CUT OUT AND A NEW PAN WAS INSTALLED IAW SRM 51-10-3, PAGE 1, 51-30-2, P AGE1, AND 53-05, PAGE 113. 2 L 7 2 4F A6WE 1999092400561 19990924 00561 WP 1999 9 24 CALA9901255 1 19990918 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND EMERGENCY PATH LIGHTING IN AFT ACCESS SECTION WITH AFT LIGHT WIRING DAMAGED. THE WIRING WAS REPAIRED A ND OPERATION CHECKED GOOD IAW MM 33-50-00. 2 L 7 2 4F A6WE 1999092400562 19990924 00562 NM 1999 9 24 CALA9901256 1 19990918 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 373 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17309 23360 INSPECTION FOUND A 2 INCH CRACK IN FORWARD LOWER FUSELAGE SKIN AT BS 373 AT GROUND BLOWER EXHAUST. THE CRACK WAS STOP D RILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02870. 2 L 7 2 4F RT A16WE 1999092400563 19990924 00563 WP 1999 9 24 CALA9901257 1 19990918 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 731 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FRAME LOWER LEG CORRODED AT STA 731, LONGERON 30. THE LOWER FRAME ANGLE WAS REMOVED AND REPLACED IAW S RM 51-30-05. 2 L 7 2 4F A6WE 1999092400564 19990924 00564 WP 1999 9 24 CALA9901258 1 19990918 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RT CUSP WEB CORRODED AT FS 218, RBL 54. THE AREA WAS REPAIRED IAW SRM 51-10-3, 51-10-4, AND 53-01, FIG URE 2, SHEET 3. 2 L 7 2 4F A6WE 1999092400565 19990924 00565 WP 1999 9 24 CALA9901259 1 19990918 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RT GALLEY SUPPORT FITTING CORRODED AT FS 200, RBL 48. THE GALLEY SUPPORT FITTING WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999092400566 19990924 00566 WP 1999 9 24 CALA9901260 1 19990919 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 731 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 2 INCH CRACK IN MID CARGO PIT LEFT CEILING SUPPORT AT STA 731, LBL 24. THE CRACK WAS STOP DRILLED IA W SRM 53-01, FIGURE 2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 53-10, FIGURE 2. 2 L 7 2 4F A6WE 1999092400567 19990924 00567 WP 1999 9 24 CALA9901261 1 19990919 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FORWARD CARGO DOOR PAN LOWER SIDE CORRODED AROUND RIB NUTS. THE PAN WAS REMOVED AND A NEW PAN WAS INST ALLED IAW SRM 51-30-2, 51-30-5, 51-30-1, 51-30-7, AND 51-20-0. 2 L 7 2 4F A6WE 1999092400568 19990924 00568 WP 1999 9 24 CALA9901262 1 19990919 A 5720 VANE DOUG DC9 DC982 3022082 WP LT WING PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND LT WING I/B FIXED VANE PUNCTURED ON TOP CENTER. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-03. 2 L 7 2 4F A6WE 1999092400569 19990924 00569 WP 1999 9 24 CALA9901263 1 19990919 A 5755 SKIN DOUG DC9 DC982 3022082 WP RT SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RT GROUND SPOILER DELAMINATED. THE SPOILER WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-62-01. 2 L 7 2 4F A6WE 1999092400570 19990924 00570 WP 1999 9 24 CALA9901264 1 19990919 A 5720 VANE DOUG DC9 DC982 3022082 WP RT WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RT WING O/B NR 2 FIXED VANE GOUGED. THE FIXED VANE WAS REMOVED AND REPAIRED IAW DRAWING NR SR09570025. THE VANE WAS REINSTALLED IAW MM 27-51-03. 2 L 7 2 4F A6WE 1999092400571 19990924 00571 WP 1999 9 24 CALA9901265 1 19990919 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 1174-1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND DOUBLER AT SILL OF DOOR JAMB CORRODED AT FS 1174-1183, LONGERON 27R (AFT PIT). THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-1, 53-14-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999092400572 19990924 00572 WP 1999 9 24 CALA9901266 1 19990919 A 5350 FAIRING DOUG DC9 DC982 3022082 WP RT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 3 INCH CRACK IN RT HORIZONTAL STABILIZER FAIRING. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INST ALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999092400573 19990924 00573 SO 1999 9 24 COMA9910148 1 19990916 A 5270 SWITCH EMB 120 EMB120RT SO FUEL DOOR OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 261CA 120254 SERVICE DOOR WARNING DURING TAKEOFF. ADJUSTED FUEL SERVICE DOOR SWITCH. 2 L 7 2 4T RT A31SO 1999092400574 19990924 00574 NE 1999 9 24 COMA9960532 2 19990920 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT VIBRATION A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 956CA 7105 807283 RIGHT HAND ENGINE N1 VIB 2.7 ABOVE LIMITS. BALANCED ENGINE TO ACCEPTABLE LIMITS. 2 L 7 2 4F 4 F RT A21EA E15NE 1999092400575 19990924 00575 EA 1999 9 24 COMA9960533 1 19990919 A 5330 601R10045 SKIN CNDAIR CL600 CL6002B19 EA RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 7159 SEVEN SMALL CRACKS IN THE FORWARD AND AFT HORIZONTAL SURFACES OF RIGHT HAND WING ACCESS HOLE AT PANEL 640DB. REPAIRED C RACKS IAW BOMBARDIER REO NR 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999092400576 19990924 00576 EU 1999 9 24 QXEA9901784 1 19990821 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305C AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51- 31-01. 2 L 7 2 4F RT A20EU 1999092400577 19990924 00577 EU 1999 9 24 QXEA9901785 1 19990820 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305C AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51- 31-01. 2 L 7 2 4F RT A20EU 1999092400578 19990924 00578 EU 1999 9 24 QXEA9901786 1 19990821 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 9305C AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51- 31-01. 2 L 7 2 4F RT A20EU 1999092400579 19990924 00579 EU 1999 9 24 QXEA9901787 1 19990828 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 10346 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400580 19990924 00580 EU 1999 9 24 QXEA9901788 1 19990826 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 FRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CRACKED AT 7805 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400581 19990924 00581 EU 1999 9 24 QXEA9901789 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT 6805 AND STRINGER 19. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400582 19990924 00582 EU 1999 9 24 QXEA9901790 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT 6305 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400583 19990924 00583 EU 1999 9 24 QXEA9901791 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT 6305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400584 19990924 00584 EU 1999 9 24 QXEA9901792 1 19990823 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT 5805 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 53-01-00, PARAGRAPH 3. 2 L 7 2 4F RT A20EU 1999092400585 19990924 00585 EU 1999 9 24 QXEA9901793 1 19990831 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT 5805 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400586 19990924 00586 EU 1999 9 24 QXEA9901794 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 603 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 603. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400587 19990924 00587 EU 1999 9 24 QXEA9901795 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 601 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 601. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400588 19990924 00588 EU 1999 9 24 QXEA9901796 1 19990821 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 593 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK GOUGED AT STATION 593. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400589 19990924 00589 EU 1999 9 24 QXEA9901797 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 590 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK GOUGED AT STATION 590. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400590 19990924 00590 EU 1999 9 24 QXEA9901798 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 588 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 588. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400591 19990924 00591 EU 1999 9 24 QXEA9901799 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 580 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 580. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400592 19990924 00592 EU 1999 9 24 QXEA9901800 1 19990901 A 5712 RIB FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - CRACK AT Z STRINGER CUTOUT AT BL 225R AT STRINGER 2.05. REPAIRED IAW HORIZON AIR EA 4-57-303, STEPS 3-6. 2 L 7 2 4F RT A20EU 1999092400593 19990924 00593 EU 1999 9 24 QXEA9901801 1 19990901 A 5712 RIB FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - CRACK AT Z STRINGER CUTOUT AT BL 225R AT STRINGER 2.04. REPAIRED IAW HORIZON AIR EA 4-57-303, STEPS 3-6. 2 L 7 2 4F RT A20EU 1999092400594 19990924 00594 EU 1999 9 24 QXEA9901802 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 74D MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 8-9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999092400595 19990924 00595 EU 1999 9 24 QXEA9901803 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 74C MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999092400596 19990924 00596 EU 1999 9 24 QXEA9901804 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 74B MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999092400597 19990924 00597 EU 1999 9 24 QXEA9901805 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 74A MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999092400598 19990924 00598 EU 1999 9 24 QXEA9901806 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 72A MOUNT FLANGE ON RIGHT-HAND WING LOWER SKIN HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8-9, PARAGRAPH 4A. 2 L 7 2 4F RT A20EU 1999092400599 19990924 00599 EU 1999 9 24 QXEA9901807 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 71A HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999092400600 19990924 00600 EU 1999 9 24 QXEA9901808 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 73A HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999092400601 19990924 00601 EU 1999 9 24 QXEA9901809 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 73B HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400602 19990924 00602 EU 1999 9 24 QXEA9901810 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 73C HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400603 19990924 00603 EU 1999 9 24 QXEA9901811 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL PANEL 73D HAS FRETTING CORROSION ON MATING SURFACE. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400604 19990924 00604 EU 1999 9 24 QXEA9901812 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL TANK 73D SURROUND OPENING HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400605 19990924 00605 EU 1999 9 24 QXEA9901813 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL TANK 73C SURROUND OPENING HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400606 19990924 00606 EU 1999 9 24 QXEA9901814 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL TANK SURROUND OPENING 73B HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400607 19990924 00607 EU 1999 9 24 QXEA9901815 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL TANK SURROUND OPENING 71A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400608 19990924 00608 EU 1999 9 24 QXEA9901816 1 19990820 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUEL TANK SURROUND OPENING 73A HAS FRETTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999092400609 19990924 00609 EU 1999 9 24 QXEA9901817 1 19990820 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400610 19990924 00610 EU 1999 9 24 QXEA9901818 1 19990824 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400611 19990924 00611 EU 1999 9 24 QXEA9901819 1 19990824 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400612 19990924 00612 EU 1999 9 24 QXEA9901820 1 19990824 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400613 19990924 00613 EU 1999 9 24 QXEA9901821 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400614 19990924 00614 EU 1999 9 24 QXEA9901822 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400615 19990924 00615 EU 1999 9 24 QXEA9901823 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 BELOW STRINGER 26. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400616 19990924 00616 EU 1999 9 24 QXEA9901824 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 ABOVE STRINGER 26. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400617 19990924 00617 EU 1999 9 24 QXEA9901825 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 25, REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400618 19990924 00618 EU 1999 9 24 QXEA9901826 1 19990822 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 21. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400619 19990924 00619 EU 1999 9 24 QXEA9901827 1 19990821 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 20. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400620 19990924 00620 EU 1999 9 24 QXEA9901828 1 19990821 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 15205 AND STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400621 19990924 00621 EU 1999 9 24 QXEA9901829 1 19990825 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 14755 AND STRINGER 39. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400622 19990924 00622 EU 1999 9 24 QXEA9901830 1 19990825 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 14755 AND STRINGER 27. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7B. 2 L 7 2 4F RT A20EU 1999092400623 19990924 00623 EU 1999 9 24 QXEA9901831 1 19990825 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 14205 AND STRINGER 20. REPAIRED IAW FOKKER 51-31-01, PAGE 13, PARAGRAPH 7B. 2 L 7 2 4F RT A20EU 1999092400624 19990924 00624 EU 1999 9 24 QXEA9901832 1 19990828 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815B AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400625 19990924 00625 EU 1999 9 24 QXEA9901833 1 19990826 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815B AND STRINGER 43. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7B. 2 L 7 2 4F RT A20EU 1999092400626 19990924 00626 EU 1999 9 24 QXEA9901834 1 19990828 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815B AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400627 19990924 00627 EU 1999 9 24 QXEA9901835 1 19990830 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400628 19990924 00628 EU 1999 9 24 QXEA9901836 1 19990830 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-30-02, P AGE 10 PARAGRAPH C. 2 L 7 2 4F RT A20EU 1999092400629 19990924 00629 EU 1999 9 24 QXEA9901837 1 19990831 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400630 19990924 00630 EU 1999 9 24 QXEA9901838 1 19990830 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400631 19990924 00631 EU 1999 9 24 QXEA9901839 1 19990830 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400632 19990924 00632 EU 1999 9 24 QXEA9901840 1 19990830 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815A AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400633 19990924 00633 EU 1999 9 24 QXEA9901841 1 19990901 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - STRINGER 35 CRACKED AT INSULATION RETAINER HOLE, CRACK IS 2 AFT OF FRAME 13815. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1, SRM 51-31-01 AND SRM 51-10-4, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999092400634 19990924 00634 EU 1999 9 24 QXEA9901842 1 19990831 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400635 19990924 00635 EU 1999 9 24 QXEA9901843 1 19990831 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13815 AND STRINGER 40. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B-C AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400636 19990924 00636 EU 1999 9 24 QXEA9901844 1 19990831 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 13345 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-10-4, PAG E 9, PARAGRAPH 4B-C. 2 L 7 2 4F RT A20EU 1999092400637 19990924 00637 EU 1999 9 24 QXEA9901845 1 19990831 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU RT EMER EXIT GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND AFT EMERGENCY EXIT APERTURE TOP TORSION BOX COVER HAS TWO GOUGE MARKS CAUSED BY SCREWS FROM EMERGENCY E XIT. REPAIRED IAW HORIZON AIR EA 4-53-856. 2 L 7 2 4F RT A20EU 1999092400638 19990924 00638 EU 1999 9 24 QXEA9901846 1 19990831 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 10966 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400639 19990924 00639 EU 1999 9 24 QXEA9901847 1 19990821 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 12405 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400640 19990924 00640 EU 1999 9 24 QXEA9901848 1 19990821 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 12405 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400641 19990924 00641 EU 1999 9 24 QXEA9901849 1 19990829 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400642 19990924 00642 EU 1999 9 24 QXEA9901850 1 19990829 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3- 4-5. 2 L 7 2 4F RT A20EU 1999092400643 19990924 00643 EU 1999 9 24 QXEA9901851 1 19990829 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3- 4-5. 2 L 7 2 4F RT A20EU 1999092400644 19990924 00644 EU 1999 9 24 QXEA9901852 1 19990829 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 45. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3- 4-5. 2 L 7 2 4F RT A20EU 1999092400645 19990924 00645 EU 1999 9 24 QXEA9901853 1 19990829 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 12875 AND STRINGER 46. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, 1-2-3-4 -5. 2 L 7 2 4F RT A20EU 1999092400646 19990924 00646 EU 1999 9 24 QXEA9901886 1 19990910 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - LEFT-HAND WING INBOARD FUEL PANEL MOUNTING FLANGE HAS A SAND THROUGH OPENING IN THE SKIN THAT MATES THE FUEL PANE L. REPAIRED IAW HORIZON AIR EA 4-57-311. 2 L 7 2 4F RT A20EU 1999092400647 19990924 00647 EU 1999 9 24 QXEA9901887 1 19990908 A 5755 BRACKET FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - CRACK IN LIGHTENING HOLE SPEED BRAKE SUPPORT BRACKET, FORWARD RIGHT-HAND SIDE. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 10, FIGURE 8. 2 L 7 2 4F RT A20EU 1999092400648 19990924 00648 EU 1999 9 24 QXEA9901888 1 19990902 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND FRAME 67-2 IS CRACKED PAST STOP DRILL AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-10-05. 2 L 7 2 4F RT A20EU 1999092400649 19990924 00649 EU 1999 9 24 QXEA9901889 1 19990820 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FRAME 4900 DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND FLOORBEAM 1127 REQUIRES CLEANING IN THE AREA OF FRAME 4900. CLEANED AREA AS REQUIRED. 2 L 7 2 4F RT A20EU 1999092400650 19990924 00650 EU 1999 9 24 QXEA9901890 1 19990821 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 16660 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUSELAGE INTERIOR SKIN HAS GOUGE MARKS STARTING 3 FORWARD OF FRAME 16660 BETWEEN STRINGERS 32 AND 33. REPAIRED IA W FOKKER SRM 51-10-4, PAGE 8, 3C, NR 4. 2 L 7 2 4F RT A20EU 1999092400651 19990924 00651 EU 1999 9 24 QXEA9901891 1 19990821 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 16060 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FUSELAGE FRAME 16060 HAS GOUGE MARKS ON FRAME CAP BETWEEN STRINGERS 33 AND 34. REPAIRED IAW FOKKER SRM 51-10-4, P AGE 8, 3C, NR 4. 2 L 7 2 4F RT A20EU 1999092400652 19990924 00652 EU 1999 9 24 QXEA9901892 1 19990823 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 5805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRA PH 3 AND SRM 51-11-01. 2 L 7 2 4F RT A20EU 1999092400653 19990924 00653 EU 1999 9 24 QXEA9901893 1 19990902 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 5805 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1999092400654 19990924 00654 EU 1999 9 24 QXEA9901894 1 19990823 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5803 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 5803 AND STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAP H 3, SRM 51-11-01. 2 L 7 2 4F RT A20EU 1999092400655 19990924 00655 EU 1999 9 24 QXEA9901895 1 19990823 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FRAME CLIP CRACKED AT FRAME 5305 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, SRM 53-01-00, PARAGRAP H 3, AND SRM 51-11-01. 2 L 7 2 4F RT A20EU 1999092400656 19990924 00656 EU 1999 9 24 QXEA9901896 1 19990820 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 548 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - LEFT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 548. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400657 19990924 00657 EU 1999 9 24 QXEA9901897 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 659 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 659. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C . 2 L 7 2 4F RT A20EU 1999092400658 19990924 00658 EU 1999 9 24 QXEA9901898 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 639 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK IS GOUGED AT STATION 639. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C . 2 L 7 2 4F RT A20EU 1999092400659 19990924 00659 EU 1999 9 24 QXEA9901899 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 610 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT HAND OUTBOARD SEAT TRACK GOUGED AT STATION 610. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400660 19990924 00660 EU 1999 9 24 QXEA9901900 1 19990829 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 357 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS SURFACE CORROSION AT STATION 357. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PA RAGRAPH 4A AND HORIZON AIR EA 4-53-864. 2 L 7 2 4F RT A20EU 1999092400661 19990924 00661 EU 1999 9 24 QXEA9901901 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 647 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 647. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400662 19990924 00662 EU 1999 9 24 QXEA9901902 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 639 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 639. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400663 19990924 00663 EU 1999 9 24 QXEA9901903 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 618 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 618. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400664 19990924 00664 EU 1999 9 24 QXEA9901904 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 588 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 588. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400665 19990924 00665 EU 1999 9 24 QXEA9901905 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 572 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 572. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400666 19990924 00666 EU 1999 9 24 QXEA9901906 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 567 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 567. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400667 19990924 00667 EU 1999 9 24 QXEA9901907 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 530 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK GOUGED AT STATION 530. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400668 19990924 00668 EU 1999 9 24 QXEA9901908 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 498 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK GOUGED AT STATION 498. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400669 19990924 00669 EU 1999 9 24 QXEA9901909 1 19990828 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 481 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK INBOARD FLANGE HAS A GOUGE MARK AT STATION 481. REPAIRED IAW HORIZON AIR EA 4-58-86 1, STEPS 1 THROUGH 3. 2 L 7 2 4F RT A20EU 1999092400670 19990924 00670 EU 1999 9 24 QXEA9901910 1 19990822 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 480 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - RIGHT-HAND INBOARD SEAT TRACK IS GOUGED AT STATION 480. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 1999092400671 19990924 00671 EU 1999 9 24 QXEA9901911 1 19990911 A 5210 BEAM FOKKER F28 F28MK4000 4990810 EU PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - MAIN CABIN DOOR HEADER BEAM IS CRACKED AT FORWARD END AT FRAME 3450. REPAIRED IAW HORIZON AIR EA 4-53-879. 2 L 7 2 4F RT A20EU 1999092400672 19990924 00672 EU 1999 9 24 QXEA9901912 1 19990908 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - SKIN UNDER LOWER COMM ANTENNA IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-868. 2 L 7 2 4F RT A20EU 1999092400673 19990924 00673 EU 1999 9 24 QXEA9901913 1 19990828 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - AFT CARGO PIT FRAME 16060 HAS A CRACK IN THE CASTELLATION AT STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999092400674 19990924 00674 EU 1999 9 24 QXEA9901914 1 19990828 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - CLIP CRACKED AT FRAME 16060 AND STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400675 19990924 00675 EU 1999 9 24 QXEA9901915 1 19990906 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - UPPER FLANGE ON HORIZONTAL BEAM I DAMAGED DURING RIVET INSTALLATION AT BL 425R, NEXT TO UPPER CONSOLE. REPAIRED I AW 53-02-18, PAGE 36, FIGURE 13, SECTION B-B. 2 L 7 2 4F RT A20EU 1999092400676 19990924 00676 EU 1999 9 24 QXEA9901916 1 19990908 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - NAV COMM LOWER FUSELAGE SKIN HAS CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-868. 2 L 7 2 4F RT A20EU 1999092400677 19990924 00677 EU 1999 9 24 QXEA9901917 1 19990906 A 5320 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - AFT CARGO DOOR APERTURE FORWARD FRAME HAS DENT WITH DEEP GOUGES AT BL 700R AFT OF STRINGER 67. REPAIRED IAW FOKKE R SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999092400678 19990924 00678 EU 1999 9 24 QXEA9901918 1 19990829 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FORWARD CARGO DOOR INNER SKIN BULGED AND DENTED FROM LOWER EDGE UP EIGHT INCHES. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 53-02-01. 2 L 7 2 4F RT A20EU 1999092400679 19990924 00679 EU 1999 9 24 QXEA9901919 1 19990902 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CANNING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - CENTER CARGO DOOR INNER SKIN IS OIL CANNING AT LOWER END IN CENTER. REPAIRED IAW HORIZON AIR EA 4-52-262. 2 L 7 2 4F RT A20EU 1999092400680 19990924 00680 EU 1999 9 24 QXEA9901920 1 19990829 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FORWARD CARGO COMPARTMENT FRAME 9305A HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW FO KKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999092400681 19990924 00681 EU 1999 9 24 QXEA9901921 1 19990829 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FORWARD CARGO COMPARTMENT FRAME 9305 HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW FOK KER SRM 51-31-01 AND HORIZON AIR EA 4-53-852. 2 L 7 2 4F RT A20EU 1999092400682 19990924 00682 EU 1999 9 24 QXEA9901922 1 19990829 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FORWARD CARGO COMPARTMENT FRAME 8305 HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW HOR IZON AIR EA 4-53-858. 2 L 7 2 4F RT A20EU 1999092400683 19990924 00683 EU 1999 9 24 QXEA9901923 1 19990828 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - FORWARD CARGO COMPARTMENT FRAME 7805 HAS CORROSION AT TWO NUT PLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW FOK KER SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 1999092400684 19990924 00684 EU 1999 9 24 QXEA9901924 1 19990907 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - BEAM V HAS A CRACK ALONG UPPER ROW OF RIVETS AT BLL 0 CL. REPAIRED IAW HORIZON AIR EA 4-53-849. 2 L 7 2 4F RT A20EU 1999092400685 19990924 00685 EU 1999 9 24 QXEA9901925 1 19990820 A 5320 POST FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 PDX - LEFT-HAND NR 2 WINDOW POST LOWER STRUCTURE HAS A BRACKET THAT IS CRACKED THROUGH TWO RIVETS. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A, 1-2-3-4-5. 2 L 7 2 4F RT A20EU 1999092400686 19990924 00686 NM 1999 9 24 QXEA9901930 1 19990918 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM COCKPIT LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 829PH 304 PDX - EMERGENCY LIGHTS DO NOT OPERATE FROM FLIGHT ATTENDENTS PANEL SWITCH. PILOTS SWITCH OPERATES NORMAL. RECONNECTED LOOSE WIRE AT SWITCH, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2 H 7 2 4T RT A13NM 1999092400687 19990924 00687 EU 1999 9 24 QXEA9901931 1 19990919 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 SEVERAL LIGHTS OUT IN EMERGENCY SIGN. REMOVED AND REPLACED EMERGENCY LIGHT CIRCUIT BOARD, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999092400688 19990924 00688 EU 1999 9 24 QXEA9901932 1 19990919 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 492US 11159 EMERGENCY EXIT SIGN OVER COAT CLOSET HAS INOPERATIVE LIGHTS. REMOVED AND REPLACED EXIT SIGN ASSEMBLY, OPERATIONAL CHEC K GOOD. 2 L 7 2 4F RT A20EU 1999092400689 19990924 00689 EU 1999 9 24 QXEA9901933 1 19990918 A 3350 6008903 POWER SUPPLY GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 LEFT HAND OVERWING EXIT SIGN HAS INOPERATIVE LIGHTS. REMOVED AND REPLACED NR 5 POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999092400690 19990924 00690 NM 1999 9 24 99FDEA00394 1 19990917 A 2612 FIRE WIRE DOUG MD11 MD11F 3023600 NM NR 2 ENGINE FAILED A FDEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TO TAKEOFF 1 SO 25 605FE 48514 SHUTDOWN NR 2 ENG IN FLT DUE TO FIRE WARN IND, DISCHARGED FIRE-X BOTTLE. REMOVED AND REPLACED HARNESSES 420804-0000, 42 0896-0000, & 224W9727-517. ALSO, REPLACED FIRE-X BOTTLE (P/N 895564-10. RAN ENG, CHECK GOOD. 2 L 7 3 4F RT A22WE 1999092400691 19990924 00691 NM 1999 9 24 99FDEA00395 1 19990920 A 3230 RETRACT MECH DOUG MD11 MD11F 3023600 NM NLG LACK OF LUBE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 585FE 48481 RETRACT LANDING GEAR ON CLIMBOUT, BOTH PRIMARY GEAR SHOW NOSE GEAR UNSAFE (RED). LUBED NOSE GEAR PER 12-21-03-3. JACKE D MLG AND CYCLED 15 TIMES, 7 SEC TO RETRACT, 17 SEC TO EXTEND. WITHIN LIMITS PER 32-30-17-02. 2 L 7 3 4F RT A22WE 1999092400692 19990924 00692 SO 1999 9 24 SWIA971561 1 19990903 A 3230 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 LANDING GEAR WOULD NOT RETRACT ON DEPARTURE. RETURNED TO SAN. REMOVED AND REPLACED LANDING GEAR CONTROL BOX. OPERATED LANDING GEAR SEVERAL TIMES WITH NO DISCREPANCIES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400693 19990924 00693 SO 1999 9 24 SWIA971562 1 19990904 A 7603 POWER LEVER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE JAMMED A SWIA E ENGINE SHUTDOWN F FLT CONT AFFECTED DE DESCENT 1 NM 07 564SW 120339 RIGHT POWER LEVER STUCK AT 85 PERCENT TQ INFLIGHT. UNABLE TO RETARD POWER LEVER. SHUT ENGINE DOWN. FOUND BONDING STRA P HOOKED ON RIGHT POWER LEVER FLIGHT IDLE SOLENOID HOOK ON BELLCRANK. REMOVED BONDING STRAP AND INSTALLED SHORTER STRAP . MOVED POWER LEVER THROUGH FULL RANGE AND CHECKED CLEARANCE. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400694 19990924 00694 SO 1999 9 24 SWIA971563 1 19990908 A 3320 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE ROW 9A SHORTED A SWIA A F UNSCHED LANDING ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 NM 07 291SW 120318 WHILE EN ROUTE LAX FROM MRY, FLIGHT ATTENDANT NOTICED SMOKE AND FLAME FROM OVERHEAD AREA OF SEAT POSITION 9A. FLIGHT AT TENDANT EXTINGUISHED FLAMES WITH EXTINGUISHER. CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO SBP WHERE A NORMAL LANDING WAS MADE. MAINTENANCE DISCOVERED LIGHT FIXTURE AT SEAT 9A SHORTED, CAUSING A 2 SQUARE INCH BURNED SPOT ON THE OVERHEAD LINER. AIRCRAFT FERRIED TO FAT WHERE REPLACEMENT OF LIGHT FIXTURE AND REPAIR OF OVERHEAD LINING WAS ACCOMPLISHED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999092400695 19990924 00695 NM 1999 9 24 VNAA9909004 1 19990917 A 3240 BRAKE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG REQD SERVICE A VNAA K NONE O OTHER NR NOT REPORTED 1 GL 07 442JS 3060 THE CAPTAIN REPORTED THAT THE AIRCRAFT BRAKES WOULD NOT RESPOND WHEN PEDAL FORCE WAS APPLIED. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED AND BLED THE CAPTAINS BRAKE SYSTEMS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 3 2-42-00. FUNCTION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999092400696 19990924 00696 NM 1999 9 24 VNAA9909005 1 19990916 A 5242 001A524A0100D01 HINGE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE SERVICE DOOR DAMAGED A VNAA K NONE O OTHER NR NOT REPORTED 1 GL 07 429JS 3043 THE OXYGEN SERVICE DOOR WAS FOUND TO HAVE THE FORWARD HINGE DAMAGED WHILE PARKED ON THE RAMP IN CLT. OUTSTATION MAINTEN ANCE INSPECTED THE AIRCRAFT AND APPROVED A FERRY FLIGHT TO CAK FOR REPAIRS. THE FERRY FLIGHT WAS COMPLETED WITHOUT ANY PROBLEMS. CAK MAINTENANCE REPLACED THE OXYGEN SERVICE DOOR IN ACCORDANCE WITH JIC 06-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999092400697 19990924 00697 EU 1999 9 24 RAIA9909006 1 19990903 A 5753 14157614403 SKIN JETAIR JETSTM JETSTM4101 1500501 EU LT TE FLAP DAMAGED A RAIA K NONE C F.O.D. IN INSP/MAINT 1 CE 03 551HK 41040 MX-STL- LEFT FLAP STRUCK BY GROUND EQUIPMENT. MAINTENANCE REPAIRED LEFT FLAP IAW EO NR J4100-27-001-1. 2 L 7 2 4T RT A41NM 1999092400698 19990924 00698 SO 1999 9 24 RAIA9909007 1 19990918 A 5330 SKIN EMB 145 EMB145ER SO FUSELAGE DAMAGED A RAIA K NONE C F.O.D. IN INSP/MAINT 1 CE 03 803HK 145077 MX-SBN- REAR FUSELAGE SKIN SUSTAINED DAMAGE FROM GROUND EQUIPMENT. MAINTENANCE REPAIRED DAMAGE IAW EO NR EMB145-53-001 -1. 2 L 7 2 4F RT T00011AT 1999092400730 19990924 00730 NE 1999 9 24 99ZZZX3612 2 19990717 A 8520 BEARING DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE ENGINE FAILED A VLLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 932H 13225 323 34368 CP352830 AFTER TAKEOFF ON DEPARTURE FROM OMA, LEFT OIL TEMPERATURE INCREASED TO RED LINE AND OIL PRESSURE DROPPED TO RED LINE. A IRCRAFT RETURNED TO OMA. METAL WAS FOUND IN OIL SCREEN. SUSPECT MASTER ROD BEARING FAILURE. 2 L 7 2 4R 4 R A669 5E4 1999092400744 19990924 00744 WP 1999 9 24 AALA991240 1 19990802 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 451-454 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 285AA 49297 TUL - NR 4 SEAT TRACK CORRODED. REPAIRED SEAT TRACK WITH PLUG REPAIR AS PER SRM 53-05 PART 1. (M) 2 L 7 2 4F A6WE 1999092400745 19990924 00745 EU 1999 9 24 SIMA992382 1 19990826 A 3350 66363 LIGHT SAAB SF340 340B 7860101 EU ROW 8-10 FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 382AE 340B382 DFW - FLT 3915 - EMERGENCY FLOOR PROXIMITY LIGHT FROM 8-10 DO NOT ILLUMINATE. REMOVED AND REPLACED FLOOR LIGHT STRIP. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999092400746 19990924 00746 EU 1999 9 24 SIMA992371 1 19990825 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 256AE A4555 340B256 RDU - FLT 4437 - CARGO SMOKE LIGHT CAME ON FOR 3-4 SECONDS AT 17,000 AGL. DISCHARGED NR 1 FIRE EXTINGUISHER. VERIFIED EVENT AS FALSE WARNING. REMOVED AND REPLACED BOTH CARGO BAY SMOKE DETECTORS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400747 19990924 00747 EU 1999 9 24 99ZZZM637 1 19990825 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 256AE A2894 340B256 RDU - FLT 4437 - CARGO SMOKE LIGHT CAME ON FOR 3-4 SECONDS AT 17,000 AGL. DISCHARGED NR 1 FIRE EXTINGUISHER. VERIFIED EVENT AS FALSE WARNING. REMOVED AND REPLACED BOTH CARGO BAY SMOKE DETECTORS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400748 19990924 00748 SO 1999 9 24 SIMA992301 1 19990819 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 603AE 100865 145055 ORD - FLT 4095 - TWO EMERGENCY EXIT SIGNS ON THE FORWARD CABIN BULKHEAD DO NOT ILLUMINATE. REMOVED AND REPLACED NR 1 BA TTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT T00011AT 1999092400749 19990924 00749 WP 1999 9 24 ASAA9980155 1 19990713 A 5350 LANYARD DOUG DC9 DC983 3022083 WP TAILCONE DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 964AS 53078 PDX - DURING MAINTENANCE CHECK, THE TAILCONE RELEASE LANYARD WAS FOUND DISCONNECTED FROM THE RETAINER PIN. RECONNECTED LANYARD TO RELEASE MECHANISM RETAINER PIN. (M) 2 L 7 2 4F RT A6WE 1999092400750 19990924 00750 WP 1999 9 24 ASAA9980130 1 19990602 A 5755 5926059 FITTING DOUG DC9 DC983 3022083 WP LT SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 OAK - DURING 30K CHECK, FOUND CORROSION ON LEFT WING INBOARD FLIGHT SPOILER INBOARD HINGE BRACKET TRUNNION END BEARING L OCK BOLT HOLE. REPAIRED IAW ASA EA 5740-01170. (M) 2 L 7 2 4F RT A6WE 1999092400751 19990924 00751 WP 1999 9 24 ASAA9980165 1 19990725 A 3350 0105606003 LAMP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 934AS 49235 SEA - AFTER ARRIVAL OF FLIGHT 655, CREW REPORTED ONE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WAS FOUND INOPERAT IVE. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999092400752 19990924 00752 WP 1999 9 24 ASAA9980163 1 19990724 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 0071 49235 OAK - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999092400753 19990924 00753 NM 1999 9 24 ASAA9940143 1 19990820 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 14-18 LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 792AS 28887 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 THROUGH 18 WERE FOUND INOPERATIVE. REC ONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999092400754 19990924 00754 NM 1999 9 24 ASAA9940142 1 19990813 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 1 LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 1 WERE FOUND LOOSE AND INOPERATIVE. REPLAC ED WIRING, LIGHTS AND TRACK COVER IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999092400755 19990924 00755 NM 1999 9 24 99ZZZM638 1 19990813 A 3350 LIGHTS BOEING 737 7374Q8 NM ROW 1 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 1 WERE FOUND LOOSE AND INOPERATIVE. REPLAC ED WIRING, LIGHTS AND TRACK COVER IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999092400756 19990924 00756 NM 1999 9 24 ASAA9910233 1 19990819 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE NR 1 PALLET WAS RECEIVING ONLY ON TRANSMITTER. REPLACED BATTERY PACK AND RECEIVER, AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400757 19990924 00757 NM 1999 9 24 99ZZZM639 1 19990819 A 3350 8821004 RECEIVER BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE NR 1 PALLET WAS RECEIVING ONLY ON TRANSMITTER. REPLACED BATTERY PACK AND RECEIVER, AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400758 19990924 00758 NM 1999 9 24 ASAA9910232 1 19990813 A 3350 6104781 BATTERY GRIMES BOEING 737 737210C 1384459 NM ROW 14 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - AFTER RECON, THE EMERGENCY EXIT TRACK LIGHT CHECK FAILED. REPLACED BATTERY AT ROW 14 AND BATTERY PACK AT ROW 16, EMERGENCY EXIT LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400759 19990924 00759 NM 1999 9 24 99ZZZM640 1 19990813 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM ROW 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - AFTER RECON, THE EMERGENCY EXIT TRACK LIGHT CHECK FAILED. REPLACED BATTERY AT ROW 14 AND BATTERY PACK AT ROW 16, EMERGENCY EXIT LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400760 19990924 00760 NM 1999 9 24 ASAA9910231 1 19990731 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM ROWS 6/7 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 6/7. REPLACED BATT ERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400761 19990924 00761 NM 1999 9 24 ASAA9910230 1 19990730 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM ROW 12 INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 SEA - PRIOR TO FLIGHT 65, THE EMERGENCY EXIT LIGHT RECEIVER AT ROW 12 WAS FOUND TO BE INOPERATIVE. REPLACED RECEIVER AN D LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999092400762 19990924 00762 NM 1999 9 24 ASAA9910229 1 19990729 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM ROW 18 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT TEST FAILED ON PALLET AT ROW 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400763 19990924 00763 NM 1999 9 24 ASAA9910228 1 19990726 A 3350 883200312 RECEIVERS BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT WERE FOUND INOPERATIVE AT PALLETS 6-8, 1-5, 2-1, 7- 4 AND 9-1. REPLACED RECEIVERS AT 1-5, 2-1, 7-4 AND 9-1, AND BATTERY AT PALLET 6-8, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400764 19990924 00764 NM 1999 9 24 99ZZZM641 1 19990726 A 3350 6104781 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT WERE FOUND INOPERATIVE AT PALLETS 6-8, 1-5, 2-1, 7- 4 AND 9-1. REPLACED RECEIVERS AT 1-5, 2-1, 7-4 AND 9-1, AND BATTERY AT PALLET 6-8, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400765 19990924 00765 NM 1999 9 24 ASAA9910227 1 19990723 A 3350 8731002142 LIGHT BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY STROBE LIGHT WAS FOUND INOPERATIVE. REPLACED BARRIER LIGHT ASSEMBLY AND BATTERY, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400766 19990924 00766 NM 1999 9 24 99ZZZM642 1 19990723 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY STROBE LIGHT WAS FOUND INOPERATIVE. REPLACED BARRIER LIGHT ASSEMBLY AND BATTERY, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400767 19990924 00767 NM 1999 9 24 ASAA9910226 1 19990723 A 3397 WIRE BOEING 737 737210C 1384459 NM ROWS 6/7 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 6 AND 7 WERE FOUND INOPERATIVE. REPLACED RECEIVER AND REPAIRED WIRING, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400768 19990924 00768 NM 1999 9 24 99ZZZM643 1 19990723 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM ROWS 6/7 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 6 AND 7 WERE FOUND INOPERATIVE. REPLACED RECEIVER AND REPAIRED WIRING, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400769 19990924 00769 NM 1999 9 24 ASAA9910225 1 19990722 A 3350 8821004 BATTERY PACKS BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 740AS 22578 ANC - PRIOR TO FLIGHT 41, SEVERAL EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACKS AS R EQUIRED AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999092400770 19990924 00770 CE 1999 9 24 MASA99145 1 19990822 A 3250 1148200313 DISCONNECT CAM BEECH 1900 1900D 1154162 CE NLG STEERING FAILED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 125YV UE125 FLT 5482 - BOS-MVY - WHEN PREPARING FOR LANDIN IN MVY, THE CREW REPORTED THEY RECEIVED NO DOWN AND LOCK INDICATION FOR T HE NOSE GEAR UPON GEAR EXTENSION. THE CREW RECYCLED THE GEAR BUT THE NOSE GEAR DID NOT EXTEND. THIS WAY CONFIRMED BY T HE TOWER. THE CREW THEN MANUALLY EXTENDED THE GEAR AND RECEIVED THREE GREEN DOWN AND LOCKED INDICATION. THE TOWER CONF IRMED THE NOSE GEAR WAS DOWN AND INDICATED THAT THE NOSE TIRE WAS TURNED TO THE RIGHT APPROXIMATELY 90 DEGREES. THE CRE W DECIDED TO RETURN TO BOS WHERE THEY DECLARED EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND DEPLANED ON THE RUNWAY. MAINTENANCE REPLACED THE NOSE GEAR CENTERING CAM. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 1999092400771 19990924 00771 CE 1999 9 24 MASA99148 1 19990824 A 3230 1148200773 BRACKET BEECH 1900 1900D 1154162 CE NLG JAMMED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 125YV UE125 FLT 5384 - BOS-PQI - DURING PREPARATION FOR LANDING IN PQI, THE CREW RECEIVED A GEAR UNSAFE INDICATION. THE AIRCRAFT DI VERTED TO BGR WHERE THEY DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BOLT LODGED BETWEEN THE DOWNLOCK SWITCH AND THE SWITCH CONTACT BRACKET. MAINTENANCE REPLACED THE DRAG BRACE DOWNLOCK SWITCH BRACKET . OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999092400772 19990924 00772 EA 1999 9 24 MASA99135 1 19990723 A 5260 1015141933 LATCH CNDAIR CL600 CL6002B19 EA AIRSTAIR DOOR DIRTY A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 27173 7173 FLT 5124 - CMH-MDW - PRIOR TO DEPARTURE, THE CREW REPORTED THE CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE C LEANED AND LUBED THE DOOR ROTARY LATCH, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999092400773 19990924 00773 EA 1999 9 24 MASA99136 1 19990726 A 5260 10151403021 LATCH CNDAIR CL600 CL6002B19 EA AIRSTAIR DOOR DIRTY A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 47202 7202 FLT 5771 - CLT-LIT - PRIOR TO DEPARTURE, THE CREW REPORTED THAT THE AIRSTAIR DOOR WOULD NOT LOCK. MAINTENANCE CLEANED A ND LUBED THE UPPER LATCH ROLLER, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999092400774 19990924 00774 EA 1999 9 24 MASA99138 1 19990811 A 3230 864202 PROX SENSOR CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJUST A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77181 7181 FLT 6138 - PHX-MRY - AFTER DEPARTURE FROM PHX, THE CREW REPORTED THAT THE NOSE GAER WOULD NOT RETRACT. THE AIRCRAFT RET URNED TO THE FIELD. MAINTENANCE FOUND THAT THE NOSE PROXIMITY SENSOR HAD BEEN HIT BY A PUSH CART. MAINTENANCE READJUST ED THE PROXIMITY SENSOR, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999092400775 19990924 00775 NM 1999 9 24 USAA089906 1 19990823 A 3213 651765737 STRUT BOEING 727 727227 1384078 NM RT MLG FAILURE A USAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 926TS 20774 FLT 6511 - LGA-DCA - ON NORMAL LANDING IN DCA, AS EXITING RUNWAY 18 TAXIWAY F, ALTERNATING RED AND GREEN RIGHT MAIN GEAR DOOR LIGHTS INDICATION, PULSATING FELT THROUGH PLANE. RIGHT MAIN GEAR SIDE STRUT CAME APART DAMAGE BEING DETERMINED. R EPLACED RIGHT MLG SIDE STRUT ASSEMBLY. (M) 2 L 7 3 4F A3WE 1999092400776 19990924 00776 NM 1999 9 24 USAA089904 1 19990821 A 5260 F2523 CHAIN BOEING 727 727225 1384077 NM AFT AIRSTAIRS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918TS 20445 AFT AIRSTAIR EXIT DOOR HOLD-OPEN CHAIN BROKEN. INSTALLED NEW HOLD-OPEN CHAIN. (M) 2 L 7 3 4F A3WE 1999092400777 19990924 00777 NM 1999 9 24 USAA990865 1 19990728 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 294.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 VISUAL INSPECTION, FOUND A AREA OF CORROSION IN CLIPNUT HOLES T-CAP OF FLOORBEAM STATION 294.5, RBL 15- 52. CORROSION LEVEL 2. REPLACED T-CAP PER SRM 53-10-51 AND SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999092400778 19990924 00778 NM 1999 9 24 USAA990857 1 19990814 A 5512 SKIN BOEING 737 737401 1384701 NM HORIZ STABILIZER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30259 23990 CLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK LOWER SKIN RIGHT HORIZ STAB S TATION 96 TO 97.5, 1.25 INCH FORWARD OF AFT SPAR. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER TR 55-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999092400779 19990924 00779 NM 1999 9 24 USAA990856 1 19990814 A 5512 SKIN BOEING 737 737401 1384701 NM HORIZ STABILIZER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30259 23990 CLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.625 INCH CRACK LOWER SKIN RIGHT HORIZ STAB ILIZER STATION 124 TO STATION 125.6, 1.25 INCH FORWARD OF AFT SPAR. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLE R AND DOUBLER PER TR 55-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999092400780 19990924 00780 NM 1999 9 24 USAA990866 1 19990728 A 5320 Z-ANGLE BOEING 737 737401 1384701 NM BS 947-986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 30365 23987 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION AT NUTPLATE STATION 947-986.5, LBL 45 Z-ANGLE. CORR OSION LEVEL 2. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999092400781 19990924 00781 WP 1999 9 24 USAA990929 1 19990825 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 427-466 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 48741 48026 PIT - DURING Q1/C4 CHECK, FOUND CORROSION .020 DEEP AT LONGERON 296, STATION 427 TO 446, CORROSION TASK NR C51-53300, CO RROSION LEVEL 1. SPLICED IN NEW SECTION PER EA 52620 AND SRM 53-02 FIG 4. (M) 2 L 7 2 4F A6WE 1999092400782 19990924 00782 WP 1999 9 24 USAA990930 1 19990825 A 5320 CUSP DOUG DC9 DC981 3022081 WP BS 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 48741 48026 PIT - DURING Q1/C4 CHECK, FOUND HOLE IN CUSP MEMBRANE DUE TO CORROSION AT STATION 200, LEFT SIDE. CUSP MEMBRANE REPLACE D PER EA 52552 REV A. (M) 2 L 7 2 4F A6WE 1999092400783 19990924 00783 NE 1999 9 24 USAA089905 2 19990819 A 7230 COMPRESSOR BOEING 727 727227 1384078 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE STALLED A USAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 19 927TS 20837 653939 NR 2 ENGINE TOOK 12 SECONDS TO REACH 1.4 EPR AT WHICH TIME HAD TWO COMPRESSOR STALLS. WINDS LIGHT AND VARIABLE. TROUBL ESHOOTING IN PROGRESS. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999092400784 19990924 00784 NM 1999 9 24 USAASB99204 1 19990818 A 2913 6507506 PUMP BOEING 737 7374B7 1384702 NM NR 1 ENGINE FAILED A USAA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 EA 19 446US 5137 24873 CLT - FLT 806 - EN ROUTE FROM FLL-CLT, THE SYSTEM 'A' HYDRAULIC QTY INDICATOR DROPPED TO .25 INDICATION. F/O CONFIRMED VISUALLY A LEAK OFF THE LEFT WING NEAR THE ENGINE AND FLAP. THE NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINAT ED FOLLOWED SHORTLY BY SYSTEM 'A' HYDRAULIC QTY DECREASING TO ZERO. TOTAL LOSS OF SYSTEM 'A' HYDRAULIC PRESSURE DID NOT OCCUR. CREW ELECTED TO CONTINUE FLIGHT TO CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE UNDER IT S OWN POWER. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED. REMOVED A ND REPLACED SAME PER MM 29-15-12. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999092400785 19990924 00785 WP 1999 9 24 USAAD99115 1 19990815 A 2131 10256852 CONTROLLER DOUG DC9 DC931 3022065 WP COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 932VJ 38659 47189 PIT - ITH - FLT 1572 - AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PRESSURIZATION CONTROLLER. (M) 2 L 7 2 4F A6WE 1999092400786 19990924 00786 WP 1999 9 24 USAAD99116 1 19990818 A 2150 39271411 VALVE DOUG DC9 DC982 3022082 WP CABIN FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 825US 47803 49237 CLT-CMH - FLT 8003, THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF AND THE FLOW LIGHT WAS ON CONTINUOUSLY. THE AIRCRAF T RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING PRESSURE REGULATOR VALVE AND REPLACED THE CLAMPS ON A LOOSE DUCT ON THE RIGHT HEAT EXCHANGER. (M) 2 L 7 2 4F A6WE 1999092400787 19990924 00787 NM 1999 9 24 USAASB99212 1 19990828 A 2910 BACH8A06NN0263T LINE BOEING 737 737201 1384454 NM NLG FAILED A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 233US 22273 MCO FLT 2692 - SHORTLY AFTER TAKEOFF FROM MCO, AFTER GEAR AND FLAP RETRACTION, THE 'A' HYDRAULIC SYSTEM LOW PRESSURE LIG HT AND MASTER CAUTION LIGHT FLICKERED. HYDRAULIC QUANTITY RAPIDLY WENT TO ZERO. AIRCRAFT LEVELED OFF AT 5,000 FEET AS CREW ACCOMPLISHED CHECKLIST. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT MCO. FLIGHT LANDED WITHOUT INCIDENT B UT HAD TO BE TOWED TO THE GATE. MAINTENANCE FOUND THE NLG ACTUATOR LINE TO BE AT FAULT. REPLACED SAME. DUE TO HYDRAUL IC LOSS, MAINTENANCE ALSO REMOVED AND REPLACED BOTH ENGINE DRIVEN HYDRAULIC PUMPS AND FILTERS. SERVICED HYDRAULIC SYSTE M. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999092400788 19990924 00788 NM 1999 9 24 USAASB99213 1 19990828 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 284AU 23131 BWI - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE B ATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999092400789 19990924 00789 NM 1999 9 24 USAASB99214 1 19990829 A 3260 405FW504B CIRCUIT CARD BOEING 737 737401 1384701 NM NLG FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 412US 23881 IND - FLT 696 - AS LANDING GEAR WAS LOWERED IN PREPARATION FOR LANDING AT IND, THE CREW RECEIVED A NOSE GEAR UNSAFE LIGH T. CREW RECYCLED THE LANDING GEAR THREE TIMES AND ACCOMPLISHED A TOWER FLYBY. TOWER STATED NOSE WHEEL LOOKED DOWN BUT CAPTAIN CHECKED SCOPE AND GEAR DID NOT SEEM TO LINE UP. CREW CYCLED GEAR TWO MORE TIMES AND CHECKED SCOPE AGAIN. GEAR AGAIN DID NOT SEEM TO LINE UP. AFTER SECOND FLYBY, GEAR LOOKED DOWN AGAIN, BUT STILL HAD UNSAFE LIGHT. CREW DECLARED A N EMERGENCY AND THE CABIN WAS PREPPED FOR AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE NOSE GEAR WAS PINN ED AND THE AIRCRAFT TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE M1215 AND M1214 (P/N 8-060-02) PRINTED CIR 2 L 7 2 4F RT A16WE 1999092400790 19990924 00790 WP 1999 9 24 USAAD99117 1 19990819 A 3350 408822101 BATTERY DOUG DC9 DC981 3022081 WP ROW 13-18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 804US 48052 ROC - THE CEILING EMERGENCY LIGHTS AT ROWS 13 TO 18 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIE S. (M) 2 L 7 2 4F A6WE 1999092400791 19990924 00791 WP 1999 9 24 USAADD99114 1 19990817 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 973VJ 47099 IND - THE MAIN ENTRANCE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999092400792 19990924 00792 WP 1999 9 24 USAAD99112 1 19990814 A 3350 P4100020 BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 958VJ 47351 IND - THE MAIN ENTRANCE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999092400793 19990924 00793 WP 1999 9 24 USAAD99113 1 19990815 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 983VJ 48159 IND - ONE SECTION OF THE CEILING EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999092400794 19990924 00794 1999 9 24 RAIA990834 4 19990826 A 3442 MI5853505 RADAR R/T AEROSP ATR72 ATR72202 8680940 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 722TE 220 FLT 7406 - STL - WEATHER RADAR POPS C/B. MAINTENANCE REPLACED RADAR TRANCEIVER. (M) 2 H 7 2 4T RT A53EU 1999092400795 19990924 00795 1999 9 24 RAIA990835 3 19990826 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 429AM 879 FLT 7478 - STL - RIGHT BETA LIGHT FLICKERS. MAINTENANCE REPLACED SEAT SWITCH ON RIGHT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999092400796 19990924 00796 1999 9 24 RAIA99836 4 19990830 A 2330 M7850B CHIME UNIT BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 427AM 876 FLT 7472 - STL - BOTH CCS C/B POPPED DURNIG TAXI WHEN TAXI LIGHT IS ON. MAINTENANCE REPLACED CHIME UNIT. (M) 2 L 7 2 4T RT A56EU 1999092400797 19990924 00797 EU 1999 9 24 RAIA990837 1 19990824 A 2612 S5411060301551 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU NR 2 ENGINE LOOSE A RAIA E ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 CE 03 422TE 106 FLT 7140 - STL - NR 2 ENGINE FIRE INDICATION, SHUT DOWN ENGINE. MAINTENANCE TIGHTENED LOOSE CONNECTION ON LOWER COWLING . (M) 2 H 7 2 4T RT A53EU 1999092400798 19990924 00798 EU 1999 9 24 RAIA990838 1 19990807 A 2844 1103P0645 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT FUEL SYSTEM FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 436AM 891 FLT 7468 - STL - RIGHT FUEL CAP LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT FUEL PRESS SWITCH. (M) 2 L 7 2 4T RT A56EU 1999092400799 19990924 00799 EU 1999 9 24 RAIA990839 1 19990812 A 3610 6411343 SWITCH AEROSP ATR42 ATR42300 8680920 EU NR 1 BLEED SYS FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 424TE 124 FLT 7324 - STL - NR 1 BLEED FAULTED. MAINTENANCE REPLACED BLEED SWITCH. (M) 2 H 7 2 4T RT A53EU 1999092400800 19990924 00800 EU 1999 9 24 RAIA990840 1 19990819 A 7931 1241013 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 560HK 41076 FLT 7744 - DCA - LEFT ENGINE OIL PRESSURE GAUGE ERRATIC. MAINTENANCE REPLACED OIL PRESSURE TRANSDUCER ON LEFT ENGINE. ( M) 2 L 7 2 4T RT A41NM 1999092400801 19990924 00801 EU 1999 9 24 RAIA990828 1 19990820 A 2424 51539019E GCU JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 560HK 41076 FLT 7741 - JFK - RIGHT GENERATOR INOPERATIVE. MAINTENANCE REPLACED RIGHT GENERATOR CONTROL UNIT. (M) 2 L 7 2 4T RT A41NM 1999092400802 19990924 00802 WP 1999 9 24 RAIA990829 2 19990821 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA O OTHER Y ENGINE STOPPAGE CL CLIMB 1 CE 03 342TE 13850 954 66069 FLT 7361 - PAH - LEFT ENGINE FAILED SUDDENLY IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999092400803 19990924 00803 EU 1999 9 24 RAIA990830 1 19990824 A 7110 S5411060301551 COWL AEROSP ATR42 ATR42300 8680920 EU NR 2 ENGINE FAILED A RAIA E ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 CE 03 422TE 106 FLT 7011 - STL - NR 2 ENGINE FIRE INDICATION CAME ON, PERFORMED SHUTDOWN PROCEDURE AND FIRED BOTH BOTTLES. MAINTENANCE REPLACED NR 2 ENGINE LOWER COWL ASSY, WHICH INCLUDES FIRE LOOP ASSY AS PART OF COWL. (M) 2 H 7 2 4T RT A53EU 1999092400804 19990924 00804 1999 9 24 RAIA990831 4 19990825 A 3425 301A7M1 STANDBY ADI BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 340TE 939 FLT 7504 - STL - STANDBY ATTITUDE INDICATOR INOPERATIVE. MAINTENANCE REPLACED STANDBY ATTITUDE INDICATOR. (M) 2 L 7 2 4T RT A56EU 1999092400805 19990924 00805 EU 1999 9 24 RAIA990832 1 19990825 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 342TE 3390 954 RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED TORQUE SIGNAL CONDITIONER. (M) 2 L 7 2 4T RT A56EU 1999092400806 19990924 00806 1999 9 24 RAIA990833 4 19990825 A 6122 89741016 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 867AE 375 867 FLT 4718 - SMF - RIGHT BETA LIGHT ON DURING TAXI. MAINTENANCE REPLACED RIGHT PROP GOVERNOR. (M) 2 L 7 2 4T RT A56EU 1999092400807 19990924 00807 EU 1999 9 24 PLGA990810 1 19990810 A 2121 EVCTA465A FAN SAAB SF340 340B 7860101 EU RIGHT FAILED A PLGA D H RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS O OTHER TX TAXI/GRND HDL 1 NE 05 347BE 705 340B187 BOS - FLT 6447 - DURING TAXI OUT, CREW NOTED INTERMITTENT ODOR. SIMILAR TO BLEED OR FAN BURNING ODOR. F/A REPORTED SCR ATCHING NOISE NEAR WING ROOT. AIRCRAFT RETURNED TO GATE WERE MAINTENANCE DEFERRED THE RT RECIRC FAN ASSY. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400808 19990924 00808 EA 1999 9 24 MASA99131 1 19990809 A 3230 864202 PROX SENSOR CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJUST A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77181 7181 FLT 6162 - MAS-PHX - AFTER DEPARTURE FROM MAS, THE AIRCRAFT RETURNED TO THE FIELD DUE TO THE NOSE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND PROXIMITY SENSOR HAD BEEN BENT BY THE PUSH BACK CART. MAINTENANCE REPAIRED THE PROXIMITY S ENSOR. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999092400809 19990924 00809 CE 1999 9 24 MASA99130 1 19990808 A 5610 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE RT WINDSHIELD CRACKED A MASA K NONE O OTHER CR CRUISE 1 SW 07 132YV UE132 FLT 6494 - PHX-GYM - THE CAPTAIN REPORTED THAT THE F/O'S WINDSHIELD CRACKED IN FLIGHT. THE AIRCRAFT LANDED IN GYM WITHO UT INCIDENT. THE AIRCRAFT WAS FOUND TO BE AIRWORTH FOR FERRY TO FMN. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999092400810 19990924 00810 NM 1999 9 24 TSAA9933417 1 19990827 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK FOR BEING LOW. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999092400811 19990924 00811 NM 1999 9 24 TSAA9933418 1 19990829 A 3350 8731002511 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED FORWARD CENTER AISLE LIGHT EMERGENCY BATTERY DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999092400812 19990924 00812 NM 1999 9 24 TSAA9933419 1 19990828 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999092400813 19990924 00813 NM 1999 9 24 TSAA9933420 1 19990827 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999092400814 19990924 00814 WP 1999 9 24 GTIA9901061 1 19990809 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP ROW 1/2 DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 ROWS 1 AND 2 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-40 IAW 33-53-0. OPERATIONAL C HECKS GOOD. (M) 2 L 7 2 4F A6WE 1999092400815 19990924 00815 WP 1999 9 24 GTIA9901060 1 19990803 A 3350 BULB DOUG DC9 DC932 3022066 WP LT COCKPIT FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942ML 47478 LEFT COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BULB OPERATION CHECKED GOOD IAW 33-50-DC-9 MAINTENANCE MANUAL. (M) 2 L 7 2 4F A6WE 1999092400816 19990924 00816 WP 1999 9 24 GTIA9901059 1 19990803 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-40 IAW MM CHAPTER 33-53-0. OPERATI ON CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1999092400817 19990924 00817 WP 1999 9 24 GTIA9900976 1 19990510 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1370 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 MHV - STATION 1370 RIGHT LONGERON 18 OUTBOARD CUSP ANGLE HAS EXFOLIATION AT LAV FLOOR ATTACH HOLE. REMOVED DAMAGED CUSP ANGLE FABRICATED REPAIR PARTS FROM S2777976 QQA20013F 202473 EXTRUSION TREATED AND PRIMED REPAIR PARTS IAW SRM MD80 53- 05 FIG 25. INSTALLED FILLER AND SPLICES IAW MD80 SRM 53-05 FIG 25. (M) 2 L 7 2 4F A6WE 1999092400818 19990924 00818 WP 1999 9 24 GTIA9900975 1 19990516 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1129 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 MHV - AFT CABIN GH LAB STATION Y1129 LBL 60 FLOOR SUPPORT PLATE 1 LAF CORRODED BEYOND LIMITS. FABRICATED NEW FLOOR SUPP ORT PLATE AND INSTALLED IAW MD80 SRM 51-01 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1999092400819 19990924 00819 WP 1999 9 24 GTIA9900969 1 19990514 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 MHV - STATION 1155 LBL 25-38 APPROX CORROSION TOP AND BOTTOM OF TOP CAP NEAR GALLEY SERVICE DOOR THRESHOLD. REMOVED TOP CAP STATION 1155 ORDERED NEW PART P/N 5930544-97. REINSTALLED PART IAW SRM MD80 51-30-2 LOCATED AND DRILLED PART SRM MD80 51-10-4. (M) 2 L 7 2 4F A6WE 1999092400820 19990924 00820 WP 1999 9 24 GTIA9900905 1 19990204 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 211 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 FS 211 R61 WEB AT 1.5 INCH LIGHTNING HOLE FORWARD OF OVAL DUCT IS CRACKED AT RIVET SIDEWALL AREA AFT OF FORWARD GALLEY D OOR. REPAIR OF WEB WILL BE ACCOMPLISHED ON A066C03W258 INSTALLATION OF 2 ANGLE AND OVAL DOCT TO BE INSTALLED ON A066S03 W255. (M) 2 L 7 2 4F A6WE 1999092400821 19990924 00821 WP 1999 9 24 GTIA9900884 1 19990201 A 5755 SKIN DOUG DC9 DC932 3022066 WP LT SPOILER DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 13512 48111 LEFT WING UPPER SURFACE OUTBOARD SPOILER IS DELAMINATED AT UPPER INBOARD SECTION APPROX 6 INCH BY 5 INCH OF DELAM ON PAR T RACK. DELAMINATION AREA IS LARGER THAN ALLOWED LIMITS IN SRM REQUIRES OUTSIDE VENDOR REPAIR REMOVED AND REPLACED. (M ) 2 L 7 2 4F A6WE 1999092400822 19990924 00822 WP 1999 9 24 GTIA9900939 1 19990622 A 5754 SLAT DOUG DC9 DC932 3022066 WP NR 4 LE SLAT DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 EWR - LEFT WING HAS DAMAGED AREAS. NR 4 L/E SLAT. REMOVED AND REPLACED NR 4 L/E SLAT IAW DC-9 MM 27-80-1. (M) 2 L 7 2 4F A6WE 1999092400823 19990924 00823 1999 9 24 GTIA9901086 4 19990818 A 2565 1133106DME SLIDE DOUG DC9 DC931 3022065 WP L1 DOOR DEPLOYED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 6850 47326 L-1 DOOR SLIDE PACK FELL TO GROUND AND DEPLOYED. REPLACED L-1 DOOR SLIDE PACK IAW DC-9 MM 25-61-00. (M) 2 L 7 2 4F A6WE 1999092400824 19990924 00824 WP 1999 9 24 GTIA9901087 1 19990821 A 2560 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR DETACHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 132NK 47202 GALLEY SERVICE DOOR SLIDE PACK WAS FOUND LAYING ON GALLEY FLOOR. NEEDS TO BE REPLACED. REINSTALLED GALLEY SERVICE DOOR SLIDE PACK IAW DC9 MM 25-61-00. (M) 2 L 7 2 4F A6WE 1999092400825 19990924 00825 NM 1999 9 24 GTIA99128 1 19990828 A 3610 6526663978 DUCT BOEING 727 727223 1384074 NM NR 3 PYLON LEAKING A GAIA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 07 858AA 21085 FLT 718 - ENCOUNTERED DURING CRUISE FROM TOL TO OMA, NR 3 STRUT OVERHEAT LIGHT WITH THE BLEED OFF AND ENGINE AT IDLE. T HE AIRCRAFT CONTINUED TO OMA AND LANDED AT OMA WITHOUT ANY FURTHER DIFFICULTIES. CONFIRMED LEAKAGE AT DUCT AND COUPLING IN THE NR 3 PYLON. REMOVED AND REPLACED COUPLING, DUCT AND RETAINER. LEAK CHECKED ENGINE AT IDLE AND FULL POWER WITH NO OVERHEAT LIGHT INDICATION AND NO FURTHER LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999092400826 19990924 00826 NM 1999 9 24 GAIA99127 1 19990828 A 3610 SEALS BOEING 727 727223 1384074 NM NR 3 PYLON LEAKING A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 858AA 21085 FLT 509 - ENCOUNTERED ON CLIMB-OUT FROM MEM TO TOL, NR 3 STRUT OVERHEAT LIGHT WITH THE BLEED OFF AND ENGINE AT IDLE. TH E AIRCRAFT CONTINUED TO TOL AND LANDED AT TOL WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED BLOWN FIREWALL SEA L GASKETS AT THE 13TH STAGE BLEED AIR DUCT. ALSO, REPLACED SEALS ON THE ANTI-ICE VALVE. ALL DUCTS IN NR 3 ENGINE STRUT LEAKS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999092400827 19990924 00827 WP 1999 9 24 USAA990890 1 19990819 A 5280 5936404504 HINGE DOUG DC9 DC982 3022082 WP RT MLG DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 47144 49119 PIT - DURING C2 CHECK, FOUND HINGE LUG BROKEN, RIGHT MLG DOOR. REPLACED WITH IDENTICAL PART PER DOUGLAS DRAWING SR09520 022. (M) 2 L 7 2 4F A6WE 1999092400828 19990924 00828 WP 1999 9 24 USAA990892 1 19990819 A 5280 5930583192 PAN DOUG DC9 DC982 3022082 WP RT MLG DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 47144 49119 PIT - DURING C2 CHECK, FOUND CRACK 1.5 INCH LONG AT RT MAIN LANDING GEAR DOOR FORWARD INBOARD CORNER OF PAN. INSTALLED FACTORY DOUBLER J06020038 PER SRM 52-05 FIG 28. (M) 2 L 7 2 4F A6WE 1999092400829 19990924 00829 WP 1999 9 24 USAA990891 1 19990819 A 5280 5930583186 RIB DOUG DC9 DC982 3022082 WP RT MLG DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 47144 49119 PIT - DURING C2 CHECK, FOUND 3.5 CRACK IN RT MLG DOOR OUTER SKIN AT GROUND SKID RIB FRAME 4/5, NR 4 RIB CRACKED. INSTAL LED TYPICAL REPAIR TO FRAME RIB NR 4 PER EA 52695. (M) 2 L 7 2 4F A6WE 1999092400830 19990924 00830 NE 1999 9 24 USAASB99200 2 19990812 A 7510 577957 FUEL BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 277AU 2917 22889 MCO - FLT 2666 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED AT REDUCED THRUS T. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 2 ENGINE FUEL HEAT UPPER MANIFOLD ASSEMBLY SEPARATED. DROPPED NR 2 ENGINE PER MM 71-00 FOR ACCESS. REMOVED AND REPLACED UPPER MANIFOLD ASSEMBLY. REINSTALLED NR 2 ENGINE. ENGINE RUN CHECKS NORMAL. NO LEAKS NOTED. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999092400831 19990924 00831 NM 1999 9 24 TSAA9957416 1 19990826 A 5720 658276415 BEAM BOEING 737 737282 13844AT NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 LEFT MLG BEAM CORRODED BEYOND LIMITS. REPLACED LEFT MLG BEAM (PERFORMED BY BOEING AOG TEAM). AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999092400832 19990924 00832 NM 1999 9 24 TSAA9952415 1 19990826 A 5210 65C2725730 FRAME BOEING 737 737282 13844AT NM PAX DOOR CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 FORWARD ENTRY DOOR FRAME CORRODED AT LWR AFT CORNER ABOVE DOOR SILL. REPAIRED IAW ECO 2992. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1999092400833 19990924 00833 SO 1999 9 24 C2XA99BT074 1 19990717 A 4920 4501968B APU EMB 145 EMB145LR SO AFT FUSELAGE SMOKING A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 13949 145057 EWR - FLT 4315 - CREW REPORTED APU CAUSED SMOKE ON GROUND WITH PACKS RUNNING, MAINTENANCE FOUND APU INOPERATIVE. PLACED APU ON MEL 49-00-00. AFTER MAINTENANCE TROUBLESHOOTING FOUND APU TO BE CAUSING THE SMOKE PROBLEM. REMOVED AND REPLACE D APU WITH SERVICEABLE UNIT. OPS CHECKED APU AND PACKS GOOD. (M) 2 L 7 2 4T RT T00011AT 1999092400834 19990924 00834 SO 1999 9 24 C2XA99BT073 1 19990718 A 4920 4501968B APU EMB 145 EMB145 SO AFT FUSELAGE SMOKING A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 14959 145091 SMOKE IN CABIN WITH PACK NR 2 OVERHEAT INDICATION. MAINTENANCE REMOVED AND REPLACED THE APU FOUND APU SOURCE OF SMOKE. OPS CHECKED OF APU AND PACK NR 2 GOOD. (M) 2 L 7 2 4F RT T00011AT 1999092400835 19990924 00835 SO 1999 9 24 C2XA99IA447 1 19990825 A 5315 FLOORBEAM EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14942 145037 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE P ERFORMED A DOUBLER REPAIR IAW EMBRAER145 FAX SST=1287/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400836 19990924 00836 SO 1999 9 24 C2XA99IA448 1 19990825 A 5530 14531597602 DRAG ANGLE EMB 145 EMB145 SO VERT STABILIZER CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14942 145037 IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER TO FUSELAGE RIGHT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHOR IZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400837 19990924 00837 SO 1999 9 24 C2XA99IA449 1 19990825 A 5530 14531597601 DRAG ANGLE EMB 145 EMB145 SO VERT STABILIZER CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14942 145037 IAH - DURING C-CEHCK INSPECTION, THE VERTICLE STABILIZER TO FUSELAGE LEFT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORI ZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400838 19990924 00838 SO 1999 9 24 C2XA99IA450 1 19990825 A 3350 3025101 BATTERY CHARGER EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14942 145037 IAH - DURING C-CHECK INSPECTION, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATAIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400839 19990924 00839 SO 1999 9 24 C2XA99IA451 1 19990824 A 7830 TY203905B ACTUATOR EMB 145 EMB145ER SO LT ENG TR UNIT MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION LD LANDING 1 SW 09 14943 145040 CRP - UPON LANDING AT CRP, THE CREW REPORTED ANR 1 ENGINE THRUST REVERSER DISAGREE MESSAGE ON THE EICAS. MAINTENANCE I NSPECTED THE AIRCRAFT AND FOUND THE NR 1 ENGINE UPPER THRUST REVERSER ACTUATOR ADJUSTABLE ROD END TO BE BROKEN. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED THRUST REVERSER ACTUATOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4F RT T00011AT 1999092400840 19990924 00840 EU 1999 9 24 C2XA99IA446 1 19990818 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17831 185 EFD - DURING MAINTENANCE INSPECTION, THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 1999092400841 19990924 00841 SO 1999 9 24 C2XA99CL071 1 19990806 A 2150 1173T030203 OVERTEMP SWITCH EMB 120 EMB120RT SO LT PACK FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17720 1260 120142 CLE - FLT 3147 - THE CREW REPORTED THAT AFTER TAKEOFF WHEN THE BLEED WAS OPENED THE T6 WENT ABOVE 816C. THE AIRCRAFT RET URNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK OVERHEAT SWITCH AND PERFORM ED OPERATIONAL CHECKS IAW EMB120 MM 21-50-04. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999092400842 19990924 00842 SO 1999 9 24 C2XA99CL109 1 19990828 A 2422 PC2511C INVERTER EMB 120 EMB120RT SO E/E COMPT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17728 3485 120182 FLT 3757 - THE CREW REPORTED, THE NR 1 INVERTER INOPERATIVE LIGHT ILLUMINATED AND THEY WERE UNABLE TO RESET IT. THE AIR CRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER IAW EMB120MM 2 4-20-01 OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999092400843 19990924 00843 SO 1999 9 24 C2XA99CL108 1 19990827 A 7830 TR UNIT EMB 145 EMB145 SO NR 2 ENGINE MALFUNCTIONED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 17928 145007 PVD - FLT 4043 - THE CREW REPORTED THE ENGINE NR 2 REV DISAGREE INDICATION ON TAKEOFF. THE AIRCRAFT RETURNED TO THE GAT E WITHOUT FURTHER INCIDENT. MAINTENANCE DEACTIVATED THE T/R IAW EMB145 MM 78-31-01 AND 78-33-01 AND RELEASED THE AIRCRA FT IAW MEL 78-34-00 CAT 'C' CONTROL NUMBER 184953. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400844 19990924 00844 SO 1999 9 24 C2XA99CL101 1 19990824 A 3350 LIGHT EMB 145 EMB145 SO EXTERNAL INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 MAINTENANCE REPORTED THAT THE AFT EXTERNAL EMERGENCY LIGHTS ARE NOT WORKING. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 33-50-00 CAT 'C' CONTROL NUMER 184927. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400845 19990924 00845 SO 1999 9 24 C2XA99CL102 1 19990824 A 2434 GENERATOR EMB 145 EMB145 SO NR 3 MALFUNCTIONED A C2XA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 09 17928 145007 CLE - FLT 4049 - THE CREW REPORTED THE NR 3 GENERATOR DROPPED OFF LINE NUMEROUS TIMES AFTER TAKEOFF. THE AIRCRAFT RETUR NED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 24-31-01 CAT 'C' CONTROL NUMBER 18 4935. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400846 19990924 00846 SO 1999 9 24 C2XA99CL103 1 19990824 A 2750 3635001001 BRAKE EMB 145 EMB145 SO TE FLAPS FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12957 145080 CLE - FLT 3973 - THE CREW REPORTED THEY GOT A FLAP FAIL CAUTION MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELA ND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT AND LEFT FLAP TRANSMISSION BRAKES IAW EMB145 MM 27-51-01, AND REMOVED AND REPLACED THE RIGHT FLAP FLEXIBLE SHAFT NR 5 IAW EMB145 MM 27, THE FLAP CONTROL SYSTEM OPS CHE CKED GOOD IAW EMB145 MM 27-51-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400847 19990924 00847 SO 1999 9 24 C2XA99CL104 1 19990825 A 7830 WARNING LIGHT EMB 145 EMB145 SO NR 2 TR ILLUMINATED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17928 145007 CLE - FLT 4030 - THE CREW REPORTED THE ENGINE NR 2 TR DISAGREE MESSAGE ILLUMINATED ON TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 78-34-00 CONTROL NUMBER 184939. THE AIR CRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999092400848 19990924 00848 SO 1999 9 24 C2XA99CL105 1 19990825 A 2120 AIR DIST EMB 120 EMB120RT SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 16723 120169 IND-CLE - FLT 3062 - THE CREW REPORTED THAT BOTH PACKS HAVE A BURNING SMELL ON THE GROUND. THE AIRCRAFT TAXIED TO THE G ATE WITHOUT FURTHER INCIDENT. MAINTENANCE RAN BOTH PACKS ON THE GROUND AND FOUND NO DEFECTS WITH THE SYSTEM IAW EMB120M M 21-50-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999092400849 19990924 00849 CE 1999 9 24 C2XA99CL106 1 19990826 A 7712 1143800653 INDICATOR BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 09 53545 243 UE185 CLE - FLT 3129 - THE CREW REPORTED THE RIGHT TQ DID NOT INCREASE OR RISE DURING TAKEOFF, IT WAS STUCK AT 300. THE AIRCR AFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT TQ INDICATOR IAW B1900D MM 7 7-10-00 OPERATIONAL CHECK WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999092400850 19990924 00850 SO 1999 9 24 C2XA99CL107 1 19990827 A 3350 CONNECTOR EMB 120 EMB120ER 3260203 SO CABIN LOOSE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 16718 120136 CLE-RDU - FLT 3085 - THE CREW REPORTED THE FLOOR EMEGENCY LIGHTS ARE OUT. THE AIRCRAFT WAS AT THE GATE. MAINTENANCE RE SECURED A CONNECTOR AND PERFORMED OPERATIONAL CHECKS, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999092400851 19990924 00851 EU 1999 9 24 C2XA99BT082 1 19990827 A 3260 141FL01D3 SWITCH AEROSP ATR42 ATR42300 8680920 EU NLG INTERMITTENT A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 09 16824 166 EWR - 4345 - CREW REPORTED LANDING GEAR SYSTEM NR 2 NOSEWHEEL UNLOCK LIGHT INTERMITTENTLY ILLUMINATED. MAINTENANCE REMO VED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX SWITCH. OPS CHECKED SYSTEM GOOD. RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999092400852 19990924 00852 NM 1999 9 24 EISA99152 1 19990806 A 2611 774001 DETECTOR BOEING 727 7272M7 138407S NM CABIN MALFUNCTIONED A EISA K NONE N FALSE WARNING AP APPROACH 1 SW 07 721RW 3181 21200 SMOKE DETECTOR ILLUMINATES ON APPROACH, CHECKED CABIN NO SIGN OF SMOKE. CLEARED MOISTURE OUT OF VACUUM TUBE AND TESTED SYSTEM IAW MM CHAPTER 26-17. OPS CHECK GOD. (M) 2 L 7 3 4F A3WE 1999092400853 19990924 00853 NM 1999 9 24 EISA99151 1 19990806 A 7931 795898013 OIL LINE BOEING 727 7272M7 138407S NM NR 2 ENGINE CHAFED A EISA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 721RW 21200 NR 2 ENGINE LOW OIL PRESSURE, LIGHT CAME ON. OIL QTY INDICATION DROPPING. SHUT DOWN ENGINE IN FLIGHT. RIGHT ENGINE OI L PRESSURE TRANSMITTER LINE CHAFFED. INSTALLED UNION. RAN ENGINE LEAK CHECKS GOOD. NO DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 1999092400854 19990924 00854 NM 1999 9 24 EISA99154 1 19990809 A 5320 ANGLE BOEING 727 72731 1384010 NM BS 344 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 240NE 18906 DURING ACCOMPLISHMENT OF ROUTINE 'B' CHECK WORKCARD, FOUND CORROSION UNDER FORWARD LAV FLOOR STATION 344. REMOVED CORRO SION FABRICATED AND INSTALLED ANGLE, SHIM AND FILLER PER SRM 53-10-8 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999092400855 19990924 00855 NM 1999 9 24 EISA99159 1 19990823 A 5610 5717644 WINDOW BOEING 727 72725 1384006 NM COCKPIT CRACKED A EISA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 290NE 18972 R2 WINDOW CRACKED. REMOVED AND REPLACED R-2 WINDOW, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999092400856 19990924 00856 NM 1999 9 24 EISA99160 1 19990825 A 2750 AV1JJ5101 BYPASS VALVE BOEING 727 727223 1384074 NM TE FLAPS DEFECTIVE A EISA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SW 07 311NE 19703 SPLIT FLAPS ON TAKEOFF. REMOVED AND REPLACED OUTBOARD FLAP. BYPASS VALVE AND ALT FLAP MASTER SWITCH. (M) 2 L 7 3 4F A3WE 1999092400857 19990924 00857 NM 1999 9 24 99ZZZM644 1 19990825 A 2750 H1010262 SWITCH BOEING 727 727223 1384074 NM TE FLAPS DEFECTIVE A EISA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SW 07 311NE 19703 SPLIT FLAPS ON TAKEOFF. REMOVED AND REPLACED OUTBOARD FLAP. BYPASS VALVE AND ALT FLAP MASTER SWITCH. (M) 2 L 7 3 4F A3WE 1999092400858 19990924 00858 NM 1999 9 24 EISA99157 1 19990821 A 2751 1812993 INDICATOR BOEING 727 727223 1384074 NM TE FLAPS DEFECTIVE A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 311NE 0390NH 19703 FLAPS LOCKED OUT. REMOVED AND REPLACED FLAP INDICATOR. OPS CHECK GOOD PER MM CHAPTER 27. (M) 2 L 7 3 4F A3WE 1999092400859 19990924 00859 NM 1999 9 24 EISA99141 1 19990629 A 3260 1030875 SWITCH BOEING 727 727225 1384077 NM MLG OUT OF ADJUST A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 352PA 120 20616 RIGHT MLG LIGHT (RED AND GREEN) CAME ON AT SAME TIME (FALSE INDICATOR) MLG UP AND LOCKED. ADJUSTED F/M MLG TARGET PLATE TO UPLOCK SWITCH. CYCLED UPLOCK MECHANISM. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999092400860 19990924 00860 NM 1999 9 24 EISA99162 1 19990830 A 2432 25582005 BATTERY BOEING 727 727223 1384074 NM BATT COMPT DISCHARGED A EISA K NONE O OTHER LD LANDING 1 SW 07 6813 19488 ON LANDING, APU FAILED TO START FOUND BATTERY VOLTAGE AT 4, BATTERY CHARGER C/B POPPED. BATTERY WARMS TO TOUCH. NOTICE D SMOKE IN COCKPIT. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER. (M) 2 L 7 3 4F A3WE 1999092400861 19990924 00861 WP 1999 9 24 ORJA99251 1 19990815 A 3350 BR9661105 BATTERY CHARGER DOUG DC9 DC982 3022082 WP ROW 12/14/15/17 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 SJC - EMERGENCY PATH LIGHTS OUT IN ROWS 12, 14, 15 AND 17. CHANGED BATTERY PACK FOR EMERGENCY PATH LIGHTS. OPS CHECK G OOD. (M) 2 L 7 2 4F A6WE 1999092400862 19990924 00862 WP 1999 9 24 ORJA99253 1 19990813 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP AFT AIRSTAIR DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 755RA 49727 RNO - EMERGENCY LIGHT BATTERY CHARGER BY AFT AIRSTAIR DOOR IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER 33-53- 00. (M) 2 L 7 2 4F RT A6WE 1999092400863 19990924 00863 WP 1999 9 24 ORJA99254 1 19990805 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 9 LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 RNO - E-PATH LIGHT AT SEAT 9D INOPERATIVE. RECONNECTED ELECTRICAL CONNECTORS. OPS NO WORK PER MM 33-53-01. (M) 2 L 7 2 4F RT A6WE 1999092400864 19990924 00864 WP 1999 9 24 ORJA99256 1 19990810 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 8D-11D DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 RNO - EMERGENCY LIGHTS INOPERATIVE AT SEAT 8D-11D. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD 33-53-00. (M) 2 L 7 2 4F RT A6WE 1999092400865 19990924 00865 WP 1999 9 24 ORJA99255 1 19990805 A 3350 6011779 POWER PACK DOUG DC9 DC983 3022083 WP ROW 20 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 RNO - EMERGENCY LIGHT POWRE PACK AT 20F INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK AT 20F AS REQUIRED OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999092400866 19990924 00866 EA 1999 9 24 MASA99139 1 19990816 A 3350 OL3071BPEGPL BULBS CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 FLT 5776 - CLT-LIT - DURING PREFLIGHT INSPECTION, MAINTENANCE FOUND SEVERAL ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED SEVERAL BULBS, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999092400867 19990924 00867 1999 9 24 MASA99141 4 19990817 A 6122 1223890373 GOVERNOR BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 132YV UE132 FLT 6461 - FMN-PHX - AFTER DEPARTURE FROM FMN, THE CREW REPORTED THAT BOTH PROPELLERS WOULD NOT EXCEED TO 1550 RPM. THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERSPEED GOVERNOR. ALSO, INSPECTED THE LE FT PROPELLER, NO DISCREPANCIES WERE NOTED. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999092400868 19990924 00868 WP 1999 9 24 HALA0000172 1 19990829 A 3230 ACTUATOR DOUG DC9 DC951 3022051 WP NLG FAILED A HALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 13 672MC 47661 FLT 162 - HNL - NOSE LANDING GEAR WOULD NOT EXTEND. CYCLED THREE TIMES. PULLED ALTERNATE GEAR EXTENSION LEVER, NOSE GE AR EXTENDED WITH NORMAL INDICATIONS. STOWED ALT LEVER. CHECKED NOSE GEAR COND AND SERVICE CHECK OK. REPLACED NOSE GEA R BUNGEE CYL PER MM 32-32-7, OPS AND LEAK CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999092400869 19990924 00869 NM 1999 9 24 GAIA99129 1 19990901 A 2611 LAMP BOEING 727 727251 138408H NM CARGO COMPT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278US 21157 DURING ROUTINE MAINTENANCE IN PHX, THE SMOKE DETECTOR NR 6 POSITION WOLD NOT TEST. REMOVED AND REPLACED THE NR 6 SMOKE DETECTOR TEST LAMP. OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999092400870 19990924 00870 NM 1999 9 24 GAIA99132 1 19990907 A 3350 1000679 BATTERIES BOEING 727 727251 138408H NM L1 DOOR DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 264US 19983 DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE INTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND R EPLACED THE EMERGENCY LIGHT BATTERY PACK AT THE FORWARD ENTRANCE DOOR. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999092400871 19990924 00871 NM 1999 9 24 GAIA99130 1 19990901 A 3610 CLAMP BOEING 727 727223 1384074 NM AFT FUSELAGE LOOSE A GAIA K NONE J M WARNING INDICATION OVER TEMP CR CRUISE 1 SW 07 855AA 20996 EN ROUTE FROM TOL-MSP, FLT 710, LOWER BODY OVERHEAT LIGHT BLINKED, THEN STAYED ON CONTINUOUSLY. PERFORMED CHECKLIST PRO CEDURES AND LIGHT WENT OUT WHEN NR 1 ENGINE BLEED VLV WAS TURNED OFF. AIRCRAFT MADE AN UNEVENTFULLY LANDING IN MSP. FO UND AIR LEAK ON LEFT SIDE OF AIRSTAIRS. ADJUSTED AND TIGHTENED CLAMP. NO ADDITIONAL LEAKS NOTED. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999092400872 19990924 00872 NM 1999 9 24 GAIA99131 1 19990906 A 3610 CLAMP BOEING 727 727223 1384074 NM AFT FUSELAGE LEAKING A GAIA K NONE M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 855AA 20996 EN ROUTE FROM STL-TOL, FLT 1721 - ON CLIMB-OUT, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED FLASHING THEN STEADY. THE LOWER AFT BODY OVERHEAT CHECKLIST PROCEDURES WERE PERFORMED. THE LIGHT WENT OUT WITH THE THROTTLE REDUCTION ON THE NR 1 ENGINE. AIRCRAFT MADE AN UNEVENTFUL LANDING IN TOL. REMOVED GILL LINER IN AFT BELLY, ALSO KEEL BEAM ACCESS PANEL. R AN ENGINES TO POWER FOR LEAK CHECK. FOUND SEVERAL CLAMPS IN KEEL BEAM AREA LEAKING. TIGHTENED CLAMPS AND RAN ENGINES. NO OTHER LEAKS WERE NOTED. BODY OVERHEAT LIGHT DID NOT ILLUMINATE. REINSTALLED GILL LINER AND ACCESS PANEL. PERFORME D MORE ENGINE RUNS TO POWER. OVERHEAT LIGHT DID NOT COME ON. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999092400873 19990924 00873 EU 1999 9 24 SIMA992391 1 19990827 A 3230 8P848430621 CONTROL VALVE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 386AE 1544 340B386 ABI - FLT 5251 - MAIN LANDING GEAR WOULD NOT EXTEND. HAD TO USE MANUAL OVERRIDE. REMOVED AND REPLACED LANDING GEAR CON TROL VALVE. LEAK AND FUNCTIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400874 19990924 00874 SO 1999 9 24 SIMA992383 1 19990826 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 611AE 145074 ORD - FLT 4233 - AFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT LOCATION NR 4. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 1999092400875 19990924 00875 EU 1999 9 24 SIMA992451 1 19990902 A 3350 MS274061 SWITCH SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 243AE 340B243 DFW - FLT 3553 - COCKPIT EMERGENCY ARM LIGHT SWITCH DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400876 19990924 00876 EU 1999 9 24 SIMA992421 1 19990830 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY FAILED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 353SB A4477 340B353 SBP - FLT 3319 - LAVATORY SMOKE WARNING LIGHT ILLUMINATED. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED LAV ATORY SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400877 19990924 00877 EU 1999 9 24 SIMA992411 1 19990829 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 254AE 18250 340B254 LCH - FLT 5324 - ALL EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED TWO EMERGENCY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400878 19990924 00878 EU 1999 9 24 99ZZZM645 1 19990829 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 254AE 17384 340B254 LCH - FLT 5324 - ALL EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED TWO EMERGENCY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999092400879 19990924 00879 NM 1999 9 24 99ZZZM646 1 19990428 A 3610 652244143 DUCT BOEING 727 72722C 138400F NM NR 2 ENGINE FAILED A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 428EX 19097 FLT 601 - IND - AT APPROXIMATELY 1000 FT, ALTITUDE AFTER TAKEOFF, NR 2 ENGINE, ENGINE PRESSURE RATION BEGAN TO DROP OFF. MOVING THROTTLE FELT STIFF. GOT NR 2 FIRE INDICATION. PERFORMED ENGINE FIRE CHECKLIST, NR 2 GENERATOR AND NR 2 ENGIN E APPROACH CHECKLIST. FOUND NR 2 ENGINE 13TH STAGE SADDLE DUCT BLOWN, REPLACED SAME. (M) 2 L 7 3 4F A3WE 1999092400880 19990924 00880 NM 1999 9 24 99ZZZM647 1 19990424 A 3040 CONTROLLER BOEING 727 72722C 138400F NM RT COCKPIT LOOSE A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 426EX 19089 FLT 704 - OUT OF JAX - DURING CLIMB-OUT THROUGH 16,000 FEET, HAD A STRONG SMELL OF ELECTRICAL WIRE BURNING. TURNED BACK TO JAX. JUST PRIOR TO LANDING, HAD RIGHT WINDOW OVERHEAT LIGHT ILLUMINATE. DUMPED 10,000 LBS OF FUEL TO LAND WITHIN W EIGHT LIMITS. FOUND PIN PUSHED BACK ON WINDOW HEAT CONTROLLER RE-SET PIN, WINDOW HEAT NORMAL, CLEANED DIRT AND DUST FRO M AREA, NO SIGN OF BURNED WIRES AND COULD NOT DUPLICATE. (M) 2 L 7 3 4F A3WE 1999092400881 19990924 00881 WP 1999 9 24 99ZZZM648 1 19990426 A 3350 110049 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 571SC 46645 FLT 007 - SFO - ON PREFLIGHT CHECK NUMEROUS EMERGENCY LIGHTS FAILED TO TEST IN FORWARD CABIN. RIGHT FLOOR LIGHTS AND SE VERAL DOOR AND FORWARD BULKHEAD LIGHTS. REPLACED FAULTY BATTERY POWER SUPPLY BOX. (M) 2 L 7 3 4F A22WE 1999092400882 19990924 00882 WP 1999 9 24 99ZZZM649 1 19990805 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 571SC 46645 FLT 9001 - SFO - FORWARD RIGHT PORTION OF ZONE 'A' EMERGENCY LIGHTS FLOOR AISLE INOPERATIVE. ISOLATED SHORT CIRCUIT EME RGENCY (FLOOR AISLE) LIGHTS OPERATION CHECKS NORMAL. (M) 2 L 7 3 4F A22WE 1999092400883 19990924 00883 NM 1999 9 24 99ZZZM650 1 19990817 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 29SW 21340 FLT 801 - ACY, ON DAILY SERVICE CHECK, MID CABIN CENTER AISLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A16WE 1999092400884 19990924 00884 NM 1999 9 24 99ZZZM651 1 19990901 A 2897 WIRE BOEING 757 7572G7 1384963 NM RT FUEL VLV DAMAGED A AWXA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 908AW 24233 GATE RETURN FOR NR 2 ENGINE FLAME OUT AFTER ONE MINUTE AFTER START. RT ENGINE VALVE AND SPAR VALVE LIGHT ILLUMINATED AN D EICAS MESSAGE. RT FUEL SPAR VLV AND RT ENGINE FUEL VLV DISPLAYED, WITH FUEL CONTROL SWITCH IN RUN. NO FUEL FLOW INDI CATED. REPAIR BAD WIRE ON PIN 2 OF RT WING SPAR VALVE CANNON PLUT. OPS CHECKED GOOD ON ENGINE RUNS AT THIS TIME (WIRE WAS BARE AND BROKEN INSIDE PER MECHANIC). (M) 2 L 7 2 4F RT A2NM 1999092400885 19990924 00885 WP 1999 9 24 FJT99089211 2 19990813 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT FAILED A FJTA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 03 921AE 921 P66236C MWCR - FLT CREW REPORTED 20 MINUTES FROM DESTINATIN AIRPORT MWRC, THE RIGHT ENGINE EXPERIENCED LOSS OF OIL PRESSURE. VE RIFIED BY BOTH THE INDICATOR READING OF ZERO AN THE ILLUMINATION OF THE LOW OIL PRESSURE WARNING LIGHT. THE RIGHT ENGIN E WAS SECURED AND AN UNEVENTFUL LANDING ACCOMPLISHED. INVESTIGATION REVEALED THE OIL FILTER CONTAINED METAL AND A TEST OF THE CHIP DETECTOR REVEALED THAT METAL WAS PRESENT. THE ENGINE WAS REMOVED AND REPLACED WITH A SERVICEABLE ENGINE. ( M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999092400886 19990924 00886 EU 1999 9 24 A6WA9900091 1 19990803 A 2760 HC921G0451000 CIRCUIT BREAKER BAG BAE146 BAE146200A 1500266 EU AIRBRAKES FAILED A A6WA K NONE N FALSE WARNING DE DESCENT 1 GL 31 183US 150 E2043 UNCOMMANDED AIRBRAKE OPERATION INTERMITTENTLY. REMOVED AND REPLACED AIRBRAKE CONTROL PC BOARD. (M) 2 H 7 4 4F RT A49EU 1999092400887 19990924 00887 NM 1999 9 24 A6WA9900092 1 19990805 A 5270 CONNECTOR DORNER DO32 DO328100 2996000 NM AC COMPT LOOSE A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 328MX 3071 FLT 7057 - DEN - ON CLIMB-OUT, DOORS PAGE CAME UP SHOWING A/C DOOR OPEN. RESECURED A/C DOOR, FOUND A/C PLUG LOOSE. RES ECURED PLUG, DOOR WAS NOT OPEN ON LANDING. (M) 2 H 7 2 4T RT A45NM 1999092400888 19990924 00888 EU 1999 9 24 A6WA9900098 1 19990827 A 2910 SA7670006122 HYD LINE BAG BAE146 BAE146200A 1500266 EU LT MLG CRACKED A A6WA K NONE K FLUID LOSS CR CRUISE 1 GL 31 183US E2043 EN ROUTE TO DEN FROM RAP, OBSERVED HYDRAULIC LOOKUP, FOLLOWED BY GREEN SYSTEM LOW PSI AND LOW QTY LIGHTS. C/W ABNORMAL CHECKLIST ITEMS. REMOVED AND REPLACED MLG RETURN LINE FROM THE LT MLG RETRACTION JACK TO THE MANIFOLD. OPS AND LEAK CH ECK GOOD. (M) 2 H 7 4 4F RT A49EU 1999092400889 19990924 00889 NM 1999 9 24 A6WA9900097 1 19990824 A 7931 APS3D1000100DA SWITCH DORNER DO32 DO328100 2996000 NM LT OIL PRESSURE FAILED A A6WA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 31 335PH 3013 FLT 9500 - COS-DIV - EN ROUTE NOTICED LEFT OIL PRESSURE IN AMBER RANGE, SYSTEM PAGE INDICATED 66 PSI. FOLLOWED CHECKLIS T AND FEATHERED PROP, PRESSURE REMAINED AT 66 PSI AND PROP OIL PRESSURE CAS MESSAGE ILLUMINATED, FOLLOWED CHECKLIST AND SECURED ENGINE. REMOVED AND REPLACED OIL PRESSURE SWITCH, OPS AND LEAK CHECK GOOD IAW JIC. (M) 2 H 7 2 4T RT A45NM 1999092400890 19990924 00890 EU 1999 9 24 A6WA9900096 1 19990816 A 2120 AIR DIST BAG BAE146 BAE146200A 1500266 EU CABIN ODOR A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 608AW E2049 CAUSTIC FUMES IN CABIN WITH BLEED AIR SUPPLYING PACKS, NO NOTICEABLE ON APU AIR. PERFORMED PACK BURNOUT PER MM. RAN PA CKS WITH ENGINE AIR, NO NOTICEABLE SMELL. (M) 2 H 7 4 4F RT A49EU 1999092400891 19990924 00891 EA 1999 9 24 ASOA99056 1 19990629 A 3246 50105712 WHEEL CNDAIR CL600 CL6002B19 EA MLG DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 825AS 7207 MAIN WHEEL SUB-ASSEMBLY FOUND CRACKED AT TIRE CHANGE. THIS IS A NEW AIRCRAFT APPROXIMATELY 1200 CYCLES ON WHEEL ASSY. M AINTENANCE REPLACED THE MAIN WHEEL ASSY, P/N 5010571-1 AND S/N MAR98-1715, REMOVED FROM THE LEFT INBOARD POSITION. MAIN TENANCE IS CURRENTLY WAITING ON REPLACEMENT PART FROM A/C BRAKING SYSTEMS (WHEEL TIRE DIVISION). (M) 2 L 7 2 4F RT A21EA 1999092400892 19990924 00892 WP 1999 9 24 ARWA990903 1 19990910 A 7931 42D4910 SWITCH DOUG DC8 DC863F 302198F WP NR 3 ENGINE FAILED A ARWA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 19 441J 624 45988 PTY - FLT 618 - NR 3 ENGINE OIL QTY DOWN TO 1 GALLON. DIVERTED TO MPTO. LANDED WITH NO FURTHER INCIDENT. FOUND LEAK. REMOVED AND REPLACED DIFFERENTIAL PRESS SWITCH IAW 79-31-00. NO LEAKS NOTED. (M) 2 L 7 4 4F 4A25 1999092400893 19990924 00893 SW 1999 9 24 99ZZZM652 1 19990816 A 2910 2781032081 HYD LINE SWRNGN SA227 SA227AC 8780603 SW NLG CRACKED A MEJA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 17 366AE AC681 AFTER DEPARTURE FROM SLU, THE CAPTAIN'S NOSE GEAR LIGHT REMAINED ILLUMINATED AFTER CYCLING THE GEAR. THE CREW CYCLED TH E GEAR AGAIN AND THE AIRCRAFT LOST ALL HYDRAULIC POWER. THE A/C RETURNED TO SLU WITH THE GEAR STILL IN THE DOWN POSITIO N. MAINTENANCE REMOVED AND REPLACED THE RIGHT HYDRAULIC PUMP WITH A CONTINUED TIME ITEM. OPERATION CHECK FOR THE HYDRA ULIC PUMP WAS GOOD, BUT UPON GEAR RETRACTION, THE NOSE GEAR DOORS WOULD NOT CLOSE. AIRCRAFT WAS FERRIED TO SJU WITH THE LANDING GEAR DOWN. MAINTENANCE REPLACED THE NOSE LANDING GEAR UP LINE AND PERFORMED A GEAR RETRACTION CHECK. THE OPER ATIONS CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1999092400894 19990924 00894 NM 1999 9 24 P2EA99227 1 19990828 A 2750 MECHANISM BOEING 737 737205 NM TE FLAPS OUT OF ADJUST A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PIT - FLT 422 - NO EMERGENCY DECLARED, LANDING NORMAL. STRONG VIBRATION NOTED IN MID CABIN WHEN FLAPS EXTENDED FOR LAND ING. ADJUSTED LEFT TRAILING EDGE AFT FLAP PER MM 27-51-12, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999092400895 19990924 00895 NM 1999 9 24 AALA991228 1 19990819 A 2530 8609010000 OVEN BOEING 767 767223 1385123 NM CABIN DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 338AA 22335 LHR - FLT 142 - NR 2 GALLEY OVEN SMOKES WHEN HEATED. OVEN DEACTIVATED AND FLIGHT LANDED LHR WITHOUT INCIDENT. CLEANED RESIDUAL FOOD FROM OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999092400896 19990924 00896 NM 1999 9 24 AALA991234 1 19990819 A 2612 CONNECTOR BOEING 767 767323 1385205 NM RT ENGINE BROKEN A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 355AA 24036 MIA-GRU - FLT 921 - DURNG CLIMB-OUT, RIGHT ENGIE FIRE LOOP NR 2 OVERHEAT LIGHT ILUMINATED. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPAIRED BROKEN CONNECTOR AT NR 2 FIRE LOOP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999092400897 19990924 00897 NM 1999 9 24 AALA991218 1 19990730 A 2120 AIR DIST BOEING 767 767323 1385205 NM CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 390AA 27450 LAX-JFK - FLT 200 - ELECTRICAL BURNING SMELL NOTED IN CABIN. SMELL DISSIPATED BUT RETURNED WHEN GEAR LOWERED UPON RETUR N TO LAX. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED WHEEL WELLS, BRAKES, AIR CONDITIONING PACKS AND APU COMPARTMENT WITH NO FAULTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999092400898 19990924 00898 NM 1999 9 24 AALA991265 1 19990823 A 3240 S274T6105 FITTING BOEING 767 767323 1385205 NM NR 1 BRAKE DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7375A 25202 GRU - FLT 998 - UPON LANDING AT GRU FROM MVD, NR 1 MAIN LANDING GEAR TIRE BLOWOUT. REPLACED NR 1 WHEEL AND TIRE ASSY AN D ADJACENT NR 2 MAIN WHEEL AND TIRE ASSY. NR 1 BRAKE SEIZED DURING TEST AFTER WHEEL AND TIRE REPLACEMENT. REPLACED FAU LTY HYDRAULC FLUID QUICK DISCONNECT VALVE TO NR 1 BRAKE AND PRECAUTIONARY REPLACEMENT OF NR 1 BRAKE ASSEMBLY. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999092400899 19990924 00899 NM 1999 9 24 AALA991225 1 19990818 A 2841 HG1057ER03 PROCESSOR UNIT BOEING 767 767223 1385123 NM E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 320AA J002601 22321 DFW - FLT 947 - AFTER TAKEOFF DFW, LIM RIGHT FUEL QTY INDICATOR INDICATED 2000 TO 2500 LBS GREATER THAN LEFT FUEL QTY IN DICATOR. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FUEL QTY PROCESSOR UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999092400900 19990924 00900 NM 1999 9 24 AALA991126 1 19990801 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT STAIRWELL DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843AA 2176 20984 DFW - DURNG OVERNIGHT MAINTENANCE, AFT STAIRWELL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIRWELL EMERGENCY EXI T LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400901 19990924 00901 NM 1999 9 24 AALA991111 1 19990729 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 731AA 20738 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS IN CABIN MID SECTION INOPERATIVE. REPLACE D WIRING TO EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 3 4F A3WE 1999092400902 19990924 00902 EU 1999 9 24 AALA991123 1 19990731 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1425A 11408 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE TO LEFT AFT OVERW ING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999092400903 19990924 00903 EU 1999 9 24 AALA991059 1 19990720 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1444N 11447 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIPS MID CABIN INOPERATIVE. REPAIRED A SHORTED WI RE CONNECTED TO THE EMERGENCY EXIT FLOOR PATH LIGHT STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999092400904 19990924 00904 EU 1999 9 24 AALA991060 1 19990719 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1455K 11467 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FORWARD ENTRY DOOR FLOOR PATH LIGHTS BETWEEN GALLEY AND FIRST CLASS S ECTION INOPERATIVE. RESECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999092400905 19990924 00905 EU 1999 9 24 AALA991049 1 19990716 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1464A 11490 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIPS FROM ROW 15 AFT INOPERATIVE. REPAIRED SEVERA L WIRES ON EMERGENCY EXIT FLOOR PATH LIGHT STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999092400906 19990924 00906 WP 1999 9 24 AALA991217 1 19990818 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 12D/26D DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 DFW DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEATS 12D AND 26D INOPERATIVE. REPLACED EMER GENCY EXIT FLOOR PATH LIGHT STRIP AT SEATS 12D AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400907 19990924 00907 WP 1999 9 24 AALA991232 1 19990819 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 14D BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 576AA 53153 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED PATHWAY LIGHTS AT SEAT ROW 14D/E/F INOPERATIVE. REPAIRE D WIRING TO EMERGENCY EXIT SEAT MOUNTED PATHWAY LIGHTS AT SEAT ROW 14D/E/F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 1999092400908 19990924 00908 WP 1999 9 24 AALA991221 1 19990818 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L1 DOORWAY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR L-1 EMERGENCY WALK AROUND LIGHT INOPERATIVE. REPLACED FORWARD EN TRY DOOR L-1 EMERGENCY WALK AROUND LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400909 19990924 00909 WP 1999 9 24 AALA991256 1 19990823 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 274AA 49271 DFW - DURING OVERNIGHT MAINTENANCE, AFT FLIGHT ATTENDANT EMERGENCY WALK AROUND LIGHT HAD BROKEN BASE. REPLACED AFT FLIG HT ATTENDANT EMERGENCY WALK AROUND LIGHT. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400910 19990924 00910 WP 1999 9 24 AALA991244 1 19990821 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7512A 49806 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FORWARD GALLEY INOPERATIVE. REPAIR ED WIRING TO EMERGENCY FLOOR PATH LIGHTING STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400911 19990924 00911 WP 1999 9 24 AALA991170 1 19990813 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP AIRSTAIR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 591AA 53254 DFW - DURING OVERNIGHT MAINTENANCE, AIRSTAIRS LEFT SIDE PANEL EMERGENCY LIGHT NOPERATIVE. REPLACED AIRSTAIRS LEFT SIDE PANEL EMERGENCY LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999092400912 19990924 00912 WP 1999 9 24 AALA991158 1 19990810 A 3350 LIGHT DOUG DC9 DC983 3022083 WP STAIRWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 569AA 49351 ORD - DURING OVERNIGHT MAINTENANCE, AFT VENTRAL STAIRWAY FORWARD EMERGENCY EXIT LIGHT ASSY BROKEN. REPLACED AFT VENTRAL STAIRWAY FORWARD EMERGENCY EXIT LIGHT ASSY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999092400913 19990924 00913 WP 1999 9 24 AALA991194 1 19990816 A 3350 BULB DOUG DC9 DC982 3022082 WP ROW 21 SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 236AA 49251 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 21 AFT INOPERATIVE. REPLACED EMERGENCY EX IT LIGHT BULBS AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400914 19990924 00914 WP 1999 9 24 AALA991195 1 19990816 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L1 DOORWAY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 224AA 49174 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT WALK AROUND LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT WA LK AROUND LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400915 19990924 00915 WP 1999 9 24 AALA991196 1 19990816 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 578AA 53155 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDE WALL MARKER LIGHT CONNECTORS ON AFT STAIRWAY BURNED. REPLACED C ONNECTORS TO EMERGENCY EXIT SIDE WALL MARKER LIGHTS ON AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400916 19990924 00916 WP 1999 9 24 AALA991202 1 19990818 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 21D BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 245AA 49257 DFW - FLT 521 - AFTER ARRIVAL DFW FROM MCI, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 21D BROKEN. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT STRIP AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400917 19990924 00917 WP 1999 9 24 AALA991206 1 19990816 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1474 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - VERTICAL TO FUSELAGE LEFT ATTACH ANGLE IS CRACKED AT STATION 1474. INSTALLED DOUBLER ON LEFT ATTACH ANGLE VERTICA L TO FUSELAGE PER AARD 53-10-00-2. (M) 2 L 7 2 4F A6WE 1999092400918 19990924 00918 NM 1999 9 24 AALA991230 1 19990819 A 3350 CONNECTOR BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 727AA 20734 BNA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIPS FROM FRONT OF COACH TO FRONT OF FIRST CLASS I NOPERATIVE. REPLACED CONNECTOR BETWEEN FIRST CLASS AND COACH EMERGENCY EXIT FLOOR PATH LIGHTS STRIPS. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400919 19990924 00919 NM 1999 9 24 AALA991231 1 19990819 A 3350 1001141 LIGHT GRIMES BOEING 727 727227 1384078 NM AFT STAIRWAY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 730AA 20737 DFW - DURNG OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT BOTTOM OF AFT STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400920 19990924 00920 NM 1999 9 24 AALA991242 1 19990821 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 889AA 21527 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EX IT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400921 19990924 00921 NM 1999 9 24 AALA991258 1 19990823 A 3350 1001141 BATTERY BOEING 727 727223 1384074 NM AFT AIRSTAIR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6835 20188 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONTACTS AT BATTERY PACK AND BATTERY CHARGER FOR AFT AIRSTAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400922 19990924 00922 WP 1999 9 24 AALA991159 1 19990810 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP MLG DOOR OUT OF ADJUST A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 7542A 49996 DTW - FLT 2080 - EN ROUTE DFW-DTW, WHEEL GEAR DOOR OPEN LIGHT ILLUMINATED IN CRUISE. TURNED RIGHT HYDRAULIC PUMP ON HIG H TO KEEP LIGHT EXTINGUISHED. LANDED DTW WITHOUT INCIDENT. ADJUSTED GAP ON GEAR DOOR PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400923 19990924 00923 NM 1999 9 24 AALA991257 1 19990823 A 3350 1001141 BATTERY GRIMES BOEING 727 727223 1384074 NM AFT AIRSTAIR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 869AA 21374 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONTACTS AT BATTERY PACK AND BATTERY CHARGER FOR AFT AIRSTAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400924 19990924 00924 NM 1999 9 24 AALA991246 1 19990822 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT AIRSTAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 21387 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400925 19990924 00925 NM 1999 9 24 AALA991247 1 19990822 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 21387 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP FORWARD OF FIRST CLASS INOPERATIVE. REPLAC ED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP FORWARD OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400926 19990924 00926 NM 1999 9 24 AALA991144 1 19990805 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 873AA 21385 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT IN FORWARD GALLEY INOPERATIVE. RESEATED OVERHEAD EMER GENCY EXIT LIGHT IN FORWARD GALLEY SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400927 19990924 00927 NM 1999 9 24 AALA991145 1 19990808 A 3397 WIRE BOEING 727 727223 1384074 NM ROW 22 OUT OF POSITION A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROW 22 INOPERATIVE. REPOSITIONED WIRES ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400928 19990924 00928 NM 1999 9 24 AALA991192 1 19990816 A 3350 AG113C1 LIGHT HONEYWELL BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843AA G11B1 20984 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDE MARKER LIGHT BY FORWARD SERVICE DOOR LOOSE FROM WALL. REPLACED EMERGENCY EXIT SIDE MARKER LIGHT BY FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400929 19990924 00929 NM 1999 9 24 AALA991178 1 19990815 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT AIRSTAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 871AA 2162 21383 TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGECY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400930 19990924 00930 WP 1999 9 24 AALA991220 1 19990815 A 3244 5930594539 TIRE DOUG DC9 DC982 3022082 WP MLG WORN A AALA O OTHER O OTHER TO TAKEOFF 1 SW 07 513AA B4121 49890 TPA - FLT 1621 - ON ARRIVAL TPA FROM LGA, POSSIBLE TIRE FAILURE OF NR 4 TIRE ON TAKEOFF FROM LGA. EMERGENCY EQUIPMENT W AS CALLED TO MEET FLIGHT ON LANDING. AIRCRAFT LANDED TPA WITHOUT INCIDENT. NR 4 TIRE WORN TO LIMITS. REPLACED NR 4 TI RE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400931 19990924 00931 WP 1999 9 24 AALA991222 1 19990818 A 3260 H141016 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 449AA 49475 DFW - FLT 2213 - AFTER TAKEOFF ORD-DFW, NOSE GEAR WARNING LIGHT ILLUMINATED INTERMITTENTLY AND THEN WENT OUT IN CRUISE. CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK SENSOR. CYCLED NOSE LANDING GEAR. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400932 19990924 00932 WP 1999 9 24 AALA991223 1 19990818 A 3260 SENSOR DOUG DC9 DC982 3022082 WP LT MLG DOOR NEEDED ADJUSTING A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 205AA 49155 DFW - FLT 1122 - DURING CLIMB-OUT, GDL-DFW, MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AND THEN WENT OUT. CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEAR DOOR UPLOCK TARGET. CYCLED LANDING GEAR. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400933 19990924 00933 WP 1999 9 24 AALA991235 1 19990819 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP LT MLG OUT OF ADJUST A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 232AA 49179 DFW - FLT 751 - EN ROUTE TUL-DFW, LEFT MAIN LANDING GEAR LIGHT ILLUMINATION WITH GEAR HANDLE IN UP POSITION. AIRCRAFT L ANDED DFW WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SENSOR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400934 19990924 00934 NM 1999 9 24 AALA990992 1 19990704 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722AA 20730 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY EXIT FLOOR PATH LIGHTING BY AFT DOOR INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400935 19990924 00935 NM 1999 9 24 AALA990984 1 19990703 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400936 19990924 00936 NM 1999 9 24 AALA990985 1 19990703 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT MIDDLE OF COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400937 19990924 00937 NM 1999 9 24 AALA990924 1 19990622 A 3350 BATTERY BOEING 727 727223 1384074 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 884AA 21523 MIA - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED CONTACTS ON BATTERY PACK. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400938 19990924 00938 NM 1999 9 24 AALA991012 1 19990708 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 864AA 21369 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FORWARD FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400939 19990924 00939 NM 1999 9 24 AALA990991 1 19990705 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 876AA 21388 MIA - DURING OVERNIGHT CHECK, RIGHT EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE AT RIGHT AFT EXIT LIGHT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400940 19990924 00940 NM 1999 9 24 AALA990990 1 19990704 A 3350 BATTERY BOEING 727 727223 1384074 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6835 20188 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS FOR AFT ST AIRWAY EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400941 19990924 00941 WP 1999 9 24 AALA991227 1 19990818 A 2910 HYD SYSTEM DOUG DC9 DC982 3022082 WP RIGHT MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 90511 49805 LAX - FLT 613 - EN ROUTE BUR FROM DFW, RIGHT THRUST REVERSER ACCUMULATOR LIGHTS ILLUMINATED WITH LOSS OF RIGHT HYDRAULIC SYSTEM. AIRCRAFT DIVERTED TO LAX AND ALTERNATE GEAR EXTENSION ACCOMPLISHED. LANDING ACCOMPLISHED WITH GEAR DOORS IN O PEN POSITION. HYDRAULIC SYSTEM CHECKED WITH NO FAULTS NOTED. FUNCTIONAL CHECK FLIGHT ACCOMPLISHED. COULD NOT DUPLICAT E PROBLEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400942 19990924 00942 EU 1999 9 24 AALA991249 1 19990821 A 2910 A25240003 VALVE AIRBUS 300 A300B4605R 3930308 EU GREEN HYD SYSTEM DEFECTIVE A AALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 90070 N602 513 JFK - FLT 106 - PRIOR TO DEPARTURE GREEN SYSTEM HYDRAULIC PRESSURE WAS LOW. REPLACED LANDING GEAR EMERGENCY EXTENSION F REE FALL CUTOUT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999092400943 19990924 00943 NM 1999 9 24 AALA991174 1 19990814 A 3350 CONNECTOR BOEING 757 757223 1384957 NM ROW 31/34 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 669AA 25334 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 31ABC AND 34ABC INOPERATIVE. RESECURED CO NNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 31ABC AND 34ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999092400944 19990924 00944 NM 1999 9 24 AALA991177 1 19990815 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645AA 24603 DFW - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. CLEANED A ND RESECURED CONNECTOR TO LEFT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OP ERATIONS. (M) 2 L 7 2 4F RT A2NM 1999092400945 19990924 00945 NM 1999 9 24 AALA991197 1 19990816 A 3350 SOCKET BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 382AN 25451 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON RIGHT SIDE OVERWING EXIT INOPERATIVE. RESECURED LAMP SOCKET WITHIN EMERGENCY EXIT LIGHT ASSEMBLY ON RIGHT SIDE OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999092400946 19990924 00946 NM 1999 9 24 AALA991179 1 19990815 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 669AA 25334 MIA - DURING OVERNIGHT CHECK, OVERHEAD EMERGENCY EXIT SIGNS IN AFT GALLEY AND ABOVE L3 DOOR INOPERATIVE. RESEATED CONNE CTOR TO OVERHEAD EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999092400947 19990924 00947 NM 1999 9 24 AALA991107 1 19990729 A 3397 WIRE BOEING 757 757223 1384957 NM COCKPIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 625AA 24583 DFW - DURING OVERNIGHT MAINTENANCE, FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED WIRE TO FLIGHT DECK EMERGEN CY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999092400948 19990924 00948 NM 1999 9 24 AALA991226 1 19990818 A 2760 65375594 ACTUATOR BOEING 727 727223 1384074 NM NR 8 SPOILER BROKEN A AALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 07 865AA 124 21370 ORD - FLT 515 - ON APPROACH TO ORD FROM EWR, AIRCRAFT ROLLS RIGHT WITH FLAPS AT 25 DEGREES. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED NR 8 GROUND SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999092400949 19990924 00949 WP 1999 9 24 AALA991236 1 19990819 A 7830 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP LT TR UNIT LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 295AA 49307 ORD - FLT 2326 - EN ROUTE DFW-ORD, LEFT HYDRAULC FLUID QTY DROPPED TO RED BAND. ABNORMAL PROCEDURE FOR SLAT/FLAP EXTENS ION ACCOMPLISHED AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED LEFT THRUST REVERSER CONTROL VALVE HYDRAULIC PRESSU RE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400950 19990924 00950 WP 1999 9 24 AALA991264 1 19990824 A 2120 AIR DIST DOUG DC9 DC982 3022082 WP CABIN ODOR A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7522A 49899 DFW - FLT 751 - DURING CLIMB FROM TUL-DFW, SLIGHT BURNING SMELL NOTED IN COCKPIT AND CABIN. SMELL DISSIPATED EN ROUTE. AIRCRAFT LANDED DFW WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT OF BOTH PACKS. NO INDICATION OF SMELL OR SMOKE FOLLOW ING BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400951 19990924 00951 WP 1999 9 24 AALA991270 1 19990825 A 7830 0711346003 VALVE DOUG DC9 DC982 3022082 WP LT TR UNIT LEAKING A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 7541A 1464A 49995 DFW - FLT 892 - ON TAXI TO GATE AFTER LANDING DFW FROM FAT, CABIN FILLED WITH SMOKE. REPLACED LEFT THRUST REVERSER ISOL ATION VALVE. ACCOMPLISHED PACK BURN OUT OF BOTH AIR CONDITIONING PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400952 19990924 00952 WP 1999 9 24 AALA991275 1 19990825 A 4990 2651 GASKET DOUG DC9 DC982 3022082 WP APU DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 289AA 49301 DFW - FLT 896 - EN ROUTE SNA-DFW, NON ELECTRICAL ODOR AND HAZY SMOKE NOTED IN CABIN DURING HIGH POWER SETTINGS. ODOR AN D HAZY SMOKE DISSIPATED DURING CRUISE BUT RETURNED ON DESCENT. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED SEAL ON APU OIL TANK CAP. REMOVED AND REPLACED AIR CONDTIONER COALESCER BAGS. ACCOMPLISHED AIR CONDITONER PACK BURN OUT. BOTH ENGINES, APU, AND AIR CONDITIONER PACKS WERE OPERATED WITH NO ODOR OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F A6WE 1999092400953 19990924 00953 NM 1999 9 24 AALA991274 1 19990825 A 7920 OIL LINE BOEING 767 767323 1385205 NM NR 2 ENGINE LOOSE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 07 389AA 27449 DFW - FLT 19 - EN ROUTE JFK-LAX - NUMBER 2 ENGINE OIL QUANTITY DROPPED FROM 21 TO 6 QUARTS OVER 3 HOUR PERIOD. ENGINE S HUT DOWN TO CONSERVE REMAINING OIL. AIRCRAFT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. TIGHTENED LOOSE B-NUT ON OIL SCAVENGE PUMP ON NR 2 ENGINE. ENGINE RUNUP ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999092400954 19990924 00954 WP 1999 9 24 AALA991286 1 19990827 A 4920 38005041 APU DOUG DC9 DC982 3022082 WP AFT FUSELAGE DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 70529 P80447 49921 DFW - FLT 1639 - INBOUND TO DFW FROM PBI, FLIGHT ATTENDANTS REPORTED STRONG FUEL FUMES IN CABIN. AIRCRAFT LANDED DFW WI THOUT INCIDENT. APU WAS FOUND TO BE THE SOURCE OF ODOR. REPLACED APU. ACCOMPLISHED BURN OUT OF AIR CONDITIONING PACKS . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400955 19990924 00955 WP 1999 9 24 AALA991294 1 19990828 A 2150 20495061 TURBINE DOUG DC9 DC982 3022082 WP LT PACK DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 292AA 49304 LAS - FLT 482 - AFTER TAKEOFF LAS-DFW, ELECTRICAL ODOR AND SMOKE NOTED IN AIRCRAFT. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. REPLACED LEFT AIR CONDITIONING PACK TURBINE. ALSO, REPLACED LEFT AIR CONDITIONING PACK TEMPERATURE CONTROL VALVE AND COALESCER BAGS FOR BOTH AIR CONDITIONING PACKS. BOTH AIR CONDITIONING PACKS OPERATED WITH NO SMOKE OR SMELL NOTED IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400956 19990924 00956 WP 1999 9 24 AALA991272 1 19990825 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 552AA 53034 DFW - DURING OVERNIGHT MAINTENANCE, AFT DOOR TO STAIRWAY EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REPLACED CONNECTOR TO AFT DOOR TO STAIRWAY EMERGENCY EXIT MARKER LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400957 19990924 00957 WP 1999 9 24 AALA991103 1 19990729 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 494AA 49732 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP IN AFT CABIN INOPERATIVE. REPLACED 25 FOOT SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTING STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400958 19990924 00958 WP 1999 9 24 AALA991289 1 19990828 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 15 DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 467AA 49597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT SEAT ROW 15 FOUND DAMAGED. REPLACED EME RGENCY EXIT FLOOR PATH LIGHTING STRIP AT SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999092400959 19990924 00959 EU 1999 9 24 AALA991301 1 19990831 A 2131 21185266 CONTROLLER FOKKER F28 F28MK0100 4990807 EU E/E COMPT DEFECTIVE A AALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 1425A 32A0023 11408 DFW - FLT 711 - EN ROUTE DFW-COS, AT FL310 CABIN PRESSURE CONTROL CHANGE MESSAGE ILLUMINATED ON MFDU. MANUAL PRESSURIZA TION CONTROL WAS SELECTED BUT CABIN PRESSURE CONTINUED TO CLIMB. EMERGENCY DESCENT ACCOMPLISHED TO 10,000 FT. PASSENGE R OXYGEN MASKS WERE DROPPED DURING DESCENT. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 CABIN PRESSURE CONTROLLER. NR 2 CABIN PRESSURE CONTROLLER ALSO REPLACED AS A PRECAUTION. REPLACED OXYGEN CANISTERS AND REPAC KED OXYGEN MASKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999092400960 19990924 00960 WP 1999 9 24 AALA991311 1 19990901 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP MLG MALFUNCTIONED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - DURING AIRCRAFT 'RCF' AFTER HEAVY C-CHECK, THE MAIN LANDING GEAR EMERGENCY EXTENSION SYSTEM WAS ACTUATED BUT DID N OT OPERATE PROPERLY. MAIN LANDING GEAR DID NOT EXTEND, COULD NOT RELEASE MECHANISM. CHECK AND RE-RIGGED EMERGENCY EXTE ND CABLES. PERFORMED GEAR SWING WITH EMPHASIS ON EMERGENCY EXTEND SYSTEM. (M) 2 L 7 2 4F A6WE 1999092400961 19990924 00961 WP 1999 9 24 AALA991312 1 19990831 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1212-1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 207AA 49158 TUL - FOUND LEFT TIE DOWN TRACK IN AFT CARGO IS HEAVILY CORRODED, TOP AND BOTTOM SIDES, FROM STATION 1212 TO 1322. REMO VED CORRODED TRACK. INSTALLED NEW TRACK SECTION PER SRM 53-01. (M) 2 L 7 2 4F A6WE 1999092400962 19990924 00962 NM 1999 9 24 AALA991263 1 19990823 A 5330 SKIN BOEING 727 727227 1384078 NM BS 245 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND DENT IN SKIN BS 245, STRINGER 16R AND 17R. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999092400963 19990924 00963 NM 1999 9 24 AALA991260 1 19990823 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 320 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND CORROSION ON RIGHT SKATE ANGLE STATION 310-320. FABRICATED AND INSTALLED REPAIR PER ESO 11697, DATED 8/23/9 9. (M) 2 L 7 3 4F A3WE 1999092400964 19990924 00964 NM 1999 9 24 AALA991262 1 19990821 A 5330 SKIN BOEING 727 727227 1384078 NM BS 833-837 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND CENTER TANK LOWER SKIN HAS 4 AREAS OF CORROSION ABOVE LEFT PRIMARY HEAT EXCHANGER STATION 833-837. INSTALLE D DOUBLER AND TRIPLER REPAIR PER ESO 11697, DATED 8-19-99. (M) 2 L 7 3 4F A3WE 1999092400965 19990924 00965 NM 1999 9 24 AALA991261 1 19990817 A 5330 SKIN BOEING 727 727227 1384078 NM BS 500-517 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND SKIN LAP CORROSION STRINGER 19R, 17 INCH LENGTH BULGED AND CRACKED. CUT OUT CORRODED AREA OF THE SKIN LAP A ND INSTALLED DOUBLER PER 53-30-3 FIG 5 P20-23. (M) 2 L 7 3 4F A3WE 1999092400966 19990924 00966 NM 1999 9 24 AALA991267 1 19990819 A 5320 BOEING 727 727223 1384074 NM UNKNOWN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - HFEC INDICATES A 1 INCH CRACK ON RT MLG WW PRESS DECK BEAD AT RT OUTBOARD AFT CORNER AT BS 947 ABOVE PULLEY. INST ALLED PRESSURE DECK REPAIR PER ECO 11697. (M) 2 L 7 3 4F A3WE 1999092400967 19990924 00967 EU 1999 9 24 99ZZZM653 1 19990824 A 2432 40782 BATTERY AEROSP ATR72 ATR72212 EU BATT COMPT DISCHARGED A TRBA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 21 408AT 408 MAIN BATTERY KEEPS FALLING OUT (OFF). RECYCLED 2 AFTER TAKEOFF AND STAYS INOP. SMELL OF ELECTRICAL BURNING. REMOVED A ND REPLACED MAIN BATTERY AS PER 24-31-85. FOUND MAIN BATTERY CHARGING SYSTEM WORKING PROPERLY AT THIS TIME. PERFORMED VISUAL INSPECTION. NO DEFECTS FOUND. (M) 2 H 7 2 4T RT A53EU 1999092400968 19990924 00968 EU 1999 9 24 99ZZZM654 1 19990603 A 5315 S53672410200 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FRAME 41 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FOUND CORROSION ON FLOORBEAM FRAME 41 CENTER AREA BY FITTING. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL CORROSI ON BLENDED AND FOUND BEYOND LIMITS IAW SRM 53-61-00 FIG 301. (M) 2 H 7 2 4T RT A53EU 1999092400969 19990924 00969 EU 1999 9 24 99ZZZM655 1 19990603 A 5311 S5397140226151 FRAME AEROSP ATR42 ATR42300 8680920 EU FRAME 27A CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FOUND FRAME 27A RT CORRODED INBOARD AND OUTBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTA L CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M) 2 H 7 2 4T RT A53EU 1999092400970 19990924 00970 EU 1999 9 24 99ZZZM656 1 19990603 A 5230 S5237610420751 FRAME AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FOUND FORWARD CARGO DOOR INNER STRUCTURE HAS CORROSION AFT OF PRESSURE DOOR. CAUSE OF CORROSION DETERMINED TO BE ENVIRO NMENTAL. CORROSION REMOVED AND FOUND BEYOND LIMITS IAW SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1999092400971 19990924 00971 EU 1999 9 24 99ZZZM657 1 19990603 A 5320 S5397450221502 INTERCOSTAL AEROSP ATR42 ATR42300 8680920 EU FRAME 27/28 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FOUND INTERCOSTAL BETWEEN FRAMES 27A RT AND 28A RT BELOW STRINGER 19 CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVI RONMENTAL. CORROSION REMOVED AND FOUND BEYOND LIMITS. (M) 2 H 7 2 4T RT A53EU 1999092400972 19990924 00972 EU 1999 9 24 99ZZZM658 1 19990603 A 5311 S5397140220301 FRAME AEROSP ATR42 ATR42300 8680920 EU FRAME 27 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FOUND UPPER CHORD ON FRAME 27A RT CORRODED INBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMEN TAL. CORROSION REMOVED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M) 2 H 7 2 4T RT A53EU 1999092400973 19990924 00973 EU 1999 9 24 99ZZZM659 1 19990603 A 5320 S5397450221402 INTERCOSTAL AEROSP ATR42 ATR42300 8680920 EU FRAME 27/28 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 INTERCOSTAL BETWEEN FRAMES 27A LT AND 28A LT BELOW STRINGER 19 CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMEN TAL. CORROSION REMOVED AND FOUND BEYOND LIMITS. (M) 2 H 7 2 4T RT A53EU 1999092400974 19990924 00974 EU 1999 9 24 99ZZZM660 1 19990603 A 5320 S53914072102 INTERCOSTAL AEROSP ATR42 ATR42300 8680920 EU FRAME 27/28 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FOUND INTERCOSTAL BETWEEN FRAMES 27A RT AND 28 RT BELOW STRINGER 16R CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVI RONMENTAL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M) 2 H 7 2 4T RT A53EU 1999092400975 19990924 00975 EU 1999 9 24 99ZZZM661 1 19990603 A 5311 S53971403201051 FRAME AEROSP ATR42 ATR42300 8680920 EU FRAME 28 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FOUND FRAMES 28A RT CORRODED INBOARD AND OUTBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENT AL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M) 2 H 7 2 4T RT A53EU 1999092400976 19990924 00976 EU 1999 9 24 99ZZZM662 1 19990603 A 5313 S53574300200 STRINGER AEROSP ATR42 ATR42300 8680920 EU FRAME 24/27 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 SPECIAL STRINGER ON LOWER KEEL BEAM, LEFT SIDE HAS CORROSION BETWEEN FRAMES 24A LT AND 27A LT. CAUSE OF CORROSION DETER MINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW 32 PERCENT MATERIAL THICKNESS SRM 53-51-00 PAG E 304. REMOVED AND REPLACED SPECIAL STRIGNER ON LOWER KEEL BEAM, LEFT SIDE BETWEEN FRAMES 24A AND 27A LEFT IAW SRM 53-0 0-00. (M) 2 H 7 2 4T RT A53EU 1999092400984 19990924 00984 1999 9 24 TWAA9913001 4 19990921 A 2565 D29982113 SLIDE DOUG DC9 DC982 3022082 WP R1 DOORWAY WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 957U 49702 DURING PREFLIGHT, FOUND THE ESCAPE SLIDE AT THE FORWARD RT SIDE DOOR HAD DISCONNECTED AND WAS STARTING TO COME APART. R EPLACED THE SLIDE. CHECK-C 12-23-98 STL. 2 L 7 2 4F A6WE 1999092400985 19990924 00985 EU 1999 9 24 MALA976574 1 19990915 A 5411 FRAME SAAB SF340 SF340A 7850100 EU NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 076 DURING HEAVY CHECK, SOME RIVETS ATTACHING TO LOWER FRAME THROUGH THE EXTERNAL SKIN, NEAR NAC WL 94, HAVE POOR PITCH & ED GE DISTANCE. THERE IS A CRACK IN THE LOWER FRAME IN THIS AREA STARTING FROM A FASTENER HOLE GOING TO THE EDGE OF THE FR AME. MAINTENANCE REPAIR PER EO NR S54020 AND SAAB STATEMENT 72SDS1756 REV A DATED 9/13/99. 2 L 7 2 4T RT A52EU 1999092400986 19990924 00986 EU 1999 9 24 MALA976575 1 19990916 A 7931 523535 GAUGE SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 110XJ 340A110 WHILE EN ROUTE AT 16,000 FT, NOTICED THE LEFT PROP OIL PRESSURE INDICATING 160 PSI, COMPLETED QRH. MONITORED PROP OIL P RESSURE WAS FLUCTUATING UP TO 190 PSI. DIVERTED TO MKG. MAINTENANCE INSPECTED LT PGB OIL SYSTEM, RAN A/C AT HIGH POWER SETTING TO DUPLICATE PROBLEM, INSTALLED NEW RT GAUGE. ALL CHECKS NORMAL. 2 L 7 2 4T RT A52EU 1999092400987 19990924 00987 EU 1999 9 24 MALA976576 1 19990917 A 2436 51539007B GCU SAAB SF340 340B 7860101 EU LT GC GEN FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 407XJ 340B407 LT DC GEN DROPPED OFF LINE. CREW FOLLOWED QRH, GEN RESET 10 MIN LATER LT DC GEN DROPPED OFF LINE AND WOULDN'T COME BACK ON LINE, UNTIL APPROX 10 MINUTES LATER. AIRCRFAT RETURNED TO DTW. MAINTENANCE REPLACED LT DC GCU. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999092400988 19990924 00988 EU 1999 9 24 MALA976577 1 19990921 A 7931 IPTE551000200 TRANSDUCER SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 110XJ 340A110 AFTER TAKEOFF, LEFT PROP OIL INCREASED TO 150 PSI. CREW BEGAN QRH PROCEDURES AND LEFT RPM BEGAN TO FLUCTUATE AND LEFT P ROP PSI BEGAN TO INCREASE. CREW ACCOMPLISHED ENGINE SHUTDOWN AS PER QRH AND LANDED IN CWA. MAINTENANCE FOUND GAUGE STU CK AT 160 PSI, REMOVED TRANSDUCER CANNON PLUG AND GAUGE DROPPED TO ZERO. MAINTENANCE REPLACED PGB TRANSDUCER. OPS CHEC K DURING GROUND RUN GOOD. TEST FLIGHT REQUIRED DUE TO REPEAT LT PGB OIL PRESSURE GOING HIGHER THAN NORMAL IN FLIGHT. T EST FLIGHT SATISFACTORY, COMPLETED WALKAROUND OF AIRCRAFT. NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 1999092400989 19990924 00989 EU 1999 9 24 MALA976578 1 19990915 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 429XJ 429 DURING INSPECTION, 6A FLOOR TRACK LIGHTING STRAP LOOSE. MAINTENANCE RESECURED FLOOR TRACK LIGHT STRIP, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999092400990 19990924 00990 EU 1999 9 24 MALA976579 1 19990918 A 2450 BUS BAR BAC 146 AVRO146RJ85A 1500097 EU E&E COMPT NOT ACTIVATED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 514XJ E2330 DURING PREFLIGHT TESTING, FIREBELL WON'T TEST WHEN ENGINE 1-4 AND APU FIRE TEST BUTTONS ARE PRESSED. MAINTENANCE ENERGI ZED BUSS BARS, POWERED AIRCRAFT AND PERFORMED TEST PER RJ MM 31-52-11 TEST. AIRCRAFT READY FOR FLIGHT. 2 H 7 4 4F RT A49EU 1999092400991 19990924 00991 1999 9 24 MALA976580 4 19990914 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOORWAY DEPLOYED A MALA O OTHER O OTHER IN INSP/MAINT 1 GL 15 522XJ E2347 FORWARD LEFT PAX DOOR EMERGENCE ESCAPE SLIDE DEPLOYED. MAINTENANCE REPLACED EVACUATION SLIDE, OPS CHECK GOOD IAW AVRO A MM 25-60-11-401. 2 H 7 4 4F RT A49EU 1999092400992 19990924 00992 NM 1999 9 24 UPS99230676 1 19990922 A 3350 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMERGENCY LIGHT SYSTEM NOT OPERATING PROPERLY. PERFORMED EMERGENCY LIGHTING ADJ/TEST IAW MM 33-50- 01. RESET EMERG LIGHT SWITCH CARGO POSITION, SYS OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 1999092400993 19990924 00993 NM 1999 9 24 UPS99230677 1 19990920 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 720-740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, FOUND SEAT TRACK BS 720-740 RBL 25, WL 208 TO BE CORRODED UNDER NUT PLATE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED SEAT TRACK REPAIR PER SRM 51-30-2, SRM 51-30-5, AND 51-30-8. 2 L 7 3 4F A3WE 1999092400994 19990924 00994 NM 1999 9 24 UPS99230678 1 19990824 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) FUSELAGE SHEAR TIE UPPER LEG IS CORRODED AT BS 351, WL 160, RBL 33. RE MOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-1, 53-10-4. 2 L 7 3 4F A3WE 1999092400995 19990924 00995 NM 1999 9 24 UPS99230679 1 19990920 A 5320 BAC15057075 BEAM BOEING 727 72725C 138400H NM BS 835 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION ON TOP SURFACE ON LONGITUDINAL BEAM AT BS 835, RBL 2, WL 208. REMOVED CORROSION ON BEAM A T BS 835, RBL 2, WL 208 IN A 5.0 X 1.5 X .019 AREA ORIG THICKNESS OF .130, FOUND TO BE OUT OF LIMITS. REMOVED BEAM FROM BS 740 - 870 AND REPLACED WITH NEW FABRICATED BEAM IAW SRM 51-30-5, SRM 51-30-2, SRM 51-30-8. 2 L 7 3 4F A3WE 1999092400996 19990924 00996 NM 1999 9 24 UPS99530675 1 19990922 A 5350 121N782012 RADOME BOEING 757 75724APF 1384969 NM FWD FUSELAGE DAMAGED A IPXA O OTHER C F.O.D. NR NOT REPORTED 1 SO 01 420UP 23907 INSPECTION TYPE:N/A, PILOT REPORT, RADOME DAMAGED FROM BIRD STRIKE EXCEEDS LIMITS. REMOVED AND REPLACED RADOME PER MM 5 3-12-01 PAGE 201 (P/N 4910-400), (S/N 393NF) ON, (P/N 121N 7820-12), (S/N 150) OFF. 2 L 7 2 4F RT A2NM 1999092400997 19990924 00997 WP 1999 9 24 UPS99830667 1 19990905 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1660 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, FRAME FACE GOUGED IN RADIUS AT STA 1660 LONG 4L. TRIMMED OUT DAMAGE AND REPAIRED IAW REO-06735. 2 L 7 4 4F RT 4A25 1999092400998 19990924 00998 WP 1999 9 24 UPS99830668 1 19990905 A 5240 BEAM DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, RT AFT DOOR HAS CRACKED FRAME AT UPPER FWD CORNER. OPENED INNER WEB AND REMOVED CRACKED DOOR BEAM. FABRICATED NEW DOOR BEAM (P/N 5772639-21) IAW DC8 SRM 51-1-21, INSTALLED IAW DC8 SRM 51-1-2 0D, 51-1-21 AND REINSTALLED INNER WEB IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999092400999 19990924 00999 WP 1999 9 24 UPS99830669 1 19990905 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 600 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, STA 600 SEAT TRACK F SCALLOPS GOUGED BLENDED DAMAGED IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIM ITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED OUT OF LIMITS SECTION STA 570-610 IAW DC8 SRM UPS ADDENDUM DC8-53B-003. 2 L 7 4 4F RT 4A25 1999092401000 19990924 01000 WP 1999 9 24 UPS99830670 1 19990906 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, RT I/B FLAP LOWER SKIN HAS 2 DENTS STA XRS 74 AND XRS 172. REMOVED DAMAGE FROM FLAP, FABBED AND INS TALLED DOUBLERS IAW DC8 SRM 57 2-1 & 51-1-21. 2 L 7 4 4F RT 4A25 1999092401001 19990924 01001 WP 1999 9 24 UPS99830671 1 19990907 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, LONGERON 10R FS 680 BATHTUB FITTING IS CRACKED. REMOVED LONGERON FITTING, LOCATED AND DRILLED UP FI TTING AND INSTALLED IAW DC8 SRM 51-1-24, 51-1-21, 51-1-20D & 51-3-0. 2 L 7 4 4F RT 4A25 1999092401002 19990924 01002 WP 1999 9 24 UPS99830672 1 19990907 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, LONGERON 7R, FS 680 BATHTUB FITTING IS CRACKED. REMOVED LONGERON FITTING, LOCATED AND DRILLED UP FI TTING AND INSTALLED IAW DC8 SRM 51-1-24, 51-1-21, 51-1-20D, & 51-3-0. 2 L 7 4 4F RT 4A25 1999092401003 19990924 01003 WP 1999 9 24 UPS99830673 1 19990907 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, AFT PRESSURE BULKHEAD AT STA 1766 LONG 11R IS CRACKED. FABBED DOUBLERS -25.032 7075-T6 & -27.063 70 75-T6 PER DWG NR SRO 85300 07. FABBED ANGLE (P/N 5772638-48.063) 7075-T6, FABBED FILLERS -19.090 7075-T6, -9.050 7075- T6 & -11.063 7075-T6 PER DWG SRM 8530007. INSTALLED DOUBLER, FILLERS AND ATTACH ANGLE PER DWG NR SRO 8530007 & DC8 SRM 51-1-20 & 51-1-21D. 2 L 7 4 4F RT 4A25 1999092401004 19990924 01004 NM 1999 9 24 99UAL900445 1 19990824 A 2130 VALVE ALLIEDSIGNAL 3964421 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RIGHT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 308UA 1470 23669 UNABLE TO PRESSURIZE BEYOND .8 PSI DIFFERENTIAL AT 10,000 FT WITH APU BLEED OFF AND RIGHT PACK TO HIGH. *S/D* RIGHT HA ND FLOW CONTROL AND MODULATION VALVE FAILED TO THE CLOSED POSITION. REPLACED THE RIGHT HAND FLOW CONTROL AND MODULATION VALVE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999092401005 19990924 01005 NM 1999 9 24 99UAL900470 1 19990912 A 2421 IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT INOP A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 29 652UA 25390 AIRCRAFT DISPATCHED WITH LT INTEGRATED DRIVE GENERATOR (IDG) INOP. APU AUTO SHUTDOWN CAUSING APU GENERATOR AND UTILITY BUSSES TO TRIP. FLIGHT DIVERTED TO MSY. REPLACED LT IDG. SHOP FOUND CONTAMINATION IN IDG SYSTEM. 2 L 7 2 4F 4 F RT A1NM E24NE 1999092401006 19990924 01006 1999 9 24 99UAL900471 4 19990909 A 3442 RT UNIT COLLINS 6225122103 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RADAR SYS FAILED A UALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 WP 29 374UA 460 24639 WEATHER RADAR INTERMITTENTLY INOP. *S/D* REPLACED THE WEATHER RADAR RECEIVER/TRANSMITTER UNIT. 2 L 7 2 4F 4 F RT A16WE E2GL 1999092401007 19990924 01007 NM 1999 9 24 99UAL900472 1 19990913 A 2450 91252ZC7C4001 R3 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E&E COMPT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 360UA 24453 NR 1 NORMAL TRANSFER BUS CIRCUIT BREAKER ON THE P6-11 POPPED AND TRANSFER BUS DID NOT TRIP OFF. RESET AND IT POPPED AGA IN AFTER 5 MINUTES. SHORTLY AFTER, THE FOLLOWING LIGHTS CAME ON, NR 1 B ELECTRIC LOW PRESSURE, NR 1 AFT FUEL BOOST PUMP LOW PRESSURE, ANTI-SKID INOP LIGHT AND AUTOBRAKE DISARM LIGHT. R3 TRANSFER RELAY FAILED. REPLACED R3 TRANSFER RELAY. 2 L 7 2 4F 4 F RT A16WE E2GL 1999092401008 19990924 01008 NM 1999 9 24 99UAL900473 1 19990912 A 3350 34145410 EPSU AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 810UA 843 EPSU UNIT FWD L FAILED TEST PER NR 3 SVC. EPSU UNIT WAS THE CAUSE OF THIS MALFUNCTION. THE EPSU WAS REPLACED AND THE S YSTEM TESTED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 1999092401009 19990924 01009 NM 1999 9 24 99UAL900474 1 19990910 A 5531 SPAR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7454U 21908 THE VERTICAL STABLE MID SPAR CHORD AT FIN STATION 215 ON THE LEFT SIDE WAS FOUND CHAFED TO BELOW THE MINIMUM ALLOWABLE T HICKNESS OF THE CHORD. THE DAMAGED AREA WAS BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INSTALLED PER TIMCO REPAIR I NSTRUCTIONS. THIS REPAIR WAS APPROVED BY BOEING'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999092401010 19990924 01010 NM 1999 9 24 99UAL900476 1 19990915 A 2121 4100943B FAN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 784UA 11531 26951 FLIGHT ATTENDANT REPORTED THAT THERE WAS A STRONG ELECTRIC SMELL IN THE AFT CABIN. AN AMBER ALERT WAS DECLARED AND THE FLIGHT DIVERTED INTO MIA MAKING A NORMAL LANDING. *S/D* FOUND THE RIGHT LOWER AIR RECIRCULATION FAN FAILED. FAN WAS R EPLACED. SHOP FINDINGS REVEALED THAT RECIRCULATION FAN HAD FAILED BEARINGS WHICH HAS CAUSED ITS MOTOR TO OVERHEAT. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999092401011 19990924 01011 NM 1999 9 24 99UAL900477 1 19990916 A 2530 OVEN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE GALLEY DIRTY A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 153UA 20102 PER CREW SMOKE IN CABIN BETWEEN DR2 AND DR3 CABIN AREA. BURNT MEALS IN THE FORWARD LOWER LOBE GALLEY, OVEN NR 3 WERE TH E SOURCE OF THE CABIN SMOKE. 2 L 7 4 4F 4 F A20WE E20EA 1999092401012 19990924 01012 WP 1999 9 24 99UAL900478 1 19990916 A 2560 INDICATOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL DOOR 3L SLIDE MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1837U 47969 3L DOOR SLIDE LIGHT WILL NOT TEST. *S/D* REPLACED SLIDE REMOTE PRESSURE INDICATOR. 2 L 7 3 4F 4 F A22WE E23EA 1999092401013 19990924 01013 NM 1999 9 24 99UAL900479 1 19990916 A 2150 33990047U1 PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 579UA 26697 DIVERTED TO JFK DUE TO CABIN DECOMPRESSION. AIRCRAFT DIVERTED DUE TO THE LOSS OF THE RT PNEUMATIC SYSTEM. THE LT PACK WAS INOP ON TAKEOFF. THE LT ACM WAS REPLACED AND A PNEUMATIC HEALTH CHECK WAS PERFORMED ON BOTH ENGINES. THE RT ENGINE WAS FOUND WITH A BAD HIGH PRESSURE CONTROLLER (3399004-7U1) AND THE 490 AND FAN AIR TEMP SENSORS WERE REPLACED AS A PRE CAUTIONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 1999092401014 19990924 01014 NM 1999 9 24 99UAL900480 1 19990916 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 680 INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7442U 21896 EMERGENCY AISLE LIGHT AT STATION 680 IS INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1999092401015 19990924 01015 NM 1999 9 24 99UAL900481 1 19990916 A 2530 321897 CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7459U 21913 GALLEY HOT PLATE SMOKING AND SPARKING. HOT PLATE CORD FRAYED AND EXPOSED. *S/D* REMOVED HOT PLATES, INSPECTED WIRING FROM GALLEY WALL TO PLATES AND NO DAMAGE, NO OPEN INSULATION, NO BRITTLENESS. INSTALLED NEW CONNECTORS, CLEANED AREA, R ECONNECTED HOT PLATES (INCLUDING REPLACEMENT). RESET CB, HOT PLATES OPERATE NORMALLY. 2 L 7 3 4F 4 F A3WE E2EA 1999092401016 19990924 01016 NM 1999 9 24 99UAL900482 1 19990916 A 3233 99C55202101 VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NLG OUT OF ADJUSTED A UALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION TO TAKEOFF 1 WP 29 782UA 26948 ON TAKEOFF, NOSE LANDING GEAR SHOWED DISAGREE. NOSE GEAR APPEARED STUCK DOWN. FLIGHT RETURNED TO ORD, LANDING UNDER AM BER ALERT. *S/D* COULD NOT DUPLICATE MALFUNCTION ON GROUND. REPLACED THE NLG RETRACT ACTUATOR AND NLG LOCK ACTUATOR A S PRECAUTIONARY. SHOP FINDINGS FOUND NO FAULTS WITH ACTUATORS. REPLACED THE NLG SELECTOR BYPASS VALVE (99C55202-101), PERFORMED RIG CHECK OF THE NLG DOOR OPERATED SEQUENCE VALVE LINKAGE AS A FOLLOWUP AT A LATER DATE. THE NLG DOOR OPERATI NG SEQUENCE VALVE WAS FOUND SLIGHTLY OUT OF ADJUSTED. THIS WAS CORRECTED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999092401017 19990924 01017 NM 1999 9 24 VNAA9909006 1 19990917 A 2721 DOLN1081M4D4NC RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RUDDER TRIM MALFUNCTIONED A VNAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 07 458PS 8793 3068 DURING DESCENT TO GSP AN UNCOMMANDED RUDDER TRIM WAS NOTICED BY THE FLIGHT CREW. A NORMAL LANDING WAS PERFORMED IN GSP. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE 26CC AND 28CC RELAYS IN ACCORDANCE WITH MAINTENANCE MANUAL 27-22-0 0. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999092800001 19990928 00001 WP 1999 9 28 GTIA9901013 1 19990522 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 550-570 MISDRILLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 934ML 47526 MHV - PASSENGER CABIN INTERNAL STATION 550 TO 570 STRINGER L-17 THERE ARE APPROX 25 HOLES WITH SHORT C/C SPACING S/B .60 0 IAW SRM 53-02 FIG 18 SH 6 ARE .48-.58 REF NR A092-S03-W084. REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STAT ION 531 TO STATION 588 PRODUCTION SPLICE PER ENGINEERING DWG 53-99197-1 (CABIN PRESSURIZATION WILL BE ACCOMPLISHED ON WO RK CARD NR A092A09Z025). (M) 2 L 7 2 4F A6WE 1999092800002 19990928 00002 WP 1999 9 28 GTIA9901010 1 19990522 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 669-775 WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - LEFT CABIN FLOOR PANEL STATION 669 TO 775 SKIN AROUND NUMEROUS SCREW HOLES TO THIN. RESKINNED FLOOR PANEL IAW SRM DC9 53-20 AND 53-05, FABRICATED SKIN PANEL ALODINED AND PRIMED. (M) 2 L 7 2 4F A6WE 1999092800003 19990928 00003 WP 1999 9 28 GTIA9901009 1 19990522 A 5320 SHEAR TIE DOUG DC9 DC931 3022065 WP BS 940 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 REMOVED B/S REPAIR RT FUSE CRACK IN SHEAR TIE APPRON STATION 940 BETWEEN STRINGER 15/16. FABRICATED ANGLE DOUBLER PER D C9 IAW SRM 51-10-2 PAGE 1 FIG 2 PER SAMPLE SUPPLIED. (M) 2 L 7 2 4F A6WE 1999092800004 19990928 00004 WP 1999 9 28 GTIA9901004 1 19990522 A 5320 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 484 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 MHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO F ACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 S RM 51-30-5 AND 51-10-4 PAGE 1 AND 4A FIG 3A. (M) 2 L 7 2 4F A6WE 1999100100001 19991001 00001 EU 1999 10 1 SIMA991831 1 19990702 A 5330 7253814435 SKIN SAAB SF340 340B 7860101 EU FUSELAGE PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 222NE 340B222 ABI - DAMAGE TO LOWER FUSELAGE CONSISTING OF TEAR TO SKIN BETWEEN SL 1524, SL 1528, AND BS 622-649, BUCKLING OF FRAMES A T BS 630, 640, 649, FLANGE BUCKLING OF STR TIE SL 1527, 1528. REMOVED DAMAGED AREAS AND STR TIE SL 1527. PERFORMED EDD Y CURRENT INSP. FABBED SKIN SPLICE AND DBLR .050 INCH THK. FABBED FRAME DBLR .040 INCH THK AT BS 630. FABBED DBLR .04 0 INCH THK BS 674 FOR FRAME AT BS 649. FABBED FILLER, DBLR, AND ANGLE .040 INCH THK AT BS 649. REPLACED STR TIE SL 152 7. FABBED STR DBLR .063 INCH THK AND SPLICE STRAP .071 INCH THK AT BS SL 1528. INSTALLED IAW SAAB REPAIR NR 72SD1600 S AAB 340 SRM 51-70-20/30 STD PRACTICES. REF: OPER CNTRL NR 99ZZZX3626 - 99ZZZX3628. (X) 2 L 7 2 4T RT A52EU 1999100100002 19991001 00002 EU 1999 10 1 99ZZZX3626 1 19990702 A 5311 7253814437 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 222NE 340B222 ABI - DAMAGE TO LOWER FUSELAGE CONSISTING OF TEAR TO SKIN BETWEEN SL 1524, SL 1528, AND BS 622-649, BUCKLING OF FRAMES A T BS 630, 640, 649, FLANGE BUCKLING OF STR TIE SL 1527, 1528. REMOVED DAMAGED AREAS AND STR TIE SL 1527. PERFORMED EDD Y CURRENT INSP. FABBED SKIN SPLICE AND DBLR .050 INCH THK. FABBED FRAME DBLR .040 INCH THK AT BS 630. FABBED DBLR .04 0 INCH THK BS 674 FOR FRAME AT BS 649. FABBED FILLER, DBLR, AND ANGLE .040 INCH THK AT BS 649. REPLACED STR TIE SL 152 7. FABBED STR DBLR .063 INCH THK AND SPLICE STRAP .071 INCH THK AT BS SL 1528. INSTALLED IAW SAAB REPAIR NR 72SD1600 S AAB 340 SRM 51-70-20/30 STD PRACTICES. REF: OPER CNTRL NR SIMA 991831, 99ZZZX3627 - 99ZZZX3628. 2 L 7 2 4T RT A52EU 1999100100003 19991001 00003 EU 1999 10 1 99ZZZX3627 1 19990702 A 5320 7253700049 STRINGER TIE SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 222NE 340B222 ABI - DAMAGE TO LOWER FUSELAGE CONSISTING OF TEAR TO SKIN BETWEEN SL 1524, SL 1528, AND BS 622-649, BUCKLING OF FRAMES A T BS 630, 640, 649, FLANGE BUCKLING OF STR TIE SL 1527, 1528. REMOVED DAMAGED AREAS AND STR TIE SL 1527. PERFORMED EDD Y CURRENT INSP. FABBED SKIN SPLICE AND DBLR .050 INCH THK. FABBED FRAME DBLR .040 INCH THK AT BS 630. FABBED DBLR .04 0 INCH THK BS 674 FOR FRAME AT BS 649. FABBED FILLER, DBLR, AND ANGLE .040 INCH THK AT BS 649. REPLACED STR TIE SL 152 7. FABBED STR DBLR .063 INCH THK AND SPLICE STRAP .071 INCH THK AT BS SL 1528. INSTALLED IAW SAAB REPAIR NR 72SD1600 S AAB 340 SRM 51-70-20/30 STD PRACTICES. REF: OPER CNTRL NR SIMA 991831, 99ZZZX3626 - 99ZZZX3628. 2 L 7 2 4T RT A52EU 1999100100004 19991001 00004 EU 1999 10 1 99ZZZX3628 1 19990702 A 5313 7253813051 STRINGER SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 222NE 340B222 ABI - DAMAGE TO LOWER FUSELAGE CONSISTING OF TEAR TO SKIN BETWEEN SL 1524, SL 1528, AND BS 622-649, BUCKLING OF FRAMES A T BS 630, 640, 649, FLANGE BUCKLING OF STR TIE SL 1527, 1528. REMOVED DAMAGED AREAS AND STR TIE SL 1527. PERFORMED EDD Y CURRENT INSP. FABBED SKIN SPLICE AND DBLR .050 INCH THK. FABBED FRAME DBLR .040 INCH THK AT BS 630. FABBED DBLR .04 0 INCH THK BS 674 FOR FRAME AT BS 649. FABBED FILLER, DBLR, AND ANGLE .040 INCH THK AT BS 649. REPLACED STR TIE SL 152 7. FABBED STR DBLR .063 INCH THK AND SPLICE STRAP .071 INCH THK AT BS SL 1528. INSTALLED IAW SAAB REPAIR NR 72SD1600 S AAB 340 SRM 51-70-20/30 STD PRACTICES. REF: OPER CNTRL NR SIMA 991831, 99ZZZX3626 - 99ZZZX3627. 2 L 7 2 4T RT A52EU 1999100100011 19991001 00011 NM 1999 10 1 99ZZZX3635 1 19990818 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 106 20289 RIGHT WING FORWARD EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY PACK IAW 33-50-22. 2 L 7 3 4F A3WE 1999100100012 19991001 00012 NM 1999 10 1 99ZZZX3636 1 19990818 A 3350 BATTERY CHARGER BOEING 727 727251 138408H NM FORWARD CABIN FAILED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 3653 20289 LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY CHARGER IAW 33-50-22. 2 L 7 3 4F A3WE 1999100100013 19991001 00013 NM 1999 10 1 99ZZZX3637 1 19990818 A 3350 BATTERY CHARGER BOEING 727 727251 138408H NM AFT CABIN FAILED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 1079 20289 LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY CHARGER IAW 33-50-22. 2 L 7 3 4F A3WE 1999100100014 19991001 00014 NM 1999 10 1 99ZZZX3638 1 19990816 A 3350 BULB BOEING 727 727260 NM CABIN FAILED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 901PG 21978 ONE BULB INOPERABLE ON RIGHT OVERWING FORWARD EMERGENCY LIGHT. RELAMPED. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 1999100100015 19991001 00015 NM 1999 10 1 99ZZZX3639 1 19990816 A 3350 BULB BOEING 727 727260 NM CARGO BAY FAILED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 901PG 21978 ONE BULB INOPERABLE ON EMERGENCY LIGHT ON AFT CARGO DOOR. RELAMPED. OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1999100100016 19991001 00016 NM 1999 10 1 99ZZZX3640 1 19990816 A 3350 LIGHT BOEING 727 727260 NM GALLEY INOPERABLE A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 901PG 21978 EMERGENCY LIGHT (INTERIOR) OVER R2 GALLEY DOOR INOPERABLE. REMOVED AND REPLACED BATTERY PACK PN 9505-42, SN OFF 25262; S/N ON 7071. 2 L 7 3 4F RT A3WE 1999100100017 19991001 00017 NM 1999 10 1 99ZZZX3641 1 19990816 A 3350 LIGHT BOEING 727 727260 NM CABIN INOPERABLE A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 901PG 21978 VARIOUS FLOOR 'E' PATH LIGHTS INOPERABLE. RELAMPED 3 PATHWAY LIGHTS. OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1999100100019 19991001 00019 NM 1999 10 1 99ZZZX3643 1 19990818 A 3350 1102837 LIGHT BOEING 727 727251 138408H NM CABIN INOPERABLE A S84A K NONE O OTHER IN INSP/MAINT 1 EA 21 267US 2681 20289 EMERGENCY LIGHT IN AFT AIRSTAIR AREA INOPERABLE. REMOVED AND REPLACED LIGHT ASSY IAW 33-50-0. M14/M25. 2 L 7 3 4F A3WE 1999100100020 19991001 00020 NM 1999 10 1 99ZZZX3644 1 19990818 A 3350 1102837 LIGHT BOEING 727 727251 138408H NM CABIN INOPERABLE A S84A K NONE O OTHER IN INSP/MAINT 1 EA 21 267US 1886 20289 EMERGENCY LIGHT IN AFT AIRSTAIR AREA INOPERABLE. REMOVED AND REPLACED LIGHT ASSY IAW 33-50-0. M14/M25. 2 L 7 3 4F A3WE 1999100100021 19991001 00021 NM 1999 10 1 99ZZZX3645 1 19990806 A 3260 BULB BOEING 727 727276 138408R NM MLG FAILED A S84A O OTHER L NO TEST NR NOT REPORTED 1 EA 21 908PG 20951 JFK - FLT 302 - WHEN GEAR WAS LOWERED, RIGHT GEAR DID NOT SHOW DOWN. LIGHTS DID NOT TEST. REPLACED BULBS, LOWERED GEAR OPERATED NORMAL. INSPECTED LANDING GEAR POSITION SENSORS. RELAMPED ALL MODULES AND OPS CHECKED (PT7) PER 32-61-01. 2 L 7 3 4F RT A3WE 1999100100022 19991001 00022 NM 1999 10 1 99ZZZX3646 1 19990806 A 3350 SIGN BOEING 727 727276 138408R NM ROW 8 LOOSE A S84A K NONE O OTHER IN INSP/MAINT 1 EA 21 908PG 20951 JFK - FLT 302 - EXIT SIGN IN AISLE AROUND ROW 8 SWAYING. ADJUSTED HOLD-DOWN SCREW AND SECURED SIGN ASSEMBLY. 2 L 7 3 4F RT A3WE 1999100100038 19991001 00038 SO 1999 10 1 99ZZZX3662 1 19990826 A 2134 INLET COUPLING AIRESRCH 18369021 GULSTM G1159 G1159A 3970109 SO HEAT EXCHANGER FAILED A ABFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 01 700SB 8217 21410 334 DURING CLIMB-OUT, CREW NOTICED THE CABIN WAS NOT PRESSURIZING (CABIN WAS CLIMBING WITH AIRCRAFT). THE AIRCRAFT THEN RET URNED TO TAKEOFF POINT. INVESTIGATION OF THE AIRCRAFT REVEALED THE INLET COUPLING ON THE PRIMARY HAT EXCHANGER FAILED R ESULTING IN NO AIR TO THE CABIN FOR PRESSURIZATION OR AIR CONDITIONING. ACTT: 8,216.5. HOURS. ACTC: 5,365. 2 L 7 2 4F A12EA 1999100100040 19991001 00040 EA 1999 10 1 99ZZZX3664 2 19990908 A 8520 75456 CRANKSHAFT PIPER PA31 PA31P 7103120 SO LYC O541 TIGO541E1A 41539 EA ENGINE FAILED A EKIA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 07 252MA 542 31P33 L51662 COUNTERWEIGHT ON NR 3 ATTACH PORT ON CRANKSHAFT CAME OFF. CRANKSHAFT ATTACH PORTS BOTH FAILED. AIRCRAFT RETURNED TO AI RPORT AND LANDED SAFELY. 1 L 7 2 3O 3 O A8EA E19EA 1999100100043 19991001 00043 1999 10 1 AWXA9900323 4 19990921 A 3444 9650648004 COMPUTER BOEING 757 7572S7 1384962 NM E&E COMP MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 904AW 62001 246 23566 MULTIPLE TERRAIN WARNINGS IN FLIGHT IN IMC CONDITIONS, TERRAIN AVOIDANCE PROCEDURES ACCOMPLISHED. PERFORMED T/S IAW FIM 34-46-00 AND REMOVED AND REPLACED GPWS COMPUTER, OPS CHECKED OK IAW TASK CARD F1B34601. 2 L 7 2 4F RT A2NM 1999100100044 19991001 00044 EU 1999 10 1 AWXA9900324 1 19990921 A 2170 20499002 FILTER AIRBUS 320 A320232 3930326 EU AC SYS DIRTY A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 647AW 6965 762 STRONG ODOR NOTICED ON DESCENT, UNABLE TO ISOLATE WHICH PACK WAS PRODUCING SMELL. ENGINE BLEEDS OK, APU BLEED ON SEEMS TO PRODUCE SMELL. REMOVED AND REPLACED LT AND RT OZONE FILTERS, INSPECTED APU INLET, NO OIL LKS NOTED. 2 L 7 2 4F RT A28NM 1999100100045 19991001 00045 NM 1999 10 1 CALA9901267 1 19990918 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 726.75 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17386 26321 INSPECTION FOUND THREE 2 CRACKS IN LOWER KEEL BEAM SKIN PANEL AT BS 726.75, LBL 6 TO RBL 6. THE CRACKS WERE STOP DRILLE D AND REPAIRED IAW SRM 53-60-12, FIGURE 202 AND ECRA 5330-02861. A DIP WAS ISSUED TO REINSPECT BLIND FASTENERS EVERY 3, 000 FLIGHT CYCLES AND ACCOMPLISH A PERMANENT REPAIR NO LATER THAN 12/31/01 OR 20,000 CYCLES, WHICHEVER OCCURS FIRST. 2 L 7 2 4F RT A16WE 1999100100046 19991001 00046 NM 1999 10 1 CALA9901268 1 19990920 A 5753 TRACK BOEING 727 727224 1384076 NM RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT WING NR 5 FLAP TRACK CORRODED. THE FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-31, PAGE 402-41 0. 2 L 7 3 4F A3WE 1999100100047 19991001 00047 NM 1999 10 1 CALA9901269 1 19990920 A 5720 651628912 FITTING BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A .75 INCH CRACK IN RT WING REAR SPAR O/B ATTACH FITTING FOR MLG. THE FITTING WAS REMOVED AND REPLACED IAW ECRA 5740-01901. 2 L 7 3 4F A3WE 1999100100048 19991001 00048 NM 1999 10 1 CALA9901270 1 19990920 A 5720 FITTING BOEING 727 727224 1384076 NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT MLG BEAM H FITTING ATTACH HOLE AND UPPER FORWARD LUG CORRODED. THE ATTACH HOLE WAS REPAIRED IAW ECR A 5740-01903, PAGE 2 AND THE FITTING WAS REPLACED. 2 L 7 3 4F A3WE 1999100100049 19991001 00049 NM 1999 10 1 CALA9901271 1 19990920 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1035 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND FLOOR SUPPORT CORRODED AT CENTERLINE FLOORBEAM, STA 1035. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPP ORT WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999100100050 19991001 00050 NM 1999 10 1 CALA9901272 1 19990920 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 344-380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND G-1 GALLEY SEAT TRACK CORRODED AT STA 344-380. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NE W SECTION WAS INSTALLED IAW SRM 51-30-1, 51-10-06, 53-10-5, AND ECRA 5100-01844. 2 L 7 3 4F A3WE 1999100100051 19991001 00051 NM 1999 10 1 CALA9901273 1 19990920 A 5755 SKIN BOEING 727 727232 1384082 NM NR 7 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND O/B END UPPER SURFACE OF LT WING NR 7 SPOILER DELAMINATED. THE NR 7 SPOILER WAS REMOVED AND REPLACED I AW MM 27-62-1. 2 L 7 3 4F A3WE 1999100100052 19991001 00052 NM 1999 10 1 CALA9901274 1 19990920 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 294-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED AT BS 294-344. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999100100053 19991001 00053 NM 1999 10 1 CALA9901275 1 19990921 A 5320 INTERCOSTAL BOEING 757 757224 1384958 NM BS 700-680 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 700-680, RBL 54. A NEW INTERCOSTAL WAS INSTALLED IAW DRAWING NR 143N5845. 2 L 7 2 4F RT A2NM 1999100100054 19991001 00054 NM 1999 10 1 CALA9901276 1 19990921 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 967-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 967-986, LOWER DOOR JAMB AREA. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999100100055 19991001 00055 WP 1999 10 1 CALA9901277 1 19990922 A 5754 SKIN DOUG DC9 DC982 3022082 WP LT LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND LT SLAT 0 DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 57-6, FIGURE 1. A REPAIR WAS INSTALLED IAW ECRA 5720-01170. 2 L 7 2 4F A6WE 1999100100056 19991001 00056 NM 1999 10 1 CALA9901278 1 19990922 A 5347 SEAT TRACK BOEING 757 757224 1384958 NM BS 532 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 532, LBL 24.75. THE SEAT TRACK WAS REPLACED IAW DRAWING 141N5130. 2 L 7 2 4F RT A2NM 1999100100057 19991001 00057 NM 1999 10 1 CALA9901279 1 19990922 A 5230 SKIN BOEING 757 757224 1384958 NM CARGO DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR AFT LOWER DOOR SKIN. THE AREA WAS REPAIRED IAW ECRA 5231-01020. 2 L 7 2 4F RT A2NM 1999100100058 19991001 00058 NM 1999 10 1 9903962769 1 19990919 A 3260 SWITCH BOEING 727 7272M7 138407S NM NLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 729RW 21742 DURING CLIMB AFTER GEAR RETRACTION, NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL REMAINED ILLUMINATED. CREW RECYCLED GEAR AND LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MSP MAINTENANCE REPLACED BOTH NOSE LANDING GEAR DOOR WARNING SWITCHES, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999100100059 19991001 00059 NE 1999 10 1 9903976730 2 19990921 A 7200 ENGINE BOEING 747 7472J9F 1384806 NM PWA JT9 JT9D7J 52054 NE NR 4 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 GL 01 630US 21668 689632 DURING APPROACH, THE NR 4 ENGINE FLAMED OUT AT APPROXIMATELY 3,500 FEET. FLIGHT CREW CONTINUED APPROACH AND PERFORMED A N UNEVENTFUL LANDING. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED INLET, EXHAUST, AND BLEED PORTS. NO DAMAGE OR DEBRIS WAS FOUND. FUEL PRESSURE AT FP-12 PORT CHECKED AND FOUND WITHIN LIMITS. REPLACED THE FUEL FILTER. ENGINE GROUN D RUN AND ALL PARAMETERS NORMAL. 2 L 7 4 4F 4 F RT A20WE E20EA 1999100100060 19991001 00060 WP 1999 10 1 9903999866 1 19990918 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999100100061 19991001 00061 SO 1999 10 1 COMA9910149 1 19990919 A 5270 WARNING EMB 120 EMB120RT SO SERVICE DOOR ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 247CA 120225 SERVICE DOOR WARNING DURING TAKEOFF. DOOR WARNING SYSTEM PREVIOUSLY DEFERRED PER MEL. 2 L 7 2 4T RT A31SO 1999100100062 19991001 00062 SO 1999 10 1 COMA9910150 1 19990918 A 5270 WARNING EMB 120 EMB120RT SO SERVICE DOOR ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 247CA 120225 SERVICE DOOR WARNING DURING TAKEOFF. DEFERRED DOOR WARNING SYSTEM PER MEL. 2 L 7 2 4T RT A31SO 1999100100063 19991001 00063 NE 1999 10 1 COMA9960534 2 19990918 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT FAILED A COMA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 949CA 7080 807468 RIGHT HAND ENGINE FAILED AFTER TAKEOFF (IFSD). REPLACED THE RIGHT HAND ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999100100064 19991001 00064 EA 1999 10 1 COMA9960535 1 19990917 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA PAX DOOR DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 958CA 71111 EXIT SIGNS AT CABIN DORO ARE INOPERABLE. CLEANED WIRING CONNECTIONS AT FORWARD FLOOR PATH LIGHT STRIP. SYSTEM TEST NOR MAL. 2 L 7 2 4F RT A21EA 1999100100065 19991001 00065 NM 1999 10 1 UPS99230685 1 19990913 A 7830 BRACKET BOEING 727 72731C 1384011 NM NR 3 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, ENGINE NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 78-30-00. 2 L 7 3 4F A3WE 1999100100066 19991001 00066 NM 1999 10 1 UPS99230686 1 19990913 A 7830 BRACKET BOEING 727 72731C 1384011 NM NR 1 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, ENGINE NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW MM 78-30-00. 2 L 7 3 4F A3WE 1999100100067 19991001 00067 NM 1999 10 1 UPS99230687 1 19990913 A 5330 SKIN BOEING 727 72731C 1384011 NM PAX DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, SUSPECT SKIN CRACK AT FWD ENTRY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT IAW EO B727-5330-14 60-C. 2 L 7 3 4F A3WE 1999100100068 19991001 00068 NM 1999 10 1 UPS99230688 1 19990916 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 203 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, CRACK ON SKIN BS 203 WL 219 RT. REPAIRED IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1999100100069 19991001 00069 NM 1999 10 1 UPS99230689 1 19990916 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 251.6 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, CRACK IN SKIN BS 251.6 AT WL 215.5 RT SIDE. REPAIRED IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1999100100070 19991001 00070 WP 1999 10 1 UPS99830651 1 19990920 A 2910 HYD LINE DOUG DC8 DC871F 302199D WP BRAKE SYS LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 748UP 45948 INSPECTION TYPE:N/A, ATB-DISCOVERED HYD QTY LOSS. DECREASED TO AUX WITH ENGINE HYD PUMPS IN BYPASS. AFTER LANDING MX F OUND STAB TRIM HYDRAULIC MOTOR BRAKE RETURN LINE LEAKING. *S/D* INSTALLED INTERIM REPAIR (FLEX LINE) AT THE STAB TRIM HYD BRAKE PER GMM 3-24-1, LEAKS AND OPS CHECK GOOD. TRANSFERRED TO D178926. 2 L 7 4 4F RT 4A25 1999100100071 19991001 00071 WP 1999 10 1 UPS99830681 1 19990907 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, FLOOR WEB CRACKED AT SHACKLEBOX, STA 55, X=-40. REMOVED FLOORBOARD TO GAIN ACCESS TO REPAIR AREA. M AT ID FOR WEB .02 5 2024T3 IAW DC8 SRM 53-3-3 FIG 5 MAT ID FOR REPAIR DOUBLER .025 202 4T3 IAW DC8 SRM 53-2-0 FIG 1B. F ABBED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21 & 53-2-0. 2 L 7 4 4F RT 4A25 1999100100072 19991001 00072 WP 1999 10 1 UPS99830682 1 19990907 A 5245 DOOR TRACK DOUG DC8 DC873F 302199F WP BS 35 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, AIR CONDITIONING COMPT DOOR FWD TRACK IS CRACKED. REMOVED RIVETS, REMOVED TRACK AND REPLACED TRACK WITH RIVETS IAW DC8 S RM 51-1-21. 2 L 7 4 4F RT 4A25 1999100100073 19991001 00073 WP 1999 10 1 UPS99830683 1 19990907 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 45-55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, SHACKLEBOX AND FLOOR WEB ARE CRACKED AT STA 45-55, X=-20. SHACKLEBOX REMOVED, MAT ID FOR DOUBLER RE PAIR 032 2024T3 IAW DC8 SRM 53-2-0 FIG 1B PO NR 297210 MAT ID FOR WEB .025 2024T3 IAW DC8 SRM 53-3-3 FIG 5. FABBED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-0 FIG 1B & 51-1-21. 2 L 7 4 4F RT 4A25 1999100100074 19991001 00074 WP 1999 10 1 UPS99830684 1 19990905 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, STA 1270 SEAT TRACK G HAS CORROSION DOWN CENTER. FABRICATED SPLICE CHANNEL IAW DC8 5320-8309 APP-B. DRILLED AND LOCATED SEAT TRACK SPLICES AND SEAT TRACK IAW DC8 SRM 51-1-24. INSTALLED SEAT TRACK SPLICES & SEAT TRACK IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999100100075 19991001 00075 WP 1999 10 1 UPS99830690 1 19990923 A 5210 MECHANISM DOUG DC8 DC873F 302199F WP PAX DOOR OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A, MAIN CABIN DOOR VERY HARD TO OPEN OR CLOSE. *S/D* ADJUSTED AND TESTED MAIN CABIN DOOR PER MM 52-1 1-01, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999100100076 19991001 00076 EU 1999 10 1 QXEA9901935 1 19990921 A 3350 BULB GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 SEVERAL BULBS OUT IN EMERGENCY EXIT SIGN ABOVE FLIGHT COMPARTMENT ENTERANCE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY, O PERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999100100077 19991001 00077 EU 1999 10 1 QXEA9901936 1 19990922 A 2611 SMOKE ALARM FOKKER F28 F28MK4000 4990810 EU COCKPIT ACTIVATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 491US 11156 BOI- LAVATORY SMOKE ALARM SOUNDED FOR SEVERAL MINUTES DURING CLIMB. NO SMOKE NOTED BY CREW. DEFERED AND PLACED ON RESC HEDULED INSPECTION, IAW MEL 26-7 A & B. AIRCRAFT RETURNED TO SERVICE. FAULT WAS LATER DEEMED TO BE CAUSED BY RESIDUAL OIL FROM APU. 2 L 7 2 4F RT A20EU 1999100100078 19991001 00078 NM 1999 10 1 99FDEA00396 1 19990922 A 5320 65561242 SHEAR TIE BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 278FE 22345 NR 194 - CORROSION ON 950F FRAME WL 154, RBL 9.5. REMOVED CORROSION. INSTALL REPAIR PARTS PER IAW FEDEX SRM 53-10-4, E A 7-5310-97811A. 2 L 7 3 4F RT A3WE 1999100100079 19991001 00079 NM 1999 10 1 DL72L992083 1 19990915 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 660-680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 660 & 680. THE CRACK WAS ROUTED OUT OF TH E SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30, FIG 5 AND ER/A 368263-14AD. 2 L 7 3 4F A3WE 1999100100080 19991001 00080 NM 1999 10 1 DL72L992084 1 19990916 A 5542 SKIN BOEING 727 727232 1384082 NM RUDDER DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 UPPER RUDDER DAMAGED TORN 2 INCHES BY 7 INCHES AT L/E RUDDER STA 180 TO 187. DRILLED UP REPAIR PER SRM 55-20-3 FIG 1. I NSTALLED REPAIR PER SRM 55-20-3. 2 L 7 3 4F A3WE 1999100100081 19991001 00081 NM 1999 10 1 DL72L992085 1 19990915 A 5330 SKIN BOEING 727 727232 1384082 NM BS 685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 THE LOWER SKIN OF THE STRINGER 26R SKIN LAP SPLICE WAS FOUND WITH A 5 INCH LONG AREA OF CORROSION OVER THE UPPER TWO FAS TENER ROWS. THE CORRODED AREA WAS CUT AWAY AND REPAIRED WITH AN INTERNAL REPAIR DOUBLER PER ER/A 368232-14, REV A. 2 L 7 3 4F A3WE 1999100100082 19991001 00082 1999 10 1 DLL10992086 2 19990916 A 7210 GEAR BOX LKHEED 1011 10113851 5265010 WP NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 SO 27 727DA 26845 193C1167 10632 ENGINE OIL QTY WENT TO ZERO SHORTLY AFTER TAKEOFF FROM OGG, OIL PRESS TO 18 LBS AND SLOWLY DECREASING. NORMAL ENGINE SH UT DOWN WITH NORMAL OIL TEMP. ENGINE WINDMILLED 15 MIN WITH 5 LBS OIL PRESS. 2 L 7 3 4F A23WE 1999100100083 19991001 00083 NM 1999 10 1 DL72L992087 1 19990901 A 5320 FRAME BOEING 727 727232 1384082 NM BS 740 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND DURING MV2 CORROSION VISIT NRC 226, CORROSION AT SUPPORT FRAME FOR ACCESS PANEL 3455R AT LWR SURFACE I/B OF FWD HI NGE. REPAIRED PER M/M 53-30-1 FIG 804. 2 L 7 3 4F A3WE 1999100100084 19991001 00084 NM 1999 10 1 DL72S992088 1 19990917 A 2782 BRACKET BOEING 727 727225 1384077 NM NR 8 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 THREE INCH CRACK IN NR 8 SLAT ACTUATOR I/B SUPPORT BRACKET. REPAIRED PER MM 51-20-21. 2 L 7 3 4F A3WE 1999100100085 19991001 00085 NM 1999 10 1 DLM88992089 1 19990917 A 3030 1049491 HEATER DOUG MD88 MD88 3023688 NM RT FUSELAGE FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 947DL 49878 SMOKE IN CABIN AT FL230 60KMI OUT OF CVG - RT SIDE OF A/C AT SEAT 11E. FOUND EVIDENCE OF INSULATION FIRE DUE TO FAULT W ITH ALT STATIC PORT HEATER OR ASSOCIATED WIRING. 2 L 7 2 4F RT A6WE 1999100100086 19991001 00086 1999 10 1 DLM88992091 4 19990917 A 2565 029001305 SLIDE DOUG MD88 MD88 3023688 NM TAIL CONE DEPLOYED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 994DL 53346 TAIL CONE AND SLIDE FOUND DEPLOYED. REPLACED SLIDE AND REINSTALLED TAIL CONE. DEPLOYMENT WAS SUCCESSFUL. 2 L 7 2 4F RT A6WE 1999100100087 19991001 00087 NE 1999 10 1 DL76L992092 2 19990918 A 7397 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 181DN 29851 25986 724656 PER MSU - RECORD WIRE REPAIRED ON INSPECTION OF LT ENG EEC CONTROL WIRES. FOUND 3 WIRES WITH CHAFE ON INSULATION. NO L EGIBLE WIRE NR FOUND. REPAIRED WIRES PER CHAP 20 OF BOEING WIRING MANUAL FWD TO MCO. NO WIRES DAMAGED ONLY INSULATION. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100100088 19991001 00088 NE 1999 10 1 DL73E992093 2 19990918 A 7250 TURBINE BOEING 737 737247 138448D NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 377DL 66240 23604 695203 NR 1 ENG OIL QTY DOWN TO -0-. LOW OIL PRESS LIGHT ILLUMINATED. CREW SHUT DOWN ENG PER POM. FOUND OIL LEAKAGE IN TURBINE SECTION. REPLACED ENGINE. 2 L 7 2 4F 4 F A16WE E2EA 1999100100089 19991001 00089 NM 1999 10 1 DL76S992094 1 19990918 A 3233 ACTUATOR 273T41124 BOEING 767 767332 1382001 NM NLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 00253 24080 NOSE GEAR ACTUATOR FOUND CRACKED AT LOWER END. FOUND DURING LETTER CHECK VISIT. 2 L 7 2 4F RT A1NM 1999100100090 19991001 00090 NM 1999 10 1 DL76G992095 1 19990918 A 3350 0201720001 LIGHT BOEING 767 767332 1382001 NM ROW 32FG INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1602 29694 SEAT MOUNTED PROXIMITY LIGHTING SYSTEM INOP AT 32 FG. RELAMPED SAME AND REPLACED LUMINATOR SOCKET ASSY (2), NO HELP. FWD TO MCO / PLACARD PER MEL 33-51-03B. 2 L 7 2 4F RT A1NM 1999100100091 19991001 00091 NM 1999 10 1 DL757992098 1 19990918 A 5220 ASSIST BOTTLE 80330033 BOEING 757 757232 1384965 NM 2R DOOR LOW PRESSURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL R5664 24390 ON LAYOVER, FOUND DOOR ASSIST POWER RESERVOIR AT DOOR 2R PRESSURE LOW. REPLACED DOOR BOTTLE PER MM. 2 L 7 2 4F RT A2NM 1999100100092 19991001 00092 NM 1999 10 1 DL72W992099 1 19990918 A 3350 900542 POWER SUPPLY BOEING 727 727247 138408F NM ROW 3 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2810W 20648 DURING S/C, FOUND OVERHEAD EMERGENCY EXIT SIGN AT ROW 3 INOP. REPLACED POWER SUPPY RACK ASSY, OPS NORMAL. 2 L 7 3 4F A3WE 1999100100093 19991001 00093 NE 1999 10 1 DL76L992101 2 19990918 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 LT PYLON EEC WIRING UNDER PLATE 432FR, ONE WIRE HAS INSULATION CHAFE. WRAPPED WIRE WITH TAPE UNTIL REPLACEMENT IS DONE AT A LATER DATE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100100094 19991001 00094 WP 1999 10 1 DLL14992102 1 19990919 A 3231 1547856103 ROD LKHEED 1011 1011385115 5265015 WP LT MLG DOOR MISSING A DALA A UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 SO 27 740DA 193C1244 VIBRATION IN FLOOR CAPTS SIDE NEAR SEAT ROWS 31, 32 AND 33. 2 L 7 3 4F A23WE 1999100100095 19991001 00095 NM 1999 10 1 DL733992103 1 19990919 A 2910 AS116080264 LINE BOEING 737 737347 1384647 NM B HYD SYS FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 311WA 23597 LOST TOTAL HYDRAULIC B-SYSTEM OUANTITY. ENGINE NR 2 LOW PRESSURE LIGHT ILLUMINATED. SYSTEM B-PRESSURE BEGAN TO FLUCTUA TE, SYSTEM B QUANTITY DROPPED TO E. ELEC 1 (B SYS) LIGHT THEN ILLUMINATED. FOUND FLEXIBLE HYDRAULIC LINE TO B-SYSTEM E LEC HYDRAULIC PUMP WITH HOLE. REPLACED FLEX LINE, ELEC HYDRAULIC PUMP, AND CASE DRAIN FILTERS. SYSTEM CHECKED GOOD AND A/C RTS AT 2100M. 2 L 7 2 4F RT A16WE 1999100100096 19991001 00096 NM 1999 10 1 DL733992105 1 19990920 A 5312 65163007 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 THE FS 178 BULKHEAD WEB WAS FOUND CRACKED AT THREE LOCATIONS DURING A MV VISIT IN ATL. THE DAMAGE WAS REPAIRED PER ERA 333565 14. 2 L 7 2 4F RT A16WE 1999100100097 19991001 00097 NE 1999 10 1 DL76L992106 2 19990918 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE LT ENGINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 INSP WIRING FOR LEFT ENG EEC, FOUND DAMAGE TO LEFT ENG CONTROL WIRE. MADE APPROVED REPAIR PER BOEING WIRING STD PRACTIC E MNL, FW TO MCO. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100100098 19991001 00098 NM 1999 10 1 DL733992107 1 19990920 A 5743 FITTING BOEING 737 737347 1384647 NM LT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 THE LT MAIN LANDING GEAR BEAM ATTACH FITTING WAS FOUND CRACKED AT MV IN ATLANTA. ERA 333578-14 REPAIRED THE DAMAGE . 2 L 7 2 4F RT A16WE 1999100100099 19991001 00099 NM 1999 10 1 DL733992108 1 19990920 A 5743 FITTING BOEING 737 737347 1384647 NM RT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312WA 23598 THE RT MAIN LANDING GEAR BEAM ATTACH FITTING WAS FOUND CRACKED AT MV. ERA 333585-14 REPAIRED THE DAMAGE. 2 L 7 2 4F RT A16WE 1999100100100 19991001 00100 NM 1999 10 1 DL72W992109 1 19990920 A 2121 6056751 FAN BOEING 727 727247 138408F NM RT PACK FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 2812W 20868 RT PACK PEGGED AC AMP METER, SMOKE IN COCKPIT AND CABIN. REPLACED RT PACK FAN. 2 L 7 3 4F A3WE 1999100100101 19991001 00101 NE 1999 10 1 DL76L992110 2 19990919 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 7460 25061 724687 DURING INSPECTION OF PYLON WIRE HARNESS FOUND TOTAL OF 8 WIRES CHAFED. WIRES REPAIRED PER BOEING STD MANUAL CHAPTER 20. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100100102 19991001 00102 NE 1999 10 1 DL76L992111 2 19990919 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 3280 25061 727830 DURING INSPECTION OF PYLON WIRE HARNESS FOUND 12 WIRES CHAFFED THROUGH INSULATION. REPAIRED WIRES PER BOEING STD MANUAL CHAPT. 20. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100100103 19991001 00103 NE 1999 10 1 DL76L992112 2 19990920 A 7320 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CHAFED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 185DN 30501 27961 723834 FOUND 5 WIRES DAMAGED ON NR 1 ENG PYLON DURING MSU. REPAIRED WIRES PER BOEING STD PRACTICE CHAP 20. WIRES ONLY DAMAGED ON OUTER INSULATION FWD TO MCO PER MSU. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100100104 19991001 00104 NM 1999 10 1 DL72E992113 1 19990921 A 5713 651858913 STRINGER BOEING 727 727247 138408F NM WS 304 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 THE LEFT WING STRINGER 17 WAS FOUND CRACKED AT WS 304. THE DAMAGE WAS REPAIRED PER ERA 333619-14 AT HMV. 2 L 7 3 4F A3WE 1999100100105 19991001 00105 NM 1999 10 1 DL75A992114 1 19990921 A 3350 61020 BATTERY BOEING 757 757212 NM 4R DOOR DRAINED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 751AT 23125 FLASHLIGHT AT 4R DOOR NOT FLASHING. REPLACED BATTERY, CHECK NORMAL. 2 L 7 2 4F RT A2NM 1999100100106 19991001 00106 NM 1999 10 1 DL72S992115 1 19990921 A 5530 CASTING BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 VERT STAB LT TENSION TIE BOLT CASTING CRACKED I/B SIDE. REPLACED FITTING PER BAC DWG 65-17509 REV M. TPA LTR CHK D-2 0 9/21/99. 2 L 7 3 4F A3WE 1999100100107 19991001 00107 NM 1999 10 1 DL72S992116 1 19990921 A 5400 SKIN BOEING 727 727232 1384082 NM S DUCT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 TPA LTR CHK D-2 9/21/99, 1 CRACK ON S-DUCT HOUSING RT SIDE AT UPPER END OF PANEL 9524. REPAIRED PER MM 54-30-0. 2 L 7 3 4F A3WE 1999100100108 19991001 00108 NM 1999 10 1 DL72S992117 1 19990921 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 ONE CRACK ON VERT WEB ABOVE S-DUCT AT STA 1303 ON LT SIDE AT STR CUTOUT. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999100100109 19991001 00109 NM 1999 10 1 DL72S992119 1 19990921 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1250 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 TPA LTR CHK D-2 09/21/99, .625 INCH CRACK AT FUSE SKIN STA 1250 AND STR 21R. REPAIRED PER SRM 53-30-03 FIG 25 AND ERA 3 68334-14. 2 L 7 3 4F A3WE 1999100100110 19991001 00110 NM 1999 10 1 DLM11992120 1 19990921 A 2597 WIRE DOUG MD11 MD11 3023602 NM ROW 11C SHORTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 813DE 48600 WHEN OPERATING B/C SEAT 11C SPARKS AND SMOKE CAME FROM UNDER SEAT. FOUND HARNESS SHORTED TO FOOT REST ACTUATOR. REPAIR ED SAME. 2 L 7 3 4F RT A22WE 1999100100111 19991001 00111 NM 1999 10 1 DLM88992121 1 19990921 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM BS 570 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DL 49591 A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT FS 570 JUST ABOVE LONGERON 26L. THE DAMAGE WAS REPAIRED PER ERA 333518-14 AT HMV. 2 L 7 2 4F RT A6WE 1999100100112 19991001 00112 NM 1999 10 1 DL76K992122 1 19990922 A 3240 BRAKE 321002917 BOEING 767 767332 1382001 NM NR 7 FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 172DZ B5940 29691 ON TAXI OUT BRAKES WERE GRABBING AND CHATTERING. FOUND NR 7 BRAKE FAILED. REPLACED BRAKE AND WHEEL ASSY, ACCT DAMAGED BY BRAKE. ANTI SKID BITE CK NML. 2 L 7 2 4F RT A1NM 1999100100113 19991001 00113 NM 1999 10 1 DLM88992123 1 19990922 A 7312 VALVE 320115DALFH DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 940DL 3524 49813 726077 CLIMBING OUT OF COS, RIGHT ENGINE OIL TEMP EXCEEDED 135 DEGREES ALONG WITH RT FUEL HEAT VALVE OPEN MESSAGE. C/W POM PROC EDURE, NO HELP. AIR TURNBACK TO COS. ON FINAL APPROACH MSG WENT OUT AND TEMP RETURNED TO NORMAL. REPLACED FUEL HEAT V ALVE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999100100114 19991001 00114 NM 1999 10 1 DL72E992124 1 19990909 A 5713 STRINGER BOEING 727 727247 138408F NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 FOUND AT HMV, HFEC SHOWS CRACK INDICATION: R/W STR TO RIB UPPER FWD FASTENER HOLE MARKED NR 7 AT WS 601-5. CUTOUT HOLE PER MM 57-13-0, DRILLED REPAIR ANGLE PER, DISCONNECTED FUEL TRANS TUBE, INSTALLED PARTS, REINSTALLED COVER CONT N/R 1282 , RESTALLED TUBE, SEALED PER MM 57-13-00. 2 L 7 3 4F A3WE 1999100100115 19991001 00115 NM 1999 10 1 DL72S992125 1 19990922 A 5754 STIFFENER BOEING 727 727232 1384082 NM LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 I/B SPAR STIFFENER CRACKED NR 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21 P 813. 2 L 7 3 4F A3WE 1999100100116 19991001 00116 NM 1999 10 1 VNAA9909007 1 19990922 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 442JS 8647 141 3060 A SECTION OF THE EMERGENCY FLOOR LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERG ENCY BATTERY PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIR CRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999100100117 19991001 00117 1999 10 1 SWAA991593 4 19990923 A 2565 65C36533 CABLE BOEING 737 7372H4 138448C NM ESCAPE SLIDE MISINSTALLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE CABLE ROUTED INCORRECTLY. ROUTED CABLE CORRECTLY PER M M. 2 L 7 2 4F A16WE 1999100100118 19991001 00118 NM 1999 10 1 SWAA991594 1 19990923 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR NOT IN VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999100100119 19991001 00119 NM 1999 10 1 SWAA991595 1 19990923 A 5320 6552988 SPLICE BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, STRINGERS 4L AND 4R. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2 L 7 2 4F RT A16WE 1999100100120 19991001 00120 NM 1999 10 1 SWAA991596 1 19990923 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND 3 EACH FUSELAGE FRAMES CRACKED, BS 827, BS 867 AND BS 907, WL 266, LBL 65. REPAIRED FRA MES PER ER 99-6050A. 2 L 7 2 4F RT A16WE 1999100100121 19991001 00121 NM 1999 10 1 SWAA991597 1 19990923 A 5320 65C27314 CLIP BOEING 737 7373H4 1384600 NM BS 767&807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND 2 EACH FUSELAGE STRINGER CLIPS CRACKED, BS 767 AND BS 807, STRINGER 4R. REMOVED AND REP LACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 1999100100122 19991001 00122 NM 1999 10 1 SWAA991598 1 19990923 A 5311 6546804 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND 3 EACH FUSELAGE FRAMES CRACKED, BS 380 AND BS 440, WL 283, LBL 55, AND BS 440, WL 283, RBL 55. REPAIRED FRAMES PER ER 99-6050A. 2 L 7 2 4F RT A16WE 1999100100123 19991001 00123 NM 1999 10 1 SWAA991599 1 19990923 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND BS 986 FLOORBEAM UPPER CHORD CORRODED, LBL 45 - RBL 45. REPAIRED FLOORBEAM PER ER 99-60 52. 2 L 7 2 4F RT A16WE 1999100100124 19991001 00124 NM 1999 10 1 SWAA991600 1 19990923 A 5753 6546435273 SKIN BOEING 737 7373H4 1384600 NM LT TE AFT FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED BC1 CHECK, FOUND LT OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999100100125 19991001 00125 NM 1999 10 1 SWAA991585 1 19990921 A 5320 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED, BS 420, RBL 74. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 1999100100126 19991001 00126 NM 1999 10 1 SWAA991586 1 19990921 A 5311 6546546 FRAME BOEING 737 7373H4 1384600 NM BS 794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED, BS 794, RBL 8, WL 150. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999100100127 19991001 00127 NM 1999 10 1 SWAA991587 1 19990921 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 1. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999100100128 19991001 00128 NM 1999 10 1 SWAA991588 1 19990922 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 14&15 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS LIGHT OUT OF TRACK AND INOP AT ROWS 14 AND 15. REINSTALLED AND RECONNECTED WIRES ON LIGHT ASSY PER MM. OPS CK GO OD. 2 L 7 2 4F RT A16WE 1999100100129 19991001 00129 NM 1999 10 1 SWAA991589 1 19990922 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND FWD SECTION OF EEPLS DIM. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999100100130 19991001 00130 NM 1999 10 1 SWAA991590 1 19990922 A 2560 6567380 COVER BOEING 737 7373H4 1384600 NM DOOR SLIDE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE SHROUD COVER DAMAGED. REPAIRED SHROUD COVER PER MM. 2 L 7 2 4F RT A16WE 1999100100131 19991001 00131 NM 1999 10 1 SWAA991591 1 19990922 A 5320 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND BS 500C SHEAR TIE CRACKED BETWEEN STRINGERS 13L - 14L. REMOVED AND REPLACED SHEAR TIE P ER SRM. 2 L 7 2 4F RT A16WE 1999100100132 19991001 00132 NM 1999 10 1 SWAA991592 1 19990922 A 5753 6573732 SKIN BOEING 737 7373H4 1384600 NM RT TE AFT FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 DURING SCHEDULED C1 CHECK, FOUND RT OUTBOARD AFT FLAP DELAMINATED ON INBOARD CORNER. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 1999100100133 19991001 00133 NM 1999 10 1 SWAA991579 1 19990921 A 3350 6574550 CONNECTOR BOEING 737 7373T0 1384582 NM PAX DOORWAY LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 FWD ENTRY EXTERIOR EMERGENCY ESCAPE LIGHT BEZEL LOOSE AND INOP. RESEATED CONNECTOR ON M1132 BATTERY PACK PER MM. OPS C K GOOD. 2 L 7 2 4F RT A16WE 1999100100134 19991001 00134 NM 1999 10 1 SWAA991580 1 19990921 A 3397 BR2013 WIRE BOEING 737 7377H4 1384404 NM ROW 20 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701GS 27836 EEPLS WIRING LOOSE AT ROW 20. SECURED WIRING AND TRACK PER MM. 2 L 7 2 4F RT A16WE 1999100100135 19991001 00135 NM 1999 10 1 SWAA991581 1 19990921 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM ROW 18 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 706SW 28740 EEPLS LIGHT LOOSE AT ROW 18. SECURED LIGHT ASSY TO TRACK PER MM. 2 L 7 2 4F RT A16WE 1999100100136 19991001 00136 NM 1999 10 1 SWAA991582 1 19990921 A 3350 P2070001 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312SW 23334 AFT LOWER EMERGENCY FLASHLIGHT BLINKER INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 1999100100137 19991001 00137 NM 1999 10 1 SWAA991583 1 19990921 A 5320 6558280 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED FUSELAGE SHEAR TIE, BS 360, BETWEEN STRINGERS 14R-15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999100100138 19991001 00138 NM 1999 10 1 SWAA991584 1 19990921 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SPECIAL VISIT, FOUND 3 EACH STRINGER CLIPS CRACKED, STRINGER 4R, BS 727A, BS 727B, AND BS 767. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F A16WE 1999100100139 19991001 00139 NM 1999 10 1 SWAA991565 1 19990920 A 5312 6517582 BULKHEAD ANGLE BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT OUTBOARD CHORD ANGLE CRACKED, LBL 29, WL 207. REMOVED AND REPLACE D CHORD ANGLE SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999100100140 19991001 00140 1999 10 1 SWAA991566 4 19990919 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999100100141 19991001 00141 NM 1999 10 1 SWAA991567 1 19990920 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED 18 INCHES BELOW AFT ENTRY DOOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999100100142 19991001 00142 NM 1999 10 1 SWAA991568 1 19990920 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING WALK ARROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 727D, STRINGER 18L AND STRINGER 18R. REPAIRED CRACKS PE R SRM. 2 L 7 2 4F RT A16WE 1999100100143 19991001 00143 NM 1999 10 1 SWAA991569 1 19990919 A 3350 604068 BATTERY BOEING 737 7372H4 138448C NM LT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999100100144 19991001 00144 NM 1999 10 1 SWAA991570 1 19990919 A 5320 6546526 SHEAR TIE BOEING 737 7372H4 138448C NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED BS 400, STRINGER 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999100100145 19991001 00145 NM 1999 10 1 SWAA991571 1 19990919 A 5330 6552988 SKIN BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE AT FUSELAGE SKIN, BS 947, STRINGER 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999100100146 19991001 00146 NM 1999 10 1 SWAA991572 1 19990919 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 24 INCHES BELOW AFT ENTRY DOOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999100100147 19991001 00147 NM 1999 10 1 SWAA991573 1 19990920 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 EEPLS MISSING COVER AT OVERWING EXIT. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999100100148 19991001 00148 NM 1999 10 1 SWAA991574 1 19990920 A 5330 6545877 SKIN BOEING 737 7372H4 138448C NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 312, STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999100100149 19991001 00149 NM 1999 10 1 SWAA991575 1 19990920 A 3350 6574550 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED D CHECK, FOUND AFT LT AND RT EMERGENCY EVACUATION SLIDE EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT A SSY'S PER MM. 2 L 7 2 4F A16WE 1999100100150 19991001 00150 NM 1999 10 1 SWAA991576 1 19990920 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON BS 986 FLOORBEAM, RBL 20 - RBL 40. REPAIRED BEAM PER ER 99-6080 AND SRM . 2 L 7 2 4F RT A16WE 1999100100151 19991001 00151 NM 1999 10 1 SWAA991577 1 19990917 A 5230 6547953 SKIN BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED SERVICE CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT SKIN CRACKED. REPAIRED SKIN PER SWA RA NR 1-252-0336 . 2 L 7 2 4F A16WE 1999100100152 19991001 00152 NM 1999 10 1 SWAA991578 1 19990920 A 5542 65C25841 SKIN BOEING 737 7373A4 1384585 NM RUDDER. DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED SERVICE CHECK, FOUND LT UPPER SIDE OF RUDDER CONDUCTIVE MATERIAL SKIN PEELED BACK. REPAIRED SKIN PER S WA RA NR 1-355-0314. 2 L 7 2 4F RT A16WE 1999100100153 19991001 00153 NM 1999 10 1 SWAA991553 1 19990918 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 10. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999100100154 19991001 00154 NM 1999 10 1 SWAA991554 1 19990918 A 5753 654643 SKIN BOEING 737 7373H4 1384600 NM TE FLAPS DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED C3 CHECK, FOUND LT AND RT OUTBOARD AFT FLAPS DELAMINATED ON INBOARD CORNERS. REMOVED AND REPLACED BOTH AFT FLAPS PER MM. 2 L 7 2 4F RT A16WE 1999100100155 19991001 00155 1999 10 1 SWAA991555 4 19990918 A 2565 63551101 SLIDE BOEING 737 7377H4 NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 750SA 29802 AFT SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999100100156 19991001 00156 NM 1999 10 1 SWAA991556 1 19990917 A 5330 6545802 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FUSELAGE SKIN, FWD SERVICE DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER ER NR 99-6084A. 2 L 7 2 4F RT A16WE 1999100100157 19991001 00157 NM 1999 10 1 SWAA991557 1 19990917 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM BS 440 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE ON FUSELAGE SKIN, BS 440, BETWEEN STRINGERS 27R- 28R. REPAIRED SKIN PER DALFORT XEA X2-53-255. 2 L 7 2 4F A16WE 1999100100158 19991001 00158 1999 10 1 SWAA991558 4 19990917 A 2565 63550101 SLIDE BOEING 737 7377H4 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 742SW 29278 FWD SERVICE DOOR EVACUATION SLIDE DEPLOYED ACCIDENTALLY. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999100100159 19991001 00159 1999 10 1 SWAA991559 4 19990917 A 2565 D31354 SLIDE BOEING 737 7373T5 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 668SW 23060 FWD SERVICE DOOR EVACUATION SLIDE DEPLOYED ACCIDENTALLY. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999100100160 19991001 00160 NM 1999 10 1 SWAA991560 1 19990917 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM SERVICE DOOR BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 623SW 27933 AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999100100161 19991001 00161 NM 1999 10 1 SWAA991561 1 19990917 A 3350 P2070001 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 105SW 23249 FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY. 2 L 7 2 4F A16WE 1999100100162 19991001 00162 NE 1999 10 1 SWAA991562 2 19990918 A 7320 8901326 T2 SENSOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 383SW 26589 ABORTED TAKEOFF, NR 2 ENG SLOW TO ACCELERATE DURING TAKEOFF. REMOVED AND REPLACED NR 2 ENG T2 SENSOR, AND ADJUSTED SPEC IFIC GRAVITY. OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999100100163 19991001 00163 NM 1999 10 1 SWAA991563 1 19990918 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM ROW 11 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26573 EEPLS TRACK COVER MISSING AT ROW 11. REPLACED COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 1999100100164 19991001 00164 NM 1999 10 1 SWAA991564 1 19990918 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 8 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 637SW 27710 EEPLS LIGHT INOP AT ROW 8. RECONNECTED EEPLS WIRING PER MM. 2 L 7 2 4F RT A16WE 1999100100165 19991001 00165 WP 1999 10 1 TWAA9913101 1 19990912 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND NUMBER 3 CHAIR TRACK CORRODED BETWEEN STA 200 AND 218. REPLACED TRACK PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999100100166 19991001 00166 WP 1999 10 1 AT9900641 1 19990910 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 574 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 DURING RAMP OPERATIONS, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT BS 574 BETWEEN LONGERONS 29L AND 29R. THE AREA HAS AN EXISTING SKIN CUTOUT AND AN EXTERNAL DOUBLER. CRACKS WERE ALSO FOUND ON 2 LONGERONS. THE DAMAGED SKIN AND EXISTING REPAIR WERE REMOVED. A NEW SKIN SECTION WAS FABRICATED AND SPLICED IN PLACE FROM BS 550 TO BS 588 BETWEEN L-26L AND L-2 6R IAW TIMCO RES NR 05013 AND EO NR 99-1255. THE LONGERONS WERE REPAIRED BY SPLICING IN NEW SECTIONS IAW DC9 SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 1999100100167 19991001 00167 NM 1999 10 1 UPS99230708 1 19990913 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 259.5 LIGHTNING STRIKE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C LIGHTNING STRIKE BS 259.5 BETWEEN S20R AND 21R. REPAIRED IAW SRM 53-30-03 FIG 20. 2 L 7 3 4F A3WE 1999100100168 19991001 00168 NM 1999 10 1 UPS99230709 1 19990914 A 5320 WEB BOEING 727 72731C 1384011 NM BS 1306 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C CRACK ON WEB AT LT SIDE OF AIRSTAIRS AT STA BS 1306 AT LWR LIGHTNING HOLE CRACK STOP DRILLED IAW S RM CH 51-10-2 . AREA REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999100100169 19991001 00169 NM 1999 10 1 UPS99230710 1 19990914 A 5523 SKIN BOEING 727 72731C 1384011 NM LT ELEV TAB DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C SMALL DENT ON LWR SKIN OF LT ELEV TAB AT OUTBOARD END. REPAIRED IAW SRM 51-40-6 FIG 39. 2 L 7 3 4F A3WE 1999100100170 19991001 00170 NM 1999 10 1 UPS99230711 1 19990916 A 5753 SKIN BOEING 727 72731C 1384011 NM RT TE FOREFLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C DENT ON UPPER SURFACE OF RT O/B FORE FLAP UPPER SURFACE MID-SPAN. REPAIRED IAW SRM 51-40-6 FIG 35. 2 L 7 3 4F A3WE 1999100100171 19991001 00171 NM 1999 10 1 UPS99230712 1 19990916 A 5753 BRACKET BOEING 727 72731C 1384011 NM TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C ON INSP BRACKET FOUND CRACKED ON NR 1 FLAP TRACK MID FLAP FAIRING. REMOVED FAIRING TRACK FOR ACCESS I AW SRM 51-30-2. REMOVED CRACKED BRACKET IAW SRM 51-30-02. INSTALLED BRACKET IAW SRM 51-30-02. INSTALLED FLAP TRACK IA W SRM 51-30-02. 2 L 7 3 4F A3WE 1999100100172 19991001 00172 NM 1999 10 1 UPS99230713 1 19990915 A 5280 SKIN BOEING 727 72731C 1384011 NM LT MLG DOOR NICKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C LT LANDING GEAR DOOR OUTER SECTION HAS NICK ON OUTER SKIN -30 APPROX FROM FWD END. DAMAGED AREA CUT O UT AND REPAIR CARRIED OUT IAW SRM 52-80-02. 2 L 7 3 4F A3WE 1999100100173 19991001 00173 NM 1999 10 1 UPS99530715 1 19990915 A 5743 TRUNNION BOEING 757 75724APF 1384969 NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 403UP 23725 INSPECTION TYPE:C LT MLG FWD TRUNNION BRG BORE HAS CORROSION AT REAR SPAR. REMOVED LT FWD TRUNNION BRG SUPPORT BRACKET. REMOVED LT BEARING SUPPORT. REMOVED BEARING FROM SUPPORT CLEAN AND INSPECT SUPPORT REINSTALLED. 2 L 7 2 4F RT A2NM 1999100100174 19991001 00174 NM 1999 10 1 UPS99530716 1 19990915 A 5743 S113N1081 TRUNNION BOEING 757 75724APF 1384969 NM RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 403UP 23725 INSPECTION TYPE:C CORROSION (C57-651-02-11) RT MLG TRUNNION BRG BORE HAS CORRODED AT REAR SPAR REMOVED AND REPLACED FWD TRUNNION BEARING MM 57-54-05 PARA 2 PG 401 2 L 7 2 4F RT A2NM 1999100100175 19991001 00175 WP 1999 10 1 UPS99830691 1 19990922 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 1 INCH CRACK LEFT WING LWR SURFACE (18 INCHES INBOARD NR 1 PYLON). 2 L 7 4 4F RT 4A25 1999100100176 19991001 00176 WP 1999 10 1 UPS99830692 1 19990910 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 AFT PIT FS 1240 FITTING THAT CONNECTS INTERCOSTAL TO FRAME AT L35R IS CRACKED. REMOVE AND REPLACE F ITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100177 19991001 00177 WP 1999 10 1 UPS99830693 1 19990908 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 STA 1140 35R LONGERON FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-2. 2 L 7 4 4F RT 4A25 1999100100178 19991001 00178 WP 1999 10 1 UPS99830694 1 19990907 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 BATHTUB FITTING AT FS 860 L5L CRACKED. REMOVED OLD FITTING, LOCATED, DRILLED AND INSTALLED NEW FITTI NG P/N 37 79659-501 PER DC8 SRM 51-1-20D, 51-1-21, 51-3-0, AND 51-3-1. 2 L 7 4 4F RT 4A25 1999100100179 19991001 00179 WP 1999 10 1 UPS99830695 1 19990907 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 LONGERON 3R BATHTUB FITTING AT FS 860 IS CRACKED. REMOVED AND REPLACED FITTING P/N 3779659-501N IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100180 19991001 00180 WP 1999 10 1 UPS99830696 1 19990907 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 LONGERON 4R BATHTUB FITTING AT FS 860 IS CRACKED. REMOVED AND REPLACED FITTING P/N 3779659-501N IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100181 19991001 00181 WP 1999 10 1 UPS99830697 1 19990907 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 LONGERON 7R BATHTUB FITTING AT FS 860 IS CRACKED. REMOVED AND REPLACED FITTING P/N 3779654-501N IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100182 19991001 00182 WP 1999 10 1 UPS99830698 1 19990915 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 AFT PIT FITTING AT FS 1180 L29L-L30L CORRODED. REMOVED FITTING, DRILLED UP NEW FITTING IAW DC8 SRM 5 1-3-2. INSTALL ED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100183 19991001 00183 WP 1999 10 1 UPS99830699 1 19990906 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 1 SPOILER PUNCTURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 PUNCTURE, UNDERSIDE NR 1 SPOILER, DOT E972. MATERIAL ID FILLER AND DOUBLER 7075-T-6.016 PO NR 271715 , FABBED FILLER AND DOUBLER IAW SRM 51-1-9A. BONDED FILLER AND DOUBLER IAW DC8 SRM 51-1- 9A. REINSTALLED SPOILER IAW DC8 MM 27-61-01. 2 L 7 4 4F RT 4A25 1999100100184 19991001 00184 WP 1999 10 1 UPS99830700 1 19990908 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 FRAME FITTING AT STA 840 LEFT CRACKED P/N 3779978-2. REMOVED CRACKED FITTING, FABRICATED NEW FITTING ON TIMCO ROUTINE 197 126, 50015 AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100185 19991001 00185 WP 1999 10 1 UPS99830701 1 19990920 A 5312 BULKHEAD ANGLE DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 CORROSION ON AND AROUND T-ANGLE AND FASTENERS AT STA 70 BULKHEAD, RBL 28. REMOVED BOLTS IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW DC8 SRM 51- 1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED ANGLE P/N NR 2615487-1 PO NR 304895. REMOVED CORROSION AROUND L-ANGLE, WITHIN LIMITS. LOCATED, DRILLED AND DEBURRED ANGLE IAW DC8 SRM 51-1-24. IN STALLED ANGLE IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999100100186 19991001 00186 WP 1999 10 1 UPS99830702 1 19990908 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 STA 640 LONGERON 31R CORRODED, DOT F-744. REPAIRED IAW REO 06757. 2 L 7 4 4F RT 4A25 1999100100187 19991001 00187 WP 1999 10 1 UPS99830703 1 19990907 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 RT WING UPPER SIDE FUEL TANK ACCESS PANEL 505F CUTOUT CRACKED 2 PLACES. MAT ID FOR EXTERNAL DOUBLER 7075-T6.160 PO NR 287514, INTERNAL DOUBLER 7075-T6.063 PO#300912, AND FILLER 7075-T6.375 PO NR 254136, IAW DC8 SRM 5 7-2 -1. FABBED DOUBLERS AND FILLER IAW DC8 SRM 57-2-1. CUT OUT DAMAGED AREA IAW DC8 SRM 57-2-1. INSTALLED ALL PARTS IAW D C8 SRM 57-2-1 AND 51-1-20D. LEAK CHECK TO PERFORMED ON UPS TASK CARD NR 8000. 2 L 7 4 4F RT 4A25 1999100100188 19991001 00188 WP 1999 10 1 UPS99830704 1 19990906 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 RT LONGERON 24 FITTING AT STA 879 HAS CORROSION FWD AND AFT (REMOVED FITTING AND FOUND 2 CRACKS). RE MOVED FITTING, REMOVED CORROSION. REPAIRED CRACKS ON LONG 24 WITH REPAIR ANGLES IAW DC8 SRM 53-2-2 FIG 5. 2 L 7 4 4F RT 4A25 1999100100189 19991001 00189 WP 1999 10 1 UPS99830705 1 19990906 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 INTERCOSTAL AT FS 280, LONGERON 11R IS BENT, CRACKED AND CORRODED. REMOVED DAMAGED INTERCOSTAL. FAB RICATED NEW INTERCOSTAL IAW DAC DWG 3704510. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100190 19991001 00190 WP 1999 10 1 UPS99830706 1 19990905 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1600 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 STA 1600 19 ABOVE CUSP, FRAME AS DRILL DAMAGE IN RADIUS OF FLANGE GEN RFTS N836UP-03-20183 ON 9-7-99, REC'D RFTS 9-8-99. MATERIAL VERIF ICATION 7075-0.071 PO NR 296823, FABBED FILLER AND SPLICES IAW DC8 SRM 53 -2-0; LOCA TED, DRILLED AND TRIMMED FILLER AND SPLICES IAW DC8 SRM 53-2-0 . INSTALLED FILLER AND SPLICES IAW DC8 SRM 53-2-0, 51-1- 20D. 2 L 7 4 4F RT 4A25 1999100100191 19991001 00191 WP 1999 10 1 UPS99830707 1 19990905 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1580 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 STA 1580 R/S 26 ABOVE CUSP FRAME AND GUSSETT HAS DRILL DAMAGE. REMOVED DAMAGED GUSSETT AND FASTENER IAW DC8 SRM 51-21-1. REMOVED DAMAGE FROM FRAME IAW REO 06735. FABBED AND INSTALLED NEW GUSSET AND REPAIR ANGLE IAW DAC DWG 9751061, REO 06735, AND DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999100100192 19991001 00192 WP 1999 10 1 UPS99830714 1 19990924 A 3510 15830M REGULATOR DOUG DC8 DC873F 302199F WP RT COCKPIT INOP A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 CO-PILOTS OXYGEN DOES NOT SHUTOFF WHEN IN THE OFF POSITION. REMOVED AND REPLACED CO-PILOTS O2 REGULATOR ASSY, LEAK CHEC K AND OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999100100193 19991001 00193 NE 1999 10 1 99FDEA00397 2 19990924 A 7200 ENGINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A FDEA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 25 268FE 21674 99-244 - NR 3 ENG COMPRESSOR STALL. BLEED WAS FEED RIGHT PACK. REMOVED AND REPLACED NR 3 ENG PER WORK CARD 70T0001-03 OPER CK GOOD. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 1999100100194 19991001 00194 WP 1999 10 1 ABXA9900723 1 19990918 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOP A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 938AX 199 47009 EMERGENCY EVACUATION LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SOURCE. 2 L 7 2 4F A6WE 1999100100195 19991001 00195 WP 1999 10 1 ABXA9900724 1 19990920 A 4930 3917259501 FUEL LINE DOUG DOUG DC9 DC931 3022065 WP APU COMP LOOSE A ABXA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 937AX 47074 ON DESCENT, FUEL/EXHAUST FUMES SMELL COMING FROM AIR CONDITIONING SYSTEM. CREW USED OXYGEN FROM 1300 FEET. RETORQUED F UEL LINE IN APU COMPARTMENT. 2 L 7 2 4F A6WE 1999100100196 19991001 00196 NM 1999 10 1 DHL99740004 1 19990924 A 2611 303261 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM CARGO COMPT FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 740DH 21930 CARGO SMOKE WARNING LIGHT CAME ON IN FLIGHT AT FL 290. PERFORMED EMERGENCY LANDING AT SDF. REMOVED AND REPLACED SMOKE DETECTOR AMO PER MM 26-13-10. 2 L 7 3 4F RT A3WE 1999100100197 19991001 00197 NM 1999 10 1 DHL99741004 1 19990921 A 3260 RELAY BOEING 727 7272Q9 138448M NM LT MLG FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 741DH 21931 AFTER TAKEOFF, GEAR HANDLE WOULD NOT GO PAST OFF. TAKEOFF WARNING HORN SOUNDED WHEN FLAPS RETRACTED TO 2 DEGREES. CHEC KED HANDLE, REMOVED AND REPLACED R92 SAFETY RELAY NAD AIR SENSOR ON LEFT GEAR. CHECKED WIRING AS PER WD 32-31-01. TREA TED GEAR HANDLE OPERATION PER MM 32-31-11. OPERATION FOUND TO BE NORMAL. 2 L 7 3 4F RT A3WE 1999100100198 19991001 00198 SO 1999 10 1 SWIA971564 1 19990901 A 5220 DOOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT EMER EXIT NOT LATCHED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 292SW 120319 UNABLE TO PRESSURIZE CABIN. RETURNED TO SLC. LATCHED RIGHT FOWARD EMERGENCY EXIT. EXIT NOW SECURE. NO OTHER PRESSUR IZATION PROBLEMS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999100100199 19991001 00199 SO 1999 10 1 SWIA971565 1 19990905 A 7712 TQ PROBE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 229SW 120305 DURING FLIGHT, RIGHT TORQUE FLUCTUATES FROM 64 PERCENTS DOWN TO 0 PERCENTS (ANALOG AND DIGITAL). RETURNED TO SFO. REPL ACED RIGHT ENGINE TORQUE PROBE. OPS CHECKED GOOD ON ENGINE RUN. 2 L 7 2 4T 4 T RT A31SO E20NE 1999100100200 19991001 00200 NE 1999 10 1 SWIA971566 2 19990907 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118A NE RIGHT MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 284YV 120284 INADVERTENT AUTOFEATHER AT 1200 FEET. TORQUE WENT TO 146 PERCENT ON LEFT ENGINE. RETURNED TO LAX. INSTALLED SERVICEAB LE LEFT ENGINE IAW MM 71-00-00. CHANGED LEFT PROPELLER ALSO. CAUSE OF AUTOFEATHER UNKNOWN UNTIL FURTHER TEARDOWN OF CO MPONENTS COMPLETED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999100100208 19991001 00208 SO 1999 10 1 99ZZZX3674 1 19990907 A 8120 4091709001 TURBOCHARGER GARRTT PIPER PA31 PA31350 7103110 SO EXHAUST FAILED A BSYA A UNSCHED LANDING K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 07 2KC 8525 1509 AG023046 317952217 RIGHT ENGINE CUT BACK ON POWER AFTER TAKEOFF OUT OF CLE. RETURNED TO CLE AND HAD MAINT LOOK AT ENGINE. MAINTENANCE FOU ND OIL COMING OUT THE EXHAUST OF TURBOCHARGER. OPS CHECKS GOOD. 1 L 7 2 3O A20SO 1999100100214 19991001 00214 NE 1999 10 1 99ZZZX3680 2 19990823 A 8520 BEARING DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE LEFT ENGINE FAILED A VLLA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 05 907Z 22738 1148 12300 CP360143 AT CRUISE POWER SETTING, LEFT ENGINE LOST POWER. AIRCRAFT DIVERTED TO VIN. FOUND METAL IN SCREEN AND REAR VALVES NOT M OVING. SUBMITTER SUSPECTED REAR MAIN BEARING FAILURE. 2 L 7 2 4R 4 R A669 5E4 1999100100218 19991001 00218 NE 1999 10 1 99ZZZX3684 1 19990823 A 7600 23065125 GOVERNOR SKRSKY S76 S76A 8143006 NE NR 2 ENGINE FAILED A ALGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 519AL 5094 1105 760058 AFTER LEVELING OFF AT 3,500 FEET, A LARGE TORQUE SPLIT WITH NR 2 ENGINE DROPPING TO 61 PERCENT N1 - T5 450 DEGREES TORQU E 30 PERCENT, COLLECTIVE WAS REDUCED TO CONTROL TORQUE AND T5 ON ENGINE NR 1 AND MAINTAINED LEVEL FLIGHT. DIVERTED FOR LANDING. REPLACED GOVERNOR AND BEEP MOTOR AND TORQUE SHAFT. 1 G 7 2 3U H1NE 1999100100219 19991001 00219 NE 1999 10 1 99ZZZX3685 1 19990823 A 7600 7630103501042 BEEP MOTOR SKRSKY S76 S76A 8143006 NE NR 2 ENGINE FAILED A ALGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 519AL 5094 1105 760058 AFTER LEVELING OFF AT 3,500 FEET, A LARGE TORQUE SPLIT WITH NR 2 ENGINE DROPPING TO 61 PERCENT N1 - T5 450 DEGREES TORQU E 30 PERCENT, COLLECTIVE WAS REDUCED TO CONTROL TORQUE AND T5 ON ENGINE NR 1 AND MAINTAINED LEVEL FLIGHT. DIVERTED FOR LANDING. REPLACED GOVERNOR AND BEEP MOTOR AND TORQUE SHAFT. 1 G 7 2 3U H1NE 1999100100220 19991001 00220 NE 1999 10 1 99ZZZX3686 1 19990823 A 7600 7630103004042 TORQUE SHAFT SKRSKY S76 S76A 8143006 NE NR 2 ENGINE FAILED A ALGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 519AL 5094 1105 760058 AFTER LEVELING OFF AT 3,500 FEET, A LARGE TORQUE SPLIT WITH NR 2 ENGINE DROPPING TO 61 PERCENT N1 - T5 450 DEGREES TORQU E 30 PERCENT, COLLECTIVE WAS REDUCED TO CONTROL TORQUE AND T5 ON ENGINE NR 1 AND MAINTAINED LEVEL FLIGHT. DIVERTED FOR LANDING. REPLACED GOVERNOR AND BEEP MOTOR AND TORQUE SHAFT. 1 G 7 2 3U H1NE 1999100100221 19991001 00221 WP 1999 10 1 TWAA9913201 1 19990924 A 3350 58531 CONDUCTOR DOUG DC9 DC932 3022066 WP CABIN WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 923L 47109 THE FWD SECTION OF COACH FLOOR EGRESS LIGHTING WAS INOPERATIVE IN TEST. REPLACED THE CONDUCTOR STRIP FROM THE BATTERY T O THE LIGHT STRIP. CHECK-C 3-26-99 MCI. 2 L 7 2 4F A6WE 1999100100222 19991001 00222 WP 1999 10 1 TWAA9913202 1 19990925 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9303K 49529 THE EMERGENCY LIGHTS WERE INOPERATIVE IN THE AFT TAIL CONE AREA. REPLACED THE POWER SUPPLY. CHECK-C 11-25-98 MCI. 2 L 7 2 4F RT A6WE 1999100100223 19991001 00223 WP 1999 10 1 TWAA9913203 1 19990926 A 2120 AIR DIST DOUG DC9 DC983 3022083 WP CABIN SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 964TW 53614 IN CRUISE CABIN GRADUALLY FILLED WITH BLUE SMOKE AND OIL SMELL. CABIN TEMP WAS TURNED DOWN AND ANTI ICE TURNED OFF. RT PACK PRESSURE WAS 10 PSI WHEN SMOKE APPEARED BUT RETURNED TO NORMAL WHEN ENG ANTI ICE TURNED OFF. BLUE SMOKE AND OIL S MELL GRADUALLY DISIPATED. INSPECTED RT ENG 13TH AND 8TH STAGE END CAPS FOR SIGNS OF OIL CONTAMINATION. NO OIL NOTICED. INSPECTED INLET FOR SIGN OF OIL LEAKAGE BUT NO LEAKS NOTED. ENG OIL QTY FULL. PERFORMED OP CHECK OF RH PACK IN AUTO AND MANUAL FULL HOT AND COLD AND NO DEFECTS NOTED. 2 L 7 2 4F RT A6WE 1999100100224 19991001 00224 1999 10 1 TWAA9913204 4 19990926 A 2565 61571128 SLIDE BOEING 757 757231 1384950 NM R4 DOOR WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 714P 28482 WHILE PARKED AT THE GATE THE NUMBER 4 CABIN DOOR ON THE RT SIDE OF THE AIRCRAFT WAS OPENED WHILE THE ESCAPE SLIDE WAS AR MED. THE ESCAPE SLIDE DID NOT FULLY DEPLOY. REPLACED THE ESCAPE SLIDE. CHECK-C 2-20-99 LAX. 2 L 7 2 4F RT A2NM 1999100100225 19991001 00225 NM 1999 10 1 RAAA99B1017 1 19990905 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM AIRSTAIR DIRTY A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 AIRSTAIR EMERGENCY LIGHT INOP. CLEANED BATTERY CONTACTS. 2 L 7 3 4F A3WE 1999100100226 19991001 00226 SO 1999 10 1 RAAA99E8051 1 19990802 A 3350 86210144 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 11CDE DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 PAX ROW 11CDE EXIT ID LIGHT WILL NOT TEST. REPLACED BATTERY. 2 L 7 4 4T 4A22 1999100100227 19991001 00227 SO 1999 10 1 RAAA99E8052 1 19990919 A 3350 86210144 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 11AB DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY LIGHT AT ROW 11AB INOP. REPLACED BATTERY. 2 L 7 4 4T 4A22 1999100100228 19991001 00228 SO 1999 10 1 RAAA99E9024 1 19990822 A 3350 86210144 BATTERY PACK INTVLV 87300112 LKHEED 188 188C 5262604 SO ROW 17CDE DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 17 CDE WILL NOT TEST. REPLACED BATTERY. 2 L 7 4 4T 4A22 1999100100229 19991001 00229 NM 1999 10 1 RAAAB1018 1 19990906 A 3350 900835A BATTERY PACK GRIMES 1000679LB BOEING 727 72722C 138400F NM LT EMER EXIT DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 LEFT AFT EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999100100230 19991001 00230 SO 1999 10 1 COMA9910151 1 19990919 A 3234 12038594001 SELECTOR EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 258CA 1247 GEAR SELECTOR WOULD NOT MOVE TO UP POSITION AFTER TAKEOFF. COULD NOT DUPLCIATE WRITE-UP, GEAR SWUNG IAW 32-30-00. 2 L 7 2 4T RT A31SO 1999100100231 19991001 00231 SO 1999 10 1 COMA9910152 1 19990921 A 3260 DP120 SENSOR EMB 120 EMB120RT SO NLG FAIELD A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 269CA 1263 AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATION WAS RED B, LIGHTS REMAINED ON AFTER CYCLING GEAR. REMOVED AND R EPLACED NOSE LANDING GEAR PROX SENSOR FOR B SYSTEM. 2 L 7 2 4T RT A31SO 1999100100232 19991001 00232 SO 1999 10 1 COMA9910153 1 19990921 A 3350 363782 BULB EMB 120 EMB120RT SO ROW 9A FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 267CA 1259 FLOOR TRACK LIGHT AT SEAT 9A IS INOPERABLE. REMOVED AND REPLACED BULB. 2 L 7 2 4T RT A31SO 1999100100233 19991001 00233 NE 1999 10 1 COMA9910154 2 19990921 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE NR 1 FAILED A COMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 249CA 1230 115660 EN ROUTE AT 15,000 NR 1 ENGINE FAILED. EEC LIGHT/ENGINE OIL PRESSURE LIGHT ON MAP, ENGINE FAILED TO FEATHER DURING SHUT DOWN. REPLACED LEFT ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999100100234 19991001 00234 EA 1999 10 1 COMA9960536 1 19990924 A 2150 601R956205 TRANSDUCER CNDAIR CL600 CL6002B19 EA RT PACK FAILED A COMA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 SO 01 977CA 7157 DURING CLIMBOUT, THE RIGHT AIR CONDITIONING PACK INDICATED A HIGH PRESSURE FAULT. REPLACED THE RIGHT PACK PRESSURE TRAN SDUCER. 2 L 7 2 4F RT A21EA 1999100100235 19991001 00235 NE 1999 10 1 COMA9960537 2 19990918 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 945CA 7069 807384 IDG NR 2 CAUTION MESSAGE, FOLLOWED BY GEN NR 2 CAUTION MESSAGE ON TAKEOFF. IDG NR 2 CAUTION MESSAGE WENT OUT DURING ABO RT. NR 2 GEN WAS RESET. FOUND SKYDROL IN ACCESSORY GEARBOX OF RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999100100236 19991001 00236 1999 10 1 COMA9960538 2 19990919 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA RIGHT FAILED A COMA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 01 945CA 7069 ON CLIMBOUT, RIGHT ENGINE OIL PSI MESSAGE ON ED-1 SHUT DOWN NR 2 ENGINE. DROPPED TO 22 PSI. FOUND SKYDROL IN ACCESSORY GEARBOX. REMOVED AND REPLACED RIGHT ENGINE. 2 L 7 2 4F RT A21EA 1999100100237 19991001 00237 EA 1999 10 1 COMA9960539 1 19990919 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 95.95 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 7159 SEVEN SMALL CRACKS IN THE FWD AND AFT HORIZONTAL SURFACES OF RIGHT HAND WING ACCESS HOLE AT PANEL 640 DB. REPAIRED CRAC KS IAW BOMBARDIER REO NR 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999100100238 19991001 00238 EA 1999 10 1 COMA9960540 1 19990921 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA ROW 5 FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 EMERGENCY LIGHT IN CEILING ABOVE ROW 5 IS INOPERABLE. REMOVED AND REPLACED BULK. 2 L 7 2 4F RT A21EA 1999100100239 19991001 00239 EA 1999 10 1 COMA9960541 1 19990921 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 932CA 7038 RIGHT OVERWING EXIT SIDEWALL EMERGENCY LIGHTING INOP. FOUND CONNECTOR CONTAMINATED. CLEANED AND REINSTALLED CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1999100100241 19991001 00241 EA 1999 10 1 COMA9960543 1 19990918 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA ROW 8 LOOSE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 932CA 7038 EMERGENCY FLOOR LIGHTS BY SEAT 5-8 ARE INOP. TIGHTENED CONNECTOR BY ROW 8, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1999100100242 19991001 00242 1999 10 1 COMA9960544 4 19990921 A 2210 6229815404 FCC CARD CNDAIR CL600 CL6002B19 EA RIGHT FAILED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 981CA 2325 7163 NR 2 YAW DAMPER WILL NOT RESET. REMOVED AND REPLACED FCC CARD. 2 L 7 2 4F RT A21EA 1999100100243 19991001 00243 EA 1999 10 1 COMA9960545 1 19990920 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 7037 FRAME AT FS 718.00 RHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 2.6 ABOVE STRINGER 11 IN THE FLANGE ATTACHING TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING TO THE FIRST FASTENER HOLE BELOW STRINGER II. PER FORMED A TEMPORARY MAJOR REPAIR TO CRACKED FRAME FS 718.00 STR 11 RHS IAW WVAC EO 601R-53-0338B. 2 L 7 2 4F RT A21EA 1999100100244 19991001 00244 EA 1999 10 1 COMA9960546 1 19990920 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 7037 FRAME AT FS 718.00 RHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING 2.6 ABOVE STRINGER 11 IN THE FLANGE ATTACHI NG TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING TO THE FIRST FASTENER HOLE BELOW STRINGER II. PERFORMED A TEMPO RARY MAJOR REPAIR TO CRACKED FRAME FS 718.00 STR 11 RHS IAW WVAC EO 601R-53-0338A. 2 L 7 2 4F RT A21EA 1999100100245 19991001 00245 EA 1999 10 1 COMA9960547 1 19990918 A 5320 6003106819 DOUBLER CNDAIR CL600 CL6002B19 EA BS 461 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 948CA 7079 DOUBLER PLATE (P/N 600-31068-19) AT RBL 9 AT 461.00 CRACKED. REPLACED DOUBLER PLATE FOR RBL 9 AT FS 461.00 IAW WVAC EO 601R-53-0342. 2 L 7 2 4F RT A21EA 1999100100246 19991001 00246 EA 1999 10 1 COMA9960548 1 19990919 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 EA BS 217-226 MISDRILLED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 948CA 7079 HOLES FOR A CANNON PLUG MOUNTING BRACKET WERE INCORRECTLY LOCATED ON THE INTERCOSTAL BETWEEN FS 217.75 AND FS 226 AT RBL 12 DURING ACCOMPLISHMENT OF COMAIR EO 601R-31-023 FOR MOD PART A & B. REPAIRED INTERCOSTAL BETWEEN FS 217.75 AND FS 22 6 IAW WVAC EO 601R-53-0343. 2 L 7 2 4F RT A21EA 1999100100247 19991001 00247 EA 1999 10 1 COMA9960549 1 19990926 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 FRAME AT FS 718.00 HAD A TEMPORARY REPAIR PER WVAC EO 601R-53-0056B ON THE FRAME PREVIOUSLY INSTALLED. PERFORMED A PERM ANENT MAJOR REPAIR TO CRACKED FRAME FLANGE AT FS 718.00 STR 11 LHS IAW WVAC EO 601-53-0347. 2 L 7 2 4F RT A21EA 1999100100248 19991001 00248 EA 1999 10 1 COMA9960550 1 19990925 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 7037 PERMANENT REPAIR FOR WVAC EO 601R-53-0338B - FRAME FLANGE CRACKED AT FS 718 AND STR 11 RHS AND WVAC EO 601R-53-0339A - D OUBLER CRACKED AT FS 718 AND STR 11 RHS. PERFORMED A PERMANENT MAJOR REPAIR TO CRACKED FRAME FLANGE AND DOUBLER AT FS 7 18.0 STR 11 RHS IAW WVAC EO 601R-53-0350. 2 L 7 2 4F RT A21EA 1999100100249 19991001 00249 EA 1999 10 1 COMA9960551 1 19990926 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 95.95 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 THREE SMALL CRACKS DETECTED IN THE LOWER HORIZONTAL SURFACE OF THE LEFT HAND LOWER WING AT ACCESS HOLE 540 DB. BLENDED OUT THE DAMAGED AREAS, ROTO-PEENED AND ALODINED IAW BOMBARDIER REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999100100250 19991001 00250 EA 1999 10 1 COMA9960552 1 19990926 A 5753 601R1430353 CAP CNDAIR CL600 CL6002B19 EA RT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 931CA 7037 MAJOR REPAIR FLAP VANE CAP IS CHAFED ON RIGHT HAND INBOARD FLAP AND LEFT HAND INBOARD FLAP. REMOVED DAMAGED RIGHT HAND INBOARD VANE CAP AND REPLACED WITH NEW VANE CAP IAW AERO DESIGN AIRCRAFT ENGINEERING REPORT 1286-1. BLENDED AND TREATED LEFT HAND INBOARD VANE CAP IAW REO 601R-57-52-004 REV A DATED 29 NOV 94. 2 L 7 2 4F RT A21EA 1999100100251 19991001 00251 NM 1999 10 1 UPS99230719 1 19990915 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 825.95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C DURING INSPECTION OF BS 825.95 L FRAME A CRACK WAS FOUND EMINATING FROM 3RD FASTENER HOLE ABOVE FLOOR FRAME BS 825.95 LT. REPAIRED IAW APPENDIX C OF EO B727-5310-5474- C & SMRO EO 99-30-002 UPS ENGINEERING FILE NR 531 0-2172. 2 L 7 3 4F A3WE 1999100100252 19991001 00252 NM 1999 10 1 UPS99230720 1 19990915 A 5753 TRACK BOEING 727 72731C 1384011 NM TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, NR 6 FLAP TRACK MID FAIRING O/B ROLLER TRACK CRACKED. TRACK REPLACED IAW SRM 51-30-2 AND DRG 65-2179 6. 2 L 7 3 4F A3WE 1999100100253 19991001 00253 NM 1999 10 1 UPS99230721 1 19990914 A 5320 WEB BOEING 727 72731C 1384011 NM BS 1306 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, CRACK ON WEB AT RT SIDE OF AIRSTAIRS AT STA BS 1306 UPPER LIGHTENING HOLE. CRACK STOP DRILLED IAW SR M CH 51-10-2 AREA REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999100100254 19991001 00254 NM 1999 10 1 UPS99230722 1 19990920 A 5320 BEAM BOEING 727 72731C 1384011 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, DURING REMOVAL TO FACILITATE REPLACEMENT OF BS 940 FITTING, FLAP ROLLER TRACK SUPPORT FOUND CRACKED I N THREE PLACES. BEAM ASSY REPLACED IAW SRM 51-30-2 AND OHM 20-50-01. 2 L 7 3 4F A3WE 1999100100255 19991001 00255 NM 1999 10 1 UPS99230723 1 19990920 A 5320 BRACKET BOEING 727 72731C 1384011 NM BS 440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, FLOOR SUPPORT BRACKET CRACKED AT BS 440 RT IN E & E BAY. BRACKET REPAIRED IAW SRM 51-40-3 FIG 1 AND REPROTECTED IAW SRM 51-10 -2. 2 L 7 3 4F A3WE 1999100100256 19991001 00256 NM 1999 10 1 UPS99230724 1 19990918 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, ANGLE CRACKED ON AFT SIDE OF FRAME BS 560 STR 17 L. ANGLE REPLACED IAW SRM 51-40-03 FIG 1 & SRM 53-1 0-02. 2 L 7 3 4F A3WE 1999100100257 19991001 00257 NM 1999 10 1 UPS99230725 1 19990924 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM RT GALLEY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERGENCY LIGHT AT RT GALLEY INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY RT GALLEY, OP S CHECK GOOD. 2 L 7 3 4F A3WE 1999100100258 19991001 00258 NM 1999 10 1 UPS99230726 1 19990924 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 4 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT, SEAT ROW 4 INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AT SEAT R OW 4, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999100100259 19991001 00259 NM 1999 10 1 UPS99230727 1 19990924 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 4 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT, SEAT ROW 4 INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AT SEAT R OW 4, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100100260 19991001 00260 NM 1999 10 1 UPS99230730 1 19990924 A 3510 REGULATOR BOEING 727 727173C 1384059 NM LT COCKPIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:N/A, CAPT'S O2 MASK AND SYSTEM FAILED NORMAL O2 TEST. FLOW METER INDICATES FLOW IN OFF. REMOVED AND RE PLACED CAPT'S O2 REGULATOR, OPS AND LEAK CHECKS GOOD. 2 L 7 3 4F A3WE 1999100100261 19991001 00261 NM 1999 10 1 UPS99430728 1 19990924 A 3350 SIGN BOEING 747 747121 1384871 NM L1 EMER EXIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:N/A, L1 DOOR EMERGENCY EXIT SIGN INOP. REPLACED EMERGENCY EXIT SIGN, OPS CHECK GOOD. 2 L 7 4 4F A20WE 1999100100262 19991001 00262 1999 10 1 UPS99530652 2 19990921 A 7200 ENGINE BOEING 757 75724APF 1384969 NM NR 1 FAILED A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 426UP 25457 INSPECTION TYPE:N/A, AIR TURNBACK - CARGO FIRE WARNING WITH ACRID SMOKE. CARGO FIRE SWITCH DEPRESSED. ACFT EVACUATED O N TAXIWAY AFTER LANDING. INFLT, AUTOPILOT WOULD NOT ENGAGE, COLOR WAS NOT PRESENT ON ADI'S. *S/D* T/S FOUND ENG LEAKI NG OIL IN BLEED AIR SYSTEM AT TAKEOFF POWER. REMOVED AND REPLACED ENGINE PER TC 5001PW AND RA N PER 5002PW. ALL OPS CH ECKED GOOD. 2 L 7 2 4F RT A2NM 1999100100263 19991001 00263 WP 1999 10 1 UPS99830717 1 19990905 A 5320 56410061 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C1, FLOORBEAM LWR TIE FITTING IS CRACKED AT STA 759, LBL 48. REPAIRED AREA IAW 8110-3 APPROVED DH SK 85 2-726. 2 L 7 4 4F RT 4A25 1999100100264 19991001 00264 WP 1999 10 1 UPS99830718 1 19990911 A 5320 377551181 FITTING DOUG DC8 DC873F 302199F WP BS 1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C1, LONGERON SPLICE FITTING IS CRACKED AT STA 1350 LONG 23R & 24R. REMOVED AND REPLACED FITTINGS IAW DW G 3755118 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100265 19991001 00265 WP 1999 10 1 UPS99830729 1 19990924 A 3240 1542522 BRAKE DOUG DC8 DC871F 302199D WP MLG INOP A IPXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 715UP 45915 INSPECTION TYPE:N/A, BTB - NUMBER 8 BRAKE STUCK. REMOVED AND REPLACED MAIN BRAKE ASSY PER MM 32-42-01. 2 L 7 4 4F RT 4A25 1999100100266 19991001 00266 NM 1999 10 1 QXEA9902003 1 19990925 A 3350 1013079 LIGHT DHAV 82520977001 DHAV DHC8 DHC8202 2809007 NM CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 379PH 530 SEA - FORWARD EMERGENCY LIGHT DOES NOT HAVE RED LIGHTS INSTALLED. REMOVED AND REPAIRED FORWARD LIGHT STRIP, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999100100267 19991001 00267 WP 1999 10 1 DHL99803004 1 19990921 A 5753 56423421 FITTING DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 LEFT HAND I/B FLAP HINGE ATTACH FITTING HAD 2 INCH CRACK. REPLACED FITTING. 2 L 7 4 4F RT 4A25 1999100100268 19991001 00268 NM 1999 10 1 VNAA9909008 1 19990923 A 3350 321430 BATTERY PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7LK DSCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 438JS 10543 807 3056 A SECTION OF THE EMERGENCY FLOOR LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERG ENCY BATTERY PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIR CRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999100100325 19991001 00325 NM 1999 10 1 ASAA9940134 1 19990701 A 3397 WIRE BOEING 737 737490 1384715 NM ROW 14 DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 713AS 30161 SFO - PRIOR TO FLT 357, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 14. RECONNECTED WIRING AT R OW 14, AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999100100326 19991001 00326 NM 1999 10 1 ASAA9940141 1 19990808 A 3397 WIRE BOEING 737 737490 1384715 NM ROW 15 DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 713AS 30161 OAK - PRIOR TO FLT 381, THE EMERGENCY EXIT FLOOR TRACKS LIGHTS WERE FOUND INOPERABLE IN THE CENTER CABIN AREA. RECONNEC TED WIRE AT ROW 15 AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999100100327 19991001 00327 NM 1999 10 1 L7RA001 1 19990731 A 3350 6013211 POWER SUPPLY GRIMES BOEING 737 737247 138448D NM CABIN INOPERABLE A L7RA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903RC 1019 19598 EMERGENCY EXIT LIGHTS, 2 EACH, BEHIND ELEPHANT EAR (AFT BULLNOSE) VERY DIM. (X) 2 L 7 2 4F A16WE 1999100100328 19991001 00328 NM 1999 10 1 99ZZZX3700 1 19990810 A 2130 39268631 REGULATOR BOEING 737 737230 NM NR 1 ENGINE FAILED A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 123NJ P2237 22121 MCI - FLT 404 - DURING CLIMB-OUT, DUCT PRESSURE SPLIT EXCEEDED 40 PSI: L - 42, R = 80. ON GROUND, PRESSURE INDICATES E QUAL. REPLACED NR 1 ENGINE HIGH PRESSURE REGULATOR IAW MM 21-11-31. (X) 2 L 7 2 4F RT A16WE 1999100100329 19991001 00329 EA 1999 10 1 99ZZZX3701 1 19990731 A 3350 487190 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN BROKEN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 827AS 7212 DURING INSPECTION, FOUND FORWARD MOST WIRE CONNECTOR BROKEN ON FLOOR EMERGENCY LIGHTING. MAINTENANCE REPLACED THE EMERG ENCY LIGHT WIRE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999100100330 19991001 00330 EA 1999 10 1 99ZZZX3702 1 19990726 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 838AS 1517 7276 DURING INSPECTION, NR 1 EMERGENCY LIGHTING SYSTEM BATTERY PACK FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGEN CY LIGHTING SYSTEM BATTERY PACK. OPERATIONAL CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999100100331 19991001 00331 EA 1999 10 1 RU3A99007 1 19990629 A 2810 457370 FUEL CAP 3007675 CNDAIR CL600 CL6002B16 1900305 EA RT WING DIRTY A RU3A A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 87 5190 FUEL OBSERVED STREAMING DOWN THE RIGHT-HAND WING DURING FLIGHT. FUEL WAS LEAKING AT THE RIGHT-HAND OUTBOARD FUEL CAP. A IRCRAFT MADE UNSCHEDULED LANDING. THE LOCKING DEVICE ON THE CAP WAS INSPECTED AND FOUND TO BE FUNCTIONING PROPERLY. FO REIGN MATTER WAS FOUND UNDER THE FUEL CAP SEAL. FOREIGN MATTER REMOVED, CAP RE-INSTALLED AND NO OTHER DISCREPANCIES NOT ED. (X) 2 L 7 2 4F RT A21EA 1999100100332 19991001 00332 EU 1999 10 1 RU3A99009 1 19990804 A 2150 1250160 COMPRESSOR BRAERO DH125 BAE125800A 1500285 EU AUXILIARY PACK SEIZED A RU3A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 96 258134 CREW NOTICED ACRID BURNING SMELL IN COCKPIT DURING FLIGHT. CREW DECLARED AN EMERGENCY AND LANDED. MAINTENANCE FOUND AU XILIARY COOLING PACK COMPRESSOR SEIZED. (X) 2 L 7 2 4F RT A3EU 1999100100333 19991001 00333 1999 10 1 99ZZZX3703 4 19990623 A 3416 KEA346066306208 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT MALFUNCTIONED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 153GL 883 4446 UE153 PILOT REPORTED THE PILOT'S ALTIMETER TO BE READING 150 FEET HIGH. REMOVED AND REPLACED PILOT'S ALTIMETER. SUBSEQUENT BE NCH CHECK VERIFIED ALTIMETER TO BE INDICATING 150 FEET HIGH. THE BAROMETRIC WINDOWS DISPLAYED 1,017 MILLIBARS AT 29.92 IHG. 2 L 7 2 4T RT A24CE 1999100100334 19991001 00334 1999 10 1 99ZZZX3704 4 19990726 A 3422 DGS656226136002 DIRECTIONAL GYRO COLLINS BEECH 1900 1900D 1154162 CE E/E COMPT FAILED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 154GL 4564 UE154 FLIGHT CREW REPORTED THE COMPASS CARD DID NOT MOVE IN THE FREE OR SLAVED MODES WHEN THE AIRCRAFT WAS TURNED. REMOVED AN D REPLACED DIRECTIONAL GYRO. SUBMITTER STATED THIS IS THE FOURTH TIME THIS GYRO HAS HAD THIS PROBLEM REPORTED (DIFFEREN T AIRCRAFT). ALL SHOP VISITS HAVE RESULTED IN 'NO FAULT FOUND'. 2 L 7 2 4T RT A24CE 1999100100335 19991001 00335 1999 10 1 99ZZZX3705 4 19990623 A 3416 KEA346066306208 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT FAILED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 260GL 1161 2857 UE260 PILOT REPORTED THE ADJUSTMENT KNOB WOULD SET THE ALTITUDE, BUT WOULD NOT ADJUST THE BAROMETRIC WINDOW SETTING. REMOVED AND REPLACED PILOT'S ALTIMETER. DEFECT WAS VERIFIED DURING BENCH CHECK. 2 L 7 2 4T RT A24CE 1999100100336 19991001 00336 NM 1999 10 1 99ZZZX3706 1 19990822 A 2750 PUSH ROD BOEING 747 747122 1384872 NM TE FLAP FAILED B GK4Y K NONE O OTHER IN INSP/MAINT 1 WP 03 852FT 19757 DURING WALK-AROUND INSPECTION, NR 3 FAIRING CANOE WAS FOUND PIERCED WITH FLAP PUSH ROD. ON INVESTIGATION AFTER DROPPING THE FLAPS (T/E), FOUND THE FLAP PUSH ROD HAD SHEARED ON THE FORWARD END. THE BROKEN PUSH ROD PIERCED THE FAIRING DURIN G FLAP RETRACTION. PRELIMINARY INSPECTION FOUND PUSH ROD ON NR 4 FAIRING ALSO DAMAGED. PUSH RODS REMOVED AND REPLACED PER PAC MM AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 1999100100339 19991001 00339 WP 1999 10 1 TWAA9913301 1 19990928 A 3350 LAMP DOUG DC9 DC983 3022083 WP GALLEY DOORWAY FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9627R 53597 TWO RED EGRESS LIGHTS WERE INOPERATIVE AT THE AFT GALLEY DOOR. REPLACED A LAMP ASSEMBLY, (P/N 0105606-002) AND A LAMP M ODULE, (P/N 0105606-004). 2 L 7 2 4F RT A6WE 1999100100340 19991001 00340 NM 1999 10 1 TWAA9913302 1 19990928 A 3350 59122 LIGHT BOEING 767 767231 1385131 NM CABIN DAMAGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 602TW 22565 FOUND CABIN EGRESS LIGHTS INOPERATIVE AT THE NUMBER 2 CROSSOVER POINT. REPLACED THE LIGHT STRIP. CHECK-C 8-25-99 LAX. 2 L 7 2 4F RT A1NM 1999100100341 19991001 00341 1999 10 1 TWAA9913303 4 19990928 A 2397 WIRE DOUG DC9 DC983 3022083 WP BS 110-160 FAILED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9628W 53598 WIRE NUMBER 1RL49B24 THAT IS PART OF THE SELCAL SYSTEM, WAS FOUND WITH BURNED INSULATION FROM STA 110 S-30-119 PIN 67 TO STA 160 RT S-30-22 PIN 18, IT HAD ALSO BURNED THROUGH. THE WIRE WAS REMOVED AND NOT REPLACED BECAUSE IT WAS NOT PART O F THE SYSTEM DESIGN. THE AIRCRAFT WAS MANUFACTURED IN DEC, 1998. 2 L 7 2 4F RT A6WE 1999100100342 19991001 00342 NM 1999 10 1 AT9900672 1 19990923 A 3350 1000679 LIGHT BOEING 737 7372L9 1384497 NM L2 DOOR INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 DURING INSPECTION FOUND L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F RT A16WE 1999100100343 19991001 00343 EU 1999 10 1 MALA976581 1 19990925 A 7722 10227N01T00 ITT GAUGE SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 434XJ 434 RIGHT ENGINE TEMP GAUGE FLUCTUATING AND ERRATIC -100 DEGREES TO LEFT AT ONE. AT HIGH POWER IT WOULD FLUCTUATE -20 TO 60 DEGREES. ALL OTHER ENGINE GAUGES STABLE AND NORMAL. AFTER POWER REDUCED IN CLIMB, RIGHT ENGINE TEMP GAUGE WOULD TICK WITHIN 10 DEGREES. MAINTENANCE REPLACED RIGHT ITT GAUGE. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999100100344 19991001 00344 1999 10 1 MALA976582 2 19990920 A 7510 6058T80P03 ANTI ICE VALVE SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 99XJ 099 RIGHT AIR VALVE LIGHT ILLUMINATED WHEN ENGINE ICE SELECTED ON. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED ANTI ICE VALVE IAW CMM CHAPTER 75, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999100100345 19991001 00345 EU 1999 10 1 MALA976583 1 19990925 A 3230 RETRACT MECH SAAB SF340 SF340A 7850100 EU LANDING GEAR MALFUNCTIONED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 107XJ 340A107 LANDING GEAR DID NOT COME DOWN AFTER SELECTED. CREW FOLLOWED QRH AND FOUND F7 CIRCUIT BREAKER OUT, RESET AND SYSTEM WOR KED NORMALLY. MAINTENANCE PERFORMED SEVERAL CYCLES OF THE LANDING GEAR ON JACKS. ALL CHECKS GOOD IAW AMM 32-30-00. 2 L 7 2 4T RT A52EU 1999100100346 19991001 00346 NE 1999 10 1 MALA976584 2 19990919 A 7510 6058T80P03 ANTI ICE VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 102XJ 340A102 WHEN RIGHT ENGINE ANTI ICE IS TURNED ON, TORQUE DROPS 10 PERCENT AND ITT RISES 20 DEGREES. AIRCRAFT RETURNED TO MSP. M AINTENANCE REPLACED ANTI ICE BLEED VALVE AND BLEED AIR SHUT OFF VALVE. ALL WORK DONE IAW GE MM 75-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999100100347 19991001 00347 NE 1999 10 1 MALA976585 2 19990924 A 7320 HMU BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 2 FAILED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 514XJ E2330 ON SHORT FINAL TO MSP, NR 2 ENGINE WOULD NOT RESPOND TO THRUST LEVER. ENGINE REMAINED AT APPROXIMENTLY 49 PERCENT N2. A FTER LANDING N2 REDUCED TO 41 PERCENT. NO OTHER ENGINE WARNINGS. MAINTENANCE REPLACED NR 2 HMA IAW AVRO MM 73-20-01, 7 1-00-00, OPS AND LEAK CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 1999100100348 19991001 00348 EU 1999 10 1 MALA976586 1 19990905 A 3320 D75602001 LIGHT SAAB SF340 340B 7860101 EU ROW 5A FAILED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 406XJ 406 DURING PREFLIGHT INSPECTION, NOTED OVERHEAD LIGHT ABOVE 5A SMOKING. MAINTENANCE DEFERRED LIGHT AND CLEARED ON 9/11 BY R EPLACING LAMP HOLDER ASSEMBLY, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999100100349 19991001 00349 EU 1999 10 1 MALA976587 1 19990919 A 2560 LATCH LEVER BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR SLIDE OUT OF ADJUST A MALA O OTHER O OTHER CR CRUISE 1 GL 15 525XJ E2350 LEFT FORWARD PAX DOOR EMERGENCY SLIDE ARM/DISARM LEVER DISARMED CLIMBING THRU 9000 FT MSL. MAINTENANCE ADJUSTED LATCH A SSEMBLY. CMM 52-10-13 PARAGRAPH C. 2 H 7 4 4F RT A49EU 1999100100350 19991001 00350 NE 1999 10 1 AWXA9900325 2 19990923 A 7314 5008735F FUEL PUMP AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 28 643AW 24911 14338 315 DURING CLIMB THROUGH FL180, NR 2 ENG COMPRESSOR STALLED 3X. DURING DESCENT BACK INTO CMH ENG RPM AND F/F WAS LOWER THAN NR 1. DURING TAXI BACK, NR 2 ENG FAILED. REMOVED AND REPLACED NR 2 ENG MAIN FUEL PUMP IAW TASK CARD R5M73304. OPS CK NML. AFTER DIRECTION TO PERFORM POWER ASSURANCE TEST NR 2 ENGINE COMP STALLED AT 1.345 EPR. FURTHER T/S RESULTED IN R EPLACEMENT OF ENGINE, 26 SEP 99, MFG P/N V2500A1, MFG S/N V0025. TOT 24560, TOC 11882, TSR 24560. 2 L 7 2 4F 4 F RT A28NM E311NE 1999100100351 19991001 00351 EU 1999 10 1 AWXA9900326 1 19990923 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 618AW 27638 3223 304 SEVERAL CABIN EMERGENCY LIGHTS INOP WHEN TESTED AT FAP ONLY. REMOVED AND REPLACED AFT CABIN EMERGENCY LT PWR SUPPLY. 2 L 7 2 4F RT A28NM 1999100100352 19991001 00352 NM 1999 10 1 AWXA9900327 1 19990924 A 2133 OUTFLOW VALVE BOEING 737 7373Y0 1384671 NM CABIN MALFUNCTIONED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 331AW 23747 CABIN ALTITUDE CLIMBED TO 10,500 WHILE A/C CLIMBED THRU 32,500. WENT TO MANUAL AND CLOSED OUTFLOW VALVE, GOT CONTROL O F CABIN AT LOWER ALTITUDE. PERFORMED AUTO PRESSURIZATION TEST, OPS CHECK GOOD MM 21-31-00. PERFORMED CABIN LEAK-DOWN C HECK, LK AND OPS CK GOOD MM 05-51-91. 2 L 7 2 4F RT A16WE 1999100100353 19991001 00353 NM 1999 10 1 AWXA9900328 1 19990924 A 5751 65C259111A SPAR BOEING 737 737301 1384611 NM LT AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 LOWER FLANGE OF LT AILERON FWD SPAR DELAMINATED IN 7 SPOTS FWD SPAR WBL 322.536 TO WBL 417.230. REPAIRED PER AWA ER 57 -51-17B, PAINTED PER SRM 51-21-00. 2 L 7 2 4F RT A16WE 1999100100354 19991001 00354 NM 1999 10 1 AWXA9900329 1 19990824 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 FUSELAGE SKIN CRACKED JUST AFT OF E & E EXHAUST OUTLET. REPAIRED IAW EO 53-30-13. 2 L 7 2 4F RT A16WE 1999100100355 19991001 00355 NM 1999 10 1 AWXA9900330 1 19990531 A 5330 6545800 SKIN BOEING 737 73733A 1384673 NM L1 DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 L-1 DOOR LOWER HINGE CUTOUT, .25 INCH CRACK ON DOOR. STOP DRILLED CRACK PER BF32 NTM PT 6, 51-00-00 FIG 23, FABRICATED AND INSTALLED DOUBLER REPAIR IAW EO 52-00-02, MAT .063 R024T3. 2 L 7 2 4F RT A16WE 1999100100356 19991001 00356 NM 1999 10 1 AWXA9900331 1 19990531 A 5210 65C33756 SKIN BOEING 737 73733A 1384673 NM R1 DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 R1 CUTOUT AFT LWR CORNER .375 INCH CRACK ENDS AT FASTENER. CUT OUT AND INSTALLED DAMAGED AREA IAW SRM 53-10-01. FABRIC ATED DOUBLER AND TRIPLER REPAIR 2024 TS .063, TRIPLER FILLER 2024T3 .063 & .071. 2 L 7 2 4F RT A16WE 1999100100357 19991001 00357 NM 1999 10 1 AWXA9900332 1 19990927 A 2910 65445101803 LINE BOEING 737 7372A6 138448B NM A HYD SYS LEAKING A AWXA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 WP 28 145AW 20194 LOSS OF A-SYSTEM IN FLIGHT. REPLACED A-SYSTEM RETURN LINE. LEAK CK OK, SERVICED SYS TO FULL IAW 29-12 M & E (P/N 15-29 00-3-0004). 2 L 7 2 4F A16WE 1999100100358 19991001 00358 NM 1999 10 1 AWXA9900333 1 19990927 A 3350 864705 PWR SUPPLY BOEING 737 7372U9 1384498 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 SEAT EMERGENCY LIGHTS SYSTEM INOP AFT OF FIRST CLASS. REMOVED AND REPLACED FOUR BATT PACKS AND POWER SUPPLY. 2 L 7 2 4F RT A16WE 1999100100359 19991001 00359 NM 1999 10 1 AWXA9900334 1 19990608 A 5320 6545834 ANGLE BOEING 737 73733A 1384673 NM BS 312 GOUGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 CONDITION: C-CHECK DAMAGE NR 5068128DISCREPANCY: FWD CABIN FS 312 RBL 11 INTERCOSTAL TOP ANGLE IS GOUGED *************SUPPLEMENTAL DATA**************CORRECTIVE ACTION: REMOVED DAMAGED ANGLE PER SR M 51-40-2, FABRICATED REPLACEMENT ANGLE AND SHIM OF 2024 T 3492 IAW 737SRM 51-30-01 QQA2003FR684482 -- TREATED AND PRI MED PER SRM 51-20-1 INSTALLED IAW SRM 51-20-1 2 L 7 2 4F RT A16WE 1999100100360 19991001 00360 NM 1999 10 1 RAAA99B1020 1 19990927 A 3397 873100212 WIRE INTVLV BOEING 727 72722C 138400F NM ROW 11DEF LOOSE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 EXIT IDENTIFER AT ROW 11 D, E, F LEAD DISCONNECTED. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999100100361 19991001 00361 NM 1999 10 1 RAAA99B1021 1 19990927 A 3350 86210144 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM ROW ABC DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 EMERGENCY LIGHT AT ROW A, B, C FAILED SELF TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999100100362 19991001 00362 NM 1999 10 1 RAAAB1019 1 19990922 A 3350 86210066 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 7ABC DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 ROW 7 ABC EGRESS LIGHT WOULD NOT EXTINGUISH. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999100100363 19991001 00363 NM 1999 10 1 RAAAB2052 1 19990923 A 3350 86210066 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 14 DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 ROW 14 AISLEWAY EGRESS LIGHT DID NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999100100364 19991001 00364 NM 1999 10 1 RAAAB2053 1 19990923 A 3350 86210066 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 15 DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 ROW 15 AISLEWAY EGRESS LIGHT DID NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999100100365 19991001 00365 NM 1999 10 1 RAAAB2054 1 19990923 A 3350 900835A BATTERY PACK GRIMES 1000679 BOEING 727 72722C 138400F NM CABIN DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AFT ENTRY EMERGENCY LIGHT DID NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999100100366 19991001 00366 SO 1999 10 1 RAAAE9025 1 19990920 A 3350 86210144 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FORWARD CABIN EXIT ID LIGHT WILL NOT TEST. REPLACED BATTERY. 2 L 7 4 4T 4A22 1999100100367 19991001 00367 NM 1999 10 1 CALA9901283 1 19990923 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 629.0 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A 5 INCH CRACK AT ATTACH POINT IN LT WING UPPER FORWARD STRINGER AT WING STA 629.0. THE CRACKED AREA W AS CUT OUT, REPAIR PARTS WERE INSTALLED IAW EA 5762-01050. 2 L 7 3 4F A3WE 1999100100368 19991001 00368 NM 1999 10 1 CALA9901284 1 19990923 A 5330 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 INSPECTION FOUND A .25 INCH CRACK IN NR 1 LT WINDOW CUTOUT. REPAIRED IAW ECRA 5330-02877. 2 L 7 2 4F RT A16WE 1999100100369 19991001 00369 NM 1999 10 1 CALA9901285 1 19990923 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 827-892 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17356 23942 INSPECTION FOUND STRINGER 5L DENTED AT STA 827 AND BETWEEN STA 842 AND 892. STRINGER REPAIRS WERE INSTALLED IAW SRM 53- 00-03, FIGURE 201 AND 203. 2 L 7 2 4F RT A16WE 1999100100370 19991001 00370 NM 1999 10 1 CALA9901286 1 19990924 A 5320 DECK BOEING 757 757224 1384958 NM BS 1720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND SHEAR DECK CORRODED AT STA 1720, BL 0 AND LBL 49. REPAIRS WERE ACCOMPLISHED IAW ECRA 5321-01069. 2 L 7 2 4F RT A2NM 1999100100371 19991001 00371 NM 1999 10 1 CALA9901287 1 19990925 A 5755 SKIN BOEING 727 727224 1384076 NM NR 7 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A 2 INCH CRACK IN LT WING NR 7 SPOILER PANEL SKIN WITH DENTS ON LOWER SURFACE. THE SPOILER PANEL WAS R EMOVED, REPAIRED, AND REINSTALLED IAW SRM 57-30-00, PAGE 30 AND MM 27-62-1, PAGE 403. 2 L 7 3 4F A3WE 1999100100372 19991001 00372 NM 1999 10 1 CALA9901288 1 19990924 A 3350 BATTERY PACK BOEING 727 727224 1384076 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND CABIN EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE AND INOPERATIVE BATTER Y. THE FUSE AND BATTERY PACK WERE REMOVED AND REPLACED IAW MM 33-50-1. 2 L 7 3 4F A3WE 1999100100373 19991001 00373 NM 1999 10 1 CALA9901289 1 19990924 A 5755 SKIN BOEING 727 727224 1384076 NM NR 2 SPOILER DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND LT WING NR 2 SPOILER UPPER SKIN DEBONDED WITH SURFACE CORROSION AROUND SCREW HEADS. THE NR 2 SPOILER P ANEL WAS REMOVED AND REPLACED IAW MM 27-61-1, PAGE 407. 2 L 7 3 4F A3WE 1999100100374 19991001 00374 NM 1999 10 1 CALA9901290 1 19990924 A 5743 FITTING BOEING 727 727224 1384076 NM RT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A 1.5 CRACK IN RT MLG BEAM SUPPORT FITTING. THE SUPPORT FITTING AND BUSHING WERE REMOVED AND REPLACED IAW ECRA 5740-01102. 2 L 7 3 4F A3WE 1999100100375 19991001 00375 NM 1999 10 1 CALA9901291 1 19990925 A 5754 SKIN BOEING 727 727224 1384076 NM NR 5 LE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND NR 5 L/E FLAP BULL NOSE CORRODED. THE FLAP BULL NOSE WAS REMOVED AND REPLACED IAW MM 27-81-1, PAGE 401 . 2 L 7 3 4F A3WE 1999100100376 19991001 00376 WP 1999 10 1 9903989913 1 19990916 A 2120 DUCT DOUG DC9 DC931 3022065 WP LT PACK DISCONNECTED A NWAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION DE DESCENT 1 GL 01 963N 47415 LOSS OF CABIN PRESSURIZATION OCCURRED AT START OF DESCENT FROM 26,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN AND EMERGENCY DESCENT WAS ACCOMPLISHED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DUCT BETWEEN LEFT AIR CYC LE MACHINE AND WATER SEPARATOR DISCONNECTED. REINSTALLED DUCT AT RUBBER SLEEVE AND HOSE CLAMPS, OPERATIONAL CHECK NORMA L. 2 L 7 2 4F A6WE 1999100100377 19991001 00377 NM 1999 10 1 9904005517 1 19990920 A 2751 WARNING BOEING 757 757251 1384970 NM TE FLAPS ILLUMINATED A NWAA K NONE N FALSE WARNING AP APPROACH 1 GL 01 517US 23205 ON APPROACH SEA, TRAILING EDGE FLAP ASYMMETRY WARNING ILLUMINATED AND FLAPS STOPPED AT 17 DEGREES. FLIGHT DECLARED AN E MERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED TRAILING EDGE FLAP SYSTEM TESTS. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A2NM 1999100100378 19991001 00378 EU 1999 10 1 9904013247 1 19990920 A 2730 31075440 SERVO AIRBUS 320 A320212 EU LT ELEVATOR LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 347NW 408 DURING CRUISE, RECEIVED HYD B SYS LOW PR MESSAGE. LOW SYSTEM QUANTITY AND LOW SYSTEM PRESSURE WAS CONFIRMED. SHUT OFF BLUE SYSTEM HYDRAULIC PUMP, CONTINUED TO DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING LEFT OU TBOARD ELEVATOR SERVO. LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999100100379 19991001 00379 WP 1999 10 1 9904029155 1 19990923 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. 2 L 7 2 4F A6WE 1999100100380 19991001 00380 WP 1999 10 1 9904039970 1 19990922 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PO WER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999100100381 19991001 00381 NM 1999 10 1 QXEA9901987 1 19990913 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - CORROSION ON LEFT-HAND AND RIGHT-HAND SEAT TRACKS IN AREA OF GALLEY, LAVATORY AND WARDROBE. REPAIRED IAW DHC-8 SR M 51-20-16 AND SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999100100382 19991001 00382 NM 1999 10 1 QXEA9901988 1 19990913 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - DENT ON LEFT-HAND PASSENGER DOOR AT FS X240.500 AND Z162.0. REPAIRED IAW RD 8-52-406. 2 H 7 2 4T RT A13NM 1999100100383 19991001 00383 NM 1999 10 1 QXEA9901989 1 19990914 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - RIGHT-HAND WING INBOARD FLAP HAS CHAFING WEAR ON THE UPPER SURFACE OF THE FLAP AT YW72.00. REPAIRED IAW RD 8-57-1 022. 2 H 7 2 4T RT A13NM 1999100100384 19991001 00384 NM 1999 10 1 QXEA9901990 1 19990914 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - RIGHT-HAND WING OUTBOARD FLAP HAS CHAFING WEAR ON THE UPPER SURFACE OF THE FLAP AT YW 202.00. REPAIRED IAW RD 57- 1022. 2 H 7 2 4T RT A13NM 1999100100385 19991001 00385 NM 1999 10 1 QXEA9901991 1 19990914 A 5754 SKIN DHAV DHC8 DHC8202 2809007 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - LEFT-HAND WING OUTBOARD FLAP HAS CHAFING WEAR ON THE UPPER SURFACE OF THE FLAP AT YW225.00. REPAIRED IAW RD 57-10 22. 2 H 7 2 4T RT A13NM 1999100100386 19991001 00386 NM 1999 10 1 QXEA9901992 1 19990914 A 2750 COUPLING DHAV DHC8 DHC8202 2809007 NM LT TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - LEFT-HAND WING PRIMARY FLAP DRIVE TORQUE TUBE ASSEMBLY, INBOARD DRIVE COUPLING IS WORN. REPAIRED IAW MM 27-52-20, PAGE 401-408. 2 H 7 2 4T RT A13NM 1999100100387 19991001 00387 NM 1999 10 1 QXEA9901993 1 19990914 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - SEVERAL TOOLING SCRATCHES ON THE LEFT-HAND WING SPAR CAP LEADING EDGE UPPER ATTACH AREA. REPAIRED IAW RD 8-57-119 . 2 H 7 2 4T RT A13NM 1999100100388 19991001 00388 NM 1999 10 1 QXEA9901994 1 19990917 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - CHAFE ON LEFT-HAND AFT NACELLE UPPER DECK UNDER FINGERNAIL. REPAIRED IAW RD 8-54-866 AND DHC -8 SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999100100389 19991001 00389 NM 1999 10 1 QXEA9901995 1 19990916 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 240 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - EXTERIOR FUSELAGE RIGHT-HAND SIDE AT STATION X240 NICK IN SKIN. REPAIRED IAW HORIZON AIR EA 2-53-100 AND BOMBARDI ER RD 8-53-4501. 2 H 7 2 4T RT A13NM 1999100100390 19991001 00390 NM 1999 10 1 QXEA9901996 1 19990914 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 151.6 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - EXTERIOR FUSELAGE RIGHT-HAND SIDE DENT WITH GOUGE AT STATION 151.6. REPAIRED IAW BOMBARDIER RD 8-53-4491. 2 H 7 2 4T RT A13NM 1999100100391 19991001 00391 NM 1999 10 1 QXEA9901997 1 19990914 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 325 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - FUSELAGE UPPER SURFACE DENT AT STATION X325 AND STRINGER 3, LEFT-HAND SIDE. REPAIRED IAW BOMBARDIER RD 8-53-4481. 2 H 7 2 4T RT A13NM 1999100100392 19991001 00392 NM 1999 10 1 QXEA9901998 1 19990902 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 352PH 494 YXX - WIRES FOR EMERGENCY LIGHTING AT AFT MOST FLOOR BOARD LOOSE. REPLACED ALL FLOOR TRACK LIGHTING. 2 H 7 2 4T RT A13NM 1999100100393 19991001 00393 NM 1999 10 1 QXEA9901999 1 19990917 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 422 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - FUSELAGE EXTERNAL BELLY SKIN AT STATION X 422.00, LEFT-HAND SIDE GOUGED. REPAIRED IAW BOMBARDIER RD 8-53-4496, CO NAIR EO 2429 AND HORIZON AIR EA 2-53-101. 2 H 7 2 4T RT A13NM 1999100100394 19991001 00394 NM 1999 10 1 QXEA9902000 1 19990915 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 322 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - RIGHT-HAND LOWER FUSELAGE EXTERNAL AT STATION X322.00 SKIN SCRATCHED. REPAIRED IAW DHC-8 SRM 53-00-16, TABLE 1, S HEET 2, SRM 51-20-11, PAGE 7-8, FIGURE 4. 2 H 7 2 4T RT A13NM 1999100100395 19991001 00395 NM 1999 10 1 QXEA9902001 1 19990910 A 5320 RAIL DHAV DHC8 DHC8202 2809007 NM BS 201-222 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - TWO FLOOR BOARD RAILS AT STATION X201-X222, LEFT-HAND SIDE HAD SURFACE CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11 , PAGE 1-10. 2 H 7 2 4T RT A13NM 1999100100396 19991001 00396 NM 1999 10 1 QXEA9902002 1 19990914 A 5320 RAIL DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 YXX - CARGO COMPARTMENT INBOARD RAILS HAVE SURFACE CORROSION AT STATION X.600. REPAIRED IAW DHC-8 SRM 51-00-06 AND BOMB ARDIER RD 8-53-784. 2 H 7 2 4T RT A13NM 1999100100398 19991001 00398 WP 1999 10 1 99FDEA00399 1 19990113 A 5230 NDA6066503 SKIN DOUG DC10 DC1010 3022110 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 DURING AC PF CONVERSION AT OAN, 2 3/4 CRACKS FOUND ON OUTER SKIN & INTERNAL DOUBLER OF FWD LWR CARGO DOOR. REPAIR INSTA LLED INNER AND EXTERNAL DOUBLERS IAW EA NR 8-5210-45542. 2 L 7 3 4F A22WE 1999100100399 19991001 00399 WP 1999 10 1 99FDEA00400 1 19990313 A 5713 ARB09421 STRINGER DOUG DC10 DC1010 3022110 WP WS 130 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 DURING AC PF CONVERSION AT OAN, CRACK FOUND ON VERTICAL FLANGE OF STR 34 LT WING STR AT XOR=130. SRM DOES NOT COVER WIN G STR REPAIRS OF THIS CROSS SECTION AND LOCATION. REPAIR CUT OUT DAMAGE, PERF HFEC INSPECTION, INSTALLED 2 C ANGLES IAW NR 8-5711-44037. 2 L 7 3 4F A22WE 1999100100400 19991001 00400 WP 1999 10 1 MWEA99614 1 19990924 A 5320 4913325503 CLIP DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 LONGERON 17R AT STATION 1121 WAS CORRODED AT END CLIP. MTC FABRICATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999100100401 19991001 00401 WP 1999 10 1 MWEA99615 1 19990924 A 5312 9911520115 BULKHEAD WEB DOUG DC9 DC932 3022066 WP CARGO COMPT HOLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FORWARD CARGO COMPARTMENT FORWARD BULKHEAD WEB HAD A HOLE IN LOWER CENTER DOUBLER. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999100100402 19991001 00402 WP 1999 10 1 MWEA99616 1 19990924 A 5311 99118593 FRAME DOUG DC9 DC932 3022066 WP BS 1104 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 STATION 1104 HAD CORROSION AT LONGERON 12-22L AND WAS CRACKED AT LONGERON 13L. MTC FABRICATED AND INSTALLED FRAME SECTI ON. 2 L 7 2 4F A6WE 1999100100403 19991001 00403 WP 1999 10 1 MWEA99617 1 19990924 A 5313 591140125 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 LONGERON 23 AND 24 WAS CRACKED AT STATION 200 AND LONGERON 25 WAS CRACKED AT STATION 160. MTC FABRICATED AND INSTALLED LONGERONS. 2 L 7 2 4F A6WE 1999100100404 19991001 00404 WP 1999 10 1 MWEA99618 1 19990924 A 5312 59101307 BULKHEAD SKIN DOUG DC9 DC932 3022066 WP AFT PRESS BULKHD HOLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 HOLE WORN THROUGH AFT PRESSURE BULKHEAD BELOW LEFT THRUST REVERSER CONTROL SECTOR. MTC FABRICATED AND INSTALLED DOUBLER . 2 L 7 2 4F A6WE 1999100100405 19991001 00405 WP 1999 10 1 MWEA99619 1 19990924 A 5532 59121669 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 VERTICAL STABILIZER IS CHAFED AT AFT END. MTC FABRICATED AND INSTALLED NEW SKIN AND ANGLE. 2 L 7 2 4F A6WE 1999100100406 19991001 00406 WP 1999 10 1 MWEA99620 1 19990924 A 5330 59114282 SKIN DOUG DC9 DC932 3022066 WP BS 945 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 TWO DENTS ON SKIN AFT OF STATION 945 BELOW LONGERON 25R. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999100100407 19991001 00407 WP 1999 10 1 MWEA99621 1 19990924 A 5311 99115075 FRAME DOUG DC9 DC932 3022066 WP BS 120 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FRAME WAS CRACKED AT STATION 120. MTC FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 1999100100408 19991001 00408 WP 1999 10 1 MWEA99622 1 19990924 A 5532 591216610 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 VERTICAL STABILIZER WAS CHAFED AT AFT END FROM HORIZONTAL STABILIZER FAIRINGS ON RIGHT SIDE. MTC FABRICATED AND INSTALL ED NEW SKIN AND ANGLE. 2 L 7 2 4F A6WE 1999100100409 19991001 00409 WP 1999 10 1 MWEA99623 1 19990924 A 5532 591216612 PANEL DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 VERTICAL STABILIZER CANOE PANEL WAS CHAFED AT AFT END FROM HORIZONTAL STABILIZER FAIRINGS ON LEFT AND RIGHT SIDE. MTC F ABRICATED AND INSTALLED REPLACEMENT PANEL. 2 L 7 2 4F A6WE 1999100100410 19991001 00410 NM 1999 10 1 SCNA99727 1 19990922 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON FLOORBEAM TOP CAP AT STA 1070 JUST AFT OF L2 DOOR. REMOVED CORROSION FROM FLOORBEAM IAW SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 531008, FABRICATED TWO DOUBLER AND FILLER, ANGLE 1 FROM BAC 14902888 AND ANGLE 2 FROM 14902831 AND FILLER FROM BAC 1505100617 IAW B727 SRM 531008. TREATED AND PRIMED IAW B727 SRM 512002 AND MM 511002. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F RT A3WE 1999100100411 19991001 00411 NM 1999 10 1 SCNA99726 1 19990922 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 380 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS IN THE FORWARD MAIN CABIN SEAT TRACK, STA 380 RBL 24. REMOVED CORROSION PER SRM 511006. REMOVED DAMAGED SEAT TRACK PER SRM 513002. FABRICATED PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED PER SRM 512002 AND MM 511002. INSTALLED IAW SRM 531005. 2 L 7 3 4F RT A3WE 1999100100412 19991001 00412 NM 1999 10 1 SCNA99121 1 19990925 A 3350 LIGHT BOEING 727 7272J4 1384006 NM ROW 17ABC INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTING AT SEAT 17 ABC WAS FOUND WITH TWO LIGHTS INOPERATIVE. REM OVED AND REPLACED TWO EMERGENCY LIGHTS AT SEAT 17 ABC, OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F RT A3WE 1999100100413 19991001 00413 NM 1999 10 1 SCNA99122 1 19990927 A 3350 SIGN BOEING 727 727259 138408J NM L2 DOORWAY INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT SIGN AT THE LOWER RIGHT SIDE OF L2 DOOR WAS FOUND INOPERATIVE. REMO VED AND REPLACED THE LOWER L2 DOOR EMERGENCY EXIT SIGN, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999100100414 19991001 00414 EU 1999 10 1 RAIA9909011 1 19990927 A 7600 21188408 IEC COMPUTOR JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 556HK 41073 RIGHT ENGINE TORQUE INDICATION FLUCTUATING. MAINTENANCE REPLACED IEC COMPUTOR FOR RIGHT ENGINE. 2 L 7 2 4T RT A41NM 1999100100415 19991001 00415 EU 1999 10 1 99ZZZM663 1 19990603 A 5313 S53574300200 STRINGER AEROSP ATR42 ATR42300 8680920 EU FRAME 24/27 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 SPECIAL STRINGER ON LOWER KEEL BEAM, RIGHT SIDE HAS CORROSION BETWEEN FRAMES 24A RT AND 27A RT. CAUSE OF CORROSION DETE RMINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW 26 PERCENT MATERIAL THICKNESS SRM 53-51-00 PA GE 304. (M) 2 H 7 2 4T RT A53EU 1999100100416 19991001 00416 EU 1999 10 1 99ZZZM664 1 19990603 A 5320 S5397000420000 FITTING AEROSP ATR42 ATR42300 8680920 EU FRAME 27 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FUSELAGE ATTACH FITTING FOR SPLICE CONNECTING FRAMES 27A RT AND LT CORRODED. CAUSE OF CORROSION DETERMINED TO BE ENVIR ONMENTAL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M) 2 H 7 2 4T RT A53EU 1999100100417 19991001 00417 EU 1999 10 1 99ZZZM665 1 19990603 A 5312 S53174000200 BULKHEAD WEB AEROSP ATR42 ATR42300 8680920 EU FWD PRESS BLKHD CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FORWARD BULKHEAD BONDING STRIP AT 11:00 O'CLOCK POSITION HAS CORROSION PITTING. CAUSE OF CORROSION DETERMINED TO BE ENV IRONMENTAL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M) 2 H 7 2 4T RT A53EU 1999100100418 19991001 00418 EU 1999 10 1 99ZZZM666 1 19990603 A 5311 S5397140226051 FRAME AEROSP ATR42 ATR42300 8680920 EU FRAME 27 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 FRAME 27A LT CORRODED INBOARD OF LOWER INTERCOSTAL. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLEND ED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M) 2 H 7 2 4T RT A53EU 1999100100419 19991001 00419 1999 10 1 RAIA990902 4 19990902 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 552HK 41057 FLT 7174 - STL - COMPARATOR ERROR NR 2 AHRS. MAINTENANCE REPLACED NR 2 AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999100100420 19991001 00420 1999 10 1 RAIA990903 4 19990902 A 2350 7510700806 RMU JETAIR JETSTM JETSTM4101 1500501 EU NR 2 COM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 560HK 5338 41076 FLT 6192 - JFK - UNABLE TO TRANSMIT ON NR 2 COM. MAINTENANCE REPLACED RADIO MANAGEMENT UNIT ON F/O'S SIDE. (M) 2 L 7 2 4T RT A41NM 1999100100421 19991001 00421 NE 1999 10 1 RAIA990901 2 19990902 A 7200 ENGINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 421TE 22157 102 120530 FLT 7109 - NR 2 ENGINE TEMPS OUT BEFORE REACHING TARGET TORQUE. MAINTENANCE REPLACED NR 2 ENGINE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999100100422 19991001 00422 1999 10 1 RAIA990905 4 19990904 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 560HK 7613 41076 FLT 6153 - JFK - HEADING COMPARATOR. MAINTENANCE REPLACED NR 2 AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999100100423 19991001 00423 EU 1999 10 1 RAIA990906 1 19990905 A 3244 TIRE BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 871JX 871 FLT 4733 - LAX - RIGHT MAIN TIRE BLOWN. MAINTENANCE REPLACED RIGHT MAIN WHEEL ASSY. (M) 2 L 7 2 4T RT A56EU 1999100100424 19991001 00424 EU 1999 10 1 RAIA990907 1 19990905 A 3242 AH54450 BRAKE BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 871JX 871 FLT 4733 - LAX - RIGHT MAIN TIRE BLEW ON TAKEOFF. MAINTENANCE REPLACED RIGHT MAIN BRAKE ASSY. (M) 2 L 7 2 4T RT A56EU 1999100100425 19991001 00425 EU 1999 10 1 RAIA990841 1 19990821 A 7931 1241012 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 560HK 41076 FLT 7710 - JFK - LEFT OIL PRESS FLUCTUATING. MAINTENANCE REPLACED OIL PRESS TRANSDUCER FOR LEFT ENGINE. (M) 2 L 7 2 4T RT A41NM 1999100100426 19991001 00426 EU 1999 10 1 RAIA990908 1 19990907 A 2913 PV304426 HYD PUMP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 343TE 9407 955 FLT 7533 - FWA - RIGHT ENGINE HYDRAULIC PRESSURE DROPPED TO ZERO. MAINTENANCE REPLACED RIGHT ENGINE HYD PUMP. (M) 2 L 7 2 4T RT A56EU 1999100100427 19991001 00427 NM 1999 10 1 99ZZZM667 1 19990831 A 7921 AS3209219 PACKING DHAV DHC8 DHC8103 1386005 NM LT OIL COOLER CUT A ERAA E ENGINE SHUTDOWN K Y FLUID LOSS ENGINE STOPPAGE CR CRUISE 1 AL 03 881EA 01901009 233 OIL PRESS CAUTION LIGHT FLICKERED DURING CLIMB-OUT FROM CDV. NR 2 ENGINE OIL PRESS DROPPED TO ZERO IN CRUISE. SHUTDOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT ANC. OIL LEAK AT NR 2 ENGINE OIL COOLER INLET DUE TO CUT O-RING. ENGINE RE PLACED DUE TO OIL STARVATION. (M) 2 H 7 2 4T RT A13NM 1999100100428 19991001 00428 EU 1999 10 1 C2XA99BT084 1 19990831 A 3350 301210 LIGHT AEROSP ATR72 ATR72212 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69901 379 EWR - FLT 3354 - DURING MAINTENANCE, FOUND AIRSTAIR DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AIRSTAI R DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999100100429 19991001 00429 EU 1999 10 1 C2XA99IA453 1 19990902 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING SCHEDULED MAINTENANCE, SEVERAL AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NR 2 AND NR 3 EMERGENCY LIGHT BATTERIES. THE SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100430 19991001 00430 SO 1999 10 1 C2XA99BT083 1 19990901 A 3350 1317 BULBS EMB 145 EMB145 SO EXTERIOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15941 145035 BTV - FLT 4218 - DURING 3A INSPECTION, MAINTENANCE FOUND BOTH RT AND LT EXTERIOR EMERGENCY EXIT LIGHTS TO BE INOPERATIVE . REMOVED AND REPLACED LIGHT BULBS ON LT AND RT. OVERWING EMERGENCY EXIT LIGHTS. OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999100100431 19991001 00431 NE 1999 10 1 C2XA99IA454 2 19990901 A 7200 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE RIGHT FAILED A C2XA A E UNSCHED LANDING ENGINE SHUTDOWN Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 SW 09 42836 200 PCE120791 BPT - FLT 404 - DURING A TRAINING FIGHT, THE PILOT REPORTE THAT THE NR 2 ENGINE PRODUCED 4 LOUD BANGS, ASSOCIATED WITH A FIRE INDICATION. THE CREW DISCHARGED THE ENGINE FIRE BOTTLES AND LANDED AT BPT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE ENGINE TO HAVE SUFFERED INTERNAL DAMAGE, CAUSING DAMAGE TO ADJACENT COMPONENTS. MAINTENANCE REMOVED AND REPLA CED THE ENGINE AND AFFECTED COMPONENTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999100100432 19991001 00432 EU 1999 10 1 C2XA99IA452 1 19990829 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14451 512 IAH - DURING SCHEDULED MAINTENANCE, SEVERAL AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NR 3 EMERGENCY LIGHT BATTERY. THE SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100433 19991001 00433 GL 1999 10 1 C2XA99BT085 2 19990902 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XA O OTHER M OVER TEMP TX TAXI/GRND HDL 1 SW 09 12934 4116 145019 CAE310073 AFTER LANDING IN YUL, REPORTED NR 1 ENGINE HIGH ITT AND ENGINE AUTO SHUTDOWN. MAINTENANCE TROUBLESHOT ENGINE FOUND NO D EFECTS WITH BOROSCOPE AND POWER ASSURANCE RAN ENGINE WITHIN LIMITS. MAINTENANCE FERRIED AIRCRAFT TO BTV AND PERFORMED E NGINE CHANGE. OPS CHECKED ENGINE GOOD. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999100100434 19991001 00434 NE 1999 10 1 C2XA99BT086 2 19990906 A 7200 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 18814 FAILED 103 120894 EWR - CREW REPORTED NR 2 ENGINE BLOWING SMOKE IN CABIN. MAINTENANCE FERRIED AIRCRAFT TO BTV FOUND OIL LEAKAGE INTO COMP RESSOR SECTION, PERFORMED ENGINE CHANGE. OPS CHECKED ENGINE, NO SMOKE IN CABIN, AND RETURNED AIRCRAFT TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999100100435 19991001 00435 GL 1999 10 1 C2XA99BT075 2 19990726 A 7230 COMPRESSOR EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 1 ENGINE DAMAGED A C2XA E ENGINE SHUTDOWN E VIBRATION/BUFFET LD LANDING 1 SW 09 14952 2452 145067 310104 EWR - FLT 3984 - CREW REPORTED NR 1 ENGINE SHUTDOWN UPON LANDING GOING INTO REVERSE. MAINTENANCE FOUND NR 1 ENGINE HP V IBRATION TO BE OFF THE SCALE, BOROSCOPED 9TH STAGE COMPRESSOR AND FOUND DAMGE WITH METAL IN INNER BYPASS DUCT. REMOVED AND REPLACED THE ENGINE PERFORMED OPS CHECKS, ALL CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 1999100100436 19991001 00436 NE 1999 10 1 ASOA99083 2 19990826 A 7200 ENGINE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE LEFT FAILED A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 634AS 370 127020 EN ROUTE TO ATL, LEFT ENGINE OIL PRESSURE DROPPED TO 0 PSI. CAPTAIN PERFORMED ENGINE FAILURE IN FLIGHT CHECKLIST, DECLA RED AN EMERGENCY, AND PERFORMED A SAFE SINGLE ENGINE LANDING AT CSG. MCN MAINTENANCE CREW FOUND NR 3/4 BEARING OIL TUBE CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE ASSY AND OIL COOLER. PROPELLER ACTUATOR WAS ALSO REPLACED D UE TO METAL CONTAMINATION. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999100100437 19991001 00437 WP 1999 10 1 ORJA99258 1 19990811 A 3240 26088921 BRAKE DOUG DC9 DC983 3022083 WP NR 1 BRAKE ASSY FAILED A ORJA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 11 882RA 49949 LAS-LAX - FLT 2803 - HEAVY BRAKING REQUIRED DURING TAXI FOR TAKEOFF. NR 1 BRAKE LOCKED UP, AIRCRAFT UNABLE TO TAXI UNDE R POWER. AIRCRAFT TOWED TO GATE. REMOVED AND REPLACED NR 1 BRAKE ASSY PER MM 32-42-01. LEAK AND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999100100438 19991001 00438 NE 1999 10 1 EISA99158 2 19990821 A 7200 ENGINE BOEING 727 7272A7 138407K NM PWA JT8 JT8D7B 52053 NE NR 3 FAILED A EISA O OTHER M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 07 310NE 20241 648852 NR 3 ENGINE EGT REACHED RED LINE ON TAKEOFF. REPLACED NR 3 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999100100459 19991001 00459 WP 1999 10 1 AALA991328 1 19990906 A 2530 2510000308 OVEN DOUG DC9 DC982 3022082 WP NR 3 GALLEY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 556AA 0896 53086 MIA-YUL - FLT 470 - AFTER TAKEOFF, SMOKE NOTED FROM NR 3 GALLEY OVEN. GALLEY POWER WAS TURNED OFF IN FLIGHT AND AIRCRAF T RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 3 GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100460 19991001 00460 WP 1999 10 1 AALA991369 1 19990910 A 2612 892809040003 FIRE CONTROLLER DOUG DC9 DC982 3022082 WP E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 472AA 6388 49647 MCI-ORD - FLT 1546 - AFTER TAKEOFF, APU FIRE WARNING LIGHT FLICKERED ON AND OFF. APU WAS SHUT DOWN AND AIRCRAFT LANDED MCI WITHOUT INCIDENT. REPLACED APU FIRE DETECTION LOOP CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100461 19991001 00461 WP 1999 10 1 AALA991366 1 19990909 A 3222 59104475071 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 489AA 49682 DFW - FLT 1949 - ON TAKEOFF, AUS NOSE LANDING GEAR DID NOT RETRACT WHEN GEAR RETRACT HANDLE RAISED. AIRCRAFT RETURNED T O DFW AND LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT ASSEMBLY AND CYCLED NOSE LANDING GEAR. SYSTEM GROUND CHECKED NO RMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100462 19991001 00462 NM 1999 10 1 AALA991332 1 19990907 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 603AA 27054 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXI TFLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. RECONNECTED WIRING TO EM ERGENCY EXIT FLOOR PATH LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999100100463 19991001 00463 NM 1999 10 1 AALA991325 1 19990905 A 3350 1000679 LIGHT BOEING 767 767323 1385205 NM COCKPIT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373AA 25200 JFK - FLT 34 - ON LANDING, FLIGHT DECK EMERGENCY EXIT LIGHT ASSY DISLODGED FROM SOCKET. REPLACED FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999100100464 19991001 00464 NM 1999 10 1 AALA991313 1 19990831 A 3350 S283N00219 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 632AA 24590 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD LEFT OVERWING EXIT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT FORWARD LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999100100465 19991001 00465 NM 1999 10 1 AALA991319 1 19990901 A 3350 CONNECTOR BOEING 757 757223 1384957 NM ROW 16D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 184AN 29594 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEAT ROW 16D AND 1E INOPERATIVE. RESEATED ELECTRICAL CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEAT ROW 16D AND 1E. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A2NM 1999100100466 19991001 00466 NM 1999 10 1 AALA991320 1 19990902 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636AM 24594 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT AFT RIGHT LAVATORY INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHT STRIP AT AFT RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999100100467 19991001 00467 NM 1999 10 1 AALA991307 1 19990901 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 9D DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 662AA 25296 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 9D INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT STRIP AT SEAT ROW 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999100100468 19991001 00468 EU 1999 10 1 AALA991296 1 19990830 A 2133 88005B0306 OUTFLOW VALVE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CONTAMINATED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77080 536 626 MIA-LIM - FLT 917 - DURING CLIMB-OUT, UNABLE TO CONTROL CABIN PRESSURIZATION OR OUTFLOW VALVE. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND INSULATION BLOCKING OUTFLOW VALVE AND CLOGGING SCREEN. CLEARED INSULATION AND REPL ACED OUTFLOW VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999100100469 19991001 00469 EU 1999 10 1 AALA991326 1 19990901 A 2130 A90A CHECK VALVE FOKKER F28 F28MK0100 4990807 EU FWD FUSELAGE DEFECTIVE A AALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 1425A 11408 MEM - FLT 1460 - EN ROUTE DFW-GSO, UNABLE TO CONTROL CABIN PRESSURIZATION IN AUTO OR MANUAL MODE. EMERGENCY DESCENT ACC OMPLISHED TO 10,000 FT. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO DFW. REPLACED PRECO NDITIONED AIR CHECK VALVE. ALSO, REPLACED PRESSURIZATION CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. FUNCT IONAL CHECK FLIGHT ACCOMPLISHED WITH SATISFACTORY OPERATION NOTED. (M) 2 L 7 2 4F RT 1999100100470 19991001 00470 EU 1999 10 1 AALA991327 1 19990903 A 2131 21185266 CONTROLLER FOKKER F28 F28MK0100 4990807 EU E/E COMP DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1445B 29457 11448 ORD - FLT 528 - AFTER TAKEOFF, AIRCRAFT FAILED TO PRESSURIZE. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. RE PLACED NR 1 CABIN AIR PRESSURE CONTROLLER AND ALSO REPLACED STATIC OUTFLOW VALVE FILTER. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F RT 1999100100471 19991001 00471 EU 1999 10 1 AALA991316 1 19990902 A 3240 AAP2806 BRAKE FOKKER F28 F28MK0100 4990807 EU RT MLG DEFECTIVE A AALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 07 1436A MAY930976 11426 DFW - FLT 2087 - UPON LANDING AT DFW FROM OMA, NR 3 AND 4 MLG BRAKES LOCKED. NR 3 AND 4 BRAKES SMOKED WHICH REQUIRED AP PLICATION OF FIRE SUPRESSION FOAM. PASSENGERS WERE DEPLANED ON TAXI WAY. REPLACED NR 3 AND 4 BRAKES AND WHEEL/TIRE ASS EMBLIES. RIGHT WING, FUSELAGE AND RIGHT MAIN LANDING GEAR CLEANED OF FIRE SUPPRESSION FOAM. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F RT 1999100100472 19991001 00472 WP 1999 10 1 AALA991368 1 19990910 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 292AA 49304 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT FIRST CLASS GALLEY INOPERATIVE. REPLACE D EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100473 19991001 00473 WP 1999 10 1 AALA991382 1 19990912 A 3350 0201720003 LIGHT DOUG DC9 DC982 3022082 WP EXTERIOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 420AA 49332 ORD - DURING OVERNIGHT MAINTENANCE, LEFT OUTBOARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT OUTBOARD EXT ERIOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100474 19991001 00474 WP 1999 10 1 AALA991365 1 19990909 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77421 49333 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH MARKER LIGHT AT AFT GALLEY INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH MARKER LIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100475 19991001 00475 WP 1999 10 1 AALA991356 1 19990908 A 3350 L201919 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 249AA 49269 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON CEILING IN FRONT OF AFT CABIN DOOR INOPERATIVE. REPLACED LI GHT ASSEMBLY ON CEILING IN FRONT OF AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100476 19991001 00476 WP 1999 10 1 AALA991305 1 19990901 A 3350 P4010051111 CONTROL MODULE DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 594AA 53284 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED AISLE PATH LIGHTING CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1999100100477 19991001 00477 WP 1999 10 1 AALA991308 1 19990830 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437AA 49455 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100478 19991001 00478 WP 1999 10 1 AALA991315 1 19990902 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 499AA 49737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY AND AFT OF COACH CABIN INOPERAT IVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AT FORWARD GALLEY AND AFT OF COACH CABIN. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100479 19991001 00479 WP 1999 10 1 AALA991314 1 19990902 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT AIRSTAIRS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 496AA 49734 IAH - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPAIRED WIRE TO EMERGENCY LIGHT AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100480 19991001 00480 WP 1999 10 1 AALA991322 1 19990903 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7517A 49894 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD OVERWING EXIT INOPERATIVE. REPLACE D EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100481 19991001 00481 WP 1999 10 1 AALA991324 1 19990906 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP AFT AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 486AA 49679 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASS EMBLY AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999100100482 19991001 00482 WP 1999 10 1 AALA991335 1 19990907 A 3350 L201919 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 288AA 49300 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT CEILING FORWARD OF VENTRAL AIRSTAIR DOOR INOPERATIVE. R EPLACED EMERGENCY EXIT LIGHT AT AFT CEILING FORWARD OF VENTRAL AIRSTAIR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 1999100100483 19991001 00483 NM 1999 10 1 GAIA99133 1 19990909 A 3610 10610652 DUCT BOEING 727 727223 1384074 NM NR 3 PYLON LEAKING A GAIA K NONE M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 07 858AA 21085 FLT 727 - MKE-TOL - ENCOUNTERED DURING CRUISE AN OVERHAT DETECTION ON NR 3 PYLON. THE LIGHT EXTINGUISHED WHEN THE THROT TLE WAS RETURNED TO IDLE. THE AIRCRAFT CONTINUED TO TOL AND LANDED SAFELY WITHOUT FURTHER DIFFICULTIES. REMOVED AND RE PLACED THE HIGH PRESSURE BLEED FLEX DUCT IN NR 3 PYLON. LEAK CHECK GOOD ON GROUND. THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 3 4F A3WE 1999100100484 19991001 00484 NM 1999 10 1 GAIA99134 1 19990807 A 2613 OVERHEAT LIGHT BOEING 727 727222 1384073 NM NR 3 ENGINE ILLUMINATED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 90AX 20040 FLT 302 - DFW-TYS - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. FOLLOWED KHA PROCEDURE AND CONT INUED OPERATION ON NR 2 BLEED. THE AIRCRAFT LANDED SAFELY AT TYS WITHOUT FURTHER DIFFICULTY. INSPECTED ALL BLEED AIR P LUMBING, FITTINGS, OVERHEAT CONNECTORS AND CLAMPS. GROUND RAN ENGINE AND NO LEAKS OR DEFECTS NOTED. THE AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999100100485 19991001 00485 NM 1999 10 1 GAIA99136 1 19990815 A 2613 OVERHEAT LIGHT BOEING 727 727222 1384073 NM NR 3 ENGINE ILLUMINATED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 90AX 20040 FLT 202 - TYS-DFW - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. FOLLOWED PROCEDURE IN AOM AND L IGHT EXTINGUISHED. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER DIFFICULTY. RAN NR 3 ENGINE AT 80 PERCENT EPR AND COULD NOT DUPLICATE PROBLEM ON GROUND. OPERATIONAL CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1999100100486 19991001 00486 NM 1999 10 1 GAIA99138 1 19990901 A 2612 65249203 FIRE LOOP BOEING 727 727223 1384074 NM LOWER BODY INTERMITTENT A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 855AA 20996 MDT-TOL - FLT 1503 - LOWER BODY OVERHEAT LIGHT FLASHED THEN ILLUMINATED STEADY WHILE CLIMBING THROUGH 14,000 FT. RETARD ED NR 2 ENGNE TO IDLE AND LIGHT FLICKERED 30 SECONDS THEN WENT OUT. NR 2 BLEEDS WERE CLOSED AND NO DUCT TEMP WAS NOTED. ADVANCED NR 2 THROTTLE AND LIGHT STAYED OUT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT TOL. REMOVED AND REPLACED FIRE A ND OVERHEAT DETECTION BOX. RAN ENGINES TO TAKEOFF POWER AND COULD NOT FIND ANY PNEUMATIC LEAKS. NO OTHER DEFECTS FOUND WITH OVERHEAT SYSTEM. GROUND TESTED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999100100487 19991001 00487 NM 1999 10 1 GAIA99139 1 19990903 A 3610 CLAMPS BOEING 727 727223 1384074 NM AFT AIRSTAIR LOOSE A GAIA K NONE M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 07 855AA 20996 ATL-TOL - FLT 517 - WHILE TURNING ON ENGINE ANTI-ICE, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. TURNING OFF LEFT PACK AND REDUCING ENGINE NR 1 THRUST HAD NO AFFECT. TURNING OFF RIGHT PACK AND ENGINE NR 3 BLEED VALVE MADE LGIHT EXTINGUISH . AIRCRAFT MADE AN UNEVENTFUL LANDING AT TOL. FOUND LOOSE CLAMPS IN AFT AIRSTAIR AREA. SECURED CLAMPS AND READJUSTED AFT AIRSTAIR OVERHAT LOOP. RAN ENGINES AT POWER WITH BOTH PACKS ON AND ENGINE ANTI-ICE ON, NR 1 AND NR 3 BLEEDS OPEN. A FT BODY OVERHEAT DID NOT ILLUMINATE. COULD NOT DUPLICATE ON GROUND. SYSTEM TEST OK AND AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 3 4F A3WE 1999100100488 19991001 00488 NM 1999 10 1 GAIA99135 1 19990813 A 2613 OVERHEAT LIGHT BOEING 727 727222 1384073 NM NR 3 ENGINE ILLUMINATED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 90AX 20040 FLT 202 - DFW-SEA - DURING CRUISE, HAD THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATE. ACCOMPLISHED PROCEDURE AS PER A OM VOL 1 AND LIGHT EXTINGUISHED. THE AIRCRAFT LANDED SAFELY AT TYS WITHOUT FURTHER DIFFICULTY. INSPECTED NR 3 ENGINE A ND STRUT FIRE LOOPS AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999100100489 19991001 00489 NM 1999 10 1 GAIA99137 1 19990824 A 3610 CLAMP BOEING 727 727223 1384074 NM NR 3 STRUT LOOSE A GAIA K NONE M N OVER TEMP FALSE WARNING CR CRUISE 1 SW 07 858AA 21085 FLT 709 - MSP-TOL - ENCOUNTERED DURING CRUISE AN OVERHEAT DETECTION ON NR 3 PYLON. THE AIRCRAFT CONTINUED TO TOL AND LA NDED SAFELY WITHOUT FURTHER DIFFICULTIES. FOUND LOOSE DUCT CLAMP IN NR 3 ENIGNE STRUT. TIGHTENED CLAMP AND DUCT LEAKS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999100100490 19991001 00490 NM 1999 10 1 GAIA99140 1 19990914 A 2613 356644400 OVERHEAT LOOP BOEING 727 727223 1384074 NM NR 3 STRUT INTERMITTENT A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 858AA 21085 ORD-TOL - FLT 713 - ON CLIMB-OUT, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED STRUT OVERHEAT CHECKLIST. THE LIGHT EXTINGUISHED WHEN THE RIGHT PACK AND NR 3 BLEED SWITCHES WERE CLOSED. THE AIRCRAFT CONTINUED TO TOL AND LANDED SAFELY WITHOUT FURTHER DIFFICULTIES. REMOVED AND REPLACED NR 3 STRUT OVERHEAT SENSING LOOP. RAN ENGINES AT POWER AND CRUISE S ETTINGS WITH RT PAC ON AND NR 3 BLEED OPEN. NO LEAKS WERE FOUND AND THE STRUT OVERHEAT LIGHT DID NOT ILLUMINATE. A 34 MINUTE EVALUATION FLIGHT WAS PERFORMED (CLIMB AND CRUISE) WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 L 7 3 4F A3WE 1999100100491 19991001 00491 EU 1999 10 1 RAIA990915 1 19990913 A 7712 8972605 DELTA P/P BOX BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 340TE 939 FLT 7542 - COU - RIGHT ENGINE WOULD'NT MAKE TARGET TORQUE. MAINTENANCE REPLACED DELTA P/P BOX. (M) 2 L 7 2 4T RT A56EU 1999100100492 19991001 00492 EU 1999 10 1 RAIA990914 1 19990912 A 7722 6100116 EGT GAUGE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 03 340TE 939 FLT 7038 - COU - LEFT ENGINE EGT ERRATIC. MAINTENANCE REPLACED LEFT EGT GAUGE. (M) 2 L 7 2 4T RT A56EU 1999100100493 19991001 00493 EU 1999 10 1 RAIA990910 1 19990911 A 7712 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 343TE 4777 955 FLT 7444 - STL - RIGHT ENGINE RPM GAUGE INOPERATIVE. MAINTENANCE REPLACED TACH GENERATOR FOR RIGHT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999100100494 19991001 00494 1999 10 1 RAIA990909 4 19990908 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 560HK 41076 FLT 6215 - JFK - LEFT PITCH, ROLL AND ATTITUDE COMPARITOR. MAINTENANCE REPLACED NR 1 AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999100100495 19991001 00495 WP 1999 10 1 RAIA990913 2 19990912 A 7310 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 871JX 871 66065 FLT 4705 - PSP - LEFT ENGINE WILL NOT MAKE TORQUE. MAINTENANCE REPLACED FUEL BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999100100496 19991001 00496 EU 1999 10 1 RAIA990911 1 19990913 A 7712 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 342TE 2858 954 FLT 7456 - STL - RIGHT RPM FLUCTUATES. MAINTENANCE REPLACED TACH GENERATOR FOR RIGHT ENGINE. (M) 2 L 7 2 4T RT A56EU 1999100100497 19991001 00497 EU 1999 10 1 RAIA990912 1 19990913 A 6120 31058993 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 569HK 7616 41088 FLT 6221 - JFK - LEFT ENGINE IEC FAILED. MAINTENANCE REPLACED NTS PRESS SWITCH FOR LEFT ENGINE. (M) 2 L 7 2 4T RT A41NM 1999100100498 19991001 00498 NM 1999 10 1 99ZZZM688 1 19990913 A 2923 5718610 PUMP BOEING 737 7373G7 1384595 NM LEFT FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 150AW 50746 2586 23218 CLIMBING OUT AT 4000 FT, THE 'A' HYDRAULIC PUMP OVERHEAT LIGHT CAME ON. PUMP TURNED OFF PER QPH. MAINTENANCE NOTIFIED AND RETURNED LAS. REPLACED 'A' PUMP IAW CARD R4M29002. (M) 2 L 7 2 4F RT A16WE 1999100100499 19991001 00499 WP 1999 10 1 GTIA9900980 1 19990505 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1305 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 MHV - PREVIOUS REPAIRED PANEL CRACKED AT LIGHTENING HOLE AND RIVETS FS 1305 LEFT SIDE BELOW FLOOR ON SUPPORT. REMOVED P REVIOUS REPAIR CUT OUT DAMAGE FABRICATED REPAIR DOUBLER PO NR B1056 7075T6.050 ALODINED AND PRIMED REPAIR PART IAW MD80 SRM 51-10-3. INSTALLED FASTENERS AND REPAIR PART WET WITH PR1422 SEALANT B.5 PER MD80 SRM 53-01 PAGE 9 FIG 2 SHEET 3 AN D MD80 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999100100500 19991001 00500 WP 1999 10 1 GTIA9900981 1 19990517 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 527779761200 49144 MHV - AFT LEFT LAV CUSP ANGLE AT CENTER OUTBOARD FLOOR LEVEL SHOWS EVIDENCE OF CORROSION. REMOVED DAMAGED PORTION OF LT CUSP STATION 1338 L18. INSTALLED DOUBLER AND EXTRUSION IAW DC9 MD80 SRM 53-14-3, 53-05 FIG 25 AND 51-10-3. (M) 2 L 7 2 4F A6WE 1999100100501 19991001 00501 WP 1999 10 1 GTIA9900982 1 19990514 A 5320 HAT SECTION DOUG DC9 DC982 3022082 WP BS 1120 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 800NK 49144 MHV - STATION 1120 LBL 50 SMALL HAT SECTION NEAR GALLEY SERVICE DOOR HAS EXFOLIATION CORROSION AND INTERGRANULAR CORROSI ON. FABRICATED REPLACEMENT HAT SECTION SUPT PER EXAMPLE SUPPLIED IN REF MD MM 51-10 HEAT TREATED AND AGE HARDENED PER A MS-H-6088 DELIVERED TO A/C FOR FIT AND INSTALL ON W/O A093-S03-Y035. (M) 2 L 7 2 4F A6WE 1999100100502 19991001 00502 WP 1999 10 1 GTIA9901035 1 19990608 A 5313 LONGERON DOUG DC9 DC941 302207N WP BS 1041 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FOUND STATION 1041, STATION 1051 LONGERON NR 17 CRACKED BOTH MARKED IN RED. REMOVED AND REPLACED LONGERON NR 17 S TATION 1041 AND 1051 AND SHOVEL CUPS PER SRM 51-10-1 AND 51-30-2 LONGERON INSTALLED USING EXISTING SPLICES. (M) 2 L 7 2 4F A6WE 1999100100503 19991001 00503 WP 1999 10 1 GTIA9901036 1 19990609 A 5320 ANGLE DOUG DC9 DC941 302207N WP BS 1041 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FOUND STATION 1041 LEFT SIDE A/C AFT SIDE OF FRAME ANGLE (FRAME TO LONGERON) AT LONGERON NR 17 CRACKED. REMOVED A ND REPLACED ANGLE IAW SRM 51-01 PAGE 1 APPLIED SEALANT IAW SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS IA W SRM 51-01 PAGE 1 APPLIED SEALANT IAW SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS IAW SRM 51-30-2 PAGE 6 FIG 5 REF FO54 FOR FABRICATED ANGLE. (M) 2 L 7 2 4F A6WE 1999100100504 19991001 00504 WP 1999 10 1 GTIA9901037 1 19990528 A 5320 CLIP DOUG DC9 DC941 302207N WP BS 1041 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - STATION 1041 LEFT SIDE A/C FORWARD SIDE OF FRAME SHEER CLIP BETWEEN LONGERON 16 AND 17 CRACKED. REMOVED AND REPLA CED SHEAR CLIP IAW SRM 51-01 PAGE 1 APPLIED SEALANT IAW DC9 SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS I AW SRM DC9 51-30-2 PAGE 6 FIG 5. (M) 2 L 7 2 4F A6WE 1999100100505 19991001 00505 WP 1999 10 1 GTIA9901038 1 19990602 A 5330 6AL4V SKIN DOUG DC9 DC941 302207N WP BS 313 DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FORWARD FUSELAGE SKIN AT STATION 313 NEAR BOTTOM OF FUSELAGE HAS A 1.5 INCH BY 1 INCH DENT. CUT OUT DAMAGE IAW DC 9 SRM 53-04 FIG 38 VIEW 1. FABRICATED DOUBLER AND FILLER INSTALLED REPAIR COMPLETE IAW SRM 53-04 FIG 38 AND DC9 SRM 51- 30-2. (M) 2 L 7 2 4F A6WE 1999100100506 19991001 00506 WP 1999 10 1 GTIA9901039 1 19990610 A 5315 FLOORBEAM DOUG DC9 DC941 302207N WP BS 180 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - E/E BAY STATION 180 LBL 22 FLOORBEAM WEB CRACKED FORWARD SIDE AND ANGLE ON AFT SIDE CRACKED. FABRICATED DOUBLER I W DC9 SRM 53-05 PAGE 227. TREATED AND PRIMED DOUBLER IAW DC9 SRM 51-10-3. INSTALLED DOUBLER IAW DC9 SRM 53-05 PAGE 227 . (M) 2 L 7 2 4F A6WE 1999100100507 19991001 00507 WP 1999 10 1 GTIA9901040 1 19990611 A 5315 FLOORBEAM DOUG DC9 DC941 302207N WP BS 180 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - E/E BAY STATION 180 UPPER FLOORBEAM AT BL 0 AFT ANGLE CRACKED AND WEB BOW. REMOVED DAMAGED ANGLE FABRICATED NEW A NGLE FROM 7075T6.032 PO NR 84365 ALODINED AND PRIMED ANGLE IAW SRM 51-10-3 AND INSTALLED ANGLE IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999100100508 19991001 00508 WP 1999 10 1 GTIA9901041 1 19990610 A 5315 FLOORBEAM DOUG DC9 DC941 302207N WP BS 180 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - E/E BAY STATION 180 LBL 20 FLOORBEAM CRACKED 3 PLACES FORWARD SIDE OF WEB. FABRICATED REPAIR DOUBLER PER SRM 53-0 5 PAGE 227 AND 247 FIG 17 FROM 7075T6.032 PO NR 84365 ALODINED AND PRIMED PARTS PER SRM 51-10-3 AND INSTALLED DOUBLER IA W DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999100100509 19991001 00509 WP 1999 10 1 GTIA9901042 1 19990616 A 5313 LONGERON DOUG DC9 DC941 302207N WP BS 237-323 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 27774221 47604 MHV - FOUND STATION 237-277 STRINGER 16L AND STATION 237-323 STRINGER 17L LONGERONS CRACKED AT FRAME ATTACH POINTS. REM OVED AND REPLACED STRINGER 16L FROM STATION 237-277 STRINGER 17L FROM 237-323 IAW DC940 SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999100100510 19991001 00510 WP 1999 10 1 GTIA9901043 1 19990612 A 5330 MS247054 SKIN DOUG DC9 DC941 302207N WP BS 1123 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - REF CARRY OVER ITEM NR 0154 AT FS 1123 NON PRESSURIZED SKIN AT LONGERON 10R, THERE IS A 3 INCH CRACK WITH A CLASS III TEMP REPAIR INSTALLED. CUTOUT DAMAGE AREA IAW DC9 SRM 53-01 FIG 4 SHT 2. FABRICATED DOUBLER AND PLATE IAW DC9 SRM 53-01 FIG 4 SHT 3. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED DOUBLER AND PLATE IAW DC9 SRM 51-30-2 PAGE 1. ( M) 2 L 7 2 4F A6WE 1999100100511 19991001 00511 WP 1999 10 1 GTIA9901045 1 19990613 A 5330 SKIN DOUG DC9 DC941 302207N WP BS 229-305 GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - W/O'S A096-503-F032, F034, F029 SKIN DENTS AND GOUGE STATION 229 TO STATION 305 APPROX TO BE WORKED ON THIS NON-RO UTINE. REMOVED DENTS AND GOUGES AT STATION 229 TO STATION 305 APPROX BETWEEN STRINGER 16L AND 17L AND REPAIRED PER DRAW ING NR 53-99294-1. (M) 2 L 7 2 4F A6WE 1999100100512 19991001 00512 WP 1999 10 1 GTIA9901046 1 19990610 A 5320 SB0953018611 DOUBLER DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - AS MARKED EDDY CURRENT INSPECTION REVEALS A CRACK ON THE FWD PART OF DOUBLER FROM THE FASTENER HOLE TO THE END ON UPPER ANTI-COLLOSION LIGHT. RADIUS OUT CRACK, CRACK REMOVAL BOUGHT OFF BY NDT TRIMMED -17 SHIM AND LAYOUT OF -11 DOUBLE R PER SB 53-186 PAGE 41 FIG 5 SHT 5 - 7. COUNTER SANK ALODINED AND PRIMED IAW DC9 SRM 51-10-3 AND INSTALLED -17 SHIM AN D -11 DOUBLER IAW SB 53-186 PAGE 43 FIG 5 SHT 5 O 7. (M) 2 L 7 2 4F A6WE 1999100100513 19991001 00513 WP 1999 10 1 GTIA9901047 1 19990610 A 5312 BULKHEAD DOUBLER DOUG DC9 DC941 302207N WP BS 1219-1244 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 7075T6X071 47604 MHV - STATION 1219-1244 FORWARD OF CANTED BULKHEAD DOUBLER WHERE HARNESS GOES THROUGH IS EXFOLIATING AND CRACKED AFT ACC ESSORY AREA. FABRICATED NEW DOUBLER AND INSTALLED IAW DC9 SRM 53-01 FIG 4 SHT 3. (M) 2 L 7 2 4F A6WE 1999100100514 19991001 00514 WP 1999 10 1 GTIA9901048 1 19990612 A 5320 CLIP DOUG DC9 DC941 302207N WP BS 1219-1244 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FOUND STATION 1219-1244 RT RBL 24 UPPERMOST CLIP UNDER VENT BOX CRACKED COMPLETELY THROUGH AFT ACCESSORY AREA. IN STALLED NEW CLIP AS PER SRM 51-10-1. (M) 2 L 7 2 4F A6WE 1999100100515 19991001 00515 WP 1999 10 1 GTIA9901050 1 19990608 A 5320 591000644 ANGLE DOUG DC9 DC941 302207N WP BS 710 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - RIGHT WING ROOT AREA .5 INCH CRACK INDICATION ON ANGLE 5910465-340 TO CENTER WING BOX APPROX BODY STATION 710. ND T VERIFY CRACK IN ANGLE. REMOVED AND REPLACED ANGLE AIW DC9 SRM 51-10-2, 51-10-4 AND 51-30-5. REINSTALLED FAIRINGS 3 P ANELS OPENED FOR ACCESS IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1999100100516 19991001 00516 WP 1999 10 1 GTIA9901051 1 19990610 A 5312 BULKHEAD T DOUG DC9 DC941 302207N WP BS 1127 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - T-EXTRUSION AT FS 1127 BULKHEAD IS CORRODED BEYOND USE. MACHINED T-EXTRUSION PER DC9 SRM 51-10 AND EXAMPLE ISSUED TO FLOOR IN BLANK CONDITION LOCATED AND DRILL REF A096S03L053. (M) 2 L 7 2 4F A6WE 1999100100517 19991001 00517 WP 1999 10 1 GTIA9901052 1 19990610 A 5312 1544612 BULKHEAD ANGLE DOUG DC9 DC941 302207N WP BS 1127 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - T-ANGLE ON BULKHEAD AT FS 1127 RUNNING FROM LONG L6 AND R6 HAS 3 GROUND OUT AREAS AND CORROSION IN EACH AREA. REM OVED AND REPLACED T-ANGLE PER SRM 51-10-1 AND 51-30-5 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999100100518 19991001 00518 WP 1999 10 1 GTIA9901053 1 19990615 A 5532 NAS1097AD65 SKIN DOUG DC9 DC941 302207N WP VERT STABILIZER MISREPAIRED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 130NK 47604 MHV - VERTICAL STABILIZER L/E ASSY AT STATION 2 FS 52.300 THERE IS AN EXISTING REPAIR THAT IS BLENDED AND FILLED WITH EP OXY 4 COUNTER SINKS BONDO HAS FALLEN OUT. CUT OFF BONDED FINGER DOUBLER FABRICATED TITANIUM REPAIR DOUBLER PER ENG G IN STRUCTION (DRAWING) AND INSTALLED FABRICATED REPAIR DOUBLER PER DC9 SRM 51-30-2 ( RIVET INSTALL) AND SRM 51-30-5 (HILOCK INSTALL). (M) 2 L 7 2 4F A6WE 1999100100519 19991001 00519 WP 1999 10 1 GTIA9901054 1 19990611 A 5320 JAMB DOUG DC9 DC941 302207N WP CARGO DOORWAY DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 2024T3040 47604 MHV - LOWER CARGO DOOR JAMB PAN REQ 2 EACH -19 AND -21 SPLICE ANGLE REPAIR. FABRICATED ANGLES -19 AND -21 PER DC9 IAW S RM 53-05 PAGE 107 AND 114 FIG 44 SHT 5 SECTION G-G. (M) 2 L 7 2 4F A6WE 1999100100520 19991001 00520 WP 1999 10 1 GTIA9901044 1 19990610 A 5314 S27779223040 LONGERON DOUG DC9 DC941 302207N WP BS 200 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FORWARD FUSELAGE STATION NR 200 AT LONGERON 24 LONGERON CRACKED. REMOVED CRACKED LONGERON FROM STATION 190 TO STA TION 228. FABRICATED LOCATED AND DRILLED LONGERON 24 AND SPLICE PER DC9 SRM 53-2. ALODINED AND PRIMED PER DC9 SRM 51-1 0-3. INSTALLED PARTS PER DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999100100521 19991001 00521 WP 1999 10 1 GTIA9901055 1 19990612 A 5315 FLOORBEAM DOUG DC9 DC941 302207N WP BS 237.5 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FLOORBEAM REPAIR AT STATION 237.5. MACHINED FLOORBEAM REPAIR PER DWG NR 53-9803-1. (M) 2 L 7 2 4F A6WE 1999100100522 19991001 00522 WP 1999 10 1 GTIA9901056 1 19990613 A 5330 SKIN DOUG DC9 DC941 302207N WP FUSELAGE SCRAPED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - REF SPIRIT CARRY OVER NR 0097 SKIN SCRAPES APPROX 1 FT AFT OF FORWARD BAGGAGE DOOR. NDT PERFORMED, NO CRACKS NOTE D. LIGHTLY BLENDED AREA AS REQUIRED PER SRM 53-04 FIG 38 SHT 2 FUSELAGE SKIN ALODINE AND PRIME IAW DC9 SRM 51-10-3. (M ) 2 L 7 2 4F A6WE 1999100100523 19991001 00523 WP 1999 10 1 GTIA9901057 1 19990616 A 5320 NAS1097AD65 JAMB DOUG DC9 DC941 302207N WP CARGO DOORWAY CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - LOWER AFT CORNER OF FORWARD CARGO PIT DOOR JAMB HAS A CRACK APPROX 2 INCH LONGERON IN THE TORQUE BOX. REMOVED DAM AGED AREA PER ENGINEERING AVQ-XXX-99-0001RR AND SPLICED IN NEW CARGO DOOR PAN PER DC9 -40 SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 1999100100524 19991001 00524 WP 1999 10 1 GTIA9901058 1 19990608 A 5315 FLOORBEAM DOUG DC9 DC941 302207N WP BS 237 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 130NK 47604 MHV - FORWARD CARGO CABIN FLOORBEAM STATION 237 LEFT 10 INCH CRACK IN FLOORBEAM AT SERVO FULLY BRACKET EXISTING REPAIR N EEDS FURTHER EVALUATION. COMPLETED REPAIR IAW DC9 SRM 53-05 AND RESEMBLE CARGO PANELS. (M) 2 L 7 2 4F A6WE 1999100100525 19991001 00525 WP 1999 10 1 GTIA9901074 1 19990811 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 DTW - EMERGENCY FLOOR TRACK LIGHTS BETWEEN ROWS 17 AND 21 INOPERATIVE. RESET BATTERIES AT STATION B5-237 PACK. OPERATI ONAL CHECK GOOD IAW MM 33-50-00. (M) 2 L 7 2 4F RT A6WE 1999100100526 19991001 00526 WP 1999 10 1 GTIA9901077 1 19990713 A 5330 2024T3050 SKIN DOUG DC9 DC941 302207N WP BS 261 GOUGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 MHV - GOUGE ON FUSELAGE LT SIDE STATION 261 BETWEEN L17 AND L18 APPROX 1 INCH IN LENGTH BY .032 INCH DEEP. REPAIRED FUS ELAGE PER DEM DRW 53-99357-1 CUT OUT DAMAGED SKIN FROM STATION 218-260 L15-18. FABRICATED NEW SKIN, SPLICE AND DOUBLERS IAW DWG NR 53-99357-1 AND DC9 SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW DWG 53-99357-1 AND DC9 SRM 51-30-2 AND SG 30-5 AND CORROSION TREATMENT IAW DC9 SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1999100100527 19991001 00527 WP 1999 10 1 GTIA9901078 1 19990709 A 5330 SKIN DOUG DC9 DC941 302207N WP BS 235 DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 MHV - DENT ON FUSELAGE LT STATION 235 BETWEEN L17 AND L18, 2 INCH HIGH BY 2 INCHES WIDE BY .060 DEEP. REPAIR ACCOMPLISH ED IN CONJUNCTION WITH WORK ORDER NR A107-503-F043, IAW ENGINEERING DRAWING NR 53-99357-1. (M) 2 L 7 2 4F A6WE 1999100100528 19991001 00528 WP 1999 10 1 GTIA9901079 1 19990709 A 5313 76378133 LONGERON DOUG DC9 DC941 302207N WP BS 287 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 47605 MHV - STATION 287 AT L17 LEFT LONGERON IS CRACKED AT LOWER FRAME TO LONGERON ATTACH HOLE. REPAIRED LONGERON PER DC9 SRM 53-02 PAGE 48 FIG 18 SHT 1, CUT OUT LONGERON FROM STATION 218-285. FABRICATED NEW LONGERON AND SPLICE IAW DC9 SRM 53-0 2 AND 51-10-2. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED PARTS IAW DC9 SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1999100100529 19991001 00529 WP 1999 10 1 GTIA9901080 1 19990713 A 5542 SKIN DOUG DC9 DC941 302207N WP RUDDER TORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 131NK 0502024T3 47605 MHV - RT LOWER RUDDER LOWER DAMPER ACCESS EDGE METAL TORN, CRACKED, PIECE BROKEN OUT. RUDDER REMOVED TO FACILITATE REPA IRS IAW ENG DWG 55-99375-1. RUDDER AND TAB REBALANCE AS REQUIRED PER DC9 SRM 55-40-1 AND REINSTALLED ON THE AIRCRAFT IA W DC9 MM 27-20-2. ACCOMPLISHED REPAIR IAW ENG DWG. (M) 2 L 7 2 4F A6WE 1999100100530 19991001 00530 WP 1999 10 1 GTIA9901081 1 19990817 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 10437 47526 MYR - FLT 619 - LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 320. REM OVED AND REPLACED LEFT EMERGENCY NACELLE BATTERY PACK IAW MM CHAPTER 33-53-0. OPERATION CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1999100100531 19991001 00531 WP 1999 10 1 GTIA9901084 1 19990818 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 17535 47111 MYR - BOTH EMERGENCY NACELLE LIGHTS INOPERATIVE. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 333. REPAIRED WIRING AT A FT FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS 'TEST' SWITCH. FUNCTIONAL CHECK GOOD, REF DC-9 WIRING DIAGRAMS 33-31-01. (M) 2 L 7 2 4F A6WE 1999100100532 19991001 00532 WP 1999 10 1 GTIA9901089 1 19990825 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 2651 47526 DTW - ROW TWO EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATION CHECKS GOOD IAW DC-9 MM 33-50-00. (M) 2 L 7 2 4F A6WE 1999100100533 19991001 00533 WP 1999 10 1 GTIA9901090 1 19990825 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - CENTER OVERHEAD LIGHT EMERGENCY LIGHT BROKEN. CENTER OVERHEAD PANEL ASSEMBLY REMOVED. REPLACED BULB AND SOCKET T O CENTER OVERHEAD LIGHT (EMERGENCY ASSEMBLY. REINSTALLED PANEL ASSEMBLY. SYSTEM AROUND CHECKED GOOD ALL IAW DC-9 MM SE CTION 33-00-0. (M) 2 L 7 2 4F A6WE 1999100100534 19991001 00534 WP 1999 10 1 GTIA9901091 1 19990805 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - AFT OVERHEAD EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED BULB AND SOCKET TO AFT OVERHEAD EMERGENCY LIGHT ASSEMBLY. SYSTEM CHECKED GOOD ALL IAW DC9 MM SECTION 33-00-00. (M) 2 L 7 2 4F A6WE 1999100100535 19991001 00535 WP 1999 10 1 GTIA9901092 1 19990825 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - LEFT UPPER EMERGENCY LIGHT IS OUT. RELAMPED, OPERATIONS CHECKS GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 1999100100536 19991001 00536 WP 1999 10 1 GTIA9901097 1 19990827 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP COCKPIT INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 3270 47202 DTW - COCKPIT EMERGENCY OVERHEAD LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY AND OPERATION CHECKS IAW DC-9 MM 33-50-00. OPERATION CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 1999100100537 19991001 00537 WP 1999 10 1 GTIA9901098 1 19990828 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941ML 47131 DTW - CABIN EMERGENCY FLOOR LIGHTS INTERMITTENTLY OFF IN FIRST 6 ROWS. CLEANED AND RESEATED CANNON PLUGS ON BATTERY PAC KS PERFORMED OPS CHECK IAW MM 33-50-00. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 1999100100538 19991001 00538 WP 1999 10 1 GTIA991104 1 19990831 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 ACY - FLT 430 - ONE RED STRIPPED EMERGENCY EXIT LIGHTING INOPERATIVE. REPAIRED WIRING AT EMERGENCY LIGHT STRIP IAW DC-9 MM 20-00. OPERATION CHECK OK. (M) 2 L 7 2 4F A6WE 1999100100539 19991001 00539 WP 1999 10 1 ORJA99248 1 19990721 A 3350 BR966115 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 9-15 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY LIGHTS FOR ROWS 9-15 CAME ON IN FLIGHT, EXTINGUISHED PRIOR TO LANDING, NO LONGER WORKING. REMOVED AND REPLACE D BATTERIES FOR BATTERY PACK OF EMERGENCY EXIT LIGHT OF RT EMERGENCY EXIT IAW 35-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999100100540 19991001 00540 WP 1999 10 1 ORJA99247 1 19990723 A 3350 BR9661115 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 9-12 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY LIGHTS RT SIDE ROW 9, 10, 11, 12 CAME ON. REMOVED AND REPLACED BATTERY PACK IN EMERGENCY ROW 20, OPS CHECK GO OD AT THIS TIME PER MM 33-00-00. (M) 2 L 7 2 4F RT A6WE 1999100100541 19991001 00541 CE 1999 10 1 MASA99152 1 19990830 A 3233 1143800419 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG INTERNAL LEAK A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 132YV UE132 FLT 6461 - FMN-PHX - AFTER DEPARTURE, THE CREW REPORTED THE MAIN LANDING GEAR CIRCUIT BREAKER POPPED. THE CREW RESET TH E CIRCUIT BREAKER AND IT POPPED AGAIN. THE CREW MANUALLY EXTENDED THE GEAR. THE AIRCRAFT RETURNED TO THE FIELD AND LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR. OPS CHECKED GOOD, THE AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999100100542 19991001 00542 CE 1999 10 1 MASA99149 1 19990824 A 5210 10151404715 LOCK BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR DIRTY A MASA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 5YV UE5 FLT 5972 - PIT-DUJ - PRIOR TO DEPARTURE, THE CREW REPORTED THE CABIN DOOR ANNUNCIATOR LIGHT EXTINGUISHED PRIOR TO LOCKIN G THE DOOR. MAINTENANCE CLEANED AND LUBED THE SHAFT DOOR LOCK, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A24CE 1999100100543 19991001 00543 NE 1999 10 1 MASA99153 2 19990901 A 7322 324485316 MFC DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE LT ENGINE FAILED A MASA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 448YV 448 FLT 6217 - PHX-FLG - ON PREPARATION FOR TAKEOFF, THE CREW APPLIED TAKEOFF POWER. THE LEFT ENGINE ONLY MADE 40 PERCENT P OWER. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE MFC. OPS CHECKED GOOD AND THE A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1999100100544 19991001 00544 EA 1999 10 1 MASA99140 1 19990816 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG FAILED A MASA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 37178 7178 FLT 6003 - PHX-DSM - ON SHORT FINAL INTO DSM, THE CREW RECEIVED A NOSE GEAR FAIL INDICATION UPON GEAR EXTENSION. THE CR EW RECYCLED THE GEAR AND RECEIVED GEAR DOWN AND LOCKED INDICATION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE A IRCRAFT WAS FERRIED TO PHX WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE PRIORITY VALVE. OPS CHECK GOOD. THE AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999100100545 19991001 00545 EA 1999 10 1 MASA99142 1 19990818 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17175 7175 FLT 5808 - PHL-STL - AFTER DEPARTURE FROM PHL, THE CREW REPORTED THE NOSE GEAR DOOR WOULD NOT CLOSE ON RETRACTION. THE CREW DECLARED AN EMERGENCY RETURNED TO THE FIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED T HE NOSE PRIORITY VALVE, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999100100546 19991001 00546 EA 1999 10 1 MASA99155 1 19990902 A 3234 16040109 SELECTOR ASSY CNDAIR CL600 CL6002B19 EA LANDING GEAR FAILED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 37178 7178 FLT 6080 - PHX-MAF - UPON GEAR EXTENSION, THE CREW RECEIVED A GEAR UNSAFE INDICATION. RECYCLED THE GEAR THREE TIMES AND RECEIVED GEAR DOWN AND LOCK INDICATION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO PHX WHERE. MAINTENANCE REPLACED THE SELECTOR VALVE ASSY. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999100100547 19991001 00547 EA 1999 10 1 MASA99154 1 19990901 A 2910 601R7528623 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA LT HYD SYSTEM CHAFED A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 27191 7191 FLT 5829 - SWF-RDU - DURING FLIGHT, THE CREW REPORTED A LOSS OF NR 2 LEFT HYDRAULIC PRESSURE. THE CREW DID NOT DECLARE AN EMERGENCY, HOWEVER, THE EMERGENCY EQUIPMENT WAS DISPATCHED BY THE TOWER. THE AIRCRAFT LANDED IN RDU WITHOUT INCIDENT . MAINTENANCE FOUND THAT A CLAMP HAD CHAFFED THE RETURN FILTER SERVICE LINE WHICH CAUSED IT TO CRACK. MAINTENANCE REPL ACED THE HYDRAULIC LINE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999100100548 19991001 00548 EA 1999 10 1 MASA99129 1 19990808 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DISCONNECTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7219 FLT 5827 - SDF-LGA - DURING PREFLIGHT WALK AROUND, THE CREW NOTICED THE AFT EMERGENCY FLOOR LIGHTING WAS INTERMITTENT. M AINTENANCE WAS DEFERRED PER MEL 33-51-1. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, A ELECTRICAL CONNECTOR WAS RESECURED AND THE SYSTEM SUCCESSFULLY TESTED. (M) 2 L 7 2 4F RT A21EA 1999100100549 19991001 00549 NM 1999 10 1 MASA99128 1 19990801 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 6393 - PHX-YUM - THE CAPTAIN REPORTED THAT EMERGENCY CABIN LIGHT INOPERATIVE. MAINTENANCE REPLACED ALL THE BATTERY PACK FOR LIGHT. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999100100550 19991001 00550 NM 1999 10 1 MASA99133 1 19990810 A 3350 1317 BULB DHAV DHC8 DHC8202 2809007 NM ROW 4 MISSING A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 FLT 6230 - PHX-MTJ - DURING PREFLIGHT ACCEPTANCE CHECK, THE CREW REPORTED THE RIGHT SIDE EMERGENCY EXIT PLACARD LENSE WA S MISSING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A13NM 1999100100551 19991001 00551 SO 1999 10 1 C2XA99IA462 1 19990829 A 5330 12017416045 SKIN EMB 120 EMB120RT SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FUSELAGE DENTED AT FRAME 44, STRINGER 11R. INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100552 19991001 00552 SO 1999 10 1 C2XA99IA461 1 19990829 A 5330 12026335005 SKIN EMB 120 EMB120RT SO BS 2364 GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND GOUGE IN FUSELAGE SKIN AT FS 2364.0 STRINGER 13L. INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100553 19991001 00553 SO 1999 10 1 C2XA99IA460 1 19990829 A 5320 12028877001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSSBEAM CORRODED AT FRAME 33. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40- 02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100554 19991001 00554 SO 1999 10 1 C2XA99IA459 1 19990829 A 5320 12006439001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSSBEAM CORRODED AT FRAME 42 BETWEEN LEFT AND CENTER BEAM. REMOVED AND REPL ACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100555 19991001 00555 SO 1999 10 1 C2XA99IA458 1 19990829 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CROSSBEAM CORRODED AT FRAME 36 BETWEEN CENTER AND RT BEAM. REMOVED AND REPLAC ED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100556 19991001 00556 SO 1999 10 1 C2XA99IA457 1 19990829 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT BUTTSTRAP CORRODED AT FRAME 38. REMOVED AND REPLACED BUTTSTRAP IAW SRM 51- 40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100557 19991001 00557 SO 1999 10 1 C2XA99IA456 1 19990829 A 5411 12003851002 FRAME EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW CONTINENTA L EXPRESS EC5410-01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100558 19991001 00558 SO 1999 10 1 C2XA99IA455 1 19990829 A 5411 12003851001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW CONTINEN TAL EXPRESS EC5410-01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100559 19991001 00559 WP 1999 10 1 ASAA9980172 1 19990812 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 962AS 53076 SEA - PRIOR TO DEPARTURE OF FLT 442, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RECONNECTED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999100100560 19991001 00560 WP 1999 10 1 ASAA9980171 1 19990811 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 975AS 53451 LAX - PRIOR TO DEPARTURE OF FLT 559, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999100100561 19991001 00561 WP 1999 10 1 ASAA9980170 1 19990810 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 958AS 53024 SEA - PRIOR TO DEPARTURE OF FLIGHT 720, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WI RING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999100100562 19991001 00562 WP 1999 10 1 ASAA9980169 1 19990804 A 3350 0105606004 LAMP DOUG DC9 DC983 3022083 WP ROW 29 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 SEA - DURING MAINTENANCE CHECK, ONE EMERGENCY FLOOR TRACK RED LIGHT AT ROW 29 WAS FOUND INOPERATIVE. REPLACED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999100100563 19991001 00563 WP 1999 10 1 ASAA9980167 1 19990801 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 947AS 53020 SEA - FLT 444 - CREW REPORTED, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRI NG IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999100100564 19991001 00564 NM 1999 10 1 ASAA9940144 1 19990826 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 PDX - DURING MAINTENANCE CHECK, FOUND THE AFT 4 EMERGENCY EXIT TRACK LIGHTS TO BE INOPERATIVE. RECONNECTED WIRING TO LI GHTS AND RELAMPED, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999100100565 19991001 00565 NM 1999 10 1 ASAA9910236 1 19990831 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS AT ROW 16 WOULD NOT EXTINGUISH. REPLACED BATTERY PACK AND LIG HTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999100100566 19991001 00566 NM 1999 10 1 ASAA9910235 1 19990826 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM ROWS 14-15 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 14 AND 15 WERE FOUND TO BE INOPERATIVE. REPLACE D BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999100100567 19991001 00567 NM 1999 10 1 ASAA9910234 1 19990820 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT NEAR THE L1 DOOR WAS FOUND TO BE FLASHING CONTINUOUSLY. REPLAC ED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999100100568 19991001 00568 WP 1999 10 1 ASAA9980178 1 19990822 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO BE VERY HARD TO CLOSE AND LATCH FROM THE OUTSIDE. LUBRICATED A ND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999100100570 19991001 00570 NM 1999 10 1 TSAA9933423 1 19990908 A 3350 9221009 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED AFT ENTRY IDENTIFIER LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999100100571 19991001 00571 NM 1999 10 1 TSAA9933422 1 19990908 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 1, 2, 3, 4, 5, AND 6 FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1999100100572 19991001 00572 NM 1999 10 1 TSAA9933421 1 19990907 A 3350 8731002511 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999100100573 19991001 00573 NM 1999 10 1 TSAA9933431 1 19990910 A 3350 9221009 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED RIGHT OVERWING EXIT IDENTIFIER LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999100100574 19991001 00574 NM 1999 10 1 TSAA9933432 1 19990910 A 3350 8731001511 LIGHT BOEING 737 737209 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 5 FLOOR EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999100100575 19991001 00575 NM 1999 10 1 TSAA9933433 1 19990912 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999100100576 19991001 00576 NM 1999 10 1 TSAA9933426 1 19990910 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 4 AND NR 5 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999100100577 19991001 00577 NM 1999 10 1 TSAA9933427 1 19990912 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999100100578 19991001 00578 NM 1999 10 1 TSAA9933429 1 19990911 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999100100580 19991001 00580 SO 1999 10 1 ASOA99093 1 19990906 A 2130 32144143 SHUTOFF VALVE EMB 120 EMB120RT SO FUSELAGE INOPERATIVE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 239AS 120057 AFTER ENGINE START AND PACK BROUGHT ON LINE, CABIN AND COCKPIT RAPIDLY FILLED WITH SMOKE. THE CAPTAIN SHUT AIRCRAFT DOW N AND DEPLANED NORMALLY AT THE GATE. ATLANTA MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING SHUT OFF VALVE. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100581 19991001 00581 SO 1999 10 1 ASOA99092 1 19990806 A 3350 1013073 BULB EMB 120 EMB120RT SO CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 232AS 120036 DURING INSPECTION, FOUND CABIN TRACK LIGHTING BULB INOPERATIVE. ATL MAINTENANCE REPAIRED BROKEN BULB. OPERATIONAL CHEC KS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100582 19991001 00582 SO 1999 10 1 ASOA99091 1 19990904 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 258AS 120131 DURING INSPECTION, NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100583 19991001 00583 SO 1999 10 1 ASOA99090 1 19990904 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 246AS 120100 DURING INSPECTION, NR 3 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100584 19991001 00584 SO 1999 10 1 ASOA99089 1 19990903 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 243AS 120072 DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100585 19991001 00585 EA 1999 10 1 ASOA99088 1 19990902 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 EA FUSELAGE FAILED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 827AS 7212 FLT 4623 - UPON TAXI OUT, THE TOILET SMOKE EICAS MESSAGE ILLUMINATED. THE AIRCRAFT WAS STOPPED AND THE FLGIHT ATTENDANT WAS INSTRUCTED TO INSPECT THE LAVATORY WHILE THE COCKPIT CREW EXECUTED THE APPROPRIATE CHECKLIST. THE CREW WAS INFORME D THAT THERE WAS SMOKE IN THE CABIN AND IT WAS MOVING FORWARD. CAPTAIN OPENED THE COCKPIT DOOR AND VISUALLY SAW THICK S MOKE IN CABIN, EVACUATED THE PASSENGERS, REQUESTED FIRE FIGHTING EQUIPMENT, AND SHUTDOWN THE AIRCRAFT. MAINTENANCE FOUN D NO OIL INTHE ACM. REMOVED AND REPLACED THE ACM. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A21EA 1999100100586 19991001 00586 SO 1999 10 1 ASOA99087 1 19990901 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 245AS 120075 DURING INSPECTION, NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100587 19991001 00587 SO 1999 10 1 ASOA99086 1 19990901 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 245AS 120075 DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999100100588 19991001 00588 EA 1999 10 1 ASOA99085 1 19990901 A 3350 363782 BULB CNDAIR CL600 CL6002B19 EA ROW 1AB FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 824AS 7203 DURING INSPECTION, EMERGENCY FLOOR BULB AT 1AB FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING SYSTEM BULB. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999100100589 19991001 00589 EA 1999 10 1 ASOA99084 1 19990831 A 3350 363782 BULB CNDAIR CL600 CL6002B19 EA ROW 2AB FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 832AS 7243 DURING INSPECTION, EMERGENCY FLOOR BULB AT 2AB FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING SYSTEM BULB. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999100100590 19991001 00590 NM 1999 10 1 99ZZZM689 1 19990827 A 8012 97910231 START VALVE BOEING 737 737291 138448W NM NR 2 ENGINE FAILED A USVA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 11 7375F 20363 NR 2 ENGINE START VALVE LGHT CAME O NDURING CLIMB FOLLOWED BY NR 2 FIRE WARNING INDICATION. REDUCED POWER LIGHT OFF. S HUT ENGINE DOWN AND RETURNED TO ACY. T/S SYSTEM FOUND START VALVE STUCK OPEN AND DAMAGE TO, STARTER, CSD INLINE FILTER HOUSING. REMOVED AND REPLACED NR 2 ENGINE STARTER AND START VALVE IAW MM 80-11-21. REMOVED AND REPLACED CSD INLINE FIL TER ASSEMBLY AND SERVICED CSD IAW 24-11-31. RUN UP OPS AND LEAK CHECKED. (M) 2 L 7 2 4F A16WE 1999100100591 19991001 00591 NM 1999 10 1 USAASB99220 1 19990905 A 3260 806002 PRINTED CIRCUIT BOEING 737 737401 1384701 NM LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 420US 23987 PHL - FLT 973 - FLIGHT RETURNED TO FIELD AT PHL DUE TO A LEFT MAIN LANDING GEAR UNSAFE LIGHT INDICATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE 'LEFT GEAR UP AND LOCK SWITC H' PRINTED CIRCUIT CARD M988 PER THE MM. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999100100592 19991001 00592 NM 1999 10 1 USAASB99219 1 19990904 A 4960 38762594 SWITCH BOEING 737 7374B7 1384702 NM APU FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 776AU 1099 24934 MCO - FLT 538 - FLT DEPARTED MIA WITH THE NR 2 GENERATOR ON MEL. AT FL290, THE APU INITIATED AN AUTO SHUTDOWN DUE TO AN OVERSPEED CONDITION. SINCE AIRCRAFT WAS DOWN TO A SINGLE ELECTRICAL SOURCE, THE CAPT DECLARED AN EMERGENCY AND DIVERTE D TO MCO. FLT LANDED W/O FURTHER INCIDENT. MX REMOVED AND REPLACED THE APU FUEL CONTROL (P/N 3608000-4) IN ASSOCIATION WITH MM 49-31-11. GROUND RUN CHECKED NORMAL. SUBSEQUENTLY, FLT 8052 DEPARTED MCO AND DURING CRUISE, THE APU FREQUENCI ES DRIFTED UPWARDS UNTIL AUTO SHUTDOWN OF THE APU GENERATOR OCCURRED. FLIGHT DIVERTED TO JAX THIS TIME AND LANDED WITHO UT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU ELECTRONIC THREE-SPEED SWITCH PER MM. RAN APU. OPERATIO 2 L 7 2 4F RT A16WE 1999100100593 19991001 00593 NM 1999 10 1 USAABB99040 1 19990829 A 3350 20121 BATTERY CHARGER BOEING 757 757225 1384959 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 BWI - FOUND EMERGENCY LIGHTS INOPERATIVE AT DOOR R1 (SIGN, SLIDE LIGHT AND PATH LIGHT). MAINTENANCE REPLACED THE BATTER Y PACK AND CHARGER. (M) 2 L 7 2 4F RT A2NM 1999100100594 19991001 00594 NM 1999 10 1 USAABB99039 1 19990811 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM ROW 13 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 PVD - FOUND SEAT MOUNTED EMERGENCY FLOOR LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1999100100595 19991001 00595 NM 1999 10 1 USAABB99038 1 19990813 A 3397 WIRE BOEING 767 7672B7 1385107 NM ROW 1-6 CHAFED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 CDG - FOUND RIGHT SIDE EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 1 THROUGH ROW 6. MAINTENANCE FOUND AND REPAIRED A BA RE WIRE WITHIN THE SIDE WALL. (M) 2 L 7 2 4F RT A1NM 1999100100596 19991001 00596 SO 1999 10 1 SIMA992354 1 19990823 A 3610 CAR5001574 COUPLING EMB 145 EMB145LR SO CARGO BAY LOOSE A SIMA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 21 628AE 145124 IND - FLT 4188 - BLEED LEAK INDICATED ON EICAS. BAGGAGE SMOKE WARNING CAME ON AFTER THAT. DISCHARGED BOTH FIRE EXTINGU ISHERS. FOUND LOOSE BLEED COUPLING IN THE CARGO BAY FOR THE NR 2 BLEED SYSTEM. REMOVED AND REPLACED COUPLING SEALS AND SECURED DUCT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999100100597 19991001 00597 SO 1999 10 1 99ZZZM690 1 19990823 A 3610 S2D226 O-RING EMB 145 EMB145LR SO CARGO BAY WORN A SIMA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 21 628AE 145124 IND - FLT 4188 - BLEED LEAK INDICATED ON EICAS. BAGGAGE SMOKE WARNING CAME ON AFTER THAT. DISCHARGED BOTH FIRE EXTINGU ISHERS. FOUND LOOSE BLEED COUPLING IN THE CARGO BAY FOR THE NR 2 BLEED SYSTEM. REMOVED AND REPLACED COUPLING SEALS AND SECURED DUCT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999100100598 19991001 00598 SO 1999 10 1 SIMA992311 1 19990919 A 3610 S2D226 SEALS EMB 145 EMB145 SO CARGO BAY FAILED A SIMA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 21 611AE 145074 GRR - FLT 4286 - BLEED LEAK INDICATED ON EICAS. BAGGAGE SMOKE WARNING ALSO CAME ON DURING FLIGHT. DISCHARGED FIRE EXTI NGUISHER. REMOVED AND REPLACED BLEED SEALS AT COUPLING IN CARGO BAY FOR NR 1 BLEED SYSTEM. AIRCRAFT FERRIED TO ORD FOR FIRE EXTINGUISHER REPLACEMENT AND FURTHER TROUBLESHOOTING AND THEN RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100100599 19991001 00599 SO 1999 10 1 SIMA992372 1 19990825 A 3240 156221 PRESSURE SWITCH EMB 145 EMB145LR SO LT MLG BRAKE FAILED A SIMA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 603AE 0315 145055 ORD - FLT 4390 - NR 2 HYDRAULIC SYSTEM FAILED, HAD HIGH TEMP AND LOW QTY WARNING ON EICAS. DECLARED EMERGENCY, LANDED S AFELY. REMOVED AND REPLACED NR 2 SYSTEM EMERGENCY BRAKE PRESSURE SWITCH. RESERVICED SYSTEM, PERFORMED LEAK AND OPERATI ONAL CHECK AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999100100600 19991001 00600 EU 1999 10 1 SIMA992471 1 19990904 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 346SB 18187 340B346 DFW - SOME CABIN EMERGENCY LIGHTS DID NOT ILLUMINATED. REMOVED AND REPLACED ONE EMERGENCY LIGHT BATTERY POWER SUPPLY. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999100100601 19991001 00601 EU 1999 10 1 SIMA992521 1 19990909 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU ROW 7A INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 283AE 19023 340B283 DFW - FLT 5324 - EMERGENCY EXIT LIGHT AT ROW 7A DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY. OPER ATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999100100602 19991001 00602 EU 1999 10 1 SIMA992512 1 19990908 A 5320 S5367121737400 SILL AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK IAW SRM 51-25-01 AND 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100603 19991001 00603 EU 1999 10 1 99ZZZM691 1 19990908 A 5320 S5367121729801 DRAIN TRACK AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK IAW SRM 51-25-01 AND 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100604 19991001 00604 EU 1999 10 1 SIMA992513 1 19990908 A 5320 S53678008201 SUPPORT AEROSP ATR72 ATR72212 EU FRAME 38-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT FLOOR SUPPORT CHANNEL BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REP LACED THE CHANNEL IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100605 19991001 00605 EU 1999 10 1 SIMA992514 1 19990908 A 5315 S5367240620801 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAM 36 HAD AN EXTRA HOLE DRILLED INTO IT. REPAIRED THE FLOORBEAM IAW SRM 53 -00-00 FIGURE 435. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100606 19991001 00606 EU 1999 10 1 SIMA992515 1 19990908 A 5320 S536780082002 ZEE AEROSP ATR72 ATR72212 EU FRAME 39-40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED T HE ZEE MEMBER IAW 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100607 19991001 00607 EU 1999 10 1 SIMA992511 1 19990908 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE R IGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100608 19991001 00608 EU 1999 10 1 99ZZZM692 1 19990908 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE R IGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100609 19991001 00609 EU 1999 10 1 99ZZZM693 1 19990908 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE R IGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100610 19991001 00610 EU 1999 10 1 99ZZZM694 1 19990908 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE R IGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100100611 19991001 00611 EU 1999 10 1 REXA99025 1 19990730 A 5320 7239201055 BRACKET SAAB SF340 SF340A 7850100 EU AVIONICS RACK CORRODED A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 344AM 340A030 LOWER AFT AVIONICS RACK 'L' BRACKET CORRODED. REMOVED CORRODED BRACKET, AND REPLACED WITH A NEW BRACKET. (M) 2 L 7 2 4T RT A52EU 1999100100621 19991001 00621 WP 1999 10 1 99ZZZX3718 2 19990624 A 7230 BLADE MTSBSI MU2 MU2B26A 5780414 CE GARRTT TPE331 TPE3315 01514 WP IMPELLER FAILED A DKKA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 09 333WF 387 P33064 EN ROUTE FROM SAD TO GKY, THE PIC FEATHERED THE RIGHT ENGINE DUE TO FLUCTUATING OIL PRESSURE AND DIVERTED TO ABI. THE R T ENGINE, TPE33155252M, SN P-33064 WITH 1,847.4 HOURS SINCE OVERHAUL. COMPRESSOR IMPELLER P/N 3107110-2, SN 6-03160-281 WITH 1,513.4 HOURS SINCE OVERHAUL. THE FIRST STAGE IMPELLER HAD A BROKEN BLADE. CAUSE OF BLADE FAILURE IS UNKNOWN AT THIS TIME. ENGINE IS CURRENTLY BEING REPAIRED AND THE EFFECTED IMPELLER HAS BEEN SEN FOR EVALUATION. 1 H 7 2 3T 4 T RT A10SW E4WE 1999100100643 19991001 00643 NE 1999 10 1 9904046730 2 19990926 A 7321 FUEL CONTROL BOEING 747 7472J9F 1384806 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE MALFUNCTIONED A NWAA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 GL 01 630US 21668 689632 AT 4,000 FEET ON FINAL APPROACH (KIX), THE NR 4 ENGINE FLAMED OUT. A SINGLE RESTART WAS ATTEMPTED AND ABORTED DUE TO HI GH EGT. THE LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE EXHAUST AND INTAKE WITH NO DEFECT S NOTED. THE FUEL CONTROL AND TT2 SENSOR WERE REPLACED. SUBSEQUENT ENGINE OPERATIONAL RUN WAS NORMAL. 2 L 7 4 4F 4 F RT A20WE E20EA 1999100100644 19991001 00644 NE 1999 10 1 9904056730 2 19990925 A 7200 ENGINE BOEING 747 7472J9F 1384806 NM PWA JT9 JT9D7J 52054 NE NR 4 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 GL 01 630US 21668 689632 AT 4,500 FEET ON APPROACH, THE NR 4 ENGINE FLAMED OUT WHILE AT IDLE POWER. THE ENGINE WAS RESTARTED AND OPERATED NORMAL LY FOR THE REMAINDER OF THE FLIGHT INCLUDING REVERSE AND TAXI OPERATION. MAINTENANCE INSPECTED THE ENGINE INCLUDING CHI P DETECTORS AND FUEL FILTER WITH NO DISCREPANCIES NOTED. THE FUEL TANKS WERE SUMPED AND THE FUEL FILTER WAS REPLACED. A N ENGINE OPERATIONAL TEST WAS PERFORMED WITH ALL INDICATIONS NORMAL. 2 L 7 4 4F 4 F RT A20WE E20EA 1999100100645 19991001 00645 NM 1999 10 1 9904066638 1 19990924 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 638US 23549 DURING LINE CHECK, FOUND ZONE E FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECHARGED THE BATTERY PACKS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999100100646 19991001 00646 1999 10 1 9904073236 4 19990914 A 2565 C37103101 CABLE AIRBUS 320 A320212 3930322 EU SLIDE PACK BROKEN A NWAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 01 336NW 21845 4825 355 UPON ARRIVAL AT THE GATE, THE LEFT REAR CABIN DOOR WAS OPENED WITH THE SLIDE ARMED BUT SLIDE DID NOT DEPLOY. MAINTENANC E REPLACED THE SLIDE PACK ASSEMBLY DUE TO A BROKEN SLIDE PACK RELEASE CABLE. 2 L 7 2 4F RT A28NM 1999100100647 19991001 00647 NM 1999 10 1 UPS99230731 1 19990917 A 5320 FITTING BOEING 727 72731C 1384011 NM BS 940 MISDRILLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, ON REMOVAL OF BS 940 LT FITTING 2 FASTENER HOLES THROUGH S18A AND FUSELAGE SKIN FOUND TO HAVE BEEN OV ERSIZED AND OUT OF ED (AFT UPPER AT TACH BOLTS OF 940). INVESTIGATED AND REPAIR CARRIED OUT IAW SMRO EO 99-30-001 UPS E NGINEERING FILE NR 727-53-2170. 2 L 7 3 4F A3WE 1999100100648 19991001 00648 NM 1999 10 1 UPS99230732 1 19990915 A 5320 ANGLE BOEING 727 72731C 1384011 NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, SEPARATION DETECTED ON BS 950 FITTING BY NDT INSPECTION BETWEEN S 9 & S10 DOWNWARD. SPLICE ANGLE FOU ND CORRODED NEW ANGLE FABRICATED IAW SRM 51-20-1. 2 L 7 3 4F A3WE 1999100100649 19991001 00649 NM 1999 10 1 UPS99230749 1 19990917 A 5520 T-EDGE BOEING 727 72731C 1384011 NM RT ELEVATOR LIGHTNING STRIKE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, LIGHTNING DISCHARGE DAMAGE RT ELEVATOR TIP T-EDGE AT BASE LWR SURFACE & STRUCTURE AT PREVIOUS REPAIR. REPAIR CARRIED OUT IAW SRM 55-20-3 FIG 3. 2 L 7 3 4F A3WE 1999100100650 19991001 00650 NM 1999 10 1 UPS99230750 1 19990923 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, BS 930 FRAME CRACK ON HORIZONTAL LEG OF FRAME AT FLOOR LEVEL. REPAIR TO FRAME CARRIED OUT IAW SMRO E O 99-30-003 UPS ENGINEERING FILE NR 727-53-2174. 2 L 7 3 4F A3WE 1999100100651 19991001 00651 NM 1999 10 1 UPS99230751 1 19990916 A 5753 SKIN BOEING 727 72731C 1384011 NM RT TE FOREFLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, DENT ON UPPER SURFACE OF RT O/B FORE FLAP UPPER SURFACE MID SPAN. REPAIRED IAW SRM 51-40-6 FIG 35. 2 L 7 3 4F A3WE 1999100100652 19991001 00652 NM 1999 10 1 UPS99230752 1 19990915 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 783.95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE:C, DURING INSPECTION OF 783.95 L FRAME FOR CRACKS. CRACK FOUND EMINATING FROM SECOND FASTENER HOLE BELO W FLOOR. FRAME BS 783.95 LT REPAIRED IAW APPENDIX C OF EO B727-5310-5474- C AND SMRO EO 99-30-002 UPS ENGINEERING FILE NR 5310-2172. 2 L 7 3 4F A3WE 1999100100653 19991001 00653 NM 1999 10 1 UPS99230753 1 19990922 A 5711 SPAR BOEING 727 7271A7C 13840X2 NM WS 525 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, CORROSION (C57-562-02.00E-01) AT LT WING STA 525 UPPER SPAR CHORD. REMOVED AND REPLACED SPAR (UPPER CHORD) IAW BFG ER 99-5890 (UPS FILE NR 727-57-2118). 2 L 7 3 4F A3WE 1999100100654 19991001 00654 NM 1999 10 1 UPS99230754 1 19990730 A 5754 65162276 MOUNTING LUG BOEING 727 7271A7C 13840X2 NM NR 6 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, (CORROSION C57-562-01.00-02) CORROSION ON NR 6 K-FLAP INBOARD MOUNT LUG UPPER BOLT. REMOVED NR 6 K-F LAP PER MM 27-81-01. NR 6 K-FLAP CORROSION OUT OF LIMITS PER SRM ADDENDUM EO B727-5750-5542. REPLACED K-FLAP PER MM 27 -81-01. 2 L 7 3 4F A3WE 1999100100655 19991001 00655 NM 1999 10 1 UPS99230755 1 19990729 A 5720 M890305 BRACKET BOEING 727 7271A7C 13840X2 NM RT WING SPAR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, ANGLE BRACKET CORRODED ON R/W UPPER AFT SPAR CHORD AT NR 14 SPOILER I/B SIDE HINGE. REMOVED SPOILER I/B ANGLE SUPPORT BRACKET. FABRICATED NEW SUPPORT ANGLE PER SRM 51-20-1 AND 51-30-05. INSTALLED NEW BRACKET PER SRM 51- 30-02. LEAK CHECKED FUEL TANK AND FUNCTIONAL TESTED NR 14 SPOILER PER MM 27-61-00. 2 L 7 3 4F A3WE 1999100100656 19991001 00656 WP 1999 10 1 UPS99830734 1 19990923 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, CRACKED FITTING STA 640 LONG 36. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100657 19991001 00657 WP 1999 10 1 UPS99830735 1 19990921 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, HARDWARE CORRODED AT STA 580 AT CUSP AREA RT SIDE FORWARD CARGO PIT. SEAT TRACK AT FS 590 IS OUT OF LIMITS. REMOVED DAMAGED SECTION IAW DC8 SRM 51-3-0, MAT ID S2772660 IAW DC8-53B-003, PO NR 293505. MANUFACTURED SEAT T RACK AND SEAT TRACK SPLICE IAW DC8 5313-003. INSTALLED SEAT TRACK AND AIR GRILL IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999100100658 19991001 00658 WP 1999 10 1 UPS99830736 1 19990908 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, STA 600 LONGERON 34R CRACKED 6 INCHES LONG, DOT F-758. FABRICATED LONGERON SECTION IAW REO 06771 FR OM MACH SHOP, REC'D FABBED REPAIR SPLICE AND DRILLED UP NEW LONGERON, SPLICE AND STRAPS IAW DC8 S RM 51-1-2 AND REO 0677 1. INSTALLED REPAIR SPLICE AND STRAPS IAW DC8 SRM 51-1-20D. REINSTALLED FACTORY SPLICE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100659 19991001 00659 WP 1999 10 1 UPS99830737 1 19990907 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 150 MISDRILLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:.C1, RT FUSELAGE, EXTERNAL SKIN HAD 3 EXTRA HOLES IN SKIN JUST UNDER RT SERVICE DOOR FS 150 DOT E618. R EMOVED DAMAGE, FABBED TITANIUM DOUBLER, REPAIR DOUBLER, TRIPLER, LONGERON AND FILLERS IAW REO 06755. DRILLED NEW CUSP F ITTING IAW DC8 SRM 51-1-24. INSTALLED TITANIUM DOUBLER, REPAIR DOUBLER, TRIPLER, LONGERON FILLERS, CUSP FITTING AND BUS HING IAW DC8 SRM 51-1-20D, 51-1-25 & REO 06755. 2 L 7 4 4F RT 4A25 1999100100660 19991001 00660 WP 1999 10 1 UPS99830738 1 19990907 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 50-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, FLOOR STRUCTURE INTERCOSTAL UPPER FLANGE WAS CORRODED ON LOWER SIDE, STA 50-55, X=-50. REMOVED DAMA GED AREA IAW 53-2-0. FABBED AND INSTALLED ANGLES AND FITTINGS IAW REO 06768. 2 L 7 4 4F RT 4A25 1999100100661 19991001 00661 WP 1999 10 1 UPS99830739 1 19990907 A 5312 BLKHD STIFFENER DOUG DC8 DC873F 302199F WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, VERTICAL STIFFENER FWD FLANGE WAS CORRODED, AFT SIDE OF STA 8 BULKHEA D AT L28R. FABRICATED STIFFEN ER END REPAIR ANGLES IAW TIMCO REO 06773, HEAT TREAT PERFORMED IAW TPS-1003 REV A O CONDITION TO T6. DRILLED UP IAW DC 8 SRM 51-1-24 & TIMCO REO-06773. INSTALLED STIFFENER END REPAIR ANGLES IAW TIMCO REO-06773. 2 L 7 4 4F RT 4A25 1999100100662 19991001 00662 WP 1999 10 1 UPS99830740 1 19990906 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 L24L AT STA 879 HAD CORROSION FWD AND AFT. REMOVED CORROSION FOUND FITTING OUT OF LIMITS. FABRICATE D NEW FITTING AND REPAIR PARTS IAW DC8 SRM 57-2-1 FIG 3B & RFTS NR N836UP-36-20407. INSTALLED FITTING AND REPAIR PARTS IAW DC8 SRM 51-1-20D & 51-3-0. 2 L 7 4 4F RT 4A25 1999100100663 19991001 00663 WP 1999 10 1 UPS99830741 1 19990905 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 160 DOUBLE DRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, MISDRILLED HOLE FS 160 FWD LOWER CORNER OF TORQUE BOX AND FWD PART O F FWD RT SERVICE DOOR, DOTS E76 1, E764, E768. FABBED WEB AND REPAIR ANGLE IAW DAC DWG 561570D & FDC8 SRM 53-2-0 FIG 1B. HEAT TREATED ANGLE IAW TPS 10 03 REV A. INSTALLED REPAIR ANGLE TO CORNER PAN IAW DC8 SRM 51-1-20D. WEB AND CORNER PAN TO BE INSTALLED ON AIRCRAFT ON UPS NR 001817. 2 L 7 4 4F RT 4A25 1999100100664 19991001 00664 WP 1999 10 1 UPS99830742 1 19990905 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 160 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, STA 160 SEAT TRACK F SCALLOPS GOUGED IN TRACK OUT OF LIMITS. REMOVED DAMAGED TRACK, FABBED AND INST ALLED REPLACEMENT SECTION IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999100100665 19991001 00665 WP 1999 10 1 UPS99830743 1 19990905 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, MAIN CABIN STA 1480 L3R TO L4R FRAME FWD FACE CORRODED. REMOVED CORROSION, FRAME FOUND TO BE OUT OF LIMITS. FABBED SPLICES IAW DC8 SRM 53-2-0, HEAT TREAT FOR T-6 CONDITION. GEN AND REC'D RFTS NR 836UP-24-20191 W/REO 0 6760, MAT ID S2537716-1400 7075-0 EXT PO NR 28567 8. LOCATED, REAMED, INSTALLED FRAME SEGMENTS AND SPLICES IAW DC8 SRM 51-1-24, 51-1-20D AND REO 06760. 2 L 7 4 4F RT 4A25 1999100100666 19991001 00666 WP 1999 10 1 UPS99830744 1 19990905 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1580 DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, STA 1580 LONG, L19L TO L14L HAD DRILL DAMAGE. CLEANED UP DAMAGED AREA AND REPAIRED FRAME IAW TIMCO DWG DC8 53-0229, REO 06737 AND UPS COVER SHEET DC8 53-2711. 2 L 7 4 4F RT 4A25 1999100100667 19991001 00667 WP 1999 10 1 UPS99830745 1 19990924 A 5320 WEB DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, CRACK 2.5 INCHES LONG STOP DRILL LOCATED BY RT MLG DOOR SWITCH. PERM REPAIRS AT NEXT C CHECK. FABR ICATED AND INSTALLED NEW WEB AND ANGLE IAW DC8 SRM 51-3-0 & 51-1-21L. TERMINATED AND SECURED WIRING TO GEAR SWITCH AND INTERPHONE JACK. OPS CHECKED SWITCH IAW DC8 MM 32-60-0. 2 L 7 4 4F RT 4A25 1999100100668 19991001 00668 WP 1999 10 1 UPS99830746 1 19990913 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1720-1740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, RT FUSELAGE EXTERIOR SKIN SHOWS SIGNS OF BULGING AND PULLED RIVETS BETWEEN FS 1720-1740 AT L28R-L30R . REMOVED CORRODED SECTION OF SKIN. FABRICATED REPAIR DOUBLER, FINGER DOUBLER AND FILLER IAW DC8 SRM 53-2-1, FIG 7, 5 1-1-8 & 51-1-21. 2 L 7 4 4F RT 4A25 1999100100669 19991001 00669 WP 1999 10 1 UPS99830747 1 19990906 A 5240 SKIN DOUG DC8 DC873F 302199F WP LT SERVICE DOOR DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, LT AFT SERVICE DOOR INNER LOWER STRUCTURE HAD A DOUBLE DRILLED HOLE. DOUBLE DRILLED HOLE WENT THROU GH EXISTING REPAIR. REMOVED EXISTING REPAIR DOUBLER AND EXTEND NEW DOUBLER PAST DOUBLE DRILLED HOLES. EXISTING INNER S KIN REPAIR DID NOT MEET SRM REQUIREMENTS. FABBED REPAIR DOUBLER ON INNER SKIN AND INSTALLED WITH RIVETS IAW DC8 SRM 51- 1-21, 52 -2-0, 52-3-1, 51-9-0 & 52-2-2. 2 L 7 4 4F RT 4A25 1999100100670 19991001 00670 WP 1999 10 1 UPS99830748 1 19990928 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 1999100100671 19991001 00671 WP 1999 10 1 UPS99830756 1 19990928 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:N/A, EMERGENCY LIGHTS DID NOT OPERATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY PER M/M 33-50-01, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999100100672 19991001 00672 WP 1999 10 1 UPS99830757 1 19990927 A 3350 LIGHT DOUG DC8 DC871F 302199D WP CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:N/A, EMERGENCY LIGHTS WILL NOT DISARM. PERFORMED EMERGENCY LIGHT OPERATIONAL TEST IAW MM REF 33-50-01 P AGE 201, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999100100673 19991001 00673 WP 1999 10 1 UPS99830758 1 19990908 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1320-1340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C1, STA 1320-1340, THE RT CUSP UPPER SURFACE HAS HEAVY CORROSION. REPAIRED AREA BY SPLICING NEW SECTION OF CUSP FITTING IAW SRM 53- 2-5 FIG 15A (STA 1290 TO 1380). 2 L 7 4 4F RT 4A25 1999100100674 19991001 00674 WP 1999 10 1 UPS99830759 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 448.501 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 448.501 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100675 19991001 00675 WP 1999 10 1 UPS99830760 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 722.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 722.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRE D IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100676 19991001 00676 WP 1999 10 1 UPS99830761 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 753.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 753.750 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100677 19991001 00677 WP 1999 10 1 UPS99830762 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 810 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100678 19991001 00678 WP 1999 10 1 UPS99830763 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XOLDI6.225 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRE D IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100679 19991001 00679 WP 1999 10 1 UPS99830764 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 476.897 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 476.897 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100680 19991001 00680 WP 1999 10 1 UPS99830765 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 816.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 816.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRE D IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100681 19991001 00681 WP 1999 10 1 UPS99830766 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB ATV STA XFS 772.50 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100682 19991001 00682 WP 1999 10 1 UPS99830767 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 442.185 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRE D IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100683 19991001 00683 WP 1999 10 1 UPS99830768 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 435.789 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100684 19991001 00684 WP 1999 10 1 UPS99830769 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 841.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 841.250 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100100685 19991001 00685 WP 1999 10 1 UPS99830770 1 19990912 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 257.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E UPPER SKIN AT STA XWS 257.5 IS CRACKED AT 6 HOLES AT L/E. REPAIRED AREA IAW SRM 57-2- 1 FIG 2H. 2 L 7 4 4F RT 4A25 1999100100686 19991001 00686 WP 1999 10 1 UPS99830771 1 19990915 A 5720 97532977 ANGLE DOUG DC8 DC871F 302199D WP WS 520.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING LEADING EDGE I/B SIDE OF THE XS520.168 RIB, THE SLOT AFT BULKHEAD VERTICAL ANGLE IS CRACKE D AT THE LWR END. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100687 19991001 00687 WP 1999 10 1 UPS99830772 1 19990915 A 5720 576958929 DOUBLER DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT STA XFS 304.0 IS CRACKED FWD OF THE DOUBLER T/E. REMOVED, FABRICA TED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100100688 19991001 00688 WP 1999 10 1 UPS99830773 1 19990905 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 781 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1, STA 781 SEAT TRACK G GOUGED. BLENDED SCALLOPS AT DAMAGED AREA PER DC8 SRM 51-1-8. FOUND OUT OF LIM ITS. CUT DAMAGED AREA AT G SEAT TRACK FROM STA 770 TO 810 PER UPS SRM ADDENDUM DC8-5320-8309. REPLACED DAMAGED SEAT TR ACK IAW UPS DC8 SRM ADDENDUM DC8-5320-8309. 2 L 7 4 4F RT 4A25 1999100100689 19991001 00689 1999 10 1 QXEA9902005 2 19990927 A 7321 324485317 FUEL CONTROL DHAV DHC8 DHC8202 2809007 NM ENGINE MALFUNCTION A QXEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NM 09 362PH 518 SEA - AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL. TAKEOFF ABORTED. REMOVED AND REPLACED AUTO FEATHER ARM CONTROL RELAY 6121-K5. FAILED TO ARM ON TAXI CHECK. FERRIED TO PORTLAND FOR REPAIRS. REMOVED AND REPLACED BOTH MANUEL FUEL CONTROL . OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999100100690 19991001 00690 NM 1999 10 1 99FDEA00401 1 19990929 A 5530 FITTING DOUG MD11 MD11 3023602 NM EMPENNAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 607FE 48547 SNRM 712, 719, 720, NR 4 BANJO FITTING CRACK AT RT - 712, 719, 720. REPAIR PER SRM 55-20-00 712, UPPER HOLE OVERSIZE NO CRACK FOUND 719, MID HOLE OVERSIZE NO CRACK FND 720. 2 L 7 3 4F RT A22WE 1999100100691 19991001 00691 WP 1999 10 1 99UAL900449 1 19990826 A 7830 9130M36P240 CLAMP DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE BROKEN A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 1858U 46987 AFTER T/O DURING CLIMBOUT, FIRE WARNING NR 1 ENGINE. SHUTDOWN PER SOP, DUMPED FUEL, RETURNED TO SFO. *S/D* FOUND FAIL ED V-CLAMP (P/N 9130M36P240) ON REVERSER DRIVE SUPPLY DUCT (P/N 9057M85G02). ALSO, DUCT WAS DAMAGED. DUCT AND CLAMP WE RE REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1999100100692 19991001 00692 NM 1999 10 1 99UAL900475 1 19990913 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 387UA 24662 THE FUSELAGE SKIN AND TWO FRAMES WERE DAMAGED AFTER CONTACT WITH A SERVICE TRUCK. THE SKIN WAS DAMAGED FROM STATIONS 86 6 TO 904 BETWEEN STRINGERS 26 AND 27 LT AND FROM STATIONS 865 TO 867 BETWEEN STRINGERS 24 AND 25 RT WERE DAMAGED. *S/D* THE DAMAGED FRAME SECTIONS WERE REMOVED AND REPAIRED PER SRM 53-00-07 FIGURE 204. THE SKIN WAS REPAIRED AT TWO SEPARA TE LOCATIONS PER SRM 53-00-01 FIGURE 202. 2 L 7 2 4F 4 F RT A16WE E2GL 1999100100693 19991001 00693 NM 1999 10 1 99UAL900484 1 19990919 A 3211 6546108X BEAM BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RT MLG FRACTURED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 986UA 21748 DURING ROUTINE GEAR SWINGS, THE RIGHT MAIN GEAR WAS PINNED WHEN THE RIGHT MAIN GEAR WALKING BEAM (BOEING P/N 65-46108-X) FRACTURED TWO INCHES FROM THE OUTSIDE DIAMETER OF THE SLOTTED BEARING RACE. *S/D* THE RIGHT MAIN LANDING GEAR ACTUATO R WALKING BEAM FRACTURE WAS CAUSED BY STRESS CORROSION CRACKING INDUCED BY A CORROSION PIT. REPLACED THE WALKING BEAM. 2 L 7 2 4F 4 F A16WE E2EA 1999100100694 19991001 00694 NM 1999 10 1 99UAL900485 1 19990921 A 2133 OUTFLOW VALVE HAMILTON STA 7110035 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CABIN FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 994UA 910576 22384 AT APPROXIMATELY 12K, THE CABIN PRESSURE CONTROL WENT FROM AUTO TO STANDBY. FIVE MINUTES LATER AND AT 23K, RATE OF CLIM B PRESSURE OF AIRCRAFT INCREASED TO APPROXIMATELY 1000 FEET BELOW SEA LEVEL. CABIN DIFFERENTIAL PRESSURE WAS IN YELLOW BAND BUT DID NOT EXCEED RED LINE. *S/D* MAIN OUTFLOW VALVE FAILED. REMOVED AND REPLACED MAIN OUTFLOW VALVE. 2 L 7 2 4F 4 F A16WE E2EA 1999100100695 19991001 00695 NM 1999 10 1 99UAL900486 1 19990918 A 5270 MS250111 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AIR STAIR DOOR OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 7282U 21560 AFTER DEPARTURE FROM SYRACUSE, CREW RECEIVED AN AMBER LIGHT INDICATION ON THE AFT STAIR/DOOR. RETURNED TO SYR. ADJUST ED UPLOCK SWITCH. ACTUATED AIRSTAIR SEVERAL TIMES. GROUND CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999100100696 19991001 00696 NM 1999 10 1 99UAL900487 1 19990922 A 3610 8102072 DUCT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RIGHT TORN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 776UA 14683 26937 EN ROUTE IAD-LHR, CREW RECEIVED ADVISORY MESSAGE FOR THE RIGHT WING PNEUMATIC SUPPLY INDICATING OVERHEAT CONDITION. AIR CRAFT RETURNED TO IAD. *S/D* THE RIGHT HAND PACK FAN INLET DIFFUSER HOUSING (P/N 810207-2) WAS FOUND WITH A TEAR AT TH E RUBBER ACCORDION DUCT WHICH INTERFACED WITH THE HEAT EXCHANGER RAM AIR OUTLET. RT BLEED AUTO SHUTDOWN RESULTED WHEN H OT AIR FROM THE RAM AIR EXHAUST IMPINGED ON THE ZONE 7 OVERHEAT DETECTION SYSTEM. THE FAN INLET DIFFUSER HOUSING WAS RE PLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999100100697 19991001 00697 EU 1999 10 1 99UAL900488 1 19990921 A 3350 5631188 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 408UA 457 ESCAPE PATH LIGHTS INOP AT ROW 16, 17, 18 AND ROW 22, 23, 24. REPLACED EPSU EMERGENCY POWER SUPPLY UNIT BATTERY PACK AN D POWER SUPPLY. P/N 563-1188 AND 565-2005. SYSTEM CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1999100100698 19991001 00698 WP 1999 10 1 ABXA9900725 1 19990922 A 2170 210101 COALESCER BAG DOUG DC9 DC931 3022065 WP CABIN DIRTY A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 937AX 47074 SMELL OF FUEL IN CABIN. REMOVED FLOOR PANELS OVER CENTER WING TO CHECK FOR FUEL SMELL, NONE DETECTED. RAN ENGINES AND PRESSURIZED TO 6 PSI, USED GAS DETECTOR IN COCKPIT AND CABIN. NO FUMES DETECTED. REPLACED COALESCER BAGS. 2 L 7 2 4F A6WE 1999100100699 19991001 00699 NM 1999 10 1 DL72W992126 1 19990922 A 2782 269002917 ACTUATOR BOEING 727 727247 138408F NM NR 8 LE SLAT FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 2819W 21057 ARRIVING DFW, LOST 'A' SYS HYD. GEAR CAME DOWN NORMALLY, BUT UPON LANDING ZERO QTY AND INTERMITTENT PRESSURE UNTIL PUM P SHUT DOWN AT STOP. REMOVED AND REPLACED NR 8 SLAT ACTUATOR. REPLACED SYS 'A' FILTERS AND CASE DRAIN FILTERS. LEAK C KS GOOD. SERVICED HYD. 2 L 7 3 4F A3WE 1999100100700 19991001 00700 WP 1999 10 1 DLL19992127 1 19990922 A 3210 1626464105 SNUBBER LKHEED 1011 10113853 5265020 WP LT MLG DOOR BROKEN A DALA K NONE P NO WARNING INDICATION AP APPROACH 1 SO 27 755DL 193Y1184 ON ARRIVAL, LEFT MAIN LANDING GEAR DOOR HANGING DOWN. MTC FOUND LEFT MLG DOOR SNUBBER ROD BROKEN. REPLACED LEFT MLG DOOR SNUBBER ROD. DOOR OPS NORMAL. 2 L 7 3 4F A23WE 1999100100701 19991001 00701 NM 1999 10 1 DL733992129 1 19990923 A 2780 SWITCH BOEING 737 737347 1384647 NM LE FLAPS OUT OF ADJUST A DALA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 304WA 23345 DURING FLAP EXTENSION HAD L/E INTRANSIT LIGHT FOR NR 4 SLAT AND L/E FLAPS/SLAT INTRANSIT LIGHT ON FWD PANEL. WITH FLAP S AT 15 DEG THERE WAS AN INCREASE IN AIR NOISE, LEVEL AND A/C YAWED. EMERGENCY DECLARED, FLAPS RECYCLED INDICATION REOC CURED BUT NO YAW. FOUND PROX SWITCH OUT OF ALIGNMENT. ADJUSTED SAME. LUBED FLAPS, ALL CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1999100100702 19991001 00702 NM 1999 10 1 DL72S992130 1 19990923 A 3350 BATTERY S106 BOEING 727 727232 1384082 NM AFT AIRSTAIR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 406DA 21150 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP ON L/O CHECK. REPLACED BATTERYS (P/N 334101877), OPER NOW NORMAL. 2 L 7 3 4F A3WE 1999100100703 19991001 00703 WP 1999 10 1 DLL19992131 1 19990923 A 3260 CONTROL CABLE LKHEED 1011 10113853 5265020 WP LT MLG OUT OF ADJ A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 755DL 193Y1184 MAIN LT GEAR DOOR LIGHT ON WITH DOOR INTRANS LIGHTS ON GEAR ANNUNICATOR. RAN POM CK LIST, CYCLED GEAR AUTOMATICALLY AND USING MECHANICAL RELEASE HANDLES, NO HELP. RETURN LAX. ADJUSTED LOWER PHASE INPUT CABLE PER MM 32-33-06. PERFORMED G EAR SWING, OPS CHECKS OK. 2 L 7 3 4F A23WE 1999100100704 19991001 00704 NM 1999 10 1 DL72S992132 1 19990924 A 3340 65002811 LIGHT BOEING 727 727232 1384082 NM RT WING CONTAMINATED A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 SO 27 518DA 21469 DURING GROUND TRANSFER OF FUEL, THE NR 1 VALVE INDICATOR LIGHT SPARKED AND CAUGHT ON FIRE. DE-POWERED SWITCH AND FIR E EXTINGUISHED. MAINTENANCE FOUND LIGHT ASSY FULL OF FUEL. CHECKED FOR FUEL LEAKS, NONE FOUND. REPLACED LIGHT ASSY , OPN NOW NORMAL. 2 L 7 3 4F A3WE 1999100100705 19991001 00705 NE 1999 10 1 DL72S992133 2 19990924 A 7230 COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STALLED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 535DA 73770 674304 22048 674304 AS POWER WAS INCREASING TO TAKEOFF SETTING NR 2 ENGINE HAD A HARD COMPRESSOR STALL. A HEAVY VIBRATION AND RUMBLING NOIS E WAS HEARD/FELT FROM NR 2 ENGINE. MAXIMUM CROSSWIND WAS LESS THAN 3 KTS. REPLACED NR 2 ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999100100706 19991001 00706 NM 1999 10 1 DL72S992134 1 19990922 A 5320 FRAME BOEING 727 727232 1384082 NM C1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 THE WEB OF THE C1 DOOR CUTOUT AFT JAMB WAS FOUND WITH A SMALL CRACK EMANATING FROM A FASTENER HOLE JUST BELOW THE NR 6 DOOR STOP FITTING. THE CRACK WAS REPAIRED WITH A DOUBLER PER ER/A 368332-14. 2 L 7 3 4F A3WE 1999100100707 19991001 00707 NM 1999 10 1 DL76S992135 1 19990923 A 5312 148T274010 BULKHEAD CAP BOEING 767 767332 1382001 NM BS 1809 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 130DL 24080 THE OUTER CHORD OF THE FS 1809.5 BULKHEAD WAS FOUND WITH A CRACK AT RBL 45 & WL 250. THE CRACK IS TYPICAL OF THAT DOC UMENTED IN BAC S/B 767-53-0078. THE CRACK WAS REPAIRED PER THE PROCEDURES OF THE S/B AND ER/A 368310-14. 2 L 7 2 4F RT A1NM 1999100100708 19991001 00708 NM 1999 10 1 DL76L992136 1 19990924 A 3350 0201720001 LIGHT BOEING 767 767332 1382001 NM ROW 30FG INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 175DN 24803 SEAT MOUNTED PROXIMITY LIGHTS INOP AT SEAT ROW 30 F, G. REMOVED AND REPLACED LUMINATOR AT 30 F, G, LIGHT OPS CKS GOOD. 2 L 7 2 4F RT A1NM 1999100100709 19991001 00709 NM 1999 10 1 DL757992137 1 19990924 A 2121 FAN 731376A BOEING 757 757232 1384965 NM E&E COMPT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 623DL 1015 22913 AT GATE PRIOR TO DEPARTURE, WAS NOTIFIED BY FLT CREW OF EQUIP COOLING FAN OVERHEAT MSG WITH SLIGHT ELECTRICAL FUMES IN C OCKPIT. FOUND FWD EQUIPMENT COOLING FAN POPPING CB. REMOVED FAN WAS SEIZED UP. REPLACED FWD EQUIPMENT COOLING FAN ONE . 2 L 7 2 4F RT A2NM 1999100100710 19991001 00710 NM 1999 10 1 DL72E992138 1 19990909 A 5713 STRINGER BOEING 727 727247 138408F NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 AT HMV2, FOUND HFEL SHOWS CRACK INDICATION WS 656.5 STRINGER TO RIB UPPER FASTENER HOLE FWD MOST RIB. STOP DRILLED CRAC K, DRILLED UP REPAIR PER MM 57-13-00 FIG 804, ANGLES FWD/AFT, INSTALLED ALL EXCEPT COVER PLATE PER MM 57-13-00. REPAIRE D PER MM 57-13-00 FIG 804. 2 L 7 3 4F A3WE 1999100100711 19991001 00711 NM 1999 10 1 DL72E992139 1 19990908 A 2761 ACTUATOR BOEING 727 727247 138408F NM NR 13 SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 AT HV2, FOUND NR 13 SPOILER ACTUATOR MOUNT BOX IS LOOSE AT LOWER MOUNT BOLTS 2, I/B MOUNT POINT IS MISSING SHIMS. SHIMS REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1999100100712 19991001 00712 NM 1999 10 1 DL757992140 1 19990924 A 2131 211738813 CONTROLLER 211738813 BOEING 757 757232 1384965 NM NR 1 INOP A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 651DL 122418 24391 DESCENDING THRU 28K FT CABIN ALT WARNING LIGHT ON OVERHEAD AND FWD PANEL ILLUMINATED WITH ASSOCIATED AURAL WARNING. CAB IN ALT READ 11K, CONDUCTED EMER DESCENT. REPLACED NR 1 PRESS CONTROLLER, RAN BITE ON BOTH CONTROLLERS AND OPN NORMAL. 2 L 7 2 4F RT A2NM 1999100100713 19991001 00713 NM 1999 10 1 DLM88992141 1 19990924 A 3350 3039001 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 988DL 53339 AFT CABIN E-PATH LIGHT SECTION INOP. REPLACED POWER SUPPLY AND BATTERIES, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1999100100714 19991001 00714 NM 1999 10 1 DL76L992142 1 19990923 A 2530 COFFEE MAKER BOEING 767 767332 1382001 NM AFT GALLEY CONTAMINATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 190DN 28447 F/A REPORTED ELECTRICAL BURNING SMELL IN AFT GALLEY. TURNED OFF GALLEY ITEMS AND C/BS. INDIVISUALLY REPOWERED ITEMS. S MELL DID NOT RETURN. FOUND BURNT PAPER UNDERNEATH COFFEEMAKER PULLED AND COLLARED C/BS. FWD TO MCO. 2 L 7 2 4F RT A1NM 1999100100715 19991001 00715 NM 1999 10 1 DL757992143 1 19990925 A 2422 100201021000 INVERTER 100201021 BOEING 757 757232 1384965 NM E&E COMPT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 617DL 477 22907 STRONG ELECTRICAL ODOR THROUGHOUT A/C. EICAS STATUS MSG FWD EQUIP DET 2. EQUIP COOLING TEST. FUEL QUANTITY BITE. STAN DBY INVERTER. DIVERTED TO KSAV. DETERMINED THE SOURCE OF SMOKE/ELECTRICAL ODOR TO BE THE STATIC INVERTER. REPLACED SA ME. OPN CKS NORMAL. NO ODOR NOTED. REPLACED THE FWD EQUIP DET LIGHT ASSY. SYSTEM CKS NORMAL. 2 L 7 2 4F RT A2NM 1999100100716 19991001 00716 NM 1999 10 1 DL757992144 1 19990925 A 3231 RETRACT MECH BOEING 757 757232 1384965 NM NLG DOOR MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 602DL 22809 ON GEAR RETRACTION HAD DOOR DISAGREE AND DOOR LIGHT REMAINED ON ACCOMPANIED BY WIND NOISE. ALSO HAD EICAS MESSAGE. 2 L 7 2 4F RT A2NM 1999100100717 19991001 00717 NM 1999 10 1 DL72E992145 1 19990925 A 3350 S106 BATTERY BOEING 727 727247 138408F NM R2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 EMERGENCY LIGHT AT R2 DOOR INOP. C/W REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999100100718 19991001 00718 NM 1999 10 1 DL72E992146 1 19990925 A 3350 S106 BATTERY BOEING 727 727247 138408F NM AFT AIRSTAIR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 AFT AIRSTAIR EMERGENCY LIGHT INOP. C/W REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999100100719 19991001 00719 NM 1999 10 1 DL72E992147 1 19990925 A 3350 900835A BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 F/C CABIN OVERHEAD EMERGENCY LIGHT INOP. C/W REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999100100720 19991001 00720 NM 1999 10 1 DLM88992148 1 19990925 A 2421 GENERATOR 947F9453 DOUG MD88 MD88 3023688 NM APU FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 992DL XJ2218B 53344 APU GENERATOR FAILED IN FLIGHT AND WOULD NOT RESET. LT GENERATOR ON PREVIOUS DEFERRAL. REPLACED APU GCU. 2 L 7 2 4F RT A6WE 1999100100721 19991001 00721 WP 1999 10 1 DLL14992149 1 19990926 A 8011 STARTER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 3 ENGINE FAILED A DALA O OTHER A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 740DA 27885 14874 193C1244 14874 C/B 1F18 NR 3 ENGINE HP FUEL SOV POPPED. RESET ONCE, POPPED AGAIN. UPON SHUTDOWN LAX, ENCOUNTERED A TAILPIPE FIRE NR 3 ENGINE. NR 3 TANK VALVE CLOSED/STARTER ENGAGED/ MOTORED ENG FIRE HANDLE PULLED/ FIRE EXTINGUISHED. REPLACING STARTER/ NR 3 ENG. HP FUEL SOV. INSP ENGINE PER FIM. FOUND NR 3 ENGINE GLOVE FAIRING PAINT BLISTERED. 2 L 7 3 4F 4 F A23WE E12EU 1999100100722 19991001 00722 NM 1999 10 1 DL72E992150 1 19990908 A 5754 SKIN 651622194 BOEING 727 727247 138408F NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA BN38 21484 SKIN CRACKED UNDER FENCE NR 5 SLAT. REPAIRED AS PER MM 57-54-0. 2 L 7 3 4F A3WE 1999100100723 19991001 00723 1999 10 1 DL757992151 2 19990926 A 7200 ENGINE 45100 BOEING 757 757232 1384965 NM NR 2 FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 631DL 1101 23612 1101 HEARD LOUD POP AND LOST NR 2 ENG. ALL NR 2 ENG INDICATIONS BLANK. OIL PRESS 0, QTY 22. STATUS MESSG: SEC SEL, OIL PR ESS, SEC CONT, PRI CONT, REV CONT. 2 L 7 2 4F RT A2NM 1999100100724 19991001 00724 NM 1999 10 1 DL72E992152 1 19990903 A 5730 SKIN 651622194 BOEING 727 727247 138408F NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA BN38 21484 SKIN CRACKED AND WORN SEVERAL PLACES AT FENCE MOUNT AREA. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999100100725 19991001 00725 NM 1999 10 1 DL72E992153 1 19990903 A 5713 SPAR 651622194 BOEING 727 727247 138408F NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA BN38 21484 LOWER SPAR CRACKED AT NUT PLATE ON NR 11 RIB, MARKED. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999100100726 19991001 00726 WP 1999 10 1 DLL10992155 1 19990924 A 5313 1512399103 STRINGER LKHEED 1011 10113851 5265010 WP BS 1357 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE LBL 25.5 KEELSON STRINGER WAS FOUND WITH A 1.5 INCH LONG CRACK RUNNING FWD-AFT IN THE HORIZONTAL FLANGE AT FS 1357. THE STRINGER WAS CUT AT FS 1357 AND THE AFT END REMOVED. A NEW AFT SECTION WAS FABRICATED AND SPLICED IN PER ER/A 3683 37-14, REV A. 2 L 7 3 4F A23WE 1999100100727 19991001 00727 NM 1999 10 1 DL76S992156 1 19990926 A 5312 148T274010 BULKHEAD CHORD BOEING 767 767332 1382001 NM BS 1809.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 135DL 25145 THE FS 1809.5 BULKHEAD OUTER CAP WAS FOUND WITH A CRACK TYPICAL OF BAC S/B 767-53-0078. THE CRACKED UPPER END OF THE CH ORD WAS CUT AND REMOVED. A NEW SECTION WAS SPLICED IN PER THE PROCEDURES OUTLINED IN S/B 767-53-0078 AND PER ER/A 36835 7-14. 2 L 7 2 4F RT A1NM 1999100100728 19991001 00728 NM 1999 10 1 DL72W992158 1 19990927 A 2782 ANGLE BOEING 727 727247 138408F NM NR 8 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 A 1.75 INCH CRACK AT NR 8 SLAT ACTUATOR O/B ATTACH ANGLE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999100100729 19991001 00729 NM 1999 10 1 DL72W992159 1 19990927 A 5320 ANGLE BOEING 727 727247 138408F NM BS 913.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 STA 910 AND STA 913.5 ANGLES CRACKED AT MLG UPLOCK. REPAIRED PER M/M 53-11-0 PAGE 834. 2 L 7 3 4F A3WE 1999100100730 19991001 00730 NM 1999 10 1 DLM88992160 1 19990927 A 3222 STRUT M88NG DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 917DL 49573 AFTER GEAR RETRACTION NOSE GEAR RED UNSAFE LIGHT ILLUMINATED. LOWERED GEAR THEN RAISED, AGAIN THE NOSE GEAR RED UNSAFE LIGHT STAYED ILLUMINATED ACCOMPANIED BY AN AIR NOISE LIKE THE DOOR WAS POSSIBLY OPEN. RESERVICED AND GREASED NOSE STRUT , SWUNG GEAR AND IND NORMAL. 2 L 7 2 4F RT A6WE 1999100100731 19991001 00731 NM 1999 10 1 DL72W992161 1 19990927 A 5330 SKIN BOEING 727 727247 138408F NM BS 336 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 TWO CRACKS AT FUSE SKIN APPROX .875 IN AND .625 IN AT RIVET HEAD STA 336 LEFT SIDE JUST BELOW STR 22. REPAIRED PER SRM 53-30-3 (TIME LIMITED ). 2 L 7 3 4F A3WE 1999100100732 19991001 00732 NM 1999 10 1 DL72W992162 1 19990927 A 5330 SKIN BOEING 727 727247 138408F NM BS 500 BULGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 SKIN BULDGED FS 500 BETWEEN STR 27R AND 26R. REPAIRED PER SRM 53-30-3 (TIME LIMITED). 2 L 7 3 4F A3WE 1999100100733 19991001 00733 1999 10 1 DL757992164 4 19990927 A 2397 WIRE BOEING 757 757232 1384965 NM VIDO MONITOR CHAFED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 646DL 24217 VIDEO MONITOR BY 2L DOOR SPARKED ON LANDING. FOUND CHAFED WIRES ON MONITOR. REPAIRED SAME. 2 L 7 2 4F RT A2NM 1999100100734 19991001 00734 WP 1999 10 1 DLL19992165 1 19990928 A 5311 1554194101 FRAME LKHEED 1011 10113853 5265020 WP BS 983 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 CORROSION FOUND ON THE HORIZONTAL FLANGE OF THE BS 983 FRAME AT BOTH LEFT AND RIGHT BL 16.0. REPAIRED PER ERA 333606-14 REV A. 2 L 7 3 4F A23WE 1999100100735 19991001 00735 NM 1999 10 1 DL72S992166 1 19990923 A 5753 652163241 SPAR BOEING 727 727225 1384077 NM TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 DURING ACCOMPLISHMENT OF PREVENTATIVE MODIFICATION OF MIDFLAP REAR SPAR ATTACH HOLES PER EO 4-58705-3AD, A FATIGUE CRACK WAS FOUND IN ONE OF THE MOD HOLES IN THE REAR SPAR CHORD. THE HOLE WAS REAMED UP FROM .1875 DIA TO .25 INCH DIA TO REMOVE CRACK INDICATION. AUTHORIZED COLD WORK OF FASTENER HOLE AND INSTALLATION OF OVERSIZED FASTENER. 2 L 7 3 4F A3WE 1999100100736 19991001 00736 NM 1999 10 1 DLM88992167 1 19990928 A 3610 CLAMP DOUG MD88 MD88 3023688 NM TAIL COMP LOOSE A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 916DL 49591 TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED ON CLIMBOUT. LIGHT DID NOT EXTINGUISH UNTIL ABNORMAL PROC COMPLETED. FOUN D LEFT ENGINE AUG VALVE LEAKING AT CLAMP. TIGHTENED SAME. 2 L 7 2 4F RT A6WE 1999100100737 19991001 00737 NM 1999 10 1 DL72W992168 1 19990928 A 3231 MECHANISM BOEING 727 727247 138408F NM NLG DOOR MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 2814W 20870 LANDING GEAR DOOR DID NOT CLOSE AFTER RETRACTION AND REMAINED OPEN AFTER EXTENSION. SECURED BOLT IN NOSE GEAR DO OR LINKAGE. 2 L 7 3 4F A3WE 1999100100738 19991001 00738 NM 1999 10 1 DLM90992169 1 19990928 A 2424 GCU 21B2504 DOUG MD90 MD9030 3023690 NM APU FAILED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 911DA 035C0112 53391 AT 31K FT APU GEN TRIPPED OFF LINE, RT ENG GEN ON MCO. A/C RETURNED. REPLACED APU GCU. 2 L 7 2 4F RT A6WE 1999100100739 19991001 00739 NM 1999 10 1 SCNA99601 1 19990921 A 5320 BEAM BOEING 727 7272A1 138407F NM BS 1183 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINTENANCE CHECK, THE I BEAM IN THE AFT PIT AT BL 0 OF 1183 BULKHEAD WAS FOUND TO EXHIBIT CORROSION ON T HE LOWER LEFT SIDE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. I BEAM TO BE REPLACED. 2 L 7 3 4F A3WE 1999100800001 19991008 00001 SW 1999 10 8 CA990907002 1 19990802 A 6710 206011397001 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL CYCLIC CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 665976 CAE822378 (CAN) CRACK FOUND AT RELIEF HOLE ON THE CYCLIC PIVOT SUPPORT. CAUSE OF CRACK THOUGHT TO BE OVER TIGHTENING TO COMPENSAT E FOR WORN PIVOT BEARINGS. 1 G 7 1 3U 3 U H2SW E4CE 1999100800002 19991008 00002 SW 1999 10 8 CA990907011 1 19990807 A 2820 869A6TT CHECK VALVE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL FUEL SYSTEM FAILED W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION HO HOVERING 1 CA 4575 4349 CAE895044 (CAN) WHILE SLINGING A LOAD IN THE HOVER, THE ENGINE STARTED SURGING AND THEN DECLERATED. PILOT TRIED TO MAINTAIN RPM B UT ENGINE STARTED PULSATING. PILOT LANDED AND THEN SHUT DOWN ROTORCRAFT. 1 G 7 1 3U 3 U H2SW E1GL 1999100800003 19991008 00003 NE 1999 10 8 CA990907020 1 19990823 A 3340 4609467 PIVOT SHAFT GRIMES 4501221 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL LANDING LIGHT WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE890511S (CAN) PIVOT SHAFT ASSY INTERNAL PARTS ARE OF QUESTIONABLE ORIGIN AND DO NOT RESEMBLE THE MANUFACTURER'S TYPE. ALTHOUGH THESE PARTS DID NOT RESULT IN FAILURE, A SIMILAR PART DID FAIL WHICH WAS REPORTED VIA SDR NR 990505001. 1 G 7 2 3U 3 U H1NE E1GL 1999100800004 19991008 00004 NE 1999 10 8 CA990907024 2 19990815 A 7310 0301007720 LINE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE FUEL SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 4450 7069 7069 (CAN) DURING POST-FLIGHT INSPECTION, EVIDENCE OF FIRE DAMAGE WAS NOTED ON THE COMPRESSOR CASING WHICH WAS ATTRIBUTED TO A CRACKED FLARE ON THE FUEL FITTING LINE AT THE BOTTOM OF THE B-NUT. THE SOURCE OF IGNITION IS THOUGHT TO BE EITHER TO STARTER/GENERATOR OR THE HIGH ENERGY IGNITION WIRING. THE SUBJECT FUEL SUPPLY LINE IN USED FOR INITIAL START PURPOSES O NLY AND THEN PURGED WITH COMPRESSOR P2 BLEED AIR. 1 G 7 1 3U 3 U H9EU E19EU 1999100800005 19991008 00005 GL 1999 10 8 CA990907031 2 19990716 A 7323 10560583 SPRING BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL ENGINE CONTROL BROKEN W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA CAE835698 (CAN) ENGINE PERFORMANCE ON TAKEOFF WAS ERRATIC. SUBSEQUENT INVESTIGATION REVEALED THAT GOVERNOR LEVER SPRINGS P/N 105- 60583-12 WERE BROKEN OFF ON BOTH ENGINES. 1 G 7 2 3U 3 U H3EU E4CE 1999100800006 19991008 00006 GL 1999 10 8 CA990907032 2 19990805 A 7323 D297974 ACTUATOR BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL TURBINE GOVERNOR MALFUNCTIONED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA CAE835696 (CAN) DURING TAXI, ENGINES WERE NOT IN OPERATING RANGE. FURTHER INVESTIGATION REVEALED THAT GOVERNORS HAD CHANGED FOR U NEXPLAINED REASONS. 1 G 7 2 3U 3 U H3EU E4CE 1999100800007 19991008 00007 CE 1999 10 8 CA990907045 1 19990817 A 5210 5711145604 FRAME 57111652 CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP MCAULY 3G34C6 3GFR34C601 GL PASSENGER DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5069 P31741C 816155 (CAN) FOUND LOWER DOOR FRAME CRACKED NEAR AFT HINGE ATTACHMENT. 1 L 7 2 3T 4 T RT A28CE E4WE 6 C P54GL 1999100800008 19991008 00008 CE 1999 10 8 CA990907053 1 19990807 A 2720 031019612 SPRING CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160DTM GL RUDDER PEDAL DISCONNECTED W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 712 L3987227A QG005 (CAN) PILOT REPORTED UNEVEN RUDDER PEDAL EFFORT WHILE TAXIING. RUDDER PEDAL RETURN SPRING FOUND DISCONNECTED. NO DAMAG E OR MISRIGGING WAS NOTED WITH THE SPRING OR THE RUDDER CONTROL SYSTEM. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999100800009 19991008 00009 CE 1999 10 8 CA990907065 1 19990819 A 2730 556555026 SUPPORT CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3585 71751 (CAN) WHILE PERFORMING A CONTROL COLUMN INSPECTION DURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE ELEVATOR BALANC E WEIGHT SUPPORT ARM. THE CRACK WAS LOCATED JUST ABOVE THE MOUNTING BOLT HOLE. 1 L 7 2 4F 4 F A22CE E1NE 1999100800010 19991008 00010 CE 1999 10 8 CA990907066 1 19990820 A 5320 55111523 POST 55111522 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3585 71751 (CAN) WHILE PERFORMING AN INSPECTION IAW CITATION SERVICE BULLETIN SB 550-53-30, A CRACK WAS FOUND ON THE AFT DOOR POST. THE CRACK APPEARED TO ORIGINATE FROM A GOUGE CAUSED BY INTERFERENCE WITH AN ANCHOR NUT ATTACHED TO A TRIM BRACKET. 1 L 7 2 4F 4 F A22CE E1NE 1999100800011 19991008 00011 CE 1999 10 8 CA990907068 1 19990823 A 5312 24120082 BULKHEAD CESSNA 172 172RG 2072438 CE LYC O360 O360F1A6 41514 EA MCAULY 2D34C B2D34C220 GL FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 6198 L2853436A 801019 (CAN) DURING SCHEDULED MAINTENANCE, SEVERE CORROSION INCLUDING EXFOLIATION WAS FOUND ON THE LONGITUDINAL CANTED BULKHEAD , PN. 2412008-2. DAMAGE WAS NOTED AFTER THE SUBJECT AREA WAS CLEANED OF GREASE AND EXHAUST RESIDUE. CORROSION WAS ALS O FOUND ON THE BULKHEAD AFT, P/N 2412017-2. BOTH BUKHEADS ARE LOCATED IN THE RIGHT WHEELWELL. 1 H 7 1 3O 3 O 3A17 E286 5 C P7EA 1999100800012 19991008 00012 CE 1999 10 8 CA990907070 1 19990827 A 5343 05411211 SUPPORT CESSNA 182 182B 2072706 CE CONT O470 O470L 17026 SO HARTZL HC82V HC82V* GL LT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4736 069678R T2744N (CAN) LEFT MLG OUTBOARD SUPPORT FITTING CRACKED AT REAR U-BOLT HOLE. 1 H 7 1 3O 3 O NT 3A13 E273 5 C P23EA 1999100800013 19991008 00013 EU 1999 10 8 CA990907079 1 19990820 A 3251 NB41099 STEERING RING BNORM BN2 BN2B27 7080227 EU LYC O540 O540E4C5 41532 EA HARTZL HCC2Y HCC2YK2 GL NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1164 L2142040A AU4112 (CAN) NOSE GEAR STEERING DRIVE RING FOUND CRACKED WHILE PERFORMING INSPECTION IAW THE REQUIREMENTS OF CAA AD NR 005-09-9 3 AND MANDATORY SERVICE BULLETIN BN2/214 ISSUE 2. 1 H 7 2 3O 3 O A17EU E295 5 C P920 1999100800014 19991008 00014 CE 1999 10 8 CA990907083 1 19990814 A 3297 WIRE CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO MCAULY 3AF32C 3AF32C505 GL LT MLG BROKEN W O OTHER N FALSE WARNING AP APPROACH 1 CA 183497R 803885 (CAN) LEFT MAIN LANDING GEAR GREEN (DOWN AND LOCKED LIGHT AFTER LANDING GEAR SELECTED DOWN. EMERGENCY GEAR EXTENSION SY STEM ACTIVATED WITH NO RESULTS. AFTER UNEVENTFUL LANDING, FAULT WAS TRACED TO A BROKEN WIRE AT THE LEFT GEAR DOWN AND L OCKED MICROSWITCH. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 1999100800016 19991008 00016 SW 1999 10 8 CA990915039 1 19990830 A 6210 204011151001 BOLT 204012101143 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA M/R BLADE WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 420 ADA05365 CPPS61875 (CAN) WHILE DOING A MAIN ROTOR BLADE REPLACEMENT, THE BLADE BOLTS LOOKED DIFFERENT AND WERE LATER CONFIRMED BY MANUFACTU RER TO BE BOGUS. ORIGINATOR CHECKING ON PREVIOUS HISTORY OF M/R HEAD ASSY. 1 G 7 1 4U 4 U H4SW E22EA 1999100800017 19991008 00017 SW 1999 10 8 CA990915040 1 19990831 A 6310 BEARING 206040230019 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FREEWHEEL UNIT FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 8039 1344 BLA2320 CAE821158 (CAN) ABNORMAL NOISE JUST PRIOR TO SHUTDOWN NOTED. LATER DETERMINED THAT NOISE EMANATED FROM FREEWHEEL UNIT FORWARD SUP PORT BEARING. FURTHER DISASSEMBLY REQUIRED TO DETERMINE THE FULL EXTENT OF THE DAMAGE. 1 G 7 1 3U 3 U H2SW E4CE 1999100800018 19991008 00018 NE 1999 10 8 CA990915041 1 19990907 A 6410 611730101045 BLADE SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 296016 (CAN) OVER A 6 WEEK PERIOD, 4 TAIL ROTOR BLADES HAVE BEEN REMOVED FOR SMALL POCKET CRACKS. EACH TIME A BLADE WAS REPLAC ED, THE T/R WAS REBALANCED TO 0.1 IPS. THE CRACKS OCCURRED ON TWO DIFFERNT ENT T/R ASSEMBLIES. A SPECTRUM RUN FOR VIBR ATION IN THE TAIL SECTION SHOWED NO ABNORMALTIES AND RIGGING WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. MANUFACTURER WA S NOTIFIED AND BLADES RETURNED FOR EVALUATION AND REPAIR. 2 G 7 2 4U 4 U 1H15 1E3 1999100800020 19991008 00020 SW 1999 10 8 CA990915047 1 19990810 A 2910 41000455 BOLT 41000670005 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL CONTROL LINKAGE WRONG PART W K NONE O OTHER IN INSP/MAINT 1 CA 5183 CAE820383 (CAN) WHILE COMPLYING WITH AD CF-95-11R2 AND BELL SB 206-67A-01, THE BOLTS IN THE LINKAGE ASSY WERE SUSPECTED TO BE UNAP PROVED WHICH WAS LATER CONFIRMED FOR THIS UNIT. 1 G 7 1 3U 3 U H2SW E4CE 1999100800021 19991008 00021 WP 1999 10 8 CA990915053 1 19990830 A 3210 369H600251 LEG HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL LT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE830529 (CAN) GEAR LEG ASSEMBLY TO BRACE ASSEMBLY CRACKED AT BOLT HOLE. 1 G 7 1 3U 3 U H3WE E4CE 1999100800022 19991008 00022 SW 1999 10 8 CA990915059 1 19990827 A 2435 6302FAG543661C3 BEARING LUCAS 23032027 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL STARTER/GEN WRONG PART W K NONE O OTHER IN INSP/MAINT 1 CA 803 16931 CAE820818 (CAN) BOTH ARMATURE SUPPORT BEARINGS REMOVED AND APPEAR TO BE SUB-STANDARD AND UNAPPROVED. ONE BEARING WAS FOUND GLUED INTO THE BEARING LINER WITH A LOCTITE-LIKE SUBSTANCE. APPROVED BEARINGS MFD'D BY OEM (LUCAS.) 1 G 7 1 3U 3 U H2SW E4CE 1999100800023 19991008 00023 WP 1999 10 8 CA990915064 1 19990903 A 5302 ATTACH RING 369A3500505 HUGHES 369 369HE 4470720 WP ALLSN 250C 250C18 03011 GL TAILBOOM BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 517 0062020132 CAE801229B (CAN) THE HORIZONTAL FORWARD ATTACHMENT RING ON THE TAILBOOM WAS FOUND BROKEN OFF. 1 G 7 1 3U 3 U H3WE E4CE 1999100800024 19991008 00024 EA 1999 10 8 99ZZZX3740 2 19990706 A 8550 ENGINE CESSNA 177 177RG 2073709 CE LYC O360 IO360A1B6 41514 EA OIL SYSTEM LEAKING A ALQA O OTHER K FLUID LOSS NR NOT REPORTED 1 CE 05 1938Q 177RG0337 L997351A APPROXIMATELY ONE HOUR OPERATION AFTER COMING OUT OF MAINTENANCE WHICH INCLUDED OIL AND OIL FILTER CHANGE AND REINSTALLI NG AN OVERHAULED PROP AND PROP GOVERNOR, THE ENGINE OIL PRESSURE DROPPED, ENGINE OIL PRESSURE DROPPED, ENGINE OIL EXITED , AND THE ENGINE SEIZED. CAUSE UNKNOWN. 1 H 7 1 3O 3 O A20CE 1E10 1999100800029 19991008 00029 CE 1999 10 8 99ZZZX3745 1 19990914 A 3213 07410013 STRUT CESSNA 185 A185F 2072821 CE LT MLG FAILED A EQDA O OTHER O OTHER LD LANDING 1 AL 01 85LC 2490 18502643 DURING THE LANDING ROLL-OUT, THE LEFT GEAR LEG SHEARED OFF THROUGH THE TWO UPPER BOLT HOLES THAT ARE USED TO HOLD THE AX LE ON CAUSING THE AIRCRAFT TO NOSE OVER ON ITS BACK. THE AIRCRAFT IS USED IN THE WINTER ON WHEEL SKIS AND IN THE SUMMER ON TIRES. MOST OF THE FLYING IS ON UNIMPROVED STRIPS (OFF AIRPORT). 1 H 7 1 3O 3A24 1999100800032 19991008 00032 EA 1999 10 8 99ZZZX3748 2 19990901 A 7414 M3333 IMPULSE COUPLING SLICK 6351 PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA MAGNETO FAILED A FYOA K NONE O OTHER IN INSP/MAINT 1 AL 05 8216T 202 328206087 UPON ROUTINE INSPECTION OF IMPULSE COUPLING, FOUND ONE OF THE PAWL ANCHOR PINS LOOSE IN THE BODY OF THE IMPULSE. PART W AS IN SERVICE 202 HOURS. SUBMITTER HAS FOUND 4 OR 5 CASES OF EXCESSIVE WEAR OF LOW TIME IMPULSE COUPLERS (UNDER 300 HOU RS). 1 L 7 1 3O 3 O A3SO 1E4 1999100800038 19991008 00038 SW 1999 10 8 99ZZZX3754 1 19990822 A 2822 COUPLING ROMEC RG5200F SKRSKY S58T S58T 8141800 SW BOOST PUMP WORN A BUBA K NONE O OTHER IN INSP/MAINT 1 GL 23 58S 1939 B437 581502 MOTOR TO PUMP COUPLING HAD BROKEN TEETH. WEAR APPEARED TO BE DUE TO NORMAL OPERATION. 2 G 7 1 4U NC 1H11 1999100800051 19991008 00051 WP 1999 10 8 AT9900680 1 19990923 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 158-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND CORRODED FLOOR SUPPORT AND ATTACHMENT HARDWARE AT BS 157- 218. REMOVED AND REPLACED FLOOR SUPPORT AND HARDWARE AT BS 157-218IAW DC9 SRM 51-10-3, 51-10-4, 51-30-1, 53-01 FIGURE N R 1. 2 L 7 2 4F A6WE 1999100800052 19991008 00052 WP 1999 10 8 AT9900688 1 19990929 A 5320 ANGLE DOUG DC9 DC932 3022066 WP AFT STAIRS CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND SUPPORT ANGLE FOR AFT VENTRAL STAIRS AND 3RD STEP CORRODE D. REMOVED, FABRICATED, AND INSTALLED SUPPORT ANGLE ON AFT STAIRS AND NR 3 STEP IAW DC9 SRM 51-10-3, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1999100800053 19991008 00053 WP 1999 10 8 AT9900690 1 19990928 A 5320 SUPORT DOUG DC9 DC932 3022066 WP BS 250 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FLOOR SUPPORT CORRODED AT BS 205, RBL 0-40. REMOVED, FAB RICATED, AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-10-4, 51-30-5. 2 L 7 2 4F A6WE 1999100800054 19991008 00054 WP 1999 10 8 AT9900691 1 19990913 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND PASSENGER ENTRY WAY FLOOR SUPPORT WAS CORRODED AT BS 200. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 53-10 FIGURE NR 1. 2 L 7 2 4F A6WE 1999100800055 19991008 00055 WP 1999 10 8 AT9900692 1 19990928 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FLOOR SUPPORT AT LBL 50 BS 160-200 WAS CORRODED. REMOVED , FABRICATED, AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 53-11-1. 2 L 7 2 4F A6WE 1999100800056 19991008 00056 WP 1999 10 8 AT9900693 1 19990913 A 2730 STOP DOUG DC9 DC932 3022066 WP RT ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND RIGHT INBOARD ELEVATOR TRAVEL STOP WAS CORRODED. REMOVED AND REPLACED ELEVATOR TRAVEL STOP AND CADMIUM PLATE IAW DC9 OHM 27-10-1, DC9 DPS 9.89. 2 L 7 2 4F A6WE 1999100800057 19991008 00057 WP 1999 10 8 AT9900674 1 19990902 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FORWARD ENTRY FLOOR PANEL NR 4696 WAS CORRODED. FABRICAT ED NEW SKIN FOR FLOOR PANEL NR 4696 IAW DC9 SRM 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1999100800058 19991008 00058 WP 1999 10 8 AT9900675 1 19990902 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND FORWARD ENTRY FLOOR PANEL NR 894 WAS CORRODED. FABRICATE D NEW SKIN FOR FLOOR PANEL NR 894 IAW DC9 SRM 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1999100800059 19991008 00059 WP 1999 10 8 AT9900676 1 19990909 A 5321 PANEL DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND SUBFLOOR PANEL WAS CORRODED AT LT CUSPLINE TO BS 0 AND RT CUSPLINE TO BS 160-218. REMOVED, FABRICATED, AND INSTALLED 3 EACH SUBFLOOR PANELS AT BS 160-218 IAW DC9 SRM 51-30-2, 5 3-30-2, 51-30-5, 51-30-7. 2 L 7 2 4F A6WE 1999100800060 19991008 00060 WP 1999 10 8 AT9900677 1 19990917 A 5320 TEE DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY, FL, FOUND COCKPIT MOUNTING TEE AT BS 160 WAS CORRODED. REMOVED, FA BRICATED, AND INSTALLED FLOOR MOUNT SUPPORT IAW DC9 SRM 51-30-1, 51-30-2, 53-11-1, 51-10-1, 51-10-2, 51-10-4, 53-01 FIGU RE 2, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1999100800061 19991008 00061 EU 1999 10 8 MALA976588 1 19990929 A 3020 447301 DEICE MODULE SAAB SF340 SF340A 7850100 EU RTNACELLE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 99XJ 099 RIGHT ENGINE INTAKE LIGHT ON, RECYCLED SWITCH, LIGHT REMAINS ON. LIGHT CYCLES OFF AND ON, LOOKS TO BE OPERATING ON THE TEMP LIMIT SWITCHES. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED DE-ICE MODULE IAW SAAB MM CHAPTER 30. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999100800062 19991008 00062 1999 10 8 MALA976589 4 19990927 A 2310 6226520009 CONTROL HEAD SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 79XJ 079 NR 1 RADIO IS INOP, STUCK IN TEST. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED NR 1 COMM CONTROL HEAD. ALL CHECKS GOOD IAW SF 340 MM CHAP 23. 2 L 7 2 4T RT A52EU 1999100800063 19991008 00063 EU 1999 10 8 MALA976590 1 19990929 A 2730 CIRCUIT BREAKER BAC 146 AVRO146RJ85A 1500097 EU Q FEEL HEATER TRIPPED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 510XJ E2325 ON DEPARTURE FROM MSP, THE Q FEEL HEATER FAIL ANNUNICATOR ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND RETURNED TO MSP . MAINTENANCE FOUND Q FEEL CIRCUIT BREAKER TRIPPED. ALSO, FOUND NUMEROUS OTHER CIRCUIT BREAKERS TRIPPED. ALL CB'S WER E TRIPPED DURING A-CHECK MAINTENANCE LAST NIGHT. RESET ALL CB'S. 2 H 7 4 4F RT A49EU 1999100800064 19991008 00064 SO 1999 10 8 LR7A9960 1 19990928 A 5720 24862414L STIFFENER LKHEED 382 382G 526414U SO WS 28 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 4590 DURING FUEL LEAK INVESTIGATION, FOUND OWS 28 LT WING FLAP TRACK RIB STIFFENER FITTING CRACKED APPROX 3 INCHES THROUGH TH REE LOWER INBD ATTACH HOLES. REPLACED STIFFENER IAW SMP 583-57-60 PG 7 AND SMP 583-51-130 PG 47. 2 H 7 4 4T A1SO 1999100800065 19991008 00065 SO 1999 10 8 LR7A9961 1 19990930 A 6120 582855 VALVE LKHEED 382 382G 526414U SO NR 4 PROP DEFECTIVE A LR7A E ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 03 402LC 1365 4698 NR 4 ENGINE SHUTDOWN AT 0725Z DUE PROPELLER RPM OUT OF LIMITS IN MECHANICAL AND NORMAL MODES. LANDED AS SCHEDULED AT OK O WITHOUT INCIDENT. REPLACED NR 4 VALVE HOUSING IAW HN 61135 AND HN7101. 2 H 7 4 4T A1SO 1999100800066 19991008 00066 SO 1999 10 8 LR7A9957 1 19990902 A 5313 LONGERON LKHEED 382 382G 526414U SO BS 956 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 RT SLOPING LONGERON LOWER CAP CRACKED, APPROX 2.5 INCH, IN RADUS OF LOWER CAP AT FS 956 DUE GROUND LOADING EQUIPMENT IMP ACT DAMAGE. REPAIRED IAW SRM 53-50-22. 2 H 7 4 4T A1SO 1999100800067 19991008 00067 EA 1999 10 8 JBXA9900106 1 19991003 A 5270 WARNING CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE PAX DOOR ACTIVATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 572ML 7224 ON FLT 854, CREW RECEIVED PAX DOOR OUT HANDLE MSG, ON CLIMB-OUT. CREW DEFERRED PER MEL 52-70-1. 2 L 7 2 4F 4 F RT A21EA E15NE 1999100800068 19991008 00068 1999 10 8 AWXA9900335 4 19990927 A 2210 2588880901 YAW DAMPER BOEING 737 737277 1384570 NM AUTO PILOT FAILED A AWXA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 28 185AW 47829 2451 22652 WITH AUTO PILOT ENGAGED OR NOT, THE NOSE OF AIRCRAFT MOVES CONSTANTLY ALL CONFIGURATIONS AND C RUISE. REMOVED AND REPLACED YAW DAMPER COUPLER, OPS CK GOOD IAW MM22-11-141 PG 401 CURRENT HISTORY. NO RELATED DISCREP ANCIES. 2 L 7 2 4F RT A16WE 1999100800069 19991008 00069 NM 1999 10 8 AWXA9900336 1 19990928 A 2121 6454051 FAN BOEING 737 7373S3 1384711 NM AFT GALLEY FAILED A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 313AW 43388 43388 23712 DURING DESCENT, FA REPORTED ELECTRICAL SMELL IN AFT GALLEY, CYCLING RECIRC FAN MADE DIFFERENCE INSTANTLY. REPLACED RECI RC FAN PER MM 21-21-22 PG 401. NONE RELATED RECOMMENDATION. 2 L 7 2 4F RT A16WE 1999100800070 19991008 00070 NM 1999 10 8 RAAAB1020 1 19990930 A 3350 86210144 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT FWD EMERGENCY LIGHT AT BULKHEAD PANEL INOPERATIVE. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999100800071 19991008 00071 NM 1999 10 8 UPS99230816 1 19990930 A 5313 STRINGER BOEING 727 727247 138408F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:C CORROSION ON KEEL BEAM STRINGER 29L BS 950E PLUS 12 TO 950E PLUS 15 LBL 7 WL 138 (C53-113-01.06-02). R EPAIRED PER ER NR 99-6148 AND 727 SRM. 2 L 7 3 4F A3WE 1999100800072 19991008 00072 NM 1999 10 8 UPS99230817 1 19990930 A 5313 BAC1498146 STRINGER BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:C CORROSION STR 26R CORRODED BS 720F PLUS 16 740-4. REPAIRED STR 26R SRM 53-10-3, SPLICED IN NEW SECTIO N FROM BS 720F PLUS 5 TO BS 720F PLUS 16, AFTER BLENDING CORROSION OUT OF LIMITS. 2 L 7 3 4F A3WE 1999100800073 19991008 00073 NM 1999 10 8 UPS99230818 1 19990929 A 5320 CLIP BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:C FWD CARGO COMPARTMENT STR CLIP BS 720F, STR 27R, RBL 15 IS CORRODED. REMOVED AND REPLACED CORRODED ST R CLIP BS 720F STR 27R, RBL 15 IAW 51-30-02, 51-30-05. 2 L 7 3 4F A3WE 1999100800074 19991008 00074 NM 1999 10 8 UPS99230819 1 19990929 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 870-950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:C WHILE WORKING CARD 006467 UPON REMOVAL OF FLOOR PANEL BS 870-950, RBL 45-RBL 65, FOUND SEAT TRACK AT B S 900, RBL 47, WL 208 OUTBOARD FLANGE CORRODED. REMOVED AND REPLACED CORRODED SEAT TRACK IAW 51-30-02. 2 L 7 3 4F A3WE 1999100800075 19991008 00075 NM 1999 10 8 UPS99230820 1 19990926 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM ROW 11 ABC DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY LIGHT AT SEAT 11 ABC OUT. REMOVED AND REPLACED BATTTERY PACK AT SEAT 11 ABC. OPS CHECK GOOD PER MM 33-50-00. 2 L 7 3 4F A3WE 1999100800076 19991008 00076 NM 1999 10 8 UPS99230821 1 19990926 A 3350 9621019 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY EXIT SIGN ILLUMINATED AND REMAINED ON. NO CABIN EMERGENCY LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY P ACK AT COCKPIT DOOR PER MM 33-50-00, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800077 19991008 00077 WP 1999 10 8 UPS99830812 1 19990914 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1620 MISDRILLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 L-2 DOOR JAMB FWD AFT FRAME AT L17L HAS MISDRILLED HOLE. REMOVED FASTENERS TRIMMED OUT DAMAGE AND FA BBED REPAIR STRAP PER TIM CO REO 06748. INSTALLED REPAIR PER DC8 SRM 51-1-21 AND REO 06748. 2 L 7 4 4F RT 4A25 1999100800078 19991008 00078 WP 1999 10 8 UPS99830813 1 19990909 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1614 DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 LT AFT SERVICE DOOR FWD TORQUE BOX FWD FRAME HAS DOUBLE DRILL HOLES SPLICE IN NEW FRAME SECTION P ER TIMCO REO 06750. INSTALLED PER TIMC O REO 06750. 2 L 7 4 4F RT 4A25 1999100800079 19991008 00079 WP 1999 10 8 UPS99830814 1 19990908 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 560-580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 STA 560 TO STA 580 LONG 34R HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION. FABBED REPAIR STRAPS, AND INSTALLED IAW DC8 SRM 51 -1-20D. REPAIR ACCOMPLISH IAW REO 06772 FIG 3. 2 L 7 4 4F RT 4A25 1999100800080 19991008 00080 WP 1999 10 8 UPS99830815 1 19990928 A 2120 AIR DIST DOUG DC8 DC873F 302199F WP COCKPIT SMOKE A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 868UP 45968 UPON TAXI, CREW DETECTED SMOKE IN COCKPIT AFTER PREF CHECK WAS ACCOMPLISHED, SUSPECT ELECTRICAL. PERFORMED A/C GENERATO R MAINT PRACTICES IAW MM 24-20-00. ALL CHECKS GOOD, NO EVIDENCE OF SMOKE IN COCKPIT. AIRCRAFT OK FOR SERVICE. 2 L 7 4 4F RT 4A25 1999100800081 19991008 00081 WP 1999 10 8 MWEA99624 1 19990929 A 5313 591141595 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 LONGERON 3R AND 4R IS CRACKED AT STATION 756. MAINTENANCE FABRICATED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 1999100800082 19991008 00082 WP 1999 10 8 MWEA99625 1 19990927 A 5330 5911402 SKIN DOUG DC9 DC981 3022081 WP PAX DOORWAY GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FORWARD PASSENGER DOOR HOLD OPEN CUP SKIN IS GOUGED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999100800083 19991008 00083 NM 1999 10 8 VNAA9909009 1 19990929 A 7712 311835602 SIGNAL COND DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP FAILED A VNAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 438JS 9172 2864 3056 THE LEFT PROPELLER WOULD NOT COME OUT OF FEATHER WHEN THE AUTOFEATHER TEST WAS ATTEMPTED PRIOR TO DEPARTURE. THE AIRCRA FT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FERRIED THE AIRCRAFT TO PIT. MAINTENANCE REPLACED THE L EFT TORQUE SIGNAL CONDITIONER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 77-11-02. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999100800084 19991008 00084 1999 10 8 RAIA9909010 3 19990924 A 6140 AG34 TACH GEN BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 432AM 883 66066 7426-STL - RIGHT ENGINE RPM INDICATOR INOP. MAINTENANCE REPLACED TACH GENERATOR FOR RIGHT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999100800085 19991008 00085 EU 1999 10 8 RAIA9909008 1 19990923 A 2430 6BB442 TERNMINAL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT GENERATOR FAILED A RAIA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 560HK 41076 76082 6183-JFK - RIGHT GEN DROPPED OFF LINE ON TAXI OUT. MAINTENANCE REPLACED GENERATOR WIRE TERMINAL END FOR RIGHT ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 1999100800086 19991008 00086 1999 10 8 RAIA9909009 3 19990924 A 6140 AG34 TACH GEN BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3312UA 01514 WP LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 343TE 955 66192 7509-FWA - LEFT RPM GAUGE STUCK AT ZERO. MAINTENANCE REPLACED LEFT TACH GENERATOR. 2 L 7 2 4T 3 T RT A56EU E3WE 1999100800087 19991008 00087 SO 1999 10 8 RAIA9909021 1 19990930 A 7830 TR UNIT EMB 145 EMB145 SO RT ENGINE DAMAGED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 MXX-SBN - RIGHT THRUST REVERSER SUSTAINED DAMAGE DUE TO ACTUATOR FAILURE. MAINTENANCE REPAIRED DAMAGE IAW EO NR 145-54- 004-1. 2 L 7 2 4F RT T00011AT 1999100800088 19991008 00088 EU 1999 10 8 99ZZZX3767 1 19990717 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 586 13117 S789 FUEL PRESSURE TRANSMITTER INOPERATIVE. PEGGED HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999100800089 19991008 00089 EU 1999 10 8 99ZZZX3768 1 19990720 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 372 13075 S789 FUEL PRESSURE TRANSMITTER INOPERATIVE. PEGGED HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999100800090 19991008 00090 EU 1999 10 8 99ZZZX3769 1 19990529 A 7712 L771M20C1005 INDICATOR UROCOP EC135 EC135P1 8680990 EU DUAL TORQUE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 426 0018 EC1350054 NR 2 NEEDLE WANDERS. 1 G 7 2 3U O H88EU 1999100800091 19991008 00091 1999 10 8 99ZZZX3770 4 19990806 A 3160 L316M30C1002 DISPLAY GRIMES UROCOP EC135 EC135P1 8680990 EU COCKPIT MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 94 0122 EC1350054 MISSING DISPLAY DIGITS. 1 G 7 2 3U O H88EU 1999100800092 19991008 00092 NE 1999 10 8 99ZZZX3771 2 19990713 A 7322 0164248850 FCU SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 399 548M 2817 9362 NG FLUCTUATING 1 PERCENT TO 2.5 PERCENT. 1 G 7 1 3U 3 U H9EU E19EU 1999100800093 19991008 00093 1999 10 8 R7MA0000722 4 19990804 A 3457 453505 SENSOR AGUSTA A109 A109K2 0260502 EU GPS MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 10016 GPS SLOW TO COME ON LINE. (X) 1 G 7 2 3U RT H7EU 1999100800094 19991008 00094 EU 1999 10 8 R7MA0000721 1 19990801 A 5610 109036020142 WINDOW AGUSTA A109 A109K2 0260502 EU COCKPIT CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 10018 WINDOW CRACKED IN SEVERAL PLACES. (X) 1 G 7 2 3U RT H7EU 1999100800095 19991008 00095 EU 1999 10 8 99ZZZX3772 1 19990426 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105NC 48 13302 790 NR 2 FUEL PRESSURE INDICATES 1/2 SCALE WITH BOOST PUMP ON. 1 G 7 2 3U NC H3EU 1999100800096 19991008 00096 EU 1999 10 8 99ZZZX3773 1 19990112 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105NC 65 13301 790 NR 2 FUEL PRESSURE FLUCTUATES THEN REMAINS AT FULL SCALE. 1 G 7 2 3U NC H3EU 1999100800097 19991008 00097 EU 1999 10 8 99ZZZX3774 1 19990328 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105NC 72 13277 790 NR 2 FUEL PRESSURE INDICATED 1/8TH SCALE WITH BOOST PUMP ON. 1 G 7 2 3U NC H3EU 1999100800101 19991008 00101 EU 1999 10 8 99ZZZX3778 1 19990321 A 7931 IPT70RT11000250G TRANSDUCER BOLKMS 117 BK117A3 5626015 EU OIL PRESSURE ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 127HH 216 574910797 7060 TRANSDUCER ERRATIC. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999100800102 19991008 00102 EU 1999 10 8 99ZZZX3779 1 19990716 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 563 2817 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800103 19991008 00103 EU 1999 10 8 99ZZZX3780 1 19990511 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 93LG 582 2654 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800104 19991008 00104 EU 1999 10 8 99ZZZX3781 1 19990225 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 401 2575 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800105 19991008 00105 EU 1999 10 8 99ZZZX3782 1 19990701 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 264 2575 BALL JOINT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800106 19991008 00106 EU 1999 10 8 99ZZZX3783 1 19990728 A 6230 350A37000302 BEARING SNIAS 350 AS350B 8680801 EU MAIN ROTOR MAKING METAL A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 21UM 7094 M224 1674 MAST BEARING PRODUCING METAL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800107 19991008 00107 EU 1999 10 8 99ZZZX3784 1 19990817 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 102LN 370 7130 3065 SPAR TO SEAL JUNCTION ON NR 1 BLADE CRACKED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800110 19991008 00110 NE 1999 10 8 99ZZZX3787 2 19990328 A 7250 430102301 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 755 7077 LE45111EA BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999100800111 19991008 00111 NE 1999 10 8 99ZZZX3788 2 19990328 A 7250 410106802 SPRING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SECTION WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 755 7077 LE45111EA SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999100800112 19991008 00112 NE 1999 10 8 99ZZZX3789 2 19990328 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SECTION WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 755 7077 LE45111EA SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999100800113 19991008 00113 NE 1999 10 8 99ZZZX3790 2 19990328 A 7230 410100712 SHAFT BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 2395 91F054 7077 LE45111EA SECONDARY DAMAGE TO LAB SEAL FAILURE. REPALCED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 4270. 1 G 7 2 3U 3 U H13EU E5NE 1999100800114 19991008 00114 EU 1999 10 8 99ZZZX3791 1 19990703 A 5320 L713M2059103 STIFFENER UROCOP EC135 EC135P1 8680990 EU FUSELAGE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 512 EC1350054 STIFFENER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999100800115 19991008 00115 EU 1999 10 8 99ZZZX3792 1 19990318 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 708 2818 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800116 19991008 00116 EU 1999 10 8 99ZZZX3793 1 19990301 A 2913 704A34310006 PUMP SNIAS 350 AS350B2 8680813 EU HYDRAULIC SYSTEM LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 102LN 189 70788995 3065 PUMP LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800117 19991008 00117 EU 1999 10 8 99ZZZX3794 1 19990630 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 101LN 336 3038 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WIT NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800118 19991008 00118 EU 1999 10 8 99ZZZX3795 1 19990520 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 380 2404 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800119 19991008 00119 EU 1999 10 8 99ZZZX3796 1 19990225 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 379 2575 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800120 19991008 00120 EU 1999 10 8 99ZZZX3797 1 19990324 A 6240 50071550020 SENSOR SNIAS 350 AS350B2 8680813 EU ROTOR TACHOMETER INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 981 2328 2917 UNIT INOPERATIVE. RESISTANCE BETWEEN PINS 2 AND 3 VARIES. INTERMITTENT WARNING LIGHT. REPLACED WITH NEW UNIT, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1999100800121 19991008 00121 EU 1999 10 8 99ZZZX3798 1 19990716 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 362 2817 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999100800122 19991008 00122 NE 1999 10 8 99ZZZX3799 2 19990718 A 7310 30167601 MANIFOLD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911VU 289 1ZM02531 7141 LE45807EF MANIFOLD FAILED SB 0124. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1999100800123 19991008 00123 NE 1999 10 8 99ZZZX3800 2 19990514 A 7240 410106701 SEAL RING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 433 7125 LE45023EA SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999100800126 19991008 00126 EU 1999 10 8 UF6A990810 1 19990812 A 5730 J0575J0001005 SKIN BAG ATP ATP EU WS 61 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN MX - RIGHT HAND WING TRAILING EDGE IS CRACKED AT STA 61. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW BAE ATA SRM 57 60 01. ACFT TT: 16,402.0 HOURS. 2 L 7 2 4T RT A27NM 1999100800127 19991008 00127 NE 1999 10 8 99ZZZX3803 2 19990713 A 7250 410106802 SPRING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 821 7231 LE45593EFA SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1999100800128 19991008 00128 EU 1999 10 8 99ZZZX3804 1 19990907 A 6520 350A33215300 HINGE SNIAS 350 AS350B 8680801 EU T/R GEARBOX CRACKED B FF6R K NONE O OTHER IN INSP/MAINT 1 NM 11 911NT 265 1556 CRACKS IN RUBBER, COULD NOT BALANCE TAIL ROTOR BLADES. 1 G 7 1 3U H9EU 1999100800129 19991008 00129 GL 1999 10 8 99ZZZX3805 2 19990918 A 7323 23057870 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL POWER TURBINE LEAKING B K NONE O OTHER IN INSP/MAINT 1 SW 09 108FH 996 18179 2770 831748 UNIT HAS SAL SEALS. EXTERIOR OF UNIT IS SOOTY, FITTINGS ARE SLIGHTLY RUSTY. AN AS-RECEIVED TEST WAS PERFORMED WITH THE FOLLOWING RESULTS: AT GOVERNOR BREAK TEST POINT 3.010, PR-PG LEAKAGE WAS AT 7.8 INCHES OF HG WITH NO SPEED APPLIED. P R-PG LEAKAGE IS SUPPOSED TO BE 1.2 INCHES OF HG AT 4,500 RPM. SUBMITTER STATED AS-RECEIVED TEST WAS DISCONTINUED SINCE STATIC PR-PG LEAKAGE FAR EXCEEDED THE CONDITIONS. 1 G 7 1 3U 3 U H2SW E4CE 1999100800130 19991008 00130 EU 1999 10 8 99ZZZX3806 1 19990514 A 7712 408104917 SHAFT BOLKMS 117 BK117A4 5626017 EU TORQUEMETER GROOVED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 433 7125 SHAFT EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999100800131 19991008 00131 EU 1999 10 8 99ZZZX3807 1 19990709 A 6420 10531717 BOLT BOLKMS 117 BK117A3 5626015 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 84 7058 BOLT WORN BEYOND SERVICEABLE LIMITS. 1 G 7 2 3U H13EU 1999100800163 19991008 00163 WP 1999 10 8 TWAA9913501 1 19991004 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9404V 53140 FOUND EMERGENCY EGRESS LIGHTS INOPERATIVE AT SEAT ROWS 23, 24, 26 AND 29. REPLACED LAMP AT EACH LOCATION. CHECK-C 11-2 0-98 STL. 2 L 7 2 4F RT A6WE 1999100800164 19991008 00164 WP 1999 10 8 TWAA9913502 1 19991003 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 15-22 OPEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 909TW 49170 THE EGRESS LIGHT SYSTEM WAS INOPERATIVE FROM SEAT ROWS 15 TO 22. FOUND FEEDER CABLE WITH AN ELECTRICAL OPEN. INSTALLED SPLICE IN POWER FEEDER CABLE. CHECK-C 3-1-99 STL. 2 L 7 2 4F A6WE 1999100800165 19991008 00165 WP 1999 10 8 TWAA9913503 1 19990918 A 5311 FRAME DOUG DC9 DC982 3022082 WP LT MLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 DURING CHECK-C MAINT, FOUND IN LT WHEEL WELL, THE FORWARD OUTBOARD LOWER SHELF FRAME WAS CRACKED OUT IN A Y SHAPE 2.5 IN CHES AT X1. REMOVED AND REPLACED WITH NEW SHELF FRAME AND SECURED PER SRM 51-01. 2 L 7 2 4F A6WE 1999100800166 19991008 00166 WP 1999 10 8 TWAA9913504 1 19990922 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE MISREPAIRED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 956U 49701 DURING CHECK-C MAINT, FOUND SUBSTITUTE HYLOCKS INSTALLED ON RT FUSELAGE REPAIR DUE TO DAMAGE WORK ORDER 421356. REMOVED DOUBLER AND REPLACED PER SRM 53-04, FIG 12B. 2 L 7 2 4F A6WE 1999100800167 19991008 00167 WP 1999 10 8 TWAA9913505 1 19990915 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 194 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND A SKIN DENT 1.5 INCHES LONG BY 1.75 INCH WIDE BY 0.095 INCH DEEP AT STA 194 BETWEEN LONGERON 30 AND 29R. ACCOMPLISHED NDT AND FOUND NO CRACK. REPAIRED PER SRM 53-04 FIG 12B. 2 L 7 2 4F RT A6WE 1999100800168 19991008 00168 WP 1999 10 8 TWAA9913506 1 19990915 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 197 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND A SKIN DENT .095 INCHES DEEP AND 1.75 INCHES BY 5 INCHES LONG, AT STA 197 BETWEEN LONGERON 3 0 AND 29R. ACCOMP NDT AND FOUND NO CRACKS. REPAIRED PER SRM 53-04, FIG 12B. 2 L 7 2 4F RT A6WE 1999100800169 19991008 00169 WP 1999 10 8 TWAA9913507 1 19990918 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 1303 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND A 16 INCH BY 7 INCH BY O.156 INCH DEEP DENT IN A PREVIOUS REPAIR AT STA 1303 TO 1310, BETWEE N LONGERON 25R AND 23R. FOUND NO CRACKS PER PART 6, 51-00-03. REPAIRED PER SRM 53-04 SHEET 5 FIG 12B. 2 L 7 2 4F RT A6WE 1999100800170 19991008 00170 WP 1999 10 8 TWAA9913508 1 19990922 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 205 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND FLOOR TRACK CORROSION OUT OF LIMITS AT STA 205, RBL 22. REPLACED SECTION OF TRACK PER SRM 5 3-05, FIG 4F, AT STA 200 TO 266. 2 L 7 2 4F RT A6WE 1999100800171 19991008 00171 WP 1999 10 8 TWAA9913509 1 19990927 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND CORROSION ON CHAIR TRACK AT STA 200, RBL 22. REPLACED SECTION OF TRACK PER SRM 53-05, FIG 4 F. 2 L 7 2 4F RT A6WE 1999100800172 19991008 00172 WP 1999 10 8 TWAA9913510 1 19990924 A 5321 FLOOR DOUG DC9 DC983 3022083 WP BS 1079 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR WEB AT STA 1079, APPROXIMATELY LONGERON 18R. REPAIRED PER SRM 53-01, FIG 2. 2 L 7 2 4F RT A6WE 1999100800173 19991008 00173 WP 1999 10 8 TWAA9913511 1 19990924 A 5321 FLOOR DOUG DC9 DC983 3022083 WP BS 1199 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR WEB BETWEEN STA 1199 AND 1209. INSTALLED DOUBLER PER SRM 53-01, FIGURE 2 . 2 L 7 2 4F RT A6WE 1999100800174 19991008 00174 WP 1999 10 8 TWAA9913512 1 19990924 A 5321 FLOOR DOUG DC9 DC983 3022083 WP BS 1094 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR WEB AT STA 1094, LONGERON 18R. REPAIRED PER SRM 53-01, FIG 2. 2 L 7 2 4F RT A6WE 1999100800175 19991008 00175 WP 1999 10 8 TWAA9913513 1 19990927 A 5321 FLOOR DOUG DC9 DC983 3022083 WP BS 503 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR WEB AT STA 503, LONGERON 18R. REPLACED WEB PER SRM 53-01, FIG 2, FROM ST A 503 TO 551. 2 L 7 2 4F RT A6WE 1999100800176 19991008 00176 WP 1999 10 8 TWAA9913514 1 19990927 A 5321 FLOOR DOUG DC9 DC983 3022083 WP BS 522&541 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR WEB AT STA 522 AND 541, LONGERON 18R. REPLACED WEB PER SRM 53-01, FIG 2, FROM STA 503 TO 551. 2 L 7 2 4F RT A6WE 1999100800177 19991008 00177 WP 1999 10 8 TWAA9913515 1 19990923 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND NUMBER 1 CHAIR TRACK CORRODED AND GROUND BEYOND LIMITS AT STA 200. REPLACED TRACK PER S PM 6-70-01. 2 L 7 2 4F A6WE 1999100800178 19991008 00178 WP 1999 10 8 TWAA9913516 1 19990915 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 160-200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON UPPER FLANGE OF FLOOR ATTACH ANGLES, STA 160 TO 200, BL 0 INCHES. RE PLACED FLOOR SUPPORT PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 1999100800179 19991008 00179 WP 1999 10 8 TWAA9913517 1 19990929 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND THE FLOOR MEMBRANE UNDER THE FORWARD GALLEY WATER SUPPLY PAN WAS CORRODED. REMADE GALLE Y MEMBRANE FROM SAME MATERIAL 7075-T6, 0.020. REINSTALLED RIVETS IN MEMBRANE PER SRM 51-30-2. REINSTALLED HI-LOCKS IN MEMBRANE AND FLOOR SUPPORTS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1999100800180 19991008 00180 WP 1999 10 8 TWAA9913518 1 19990914 A 5320 SPLICE DOUG DC9 DC931 3022065 WP BS 960 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LONGERON 30 SPLICE CORRODED AT STA 960. REMOVED SPLICE AND INSTALLED NEW SPLICE PER SRM 51-60-0, PAGE 27, AND SRM 51-30-5, AND DOUGLAS INSTALLATION DRAWING 5919707. 2 L 7 2 4F A6WE 1999100800181 19991008 00181 NM 1999 10 8 HNAA9900131 1 19991002 A 3221 85312780 TRUNNION DHAV DHC8 DHC8102 2809003 NM RT NLG WW CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 009 RT NLG SHOCK STRUT TRUNNION CORRODED. FWD SIDE MATING SURFACE FOR TRUNNION CAP, APPROX .016 DEEP. REPAIRD IAW RD8-53-4 535. PLACED ON A 1000 HR DEFERAL FOR PERM REPAIR. 2 H 7 2 4T RT A13NM 1999100800182 19991008 00182 NM 1999 10 8 HNAA9900132 1 19991002 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CHAFED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 009 WHEEL WELL CUT-OUT RADIUS CHAFED IN AFT RT SIDE APPROX .031 DEEP. DISPOSITION: BLEND OUT CHAFE AT 20:1 BLEND RATIO. ED DY CURRENT TO VERIFY NO CRACKS. TOUCH-UP W/ALODINE PER SRM 51-20-16 AND EPOXY PRIME PER SRM 51-20-36. COMPLIED WITH ST ATED DISPOSITION. 2 H 7 2 4T RT A13NM 1999100800183 19991008 00183 NM 1999 10 8 HNAA9900133 1 19991002 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 009 DENT LOCATED BETWEEN STRINGER 17 AND 18, 4 INCHES AFT OF ICE SHIELD, .044 DEEP .6 BY .1. C/W EO8-53-99-338 AS REQUIRED. 2 H 7 2 4T RT A13NM 1999100800184 19991008 00184 NM 1999 10 8 HNAA9900134 1 19991002 A 7921 INTERCOSTAL DHAV DHC8 DHC8102 2809003 NM NR 2 OIL COOLER CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 906HA 009 NR 2 ENGINE OIL COOLER DOOR I/B INTERCOSTAL CRACKED FROM LARGE RIVET JUST FWD OF HINGE POINT RUNNING AFT TO HINGE POINT HOLE. DEFERED PER ESR8-54-91-11. REPLACE WITH POST MOD 8/1619 INTERCOSTAL WITHIN 500 HRS. REMOVED AND REPLACED OIL CO OLER DOOR I/B INTERCOSTAL . 2 H 7 2 4T RT A13NM 1999100800185 19991008 00185 WP 1999 10 8 AT9900679 1 19990923 A 5347 5295597812000 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 217-372 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FORWARD CARGO SEAT TRACK WAS CORRODED AT BS 217-372. REMO VED AND REPLACED SEAT TRACK AT BS 217-372 IAW DC9 SRM 53-21-0. 2 L 7 2 4F A6WE 1999100800186 19991008 00186 WP 1999 10 8 AT9900689 1 19990917 A 5330 DOUBLER DOUG DC9 DC932 3022066 WP BS 75R CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 817AT 47323 FOUND 3 CRACKS IN FUSELAGE NOSE SKIN AT BS 76R BELOW RIGHT INTERCOSTAL. REMOVED, FABRICATED, AND INSTALLED REPAIR INTER NAL DOUBLERS AND FILLERS AT BS 75R IAW DC9 DWG SR09530239. 2 L 7 2 4F A6WE 1999100800187 19991008 00187 NM 1999 10 8 CALA9901292 1 19991002 A 3230 SENSOR BOEING 737 7373T0 1384582 NM LANDING GEAR OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 14334 23572 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE OVERRIDE TRIGGER WAS USED PER QRH. THE AIRCRAFT WAS RETU RNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR SAFETY SENSOR OUT OF RIG. THE SENSOR WAS ADJUS TED IAW MM 32-09-01. THE GEAR WAS SWUNG AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999100800188 19991008 00188 NM 1999 10 8 CALA9901293 1 19990927 A 5532 PANEL BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND TWO 3 CRACKS IN VERTICAL STABILIZER SADDLE PANEL. THE SADDLE PANEL WAS REMOVED, REPAIRED IAW SRM 55-30 -7, FIGURE3, AND REINSTALLED IAW MM 55-30-1, PAGE 201. 2 L 7 3 4F A3WE 1999100800189 19991008 00189 WP 1999 10 8 CALA9901294 1 19990924 A 5532 PANEL DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND A 3 CRACK IN VERTICAL STABILIZER PANEL ON LT SIDE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGUR E 2, SHEET 2, 51-60-0, PAGE 5, 51-30-5, AND 51-30-2. 2 L 7 2 4F A6WE 1999100800190 19991008 00190 WP 1999 10 8 CALA9901295 1 19990924 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1007-1320 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND RT SEAT TRACK CORRODED AT FS 1007-1320, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTA LLED IAW SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1999100800191 19991008 00191 NM 1999 10 8 CALA9901296 1 19990925 A 5315 FLOORBEAM BOEING 757 757224 1384958 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND TOP CHORD OF FLOORBEAM CORRODED AT STA 720 BETWEEN RBL 1.0 AND RBL 53. THE FLOORBEAM CHORD WAS REPAIRE D IAW ECRA 5321-01066. 2 L 7 2 4F RT A2NM 1999100800192 19991008 00192 NM 1999 10 8 CALA9901297 1 19990926 A 5347 SEAT TRACK BOEING 757 757224 1384958 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND SEAT TRACK CORRODED AT STA 720, RBL 24.75. THE SEAT TRACK WAS REPAIRED IAW DRAWING NR 140N2069. 2 L 7 2 4F RT A2NM 1999100800193 19991008 00193 NM 1999 10 8 CALA9901298 1 19990927 A 5315 FLOORBEAM BOEING 757 757224 1384958 NM BS 277-378 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND FLOORBEAMS CORRODED AT STA 277.7, RBL 43-48, STA 365, RBL 6.12-10.25, AND STA 377.7, LBL 22. THE FLOOR BEAMS WERE REPAIRED IAW ECRA 5321-01071. 2 L 7 2 4F RT A2NM 1999100800194 19991008 00194 NM 1999 10 8 CALA9901299 1 19990927 A 5320 INTERCOSTAL BOEING 757 757224 1384958 NM BS 333 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 333, RBL 2. REPAIRED IAW ECRA 5322-01003. 2 L 7 2 4F RT A2NM 1999100800195 19991008 00195 NM 1999 10 8 CALA9901300 1 19990927 A 5347 SEAT TRACK BOEING 757 757224 1384958 NM BS 377-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT BS 377.7-440, LBL 45. THE SEAT TRACK WAS REPLACED IAW DRAWING 141N5130. 2 L 7 2 4F RT A2NM 1999100800196 19991008 00196 NM 1999 10 8 CALA9901301 1 19990927 A 5753 SKIN BOEING 757 757224 1384958 NM RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND A 1.2 CRACK IN RT O/B T/E FLAP O/B LOWER SKIN. THE SKIN WAS REPAIRED IAW ECRA 5753-01086. 2 L 7 2 4F RT A2NM 1999100800197 19991008 00197 NM 1999 10 8 CALA9901302 1 19990927 A 5330 SKIN BOEING 757 757224 1384958 NM BS 600-620 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND IMPACT DAMAGE TO SKIN AT BS 600-620, S15L-16L. REPAIRED IAW ECRA 5331-01068. 2 L 7 2 4F RT A2NM 1999100800198 19991008 00198 NM 1999 10 8 CALA9901303 1 19990928 A 5730 PANEL BOEING 757 757224 1384958 NM WS 150 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND LT WING FIXED LEADING EDGE PANEL DELAMINATED AT WS 150. THE PANEL WAS REPAIRED IAW SRM 51-70-08, 57-41 -01, AND 51-40-2. 2 L 7 2 4F RT A2NM 1999100800199 19991008 00199 NM 1999 10 8 CALA9901304 1 19990927 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14324 23375 INSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON SKIN UPPER SURFACE AT NAC STA 208. A DOUBLER WAS INSTALLED IAW ECRA 5430- 01230. 2 L 7 2 4F RT A16WE 1999100800200 19991008 00200 NM 1999 10 8 CALA9901305 1 19990927 A 5320 FRAME BOEING 737 7373T0 1384582 NM L1 WINDOW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN COCKPIT L-1 WINDOW FRAME. A REPAIR WAS INSTALLED IAW ECRA 5330-02876. 2 L 7 2 4F RT A16WE 1999100800201 19991008 00201 NM 1999 10 8 CALA9901306 1 19990929 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND A 1 CRACK IN INTERCOSTAL AT R-1 DOORWAY, STA 328, STRINGER 8A. A DOUBLER WAS INSTALLED IAW SRM 51-40-2 AND DRAWING NR 65C33288-1. 2 L 7 2 4F RT A16WE 1999100800202 19991008 00202 NM 1999 10 8 CALA9901307 1 19990929 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND A 2 INCH CRACK IN R-1 DOOR AFT FRAME AT STRINGER 8A, STA 328. STRINGER 8A HAD A .5 INCH CRACK. THE FR AME AND STRINGER WERE REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 1999100800203 19991008 00203 NM 1999 10 8 CALA9901308 1 19990930 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON SKIN UPPER SURFACE. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 1999100800204 19991008 00204 NM 1999 10 8 CALA9901309 1 19990930 A 3350 TERMINAL BOEING 727 727224 1384076 NM EXIT SIGN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND THE R-2 DOOR EXIT SIGN INOPERATIVE. REPAIRED TERMINAL AT SOCKET AND OPERATION CHECKED GOOD IAW MM 33-5 3-01, PAGE 201. 2 L 7 3 4F A3WE 1999100800205 19991008 00205 NM 1999 10 8 CALA9901310 1 19990930 A 3350 BATTERY BOEING 727 727224 1384076 NM RT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND RT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RECHARGED THE BATTERY AND OPERATION CHECKED GOOD IAW MM 33-60-01, PAGE 201. 2 L 7 3 4F A3WE 1999100800206 19991008 00206 NM 1999 10 8 CALA9901311 1 19991004 A 3397 WIRE BOEING 727 727224 1384076 NM R1 DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT R-1 DOOR INOPERATIVE. REPAIRED GROUND WIRE AND POWER WIRE AND OPERATION CH ECKED GOOD IAW MM 33-50-1. 2 L 7 3 4F A3WE 1999100800207 19991008 00207 NM 1999 10 8 CALA9901312 1 19991002 A 3350 1000677 CONNECTOR GRIMES BOEING 727 727224 1384076 NM L1 DOORWAY LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND EMERGENCY EXIT LIGHT AT L-1 DOOR INOPERATIVE. RESEATED CONNECTOR PLUG TO LIGHT AND OPERATION CHECKED G OOD IAW MM 33-51-02, PAGE 501. 2 L 7 3 4F A3WE 1999100800208 19991008 00208 WP 1999 10 8 CALA9901313 1 19990930 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 229-250 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT FS 229-250, LONGERON 18L TO 17L. THE DAMAGED SECTION OF SKIN WAS REMOVED AN D NEW SKIN AND DOUBLERS WERE INSTALLED IAW SRM 51-30-2, 51-30-5, AND ECRA 5330-02445. 2 L 7 2 4F A6WE 1999100800209 19991008 00209 WP 1999 10 8 CALA9901314 1 19990930 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 6 INCH CRACK IN AFT CARGO DOOR INNER PAN AT AFT LATCH CLAMP. THE CRACK WAS STOP DRILLED IAW SRM 52-0 5, FIGURE 26A. A REPAIR ANGLE WAS INSTALLED IAW SRM 52-01, FIGURE 26A. 2 L 7 2 4F A6WE 1999100800210 19991008 00210 WP 1999 10 8 CALA9901315 1 19990930 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 220 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 220 JUST ABOVE LONGERON 18L. THE DENTED SKIN WAS REMOVED AND NEW SKIN A ND DOUBLERS WERE INSTALLED IAW ECRA 5330-02471. 2 L 7 2 4F A6WE 1999100800211 19991008 00211 WP 1999 10 8 CALA9901316 1 19990930 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 200-230 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 10 INCH CRACK IN RT CUSP WEB AT FS 200-230. THE CUSP WEB AND SUPPORT WERE REMOVED IAW SRM 51-30-2. A NEW CUSP WEB AND SUPPORT WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999100800212 19991008 00212 SO 1999 10 8 COMA9910155 1 19990928 A 3150 CIRCUIT BREAKER EMB 120 EMB120RT SO CB PANEL TRIPPED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 248CA 1228 DURING TAKEOFF FROM MCO, THE AURAL TRIM WARNING ACTIVATED. FOUND THE AURAL WARNING CIRCUIT BREAKER TRIPPPED, RESET THE AURAL TRIM WARNING CIRCUIT BREAKER. 2 L 7 2 4T RT A31SO 1999100800213 19991008 00213 SO 1999 10 8 COMA9910156 1 19991003 A 5270 SWITCHES EMB 120 EMB120RT SO PAX DOOR DIRTY A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 266CA 1258 AFTER DEPARTURE FROM LAN, THE CABIN DOOR WARNING CAUTION ACTIVATED ON MAP. AIRCRAFT RETURNED TO THE FIELD. CLEANED ALL CABIN DOOR MICROSWITCHES, OPERATIONAL CHECK INDICATED CABIN DOOR INDICATING SYSTEM SATISFACTORY. 2 L 7 2 4T RT A31SO 1999100800214 19991008 00214 SO 1999 10 8 COMA9910157 1 19991003 A 5610 WINDSHIELD EMB 120 EMB120RT SO LT COCKPIT LOOSE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 246CA 1223 LOUD AIR NOISE FROM THE CAPTAINS WINDSHIELD AFTER DEPARTURE FROM MCO, AIRCRAFT RETURNED TO THE FIELD. RETORQUED THE SCR EWS FOR THE CAPTAINS WINDSHIELD. 2 L 7 2 4T RT A31SO 1999100800215 19991008 00215 EA 1999 10 8 COA9960553 1 19991003 A 3010 WARNING CNDAIR CL600 CL6002B19 EA ANTI ICE SYS ACTIVATED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 785CA 7326 DURING CLIMB-OUT FROM CVG, THE ANIT-ICE WARNING ACTIVATED, CREW FOLLOWED QRH PROCEDURE, MESSAGE CLEARED AFTER CLOSING 14 TH STAGE BLEED AIR. PERFORMED AN ELECTRICAL CHECK OF LEFT AND RIGHT 14TH STAGE LOOPS AND PERFORMED AN OPERATIONAL CHECK , NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999100800216 19991008 00216 EA 1999 10 8 COMA9960554 1 19991003 A 5350 RADONE CNDAIR CL600 CL6002B19 EA NOSE BIRD STRIKE A COMA A UNSCHED LANDING C F.O.D. CR CRUISE 1 SO 01 784CA 7319 AFTER DEPARTURE FROM CVG, THE AIRCRAFT ENCOUNTERED A BIRD STRIKE ON NOSE SECTION. AIRCRAFT RETURNED TO THE FIELD. COMP LIED WITH BIRD STRIKE INSPECTION, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999100800217 19991008 00217 EA 1999 10 8 COMA9960555 1 19991003 A 5330 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 209 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 CRACK DETECTED IN THE RIGHT HORIZONTAL SURFACE OF LOWER WING ACCESS HOLE AT PANEL 650 CB. REPAIRED DAMAGE IAW BOMBARDIE R REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999100800218 19991008 00218 EA 1999 10 8 COMA9960556 1 19991002 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13479 7038 FRAME AND DOUBLER AT FS 718.00 RHS FOUND TO BE CRACKED BETWEEN STR 11 AND STR 12. PERFORMED A MAJOR REPAIR TO CRACKED F RAME AND DOUBLER IAW WVAC EO 601R-53-0381. 2 L 7 2 4F RT A21EA 1999100800219 19991008 00219 EA 1999 10 8 COMA9960557 1 19991003 A 5320 6003603023 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 999CA 87837 7230 THE DOUBLER AT FS 718.00 RHS STR 11 IS CRACKED. PERFORMED A MAJOR REPAIR TO FS 718.00 RHS STR 11 BY REPLACING DOUBLER I AW WVAC EO 601R-53-0388. 2 L 7 2 4F RT A21EA 1999100800220 19991008 00220 EA 1999 10 8 COMA9960558 1 19990928 A 3250 TILLER CNDAIR CL600 CL6002B19 EA COCKPIT MISRIGGED A COMA K NONE O OTHER CL CLIMB 1 SO 01 991CA 7216 STEERING INOPERATIVE MESSAGE APPEARED AFTER TAKEOFF FROM MCO, AIRCRAFT RETUREND TO THE FIELD. RE-CENTERED THE STEERING TILLER. 2 L 7 2 4F RT A21EA 1999100800221 19991008 00221 EA 1999 10 8 COMA9960559 1 19990927 A 2781 WARNINRG CNDAIR CL600 CL6002B19 EA LE FLAP ACTIVATED A COMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 959CA 7116 FLAP FAIL CAUTION MESSAGE ON EICAS WHILE ON GROUND. COMPLIED WITH AIRWORTHINESS DIRECTIVE 98-20-01 PARAGRAPH (B) 1 2 3 (A.B.C, AND 3). SYSTEM RESET AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999100800222 19991008 00222 EA 1999 10 8 COMA9960560 1 19990923 A 3260 TARGET CNDAIR CL600 CL6002B19 EA MLG WW LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 967CA 7134 DURING CLIMB-OUT FROM CVG, GEAR DISAGREE WARNING ACTIVATED WHEN WAS RETRACTED. AIRCRAFT RETURNED TO THE FIELD. SECURED LOOSE UPLOCK TARGET ON THE MAIN LANDING GEAR. 2 L 7 2 4F RT A21EA 1999100800223 19991008 00223 EA 1999 10 8 COMA9960561 1 19990927 A 2750 601R930507 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 779CA 1072 7306 DURING CLIMB-OUT FROM CVG, THE FLAPS FAIL CAUTION MESSAGE ACTIVATED, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1999100800224 19991008 00224 EA 1999 10 8 COMA9960562 1 19990927 A 5610 1393212 WINDSHIELD CNDAIR CL600 CL6002B19 EA RT COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 946CA 10412 7072 RIGHT WINDSHIELD CRACKED DURING FLIGHT AT 31,000 FEET, DESTINATION IAW. AIRCRAFT DIVERTED TO LIT. REPLACED RIGHT WINDS HIELD. 2 L 7 2 4F RT A21EA 1999100800225 19991008 00225 NM 1999 10 8 UPS99630822 1 19991001 A 2560 37912325 HOUSING BOEING 767 76734AF 1385212 NM CABIN BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 324UP 27750 EMERGENCY DESCENT, DEVICE HOUSING BENT, FOUND DURING ROUTINE MAINT CK OF S/N AND P/N, PREVENTED DESCENT DEVICE FROM BEIN G RELEASED. STRAIGHTENED HOUSING. 2 L 7 2 4F RT A1NM 1999100800226 19991008 00226 WP 1999 10 8 UPS99830823 1 19991003 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 W/E COCKPIT EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK ASSY, EMERGENCY LIGHTS OPS CKD NORMAL. 2 L 7 4 4F RT 4A25 1999100800227 19991008 00227 EU 1999 10 8 QXEA9902006 1 19990928 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU EMER EXIT INOP A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 11156 SEA- FORWARD OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999100800228 19991008 00228 NM 1999 10 8 VNAA9909010 1 19990929 A 5320 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG WW LEAKING A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 425JS 3037 ON CLIMB-OUT, THE FLIGHT CREW REPORTED A RUDDER LIMITED FAIL CAS MESSAGE ABOVE 160 KTS. THEY ALSO EXPERIENCED A CABIN P RESSURIZATION WARNING ABOVE 10000 FT. THE FLIGHT CREW RETURNED TO THE FIELD AND A NORMAL LANDING WAS PERFORMED. MAINTE NANCE INSPECTED THE AIRCRAFT AND RESEATED THE ACCESS COVER LOCATED IN THE NOSE LANDING GEAR BAY IN ACCORDANCE WITH DORNI ER MAINTENANCE MANUAL 06-40-00. THE RUDDER LIMITER SYSTEM WAS INSPECTED AND DEFERRED IN ACCORDANCE WITH THE DORNIER MIN IMUM EQUIPMENT LIST. THE RUDDER LIMITER SYSTEM WAS FUNCTIONALLY TESTED IN ACCORDANCE WITH DORNIER MAINTENANCE 27-23-04 AND FOUND TO OPERATE NORMALLY MEL WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999100800229 19991008 00229 NM 1999 10 8 VNAA9910001 1 19991003 A 3350 321430 BATTERY PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 6LK DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 434JS 9688 128 3051 A SECTION OF EMERGENCY FLOOR LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAF T WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999100800230 19991008 00230 1999 10 8 RAIA9910001 4 19991001 A 3418 C771076 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU NR1 STICK SHAKER FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 879 7440 - STL - STICK SHAKER ACTIVATED DURING TAXI. MAINTENANCE REPLACED NR 1 AND NR 2 LEFT TRANSDUCERS. 2 L 7 2 4T RT A56EU 1999100800231 19991008 00231 EU 1999 10 8 RAIA9910002 1 19991001 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU BAGGAGE COMPT FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 864AE 864 4783 - LAX - AFT BAGGAGE SMOKE LIGHT. MAINTENANCE REPLACED AFT BAGGAGE SMOKE DETECTOR. 2 L 7 2 4T RT A56EU 1999100800232 19991008 00232 1999 10 8 RAIA9910003 2 19991001 A 7320 897260 DELTA PP BOX BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 428AM 16824 12351 877 7330 - STL - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT DELTA P/P BOX. 2 L 7 2 4T RT A56EU 1999100800233 19991008 00233 EU 1999 10 8 RAIA9910004 1 19991002 A 2421 8260121 GENERATOR AEROSP ATR42 ATR42300 8680920 EU NR 2 FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 421TE 13859 5229 102 7140 - STL - NR 2 GENERATOR INOP. MAINTENANCE REPLACED NR 2 GENERATOR AND GCU. 2 H 7 2 4T RT A53EU 1999100800234 19991008 00234 EU 1999 10 8 RAIA9910005 1 19991002 A 2424 10200311 GCU AEROSP ATR42 ATR42300 8680920 EU NR 2 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 421TE 102 7140 - ST L- NR 2 GENERATOR INOP. MAINTENANCE REPLACED NR 2 GENERATOR AND GCU. 2 H 7 2 4T RT A53EU 1999100800235 19991008 00235 1999 10 8 RAIA9910007 4 19991001 A 3418 C771076 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU NR2 STICK SHAKER FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 879 7440 - STL - STICK SHAKER ACTIVATED. MAINTENANCE REPLACED BOTH LEFT TRANSDUCERS. 2 L 7 2 4T RT A56EU 1999100800236 19991008 00236 WP 1999 10 8 TWAA9913601 1 19991004 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 928TW 48012 FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE, AND LAST ROW OF EGRESS LIGHTS WERE FLASHING WHEN SYSTEM WAS ARMED. RE PLACED THE FORWARD CABIN POWER SUPPLY, AND REPAIRED WORN FEEDER CABLE CONNECTOR FOR THE AFT CABIN. CHECK-C 9-23-99 STL. 2 L 7 2 4F A6WE 1999100800237 19991008 00237 WP 1999 10 8 TWAA9913602 1 19990924 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 7-8-11&33 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 959U 49704 THE EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 7, 8, 11 AND 33, AND THE AIRSTAIRS. REPLACED THE BATTERY PACK, PART NR 58 22-2, IN THE CABIN AND REPAIRED WIRING IN THE AIRSTAIRS. CHECK-C 7-6-99 JFK. 2 L 7 2 4F A6WE 1999100800238 19991008 00238 WP 1999 10 8 TWAA9913603 1 19990806 A 3397 58541 WIRE DOUG DC9 DC951 3022051 WP ROW 17-21 WORN A TWAA O OTHER L NO TEST CR CRUISE 1 CE 05 405EA 47688 THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 3 TO 12, AND ILLUMINATED ALL THE TIME BETWEEN ROWS 17 AND 21. REPLACED THE BROKEN FEEDER MFG 5854-1 FOR THE FORWARD CABIN, AND THE MID CABIN POWER SUPPLY MFG 5822-2 FOR THE MALFUNCTION BETWEEN R OWS 17 AND 21. CHECK-C 3-30-99 STL.- 2 L 7 2 4F RT A6WE 1999100800239 19991008 00239 WP 1999 10 8 TWAA9913604 1 19990922 A 3397 0105606003 WIRE DOUG DC9 DC983 3022083 WP ROW 3 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9615W 53562 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW 3. FOUND WIRE PULLED OUT AT THE LIGHT MODULE. REPLACED THE MODULE. CH ECK-C 7-18-99 STL. 2 L 7 2 4F RT A6WE 1999100800240 19991008 00240 NM 1999 10 8 TWAA9913605 1 19990922 A 3397 1317 WIRE BOEING 757 7572Q8 1384972 NM ROW 5 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 709TW 28168 THE EGRESS LIGHTS WERE INOPERATIVE AT THE MID LAVATORY AND AT ROW 5. REPAIRED BROKEN WIRES AT THE MID LAV, AND REPLACED TWO LAMPS AT ROW 5. CHECK-C 10-24-98 LAX. 2 L 7 2 4F RT A2NM 1999100800241 19991008 00241 NM 1999 10 8 TWAA9913606 1 19991004 A 3350 59123 LIGHT BOEING 767 767231 1385131 NM GALLEY DAMAGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 603TW 22566 THE CABIN EGRESS LIGHT WAS INOPERATIVE AT THE MID GALLEY. FOUND A CUT IN THE LIGHT STRIP. REPLACED THE STRIP. CHECK-C 9-1-99 LAX. 2 L 7 2 4F RT A1NM 1999100800242 19991008 00242 WP 1999 10 8 TWAA9913608 1 19990923 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9413T 53188 THE EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 3, 5, 19, 21, AND 22. REPLACED THE LAMP, MFG PN 1315, FOR ROWS 3 AND 5, AND REPLACED THE BATTERY FOR REMAINING ROWS. CHECK-C 8-11-99 MCI. 2 L 7 2 4F RT A6WE 1999100800243 19991008 00243 1999 10 8 MALA976591 4 19990922 A 2210 CONTROL PANEL SAAB SF340 340B 7860101 EU AUTO PILOT FAILED A MALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 15 424XJ 424 SMOKE IN COCKPIT, DECLARED AN EMERGENCY, LANDED, SMOKE DISSIPATED, NORMAL SHUTDOWN. AUTO PILOT CIRCUIT BREAKER IS POPPE D. MAINTENANCE FOUND FO'S GA WIRING IN RIGHT PL SHORTED, STOWED WIRES AND PULLED AND COLLARED CAPTAIN'S AND FO'S AP CB' S. MAINTENANCE REPLACED CONTROL QUADRANT IAW SF340 CHAP 76. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999100800244 19991008 00244 EU 1999 10 8 MALA976592 1 19991004 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMP FAILED A MALA O OTHER N FALSE WARNING LD LANDING 1 GL 15 423XJ 423 CARGO SMOKE LIGHT ILLUMINATED JUST BEFORE TOUCHDOWN, EXTINGUISHER NR 1 DISCHARGED. MAINTENANCE INSPECTED AFT BULKHEAD, NO EVIDENCE OF ANY SMOKE, REPLACED FWD SMOKE DETECTOR, AFT DETECTOR, FIRE EXTINGUISHER NR 1 BOTTLE AND SQUIB. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999100800245 19991008 00245 NE 1999 10 8 PNSA990704 2 19990731 A 8530 CYLINDER GRUMAV G21 G21A 3951204 SO PWA R985 R985* 52008 NE ENGINE BROKEN A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING E K VIBRATION/BUFFET FLUID LOSS CR CRUISE 1 AL 03 7811 B122 24966 ENGINE BEGAN TO VIBRATE IN CRUISE AND SUBSEQUENTLY LOST OIL PRESSURE. SECURED ENGINE AND LANDED AIRCRAFT. ENGINE REPLA CED DUE TO CASE DAMAGE FROM BROKEN CYLINDER HOLD DOWN STUDS. 1 H 7 2 3R 3 R TC654 5E1 1999100800246 19991008 00246 WP 1999 10 8 PNSA990901 2 19990907 A 7314 8973809 PUMP CESSNA 441 441 2076020 CE GARRTT TPE331 TPE33110 01514 WP RT ENGINE SIEZED A PNSA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 AL 03 441LL 40232 441139 P77277 ON RUNWAY, SELECTED SPEEDS HIGH FOR TAKEOFF, RT ENGINE FLAMED OUT. RETURNED TO BLOCK. REPLACED ENGINE DRIVEN FUEL PUMP , OPS CHECKED OK. 1 L 7 2 3T 4 T RT A28CE E4WE 1999100800247 19991008 00247 SW 1999 10 8 PNSA990902 1 19990910 A 7797 8974697 WIRE SWRNGN SA227 SA227AC 8780603 SW LT ENG EGT IND INTERMITTENT A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 640PA AC759B DURING CLIMB, LT ENGINE BEGAN TO BYPASS FUEL DUE TO ERRATIC EGT SIGNAL. REPLACED EGT CABLE OPS CHECK OK. 2 L 7 2 4T RT A8SW 1999100800248 19991008 00248 SW 1999 10 8 PNSA990903 1 19990919 A 5270 LIGHT SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR ILLUMINATED A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 41NE AC741B DURING CLIMB, CARGO DOOR LIGHT ILLUMINATED. AIRCRAFT DEPRESSURIZED REMAINED IN PATTERN AND MADE AN UNEVENTFUL LANDING. NO FAULTS WERE FOUND DOOR WAS RESECURED AND SUBSEQUENT FLIGHTS HAVE BEEN NORMAL. 2 L 7 2 4T RT A8SW 1999100800249 19991008 00249 EU 1999 10 8 PNSA990904 1 19990927 A 2750 8565M1 POTENSIOMETER SAAB SF340 340B 7860101 EU RT TE FLAP INTERMITTANT A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 675PA 206 CLIMBING THROUGH 7000 FT, FLAPS MOMENTARILY EXTENDED 3 TO 4 DEGREES AND IMMEDIATELY RETRACTED. AIRCRAFT RETURNED TO BAS E. REPLACED RT FLAP POTENSIOMETER. OPERATIONAL CHECK WAS OK. 2 L 7 2 4T RT A52EU 1999100800250 19991008 00250 NM 1999 10 8 RAAA99B1025 1 19991001 A 3350 873100212 LIGHT INTVLV BOEING 727 72722C 138400F NM ROW 12 DEF INOP. A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 EMERGENCY LIGHT AT ROW 12 D, E, F. WILL NOT TEST, REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999100800251 19991008 00251 SO 1999 10 8 RAAA99E8053 1 19991003 A 3350 86210144 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 12 AB DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY LIGHT AT ROW 12 A/B WILL NOT TEST, REPLACED BATTERY. 2 L 7 4 4T 4A22 1999100800252 19991008 00252 WP 1999 10 8 CALA9901317 1 19990930 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1497 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND VENTRAL STAIR LOWER EXTERNAL SKIN DENTED AT STA 1497, BL 0. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-30-2. 2 L 7 2 4F A6WE 1999100800253 19991008 00253 WP 1999 10 8 CALA9901318 1 19991001 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOORBOARD SUPPORT ANGLE CORRODED AT STA 160, RBL 10-RBL 44. THE SUPPORT ANGLE WAS REMOVED AND REPLACE D IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999100800254 19991008 00254 WP 1999 10 8 CALA9901319 1 19991001 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 256-1231 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 256, L22R, STA 490, L23L, AND STA 1231, L22R. THE DENTS WERE REFORMED IAW SRM 53-04, FIGURE 38. DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-30-2, 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999100800255 19991008 00255 WP 1999 10 8 CALA9901320 1 19991001 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND MID CARGO DOOR OUTER SKIN DENTED AT STA 674, L22R. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, 52 -33-2, FIGURE 1, 52-05, FIGURE 1, AND 52-01, FIGURE 7. 2 L 7 2 4F A6WE 1999100800256 19991008 00256 WP 1999 10 8 CALA9901321 1 19991003 A 3350 BR964412 LIGHT BRUCE DOUG DC10 DC1030 3023501 WP ROW 3B INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14074 46911 INSPECTION FOUND EMERGENCY ESCAPE LIGHT INOPERATIVE AT SEAT 3B IN PASSENGER CABIN. THE ESCAPE LIGHT ASSEMBLY WAS REMOVE D AND REPLACED IAW MM 33-50-00. 2 L 7 3 4F A22WE 1999100800257 19991008 00257 WP 1999 10 8 CALA9901322 1 19991004 A 2560 BATTERIES DOUG DC10 DC1030 3023501 WP MEGAPHONE DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14074 46911 INSPECTION FOUND TWO CABIN MEGAPHONES INOPERATIVE. THE MEGAPHONE BATTERIES WERE REMOVED AND REPLACED IAW MM 25-60-00. 2 L 7 3 4F A22WE 1999100800258 19991008 00258 WP 1999 10 8 CALA9901323 1 19991004 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 218-541 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FORWARD CARGO LT FLOORBOARD TRACK CORRODED FROM STA 218 TO 541, LBL 24. THE TRACK WAS REMOVED AND A NE W TRACK WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 4G. 2 L 7 2 4F A6WE 1999100800259 19991008 00259 WP 1999 10 8 CALA9901324 1 19991004 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOORBEAM CORRODED AT FS 1322, RBL 30 TO RBL 54. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTAL LED IAW SRM 53-05, FIGURE 20A AND 51-30-05. 2 L 7 2 4F A6WE 1999100800260 19991008 00260 WP 1999 10 8 CALA9901325 1 19991004 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOORBEAM ATTACH ANGLE CORRODED AT FS 1338, RBL 50. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS I NSTALLED IAW SRM 53-14-03, FIGURE 7, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999100800261 19991008 00261 WP 1999 10 8 CALA9901326 1 19991004 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1100-1308 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND CABIN CENTER SEAT TRACK CORRODED AT FS 1100-1174, RBL 22 AND OUTBOARD SEAT TRACK WAS CORRODED AT FS 121 2-1308, RBL 54.5. THE SEAT TRACK SECTIONS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-10-4, 51-30-2, 53-05, F IGURE 4F, 51-30-00, 51-30-5, AND 53-01, FIGURE 1. 2 L 7 2 4F A6WE 1999100800262 19991008 00262 SO 1999 10 8 COMA9910158 1 19991003 A 2752 320301007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 189CA 1720 1189 FLAP DISAGREEMENT WARNING WHEN 45 DEGREES SELECTED. REPLACED THE RIGHT OUTBOARD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1999100800263 19991008 00263 SO 1999 10 8 COMA9910159 1 19991002 A 5730 12041320031 SKIN EMB 120 EMB120RT SO FWD FUSELAGE DENTED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 258CA 1247 DENT IN NOSE SKIN P/N 120-41320-031. REMOVE AND REPLACE SKIN IAW AERODESIGN AIRCRAFT ENGINEERING, INC. REPORT 3444-1. 2 L 7 2 4T RT A31SO 1999100800264 19991008 00264 SO 1999 10 8 COMA9910160 1 19991002 A 5330 12015699001 SKIN EMB 120 EMB120RT SO WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 1247 CRACK IN WING LOWER SKIN PANEL P/N 120-15699-001 AT FUEL SERVICE DOOR APPROXIMATELY 2.0. REPAIR WITH SKIN DOUBLER IAE A ERODESIGN AIRCRAFT ENGINEERING, INC REPORT NR 990-2. 2 L 7 2 4T RT A31SO 1999100800265 19991008 00265 NM 1999 10 8 UPS99230824 1 19990924 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 970-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI WHILE WORKING 997342 FOUND CORROSION ON SEAT TRACK AT FLOORBOARD HOLES BS 970-1130 LBL 25. REMOVED S EAT TRACK FABRICATED REPLACEMENT SEAT TRACK AND INSTALLED PER SRM 51-30-5, 51-30-2 AND 53-10-5. 2 L 7 3 4F A3WE 1999100800266 19991008 00266 NM 1999 10 8 UPS99230825 1 19990823 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON BS 950 FLOORBEAM UPPER CHORD, LOWER SURFACE (FWD) AND UPPER SURFACE (AFT) CUT OUT DA MAGED FLOORBEAM, FABRICATED REPLACEMENT BEAM AND STRAPS PER ERO 99-6047A. 2 L 7 3 4F A3WE 1999100800267 19991008 00267 NM 1999 10 8 UPS99230826 1 19990823 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON BS 950 FLOORBEAM UPPER CHORD, LOWER SURFACE AT LBL 16. CUT OUT DAMAGED FLOORBEAM, FABRI CATED REPLACEMENT BEAM AND STRAPS PER ERO 99-6047A ***CPCP*** 2 L 7 3 4F A3WE 1999100800268 19991008 00268 NM 1999 10 8 UPS99230827 1 19990822 A 5347 BAC15201432 SEAT TRACK BOEING 727 72725C 138400H NM BS 782-798 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON SEAT TRACK AT BS 782 AND BS 798, RBL 45, WL 208. REMOVED CORRODED TRACK, FABRICATED AND INSTALLED SEAT TRACK PER SRM 51-30-2, 51-10-2, 51-30-5 AND 53-10-5. 2 L 7 3 4F A3WE 1999100800269 19991008 00269 NM 1999 10 8 UPS99230828 1 19990822 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 360-380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON SEAT TRACK BETWEEN BS 360-380, LBL 65, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED SEAT TRACK, INSTALLED NEW SEAT TRACK PER SRM 51-30-2, SRM 51-30-2, AND SRM 51-10-2. 2 L 7 3 4F A3WE 1999100800270 19991008 00270 NM 1999 10 8 UPS99230829 1 19990827 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI RBL 25 SEAT TRACK CRACKED BS 870 WL 208. REMOVED SEAT TRACK BS 870 TO 950 FABRICATED REPLACEMENT SEA T TRACK AND INSTALLED PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999100800271 19991008 00271 NM 1999 10 8 UPS99230830 1 19990820 A 5711 SPAR CHORD BOEING 727 72725C 138400H NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION C57-581-03.00E-02 ON R/W AFT UPPER SPAR CHORD AT WBL 85.0. REMOVED DAMAGED SECTION OF CHOR D INSTALLED NEW SECTION OF REAR SPAR CHORD IAW ER NR 99-6007. 2 L 7 3 4F A3WE 1999100800272 19991008 00272 WP 1999 10 8 UPS99830831 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 347.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS347.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800273 19991008 00273 WP 1999 10 8 UPS99830832 1 19990915 A 5320 56412521 DOUBLER DOUG DC8 DC871F 302199D WP WS 305 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E LWR SKIN DOUBLER AT STA XFS 305 IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED A ND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-20. 2 L 7 4 4F RT 4A25 1999100800274 19991008 00274 WP 1999 10 8 UPS99830833 1 19990912 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS628.75 2 FWD OD THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999100800275 19991008 00275 WP 1999 10 8 UPS99830834 1 19990929 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS340 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800276 19991008 00276 WP 1999 10 8 UPS99830835 1 19990915 A 5320 5615374105 DOUBLER DOUG DC8 DC871F 302199D WP BS 1460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 STA 1460 LONG 31L FINGER DOUBLER IS CORRODED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5615374. 2 L 7 4 4F RT 4A25 1999100800277 19991008 00277 WP 1999 10 8 UPS99830836 1 19990912 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 591.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS591.25, 2 FWD OF THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2- 1 FIG 38. 2 L 7 4 4F RT 4A25 1999100800278 19991008 00278 WP 1999 10 8 UPS99830837 1 19990912 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 307 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS307.0 AT THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38 . 2 L 7 4 4F RT 4A25 1999100800279 19991008 00279 WP 1999 10 8 UPS99830838 1 19990907 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C1 BATHTUB FITTING AT FS 860 L3L CRACKED. REMOVED LONG END FITTING STA 860 L3L RECEIVED NEW FITTING PN 3779659 -501 LOCATED DRILLED AND DEBURIED IAW DC8 SRM 51-1-24. INSTALLED FITTING AT 860 STA L3L IAW DC8 SRM 51-3-00. 2 L 7 4 4F RT 4A25 1999100800280 19991008 00280 EU 1999 10 8 QXEA9902008 1 19991003 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 BOI - EMERGENCY EXIT SIGN ABOVE FLIGHT COMPARTMENT ENTERANCE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999100800281 19991008 00281 NM 1999 10 8 99FDEA00403 1 19990803 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1030 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 303 DENT IN BELLFRAME TOP FLANGE BS 1030 ABOVE STR 26L AFT CARGO. CUT OUT DAMAGED AREA AND INSTALL DOUBLER PER SRM 5 1-30-02. 2 L 7 3 4F A3WE 1999100800282 19991008 00282 NM 1999 10 8 99FDEA00404 1 19990914 A 5311 FRAME BOEING 727 72722 1384002 NM BS 760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 546 - CRACK IN BELLFRAME BS 760 AT STR 5R. CUT OUT CRACK AREA AND INSTALL .080 DOUBLER ALL PER SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 1999100800283 19991008 00283 NM 1999 10 8 99FDEA00405 1 19990914 A 5311 FRAME BOEING 727 72722 1384002 NM BS 822 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 543, CRACK IN BELLFRAME BS 822 AT STR 5R. CUT OUT CRACKED AREA AND INSTALL .090 DOUBLER ALL PER 53-10-4 FIG 2. 2 L 7 3 4F A3WE 1999100800284 19991008 00284 NM 1999 10 8 99FDEA00406 1 19990914 A 5312 BULKHEAD BOEING 727 72722 1384002 NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 379, CRACK IN 1183 BULKHEAD LT DOOR FRAME WEB AT WL 263. INSTALLED NEW BEAM SECTION AND SPLICED PER EA 7532045307 DA TED 7/16/99 AND SB 727-53-210. 2 L 7 3 4F A3WE 1999100800285 19991008 00285 NM 1999 10 8 99FDEA00407 1 19990823 A 5320 SUPPORT BOEING 727 72722 1384002 NM BS 1195 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 230 - AFT AIRSTAIR COMPT, HORSE COLLAR SUPPORT RT CASTING IS CRACKED 2 OUT FROM RADIUS BLOCK JUST BELOW SEALING WEB B S 1195. INSTALL BATHTUB FITTING REPAIR ON HORSE COLLAR PER EA 7551045356 AUG 10, 1999. 2 L 7 3 4F A3WE 1999100800286 19991008 00286 NM 1999 10 8 99FDEA00408 1 19990914 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 680 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 522, STR 4L DAMAGED O/B SIDE BS 680 4 GOUGES IN 3 SECTION, 1 GOUGE THROUGH STR. REPAIR STR PER SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1999100800287 19991008 00287 NM 1999 10 8 99FDEA00409 1 19990810 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1010 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 299 - CRACKS IN LWR AFT FLANGE OF BELLFRAME AT FASTENERS ON STR 25L AT BS 1010. REMOVED DAMAGED FLANGE PER SRM 51-40 -3. TREATED AND PRIMED REMAIN FLANGE PER MM 51-20-00. INSTALL LWR FLANGE DOUBLER PER SRM 51-40-03. 2 L 7 3 4F A3WE 1999100800288 19991008 00288 NM 1999 10 8 99FDEA00410 1 19990806 A 5311 FRAME BOEING 727 72722 1384002 NM BS 990 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 297, CRACK ON LWR AFT FLANGE OF BELLFRAME AT FASTENER BS 990, STR 25L AFT CARGO. REMOVED DAMAGED FLANGE AND INSTALL DOUBLER PER EA 7531045346. 2 L 7 3 4F A3WE 1999100800289 19991008 00289 NM 1999 10 8 99FDEA00411 1 19990914 A 5311 FRAME BOEING 727 72722 1384002 NM BS 804 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 544, BS 804, STR 5R FRAME HAS VISUAL IND OF CRACK AT STR ATTACH RIVETS. CONFIRMED CRACK WITH DYE PENATRANT. REMOVED (CUTOUT) DAMAGED AREA. INSTALL REPAIR ANGLE PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999100800290 19991008 00290 WP 1999 10 8 99FDEA00412 1 19991001 A 5753 BRACKET DOUG DC10 DC1010 3022110 WP RT TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 390FE 46624 RT WING O/B FLAP POS XMITTER CABLE PULLEY BRACKET IS SAWED-OFF AT XORS 405, FWD OF I/B AILERON O/B HINGE ATTACH AND GUID E PULLEY PIN MISSING. REMOVED AND REPLACED IAW AMM 27-51-07. 2 L 7 3 4F A22WE 1999100800291 19991008 00291 NM 1999 10 8 99FDEA00413 1 19990914 A 5312 BULKHEAD BOEING 727 72722 1384002 NM BS 348 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 991 - CORROSION ON BULKHEAD BS 348 IN NOSE W/W IN AREA OF DRAG BRACE FITTING. REMOVED AND REPLACED PER EA 7-5310-453 69 DATED AUG 16, 1999. 2 L 7 3 4F A3WE 1999100800292 19991008 00292 NM 1999 10 8 99FDEA00414 1 19990914 A 5311 FRAME BOEING 727 72722 1384002 NM BS 333 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 NR 991, CORROSION ON BELTFRAME EXTRUSION BS 333 AT LT SKATE ANGLE. CUT OUT DAMAGE AND INSTALLED REPAIR PER DRAWING 65C 15724. 2 L 7 3 4F A3WE 1999100800293 19991008 00293 NM 1999 10 8 99UAL900450 1 19990825 A 3520 MASK BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN DROPED A UALA K NONE O OTHER LD LANDING 1 WP 29 163UA 21353 SEVERAL O2 MASKS DROPPED ON LANDING. CAUSE WAS LIKELY A HARD LANDING. MASKS WERE REPACKED AFTER LANDING. THIS HAS NO SAFETY IMPACT. THE OXYGEN SYSTEM WILL STILL PROVIDE OXYGEN TO ALL PASSENGERS IF SYSTEM IS ACTIVATED. 2 L 7 4 4F 4 F A20WE E20EA 1999100800294 19991008 00294 NM 1999 10 8 99UAL900489 1 19990926 A 2781 SWITCH BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 LE SLAT FAILED A UALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 29 939UA 26672 DURING TAKEOFF, THE NUMBER TWO LEADING EDGE SLAT IN TRANSIT LIGHT INTERMITTENTLY ILLUMINATED ON THE FORWARD AND OVERHEAD PANELS. WHEN SPEED WAS REDUCED, THE IN TRANSIT LIGHT DISTINGUISHED. THE WIRING TO THE NUMBER TWO LEADING EDGE ROD END SWITCH WAS REPAIRED. OPERATIONAL CHECK CONDUCTED, NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999100800295 19991008 00295 NM 1999 10 8 99UAL900491 1 19990924 A 2910 1559A990001 O RING AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE GREEN HYD SYS FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 822UA 948 ECAM GREEN HYDRAULIC LOW QUANTITY FL 370 CRUISE. *S/D* FOUND STRONG LEAK ON GREEN HP MANIFOLD PRESSURE LINE. REPLACED O-RING, CKD FOR LEAKS THROUGHOUT AREA AND NO LEAKS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 1999100800296 19991008 00296 NM 1999 10 8 99UAL900492 1 19990927 A 2611 47310802 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO COMPT MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 506UA 24627 LANDED AT ORD UNDER AMBER ALERT DUE TO A FIRE WARNING IN THE AFT PIT. *S/D* THE CAUSE OF THE INTERMITTENT FIRE ALARM F OR THE AFT CARGO COMPARTMENT WAS DUE TO A DEFECTIVE AFT CARGO SMOKE DETECTOR INSTALLED IN THE NUMBER 2 POSITION. THIS U NIT WAS SUBSEQUENTLY REPLACED BY A NEW UNIT. SINCE THE REPLACEMENT OF THE NEW UNIT, NO FALSE FIRE ALARMS HAVE BEEN GENE RATED OR REPORTED. THE REPAIR FACILITY (WALTER KIDDE AEROSPACE) ACCOMPLISHING THE TEST/REPAIR ON UNIT 473108-02 (S/N 12 13) FOUND INTERMITTENT ALARM OUTPUT DURING VIBRATION TESTING. THE INTERNAL WIRE HARNESS ASSY WAS FOUND TO BE AT FAULT. 2 L 7 2 4F 4 F RT A2NM E17NE 1999100800297 19991008 00297 NM 1999 10 8 99UAL900493 1 19990927 A 3350 6013211LB BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7260U 21407 EMERGENCY LIGHT AT DOOR 2R INOPERATIVE. *S/D* REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1999100800298 19991008 00298 NM 1999 10 8 99UAL900494 1 19990927 A 4940 5198587 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU DEFECTIVE A UALA A UNSCHED LANDING H J K ELECT. POWER LOSS-50 PC WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 29 652UA 25390 61739 APU AUTO SHUTDOWN WITH 'APU OIL QTY' EICAS MSG DISPLAYED. DIVERTED TO ASU . *S/D* APU STARTER WAS FOUND LEAKING WHICH CAUSED THE LOP SHUTDOWN. REPLACED APU STARTER PER ENGINEER'S UPDATE. ALSO, REPLACED GEARBOX SHUTOFF VALVE AS A PRECAU TIONARY ACTION. SERVICED APU WITH OIL AND TESTED OK WITH NO FURTHER LEAKS AND OPERATION BACK TO NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100800299 19991008 00299 NM 1999 10 8 99UAL900495 1 19990928 A 2611 47310802 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO COMPT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 506UA 24627 RETURNED TO FIELD DUE TO A FIRE WARNING LIGHT. *S/D* THE CAUSE OF THE INTERMITTENT FIRE ALARM FOR THE AFT CARGO COMPAR TMENT WAS DUE TO A DEFECTIVE AFT CARGO SMOKE DETECTOR INSTALLED IN THE NR 2 POSITION. THIS UNIT WAS SUBSEQUENTLY REPLAC ED BY A NEW UNIT. SINCE THE REPLACEMENT OF THE NEW UNIT, NO FALSE FIRE ALARMS HAVE BEEN GENERATED OR REPORTED. THE REP AIR FACILITY (WALTER KIDDE AEROSPACE) ACCOMPLISHING THE TEST/REPAIR ON UNIT 473108-02 (S/N 1213) FOUND INTERMITTENT ALAR M OUTPUT DURING VIBRATION TESTING. THE INTERNAL WIRE HARNESS ASSY WAS FOUND TO BE AT FAULT. 2 L 7 2 4F 4 F RT A2NM E17NE 1999100800300 19991008 00300 NM 1999 10 8 99UAL900496 1 19990927 A 2750 RETRACT MECH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 WP 29 652UA 25390 ON FLAP RETRACTION DURING TAKEOFF (FLAPS 5), WHEN FLAPS 1 WAS CALLED FOR FLAPS STUCK AT ABOUT 3.5 DEG. TE FLAP DISAGREE EICAS MESSAGE WITH MASTER CAUTION PROCEDURE ON 7-43 WAS ACCOMPLISHED PER FLIGHT MANUAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100800301 19991008 00301 NM 1999 10 8 99UAL900497 1 19990930 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE ROW 15 INOP A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 903UA 25003 THE EMERGENCY EGRESS LIGHTS FROM ROW 15 BACK ARE INOPERATIVE. REPLACED THE EMERGENCY EGRESS LIGHTS. OPERATIONS CHECK N ORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999100800302 19991008 00302 NM 1999 10 8 99UAL900498 1 19990929 A 2820 TRANSFER SYS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT&RT WING MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 320UA 23952 DURING CRUISE, THE RIGHT WING FUEL TANK INCREASED 1000 NR WITH PROPORTIONAL LEFT WING DECREASE. ON DOWN WIND AND FINAL LEG, THE RIGHT WING FUEL TANK INCREASED 1100 NR WITH PROPORTIONAL LEFT WING DECREASE. OPENED THE FUEL TANKS AND CHECK ED THE VENT FLOAT VALVES. VALVES CHECKED GOOD. CONDUCTED MANIFOLD PRESSURE CHECK WITH THE CROSS-FEED VALVE CLOSED. NO LEAKS THROUGH THE CROSS-FEED VALVE. NOT ABLE TO DUPLICATE OCCURRENCE ON GROUND. 2 L 7 2 4F 4 F RT A16WE E2GL 1999100800303 19991008 00303 NM 1999 10 8 99UAL900499 1 19990927 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 312 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7279U 21557 FUSELAGE SKIN AFT OF FORWARD LAVATORY SERVICE PANEL FOUND WITH CRACKS AROUND AREA FASTENERS DUE TO CORROSION. 2024-T3 O .O40 INCH FUSELAGE SKIN AT STATION 312 RT SIDE, BETWEEN STRINGERS S-19 AND S-21 CORRODED. UNDERLYING BEAR STRAP, FRAME AND STRINGERS NOT AFFECTED. CORROSION DOES NOT AFFECT LAP JOINT AT STRINGER S-19. SUSPECT CAUSE OF CORROSION DUE TO LA VATORY FLUID CONTAMINATION. AFFECTED FUSELAGE SKIN REMOVED BETWEEN STATIONS 305 AND 319, BETWEEN STRINGERS S-19 AND S-2 1, APPROXIMATE SKIN AREA 152 INCHES SQUARE. LOCAL CORROSION REMOVED AND EXTERNAL SKIN DOUBLER AND TRIPLER INSTALLED PER SRM 53-30-3, FIGURE 3 REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 1999100800304 19991008 00304 NM 1999 10 8 99UAL900500 1 19990929 A 2431 OVER HEAT LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BATTERY COMPT ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 777UA 26916 EN ROUTE ORD-LHR, MAIN BATTERY OVERHEAT MESSAGE. DIVERTED TO IAD. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999100800305 19991008 00305 1999 10 8 MWEA99641 4 19990929 A 3421 2587335113 VERTICAL GYRO DOUG DC9 DC981 3022081 WP RIGHT MALFUNCTIONED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 810ME 48072 HORIZON COMPARATOR ILLUMINATED IMMEDIATELY AFTER TAKEOFF 6 DEGREES DIFFERENCE BETWEEN THE FO'S PRIMARY FLIGHT DISPLAY ND CAPT'S AND STANDBY. REPLACED VERTICAL GYRO. 2 L 7 2 4F A6WE 1999100800306 19991008 00306 WP 1999 10 8 MWEA99642 1 19991003 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 204ME 47680 THE GALLEY DOOR E. MAINTENANCE REATTACHED EMERGENCY DOOR GIRT BAR. 2 L 7 2 4F A6WE 1999100800307 19991008 00307 WP 1999 10 8 MWEA99643 1 19991004 A 2560 113317 LAYNARD DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 301ME 47190 GALLEY DOOR SLIDE COVER MISSING ATTATCHING PIN AT BOTTOM. REINSTALLED EVAC SLIDE LANYARD. 2 L 7 2 4F A6WE 1999100800308 19991008 00308 WP 1999 10 8 MWEA99644 1 19991002 A 3260 4916970502 STRIKER DOUG DC9 DC932 3022066 WP RT MLG DEFECTIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 209ME 47730 RIGHT MAIN GEAR (RED) UNSAFE LIGHT STAYS ILLUMINATED WITH GEAR RETRACTE. REPLACED MAIN GEAR UPLATCH MECHANISM AND STRIK ER ASSEMBLY. 2 L 7 2 4F A6WE 1999100800309 19991008 00309 WP 1999 10 8 RAIA9909022 2 19990924 A 7310 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 859AE 859 66121 4705- PSP - RIGHT ENGINE FUEL FLOW ERRATIC DURING TTL TEST. MAINTENANCE REPLACED FUEL BYPASS VALVE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999100800310 19991008 00310 EU 1999 10 8 RAIA9910006 1 19991005 A 5310 HL18PB610 STRUCTURE BAG JETSTM JETSTM3201 1500217 EU BS 199 MISDRILLED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 433AM 885 MX- STL - SKIN AND FRAME AT STATION 199 ON RIGHT SIDE OF AIRCRAFT WAS MISDRILLED DURING A LOCAL REPAIR. 2 L 7 2 4T RT A56EU 1999100800311 19991008 00311 EU 1999 10 8 SIMA992253 1 19990813 A 5311 S5317221920601 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 233RM 235 SAW - A/C STRUCK BY GPU THAT BECAME DISCONNECTED FROM A TUG. THE RIGHT OF THE FUSLAGE AT FRAME 12 AND STRINGER 13 WAS T ORN APPROX 8 INCHES IN LENGTH. REPAIRED FRAME 12 IAW 53-11-40 AND 51-25-02. REMOVED AND REPLACED STRINGER 13 SPLICE AN D INTERCOSTAL IAW SRM 51-25-02. REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 408. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100800312 19991008 00312 EU 1999 10 8 99ZZZM695 1 19990813 A 5313 S5307020421601 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 233RM 235 SAW - A/C STRUCK BY GPU THAT BECAME DISCONNECTED FROM A TUG. THE RIGHT OF THE FUSLAGE AT FRAME 12 AND STRINGER 13 WAS T ORN APPROX 8 INCHES IN LENGTH. REPAIRED FRAME 12 IAW 53-11-40 AND 51-25-02. REMOVED AND REPLACED STRINGER 13 SPLICE AN D INTERCOSTAL IAW SRM 51-25-02. REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 408. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100800313 19991008 00313 EU 1999 10 8 99ZZZM696 1 19990813 A 5320 S5317071320900 INTERCOSTAL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 233RM 235 SAW - A/C STRUCK BY GPU THAT BECAME DISCONNECTED FROM A TUG. THE RIGHT OF THE FUSLAGE AT FRAME 12 AND STRINGER 13 WAS T ORN APPROX 8 INCHES IN LENGTH. REPAIRED FRAME 12 IAW 53-11-40 AND 51-25-02. REMOVED AND REPLACED STRINGER 13 SPLICE AN D INTERCOSTAL IAW SRM 51-25-02. REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 408. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100800314 19991008 00314 EU 1999 10 8 99ZZZM697 1 19990813 A 5313 S5317220120805 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE TORN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 233RM 235 SAW - A/C STRUCK BY GPU THAT BECAME DISCONNECTED FROM A TUG. THE RIGHT OF THE FUSLAGE AT FRAME 12 AND STRINGER 13 WAS T ORN APPROX 8 INCHES IN LENGTH. REPAIRED FRAME 12 IAW 53-11-40 AND 51-25-02. REMOVED AND REPLACED STRINGER 13 SPLICE AN D INTERCOSTAL IAW SRM 51-25-02. REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 408. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999100800315 19991008 00315 NM 1999 10 8 AALA991137 1 19990803 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 182AN 29592 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT 2L LAVATORY INOPERATIVE. RESECURED CONNECT OR TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT 2L LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999100800316 19991008 00316 EA 1999 10 8 ASOA99080 1 19990815 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 838AS 7276 DURING INSPECTION, NR 2 EMERGENCY LIGHTING SYSTEM BATTERY PACK FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGEN CY LIGHTING SYSTEM BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999100800317 19991008 00317 WP 1999 10 8 GTIA9900936 1 19990614 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 DTW - EMERGENCY LIGHT PASSENGER OVERHEAD SOME BURN OUT. ALSO, TAIL COMPARTMENT LENS MISSING ON LIGHT. TAIL COMPARTMENT EMERGENCY RAMP LIGHT. EMERGENCY LIGHT AND LENS REPLACED IAW MD 82/83 MM 33-00-50. (M) 2 L 7 2 4F RT A6WE 1999100800318 19991008 00318 WP 1999 10 8 GTIA9901076 1 19990811 A 3350 LIGHT DOUG DC9 DC981 3022081 WP ROW 10-20 INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 981SB 48058 LGA - FLT 720 - EMERGENCY FLOOR LIGHTING NOT ILLUMINATING ON SOME AREA. FOUND LIGHTS INOPERATIVE AT ROW 10-20. TROUBLE SHOT AND FOUND WIRE PINCHED AT ROW 20. REPOSITIONED SAME IN CHANNEL. LIGHT OPERATION AND CHECKS OK IAW MM 33-50-00. ( M) 2 L 7 2 4F A6WE 1999100800319 19991008 00319 CE 1999 10 8 MASA99144 1 19990819 A 2120 AIR DIST BEECH 1900 1900D 1154162 CE COCKPIT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 76ZV UE76 FLT 5756 - PHL-STL - ON TAXI INTO STL, THE CAPTAIN REPORTED A FUEL SMELL IN THE COCKPIT WHEN THE ENVIRONMENT WAS ON. (M ) 2 L 7 2 4T RT A24CE 1999100800320 19991008 00320 SO 1999 10 8 99ZZZM698 1 19990823 A 3610 S2D226 O-RING EMB 145 EMB145LR SO NR 2 ENGINE DUCT FAILED A SIMA F D O ACTIVATE FIRE EXT. RETURN TO BLOCK OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 628AE 145124 DURING CRUISE, AT 20,000 FEET, THE NR 2 BLEED WARNING LIGHT CAME ON. MINUTES LATER THE BAGGAGE COMPARTMENT SMOKE DETECT OR ILLUMINATED, PROCEEDED TO ACTIVATE THE COMPARTMENT FIRE EXTINGUISHER. RETURNED TO INDIANAPOLIS WITHOUT FURTHER INCID ENT. FOUND THE NR 2 ENGINE PNEUMATIC DUCT LOOSE AT THE AFT RIGHT BAGGAGE COMPARTMENT ACCESS PANEL. REPLACED THE O-RING S, RESECURED THE DUCT AND NO LEAKS NOTED AT THIS TIME, OK FOR SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999100800321 19991008 00321 NM 1999 10 8 F3LA99120 1 19990905 A 3350 LIGHT BOEING 737 7372Y5 1384554 NM PAX DOORWAY INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 921WA 23039 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED F ORWARD ENTRY DOOR EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4U RT A16WE 1999100800322 19991008 00322 CE 1999 10 8 99ZZZM699 1 19990910 A 7920 330997F120290 HOSE BEECH 1900 1900D 1154162 CE LT ENGINE CHAFED A JJBA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 01 833CA UE24 EN ROUTE BETWEEN PLB AND IAD, ON A REPOSITION FLIGHT, LEFT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. UPON FURTHER OBSERVA NCE BY CREW OIL PRESSURE ANNUNCIATOR BEGAN FLASHING, AT WHICK TIME ENGINE WAS SHUT DOWN AND AIRCRAFT DIVERTED TO ABL. L EFT ENGINE OIL LINE HOSE ASSEMBLY TO OIL COOLER WAS FOUND CHAFFED AND REPLACED IAW RAYTHEON MM CHAPTER 79. OPERATIONAL LEAK CHECK AND GROUND PERFORMANCE RUN OF ENGINE SATISFACTORY IAW APPROVED WORK CARDS. (M) 2 L 7 2 4T RT A24CE 1999100800323 19991008 00323 NM 1999 10 8 P2EA99264 1 19990822 A 5330 SKIN BOEING 737 737247 138448D NM BS 540 LIGHTNING STRIKE A P2EA K NONE C F.O.D. IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LIGHTNING STRIKE AT BS 540 BETWEEN STRINGERS 4L AND 5L. REPAIRED SKIN IAW SRM 53-30-3 FIG 28. (M) 2 L 7 2 4F A16WE 1999100800324 19991008 00324 NM 1999 10 8 P2EA99263 1 19990823 A 5347 SEAT TRACK BOEING 737 737247 138448D NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SEAT TRACK WEB CRACKED AT BS 706 AND BS 727 BETWEEN WL 203.1 AND 208.1. REPAIRED IAW COOPESA EO COO-SJO-3-53-500- 98. (M) 2 L 7 2 4F A16WE 1999100800325 19991008 00325 NM 1999 10 8 P2EA99262 1 19990823 A 5315 FLOORBEAM BOEING 737 737247 138448D NM BS 360 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FLOORBEAM DAMAGED AT BS 360, WL 208 AND BETWEEN RBL 24 AND RBL 60. REPAIRED IAW SRM 53-10-9 FIG 1. (M) 2 L 7 2 4F A16WE 1999100800326 19991008 00326 NM 1999 10 8 P2EA99261 1 19990824 A 5313 STRINGER BOEING 737 737247 138448D NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - STRINGER 14L CRACKED AT BS 360. REPLACED STRINGER FROM BS 352 TO 372 IAW SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999100800327 19991008 00327 NM 1999 10 8 P2EA99260 1 19990824 A 5313 STRINGER BOEING 737 737247 138448D NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - STRINGER 15L CRACKED AT BS 360. REPLACED STRINGER SECTION FROM BS 352 TO 372 IAW SRM 51-10-0 PAGE 5. (M) 2 L 7 2 4F A16WE 1999100800328 19991008 00328 NM 1999 10 8 P2EA99259 1 19990825 A 5730 SKIN BOEING 737 737247 138448D NM LT WING CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LEFT WING FUEL TANK LOWER SKIN AT WBL 75.85 HAS CORROSION. REWORKED SKIN IAW COOPESA EO 3-57-509-99. (M) 2 L 7 2 4F A16WE 1999100800329 19991008 00329 NM 1999 10 8 P2EA99258 1 19990829 A 5313 STRINGER BOEING 737 737247 138448D NM BS 1078-1083 WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - STRINGER 22R WORN TO LIMITS BETWEEN BS 1078 AND 1083. REPLACED SECTION ON STRINGER FROM BS 1071.750 TO 1083.250 I AW SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999100800330 19991008 00330 NM 1999 10 8 P2EA99257 1 19990901 A 5313 STRINGER BOEING 737 737247 138448D NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - STRINGER 10L AT BS 727B CRACKED. REPAIRED IAW SRM 53-10-3 FIG 3. (M) 2 L 7 2 4F A16WE 1999100800331 19991008 00331 NM 1999 10 8 P2EA99256 1 19990829 A 5320 65210814 FRAME BOEING 737 737247 138448D NM RT EMER EXIT CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - RIGHT EMERGENCY EXIT HATCH OPENING MECHANISM CRACKED. REPLACED FRAME ASSEMBLY IAW SRM 51-10-0 PAGE 5 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1999100800332 19991008 00332 NM 1999 10 8 P2EA99255 1 19990824 A 5230 SKIN BOEING 737 737247 138448D NM CARGO DOOR MISREPAIRED A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FORWARD CARGO DOOR INNER SKIN REPAIR NOT PER SRM. REPAIRED IAW SRM 51-40-2 FIG 1. (M) 2 L 7 2 4F A16WE 1999100800333 19991008 00333 NM 1999 10 8 P2EA99254 1 19990824 A 5311 FRAME BOEING 737 737247 138448D NM BS 907 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FRAME CRACKED AT BS 907 BETWEEN STRINGER 16L AND 17L. REPAIRED IAW SRM 51-40-3 FIG 3. (M) 2 L 7 2 4F A16WE 1999100800334 19991008 00334 NM 1999 10 8 P2EA99253 1 19991005 A 2120 SKIN BOEING 737 737281 138448P NM RAM DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, LEFT RAM DOOR INNER SKIN CRACKED, DEFECT SIZE, LENGTH 3 INCHES AND WIDTH 1 INCH. REPAIRED RAM DOOR INTER NAL SKIN PER COOPESA EO COO-3-52-708-99 DATED DECEMBER 4, 1999. (M) 2 L 7 2 4F A16WE 1999100800335 19991008 00335 NM 1999 10 8 P2EA99252 1 19990822 A 5320 RIVETS BOEING 737 737247 138448D NM BS 1138-1156 LOOSE A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LOOSE RIVETS FROM BS 1138 TO BS 1156, STRINGER 11R AND 12R. TORQUE BOX DAMAGED AT SAME LOCATION. REPAIRED TORQUE BOX IAW SRM 51-40-2 FIGURE 1 AND REPLACED RIVETS IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999100800336 19991008 00336 NM 1999 10 8 P2EA99251 1 19990824 A 5310 STRUCTURE BOEING 737 737247 138448D NM BS 277 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FOUND CORROSION IN NOSE GEAR WHEEL WELL AT BS 277, WL 193, LBL 11. REPAIRED IAW SRM 51-10-02 PAGE 5. (M) 2 L 7 2 4F A16WE 1999100800337 19991008 00337 NM 1999 10 8 P2EA99250 1 19990822 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - BULKHEAD WEB CRACKED AT BS 178, RBL 15, WL 218. REPAIRED IAW SRM 53-10-11 FIG 1. (M) 2 L 7 2 4F A16WE 1999100800338 19991008 00338 NM 1999 10 8 P2EA99249 1 19990822 A 5311 FRAME BOEING 737 737247 138448D NM BS 460 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FRAME LOWER FLANGE CRACKED IN FORWARD CARGO AT BS 460 BETWEEN STRINGERS 28L AND 28R. REPAIRED FRAME IAW SRM 51-40 -03 FIG 1. (M) 2 L 7 2 4F A16WE 1999100800339 19991008 00339 NM 1999 10 8 P2EA99246 1 19990822 A 5330 SKIN BOEING 737 737247 138448D NM BS 860 LIGHTNING STRIKE A P2EA K NONE C F.O.D. IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LIGHTNING STRIKE AT BS 860, STRINGER 6L. REPAIRED IAW SRM 53-30-03 FIG 23. (M) 2 L 7 2 4F A16WE 1999100800340 19991008 00340 NM 1999 10 8 P2EA99247 1 19990822 A 5330 SKIN BOEING 737 737247 138448D NM BS 365 LIGHTNING STRIKE A P2EA K NONE C F.O.D. IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LIGHTNING STRIKE AT BS 365 STRINGER 5L. REPAIRED IAW SRM 53-30-03 FIG 23. (M) 2 L 7 2 4F A16WE 1999100800341 19991008 00341 NM 1999 10 8 P2EA99248 1 19990822 A 5330 SKIN BOEING 737 737247 138448D NM BS 755 LIGHTNING STRIKE A P2EA K NONE C F.O.D. IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LIGHTNING STRIKE AT BS 755 STRINGER 5L. REPAIRED IAW SRM 53-30-03 FIG 23. (M) 2 L 7 2 4F A16WE 1999100800342 19991008 00342 NM 1999 10 8 P2EA99244 1 19990823 A 5320 FRAME BOEING 737 737247 138448D NM BS 578 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FRAME ANGLE CRACKED AT BS 578 BETWEEN WL 208.1 AND WL 204.1 AT STRINGER 17R. REPLACED FRAME ANGLE IAW SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999100800343 19991008 00343 NM 1999 10 8 P2EA99241 1 19990821 A 5311 FRAME BOEING 737 737247 138448D NM BS 807 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - AFT CARGO COMPARTMENT FRAME BS 807, BETWEEN STRINGER 27R AND 26L HAS CORROSION, LENGTH 2 INCHES, WIDTH 1 INCH, DEP TH .025 INCH. FRAME REPAIRED AT BS 807 BETWEEN STRINGER 26L AND 27L PER SRM 53-10-3 FIG 7. ALL OTHER AREAS CORROSION W AS REMOVED AND FOUND WITHIN LIMITS AND TREATED PER SRM 51-10-6. (M) 2 L 7 2 4F A16WE 1999100800344 19991008 00344 SO 1999 10 8 C2XA99IA472 1 19990908 A 2150 8152403 ACM EMB 145 EMB145 SO NR 2 INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 09 16963 145116 FLT 4205 - GSP-IAH - THE CREW REPORTED A SMOKE SMELL IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MA INTENANCE REMOVED AND REPLACED THE NR 2 AIR CYCLE MACHINE IAW EMB145 MM 21-51-03, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800345 19991008 00345 SO 1999 10 8 C2XA99IA471 1 19990909 A 3350 GE1317 BULB EMB 145 EMB145ER SO RT EMER EXIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14943 145040 IAH - DURING C-CHECK INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800346 19991008 00346 SO 1999 10 8 C2XA99IA470 1 19990909 A 5530 14531597601 ANGLE EMB 145 EMB145ER SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14943 145040 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC533 0-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800347 19991008 00347 SO 1999 10 8 C2XA99IA469 1 19990909 A 5530 14531597602 ANGLE EMB 145 EMB145ER SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14943 145040 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC53 30-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800348 19991008 00348 SO 1999 10 8 C2XA99IA468 1 19990909 A 3350 7287550501 LIGHT EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14943 145040 IAH - DURING C-CHECK INSPECTION, THE NR 7 EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED AISLE PATH LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800349 19991008 00349 SO 1999 10 8 C2XA99IA467 1 19990913 A 3350 3025101 LIGHT ASSEMBLY EMB 145 EMB145ER SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14943 145040 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT EXTERNAL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB-145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800350 19991008 00350 SO 1999 10 8 C2XA99IA466 1 19990911 A 3350 C36601100 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING MAINTENANCE INSPECTION, THE REAR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 L 7 2 4T RT A31SO 1999100800351 19991008 00351 SO 1999 10 8 C2XA99IA465 1 19990909 A 7830 TY203905B ACTUATOR EMB 145 EMB145ER SO LT ENGINE BROKEN A C2XA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 14937 145026 EFD - FLT 938A - THE CREW REPORTED ENGINE ONE REVERSER DISAGREE, ENGINE ONE REVERSER FAIL, NR 1 REVERSER LEVER INOPERATI VE DURING TAXI, AND THE NR 1 UPPER THRUST REVERSER BUCKET WAS FOUND TO BE OPEN ON ENGINE SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRUST REVERSER ACTUATOR IAW EMB145MM 78-32-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800352 19991008 00352 SO 1999 10 8 C2XA99IA464 1 19990908 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 1 FOUR EMERGENCY EXIT LIGHT BATTERY PACK WAS INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800353 19991008 00353 SO 1999 10 8 C2XA99IA463 1 19990904 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO ROW 12 DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 IAH - DURING PREFLIGHT INSPECTION AT EWR, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS AT ROW 12 WERE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB145MM 33-50-08, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999100800354 19991008 00354 EU 1999 10 8 C2XA99BT089 1 19990915 A 3350 167006 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 BTV - FLT 3680 - DURING 1A INSPECTION, MAINTENANCE FOUND HALF OF THE AFT AISLE PATH EMERGENCY LIGHTS ARE INOPERATIVE WHE N ON 'POWER SUPPLY', BREAKER PULLED. REPAIRED BROKEN WIRING AND REPLACED LIGHT BULBS. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999100800355 19991008 00355 EU 1999 10 8 C2XA99BT088 1 19990915 A 3350 BULB AEROSP ATR42 ATR42300 8680920 EU PAX DOORWAY LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 BTV - FLT 3680 - DURING 1A INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT IN PASSENGER DOOR INOPERATIVE IN ALL MODES. RE POSITIONED BULB IN SOCKET AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999100800356 19991008 00356 NM 1999 10 8 99ZZZM700 1 19990825 A 3411 410740130 HOSE BOEING 757 75723APF 1384966 NM NOSE LOOSE A CLCA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 19 573CA 24971 FLT KMIA-SJO - REJECTED TAKEOFF DUE TO AIRSPEED DIFFERENCE, CAPTAIN 80 KNOTS, F/O 120 KNOTS, ABORTED AT 120 KNOTS. FOUN D CAPTAIN PITOT SYSTEM LEAKING AT ELBOW FROM FLEX LINE TO HARD LINE AT PITOT TUBE. DISCONNECTED AND RESECURED ELBOW. P ERFORMED OPERATION/LEAK CHECK IAW B757 MM 34-11-00, SYSTEM OPERATED SATISFACTORY. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1999100800357 19991008 00357 NM 1999 10 8 99ZZZM701 1 19990904 A 3230 273NZ0083 ACTUATOR BOEING 757 75723APF 1384966 NM LT MLG FAILED A CLCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 571CA 24456 KMIA - LEFT MLG DID NOT RETRACT AFTER NORMAL TAKEOFF. GEAR DISAGREE/GEAR DOOR LIGH TON, STATUS AIR/GROUND DISAGREE ON L ANDING GEAR MONITOR. FOUND LEFT MAIN LANDING GEAR DOWN LOCK ACTUATOR FAILED AFTER NUMEROUS GEAR SWINGS. REPLACED LEFT MAIN LANDING GEAR DOWN LOCK ACTUATOR, MADE SEVERAL GEAR SWINGS, CHECKED GOOD. PERFORMED TEST FLIGHT AND LEFT MAIN LANDI NG GEAR CHECKED NORMAL. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1999100800358 19991008 00358 NM 1999 10 8 99ZZZM702 1 19990831 A 3230 273N20043 ACTUATOR BOEING 757 75723APF 1384966 NM LT MLG FAILED A CLCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 571CA 24456 KMIA - LEFT MLG WOULD NOT RETRACT, GEAR DISAGREE/GEAR DOOR LIGHT ON WHEN GEAR HANDLE PLACED DOWN. FOUND LEFT MLG TILT A CTUATOR WITH INTERNAL LEAKAGE. REPLACED LEFT MLG TILT ACTUATOR WITH INTERNAL LEAKAGE. REPLACED LEFT MLG TILT ACTUATOR IAW MM 32-30-15, OPERATIONAL CHECKED GOOD NO LEAKS. RELEASED AIRCRAFT FOR TEST FLIGHT. (M) 2 L 7 2 4F RT A2NM 1999100800359 19991008 00359 NM 1999 10 8 99ZZZM703 1 19990827 A 3230 RETRACT MECH BOEING 757 75723APF 1384966 NM LT MLG LACK OF LUBE A CLCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 571CA 16566 24456 KMIA - LEFT MLG WOULD NOT RETRACT, GEAR DISAGREE/GEAR DOOR LIGHT ON WHEN GEAR HANDLE PLACED DOWN. JACKED AND SWUNG GEAR SEVERAL TIMES WITH NO DISCREPANCY NOTED. LUBRICATED LEFT MAIN LANDING GEAR. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1999100800360 19991008 00360 NM 1999 10 8 EIA990195 1 19990619 A 5400 FITTING BOEING 747 747132 1384882 NM NR 4 PYLON DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG - DURING C/D CHECK, NR 4 PYLON, LOWER FORWARD DIAGONAL BRACE FITTING HAS 3 GROOVE MARKS. FITTING REWORKED PER HAECO RS-R-54-54-34084 AND TELEX EVR-HKG-99-0077RE/0071TE. (M) 2 L 7 4 4F A20WE 1999100800361 19991008 00361 NM 1999 10 8 EIA990194 1 19990619 A 5711 SPAR BOEING 747 747132 1384882 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG - DURING C/D CHECK, LEFT WING REAR SPAR WEB CRACKED AT NR 2 TANK O/B JETTISON PUMP CUTOUT, FASTENER HOLE. WEB FASTE NER HOLE REPAIRED PER EO 747-1022-90 REV A PART 2, OVERSIZED TO .341 INCH. (M) 2 L 7 4 4F A20WE 1999100800362 19991008 00362 NM 1999 10 8 EIA990193 1 19990615 A 5330 SKIN BOEING 747 747132 1384882 NM BS 220-240 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG - DURING C/D CHECK, FUSELAGE SKIN IS BULGED FROM BS 220-240 FROM STRINGER 40R-43R. REFORMED SKIN AND REPAIRED PER S RM 53-30-03 FIG 4. (M) 2 L 7 4 4F A20WE 1999100800363 19991008 00363 NM 1999 10 8 EIA990192 1 19990615 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 460 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, MAIN DECK FLOORBEAM UPPER CHORD CRACKED AT BS 460 AT LBL 34. REPAIRED UPPER CHORD PER SRM 51-40 -4 FIG 2. (M) 2 L 7 4 4F A20WE 1999100800364 19991008 00364 NM 1999 10 8 EIA990250 1 19990711 A 5410 STRUCTURE BOEING 747 747132 1384882 NM NR 1 PYLON DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG - DURING C/D CHECK, NR 1 PYLON HAS EVIDENCE OF OVERHEAT DAMAGE, PARTIALLY REPAIRED PREVIOUSLY. NR 1 PYLON SIDE FRAM ES REPLACED AT NAC STATION 183 L/R, 210 L/R, 236 L/R, 253 L/R. STIFFENERS REPLACED NR 1 NAC STATION 221-265 LEFT, NR 2 STATION 193-221 L/R, NR 3 STATION 180-221 L/R. REPLACED MID SPAR WEB PANEL NAC STATION 186-242. REPAIRED L/R MID SPAR CHORDS NAC STATION 180-206. REPAIRED LEFT SKIN NAC STATION 180-236. REPAIRED LEFT SKIN NACE STATION 236-253. ALL REPA IRS ACCOMPLISHED PER RS-R-54-00-34112, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800365 19991008 00365 NM 1999 10 8 EIA990249 1 19990709 A 5320 FRAME BOEING 747 747132 1384882 NM PAX DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D L1 MED CUTOUT AFT FRAME CRACKED AT WEB AND DOUBLER AT NR 1 STOP FITTING. REPAIRED DOOR FRAM E AT BS 488 PER SRM 53-10-04 FIG 92. (M) 2 L 7 4 4F A20WE 1999100800366 19991008 00366 NM 1999 10 8 EIA990248 1 19990709 A 5400 PAN BOEING 747 747132 1384882 NM NR 3 PYLON WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, NR 3 PYLON FORWARD STRUT CLOSURE PAN, RT REAR CORNER SKIN WORN. CLOSURE PAN TRIMMED AND REPAIRE D PER RS-R-71-90-34115. (M) 2 L 7 4 4F A20WE 1999100800367 19991008 00367 NM 1999 10 8 EIA990247 1 19990709 A 5711 SPAR BOEING 747 747132 1384882 NM WS 670 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, LEFT WING FOWARD SPAR, WS 670 LOWER CHORD FITTING VERTICAL LEG 2 FASTENER HOLES CRACKED. FASTEN ER HOLES REPAIRED PER RS-R-57-24-34095, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800368 19991008 00368 NM 1999 10 8 EIA990246 1 19990709 A 5311 144U0053327 FRAME BOEING 747 747132 1384882 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, BS 1265 LEFT FRAME FOUND CRACKED AT WEB AND CHORD, AT WL 200. REPAIRED PER BOEING DRAWING 144U0 053 AND RS-R-53-42-34098, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800369 19991008 00369 NM 1999 10 8 EIA990245 1 19990709 A 5312 BULKHEAD FTG BOEING 747 747132 1384882 NM BS 1241 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG - DURING C/D CHECK, BS 1241 BULKHEAD FITTING AT RIGHT SIDE, CRACK FOUND OF OUTBOARD FITTING LEG UPPER MOST BOLT HOLE . REPAIRED FITTING PER RS-R-53-43-34090 REV B, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800370 19991008 00370 NM 1999 10 8 EIAA990244 1 19990709 A 5711 SPAR BOEING 747 747132 1384882 NM RIGHT CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURIGN C/D CHECK, BS 1241 BULKHEAD FITTING AT RIGHT SIDE, CRACK FOUND OF SPAR WEB AT INBOARD FITTING LEG LOWEST BO LT HOLE. REPAIRED SPAR WEB AND FITTING PER RS-R-53-43-34090 REV B, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800371 19991008 00371 NM 1999 10 8 EIA990243 1 19990709 A 5400 SPAR BOEING 747 747132 1384882 NM NR 1 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, NR 1 PYLON LOWER SPAR WEB CRACKED AT NAC 221.5 BL 0, DURING EO ACCOMPLISHMENT. REPAIRED PER SRM 54-10-03 FIG 2. (M) 2 L 7 4 4F A20WE 1999100800372 19991008 00372 NM 1999 10 8 EIA990242 1 19990709 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1348 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 1348 STRINGER 11R STRINGER END FOUND CRACKED. REPAIRED STRINGER END PER RS-R-R-53-41-340 83, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800373 19991008 00373 NM 1999 10 8 EIA990241 1 19990709 A 5532 PANEL BOEING 747 747132 1384882 NM VERT STAB DISBONDED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, VERTICAL STABILIZER T/E CAVITY ACCESS PANEL 324FL FOUND DISBONDED. ACCOMPLISHED A TIME LIMITED REPAIR PER RS-R-55-10-34113. (M) 2 L 7 4 4F A20WE 1999100800374 19991008 00374 NM 1999 10 8 EIA990240 1 19990709 A 5320 TIE BOEING 747 747132 1384882 NM BS 940 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG - DURING C/D CHECK, M/D BS 940 LEFT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED PER SB 747-53-2371 FIG 3 AND TELEX EVR-HKG-99-0101ER/0092TE, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800375 19991008 00375 NM 1999 10 8 EIA990239 1 19990709 A 5330 SKIN BOEING 747 747132 1384882 NM BS 340 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, UPPER FUSELAGE AT BS 340, RT WINDSHIELD CUTOUT HAS A CRACK AT THE LOWER AFT CORNER. SKIN REPAIR ED PER SRM 53-30-03 FIG 49. (M) 2 L 7 4 4F A20WE 1999100800376 19991008 00376 NM 1999 10 8 EIA990238 1 19990709 A 5330 SKIN BOEING 747 747132 1384882 NM BS 340 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, UPPER FUSELAGE AT BS 340, LEFT WINDSHIELD CUTOUT HAS A CRACK AT THE LOWER AFT CORNER. SKIN REPA IRED PER SRM 53-30-03 FIG 49. (M) 2 L 7 4 4F A20WE 1999100800377 19991008 00377 NM 1999 10 8 EIA990237 1 19990709 A 5320 FRAME BOEING 747 747132 1384882 NM PAX DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, R1 MED CUTOUT AFT FRAME CRACKED AT FRAME WEB AND WEB DOUBLER AT NR 1 STOP FITTING. REPAIRED DOO R FRAME AT BS 488 PER SRM 53-10-04 FIG 92. (M) 2 L 7 4 4F A20WE 1999100800378 19991008 00378 NM 1999 10 8 EIA990236 1 19990709 A 5320 FRAME BOEING 747 747132 1384882 NM PAX DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 DURING C/D CHECK, R2 MED AFT FRAME UPPER CORNER CRACKED. REPAIRED DOOR FRAME PER SRM 52-10-02 FIG 10. (M) 2 L 7 4 4F A20WE 1999100800379 19991008 00379 NM 1999 10 8 EIA990235 1 19990709 A 5400 FITTING BOEING 747 747132 1384882 NM NR 4 PYLON NICKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225 HAS SEVERAL BAD NICKS. REPAIRED PER RS-R-54- 54-34111 AND SRM 54-40-01 FIG 1, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800380 19991008 00380 NM 1999 10 8 EIA990234 1 19990709 A 5400 FITTING BOEING 747 747132 1384882 NM NR 4 PYLON CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 HKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225, CORROSION FOUND IN BUSHING BORE. REPAIRED B USHING BORE IAW SB 747-54-2164 FIG 2, INSURANCE CUT TO FINAL SIZE 2.360 INCH AND RS-R-54-34085, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800381 19991008 00381 NM 1999 10 8 EIA990233 1 19990709 A 5311 144U0053328 FRAME BOEING 747 747132 1384882 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, MAIN DECK, RT BS 1265 FRAME CRACKED AT WEB AD CHORD AT WL 200. REPAIRED FRAME CHORD AND WEB PER BOEING DRAWING 144U0053 AND RS-R-53-42-34098, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800382 19991008 00382 NM 1999 10 8 EIA990232 1 19990707 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1245 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, MAIN DECK, BS 1245 STRINGER 1L END FOUND CRACKED. REPAIRED STRINGER END PER RS-R-53-41-34087 FI G 2, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800383 19991008 00383 NM 1999 10 8 EIA990231 1 19990707 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1245 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, MAIN DECK, BS 1245 STRINGER 2L END FOUND CRACKED. REPAIRED STRINGER END PER RS-R-53-41-34087 FI G 1, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800384 19991008 00384 NM 1999 10 8 EIA990230 1 19990707 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1245 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, MAIN DECK, BS 1245 STRINGER 1R END FOUND CRACKED. REPAIRED STRINGER END PER RS-R-53-41-34087 FI G 3, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800385 19991008 00385 NM 1999 10 8 EIA990229 1 19990706 A 5412 FIREWALL BOEING 747 747132 1384882 NM NR 1 ENGINE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, NR 1 ENGINE TURBINE SECTION FIREWALL HAS A CRACK AT THE 3 O'CLOCK POSITION. FIREWALL CRACK REPA IRED PER RS-R-72-53-34080, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800386 19991008 00386 NM 1999 10 8 EIA990228 1 19990706 A 5312 BULKHEAD WEB BOEING 747 747132 1384882 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, LEFT BS 1480 BULKHEAD AREA STRINGER 36L, CHORD FASTENER HOLE CRACKED. BULKHEAD FASTENER HOLE RE PAIRED AND STRINGER END REPLACED PER RS-R-53-43-34100, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800387 19991008 00387 NM 1999 10 8 EIA990227 1 19990706 A 5320 65B0441714 STOP BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D NR 4R MED CUTOUT FORWARD FRAME AT LOWER STOP FITTING FOUND CRACKED. DOOR STOP FITTINGS REPL ACED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999100800388 19991008 00388 NM 1999 10 8 EIA990226 1 19990706 A 5320 65B083206 FITTING BOEING 747 747132 1384882 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D NR 3R MED CUTOUT FRAME AT BS 1265 NR 2 STOP FITTINGS FOUND CRACKED. DOOR STOP FITTING REPLA CED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999100800389 19991008 00389 NM 1999 10 8 EIA990225 1 19990706 A 5320 65B0831915 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D NR 3R MED CUTOUT FORWARD FRAME NR 4 AND NR 5 STOP SUPPORT FITTINGS FOUND CRACKED. DOOR STOP SUPPORT FITTINGS REPLACED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999100800390 19991008 00390 NM 1999 10 8 99ZZZM704 1 19990706 A 5320 65B0831917 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D NR 3R MED CUTOUT FORWARD FRAME NR 4 AND NR 5 STOP SUPPORT FITTINGS FOUND CRACKED. DOOR STOP SUPPORT FITTINGS REPLACED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999100800391 19991008 00391 NM 1999 10 8 EIA990224 1 19990706 A 5320 65B0831924 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D NR 3R MED CUTOUT FORWARD FRAME NR 4 STOP FITTING FOUND CRACKED. DOOR STOP FITTING REPLACED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999100800392 19991008 00392 NM 1999 10 8 EIA990223 1 19990706 A 5320 65B083200 FITTING BOEING 747 747132 1384882 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D NR 3L MED CUTOUT FORWARD FRAME NR 2 STOP SUPPORT FITTING FOUND CRACKED. DOOR STOP SUPPORT F ITTING REPLACED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999100800393 19991008 00393 NM 1999 10 8 EIA990222 1 19990706 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1745 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D STRINGER CRACKED AT BS 1745 STRINGER 1R. STRINGER END REPAIRED PER RS-R-53-61-34005, 8110-3 . (M) 2 L 7 4 4F A20WE 1999100800394 19991008 00394 NM 1999 10 8 EIA990221 1 19990706 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1481 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D STRINGER CRACKED AT BS 1481 STRINGER 1L. STRINGER END REPAIRED PER RS-R-53-61-34086, 8110-3 . (M) 2 L 7 4 4F A20WE 1999100800395 19991008 00395 NM 1999 10 8 EIA990220 1 19990706 A 5720 SHEAR TIE BOEING 747 747132 1384882 NM WS 469 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, RIGHT WING, WS 469 RIB UPPER CHORD BETWEEN FRONT SPAR AND STRINGER 30, SHEAR TIE CRACKED. SHEAR TIE FITTING REPAIRED PER SRM 57-10-05 FIG 7. (M) 2 L 7 4 4F A20WE 1999100800396 19991008 00396 NM 1999 10 8 EIA990219 1 19990706 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1486 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 DURING C/D CHECK, M/D STRINGER CRACKED AT BS 1486 STRINGER 17R. STRINGER END REPAIRED PER RS-R-53-41-34093, 8110-3. (M ) 2 L 7 4 4F A20WE 1999100800397 19991008 00397 NM 1999 10 8 EIA990218 1 19990706 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 2200 BROKEN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, AFT BULK CARGO COMPARTMENT, BS 2200 STRINGER 42L-44L SHEAR TIE ANGLE BROKEN. REPAIRED PER SRM 5 1-10-01. (M) 2 L 7 4 4F A20WE 1999100800398 19991008 00398 NM 1999 10 8 EIA990217 1 19990706 A 5311 FRAME BOEING 747 747132 1384882 NM BS 760 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 760 BODY FRAME IS CRACKED AT STRINGER CUTOUT AT STRINGER 14L. REPAIRED FRAME PER RS-R-53 -22-34099, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800399 19991008 00399 NM 1999 10 8 EIA990216 1 19990629 A 5320 SHEAR TIE BOEING 747 747132 1384882 NM BS 960 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, FORWARD CARGO COMP, BS 960 STRINGER 34R-35R, FRAME SHEAR TIE CRACKED. FRAME SHEAR TIE REPAIRED IAW SRM 53-10-04 FIG 3. (M) 2 L 7 4 4F A20WE 1999100800400 19991008 00400 NM 1999 10 8 EIA990215 1 19990629 A 5400 65B903494 BLOCK BOEING 747 747132 1384882 NM NR 3 STRUT SCRATCHED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, NR 3 NACELLE STRUT FORWARD UNIVERSAL BLOCK FOUND DEEP SCRATCH MARKS IN BUSHING BORE AREA. REPLA CED FORWARD MOUNT UNIVERSAL BLOCK ASSEMBLY PER MM 71-21-02. (M) 2 L 7 4 4F A20WE 1999100800401 19991008 00401 NM 1999 10 8 EIA990214 1 19990629 A 5711 SPAR BOEING 747 747132 1384882 NM WS 688 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, LEFT WING FRONT SPAR, 2 FASTENER HOLES FOUND CRACKED AT FSSI 688, UPPER AND LOWER CHORD AREA. W EB REPAIRED PER RS-R-21-34097, SB 747-57A2303 FIG 5, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800402 19991008 00402 NM 1999 10 8 EIA990213 1 19990629 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURNG C/D CHECK, LEFT WING L/E 'D' SECTION LOWER SURFACE CUTOUT FOR NR 12 KRUEGER FLAP OUTBOARD HINGE. REPAIRED P ER SRM 51-40-03 FIG 1. (M) 2 L 7 4 4F A20WE 1999100800403 19991008 00403 NM 1999 10 8 EIA990212 1 19990629 A 5320 REVEAL BOEING 747 747132 1384882 NM BS 1666 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, R4 DOOR FORWARD CUTOUT, UPPER AND LOWER REVEAL CRACKED AT BS 1666 STRINGER 18R AND 24R. REPAIRE D LOWER REVEAL PER SRM 53-10-04 FIG 84, REPAIRED UPPER REVEAL PER RS-R-53-61-34101, 8110-3. (M) 2 L 7 4 4F A20WE 1999100800404 19991008 00404 NM 1999 10 8 EIA990211 1 19990629 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 743 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 DURING C/D CHECK, STRINGER 3L FOUND CRACKED AT BS 743. REPAIRED PER SRM 53-10-03 FIG 5. (M) 2 L 7 4 4F A20WE 1999100800421 19991008 00421 EA 1999 10 8 99ZZZX3821 2 19990924 A 7314 RG9080J4A PUMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA FUEL SYSTEM LEAKING A TQ6A K NONE K FLUID LOSS IN INSP/MAINT 1 SO 15 48CA 115 D9800 318052003 L148568A UPON ARRIVAL AT SCOTLAND CAY, BAHAMAS (ABACO), DURING ENGINE SHUT DOWN, THE RT ENGINE DRIVEN FUEL PUMPS STARTED LEAKING. THE FUEL IGNITED ON THE EXHAUST PIPE CAUSING A SMALL FIRE. THE FIRE WAS EXTINGUISHED WITH THE ONBOARD PORTABLE FIRE E XTINGUISHER. NOTE 1: BOTH ENGINES WERE FACTORY OVERHAULED AND INSTALLED IN JULY, 1999. THE FUEL PUMPS WERE INSTALLED DURING OVERHAUL. NOTE 2: PUMP MANUFACTUERER: CRANE LEAR ROMEC. 1 L 7 2 3O 3 O A20SO E14EA 1999100800446 19991008 00446 CE 1999 10 8 99ZZZX3845 1 19990907 A 3710 FILTER DONALDSON CESSNA 402 402B 207590P CE NOSE CARGO BAY BLOCKED A HSRA K NONE O OTHER IN INSP/MAINT 1 NM 05 401NA 261 0035 IF CENTRAL INSTRUMENT AIR FILTER GETS WET, THE FILTER FIBERS EXPAND AND BLOCKS THE FLOW OF AIR TO VACUUM INSTRUMENT SYST EM. THIS BLOCKAGE OF AIR FLOW RESULTED IN THE PILOT MAKING AN EMERGENCY LANDING IN LOW CEILINGS/IFR CONDITIONS DUE TO T HE VACUUM INSTRUMENT (BOTH SIDES) FAILING. THE FILTER BECAME WET DURING A HEAVY RAIN WHILE LOADING BAGGAGE IN THE NOSE BAGGAGE COMPARTMENT. THE FILTER IS MANUFACTURED BY DONALDSON MFG (PN PIO-5290 OR 294501-0203) FOR DISTRIBUTION BY CESSN A. THIS TYPE FILTER IS INSTALLED IN THE CESSNA CE-340, AND ALL CE-400 SERIES CESSNA AIRCRAFT. MFG P/N PIO-5290 OR 2945 01-0203. 1 L 7 2 3O A7CE 1999100800455 19991008 00455 NM 1999 10 8 TWAA9913701 1 19990928 A 3350 BATTERY BOEING 767 767231 1385131 NM ROW 18-22 DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 604TW 22567 THE CABIN EMERGENCY EXIT SIGN ABOVE THE DOOR AT ROW 18, LEFT SIDE, AND THE EMERGENCY AISLE LIGHTS AT ROWS 18 TO 22, ALL ILLUMINATED WITH THE SWITCH IN THE ARMED POSITION. REPLACED THE BATTERY, MFG 2013-1A, AND THE BATTERY CHARGER, MFG 2012 -1. CORRECTED AT CHECK-C. 2 L 7 2 4F RT A1NM 1999100800456 19991008 00456 WP 1999 10 8 TWAA9913702 1 19991005 A 2450 947F9463 BUS TIE UNIT DOUG DC9 DC931 3022065 WP RIGHT WORN A TWAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 CE 05 978Z 47250 AFTER TAKEOFF, BOTH ENGINE GENERATORS TRIPPED OFF LINE. THE APU WAS RUNNING AND TOOK THE LOAD. THE RT GEN RESET BUT TH E LT WOULD NOT. FLIGHT RETURNED TO STL. REPLACED THE BUS TIE UNIT AND RESET THE LH GEN CONTROL UNIT. CHECK-C 4-30-99 STL. 2 L 7 2 4F A6WE 1999100800457 19991008 00457 WP 1999 10 8 TWAA9913703 1 19991006 A 3350 0105606004 LIGHT DOUG DC9 DC983 3022083 WP ROW 22-30 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951TW 53470 THE CABIN EMERGENCY EGRESS LIGHTS WERE INOPERATIVE FROM ROW 22 THROUGH 30. REPLACED THE LIGHT MODULE. CHECK-C 6-12-99 STL. 2 L 7 2 4F RT A6WE 1999100800458 19991008 00458 EU 1999 10 8 MALA976593 1 19991005 A 3350 6013211 POWER SUPPLY SAAB SF340 SF340A 7850100 EU ROW 20LN INOP A MALA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 15 110XJ 340A110 EMERGENCY LIGHTS ON WHEN SWITCHED IN ARMED POSITION. MAINTENANCE REPLACED POWER SUPPLY 20LN. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999100800459 19991008 00459 EU 1999 10 8 MALA976594 1 19991004 A 5270 SWITCH SAAB SF340 340B 7860101 EU PAX DOOR FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 447XJ 447 MAIN DOOR LIGHT ILLUMINATED INTERMITTENTLY AFTER DEPARTING ESC. AIRCRAFT RETURNED WITHOUT DECLARING AN EMERGENCY, LIGHT WENT OUT ON GROUND. THE SIGHT WINDOW WAS CHECKED, NO SQUEALING HEARD AND LATCHES WERE LOCKED. MAINTENANCE ADJUSTED MA IN DOOR WARNING MICROSWITCH IAW SF3 AMM CH 52-70-00-5. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999100800460 19991008 00460 EU 1999 10 8 MALA976595 1 19991003 A 2421 31342003 GENERATOR SAAB SF340 340B 7860101 EU LEFT FAILED A MALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 15 452XJ 452 LEFT AC GEN CAUTION LIGHT ON, PERFORMED QRH PROCEDURES. AC GEN REMAINED INOP. AIRCRAFT RETURNED TO DTW. MAINTENANCE R EPLACED LT AC GEN. RAN AIRCRAFT OPS CHECK GOOD IAW SAAB MM 24-00-00. 2 L 7 2 4T RT A52EU 1999100800461 19991008 00461 NM 1999 10 8 AWXA9900342 1 19991005 A 2150 20405011 ACM BOEING 737 737277 1384570 NM LEFT FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 180AW 37230 6341 22647 AIR TURNBACK, CABIN PRESS HORN WENT OFF AT 12,500 AND CABIN WOULD NOT HOLD PRESS. WOULD NOT RESTORE WITH STANDBY OR MAN . REMOVED AND REPLACED AIR CYCLE MACHINE LT PACK AND AIR CONDITION RELAY CURRENT HISTORY: ATA 21 SEVERAL WRITE-UPS IN LAST THREE DAYS, MORE HISTORY ON LT PACK. 2 L 7 2 4F RT A16WE 1999100800462 19991008 00462 NE 1999 10 8 AWXA9900343 2 19991006 A 7530 1666MK5 ACTUATOR AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE FAILED A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 646AW 271 EMERGENCY DECLARED (NOT BY PILOT) ENG NR 1 COMPRESSOR VANE FAULT ON DESCENT, NO OTHER ABNORMAL ENG INDICATIONS OR FAILUR ES. FIRST TIME FAULT FADEC CONFIRMS 2.5 BLEED ACTUATOR FAIL CURRENT HISTORY. 2 L 7 2 4F 4 F RT A28NM E311NE 1999100800463 19991008 00463 NM 1999 10 8 AWXA9900344 1 19991006 A 2910 MS219026 FITTING BOEING 737 737277 1384570 NM NR 1 TR UNIT STRIPPED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 180AW 22647 AIR TURNBACK, AFTER RAISING THE GEAR ANNUNCIATOR INDICATED HYD PROBLEM 'A' SYS HYD. QUANTITY GAUGE WENT TO ZERO. FOUND NR 1 ENG T/R SHUTTLE VALVE FITTING BAD. REMOVED AND REPLACED FITTING. 2 L 7 2 4F RT A16WE 1999100800464 19991008 00464 EU 1999 10 8 AWXA9900345 1 19991006 A 4990 38807991 OIL COOLER AIRBUS 320 A320231 3930325 EU APU LEAKING A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 646AW 271 DURING DESCENT WITH POWER AT IDLE, NOXIOUS ODORS EMANATED FROM THE LT PACK, CAPABLE OF EYE AND THROAT IRRITATION. ISOLA TED TO LEAKING OIL COOLER. REMOVED AND REPLACED OIL COOLER AND OZONE FILTERS. 2 L 7 2 4F RT A28NM 1999100800465 19991008 00465 NM 1999 10 8 UPS99230859 1 19991005 A 3350 LAMP BOEING 727 72725C 138400H NM LT GALLEY FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 LEFT GALLEY EMERGENCY LIGHT ABOVE FLIGHT ATTENDANT SEAT OUTBOARD LAMP IS BURNT OUT. REMOVED AND REPLACED LIGHT AND BATT ERY ASSY OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800466 19991008 00466 NM 1999 10 8 UPS99230860 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 RIGHT LOWER FWD OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999100800467 19991008 00467 NM 1999 10 8 UPS99230861 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 LEFT LOWER FWD OVERWING EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED BATTERY. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800468 19991008 00468 NM 1999 10 8 UPS99230862 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 LEFT EXTERIOR MIDDLE OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800469 19991008 00469 NM 1999 10 8 UPS99230863 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM OVERWING DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 RIGHT EXTERIOR TOP OVERWING EMERGENCY EXIT LIGHT OUT/DIM. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800470 19991008 00470 NM 1999 10 8 UPS99230864 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMER EXIY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 RIGHT EXTERIOR MIDDLE OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800471 19991008 00471 NM 1999 10 8 UPS99230865 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 RIGHT EXTERIOR BOTTOM OVERWING EMERGENCY EXIT LIGHT OUT/DIM. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800472 19991008 00472 NM 1999 10 8 UPS99230866 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM VENTRAL STAIRS DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 AFT VENTRAL STAIRS EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800473 19991008 00473 NM 1999 10 8 UPS99230867 1 19991005 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM LT EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 RIGHT LOWER AFT OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999100800474 19991008 00474 WP 1999 10 8 UPS99830840 1 19990911 A 5320 36429832 ANGLE DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 FWD ACCY COMPT, FS 680, BETWEEN LONG 22R AND 23R, THE ANGLE INSIDE THE A FRAME IS CRACKED. REMOVED , FABRICATED, AND REPLACED THE ANGLE IAW DWG 3642983 AND SRM 5-1-20D. 2 L 7 4 4F RT 4A25 1999100800475 19991008 00475 WP 1999 10 8 UPS99830841 1 19990911 A 5414 SKIN DOUG DC8 DC871F 302199D WP NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 NR 4 PYLON INBD SKIN AT STA YN 278 IS CRACKED THROUGH A SCREW HOLE. CUT OUT DAMAGED AREA AND REPAI RED IAW DH SK718-147. 2 L 7 4 4F RT 4A25 1999100800476 19991008 00476 WP 1999 10 8 UPS99830842 1 19990912 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 RT WING LWR SKIN ABOVE THE NR 4 PYLON HAS A 5 INCH CRACK, JUST OUTBOARD OF THE OUTBOARD SLOT, OUTBO ARD END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1A FIG 1. 2 L 7 4 4F RT 4A25 1999100800477 19991008 00477 WP 1999 10 8 UPS99830843 1 19990913 A 5320 49125671 FITTING DOUG DC8 DC871F 302199D WP BS 240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 FLOOR SUPPORT BEAM CRACKED AND ANGLE FITTING CRACKED AT FS 240, LBL 42. REMOVED AND REPLACED THE A NGLE FITTING AND REPAIRED THE FLOOR SUPPORT BEAM IAW DH SK718-388. 2 L 7 4 4F RT 4A25 1999100800478 19991008 00478 WP 1999 10 8 UPS99830844 1 19990915 A 5313 97549135 LONGERON DOUG DC8 DC871F 302199D WP BS 330-340 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 BATH TUB FITTING AND BEAM HAVE HEAVY CORROSION INSIDE WEB AT FS 330 TO 340, LONGERON 36. REMOVED A ND REPLACED THE FITTING AND THE BEAM (LONGERON) IAW SRM 51-1-20D AND 53-2-0 FIG 1F. 2 L 7 4 4F RT 4A25 1999100800479 19991008 00479 WP 1999 10 8 UPS99830845 1 19990914 A 5320 4640162502 FITTING DOUG DC8 DC871F 302199D WP BS 1306 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 CORROSION AROUND UPPER CUSP FITTING MOUNT BOLTS INBD, FWD, AND AFT AND ON FLOORBEAM FS 1306, LT SID E. REMOVED AND REPLACED THE CUSP FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999100800480 19991008 00480 WP 1999 10 8 UPS99830846 1 19990915 A 5320 4646163501 FITTING DOUG DC8 DC871F 302199D WP BS 1340-1360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 BETWEEN FS 1340 AND 1360, LONGERON 30L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800481 19991008 00481 WP 1999 10 8 UPS99830847 1 19990915 A 5313 5753744501 LONGERON DOUG DC8 DC871F 302199D WP BS 1340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LONGERON 31L BELOW THE FRAME AT FS 1340 IS CORRODED BEYOND LIMITS. CUT OUT THE DAMAGED LONGERON AN D SPLICED IN A NEW SECTION OF LONGERON IAW DH SK718-829. 2 L 7 4 4F RT 4A25 1999100800482 19991008 00482 WP 1999 10 8 UPS99830848 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 520.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E STUB WING RIB AT XS 520.168 IS CRACKED ABOVE THE ELECT CONDUIT. STOP DRILL THE CRACK A ND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800483 19991008 00483 WP 1999 10 8 UPS99830849 1 19990915 A 5720 576964679 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT INBD L/E UPPER AFT ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 5769646 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999100800484 19991008 00484 WP 1999 10 8 UPS99830850 1 19990915 A 5720 9753293 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E, INBD SIDE OF THE XS 250.089 RIB, THE INBD SLOT AFT BULKHEAD OTBD VERTICAL ANGLE IS CRA CKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999100800485 19991008 00485 WP 1999 10 8 UPS99830851 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E AT XS 250.089, ABOVE THE WIRE BUNDLES. THE RIB IS CRACKED. STOP DRILLED CRACK AND REP AIRED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800486 19991008 00486 WP 1999 10 8 UPS99830852 1 19990915 A 5320 37549301 FITTING DOUG DC8 DC871F 302199D WP BS 1210 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 BATHTUB FITTING CRACKED INSIDE WEB AT FS 1210, LONGERON 33R. REMOVED AND REPLACED THE FITTING IAW SRM 51-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999100800487 19991008 00487 WP 1999 10 8 UPS99830853 1 19990915 A 5320 3750257503 FITTING DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LONGERON SPLICE FITTING IS CRACKED AT FS 1050, LONGERON 31L. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999100800488 19991008 00488 WP 1999 10 8 UPS99830854 1 19990915 A 5720 36536791 INGERCOSTAL DOUG DC8 DC871F 302199D WP WS 115 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E AT XFS 115.0, JUST AFT OF THE ACCESS PANEL, THE INTERCOSTAL IS CRACKED AT THE 2ND FROM THE INBOARD FASTENER. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG 3653679 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800489 19991008 00489 WP 1999 10 8 UPS99830855 1 19990915 A 5320 3755854502 FITTING DOUG DC8 DC871F 302199D WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 FS 1180, AT LONGERON 33R, THE BANANA FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800490 19991008 00490 WP 1999 10 8 UPS99830856 1 19990916 A 5720 56412522 DOUBLER DOUG DC8 DC871F 302199D WP WS 305 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 RT WING LWR L/E SKIN DOUBLER AT XFS 305 IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999100800491 19991008 00491 WP 1999 10 8 UPS99830857 1 19990924 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LONGERON 35R IS CRACKED AT FS 1050. CUT OUT DAMAGED AREA AND SPLICED LONGERON IAW DH SK718-251. 2 L 7 4 4F RT 4A25 1999100800492 19991008 00492 WP 1999 10 8 UPS99830858 1 19991003 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 COCKPIT EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK ASSY. EMERGENCY LIGHT OPS CHECK NORMAL PER MM 33-50-00. 2 L 7 4 4F RT 4A25 1999100800493 19991008 00493 EU 1999 10 8 QXEA9902009 1 19990929 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 SEA - LIGHTING DIM IN EXIT SIGN ABOUT COCKPIT DOOR. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999100800494 19991008 00494 EU 1999 10 8 QXEA9902010 1 19991004 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU GALLEY INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 PDX - EXIT SIGN ABOVE GALLEY LIGHT OUT. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999100800495 19991008 00495 WP 1999 10 8 ABXA9900726 1 19990930 A 3350 41B004AD07G3 BATTERIES DOUG DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 987AX 47364 EMERGANCY LIGHTS WOULD NOT TEST. REPLACED POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1999100800496 19991008 00496 WP 1999 10 8 ABXA9900727 1 19990922 A 5311 3614994 FRAME DOUG DOUG DC8 DC863 302198A WP BS 1040 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 LOWER FRAME FLANGE OF FRAME STATION 1040 IS CRACKED JUST ABOVE LONGERON 36. REPAIRED IAW ABX REA D853-32996MR. 2 L 7 4 4F 4A25 1999100800497 19991008 00497 WP 1999 10 8 ABXA9900728 1 19990922 A 5311 561386178 FRAME DOUG DOUG DC8 DC863 302198A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 FRAME WAS CRACKED AT NOSE LANDING GEAR DOOR ATTACH IN WEB. REPAIRED FRAME IAW ABX REA D853-32728MR. 2 L 7 4 4F 4A25 1999100800498 19991008 00498 WP 1999 10 8 MWEA99646 1 19991004 A 5312 591013037 BULKHEAD WEB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT PRESSURE BULKHEAD WEB IS CRACKED AT VENTRAL DOOR JAMB. MAINTENCANCE REMOVED AND INSTALLED NEW DOOR WEB. 2 L 7 2 4F A6WE 1999100800499 19991008 00499 WP 1999 10 8 MWEA99647 1 19991004 A 5230 SB0952008945 OUTER PAN DOUG DC9 DC932 3022066 WP CARGO DOOR MISINSTALLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO DOOR OUTER PAN HAS NUMEROUS NUT PLATES IN PLACE OF FASTENERS. MAINTENANCE REMOVED AND REPLACED DOOR OUTER PAN . 2 L 7 2 4F A6WE 1999100800500 19991008 00500 WP 1999 10 8 MWEA99648 1 19991004 A 5321 9910078873 FLOOR DOUG DC9 DC932 3022066 WP BS 210 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 SUBFLOOR CRACKED AT STATION 210 AT NUT PLATE. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999100800501 19991008 00501 WP 1999 10 8 MWEA99649 1 19991004 A 5321 9910078873 FLOOR DOUG DC9 DC932 3022066 WP BS 205 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 SUBFLOOR IS CRACKED AT RIVET HOLE AT STATION 205. MAINTENANCE FABRICATED AND INSTALLED NEW FLOOR DOUBLER. 2 L 7 2 4F A6WE 1999100800502 19991008 00502 WP 1999 10 8 MWEA99650 1 19991004 A 5320 991007855 SUPPORT DOUG DC9 DC932 3022066 WP CENTER FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CENTER LINE FLOOR SUPPORT HAS NUMEROUS CRACKS ON UNDERSIDE OF BEND RADIOUS. MAINTENANCE FABRICATED AND INSTALLED NEW FL OOR SUPPORT. 2 L 7 2 4F A6WE 1999100800503 19991008 00503 WP 1999 10 8 MWEA99651 1 19991004 A 5320 991007857 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FLOOR BOARD SUPPORT AT FUSELAGE STATION 200 HAS CORROSION ON SEAT TRACKS. MAINTENANCE FABRICATED AND INSTALLED NEW SUPP ORT. 2 L 7 2 4F A6WE 1999100800504 19991008 00504 WP 1999 10 8 MWEA99652 1 19991004 A 5230 3914025502N BRACKET DOUG DC9 DC932 3022066 WP CARGO DOOR MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO DOOR NR 5 BEAM FROM TOP HAS MISDRILLED HOLE THROUGH AFT END. MAINTENANCE PLUGGED HOLE AND FABRICATED AND INST ALLED NEW BRACKET. 2 L 7 2 4F A6WE 1999100800505 19991008 00505 WP 1999 10 8 MWEA99653 1 19991004 A 5230 995766514M BEAM DOUG DC9 DC932 3022066 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 AFT CARGO DOOR TOP BEAM WEB IS GOUGED. MAINTENANCE INSTALLED REPLACEMENT WEB. 2 L 7 2 4F A6WE 1999100800506 19991008 00506 WP 1999 10 8 MWEA99654 1 19991004 A 5347 59108201 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 RIGHT OUTBOARD FLOOR SEAT TRACK SUPPORT HAS CORROSION. MAINTENANCE FABRICATED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 1999100800507 19991008 00507 WP 1999 10 8 MWEA99655 1 19991004 A 5240 593998823 DOUBLER DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 GALLEY SERVICE DOOR NR 1 BEAM, AFT OUTER CORNER HAS A CRACK. MAINTENANCE FABRICATED AND INSTALLED DOUBLER ANGLE. 2 L 7 2 4F A6WE 1999100800508 19991008 00508 WP 1999 10 8 MWEA99656 1 19991004 A 5320 5265247912000 ANGLE DOUG DC9 DC932 3022066 WP BS 160 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FLOOR ANGLE CRACKED AT STATION 160. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999100800509 19991008 00509 WP 1999 10 8 MWEA99657 1 19991004 A 5320 591214130 DOUBLER DOUG DC9 DC932 3022066 WP BS 1089 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 ATTACH FLANGE IS CRACKED AT STATION 1089. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999100800510 19991008 00510 WP 1999 10 8 MWEA99658 1 19991004 A 5311 991555965 FRAME DOUG DC9 DC981 3022081 WP BS 1401 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 CORRSION FRAME WEB AND TEE CAP AT STATION 1401 ON LONGERON 25 LEFT. MAINTENANCE FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 1999100800511 19991008 00511 WP 1999 10 8 MWEA99659 1 19991004 A 5347 59305669 SEAT TRACK DOUG DC9 DC981 3022081 WP BS 1302 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 NR 3 SEAT TRACK AT STATION 1302 HAS EXFOLIATION CORRSION. MAINTENANCE FABRICATED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 1999100800512 19991008 00512 WP 1999 10 8 MWEA99660 1 19991004 A 5347 593056625 SEAT TRACK DOUG DC9 DC981 3022081 WP BS 1117 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 SEAT TRACK LOBES ARE BLENDED OFF AT STATION 1117. MAINTENANCE FABRICATED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 1999100800513 19991008 00513 WP 1999 10 8 MWEA99661 1 19991004 A 5320 9911839180 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 2 CLIPS CRACKED AT LONGERON 3 LEFT AND 3 RIGHT. MAINTENANCE FABRICATED AND INSTALLED NEW CLIPS. 2 L 7 2 4F A6WE 1999100800514 19991008 00514 WP 1999 10 8 MWEA99662 1 19991004 A 5711 991173433 SPAR DOUG DC9 DC932 3022066 WP LT WING GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 LEFT WING AILERON TRAILING EDGE SPAR HAS PUNCTURE AND GOUGE. BLENDED GOUGE FABRICATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 1999100800515 19991008 00515 WP 1999 10 8 MWEA99663 1 19991004 A 5311 591342123 FRAME DOUG DC9 DC932 3022066 WP BS 110 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FRAME INSIDE FWD WHEEL WELL IS CRACKED AT STATION 110. STOP DRILLED CRACK AND FABRICATED DOUBLER. INSTALLED FABRICATED DOUBLERS. 2 L 7 2 4F A6WE 1999100800516 19991008 00516 WP 1999 10 8 MWEA99664 1 19991004 A 5313 99115103 LONGERON DOUG DC9 DC932 3022066 WP BS 180 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 MODERATE CORROSION AT ATTACHMENT OF LONGERON 23 LEFT AND FUSELAGE FROM 180. MAINTENANCE FABRICATED AND INSTALLED NEW DO UBLER. 2 L 7 2 4F A6WE 1999100800517 19991008 00517 WP 1999 10 8 MWEA99665 1 19991003 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 204ME 47680 GALLEY DOOR EMERGENCY SLIDE COVER AND GIRT BAR CABLE CAME OFF WHEN SERVICING GALLEY IN DCA. MAINTENANCE REATTACHED EMER GENCY DOOR GIRT BAR AND SIDE. 2 L 7 2 4F A6WE 1999100800518 19991008 00518 NM 1999 10 8 DLM90992157 1 19990927 A 3350 P2070003001 FLASHLIGHT DOUG MD90 MD9030 3023690 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DA 53389 ONE OF TWO EMERGENCY FLASHLIGHT AT FORWARD F/A STATION NOT BLINKING. REPLACED FLASHLIGHT ASSY AND BATTERY. 2 L 7 2 4F RT A6WE 1999100800519 19991008 00519 1999 10 8 DL73K992170 4 19990928 A 2210 YAW DAMPER 654486112 BOEING 737 737232 1384475 NM E&E COMP MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 SO 27 310DA 1473A 23082 UNCOMMANDED ROLL/YAW AT 31000 FT, 77 MACH AUTOPILOT ENGAGED, A/C ROLLED HARD LEFT. REQUIRED 40-50 DEGREE AILERON TO TO RIGHT TO COUNTER COMMAND ROLL. POM COMPLIED WITH YAW DAMPER DISENGAGED. A/C RETURNED TO NORMAL FLIGHT. REPLACED YAW DA MPER COUPLER AND RUDDER PCU PER M/M. REMOVED AND REPLACED FLIGHT DATA RECORDER FOR INVESTIGATION. 2 L 7 2 4F RT A16WE 1999100800520 19991008 00520 NM 1999 10 8 DL767992171 1 19990917 A 5400 311T17301 BRACE BOEING 767 767232 1385132 NM NR 1 & 2 PYLON CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 MIGRATED/ROTATED BUSHINGS WERE FOUND IN THE FORWARD LUGS OF THE NR 1 AND NR 2 PYLON DIAGONAL BRACES DURING PYLON INSTALL ATION. MINOR CORROSION DAMAGE AND FRETTING DAMAGE WAS FOUND IN THE BORES UPON BUSHING REMOVAL. 2 L 7 2 4F RT A1NM 1999100800521 19991008 00521 NM 1999 10 8 DL72E992172 1 19990908 A 5754 RIB BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 AT HMV2, FOUND NR 4 L/E SUPPORT RIB IS CRACKED UPPER LEG. REMOVED FASTENERS AND CLIP, STOP DRILLED, FABRICATED DOUBLER REPAIR PER 57-54-00 FIG 809, AND INSTALLED PER SAME. 2 L 7 3 4F A3WE 1999100800522 19991008 00522 NM 1999 10 8 DL72S992175 1 19990930 A 7931 SENSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 539DA 22385 700455 NR 2 ENG LOW OIL PRESS LIGHT ILLUMINATED ON T/O ROLL. ABORTED T/O. RETURNED TO GATE. REPLACED PRESSURE SENDING UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1999100800523 19991008 00523 NM 1999 10 8 DL76L992177 1 19990928 A 7100 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 186DN 36749 27962 724171 LOSS OF OIL ON TAKEOFF AND CLIMB, ENGINE PARAMETERS NORMAL. OIL TEMP DECREASED WHILE OIL PRESSURE RAISED. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999100800524 19991008 00524 NM 1999 10 8 DL767992178 1 19990930 A 5730 111T30131 SKIN BOEING 767 767232 1385132 NM CENTER WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 CORROSION WAS FOUND ON THE WING CENTER SECTION UPPER SKIN AREA BETWEEN LBL 67 AND 90. THE WING SKIN WAS CORRODED ABOVE STRINGERS U-1 AND U-2 AND AT THE REAR SPAR. ADDITIONALLY, THERE WAS CORROSION DAMAGE TO THE REAR SPAR CAP, PRESSURE DEC K WEB AND PRESSURE DECK ATTACH ANGLE. TO GAIN ACCESS TO ALL CORRODED AREAS, THE LBL 74.81 LONGTUDINAL FLOORBEAM LOWER C HORD WAS CUT FWD OF STRINGER U-2. 2 L 7 2 4F RT A1NM 1999100800525 19991008 00525 NM 1999 10 8 DL767992179 1 19990915 A 5330 146T32311 SKIN BOEING 767 767232 1385132 NM BS 1465 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 CORROSION DAMAGE WAS NOTED ON THE 146T3231-1 SKIN AT STA 1465 STRINGERS S-27L, S-28L AND 33L. CORROSION DAMAGE WAS ALSO FOUND ON THE 146T8220-1 BULK CARGO LOWER BEAR STRAP AT STA 1461 BETWEEN S-25L AND 26L. 2 L 7 2 4F RT A1NM 1999100800526 19991008 00526 NM 1999 10 8 DL72L992180 1 19990930 A 3350 S106 BATTERIES BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 508DA 21310 BATTERIES WEAK IN FWD COACH CLASS CABIN OVERHEAD EMERGENCY LIGHT. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1999100800527 19991008 00527 NM 1999 10 8 DLM11992181 1 19990930 A 2520 VIDEO UNIT DOUG MD11 MD11 3023602 NM ROW 13G FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 808DE 48479 FLIGHT ATTENDENTS REPORTED VIDEO DISPLAY AT SEAT 13G WAS VERY HOT EVEN THOUGH DISPLAY WAS OFF. NOTICEABLE ELECTRICAL SM ELL WAS NOTICED BY PASSENGERS THROUGHOUT B ZONE. AT SUGGESTION OF ATL MCC TURNED OFF ADB SWITCH. DISPLAY COOLED AND SM ELL DISPAYED. REPLACED DISPLAY UNIT. 2 L 7 3 4F RT A22WE 1999100800528 19991008 00528 WP 1999 10 8 DLL19992182 1 19990921 A 5712 1527033703 RIB LKHEED 1011 10113853 5265020 WP WS 555 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 THE LEFT SIDE WING UPPER RIB CAP AT IWS 555 WAS FOUND CRACKED BETWEEN STRS 15 AND 16, DURING A ROUTINE INSPECTION OF THE RIB CAPS. 2 L 7 3 4F A23WE 1999100800529 19991008 00529 NM 1999 10 8 DLM88992183 1 19991001 A 3244 TIRE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 MLG FAILED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 920DL 23951 49644 725747 ON ROTATION, NR 1 MAIN TIRE RECAP SEPARATED AND FODED OUT THE NR 1 ENGINE. REPLACED TIRE AND ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999100800530 19991008 00530 NM 1999 10 8 DL72E992184 1 19990909 A 5713 STRINGER BOEING 727 727247 138408F NM WS 629 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 AT HMV2, FOUND STRINGER TO RIB CRACKED AT ATTACHMENT HOLES WS 629.0 STR NR 3 MARKED. REMOVED FUEL PROBE REMOVED CLAMPS DISCONTINUED FUEL DUMPD, DRILLED REPAIR MM 57-13-0 FIG 802. INSTALLED REPAIR PER M/M 57-13-0 PG 802, RECONTED CLAMPS AN D TUBE. 2 L 7 3 4F A3WE 1999100800531 19991008 00531 NM 1999 10 8 DL72E992185 1 19990908 A 5754 RIB BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 AT HMV2, RIB CRACKED NR 7 L/E SLAT, NR 5 L/E SUPPORT RIB IS CRACKED AT UPPER LEG. REMOVED FASTENERS AND CLIPS, STOP DRI LLED CRACK MM 57-54-00 FIG 809. REPAIRED PARTS PER SAME, INSTALLED DOUBLER PER 57-54-00. 2 L 7 3 4F A3WE 1999100800532 19991008 00532 NM 1999 10 8 DL72S992186 1 19991001 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223&1235 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 FOUND ON F1 LETTER CK, .25 INCH CRACKS AT LIGHTENING HOLES LT LOWER TORQUE BOX WEB AT STA 1223 AND 1235. REPAIRED PER M M 53-11-0. 2 L 7 3 4F A3WE 1999100800533 19991008 00533 NM 1999 10 8 DL72S992187 1 19991001 A 3350 0201720002 LIGHT BOEING 727 727232 1384082 NM ROW 31 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 517DA 21433 EMERGENCY AISLE LT AT ROW 31 INOP. REPLACED LT ASSY, OPS NML. 2 L 7 3 4F A3WE 1999100800534 19991008 00534 NM 1999 10 8 DL76G992188 1 19991001 A 2120 AIR DIST BOEING 767 767332 1382001 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 1602 29694 SMELL LIKE BURNED PAPER AFTER OPENING AND CLOSING L1 DOOR SEEMS TO BE COMING FROM ABOVE DOOR. INSPECTED ALL ZONES AROUND L1 DOOR WITH ALL LIGHTS AND ROCKWELL SYSTEM ON. NO ODORS, NEITHER EVIDENCE OF HEAT DETECTED. AIRCRAFT OK FOR SE RVICE. 2 L 7 2 4F RT A1NM 1999100800535 19991008 00535 NM 1999 10 8 DLM90992189 1 19991002 A 2150 3965822 VALVE DOUG MD90 MD9030 3023690 NM LT PACK INOP A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 904DA 53384 LT PACK FLOW OF ABOUT 20 PERCENT FLOW LIGHT ON FROM T/O TO 10,000. NO CHANGE IN FLOW PERCENT. RATE OF A/C CLIMBING SLO WED TO 1000 PPM, STILL HAD FLOW LITE. REPLACED LT PACK FLOW CONTROL VALVE. A/C PRESSURIZED GOOD. 2 L 7 2 4F RT A6WE 1999100800536 19991008 00536 NM 1999 10 8 DL72S992190 1 19991002 A 3230 65404676 ACTUATOR BOEING 727 727232 1384082 NM NLG LOCK FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 420DA 21273 NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED NLG LOCK ACTUATOR. 2 L 7 3 4F A3WE 1999100800537 19991008 00537 NM 1999 10 8 DL767992192 1 19991003 A 2910 17014110CR0720S HOSE BOEING 767 767232 1385132 NM LT MLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 107DL 22219 ON DEPARTURE, UNABLE TO RETRACT LT MAIN LANDING GEAR. RETRACTION OF OTHER GEAR NORMAL. WITH HANDLE IN UP MODE, HAD GRE EN LT MAIN LIGHT AND AMBER GEAR LIGHT AND AMBER DOOR LIGHT. EICAS GEAR DISAGREE AND GEAR DOOR MSG'S. FOUND LT GEAR LEV ELING CYLINDER RETURN LINE LEAKING. REPLACED LINE. LEAK CHECKED SATISFACTORY. RESET FUSE PER M/M 32-32-19-4-00. 2 L 7 2 4F RT A1NM 1999100800538 19991008 00538 NM 1999 10 8 DL76G992194 1 19991003 A 3350 POWER SUPPLY BPS73 BOEING 767 7673P6 1385105 NM 1R DOOR INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 154DL 2339 25241 EMERGENCY EXIT SIGN AT 1R DOOR INOP. REPLACED POWER SUPPLY, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999100800539 19991008 00539 NM 1999 10 8 DL72S992195 1 19991003 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM ROW 27 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 482DA 20862 LEFT AFT EMERGENCY OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS NOW OK . 2 L 7 3 4F A3WE 1999100800540 19991008 00540 NM 1999 10 8 DL72W992196 1 19991003 A 2611 72130001008 SMOKE DETECTOR BOEING 727 727247 138408F NM RT LAVATORY DEFECTIVE A DALA K NONE N FALSE WARNING CR CRUISE 1 SO 27 293WA 22111 LAV SMOKE LIGHT ILLUMINATED IN FLIGHT. TWICE AT AFT LAVS. WENT OUT ON OWN FIRST TIME. HAD TO PULL CB 2ND TIME. REPLA CED AFT RT LAV SMOKE DETECTOR. 2 L 7 3 4F A3WE 1999100800541 19991008 00541 NM 1999 10 8 DL72S992197 1 19991004 A 2751 9660022001 TRANSMITTER BOEING 727 727232 1384082 NM TE FLAPS FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 516DA 21432 OUTBOARD FLAPS SPLIT WHEN FLAPS RETRACTED FROM 5 DEGS. REPLACED RIGHT OUTBOARD FLAP TRANSMITTER. 2 L 7 3 4F A3WE 1999100800542 19991008 00542 NM 1999 10 8 DL72E992198 1 19991004 A 5311 FRAME BOEING 727 727247 138408F NM BS 783.95 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 THE LT FS 783.95 OVERWING EXIT FRAME WAS FOUND CRACKED AT HMV. THE DAMAGE WAS REPAIRED PER ERA 333610-14AD. 2 L 7 3 4F A3WE 1999100800543 19991008 00543 NM 1999 10 8 DL72E992199 1 19991004 A 5330 6554583126 DOUBLER BOEING 727 727247 138408F NM FUSELAGE TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 THE AFT LAV SERVICE PANEL DOUBLER WAS FOUND TORN DURING MODIFICATION PER EO 4-69078-3AD. THE DAMAGE WAS REPAIRED PER ER A 333642-14 AT HMV. 2 L 7 3 4F A3WE 1999100800544 19991008 00544 NM 1999 10 8 DL72E992200 1 19991004 A 5330 65182175 SKIN BOEING 727 727247 138408F NM BS 360-481 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 CRACK INDICATIONS WERE FOUND IN THE FUSELAGE SKIN LAP AT STRINGER 4L BETWEEN FS 360 AND FS 481. THE DAMAGE WAS REPAIRED PER ERA 333599-14AD AT HMV. 2 L 7 3 4F A3WE 1999100800545 19991008 00545 NM 1999 10 8 DL72E992201 1 19991004 A 5730 65877421 SKIN BOEING 727 727247 138408F NM BS 820 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 THE WING CENTER SECTION LOWER SKIN WAS FOUND CORRODED AT FS 820 AND RBL 13. THE DAMAGE WAS REPAIRED PER ERA 333611-14AD AT HMV. 2 L 7 3 4F A3WE 1999100800546 19991008 00546 NM 1999 10 8 DL72E992202 1 19991004 A 5711 651620261 SPAR BOEING 727 727247 138408F NM CENTER WING MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 282WA 21484 ONE FASTENER HOLE WAS MISDRILLED AND ELONGATED IN THE WING CENTER SECTION REAR SPAR WEB AT APPROXIMATELY LBL 41 DURING T HE ACCOMPLISHMENT OF A MODIFICATION TO THE WEB. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333636-14AD. 2 L 7 3 4F A3WE 1999100800547 19991008 00547 WP 1999 10 8 DLL14992203 1 19991002 A 3230 RETRACT MECH 2680262M6 LKHEED 1011 1011385115 5265015 WP LANDING GEAR INOP A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 736DY DL2RW1 193C1227 LANDING GEAR WOULD NOT RETRACT INTRANSIT LIGHT REMAINED ON. REMOVED AND REPLACED 4-WAY 3 POSITION VLV. GEAR SWING COMP LETED ALL INDICATIONS NORMAL. 2 L 7 3 4F A23WE 1999100800548 19991008 00548 NM 1999 10 8 DL733992206 1 19991005 A 5330 655298878 SKIN BOEING 737 737347 1384647 NM BS 970 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313WA 23599 THE FUSELAGE SKIN WAS GOUGED AT FS 970, ELEVEN INCHES BELOW THE R2 DOOR AT STRINGER 19L. THE DAMAGE WAS FOUND AT AMV AN D REPAIRED PER ERA 333671-14. 2 L 7 2 4F RT A16WE 1999100800549 19991008 00549 WP 1999 10 8 DLL19992207 1 19990924 A 5330 1608990 SKIN LKHEED 1011 10113853 5265020 WP BS 1551 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 CORROSION WAS FOUND AT STA 1551 AND LONGERON 31. DAMAGE INCLUDES LONGERON 31, BONDED SKIN ASSY AND DOOR SURROUND TRIPLE R ALL DAMAGE LOCATIONS WERE ATTRIBUTED TO CORROSION. 2 L 7 3 4F A23WE 1999100800550 19991008 00550 NM 1999 10 8 DLM88992208 1 19991005 A 2560 3961899501 LANYARD DOUG MD88 MD88 3023688 NM L1 DOOR BROKEN A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 982DL 53273 AT DEPARTURE TIME, F/A FOUND LANYARD BROKEN ON L-1 DOOR SLIDE GIRT BAR. REPLACED LANYARD ASSY. 2 L 7 2 4F RT A6WE 1999100800551 19991008 00551 1999 10 8 DL76G992209 4 19991005 A 2370 VIDEO UNIT 1301273111 BOEING 767 767332 1382001 NM ROW 5 A-B FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 16065 9810001862 30199 ON LAYOVER, SEAT 5 A-B AVU OVERHEATED. REMOVED AND REPLACED AVU AND SEAT B MONITOR CABLE. 2 L 7 2 4F RT A1NM 1999100800552 19991008 00552 NM 1999 10 8 DL72S992211 1 19991003 A 5711 65192923 SPAR WEB BOEING 727 727232 1384082 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 CENTER WING, REAR SPAR, WEB LBL 17, CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A .5 TYPICAL CRACK NEAR THE UPPER SPAR CAP. THE CRACK IS TYPICAL OF BAC S/B 727-57A0182. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 368400-14AD, REV A. 2 L 7 3 4F A3WE 1999100800553 19991008 00553 WP 1999 10 8 DLL19992212 1 19991004 A 5320 1559196103 INTERCOSTAL LKHEED 1011 10113853 5265020 WP BS 1796 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 769DL 193H1218 FUSELAGE, L3 DOOR SURROUND, NR 6 DOOR STOP INTERCOSTAL, CRACK REPAIR. THE SUPPORT INTERCOSTAL FOR THE NR 6 DOOR STOP OF THE L3 DOOR CUTOUT FRAME AT FS 1796 WAS FOUND WITH A .25 TYPICAL CRACK. THE CRACK IS TYPICAL OF LAC S/B 093-53-270. T HE CRACK WAS LET GO ON A TIME-LIMITED BASIS PER THE S/B AND PER ER/A 368408-14 WITH REPETITIVE INPSECTIONS AND 2500 CYCL E LIMIT. PERMANENT REPAIR WILL REPLACE THE INTERCOSTAL. 2 L 7 3 4F A23WE 1999100800554 19991008 00554 NM 1999 10 8 DL767992213 1 19991004 A 5312 148T27409 BULKHEAD CHORD BOEING 767 767232 1385132 NM BS 1809.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 113DA 22225 FUSELAGE BULKHEAD FS 1809.5, LBL 45 OUTER CHORD, CRACK REPAIR. THE FS 1809.5 BULKHEAD OUTER CAP WAS FOUND WITH A TYPICA L CRACK AT LBL 45. THE CRACK IS TYPICAL OF BAC S/B 767-53-0078. THE CRACKED SECTION OF CHORD WAS REMOVED AND A NEW SEC TION SPLICED IN PER THE S/B AND ER/A 368414-14. 2 L 7 2 4F RT A1NM 1999100800555 19991008 00555 NM 1999 10 8 DL767992214 1 19991005 A 5313 147T30048 STRINGER BOEING 767 767232 1385132 NM BS 1010 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 102DA 22214 FUSELAGE STRINGER S-21AR, BS 1010, RBL 97.42, CORROSION REPAIR. STRINGER 21AR WAS FOUND WITH EXTENSIVE CORROSION AT FS 1010 AND RBL 97.42. THE STRINGER FORMS AN END CAP FOR THE MLG HORIZONTAL PRESSURE BULKHEAD. THE CORROSION WAS REMOVE D WITH A 5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO STEEL REPAIR ANGLES AND A REPAIR STRAP PER ER/A 368364-14, REV A. 2 L 7 2 4F RT A1NM 1999100800556 19991008 00556 NM 1999 10 8 DL72L992215 1 19990809 A 5753 652163387 SKIN BOEING 727 727232 1384082 NM LT TE MID FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 DURING SHOP VISIT, THE OB LE UPPER SKIN WAS FOUND WITH WORN AREA APPROX 3 INCH LONG AT OB END. THE SKIN WAS REPAIRED PE R MM 57-52-0, FIG 803 BY REMOVING THE DAMAGED SKIN AND INSTALLING A SKIN FILLER AND DOUBLER. 2 L 7 3 4F A3WE 1999100800557 19991008 00557 NM 1999 10 8 DL72L992216 1 19990809 A 5753 652163387 SKIN BOEING 727 727232 1384082 NM LT TE MID FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 DURING SHOP VISIT, THE LEADING EDGE OF THE UPPER SKIN WAS FOUND WORN AT THE IB END APPROX 3 LONG. THE SKIN WAS REPAIRE D PER MM 57-52-0, FIG 803 BY REMOVING THE DAMAGE AND INSTALLING A SKIN FILLER AND DOUBLER. 2 L 7 3 4F A3WE 1999100800558 19991008 00558 NM 1999 10 8 DL73K992217 1 19991002 A 5330 SKIN BOEING 737 737232 1384475 NM BS 345 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 FUSELAGE, SKIN ASSY, L1 DOOR CUTOUT, CRACK REPAIR. A CRACK WAS FOUND IN THE SKIN, DOUBLER, AND BEAR STRAP AT THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS REPAIRED WITHIN INTERIM S TRAP REPAIR PER THE S/B AND PER ER/A 368397-14. 2 L 7 2 4F RT A16WE 1999100800559 19991008 00559 NM 1999 10 8 DL73E992218 1 19991004 A 5330 65458001205 SKIN BOEING 737 737247 138448D NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 FUSELAGE, SKIN ASSY, R1 DOOR CUTOUT, LOWER AFT CORNER, CRACK REPAIR. THE FUSELAGE SKIN, DOUBLER, AND BEAR STRAP WERE FO UND WITH A 1.5 CRACK AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT. THE CRACK WAS REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERSPER B737 SRM 53-30-3, FIG 26 AND ER/A 368409-14. 2 L 7 2 4F A16WE 1999100800560 19991008 00560 NM 1999 10 8 DL72S992219 1 19991005 A 5754 RIB BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FOUND ON D1 LETTER CK, NR 1 SLAT L/E NOSE RIB CRACKED 1.5 INCH AT I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999100800561 19991008 00561 NM 1999 10 8 DL72S992220 1 19991005 A 5720 STIFFNER BOEING 727 727232 1384082 NM LT LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FOUND ON D1 LETTER CK, NR 4 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999100800562 19991008 00562 NM 1999 10 8 DL72S992221 1 19991005 A 5720 CASTING BOEING 727 727232 1384082 NM LT TE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FOUND ON D1 LETTER CK, NR 4 SLAT ACTUATOR I/B MOUNT CASTING CRACKED. REPLACED CASTING. 2 L 7 3 4F A3WE 1999100800563 19991008 00563 WP 1999 10 8 K4HA99075 1 19990817 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 910 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION. MATERIAL LOSS OF 68 PERCENT IN AN AREA 5 BY 3 OF THICKNESS CHECK. REMOVED CORROSION IAW L1011 SRM 51-21-01. REMOVED DAMAGED SECTION IAW L1011 SRM 53 -31-00 FIGURE 803. FABRICATE REPAIR PARTS IAW L1011 53-31-00 FIG 803 M-59. OK TO TREAT AND PRIME REPAIR AREA. TREATED AND PRIMED REPAIR AREA IAW L1011 SRM 51-21-02 MM 20-57-09. OK TO INSTALL REPAIR. INSTALLED REPAIR IAW L1011 SRM 53-31 -00 FIG 802 2 L 7 3 4F A23WE 1999100800564 19991008 00564 WP 1999 10 8 K4HA99076 1 19990817 A 5347 SEAT TRACK LKHEED 1011 1011385115 5265015 WP CABIN CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION. SEAT TRACK FLANGE CRACKED AND CORRODED APPROXIMATELY 8 INCHES. REMOVED DAMAGE IAW L1011 SRM 53-21-00 FIG 808. FABRICATE REPAIR DOUBLER IAW L1011 SRM 53-21-00. INSTALLED REPAIR IAW L1011 SRM 53-21-00 FIG 808. 2 L 7 3 4F A23WE 1999100800565 19991008 00565 EU 1999 10 8 RAIA9910008 1 19991005 A 3260 DN10502MK2 BRACKET BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA L ABORTED APPROACH P NO WARNING INDICATION DE DESCENT 1 CE 03 338TE 932 7336- STL - NOSE LANDING GEAR DID NOT COME DOWN IN APPROX 20 SECONDS, DID GO AROUND, CYCLED GEAR, AFTER APRROX 15 SECOND S GOT 3 GREEN. MAINTENANCE REPLACED NOSE GEAR DOWNLOCK SWITCH BRACKET. 2 L 7 2 4T RT A56EU 1999100800566 19991008 00566 EU 1999 10 8 RAIA9910009 1 19991005 A 3241 AC63740 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RT BRAKE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 879 7102 - STL - RIGHT BRAKE DOESN'T WORK. MAINTENANCE REPLACED RIGHT BRAKE ANTI-SKID TRANSDUCER. 2 L 7 2 4T RT A56EU 1999100800567 19991008 00567 WP 1999 10 8 AT9900642 1 19990824 A 5280 SKIN DOUG DC9 DC932 3022066 WP LT MLG DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE LEFT SIDE MAIN LANDING GEAR FLYING DOOR SKIN WAS FOUND TO BE CORRODED. FABRICATED SKIN REPAIR AND INSTALLED A DOUBLER REPAIR IAW DC9 SRM 52-05 FIG 1, 51-10-03, 51-30-02. 2 L 7 2 4F A6WE 1999100800568 19991008 00568 WP 1999 10 8 AT9900643 1 19990819 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND THE UPPER AND LOWER SURFACES OF THE CABIN FLOOR PANEL AT BS 160-200 CORRODED. FABRICATED AND INSTALLED NEW SKIN PANEL IAW DC9 SRM 53-05, 53-20, 51-30-2. 2 L 7 2 4F A6WE 1999100800569 19991008 00569 WP 1999 10 8 AT9900644 1 19990918 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND THE RIGHT SIDE CABIN FLOOR PANEL AT BS 200-237 CORROD ED. FABRICATED NEW PANELS AND INSTALLED NEW HAT CHANNELS IAW DC9 SRM 53-05, 51-10-04, 51-10-03, 51-30-02, 53-21-0. 2 L 7 2 4F A6WE 1999100800570 19991008 00570 WP 1999 10 8 AT9900645 1 19990818 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE RIGHT SIDE FORWARD CABIN FLOOR PANEL AT BS 200-237 WAS FOUND TO BE CORRODED. FABRICATED NEW PANEL AND INSTALLED HAT CHANNELS IAW DC9 SRM 53-21, 51-10-02, 51-10-03, 51-30-02. 2 L 7 2 4F A6WE 1999100800571 19991008 00571 WP 1999 10 8 AT9900646 1 19990818 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE FLOOR PANEL AT BS 160-200 WAS FOUND TO BE CORRODED. FA BRICATED AND INSTALLED NEW SKIN PANEL IAW DC9 53-21, 51-10-04, 51-10-03, 51-30-02. 2 L 7 2 4F A6WE 1999100800572 19991008 00572 WP 1999 10 8 AT9900647 1 19990816 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE LEFT SIDE CABIN FLOOR PANEL AT BS 200-237 WAS FOUND TO BE CORRODED. FABRICATED NEW SKIN PANEL AND INSTALLED HAT CHANNELS IAW DC9 SRM 53-21, 51-10-04, 51-10-03, 51-10-02. 2 L 7 2 4F A6WE 1999100800573 19991008 00573 WP 1999 10 8 AT9900648 1 19990831 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE FORWARD CABIN FLOOR SUPPORT AT BS 200 BL 0 WAS FOUND TO BE CORRODED. FABRICATED AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-02, 51-10-04. 2 L 7 2 4F A6WE 1999100800574 19991008 00574 WP 1999 10 8 AT9900649 1 19990813 A 5321 FLOOR DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE COCKPIT FLOORBOARD BETWEEN THE CAPTAIN AND FIRST OFFICE R BY THE INBOARD SEAT TRACKS WAS FOUND TO BE CORRODED. FABRICATED AND INSTALLED REPAIR PANEL IAW DC9 SRM 51-30-02, 51-1 0-02, 51-10-03, 51-10-04, 51-30-01. 2 L 7 2 4F A6WE 1999100800575 19991008 00575 WP 1999 10 8 AT9900650 1 19990812 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS. 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE RIGHT SIDE CABIN FLOOR PANEL AT BS 160 - 200 WAS FOUND TO HAVE CORROSION. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 53-21 FIGURE 2E. 2 L 7 2 4F A6WE 1999100800576 19991008 00576 WP 1999 10 8 AT9900651 1 19990821 A 5320 99188741 SUPPORT DOUG DC9 DC932 3022066 WP BS 165 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE CABIN FLOOR PLATE AT BS 163 LEFT BL 11 WAS FOUND TO HAV E CORROSION. REMOVED AND REPLACED BEARING PLATE IAW DC9 51-30-02. 2 L 7 2 4F A6WE 1999100800577 19991008 00577 WP 1999 10 8 AT9900652 1 19990820 A 5260 ANGLE DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND EXFOLIATED CORROSION ON 5TH STEP FROM THE TOP OF THE AFT AIR STAIRS AT THE RIGHT HAND SUPPORT ANGLE. REMOVED AND REPLACED SUPPORT ANGEL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999100800578 19991008 00578 WP 1999 10 8 AT9900653 1 19990904 A 5320 5919752501 BALANCE WT DOUG DC9 DC932 3022066 WP LT ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND LEFT OUTBOARD ELEVATOR BALANCE WEIGHT HAS SEVERAL AREAS OF CH IPPED PAINT AND CORROSION GOUGES. REMOVED AND REPLACED BALANCE WEIGHT, REMOVED AND REPLACED COVER IAW DC9 SRM 51-30-1, 51-10-4 - 51-10-3. 2 L 7 2 4F A6WE 1999100800579 19991008 00579 WP 1999 10 8 AT9900654 1 19990908 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 210 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND DENT AT BS 210. FABRICATED AND INSTALLED REPAIR DOUBLER IAW TIMCO RES NR 07634 AND DC9 SRM 53-04. 2 L 7 2 4F A6WE 1999100800580 19991008 00580 WP 1999 10 8 AT9900655 1 19990905 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND FORWARD ENTRY SUBFLOOR PANELS AND SUPPORT BRACKEST AT BS 160- 200 LBL 56 - RBL 56 CORRODED. REPLACED 3 PANELS, REMOVED AND REPLACE SUPPORT BRACKET, REPLACED RETAINER PLATE, REMOVED AND REPLACED DOUBLER AT SUBFLOOR IAW DC9 SRM 51-30-1, 51-30-5, 51-30-2, 51-10-3. 2 L 7 2 4F A6WE 1999100800581 19991008 00581 WP 1999 10 8 AT9900656 1 19990908 A 5330 591486529N SKIN DOUG DC9 DC932 3022066 WP BS 609 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND LOWER FUSELAGE SKIN BULGED AT BS 609 AND L30L. REMOVED AND R EPLACED END FITTINGS AND REPAIRED T CHORDS ON L28L AND L30L IAW DC9 SRM 53-03, FIGURE 10. 2 L 7 2 4F A6WE 1999100800582 19991008 00582 WP 1999 10 8 AT9900657 1 19990909 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 650-654 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND LOWER FUSELAGE SKIN BULGED AT LONGERON 30 BS 605-654. FABRIC ATED AND INSTALLED EXTERNAL REPAIR IAW DC9 SRM 53-01, FIGURE 2, 51-30-1, 51-10-3. 2 L 7 2 4F A6WE 1999100800583 19991008 00583 WP 1999 10 8 AT9900658 1 19990912 A 5260 9915570149 STEP DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND AFT VENTRAL STAIRS 5TH STEP FROM TOP. VERTICAL RISER ON STEP CORRODED. REMOVED AND REPLACED STEP IAW DC9 SRM 51-30-1, 52-01 FIGURE 1. 2 L 7 2 4F A6WE 1999100800584 19991008 00584 WP 1999 10 8 AT9900659 1 19990812 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 161-198 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND FLOOR SUPPORT AT BS 161 - 198 AND LBL 44 CORRODED. FABRICATE D AND INSTALLED REPAIR SUPPORT IAW DC9 SRM 51-10-3, 51-10-2, 51-10-4, 51-10-5. 2 L 7 2 4F A6WE 1999100800585 19991008 00585 WP 1999 10 8 AT9900660 1 19990812 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND CABIN FLOOR SUPPORT AT BS 200 LBL 44 - 56 CORRODED. REMOVED FLOOR SUPPORT, FABRICATED, REPAIRED AND INSTALLED REPAIR SUPPORT IAW DC9 SRM 51-30-2, 51-10-2, 51-10-3, 51-10-4, 51-30-5 . 2 L 7 2 4F A6WE 1999100800586 19991008 00586 WP 1999 10 8 AT9900661 1 19990812 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND CABIN FLOOR SUPPORT AT BS 200 LBL 1 - 20 CORRODED. REMOVED F LOOR SUPPORT, FABRICATED, REPAIRED AND INSTALLED REPAIR SUPPORT IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-5. 2 L 7 2 4F A6WE 1999100800587 19991008 00587 WP 1999 10 8 AT9900662 1 19990907 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 305-362 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND RT OUTER FLOOR PANEL NR 39 HAS ELONGATED HOLES AND CORROSION. FABRICATED NEW FLOOR PANEL SKIN AND REINSTALLED HAT CHANNELS IAW DC9 SRM 53-21-0, 51-70-3. 2 L 7 2 4F A6WE 1999100800588 19991008 00588 WP 1999 10 8 AT9900663 1 19990813 A 2720 3925170505 SWITCH DOUG DC9 DC932 3022066 WP RUDDER LIMITER CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO, LAKE CITY FL FOUND RUDDER LIMITER STOP ASSEMBLY CORRODED. REMOVED AND REPLACED AUXILIARY RUDDER THROW LIMITER STOP ASSEMBLY IAW DC9 MM 27-20-11, 27-20-0. 2 L 7 2 4F A6WE 1999100800589 19991008 00589 WP 1999 10 8 AT9900664 1 19990907 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND RT OUTER FLOOR PANEL NR 40 HAS ELONGATED HOLES AND CORROSION. FABRICATED NEW FLOOR PANEL IAW DC9 SRM 51-30-21, 51-10-2/-3/-4. 2 L 7 2 4F A6WE 1999100800590 19991008 00590 WP 1999 10 8 AT9900665 1 19990907 A 5321 FLOOR DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND FLOOR PANEL AT REAR OF COCKPIT, BETWEEN ELECTRICAL PANEL AND RIGHT SIDE WALL CORRODED. REMOVED, FABRICATED NEW SKIN. INSTALLED CHANNELS ON SKIN AND INSTALLED PANEL IAW DC9 SRM 51- 10-3, 51-10-4, 51-30-2. 2 L 7 2 4F A6WE 1999100800591 19991008 00591 WP 1999 10 8 AT9900666 1 19990905 A 5320 991007813 CUSP DOUG DC9 DC932 3022066 WP R1 DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND CORROSION AT LOWER EDGE FORWARD SERVICE DOOR CUTOUT BETWEEN S KIN AND DOUBLER. REMOVED AND REPLACED R1 DOOR CUSP IAW DC9 SRM 53-05 FIGURE 55, 51-30-1, 51-30-5. 2 L 7 2 4F A6WE 1999100800592 19991008 00592 WP 1999 10 8 AT9900667 1 19990914 A 5260 ANGLE DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND LEFT HAND AND RIGHT HAND OUTBOARD SUPPORT ANGLES FOR THE AIR STAIRS, 4TH STEP FROM THE TOP CORRODED. REMOVED, FABRICATED AND INSTALLED 2 SUPPORT ANGLES IAW DC9 SRM 51-10-2, 51-10-3 , 51-10-4, 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999100800593 19991008 00593 WP 1999 10 8 AT9900668 1 19990910 A 5260 INTERCOSTAL DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND AFT AIR STAIRS STEP NR 6 INTERCOSTAL CORRODED. FABRICATED AN D INSTALLED REPAIR INTERCOSTAL SUPPORT IAW DC9 SRM 51-10-2, 51-10-2A, 51-30-1, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1999100800594 19991008 00594 WP 1999 10 8 AT9900669 1 19990814 A 5260 2648233 INTERCOSTAL DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO, LAKE CITY FL, FOUND AFT AIR STAIRS STEP NR 6 INTERCOSTAL CORRODED. FABRICATED A ND INSTALLED REPAIR INTERCOSTAL SUPPORT IAW DC9 SRM 51-10-2, 51-10-2A, 51-30-1, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1999100800595 19991008 00595 WP 1999 10 8 AT9900670 1 19990918 A 5330 76378133 SKIN DOUG DC9 DC932 3022066 WP BS 332-362 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND THE SKIN PANEL AT BS 332 - 362 L18R TO L26R CORRODED. A CLAS S II TEMP REPAIR INSTALLED IN THE AREA. REMOVED SKIN, FABRICATED AND INSTALLED SKIN REPAIR IAW EO 99-123-9. 2 L 7 2 4F A6WE 1999100800596 19991008 00596 WP 1999 10 8 AT9900671 1 19990910 A 5260 39186471 SUPPORT DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND THE AFT VENTRAL STAIRWAY CENTER HANDRAIL SUPPORT CORRODED. R EMOVED AND REPLACED HANDRAIL SUPPORT IAW DC9 SRM 52-63-0. 2 L 7 2 4F A6WE 1999100800597 19991008 00597 WP 1999 10 8 AT9900681 1 19990810 A 5755 SKIN DOUG DC9 DC932 3022066 WP RT SPOILER DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT LAKE CITY, FL, FOUND RIGHT HAND WING I/B SPOILER TOP SURFACE WAS DELAMINATED. REPAIRED RIGHT HAND WING I/B SPOILER, INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW DC9 SRM 51-70-2, 51-10-3, 57-50-4 FIGURE 1 AN D TIMCO RES-1 08381. 2 L 7 2 4F A6WE 1999100800598 19991008 00598 WP 1999 10 8 AT9900682 1 19990814 A 5620 WINDOW DOUG DC9 DC932 3022066 WP FUSELAGE LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT HAND WINDOW NR 18 HAD 2 LIGHTNING STRIKES AT TOP FOR WARD AND AFT CORNER. REPAIRED LIGHTNING STRIKES ON WINDOW NR 18 AND INSTALLED REPAIR DOUBLER IAW TIMCO EO 99-1240 REV I R DATED 990903. 2 L 7 2 4F A6WE 1999100800599 19991008 00599 WP 1999 10 8 AT9900683 1 19990814 A 5620 WINDOW DOUG DC9 DC932 3022066 WP FUSELAGE LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT HAND WINDOW NR 22 HAS LIGHTNING STRIKES AT AFT TOP C ORNER. REPAIRED LIGHTNING STRIKES ON WINDOW NR 22 IAW TIMCO EO 99-1240 REV IR DATED 990903. 2 L 7 2 4F A6WE 1999100800600 19991008 00600 WP 1999 10 8 AT9900684 1 19990813 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 485-414 DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT WING UPPER TRAILING EDGE PANEL XRS485-XRS414 WAS DELA MINATED. REPAIRED LEFT WING UPPER TRAILING EDGE PANEL WITH BONDED PANEL AT XRS485-XRS414 IAW DC9 SRM 51-10-3, 51-30-4, 57-04-1, 57-01 FIGURE 1 AND EO 99-1236 REV IR DATED 990907. 2 L 7 2 4F A6WE 1999100800601 19991008 00601 WP 1999 10 8 AT9900685 1 19990812 A 5620 WINDOW DOUG DC9 DC932 3022066 WP FUSELAGE LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND WINDOW NR 8, 70, 72, AND 66 HAD 2 LIGHTNING STRIKES ON LOW ER FRAME. REPAIRED LIGHTNING STRIKES ON WINDOW NR 8, 70, 72, AND 66 BY BLENDING IAW TIMCO EO 99-1240 REV IR DATED 99090 3. 2 L 7 2 4F A6WE 1999100800602 19991008 00602 WP 1999 10 8 AT9900686 1 19990811 A 5730 PANEL DOUG DC9 DC932 3022066 WP WS 353-477 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT HAND O/B UPPER TRAILING EDGE PANEL XRS353-XRS477 WAS CORRODED AND DELAMINATED. REPAIRED RIGHT HAND WING O/B UPPER TRAILING EDGE, INSTALLED NEW CORE INNER DOUBLER SKIN IAW TIMCO EO 99-1235 REV IR DATED 990901. 2 L 7 2 4F A6WE 1999100800603 19991008 00603 WP 1999 10 8 AT9900687 1 19990811 A 5730 PANEL DOUG DC9 DC932 3022066 WP WS 335-477 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT WING O/B UPPER TRAILING EDGE PANEL XRS335-XRS477 WAS CORRODED AND DELAMINATED. REPAIRED LEFT HAND WING O/B UPPER TRAILING EDGE PANEL IAW TIMCO EO 99-1245 REV IR DATED 99090 7. 2 L 7 2 4F A6WE 1999100800604 19991008 00604 WP 1999 10 8 ATT9900673 1 19990927 A 7931 42D110 SWITCH DOUG DC9 DC932 3022066 WP NR 2 ENGINE FAILED A ZZDA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 15 839AT 47089 SHUTDOWN NR 2 ENGINE IN FLIGHT DUE TO OIL QUANTITY LOSS. FOUND OIL PRESSURE SWITCH DISINTEGRATED. 2 L 7 2 4F A6WE 1999100800605 19991008 00605 NM 1999 10 8 AWXA9900337 1 19990610 A 5311 6549591 RIB BOEING 737 7372M8 1384483 NM WS 185.5 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 C-CHECK, 2 INCH CRACK ON I/B UPPER ANGLE ON LEADING EDGE INT OF I/B FRAME AT WS 185.5 RT WING OF PYLON. REMOVED, FABRIC ATED, HEAT TREATED TO T3 COND, ALODINED AND REPLACED RIB IAW SRM 57-20-2 AND 57-30-2. 2 L 7 2 4F A16WE 1999100800606 19991008 00606 NM 1999 10 8 AWXA9900338 1 19990602 A 5330 6545774 SKIN BOEING 737 7372M8 1384483 NM BS 727&773 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 C-CHECK, LT FUSLAGE CRACK AT SR17L. ALSO, LT WTB BETWEEN 2ND AND 3RD REPAIR, 4 TO 5 INCHES LONG. BOTH PLACES FABRICATE D NEW REPAIR FROM 2024T3 .090 R646704 IAW SRM 53-30-3 FIG 1. TREATED AND PRIMED NEW REPAIR AND AREA, INSTALLED REPAIR D OUBLER PER 53-30-3 FIG 1. 2 L 7 2 4F A16WE 1999100800607 19991008 00607 NM 1999 10 8 AWXA9900339 1 19990602 A 5330 6552988 SKIN BOEING 737 7372M8 1384483 NM BS 950-970 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 C-CHECK, APPROX 2.5 INCH CRACK ON FUSLAGE SKIN 3.5 FT BELOW L-2 DOOR. REMOVED EXISTING DOUBLER PER SRM 51-40-2, CUTOUT DAMAGE PER PT6 51-00-00 FIG 23. FABRICATED DOUBLER AND INSTALLED PER SRM 53-30-1 FIG 1 AND 51-30-2 MATL 2024TB .090. 2 L 7 2 4F A16WE 1999100800608 19991008 00608 NM 1999 10 8 AWXA9900340 1 19990603 A 5320 693535213 TIE CLIP BOEING 737 7372M8 1384483 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 C-CHECK, STRINGER TIE CLIP CRACKED, 16L FS 727A. REMOVED STRINGER TIE CLIP IAW SRM 51-30-2, FAB'D NEW STRINGER TIE CLIP IAW 51-10-1. TREATED AND PRIMED NEW CLIP IAW SRM 51-10-2. 2 L 7 2 4F A16WE 1999100800609 19991008 00609 NM 1999 10 8 AWXA9900341 1 19990602 A 5720 6549591 ANGLE BOEING 737 7372M8 1384483 NM WS 185.5 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 C-CHECK, .75 INCH CRACK ON UPPER ANGLE OF LT WING L/E RIB I/B SIDE OF NR 1 ENG PYLON. FABRICATED AND INSTALLED REPAIR P ART AT WING STA 185.5 IAW 51-30-00, MATERIAL 2024-0 .063 HEAT TREATED TO 2024-T4. 2 L 7 2 4F A16WE 1999100800610 19991008 00610 NM 1999 10 8 UPS99230805 1 19990925 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1010 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-03) ON STA 1010 FLOORBEAM UP AND LWR SIDE OF UPPER CHORD AREA MARKED. REMO VED AND REPLACED DAMAGED SECTION OF FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999100800611 19991008 00611 NM 1999 10 8 UPS99230806 1 19990824 A 5320 CLIP BOEING 727 72725C 138400H NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION ON STRINGER CLIP AT BS 1130, STR 27L. REMOVED CLIP, FABRICATED, HEAT TREATED AND INSTALLE D STRINGER CLIP PER SRM 51-30-2, PG 8 & 9, MM 51-20-151. 2 L 7 3 4F A3WE 1999100800612 19991008 00612 NM 1999 10 8 UPS99230807 1 19990924 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-224-03.00-01) UNDER NUT PLATES ON BS 680 FLOORBEAM RBL 35, WL 208. REMOVED CORROSION AND REPLACED TOP CHORD FROM RBL 65, TO LBL 65. 2 L 7 3 4F A3WE 1999100800613 19991008 00613 NM 1999 10 8 UPS99230808 1 19990924 A 5320 WEB BOEING 727 72725C 138400H NM BS 251.6 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-221-01.03-01) ON WEB AT BS 251.6 LT WL 216 AFT SIDE AREA MARKED. REMOVED CORROSION A ND REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1999100800614 19991008 00614 NM 1999 10 8 UPS99230809 1 19990825 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION ON FLOORBEAM LOWER SURFACE HOLE BS 560, WL 208, LBL 5. REPAIRED CORRODED FLOORBEAM IAW SR M 53-10-08. 2 L 7 3 4F A3WE 1999100800615 19991008 00615 NM 1999 10 8 UPS99230810 1 19990929 A 3350 BATTERY PACK BOEING 727 727180C 138406G NM FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:N/A, CHECKED EMERGENCY LIGHT SYSTEM, FOUND FLIGHT DECK EMERGENCY LIGHT INOP. REPLACED FLIGHT DECK EMERG ENCY LIGHT BATTERIES AS PER MM 33-50-101 PAGE 201. 2 L 7 3 4F A3WE 1999100800616 19991008 00616 NM 1999 10 8 UPS99230811 1 19990928 A 3350 BATTERY PACK BOEING 727 727180C 138406G NM FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERIES A S PER MM 33-50-101 PAGE 201. 2 L 7 3 4F A3WE 1999100800617 19991008 00617 WP 1999 10 8 UPS99830774 1 19990912 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 341.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E AT FS 341.5, THE INTERNAL DOUBLER HAD A 7 INCH CRACK. REPAIRED THE DOUBLER IAW DH SK7 18-263. 2 L 7 4 4F RT 4A25 1999100800618 19991008 00618 WP 1999 10 8 UPS99830775 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 195 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT FS 195.0 WAS CRACKED AT THE AFT LWR END. REPAIRED THE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999100800619 19991008 00619 WP 1999 10 8 UPS99830776 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 227.335 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT FS 227.335 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIR ED THE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999100800620 19991008 00620 WP 1999 10 8 UPS99830777 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 335.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIB AT FS 335.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRE D THE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999100800621 19991008 00621 WP 1999 10 8 UPS99830778 1 19990916 A 5720 576960041 DOUBLER DOUG DC8 DC871F 302199D WP WS 570.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT FS 570.5 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND R EPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1999100800622 19991008 00622 WP 1999 10 8 UPS99830779 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 835 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT FS 835 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999100800623 19991008 00623 WP 1999 10 8 UPS99830780 1 19990915 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 336.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E LWR SKIN INTERNAL DOUBLER AT FS 336.75 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRIC ATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769589 AND SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1999100800624 19991008 00624 WP 1999 10 8 UPS99830781 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 735 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIB AT FS 735 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999100800625 19991008 00625 WP 1999 10 8 UPS99830782 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 297.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIB AT FS 297.5 WAS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999100800626 19991008 00626 WP 1999 10 8 UPS99830783 1 19990916 A 5720 97532978 ANGLE DOUG DC8 DC871F 302199D WP WS 520.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E, INBOARD SIDE OF THE XS 520.168 RIB, THE SLOT AFT BLKHD VERTICAL ATTACH ANGLE WAS CRAC KED AT THE BOTTOM. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800627 19991008 00627 WP 1999 10 8 UPS99830784 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 454.976 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIB AT XS 454.976 WAS CRACKED AT THE AFT UPPER END. REPAIRED THE RIB IAW SRM 57-2-0 F IG 2. 2 L 7 4 4F RT 4A25 1999100800628 19991008 00628 WP 1999 10 8 UPS99830785 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 448.581 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIB AT XS 448.581 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIR ED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800629 19991008 00629 WP 1999 10 8 UPS99830786 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS442.185 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIB AT XS 442.185 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIR ED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800630 19991008 00630 WP 1999 10 8 UPS99830787 1 19990916 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 520.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING LWR L/E SKIN INTERNAL DOUBLER AT XS 520.168 WAS CRACKED AND A PIECE WAS BROKEN OFF. REMOV ED, FABRICATED AND REPLACED THE DOUBLER IAW SRM 57-3-1 FIG 5 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999100800631 19991008 00631 WP 1999 10 8 UPS99830788 1 19990916 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIB AT FS 304.0 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800632 19991008 00632 WP 1999 10 8 UPS99830789 1 19990916 A 5720 975329424 CLIP DOUG DC8 DC871F 302199D WP WS 254.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E ABOVE AND FWD OF THE NR 3 PYLON CUTOUT STA FS 254.25, THE RIB FWD ATTACH CLIP WAS CRAC KED. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800633 19991008 00633 WP 1999 10 8 UPS99830790 1 19990912 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIBS AT FS 616.25 AND FS 622.5 ARE CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK S AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800634 19991008 00634 WP 1999 10 8 UPS99830791 1 19990914 A 5510 37014272 FITTING DOUG DC8 DC871F 302199D WP RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, VERTICAL LEG OF ANGLE (P/N 3701427-2) CRACKED AT O/B END. ANGLE INSTALLED AT I/B END OF THE RT HO RIZ STAB, FWD OF ACCESS PANEL 64I. REMOVED AND REPLACED THE ANGLE FITTING IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999100800635 19991008 00635 WP 1999 10 8 UPS99830792 1 19990914 A 5330 564932975N2 SKIN DOUG DC8 DC871F 302199D WP BS 1717 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, AFT FUSELAGE SKIN AT FS 1717, BETWEEN LONG 35R & 36 WAS CRACKED AND HEAVILY CORRODED. REMOVED AND REPLACED THE SKIN FROM FS 1690 TO 1890 IAW SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800636 19991008 00636 WP 1999 10 8 UPS99830793 1 19990911 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1750 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, THE FUSELAGE SKIN WAS CRACKED AT FS 1750 AND LONG 14L. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 1999100800637 19991008 00637 WP 1999 10 8 UPS99830794 1 19990914 A 5751 DOUBLER DOUG DC8 DC871F 302199D WP LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, THE LT I/B AILERON LOWER SURFACE INTERNAL DOUBLER FOR ACCESS PANEL 541 WAS BENT AND CRACKED. REPA IRED THE DOUBLER IAW DH SK718-668. 2 L 7 4 4F RT 4A25 1999100800638 19991008 00638 WP 1999 10 8 UPS99830795 1 19990917 A 5720 37048412 FITTING DOUG DC8 DC871F 302199D WP WS 74.9 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING O/B SIDE OF THE STA XRS 74.9, THE STR 51 AFT END FITTING WAS CRACKED. REMOVED AND REPLACE D THE FITTING IAW SRM 51-1-20D & 51-3-0. 2 L 7 4 4F RT 4A25 1999100800639 19991008 00639 WP 1999 10 8 UPS99830796 1 19990915 A 5313 975491331 LONGERON DOUG DC8 DC871F 302199D WP BS 215-220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LONGERON 35L FS 215 - 220 WAS CRACKED BEYOND THE STOP DRILL AND CORROSION WAS FORMING INSIDE THE C RACK. CUT OUT THE DAMAGED LONGERON, FS 190 - 230 AND SPLICED IN A NEW SECTION OF LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1999100800640 19991008 00640 WP 1999 10 8 UPS99830797 1 19990915 A 5320 5615374105 DOUBLER DOUG DC8 DC871F 302199D WP BS 1460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, THE FINGER DOUBLER AT FS 1460 AND LONG 31L WAS CORRODED. REMOVED, FABRICATED AND REPLACED THE FIN GER DOUBLER IAW DWG 5615374 & SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 1999100800641 19991008 00641 WP 1999 10 8 UPS99830798 1 19990915 A 5720 975329423 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E, FWD OF THE NR 2 PYLON CUTOUT THE L/E RIB FWD ATTACH CLIP WAS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800642 19991008 00642 WP 1999 10 8 UPS99830799 1 19990915 A 5320 37799191 SPLICE DOUG DC8 DC871F 302199D WP BS 1340-1360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, THE LONGERON 34R SPLICE FITTING WAS CRACKED BETWEEN FS 1340 AND 1360. REMOVED AND REPLACED THE FI TTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999100800643 19991008 00643 WP 1999 10 8 UPS99830800 1 19990912 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 738.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E RIBS AT FS 735.0 & 738.75 WERE CRACKED AT THE AFT UPPER ENDS. STOP DRILLED CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800644 19991008 00644 WP 1999 10 8 UPS99830801 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 466.651 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT FS 466.651 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800645 19991008 00645 WP 1999 10 8 UPS99830802 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 461.372 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, LT WING L/E RIB AT FS 461.372 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999100800646 19991008 00646 WP 1999 10 8 UPS99830803 1 19990912 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 572,577,610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, RT WING L/E UPPER SKIN WAS CRACKED AT 3 LOCATIONS: FS 572.0, FS 577.0, & FS 610. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999100800647 19991008 00647 WP 1999 10 8 UPS99830804 1 19990929 A 2611 SMOKE DETECTOR DOUG DC8 DC873F 302199F WP CARGO COMP INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809UP 46109 NR 6 CARGO SMOKE DETECTOR IS INOP. REPLACED NR 6 SMOKE DETECTOR TEST LAMP WITH PRO PER CM327AS15 LAMP TESTS GOOD. 2 L 7 4 4F RT 4A25 1999100800648 19991008 00648 EU 1999 10 8 99FDEA00402 1 19990930 A 3231 RETRACT MECH AIRBUS 310 A310222 3930315 EU NLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 422FE 346 NOSE DOOR WOULD NOT RETRACT WHEN GEAR HANDLE PUT IN UP POSITION. 2 L 7 2 4F RT A35EU 1999100800649 19991008 00649 NM 1999 10 8 SCNA99728 1 19990914 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 400 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS APPROX FS 400 LBL 5 ON MAIN CABIN FLOOR STRUCTURE. RE MOVED CORROSION FROM FLOORBEAM IAW B727 SRM 511006. TRIMMED DAMAGED IAW B727 SRM 531008. FABRICATED REPAIR SPLICE FROM BAC 1505100617, BAC 14902785, BAC 14902831, BAC 15123353 AND BAC 15123396. TREATED AND PRIMED IAW B727 SRM 512002 MM 5 11002. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F RT A3WE 1999100800650 19991008 00650 NM 1999 10 8 SCNA99729 1 19990914 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS APPROX FS 440 LBL 11 ON T CAP OF MAIN CABIN FLOOR STRU CTURE. REMOVED CORROSION FROM FLOORBEAM IAW B727 SRM 511006. REMOVED DAMAGE IAW B727 SRM 531008. FABRICATED REPAIR SP LICE FROM BAC 1505100617 ,BAC 14902785, BAC 14902831, BAC 15123353 AND BAC 15123396. TREATED AND PRIMED IAW B727 SRM 51 2002 MM 511002. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F RT A3WE 1999100800651 19991008 00651 NM 1999 10 8 SCNA99730 1 19990914 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS APPROX FS 440 BETWEEN RBL 6 AND 12 ON T CAP OF MAIN CA BIN FLOOR STRUCTURE. REMOVED CORROSION FROM FLOORBEAM IAW B727 SRM 511006. REMOVED DAMAGE IAW B727 SRM 531008. FABRIC ATED REPAIR SPLICE FROM BAC 1505100617, BAC 14902785, BAC 14902831, BAC 15123353 AND BAC 15123396. TREATED AND PRIMED I AW B727 SRM 512002 MM 511002. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F RT A3WE 1999100800652 19991008 00652 NM 1999 10 8 SCNA99731 1 19990914 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS APPROX FS 440 BL 0 ON T CAP OF MAIN CABIN FLOOR STRUCT URE. REMOVED CORROSION FROM FLOORBEAM IAW B727 SRM 511006. TRIMMED DAMAGE IAW B727 SRM 531008. FABRICATED REPAIR SPLI CE FROM BAC 1505100617, BAC 14902785, BAC 14902831, BAC 15123353 AND BAC 15123396. TREATED AND PRIMED IAW B727 SRM 5120 02 MM 511002. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F RT A3WE 1999100800653 19991008 00653 NM 1999 10 8 SCNA99732 1 19990914 A 5315 FLOORBEAM BOEING 727 7272J4 1384006 NM BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS APPROX FS 440 LBL 18 ON T CAP OF MAIN CABIN FLOOR STRU CTURE. REMOVED CORROSION FROM FLOORBEAM IAW B727 SRM 511006. TRIMMED DAMAGE IAW B727 SRM 531008. FABRICATED REPAIR SP LICE FROM BAC 1505100617, BAC 14902785, BAC 14902831, BAC 15123353 AND BAC 15123396. TREATED AND PRIMED IAW B727 SRM 51 2002 MM 511002. INSTALLED IAW B727 SRM 513002 AND 531008. 2 L 7 3 4F RT A3WE 1999100800654 19991008 00654 NM 1999 10 8 SCNA99733 1 19990914 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 410 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS APPROX FS 410 LBL 21 ON SEAT TRACK SUPPORT ANGLE OF MA IN CABIN FLOOR STRUCTURE. REMOVED CORROSION FROM FLOORBEAM IAW B727 SRM 511006. FABRICATED NEW SEAT TRACK BAC 1520792. TREATED AND PRIMED IAW B727 SRM 512002 MM 511002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F RT A3WE 1999100800655 19991008 00655 NM 1999 10 8 SCNA99734 1 19990914 A 5730 SKIN BOEING 727 7272J4 1384006 NM CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS LT AC BAY CENTER WING LOWER SKIN AT BS 833 TO BS 838 B L 24L TO 30L. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED 1 FILLER FROM 0.160 7075 T6. FABRICATED 1 DOUBLER FRO M 0.063 7075 T6. FABRICATED 1 DOUBLER FROM 0.071 7075 T6, ALL IAW FLIGHT VEHICLES DRAWING NUMBER 57994901.0. TREATED AN D PRIMED IAW B727 MM 512002 SRM 511002. INSTALLED IAW FLIGHT VEHICLES DRAWING NUMBER 57994901. LEAK CHECK GOOD IAW B72 7 MM 281100 PAGE 26 PARAGRAPH 8A. 2 L 7 3 4F RT A3WE 1999100800656 19991008 00656 NM 1999 10 8 SCNA99123 1 19990927 A 3350 900835A BATTERY PACK BOEING 727 727259 138408J NM LT EMER EXIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 22475 DURING A SCHEDULED MAINTENANCE CHECK, THE LEFT FORWARD AND AFT EMERGENCY OVERWING EXIT IDENTIFIERS WERE FOUND TO BE INOP ERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM 335022, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999100800657 19991008 00657 NM 1999 10 8 DHL9972701C 1 19990821 A 5510 SEAT TRACK BOEING 727 727228 NM RT HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, RT HORIZONTAL STABILIZER SLIDING SEAL AFT TRACK IS CRACKED UPPER SECTION. REPLACE SLIDING SEAL TRACK LWR SE CTION RT AFT IAW B727-SRM 51-30-2 N/R 4386. 2 L 7 3 4F A3WE 1999100800658 19991008 00658 NM 1999 10 8 DHL9972702C 1 19990817 A 5720 SUPPORT BOEING 727 727228 NM WS 499 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING REAR SPAR CAVITY AREA WS 499.0 COVE PANEL LOWER SUPPORT BRACKET CRACKED. REPLACED LT WING COVE PANE L SUPPORT BRACKET AT WS 499 PER B727 SRM 51-30-2 N/R 1423. 2 L 7 3 4F A3WE 1999100800659 19991008 00659 NM 1999 10 8 DHL9972703C 1 19990817 A 5720 SUPPORT BOEING 727 727228 NM WS 567 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING REAR SPAR CAVITY AREA WS 567.0 COVE PANEL LOWER SUPPORT CRACKET CRACKED. REPLACED COVE PANEL SUPPPO RT BRKT AT WS 567.0 PER B727 SRM 51-30-2 N/R 1422. 2 L 7 3 4F A3WE 1999100800660 19991008 00660 NM 1999 10 8 DHL9972704C 1 19990819 A 5720 BRACKET BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING COVE PANEL SUPPORT ROD I/B OF NR 2 SPOILER ACT LOWER END SUPPORT BRACKET CRACKED. REMOVED AND REPLA CED SUPPORT BRACKET IAW B727 SRM 51-30-2 N/R 1465. 2 L 7 3 4F A3WE 1999100800661 19991008 00661 NM 1999 10 8 DHL9972705C 1 19990817 A 5720 BRACKET BOEING 727 727228 NM WS 544 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING REAR SPAR CAVITY AREA WS 544.00 COVE PANEL LOWER SUPPORT BRACKET CRACKED. REMOVED AND REPLACED I/B AND O/B BRACKETS AT LT WING REAR SPAR WS 544.00 PER SRM 51-30-2 N/R 1421. 2 L 7 3 4F A3WE 1999100800662 19991008 00662 NM 1999 10 8 DHL9972706C 1 19990827 A 5313 STRINGER BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, STRINGER TIE CORRODED AT STRINGER 30 BS 950A. REPLACED CORREDED STRINGER TIE PER B727 SRM 51-40-3 USING 202 4T3 .050 8X5, ALODINED AND PRIMED REPAIR PARTS PER B727 SRM 51-10-2 N/R 3697. 2 L 7 3 4F A3WE 1999100800663 19991008 00663 NM 1999 10 8 DHL9972707C 1 19990820 A 7830 SUPPORT BOEING 727 727228 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 1 ENGINE UPPER T/R CASCADE FWD SUPPORT BRACKETS ARE CRACKED AT 11:00 AND 1:00 POSITIONS. WELDED NR 1 ENG INE UPPER T/R CASCADE FWD SUPPORT BRACKETS AT THE 1:00 POSITION PER BOEING OHM 78-30-02 PG 410A SECTION E PARA A NR 6331 . 2 L 7 3 4F A3WE 1999100800664 19991008 00664 NM 1999 10 8 DHL9972708C 1 19990823 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 1 UPPER COWL PREVIOUS REPAIR DOUBLER AFT OF NR 4 LATCH CUTOUT MISSING. REPLACED DOUBLER AT NR 1 ENG UPPE R COWL AFT OF NR 4 LATCH PER SRM 51-30-2 USING 2024T3 .032 1X8 N/R 6357. 2 L 7 3 4F A3WE 1999100800665 19991008 00665 NM 1999 10 8 DHL9972709C 1 19990821 A 5532 SKIN BOEING 727 727228 NM VERTICAL FIN ELONGATED HOLES A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, FASTENER HOLES ELONGATED ON RT SIDE VERTICAL FIN L/E PANEL NR 9601. REPLACED PANEL ON LEFT SIDE VERTICAL FI N L/E USING 2024T3 .040 PER B727 SRM 51-30-2 20 X 15 N/R 4388. 2 L 7 3 4F A3WE 1999100800666 19991008 00666 NM 1999 10 8 DHL9972710C 1 19990821 A 5320 ANGLE BOEING 727 727228 NM CARGO COMP MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, AFT LOWER CARGO FLOOR SUPPORT ANGLE MISS DRILLED HOLE IN RADIUS. INSTALLED ANGLE REPAIR PER SRM 51-40-3 AND 51-30-2 USING 2024T3 .063 ALODINED AND PRIMED PER B727 SRM 51-10-2 N/R 3658. 2 L 7 3 4F A3WE 1999100800667 19991008 00667 NM 1999 10 8 DHL9972711C 1 19990818 A 5720 BRACKED BOEING 727 727228 NM LT WING COVE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH BRACKET CRACKED I/B NR 3 SPOILER ACT. REPLACED SUPPORT ROD ATTACH BRA CKET AT LT COVE I/B AT NR 3 SPOILER ACT PER B727 SRM 51-30-2 N/R 1469. 2 L 7 3 4F A3WE 1999100800668 19991008 00668 NM 1999 10 8 DHL9972712C 1 19990819 A 5720 ANGLE BOEING 727 727228 NM LT WING COVE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH ANGLES CRACKED STA 568 OUTBD NR 2 SPOILER ACT. REPLACED LT WING COVE PANEL SUPPORT BRKT AT STA 568 O/B OF NR 2 SPOILER ACT PER B727 SRM 51-30-2 N/R 1464. 2 L 7 3 4F A3WE 1999100800669 19991008 00669 NM 1999 10 8 DHL9972713C 1 19990819 A 5753 RIB BOEING 727 727228 NM TE FLAP FAIRING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING NR 4 FLAP TRACK ASSY FIXED FAIRING MOST FWD RIB CRACKED. REMOVED AND REPLACED FWD RIB AT LT WING NR 4 FLAP TRACK FIXED FAIRING PER B727 SRM 51-10-1 AND 51-30-2. TREATED AND PRIMED PER SRM 51-10-2 N/R 1453. 2 L 7 3 4F A3WE 1999100800670 19991008 00670 NM 1999 10 8 DHL9972714C 1 19990822 A 5313 STRINGER BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LOWER AFT CARGO STA 950D AND STRINGER 28 LEFT STRINGER TIE TO FRAME DAMAGE AND CRACKED. REMOVED STR TIE CLI P AT STA 950D PER SRM 51-30-2, FABRICATED NEW STR TIE CLIP PER SRM 51-40-3 USING 2024T3 .040 4X7, ALODINED AND PRIMED PA RT IAW B727SRM 51-10-2, INSTALLED STR TIE CLIP AS PER B727 SRM 51-30-2 N/R 3668. 2 L 7 3 4F A3WE 1999100800671 19991008 00671 NM 1999 10 8 DHL9972715C 1 19990825 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 1 ENGINE UPPER COWL O/B EDGE IS WORN THRU BETWEEN NR 2 AND NR 3 COWL LATCHES. REMOVED AND REPLACED ANGLE AT NR 1 ENG UPPER COWL O/B EDGE BETWEEN NR 2 AND NR 3 COWL LATCHES PER B727 SRM 51-30-2 MAT USED .030 2024T3 24.5 X 4, TREATED AND PRIMED U ANGLE PER B727 SRM 51-10-2. N/R 6372. 2 L 7 3 4F A3WE 1999100800672 19991008 00672 NM 1999 10 8 DHL9972716C 1 19990823 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 1 LWR COWL LWR BELLY SKIN BETWEEN RIBS NR 6 AND NR 8 DENTED AND OIL CANNING. CUT OUT DAMAGE AREA AT NR 1 ENG LWR COWL LWR BELLY SKIN BETWEEN RIBS NR 6 NR 8 PER B727 SRM 54-10-3, FIG 5 11 X 16, CLEANED AREA, TREATED AND PRIME D PER B727 SRM 51-10-2, INSTALLED REPAIR PARTS PER B727 STM 54-10-3, MAT USED A) DOUBLER .040 2024T3 16 X 15, B) SKIN .0 32 2024T3 11 X 16 NR 6369. 2 L 7 3 4F A3WE 1999100800673 19991008 00673 NM 1999 10 8 DHL9972717C 1 19990823 A 7110 COWL BOEING 727 727228 NM NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 3 UPPER COWL NR 1 RIB WORN, CRACKED AND HAS JAGGED EDGE AT I/B UPPER END. REMOVED AND REPLACED CHANNEL A T NR 3 ENG UPPER COWL AT NR 1 RIB AS PER B727 SRM 51-30-2 USING 7075-0 16.25 X 5, TREATED AND PRIMED U CHANNEL PER B727 SRM 51-10-2 NR 6366. 2 L 7 3 4F A3WE 1999100800674 19991008 00674 NM 1999 10 8 DHL9972718C 1 19990823 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 1 UPPER COWL I/B INT EDGE WORN AFT OF NR 2 U BOLT. REMOVED FASTENERS AT NR 1 ENG UPPER COWL I/B INT AFT OF AT U BOLT PER B727 SRM 51-30-2, REWORKED AREA WITH DAMAGED MATERIAL PER SRM 54-10-1, INSTALLED REPAIR PER B727 SRM 51 -30-2 USING STAINLESS STEEL 301 1/4H .020 11 X 4, TREATED AND PRIMED PER B727 SRM 51-10-2 NR 6358. 2 L 7 3 4F A3WE 1999100800675 19991008 00675 NM 1999 10 8 DHL9972719C 1 19990830 A 5313 STRINGER BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, STA 950 + 10 STR 29L - CORROSION ON O/B HORIZONTAL LEG. REMOVED CORROSION AT STR 29L -.050 REMOVED IS OUT O F LIMITS PER 727 SRM 53-10-1 AT STA 950. INSTALLED EXTERNAL DOUBLER AND TRIPLER SKIN REINFORCEMENT AREA OF STR 29L + FR OM BS 950 TO 950 A PER AVITAS ENG REPAIR ORDER 99AVHM.062R01 REV 1R DATED 9/2/99 USED 7075T6 .090 13 X 9 AND 11 X 6.5, A LODINED AND PRIMED PER B727 SRM 51-10-2 NR 3712. 2 L 7 3 4F A3WE 1999100800676 19991008 00676 NM 1999 10 8 DHL9972720C 1 19990825 A 5755 SKIN BOEING 727 727228 NM NR 8 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, FOUND NR 8 SPOILER PANEL CRACKED I/B SIDE. REMOVED AND REPLACED NR 8 SPOILER PANEL IAW MM 27-61-1, ADJUSTED NR 8 PANEL PER MM 27-61-1, OPS CHECKED OK PER MM 27-61-0 NR 2511. 2 L 7 3 4F A3WE 1999100800677 19991008 00677 NM 1999 10 8 DHL9972721C 1 19990824 A 5755 MOUNT BOEING 727 727228 NM NR 5 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LEFT WING NR 5 SPOILER MOUNT CRACKED AFT SIDE ON MIDDLE HINGE I/B SIDE. CUT OUT DAMAGED SECTION I/B FLANGE 1 X 1 APPROX AT LT WS 5 SPOILER MOUNT AS PER AVITAS ENG-REPAIR ORDER 99AVHM .061 RO-1 REV 1R, DYE PENETRANT INSPECTED NR 5 SPOILER MOUNT CUT OUT NO CRACK INDICATION NOTED, INSTALLED DOUBLER REPAIR ON NR 5 SPOILER FITTING I/B LEG PER AVITAS ENG REPAIR ORDER 99AVHM .061 R0-1 REV 1R. MATERIAL USED .125 2024T3 FOR FILLER 1 X 1 AND DOUBLER 1 X 9.25, TREATED AND PRIMED PARTS AND AREA PER B727 SRM 51-10-2 NR 1551. 2 L 7 3 4F A3WE 1999100800678 19991008 00678 NM 1999 10 8 DHL9972722C 1 19990817 A 5730 PANEL BOEING 727 727228 NM LT WING DELAMIANTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING LOWER SURFACE COVE PANEL AFT OF ACCESS PANEL 8405 WITH AREAS DELAMINATED. REMOVED PANEL AT LT WING AFT OF PANEL 8405 AS PER B727 SRM 51-30-2, INSTALLED BONDING REPAIR PER SRM 51-40-6 FIG 1 SIZE 11 X 72 USING ADHESIVE FI LM AF163-2K, INSTALLED LOWER COVE PANEL AFT OF PANEL 8405 PER SRM 51-30-2 N/R 1416. 2 L 7 3 4F A3WE 1999100800679 19991008 00679 NM 1999 10 8 DHL9972723C 1 19990822 A 5313 STRINGER BOEING 727 727228 NM BS 1010 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, DAMAGED STRINGER TIE ANGLE, STIRNGER 28R STA 1010. REMOVED STRINGER TIE ANGLE AT STRINGER 28R STA 1010 IAW B727 51-30-2, FABRICATED NEW STRINGER TIE ANGLE AT STA 1010 STR 28R PER SRM 51-40-3 USING 2024T3 .040 4 X 7, ALODINED AN D PRIMED IAW SRM 51-10-2, INSTALLED NEW STRINGER TIE ANGLE AT STA 1010 STR 28R IAW SRM 51-30-2 N/R 3667. 2 L 7 3 4F A3WE 1999100800680 19991008 00680 NM 1999 10 8 DHL9972724C 1 19990819 A 5753 FAIRING BOEING 727 727228 NM NR 4 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING NR 4 FLAP TRACK ASSY FIXED FAIRING REAR CUT OUT HAVE TWO AREAS WITH MATERIAL DENTED AND CRACKED. RO UTED OUT CRACK AREA ON NR 4 FLAP TRACK FIXED FAIRING PER SRM 51-10-1 MAINTAINED EDGE DISTANCE FOUND TO BE WITHIN LIMITS, REPLACED DENTED RIB PER B727 STM 51-40-3 USING .040 2024T3 1 X 1 X 10, ALODINED AND PRIMED ROUTED AREA AND NEW RIB IAW SRM 51-10-2 N/R 1454. 2 L 7 3 4F A3WE 1999100800681 19991008 00681 NM 1999 10 8 DHL9972725C 1 19990820 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 1 ENG INLET COWL O/B AFT END SKIN DAMAGED AT 9 O'CLOCK. CUT OUT DAMAGED AREA OF OUTER SKIN AT NR 1 INLET PER SRM 54-30-3, CLEANED TREATED AND PRIMED AREA PER B727-SRM 51-10-2, INSTALLED REPAIR PARTS PER SRM 54-30-2,FIG 5. M ATERIAL USED DOUBLER .050 2024T3 10 X 3.5 FILLER .040 2024T3 5.5 X 2 N/R 6343. 2 L 7 3 4F A3WE 1999100800682 19991008 00682 NM 1999 10 8 DHL9972726C 1 19990817 A 5230 BRACKET BOEING 727 727228 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, FWD CARGO COMPARTMENT DOOR SNUBBER FWD END SUPPORT BRACKET IS CRACKED. REMOVED FWD CARGO DOOR FOR ACCESS IA W B727 MM 52-31-0. REMOVED AND REPLACED SNUBBER FWD END SUPPORT BRACKET, INSTALLED FWD CARGO DOOR PER MM 52-31-0, OPS C HECK OK PER MM 52-31-0, LEAK CHECK OK PER MM 24-31-00 N/R 3620. 2 L 7 3 4F A3WE 1999100800683 19991008 00683 NM 1999 10 8 DHL9972727C 1 19990822 A 5320 CLIP BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LOWER AFT CARGO BETWEEN STA 950 E AND E IAW SRM 51-30-2. REMOVED VERTICAL CLIP AT STR 30 BETWEEN STA 950 E AND E PER SRM 51-30-2, ALODINED AND PRIMED AREA PER SRM 51-10-2, REPLACED CLIP AT STR 30 BETWEEN STA 950 E AND E IAW SRM 51-40-3 USING 7075T6 .050 1 X 1 X 8.5 N/R 3672. 2 L 7 3 4F A3WE 1999100800684 19991008 00684 NM 1999 10 8 DHL9972728C 1 19990822 A 5313 STRINGER BOEING 727 727228 NM BS 950 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LOWER AFT CARGO STA 950F STRINGER 28 RIGHT STRINGER TIE TO FRAME DAMAGED. REMOVED DAMAGED STRINGER TIE AT S TA 950F, MADE NEW STRINGER TIE PER SRM 51-40-3, USING 2024T3 .050 6 X 4. ALODINED AND PRIMED PER SRM 57-10-2, INSTALLED STRINGER PER SRM 51-30-2 N/R 3669. 2 L 7 3 4F A3WE 1999100800685 19991008 00685 NM 1999 10 8 DHL9972729C 1 19990820 A 5320 ANGLE BOEING 727 727228 NM BS 1307 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, CRACKED ANGLE RT WING L/E 4 I/B OF L/E STA 1307 CRACKED AT THE LOWER CORNER. REMOVED AND REPLACED ATTACH AN GLE SUPPORT AT RT WING L/E 4 I/B OF STA 1307 PER SRM 57-10-1 FIG 1 AND 51-30-2 USING 2024T3 .050 17 X 1 X 1. ALODINED A ND PRIMED PER SRM 51-10-2 N/R 2483. 2 L 7 3 4F A3WE 1999100800686 19991008 00686 NM 1999 10 8 DHL9972730C 1 19990816 A 5280 SKIN BOEING 727 727228 NM LT MLG DOOR HOLE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LEFT FLYING DOOR HAS A HOLE IN THE INNER SKIN 10 AFT OF THE FWD EDGE. APPROX SIZE OF HOLE IS .5 X .0625. I NSTALLED REPAIR AT LEFT FLYING DOOR IN THE INNER SKIN USING 2024T3 .050 18 X 14 PER SRM 51-30-2. ALODINED AND PRIMED IA W SRM 51-10-2 N/R 7362. 2 L 7 3 4F A3WE 1999100800687 19991008 00687 NM 1999 10 8 DHL9972731C 1 19990816 A 5280 SKIN BOEING 727 727228 NM LT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LEFT FLYING DOOR IS CRACKED ON EXTERIOR AT FWD END WHERE DOOOR ANGLES MEET. CUT OUT DAMAGED AREA AT LEFT FL YING DOOR FWD END PER SRM 51-40-3, INSTALLED REPAIR ON EXTERIOR SKIN AT FWD END WHERE DOOR ANGLES MEET USING 2024T3 .050 PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2 N/R 7360. 2 L 7 3 4F A3WE 1999100800688 19991008 00688 NM 1999 10 8 DHL9972732C 1 19990901 A 5312 BULKHEAD ANGLE BOEING 727 727228 NM CARGO COMPT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LWR FWD CARGO COMPARTMENT RT BULKHEAD PANEL LWR ATTACH ANGLE HAS CORROSION AT LWR END. CUT OUT CORRODED ARE A PER SRM 51-10-1 17, INSTALLED ANGLE REPAIR AT FWD END USING .063 2024T3 17 X 4 PER SRM 51-40-3. ALODINED AND PRIMED P ER SRM 51-10-2 N/R 3722. 2 L 7 3 4F A3WE 1999100800689 19991008 00689 NM 1999 10 8 DHL9972733C 1 19990820 A 7830 SUPPORT BOEING 727 727228 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 2 ENG TR CASCADE FWD SUPPORT CRACKED AT 9 O'CLOCK POSITION, LEFT CASCADE. REMOVED NR 2 ENG LEFT CASCADE AS REQUIRED BY B727 MM 78-30-22, WELDED NR 2 ENG TR CASCADE SUPPPORT PER BOEING OHM 78-30-02, PG 410A, SECT E PARA A. I NSTALLED LT NR 2 ENG TR CASCADE IAW MM 78-30-22, OPS CHECK GOOD N/R 6321. 2 L 7 3 4F A3WE 1999100800690 19991008 00690 NM 1999 10 8 DHL9972734C 1 19990903 A 5320 WEB BOEING 727 727228 NM BS 386 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, HORIZONTAL WEB CRACKED AT STA 380 AND STA 386 UNDER ANTENNA PANEL - MOUNTED. CUT OUT DAMAGED AREA PER 51-10 -1 1 X 17 AREA ON STA 380 AND 1 X 10 AREA ON STA 386, PERFORMED HFEC INSP PER 727 NDT MANUAL PART 6-51-00-00 FIG 4. NO CRACK INDICATIONS AT EITHER CUTOUT, CLEANED TREATED AND PRIMED AREA PER SRM 51-10-2, INSTALLED REAPIR PARTS PER SRM 51-4 0-2 AND 51-30-2 USING FILLER .040 2024T3 1 X 22 AND DOUBLER 2024T3 4.5 X 34 N/R 3725. 2 L 7 3 4F A3WE 1999100800691 19991008 00691 NM 1999 10 8 DHL9972735C 1 19990827 A 5320 PLENUM BOEING 727 727228 NM LT HEAT EXCHGR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, CORROSION IN PLENUM ABOVE LT PRIMARY HEAT EXCHANGER. REMOVED CORROSION PER B727 SRM 51-10-6, MATERIAL LOSS .060 FOUND TO BE OUT OF LIMITS PER SRM 57-30-1 FIG 9. FLAP PEENED ALL AREA PER OHM 20-10-3, COLD WORKED ALL FASTENER HO LES PER SRM 51-30-10, INSTALLED REPAIR PER SRM 57-30-3, USING .080 2024T3 14 X 6.5 AND 13 X 6.5. ALODINED AND PRIMED PE R SRM 51-10-2. POLY WHITE ALL EXTERIOR PARTS PER MM 51-20-0, SEALED AREA PER SRM 51-20-4 N/R 3700. 2 L 7 3 4F A3WE 1999100800692 19991008 00692 NM 1999 10 8 DHL9972736C 1 19990820 A 5320 ANGLE BOEING 727 727228 NM FUEL STATION CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, CRACKED ANGLE O/B SIDE OF FUELING STATION WEB UPPER ANGLE. REMOVED FASTENERS AND CUT OUT 2 OF DAMAGED AREA ON ANGLE AT O/B SIDE OF FULING STATION PER SRM 51-30-2 AND 51-40-3. ALODINED AND PRIMED REPAIR PARTS AND MATCHING AREA PER SRM 51-10-2, INSTALLED ANGLE REAPIR 1 X 1 X 8 2024T3 .050 PER SRM 51-40-3, REPLACED FUEL LINE FOR SRM ACCESS PER MM 20-80-1, REINSTALLED VENT FUEL LINE IAW MM 20-20-1, LEAK CHECKED GOOD IAW MM 28-21-0 N/R 2480. 2 L 7 3 4F A3WE 1999100800693 19991008 00693 NM 1999 10 8 DHL9972737C 1 19990817 A 5755 SKIN BOEING 727 727228 NM NR 4 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LT WING UPPER SURFACE NR 4 SPOILER PANEL NR 2 AND NR 4 HINGE CUTOUTS CRACKED. VERIFIED CRACK INDICATIONS US ING HFEC INSP PER NDT MANUAL PART 6-51-00-00 FIG 4, STOP DRILLED CRACK PER SRM 57-30-4 AT NR 4 SPOILER PANEL NR 2 AND NR 4 HINGE CUTOUTS, HFEC INSP STOP DRILL PER NDT MANUAL 51-00-00 PART 6. NO FURTHER CRACK INDICATION NOTED. INSTALLED REP AIRS PER SRM 57-30-4 DOUBLER SIZE 6 X 4 AND 5 X 4 FROM 7075T6 .071 AND 7075T6 .063. 2 L 7 3 4F A3WE 1999100800694 19991008 00694 NM 1999 10 8 DHL9972738C 1 19990908 A 5350 FAIRING BOEING 727 727228 NM FUSELAGE DELAMIANTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LWR LT BODY FAIRING AFT OF HYD ACCESS PANEL 3519 DELAMINATED AT LWR I/B END AND ALONG EDGE. ALSO, MISSING T WO FASTENERS. REMOVED LWR LT BODY FAIRING PER SRM 51-30-2, REPLACED MISSING FASTENERS PER SRM 51-30-2, INSTALLED FG OVE RLAY REPAIR AS PER SRM 51-40-8 FIG 1 USING RESIN 50-A HARDENER 946 7781 CLOTH 25 X 10. INSTALLED LT BODY FAIRNING 3519 PER SRM 51-30-2 N/R 5841. 2 L 7 3 4F A3WE 1999100800695 19991008 00695 NM 1999 10 8 DHL9972739C 1 19990820 A 5320 ANGLE BOEING 727 727228 NM BS 356-360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, ANGLE AT STR 19L LOCATION FROM STA 360 TO 356 HAS CORROSION. REMOVED ATTACH T ANGLE STA 360 - 356 FWD OF ST R 19 LT AS PER SRM 51-30-2, FABRICATE REPLACEMENT PART PER DWG 65-18420, USING 60-10005 8 LONG USING 7075T7351 IN PLACE OF 7075T6 IAW 99AVHM 065RO-1, ACCOMPLISH PENETRANT INSPECTION OF REWORKED PART PER AVITAS 99AVHM 065R01. NO CRACKS NOTE D, ACCOMPLISH HARDNESS TEST IAW AVITAS RP 99AVHM 065R01, INSTALLED T ANGLE AT STR 19L PER SRM 51-30-2. TREATED AND PRIM ED PARTS PER SRM 51-10-2 N/R 3649. 2 L 7 3 4F A3WE 1999100800696 19991008 00696 NM 1999 10 8 DHL9972740C 1 19990820 A 5530 ANGLE BOEING 727 727228 NM VERT STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, VERT STAB HAS A T ANGLE CRACKED JUST AFT OF RT LWR ICE SHIELD. REMOVED ANGLE AT VERT STAB JUST AFT RT LWR I CE SHIELD AS PER SRM 51-30-2, INSTALLED NEW T ANGLE AT VERT STA JUST AFT RT LWR ICE SHIELD PER SRM 51-30-2 USING 60-3783 8 LONG. ALODINED AND PRIMED PER SRM 51-10-2 N/R 4375. 2 L 7 3 4F A3WE 1999100800697 19991008 00697 NM 1999 10 8 DHL9972741C 1 19990824 A 5230 SKIN BOEING 727 727228 NM CARGO DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, MCD MIDDLE STRIKER PLATES DENTED AT STA 540. FABRICATED NR 2 AND NR 3 STRIKER PLATES AT STA 540 AND STA 600 AS PER SRM 51-40-2 USING 301 .25 HARD SS 15 X 58. TREATED AND PRIMED PER SRM 51-10-2, INSTALLED STRIKER PLATES PER SRM 51-30-2, SEALED EDGE WITH PRC PER SRM 51-20-4 N/R 3684. 2 L 7 3 4F A3WE 1999100800698 19991008 00698 NM 1999 10 8 DHL9972742C 1 19990826 A 5312 BULKHEAD BEAM BOEING 727 727228 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 FOUND CRACK AT STA 1183 VERTICAL I BEAM RBL 36.83 O/B FLANGE WL 235. REMOVED FASTENERS AT BS 1183 AFT BLKHEAD VERTICAL BEAM RBL PER SRM 51-30-2, STOP DRILLED IAW NDT MANUAL 51-00-00 PART 6 FIGURE 4. NO FURTHER CRACK INDICATION NOTED. INS TALLED REPAIR KIT ON 1183 VERT I BEAM RBL 36.83 IAW SB 53-0192. ALL PARTS AND AREA TREATED AND PRIMED PER B727 SRM 51-1 0-2 N/R 3693. 2 L 7 3 4F A3WE 1999100800699 19991008 00699 NM 1999 10 8 DHL9972743C 1 19990821 A 5400 S DUCT BOEING 727 727228 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 2 ENGINE S DUCT HOUSING LT OUTER SKIN AT BS 1216 HAD 2 INCH CRACK JUST RIGHT UP OF ACCESS PANEL 9523. RE MOVED ACCESS PANEL 9523 TO GAIN ENTRY REMOVED ATTACH RING PER SRM 51-30-2 AND REMOVED PREVIOUS REPAIR. STOP DRILLED CRA CK IAW SRM 51-10-1. VISUALLY INSP STOP DRILL, NO FURTHER CRACK NOTED. NON PRESSURE AREA NDT NOT REQUIRED. FABRICATED REPAIR DOUBLER TO FIT DAMAGED AREA ON NR 2 ENG S DUCT HOUSING LT OUTER SKIN AT BS 1216 RIGHT UP OF ACCESS PANEL 9523 USI NG 7075T6 .050 18 X 9 PER SRM 54-10-3. INSTALLED REPAIR PER SRM 51-30-2 AND SRM 54-10-3, FABRICATED ACCESS PANEL 9523 T O FIT REPAIR DOUBLER FROM 2024T3 .090 PER SRM 54-10-3, INSTALLED ACCESS PANEL 9523 PER SRM 51-30-2 AND 51-20-4 N/R 4387. 2 L 7 3 4F A3WE 1999100800700 19991008 00700 NM 1999 10 8 DHL9972744C 1 19990819 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 940 LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, SEAT TRACKS LBL 48 MISSING ATTACH FASTENERS AT STA 940. REMOVED FASTENERS AT SEAT TRACK LBL 48 FROM STA 950 A TO STA 890 PER SRM 51-30-2. FOUND HOLE TO BE IN WRONG LOCATION. INSTALLED NEW CABIN SEAT TRACK LBL 48 PER SRM 53-10- 5 FIG 7. ALODINED AND PRIMED PER SRM 51-10-2, OK TO INSTALLED FLOOR PNLS, INSTALLED CABIN FLOOR PANELS PER SRM 51-30-2, SEALED FLOOR PANEL PER SRM 51-20-3 N/R 5781. 2 L 7 3 4F A3WE 1999100800701 19991008 00701 NM 1999 10 8 DHL9972745C 1 19990829 A 5320 PLENUM BOEING 727 727228 NM BS 808 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, CORROSION IN PLENUM ABOVE AND BETWEEN LT SIDE HEAT EXCHANGERS BS 808 LBL 20. REMOVED CORROSION IN PLENUM AB OVE BTW LT SIDE HEAT EXCHANGERS PER SRM 51-10-6. REMOVED .067 FOUND TO BE OUT OF LIMITS PER SRM 57-30-1 FIG 7. FLAP PE ENED ALL AREAS PER B727 SRM 20-10-2, COLD WORKED ALL FASTENER HOLES PER SRM 51-30-10, INSTALLED REPAIR PER SRM 57-30-3 F IG 7 USING .062 2024T3, 2 EA 13 X 7.25 AND 14.5 X 7.25 .080 2024T3 13 X 7.25 .080 STRAPS 6 EA 2024T3 17 X 1, ALODINED AN D PRIMED PER SRM 51-10-2, POLY WHITE ALL EXTERIOR PARTS PER MM 51-20-0, SEALED AREA PER SRM 51-20-4. N/R 1553. 2 L 7 3 4F A3WE 1999100800702 19991008 00702 NM 1999 10 8 DHL9972746C 1 19990822 A 5347 BAC15061108 SEAT TRACK BOEING 727 727228 NM BS 760-850 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, CORROSION ON NR 5 SEAT TRACK THE LAST O/B TRACK ON THE RT SIDE OF CABIN, NEXT TO THE FWD RIGHT EMERGENCY ESC APE DOOR (WING) STA 760-850. REMOVED SEAT TRACK CAP FROM STA 760 TO 850 AT NR 5 SEAT TRACK PER SRM 51-30-2. REMOVED NR 5 FLOATING SEAT TRACK PER SRM 51-30-2. REMOVED NR 5 T ANGLE SUPPORT AT STA 740 TO 850 PER SRM 51-30-2, INSTALLED NEW T ANGLE SUPPORT PER SRM 53-10-1 FIG 1 AND 51-30-2, ALODINED AND PRIMED PER SRM 51-10-2, REINSTALLED SEAT TRACKS. REMOVED ON STEP NR 1 AND 2 PER SRM 51-30-2, CLEAN PER MM 12-40-0 OK TO CLOSE. INSTALLED FLOOR PANELS PER SRM 51-30-2 N/R 5806. 2 L 7 3 4F A3WE 1999100800703 19991008 00703 NM 1999 10 8 DHL9972747C 1 19990820 A 5280 SKIN BOEING 727 727228 NM RT MLG DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, RIGHT LANDING GEAR WING DOOR INTERIOR SKIN HAD TWO SMALL GOUGED SPOTS FWD SIDE. BURNISHED TOP GOUGE ON RT M LG DOOR INTERIOR DOOR SKIN PER SRM 51-10-1. MATERIAL LOSS WAS .003 FOUND TO BE WITHIN LIMITS PER SRM 52-00-2. TREATED AND PRIMED TOP AREA PER SRM 51-10-2, BURNISHED BOTTOM GOUGE ON RT MLG DOOR INTERIOR SKIN PER SRM 51-10-1. MATERIAL LOSS WAS .020, FOUND TO BE OUT OF LIMITS PER SRM 52-00-2. CUT OUT DAMAGED AREA AT RT LANDING GEAR DOOR INTERIOR SKIN FWD SI DE USING 2024T3 .050 6 X 41 PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2 N/R 7396. 2 L 7 3 4F A3WE 1999100800704 19991008 00704 NM 1999 10 8 DHL9972748C 1 19990820 A 5311 FRAME BOEING 727 727228 NM BS 910 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 RT MLG WW FS 910 TOP O/B SIDE MLG UPLOCK FWD SUPPORT FRAME CRACKED AS VIEWED THROUGH LIGHTENING HOLE WITH MIRROR 6 BELOW PRESS DECK. REMOVED RT GEAR UPLOCK PER MM 32-32-71, REMOVED FASTENERS RT MLG WW FS 910 TOP O/B SIDE FWD SUPPORT MLG UP LOCK PER SRM 51-30-2, STOP DRILLED CRACKS PER SRM 51-10-1, PERFORMED HFEC INSP PER NDT MANUAL PART 6 51-00-00 FIG 4. NO CRACK INDICATIONS PAST STOP DRILL, REPAIRED RT MLG WW FS 910 AND 913 FS UPLOCK SUPPORT FRAME WITH KIT PER SB 53-165 FIG 2 & 3. OK TO CLOSE. INSTALLED RT GEAR UPLOCK IAW MM 32-32-71, OP CHECK PERFORMED OK IAW MM 32-32-0. INSTALLED FLOOR PANEL PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999100800705 19991008 00705 NM 1999 10 8 DHL9972749C 1 19990820 A 2782 SUPPORT BOEING 727 727228 NM LE FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, CRACK ON NR 5 L/E FLAP ACTUATOR SUPPORT BRACKET UPPER I/B SIDE BRACKET IN L/E BAY. ACCOMPLISHED PENETRANT I NSPECTION AND VERIFIED A CRACK INDICATION ON NR 5 L/E FLAP ACTUATOR SUPPORT BRACKET UPPER I/B SIDE PER STANDARD OVERHAUL MANUAL 20-20-02. REMOVED NR 5 L/E FWD ACTUATOR TO FACILITATE SM ACCESS PER MM 27-81-22. REMOVED I/B BRACKET SUPPORT A T NR 5 L/E FLAP ACTUATOR PER SRM 51-30-2, INSTALLED NEW BRACKET SUPPORT I/B SIDE AS PER SRM 57-10-1 FIG AND 51-30-2, MAT USED 7075T6 .063 9 X 7, ALODINED AND PRIMED PER SRM 51-10-2, INSTALLED NR 5 FLAP L/E ACTUATOR PER MM 27-81-22 N/R 2473. 2 L 7 3 4F A3WE 1999100800706 19991008 00706 NM 1999 10 8 DHL9972750C 1 19990829 A 5311 CIRCUMFERENTIAL BOEING 727 727228 NM BS 348&360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, CORROSION ON CIRCUMFERENTIAL WEBS OF 348.2 AND 360 ON SUPPORT WEB AND ANGLE IN BETWEEN CIR RIBS AT APPROXIMA TELY STR 20. REMOVED FASTENERS AND REMOVED CORNER BRACKET SUPPORT AND WEB AT B3 360 PER B727 SRM 51-30-2, REMOVED CORRO SION ON CIRCUMFERENTIAL BS 348 BETWEEN STR 19-20 PER SRM 51-10-6, MATERIAL LOSS .003 WITHIN LIMITS PER SRM 53-10-1 FIG 1 , ALODINED AND PRIMED PER B727 SRM 51-10-2. FOUND STRINGER TIE TO BE OUT OF LIMITS STR 20 STA 360. REMOVED AND REPLACE D CIRCUMFERENTIAL WEBS AT STA 348.2 TO 360 PER SRM 51-40-2 & 51-30-2 USING .040 2024T3 6 X 7 ALODINED AND PRIMED PER SRM 51-10-2, INSTALLED BRACKET SUPPORT AND FASTENERS THAT WERE PREVIOUSLY REMOVED PER SRM 51-30-2 N/R 3678. 2 L 7 3 4F A3WE 1999100800707 19991008 00707 NM 1999 10 8 DHL9972751C 1 19990822 A 5313 STRINGER BOEING 727 727228 NM BS 970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, LOWER AFT CARGO STA 970 BETWEEN STRINGER 28 RIGHT AND 29 RIGHT LOWER CLIPS ON FRAME HAS CORROSION. CUT OUT DAMAGED AREA FOR REPAIR PER SRM 53-10-4 BETWEEN STR 28 & 29, AT STA 970 7 INCHES LONG, FABRICATE NEW L ANGLE REPAIR AT F RAME ATTACH TO STRINGER 28 RT STA 970 PER SRM 53-10-4 FIG 14. REMOVED U CHANNEL ATTACH FRAME TO STRINGER 28RT BS 970 PE R SRM 51-30-2, FABRICATED NEW U CHANNEL AT BS 870 STR 28 RT BS 970 PER SRM 53-10-4 FIG 14 USING 7075-0 .071 8.5 X 4.5 US ED L ANGLE 7075-0 TO 7075T6 PER 98 PMSI 247 PS-01, TREATED AND PRIMED ALL PARTS PER SRM 51-10-2, INSTALLED ALL REPAIRS P ER SRM 53-10-4 FIGURE 14 N/R 3674. 2 L 7 3 4F A3WE 1999100800708 19991008 00708 NM 1999 10 8 DHL9972752C 1 19990820 A 5400 BRACKET BOEING 727 727228 NM NR 1 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C CHECK, NR 1 ENG PYLON FWD I/B END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED THRUST REV SHUTOFF VALVE. REMOVED 6 BOLTS FROM QUADRANT DISCONNECTED THRUST REV QUADRANT DRUM FOR SM ACCESS PER MM 71-11-21. REMO VED AND REPLACED BRACKET AT NR 1 ENG PYLON FWD I/B END OF ACCESS PANEL 5407 PER SRM 51-30-2 MAT USED 7075T6 .050 9 X 4. OK TO INSTALL COMPONENTS. INSTALLED QUADRANT DRUM TR PER MM 71-11-21, INSTALLED REV DIRECTIONAL VAVLE PER MM 78-30-12, LEAK CK AND EPS CHECK GOOD IAW 78-30-12 N/R 1433. 2 L 7 3 4F A3WE 1999100800709 19991008 00709 NM 1999 10 8 DHL9972753C 1 19990822 A 5311 FRAME BOEING 727 727228 NM BS 980 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, LWR AFT CARGO STA 980 O/B OF STR 28 RT FUSE FRAME HAD CORROSION AND CRACKS. REMOVED FASTENERS AT STA 980, C UT FRAME WEB AT 975, NO OTHER WEB CORROSION NOTED. FOUND LWR T ANGLE WEB ATTACH CORRODED BEYOND LIMITS. CUT OUT DAMAGE D AREA AT T ANGLE, ALODINED AND PRIMED AREA PER SRM 51-10-2, FABRICATED 2 ANGLE REPAIRS, HEAT TREATED, INSTALLED WEB REP AIR AT STA 980 FRAME AFT OF LWR CORNER OF C-2 DOOR. REMOVED AND REPLACED L ATTACH ANGLE AT STR 28R AND FRAME BS 980, IN STALLED REPAIR AT T LOWER WEB SUPPORT FROM BS 960 TO BS 980 PER AVITAS EO 99AVHM.060R0-1 7075T6 .090 FORMED ANGLES, ALOD INED AND PRIMED REPAIR PARTS PER SRM 51-10-2. 2 L 7 3 4F A3WE 1999100800710 19991008 00710 NM 1999 10 8 DHL9972754C 1 19990820 A 5315 FLOORBEAM BOEING 727 727228 NM BS 340 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, STA 340 FLOORBEAM UPPER CHORD HAS CORROSION BEYOND LIMITS FROM LBL 64 TO LBL 19. REMOVED T ANGLE FROM BS 34 4 FROM LBL 60 TO RBL 60, INSTALLED NEW T ANGLE PER SRM 53-10-2. INSTALLED NEW HAT CHANNEL FROM BS 320 TO 344 RBL 20 PER SRM 53-10-1, 36 INCHES LONG. 2 L 7 3 4F A3WE 1999100800711 19991008 00711 NM 1999 10 8 DHL9972755C 1 19990827 A 5311 FRAME BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, BS 950 A FRAME IS CORRODED FROM STRINGER 28 LEFT TO STR 30 LEFT. REMOVED FLOOR SUPPORT, CUT OUT CORRODED SH EAR TIES, FROM STR 30 TO 28 LEFT, HFEC, COUNTER SINKS AT FRAME PER SRM. INSTALLED SHEAR TIE REPAIR FROM STRINGER 28 LE FT TO 29 PER SRM 53-10-4. REINSTALLED FLOOR SUPPORTS. 2 L 7 3 4F A3WE 1999100800712 19991008 00712 NM 1999 10 8 DHL9972756C 1 19990823 A 5315 FLOORBEAM BOEING 727 727228 NM BS 328 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, STA 328 FLOORBEAM AT LBL 46 HAS FLOOR PANEL SCREW HOLE REWORKED BEYOND LIMITS. CUT OUT 3 PIECE OF FLOORBEAM , INSTALLED REPAIR PARTS PER SRM 53-10-8, 19 X 2 ANGLE 27 X 2.25 N/R 5810. 2 L 7 3 4F A3WE 1999100800713 19991008 00713 NM 1999 10 8 DHL9972757C 1 19990820 A 5400 BRACKET BOEING 727 727228 NM NR 1 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, NR 1 PYLON FWD IND END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED AND REPLACED BR ACKET PER SRM 51-30-2, 9 X 4 N/R 6338. 2 L 7 3 4F A3WE 1999100800714 19991008 00714 NM 1999 10 8 DHL9972758C 1 19990820 A 5311 FRAME BOEING 727 727228 NM BS 910 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT C-CHECK, RT MLG FS 910 TOP O/B SIDE UPLOCK FWD SUPPORT FRAME CRACKED. STOP DRILLED CRACKS, HFEC, REPAIRED FRAMES FS 910 AND 913 UPLOCK SUPPORT PER S/B 53-165 N/R 2496. 2 L 7 3 4F A3WE 1999100800715 19991008 00715 EU 1999 10 8 RAIA9909012 1 19990903 A 7330 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 426AM 874 66117 7040-COU- RIGHT ENGINE TTL TEST FAILED. MAINTENANCE REPLACED THE FUEL BY-PASS VALVE FOR THE RIGHT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999100800716 19991008 00716 EU 1999 10 8 RAIA9909013 1 19990904 A 3610 ASK226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LT DUCT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 573HK 41092 6212-DCA- DUCT FAIL LIGHT. MAINTENANCE REPLACED GAMMA DUCT SEAL ON LEFT SIDE OF A/C. 2 L 7 2 4T RT A41NM 1999100800717 19991008 00717 EU 1999 10 8 RAIA9909014 1 19990906 A 7931 1241012 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 560HK 41076 6127-JFK- LEFT ENGINE OIL PRESS FLUCTUATING. MAINTENANCE REPLACED OIL PRESS TRANSDUCER FOR LEFT ENGINE. 2 L 7 2 4T RT A41NM 1999100800718 19991008 00718 EU 1999 10 8 RAIA9909015 1 19990914 A 3610 ASK226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU LT DUCT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 563HK 41079 7086-STL- LEFT DUCT FAIL LIGHT. MAINTENANCE REPLACED LEFT DUCT SEAL. 2 L 7 2 4T RT A41NM 1999100800719 19991008 00719 EU 1999 10 8 RAIA9909016 1 19990915 A 7931 1241012 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 563HK 41079 7148-STL- LEFT OIL PRESS GAUGE FLUCTUATING. MAINTENANCE REPLACED LEFT OIL PRESS TRANSDUCER. 2 L 7 2 4T RT A41NM 1999100800720 19991008 00720 EU 1999 10 8 RAIA9909018 1 19990919 A 2150 1718D000 ACM JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 556HK 41073 7462-STL- LEFT FLOW CAUSING A STRONG ODOR IN A/C. MAINTENANCE REPLACED LEFT AIR CYCLE MACHINE. 2 L 7 2 4T RT A41NM 1999100800721 19991008 00721 EU 1999 10 8 RAIA9909019 1 19990928 A 2424 51539002A GCU BAG JETSTM JETSTM3201 1500217 EU NR 2 FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 CE 03 425AM 870 7285-DEC- NR 2 GENERATOR INOP. MAINTENANCE REPLACED NR 2 GEN CONTROL UNIT. 2 L 7 2 4T RT A56EU 1999100800722 19991008 00722 WP 1999 10 8 RAIA9909017 2 19990917 A 7310 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 879 66145 RIGHT ENGINE RPM DROPS TO 94 PERCENT DURING TTL CHECK. MAINTENANCE REPLACED FUEL BY-PASS VALVE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999100800723 19991008 00723 EU 1999 10 8 RAIA9909020 1 19990928 A 5610 1379628C401 WINDSHIELD BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 CE 03 431AM 881 7072-JLN- CAPT WINDSHIELD HEAT INOP. MAINTENANCE REPLACED CAPT'S WINDSHIELD. 2 L 7 2 4T RT A56EU 1999101300002 19991013 00002 NM 1999 10 13 DLM88991945 1 19990901 A 2421 976J2528 GENERATOR DOUG MD88 MD88 3023688 NM APU FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 915DL 7298 49546 DURING CLIMB THROUGH 300 FL, THE APU GEN TRIPPED OFF. TRIED TO RESET AND WORKED FOR A WHILE AND TRIPPED AGAIN. TRIED RE SET AND GOT AC X-TIE LOCKOUT. NOW RT GEN ONLY POWERING THE RT BUS. REPLACED APU GCU. RAN HEAVY LOAD, OP CKS GOOD. 2 L 7 2 4F RT A6WE 1999101300003 19991013 00003 NE 1999 10 13 DL757991950 2 19990902 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 SURGING A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 656DL 24396 RIGHT ENGINE SURGING ON CLIMB-OUT THROUGH 14000 FT. DISCONNECTED AUTO THROTTLES, RETARDED THROTTLES TO IDLE SURGING DIS CONTINUED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999101300004 19991013 00004 NM 1999 10 13 DLM90991952 1 19990902 A 3242 BRAKE 50121932 DOUG MD90 MD9030 3023690 NM NR 1 DRAGGING A DALA O OTHER M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 907DA DL3036 53387 AFTER TAKEOFF, LEFT OUTBOARD BRAKE TEMP REACHED 700 DEG. EXTENDED GEAR AND BRAKE COOLED TO 400 DEG. THEN RETRACTED GEA R FOLLOWED POM PROCEDURES. REPLACED BOTH NR 1 AND NR 2 MAIN WHEEL ASSY PER M/M DUE TO NR 1 MAIN FLAT WHEN REACHING GAT E. ALSO, CHANGED NR 1 BRAKE ASSY PER M/M LEAK CHECKS GOOD. 2 L 7 2 4F RT A6WE 1999101300005 19991013 00005 NM 1999 10 13 DL72E991961 1 19990904 A 3300 900542 CHARGER BOEING 727 727247 138408F NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 DURING L/O CK, FOUND EXTERIOR OVERWING EXIT AFT EMERGENCY LIGHT INOP ON LEFT SIDE. REPLACED CHARGER ASSY. OPS CKS GOOD . 2 L 7 3 4F A3WE 1999101300006 19991013 00006 NM 1999 10 13 DLM90991963 1 19990903 A 2150 ACM 20495072 DOUG MD90 MD9030 3023690 NM LEFT SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 903DA 44110 53383 STRONG UNIDENTIFIED ODOR IN COCKPIT AND CABIN RETURN TO DFW. FOUND LT ACM SEIZED, REPLACED ACM OPN NOW NORMAL. 2 L 7 2 4F RT A6WE 1999101300007 19991013 00007 NM 1999 10 13 DL73K991964 1 19990904 A 2410 O RING 000001128 BOEING 737 737247 138448D NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE CSD DEFORMED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 239WA 23187 709129 AT 30 KTS ON TAKEOFF ROLL HAD NR 1 ENG GENERATOR LOW OIL PRESS LIGHT FLICKER FOLLOWED BY GENERATOR KICKING OFF-LINE. AN ABORT WAS ACCOMPLISHED AND TAXI BACK TO THE GATE. MTC SERVICED NR 1 ENG CSD. PERFORMED ENGINE RUN AND FOUND OIL LEAKI NG FROM CHARGE FILTER AREA ON CSD. REPLACED O-RING ON CHARGE FILTER HOUSING COVER, P/N 012206891. PERFORMED ENG RUN/LE AK CHECK. GENERATOR OPN WAS GOOD. ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1999101300008 19991013 00008 NM 1999 10 13 DL72L991966 1 19990904 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND ON MV-2 CK, 1 INCH CRACK IN STA 1303 WEB WL 270 LBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999101300009 19991013 00009 NM 1999 10 13 DL72L991967 1 19990904 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND ON MV-2 CK, 1 INCH CRACK STA 1303 WEB WL 270 RBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1999101300010 19991013 00010 NM 1999 10 13 DL72L991982 1 19990901 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 936 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND DURING MV2 CORROSION VISIT NRC 196, DURING UPPER WING INSPECTION OPERATION 5621, FOUND 1.5 INCH VISIBLE CRACK AT STR 18 A RT AT STA 936, IN LOWER FLANGE OF STR 18 A. REPAIRED PER M/M 53-12-0. 2 L 7 3 4F A3WE 1999101300011 19991013 00011 NE 1999 10 13 DL75A991983 2 19990907 A 7230 COMPRESSOR BOEING 757 757212 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 750AT 36828 23126 716323 CHS OPS CALLED TO REPORT A/C RTB DUE TO COMPRESSOR STALL AND NR 2 ENG FIRE REPORTED BY THE TOWER. PER FLT CREW, ON TAXI -OUT EXPERIENCED STALL AND TOWER REPORTED FIRE FROM THE BACK OF NR 2 ENGINE. NO EPCS MESSAGES, NO OVERTEMPS. CREW PUSH ED THROTTLE UP A FEW MORE TIMES WITH SUBSEQUENT STALLS. FIRE BOTTLES NOT DISCHARGED. ATL MTC CHANGING NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999101300012 19991013 00012 NM 1999 10 13 DLM90991990 1 19990907 A 3350 POWER SUPPLY RPS1 DOUG MD90 MD9030 3023690 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 903DA 9246 53383 FIRST CLASS EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 2 4F RT A6WE 1999101300013 19991013 00013 NM 1999 10 13 DL72L991991 1 19990905 A 5313 655613522 STRINGER BOEING 727 727232 1384082 NM BS 1137 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 STRINGER 27R WAS FOUND CORRODED AT FS 1137. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333521-14. 2 L 7 3 4F A3WE 1999101300014 19991013 00014 NM 1999 10 13 DL72L991992 1 19990905 A 5713 651858914 STRINGER BOEING 727 727232 1384082 NM WS 304 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 A CRACK WAS FOUND IN THE STRINGER TO RIB ATTACH FLANGE OF WING STRINGER 17R AT WING STATION 304. THE DAMAGE WAS FOUND A T HMV AND REPAIRED PER ERA 333519-14. 2 L 7 3 4F A3WE 1999101300015 19991013 00015 NM 1999 10 13 DL72L991993 1 19990905 A 5313 6519606186 STRINGER BOEING 727 727232 1384082 NM BS 1176 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 TOOLING DAMAGE WAS FOUND ON THE LOWER SURFACE OF STRINGER 17R AT FS 1176. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333504-14K. 2 L 7 3 4F A3WE 1999101300016 19991013 00016 NM 1999 10 13 DL72L991995 1 19990905 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1096 MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 501DA 21303 THE FUSELAGE SKIN WAS MISDRILLED AT FS 1096 AND STRINGER 1 DURING THE ACCOMPLISHMENT OF EO 4-60553-3AD. THIS DAMAGE WA S ADDRESSED BY ER/A 333491-14AD AT HMV. 2 L 7 3 4F A3WE 1999101300017 19991013 00017 NM 1999 10 13 DL72L991996 1 19990905 A 5330 65184207 SKIN BOEING 727 727232 1384082 NM BS 306 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 THE FUSELAGE SKIN WAS GOUGED AT FS 306 AND WL 249 ON THE LHS OF THE AIRCRAFT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333507-14. 2 L 7 3 4F A3WE 1999101300018 19991013 00018 NM 1999 10 13 DL72L991997 1 19990905 A 5320 65561322 FRAME BOEING 727 727232 1384082 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 THE CARGO DOOR OPENING FRAME AT FS 1142 WAS FOUND TO HAVE CORROSION ON THE FORWARD SIDE OF THE WEB. THE DAMAGE WAS REPA IRED PER ER/A 333525-14. 2 L 7 3 4F A3WE 1999101300019 19991013 00019 NM 1999 10 13 DL72L991998 1 19990905 A 5530 65168163 STRINGER BOEING 727 727232 1384082 NM VERT STAB. WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 STRINGER 7L OF THE VERTICAL STABILIZER WAS FOUND TO BE WORN AT FIN STATION 228. THE DAMAGE WAS REPAIRED PER ER/A 333496 . 2 L 7 3 4F A3WE 1999101300020 19991013 00020 NE 1999 10 13 DLM90992000 2 19990908 A 7230 COMPRESSOR DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE STALLED A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 911DA 11911 53391 020035 LT ENG COMPRESSOR STALLED ON TAKEOFF. REPLACING LT ENGINE. 2 L 7 2 4F 4 F RT A6WE E40NE 1999101300021 19991013 00021 NM 1999 10 13 DL76S992002 1 19990908 A 4940 5198586 STARTER BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE APU FAILED A DALA K NONE M OVER TEMP IN INSP/MAINT 1 SO 27 130DL 23620 24080 APU INOP, WILL NOT START. FOUND APU STARTER OVERHEATED AND BURNED ON OUTER CASE. REPLACED STARTER, APU OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 1999101300024 19991013 00024 WP 1999 10 13 TWAA9912502 1 19990912 A 5330 SKIN DOUG DC9 DC933F 302207A WP L 1 DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 DURING CHECK C, A THREE EIGHTHS INCH SKIN CRACK WAS FOUND AT AFT TOP DOOR STOP. REPAIRED SKIN CRACK AT AFT TOP L-1 DOOR OPENING PER S/B 53-280 REV 1, SRO9530252 AND EMLR 69462. 2 L 7 2 4F A6WE 1999101300025 19991013 00025 NM 1999 10 13 AWXA9900301 1 19990902 A 3697 W150801120 WIRE BOEING 737 737375 13844BN NM BLEED AIR REG SHORTED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 336AW 23707 AIR TURNBACK, ON TAKEOFF NR 2 BLEED TRIPPED ON TAKEOFF ROLL. RESET, LIGHT WENT OUT. HOWEVER, RT BLEED GAUGE WOULD NOT MOVE OFF ZERO UNLESS ISO VALVE OPEN. PRESSURIZATION WENT TO 9500 SEE LOG 7395034, 35, AND 36. FOUND WIRE OPEN BETWEEN C/P D1208 AND AIR BLEED REGULATOR, RAN NEW WIRE, CONTINUITY CK GOOD. 2 L 7 2 4F RT A16WE 1999101300026 19991013 00026 NE 1999 10 13 RAIA990813 2 19990813 A 7250 31041033 SEAL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FAILED A RAIA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 CE 03 574HK 41093 76115 FLT 7461 - BHM - RIGHT OIL PRESS LOW. SHUT DOWN ENGINE. MAINTENANCE REPLACED REAR TURBINE BEARING AIR/OIL SEAL. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999101300027 19991013 00027 EU 1999 10 13 RAIA990820 1 19990806 A 2120 ASK226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 574HK 41093 FLT 7492 - STL - RIGHT DUCT FAIL LIGHT ON. MAINTENANCE REPLACED RIGHT INBOARD DUCT SEAL. (M) 2 L 7 2 4T RT A41NM 1999101400001 19991014 00001 EA 1999 10 14 COMA9960522 1 19990915 A 5321 6003401717 FLOOR CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 THE FLOOR MEMBER (P/N 600-34017-17) AT FS 280 IS CRACKED L/2, APPROXIMATELY 1 TO THE RIGHT OF FLOOR SUPPORT AT RBL 9. P ERFORMED A MAJOR REPAIR TO CRACKED FLOOR MEMBER (P/N 600-34017-17) AT FS 280 IAW WVAC EO 601R-53-0325A. 2 L 7 2 4F RT A21EA 1999101400002 19991014 00002 NM 1999 10 14 CALA9901240 1 19990918 A 3230 SWITCH BOEING 737 737824 13844BZ NM LANDING GEAR FAILED A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 18223 28932 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM PIT BOUND FOR EWR. ALL GEAR CIRCUIT BREAKERS WERE PULLED AND ATTE MPTS TO CYCLE GEAR HANDLE UP SEVERAL TIMES WERE UNSUCCESSFUL. THE GREEN AND THREE RED LIGHTS WERE DISPLAYED WITH THE HA NDLE UP. THREE GREEN LIGHTS WERE INDICATED ON THE FORWARD PANEL WITH OVERHEAD LIGHTS WITH THE HANDLE DOWN. THE AIRCRAF T LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE MANUAL GEAR DOOR EXTENSION SWITCH STUCK. THE SWITCH WAS ADJUST ED. A MAIN LANDING GEAR NORMAL AND MANUAL EXTENSION AND RETRACTION WAS PERFORMED WITH NO FAULTS NOTED. 2 L 7 2 4F RT A16WE 1999101400003 19991014 00003 NM 1999 10 14 DL733992097 1 19990917 A 2612 CFM563 FIRE PANEL BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A DALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 27 305WA D00606 23346 721581 NR 2 ENG OVERHEAT LIGHT ILLUMINATED 4 TIMES MOMENTALLY DURING CRUISE. ENG INSTALLED, CHECKED NORMAL. FIRE OVERHEAT AND PNEU SYS CHECKED OK. DESENDED TO FL 220 TO KEEP ENG AT IDLE FOR REMAINDER OF FLT. MASTER CAUTION AND OVERHEAT LIGH T REMAINED OFF. PRIOR TO DESCENT ENG OVERHEAT LIGHT REMAINED ON STEADY, PER POM SHUT DOWN NR 2 ENG AND FIRED BOTH FIRE BOTTLES. REPLACED FIRE DETECTOR PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999101400004 19991014 00004 NM 1999 10 14 DLM90992104 1 19990919 A 3240 50121932 BRAKE DOUG MD90 MD9030 3023690 NM MLG DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DN 53396 WHEN REPLACING NR 3 MAIN TIRE FOUND BRAKE DAMAGED. REPLACED NR 3 MAIN BRAKE ASSY PER M/M. SEVERAL ROTOR TABS BROKEN AN D ROTOR DISC DAMAGED. 2 L 7 2 4F RT A6WE 1999101400005 19991014 00005 1999 10 14 99UAL900490 4 19990923 A 2330 RDAX4406 ENERTAINMENT SYS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ROW 10-11 FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 615UA 21876 ELECTRICAL SMELL IN MID CABIN ROW 10-11 READING LIGHTS AND ENTERTAINMENT SYSTEM NOT ACCEPTING COMMANDS NORMALLY. *S/D* FOUND SEAT ELECTRONIC BOX AT SEAT 9 E, F BURNT. REPLACED SEAT ELECTRONIC BOX. 2 L 7 2 4F 4 F RT A1NM E3NE 1999101400006 19991014 00006 WP 1999 10 14 TWAA9913607 1 19991003 A 3350 0105606003 MODULE DOUG DC9 DC983 3022083 WP ROW 28 WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9412W 53187 THE EGRESS LIGHT STRIP WAS INOPERATIVE AFT OF SEAT ROW 28. INSTALLED A NEW LAMP MODULE. CHECK-C 9-29-99 MCI. 2 L 7 2 4F RT A6WE 1999101400007 19991014 00007 NE 1999 10 14 TWAA9913401 2 19990928 A 7321 FUEL CONTROL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE NR 2 ENGINE FAILED A TWAA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 CE 05 EIBWD 49575 1223 DURING APPROACH TO STL, THE LT ENGINE FLAMED OUT. AFTER EXTENSIVE CHECKS, REPLACED THE ENGINE FUEL CONTROL (P/N 769606- 11) AND THE ENGINE FUEL PUMP (P/N 384301-3). CHECK-C 2-6-99 MCI. 2 L 7 2 4F 4 F RT A6WE E9NE 1999101500001 19991015 00001 CE 1999 10 15 CA990907039 1 19990824 A 3230 M710501 BRUSHES AIRIGHT 10138800519 BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE HARTZL HCB4M HCB4MP3 GL MLG MOTOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1262 246 PCE95282 FW492 (CAN) COULD NOT GET LANDING GEAR DOWN. ALTERNATE GEAR EXTENSION CARRIED OUT. MAINTENANCE CARRIED OUT GEAR FUNCTION CHE CK. WHEN FOURTH RETRACTION WAS ALMOST COMPLETED, 60-AMP CIRCUIT BREAKER TRIPPED. UPON DISASSEMBLY OF HYDRAULIC POWER P ACK MOTOR, IT WAS DISCOVERED THAT THE BRUSHES WERE WORN DOWN TO THE LEAD RIVET. THE COMMUTATOR HAD SIGNS OF ARCHING, AN D THE BEARINGS WERE STARTING TO FEEL ROUGH. THIS MOTOR IS AN 'ON CONDITION' ITEM. ORIGINATOR SUGGESTS A SERVICE LIFE O F 1,200 CYCLES. 2 L 7 2 4T 4 T A24CE E4EA 6 C P56GL 1999101500002 19991015 00002 NM 1999 10 15 CA990907054 1 19990808 A 2420 MS3476L2241S CONNECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AC GENERATOR CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 21833 120584 LH1766 (CAN) NR 2 AC GENERATOR DROPPED OFF-LINE DURING TAXI. CORROSION WAS FOUND ON CANNON PLUG AND ONE PIN FROM THE GCU WAS S TUCK IN THE PLUG RECEPTACLE. PLUG AND GCU WERE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500003 19991015 00003 NM 1999 10 15 CA990907055 1 19990810 A 3234 574205 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 26179 178 120803 LH1789 (CAN) ON APPROACH, LANDING GEAR FAILED TO EXTEND. ALTERNATE GEAR EXTENSION SELECTED. DURING TAXI, NOSE WHEEL STEERING ALSO FAILED. DOWN COIL IN LANDING SELECTOR VALVE WAS U/S. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500004 19991015 00004 NM 1999 10 15 CA990907056 1 19990816 A 7931 522848 INDICATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT INACCURATE W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 19956 08871287 120329 870304 (CAN) IN CRUISE FLIGHT AT 6,000 FEET, THE CREW NOTICED THE NR 1 ENGINE OIL PRESSURE WAS BELOW 55 P.S.I. THE CREW CONTIN UED TO MONITOR THE NR 1 OIL PRESSURE, WHICH DECREASED TO 40 P.S.I. AT WHICH TIME THE CREW ELECTED TO SHUT DOWN THE NR 1 ENGINE. AT MAINTENANCE, THE OIL LEVEL WAS FOUND TO BE THREE QUARTS LOW. THE ENGINE WAS RUN, HOWEVER, THE PRESSURE WOU LD NOT RISE ABOVE 55 P.S.I. THE OIL PRESSURE INDICATOR WAS REPLACED AND AN ENGINE TEST RUN WAS CARRIED OUT WITH OIL PRE SSURE INDICATING 60 P.S.I. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500007 19991015 00007 EA 1999 10 15 CA990907088 1 19990803 A 7603 C2CE479A FRICTION LOCK CT2CE11031 DHAV DHC2 DHC2MK3 2800107 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL POWER LEVER BENT W O OTHER O OTHER DE DESCENT 1 CA PCE42603 BUA19755 (CAN) PILOT REPORTED ENGINE SURGE DURING DESCENT WHEN PULLING POWER LEVER BACK AND THEN LETTING IT GO. INVESTIGATION FO UND THE PL FRICTION LOCK SHAFT WAS BENT, WHICH CAUSED FORWARD PRESSURE ON THE PL ASSEMBLY WHEN IT WAS PULLED BACK. NEW PARTS INSTALLED. 1 H 7 1 3T 4 T A806 E4EA 6 C P15EA 1999101500008 19991015 00008 EA 1999 10 15 CA990915004 1 19990817 A 3010 3301042 DEICE BOOT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE RT WING DETERIORATED W K NONE O OTHER IN INSP/MAINT 1 CA 8536 123113 901009 (CAN) DURING INSPECTION, THE RIGHT HAND (NR 7) LEADING EDGE DEICE BOOT WAS FOUND TO BE DETERIORATED BEYOND SERVICE LIMIT S. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500009 19991015 00009 EA 1999 10 15 CA990915005 1 19990822 A 3244 31X97514 TIRE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 268 0425 123113 901009 (CAN) DURING TAXI FOR TAKEOFF, BOTH RIGHT HAND MAIN WHEEL TIRES FAILED IN THE SIDEWALL AREA. THE NR 4 TIRE CAME OFF THE RIM AND DAMAGED THE OUTBOARD 'WEIGHT ON WHEELS' SENSOR WIRING HARNESS. BOTH TIRES AND THE 'W.O.W' SENSOR WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. BOTH TIRES WERE THOMPSON RECAPS ON THEIR FIRST RECAP CYCLE. THE TIRES HAD 3 14 HOURS S.O.H. AND 268 HOURS S.O.H. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500010 19991015 00010 NM 1999 10 15 CA990915006 1 19990731 A 3242 681895 O-RING BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE DETERIORATED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 13447 1465 1126 120064 860404 (CAN) DURING ROUTINE INSPECTION,THE NR 1 BRAKE WAS FOUND TO BE LEAKING. TEAR DOWN OF THE BRAKE UNIT REVEALED DETERIORAT ED O-RINGS ON TWO OF THE BRAKE PISTONS, AND THE BACK-UP RINGS WERE FOLDED OVER THE PISTON, BETWEEN THE PISTON ASSY AND T HE SLEEVE. THE BRAKE UNIT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500011 19991015 00011 NM 1999 10 15 CA990915007 1 19990816 A 3010 153212A VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE BOOT STUCK W O OTHER O OTHER DE DESCENT 1 CA 27531 RF3907 120064 860404 (CAN) FLIGHT CREW REPORTED THAT THE LEFT NR 3 WING LEADING EDGE DEICE BOOT WOULD NOT DEFLATE AFTER CYCLING. MAINTENANC E REPLACED THE LEFT WING INBOARD DISTRIBUTOR VALVE. THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500012 19991015 00012 NM 1999 10 15 CA990915009 1 19990809 A 3242 681895 O-RING BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE DETERIORATED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 13940 2066 0661 120373 870601 (CAN) DURING ROUTINE INSPECTION ,THE NR 1 BRAKE WAS FOUND TO BE LEAKING. TEAR DOWN OF THE BRAKE UNIT REVEALED DETERIORA TED O-RINGS ON THREE OF THE BRAKE PISTONS, AND THE BACK-UP RINGS WERE FOLDED OVER THE PISTON, BETWEEN THE PISTON ASSY AN D THE SLEEVE. THE BRAKE UNIT WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500013 19991015 00013 NM 1999 10 15 CA990915010 1 19990826 A 3242 214664 BRAKE BFGOODRICH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 3 LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 14808 1024 0352 120373 870601 (CAN) WITH PARKING BRAKE APPLIED, NR 3 BRAKE WAS FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500014 19991015 00014 NM 1999 10 15 CA990915012 1 19990818 A 2910 82970010217 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 NACELLE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120152 891130 (CAN) HYDRAULIC LEAK IN NR 2 NACELLE. PRESSURE LINE BETWEEN SPOILER LIFT/DUMP VALVE FOUND LEAKING. LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500015 19991015 00015 EA 1999 10 15 CA990915013 1 19990814 A 3010 8SC0029028 DEICE BOOT 85720062006 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE RT WING SPLIT W K NONE O OTHER IN INSP/MAINT 1 CA 1525 8897490316A 123116 900837 (CAN) DURING ROUTINE INSPECTION, RIGHT L/E DEICE BOOT WAS FOUND TO HAVE A FEW SMALL SPLITS IN THE SURFACE. FURTHER INVE STIGATION REVEALED SPLITS AND PINHOLES IN EXCESS FOR ALLOWABLE PATCHING. L/E REPLACED WITH BOOT SENT TO MANUFACTURER FO R INVESTIGATION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500016 19991015 00016 NM 1999 10 15 CA990915015 1 19990823 A 2823 AV24B1318D1 ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL SYSTEM FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 21043 3428 N38386S 120854 890709 (CAN) NR 2 FUEL VALVE ON FIRE DETECTION PANEL WAS NOT FUNCTIONING. MAINTENANCE FOUND CIRCUIT BREAKER TRIPPED. VALVE RE PLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500017 19991015 00017 NM 1999 10 15 CA990915016 1 19990929 A 2611 302313 SMOKE DETECTOR KIDDE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CARGO BAY FAILED W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA 18295 0093 120229 870537 (CAN) BAGGAGE COMPARTMENT SMOKE WARNING LIGHT CAME ON MOMENTARILY AND WENT OUT. SMOKE DETECTOR U/S. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500018 19991015 00018 NM 1999 10 15 CA990915017 1 19990820 A 3234 574205 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG SELECTOR FAULTY W A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CA 6368 271 120229 870537 (CAN) CREW WAS UNABLE TO SELECT GEAR DOWN. AIRCRAFT RETURNED TO BASE AND USED ALTERNATE GEAR SELECTION. LANDING GEAR S ELECTOR VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500019 19991015 00019 NM 1999 10 15 CA990915018 1 19990823 A 3234 5352011 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT FAILED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 CA 23570 15262 161 120229 870537 (CAN) CREW REPORTED THAT GEAR DOWN SELECTION PRODUCED 3 UNSAFE INDICATIONS, NO DOOR LIGHTS AND NO GEAR MOVEMENT. NEXT A TTEMPT WAS SUCCESSFUL. UPON LANDING, CREW REPORTED A BURNING SMELL IN COCKPIT. LANDING GEAR SELECTOR HANDLE WAS REPLAC ED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500020 19991015 00020 EA 1999 10 15 CA990915019 1 19990824 A 3242 21517 ROTOR BFGOODRICH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 BRAKE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 4853 1221 0404 123110 870626 (CAN) WHILE REPLACING NR 3 MAIN WHEEL, MAINTENANCE FOUND BRAKE ROTOR TO BE BROKEN IN 3 PLACES. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500021 19991015 00021 NM 1999 10 15 CA990915023 1 19990820 A 2720 DSC474 BEARING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RUDDER PUSHROD WORN W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 CA 120648 881221 (CAN) AIRCRAFT WAS FISHTAILING DURING FLIGHT. OCCURRENCE STOPPED WHEN THE YAW DAMPER WAS SELECTED OFF. REPLACEMENT OF PUSHROD BEARING BETWEEN RUDDER QUADRANT ANDTHE FEEL UNIT WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500022 19991015 00022 EA 1999 10 15 CA990915024 1 19990826 A 3243 53200 VALVE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BRAKE FAILED W O OTHER M OVER TEMP TX TAXI/GRND HDL 1 CA 19165 656 123133 920528 (CAN) AFTER LANDING WITH NO BRAKES USED, THE NR 1 AND NR 2 BRAKES WERE HOT. LEFT BRAKE VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500023 19991015 00023 EA 1999 10 15 CA990915025 1 19990826 A 3350 6104781 POWER SUPPLY DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CABIN INOPERATIVE W K NONE L NO TEST IN INSP/MAINT 1 CA 5456 264 259 123133 920528 (CAN) SEVERAL EMERGENCY LIGHTS INOPERATIVE. POWER SUPPLY 3352-PS1 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500024 19991015 00024 NM 1999 10 15 CA990915026 1 19990816 A 3010 8SC0029028 DEICE BOOT 85720011008 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT WING DISBONDED W O OTHER E VIBRATION/BUFFET DE DESCENT 1 CA 20553 4178 0080192 121165 891129 (CAN) FLIGHT CREW REPORTED AN AUDIBLE FLUTTER ON DESCENT. MAINTENANCE FOUND THE RIGHT INBOARD L/E BOOT DISBONDING FROM THE L/E ASSY ALONG LOWER TRAILING EDGE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500025 19991015 00025 NM 1999 10 15 CA990915031 1 19990828 A 2910 82950010349 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SPOILER ACTUATOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120658 851115 (CAN) HYDRAULIC LEAK IN VICINITY OF LEFT ROLL SPOILER ACTUATOR. LINE TO ACTUATOR LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500026 19991015 00026 NM 1999 10 15 CA990915034 1 19990823 A 5610 8SC0043011 SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE WINDSCREEN LEAKING W O OTHER K FLUID LOSS CL CLIMB 1 CA 3057 98027H5791 120083 901134 (CAN) LOAD SQUEAL FROM FRONT AREA OF COCKPIT WHILE CLIMBING THROUGH 15,000 FEET. MAINTENANCE TORQUED CHECKED SCREWS BEF ORE REPLACING WINDSHIELD. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500027 19991015 00027 NM 1999 10 15 CA990915068 1 19990825 A 3231 82970010391 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG DOOR LEAKING W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA 25077 120581 LH9917 (CAN) HYDRAULIC LEAK IN NR 1 NACELLE AREA. FLUID FROM NR 2 SYSTEM DOOR CLOSED SIDE OF SOLENOID SEQUENCE VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500029 19991015 00029 GL 1999 10 15 CA990915074 1 19990915 A 2822 GP42214145 HARNESS BOMBDR BD700 BD7001A10 1390006 GL BOOST PUMP CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 1300 (CAN) WIRING DAMAGE (CHAFED INSULATION AND/OR CUTS THROUGH INSULATION TO INNER CONDUCTOR) WERE IDENTIFIED ON FUEL PUMP W IRING DURING ELECTRICAL CONNECTOR UPGRADE. CAUSE DETERMINED TO BE FROM IMPROPER TERMINATION OF THE WIRE BUNDLE BRAID AT THE BULKHEAD FEED-THROUGH CONNECTORS. CORRECTIVE ACTON FOR BOMB TO INSPECT ALL AIRCRAFT AND REPAIR, THEN REPLACED ALL DEFECTIVE WIRING WHEN MOD IS DEVELOPED BY PARKER. 2 L 7 2 4F RT T00003NY 1999101500030 19991015 00030 EU 1999 10 15 CA990915077 1 19990901 A 3233 052177 RETAINER A23721208 AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE LT MLG CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 18790 527 304255B (CAN) DURING MAINTENANCE GEAR SWING, IT WAS NOTED THE LEFT MLG ACTUATOR WAS LEAKING. UPON INSPECTION THE PACKING, RETAI NER HAD COME OUT OF THE END OF THE ACTUATOR. PARTS SENT TO DASSAULT AND NEW ACTUATOR INSTALLED. 2 L 7 2 4F 4 F RT A7EU E7EA 1999101500031 19991015 00031 NM 1999 10 15 CA990915078 1 19990902 A 3411 PH11001PH HEATER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PITOT TUBE FAILED W B H EMER. DESCENT DEACTIVATE SYST/CIRCUITS J WARNING INDICATION IN INSP/MAINT 1 CA 7637 6444 120063 860117 (CAN) DURING CRUISE FLIGHT IN ICING CONDITIONS, THE LEFT PITOT HEAT M/C ANNUNCIATED PLUS THE CIRCUIT BREAKER TRIPPED. A IRSPEED DROPPED TO ZERO, LEFT ADC ANN ON, YAW DAMPER KICKED OFF, AND AUTOPILOT DISCONNECTED. ALL LOADS TRANSFERRED. P ITOT TUBE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500032 19991015 00032 EU 1999 10 15 CA990915083 1 19990824 A 5753 F10A124201 TRACK AMD AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE7312 01518 WP RT TE FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10412 P73114C (CAN) RIGHT INBOARD FLAP TRACK FOUND CRACKED. TRACK REPLACED. 2 L 7 2 4F 4 F A33EU E6WE 1999101500033 19991015 00033 EA 1999 10 15 CA990915087 1 19990818 A 2730 C3CF4187 PUSHROD DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL ELEVATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA PCE40906 BUA19623 (CAN) DURING INSPECTION, FOUND THAT THE PUSH/PULL ROD FOR THE ELEVATOR TRIM TAB WAS SEVERELY WORN. THE WEAR SPOT OCCURR ED WHERE THE PUSH/PULL ROD RUNS THROUGH THE B/H AND CONTACTS TWO ROLLERS WHICH IT RIDES ON. THE PUSH/PULL ROD WAS REPLA CED. THE ROLLERS HAD WORN THROUGH THE ROD. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 1999101500034 19991015 00034 EA 1999 10 15 CA990915088 1 19990820 A 2710 C3CF2045 CONTROL CABLE DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL AILERON FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA PCE40906 BUA19623 (CAN) DURING INSPECTION, AILERON CABLES WERE FOUND TO HAVE SEVERAL BROKEN STRANDS. CABLE REPLACED. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 1999101500035 19991015 00035 EA 1999 10 15 CA990915090 1 19990823 A 2730 C3CF4187 PUSHROD DHAV DHC3 DHC3 2800202 EA PWA R1340 S3H1G 52016 NE HAMSTD 23D 23D40 NE ELEVATOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 15072 210666 (CAN) DURING INSPECTION, IT WAS FOUND THAT THE PUSH/PULL ROD FOR THE ELEVATOR TRIM TAB WAS SEVERELY WORN. THE WEAR SPOT OCCURRED WHERE THE PUSH/PULL ROD RUNS THROUGH THE B/H AND CONTACTS TWO ROLLERS WHICH IT RIDES ON. THE PUSH/PULL ROD WA S REPLACED. THE ROLLERS HAD WORN THROUGH THE ROD. 1 H 7 1 3R 3 R A815 E142 6 C P719 1999101500036 19991015 00036 NM 1999 10 15 CA990927004 1 19990912 A 7921 37051 OIL COOLER AEROSPACECMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 17444 0678 120229 870537 (CAN) DURING CLIMB-OUT, THE FLIGHT CREW OBSERVED THE NR 1 ENGINE OIL TEMPERATURE AT 'MAX'. THE AIRCRAFT RETURNED TO BAS E WHERE MAINTENANCE TRACED THE PROBLEM TO THE VERNATHERM FOR THE OIL COOLER DOOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500037 19991015 00037 NM 1999 10 15 CA990927010 1 19990904 A 7160 LA11A2104 ACTUATOR 1716001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 4079 T05447 120854 890709 (CAN) FLIGHT CREW REPORTED THAT THE NR 2 ENGINE INTAKE DOOR WOULD NOT OPEN. PROBLEM TRACED TO THE AIR INTAKE DOOR LINEA R ACTUATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500038 19991015 00038 NM 1999 10 15 CA990927011 1 19990905 A 3010 HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE SYSTEM DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 120854 890709 (CAN) DURING INSPECTION, MAINTENANCE FOUND DAMAGE TO THE ALTERNATE ELEVATOR HORN HEAT WIRING HARNESS IN THE AREA OF FLEX ING AT THE STABILIZER TO ELEVATOR CONNECTION. WIRING HARNESS AND CONNECTORS REPLACED IAW SYD 8-30-00 (B.R.A.D.) 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500039 19991015 00039 NM 1999 10 15 CA990927012 1 19990828 A 2710 82700567S001 CONTROL CABLE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE AILERON WORN W K NONE O OTHER IN INSP/MAINT 1 CA 19664 123124 901161 (CAN) DURING SCHEDULED INSPECTION, THE RIGHT UPPER FORWARD ROLL CONTROL CABLE WAS FOUND WORN BEYOND SERVICE LIMITS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500040 19991015 00040 EA 1999 10 15 CA990927013 1 19990906 A 7603 87600518003 CABLE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 1 ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 123113 901009 (CAN) DURING SCHEDULED MAINTENANCE, THE NR 1 LOWER ENGINE CONDITION LEVER CABLE WAS FOUND FRAYED WHERE IT RIDES ON THE S TEEL PULLEY IN THE ENGINE COMPARTMENT. THE CABLE WAS WORN WHERE IT RIDES ON THE PULLEY IN THE MIN GOVERNING POSITION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500041 19991015 00041 NM 1999 10 15 CA990927015 1 19990902 A 3242 214664 BRAKE BFGOODRICH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 5322 2582 0509 120648 881221 (CAN) DURING SCHEDULED MAINTENANCE, THE NR 1 BRAKE WAS FOUND TO BE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500042 19991015 00042 EA 1999 10 15 CA990927016 1 19990904 A 3244 31X97514 TIRE BFGOODRICH 300 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 504 0539 123133 920528 (CAN) DURING PRE-FLIGHT INSPECTION, THE FLIGHT CREW HEARD AIR LEAKING FROM THE NR 4 MAIN WHEEL TIRE. MAIN MAINTENANCE F OUND A SMALL PIN HOLE IN THE TIRE SIDEWALL. THE TIRE WAS A THOMPSON RECAP. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500043 19991015 00043 EU 1999 10 15 CA990927018 1 19990903 A 6320 350A32315220 BOLT 350A32030004 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R GEARBOX BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 3214 M619 524 (CAN) BOLTS P/N 350A32-3152-20 THAT SECURE BEVEL GEAR TO VERTICAL SHAFT OF BEVEL REDUCTION GEARBOX ASSY WERE FOUND ATTAC HED ONLY FINGER-TIGHT. ONE BOLT/NUT PAIR WAS FOUND SHEARED OFF AND THE OTHER REMAINING 19 BOLT/NUT PAIRS HELD IN POSITI ON BY LOCKPLATES. ALL BOLT SHANKS SHOWING EVIDENCE OF SHEAR FORCE APPLIED. SOME OF THE 19 BOLTS WERE FOUND BENT. 1 G 7 1 3U 3 U NC H9EU E19EU 1999101500045 19991015 00045 EU 1999 10 15 CA990927025 1 19990117 A 6720 704A34130184 CONTROL CABLE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR STUCK W K NONE O OTHER IN INSP/MAINT 1 CA 4154 (CAN) TAIL ROTOR CONTROL CABLE STICKING. CABLE REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 1999101500046 19991015 00046 EU 1999 10 15 CA990927026 1 19990120 A 5210 350A25135009 LOCK CYLINDER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE PASSENGER DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 879 (CAN) PREVIOUS REPAIR ON DOOR LOCK CYLINDER HAS BROKEN. 1 G 7 1 3U 3 U NC H9EU E19EU 1999101500047 19991015 00047 EA 1999 10 15 CA990927027 1 19990126 A 6240 611702020106 BLADE CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE MAIN ROTOR LOW PRESSURE W K NONE O OTHER IN INSP/MAINT 1 CA 3688 61M39293697 295083 (CAN) MAIN ROTOR BLADE BIM INDICATION IN COCKPIT. LOW PRESSUREON BIM TEST. 2 G 7 2 4U 4 U H8EA 1E3 1999101500048 19991015 00048 GL 1999 10 15 CA990927029 2 19990413 A 7323 23057344 GOVERNOR BENDIX BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL TURBINE FAILED W A UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 CA 320704 CAE831797 (CAN) THE TURBINE GOVERNOR WAS REMOVED FOR N2 OVERSPEED (N2 GREATER THAN 114 PERCENT). THE UNIT WAS SENT TO A REPAIR FA CILITY FOR TESTING. 1 G 7 1 3U 3 U H2SW E4CE 1999101500049 19991015 00049 1999 10 15 CA990927032 4 19990511 A 3422 200DC GYRO AIM BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL COCKPIT CRACKED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 211 CAE831797 (CAN) PILOT REPORTED SMOKE IN THE COCKPIT AND THEN LANDED. INVESTIGATION REVEALED THAT THE BACK OF THE DIRECTIONAL GYRO WAS CRACKED AND HAD MELTED PLASTIC DRIPPING OUT. DG WAS INSTALLED AT 11,355.1 HOURS. AIRFRAME TIME, 0.0 HOURS TSO. 1 G 7 1 3U 3 U H2SW E4CE 1999101500050 19991015 00050 SW 1999 10 15 CA990927033 1 19990409 A 6340 HARNESS BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ROTOR TACH MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE820310 (CAN) BAD WIRING CONNECTION TO THE ROTOR TACHOMETER/GENERATOR. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999101500052 19991015 00052 CE 1999 10 15 CA990927041 1 19990908 A 3233 1158100291 ACTUATOR NUT 99810057052 BEECH 99 99 1154002 CE PWA PT6 PT6A20 52043 EA HARTZL HCB3T HCB3TN3 GL RT MLG SEPARATED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 304 PAA83198F PCE20872 BU8002 (CAN) THE RIGHT LANDING GEAR FAILED TO RETRACT SHORTLY AFTER TAKEOFF. UPON INSPECTION IT WAS FOUND THAT THE THREADED IN SERT OF THE ACTUATOR NUT (P/N 115-810029) HAD BEEN PULLED OUT ABOUT 1.50 INCHES; THUS, RESTRICTING THE PULLING ACTION OF THE ACTUATOR SCREW. (SLEEVE PULLED OUT INSTEAD OF GEAR COMING UP). 1 L 7 2 3T 3 T A14CE E4EA 6 C P15EA 1999101500053 19991015 00053 CE 1999 10 15 CA990927042 1 19990914 A 7120 505403042 BEAM CONT CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO MCAULY 3FF32 3FF32C501 GL ENGINE MOUNT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3744 604412 802942 (CAN) DURING SCHEDULED INSPECTION, CRACKS WERE DETECTED ON BEAM CAP AT EITHER END OF THE PART, CLOSE / NEXT TO THE LONGI TUDINAL ENGINE MOUNT BEAMS. PART IS SITUATED DIRECTLY UNDER THE TURBOCHARGER. 1 L 7 2 3O 3 O A7CE E7CE 5 C P45GL 1999101500055 19991015 00055 CE 1999 10 15 CA990927048 1 19990913 A 2750 51152242 CONTROL CABLE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO TE FLAPS BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 9874 278431R (CAN) DURING PRE-FLIGHT INSPECTION, FLAPS WERE EXTENDED AND WOULD NOT RETRACT. PROBLEM WAS TRACED TO A BROKEN FLAP PRES ELECT/FOLLOW-UP CABLE UNDER CABIN FLOOR. 1 L 7 2 3O 3 O A7CE E8CE 1999101500056 19991015 00056 CE 1999 10 15 CA990927051 1 19990630 A 2720 07123091 BELLCRANK CESSNA 180 180A 2072604 CE CONT O470 O470K 17026 SO HARTZL HCC3Y PHCC3YF1 GL RUDDER BROKEN W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 6495 679477L HP285A (CAN) WHILE TAXIING FOR TAKEOFF ON FLOATS, THE RIGHT RUDDER BELLCRANK ARM BROKE AT THE CABLE ATTACHMENT HOLE, CAUSING A LOSS OF DIRECTIONAL CONTROL. AIRCRAFT RETURNED TO DOCK AND THE LEFT AND RIGHT BELLCRANKS WERE REPLACED. 1 H 7 1 3O 3 O 5A6 E273 5 C P25EA 1999101500057 19991015 00057 GL 1999 10 15 CA990927053 2 19990910 A 7323 23057869 GOVERNOR BENDIX BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TURBINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 980 7837 CAE8002228B (CAN) GOVERNOR CIRCLIP EPOXY HAD DETERIORATED TO THE EXTENT THAT THE END DRIVE HAD FALLEN OFF ALLOWING THE CIRCLIP TO MO VE AND AND EVENTUALLY WEAR A GROOVE IN THE SHAFT WHICH ALLOWED THE CIRCLIP TO FALL OFF. AS SUCH, THERE WAS NO LOCKING DEVICE HOLDING THE END DRIVE IN PLACE. 1 G 7 1 3U 3 U H2SW E4CE 1999101500058 19991015 00058 CE 1999 10 15 CA990927054 1 19990906 A 3020 101910049125 SCREEN BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3T* GL RT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE50153 BU3852 (CAN) DURING INSPECTION, THE RIGHT ENGINE INERTIAL SEPARATOR SCREEN WAS FOUND TO BE CRACKED IN SEVERAL PLACES. SUBMITTE R STATED HAD THE DEFECT GONE UNNOTICED, THE ENGINE COMPRESSOR COULD HAVE EASILY INGESTED THE SMALL PIECES. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999101500059 19991015 00059 SO 1999 10 15 CA990927055 1 19990920 A 5520 54992002 BRACKET PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL LT ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5378 PCE52025 BU5790 (CAN) DURING A SCHEDULED INSPECTION, THE LEFT ELEVATOR BALANCE WEIGHT ATTACHMENT BRACKET WAS FOUND TO BE CRACKED AT TWO POINTS, BEHIND THE WEIGHT. PART WAS REPLACED. 1 L 7 2 3T 4 T A8EA E4EA 6 C P15EA 1999101500060 19991015 00060 CE 1999 10 15 CA990927056 1 19990913 A 3230 5082001017 GEAR CHAIN BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL MLG SEPARATED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 5536 PCE51165 EAA1140M1 (CAN) UPON SELECTING GEAR UP, IN-TRANSIT LIGHT STAYED ON. GEAR WAS THEN SELECTED DOWN AND THE MAIN GREEN LIGHTS CAME ON . THE NOSE WAS ABOUT 15 DEGREES FROM DOWN AND LOCKED. THE AFT GEAR CHAIN WAS ACCESSED BY THE FLIGHT CREW AND WITH THE AID OF MAINTENANCE, THEY RE-ATTACHED THE 2 ENDS OF THE CHAIN AND MANUALLY PULLED THE CHAIN UNTIL THE NOSE WAS DOWN AND L OCKED. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 1999101500061 19991015 00061 SO 1999 10 15 CA990927063 1 19990910 A 3233 SFA2324 ACTUATOR PIPER PA44 PA44180 7104402 SO LYC O360 O360E1A6 41514 EA HARTZL HCC2Y HCC2YR2 GL LT MLG LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA RL35077T AU2359 (CAN) WHEN LANDING GEAR WAS SELECTED DOWN, CIRCUIT BREAKERS TRIPPED, RESET AND GEAR CAME DOWN. LEFT LANDING GEAR WAS LE AKING, CHECKED FLUID LEVEL LOW. FOLLOWING REMOVAL OF LEFT AND RIGHT MAIN LANDING GEAR CYLINDERS, IT WAS NOTED THAT PIS TON SHAFT TOO WORN TO ACCOMODATE NEW SEALS. AIRCRAFT HAS 5,538.8 HOURS. NO HISTORY ON PART. REPLACED WITH CLEVELAND ( P/N 455-994) CYLINDERS. 1 L 7 2 3O 3 O A19S0 E286 5 C P920 1999101500062 19991015 00062 SO 1999 10 15 CA990927064 1 19990910 A 5280 2570400 BEARING PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL MLG DOOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA L784561A DJ9338A (CAN) DURING REMOVAL OF INBOARD GEAR DOOR FOR REPLACEMENT OF ONE HINGE BEARING FOR WEAR, THE SECOND BEARING WAS FOUND TO HAVE THE INNER RACE CRACKED CIRCUMFERENTALLY AT THE RACE'S SMALLEST DIAMETER. UN-NOTICEABLE WHEN THE HINGE BOLT IS INS TALLED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999101500063 19991015 00063 CE 1999 10 15 CA990927065 1 19990914 A 2730 556555026 SUPPORT ARM CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3534 71769 (CAN) WHILE PERFORMING A CONTROL COLUMN INSPECTION DURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE ELEVATOR BALANC E WEIGHT SUPPORT ARM. THE CRACK WAS LOCATED APPROXIMATELY 1 INCH FROM BOLT HOLE AT TORQUE TUBE END. 1 L 7 2 4F 4 F A22CE E1NE 1999101500064 19991015 00064 SW 1999 10 15 CA990927066 1 19990917 A 6320 4619304024 PLANETARY AXLE 4638001001 BOLKMS 105 BO105CB* SW ALLSN 250C 250C20 03013 GL M/R GEARBOX SPALLED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 2735 306 (CAN) PLANETARY REDUCTION GEAR SPALLING FOUND ON IMPORT INSPECTION. 1 G 7 2 4U 3 U H3EU E4CE 1999101500065 19991015 00065 CE 1999 10 15 CA990927070 1 19990919 A 2730 115610010325 TORQUE TUBE BEECH 100 A100 1152915 CE PWA PT6 PT6A27 52043 EA RT & LT ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE40865 (CAN) DURING ACCOMPLISHMENT OF SERVICE BULLETIN 2145, CRACKS WERE DETECTED ON BOTH RIGHT AND LEFT TORQUE TUBE ASSEMBLIES (P/N 115-610015-325). LEFT FOUND AT INBOARD SUPPORT (P/N 115-610015-1), RIGHT FOUND AT CENTER SUPPORT (P/N 115-610018- 1). TORQUE TUBES REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 1999101500066 19991015 00066 SW 1999 10 15 CA990927093 1 19990911 A 5302 20603300411A SKIN BELL 206 206L 1181522 SW ALLSN 250C 250C20J 03013 GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA AOKP00637 CAE270419 (CAN) 2.5 INCH LONGITUDINAL CRACK FOUND ON LEFT SIDE OF TAILBOOM APPROXIMATELY 3 INCHES BELOW THE MOST REARWARD T/R DRIV ESHAFT BEARING HANGAR (BS 146 APPROX). TAILBOOM WAS BEYOND LOCAL REPAIR AND SENT BACK TO BELL FOR REPAIR/REPLACEMENT. A PPROX 4,000 HOURS ON THIS TAILBOOM. 1 G 7 1 3U 3 U H2SW E4CE 1999101500067 19991015 00067 SW 1999 10 15 CA991004022 1 19990814 A 2550 206072903101 CABLE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL CARGO HOOK BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 1851 CAE847023 (CAN) CARGO HOOK EMERGENCY RELEASE CABLE BROKE. SUSPECT OUTER SHEATH BROKE FIRST AND THEN INNER CABLE BROKE. IT IS THO UGHT THAT CABLE WAS TOO SHORT. PART SENT TO MANUFACTURER FOR EVALUATION. 1 G 7 1 3U 3 U O H2SW E1GL 1999101500068 19991015 00068 CE 1999 10 15 CA991004028 1 19990923 A 3297 G16A22 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE MLG SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 7568 PCE114352 HJ447 (CAN) LANDING GEAR 2-AMP CONTROL CIRCUIT BREAKER TRIPPED WHEN GEAR SELECTED DOWN. PROBLEM TRACKED TO WIRE NR G16A22 ABO VE TERMINAL BOARD TB, RUBBING ON AIRFRAME. RUBBED THROUGH INSULATION, CAUSING INTERMITTENT SHORT. WIRE REPAIRED AND A IRFRAME TAPED TO PREVENT RECURRENCE OF PROBLEM. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1999101500069 19991015 00069 SW 1999 10 15 CA991004035 1 19990927 A 5302 206032409001 FITTING 20603300411 BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9172 AOKP02008 CAE830889 (CAN) UPPER LEFT TAILBOOM/FUSELAGE ATTACHMENT FITTING CRACKED AT FORWARD RIVET. 1 G 7 1 3U 3 U H2SW E4CE 1999101500070 19991015 00070 EU 1999 10 15 CA991004055 1 19990823 A 2435 524031 STARTER/GENERAT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COMMUTATR BRG AS LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 675 812 (CAN) DURING ROUTINE MAINTENANCE AND BRUSH INSPECTION, IT WAS FOUND THAT THE ASSEMBLY BOLTS SECURING THE COMMUNTATOR BEA RING ASSY TO THE STARTER BODY WERE NOT TAB LOCKED AND THE BOLTS WERE ALSO LOOSE. ANOTHER STARTER/GENERATOR WAS INSPECT ED AND THE BOLTS WERE ALSO FOUND NOT TO BE TAB LOCKED PROPERLY. ALL STARTERS IN THE COMPANY ARE BEING INSPECTED FOR SI MILAR CONDITIONS. 1 G 7 1 3U 3 U H9EU E19EU 1999101500078 19991015 00078 EU 1999 10 15 99ZZZX3861 1 19990528 A 5210 1172428111 CATCHER BOLKMS 117 BK117A4 5626017 EU LEFT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 748 7127 CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500079 19991015 00079 EU 1999 10 15 99ZZZX3862 1 19990528 A 5210 1172428112 CATCHER BOLKMS 117 BK117A4 5626017 EU RT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 748 7127 CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500080 19991015 00080 EU 1999 10 15 99ZZZX3863 1 19990528 A 5210 1172427301 GUIDE BOLKMS 117 BK117A4 5626017 EU LEFT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 589 7127 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500081 19991015 00081 EU 1999 10 15 99ZZZX3864 1 19990507 A 6400 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 144 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500082 19991015 00082 EU 1999 10 15 99ZZZX3865 1 19990127 A 3210 1172428111 CATCHER BOLKMS 117 BK117A4 5626017 EU LEFT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 530 7111 CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500083 19991015 00083 EU 1999 10 15 99ZZZX3866 1 19990127 A 5210 1172428211 CATCHER BOLKMS 117 BK117A4 5626017 EU LEFT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 530 7111 CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500084 19991015 00084 EU 1999 10 15 99ZZZX3867 1 19990127 A 5210 1172428111 CATCHER BOLKMS 117 BK117A4 5626017 EU LEFT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 530 7111 CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500085 19991015 00085 EU 1999 10 15 99ZZZX3868 1 19990610 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A3 5626015 EU ENGINE TORQUE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 625MB 164 987 7108 DURING FLIGHT, TQ READS 20 PERCENT AT ITS HIGHEST POINT. WITH AC MASTER ON, THE TQ INDICATOR SPINS CLOCKWISE 2 TIMES, T HEN FLICKERS BELOW ZERO. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500086 19991015 00086 EU 1999 10 15 99ZZZX3869 1 19990121 A 6420 10531717 BOLT BOLKMS 117 BK117A3 5626015 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MV 251 7089 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500087 19991015 00087 EU 1999 10 15 99ZZZX3870 1 19990323 A 7931 IPT70RT1000250G TRANSDUCER BOLKMS 117 BK117A3 5626015 EU OIL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 127HH 4 60145B98 7060 TRANSDUCER INOPERATIVE. NO OIL PRESSURE INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500088 19991015 00088 EU 1999 10 15 99ZZZX3871 1 19990624 A 6400 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 348 7125 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500089 19991015 00089 EU 1999 10 15 99ZZZX3872 1 19990508 A 7712 L771M20C1002 INDICATOR UROCOP EC135 EC135P1 8680990 EU DUAL TORQUE INOPERATIVE A R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 11 135SJ 408 0034 EC1350054 UNIT INOPERATIVE. UNIT FAILED SELF-TEST. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999101500090 19991015 00090 EU 1999 10 15 99ZZZX3873 1 19990213 A 2842 VTG044 TRANSMITTER BOLKMS 105 BO105LSA3 5626020 EU FUEL QUANTITY MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 189 5252 2015 TUBE SEPARATED FROM SENDING UNIT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1999101500091 19991015 00091 EU 1999 10 15 99ZZZX3874 1 19990119 A 6320 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU GEARBOX INOPERATIAVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 96 V32283 2014 SWITCH INOPERATIVE. FAILS TO ILLUMINATE PRESSURE LIGHT. LIGHT FLICKERS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1999101500092 19991015 00092 EU 1999 10 15 99ZZZX3875 1 19990521 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU ENGINE FLUCTUATED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 581 1002 7229 TRANSDUCER UNIT CAUSES TORQUE INDICATOR FLUCTUATION. NEEDLE FLUCTUATES PLUS 4 PERCENT TO MINUS 4 PERCENT. REPLACED WIT H NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500093 19991015 00093 EU 1999 10 15 99ZZZX3876 1 19990625 A 7810 117651121 TAIL PIPE BOLKMS 117 BK117B1 5626012 EU EXHAUST CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 90260 780 7140 TAIL PIPE CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500094 19991015 00094 EU 1999 10 15 99ZZZX3877 1 19990511 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU ENGINE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 499 964 7231 TRANSDUCER UNIT INOPERATIVE. TORQUE GAUGE GOES TO ZERO. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500095 19991015 00095 NE 1999 10 15 99ZZZX3878 2 19990604 A 7250 414129011 ROTOR ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 2889 314 SC20486 7111 LE45305EA RETENTION LOCK-CUP FAILED. NUT LOOSENED CAUSING FLANGE TO WEAR A GROOVE INTO SPEED INDICATOR PLUG OF PT ROTOR. PART OF THE LOCK-CUP CUT A PORTION OUT OF THE ELBOW CAUSING ENGINE TO LOSE POWER. 1 G 7 2 3U 3 U H13EU E5NE 1999101500096 19991015 00096 EU 1999 10 15 99ZZZX3879 1 19990212 A 6400 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 199 7129 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WIT NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500097 19991015 00097 EU 1999 10 15 99ZZZX3880 1 19990507 A 5210 1172427301 GUIDE BOLKMS 117 BK117B1 5626012 EU DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911VU 416 7141 GUIDE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500098 19991015 00098 EU 1999 10 15 99ZZZX3881 1 19990621 A 6400 ABWT8200B BEARING BOLKMS 117 BK117B1 5626012 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911VU 461 7141 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500099 19991015 00099 EU 1999 10 15 99ZZZX3882 1 19990507 A 5210 11724274101 GUIDE BOLKMS 117 BK117B1 5626012 EU PASSENGER DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911VU 394 7141 GUIDE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500100 19991015 00100 EU 1999 10 15 99ZZZX3883 1 19990108 A 6400 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 176 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500101 19991015 00101 EU 1999 10 15 99ZZZX3884 1 19990319 A 6400 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 146 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500103 19991015 00103 EU 1999 10 15 99ZZZX3886 1 19990827 A 6330 L633M2001105 MOUNT UROCOP EC135 EC135P1 8680990 EU TRANSMISSION LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 219 678 EC1350054 MOUNT LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999101500104 19991015 00104 EU 1999 10 15 99ZZZX3887 1 19990114 A 6400 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 273 7111 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500105 19991015 00105 NM 1999 10 15 HNAA9900135 1 19991007 A 2910 8Z6069125 HYD LINE DHC 8 DHAV DHC8 DHC8102 2809003 NM NR 1 HYD SYS CHAFED A HNAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 933HA 134 134 NR 1 HYD SYS QUANTITY LOSS INFIGHT HAD TO DECLARE EMERGENCY LANDING. REMOVED AND REPLACED CHAFED LINE ANTI-SKID VALVE A ND INSTALLED TFL. SERVICED 6 QTS IN NR 1 SYS, LEAK AND OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999101500106 19991015 00106 WP 1999 10 15 AT9900698 1 19990705 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 503-516 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 FOUND DENT AT LEFT HAND BS 503-516, L-23L, FOUND TO BE 13.5 LONG EXCEEDS LIMITS OF DC9 SRM 53-04 FIGURE 38 TABLE C COND 1B PAR 3. REPAIRED, FABRICATED AND INSTALLED DOUBLER AT BS 503-516, L-23L IAW DC9 SRM 53-04 FIGURE 12B, 51-10-3, 51-30- 2 AND TIMCO EO NR 99-1193 REV IR DATED 20 JULY 99 AND APPROVED BY DC9 SRM 53-01 FIGURE 12B SHEET 2. 2 L 7 2 4F A6WE 1999101500107 19991015 00107 WP 1999 10 15 AT9900699 1 19990714 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 154 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 FOUND ATTACH FITTING TO BE CRACKED AND CORRODED AT SB 154 TO L-10R AND L-13R. TRIMMED OUT CRACK, REPAIRED, FABRICATED A ND INSTALLED GUSSET AND STRAP IAW TIMCO EO 99-1205 REV IR DATED 08/04/99. 2 L 7 2 4F A6WE 1999101500108 19991015 00108 WP 1999 10 15 AT9900700 1 19990714 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 154-11R CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 801AT 47275 FOUND ATTACH FITTING CRACKED AT BS 154 TO STRINGER 11R. TRIMMED OUT CRACK IAW EO 99-1205. REPAIRED, FABRICATED AND INS TALLED GUSSET AND L-ANGLE STRAP IAW DC9 SRM 51-10-3, TIMCO EO 99-1205 REV IR DATED 08/04/99. 2 L 7 2 4F A6WE 1999101500109 19991015 00109 WP 1999 10 15 AT9900701 1 19990723 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 37 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 FOUND CHAFE MARKS ON NOSE BULKHEAD AT BS 37 LT AND RT. BLENDED OUT CHAFE MARKS, FABRICATED AND INSTALLED 2 REPAIRS AT B S 37 LT AND RT IAW DC9 SRM 53-01 FIGURE 4, 51-30-2, 51-10-3 AND TIMCO RES-1 NR 07611. 2 L 7 2 4F A6WE 1999101500110 19991015 00110 WP 1999 10 15 AT9900702 1 19990811 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 FOUND AFT AIR STAIRS ACTUATOR LOWER MOUNT BRACKET CRACKED BEYOND STOP DRILL AT RT OUTBOARD BS 1143. REMOVED 57.5 OF CAN TED FRAME THAT WAS CRACKED BEYOND LIMITS. CUT, TRIMMED, DRILLED, AND DEBURRED NEW SECTION OF FRAME SPLICED IN NEW REPAI R SECTION OF FRAME IAW TIMCO RES-1 NR 02839, DC9 SRM 51-10-3, 51-10-4, 51-30-1, 51-30-2, AND TIMCO EO 99-1223 REV IR DAT ED 08/19/99. 2 L 7 2 4F A6WE 1999101500111 19991015 00111 WP 1999 10 15 AT9900703 1 19990725 A 5510 HINGE DOUG DC9 DC932 3022066 WP LT HORIZ STAB GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 807AT 47444 FOUND LEFT HORIZONTAL STABILIZER NR 1 HINGE BRACKET SKIN GOUGED. REMOVED LEFT HORIZONTAL STABILIZER NR 1 HINGE BRACKET. FABRICATED AND INSTALLED LEFT HORIZONTAL STABILIZER NR 1 HINGE BRACKET IAW DC9 SRM 51-10-2A, 51-10-4, 51-30-1. 2 L 7 2 4F A6WE 1999101500112 19991015 00112 WP 1999 10 15 AT9900704 1 19991002 A 3350 1864 BULB DOUG DC9 DC932 3022066 WP TAILCONE FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 813AT 47318 FOUND BOTH TAIL CONE SLIDE EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED LAMPS IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 1999101500113 19991015 00113 NM 1999 10 15 AT9900705 1 19990930 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 704AT 55006 FOUND DURING TEST SEVERAL CABIN EMERGENCY LIGHTS DID NOT REMAIN ON. REMOVED AND REPLACED BATTERY PACK IAW DC9 MM 33-51- 03. 2 L 7 2 4F TR A6WE 1999101500114 19991015 00114 NM 1999 10 15 CALA9901327 1 19991005 A 3260 656021132 ACCESSORY UNIT BOEING 727 727232 1384082 NM LANDING GEAR INOP A CALA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SW 09 59792 25468 20646 WHEN GEAR WAS RETRACTED AFTER TAKEOFF FROM IAH AND WITH GEAR HANDLE IN THE OFF POSITION ALL LIGHTS WERE OFF. SHORTLY AF TERWARDS THE RED AND GREEN GEAR WARNING LIGHTS CAME ON AND REMAINED ON. THE GEAR HANDLE WAS PLACED TO UP, BUT THE LIGHT S REMAINED ON. THE GEAR HANDLE WAS PLACED TO OFF AND THE LIGHTS WENT SEVERAL MINUTES LATER. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. A GEAR SWIN G WAS PERFORMED WITH GEAR AND LIGHTS FUNCTIONING NORMALLY. 2 L 7 3 4F A3WE 1999101500115 19991015 00115 NM 1999 10 15 CALA9901328 1 19991005 A 2170 COALESCER BOEING 737 737524 1384721 NM CABIN CONTAMINATED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 33637 27540 A STRONG ODOR WAS REPORTED IN THE MAIN CABIN BY FLIGHT ATTENDANTS JUST AFTER TAKEOFF. THE RT PACK WAS TURNED OFF AND OD OR WENT AWAY. THE ODOR WAS DESCRIBED AS HAVING THE SMELL OF BURNING MARSHMALLOWS. MAINTENANCE FOUND A COALESCER BAG CO NTAMINATED. THE BAG WAS REMOVED AND REPLACED. THE RT PACK WAS RUN FULL HOT FOR SEVERAL MINUTES WITH NO ODOR NOTED. NO OTHER DISCREPANCIES WERE NOTED. 2 L 7 2 4F RT A16WE 1999101500116 19991015 00116 WP 1999 10 15 CALA9901329 1 19991004 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 351-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND CABIN SEAT TRACKS CORRODED OR GOUGED AT STA 351-370, LBL 22, STA 1117, LBL 22, STA 1128-1172, LBL 54.5, AND STA 1170-1309, LBL 22. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-11, 51-10-1, 51-30-01, 53-0 5, FIGURES 4B AND 4F. 2 L 7 2 4F A6WE 1999101500117 19991015 00117 WP 1999 10 15 CALA9901330 1 19991004 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP BS 1155-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND CUSP WEB STIFFENER CORRODED IN AFT CARGO AREA OVERHEAD LEFT SIDE BETWEEN FS 1155 AND 1174, LBL 58. THE STIFFENER WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30. 2 L 7 2 4F A6WE 1999101500118 19991015 00118 NM 1999 10 15 CALA9901331 1 19991005 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 23364 INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 360, RBL 50. THE CORROSION WAS REMOVED AND A REPAIR ST RAP WAS INSTALLED IAW ECRA 5311-01074. 2 L 7 2 4F RT A16WE 1999101500119 19991015 00119 WP 1999 10 15 CALA9901332 1 19991005 A 3350 AD4002P BATTERIES MATHEWS DOUG DC9 DC982 3022082 WP L1&R1 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND EMERGENCY LIGHTS ABOVE L-1 AND R-1 DOORS INOPERATIVE. THE BATTERIES IN FORWARD BATTERY PACK WERE REMOV ED AND REPLACED. 2 L 7 2 4F A6WE 1999101500120 19991015 00120 WP 1999 10 15 CALA9901333 1 19991006 A 5532 SKIN DOUG DC9 DC982 3022082 WP VERT STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND VERTICAL STABILIZER LEADING EGDE SKIN GOUGED AND DENTED AT STA ZFS 159. THE DAMAGED AREA WAS TRIMMED O UT. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 55-01, FIGURE 4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999101500121 19991015 00121 WP 1999 10 15 CALA9901334 1 19991006 A 5753 SKIN DOUG DC9 DC982 3022082 WP RT TE FLAP TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND RT FLAP T/E PANEL CORNER DENTED WITH CORNER TORN OFF. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-30-1 AND 57-01, FIGURE 3. 2 L 7 2 4F A6WE 1999101500122 19991015 00122 WP 1999 10 15 CALA9901335 1 19991006 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FLOORBEAM AT STA 1174, RBL 22 CORRODED AND CHAFED FROM CARGO DOOR. THE CORROSION WAS REMOVED IAW SRM 5 1-10-3. A REPAIR FOR THE CHAFING WAS INSTALLED IAW SRM 53-05, FIGURE 86 AND 51-30-5. 2 L 7 2 4F A6WE 1999101500123 19991015 00123 WP 1999 10 15 CALA9901336 1 19991006 A 5280 SKIN DOUG DC10 DC1030 3023501 WP NLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19072 46576 INSPECTION FOUND A 2.5 INCH CRACK IN LT FORWARD NLG DOOR SKIN. THE AREA WAS REPAIRED IAW SRM 52-00-01. 2 L 7 3 4F A22WE 1999101500124 19991015 00124 WP 1999 10 15 9904099959 1 19990930 A 2420 GENERATOR DOUG DC9 DC931 3022065 WP LEFT TRIPPED A NWAA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC AP APPROACH 1 GL 01 919RW 47162 AC CROSSTIE WITH LEFT AC BUS OFF, DC BUS OFF, AND LEFT GENERATOR OFF LIGHTS ILLUMINATED ON APPROACH INTO CLT. FLIGHT CR EW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET LEFT GENERATOR AND CROSSTIE. OPERATIO NAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999101500125 19991015 00125 WP 1999 10 15 9904109970 1 19990929 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999101500126 19991015 00126 WP 1999 10 15 9904119969 1 19991002 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMP INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999101500127 19991015 00127 WP 1999 10 15 9904129140 1 19991004 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999101500128 19991015 00128 WP 1999 10 15 9904139152 1 19991004 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP FWD CABIN EM LTS DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999101500129 19991015 00129 WP 1999 10 15 9904089857 1 19990926 A 3244 95608597 TIRE DOUG DC9 DC951 3022051 WP NR 4 MAIN FAILED A NWAA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 GL 01 766NC 24514 83 47739 DURING TAKEOFF AT ORD, NR 4 MAIN TIRE BLEW AT APPROXIMATELY 140 KNOTS CAUSING EXCESSIVE VIBRATION. FLIGHT WAS CONTINUED TO DESTINATION. CREW DECLARED A YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 4 MAIN TIRE. ALSO, REPAIRED DAMAGE TO AXLE, FLYING DOOR, FLAP AND FUSELAGE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1999101500130 19991015 00130 EA 1999 10 15 COMA9960563 1 19991005 A 5321 6003401717 FLOOR CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 FS 280 IS CRACKED AT RBL 9 OUTBOARD SIDE. PERFORMED A MAJOR REPAIR, FABRICATED AND INSTALLED A REPAIR ANGLE AT FS 280, RBL 9 IAW WVAC EO 601R-53-0394. 2 L 7 2 4F RT A21EA 1999101500131 19991015 00131 EA 1999 10 15 COMA9960564 1 19991005 A 5320 601R311358 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 ANGLE OUTBOARD SIDE RBL 9 AT FS 280 WAS CRACKED. PERFORMED A MAJOR REPAIR, FABRICATED AND INSTALLED A REPAIR ANGLE AT O UTBOARD SIDE RBL 9 AT FS 280 IAW WVAC EO 601R-53-0394. 2 L 7 2 4F RT A21EA 1999101500132 19991015 00132 EA 1999 10 15 COMA9960565 1 19991006 A 5330 PANEL CNDAIR CL600 CL6002B19 EA 326 BT CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 THE LOWER RIGHT PANEL 326 BT ON THE RIGHT SIDE OF SPLIT VISOR CAP WAS WORN APPROXIMATELY 0.050 IN DEPTH, ORIGINAL THICKN ESS 0.100. PERFORMED A MAJOR REPAIR, REMOVED DAMAGED PANEL FROM SPLIT VISOR RT SIDE AND REPLACED PANEL (P/N 601R21010-6 ) PER WVAC EO 601R-55-0395A. 2 L 7 2 4F RT A21EA 1999101500133 19991015 00133 EA 1999 10 15 COMA9960566 1 19991006 A 5320 601R800045 BRACKET CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 ENVIRONMENT DUCT SUPPORT BRACKETS UNDER FLOOR BOARD 272 CRF AND 271 CLF ARE CRACKED.\NREMOVED AND REPLACED ENVIRONMENT D UCT SUPPORT BRACKETS PER WVAC E.O. 601R-36-0396. 2 L 7 2 4F RT A21EA 1999101500134 19991015 00134 EA 1999 10 15 COMA9960567 1 19991005 A 5315 601R530000 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 FLOOR SUPPORT BEAM CAP RBL 9 AND RBL 27 HAS CORROSION FROM FS 280 TO FS 349. PERFORMED A MAJOR REPAIR TO FLOOR SUPPORT BEAM CAPS RBL 9 AND RBL 27, SPLICED IN NEW FLOOR BEAMS (P/N 601R31113-67) IAW REO NR 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999101500135 19991015 00135 EA 1999 10 15 COMA9960568 1 19991005 A 5315 601R5300027 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280-409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 FLOOR SUPPORT BEAM CAP LBL 9 AND LBL 27 HAD CORROSION FROM FS 280 AND FS 409 AND FS 333 TO FS 349 + 16 (P/N 601R31113-67 ). PERFORMED A MAJOR REPAIR TO FLOOR SUPPORT BEAM CAP LBL 9 AND LBL 27 SPLICED IN NEW FLOORBEAMS (P/N 601R31113-67) IAW REO NR 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999101500136 19991015 00136 EA 1999 10 15 COMA9960569 1 19991005 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA PAX DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 PAX DOOR FLOOR SUPPORT L ANGLE CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR REMOVED A CORRODED THRESHOLD ANGLE (P/N 601R31527-181). INSTALLED A NEW THRESHOLD ANGLE MADE FROM EXTRUSION 53992T-068 IAW WVAC EO 601R-53-0392. 2 L 7 2 4F RT A21EA 1999101500137 19991015 00137 EA 1999 10 15 COMA9960570 1 19991005 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 SERVICE DOOR FLOOR SUPPORT L ANGLE CORRODED BEYOND LIMITS (P/N 601R38303-105). PERFORMED A MAJOR REPAIR, REMOVED AND IN STALLED A NEW THRESHOLD ANGLE L (P/N 601R38303-105) IAW WVAC EO 601R-53-0391. 2 L 7 2 4F RT A21EA 1999101500138 19991015 00138 EA 1999 10 15 COMA9960571 1 19991005 A 5330 3867317 PLATE CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 ALL TOP PLATES AT FS 349 WERE CORRODED (P/N 601R38673-17), (601R38673-19), (601R38673-21) AND (601R38673-25). PERFORMED A MAJOR REPAIR, REMOVED THE CORRODED PLATES AT FS 349, FABRICATED AND INSTALLED NEW PLATES USING 7075-T6 ALUMINUM IAW W VAC EO 601R-53-0393. 2 L 7 2 4F RT A21EA 1999101500139 19991015 00139 EA 1999 10 15 COMA9960572 1 19991006 A 5320 BLOCK CNDAIR CL600 CL6002B19 EA BS 718 MISSING A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 924CA 7026 LEFT HAND STRINGER 11 FRAME 718 FORWARD SIDE RADIUS BLOCK WAS MISSING. PERFORMED A MAJOR REPAIR, FABRICATED A NEW RADIU S BLOCK FROM 2024-T3 0.150 INCL AND INSTALLED IAW WVAC EO NR 601R-53-0397. 2 L 7 2 4F RT A21EA 1999101500140 19991015 00140 EA 1999 10 15 COMA9960573 1 19991005 A 5330 PANEL CNDAIR CL600 CL6002B19 EA 326 BT CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 7026 THE LOWER RIGHT PANEL 326BT ON THE RIGHT SIDE OF SPLIT VISOR CAP IS WORN APPROXIMATELY 0.050 IN DEPTH ORIGINAL THICKNESS 0.100. PERFORMED A MAJOR REPAIR, REMOVED THE DAMAGED PANEL AND FABRICATED A NEW PANEL FROM 7075-T6, 0.100 THICK IAW WV AC EO NR 601R-55-0395. 2 L 7 2 4F RT A21EA 1999101500141 19991015 00141 EA 1999 10 15 COMA9960574 1 19991004 A 3250 1C3304 RVDT CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 949CA 7080 DURING CRUISE, FLIGHT THE STEERING FAIL CAUTION MESSAGE ACTIVATED. REPLACED THE RVDT (RIGHT). 2 L 7 2 4F RT A21EA 1999101500142 19991015 00142 EA 1999 10 15 COMA9960575 1 19991005 A 3250 1C3304 RVDT CNDAIR CL600 CL6002B19 EA NLG MISRIGGED A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 964CA 7129 STEERING INOPERATIVE, MESSAGE ACTIVATED AFTER DEPARTURE FROM CVG. AIRCRAFT RETURNED TO THE FIELD. ADJUSTED THE LEFT RV DT. 2 L 7 2 4F RT A21EA 1999101500143 19991015 00143 EA 1999 10 15 COMA9960576 1 19991005 A 3411 PITOT SYS CNDAIR CL600 CL6002B19 EA NR 1&2 CONTAMINATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 937CA 7044 ABORTED TAKEOFF, DUE TO IAS FLAG ON PFD AND 20 KNOT DIFFERENCE IN ASI. PURGED NR 1 AND NR 2 PITOT SYSTEM OF MOISTURE. 2 L 7 2 4F RT A21EA 1999101500144 19991015 00144 EA 1999 10 15 COMA9960577 1 19991006 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY ACTIVATED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 986CA 7174 THE LAVATORY SMOKE WARNING ACTIVATED DURING DESCENT INTO CVG. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY. INSP ECTED THE CARGO AREA AND FOUND NO EVIDENCE OF SMOKE. PERFORMED TEST OF LAVATORY SMOKE DETECTOR, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999101500145 19991015 00145 WP 1999 10 15 UPS99830839 1 19991005 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 4 ENGINE ACTIVATED A IPXA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SO 01 730UP 46030 692602 INSPECTION TYPE:N/A, NR 4 FIRE WARNING CAME ON AFTER SHUTTING DOWN ENGINES. RAN PROCEDURES AND DISCHARGED ONE FIRE BOTT LE. LIGHT WENT OUT AFTER 30 SECONDS AND TESTED NORMAL. REMOVED AND REPLACED FIRE BOTTLE ON RIGHT WING OUTBOARD POSITIO N PER 26-20-01. INSPECTED MEC FOR RIGGING OF FUEL SHUT OFF, POWER LEVER, VSV, VBV, NO DEFECTS NOTED. CHECK OF FIRE SE NSING ELEMENTS REF LP 06 9874/2. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999101500146 19991015 00146 WP 1999 10 15 UPS99830868 1 19991006 A 5610 WINDOW DOUG DC8 DC871F 302199D WP RT COCKPIT JAMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:N/A, F/O SLIDING WINDOW WILL NOT OPEN (JAMMED SHUT). ADJUSTED F/O WINDOW PER MM 56-10-03, OPS CHECK GOO D. 2 L 7 4 4F RT 4A25 1999101500147 19991015 00147 WP 1999 10 15 UPS99830869 1 19991005 A 2150 CONNECTOR DOUG DC8 DC873F 302199F WP RT PACK FAILED A IPXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 866UP 45966 INSPECTION TYPE:N/A, RIGHT PACK COMES ON BY ITSELF WITHOUT ANY COOLING. CREW DISCOVERED SMOKE IN THE COCKPIT. *S/D* R EPLACED CONNECTOR P1-8001 AND REPAIRED BROKEN WIRE AR-7483255AO PER WDM 21-50, ALL OPERATIONAL CHECKS GOOD. 2 L 7 4 4F RT 4A25 1999101500148 19991015 00148 NM 1999 10 15 99FDEA00415 1 19991004 A 5347 X4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 615FE 48767 MAIN DECK UPPER FUSELAGE SEAT TRACK CRACK AT BS 635, X=27.5 RT , BS 635, X-8.5 RT - 135, BS 635, X=47.5 LT-136. *S/D* C ARRIED OUT REPAIR IN ACCORD WITH SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 1999101500149 19991015 00149 NE 1999 10 15 K4HA99077 2 19991002 A 7200 ENGINE BOEING 747 747269B NM PWA JT9 JT9D7J 52054 NE NR 4 FAILED A K4HA A F UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 GL 23 707CK 21541 P701655 NUMBER 4 ENGINE ON TAKEOFF LOST POWER, IFSD AND PULLED FIRE HANDLE. ABNORMAL ENGINE IND-EPR, N1, N2, FF, EGT. REMOVED AND REPLACED ENGINE. 2 L 7 4 4F 4 F RT A20WE E20EA 1999101500150 19991015 00150 WP 1999 10 15 K4HA99078 1 19990817 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 963 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION ON STRINGER. REMOVED CORROSION IAW L1011 SRM 51-21.01. FABRICATED REPAIR PARTS IAW L1011 SRM 53-13-00. INSTALLED REPAIR IAW L1011 SRM 53-13-00 FIG BO X. 2 L 7 3 4F A23WE 1999101500151 19991015 00151 WP 1999 10 15 K4HA99079 1 19990817 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 963 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION. FLOORBEAM WEB CRACKED AT TOOLI NG HOLE. REMOVED DAMAGE IAW L1011 SRM 51-50-01 FIGURE 2. FABRICATED REPAIR PARTS IAW L1011 SRM 51-50-01. INSTALLED RE PAIR IAW L1011 SRM 51-50-01 FIGURE 2. 2 L 7 3 4F A23WE 1999101500152 19991015 00152 WP 1999 10 15 K4HA99080 1 19990817 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP CARGO COMPT CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION. C-3 PIT HAS SURFACE CORROSION ON STRINGER 29. REMOVED CORROSION IAW L1011 SRM 51-21-01. FABRICATED REPAIR PER L1011 SRM 53-30-00, EDR L1-06617. INS TALLED IAW SRM L1011 51-40-01 AND AIA FAR L106617, 2 L 7 3 4F A23WE 1999101500153 19991015 00153 WP 1999 10 15 K4HA99081 1 19990817 A 5320 STIFFENER LKHEED 1011 1011385115 5265015 WP BS 963 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION AND DAMAGE TO FRAME STIFFENER. R EMOVED DAMAGED ATTACH ANGLE IAW L1011 SRM 51-40-01. FABRICATED NEW ATTACH ANGLE IAW L1011 SRM 51-10-05. INSTALLED ATTA CH ANGLE IAW L1011 SRM 51-40-01. 2 L 7 3 4F A23WE 1999101500154 19991015 00154 WP 1999 10 15 K4HA99082 1 19990817 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 1792 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION AND CRACK IN FLOORBEAM FWD UPPER FLANGE. REMOVED FLOORBEAM FLANGE ANGLE PER L1011 SRM 51-40-01. INSTALLED FABRICATED ANGLE PER L1011 SRM 51-40-01. 2 L 7 3 4F A23WE 1999101500155 19991015 00155 WP 1999 10 15 K4HA99083 1 19990817 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1653 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION UNDERNEATH FAIL-SAFE STRAP CUTOU T, APPROX DIMENSION 1.5 W X 3.5 INCHES LONG. CUT STRAP AND REMOVED CORROSION IAW L1011 SRM 53-31-00 FIG 804. FABRICATE D REPAIR PARTS IAW 53-31-00 FIG 804. INSTALLED REPAIR DOUBLER PER L1011 SRM 53-31-00 FIG 804. SEALED FASTENERS AND REP AIR PER L1011 SRM 53-31-00 FIG 816. 2 L 7 3 4F A23WE 1999101500156 19991015 00156 WP 1999 10 15 K4HA99084 1 19990817 A 5320 ANGLE LKHEED 1011 1011385115 5265015 WP BS 963 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND ATTACH ANGLE CORRORDED. REMOVED ATTACH AN GLE IAW L1011 SRM 51-40-01. FABRICATED REPAIR PARTS IAW L1011 SRM 51-50-02. INSTALLED REPAIR IAW L1011 SRM 51-50-02 FI G 2. 2 L 7 3 4F A23WE 1999101500157 19991015 00157 WP 1999 10 15 K4HA99085 1 19990817 A 5320 ANGLE LKHEED 1011 1011385115 5265015 WP BS 971 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION ON ANGLE P 53. REMOVED CORROSIO N IAW L1011 SRM 51-21-01. FABRICATED PART IAW L1011 SRM 51-40-01 AND 51-10-01. INSTALLED PART IAW L1011 SRM 31-40-01 A ND 51-10-01. 2 L 7 3 4F A23WE 1999101500158 19991015 00158 WP 1999 10 15 K4HA99086 1 19990817 A 5320 ANGLE LKHEED 1011 1011385115 5265015 WP BS 963 CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND CORROSION ON P 52 ANGLE, DIMENSION 3 X .5. REMOVED CORROSION IAW L1011 SRM 51-21-01. REMOVED DAMAGE IAW L1011 SRM 53-12-00 FIG 805. FABRICATED REPAIR PARTS IAW L1011 SRM 53-12-00 FIG 805. INSTALLED REPAIR IAW L1011 SRM 53-12-00 FIG 805. 2 L 7 3 4F A23WE 1999101500159 19991015 00159 1999 10 15 TC8A99026 4 19991006 A 2312 5222450114 NAV RECEIVER BOEING 727 72721C 138400M NM NR 1 VHF FAILED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 705A 19134 DURING TAXI-OUT, CAPT'S VOR FLAG IN VIEW. REMOVED AND REPLACED NR 1 VHF NAV RCVR AND SYSTEM OPS GOOD IAW BMM 34-31-0. 2 L 7 3 4F A3WE 1999101500160 19991015 00160 WP 1999 10 15 RAIA9910010 2 19991006 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 CE 03 859AE 15261 2994 859 66121 4710-FAT- DURING T/O ROLL, RIGHT ENGINE INDICATED MORE THAN 650 DEGREES EGT. MAINTENANCE REPLACED RIGHT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999101500187 19991015 00187 CE 1999 10 15 99ZZZX3914 1 19990916 A 3244 TIRE BEECH 99 99 1154002 CE MLG FAILED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 14MV U59 THE TIRE TREAD CAP SEPARATED FROM TIRE ON NEWLY RECAPPED TIRE, 24 TOTAL CYCLES ON TIRE. 1 L 7 2 3T A14CE 1999101500201 19991015 00201 CE 1999 10 15 99ZZZX3928 1 19990916 A 7120 50910279 MOUNT BEECH 99 99 1154002 CE PWA PT6 PT6A27 52043 EA RT ENGINE CHAFED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 199GL U15 PCE40664 UPON REMOVAL OF COMPRESSOR SECTION FROM RT SIDE, LOWER ENGINE MOUNT TUBE ASSY FOUND CHAFED ON TORSION TUBE BEYOND SERVIC EABLE LIMITS. REPLACED ENTIRE MOUNT TUBE ASSY WITH SERVICEABLE MOUNT TUBE ASSY. CHAFE AREA DETERMINED TO BE IN VICINIT Y OF STAINLESS STEEL FIRESHIELD, LOWER SIDE. REPOSITIONED FIRE SHIELD TO ALLOW PROPER CLEARANCE BETWEEN SHIELD AND TUBE ASSY. 1 L 7 2 3T 4 T A14CE E4EA 1999101500206 19991015 00206 NM 1999 10 15 SWAA991671 1 19991007 A 2760 BAC27DCT SWITCH BOEING 737 7372H4 138448C NM COCKPIT OUT OF ADJUST A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 092SW 22964 ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. SPEED BRAKE LEVER WAS CYCLED, AND HORN SILENCED. ADJUSTED SPEED BRAKE T AKEOFF WARNING SWITCH S129 PER MM. 2 L 7 2 4F A16WE 1999101500207 19991015 00207 NM 1999 10 15 SWAA991672 1 19991007 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS IN CABIN OVERHEAD INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F A16WE 1999101500208 19991015 00208 NM 1999 10 15 SWAA991673 1 19991007 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM BS 303.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 303.9, LBL 58, WL 215. REPAIRED FRAME SECTION PER SRM. 2 L 7 2 4F A16WE 1999101500209 19991015 00209 NM 1999 10 15 SWAA991674 1 19991007 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 937 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED AT BS 937. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999101500210 19991015 00210 NM 1999 10 15 SWAA991675 1 19991007 A 5753 6546434 FLAP BOEING 737 7373H4 1384600 NM LT TE AFT FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING WALK ARROUND INSPECTION, FOUND LT WING INBD AFT T/E FLAP DELAMINATED ON OUTBD CORNER. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 1999101500211 19991015 00211 NM 1999 10 15 SWAA991676 1 19991007 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ON RT SIDE ABOVE WING SCANNING LIGHT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999101500212 19991015 00212 NM 1999 10 15 SWAA991677 1 19991007 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 727B, STRINGER 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999101500213 19991015 00213 NM 1999 10 15 SWAA991678 1 19991007 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM LT&RT EMER EXIT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT OVERWING EXITS. SECURED COVERS PER MM. 2 L 7 2 4F RT A16WE 1999101500214 19991015 00214 NM 1999 10 15 SWAA991679 1 19991007 A 5240 6547952 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 630WN 27705 DURING SCHEDULED BC2 CHECK, FOUND FWD SERVICE DOOR EXTERNAL SKIN CRACKED ABOVE LOWER HINGE CUT-OUT. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 1999101500215 19991015 00215 NM 1999 10 15 SWAA991680 1 19991007 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 EMERGENCY EXIT ROW LIGHTS INOP. REPAIRED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999101500216 19991015 00216 NM 1999 10 15 SWAA991681 1 19991007 A 5320 6545410 BEAM BOEING 737 737301 1384611 NM BS 707-710 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/2D CHECK, FOUND CENTER SECTION LONGITUDINAL BEAM CRACKED ON UPPER SURFACE BS 707-710, RBL 24.5. REPA IRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999101500217 19991015 00217 NM 1999 10 15 SWAA991658 1 19991005 A 3230 A42006028305 SOLENOID BOEING 737 737317 138447P NM COCKPIT INOP A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 698SW 23176 AIR TURNBACK, DURING TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE PAST OFF POSITION. LANDING GEARS WOULD NOT RETRACT. R EMOVED AND REPLACED LANDING GEAR CONTROL LEVER SOLENOID PER MM. 2 L 7 2 4F RT A16WE 1999101500218 19991015 00218 NM 1999 10 15 SWAA991659 1 19991005 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 FUSELAGE SKIN CRACKED ON RT SIDE, 24 INCHES BELOW NR 24 WINDOW. REPAIRED FUSELAGE SKIN PER SRM. 2 L 7 2 4F A16WE 1999101500219 19991015 00219 NM 1999 10 15 SWAA991660 1 19991005 A 5330 6545774 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SPECIAL VISIT CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED APPROX BS 727D, STRINGER 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999101500220 19991015 00220 NM 1999 10 15 SWAA991661 1 19991004 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 1010 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED A2 CHECK, FOUND CORROSION AT STRINGER 27R, BS 1010. REPAIRED STRINGER SECTION PER SRM. 2 L 7 2 4F A16WE 1999101500221 19991015 00221 NM 1999 10 15 SWAA991662 1 19991004 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT AFT OF FWD SERVICE DOOR INOP. REMOVED AND REPLACAED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999101500222 19991015 00222 NM 1999 10 15 SWAA991663 1 19991005 A 2131 7638101 CONTROLLER BOEING 737 7373H4 1384600 NM E&E COMPT MALFUNCTIONED A SWAA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 354SW 25219 CABIN PRESSURIZATION FAILED AT 33,000 FEET, CABIN CLIMBED TO 10,000 FEET BEFORE MANUAL MODE CONTROL FUNCTIONED. STANDBY MODE OPS CK GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 1999101500223 19991015 00223 NM 1999 10 15 SWAA991664 1 19991005 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D CHECK, FOUND STRINGER 14R CRACKED AT BS 807. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999101500224 19991015 00224 NM 1999 10 15 SWAA991665 1 19991005 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 14 AND LBL 6. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999101500225 19991015 00225 NM 1999 10 15 SWAA991666 1 19991006 A 5753 6546435334 SKIN BOEING 737 7373H4 1384600 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED SERVICE CHECK, FOUND RT OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500226 19991015 00226 NM 1999 10 15 SWAA991667 1 19991006 A 5315 6546804 FLOORBEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION BS 328 FLOORBEAM UPPER FACE LBL 28. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999101500227 19991015 00227 NM 1999 10 15 SWAA991668 1 19991005 A 5240 6545871 FRAME BOEING 737 7373Y0 1384671 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, AFT FRAME CRACKED AT TWO PLACES. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999101500228 19991015 00228 NM 1999 10 15 SWAA991669 1 19991006 A 5315 6546804 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FACE, BS 294.5, LBL 10.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999101500229 19991015 00229 NM 1999 10 15 SWAA991670 1 19991005 A 2560 D31354 SLIDE BOEING 737 7377H4 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 743SW 29279 DURING SCHEDULED BC3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED SLIDE ASSY P ER MM. 2 L 7 2 4F RT A16WE 1999101500230 19991015 00230 NM 1999 10 15 SWAA991650 1 19991003 A 3350 604222 BATTERY CHARGER BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999101500231 19991015 00231 NM 1999 10 15 SWAA991651 1 19991003 A 3350 30043213 LIGHT BOEING 737 7373H4 1384600 NM RT EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED A1 CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500232 19991015 00232 NM 1999 10 15 SWAA991652 1 19991003 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM LT EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500233 19991015 00233 NM 1999 10 15 SWAA991653 1 19991004 A 3350 604222 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED RON, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999101500234 19991015 00234 NM 1999 10 15 SWAA991654 1 19991004 A 3350 610478 BATTERY CHARGER BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED A1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F A16WE 1999101500235 19991015 00235 NM 1999 10 15 SWAA991655 1 19991004 A 3350 1000679 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT ENTRY DOOR EMERGENCY ENTRY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F A16WE 1999101500236 19991015 00236 NM 1999 10 15 SWAA991656 1 19991004 A 3350 BR2013 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 665WN 23497 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500237 19991015 00237 NM 1999 10 15 SWAA991657 1 19991005 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 747&727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS, BS 747 AND BS 727D, AT STRINGER 19L. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 1999101500238 19991015 00238 NM 1999 10 15 SWAA991643 1 19991001 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP ASS Y PER MM. 2 L 7 2 4F RT A16WE 1999101500239 19991015 00239 NM 1999 10 15 SWAA991644 1 19991001 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE BOTTLE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500240 19991015 00240 NM 1999 10 15 SWAA991645 1 19991001 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE KEEL BEAM LOWER PANEL CRACKED AT MLG WHEEL WELL. REPAIRED PER TRM AND SB 737 -53-1104. 2 L 7 2 4F RT A16WE 1999101500241 19991015 00241 NM 1999 10 15 SWAA991646 1 19991001 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 697 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 617SW 27700 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE KEEL BEAM CRACKED, BS 697. REPAIRED PER TRM AND SB 737-53-1104. 2 L 7 2 4F RT A16WE 1999101500242 19991015 00242 NM 1999 10 15 SWAA991647 1 19991001 A 3397 W116004522 WIRE BOEING 737 737301 1384611 NM BS 975 BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/2D CHECK, FOUND EEPLS HAS BROKEN WIRE AT BATTERY PACK, BS 975. REMOVED AND REPLACED WIRING SECTION P ER MM. 2 L 7 2 4F RT A16WE 1999101500243 19991015 00243 NM 1999 10 15 SWAA991648 1 19991002 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 857 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 857, STRINGER 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999101500244 19991015 00244 NM 1999 10 15 SWAA991649 1 19991003 A 3231 65462052 LINK BOEING 737 7372H4 138448C NM NLG DOOR BROKEN A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 095SW 23054 AIR TURNBACK, DURING CLIMB AND GEAR RETRACTION, A LOUD NOISE FOLLOWED BY A MODERATE VIBRATION WAS HEARD AND FELT. FOUND NOSE LANDING GEAR RT DOOR LINK ASSY BROKEN. REMOVED AND REPLACED DOOR LINK ASSY PER MM. 2 L 7 2 4F A16WE 1999101500245 19991015 00245 NM 1999 10 15 SWAA991641 1 19990930 A 5330 6552880 SKIN BOEING 737 7375H4 138449D NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR LOWER FWD CUT OUT. REPAIRED SKIN PER SWA R A NR 1-553-2164. 2 L 7 2 4F RT A16WE 1999101500246 19991015 00246 NM 1999 10 15 SWAA991642 1 19990929 A 5101 STRUCTURE BOEING 737 7373H4 1384600 NM AIRFRAME BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 354SW 25219 AIR TURNBACK, ACFT STRUCK SEVERAL BIRDS DURING TAKEOFF. C/W BIRD STRIKE INSPECTION PER MM. NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1999101500247 19991015 00247 NM 1999 10 15 SWAA991635 1 19990929 A 5753 654643577 SKIN BOEING 737 7373H4 1384600 NM LT TE AFT FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD AFT FLAP DELAMINATED BETWEEN 2ND AND 3RD TRACKS. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500248 19991015 00248 NM 1999 10 15 SWAA991636 1 19990929 A 2121 65771 FAN BOEING 737 7373H4 1384600 NM E&E COMPT OVERHEATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 331SW 23695 AIRCRAFT DIVERSION, DURING CRUISE ALT, SMOKE SMELL IN MAIN CABIN AND COCKPIT. DIVERTED TO ABQ. FOUND EQUIPMENT COOLING FAN FAILURE. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM. 2 L 7 2 4F RT A16WE 1999101500249 19991015 00249 NM 1999 10 15 SWAA991637 1 19990930 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN DETACHED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 508SW 24185 EEPLS DETACHED AT FWD END. REMOVED AND REPLACED EEPLS FWD SECTION PER MM. 2 L 7 2 4F RT A16WE 1999101500250 19991015 00250 1999 10 15 SWAA991638 4 19990930 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM ESCAPE SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE RELEASE CABLE IMPROPERLY ROUTED. REROUTED CABLE PER MM . 2 L 7 2 4F A16WE 1999101500251 19991015 00251 NM 1999 10 15 SWAA991639 1 19990930 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOORWAY DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED RON, FOUND BOTH FWD ENTRY AND SERVICE DOOR EVACUATION SLIDES COMING OUT OF COVER. INSTALLED SLIDES PER MM. 2 L 7 2 4F RT A16WE 1999101500252 19991015 00252 1999 10 15 SWAA991640 4 19990930 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOORWAY TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EVACUATION SLIDE TORN ON AFT SIDE. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500253 19991015 00253 NM 1999 10 15 SWAA991622 1 19990929 A 3230 233A5502 BREAKER BOEING 737 7377H4 NM COCKPIT TRIPPED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 726SW 27858 AIR TURNBACK, AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT GO INTO THE UP POSITION. FOUND GEAR LATCH AND PRESSURE WARNIN G C/B TRIPPED. RESET C/B AND OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999101500254 19991015 00254 NM 1999 10 15 SWAA991623 1 19990929 A 3350 BR2013 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 637SW 27710 FWD EEPLS MISSING LENS AND LOOSE COVER. REMOVED AND REPLACED LENS AND REINSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 1999101500255 19991015 00255 NM 1999 10 15 SWAA991624 1 19990928 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 EEPLS INOP. REPAIRED WIRE IN AFT CABIN PER WIRING DIAGRAM. 2 L 7 2 4F RT A16WE 1999101500256 19991015 00256 NM 1999 10 15 SWAA991625 1 19990928 A 3350 100031 CONNECTOR BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED C2 CHECK, FOUND MID AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPAIRED D5118 CONNECTOR. OP CHECKED GOOD. 2 L 7 2 4F A16WE 1999101500257 19991015 00257 NM 1999 10 15 SWAA991626 1 19990928 A 2560 65C19901 CABLES BOEING 737 7372H4 138448C NM SERVICE DOOR MISSROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 FWD AND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE NOT ROUTED PROPPERLY. REROUTED SLIDE CABLES PER MM. 2 L 7 2 4F A16WE 1999101500258 19991015 00258 NM 1999 10 15 SWAA991627 1 19990928 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM AT FASTENER HOLE, BS 986, RBL 38. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999101500259 19991015 00259 NM 1999 10 15 SWAA991628 1 19990929 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SPECIAL VISIT, FOUND SEVERAL EEPLS INOP. REMOVED AND REPLACED LIGHTS PER MM. 2 L 7 2 4F A16WE 1999101500260 19991015 00260 1999 10 15 SWAA991629 4 19990929 A 2565 65C19901 CABLE BOEING 737 7373H4 1384600 NM PAX DOORWAY FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY EVACUATON SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED SLIDE ASSY PER MM . 2 L 7 2 4F RT A16WE 1999101500261 19991015 00261 NM 1999 10 15 SWAA991630 1 19990929 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AROUND AIR CONDITIONING GROUND SERVICE CONNECTION CUT OUT. REPAIR ED SKIN PER SRM AND ER NR 99-6051A. 2 L 7 2 4F RT A16WE 1999101500262 19991015 00262 NM 1999 10 15 SWAA991631 1 19990929 A 3350 6574550 CONNECTOR BOEING 737 7373H4 1384600 NM SERVICE DOORWAY BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE EXTERIOR LIGHT CONNECTOR CAP BROKEN. REMOVED AND REPL ACED LIGHT HOUSING PER MM. 2 L 7 2 4F RT A16WE 1999101500263 19991015 00263 NM 1999 10 15 SWAA991632 1 19990929 A 5320 6969854 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED ON LOWER END. REPAIRED FRAME PER BOEING REPAIR DR AWING. 2 L 7 2 4F RT A16WE 1999101500264 19991015 00264 NM 1999 10 15 SWAA991633 1 19990929 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 714CB 27848 DURING SCHEDULED SERVICE CHECK, FOUND FWD EEPLS LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999101500265 19991015 00265 NM 1999 10 15 SWAA991634 1 19990929 A 2612 894091 FIRE LOOP BOEING 737 7372H4 138448C NM NR 1 ENGINE FAILED A SWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 07 061SW 21970 AIR TURNBACK, IN FLIGHT ENGINE SHUT DOWN. DURING CLIMB, NR 1 ENG INDICATED FIRE WARNING. BOTH FIRE BOTTLES WERE DISCHA RGED. REMOVED AND REPLACED FAULTY UPPER FIRE LOOP DETECTOR AT PYLON PER MM. 2 L 7 2 4F A16WE 1999101500266 19991015 00266 NM 1999 10 15 SWAA991616 1 19990928 A 3230 6554219 LEVER BOEING 737 7373H4 1384600 NM LANDING GEAR MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 687SW 23388 AIR TURNBACK, LANDING GEAR LEVER WOULD NOT GO INTO UP POSITION AFTER TAKEOFF. PERFORMED LANDING GEAR RETRACTION TEST AN D LANDING GEAR SAFETY SENSOR TEST PER MM. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999101500267 19991015 00267 NM 1999 10 15 SWAA991617 1 19990928 A 2810 MS29513 O-RING BOEING 737 7373H4 1384600 NM LTWING LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 311SW 23333 AIR TURNBACK, PASSENGER REPORTED FLUID LEAKING (APPARENTLY FUEL) FROM LT WING UPPER SURFACE AROUND FUEL CAP. INSPECTED LT UPPER WING. NO LEAK FOUND. REMOVED AND REPLACED LT WING UPPER FUELING CAP O-RING AS A PRECAUTION. 2 L 7 2 4F RT A16WE 1999101500268 19991015 00268 NM 1999 10 15 SWAA991618 1 19990927 A 3350 P2070001 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999101500269 19991015 00269 NM 1999 10 15 SWAA991619 1 19990927 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999101500270 19991015 00270 NM 1999 10 15 SWAA991620 1 19990927 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS, BS 178 BULKHEAD, RBL 5 AND LBL 5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999101500271 19991015 00271 NM 1999 10 15 SWAA991621 1 19990927 A 5312 6517582 BULKHEAD CHORD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED 1/4D CHECK, FOUND BS 178, RT SIDE CHORD CRACKED, RBL 26. REMOVED AND REPLACED CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999101500272 19991015 00272 NM 1999 10 15 SWAA991615 1 19990928 A 2560 65C16820 GIRT BAR BOEING 737 7373H4 1384600 NM PAX DOORWAY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR OUT OF HANGERS. REPOSITIONED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 1999101500273 19991015 00273 NM 1999 10 15 SWAA991609 1 19990927 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 EEPLS INOP. RECONNECTED AFT EEPLS WIRING AT CANNON PLUG PER WIRING DIAGRAM. 2 L 7 2 4F RT A16WE 1999101500274 19991015 00274 NM 1999 10 15 SWAA991610 1 19990925 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701GS 27836 EEPLS TRACK LOOSE AT FWD END. REINSTALLED TRACK ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500275 19991015 00275 NM 1999 10 15 SWAA991611 1 19990925 A 5755 6573730 SKIN BOEING 737 7372H4 138448C NM NR 2&7 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED SPECIAL VISIT, FOUND NR 2 AND NR 7 FLIGHT SPOILERS DELAMINATED. REMOVED AND REPLACED BOTH SPOILER ASSY 'S PER MM. 2 L 7 2 4F A16WE 1999101500276 19991015 00276 NM 1999 10 15 SWAA991612 1 19990925 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND BS 328 FLOORBEAM UPPER CHORD CORRODED, RBL 20-RBL 40. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999101500277 19991015 00277 NM 1999 10 15 SWAA991613 1 19990926 A 3350 312062 LENS BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 308SA 23498 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500278 19991015 00278 NM 1999 10 15 SWAA991614 1 19990926 A 3350 6556633 BULB BOEING 737 7373G7 1384595 NM RT EMER EXIT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXIT SIGN INOP. RELAMPED SIGN PER MM. 2 L 7 2 4F RT A16WE 1999101500279 19991015 00279 NM 1999 10 15 SWAA991601 1 19990926 A 2530 A97002G LATCH BOEING 737 7373H4 1384600 NM FWD LAVATORY BROKEN A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 368SW 26579 AIR TURNBACK, AFTER TAKEOFF, A THUMPING NOISE HEARD ON FWD LAV. FOUND FWD LAV SINK CABINET DOOR OPENED AND LATCH BROKEN . REMOVED AND REPLACED LATCH ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500280 19991015 00280 NM 1999 10 15 SWAA991602 1 19990924 A 2560 63550101 SLIDE BOEING 737 7377H4 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 730SW 27862 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT DURING DOOR OPENING. (DID NOT DEPLOYED). REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500281 19991015 00281 NM 1999 10 15 SWAA991603 1 19990924 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 EEPLS TRACK LOOSE AT MID CABIN. REINSTALLED EEPLS TRACK LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500282 19991015 00282 NM 1999 10 15 SWAA991604 1 19990924 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT DURING DOOR OPENING. (DID NOT DEPLOYED). REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500283 19991015 00283 NM 1999 10 15 SWAA991605 1 19990924 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 AFT SERVICE DOOR SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999101500284 19991015 00284 NM 1999 10 15 SWAA991606 1 19990924 A 2131 7638101 CONTROLLER BOEING 737 7373H4 1384600 NM E&E COMPT MALFUNCTIONED A SWAA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 SW 07 687SW 23388 AIR TURNBACK, DURING FLIGHT AT 37,000 FEET, CABIN ALTITUDE WARNING HORN SOUNDED ALERTING THE CABIN ALTITUDE WAS 10,000 F T. DECLARED EMERGENCY LANDING. CABIN ALTITUDE NEVER GOT ABOVE 10,000 FT AND THE DESCENT WAS NORMAL. INSPECTED ALL DOO R PRESS SEALS, PRESS DUCTINGS, C/W BITE CHECK ON PRESS CONTROLLER, PRESSURIZED ACFT AND PERFORMED LEAK CHECK. NO LEAKS FOUND AND PRESS SYSTEM OP CHECKED GOOD. LATER AT HOU, REMOVED AND REPLACED PRESS RATIO AUTO CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 1999101500285 19991015 00285 NM 1999 10 15 SWAA991607 1 19990924 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 907, LBL 2, WL 303. REPAIRED FRAME PER ER NR 99-6081. 2 L 7 2 4F RT A16WE 1999101500286 19991015 00286 NM 1999 10 15 SWAA991608 1 19990924 A 5320 6546529 SHEAR TIES BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED D CHECK, FOUND 2 EACH FUSELAGE SHEAR TIES CRACKED, BS 360 BETWEEN STRINGERS 14L-15L AND 14R-15R. REPAI RED SHEAR TIES PER SRM. 2 L 7 2 4F RT A16WE 1999101500287 19991015 00287 NM 1999 10 15 TWAA9913801 1 19991006 A 2910 LINE BOEING 727 727231 1384079 NM B HYD SYS RUPTURED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 05 54350 21969 DURING FLIGHT THE 'B' HYDRAULIC SYSTEM FLUID WAS LOST RESULTING IN LOSS OF THE SYSTEM HYDRAULIC PUMPS. USED PNEUMATIC B RAKES DURING LANDING. REPLACED TWO HYDRAULIC LINES, MFG AE1008787H290 AND AE3660130K0290. CHECK-C 1-29-99 MCI. 2 L 7 3 4F A3WE 1999101500288 19991015 00288 WP 1999 10 15 TWAA9913802 1 19991007 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP ROW 2,4,10&33 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9409F 53121 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW 2, 4, 10, AND 33. REPLACED LAMP AT EACH LOCATION. CHECK-C 5-18-99 STL. 2 L 7 2 4F RT A6WE 1999101500289 19991015 00289 WP 1999 10 15 TWAA9913901 1 19991009 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC983 3022083 WP ROW 8DEF DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9403W 53139 THE EMERGENCY LIGHTS WERE INOPERATIVE AT SEAT ROWS 8, 9, AND 10. REPLACED THE POWER SUPPLY. CHECK-C 9-1-99 STL. 2 L 7 2 4F RT A6WE 1999101500290 19991015 00290 WP 1999 10 15 TWAA9913902 1 19991009 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC983 3022083 WP PAX DOOR INOP A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9622A 53593 THE EMERGENCY EXIT LIGHTS IN THE COCKPIT WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-4-99 STL. 2 L 7 2 4F RT A6WE 1999101500291 19991015 00291 WP 1999 10 15 TWAA9913903 1 19991009 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC983 3022083 WP ROW 12 INOP A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9618A 9 53565 THE EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN ROWS 4 AND 12. REPLACED THE POWER SUPPLY. CHECK-C 9-3-99 STL. 2 L 7 2 4F RT A6WE 1999101500292 19991015 00292 NM 1999 10 15 TWAA9913904 1 19991010 A 7930 8D1467 SWITCH BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 05 602TW 22565 4605 IN AN ETOPS FLIGHT SEGMENT THE LEFT ENGINE FILTER BYPASS LIGHT BLINKED THEN CAME ON STEADY. THE ENGINE WAS SHUT DOWN AN D THE FLIGHT DIVERTED TO TER. THE MAIN OIL SCREEN AND CHIP DETECTORS WERE CLEAN. PLACARD THE FILTER BYPASS LIGHT INOPE RATIVE PER MEL AND THE FLIGHT CONTINUED. CHECK-C 8-25-99 LAX. *S/D* THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH WAS R EPLACED TO CORRECT THE MALFUNCTION. 2 L 7 2 4F 4 F RT A1NM E3NE 1999101500293 19991015 00293 WP 1999 10 15 TWAA9913905 1 19991008 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 680 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 976Z 47248 DURING CHECK-C MAINT, FOUND LONGERON 8L WAS CRACKED .375 INCHES AT STA 680. SPLICED NEW SECTION OF LONGERON USING SRM 5 3-02, FIG 18 FOR SPLICE. 2 L 7 2 4F A6WE 1999101500294 19991015 00294 NM 1999 10 15 HNAA9900136 1 19991010 A 2120 AIR DIST DHAV DHC8 DHC8201 2809001 NM CABIN SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 965HA 450 DURING ENGINE START (NR 2), CABIN AND COCKPIT FILLED WITH LIGHT SMOKE. 2 H 7 2 4T RT A13NM 1999101500295 19991015 00295 WP 1999 10 15 AT9900694 1 19991003 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND IN CABIN FORWARD SECTION AT RIGHT FLOOR SUPPORT 10 FROM SERVICE DOOR WAS CORRODED, BS 160-200. REMOVED CORRODED F LOOR SUPPORT, FABRICATED AND INSTALLED REPAIR SUPPORT IAW DC9 SRM 51-10-2, 51-10-4, 51-10-3, 53-01 FIGURE 1, 51-30-5. 2 L 7 2 4F A6WE 1999101500296 19991015 00296 WP 1999 10 15 AT9900708 1 19990928 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND FLOOR SUPPORT AT BS 200-218 WAS CORRODED, ABOUT 14 FROM CENTER LINE. REMOVED FLOOR SUPPORT, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-4, 51-30-1. 2 L 7 2 4F A6WE 1999101500297 19991015 00297 WP 1999 10 15 AT9900709 1 19990911 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 455.3 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND A DENT OUT OF LIMITS AT BS 445.3 BELOW L 19R. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR IAW TIMCO EO 99-1281 REV DATED 10/01/99. 2 L 7 2 4F A6WE 1999101500298 19991015 00298 WP 1999 10 15 AT9900710 1 19990912 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEV CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT OUTBOARD ELEVATOR UPPER TRAILING EDGE AT THE TIP WAS CORRODED. CUT OUT CORROSION. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2 AND 55-03 FIGURE 5. 2 L 7 2 4F A6WE 1999101500299 19991015 00299 WP 1999 10 15 AT9900711 1 19990924 A 5260 STEP DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND AFT AIRSTAIR, FOURTH STEP FROM THE BOTTOM, WEB ON INBOARD AND OUTBOARD SIDE OF STEP WAS CORRODED. CUT OUT CORROSI ON, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLERS AND ATTACH ANGLE IAW DC9 SRM 52-01 FIGURE 1, 51-30-2, 51-20-4, 51- 10-2. 2 L 7 2 4F A6WE 1999101500300 19991015 00300 WP 1999 10 15 AT9900713 1 19991006 A 5400 ANGLE DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT PYLON WEB LOWER SUPORT ANGLE FOUND 3 CRACK, PYLON STATION 105 3 BELOW PYLON REFERANCE PLANE, 5 OUTBOARD FUSE LAGE SKIN. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2, 51- 30-4. 2 L 7 2 4F A6WE 1999101500301 19991015 00301 WP 1999 10 15 AT9900714 1 19991001 A 5320 59122851 WINDOW FRAME DOUG DC9 DC932 3022066 WP BS 699 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND UPPER CORNER OF WINDOW FRAME WAS CRACKED AT BS 699R. REMOVED WINDOW FRAME, INSTALLED NEW WINDOW FRAME IAW DC9 SRM 51-30-5, 53-04 FIGURE 34. 2 L 7 2 4F A6WE 1999101500302 19991015 00302 EA 1999 10 15 JBXA9900107 1 19991010 A 2742 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE HORIZ STAB FAILED A JBXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 05 582ML 7322 ON FLT NR 289, CLIMB-OUT FROM RDU, CREW RECEIVED AP PITCH TRIM AND AP MACH TRIM MESSAGE. CREW HAD TO USE MANUAL TRIM. R EMOVED AND REPLACED HSTA IAW MM 27-42-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999101500303 19991015 00303 NM 1999 10 15 AWXA9900346 1 19991004 A 2761 65445616 ACTUATOR BOEING 737 7373G7 1384595 NM NR 6 SPOILER FAILED A AWXA D RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 28 155AW 48179 23582 23777 AIR TURNBACK, AIRFRAME VIBRATION, LOG 7555408, ON CLIMB-OUT OF MCI, AFTER FLAPS RETRACTED AND ACCELERATION THROUGH FL230 , STARTED FEELING VIBRATION THROUGHOUT A/C. DID NOT GO AWAY AFTER PWR REDUCTION ON EACH ENGINE . TROUBLESHOT AND REPLACED NR 6 SPOILER ACTUATOR PER R3M27021. OPS CK GOOD 2 L 7 2 4F RT A16WE 1999101500304 19991015 00304 NM 1999 10 15 AWXA9900347 1 19991008 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM FWD/AFT CABIN UNSERVICEABLE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 SEVERAL EMERGENCY LTS INOP IN FWD AND AFT SECTIONS OF A/C. REMOVED AND REPLACED FWD AND AFT BATTERY PACKS, ALSO L1 AND R1 DOOR BATTERIES. 2 L 7 2 4F RT A16WE 1999101500305 19991015 00305 NM 1999 10 15 AWXA9900348 1 19991008 A 5753 654648195 CARRIAGE BOEING 737 737277 1384570 NM LT TE FLAP FAILED A AWXA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 WP 28 189AW 22656 AFTER EXTENDING FLAPS PAST 10 DEG EXTREME RT AILERON WAS REQUIRED UP (200X), WIND NO FACTOR REFER TO LOG 7554389. FOUN D NR 2 FLAP CARRIAGE BROKEN AT SPINDLE. REMOVED AND REPLACED OF CARRIAGE IN PROGRESS. 2 L 7 2 4F RT A16WE 1999101500306 19991015 00306 EU 1999 10 15 AWXA9900349 1 19991011 A 3240 8825604644 ACCUMULATOR AIRBUS 320 A320231 3930325 EU BRAKE SYS FAILED A AWXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 28 634AW 225 225 091 WHEN PUSH WAS COMPLETED SET BRAKE AND FOUND NO ACCUMULATOR PRESSURE OR BRAKE PRESSURE. RE MOVED AND REPLACED BRAKE ACCUMULATOR, OPS AND LK CK GOOD. 2 L 7 2 4F RT A28NM 1999101500307 19991015 00307 EU 1999 10 15 AWXA9900350 1 19991011 A 3250 C20216332292C BSCU AIRBUS 320 A320231 3930325 EU NLG STEERING FAILED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 28 627AW 21248 5528 66 ABORTED TAKEOFF, UNCOMMANDED VEERING TO THE RIGHT THEN TO THE LEFT, BSCU CHANNEL 2 FAULT ON U PPER ECAM NO ASSOCIATED DATA. REMOVED AND REPLACED BSCU, OPS CK NML IAW MM 32-42-000-001. 2 L 7 2 4F RT A28NM 1999101500308 19991015 00308 NM 1999 10 15 AWXA9900351 1 19991011 A 8011 35057163 STARTER BOEING 737 73733A 1384673 NM NR 2 ENGINE FAILED A AWXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 28 167AW 63497 37479 23628 DURING ENG START GROUND CREW REPORTED ENG NR 2 FIRE. COMPLIED WITH ENG FIRE SERVICE. DAMAGE CHECKLIST FOLLOWED BY QRL CK, NO IND IN FIRE HANDLE. NOTED SPARKS IN FRONT OF ENGINE, NO FIRE IN REAR. REMOVED AND REPLACED NR 2 ENG STARTER. 2 L 7 2 4F RT A16WE 1999101500309 19991015 00309 NM 1999 10 15 AWXA9900352 1 19991011 A 4950 38042861 APU BOEING 737 73733A 1384673 NM APU COMP MALFUNCTIONED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 28 509DC 61695 13978 23636 FAINT BURNING SMELL IN COCKPIT. T/S AIR CONDITIONING SYSTEM, DETERMINED TO BE APU BLEED. PLACED ON MEL 49-01, CNTL NR 121373. 2 L 7 2 4F RT A16WE 1999101500310 19991015 00310 EU 1999 10 15 AWXA9900353 1 19991011 A 3397 WIRE AIRBUS 320 A320231 3930325 EU ROW 9 BROKEN A AWXA O OTHER L NO TEST IN INSP/MAINT 1 WP 28 646AW 271 SEAT 9 RT EMERGENCY EXIT LIGHT INOP. REPAIRED WIRING, OPS CK NML. 2 L 7 2 4F RT A28NM 1999101500311 19991015 00311 NM 1999 10 15 AWXA9900354 1 19991011 A 3350 900835A BATTERY PACK BOEING 737 7372U9 1384498 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 AFT SECTION OF EMERGENCY LTS REMAIN ON AFTER ALL POWER IS SECURED FROM AIRCRAFT. REMOVED AND REPLACED BATTERY PACK, OPS CK NML. 2 L 7 2 4F RT A16WE 1999101500312 19991015 00312 WP 1999 10 15 CALA9901337 1 19991007 A 3232 59370365001 ACTUATOR DOUG DC9 DC982 3022082 WP LT MLG DOOR INOP A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 93875 48178 49125 THE LT MLG SHOWED RED UNSAFE LIGHT WITH DOOR LIGHT OUT AFTER GEAR RETRACTION. THE GEAR WAS RECYCLED IAW CHECKLIST AND G EAR INDICATED NORMAL. THE LT GEAR ACTUATING CYLINDER WAS REMOVED AND REPLACED IAW MM 32-32-02. THE LT MLG DOOR ACTUATI NG CYLINDER AND DOOR LATCH MECHANISM WERE ADJUSTED IAW MM 32-32-04 AND MM 32-31-04, STEPS 6-20. THE DOOR LATCH WAS TEST ED IAW MM 32-31-04 AND THE GEAR WAS SWUNG SEVERAL TIMES WITH NO FAULTS FOUND. 2 L 7 2 4F A6WE 1999101500313 19991015 00313 WP 1999 10 15 CALA9901338 1 19991007 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 389 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A GOUGE IN FORWARD CARGO COMPARTMENT CEILING BEAM AT STA 389, RBL 2. THE GOUGED AREA WAS BLENDED OUT A ND REPAIR PARTS WERE INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4, 51-10-3, 51-30-5, AND 53-03, FIGURE 86. 2 L 7 2 4F A6WE 1999101500314 19991015 00314 WP 1999 10 15 CALA9901339 1 19991007 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 229-294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION SEAT TRACKS CORRODED AT STA 229, RBL 22, STA 237-250, RBL 22, AND STA 237-294, LBL 22. THE SEAT TRACK SECTIO NS WERE REMOVED AND REPLACED IAW SRM 53-05, FIGURE4F, 51-10-03, AND 51-30-01. 2 L 7 2 4F A6WE 1999101500315 19991015 00315 WP 1999 10 15 CALA9901340 1 19991008 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 617-1103 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND SEAT TRACKS CORRODED AT FS 617-712, RBL 54.5 AND FS 1098-1103, LBL 22. THE SEAT TRACK SECTIONS WERE RE MOVED AND REPLACED IAW SRM 51-30-1, 51-10-4, 51-30-5, AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999101500316 19991015 00316 WP 1999 10 15 CALA9901341 1 19991007 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 230 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 3 INCH CRACK IN CUSP WEB AT STA 230, LONGERON 18L. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999101500317 19991015 00317 WP 1999 10 15 CALA9901342 1 19991007 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 267 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A .5 INCH CRACK IN RT WING UPPER SKIN AT I/B SPOILER O/B HINGE, XRS 267. THE PANEL WAS REMOVED IAW MM 27-62-01, SRM 51-30-1, 51-30-2, AND 51-30-5. THE PANEL WAS REPAIRED AND REINSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND MM 27-62-01. 2 L 7 2 4F A6WE 1999101500318 19991015 00318 WP 1999 10 15 CALA9901343 1 19991008 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 207 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 E AND E BAY CEILING STA 207 LBL 6 CORROSION ON FLOOR. FABRICATED REPAIR FROM 7075-T6 .020. TREATED, PRIMED, INSTALLED PER SRM 53-01 AND 53-10-3. 2 L 7 2 4F A6WE 1999101500319 19991015 00319 WP 1999 10 15 CALA9901344 1 19991008 A 5340 J0602283 PAN DOUG DC9 DC982 3022082 WP FS370-427 LONG28 CORRODED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 16802 49222 FORWARD CARGO DOOR LOWER JAMB SUPPORT HAS CORROSION FS 370 - 427 STR 28 O/B SIDE. CUT OUT DAMAGED AREA FABRICATED SPLIC ES INSTALLED PAN, SPLICES AND SCUFF PLATED PER SRM 53-0151-10-2, 53-05 AND 51-30-5. 2 L 7 2 4F A6WE 1999101500320 19991015 00320 WP 1999 10 15 CALA9901345 1 19991008 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 CUSP WEB HEAVY CORROSION AT LONGERON 18R AND STA 237. CUT OUT DAMAGED AREA. FABRICATED, TREATED, PRIMED, AND INSTALLED DOUBLER PER SRM 53-01, 51-10-04, AND 51-10-03. 2 L 7 2 4F A6WE 1999101500321 19991015 00321 WP 1999 10 15 CALA9901346 1 19991008 A 5320 2929169 SUPPORT DOUG DC9 DC982 3022082 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 FLOOR BOARD SUPPORT ANGLE IS CORRODED STA 180 RBL 8 - 44. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-10-04 AND 51- 30-02. 2 L 7 2 4F A6WE 1999101500322 19991015 00322 WP 1999 10 15 CALA9901347 1 19991008 A 5320 2929169 SUPPORT DOUG DC9 DC982 3022082 WP BS 200-220 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 FLOOR SUPPORT ANGLE IS CORRODED STA 200 - 220 LBL 14. REMOVED OLD ANGLE. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F A6WE 1999101500323 19991015 00323 NM 1999 10 15 CALA9901348 1 19991011 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM ROW 16-20 BISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 511PE 20634 E PATH LIGHT OUT BETWEEN SEAT ROWS 16 - 20. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999101500324 19991015 00324 NM 1999 10 15 CALA9901349 1 19991010 A 3350 6104781 BATTERY PACK BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 511PE 20634 LEFT OVERWING EXIT LIGHT OUT. REMOVED BATTERY, CLEANED TERMINALS , CHARGED AND REINSTALLED BATTERY PER MM 33-50-00. 2 L 7 3 4F A3WE 1999101500325 19991015 00325 NM 1999 10 15 CALA9901350 1 19991010 A 3350 6104781 BATTERY BOEING 727 727232 1384082 NM L1 DOORWAY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 511PE 20634 EXIT LIGHT AT L1 DOOR IS OUT. REMOVED BATTERY. CLEANED TERMINALS, CHARGED AND REINSTALLED BATTERY PACK PER MM 33-50-00 . 2 L 7 3 4F A3WE 1999101500326 19991015 00326 NM 1999 10 15 CALA9901351 1 19991010 A 3350 610478 BATTERY BOEING 727 727232 1384082 NM R1 DOORWAY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 511PE 20634 EXIT LIGHT AT R1 DOOR IS OUT. REMOVED BATTERY PACK. CLEANED TERMINALS, CHARGED BATTERY, AND REINSTALLED BATTERY PER MM 33-50-00. 2 L 7 3 4F A3WE 1999101500327 19991015 00327 WP 1999 10 15 CALA9901352 1 19991010 A 5315 S292916912000 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59083 47926 FLOOR BEAM J SECTION CORRODED AT ST 1887 AT 39L TO 58 L. REMOVED CORROSION AND INSTALLED NEW SECTION PER SRM 51-21-00 A ND GMM 10-900-01. 2 L 7 3 4F A22WE 1999101500328 19991015 00328 WP 1999 10 15 CALA9901353 1 19991010 A 5315 S2929169 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59083 47926 FLOORBEAM J SECTION CORRODED AT ST 1887 AT 60R - 90R. REMOVED CORROSION. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01. 2 L 7 3 4F A22WE 1999101500329 19991015 00329 WP 1999 10 15 CALA9901354 1 19991010 A 5315 S292916912000 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59083 47926 FLOORBEAM J SECTION AT STA 1887 AT 60L - 90L CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01. 2 L 7 3 4F A22WE 1999101500330 19991015 00330 WP 1999 10 15 CALA9901355 1 19991010 A 5315 S292916912000 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59083 47926 FLOORBEAM J SECTION AT STN 1887 AT 27R - 33R CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01. 2 L 7 3 4F A22WE 1999101500331 19991015 00331 NM 1999 10 15 CALA9901356 1 19991011 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 511PE 20634 E PATH LIGHTING OUT IN FIRST CLASS SECTION. REMOVED, CHARGED, AND REINSTALLED E PATH BATTERY PACK PER MM 33-51-02. 2 L 7 3 4F A3WE 1999101500332 19991015 00332 WP 1999 10 15 CALA9901357 1 19991007 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 FLOORBOARD SUPPORT ANGLE IS CORRODED AT STA 160 RBL 10 - 44. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-30-02. 2 L 7 2 4F A6WE 1999101500333 19991015 00333 WP 1999 10 15 CALA9901358 1 19991007 A 5230 59101412 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 MID CARGO DOOR INSIDE FACE HAS SEVERAL AREAS OF SURFACE CORROSION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER SRM 52- 01 AND 53-30-3. 2 L 7 2 4F A6WE 1999101500334 19991015 00334 WP 1999 10 15 CALA9901359 1 19991007 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 WEB CORRODED AT FS 1338 UNDER L ANGLE AT RBL 56. REMOVED DAMAGED WEB AREA. FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR DOUBLER PER SRM 51-10-3, 53-01, AND 51-30-02. 2 L 7 2 4F A6WE 1999101500335 19991015 00335 WP 1999 10 15 CALA9901360 1 19991007 A 5754 SKIN DOUG DC9 DC982 3022082 WP LE LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 LEFT WING NUMBER 0 SLAT LOWER SURFACE IN CENTER AREA HAS A 3 CRACK IN SKIN NEAR TRAILING EDGE OF SLAT. FABRICATED AND I NSTALLED REPAIR DOUBLER PER SRM 57-01 AND MM 51-00-00. 2 L 7 2 4F A6WE 1999101500336 19991015 00336 WP 1999 10 15 CALA9901361 1 19991008 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 562 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19072 46576 LEFT WING LEADING EDGE INTERNAL SKIN CRACKED (4) AT STA XORS562. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-00 AND DWG ARB 3954. 2 L 7 3 4F A22WE 1999101500337 19991015 00337 WP 1999 10 15 CALA9901362 1 19991008 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19072 46576 RIGHT WING OUTBOARD FLAP OUTBOARD FAIRING RIGHT SIDE ANGLE IS CRACKED (0.5). REPLACED ANGLE PER SRM 51-33-01. 2 L 7 3 4F A22WE 1999101500338 19991015 00338 WP 1999 10 15 CALA9901363 1 19991008 A 5400 SUPPORT DOUG DC10 DC1030 3023501 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19072 46576 PYLON NUMBER ONE SUPPORT PANELS 437DR/437ML CRACKED (0.5). REPLACED SUPPORT PER SRM 51-31-01. 2 L 7 3 4F A22WE 1999101500339 19991015 00339 NM 1999 10 15 CALA9901364 1 19991008 A 3350 20131A BATTERY RADIANT BOEING 737 7373T0 1384582 NM BS 960 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14335 23573 L2 EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED BATERY PACK PER WD 33-51-21. 2 L 7 2 4F RT A16WE 1999101500340 19991015 00340 WP 1999 10 15 CALA9901365 1 19991008 A 5320 2929169 SUPPORT DOUG DC9 DC982 3022082 WP BS 150-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 FORWARD ENTRY DOOR FLOOR PANEL SUPPORT ANGLE IS CORRODED AT LBL 56 STA 150 - 200. REMOVED FLOOR SUPPORT. FABRICATED AN D INSTALLED NEW SUPPORT PER SRM 51-10-03, 53-01, 51-10-04, 53-5, 51-30-02, AND 51-30-05. 2 L 7 2 4F A6WE 1999101500341 19991015 00341 NM 1999 10 15 9904146614 1 19990822 A 5711 SPAR BOEING 747 747251B 1384892 NM WS 1390 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614US 20359 DURING L CHECK, FOUND CORROSION ON LEFT WING FRONT SPAR LOWER CHORD TO PLANK AT WS 1390. REPAIRED PER EA 66-169480. 2 L 7 4 4F A20WE 1999101500342 19991015 00342 NM 1999 10 15 9904156636 1 19990823 A 5711 SPAR BOEING 747 747251B 1384892 NM RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 636US 23547 DURING M CHECK, FOUND CRACK AT FASTENER HOLES 127 AND 129 ON RIGHT WING MID SPAR. REPAIRED PER EA 66-168597. 2 L 7 4 4F A20WE 1999101500343 19991015 00343 NM 1999 10 15 9904166636 1 19990909 A 5320 SIDEWALL BOEING 747 747251B 1384892 NM BS 1739 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 636US 23547 DURING M CHECK, FOUND CRACK AT FASTENER HOLE FS 1739, RIGHT SIDEWALL. REPAIRED PER EA 66-170395. 2 L 7 4 4F A20WE 1999101500344 19991015 00344 NM 1999 10 15 9904172715 1 19990813 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM BS 1050 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 719RC 22490 DURING M CHECK, FOUND CORROSION ON THE UPPER FLANGE OF THE FS 1050 FLOORBEAM BETWEEN LBL 2 AND THE ENF OF THE BEAM ON TH E LEFT SIDE. REPAIRED PER EA 27-167983. 2 L 7 3 4F A3WE 1999101500345 19991015 00345 NM 1999 10 15 9904182715 1 19990813 A 5314 KEEL BEAM BOEING 727 7272S7 138407Z NM BS 950-980 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 719RC 22490 DURING M CHECK, FOUND CORROSION ON THE LOWER OUTBOARD FLANGE OF THE LEFT KEEL BEAM FS 950 - 980. REPAIRED PER E A 27-16 7920 MFG PART NUMBER 65-56441-5. 2 L 7 3 4F A3WE 1999101500346 19991015 00346 WP 1999 10 15 9904191162 1 19990913 A 5320 JAMB DOUG DC10 DC1040 3023508 WP BS 1701-1708 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING M CHECK, FOUND CORROSION ON CENTER CARGO DOOR JAMB RAIL AND FRAME OUTER CAP BETWEEN FS 1701 - 1708. REPAIRED PER EA 11-170067. 2 L 7 3 4F A22WE 1999101500347 19991015 00347 WP 1999 10 15 9904201162 1 19990901 A 5315 BEAM DOUG DC10 DC1040 3023508 WP FUS 879 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING M CHECK, FOUND CRACK ON FLOORBEAM AT FS 879, RBL 30. REPAIRED PER EA 11-167477. 2 L 7 3 4F A22WE 1999101500348 19991015 00348 WP 1999 10 15 9904211162 1 19990902 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 420 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING M CHECK, FOUND CRACK ON NR 1 RIGHT DOOR FITTING AT FS 420, LONGERON 27R. REPAIRED PER EA 11-170063. 2 L 7 3 4F A22WE 1999101500349 19991015 00349 1999 10 15 COMA9910161 4 19991007 A 3425 EFIS EMB 120 EMB120RT SO RT COCKPIT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 259CA 1252 THE CO-PILOTS TOP EFIS TUBE WENT BLANK DURING TAKEOFF, AIRCRAFT RETURNED TO THE GATE. RESET THE CO-PILOTS AHRS SYSTEM. 2 L 7 2 4T RT A31SO 1999101500350 19991015 00350 EA 1999 10 15 COMA9960578 1 19991007 A 5320 601R3114810 SILL CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 THE FLOOR SILL AFT OF THE SERVICE DOOR IS CORRODED. PERFORMED A MAJOR REPAIR, REMOVED THE DAMAGED SILL AND FABRICATED A ND INSTALLED A NEW SILL AND INSTALLED IAW WVAC EO NO 601R-53-0411. 2 L 7 2 4F RT A21EA 1999101500351 19991015 00351 EA 1999 10 15 COMA9960579 1 19991007 A 5320 601R3111383 INTERCOSTAL CNDAIR CL600 CL6002B19 EA BS 310 & 319 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 OUTBOARD SIDE OF WEB AT RBL 9 BETWEEN FS 310 AND FS 319 HAS A DENT AND CRACK. PERFORMED A MAJOR REPAIR REMOVED A DAMAGE D INTERCOSTAL FOR THE SEAT RAIL AT RBL 9.0 BETWEEN FS 310 AND 319 IAW WVAC EO NR 601R-53-040-4. 2 L 7 2 4F RT A21EA 1999101500352 19991015 00352 EA 1999 10 15 COMA9960580 1 19991007 A 5320 601R31527797 ANGLE CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 UPON REMOVAL OF PAX DOOR ANGLE, FOUND AFT FLOOR BOARDS SUPPORT ANGLE CORRODED AT F/S 349 P/N 601R31527-797. PERFORMED A MAJOR REPAIR REMOVED THE CORRODED THRESHOLD ANGLE CLIPS FABRICATED AND INSTALLED NEW CLIPS IAW WVAC EO NR 601R-53-0405. 2 L 7 2 4F RT A21EA 1999101500353 19991015 00353 EA 1999 10 15 COMA9960581 1 19991009 A 5320 6003603031 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 7756 7141 FS 718.00 AT STR 11 LT AND RT SIDES HAVE CRACKED DOUBLERS. REMOVED CRACKED DOUBLERS AT FS 718.00 AT STR 11 BOTH LT AND RT REPLACED DOUBLERS WITH NEW DOUBLERS IAW WVAC EO 601R-53-0422. 2 L 7 2 4F RT A21EA 1999101500354 19991015 00354 EA 1999 10 15 COMA9960582 1 19991010 A 5320 601R3111334 INTERCOSTAL CNDAIR CL600 CL6002B19 EA BS 310-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 OUTBOARD SIDE OF INTERCOSTAL WEB AT RBL 9 BETWEEN FS 310 AND FS 319 WAS DAMAGED BY RIVET GUN. PERFORMED MAJOR REPAIR TO INTERCOSTAL WEB AT RBL 9 BETWEEN FS 310 AND FS 319 IAW WVAC EO 601R-53-0404A. 2 L 7 2 4F RT A21EA 1999101500355 19991015 00355 EA 1999 10 15 COMA9960583 1 19991010 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA BS 310-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 PAX DOOR FLOOR SUPPORT ANGLE CORRODED BEYOND LIMITS, P/N 601R31527-181, PERFORMED MAJOR REPAIR BY REMOVING CORRODED ANGL E AND INSTALLING NEW ANGLE, P/N 601R31527-181, IAW WVAC EO 601R-53-0392A. 2 L 7 2 4F RT A21EA 1999101500356 19991015 00356 EA 1999 10 15 COMA9960584 1 19991009 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA BS 310-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13573 7038 PAX DOOR THRESHOLD ANGLES, P/N 601R31527-181 AND P/N ARE SEVERELY CORRODED. PERFORMED MAJOR REPAIR BY REPLACING PAX DOO R THRESHOLD ANGLES IAW WVAC EO'S 601R-53-0424 AND 601R-53-0425. 2 L 7 2 4F RT A21EA 1999101500357 19991015 00357 EA 1999 10 15 COMA9960585 1 19991005 A 5320 601R3830310 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 SERVICE DOOR FLOOR SUPPORT L ANGLE CORRODED BEYOND LIMITS P/N 601R383-105. PERFORMED A MAJOR REPAIR, REMOVED AND INSTAL LED 9 NEW THRESHOLD ANGLE (P/N 601R38303-239) IAW WVAC EO 601R-53-0391A. 2 L 7 2 4F RT A21EA 1999101500358 19991015 00358 EA 1999 10 15 COMA9960586 1 19991007 A 5320 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA BS 310-319 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 DOUBLER PLATE BETWEEN FS 310 AND 319 RIGHT SIDE AT RBL 4Z IS CORRODED, P/N 601R38669-49. PERFORMED A MAJOR REPAIR REMOV ED AND INSTALLED A NEW DOUBLER PLATE P/N 601R38669-49 IAW WVAC EO 601R-53-0407. 2 L 7 2 4F RT A21EA 1999101500359 19991015 00359 EA 1999 10 15 COMA9960587 1 19991010 A 5320 601R383253 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 SERVICE DOOR THRESHOLD ANGLE, P/N 601R38303-253 IS SEVERELY CORRODED. PERFORMED A MAJOR REPAIR IN REMOVING CORRODED ANG LE AND INSTALLING NEW ANGLE FABRICATED FROM EXTRUSION SD0325068-081 IAW WVAC EO 601R-53-0406A. 2 L 7 2 4F RT A21EA 1999101500360 19991015 00360 EA 1999 10 15 COMA9960588 1 19991007 A 5320 601R383253 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 THRESHOLD ANGLE, P/N 601R38303-253 AT THE SERVICE DOOR ENTRANCE IS SEVERELY CORRODED. PERFORMED A MAJOR REPAIR REMOVED A DAMAGED ANGLE P/N 601R38303-253 AND FABRICATED AND INSTALLED A NEW ANGLE IAW WVAC 601R-53-0406. 2 L 7 2 4F RT A21EA 1999101500361 19991015 00361 EA 1999 10 15 COMA9960589 1 19991010 A 5330 601R10045 PLANK CNDAIR CL600 CL6002B19 EA WS 136.676 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 7048 2 CRACKS DETECTED IN THE LOWER HORIZONTAL SURFACE OF LEFT LOWER WING ACCESS HOLE AT PANEL 540FB. BLENDED OUT DAMAGED AR EA ROTO PEENED AND ALODINED IAW BOMBARDIER REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999101500362 19991015 00362 EA 1999 10 15 COMA9960590 1 19991009 A 5320 STIFFENER CNDAIR CL600 CL6002B19 EA BS 280 DRILLED THROUG A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 WHILE REMOVING CRACK AT FS 280.00/RBL 9 OUTBOARD SIDE THE VERTICAL WAS DRILLED THROUGH. REPAIRED VERTICAL STIFFENER AT FS 280.00 OUTBOARD OF RBL9 IAW WVAC EO 601R-53-0349A. 2 L 7 2 4F RT A21EA 1999101500363 19991015 00363 EA 1999 10 15 COMA9960591 1 19991005 A 5330 3867317 PLATE CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 ALL TOP PLATES AT FS 349 ARE CORRODED P/N 601R38673-17, 601R38673-19, 601R38673-21 AND 601R38673-25. PERFORMED A MAJOR REPAIR REMOVED THE CORRODED PLATES AT FS 349 FABRICATED AND INSTALLED NEW PLATES USING 7075-T6 ALUMINUM IAW WVAC EO 6015 3-0393A. 2 L 7 2 4F RT A21EA 1999101500364 19991015 00364 EA 1999 10 15 COMA9960592 1 19991010 A 2820 601A62002 FITTING 6006278110 CNDAIR CL600 CL6002B19 EA RT FUEL SYS DEFECTIVE A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 936CA 30399 235 7043 DURING COLLECTOR TANK CHECK VALVE FUNCTIONAL TEST, THE RIGHT CHECK VALVE WAS FOUND TO BE LEAKING. DURING INVESTIGATION, THE CHECK VALVE FITTING WAS FOUND TO HAVE A MANUFACTURING DEFECT, NOT ALLOWING THE CHECK VALVE TO SEAT PROPERLY. THE F ITTINGS CHECK VALVE MATING SURFACE HAS A RISE, WITH A SMALL CRACK NEXT TO IT. THE CHECK VALVE FITTING WAS REPLACED. 2 L 7 2 4F RT A21EA 1999101500365 19991015 00365 WP 1999 10 15 UPS99830870 1 19990908 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 8-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:SV STA 8 TO 70 FINGER DOUBLER RT SIDE HAS CORROSION. REMOVED AND REPLACED FINGER DOUBLER IAW DC8 SRM 51 -1-21, 53-3-1. 2 L 7 4 4F RT 4A25 1999101500366 19991015 00366 EU 1999 10 15 QXEA9902011 1 19991006 A 3350 6008905 BATTERY GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 1848 11228 BOI - BACK THREE EVACUATION CEILING LIGHTS INOPERABLE. INSTALLED NEW BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999101500367 19991015 00367 EU 1999 10 15 QXEA9902047 1 19991006 A 3350 LIGHT GRIMES 5515900004 FOKKER F28 F28MK4000 4990810 EU ROW 8 INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 GEG - ROW 8 AISLE EMERGENCY SIGN, SOME LIGHTS INOPERATIVE. REPLACED LAMP BOARD. CHECKS GOOD ALL MODES. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1999101500368 19991015 00368 NM 1999 10 15 QXEA9902053 1 19991007 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 831PH 328 SEA - FORWARD FOUR RED CENTER AISLE EMERGENCY LIGHTS INOPERATIVE. CONNECTED FORWARD FOUR RED EGRESS LIGHTS CONNECTOR TO POWER SUPPLY CONNECTOR UNDER FLOOR BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999101500369 19991015 00369 NM 1999 10 15 99FDEA00416 1 19991008 A 3260 CONNECTOR BOEING 727 72722 1384002 NM LT MLG DIRTY A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 185FE 18871 99-247 - LEFT MAIN GEAR NOT DOWN AND LOCKED WITH HANDLE DOWN. NEGATIVE G PER RED TABS LOCK DOWN GEAR. CLEANED CANNON P LUG ON DOWN LOCK SWITCH LEFT GEAR. OPER CK GOOD PER GENERAL MM. 2 L 7 3 4F A3WE 1999101500370 19991015 00370 NM 1999 10 15 99FDEA00417 1 19991008 A 3260 SWITCH BOEING 727 72722 1384002 NM LT MLG MALFUNCTION A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 185FE 18871 99-248 REPEAT, LEFT MAIN GEAR IND GREEN LIGHT MALFUNCTION. SUSPECT DOWN LOCK SWITCH. REPLACED DOWNLOCK SWITCH PER 727 MM 32-61-021-4. PERF ADJUST AND TEST PER MM 32-61-021-5, OPER CK GOOD. OK FOR SERV. 2 L 7 3 4F A3WE 1999101500371 19991015 00371 WP 1999 10 15 99FDEA00418 1 19991006 A 5400 HARDWARE DOUG DC10 DC1030F 3023504 WP NR 1 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 12 OFF MOUNTING BOLTS LOOSE AND 3 OFF NUTS MISSING FROM SHEAR WEB FORGINGS ON AFT NR 1 PYLON FRAME, ADJACENT TO SPHERICA L BEARING FITTING. REMOVED AND REPLACED PER MM 70-00-00-2. 2 L 7 3 4F RT A22WE 1999101500372 19991015 00372 NM 1999 10 15 99FDEA00419 1 19991009 A 3230 CONNECTOR BOEING 727 727247 138408F NM LANDING GEAR CONTAMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 233FE 21327 ON GEAR RETRACTION ALL IND NORM WITH GEAR HANDLE UP POSITION. WHEN GEAR HANDLE OFF, DOOR IND UNSAFE WITH RED DOOR LIGHT S. ACCOMPLISHED RED TAB PROC, LIGHT EXTINGUISHED WHEN GEAR HANDLE WAS IN UP POS. *S/D* REMOVED CANNON PLUG TO SWITCH, REMOVED FOREIGN OBJECT (GROMMET) AND RECONNECTED CANNON PLUG PER MM 32-62-011-5. 2 L 7 3 4F A3WE 1999101500373 19991015 00373 WP 1999 10 15 ABXA9900729 1 19990927 A 5320 99578835 INTERCOSTAL DOUG DOUG DC9 DC932 3022066 WP BS 200-207 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND INTERCOSTAL CRACKED BETWEEN STATION 200 AND 207 AT LONGERON 11 RIGHT. REPAIRED INTERCOSTAL IAW D C9 SRM DWG 05159. 2 L 7 2 4F A6WE 1999101500374 19991015 00374 WP 1999 10 15 ABXA9900730 1 19990929 A 5711 5597831 SPAR DOUG DOUG DC8 DC863 302198A WP WS 207-255 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 RIGHT WING FORWARD SPAR HAD CORROSION DAMAGE FROM XFS 207 TO 255. REPAIRED IAW ABX REA D857-32981MR. 2 L 7 4 4F 4A25 1999101500375 19991015 00375 WP 1999 10 15 ABXA9900731 1 19990927 A 5230 591014167 PAN DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED AT NR 5 BEAM AT THE FORWARD UPPER CORNER AND THE FORWARD LOWE R CORNER. REPAIRED DOOR PAN IAW DC9 SRM 52-03. 2 L 7 2 4F A6WE 1999101500376 19991015 00376 WP 1999 10 15 ABXA9900732 1 19990927 A 5320 39123721 SPLICE DOUG DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND FLOORBEAM TO FRAME SPLICE PLATE CRACKED STATION 718 LEFT SIDE. REPLACE SPLICE PLATE IAW DC9 SRM. 2 L 7 2 4F A6WE 1999101500377 19991015 00377 WP 1999 10 15 ABXA9900733 1 19990901 A 5753 5701110502 VANE DOUG DOUG DC8 DC863 302198A WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 DURING C-CHECK, FOUND RIGHT FLAP VANE DELAMINATED APPROXIMATELY 40 PERCENT. REPAIRED UNIT COMPLETE. 2 L 7 4 4F 4A25 1999101500378 19991015 00378 WP 1999 10 15 MWEA99666 1 19991004 A 5220 9915565137 DOOR DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 AFT VENTRAL DOOR HAS CRACK IN THE RADIOUS, RIGHT SIDE JUST ABOVE THE FIRST OFFICERS SEAT. MAINTENANCE FABRICATED AND IN STALLED REPAIR PARTS. 2 L 7 2 4F A6WE 1999101500379 19991015 00379 WP 1999 10 15 MWEA99667 1 19991008 A 3350 L00865 BATTERY PACK DOUG DC9 DC932 3022066 WP ROW 1-6 DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FLOOR TRACK LIGHTING INOPERATIVE ROWS 1 THROUGH 6. REPLACED FLOOR TRACK BATTERY PACK. 2 L 7 2 4F A6WE 1999101500380 19991015 00380 WP 1999 10 15 MWEA99668 1 19991007 A 2560 100502121 COVER DOUG DC9 DC981 3022081 WP GALLEY SLIDE LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 803ME 48029 THE COVER ON THE AFT GALLEY DOOR SLIDE IS LOOSE. RESUECURED SLIDE COVER. 2 L 7 2 4F A6WE 1999101500381 19991015 00381 NM 1999 10 15 SCNA99735 1 19990915 A 5313 STRINGER BOEING 727 7272J4 1384006 NM BS 294 29 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS IN EQUIPMENT AND ELECTRICAL BAY DOG HOUSE AREA, STR 24 , AT BS 294. REMOVED CORROSION PER SRM 511006. FABRICATED CHANNEL REPAIR FORM BAC 498131 IAW B727 SRM 531003 FIGURE 2. TREATED AND PRIMED IAW B727 SRM 512002 MM 511002. INSTALLED IAW B727 SRM 513002 AND 531003 FIGURE 2. 2 L 7 3 4F RT A3WE 1999101500382 19991015 00382 NM 1999 10 15 SCNA99736 1 19990915 A 5312 BULKHEAD BOEING 727 7272J4 1384006 NM BS 870 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS IN LT WHEEL WELL FORWARD BULKHEAD AT BS 870, LBL 56 ST IFFENER CORRODED NUMEROUS PLACES FROM TOP TO BOTTOM. CLEANED CORROSION IAW B727 SRM 511006 AND 531001 FIGURE 1. FABRIC ATED FILLER IAW B727 SRM 511004 AND DOUBLER IAW B727 SRM 511004. TREATED AND PRIMED IAW B727 MM 512002 SRM 511002. INS TALLED IAW B727 SRM 513002 AND 514004 FIGURE 1. 2 L 7 3 4F RT A3WE 1999101500383 19991015 00383 NM 1999 10 15 SCNA99737 1 19990926 A 5320 INTERCOASTAL BOEING 727 7272J4 1384006 NM BS 330-400 ELONGATED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK STATION 330 TO 400 RBL 7 APPROXIMATELY, INTERCOSTAL HAS ELONGATED HOLES AT FLOORBEAM ATTA CH ANGLE. REMOVED INTERCOASTAL IAW B727 SRM 513002. FABRRICATED DOUBLER REPAIR FORM 2024 T3 .050 IAW B727 SRM 514002 M ATERIAL ID PER SRM 531002. TREATED AND PRIMED IAW B727 SRM 512002 MM 511002. INSTALLED IAW B727 SRM 513002 AND 514002. 2 L 7 3 4F RT A3WE 1999101500384 19991015 00384 NM 1999 10 15 SCNA99738 1 19991007 A 3350 LIGHT BOEING 727 7272J4 1384006 NM ROW 32D INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, RED FLOOR TRACK LIGHT INOPERATIVE AT AT SEAT 32D AREA. REPAIRED IAW B277 MM 335101. 2 L 7 3 4F RT A3WE 1999101500385 19991015 00385 NM 1999 10 15 SCNA99739 1 19991007 A 3350 BULB BOEING 727 7272J4 1384006 NM AIR STAIRS FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE CHECK, CEILING EMERGENCY LIGHT INOP IN TAIL STAIR COMPARTMENT. REMOVED AND REPLACED LIGHT BULB S IN EMERGENCY LIGHT IAW B727 MM 331001 PAGE 401. 2 L 7 3 4F RT A3WE 1999101500386 19991015 00386 WP 1999 10 15 DHL9980601C 1 19990823 A 5752 SKIN DOUG DC8 DC873F 302199F WP RT AILERON TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RT WING AIL CONTROL TAB DELAMINATED. REMOVED AND REPLACED CONTROL TAB PER DC8 MM 27-11-4 PG 201. NR CARD N R 0047 2 L 7 4 4F RT 4A25 1999101500387 19991015 00387 WP 1999 10 15 DHL9980602C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 670 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING LOWER T/E PANEL APPROX STA 670 DELAMINATED. REMOVED AND REPLACED PANEL IAW DC8 SRM 51-3-0, N/R CARD NR 0048. 2 L 7 4 4F RT 4A25 1999101500388 19991015 00388 WP 1999 10 15 DHL9980603C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING LOWER T/E AILERON POWER PACK PANEL IS DELAMINATED. REMOVED DELAMINATED PANEL AT RT WING LOWER SU RFACE T/E POWER PACK ACCESS IAW DC8 SRM 51-3-0 PG 2 FIG 52A. INSTALLED REPAIRED PANEL IAW DC8 SRM 51-3-0 PG 1. NR CARD NR 0049. 2 L 7 4 4F RT 4A25 1999101500389 19991015 00389 WP 1999 10 15 DHL9980604C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 589-624 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT WING UPPER SIDE T/E PANEL DELAMINATED LOCATED AT IB AILERON AREA BETWEEN XW 589 TO XW 624. REMOVED DELAM INATED PANEL FROM XW 589 TO XW 624. INSTALLED OVERHAULED PANEL IAW DC8 SRM 51-1-15 PG 1. NR CARD NR 0052. 2 L 7 4 4F RT 4A25 1999101500390 19991015 00390 WP 1999 10 15 DHL9980605C 1 19990823 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 2 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING FLIGHT SPOILER NR 2 IS DELAMINATED REMOVED AND REPLACED FLIGHT SPOILER PANEL NR 2 IAW DC8 MM 27-6 0-1 PG 201. PERFORMED ADJUSTMENT AND OPS CK IAW DC8 MM 27-60 PG 501, NR CARD NR 0053. 2 L 7 4 4F RT 4A25 1999101500391 19991015 00391 WP 1999 10 15 DHL9980606C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 624 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING UPPER TRAILING EDGE PANEL AT STA XRS 624 IS DELAMINATED. REMOVED DELAMINATED PANEL AT RT WING UP PER SURFACE TE STA XRS 624 IAW DC8 SRM 51-3-0 PG 2 FIG 52A. INSTALLED SERVICEABLE PANEL PER DC8 SRM 51-3-0 PG 2 52A NR CARD NR 0057 2 L 7 4 4F RT 4A25 1999101500392 19991015 00392 WP 1999 10 15 DHL9980607C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 5-47 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT WING UPPER SURFACE PANEL DELAMINATED LOCATED BETWEEN STA XW 5.000 TO XW 47.000. INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-9, PG 3, AND SRM 51-3-0, PAR 1 AND 2. N/R CARD NR 0058. 2 L 7 4 4F RT 4A25 1999101500393 19991015 00393 WP 1999 10 15 DHL9980608C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING O/B AILERON WEIGHTS ACCESS PANEL SHOWS DELAMINATION. REMOVED AND REPLACED PANEL IAW DC8 SRM 51-3-0, PG 1. N/R CARD NR 0059. 2 L 7 4 4F RT 4A25 1999101500394 19991015 00394 WP 1999 10 15 DHL9980609C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 98-162 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING I/B T/E PANEL BETWEEN STA XW 98 TO XW 162 SHOWS DELAMINATION. REMOVED AND REPLACED PANEL IAW DC8 SR M 51-3-0 AND 51-1-21, PAR 1. N/R CARD NR 0062. 2 L 7 4 4F RT 4A25 1999101500395 19991015 00395 WP 1999 10 15 DHL9980610C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 5-98 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING I/B T/E PANEL LOCATED BETWEEN XW STA 5.000 TO STA 98 SHOWS SEVERAL DENTS. REMOVED AND REPLACED PANE L IAW DC8 SRM 51-30-0 PAR 1 AND 2 FIG 52A AND 52B. N/R CARD NR 0063. 2 L 7 4 4F RT 4A25 1999101500396 19991015 00396 WP 1999 10 15 DHL9980611C 1 19990824 A 5320 FITTING DOUG DC8 DC873F 302199F WP LT MLG W/W CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT MLG W/W TRAPEZOIDAL FITTING SHOWS CRACKED AT WEB SIDE. REPAIRED PER CONDITION 4 OF S/B 53/61. INSTALLED NEW SPLICE FITTINGS PER S/B 53-61 FIG 3 STEPS 1 THROUGH 26. N/R CARD NR 0115. 2 L 7 4 4F RT 4A25 1999101500397 19991015 00397 WP 1999 10 15 DHL9980612C 1 19990825 A 5330 SKIN DOUG DC8 DC873F 302199F WP LT MLG WW DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT MLG W/W CUT OUT REAR SIDE T/E PANEL FRAME SHOWS DAMAGED AREA. REMOVED DAMAGED SECTION, FABRICATED NEW SE CTION IAW SRM 51-1-4 PAR 4. INSTALLED IAW SRM 51-1-20D PAR 7 AND SRM 51-1-21 PAR 1 FIG 32. N/R CARD NR 0180. 2 L 7 4 4F RT 4A25 1999101500398 19991015 00398 WP 1999 10 15 DHL9980613C 1 19990916 A 5280 SKIN DOUG DC8 DC873F 302199F WP RT MLG DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT MLG I/B DOOR LOWER SIDE FWD CORNER SHOWS DAMAGED AREA. BLENDED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW DER 99090201. N/R CARD NR 0244. 2 L 7 4 4F RT 4A25 1999101500399 19991015 00399 WP 1999 10 15 DHL9980614C 1 19990826 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LWR EXTERIOR FUSELAGE SKIN BULGING AT STA 1360, BETWEEN LONGERON 33L TO 33R. CUT OUT DAMAGED AREA AND INSTA LLED DOUBLER IAW E/O NR 99090202. N/R CARD NR 0270. 2 L 7 4 4F RT 4A25 1999101500400 19991015 00400 WP 1999 10 15 DHL9980615C 1 19990826 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 20-80 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LOWER EXTERIOR FUSELAGE BETWEEN FS 20 TO 80 AND LONGERON 36 TO 31R SKIN IS BULGING AND AREA AROUND RIVET HEA D CRACKED. CUT OUT DAMAGED AREA OF SKIN, AND INSTALLED DOUBLER IAW E/O NR 99090301. N/R CARD NR 0296. 2 L 7 4 4F RT 4A25 1999101500401 19991015 00401 WP 1999 10 15 DHL9980616C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1306 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 3 SEAT TRACK FS 1400 HAS SURFACE CORROSION AND ELONGATED TRACK HOLES. INSTALLED FOUR HOLE CARGO TRACK RE PAIR IAW DC8 SRM 53-2-3, FIG 6D, SHEET 1-3. N/R CARD NR 0300. 2 L 7 4 4F RT 4A25 1999101500402 19991015 00402 WP 1999 10 15 DHL9980617C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1210 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 4 SEAT TRACK FS 1210 THROUGH 1220 PREVIOUS PLUG REPAIR SHOWS DENTS AND SURFACE CORROSION. REMOVED DAMAGE D REPAIR PLUGS AND INSTALLED NEW 4 HOLE TRACK REPAIR IAW DC8 SRM 53-2-3, FIG 6D, SHEET 1 THROUGH 3. N/R CARD NR 0306. 2 L 7 4 4F RT 4A25 1999101500403 19991015 00403 WP 1999 10 15 DHL9980618C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 789) CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 5 SEAT TRACK FS 789 THROUGH 845 PREVIOUS PLUG REPAIR HAS SURFACE CORROSION AND WORN AREAS. REMOVED DAMAG ED SECTION OF TRACK AND REPAIRED IAW DC8 SRM 4 HOLE REPAIR, SRM 53-2-3 FIG 6D. N/R CARD NR 0315. 2 L 7 4 4F RT 4A25 1999101500404 19991015 00404 WP 1999 10 15 DHL9980619C 1 19990826 A 5320 FITTING DOUG DC8 DC873F 302199F WP RT EMER EXIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RT OVERWING EXIT WINDOW (FWD) UPPER LOCK SUPPORT FITTING CRACKED. REMOVED AND REPLACED LOCK SUPPORT FITTING IAW DC8 SRM 51-3-0, PAR 1 AND 2. OPS CKD IAW DC8 MM 52-21-1. N/R CARD NR 0330. 2 L 7 4 4F RT 4A25 1999101500405 19991015 00405 WP 1999 10 15 DHL9980620C 1 19990829 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT WING L/E INTERIOR CRACK STOP DRILLED ON WEB SECTION MARKED DOT 32-60. FABRICATED DOUBLER IAW DC8 SRM 57- 2-0, INSTALLED DOUBLER IAW DC8 SRM 51-1-21, PG 1. N/R CARD NR 0544. 2 L 7 4 4F RT 4A25 1999101500406 19991015 00406 WP 1999 10 15 DHL9980621C 1 19990829 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, C3 DOOR SHOWS SKIN DAMAGED AT BOTTOM SIDE. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED NEW SECTION IAW DC8 SRM 52-2-0, INSTALLED SKIN SECTION IAW DC8 SRM 52-2-0 FIG 4, SRM 51-1-21, PAR 1 FIG 32. N/R CARD NR0547 2 L 7 4 4F RT 4A25 1999101500407 19991015 00407 WP 1999 10 15 DHL9980622C 1 19990830 A 5755 PANEL DOUG DC8 DC873F 302199F WP NR 1 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 1 RT SPOILER PANEL O/B FITTING IS CRACKED. REMOVED AND REPLACED SPOILER PANEL IAW DC8 MM 27-61-1, PG 201 , OPS CKD IAW DC8 MM 27-60-0, PG 501. N/R CARD NR 0635. 2 L 7 4 4F RT 4A25 1999101500408 19991015 00408 1999 10 15 DHL9980623C 4 19990831 A 3442 BASE DOUG DC8 DC873F 302199F WP RADAR ANTENNA CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RADAR ANTENNA BASE ON BULKHEAD HAS CRACK AROUND HOLE. ROUNDED OUT HOLE, DID NOT REQUIRE REPAIR IAW DC8 SRM 53-2-0, PG 2, FIG 1F. N/R CARD NR 0675. 2 L 7 4 4F RT 4A25 1999101500409 19991015 00409 WP 1999 10 15 DHL9980624C 1 19990831 A 5230 BRACKET DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, AFT CARGO DOOR C4 SHOWS TWO SUPPORT BRACKETS CRACKED UPPER SECTOR OF DOOR. REMOVED AND REPLACED BRACKETS IA W DC8 SRM 51-30-0 PAR 1 AND 2. N/R CARD NR 0679. 2 L 7 4 4F RT 4A25 1999101500410 19991015 00410 WP 1999 10 15 DHL9980625C 1 19990831 A 5720 STRIP DOUG DC8 DC873F 302199F WP WS 50 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT WING UPPER EXTERIOR SURFACE CTR SPAR TRIM ANGLE BROKEN XRS 50. REMOVED DAMAGED STRIP AND FABRICATED NEW METAL STRIP FROM SAME MATERIAL IAW DC8 SRM 51-1-4 PAR 3. INSTALLED STRIP IAW DC8 SRM 51-1-15, PAR 2. N/R CARD NR 0711. 2 L 7 4 4F RT 4A25 1999101500411 19991015 00411 WP 1999 10 15 DHL9980626C 1 19990823 A 5330 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, FUSELAGE LOWER PANEL NR 162Q DELAMINATED. CUT OUT DAMAGED SECTION OF PANEL, FABRICATED DOUBLER IAW DC8 SRM 51-1-9 PG 37. INSTALLED DOUBLER IAW DC8 SRM 51-1-9 PG 37. N/R CARD NR 0068. 2 L 7 4 4F RT 4A25 1999101500412 19991015 00412 WP 1999 10 15 DHL9980627C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 670 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RT WING LOWER T/E PANEL STA XRS 670 IS DELAMINATED. REMOVED AND REPLACED PANEL IAW DC8 SRM 51-3-0, PG 1. N /R CARD NR 0048. 2 L 7 4 4F RT 4A25 1999101500413 19991015 00413 WP 1999 10 15 DHL9980628C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING T/E AILERON POWER PACK PANEL IS DELAMINATED. REMOVED AND REPLACED PANEL IAW DC8 SRM 51-3-0, PG 1 . N/R CARD NR 0049. 2 L 7 4 4F RT 4A25 1999101500414 19991015 00414 WP 1999 10 15 DHL9980629C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 340-410 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING LOWER T/E PANEL BETWEEN STA XW 410 AND 340 IS DELAMINATED. PERFORMED METAL TO METAL BOND REPAIR AT R/WING LOWER T/E PANEL IAW DC8 SRM 51-1-9, PG 3. N/R CARD NR 0050. 2 L 7 4 4F RT 4A25 1999101500415 19991015 00415 WP 1999 10 15 DHL9980630C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 219-340 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING LOWER T/E PANEL BETWEEN STA 340 AND XW 219 IS DELAMINATED. PERFORMED METAL TO METAL BOND REPAIR IAW DC 8 SRM 51-1-9, PG 3. N/R CARD NR 0051. 2 L 7 4 4F RT 4A25 1999101500416 19991015 00416 WP 1999 10 15 DHL9980631C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING STA. 624 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING UPPER T/E PANEL AT STA 624 IS DELAMINATED. REMOVED AND REPLACED PANEL PER DC8 SRM 51-3-0, PG 2, FIG 52A. N/R CARD NR 0057. 2 L 7 4 4F RT 4A25 1999101500417 19991015 00417 WP 1999 10 15 DHL9980632C 1 19990824 A 5522 COVER DOUG DC8 DC873F 302199F WP LT ELEV CRACKED. A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT ELEVATOR UPPER SURFACE CONTROL ROD COVER PANEL CRACKED. CUT OUT DAMAGED AREA ON COVER, FABRICATED DOUBLE R IAW DC8 SRM 55-2-0 FIG 4. INSTALLED DOUBLER IAW DC8 SRM 51-1-21, PAR 1, FIG 32. N/R CARD NR 0120. 2 L 7 4 4F RT 4A25 1999101500418 19991015 00418 WP 1999 10 15 DHL9980633C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 860 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 2 SEAT TRACK FS STA 860 THROUGH 879 TRACK WORN AND SURFACE CORROSION. CUT OUT DAMAGED SECTION OF TRACK. INSTALLED FOUR HOLE CARGO TRACK REPAIR IAW DC8 SRM 53-2-3, FIG 6D, SHEET 1 THROUGH 3. N/R CARD NR 0264. 2 L 7 4 4F RT 4A25 1999101500419 19991015 00419 WP 1999 10 15 DHL9980634C 1 19990826 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1260 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LWR EXT FUSELAGE FOUND SKIN BULGING AT FS STA 1260 LONGERON 33L. CUT OUT DAMAGED SECTION OF SKIN, FABRICATE D DOUBLER AND INSTALLED SAME IAW EO NR 99090203. N/R CARD NR 0272. 2 L 7 4 4F RT 4A25 1999101500420 19991015 00420 WP 1999 10 15 DHL9980635C 1 19990829 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 291 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT WING L/E LOWER SURFACE CRACK AT RIVET HOLE MARKED DOT 32-59 XFS 291. FABRICATED AND INSTALLED REPAIR DOU BLER IAW E/O NR 99090302 N/R CARD NR 0545. 2 L 7 4 4F RT 4A25 1999101500421 19991015 00421 WP 1999 10 15 DHL9980636C 1 19990901 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1160 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, C3 CARGO COMPT FLOOR FROM STA 1140-1160 CENTER HAS CRACK AROUND GOUGE ON LWR SIDE. TRIMMED CRACKED AREA OF FLOOR BOARD, FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. INSTALLED DOUBLER IAW DC8 SRM 51-1-21, PG 1. N/R CAR D NR 0810. 2 L 7 4 4F RT 4A25 1999101500422 19991015 00422 WP 1999 10 15 DHL9980637C 1 19990823 A 5753 VANE DOUG DC8 DC873F 302199F WP RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING FLAP VANE BETWEEN STA XW 0 AND XW 98 IS DELAMINATED. REMOVED AND REPLACED FLAP VANE IAW DC8 MM 2 7-51-14, PG 201. N/R CARD NR 0054. 2 L 7 4 4F RT 4A25 1999101500423 19991015 00423 WP 1999 10 15 DHL9980638C 1 19990823 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT WING T/E PANEL DELAMINATED, LOCATED AT NR 5 SPOILER AREA. PERFORMED METAL TO METAL BOND REPAIR IAW DC8 S RM 51-1-9, PG 3, N/R CARD NR 0055. 2 L 7 4 4F RT 4A25 1999101500424 19991015 00424 WP 1999 10 15 DHL9980639C 1 19990823 A 5753 VANE DOUG DC8 DC873F 302199F WP RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RIGHT WING FLAP VANE BETWEEN XW 340 AND XW 219 IS DELAMINATED. REMOVED AND REPLACED FLAP VANE NR 4 TO RT WI NG IAW DC8 MM 27-50-0, PG 201 AND 27-51-14, PG 201. PERFORMED OPS CK ON FLAP VANE IAW DC8 MM 27-50-0 PG 201, N/R CARD N R 0056. 2 L 7 4 4F RT 4A25 1999101500425 19991015 00425 WP 1999 10 15 DHL9980640C 1 19990823 A 5753 VANE DOUG DC8 DC873F 302199F WP LT TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT WING NR 6 FLAP VANE SHOWS WORN AREAS. REMOVED AND REPLACED NR 6 FLAP VANE IAW DC8 MM 27-50-0 PG 201 AND 27 51-14 PG 201. N/R CARD NR 0066. 2 L 7 4 4F RT 4A25 1999101500426 19991015 00426 WP 1999 10 15 DHL9980641C 1 19990824 A 5320 57601941 TRAP PANEL DOUG DC8 DC873F 302199F WP LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LT MLG TRAPEZOIDAL FITTING SHOWS CRACKED AREA AT WEB SIDE. REPAIRED IAW SB 5361, CONDITION 4. REMOVED AND REPLACED INBD AND OTBD SPLICE PLATES IAW SB 53-61. N/R CARD NR 0115. 2 L 7 4 4F RT 4A25 1999101500427 19991015 00427 WP 1999 10 15 DHL9980642C 1 19990831 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 170 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, MAIN CARGO DOOR CUTOUT LWR AREA EXISTING DOUBLER REPAIR IS CRACKED AT STA 170.00. REMOVED DAMAGED EXISTING DOUBLER, FABRICATED REPAIR DOUBLER AND INSTALLED IAW E/O NR 999090303. N/R CARD NR 0684. 2 L 7 4 4F RT 4A25 1999101500428 19991015 00428 1999 10 15 DHL9980643C 4 19990908 A 3130 TRANSDUCER DOUG DC8 DC873F 302199F WP FLIGHT DATA REC BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, TRANSDUCER FOR FDR LINE BROKEN TO RUDDER ACTUATOR. REMOVED AND REPLACED TRANSDUCER PER DC8 MM 31-22-0, OPS CKD PER DC8 MM 31-22-0. N/R CARD NR 0864. 2 L 7 4 4F RT 4A25 1999101500429 19991015 00429 WP 1999 10 15 DHL9980644C 1 19990908 A 2720 PULLEY DOUG DC8 DC873F 302199F WP RUDDER CONTROL BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, A/C RUDDER PACK LT CONTROL CABLE PULLEY ACCESSIBLE THROUGH DOOR 362 AT TAIL CONE IS BROKEN. REMOVED AND REP LACED PULLEY IAW DC8 MM 20-17-0 PG 201 AND 27-21-0 PG 1. OPS CKD IAW DC8 MM 27-20-0 PG 601-605. N/R CARD, NR 0866. 2 L 7 4 4F RT 4A25 1999101500430 19991015 00430 WP 1999 10 15 DHL9980645C 1 19990909 A 2720 PULLEY DOUG DC8 DC873F 302199F WP REUDDER CONTROL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, AFT ACCESSORY CPMPT THROUGH ACCESS DOOR NR 62 RUDDER LEFT CABLE CONTROL PULLEY, DAMAGED. REMOVED AND REPLAC ED PULLEY IAW DC 8 MM 20-17-0 PG 201 AND 27-21-0 PG 1. OPS CKD IAW DC8 MM 27-20-0, PG 601-605. N/R CARD NR 0877. 2 L 7 4 4F RT 4A25 1999101500431 19991015 00431 WP 1999 10 15 DHL9980646C 1 19990913 A 2720 3654952537 CONTROL CABLE DOUG DC8 DC873F 302199F WP AFT PRESS BLKHD FRAYED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, EMPENAGE AREA AFT PRESS BULKHEAD RT RUDDER CONTROL CABLE FRAYED. REMOVED AND REPLACED CABLE RUN NR RL IAW D C8 MM 27-20-0 PG 502, RIG CK IAW DC8 MM 27-20-0 PG 510. RUDDER TAB OPS CK PERFORMED IAW DC8 MM 27-20-0 PG 601-605. N/ R CARD NR 0909. 2 L 7 4 4F RT 4A25 1999101500432 19991015 00432 WP 1999 10 15 DHL9980647C 1 19990922 A 2730 2653848501 CONTROL CABLE DOUG DC8 DC873F 302199F WP COCKPIT FRAYED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, F/O SIDE AT FLOOR LEVEL, PTC CENTERING CABLE IS FRAYED. REMOVED AND REPLACED CABLE ASSY (PTC REACTION) IAW DC8 MM 27-30-0 PG 503, RIG AND OPS CK IAW DC8 MM 27-30-0. N/R CARD NR 0998. 2 L 7 4 4F RT 4A25 1999101500433 19991015 00433 WP 1999 10 15 DHL9980648C 1 19990823 A 5330 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, FUSELAGE LOWER PANEL NR 162Q DELAMINATED. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER IAW DC8 SRM 51-1-9 PG 37. INSTALLED REPAIR DOUBLER PER DC8 SRM 51-1-9 PG 37. N/R CARD NR 0068. 2 L 7 4 4F RT 4A25 1999101500434 19991015 00434 WP 1999 10 15 DHL9980649C 1 19990826 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 3 CORRODDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RT WING UPPER SKIN AT XW 3.00 AND FUS STA 902 SHOWS WORN AREA. BURNISHED WORN AREA, FABRICATED DOUBLER REP AIR 4 BY 12 PER SM 51-1-9. N/R 239. 2 L 7 4 4F RT 4A25 1999101500435 19991015 00435 WP 1999 10 15 DHL9980650C 1 19990916 A 5280 SKIN DOUG DC8 DC873F 302199F WP RT MLG DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RT MLG I/B DOOR LOWER SIDE FWD CORNER SHOWS DAMAGED AREA. FABRICATED DOUBLER REPAIR 8 BY 2 PER EO 99090201 AND INSTALLED DOUBLER PER SRM 51-1-8. N/R 244. 2 L 7 4 4F RT 4A25 1999101500436 19991015 00436 WP 1999 10 15 DHL9980651C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 781 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 2 SEAT TRACK FS 781 BROKEN TEETH AND SURFACE CORROSION. CUT OUT DAMAGED SECTIONS. INSTALLED CARGO TRACK REPAIR PER SRM 53-2-3, N/R 263. 2 L 7 4 4F RT 4A25 1999101500437 19991015 00437 WP 1999 10 15 DHL9980652C 1 19990826 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1260 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LOWER EXT FUSELAGE FOUND SKIN BULGING FS 1260 LONGERON 33L. REMOVED DOUBLER REPAIR, CUT OUT DAMAGED SECTIO N AND FABRICATED NEW REPAIR AND INSTALLED PER EO 99090203. REPAIR DOUBLER 20.5 BY 18, FILLER 2.5 BY 2.0, N/R 272. 2 L 7 4 4F RT 4A25 1999101500438 19991015 00438 WP 1999 10 15 DHL9980653C 1 19990826 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 170 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LOWER EXTERIOR FUSELAGE AT STA 170 BETWEEN LONGERON 35R TO 3L IS BULGING AND RIVET POPPED. SHORED AND LEVEL ED A/C. REMOVED CORRODED SPLICES FROM FWD CARGO COMPTS, FABRICATED NEW SPLICES 63 BY 4 AND INSTALLED PER SRM 54-4-1. N /R 298. 2 L 7 4 4F RT 4A25 1999101500439 19991015 00439 WP 1999 10 15 DHL9980654C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 930 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 4 SEAT TRACK FS S930- 920 PREV REPAIR PLUG HAS SURFACE CORROSION AND ELONGATED HOLES. REMOVED AND REPLAC ED PER SRM 51-1-8, N/R 305. 2 L 7 4 4F RT 4A25 1999101500440 19991015 00440 WP 1999 10 15 DHL9980655C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 5 SEAT TRACK FS 950 THROUGH 960 HAS SURFACE CORROSION. REMOVED AND REPLACED CARGO TRACK PER SRM 51-1-8, N/R 313. 2 L 7 4 4F RT 4A25 1999101500441 19991015 00441 WP 1999 10 15 DHL9980656C 1 19990826 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1570 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, NR 6 SEAT TRACK FS 1680 TO 1510 HAS CORROSION AND BROKEN. CUT OUT SECTION FROM 1570 TO 1630 AND REPLACED P ER SRM 51-1-8. N/R 323. 2 L 7 4 4F RT 4A25 1999101500442 19991015 00442 WP 1999 10 15 DHL9980657C 1 19990827 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 270 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, SEAT TRACK WORN NR 4 BETWEEN FS 270 AND 290. CUT OUT DAMAGED SECTION, AND INSTALLED REPAIR PER SRM 53-2-3. N/R 418. 2 L 7 4 4F RT 4A25 1999101500443 19991015 00443 WP 1999 10 15 DHL9980658C 1 19990827 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 320 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, SEAT TRACK NR 4 BETWEEN FS 320 AND 340 IS WORN. REMOVED AND REPLACED SEAT TRACK FROM THOSE AREAS PER SRM 5 1-1-18, N/R 419. 2 L 7 4 4F RT 4A25 1999101500444 19991015 00444 WP 1999 10 15 DHL9980659C 1 19990827 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 670 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, SEAT TRACK BETWEEN FS 670 AND 690 IS WORN. REMOVED DAMAGED TRACK AND REPLACED PER SRM 51-1-8. N/R 420. 2 L 7 4 4F RT 4A25 1999101500445 19991015 00445 WP 1999 10 15 DHL9980660C 1 19990927 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 660 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, MAIN CARGO COMPT SEAT TRACK ROW NR 5 PLUG REPAIR BETWEEN FS 680 AND 660 WORN. REMOVED EXISTING PLUG AND REI NSTALLED NEW PER SRM 53-2-3. N/R 422. 2 L 7 4 4F RT 4A25 1999101500446 19991015 00446 WP 1999 10 15 DHL9980661C 1 19990827 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 320 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, MAIN CARGO COMPT SEAT TRACK ROW NR 5 BETWEEN STA 320 AND 340 IS WORN. REMOVED AND REPLACED DAMAGED AREA PER SRM 53-2-3. N/R 424. 2 L 7 4 4F RT 4A25 1999101500447 19991015 00447 WP 1999 10 15 DHL9980662C 1 19990827 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 140 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, SEAT TRACK ROW 5 BETWEEN STA 140 AND 160 PLUG REPAIRS WORN. REMOVED AND REPLACED DAMAGED PLUGS PER SRM 51-1 -8. N/R 425. 2 L 7 4 4F RT 4A25 1999101500448 19991015 00448 WP 1999 10 15 DHL9980663C 1 19990827 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 150 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, SEAT TRACK NR 6 PLUG REAPIRS BETWEEN FS 150 AND 170 WORN. REMOVED AND REPLACED SEAT TRACK PER SRM 51-1-8. N /R 427. 2 L 7 4 4F RT 4A25 1999101500449 19991015 00449 WP 1999 10 15 DHL9980664C 1 19990829 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 519 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LEFT WING L/E INTERIOR LOWER AREA CRACKED. STOP DRILLED ON WEB SECTON XFS ACCESS PANEL 519 C. FABRICATED R EPAIR WEB AND INSTALLED PER SRM 51-1-21.3 BY 2.75, N/R 533. 2 L 7 4 4F RT 4A25 1999101500450 19991015 00450 WP 1999 10 15 DHL9980665C 1 19990829 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 291 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LEFT WING L/E LOWER SURFACE CRACKED AT RIVET HOLE XFS 291. STOP DRILLED ENDS OF CRACKS. INSTALLED REAPAIR DOUBLER PER EO 99090302, 18 BY 9 N/R 545. 2 L 7 4 4F RT 4A25 1999101500451 19991015 00451 WP 1999 10 15 DHL9980666C 1 19990831 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, BELOW FLOOR PANEL AT COCKPIT, INTERCOSTAL PANEL AT CENTER LINE REAR UPPER FLANGE CRACKED. STOP DRILLED END OF CRACK, FABRICATED ANGLE PER SRM 53-2-0 AND INSTALLED 7 BY 3.5, N/R 693. 2 L 7 4 4F RT 4A25 1999101500452 19991015 00452 WP 1999 10 15 DHL9980667C 1 19990901 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 33 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, RT WING T/E SECTION I/B AREA APPROX STA XW 33 WEB HAS CRACK. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER PER SRM 51-1-8 AND INSTALLED PER SRM 57-2-0, 7 BY 2 N/R 773. 2 L 7 4 4F RT 4A25 1999101500453 19991015 00453 WP 1999 10 15 DHL9980668C 1 19990901 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1240 PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, CENTER FLOOR STA 1240-1260 HAS HOLES IN MIDDLE OF PANEL. FABRIACATED DOUBLERS TWO 3 BY 3 FT AND TWO 1 BY 1 PER SRM 53-2-0. N/R 802. 2 L 7 4 4F RT 4A25 1999101500454 19991015 00454 WP 1999 10 15 DHL9980669C 1 19990903 A 5330 SKN DOUG DC8 DC873F 302199F WP BS 800 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, LOWER EXT FUSELAGE STA 800 RIGHT SIDE AREA AROUND RIVET IS CRACKED. CUT OUT DAMAGED SECTION AREA OF SKIN. FABRICATED NEW SKIN AND INSTALLED PER SRM 53-3-0. N/R 835. 2 L 7 4 4F RT 4A25 1999101500455 19991015 00455 NE 1999 10 15 DHL99709003 2 19991005 A 7200 ENGINE BOEING 727 72782C 1384026 NM PWA JT8 JT8D7 52053 NE NR 3 FAILED A DHLA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CR CRUISE 1 SO 01 709DH 19968 657636 NR 3 OIL TEMP ABOVE 157C APPROX 5 MINUTES UNTIL ENGINE SHUT DOWN WAS ACCOMPLISHED. AFTER SHUT DOWN, OIL TEMP SLOWLY CA ME DOWN. 20 MIN AFTER SHUTDOWN, TEMP WAS 65C AS OIL COOLED PRESSURE INCREASED WIND MILLED FOR APPROX 10 MIN WITH LOW OI L PRESSURE LIT ON AND PRESSURE BELOW 35. REMOVED AND REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999101500456 19991015 00456 NM 1999 10 15 VNAA9910005 1 19991009 A 2913 42086 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT HYD SYS FAILED A VNAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 440JS 10116 3058 ON TAXI, THE FLIGHT CREW RECEIVED A FLAP CONTROL FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND THE MAIN HYDRAULIC P UMP WAS NOT WORKING. THE AIRCRAFT WAS FERRIED TO CAK WHERE MAINTENANCE REPLACED THE MAIN HYDRAULIC PUMP/MOTOR ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-11-04. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999101500457 19991015 00457 NM 1999 10 15 VNAA9910004 1 19991007 A 3250 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING STICKING A VNAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 07 423JS 3032 FLIGHT 4087- WAS ON APPROACH TO PIT WHEN A NOSE WHEEL STEERING POWER-UP CAS MESSAGE WAS DISPLAYED. THE FLIGHT CREW REVI EWED THE QRH AND PERFORMED A SECOND APPROACH AND LANDED WITHOUT DIFFICULTIES. MAINTENANCE INSPECTED AND FOUND THE RT CO NDITION LEVER MICROSWITCH TO BE STUCK. MAINTENANCE EXERCISED THE MICROSWITCH AND PERFORMED OPERATIONAL CHECKS IN ACCORD ANCE WITH DORNIER MAINTENANCE MANUALS 76-11-05 AND 32-51-00 AND ALL WAS FOUND TO OPERATE NORMALLY. THE AIRCRAFT WAS RET URNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999101500458 19991015 00458 NM 1999 10 15 VNAA9910003 1 19991007 A 3350 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 9A LOOSE A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 328LS 3025 THE FLIGHT CREW REPORTED THAT THE FLOOR EMERGENCY LIGHT AT SEAT 9A WAS INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECT ED THE ELECTRICAL CONNECTOR AT 45LK LIGHT STRIP AND OPERATIONAL CHECKS WERE ACCOMPLISHED IN ACCORDANCE WITH DORNIER MAIN TENANCE MANUAL 33-51-00 AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999101500459 19991015 00459 NE 1999 10 15 VNAA9910002 2 19991006 A 7261 AS3209133 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 423JS 3032 116092 HL351 WHILE IN CRUISE FLIGHT, THE LEFT ENGINE OIL PRESSURE INDICATION BEGAN TO FLUCTUATE AND THEN TURNED AMBER. THE FLIGHT CR EW FOLLOWED THE QRH AND FEATHERED THE LEFT PROPELLER. THE LEFT ENGINE OIL PRESSURE CONTINUED TO FLUCTUATE AND THEN TURN ED INTO A RED INDICATION WHICH RESULTED IN THE FLIGHT CREW SHUTTING DOWN THE LEFT ENGINE. THE AIRCRAFT DIVERTED TO CRW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT ENGINE ALTERNATOR GARLOCK SEAL TO BE LEAKING. THE SEAL WAS REPLACED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-10-04. OPERATIONAL AND LEAK CHECKS WE RE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999101500460 19991015 00460 SO 1999 10 15 RAIA9910012 1 19991009 A 3010 3294453 VALVE EMB 145 EMB145ER SO HORIZ STAB FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 803HK 316 316 145077 5788 - ORD- STAB ANTI-ICE INOP MESSAGE ON. MAINTENANCE REPLACED STAB ANTI-ICE VALVE. 2 L 7 2 4F RT T00011AT 1999101500461 19991015 00461 EU 1999 10 15 RAIA9910013 1 19991009 A 2910 1379007D474 LINE BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA A B UNSCHED LANDING EMER. DESCENT K FLUID LOSS LD LANDING 1 CE 03 343TE 955 7334 - STL - LOST ALL HYDRAULIC PRESSURE. MAINTENANCE REPLACED HYD LINE ON RIGHT SIDE OF AIRCRAFT. 2 L 7 2 4T RT A56EU 1999101500462 19991015 00462 WP 1999 10 15 TWAA9914001 1 19991011 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 928TW 48012 THE FIRST CLASS CABIN EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 2-2-99 MCI. 2 L 7 2 4F A6WE 1999101500463 19991015 00463 WP 1999 10 15 TWAA9914002 1 19990928 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 316 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT FOUND A 4 IN LONG BY 2 IN WIDE BY 0.180 DEEP DENT IN THE FUSELAGE SKIN AT STA 316, LONGERON 22L. R EPAIRED PER SRM 53-04, PAGE 35. 2 L 7 2 4F RT A6WE 1999101500464 19991015 00464 WP 1999 10 15 TWAA9914003 1 19990928 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 389 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT FOUND THE FUSELAGE SKIN HAD A BULGE AT STA 389, LONGERON 30 TO 28R. ACCOMP NDT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REPAIRED PER SRM 53-04, PAGE 35. 2 L 7 2 4F RT A6WE 1999101500465 19991015 00465 WP 1999 10 15 TWAA9914004 1 19990927 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 979Z 47343 DURING OP 16 MAINT CHECK FOUND CABIN STRINGER 4L CRACKED AT FORMER STA 200. REPLACED STRINGER FROM APPROX STA 230 TO 17 0. INSTALLED REPAIR SPLICE AT STA 170 PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1999101500466 19991015 00466 WP 1999 10 15 TWAA9914005 1 19990929 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 350 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK-C MAINT FOUND FUSELAGE SKIN BULGED AT STA 350 BETWEEN LONGERON 22L AND 23L. ACCOMP HFEC PER NDT MANUAL PAR T 6, 51-00-03, AND NO CRACK FOUND. REPAIRED PER SRM 53-04, PAGE 35, FIG 12B. 2 L 7 2 4F RT A6WE 1999101500467 19991015 00467 WP 1999 10 15 AT9900695 1 19990910 A 3340 59203562 LIGHT DOUG DC9 DC932 3022066 WP RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND RIGHT HAND LEADING EDGE LIGHT FIXTURE WAS CORRODED OUT OF LIMITS. REMOVED CORROSION INSIDE LIGHT FIXTURE, NET LOS S 80 PERCENT, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LIGHT FIXTURE IAW DC SRM 51-10-3, 51-10-4, 51-30-2. 2 L 7 2 4F A6WE 1999101500468 19991015 00468 WP 1999 10 15 AT9900696 1 19990909 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 579-682 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FLOOR PANEL AT FS 598 CRACKED AND CUT, 3 HAT CHANNELS CRACKED. FABRICATED NEW PANEL AND INSTALLED NEW HAT CHANNEL S IAW DC9 SRM 51-10-1, 51-10-2, 51-10-4, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1999101500469 19991015 00469 WP 1999 10 15 AT9900697 1 19990909 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 120-131 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FLOOR PANEL UNDER 1ST OFFICERS SEAT CORRODED AT BS 120-131. FABRICATED NEW FLOOR PANEL AND HAT FRAMES. INSTALLED NEW HAT FRAMES AND FLOOR PANEL IAW DC9 SRM 53-05 FIGURE 1, 51-30-2. 2 L 7 2 4F A6WE 1999101500470 19991015 00470 NM 1999 10 15 AT9900712 1 19991008 A 3350 900542 BATTERY CHARGER BOEING 737 7372L9 1384497 NM BS 747 CRACKED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CRACKED BATTERY CHARGER HOUSING AT CEILING EMERGENCY LIGHT BS 747. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY C HARGER/POWER PACK AT BS L747 IAW 737 MM 33-51-81, 33-51-0. 2 L 7 2 4F RT A16WE 1999101500471 19991015 00471 WP 1999 10 15 AT9900715 1 19991007 A 5320 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FORWARD COMPARTMENT LOWER DOOR JAMB CORNER CRACKED .5 INCH ON OUTER SKIN. CUT OUT CRACKED AREA, FABRICATED AND I NSTALLED DOUBLER AND TRIPLER REPAIR IAW EO 99-1262, DC9 SRM 51-10-3, 51-30-2, 51-20-0, 51-30-0. 2 L 7 2 4F A6WE 1999101500472 19991015 00472 WP 1999 10 15 AT9900716 1 19991009 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 120-160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND WEB AT BS 120, RBL 16 TO RBL 20 CORRODED, FORWARD AND AFT OF FLOORBEAM WAS BULDGED AND CRACKED. FABRICATED AND I NSTALLED REPAIR WEBS AND 5 SPLICES IAW DC9 SRM 51-10-3, 51-10-4, 51-30-1, 51-30-2, 51-30-5, 53-20-1, 27-20-2, 27-10-0. 2 L 7 2 4F A6WE 1999101500473 19991015 00473 WP 1999 10 15 AT9900717 1 19990913 A 5210 5934796523N BEAM DOUG DC9 DC932 3022066 WP L1 DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND L-1 DOOR NR 4 BEAM WAS CRACKED AT THE AFT END. INSTALLED NEW FITTING, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 52-01 FIGURE 1, 51-30-2, 51-10-3, 51-10-4. 2 L 7 2 4F A6WE 1999101500474 19991015 00474 WP 1999 10 15 AT9900718 1 19990912 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT ELEVATOR CRACKED IN THE SECONDARY SKIN AT THE RIVET OF THE OUTBOARD TRIM ATTACH POINT. STOP DRILLED HOLE ND T REVEALED CRACK CONTINUED. FABRICATED AND INSTALLED REPAIR STRIP IAW DC9 SRM 51-30-8, 53-10-2, 51-10-2, 51-10-4, 51-10 -3. 2 L 7 2 4F A6WE 1999101500475 19991015 00475 WP 1999 10 15 AT9900719 1 19990913 A 5347 52914913138500 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 908 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND LEFT OUTBOARD SEAT TRACK WAS GOUGED AT BS 908. REMOVED AND REPLACED TRACK IAW DC9 SRM 53-05 FIGURE 4F 53-20-1, 51 -10-3, 51-10-4. 2 L 7 2 4F A6WE 1999101500476 19991015 00476 WP 1999 10 15 AT9900720 1 19990917 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND PANEL SUPPORT AT BL 0 SB 160-218 WAS CORRODED. REMOVED CORRODED SUPPORT, FABRICATED NEW SUPPORT DEBURRED, TREATED , PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-2, 51-30-5. 2 L 7 2 4F A6WE 1999101500477 19991015 00477 WP 1999 10 15 AT9900722 1 19991009 A 2150 QS100MS68 CLAMP DOUG DC9 DC932 3022066 WP RT ACM DUCT FAILED A ZZDA G O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 SO 15 866AT 47168 INBOUND TO ATL LOST CABIN PRESSURIZATION AT 14,000 FT, PASSENGER OXYGEN MASKS DEPLOYED. BOTH AIR CONDITIONING PACKS QUI T AT THE SAME TIME. BOTH PACKS WERE RESTARTED BUT THEY QUIT AGAIN. FOUND RIGHT AIR CYCLE MACHINE DISCHARGE DUCT BLOWN. RE-SECURED BLOWN DUCT AND CHANGED CLAMPS. OPERATED BOTH PACKS AND PRESSURIZED AIRCRAFT. NO LEAKS OR DEFECTS NOTED IN AIR-CONDITIONING SYSTEM. ALL WORK DONE IAW DC9 MM 21-50. 2 L 7 2 4F A6WE 1999101500478 19991015 00478 1999 10 15 MALA976596 2 19991001 A 7200 ENGINE BAC 146 AVRO146RJ85A 1500097 EU NR 4 FAILED A MALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 507XJ E2316 EN ROUTE DTW - DLH, NR 4 ENGINE OIL PRESSURE LIGHT ILLUMINATED, INDICATION WAS AT ZERO. CREW STARTED TO PERFORM QRH PRO CEDURES WHEN ENGINE NR 4 OVERSPEED AND SHUT ITSELF DOWN. COMPLETED QRH AND DIVERTED TO TVC. MAINTENANCE REPLACED NR 4 ENGINE ASSEMBLY IAW AMM AND ASSOCIATED ENGINE CHANGE TASK CARDS. OPS AND LEAK CHECK GOOD. 2 H 7 4 4F RT A49EU 1999101500479 19991015 00479 EU 1999 10 15 MALA976597 1 19991007 A 3020 NH2466916901 DUCT SAAB SF340 340B 7860101 EU LT ENGINE INLET SHORTED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 404XJ 340B404 LEFT INTAKE LIGHT ILLUMINATED. TRIED TO RESET PER QRH, WOULD N'T RESET. RETURNED TO MSP. MAINTENANCE REPLACED SHORTED INLET DUCT IAW SAAB 340 AMM 71-60-05 AND CONTROLLER IAW SAAB AMM 30-20-15. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999101500480 19991015 00480 EU 1999 10 15 MALA976598 1 19991009 A 2612 CGAB120100 FIRE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY DAMAGED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 448XJ 448 CARGO COMPARTMENT FIRE INDICATION IN COCKPIT. DIVERTED TO GRR, LANDED WITHOUT PROBLEM. TURNED CARGO COMPARTMENT FIRE E XTINGUISHER AND BOTH ENGINE FIRE EXTINGUISHERS ON. TURNED ON EMERGENCY LIGHT, ELT AND PRESSURIZATION DUMP SWITCHES. MA INTENANCE REPLACED FIRE BOTTLES AND CARGO SMOKE DETECTOR, OPS CHECKS GOOD. RESET SWITCHES. 2 L 7 2 4T RT A52EU 1999101500481 19991015 00481 EU 1999 10 15 MALA976599 1 19991005 A 3244 TIRE SAAB SF340 340B 7860101 EU LT MLG FAILED A MALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 454XJ 454 ON TAXI OUT, THE HYDRAULIC QUANTITY WENT TO ZERO. RETURNED TO GATE. MAINTENANCE FOUND LT O/B TIRE BLOWN AND BRAKE LINE SHEARED. REPLACED TIRE AND BRAKE LINE, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999101500482 19991015 00482 EU 1999 10 15 MALA976600 1 19991008 A 2780 RETRACT MECH BAC 146 AVRO146RJ85A 1500097 EU LE FLAPS LACK OF LUBE A MALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 15 523XJ E2348 ON APPROACH TO DTW, WHEN SELECTING FLAPS 18 DEGREES TO FLAP 24 DEGREES RECEIVED FLAP INOP AND FLAP FAULT, FLAPS WERE STU CK AT 18 DEGREES. AFTER COMPLYING WITH QRH AND FIGURING NEW LANDING DISTANCE, CAME BACK AROUND WITH NO FURTHER INCIDENC E. MAINTENANCE GREASED 1, 2, 3, 4 BALL JACK ASSEMBLIES AS REQUIRED. RERACKED FLAP CONTROL UNIT, GROUND RUN FLAPS THRU SEVERAL CYCLES. ALL CHECKS GOOD IAW AVRO AMM CH 27. NO FAULTS NOTED AT THIS TIME. 2 H 7 4 4F RT A49EU 1999101500483 19991015 00483 NE 1999 10 15 MALA976601 2 19991009 A 7320 219333009 HMA BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 1 ENGINE FAILED A MALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 502XJ E2307 NR 1 ENGINE N1 FLUCUATED AFTER TAKEOFF AT 10 TO 11K FT, THEN 3 TIMES IN CRUISE, NOT HIGHER THAN 101 PERCENT. ON DESCENT WITH POWER BACK IT STARTED FLUCUATING SEVERAL TIMES RAPIDLY. TURNED NR 1 FADEC OFF, NO DIFFERENCE, SHUT NR 1 ENGINE DO WN 35 MILES OUT OF DTW. MAINTENANCE REPLACED NR 1 HMA ASSEMBLY IAW ALLIED SIGNAL EMM 72-00-61. OPS, LEAK, SECURITY CHE CK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500484 19991015 00484 EU 1999 10 15 MALA976602 1 19991008 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 442XJ 442 CARGO SMOKE LIGHT ILLUMINATED EN ROUTE TO TYS. COMPLETED QRH, DISCHARGED BOTH CARGO SMOKE BOTTLES. LANDED IN LEX. MAI NTENANCE INSPECTED AND CLEANED FWD AND AFT SMOKE DETECTION UNITS IAW 26-13-00-7. PERFORMED OPS CHECK, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999101500485 19991015 00485 EU 1999 10 15 MALA976603 1 19991008 A 2611 CGAB1201001 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 442XJ 442 CARGO SMOKE LIGHT ILLUMINATED ON FINAL INTO DTW, (LIGHT ON & OFF SEVERAL TIMES). COMPLETED QRH, LANDED IN DTW. MAINTEN ANCE REPLACED BOTH CARGO FIRE BOTTLES AND FWD CARGO SMOKE DETECTOR. ALL WORK DONE IAW SF 340 M/M 26-23-10. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999101500486 19991015 00486 EU 1999 10 15 MALA976604 1 19991008 A 2611 M835362024M RELAY SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 442XJ 442 CARGO SMOKE ANNUNICATOR ILLUMINATED. INSPECTED CARGO, NO SMOKE NOTED. SUSPECT FAULTY DETECTION. MAINTENANCE REPLACED TEST BOX RELAY, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999101500487 19991015 00487 EU 1999 10 15 MALA976605 1 19991009 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 442XJ 442 CARGO SMOKE LIGHT ILLUMINATED ON GROUND WITH DOOR OPEN, VISUALLY VERIFIED NO SMOKE. MAINTENANCE REPLACED AFT CARGO SMOK E DETECTOR PER SAAB MM 26-13-15. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999101500488 19991015 00488 WP 1999 10 15 IXXA900024 1 19991006 A 3230 UPLATCH DOUG DC8 DC871F 302199D WP NLG DIRTY A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 823BX 80275 2961 46064 EN ROUTE FROM LAX TO TOL, THE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCL ED THE GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANC E INSPECTED THE LANDING GEAR WHICH REVEALED THE NOSE GEAR UPLATCH IN NEED OF LUBRICATION. MAINTENANCE CLEANED AND LUBRI CATED THE NOSE UPLATCH MECHANISM. MAINTENANCE PERFORMED A SUCCESSFUL GEAR SWING, AND THE AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 4 4F RT 4A25 1999101500489 19991015 00489 1999 10 15 COMA9910162 3 19991009 A 6140 SELOC29DH NP INDICATOR EMB 120 EMB120RT SO RT PROP FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 152CA 24574 1152 DURING TAKEOFF ROLL, THE RIGHT PROPELLER INDICATED 97.6 PERCENT NP. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GA TE. REPLACED THE RIGHT NP INDICATOR. 2 L 7 2 4T RT A31SO 1999101500490 19991015 00490 EA 1999 10 15 COMA9960593 1 19991010 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 786CA 178 7333 DURING APPROACH INTO CVG, THE FLAP FAIL WARNING MESSAGE ACTIVATED. REPLACED THE BRAKE POSITIONING SENSING UNIT. 2 L 7 2 4F RT A21EA 1999101500491 19991015 00491 EA 1999 10 15 COMA9960594 1 19991009 A 2150 ACM CNDAIR CL600 CL6002B19 EA LEFT FAILED A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 995CA 7229 DURING APPROACH INTO CVG, A STRONG SMELL OF ELECTRICAL ODOR WAS NOTED IN THE COCKPIT AND CABIN ASSOCIATED WITH SMOKE. T HE CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. INVESTIGATION REVEALED THE LEFT AIR CONDITIONING UNIT FAILED CA USING SLIGHT SMOKE AND FOUL ODOR. THE LEFT ACM WAS DEFERRED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999101500492 19991015 00492 EA 1999 10 15 COMA9960595 1 19991008 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 EA RIGHT FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 918CA 11452 7018 DURING APPROACH INTO CVG THE FLAP FAIL WARNING MESSAGE ACTIVATED.\NREPLACED THE RIGHT P.D.U. ASSEMBLY. 2 L 7 2 4F RT A21EA 1999101500493 19991015 00493 1999 10 15 COMA9960596 4 19991010 A 3418 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA RT AOA TRIPPED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 785CA 7326 DURING CLIMBOUT FROM CVG, THE RIGHT AOA CAUTION MESSAGE ACTIVAGED. AIRCRAFT RETURNED TO THE FIELD. CYCLED THE CIRCUIT BREAKER FOR THE RIGHT AIR DATA SENSING HEATER CONTROLLER. 2 L 7 2 4F RT A21EA 1999101500494 19991015 00494 EA 1999 10 15 COMA9960597 1 19991008 A 2740 601R517063 CONTROL PANEL CNDAIR CL600 CL6002B19 EA STAB TRIM FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 963CA 14854 7127 STABILIZER CHANNEL NR 1 INOPERATIVE MESSAGE APPEARED SEVERAL TIMES AFTER DEPARTURE FROM CVG. AIRCRAFT RETURNED TO THE F IELD. REPLACED THE STABILIZER TRIM PANEL. 2 L 7 2 4F RT A21EA 1999101500495 19991015 00495 NM 1999 10 15 UPS99230872 1 19991009 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM BAGGAGE COMPT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY LIGHT RIGHT SIDE JUST FWD OF AFT LOWER PIT DOOR INOP. REMOVED AND REPLACED LIGHT BATTERY PACK, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999101500496 19991015 00496 NM 1999 10 15 UPS99230873 1 19991009 A 5321 FLOOR BOEING 727 727173C 1384059 NM CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 INSPECTION TYPE:N/A, CRACK APPROX 6 INCHES LONG IN AFT LOWER PIT FLOOR JUST FORWARD OF DOOR. FABRICATED AND INSTALLED F LOOR PANEL I/B OF DOOR PER SRM 51-10-1. 2 L 7 3 4F A3WE 1999101500497 19991015 00497 WP 1999 10 15 UPS99830871 1 19991010 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE:N/A, EMERGENCY LIGHTS DISARM CHECK FAILED. REPLACED DEAD BATTERY AND RELAY ASSY IAW MM 35-50-01, REPAIR ED OPEN IN WIRE HVL9812R22 IN CHARGING CIRCUIT. REPAIRES OPEN AT SWITCH S1-3 27 A1 WIRE L9608A24. SYSTEM OPS NORMAL RE F WDM 33-50-01. 2 L 7 4 4F RT 4A25 1999101500498 19991015 00498 WP 1999 10 15 UPS99830874 1 19991007 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 1.5 INCH CRACK RIGHT WING LOWER SURFACE INB'D OF NR 3 PYLON. CRACK IS ON BOTH SIDES OF RIVET. REPAIRED AREA IAW SRM 5 7-2-1 FIG 35 AND SRM 57-2-1. 2 L 7 4 4F RT 4A25 1999101500499 19991015 00499 WP 1999 10 15 UPS99830875 1 19991009 A 5321 FLOOR DOUG DC8 DC873F 302199F WP CABIN MISINSTALLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:N/A, EVACUATION SLIDE GIRT BAR COULD NOT BE INSTALLED BECAUSE OF FLOOR PANEL RAISED TO HIGH. REINSTALLE D FLOOR PANEL TO BE FLUSH WITH FLOOR, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999101500500 19991015 00500 WP 1999 10 15 UPS99830876 1 19991010 A 2560 SMOKE CURTIAN DOUG DC8 DC873F 302199F WP CABIN UNSECURED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:N/A, SMOKE CURTAIN NOT ATTACHED TO FLOOR NEAR ENTRY DOOR. SECURED SMOKE CURTAIN TO FLOOR AS REQUIRED. O K FOR SERVICE. 2 L 7 4 4F RT 4A25 1999101500501 19991015 00501 NM 1999 10 15 99FDEA00420 1 19991011 A 3260 SWITCH BOEING 727 727225 1384077 NM LANDING GEAR DIRTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 467FE 21449 ON T/O LANDING GEAR RED DOOR LIGHT AND AMBER NOSE GEAR LIGHT REMAIN ON WITH GEAR UP. COMPLIED WITH RED TABS AND LIGHT R EMAIN ON. CLEANED DOOR AND GEAR SWITCHES, CHECKED FOR ADJUSTMENT AND ALL INDICATIONS NORMAL. 2 L 7 3 4F A3WE 1999101500502 19991015 00502 WP 1999 10 15 ABXA9900734 1 19990627 A 5753 5654743405 SKIN DOUG DOUG DC8 DC863 302198A WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LEFT INBOARD FLAP, INBOARD AFT UPPER SKIN CORRODED. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5642960. 2 L 7 4 4F 4A25 1999101500503 19991015 00503 WP 1999 10 15 ABXA9900735 1 19990627 A 5730 57696004 SKIN DOUG DOUG DC8 DC863 302198A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT WING LEADING EDGE, LOWER SKIN ABOVE THE NR 4 PYLON AT LEADING EDGE OF PYLON CUTOUT HAD A 3 INCH CRACK. REPAIRED I AW DC8 SRM 57-2-1A. 2 L 7 4 4F 4A25 1999101500504 19991015 00504 WP 1999 10 15 ABXA9900736 1 19990627 A 5730 57698579 SKIN DOUG DOUG DC8 DC863 302198A WP WS 467 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 LEFT WING LEADING EDGE ABOVE NR 1 PYLON INTERNAL SKIN WAS CRACKED AT STATION XW 467. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-11. 2 L 7 4 4F 4A25 1999101500505 19991015 00505 WP 1999 10 15 ABXA9900737 1 19990708 A 5753 5912168501 SKIN DOUG DOUG DC9 DC931 3022065 WP LT TE FLAP VANE DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 80892 1683 47065 APPROXIMATELY 80 PERCENT OF LEFT WING VANE SKIN DELAMINATED. REPAIRED UNIT IAW DC9 SRM. 2 L 7 2 4F A6WE 1999101500506 19991015 00506 WP 1999 10 15 ABXA9900738 1 19990711 A 5755 56551652 SKIN DOUG DOUG DC8 DC861 3021952 WP RT SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 RIGHT WING SPOILER DELAMINATED, 6 INCH WIDE AREA APPROXIMATELY 75 PERCENT OF LENGTH OF TRAILING EDGE. REPAIRED UNIT COM PLETE IAW DC8 SRM. 2 L 7 4 4F 4A25 1999101500507 19991015 00507 NM 1999 10 15 SCNA99124 1 19991005 A 3350 LIGHT BOEING 727 727225 1384077 NM ROW 28 INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE FLOOR EMERGENCY TRACK LIGHTING AT ROW 28 WAS FOUND INOPERATIVE. REPAIRED WIRING AT TRACK AT ROW 28. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999101500508 19991015 00508 NM 1999 10 15 SCNA99125 1 19991004 A 3350 LIGHT BOEING 727 727225 1384077 NM ROW 20 INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECKTHE CENTER SECTION FLOOR EMERGENCY TRACK WAS FOUND INOPERATIVE. REMOVED AND REPLACED ROW 20 EMERGENCY PATHWAY LIGHT SOCKET. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999101500509 19991015 00509 NM 1999 10 15 DHL99740005 1 19991009 A 3230 RETRACT MECH BOEING 727 7272Q9 138448M NM LANDING GEAR MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 740DH 21930 WHEN F/O ATTEMPED TO RETRACT GEAR, HANDLE WOULD NOT COME UP PAST NEUTRAL POSITION. PERFORMED CHECKLIST, AT FLAPS 2 WARN ING HORN DID NOT SOUND. PULLED GEAR OVERRIDE TRIGGER IN ACCORDANCE WITH CHECK LIST. WITH GEAR HANDLE UP, BOTH YELLOW G EAR WARNING LIGHTS AND BOTH RED GEAR WARNING LIGHT PLUS DOOR LIGHT WERE ILLUMINATED. PERFORMED LANDING GEAR LIGHT CHEC K LIST AND LOWERED LANDING GEAR. LANDED OK. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT, NO HELP. CHECKED LEVER TACH SOLENOID. CLEANED AIR/GND SENSOR FOR PRECAUTION. PERFORMED GEAR SWING, OPS CHECK GOOD PER MM 32-61. 2 L 7 3 4F RT A3WE 1999101500510 19991015 00510 SO 1999 10 15 SWIA971567 1 19990901 A 3010 PRESS REG EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT DEICE SYS FAILED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 224SW 120294 ON CLIMBOUT FROM SLC RIGHT DUCT LEAK CAME ON. RETURNED TO SLC. REPLACED RIGHT DEICE PRESSURE REGULATOR. OPS CHECKS GO OD WITH NO LEAKS FOUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999101500511 19991015 00511 SO 1999 10 15 SWIA971568 1 19990901 A 3610 GASKET EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PRESS REG MISINSTALLED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J W OVER TEMP WARNING INDICATION INADEQUATE Q C CL CLIMB 1 NM 07 224SW 120294 RIGHT DUCT LEAK LIGHT CAME ON CLIMBING OUT OF GJT. SHUT DOWN ENGINE AFTER THREE MINUTES. FOUND GASKET ON RIGHT PRESSUR E REGULATOR CANISTER TO HAVE BEEN INCORRECTLY INSTALLED. REINSTALLED GASKET IN PRESSURE REGULATOR CANISTER IAW MM 30-10 -00. RAN AIRCRAFT AND OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999101500512 19991015 00512 SO 1999 10 15 SWIA971569 1 19990905 A 3231 RETRACT MECH EMB 120 EMB120RT SO PWA 118 PW118A NE NLG DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 284YV 120284 LEFT NOSE LANDING GEAR DOOR REMAINED OPENED AFTER GEAR RETRACTION. RETURNED TO PSP. LATCHED GEAR DOOR AND CHECKED DOOR S FOR SECURITY. FOUND DOORS SECURE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999101500513 19991015 00513 SO 1999 10 15 SWIA971570 1 19990906 A 7712 TQ SIG COND EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 204SW 120243 LEFT ENGINE INADVERTENT AUTO FEATHER AFTER TAKEOFF. RETURNED TO FIELD. REMOVED AND REPLACED LEFT TORQUE SIGNAL CONDITI ONER. ALSO, REMOVED AND REPLACED LEFT TORQUE PROBE PER MM 77-11-2. OPS CHECKS GOOD PER MM 71-00-00. NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999101500514 19991015 00514 EU 1999 10 15 CA990420002 1 19990329 A 6730 AC67244 SERVO DUNLOP EE149 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 5188 22 4304 (CAN) DURING WALK-AROUND, A LARGE AMOUNT OF HYDRAULIC FLUID WAS FOUND ON THE INSIDE OF THE RIGHT HAND MAIN GEARBOX COWL. AIRCRAFT WAS RUN-UP AND HYDRAULIC FLUID WAS FOUND LEAKING FROM THE UPPER VENT HOLE. SUBSEQUENT INFORMATION REVEALED T HAT LEAKAGE FR0M THE VENT HOLE WAS CAUSED BY THE PISTON ROD RUBBING AGAINST THE RING WIPER THEREBY CAUSING WEAR AND SUBS EQUENT FLUID LEAKAGE. 1 G 7 1 3U 3 U NC H9EU E19EU 1999101500515 19991015 00515 NE 1999 10 15 CA990521002 2 19990412 A 7322 0164448390 FCU SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAULTY W O OTHER E VIBRATION/BUFFET LD LANDING 1 CA 315 4147 4147 (CAN) VERY PROMINENT ENGINE NOISE ON SHUTDOWN. NOISE WAS ISOLATED TO THE FUEL CONTROL UNIT. IT SOUNDED LIKE A BEARING BEING RUN DRY. THE FUEL CONTROL UNIT WAS SENT FOR EVALUATION. 1 G 7 1 3U 3 U H9EU E19EU 1999101500517 19991015 00517 GL 1999 10 15 CA990907004 2 19990805 A 7230 23066737 VANE 23063379 BELL 407 407 SW ALLSN 250C 250C47B GL COMPRESSOR CRACKED W B EMER. DESCENT E VIBRATION/BUFFET CR CRUISE 1 CA 69 CAC44046 CAE847027 (CAN) FAILED COMPRESSOR SCROLL TURNING VANES REPORTED PREVIOUSLY, THE CAUSE OF THIS INCIDENT WAS A FAILED SCROLL 70 HRS POST REPAIR. 1 G 7 1 3U 3 U O H2SW E1GL 1999101500518 19991015 00518 EA 1999 10 15 CA990907006 2 19990812 A 8530 LW11775 PLUG CESSNA 172 172N 2072434 CE LYC O320 O320D2J 41508 EA MCAULY 1C160 1C160DTM GL CYLINDER WORN W K NONE O OTHER IN INSP/MAINT 1 CA L117339 733708 (CAN) METAL CONTAMINATION FOUND IN FILTER SCREEN FROM PISTON PIN WARE. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999101500519 19991015 00519 GL 1999 10 15 CA990907009 3 19990814 A 6114 B3339 BOLTS HARTZL HCB5MP3CM108 STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE HARTZL HCB5M HCB5MP3 GL PROP HUB SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 1499 EV515 PCE97047 EV515 (CAN) ONE BOLT FOUND SHEARED AND BETA ROD PN B-3475A-3 WAS PULLED OUT. ON REMOVAL OF THE PROP, ANOTHER BOLT SHEARED. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 1999101500521 19991015 00521 1999 10 15 CA990907033 4 19990812 A 3452 5222703000 TRANSPONDER BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE E/E BAY INTERMITTENT W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION NR NOT REPORTED 1 CA 3174 649100 (CAN) AIRCRAFT REPORTED INTERMITTENT MODE C OPERATION. AIRCRAFT HAS TWO TRANSPONDERS CONNECTED TOGETHER TO 1 AIR DATA SOURCE. NR 2 TRS HAD AN INTERNAL MODE C CODE A4 INTERMITTENT SHORT WHICH EFFECTED BOTH. TRS REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999101500524 19991015 00524 NM 1999 10 15 CA990907057 1 19990812 A 5230 SWITCH BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE CARGO DOOR OUT OF ADJUST W O OTHER N FALSE WARNING DE DESCENT 1 CA (CAN) CARGO DOOR LIGHT ON S/OS PANEL ON DESCENT. LATCH LOCK PIN NOT ENGAGED ON DOOR CONTROL. AFT LATCH LOCK PIN MICROS WITCH FOUND OUT OF ADJUSTMENT, ADJUSTED. 2 L 7 3 4F 4 F RT A3WE E2EA 1999101500525 19991015 00525 EU 1999 10 15 CA990907058 1 19990804 A 5610 STA320141 WINDSHIELD AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A3 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 11594 731830 (CAN) IN CRUISE, LEFT PILOT'S WINDSHIELD OUTER PLY CRACKED. AIRCRAFT LANDED AND WINDSHIELD REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999101500526 19991015 00526 1999 10 15 CA990907059 4 19990812 A 3160 ECAM AIRBUS 330 A330322 3930325 EU PWA 4168 PW4168 NE COCKPIT FALSE SIGNAL W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA 00127 733336 (CAN) ECAM MESSAGE ON TAKEOFF INDICATED LOSS OF THRUST AND ENGINE ANTI-ICE FAULT WITH NO APPARENT FAULT. AIRBUS OIT 99 9.0106/96/SB AND TFU 73.25.000016. 2 L 7 2 4F 4 F RT A46NM E36NE 1999101500527 19991015 00527 NM 1999 10 15 CA990907074 1 19990730 A 2420 D309B GCU HG1804312 BOEING 737 7372E1 138448F NM PWA JT8 JT8D9A 52048 NE NR 1 TRIPPED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA A117076 665978 (CAN) DURING CLIMB AT 23,000 FEET, NR 1 GENERATOR TRIPPED OFFLINE, NR 1 GCU REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999101500528 19991015 00528 CE 1999 10 15 CA990907089 1 19990806 A 7160 SEALER CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160DTM GL AIR BOX DISLODGED W K NONE O OTHER IN INSP/MAINT 1 CA L4281827AZ L4281827AZ 730956 (CAN) SEALER USED IN ASSEMBLY OF CARBURETOR. HEAT BOX DISLODGED AND CAUGHT AROUND CARBURETOR VENTURI. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999101500529 19991015 00529 EU 1999 10 15 CA990915008 1 19990808 A 2810 0733095 O-RING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE RT FUEL DRAIN LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA LF05464A (CAN) RIGHT FUEL WATER DRAIN LEAKING.......ASSY REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500530 19991015 00530 NE 1999 10 15 CA990915027 2 19990826 A 7210 GEARBOX DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 15251 5732 121165 121165 891129 (CAN) NR 1 ENGINE MAKING METAL IN REDUCTION GEARBOX. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500531 19991015 00531 EU 1999 10 15 CA990915028 1 19990827 A 2910 SA7670006116 LINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA LF05542A (CAN) LOSS OF YELLOW SYSTEM HYDRAULIC FLUID IN--FLIGHT DUE TO FLEX LINE FROM PTU TO SHUTOFF VALVE LEAKING..LINE REPLACED . 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500532 19991015 00532 EU 1999 10 15 CA990915029 1 19990731 A 3240 VALVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE BRAKE SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 12837 30 JB116 LF05629A (CAN) HYDRAULIC FLUID TRANSFER FROM YELLOW TO GREEN SYSTEM. SHUTTLE VALVE FOUND FAULTY IN RECENTLY REPLACED BRAKE UNIT. BRAKE REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500533 19991015 00533 EU 1999 10 15 CA990915032 1 19990819 A 2913 716988 PUMP BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 20059 2783 F7847907 LF05464A (CAN) YELLOW HYDRAULIC SYSTEM INDICATED LOW AND FLUID OBSERVED LEAKING FROM NR 2 EDP. PUMP REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500534 19991015 00534 NE 1999 10 15 CA990915061 2 19990820 A 7322 C2CE347A LAYSHAFT DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HAMSTD 2D 2D30 NE CARBURETOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 13738 JP211757 JP211757 T25771 (CAN) LOWER THROTTLE CONTROL LAYSHAFT FOUND BROKEN DUE TO CORROSION. 1 H 7 1 3R 3 R A806 5E1 5 C P206 1999101500535 19991015 00535 EA 1999 10 15 CA990915065 2 19990907 A 7414 675421 BEARING LW1381 BNORM BN2 BN2A27 1520227 EU LYC O540 O540E4C5 41532 EA HARTZL HCC2Y HCC2YK2 GL MAGNETO WORN W K NONE O OTHER IN INSP/MAINT 1 CA 3454 1640 L1531140 AU491 (CAN) MAGNETO BEARING FAILED. 1 H 7 2 3O 3 O A17EU E295 5 C P920 1999101500536 19991015 00536 EU 1999 10 15 CA990915091 3 19990914 A 6114 RA58551 BOLTS BRAERO 748 HS7482A 4231001 EU RROYCE ROTOL R4304 R2124304 EU PROP HUB SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 10018 3392 DRG1676 DRG1676 (CAN) 3 OF 8 BOLTS SECURING THE HUB DRIVING CENTER TO THE HUB REAR FACE HAD SHEARED OFF AT THE HEADS. OPERATOR PREVIOUS LY EXPERIENCED THIS SAME CONDITION. 2 L 7 2 3T A24EU 6 C P899 1999101500537 19991015 00537 WP 1999 10 15 CA990916001 1 19990823 A 2612 672036285 FIRE LOOP LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE FAILED W E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 CA 10459 (CAN) FIRE DETECT LOOP B HAD INTERMITTENT FAILURE. 2 L 7 3 4F 4 F A23WE E12EU 1999101500538 19991015 00538 EU 1999 10 15 CA990916006 1 19990806 A 2810 VALVE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE RT WING LEAKING W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 731599 (CAN) AFTER TAKEOFF, FUEL OBSERVED LEAKING FROM RIGHT WING. AIRCRAFT LANDED. RIGHT AIR RELEASE VALVE FOUND TO BE UNSE RVICEABLE, UNIT REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999101500539 19991015 00539 NM 1999 10 15 CA990916010 1 19990730 A 2910 O-RING AIRBUS A319 A319114 NM NR 2 HYD SYS LEAKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA (CAN) LOSS OF NR 2 HYDRAULIC SYSTEM FLUID DUE TO LEAKING UNION AT POWER TRANSFER UNIT PRESSURE LINE. O-RING FOUND TO BE FAULTY. 2 L 7 2 4F RT A28NM 1999101500540 19991015 00540 GL 1999 10 15 CA990916020 2 19990820 A 7314 6899253 PUMP BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL FUEL SYS NOISY W K NONE O OTHER IN INSP/MAINT 1 CA 512 T102650 CAE835632 (CAN) GREASE WASHED OUT OF INTERNAL SPLINE OF THE FUEL PUMP. 1 G 7 2 3U 3 U H3EU E4CE 1999101500541 19991015 00541 EU 1999 10 15 CA990927001 1 19990913 A 5610 NP1653115 WINDSHIELD AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 18866 731468 (CAN) PILOT'S WINDSHIELD OUTER PLY CRACKED.....REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999101500542 19991015 00542 EU 1999 10 15 CA990927002 1 19990909 A 2722 3545H7 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE RUDDER ROUGH W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA 28155 FYH160604 LF05464A (CAN) CREW REPORTED RUDDER FEELS ROUGH. UPPER ACTUATOR REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500543 19991015 00543 NE 1999 10 15 CA990927003 2 19990910 A 7321 202255053 FCU AIRESRCH BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 ENGINE STICKING W O OTHER Y J ENGINE STOPPAGE WARNING INDICATION LD LANDING 1 CA 16096 6438 124353 LF05464A (CAN) NR 1 ENG SHUTDOWN DURING LANDING. INVESTIGATION REVEALED THAT THE NR 1 ENGINE TMS ACTUATOR HAD STUCK IN THE FULLY RETRACTED POSITION CAUSING THE FCU TO MOVE INTO THE SHUT-OFF POSITION WHEN THE THROTTLE WAS RETARDED TO FLIGHT IDLE. A CTUATOR REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500544 19991015 00544 EU 1999 10 15 CA990927005 1 19990910 A 3242 AHM1017 STATOR DUNLOP AHA2174 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE BRAKE DISINTEGRATED W K NONE O OTHER IN INSP/MAINT 1 CA 2842 HW026 LF05629A (CAN) NR 4 BRAKE ASSY REPLACED DUE TO WEAR. DISSASEMBLY REVEALED COMPLETE DISINTEGRATION OF SPREADER PLATE AND THE SPRE ADER PLATE WAS IN DIRECT CONTACT WITH THE ROTOR. SUBMITTER REPORTS THAT THE BRAKE WAS FULLY FUNCTIONAL IN THIS CONDITIO N. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500545 19991015 00545 1999 10 15 CA990927006 4 19990904 A 2312 071128271 CONTROL HEAD KING COMMCNTRL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE VHF SYSTEM MALFUNCTIONED W O OTHER O OTHER CR CRUISE 1 CA 6793 25 X2347 123132 901056 (CAN) CREW REPORTED NR 1 COMM SOMETIMES EXPERIENCES UNCOMMANDED FREQUENCY CHANGES, UNCOMMANDED TRANSMISSIONS, AND CAN BE DIFFICULT TO TUNE. REPLACED WITH SERVICEABLE UNIT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500546 19991015 00546 NM 1999 10 15 CA990927007 1 19990901 A 3242 68728 SEAL BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE DAMAGED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 254 1673 PCE120658 851115 (CAN) DURING INSPECTION OF THE AIRCRAFT, THE NR 2 BRAKE ASSY WAS FOUND LEAKING. THE PROBLEM WAS TRACED TO FAILURE OF TH E PISTON SEAL CAUSED BY DAMAGED/DISTORTED BACK-UP RINGS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500547 19991015 00547 NM 1999 10 15 CA990927009 1 19990907 A 2133 1036721 OUTFLOW VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUSELAGE FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 26679 12092 121165 891129 (CAN) DURING SCHEDULED INSPECTION, THE NORMAL OUTFLOW VALVE FAILED TASK NR 2130/03 (FUNCTION TEST NORMAL OUTFLOW VALVE P RESSURE RELIEF VALVE). THE OUTFLOW VALVE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500548 19991015 00548 GL 1999 10 15 CA990927030 2 19990413 A 7321 23065123 FCU BENDIX BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL ENGINE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 8558 CAE831797 (CAN) FCU SUSPECTED CAUSE FOR N2 OVERSPEED CONDITION. 1 G 7 1 3U 3 U H2SW E4CE 1999101500549 19991015 00549 NM 1999 10 15 CA990927045 1 19990907 A 2750 69638951 BRACKET BOEING 737 737204 1384458 NM PWA JT8 JT8D15 52051 NE NR 4 SPOILER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P688672 (CAN) NR 4 SPOILER ACTUATOR FORWARD SUPPORT BRACKET CRACKED AT ATTACH BOLT HOLE, REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999101500550 19991015 00550 WP 1999 10 15 CA990927074 1 19990920 A 7900 37604331 SEAL FC3520100 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE ENGINE OIL LEAKING W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 14829 (CAN) IN-FLIGHT SHUTDOWN DUE TO DECREASING OIL QUANTITY. ENGINE OIL CAP O-RING FOUND TO BE UNSERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 1999101500551 19991015 00551 WP 1999 10 15 CA990927075 1 19990910 A 2930 CONNECTOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE TRANSMITTER LOOSE W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 CA 14827 (CAN) AIRCRAFT LANDED DUE TO LOW HYDRAULIC QUANTITY SYS A. INVESTIGATION REVEALED A LOOSE CONNECTOR AT THE SENDING UNI T. 2 L 7 3 4F 4 F A23WE E12EU 1999101500552 19991015 00552 NM 1999 10 15 CA990927082 1 19990819 A 2530 OVEN BOEING 747 747433 NM PWA 4056 PW4056 NE GALLEY MALFUNCTIONED W A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P724696 (CAN) EN ROUTE ELECTRICAL SMELL IN FORWARD GALLEY, GALLEY POWER TURNED OFF BURN SMELL PERSISTED, EMERGENCY DECLARED AND AIRCRAFT LANDED. OVEN REMOVED AND ROUTED FOR REPAIR. NEW OVEN INSTALLED AND RUN FOR ONE HOUR AND NO SMELL. 2 L 7 4 4F 4 F RT A20WE E24NE 1999101500553 19991015 00553 NE 1999 10 15 CA990927083 2 19990802 A 7200 BEARING BOEING 767 767333 NM PWA 4060 PW4060 52119 NE RT ENGINE LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P724730 P724730 (CAN) ON TAKEOFF, SMOKE DETECTED IN CENTER LAV MS2 ACTIVATED, ELECTRICAL SMELL REPORTED NEAR MIDDLE GALLEY, BUSSES TURNE D OFF, SMELL DISSIPATED. CHECKED FOR ELECTRICAL SMELL WHILE PACKS AND RECYCLING FAN RUNNING, NO SMELL. RIGHT ENGINE BE ARING LEAKING ENGINE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 1999101500554 19991015 00554 NM 1999 10 15 CA990927084 1 19990905 A 2780 ECU BOEING 767 767275 1385155 NM PWA JT9 JT9D7R4D 52054 NE SLATS FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA P709606 (CAN) AFTER TAKEOFF, LEADING EDGE SLAT ASSYMETRY CAUTION CAME ON, QRH PROCEDURE CARRIED OUT. FLAP SLAT ELECTRONIC UNIT REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999101500555 19991015 00555 WP 1999 10 15 CA990927085 1 19990819 A 5330 PANEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P656999D (CAN) LEFT TRAPEZOIDAL PANEL FLANGE CRACKED ALONG FORWARD UPPER HORIZONTAL OUTER FLANGE. REPAIRED. 2 L 7 2 4F 4 F A6WE E2EA 1999101500556 19991015 00556 NM 1999 10 15 CA990927088 1 19990626 A 5610 WINDSHIELD AIRBUS A319 A319114 NM COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA (CAN) COPILOT'S WINDSHIELD OUTER PLY CRACKED.....REPLACED. 2 L 7 2 4F RT A28NM 1999101500557 19991015 00557 EU 1999 10 15 CA990927089 1 19990904 A 2611 SMOKE DETECTOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE E/E BAY MALFUNCTIONED W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA 731937 (CAN) AVIONIC BAY SMOKE INDICATION WITH NO OBSERVED SMOKE. NO FAULT FOUND. 2 L 7 2 4F 4 F RT A28NM E29NE 1999101500558 19991015 00558 EU 1999 10 15 CA990927090 1 19990829 A 2913 PUMP AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE HYDRAULIC SYS FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 731358 (CAN) BLUE SYSTEM HYDRAULIC FAILURE DUE TO LOSS OF PRESSURE. BLUE HYDRAULIC SYSTEM PUMP REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999101500559 19991015 00559 NM 1999 10 15 CA991004001 1 19990913 A 3242 68728 SEAL BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE ASSY FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 678 0929 PCE120658 851115 (CAN) DURING PRE-FLIGHT, THE FLIGHT CREW NOTICED A FLUID LEAK FROM THE NR 3 BRAKE ASSEMBLY. TEAR-DOWN OF THE BRAKE ASSE MBLY REVEALED A PISTON SEAL BACK-UP RING FOLDED OVER THE PISTON WHICH CAUSED THE O-RING TO FAIL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500560 19991015 00560 NM 1999 10 15 CA991004002 1 19990912 A 3242 68728 SEAL BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE ASSY FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1349 1773 120854 890709 (CAN) DURING INSPECTION, MAINTENANCE NOTICED A FLUID LEAK FROM THE NR 1 BRAKE ASSEMBLY. TEAR-DOWN OF THE BRAKE ASSEMBLY REVEALED A PISTON SEAL BACK-UP RING FOLDED OVER THE PISTON WHICH CAUSED THE O-RING TO FAIL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500561 19991015 00561 NM 1999 10 15 CA991004004 1 19990914 A 3242 68728 SEAL BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE ASSY FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 232 1777 120373 870601 (CAN) DURING PRE-FLIGHT, THE FLIGHT CREW NOTICED A FLUID LEAK FROM THE NR 2 BRAKE ASSEMBLY. TEAR-DOWN OF THE BRAKE ASSE MBLY REVEALED A PISTON SEAL BACK-UP RING FOLDED OVER THE PISTON WHICH CAUSED THE O-RING TO FAIL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500562 19991015 00562 EA 1999 10 15 CA991004005 1 19990908 A 3510 90070003659 OXYGEN MASK DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE COCKPIT LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 14012 38 S1467 123116 900837 (CAN) LOW TIME OXYGEN MASK INSTALLED IN-FLIGHT, CREW POSITION FOUND TO BE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500563 19991015 00563 EA 1999 10 15 CA991004006 1 19990919 A 2150 78279016 ACM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CABIN SEIZED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 24594 5157 123116 900837 (CAN) DURING FLIGHT,THE CREW NOTICED THAT THEY COULD NOT LOWER THE FLIGHT COMPARTMENT TEMPERATURE. MAINTENANCE TRACED T HE PROBLEM TO A SEIZED ACM. THE ACM, HEAT EXCHANGER, AND CONDENSER/MIXER WERE REPLACED AND THE AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500564 19991015 00564 NM 1999 10 15 CA991004007 1 19990914 A 2910 NAS161210 O-RING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120229 870537 (CAN) DURING MAINTENANCE, A HYDRAULIC FLUID LEAK WAS NOTED ON THE NR 1 HYDRAULIC PRESSURE MANIFOLD. ADAPTER O-RING WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500565 19991015 00565 EA 1999 10 15 CA991004009 1 19990913 A 3350 6104781 POWER SUPPLY DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CABIN INOPERATIVE W K NONE L NO TEST IN INSP/MAINT 1 CA 5563 209 689 123113 901009 (CAN) DURING MAINTENANCE, TWO FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE TRACED THE PROBLEM TO AN EME RGENCY LIGHTING POWER SUPPLY (3352-PS2). 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500566 19991015 00566 EA 1999 10 15 CA991004011 1 19990906 A 2120 82110032011 SHROUDED PIPE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BLEED AIR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 19228 123133 920528 (CAN) DURING MAINTENANCE, A SHROUDED BLEED AIR PIPE WAS FOUND TO BE LEAKING. THE PIPE WAS REPLACED WITH A POST MOD 8/26 13 PIPE ASSY, PN 16032-511. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999101500567 19991015 00567 EU 1999 10 15 CA991004015 1 19990913 A 5270 6981005 HARNESS ASSY BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE PASSENGER DOOR OPEN W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA LF05464A (CAN) MAIN PASSENGER DOOR OPEN INDICATION WITH DOOR CLOSED. INVESTIGATION REVEALED THAT THE CIRCUIT WAS FAULTY. WIRING LOOM REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500568 19991015 00568 EU 1999 10 15 CA991004016 1 19990814 A 7603 188949 CABLE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 ENGINE STICKING W O OTHER O OTHER CR CRUISE 1 CA LF05542A LF05542A (CAN) NR 4 ENGINE POWER LEVER STIFF AT ALL TIMES. ENGINE LOWER TELEFLEX CABLE REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999101500569 19991015 00569 WP 1999 10 15 CA991004020 1 19990920 A 3610 8986263 VALVE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE ENGINE FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 CA 59175 18315 517617 (CAN) ON CLIMB, NR 3 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED, INDICATED 90 PSI AND 220 DEGREE TEMPERATURE. ACCOMPLISH ED CHECK LIST. THROTTLE BACK NR 3 TO BRING PRESSURE AND TEMP BACK. ENGINE PRESSURE VALVE REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1999101500570 19991015 00570 CE 1999 10 15 CA991004029 1 19990916 A 5740 351150583 FITTING BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE50747 BUA21085 (CAN) ON SCHEDULED INSPECTION, INDICATIONS WERE PRESENT WHEN DOING LEVEL 2 LPI. FITTING REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999101500571 19991015 00571 CE 1999 10 15 CA991004030 1 19990917 A 5740 351150595 FITTING BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL WING DAMAGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA PCE50747 BUA21085 (CAN) FITTING REPLACED DUE TO EXCESSIVE TOOL DAMAGE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999101500572 19991015 00572 EA 1999 10 15 CA991004045 1 19990927 A 7931 ENGINE GE CF343B1 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) LOW OIL PRESSURE EXPERIENCED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999101500573 19991015 00573 EA 1999 10 15 CA991004046 1 19990927 A 7931 ENGINE GE CF343B1 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 FAILED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) LOW OIL PRESSURE REPORTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999101500574 19991015 00574 NE 1999 10 15 CA991004048 2 19990927 A 7200 ENGINE GE CF343B1 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE LEFT FAILED W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION AP APPROACH 1 CA (CAN) REPORT FROM COMAIR, HIGH VIBRATION. 2 L 7 2 4F 4 F RT A21EA E15NE 1999101500575 19991015 00575 NE 1999 10 15 CA991004049 2 19990927 A 7200 ENGINE GE CF343B1 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 VIBRATION W D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 CA (CAN) HIGH VIBRATIONS REPORTED BY COMAIR. 2 L 7 2 4F 4 F RT A21EA E15NE 1999101500577 19991015 00577 CE 1999 10 15 CA991004052 1 19990913 A 2710 05232182 ROD CESSNA 172 172K 2072430 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160DTM GL LT AILERON BROKEN W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA 8671 L3616627A 729978 (CAN) DURING FLIGHT, A STUDENT PILOT EXPERIENCED LOSS OF CONTROL OF THE AIRCRAFT. TAKING CONTROL, THE INSTRUCTOR NOTICE D THAT THE LEFT AILERON FAILED TO RESPOND TO CONTROL WHEEL INPUT. THE INSTRUCTOR LANDED THE AIRCRAFT SAFELY. MAINTENAN CE DETERMINED THAT THE LEFT AILERON PUSH-PULL ROD HAD FRACTURED AT THE FORWARD THREADED END. THE FAILED PUSH-PULL ROD W AS REPLACED WITH A NEW PART. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999101500578 19991015 00578 CE 1999 10 15 CA991004053 1 19990918 A 3340 S21605 SWITCH CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA MCAULY 1A103 1A103TCM GL COCKPIT BURNT W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA L2029915 RJC015 (CAN) WHILE IN THE CIRCUIT WITH THE LANDING LIGHT SELECTED ON, THE PILOT NOTICED SMOKE AND FUMES IN THE COCKPIT, DECLARE D AN EMERGENCY AND LANDED THE AIRCRAFT. MAINTENANCE TRACED THE PROBLEM TO AN OVERHEATED LANDING LIGHT SWITCH AND REPLA CED THE SWITCH. 1 H 7 1 3O 3 O NT 3A19 E223 5 N P50GL 1999101500580 19991015 00580 WP 1999 10 15 EIA990152 1 19990316 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 786 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, THE MAIN CABIN LEFT SEAT TRACK ATTACH POINT WAS FOUND TO HAVE HEAVY CORROSION AT STATION 786 APPRO X 21 INCHES FROM CENTER. REPAIRED SEAT TRACK AS REQUIRED PER ECRA 915-53-045-2. (M) 2 L 7 2 4F A6WE 1999101500581 19991015 00581 WP 1999 10 15 EIA990151 1 19990311 A 5312 T-CAP BULKHEAD DOUG DC9 DC915F 3022037 WP CARGO COMPT CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, THE AFT PIT AFT BULKHEAD LOWER T-CAP WAS FOUND TO HAVE EXFOLIATION CORROSION. LOWER T-CAP BLENDED . AREA FOUND OUT OF LIMITER PER SRM 53-01 PAGE 6. ORIGINAL MATERIAL IS 7075-T6 511. 125 TEE ANGLE AND REPAIRED MATERI AL IS 7075-T6.065, TWO DOUBLER PO 199241 PER SRM 53-01 PAGE 10. ALODINED AND PRIMED TWO DOUBLERS PER SRM 51-30-2 PAGE 1 6-20. INSTALLED DOUBLER 7075-T6.063 PER SRM 51-30-2 PAGE 1-14. (M) 2 L 7 2 4F A6WE 1999101500582 19991015 00582 WP 1999 10 15 EIA990150 1 19990309 A 5312 39253891 BULKHEAD PLATE DOUG DC9 DC915F 3022037 WP BS 840 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, THE MAIN CABIN AFT PRESSURE BULKHEAD AT STATION 840, LEFT SIDE OF DOOR JAMB, LOWER PLATE WAS FOUND TO HAVE HEAVY CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER DC-9 SRM 51-110-3 PAGE 1-36 AND 53-01 FIG 1-4 . DRILLED NEW GUSSET UP PER DC-9 SRM 51-10-4 PAGE 1-2. ALODINE GUSSET PER DC-9 SRM 51-10-3 PAGE 18. PRIMED GUSSET PER DC-9 51-10-3 PAGE 16. INSTALLED NEW GUSSET PER DC-9 SRM 51-30-5 PAGE 1-30 FIG 1-17. (M) 2 L 7 2 4F A6WE 1999101500583 19991015 00583 WP 1999 10 15 EIA990149 1 19990329 A 5720 FITTING DOUG DC9 DC915F 3022037 WP LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHEC, THE LEFT WING OUTBOARD TRAILING EDGE CONE WAS FOUND TO HAVE A CRACK IN THE FITTING. REMOVED AND RE PLACED PER DC-9 SRM 51-10-1 PAGE 4-6. INSTALLED FITTING AND WEB AT STATION 164 PER 51-30-2 PAGE 1-14. (M) 2 L 7 2 4F A6WE 1999101500584 19991015 00584 WP 1999 10 15 EIA990148 1 19990329 A 5712 RIB DOUG DC9 DC915F 3022037 WP WS 136 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, THE LEFT WING INBOARD AT ABOUT STATION 136 REAR WING RIB WAS FOUND DAMAGED. REMOVED DAMAGED RIB A T STATION 136 PER SRM 51-10-4 PAGE 1-4. REMOVED ATTACHMENT FROM OL RIB PER SRM 51-30-2 PAGE 1-14 FIG 1-23. MATERIAL ID FOR L-ANGLES (2) AND FILLER (1) CHEM TEST FAA-AC43.4 PARAGRAPH 618D PAGE 131. MEASURED THICKNESS PER EAC93-0106 DIAL C ALIPER OF L-ANGLES AND FILLER. FABRICATED ANGLES AND FILLER PER SRM 51-10-4 PAGE 1-18. ALODINED PER 51-10-3 PAGE 18. P RIMED PER 51-10-3 PAGE 1-18. ASSEMBLED PER 51-30-1 PAGE 1 FIG 1-3 PER 51-30-2 PAGE 1-14 FIG 1-23. (M) 2 L 7 2 4F A6WE 1999101500585 19991015 00585 WP 1999 10 15 EIA990147 1 19990201 A 5320 ANGLE DOUG DC9 DC915F 3022037 WP BS 776 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, STATION 776 APPROX 21 INCH FROM CENTER LEFT SIDE, A PREVIOUS REPAIR WAS FOUND TO HAVE CORROSION GO ING BETWEEN THE ANGLES. FABRICATED FILLER ANGLE AND SPLICE ANGLE PER ECRA 915-53-44-2. LOCATED HOLE AND DEBURRED PER E CRA 915-53-44-2. ALODINED PER SRM 51-10-3 PAGE 18. PRIMERED PER SRM 51-10-3 PAGE 18. (M) 2 L 7 2 4F A6WE 1999101500586 19991015 00586 WP 1999 10 15 EIA990146 1 19990210 A 5312 BULKHEAD CHORD DOUG DC9 DC915F 3022037 WP CARGO COMPT CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, THE FORWARD PIT, AFT BULKHEAD, LOWER CHORD BETWEEN S28L THROUGH S29R WAS FOUND TO HAVE CORROSION, HEAVY IN SOME SPOTS. REPAIRED PER ECRA 915-53-039-2 REV A. (M) 2 L 7 2 4F A6WE 1999101500587 19991015 00587 WP 1999 10 15 EIAA990145 1 19990209 A 5320 JAMB DOUG DC9 DC915F 3022037 WP CARGO DOORWAY CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, THE FORWARD LOWER CARGO DOOR JAMB EXT SKIN AND IN BETWEEN LAYERS FROM FORWARD FRAME TO AFT FRAME C UTOUT WAS FOUND TO HAVE CORROSION. REPAIRED PER ECRA 915-53-038-2. (M) 2 L 7 2 4F A6WE 1999101500588 19991015 00588 WP 1999 10 15 EIA990144 1 19990505 A 5313 LONGERON DOUG DC9 DC915F 3022037 WP BS 880 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 EAC - DURIGN C-CHECK, LONGERON 27R WAS FOUND TO HAVE CORROSION AT STATION 880. REMOVED 27R LONGERON PER SRM 51-30-2 PAG E 1-14. REMOVED CORROSION, FOUND CRACK ON CAP ANGLE, OUT OF LIMITS PER SRM 53-01 PAGE 4-6. INSTALLED NEW CAP ANGLE. ( M) 2 L 7 2 4F A6WE 1999101500589 19991015 00589 NM 1999 10 15 EIA990141 1 19990422 A 5320 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 HKG - DURING C-CHECK, A CRACK WAS FOUND AT RIGHT NR 1 MED LOWER HINGE CUTOUT LOWER CORNER, SKIN CRACK .25 INCH - .375 IN CH APPROX, RUNNING UNDERNEATH THE EXTERNAL DOUBLER. CRACK END CAN'T BE LOCATED. CRACK STOP DRILLED PER SRM 53-30-02, R EPAIRED IAW HXRS 52-11-33. (M) 2 L 7 4 4F A20WE 1999101500590 19991015 00590 NM 1999 10 15 EIA990133 1 19990529 A 5712 65B0807721 RIB BOEING 747 747SR46 NM RT WING GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 21033 MZJ - DURING C-CHECK, THE RIGHT WING NR 15 LEADING EDGE INBOARD SUPPORT ARM UPPER END RIBS WERE FOUND WORN AND GOUGED. S USPECTED CAUSE IS IMPROPER BUSHING INSTALLATION ON INBOARD BEARING. REPAIRED PER ECRA NR 478-57-091-2. (M) 2 L 7 4 4F A20WE 1999101500591 19991015 00591 NM 1999 10 15 EIA990131 1 19990529 A 5753 SKIN BOEING 747 747SR46 NM RT TE FLAP MISDRILLED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 21033 MZJ - DURING C-CHECK, THE RIGHT OUTBOARD MIDFLAP, OUTBOARD END, UPPER SURFACE WAS FOUND TO HAVE 2 SCREWS MISSING. INSPE CTION REVEALED OVERSIZED FASTENER HOLES. REPAIRED PER ECRA NR 478-57-094-2, PART A/B COMPLETED, PART C REQUIRING REOCCU RING INSPECTION AT NOT MORE THAN 200 FLIGHTS. (M) 2 L 7 4 4F A20WE 1999101500592 19991015 00592 NM 1999 10 15 EIAA990160 1 19990212 A 5320 OUTLET BOEING 747 747121 1384871 NM BS 570 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK AT STATION 570, EQUIPMENT COOLING OUTLET, 3 FASTENER HOLED WERE FOUND CRACKED. REPAIRED, REFERENCE THE F OLLOWING DOCUMENTS. 1) NRC 7192, 2) CWS 123457, 3) COMP WORK PROCESS CARD Z52E013 4) BOEING TELEX EVR-HKG-99-0023 RE 2/ 9/99, 1024 TE 2/18/99 8009 RE, 5) HAECO R53-11-34043. (M) 2 L 7 4 4F A20WE 1999101500593 19991015 00593 NM 1999 10 15 EIA990159 1 19990207 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 960-980 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK AT M/D, FROM STATION 960 TO STATIO N980, STRINGER 7R WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M) 2 L 7 4 4F A20WE 1999101500594 19991015 00594 NM 1999 10 15 EIA990157 1 19990215 A 5313 BAC1498145 STRINGER BOEING 747 747121 1384871 NM BS 1959 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK ON M/D AT BS 1959, STRINGER 3R END WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M) 2 L 7 4 4F A20WE 1999101500595 19991015 00595 NM 1999 10 15 EIA990158 1 19990207 A 5320 65B072792 SPLICE BOEING 747 747121 1384871 NM BS 1000 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK ON M/D AT STATION 1000, STRINGER 7R ATTACH SPLICE WAS FOUND CRACKED. INSTALLED NEW SPLICE. (M) 2 L 7 4 4F A20WE 1999101500596 19991015 00596 NM 1999 10 15 EIA990156 1 19990215 A 5313 BAC1498145 STRINGER BOEING 747 747121 1384871 NM BS 1959 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK ON M/D AT STATION 1959 AT STRINGER 2L, END CRACKED. INSTALLED NEW STRINGER. (M) 2 L 7 4 4F A20WE 1999101500597 19991015 00597 NM 1999 10 15 EIA990155 1 19990301 A 5313 BAC1493522 STRINGER BOEING 747 747121 1384871 NM BS 1485 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK ON M/D AT BS 1485, STRINGER 15R WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M) 2 L 7 4 4F A20WE 1999101500598 19991015 00598 NM 1999 10 15 EIA990154 1 19990215 A 5313 BAC1498145 STRINGER BOEING 747 747121 1384871 NM BS 1959 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK ON M/D AT BS 1959 STRINGER 4R, STRINGER END WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M) 2 L 7 4 4F A20WE 1999101500599 19991015 00599 NM 1999 10 15 EIA990153 1 19990215 A 5313 BAC1498145 STRINGER BOEING 747 747121 1384871 NM BS 1959 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK ON M/D AT BS 1959 S3L, STRINGER END WAS FOUND CRACKED. INSTALLED NEW STRINGER. (M) 2 L 7 4 4F A20WE 1999101500600 19991015 00600 NM 1999 10 15 EIA990170 1 19990312 A 5311 FRAME BOEING 747 747121 1384871 NM BS 340 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, THE BS 340 FRAME WEB ON BOTH LEFT AND RIGHT STRINGER 24A WAS FOUND CRACKED. REPAIRED PER HAECO RE PAIR SCHEME NR R-53-12-34025. (M) 2 L 7 4 4F A20WE 1999101500601 19991015 00601 NM 1999 10 15 EIA990169 1 19990209 A 5311 FRAME BOEING 747 747121 1384871 NM BS 380 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK, THE S25L FRAME WAS FOUND CRACKED AT STATION 380. REPLACED WITH NEW. (M) 2 L 7 4 4F A20WE 1999101500602 19991015 00602 NM 1999 10 15 EIA990168 1 19990209 A 5312 BULKHEAD BOEING 747 747121 1384871 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK, THE LEFT BS 1480 BULKHEAD AND STRINGER INTERFACE WERE FOUND CRACKED AT STRINGER 34. REPAIRED BULKHEAD A ND STRINGER INTERFACE. (M) 2 L 7 4 4F A20WE 1999101500603 19991015 00603 NM 1999 10 15 EIA990167 1 19990312 A 5320 SPLICE BOEING 747 747121 1384871 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK, THE FRAME SPLICE WEB AT BS 1265 LBL 120 WAS FOUND CRACKED. REPAIRED FRAME SPLICE WEB. (M) 2 L 7 4 4F A20WE 1999101500604 19991015 00604 NM 1999 10 15 EIA990165 1 19990312 A 5311 65B103656 FRAME BOEING 747 747121 1384871 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, THE M/D NR 3 DOOR FORWARD FRAME CHORD AT BS 1265, RBL 120 WAS FOUND CRACKED. REPAIRED NR 3 DOOR F ORWARD FRAME CHORD. (M) 2 L 7 4 4F A20WE 1999101500605 19991015 00605 NM 1999 10 15 EIA990166 1 19990312 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK, THE RIGHT FRAME, INBOARD CHORD ATTACH WEB WAS FOUND CRACKED AT BS 1265. REPLACED WITH NEW. (M) 2 L 7 4 4F A20WE 1999101500606 19991015 00606 NM 1999 10 15 EIA990164 1 19990311 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1485 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, THE M/D S17R AT BS 1485 WAS FOUND CRACKED. REPAIRED S17R. (M) 2 L 7 4 4F A20WE 1999101500607 19991015 00607 NM 1999 10 15 EIA990163 1 19990311 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1478 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 HKG - DURING C-CHECK, THE M/D BS 1478 STRINGER 6L, STRINGER END WAS FOUND CRACKED. REPAIRED CRACKED AREA. (M) 2 L 7 4 4F A20WE 1999101500608 19991015 00608 NM 1999 10 15 EIA990162 1 19990205 A 5320 TIE BOEING 747 747121 1384871 NM BS 880 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 DURING C-CHECK, THE M/D BS 880 STRINGER 9R TENSION TIE WAS FOUND CRACKED. REPLACED WITH NEW. (M) 2 L 7 4 4F A20WE 1999101500614 19991015 00614 NM 1999 10 15 EIA990210 1 19990629 A 5311 FRAME BOEING 747 747132 1384882 NM BS 960 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, BS 960 FRAME CRACKED BETWEEN STRINGER 5R AND 6R. REPAIRED PER SRM 53-10-04 FIG 54. (M) 2 L 7 4 4F A20WE 1999101500615 19991015 00615 NM 1999 10 15 EIA990209 1 19990629 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 956 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D STRINGER 9L CRACKED AT BS 956. REPAIRED PER SRM 53-10-03 FIG 4. (M) 2 L 7 4 4F A20WE 1999101500616 19991015 00616 NM 1999 10 15 EIA990208 1 19990629 A 5320 CHANNEL BOEING 747 747132 1384882 NM BS 840 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 840 LEFT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SB 747-53-2371 FIG 3 AD T ELEX EVR-HKG-99-0101RE/0092TE. (M) 2 L 7 4 4F A20WE 1999101500617 19991015 00617 NM 1999 10 15 EIA990207 1 19990629 A 5320 CHANNEL BOEING 747 747132 1384882 NM BS 900 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 900 RT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SB 747-53-2371 FIG 3 AND TE LEX EVR-HKG-99-0101RE/0092TE. (M) 2 L 7 4 4F A20WE 1999101500618 19991015 00618 NM 1999 10 15 EIA990206 1 19990629 A 5320 CHANNEL BOEING 747 747132 1384882 NM BS 920 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 920 RT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SB 747-53-2371 FIG 3 AND TE LEX EVR-HKG-99-0101RE/0092TE. (M) 2 L 7 4 4F A20WE 1999101500619 19991015 00619 NM 1999 10 15 EIA990205 1 19990629 A 5320 CHANNEL BOEING 747 747132 1384882 NM BS 940 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 940 RT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SB 747-53-2371 FIG 3 AND TE LEX EVR-HKG-99-0101RE/0092TE. (M) 2 L 7 4 4F A20WE 1999101500620 19991015 00620 NM 1999 10 15 EIA990203 1 19990629 A 5320 CHANNEL BOEING 747 747132 1384882 NM BS 900 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 900 LEFT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SB 747-53-2371 FIG 3 AND TELEX EVR-HKG-99-0101RE/0092TE. (M) 2 L 7 4 4F A20WE 1999101500621 19991015 00621 NM 1999 10 15 EIA990204 1 19990629 A 5320 CHANNEL BOEING 747 747132 1384882 NM BS 880 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 880 LEFT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SB 747-53-2371 FIG 3 AND TELEX EVR-HKG-99-010RE/0092TE. (M) 2 L 7 4 4F A20WE 1999101500622 19991015 00622 NM 1999 10 15 EIA990202 1 19990629 A 5320 TIE CLIP BOEING 747 747132 1384882 NM BS 2220 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURNIG C/D CHECK, CABIN FRAME TIE CLIP CRACKED AT BS 2220 AT STRINGER 20L. FRAME TIE CLIP REPLACED IAW SRM 51-10- 01. (M) 2 L 7 4 4F A20WE 1999101500623 19991015 00623 NM 1999 10 15 EIA990201 1 19990626 A 5400 FITTING BOEING 747 747132 1384882 NM NR 2 PYLON CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, NR 2 PYLON DIAGONAL BRACE AFT WING FITTING HAS 2 BOLT HOLES WITH CORROSION IN BORES. NR 2 PYLON DIAGONAL BRACE AFT WING FITTING BOLT HOLE CORROSION REMOVED BY OVERSIZING. HOLE SIZES TO MAX LIMIT PER SB 54-2159. (M ) 2 L 7 4 4F A20WE 1999101500624 19991015 00624 NM 1999 10 15 EIA990200 1 19990626 A 5320 SHEAR TIE BOEING 747 747132 1384882 NM BS 780 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 780 STRINER 0 TO STRINGER 1L, FRAME SHEAR TIE CRACKED. SHEAR TIE REPAIRED PER SRM 53-10- 04 FIG 4. (M) 2 L 7 4 4F A20WE 1999101500625 19991015 00625 NM 1999 10 15 EIA990199 1 19990626 A 5400 PAN BOEING 747 747132 1384882 NM NR 1 PYLON WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, NR 1 PYLON FORWARD STRUT CLOSURE PAN LEFT AND RIGHT SKIN WORN. STRUT CLOSURE PAN REPAIRED PER R S-R-71-90-34116, 8110-3. (M) 2 L 7 4 4F A20WE 1999101500626 19991015 00626 NM 1999 10 15 EIA990198 1 19990625 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1460 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, M/D BS 1460 AT STRINGER 12L, UPPER SPLICE AREA OF FRAME, FRAME IS CRACKED. REPAIRED FRAME IAW S RM 53-10-04 FIG 31. (M) 2 L 7 4 4F A20WE 1999101500627 19991015 00627 NM 1999 10 15 EIA990197 1 19990625 A 5720 65B010201137 FITTING BOEING 747 747132 1384882 NM WS 670 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, LEFT WING WS 670 FRONT SPAR VERTICAL SUPPORT FITTING HAS 2 FASTENER HOLES CRACKED. RIB FITTING REPLACED IAW SB 747-57A2273 FIG 5. (M) 2 L 7 4 4F A20WE 1999101500628 19991015 00628 NM 1999 10 15 EIA990196 1 19990625 A 5320 WEB BOEING 747 747132 1384882 NM BS 328 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 93105 19896 HKG - DURING C/D CHECK, RT NOSE TUNNEL AT BS 328 WL 180, VERTICAL BEAM WEB CRACKED. REPAIRED WEB IAW SRM 51-40-02. (M) 2 L 7 4 4F A20WE 1999101500629 19991015 00629 NM 1999 10 15 TSAA9933434 1 19990914 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 2 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1999101500630 19991015 00630 1999 10 15 ARWA990905 4 19990926 A 3441 278262 BATTERY LKHEED 1011 1011385115 5265015 WP INS SYSTEM DISCHARGED A ARWA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION TO TAKEOFF 1 SO 19 306GB 7503357 193U1138 MIA - FLT 707 - ON TAKEOFF, NR 2 INS INOPERATIVE BATTERY WARNING AND ISU WARNING LIGHT ON. DUMPED 25.2K FUEL AND RETURN ED TO MIA. REMOVED AND REPLACED NR 2 INS BATTERY. SYSTEM CHECKED NORMAL IAW MM 34-40-0. (M) 2 L 7 3 4F A23WE 1999101500631 19991015 00631 WP 1999 10 15 AALA991360 1 19990826 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FS 160 LONG 4 LEFT CRACK IN LONGERON AT FRAME ATTACHMENT AREA. INSTALLED NEW LONGERON AND HAT SPLICE STATION 160 AS PER SRM 53-02. (M) 2 L 7 2 4F A6WE 1999101500632 19991015 00632 WP 1999 10 15 AALA991359 1 19990827 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND LONGERON 3L CRACKED INBOARD SIDE FS 160. INSTALLED NEW SECTION OF LONGERON AND SPLICE IAW SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999101500633 19991015 00633 WP 1999 10 15 AALA991358 1 19990909 A 5320 5912270502 POST DOUG DC9 DC982 3022082 WP BS 101 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - WINDSHIELD POST BETWEEN RT WINDSHIELD AND RIGHT CLEARVIEW HAS TOP ATTACH HOLE DAMAGED. REMOVED DAMAGED POST AND I NSTALLED NEW ONE PER SRM 51-01 1C. (M) 2 L 7 2 4F A6WE 1999101500634 19991015 00634 WP 1999 10 15 AALA991357 1 19990830 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 378 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FUSELAGE SKIN GOUGED AND DAMAGED FROM LONGERON 26R AND 29R AT STATION 378. INSTALLED DOUBLER PER SRM 53-04 PAGE 3 7 FIG 12B. (M) 2 L 7 2 4F A6WE 1999101500635 19991015 00635 EU 1999 10 15 AALA991241 1 19990818 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 34078 615 TUL - FOUND CORROSION ON TOP OF FLOOR SUPPORT FROM FRAME 71.5 TO 73.5 SUPPORT LEFT OUTBOARD OF CENTER. REMOVED AND REPL ACED FLOOR SUPPORT BEAM FROM FRAME 72-75 AS PER SRM 51-74. (M) 2 L 7 2 4F RT A35EU 1999101500636 19991015 00636 EU 1999 10 15 AALA991259 1 19990820 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 34078 615 TUL - FOUND UPPER SURFACE CORRODED IN TWO AREAS BEYOND LIMITS. SPLICED IN NEW SECTION PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1999101500637 19991015 00637 WP 1999 10 15 USAAD99136 1 19990919 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN CHAFED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927VJ 48154 PHL - THE LAST FOUR SEAT ROWS AND THE ENTIRE TAIL SECTION EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPAIRED A CHA FFED WIRE AT SEAT ASSEMBLY 21 E/F. (M) 2 L 7 2 4F A6WE 1999101500638 19991015 00638 WP 1999 10 15 USAAD99137 1 19990921 A 3350 40882201 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 983VJ 48159 IND - THE FORWARD ENTRY AREA AND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE F ORWARD ENTRY AREA AND FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999101500639 19991015 00639 WP 1999 10 15 99ZZZM707 1 19990921 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 983VJ 48159 IND - THE FORWARD ENTRY AREA AND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE F ORWARD ENTRY AREA AND FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999101500640 19991015 00640 WP 1999 10 15 USAAD99129 1 19990909 A 3260 0331881002 SOCKET DOUG DC9 DC931 3022065 WP LANDING GEAR FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 932VJ 47189 PIT-CMH - FLT 933 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THE LEFT GEAR GREEN LIGHT REMAINED ILLUMINATED. THE AIRCR AFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT LANDING GEAR GREEN LIGHT INDICATIO N SOCKET. (M) 2 L 7 2 4F A6WE 1999101500641 19991015 00641 WP 1999 10 15 USAAD99131 1 19990913 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 923VJ 48143 PIT - THE SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999101500642 19991015 00642 NM 1999 10 15 USAA099902 1 19990912 A 3350 110047 CHARGER BOEING 727 727225 1384077 NM L1/L2 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS 20447 FLT 6141 - BOS-LGA - EMERGENCY EXIT SIGN AT L-1 AND R-1 DOORS INOPERATIVE. REPLACED BATTERY PACK CHARGER, CHECKS OK. ( M) 2 L 7 3 4F A3WE 1999101500643 19991015 00643 EU 1999 10 15 USAAF99046 1 19990919 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 856US 11286 IND - FOUND AFT SECTION OF LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. (M) 2 L 7 2 4F RT 1999101500644 19991015 00644 WP 1999 10 15 USAAD99138 1 19990923 A 7711 AN8153D UNION DOUG DC9 DC931 3022065 WP LT ENGINE LOOSE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 927VJ 48154 PHL-ATL - FLT 1243 - DURING CLIMB-OUT, THE LEFT ENGINE REQUIRED HIGHER THROTTLE SETTINGS TO MAINTAIN EQUAL EPR READINGS. THE HIGHER THE ALTITUDE THE GREATER THE THROTTLE SPREAD BETWEEN THE TWO ENGINES. THE AIRCRAFT RETURNED TO THE FIELD A ND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED THE UNION AT THE PT2 FLEX HOSE. (M) 2 L 7 2 4F A6WE 1999101500645 19991015 00645 NM 1999 10 15 UIEA99060 1 19990831 A 5743 BACB30M77T20 BOLT BOEING 747 7472D7B 1384803 NM RT WING FAILED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 73059 21784 RT WING GEAR FORWARD TRUNNION OUTBOARD SIDE SUPPORT FITTING HAS SHEARED BOLT ON OUTBOARD UPPER ATTACHMENT. INSPECTED AR EA, FOUND NO DAMAGE. REPLACED BOLT PER DRAWING 65B010222 FR 2 10-2480. REPLACED SHEARED BOLT WITH P/N BACB30US7K20. ( M) 2 L 7 4 4F RT A20WE 1999101500646 19991015 00646 NM 1999 10 15 UIEA99061 1 19990831 A 5320 BACB30M77T20 BOLT BOEING 747 7472D7B 1384803 NM BS 2360 FAILED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 73059 21784 AFT PRESSURE BULKHEAD HAS SHEARED BOLT AT STRINGER 14 RT SIDE. INSPECTED AREA FOUND ON DEFECTS. REPLACED BOLT. TORQUE D PER MM 20-51-00. (M) 2 L 7 4 4F RT A20WE 1999101500647 19991015 00647 NM 1999 10 15 UIEA99062 1 19990831 A 5320 BACB30MT721 BOLT BOEING 747 7472D7B 1384803 NM BS 1241 FAILED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 73059 21784 BOLTS SHEARED AT BODY STATION 1241 LBL 110 AND LBL 118. INSPECTED AREA, FOUND NO DEFECTS. PERFORMED HFEC INSPECTION PE R D6-7170 51-00-00 PART 6, FOUND NO CRACKS. REPLACED BOLTS. TORQUED BOLTS PER 20-51-00. (M) 2 L 7 4 4F RT A20WE 1999101500648 19991015 00648 NM 1999 10 15 UIEA99063 1 19990831 A 5753 65B155995 DRIVE LINK BOEING 747 747230B 1384889 NM TE FLAPS CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 NR 3 FLAP TRACK MOVEABLE CANOE FAIRING FIXED DRIVE LINK CHAFED, BLENDED OUT DAMAGE AND NDT INSPECTED. SHOT PEENED AND R EPAIRED IAW BOEING TELEX. (M) 2 L 7 4 4F A20WE 1999101500649 19991015 00649 NM 1999 10 15 UIEA99064 1 19990831 A 5411 65B89049383 FRAME BOEING 747 747230B 1384889 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 NR 3 PYLON INTERIOR AFT MOUNT BULKHEAD WEB AFT SIDE AT NAC STATION 286 FOUND WITH CRACK. DAMAGED AREA WAS TRIMMED OUT, NDT INSPECTED, REPAIRED IAW BOEING TELEXS. (M) 2 L 7 4 4F A20WE 1999101500650 19991015 00650 NM 1999 10 15 UIEA99065 1 19990831 A 5400 302U000015 DOUBLER BOEING 747 747230B 1384889 NM NR 1 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 NR 1 PYLON CAP SKIN MOD MO 54-0074 AREA FOUND WITH EXISTING DOUBLER, BULKHEAD FRAME CRACK AT STATION 270. THE CRACKED F RAME FLANGE WAS TRIMMED TO REMOVED DAMAGE, NDT PERFORMED TO VERIFY NO OTHER CRACKS. NEW REPAIR ANGLES AND NEW DOUBLER I NSTALLED IAW BOEING TELEXS. (M) 2 L 7 4 4F A20WE 1999101500651 19991015 00651 NM 1999 10 15 UIEA99066 1 19990831 A 5711 65B12228 SPAR WEB BOEING 747 747230B 1384889 NM WS 1314-1322 CORROSION A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 LEFT WING FRONT SPAR WEB CORRODED BETWEEN FSSO 1314 TO FSSO 1322. TRIMMED OUT CORRODED AREAS, NDT WEB NO CRACK INDICATI ON. REPAIRED IAW BOEING TELEXS. (M) 2 L 7 4 4F A20WE 1999101500652 19991015 00652 NM 1999 10 15 UIEA99067 1 19990831 A 5711 65B172461 SPAR WEB BOEING 747 747230B 1384889 NM WS 385-400 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 LEFT WING MID SPAR AND UPPER CHORD, FASTENER HOLES ELONGATED AND CRACKED. ALSO, EXISTING REPAIR DOUBLER FASTENER HOLE C HIPPED FROM WS 400 TO WS 385. AT 12 HOLE LOCATIONS BETWEEN WS 388 AND 407 OVERSIZE HI-LOCKS WERE INSTALLED AND AT ONE L OCATION SEPARATE FREEZE PLUGS WERE INSTALLED COMMON TO THE WEB AND UPPER SPAR CHORD AND HI-LOCK INSTALLED. AT MSS 400, THE CRACKED HOLE WAS TRIMMED OUT AND A PERMANENT REPAIR WAS INSTALLED IAW BOEING TELEXS. (M) 2 L 7 4 4F A20WE 1999101500653 19991015 00653 NM 1999 10 15 UIEA99069 1 19990831 A 5400 REFMO540097 FITTING BOEING 747 747230B 1384889 NM NR 1/4 PYLONS OVERSIZE A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 NR 1 AND NR 4 PYLONS FOUND FASTENER HOLE SIZE TO EXCEED TOLERANCE PER SB 747-54A2152 IN SPRINGBEAM SUPPORT FITTINGS IN 3 HOLE LOCATIONS. HOLES WERE OVERSIZED, NDT PERFORMED TO VERIFY NO CRACKS. NO INSURANCE CUT WAS PERFORMED AND FASTENERS INSTALLED. THIS IS A TIME LIMITED REPAIR APPROVED AS AN ALTERNATE METHOD OF COMPLIANCE BY BOEING. PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO MARCH 28, 2000. (M) 2 L 7 4 4F A20WE 1999101500654 19991015 00654 NM 1999 10 15 UIEA99070 1 19990831 A 5400 65B741097 STRAP BOEING 747 747230B 1384889 NM NR 4 PYLON CRACKS A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 NR 4 PYLON INTERIOR, LEFT BULKHEAD STRAP AT NAC STATION 286 FOUND CRACKED. REPAIRED IAW BOEING TELEXS, TO BE RE-INSPECT ED EVERY C-CHECK NOT TO EXCEED 18 MONTHS OR 1000 FLTS. (M) 2 L 7 4 4F A20WE 1999101500655 19991015 00655 NM 1999 10 15 UIEA99071 1 19990831 A 5400 65B8910820 STRAP BOEING 747 747230B 1384889 NM PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 NR 1, 2, 3, 4, PYLONS EXTERIOR RIGHT PRE-COOLER EXHAUST CUTOUT FOUND WITH CRACK,AND NR 3 STIFFENER CRACK. REPAIRS CARRI ED OUT IAW BOEING TELEXS AND SB 747-54-2163 R1 AND SB 747-54A2158 R2. THE SB REVS HAVE BEEN APPROVED ALTERNATE METHOD O F COMPLIANCE. (M) 2 L 7 4 4F A20WE 1999101500656 19991015 00656 NM 1999 10 15 UIEA99074 1 19990909 A 5755 65B080996 FITTING BOEING 747 7472D7B 1384803 NM NR 6 SPOILER CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 73059 21784 NR 6 SPOILER SUPPORT FITTING CRACKED AT LOWER LEFT SIDE ATTACHING FLANGE APPROXIMATELY 2 INCHES BETWEEN AND OUT OF SECON D AND THIRD RIVET HOLE. FITTING ATTACHED TO THE AFT SIDE OF WING GEAR AFT SUPPORT BEAM. FITTING REPLACED DURNIG CURREN T C-CHECK AT KLM. (M) 2 L 7 4 4F RT A20WE 1999101500657 19991015 00657 NM 1999 10 15 UIEA99068 1 19990831 A 5711 65B172461 SPAR WEB BOEING 747 747230B 1384889 NM WS 382-411 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 RIGHT WING FUEL TANK INTERIOR WS 382 TO WS 411 MID SPAR AFT UPPER WEB SURFACE FOUND CRACK PROPAGATING FROM EXISTING REPA IR. MID SPAR WEB CRACK AT MSS 400 WAS TRIMMED OUT AND A PERMANENT REPAIR INSTALLED. AT MSS 394 A FREEZE PLUG WAS INSTA LLED COMMON TO THE WEB AND A HI-LOCK WAS INSTALLED AT THE LOCATION IAW BOEING TELEXS. (M) 2 L 7 4 4F A20WE 1999101500658 19991015 00658 NM 1999 10 15 UIEA99073 1 19990831 A 5311 FRAME BOEING 747 747230B 1384889 NM BS 1265 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 FUSELAGE FRAME AT BS 1265 LEFT SIDE FOUND WEB CRACK AND SEVERAL FASTENER HOLES ELONGATED. INTERIM REPAIR IAW BOEING TEL EXS TO BE INSPECTED EVERY 2000 FLIGHTS. (M) 2 L 7 4 4F A20WE 1999101500659 19991015 00659 WP 1999 10 15 USAAD99133 1 19990916 A 3260 SWITCH DOUG DC9 DC931 3022065 WP LANDING GEAR DIRTY A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 918VJ 48138 BUF-DCA - FLT 1263 - DURING LANDING GEAR EXTENSION, ALL THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED WITH NO GREEN LIGH TS. AFTER GEAR WAS RECYCLED, INDICATION WAS NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DUPLICATED PR OBLEM WITH LANDING GEAR HANDLE SWITCH BEFORE RETRACTION CHECK. CLEANED SWITCH AT LANDING GEAR HANDLE AND PERFORMED GEAR RETRACTION CHECK SEVERAL TIMES. SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F A6WE 1999101500660 19991015 00660 WP 1999 10 15 USAAD99130 1 19990912 A 2810 FUEL TANK DOUG DC9 DC931 3022065 WP LT WING LEAKING A USAA K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CR CRUISE 1 EA 19 980VJ 48156 DCA-SDF - FLT 1312 - THE CREW REPORTED A STRONG SMELL OF FUEL DURING FLIGHT. MAINTENANCE REPLACED THE AIR CONDITIONING COALESCER BAGS AND THE SMELL WENT AWAY. THE SMELL WAS REPORTED AGAIN AFTER THE NEXT FLIGHT. THE ENGINES WERE RUN AT AB OVE IDLE AND INSPECTED FOR LEAKS, NO ODOR WAS NOTED AT THAT TIME. TWO FLIGHTS LATER THE ODOR WAS REPORTED AGAIN. MAINT ENANCE FOUND FUEL LEAKING BEHIND A DOUBLE AND PULLEY FITTING ON THE AFT SPAR, UPPER LEFT CORNER IN THE LEFT WHEEL WELL. (M) 2 L 7 2 4F A6WE 1999101500661 19991015 00661 NM 1999 10 15 USAASB99233 1 19990919 A 3260 189929 SENSOR BOEING 737 737401 1384701 NM NLG OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 412US 23881 CLT - FLT 731 - EN ROUTE FROM PHL TO MSY, THE NLG UNSAFE ILLUMINATED AND REMAINED ON. CREW RECYCLED GEAR AT 230 KNOTS B UT LIGHT REMAINED ON. CAPTAIN ACCOMPLISHED VISUAL CHECK AND DETERMINED GEAR WAS STOWED AND DOORS WERE CLOSED. SINCE TH ERE WAS NO MAINTENANCE IN MSY, FLIGHT DIVERTED TO CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAI NTENANCE SHIMMED THE NOSE GEAR DOWNLOCK SENSOR IN ASSOCIATION WITH MM 32--61-21. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999101500662 19991015 00662 WP 1999 10 15 USAA991037 1 19990918 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 628 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 828US 50160 48028 PIT - DURING RON VISIT, FOUND 1 INCH LONG CRACK AT STATION 628 AT LONGERON 30 ON SKIN. INSTALLED INTERNAL TITANIUM DOUB LER PER EA 52938A. (M) 2 L 7 2 4F A6WE 1999101500663 19991015 00663 WP 1999 10 15 USAA991036 1 19990915 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 58.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 819US 47814 48099 PIT - DURING RON, FOUND 1 INCH CRACK IN SKIN WITH EXTERNAL DOUBLER WITHIN 24 INCHES OF AOA VANE AT STATION 58.750, 4 INC HES BELOW FLOOR LINE LEFT SIDE. INSTALLED FLUSH REPAIR PER SRM 53-01 FIG 4 SHT 2. (M) 2 L 7 2 4F A6WE 1999101500664 19991015 00664 WP 1999 10 15 USAA991035 1 19990915 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 58 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 49012 48117 PIT - DURING RON FOUND, .25 INCHES AND .5 INCH CRACK IN SKIN AT STATION 58 LEFT SIDE 5TH AND 6TH RIVETS FROM TOP PRESSUR E B/H. INSTALLED DOUBLER PER SRM 53-31-0 FIG 1, EA 52848. (M) 2 L 7 2 4F A6WE 1999101500665 19991015 00665 WP 1999 10 15 USAA991038 1 19990920 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 58.750 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823US 44133 49142 PIT - DURING RON VISIT, FOUND TWO CRACKS .5 INCH LENGTH IN SKIN AT STATION 58.750 LEFT, 5TH AND 6TH RIVETS BELOW FLOOR L INE. INSTALLED DOUBLER PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F A6WE 1999101500666 19991015 00666 1999 10 15 99ZZZM708 4 19990917 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 192GL 4581 UE192 PILOTS ALTIMETER FLAGGED ON TAKEOFF. REMOVED AND REPLACED ALTIMETER. TESTED OK. (M) 2 L 7 2 4T RT A24CE 1999101500667 19991015 00667 NM 1999 10 15 F3LA99123 1 19990922 A 5522 65C25746132 SKIN BOEING 737 7373M8 1384615 NM RT ELEVATOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 DEN - DURING C-CHECK INSPECTION, REPORTED A .250 INCH HOLE IN THE UPPER SURFACE OF THE RT ELEVATOR. MAINTENANCE REPAIRE D DAMAGED AREA PER EA 27-737-017 AND SRM 51-70-05, FIGURE 10; BALANCED RT ELEVATOR PER SRM 51-60-04; AND REINSTALLED RT ELEVATOR PER B737-300 MM 27-31-11. (M) 2 L 7 2 4F RT A16WE 1999101500668 19991015 00668 NM 1999 10 15 USAASB99215 1 19990831 A 7930 STUD BOEING 737 7373B7 1384580 NM NR 1 ENGINE LOOSE A USAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 394US 23316 DFW - FLT 870 - CAPTAIN REPORTED THAT AFTER TAKEOFF FROM DFW AND CLIMBING THROUGH 17,000 FT, THE NR 1 ENGINE OIL TEMPERA TURE ROSE ABOVE THE RED RADIAL. CREW SHUTDOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT DFW. FLI GHT LANDED WITHOUT FURTHER INCIDENT AND TOWED TO THE GATE BY MAINTENANCE. TOTAL SINGLE ENGINE TIME WAS 16 MINUTES. MA INTENANCE FOUND GROUNDING STUD 16A LOOSE. VERIFIED FLUCTUATIONS AND RISE IN GAUGE. CLEANED AND TIGHTENED STUD AND TERM INAL. RAN ENGINE TO FULL POWER. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999101500669 19991015 00669 NM 1999 10 15 P2EA99278 1 19990823 A 5320 ANGLE BOEING 737 737247 138448D NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SEAT TRACK ANGLE CRACKED AT BS 727, RBL 25 AND WL 203.1. REPAIRED IAW EO COO-3-53-499-99. (M) 2 L 7 2 4F A16WE 1999101500670 19991015 00670 NM 1999 10 15 P2EA99277 1 19990821 A 5320 SPLICE BOEING 737 737247 138448D NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - STRINGER 27L SPLICE CRACKED BETWEEN BS 727 PLUS 10 TO 727A. REPAIRED IAW 5310-06. (M) 2 L 7 2 4F A16WE 1999101500671 19991015 00671 NM 1999 10 15 P2EA99276 1 19990821 A 5754 SKIN BOEING 737 737247 138448D NM LT LE FLAP DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LEFT WING NR 2 KRUEGER FLAP DENTED. REPAIRED IAW EO COO-3-57-511-99. (M) 2 L 7 2 4F A16WE 1999101500672 19991015 00672 NM 1999 10 15 P2EA99273 1 19990917 A 5755 654645123 PANEL BOEING 737 737247 138448D NM NR 5 SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP MA315 19607 FLT 410 - MCI - DURING POST FLIGHT WALK AROUND, MAINTENANCE FOUND NR 5 SPOILER DELAMINATED AT TRAILING EDGE. REPLACED N R 5 SPOILER PANEL PER MM 27-61-11. (M) 2 L 7 2 4F A16WE 1999101500673 19991015 00673 SO 1999 10 15 ASOA99098 1 19990910 A 5313 STRINGER EMB 120 EMB120RT SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 264AS 120165 DURING INSPECTION, FOUND CRACKS ON THE LEFT AND RIGHT NR 10 STRINGER. REPAIRS WERE MADE IAW THE EO 120-57-0081 AND EO 1 20-57-0082. (M) 2 L 7 2 4T RT A31SO 1999101500674 19991015 00674 SO 1999 10 15 ASOA99096 1 19990907 A 3242 21585 BRAKE EMB 120 EMB120RT SO MLG LOCKED A ASOA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 11 264AS 1411 120165 FLT 4881 - WHILE TAXING OUT FOR DEPARTURE THE BRAKES LOCKED UNCOMMANDED, RENDERING THE AIRCRAFT UNABLE TO MOVE. ATL MAI NTENANCE WAS CONTACTED VIA ATLANTA RADIO. AIRCRAFT WAS DISABLED ON THE TAXI-WAY AND THE TIRE MOUNTED ON THE LOCKED BRAK E WAS DEFLATED SO THE AIRCRAFT COULD BE TOWED. MAINTENANCE REMOVED AND REPLACED BRAKE AND BOTH TIRES ON LOCKED SIDE. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999101500675 19991015 00675 SO 1999 10 15 ASOA99094 1 19990907 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 233AS 120031 DURING INSPECTION, NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999101500676 19991015 00676 NM 1999 10 15 USAA990847 1 19990913 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 400L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999101500677 19991015 00677 NM 1999 10 15 USAA990846 1 19990913 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 380L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999101500678 19991015 00678 NM 1999 10 15 USAA991008 1 19990909 A 5330 SKIN BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 32103 23881 PHL/PIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT IN PHL FOUND 1.125 INCH LONG CRACK IN SKIN AT STATION 727D AT STR INGER 25 RT. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01, FIG L02, SH 3 AND EA 52813. (M) 2 L 7 2 4F RT A16WE 1999101500679 19991015 00679 NM 1999 10 15 USAA990974 1 19990913 A 5320 FRAME BOEING 737 737401 1384701 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK LOWER OUTBOARD CORNER OF FORWARD SERVICE DOOR UPPER FO RWARD STOP PAN FITTING FRAME. REPLACED DEFECTIVE PART PER DRAWING 65-45807. (M) 2 L 7 2 4F RT A16WE 1999101500680 19991015 00680 NM 1999 10 15 USAA990975 1 19990913 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 601 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 601, WL 203 LEFT SIDE CHORD ANGLE. REPAIRED STIFFE NER ANGLE PER EA 65335 ADN TR 53-10-23. (M) 2 L 7 2 4F RT A16WE 1999101500681 19991015 00681 NM 1999 10 15 USAA990977 1 19990913 A 5512 SKIN BOEING 737 737401 1384701 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK RT HORIZONTAL STAB TORQUE BOX LOWER SKIN ACCESS. INSTA LLED REPAIR DOUBLER ACCESS PANEL PER EA 65418. (M) 2 L 7 2 4F RT A16WE 1999101500682 19991015 00682 NM 1999 10 15 USAA990965 1 19990913 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 1016, RBL 31 FLOORBEAM. CORROSION LEVE L 2, CORROSION TASK NR C53-107-02. REPAIRED PER EA 65407. (M) 2 L 7 2 4F RT A16WE 1999101500683 19991015 00683 NM 1999 10 15 USAA990932 1 19990913 A 5330 SKIN BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK FUSELAGE SKIN STATION 727D PLUS 10, CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202 AND EA 65488. (M) 2 L 7 2 4F RT A16WE 1999101500684 19991015 00684 NM 1999 10 15 USAA990967 1 19990913 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 440L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBL ER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999101500685 19991015 00685 NM 1999 10 15 USAA990971 1 19990913 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480L BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBL ER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999101500686 19991015 00686 NM 1999 10 15 USAA990972 1 19990913 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480R BETWEEN STRINGER 8/9 FRAME. INSTALLED DOUBL ER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999101500687 19991015 00687 NM 1999 10 15 USAA990973 1 19990913 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE INNER CHORD ANGLE BS 616 FUSELAGE FRAME WL 200 LEFT SIDE. INSTALLED DOUBLER PER EA 65335. (M) 2 L 7 2 4F RT A16WE 1999101500688 19991015 00688 NM 1999 10 15 USAA990874 1 19990913 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 312-328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AT STATION 312-328, RBL 30 UPPER CH ORD INTERCOSTAL. CORROSION LEVEL 1. REPAIRED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999101500689 19991015 00689 NM 1999 10 15 USAA990873 1 19990913 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUT PLATE HOLES ON T-CAP FLOORBEAM STATION 328, LBL 28, AND LBL 11. CORROSION LEVEL 1. REPLACED T-CAP. INSTALLED PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999101500690 19991015 00690 NM 1999 10 15 USAA990881 1 19990913 A 5315 BOEING 737 737401 1384701 NM UNKNOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM 321 UPPR CHORD AT LBL 12.5 T-CAP. C ORROSION LEVEL 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999101500691 19991015 00691 NM 1999 10 15 USAA990894 1 19990913 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION TOP Z-ANGLE FORWARD ENTRY. CORROSION LEVEL 1. REPA IRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999101500692 19991015 00692 NE 1999 10 15 ASOA99099 2 19990915 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A ASOA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 502AS 28538 120274 TEN MILES FROM MEI, SMOKE EVIDENT IN COCKPIT. CREW REQUESTED PRIORITY TO LAND AND FIRE EQUIPMENT. SMOKE CLEARED FROM AI RCRAFT. UPON SHUTDOWN, FIRE CREW AND STATION AGENTS OBSERVED SMOKE 'BELLOWING' NEAR LEFT ACM. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE ASSEMBLY. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999101500693 19991015 00693 NM 1999 10 15 GAIA99141 1 19990917 A 3260 MS250111 SWITCH BOEING 727 727222 1384073 NM NLG DOOR OUT OF ADJUST A GAIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 90AX 20040 FLT 518 - TOL-ATL, AFTER TAKEOFF, THE CREW RETRACTED THE GEAR AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. THE AI RCRAFT RETURNED TO TOL AND LANDED SAFELY WITHOUT ANY FURTHER DIFFICULTIES. ADJUSTED THE NOSE LANDING GEAR DOOR SWITCHES AND PERFORMED A RETRACTION TEST OF THE NOSE GEAR. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999101500694 19991015 00694 NM 1999 10 15 GAIA99142 1 19990921 A 3350 1000677 LIGHT BOEING 727 727222 1384073 NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90AX 20040 DURING ROUTINE INSPECTION, COCKPIT EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED COCKPIT EMERGENCY EXI T LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999101500695 19991015 00695 NM 1999 10 15 GAIA99143 1 19990922 A 3350 1000677 LIGHT BOEING 727 727223 1384074 NM PAX DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6807 19482 DURING ROUTINE INSPECTION, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REMOVED AND REPLACED FORWARD EN TRY DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOO. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999101500696 19991015 00696 NM 1999 10 15 GAIA99144B 1 19990923 A 3222 6598641 STRUT BOEING 727 727222 1384073 NM NLG LEAKING A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 90AX 20040 TOL- ATL - FLT 518 - DURING TAKEOFF, THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER THE GEAR WAS SELECTED UP. THE L IGHT ON THE FLIGHT ENGINEERS DOOR WARNING PANEL. THE CREW CARRIED OUT AOM PROCEDURES, AND RETURNED TO TOL MAKING A ROUT INE AND SAFE LANDING. FERRIED AIRCRAFT TO OSC FROM TOL. MAINTENANCE ADJUSTED THE NOSE GEAR WARNING SWITCHES IAW UAL B7 27 MM 32-63-02. OPERATIONAL CHECKED NORMAL IAW UAL B727 MM 32-63-04. PERFORMED NOSE GEAR STRUT REPACK IAW UAL MM 32-21 -31. NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED BACK TO SERVICE. (M) 2 L 7 3 4F A3WE 1999101500697 19991015 00697 NM 1999 10 15 USAA099903 1 19990917 A 2611 824PY SMOKE DETECTOR BOEING 727 727254 138408L NM LAVATORY FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913TS 20250 FLT 6511 - LGA-DCA - FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR. OPERATIONAL CHECK NORMAL. ( M) 2 L 7 3 4F A3WE 1999101500698 19991015 00698 NM 1999 10 15 TSAA9921425 1 19990908 A 2131 7638101 CONTROLLER BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 819AL 23791 FLT 270 - HNL-KOA - EN ROUTE TO KONA, AIRCRAFT PRESSURIZATION FAILED. RETURNED TO HNL. UNEVENTFUL LANDING. FOUND AC A ND DC MANUAL C/B'S OPEN FOR PRESSURIZATION CONTROL. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. GROUND CHECK OK. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999101500699 19991015 00699 NM 1999 10 15 P2EA99286 1 19990826 A 5755 SPOILER BOEING 737 737247 138448D NM NR 4 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SPOILER NR 4 DAMAGED. REPAIRED IAW COOPESA EO COO-CMP-3-57-532-99. (M) 2 L 7 2 4F A16WE 1999101500700 19991015 00700 NM 1999 10 15 P2EA99284 1 19990822 A 5330 SKIN BOEING 737 737247 138448D NM BS 186-188 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN FROM BS 186 TO BS 188 AT WL 170 DENTED, IN PROXIMITY TO EXTERNAL REPAIR AT BS 180 STRINGER 24R. REPAIRED IAW COOPESA WO NR COO-3-53-524-99. (M) 2 L 7 2 4F A16WE 1999101500701 19991015 00701 NM 1999 10 15 P2EA99285 1 19990924 A 5330 SKIN BOEING 737 737247 138448D NM BS 235-243 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN DAMAGED, FROM BS 235 TO BS 243 BETWEEN STRINGER 20R AND 21R. REPAIRED IAW COOPESA EO COO-3-528-99. (M) 2 L 7 2 4F A16WE 1999101500702 19991015 00702 NM 1999 10 15 P2EA99283 1 19990923 A 2133 OUTFLOW VALVE BOEING 737 737230 NM CABIN MALFUNCTIONED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 123NJ 22121 MCI - FLT 817 - AFT OUTFLOW VALVE WOULD NOT CLOSE. AIRCRAFT WOULD NOT PRESSURIZE. OPS CHECKED PRESSURIZATION SYSTEM PE R MM 21-31-0, NO DEFECTS FOUND. (M) 2 L 7 2 4F RT A16WE 1999101500703 19991015 00703 SO 1999 10 15 99ZZZM709 1 19990921 A 5720 1159W201941X CHANNEL GULSTM G1159 GIV 3980115 SO RT WING CRACKED A P COZA K NONE O OTHER IN INSP/MAINT 1 WP 27 232K 1232 DURING FIRST ROUTINE 72 MONTH INSPECTION ON THIS AIRCRAFT, WHEN RIGHT WING WEDGE WAS REMOVED, INSPECTION FOUND THE INBOA RD SUPPORT CHANNEL, P/N 1159W20194-1XD, S/N 860100 WAS CRACKED. THIS WAS CAUSED BY IMPROPER INSTALLATION DURING AIRCRAF T PRODUCTION. THE WING WEDGE HAS TO SLOPE TO INTERFACE WITH THE WING. THIS WING WEDGE WAS FLAT, CAUSING STRESS ON THE CHANNEL, WHICH THEN CRACKED. (M) 2 L 7 2 4F RT A12EA 1999101500704 19991015 00704 SO 1999 10 15 99ZZZM710 1 19990810 A 3233 1159H202625 ACTUATOR GULSTM G1159 G1159 3953505 SO NLG CRACKED A P COZA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 27 102CX 102 AFTER AIRCRAFT WAS PARKED, CREW NOTICED HYDRAULIC FLUID LEAKING FROM THE NOSE WHEEL WELL. INVESTIGATION FOUND THE ROD E ND FITTING, P/N 1159HM20116, WAS CRACKED ON THE NOSE GEAR ACTUATOR ALLOWING COMBINED HYDRAULIC SYSTEM FLUID TO DRAIN. A CTUATOR, S/N 32-105, HAS BEEN SENT TO GAC, SAV FOR EVALUATION. (M) 2 L 7 2 4F RT A12EA 1999101500705 19991015 00705 NM 1999 10 15 TWRA9937 1 19990827 A 3350 S1356B37 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 R1 OVERHEAD LIGHT EMERGENCY INOPERATIVE. REPLACED BAD LIGHT ASSEMBLY. OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1999101500706 19991015 00706 NM 1999 10 15 TWRA9938 1 19990827 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 E-ZONE L4 OVERHEAD EMEGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M) 2 L 7 4 4F A20WE 1999101500707 19991015 00707 NM 1999 10 15 TWRA9939 1 19990822 A 3397 WIRE BOEING 747 747212B 1384886 NM ROW 24/25 BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 624FF 21439 EMERGENCY EXIT LIGHTING ON SEAT 24 AND 35 ARE INOPERATIVE. FOUND BROKEN WIRE. REPAIRED WIRE PERFORMED OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1999101500708 19991015 00708 NM 1999 10 15 TSAA9930443 1 19990921 A 3030 851CM2 HEAT PROBE BOEING 737 7372T4 1384492 NM LT PITOT FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 808AL 23445 FLT 505 - HNL-CXI - LEFT ELEVATOR PITOT HEAT LIGHT CAME ON IMMEDIATELY AFTER TAKEOFF. RETURNED TO HNL. UNEVENTFUL LAND ING. REMOVED AND REPLACED LEFT ELEVATOR PITOT PROBE. OPS CHECK OK IAW MM 27-31-141. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A16WE 1999101500709 19991015 00709 NM 1999 10 15 TSAA9922442 1 19990922 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999101500710 19991015 00710 NM 1999 10 15 TSAA9933438 1 19990917 A 3350 1000679 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999101500711 19991015 00711 NM 1999 10 15 TSAA9953439 1 19990918 A 5330 65558211 SKIN BOEING 737 737230 NM BS 957/970 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 FOUND TWO CRACKS ON LEFT OF AIRCRAFT BELOW AFT ENTRY DOOR, BELOW STRINGER 21L AT BS 957 AND 970. REPAIRED PER SRM 53-30 -3 PAGE 2B. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999101500712 19991015 00712 EU 1999 10 15 SIMA992671 1 19990917 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 283AE 16057 340B283 DFW - DURING PS-2 CHECK, FOUND THE FLOOR PROXIMITY LIGHT AFT OF SEAT 7B DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGE NCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999101500713 19991015 00713 EU 1999 10 15 SIMA992661 1 19990923 A 3350 005W800 WEU SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 383AE 1375 340B383 DFW - FLT 3752 - EMERGENCY LIGHTS DISARMED INDICATOR ON THE CWP DOES NOT ILLUMINATE WITH ARM SWITCH IN THE OFF POSITION. PRESS TO TEST FUNCTION IS NORMAL. REMOVED AND REPLACED WARNING ELECTRONIC UNIT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999101500714 19991015 00714 EU 1999 10 15 SIMA992652 1 19990922 A 3397 WIRE SAAB SF340 340B 7860101 EU CABIN BROKEN A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 301AE 340B301 JFK - FLT 5006 - EMERGENCY OVERHEAD LIGHTS AT SEATS 8BC, 10BC, AND 12 BC DO NOT ILLUMINATE. REPAIRED BROKEN WIRES AT FU SE HOLDERS 71 AND 72 LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999101500715 19991015 00715 EU 1999 10 15 SIMA992651 1 19990922 A 3350 74332 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 383AE 340B383 DFW - FLT 3270 - EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROW 11 IS BROKEN. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999101500716 19991015 00716 EU 1999 10 15 SIMA992631 1 19990920 A 3350 7239410009 SIGN SAAB SF340 340B 7860101 EU ROW 7A BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 320AE 340B320 SBP - DURING PS-2 INSPECTION, FOUND THE EMERGENCY FLOOR PROXIMITY LIGHT COVER AND THE EMERGENCY EXIT SIGN AT SEAT 7A WER E BOTH BROKEN. REMOVED AND REPLACED FLOOR LIGHT COVER AND EMERGENCY EXIT LIGHT SIGN AT SEAT 7A. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 1999101500717 19991015 00717 EU 1999 10 15 99ZZZM711 1 19990920 A 3350 7239410001 COVER SAAB SF340 340B 7860101 EU ROW 7A BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 320AE 340B320 SBP - DURING PS-2 INSPECTION, FOUND THE EMERGENCY FLOOR PROXIMITY LIGHT COVER AND THE EMERGENCY EXIT SIGN AT SEAT 7A WER E BOTH BROKEN. REMOVED AND REPLACED FLOOR LIGHT COVER AND EMERGENCY EXIT LIGHT SIGN AT SEAT 7A. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 1999101500718 19991015 00718 1999 10 15 99ZZZM712 4 19990714 A 2565 5WD230100301 SLIDE DOUG DC10 DC1010 3022110 WP L1 DOOR DEPLOYED A RYNA O OTHER O OTHER IN INSP/MAINT 1 CE 07 571SC 46645 FLT 9154 - SLC, LEFT NR 1 DOOR SLIDE DEPLOYED INADVERTENTLY. DEFERRED IN SLC CLEARED IN LAX. REPLACED ESCAPE SLIDE/RAF T PACK. (M) 2 L 7 3 4F A22WE 1999101500719 19991015 00719 NM 1999 10 15 99ZZZM713 1 19990911 A 2612 1825280037525 FIRE LOOP BOEING 727 72777C 1380420 NM NR 3 OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 526PC 20370 FLT 607 - SFO, NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATES IN FLIGHT. REPOSITIONED NR 3 FIRE LOOP, SECURED COWL ING. (M) 2 L 7 3 4F A3WE 1999101500720 19991015 00720 WP 1999 10 15 TWAA9914101 1 19991008 A 3397 WIRE DOUG DC9 DC983 3022083 WP GALLEY CHAFED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 EIBWD 49575 THE COCKPIT OVERHEAD EMERGENCY LIGHTS GLOWED DIMLY AND WOULD NOT SHUT OFF. REPAIRED CHAFED WIRES AT THE FIRST CLASS GAL LEY, AROUND THE GALLEY WORK LIGHTS. CHECK-C 2-6-99 MCI. 2 L 7 2 4F RT A6WE 1999101500721 19991015 00721 WP 1999 10 15 TWAA9914102 1 19991005 A 5330 SKIN DOUG DC9 DC931 3022065 WP CARGO DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND CRACK INDICATION AT THE FORWARD CARGO DOOR, UPPER FORWARD CORNER OF THE FUSELAGE SKIN. R EPAIRED SKIN CRACK PER DOUGLAS SERVICE BULLETIN 53-277 AND SRM 53-05, FIG 105. 2 L 7 2 4F A6WE 1999101500722 19991015 00722 WP 1999 10 15 TWAA9914103 1 19991008 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 976Z 47248 DURING CHECK-C, MAINT FOUND LONGERON 6R CRACKED .375 INCH AT STA 756. REPAIRED PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1999101500723 19991015 00723 WP 1999 10 15 TWAA9914104 1 19991001 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND CORROSION ON THE UPPER FLANGE OF FLOOR ATTACH ANGLE, STA 160 RBL 1.5 INCHES TO 10 IN. R EMADE FLOOR SUPPORT ANGLE WITH (P/N S2652479-12000). REINSTALLED FASTENERS IN FLOOR SUPPORT PER SRM 51-30-5. 2 L 7 2 4F A6WE 1999101500724 19991015 00724 NM 1999 10 15 AT990721 1 19991008 A 3520 MASK BOEING 717 717200 1383700 NM ROW 1R&19L FAILED TEST A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 942AT 55005 DURING OXYGEN MASK DROP TEST, OXYGEN MASKS AT SEAT 1R AND 19L DID NOT DROP. 2 L 7 2 4F TR A6WE 1999101500725 19991015 00725 NM 1999 10 15 RAAA99B2055 1 19991011 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 EMERGENCY LIGHT AT MID CABIN EXIT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999101500726 19991015 00726 SO 1999 10 15 RAAA99E8054 1 19991011 A 3350 873100112 LIGHT INTVLV LKHEED 188 188C 5262604 SO ROW 13DEF BROKEN A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FLOOR PROXIMITY LIGHT AT ROW 13 D, E, F MISSING LENS, REFLECTOR AND BULB. REPLACED LIGHT ASSY. 2 L 7 4 4T 4A22 1999101500727 19991015 00727 WP 1999 10 15 CALA9901366 1 19991013 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP EMER EXIT INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14816 49370 FORWARD OVERWING EMERGENCY EXIT LIGHT STAYS ON CONTINUOUSLY. REPLACED POWER SUPPLY PER MM 33-53-00. 2 L 7 2 4F A6WE 1999101500728 19991015 00728 NM 1999 10 15 CALA9901367 1 19991013 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE MID FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 LEFT OUTBOARD MIDFLAP UPPER SKIN GOUGED INBOARD OF INBOARD FLAP TRANSMISSION. CUT OUT DAMAGED AREA, FABRICATED, TREATED , PRIMED, AND INSTALLLED REPAIR DOUBLER AND FILLER PER SRM 51-30-4, 51-50-1, AND 51-30-2. 2 L 7 3 4F A3WE 1999101500729 19991015 00729 NE 1999 10 15 9904222201 2 19991010 A 7510 SADDLE DUCT BOEING 727 727251 138408H NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE BLOWN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 201US 22154 649472 DURING CLIMBOUT, THE NR 1 ENGINE FIRE WARNING ACTIVATED WITH EPR GOING FROM 1.94 TO 1.8 AND EGT AT RED LINE. CREW DECLA RED A YELLOW EMERGENCY, NR 1 ENGINE WAS SHUT DOWN, AND THE FLIGHT WAS RETURNED TO DTW. AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE FOUND 13TH STAGE SADDLE DUCT BLOWN WITH HOLE IN ENGINE COWL. REPLACED DUCT AND UPPER COWLING ASSEMBLY, O PERATIONAL CHECK NORMAL ON ENGINE RUN. 2 L 7 3 4F 4 F A3WE E2EA 1999101500730 19991015 00730 EU 1999 10 15 9904233251 1 19991006 A 7830 9203074 FILTER AIRBUS 320 A320212 EU NR 2 TR UNIT LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 351MW 766 DURING CRUISE, RECEIVED HYD-Y RESERVOIR LOW LEVEL MESSAGE. SECURED YELLOW HYDRAULIC SYSTEM PER COM PROCEDURES. CONTINU ED TO FINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE THRUST REVERSER ISOLATION VALVE F ILTER AND RESERVICED SYSTEM. LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999101500731 19991015 00731 WP 1999 10 15 9904249874 1 19991006 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 783NC 48108 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999101500732 19991015 00732 NM 1999 10 15 9904252203 1 19991011 A 2910 LINE BOEING 727 727251 138408H NM A HYD SYS CHAFED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 203US 22543 AT CRUISE, CREW REPORTED TOTAL LOSS OF A SYSTEM HYDRAULICS. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. DTW MA INTENANCE FOUND AND REPLACED CHAFED/RUPTURED PRESSURE LINE. ALL LEAK AND OPERATIONAL CHECKS OK. 2 L 7 3 4F A3WE 1999101500733 19991015 00733 NM 1999 10 15 UPS99230878 1 19991007 A 5712 651850210 SHEAR TIE BOEING 727 72725C 138400H NM WS 225-229 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI ,CORROSION (C57-571-01.01-02) R/W NR 3 FUEL CELL INTERNAL AFT LOWER SPAR CHORD AT WS 225-WS 229. REP AIRED PER ER 99-6094. 2 L 7 3 4F A3WE 1999101500734 19991015 00734 NM 1999 10 15 UPS99230879 1 19990825 A 2760 41400600 MOUNT BOEING 727 72725C 138400H NM SPOILER MIXER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING NRC 997902 (WINGS 169) FOUND UPPER MOUNT LEGS CORRODED ON SPOILER MIXER. CORROSION FO UND TO BE OUT OF LIMITS. NEW SPOILER MIXER INSTALLED PER MM 27-61-31. 2 L 7 3 4F A3WE 1999101500735 19991015 00735 NM 1999 10 15 UPS99230880 1 19990820 A 2760 41400105 BEAM BOEING 727 72725C 138400H NM SPOILER MIXER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, SPOILER MIXER RIGGING BEAM IS CORRODED AT LOWER O/B MOUNTING BOLT. BEAM WAS FOUND TO BE CORRODED BE YOND LIMITS. NEW BEAM WAS INSTALLED PER MM 27-61-31. 2 L 7 3 4F A3WE 1999101500736 19991015 00736 NM 1999 10 15 UPS99230881 1 19990821 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 540-660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-111-01.00-02) ON BEAM BS 540-660 BL 0 WL 200. CUT OUT DAMAGED FLOOR STRAP BS 510 TO 6.70, FABRICATED REPLACEMENT PART AND SPLICE ANGLES, INSTALLED REPAIR PART PER ERO 99-6120. 2 L 7 3 4F A3WE 1999101500737 19991015 00737 NM 1999 10 15 UPS99230882 1 19991011 A 5347 M706451 SEAT TRACK BOEING 727 72725C 138400H NM BS 540-720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, SEAT TRACK BS 720-540 REQUIRES REPLACEMENT DUE TO EXTENSIVE FLOORBEAM REPAIRS (RBL 25). REPLACED SE AT TRACK BS 720-540 RBL PER SRM 53-10-5, 51-30-2. 2 L 7 3 4F A3WE 1999101500738 19991015 00738 NM 1999 10 15 UPS99230883 1 19990825 A 5315 M840065 FLOORBEAM BOEING 727 72725C 138400H NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM LOWER SURFACE AROUND FASTENER HOLES BS 600 WL 208 RBL 50. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8, FIG 5, 53-10-8 PG 33, 51-10-2 PG 33. 2 L 7 3 4F A3WE 1999101500739 19991015 00739 NM 1999 10 15 UPS99230884 1 19991011 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1130-1150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING 997311 FOUND CORROSION ON STR 6 LT BS 1130 TO BS 1150. REPAIRED STR 6 LT AT BS 1130 T O BS 1150 PER SRM 53-10-3, 51-30-2. 2 L 7 3 4F A3WE 1999101500740 19991015 00740 NM 1999 10 15 UPS99230885 1 19990825 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM LOWER SURFACE AROUND FASTENER HOLES AT SEAT TRACK ATTACH P OINT BS 520, WL 208, LBL 25. REPAIRED CORRODED FLOORBEAM IAW SRM 53-10-08. 2 L 7 3 4F A3WE 1999101500741 19991015 00741 WP 1999 10 15 UPS99830877 1 19991012 A 2120 PACK DOUG DC8 DC873F 302199F WP AIR DISTRIBUTION FAILED A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 806UP 46006 NR 1 BUS PWR FAIL LIGHT ILLUMINATED ON BLOCK IN. COCKPIT FILLED W/PACK SMOKE EVEN THOUGH PACK WAS OFF. COULD STILL HEA R FAN OPERATING AND COOLING DOORS OPEN. TROUBLESHOT SYSTEM PER MM 24-20-00. RECONNECTED NR 3 GENERATOR, RAN ENGINE, SY STEM OPS CHECKS GOOD. SEE M180145. 2 L 7 4 4F RT 4A25 1999101500742 19991015 00742 EU 1999 10 15 QXEA9902054 1 19991009 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU COCKPIT INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 PDX- EMERGENCY SIGN OVER COCKPIT DOOR HAD LIGHTS INOP. REPLACED CIRCUIT BOARD OVER COCKPIT DOOR. 2 L 7 2 4F RT A20EU 1999101500743 19991015 00743 NM 1999 10 15 99FDEA00421 1 19991013 A 3260 SWITCH BOEING 727 727225 1384077 NM LT MLG DOOR LACK OF LUBE A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 463FE 22551 CONFIGURED AC WITH GEAR AND 15 DEG FLAPS DURING APPROACH. GEAR EXTENSION NORMAL, BUT DOOR LIGHT AND LEFT GEAR DOOR LIGH T REMAINED ILLUMINATED. LUBED DOOR WARNING SWITCH, GEAR DOOR WARNING SYS CK GOOD PER MM 32-62-011. 2 L 7 3 4F A3WE 1999101500744 19991015 00744 NM 1999 10 15 99FDEA00422 1 19991013 A 3230 SWITCH BOEING 727 72725 1384006 NM NLG FAILED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 509FE 18280 ON 1ST APPROACH NOSE LANDING GEAR DID NOT COME DOWN WHEN SEL. GEAR WARNING HORN SOUNDED. FLAPS WERE SEL AT 15. REMOVE D AND REPLACED NOSE LANDING GEAR LOCK SWITCH AND POSITION SWITCH PER 727-100 MM 32-61-021-4. OPER CHECK GOOD. 2 L 7 3 4F A3WE 1999101500745 19991015 00745 NM 1999 10 15 99FDEA00424 1 19991007 A 2781 WARNING DOUG MD11 MD11F 3023600 NM LE SLAT ACTIVATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 586FE 48487 AFT SLAT RETRACTION RECEIVED A LEVEL 2. *S/D* REMOVED AND REPLACED R2-5060 RELAY PER SRM. REMOVED AND REPLACED FLAP H ANDLE TRANSMITTER PER MM 27-54-03-4 & 27-54-00-5. PERFORMED FCC 1 & 2 SENSOR READOUT ANALOG VALUE EACH DEG ALL READ SAT AND OPS CHECK NORM. 2 L 7 3 4F RT A22WE 1999101500746 19991015 00746 1999 10 15 MWEA99669 4 19991009 A 3416 51828007204 ALTIMETER DOUG DC9 DC932 3022066 WP LT COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 209ME 47730 PASSING THROUGH 20,000 FEET, CAPTAINS ALTIMETER BEGAN RAPID CLIMB TO 51,300 FEET AND FLAGGED OFF. MTC REMOVED AND REPLA CED CAPTAINS ALTIMETER. 2 L 7 2 4F A6WE 1999101500747 19991015 00747 WP 1999 10 15 MWEA99670 1 19991005 A 5753 9957578505 SKIN DOUG DC9 DC914 3022034 WP RT TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 RIGHT FLAP NR 3 WEDGE HAD A DENT OUT OF LIMITS. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999101500748 19991015 00748 WP 1999 10 15 MWEA99671 1 19991005 A 5753 99576101 CHANNEL DOUG DC9 DC914 3022034 WP RT TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 RIGHT FLAP NR 3 WEDGE TRAILING EDGE V-CHANNEL HAD A DENT. MTC REMOVED AND REPLACED V-CHANNEL. 2 L 7 2 4F A6WE 1999101500749 19991015 00749 WP 1999 10 15 MWEA99681 1 19991012 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 LEFT EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LEFT EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1999102200026 19991022 00026 NM 1999 10 22 AALA991157 1 19990810 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AN 29425 BOS - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIG HT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999102200027 19991022 00027 EA 1999 10 22 99ZZZX3958 2 19990823 A 7320 3031829 P3 LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE BROKEN A FFSA O OTHER Y ENGINE STOPPAGE NR NOT REPORTED 1 AL 01 575A 2229 UC83 PCE32326 RIGHT ENGINE FAILED. ROLLED BACK TO IDLE. FOUND EXTERNAL P3 BLEED LINE BROKEN. 2 L 7 2 4T 4 T RT A24CE E4EA 1999102200028 19991022 00028 EU 1999 10 22 99ZZZX3959 1 19990704 A 6710 704A44831140 SERVO SNIAS AS350 AS350B3 8680954 EU TAIL ROTOR CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 104LN 27 343 3134 SUSPECT CRACK OR MACHINE DEFECT ON THE BOTTOM TUBE OF SERVO. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U NC H9EU 1999102200029 19991022 00029 SO 1999 10 22 99ZZZX3960 1 19990607 A 2612 D889N FIRE LOOP GULSTM G159 G159 3952202 SO LT ENGINE SHORTED A ESPA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 11 190PA 4224 195 EWR/TXKF - EN ROUTE, WHEN LEFT FIRE LIGHT CAME ON. CREW DID VISUAL INSPECTION OF ENGINE AND ENGINE INSTRUMENTS. NO IND ICATION OF ANYTHING UNUSUAL. FIRE LIGHT WENT OUT, CREW TRIED TO TEST SYSTEM FIRE LOOP LOCATED IN ENGINE COMPARTMENT. W OULD NOT TEST. CREW SHUT DOWN ENGINE AND DISCHARGED BOTTLE. LANDED IN TXKF WITH NO PROBLEMS. AIRCRAFT INSPECTED AT TX KF, NO INDICATIONS OF ANY FIRE OR FIRE LOOP WEAR OR CHAFING. REPLACED FIRE BOTTLE, AND REPLACED ONE SECTION OF LOOP THA T HAD HIGHER THAN NORMAL RESISTANCE. SYSTEM CHECKED PER MM, CHAPTER 26. 2 L 7 2 4T 1A17 1999102200030 19991022 00030 1999 10 22 99ZZZX3961 4 19990729 A 2565 D31865103 SLIDE AIRBUS 320 A320231 3930325 EU LT EMERG EXIT DEPLOYED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 GSUEE 363 DEN - LEFT OVERWING SLIDE BLOWN. REPLACED LEFT HAND OVERWING SLIDE. 2 L 7 2 4F RT A28NM 1999102200031 19991022 00031 1999 10 22 AALA991172 4 19990812 A 2397 WIRE BOEING 777 777223 1385213 NM CABIN DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 774AN 29581 NRT - FLT T0061 - VIDEO CONTROL BOX FAILURE CAUSED SMOKE TO ISSUE FROM SEAT 14E PERSONAL CONTROL UNIT (PCU). REPLACED W IRING HARNESS FOR DEPLOYMENT UNIT, VIDEO CHECKED GOOD. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 1999102200032 19991022 00032 1999 10 22 AALA991237 4 19990817 A 2350 1301273110 AUDIO VISUAL COLLINS BOEING 777 777223 1385213 NM CABIN DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 774AN 9809000072 29581 NRT - FLT T153 - EN ROUTE ORD, NRT ELECTRICAL SMELL NOTED FROM ENTERTAINMENT UNIT. SYSTEM SHUT DOWN AND SMELL DISSIPATE D. REPLACED AUDIO VISUAL UNIT AT SEAT ROW 9D/E/G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 1999102200033 19991022 00033 EU 1999 10 22 AWXA9900358 1 19991004 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 765 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 C-CHECK, FLOOR TRACK AT 765 RT CORRODED FR 20. REPLACED SECTION OF TRACK AS PER SRM 51-77-00 PG 1 AND SRM 53-11-15 PG 2 13, TREATED, PRIMED AND PAINTED AS PER SRM 51-21-00. 2 L 7 2 4F RT A28NM 1999102200034 19991022 00034 EU 1999 10 22 AWXA9900359 1 19991004 A 5315 FLOORBEAM AIRBUS 320 A320231 3930325 EU BS 7087-8077 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 C-CHECK, FLOORBEAM BETWEEN STA 7087 & 8077, SIX INCHES RIGHT OF CENTER LINE HAS EVIDENCE OF CORROSION ON TOP SURFACE (FR 16 TO FR 20). REMOVED EXISTING FILLER PLATE, FABRICATED NEW FILLER OF .080 2024T3--MATERIAL, TREATED, PRIMED, PAINTED AND INSTALLED FILLER PLATE AS PER SRM 53-00-14 PG 206 SHT 1. 2 L 7 2 4F RT A28NM 1999102200035 19991022 00035 EU 1999 10 22 AWXA9900360 1 19991004 A 5315 D53112818200 FLOORBEAM AIRBUS 320 A320231 3930325 EU BS 8433 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 C-CHECK, STA 8433 FLOORBEAM CORRODED, 12 INCHES LEFT OF CENTER FR 21. REPLACED SECTION OF H-ANGLE FLOORBEAM NR D5311281 8200 AS PER SRM 51-72-00 PG 1. TREATED, PRIMED AND PAINTED AS PER SRM 51-21-00. 2 L 7 2 4F RT A28NM 1999102200036 19991022 00036 EU 1999 10 22 AWXA9900361 1 19991004 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 1292 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 C-CHECK, FLOORBEAM TRACK Y 1292 RT CORRODED FR 16 TO FR 20. REPLACED SECTION OF TRACK NR D 53112782200 AS PER SRM 51-72 -00 PG 1 AND SRM 53-11-15 PG 213, TREATED, PRIMED AND PAINTED AS PER 51-21-00. 2 L 7 2 4F RT A28NM 1999102200037 19991022 00037 NM 1999 10 22 AWXA9900363 1 19991014 A 5330 6545775 SKIN BOEING 737 7373Y0 1384671 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 329AW 23500 C-CHECK, FUSELAGE SKIN CRACKED STA 727D BETWEEN S24 & S25R. SKIN REPAIRED AS PER B737 SRM 53-00-01 FIG 201 PG 201 - 203 . 2 L 7 2 4F RT A16WE 1999102200038 19991022 00038 NM 1999 10 22 AWXA9900364 1 19991014 A 5313 69489485D STRINGER BOEING 737 7373Y0 1384671 NM BS 354 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 329AW 23500 C-CHECK, CORROSION ON STRINGER 29 RT AT STA 354-360. REMOVED AND REPLACED STRINGER PER DRAWING 65-45800. 2 L 7 2 4F RT A16WE 1999102200039 19991022 00039 NM 1999 10 22 AWXA9900365 1 19991014 A 5311 6558280 FRAME BOEING 737 7373Y0 1384671 NM BS 360 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 329AW 23500 C-CHECK, FRAME AT STA 360 BETWEEN STR 27R & 28R CORRODED. REPAIRED PER SRM 53-00-07 FIG 205. 2 L 7 2 4F RT A16WE 1999102200040 19991022 00040 NM 1999 10 22 CALA9901368 1 19991013 A 5720 115A375812 BEAM BOEING 737 737824 13844BZ NM WS 253 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12216 28776 TWO CRACKS AT STATION 253 ON TRAILING EDGE MID SPAN BEAM (.75 EACH). INSTALLED DOUBLERS ON RIGHT WING MID SPAN BEAM AND FITTING PER EC/RA 5750-03303. 2 L 7 2 4F RT A16WE 1999102200041 19991022 00041 NM 1999 10 22 CALA9901369 1 19991013 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 290.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 RIGHT OUTBOARD SEAT TRACK CORRODED AT STA 290.5. FABRICATED AND INSTALLED NEW SECTION OF TRACK PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999102200042 19991022 00042 NM 1999 10 22 CALA9901370 1 19991014 A 5330 143N3320 SKIN BOEING 757 757224 1384958 NM BS 610 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13113 27555 IMPACT DAMAGE (1)ON LEFT SIDE FUSELAGE STATION 610 BETWEEN STRINGERS 15 AND 16 LEFT. REPAIRED PER SRM 53-00-01 FIG 208. 2 L 7 2 4F RT A2NM 1999102200043 19991022 00043 EA 1999 10 22 COMA9960598 1 19991013 A 5320 601R38303253 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 THE THRESHOLD ANGLE AT THE SERVICE DOOR IS SEVERELY CORRODED. PERFORMED A MAJOR REPAIR REMOVED THE DAMAGED ANGLE FABRIC ATED AND INSTALLED A NEW ANGLE IAW WVAC EO 601R-53-0415. 2 L 7 2 4F RT A21EA 1999102200044 19991022 00044 EA 1999 10 22 COMA9960599 1 19991013 A 5320 601R3111358 CLIPS CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 THE CLIPS AT FS 280 AND LBL 9.0 WERE CRACKED. PERFORMED A MAJOR REPAIR, REMOVED THE DAMAGED CLIPS, FABRICATED AND INSTA LLED NEW CLIPS IAW WVAC EO 601R-53-0418. 2 L 7 2 4F RT A21EA 1999102200045 19991022 00045 EA 1999 10 22 COMA9960600 1 19991013 A 5330 601R3867317 PLATES CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 THE TOP PLATES AT FS 349 FROM RBL 42 TO LBL 42 ARE CORRODED (P/N 601R38673-17), (601R38673-19), (601R387673-21), (601R38 673-25). PERFORMED A MAJOR REPAIR, REMOVED THE CORRODED PLATES AT FS 349 AND INSTALLED NEW PLATES IAW WVAC EO 601R-53-0 416. 2 L 7 2 4F RT A21EA 1999102200046 19991022 00046 EA 1999 10 22 COMA9960601 1 19991013 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 EA PAX DOOR ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 931CA 7037 CABIN DOOR LATCH CAUTION WARNING AFTER DEPARTURE FROM YUL. AIRCRAFT RETURNED TO THE FIELD. PERFORMED OPERATIONAL CHECK OF CABIN DOOR WARNING INDICATION, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999102200047 19991022 00047 EA 1999 10 22 COMA9960602 1 19991013 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 EA LT & RT TE FLAPS MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 786CA 7333 DURING FINAL APPROACH INTO CVG, THE FLAP FAIL CAUTION WARNING ACTIVATED. REPLACED SEVEN FLAP ACTUATORS (S/N 1724A) (173 7A) (1047A) (1721A) (1748A) (0973A) AND (0867), (P/N 852D100-11) (853D100-12) AND (854D100-12). 2 L 7 2 4F RT A21EA 1999102200048 19991022 00048 EA 1999 10 22 COMA9960603 1 19991013 A 2751 855D1009 SENSING UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING IN INSP/MAINT 1 SO 01 796CA 126 7338 WHEN FLAPS WERE SELECTED TO 30 DEGREES ON GROUND THE FLAP FAIL MESSAGE ACTIVATED. REPLACED THE LEFT BRAKE POSITIONING S ENSING UNIT. 2 L 7 2 4F RT A21EA 1999102200049 19991022 00049 EA 1999 10 22 COMA9960604 1 19991012 A 2750 860D10018 CONTROL CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 786CA 7333 DURING APPROACH INTO CVG, THE FLAP FAIL WARNING MESSAGE APPEARED WHEN SELECTING 42 DEGREES. REPLACED THE FLAP CONTROL H ANDLE. 2 L 7 2 4F RT A21EA 1999102200050 19991022 00050 EA 1999 10 22 COMA9960605 1 19991011 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 933CA 7040 FLAP FAIL CAUTION MESSAGE DURING CRUISE FLIGHT. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY AT CVG. REPLACED T HE LEFT BRAKE POSITIONING SENSING UNIT. 2 L 7 2 4F RT A21EA 1999102200051 19991022 00051 EA 1999 10 22 COMA9960606 1 19991010 A 5270 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 AFTER TAKEOFF FROM CVG, CABIN DOOR UNSAFE WARNING ACTIVATED. AIRCRAFT DIVERTED TO LEX. REPLACED TWO CABIN DOOR PROXIMI TY SENSORS. 2 L 7 2 4F RT A21EA 1999102200052 19991022 00052 EA 1999 10 22 COMA9960607 1 19991011 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA K NONE N FALSE WARNING LD LANDING 1 SO 01 786CA 7333 FLAP FAIL CAUTION MESSAGE DURING LANDING AT TOL.\NREPLACED THE RIGHT BRAKE POSITIONING SENSING UNIT. 2 L 7 2 4F RT A21EA 1999102200053 19991022 00053 EU 1999 10 22 QXEA9902057 1 19991004 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200054 19991022 00054 EU 1999 10 22 QXEA9902058 1 19991004 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200055 19991022 00055 EU 1999 10 22 QXEA9902059 1 19991004 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200056 19991022 00056 EU 1999 10 22 QXEA9902060 1 19991004 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200057 19991022 00057 EU 1999 10 22 QXEA9902061 1 19991004 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200058 19991022 00058 EU 1999 10 22 QXEA9902062 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 7805 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200059 19991022 00059 EU 1999 10 22 QXEA9902063 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200060 19991022 00060 EU 1999 10 22 QXEA9902064 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200061 19991022 00061 EU 1999 10 22 QXEA9902065 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200062 19991022 00062 EU 1999 10 22 QXEA9902066 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200063 19991022 00063 EU 1999 10 22 QXEA9902067 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200064 19991022 00064 EU 1999 10 22 QXEA9902068 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200065 19991022 00065 EU 1999 10 22 QXEA9902069 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12405 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200066 19991022 00066 EU 1999 10 22 QXEA9902070 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200067 19991022 00067 EU 1999 10 22 QXEA9902071 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 12875 AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200068 19991022 00068 EU 1999 10 22 QXEA9902072 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200069 19991022 00069 EU 1999 10 22 QXEA9902073 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200070 19991022 00070 EU 1999 10 22 QXEA9902074 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200071 19991022 00071 EU 1999 10 22 QXEA9902075 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200072 19991022 00072 EU 1999 10 22 QXEA9902076 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200073 19991022 00073 EU 1999 10 22 QXEA9902077 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200074 19991022 00074 EU 1999 10 22 QXEA9902078 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200075 19991022 00075 EU 1999 10 22 QXEA9902079 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200076 19991022 00076 EU 1999 10 22 QXEA9902080 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200077 19991022 00077 EU 1999 10 22 QXEA9902081 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200078 19991022 00078 EU 1999 10 22 QXEA9902082 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815A AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200079 19991022 00079 EU 1999 10 22 QXEA9902083 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200080 19991022 00080 EU 1999 10 22 QXEA9902084 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200081 19991022 00081 EU 1999 10 22 QXEA9902085 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13185 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200082 19991022 00082 EU 1999 10 22 QXEA9902086 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200083 19991022 00083 EU 1999 10 22 QXEA9902087 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200084 19991022 00084 EU 1999 10 22 QXEA9902088 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200085 19991022 00085 EU 1999 10 22 QXEA9902089 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200086 19991022 00086 EU 1999 10 22 QXEA9902090 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 13815B AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200087 19991022 00087 EU 1999 10 22 QXEA9902091 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 14755 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200088 19991022 00088 EU 1999 10 22 QXEA9902092 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 14755 AND STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200089 19991022 00089 EU 1999 10 22 QXEA9902093 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 15205 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200090 19991022 00090 EU 1999 10 22 QXEA9902094 1 19991003 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 6900 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT-HAND FUSELAGE SKIN HAS TWO SCRAPES THROUGH PAINT AT STATION 6900 AND WL-400. REPAIRED IAW FOKKER SRM 53-01-0 1, PARAGRAPH 3B, AREA B, FIGURE 1. 2 L 7 2 4F RT A20EU 1999102200091 19991022 00091 EU 1999 10 22 QXEA9902095 1 19991002 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 6565 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - DENT IN LEFT-HAND FUSELAGE SKIN AT STATION 6565 AND WL-420, 1.5 WIDE .080 DEEP. REPAIRED IAW FOKKER SRM 53-02-07, PAGE 5, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200092 19991022 00092 EU 1999 10 22 QXEA9902096 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200093 19991022 00093 EU 1999 10 22 QXEA9902097 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 43. ALSO, FRAME IS DENTED. REPAIRED IAW FOKKER SRM 53-02- 13, PAGE 4, FIGURE 2 AND SRM 51-10-4, PAGE 9, PARAGRAPH 4B-C. 2 L 7 2 4F RT A20EU 1999102200094 19991022 00094 EU 1999 10 22 QXEA9902098 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200095 19991022 00095 EU 1999 10 22 QXEA9902099 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200096 19991022 00096 EU 1999 10 22 QXEA9902100 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 5805 AND STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200097 19991022 00097 EU 1999 10 22 QXEA9902101 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200098 19991022 00098 EU 1999 10 22 QXEA9902102 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200099 19991022 00099 EU 1999 10 22 QXEA9902103 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 6305 AND STRINGER 33. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200100 19991022 00100 EU 1999 10 22 QXEA9902104 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 7805 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200101 19991022 00101 EU 1999 10 22 QXEA9902105 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305 AND STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200102 19991022 00102 EU 1999 10 22 QXEA9902106 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200103 19991022 00103 EU 1999 10 22 QXEA9902107 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9035 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200104 19991022 00104 EU 1999 10 22 QXEA9902108 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9035 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200105 19991022 00105 EU 1999 10 22 QXEA9902109 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9035 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200106 19991022 00106 EU 1999 10 22 QXEA9902110 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9035 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200107 19991022 00107 EU 1999 10 22 QXEA9902111 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9035 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9035A AND STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200108 19991022 00108 EU 1999 10 22 QXEA9902112 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305B AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200109 19991022 00109 EU 1999 10 22 QXEA9902113 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 9305C AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200110 19991022 00110 EU 1999 10 22 QXEA9902114 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200111 19991022 00111 EU 1999 10 22 QXEA9902115 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200112 19991022 00112 EU 1999 10 22 QXEA9902116 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200113 19991022 00113 EU 1999 10 22 QXEA9902117 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10346 AND STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200114 19991022 00114 EU 1999 10 22 QXEA9902118 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 10966 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200115 19991022 00115 EU 1999 10 22 QXEA9902119 1 19991002 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CABIN FRAME CLIP IS CRACKED AT FRAME 11405 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200116 19991022 00116 EU 1999 10 22 QXEA9902120 1 19991002 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FRAME 4175-4610 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CORROSION ON TOP OF LONGITUDINAL FLOORBEAM THAT EXTENDS FORWARD FROM RIGHT-HAND OUTBOARD SEAT TRACK BETWEEN FRAME 4175 AND 4610. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999102200117 19991022 00117 EU 1999 10 22 QXEA9902121 1 19991001 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CENTER CARGO DOOR INNER SKIN HAS SEVERAL DENTS AND ONE AREA ALL CANNING IN TOP 15 INCHES. REPAIRED IAW HORIZON AIR EA 4-52-271. 2 L 7 2 4F RT A20EU 1999102200118 19991022 00118 EU 1999 10 22 QXEA9902122 1 19990927 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CLIP CRACKED ON RIGHT-HAND SIDE AT FRAME 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999102200119 19991022 00119 NM 1999 10 22 99FDEA00425 1 19991013 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 755 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 MAIN DECK, SEAT TRACK FOUND CRACK AT BS 755 X=27.5 RT LENGTH 3 IN. *S/D* REPAIRED PER SRM 53-70-00 FIG 1 VOL 1. REPAI RED SPLICE AND TRACK AS PER SRM 53-70-00. REPAIR PARTS INSTALLED. 2 L 7 3 4F RT A22WE 1999102200120 19991022 00120 NE 1999 10 22 99UAL900451 2 19990826 A 7230 COMPRESSOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE STALLED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 785UA 26954 222009 SHORTLY AFTER DEPARTURE IAD ENROUTE TO FRA, LEFT ENGINE INDICATED HIGH EGT ACCOMPLANIED BY ENGINE SURGE. ACCOMPLISH ENG INE SHUTDOWN AND RETURNED TO IAD. SUPPLEMENTAL DATA UPDATE COMPRESSOR STALL WAS CAUSED BY COMPRESSOR VARIABLE VANE SYSTE M FAILSAFED TO FULL OPEN POSITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200121 19991022 00121 NM 1999 10 22 99UAL900501 1 19991002 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE ROW 14 INOP A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 952UA 26699 THE EMERGENCY EGRESS LIGHTS FROM ROW 14 BACK ARE INOPERATIVE. REPLACED THE EMERGENCY EGRESS LIGHTS, OPERATIONS CHECK NO RMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102200122 19991022 00122 NM 1999 10 22 99UAL900502 1 19991001 A 3231 RETRACT MECH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG DOORS OUT OF ADJUST A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 331UA 24192 CREW REPORTED, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH THE GEAR UP. WHEN THE HANDLE WAS PLACED TO THE OFF POSITION, THE NOSE GEAR DROPPED OUT OF THE WHEEL WELL. *S/D* MAINTENANCE RE-RIGGED NOSE GEAR DOORS PER APPLICABLE AIRCRAFT MAIN TENANCE MANUAL. CHECKS OK ON GEAR RETRACTION. NOSE LANDING GEAR LIGHT OK AND GEAR LOCKS OVER CENTER. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102200123 19991022 00123 NM 1999 10 22 99UAL900503 1 19991001 A 2530 FOOD CART BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 540UA 25252 AFT GALLEY ELECTRICAL PIGTAIL GAVE OFF SPARKS AND ODOR. *S/D* INSPECTED CABLES AT ALL POSITIONS AND FOUND NO EVIDENCE OF BURNED, BENT, DAMAGED. SUSPECT BAD CARTS. REMOVED AND REPLACED FOOD CARTS. 2 L 7 2 4F 4 F RT A2NM E17NE 1999102200124 19991022 00124 NM 1999 10 22 99UAL900504 1 19991001 A 5730 65C35221 ACCESS PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT WING LOOSE A UALA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 WP 29 7451U 21905 PASSENGER REPORTED FUEL DRAINING FROM LEFT WING TIP. CREW REPORTED QUANTITY DECREASING. RETURNED TO ABQ. *S/D* TORQU ED NR 15 LEFT HAND WING ACCESS PANEL. 2 L 7 3 4F 4 F A3WE E2EA 1999102200125 19991022 00125 1999 10 22 99UAL900505 4 19991004 A 3425 HSI BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE LT COCKPIT FLAGGED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 992UA 22089 THE CAPTAIN'S HSI AND THE FIRST OFFICER'S RMI FLAGS INTERMITTENTLY CAME IN VIEW. 2 L 7 2 4F 4 F A16WE E2EA 1999102200126 19991022 00126 NM 1999 10 22 99UAL900506 1 19991001 A 3320 335233 BALLAST DEIHL PCB77411069 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ROW 43 HJ FAILED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 785UA 26954 CREW REPORTS A BAD SMELL BY ROWS 42HJ AND 43CDE. SMELLS ELECTRICAL IN AREA OF CEILING PANELS. *S/D* INDIRECT CEILING LIGHT BALLAST AT ROW 43HJ FAILED. ASSEMBLY WAS REPLACED AND SYSTEM OPERATES NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200127 20001010 00127 NM 2000 10 10 99UAL900507 1 19990130 A 4940 A703CD RELAY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU START DEFECTIVE A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 668UA 30024 61877 HIGH ALTITUDE START OF APU UNSUCCESSFUL X3. *S/D* APU IN THE SHOP WAITING FOR FINDINGS. APU WILL BE TESTED IN TEST CE LL AS RECEIVED, TO VERIFY IF THERE IS A DEFECTIVE COMPONENT. DUE TO MANY APU BATTERY AND CHARGER PROBLEMS, IT IS SUSPEC TED THAT THE BATTERY VOLTAGE WAS TOO LOW TO CRANK A COLD SOAKED APU. HOWEVER, THE APU STARTED ON THE GROUND AFTER ARRIV AL. AFTER APU REPLACEMENT ON OCTOBER 2, IT FAILED ALTITUDE START, VOLTAGE AT STARTER TERMINALS WAS 10.5V WHICH IS TOO L OW TO CRANK APU TO SPEED. THE STARTER WAS ALSO REPLACED AS A PRECAUTION, DUE TO LOW BATTERY VOLTAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999102200128 19991022 00128 NM 1999 10 22 99UAL900508 1 19991004 A 2913 4205401 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 HYD SYS OVERHEATED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 575UA 26689 LANDED UNDER AMBER ALERT DUE TO A NR 2 HYDRAULIC SYSTEM FAILURE. S/D, THE PARTING SURFACE OF THE ENGINE DRIVEN PUMP FAI LED WHEN THE PUMP OVERHEATED, ALLOWING FLUID TO LEAK. CAUSE OF OVERHEAT IS UNKNOWN BUT MOST LIKELY A RESULT OF A FAILED SHAFT BEARING. THE PUMP WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999102200129 19991022 00129 NM 1999 10 22 99UAL900509 1 19991005 A 5311 FRAME BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 760.95 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7452U 21906 A CRACK WAS FOUND IN THE BODY STATION 760.95 FRAME STUB WEB (P/N 65-16325-18) AT THE CORNER OF AN EXISTING ACCESS HOLE C UTOUT. THE CRACK WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APP ROVED BY TIMCO'S DER WITH AN 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999102200130 19991022 00130 NM 1999 10 22 99UAL900510 1 19991007 A 7933 11225146000 OIL TEMP BULB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 338UA 24242 726390 ERRATIC OIL TEMPERATURE INDICATION ON NUMBER TWO ENGINE. REPLACED THE TEMPERATURE BULB AND PERFORMED OPERATIONAL CHECK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102200131 19991022 00131 WP 1999 10 22 MWEA99672 1 19991013 A 5312 59101307 BULKHEAD SKIN DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 TOOL MARKS PRESENT ON AFT FACE OF AFT PRESSURE BULKHEAD SKIN. MAINTENANCE BLENDED OUT TOOL MARKS. 2 L 7 2 4F A6WE 1999102200132 19991022 00132 WP 1999 10 22 MWEA99673 1 19991013 A 5210 49139471 HINGE DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 PASSENGER DOOR UPPER HINGE FITTING (FUSELAGE SIDE) WAS CRACKED. MAINTENANCE REMOVED AND REPLACED HINGE FITTING. 2 L 7 2 4F A6WE 1999102200133 19991022 00133 WP 1999 10 22 MWEA99674 1 19991013 A 5220 59131951 PAN DOUG DC9 DC932 3022066 WP EMER EXIT DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CRACK ON INNER PAN LOWER FORWARD CORNER OF RIGHT AFT OVERWING EMERGENCY EXIT DOOR. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999102200134 19991022 00134 WP 1999 10 22 MWEA99675 1 19991013 A 5230 591014211 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 401ME 47133 FORWARD CARGO DOOR JAMB WEB HAS MISDRILLED HOLES ON OUTSIDE. MAINTENANCE REMOVED AND REPLACED FORWARD CARGO DOOR JAMB W EB. 2 L 7 2 4F A6WE 1999102200135 19991022 00135 WP 1999 10 22 MWEA99676 1 19991013 A 5320 953017217 JAMB DOUG DC9 DC932 3022066 WP GALLEY DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 GALLEY SERVICE DOOR JAMB SKIN WAS CRACKED AT LOWER AFT CORNER. MAINTENANCE FABRICATED AND INSTALLED REPAIR FILLER AND D OUBLER. 2 L 7 2 4F A6WE 1999102200136 19991022 00136 WP 1999 10 22 MWEA99677 1 19991013 A 5312 59174637 JAMB DOUG DC9 DC932 3022066 WP VENTRAL DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 VENTRAL DOOR FRAME SKIN IS CRACKED ON FORWARD SIDE BELOW RIGHT HAND TOP CORNER. MAINTENANCE SPLICED IN NEW SECTION OF D OOR JAMB. 2 L 7 2 4F A6WE 1999102200137 19991022 00137 WP 1999 10 22 MWEA99678 1 19991013 A 5320 99155872 WINDOW FRAME DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 CABIN WINDOW FRAME AT SEAT 24 RIGHT HAS EVIDENCE OF LIGHTNING STRIKE. MAINTENANCE BLENDED OUT LIGHTNING STRIKE DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999102200138 19991022 00138 WP 1999 10 22 MWEA99679 1 19991013 A 5330 9911535503 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE NICKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 WINDOW BELT SKIN HAS SMALL NICK AT LOWER AFT CORNER ADJACENT TO WINDOW 33 LEFT. MAINTENANCE BLENDED OUT NICK AND INSTAL LED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999102200139 19991022 00139 WP 1999 10 22 MWEA99680 1 19991013 A 5210 4955948IN HOUSING DOUG DC9 DC932 3022066 WP PAX DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FORWARD PASSENGER DOOR HOLD OPEN HOOK HOUSING HAS CHAFE MARK ON BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED FORWARD P ASSENGER DOOR HOLD OPEN HOOK HOUSING. 2 L 7 2 4F A6WE 1999102200140 19991022 00140 WP 1999 10 22 MWEA99682 1 19991013 A 5240 395368633 BEAM DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 GALLEY SERVICE DOOR NR 4 BEAM HAD A CRACK ON FORWARD END. ATC FABRICATED AND INSTALLED FITTING AND DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999102200141 19991022 00141 NM 1999 10 22 DL733992223 1 19991005 A 2120 UNKNOWN 0802032501 BOEING 737 737347 1384647 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 304WA 4066 23345 PAX AT 2C SMELLED SLIGHT ODOR IN CABIN, F/O REPORTED A FAINT ODOR, BUT COULD NOT RECOGNIZE WHAT TYPE. RECIRCULATION FAN AND CABIN BALLAST LIGHT TURNED OFF. NR 2 TR C/B POPPED, DID NOT RESET DUE TO PREVIOUS WRITE-UP. ON PREVIOUS FLT 1450 IAH, REPLACED NR 2 TR FOR POPPED C/B. BORROWED TR PN 244001015 SN 4066. THIS PART FAILED ON FLT 1895 SLC CAUSING SMOK E IN CABIN. REPLACED BORROWED TR SN 4066 WITH DL PART SN 2299. CKD WIRING PER WDM FROM NR 2 TRCB TO TR. ALL PWR AND G NDS CHKD GOOD. PHASE TO PHASE GOOD. 2 L 7 2 4F RT A16WE 1999102200142 19991022 00142 1999 10 22 DL76L992224 4 19991006 A 2565 BATTERY 20131A BOEING 767 767332 1382001 NM ESCAPE SLIDE INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 199DN 28456 RIGHT EMERGENCY ESCAPE SLIDE SQUIB WOULD NOT TEST ON TEST 1. REPLACED BATTERY, TEST CHECKS OK. 2 L 7 2 4F RT A1NM 1999102200143 19991022 00143 1999 10 22 DL76L992225 4 19991006 A 2565 CHARGER BPS73 BOEING 767 767332 1382001 NM ESCAPE SLIDE INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 199DN 43535 28456 LEFT EMERGENCY ESCAPE SPOILER SQUIB WOULD NOT TEST ON TEST 2. REPLACED CHARGER, TEST CHECKS OK. 2 L 7 2 4F RT A1NM 1999102200144 19991022 00144 NM 1999 10 22 DL72S992226 1 19991006 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1045 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 1.75 CRACK FUSELAGE SKIN SAT 1045 STRINGER 28L. REPAIRED PER MM 53-30-3 FIG 25. 2 L 7 3 4F A3WE 1999102200145 19991022 00145 NM 1999 10 22 DL72K992228 1 19991006 A 3350 900835 BATTERY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 525DA 21585 ON L/O, FOUND FWD OVERWING EMERGENCY LIGHT OUT. REPLACED SLED ASSY AND BATTERY. 2 L 7 3 4F A3WE 1999102200146 19991022 00146 NM 1999 10 22 DLM88992229 1 19991006 A 3244 M88M TIRE DOUG MD88 MD88 3023688 NM MLG FAILED A DALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 27 910DE 53419 NUMBER 4 TIRE LOST RECAP AFTER T/O, DAMAGE TO BRAKE, FLAP, AND ENGINE FAN BLADES. REPAIRED ALL, REPLACED FAN. 2 L 7 2 4F RT A6WE 1999102200147 19991022 00147 NM 1999 10 22 DL733992230 1 19991006 A 5330 657377678 SKIN BOEING 737 737301 1384611 NM BS 807 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948WP 23259 FUSELAGE SKIN FS 807-907, STRINGER 25L-27R, SKIN GOUGE REPAIR. THE FUSELAGE SKIN WAS BADLY SCRATCHED AND GOUGED FROM FS 807 TO FS 907 BETWEEN STRINGERS 25L AND 27R DUE TO IMPACT WITH GROUND EQUIPMENT. THE SKIN WAS CUT AT FS 807 BETWEE N STRINGER 25L AND 27R AND THE AFT SECTION REMOVED TO THE EXISTING BUTT SPLICE AT FS 907. A NEW SECTION OF SKIN WAS SPL ICED IN WITH AN EXTERNAL REPAIR STRAP PER ER/A 368360-14, REV A. 2 L 7 2 4F RT A16WE 1999102200148 19991022 00148 NE 1999 10 22 DLL10992231 2 19991005 A 7200 ENGINE M06157 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 MALFUNCTIONED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 733DS AM623 193C1224 010399 SHUT DOWN NR 2 ENGINE IN CRUISE DUE TO FILTER PRESSURE LIGHT ON S/O PANEL AS WELL AS LOW OIL QUANTITY, QUANTITY DECRE ASING. REPLACED NR 2 ENG GEARBOX HIGHSPEED EXTERNAL PER OPN NR 62304, 72312, REF ITEM 4,14 THIS LOG ITEM 4. CHIP DET ECTORS REMOVED AND INSTALLED ITEM 14 TESTS 1-3-9-18-20 DUE C/W ALL TEST. 2 L 7 3 4F 4 F A23WE E12EU 1999102200149 19991022 00149 NM 1999 10 22 DL72K992232 1 19991007 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 496DA 21076 AISLE EMERGENCY LIGHT OUT AT OVERWING EXIT. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1999102200150 19991022 00150 NM 1999 10 22 DL72S992233 1 19990724 A 5753 652163361 SKIN BOEING 727 727232 1384082 NM TE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 LWR L/E SKIN WORN ON I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999102200151 19991022 00151 NM 1999 10 22 DLM88992234 1 19991008 A 5330 595305077 SKIN DOUG MD88 MD88 3023688 NM BS 229 - 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DE 53421 THE FUSELAGE SKIN WAS DENTED BETWEEN FS 229 AND 237 BETWEEN STRINGERS 18L AND 19L. THE DAMAGE WAS REPAIRED PER ERA 3336 63-14 AT HMV. 2 L 7 2 4F RT A6WE 1999102200152 19991022 00152 NM 1999 10 22 DL733992235 1 19991008 A 5711 6545321516 SPAR BOEING 737 737347 1384647 NM RT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313WA 23599 THE RIGHT WING REAR SPAR WAS GOUGED AT THE MLG BEAM AFT ATTACH FITTING. THE DAMAGE WAS REPAIRED AT MV PER ER/A 333653-1 4. 2 L 7 2 4F RT A16WE 1999102200153 19991022 00153 NM 1999 10 22 DL733992236 1 19991008 A 5313 STRINGER BOEING 737 737347 1384647 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313WA 23599 THE LEFT STRINGER 18A WAS FOUND CRACKED AT FS 727. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 333643-14. 2 L 7 2 4F RT A16WE 1999102200154 19991022 00154 NM 1999 10 22 DL733992237 1 19991008 A 5312 65163007 BULKHEAD BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313WA 23599 THE FS 178 BULKHEAD WEB AND SIDE CHORD WERE FOUND CRACKED. THE DAMAGE WAS REPAIRED AT MV PER ERA 333649-14. 2 L 7 2 4F RT A16WE 1999102200155 19991022 00155 NM 1999 10 22 DLM88992241 1 19991008 A 3244 MD88M TIRE DOUG MD88 MD88 3023688 NM MLG FAILED A DALA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 909DE 53418 AT ROTATION SPEED, ENCOUNTERED AN UNSAFE GEAR INDICATION ON THE RIGHT MAIN LANDING GEAR. LEFT THE GEAR DOWN AND WENT TH ROUGH ALL APPLICABLE CHECKLISTS PER POM. NUMBER 3 TIRE SHED RETREAD AND DAMAGED PROX SWITCH AND CONDUIT. REPLACED SAME . 2 L 7 2 4F RT A6WE 1999102200156 19991022 00156 NM 1999 10 22 DL757992242 1 19991009 A 2530 OVEN BOEING 757 757232 1384965 NM GALLEY STEAMING A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 646DL 24217 AFT F/A REPORTED SMOKE NEAR CEILING JUST PRIOR TO TAKEOFF. FOUND EXCESSIVE MOISTURE/STEAM COMING FROM MEALS IN THE OVEN S. 2 L 7 2 4F RT A2NM 1999102200157 19991022 00157 NE 1999 10 22 DL72S992243 2 19991009 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 544DA 70270 22493 687397 ON CLIMB-OUT, NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED. S/D ENG PER POM. OIL FILTER FOUND CLEAN. REPLACED SAME, E NGINE RUN CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999102200158 19991022 00158 NM 1999 10 22 DL73K992245 1 19991009 A 2560 61020 BATTERY BOEING 737 737247 138448D NM FLASHLIGHT DISCHARGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 243WA 23517 AFT TOP EMERGENCY FLASHLIGHT INDICATOR NOT FLASHING. REPLACED BATTERY, NOW CKS OK. 2 L 7 2 4F A16WE 1999102200159 19991022 00159 NM 1999 10 22 DL76P992247 1 19991009 A 3350 NONE CONNECTOR BOEING 767 767332 1382001 NM ROW 35 DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 143DA 25991 EMERGENCY LIGHTS INOP LT AND RT SIDES ROW 35 AFT. REPAIRED EMERGENCY LIGHT CONNECTOR AT 40FG. OPS CK GOOD. 2 L 7 2 4F RT A1NM 1999102200160 19991022 00160 WP 1999 10 22 DLL10992250 1 19991010 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP PAX DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 193C1173 ON L/O, FOUND SEVERAL EMERGENCY LIGHT STRIPS IN 1ST CLASS AND COACH INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK AT R1 DOOR, CKS GOOD. 2 L 7 3 4F A23WE 1999102200161 19991022 00161 NM 1999 10 22 DL72S992251 1 19991010 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM AIRSTAIR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 406DA 21150 AFT AIRSTAIR EMERGENCY LIGHTS INOP. REPLACED BATTERY'S, OPS NOW OK. 2 L 7 3 4F A3WE 1999102200162 19991022 00162 NM 1999 10 22 DL72S992252 1 19991010 A 3350 90082 POWER SUPPLY BOEING 727 727232 1384082 NM ROW 2 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 498DA 21142 CABIN OVERHEAD EMERGENCY LIGHTS INOP ROW 2. REPLACED POWER SUPPLY AND BATTERY PACK. 2 L 7 3 4F A3WE 1999102200163 19991022 00163 NM 1999 10 22 DL72L992253 1 19991009 A 5330 6518420763 SKIN BOEING 727 727232 1384082 NM BS 348 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 FUSELAGE SKIN ASSY L1 DOOR CUTOUT, FS 348 LWR AFT CORNER, CRACK REPAIR. THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT (FS 348) WAS FOUND WITH A 4.5 INCH CRACK IN THE SKIN AND BEAR STRAP. THE CRACK WAS CUT OUT OF ALL LAYERS AND AN EXTERNAL DOUBLER AND TRIPLER INSTALLED TO REPAIR THE AREA PER ER/A 368449-14, REV A. 2 L 7 3 4F A3WE 1999102200164 19991022 00164 NM 1999 10 22 DL72L992254 1 19991010 A 3350 0201720002 SOCKET BOEING 727 727232 1384082 NM SEAT 10 FAILED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 505DA 21307 PILOT REPORT, FIRST CLASS SECTION EMERGENCY TRACK LIGHTING INOP. FOUND BAD SOCKET AT 10DEF REPLACED FUSE AT FWD POWER S UPPLY PACK. SYSTEM OPS NORMAL DEFERED SOCKET AT 10DEF PER MEL 33-00-17B SOCKET DISCONECTED AND WIRE HARNESS SECURED. R EPLACED SEAT MOUNTED LIGHT ASSY. 2 L 7 3 4F A3WE 1999102200165 19991022 00165 NM 1999 10 22 DL72S992255 1 19991011 A 3240 BRAKE 2114730PT3 BOEING 727 727232 1384082 NM MLG FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 532DA DL313AD 22045 ON LANDING, NR2 BRAKE LOCKED AND BLEW NR 2 MAIN TIRE. REPLACED NR 2 BRAKE, NR 1 AND NR 2 WHEEL ASSY. T/S NR 2 WHEEL A NTI-SKID SYSTEM. OPERATION NORMAL. 2 L 7 3 4F A3WE 1999102200166 19991022 00166 NM 1999 10 22 DL72S992256 1 19991006 A 5755 MOUNT BOEING 727 727232 1384082 NM SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 AT HMV, FOUND NR 13 SPOILER MOUNT BOX IS LOOSE AT LOWER ATTACH BOLTS. REPAIRED PER MM 57-42-0 PG 804. 2 L 7 3 4F A3WE 1999102200167 19991022 00167 NM 1999 10 22 DL72S992257 1 19991006 A 5755 BOLT BOEING 727 727232 1384082 NM SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 AT HMV, FOUND RW NR 12 SPOILER MOUNT BOX I/B LOWER ATTACH BOLT HAS PLAY. REPAIRED PER MM 57-42-0 PG 804. 2 L 7 3 4F A3WE 1999102200168 19991022 00168 NM 1999 10 22 DL72S992258 1 19991006 A 5755 BOLT BOEING 727 727232 1384082 NM SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 AT HMV, FOUND NR 14 SPOILER MOUNT BOX IS LOOSE AT LOWER ATTACH BOLTS. REPAIRED PER MM 57-42-0 PG 804. 2 L 7 3 4F A3WE 1999102200169 19991022 00169 NM 1999 10 22 DL76L992260 1 19991010 A 3350 FUSE BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 AFT EMERGENCY TRACK LIGHTS FAIL TEST. REPLACED FUSE AND LIGHT SOCKET AT 35B. CKS GOOD. 2 L 7 2 4F RT A1NM 1999102200170 19991022 00170 NM 1999 10 22 DL72S992261 1 19991011 A 5755 659892428 ANGLE BOEING 727 727232 1384082 NM SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 NR 14 SPOILER ACT O/B MOUNT CASTING CRACKED {ATTACH ANGLE}. REPLACED ANGLE PER M/M 57-42-0.. 2 L 7 3 4F A3WE 1999102200171 19991022 00171 NM 1999 10 22 DL72S992262 1 19991012 A 5330 65545827 SKIN BOEING 727 727232 1384082 NM BS 1100 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 THE FUSELAGE SKIN WAS FOUND WORN AT FS 1100 AND STRINGER 1. REPAIRED PER ERA 333691-14AD. 2 L 7 3 4F A3WE 1999102200172 19991022 00172 NM 1999 10 22 DL733992263 1 19991011 A 5312 65163007 BULKHEAD BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313WA 23599 THE FS 178 BULKHEAD WEB WAS FOUND TO BE CRACKED IN 3 PLACES. THE LHS CHORD WAS ALSO FOUND CRACKED. THE SIDE CHORD WAS REPAIRED PER SB 737-53A1173 AND THE WEB WAS REPAIRED PER ERA 333649-14. 2 L 7 2 4F RT A16WE 1999102200173 19991022 00173 NM 1999 10 22 DL733992265 1 19991011 A 2761 ACTUATOR 65C268643 BOEING 737 737347 1384647 NM SPOILER CRACKED A DALA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 308WA 0486 23441 AFTER LANDING, LOST HYD SYS A GROUND PERSONNEL REPORTED LEAK RT WING AREA. FOUND NR 8 GROUND SPOILER ACT LEAKING, REPLA CED SAME. . 2 L 7 2 4F RT A16WE 1999102200174 19991022 00174 NM 1999 10 22 DL72S992266 1 19991012 A 5320 WEB BOEING 727 727232 1384082 NM TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 FOUND ON D2 LETTER CK, .25 INCH CRACK LEFT VERTICAL TORQUE BOX WEB LIGHTENING HOLE STA 1323.. ALSO, RT VERTICAL TORQUE BOX WEB AT LIGHTENING HOLE AT STA 1233 CRACKED .25 INCH. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999102200175 19991022 00175 NE 1999 10 22 DL757992267 2 19991013 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA E C ENGINE SHUTDOWN ABORTED TAKEOFF A FLAME/FIRE TO TAKEOFF 1 SO 27 686DA 41416 27589 716432 ON ENGINE RUN-UP PRIOR TO TAKEOFF, GOT A COMPRESSOR STALL AND SMOKE AND FLAMES OUT OF INLET AND EXHAUST. CREW PULLED OF F ACTIVE ON TO TAXIWAY SAW OIL PRESS AT ZERO AND THEN SHUT ENG DOWN. FIRE DEPT RESPONDED AND SHOT FIRE RETARDANT AND WA TER INTO INTAKE AND EXHAUST. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999102200176 19991022 00176 NE 1999 10 22 DLM88992268 2 19991013 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 957DL 16360 49976 726865 NR 1 ENGINE FAILED TO ACHIEVE FULL THRUST (ONLY 90 PERCENT AND 1.90 EPR). REPLACED ENGINE FOR CRACKED FUEL MANIFOLD. 2 L 7 2 4F 4 F RT A6WE E9NE 1999102200177 19991022 00177 NM 1999 10 22 DL767992269 1 19991013 A 3240 SWITCH 014203094 BOEING 767 767232 1385132 NM BRAKE INOPERATIVE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 106DA 22218 ABORTED T/O DUE TO T/O CONFIG HORN, PARKING ON EICAS PARKING BRAKE HANDLE WAS DOWN. REPLACED PARKING BRAKE SWITCH PER M /M 32-44-08 TEST OK PER M/M AND PERFORMED T/O CONFIG TEST, ALL OPS CKS OK. 2 L 7 2 4F RT A1NM 1999102200178 19991022 00178 1999 10 22 DL76L992270 4 19991013 A 3414 4040800911 COMPUTER BOEING 767 767332 1382001 NM E/E BAY FAILED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 193DN 28450 NO AIRSPEED INDICATION CAPTS SIDE ON T/O ROLL. REPLACED CADC. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999102200179 19991022 00179 NM 1999 10 22 SCNA99126 1 19991012 A 2510 SIDEWALL BOEING 727 7272J4 1384006 NM RT COCKPIT LOOSE A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 15 288SC 20765 DURING TAKEOFF ROLL, A SIDEWALL PANEL CAME LOOSE ON THE RIGHT SIDE OF THE FIRST OFFICER'S SEAT JAMMING THE RIGHT RUDDER PEDALS. ABORTED TAKEOFF. INSTALLED FASTENERS AS REQUIRED ON THE PANEL AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999102200180 19991022 00180 NM 1999 10 22 VNAA9910007 1 19991013 A 2120 AIR DIST DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ODOR A VNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 460PS 3061 WHILE AT THE GATE AND AFTER STARTING BOTH ENGINES AND REMOVING GROUND POWER, THE FLIGHT CREW REPORTED A STRONG ELECTRICA L / FIRE SMELL. MAINTENANCE INSPECTED ALL ELECTRICAL COMPONETS OF THE AFFECTED SYSTEMS AND PERFORMED GROUND OPERATIONAL CHECKS WITH NO DISCREPANCIES DETECTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102200181 19991022 00181 NM 1999 10 22 VNAA9910006 1 19991012 A 2120 AIR DIST DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT SMOKING A VNAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 427JS 3039 ON DESCENT INTO CAE WITH ENVIROMENTAL SYSTEMS SET TO FULL COLD, THE FLIGHT CREW REPORTED SMOKE ENTERING THE COCKPIT. TH E FLIGHT LANDED IN CAE WITHOUT ANY DIFFICULTIES. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS WITH THE AIRCR AFT. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102200200 19991022 00200 CE 1999 10 22 99ZZZX3980 1 19990914 A 3230 1EN18 SWITCH LEAR 35 35A 5170602 CE RT MLG FAILED A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 959SA 076 MEM - RT MAIN GEAR NOT SHOWING DOWN AND LOCK, RETURNED TO CMH AND LANDED, NO PROBLEMS. REMOVED AND REPLACED SWITCH. OP S CHECK GOOD. 2 L 7 2 4F A10CE 1999102200232 19991022 00232 EU 1999 10 22 99ZZZX4012 1 19990915 A 2910 MY20743103 LINE AMD FALC20 FALCON20C 273004 EU AIRBRAKE CRACKED A KKFA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 70CK 11127 128 AIRCRAFT EXPERIENCED TOTAL LOSS OF NR 1 HYDRAULIC SYSTEM PRESSURE AND QUANTITY. REPLACED CRACKED NR 4 HYDRAULIC HARD LI NE AT AIRBRAKE DISTRIBUTER WITH NEW. CLEANED AND CHECKED HYDRAULIC SYSTEM FILTERS. REPLACED NR 1 ENGINE DRIVEN HYDRAUL IC PUMP WITH SERVICEABLE UNIT AS A PRECAUTIONARY MEASURE. BLED SYSTEM AND LEAKED CHECKED IAW FALCON 20 MM. 2 L 7 2 4F RT A33EU 1999102200234 19991022 00234 SO 1999 10 22 99ZZZX4014 1 19990924 A 7603 454218 CONTROL CABLE PIPER PA31 PA31350 7103110 SO THROTTLE FAILED A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 3547C 318052018 CLE - RT ENGINE THROTTLE CABLE BROKE GOING INTO CLEVLEAND, OH. REMOVED AND REPLACED THROTTLE CABLE. OPS CHECKS GOOD. 1 L 7 2 3O A20SO 1999102200239 19991022 00239 NM 1999 10 22 SWAA991708 1 19991014 A 7722 TLC16500 LEAD BOEING 737 7373G7 1384595 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE EGT CORRODED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 691WN 23781 856305 AIR TURNBACK, AFTER TAKEOFF, NR 1 ENG EGT IND OVERTEMPED TO 955 DEGREES FOR APPROX 2 SECONDS. C/W HOT SECTION BORESCOPE INSPECTION, CALIBRATED EGT IND, TROUBLESHOT AND REMOVED AND REPLACED NR 1 ENG EGT SOFT LEAD AT ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102200240 19991022 00240 NM 1999 10 22 SWAA991709 1 19991014 A 2720 6545160 PCU BOEING 737 7373H4 1384600 NM RUDDER INOP A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 SW 07 300SW 22940 ABORTED TAKEOFF, DURING TAKEOFF, RUDDER WAS HARD TO OPERATE. REMOVED AND REPLACED RUDDER PCU AND RUDDER CENTERING AND F IELD ASSY. 2 L 7 2 4F RT A16WE 1999102200241 19991022 00241 NM 1999 10 22 SWAA991710 1 19991013 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM ROW 2,12,&22 CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 711HK 27845 DURING SCHEDULED BC2 CHECK, FOUND EEPLS STRIPS CRACKED AT ROWS 2, 12, 22. REMOVED AND REPLACED LIGHT STRIPS PER MM. 2 L 7 2 4F RT A16WE 1999102200242 19991022 00242 NM 1999 10 22 SWAA991711 1 19991013 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 8 - RBL 6.7. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999102200243 19991022 00243 NM 1999 10 22 SWAA991712 1 19991013 A 5315 6546804 FLOOR BEAM BOEING 737 7373Y0 1384671 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND BS 947 FLOORBEAM UPPER SECTION CORRODED AT LBL 9. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999102200244 19991022 00244 NM 1999 10 22 SWAA991713 1 19991014 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 11- RBL 7. REMOVED AND REPLACED BULKHEAD WEB PER ACO 71 54-53. 2 L 7 2 4F RT A16WE 1999102200245 19991022 00245 NM 1999 10 22 SWAA991714 1 19991014 A 5311 65C25723 RIB BOEING 737 7373Y0 1384671 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE CENTER SECTION, BS 616, RBL 60 RIB ASSY CRACKED. REPAIRED RIB SECTION PER T I-153-018. 2 L 7 2 4F RT A16WE 1999102200246 19991022 00246 NM 1999 10 22 SWAA991715 1 19991014 A 5320 65C27314 CLIP BOEING 737 7373Y0 1384671 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED, BS 294, STRINGERS 13L AND 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 1999102200247 19991022 00247 NM 1999 10 22 SWAA991716 1 19991014 A 5315 6546804 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOOR BEAM, BS 986.5, LBL 16 - LBL 60. REPAIRED BEAM PER TI-453-037. 2 L 7 2 4F RT A16WE 1999102200248 19991022 00248 NM 1999 10 22 SWAA991717 1 19991013 A 5312 963820 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND THROUGH EDDY CURRENT INSP, BS 178 BULKHEAD SIDE CHORD CRACKED, LBL 26, AND RBL 26. R EMOVED AND REPLACED SIDE CHORD SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 1999102200249 19991022 00249 NM 1999 10 22 SWAA991718 1 19991014 A 2560 6556685 HOLDER BOEING 737 7373H4 1384600 NM PAX DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 631SW 27706 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR HOLDER LOOSE. REMOVED AND REPLACED GIRT BAR H OLDER FASTENER PER MM. 2 L 7 2 4F RT A16WE 1999102200250 19991022 00250 NM 1999 10 22 SWAA991719 1 19991014 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED, BS 520, STRINGERS 19L AND 19R. REMOVED AND REPLACED ST RINGER CLIPS PER SRM. 2 L 7 2 4F A16WE 1999102200251 19991022 00251 NM 1999 10 22 SWAA991720 1 19991013 A 5610 571762 WINDOW BOEING 737 7377H4 NM COCKPIT LEAKING A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 714CB 27848 AIR TURNBACK, LOUD PRESS LEAK NOISE AT F/O'S SLIDING WINDOW AT 12,000 FEET. CABIN PRESSURE SYSTEM WAS OK. OPENED AND I NSPECTED F/O'S SLIDING WINDOW. NO DEFECTS NOTED. PRESSURIZED AIRCRAFT NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 1999102200252 19991022 00252 NM 1999 10 22 SWAA991693 1 19991011 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT OVERWING AND AFT END ON CABIN. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F A16WE 1999102200253 19991022 00253 NM 1999 10 22 SWAA991694 1 19991011 A 5320 6558280 ANGLE BOEING 737 737301 1384611 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE ANGLE CRACKED, BS 360, LBL 68, WL 230. REMOVED AND REPLACED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 1999102200254 19991022 00254 NM 1999 10 22 SWAA991695 1 19991011 A 5320 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM BS 787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FUSELAGE SHEAR TIE, BS 787, STRINGER 27R. REPAIRED SHEARTIE PER SRM. 2 L 7 2 4F RT A16WE 1999102200255 19991022 00255 NM 1999 10 22 SWAA991696 1 19991011 A 5311 6545871 FRAME BOEING 737 7373Y0 1384671 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FUSELAGE FRAME, BS 294, RBL 54 AT FWD GALLEY DOOR CUT OUT. REPAIRED FRAME PE R SRM. 2 L 7 2 4F RT A16WE 1999102200256 19991022 00256 NM 1999 10 22 SWAA991697 1 19991012 A 5754 6573714 SKIN BOEING 737 7372H4 138448C NM NR 4 LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND NR 4 L/E SLAT DELAMINATED ON OUTBOARD UPPER CORNER. REPAIRED SLAT PER SRM. 2 L 7 2 4F A16WE 1999102200257 19991022 00257 NM 1999 10 22 SWAA991698 1 19991012 A 3350 101114 LENS BOEING 737 7372H4 138448C NM ROW 10F FADED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT SIGN LENS FADED BY SEAT 10F. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F A16WE 1999102200258 19991022 00258 NM 1999 10 22 SWAA991699 1 19991012 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM ROW 10 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROW 10. RELAMPED PER MM. 2 L 7 2 4F A16WE 1999102200259 19991022 00259 NM 1999 10 22 SWAA991700 1 19991012 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM SERVICE DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS LOOSE. TIGHTENED BRACKETS PER MM. 2 L 7 2 4F A16WE 1999102200260 19991022 00260 NM 1999 10 22 SWAA991701 1 19991012 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5 AND LBL 5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999102200261 19991022 00261 NM 1999 10 22 SWAA991702 1 19991013 A 3350 BR2013 LIGHT BOEING 737 7373A4 1384585 NM ROW 7 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 677AA 23289 EEPLS TRACK LOOSE AT ROW 7. RESECURED TRACK LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102200262 19991022 00262 NM 1999 10 22 SWAA991703 1 19991013 A 5730 65C26539 SKIN BOEING 737 7373Y0 1384671 NM WS 345&475 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND RT WING UPPER SURFACE SKIN CORRODED AROUND IN SPAR, WS 345 AND WS 475. REPAIRED SKIN PER SWA RA NR 1-357-0754, REVISION 1. 2 L 7 2 4F RT A16WE 1999102200263 19991022 00263 NM 1999 10 22 SWAA991704 1 19991013 A 2560 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 FWD SERVICE DOOR EVACUATION SLIDE LOOSE AT DOOR. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102200264 19991022 00264 NM 1999 10 22 SWAA991705 1 19991013 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999102200265 19991022 00265 NM 1999 10 22 SWAA991706 1 19991013 A 3350 07912 LIGHT BOEING 737 7372H4 138448C NM ROW 18 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK MISSING AT ROW 18. INSTALLED TRACK COVER PER MM. 2 L 7 2 4F A16WE 1999102200266 19991022 00266 NM 1999 10 22 SWAA991707 1 19991013 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM SERVICE DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED C3 CHECK, FOUND FWD AND AFT SERVICE DOOR GIRT BAR FLOOR ATTACH BRACKETS LOOSE. TIGHTENED BRACKETS PER MM. 2 L 7 2 4F A16WE 1999102200267 19991022 00267 NM 1999 10 22 SWAA991689 1 19991009 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 EEPLS ILLUMINATED WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED FWD OVERHEAD BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999102200268 19991022 00268 NM 1999 10 22 SWAA991690 1 19991009 A 5753 6573732 SKIN BOEING 737 7373H4 1384600 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C2 CHECK, FOUND RT OUTBOARD AFT FLAP DELAMINATED AT INBOARD CORNER. REPAIRED FLAP PER MM. 2 L 7 2 4F RT A16WE 1999102200269 19991022 00269 NM 1999 10 22 SWAA991691 1 19991010 A 2560 6547654 LATCH BOEING 737 7375H4 138449D NM COCKPIT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 F/O'S EMERGENCY ESCAPE ROPE DOOR LATCH BROKEN. REMOVED AND REPLACED PANEL ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102200270 19991022 00270 NM 1999 10 22 SWAA991692 1 19991010 A 5315 6546804 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM, BS 1006, LBL 19. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999102200271 19991022 00271 NM 1999 10 22 SWAA991682 1 19991009 A 3350 P4010021 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 ONE FWD AND ANOTHER AFT EMERGENCY FLASHLIGHTS FOUND ILLUMINATED. REMOVED AND REPLACED BOTH FLASHLIGHT BATTERIES PER MM. 2 L 7 2 4F A16WE 1999102200272 19991022 00272 NM 1999 10 22 SWAA991683 1 19991008 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 725SW 27857 FWD EEPLS TRACK LOOSE. RESECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 1999102200273 19991022 00273 NM 1999 10 22 SWAA991684 1 19991008 A 5330 6575774 SKIN BOEING 737 7372H4 138448C NM BS 887 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED, BS 887, BETWEEN STRINGERS 25R-26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999102200274 19991022 00274 NM 1999 10 22 SWAA991685 1 19991008 A 5320 6545871 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT LOWER END. REPAIRED FRAME PER BOEING DRAWING. 2 L 7 2 4F RT A16WE 1999102200275 19991022 00275 NM 1999 10 22 SWAA991686 1 19991008 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 17 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT ROW 17. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999102200276 19991022 00276 NM 1999 10 22 SWAA991687 1 19991008 A 5315 6546804 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOORBEAM UPPER SURFACE CORRODED BETWEEN LBL 15 - RBL 58. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999102200277 19991022 00277 NM 1999 10 22 SWAA991688 1 19991009 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOORWAY DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 AFT SERVICE DOOR EVACUATION SLIDE SECTION FELL OUT OF CONTAINER. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999102200278 19991022 00278 NM 1999 10 22 CALA9901371 1 19991015 A 3220 651637113 SCISSOR LINK BOEING 727 727232 1384082 NM NLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 NLG LOWER SCISSOR LINK CRACKED (1) AT RIGHT SIDE WHERE IT CONNECTS TO CENTER PIN. REPLACED LINK SCISSOR PER MM 32-21-21 . 2 L 7 3 4F A3WE 1999102200279 19991022 00279 NM 1999 10 22 CALA9901372 1 19991014 A 5320 50826162 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 303 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17328 23458 INTERCOSTAL CRACKED (3.5) AT STA 303 AND STR 5L. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999102200280 19991022 00280 WP 1999 10 22 CALA9901373 1 19991014 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 408-448 SCRATCHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 EXTERNAL FUSELAGE LEFT SIDE HAS TWO SCRATCHES BETWEEN FS 408 AND 448 AT LONG 20L AND 22L. REPAIRED IN ACCORDANCE WITH S RM 53-04 FIG 38. 2 L 7 2 4F A6WE 1999102200281 19991022 00281 WP 1999 10 22 CALA9901374 1 19991014 A 5347 S00483 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200 - 237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 CABIN LEFT SEAT TRACK HAS CORROSION BETWEEN FS 200 AND 237. FABRICATED SPLICES. INSTALLED SEAT TRACK AND SPLICES PER S RM 51-30-5, 53-05, AND 51-10-03. 2 L 7 2 4F A6WE 1999102200282 19991022 00282 WP 1999 10 22 CALA9901375 1 19991014 A 5315 2921948 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 FLOORBEAM 1322 AFT LEFT CORRODED ON UPPER CHORD. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED ANGLES, SHIM, AND FILL ER PER SRM 53-05, 51-10-4 AND 51-10-02. 2 L 7 2 4F A6WE 1999102200283 19991022 00283 WP 1999 10 22 CALA9901376 1 19991014 A 5754 99375682 RIB DOUG DC9 DC982 3022082 WP NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 SLAT END FITTING DAMAGED (3 CRACK). REMOVED DAMAGED SLAT END FITTING AND REPLACED WITH NEW PART PER SRM 51-30-8. 2 L 7 2 4F A6WE 1999102200284 19991022 00284 WP 1999 10 22 CALA9901377 1 19991014 A 5320 2929169 SUPPORT DOUG DC9 DC982 3022082 WP BS 210 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 FLOOR BOARD SUPPORT ANGLE IS CORRODED AT STA 210. REMOVED AND INSTALLED NEW SUPPORT ANGLE PER SRM 51-30-5 AND 51-10-3. 2 L 7 2 4F A6WE 1999102200285 19991022 00285 WP 1999 10 22 CALA9901378 1 19991014 A 5320 2777930S8 SUPPORT DOUG DC9 DC982 3022082 WP BS 541 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 FWD CARGO STA 541 FLOOR SUPPORT IS CORRODED JUST ABOVE LONG 27R. REMOVED DAMAGED FLOOR SUPPORT FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-01, 53-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1999102200286 19991022 00286 WP 1999 10 22 CALA9901379 1 19991014 A 5720 FORMER DOUG DC10 DC1010 3022110 WP LT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 LEFT WING TIP CRACKED IN THREE PLACES (3) INSIDE PANEL. REMOVED FORMER. FABRICATED AND INSTALLED NEW FORMER PER SRM 51 -31-01, 57-23-01 AND 51-10-04. 2 L 7 3 4F A22WE 1999102200287 19991022 00287 WP 1999 10 22 CALA9901380 1 19991014 A 5320 4616493 STIFFENER DOUG DC9 DC982 3022082 WP BS 1136-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 AFT CARGO BETWEEN FS 1136 AND 1155 OVERHEAD CUSP WEB STIFFENER CORRODED. REMOVED AND REPLACED STIFFENER PER SRM 53-01-0 1 AND 51-30-2. 2 L 7 2 4F A6WE 1999102200288 19991022 00288 WP 1999 10 22 CALA9901381 1 19991014 A 5320 GUSSET DOUG DC9 DC982 3022082 WP BS 427 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 FWD CARGO STA 427 JUST INSIDE DOORWAY FLOOR SUPPORT IS CORRODED. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED NEW SECTION PER SRM 53-01-1, 51-10-3, 53-01, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1999102200289 19991022 00289 NM 1999 10 22 UPS99230904 1 19991013 A 3350 BATTERY PACK BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 914UP 19246 EMERGENCY EXIT LIGHTS ABOVE FWD DOOR COMES ON. BATTERY PACK LOW. RECHARGED EMERGENCY EXIT BATTERY PER MM 33-55-00. OP S CK GOOD. 2 L 7 3 4F A3WE 1999102200290 19991022 00290 NM 1999 10 22 UPS99630907 1 19991014 A 2510 11743407 SEAT BELT BOEING 767 76734AF 1385212 NM RT COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 F/O SEAT BELT DEFECTIVE. REMOVED AND REPLACED SEAT BELT. 2 L 7 2 4F RT A1NM 1999102200291 19991022 00291 WP 1999 10 22 UPS99830887 1 19990915 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 0.7095 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT WING L/E RIB AT XILD O.7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED TH E RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999102200292 19991022 00292 WP 1999 10 22 UPS99830888 1 19990914 A 5310 4640162502 FITTING DOUG DC8 DC871F 302199D WP MAIN CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 CORROSION AROUND THE UPPER CUSP FITTING MOUNT BOLTS AT FS 1306 LT. REMOVED AND REPLACED THE CUSP F ITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999102200293 19991022 00293 WP 1999 10 22 UPS99830889 1 19990913 A 5320 4645516501 ANGLE DOUG DC8 DC871F 302199D WP BS 839 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 LT SIDE OF THE LWR KEEL BEAM AT FS 839, BL 0, BETWEEN THE MLG DOORS, INTERCOSTAL ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999102200294 19991022 00294 WP 1999 10 22 UPS99830890 1 19990914 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123 SIX INCH CRACK AT FS 1766, UPPER CABIN BULKHEAD ANGLE BETWEEN LONGERON 10L AND 11L. STOP DRILLED C RACK AND REPAIRED THE ANGLE IAW SRM 53-2-5 FIG 1F. 2 L 7 4 4F RT 4A25 1999102200295 19991022 00295 WP 1999 10 22 UPS99830891 1 19990930 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 FUSELAGE FRAME AT FS 55 AT LONGERON 24L IS CRACKED AT THE ATTACH ROD. CUT OUT DAMAGED AREA AND REPAI RED THE FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999102200296 19991022 00296 WP 1999 10 22 UPS99830892 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 210.29 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XFS 210, 29 FWD OF THE SPAR IS CRACKED. STOP DRILLED THE CRACK AND REPAIRE D THE SKIN IAW EO DC8-5720-7767. 2 L 7 4 4F RT 4A25 1999102200297 19991022 00297 WP 1999 10 22 UPS99830893 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 257.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E LWR SKIN AT XW 257.75, JUST AFT OF THE L/E IS CRACKED AT 2 FASTENERS. CUT OUT DAMAGED AR EA AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 1999102200298 19991022 00298 WP 1999 10 22 UPS99830894 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XFS 610.0, 2 FWD OF THE SPAR IS CRACKED. STOP DRILLED CRACK AND REPAIRED T HE SKIN IAW EO DC8-5720-7767. 2 L 7 4 4F RT 4A25 1999102200299 19991022 00299 WP 1999 10 22 UPS99830895 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 761.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E SKIN, AT THE L/E, AT XW 761.5, HAS MODERATE INTERGRANNULAR CORROSION AND IS CRACKED AT 2 FASTENERS. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-0 FIG 2H. 2 L 7 4 4F RT 4A25 1999102200300 19991022 00300 WP 1999 10 22 UPS99830896 1 19991001 A 5753 5642960103 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 LT INBD FLAP OTBD T/E WEDGE SKIN IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FLAP WEDGE SKIN I AW DWG 5642960 AND SRM 51-1-21 AND 51-1-21A. 2 L 7 4 4F RT 4A25 1999102200301 19991022 00301 WP 1999 10 22 UPS99830897 1 19991001 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 FUSELAGE FRAME AT FS 220, JUST ABOVE LONGERON 21R IS CRACKED AT A FASTENER HOLE. CUT OUT DAMAGED ARE A AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 1F. 2 L 7 4 4F RT 4A25 1999102200302 19991022 00302 WP 1999 10 22 UPS99830898 1 19991001 A 5320 37549181 FITTING DOUG DC8 DC873F 302199F WP BS 1160-1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 CUSP FITTING CRACKED INSIDE RT TORQUE BOX BETWEEN FS 1160 AND 1180. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999102200303 19991022 00303 WP 1999 10 22 UPS99830899 1 19991002 A 5320 47516401 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 MODERATE CORROSION ON THE LONGERON 18L INTERCOSTAL TO FRAME 822 ATTACH FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999102200304 19991022 00304 WP 1999 10 22 UPS99830900 1 19991002 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 246.6 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XS 246.6 IS GOUGED AND CORRODED AT THE FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 1999102200305 19991022 00305 WP 1999 10 22 UPS99830901 1 19991003 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 448.581 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E RIB AT XS 448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE R IB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999102200306 19991022 00306 WP 1999 10 22 UPS99830902 1 19991003 A 5320 4641326N FITTING DOUG DC8 DC873F 302199F WP BS 1690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 HEAVY CORROSION ON LONGERON END FITTING, FWD SIDE OF FS 1690 AT LONGERON 22R. REMOVED AND REPLACED T HE FITTING IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999102200307 19991022 00307 WP 1999 10 22 UPS99830903 1 19991013 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 EMERGENCY LIGHT VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK AND RELAY UNIT. OPS CK NORMAL PER MM 33-50-01. 2 L 7 4 4F RT 4A25 1999102200308 19991022 00308 WP 1999 10 22 UPS99830905 1 19991011 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 EMERGENCY LIGHTS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND OPS CHECK OK IAW MM 33-50-00. 2 L 7 4 4F RT 4A25 1999102200309 19991022 00309 WP 1999 10 22 UPS99830906 1 19991013 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 772UP 46072 EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT PER MM 33-50-01, LIGHTS TEST OK. 2 L 7 4 4F RT 4A25 1999102200310 19991022 00310 WP 1999 10 22 UPS99830908 1 19991002 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 LONGERON 32R END FITTING AT FS 1690 IS HEAVILY CORRODED AND CRACKED. REMOVED AND REPLACED THE FITTIN G IAW SRM 51-1-21 AND 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999102200311 19991022 00311 WP 1999 10 22 UPS99830909 1 19991003 A 5320 DC853B0093 SPLICE DOUG DC8 DC873F 302199F WP BS 1766 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 LONGERON 32R END FITTING, FWD SIDE OF THE FS 1766 FRAME IS HEAVILY CORRODED. REMOVED AND REPLACED TH E FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999102200312 19991022 00312 WP 1999 10 22 UPS99830910 1 19991004 A 5320 3754473501 FITTING DOUG DC8 DC873F 302199F WP BS 390 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 LONGERON 31L SPLICE FITTING AT FS 390 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999102200313 19991022 00313 WP 1999 10 22 UPS99830911 1 19991004 A 5320 37502571 FITTING DOUG DC8 DC873F 302199F WP BS 470 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 LONGERON 31L SPLICE FITTING AT FS 470 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1999102200314 19991022 00314 WP 1999 10 22 UPS99830912 1 19991005 A 5720 TEE CHORD DOUG DC8 DC873F 302199F WP WS 520.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E AT XS 520.168, THE OTBD SLOT, UPPER TEE CHORD IS CRACKED AT THE OTBD END. STOP DRILLED T HE CRACK AND REPAIRED THE TEE CHORD IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999102200315 19991022 00315 WP 1999 10 22 UPS99830913 1 19991004 A 5320 4758514511 FITTING DOUG DC8 DC873F 302199F WP BS 1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 INTERCOSTAL TO FRAME FITTING CRACKED, FWD SIDE FS 1280 AT LONGERON 33R. REMOVED AND REPLACED THE FIT TING IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999102200316 19991022 00316 WP 1999 10 22 UPS99830914 1 19991004 A 5320 5645332127 DOUBLER DOUG DC8 DC873F 302199F WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 SHEARED FASTENERS AND CORROSION UNDER THE FINGER DOUBLER AT FS 879 TO FS 902, BL 0. REMOVED THE FING ER DOUBLER, REMOVED LIGHT CORROSION FROM WEB IAW SRM 51-1-8, WEB WITHIN LIMITS IAW SRM 53-2-0 FIG 1F. FABRICATED REPLAC EMENT FINGER DOUBLER IAW DWG 5645332 AND REPLACED THE FINGER DOUBER IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999102200317 19991022 00317 WP 1999 10 22 UPS99830915 1 19991005 A 5720 97532978 ANGLE DOUG DC8 DC873F 302199F WP WS 522.168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 RT WING L/E OTBD VERTICAL ANGLE AT XS 522.168 IS CRACKED PAST THE STOP DRILL. REMOVED, FABRICATED, A ND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999102200318 19991022 00318 WP 1999 10 22 UPS99830916 1 19991007 A 5312 BULKHEAD CHORD DOUG DC8 DC873F 302199F WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 ACCOMPLISH APPENDIX C OF EO DC8-5310-10158-A, FS 70 BLKHD LWR CHORD AT LONGERON 33L IS CRACKED AND CO RRODED. REPAIRED FS 70 BLKHD LWR CHORD AT LONGERON 33L IAW EO DC8-5310-10158-A APPX C. 2 L 7 4 4F RT 4A25 1999102200319 19991022 00319 WP 1999 10 22 UPS99830917 1 19991009 A 5320 37585701 FITTING DOUG DC8 DC873F 302199F WP BS 1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 FS 1230 FRAME ATTACH FITTING AT LONGERON 35L IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1999102200320 19991022 00320 WP 1999 10 22 UPS99830918 1 19991009 A 5313 S1418997 LONGERON DOUG DC8 DC873F 302199F WP BS 1766 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 LONGERON 32R, FWD OF FS 1766 IS CORRODED OUT OF LIMITS UNDER THE SPLICE FITTING. CUT OUT DAMAGED SEC TION OF THE LONGERON AND SPLICED IN A NEW SECTION IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1999102200321 19991022 00321 NM 1999 10 22 QXEA9902123 1 19991012 A 2435 23088002A STARTER GEN DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE FAILED A QXEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. B H P SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 364PH 20099 886 524 PDX- AFTER STARTING ENGS FOR TAXI TO MX HANGAR, ELECTRICAL POWER WAS LOST IN THE COCKPIT ON COPILOTS SIDE, AND IN THE CA BIN. EXTERNAL PWR WAS RECONNECTED. AT THAT TIME SMOKE WAS NOTICED COMING FROM NR 2 ENG. ENG SHUT DOWN PROCEDURE ACCOM P ON BOTH ENG'S, THE T HANDLE WAS PULLED AND FIRE EXTINGUISHER (FWD BOTTLE) FIRED. MX FIRED GROUND EXTINGUISHER INTO TH E INTAKE/EXHAUST PORTS OF NR 2 ENG. THERE WERE NO FIRE WARNING IND'S IN COCKPIT OR ANY UNUSUAL CAUTION LIGHTS. MX INSP ECTED THE ENG AND NOTED NO EXTERNAL OR ENG DAMAGE NOTED. MX REPLACED THE NR 2 STARTER/GEN, GARLOCK SEAL, D.C.GCU, AND T HE FIRE BOTTLE. THE ENG WAS ALSO CLEANED TO REMOVE RESIDUAL FROM THE EXTINGUISHER(S). ALL OP'S CHECKS GOOD. A/C RETUR 2 H 7 2 4T RT A13NM 1999102200322 19991022 00322 NM 1999 10 22 99FDEA00426 1 19991015 A 2611 SMOKE WARNING BOEING 727 7272S2F 1384O81 NM CARGO COMPT ILLUMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 203FE 22925 99-253 - AFT T/O ON CLIMB-OUT LANDING GEAR MAIN CARGO COMP SMOKE WARNING LIGHT NR 4 ILLUM WITH AURAL WARN FOLLOW SHORTLY BY FUMES AND NR 5 WARN LIGHT ILLUM. REMOVED AND REPLACED GRD/AIR SHUTOFF ACTUATOR PER MM 21-00. 2 L 7 3 4F A3WE 1999102200323 19991022 00323 NM 1999 10 22 99FDEA00427 1 19991016 A 3260 40143 SWITCH BOEING 727 72722 1384002 NM LT MLG INOP A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 150FE 19141 99-254 - ON APPROACH LANDING GEAR WAS SEL DOWN AND SHOW 3 GREEN LIGHTS. THE LMG LIGHT WENT OUT AND THE GEAR WARN HORN S OUND. REMOVED AND REPLACED LMG DOWNLOCK SWITCH AND TEST IN ACCORDANCE WITH 727-100 MM 32-61-021. ALL IND NORMAL. 2 L 7 3 4F A3WE 1999102200324 19991022 00324 NM 1999 10 22 99FDEA00428 1 19991016 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 755 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 MAIN DECK, SEAT TRACK FOUND CRACK AT BS 755 X=8.5 RT. *S/D* REPAIRED, FABBED AND INSTALLED AS PER SRM 53-70-00 FIG 1 V OL 1. 2 L 7 3 4F RT A22WE 1999102200325 19991022 00325 WP 1999 10 22 99FDEA00423 1 19991005 A 2780 CONTROL CABLE DOUG DC10 DC1030F 3023504 WP NR 6 LE SLAT BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 LT WING NR 6 SLAT EXTEND CABLE FOUND SNAPPED OFF. REMOVED AND REPLACED IAW MM 27-89-11-4. CABLES RE-RIGGED AND FUNCTIO NAL TEST CARRIED OUT IAW MM 27-80-00-05. FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 1999102200326 19991022 00326 WP 1999 10 22 ABXA9900739 1 19991013 A 2910 AE2460001J0630 LINE DOUG DOUG DC8 DC861 3021952 WP NR 2 ENGINE DEFECTIVE A ABXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 841AX 45908 LOST HYDRAULIC QUANTITY DOWN TO STAND PIPE. DECLARED EMERGENCY. REPLACED HYDRAULIC LINE AT NR 2 ENGINE DRIVEN HYDRAULI C PUMP IAW DC8 MM. 2 L 7 4 4F 4A25 1999102200327 19991022 00327 WP 1999 10 22 MWEA99683 1 19991012 A 5532 59121669N SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LEFT VERTICAL STABILIZER SKIN HAS A HOLE CHAFED THROUGH. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 1999102200328 19991022 00328 WP 1999 10 22 MWEA99684 1 19991014 A 5320 9911840139 SHEAR TIE DOUG DC9 DC981 3022081 WP BS 1440 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 SHEAR TIE AT STATION 1440 OUTBOARD OF JAMB IS CORRODED. MAINTENANCE FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 1999102200329 19991022 00329 WP 1999 10 22 MWEA99685 1 19991014 A 5230 593644313 SEAL DOUG DC9 DC981 3022081 WP CARGO DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 AFT CARGO DOOR SEAL DEPRESSOR ON BOTTOM SIDE OF DOOR JAMB IS BENT, DENTED AND GOUGED. MAINTENANCE FABRICATED AND INSTAL LED REPAIR ANGLE. 2 L 7 2 4F A6WE 1999102200330 19991022 00330 WP 1999 10 22 MWEA99686 1 19991014 A 5320 991199217 ANGLE DOUG DC9 DC981 3022081 WP BS 1497-1510 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 AFT ACCESSORY ANGLE EXTENSION AT STATION 1497-1510 IS CORRODED. MAINTENANCE FABRICATED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 1999102200331 19991022 00331 WP 1999 10 22 MWEA99687 1 19991014 A 5320 991199027 ANGLE DOUG DC9 DC981 3022081 WP BS 1463 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 ANGLE CAP AT STATION 1463 AT JAMB ASSEMBLY HAS HEAVY CORROSION. MAINTENANCE FABRICATED AND INSTALLED NEW ANGLE CAP. 2 L 7 2 4F A6WE 1999102200332 19991022 00332 WP 1999 10 22 MWEA99688 1 19991014 A 5330 593600423 SKIN DOUG DC9 DC981 3022081 WP BS 794 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 MISDRILLED FASTENER HOLE OUTER SKIN AT STATION 794 BETWEEN LONGERON 29 AND 28L. MAINTENANCE FABRICATED AND INSTALLED DO UBLER. 2 L 7 2 4F A6WE 1999102200333 19991022 00333 WP 1999 10 22 MWEA99689 1 19991014 A 5320 591359513 SHEAR TIE DOUG DC9 DC981 3022081 WP BS 1418 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 HEAVY CORROSION ON SHEAR TIE AT STATION 1418 FROM LONGERON 22L TO 24L. MAINTENANCE FABRICATED AND INSTALLED NEW SHEAR T IE. 2 L 7 2 4F A6WE 1999102200334 19991022 00334 WP 1999 10 22 MWEA99690 1 19991014 A 5755 4923262501 FITTING DOUG DC9 DC981 3022081 WP WING SPOILER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 CENTER SPOILER TORSION BAR INBOARD SUPPORT STRAP ATTACH FITTING IS CRACKED. MAINTENANCE REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 1999102200335 19991022 00335 WP 1999 10 22 MWEA99691 1 19991014 A 5320 9910073101 FITTING DOUG DC9 DC981 3022081 WP BS 58.75-69.55 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 T-FITTING ON NOSE WHEEL WELL PRESSURE PANEL AT STATION 58.750 TO STATION 69.550 IS CORRODED. MAINTENANCE REMOVED CORROD ED FITTING AND INSTALLED NEW FABRICATED FITTING. 2 L 7 2 4F A6WE 1999102200336 19991022 00336 WP 1999 10 22 MWEA99692 1 19991014 A 5720 3923258503N SUPPORT DOUG DC9 DC981 3022081 WP WS 292 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT WING SUPPORT AT STATION XTE 292 HAS A CRACK. MAINTENANCE REMOVED AND REPLACED SUPPORT. 2 L 7 2 4F A6WE 1999102200337 19991022 00337 WP 1999 10 22 MWEA99693 1 19991014 A 5320 991556171 ANGLE DOUG DC9 DC981 3022081 WP BS 1338 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT LAVATORY FLOOR SUPPORT FRAME AT STATION 1338 HAS CORROSION. MAINTENANCE REMOVED CORROSION AND FABRICATED AND INSTA LLED ANGLE. 2 L 7 2 4F A6WE 1999102200338 19991022 00338 WP 1999 10 22 MWEA99694 1 19991014 A 5320 991183975 DOUBLER DOUG DC9 DC981 3022081 WP BS 1463 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 SKIN SPLICE DOUBLER AT STATION 1463 FROM L25L TO JAMB IS CORRODED. MAINTENANCE FABRICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 1999102200339 19991022 00339 WP 1999 10 22 MWEA99695 1 19991014 A 5320 3957175503 FITTING DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT AFT FITTING AT FUSELAGE STATION 1463 IS CRACKED. MAINTENANCE REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 1999102200340 19991022 00340 NM 1999 10 22 DHL9974203C 1 19990726 A 5530 ANGLE BOEING 727 727225 1384077 NM VERTICAL STAB WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, ANTI-ICE SUPPORT BRACKETS WORN AT VERTICAL FIN FRONT SPAR. REMOVED AND REPLACED BRACKETS PER SRM 51-30-2 9 .25 BY 2 BY .75, N/R 4267. 2 L 7 3 4F A3WE 1999102200341 19991022 00341 NM 1999 10 22 DHL9974204C 1 19990924 A 7110 COWL BOEING 727 727225 1384077 NM NR 3 ENGINE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, NR 4 ENGINE INLET COWL OUTER SKIN DAMAGED ALONG TRAILING EDGE AT 4 O' CLOCK. CUT OUT DAMAGED AREA. INSTALL ED DOUBLER REPAIR PER SRM 54-30-3, 8.25 BY 4.75, N/R 6625. 2 L 7 3 4F A3WE 1999102200342 19991022 00342 NM 1999 10 22 DHL9974205C 1 19990923 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 7 LE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, RIGHT WING L/E SLAT CRACKED JUST BELOW FWD END OF ANTI-ICE DUCT. CUT OUT DAMAGED SECTION OF ATTACH ANGLE. INSTALLED FORMED SECTION REPAIR PER SRM 51-40-3. 18 BY 1 BY 1, N/R 2271. 2 L 7 3 4F A3WE 1999102200343 19991022 00343 NM 1999 10 22 DHL9974206C 1 19990924 A 5730 SKIN BOEING 727 727225 1384077 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LT FIXED LEADING EDGE CUT OUT FOR NR 3 SLAT OUTBD TRACK IS CRACKED. CUT OUT DAMAGED AREA. INSTALLED FLUSH REPAIR PER SRM 57-30-4 2 BY 2, N/R 1029. 2 L 7 3 4F A3WE 1999102200344 19991022 00344 NM 1999 10 22 DHL9974207C 1 19990927 A 5753 BRACKET BOEING 727 727225 1384077 NM LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, LT WING OUTBD FLAP COVE PANEL OUTBD ROD SUPPORT BRACKET CRACKED BELOW NR 2 FLIGHT SPOILER. REMOVED AND REPL ACED SUPPORT BRACKET PER SRM 51-30-2, N/R 1074. 2 L 7 3 4F A3WE 1999102200345 19991022 00345 NM 1999 10 22 DHL9974208C 1 19990927 A 5510 RUB BLOCK BOEING 727 727225 1384077 NM LT HORIZ STAB CORORODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, LEFT STABILIZER RUB BLOCK TRACK HAS CORROSION BULGE. REMOVED AND INSTALLED NEW TRACK PER SRM 51-30-2, N/R 4 297. 2 L 7 3 4F A3WE 1999102200346 19991022 00346 NM 1999 10 22 DHL9974209C 1 19990928 A 7820 MIXER BOEING 727 727225 1384077 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, NR 2 ENGINE EXHAUST MIXER HAS BRACKET BROKEN AT 6 O'CLOCK. WELDED CRACKED PER MM 72-55-02, N/R 6672. 2 L 7 3 4F A3WE 1999102200347 19991022 00347 NM 1999 10 22 DHL9974210C 1 19990930 A 5753 BRACKET BOEING 727 727225 1384077 NM NR 4 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, 4 FLAP TRACK FWD FIXED FAIRING BRACKET CRACKED AT FWD OUTBD CORNER. REPLACED FIXED FAIRING BRACKET PER SRM 51-40-2, 14 BY 14, N/R 7307. 2 L 7 3 4F A3WE 1999102200348 19991022 00348 NM 1999 10 22 DHL9974211C 1 19990925 A 7110 FRAME BOEING 727 727225 1384077 NM NR 3 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, NR 3 ENGINE LOWER COWL, HORIZONTAL FRAME DAMAGED INBD SIDE 27 AFT FOF FWD EDGE. REMOVED AND REPLACED DAMAGE D FRAME PER SRM 1-10-2, N/R 6634. 2 L 7 3 4F A3WE 1999102200349 19991022 00349 NM 1999 10 22 DHL9974212C 1 19990924 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 530 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, NR 4 SEAT TRACK WORN AT STA 530 . CUT OUT DAMAGED SECTION, INSTALLED NEW SECTION, PER SRM 53-10-5, 20 LONG, N/R 3048. 2 L 7 3 4F A3WE 1999102200350 19991022 00350 NM 1999 10 22 DHL9974213C 1 19990925 A 7110 COWL BOEING 727 727225 1384077 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, NR 1 ENGINE NOSE COWL AFT EDGE OF COWL SKIN IS BENT AND PULLED LOOSE FROM RIVET HEAD AND SKIN FLUSH REPAIR NOT FITTED PROPERLY. REMOVED FLUSH REPAIR, CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-30-2 11.5 BY 5, N/R 6641. 2 L 7 3 4F A3WE 1999102200351 19991022 00351 NM 1999 10 22 DHL9974214C 1 19990924 A 7110 COWL BOEING 727 727225 1384077 NM NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, NR 3 ENGINE INLET COWL OUTER SKIN CRACKED AT FASTENER AT 1 O'CLOCK APPROX 6 AFT OF LEADING EDGE. CUT OUT D AMAGED AREA, INSTALLED DOUBLER PER SRM 54-30-3, 10 BY 2, N/R 6624. 2 L 7 3 4F A3WE 1999102200352 19991022 00352 NM 1999 10 22 DHL9974215C 1 19990925 A 5755 ANGLE BOEING 727 727225 1384077 NM NR 13 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, RT WING COVE PANEL SUPPORT ROD INBD ATTACH ANGLE CRACKED UNDER INBD END OF NR 13 SPOILER PANEL. REMOVED AN D REPLACED ANGLE PER SRM 51-30-2, N/R 2324. 2 L 7 3 4F A3WE 1999102200353 19991022 00353 NM 1999 10 22 DHL9974216C 1 19990926 A 7110 COWL BOEING 727 727225 1384077 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, NR 1 ENGINE UPPER COWL PANEL REPAIR DOUBLER AT FWD INBD CORNER IS CRACKED. REPLACED DOUBLER AT CORNER PER SRM 54-30-3, 14 BY 6, N/R 6668. 2 L 7 3 4F A3WE 1999102200354 19991022 00354 NM 1999 10 22 DHL9974217C 1 19990926 A 7110 COWL BOEING 727 727225 1384077 NM NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, NR 3 ENG NOSE COWL AFT WEB CRACKED OUT. INSTALLED WEB REPAIR PER SRM 51-40-2, 27 BY 6, N/R 6671. 2 L 7 3 4F A3WE 1999102200355 19991022 00355 NM 1999 10 22 DHL9974218C 1 19991005 A 5754 BRACKET BOEING 727 727225 1384077 NM NR 4 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, NR 4 TRAILING EDGE FLAP INBD BEARING BRACKET TO BULL NOSE CRACKED. REMOVED AND REPLACED NR 4 LE FLAP PER MM 27-81-4. N/R 2366. 2 L 7 3 4F A3WE 1999102200356 19991022 00356 NM 1999 10 22 DHL9974219C 1 19991007 A 5350 FAIRING BOEING 727 727225 1384077 NM WS 720 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, DENT AT WING TO FUSELAGE FAIRING AT APPROX STA 720E ATR 26RT. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAI R PER SRM 51-40-2, 6.5 BY 2.5, N/R 5461. 2 L 7 3 4F A3WE 1999102200357 19991022 00357 NM 1999 10 22 DHL9974220C 1 19990924 A 5720 ANGLE BOEING 727 727225 1384077 NM WS 130 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, LEFT WING L/E CAVITY AT WS 130 RIB ATTACH ANGLE IS CRACKED BEYOND OLD DOUBLER. STOP DRILLED BOTH ENDS OF C RACK ON ANGLE, BEYOND LIMITS. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. N/R 1033. 2 L 7 3 4F A3WE 1999102200358 19991022 00358 NM 1999 10 22 DHL9974221C 1 19990925 A 5320 ANGLE BOEING 727 727225 1384077 NM BS 1273 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, AFT AIRSTAIR RT LOWER TORQUE BOX UNDER STAIR ACTUATOR FITTING, HAS CRACK IN ANGLE ALONG STA 1273 INBD SIDE. REMOVED ANGLE SUPPORT AND INSTALLED NEW SUPPORT PER S/B 53-0129, N/R 4260. 2 L 7 3 4F A3WE 1999102200359 19991022 00359 NM 1999 10 22 DHL9974222C 1 19991004 A 7110 COWL BOEING 727 727225 1384077 NM NR 1 ENGINE PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C CHECK, NR 1 NOSE COWL HAS SMALL PUNCTURES IN SKIN AT FRAME APPROX NAC STA 92. CUT OUT DAMAGED AREA. INSTALLED DOU BLER 4 BY 8 PER SRM 54-30-3. N/R 6679. 2 L 7 3 4F A3WE 1999102200360 19991022 00360 NM 1999 10 22 DHL9974223C 1 19991004 A 7110 COWL BOEING 727 727225 1384077 NM NR 1 ENGINE MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, NR 1 ENGINE NOSE COWL HAS IMPROPER REPAIR TO SKIN EDGE AT FRAME APPROX NAC STA99. REMOVED OLD REPAIR. INST ALLED DOUBLER PER SRM 51-40-2, 4 BY 7.5, N/R 6680. 2 L 7 3 4F A3WE 1999102200361 19991022 00361 NM 1999 10 22 DHL9974224C 1 19990925 A 5753 FAIRING BOEING 727 727225 1384077 NM RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, RT WING INBD FLAP INBD TRACK AFT FAIRING CRACKED AT 2 LOCATIONS. REMOVED DOUBLER AT UPPER END AND REPLACED PER SRM 51-30-2, 4 BY 8. WELDED OTHER CRACK, N/R 2333. 2 L 7 3 4F A3WE 1999102200362 19991022 00362 NM 1999 10 22 DHL9974225C 1 19990924 A 5753 SKIN BOEING 727 727225 1384077 NM RT TE FOREFLAP CHAFFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, CHAFFED MARK ON LE OF RT INBD FOREFLAP AT NR 5 FLAP TRACK. REMOVED OLD REPAIR, INSTALLED FLUSH REPAIR PER S RM 57-50-4, 20.25 BY 9.5, N/R 2318. 2 L 7 3 4F A3WE 1999102200363 19991022 00363 NM 1999 10 22 DHL9974226C 1 19990927 A 5510 RUB BLOCK BOEING 727 727225 1384077 NM RT HORIZ STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 AT C-CHECK, RT STABILIZER RUB BLOCK TRACK HAS CORROSION BULGE. REMOVED RACK. INSTALLED NEW TRACK PER SRM 51-30-2, N/R 4298. 2 L 7 3 4F A3WE 1999102200364 19991022 00364 WP 1999 10 22 DHL99802002 1 19991014 A 3510 OXYGEN SYS DOUG DC8 DC873F 302199F WP COCKPIT LEAKING A DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 802DH 46076 LOST O2 PRESSURE FROM 1600 TO 200 PSI. SERVICED AND LEAK CHECKED CREW O2 PER MM 35-10-00. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 1999102200365 19991022 00365 SO 1999 10 22 SWIA971571 1 19990928 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 234SW 120308 INBOARD FLAP DISAGREEMENT, FLAPS WON'T RETRACT. RETURNED TO FIELD. RESET FLAPS SYSTEM. OPS CHECKS GOOD. REPLACED FLA P CONTROL UNIT FOR TROUBLESHOOTING. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200366 19991022 00366 SO 1999 10 22 SWIA971572 1 19991004 A 3610 VENTURI EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PACK LEAKING A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 291SW 120318 DUCT LEAK LIGHT CAME ON AFTER TAKEOFF. LIGHT WENT OUT AFTER QRH INSTRUCTIONS. RETURNED TO SFO. FOUND RIGHT PACK VENTU RI IS LEAKING. REPLACED VENTURI AND PACKING. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200367 19991022 00367 SO 1999 10 22 SWIA971573 1 19991005 A 3150 39948E2903 AURAL WARNING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ACTIVATED A SWIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 NM 07 560SW 120334 AT V' RECEIVED TRIPLE CHIME AND HIGH SPEED WARNING. CONSULTED QRH, UNABLE TO SILENCE WARNING AND AURAL WARNING. FINALL Y SILENCED AT 150 KTS AIRSPEED AND FLAPS 25'. RETURNED TO SAN. REPLACED FO'S AIRSPEED INDICATOR. PERFORMED CHECK OF H IGH SPEED AURAL WARNING SYSTEM. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200368 19991022 00368 SO 1999 10 22 SWIA971574 1 19991005 A 2460 DC BUS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E&E COMP FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 563SW 120338 ON CLIMB-OUT (90,00+) ELECTRIC LIGHT ON MAP ILLUMINATED, EMERGENCY BUS OFF LIGHT ILLUMINATED. ELECTRIC BUSSES OFF RELAY S EMERGENCY BUSSES 1 CB POPPED. ELECTRIC DC INDICATION (EMERGENCY) 1 POPPED. DIVERTED TO FAT. REPLACED EMERGENCY DC B US 1 OFF RELAY (K0439). OPS CHECKS GOOD IAW MM 24-52-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200369 19991022 00369 SO 1999 10 22 SWIA971575 1 19991007 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 214SW 120280 SERVICE DOOR LIGHT INFLIGHT. RETURNED TO LAX. ADJUSTED FUEL DOOR MICROSWITCHES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200370 19991022 00370 SO 1999 10 22 SWIA971576 1 19991009 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG FAILED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 227SW 120304 NOSE GEAR WOULD NOT RETRACT ON RETRACTION SEQUENCE AND RED NOSE GEAR LIGHTS, FLUTTER FROM NOSE GEAR EXTENDED GEAR AND AL L LIGHTS GOOD. RETRACTED AGAIN SAME, NOSE GEAR RETRACTED 1 1/2 MINUTES AFTER SELECTIONS. REMOVED AND REPLACED LT SEQUE NCE VALVE. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200371 19991022 00371 SO 1999 10 22 SWIA971577 1 19991009 A 3233 2060500005 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 227SW 120304 NOSE GEAR WOULD NOT RETRACT ON RETRACTION SEQUENCE AND RED NOSE GEAR LIGHTS WITH FLUTTER FROM NOSE GEAR. EXTENDED GEAR AND ALL LIGHTS GOOD. RETRACTED AGAIN SAME. NOSE GEAR RETRACTED 1 1/2 MINUTES AFTER SELECTIONS. RETURNED TO FAT. REMO VED AND REPLACED NLG MAIN ACTUATOR. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200372 19991022 00372 1999 10 22 SWIA971578 4 19991010 A 3425 AHARS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT& RT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 564SW 120339 AFTER TAKEOFF ROLL, HSI/EADI PILOT AND COPILOT AHARS FAILED. RETURNED TO MRY. RERACKED AHARS COMPUTER. OPS CHECK GOOD . 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200373 19991022 00373 SO 1999 10 22 SWIA971579 1 19991010 A 7712 TQ SIG COND EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 197SW 120186 EXPERIENCED PLUS AND MINUS 10 TO 12 PERCENT TORQUE FLUCTUATIONS ON RIGHT ENGINE AT CLIMB POWER SETTINGS. FLUCTUATIONS C AUSED REDUCED POWER SETTINGS. RETURNED TO GJT. FLUCTUATIONS OCCURRED BETWEEN 8,500 FT AND 10,000 FT. REMOVED AND REPL ACED THE TORQUE SIGNAL CONDITION UNIT IAW 77-11-1. RAN ENGINE AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200374 19991022 00374 SO 1999 10 22 SWIA971580 1 19991010 A 3231 RETRACT MECH EMB 120 EMB120RT SO PWA 118 PW118A NE NLG DOORS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 251YV 120251 NOSE GEAR DOOR OPEN AFTER GEAR RETRACTION. CHECKED ALL FOUR NOSE GEAR DOORS FOR DISCREPANCY. CHECKS GOOD. OK FOR CONT INUED SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200375 19991022 00375 SO 1999 10 22 SWIA971581 1 19991010 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120RT SO PWA 118 PW118A NE LT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 251YV 120251 BOTH NOSE GEAR DOORS OPEN AFTER GEAR RETRACTION. RETURNED TO FIELD. REPLACED SEQUENCE VALVE ON LEFT MAIN OUTBOARD GEAR DOOR. REMOVED AND REPLACED LANDING GEAR RELAY BOX. CYCLED GEAR SEVERAL TIMES. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102200376 19991022 00376 EA 1999 10 22 SWIA971582 1 19991012 A 2751 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT TE FLAP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 407SW 7034 CLIMBING THROUGH 22,000 FEET, FLAPS FAIL MESSAGE ON EICAS. CYCLED CIRCUIT BREAKERS PER MAINTENANCE CONTROL WITH NO CHAN GE. RETURNED TO SLC AND LANDED O FLAPS, (FLAPS FAILED AT 0 DID NOT OPERATE FLAP SELECTOR). REMOVED AND REPLACED LEFT B RAKE POSITION SENSOR UNIT IAW MM 27-51-01. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999102200377 19991022 00377 EU 1999 10 22 RAIA9910014 1 19991012 A 3230 1862F RADIUS ROD BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 424AM 865 7486 - STL - LIGHT LANDING GEAR INTRANSIT LIGHT ON CONSTANTLY. MAINTENANCE REPLACED RIGHT RADIUS ROD. 2 L 7 2 4T RT A56EU 1999102200378 19991022 00378 1999 10 22 RAIA9910015 4 19991012 A 3421 7001182902 VERT GYRO BAG JETSTM JETSTM3201 1500217 EU NR 1 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 338TE 932 7334 - STL- NR 1 ADI SHOWING FLAGS. MAINTENANCE REPLACED NR 1 VERTICAL GYRO. 2 L 7 2 4T RT A56EU 1999102200379 19991022 00379 1999 10 22 RAIA9910016 4 19991001 A 3425 7001182902 ADI BAG JETSTM JETSTM3201 1500217 EU NR 1 FLAGGED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 338TE 932 7334 - STL - NR 1 ADI FLAGGING. MAINTENANCE REPLACED NR 1 ADI. 2 L 7 2 4T RT A56EU 1999102200380 19991022 00380 EU 1999 10 22 RAIA9910017 1 19991014 A 2431 23079009A GENERATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 CE 03 422AM 856 7434 - STL - LEFT GENERATOR INOP. MAINTENANCE REPLACED LEFT GENERATOR. 2 L 7 2 4T RT A56EU 1999102200381 19991022 00381 WP 1999 10 22 TWAA9914201 1 19991016 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP ROW 28 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 EIBWD 49575 THE AFT STAIR EMERGENCY LIGHT AND 3 EGRESS LIGHTS AFT OF ROW 28 WERE INOPERATIVE. RELAMPED, (P/N 7732) THE AFT STAIR EM ERGENCY LIGHT AND REPLACED THE LAMP, (P/N 7732) AND REPAIRED CONNECTORS FOR THE EGRESS LIGHTS. CHECK-C 2-6-99 MCI. 2 L 7 2 4F RT A6WE 1999102200382 19991022 00382 WP 1999 10 22 TWAA9914202 1 19991017 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN LOOSE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 980Z 47344 THE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. RESEATED THE EGRESS POWER STRIP CONNECTOR THAT HAD BECOME LOOSE. CHECK-C 9-23-99 STL. 2 L 7 2 4F A6WE 1999102200383 19991022 00383 NM 1999 10 22 HNAA9900137 1 19991017 A 3350 CONNECTOR DHAV DHC8 DHC8201 2809001 NM ROW 1DF LOOSE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 965HA 450 RIGHT HAND SIDE WALL EMERGENCY EXIT LIGHT AT 1DF INOP IN TEST. RESEATED PIN AT MOLEX CONNECTOR FOR LIGHT ASSEMBLY. 2 H 7 2 4T RT A13NM 1999102200384 19991022 00384 WP 1999 10 22 AT9900669R1 1 19990814 A 2750 2648233 SPRING DOUG DC9 DC932 3022066 WP BS 717 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 FOUND LEFT WHEEL WELL FLAP FOLLOW-UP INBOARD DRUM SPRING CORRODED. REMOVED AND REPLACED SPRING IAW SRM 51-10-3 AND MM 2 7-52-0. 2 L 7 2 4F A6WE 1999102200385 19991022 00385 WP 1999 10 22 AT9900673R1 1 19990927 A 7930 42D110 SWITCH DOUG DC9 DC932 3022066 WP NR 2 ENGINE MALFUNCTIONED A ZZDA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 SO 15 839AT 47089 SHUT DOWN NR 2 ENGINE IN FLIGHT DUE TO OIL QUANTITY LOSS. FOUND OIL PRESSURE SWITCH DISINTEGRATED. REMOVED AND REPLACE D OIL PRESSURE DIFFERENTIAL SWITCH AND LOW OIL PRESSURE SWITCH IAW MM 79-32. 2 L 7 2 4F A6WE 1999102200386 19991022 00386 WP 1999 10 22 AT9900723 1 19991007 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND TOP SURFACE OF UPPER FLOORBOARD SUPPORT AT BS 200 - 237 CORRODED. REMOVED OLD FLOOR SUPPORT, FABRICATED REPAIR SU PPORT, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR SUPPORT. WORK DONE IAW DC9 SRM 51-30-2, 51-10-1 AND 51- 30-2. 2 L 7 2 4F A6WE 1999102200387 19991022 00387 WP 1999 10 22 AT9900724 1 19991007 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1143 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FUSELAGE SKIN JUST FORWARD OF TAIL CONE EXTERIOR JETTISON HANDLE AT BS 1143 CORRODED. REMOVED CORROSION, FABRICAT ED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-3, 53-01 FIG 2, 51-10-3. 2 L 7 2 4F A6WE 1999102200388 19991022 00388 WP 1999 10 22 AT9900725 1 19991008 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 351-465 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FORWARD CARGO FLOOR PANEL TIE-DOWN STRAPS AT BS 351-465 CORRODED. REMOVED CORROSION, OBTAINED NEW TIE-DOWN EXTRUS ION, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED AND INSTALLED TIE-DOWN STRAPS IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4 AND 53-05 FIG 4C. 2 L 7 2 4F A6WE 1999102200389 19991022 00389 WP 1999 10 22 AT9900726 1 19990827 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FLIGHT DECK CENTER FLOOR PANEL CORRODED AT BS 160 LONG 30. FABRICATED FLOOR PANEL IAW DC9 SRM 51-10-2, 51-30-2. 2 L 7 2 4F A6WE 1999102200390 19991022 00390 WP 1999 10 22 AT9900727 1 19990908 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FORWARD ENTRY FLOOR PANEL 4692B WAS CORRODED, 3 HAT SECTIONS LOOSE, AND GIL LINER STRIPS MISSING. FABRICATED NEW PANEL IAW DC9 SRM 53-21-0, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1999102200391 19991022 00391 WP 1999 10 22 AT9900728 1 19990907 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FLOOR PANEL 4697B CRACKED AND CORRODED. FABRICATED NEW PANEL IAW DC9 SRM 51-10-2 TO 51-30-2. 2 L 7 2 4F A6WE 1999102200392 19991022 00392 WP 1999 10 22 AT9900729 1 19990808 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FORWARD ENTRY FLOOR PANEL 4692 HAD 2 CRACKED CHANNELS, TWO CHANNELS LOOSE, AND CORROSION ON EDGE OF PANEL. FABRIC ATED NEW PANEL IAW DC9 SRM 53-21-0, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1999102200393 19991022 00393 WP 1999 10 22 AT9900730 1 19990907 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-251 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FORWARD ENTRY FLOOR PANEL NR 4698 WAS CORRODED AND HAD ELONGATED MOUNT HOLES. FABRICATED NEW PANEL IAW DC9 SRM 51 -10-2, DPS3-40.9. 2 L 7 2 4F A6WE 1999102200394 19991022 00394 WP 1999 10 22 AT9900731 1 19990909 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND FORWARD ENTRY FLOOR PANEL NR 4699 CHANNEL TIPS CHAFED, CORROSION AROUND NUT PLATES, AND CORROSION ON TOP AND BOTTO M SURFACES. FABRICATED NEW PANEL AND HAT SECTIONS IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2, 53-21-0. 2 L 7 2 4F A6WE 1999102200395 19991022 00395 NM 1999 10 22 AT9900732 1 19991012 A 3350 HOLDER BOEING 737 7372L9 1384497 NM CABIN FAILED A ZZDA K NONE L NO TEST CR CRUISE 1 SO 15 464AT 21278 DURING FLIGHT, AFT LEFT DOOR EMERGENCY EXIT LIGHT FELL OUT OF HOLDER. REPLACED LIGHT IN HOLDER PER 737 MM 33-51-101 PA GE 203, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 1999102200396 19991022 00396 NM 1999 10 22 RAAA99B1026 1 19991017 A 3350 873100212 SIGN INTVLV BOEING 727 72722C 138400F NM EMER EXIT INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 EMERGENCY EXIT LIGHT AT RIGHT HAND MID CABIN DOOR FAILED SELF TEST. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999102200397 19991022 00397 SO 1999 10 22 RAAA99E4005 1 19990508 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 483 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK PER CARD 42.03.49, FOUND CORROSION BULGE IN FUSELAGE SKIN AT FS 483 LT STRINGER 40-45. REPA IRED PER SRM 53-2-1 M-54 NR 21, SEALED REPAIR PER SRM 51-2-16. 2 L 7 4 4T 4A22 1999102200398 19991022 00398 SO 1999 10 22 RAAA99E4006 1 19990508 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 426-440 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK PER CARD 42.02.49, FOUND CORROSION BULGE IN FUSELAGE STRINGER NR 38 AT FS 426-440. REMOVED SKIN, STRINGER HAD NEGLIGIBLE DAMAGE. TREATED AND PRIMED, REPLACED SKIN PER SRM 51-2-12, M-54 NR 22. 2 L 7 4 4T 4A22 1999102200399 19991022 00399 SO 1999 10 22 RAAA99E4007 1 19990508 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 426-454 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK PER CARD 42.03.49, CORROSION BULGE IN SKIN AT FS 426-454 STINGER 41-45. REPLACED SKIN AT IN TERNAL DOUBLER PER SRM 51-2-12, SPLICED LWR CORNER OF SKIN PER SRM 53-2-1 FIG, M-54 NR 23. 2 L 7 4 4T 4A22 1999102200400 19991022 00400 SO 1999 10 22 RAAA99E4008 1 19990508 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 150LH CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK PER CARD 42.03.49, FOUND MULTIPLE CRACKS IN FUSELAGE SKIN AT PILOTS AFT WINDOW, LOWER AFT ED GE, EXTENDING APPROXIMATELY 6 FS 150 LT. INSTALLED DOUBLER PER 53-2-1 FIG 2 M-54 NR 28. 2 L 7 4 4T 4A22 1999102200401 19991022 00401 SO 1999 10 22 RAAA99E4009 1 19990508 A 5320 ANGLE LKHEED 188 188C 5262604 SO BS 103&124 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK FOUND TWO ANGLES CRACKED, NLG WHEEL WELL FWD OF LT PIVOT HINGE FS 103, FWD OF CENTER HINGE F S 124. REPLACED ANGLES PER SRM 51-2-1 M-54 NR 53. 2 L 7 4 4T 4A22 1999102200402 19991022 00402 SO 1999 10 22 RAAA99E4010 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 571 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK FOUND SEAT TRACK CORRODED AT ATTACH SCREW HOLE FS 571 LBL 56 M-54 NR 71. REPLACED SEAT TRAC K PER ECO 99-05. 2 L 7 4 4T 4A22 1999102200403 19991022 00403 SO 1999 10 22 RAAA99E4011 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 512-540 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK FOUND SEAT TRACK CORRODED AT FS 512-540 AT LBL 27 ON NUT PLATE FLANGE. REPLACED SEAT TRACK PER ECO 99-05. 2 L 7 4 4T 4A22 1999102200404 19991022 00404 WP 1999 10 22 CALA9901382 1 19991015 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 200-218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND CUSP WEB CORRODED AT FS 200-218, LBL 40-58. THE CORRODED AREA WAS REMOVED IAW SRM 51-30-02 AND 51-10-0 4. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-03, AND 51-30-02. 2 L 7 2 4F A6WE 1999102200405 19991022 00405 WP 1999 10 22 CALA9901383 1 19991015 A 5230 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR AFT VERTICAL RIB LOWER END FITTING. THE FITTING WAS REMOVED AND REPL ACED IAW SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999102200406 19991022 00406 WP 1999 10 22 CALA9901384 1 19991015 A 5754 SKIN DOUG DC9 DC982 3022082 WP NR 2 LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND RT WING NR 2 SLAT DENTED. A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1. 2 L 7 2 4F A6WE 1999102200407 19991022 00407 WP 1999 10 22 CALA9901385 1 19991015 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND CENTER SEAT TRACK CORRODED BETWEEN FS 1174-1212, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW S RM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999102200408 19991022 00408 WP 1999 10 22 CALA9901386 1 19991015 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1429 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 1 INCH CRACK IN FLANGE OF LONGERON 2R AT FS 1429. THE CRACKED SECTION OF LONGERON WAS REMOVED IAW SR M 51-30-2 AND 51-30-4. A NEW SECTION OF LONGERON WAS INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-3, 51-10-4, AND 51-30-05 . 2 L 7 2 4F A6WE 1999102200409 19991022 00409 WP 1999 10 22 CALA9901387 1 19991015 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1332-1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND INTERCOSTAL CORRODED AT FS 1338-1332, LONGERON 28L TO 27L. THE INTERCOSTAL WAS REMOVED AND A NEW ONE W AS INSTALLED IAW SRM 51-10-04, 51-10-03, 51-30-2, AND 51-30-05. 2 L 7 2 4F A6WE 1999102200410 19991022 00410 WP 1999 10 22 CALA9901388 1 19991015 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1338-1328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND CUSP WEB CORRODED AT FS 1338-1328, LONGERON 18L. A NEW CUSP SECTION WAS INSTALLED IAW SRM 51-10-03 AND 53-05, FIGURE 25. 2 L 7 2 4F A6WE 1999102200411 19991022 00411 WP 1999 10 22 CALA9901389 1 19991015 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND AFT CABIN SERVICE DOOR OPENING FLOOR SUPPORT CORRODED AT STA 1155, LBL 48. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-03 AND 51-10-04. 2 L 7 2 4F A6WE 1999102200412 19991022 00412 WP 1999 10 22 CALA9901390 1 19991015 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 598-636 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND RT FLOOR SUPPORT CORRODED FROM STA 598-636, LONGERON 28R. THE SUPPORT WAS REMOVED AND A NEW ONE WAS IN STALLED IAW SRM 51-10-01, 51-10-03, AND 51-30-02. 2 L 7 2 4F A6WE 1999102200413 19991022 00413 WP 1999 10 22 CALA9901391 1 19991015 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 207 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 207, RBL 54.5. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS I NSTALLED IAW SRM 53-05, 51-30-01, AND 51-30-05. 2 L 7 2 4F A6WE 1999102200414 19991022 00414 EA 1999 10 22 COMA9960608 1 19991007 A 5320 601R31527179 ANGLE CNDAIR CL600 CL6002B19 EA PAX DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 ANGLE AT PAX DOOR ENTRANCE CORRODED (P/N 601R31527-179). PERFORMED A MAJOR REPAIR. REMOVED DAMAGED ANGLE AND INSTALLED A NEW FABRICATED ANGLE IAW WVAC EO NR 601R-53-0399A. 2 L 7 2 4F RT A21EA 1999102200415 19991022 00415 EA 1999 10 22 COMA9960609 1 19991007 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 THIS EO PROVIDES FOR THE DEVIATION FROM THE ORIGINAL REO. PERFORMED A MAJOR REPAIR SPLICE THE FLOORBEAM USING CANADAIR REO 601R-53-00-027 IAW 601R-53-0409. 2 L 7 2 4F RT A21EA 1999102200416 19991022 00416 EA 1999 10 22 COMA9960610 1 19991017 A 3260 WARNING LIGHT CNDAIR CL600 CL6002B19 EA LANDING GEAR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 920CA 7022 GEAR DISAGREE WARNING DURING CLIMBOUT OF CVG. AIRCRAFT RETURNED TO THE FIELD. PERFORMED FUNCTIONAL CHECK OF THE LANDIN G GEAR RETRACTION/EXTENSION SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999102200417 19991022 00417 EA 1999 10 22 COMA9960611 1 19991015 A 5210 HANDLE CNDAIR CL600 CL6002B19 EA PAX DOOR CONTAMINATED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 712CA 7244 CABIN DOOR OUTER HANDLE CAUTION MESSAGE AFTER DEPARTURE FROM OMA. AIRCRAFT RETURNED TO THE FIELD. REMOVED EXCESSIVE CR EASE CAUSING HYDRAULIC LOCK IN THE CABIN DOOR HANDLE ASSEMBLY. 2 L 7 2 4F RT A21EA 1999102200418 19991022 00418 EA 1999 10 22 COMA9960612 1 19991015 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR LACK OF LUBE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 931CA 7037 CABIN DOOR CAUTION MESSAGE AFTER DEPARTURE FROM YUL. AIRCRAFT RETURNED TO THE FIELD. LUBRICATED THE CABIN DOOR LATCH M ECHANISM. OPERATION OF THE CABIN DOOR WARNING SYSTEM SATISFACTORY. 2 L 7 2 4F RT A21EA 1999102200419 19991022 00419 EA 1999 10 22 COMA9960613 1 19991005 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 SERVICE DOOR FLOOR SUPPORT L ANGLE CORRODED BEYOND LIMITS (P/N 601R38303-105). PERFORMED A MAJOR REPAIR. REMOVED AND I NSTALLED A NEW THRESHOLD ANGLE (P/N 601R38303-239) IAW WVAC EO 601R-53-0391A. 2 L 7 2 4F RT A21EA 1999102200420 19991022 00420 EA 1999 10 22 COMA9960614 1 19991008 A 5320 601R31527131 CLEAT CNDAIR CL600 CL6002B19 EA PAX DOORWAY DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 THE CLEAT ON THE BRACKET AT THE PASSENGER DOOR THRESHOLD WAS DAMAGED. PERFORMED A MAJOR REPAIR. REMOVED THE DAMAGED CL EAT, FABRICATED AND INSTALLED A NEW CLEAT IAW WVAC EO 601R-53-0403. 2 L 7 2 4F RT A21EA 1999102200421 19991022 00421 NM 1999 10 22 UPS99230920 1 19991005 A 5751 HINGE BOEING 727 72722C 138400F NM RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, RT OUTBOARD AILERON OUTBOARD HINGE SUPPORT CRACKED. REPLACED AILERON HINGE CASTING IAW DWG NR 65-192 77. 2 L 7 3 4F A3WE 1999102200422 19991022 00422 NM 1999 10 22 UPS99230921 1 19991011 A 2730 BRACKET BOEING 727 72722C 138400F NM LT&RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, LT AND RT ELEVATOR POSITION SENSOR BRACKETS CRACKED. LT AND RT ELEVATOR POSITION SENSOR BRACKETS REP LACED IAW MM 20- 80-01. 2 L 7 3 4F A3WE 1999102200423 19991022 00423 NM 1999 10 22 UPS99230923 1 19991006 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 1148 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, WEB CRACKED ON LWR LEG AFT OF BS 1148 LBL 3 INTERCOSTAL. INTERCOSTAL REPAIRED IAW SRM 51-40-03 FIG 1. 2 L 7 3 4F A3WE 1999102200424 19991022 00424 NM 1999 10 22 UPS99230924 1 19991009 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, STRINGER CORRODED AT BS 480 STR 28L. STRINGER SPLICE SECTION REPAIRED IAW SRM 51-20-1 FIG 7. 2 L 7 3 4F A3WE 1999102200425 19991022 00425 NM 1999 10 22 UPS99230925 1 19991009 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, SEAT TRACK CRACKED AT BS 560 RT SIDE. REPAIRED IAW SRM 53-10-5 FIG 5. 2 L 7 3 4F A3WE 1999102200426 19991022 00426 NM 1999 10 22 UPS99230926 1 19991005 A 5753 CASTING BOEING 727 72722C 138400F NM NR 3 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, SUSPECT CRACK ON NR 3 L/E FLAP I/B ATTACH CASTING. NR 3 L/E FLAP REPLACED IAW MM 27-81-01. 2 L 7 3 4F A3WE 1999102200427 19991022 00427 NM 1999 10 22 UPS99230927 1 19991006 A 5230 BEAM BOEING 727 72722C 138400F NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, ON REMOVAL OF ACCORDION SEAL, CORROSION FOUND ON UPPER BEAM OF MAIN CARGO DOOR. CORROSION REMOVED FR OM UPPER BEAM, LIMITS CHECKED AND FOUND OUTSIDE REF SRM 51-10-6. BEAM REPLACED IAW SRM 51-30-2, WITH REF TO BOEING DWG NR 65-25337. ALL AREA RE-PROTECTED AND SEALED REF SRM 51-10-2. 2 L 7 3 4F A3WE 1999102200428 19991022 00428 NM 1999 10 22 UPS99230928 1 19991007 A 5230 SKIN BOEING 727 72722C 138400F NM CARGO DOOR NICKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, FWD CARGO DOOR LWR AFT CORNER SKIN NICKED. NICKED SKIN FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. S KIN BLENDED OUT LIMITS IAW SRM 52-00-2 FIG 1. FWD CARGO DOOR REPAIRED IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4. 2 L 7 3 4F A3WE 1999102200429 19991022 00429 NM 1999 10 22 UPS99230929 1 19991004 A 5320 FITTING BOEING 727 72722C 138400F NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, CRACK FOUND ON 940 FRAME FITTING UPPER FWD FLANGE BELOW FLOOR LEVEL NDT. COFIRMED CRACK, REPAIRED PE R EO B727-5310-3787. 2 L 7 3 4F A3WE 1999102200430 19991022 00430 NM 1999 10 22 UPS99230930 1 19991007 A 5320 WEB BOEING 727 72722C 138400F NM BS 277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, NOSE WHEEL WELL, CEILING WEB HAD SUSPECT CRACK AT BS 277 APPROX AND RBL 14. DAMAGED AREA TRIMMED OUT IAW SRM 51-40-2, ALL EXISTING FASTENER HOLES IN PERIMETER ROW OF DOUBLER ZERO-TIMED PER SRM 51-10-1. WEB REPAIRED IAW SRM 51-40-02. 2 L 7 3 4F A3WE 1999102200431 19991022 00431 NM 1999 10 22 UPS99230931 1 19991005 A 5230 BRACKET BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, AFT CARGO DOOR AFT HINGE AFT BRACKET CRACKED. REPLACED AFT CARGO AFT HINGE BRACKET IAW DRAWING NR 65 -18625. 2 L 7 3 4F A3WE 1999102200432 19991022 00432 NM 1999 10 22 UPS99230932 1 19991004 A 5230 ANGLE BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, CRACK IN AFT CARGO DOOR FWD HINGE FWD ANGLE. REPLACED ANGLE IAW DRAWING NR 65-18625. 2 L 7 3 4F A3WE 1999102200433 19991022 00433 NM 1999 10 22 UPS99230933 1 19991005 A 5260 WEB BOEING 727 72722C 138400F NM AFT AIRSTAIRS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, CRACK ON WEB AT LIGHTNING HOLE (UPPER ROW 2ND FROM AFT) RT TORQUE BOX AFT AIRSTAIRS. CRACK STOP DRIL LED IAW SRM 51-10-1, REPAIRED AREA IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999102200434 19991022 00434 NM 1999 10 22 UPS99230934 1 19990914 A 5741 69139017 PIN BOEING 727 72725C 138400H NM LT WING/FUS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-100-05.00-03) FOUND ON LEFT WING REAR BOTTLE PIN. REMOVED LT REAR BOTTLE PIN FOR COR ROSION. CORROSION WAS OUT OF LIMITS. INSTALLED NEW REAR LT BOTTLE PIN, ALL WORK DONE IAW MM 57-41-1 PG 403-404. 2 L 7 3 4F A3WE 1999102200435 19991022 00435 NM 1999 10 22 UPS99230935 1 19990910 A 5720 BAC15171406 STIFFNER BOEING 727 72725C 138400H NM WS 173.25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING CUSTOMER CARD NR 997970, (WINGS 237) FOUND STIFFENER AT WS 173.25 CORRODED BEYOND ALLO WABLE LIMITS. REPLACEMENT OF STIFFENER WILL BE ACCOMPLISHED ON CUSTOMER ID 997970, PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999102200436 19991022 00436 NM 1999 10 22 UPS99230936 1 19990910 A 5720 BAC15171406 STIFFNER BOEING 727 72725C 138400H NM WS 185.3 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING CUST ID 997970, DISCOVERED RWS 185.30 VERTICAL STIFFENER CORRODED BEYOND ALLOWABLE LIM ITS. REPLACEMENT OF STIFFENER WILL BE ACCOMPLISHED ON CUSTOMER ID 997970 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999102200437 19991022 00437 NM 1999 10 22 UPS99230937 1 19991016 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 344-360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK BETWEEN BS 344 AND 360 LBL 25 WL 208. REPLACED SEAT TRACK AT 340 TO 480, LB L 25 WL 208 PER SRM 51-30-2, 53-10-5 AND 53-10-1. 2 L 7 3 4F A3WE 1999102200438 19991022 00438 NM 1999 10 22 UPS99230938 1 19991008 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING 997311 FOUND CORROSION ON STR 5 LT BS 1130 - BS 1148. CORROSION FOUND OUT OF LIMIT. C UT OUT DAMAGED AREA BS 1112 - 1165 STR 5 LT, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1999102200439 19991022 00439 NM 1999 10 22 UPS99230939 1 19991006 A 5320 SHEAR WEB BOEING 727 72725C 138400H NM BS 635-675 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, UPON REMOVAL OF SEAT TRACK AT RBL 65 FOUND SHEAR WEB AT MID GALLEY DOOR CRACKED AND DAMAGED BS 635 T O BS 675. REMOVED DAMAGED AREA AND CORRODED STIFFENER BRACKET, FABRICATED REPAIR PARTS AND INSTALLED PER 727 SRM 51-30- 5, 51-30-2, 51-40-2. 2 L 7 3 4F A3WE 1999102200440 19991022 00440 NM 1999 10 22 UPS99230940 1 19991013 A 5320 BEAM BOEING 727 72725C 138400H NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING CUSTOMER CARD NR 997322 (FUSELAGE 87) FOUND CORROSION ON SIDE LOAD BEAM AT BS 740, RBL 20 - RBL 32, WL 170. REMOVED AND REPLACED SIDE LOAD BEAM PER SRM 51-30-2 AND DRAWING NR 65-15940. 2 L 7 3 4F A3WE 1999102200441 19991022 00441 NM 1999 10 22 UPS99230941 1 19990923 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI WHILE WORKING 997306 FOUND SHEAR TIE CRACKED AT BS 320 BETWEEN 524 AND 525 RT. REMOVED CRACKED SHEAR TIE AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1999102200442 19991022 00442 NM 1999 10 22 UPS99230942 1 19991005 A 5260 WEB BOEING 727 72722C 138400F NM AFT AIRSTAIRS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, CRACK ON WEB AT FWD LOWER LIGHTNING HOLE RT TORQUE BOX AFT AIRSTAIRS. REPAIRED AREAS IAW SRM 51-40-3 . 2 L 7 3 4F A3WE 1999102200443 19991022 00443 WP 1999 10 22 UPS99830919 1 19991004 A 5720 5804007T6013 FITTING DOUG DC8 DC871F 302199D WP WS 508 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, FITTING (P/N 5804007T6013) AT XRS 508, LT WING FOUND TO BE CRACKED. REMOVED, FABRICATED AND REPLA CED THE FITTING IAW DWG 5804007 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999102200444 19991022 00444 WP 1999 10 22 UPS99830943 1 19991010 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:SV 1 CRACK IN WING SKIN LT WING 18 I/B OF NR 1 PYLON. FABRICATED AND INSTALLED ALL BUSHINGS IAW REO 067 99. FABBED STRAPS, SPLICES, DOUBLER, TRIPLER AND SKIN FILLER. CUT INTERNAL DOUBLER AND FABBED REPLACEMENT SEGMENT OF I NTERNAL DOUBLER, TRIPLER. REAMED AND COINED HOLES AS MARKED IAW REO 06799. INSTALLED REPAIR PARTS IAW REO 06799. 2 L 7 4 4F RT 4A25 1999102200445 19991022 00445 WP 1999 10 22 UPS99830944 1 19990907 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 80 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:SV, FUSELAGE FRAME AT STA 80 LT O/B NOSE WHEEL WELL IS DAMAGED. REC'D SERVICEABLE FRAME SECTION FROM AI RCRAFT (S/N 46038), HEAT TREATED REPAIRS DOUBLERS 7075-0--063 TO 7075-T6 IAW TPS 1003 REV A. FABBED DOUBLERS IAW REO 06 791. DYE PENT REPAIR DOUBLERS IAW MIL STD .153 7B. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51 -1-20D & 51-1-11. 2 L 7 4 4F RT 4A25 1999102200446 19991022 00446 WP 1999 10 22 UPS99830945 1 19990820 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 87 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:SV 2 FRAME DAMAGED AT -87 LEFT O/B NWW. FABBED AND INSTALLED FRAME AND REPAIR PARTS (SPLICES) IAW REO 0 6776 & DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999102200447 19991022 00447 WP 1999 10 22 UPS99830946 1 19990820 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 87 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:SV 2 FRAME DAMAGED AT -87 RT O/B OF NWW. REC'D SERVICEABLE FRAME SECTION FROM A/C (S/N 46038). HEAT TR EATED REPAIR PARTS 7075-0 TO 7075 T6.063 IAW TPS-1003 REV A. INSTALLED SERVICEABLE FRAME SECTION IAW DC8 SRM 51-1-20D & 51-1-21. FABBED AND INSTALLED REPAIR SPLICES IAW DC8 SRM 51-1-20D. FABBED AND INSTALLED NEW (P/N 5613861-68) CHANNEL IAW DWG 5613861 & DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999102200448 19991022 00448 NM 1999 10 22 SCNA99602 1 19991012 A 5320 BEAM BOEING 727 7272A1 138407F NM BS 1183 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINTENANCE CHECK, A CRACKED DOUBLER WAS FOUND AT BS 1183 PRESSURE WEB AT THE 6 O'CLOCK POSITION ON THE L EFT VERTICAL I BEAM ON THE BOTTOM. REMOVED AND REPLACED THE VERTICAL STIFFENER. 2 L 7 3 4F A3WE 1999102200449 19991022 00449 NE 1999 10 22 RAIA9910018 2 19991015 A 7310 5905587 FILTER AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE CLOGGED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 422TE 106 121018 7412-STL - RIGHT ENGINE FUEL CLOG LIGHT ON. MAINTENANCE REPLACED FUEL PUMP INLET FILTER. 2 H 7 2 4T 4 T RT A53EU E20NE 1999102200450 19991022 00450 SO 1999 10 22 RAIA9910019 1 19991015 A 3240 0132AEV1 SENSOR EMB 145 EMB145 SO RT MLG BRAKE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 806HK 635 635 145112 6237-JFK - RIGHT OUTBOARD BRAKE TEMP INDICATOR FLUCTUATES. MAINTENANCE REPLACED TEMP SENSOR. 2 L 7 2 4F RT T00011AT 1999102200451 19991022 00451 1999 10 22 RAIA9910020 3 19991017 A 6140 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 4785 4785 41039 76082 6165-JFK - RIGHT GREEN BETA LIGHT INOP. MAINTENANCE REPLACED BETA SWITCH. 2 L 7 2 4T 4 T RT A41NM E18NE 1999102200452 19991022 00452 EU 1999 10 22 RAIA9910021 1 19991017 A 3610 M832481226 O-RING JETAIR JETSTM JETSTM4101 1500501 EU RT WING LE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 553HK 41066 6115-JFK - RIGHT DUCT OVERTEMP LIGHT ON. MAINTENANCE REPLACED LEADING EDGE DUCT O-RING. 2 L 7 2 4T RT A41NM 1999102200453 19991022 00453 WP 1999 10 22 EIAA990138 1 19990502 A 5320 PAN DOUG DC9 DC933F 302207A WP BS 579 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A CRACK WAS FOUND IN THE WINDOW RING PAN, LOWER FORWARD CORNER, AT STA 579-L14R. FABRICATED REPAI R ANGLE AND INSTALLED PER ECRA 942-53-026-2. (X) 2 L 7 2 4F A6WE 1999102200454 19991022 00454 WP 1999 10 22 EIAA990142 1 19990421 A 5730 SKIN DOUG DC9 DC933F 302207A WP WS 515 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 DURING C-CHECK, THE RIGHT AND LEFT WING LEADING EDGE SKIN WAS FOUND TO HAVE CORROSION AT STA 515.156 (LT), STA 526.718 ( RT), AND STA 464.750 (RT). REPAIRED PER ECRA NR 942-57-015-2. (X) 2 L 7 2 4F A6WE 1999102200455 19991022 00455 WP 1999 10 22 EIAA990143 1 19990422 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 351 MISDRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE SUPPORT FITTING AT STA 351, LONGERON 23R WAS FOUND TO HAVE A HOLE DRILLED IN RADIUS. ALSO, HO LE DRILLED IN FRAME RADIUS AT SAME LOCATION. REMOVED AND REPLACED NEW FITTING PER SRM 51-10-1 PAGES 4-6. FABRICATED DO UBLER AND SHIMS PER SRM 53-03 FIG 2A SHEETS 1-5. CUT AND TRIMMED DAMAGED PORTIONS OF FRAME PER SRM 53-03 FIG 5. INSTAL LED DOUBLERS AND SHIMS. (X) 2 L 7 2 4F A6WE 1999102200456 19991022 00456 WP 1999 10 22 EIAA990174 1 19990414 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 446 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, SKIN DAMAGE WAS FOUND ON THE RT FUSELAGE AT STA 446 BETWEEN L24 AND L25. HFEC INSPECTED THE TRIM- OUT IN THE SKIN FOR CRACKS AND CORROSION PER DOUGLAS NDT SPM, PART 6, 06-00-07, FIG 1. FABRICATED A REPAIR FILLER FROM 2014-T6 OR 2024-T3, 0.05 INCH THICK. FABRICATED AN INTERNAL FINGER DOUBLER FROM 6AL-4V TITANIUM, 0.025 INCH THICK. REP AIRED PER ECRA 942-53-007-2 AND DC9 SRM 53-04 FIG 38. (X) 2 L 7 2 4F A6WE 1999102200457 19991022 00457 WP 1999 10 22 EIAA990175 1 19990413 A 5400 FAIRING DOUG DC9 DC933F 302207A WP NR 2 ENGINE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING -CHECK, CRACKS WERE FOUND ON THE NR 2 ENGINE INBD AFT FAIRING AND DOUBLER. REPAIRED PER ECRA 942-78-004-2. REF: OPER CONTROL NR 99ZZZX4019. (X) 2 L 7 2 4F A6WE 1999102200458 19991022 00458 WP 1999 10 22 99ZZZX4019 1 19990413 A 5400 DOUBLER DOUG DC9 DC933F 302207A WP NR 2 ENGINE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING -CHECK, CRACKS WERE FOUND ON THE NR 2 ENGINE INBD AFT FAIRING AND DOUBLER. REPAIRED PER ECRA 942-78-004-2. REF: OPER CONTROL NR EIAA990175. 2 L 7 2 4F A6WE 1999102200459 19991022 00459 WP 1999 10 22 EIAA990176 1 19990401 A 5280 SKIN DOUG DC9 DC933F 302207A WP RT MLG DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A SMALL CRACK WAS FOUND ON THE INNER SKIN OF THE RT MAIN LANDING GEAR DOOR. CUT OUT CRACKED AREA OF DOOR INNER SKIN, NDT INSPECTED FORMER AND SKIN, NO CRACKS FOUND. FABRICATED FILLER AND DOUBLER, ALODINED, PRIMED AND INSTALLED WET WITH SEALANT PER ECRA 942-52-009-2 AND DC9 SRM 51-30-3 PAGES 16 AND 18, SRM 51-30-2 PAGES 1-14, SPM PART 6, 06-00-07. (X) 2 L 7 2 4F A6WE 1999102200460 19991022 00460 WP 1999 10 22 EIAA990177 1 19990528 A 5320 SILL DOUG DC9 DC933F 302207A WP R5 DOORWAY CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 EAC - DURING C-CHECK, THE R5 DOOR CUT-OUT, UPPER INTERNAL SILL CONTACT AREA WAS FOUND TO HAVE CHAFE MARKS. BLENDED AREA PER SPM 53-30-01 FIG 1. FABRICATED NEW SHIM AND ALODINED PER SRM 31-10-02 PAGE 1. PRIMED NEW SHIM IAW SRM 30-40-05 PA GES 1-4. INSTALLED NEW SHIM IAW SRM 51-10-02, PAGES 1-41. (X) 2 L 7 2 4F A6WE 1999102200461 19991022 00461 WP 1999 10 22 EIAA990124 1 19990505 A 5720 FITTING DOUG DC9 DC933F 302207A WP RT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE RIGHT MLG FITTING BRACE ATTACH LUG FACE WAS FOUND CORRODED. REPAIRED PER ECRA NR 942-57-003-2 . (X) 2 L 7 2 4F A6WE 1999102200462 19991022 00462 WP 1999 10 22 EIAA990125 1 19990125 A 5720 FITTING DOUG DC9 DC933F 302207A WP LT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE LEFT MLG FITTING BRACE ATTACH LUG FACE WAS FOUND CORRODED. REPAIRED PER ECRA NR 942-57-003-2. (X) 2 L 7 2 4F A6WE 1999102200463 19991022 00463 EU 1999 10 22 99ZZZX4020 1 19990822 A 2810 SD3560002XJ FUEL TANK STBROS SD3 SD330 8100602 EU NR 1 CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 331SB 1200 SH3015 MAINTENANCE DISCOVERED A FUEL LEAK IN FORWARD FUEL CELL NR 1. TROUBLESHOOTING REVEALED TANK TO BE CRACKED. 1.5 INCH LO NG CRACK IN BOTTOM OF FUEL TANK. FUEL TANK CRACKED NEAR LEFT SIDE. AFT GRAVITY FEED ADAPTER MOUNTING FLANGE. REPAIRED IAW SD3-30 STRUCTURAL REPAIR MANUAL AND AC 4313-1B CHAPTER 2 SECTION 4. DOCUMENTED ON FAA FORM 337. PERFORMED LEAK AN D FUNCTIONAL CHCKS, AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T A41EU 1999102200464 19991022 00464 CE 1999 10 22 99ZZZX4021 1 19990809 A 5311 26110197 FRAME CESSNA 208 208B 2073701 CE BS 234 DAMAGED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 948FE 208B0052 BIL - DAMAGED SUB-FLOOR FRAMES IN AFT CARGO AREA. FIVE FRAMES REQUIRED REPLACEMENT DUE TO DISFIGURATION. 1 H 7 1 3T A37CE 1999102200465 19991022 00465 CE 1999 10 22 99ZZZX4022 1 19990809 A 5311 261102917 FRAME CESSNA 208 208B 2073701 CE BS 234 DAMAGED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 948FE 208B0052 BIL - DAMAGED SUB-FLOOR FRAMES IN AFT CARGO AREA. FIVE FRAMES REQUIRED REPLACEMENT DUE TO DISFIGURATION. 1 H 7 1 3T A37CE 1999102200466 19991022 00466 CE 1999 10 22 99ZZZX4023 1 19990809 A 5311 26110341 FRAME CESSNA 208 208B 2073701 CE BS 246.5 DAMAGED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 948FE 208B0052 BIL - DAMAGED SUB-FLOOR FRAMES IN AFT CARGO AREA. FIVE FRAMES REQUIRED REPLACEMENT DUE TO DISFIGURATION. 1 H 7 1 3T A37CE 1999102200467 19991022 00467 CE 1999 10 22 99ZZZX4024 1 19990809 A 5311 261102919 FRAME CESSNA 208 208B 2073701 CE BS 246.5 DAMAGED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 948FE 208B0052 BIL - DAMAGED SUB-FLOOR FRAMES IN AFT CARGO AREA. FIVE FRAMES REQUIRED REPLACEMENT DUE TO DISFIGURATION. 1 H 7 1 3T A37CE 1999102200468 19991022 00468 CE 1999 10 22 99ZZZX4025 1 19990809 A 5311 261103411 FRAME CESSNA 208 208B 2073701 CE BS 259 DAMAGED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 948FE 208B0052 BIL - DAMAGED SUB-FLOOR FRAMES IN AFT CARGO AREA. FIVE FRAMES REQURIED REPLACEMENT DUE TO DISFIGURATION. 1 H 7 1 3T A37CE 1999102200469 19991022 00469 NM 1999 10 22 P2EA99239 1 19990906 A 2550 INSULATION BOEING 737 737230 NM CARGO COMPT OUT OF POSITION A P2EA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 05 122NJ 22120 MCI - THE FOLLOWING WAS REPORTED DURING CREW PRE-DEPARTURE WALK-AROUND. ODOR COMING FROM AIR CONDITIONING DUCTING. FOU ND APU BLEED DUCT INSULATION BLANKET, IN AFT CARGO PIT BEHIND FORWARD WALL, SECURED WITH CARGO PIT TAPE. TAPE WAS BURNE D AND BRITTLE. PROPERLY SECURED NEW BLANKET, RAN A/C PACKS, NO MORE ODOR NOTED. (X) 2 L 7 2 4F RT A16WE 1999102200470 19991022 00470 NE 1999 10 22 CA990927072 2 19990910 A 7314 7214003 INLET STRAINER AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211* 54555 NE INLET STRAINER DISINTEGRATED W K NONE O OTHER IN INSP/MAINT 1 CA 41063 (CAN) NO FUEL FLOW AT START-UP. INLET STRAINER ON LP FUEL PUMP DISINTEGRATED AND WAS INGESTED BY THE FUEL METERING UNIT INLET SCREEN. 2 L 7 2 4F 4 F RT A46NM A12EU 1999102200471 19991022 00471 EU 1999 10 22 99ZZZX4026 1 19990607 A 6710 SC5083 SERVO SNIAS AS350 AS350B3 8680954 EU MAIN ROTOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 103LN 79 671 3128 LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U NC H9EU 1999102200472 19991022 00472 EU 1999 10 22 99ZZZX4027 1 19990210 A 6210 1051585403 BUSHING BOLKMS 117 BK117B1 5626012 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 62LF 510 7163 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999102200473 19991022 00473 NM 1999 10 22 ASAA9940146 1 19990904 A 3397 WIRE BOEING 737 7374Q8 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 SEA - DURING MAINTENANCE CHECK, 2 EACH AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED WIRING A ND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999102200474 19991022 00474 SO 1999 10 22 C2XA99BT087 1 19990911 A 3350 20131A BATTERY EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14974 145161 EWR - DURING ROUTINE CHECK, FOUND NR 2 BATTERY PACK LOW CHARGE. REMOVED AND REPLACED BATTERY PACK WITH SERVICEABLE UNIT . OPS CHECKED, SYSTEM GOOD. (X) 2 L 7 2 4F RT T00011AT 1999102200475 19991022 00475 EA 1999 10 22 MASA99150 1 19990826 A 3510 380270260 OXYGEN LINE VF5341 CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A MASA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SW 07 7305V RCF6706 7305 BHM/PHL - FLT 5751 - DURING TAXI OUT, THE CREW REPORTED THE OXYGEN PRESSURE WENT TO ZERO. THE AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE FOUND THE OXYGEN LINE CRACKED. MAINTENANCE REMOVED AND REPLACED THE OXYGEN LINE, OPS CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999102200476 19991022 00476 WP 1999 10 22 GTIA9901102 1 19990901 A 2560 PACK DOUG DC9 DC982 3022082 WP R1 DOORWAY DETACHED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 DTW - FLT 612 - R1 SLIDE PACK CAME OFF. R1 SLIDE PACK INSTALLED IAW 25-61 OF MD-80 MM. NO DEFECTS NOTED. (X) 2 L 7 2 4F A6WE 1999102200477 19991022 00477 WP 1999 10 22 GTIA9901103 1 19990902 A 3350 SOCKET DOUG DC9 DC987 3022087 WP ROW 3F DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 807NK 49777 EMERGENCY FLOOR TRACK LIGHT BULB NEAR SEAT 3F INOPERATIVE AS WITH BARE WIRE SHOWING. FOUND BAD LIGHT SOCKET ASSEMBLY. R EMOVED AND REPLACED SOCKET ASSEMBLY AS REQUIRED. OPERATION CHECK GOOD ON RAMP AT THIS TIME IAW MM 33-00-0. (X) 2 L 7 2 4F RT A6WE 1999102200478 19991022 00478 NM 1999 10 22 AALA991321 1 19990902 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 776AN 29582 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY ON FORWARD LEFT SIDE OF FORWARD GALLEY COAT CLOSET INO PERATIVE. REPLACED EMERGENCY EXIT LIGHT ON FORWARD LEFT SIDE OF FORWARD GALLEY COAT CLOSET. SYSTEM GROUND CHECKED, NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 1999102200479 19991022 00479 NM 1999 10 22 99ZZZX4028 1 19990813 A 7830 BACTJ6AY0B0806D TEE BOEING 737 737236 1384476 NM LT MLG WW CRACKED A E6RA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 625AC 23165 FLIGHT ATTENDANT REPORTED SMOKE IN FORWARD GALLEY. SMOKE SPREAD THROUGHOUT THE AIRCRAFT. FOUND THRUST REVERSER LOCK-OU T FITTING LEAKING. REPLACED FITTING. 2 L 7 2 4F RT A16WE 1999102200480 19991022 00480 NM 1999 10 22 BJNA990802 1 19990818 A 3350 1000679 LIGHT BOEING 737 737282 13844AT NM L2 DOOR INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 EMERGENCY EXIT LIGHT ON L-2 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON L-2 DOOR PER 33-51-101. (X) 2 L 7 2 4F RT A16WE 1999102200481 19991022 00481 NE 1999 10 22 N8TA990801 2 19990801 A 7313 FUEL NOZZLE BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE DISPLATED A N8TA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE TO TAKEOFF 1 WP 19 757NA 24567 30725 DURING TALKEOFF, FIRE WARING ACTIVATED FOR NR 2 ENGINE. CREW INITIATED FIRE EXTINGUISHER AND ENGINE SHUT DOWN PROCEDURE S. PRELIMINARY INVESTIGATION REVEALED COMBUSTION CASE BURN-THROUGH AT NR 9 FUEL NOZZLE. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1999102200489 19991022 00489 EU 1999 10 22 99ZZZX4036 1 19990825 A 2612 FIRE DETECTOR AEROSP AS355 AS355E 8680805 EU NR 1 ENGINE FAILED A ALGA O OTHER N FALSE WARNING CR CRUISE 1 SW 03 372E 5208 DURING CRUISE FLIGHT, NR 1 ENGINE FIRE LIGHT ILLUMINATED. BROKEN TERMINAL ON NR 1 ENGINE FIRE DETECTOR SENSOR. (FALSE INDICATION). 1 G 7 2 3U H11EU 1999102200493 19991022 00493 WP 1999 10 22 9904269152 1 19991012 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F A6WE 1999102200494 19991022 00494 NM 1999 10 22 DL76G992272 1 19991009 A 2120 AIR DIST BOEING 767 767332 1382001 NM ROW 10 ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1604R 30180 ELECTRICAL SMELL COMING FROM MID CABIN JUST AFT OF MID GALLEY. FUMES ONLY DEPOWERED UTILITY BUSSES AND AIRSHOW P ASSENGER NOTED CRACKLING IN HEADSET ALONG WITH FUMES ROW 10. DROPPED CEILING PANEL AND CHECKED AREA, FREEZER, OVE N AND CHILLER OPERATING, UNABLE TO DETECT ANY FUMES. REF CMI C/N 101490364 AND 101290324 FOR POSSIBLE CAUSE. 2 L 7 2 4F RT A1NM 1999102200495 19991022 00495 WP 1999 10 22 DLL19992273 1 19991015 A 2130 DUCT LKHEED 1011 10113853 5265020 WP RIGHT LOOSE A DALA B EMER. DESCENT O OTHER CR CRUISE 1 SO 27 769DL 193H1218 AT FL 350 MUFFLED POP SOUND HEARD IN COCKPIT. FIRST CLASS CABIN PRESS CONTROL LOST UNCOMMANDED 1500 RPM CABIN RATE OF C LIMB. PNEUMATIC SYS ISOLATED AS PER SOP AND ACFT DESCENDED TO 18000 FT, CABIN PRESS CONTROL REGAINED AS ACFT DESCEND ED BELOW FL 200 MAX CABIN ALT 9000 FT. FOUND DUCT LOOSE IN ECS COMPARTMENT. REINSTALLED SAME. 2 L 7 3 4F A23WE 1999102200496 19991022 00496 NM 1999 10 22 DL73E992274 1 19991015 A 2150 DUCT BOEING 737 737247 138448D NM APU BLEED FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 236WA 20232 23184 AIRCRAFT WOULD NOT PRESSURIZE AFTER T/O CONFIGURED FOR RIGHT BLEED AND RIGHT PACK OPERATION. AUTO/STBY/AND MANUAL MODES ATTEMPED. OUTFLOW VALVE FULL CLOSED FWD OUTFLOW VALVE CLOSED. FOUND APU BLEED AIR DUCT RUPTURED. REPLACED SAME. 2 L 7 2 4F A16WE 1999102200497 19991022 00497 NM 1999 10 22 DL72E992275 1 19990913 A 5753 652163362 SKIN BOEING 727 727247 138408F NM NR 4 TE MIDFLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 DURING SHOP INSPECTION, THE UPPER SKIN WAS FOUND WORN AT THE OUTBOARD END LEADING EDGE. THE SKIN WAS REPAIRED PER CMM 5 7052-0, FIG 803, BY CUTTING OUT THE DAMAGE AND INSTALLING A DOUBLER AND FILLER. 2 L 7 3 4F A3WE 1999102200498 19991022 00498 NM 1999 10 22 DL76L992277 1 19991015 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 185DN 27961 EMERGENCY EXIT LIGHT BATTERY CHARGER FAILED TO CHARGE BATTERY. UNIT ALSO FAILED SELF TEST. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 1999102200499 19991022 00499 NM 1999 10 22 DLM88992279 1 19991016 A 2121 FAN 6054578 DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 904DE 53409 AFTER T/O, F/A REPORTED A STRONG ELEC/CHEM ODOR COMING FROM THE AFT OF A/C. ODOR BECAME SO STRONG F/A COULD NOT GO AFT OF THE GALLEY. EMERGENCY LANDING BY CREW AT YYZ. CAPT REFUSED AIRCRAFT. CABIN RECIRC FAN FOUND TO HAVE INTERNAL DAMAG E. PLACARD PER MEL 21-00-43. C/BS J-8 J-9 J-10 PULLED AND COLLARED. 2 L 7 2 4F RT A6WE 1999102200500 19991022 00500 NM 1999 10 22 DLM88992280 1 19991016 A 3350 POWER SUPPLY RPS1 DOUG MD88 MD88 3023688 NM ROW 24-33 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 953DL 0339 49884 ON INSPECTION, FOUND EMERGENCY PATH LIGHTS FROM ROWS 24 TO 33 WOULD NOT TEST. REPLACED AFT POWER SUPPLY, OPS OF LIGHTS NORMAL. 2 L 7 2 4F RT A6WE 1999102200501 19991022 00501 NM 1999 10 22 DL757992281 1 19991016 A 3350 BULB 767 BOEING 757 757232 1384965 NM L1 DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 690DL 27585 L1 EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 2 4F RT A2NM 1999102200502 19991022 00502 NM 1999 10 22 DL757992282 1 19991016 A 2530 FILTER BOEING 757 757232 1384965 NM GALLEY CLOGGED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 629DL 22919 SLIGHT ELECTRICAL/BURNING PLASTIC SMELL IN F/C GALLEY. SECURED POWER TO F/C GALLEY AND ODOR DISSIPATED. REPLACED F/C F REEZER FILTER. 2 L 7 2 4F RT A2NM 1999102200503 19991022 00503 NM 1999 10 22 DL72S992284 1 19991007 A 5754 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 RIB CRACKED 2ND FROM I/B END ON NR 5 L/E SLAT. STOP DRILLED CRACK 2ND FROM I/B RIB ON NR 5 L/E SLAT. DRILLED VP DOUBLE R FOR RIB 2ND FROM I/B NR 5 L/E SLAT. TREAT AND PAINT PER P/S 900-2-5. OK INSTALLED REPAIR. INSTALLED REPAIR DOUBLER PER M/M 57-40-0 FIG 805. 2 L 7 3 4F A3WE 1999102200504 19991022 00504 NM 1999 10 22 DL72S992285 1 19991007 A 5754 RIB BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 RIB CRACKED NR 8 L/E SLAT O/B RIB. FABRICATED DOUBLER, REPAIRED PER M/M 57-54-0 FIG 814. 2 L 7 3 4F A3WE 1999102200505 19991022 00505 NM 1999 10 22 DL72L992286 1 19991017 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM AFT AIRSTAIR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 509DA 21311 AFT OVERHEAD AIRSTAIR DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY AND BATTERY'S OPS NOW OK. 2 L 7 3 4F A3WE 1999102200506 19991022 00506 NM 1999 10 22 DLM11992287 1 19991017 A 3244 TIRE DOUG MD11 MD11 3023602 NM LT MLG FAILED A DALA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 809DE 48480 LOST NR 6 MAIN TIRE RETREAD ON T/O. AFTER GEAR EXTENSION SYSTEM 1 HYD QTY STARTED TO DECREASE AND HAD ANTISKID FAULT. R EPLACED WHEEL ASSY, REPLACED RUPTURED HYDRAULIC LINES. 2 L 7 3 4F RT A22WE 1999102200507 19991022 00507 NM 1999 10 22 DL72S992288 1 19990714 A 5753 652163361 SKIN BOEING 727 727232 1384082 NM LT TE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 LWR L/E SKIN WORN I/B END OF FLAP. REPAIRED OER MM 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999102200508 19991022 00508 NM 1999 10 22 DL72S992289 1 19990714 A 5753 652163361 SKIN BOEING 727 727232 1384082 NM LT TE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 APPROXIMATELY 3 INCH LONG WEAR AREA, LWR L/E SKIN O/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999102200509 19991022 00509 NM 1999 10 22 VNAA9910008 1 19991015 A 3240 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARKING BRAKE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 436JS 664 3052 AIRCRAFT WAS EN ROUTE TO PIT WHEN THE EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE ILLUMINATED. THE FLIGHT CREW REFE RENCED THE QRH AND ATTEMPTED TO CLEAR THE MESSAGE. THE WARNING DID NOT EXTINGUISH AND THE CREW DIVERTED TO CHO. THE AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FERRIED THE AIRCRAFT TO PIT. REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-43-00. FUNCTIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102200510 19991022 00510 NM 1999 10 22 VNAA9910009 1 19991016 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 9A DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 434JS 8489 103 3051 THE FLIGHT CREW FOUND THE EMERGENCY EXIT LIGHT AT SEAT 9A WAS NOT WORKING. MAINTENANCE REPLACED THE EMERGENCY BATTERY A T THE 6LK POSITION IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED AND TH E AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102200511 19991022 00511 NM 1999 10 22 VNAA9910010 1 19991016 A 2913 42086 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 459PS 4319 3070 DURING CLIMBOUT, THE FLIGHT CREW RETRACTED THE LANDING GEAR AND RECEIVED MULTIPLE CAS MESSAGES INDICATING THAT MAIN HYDR AULIC POWER WAS LOST. THE FLIGHT CREW REFERENCED THE QRH AND DIVERTED TO TOL. THE AIRCRAFT LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED THE MAIN HYDRAULIC AC PUMP ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-11-00. FUNCTIO NAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102200512 19991022 00512 WP 1999 10 22 RAIA9910022 2 19991018 A 7310 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 871JX 46957 46957 871 66065 LAX- LEFT ENGINE DIDN'T MAKE TARGET TORQUE. MAINTENANCE REPLACED FUEL BY-PASS VALVE FOR LEFT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999102200513 19991022 00513 1999 10 22 RAIA9910023 3 19991017 A 6112 DEICE JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 553HK 7466 7466 41066 JFK- RIGHT PROP DEICE FAILED. MAINTENANCE REPLACED RIGHT PROP. 2 L 7 2 4T RT A41NM 1999102200514 19991022 00514 WP 1999 10 22 AT9900678 1 19990909 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 680-756 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 CABIN FLOOR PANEL (NR 75) HAD CORROSION AROUND THE ATTACHMENT DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, TH E HOLES. REMOVED CORROSION AROUND FASTENER HOLES OF FLOOR PANEL NR 75. CHECKED WITH CALIPER NR A-2542 IAW DC9 SRM 53-0 1 AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOOR PANEL WITH 7075 T-6 .025 21 X 76 7/8 AND NEW HAT CHANNELS TREATED AND PRIMED FLOOR PANEL AND HAT CHANNELS IAW DC9 SRM 51-10-03, IAW DC9 SRM 57-10-03, IAW DC9 SRM 51-10-02 AND 53-21-0 FI G 4. 2 L 7 2 4F A6WE 1999102200515 19991022 00515 WP 1999 10 22 AT9900733 1 19991003 A 5310 SUB-FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, CORROSION WAS FOUND IN THE SUB FLOOR AT 160-200. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-02, 51-30-08, AND 53-01 FIG 2. 2 L 7 2 4F A6WE 1999102200516 19991022 00516 WP 1999 10 22 AT9900734 1 19990925 A 5311 9919619503 FRAME DOUG DC9 DC932 3022066 WP BS 737 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, BS 737 MAINFRAME LEFT SIDE HAS THREE CRACKS. REMOVED AND REPLAC ED LEFT MAINFRAME BS 737 IAW DC9 EO 12-5311-29-B1044. 2 L 7 2 4F A6WE 1999102200517 19991022 00517 WP 1999 10 22 AT9900735 1 19991003 A 5311 9915842135 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN CANTED FRAME AT BS 1143R. CUT AND REMOVED CANTED FRAME AT BS 1143R IAW EO 99-1285. 2 L 7 2 4F A6WE 1999102200518 19991022 00518 WP 1999 10 22 AT9900736 1 19990917 A 5347 2955978 CARGO TRACK DOUG DC9 DC932 3022066 WP BS 218-351 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FORWARD PIT CARGO TRACK BS 218-484. FOUND AR EA AT BS 218-351RIGHT SIDE TO BE OUT OF LIMITS USING CALIPER NR A2543. REMOVED AFFECTED AREA OF TRACK AND CLEANED CORRO SION ON REMAINING AREA OF TRACK. ALL WORK DONE IAW DC9 SRM 53-05 FIG 4C, 51-30-01, 51-10-04, AND 51-10-03. 2 L 7 2 4F A6WE 1999102200519 19991022 00519 WP 1999 10 22 AT9900737 1 19990912 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 579-690 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL,FOUND FLOORBOARD #71 TO HAVE CRACKED HAT CHANNEL AND CORRODED SKI N BEYOND LIMITS. CORRECTIVE ACTION: REMOVED AND FABRICATED FLOORBOARD #71 SKIN AND HA T CHANNEL IAW DC9 SRM 51-30-02, 53-01 FIG 1, 53-20-0, 51-10-03, AND 51-10-04. 2 L 7 2 4F A6WE 1999102200520 19991022 00520 WP 1999 10 22 AT9900738 1 19990910 A 5310 4912798501 STRUCTURE DOUG DC9 DC932 3022066 WP BS 207 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOORBOARD NR 71 TO HAVE CRACKED HAT CHANNEL AND CORRODED SKIN BEYOND LIMITS. REMOVED AND FABRICATED FLOORBOARD NR 71 SKIN AND HAT CHANNEL IAW DC9 SRM 51-30-02, 53-01 FIG 1, 53- 20-0, 51-10-03, AND 51-10-04. 2 L 7 2 4F A6WE 1999102200521 19991022 00521 WP 1999 10 22 AT9900739 1 19991004 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 155 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 831AT 47674 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENT THAT WAS FORMED FROM INSIDE. FABRICATED REPAIR DOUBL ER AND FILLER IAW RES NR 07421, DC9 SRM 53-04 FIG 1, 51-10-04, AND 51-10-03. 2 L 7 2 4F A6WE 1999102200522 19991022 00522 WP 1999 10 22 AT9900740 1 19991013 A 3350 1864 LAMP DOUG DC9 DC932 3022066 WP TAILCONE FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 806AT 47379 FOUND TAIL CONE EMERGENCY LIGHT ABOVE SIDE WOULD NOT ILLUMINATE. REMOVED AND REPLACED LAMPS IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 1999102200523 19991022 00523 WP 1999 10 22 CALA9901392 1 19991015 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 200, LBL 6 TO RBL 6. A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51- 30-5. 2 L 7 2 4F A6WE 1999102200524 19991022 00524 WP 1999 10 22 CALA9901393 1 19991015 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 218-237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT FS 218-237, LONGERON 18L TO 19L. THE DENTED SECTION OF SKIN WAS CUT OUT, FI NGER DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 25. 2 L 7 2 4F A6WE 1999102200525 19991022 00525 WP 1999 10 22 CALA9901394 1 19991015 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 468 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 468, LONGERON 24R. REPAIRED IAW SRM 53-04, FIGURE 35 & 64 AND ECRA 5330-02 890. 2 L 7 2 4F A6WE 1999102200526 19991022 00526 WP 1999 10 22 CALA9901395 1 19991015 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 784 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FRAME AND FORMER CORRODED AT FS 784, LONGERON 27R-27L. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-30-5 , AND 53-01, FIGURE 1. 2 L 7 2 4F A6WE 1999102200527 19991022 00527 WP 1999 10 22 CALA9901396 1 19991015 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 784 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 784, LONGERON 27R AND 28R. THE CORRODED AREA OF SKIN WAS REMOVED IAW SRM 53-04, FIGURE 53. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 53 AND 53-02, FIGURE 17. 2 L 7 2 4F A6WE 1999102200528 19991022 00528 WP 1999 10 22 CALA9901397 1 19991015 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 180, LBL 12 TO LBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPP ORT WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999102200529 19991022 00529 WP 1999 10 22 CALA9901398 1 19991015 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 THE STOP PAD SKIN OF MID CARGO DOOR WAS FOUND GOUGED WITH A .5 INCH CRACK IN BOTH LOWER STOP FITTINGS. THE DOOR STOP PA DS WERE REPAIRED IAW SRM 52-03, FIGURE 8 AND ECRA 5230-01485. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-5, 5 1-10-1, AND 51-30-1. 2 L 7 2 4F A6WE 1999102200530 19991022 00530 WP 1999 10 22 CALA9901399 1 19991015 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 446-541 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND UPPER AND LOWER SURFACES OF RT FLOORBOARD TRACK CORRODED AT FS 446-541, RBL 24. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999102200531 19991022 00531 NM 1999 10 22 CALA9901400 1 19991015 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16R AT STA 500C. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, F IGURE 201. 2 L 7 2 4F RT A16WE 1999102200532 19991022 00532 WP 1999 10 22 CALA9901401 1 19991018 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 636-693 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 636-693, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INST ALLED IAW SRM 51-30-02, 51-10-4, AND 51-30-1. 2 L 7 2 4F A6WE 1999102200533 19991022 00533 WP 1999 10 22 CALA9901402 1 19991018 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND THE FORWARD CARGO DOOR STOP PAD SKIN WORN AND GOUGED. THE WORN AND GOUGED AREA WAS REMOVED IAW SRM 52- 03, FIGURE 3. A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND ECRA 5230-01486. 2 L 7 2 4F A6WE 1999102200534 19991022 00534 SO 1999 10 22 COMA9910163 1 19991016 A 5246 FASTENER EMB 120 EMB120RT SO FUEL DOOR LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 264CA 1256 DOOR CAUTION LIGHT ILLUMINATED DURING TAKEOFF FROM CVG. ABORTED TAKEOFF AND RETURNED TO THE GATE. SECURED LOOSE FUEL S ERVICE DOOR FASTENER. 2 L 7 2 4T RT A31SO 1999102200535 19991022 00535 NM 1999 10 22 UPS99230947 1 19991008 A 5751 PANEL BOEING 727 72722C 138400F NM RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C, RT OUTBOARD AILERON LOWER SURFACE ACCESS PANEL T/E EXTRUSION CRACKED. EXTRUSION REPLACED IAW SRM 51- 30-02. 2 L 7 3 4F A3WE 1999102200536 19991022 00536 NM 1999 10 22 UPS99230948 1 19991018 A 3397 WIRE BOEING 727 72725C 138400H NM ROW 1R LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, POS NR 1R FLOOR LIGHT INVERTER WIRE PULLED FROM CONNECTOR. RECONNECTED WIRE. 2 L 7 3 4F A3WE 1999102200537 19991022 00537 NM 1999 10 22 UPS99230949 1 19991019 A 5320 ANGLE BOEING 727 72751C 1384015 NM BS 940-950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:C, RIGHT MLG WHEEL WELL O/B AFT SIDE, HORIZONTAL SHELF 10 BELOW PRESS DECK BETWEEN FS 940 FORGING AND FS 950 FORGING, LOWER O/B ATTACH ANGLE CRACKED. REMOVED DAMAGED AREA AND INSTALLED FITTING AS PER B727-5310-4177A AT RIGH T MLG WHEEL WELL O/B AFT SIDE HORIZONTAL SHELF 10 O/B ATTACH ANGLE AS PER UPS EO B727-5310-4177-A. 2 L 7 3 4F A3WE 1999102200538 19991022 00538 NM 1999 10 22 QXEA9902125 1 19991011 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 SEA- MAIN CABIN DOOR HARD TO OPEN. CLEANED AND LUBED DOOR ROLLERS, TRACKS AND STOPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999102200539 19991022 00539 NM 1999 10 22 QXEA9902126 1 19991014 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 824PH 157 SEA- MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED DOOR STOP/RAMPS, OPERATIONAL CHECKS OK. AIRCRAFT RETURNED TO SERVICE. N O PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999102200540 19991022 00540 WP 1999 10 22 ABXA9900740 1 19991004 A 5313 2777922425000 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 945. REPLACED LONGERON 17 LEFT AT STATION 945 IAW DC9 SRM 51- 30-2. 2 L 7 2 4F A6WE 1999102200541 19991022 00541 WP 1999 10 22 ABXA9900741 1 19991004 A 5320 991050118 WEB DOUG DOUG DC9 DC931 3022065 WP BS 598 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED AT STATION 598. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999102200542 19991022 00542 WP 1999 10 22 ABXA9900742 1 19991004 A 5320 9910073 PRESSURE PANEL DOUG DOUG DC9 DC931 3022065 WP BS 83 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND UPPER PRESSURE PANEL AT STATION 83 CRACKED. REPAIRED IAW ABX REA D953-33358MR. 2 L 7 2 4F A6WE 1999102200543 19991022 00543 WP 1999 10 22 ABXA9900743 1 19991004 A 5330 592032329 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 427 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED AT STATION 427 AND LONGERON 23. REPAIRED IAW DC9 SRM 53-05 AND D953-33534MR . 2 L 7 2 4F A6WE 1999102200544 19991022 00544 WP 1999 10 22 ABXA9900744 1 19991012 A 5313 S27779224 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND LONGERON 17 LEFT AT STATION 1041 CRACKED. REPLACED LONGERON SECTION IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999102200545 19991022 00545 WP 1999 10 22 MWEA99696 1 19991019 A 5753 5910041506 VANE DOUG DC9 DC932 3022066 WP LT TE FLAP DEBONDING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 INBOARD FIXED VANE DEBONDING UNDER OUTBOARD RUB STRIP LEFT WING. MTC FABRICATED AND INSTALLED FILLER AND DOUBLER ON LEF T FIXED VANE RUB STRIP. 2 L 7 2 4F A6WE 1999102200546 19991022 00546 WP 1999 10 22 MWEA99697 1 19991019 A 5740 5910040505 VANE DOUG DC9 DC932 3022066 WP LT TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 LEFT INBOARD FIXED VANE HAS A SMALL DENT APPROX 24 INCHES FROM INBOARD END. MTC FABRICATED AND INSTALLED DOUBLER ON LEF T FIXED VANE. 2 L 7 2 4F A6WE 1999102200547 19991022 00547 WP 1999 10 22 MWEA99698 1 19991019 A 5753 5910040510 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 RIGHT FLAP AFT MOVEABLE VANE HAD DENT ON TOP SURFACE. MTC FABRICATED AND INSTALLED DOUBLER ON RIGHT FLAP MOVEABLE VANE. 2 L 7 2 4F A6WE 1999102200548 19991022 00548 WP 1999 10 22 MWEA99699 1 19991013 A 2620 5244 EXTINGUISHER DOUG DC9 DC932 3022066 WP RT ENGINE FAILURE TEST A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 401ME 47133 RIGHT ENGINE FIRE EXTINGUISHER CARTRIDGE TEST FAILED WHEN NUMBER ONE BOTTLE WAS SELECTED. MAINTENANCE TROUBLESHOT AND F OUND CABLE ACTIVATING SYSTEM OUT OF RIG. ADJUSTED CABLE SYSTEM. 2 L 7 2 4F A6WE 1999102200549 19991022 00549 WP 1999 10 22 MWEA99700 1 19991019 A 5312 591013087 DOUBLER DOUG DC9 DC932 3022066 WP VENTRAL DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 VENTRAL DOOR JAMB LOWER LEFT DOOR CORNER DOUBLER HAS CRACK. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999102200550 19991022 00550 WP 1999 10 22 MWEA99701 1 19991019 A 5313 27779221 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LONGERON 4 RIGHT IS CRACKED AT STATION 756. MAINTENANCE FABRICATED AND INSTALLED LONGERON REPAIR SECTION. 2 L 7 2 4F A6WE 1999102200551 19991022 00551 WP 1999 10 22 MWEA99702 1 19991019 A 5313 27779221 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LONGERON 3 RIGHT AT STATION 756 WAS CRACKED. MAINTENANCE FABRICATED AND INSTALLED LONGERON REPAIR SECTION. 2 L 7 2 4F A6WE 1999102200552 19991022 00552 WP 1999 10 22 MWEA99703 1 19991019 A 5230 1660871 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD UPPER STOP FITTING ON FORWARD CARGO DOOR IS CRACKED. MAINTENANCE INSTALLED NEW STOP FITTING. 2 L 7 2 4F A6WE 1999102200553 19991022 00553 1999 10 22 99ZZZM714 4 19990922 A 3425 622968100 EFD84 BEECH 1900 1900D 1154162 CE INST PANEL FAILED A JJBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 01 833CA 14604 UE24 WHILE EN ROUTE CREW EXPERIENCED SMOKE IN THE COCKPIT. EMERGENCY LANDING WAS DECLARED AND LANDED WITHOUT INCIDENT. IT W AS DETERMINED THAT THE NR 2 EHSI, EFD-84, WAS THE CAUSE OF THE SMOKE. THE EFD-84 WAS REMOVED AND REPLACED WITH A SERVIC EABLE UNIT AND SYSTEM OPERATED SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1999102200554 19991022 00554 WP 1999 10 22 EIA990251 1 19990824 A 3010 3919532505 DUCT DOUG DC9 DC933F 302207A WP LT WING BENT A EIAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 933F 47191 SYR - WITH FLAPS AND SLATS SELECTED UP, CONTROL WHEEL REQUIRED 45 DEGREE RIGHT TURN TO MAINTAIN STRAIGHT AND LEVEL FLIGH T UNTIL LOUD BANGING SOUND, THEN CONTROL WHEEL WOULD BE CENTERED AND NORMAL, REQUIRED 4-5 SECONDS. MAINTENANCE CREWS FO UND LEFT WING AIRFOIL TELESCOPING DUCT BINDING AND HANGING UP. MAINTENANCE REMOVED AND REPLACED LEFT WING AIRFOIL OUTER TELESCOPING DUCT AND ASSOCIATED HARDWARE IAW MM 30-10-07. SYSTEM CHECKS NORMAL WITH NO BINDING OR HANGING UP. (M) 2 L 7 2 4F A6WE 1999102200555 19991022 00555 WP 1999 10 22 EIA990254 1 19990917 A 2750 RETRACT MECH DOUG DC9 DC933F 302207A WP TE FLAPS MALFUNCTIONED A EIAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 933F 47191 BUF - WITH FLAPS AND SLATS SELECTED DOWN, A LOUD THUMP WAS HEARD THEN CONTROL WHEEL REQUIRED 90 DEGREE CONTROL INPUT TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. SPLIT FLAP INDICATION ON GAUGE. (M) 2 L 7 2 4F A6WE 1999102200556 19991022 00556 NM 1999 10 22 BJNA990901 1 19990926 A 2910 69547678 HOSE BOEING 737 737282 13844AT NM LT MLG WW RUPTURED A BJNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 11 344TM 23044 LOSS OF 'A' SYSTEM HYDRAULICS IN FLIGHT. REMOVED AND REPLACED HYDRAULIC LINE IN LEFT WHEEL WELL IAW BOEING MM 20-10-51, LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999102200557 19991022 00557 SO 1999 10 22 ASOA99102 1 19990920 A 2450 2540 RELAY EMB 120 EMB120RT SO APU INOPERATIVE A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 235AS 120047 FLT 4011 - CREW NOTICED SMOKE IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED APU FEEDER PROTECTION RELAY. OPERATIONA L CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102200558 19991022 00558 SO 1999 10 22 ASOA99101 1 19990919 A 5230 SEAL EMB 120 EMB120RT SO CARGO DOOR INOPERATIVE A ASOA B EMER. DESCENT O OTHER CL CLIMB 1 SO 11 246AS 120100 CLIMBING THROUGH 15,000 FT OUT OF DFW ON THE WAY TO AEX, CABIN REPAIDLY LOST PRESSURIZATION. CREW PERFORMED RAPID DEPRE SSURIZATION PROCEDURES AND ADVISED ATC OF THE NEED TO DESCEND TO 10,000. CREW PERFORMED EMERGENCY DESCENT TO 10,000 FT AND RAN POH PROCEDURES. ATTEMPTS TO RETAIN PRESSURIZATION FAILED. FCC ADVISED CONTINUATION TO AEX. AIRCRAFT LANDED WI THOUT FURTHER INCIDENT. MAINTENANCE RESECURED THE CARGO DOOR SEAL. OPERATION CHECKS WERE GOOD. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4T RT A31SO 1999102200559 19991022 00559 SO 1999 10 22 ASOA99100 1 19990917 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 268AS 120202 DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102200560 19991022 00560 NE 1999 10 22 ASOA99083S 2 19990826 A 7260 GEARBOX AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE LT ENGINE FRACTURED A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SO 11 634AS 370 EN ROUTE TO ATL, LEFT ENGINE OIL PRESSURE DROPPED TO 0 PSI. CAPTAIN PERFORMED ENGINE FAILURE IN FLIGHT CHECKLIST, DECLA RED AN EMERGENCY, AND PERFORMED A SAFE SINGLE ENGINE LANDING AT CSG. MCN MAINTENANCE CREW FOUND NR 3/4 BEARING OIL TUBE CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE ASSEMBLY AND OIL COOLER. PROPELLER ACTUATOR WAS ALSO REPLAC ED DUE TO METAL CONTAMINATION. TEARDOWN REPORT SHOWS ACCESSORY GEARBOX DRIVE FRACTURED BELOW THE SPLINES. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999102200561 19991022 00561 NM 1999 10 22 AALA996004 1 19990901 A 2560 D29982107 COVER DOUG MD90 MD9030 3023690 NM DOOR SLIDE LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 904RA 53570 SNA - AFT SERVICE DOOR SLIDE COVER IS LOOSE. SERVICED SLIDE COVER CHECKS OK. (M) 2 L 7 2 4F RT A6WE 1999102200562 19991022 00562 WP 1999 10 22 AALA996001 1 19990825 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP LT EMER EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 871RA 49788 LAX - AFTER DEPARTURE FROM GATE, FA 1 ADVISED THERE ARE 4 WHITE LIGHTS, EMERGENCY ESCAPE, RIGHT SIDE, ROWS 12-16, ILLUMI NATED. NO FLY. RETURN TO GATE. LEFT OVERWING FWD HATCH SIDEWALL EMERGENCY EXIT LIGHT BAD. REPLACED SAME WITH SPARE L IGHT ASSY FROM COCKPIT AND OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1999102200563 19991022 00563 WP 1999 10 22 USAAD99140 1 19990925 A 3350 6003041LB SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927VJ 48154 THE ENTRANCE AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE ENTRANCE AREA EMERGENCY LIGHTS POWER SUPP LY AND BATTERIES. (M) 2 L 7 2 4F A6WE 1999102200564 19991022 00564 WP 1999 10 22 USAAD99134 1 19990915 A 3350 MISC0639 BATTERY DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 967VJ 47375 IND - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999102200565 19991022 00565 NM 1999 10 22 USAA990893 1 19990913 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION TOP ANGLE FORWARD SERV, CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999102200566 19991022 00566 NM 1999 10 22 USAA990889 1 19990913 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 601 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FAST HOLE INNER CHORD ANGLE BS 601 FUSELAGE FRAM E, WL 203 LEFT SIDE. INSTALLED DOUBLER PER EA 65335 AND TR 53-10-23. (M) 2 L 7 2 4F RT A16WE 1999102200567 19991022 00567 NM 1999 10 22 USAA990888 1 19990913 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 328-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STATION 328-344 RBL 10.5 INTERCOSTAL. CORROS ION LEVEL 1. REPAIRED PER SRM 53-10-02. (M) 2 L 7 2 4F RT A16WE 1999102200568 19991022 00568 NM 1999 10 22 USAA990887 1 19990913 A 5330 SKIN BOEING 737 737401 1384701 NM BS 128 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RT HORIZONTAL STABILIZER STAB AFT SPAR STAB STATION 12 8 LOWER SKIN. REPAIRED PER SRM 55-10-01 FIG 206 AND TR 55-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999102200569 19991022 00569 NM 1999 10 22 USAA990886 1 19990913 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 601 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FAST HOLE INNER CHORD ANGLE BS 601, FUSELAGE FRA ME, WL 203 RT SIDE. INSTALLED REPAIR DOUBLER AND HI-LOCKS PER TR 53-10-23, EA 65335 AND SRM 53-60-07. (M) 2 L 7 2 4F RT A16WE 1999102200570 19991022 00570 NM 1999 10 22 USAA990911 1 19990913 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 C.T - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 827L, STRINGER 8/9 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999102200571 19991022 00571 NM 1999 10 22 USAA990912 1 19990913 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLES ON UPPER T-CAP OF FLOORBEAM AT BS 947, LBL 1 4 TO RBL 14, WL 208. CORROSION LEVEL 1. SPLICED NEW UPPER CHORD/DOUBLERS PER SRM 53-00-51 AND TR 53-60-02. (M) 2 L 7 2 4F RT A16WE 1999102200572 19991022 00572 NM 1999 10 22 USAA990921 1 19990913 A 5320 FRAME BOEING 737 737401 1384701 NM SERVICE DOORWAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH CORRODED AREA FORWARD SERVICE DOOR CUTOUT FRAME FWD I NBOARD CHORD AT BOTTOM END JUST ABOVE CREASE BEAM INNER CHORD ANGLE, CORROSION LEVEL 1. REMOVED MINOR CORROSION PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999102200573 19991022 00573 NM 1999 10 22 USAA990922 1 19990913 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 30709 23985 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 440R BETWEEN STRINGER 8 AND 9 FRAME. INSTALLED D OUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999102200574 19991022 00574 NM 1999 10 22 USAA990848 1 19990815 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 49248 22275 TPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 4 INCH CRACK IN SKIN AT STATION 727B PLUS 14 AND STRINGER 18L. REPAIRED PER SRM 53-30-3 FIG 25. (M) 2 L 7 2 4F A16WE 1999102200575 19991022 00575 NM 1999 10 22 USAA990849 1 19990815 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 49248 22275 TPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 1 INCH CRACK IN SKIN AT STATION 727A PLUS 7 AND STRINGER 19L. R EPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999102200576 19991022 00576 NM 1999 10 22 USAA990861 1 19990802 A 5330 SKIN BOEING 737 737296 1384486 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 48634 22398 BOS - DURING RON, FOUND 1.25 INCH CRACK IN SKIN AT STRINGER 16L STATION 767. INSTALLED DOUBLER .080/2024T42 FASTENER 20 426D5 PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F RT A16WE 1999102200577 19991022 00577 NM 1999 10 22 USAA990851 1 19990820 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 45965 22757 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A 3.25 INCH CRACK IN SKIN LONGERON 17R, STATION 727A. INSTALLED DOUBLE R PER SRM 53-30-3 FIG 6 AND EA 65090. (M) 2 L 7 2 4F A16WE 1999102200578 19991022 00578 NM 1999 10 22 USAA990880 1 19990820 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 45965 22757 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK IN SKIN STATION 727B STRINGER 17L. INSTALLED DOUBLER PE R SRM 53-30-3 FIG 1 AND EA 64759. (M) 2 L 7 2 4F A16WE 1999102200579 19991022 00579 NM 1999 10 22 USAA990953 1 19990910 A 5330 SKIN BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 49382 22275 CLT - DURING WALKAROUND CHECK, VISUAL INSPECTION, FOUND A .625 INCH CRACK IN SKIN AT STATION 380 2 INCHES LEFT OF CENTER LINE. INSTALLED REPAIR DOUBLERS PER TR 53-30-04, DRAWING 65C3390. (M) 2 L 7 2 4F A16WE 1999102200580 19991022 00580 NM 1999 10 22 USAA990931 1 19990908 A 5330 SKIN BOEING 737 737201 1384454 NM BS 938 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 45779 22751 TPA - DURING CX-4 CHECK VISUAL INSPECTION VERIFIED WITH EDDY CURRENT, FOUND A 3 INCH CRACK IN SKIN STATION 938, STRINGER 24L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999102200581 19991022 00581 NM 1999 10 22 USAA990947 1 19990901 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 45022 22796 BOS - DURING RON FOUND 1.125 INCH CRACK IN SKIN AT 767, 1.5 INCH ABOVE STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3, PAGE 2E, FIG 1 SHT 4. (M) 2 L 7 2 4F A16WE 1999102200582 19991022 00582 NM 1999 10 22 USAA990946 1 19990901 A 5330 SKIN BOEING 737 737201 1384454 NM BS 770 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 45022 22796 BOS - DURING RON, FOUND 1.5 INCH CRACK IN SKIN AT STATION 770, .5 INCH BELOW STRINGER 18R. INSTALLED DOUBLER PER SRM 53 -30-3, PAGE 2E, FIG 1 SHT 4. (M) 2 L 7 2 4F A16WE 1999102200583 19991022 00583 NM 1999 10 22 USAA990867 1 19990812 A 5751 65464542 AILERON BOEING 737 737296 1384486 NM RT WING MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 48711 22398 PIT - DURING FLIGHT THERE WAS A VIBRATION AND A PASSENGER NOTICED A PORTION OF THE RIGHT AILERON OUTBOARD END TRAILING E DGE COMING OFF OF AIRCRAFT. REPAIRED PER BOEING MANUAL 737-200 NR 27-11-11. (M) 2 L 7 2 4F RT A16WE 1999102200584 19991022 00584 NM 1999 10 22 USAA991009 1 19990909 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 44899 22890 RDU/PIT - DURING UNSCHEDULED MAINTENANCE FROM PILOT REPORT IN RDU, FOUND .625 INCH CRACK IN FUSELAGE SKIN AT STATION 380 BETWEEN STRINGER 28 LEFT/28 RIGHT OF CENTER LINE. INSTALLED EXTERNAL DOUBLER PER TYPICAL REPAIR 53-30-04. (M) 2 L 7 2 4F A16WE 1999102200585 19991022 00585 NM 1999 10 22 USAA990811 1 19990803 A 5510 ANGLE BOEING 737 737301 1384611 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT HORIZONTAL STABILIZER CROSSBEAM ATTACH ANGLE 7 INCH LBL. FABRICATED NEW ANGLE SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999102200586 19991022 00586 WP 1999 10 22 USAA990969 1 19990904 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 58.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 71760 47508 PIT - DURING RON, FOUND 3 VERTICAL CRACKS .5 INCH, .75 INCH, .75 INCH LEFT SIDE STATION 58.750 FORWARD RIVET LINE BETWEE N 2.5 AND 5 INCH BELOW COCKPIT FLOOR LINE. STOP DRILLED CRACKS, INSTALLED EXTERNAL DOUBLER PER SRM 53-01, FIG 2. (M) 2 L 7 2 4F A6WE 1999102200587 19991022 00587 WP 1999 10 22 USAA990968 1 19990902 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 218 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 965VJ 74803 47374 PIT - DURING A/C TURNAROUND, FOUND 4 INCH BY 5.5 INCH CORROSION AREA BETWEEN INTERNAL DOUBLER AND SKIN AT STATION 218 BE TWEEN LONGERONS 21L AND 22L. CUTOUT CORRODED SKIN AREA, INSTALLED FILLER AND DOUBLER CLASS II TEMPORARY PER SRM 53-04 F IG 12B AND TYPE REPAIR 53-04-01A. (M) 2 L 7 2 4F A6WE 1999102200588 19991022 00588 NM 1999 10 22 USAA990991 1 19990914 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 526AU 38611 23861 CLT - DURING A DAILY CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK AT BS 727D PLUS 2 INCH BETWEEN STRINTER 23L AND ST RINGER 24L SKIN FUSELAGE. CUTOUT DAMAGE SKIN AND FABRICATED AND INSTALLED REPAIR DOUBLER PER TR 53-60-03. (M) 2 L 7 2 4F RT A16WE 1999102200589 19991022 00589 WP 1999 10 22 USAA991006 1 19990909 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 58.750 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 824US 43779 49143 PIT - DURING RON, FOUND 2 CRACKS, ONE IS .625 INCH AT 5TH RIVET AND ONE IS .5 INCH AT 4TH RIVET ON SKIN AT STATION 58.75 0, 4TH AND 5TH RIVETS BELOW FLOOR LINE FORWARD SIDE LEFT SIDE. INSTALLED FILLER AND INTERNAL DOUBLER FLUSH REPAIR PER S RM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 1999102200590 19991022 00590 WP 1999 10 22 USAA991007 1 19990902 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 218 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 965VJ 74803 47374 PIT - DURING A/C TURN AROUND, FOUND SEVERAL FASTENER HOLES WITH RADIAL CRACKS .125 INCH, .125 INCH , .375 INCH, .25 INCH , AND .375 INCH ON SKIN AT STATION 218 BETWEEN LONGERONS 21L AND 22L. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLER, CLA SS III TEMP. REPAIR PER SRM 53-04 FIG 12B AND TYPICAL REPAIR 53-04-01A. (M) 2 L 7 2 4F A6WE 1999102200591 19991022 00591 NM 1999 10 22 USAA990827 1 19990807 A 5240 6545871523 SKIN BOEING 737 7372B7 1384560 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 288AU 41388 23135 TPA - DURING CX-2 CHECK EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK LOWER HINGE CUTOUT FORWARD SERVICE DOOR SKIN. R EMOVED CRACK AND INSTALLED DOUBLER PER SB 737-52-1096 AND SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1999102200592 19991022 00592 NM 1999 10 22 USAA990828 1 19990807 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 950.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 288AU 41388 23135 TPA - DURING CX-2 CHECK EDDY CURRENT INSPECTION, FOUND A .2 5INCH CRACK IN SKIN AT UPPER HINGE CUTOUT STATION 950.5 STRI NGER 13R AND 11R. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 78A FIG 21A SHEET 1/2. (M) 2 L 7 2 4F A16WE 1999102200593 19991022 00593 NM 1999 10 22 USAA990850 1 19990815 A 5320 654656311 SHEAR TIE BOEING 737 737201 1384454 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 49248 22275 TPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND CORROSION ATTACH ANGLE SHEAR TIP STRINGER 26L STATION 967 FRAME. CORROSION LEVEL 1. REINSTALLED STRINGER SHEAR TIP PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999102200594 19991022 00594 WP 1999 10 22 USAA991011 1 19990911 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 69 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 48993 48117 PHL/PIT - PHL LINE MTC FOUND 1 INCH CRACK IN FUSELAGE SKIN AT STATION 69 RIGHT SIDE AT STRINGER 21R LEVEL. INSTALLED EX TERNAL DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 1999102200595 19991022 00595 WP 1999 10 22 USAA991010 1 19990911 A 5350 FAIRING DOUG DC9 DC931 3022065 WP BS 714 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 974VJ 81497 47130 CMH/PIT - CMH LINE MAINTENANCE FOUND 10 INCH CRACK AT UPPER RIGHT FUSELAGE TOWING FAIRING STATION 714. INSTALLED EXTERN AL DOUBLER PER EA 52894 AND SRM 53-40-02. (M) 2 L 7 2 4F A6WE 1999102200596 19991022 00596 WP 1999 10 22 USAA991013 1 19990915 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 58.750 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 819US 47814 48099 PIT - DURING THROUGH FLIGHT, FOUND 1.25 INCH CRACK IN SKIN AT STATION 58.750, 4.5 INCH BELOW FLOOR LINE RT SIDE. INSTAL LED FLUSH REPAIR PER SRM 53-01, FIG 4 SHT 2. (M) 2 L 7 2 4F A6WE 1999102200597 19991022 00597 WP 1999 10 22 USAA991012 1 19990824 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 58.750 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919VJ 43576 48139 PIT - DURING RON FOUND 3 CRACKS 2.5 INCH BY 1 INCH LONG AT STATION 58.750 LT, LONGERON 18/19. INSTALLED DOUBLER AND FIL LER PER SRM 53-01 FIG 2 SHEET 3, PAGE 9. (M) 2 L 7 2 4F A6WE 1999102200598 19991022 00598 NM 1999 10 22 USAASB99225 1 19990909 A 2150 123CH1A SENSOR BOEING 737 7374B7 1384702 NM COOLING COMP FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 445US 24863 CLT - FLT 1142 - AT FL360, 180 MILES SOUTH OF CLT, THE EQUIPMENT COOLING LIGHT ILLUMINATED. CREW RESET CIRCUIT BREAKER WITH NO HELP. UPON DESCENDING TO FL310, THE LIGHT BECAME INTERMITTENT AND EVENTUALLY EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE EQUI PMENT COOLING EXHAUST FLOW SENSOR. OPERATIONAL CHECK GOOD PER MM. (M) 2 L 7 2 4F RT A16WE 1999102200599 19991022 00599 1999 10 22 USAASB99209 4 19990824 A 2297 WIRE BOEING 737 737201 1384454 NM AUTOPILOT DAMAGED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 223US 21665 CLT - FLT 8031 - AFTER TAKEOFF FROM CLT, THE AIRCRAFT YAWED LEFT AND RIGHT. AIRCRAFT CONTROL WAS MAINTAINED AND QUICK R EF HANDBOOK PROCEDURES WERE ACCOMPLISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMER GENCY WAS DECLARED. MX FOUND WIRING ASSOCIATED TO THE AUTOPILOT STABILIZER TRIM AT THE AFT PRESSURE BULKHEAD DAMAGED. R EPAIRED WIRE NUMBERS 379-201 AND 379-202 IN THE AFT PRESSURE BULKHEAD AREA (RUDDER LVDT) IN ASSOCIATION WITH STANDARD WI RING PRACTICE MANUAL. ALSO, REMOVED AND REPLACED STABILIZER TRIM MOTOR (P/N AR6460M1) AND AUTOPILOT PITCH COMPUTER (P/N 4050735-901) FOR FAILING (BURNING UP). ACCOMPLISHED OPERATIONAL CHECK OF YAW DAMP SYSTEM. NO FAULTS NOTED. (M) 2 L 7 2 4F A16WE 1999102200600 19991022 00600 WP 1999 10 22 USAAD99132 1 19990914 A 2560 LANYARD DOUG DC9 DC981 3022081 WP 2L DOOR SLIDE LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 48037 ROC - THE 2L DOOR ESCAPE SLIDE AUTO FIRING LANYARD WAS NOT ATTACHED TO THE GIRT BAR. MAINTENANCE ATTACHED THE LANYARD. (M) 2 L 7 2 4F A6WE 1999102200601 19991022 00601 NM 1999 10 22 USAASB99196 1 19990809 A 2934 BACC45FT10A2S CONNECTOR BOEING 737 737201 1384454 NM HYD SYSTEM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 233US 22273 BWI - FLT 2620 - AFTER TAKEOFF, THE STANDBY HYDRAULIC QTY LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGNCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG FOR THE STANDBY HYDRAULIC LOW QUANTITY SWITCH. (M) 2 L 7 2 4F A16WE 1999102200602 19991022 00602 NM 1999 10 22 USAASB99211 1 19990825 A 2910 651782114 MODULE BOEING 737 737201 1384454 NM 'A' HYD SYSTEM FAILED A USAA O OTHER J K WARNING INDICATION FLUID LOSS AP APPROACH 1 EA 19 229US 21818 SDF - FLT 1473 - AIRCRAFT WAS PREPARING TO LAND AT ADF, WHEN THE MASTER CAUTION FLIGHT CONTROL ANNUNCIATOR ILLUMINATED A LONG WITH THE 'A' HYDRAULIC SYSTEM LOW PRESSURE LIGHT. SYSTEM PRESSURE WAS AT 1,200 PSI WHILE QTY REMAINED CONSTANT AT 3.5 GALLONS. THE LANDING GEAR DID NOT WANT TO DEPLOY SO THE CREW USED THE MANUAL GEAR EXTENSION. THE FLIGHT LANDED WIT HOUT INCIDENT AT SDF, BUT HAD TO BE TOWED TO THE GATE DUE TO LOSS OF NOSE WHEEL STEERING. NO EMERGENCY WAS DECLARED. M X TROUBLESHOT THE PROBLEM TO THE 'A' SYSTEM HYDRAULIC MODULE. REPLACED SAME. SERVICED HYDRAULIC SYSTEM. OPERATIONAL C HECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999102200603 19991022 00603 NM 1999 10 22 USAASB99216 1 19990831 A 2730 162300103 COMPUTER BOEING 737 7373B7 1384580 NM ELEVATOR FEEL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 397US 23319 CLT - FLT 8052 - AIRCRAFT WAS FERRYING TO ABE FOR SCHEDULED SERVICE WHEN THE CAPTAIN REPORTED THE ELEVATOR FEEL DIFFEREN TIAL PRESSURE LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED . MAINTENANCE REMOVED AND REPLACED THE ELEVATOR FEEL COMPUTER PER MM 27-31-37. OPERATIONAL TEST GOOD. (M) 2 L 7 2 4F RT A16WE 1999102200604 19991022 00604 NM 1999 10 22 UIEA99072 1 19990831 A 5320 ANGLE BOEING 747 747230B 1384889 NM BS 980 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 509MC 95346 21221 MAIN DECK, CREASEBEAM ATTACHED ANGLE AT BS 980 STRINGER 5L AND 5R FOUND CRACK. THE CRACKED FLANGE WAS TRIMMED OUT AND R EPAIR DOUBLER AND ANGLE WERE INSTALLED IAW BOEING TELEXS. (M) 2 L 7 4 4F A20WE 1999102200605 19991022 00605 NM 1999 10 22 TSAA9933435 1 19990915 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 6 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999102200606 19991022 00606 NM 1999 10 22 TSAA9933436 1 19990915 A 3350 9221009 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED POWER PACK IN AFT ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999102200607 19991022 00607 NM 1999 10 22 99ZZZM715 1 19990917 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING DE DESCENT 1 CE 07 429EX 19100 FLT 714 - IND - NR 3 ENGINE FIRE DETECTOR CIRCUIT GROUND FAULT LIGHT CAME ON DURING DESCENT. REPOSITIONED NR 3 ENGINE F IRE DETECTION LOOP. LIGHT REMAINS OFF. (M) 2 L 7 3 4F A3WE 1999102200608 19991022 00608 NM 1999 10 22 99ZZZM716 1 19990917 A 2611 308 BULB BOEING 727 72751C 1384015 NM SMOKE DETECTOR FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 435EX 19288 FLT 718 - IND - UPPER RIGHT SMOKE DETECTOR BACKGROUND LIGHT INOPERATIVE. REPLACED UPPER RIGHT SMOKE DETECTOR LIGHT BULB . (M) 2 L 7 3 4F A3WE 1999102200609 19991022 00609 WP 1999 10 22 99ZZZM717 1 19990915 A 3350 EMBS1392 BATTERY DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 572SC 46977 FLT 902 - GYR - LEFT NR 1 AND RT NR 1 DOOR HANDLE EXIT LIGHT ILLUMINATED WHEN ATTENDANTS LIGHT SWITCH IS TURNED ON. LIG HT FAILS TO ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS TURNED ON FROM COCKPIT. REPLACED EMERGENCY BATTERY OPERATIONAL CH ECKS NORMAL. (M) 2 L 7 3 4F A22WE 1999102200610 19991022 00610 NM 1999 10 22 99ZZZM718 1 19990922 A 2612 1825280037525 FIRE LOOP BOEING 727 72751C 1384015 NM NR 2 ENGINE GROUNDED A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 436EX 19289 FLT 707 (DEN-IND) NR 2 ENGINE GROUND CIRCUIT DETECTOR LIGHT ILLUMINATES. RE-POSITIONED NR 2 ENGINE FIRE LOOP. (M) 2 L 7 3 4F A3WE 1999102200611 19991022 00611 WP 1999 10 22 99ZZZM719 1 19990828 A 3350 276005 FUSE DOUG DC10 DC1010 3022110 WP CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 572SC 46977 FLT 104 - LAX - ON SERVICE CHECK, FOUND FORWARD CABIN EMERGENCY LIGHTING POWER SUPPLY INOPERATIVE. FOUND BURNED FUSE ON FORWARD CABIN BATTERY PACK CHARGER, REPLACED FUSE. (M) 2 L 7 3 4F A22WE 1999102200612 19991022 00612 EU 1999 10 22 PLGA990901A 1 19990901 A 3230 MS33205 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A PLGA D H RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TO TAKEOFF 1 NE 05 347BE 340B187 BOS - FLT 6386 - AFTER TAKEOFF FROM BOS TO SYR, WHEN THE LANDING GEAR WAS RETRACTED THE HYD LOW PRESS LIGHT CAME ON, HYD PRESSURE DROPPED AND THE HYD PUMP AUTO BREAKER POPPED. HYD OVERRIDE WAS SELECTED AND GEAR WAS EXTENDED. AIRCRAFT LAND ED WITHOUT INCIDENT. BOS MAINTENANCE TROUBLESHOT AND MEL'D THE AUTO MODE. THE CIRCUIT BREAKER FOR AUTO MODE WAS REPLAC ED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 2 4T RT A52EU 1999102200613 19991022 00613 EU 1999 10 22 PLGA990901 1 19990901 A 3297 WIRE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 347BE 340B187 BOS - FLT 6356 - THE FLIGHT CREW COULD NOT PUT THE GEAR HANDLE IN THE UP POSITION. THE CREW DID NOT FOLLOW THE ABNORMAL CHECKLIST TO OVERRIDE THE LATCH SOLENOID. AIRCRAFT RETURNED WITHOUT INCIDENT. THE LANDING GEAR WAS MEL'D AND THE AIRC RAFT REPOSITIONED TO ALB. IN ALB, MAINTENANCE REPAIRED WIRES AT SWITCH 7DG IN THE LEFT WHEEL WELL. SYSTEM WAS OPERATIO NALLY CHECKED GOOD AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999102200614 19991022 00614 EU 1999 10 22 PLGA990910 1 19990910 A 3620 CONNECTOR SAAB SF340 SF340A 7850100 EU BLEED AIR SYSTEM DIRTY A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 742BA 340A092 BOS - FLT 6363 - THE CREW NOTED A BLEED LEAK FAIL LIGHT ON THE CENTRAL WARNING PANEL. AIRCRAFT RETURNED TO BOS WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FERRIED TO BGR. MAINTENANCE IN BGR WAS DISPATCHED AND FOUND CONNECTOR 6WUP1 TO BE DIRTY. AFTER CLEANING THE CONNECTOR IT WAS RESEALED AND SYSTEM OPERATIONAL TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999102200615 19991022 00615 NM 1999 10 22 P2EA99272 1 19990826 A 5755 SKIN BOEING 737 737247 138448D NM NR 6 SPOILER DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - NR 6 SPOILER DAMAGED. REPAIRED IAW COOPESA EO NR COO-CMP-3-57-503-99. (M) 2 L 7 2 4F A16WE 1999102200616 19991022 00616 NM 1999 10 22 P2EA99271 1 19990820 A 5313 STRINGER BOEING 737 737247 138448D NM BS 967 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - AFT CARGO COMPARTMENT, STRINGER 21L CRACKED AT BS 967. REPAIRED STRINGER FROM BS 975 TO BS 959 IAW SRM 53-10-03 F IG 1. (M) 2 L 7 2 4F A16WE 1999102200617 19991022 00617 NM 1999 10 22 P2EA99270 1 19990825 A 5540 LUG BOEING 737 737247 138448D NM RUDDER WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - RUDDER LOWER HINGE LUG WORN. REPAIRED IAW COOPESA EO COO-3-55-507-99. (M) 2 L 7 2 4F A16WE 1999102200618 19991022 00618 NM 1999 10 22 P2EA99269 1 19990826 A 5755 SKIN BOEING 737 737247 138448D NM NR 8 SPOILER DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - RIGHT WING NR 8 SPOILER DAMAGED. REPAIRED NR 8 SPOILER IAW EO COO-CMP-3-57-504-99. (M) 2 L 7 2 4F A16WE 1999102200619 19991022 00619 NM 1999 10 22 P2EA99268 1 19990822 A 5754 ANGLE BOEING 737 737247 138448D NM RT LE SLAT CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - RIGHT WING NR 6 SLAT INTERNAL ANGLE CRACKED. REPLACED ANGLE FROM SLAT STATION 385.36 TO 254.24 BY FABRICATION IAW SRM 51-10-01 PAGE 5 AND 51-30-02. (M) 2 L 7 2 4F A16WE 1999102200620 19991022 00620 NM 1999 10 22 P2EA99267 1 19990913 A 2611 CONTROL PANEL BOEING 737 737222 1384473 NM CABIN FAILED A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 603DJ 19955 FLT 416 - MDW - AIR RETURN, LANDING UNEVENTFUL. AT ABOUT 4000 FT AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED THAT A SM OKE DETECTOR WENT OFF. LIGHT FLASHING AND HORN GOING. DEFERRED PER MEL 26-16, CI M603392 AND M603393 ASSIGNED. REF ME L 26-16, M603392 AND M603393. FOUND SMOKE DETECTOR CONTROL PANEL HAD ELECTRICAL FAULT. ACCOMPLISHED EO 973726A037, DEA CTIVATING HARD-WIRED FORWARD AND AFT LAVATORY SMOKE DETECTOR SYSTEM, AND INSTALLING SELF CONTAINED BATTERY POWERED DETEC TORS, 1 IN EACH LAVATORY. (M) 2 L 7 2 4F A16WE 1999102200621 19991022 00621 NM 1999 10 22 P2EA99266 1 19990913 A 3260 SWITCH BOEING 737 737297 1384480 NM LANDING GEAR OUT OF ADJUST A P2EA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 5WM 22629 MCI - FLT 416 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. WITH THE GEAR UP AND THE FLAPS UP, GEAR WARNING HORN SOUNDS (INTERMITTENTLY) WHEN THE THROTTLES ARE REDUCED TO IDLE. ADJUSTED FLAP TAKEOFF WARNING SWITCH PER MM 31-26-23. OPS CHE CK OK PER MM 31-26-12. (M) 2 L 7 2 4F A16WE 1999102200622 19991022 00622 NM 1999 10 22 P2EA99265 1 19990822 A 5320 WEB BOEING 737 737247 138448D NM BS 1134 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LEFT VERTICAL WEB CRACKED IN APU COMPARTMENT AT BS 1134, LBL 22. REPAIRED IAW SRM 51-40-2 FIG 2. (M) 2 L 7 2 4F A16WE 1999102200623 19991022 00623 NM 1999 10 22 ASAA9910180 1 19990625 A 5320 65516983 SPLICE BOEING 737 737210C 1384459 NM BS 907 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE STRINGER SPLICE AT STATION 907 STRINGER 21L WAS FOUND CORRODED. REPAIRED PER SRM 53 -10-3. (M) 2 L 7 2 4F A16WE 1999102200624 19991022 00624 NM 1999 10 22 ASAA9910181 1 19990625 A 5313 STRINGER BOEING 737 737210C 1384459 NM BS 986.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 21L STATION 986.5 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999102200625 19991022 00625 NM 1999 10 22 ASAA9910182 1 19990625 A 5313 BAC1498156 STRINGER BOEING 737 737210C 1384459 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 22L STATION 947 TO 1016 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-10-1. ( M) 2 L 7 2 4F A16WE 1999102200626 19991022 00626 NM 1999 10 22 ASAA9910183 1 19990625 A 5313 STRINGER BOEING 737 737210C 1384459 NM BS 847-857 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FASTENERS ON THE OUTBOARD SIDE OF STRINGER 24L BETWEEN STATION 847 AND 857 WERE FOUN D TO BE CORRODED. REPAIRED PER SRM 53-10-2. (M) 2 L 7 2 4F A16WE 1999102200627 19991022 00627 NM 1999 10 22 ASAA9910184 1 19990625 A 5313 STRINGER BOEING 737 737210C 1384459 NM BS 857 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE OUTBOARD SIDE OF STRINGER 25R STATION 857 WAS FOUND TO BE CORRODED. REPAIRED PER SR M 53-10-3. (M) 2 L 7 2 4F A16WE 1999102200628 19991022 00628 NM 1999 10 22 ASAA9910185 1 19990625 A 5313 BAC1498156 STRINGER BOEING 737 737210C 1384459 NM BS 960-990 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE INBOARD SIDE OF STRINGER 27L STATION 960 TO 990 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-10-1. (M) 2 L 7 2 4F A16WE 1999102200629 19991022 00629 NM 1999 10 22 ASAA9910186 1 19990625 A 5313 BAC1498156 STRINGER BOEING 737 737210C 1384459 NM BS 1006 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 22L STATION 1006 CRACKED ON INBOARD FLANGE. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999102200630 19991022 00630 NM 1999 10 22 ASAA9910187 1 19990625 A 5313 STRINGER BOEING 737 737210C 1384459 NM BS 500 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 22R STATION 500 WAS FOUND CRACKED. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999102200631 19991022 00631 NM 1999 10 22 ASAA9910188 1 19990625 A 5313 STRINGER BOEING 737 737210C 1384459 NM BS 500 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 24R STATION 500 AND 500B WAS FOUND TO BE DENTED. REPAIRED PER SRM 53-10-3. (M ) 2 L 7 2 4F A16WE 1999102200632 19991022 00632 NM 1999 10 22 ASAA9910189 1 19990625 A 5313 BAC93S7X STRINGER BOEING 737 737210C 1384459 NM BS 986 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 19L STATION 986 DENTED. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999102200633 19991022 00633 NM 1999 10 22 ASAA9910190 1 19990625 A 5311 FRAME BOEING 737 737210C 1384459 NM BS 947 MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, FRAME STATION 947 ABOVE STRINGER 18R HAS THREE ELONGATED HOLES. REPAIRED EPR SRM 53-10- 02. (M) 2 L 7 2 4F A16WE 1999102200634 19991022 00634 NM 1999 10 22 ASAA9910191 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 290-360 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE SKIN AT STATION 290 TO 360 STRINGER 18R WAS FOUND TO BE DAMAGED. REPAIRED PER EA 53 30-01388. (M) 2 L 7 2 4F A16WE 1999102200635 19991022 00635 NM 1999 10 22 ASAA9910192 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 306-360 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, FUSELAGE SKIN BELOW L1 DOOR STATION 306 TO 360 BETWEEN STRINGER 17L AND 18L WAS FOUND TO BE DINGED AND GOUGED. REPAIRED PER EA 5330-01385. (M) 2 L 7 2 4F A16WE 1999102200636 19991022 00636 NM 1999 10 22 ASAA9910193 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 747 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE SKIN AT STATION 747 BETWEEN STRINGER 27L AND 28L WAS FOUND TO BE CRACKED. R EPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102200637 19991022 00637 NM 1999 10 22 ASAA9910194 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 912 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE SKIN STATION 912 STRINGER 27L WAS FOUND TO BE CORRODED. REPAIRED PER SRM 5 3-30-3. (M) 2 L 7 2 4F A16WE 1999102200638 19991022 00638 NM 1999 10 22 ASAA9910195 1 19990625 A 5320 DOUBLER BOEING 737 737210C 1384459 NM BS 948 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK INTERNAL SKIN DOUBLER AT STATION 948 ABOVE STRINGER 23L WAS FOUND TO BE CRACKED AT FASTEN ER HOLE. REPAIRED PER EA 5330-01382. (M) 2 L 7 2 4F A16WE 1999102200639 19991022 00639 NM 1999 10 22 ASAA9910196 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 460 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RIGHT SIDE FUSELAGE WAS FOUND TO BE DENTED ON FRAME AT STATION 460 STRINGER 28L TO 2 6R. REPAIRED PER EA 5330--1386. (M) 2 L 7 2 4F A16WE 1999102200640 19991022 00640 WP 1999 10 22 ASAA9980184 1 19990902 A 5610 PIN DOUG DC9 DC983 3022083 WP LT COCKPIT OUT OF POSITION A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 962AS 53076 SEA - FLT 650 - AFTER ARRIVAL, CREW REPORTED THE FLIGHT COMPARTMENT LT SLIDING WINDOW WOULD NOT OPEN. RESEATED FORWARD UPPER HINGE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999102200641 19991022 00641 WP 1999 10 22 ASAA9980185 1 19990904 A 5610 LATCH DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF POSITION A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 955AS 48080 LAX - FLT 320 - AFTER ARRIVAL, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. RESEATED FORWAR D UPPER LATCH PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999102200642 19991022 00642 WP 1999 10 22 ASAA9980188 1 19990906 A 5210 HOOK DOUG DC9 DC983 3022083 WP L1 DOOR DAMAGED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 982AS 53473 SEA - FLT 94 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE, DOOR RESTING ON JETWAY. STRAIGHTENED LOWE R RT CORNER OF DOOR AND STRAIGHTENED HOLD OPEN HOOK. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999102200643 19991022 00643 WP 1999 10 22 ASAA9980193 1 19990916 A 5240 MECHANISM DOUG DC9 DC983 3022083 WP L2 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 963AS 53077 SEA - FLT 446 - AFTER ARRIVAL, CREW REPORTED THE L2 DOOR WOULD NOT OPEN FROM INSIDE. ADJUSTED THE TORQUE TUBE AND ADJUS TED THE L2 DOOR AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999102200644 19991022 00644 NM 1999 10 22 ASAA9940147 1 19991011 A 5210 SEAL BOEING 737 737490 1384715 NM R1 DOOR OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 799AS 29270 SNA - FLT 413, PRIOR TO FLIGHT, THE R1 DOOR WAS FOUND TO BE BINDING AND WAS DIFFICULT TO CLOSE. CONTRACT MAINTENANCE IN SPECTED AND FOUND THAT THE DOOR SEAL HAD COME OUT OF TRACK. REINSTALLED DOOR SEAL INTO TRACK AND DOOR OPERATED NORMALLY . (M) 2 L 7 2 4F RT A16WE 1999102200645 19991022 00645 NM 1999 10 22 ASAA991037 1 19990626 A 5610 BEARING BOEING 737 7372Q8C 138448S NM RT WINDOW LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 741AS 21959 SEA - FLT 887 - PRIOR TO FLIGHT, CREW REPORTED THAT THE F/O'S SIDE WINDOW WOULD NOT CLOSE. INSPECTED AND FOUND LOWER FO RWARD BEARING LOOSE. REPLACED BEARING AND WINDOW OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999102200646 19991022 00646 NM 1999 10 22 ASAA9910215 1 19990701 A 5260 HANDLE BOEING 737 7372X6C 1384552 NM AIRSTAIR DOOR INOPERATIVE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 746AS 23123 ANC - PRIOR TO FLT 41, THE AFT AIRSTAIR DOOR HANDLE WAS FOUND TO BE INOPERATIVE. INSPECTED AND FOUND THE PUSH PULL CABL E SHEAR RIVET BROKEN. REPLACED SHEAR RIVET AND THE DOOR HANDLE OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999102200647 19991022 00647 NM 1999 10 22 ASAA9910138 1 19990625 A 5320 ANGLE BOEING 737 737210C 1384459 NM BS 270 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FLOORBEAM UPPER SURFACE ATTACH ANGLE BETWEEN LBL 10 AND RBL 10 AT STATION 270 WAS FO UND TO BE CORRODED. REPAIRED PER EA 5320-01098. (M) 2 L 7 2 4F A16WE 1999102200648 19991022 00648 NM 1999 10 22 ASAA9910139 1 19990625 A 5330 654577456 SKIN BOEING 737 737210C 1384459 NM BS 767-907 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE LEFT SIDE OF FUSELAGE STATION 767 TO 907 STRINGER 20L TO 25L WAS FOUND TO HAVE NUMER OUS DENTS AND GOUGES. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999102200649 19991022 00649 NM 1999 10 22 ASAA9910140 1 19990625 A 5330 654577762 SKIN BOEING 737 737210C 1384459 NM BS 907-1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE LEFT SIDE OF FUSELAGE STATION 907 TO 1016 STRINGER 20L TO 25L WAS FOUND TO HAVE NUME ROUS DENTS AND GOUGES. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999102200650 19991022 00650 NM 1999 10 22 ASAA9910141 1 19990625 A 5330 65C36745116 SKIN BOEING 737 737210C 1384459 NM BS 907-1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RT SIDE OF FUSELAGE STATION 907 TO 1016 STRINGER 20R TO 25R WAS FOUND TO HAVE NUMERO US DENTS AND GOUGES. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999102200651 19991022 00651 NM 1999 10 22 ASAA9910142 1 19990625 A 5320 TIE BOEING 737 737210C 1384459 NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE STRINGER TIE ON STRINGER 21L AT STATION 767 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999102200652 19991022 00652 NM 1999 10 22 ASAA9910143 1 19990625 A 5311 654656437 FRAME BOEING 737 737210C 1384459 NM BS 986.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE LOWER LOBE AREA ON THE 986.5 FRAME WEB BETWEEN STRINGER 18L AND 21L WAS FOU ND TO BE CORRODED. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999102200653 19991022 00653 NM 1999 10 22 ASAA9910144 1 19990625 A 5313 65516985 STRINGER BOEING 737 737210C 1384459 NM BS 907 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 20L AT STATION 907 WAS FOUND TO BE BROKEN. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999102200654 19991022 00654 NM 1999 10 22 ASAA991045 1 19990625 A 5320 6546822 BEAM BOEING 737 737210C 1384459 NM BS 727-747 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE CREASE BEAM WEB BETWEEN STATION 727B AND 747 RT WAS FOUND CRACKED AND CORRODED. REP AIRED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999102200655 19991022 00655 NM 1999 10 22 ASAA9910146 1 19990625 A 5315 6546812185 FLOORBEAM BOEING 737 737210C 1384459 NM BS 520 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FLOORBEAM TOP SURFACE AT STATION 520 RBL 0 TO RBL 58.25 AND LBL 26 WAS FOUND TO BE C ORRODED. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999102200656 19991022 00656 NM 1999 10 22 ASAA9910147 1 19990625 A 5315 6554907 FLOORBEAM BOEING 737 737210C 1384459 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE CABIN FLOORBEAM TOP SURFACE AT STATION 727B LBL 18 WAS FOUND TO BE CORRODED. REPAIR ED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999102200657 19991022 00657 NM 1999 10 22 ASAA9910148 1 19990625 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM BS 986 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FLOORBEAM AFT UPPER FLANGE STATION 986 LBL 35 WAS FOUND TO BE GOUGED AND CORRODED. R EPAIRED PER SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1999102200658 19991022 00658 NM 1999 10 22 ASAA9910149 1 19990625 A 5320 656714024 BEAM BOEING 737 737210C 1384459 NM BS 520 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE TRANSVERSE BEAM LOWER INBOARD SIDE STATION 520 LBL 24.5 WAS FOUND TO BE CORRODED. R EPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999102200659 19991022 00659 NM 1999 10 22 ASAA9910150 1 19990625 A 5320 6545855 BEAM BOEING 737 737210C 1384459 NM BS 927-986.5 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE R2 AFT SERVICE DOOR TRANSVERSE BEAM FROM STATION 927 TO 986.5 WAS FOUND CORRODED. R EPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999102200660 19991022 00660 NM 1999 10 22 ASAA9910151 1 19990625 A 5311 6953095 FRAME BOEING 737 737210C 1384459 NM BS 980 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE STUB FRAME AT STATION 980 STRINGER 19L TO 21L WAS FOUND CORRODED. REPAIRED PER SRM 51-30-3. (M) 2 L 7 2 4F A16WE 1999102200661 19991022 00661 NM 1999 10 22 ASAA9910152 1 19990625 A 5312 BULKHEAD WEB BOEING 737 737210C 1384459 NM BS 182 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE WEB ON THE AFT SIDE OF BULKHEAD STATION 182 RBL 20 WAS FOUND CRACKED. REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1999102200662 19991022 00662 NM 1999 10 22 ASAA9910153 1 19990625 A 5311 FRAME BOEING 737 737210C 1384459 NM BS 460 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FRAME AT STATION 460 BETWEEN STRINGERS 20L AND 21L IS CRACKED. REPAIRED PER SRM 51- 40-3. (M) 2 L 7 2 4F A16WE 1999102200663 19991022 00663 NM 1999 10 22 ASAA9910154 1 19990625 A 5311 FRAME BOEING 737 737210C 1384459 NM BS 480 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FRAME AT STATION 480 BETWEEN STRINGERS 21L AND 22 WAS FOUND TO BE CRACKED. REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1999102200664 19991022 00664 NM 1999 10 22 ASAA9910155 1 19990625 A 5320 656210030 SILL BOEING 737 737210C 1384459 NM L1 DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE L1 DOOR SILL TRANSVERSE CHORD STATION 270 TO 360 LBL 60 WAS FOUND CORRODED. REPAIRE D PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1999102200665 19991022 00665 NM 1999 10 22 ASAA9910156 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 277 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE SKIN STATION 277 STRINGER 17L WAS FOUND DENTED. REPAIRED PER SRM 53-00-01. (M) 2 L 7 2 4F A16WE 1999102200666 19991022 00666 NM 1999 10 22 ASAA9910157 1 19990625 A 5320 6547957503 ANGLE BOEING 737 737210C 1384459 NM BS 857 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, CORROSION WAS FOUND ON THE ANGLE (CHORD) STATION 857 BETWEEN STRINGER 25R AND 26R CORROD ED. REPAIRED PER EA 5310-01704. (M) 2 L 7 2 4F A16WE 1999102200667 19991022 00667 NM 1999 10 22 ASAA9910158 1 19990625 A 5320 6567140 CHORD BOEING 737 737210C 1384459 NM BS 520-727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, CORROSION WAS FOUND ON A PREVIOUSLY REPAIRED CHORD STATION 520 TO 727 RBL 45.5 AND LBL 4 5.5. REPAIRED PER EA 5310-01706. (M) 2 L 7 2 4F A16WE 1999102200668 19991022 00668 NM 1999 10 22 ASAA9910159 1 19990625 A 5315 65549021 FLOORBEAM BOEING 737 737210C 1384459 NM BS 967 MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, A DOUBLE DRILLED HOLE WAS FOUND IN THE FLOORBEAM STATION 967 WHERE IT ATTACHES TO THE 17 R CUSP ANGLE. REPAIRED PER EA 5310-01708. (M) 2 L 7 2 4F A16WE 1999102200669 19991022 00669 NM 1999 10 22 ASAA9910160 1 19990625 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM BS 460 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FLOORBEAM LOWER FORWARD SIDE STATION 460 BETWEEN LBL 30 AND LBL 50 WAS FOUND CORRODE D. REPAIRED PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1999102200670 19991022 00670 NM 1999 10 22 ASAA9910161 1 19990625 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM BS 294 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE MAIN CABIN FLOORBEAM UPPER SURFACE STATION 294 LBL 14 TO RBL 14 WAS FOUND CORRODED. REPAIRED PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1999102200671 19991022 00671 NM 1999 10 22 ASAA9910162 1 19990625 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM BS 1006 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE MAIN CABIN FLOORBEAM TOP FLANGE STATION 1006 BL 0 TO LBL 20 WAS FOUND CORRODED. REP AIRED PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1999102200672 19991022 00672 NM 1999 10 22 ASAA9910163 1 19990625 A 5315 BAC1505100186 FLOORBEAM BOEING 737 737210C 1384459 NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE MAIN CABIN FLOORBEAM UPPER SURFACE STATION 312 LBL 14 TO RBL 14 WAS FOUND CORRODED. REPAIRED PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1999102200673 19991022 00673 NM 1999 10 22 MZZA99183 1 19990905 A 2710 CONTROL CABLE BOEING 727 727224 1384076 NM AILERON BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A BROKEN AILERON BUS CABLE WAS FOUND AROUND PULLEY, JUST FORWAR D OF LEFT MLG WALKING BEAM. THE DAMAGED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 27-10-71, 27-10-00 AND OPERA TIONAL CHECK FOUND SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999102200674 19991022 00674 NM 1999 10 22 MZZA99182 1 19990905 A 2760 CONTROL CABLE BOEING 727 727224 1384076 NM LT SPOILER CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 4 RUSTED SPOILER CABLES WERE FOUND ON LT WING TE CAVITY FORWARD OF APU FIRE EXTINGUISHER BOTTLE. THE DAMAGED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAP 27-61-41, 27-61-00 AND OP ERATIONAL CHECK. FOUND SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999102200675 19991022 00675 NM 1999 10 22 MZZA99181 1 19990905 A 2710 CONTROL CABLE BOEING 727 727224 1384076 NM LT AILERON RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RUSTED AILERON CABLE WAS FOUND ON LEFT WING TE CAVITY, FORWAR D OF APU OF FIRE EXTINGUISHER BOTTLE. THE DAMAGED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 27-10-71, 27-10-00 AND OPERATIONALLY CHECK. FOUND SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999102200676 19991022 00676 NM 1999 10 22 MZZA99180 1 19990908 A 5330 2024T3 SKIN BOEING 727 727224 1384076 NM BS 1044 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A BULGE WAS FOUND ON BS 1044 FUSELAGE BELLY SKIN AT S-30. THE DAMAGED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 4. (M) 2 L 7 3 4F A3WE 1999102200677 19991022 00677 NM 1999 10 22 MZZA99179 1 19990904 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1218 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 5330 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .25 INCH LONG CRACK WAS FOUND ON BS 1218 FUSELAGE SKIN. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 53-30-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999102200678 19991022 00678 NM 1999 10 22 MZZA99178 1 19990910 A 5330 SKIN BOEING 727 727224 1384076 NM BS 510 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 12 INCH BY 13 INCH SKIN AREA BULGE WAS FOUND ON BS 510 AND BL 0. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER SRM CHAPTER 53-30-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999102200679 19991022 00679 NM 1999 10 22 MZZA99177 1 19990907 A 5314 KEEL BEAM BOEING 727 727224 1384076 NM BS 950 CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA CORROSION WAS FOUND ON RT KEEL BEAM STRING ER S-29 VERTICAL O/B FLANGE EXTENDING INTO THE RADIUS AT BS 950 PLUS 11. THE CORRODED AREA WAS BLENDED OUT AND REPAIRED PER CONTINENT ECRA NR 5310-01425. (M) 2 L 7 3 4F A3WE 1999102200680 19991022 00680 NM 1999 10 22 MZZA99176 1 19990908 A 5312 BULKHEAD TEE BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY 1 INCH AREA CORROSION WAS FOUNDON BS 950 BULKHEAD L OWER TEE CHORD ADJACENT OT KEEL BEAM STRINGER S-29R. THE CORRODED AREA WAS BLENDED OUT AND REPAIRED PER CONTINENT ECRA NR 5310-3923. (M) 2 L 7 3 4F A3WE 1999102200681 19991022 00681 NM 1999 10 22 MZZA99175 1 19990906 A 5320 WEB BOEING 727 727224 1384076 NM BS 1213 CRACK A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON RT LOWER TORQUE BOX VERTICAL WEB AT BS 1213. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 1. (M) 2 L 7 3 4F A3WE 1999102200682 19991022 00682 NM 1999 10 22 AALA991281 1 19990824 A 5330 SKIN BOEING 727 727227 1384078 NM BS 205 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND CRACK IN FUSELAGE SKIN BELOW CAPTAINS WINDOW C-D POST (FORWARD OF NR 2 WINDOW). INSTALLED REPAIR DOUBLR ON FUSE SKIN BELOW CAPTAINS C-D WINDOW POST (FWD OF NR 2 WINDOW). INSTALLED REPAIR DOUBLER ON FUSE SKIN BELOW CAPTAINS C-D WINDOW POST PER SRM 53-30-3, PAGE 40 FIGURE 8, SHT 11. (M) 2 L 7 3 4F A3WE 1999102200683 19991022 00683 NM 1999 10 22 AALA991282 1 19990825 A 5510 CHORD BOEING 727 727227 1384078 NM RT HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - RIGHT HORIZONTAL STABILIZER HAS AREA OF CORROSION ON T/E UPPER CHORD JUST INBOARD OF NR 2 ELEV HINGE AT EXISTING R EPAIR, OUTBOARD OF STATION 190. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER ESO 11697, DATED 8-23-99 USIN G SRM 55-10-6 INSTALLATION. (M) 2 L 7 3 4F A3WE 1999102200684 19991022 00684 NM 1999 10 22 AALA991283 1 19990824 A 5730 SKIN BOEING 727 727227 1384078 NM WS 655 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - UPPER L/E SPAR CAP COVER STRIP AND SEALANT BULGED UP AT NR 2 SLAT. CUT OUT SECTION OF L/E SKIN TO GAIN ACCESS TO SPAR CAP. REMOVED SURFACE CORROSION FROM SPAR CAP. TREATED, PAINTED AND INSTALLED A DOUBLER REPAIR TO L/E SKIN AS PER SRM 57-30-4. (M) 2 L 7 3 4F A3WE 1999102200685 19991022 00685 NM 1999 10 22 AALA991284 1 19990825 A 5320 TORQUE BOX BOEING 727 727227 1384078 NM BS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - RIGHT GALLEY DOOR UPPER HINGE TORQUE BOX AT FUSE CRACKED. INSTALLED REPAIR STRAP TO UPPER HINGE TORQUE BOX PER ES O 11697, DATED 8-24-99. (M) 2 L 7 3 4F A3WE 1999102200686 19991022 00686 NM 1999 10 22 F3LA99119 1 19990904 A 3222 65462153 AXLE BOEING 737 737201 1384454 NM NLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 DEN - DURING C-4 CHECK, INSPECTION REPORTED DAMAGE FROM CORROSION PITTING ON NOSE LANDING GEAR RT AXLE. REPLACED INNER CYLINDER ASSY PER BOEING MM 32-21-11. (M) 2 L 7 2 4F A16WE 1999102200687 19991022 00687 NM 1999 10 22 F3LA99121 1 19990917 A 3260 INDICATION BOEING 737 737317 138447P NM LANDING GEAR MALFUNCTIONED A F3LA O OTHER N FALSE WARNING AP APPROACH 1 NM 03 EICHH 23177 DFW - FLT 124 - FLIGHT CREW REPORTED NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE UPON APPROACH, RED LIGHT REMAINED ILLUMINA TED. RECYCLED GEAR AND ALL THREE GREEN LIGHTS ILLUMINATED. MAINTENANCE INSPECTED NOSE LANDING GEAR PER MM 32-00 AND CO NTROL LEVER LOCK SYSTEM PER MM 32-31. CYCLED GEAR SEVERAL TIMES AND ALL INDICATIONS WERE NORMAL. (M) 2 L 7 2 4F RT A16WE 1999102200688 19991022 00688 WP 1999 10 22 ARWA990904 1 19990914 A 2750 CONTROL VLV DOUG DC8 DC863F 302198F WP TE FLAPS FAILED A ARWA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 19 441J 45988 SJO - FLT 521 - WITH FLAPS SELECTED TO 23 DEGREES, LEFT FLAP INDICATED 23 DEGREES, RIGHT FLAP INDICATED 28 DEGREES. A/C ROLLED TO THE LEFT. WITH FLAPS SELECTED TO 35 DEGREES, LEFT FLAP INDICATED 35 DEGREES, RT FLAP INDICATED 42 DEGREES. A /C ROLLED RATE INCREASED TO THE LEFT, ON GROUND FLAPS INDICATED NORMAL IN ALL POSITIONS. REMOVED AND REPLACED FLAP CONT ROL VALVE AND RIGGED IAW DACO MM. OPS CHECK OK. (M) 2 L 7 4 4F 4A25 1999102200689 19991022 00689 NM 1999 10 22 USAA089907 1 19990823 A 3350 110049 CHARGER BOEING 727 727225 1384077 NM L1/R1 DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS 20447 FLT 6150 - LGA-BOS, FOUND ON L/S, EPL EXIT LIGHT AT L1 AND R1 INOPERATIVE. REPLACED FORWARD BATTERY CHARGER, CHECK OK P ER MM 33-50-01. (M) 2 L 7 3 4F A3WE 1999102200690 19991022 00690 NM 1999 10 22 USAA089901 1 19990811 A 3350 20362 CHARGER BOEING 727 727227 1384078 NM RT EXTERIOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924TS 21041 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED CHARGER AND BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999102200691 19991022 00691 WP 1999 10 22 USAA990860 1 19990901 A 5320 SUBFLOOR DOUG DC9 DC981 3022081 WP BS 155 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 48741 48026 PIT - DURING Q1/C4 CHECK, FOUND EXTENSIVE CORROSION OF SUB FLOOR AT STATION 155 AREA BY EPC. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 1999102200692 19991022 00692 WP 1999 10 22 USAA990944 1 19990829 A 5730 SKIN DOUG DC9 DC981 3022081 WP WS 214 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808US 49028 48040 PIT - DURING RON, FOUND 6 INCH CRACK AT LEFT WING, STATION XRS-214, OUTBOARD OF NR 7 SLAT TRACK AT L/E SKIN. INSTALLED DOUBLER PER SRM 57-068 FIG 4. (M) 2 L 7 2 4F A6WE 1999102200693 19991022 00693 WP 1999 10 22 USAA990941 1 19990901 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 76.55 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 960VJ 71902 47505 PIT - DURING C-5 CHECK, FOUND FOUR .125 INCH CRACKS COMING FROM RIVET IN SKIN PANEL AT STATION 76.55 BETWEEN LEFT LOGNER ONS 2 AND 3. REPAIR ACCOMPLISHED PER SERVICE REWORK DRAWING SR 09530239-7021 THROUGH 7027. (M) 2 L 7 2 4F A6WE 1999102200694 19991022 00694 WP 1999 10 22 USAA990942 1 19990901 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 76 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 960VJ 71902 47505 PIT - DURING C-5 CHECK FOUND TWO .125 INCH CRACKS AT LONG 2 AND 3 STATION 76. INSTALLED FILLER AND DOUBLER PER SR095302 39. (M) 2 L 7 2 4F A6WE 1999102200695 19991022 00695 WP 1999 10 22 USAA990943 1 19990830 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 58.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 935VJ 49155 48115 PHL - DURING RON, FOUND .75 INCH VERTICAL CRACK IN SKIN AT STATION 58.750 IN RIVET LINE 6 INCH BELOW FLOOR LEVEL RT SIDE NOSE. INSTALLED DOUBLER PER SRM 53-01 FIG 2, PAGE 9. (M) 2 L 7 2 4F A6WE 1999102200696 19991022 00696 WP 1999 10 22 USAA990945 1 19990901 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 76.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 978VJ 77743 47371 PIT - DURING C-4 CHECK, FOUND .125 INCH CRACK AT RIVET HOLES AT TOP FUSELAGE SKIN FS 76.5 FORWARD OF CAPTAINS FO'S PITOT TUBES. REPAIRED PER SRO 9530239-7021 AND 7023. (M) 2 L 7 2 4F A6WE 1999102200697 19991022 00697 WP 1999 10 22 USAAD99125 1 19990902 A 2150 3916537 SEAL DOUG DC9 DC981 3022081 WP ACM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 811US 48043 MKE-CLT - FLT 751 - AFTER TAKEOFF AND CLIMBING THROUGH 17,000 FT THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT DIVERT ED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AIR CYCLE MACHINE AND PERI-SEALS. (M) 2 L 7 2 4F A6WE 1999102200698 19991022 00698 WP 1999 10 22 USAAD99124 1 19990902 A 2120 AIR DIST DOUG DC9 DC931 3022065 WP CABIN ODOR A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 976VJ 48147 BOS-DCA - FLT 2423 - DURING FLIGHT, THE FLIGHT ATTENDANTS COMPLAINED OF A FUEL ODOR IN THE CABIN. FLIGHT WAS COMPLETED AND LANDED AT DCA WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT AND LEFT AIR CONDITIONING PACK SYSTEMS. NO FAULTS NOTED. RAN APU AND BOTH ENGINES. NO FUEL SMELL NOTED IN CABIN WITH BOTH PACKS ON. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 1999102200699 19991022 00699 EU 1999 10 22 USAAF99042 1 19990828 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 859US 11293 RDU - FOUND FORWARD FLOOR PROXIMITY LIGHTS AND NR 1 AISLE CEILING LIGHT INOPERATIVE DURING EMERGENCY LIGHT TEST. MAINTE NANCE REPLACED THE BATTERY PACK AND SUPPLY UNIT. (M) 2 L 7 2 4F RT 1999102200700 19991022 00700 EU 1999 10 22 USAAF99043 1 19990828 A 3350 6104789 BATTERY PACKS FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 858US 11291 IND - FOUND LEFT EXIT, MID CEILING AND LEFT EXTERIOR LIGHTS INOPERATIVE. MAINTENANCE REPLACED TWO BATTERY PACKS. (M) 2 L 7 2 4F RT 1999102200701 19991022 00701 EU 1999 10 22 USAAF99041 1 19990823 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 886US 11346 CLT - FOUND THE NR 8 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1999102200702 19991022 00702 EU 1999 10 22 USAAF99040 1 19990804 A 3350 ES415142B RELAY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST AP APPROACH 1 EA 19 861US 11297 CLT - FLT 1160 - THE EMERGENCY EXIT ADVISORY LIGHTS DID NOT ILLUMINATED WHEN THE GEAR WAS LOWERED. MAINTENANCE REPLACED THE K2618A RELAY. (M) 2 L 7 2 4F RT 1999102200703 19991022 00703 WP 1999 10 22 USAAD99128 1 19990906 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 935VJ 48115 CMH - THE FORWARD ENTRY AND COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD ENTRY AND COCKP IT EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999102200704 19991022 00704 WP 1999 10 22 USAAD99126 1 19990903 A 3260 92743643 RELAY DOUG DC9 DC931 3022065 WP LANDING GEAR FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 974VJ 47130 CLT-ATL - FLT 2264 - AFTER TAKEOFF AND LANDING GEAR RETRACTION, ALL THREE GEAR LIGHTS REMAINED RED. MAINTENANCE REPLACE D THE R2-29 RELAY. (M) 2 L 7 2 4F A6WE 1999102200705 19991022 00705 WP 1999 10 22 USAAD99127 1 19990905 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 935VJ 48115 IND - THE FORWARD OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT POWR SUPPLY. (M) 2 L 7 2 4F A6WE 1999102200706 19991022 00706 WP 1999 10 22 USAAD99108 1 19990806 A 3350 60030451LB SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 936VJ 48116 THE CEILING EMERGENCY LIGHTS FOR ROWS 1-3 ILLUMINATE WHEN ALL POWER IS TURNED OFF. MAINTENANCE REPLACED THE FORWARD CAB IN EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999102200707 19991022 00707 WP 1999 10 22 USAAD99109 1 19990806 A 3350 408822101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 922VJ 48142 THE CEILING EMERGENCY LIGHTS FOR ROWS 10-13 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE ROW 10-13 CEIL ING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999102200708 19991022 00708 WP 1999 10 22 USAAD99123 1 19990909 A 3350 408822101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913VJ 45846 IND - THE FORWARD PASSENGER CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD PASSENGE R CABIN OVERHEAD EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999102200709 19991022 00709 WP 1999 10 22 USAAD99121 1 19990829 A 3350 408822101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 811US 48043 PIT - THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD CABIN EMERGENCY LIGHTS BATT ERIES. (M) 2 L 7 2 4F A6WE 1999102200710 19991022 00710 WP 1999 10 22 USAAD99120 1 19990826 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816US 48096 LGA - THE AFT LOW LEVEL EMERGNCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT LOWER LEVEL EMERGENCY LIGHT BATT ERIES. (M) 2 L 7 2 4F A6WE 1999102200711 19991022 00711 WP 1999 10 22 USAAD99122 1 19990831 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 PIT - SEVERAL LOW LEVEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999102200712 19991022 00712 NM 1999 10 22 USAABB99041 1 19990831 A 2150 6259283 TEMP SWITCH BOEING 757 7572B7 1384964 NM LT PACK FAILED A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 616AU 27147 FLT 615 - EN ROUTE CLT-LAS, AT FL240, CREW RECEIVED ALTITUDE WARNING FOR LEFT PACK. RIGHT PACK WAS ALREADY ON MEL. CRE W PERFORMED EMERGENCY DESCENT. FLT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MX CLEARED THE MEL ON THE RT P ACK BY REPLACING IT AND RELEASED THE A/C WITH AN MEL ON LEFT PACK. ON 9/2/99, FLT 96, THE CREW RECEIVED THE E/M'S 'CABI N ALT' AND LIGHTS DISPLAYED. CREW COULD NOT MAINTAIN PRESSURIZATION USING MANUAL MODE, AND AGAIN DESCENDED. FLIGHT DIV ERTED TO LAS. AIRCRAFT WAS THEN MAINTENANCE FERRIED TO LAX. MAINTENANCE IN LAX REPLACED THE TS41 COMPRESSOR OUTLET TEM PERATURE SWITCH. (M) 2 L 7 2 4F RT A2NM 1999102200713 19991022 00713 NM 1999 10 22 USAASB99218 1 19990902 A 3350 20121 POWER SUPPLY BOEING 737 7373B7 1384580 NM ROW 2/10/12 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 521AU 23856 DCA - DURING WEEKLY CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS LOCATED AT SEAT ROWS 2L, 10R AND 12L INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED M1136 POWER SUPPLY AT STATION 753 PER MM 33-51-00. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999102200714 19991022 00714 NM 1999 10 22 USAASB99217 1 19990808 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 276AU 22888 CLT - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT IN THE COCKPIT REMAINS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AS PER THE MM. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999102200715 19991022 00715 NM 1999 10 22 P2EA99245 1 19990824 A 5755 SUPPORT BOEING 737 737247 138448D NM NR 4 SPOILER CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LEFT WING SPOILER NR 4 SUPPORT LUG CRACKED. REPAIRED IAW EO COO-SJO-99-00186H, DATED 8/30/99. (M) 2 L 7 2 4F A16WE 1999102200716 19991022 00716 NM 1999 10 22 P2EA99243 1 19990822 A 5311 FRAME BOEING 737 737247 138448D NM BS 1156 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SECTION 48 APU COMPARTMENT AT BS 1156 RBL 14 HAS CRACKED FRAME. REPAIRED FRAME AT BS 1156 BETWEEN RBL 15.25 AND R BL 12.750 IAW SRM 51-40-2 FIG 1. (M) 2 L 7 2 4F A16WE 1999102200717 19991022 00717 NM 1999 10 22 P2EA99242 1 19990822 A 5313 STRINGER BOEING 737 737247 138448D NM BS 500 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FORWARD CARGO COMPARTMENT AT BS 500A STRINGER 26R HAS CORROSION. REPAIRED STRINGER 26R BETWEEN BS 500A AND BS 514 IAW SRM 53-10-3 FIG 3. (M) 2 L 7 2 4F A16WE 1999102200718 19991022 00718 NM 1999 10 22 P2EA99240 1 19990822 A 5330 SKIN BOEING 737 737247 138448D NM BS 188-196.5 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FUSELAGE FROM BS 188 TO BS 196.5 AT LAP JOINT, SKIN DENTED, STRINGER 20L. DEFECT SIZE, DEPTH .220. REPAIRED PER S RM 53-30-3 FIG 3. (M) 2 L 7 2 4F A16WE 1999102200719 19991022 00719 NM 1999 10 22 P2EA99238 1 19990821 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 1025 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - AFT PRESSURE BULKHEAD WEB DENTED AT BS 1025, WL 196, RBL 8 INCHES. DEFECT SIZE, DEPTH .300 INCH. PRESSURE BULKHE AD SECTION BS 1025, WL 198.1, WL 198, RBL 7 INCH TO 11.20 REPAIRED PER SRM 53-10-4 FIG 3. (M) 2 L 7 2 4F A16WE 1999102200720 19991022 00720 NM 1999 10 22 P2EA99237 1 19990824 A 5313 STRINGER BOEING 737 737247 138448D NM BS 294.5 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - STRINGER 11 LEFT CRACKED AT BS 294.5, DEFECT SIZE, LENGTH .500 INCH. REPAIRED STRINGER 11 LEFT BETWEEN BS 293.5 A ND STRINGER 299.5 PER SRM 53-10-3, FIG 2. (M) 2 L 7 2 4F A16WE 1999102200721 19991022 00721 NM 1999 10 22 P2EA99236 1 19990906 A 3260 655281162 MODULE BOEING 737 7372Q8 138448K NM LANDING GEAR UNSERVICEABLE A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 121NJ 21735 MSP - FLT 703 - NO EMERGENCY DECLARED, LANDING NORMAL. LANDING GEAR UNSAFE LIGHTS, 3 RED, REMAINED ON AFTER TAKEOFF. A IRCRAFT WAS INSPECTED THEN REPOSITIONED TO MCI ON SPECIAL FLIGHT PERMIT. REPLACED LANDIGN GEAR MODUEL, OPS CHECK NORMAL PER MM 32-09-100. (M) 2 L 7 2 4F RT A16WE 1999102200722 19991022 00722 SO 1999 10 22 GLBA99051 1 19990908 A 2150 HEAT EXCHANGER EMB 120 EMB120ER 3260203 SO LT PACK DIRTY A GLBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 01 71GL 120071 SMELL OF SMOKE IN COCKPIT WHILE TAXIING ALSO LEFT PACK FAILED. FOUND CONTAMINATION IN HEAT EXCHANGER. CLEANED HEAT EXC HANGER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1999102200723 19991022 00723 SO 1999 10 22 GLBA99057 1 19990817 A 2910 SEAL EMB 120 EMB120RT SO HYD TUBE LEAKING A GLBA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 01 281UE 120092 UNCOMMANDED YAW TO THE LEFT ON TAKEOFF. REPLACED TRANSFER TUBE SEALS AND RESEATED TUBE. (M) 2 L 7 2 4T RT A31SO 1999102200724 19991022 00724 NM 1999 10 22 AALA991300 1 19990828 A 2612 285N002836 FIRE CARD BOEING 767 767223 1385123 NM E/E COMP DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 306AA 22312 LAS - FLT 160 - EN ROUTE SAN-JFK, EICAS MESSAGE NOTED FOR FIRE/OVERHEAT SYSTEM. FIRE/OVERHEAT SYSTEM FAIL LIGHT ILLUMIN ATED ON CONSOLE. AIRCRAFT DIVERTED AND LANDED LAS WITHOUT INCIDENT. REPLACED ENGINE FIRE/OVERHEAT DETECTION CARD AT TH E NR 1 POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102200725 19991022 00725 EU 1999 10 22 AALA991102 1 19990728 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 91050 423 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT CABIN INOPERATIVE. RESECURED CONNECTOR TO AFT CABIN EM ERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200726 19991022 00726 EU 1999 10 22 AALA991063 1 19990720 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROW 9B INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70054 461 JFK - DURING OVERNIGHT MAINTENANCE, EMEREGNCY EXIT FLOOR PATH LIGHT STRIP BY SEAT 9B INOPERATIVE. REPLACED EMERGENCY EX IT FLOOR PATH LIGHT STRIP FROM SEAT 12B FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200727 19991022 00727 EU 1999 10 22 AALA991088 1 19990724 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 23-25 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80058 466 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 23 TO 25 INOPERATIVE. RESEATED EMERGE NCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200728 19991022 00728 EU 1999 10 22 AALA991162 1 19990812 A 3350 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU ROW 12H-14H DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 40064 507 JFK - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN SEATS 12H AND 14H INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHTING BETWEEN SEATS 12H AND 14H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200729 19991022 00729 EU 1999 10 22 AALA991168 1 19990814 A 3350 SSA3110 SWITCH AIRBUS 300 A300B4605R 3930308 EU L1 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14068 511 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING TEST BUTTON AT L1 DOOR INOPERATIVE. REPLACED EME RGENCY EXIT FLOOR PATH LIGHTING TEST BUTTON AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200730 19991022 00730 EU 1999 10 22 AALA991169 1 19990814 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU L1 DOORWAY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14068 511 JFK - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT CEILING LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT CEILING LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200731 19991022 00731 EU 1999 10 22 AALA991193 1 19990816 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROW 33C DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 33069 512 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33C INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEAT 33C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200732 19991022 00732 EU 1999 10 22 AALA991125 1 19990802 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU 3L DOORWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT DOOR 3L INOPERATIVE. REPAIRED WIRE TO EMERGENCY EXIT LIGHT AT DOOR 3L. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200733 19991022 00733 EU 1999 10 22 AALA991064 1 19990720 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 18HJ DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 18HJ INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200734 19991022 00734 EU 1999 10 22 AALA991106 1 19990729 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70079 619 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT CENTER DIVIDER IN ZONE B/C INOPERATIVE. RE SECURED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT CENTER DIVIDER IN ZONE B/C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200735 19991022 00735 EU 1999 10 22 AALA991163 1 19990812 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU 2R DOORWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70079 619 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AFT OF 2R DOOR INOPERATIVE. REPLACED WIRE TO EME RGENCY EXIT FLOOR PATH LIGHTING AFT OF 2R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200736 19991022 00736 EU 1999 10 22 AALA991164 1 19990812 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU 2L DOORWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70079 619 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AFT OF 2L DOOR INOPERATIVE. REPLACED WIRE TO EME RGENCY EXIT FLOOR PATH LIGHTING AFT OF 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200737 19991022 00737 EU 1999 10 22 AALA991154 1 19990809 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU ROW 1A LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59081 639 JFK - DURING OVERNIGHT MAINTENANCE, THE EMERGENCY EXIT LIGHTS WERE FLICKERING. RECONNECTED AND SECURED CONNECTOR AT 1A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200738 19991022 00738 EU 1999 10 22 AALA990785 1 19990530 A 2560 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU R3 EVAC BUTTON LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 JFK - DURING OVERNIGHT MAINTENANCE, R2 EVACUATION SIGNAL PUSH BUTTON INOPERATIVE. SECURED CONNECTOR ON R3 EVACUATION SI GNAL PUSH BUTTON. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999102200739 19991022 00739 NM 1999 10 22 AALA991250 1 19990822 A 3350 SOCKET BOEING 757 757223 1384957 NM R2 DOOR CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 646AA 24604 ORD - DURING OVERNIGHT MAINTENANCE, R2 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CORROSION FROM LAMP SOCKET AN D RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102200740 19991022 00740 NM 1999 10 22 AALA991248 1 19990821 A 3350 1703663 CONNECTOR BOEING 767 767323 1385205 NM ROW 28H BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 28H INOPERATIVE. REPLACED FEMALE SEAT CONNECTOR AN D PINS AT EMERGENCY EXIT SEAT LIGHT AT ROW 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102200741 19991022 00741 NM 1999 10 22 AALA991175 1 19990814 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313AA 22316 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 28B AND 32B INOPERATIVE. RESECURED CONNEC TOR TO EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 28B AND 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102200742 19991022 00742 NM 1999 10 22 AALA991317 1 19990901 A 7120 FITTING BOEING 727 727223 1384074 NM NR 3 ENGINE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND 2 UPPER TANG 'F' HOLES ELONGATED AND GOUGED 4 HOLES ELONGATED AT NR 3 ENGINE UPPER FORWARD FITTING. TWO 'E' TAN HOLES OVERSIZED AND FASTENERS INSTALLED 4 'D' HOLES OVERSIZED AND DOUBLER AND TRIPLER INSTALLED PER ESO 11697, DATE D 8-27-99 AND 8-31-99. (M) 2 L 7 3 4F A3WE 1999102200743 19991022 00743 NM 1999 10 22 AALA991303 1 19990827 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 294 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND FLOORBEAM LOWER FLANGE BROKEN COMPLETELY THROUGH THE WIRE BUNDLE STANDOFF SCREW HOLE. INSTALLED ANGLE, EQUA L LEG THICKNESS STAINLESS REPAIR PER SRM 51-40-4 PAGE 5. (M) 2 L 7 3 4F A3WE 1999102200744 19991022 00744 NM 1999 10 22 UIEA99084 1 19990929 A 5210 65B223504 DOUBLER BOEING 747 7472D7B 1384803 NM R1 DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 72098 22337 L1 DOOR HINGE CUTOUT DOUBLER, PREVIOUSLY INSTALLED, AT THE LOWER CUTOUT FOUND CRACKED. REPLACED DOUBLER ON DOOR HINGE C UTOUT PER SB 747-52-2144. (M) 2 L 7 4 4F RT A20WE 1999102200745 19991022 00745 NM 1999 10 22 UEIA99080 1 19990928 A 5753 SAFETY WIRE BOEING 747 74747UF 1384949 NM TE AFT FLAP BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 493MC 4376 29254 INSPECTED A/C PER ATLAS AIR FCD99-17, FOUND THE FOLLOWING AFT FLAP TRACK CARRIAGE BOGIE PIN ASSEMBLIES WITH FAILED SAFET Y WIRE AT TWO POSITIONS; NR 7 INBOARD PIN, WIRE BROKEN, TORQUE ON BOLT OK. NR 8 INBOARD, WIRE BROKEN, TORQUE ON BOLT OK . NO BOLT OR PIN MIGRATION AT THE FAILED WIRE POSITIONS. ALL OTHER POSITIONS OK. AIRCRAFT REPAIRED IAW ATLAS AIR FCD 99-17, REFERENCE IPC 27-51-28-01. (M) 2 L 7 4 4F RT 1384945 1999102200746 19991022 00746 NM 1999 10 22 UIEA99079 1 19990923 A 5753 SAFETY WIRE BOEING 747 74747UF 1384949 NM TE AFT FLAP BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 408MC 2696 29261 INSPECTED A/C PER ATLAS AIR FCD 99-17, FOUND THE FOLLOWING AFT FLAP TRACK CARRIAGE BOGIE PIN ASSEMBLY WITH FAILED SAFETY WIRE ON ONE POSITION; NR 1 OUTBOARD PIN, WIRE BROKEN, TORQUE ON BOLT OK. AIRCRAFT REPAIRED PER ATLAS AIR FCD 99-17, RE F IPC 27-51-28-01. (M) 2 L 7 4 4F RT 1384945 1999102200747 19991022 00747 NM 1999 10 22 UIEA99086 1 19990929 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM BS 1480 MISDRILLED A UIEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 15 526MC 72098 22337 DURING ACCOMPLISHMENT OF SB 747-53A2390 FIG 19, DETAIL L, OVERSIZING HOLES AT STRINGER 39 LEFT AND RIGHT SIDES FROM .25 INCH BY .375 INCH WOULD CAUSE UNACCEPATABLE EDGE DISTANCE. PER TELEX TLS-AMS-99-00033H, PERFORMED HFEC OPEN HOLE INSPEC TION, OVERSIZED HOLE BY .0625 INCH AND INSTALLED BOLT BACB30NX10K BOLT. (M) 2 L 7 4 4F RT A20WE 1999102200748 19991022 00748 NM 1999 10 22 UIEA99085 1 19990929 A 5312 BULKHEAD BOEING 747 7472D7B 1384803 NM BS 1480 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 72098 22337 WHILE ACCOMPLISHING SB 747-53A2390, HFEC INSPECTION OF BS 1480 HOLE NR 19 REVEALED A CRACK IN THE WEB PANEL ONLY. PER S B 747-53A2390 HOLE WAS OVERSIZED TO .5625 INCH WEB PANEL ONLY. INSTALLED FREEZE PLUG. FABRICATED SEPARATE BUSHING FOR THE WEB SPLICE PLATE, BULKHEAD AND OUTER CHORD SPLICE FITTING. (M) 2 L 7 4 4F RT A20WE 1999102200749 19991022 00749 NM 1999 10 22 UIEA99083 1 19990929 A 5210 65B223504 DOUBLER BOEING 747 7472D7B 1384803 NM R1 DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 72098 22337 R1 DOOR HINGE CUTOUT DOUBLER CRACKED, PREVIOUSLY INSTALLED AT UPPER CUTOUT. REPLACED DOOR HINGE CUTOUT DOUBLER PER SB 7 47-52-2144. (M) 2 L 7 4 4F RT A20WE 1999102200750 19991022 00750 NM 1999 10 22 UIEA99082 1 19990929 A 5320 65U6624227 FITTING BOEING 747 7472D7B 1384803 NM BS 1480 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 72098 22337 DURING HFEC INSPECTION OF BS 1480, FOUND LEFT OUTERCHORD SPLICE FITTING CRACKED BETWEEN HOLES NR 14 AND NR 15. REPLACED SPLICE FITTING IAW SB 747-53A2390. (M) 2 L 7 4 4F RT A20WE 1999102200751 19991022 00751 NM 1999 10 22 UIEA99081 1 19990929 A 2761 65B080996 FITTING BOEING 747 7472D7B 1384803 NM NR 6 SPOILER ACT CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 72098 22337 DURING ROUTINE INSPECTION, FOUND NR 6 SUPPORT ACTUATOR SUPPORT FITTING CRACKED ON SPOILER SUPPORT BEAM. REPLACED SUPPOR T FITTING PER SRM 51-30-02. (M) 2 L 7 4 4F RT A20WE 1999102200752 19991022 00752 1999 10 22 99ZZZM720 4 19990907 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION DE DESCENT 1 CE 01 97UX X3919 UE97 CAPTAINS ALTIMETER FLAGGED ON DESCENT. REMOVED AND REPLACED ALTIMETER. THIS IS THE FOURTH REPORT OF A FLAGGING PROBLEM WITH THIS ALTIMETER. BENCH TEST DID NOT VERIFY THE FAULT. (M) 2 L 7 2 4T RT A24CE 1999102200753 19991022 00753 EU 1999 10 22 C2XA99IA474 1 19990919 A 3350 LP1670 BULB AEROSP ATR42 ATR42320 8680930 EU ROW 9 FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING 4A INSPECTION, THE AISLE PATH EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 9. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102200754 19991022 00754 SO 1999 10 22 C2XA99IA473 1 19990917 A 3350 1317 BULB EMB 120 EMB120RT SO RT EXTERIOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING PREFLIGHT INSPECTION, THE TOP RIGHT EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102200755 19991022 00755 NM 1999 10 22 AALA994137 1 19990730 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM BS 1383 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 633AA 24591 AFW - LOWER SILL INNER CHORD HAS CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED BLENDED AREA WITH STRAP PER MRB 757-1509 , TREATED AND PRIMED. (M) 2 L 7 2 4F RT A2NM 1999102200756 19991022 00756 NM 1999 10 22 AALA994139 1 19990804 A 5330 14843611 SKIN BOEING 757 757223 1384957 NM BS 1862 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 633AA 24591 AFW - LEFT SIDE FUSELAGE SKIN AT STATION 1862 HAS SMALL AREA OF WEAR BEYOND SRM LIMITS. BLENDED SHARP EDGES, PERFORMED DYE PENETRANT INSPECTION FOR CRACKS, NONE FOUND. REPLACED ONE FASTENER IAW MRB 1511. (M) 2 L 7 2 4F RT A2NM 1999102200757 19991022 00757 NM 1999 10 22 AALA994138 1 19990804 A 5541 SPAR BOEING 757 757223 1384957 NM RUDDER DISBONDED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 633AA 24591 AFW - RUDDER FRON SPAR SKIN SHOWS DISBOND INDICATIONS AT STATION 226.5-228. CUTOUT DELAMINATION. PUT DRY CYCLE AND CUT OUT REPAIR PLYS, LAYUP AND COOK. TOP CHECK OK. (M) 2 L 7 2 4F RT A2NM 1999102200758 19991022 00758 NM 1999 10 22 AALA994145 1 19990816 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM BS 1681 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 630AA 24588 AFW - FLOORBEAM AT STATION 1681 HAS CORROSION REMOVED. A .080 THICK 7075-T6 REPAIR ANGLE WILL BE INSTALLED UNDER FORWRD FLANGE OF FLOORBEAM. A .071 THICK 7075-T6 FILLER WILL BE ADDED IN THE AREA OF THE REMOVED DECK PLATE. A .080 THICK 70 75-T6 DOUBLER WAS FASTENED OVER THE FILLER AND DECK PLATE. (M) 2 L 7 2 4F RT A2NM 1999102200759 19991022 00759 NM 1999 10 22 AALA994157 1 19990910 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 634AA 24592 AFW - FLOORBEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND LIMITS. BLEND OUT CORROSON AND REFINISH THE SRM. FILL BLE NDS ON THE UPPER HORIZONTAL FLANGE SURFACE WITH BM55-95 SEALANT. (M) 2 L 7 2 4F RT A2NM 1999102200760 19991022 00760 NM 1999 10 22 AALA994156 1 19990910 A 5320 SILL BOEING 757 757223 1384957 NM BS 1420 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 634AA 24592 AFW - AFT CARGO DOOR LOWR SILL T-CHORD HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT THE CORROSION AND RE-FINISH ED THE SURFACE FILLED BLENDS ON THE UPPER HORIZONTAL FLANGE SURFACE WITH BMS 5-95 SEALANT. (M) 2 L 7 2 4F RT A2NM 1999102200761 19991022 00761 NM 1999 10 22 AALA991391 1 19990906 A 5320 BEAM BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - STATION 1183 RIGHT VERTICAL BEAM IS CRACKED .25 INCH AT BL 8 IN RADIUS AT BEAM LOWER CHORD. REPAIRED VERTICAL BEA M AT STATION 1183 RBL 8 INCH IAW SB 727-53-0175, PER SRM 53-10-9. (M) 2 L 7 3 4F A3WE 1999102200762 19991022 00762 NM 1999 10 22 AALA991393 1 19990914 A 5311 FRAME BOEING 727 727223 1384074 NM BS 913 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - LEFT STATION 913 UPLOCK SUPPORT FRAME CRACKED ABOVE TOP RADIUS BLOCK. HFEC AREA VERIFIED ENDS OF CRACK AND STOP D RILLED. INSTALLED REPAIR PER SRM 53-10-2 PART 2. (M) 2 L 7 3 4F A3WE 1999102200763 19991022 00763 NM 1999 10 22 AALA991392 1 19990909 A 5311 FRAME BOEING 727 727223 1384074 NM BS 910 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - STATION 910 FRAME CRACKED ABOVE THE TOP RADIUS BLOCK R/W/W. STOP DRILLED THE CRACK AND INSTALLED REPAIR PER SRM 5 3-10-2 PAGE 2. (M) 2 L 7 3 4F A3WE 1999102200764 19991022 00764 NM 1999 10 22 AALA991412 1 19990913 A 5730 SKIN BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND LEFT SIDE OF AC BAY ABOVE PRIMARY HEAT EXCHANGER SKIN HAS CORROSION. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 1999102200765 19991022 00765 NM 1999 10 22 AALA991413 1 19990913 A 5730 SKIN BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - RIGHT SIDE OF AC BAY ABOVE PRIMARY HEAT EXCHANGER SKIN HAS CORROSION. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30 -3. (M) 2 L 7 3 4F A3WE 1999102200766 19991022 00766 NM 1999 10 22 AALA991414 1 19990913 A 5730 SKIN BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - RIGHT SIDE OF AC BAY ABOVE PRIMARY HEAT EXCHANGER SKIN HAS CORROSION. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30 -3. (M) 2 L 7 3 4F A3WE 1999102200767 19991022 00767 NM 1999 10 22 AALA991415 1 19990916 A 5330 SKIN BOEING 727 727223 1384074 NM BS 820-831 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - LEFT SIDE OF AC BAY ABOVE HEAT EXCHANGER SKIN IS CORRODED AT STATIONS 824 LBL 32, 826 LBL 44, 827 LBL 35 AND 826 L BL 32. REMOVED CORROSION, INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 1999102200768 19991022 00768 NM 1999 10 22 AALA991200 1 19990817 A 3241 S274T12010 VALVE BOEING 757 757223 1384957 NM RT ANTI-SKID DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 644AA 24602 DFW - FLT 1597 - EN ROUTE FROM ORD-MEX, RIGHT HYDRAULIC FLUID QTY DECREASED TO .56 WHILE LEFT HYDRAULIC FLUID QTY INCREA SED TO 1.35. RIGHT HYDRAULIC PUMPS DEACTIVATED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED LEFT AND RIGHT ANTI- SKID SHUTTLE VALVES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102200769 19991022 00769 WP 1999 10 22 AALA991425 1 19990921 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN NEED REPAIR A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 233AA 49180 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. REPAIRED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200770 19991022 00770 WP 1999 10 22 AALA991385 1 19990913 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 223AA 49173 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED WIRING CONN ECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200771 19991022 00771 WP 1999 10 22 AALA991384 1 19990913 A 3350 SPLICES DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505AA 49799 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIDEWALL LIGHTS AND EXIT SIGN LIGHTS INOPERATIVE. REPLACED WIRE SPLI CES TO EMERGENCY EXIT SIDEWALL LIGHTS AND EXIT SIGN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200772 19991022 00772 WP 1999 10 22 AALA991390 1 19990913 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS HAVE SECTIONS IN COACH CABIN AND AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIPS IN COACH CABIN AND AT FORWARD GALLEY. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200773 19991022 00773 WP 1999 10 22 AALA991394 1 19990914 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 207AA 49158 DFW - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED CONNECTOR ON BATTERY PACKS FOR EXTERIOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200774 19991022 00774 WP 1999 10 22 AALA991395 1 19990915 A 3397 WIRE DOUG DC9 DC982 3022082 WP AIRSTAIRS CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 440AA 49549 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED WIRING TO AFT AIRSTAIRS EM ERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200775 19991022 00775 WP 1999 10 22 AALA991404 1 19990918 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L1 DOORWAY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 207AA 49158 DFW - DURING OVERNIGHT MAINTENANCE, L1 DOOR EMERGENCY EXIT WALK AROUND LIGHT ARMED LIGHT INOPERATIVE. REPLACED EMERGENC Y EXIT WALK AROUND LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200776 19991022 00776 WP 1999 10 22 AALA991409 1 19990919 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 556AA 53086 DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT INOPERATIVE. SPLICED WIRE ON AFT EMERGENCY EXIT LIGHT. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102200780 19991022 00780 EU 1999 10 22 99ZZZX4043 1 19991004 A 3310 1179203103 CONTROL LUNIT BOLKMS 117 BK117B2 5626013 EU COCKPIT SHORT A R7MA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 11 7059N 0451 7154 INSTRUMENT LIGHTS FAILED. TWO MINUTES LATER, THE INSTRUMENT LIGHTS CIRCUIT BREAKER TRIPPED. PILOT RESET THE CIRCUIT BR EAKER. APPROXIMATELY FOUR MINUTES LATER, THE SMELL OF SMOKE WAS OBSERVED. AIRCRAFT WAS ON FINAL APPROACH AT THIS TIME AND SAFE LANDING WAS ACCOMPLISHED. NO EVIDENCE OF FLAME INSIDE OR AROUND LIGHT CONTROL UNIT. APPARENT INTERNAL SHORT O F CIRCUIT BOARD CAUSED ODOR OF BURNING WIRES AND SMOKE. 1 G 7 2 3U NC H13EU 1999102200784 19991022 00784 SW 1999 10 22 99ZZZX4047 1 19991006 A 6300 406310405101 UNIVERSAL 406010413117 BELL 407 407 SW M/R PITCH LINK FAILED A A FW7A K NONE O OTHER IN INSP/MAINT 1 EA 07 407P 238 RXFS4573 53028 THE MAIN ROTOR TRUNNION BEARNG HAS A LIFE LIMIT OF 5,000 HOURS. THREE OF THEM HAVE FAILED WITH LESS THAN 1,000 HOURS TT . ONE AT 789 HOURS, ONE AT 761 HOURS, AND ONE AT 238 HOURS TT. EACH TIME THE BEARING WAS REJECTED FOR AXIAL PLAY BEYON D .005 INCH. 1 G 7 1 3U O H2SW 1999102200809 19991022 00809 WP 1999 10 22 TWAA9914301 1 19991020 A 3350 LIGHT DOUG DC9 DC983 3022083 WP ROW 3-8 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 969TW 53619 THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 3 TO 8 AND AT ROW 11. THE AFT EMERGENCY PATHWAY LIGHTS AND TWO TAIL CONE LIG HTS WERE INOPERATIVE. REPLACED THE ELBOW ASSEMBLY (P/N 0105614-001), FOR ROWS 3 TO 8. REPLACED THE BULB, (P/N 7732) AT ROW 11 AND REPLACED THE BATTERY, (P/N 408822-101) FOR TAIL CONE AREA. 2 L 7 2 4F RT A6WE 1999102200810 19991022 00810 EU 1999 10 22 9904273202 1 19990930 A 5315 FLOORBEAM AIRBUS 320 A320211 3930320 EU FRAME 16-18 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 302US 32 DURING M-CHECK, FOUND CORROSION ON FLOORBEAM 1292L BETWEEN FRAME 16 AND 18. REPAIRED PER EA 32-163484. 2 L 7 2 4F RT A28NM 1999102200811 19991022 00811 EU 1999 10 22 9904283202 1 19991008 A 5315 FLOORBEAM AIRBUS 320 A320211 3930320 EU FRAME 16-24 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 302US 32 DURING M-CHECK, FOUND CORROSION ON FLOORBEAM 254R AND 765R BETWEEN FRAMES 16-24R. REPAIRED PER EA 163484 AND SRM 51-72- 11. 2 L 7 2 4F RT A28NM 1999102200812 19991022 00812 NM 1999 10 22 9904292717 1 19990917 A 5311 FRAME BOEING 727 7272S7 138407Z NM BS 950 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 721RC 22492 DURING M-CHECK, FOUND CRACK ON FRAME INNER CHORD AT FS 950, STR 24L. REPAIRED PER EA 27-120691A. 2 L 7 3 4F A3WE 1999102200813 19991022 00813 NM 1999 10 22 9904302717 1 19990915 A 5314 KEEL BEAM BOEING 727 7272S7 138407Z NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 721RC 22492 DURING M-CHECK, FOUND CORROSION ON THE OUTBOARD FLANGE OF THE LEFT KEEL BEAM AT FS 950A+2, WL 148, STR 29L. REPAIRED PE R EA 27-168000. 2 L 7 3 4F A3WE 1999102200814 19991022 00814 NM 1999 10 22 9904312717 1 19990830 A 5314 KEEL BEAM BOEING 727 7272S7 138407Z NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 721RC 22492 DURING M-CHECK, FOUND CORROSION ON KEEL BEAM LOWER OUTBOARD FLANGE FS 950B+4, WL 148, LBL 8, STR 29L. REPAIRED PER EA 2 7-168001. 2 L 7 3 4F A3WE 1999102200815 19991022 00815 NM 1999 10 22 9904322717 1 19990920 A 5315 FLOORBEAM BOEING 727 7272S7 138407Z NM BS 767 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 721RC 22492 DURING M-CHECK, FOUND MECHANICAL DAMAGE ON UPPER INBOARD FLANGE OF THE LONGITUDINAL FLOORBEAM FS 767, WL 208, LBL 45.5. REPAIRED PER EA 27-170698. 2 L 7 3 4F A3WE 1999102200816 19991022 00816 NM 1999 10 22 UPS99230955 1 19991019 A 5311 BAC1489235 FRAME BOEING 727 72725C 138400H NM BS 344 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI WHILE WORKING NRC 997306, FOUND SHEAR TIE CRACKED AT BS 344 RBL 32 BETWEEN 25 AND 26 RT STR. REPAIRE D IAW SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 1999102200817 19991022 00817 NM 1999 10 22 UPS99230957 1 19990822 A 5320 BEAM BOEING 727 72725C 138400H NM BS 266 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION ON 25 G-BEAM AT BS 266 LBL 8 TO RBL 3, WL 208 IN COCKPIT. REMOVED CORRODED G-BEAM AND REP LACED IAW SRM 51-30-02, 51-30-05. 2 L 7 3 4F A3WE 1999102200818 19991022 00818 NM 1999 10 22 UPS99230959 1 19990823 A 5730 SKIN BOEING 727 72725C 138400H NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION ON CUTOUT FOR ACCESS PANEL NR 7540, AFT SURFACE. REPAIRED CORROSION ON CUTOUT FOR ACCESS PANEL NR 7540 IAW ER NR 99-6029. 2 L 7 3 4F A3WE 1999102200819 19991022 00819 NM 1999 10 22 UPS99230960 1 19990822 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 481-580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, AREAS OF CORROSION ON SEAT TRACK BETWEEN BS 481 AND BS 580 LBL 25, WL 208. REMOVED CORRODED SEAT TR ACK, FABRICATED NEW ONE, AND INSTALLED IAW 53-10-05. 2 L 7 3 4F A3WE 1999102200820 19991022 00820 WP 1999 10 22 UPS99830950 1 19991019 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A, DURING MECHANICS PRE-DEPARTURE EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED EMERGENCY B ATTERY PACK, SYS OPS NORMAL PER 33-50-01. 2 L 7 4 4F RT 4A25 1999102200821 19991022 00821 WP 1999 10 22 UPS99830951 1 19990930 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, FUSELAGE FRAME AT FS 55 WAS CRACKED AT THE ATTACH ROD AT LONG 24R. CUT OUT DAMAGED AREA AND REPAIRE D THE FRAME IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999102200822 19991022 00822 WP 1999 10 22 UPS99830952 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, LT WING L/E UPPER SKIN BETWEEN XFS 703.75 AND 710 WAS CRACKED. STOP DRILLED THE CRACKS AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999102200823 19991022 00823 WP 1999 10 22 UPS99830953 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, LT WING LWR L/E SKIN AT EXTERNAL DOUBLER ABOVE THE NR 2 PYLON WERE CRACKED. REMOVED CRACKED EXTERNA L DOUBLER, NDT VERIFIED SKIN CRACK WAS TERMINATED BY THE EXISTING STOP DRILL. FABRICATED AND INSTALLED INTERNAL AND EXT ERNAL DOUBLERS IAW SRM 57-2-1A FIG 1. 2 L 7 4 4F RT 4A25 1999102200824 19991022 00824 WP 1999 10 22 UPS99830954 1 19991003 A 5230 5641013501 JAMB DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, THE D-PIT DOOR JAMB WEB WAS CRACKED AND CORRODED AT SEVERAL FASTENER HOLES ACROSS THE BOTTOM. CUT O UT THE DAMAGED AREA, FABRICATED REPLACEMENT PARTS, INSTALLED REPLACEMENT PARTS IAW DWG 5641013 AND SRM 51-1-21A. 2 L 7 4 4F RT 4A25 1999102200825 19991022 00825 WP 1999 10 22 UPS99830956 1 19991004 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 187 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, THE FUSELAGE SKIN AT FS 187, JUST ABOVE THE CUSP AT THE FWD SERVICE DOOR AFT LWR CORNER WAS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 1999102200826 19991022 00826 WP 1999 10 22 UPS99830958 1 19991004 A 5330 SKIN DOUG DC8 DC873F 302199F WP SERVICE DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, THE FUSELAGE SKIN AT THE FWD UPPER CORNER OF THE FWD SERVICE DOOR WAS CRACKED. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-0 FIG 14. 2 L 7 4 4F RT 4A25 1999102200827 19991022 00827 WP 1999 10 22 UPS99830961 1 19991005 A 5330 57503653 SKIN DOUG DC8 DC873F 302199F WP BS 660&710 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, FUSELAGE SKIN AT FS 660 AND 710 WERE CORRODED BEYOND LIMITS. CUT OUT DAMAGED SKIN AND INSTALLED REP LACEMENT SECTION BETWEEN FS 610, FS 780, LONG 31L TO 31R IAW DH SK814-107. 2 L 7 4 4F RT 4A25 1999102200828 19991022 00828 WP 1999 10 22 UPS99830962 1 19991016 A 5311 SPAR DOUG DC8 DC871F 302199D WP CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C123, THE CENTER WING REAR SPAR LOWER CHORD WAS CRACKED AT XCW 0 TO XCW 2.5. STOP DRILLED CRACKS AND RE PAIRED THE SPAR CHORD IAW DH SK718-583. 2 L 7 4 4F RT 4A25 1999102200829 19991022 00829 WP 1999 10 22 UPS99830963 1 19991019 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 809UP 46109 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK ASSY PER MM 33-50-01. 2 L 7 4 4F RT 4A25 1999102200830 19991022 00830 NM 1999 10 22 99FDEA00429 1 19991019 A 5311 6556116 FRAME BOEING 727 7272S2F 1384O81 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 CORROSION ON FRAME AT BS 720D BETWEEN STR 4L AND STR 4R OUT OF LIMITS. *S/D* REMOVED CORROSION, FABRICATED AND INSTALL ED REPAIR PARTS IAW FEDEX SRM 53-10-4 FIG 1 STR 5L TO STR 3R. 2 L 7 3 4F A3WE 1999102200831 19991022 00831 NM 1999 10 22 99FDEA00430 1 19991019 A 5311 6556115 FRAME BOEING 727 7272S2F 1384O81 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 CORROSION (C53-244-01, 1) ON FRAME BS 720C, STR 4 LT - STR 5 RT. *S/D* REPAIRED FRAME IAW FEDEX SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 1999102200832 19991022 00832 NM 1999 10 22 99FDEA00431 1 19991019 A 5311 6556117 FRAME BOEING 727 7272S2F 1384O81 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 CORROSION ON FRAME BS 720E, STR 2 LT TO STR 4 RT OUT OF LIMITS. *S/D* REMOVED CORRODED SECTION, FAB AND INSTALLED REP AIR PARTS IAW FEDEX SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 1999102200833 19991022 00833 NM 1999 10 22 99FDEA00432 1 19991019 A 5311 6551113 FRAME BOEING 727 7272S2F 1384O81 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 CORROSION (C53-224-01,1) ON FRAME BS 720A, STR 2-3 RT. *S/D* REPAIRED FRAME IAW FEDEX SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 1999102200834 19991022 00834 NM 1999 10 22 99FDEA00433 1 19991019 A 5330 6525331651 SKIN BOEING 727 7272S2F 1384O81 NM BS 720 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 CHAFING ON EXTERIOR SKIN BS 720D+14 S19R. *S/D* REPAIRED EXT SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1999102200835 20000613 00835 NM 2000 6 13 99FDEA00434 1 19991019 A 5330 6525331951 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 NR 593 CHAFFING ON EXTERIOR SKIN BS 720D + 14 S19L. ** S/D ** REPAIRED SKIN PER IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1999102200836 20000613 00836 NM 2000 6 13 99FDEA00435 1 19991019 A 5315 6563169 FLOORBEAM BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 NR 346 CORROSION (C53-224-01(1)) AROUND NUT CLIP HOLES BS 344 FLOORBEAM UPPER CHORD AT LBL 13 AND RBL 10-12, WL 208. * * S/D ** REPAIRED PER IAW FEDEX SRM 53-10-8, 51-30-2, 51-10-2. 2 L 7 3 4F A3WE 1999102200837 19991022 00837 NM 1999 10 22 99UAL900437 1 19990822 A 2560 101655304 SLIDE GOODRICH 101655304 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT EMER EXIT DEPLOYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 RT WING SLIDE DEPLOYED INADVERTENTLY. SLIDE DOOR HAD 7 INCH HAIRLINE CRACK IN HONEYCOMB. THERE ARE THREE INNER HINGES BROKEN AND FOUR KEEPERS RUPTURED. *S/D* THE SLIDE INADVERTENTLY DEPLOYED WHILE PINNING THE INFLATION CYLINDER. THE DE PLOYMENT WAS HENCE OUT OF TYPICAL SEQUENCE. THE COMPARTMENT DOOR WAS NOT COMMANDED TO OPEN. THE SLIDE INFLATED INSIDE THE COMPARTMENT AND FORCED THE DOOR OPEN, THUS DAMAGING THE DOOR BY CRACKING THE HONEYCOMB, BREAKING THREE HINGES AND RU PTURING THE FOUR KEEPERS. THE ROOT CAUSE WAS HUMAN ERROR. 2 L 7 2 4F 4 F RT A1NM E24NE 1999102200838 19991022 00838 NM 1999 10 22 99UAL900512 1 19991008 A 3270 65579288 TAILSKID BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT FUSELAGE DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7277U 21424 POSSIBLE TAIL STRIKE ON TAKEOFF FROM BDL. TAIL STRIKE ILLUMINATION LIGHT ON. OVER SYR UNABLE TO MAINTAIN PRESSURE. DI VERTED TO CLE. *S/D* REPLACED CYLINDER AND SKID STRIKE PAD, OPERATIONALLY CHECKED OK. ALSO, PERFORMED CABIN PRESSURIZ ATION SYSTEM CHECK, CABIN PRESSURIZATION OPS CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1999102200839 19991022 00839 NM 1999 10 22 99UAL900513 1 19991010 A 3231 1U10851 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG DOOR CRACKED A UALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 WP 29 7269U 21416 AFTER DEPARTURE FROM BDL, AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE. DIVERTED TO BOSTON. *S/D* FOUND RT MLG LOCK OPER ATED DOOR SEQUENCE VALVE ASSY CRACKED. REPLACED VALVE. JACKED AIRCRAFT, ACP'D GEAR SWING FIVE COMPLETE CYCLES AND CYCL ED ALL FLIGHT CONTROLS. RT MLG AND WHEEL WELL CLEANED OF HYDRAULIC FLUID. HYD QTY SERVICED TO FULL. 2 L 7 3 4F 4 F A3WE E2EA 1999102200840 19991022 00840 NM 1999 10 22 99UAL900514 1 19991008 A 3020 VALVE WHITTAKER 1726257 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ANTI ICE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 315UA 1839 23947 NUMBER TWO ANTI-ICE VALVE OPEN INDICATION ILLUMINATED WITH THE SELECT SWITCH IN THE ON POSITION. WHEN ATTEMPTED TO OPEN THE VALVE, THERE WERE NO INDICATION OF EXHAUST GAS TEMPERATURE INCREASE. *S/D* REPLACED NUMBER TWO ENGINE ANTI-ICE VA LVE AND UNLOCKED THE HI STAGE VALVE PER MM 30-21-11 AND MM 30-21-00. OPERATIONS CHECK GOOD, NO LEAKS. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102200841 19991022 00841 NM 1999 10 22 99UAL900515 1 19991007 A 5531 SPAR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7452U 21906 THE VERTICAL STABILIZER MID SPAR CHORD AT FIN STATION 215 ON BOTH THE RIGHT AND LEFT SIDES WERE FOUND CHAFED TO BELOW T HE MINIMUM ALLOWABLE THICKNESS OF THE CHORD. THE DAMAGED AREAS WERE BLENDED OUT AND A REINFORCING REPAIR ANGLE WAS INST ALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED BY BOEING'S DER WITH AN 8110=3. 2 L 7 3 4F 4 F A3WE E2EA 1999102200842 19991022 00842 NM 1999 10 22 99UAL900516 1 19991010 A 2751 INDICATOR 1812996 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE TE FLAPS FAILED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 912UA 0439 25290 THERE IS A FIVE DEGREE DISCREPANCY BETWEEN THE COMMANDED AND DISPLAYED INDICATIONS ON THE TRAILING EDGE FLAPS. ALTERNAT E FLAPS WERE USED TO FULLY EXTEND THE FLAPS. S/D, INSTALLED A SERVICEABLE FLAP POSITION INDICATOR. THE INDICATOR TESTED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102200843 19991022 00843 NM 1999 10 22 99UAL900517 1 19991012 A 2120 AIR DIST BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE ROW 2B ODOR A UALA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 WP 29 609UA 21870 ELETRICAL OVERHEAT SMELL FROM AREA OF SEAT 2B. S/D, EWR OP CHECKED SEATS 2 A/B ON ARRIVAL 10/12. NO SMELL NOTED. ALSO , CHECKED VIDEO SYSTEM AND NO SMELL NOTED. CLEANED AREA UNDER SEAT AND RETURN AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999102200844 19991022 00844 NM 1999 10 22 99UAL900518 1 19991012 A 2150 ROTOR HAMILTON STD 8102093 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ACM WORN A UALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 WP 29 773UA 940414 26929 AFTER T/O, SMELL OF SMOKE IN COCKPIT, DISSIPATED AFTER FEW MINUTES. ALSO REPORTED NOISE ON LEFT SIDE OF CABIN MID-SHIP FOLLOWED BY PACK MODE L ADVISORY MESSAGE. AIRCRAFT RETURNED TO IAD. *S/D* REPLACED LEFT AIR CYCLE MACHINE. THIS WAS A 810209-3 ACM, AND IT WAS RETURNED TO THE VENDOR FOR INVESTIGATION, ANALYSIS AND UPGRADE. ANALYSIS AND INVESTIGATION O N THE REMOVED ACM BY HAMILTON STANDARD AND BOEING REVEALED THAT THE ROTOR WAS RUBBING AGAINST THE ACM HOUSING (RIGHT BEF ORE ACM SEIZING), THIS EXPLAINED THE HAZE AND SMELL OF METAL TO METAL FRICTION EXPERIENCED BY FLIGHT CREW. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200845 19991022 00845 NM 1999 10 22 99UAL900519 1 19991009 A 3350 LIGHT PAGE AEROSPA D71702001 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 NUMEROUS EMERGENCY LIGHTS INOPERATIVE ASSOCIATED WITH COMMON BATTERY PACK FOUND INOPERATIVE DURING A-CHECK. *S/D* FOUN D SINGLE EMERGENCY LIGHT ASSEMBLY SHORTED TO GROUND CAUSING ASSOCIATED BATTERY SUPPLY TO BECOME DEPLETED. REPLACED ASSE MBLY AND OPERATIONALLY CHECKED SUCCESSFULLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200846 19991022 00846 NM 1999 10 22 99UAL900520 1 19991009 A 3350 BATTERY PACK PAGE AEROSPA D71702001 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 FOUND EMERGENCY LIGHTS GO OUT AFTER ONE MINUTE FOR SEVERAL BATTERY PACKS. *S/D* REPLACED BATTERY PACKS (P/N D717-02-00 1) DUE TO TWO OF FOUR INTERNAL FUSES OPEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200847 19991022 00847 NM 1999 10 22 99UAL900521 1 19991006 A 4930 4417616 FUEL CLUSTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU FAILED A UALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 29 798UA 3017 26928 P1162 APU WOULD NOT START ON LANDING. *S/D* PRIMARY CAUSE WAS ATTRIBUTED TO A FAILED FUEL CLUSTER. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200848 19991022 00848 NM 1999 10 22 99UAL900522 1 19990925 A 2450 CABLES BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN CHAFED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 796UA 26931 WHILE CHECKING INOPERATIVE VIDEO ENTERTAINMENT SYSTEM PROBLEM, FOUND BUFFER BOX NR 2 AND NR 3 CIRCUIT BREAKERS POPPED. A TTEMPTED RESET RESULTED IN SPARKS IN VIDEO CLOSET BEHIND VIDEO EQUIPMENT. SUBSEQUENT INVESTIGATION UNCOVERED BURNED WIR ES AT CONNECTOR P3-D9030, P3-D9032 AND P3-D9031. *S/D* WIRES REPAIRED AND CABLE ASSEMBLY RE-ROUTED AND SECURED WITH C ABLE CLAMP. CHAFING PROTECTION INSTALLED TO PANEL EDGE AND WIRE BUNDLES. CABLE (P/N'S 17704401, 17704101, 17704601). 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200849 19991022 00849 NM 1999 10 22 99UAL900523 1 19991013 A 3230 CIRCUIT CARD 2899111 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 941UA 26676 LANDING GEAR EXTENSION WAS NORMAL, BUT RETRACTION REQUIRED LOCK OVERRIDE. THE FLIGHT CREW CYCLED THE LANDING GEAR CIRCU IT BREAKER, BUT NO RESPONSE FROM THE LANDING GEAR. *S/D* REPLACED THE GROUND SENSING SQUAT SWITCH CIRCUIT CARD, M990. CONDUCTED OPERATIONAL CHECKS ON THE LANDING GEAR, ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102200850 20001010 00850 NE 2000 10 10 99UAL900524 2 19991013 A 7321 7791005 FUEL CONTROL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE OUT OF ADJ A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 560UA 26660 718000 DIVERTED TO MCI DUE TO NR 1 ENGINE SURGE. *S/D* THE FUEL CONTROL UNIT WAS FOUND TO BE OUT OF ADJUSTMENT. THE FCU WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999102200851 19991022 00851 EU 1999 10 22 99UAL900525 1 19991012 A 3350 GE1810 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 424UA 506 UNIT EMER L AND COMM EMER L ATA 33-51-38 DISPLAYED AFTER TEST. *S/D* UNIT EMER L AND COM EMER L WERE SHOWN IN TEST DUR ING NR 3 SERVICE. LT OVERWING EPSU INDICATED 3 RED LIGHTS. NEW EPSU AND BATTERY DID NOT HELP. OVERWING EXTERIOR LIGHT S WERE RELAMPED AND CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999102200852 19991022 00852 1999 10 22 99UAL900526 4 19991014 A 2210 COUPLER HONEYWELL 4030952902 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE E/E COMP FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 994UA 33 22384 DURING TAKEOFF AT 120 KNOTS, AIRCRAFT YAWED TO THE RIGHT. AT THE TIME, NUMBER 1 AND 2 ENGINE OUTPUTS WERE EQUAL. *S/D* REPLACED THE YAW DAMPER COUPLER. REPLACED THE BEARINGS AS A PRECAUTION. 2 L 7 2 4F 4 F A16WE E2EA 1999102200853 19991022 00853 NM 1999 10 22 99UAL900527 1 19991013 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 796UA 26931 EMERGENCY LIGHT OUTSIDE DOOR 1L WAS INOPERATIVE. *S/D* FOUND SOME LIGHT CORROSION IN SOCKET. CLEANED OUT SOCKET AND R EPLACED BULB. OPERATIONAL CHECK WAS SATISFACTORY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200854 19991022 00854 NM 1999 10 22 99UAL900528 1 19991013 A 3397 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ROW 2F LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 796UA 26931 EMERGENCY LIGHTS AT SEATS 1EF AND 2F ARE INOPERATIVE. *S/D* SECURED WIRES IN CENTER BETWEEN SEATS 2B, C. ALL LIGHTS O PERATIONALLY CHECK NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102200855 19991022 00855 NM 1999 10 22 SCNA99603 1 19990918 A 5320 BEAM BOEING 727 7272A1 138407F NM BS 740 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINTENANCE CHECK, A CREASE BEAM WAS FOUND CRACKED AT LEFT FS 740 SIDE. FABRICATED A NEW ATTACH Z-ANGLE OUT OF 7075 T6 .040 PER B727 SRM 51-20-1. FABRICATED REPAIR ANGLES OUT OF 7075 T6 .063 IAW BAC 727 SRM 51-40-4. INSTAL LED REPAIR ANGLES AND Z-ANGLES. 2 L 7 3 4F A3WE 1999102200856 19991022 00856 NM 1999 10 22 SCNA99604 1 19990831 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 950F CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINTENANCE CHECK IN THE AFT CARGO COMPARTMENT AT FS 950F WL 203 RBL 55. THE FUSELAGE SKIN FRAME WAS FOU ND CRACKED FWD OF THE DOOR WARNING SWITCH ON THE SECONDARY LIP FLANGE. FOUND SEAL DEPRESSOR DAMAGED BEYOND REPAIR. FAB RICATED A NEW SEAL DEPRESSOR IAW B727 SRM 51201. ALODINED, PRIMED AND INSTALLED SEAL DEPRESSOR. INSTALLED SEAL RETAINE R IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 1999102200857 19991022 00857 NM 1999 10 22 SCNA99605 1 19991012 A 3350 BATTERY PACK BOEING 727 7272A1 138407F NM R1 SLIDE DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINTENANCE CHECK, THE R1 SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 3350 22, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999102200858 19991022 00858 NM 1999 10 22 SCNA99127 1 19991017 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM L1& R1 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 21676 DURING A LINE MAINTENANCE CHECK, THE OVERHEAD AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE AT THE L1 R1 DOOR. REMOVED AN D REPLACED ASSOCIATED BATTERY PACK FOR OVERHEAD AISLE EMERGENCY LIGHT, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999102200859 19991022 00859 NM 1999 10 22 SCNA99128 1 19991018 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 21676 DURING A LINE MAINTENANCE CHECK, THE OVERHEAD OVERWING AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACE D ASSOCIATED BATTERY CARTRIDGE FOR THE OVERHEAD AISLE EMERGENCY LIGHT, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999102200860 19991022 00860 EU 1999 10 22 RAIA9910027 1 19991006 A 2150 22051204 COOLING TURBINE AEROSP ATR72 ATR72202 8680940 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 723TE 283 STL- LEFT PACK DUCT OVERHEATING. MAINTENANCE REPLACED COOLING TURBINE ON LEFT SIDE. 2 H 7 2 4T RT A53EU 1999102700001 19991027 00001 EA 1999 10 27 CA990907071 1 19990829 A 2910 60075123119 HOSE CNDAIR CL601 CL6012A12 1900303 EA NR 1 HYD SYS LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) NR 1 EDP HYDRAULIC PRESSURE HOSE FLEXIBLE LEAKING CAUSING SYSTEM QUANTITY AND PRESSURE LOSS IN-FLIGHT. HOSE SHOW S SIGNS OF TEFLON COMING OUT THROUGH STAINLESS STEEL BRAID. 2 L 7 2 4F RT A21AE 1999102700002 19991027 00002 SO 1999 10 27 CA990927019 1 19990913 A 2730 710563 SPRING PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 836 RL103161 (CAN) INSPECTION CARRIED OUT IN ACCORDANCE WITH ALERT AL 99-04. FOUND SPRING CRACKED AT ATTACH LOOP. 1 L 7 2 3O 3 O A20SO E14EA 1999102700003 19991027 00003 WP 1999 10 27 AT9900706 1 19990929 A 5260 ANGLE DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND AFT AIRSTAIR, FIFTH STEP FROM THE BOTTOM AT SUPPORT ANGLE, WAS CORRODED. REMOVED CORRODED ANGLE, FABRICATED, TRE ADED, PRIMED, AND INSTALLED NEW ATTACH ANGLE IAW DC9 SRM 51-10-1, 52-60-0, 51-10-3, 51-10-5, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1999102700004 19991027 00004 WP 1999 10 27 AT9900707 1 19990928 A 5260 STEP DOUG DC9 DC932 3022066 WP AFT AIR STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND AFT AIRSTAIR NR 3 WAS CORRODED. REMOVED AND REPLACED STEP IAW DC9 SRM 51-10-3, 53-01, 53-30-1. 2 L 7 2 4F A6WE 1999102700005 19991027 00005 1999 10 27 CA990907048 4 19990826 A 2565 2N1068 SLIDE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU FUSELAGE DETACHED W K NONE O OTHER IN INSP/MAINT 1 CA 1355 19309 DRG25466 (CAN) DURING CREW TRAINING, THE BAGGAGE DOOR ESCAPE CHUTE WAS DEPLOYED. AS THE FIRST CREW MEMBER DESCENDED, THE CHUTE S TE SLIDE BODY DETACHED FROM THE DETACHMENT STRAP CAUSING THE CHUTE TO COLLAPSE. THE STITCHING BETWEEN THE SLIDE BODY AN D THE A TRAP HAD FAILED ALLOWING THE ASSY TO SEPARATE. 2 L 7 2 3T 4 T A24EU A196 6 C P899 1999102700006 19991027 00006 EU 1999 10 27 CA990907049 1 19990826 A 2612 162D FIRE RELAY BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU NR 1 ENGINE MALFUNCTIONED W A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CA 7024 19309 DRG25466 (CAN) IN CRUISE, NR 1 ENGINE FIRE WARNING LIGHT AND FIRE ALARM BELL ACTIVATED. THE ENGINE WAS SHUT DOWN AND BOTH FIRE B OTTLES DISCHARGED INTO THE ENGINE. AIRCRAFT RETURNED TO BLOCKS. DURING RETURN FLIGHT, THE FIRE WARNING REMAINED ON, BUT EVIDENCE OF FIRE COULD NOT BE SEEN. INVESTIGATION REVEALED NO EVIDENCE OF FIRE. NR 1 FIRE RELAY INSTALLED ON NR 2 ENGINE AND SNAG MOVED TO NR 2 ENGINE. RELAY REPLACED. 2 L 7 2 3T 4 T A24EU A196 6 C P899 1999102700008 19991027 00008 EU 1999 10 27 CA990915076 1 19990906 A 3020 FYLB521452 VALVE AIRBUS 330 A330202 3930316 EU ANTI-ICE SYSTEM FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) REJECTED TAKEOFF DUE TO ECAM ENGINE THRUST LOSS MESSAGE. ANTI-ICE VALVE REPLACED. 2 L 7 2 4F RT A46NM 1999102700009 19991027 00009 SW 1999 10 27 CA990916018 1 19990826 A 2900 170F0016CR0344 HOSE SWRNGN SA226 SA226TC 8780404 SW HYDRAULIC SYS LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) LEFT HYDRAULIC PUMP OUTLET HOSE DEVELOPED A LEAK WHICH CAUSED A TOTAL LOSS OF THE FLUID IN THE MAIN HYDRAULIC SYST EM. 2 L 7 2 4T RT A8SW 1999102700010 19991027 00010 EU 1999 10 27 CA990927034 1 19990910 A 5610 A212500009 WINDSHIELD PPG A21500009 FOKKER F28 F28MK1000 4990808 EU COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 96171H9995 (CAN) AT HEIGHT OF CLIMB, CAPTAIN'S WINDSHIELD DEVELOPED A CRACK. AIRCRAFT SLOWED DOWN AND CONTINUED TO DESTINATION, E N ROUTE ADDITIONAL CRACKING OCCURRED, IN OUTER LAYER. WINDOW REPLACED. 2 L 7 2 4F RT A20EU 1999102700011 19991027 00011 EA 1999 10 27 CA990927062 2 19990908 A 8520 LW11775 PLUG PIPER PA28 PA28161 7102803 SO LYC O320 O320D3G 41508 EA ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 523 C1318639A C1318639A (CAN) NEW PISTON PLUGS, PN 72198, INSTALLED PER SI NR 1267C. 1 L 7 1 3O 3 O 2A13 E274 1999102700012 19991027 00012 EU 1999 10 27 CA991004027 1 19990916 A 7931 OIL PRESSURE PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE ENGINE FLUCTUATED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 1087 (CAN) DURING FLIGHT, AIRCRAFT EXPERIENCED INDICATIONS OF FLUCTUATING OIL PRESSURE. PRESSURE FLUCTUATED FROM TOP TO BOTT OM OF INDICATOR RANGE SEVERAL TIMES, WHEREUPON THE CREW ELECTED TO RETURN TO BASE. 10 MINUTES PRIOR TO LANDING, THE OIL PRESSURE INDICATIONS RETURNED TO NORMAL. MAINTENANCE INSPECTED THE OIL SYSTEM INCLUDING THE OIL FILTER AND FOUND NO CO NTAMINATION. REPLACED THE OIL FILTER AND ASSOCIATED O-RINGS, REPLACED THE O-RING ON THE OIL PRESSURE REGULATOR. FUNTIO NAL TESTS AND GROUND RUN WAS CARRIED OUT AND NO FAULTS COULD BE FOUND OR FLUCTUATING OIL PRESSURE READINGS DUPLICATED. A IRCRAFT RETURNED TO SERVICE, NO FURTHER FAULTS NOTED IN 30 HOURS OF OPS. 1 L 7 1 3T 4 T RT A78EU E26NE 1999102700013 19991027 00013 SO 1999 10 27 CA991004032 1 19990908 A 3242 953463 DISC GULSTM G159 G159 3952202 SO RROYCE DART DART5298X 54507 EU BRAKE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 16272 (CAN) CREW TAXIED FROM RAMP THEN HEARD NOISE FROM RIGHT SIDE OF AIRCRAFT. INCREASED POWER TO MOVE AIRCRAFT - WOULD NOT MOVE. FOUND NR 4 BRAKE DISC BROKEN AND JAMMED IN WHEEL RIM. WHEEL, BRAKE, AND DISC REPLACED. 2 L 7 2 4T 4 T 1A17 E297 1999102700014 19991027 00014 SO 1999 10 27 CA991004051 1 19990907 A 2460 AN33701 RELAY PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA BATTERY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1331 752 RL260661A (CAN) IN IFR FLIGHT DURING DESCENT, SMOKE APPEARED IN THE COCKPIT. CREW SHUT THE HEATER AND THE MASTER SWITCH, OPENED S IDE WINDOWS TO CLEAR THE SMOKE. AFTER LANDING, THE AME NOTED THAT THE BATTERY RELAY HAD HEATED AND THAT TERMINAL 2 OF T HE RELAY HAD MELTED. DETAILED INSPECTION OF THE BATTERY AND ELECTRICAL WIRING WAS DONE. THE RELAY WAS REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 1999102700015 19991027 00015 SW 1999 10 27 CA991004057 1 19990915 A 2731 DL5040M5 ACTUATOR 274300056 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP PITCH TRIM SEIZED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 2135 P54024 (CAN) IN PREPARATION FOR DESCENT, THE PILOT WAS UNABLE TO OPERATE THE PITCH (STABILIZER) TRIM. THE AIRCRAFT LANDED WITH NO PITCH TRIM CONTROL. MAINTENANCE DETERMINED THE TRIM ACTUATOR WAS SEIZED AND REPLACED IT. 2 L 7 2 4T 4 T RT A8SW E4WE 1999102900001 19991029 00001 NM 1999 10 29 S84A94 1 19990912 A 3350 CONNECTOR BOEING 727 727251 138408H NM SWITCH LOOSE A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 65035 20289 EWR - DURING A-CHECK, FOUND AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH DID NOT TURN ON LIGHTS. TIGHTENED LOOSE CONNECTION ON SWITCH. (X) 2 L 7 3 4F A3WE 1999102900002 19991029 00002 NM 1999 10 29 S84A95 1 19990912 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 65035 20289 EWR - DURING A-CHECK, FOUND LEFT AFT (OPPOSITE CARGO DOOR) EMERGENCY LIGHT OUT. CHARGED BATTERIES, OPS CHECK OK. (X) 2 L 7 3 4F A3WE 1999102900003 19991029 00003 NM 1999 10 29 S84A96 1 19990912 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 65035 20289 EWR - DURING A-CHECK, FOUND RIGHT AFT (CARGO DOOR) EMERGENCY LIGHT OUT. CHARGED BATTERIES. OPS CHECK OK. (X) 2 L 7 3 4F A3WE 1999102900004 19991029 00004 NM 1999 10 29 S84A97 1 19990912 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 65035 20289 EWR - DURING A-CHECK, FOUND AIRSTAIR EMERGENCY LIGHT OUT. CHARGED BATTERIES. OPS CHECK OK. (X) 2 L 7 3 4F A3WE 1999102900005 19991029 00005 NM 1999 10 29 S84A98 1 19990912 A 3350 BULB BOEING 727 727251 138408H NM CABIN LOOSE A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 65035 20289 EWR - DURING A-CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT BULB OUT. FOUND LIGHT BULB LOOSE. RE-INSTALLED. (X) 2 L 7 3 4F A3WE 1999102900006 19991029 00006 NM 1999 10 29 S84A91 1 19990906 A 3350 S106 BATTERY BOEING 727 727276 138408R NM ROW 18 DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 908PG 53445 20951 EWR - DURING A-CHECK, FOUND EMERGENCY EXIT LIGHT AISLE ROW 18 INOPERABLE. REMOVED AND REPLACED BATTERIES PER MM 33-50- 22. P/N OFF S106. P/N ON S106. (X) 2 L 7 3 4F RT A3WE 1999102900007 19991029 00007 NM 1999 10 29 S84A99 1 19990919 A 3350 900835A BATTERY PACK BOEING 727 727276 138408R NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 908PG 18290 20951 DURING A-CHECK INSPECTION, THE L2 AND R2 E-PATH LIGHTS WERE FOUND INOPERABLE. REMOVED AND REPLACED BATTERY PACK ASSY. ( X) 2 L 7 3 4F RT A3WE 1999102900008 19991029 00008 NM 1999 10 29 S84A92 1 19990906 A 3350 900542 BATTERY PACK BOEING 727 727276 138408R NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 908PG 53445 8361 20951 EWR - DURING A-CHECK, AFT SERVICE DOOR'S EXIT SIGN FLOOR LEVEL FOUND INOPERABLE. LEFT AND RIGHT SIDES. REMOVED AND REP LACED POWER SUPPLY AND BATTERY PACK PER MM 33-50-22. OPS CHECK OK. POWER SUPPLY P/N ON 9005-42. P/N OFF 9005-42. S/N ON 19886. S/N OFF 8361. (X) 2 L 7 3 4F RT A3WE 1999102900009 19991029 00009 NM 1999 10 29 S84A93 1 19990906 A 3350 900542 BATTERY PACK BOEING 727 727276 138408R NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 908PG 53445 361 20951 EWR - FORWARD OVER WING EXIT SIGN'S FLOOR LEVEL INOPERABLE, LEFT AND RIGHT SIDES. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK PER MM 33-50-22. OPS CHECK OK. POWER SUPPLY, P/N ON 9005-42. P/N OFF 9005-42. S/N ON A6959. S/N OFF 3 61. (X) 2 L 7 3 4F RT A3WE 1999102900010 19991029 00010 NE 1999 10 29 99ZZZX4071 2 19990820 A 7250 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 131 120987 7125 LE45218EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999102900011 19991029 00011 NE 1999 10 29 99ZZZX4072 2 19990406 A 7420 430111202 LEAD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE IGNITION SYSTEM WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 332 2650 7127 LE45385E LEAD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999102900012 19991029 00012 EU 1999 10 29 99ZZZX4073 1 19990718 A 6240 430106202 SPEED PICKUP BOLKMS 117 BK117A3 5626015 EU NG TACHOMETER INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 134 98H0055 7058 SPEED PICKUP INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999102900013 19991029 00013 NE 1999 10 29 99ZZZX4074 2 19990827 A 7420 430111202 LEAD BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE IGNITION S YSTEM WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 615 2017 7063 LE45322E LEAD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999102900014 19991029 00014 NE 1999 10 29 99ZZZX4075 2 19990416 A 7420 430111202 LEAD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE IGNITION SYSTEM CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 918 2431 7173 LE45583EFA INSULATOR CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1999102900015 19991029 00015 NE 1999 10 29 99ZZZX4076 2 19990603 A 7420 430111202 LEAD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE IGNITION SYSTEM CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 90260 355 2590 7140 LE45514EF LEAD CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1999102900016 19991029 00016 SW 1999 10 29 99ZZZX4077 1 19991011 A 2432 BATTERY CONCORDEBATT BELL 222 222U 1182140 SW BATTERY TRAY FAILED A NXTA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 19 144CF 200 CBC345380 47535 NR 2 GENERATOR LIGHT CAME ON. PILOT ABORTED FLIGHT AND LANDED AT NEAREST AIRPORT. TECHNICIAN IDENTIFIED WHAT APPEARED TO BE A SHORTED LEAD ACID BATTERY. BATTERY WAS REPLACED AND NO DEFECTS NOTED AT THIS TIME. 1 G 7 2 3U H9SW 1999102900017 19991029 00017 SW 1999 10 29 99ZZZX4078 1 19990912 A 6510 407340339103 BEARING 407040303105 BELL 407 407 SW ALLSN 250C 250C47B GL TAIL ROTOR FAILED A A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 467AL 302 79 AFS1323 53190 CAE847287 DURING STRAIGHT AND LEVEL FLIGHT AT 3,700 FEET, TWO SHARP VIBRATIONS, EACH LASTING TWO SECONDS, APPROXIMATELY ONE SECOND APART WERE FELT IN THE AIRFRAME. A PRECAUTIONARY LANDING AT NEAREST PLATFORM WAS ACCOMPLISHED. DURING POST-FLIGHT INSP ECTION, NOTICED INDIVIDUAL BEARING BALLS FROM THE NR 2 DRIVE SHAFT HANGER BEARING WERE NO LONGER IN THE BEARING ASSEMBLY . NOTIFIED MAINTENANCE. UNCONTAINED FAILURE OF FORWARD BEARING ON THE NR 2 SHAFT AND BLOWER ASSEMBLY. 1 G 7 1 3U 3 U O H2SW E1GL 1999102900019 19991029 00019 SW 1999 10 29 99ZZZX4080 1 19990825 A 6510 407340340101 DISC PACK 407040302103 BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL 52 25 A1199 53284 DURING 25-HOUR AD INSPECTION, FOUND NR 7 COUPLING CRACKED, FIRST FORWARD DISC. 1 G 7 1 3U O H2SW 1999102900020 19991029 00020 NE 1999 10 29 P2EA99275 2 19990913 A 7200 ENGINE BOEING 737 7372T5 NM PWA JT8 JT8D15 52051 NE NR 1 BIRD STRIKE A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 CE 05 120NJ 22979 708303 MDW - FLT 815 - ABORTED TAKEOFF, NO EMERGENCY DECLARED, RETURNED TO BLOCKS. AT APPROXIMATELY 100 KNOTS DURING TAKEOFF R OLL, INGESTED BIRD IN NR 1 ENGINE. (X) 2 L 7 2 4F 4 F RT A16WE E2EA 1999102900021 19991029 00021 EA 1999 10 29 ASOA99095 1 19990907 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 820AS 7188 7188 DURING INSPECTION, CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMRGENCY CEILING LIGHTING SYSTEM BULB. OP ERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999102900022 19991029 00022 EA 1999 10 29 ASOA99097 1 19990909 A 3350 20131A EMERG BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 830AS 3073 7236 7236 DURING DAILY INSPECTION, FOUND EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PACK . OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999102900024 19991029 00024 NM 1999 10 29 99ZZZX4082 1 19990730 A 7920 MS9388124 O-RING BOEING 727 72723 1384004 NM NR 3 ENGINE WORN A NACA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 992AJ 19428 IN-FLIGHT, SHUT DOWN OF NR 3 ENGINE DUE TO LOW OIL PRESSURE/QUANTITY INDICATION. AIRCRAFT RETURNED TO KATL. MAINTENANC E REPLACED O-RING ON OIL LINE BANJO FITTING FORWARD OF STARTER. 2 L 7 3 4F A3WE 1999102900025 19991029 00025 SO 1999 10 29 SIMA992593 1 19990916 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145LR SO BAGGAGE COMPT FAILED A SIMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 21 620AE 05837 145102 GRR - FLT 3796 - BAGGAGE SMOKE WARNING CAME ON. DEPLOYED FIRE BOTTLE. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS IN THE AFT BAGGAGE COMPARTMENT. OPERATIONAL CHECK GOOD. REF: OPER CONTROL NR 99ZZZX4083. (X) 2 L 7 2 4T RT T00011AT 1999102900026 19991029 00026 SO 1999 10 29 99ZZZX4083 1 19990916 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145LR SO BAGGAGE COMPT FAILED A SIMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 21 620AE 05917 145102 GRR - FLT 3796 - BAGGAGE SMOKE WARNING CAME ON. DEPLOYED FIRE BOTTLE. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED FORWARD AND AFT SMOKE DETECTORS IN THE AFT BAGGAGE COMPARTMENT. OPERATIONAL CHECK GOOD. REF: OPER CONTROL NR SIMA992593. 2 L 7 2 4T RT T00011AT 1999102900027 19991029 00027 EU 1999 10 29 USAA991004 1 19990914 A 5220 D31865110 SKIN AIRBUS 320 A320214 EU SLIDE DOOR DISBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 103US 957 0861 DURING A-2 CHECK VISUAL INSPECTION, FOUND A 12 INCH BY 36 INCH DISBONDED AREA AT SLIDE DOOR COVERING OUTER SKIN AND LEFT A/C RT OFF WING SLIDE DOOR. REMOVED AND REPLACED SLIDE. (X) 2 L 7 2 4F RT A28NM 1999102900028 19991029 00028 EU 1999 10 29 USAASA99005 1 19990915 A 2560 60592101 SLIDE AIRBUS A319 A319112 EU RT EMERG EXIT LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 0997 PHL - THE 'EMERG R' MESSAGE APPEARED ON THE CIDS DURING THE OVERNIGHT MAINTENANCE CHECK. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY SLIDE PRESSURE BOTTLE. (X) 2 L 7 2 4F RT A28NM 1999102900029 19991029 00029 WP 1999 10 29 IXXA9900025 1 19991021 A 3310 BALLAST DOUG DC8 DC871F 302199D WP COCKPIT ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 829BX 45994 EN ROUTE FROM TOL TO LAX, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT. THE FLIGHT CREW EXTINGISHED THE OVERHEAD FLUOR ESCENT LIGHTING SYSTM AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPEC TED THE LIGHTING SYSTEM CIRCUITRY AND BALLAST ASSEMBLY WITH NO DISCREPANCIES NOTED. MAINTENANCE PERFORMED AN OPERATIONA L TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL WITH NO DISCREPANCIES NOTED. 2 L 7 4 4F RT 4A25 1999102900030 19991029 00030 NM 1999 10 29 AWXA9900366 1 19991015 A 5320 6548654 ANGLE BOEING 737 7373G7 1384595 NM BS 540 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 C-CHECK, CRACKED ANGLE AT STA 540L, LT A/C BAY AT END OF DRAG ANGLE. REMOVED CRACKED ANGLE IAW SRM 51-40-02, FABBED REP AIR ANGLE FROM 2024T3 .063 QQA 250/13 R682091 IAW SRM 53-30-71. TREATED AND PRIMED ANGLE IAW SRM 51-20-01. 2 L 7 2 4F RT A16WE 1999102900031 19991029 00031 NM 1999 10 29 AWXA9900367 1 19991015 A 5315 69389337 FITTING BOEING 737 7373G7 1384595 NM BS 730 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 C-CHECK, MAIN CABIN CENTERLINE FLOORBEAM, LT VERTICAL STIFFENER ATTACHED TO FLOORBEAM AT BS 727 CRACKS MIGRATING FROM FA STENERS. REMOVED AFT CARGO FWD PNL FOR ACCESS IAW SRM 51-30-2. REMOVED FITTING AND INSTALLED NEW FITTING PER SRM 51-30 -2. REINSTALLED ACCESS PNL IAW 25-52-81. 2 L 7 2 4F RT A16WE 1999102900032 19991029 00032 NM 1999 10 29 AWXA9900368 1 19990922 A 5320 6552878U97 SILL BOEING 737 7373G7 1384595 NM BS 986.5 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 C-CHECK, CORROSION ON MOP SILL L-2 DOOR BS 986.5. REMOVED AND REPLACED MOP SILL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999102900033 19991029 00033 NM 1999 10 29 AWXA9900369 1 19990922 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 C-CHECK, CORROSION ON FLOORBEAM AT FUSELAGE STA 967 LBL 24 TO 56. REMOVED DAMAGED SECTION OF UPPER CHORD, FABRICATED RE PAIR PARTS OF 1505-100617 7070T. TREATED AND PRIMED IAW SRM 51-20-01 AND INSTALLED REPAIR PER SRM 53-00-51, 53-60-51. 2 L 7 2 4F RT A16WE 1999102900034 19991029 00034 NM 1999 10 29 AWXA9900370 1 19991019 A 2751 1817389 TRANSMITTER BOEING 737 7373G7 1384595 NM LT TE FLAP FAILED A AWXA B EMER. DESCENT F FLT CONT AFFECTED AP APPROACH 1 WP 28 302AW 39292 15310 24009 EMERGENCY DECLARED, ON APPROACH AN ASYMMETRICAL TRAILING EDGE PROBLEM OCCURRED. THE LEFT FLAP STUCK AT 7-8 DEG WHILE TH E RT FLAP STUCK AT 10 DEG--SLATS WERE AT FULL EXTEND. REMOVED AND REPLACED LEFT FLAP POS TRANSMITTER, OPS CK NORMAL. T T 0097274. THREE FLAP SPLIT WRITE-UPS IN LAST 90 DAYS, THIS IS FIRST LT X-MITTER CHANGE. 2 L 7 2 4F RT A16WE 1999102900035 19991029 00035 EU 1999 10 29 AWXA9900371 1 19991019 A 3397 BMS13131122 WIRE AIRBUS 320 A320231 3930325 EU ROW 19ABC SHORTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 FIVE AISLE AND ONE COVE EMERGENCY EXIT LIGHTS OUT. FOUND SHORTED WIRE AT SEAT 19 ABC. REPAIRED WIRE, OPS CK GOOD. 2 L 7 2 4F RT A28NM 1999102900036 19991029 00036 NM 1999 10 29 AWXA9900372 1 19991020 A 2121 10605471 FAN BOEING 737 737112 1384412 NM EQUIP BAY FAILED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 708AW 21084 576 19771 BURNT ODOR DURING INITIAL CLIMB, NOTICED 2X IT GOES AWAY AFTER 5 MINUTES. FOUND POPPED C/B ON NORMAL EQUIPMENT COOLING FAN. REMOVED AND REPLACED FAN, OPS CK NORMAL. FAN WAS REPLACED 07/27/99 FOR BREAKERS W/N SET. 2 L 7 2 4F A16WE 1999102900037 19991029 00037 SO 1999 10 29 RAAA99E4012 1 19990509 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 521 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM CORRODED AT FS 521 LBL 28 TO LBL 55 TOP FLANGE. REPLACED FLOORB EAM AS PER SRM 51-2-9. INSTALLED AS PER SRM 51-2-12 M-54. 2 L 7 4 4T 4A22 1999102900038 19991029 00038 SO 1999 10 29 RAAA99E4013 1 19990509 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 540 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANVERSE FLOORBEAM CORRODED AT FS 540 LBL 27 TO LBL 55 TOP FLANGE. REPLACED FLOORBE AM PER SRM 51-2-9. INSTALLED FLOORBEAM PER SRM 51-2-12 M-54. 2 L 7 4 4T 4A22 1999102900039 19991029 00039 SO 1999 10 29 RAAA99E4014 1 19990509 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 571 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM CORRODED AT FS 571 LBL 26 TO LBL 45 TOP FLANGE. REPLACED FLOORB EAM PER SRM 51-2-9. INSTALLED PER SRM 51-2-12 M-54. 2 L 7 4 4T 4A22 1999102900040 19991029 00040 SO 1999 10 29 RAAA99E4015 1 19990509 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 445 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM CORRODED AT FS 445 FROM LBL 27 TO LBL 55 ON TOP FLANGE. REPAIRED PER SRM 53-2-4, M-54. 2 L 7 4 4T 4A22 1999102900041 19991029 00041 SO 1999 10 29 RAAA99E4016 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 445-450 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT FS 445-450 LBL 55. REPAIRED AS PER ECO 99-05 M-54. 2 L 7 4 4T 4A22 1999102900042 19991029 00042 SO 1999 10 29 RAAA99E4017 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 571-695 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK ACCESS FOR A/D 67-11-04, FOUND LOCK LUGS CHIPPED AND WORN IN SEAT TRACK AT FS 571-695 RBL 54 . REPLACED SEAT TRACK PER ECO 99-05 M-54. 2 L 7 4 4T 4A22 1999102900043 19991029 00043 SO 1999 10 29 RAAA99E4018 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 571-695 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK ACCESS FOR A/D 67-11-04, FOUND LOCK LUGS CHIPPED AND WORN IN SEAT TRACK AT FS 572-695 RBL 42 . REPLACED SEAT TRACK PER ECO 99-05,M-54 NR 119. 2 L 7 4 4T 4A22 1999102900044 19991029 00044 SO 1999 10 29 RAAA99E4019 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 571-695 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK ACCESS FOR A/D 67-11-04, FOUND LOCK LUGS CHIPPED AND WORN IN SEAT TRACK AT FS 571-695 BL 0. REPLACED SEAT TRACK AS -PER ECO 99-05, M-54 NR 120. 2 L 7 4 4T 4A22 1999102900045 19991029 00045 SO 1999 10 29 RAAA99E4020 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 571-695 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK ACCESS FOR A/D 67-11-04, FOUND SEAT TRACK LOCK LUGS CHIPPED AND CORRODED AT FS 571-695 LBL 2 3. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 121. 2 L 7 4 4T 4A22 1999102900046 19991029 00046 SO 1999 10 29 RAAA99E4021 1 19990509 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 571-695 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK ACCESS A/D 67-11-04, FOUND SEAT TRACK LOCK LUGS CHIPPED AND CORRODED AT FS 571-695 LBL 54. R EPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 122. 2 L 7 4 4T 4A22 1999102900047 19991029 00047 SO 1999 10 29 RAAA99E4022 1 19990510 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 613-620 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT FS 613-620 LBL 26. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 124. 2 L 7 4 4T 4A22 1999102900048 19991029 00048 NM 1999 10 29 CALA9901403 1 19991019 A 3231 3910027103 SELECT VLV BOEING 777 777224 1385225 NM MLG DOOR INOP A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 78009 29479 A POP WAS HEARD WHILE ON APPROACH TO EWR AT 4,000 FEET. THE GEAR WAS LOWERED, BUT THE GEAR DOOR REMAINED OPEN. THE AIR CRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MLG SELECTOR /BYPASS VALVE IAW MM 32-31-03, PAGE 401. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00001SE 1999102900049 19991029 00049 WP 1999 10 29 CALA9901404 1 19991018 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 731 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND AN 8 INCH CRACK IN FLOORBOARD SUPPORT AT FS 731, LBL 10 - LBL 18. THE SUPPORT WAS REMOVED AND A NEW SU PPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1999102900050 19991029 00050 WP 1999 10 29 CALA9901405 1 19991018 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM FITTING AT FS 1338, RBL 54. THE FITTING WAS REMOVED AND A NEW FITTING WA S INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1999102900051 19991029 00051 WP 1999 10 29 CALA9901406 1 19991018 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 427-446 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT CORRODED AT BETWEEN STA 427 AND 446, LONGERON 28R. THE FLOOR SUPPORT WAS R EMOVED AND REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999102900052 19991029 00052 WP 1999 10 29 CALA9901407 1 19991018 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 540, LONGERON 27L-27R AND STA 541, LONGERON 28L - 28R. THE FLOOR SUPPORT S WERE REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999102900053 19991029 00053 WP 1999 10 29 CALA9901408 1 19991018 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 427 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT BRACKET AT FS 427, STRINGER 28R. THE FLOOR SUPPORT BRACKET WAS REMOVED AND A NEW FLOOR SUPPORT BRACKET WAS INSTALLED IAW SRM 51-30-5, 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999102900054 19991029 00054 WP 1999 10 29 CALA9901409 1 19991018 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 598 & 636 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 636 AND 598 FROM LONGERON 28L TO L28R. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-1, 51-30-4, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1999102900055 19991029 00055 WP 1999 10 29 CALA9901410 1 19991018 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 540-784 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND TRACK CORRODED AT STA 540-784, LBL 24. THE TRACK WAS REMOVED AND A NEW TRACK AND SPLICES WERE INSTALLE D IAW SRM 51-10-4 AND 53-05, FIGURE 46. 2 L 7 2 4F A6WE 1999102900056 19991029 00056 WP 1999 10 29 CALA9901411 1 19991018 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 786 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND MID CARGO PIT TIE DOWN TRACK ON RT SIDE AFT OF CARGO DOOR TO THE AFT END OF THE CARGO PIT CORRODED AT F S 786, RBL 24. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-30-3. 2 L 7 2 4F A6WE 1999102900057 19991029 00057 WP 1999 10 29 CALA9901412 1 19991018 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 541-617 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND THE RIGHT O/B SEAT TRACK CORRODED AT FS 541-617, RBL 54.5. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-30-5, AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999102900058 19991029 00058 WP 1999 10 29 CALA9901413 1 19991018 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP BS 775-795 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND LONGERON AND SKIN CORRODED AT STA 775-795, LONGERONS 27L - 28L. THE SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 53. LONGERON 28L AND A FLOOR ANGLE SUPPORT WERE REMOVED AND REPLACED IAW SRM 53-02, FIG URE 17. 2 L 7 2 4F A6WE 1999102900059 19991029 00059 WP 1999 10 29 CALA9901414 1 19991018 A 5230 ANGLE DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A .75 INCH CRACK IN AFT CARGO DOOR FORWARD VERTICAL LOWER RIB TO SKIN ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE AND FITTING WERE INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2. 2 L 7 2 4F A6WE 1999102900060 19991029 00060 WP 1999 10 29 CALA9901415 1 19991018 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1136-1150 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 2 INCH CRACK IN FLOOR SUPPORT AT STA 1136, LONGERON 27R AND A 4 INCH CRACK IN FLOOR SUPPORT AT STA 11 50, LONGERON 27R-26R. THE FLOOR SUPPORTS WERE REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-3. 2 L 7 2 4F A6WE 1999102900061 19991029 00061 WP 1999 10 29 CALA9901416 1 19991018 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1250 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 6 INCH CRACK IN FLOOR SUPPORT AT STA 1250, LONGERON 28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999102900062 19991029 00062 1999 10 29 QXEA9902127 4 19991018 A 3442 RT UNIT ALLIED SIGNA 20671570153 FOKKER F28 F28MK4000 4990810 EU RADAR SYS FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 498US 11181 HLN - ELECTRICAL SMOKE COMING FROM RADIO RACK, TOP LEFT AREA. REMOVED AND REPLACED RADAR RECEIVER TRANSMITTER, OPERATIO NAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999102900063 19991029 00063 WP 1999 10 29 99FDEA00436 1 19991019 A 5270 WARNING DOUG DC10 DC1030F 3023504 WP AC DOOR ACTIVATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 309FE 48298 AIR COND DOOR LIGHT ON S/O PNL ILLUM IN FLT DURING CLIMB. VERIFIED AND RECORDED IN AML. AC DOORS ARE CLOSED BY VISUAL INSP PRIOR TO EACH DEPARTURE. 2 L 7 3 4F RT A22WE 1999102900064 19991029 00064 WP 1999 10 29 99FDEA00437 1 19990714 A 2150 ACM70281 BEARING DOUG DC10 DC1010 3022110 WP RAM AIR VALVE FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 395FE 46629 DURING D-CK INSP, FOUND VALVE ASSY EXHAUST, RAM AIR BEARING (P/N DT16A) DAMAGED. DURING BEARING REMOVAL I/B FLANGE WERE DAMAGED. FLANGE REPAIRED INSTALLING BUSHING IAW FEDEX EA NR 8-2160-45652. 2 L 7 3 4F A22WE 1999102900065 19991029 00065 WP 1999 10 29 99FDEA00438 1 19990416 A 5330 ADA30241 DOUBLER DOUG DC10 DC1010 3022110 WP CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 395FE 46629 DURING A/C P-F CONV AT AERONAVALI, INSP FOUND SEV DENTS AFFECTING THE FWD CARGO DOOR DOUBLER AT Y=996 BETWEEN LONGERONS 45R-46R. REMOVED AND REPLACED SECTION OF DOUBLER (P/N ADA3024-1) AND INSTALLED SPLICE IAW FEDEX EA 8-5333-45543. 2 L 7 3 4F A22WE 1999102900066 19991029 00066 WP 1999 10 29 MWEA99704 1 19991021 A 5320 9913440512 BRACKET DOUG DC9 DC932 3022066 WP RT< MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LEFT AND RIGHT MAIN WHEEL WELL, OUTBOARD FORWARD AREA, THE ANGLE JUST OUTBOARD F/O SKI FITTING (BOZIKICHY BRACKET) IS CR ACKED. MTC FABRICATED AND INSTALLED NEW ANGLES FOR LEFT AND RIGHT WHEEL WELLS. 2 L 7 2 4F A6WE 1999102900067 19991029 00067 WP 1999 10 29 MWEA99705 1 19991021 A 5712 99581014 RIB DOUG DC9 DC932 3022066 WP RT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FIRST AND SECOND RIB OF THE RIGHT HAND WING TRAILING EDGE, INBOARD OF THE END CAP AND CHANNEL, DAMAGED. MTC REMOVED AND REPLACED FIRST AND SECOND RIB AS REQUIRED. 2 L 7 2 4F A6WE 1999102900068 19991029 00068 WP 1999 10 29 MWEA99706 1 19991021 A 5712 99530104 RIB DOUG DC9 DC932 3022066 WP RT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT HAND TRAILING EDGE PANEL, AND RIB CAP DAMAGED ON OUTBOARD FLAP. MTC REMOVED AND REINSTALLED RIB. 2 L 7 2 4F A6WE 1999102900069 19991029 00069 WP 1999 10 29 MWEA99707 1 19991021 A 5730 99575766 SKIN DOUG DC9 DC932 3022066 WP RT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 RIGHT HAND FLAP OUTBOARD REMOVABLE TRAILING EDGE PANEL LOWER SKIN DAMAGED. MTC REMOVED AND REPLACED SKIN. 2 L 7 2 4F A6WE 1999102900070 19991029 00070 WP 1999 10 29 MWEA99708 1 19991019 A 3350 110049 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 600ME 45725 FORWARD FLOOR TRACK LIGHTS WERE DIM. MTC REMOVED AND REPLACED EMERGENCY FLOOR BATTERY PACK. 2 L 7 2 4F A6WE 1999102900071 19991029 00071 WP 1999 10 29 MWEA99709 1 19991021 A 5530 59121753 FAIRING DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LEFT HAND HORIZONTAL VERTICAL STAB FAIRING CHAFING AT AFT VERTICAL SKIN. MTC FABRICATED AND INSTALLED NEW DOUBLER ON VE RTICAL STAB. 2 L 7 2 4F A6WE 1999102900072 19991029 00072 WP 1999 10 29 MWEA99710 1 19991021 A 5230 39132492 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FITTING IS CRACKED AT THE AFT END BEAM NR 5 FORWARD CARGO DOOR. MTC LOCATED AND DRILLED NEW FITTINGS. NEW FITTINGS WER E INSTALLED ON BEAM NR 5. 2 L 7 2 4F A6WE 1999102900073 19991029 00073 WP 1999 10 29 MWEA99711 1 19991021 A 5313 39146771 LONGERON DOUG DC9 DC932 3022066 WP BS 800 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT CARGO COMP STATION 800 LONGERON 30 SPLICE IS CRACKED. MTC FABRICATED AND INSTALLED NEW SPLICE AT STATION 800, LONGE RON 30. 2 L 7 2 4F A6WE 1999102900074 19991029 00074 WP 1999 10 29 MWEA99712 1 19991021 A 5230 591014167 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO DOOR OUTER PAN IS CHAFED AT TOP AFT CORNER AROUND DOOR STOP PLATE. MTC FABRICATED AND INSTALLED CARGO DOO R OUTER PAN DOUBLER. 2 L 7 2 4F A6WE 1999102900075 19991029 00075 WP 1999 10 29 MWEA99713 1 19991021 A 5230 59101417 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO DOOR IS CRACKED AT FWD LOCKING CAM OUTER BEARING AREA. MTC FABRICATED AND INSTALLED DOUBLER ON CARGO DOOR INNER PAN. 2 L 7 2 4F A6WE 1999102900076 19991029 00076 WP 1999 10 29 MWEA99714 1 19991015 A 5313 591142345 LONGERON DOUG DC9 DC932 3022066 WP BS 935 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT CARGO COMPARTMENT AT STATION 935, LONGERON 22, LEFT HAND HAS CORROSION AROUND FASTENERS. MTC DRILLED AND REPLACED N EW LONGERON AT STATION 935. 2 L 7 2 4F A6WE 1999102900077 19991029 00077 NM 1999 10 29 DHL99715001 1 19991015 A 5230 HINGE BOEING 727 727155C 138404Z NM CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 MAIN CARGO DOOR HINGE ACTUATORS ATTACH POINT HOLES ELONGATED. FABRICATED AND REPAIRED HOLES AND PARTS PER TIMCO EO W000 01 REV C AND BOEING SRM 51-10-7. 2 L 7 3 4F A3WE 1999102900078 19991029 00078 1999 10 29 DHL99804007 4 19991016 A 3422 25883025 DIR GYRO DOUG DC8 DC873F 302199F WP NR 1 FAILED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 804DH 46124 F/O COMPASS DRIFTS (HSI) EXCESS + - 30 DEGREES OR MORE. REPLACED NR 1 DG PER MM 34-21-1, SYSTEM CHECKED GOOD. 2 L 7 4 4F RT 4A25 1999102900079 19991029 00079 WP 1999 10 29 RRXA991522 1 19991012 A 7110 COWL DOUG DC8 DC863 302198A WP NR 1 ENGINE SEPARATED A RRXA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 WP 15 796AL 46054 ON POST FLIGHT, NOTED NR 1 ENGINE COWLINGS MISSING AND DAMAGE TO UNDERSIDE OF WING. REPAIRED PYLON IAW COTNEY EA NR EAJ 47-1, REPAIRED WING IAW EAJ47-1. 2 L 7 4 4F 4A25 1999102900080 19991029 00080 EU 1999 10 29 RAIA9910026 1 19991019 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 343TE 1575 1575 955 66271 STL- RIGHT ENGINE RPM GAUGE INOP. MAINTENANCE REPLACED TACH GENERATOR ON RIGHT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999102900081 19991029 00081 1999 10 29 RAIA9910028 4 19991020 A 3425 H6201QAC02 AHRS EMB 145 EMB145 SO RT COCKPIT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 806HK 145112 JFK- F/O'S AHRS FAIL. MAINTENANCE REPLACED F/O'S AHRS COMPUTER. 2 L 7 2 4F RT T00011AT 1999102900082 19991029 00082 SO 1999 10 29 COMA9910164 1 19991019 A 5320 12005805003 BUTT STRAP EMB 120 EMB120 3260201 SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 5568 120262 WHILE PERFORMING MAINTENANCE ON THE FLIGHT CONTROL CABLES, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER FORWARD BUTT-STRA P WAS FOUND TO BE CORRODED. THE BUTT-STRAP WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES. AIRCRAFT RETURNED TO SERVICE. THIS SAME PART WAS PREVIOUSLY REPLACED ON 5-15-97, FOR CORROSION. 2 L 7 2 4T RT A31SO 1999102900083 19991029 00083 SO 1999 10 29 COMA9910165 1 19991015 A 3610 97962641 BLEED VALVE EMB 120 EMB120RT SO ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 256CA 25938 1245 DURING CLIMB-OUT OF MCO, THE CROSS BLEED VALVE WOULD NOT CLOSE. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE CROSS BLE ED VALVE. 2 L 7 2 4T RT A31SO 1999102900084 19991029 00084 EA 1999 10 29 COMA9960617 1 19991019 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 MISDRILLED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 932CA 7038 HOLES WERE INCORRECTLY LOCATED IN ANGLE AT FS 280 AND ORIGINAL PLATE FASTENER HOLES WILL NOT ALIGN. FABRICATED AND INST ALLED NEW PLATE IAW WVAC EO 601R-53-0458. 2 L 7 2 4F RT A21EA 1999102900085 19991029 00085 EA 1999 10 29 COMA9960618 1 19991019 A 5320 CLIP CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 ANGLE CLIP INSIDE OF LBL 1 FOUND CRACKED (FOUND WHILE ACCOMPLISHING REPAIR FOR FLOORBEAM WEB). REMOVING CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW WVAC EO 601R-53-0446A. 2 L 7 2 4F RT A21EA 1999102900086 19991029 00086 EA 1999 10 29 COMA9960619 1 19991021 A 5320 601R35031237 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 995CA 3945 7229 RT SIDE FS 621 FLOOR SUPPORT ANGLE IN BAGGAGE BAY IS CRACKED. REPAIRED RT SIDE FS 621 FLOOR SUPPORT ANGLE IAW CANADAIR REO 601R53-61-117REVA. 2 L 7 2 4F RT A21EA 1999102900087 19991029 00087 EA 1999 10 29 COMA9960620 1 19991020 A 5320 601R5361193 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 995CA 3945 7229 DOUBLERS CRACKED AT FS 718.00 STRG 11 LT AND RT SIDES. REMOVED AND REPLACED CRACKED DOUBLERS IAW WVAC EO 601R-53-0468. 2 L 7 2 4F RT A21EA 1999102900088 19991029 00088 EA 1999 10 29 COMA9960623 1 19991019 A 5320 601R31148127 INTERCOSTAL CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 INTERCOSTAL WEBBING AT FS 349-RBL42 IS CORRODED P/N 601R31148-127. PERFORMED A MAJOR REPAIR. REMOVED CORROSION ON INTE RCOSTAL WEBBING AT FS 349 REF WVAC EO NR 601R-53-0445. 2 L 7 2 4F RT A21EA 1999102900089 19991029 00089 EA 1999 10 29 COMA9960624 1 19991019 A 5240 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 THE THRESHOLD ANGLE AT THE SERVICE DOOR IS SEVERELY CORRODED. PERFORMED A MAJOR REPAIR BY REMOVING THE DAMAGED ANGLE AN D INSTALLING A NEW PART 601R38303-105 IAW WVAC EO 601R-53-0415A. 2 L 7 2 4F RT A21EA 1999102900090 19991029 00090 EA 1999 10 29 COMA9960625 1 19991019 A 5310 SILL CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 THE FLOOR SILL AFT OF THE SERVICE DOOR (AFT FS 349) IS CORRODED. REPAIRED FLOOR SILL AFT OF FS 349 BY REMOVING FLOOR SI LL, REMOVING CORROSION. ALODINE, PRIME, AND EPOXY TOP COAT, REMOVED SILL, AND REINSTALLING SAME SERVICEABLE SILL IAW WV AC EO 601R-53-0445. 2 L 7 2 4F RT A21EA 1999102900091 19991029 00091 EA 1999 10 29 COMA9960626 1 19991019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 CENTER SECTION OF FLOORBEAM STRUCTURE AT FS 280 HAS CORROSION AT FRONT AND AFT ANGLES OF THE FLOOR FRAME WEB. PERFORMED A MAJOR REPAIR OF THE FLOOR FRAME WEB FRONT AND AFT ANGLES AT FS 280 BY CUTTING OUT DAMAGED AREAS AND SPLICING IN NEW S ECTIONS IAW WVAC EO 601R-53-0436A. 2 L 7 2 4F RT A21EA 1999102900092 19991029 00092 EA 1999 10 29 COMA9960627 1 19991005 A 5315 601R530000 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 - 409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 FLOOR SUPPORT BEAM CAP RBL9 AND RBL27 HAS CORROSION FROM FS 280.00 TO FS 349.0 0 AND FS 280 AND 409.00 P/NS 601R31113-67 . PERFORMED A MAJOR REPAIR TO FLOOR SUPPORT BEAM CAPS RBL9 AND RBL27. SPLICED IN NEW FLOORBEAMS P/N 601R31113-67 IAW R EO NO 601R-53-00-027. 2 L 7 2 4F RT A21EA 1999102900093 19991029 00093 EA 1999 10 29 COMA9960628 1 19991005 A 5315 601R5300027 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 FLOORBEAM CAP LBL 9 AND LBL 27 HAS CORROSION FROM FS 280 AND FS 409 AND FS 333.0 TO FS 349.00 AND 16 P/N 601R31113-67. PERFORMED A MAJOR REPAIR TO FLOORBEAM CAPS LBL 9 AND LBL 27. SPLICED IN NEW FLOOR BEAMS P/N 601R31113-67 IAW REO NO 601 R-53-00-029. 2 L 7 2 4F RT A21EA 1999102900094 19991029 00094 EA 1999 10 29 COMA9960629 1 19991005 A 5240 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 SERVICE DOOR FLOOR SUPPORT L ANGLE CORRODED BEYOND LIMITS P/N 601R38303-105. PERFORMED A MAJOR REPAIR, REMOVED AND INST ALLED A NEW THRESHOLD ANGLE (PART NUMBER 601R38303-239) IAW WVAC EO 601R-53-0391A. 2 L 7 2 4F RT A21EA 1999102900095 19991029 00095 EA 1999 10 29 COMA9960630 1 19991016 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 116 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 CRACK DETECTED IN THE LOWER HORIZONTAL SURFACE OF RT LOWER WING ACCESS HOLE AT 640EB. BLENDED OUT DAMAGE AREA, ROTO-PEE NED ALODINED IAW BOMBARDIER REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999102900096 19991029 00096 EA 1999 10 29 COMA9960631 1 19991016 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 116 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 CRACK DETECTED IN THE LOWER HORIZONTAL SURFACE OF LT LOWER WING ACCESS HOLE AT 540EB. BLENDED OUT DAMAGED AREA, ROTO-PE ENED AND ALODINED IAW BOMBARDIER REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999102900097 19991029 00097 EA 1999 10 29 COMA9960632 1 19991016 A 5730 601R10045 SKIIN CNDAIR CL600 CL6002B19 EA WS 54 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 943CA 7062 2 CRACKS DETECTED IN THE LOWER HORIZONTAL SURFACE LT LOWER WING ACCESS HOLE AT 540AB. BLENDED OUT DAMAGED AREAS, ROTO-P EENED, ALODINED IAW BOMBARDIER REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999102900098 19991029 00098 EA 1999 10 29 COMA9960633 1 19991014 A 5330 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA BS 310 - 319 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 DOUBLER PLATE BETWEEN FS 310-319, RT SIDE FORWARD OF SERVICE DOOR IS CORRODED. REMOVED DOUBLER PLATE BETWEEN FS 310-319 RT SIDE FORWARD OF SERVICE DOOR P/N 601R-38669-49. INSTALLED NEW DOUBLER PLATES FWD OF DOOR IAW WVAC EO NR 601R-53-043 3. 2 L 7 2 4F RT A21EA 1999102900099 19991029 00099 EA 1999 10 29 COMA9960634 1 19991014 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 - 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 FOUND CORROSION ON FLOOR CAPS LBL27, LBL9, RBL9, RBL27, FS280 TO FS349 AND FS310 TO FS349. PERFORMED MAJOR REPAIR REMOV ED AND REPLACED FLOORBEAMS P/N 601R31113-67 IAW REO 601R-53-00-027, WVAC EO 601R-53-0414A AND WVAC EO 601R-53-0419A. 2 L 7 2 4F RT A21EA 1999102900100 19991029 00100 EA 1999 10 29 COMA9960635 1 19991014 A 5320 601R3111357 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 ANGLE ON INBOARD AND OUTBOARD SIDE LBL9 AT FS 280 IS CRACKED P/N 601R31113-57. PERFORMED A MAJOR REPAIR REMOVED DAMAGED CLIPS FABRICATED AND INSTALLED NEW CLIPS IAW WVAC EO 601R-53-041. 2 L 7 2 4F RT A21EA 1999102900101 19991029 00101 EA 1999 10 29 COMA9960636 1 19991015 A 5320 601R3527221 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 FAX DOOR ENTRANCE FLOOR SUPPORT ANGLE HAS CORROSION. PERFORMED A MAJOR REPAIR. REMOVED FLOOR SUPPORT ANGLE P/N 601R315 27-46 AND P/N 601R31527-221 IAW EO 601R-53-0424A. 2 L 7 2 4F RT A21EA 1999102900102 19991029 00102 EA 1999 10 29 COMA9960637 1 19991007 A 5320 601R31527179 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 ANGLE AT PAX DOOR ENTRANCE CORRODED P/N 601R31527-179. PERFORMED A MAJOR REPAIR. REMOVED DAMAGED ANGLE AND INSTALLED A NEW FABRICATED ANGLE IAW WVAC EO NO 601R-53-0399A. 2 L 7 2 4F RT A21EA 1999102900103 19991029 00103 EA 1999 10 29 COMA9960638 1 19991008 A 5320 601R31527131 BRACKET CNDAIR CL600 CL6002B19 EA DOOR SILL DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 THE CLEAT ON THE BRACKET AT THE PASSENGER DOOR THRESHOLD WAS DAMAGED. PERFORMED A MAJOR REPAIR REMOVED THE DAMAGED CLEA T FABRICATED AND INSTALLED A NEW CLEAT IAW WVAC EO 601R-53-0403. 2 L 7 2 4F RT A21EA 1999102900104 19991029 00104 EA 1999 10 29 COMA9960639 1 19991017 A 5330 SKIN CNDAIR CL600 CL6002B19 EA BS 349 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 7794 7041 FUSELAGE SKIN AT 349.0, STR 16 LT DAMAGED BY PAX DOOR PIN. REPAIRED FUSELAGE SKIN AT FS 349.0, IAW CANADAIR REO 601R-53 -21-186. 2 L 7 2 4F RT A21EA 1999102900105 19991029 00105 EA 1999 10 29 COMA9960640 1 19991010 A 5320 601R38303253 ANGLE CNDAIR CL600 CL6002B19 EA BS 319 - 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 14877 7026 SERVICE DOOR THRESHOLD ANGLE P/N 601R38303-253 IS SEVERELY CORRODED. PERFORMED A MAJOR REPAIR BY FABRICATING AND INSTAL LING SERVICE DOOR THRESHOLD ANGLE IAW WVAC EO 601R-53-0406B. 2 L 7 2 4F RT A21EA 1999102900106 19991029 00106 EA 1999 10 29 COMA9960641 1 19991020 A 2750 854D100MD101 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAP FAILED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 945CA 6521 7069 FLAP FAIL CAUTION WARNING ACTIVATED DURING DESCENT INTO CVG. REPLACED THE RIGHT OUTER FLAP INBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 1999102900107 19991029 00107 EA 1999 10 29 COMA9960642 1 19991020 A 2750 853D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAP FAILED A COMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 945CA 511 7069 FLAP FAIL CAUTION WARNING ACTIVATED DURING DESCENT INTO CVG. REPLACED THE RIGHT OUTBOARD OUTER FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 1999102900108 19991029 00108 EA 1999 10 29 COMA9960643 1 19991020 A 2750 852D100MD91 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAP FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 960CA 8802 7117 FLAP FAIL CAUTION WARNING ACTIVATED DURING APPROACH INTO CVG. REPLACED THE INBOARD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 1999102900109 19991029 00109 NM 1999 10 29 SWAA991739 1 19991019 A 2612 899315 FIRE DETECTOR BOEING 737 7373H4 1384600 NM E/E BAY ERRATIC A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 639SW 27712 ABORTED TAKEOFF, NR 2 ENG OVERHEAT LIGHT ILLUMINATED, REDUCED THRUST TO IDLE AND LIGHT EXTINGUISHED. REMOVED AND REPLAC ED P-8 FIRE CONTROL PANEL AND FIRE DETECTOR UNIT PER MM. 2 L 7 2 4F RT A16WE 1999102900110 19991029 00110 NM 1999 10 29 SWAA991740 1 19991019 A 2731 BACB28AM06B BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SW 07 388SW 26591 AIR TURNBACK, AIRFRAME VIBRATION DURING CLIMB. VIBRATION GREATER AT HIGHER SPEEDS. REMOVED AND REPLACED RT ELEVATOR OU TBOARD TAB HINGE BUSHINGS AND LT ELEVATOR INBOARD TAB HINGE BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 1999102900111 19991029 00111 1999 10 29 SWAA991741 4 19991019 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM AFT ENTRY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED C CHECK, FOUND AFT ENTRY DOOR SLIDE GIRT BAR CABLE OUT OF POSITION. REROUTED SLIDE CABLE PER MM. 2 L 7 2 4F A16WE 1999102900112 19991029 00112 NM 1999 10 29 SWAA991742 1 19991019 A 5753 6546435273 SKIN BOEING 737 7373H4 1384600 NM LT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD FLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900113 19991029 00113 NM 1999 10 29 SWAA991743 1 19991019 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROWS 23/24 INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROWS 23 AND 24. REPAIRED LIGHT WIRES PER MM. 2 L 7 2 4F RT A16WE 1999102900114 19991029 00114 NM 1999 10 29 SWAA991744 1 19991019 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND BS 328 FLOORBEAM CORRODED ON UPPER FACE. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999102900115 19991029 00115 NM 1999 10 29 SWAA991745 1 19991019 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND BS 967 FLOORBEAM CORRODED ON UPPER AND LOWER FACES, RBL 27. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999102900116 19991029 00116 NM 1999 10 29 SWAA991746 1 19991020 A 2751 BACC18AD2 WIRE BOEING 737 7377H4 1384404 NM LT MLG WW CHAFED A SWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 745SW 29491 ABORTED TAKEOFF, 80 KNOTS DURING TAKEOFF, WARNING HORN SOUNDED. FOUND CHAFING WIRES TO NR 4 SKEW SENSOR CONNECTOR IN LT WHEEL WELL. REPAIRED WIRES PER WDM. 2 L 7 2 4F RT A16WE 1999102900117 19991029 00117 NM 1999 10 29 SWAA991747 1 19991020 A 5220 144A6500 SENSOR BOEING 737 7377H4 NM EMERGENCY EXIT ACTIVATED A SWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 745SW 29491 ABORTED TAKEOFF, PSEU LIGHT ILLUMINATED WHEN FLAP EXTENDED AND THRUST POWER APPLIED. C/W BITE CK, FAULT INFO SHOWED OVE RWING DOORS DISAGREE PROBLEM. CYCLED BOTH OVERWING DOORS AND C/W FIM TASK. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999102900118 19991029 00118 NM 1999 10 29 SWAA991748 1 19991020 A 5311 6545807 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR UPPER FUSELAGE CUT OUT STUB FRAME CRACKED. REPAIRED FRAME PER SWA RA NR 1-353-2169. 2 L 7 2 4F RT A16WE 1999102900120 19991029 00120 NE 1999 10 29 SWAA991732 2 19991018 A 7230 9527M99P08 BLADES BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE SHINGLED A SWAA D RETURN TO BLOCK E VIBRATION/BUFFET CL CLIMB 1 SW 07 371SW 26598 720244 AIR TURNBACK, DURING CLIMB NR 2 ENG INGESTED BIRD. VIBRATION DEVELOPED IN ENG. C/W BIRD STRIKE INSP, BORESCOPE INSP. N O DAMAGED NOTED EXCEPT FOR NR 2 AND NR 27 FAN BLADES WHICH WERE SHINGLED. UNSHINGLED FAN BLADES PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102900121 19991029 00121 NM 1999 10 29 SWAA991733 1 19991018 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 717SA 27851 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP NEAR OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900122 19991029 00122 NM 1999 10 29 SWAA991734 1 19991018 A 3350 100067 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999102900123 19991029 00123 NM 1999 10 29 SWAA991735 1 19991018 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F A16WE 1999102900124 19991029 00124 NM 1999 10 29 SWAA991736 1 19991018 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED RON, FOUND EEPLS FWD LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900125 19991029 00125 1999 10 29 SWAA991737 4 19991018 A 2565 D31354 INDICATOR BOEING 737 7372H4 138448C NM SLIDE OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999102900126 19991029 00126 NM 1999 10 29 SWAA991738 1 19991018 A 2560 P4010021 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FWD FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F A16WE 1999102900127 19991029 00127 NM 1999 10 29 SWAA991721 1 19991016 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 9. REPAIRED CRACKED PER SRM. 2 L 7 2 4F RT A16WE 1999102900128 19991029 00128 NM 1999 10 29 SWAA991722 1 19991016 A 3350 BR2013 LIGHT BOEING 737 7373G7 1384595 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND EEPLS FWD AND AFT END CAPS MISSING. REPLACED END CAPS PER MM. 2 L 7 2 4F RT A16WE 1999102900129 19991029 00129 1999 10 29 SWAA991723 4 19991015 A 2565 63550101 BOTTLE BOEING 737 7377H4 NM SLIDE DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 725SW 27857 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900130 19991029 00130 NM 1999 10 29 SWAA991724 1 19991015 A 5320 6567127 WEB BOEING 737 7375H4 138449D NM LT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED SPECIAL VISIT, FOUND LT MLG WHEEL WELL PRESSURE WEB CRACKED NEXT TO TOWER SHAFT. REPAIRED WEB PER ER N R 99-6239. 2 L 7 2 4F RT A16WE 1999102900131 19991029 00131 1999 10 29 SWAA991725 4 19991015 A 2565 1061323475 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED SPECIAL VISIT, FWD SERVICE DOOR EVACUATION SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE AS SY PER MM. 2 L 7 2 4F RT A16WE 1999102900132 19991029 00132 NM 1999 10 29 SWAA991726 1 19991015 A 3350 6556633 LENS BOEING 737 7375H4 138449D NM EXIT LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900133 19991029 00133 NM 1999 10 29 SWAA991727 1 19991015 A 3350 07912 LIGHT COVER BOEING 737 7373H4 1384600 NM ROW 21 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 603SW 27954 EEPLS MISSING COVER AT ROW 21. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999102900134 19991029 00134 1999 10 29 SWAA991728 4 19991015 A 2397 W323303224 WIRE BOEING 737 7372T4 1384492 NM COMMUNICATIONS FAILED A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 702ML 22054 AIR TURNBACK, BOTH COMMUNICATION RADIOS INOP AFTER TAKEOFF. REPAIRED SHORT WIRE IN CAPT'S SIDEWALL PANEL, AND REMOVED A ND REPLACED CAPT'S HAND MIC JACK. 2 L 7 2 4F A16WE 1999102900135 19991029 00135 NM 1999 10 29 SWAA991729 1 19991015 A 5270 6552873 DOOR WARNING BOEING 737 7373H4 1384600 NM COCKPIT ILLUMINATED A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 642WN 27715 ABORTED TAKEOFF, AFT ENTRY DOOR LIGHT ILLUMINATED 80 KNOTS DURING TAKEOFF. OPERATED AND INSPECTED AFT ENTRY DOOR SEVERA L TIMES PER MM. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999102900136 19991029 00136 NM 1999 10 29 SWAA991730 1 19991017 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 10 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS LOOSE AT ROW 10. REMOVED AND REPLACED TRACK SECTION PER MM. 2 L 7 2 4F RT A16WE 1999102900137 19991029 00137 WP 1999 10 29 TWAA9914401 1 19991021 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP ROWS 8-9-11 DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 952U 49266 EMERGENCY EGRESS LIGHTS INOP ROWS 8, 9 AND 11. REPLACED BATTERY. CHECK C 03/26/99 STL. 2 L 7 2 4F A6WE 1999102900138 19991029 00138 WP 1999 10 29 TWAA9914402 1 19991019 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOP A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 987Z 47137 FIRST CLASS EGRESS LIGHTS INOPERATIVE. REMOVED MOISTURE FROM TRACK AND RESECURED CONNECTIONS. CHECK C 04/26/99 MCI. 2 L 7 2 4F A6WE 1999102900139 19991029 00139 WP 1999 10 29 TWAA9914403 1 19991020 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 986Z 47589 THE FIRST CLASS CABIN OVERHEAD EMERGENCY LIGHTS WERE WEAK. REPLACED THE BATTERIES. CHECK-C 3-3-99 MCI. 2 L 7 2 4F A6WE 1999102900140 19991029 00140 WP 1999 10 29 TWAA9914404 1 19991012 A 5280 5930583229 SPLICE DOUG DC9 DC983 3022083 WP LT MLG DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9302B 49528 DURING CHECK C, LT MLG DOOR HAD A CRACK IN DOUBLER AT AFT EDGE OF DOOR ABOUT 2 AND ONE HALF INCHES LONG. REMOVED AND RE PLACED DOUBLER PER MSA 692, SPM 6-70-01 AND SRM 51-01 PAGE 1. CHECK C 9/8/99 MCI. 2 L 7 2 4F RT A6WE 1999102900141 19991029 00141 EU 1999 10 29 MALA976606 1 19991011 A 3230 643500300 SWITCH BAC 146 AVRO146RJ85A 1500097 EU MLG FAILED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 514XJ E2330 DURING CLIMB, THE CREW COULDN'T BRING LANDING GEAR UP, SELECTED OVERRIDE LEVER TO BRING GEAR UP. MAINTENANCE REPLACED U NDERCARRIAGE SELECTOR SWITCH. OPS CHECK GOOD IAW RJ 85 AMM 32-30-14. 2 H 7 4 4F RT A49EU 1999102900142 19991029 00142 EU 1999 10 29 MALA976607 1 19991013 A 3260 AIR130900 SWITCH SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 416XJ 416 CREW DIDN'T REEIVE GREEN NOSE DOWN LIGHT, FOLLOWED QRH, TRANSIT LIGHT OPERATION NORMAL, CYCLED GEAR SEVERAL TIMES. RECE IVED GREEN NOSE LIGHT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK SWITCH TO BE FAULTY. REPLACED DOWNLOCK SWITCH IAW MM 32-61-05. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999102900143 19991029 00143 EU 1999 10 29 MALA976608 1 19991018 A 5347 7253799383 SEAT TRACK SAAB SF340 SF340A 7850100 EU BS 294 - 387 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 48XJ 048 DURING HEAVY CHECK, FOUND CORROSION ON SEAT TRACK ASSEMBLY TO BE OUT OF LIMITS. MAINTENANCE REPLACED SEAT TRACK AT STA 294.0 - 387.5, BLO IAW SRM 53-70-60 AND EO S53060. 2 L 7 2 4T RT A52EU 1999102900144 19991029 00144 EU 1999 10 29 MALA976609 1 19991011 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 319 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426XJ 426 DENT IN FORWARD CABIN BOTTOM SKIN JUST FWD OF STA 319.0 AND BETWEEN SL1626 AND SL1627. MAINTENANCE REPAIRED DENT PER EO NR S53062. 2 L 7 2 4T RT A52EU 1999102900145 19991029 00145 EU 1999 10 29 MALA976610 1 19991019 A 3350 LIGHT SAAB SF340 340B 7860101 EU ROW 5 & 6 LOOSE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 429XJ 429 EMERGENCY LIGHT STRIP ALONG FLOOR AT SEATS 5 AND 6 A COMING LOOSE. MAINTENANCE RESECURED LIGHT STRIP. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999102900146 19991029 00146 1999 10 29 MALA976611 4 19991019 A 3420 6226190113 COMPUTER SAAB SF340 340B 7860101 EU AVIONICS RACK MALFUNCTIONED A MALA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 GL 15 447XJ 447 AFTER TAKEOFF, CLIMBING THROUGH 5000 FT, AVIONICS ANNUNCIATOR WITH A ROLL FLAG ILLUMINATED. THE NR 1 AI WAS SHOWING 5 D EGREES BANK IN STRAIGHT AND LEVEL, ABOUT 10 MINUTES PRIOR TO LANDING ALL ANNUNCIATORS CLEARED AND INDICATIONS WERE NORMA L. MAINTENANCE REPLACED NR 1 AHARS COMPUTER. OPS CHECK GOOD IAW SF340 MM CHAP 34. 2 L 7 2 4T RT A52EU 1999102900147 19991029 00147 EU 1999 10 29 MALA976612 1 19991020 A 3350 LIGHT BAC 146 AVRO146RJ85A 1500097 EU COCKPIT INOP A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 511XJ E2326 FLIGHT DECK EMERGENCY LIGHT LOCATED UNDER THE CENTER OF THE GLARE SHEILD INOP. MAINTENANCE RELAMPED. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999102900148 19991029 00148 WP 1999 10 29 IXXA9900026 1 19991021 A 2120 UNKNOWN DOUG DC8 DC862 3021970 WP COCKPIT ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 61CX 46142 EN ROUTE FROM AVB TO RMS, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE OVER HEAD FLORESENT LIGHTING SYSTEM WAS ILLUMINATED. THE CREW TURNED THE LIGHTS OFF AND THE ODOR SUBSIDED, THE FLIGHT CONTINUED TO RMS FOR AN UNEVENTFUL LANDI NG. MAINTENANCE INSPECT THE LIGHTING SYSTEM CIRCUITRY AND OPERATED THE SYSTEM WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999102900149 19991029 00149 SO 1999 10 29 RAAA99E4023 1 19991005 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 695 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT FUS/STA 695 LBL 56. REPLACED SEAT TRACK AS PER ECO 99-05, M-5 4 NR 125. 2 L 7 4 4T 4A22 1999102900150 19991029 00150 SO 1999 10 29 RAAA99E4024 1 19991005 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 654 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK FLANGE CORRODED AT FUS/STA 654 LBL55. REPLACED SEAT TRACK AS PER ECO 99-0 5, M-54 NR 126. 2 L 7 4 4T 4A22 1999102900151 19991029 00151 SO 1999 10 29 RAAA99E4025 1 19991005 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 371-502 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT FUS/STA 371 TO 502 LBL 26. REPLACED SEAT TRACK AS PER ECO 99- 05, M-54 NR 127. 2 L 7 4 4T 4A22 1999102900152 19991029 00152 SO 1999 10 29 RAAA99E4026 1 19991005 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 637 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM CORRODED AT FUS/STA 637 LBL 0-LBL 20. REPLACED FLOORBEAM AS PER SRM 51-2-9. INSTALLED FLOORBEAM AS PER SRM 51-2-12, M-54 NR 128. 2 L 7 4 4T 4A22 1999102900153 19991029 00153 SO 1999 10 29 RAAA99E4027 1 19991005 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 502 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM CORRODED AT FUS/STA 502 BBL 0 TO LBL 25. REPAIRED AS PER SRM 53 -2-4, M-54 NR 129. 2 L 7 4 4T 4A22 1999102900154 19991029 00154 SO 1999 10 29 RAAA99E4028 1 19991005 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 371-502 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT BBL 0 FUS/STA 371-502. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 130. 2 L 7 4 4T 4A22 1999102900155 19991029 00155 SO 1999 10 29 RAAA99E9026 1 19991019 A 5350 RADOME LKHEED 188 188C 5262604 SO FUSELAGE DAMAGED A RAAA O OTHER O OTHER AP APPROACH 1 AL 03 1968R 188C2007 DURING APPROACH TO ANC, AIRCRAFT STRUCK BY LIGHTNING. RADOME RECEIVED DAMAGE. REPAIRED PER SRM 53-1-6 NEGLIGIBLE DAMAG E. 2 L 7 4 4T 4A22 1999102900156 19991029 00156 1999 10 29 RAAA99E9027 4 19991019 A 3432 4735541 ANTENNA LKHEED 188 188C 5262604 SO FUSELAGE DAMAGED A RAAA O OTHER O OTHER AP APPROACH 1 AL 03 1968R 188C2007 DURING APPROACH TO ANC, AIRCRAFT STRUCK BY LIGHTNING, G/S ANTENNA DAMAGED. REPLACED G/S ANTENNA. OPS CHECKED PER LAC M M 34-13-13. 2 L 7 4 4T 4A22 1999102900157 19991029 00157 SO 1999 10 29 RAAA99E9028 1 19991022 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 9 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EMERGENCY PROXIMITY LIGHTAT ROW 9 CDE DOES NOT TEST. REPLACED BATTERY PACK. 2 L 7 4 4T 4A22 1999102900158 19991029 00158 SO 1999 10 29 RAAA99E9029 1 19991022 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 21 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EMERGENCY PROXIMITY LIGHT AT ROW 21 CDE, DOES NOT TEST. REPLACED BATTERY PACK. 2 L 7 4 4T 4A22 1999102900159 19991029 00159 WP 1999 10 29 9904339857 1 19991014 A 3244 95608597 TIRE DOUG DC9 DC951 3022051 WP MLG FAILED A NWAA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 GL 01 766NC 47739 DURING TAKEOFF AT MDW, THE LEFT OUTBOARD NR 1 MAIN WHEEL AND TIRE ASSEMBLY DEPARTED THE AIRCRAFT. FLIGHT CONTINUED TO D ESTINATION (DTW) AND LANDED WITHOUT INCIDENT. FLIGHT CREW DECLARED AN EMERGENCY. MAITNENANCE REPLACED THE LEFT BOTTOM MAIN LANDING GEAR STRUT AND NR 1 MAIN WHEEL ANTI-SKID TRANSDUCER. INSPECTED HYDRAULIC LINES AND LEFT LANDING GEAR ANTI- SKID WIRING AND REPLACED NR 1 AND NR 2 MAIN TIRE AND BRAKE ASSEMBLIES. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1999102900160 19991029 00160 WP 1999 10 29 9904349981 1 19991017 A 2131 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE FAILED A NWAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 01 994Z 47097 DURING CLIMB-OUT FROM PHL, LOSS OF CABIN PRESSURIZATION OCCURRED AT APPROXIMATELY 27,000 FEET. CREW EXECUTED AN EMERGEN CY DESCENT TO 10,000 FEET. RED CABIN PRESSURE WARNING LIGHT ILLUMINATED AND CABIN ALTITUDE CLIMBED TO 12,000 FEET. FLI GHT WAS RETURNED TO PHL AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED FOR VESSEL LEAKS AND NONE WERE FOUND. REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999102900161 19991029 00161 EU 1999 10 29 9904353219 1 19991018 A 2133 90231570381 OUTFLOW VALVE AIRBUS 320 A320211 3930320 EU CABIN PRESSURE FAILED A NWAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 319US 26521 18517 208 DURING CRUISE, RECEIVED CABIN PRESSURE SYS 1 AND 2 FAULT AND CABIN PRESSURE EXCESS CAB ALT MESSAGES WITH AUTOMATIC DROP OF OXYGEN MASKS. INITIATED RAPID DESCENT DUE TO A MODERATELY RAPID DECOMPRESSION. DIVERTED TO MCI AND LANDED WITHOUT I NCIDENT. MAINTENANCE REPLACED NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS AND THE OUTFLOW VALVE. SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 1999102900162 19991029 00162 NM 1999 10 29 UPS99230969 1 19991020 A 5330 SKIN BOEING 727 72725C 138400H NM BS 345 - 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI PILLOWING SKIN AND DISHED RIVET HEADS BS 345-360, WL 148, RBL 10 EXTERIOR SKIN. REMOVED, FABRICATED, AND REPLACED SKIN STA 345-360, WL 148, LBL 13 TO RBL 13. 2 L 7 3 4F A3WE 1999102900163 19991029 00163 NM 1999 10 29 UPS99230970 1 19990827 A 5314 KEEL BEAM BOEING 727 72725C 138400H NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI WHILE WORKING CUSTOMER CARD NR 997349, FOUND KEEL BEAM CRACKED AT BS 1070, WL 142, RBL 8. REPAIRED C RACKED KEEL BEAM IAW ER NR 99-6118. 2 L 7 3 4F A3WE 1999102900164 19991029 00164 NM 1999 10 29 UPS99230971 1 19990823 A 5730 PANEL BOEING 727 72725C 138400H NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION (C57-571-01.02-02) ON CUTOUT FOR ACCESS PANEL NR 7602, UPPER SURFACE. REPAIRED PER EO 99-6 029. 2 L 7 3 4F A3WE 1999102900165 19991029 00165 NM 1999 10 29 UPS99230972 1 19991010 A 5320 7075T6 WEB BOEING 727 72725C 138400H NM BS 720 - 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI WHILE WORKING CUST CARD 997529 FOUND WEB TO BE CRACKED BS 720-740 LBL 60. REMOVED CRACKED WEB, INSTA LLED REPLACEMENT WEB PER SRM 51-40-2 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999102900166 19991029 00166 NM 1999 10 29 UPS99230973 1 19991010 A 5347 202543 SEAT TRACK BOEING 727 72725C 138400H NM BS 550 - 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON SEAT TRACK AT BS 600, BS 640, BS 660 AND BS 700, BL 0, WL 208. REPLACED SEAT TRACK FROM BS 550-720, BL 0, WL 208 PER SRM 51-30-2, 53-10-1 AND 51-10-02. 2 L 7 3 4F A3WE 1999102900167 19991029 00167 NM 1999 10 29 UPS99230974 1 19990825 A 5315 M249633 FLOORBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: SI, CORROSION ON FLOORBEAM AT NUTPLATE BS 720 LBL 57 WL 208. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999102900168 19991029 00168 NM 1999 10 29 UPS99230975 1 19990823 A 5315 M241110 FLOORBEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: SI, CORROSION ON STA 970, LBL 57, WL 208 ON FLOORBEAM UNDER NUTPLATE. REMOVED DAMAGE, FABRICATE REPAI R AND INSTALLED PER SRM 53-10-8, FIG 5, 51-30-2. 2 L 7 3 4F A3WE 1999102900169 19991029 00169 NM 1999 10 29 UPS99630965 1 19991021 A 3240 BRAKE BOEING 767 76734AF 1385212 NM NR 3 BURNED A IPXA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 01 312UP 27763 NR 3 MAIN BRAKE CAUGHT ON FIRE AFTER ARRIVAL. FOUND TO BE ONLY GREASE ON BRAKE BURNING. PUT OUT FIRE. REPLACED TIRE A SSY PRECAUTIONARY. PLACARDED NR 3 BRAKE INOP PER MEL. 2 L 7 2 4F RT A1NM 1999102900170 19991029 00170 WP 1999 10 29 UPS99830964 1 19991013 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 EMERGENCY LIGHT VERY DIM. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT. OPS CHECK NORMAL PER DC8 DC8 MM 33-50-01 . 2 L 7 4 4F RT 4A25 1999102900171 19991029 00171 WP 1999 10 29 UPS99830966 1 19991021 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 709UP 45914 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999102900172 19991029 00172 WP 1999 10 29 UPS99830967 1 19991021 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 1999102900173 19991029 00173 WP 1999 10 29 UPS99830968 1 19991022 A 3230 LIGHT DOUG DC8 DC873F 302199F WP RT WING INOP A IPXA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 880UP 46080 ON APPROACH TO ONT, RIGHT WING LANDING LIGHT FAILED TO ILLUMINATE WITH SWITH ON. PERFORMED T/S PER FIM 33-42-00 FIG 107 , RELAMPED PER MM 33-42-03. 2 L 7 4 4F RT 4A25 1999102900174 19991029 00174 EU 1999 10 29 99FDEA00439 1 19991021 A 7830 SWITCH AIRBUS 310 A310222 3930315 EU NR 1 ENGINE TR OUT OF ADJUST A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 449FE 217 NR 1 ENG REV UNLOCK LIGHT CAME ON AT APPROX 55 KTS ON T/O ROLL. ABORTED T/O. NR 1 THRUST REVERSER WAS DEFERRED MEL 78- 1 CTRL NR 61783. ADJUSTED STOW SWITCHES PER A310 MM 78-31-00 PG 513. REACTIVATED T/R'S AND CLOSED FOA COWL DOORS PER A 310 MM 71-13-00. RAN NR 1 ENG TO OPS CHECK T/R AND ALL PARAMETERS MET PER JRH. 2 L 7 2 4F RT A35EU 1999102900175 19991029 00175 WP 1999 10 29 99FDEA00440 1 19991020 A 3230 ACTUATOR DOUG DC10 DC1030F 3023504 WP LT MLG DNLOCK LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LT MAIN LANDING GEAR DOWNLOCK ACTUATOR FOUND ACTUATOR END WITH BOLT LOOSE AND NUT MISSING. *S/D* REPLACED AND TIGHTENE D BUSHING AND NUT PER MM 20-50-02-2. 2 L 7 3 4F RT A22WE 1999102900176 19991029 00176 NM 1999 10 29 99FDEA00441 1 19991022 A 5330 ABA70501 SKIN DOUG MD11 MD11F 3023600 NM BS 275-313 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 FUSELAGE EXT SKIN DENTS BETWEEN Y STA 275-313, X LONGERON 23-24 LT. TRIMMED OFF AND FAB REPAIR DOUBLER AND INNER FINGER DOUBLER, INSTALLED PER SRM 53-20-00 FIG 2 VOL 1. 2 L 7 3 4F RT A22WE 1999102900177 19991029 00177 NM 1999 10 29 99FDEA00442 1 19991022 A 2742 B272701301 ACTUATOR BOEING 727 72725 1384006 NM HORIZ STAB MALFUNCTIOND A FDEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 506FE 18277 99-257 JAMMED STABILIZER TRIM AT 210K ON DEPART FROM STL PRIMARY TRIM & COURSE TRIM BOTH INOP. ** S/D ** REPLACED S TABILIZER TRIM ACTUATOR PER B727-100 MM 27-40-031-2 & 27-12-061-2. THIS CORRECTION CHANGES THE CAT STATUS OF THE A/C. 2 L 7 3 4F A3WE 1999102900178 19991029 00178 NM 1999 10 29 99FDEA00443 1 19991022 A 2120 UNKNOWN BOEING 727 727277 138408S NM COCKPIT ODOR A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 243FE 21480 99-258 - BURNT RUBBER SMELL WAS NOTICED SHORTLY AFTER TAKEOFF. LEFT PACK ON ENG NR 1 WAS BLEED SOURCE. RAN LEFT PACK, WITH NR 1 ENG AS AIR SOURCE FOR ABOUT 20 MIN. NO BURNT RUBBER SMELL NOTICED. 2 L 7 3 4F RT A3WE 1999102900179 19991029 00179 1999 10 29 99FDEA00444 2 19991022 A 7320 441790 HMU AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE FAILED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 660FE 759 99-259 AT APPROX 85 KTS ON TO RECD MASTER CAUTION & ECAM MESSAGE ENG #1 SHUT DOWN, REJECTED TO. AFT RETURN TO RAMP ENG WOULD NOT SHUT DOWN NORM. PULL FIRE HANDLE. ** S/D ** R&R #1 ENG HMU PER A300 MM 73-13-00-4. OPS CK NORM. 2 L 7 2 4F RT A35EU 1999102900180 19991029 00180 1999 10 29 99FDEA00445 4 19991025 A 3140 20035012007 MFDU DOUG MD11 MD11F 3023600 NM COCKPIT FAILED A FDEA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 603FE 48459 99-260 - AT FLT LEVEL 330, ON CLIMB-OUT RECEIVED AIR MANIFOLD 2 FAIL GOT ALERT AIR SYS 1/2 FAIL, NOTE THE NR 2 ENGINE BL D VALVE DID NOT CLOSE. REMOVED AND REPLACED THE MANIFOLD FAILURE CONTROLLER PER MM 36-23-00-5. SYSTEM TEST NORMAL. 2 L 7 3 4F RT A22WE 1999102900181 19991029 00181 WP 1999 10 29 ABXA9900745 1 19991019 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 987AX 47364 DURING PREDEPARTURE CHECK AT BNA, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1999102900182 19991029 00182 WP 1999 10 29 SCNA99538 1 19991018 A 5320 WEB DOUG DC10 DC1015 3022118 WP BS 1541 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK IN THE CARGO BAY STA 1541 AT LGR 43L WAS FOUND TO HAVE A 1 INCH CRACK IN THE WEB UNDER THE CARGO ROLLER TRACKS. REMOVED WEB AND FABRICATED A NEW ONE PER SRM 512101 AND 513000. 2 L 7 3 4F A22WE 1999102900183 19991029 00183 WP 1999 10 29 SCNA99539 1 19991018 A 5320 ANGLE DOUG DC10 DC1015 3022118 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK IN THE AFT CARGO COMPARTMENT CORROSION WAS FOUND AT STA 1964 AT LBL 50 TO RBL 50. REMO VED AFT THRESHOLD ANGLE AND FABRICATED NEW THRESHOLD ANGLE AND INSTALLED. 2 L 7 3 4F A22WE 1999102900184 19991029 00184 WP 1999 10 29 SCNA99540 1 19991018 A 3520 OXYGEN GEN DOUG DC10 DC1015 3022118 WP SEAT 20 DISCHARGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE OXYGEN GENERATOR AT SEAT 20D AND 20E WAS FOUND DISCHARGE. REMOVED AND REPLACED OX YGEN GENERATOR PER MM 352003. 2 L 7 3 4F A22WE 1999102900185 19991029 00185 WP 1999 10 29 SCNA99541 1 19991018 A 5320 INTERCOSTAL DOUG DC10 DC1015 3022118 WP BS 495 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK INTERCOSTAL AT STA 495X EQUALS PLUS AND MINUS 45 WAS FOUND CORRODED AT THE UPPER END. 1 00 PERCENT MATERIAL LOSS WAS NOTED. REMOVED INTERCOSTAL AND INTERCOSTAL UPPER CAP. FABRICATED NEW INTERCOSTAL AND INST ALLED PER SRM 512101. 2 L 7 3 4F A22WE 1999102900186 19991029 00186 WP 1999 10 29 SCNA99542 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 465 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, SEAT TRACK AT STA 465 48 RT IN THE MAIN CABIN WAS FOUND CORRODED. REMOVED AND REPLACE D SEAT TRACK PER SRM 537000. 2 L 7 3 4F A22WE 1999102900187 19991029 00187 WP 1999 10 29 SCNA99543 1 19991018 A 5320 CHANNEL DOUG DC10 DC1015 3022118 WP BS 1841- 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK IN THE AFT CARGO PIT STA 1841 TO 1964 RT SIDE LOWER CENTER FLOOR TO LOWER SIDE FLOOR Z CHANNEL HAS CORROSION ON ENTIRE LENGTH. REMOVED CORROSION AND WAS FOUND OUT OF LIMITS. REMOVED AND INSTALLED NEW CHANN EL PER SRM 513101. 2 L 7 3 4F A22WE 1999102900188 19991029 00188 WP 1999 10 29 SCNA99544 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 495 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STA 459 X MINUS 30 AND Z MINUS 18 WAS FOUND CORRODED. REMOVED CO RROSION FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT FABRICATED AND REINSTALLED FLOOR SUPPORT PER SRM 513101. 2 L 7 3 4F A22WE 1999102900189 19991029 00189 WP 1999 10 29 SCNA99545 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 459 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STA 459 X PLUS 20 Z MINUS 18 WAS FOUND TO BE CORRODED. REMOVED C ORROSION FOUND TO BE OUT OF LIMITS. REMOVED FABRICATED AND REINSTALLED FLOOR SUPPORT IAW 511001 FIG 17 AND 513501. 2 L 7 3 4F A22WE 1999102900190 19991029 00190 WP 1999 10 29 SCNA99546 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1841 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 1841 X PLUS WAS FOUND CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 537000. 2 L 7 3 4F A22WE 1999102900191 19991029 00191 WP 1999 10 29 SCNA99547 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 495 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STA 495 X PLUS 62 Z MINUS 18 WAS FOUND CORRODED. REMOVED CORROSI ON FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AND REINSTALLED NEW FLOOR SUPPORT IAW SRM 513501 AND 512101. 2 L 7 3 4F A22WE 1999102900192 19991029 00192 WP 1999 10 29 SCNA99548 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 414 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STA 414 X MINUS 20 WAS FOUND CORRODED ON THE UPPER SURFACE. REMO VED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 513101. 2 L 7 3 4F A22WE 1999102900193 19991029 00193 WP 1999 10 29 SCNA99549 1 19991018 A 5320 TIE DOWN DOUG DC10 DC1015 3022118 WP BS 795 - 859 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE TIE DOWN CHANNEL AT STA 795 TO 859 WAS FOUND CORRODED AT RBL 50. REMOVED CORROSIO N FOUND TO BE OUT OF LIMITS. REMOVED FABRICATED AND INSTALLED NEW TIE DOWN CHANNEL PER SRM 537000 FIG 1 VOLUME 1. 2 L 7 3 4F A22WE 1999102900194 19991029 00194 WP 1999 10 29 SCNA99550 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1902 - 2607 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR BOARD SUPPORT AT STA 1902 TO 2607 X MINUS 57 WAS FOUND TO BE CORRODED. REMO VED CORRODED SUPPORT FOUND OUT OF LIMITS. INSTALLED NEW SUPPORT PER SRM 513101. 2 L 7 3 4F A22WE 1999102900195 19991029 00195 WP 1999 10 29 SCNA99551 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1914 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT DOG BONE AT STA 1914 X MINUS 54 WAS FOUND TO BE CORRODED. REMOVED C ORRODED FLOOR SUPPORT DOG BONE AND INSTALLED NEW FLOOR SUPPORT PER SRM 513101. 2 L 7 3 4F A22WE 1999102900196 19991029 00196 WP 1999 10 29 SCNA99552 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, A FLOOR SUPPORT CHANNEL AT STA 440 RBL 70 WAS FOUND TO BE CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NEW SUPPORT PER SRM 513101. 2 L 7 3 4F A22WE 1999102900197 19991029 00197 WP 1999 10 29 SCNA99553 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, A FLOOR SUPPORT AT STA 1887 X EQUALS PLUS 91 TO MINUS 91 WAS FOUND TO BE CORRODED. RE MOVED FABRICATED AND INSTALLED NEW FLOOR SUPPORT PER SRM 513501. 2 L 7 3 4F A22WE 1999102900198 19991029 00198 WP 1999 10 29 SCNA99554 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 825 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, A FLOOR SUPPORT AT STA 825 FROM RBL 30 TO RBL 50 WAS FOUND TO BE CORRODED. REMOVED AN D REPLACED WITH NEW FLOOR SUPPORT AND INSTALLED PER SRM 513301. 2 L 7 3 4F A22WE 1999102900199 19991029 00199 WP 1999 10 29 SCNA99555 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1902 - 1965 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 1902 TO 1965 WAS FOUND TO BE CORRODED. CORROSION REMOVED WAS FO UND TO BE OUT OF LIMITS. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW 537000. 2 L 7 3 4F A22WE 1999102900200 19991029 00200 WP 1999 10 29 SCNA99556 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1841 - 1886 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, ALL LAVATORY SUPPORT RAILS FROM STA 1841 TO 1886 36LT TO 36RT WERE FOUND TO BE CORRODE D. REMOVED AND INSTALLED NEW LAV SUPPORTS PER SRM 513101. 2 L 7 3 4F A22WE 1999102900201 19991029 00201 WP 1999 10 29 SCNA99557 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP GALLEY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE LOWER AFT RT GALLEY BOTTOM FLANGE WAS FOUND CORRODED. REMOVED FABRICATED ANGLES A ND INSTALLED PER SAMPLE. 2 L 7 3 4F A22WE 1999102900202 19991029 00202 WP 1999 10 29 SCNA99558 1 19991018 A 5320 SPLICE DOUG DC10 DC1015 3022118 WP BS 795 - 859 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK THE HAT SPLICE NEEDS TO BE FABRICATED FROM STA 795 TO 859 AT X MINUS 50 IN CONJUNCTION WITH SEAT TRACK REPAIR AT SAME STA. FABRICATED AND INSTALLED SPLICE HAT PER SRM 5370 FIG 1. 2 L 7 3 4F A22WE 1999102900203 19991029 00203 WP 1999 10 29 SCNA99559 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 795 - 825 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 795 TO 825 LBL 6 WAS FOUND TO BE CORRODED. FABRICATED SEAT TRAC K PER SAMPLE AND INSTALLED PER SRM 537000. 2 L 7 3 4F A22WE 1999102900204 19991029 00204 WP 1999 10 29 SCNA99560 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1841 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT DOG BONE AT STA 1841 X PLUS 10 TO 26 WAS FOUND TO BE CORRODED. REMO VED FABRICATED AND INSTALLED FLOOR SUPPORT PER SRM 513101. 2 L 7 3 4F A22WE 1999102900205 19991029 00205 WP 1999 10 29 SCNA99561 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1841 CORRODED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 1841 X EQUALS PLUS 27 WAS FOUND TO BE CORRODED. REMOVED CORROSI ON FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 537000. 2 L 7 3 4F A22WE 1999102900206 19991029 00206 WP 1999 10 29 SCNA99562 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 440 - 470 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 440 TO 470 AT RBL 85 WAS FOUND TO BE CORRODED. SEAT TRACK WAS F OUND TO BE EXFOLIATED COMPLETELY THROUGH. SEAT TRACK WAS REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1999102900207 19991029 00207 WP 1999 10 29 SCNA99563 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 824 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, A FLOOR SUPPORT AT STA 824 LBL 86 WAS FOUND TO BE BROKEN. REMOVED AND INSTALLED SUPPO RT IAW 513501. 2 L 7 3 4F A22WE 1999102900208 19991029 00208 WP 1999 10 29 SCNA99564 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1914 - 2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STA 1914 TO 2007 AT X PLUS 23 WAS FOUND TO BE CORRODED. REMOVED CORRODED SUPPORT AND INSTALLED NEW SUPPORT IAW SRM 513101. 2 L 7 3 4F A22WE 1999102900209 19991029 00209 WP 1999 10 29 SCNA99565 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 795 - 825 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 795 TO 825 LBL 25 WAS FOUND TO BE CORRODED. REMOVED CORROSION A ND INSTALLED FABRICATED PARTS PER SRM 536001. 2 L 7 3 4F A22WE 1999102900210 19991029 00210 WP 1999 10 29 SCNA99566 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 19105 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT DOG BONE AT STA 1910 X MINUS 60 TO X MINUS 86 WAS FOUND TO BE CORRO DED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW 530001. 2 L 7 3 4F A22WE 1999102900211 19991029 00211 WP 1999 10 29 SCNA99567 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1884 - 2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT STA 1884 TO 2007 X MINUS 23 WAS FOUND TO BE CORRODED. REMOVED AND R EPLACED SUPPORT IAW SRM 513101. 2 L 7 3 4F A22WE 1999102900212 19991029 00212 WP 1999 10 29 SCNA99568 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 808 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 808 RBL 95 WAS FOUND TO BE CRACKED. REMOVED AND REPLACED STRAP IAW 504101. 2 L 7 3 4F A22WE 1999102900213 19991029 00213 WP 1999 10 29 SCNA99569 1 19991018 A 5320 CHANNEL DOUG DC10 DC1015 3022118 WP BS 440 - 470 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE TIE DOWN CHANNEL AT STA 440 TO 470 RBL 65 WAS FOUND CORRODED. REMOVED AND REPLACE D CORRODED SEAT TRACK REF SRM 531101 AND 513501. 2 L 7 3 4F A22WE 1999102900214 19991029 00214 WP 1999 10 29 SCNA99570 1 19991018 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STA 440 32 LT WAS FOUND CORRODED. REMOVED FABRICATED AND INSTALLED SEAT TRACK PER SRM 513101. 2 L 7 3 4F A22WE 1999102900215 19991029 00215 WP 1999 10 29 SCNA99571 1 19991018 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1910 - 2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE LAV AND GALLEY SUPPORT NUT CLIP HOLE WAS FOUND TO BE CORRODED AT STA 1910 TO 2007 X PLUS 52. REMOVED GALLEY SUPPORT AND INSTALLED NEW SUPPORT IAW 513501. 2 L 7 3 4F A22WE 1999102900216 19991029 00216 WP 1999 10 29 SCNA99572 1 19991018 A 5511 RIB DOUG DC10 DC1015 3022118 WP HORIZ STAB CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE RT HORIZONTAL STABILIZER CLOSING RIB WAS FOUND CRACKED IN TWO PLACES APPROXIMATELY STA XE 26. REMOVED DAMAGED AREA PER SRM 550001 FIG 3. NO CRACKS REMAINING PER 551101 AND FABRICATED DOUBLER PER SRM 5 50001 FIG 3 AND INSTALLED. 2 L 7 3 4F A22WE 1999102900217 19991029 00217 WP 1999 10 29 SCNA99573 1 19991018 A 5520 ANGLE DOUG DC10 DC1015 3022118 WP ELEVATOR CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE RT INBOARD ELEVATOR TRAILING EDGE WAS FOUND TO HAVE A CRACK IN THE INBOARD CORNER. REMOVED CORNER CAP AND FABRICATED NEW REPAIR ANGLE AND INSTALLED PER SRM 513501. 2 L 7 3 4F A22WE 1999102900218 19991029 00218 WP 1999 10 29 SCNA99574 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 50 END CAP FITTING WAS FOUND TO BE CORROD ED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900219 19991029 00219 WP 1999 10 29 SCNA99575 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 51 END CAP FITTING WAS FOUND TO BE CORROD ED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900220 19991029 00220 WP 1999 10 29 SCNA99576 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 52 RIGHT AND LEFT END CAP FITTING WAS FOU ND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900221 19991029 00221 WP 1999 10 29 SCNA99577 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 51 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900222 19991029 00222 WP 1999 10 29 SCNA99578 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 48 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900223 19991029 00223 WP 1999 10 29 SCNA99579 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 48 LEFT END CAP FITTING WAS FOUND TO BE C ORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900224 19991029 00224 WP 1999 10 29 SCNA99580 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 49 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900225 19991029 00225 WP 1999 10 29 SCNA99581 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 49 LEFT END CAP FITTING WAS FOUND TO BE C ORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900226 19991029 00226 WP 1999 10 29 SCNA99582 1 19991018 A 5714 ENDCAP DOUG DC10 DC1015 3022118 WP CENTER WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE CENTER WING LOWER BARREL AT STA 1521 LGR 50 RIGHT END CAP FITTING WAS FOUND TO BE CORRODED. REMOVED AND FABRICATED NEW FITTING AND INSTALLED PER SRM 513101. 2 L 7 3 4F A22WE 1999102900227 19991029 00227 WP 1999 10 29 SCNA99583 1 19991018 A 5713 STRINGER CLIP DOUG DC10 DC1015 3022118 WP WS 402 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A HEAVY MAINTENANCE CHECK, THE RIGHT WING NUMBER THREE TANK STA XORS 402 STRINGER CLIP IS CRACKED AT STRINGER 7. REMOVED FABRICATED AND INSTALLED NEW CLIP PER SRM 513020 AND AMS EO. 2 L 7 3 4F A22WE 1999102900228 19991029 00228 SO 1999 10 29 SWIA971583 1 19991018 A 3610 DUCT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING K M FLUID LOSS OVER TEMP CL CLIMB 1 NM 07 291SW 120318 DUCT LEAK WARNING AFTER TAKEOFF STAYS ON THREE MINUTES. LEFT ENGINE SHUT DOWN AND RETURNED TO LAX FOR LANDING. REPLACE D TUBE ASSEMBLY FORWARD OF LEFT HEAT EXCHANGER ALSO CHANGED CLAMP ASSEMBLY. RAN ENGINE AT 100 PERCENT FOR SEVERAL MINUTE S. OPS CHECKS GOOD. NO DUCT LEAK WARNINGS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102900229 19991029 00229 SO 1999 10 29 SWIA971584 1 19991018 A 3610 38E966A DUCT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CR CRUISE 1 NM 07 291SW 120318 EN ROUTE FROM FAT TO SFO, DUCT LEAK LIGHT FOR LEFT ENGINE CAME ON. LIGHT STAYED ON FOLLOWING QRH PROCEDURES. SHUT DOWN LEFT ENGINE AND MADE AN DIVERTED TO MOD. LEFT PRESSURE REGULATOR FOUND BAD, ALONG WITH TWO BAD SENSORS. DUCT SENSORS REPLACED. REMOVED AND REPLACED LEFT PRESSURE REGULATOR. RAN ENGINE AT POWER FOR SEVERAL MINUTES. PERFORMED TEST FLIGH T. NO DUCT LEAKS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999102900230 19991029 00230 NM 1999 10 29 VNAA9910011 1 19991019 A 2434 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 3068 116144 ON THE TAKEOFF ROLL, THE LEFT ENGINE ECU FAILED AND THE NH REACHED 104 PERCENT FOR ONE SECOND. THE CREW ABORTED THE TAK EOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE FOR FOD INGESTION AND DETERMINED THE AIRCRAFT WAS SAFE FOR FERRY FLIGHT TO DAY FOLLOWING A POWER ASSURANCE RUN. THE FERRY FLIGHT WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE THEN COMPLETED A SOFT MATERIAL INGESTION INSPECTION IN ACCORDANCE WITH SPECIAL INSPECTION 05-57-07. NO DAMAGE WAS NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102900231 19991029 00231 1999 10 29 RAIA9910029 4 19991012 A 3450 6222506004 INDICATOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 427AM 1794 1794 876 7504 - STL-FO'S RMI FLAGGED. MAINTENANCE REPLACED FO'S RMI. 2 L 7 2 4T RT A56EU 1999102900232 19991029 00232 EU 1999 10 29 RAIA9910030 1 19991021 A 2910 PV304426 PUMP BAG JETSTM JETSTM3201 1500217 EU HYD SYSTEM FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 424AM 865 7510 - STL - RIGHT HYD PUMP FAILED. MAINTENANCE REPLACED RIGHT HYD PUMP. 2 L 7 2 4T RT A56EU 1999102900233 19991029 00233 NM 1999 10 29 SWAA991749 1 19991021 A 3350 07912 COVER BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674AA 23252 EEPLS TRACK COVERS LOOSE. SECURED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 1999102900234 19991029 00234 NM 1999 10 29 SWAA991750 1 19991020 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 EEPLS WIRING LOOSE AT OVERWING EXIT. SECURED AND INSTALLED LOOSE WIRING PER MM. 2 L 7 2 4F RT A16WE 1999102900235 19991029 00235 NM 1999 10 29 SWAA991751 1 19991020 A 3350 612825 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND SERVICE DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATT ERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999102900236 19991029 00236 NM 1999 10 29 SWAA991752 1 19991020 A 2560 P4010021 BATTERY BOEING 737 7373L9 1384470 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED A2 CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999102900237 19991029 00237 1999 10 29 SWAA991753 4 19991021 A 2565 65C19901 CHAIN BOEING 737 7373H4 1384600 NM SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 FWD ENTRY DOOR EVACUATION SLIDE LATCH CHAIN BROKEN. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900238 19991029 00238 NM 1999 10 29 SWAA991754 1 19991021 A 3350 610478 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED C CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERNAL LIGHT BATTERY CHARGE LOW. REMOVED AND REPLACED BATT ERY PACK PER MM. 2 L 7 2 4F A16WE 1999102900239 19991029 00239 NM 1999 10 29 SWAA991755 1 19991021 A 5320 6549892 FITTING BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D CHECK, FOUND CORROSION AT STRINGER FITTING, BS 1016, STRINGER 27R. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F A16WE 1999102900240 19991029 00240 NM 1999 10 29 SWAA991756 1 19991021 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK LOOSE AT FWD END. REINSTALLED AND SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900241 19991029 00241 NM 1999 10 29 SWAA991757 1 19991021 A 3350 20131A BATTERY BOEING 737 7373A4 1384585 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY AND BATTER Y CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999102900242 19991029 00242 NM 1999 10 29 SWAA991758 1 19991021 A 3350 07912 COVER BOEING 737 7373G7 1384595 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROWS 4 THROUGH 8. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999102900243 19991029 00243 NM 1999 10 29 SWAA991759 1 19991021 A 3350 BR2013 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/2D CHECK, FOUND EEPLS INOP AT ROW 20. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999102900244 19991029 00244 1999 10 29 SWAA991760 4 19991021 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT DRAGGING ON FLOOR. REINSTALLED SLIDE ASSY PER M M. 2 L 7 2 4F RT A16WE 1999102900245 19991029 00245 NM 1999 10 29 TWAA9914501 1 19991024 A 3350 900542 POWER SUPPLY BOEING 727 727231 1384079 NM LT EMER EXIT INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54350 21969 THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED POWER SUPPLY. CHECK-C 1-29-99 MCI. 2 L 7 3 4F A3WE 1999102900246 19991029 00246 WP 1999 10 29 TWAA9914502 1 19991024 A 3246 5930594523 WHEEL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 2 FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN D INFLIGHT SEPARATION TO TAKEOFF 1 CE 05 940AS 49825 1470 DURING TAKEOFF, THE NUMBER 2 WHEEL ASSEMBLY FAILED. RUBBER FROM THE TIRE CAUSED DAMAGE TO THE LT LANDING GEAR, GEAR WIR ING, T/E FLAP AND THEN ENTERED THE LT ENGINE. THE ENGINE STALLED AND WAS SHUT DOWN. THE FLIGHT RETURNED TO OKC. REPL ACED THE WHEEL ASSEMBLY, AND REPAIRED THE DAMAGE, INCLUDING REPLACEMENT OF THE ENGINE FIRST STAGE FAN. CHECK-C 7-11-99 MCI. 2 L 7 2 4F 4 F A6WE E9NE 1999102900247 19991029 00247 WP 1999 10 29 TWAA9914503 1 19991024 A 3246 5930594523 WHEEL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN D INFLIGHT SEPARATION TO TAKEOFF 1 CE 05 9401W 53137 1462 DURING TAKEOFF, THE NUMBER 2 WHEEL ASSEMBLY FAILED. RUBBER FROM THE TIRE CAUSED DAMAGE TO THE LT LANDING GEAR, GEAR WIR ING, T/E FLAP AND THEN ENTERED THE LT ENGINE. A LOUD BANG WAS HEAR FROM THE ENGINE AND THE CREW SHUT IT DOWN. THE FLIG HT RETURNED TO BWI. REPLACED THE WHEEL ASEMBLY, AND REPAIRED THE DAMAGE, INCLUDING REPLACEMENT OF THE ENGINE FIRST STAG E FAN. CHECK-C 12-5-98 MCI. 2 L 7 2 4F 4 F RT A6WE E9NE 1999102900248 19991029 00248 NM 1999 10 29 TWAA9914504 1 19991025 A 3350 767 LAMP BOEING 757 757231 1384950 NM R4 DOORWAY FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 719TW 28487 THE EMERGENCY LIGHT FOR THE NUMBER 4 CABIN DOOR ON THE RT SIDE OF THE AIRCRAFT, WAS INOPERATIVE. REPLACED THE BULB. 2 L 7 2 4F RT A2NM 1999102900249 19991029 00249 WP 1999 10 29 TWAA9914505 1 19991021 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING CHECK-C, MAINT FOUND LONGERON 2L AT STA 1076 HAD A 1 INCH CRACK. SPLICED SECTION PER SRM 53-02, PAGE 18. 2 L 7 2 4F A6WE 1999102900250 19991029 00250 WP 1999 10 29 TWAA9914506 1 19991021 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING CHECK-C, MAINT FOUND A 1 INCH CRACK AT STA 1076, LONGERON 2R. SPLICED SECTION PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1999102900251 19991029 00251 NM 1999 10 29 HNAA9900138 1 19991024 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8201 2809001 NM RT EMER EXIT DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 997HA 1811 507 RIGHT FORWARD EMERGENCY EXIT FORE AND AFT EGRESS LIGHT INOP. REMOVED AND REPLACED RIGHT FORWARD EMERGENCY EXIT LIGHT BA TTERY PACK, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999102900252 19991029 00252 SO 1999 10 29 RAAA99E4029 1 19990510 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 502 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM WITH CORROSION AND HOLE DAMAGE, FS 502, LBL 22-26. REPAIRED AS PER SRM 53-2-4, M-54 NR 134. 2 L 7 4 4T 4A22 1999102900253 19991029 00253 SO 1999 10 29 RAAA99E4030 1 19990510 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 250-371 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON SEAT TRACK AT BBL 0, FS 250-371. REPLACED SEAT TRACK AS PER ECO 99-05 M -54 NR 135. 2 L 7 4 4T 4A22 1999102900254 19991029 00254 SO 1999 10 29 RAAA99E4031 1 19990510 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 250-371 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON SEAT TRACK AT FS 250-371 LBL 26. REPLACED SEAT TRACK AS PER ECO 99-05 M -54 NR 137. 2 L 7 4 4T 4A22 1999102900255 19991029 00255 SO 1999 10 29 RAAA99E4032 1 19990510 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 695-837. CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED #1 CHECK, FOUND SEAT TRACK LOCK LUGS CHIPPED & WORN @ FUS/STA 695-837 RBL 54. REPLACED SEAT TRACK AS PE R ECO 99-05 M-54 # 140. 2 L 7 4 4T 4A22 1999102900256 19991029 00256 SO 1999 10 29 RAAA99E4033 1 19990510 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 695-768 CHIPPED & WORN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK LOCK LUGS CHIPPED AND WORN AT FS 695-768 LBL 54. REPLACED SEAT TRACK AS P ER ECO 99-05 M-54 NR 142. 2 L 7 4 4T 4A22 1999102900257 19991029 00257 SO 1999 10 29 RAAA99E4034 1 19990510 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 695-768. CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK LOCK LUGS CHIPPED AND WORN AT FS 695-768 LBL 23. REPLACED SEAT TRACK AS E CO 99-05, M-54 NR 143. 2 L 7 4 4T 4A22 1999102900258 19991029 00258 SO 1999 10 29 RAAA99E4035 1 19990510 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO F/S 695-837 C HIPPED & WORN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOULD SEAT TRACK LOCK LUGS CHIPPED AND WORN AT FS 695-837, BBL 0. REPLACED SEAT TRACK AS P ER ECO 99-05 M-43 NR 144. 2 L 7 4 4T 4A22 1999102900259 19991029 00259 SO 1999 10 29 RAAA99E4036 1 19990511 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 787-837 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON SEAT TRACK AT FS 787-837 LBL 56. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 150. 2 L 7 4 4T 4A22 1999102900260 19991029 00260 SO 1999 10 29 RAAA99E4037 1 19990511 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 806-844 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON SEAT TRACK AT FS 806-844, LBL 26. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 151. 2 L 7 4 4T 4A22 1999102900261 19991029 00261 SO 1999 10 29 RAAA99E4038 1 19990511 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 844 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERES FLOORBEAM AT FS 844, BL 0 TO LBL 54. REPAIRED FLOORBEAM AS P ER SRM 53-2-4 M54 NR 155. 2 L 7 4 4T 4A22 1999102900262 19991029 00262 WP 1999 10 29 CALA9901417 1 19991018 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND AFT CARGO COMPARTMENT FRAME AT STA 1309, LONGERON 28L-28R CORRODED. REPAIR DOUBLERS AND SPLICES WERE I NSTALLED IAW SRM 51-10-4 AND 53-03, PAGE 4C, FIGURE 2A. 2 L 7 2 4F A6WE 1999102900263 19991029 00263 WP 1999 10 29 CALA9901418 1 19991015 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND FRAME IN E&E BAY AT STA 180 LONGERON 30 CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-3. A ROLLED Z-FRAME REPAIR SPLICE WAS INSTALLED IAW SRM 53-03, FIGURE 2A. 2 L 7 2 4F A6WE 1999102900264 19991029 00264 WP 1999 10 29 CALA9901419 1 19991018 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 798 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16802 49222 INSPECTION FOUND A 1 INCH CRACK IN RT MLG WHEEL WELL I/B KEEL FORWARD SUPPORT ANGLE AT FS 798, RBL 12. THE ANGLE WAS RE MOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, AND 51-30-3. 2 L 7 2 4F A6WE 1999102900265 19991029 00265 NM 1999 10 29 CALA9901420 1 19991018 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 967-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17328 23458 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 967-986, RBL 17, WL 208. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1999102900266 19991029 00266 NM 1999 10 29 CALA9901421 1 19991019 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 344-348 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 344-348. A NEW SECTION OF SEAT TRACK WAS SPLICED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999102900267 19991029 00267 WP 1999 10 29 CALA9901422 1 19991020 A 3350 60030451 POWER SUPPLY GRIMES DOUG DC9 DC982 3022082 WP CABIN INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93875 49125 INSPECTION FOUND CABIN OVERHEAD EMERGENCY LIGHTS FORWARD OF OVERWING EXITS INOPERATIVE. REMOVED AND REPLACED THE EMERGE NCY LIGHTS POWER SUPPLY AND OPERATION CHECKED GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 1999102900268 19991029 00268 NM 1999 10 29 CALA9901423 1 19991020 A 5347 SEAT TRACK BOEING 757 757224 1384958 NM BS 377-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13113 27555 INSPECTION FOUND I/B SEAT TRACK CORRODED AT BS 377-400, LBL 25 AND O/B SEAT TRACK WAS CORRODED AT BS 377-440, LBL 45. T HE SEAT TRACKS WERE REPLACED IAW SRM 53-10-00 AND BOEING DRAWING 141N5130. 2 L 7 2 4F RT A2NM 1999102900269 19991029 00269 NM 1999 10 29 CALA9901424 1 19991020 A 5320 INTERCOSTAL BOEING 757 757224 1384958 NM BS 1620-1640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13113 27555 INSPECTION FOUND INTERCOSTAL ON FLOOR STRUCTURE CORRODED AT BS 1620-1640. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWINGS 146N5300 AND 143N5554-6. 2 L 7 2 4F RT A2NM 1999102900270 19991029 00270 NM 1999 10 29 CALA9901425 1 19991022 A 5310 TIE STRAP BOEING 737 7373T0 1384582 NM STA 767-867 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND A .75 INCH CRACK IN AFT BAGGAGE BIN DOOR JAMB FORWARD CORNER TIE STRAP AT STA 767-867, RBL 26. THE STR AP WAS REPLACED IAW SRM 51-30-02. 2 L 7 2 4F RT A16WE 1999102900271 19991029 00271 NM 1999 10 29 CALA9901426 1 19991022 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17328 23458 INSPECTION FOUND FLOORBEAM CORRODED AT STA 360, RBL 52. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5330-02893 AND 53-00-51. 2 L 7 2 4F RT A16WE 1999102900272 19991029 00272 NM 1999 10 29 CALA9901427 1 19991022 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17328 23458 INSPECTION FOUND A 1/4 CRACK IN #1 ENGINE PYLON SKIN UPPER SURFACE AT PANEL 5727 CUTOUT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230. 2 L 7 2 4F RT A16WE 1999102900273 19991029 00273 NM 1999 10 29 CALA9901428 1 19991022 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016. A NEW UPPER T-CHORD WAS INSTALLED ON FLOORBEAM IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999102900274 19991029 00274 NM 1999 10 29 CALA9901429 1 19991023 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND FUSELAGE SKIN DENTED ON LT SIDE JUST AFT OF RADOME AND JUST BELOW STRINGER 19 LAP SEAM. THE DENTED ARE A WAS CUT OUT IAW SRM 53-30-3, PAGES 5, 6, & 8. A DOUBLER WAS INSTALLED IAW SRM 53-30-3, PAGE 163, 51-10-2, PAGE 1, AND 51-40-5, PAGE 5 & 6. 2 L 7 3 4F A3WE 1999102900275 19991029 00275 EA 1999 10 29 COMA9960644 1 19991014 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280-349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 13513 7038 FOUND CORROSION ON FLOOR CAPS LBL 27, LBL 9, RBL 9 AND RBL 27 FS 280 TO FS 349 AND FS 310 TO FS 349. PERFORMED MAJOR RE PAIR. REMOVED AND REPLACED FLOORBEAMS (P/N 601R31113-67) IAW REO 601R-53-00-027 , WVAC EO 601R-53-0414A AND WVAC EO 601 R-53-0419A. 2 L 7 2 4F RT A21EA 1999102900276 19991029 00276 EA 1999 10 29 COMA9960645 1 19991021 A 5210 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 978CA 7158 DURING CLIMBOUT OF CAE, THE CABIN DOOR OUTER HANDLE CAUTION MESSAGE ACTIVATED. AIRCRAFT RETURNED TO THE FIELD. INSPECT ED AND OPERATED CABIN DOOR HANDLE MECHANISM, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 1999102900277 19991029 00277 EA 1999 10 29 COMA9960646 1 19991023 A 5210 LATCH MECH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 CABIN DOOR WARNING MESSAGE.\NADJUSTED THE CABIN DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1999102900278 19991029 00278 EA 1999 10 29 COMA9960647 1 19991023 A 5270 CNDAIR CL600 CL6002B19 EA UNKNOWN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 931CA 7037 CABIN DOOR WARNING MESSAGE. REPAIRED WIRING CONNECTION P1M13 AT CABIN DOOR. 2 L 7 2 4F RT A21EA 1999102900279 19991029 00279 EA 1999 10 29 COMA9960648 1 19991023 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A COMA K NONE O OTHER CR CRUISE 1 SO 01 984CA 2054 7171 PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1999102900280 19991029 00280 EA 1999 10 29 COMA9960649 1 19991024 A 3030 7858062 ADSHC CNDAIR CL600 CL6002B19 EA LEFT INOP A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 936CA 13127 7043 PITOT BASE HEAT CAUTION MESSAGE.\NREPLACED THE ADSHC. 2 L 7 2 4F RT A21EA 1999102900281 19991029 00281 EA 1999 10 29 COMA9960650 1 19991022 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 971CA 7145 FLAPS FAILED AT ZERO DURING APPROACH. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999102900282 19991029 00282 1999 10 29 COMA9910166 4 19991021 A 3460 22312664A FDAU EMB 120 EMB120RT SO AVIONICS COMP MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 256CA 17922 120245 FDAU CIRCUIT BREAKER TRIPPED. REPLACED THE FDAU. 2 L 7 2 4T RT A31SO 1999102900283 19991029 00283 NM 1999 10 29 UPS99230982 1 19991023 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE:N/A LH INBD FLAP OUTBD TRACK CRACKED ***MRR FILED AS OPEN*** 2 L 7 3 4F A3WE 1999102900284 19991029 00284 NM 1999 10 29 UPS99230985 1 19991022 A 3350 LIGHT BOEING 727 72725C 138400H NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A COCKPIT EMERG LIGHT DOES NOT FLASH DURING TEST EXIT LIGHT TESTED GOOD PER TC3000 AND MM 2 L 7 3 4F A3WE 1999102900285 19991029 00285 NM 1999 10 29 UPS99430980 1 19991022 A 5220 SKIN BOEING 747 747123 1384873 NM R3 EMER EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A, R3 DOOR HAD A 5 INCH CRACK ON SKIN AND WAS LEAKING. FABRICATED AND INSTALLED DOUBLER PER SRM 52-00 -03. 2 L 7 4 4F A20WE 1999102900286 19991029 00286 NM 1999 10 29 UPS99430981 1 19991021 A 5210 SKIN BOEING 747 747123 1384873 NM R1 DOOR DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE:N/A, R1 DOOR SKIN PEELED BACK-DOOR LEAKING PROFUSELY ON LEADING EDGE BELOW FWD DOOR HINGE. DOOR BULGES OUT APPROX 1 INCH AND APPEARS TO BE IN ERNAL DAMAGE. *S/D* ASSIGNED ECA FORM 04927 TO IEM REPAIR ACCOMPLISHED IAW EO B 747-520-1 1894A DISSIMIAL METAL REPAIR TO BE ACCOMPLISHED BY NEXT C CHECK D180 797 ASSIGNED. 2 L 7 4 4F A20WE 1999102900287 19991029 00287 WP 1999 10 29 UPS99830976 1 19990908 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 105 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:S/V STA-105 FRAME CRACKED BOTTOM FWD OF NOSE. FAB REPAIR ANGLES AND FILLERS IAW REO 06767 DYE PENNED RE PAIR PARTS IAW MIL STD 15378, NO CRACKS NOTED ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC 8 51-1-20D. 2 L 7 4 4F RT 4A25 1999102900288 19991029 00288 WP 1999 10 29 UPS99830977 1 19990908 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 117 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:S/V, STA-117 FRAME CRACKED AT BOTTOM FWD OF NOSE GEAR. FABBED AND INSTALLED REPAIR IAW REA-O6756 DYE PE NNED REPAIR PARTS IAW ASTM-E-7417-95A. NO CRACKS NOTED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999102900289 19991029 00289 WP 1999 10 29 UPS99830978 1 19991022 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A, DURING MX INSPECTION EMERGENCY LIGHT FAILED TO TEST. *S/D* REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 1999102900290 19991029 00290 WP 1999 10 29 UPS99830979 1 19991025 A 5220 FASTENERS DOUG DC8 DC871F 302199D WP RT EMER EXIT MISSING A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:N/A, AFT RT EMERGENCY EXIT DOOR LWR EDGE HAS SEVEN MISSING FASTENERS. *S/D* REMOVED R5 DOOR, REPLACED NUT PLATE CHANNEL AND INSTALLED SCREWS IAW SRM 51-3-0. REINSTALLED DOOR REF LG 416910 ITEM 2. 2 L 7 4 4F RT 4A25 1999102900291 19991029 00291 WP 1999 10 29 UPS99830983 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 735 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1 L/H WING L/E UPPER SKIN CRACKED AT STA. XFS735.00. REPAIRED AREA I.A.W. SRM 57-2-1 FIG.38. 2 L 7 4 4F RT 4A25 1999102900292 19991029 00292 WP 1999 10 29 UPS99830984 1 19991001 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 766.25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C1, LEFT WING L/E UPPER SKIN AT XFS 766.25 & 785.0 WAS CORRODED BEYOND LIMITS. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW DH SK814-312. 2 L 7 4 4F RT 4A25 1999102900293 19991029 00293 1999 10 29 RAIA9910031 4 19991022 A 6122 89741016 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 427AM 12354 2206 876 7434-STL- RIGHT ENGINE ONLY MADE 84 PERCENT TORQUE. MAINTENANCE REPLACED RIGHT PROP GOVERNOR. 2 L 7 2 4T RT A56EU 1999102900294 19991029 00294 EU 1999 10 29 RAIA9910032 1 19991024 A 7712 31024766 TQ SIGNAL COND. BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 871JX 871 4711-LAX- LEFT TORQUE GAUGE ERRATIC. MAINTENANCE REPLACED TORQUE SIGNAL CONDITIONER FOR LEFT ENGINE. 2 L 7 2 4T RT A56EU 1999102900295 19991029 00295 WP 1999 10 29 CA990907014 1 19990829 A 2810 FUEL CELL ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA FUSELAGE CONTAMINATED W O OTHER W INADEQUATE Q C NR NOT REPORTED 1 CA L2497140A (CAN) WRONG FUEL ADDED FROM FUEL CACHES. 1 G 7 1 3O 3 O H11NM E295 1999102900296 19991029 00296 GL 1999 10 29 CA990907023 2 19990815 A 7322 23034702 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 3815 1AAC406 CAE822492 (CAN) FUEL CONTROL LEAKING AT IDLE ADJUSTMENT SCREW. THROTTLE CONTROL HAD NO EFFECT ON NR WHICH REMAINED AT 100 PERCENT DUE TO THE CONDITION. 1 G 7 1 3U 3 U H2SW E4CE 1999102900299 19991029 00299 EA 1999 10 29 CA990915002 1 19990806 A 7714 ST3086110 O RING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NL PROBE DETERIORATED W O OTHER K FLUID LOSS NR NOT REPORTED 1 CA 17522 3732 123150 901009 (CAN) O-RINGS DETERIORATED ON NL SENSOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900300 19991029 00300 EA 1999 10 29 CA990915003 1 19990823 A 6120 78249047 PCU DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PROPELLER LEAKING W O OTHER K FLUID LOSS IN INSP/MAINT 1 CA 5064 910749 901009 (CAN) LEAKING PCU. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900301 19991029 00301 NE 1999 10 29 CA990915011 2 19990814 A 7321 7898426009 ECU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE FAILED W O OTHER O OTHER CR CRUISE 1 CA 9993 3248 87093628 891130 (CAN) TORQUE FLUCTUATIONS, EEFCU REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900302 19991029 00302 NE 1999 10 29 CA990915014 2 19990817 A 7314 7863916 PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 11243 9385 F6300 120854 890709 (CAN) SHAFT SEAL LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900303 19991029 00303 NE 1999 10 29 CA990915021 3 19990829 A 6112 8022523 RELAY DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PROP DEICE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 6475 2237 123124 86978215 (CAN) RELAY 3061-K4 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900304 19991029 00304 WP 1999 10 29 CA990915037 1 19990830 A 3610 HOSE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN DAMAGED W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 CA 517958 (CAN) LOUD NOISE WITH HEAT REPORTED BEHIND SEAT 36A. FLOOR BECAME TOO HOT TO TOUCH. NR 2 PNEUMATIC SYSTEM SELECTED OFF , NOISE STOPPED, BUT AREA BETWEEN 36A AND LAVATORY BECAME HOTTER. PNEUMATIC ISOLATION VALVE 1-2 IN THE NORMAL POSITION (CLOSED). OVER A PERIOD OF 30 MINUTES, AREA BEGAN TO COOL. AIRCRAFT DIVERTED. FOUND AFT LAV/GALLEY VENT REGULATING L INE DAMAGED. LINE AND BULK CARGO HEAT VALVE REPLACED AND LEAK CHECK CARRIED OUT OK. 2 L 7 3 4F 4 F A22WE E23EA 1999102900305 19991029 00305 EU 1999 10 29 CA990915044 1 19990901 A 3232 125253 ACTUATOR MENASCO FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU MLG DOOR FAILED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 22118301 9301 (CAN) AIRCRAFT HAD TURNBACK DUE TO LOSS OF HYDRAULIC FLUID. LANDING GEAR DOOR ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A20EU E2EU 1999102900306 19991029 00306 GL 1999 10 29 CA990915052 2 19990825 A 7240 23030889 COMBUSTION CAN BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE821208 (CAN) CRACK FOUND IN OUTER COMBUSTION CAN RUNNING HORIZONTALLY IN ARM PIT AREA. CRACK RUNS THROUGH WELDED MESH PATCH. 1 G 7 1 3U 3 U H2SW E4CE 1999102900310 19991029 00310 NM 1999 10 29 CA990915058 1 19990819 A 5540 6573788501 STRUCTURE BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE RUDDER CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 60303 0741 687721 (CAN) RUDDER REMOVED FOR PAINTING AND BALANCING. WATER FOUND IN TRAILING EDGE OF RUDDER AT STA 121.64. WATER REMOVED A ND RUDDER REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 1999102900311 19991029 00311 SO 1999 10 29 CA990915062 1 19990827 A 8120 LW12463 TURBOCHARGER GARRTT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL ENGINE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 2078 WFL0127 L487461A DJ8764A (CAN) TURBOCHARGER FOUND SEIZED. NO FOD FOUND. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999102900312 19991029 00312 EU 1999 10 29 CA990915063 1 19990901 A 2910 4Q2395 LINE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ROTOL R4304 R2124304 EU HYDRAULIC SYSTEM FAILED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 19241 DRG41567 (CAN) IN CRUISE, BOTH HYDRAULIC FLOW LIGHTS WERE SEEN TO ILLUMINATE AND THE MAIN HYDRAULIC PRESSURE WAS SEEN TO FALL ON THE MAIN HYDRAULIC GAUGE. EMERGENCY LANDING GEAR LOWERING CARRIED OUT AND AN UNEVENTFUL LANDING CARRIED OUT. PORT RET RACTION JACK-UP LINE HAD BURST 3 INCHES FROM SKIN ADAPTOR. SLIGHT MISALIGNMENT OF BANJO FITTING ALLOWED THE HOSE TO CHA FE ON THE LANDING GEAR DOOR WHEN GEAR RETRACTED. FITTING ADJUSTED AND NEW HOSE INSTALLED. 2 L 7 2 3T 4 T A24EU A196 6 C P899 1999102900313 19991029 00313 SO 1999 10 29 CA990915072 2 19990909 A 8520 535661 CAMSHAFT CESSNA 310 310Q 2074242 CE CONT O470 IO470V 17026 SO MCAULY 2AF34C D2AF34C71 GL ENGINE SPALLING W K NONE O OTHER IN INSP/MAINT 1 CA 645 1484758VO 730584 (CAN) SEVERE SPALLNG OF REAR CAM LOBE. 1 L 7 2 3O 3 O 3A10 3E1 5 C P5EA 1999102900315 19991029 00315 NM 1999 10 29 CA990916003 1 19990901 A 2910 S270T23023 COUPLING BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RT HYD SYS BROKEN W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 30734 (CAN) DURING FLIGHT, CREW OBSERVED RT HYDRAULIC LOW PRESSURE AND QUANTITY LOW. AIRCRAFT LANDED. HIGH PRESSURE QUICK D ISCONNECT ON NR 2 ENGINE BROKEN IN TWO PIECES. FITTING REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999102900316 19991029 00316 WP 1999 10 29 CA990916007 1 19990805 A 5280 RIVET DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE LT MLG DOOR SHEARED W O OTHER J WARNING INDICATION LD LANDING 1 CA P654122D (CAN) ON GEAR DOWN SELECTION, LT DOOR DID NOT RETRACT. QRH PROCEDURE CARRIED OUT, AIRCRAFT LANDED. GEAR DOOR LATCH TOR QUE TUBE RIVET SHEARED. MINOR DAMAGE TO DOOR. SHEARED RIVET REPLACED WITH BOLT, RETRACTION TEST CARRIED OUT, SERVICEAB LE. 2 L 7 2 4F 4 F A6WE E2EA 1999102900317 19991029 00317 EA 1999 10 29 CA990916013 1 19990910 A 2913 NAS1601111 O-RING CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE HYDRAULIC PUMP LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) SUBMITTED BY BOMBARDIER AGAINST AIR LITTORAL (FRANCE). FR REG F-GPTI. EN ROUTE, THE CREW OBSERVED THE NR 3 HYDRA ULIC PRESSURE DROPPED TO ZERO PSI AND THAT THE QUANTITY HAD DROPPED TO ZERO. MAINTENANCE FOUND A HYDRAULIC LEAK AT THE HOUSING OF THE NR 3 AC MOTOR DRIVEN HYDRAULIC PUMP. THE OUTLET FITTING, O-RING WAS REPLACED 2 L 7 2 4F 4 F RT A21EA E15NE 1999102900318 19991029 00318 1999 10 29 CA990916016 4 19990827 A 2340 D04250J INTERPHONE BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE CABIN SHORT W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 687845 (CAN) DURING CLIMB, CREW HEARD RINGING CHIME AND THE CALL LIGHT WAS FLASHING INTERMITTENTLY. SMELL OF SMOKE WAS NOTICED FROM THE 3R COMMUNICATION PANEL AT R2 DOOR. WHEN DOOR OPENED, A SMALL FLAME WAS PRESENT ON THE ELECTRICAL PLUG OF THE PASSENGER ADDRESS INTERPHONE SYSTEM. SUSPECT WATER INFILTRATION FROM AN ICEBOX STORED IN THE COMPARTMENT. TEMPORARY REP AIR CARRIED OUT AS PER MM AND AIRCRAFT RETURNED TO SERVICE. AFFECTED PLUG REPLACED AND AFFECTED WIRES REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 1999102900320 19991029 00320 SW 1999 10 29 CA990916019 1 19990916 A 3242 212031 BRAKE BFGOODRICH SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313U303G 01514 WP HARTZL HCB3T HCB3TN5 GL NR 1 & 4 SEIZED W O OTHER O OTHER LD LANDING 1 CA P03551C BV4216 (CAN) ON LANDING, BOTH NR 1 AND NR 4 BRAKES SEIZED. SUPPLEMENTAL TEARDOWN INDICATED OVERHEATED BRAKES AND INCORRECT PAR T NUMBER BRAKE ADJUSTERS INSTALLED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 1999102900321 19991029 00321 NM 1999 10 29 CA990927008 1 19990907 A 3060 7826891 BRUSH BLOCK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 PROP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15677 120064 860404 (CAN) BRUSH BLOCK CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900322 19991029 00322 EA 1999 10 29 CA990927017 2 19990831 A 8530 CYLINDER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL NR 3 LEAKING W E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA 1153 L448161A DJ11547A (CAN) CRANKCASE CRACKED AT BOTTOM OF NR 3 CYLINDER. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999102900323 19991029 00323 SW 1999 10 29 CA990927020 1 19990714 A 7312 10544C HEATER BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA FUEL SYSTEM FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 1915 2738 60278 (CAN) THE ENGINE DRIVEN PUMP WAS UNABLE TO MAINTAIN FUEL PRESSURE WITH THE LOSS OF BOOST PUMP PRESSURE. THE CAUSE WAS F OUND TO BE FUEL HEATER PARTIAL BLOCKAGE. (FUNGI CONTAMINATION) . 1 G 7 1 4U 4 U H4SW E22EA 1999102900324 19991029 00324 NE 1999 10 29 CA990927021 2 19990909 A 7260 5040T12P01 BEARING SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE ACCESSORY DRIVE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 265 296005 (CAN) PINION BEARING WAS IN INITIAL STAGES OF FAILURE. 2 G 7 2 4U 4 U 1H15 1E3 1999102900326 19991029 00326 EA 1999 10 29 CA990927023 1 19990824 A 2620 1808325 SQUIB DHAV DHC7 DHC7103 2802710 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL FIRE BOTTLE DISCHARGED W K NONE O OTHER IN INSP/MAINT 1 CA PCE86591 237608 (CAN) DURING SCHEDULED MAINTENANCE, THE PORT WING AFT FIRE BOTTLE DISCHARGE DISK WAS FOUND TO BE MISSING. SUBSEQUENT IN SPECTION FOUND THE FIRE BOTTLE SQUIB FIRED, AND THE BOTTLE DISCHARGED. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 1999102900327 19991029 00327 GL 1999 10 29 CA990927028 2 19990215 A 7532 23053176 BLEED VALVE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA 56 FF12106 CAE830896 (CAN) BLEED VALVE NOT FUNCTIONING PROPERLY. 1 G 7 1 3U 3 U H3WE E4CE 1999102900328 19991029 00328 GL 1999 10 29 CA990927031 2 19990413 A 7200 6898735 ENGINE ALLSN BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL ENGINE BAY OVERSPEED W O OTHER O OTHER NR NOT REPORTED 1 CA CAT34895 CAE831797 (CAN) REPORTED OVERSPEED = 114 PERCENT. 1 G 7 1 3U 3 U H2SW E4CE 1999102900329 19991029 00329 EU 1999 10 29 CA990927037 2 19990825 A 7314 GD144 PUMP FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU FUEL SYSTEM LEAKING W C ABORTED TAKEOFF K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA 3690 9244 (CAN) FUEL LINE FROM HP FUEL PUMP TO FFR BLEW 0FF. 2 L 7 2 4F 4 F RT A20EU E2EU 1999102900330 19991029 00330 NM 1999 10 29 CA990927038 1 19990916 A 3250 86005 MANIFOLD DOWTY 83220001001 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NLG STEERING SYS LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 23355 3377 123076 891118 (CAN) DURING CRUISE FLIGHT, THE CREW GOT A HYDRAULICS ISOLATION VALVE CAUTION LIGHT. THE NR 2 HYDRAULIC SYSTEM SHOWED A QUANTITY OF ONLY 1 QUART OF FLUID REMAINING. THE AIRCRAFT RETURNED TO THE POINT OF DEPARTURE AND MADE A SAFE LANDING A FTER MAKING AN ALTERNATE LANDING GEAR EXTENSION. MAINTENANCE DETERMINED THAT 2 BOLTS HAD SHEARED AT THE STEERING MANIFO LD PRESSURE INLET, CAUSING THE COVER TO BECOME DISPLACED, WHICH ALLOWED THE LOSS OF ALL THE NR 2 HYDRAULIC SYSTEM FLUID. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900333 19991029 00333 SO 1999 10 29 CA990927050 1 19990601 A 8120 LW12463 SHAFT D PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL TURBOCHARGER FAILED W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA 515 L226368A DJ10178A (CAN) BROKEN TURBOSHAFT. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999102900334 19991029 00334 EA 1999 10 29 CA990927052 2 19990830 A 8530 CYLINDER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL LT ENGINE CRACKED W O OTHER O OTHER NR NOT REPORTED 1 CA 1706 L611361A DJ8079A (CAN) NR 5 CYLINDER CRACKED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999102900335 19991029 00335 NM 1999 10 29 CA990927058 1 19990907 A 5753 734380B TORQUE TUBE 734380B DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE TE FLAP FAILED W K NONE F J FLT CONT AFFECTED WARNING INDICATION IN INSP/MAINT 1 CA 24883 0277 121075 LH532 (CAN) AFTER PERFORMING MAINTENANCE ON THE FLAP SYSTEM, WHILE RETRACTING THE FLAPS, THE FLAP DRIVE CAUTION LIGHT ILLUMINA TED. INVESTIGATION REVEALED THE ELASTOMERIC COUPLINGS AT BOTH ENDS OF THE RIGHT INBOARD TORQUE TUBE HAD FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900336 19991029 00336 NM 1999 10 29 CA990927059 1 19990914 A 2820 82820107005 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 25152 120458 LH707 (CAN) FUEL WAS NOTICED DRIPPING FROM THE DRAIN PIPE ON THE RT AFT ENGINE NACELLE. INVESTIGATION REVEALED THE RE-FUEL LI NE, UNDER THE EXHAUST 'FINGERNAIL', HAD A SMALL PIN HOLE IN IT. THE HOLE WAS CAUSED BY CHAFING AGAINST THE INNER WIRE CO IL OF THE PROTECTIVE SHROUD (P/N DSC 427-1). 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900337 19991029 00337 EA 1999 10 29 CA990927067 1 19990921 A 2720 C6CFM121028 PEDAL DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13265 PCE42454 BU3969 (CAN) DURING SCHEDULED MAINTENANCE, A CRACK WAS FOUND IN THE PILOT'S RT RUDDER PEDAL. THE CRACK RAN FROM THE BOTTOM EDGE OF THE CASTING TO THE PIVOT BUSHING AND THEN TO THE UPPER FORWARD HI-SHEAR RIVET. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 1999102900338 19991029 00338 EU 1999 10 29 CA990927068 1 19990916 A 2440 PG1E1 WIRE AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE EXTERNAL POWER MELTED W K NONE O OTHER IN INSP/MAINT 1 CA 11392 245U237 (CAN) AFTER READING A SERVICE DIFFICULTY REPORT IN 'AVIATION MAINTENANCE' MAGAZINE, AN INVESTIGATION OF THE GROUND POWER PLUG CONNECTIONS REVEALED THE POSITIVE CABLE ON THE PLUG TO BE BURNED AND MELTED. THE PLUG PINS AND CONNECTIONS SHOWED NO SIGN OF DAMAGE. 2 L 7 2 4F 4 F RT A7EU E7EA 1999102900340 19991029 00340 EA 1999 10 29 CA990927076 1 19990813 A 2750 ECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807399 (CAN) ON APPROACH, FLAPS SELECTED FROM 8-20, LT FLAP STOPPED AT 13 AND RT AT 14. REPLACED FLAP SYSTEM ELECTRONIC UNIT AND RT BRAKE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999102900341 19991029 00341 EA 1999 10 29 CA990927081 1 19990814 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807399 (CAN) FLAP FAIL MESSAGE ON FINAL AFTER FLAPS APPEARED TO REACH 45 DEGREES. FLAP FLEX SHAFTS INSPECTED, LUBRUCATED. NR 3 RT ACTUATOR REPLACED AND SYSTEM RIGGED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999102900342 19991029 00342 NM 1999 10 29 CA990927094 1 19990913 A 3320 069672 FIXTURE BRUCE BR63031021 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN BURNT W K NONE O OTHER IN INSP/MAINT 1 CA 1465 TM120358 890709 (CAN) DURING SCHEDULED MAINTENANCE, THE CABIN FLOURESCENT LIGHT FIXTURE LAMPHOLDER ASSEMBLY WAS FOUND BURNED AND MELTED. SUBMITTER STATES THIS IS NOT AN ISOLATED CASE AND FEELS THE PROBLEM COULD LEAD TO AN IN-FLIGHT FIRE. SUBMITTER BELEI VES THE HEAT IS PRODUCED BY ELECTRICAL ARCING BETWEEN LAMPHOLDER SOCKETS AND LAMP PINS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900343 19991029 00343 NE 1999 10 29 CA991004003 2 19990918 A 7324 311851201A FLOW DIVIDER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 417 120854 890709 (CAN) FLOW DIVIDER AND DUMP VALVE PASSING EXCESS FUEL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900344 19991029 00344 NE 1999 10 29 CA991004008 2 19990909 A 7320 7982132001 ECU DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE ENGINE FAILED W O OTHER O OTHER IN INSP/MAINT 1 CA 17346 89072660 123113 901009 (CAN) ELECTRONIC CONTROL UNIT FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900345 19991029 00345 EA 1999 10 29 CA991004012 1 19990906 A 5753 734187B TORQUE TUBE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE TE FLAP DETERIORATED W K NONE O OTHER IN INSP/MAINT 1 CA 19228 0406 123133 920528 (CAN) DURING SCHEDULED MAINTENANCE, THE LEFT INBOARD FLAP PRIMARY DRIVE TORQUE TUBE WAS FOUND TO HAVE A DETERIORATED ELA STOMERIC COUPLING AT THE INBOARD END. A NEW TUBE ASSY WAS INSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900346 19991029 00346 NM 1999 10 29 CA991004013 1 19990916 A 3510 52590003206 COUPLING DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE OXYGEN SYSTEM LEAKING W O OTHER K FLUID LOSS CR CRUISE 1 CA 123124 901161 (CAN) FLIGHT CREW REPORTED OXYGEN SYSTEM LOSING PRESSURE. MAINTENANCE TRACED PROBLEM TO A LEAKING OXYGEN MASK HOSE COUP LING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900347 19991029 00347 NM 1999 10 29 CA991004014 1 19990918 A 7500 82110032011 PIPE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BLEED AIR SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 19655 123124 901161 (CAN) WHILE INVESTIGATING A HIGHER THAN AMBIENT OAT INDICATION, MAINTENANCE FOUND A LEAKING BLEED AIR PIPE. THE PIPE WA S REPLACED WITH A POST MOD 8/2613 PIPE ASSEMBLY PN 16032-511. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900348 19991029 00348 NE 1999 10 29 CA991004017 2 19990913 A 7321 7863916 FCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE INOPERATIVE W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA 5878 F12530 120083 901134 (CAN) HYDRAULIC MECH FUEL CONTROL UNIT SHOWED SIGNS OF SPIKING DURING POTENTIOMETER RESISTANCE CHECKS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900349 19991029 00349 NM 1999 10 29 CA991004018 1 19990919 A 7603 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT CONTAMINATED W E ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 CA 120373 870601 (CAN) WHILE STARTING NR 2 ENGINE, FLIGHT CREW NOTICED EXCESSIVE ENGINE TORQUE. MAINTENANCE TRACED THE PROBLEM TO MICROS WITCH 7611-S8 UNDER THE CONDITION LEVER CONSOLE. THE SWITCH WAS CONTAMINATED WITH COFFEE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900350 19991029 00350 EA 1999 10 29 CA991004019 2 19990915 A 8530 2813 STUD PIPER PA31 PA31 7103102 SO LYC O540 TIO540A1A 41532 EA HARTZL HCE3Y HCE3YR2 GL CYLINDER BROKEN W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 1857 RL33461A DJ8215A (CAN) CYLINDER STUDS FAILED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999102900351 19991029 00351 NE 1999 10 29 CA991004021 2 19990501 A 8530 39288 PUSH ROD DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HAMSTD 2D 2D30 NE NR 8 CYLINDER DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 200320 T34544 (CAN) BROKEN PUSH ROD. 1 H 7 1 3R 3 R A806 5E1 5 C P206 1999102900353 19991029 00353 EA 1999 10 29 CA991004025 1 19990923 A 2916 3810041104 RESERVOIR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 HYD SYS LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 123059 890527 (CAN) IN CRUISE FLIGHT, THE CREW GOT A LOW FLUID WARNING IN THE NR 2 HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT INCI DENT. MAINTENANCE DETERMINED THE NR 2 HYDRAULIC RESERVOIR WAS LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999102900355 19991029 00355 EA 1999 10 29 CA991004033 1 19990910 A 2841 INDICATOR DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL FUEL QUANTITY MALFUNCTIONED W O OTHER O OTHER CR CRUISE 1 CA PCE40393 BU4586 (CAN) ERRATIC FUEL QUANTITY DURING FLIGHT. NR 3-4 TRANSMITTERS AND INDICATOR REPLACED. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 1999102900356 19991029 00356 GL 1999 10 29 CA991004034 3 19990921 A 6111 A3496 SPRING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL PROPELLER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 167 PCE32570 FW1187 (CAN) LIGHTNING STRIKE SUSPECT IN CAUSING PART DAMAGE. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 1999102900357 19991029 00357 EA 1999 10 29 CA991004039 1 19990918 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE TE FLAP FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) UNSCHEDULED LANDING FOR FLAP FAIL AFTER TAKEOFF. BRAKE POSITION SENSOR REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999102900361 19991029 00361 EA 1999 10 29 CA991004043 1 19990925 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NLG FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) GEAR DISAGREE CAPTION ON GEAR UP SELECTION. NOSE GEAR SELECTOR VALVE REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999102900363 19991029 00363 EA 1999 10 29 CA991004054 2 19990920 A 7314 PUMP PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE2Y HCE2YR2 GL LT ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 254 L161761 CJ505 (CAN) FUEL PRESSURE BELOW SPECIFICATIONS. 1 L 7 2 3O 3 O A20SO E14EA 5 C P9EA 1999102900364 19991029 00364 EA 1999 10 29 CA991004056 2 19990914 A 8500 76770 BRACKET PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE2Y HCE2YR2 GL REAR ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 625 L161761 CJ505 (CAN) BRACKET IMPROPERLY INSTALLED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P9EA 1999102900365 19991029 00365 GL 1999 10 29 CA991004058 2 19990921 A 7314 2300314 O-RING BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL FUEL PUMP WORN W K NONE O OTHER IN INSP/MAINT 1 CA 74 CAE835628 (CAN) FUEL PUMP NOISY ON SPOOL-UP AND SHUT DOWN. 1 G 7 2 3U 3 U H3EU E4CE 1999102900366 19991029 00366 NM 1999 10 29 CA991007015 1 19990923 A 2917 72909 REGULATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE HYDRAULIC SYSTEM LEAKING W O OTHER J WARNING INDICATION DE DESCENT 1 CA 28215 709396 (CAN) AFTER 4 HOURS OF FLIGHT, STARTED DESCENT, NR 1 HYDRAULIC PRESSURE LOW LIGHT ON. EMERGENCY CHECK LIST CARRIED OUT , THEN THE NR 2 HYDRAULIC LOW PRESSURE LIGHT ON. A HYDRAULIC PRESSURE WENT TO 35 PSI. NO NOTICEABLE HYD FLUID LOSS. E MERGENCY DECLARED. AIRCRAFT LANDED AND STOPPED ON RUNWAY. REPLACED NR 2 ENGINE CASE RETURN FILTER, HYD RESEVOIR AIR PR ESS REGULATOR. 2 L 7 2 4F 4 F A16WE E2EA 1999102900367 19991029 00367 WP 1999 10 29 CA991007016 1 19990929 A 5713 STRINGER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE LT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 84607 517958 (CAN) FOUND LEFT WING STRINGER 41 CRACKED. AIRCRAFT FERRIED FOR REPAIR. 2 L 7 3 4F 4 F A22WE E23EA 1999102900368 19991029 00368 NM 1999 10 29 CA991007017 1 19990929 A 2781 106122629 SENSOR BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE LE FLAP FAULTY W O OTHER J WARNING INDICATION AP APPROACH 1 CA 674313 (CAN) ON APPROACH, NR 4 LEADING EDGE IN-TRANSIT LIGHT ON, FORWARD PANEL LEADING EDGE TRANSIT ON ALSO. DUE FLAP DISAGREE AND SHORT LANDING RUNWAY, EMERGENCY DECLARED. AIRCRAFT LANDED OK. NR 4 LEADING EDGE MID EXTEND SENSOR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999102900369 19991029 00369 NM 1999 10 29 CA991007018 1 19990929 A 3260 LIGHT BOEING 767 767383 1385214 NM GE CF6 CF680C2B6 30025 NE MLG FAILED W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA 702610 (CAN) NO INDICATION OF NOSE GEAR DOWN. REPLACED LAMPS, STILL U/S. FLY-BY CONFIRMED GEAR DOWN. NOSE GEAR LIGHT CONTACT S CLAEANED AND BULB REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 1999102900370 19991029 00370 EA 1999 10 29 CA991007025 2 19990903 A 8520 AL75060 BOLT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL NR 3 ROD FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1152 L448161A DJ11547A (CAN) NR 3 CONNECTING ROD BOLT FAILED. CAUSE UNKNOWN AT THIS TIME. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999102900371 19991029 00371 GL 1999 10 29 CA991007037 2 19990314 A 7314 23034702 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1826 1AAC2645 CAE820180B (CAN) FUEL LEAKING FROM OVERBOARD DRAIN. 1 G 7 1 3U 3 U H2SW E4CE 1999102900372 19991029 00372 GL 1999 10 29 CA991007038 2 19990916 A 7313 6898734 NOZZLE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL 1ST STAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11731 48606 CAT30674P CAE820180B (CAN) FIRST STAGE NOZZLE FOUND CRACKED ON THE OUTER BAND AT APPROXIMATLY 5 O'CLOCK POSITION. 1 G 7 1 3U 3 U H2SW E4CE 1999102900375 19991029 00375 GL 1999 10 29 CA991007049 2 19990507 A 7200 6898735 ENGINE ALLSN BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE BAY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 19839 398 CAT33984 CAE823527 (CAN) TURBINE REMOVED FOR EXESSIVE OIL CONSUMPTION. 1 G 7 1 3U 3 U H2SW E4CE 1999102900376 19991029 00376 GL 1999 10 29 CA991007057 2 19990604 A 7240 6870992 COMBUSTION CASE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 32439 CAE836260 (CAN) COMBUSION CASE RECEIVED WITH THE IGNITOR HOLE DIMMENSION UNDER SIZED BY .25 INCH. 1 G 7 2 3U 3 U H3EU E4CE 1999102900377 19991029 00377 GL 1999 10 29 CA991007058 2 19990607 A 7240 6870992 COMBUSTION CASE ALLSN BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 32040 CAE836260 (CAN) CRACK FOUND IN ARMPIT AREA OF THJE OUTER COMBUSTION CASE. 1 G 7 2 3U 3 U H3EU E4CE 1999102900378 19991029 00378 GL 1999 10 29 CA991007059 2 19990615 A 7321 23057344 FCU BENDIX BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1925 333650 CAE830542 (CAN) FCU CUT FUEL OFF AT 24 DEGREES RATHER THAN 10 DEGREES. 1 G 7 1 3U 3 U H2SW E4CE 1999102900379 19991029 00379 EA 1999 10 29 CA991007061 1 19990702 A 2821 400ST01P03 FUEL FILTER GE CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE FUEL SYSTEM CLOGGED W K NONE O OTHER IN INSP/MAINT 1 CA 409 9387 295059 (CAN) FUEL FILTERS BLOCKED WITH ALLUMINUM, FROM PURIFIER WEAR. 2 G 7 2 4U 4 U H8EA 1E3 1999102900380 19991029 00380 WP 1999 10 29 CA991007062 2 19990918 A 7230 31070511 SEAL BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP HARTZL HCB4T HCB4TN5 GL LT ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1552 P27035 C0A3796 (CAN) OIL FOUND IN AIR INTAKE AND ON COMP. IMPELLOR. SEAL KIT REPLACED 1 L 7 2 4T 4 T A14CE E2WE 6 C P40EA 1999102900383 19991029 00383 CE 1999 10 29 CA991007071 1 19991007 A 3230 504100112 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520MB 17032 SO MCAULY 3AF32C 3AF32C87 GL RT MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 10165 210906 773849 (CAN) BELLCRANK ATTACH BOLT AND TRUNNION ATTACH LUGS FAILED. BELLCRANK LOWER AFT LUG ALSO FAILED RESULTING IN THE SIDE BRACE NOT LOCKING AND ALLOWING THE RIGHT GEAR TO COLLAPSE ON LANDING. SUBMITTER STATES THAT THE LANDING GEAR WAS INDICA TED AS BEING SAFE BY THE ILLUMINATION OF THE DOWN AND LOCKED (GREEN) INDICATOR LIGHT. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 1999102900385 19991029 00385 NM 1999 10 29 CA991007087 1 19990925 A 3221 69181946 BRACKET BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 689961 (CAN) NLG ACTUATOR UPPER SUPPORT BRACKET CRACKED AT TRUNNION SUPPORT LT AND RT LOWER ATTACH HOLES CRACKED. REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1999102900386 19991029 00386 NM 1999 10 29 CA991007091 1 19990928 A 5551 10618841 BEARING BOEING 65727961 BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE HORIZ STABILIZER SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA BNJ106 666036 (CAN) DURING INSPECTION OF HORIZONTAL STABILIZER FOR EXCESSIVE PLAY IN THE LT AFT ATTACH POINT. ON REMOVAL, THE LT BEAR ING WAS FOUND SEIZED AND ALLOWED THE ANTI-LOCKING RING TO MOVE CAUSING DAMAGE TO THE STABILIZER FITTING. MANUFACTURER N OTIFIED AWAITING REPAIR OR REPLACEMENT INSTRUCTIONS. 2 L 7 3 4F 4 F A3WE E2EA 1999102900387 19991029 00387 EU 1999 10 29 CA991007092 1 19990930 A 2110 F210R16774 CONNECTING ROD AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE7312 01518 WP AIR DISTRIBUTION FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1719 A0850453 P73114C (CAN) COMPRESSOR CONNECTING ROD FAILURE AT JOURNAL. 2 L 7 2 4F 4 F A33EU E6WE 1999102900388 19991029 00388 1999 10 29 CA991008001 4 19990730 A 3417 CONNECTOR HG1804312 BOEING 737 7372E1 138448F NM PWA JT8 JT8D9A 52048 NE ADC DAMAGED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA A117076 665978 (CAN) AUTOPILOT DISCONNECTED, EXPERIENCED DIFFICULTY CONTROLLING AIRCRAFT. REQUIRED 20 DEGREES OF RT AILERON TO MAINTAI N LEVEL FLIGHT. AIR DATA CONNECTOR PIN 26 BENT ACROSS PINS 23, 24 AND PIN 25 BROKEN OFF. REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 1999102900389 19991029 00389 GL 1999 10 29 CA991008002 2 19990824 A 7310 6895832 LINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FUEL SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA CAE890165S (CAN) FUEL LINE CRACKED AT FERREL PRIOR TO FUEL FILTER. 1 G 7 2 3U 3 U H1NE E1GL 1999102900390 19991029 00390 EU 1999 10 29 CA991008004 2 19990917 A 7240 BLADE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 1 ENGINE BENT W K NONE O OTHER IN INSP/MAINT 1 CA 9238 (CAN) LP1 AND LP2 TURBINE BLADE FAILED. 2 L 7 2 4F 4 F RT A20EU E2EU 1999102900391 19991029 00391 NM 1999 10 29 CA991008006 1 19990925 A 5610 7561090002 WINDOW BOEING 737 7372E1 138448F NM PWA JT8 JT8D9A 52048 NE COCKPIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA 5266 665978 (CAN) DURING DESCENT, F/O COCKPIT WINDOW CRACKED. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999102900392 19991029 00392 NM 1999 10 29 CA991008008 1 19990911 A 2432 BATTERY BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE APU FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA P709633 (CAN) ON APPLICATION OF GROUND SERVICE POWER TO AIRCRAFT, BURNING SMELL REPORTED IN AIRCRAFT CABIN. TRUCKS CALLED. APU BATTERY FOUND TWO CELLS MELTED AND BATTERY SHOWING SIGNS OF OVERHEAT. REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999102900399 19991029 00399 WP 1999 10 29 AALA991456 1 19990827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - NR 6 SEAT TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUS PER AARD 53-20-00-10. TST: 45,407 HOURS. CYCLES: 24,7 73. (X) 2 L 7 2 4F A6WE 1999102900400 19991029 00400 WP 1999 10 29 AALA991455 1 19990827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 734 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - NR 6 SET TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUS PER AARD 53-20-00-10. TST: 45,407 HOURS. CYCLES: 24,77 3. (X) 2 L 7 2 4F A6WE 1999102900401 19991029 00401 WP 1999 10 29 AALA991467 1 19990927 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP FRAME 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 262AA 49290 TUL - DOUBLER PLATE CORRODED 1 INCH BY 1 INCH FAYING SURFACE. INSTALLED NEW OUTFLOW VALVE FUSE SKIN DOUBLER PER ESO 805 59 AND DWG 5936021. TST: 44,040 HOURS. CYCLES: 24,199. (X) 2 L 7 2 4F A6WE 1999102900402 19991029 00402 EU 1999 10 29 AALA991416 1 19990917 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7055A 462 TUL - STR 35R CORRODED AT FRAME 65. REMOVED AND REPLACED CORRODED STRINGER PER SRM 53-10-18. TST: 32,012.26 HOURS. C YCLES: 12,872. (X) 2 L 7 2 4F RT A35EU 1999102900403 19991029 00403 EU 1999 10 29 AALA991436 1 19990921 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAMES 68-69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7055A 462 TUL - CORROSION ON STR 43L BETWEEN FRAMES 68-69. REPLACED STRINGER PER SRM 53-10-14. TST: 32,012.26. CYCLES: 12,872. (X) 2 L 7 2 4F RT A35EU 1999102900404 19991029 00404 EU 1999 10 29 AALA991448 1 19990915 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 18 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7055A 462 TUL- CORROSION ON FLOORBOARD SUPPORT AT STA 18R. INSTALLED NEW LONGITUDINAL BEAM 'E' RT PART NR A5327920720151 FROM FRA ME 74/75 THROUGH FRAME 80. REF: 51-72-10-0 SRM. TST: 32,012.26 HOURS. CYCLES: 12,872. (X) 2 L 7 2 4F RT A35EU 1999102900405 19991029 00405 EU 1999 10 29 AALA991400 1 19990915 A 5320 4081387 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7055A 462 TUL - FLOORBOARD SUPPORT AFT OF FRAME 73 HAS CORROSION AT STA 73R UNDER LAVATORY 2. REMOVED DAMAGED SUPPORT. INSTALLE D BLOCKS ON NEW SUPPORT AND INSTALLED ASSY. REF: A300 SRM 51-72-10. TST: 32,012.26 HOURS. CYCLES: 12,872. (X) 2 L 7 2 4F RT A35EU 1999102900406 19991029 00406 EU 1999 10 29 AALA991399 1 19990915 A 5320 5467687 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7055A 462 TUL - LAVATORY L SUPPORT HAS CORROSION FROM FRAME 30 TO FRAME 33 BETWEEN SEAT TRACKS B ANC C. COMPLETED CORROSION REPA IR AS REQUIRED PER SRM. REMOVED AND REPLACED AS DESCRIBED IN SRM 51-72-10-0. TST: 32,012.26. CYCLES: 12,872. (X) 2 L 7 2 4F RT A35EU 1999102900407 19991029 00407 WP 1999 10 29 AALA991490 1 19990924 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - NR 3 SEAT TRACK STA 1174 HAS CORROSION. BLENDED CORROSION, INSTALLED PLUG PER SRM 53-05 PART 1 FIG 4A. ALODINED AND PAINTED PER SRM 51-10-1. TST: 45,869 HOURS. CYCLES: 25,467. (X) 2 L 7 2 4F A6WE 1999102900408 19991029 00408 WP 1999 10 29 AALA991489 1 19990922 A 5320 SPLICE DOUG DC9 DC982 3022082 WP BS 579 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - CORROSION AROUND HI-LOKS IN LONGERON SPLICE. REMOVED AND REPLACED SPLICE PART MADE IN HOUSE PER AARD INTRO PAGE 8 SPLICE REPLACEMENT PER SRM 53-02. TST: 45,869.2 HOURS. CYCLES: 25,467. (X) 2 L 7 2 4F A6WE 1999102900409 19991029 00409 WP 1999 10 29 AALA991475 1 19990927 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7508 49802 TUL - CORROSION AND SCRATCHES IN FUSELAGE SKIN AROUND LOWER ANTENNA CUT OUT STA 402 BETWEEN LONGERON 30 AND LONGERON 29L . (REF: E-58 NR 3097727). REMOVED CORROSION AND BLENDED SCRATCHES AT LOWER ANTENNA CUT-OUT STA 402. TST: 29,797.31 HOURS. CYCLES: 15,463. (X) 2 L 7 2 4F A6WE 1999102900410 19991029 00410 WP 1999 10 29 AALA991485 1 19990927 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7508 49802 TUL - CORROSION AND DEEP SCRATCHES IN FUSELAGE SKIN AROUND LOWER ANTENNA CUT-OUT STA 380 BETWEEN LONGERON 30 AND LONGERO N 29L (REF: E58 NR 3097726). REMOVED CORROSION AT LOWER ANTENNA CUT-OUT STA 380. DYE CHECKED SCRATCH PER ESO 80559 DA TED 9-29-99. NO CRACKS FOUND. (X) 2 L 7 2 4F A6WE 1999102900411 19991029 00411 WP 1999 10 29 AALA991506 1 19991001 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP BS 200-218 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 262AA 49290 TUL - CORROSION OUT OF LIMITS ON SUB-FLOOR FORWARD AND INBOARD OF NR 6 SEAT TRACK STA 200 - STA 218. INSTALLED NEW CUSP SECTION (SUB-FLOOR) STA 200 - STA 218 PER AARD 53-00-00-02 INBOARD NR 6 SEAT TRACK. TST: 44,040 HOURS. CYCLES: 24,1 99. (X) 2 L 7 2 4F A6WE 1999102900412 19991029 00412 WP 1999 10 29 AALA991487 1 19990930 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 235 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 262AA 49290 TUL - FORWARD LEFT FUSELAGE SKIN DOUBLER GOUGED AT STA 235, LONGERON 18L. REMOVED EXISITNG REPAIR DOUBLER. CUT-OUT SE CTION OF FUSELAGE SKIN. DYE CHECKED CUT-OUT AREA. NO CRACKS NOTED. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-04, FIG 12B. TST: 44,040 HOURS. CYCLES: 24,199. (X) 2 L 7 2 4F A6WE 1999102900413 19991029 00413 NM 1999 10 29 AALA991463 1 19990927 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 35B BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39367 25194 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 35B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CO NNECTOR AT SEAT 35B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900414 19991029 00414 NM 1999 10 29 AALA991502 1 19991004 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT MARKERS AT SEVERAL SEATS INOPERATIVE. SECURED EMERGENCY E XIT SEAT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900415 19991029 00415 NM 1999 10 29 AALA991478 1 19991001 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645AA 24603 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS FROM 1R DOOR TO 2R DOOR INOPERATIV E. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999102900416 19991029 00416 NM 1999 10 29 AALA991480 1 19990925 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 685AA 25342 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS RIGHT SIDE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999102900417 19991029 00417 NM 1999 10 29 AALA991482 1 19991002 A 3350 MS252575 LIGHT WEBER BOEING 767 767323 1385205 NM G4 GALLEY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388AA 27448 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE G4 GALLEY EMERGENCY EXIT FLOODLIGHT INOPERATIVE. REPLACED RIGHT SIDE G4 GALLEY EMERGENCY EXIT FLOOD LIST. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900418 19991029 00418 NM 1999 10 29 AALA991483 1 19991002 A 3350 0201922001 SOCKET BOEING 767 767323 1385205 NM ROW 29B DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39367 25194 SFO - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT SEAT LIGHTS AT 29B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT S OCKET AT SEAT 29B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900419 19991029 00419 NM 1999 10 29 AALA991484 1 19991002 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM ROW 35B DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39367 25194 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 35B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT C ONNECTOR AT SEAT 35B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900420 19991029 00420 NM 1999 10 29 AALA991500 1 19991003 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372AA 25199 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SEAT LIGHTS FROM 32 TO 41 AB INOPERATIVE. REPLACED EMERGENCY EXIT SEA T LIGHT ASSY DUE TO SHORTED WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900421 19991029 00421 NM 1999 10 29 AALA991432 1 19990922 A 3350 B973521385 LIGHT BOEING 767 767323 1385205 NM ROW 23H DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389AA 27449 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED PATH LIGHT AT 23H INOPERATIVE. REPLACED EMERGENCY EXIT SEAT MOUNTED PATH LIGHT AT SEAT 23H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900422 19991029 00422 NM 1999 10 29 AALA991433 1 19990922 A 3350 B973521385 LIGHT BOEING 767 767323 1385205 NM ROW 41B DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389AA 27449 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED PATH LIGHT AT 41B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT MOUNTED PATH LIGHT AT SEAT 41B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900423 19991029 00423 NM 1999 10 29 AALA991444 1 19990924 A 3350 LAMP BOEING 767 767323 1385205 NM LT EMERG EXIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. SECURED LAMP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900424 19991029 00424 NM 1999 10 29 AALA991446 1 19990925 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 685AA 25342 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT EXIT IN FIRST CLASS INOPERATIVE. REPLACED EMERG ENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999102900425 19991029 00425 NM 1999 10 29 AALA991447 1 19990924 A 3397 WIRE BOEING 767 767223 1385123 NM ROW 17 HJ BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339AA 22336 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT 17 HJ TO 30 HJ INOPERATIVE. REPAIRED WIRES AT 17 HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900426 19991029 00426 NM 1999 10 29 AALA991469 1 19990924 A 3397 WIRE BOEING 767 767323 1385205 NM ROWS 25 AND 30 SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362AA 24043 SFO - DURING OVERNIGHT MAINTENANCE, LEFT SIDE COACH EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRES TO EMERGENCY EXIT LIGHTS AT 25 AND 30. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999102900427 19991029 00427 WP 1999 10 29 AALA991477 1 19990930 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 478AA 49653 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED WIRE ON EME RGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900428 19991029 00428 WP 1999 10 29 AALA991509 1 19991005 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 20 D DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 410AA 49321 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT 20D INOPERATIVE. REPLACED EMERGENCY EXIT FLOO R PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900429 19991029 00429 WP 1999 10 29 AALA991505 1 19991004 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 475AA 49650 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE ON FOR WARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900430 19991029 00430 WP 1999 10 29 AALA991504 1 19991004 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 210AA 49161 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE ON FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900431 19991029 00431 WP 1999 10 29 AALA991435 1 19990922 A 2620 AAP2898 EXTINGUISHER DOUG DC9 DC982 3022082 WP TAIL DEFECTIVE A AALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 405A 49316 BNA - ON POWERING UP THE AIRCRAFT FOR FIRST FLIGHT, NR 2 AGENT LOW LIGHT WAS ILLUMINATED FOR FIRE PROTECTION SYSTEM. RE PLACED FIRE EXTINGUISHER BOTTLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900432 19991029 00432 WP 1999 10 29 AALA991408 1 19990919 A 4990 5940405503 APU DOUG DC9 DC982 3022082 WP TAIL LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 480AA BBGJSKW 49655 ORD - FLT 0453 - AFTER TAKEOFF ORD, SMOKE WAS DETECTED IN THE CABIN. FLIGHT ATTENDANTS NOTED SMOKE IN THE CABIN AND COC KPIT CREW EXPERIENCED SMOKE IN THE COCKPIT WITH THE SMELL OF BURNING OIL OR RUBBER. AIR CONDITIONING PACKS WERE TURNED OFF IMMEIDATELY; AFTER PACKS WERE TURNED OFF, IT APPEARED THAT NO FURTHER SMOKE WAS PRODUCED, BUT SMOKE REMAINED IN THE AIRCRAFT. AIR INTERRUPTED AND LANDED ORD WITHOUT INCIDENT. APU IS LEAKING OIL. REPLACED APU. ACCOMPLISHED LEFT AND R IGHT PACK BURN IAW MM. REPLACED COALESCER BAGS IAW MM. OPERATION AND LEAK CHECKS NORMAL. SYSTEM GROUND CHECKED, NORMA L OPERATION. (X) 2 L 7 2 4F A6WE 1999102900433 19991029 00433 WP 1999 10 29 AALA991442 1 19990922 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 208AA 49159 DFW - DURING OVERNIGHT MAINTENANCE, MID-CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED MID-CABIN EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900434 19991029 00434 WP 1999 10 29 AALA991449 1 19990926 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 33 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 464AA 49594 DFW - DURING OVERNIGHT MAINTENANCE, SEVERAL SECTIONS OF EMERGENCY EXIT FLOOR PATH TRACK LIGHTING INOPERATIVE. REPAIRED WIRE SPLICE AT ROW 33. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900435 19991029 00435 WP 1999 10 29 AALA991471 1 19990928 A 3230 59164605509 VALVE DOUG DC9 DC982 3022082 WP LANDING GEAR DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 7522A CAN042 49899 DFW - FLT 1739 - ON APPROACH DFW, LANDING GEAR INDICATED ALL THREE RED UPON LOWERING GEAR HANDLE. BOTH HYDRAULIC QUANTI TY AND PRESSURE WAS NORMAL. PERFORMED EMERGENCY GEAR EXTENSION ACCORDING TO THE OPERATING MANUAL. VISUALLY VERIFIED LA NDING GEAR DOWN AND LOCKED THROUGH PORT. LANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL VALVE. ACCOMPLISH ED GEAR SWING AND LEAK CHECK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999102900436 19991029 00436 NM 1999 10 29 USAA991027 1 19990924 A 5330 SKIN BOEING 737 737201 1384454 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 55011 21667 CLT - DURING A RON VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 2 INCH BY 8 INCH AT BS 500B PLUS 14 INCHES, STR 28R SKIN. DAMAGE CUT-OUT AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-03 FIG 6. (X) 2 L 7 2 4F A16WE 1999102900437 19991029 00437 NM 1999 10 29 USAA991028 1 19990924 A 5313 6562125502 STRINGER BOEING 737 737201 1384454 NM BS 500B CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 55011 21667 CLT - DURING A RON VISUAL INSPECTION FOUND CORROSION 9 INCHES BY 2 INCHES BY .075 INCH AT BS 500B PLUS 14 INCHES, STR 28 R STRINGER (KEEL BEAM). CORROSION LEVEL 2. REMOVED CORROSION, INSTALLED KEEL BEAM REPAIR ANGLES AND SHIMS PER EA 65660 . (X) 2 L 7 2 4F A16WE 1999102900438 19991029 00438 NM 1999 10 29 USAA991025 1 19990925 A 5240 6545871523 SKIN BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 48988 22353 TPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN UPPER AFT CORNER OF TOP HINGE CUT-OUT SERVICE DOO R SKIN. INSTALLED DOUBLER PER TR 52-40-03A FIG 2. (X) 2 L 7 2 4F A16WE 1999102900439 19991029 00439 NM 1999 10 29 USAA991070 1 19991005 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 40206 23856 TPA - DURING CX-5 CHECK EDDY CURRENT AND VISUAL INSPECTION, FOUND A .3750 INCH CRACK IN FUSELAGE SKIN AT STA 380 AFT OF EQUIPMENT COOLING DUCT CUT-OUT. INSTALLED REPAIR DOUBLER PER TR 53-30-07 AND DRG 65C33930. (X) 2 L 7 2 4F RT A16WE 1999102900440 19991029 00440 NM 1999 10 29 USAA991058 1 19990930 A 5330 SKIN BOEING 737 737201 1384454 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 45984 22758 TPA - DURING CX-1 CHECK EDDY CURRENT, FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 787, STR 17L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (X) 2 L 7 2 4F A16WE 1999102900441 19991029 00441 NM 1999 10 29 USAA991062 1 19990930 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 55329 21665 CLT - DURING RON VISUAL INSPECTION, FOUND A 2.7 INCH CRACK AT BS 727A PLUS 8 INCHES, 0.5 INCH ABOVE STR 19L FUSELAGE SKI N. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3 FIG 6. (X) 2 L 7 2 4F A16WE 1999102900442 19991029 00442 NM 1999 10 29 USAA991063 1 19990930 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 55329 21665 CLT - DURING RON VISUAL INSPECTION, FOUND A 1.6 INCH CRACK AT BS 727 PLUS 17 INCHES, 1.75 INCHES ABOVE STR 18L SKIN. IN STALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1999102900443 19991029 00443 NM 1999 10 29 USAA991064 1 19990930 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 55329 21665 CLT - DURING RON VISUAL INSPECTION FOUND A 2.4 INCH CRACK AT BS 727A PLUS 8 INCHES, 0.5 INCH ABOVE STR 18L SKIN. INSTAL LED REPAIR DOUBLER AND FILLER PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1999102900444 19991029 00444 NM 1999 10 29 USAA991065 1 19990930 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 55329 21665 CLT - DURING RON VISUAL INSPECTION, FOUND A 0.9 INCH CRACK AT BS 727A PLUS 17.5 INCHES , 0.5 INCH ABOVE STR 18L SKIN. I NSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-3-3 FIG 6. (X) 2 L 7 2 4F A16WE 1999102900445 19991029 00445 NM 1999 10 29 USAA991066 1 19990930 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 55329 21665 CLT - DURING RON VISUAL INSPECTION, FOUND A 1.2 INCH CRACK AT BS 727A PLUS 3 INCHES, 0.5 INCH BELOW STR 18L SKIN. INSTA LLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1999102900446 19991029 00446 NM 1999 10 29 USAA991067 1 19990930 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 55329 21665 CLT - DURING RON VISUAL INSPECTION, FOUND A 1.2 INCH CRACK AT BS 727B PLUS 18 INCHES, 0.4 INCH ABOVE STR 18L FUSELAGE SK IN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3 FIG 6. (X) 2 L 7 2 4F A16WE 1999102900447 19991029 00447 NM 1999 10 29 USAA991026 1 19990925 A 5313 6546567503 STRINGER BOEING 737 737201 1384454 NM BS 930 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 48988 22353 TPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA LOCATED UNDER STR 27R, STA 930, CORROSION LEVEL 1. R EPLACED CORRODED AREA PER SRM 53-10-3 FIG 1. (X) 2 L 7 2 4F A16WE 1999102900448 19991029 00448 NM 1999 10 29 USAA990963 1 19990917 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 44592 22887 TPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK STA 747, STR 19L SKIN. INSTALLED DOUBL ER PER SRM 53-30-3 FIG 6. (X) 2 L 7 2 4F A16WE 1999102900449 19991029 00449 NM 1999 10 29 USAA990964 1 19990917 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 44592 22887 TPA - DURING CX-4 VISUAL INSPECTION, FOUND A 1 INCH CRACK STA 727B, STR 18L SKIN. INSTALLED DOUBLER PER SRM 53-30-3. ( X) 2 L 7 2 4F A16WE 1999102900450 19991029 00450 NM 1999 10 29 USAA991024 1 19990925 A 5230 6547952524M SKIN BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 45676 22445 TPA - DURING A CX-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN LOWER INNER LINER OF CARGO DOOR SKIN. INSTALLED RE PAIR DOUBLER PER SRM 53-00-2 FIG 1. (X) 2 L 7 2 4F A16WE 1999102900451 19991029 00451 NM 1999 10 29 USAA990917 1 19990927 A 5320 BEAM BOEING 737 737301 1384611 NM BS 360-380 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING RON CHECK VISUAL INSPECTION, FOUND 7 EACH 1 INCH BY .50 INCH AREAS OF CORROSION AROUND CLIP NUT HOLES AT BS 360 - BS 380, LT CREASE BEAM INBOARD ANGLE CORROSION LEVEL 1. REMOVED CORROSION WITHIN LIMITS PER SRM 53-10-51. (X) 2 L 7 2 4F RT A16WE 1999102900452 19991029 00452 NM 1999 10 29 USAA990916 1 19990927 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT BS 520, RBL 47 CABIN FLOORBEAM UPPER CHORD. STOP DRIL LED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X) 2 L 7 2 4F RT A16WE 1999102900453 19991029 00453 NM 1999 10 29 USAA990915 1 19990927 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 47 CABIN FLOORBEAM UPPER CHORD. STOP DRIL LED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X) 2 L 7 2 4F RT A16WE 1999102900454 19991029 00454 NM 1999 10 29 USAA990914 1 19990927 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 24 CABIN FLOORBEAM UPPER CHORD. STOP DRIL LED CRACK AND INSTALLED DOUBLER PER EA 65271 AND SB 737-53-1120. (X) 2 L 7 2 4F RT A16WE 1999102900455 19991029 00455 NM 1999 10 29 USAA990913 1 19990927 A 5320 69353502 CLIP BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 520 AND STR 16L FRAME TIE CLIP. REMOVED AND R EPLACED TIE CLIP PER BOEING DWG 65-46534 SHEET 3 AND SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999102900456 19991029 00456 NM 1999 10 29 USAA990920 1 19990920 A 5754 SKIN BOEING 737 737301 1384611 NM NR 1 LE SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 EACH, .50 INCH CRACKS, NR 1 SLAT INBOARD EDGE OF LOWER SKIN AFT FASTEN ER ROW. INSTALLED DOUBLER PER BOEING DWG 65C30133 AND TR 57-50-01 REV H. (X) 2 L 7 2 4F RT A16WE 1999102900457 19991029 00457 NM 1999 10 29 USAASB99235 1 19990922 A 3241 39353 VALVE BOEING 737 7372B7 1384560 NM LT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 267AU 22879 ORD - FLT 2704 - AFTER TAKEOFF FROM BWI, THE INBOARD ANTI-SKID LIGHT ILLUMINATED AND DID NOT EXTINGUISH AFTER GEAR RETRA CTION. FLIGHT DIVERTED TO ORD FOR MAINTENANCE AND LONGER RUNWAYS. LIGHT REMAINED ON WHEN LANDING GEAR WAS DOWN AS WELL . FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD ANTI-S KID VALVE PER MM 32-42-31. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F A16WE 1999102900458 19991029 00458 WP 1999 10 29 AALA991486 1 19990930 A 5320 SPLICE DOUG DC9 DC982 3022082 WP BS 229 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 262AA 49290 TUL - PRODUCTION SPLICE STRAP HOLES ELONGATED FROM LONGERON 17L TO LONGERON 18L AT STA 229. CUT OUT SECTION OF SPLICE S TRAP. INSTALLED FILLER AND STRAP DOUBLER PER ESO 80559 DATED 9-30-99. (X) 2 L 7 2 4F A6WE 1999102900459 19991029 00459 NM 1999 10 29 AALA991160 1 19990806 A 2560 416N222022 BOTTLE BOEING 757 757223 1384957 NM LT EMERG EXIT FAILED TEST A AALA O OTHER L NO TEST IN INSP/MAINT 1 SW 07 674AN 29424 MEX - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERWING SLIDE BOTTLE WOULD NOT TEST FROM CABIN. PLACARDED LEFT OVERWING BOTTLE 'TEST INOP' PER MEL. REPLACED EMERGENCY OVERWING SLIDE BOTTLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999102900460 19991029 00460 NM 1999 10 29 AALA991243 1 19990821 A 3397 WIRE BOEING 757 757223 1384957 NM ROWS 9D-17D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 674AN 29424 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS FROM SEAT 9D TO SEAT 17D INOPERATIVE. RE- SECURED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS BETWEEN SEATS 9D AND 17D. SYSTEM GROUND CHECKED, NORMAL OPERA TION. (X) 2 L 7 2 4F RT A2NM 1999102900461 19991029 00461 WP 1999 10 29 AALA6002 1 19990903 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 755RA 49727 RNO - CHECK EMERGENCY AISLE BATTERY PACK. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT SEAT 20A DUE TO ROWS 15 THROUG H 18 INTERMITTENT, OPS CHECK GOOD AT THIS TIME. (X) 2 L 7 2 4F RT A6WE 1999102900462 19991029 00462 NM 1999 10 29 AALA991371 1 19990910 A 5270 630261 SWITCH BOEING 737 737823 13844BZ NM LT EMERG EXIT OUT OF ADJUST A AALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 901AN 29503 DTW - FLT 1183 - ON TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS, LEFT FORWARD OVERWING EMERGENCY EXIT DOOR LIGHT ILLUMINATED IN COCKPIT. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. RESET SWITCHES ON LEFT FORWARD OVERWING EMERGENCY EXIT DOOR. S YSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A16WE 1999102900463 19991029 00463 1999 10 29 99ZZZX4085 4 19990917 A 3416 ALTIMETER ALIDSG BEECH 1900 1900D 1154162 CE LT COCKPIT MALFUNCTIONED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 184UX 2094 3035 UE184 CAPTAIN'S ALTIMETER READS 80 FEET - 100 FEET HIGH AT ALL ALTITUDES AND ENCODER TRANSITION POINTS ARE OUT OF TOLERANCE. R EMOVED AND REPLACED ALTIMETER. BENCH TEST VERIFIED ALTIMETER TO BE INDICATING 80 FEET HIGH AT 1,500 FEET AND 110 FEET H IGH AT 10,000 FEET. COMP P/N KEA-346/066-03062-00. (X) 2 L 7 2 4T RT A24CE 1999102900464 19991029 00464 1999 10 29 99ZZZX4086 4 19990913 A 3416 ALTIMETER ALIDSG BEECH 1900 1900D 1154162 CE LT COCKPIT MALFUNCTIONED A GLBA K NONE J WARNING INDICATION CR CRUISE 1 CE 01 254GL 666 4245 UE254 CAPTAIN'S ALTIMETER FLAGGED DURING CRUISE FLIGHT. REMOVED AND REPLACED ALTIMETER. SUBMITTER STATED THIS IS THE SECOND REPORT OF A FLAGGING PROBLEM WITH THIS ALTIMETER IN THE PAST 12 MONTHS. BENCH TEST DID NOT VERIFY THE FAULT. COMP P/N KEA-346/066-03062-0008. (X) 2 L 7 2 4T RT A24CE 1999102900465 19991029 00465 NM 1999 10 29 UIEA99078 1 19990921 A 5753 SAFETY WIRE BOEING 747 74747UF 1384949 NM TE AFT FLAP BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 491MC 4637 818 29252 INSPECTED ACFT PER ATLAS AIR FCD 99-17. FOUND FOLLOWING AFT FLAP TRACK CARRIAGE BOGIE PIN ASSYS WITH FAILED SAFETY WIRE AT 5 POSITIONS: OUTBOARD PIN (WIRE STRETCHED, TORQUE ON SAFETY BOLT 140 INCHES/POUNDS); OUTBOARD PIN (WIRE BROKEN, TOR QUE ON BOLT OK); INBOARD PIN (WIRE BROKEN, TORQUE ON BOLT OK); OUTBOARD PIN (WIRE BROKEN, TORQUE OK); INBOARD PIN (WIRE BROKEN, TORQUE ON SAFETY BOLT 80 INCHES/POUNDS). AIRCRAFT REPAIRED IAW ATLAS AIR FCD 99-17. (REFERENCE IPC 27-51-28-01) . (X) 2 L 7 4 4F RT 1384945 1999102900466 19991029 00466 WP 1999 10 29 AT9900741 1 19991015 A 5320 SKIN DOUG DC9 DC932 3022066 WP SERVICE DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND FORWARD SERVICE DOOR JAMB LOWER AFT CORNER OF SKIN CRACKED OUT OF LIMITS. FABRICATED 2 DOUBLERS, FILLERS, TRIMMED FILLER TO FIT, BACK DRILLED AND PRIMED REPAIR AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, AND EO 09-5310-29-E1472. 2 L 7 2 4F A6WE 1999102900467 19991029 00467 WP 1999 10 29 AT9900742 1 19990911 A 5313 3924809503N LONGERON DOUG DC9 DC932 3022066 WP BS 598 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND A BULGE AT BS 598, LB 0, GAINED ACCESS AND FOUND CORROSION AT LONGERON 30. REMOVED LONGERON 30 LEFT AND RIGHT HAN D WEB ASSEMBLY, INSTALLED NEW LONGERON, FABRICATED AND INSTALLED WEB REPAIRS IAW DC9 SRM 53-04 FIGURE 43, 51-30-2, AND D C9 MM 30-10-7. 2 L 7 2 4F A6WE 1999102900468 19991029 00468 WP 1999 10 29 AT9900744 1 19991015 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND FLOORBEAM UPPER ATTACH ANGLE HAD EXFOLIATION CORROSION AT BS 980 RBL 35-RBL 49. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIGURE 20A. 2 L 7 2 4F A6WE 1999102900469 19991029 00469 WP 1999 10 29 AT9900745 1 19991010 A 5730 PANEL DOUG DC9 DC932 3022066 WP LT WING GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND LEFT WING PANEL GOUGED BEYOND LIMITS. FABRICATED PANEL REPAIR IAW EO 99-1288. 2 L 7 2 4F A6WE 1999102900470 19991029 00470 WP 1999 10 29 AT9900746 1 19990929 A 5320 S124539912000 ANGEL DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND CAP L ANGEL CORRODED AND CRACKED 4AT BS 965-BL24R. REMOVED CAP ANGEL AND REPLACED, FABRICATED AND INSTALLED 8 TRA CKED ANGLE REPAIR IAW TIMCO RES 07186 AND DC9 SRM 53-30-5. 2 L 7 2 4F A6WE 1999102900471 19991029 00471 WP 1999 10 29 AT9900751 1 19990922 A 5260 49188831 ROD ASSY DOUG DC9 DC932 3022066 WP FORWARD AIRSTAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND FORWARD AIRSTAIRS AND LOWER ROD ASSEMBLY WERE CORRODED. REMOVED AND REPLACED THE LOWER ROD ASSEMBLY OF FORWARD AI RSTAIRS, AND RIGGED IAW DC9 MM 20-10-0, 52-62. 2 L 7 2 4F A6WE 1999102900472 19991029 00472 WP 1999 10 29 AT9900752 1 19990927 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND CABIN FLOOR SUPPORT BS 200 BL 0-BL 42L WAS CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF FLOOR SUPPORT, FAB RICATED AND INSTALLED REPAIR FLOOR SUPPORT IAW DC9 SRM 53-11-1, 51-10-3, 51-10-4, 51-30-5. 2 L 7 2 4F A6WE 1999102900473 19991029 00473 WP 1999 10 29 AT9900753 1 19991004 A 5520 5919752505 BALANCE WT DOUG DC9 DC932 3022066 WP RT ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT ELEVATOR BALANCE WEIGHT WAS CORRODED. REMOVED AND REPLACED RIGHT ELEVATOR BALANCE WEIGHT IAW DC9 SRM 55-01 PG 3, 51-30-1. 2 L 7 2 4F A6WE 1999102900474 19991029 00474 WP 1999 10 29 AT9900754 1 19991018 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND FLOORBEAM AT BS 996 RBL 35-RBL49 WAS CORRODED. FABRICATED FLOORBEAM AND INSTALLED IAW DC9 SRM 53-05 FIGURE 108, M M 27-20-0, 20-17-0. 2 L 7 2 4F A6WE 1999102900475 19991029 00475 WP 1999 10 29 AT9900757 1 19991019 A 5320 JAMB DOUG DC9 DC932 3022066 WP SERVICE DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND SERVICE DOOR JAMB, LOWER AFT CORNER CRACKED .700 ALONG OUTER SKIN. FABRICATED AND INSTALLED 2 DOUBLER AND FILLERS IAW EO 09-5310-29-E1472. 2 L 7 2 4F A6WE 1999102900476 19991029 00476 NM 1999 10 29 AT9900758 1 19991018 A 3350 900835A POWER SUPPLY BOEING 737 7372L9 1384497 NM CABIN INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 FOUND FORWARD AND AFT EMERGENCY EXIT AISLE SIGNS INOPERATIVE. REPLACED POWER SUPPLY IN EACH FORWARD AND AFT EMERGENCY E XIT SIGNS. 2 L 7 2 4F RT A16WE 1999102900477 19991029 00477 NM 1999 10 29 AWXA9900373 1 19991021 A 3350 864705 POWER SUPPLY BOEING 737 737297 1384480 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 147AW 22630 CONDITION: NON-ROUTINE-- EMER LTNG LOG 3203678DISCREPANCY: EMERGENCY LIGHTS ROW 6 THROUGH 14 INOPCORRECTIVE ACTION: R EPLACED POWER SUPPLY AND BATTERYCURRENT HISTORY: 6 WRITE-UPS SINCE 07/01/99 NONE RELATED 2 L 7 2 4F A16WE 1999102900478 19991029 00478 NM 1999 10 29 AWXA9900374 1 19990923 A 5320 65C87351 SILL BOEING 737 7373G7 1384595 NM BS 985-1006 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 C-CHECK, CORROSION ON R2 DOOR SILL BS 985 TO 1006. REMOVED AND REPLACED DAMAGED CHORD PER 737 SRM 51-40-3, SEALED PER S RM 51-20-5. 2 L 7 2 4F RT A16WE 1999102900479 19991029 00479 NM 1999 10 29 AWXA9900375 1 19990925 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 907 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 C-CHECK, CORROSION ON SEAT TRACK AT BS 907 RBL 45. REMOVED DAMAGED SECTION OF TRACK, FABRICATED SPLICE, SEAT TRACK AND FILLER FROM .0125 7075 T-6 FILLER SPLICE MATERIAL .032 301 1/2 HARD R607099, SEAT TRACK MAT BAC 1520-792 7178-T6. PA RTS ALODINED AND PRIMED PER SRM 51-20-01. INSTALLED PER SRM 53-00-52 FIG 204. 2 L 7 2 4F RT A16WE 1999102900480 19991029 00480 NM 1999 10 29 AWXA9900376 1 19990921 A 5330 6545877 SKIN BOEING 737 7373G7 1384595 NM R1 DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 C-CHECK, FWD GALLEY DOOR CUTOUT FUSELAGE SKIN LWR AFT CORNER CRACKED APPROX .5 INCH LONG AND TERMINATES IN FASTENER HOLE . CRACK AT FASTENER HOLE OVERSIZE HOLE AND PLUG, INSTALLED CONICAL WASHERS, FABBED REPAIR PTS FR 7075T6 .063 R708344 & 594854, REPAIR DOUBLERS FR 7075T6 R699111 & R712283 AND TAPERED FILLER FR 2024T3 .071& 2024T3 .125. ALODINED, PRIMED AN D INSTALLED WET PER SRM 53-10-1 FIG 202 AND 51-40-02. 2 L 7 2 4F RT A16WE 1999102900481 19991029 00481 NM 1999 10 29 AWXA9900377 1 19990919 A 5315 654681143 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 C-CHECK, CORROSION ON FLOORBEAM B/S 980 RBL 0-30. REMOVED T-CAP FROM BS 980 LBL RBL IAW SRM 51-40-2. FABRICATED UPPER T-CAP FROM MATL BAC 1505-100952/7075 T6R719554 IAW SRM 53-00-51. TREATED AND PRIMED T-CHORD IAW SRM 51-20-01. INSTALLE D UPPER T-CAP IAW SRM 51-00-51 AND 51-40-2. 2 L 7 2 4F RT A16WE 1999102900482 19991029 00482 NM 1999 10 29 AWXA9900378 1 19990920 A 5330 6584500 SKIN BOEING 737 7373G7 1384595 NM L2 DOORWAY CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 C-CHECK, FUSELAGE SKIN AT L-2 DOOR AFT CUTOUT CHAFED BEYOND LIMITS. NO CRACKS NOTED ON DOOR CUTOUT IAW 737 NDT MPT 6-51 -00-00. FABRICATED REPAIR DOUBLERS 2 OF QQA250-5, 2024T3 .063 R687660, 1 OF 2024T3 .125 R694504 AND FILLER INSTALLED I AW 737 SRM 53-30-03, FILLER QQA250/5 .032 R698474. 2 L 7 2 4F RT A16WE 1999102900483 19991029 00483 NM 1999 10 29 AWXA9900380 1 19991022 A 2931 211C223212 SWITCH BOEING 757 7572S7 1384962 NM LT HYD SYS LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 WP 28 902AW 23322 EMERGENCY LANDING, LT SYS QTY ZERO. PERFORMED QRH PROCEDURES, PRESS REMAINED IN L/G SYS. FOUND PRESS SWITCH LEAKING. R EMOVED AND REPLACED PRESS SWITCH AND UNION AS REQUIRED. RESERVICED, LEAK CHECKED OK. 2 L 7 2 4F RT A2NM 1999102900484 19991029 00484 EU 1999 10 29 PNSA991001 1 19991025 A 2612 FIRE DETECTOR KIDDE 478079 SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A PNSA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 AL 03 675PA 01390136 206 ON APPROACH TO ANC, OVER THE OUTER MARKER THE CARGO FIRE LIGHT ILLUMINATED. THE NUMBER 1 CARGO FIRE BOTTLE WAS DISCHARG ED AND AN EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. EMERGENCY CREWS OPENED CARGO COMPARTMENT AND FOUND NO SMOKE OR F IRE. SMOKE DETECTORS WERE FOUND TO BE SATURATED WITH CONDENSATION. REPLACED DETECTORS, NO FURTHER DISCREPANCIES WERE F OUND. 2 L 7 2 4T RT A52EU 1999102900485 19991029 00485 SO 1999 10 29 RAAA99E4039 1 19991024 A 3350 873100212 LIGHT LKHEED 188 188C 5262604 SO ROW 12CDE INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND ROW 12 C, D, E EXIT IDENTIFIER LIGHT WILL NOT TEST. REPLACED LIGHT ASSY. 2 L 7 4 4T 4A22 1999102900486 19991029 00486 SO 1999 10 29 RAAA99E4040 1 19990511 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 856 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK LUGS DAMAGED AT BBL 0, FS 856. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 157. 2 L 7 4 4T 4A22 1999102900487 19991029 00487 SO 1999 10 29 RAAA99E4041 1 19990511 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 930-1000 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK LOCK LUGS AT FS 930-1000 LBL 24 DAMAGED. REPLACED SEAT TRACK AS PER ECO 9 9-05, M-54 NR 158. 2 L 7 4 4T 4A22 1999102900488 19991029 00488 SO 1999 10 29 RAAA99E4042 1 19990511 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO F/S 939-1000 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED #1 CHECK, FOUND SEAT TRACK LUGS DAMAGED @ FUS/STA 939-1000 LBL 54. REPLACED SEAT TRACK AS PER ECO 99-05 , M-54 # 159. 2 L 7 4 4T 4A22 1999102900489 19991029 00489 SO 1999 10 29 RAAA99E4043 1 19990511 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 891-996 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK LOCK LUGS DAMAGED AT FS 891 TO 966 RBL 17. REPLACED SEAT TRACK AS PER ECO 99-05 M-54 NR 160. 2 L 7 4 4T 4A22 1999102900490 19991029 00490 SO 1999 10 29 RAAA99E4044 1 19990512 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 844-863 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON SEAT TRACK FLANGE AT FS 844-863 BBL 0. REPLACED SEAT TRACK AS PER ECO 9 9-05, M-54 NR 167. 2 L 7 4 4T 4A22 1999102900491 19991029 00491 SO 1999 10 29 RAAA99E4045 1 19990512 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 882 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOORBEAM FS 882 BBL 0-LBL 20. REPAIRED AS PER SRM 53-2-4, M -54 NR 169. 2 L 7 4 4T 4A22 1999102900492 19991029 00492 SO 1999 10 29 RAAA99E4046 1 19990512 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 236-240 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON SEAT TRACK FLANGE AT FS 236-430 RBL 21 SEVERAL SPOTS. REPLACED SEAT TRA CK AS PER ECO 99-05, M-54 NR 172. 2 L 7 4 4T 4A22 1999102900493 19991029 00493 SO 1999 10 29 RAAA99E4047 1 19990512 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 374-445 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON SEAT TRACK AT FS 374-445, RBL 41. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 173. 2 L 7 4 4T 4A22 1999102900494 19991029 00494 SO 1999 10 29 RAAA99E8055 1 19991024 A 3350 873100112 LIGHT LKHEED 188 188C 5262604 SO ROW 17AB INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY LIGHT AT ROW 17 A, B, FAILS SELF TEST. REPLACED LIGHT ASSY. 2 L 7 4 4T 4A22 1999102900495 19991029 00495 SO 1999 10 29 COMA9910167 1 19991025 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT FAILED A COMA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 01 249CA 4003 120230 FLAPS FAILED AT ZERO. REPLACED THE FLAP ANNUNCIATOR. 2 L 7 2 4T RT A31SO 1999102900496 19991029 00496 SO 1999 10 29 COMA9910168 1 19991025 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 246CA 16823 120223 FWD FLOOR PATH EMERGENCY LIGHTS ARE INOP. REPLACED THE NR 1 POSITION EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1999102900497 19991029 00497 EA 1999 10 29 COMA9960651 1 19991025 A 3350 363782 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920CA 7022 ONE FLOOR PATCH EMERGENCY LIGHT IS INOP. REPLACED LIGHTING STRIP. 2 L 7 2 4F RT A21EA 1999102900498 19991029 00498 EA 1999 10 29 COMA9960652 1 19991025 A 3250 16650101 TILLER CNDAIR CL600 CL6002B19 EA NLG STEERING MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 769CA 4622 7292 AIRCRAFT PULLED SHARPLY TO RIGHT DURING TAKEOFF. REPLACED STEERING TILLER. 2 L 7 2 4F RT A21EA 1999102900499 19991029 00499 NM 1999 10 29 UPS99230988 1 19991026 A 5754 SKIN BOEING 727 72725C 138400H NM LT TE FOREFLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, LEFT O/B FOREFLAP DELAMINATED REMOVED L/H FOREFLAP PER MM 27-51-11. INSTALLED TEMPORARY REPAIR PER EO B727-5750-3081-C. INSTALLED LT FOREFLAP PER MM 27-51-11, OP CHECKS NORMAL. 2 L 7 3 4F A3WE 1999102900500 19991029 00500 NM 1999 10 29 UPS99430987 1 19991025 A 2750 RETRACT MECH BOEING 747 747212B 1384886 NM RT TE FLAP MALFUNCTIONED A IPXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 520UP 21943 INSPECTION TYPE:N/A, ATB-OUTBOARD FLAPS RETRACTED UNCOMMANDED. 2 L 7 4 4F A20WE 1999102900501 19991029 00501 WP 1999 10 29 UPS99830986 1 19991022 A 3297 WIRE DOUG DC8 DC873F 302199F WP LT MLG BROKEN A IPXA O OTHER N FALSE WARNING LD LANDING 1 SO 01 880UP 46080 INSPECTION TYPE:N/A, LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE ON LANDING IN ONT. AFTER CHECKLIST COMPLETE, A NOR MAL LANDING WAS MADE. GEAR PINNED. REPLACED BROKEN WIRE BETWEEN TERMINAL BOARD S3-5 AND L/G DOWN LIMIT SWITCH. WIRE G 322E24. LEFT LANDING GEAR LIGHT OPERATED NORMAL REF WDM 3201 SHEET 2 PG 2. 2 L 7 4 4F RT 4A25 1999102900502 19991029 00502 EU 1999 10 29 QXEA9902146 1 19991024 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU EMER EXIT FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 PDX- CENTER OVERHEAD EMERGENCY EXIT SIGN IS DIM. REMOVED AND REPLACED EMERGENCY CIRUIT BOARD, OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999102900503 19991029 00503 EU 1999 10 29 QXEA9902147 1 19991022 A 3350 5515900004 CIRUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU EMER EXIT FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 PDX- CENTER CABIN OVERHEAD EMERGENCY SIGN LIGHTS ARE DIM. REMOVED AND REPLACED FORWARD AND AFT EMERGENCY SIGN CIRCUIT B OARDS, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999102900504 19991029 00504 EU 1999 10 29 QXEA9902148 1 19991022 A 3350 LIGHT GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU ROW 9E INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11173 BOI- EMERGENCY LIGHT AT ROW 9E INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1999102900505 19991029 00505 WP 1999 10 29 99FDEA00446 1 19991021 A 5510 ALC750618 STRAP DOUG DC10 DC1030F 3023504 WP RT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 RT HORIZ STAB LEADING EDGE PNL 3RD FROM I/B (CENTER) FOUND TOP TEE BRACKET CRACKED (XFS 172.161) APPROX 26 .75 LONG. *S /D* NEW STRAP FAB PER DWG ALC7506, REMOVED AND REPLACED PER SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 1999102900506 19991029 00506 WP 1999 10 29 99FDEA00447 1 19991021 A 5510 ALC705219 TEE DOUG DC10 DC1030F 3023504 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LT HOR-STAB LEAD EDGE PNL 2ND FROM I/B (CTR I/B) FOUND TOP CAP CRACKED (XFS.166.161) APPROX 46 .375 LONG. *S/D* REMOVE D AND REPLACED NEW CAP PER SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 1999102900507 19991029 00507 NM 1999 10 29 99FDEA00448 1 19991026 A 2910 651784940C1 LINE BOEING 727 727227 1384078 NM B HYD SYS LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 492FE 21530 BOTH B-SYS PUMP LOW PRESS LIGHTS ON 2ND OFF PANEL AND ALL 3 SYS-B FLT CONTROL LIGHT ON FWD PANEL ILLUM IN FLT. *S/D* I NSTALLED TUBE ASSY PACK AND UNION PER B727 MM 20-10-005-4. LEAK CHECK OK, B CHECK OK. 2 L 7 3 4F A3WE 1999102900508 19991029 00508 NM 1999 10 29 99UAL900529 1 19991016 A 2613 355604310 OVERHEAT DET FENWAL 2003500830 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RIGHT FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 363UA 240 24532 DURING CLIMB, THE RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED. *S/D* FOLLOWING TROUBLESHOOTING, CAUSE ISOLATED TO M488 ENGINE STRUT CAVITY OVERHEAT DETECTOR. REPLACED THE OVERHEAT DETECTOR. REPLACED THE M237 OVERHEAT CONTROL MODULE AS A PRECAUTION. AIRCRAFT RETURNED TO REVENUE SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102900509 19991029 00509 1999 10 29 99UAL900531 4 19991016 A 2370 271150056001 VIDEO UNIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 25C FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 774UA 26936 EN ROUTE CDG-IAD BURNING SMELL AT ROWS 21-25AB. POWER TO SEAT CONTROL AND AUDIO ENTERTAINMENT TURNED OFF AND SMOKE DISS IPATED. *S/D* SEAT VIDEO UNIT FAILED INTERNALLY. 5 VDC PINS SHORTED CAUSING CONNECTOR TO MELT IN AREA. CURRENTLY CON SIDERED AN ISOLATED INCIDENT, THE EXACT CAUSE IS UNDER INVESTIGATION WITH UNITED, BOEING AND POSSIBLY THE OEM (GMIS). T HE UNIT WAS REPLACED AND SYSTEM OPERATIONALLY TESTED SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999102900510 19991029 00510 NM 1999 10 29 99UAL900532 1 19991016 A 2430 KCD4N RELAY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E/E COMP FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 924UA 26645 DIRECT CURRENT FAIL LIGHT ILLUMINATED ON BOTH INERTIAL REFERENCE UNITS ON TAKEOFF. *S/D* RELAY R41 FAILED. REPLACED R 41 RELAY. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102900511 20001016 00511 NM 2000 10 16 99UAL900533 1 19991016 A 3397 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7257U 21404 EMERGENCY LIGHT OUT ABOVE FORWARD GALLEY DOOR. *S/D* LOOSE GROUND CONNECTION. REPAIRED LOOSE GROUND GD352. WD 33-51-0 2. OPS CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999102900512 19991029 00512 NM 1999 10 29 99UAL900534 1 19991016 A 2120 UNKNOWN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 7287U 21565 UPON ROTATION EXPERIENCED HAZE IN THE COCKPIT ALONG WITH A BURNING RUBBER SMELL. SMELL WOULD GO AWAY AND COME BACK. RE TURNED TO ORD AND DID A FLY-BY TO DETERMINE IF THERE WAS A PROBLEM WITH THE GEAR BEFORE MAKING A NORMAL LANDING. *S/D* MAINTENANCE SPECULATED THAT PERHAPS DEBRIS FROM RUNWAY MAY HAVE BEEN INGESTED. CHECKED PACKS AND ENGINES AND COULD NO T DUPLICATE PROBLEM. ALSO, CHECKED ENGINES FOR SIGN OF INGESTION AND FOUND THAT C1 BLADE NR 12 HAD A LEADING EDGE TEAR. TEAR BLENDED OUT. 2 L 7 3 4F 4 F A3WE E2EA 1999102900513 19991029 00513 NM 1999 10 29 99UAL900535 1 19991016 A 2520 SEAT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 14 LOOSE A UALA O OTHER O OTHER CL CLIMB 1 WP 29 7285U 21563 AFTER TAKOFF FROM FLL SEAT ROW 14 DEF CAME OUT OF THE TRACK. MOVED PASSENGERS AND CREW WAS ABLE TO PUT ROW OF SEATS BA CK INTO THE TRACK. SUPPLEMENTAL DATA UPDATE SECURED SEATS AT ATTACH POINTS. 2 L 7 3 4F 4 F A3WE E2EA 1999102900514 19991029 00514 NM 1999 10 29 99UAL900536 1 19991018 A 3350 582214 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7279U 21557 EEL STRIPS INOPERATIVE IN CENTER PORTION OF CABIN. ALSO, WALL MOUNTED EXIT SIGNS ON LOWER LEFT SIDEWALL BY THE OVERWING DOORS INOPERATIVE. *S/D* REPLACED POWER SUPPLY AND 2 LIGHT SEGMENTS. 2 L 7 3 4F 4 F A3WE E2EA 1999102900515 19991029 00515 NM 1999 10 29 99UAL900537 1 19991018 A 5313 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 950-1010 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7458U 21912 CORROSION DAMAGE WAS FOUND ON STRINGER 29 LEFT BETWEEN STATION 950-1010 THAT WAS BEYOND ALLOWABLE LIMITS. UAL REPAIR PR OCEDURES CUT OUT THE BELLY SKIN TO ALLOW ACCESS TO REPLACE STRINGER 29. DURING THE CUTTING OF THE SKIN THE EDGE MARGIN OF THE FASTENER ROW ADJACENT TO THE CUT WAS TOO SHORT. THE CUTOUT WAS ENLARGED TO REMOVE THE FASTENER ROW. A PREVIOUSL Y INSTALLED SKIN REPAIR FOR STRINGER 29 RIGHT WAS REMOVED AND ONE LARGE REPAIR WAS USED TO REPAIR THE SKIN CUTOUTS FOR S TRINGER 29 RIGHT AND LEFT. THE REPAIR WAS PER TIMCO'S REPAIR INSTRUCTIONS AND WAS APPROVED BY 8110-3. 2 L 7 3 4F 4 F A3WE E2EA 1999102900516 20001010 00516 NE 2000 10 10 99UAL900538 2 19991021 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 OVERTEMP A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 605UA 21866 709678 NR 2 ENGINE OIL TEMP IN RED RANGE. RETURNED TO LAX. OVERWEIGHT LANDING. EICAS AUTO EVENT 163 DEG. DURATION EST MORE THAN 15 MINUTES. *S/D* ON ENGINE TEARDOWN, NOTHING WAS FOUND THAT WOULD CONTRIBUTE TO THE REPORTED HIGH OIL TEMPERATUR E. REPLACEMENT OF NR 2 ENGINE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999102900517 19991029 00517 NM 1999 10 29 99UAL900539 1 19991020 A 3244 TIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG FAILED A UALA O OTHER C F.O.D. TO TAKEOFF 1 WP 29 398UA 24673 FLIGHT CREW REPORTED THAT THE AIRCRAFT STRUCK A LARGE PIECE OF CONCRETE ON THE RUNWAY. FLIGHT CREW SUSPECTED THAT THE N OSE TIRES WERE BLOWN. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102900518 19991029 00518 NE 1999 10 29 99UAL900540 2 19991020 A 7200 ENGINE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 1 LEAKING A UALA A UNSCHED LANDING K FLUID LOSS UK UNKNOWN 1 WP 29 991UA 21981 FLIGHT CREW SUSPECTED FLUID LEAK ON NUMBER ONE ENGINE. 2 L 7 2 4F 4 F A16WE E2EA 1999102900519 19991029 00519 NE 1999 10 29 99UAL900541 2 19991020 A 7200 ENGINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 BIRD STRIKE A UALA O OTHER C E F.O.D. VIBRATION/BUFFET TO TAKEOFF 1 WP 29 342UA 24246 ON TAKEOFF, NUMBER TWO ENGINE ENCOUNTERED A BIRD STRIKE. THIS RESULTED IN A JUMP OF ENGINE VIBRATION FROM ZERO TO TWO. 2 L 7 2 4F 4 F RT A16WE E2GL 1999102900520 19991029 00520 NM 1999 10 29 99UAL900542 1 19991019 A 2130 WARNING HORN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT ACTIVATED A UALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 7278U 21425 FLIGHT HAD ALTITUDE WARNING HORN. MADE AN EMERGENCY DESCENT TO 10,000 FEET. STANDBY CABIN PRESSURE WAS SELECTED. FLI GHT CONTINUED ON TO JAX. *S/D* NO PROBABLE CAUSE WAS DETECTED. A PRESSURIZATION CONTROL TEST WAS ACCOMPLISHED AND SYS TEM CHECKED OUT OK. 2 L 7 3 4F 4 F A3WE E2EA 1999102900521 19991029 00521 NM 1999 10 29 99UAL900543 1 19991020 A 3350 582233 POWER PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 15-18 INOP A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHTS AT ROWS 15-18 LEFT SIDE ARE INTERMITTENT. UPPER DECK EEL POWER PACK FAILED. REPLACED POWER PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 1999102900522 19991029 00522 NM 1999 10 29 99UAL900544 1 19991021 A 3397 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 19-26 BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7263U 21410 EEL LIGHTING INOPERATIVE FROM ROWS 19 TO 26. *S/D* REPAIRED BROKEN WIRE TO BATTERY PACK AT SEAT 20, OPERATIONALLY CHEC KED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999102900523 19991029 00523 NM 1999 10 29 99UAL900545 1 19991021 A 2782 656021211 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE FLAPS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7251U 21398 SLATS NR 2, 3, 6 AND 7 WOULD NOT RETRACT WHEN FLAP 2 DEGREES SELECTED FROM 5 DEGREES. NR 4 SLAT TRANSITION LIGHT DID N OT ILLUMINATE DURING RETRACTION. RETURNED TO ORD. *S/D* REPLACED LEADING EDGE POSITION CONTROL UNIT, OPERATIONAL CHEC K NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999102900524 19991029 00524 WP 1999 10 29 ABXA9900746 1 19991007 A 5320 995773925 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1021 BETWEEN LONGERON 15 AND 16 LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999102900525 19991029 00525 WP 1999 10 29 ABXA9900747 1 19991007 A 5330 5910228195 SKIN DOUG DOUG DC9 DC941 302207N WP BS 1208 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED, LEFT SIDE APPROXIMATELY 12 INCHES ABOVE VENTRAL STAIRWAY AT STATION 1208. REPAIRED IAW DC9 SRM 53-01-00. 2 L 7 2 4F A6WE 1999102900526 19991029 00526 WP 1999 10 29 ABXA9900748 1 19991007 A 5312 591472983 BLKHD STIFFENER DOUG DOUG DC9 DC941 302207N WP BS 549 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND VERTICAL STIFFENER NR 7 CRACKED AT STATION 549 BULKHEAD LOWER END. REPAIRED IAW DC9 SRM DWG K0515 9. 2 L 7 2 4F A6WE 1999102900527 19991029 00527 WP 1999 10 29 ABXA9900749 1 19991007 A 5320 99155541 ANGLE DOUG DOUG DC9 DC941 302207N WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND ANGLE CRACKED AT STATION 237 BETWEEN LONGERON 27 AND 28 LEFT. REPLACED ANGLE IAW DC9 SRM 51-30-0 5. 2 L 7 2 4F A6WE 1999102900528 19991029 00528 WP 1999 10 29 ABXA9900750 1 19991007 A 5341 59324506 FITTING DOUG DOUG DC9 DC941 302207N WP BS 642 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND RIGHT WING TO FUSELAGE ATTACH FITTING CRACKED AT STATION 642. REPAIRED FITTING IAW ABX REA D957-3 3523MR. 2 L 7 2 4F A6WE 1999102900529 19991029 00529 WP 1999 10 29 MWEA99715 1 19991025 A 5330 59114092 SKIN DOUG DC9 DC914 3022034 WP BS 455 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 RIGHT SIDE OF FUSELAGE AT STATION 455 BETWEEN 17L AND 16L HAD A DENT. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999102900530 19991029 00530 NM 1999 10 29 MWEA99716 1 19991025 A 3350 60030431 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 701ME 49760 EMERGENCY LIGHTING FLOOR TRACK LIGHTS DID NOT TEST PROPERLY. REMOVED AND REPLACED FORWARD FLOOR TRACK BATTERY PACK. 2 L 7 2 4F RT A6WE 1999102900531 19991029 00531 WP 1999 10 29 MWEA99717 1 19991020 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROW 16-20 CRIMPED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 FLOOR PATH EMERGENCY LIGHTING SYSTEM INOPERATIVE LAST SECTION OF LIGHTS, ROWS 16 TO 20. MAINTENANCE FOUND WIRING CRIMPE D AND SHORTING. REPAIRED WIRING. 2 L 7 2 4F A6WE 1999102900532 19991029 00532 WP 1999 10 29 MWEA99718 1 19991021 A 5320 991199117 ANGLE DOUG DC9 DC981 3022081 WP BS 1401-1420 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND CORROSION ON RIGHT ANGEL CAP AT FUSELAGE STATION 1401 TO 1420. CHECKED AND INSTALLED NEW ANGLE CAP. 2 L 7 2 4F A6WE 1999102900533 19991029 00533 WP 1999 10 29 MWEA99719 1 19991021 A 5311 991183969 FRAME DOUG DC9 DC981 3022081 WP BS 14 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND CORROSION ON LOWER END OF FRAME AT FUSELAGE STATION 14. MAINTENANCE FABRICATED AND INSTALLED FRAME REPAIR. 2 L 7 2 4F A6WE 1999102900534 19991029 00534 WP 1999 10 29 MWEA99720 1 19991021 A 5520 591041279 TIP DOUG DC9 DC981 3022081 WP RT ELEVATOR LIGHTING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND EVIDENCE OF LIGHTNING DISCHARGE ON RIGHT ELEVATOR END CAP. MAINTENANCE FITTED AND INSTALLED NEW END CAP. 2 L 7 2 4F A6WE 1999102900535 19991029 00535 WP 1999 10 29 MWEA99721 1 19991021 A 5320 991555920 FORMER DOUG DC9 DC981 3022081 WP BS 1401 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND CORROSION ON FORMER AT STATION 1401 BETWEEN LONGERON 23 AND 24 RIGHT. MAINTENANCE FABRICATED AND INSTALLED REPAIR PART SECTION. 2 L 7 2 4F A6WE 1999102900536 19991029 00536 WP 1999 10 29 MWEA99722 1 19991023 A 3350 60030431 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 80ME 45795 TWO CEILING LIGHTS BETWEEN GALLEY AND COAT CLOSET DID NOT EXTINGUISH WITH EMERGENCY LIGHTS OF. MTC REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1999102900537 19991029 00537 WP 1999 10 29 MWEA99723 1 19991024 A 3350 100865 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 700ME 45696 CENTER SECTION OF FLOOR TRACK LIGHTS ARE INOPERATIVE. MTC REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1999102900538 19991029 00538 WP 1999 10 29 MWEA99724 1 19991025 A 5320 995823925 FORMER DOUG DC9 DC981 3022081 WP BS 1361 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 806ME SHEAR CLIP FOUND CORRODED AT STATION 1361 ABOVE FORMER LONGERON 24 LEFT. MAINTENANCE FABRICATED AND INSTALLED NEW SHEAR CLIP. 2 L 7 2 4F A6WE 1999102900539 19991029 00539 WP 1999 10 29 MWEA99725 1 19991025 A 5330 591142269 SKIN DOUG DC9 DC981 3022081 WP BS 1250 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND PREVIOUS SKIN REPAIR AT STATION 1250 BETWEEN LONGERON 7 RIGHT AND 8 RIGHT WAS NOT DOCUMENTED. MAINTENANCE REMOVED OLD REPAIR, FABRICATED NEW PATCH AND FINGER DOUBLER REPAIR AND INSTALLED. 2 L 7 2 4F A6WE 1999102900540 19991029 00540 WP 1999 10 29 MWEA99726 1 19991025 A 5520 5919752505 BALANCE WEIGHT DOUG DC9 DC981 3022081 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND LEFT ELEVATOR OUTBOARD BALANCE WEIGHT CORRODED. MAINTENANCE FABRICATED AND INSTALLED NEW BALANCE WEIGHT. 2 L 7 2 4F A6WE 1999102900541 19991029 00541 WP 1999 10 29 MWEA99727 1 19991025 A 5320 3924814501 SPLICE DOUG DC9 DC981 3022081 WP FRAME 1431-1446 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND LIGHT CORROSION AND DRILL STOPS ON LONGERON 17 RIGHT BETWEEN CANTED FRAME 1431 AND 1446. MAINTENANCE FABRICATED A ND INSTALLED NEW LONGERON SPLICE. 2 L 7 2 4F A6WE 1999102900542 19991029 00542 WP 1999 10 29 MWEA99728 1 19991025 A 5313 591142923 LONGERON DOUG DC9 DC981 3022081 WP BS 1382 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND LONGERON 24 LEFT FROM AFT SIDE OF AFT PRESSURE BULKHEAD TO STATION 1382 TO HAVE AREAS OF CORROSION. MAINTENANCE F ABRICATED AND INSTALLED NEW SECTION OF LONGERON. 2 L 7 2 4F A6WE 1999102900543 19991029 00543 WP 1999 10 29 MWEA99729 1 19991025 A 5330 59114023 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND GOUGES IN FUSELAGE SKIN FROM PASSENGER DOOR HOLD OPEN HOOK RECEPTICAL AFT APPROX TWO INCHES. MAINTENANCE FABRICAT ED AND INSTALLED SKIN REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999102900544 19991029 00544 NM 1999 10 29 VNAA9910012 1 19991022 A 3260 OL3092 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG FAILED A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 459PS 3070 ON APPROACH TO DCA THERE WAS NOT A RT MAIN LANDING GEAR DOWN AND LOCKED INDICATION WHEN THE LANDING GEAR WAS SELECTED DO WN. THE CREW REFERENCED THE QRH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN DCA. MAINTENANCE INSPECT ED AND REPLACED THE RT MAIN LANDING GEAR DOWN LOCKED INDICATION BULBS IN ACCORDANCE WITH DORNIER. MAINTENANCE MANUAL 32 -61-12. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102900545 19991029 00545 NM 1999 10 29 VNAA9910013 1 19991021 A 3260 329630 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 423JS 9509 3032 ON THE TAKEOFF ROLL, THE CREW RECEIVED A NOSE WHEEL STEERING POWER UP FAIL MESSAGE. ONCE THE TAKEOFF WAS ABORTED, THE C REW RECEIVED THREE GEAR UNSAFE INDICATIONS ALONG WITH THREE GEAR DOWN AND LOCKED INDICATIONS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LIGHT DIMMER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-13-11. OPERATIONA L CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102900546 19991029 00546 NM 1999 10 29 VNAA9910014 1 19991024 A 2130 22260A030201 PRESS CONTL PNL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 427JS 3432 155 3039 WHILE EN ROUTE TO TYS AND WHILE CLIMBING THROUGH 11,000 FEET, AIRCRAFT AUTOMATIC PRESSURIZATION BECAME UNCONTROLLABLE. T HE CREW REFERENCED THE QRH AND SWITCHED TO MANUAL CONTROL BUT PRESSURIZATION WAS STILL UNCONTROLLABLE. THE FLIGHT THEN RETURNED TO PIT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CABIN PRESSURIZATION CONTROL SYSTEM PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-31-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102900547 19991029 00547 NM 1999 10 29 VNAA9910015 1 19991025 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 437JS 7015 155 3055 EN ROUTE TO CHS, THE FLIGHT CREW RECEIVED A NUMBER 2 BATTERY OVERHEAT CAS MESSAGE. THE AIRCRAFT THEN RETURNED TO PIT. T HE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NUMBER 2 MAIN BATTERY IN ACCORDANCE WITH DO RNIER MAINTENANCE 24-32-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102900548 19991029 00548 NE 1999 10 29 VNAA9910016 2 19991025 A 7200 ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT BIRD STRIKE A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 432JS 3045 116061 HL271 ON PREFLIGHT INSPECTION THE FLIGHT CREW FOUND BIRD REMAINS ON THE LT PROPELLER AND THE LT ENGINE INTAKE. MAINTENANCE IN SPECTED THE AIRCRAFT AND FOUND NO EXTERNAL DAMAGE TO THE PROPELLER OR THE ENGINE. A POWER ASSURANCE WAS COMPLETED AND F OUND ACCEPTABLE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00. THE AIRCRAFT WAS FERRIED TO CAK WHERE MAINTENAN CE COMPLETED A BORESCOPE INSPECTION AND COMPRESSOR WASH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-00-00. NO ADDI TIONAL DEFECTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999102900549 19991029 00549 1999 10 29 RAIA9910033 4 19991024 A 3418 C771065 SIG SUMMING UNIT BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 430AM 880 7356-STL- RIGHT STALL CAP ON. MAINTENANCE REPLACED SIGNAL SUMMING UNIT. 2 L 7 2 4T RT A56EU 1999102900550 19991029 00550 WP 1999 10 29 RAIA9910034 2 19991025 A 7314 8974007 FUEL PUMP BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 862JX 4914 4464 862 4797-MRY- RIGHT FUEL CAP LIGHT CAME ON AND RIGHT FUEL PRESS LOW. MAINTENANCE REPLACED RIGHT ENGINE FUEL PUMP. 2 L 7 2 4T 4 T RT A56EU E4WE 1999102900551 19991029 00551 SO 1999 10 29 RAIA9910035 1 19991025 A 3350 7287108507 CONTROL MODULE EMB 145 EMB145 SO CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 805HK 145096 6263-BOS- EMERGENCY LIGHT NOT ARMED LIGHT ON. MAINTENANCE REPLACED LIGHTING CONTROL MODULE. 2 L 7 2 4F RT T00011AT 1999102900552 19991029 00552 WP 1999 10 29 AALA991407 1 19990918 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 226AA 49176 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT FLOOR PATH EXIT MARKER HAS THREE LIGHTS INOPERATIVE. R EPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102900553 19991029 00553 WP 1999 10 29 AALA991406 1 19990918 A 3350 SOCKET DOUG DC9 DC982 3022082 WP ROW 19D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 428AA 49340 ORD - DURING OVERNIGHT CHECK, INTERIOR EMERGENCY EXIT LIGHT AT SEAT 19D INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT SOCK ET AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999102900554 19991029 00554 1999 10 29 AALA991309 4 19990901 A 2370 6166860001 VIDEO UNIT BOEING 767 767323 1385205 NM ROW 2HJ DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 39364 9506000255 24045 LAX - FLT 137 - EN ROUTE LHR-LAX - LAX SMOKE WAS NOTED FROM CENTER ARM REST OF SEATS 2HJ. SMOKE STOPPED WHEN POWER TO V IDEO UNIT AT SEAT 2HJ WAS DISCONNECTED. AIRCRAFT CONTINUED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED VIDEO POWER UN IT AT CENTER ARM REST OF SEAT 2HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900555 19991029 00555 NM 1999 10 29 AALA991387 1 19990913 A 3350 SOCKET BOEING 757 757223 1384957 NM R4 DOORWAY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 690AA 25696 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R4 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SOCKET A T R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102900556 19991029 00556 NM 1999 10 29 AALA991389 1 19990914 A 3350 SOCKET BOEING 767 767223 1385123 NM LT EMER EXIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339AA 22336 SFO - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT SOCKET IN LE FT FORWARD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900557 19991029 00557 NM 1999 10 29 AALA991396 1 19990914 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 1 DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645AA 24603 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEAR SEAT ROW 1 MISSING 18 INCH SECTION. REPL ACED EMERGENCY FLOOR PATH LIGHTING STRIP AT SEAT ROW 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102900558 19991029 00558 NM 1999 10 29 AALA991398 1 19990914 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 38H BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 38H INOPERATIVE. REPAIRED WIRING TO EMERGEN CY EXIT FLOOR PATH LIGHT AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900559 19991029 00559 NM 1999 10 29 AALA991354 1 19990908 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 679AN 29589 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY EX IT FLOOR PATH LIGHT STRIP AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102900560 19991029 00560 NM 1999 10 29 AALA991355 1 19990909 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 647AM 24605 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT LAST 3 SEAT ROWS OF FIRST CLASS CABIN INOPERATIVE . REPLACED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AT DIVIDER BETWEEN FIRST CLASS AND COACH SECTION OF CABI N. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102900561 19991029 00561 NM 1999 10 29 AALA991379 1 19990911 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 38AB DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389AA 27449 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 38AB INOPERATIVE. REPLACED CONNECTOR TO EMERGENCY EXIT SEAT LIGHT AT ROW 38AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900562 19991029 00562 NM 1999 10 29 AALA991293 1 19990830 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659AA 24617 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP LOCATED FORWARD OF COACH CABIN INOPERATIVE. R EPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP FORWARD OF COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102900563 19991029 00563 NM 1999 10 29 AALA991291 1 19990828 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 38H DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383AN 26995 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 38H INOPERATIVE. FOUND BROKEN WIRE AT CO NNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 38J. REPLACED CONNECTOR AND CONNECTOR PINS TO EMERGENCY EXIT FLOO R PATH LIGHTS AT SEAT 39J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900564 19991029 00564 NM 1999 10 29 AALA991280 1 19990826 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 22H AND 31H BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387AM 27184 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATHWAY LIGHTS AT SEATS 22H AND 31H INOPERATIVE. REPLACED BROKEN CON NECTOR PINS TO EMERGENCY EXIT PATHWAY LIGHTS AT SEATS 22H AND 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900565 19991029 00565 NM 1999 10 29 AALA991426 1 19990922 A 3350 SOCKET BOEING 767 767223 1385123 NM EXTERIOR DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 329AA 22329 SFO - DURING OVERNIGHT MAINTENANCE, RIGHT AFT FUSELAGE EMERGENCY EXIT GROUND ILLUMINATION LIGHT INOPERATIVE. CLEANED LI GHT SOCKET OF RIGHT AFT FUSELAGE EMERGENCY EXIT GROUND ILLUMINATION LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900566 19991029 00566 NM 1999 10 29 AALA991423 1 19990920 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST CR CRUISE 1 SW 07 322AA 22323 MIA - FLT 2198 - EN ROUTE MEX-MIA - CABIN EMERGENCY LIGHTS ILLUMINATED FOR ONE MINUTE THEN EXTINGUISHED. ALL SWITCHES W ERE IN NORMAL (ARMED) POSITION. FLIGHT CONTINUED AND LANDED MIA WITHOUT INCIDENT. INSPECTED EMERGENCY LIGHTING SYSTEM COULD NOT DUPLICATE FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900567 19991029 00567 NM 1999 10 29 AALA991422 1 19990920 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 662AA 25296 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE IN FIRST CLASS CABIN. REPAIRED WIRIN G TO EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999102900568 19991029 00568 NM 1999 10 29 AALA991429 1 19990920 A 2760 O-RING BOEING 767 767323 1385205 NM NR 9 SPOILER TORN A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 386AA 27060 ORD - FLT 84 - AFTER TAKEOFF ORD-FRA, CENTER HYDRAULIC SYSTEM LOST QUANTITY FOLLOWED BY LOSS OF PRESSURE. RESERVE BRAKE S/STEERING SWITCH SELECTED FOLLOWING GEAR EXTENSION WHICH MOMENTARILY RESTORED PRESSURE. ALTERNATE FLAP EXTENSION PERFO RMED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED O-RING IN NR 9 SPOILER ACTUATOR. ALSO, REPLACED AC MOTOR DRIVEN HYDRAULIC PUMPS, AIR DRIVEN HYDRAULIC PUMP, AND FILTERS AS PRECAUTIONARY MEASURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999102900569 19991029 00569 NM 1999 10 29 AALA991420 1 19990920 A 2530 2510000405 OVEN BOEING 767 767323 1385205 NM GALLEY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 390AA 0243 27450 MIA - FLT 1543 - EN ROUTE MIA-SDQ - FLIGHT ATTENDANTS NOTICED SMELL OF SMOKE AND HAZE IN FIRST CLASS GALLEY. AIRCRAFT R ETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED OVEN IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (M) 2 L 7 2 4F RT A1NM 1999102900570 19991029 00570 NM 1999 10 29 AALA991373 1 19990911 A 3240 AAP3275 BRAKE BOEING 777 777223 1385213 NM MLG DEFECTIVE A AALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SW 07 775AN 29584 ORD - FLT 86 - ON ARRIVAL AT GATE OPEN FLAMES WERE SEEN COMING FROM NR 2 AND NR 6 MAIN LANDING GEAR BRAKES. FIRE WAS EX TINGUISHED BY GROUND PERSONNEL. AIRCRAFT PASSENGER DEPLANED AT GATE WITHOUT INCIDENT. REPLACED NR 2 AND NR 6 BRAKES AN D TIRE/WHEEL ASSEMBLIES. LANDING GEAR INSPECTED FOR DAMAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 1999102900571 19991029 00571 WP 1999 10 29 AALA991383 1 19990911 A 2916 AYG70275015 RESERVOIR DOUG DC10 DC1030 3023501 WP NR 3 HYD SYSTEM DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 164AA 46950 DFW - FLT 5 - AFTER TAKEOFF DFW-HNL, NR 3 HYDRAULIC TEMPERATURE REACHED 103 DEGREES AND CONTINUED TO CLIMB WITH BOTH ENG INE DRIVEN PUMPS OFF AND THE 2-3 REVERSIBLE PUMP OPERATING. AIRCRAFT RETURNED TO DFW, DUMPED FUEL, AND LANDED WITHOUT I NCIDENT. REPLACED NR 3 HYDRAULIC RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999102900572 19991029 00572 WP 1999 10 29 AALA991372 1 19990910 A 2170 1879421 COALESCER BAG DOUG DC10 DC1030 3023501 WP CABIN DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 163AA 46914 SFO - FLT 73 - EN ROUTE ORD-HNL - FAINT BURNING ODOR NOTED AROUND 3R DOOR. AIRCRAFT DIVERTED TO SFO AND LANDED WITHOUT INCIDENT. INSPECTED WIRING, LIGHT BALLASTS AND COOLING FANS IN AREA OF 3R DOORWAY. CHANGED COALESCER BAGS ON AIR CONDI TIONING PACKS 1, 2 AND 3. NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999102900573 19991029 00573 WP 1999 10 29 AALA991255 1 19990823 A 2842 003001001 PROBE DOUG DC10 DC1030 3023501 WP FUEL TANK DEFECTIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 144AA 1005 47848 LAX - FLT 123 - EN ROUTE DFW-HNL - NUMBER 2 FUEL TANK QTY GAUGE INDICATED 5000 LBS LESS THAN TANKS 1 AND 3. FUEL WAS TR ANSFERRED AND TANKS BALANCED. CONTINUED FLIGHT UNTIL FUEL GAUGES INDICATED APPROXIMATELY 5000 LBS FUEL LESS THAN PLANNE D USAGE. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED LEFT FUEL JUNCTION PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999102900574 19991029 00574 1999 10 29 AALA991310 4 19990902 A 2565 EDR091276108 SLIDE DOUG DC10 DC1010 3022110 WP R-3 DOOR DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 0438 47828 SFO - DURING OVERNIGHT MAINTENANCE, INADVERENT SLIDE DEPLOYMENT OF OVERWING SLIDE AT DOOR R-3. SLIDE DEPLOYED ON THE WI NG BUT DID NOT DEPLOY TO THE GROUND. REPLACED OVERWING SLIDE AT R-3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999102900575 19991029 00575 NM 1999 10 29 AALA991149 1 19990807 A 2910 AE1011181H1190 LINE DOUG MD11 MD11 3023602 NM LT MLG DEFECTIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 1763 48553 MIA - FLT 901 - AFTER TAKEOFF MIA, UNABLE TO RAISE LANDING GEAR HANDLE. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPL ACED HYDRAULIC LINE ON LEFT MAIN LANDING GEAR TO TRUCK BEAM TRIM CYLINDER. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999102900576 19991029 00576 1999 10 29 G60A035 4 19990927 A 2350 CP1600A AUDIO CONTROL DOUG DC10 DC1030F 3023504 WP F/E'S PANEL FAILED A G6OA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 600GC 1325 46965 F/E AUDIO CONTROL PANEL INOPERATIVE AND STARTED SMOKING. DISCONNECTED CONTROL PANEL. REMOVED AND REPLACED AUDIO CONTRO L PANEL AND SYSTEM OPS CHECK NORMAL IAW MM 23-44-00. (M) 2 L 7 3 4F RT A22WE 1999102900577 19991029 00577 NM 1999 10 29 USAASB99195 1 19990808 A 2150 65789473 DUCT BOEING 737 7372B7 1384560 NM AIR COND BAY DETERIORATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 281AU 23114 BUF - FLT 2689 - AFTER TAKEOFF FROM BUF, WHILE ACCOMPLISHING AFTER TAKEOFF CHECKLIST, CREW HEARD A LOUD BANG AS PACKS WE RE TURNED ON. FLIGHT ATTENDANT IN REAR OF AIRCRAFT REPORTED A WHITE/GRAY SMOKE IN THE REAR OF THE CABIN. CREW TURNED P ACKS OFF AND SMOKE APPEARED TO SUBSIDE. FLIGHT RETURNED TO FIELD AT BUF AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGE NCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT MIX CHAMBER AND SUPPLY DUCT DETERIORATED. REMOVED AND REPLACED SAME. RA N AIR CONDITIONING SYSTEM. NO PRESSURE LEAKS OR SMOKE NOTED. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999102900578 19991029 00578 WP 1999 10 29 USAAD99139 1 19990923 A 3231 39567851 LINK DOUG DC9 DC931 3022065 WP NLG DOOR FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 926VJ 48146 CLT-PIT - FLT 1230 - AFTER TAKEOF AND THE LANDING GEAR WAS RETRACTED, THERE WAS A NOISE IN THE NOSE GEAR WELL. A VIBRAT ION THEN OCCURRED. WHEN THE LANDING GEAR WAS LOWERED TO RETURN TO THE FIELD THE VIBRATION CEASED. THERE WERE NO ABNORM AL INDICATIONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT NOSE LANDING GEAR DOO R LINK ASSY. ADJUSTED RIGHT NOSE LANDING GEAR DOOR. JACKED AND SWUNG NOSE GEAR PER MM 32-30-0. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4F A6WE 1999102900579 19991029 00579 EU 1999 10 29 USAAF99047 1 19990924 A 3350 362624 LIGHT FOKKER F28 F28MK0100 4990807 EU FORWARD INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 860US 11295 IND - FOUND FLOOR EMERGENCY LIGHTS IN THE FIRST CLASS SECTION INOPERATIVE. MAINTENANCE REPLACED BOTH LIGHT STRIPS. (M) 2 L 7 2 4F RT 1999102900580 19991029 00580 NM 1999 10 29 USAABB99044 1 19990922 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM ROW 6/13/18/33 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 PHL - FOUND EMERGENCY LIGHTS AT ROWS 6, 13, 18 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M) 2 L 7 2 4F RT A2NM 1999102900581 19991029 00581 NM 1999 10 29 USAASB99231 1 19990916 A 7921 6A47000 CSD OIL COOLER BOEING 737 737201 1384454 NM NR 2 ENGINE BIRD STRIKE A USAA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 244US 31878 22752 BOS - FLT 2851 - DURING TAKEOFF, TWO SEA GULLS STRUCK THE NR 2 ENGINE. AFTER INGESTION, THERE WAS A SMELL IN THE CABIN. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLI SHED BIRD STRIKE CONDITIONAL INSPECTION PER MM 5-51-201 AND ACCOMPLISHED TAKEOFF POWER CHECK PER MM 5-51-20. REMOVED AN D REPLACED THE NR 2 ENGINE CSD OIL COOLER PER MM 24-11-21 DUE TO CONDITIONAL INSPECTION CHECK. PERFORMED ENGINE RUNUP. ALL PARAMETERS WITHIN LIMITS. NO LEAKS NOTED. (M) 2 L 7 2 4F A16WE 1999102900582 19991029 00582 NE 1999 10 29 USAAD99135 2 19990917 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LEFT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 927VJ 48154 687849 PHL-SYR - FLT 725 - AFTER TAKEOFF, THE LEFT ENGINE DEVELOPED COMPRESSOR STALLS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999102900583 19991029 00583 WP 1999 10 29 USAAD99141 1 19990928 A 3350 60030451LB SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 IND - AFT FLIGHT ATTENDANT EMERGENCY LIGHTS INOPERATIVE. TAILCONE ACTIVATED EMERGENCY LIGHT INOPERATIVE. CEILING EMERG ENCY LIGHTS AT SEAT ROWS 5 TO 9 DIM. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERIES FOR THE AFT FLIGHT ATTENDANT E MERGENCY LIGHS AND REPLACED THE BATTERIES FOR THE AFT FLIGHT ATTENDANT EMERGENCY LIGHTS AND REPLACED THE BATTERIES FOR T HE TAIL CONE ACTIVATED EMERGENCY LIGHT AND THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 5 TO 9. (M) 2 L 7 2 4F A6WE 1999102900584 19991029 00584 WP 1999 10 29 99ZZZM721 1 19990928 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 IND - AFT FLIGHT ATTENDANT EMERGENCY LIGHTS INOPERATIVE. TAILCONE ACTIVATED EMERGENCY LIGHT INOPERATIVE. CEILING EMERG ENCY LIGHTS AT SEAT ROWS 5 TO 9 DIM. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERIES FOR THE AFT FLIGHT ATTENDANT E MERGENCY LIGHS AND REPLACED THE BATTERIES FOR THE AFT FLIGHT ATTENDANT EMERGENCY LIGHTS AND REPLACED THE BATTERIES FOR T HE TAIL CONE ACTIVATED EMERGENCY LIGHT AND THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 5 TO 9. (M) 2 L 7 2 4F A6WE 1999102900585 19991029 00585 WP 1999 10 29 99ZZZM722 1 19990928 A 3350 408822101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 IND - AFT FLIGHT ATTENDANT EMERGENCY LIGHTS INOPERATIVE. TAILCONE ACTIVATED EMERGENCY LIGHT INOPERATIVE. CEILING EMERG ENCY LIGHTS AT SEAT ROWS 5 TO 9 DIM. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERIES FOR THE AFT FLIGHT ATTENDANT E MERGENCY LIGHS AND REPLACED THE BATTERIES FOR THE AFT FLIGHT ATTENDANT EMERGENCY LIGHTS AND REPLACED THE BATTERIES FOR T HE TAIL CONE ACTIVATED EMERGENCY LIGHT AND THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 5 TO 9. (M) 2 L 7 2 4F A6WE 1999102900586 19991029 00586 WP 1999 10 29 USAAD99143 1 19990930 A 3350 408822101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816US 48096 IND - THE CEILING EMERGENCY LIGHTS IN THE FIRST CLASS SECTION WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE FIRST CLASS SECTION CEILING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999102900587 19991029 00587 1999 10 29 USAAD99142 4 19990929 A 3460 15000532 CIRCUIT BREAKER DOUG DC9 DC981 3022081 WP EPC PANEL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 813US 48093 BOS-ATL - FLT 1957 - PRIOR TO REACHING CRUISE THE CAPTAINS FLIGHT DIRECTOR FAILED, THE AUTO PILOT AND AUTO THROTTLE DISC ONNECTED. SWITCH 'A' FOR THE DFGS WOULD NOT RESET. THE AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENA NCE REPLACED THE CIRCUIT BREAKER TO THE 'A' SWITCH FOR THE DFGS. (M) 2 L 7 2 4F A6WE 1999102900588 19991029 00588 WP 1999 10 29 GTOAA036 1 19990929 A 3350 EMBS139 BATTERY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A G6OA K NONE L NO TEST IN INSP/MAINT 1 EA 27 605GC 64915 47925 EMERGENCY LIGHT TEST DOES NOT COME ON WITH TEST. REMOVED AND REPLACED EMERGENCY BATTERY IAW MM 24-24-00. OPS CHECKED G OOD. (M) 2 L 7 3 4F A22WE 1999102900589 19991029 00589 SO 1999 10 29 ASOA99105 1 19990925 A 5230 12023117001 SEAL EMB 120 EMB120RT SO CARGO DOOR FAILED A ASOA B EMER. DESCENT O OTHER CL CLIMB 1 SO 11 247AS 120113 CLIMBING THROUGH 17,000 FEET, CREW FELT PRESSURIZATION FALL. PRESSURIZATION PANEL SHOWED CABIN PRESSURE CLIMBING. PILO T DECIDED TO START A DESCENT AND CABIN ALTITUDE REACHED 10,000 ALMOST IMMEDIATELY THE ALTITUDE REACHED 14,000 FEET. CRE W PERFORMED AN EMERGENCY DESCENT AND FOLLOWED PROCEDURES OUTLINED IN QRH. OXYGEN MASKS DROPPED AND FLIGHT RETURNED TO F LO. AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND CARGO DOOR SEAL BLOWN OUT. INSTALLED NEW CARGO DOOR SEAL. PRESSURIZED AIRCRAFT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102900590 19991029 00590 SO 1999 10 29 ASOA99104 1 19990924 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 239AS 12535 120057 DURING INSPECTION, NR 3 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102900591 19991029 00591 SO 1999 10 29 ASOA99103 1 19990922 A 2150 22045402 ACM EMB 120 EMB120RT SO LEFT INOPERATIVE A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 267AS 120198 FLT 4254 - WHILE AT GATE, CREW SMELLED SMOKE FROM F/O SIDE CONSOLE. SMOKE WAS COMING FROM COCKPIT VENTS. MAINTENANCE R EMOVED AND REPLACED THE LEFT ACM. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102900592 19991029 00592 NM 1999 10 29 ASAA9910197 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 750 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RIGHT FUSELAGE SKIN STATION 750 BETWEEN STRINGER 24R AND 25R WAS FOUND TO BE DAMAGED . REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102900593 19991029 00593 NM 1999 10 29 ASAA9910198 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 727 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE SKIN AT STATION 727B TO 747 BETWEEN STRINGER 23R AND 24R WAS FOUND TO BE DE NTED AND CANNING. REPAIRED PER SRM 53-30-03. (M) 2 L 7 2 4F A16WE 1999102900594 19991029 00594 NM 1999 10 29 ASAA9910199 1 19990625 A 5330 6545775561 SKIN BOEING 737 737210C 1384459 NM BS 727 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE SKIN AT STATION 727 TO 908 STRINGER 20R TO 26R WAS FOUND TO BE DAMAGED. RE PAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102900595 19991029 00595 NM 1999 10 29 ASAA9910200 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 861 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE SKIN AT STATION 861 JUST BELOW STRINGER 24R WAS FOUND TO BE DAMAGED. REPAI RED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102900596 19991029 00596 NM 1999 10 29 ASAA9910201 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 883 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RT FUSELAGE SKIN AT STATION 877 AND 883 BETWEEN STRINGER 20R AND 21R WAS FOUND TO BE DAMAGED. REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102900597 19991029 00597 NM 1999 10 29 ASAA9910202 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 880 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RIGHT FUSELAGE SKIN AT STATION 880 BELOW STRINGER 23R WAS FOUND TO BE DAMAGED. REPA IRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102900598 19991029 00598 NM 1999 10 29 ASAA9910203 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 897 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RIGHT FUSELAGE SKIN AT STATION 897 BETWEEN STRINGER 23R AND 24R WAS FOUND TO BE DAMA GED. REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102900599 19991029 00599 NM 1999 10 29 ASAA9910204 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 890 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RIGHT FUSELAGE SKIN AT STATION 890 BETWEEN STRINGER 21R AND 22R WAS FOUND TO BE DAMA GED. REPAIRED PER SRM 53-30-3 AND SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999102900600 19991029 00600 NM 1999 10 29 ASAA9910205 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 898 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE RIGHT FUSELAGE SKIN AT STATION 898 BETWEEN STRINGER 22R AND 23R WAS FOUND TO BE DAMA GED. REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1999102900601 19991029 00601 NM 1999 10 29 ASAA9910206 1 19990625 A 5330 SKIN BOEING 737 737210C 1384459 NM BS 1088 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE EXTERNAL FUSELAGE SKIN AT STATION 1088 STRINGER 25R WAS FOUND TO BE GOUGED. REPAIRE D PER SRM 53-00-01. (M) 2 L 7 2 4F A16WE 1999102900602 19991029 00602 NM 1999 10 29 ASAA9910207 1 19990625 A 5311 69432861 FRAME BOEING 737 737210C 1384459 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE STUB FRAME AFT OF STATION 947 STRINGER 21L WAS FOUND TO BE CORRODED. REPAIRED PER D WG 69-43286-1. (M) 2 L 7 2 4F A16WE 1999102900603 19991029 00603 NM 1999 10 29 ASAA9910208 1 19990625 A 5320 6549914543 FITTING BOEING 737 737210C 1384459 NM BS 1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, STRINGER 21L END FITTING WAS FOUND TO BE CORRODED AT STATION 1016. REPAIRED PER DWG 654 9914. (M) 2 L 7 2 4F A16WE 1999102900604 19991029 00604 NM 1999 10 29 ASAA9910164 1 19990625 A 5315 6554913502 FLOORBEAM BOEING 737 737210C 1384459 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE CABIN FLOORBEAM UPPER FLANGE STATION 947 LBL 40 TO RBL 40 WAS FOUND CORRODED. REPAI RED PER BOEING DRAWING 6554913. (M) 2 L 7 2 4F A16WE 1999102900605 19991029 00605 NM 1999 10 29 ASAA9910165 1 19990625 A 5315 6554906501 FLOORBEAM BOEING 737 737210C 1384459 NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE CABIN FLOORBEAM TOP SURFACE STATION 500A FROM BL 0 TO RBL 58.25 AND FROM BL 0 TO LBL 45.5 WAS FOUND CORRODED. REPAIRED PER EA 5310-01699. (M) 2 L 7 2 4F A16WE 1999102900606 19991029 00606 NM 1999 10 29 ASAA9910166 1 19990625 A 5320 BAC1498156 LOBE BOEING 737 737210C 1384459 NM BS 965-975 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FUSELAGE LOWER LOBE AREA STATION 965 TO 975 STRINGER 27L WAS FOUND CORRODED. REPAIR ED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1999102900607 19991029 00607 NM 1999 10 29 ASAA9910167 1 19990625 A 5311 601461 FRAME BOEING 737 737210C 1384459 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE LOWER FORWARD AND AFT SIDE OF THE FRAME STATION 727A STRINGER 22L WAS FOUND CORRODED . REPARIED PER SRM 53-10-1. (M) 2 L 7 2 4F A16WE 1999102900608 19991029 00608 NM 1999 10 29 ASAA9910168 1 19990625 A 5311 1530030136 FRAME BOEING 737 737210C 1384459 NM BS 847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FRAME AT STATION 847 STRINGER 24R TO 25R WAS FOUND CORRODED. REPAIRED PER SB 737-53 -1096. (M) 2 L 7 2 4F A16WE 1999102900609 19991029 00609 NM 1999 10 29 ASAA9910169 1 19990625 A 5311 6546563502 FRAME BOEING 737 737210C 1384459 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE FRAME AT STATION 967 STRINGER 22L WAS FOUND CORRODED. REPAIRED PER SRM 53-10-1. (M ) 2 L 7 2 4F A16WE 1999102900610 19991029 00610 NM 1999 10 29 ASAA9910170 1 19990625 A 5347 SEAT TRACK BOEING 737 737210C 1384459 NM BS 663-727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, MAIN CABIN SEAT TRACK AT STATION 663 TO 727 RBL 45.5 WAS FOUND CORRODED. REPAIRED PER S RM 53-10-5. (M) 2 L 7 2 4F A16WE 1999102900611 19991029 00611 NM 1999 10 29 ASAA9910171 1 19990625 A 5320 6567140 BEAM BOEING 737 737210C 1384459 NM BS 540-706 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE MAIN CABIN TOP OF THE SEAT TRACK SUPPORT BEAM TOP AND BOTTOM SIDES WERE FOUND CORROD ED AT STATION 540 TO 706 RBL 24.5. REPAIRED PER EA 5310-01707. (M) 2 L 7 2 4F A16WE 1999102900612 19991029 00612 NM 1999 10 29 ASAA9910172 1 19990625 A 5320 6567140 BEAM BOEING 737 737210C 1384459 NM BS 540-706 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE MAIN CABIN TOP OF THE SEAT TRACK SUPPORT BEAM TOP AND BOTTOM SIDES WERE FOUND CORROD ED AT STATION 540 TO 706 BL 0. REPAIRED PER EA 5310-1707. (M) 2 L 7 2 4F A16WE 1999102900613 19991029 00613 NM 1999 10 29 ASAA9910173 1 19990625 A 5312 6516300301 BULKHEAD CHORD BOEING 737 737210C 1384459 NM BS 178 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - FOUND SCHEDULED D-CHECK, THE BULKHEAD SIDE CHORD RADIUS STATION 178 AT WL 207 FOUND CRACKED. REPAIRED PER SB 737- 53A1173. (M) 2 L 7 2 4F A16WE 1999102900614 19991029 00614 NM 1999 10 29 ASAA9910174 1 19990625 A 5320 6545855 ANGLE BOEING 737 737210C 1384459 NM BS 967 MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, A DOUBLE DRILLED HOLE WAS FOUND IN THE CUSP ANGLE AT STATION 967 STRINGER 17R. REPAIRED PER EA 5310-01703. (M) 2 L 7 2 4F A16WE 1999102900615 19991029 00615 NM 1999 10 29 ASAA9910175 1 19990625 A 5312 BULKHEAD BOEING 737 737210C 1384459 NM BS 178 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE BULKHEAD AT STATION 178 RBL 11 AND WL 218 FORWARD SIDE CRACKED. REPAIRED PER SRM 53 -10-11. (M) 2 L 7 2 4F A16WE 1999102900616 19991029 00616 NM 1999 10 29 ASAA9910176 1 19990625 A 5312 BULKHEAD CHORD BOEING 737 737210C 1384459 NM BS 178 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE BULKHEAD VERTICAL CHORD STATION 178 LBL 5.7 AT WL 190 CRACKED. REPAIRED PER SRM 53- 10-11. (M) 2 L 7 2 4F A16WE 1999102900617 19991029 00617 NM 1999 10 29 ASAA9910177 1 19990625 A 5320 65C25211 FITTING BOEING 737 737210C 1384459 NM BS 639 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE OVERWING STUB FRAME ATTACH FITTING STATION 639 RBL 45.5 CRACKED WERE FRAME TIES INTO SEAT TRACK FRAME WEB. REPAIRED PER SB 737-53-1061. (M) 2 L 7 2 4F A16WE 1999102900618 19991029 00618 NM 1999 10 29 ASAA9910178 1 19990625 A 5320 6935352 TIE BOEING 737 737210C 1384459 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE AFT CARGO COMPARTMENT STRINGER TIE CHORD STATION 967 STRINGER 20L WAS FOUND CORRODED . REPAIRED PER SRM 53-10-04. (M) 2 L 7 2 4F A16WE 1999102900619 19991029 00619 NM 1999 10 29 ASAA9910179 1 19990625 A 5313 STRINGER BOEING 737 737210C 1384459 NM BS 950 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 PHX - DURING SCHEDULED D-CHECK, THE INBOARD SIDE OF STRINGER 21R STATION 950 WAS FOUND CORRODED. REPAIRED PER SRM 53-10 -3. (M) 2 L 7 2 4F A16WE 1999102900620 19991029 00620 EU 1999 10 29 C2XA99IA494 1 19990923 A 5312 S53971402260 BULKHEAD AEROSP ATR42 ATR42320 8680930 EU MLG WW CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FRAME 27 BULKHEAD WAS FOUND TO BE CORRODED IN THE MAIN LANDING GEAR WHEEL WELL. MAINTE NANCE REPAIRED THE BULKHEAD IAW ATR REPAIR DRAWING 5539R0068, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900621 19991029 00621 SO 1999 10 29 C2XA99BT090 1 19990924 A 3350 20131A POWER SUPPLY EMB 145 EMB145 SO LT/RT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 BTV - DURING 4A INSPECTION MAINTENANCE, FOUND LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE AND TWO AFT EMERGENCY CEILING LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY. OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999102900622 19991029 00622 SO 1999 10 29 C2XA99BT091 1 19990924 A 2760 14533022405 CONTROL UNIT EMB 145 EMB145LR SO SPOILER SYSTEM FAILED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 13949 145057 EWR - FLT 4088 - CREW REPORTED ASYMETRIC SPOILER DEPLOYMENT AT FL350-360 AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AN D REPLACED SPOILER CONTROL UNIT AND OPS CHECKED SPOILERS AND SPEED BRAKE GOOD. (M) 2 L 7 2 4T RT T00011AT 1999102900623 19991029 00623 EU 1999 10 29 C2XA99IA492 1 19990918 A 5320 S53571401209 DOUBLER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND PREVIOUS REPAIR DOUBLER GOUGED ABOVE FUELING CONTROL PANE. REMOVED AND REPLAC ED DOUBLER IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900624 19991029 00624 EU 1999 10 29 C2XA99IA491 1 19990918 A 5311 S5367121721101 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RT WEB AT FRAME 36. REMOVED AND REPLACED WEB IAW SRM 51-25-02 AN D 51-21-31. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900625 19991029 00625 EU 1999 10 29 C2XA99IA490 1 19990918 A 5315 S53672406200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON FRAME 36 FLANGE AT RT STRINGER 14. REMOVED CORROSION, REPAIRED F RAME IAW SRM 51-21-42, 51-21-17, 51-21-31 AND 53-61-40. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900626 19991029 00626 EU 1999 10 29 C2XA99IA489 1 19990918 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT FLOORBEAM AT FRAME 38 CORRODED. REMOVED CORROSION IAW SRM 51-21-42, REPA IRED FLOORBEAM IAW CONTINENTAL EXPRESS DC5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900627 19991029 00627 EU 1999 10 29 C2XA99IA488 1 19990818 A 5315 S53672408202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT FLOORBEAM AT FRAME 39 CORRODED. REMOVED CORROSION IAW SRM 51-21-42. RE PAIRED FLOORBEAM IAW CONTINENTAL EXPRESS EC5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900628 19991029 00628 EU 1999 10 29 C2XA99IA487 1 19990918 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 34-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT CENTER SEAT TRACK CORRODED BETWEEN FRAMES 34 AND 36. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900629 19991029 00629 EU 1999 10 29 C2XA99IA486 1 19990918 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT AFT SEAT TRACK CORRODED BETWEEN FRAMES 39 AND 40. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-25-03. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900630 19991029 00630 EU 1999 10 29 C2XA99IA485 1 19990918 A 5320 S5367800920102 ANGLE AEROSP ATR42 ATR42320 8680930 EU FRAME 36-38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT FLOOR SUPPORT CORRODED BETWEEN FRAMES 36 AND 38. REMOVED AND REPLACED F LOOR SUPPORT ANGLES IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900631 19991029 00631 EU 1999 10 29 C2XA99IA484 1 19990918 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT CENTER SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 39. REMOVED AND REPLACE D SEAT TRACK IAW SRM 51-25-03. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900632 19991029 00632 EU 1999 10 29 C2XA99IA483 1 19990918 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT CENTER SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 39. REMOVED AND REPLAC ED SEAT TRACK IAW SRM 51-25-03. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900633 19991029 00633 SO 1999 10 29 C2XA99IA482 1 19990918 A 5713 12016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19704 120086 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT WING LOWER SKIN 2ND STRINGER CRACKED AT PANEL 522EB. REMOVED DAMAGED SEC TION OF STRINGER, SPLICED IN NEW SECTION IAW CONTINENTAL EXPRESS EC5710-01010 REV B. AIRCRAFT APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A31SO 1999102900634 19991029 00634 SO 1999 10 29 C2XA99IA481 1 19990918 A 5713 12016079001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19704 120086 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT WING LOWER SKIN 4TH STRINGER CRACKED AT PANEL 522EB. REMOVED DAMAGED SEC TION OF STRINGER, SPLICED IN NEW SECTION IAW CONTINENTAL EXPRESS EC5710-01010 REV B. AIRCRAFT APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A31SO 1999102900635 19991029 00635 SO 1999 10 29 C2XA99IA480 1 19990918 A 5713 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19704 120086 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT WING INTERNAL LOWER STRINGER CRACKED FORWARD OF PANEL 622EB. REMOVED EX ISTING STRINGER SPLICE AND INSTALLED NEW SPLICE IAW CONTINENTAL EXPRESS EC5710-01010 REV B AND DER REPORT NR 99-150. AI RCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102900636 19991029 00636 SO 1999 10 29 C2XA99IA479 1 19990918 A 5730 12042999003 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19704 120086 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT WING LOWER SKIN CRACKED AT REFUEL/DEFUEL ADAPTOR ACCESS PANELS. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102900637 19991029 00637 SO 1999 10 29 C2XA99IA478 1 19990918 A 5730 12042336002 SKIN EMB 120 EMB120RT SO WS 2480 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19704 120086 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT WING LOWER SKIN CRACKED AT STATION YA2480 FORWARD OF PANEL 622EB. STOP DRI LLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW GRISWOLD ENGINEERING DER REPORT NR 99-150. AIRCRAFT APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102900638 19991029 00638 SO 1999 10 29 C2XA99IA477 1 19990918 A 5330 12019229002 SKIN EMB 120 EMB120RT SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19704 120086 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT FUSELAGE SKIN CHAFFED BY A/C HEAT EXCHANGER AND DUCTS. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02 AND 51-21-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999102900639 19991029 00639 EU 1999 10 29 C2XA99IA476 1 19990921 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR42-320 MM 33-51-20, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900640 19991029 00640 SO 1999 10 29 C2XA99IA475 1 19990920 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 IAH - DURING MAINTENANCE INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999102900641 19991029 00641 NM 1999 10 29 EIA990191 1 19990817 A 2710 69B81284 SPRING BOEING 747 747212B 1384886 NM AILERON BROKEN A EIAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 485EV 20712 DURING FLIGHT, THE FIRST OFFICERS CONTROL COLUMNS LATERAL MOVEMENT BECAME HEAVY WITH A CONSIDERABLE AMOUTN OF SLACK. A L OUD POPPING NOISE WAS HEARD FROM F/O'S FLOOR AREA. MAINTENANCE PERSONNEL FOUND THE AILERON SYSTEM LOAD LIMIT SPRING BRO KEN. SPRING WAS REPLACED AND RIGGED IAW MM. (M) 2 L 7 4 4F A20WE 1999102900642 19991029 00642 NE 1999 10 29 EIA990190 2 19990817 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 1 SHUT DOWN A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 480EV 20348 662480 VHHH - THE NR 1 ENGINE SHUT DOWN ON CLIMB-OUT. ENGINE WAS RESTARTED AND RUN AT PARTIAL POWER UNTIL EGT REACHED 750. EN GINE WAS SHUT DOWN AT THAT POINT FOR REMAINEDER OF FLIGHT. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999102900643 19991029 00643 NM 1999 10 29 EIA990189 1 19990814 A 2820 7583149 FILTER BOEING 747 747132 1384882 NM MAIN FUEL TANK CONTAMINATED A EIAA O OTHER J WARNING INDICATION DE DESCENT 1 NM 09 481EV 19896 VHHH - ON DESCENT, THROUGH FL310, CREW NOTED THE SUDDEN ROLL BACK OF THE NR 3 ENGINE. ENGINE WAS RESTARTED AND FLIGHT C ONTINUED. MAINTENANCE FOUND A CONTAMINATED MAIN FUEL FILTER. FILTER WAS REPLACED AND TANK SUMPED. (M) 2 L 7 4 4F A20WE 1999102900644 19991029 00644 WP 1999 10 29 EIA990188 1 19990726 A 2720 PEDAL DOUG DC9 DC933F 302207A WP RUDDER BINDING A EIAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 09 945F 47279 KSEA - ON FLIGHT 823, CRWE REPORTED THAT ON TAKEOFF ROLL AT ABOUT 100 KTS AIRCRAFT BEGAN PULLING TO THE RIGHT. CAPTAIN APPLIED HEAVY LEFT FOOT PRESSURE ON THE LEFT RUDDER AND HEARD AN AUDIBLE SNAP. CAPTAIN THEN RELEASED PRESSURE ON PEDAL AND AIRCRAFT IMMEDIATELY STARTED RIGHT. CAPTAIN THEN ABORTED TAKEOFF AT APPROX 120 KNOTS. MAINTENANCE FOUND RUDDER PED AL TRIM BINDING ON CAPTAINS RUDDER PEDAL. MAINTENANCE REMOVED OBSTRUCTION AND SECURED TRIM PER MM. (M) 2 L 7 2 4F A6WE 1999102900645 19991029 00645 WP 1999 10 29 EIA990187 1 19990722 A 7830 5958782503 DRIVE LINK DOUG DC9 DC933F 302207A WP NR 2 ENGINE BROKEN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47279 AFTER LANDING AT PAJN, RIGHT ENGINE THRUST REVERSER WOULD NOT STOW. THRUST REVERSER DRIVE LINK P/N 5958782-503 FOUND BR OKEN. (M) 2 L 7 2 4F A6WE 1999102900646 19991029 00646 WP 1999 10 29 EIA990179 1 19990630 A 3246 9550267 WHEEL DOUG DC9 DC933F 302207A WP NLG OUT OF BALANCE A EIAA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 NM 09 944F 47194 SYR - ON TAKEOFF ROLL AT APPROX 60-80 KNOTS, AIRCRAFT EXPERIENCED SEVERE VIBRATION APPEARED TO BE COMING FROM NOSEWHEEL. TAKEOFF WAS ABORTED AND VIBRATION STOPPED AT APPROX 25 KNOTS. REPLACED NOSEWHEEL TIRES AFTER INSPECTION OF NOSE GEAR PER MM 32-40-2. (M) 2 L 7 2 4F A6WE 1999102900647 19991029 00647 WP 1999 10 29 EIA990171 1 19990404 A 5310 STRUCTURE DOUG DC9 DC915F 3022037 WP BS 503 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 MZJ - DURING C-CHECK, THE KEEL BEAM AND STRINGER 29L WAS FOUND TO HAVE HEAVY CORROSION. SKIN AND WEB ATTACHED TO KEEL B EAM AT FS 483 TO FS 503 ALSO SHOWED SIGNS OF CORROSION. REPAIR COMPLETED WITH ECRA 915-53-35-2. TREATED ALL REPAIRED P ARTS AND AREAS PER SRM DC9 51-10-3 PAGE 18. PRIMED REPAIRED PARTS AND AREAS PER DC9 51-10-3 PAGE 16. (M) 2 L 7 2 4F A6WE 1999102900648 19991029 00648 NM 1999 10 29 EIAA990003 1 19990120 A 3350 BATTERY BOEING 747 747SR46 NM CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478EV 21033 KSUU - MAINTENANCE PERSONNEL DISCOVERED A PORTABLE FLASHLIGHT ONBOARD AIRCRAFT THAT DID NOT SHOW A CHARGE AND WAS NOT CH ARGED. MAINTENANCE CREW DEFERRED THIS ITEM AND INSTALLED PLACARDS. (M) 2 L 7 4 4F A20WE 1999102900649 19991029 00649 NM 1999 10 29 EIAA990001 1 19990110 A 5411 FRAME BOEING 747 747132 1384882 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 91782 19896 HKG - DURING B-CHECK, NR 2 PYLON NACELLE STATION 162 LEFT AND RIGHT FRAMES FOUND CRACKED ADJACENT TO FIRE BOTTLE ATTACHM ENTS. REPAIRED PER SRM 54-10-03 FIG 1. (M) 2 L 7 4 4F A20WE 1999102900657 19991029 00657 EU 1999 10 29 F3LA99125 2 19991006 A 7230 BEARING BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE FAILED A F3LA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 NM 03 304FL 27633 BHM - EN ROUTE FROM MCO TO DEN, FLIGHT CREW REPORTED TWO LOUD BANGS FROM NR 2 ENGINE AND EGT ROSE TO 900 DEGREES. THE N R 2 ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT WAS DIVERTED TO BHM AND LANDED WITHOUT INCIDENT. FLIGH T CREW OBSERVED METAL IN THE TAILPIPE ON POST FLIGHT WALKAROUND. AIRCRAFT IS CURRENTLY IN BHM AWAITING INSTALLATION OF A REPLACEMENT ENGINE. CAUSE OF DAMAGE WS DUE TO NR 3 BEARING FAILURE. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1999102900660 19991029 00660 EU 1999 10 29 SIMA992432 1 19990831 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 277AT 1007 277 SAW - DURING PS-2 INSPECTION, FOUND THE PASSENGER DOOR EMERGENCY LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE LIG HT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999102900661 19991029 00661 EU 1999 10 29 SIMA992431 1 19990831 A 3350 1155561 LAMP HOLDER AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 246AE 243 SAW - DURING PS-2 INSPECTION, FOUND THE THREE FORWARD EMERGENCY FLOOR LIGHTS DID NOT ILLUMINATE. REPAIRED THE HARNESS A T 33WL. REMOVED AND REPLACED LAMP HOLDERS AND SOCKETS. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999102900662 19991029 00662 EU 1999 10 29 99ZZZM723 1 19990831 A 3350 LH6151 SOCKET AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 246AE 243 SAW - DURING PS-2 INSPECTION, FOUND THE THREE FORWARD EMERGENCY FLOOR LIGHTS DID NOT ILLUMINATE. REPAIRED THE HARNESS A T 33WL. REMOVED AND REPLACED LAMP HOLDERS AND SOCKETS. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999102900663 19991029 00663 EU 1999 10 29 SIMA992352 1 19990823 A 3350 301151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 47AE 4195 047 SAW - DURNG PS-2 INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY PACK AT LOCATION 18WL TO BE DISCHARGED. REMOVED AND REPL ACED THE BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900664 19991029 00664 EU 1999 10 29 SIMA992351 1 19990823 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AE 19797 243 SAW - DURING PS-2 INSPECTION, FOUND EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 5A DOES NOT ILLUMINATE. REMOVED AND REPLACE D EMERGENCY LIGHT BATTERY PACK AT LOCATION 3WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900665 19991029 00665 EU 1999 10 29 SIMA991932 1 19990710 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 3539 223 SAW - DURING PS-2 INSPECTION, FOUND SEVERAL INTERIOR EMERGENCY LIGHTS THAT DID NOT ILLUMINATE. REMOVED AND REPLACED EME RGENCY LIGHT BATTERY PACK AT LOCATION 29WL IAW 33-51-21-RAI-10010-004. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999102900666 19991029 00666 EU 1999 10 29 SIMA992571 1 19990914 A 3350 EU24628A0 RELAY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST CR CRUISE 1 SW 21 348AE 349 HOU - FLT 3618 - SEVERAL EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED EMERGENCY LIGHT RELAY 12LF AND OPE RATIONAL CHECKED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900667 19991029 00667 EU 1999 10 29 SIMA992541 1 19990911 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 533AT 1187 533 SGF - FLT 3560 - AFT CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. AIRC RAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900668 19991029 00668 EU 1999 10 29 SIMA992516 1 19990908 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 536AT 0890 536 HOU - FLT 3541 - AFT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900669 19991029 00669 EU 1999 10 29 SIMA992402 1 19990828 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 538AT 0701 538 DFW - FLT 3739 - SEVERAL EMERGENCY EXIT LIGHTS AND FLOOR PROXIMITY LIGHTS REMAIN ILLUMINATED WITH POWER OFF. REMOVED AN D REPLACED TWO EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 43WL AND 62WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900670 19991029 00670 EU 1999 10 29 99ZZZM724 1 19990828 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 538AT 0710 538 DFW - FLT 3739 - SEVERAL EMERGENCY EXIT LIGHTS AND FLOOR PROXIMITY LIGHTS REMAIN ILLUMINATED WITH POWER OFF. REMOVED AN D REPLACED TWO EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS 43WL AND 62WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900671 19991029 00671 EU 1999 10 29 SIMA992401 1 19990828 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 494AE 1123 494 DFW - FLT 3506 - FORWARD EMERGENCY EXIT LIGHT, ONE OVERHEAD, AND EIGHT FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REPLAC ED BATTERY PACK AT LOCATION 61WL. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900672 19991029 00672 EU 1999 10 29 SIMA991862 1 19990705 A 3260 DHE1148 SWITCH AEROSP ATR72 ATR72212A 8680902 EU LANDING GEAR FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 538AT 7287 538 DFW - FLT 3626 - LANDING GEAR HANDLE WOULD NOT MOVE TO RAISE GEAR AFTER TAKEOFF. REMOVED AND REPLACED RIGHT OUTBOARD WO W SWITCH. LANDING GEAR OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900673 19991029 00673 EU 1999 10 29 SIMA992591 1 19990916 A 3350 1317 BULB SAAB SF340 340B 7860101 EU ROW 4A FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 339SB 340B339 SBP - DURING PS-2 INSPECTION, FOUND OVERHEAD EMERGENCY LIGHT AT LOCATION 4A FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW AMM 33-50-00. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999102900674 19991029 00674 EU 1999 10 29 SIMA992601 1 19990917 A 3350 9HB00593312 PANEL SAAB SF340 340B 7860101 EU ROW 8A BROKEN A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 247AE 340B247 DFW - FLT 3738 - EMERGENCY EXIT LIGHT AT SEAT 8A IS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PANEL OVER SEAT 8A . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999102900675 19991029 00675 NM 1999 10 29 USAASB99224 1 19990904 A 3397 WIRE BOEING 737 7373B7 1384580 NM ROW 5 DEF BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 518AU 23704 PHL - DURING OVERNIGHT MAINTENANCE CHECK, MAINTENANCE FOUND A SECTION EMERGENCY FLOOR PATH LIGHTING THAT WOULD NOT TEST ON THE RIGHT SIDE OF THE CABIN. MAINTENANCE TROUBLESHOT AND FOUND BROKEN WIRES AT SEAT ROW 5 DEF. REPAIRED BROKEN WIRE S. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1999102900676 19991029 00676 NM 1999 10 29 USAASB99226 1 19990904 A 3350 900835A POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 267AU 22879 BOS - MAINTENANCE FOUND THE AFT EMERGENCY LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERA TIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999102900677 19991029 00677 NM 1999 10 29 USAASB99228 1 19990912 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 782AU 25021 EWR - MAINTENANCE FOUND THE EMERGENCY EXIT AND AFT GALLEY AREAS GO DIM WITHIN SECONDS OF SWITCHING THEM ON. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT SEAT ROW 12 CEILING, LEFT SIDE AND THE AFT ENTRY LIGHT, RIGHT SIDE. OPERATIO NAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999102900678 19991029 00678 EU 1999 10 29 SIMA992691 1 19990924 A 3234 F96GA0102 GEAR CONTROL AEROSP ATR72 ATR72212 EU COCKPIT FAILED A SIMA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 21 431AT 583 431 NAS - FLT 5343 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE AS SEMBLY AND RECONNECTED CANNON PLUG AT LANDING GEAR CONTROL VALVE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900679 19991029 00679 EU 1999 10 29 SIMA992711 1 19990928 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE AND AFT OUTBOARD, THE LEFT AND RIGHT FLT ATTENDANT, THE LEFT AFT I NBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900680 19991029 00680 EU 1999 10 29 99ZZZM725 1 19990928 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE AND AFT OUTBOARD, THE LEFT AND RIGHT FLT ATTENDANT, THE LEFT AFT I NBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900681 19991029 00681 EU 1999 10 29 99ZZZM726 1 19990928 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE AND AFT OUTBOARD, THE LEFT AND RIGHT FLT ATTENDANT, THE LEFT AFT I NBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900682 19991029 00682 EU 1999 10 29 99ZZZM727 1 19990928 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE AND AFT OUTBOARD, THE LEFT AND RIGHT FLT ATTENDANT, THE LEFT AFT I NBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900683 19991029 00683 EU 1999 10 29 99ZZZM728 1 19990928 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE AND AFT OUTBOARD, THE LEFT AND RIGHT FLT ATTENDANT, THE LEFT AFT I NBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900684 19991029 00684 EU 1999 10 29 99ZZZM729 1 19990928 A 5347 S53070308200 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE AND AFT OUTBOARD, THE LEFT AND RIGHT FLT ATTENDANT, THE LEFT AFT I NBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900685 19991029 00685 EU 1999 10 29 SIMA992701 1 19990925 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 11709 017 SAW - DURING PS-2 INSPECTION, SEVERAL CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED THE EMERGENCY L IGHT BATTERY PACK AT LOCATION 18WL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900686 19991029 00686 EU 1999 10 29 SIMA992641 1 19990920 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 314AM 964 314 SAW - DURING PS-2 INSPECTION, FOUND THE PASSENGER DOOR EMERGENCY LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE LIG HT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900687 19991029 00687 EU 1999 10 29 SIMA992582 1 19990915 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 142DD 17799 040 SAW - DURING PS-2 INSPECTION, FOUND SEVERAL CABIN EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY L IGHT BATTERY PACK AT LOCATION 3WL IAW JIC 335121-RAI-10000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900688 19991029 00688 EU 1999 10 29 SIMA992581 1 19990915 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 16638 211 SAW - DURING PS-2 INSPECTION, FOUND SEVERAL CABIN EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY L IGHT BATTERY PACK AT LOCATION 10WL IAW JIC335121-RAI-10000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900689 19991029 00689 EU 1999 10 29 SIMA992681 1 19990925 A 2520 8E500556800 PSU AEROSP ATR72 ATR72212 EU ROW 5A FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 440AM 440 MIA - FLT 5386 - PASSENGER SERVICE UNIT ABOVE SEAT 5A EXCESSIVELY HOT WITH ASSOCIATED SMOKE AND ODOR. TURNED OFF MAIN S WITCH FOR ALL PASSENGER READING LIGHTS, HEAT, SMOKE AND ODOR DISSIPATED. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED PASSENGER SERVICE UNIT ABOVE SEAT 5A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900690 19991029 00690 1999 10 29 SIMA992674 4 19990924 A 3445 6228971120 TCAS COMPUTER AEROSP ATR72 ATR72212 EU AVIONICS BAY FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 420AT 1939 420 DFW - FLT 3506 - SULFUR LIKE SMELL IN THE COCKPIT. NO SMOKE. ALL INDICATIONS WERE NORMAL. HOWEVER, THE TCAS FELL OFF LINE AT THE SAME TIME. INSEPCTED TCAS CONNECTORS WITH NO DEFECTS NOTED. REMOVED AND REPLACED TCAS COMPUTER. OPERATION AL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900691 19991029 00691 EU 1999 10 29 SIMA992602 1 19990917 A 3350 OL6839BPE LAMP AEROSP ATR72 ATR72212 EU ROW 6 FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 434AT 434 MIA - FLT 5315 - CABIN EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 6 DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERAT IONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999102900692 19991029 00692 EU 1999 10 29 SIMA992592 1 19990916 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 540AM 1244 540 HOU - FLT 3635 - PASSENGER AND SERVICE DOOR EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999102900693 19991029 00693 EU 1999 10 29 SIMA992751 1 19991002 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 8A FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 231LN 340B231 DFW - FLT 3906 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999102900694 19991029 00694 EU 1999 10 29 SIMA992702 1 19990927 A 3350 1317 BULB SAAB SF340 340B 7860101 EU ROW 8BC FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 354SB 340B354 DFW - FLT 3708 - EMERGENCY LIGHT AT SEAT 8BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB OVER SEAT 8BC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999102900695 19991029 00695 NM 1999 10 29 P2EA99289 1 19990929 A 2612 FIRE LOOP BOEING 737 737247 138448D NM NR 1 ENGINE MALFUNCTIONED A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 912MP 19607 MCI - FLT 301 - AIR RETURN, EMERGENCY DECLARED, LANDING UNEVENTFUL. DURING CLIMB, NR 1 ENGINE FIRE LIGHT ILLUMINATED. P RECAUTIONARY ENGINE SHUT DOWN WAS ACCOMPLISHED PER CHECKLIST. REPLACED FIRE CONTROL MODULE, NO HELP, REINSTALLED ORIGIN AL. REPLACED ADEL CLAMP INSULATORS ON NR 1 ENGINE LOWER FIRE LOOP. CLEANED FORWARD AND AFT CONNECTORS ON LOWER FIRE LO OP. RAN ENGINE. FIRE DETECTION SYSTEM OPERATES NORMAL. (M) 2 L 7 2 4F A16WE 1999102900696 19991029 00696 NM 1999 10 29 P2EA99298 1 19990825 A 5320 BEAM BOEING 737 737247 138448D NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SPAN WISE BEAM NR 2, STRINGER 16C CRACKED AT BL 0. REPAIRED IAW EO COO-3-57-519-99. (M) 2 L 7 2 4F A16WE 1999102900697 19991029 00697 NM 1999 10 29 P2EA99297 1 19990822 A 5330 SKIN BOEING 737 737247 138448D NM BS 755 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN CRACKED AT BS 755 BETWEEN STRINGERS 17L AND 18L. REPAIRED IAW COOPESA EO COO-3-53-542-99. (M) 2 L 7 2 4F A16WE 1999102900698 19991029 00698 NM 1999 10 29 P2EA99296 1 19990821 A 5330 SKIN BOEING 737 737247 138448D NM BS 727 CANNED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN OIL CANNED AT BS 727B PLUS 14 BETWEEN STRINGERS 20L AND 21L. REPAIRED IAW COOPESA EO COO-3-53-542-99. (M) 2 L 7 2 4F A16WE 1999102900699 19991029 00699 NM 1999 10 29 P2EA99295 1 19990827 A 5330 SKIN BOEING 737 737247 138448D NM BS 807/840 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN DENTED AT BS 807 AND BS 840 BETWEEN 20R AND 24R. REPAIRED IAW SRM 51-10-01 PAGE 6. (M) 2 L 7 2 4F A16WE 1999102900700 19991029 00700 NM 1999 10 29 AALA996006 1 19990921 A 2760 FAIL LIGHT DOUG MD90 MD9030 3023690 NM AUTO SLAT ILLUMINATED A AALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 904RA 53570 RNO - AUTO SLAT SPOILER FAIL LIGHT CAME ON DURING TAKEOFF ROLL AT 65 KNOTS. TRANSFERRED TO DMI NR 18690 PER MEL 27-62-0 1 OPTION 1 PULLED CB 37-243 MANUAL USE ONLY. (M) 2 L 7 2 4F RT A6WE 1999102900701 19991029 00701 WP 1999 10 29 99ZZZM730 1 19990920 A 3340 8906K1665 SWITCH LKHEED 1011 10113851 5265010 WP OVERHEAD PANEL FAILED A AMTA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 197AT 193P1082 DURING CLIMB, SMOKE AND SMELL FOUND COMING FROM OVERHEAD PANEL BY LANDING LIGHT SWITCHES. TURNED OFF ALL SWITCHES, PULL ED CIRCUIT BREAKERS AND RETURNED FOR LANDING. REPLACED RIGHT LANDING LIGHT SWITCH. REPLACED H V LEAD TO LANDING LIGHT, CLEANED CONNECTIONS. OPERATIONALLY CHECKED AND NO SMOKE NOTED. (M) 2 L 7 3 4F A23WE 1999102900702 19991029 00702 WP 1999 10 29 99ZZZM731 1 19990916 A 5210 7424281 CABLE LKHEED 1011 10113851 5265010 WP L1 DOOR FAILED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 190AT 193C1086 DURING PREFLIGHT, THE L1 DOOR WILL NOT OPEN ELECTRICALLY OR MECHANICALLY. REPLACED L1 DOOR LOCK MECHANISM CONTROL CABLE IAW MM 52-12-27. OPS CHECKED NORMAL, OK FOR SERVICE. (M) 2 L 7 3 4F A23WE 1999102900703 19991029 00703 EU 1999 10 29 A6WA9900112 1 19990831 A 5210 BRACKET BAG BAE146 BAE146200A 1500266 EU PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 LEFT FORWARD PAX DOOR INTERNAL STRUCTURE HAS 2 ANGLE BRACKETS WITH 1 CRACK IN EACH. MFG AND REPLACED ABOVE 2 ANGLE BRAC KETS USING SRM AND DRAWINGS HC521H0507-000 AND HC521H0508-000. REAR 2 EACH TOP AND BOTTOM FASTENERS REPLACED WITH NAS B OLTS PER FAX DJR/RJ0318-97. (M) 2 H 7 4 4F RT A49EU 1999102900704 19991029 00704 EU 1999 10 29 A6WA9900101 1 19990903 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU BS 3/7/15/19/20 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 MAIN LANDING GEAR ROOF LONGERONS ARE CRACKED AT STATION 3, 7, 15, 19 AND 20 AT FRAME 29. REPAIRED IAW BAE REPAIR DRAWIN G HC536H9211 AND FAX REF NR DJR/RJ0207-97. (M) 2 H 7 4 4F RT A49EU 1999102900705 19991029 00705 EU 1999 10 29 A6WA9900102 1 19990903 A 5320 INTERCOSTAL BAG BAE146 BAE146200A 1500266 EU BS 9 CRACKED A A6WA O OTHER O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 INTERCOSTAL IS CRACKED JUST FORWARD OF MAIN LANDING GEAR ROOF LONGERONS AT STATION 9 FRAME 29 LOWER FLANGE. REPAIRED IA W BAE REPAIR DRAWINGS HC536H9211 AND FAX REF NR DJR/RJ0207/97. (M) 2 H 7 4 4F RT A49EU 1999102900706 19991029 00706 EU 1999 10 29 A6WA9900103 1 19990910 A 5320 INTERCOSTAL BAG BAE146 BAE146200A 1500266 EU BS 9 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 INTERCOSTAL IS CRACKED JUST FORWARD OF MAIN LANDING GEAR ROOF LONGERONS AT STATION 9 FRAME 29 FLOOR LOCKDOWN PLATE. REP AIRED IAW FAX REF BARA/AVR/4205/99. (M) 2 H 7 4 4F RT A49EU 1999102900707 19991029 00707 EU 1999 10 29 A6WA9900104 1 19990906 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 THE RIGHT AIRBRAKE UPPER HINGE OPENING UPPER AND LOWER FRAMES HAVE BEEN BADLY CHAFED BY CONTACT WITH THE AIRBRAKE ACTUAT OR. REPLACED UPPER LONGERON PER SRM AND FAX BARA/AVR/4144/99. NEW WORKCARD GENERATED TO REPAIR LOWER LONGERON. (M) 2 H 7 4 4F RT A49EU 1999102900708 19991029 00708 EU 1999 10 29 A6WA9900105 1 19990907 A 5712 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 LEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF RIB 9 IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING E DGE STIFFENER INBOARD OF RIB 9 IAW BAE FAX DJR/RJ0630-98. (M) 2 H 7 4 4F RT A49EU 1999102900709 19991029 00709 NM 1999 10 29 USAASB99223 1 19990907 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 244US 22752 BWI - FLT 2639 - BEFORE DEPARTURE, THE CAPTAIN REPORTED THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOR WAS INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999102900710 19991029 00710 NM 1999 10 29 USAASB99232 1 19990917 A 3350 6104789 BATTERY PACK BOEING 737 7372Q9 138448M NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 231US 21976 CLE - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING AND LOWER AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY (P/N 60-1321-1). OPERATIONAL CHECK GOOD (M) 2 L 7 2 4F A16WE 1999102900711 19991029 00711 WP 1999 10 29 USAAD99146 1 19991004 A 2150 PACK DOUG DC9 DC981 3022081 WP LEFT MALFUNCTIONED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 813US 48093 MSP-PIT - FLT 1426 - AFTER TAKEOFF SMOKE APPEARED IN THE COCKPIT ALONG WITH THE INABILITY TO CONTROL THE LEFT AIR CONDIT IONING TEMP CONTROL VALVE, STUCK IN FULL HOT. THE LEFT AIR CONDITIONING PACK WAS TURNED OFF AND THE SMOKE SUBSIDED. TH E AIRCRAFT RETURNE TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE LEFT AIR CONDITIONING PACK ON MEL A ND DISPATCHED THE AIRCRAFT. LATER MAINTENANCE OPERATED THE LEFT AIR CONDITIONING SYSTEM AND ALL OPERATION WAS NORMAL. ( M) 2 L 7 2 4F A6WE 1999102900712 19991029 00712 WP 1999 10 29 USAAD99145 1 19991002 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927VJ 48154 IND - THE AFT CABIN AND TAIL COMPARTMENT FLOOR TRACK EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT C ABIN AND TAIL COMPARTMENT FLOOR TRACK EMERGENCY LIGHT BATTERY CHARGER. (M) 2 L 7 2 4F A6WE 1999102900713 19991029 00713 WP 1999 10 29 USAA991069 1 19990926 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 69.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807US 49416 48039 PIT - DURING RON VISIT, FOUND 1 INCH CRACK IN SKIN AT RIGHT STATION 69.5 LONGERON 20 RT. INSTALLED DOUBLER PER SRM 53-0 1 FIG 4. (M) 2 L 7 2 4F A6WE 1999102900714 19991029 00714 WP 1999 10 29 USAAD99144 1 19990930 A 3231 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG DOORS LACK OF LUBE A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 816US 48096 CLT-SRQ - FLT 1448 - AFTER LANDING GEAR RETRACTION THERE WAS A LOUD NOISE IN THE NOSE GEAR AREA. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBED THE NOSE GEAR DOOR RELEASE/LOCK HANDLES AND CLO SED THE NOSE GEAR DOORS. (M) 2 L 7 2 4F A6WE 1999102900715 19991029 00715 NM 1999 10 29 USAA099904 1 19990929 A 2424 939D1502 VOLTAGE REGULATO BOEING 727 727227 1384078 NM NR 2 ENGINE FAILED A USAA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 EA 19 924TS 21041 FLT 6071 - BOS-LGA - ABORTED TAKEOFF DUE TO NR 2 GENERATOR DIFFERENTIAL FAULT, OVERVOLTAGE LIGHT ILLUMINATED. REPLACED NR 2 ENGINE VOLTAGE REGULATOR. OPERATIONAL CHECK NORMAL IAW MM CHAPTER 24-20-0. (M) 2 L 7 3 4F A3WE 1999102900716 19991029 00716 NM 1999 10 29 USAA109902 1 19991002 A 2611 824PY SMOKE DETECTOR BOEING 727 727225 1384077 NM AFT LAVATORY FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 922TS 20415 RIGHT AFT LAV SMOKE DETECTOR WON'T TEST. REPLACED SMOKE DETECTOR, CHECKS OK PER MM 26-10-0. (M) 2 L 7 3 4F A3WE 1999102900717 19991029 00717 NM 1999 10 29 TSAA9933446 1 19990929 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 4 AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1999102900718 19991029 00718 NM 1999 10 29 TSAA9933447 1 19990929 A 3350 900542 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY PACK FOR CENTER AISLE EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNE TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999102900719 19991029 00719 NM 1999 10 29 TSAA9933448 1 19991003 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999102900720 19991029 00720 NM 1999 10 29 TSAA9933449 1 19991002 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 6 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999102900721 19991029 00721 NM 1999 10 29 99ZZZM732 1 19990929 A 2750 65219458 PDU BOEING 727 727224 1384076 NM TE FLAPS BINDING A FX7A A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 19 79750 22452 FLT 201 - KMIA-SDQ - DURING CLIMB AND WHILE RETRACTING FLAPS, OUTBOARD FLAPS STAYED AT 5 DEGREES. RECYCLING BY NORMAL ME ANS DID NOT WORK. A/C AIR RETURNED BACK TO KMIA. NO FUEL WAS DUMPED, A/C ACCOMPLISHED NORMAL OVERWEIGHT LANDING. WHIL E EXTENDING FLAPS FOR LANDING OUTBOARD FLAP DID NOT GO FURTHER THAN 25 DEGREES. ON GROUND MAINTENANCE FOUND BINDING ON THE OUTBOARD FLAP POWR DRIVE UNIT AND FLAP POWER DRIVE MOTOR. PARTS WHERE REPLACED AND OPS CHECKED NORMAL PER 27-52-1. MAINTENANCE ALSO C/W OVERWEIGHT LANDING INSPECTION PER FAE FROM 100-1RR. NO DISCREPANCIES FOUND. A/C RELEASED TO SERV ICE. (M) 2 L 7 3 4F A3WE 1999102900722 19991029 00722 EU 1999 10 29 A6WA9900106 1 19990907 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 UPPER TRAILING EDGE STIFFENER INBOARD OF NR 3 FLAP TRACK IS CRACKED AT FORWARD END, LEFT WING. REPLACED LEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF NR 3 FLAP TRACK. WORK ACCOMPLISHED IAW BAE SRM STD PRACTICES. (M) 2 H 7 4 4F RT A49EU 1999102900723 19991029 00723 EU 1999 10 29 A6WA9900107 1 19990907 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF CENTER LIFT SPOILER JACK IS CRACKED AT FORWARD END. REPAIRED LEFT W ING UPPER TRAILING EDGE STIFFENER OUTBOARD OF CENTER LIFT SPOILER JACK. WORK ACCOMPLISHED IAW BAE FAX REF JM/RJO317/97 AND FAX REF DJR/RJ0630-98. (M) 2 H 7 4 4F RT A49EU 1999102900724 19991029 00724 EU 1999 10 29 A6WA9900108 1 19990907 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF RIB 8 IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING EDGE STIFFENER OUTBOARD OF RIB 8 IAW BAE FAX DJR/RJ0630-98. (M) 2 H 7 4 4F RT A49EU 1999102900725 19991029 00725 EU 1999 10 29 A6WA9900109 1 19990908 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 RIGHT WING UPPER WING STIFFENER INBOARD OF RIB 9 IS CRACKED AT FORWARD END. REPLACED UPPER WING STIFFENER INBOARD OF RI B 9 AT THIS TIME IAW FAX REF DJR/RJ0630-98. (M) 2 H 7 4 4F RT A49EU 1999102900726 19991029 00726 EU 1999 10 29 A6WA9900110 1 19990908 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 RIGHT WING UPPER WING STIFFENER OUTBOARD OF RIB 8 IS CRACKED AT FORWARD END. REPLACED RT WING UPPER WING STIFFENER AT T HIS TIME OUTBOARD OF RIB 8 IAW BAE FAX NR REF DJR/RJ0630-98. (M) 2 H 7 4 4F RT A49EU 1999102900727 19991029 00727 EU 1999 10 29 A6WA9900111 1 19990908 A 5320 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 291UE E2084 RIGHT WING SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END AND BETWEEN RIBS 9/10. REPLACED RT WING STIFFENER BETWEEN R IBS 9/10 AT THIS TIME IAW BAE FAX REF DJR/RJ0630-98. (M) 2 H 7 4 4F RT A49EU 1999102900728 19991029 00728 EU 1999 10 29 UF6A990929 1 19990923 A 2510 JD922J0142000 PANEL BAG ATP ATP EU FLT DECK DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE FLIGHT DECK OVERHEAD PANEL HAS WORN AND OVERSIZED ATTACHMENT HOLES. MAINTENANCE REPAIRED AND RESECURED PANEL. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-185. (M) 2 L 7 2 4T RT A27NM 1999102900729 19991029 00729 EU 1999 10 29 UF6A990928 1 19990923 A 5753 2F11987 SHROUD BAG ATP ATP EU RT TE FLAP CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - RIGHT FLAP TRACK SHROUD AT STATION 0 IS CRACKED. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW BAE ATP SRM 5 1-10-01. (M) 2 L 7 2 4T RT A27NM 1999102900730 19991029 00730 EU 1999 10 29 UF6A990927 1 19990923 A 5320 5D11186 INTERCOSTAL BAG ATP ATP EU BS 360-343 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL BETWEEN STATIONS 360FS AND 343FS IS CORRODED. MAINTENANCE FABRICATED INTERCOSTAL AND INSTALLED. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-13 AND 51-40-00. (M) 2 L 7 2 4T RT A27NM 1999102900731 19991029 00731 EU 1999 10 29 UF6A990926 1 19990923 A 5320 102D11186 INTERCOSTAL BAG ATP ATP EU BS 378-360 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL BETWEEN STATIONS 378FS AND 360FS IS CORRODED. MAINTENANCE REMOVED CORROSION AND REPAIRED INTERCOSTAL. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-04 FIGURE 3. (M) 2 L 7 2 4T RT A27NM 1999102900732 19991029 00732 EU 1999 10 29 UF6A990925 1 19990923 A 5210 C7682 TRACK BAG ATP ATP EU BS 324 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - AIRSTAIR SLIDING TRACK IS CORRODED. MAINTENANCE REPLACED TRACK. (M) 2 L 7 2 4T RT A27NM 1999102900733 19991029 00733 EU 1999 10 29 UF6A990924 1 19990923 A 5315 JD533J0182000 FLOORBEAM BAG ATP ATP EU BS 343 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - FLOORBEAM AT STATION 343AS IS CORRODED. MAINTENANCE REPAIRED FLOORBEAM. ALL WORK WAS DONE IAW BAE ATP SRM 53-10- 13 FIGURE 11. (M) 2 L 7 2 4T RT A27NM 1999102900734 19991029 00734 EU 1999 10 29 UF6A990921 1 19990923 A 5315 JD533J0245000 FLOORBEAM BAG ATP ATP EU BS 270 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - FLOORBEAM IN THE GALLEY AREA AT STATION 270AS IS CORRODED. MAINTENANCE FOUND AREA TO BE CRACKED. FLOORBEAM WAS R EPAIRED AND TREATED. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-04 AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999102900735 19991029 00735 EU 1999 10 29 UF6A990920 1 19990922 A 5320 BRACKET BAG ATP ATP EU E/E COMPT CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE FORWARD AVIONICS CRATE ATTACHMENT BRACKETS ARE CRACKED, TOTAL OF 4. MAINTENANCE REPAIRED ALL BRACKETS. ALL W ORK WAS DONE IAW BAE ATP SRM MM 53-10-00 FIGURE 201. (M) 2 L 7 2 4T RT A27NM 1999102900736 19991029 00736 EU 1999 10 29 UF6A990919 1 19990922 A 5320 JD256J0068000 BRACKET BAG ATP ATP EU CARGO DOORWAY DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE AFT BAGGAGE DOOR TOP ESCAPE SLIDE ATTACHMENT BRACKET IS BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRACKET. (M) 2 L 7 2 4T RT A27NM 1999102900737 19991029 00737 EU 1999 10 29 UF6A990918 1 19990922 A 7810 JD780J0003000 JET PIPE BAG ATP ATP EU NR 2 ENGINE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - RIGHT FORWARD JET PIPE ATTACHMENT BRACKET IS BROKEN. MAINTENANCE REMOVED AND REPLACED THE NR 2 FORWARD JET PIPE. (M) 2 L 7 2 4T RT A27NM 1999102900738 19991029 00738 EU 1999 10 29 UF6A990917 1 19990922 A 5315 JD533J0021000 FLOORBEAM BAG ATP ATP EU BS 343 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - FLOORBEAM AT STATION 343FS IS CORRODED AROUND LAVATORY AREA ONLY. MAINTENANCE REMOVED CORROSION AND REPAIRED FLOO RBEAM. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-03. (M) 2 L 7 2 4T RT A27NM 1999102900739 19991029 00739 EU 1999 10 29 UF6A991012 1 19991005 A 5411 FORMER BAG ATP ATP EU NR 2 NACELLE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE RIGHT MODULAR 7 HAS A CRACKED THIRD INBOARD FORMER. MAINTENANCE REPAIRED FORMER. ALL WORK WAS DONE IAW BAE A TP SRM 51-60-01 FIGURE 1. (M) 2 L 7 2 4T RT A27NM 1999102900740 19991029 00740 NM 1999 10 29 USAA990919 1 19990927 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY .300 INCH CRACK AT STATION 178, BULKHEAD LBL 7, 32 INCHES FR OM BOTTOM OF BULKHEAD. INSTALLED FILLER AND DOUBLER PER SRM 53-10-08 FIG 209. (M) 2 L 7 2 4F RT A16WE 1999102900741 19991029 00741 NM 1999 10 29 USAA990924 1 19990927 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES BS 344, LBL 49 FLOORBEAM. CORROSION LEVEL 1 . INSTALLED T-CAP PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 1999102900742 19991029 00742 NM 1999 10 29 USAA990923 1 19990927 A 5320 SPLICE BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK, 2 RIVETS WORKING AND CRACKED AT BS 907, STRINGER SPLICE 4L. INSTALLED NEW SPLICE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999102900743 19991029 00743 NM 1999 10 29 USAA990938 1 19990927 A 5320 CLIP BOEING 737 737301 1384611 NM BS 1040 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 1040, STRINGER 2R TO 3R SHEAR TIE CLIP. INSTALLED FABRICATED SHEAR TIE CLIP PER DWG 65-46369. (M) 2 L 7 2 4F RT A16WE 1999102900744 19991029 00744 NM 1999 10 29 USAA990937 1 19990927 A 5312 BULKHEAD WEB BOEING 737 737301 1384611 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURNG Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH AREA OF CORROSION LEFT FACE OF BS 1016 PRESSURE BULKH EAD CTR BL 0 STIFFENER. CORROSION LEVEL 2. INSTALLED DOUBLER PER SRM 53-80-08 AND EA 65447. (M) 2 L 7 2 4F RT A16WE 1999102900745 19991029 00745 NM 1999 10 29 USAA990936 1 19990927 A 5311 FRAME BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE BS 616 FUSELAGE FRAME INNER CHORD WL 203. INSTALLED DOUBLER AND FILLER PER EA 65336A AND TR 53-10-23. (M) 2 L 7 2 4F RT A16WE 1999102900746 19991029 00746 NM 1999 10 29 USAA990935 1 19990927 A 5311 FRAME BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE BS 616 FUSELAGE FRAME INNER CHORD WL 203 LEFT SIDE. INSTALLED DOUBLER AND FILLER PR EA 65336A AND TR 53-10-23. (M) 2 L 7 2 4F RT A16WE 1999102900747 19991029 00747 NM 1999 10 29 USAA990934 1 19990927 A 5320 BAC1505100246 T-CAP BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLE BS 344, LBL 49 FORWARD FLANGE AND LBL 31 SPLI CE T-CAP. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51 FIG 1 AND TR 53-10-13 AND EA 65489. (M) 2 L 7 2 4F RT A16WE 1999102900748 19991029 00748 NM 1999 10 29 USAA990933 1 19990927 A 5320 CLIP BOEING 737 737301 1384611 NM BS 1040 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK IN RADIUS BS 1040 BETWEEN STRINGER 6R AND STRINGER 7R SHEAR TIE CLIP. FABRICATED NEW SHEAR TIE PER SRM 51-10-02 AND DRAWING 65-46569. (M) 2 L 7 2 4F RT A16WE 1999102900749 19991029 00749 NM 1999 10 29 USAA990962 1 19990927 A 5330 SKIN BOEING 737 737301 1384611 NM BS 379 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 379, LBL 2.5 AFT SIDE OF EQUIP COOLING EXHAUST O UTLET FUSELAGE SKIN. INSTALLED SKIN DOUBLER PER TR 53-30-07 AND BOEING DWG 65C33930. (M) 2 L 7 2 4F RT A16WE 1999102900750 19991029 00750 NM 1999 10 29 USAA990961 1 19990927 A 5330 SKIN BOEING 737 737301 1384611 NM BS 327 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 327 FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER EXTERIOR SKIN. INSTALLED TRIPLER PER SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 1999102900751 19991029 00751 NM 1999 10 29 USAA990960 1 19990927 A 5320 WEB BOEING 737 737301 1384611 NM BS 709-712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKS AT FAST HOLES ALONG WEB SKIN AT BS 709-712, WL 203 , BBL 0. INSTALLED WEB REPAIR PER EA 65480 AND SB 737-57-1210. (M) 2 L 7 2 4F RT A16WE 1999102900752 19991029 00752 NM 1999 10 29 USAA990959 1 19990927 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 178, RBL 24, WL 195 INTERCOSTAL. INSTALLED NEW INT ERCOSTAL PER TR 53-10-15/SRM 51-40-03 FIG 1/SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999102900753 19991029 00753 NM 1999 10 29 USAA990966 1 19990927 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 178, BL 5 LEFT 10.5 INCH FROM BOTTOM BULKHEAD WEB ATTACH ANGLE. INSTALLED REPAIR FILLER, ANGLES, RADIUS STRAPS PER SRM 53-10-08 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999102900754 19991029 00754 NM 1999 10 29 USAA990983 1 19990927 A 5320 CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AND .500 INCH CRACK AFT CARGO AT BS 727D BL 3L AND 3R C LIP. INSTALLED REPAIR ANGLES PER SRM 51-10-02 AND BOEING DRAWING 65-65710. (M) 2 L 7 2 4F RT A16WE 1999102900755 19991029 00755 NM 1999 10 29 USAA990982 1 19990927 A 5330 SKIN BOEING 737 737301 1384611 NM BS 664 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2.75 INCH CRACKS IN UPPER PRESS DECK OF LEFT MLG W/W BS 664, LBL 30, WL 203 SKIN. INSTALLED DOUBLER PER EA 65333. (M) 2 L 7 2 4F RT A16WE 1999102900756 19991029 00756 NM 1999 10 29 USAA990981 1 19990927 A 5320 BRACKET BOEING 737 737301 1384611 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .2 5INCH CRACK INBOARD COAT CLOSET BRACKET AT BS 1016. REPLACED BRACK ET PER REPAIR DOCUMENT 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999102900757 19991029 00757 NM 1999 10 29 USAA990980 1 19990927 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, F OUND 2 CRACKS .750 LEFT AND .500 RIGHT AFT CARGO BS 727D, LBL 3 AND RBL 3 FR AME. INSTALLED DOUBLER PER EA 65325. (M) 2 L 7 2 4F RT A16WE 1999102900758 19991029 00758 NM 1999 10 29 USAA990979 1 19990927 A 5320 BEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION RUNNING ALONG TOP AND SECONDARY CAPS OF BEAM APPROX 1 INCH BEA M 986.5, LBL 04, CORROSION LEVEL 1. INSTALLED UPPER BEAM CAP REPAIR PER SRM 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999102900759 19991029 00759 NM 1999 10 29 USAA990993 1 19990927 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 3 INCHES AT STATION 986.5, 44 RBL FLOORBEAM. CORROSION LEVEL 2. INSTALLED BEAM CAP REPAIR PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999102900760 19991029 00760 NM 1999 10 29 USAA990999 1 19990927 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 24 INCH AREA OF CORROSION AT STATION 1016 FLOORBEAM AND INTERC OSTAL. CORROSION LEVEL 2. REPLACED INTERCOSTAL. INSTALLED REPAIR DOUBLERS AND STRAPS PER EA 65584. (M) 2 L 7 2 4F RT A16WE 1999102900761 19991029 00761 NM 1999 10 29 USAA991001 1 19990927 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 1138 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4.5 INCH CRACK BS 1138 TO STATION 1143 STRINGER 5R. INSTALLED REPAIR ANGLE PER EA 65627A. (M) 2 L 7 2 4F RT A16WE 1999102900762 19991029 00762 NM 1999 10 29 USAA991019 1 19990927 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 947.5-986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 20 INCH AREA OF CORROSION RT SERVICE DOOR Z-ANGLE BETWEEN STATION 947. 5 AND 986.5. CORROSION LEVEL 1. INSTALLED NEW Z-ANGLE PER SRM 53-60-51, LIMITS AND SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999102900763 19991029 00763 NM 1999 10 29 USAA991018 1 19990927 A 5320 65C158011 ANGLE BOEING 737 737301 1384611 NM BS 312-370 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH AREAS OF CORROSION AT ANCHOR NUT HOLES BS 312 T O BS 370 FORWARD ENTRY SILL Z-ANGLE. CORROSION LEVEL 2. REPAIRED AND REPLACED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999102900764 19991029 00764 NM 1999 10 29 USAA991017 1 19990927 A 5320 SPLICE BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT RIVETS BS 907, STRINGER SPLICE 4R. INSTALLED NEW SP LICE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999102900765 19991029 00765 NM 1999 10 29 USAA991016 1 19990927 A 5311 FRAME BOEING 737 737301 1384611 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CORROSION SPOT AT FRAME BS 500 RBL 25 FORWARD CARGO. CORROSION LEVEL 1. INSTALLED REPAIR DOUBLER PER EA 65486 REV A AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999102900766 19991029 00766 WP 1999 10 29 USAA991087 1 19991008 A 5330 SKIN DOUG DC9 DC981 3022081 WP MED DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND 1.5 INCH CRACK IN SKIN AT FORWARD UPPER CORNER MED DOORWAY. DOUBLERS INSTALLED PER SRM 53- 05, FIG 26. (M) 2 L 7 2 4F A6WE 1999102900767 19991029 00767 NM 1999 10 29 USAA991085 1 19991004 A 5330 SKIN BOEING 737 737301 1384611 NM BS 690-727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 353US 35627 23556 PIT - DURING RON VISIT, FOUND 4 CRACKS TOTAL .5 INCH LONG, 1 INCH LONG, 1.25 INCH LONG AND 1.5 INCH LONG IN LOWER WEB SK IN PANEL AT KEEL BEAM BETWEEN STATION 690 AND 727. EXTERNAL DOUBLER INSTALLED WITH TEMPORARY FASTENERS PER SRM 53-60-12 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999102900768 19991029 00768 NM 1999 10 29 USAA991068 1 19991002 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 25980 24842 CLT - DURING WALK AROUND VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.25 INCH CRACK LEFT HORIZ STABILIZER LOWER SKIN AT REAR SPAR STAB STATION 117.5. CUTOUT CRACK AND INSTALLED DOUBLER AND FILLER PER EA 65824. (M) 2 L 7 2 4F RT A16WE 1999102900798 19991029 00798 SO 1999 10 29 99ZZZX4107 1 19991012 A 2822 RG9080J4 PUMP ROMEC PIPER PA31 PA31350 7103110 SO FUEL SYSTEM LEAKING A TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 700TS B9064 318152157 CHECKED AD 98-18-12 AND PIPER SB 1035. FOUND SCREW BELOW TORQUE VALVE AFTER RE-TORQUE OF SCREWS. THE PUMP LEAKED. 1 L 7 2 3O A20SO 1999102900802 19991029 00802 CE 1999 10 29 99ZZZX4111 1 19990927 A 2430 A700ZC7 RELAY HARTMAN BEECH 99 99A 1154003 CE GENERATOR INOPERABLE A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 99GH U112 RIGHT GENERATOR WOULD NOT COME ON LINE. FOUND REVERSE CURRENT RELAY INOPERABLE. 1 L 7 2 3T A14CE 1999102900803 19991029 00803 CE 1999 10 29 99ZZZX4112 1 19990927 A 3340 4001273 BEACON GRIMES BEECH 99 99A 1154003 CE RUDDER INOPERABLE A TIMA K NONE L NO TEST IN INSP/MAINT 1 NM 07 99GH U112 UPPER BEACON INOPERABLE. MOTOR THAT ROTATES BULBS SHORTED OUT. RESULT OF BLOWN CIRCUIT BREAKER. 1 L 7 2 3T A14CE 1999102900804 19991029 00804 CE 1999 10 29 99ZZZX4113 1 19991001 A 2822 1D212 PUMP AIRBORNE BEECH 99 99 1154002 CE FUEL BOOST INOPERABLE A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 24BH AC43 U67 FUEL BOOST PUMP INOPERABLE. 1 L 7 2 3T A14CE 1999102900805 19991029 00805 CE 1999 10 29 99ZZZX4114 1 19991018 A 3260 327 BULB GE BEECH 200 200BEECH 1152920 CE MLG FAILED A DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 204JS BB942 LEFT GEAR DOWN AND LOCKED LAMP INOPERABLE. PILOT LANDED AT MKB WITHOUT INCIDENT. TROUBLESHOT TO BURNED OUT LAMP. REPL ACED LAMP AND RAN 10 GEAR RETRACTION TESTS. OPS CHECKED OK. 1 L 7 2 4T A24CE 1999102900811 19991029 00811 EU 1999 10 29 99ZZZX4121 1 19991026 A 6240 109013105115 TRUNNION 109813102125 AGUSTA A109 A109K2 0260502 EU TAIL ROTOR SCORED A P A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 1650 A0132 10018 DURING A PRE-FLGIHT INSPECTION, PILOT NOTED FLAPPING OF TAIL ROTOR BLADES TO BE TIGHTER THAN NORMAL AND FELT TO BE ROUGH . MAINTENANCE NOTIFIED, TAIL ROTOR ASSY REMOVED AND INSPECTED. TAIL ROTOR TRUNNION WAS FOUND SCORED WITH TWO AREAS THA T APPEARED TO BE PITS. THE FIRST AREA WAS .75 INCH LONG AND .25 INCH WIDE AT THE WIDEST POINT. THE SECOND AREA WAS .6 INCH LONG. THE AREAS ARE APPROXIMATELY .050 INCH. THE TAIL ROTOR HUB BUSHING REFLECTED THE SAME PITTING TYPE DAMAGE. ACFT TT: 2684.8 HOURS. ACFT TSO: 2640.3 HOURS. 1 G 7 2 3U RT H7EU 1999102900813 19991029 00813 NM 1999 10 29 HNAA9900139 1 19991026 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 981HA 378 FIRST 2 RED FLOOR PATH LIGHTS INOP. REMOVED AND REPLACED BULBS AND BATTERY, NO HELP. REMOVED AND REPLACED BASE ASSY. 2 H 7 2 4T RT A13NM 1999102900814 19991029 00814 EU 1999 10 29 MALA976613 1 19991023 A 3150 WEU SAAB SF340 SF340A 7850100 EU COCKPIT TRIPPED A MALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 15 112XJ 340A112 ON APPROACH, CONFIG HORN SOUNDED WHEN FLAPS WERE SELECTED TO 20 DEGREES, GEAR WAS DOWN AND LOCKED, WENT AROUND ON SECOND APPROACH NO CONFIG HORN. MAINTENANCE CYCLED POWER AFTER RE-RACKING THE WEU. PERFORMED CONFIG TEST, ALL CHECKS GOOD IA W SF340 AMM. 2 L 7 2 4T RT A52EU 1999102900815 19991029 00815 EU 1999 10 29 MALA976614 1 19991024 A 3350 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU CABIN INOP A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 EMERGENCY POWER LIGHT ON. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY IAW SAAB AMM 24-35-00. 2 L 7 2 4T RT A52EU 1999102900816 19991029 00816 EU 1999 10 29 MALA976615 1 19991022 A 3610 CLAMP BAC 146 AVRO146RJ85A 1500097 EU NR 1 ENGINE LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 517XJ E2335 LEFT ZONE HIGH TEMP, ENGINE AIR 1 FAULT AND VALVE ENGINE AIR 2 FAULT, VALVE AND PACK 1 VALVE ALL ILLUMINATED. RETURNED TO DTW TO AVOID ICING CONDITIONS. MAINTENANCE TIGHTENED PERI SEAL CLAMP IN ZONE 2. GROUND RAN A/C AT 80 PERCENT N2 FOR 15 MINUTES, NO FAULTS FOUND. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999102900817 19991029 00817 EU 1999 10 29 MALA976616 1 19991018 A 5311 FRAME SAAB SF340 SF340A 7850100 EU BS 224 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 48XJ 048 SEVEN SPOTS OF CORROSION FOUND ON THE STEP UP SILL ON FRAME STA 224, ALL OF WHICH ARE LOCATED ABOVE THE FLOOR BOARD ATTA CHMENT ANGLE. MAINTENANCE REPAIRED PER EO NR S53061 AND SAAB STATEMENT 72SDS1841. 2 L 7 2 4T RT A52EU 1999102900818 19991029 00818 EU 1999 10 29 MALA976617 1 19991014 A 5311 FRAME SAAB SF340 SF340A 7850100 EU BS 258 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 48XJ 048 DURING HEAVY CHECK INSPECTION, CORROSION FOUND ON THE FRAME FLANGE STA 258. MAINTENANCE REPAIRED PER EO NR S53063 AND S AAB STATEMENT 72SDS1838. 2 L 7 2 4T RT A52EU 1999102900819 19991029 00819 EU 1999 10 29 MALA976618 1 19991024 A 3213 201106001 STRUT BAC 146 AVRO146RJ85A 1500097 EU RT MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 524XJ E2349 DURING CLIMB, THE GEAR LEVER WOULD NOT MOVE FROM THE DOWN POSITION. THE FLIGHT DIRECTORS WERE NO LONGER DISPLAYED ON EI THER DISPLAY. RETURNED TO MSP. MAINTENANCE FOUND RT OLED SYSTEMS 1 & 2 DOLES EYES TRIPPED. RESET, CHECKED NITROGEN CH ARGE ON RT OLED, LUBED LT AND RT MLG, ADJUSTED RT MLG SQUAT SWITCHES. OPS AND RIG CHECK GOOD. TEST FLIGHT UNSATISFACTO RY. MX REPLACED RIGHT MLG SHOCK STRUT. SECURITY CHECK GOOD. 2 H 7 4 4F RT A49EU 1999102900820 19991029 00820 SO 1999 10 29 RAAA99E4048 1 19990512 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 844 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOORBEAM AND BETWEEN REPAIR ANGLE AND TOP FLANGE AT FS 844 L BL 60 AT AFT PAX DOOR SILL. REPAIRED PER SRM 53-2-4 AND 51-2-12, M-54 NR 176. 2 L 7 4 4T 4A22 1999102900821 19991029 00821 SO 1999 10 29 RAAA99E4049 1 19990525 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 863 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION AT TRANVERSE FLOORBEAM FS 863 RBL 50-58. REPAIRED AS PER SRM 53-2-4 M-54 N R 221. 2 L 7 4 4T 4A22 1999102900822 19991029 00822 SO 1999 10 29 RAAA99E4050 1 19990610 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 371 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOORBEAM UPPER AT FS 371 LBL 20-54. REPLACED FLOORBEAM AS PE R SRM 51-2-1, M-54 NR 225. 2 L 7 4 4T 4A22 1999102900823 19991029 00823 SO 1999 10 29 RAAA99E4051 1 19990610 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 352 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM UPPER FLANGE, FS 532 LBL 50-54. REPLACED FLOORBEAM A S PER SRM 51-2-1, M-54 NR 226. 2 L 7 4 4T 4A22 1999102900824 19991029 00824 SO 1999 10 29 RAAA99E4052 1 19990610 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 333 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM UPPER FLANGE FS 333 LBL 40-53. REPLACED FLOORBEAM A S PER SRM 51-2-1 M-54 NR 227. 2 L 7 4 4T 4A22 1999102900825 19991029 00825 SO 1999 10 29 RAAA99E4053 1 19990610 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 293 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM, UPPER FLANGE FS 293 LBL 40. REPLACED FLOORBEAM AS PER SRM 51-2-1 M-54 NR 228. 2 L 7 4 4T 4A22 1999102900826 19991029 00826 SO 1999 10 29 RAAA99E4054 1 19990610 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 274 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED # 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOOR BEAM, UPPER FLANGE @ FUS/STA 274 LBL 54. REPLACED FLOOR BEAM AS PER SRM 51-2-1 M-54 # 229. 2 L 7 4 4T 4A22 1999102900827 19991029 00827 SO 1999 10 29 RAAA99E4055 1 19990611 A 5320 INTERCOSTAL LKHEED 188 188C 5262604 SO BS 863-920 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON INTERCOSTAL FS 863-920 BL 0. REPLACED INTERCOSTAL AS PER SRM 51-2-12. 2 L 7 4 4T 4A22 1999102900828 19991029 00828 SO 1999 10 29 RAAA99E4056 1 19990611 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 901 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION AT TRANSVERSE FLOORBEAM TOP CAP FS 901 BL 0. REPAIRED AS PER SRM 53-2-4, M -54 NR 231. 2 L 7 4 4T 4A22 1999102900829 19991029 00829 SO 1999 10 29 RAAA99E4057 1 19990611 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 920 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOORBEAM, TOP CAP FS 920 BL 0. REPAIRED AS PER SRM 53-2-4, M-54 NR 232. 2 L 7 4 4T 4A22 1999102900830 19991029 00830 NM 1999 10 29 99FDEA00449 1 19991026 A 5320 65C26023 WEB BOEING 727 7272S2F 1384O81 NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 NR 352 - WHILE CLOSING FLOOR BDS FOUND CORROSION ON WEB BS 640, WL 208, LBL 47.5 TO 50. REPAIRED WEB PER FEDEX SRM 51-4 0-2, FIG 1. 2 L 7 3 4F A3WE 1999102900831 19991029 00831 NM 1999 10 29 99FDEA00450 1 19991026 A 5320 65583799 CREASE BEAM BOEING 727 7272S2F 1384O81 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 NR 315 - CRACK FROM FASTENER HOLE AT S-17L BS 740 (ON AFT SIDE OF FRAME). REPAIRED CRACK PER FEDEX EA NR 7-5310-47834. 2 L 7 3 4F A3WE 1999102900832 19991029 00832 NM 1999 10 29 99FDEA00451 1 19991026 A 2131 7909601 CONTROLLER BOEING 727 727233 138408A NM E&E COMP INOP A FDEA A UNSCHED LANDING G MULTIPLE FAILURE UK UNKNOWN 1 SO 25 269FE 21675 AUTO PRESSURIZATION FAILURE IN FLT. COULD NOT CONTROL CABIN ALT IN ANY PRESSURIZATION MODE. REMOVED AND REPLACED PRESS URE CONTROLLER PER MM 21-31-010-4. OPER CHECK NORM. 2 L 7 3 4F RT A3WE 1999102900833 19991029 00833 WP 1999 10 29 MWEA99730 1 19990929 A 5330 99360791 SKIN DOUG DC9 DC981 3022081 WP BS 835-1003 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 AIRCRAFT SUBSTAINED FIRE DAMAGE TO LEFT OVERWING EMERGENCY EXITS, STATION 835 TO 1003. MAINTENANCE FABRICATED AND INSTA LLED NEW/REPAIRED SECTIONS TO THE LEFT WINDOW BELT SKIN PANEL, BOTH LEFT OVERWING EMERGENCY EXIT DOOR SKIN PANELS, THE L EFT WING TRAILING EDGE SKIN PANEL AND LEFT WING FILLET PANEL. 2 L 7 2 4F A6WE 1999102900834 19991029 00834 WP 1999 10 29 MWEA99731 1 19991026 A 5330 59360312 SKIN DOUG DC9 DC981 3022081 WP BS 984 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND FUSELAGE SKIN CORRODED AT STATION 904, LONGERON 18 RIGHT. MAINTENANCE FABRICATED AND INSTALLED SKIN REPAIR DOUBLE R. 2 L 7 2 4F A6WE 1999102900835 19991029 00835 WP 1999 10 29 MWEA99732 1 19991026 A 5330 59327175 SKIN DOUG DC9 DC981 3022081 WP BS 170 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 FOUND PREVIOUS SKIN REPAIR AT STATION 970, BELOW LONGERON 3 RIGHT. MAINTENANCE FABRICATED AND INSTALLED SKIN REPAIR DOU BLER. 2 L 7 2 4F A6WE 1999102900836 19991029 00836 WP 1999 10 29 MWEA99733 1 19991026 A 5315 9922308501 FLOORBEAM DOUG DC9 DC981 3022081 WP BS 1322 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND AREAS OF LIGHT CORROSION ON LEFT LAV FLOORBEAM AT STATION 1322. MAINTENANCE FABRICATED AND INSTALLED FLOORBEAM RE PAIR. 2 L 7 2 4F A6WE 1999102900837 19991029 00837 WP 1999 10 29 MWEA99734 1 19991026 A 5347 593056675 SEAT TRACK DOUG DC9 DC981 3022081 WP BS 1117&1123 WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 SEAT TRACK LOBES ARE BLENDED OFF AT STATION 1117 AND 1123 TRACK Z. MTC FABRICATED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 1999102900838 19991029 00838 WP 1999 10 29 MWEA99735 1 19991026 A 5320 591014211 JAMB DOUG DC9 DC981 3022081 WP JAMB 370 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FORWARD CARGO COMPARTMENT FORWARD LOWER DOOR JAMB AT STATION 370 HAD A DRILL MARK. MAINTENANCE FABRICATED AND INSTALL J AMB DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999102900839 19991029 00839 WP 1999 10 29 MWEA99736 1 19991026 A 5230 59101413 SKIN DOUG DC9 DC981 3022081 WP CARGO DOOR MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 MID CARGO COMPARTMENT DOOR SKIN HAS IMPROPER PREVIOUS REPAIR. MAINTENANCE FABRICATED INSTALLED NEW REPAIR. 2 L 7 2 4F A6WE 1999102900840 19991029 00840 WP 1999 10 29 MWEA99737 1 19991026 A 5530 991196213 FORMER DOUG DC9 DC981 3022081 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 VERTICAL STABLIZER FORMER CRACKED IN TWO PLACES UNDER FORWARD WEB ATTACH ANGLES. MAINTENANCE FABRICATED AND INSTALLED F ORMER WEB REPAIR. 2 L 7 2 4F A6WE 1999102900841 19991029 00841 WP 1999 10 29 MWEA99738 1 19991026 A 5320 9912246115 TEE DOUG DC9 DC981 3022081 WP BS 1380 MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND PREVIOUS TEE REPAIR AT STATION 1380 AT LOWER INSIDE FUSELAGE LONGERON 28 RIGHT TO 30 RIGHT. MAINTENANCE FABRICATE D AND INSTALLED NEW REPAIR SECTION. 2 L 7 2 4F A6WE 1999102900842 19991029 00842 WP 1999 10 29 MWEA99739 1 19991026 A 5320 991556317 INTERCOSTAL DOUG DC9 DC981 3022081 WP BS 1380 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 FOUND PREVIOUS INTERCOSTAL REPAIR AT BOTTOM INSIDE OF FUSELAGE FROM STATION 1380 TO 1385 LONGERON 28 LEFT AND 28 RIGHT. MAINTENANCE FABRICATED AND INSTALLED NEW REPAIR SECTION. 2 L 7 2 4F A6WE 1999102900843 19991029 00843 WP 1999 10 29 MWEA99740 1 19991025 A 7711 J6908A18 INDICATOR DOUG DC9 DC932 3022066 WP COCKPIT FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 205ME 74601 AFTER TAKEOFF RAT/EPR GAUGE STARTED RISING. AT 29,000 FEET THE RAT/EPR GAUGE READ -40 DEGREES. MTC REMOVED AND REPLACE D RAT/EPR GAUGE INDICATOR. 2 L 7 2 4F A6WE 1999102900844 19991029 00844 WP 1999 10 29 MWEA99741 1 19991025 A 7711 J6908A18 INDICATOR DOUG DC9 DC932 3022066 WP COCKPIT FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 205ME 47601 AFTER TAKEOFF THE RAT/EPR GAUGE WENT TO BOTTOM OF SCALE. MTC REMOVED AND REPLACED RAT/EPR INDICATOR AND RAT PROBE. 2 L 7 2 4F A6WE 1999102900845 19991029 00845 WP 1999 10 29 MWEA99742 1 19991025 A 2560 100502121 COVER DOUG DC9 DC981 3022081 WP GALLEY DOORWAY DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 803ME 48029 AFT GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE COVER DETACHED ON BOTTOM OF SLIDE. MAINTENANCE RESECURED SLIDE COVER . 2 L 7 2 4F A6WE 1999102900846 19991029 00846 WP 1999 10 29 MWEA99743 1 19991027 A 3350 80130724 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 212ME 47701 AFT BATTERY POWER SUPPLY FAILED OPERATIONAL CHECK. MTC REMOVED AND REPLACED AFT EMERGENCY BATTERY. 2 L 7 2 4F A6WE 1999102900847 19991029 00847 1999 10 29 DLM90992290 4 19991018 A 3197 V2528D5 WIRE DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE NR 2 ENGINE SHORTED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 903DA 53383 PASSING 28,000 STATUS LT AND RT ENG SYSTEM FAIL MESSAGE CAME ON. ENG WENT INTO N1 DEFAULT MODE. EPR AND EPR LIMIT INDI CATIONS WENT AWAY AND AUTO THROTTLES DISENGAGED. FOUND WIRE 4 INCH AFT OF DISCONNECT P1-8066 GOING TO P1-8078 T2 CHANN EL A SHORTED TO ENG CASE. REPAIRED DAMAGED WIRE, RAN ENGINE AND OPN NORMAL. 2 L 7 2 4F 4 F RT A6WE A40NE 1999102900848 19991029 00848 NM 1999 10 29 DL72S992291 1 19991017 A 2751 TRANSMITTER 9660022001 BOEING 727 727232 1384082 NM RT TE FLAP FAILED A DALA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 27 495DA 9072 21075 OUTBOARD FLAPS LOCKED OUT AT 2 DEGREES ON FLAP EXTENSION INBOUND TO ORF ON FLT 1220/17. DIVERTED TO RIC. MTC FOUND THE RT POSITION TRANSMITTER TO BE AT FAULT. REPLACED THE RT OUTBOARD POSITION TRANSMITTER, OPS CHECK NORM. 2 L 7 3 4F A3WE 1999102900849 19991029 00849 NM 1999 10 29 DL73K992292 1 19991018 A 2780 RETRACT MECH 6546422305 BOEING 737 737247 138448D NM NR 2 LE SLAT MALFUNCTIONED A DALA K NONE P NO WARNING INDICATION AP APPROACH 1 SO 27 242WA 23516 DURING FLIGHT, NR 2 SLAT WOULD NOT RETRACT FULLY. COCKPIT INDICATIONS SHOWED NR 2 RETRACTED. DURING EXTENSION FROM 1-5 DEGRESS IT DID NOT EXTEND, BUT FROM 5-10 DEGREES IT SLAMMED TO FULL EXTEND AND THEN RETRACTED TO EXT WITH ASSOCIATED L/ E INTRANSIT LIGHT AND OVERHEAD AMBER IND. ALL OTHER FLAPS/SLATS OPERATED NORMALLY. FOUND I/B PROGRAM TRACK ATTACH POIN T ON SLAT BROKEN. REPLACED SLAT, ACTUATOR, CLOSEOUT DOOR, 2 HYDRAULIC LINES AND MADE SHEET METAL REPAIR TO INBOARD SLAT TRACK CUTOUT PER M/M. 2 L 7 2 4F A16WE 1999102900850 19991029 00850 NM 1999 10 29 DL76L992294 1 19991019 A 2597 WIRE BOEING 767 767332 1382001 NM ROW 3D-4D SHORTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 192DN 28449 LAX - SEAT 4D ARCS AND SPARKS WHEN FOOT REST IS EXTENDED. DISCONNECTED SEAT TO SEAT ELECTRICAL HARNESS BETWEEN SEAT 4D AND 3D. DUE TO ACTUATOR EXTENSION SHAFT CUTTING INTO WIRE HARNESS NEED NEW SEAT TO SEAT HARNESS. FWD TO MCO/PLAC MEL25-20-01. 2 L 7 2 4F RT A1NM 1999102900851 19991029 00851 NM 1999 10 29 DL777992296 1 19991019 A 2530 1105011 COFFEE MAKER BOEING 777 777232 1385232 NM CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 860DA 29951 COFFEEMAKERS INOP AFT CO-PILOTS SIDE, COFFEEMAKERS 108, 109, 110. ELECTRICAL SMELL NOTICED IN AREA AND CIRCUIT BREAKERS PULLED. REPLACED COFFEEMAKERS. 2 L 7 2 4F RT T00001SE 1999102900852 19991029 00852 NM 1999 10 29 DL73K992297 1 19991019 A 5330 SKIN BOEING 737 737232 1384475 NM BS 767 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309DL 23081 A 2.25 INCH CRACK IN FUSE SKIN STA 767 ABOVE STR 19 RT. INSTALLED DOUBLER PER SRM 53-30-3 F1. 2 L 7 2 4F RT A16WE 1999102900853 19991029 00853 NM 1999 10 29 DL73K992298 1 19991019 A 5330 SKIN BOEING 737 737232 1384475 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309DL 23081 A 2.25 INCH CRACK IN FUSE SKIN STA 727B STR 18 RT. INSTALLED DOUBLER PER SRM 53-30-3 F1. 2 L 7 2 4F RT A16WE 1999102900854 19991029 00854 NM 1999 10 29 DL73K992299 1 19991019 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309DL 23081 A .125 INCH CRACK AT FUSE SKIN AT L-1 WINDOW UPPER O/B CORNER. INSTALLED DOUBLER PER SRM 53-30-3 REPAIR II FIG 11. 2 L 7 2 4F RT A16WE 1999102900855 19991029 00855 NM 1999 10 29 DL73K992301 1 19991019 A 3350 20131A BATTERY BOEING 737 737232 1384475 NM ROW 17-20 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 326DL 23098 ON L/O, FOUND AFT SECTION EMERGENCY LIGHTS INOP ROWS 17 TO 20 INCLUDING RT SIDE GALLEY. FOUND BATTERY AT MODULE M9222 I NOP. REPLACED BATTERY, EMERGENCY LIGHTS OPN CKS NORMAL. 2 L 7 2 4F RT A16WE 1999102900856 19991029 00856 NM 1999 10 29 DL72S992302 1 19991015 A 5311 FRAME BOEING 727 727232 1384082 NM BS 378 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 REPAIRED .5 INCH CRACK AT BOTTOM OF STA 378 (R1 DOOR) FRAME PER SRM 53-10-4 FIG 24. 2 L 7 3 4F A3WE 1999102900857 19991029 00857 NM 1999 10 29 DLM88992303 1 19991018 A 3030 HEATER 1058461 DOUG MD88 MD88 3023688 NM STATIC PORT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 961DL 6333 49980 FLIGHT ATTENDANTS REPORTED BURNING SMELL NEAR FIRST CLASS/ COACH DIVIDER. A/C ON APU POWER/AIR FOR 3-5 MINUTES. TURNE D OFF STATIC PORT HEATERS, ODOR DIMINISHED. DEACTIVATED STATIC HEAT REMOVING 4 CANNON PLUGS AT HEATERS. FWD TO MCO AND PLACARD. SUBSEQUENTLY REPLACED THE CAPTAINS PRIMARY STATIC PORT HEATER ON LOG NR 083545003. 2 L 7 2 4F RT A6WE 1999102900858 19991029 00858 NM 1999 10 29 DL72S992304 1 19991012 A 5311 FRAME BOEING 727 727232 1384082 NM BS 772.45 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FOUND DURING MV2 CORROSION VISIT NRC 202, CORROSION 3 PLACES AT BODY FAIRING SUPPORT FRAME I/B SIDE AND FWD SIDE SURROUN DING RT SECONDARY HEAT EXCHANGER. REPAIRED PER M/M 53-30-1 FIG 804, PG 807-808. 2 L 7 3 4F A3WE 1999102900859 19991029 00859 NM 1999 10 29 DL72S992305 1 19991015 A 5311 FRAME BOEING 727 727232 1384082 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FOUND DURING MV2 CORROSION VISIT NRC 215, .5 INCH CRACK IN FRAME STA 378 WL 208.9 - R1 DOOR CUT OUT FWD FRAME. FOUND WH ILE WORKING NRC 29. REPAIRED PER SRM 53-10-4 FIG 24. 2 L 7 3 4F A3WE 1999102900860 19991029 00860 NM 1999 10 29 DL72S992306 1 19991018 A 5754 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 AT HMV FOUND NR 5 SLAT ACT MOUNT O/B RIB CRACKED. REF N/R 1140 - RIB NR 11 FROM O/B FWD. STOP DRILLED CRACK AND FABBED REPAIR PER MM 57-54-0 PG 805 AND INSTALLED PER SAME. 2 L 7 3 4F A3WE 1999102900861 19991029 00861 NM 1999 10 29 DLM88992309 1 19991020 A 3244 446K822 TIRE DOUG MD88 MD88 3023688 NM NR 4 FAILED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 935DL 49722 ON T/O PVD NR 4 MLG TIRE TREAD SEPARATED AND TREAD SUBSEQUENTLY INGESTED INTO RIGHT ENGINE. REPLACED WHEEL ASSY AND ENGINE. 2 L 7 2 4F RT A6WE 1999102900862 19991029 00862 NM 1999 10 29 DL73S992310 1 19991020 A 5330 655298878 SKIN BOEING 737 737232 1384475 NM BS 965 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 A .8 LONG CRACK WAS FOUND IN THE SKIN AND BONDED DOUBLER AT THE LOWER FORWARD CORNER OF THE L2 DOOR CUTOUT. THE CRA CK WAS ROUTED OUT OF THE SKIN AND BONDED DOUBLER (BEAR STRAP WAS UNDAMAGED) AND REPAIRED WITH AN EXTERNAL ALUMINUM DOU BLER AND TRIPLER PER B737 SRM 53-30-3, FIG 24 AND ER/A 368546-14, REV A. 2 L 7 2 4F RT A16WE 1999102900863 19991029 00863 NM 1999 10 29 DL767992311 1 19990928 A 5755 113T51021A SKIN BOEING 767 767232 1385132 NM NR 4 SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 LT WING NR 4 SPOILER, 12 IN X 17 IN UPPER SKIN TO CORE DELAMINATION LOCATED IN CENTER OF PANEL. AUTHORIZED WET LAYUP, 1 80 DEG F CURE REPAIR. 2 L 7 2 4F RT A1NM 1999102900864 19991029 00864 NM 1999 10 29 DL73S992312 1 19991020 A 5330 65458001206 SKIN BOEING 737 737232 1384475 NM BS 330 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A .7 TYPICAL CRACK THROUGH THE SKIN AND BONDED DOUBLER. THE B EAR STRAP WAS UNDAMAGED. THE CRACK WAS ROUTED OUT OF THE SKIN AND DOUBLER AND REPAIRED WITH AN EXTERNAL ALUMINUM D OULBER AND TRIPLER PER B737 SRM 53-30-3, FIG 16 AND ER/A 368547-14, REV A. 2 L 7 2 4F RT A16WE 1999102900865 19991029 00865 NM 1999 10 29 DL72L992313 1 19990813 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 DURING SHOP INSP, THE LOWER AFT SPAR ANGLE WAS FOUND CRACKED 19 FROM I/B END. A SECTION OF THE CAP WAS REPLACED AND A D OUBLER INSTALLED PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999102900866 19991029 00866 NM 1999 10 29 DL72L992314 1 19990813 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 DURING SHOP INSP, THE LOWER AFT SPAR ANGLE/CAP WAS FOUND CRACKED 33 AND 37 FROM THE I/B END. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1999102900867 19991029 00867 NM 1999 10 29 DL72L992315 1 19990813 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 DURING SHOP INSP, THE LOWER AFT SPAR CAP/ANGLE WAS FOUND CRACKED 53 FROM THE I/B END. THE ANGLE WAS REPAIRED BY REPL ACING A SECTION OF THE ANGLE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999102900868 19991029 00868 NM 1999 10 29 DL72L992316 1 19990827 A 5753 652163262 SKIN BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 DURING SHOP VISIT, THE AFT LOWER COVE SKIN WAS FOUND CRACKED 52 FROM I/B END OF THE FLAP. THE SKIN WAS REPAIRED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 809. 2 L 7 3 4F A3WE 1999102900869 19991029 00869 NM 1999 10 29 DL72S992317 1 19991021 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND AT F-2 LTR CK, AFT ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE BELOW A/C DATA PLATE. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999102900870 19991029 00870 NM 1999 10 29 DL757992318 1 19991021 A 3610 DUCT 212N30453 BOEING 757 757232 1384965 NM TAIL COMP RUPTURED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 612DL 22819 APU BLEED DUCT LOCATED IN THE AFT ACCESSORY COMPARTMENT RUPTURED ON TAXI OUT. DUCT MATERIAL BROKE ONE OF THE ALTERNATE STAB TRIM CONTROL CABLE PULLEYS CAUSING THE ALTERNATE STAB TRIM CONTROL CABLE TO BIND. REPLACED DUCT, REPAIRED STAB CON TROL SYSTEM. 2 L 7 2 4F RT A2NM 1999102900871 19991029 00871 NM 1999 10 29 DL72S992320 1 19991021 A 5320 WEB BOEING 727 727232 1384082 NM BS 1235 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 TPA LTR CHECK F-2, LT TORQUE BOX VERT WEB CRACKED 1 AT STA 1235. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999102900872 19991029 00872 NM 1999 10 29 DL72S992321 1 19991021 A 5330 SKIN BOEING 727 727232 1384082 NM BS 231 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 TWO .25 INCH CRACKS IN F/S 231 STR 21R. INSTALLED DOUBLER PER SRM 53-30-3 F 26. 2 L 7 3 4F A3WE 1999102900873 19991029 00873 NM 1999 10 29 DL72S992322 1 19991021 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 NR 1 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER M/M 57-20-21 PG 812. 2 L 7 3 4F A3WE 1999102900874 19991029 00874 NM 1999 10 29 DL72S992323 1 19991021 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 STRINGER 18A CRACKED AT LWR AFT BOLT STA 940. REPAIRED PER MM 53-12-0 PG 816. 2 L 7 3 4F A3WE 1999102900875 19991029 00875 NM 1999 10 29 DLM11992324 1 19991022 A 3246 WHEEL DOUG MD11 MD11 3023602 NM CTR MLG DAMAGED A DALA O OTHER O OTHER LD LANDING 1 SO 27 803DE 48474 DURING LANDING ROLL ACFT ENTERED OVERRUN AREA, REMAINED ON PAVEMENT. REPLACED TWO CENTER MAIN WHEEL ASSYS, NO OTHER DAM AGE. 2 L 7 3 4F RT A22WE 1999102900876 19991029 00876 NM 1999 10 29 DL76S992325 1 19991021 A 5330 141T32316 SKIN BOEING 767 767332 1382001 NM BS 370 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 SKIN AT STA 370 AND STR 34R HAS A GASH MEASURING APPROX 6 X 3. ALSO, STRINGER 34R DAMAGED AT THIS LOCATION. BOTH SKIN AND STRINGER ARE BEING REPAIRED ER/A 265466-14 REV B. 2 L 7 2 4F RT A1NM 1999102900877 19991029 00877 NM 1999 10 29 DL72S992326 1 19991022 A 2782 FITTING BOEING 727 727232 1384082 NM NR 4 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 NR 4 L/E SLAT I/B ACTUATOR ATTACH FITTING WAS CRACKED 3 EA LOCATION THROUGH AN EXISTING REPAIR. REPAIRED DOUBLER PER M/ M 57-54-0 FIG 804. REMOVED CRACKED PLATE, REPLACED CLIP PER 51-00. OK TO INSTALL. INSTALLED REPAIR PER M/M 57-54-0 FI G 804. 2 L 7 3 4F A3WE 1999102900878 19991029 00878 WP 1999 10 29 DLL14992327 1 19991021 A 2910 LINE 000AE5616T0 LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 741DA 193C1245 1.5 HRS AFTER T/O, C-SYS HYD LO QTY LIGHT SAME ON AND QTY WENT MOMENTARILY TO 1/4 THEN BACK TO 3/8. FOLLOWED POM AND W ITH NO PUMPS ON / NO SYS PRESS / QTY SLOWLY DECREASED OVER NEXT 3 HRS TO 1/16 LEVEL AND REMAINED THERE. EDP LOW PRESS LIGHT WAS ON BRIEFLY UNTIL EDP TURNED OFF. FOUND C-SYS PRESS LINE LEAKING. REPLACED SAME. LEAK CHECK OK AND SERVICED HYD SYS. 2 L 7 3 4F A23WE 1999102900879 19991029 00879 NM 1999 10 29 DL72S992328 1 19991022 A 2750 SWITCH BOEING 727 727232 1384082 NM TE FLAPS FAILED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 495DA 21075 RUDDER LIMITER WITH FLAPS EXT. REPLACED FLAP UP LIMIT SWITCH. 2 L 7 3 4F A3WE 1999102900880 19991029 00880 NM 1999 10 29 DL73K992329 1 19991022 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM ROW 1-16 INOP A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 311DL 23083 AT DEPARTURE TIME, EMERGENCY LIGHTS ROWS 1 THRU 16 WOULD NOT TURN OFF. REPLACED POWER SUPPLY AND BATTERY LIGHTS OPERAT ION NORMAL. 2 L 7 2 4F RT A16WE 1999102900881 19991029 00881 NM 1999 10 29 DL72S992330 1 19990715 A 5753 652163261 ANGLE BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 DURING SHOP VISIT, THE AFT LOWER SPAR/ANGLE WAS FOUND CRACKED 19 INCHES FROM THE I/B END. A REPLACEMENT SECTION OF ANGL E WAS INSTALLED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999102900882 19991029 00882 NM 1999 10 29 DL72S992331 1 19990715 A 5753 652163261 ANGLE BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 DURING SHOP VISIT, THE AFT LOWER SPAR/CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. A REPLACEMENT SECTIO N OF ANGLE WAS INSTALLED ALONG WITH A DOUBLER PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999102900883 19991029 00883 NM 1999 10 29 DL72S992332 1 19990715 A 5753 652163261 ANGLE BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 DURING SHOP INSPECTION THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 56 INCHES FROM I/B END OF FLAP. A SECTION OF ANGLE WA S REPLACED AND A DOUBLER INSTALLED PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999102900884 19991029 00884 NM 1999 10 29 DL76L992333 1 19991022 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM ROW 32 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 198DN 28455 ON PRE-DEPARTURE CHECK, FOUND E-PATH LIGHTS FROM ROW 32 AFT INOP. REPLACED BATTERY PACK, SYSTEM CHECKS. 2 L 7 2 4F RT A1NM 1999102900885 19991029 00885 NE 1999 10 29 DL76L992334 2 19991022 A 7321 FUEL CONTROL 7911004089 BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 187DN 40000564 27582 DURING CLIMB FORM 330 TO 350 RT ENG DID NOT ACCELERATE. RT THROTTLE WAS MOVED TO FIREWALL WITH NO RESULTS. AS THROTTLE WAS BROUGHT BACK IN ALIGNMENT THE ENG STARTED WORKING NORMAL. REPLACED RIGHT ENGINE FUEL CONTROL, SYSTEM OPS CHECK NOR MAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999102900886 19991029 00886 NM 1999 10 29 DL757992335 1 19991023 A 2760 WARNING 285T025919 BOEING 757 757232 1384965 NM SPOILER SYS ACTIVATED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 647DL D00205 24218 FIRST FLIGHT OF THE DAY DELAY AIRCRAFT 647, ABORTED T/O TWICE FOR SPOILER WARNING. AFTER FIRST T/O ABORT, SPOILERS WERE VISUALLY CHECKED AND RELATED COMPONENTS CHECKED, SHOWED NO FAULTS. LOG ENTRY MADE, AIRCRAFT DEPARTED GATE. ON SECOND T/O ABORT, SPOILER WARNING AND T/O CONFIG CAME ON. AIRCRAFT RETURNED TO GATE. FOUND T/O CONFIG WARNING CARD M620 BAD. REPLACED CARD, ALL SYSTEMS CHECKED NORMAL. AIRCRAFT DEPARTED PDX OK. FIRST ABORT SPEED 80 KNOTS, SECOND ABORT SPEED 4 0 KNOTS. NO DANGER REPORTED BY CREW DURING BOTH T/O ATTEMPTS. NO DANGER TO PASSENGERS OR CREW. 2 L 7 2 4F RT A2NM 1999102900887 19991029 00887 NM 1999 10 29 DL76G992337 1 19991023 A 2530 CHILLER BOEING 767 7673P6 1385105 NM MID GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 155DL 25269 MID GALLEY AFT CHILLER FAULT LIGHT ILLUMINATED. SHORTLY THERE AFTER NOXIOUS PLASTIC SMELL CAME FROM VENT AREA BETWEEN THE OVEN AND THE FREEZER CHILLER. OVEN C/B PULLED, BOTH ITEMS PUT ON MCO 25-20-01. 2 L 7 2 4F RT A1NM 1999102900888 19991029 00888 NM 1999 10 29 DL76G992338 1 19991023 A 2120 AIR DIST BOEING 767 767324 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 394DL 27394 ELECT ODOR IN FWD CAB AND AFTER CAPTS SIG GEN WENT OUT, OUTSIDE ELECTRICAL ACTIVITY WAS HIGH. AFTER SHUTTING OFF UTIL B USSES THE ODOR WENT AWAY IMMEDIATELY. LATER INFLIGHT ALL GALLEY C/BS PULLED AND RT UTILITY BUS TURNED ON WITH RECIRC FA NS OFF. NO FUMES REST OF FLT. COULD NOT DUPLICATE ELECT ODOR. BOTH UTIL BUSSES RESET ON EACH, RECIRC FAN OPERATED IND IVIDUALLY. ALL GALLEY C/BS RESET AND GALLEY EQUIP OPERATED FOR 1 HR. ELEC EQUIP BAY INSPECTED, C/BS CHECKED. ALL NORM AL, NO PREVIOUS HISTORY. PER ATL OCC, A/C TO BE MONITORED. 2 L 7 2 4F RT A1NM 1999102900889 19991029 00889 NE 1999 10 29 DL76L992339 2 19991024 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE BIRD STRIKE A DALA A UNSCHED LANDING C D F.O.D. INFLIGHT SEPARATION CL CLIMB 1 SO 27 194DN 32069 28451 724416 ON TAKEOFF HAD BIRD STRIKE LT ENGINE. ENGINE VIBS WENT AS HIGH AS 4.0. SUSPECTED DAMAGE, DIVERTED FLT TO FRA FOR INSP AND REPAIRS. LT ENGINE WAS NOT SHUTDOWN, A/C LANDED SAFELY. FOUND 3 FAN BLADES DAMAGED, FOUND BIRD STRIKE ON RT ENGINE . REQUIRED REPAIRS AND BORO INSPECTION. BORO INSPECTION OF RT ENG WAS GOOD, NO DAMAGE FOUND. (S/N 727718). 2 L 7 2 4F 4 F RT A1NM E24NE 1999102900890 19991029 00890 NM 1999 10 29 DL72W992340 1 19991024 A 3350 1001141 LIGHT BOEING 727 727247 138408F NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 22110 AFT STAIR EMERGENCY OVERHEAD LIGHT INOP. REPLACED LIGHT PACK ASSY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999102900891 19991029 00891 NM 1999 10 29 DL76S992342 1 19991006 A 5313 146T300323 STRINGER BOEING 767 767332 1382001 NM BS 1540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 CORROSION WAS FOUND IN STRINGER 39L AT STATION 1540 AND WAS BEYOND ALLOWABLE LIMITS. A REPLACEMENT SECTION OF STRINGER WAS SPLICED IN PER SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999102900892 19991029 00892 NM 1999 10 29 DL76S992343 1 19991006 A 5313 146T300315 STRINGER BOEING 767 767332 1382001 NM BS 1540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 STRINGER 38L AT STATION 1540 WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS. A REPLACEMENT SECTION OF STRINGER WAS INSTALLE D PER SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999102900893 19991029 00893 NM 1999 10 29 DLM11992344 1 19991024 A 2597 PS46010102 WIRE HARNESS DOUG MD11 MD11 3023602 NM ROW 3B FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 815DE 48624 SEAT HARNESS AT 3B CHAFED AND ARCING WHEN RECLINING SEAT TO CHANGE ACTUATOR. C/B DID NOT POP. REPLACED HARNESS. 2 L 7 3 4F RT A22WE 1999102900894 19991029 00894 NM 1999 10 29 DL76S992345 1 19991006 A 5320 140T2102656 SHEAR TIE BOEING 767 767332 1382001 NM BS 1562 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 SKIN TO FRAME ATTACH CLIP WAS FOUND CORRODED AT STA 1562 BETWEEN STRINGERS 38L AND 38R ON FWD SIDE OF STA 1562 FRAME. T HE (P/N 140T2102-656) ATTACH CLIP WAS REPLACED PER SRM 51-10-00 AND DWG 146T1223. STRINGERS 39L AND 39R NEEDED TO BE RE MOVED FOR ACCESS BETWEEN STA 1540 AND STA 1562. 2 L 7 2 4F RT A1NM 1999102900895 19991029 00895 NM 1999 10 29 DL76S992346 1 19991006 A 5313 146T300324 STRINGER BOEING 767 767332 1382001 NM BS 1540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 STRINGER 39R WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS AT STA 1540. A REPLACEMENT SECTION OF STRINGER WAS INSTALLED PE R SRM 53-00-03-2-202. 2 L 7 2 4F RT A1NM 1999102900896 19991029 00896 NM 1999 10 29 DL76S992347 1 19991006 A 5320 140T210223 CLIP BOEING 767 767332 1382001 NM BS 1562 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 FUSELAGE FRAME TO SKIN CLIP WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS AT STA 1562 AND BL 0 BETWEEN STRINGERS 38L AND 38 R. THE (P/N 140T2102-23) SKIN CLIP WAS REPLACED PER SRM 51-10-00 AND DWG 146T1223. 2 L 7 2 4F RT A1NM 1999102900897 19991029 00897 NM 1999 10 29 DL76S992348 1 19991015 A 5320 146T122330 CHORD BOEING 767 767332 1382001 NM BS 1562 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 FUSELAGE STATION 1562 FRAME CHORD WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS BETWEEN STRINGERS 38L AND 38R. THE (P/N 14 6T1223-30) CHORD WAS REPLACED PER DWG 146T1223. 2 L 7 2 4F RT A1NM 1999102900898 19991029 00898 NM 1999 10 29 DL76S992349 1 19991012 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 STRINGER 35L SPLICE WAS FOUND CORRODED AT STA 434, NO DAMAGE TO THE STRINGER WAS FOUND. THE (P/N 140T0115-16) SPLICE WA S REPLACED PER DWG 145T3210. 2 L 7 2 4F RT A1NM 1999102900899 19991029 00899 NM 1999 10 29 DL76S992350 1 19991012 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 STRINGER 38L SPLICE WAS FOUND CORRODED AT STATION 434, NO DAMAGE TO STRINGER WAS FOUND. THE (P/N 140T0115-16) SPLICE WA S REPLACED PER DWG 143T3210. 2 L 7 2 4F RT A1NM 1999102900900 19991029 00900 NM 1999 10 29 DL76S992351 1 19991012 A 5320 140T011525 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 STRINGER 36R SPLICE WAS FOUND CORRODED AT STATION 434, NO DAMAGE TO THE STRINGER WAS FOUND. THE (P/N 140T0115-25) SPLIC E WAS REPLACED PER DWG 143T3210. 2 L 7 2 4F RT A1NM 1999102900901 19991029 00901 NM 1999 10 29 DL76S992352 1 19991012 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 STRINGER 36L SPLICE WAS FOUND CORRODED AT STATION 434, NO DAMAGE TO STRINGER WAS FOUND. THE (P/N 140T0115-16) SPLICE WA S REPLACED PER DWG 145T3210. 2 L 7 2 4F RT A1NM 1999102900902 19991029 00902 NM 1999 10 29 DL76S992353 1 19991013 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 STRINGER 38R SPLICE WAS FOUND CORRODED AT STATION 434, NO DAMAGE TO THE STRINGER WAS FOUND. THE (P/N 140T0115-16) SPLIC E WAS REPLACED PER DWG 143T3210. 2 L 7 2 4F RT A1NM 1999102900903 19991029 00903 NE 1999 10 29 DL75A992354 2 19991025 A 7200 ENGINE BOEING 757 757212 NM PWA 2037 PW2037 NE NR 2 SURGED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 757AT 28579 23127 716339 DURING CLIMBOUT, RIGHT ENGINE SURGED. FLIGHT CREW ELECTED TO RETARD ENGINE TO IDLE AND RETURN TO LIMA. FERRIED A/C TO ATL FOR ENGINE CHANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999102900904 19991029 00904 NM 1999 10 29 DL72W992355 1 19990831 A 2497 BMS1331 INSULATION BOEING 727 727247 138408F NM NR 3 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING S ERVICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999102900905 19991029 00905 NM 1999 10 29 DL72L992356 1 19990920 A 2497 BMS1331 INSULATION BOEING 727 727232 1384082 NM NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FOR SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING S ERVICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999102900906 19991029 00906 NM 1999 10 29 DL72L992357 1 19990920 A 2497 BMS1358 INSULATION BOEING 727 727232 1384082 NM NR 3 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION ON ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING S ERVICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999102900907 19991029 00907 NM 1999 10 29 DL72W992358 1 19991007 A 2497 BMS1331 INSULATION BOEING 727 727247 138408F NM NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 ON HUSH KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING S ERVICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999102900908 19991029 00908 NM 1999 10 29 DL72W992359 1 19991007 A 2497 BMS1331 INSULATION BOEING 727 727247 138408F NM NR 3 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 ON HUSH KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING S ERVICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999102900909 19991029 00909 NM 1999 10 29 DL72S992360 1 19991025 A 5532 65174633 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 THE LT SKIN OF THE VERTICAL STABLIZER WAS DAMAGED RESULTING IN A 1.2 X 1.2 CUTOUT BETWEEN STRINGERS 7 AND 8 AT FIN STATI ON 204. REPAIRED PER ERA 333721-14 AT HMV. 2 L 7 3 4F A3WE 1999102900910 19991029 00910 NM 1999 10 29 DL72S992361 1 19991025 A 5330 6554580 SKIN BOEING 727 727232 1384082 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 THE FUSELAGE SKIN WAS GOUGED AT FS 990 AT STRINGER 24R. REPAIRED PER ERA 333703-14 AT HMV. 2 L 7 3 4F A3WE 1999102900911 19991029 00911 NM 1999 10 29 DL733992362 1 19991025 A 5312 65163007 BULKHEAD WEB BOEING 737 73735B NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 221DL 23970 THE FS 178 BULKHEAD WEB WAS FOUND TO HAVE 3 CRACKS. TWO CRACKS WERE AT APPROXIMATELY LBL 4.7 AND WL 205, THE THIRD WAS AT RBL 4.7 AND WL 205. THE DAMAGE WAS REPAIRED BY ERA 333717-14 ATMV. 2 L 7 2 4F RT A16WE 1999102900912 19991029 00912 NM 1999 10 29 DLM88992363 1 19991025 A 3397 WIRE DOUG MD88 MD88 3023688 NM 1R DOOR BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 937DL 49810 RED EMERGENCY TRACK LIGHTING AT 1R INOP. FOUND WIRES TO LIGHT ASSY BROKEN. REPAIRED SAME, CHECKS GOOD. 2 L 7 2 4F RT A6WE 1999102900913 19991029 00913 NM 1999 10 29 DL72S992364 1 19991024 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 21020 ON L/O, FOUND LT OVERWING EMER EXIT LIGHT INOP. REPLACED BATTERY PACK, CHECKS GOOD. 2 L 7 3 4F A3WE 1999102900914 19991029 00914 NM 1999 10 29 DL72S992365 1 19991024 A 3350 90054200835 BATTERY PACK BOEING 727 727232 1384082 NM L1 DOORWAY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 21020 ON L/O, FOUND L1 EMER EXIT LIGHT INOP. REPLACED BATTERY PACK, RACK AND REFLECTOR. 2 L 7 3 4F A3WE 1999102900915 19991029 00915 NM 1999 10 29 DL72S992366 1 19991025 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 TPA LTR CHK F-2, 1 VISIBLE CRACK O/B ATTACH BRACKET NR 1 SLAT ACTUATOR. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999102900916 19991029 00916 NM 1999 10 29 DL72S992367 1 19991025 A 2782 ANGLE BOEING 727 727232 1384082 NM NR 8 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 NR 8 SLAT ACTUATOR O/B ATTACH ANGLE WAS CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999102900917 19991029 00917 NM 1999 10 29 DLM88992368 1 19991025 A 2130 VALVE DOUG MD88 MD88 3023688 NM FUSELAGE CONTAMINATED A DALA I CABIN DEPRESSURIZATION P NO WARNING INDICATION DE DESCENT 1 SO 27 911DE 49967 CABIN COMPLETELY DEPRESSURIZES ON DESCENT THROUGH 4000 FT. NO LIGHTS ASSOCIATED. AUTO 1 SELECTED WITH CORRECT ALTIMET ER AND FIELD ELEVATION. FOUND DEBRIS IN PRESSURE RELIEF VALVE. CLEARED SAME. 2 L 7 2 4F RT A6WE 1999102900918 19991029 00918 NM 1999 10 29 DLM88992369 1 19991025 A 3350 POWER SUPPLY 8039001 DOUG MD88 MD88 3023688 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DL 49535 FOUND FWD OVERWING E-PATH EXIT LIGHTS INOP AND BOTH LEFT AND RIGHT EXT OVERWING LIGHTS INOP. REPLACED POWER SUPPLY B5-1 04 AND OVERWING POWER SUPPLY AT STATION 1050L, OPS CHECK NORMAL PER MM. 2 L 7 2 4F RT A6WE 1999102900919 19991029 00919 NM 1999 10 29 DL76L992372 1 19991026 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM 1L DOORWAY INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 185DN 27961 EMERGENCY EXIT LIGHT AT DOOR 1L WOULD NOT TURN OFF WITH ALL SWITCHES OFF. REPLACED POWER SUPPLY AND BATTERY PACK. 2 L 7 2 4F RT A1NM 1999102900920 19991029 00920 NM 1999 10 29 DL76L992373 1 19991026 A 3350 BATTERY PACK BPS73 BOEING 767 767332 1382001 NM 1L DOORWAY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 185DN 18165 27961 EMERGENCY LIGHT AT 1L STAYS ILLUMINATED. REPLACED BATTERY PACK AND POWER SUPPLY, CHECKS OK. 2 L 7 2 4F RT A1NM 1999102900921 19991029 00921 NM 1999 10 29 DL72L992374 1 19991026 A 3350 BATTERY PACK RPS1 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 0672 21306 F/C SEAT MOUNTED EMERGENCY LIGHTS WON'T TEST. REPLACED RACK AND BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 1999102900922 19991029 00922 NM 1999 10 29 VNAA9910017 1 19991026 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7LK DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 425JS 6710 760 3037 THE FLIGHT CREW REPORTED THE EMERGENCY LIGHTS AT 7 THROUGH 9 WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999103000001 19991030 00001 NM 1999 10 30 AWXA9900362 1 19991013 A 5610 WINDOW BOEING 737 7373G7 1384595 NM RT COCKPIT CRACKED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 322AW 25400 AIR TURNBACK, F/O'S SLIDING WINDOW CRACKED AT 13,700 MSL WITH ARCING AT TRAILING EDGE OF WINDOW. REMOVED AND REPLACED F /O'S SLIDING WINDOW AND RT WINDOW CONTROLLER. 2 L 7 2 4F RT A16WE 1999103000002 19991030 00002 NM 1999 10 30 DLM90992244 1 19991008 A 2610 HARNESS DOUG MD90 MD9030 3023690 NM NR 1 ENGINE DAMAGED A DALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 910DN 53390 000000 LEFT ENGINE FIRE WARNING ON T/O. FIRE BOTTLE DISCHARGED. A/C RETURNED TO BLOCKS, B-LOOP CORE HARNESS BAD, A-LOOP CHECK ED GOOD. 2 L 7 2 4F RT A6WE 1999103000003 19991030 00003 EA 1999 10 30 COMA9960615 1 19991015 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 796CA 7338 FLAP FAIL CAUTION MESSAGE ACTIVATED DURING APPROACH INTO IND. AIRCRAFT LANDED SAFETLY. REPLACED THE LEFT BRAKE POSITIO N SENSING UNIT. 2 L 7 2 4F RT A21EA 1999110500001 19991105 00001 NM 1999 11 5 TWRA9940 1 19990902 A 2620 SQUIB 33603903P BOEING 747 747238B 1384828 NM NR 1 ENGINE DID NOT TEST A TWRA K NONE L NO TEST DE DESCENT 1 EA 15 607FF M319 20011 FLT 390 - AT TOP OF DESCENT, THE ENGINE RT BOTTLE SQUIB INDICATION DIP DID NOT TEST. LEFT OK. DURING DESCENT WHEN TESTI NG THE NR 2 RIGHT BOTTLE SQUIB, LIGHT FLICKERED ON AND OFF. OPS CHECK NORMAL ON THE GROUND. PERFORMED SQUIB TEST OF NR 1 ENGINE, FOUND RIGHT SQUIB DID NOT TEST, LEFT SIDE OK. NR 2 ENGINE DID NOT CHECK OK ON GROUND WITH ENGINE RUNNING, RI GHT SQUIB LIGHT FLICKERED. RE-SECURED SQUIB WIRE AT BACKSHELL CONNECTOR WDM 26 21 11. SQUIB TEST OK MM 2620 00. REMOV ED AND REPLACED THE NR 1 ENGINE FIRE BOTTLE AND SQUIB MM 26-20-00. (X) 2 L 7 4 4F A20WE 1999110500002 19991105 00002 NE 1999 11 5 CA991007090 2 19990926 A 7210 BEARING CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15* 52060 NE NR 19 MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA PCE76043 (CAN) ELECTROLITIC DAMAGE TO BEARING FOUND. CAUSE UNDETERMINED. 1 L 7 2 4F 4 T A22CE E1NE 1999110500003 19991105 00003 NE 1999 11 5 AWXA9900379 2 19991022 A 7200 ENGINE AIRBUS A319 A319132 NM IAE V2522 V2522A5 NE RIGHT DAMAGED A AWXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 28 801AW 889 AIR TURNBACK, AFTER TAKEOFF 5 MIN & 6000 RT ENG CLASS 1 EGT OVERLIMIT WITH LOUD BANG AND ENG SPOOL DOWN. REPLACED NR 2 ENG IAW R5M71302, 4TH STAGE BLADE DAMAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 1999110500005 19991105 00005 NM 1999 11 5 DL72S992319 1 19991021 A 5512 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 TPA LTR CHECK F-2, 1 CRACK IN VERT STAB SKIN LT SIDE AT LWR SIDE OF CUTOUT FOR ACCESS PANEL 9523. REPAIRED PER MM 54-30 -0. 2 L 7 3 4F A3WE 1999110500006 19991105 00006 WP 1999 11 5 IXXA9900027 1 19991023 A 3260 STRIKER DOUG DC8 DC863F 302198F WP RT MLG DOOR LOOSE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 906R 46087 EN ROUTE FROM TOL TO CLT, AFTER GEAR RETRACTION, THE GEAR NOT LATCH LIGHT ILLUMINATED ACCOMPANIED BY AN ALTERNATE RIGHT MAIN GEAR DOOR WARNING LIGHT. THE FLIGHT CREW CYCLED THE GEAR, THE GEAR NOT LATCH LIGHT REMAINED ILLUMINATED AND THE ALTERNATE GEAR DOOR WARNING LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO CLT FOR AN UNEVENTFUL LANDING. MAINTENANCE INS PECTED THE LANDING GEAR WARNING SYSTEM WHICH REVEALED THE RIGHT MAIN GEAR DOOR SWITCH STRIKER NOT SECURED. MAINTENANCE SECURED THE RIGHT MAIN GEAR DOOR STRIKER AND PERFORMED A SUCCESSFUL OPERATIONAL TEST. 2 L 7 4 4F 4A25 1999110500007 19991105 00007 NE 1999 11 5 IXXA9900028 2 19991027 A 7310 FUEL FILTER DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE DIRTY A IXXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 829BX 45994 692325 EN ROUTE FROM LAX TO TOL, THE NUMBER ONE ENGINE FLAMED OUT DURING CRUISE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES A ND CONTINUED TO TOL FOR AN UNEVENFULL LANDING. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED THE NECESSARY TROUBLESHOO TING PROCEDURES IN ACCORDANCE WITH THE CFMI MAINTENANCE MANUAL. MAINTENANCE INSPECTED AND REPLACED THE FUEL FILTER AS P RECAUTIONARY. MAINTENANCE PERFORMED ENGINE POWER ASSURANCE CHECKS IN ACCORDANCE WITH THE COMPANY JET RUN HANDBOOK WITH N O DEFECTS NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999110500008 19991105 00008 WP 1999 11 5 IXXA9900029 1 19991028 A 3260 SWITCH DOUG DC8 DC863F 302198F WP LT MLG CORRODED A IXXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 906R 46087 DURING APPROACH INTO TOL, AFTER THE LANDING GEAR WAS EXTENDED THE LEFT MAIN GEAR DOWN AND LOCK INDICATION LIGHT FAILED T O ILLUMINATE. THE FLIGHT CREW CYCLED THE LANDING GEAR SEVERAL TIMES BEFORE THE DOWN AND LOCK LIGHT ILLUMINATED. MAINTENA NCE INSPECTED THE LANDING GEAR POSITIONING INDICATION SYSTEM WHICH REVEALED THE LEFT MAIN GEAR SWITCH ELECTRICAL CONNECT OR CORRODED. MAINTENANCE CLEANED THE ELECTRICAL CONNECTOR AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999110500009 19991105 00009 1999 11 5 AWXA9900381 4 19991024 A 3414 2083111 AIRSPEED IND BOEING 737 737277 1384570 NM LT COCKPIT MALFUNCTIONED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 189AW 30228 4690 22656 ABORTED TAKEOFF, AT APPROXIMATELY 80 KNOTS, CAPT KNOTS INDICATOR FLAGGED. REMOVED AND REPLACED CAPT'S AIRSPEED/MACH IN DICATOR, OPS NORMAL IAW MM34-12-2. SYSTEM WAS NOT ABLE TO BE FAULTED. TT 0104593. 2 L 7 2 4F RT A16WE 1999110500010 19991105 00010 1999 11 5 AWXA9900382 4 19991024 A 3441 5062010 PROBE AIRBUS 320 A320231 3930325 EU RT PITOT CLOGGED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 28 636AW 098 ABORTED TAKEOFF, F/O AIRSPEED INOP ON T/O ROLL. REMOVED AND REPLACED ADRIU NR 2 IAW MM 34-12-34, OPS CK OK. TT 0081682 . REMOVED AND REPLACED ADM NR 2 PITOT IAW MM 34-11-17, OPS CK OK. TT 0100724. REMOVED AND REPLACED F/O'S PITOT PROBE I AW MM 34--11-15, OPS CK OK. TT 0072478. LOW LEVEL LK CK PERFORMED IAW TASK CARD A1B34333. FOUND PROBLEM DUE TO WAX IN PITOT PROBE. NONE RELATED 120 DAY SNAPSHOT. 2 L 7 2 4F RT A28NM 1999110500011 19991105 00011 NM 1999 11 5 AWXA9900383 1 19991026 A 3350 900542 POWER SUPPLY BOEING 737 737277 1384570 NM L1 DOOR INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22647 L1 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOP. REMOVED AND REPLACED PWR SUPPLY M571, OPS CK GOOD ON GROUND AT THIS TIME. MEL REMOVED. MX CONTROL NOTIFIED (BATT PACK AND CHARGER WERE PREVIOUSLY CHANGED WITH NO HELP-- PLACED ON MEL). 2 L 7 2 4F RT A16WE 1999110500012 19991105 00012 NM 1999 11 5 AWXA9900384 1 19991026 A 2121 6454051 FAN BOEING 737 7373G7 1384595 NM CABIN FAILED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 302AW 46557 2330 24009 FLT ATTENDANTS REPORT AN ACRID SMELL NEAR THE FORWARD BULKHEAD AND IN THE REAR OF THE AIRCRAFT. REPLACED RECIRCULATION FAN IAW MM 21-21-22, OPS CK GOOD. 8 UN-RELATED WRITE-UPS IN LAST 120 DAYS. 2 L 7 2 4F RT A16WE 1999110500013 19991105 00013 NM 1999 11 5 AWXA9900385 1 19991027 A 3610 6714D060000AMDTA VALVE AIRBUS A319 A319132 NM NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 801AW 5558 3180 889 CONDITION: AIR TURN-BACK ENGINE BLEED FAULT LP 7559931DISCREPANCY: ENG 2 BLEED FAULT AT 1500 FT AGL AFTER TAKE-OFFCO RRECTIVE ACTION: R&R'D ENG 2 BLEED PRESSURE VALVE IAW MM 36 36-11-52-401--LEAK AND OPS GOOD TT 0065680CURRENT HI STORY: BLEED FAULT DAY PRIOR--RESET FAULT DID NOT RETURN 2 L 7 2 4F RT A28NM 1999110500014 19991105 00014 1999 11 5 AWXA9900386 2 19991028 A 7200 ENGINE AIRBUS 320 A320231 3930325 EU NR 1 FAILED A AWXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 622AW 27252 6178 054 EMERGENCY LANDING, ENG SHUTDOWN IN FLT NR 1 ENGINE FAILED AT FL 310. DIVERTED TO ICT FOLLOWED ALL ECAM ACTIONS. REMOVE D AND REPLACED NR 1 ENG PER CARD R5M71302 & F5M71301, OPS AND LEAK CHECK GOOD. TT 0023326. 2 L 7 2 4F RT A28NM 1999110500015 19991105 00015 SW 1999 11 5 PNSA991002 1 19991027 A 2730 CONRTOLS SWRNGN SA227 SA227AC 8780603 SW ELEVATOR ICED UP A PNSA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 AL 03 41NE AC741B EN ROUTE CAPTAIN NOTICED ELEVATOR CONTROL WAS STIFF. AIRCRAFT DIVERTED TO NEAREST AIRPORT. LANDING WAS UNEVENTFUL. MA INTENANCE PERSONNEL DISCOVERED THE ELEVATOR PULLEYS AT FUSELAGE STATION 512 WERE ENCASED IN ICE. AIRCRAFT WAS THAWED, W ATER DRAINED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A8SW 1999110500016 19991105 00016 SO 1999 11 5 RAAA99E4058 1 19990614 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 654 OUT OF LIMITS A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED #1 CHECK, FOUND FLOOR BEAM DRESSED OUT BEYOND LIMITS @ TRACK ATTACH FASTENER ON AFT FLANGE FUS/STA 654 LBL 55. REPLACED FLOOR BEAM AS PER SRM 51-2-9, INSTALLED FLOOR BEAM AS PER SRM 51-2-12, M-54 # 234. 2 L 7 4 4T 4A22 1999110500017 19991105 00017 SO 1999 11 5 RAAA99E4059 1 19990625 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 1130 PUNCTURED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, AIRCRAFT DAMAGED BY STAND, HOLE PUNCHED IN FUSELAGE SKIN AT FS 1130 STRINGER 42 DAMAGED. R EPAIRED STRINGER AS PER SRM 53-3-2. REPAIRED SKIN PER SRM 53-2-1, M-43 NR 238. 2 L 7 4 4T 4A22 1999110500018 19991105 00018 SO 1999 11 5 RAAA99E4060 1 19990629 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 597 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME CRACKED AT FLOORBEAM FLANGE FS 597 RBL 60. REPLACED FRAME SECT ION AT FACTORY SPLICE AS PER SRM 51-2-1 AND 51-2-12 M-43 NR 239. 2 L 7 4 4T 4A22 1999110500019 19991105 00019 SO 1999 11 5 RAAA99E4061 1 19990629 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 654 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME CORRODED AT FS 654 AT FLOORBEAM RBL 60. REPLACED FRAME SECTION AT FACTORY SPLICE PER SRM 51-21-1 AND 51-2-12 M-54 NR 240. 2 L 7 4 4T 4A22 1999110500020 19991105 00020 SO 1999 11 5 RAAA99E4062 1 19990629 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 673 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME CRACKED AT FS 673 AT FLOORBEAM FLANGE RBL 60. REPLACED FRAME S ECTION AT FACTORY SPLICE AS PER SRM 51-2-1 AND 51-2-12 M-54 NR 241. 2 L 7 4 4T 4A22 1999110500021 19991105 00021 SO 1999 11 5 RAAA99E4063 1 19990629 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 654 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME BENT AND HOLE TORN AT FS 654, 5-50. REPLACED FRAME TIP AS PER SRM 51-2-12, M-54 NR 246. 2 L 7 4 4T 4A22 1999110500022 19991105 00022 SO 1999 11 5 RAAA99E4064 1 19990609 A 5311 ANGLE LKHEED 188 188C 5262604 SO BS 654 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED # 1 CHECK, FOUND CORROSION UNDER SEALANT ON FRAME TIE ANGLE FUS/STA 654 S-50. REPLACED FRAME TIE ANGLE AND FRAME TIP AS PER SRM 51-2-12. M-54 # 247. 2 L 7 4 4T 4A22 1999110500023 19991105 00023 SO 1999 11 5 RAAA99E4065 1 19990629 A 5320 ANGLE LKHEED 188 188C 5262604 SO BS 588-610 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON FLOORBOARD ATTACH PLATE AT FS 588-610 LBL 60. INSTALLED NEW ATTACH ANGL E AS PER SRM 51-2-7 M-54 NR 248. 2 L 7 4 4T 4A22 1999110500024 19991105 00024 SO 1999 11 5 RAAA99E4066 1 19990629 A 5320 INTERCOSTAL LKHEED 188 188C 5262604 SO BS 502 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED AT FS 502 RBL 13. REPLACED INTERCOSTAL AS PER SRM 5 1-2-7 M-54 3 250. 2 L 7 4 4T 4A22 1999110500025 19991105 00025 SO 1999 11 5 RAAA99E4067 1 19990629 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 236 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOORBEAM CAP AT FS 236 LBL 27 - LBL 60. REPLACED FLOORBEAM AS PER SRM 51-2-1 M-54 NR 251. 2 L 7 4 4T 4A22 1999110500026 19991105 00026 SO 1999 11 5 RAAA99E4068 1 19990629 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 275 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM AT TOP FLANGE FS 275, LBL 22-LBL 52. REPLACED FLOOR BEAM AS PER SRM 51-2-1, M-54 NR 256. 2 L 7 4 4T 4A22 1999110500027 19991105 00027 SO 1999 11 5 RAAA99E4069 1 19990629 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 293 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM AT TOP FLANGE FS 293 LBL 22 - LBL 52. REPLACED TRAN VERSE FLOORBEAM AS PER SRM 51-2-1 M-54 NR 257. 2 L 7 4 4T 4A22 1999110500028 19991105 00028 SO 1999 11 5 RAAA99E4070 1 19990630 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 309 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM AT TOP FLANGE FS 309 LBL 29 - LBL 50. REPLACED TRAN VERSE FLOORBEAM PER SRM 51-2-1, M-54 NR 59. 2 L 7 4 4T 4A22 1999110500029 19991105 00029 SO 1999 11 5 RAAA99E4071 1 19990630 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 333 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM FS 333 LBL 55, BETWEEN REPAIR AND TOP FLANGE. REPLA CED FLOORBEAM AS PER SRM 51-2-1 M-54 NR 260. 2 L 7 4 4T 4A22 1999110500030 19991105 00030 SO 1999 11 5 RAAA99E4072 1 19990630 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 333 OUT OF LIMITS A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND TRANVERSE FLOORBEAM DRESSED OUT BEYOND LIMITS, FS 333 LBL 50. REPLACED TRANVERSE FLO ORBEAM AS PER SRM 51-2-1, M-54 NR 261. 2 L 7 4 4T 4A22 1999110500031 19991105 00031 SO 1999 11 5 RAAA99E4073 1 19990630 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 371 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM, TOP FLANGE AT FS 371 LBL 22 - LBL 58. REPLACED TRA NVERSE FLOORBEAM AS PER SRM 51-2-1, M-54 NR 263. 2 L 7 4 4T 4A22 1999110500032 19991105 00032 SO 1999 11 5 RAAA99E4074 1 19990629 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 695 MISDRILLED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FS 695 FRAME INNER FLANGE HAS RANDOM HOLES DRILLED IN AFT VERTICAL FLANGE BETWEEN S-54 AND S-54A, L-H. REPAIRED AS PER LDS DRAWING 188359, NEGLIGIBLE DAMAGE. 2 L 7 4 4T 4A22 1999110500033 19991105 00033 SO 1999 11 5 RAAA99E9030 1 19991026 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EMERGENCY LIGHT AT ROW 3 C, D, E, WILL NOT TEST. REPLACED BATTERY PACK. 2 L 7 4 4T 4A22 1999110500034 19991105 00034 NM 1999 11 5 CALA9901431 1 19991023 A 5320 WINDOW POST BOEING 737 7373T0 1384582 NM L-1 WINDOW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND A 0.37 INCH CRACK IN CAPTAIN'S L-1 WINDOW POST AT AFT UPPER CORNER. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02833. 2 L 7 2 4F RT A16WE 1999110500035 19991105 00035 NM 1999 11 5 CALA9901432 1 19991023 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312&344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59338 23576 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 0 TO RBL 10 AND AT STA 344, RBL 0 TO RBL 2. THE CORRODED SECTIONS O F FLOORBEAM WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-10-51, FIGURE 205 AND 53-00-51. 2 L 7 2 4F RT A16WE 1999110500036 19991105 00036 NM 1999 11 5 CALA9901433 1 19991024 A 5230 FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17321 23372 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR FRAME AT LOWER FORWARD CORNER. THE FORWARD CARGO CORNER DOOR FRAM E WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999110500037 19991105 00037 WP 1999 11 5 CALA9901434 1 19991025 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 783 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14079 46927 INSPECTION FOUND A 0.9 INCH CRACK IN RT WING LEADING EDGE SKIN AT XORS 783. A REPAIR WAS INSTALLED IAW SRM 57-10-00, FI GURE 68. 2 L 7 3 4F A22WE 1999110500038 19991105 00038 WP 1999 11 5 CALA9901435 1 19991026 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 940 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 940, LONGERON 23. THE DENTED AREA WAS CUT OUT AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2, PAGE 4. 2 L 7 2 4F A6WE 1999110500039 19991105 00039 NM 1999 11 5 CALA9901436 1 19991026 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 45 TO LBL 45. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW ECRA 5310- 03851. 2 L 7 2 4F RT A16WE 1999110500040 19991105 00040 NM 1999 11 5 CALA9901437 1 19991025 A 5730 PANEL BOEING 757 757224 1384958 NM WS 421-471 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13113 27555 INSPECTION FOUND A 10 AND 6 INCH CRACK IN LT WING FIXED LEADING EDGE PANEL AFT OF NR 4 L/E SLAT, WS 421-471. A FIBERGLA SS REPAIR WAS INSTALLED IAW ECRA 5720-01668. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK. 2 L 7 2 4F RT A2NM 1999110500041 19991105 00041 NM 1999 11 5 CALA9901438 1 19991025 A 5730 PANEL BOEING 757 757224 1384958 NM WS 421-471 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13113 27555 INSPECTION FOUND A 6 AND 7 INCH CRACK IN RT WING FIXED L/E PANEL AT WS 421-471. REPAIRED IAW ECRA 5720-01668. A DIP WA S INITIATED TO REINSPECT THE AREAS EVERY 1000 HOURS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK. 2 L 7 2 4F RT A2NM 1999110500042 19991105 00042 NM 1999 11 5 UPS99230990 1 19991026 A 3350 BATTERY PACK BOEING 727 7272A1 138407F NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999110500043 19991105 00043 NM 1999 11 5 UPS99230991 1 19991026 A 3350 BATTERY PACK BOEING 727 7272A1 138407F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999110500044 19991105 00044 NM 1999 11 5 UPS99230992 1 19991026 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 6A DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERGENCY LIGHT AT SEAT ROW 6A INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 6A, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999110500045 19991105 00045 NM 1999 11 5 UPS99230993 1 19991026 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 10R DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERGENCY LIGHTS AT SEAT ROW 10R OVERWING DOOR, LOWER WOULD NOT ILLUMINATE. REMOVED AND REPLACED B ATTERY PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999110500046 19991105 00046 NM 1999 11 5 UPS99230994 1 19991026 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 12R DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE:N/A, EMERGENCY LIGHT, SEAT ROW 12R OVERWING DOOR LOWER WOULD NOT ILLUMINATE, OPERATIONAL CHECKS OK AFTER TIGHTENING BATTERY PACK. 2 L 7 3 4F A3WE 1999110500047 19991105 00047 1999 11 5 UPS99830989 4 19991027 A 2350 INTERCOM DOUG DC8 DC871F 302199D WP RT COCKPIT INOP A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A, F/O'S OXYGEN MASK INTERCOM DOES NOT WORK. REMOVED AND REPLACED F/O'S O2 MASK. PERFORMED LEAK CK A ND OPS CK GOOD PER MM 35-00. 2 L 7 4 4F RT 4A25 1999110500048 19991105 00048 WP 1999 11 5 99FDEA00452 1 19991028 A 2740 SB102702085 CONTROL VALVE DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 392FE 46626 HORIZONTAL STABILIZER UPPER TRIM CONTROL VALVE HAD CRACKED IND INSIDE FLOW CONTROL VALVE BORE APPROX .5 INCH. *S/D* RE MOVED AND REPLACED HORIZONTAL STABILIZER PER M/M 27-43-03-4 OPS AND LEAK CK OK. 2 L 7 3 4F A22WE 1999110500049 19991105 00049 NM 1999 11 5 99FDEA00454 1 19991028 A 5330 6517555 SKIN BOEING 727 7272S2F 1384O81 NM BS 1398 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 NR 248 - DENT IN EXTERNAL SKIN AT BS 1398 2 ABOVE RAIN GUTTER ON LT SIDE. REPAIRED SKIN PER FEDEX EA 7-5430-47837. 2 L 7 3 4F A3WE 1999110500050 19991105 00050 NM 1999 11 5 99FDEA00455 1 19991028 A 5330 6517555 SKIN BOEING 727 7272S2F 1384O81 NM BS 1364 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 NR 247 - DENT IN EXTERNAL SKIN AT BS 1364 3 ABOVE RAIN GUTTER ABOVE NR 2 ENGINE ON LT SIDE. REPAIRED SKIN PER FEDEX EA 7-5430-47837. 2 L 7 3 4F A3WE 1999110500051 19991105 00051 WP 1999 11 5 ABXA9900751 1 19991018 A 5330 595256210 SKIN DOUG DOUG DC9 DC941 302207N WP BS 1072 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND CRACK IN SKIN AT LONGERON 14 RIGHT AND STATION 1072. REPAIRED IAW ABX REA D953-33715MR. 2 L 7 2 4F A6WE 1999110500052 19991105 00052 WP 1999 11 5 ABXA9900752 1 19991018 A 5230 49122791 FITTING DOUG DOUG DC9 DC941 302207N WP FORWARD CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR LOWER FORWARD STOP FITTING CRACKED. REPLACED FITTING IAW DC9 MM 51-30-5. 2 L 7 2 4F A6WE 1999110500053 19991105 00053 WP 1999 11 5 ABXA9900753 1 19991014 A 5400 59137627 ANGLE DOUG DOUG DC9 DC932 3022066 WP NR 2 NACELLE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND NR 2 ENGINE PYLON UPPER ATTACH ANGLE CRACKED AT STATION 950. REPAIRED ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1999110500054 19991105 00054 NM 1999 11 5 DHL99720007 1 19991025 A 5270 BZ2RQ18A2 SWITCH BOEING 727 727228 NM CARGO DOOR BROKEN A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 720DH 19544 CARGO DOOR LIGHT ILLUMINATED CARGO DOOR UNLOCK PASSING THROUGH APPROX 9000 AND 6.5 PSI , THEN WENT OUT AT APPROX 16,000 AND 6.2 PSI. STAYED OUT REMAINDER OF FLIGHT. FOUND AFT AUX LATCH PIN SWITCH BROKEN. REPLACED PER PEMCO MM 52-32-21. 2 L 7 3 4F A3WE 1999110500055 19991105 00055 NE 1999 11 5 DHL99802003 2 19991023 A 7321 8062479 MEC DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 3 ENGINE UNSERVICABLE A DHLA E ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 01 802DH 46076 NR 3 ENGINE N1 OCCILATION AND MODERATE VIBRATIONS CONCURRENT WITH OCCILATIONS. PRECAUTIONARY SHUTDOWN. CHANGED NR 3 ME C AND CIT SENSOR. OPS AND LEAK CHECK OK PER MM 73-20-1 AND 73-20-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 1999110500056 19991105 00056 NM 1999 11 5 VNAA9910018 1 19991026 A 3260 OL3092 LAMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG FAILED A VNAA K NONE P NO WARNING INDICATION AP APPROACH 1 GL 07 422JS 3018 ON APPROACH TO PIT FLIGHT 4172 HAD A GEAR INTRANSIT INDICATION BUT NO GREEN LIGHT INDICATION ON THE RT MAIN LANDING GEAR . THE CREW DID A TOWER FLY-BY TO CONFIRM GEAR DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R EPLACED THE RT MAIN LANDING GEAR DOWN AND LOCKED INDICATION BULBS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-61-12 . OPERATIONAL CHECKS WERE COMPLETED AND AIRCRAFT RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500057 19991105 00057 1999 11 5 VNAA9910019 4 19991027 A 6122 A5651 GOVERNOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 460PS 3061 UPON APPLICATION OF TAKEOFF POWER THE FLIGHT CREW RECEIVED ABNORMAL TORQUE INDICATIONS ON THE RIGHT HAND ENGINE. THE TA KEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REPLACED THE RIGHT HAND PROPELLER OVERSPEED GOVERNOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RELEASED FOR S ERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500058 19991105 00058 EU 1999 11 5 99ZZZX4123 1 19990824 A 7711 960137630 SWITCH 2887 BOLKMS BK117 BK117C1 5626025 EU NR 2 ENGINE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117SU 6 7527 PRESSURE SWITCH INOPERATIVE. COCKPIT LIGHT WILL NOT GO OFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H13EU 1999110500059 19991105 00059 1999 11 5 99ZZZX4124 4 19990811 A 3414 117940471 INDICATOR BOLKMS BK117 BK117C1 5626025 EU COCKPIT STICKS A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117SU 6 726507 7527 AIRSPEED INDICATOR NEEDLE STICKS AT 90 KNOTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H13EU 1999110500072 19991105 00072 SO 1999 11 5 99ZZZX4137 2 19990929 A 7421 RHB32E SPARK PLUG CHAMPION CESSNA 210 210M 2073450 CE CONT O520 IO520L 17032 SO ENGINE MISMANUFACTURED A A DKBA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 09 9163M 21062067 294984R SPARK PLUGS WERE REPLACED BECAUSE OF WEAR. UPON INSPECTION OF NEW PLUGS, FOUND WIRE WRAPPED AROUND CENTER ELECTRODE ON TWO OF THE NEW PLUGS (WHICH GROUNDED IT OUT) AND ANOTHER SIX WOULD NOT TEST GOOD IAW CHAMPION TEST PROCEDURES. OBTAINE D ANOTHER NEW SET OF PLUGS AND FOUND ONE LUG WITH WIRE AROUND CENTER ELECTRODE AND TWO OTHERS WOULD NOT TEST GOOD. BOTH SETS CAME FROM THE SAME BATCH OR LOT. LOT NR 4G99. 1 H 7 1 3O 3 O 3A21 E5CE 1999110500073 19991105 00073 SO 1999 11 5 99ZZZX4138 2 19990929 A 7421 RHB32E SPARK PLUG CHAMPION CESSNA 210 210M 2073450 CE CONT O520 IO520L 17032 SO ENGINE MISMANUFACTURED A A DKBA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 09 9163M 21062067 INSTALLED NEW PLUGS IN ENGINE. PERFORMED RUN-UP. OPS OK. FOUR HOURS LATER, ENGINE HAD A 600 RPM DROP. REMOVED SPARK P LUGS, FOUND A PIECE OF WIRE AROUND CENTER ELECTRODE OF 3 PLUGS AND 4 OTHER PLUGS NOT FIRING VERY HOT ON PLUG TESTER. OP ENED ANOTHER SET OF LUGS AND FOUND PIECE OF METAL RING AROUND CENTER ELECTRODE. APPEARED TO BE FROM MANUFACTURING PROCE SS. LOT NR 4G99. 1 H 7 1 3O 3 O 3A21 E5CE 1999110500074 19991105 00074 SO 1999 11 5 99ZZZX4139 2 19990930 A 7421 RBH32E SPARK PLUG CHAMPION CESSNA 210 210M 2073450 CE CONT O520 IO520L 17032 SO ENGINE MISMANUFACTURED A A DKBA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 09 761PS 21062415 UPON INSPECTION OF PLUGS, FOUND PLUGS, 4 EACH, TO TEST WEAK AND NOT APPROPRIATE FOR INSTALLATION ON AIRCRAFT. NOTE: BY DOM AIR CARRIERS, ONE OF THE FOUR SPARK PLUGS HAD A RED DISCOLORATION AT BASE OF ELECTRODE AND CERAMIC. LOT NR 4G99. 1 H 7 1 3O 3 O 3A21 E5CE 1999110500098 19991105 00098 NM 1999 11 5 SWAA991781 1 19991026 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 EXTERNAL FUSELAGE SKIN CRACKED, APPROX BS 727C, STRINGER 14L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999110500099 19991105 00099 NM 1999 11 5 SWAA991782 1 19991025 A 3350 BR2013 LENS BOEING 737 7373H4 1384600 NM EMER EXIT MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386SW 26601 EEPLS MISSING LENS AT OVERWING EXIT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 1999110500100 19991105 00100 NM 1999 11 5 SWAA991783 1 19991025 A 5320 6545409 WEB BOEING 737 7372H4 138448C NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND NLG WHEEL WELL CEILING CRACKED, BS 277 RT SIDE. REPAIRED WEB PER SRM. 2 L 7 2 4F A16WE 1999110500101 19991105 00101 NM 1999 11 5 SWAA991784 1 19991025 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED, BS 312, RBL 6. REPAIRED BEAM PER SRM. 2 L 7 2 4F A16WE 1999110500102 19991105 00102 NM 1999 11 5 SWAA991785 1 19991025 A 2560 6557463 BRACKET BOEING 737 7372H4 138448C NM SERVICE DR SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND FWD SERVICE SLIDE EVACUATION SLIDE FWD GIRT BAR MOUNT BRACKET CRACKED. REMOVED AND REPL ACED BRACKET PER OHM. 2 L 7 2 4F A16WE 1999110500103 19991105 00103 NM 1999 11 5 SWAA991786 1 19991025 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 900-933 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND STRINGER 26L CRACKED AND CORRODED, BS 900-933. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999110500104 19991105 00104 NM 1999 11 5 SWAA991787 1 19991025 A 5510 6547527 CHORD BOEING 737 7372H4 138448C NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB AFT UPPER TEE CHORD CRACKED AT ELEV STA 94.07. REPAIRED CHORD PER SR M AND BOEING DRAWING. 2 L 7 2 4F A16WE 1999110500105 19991105 00105 NM 1999 11 5 SWAA991789 1 19991025 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR WAY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF POSITION INSIDE CONTAINER. REPOSITIONED SLI DE ASSY PER MM. 2 L 7 2 4F A16WE 1999110500106 19991105 00106 NM 1999 11 5 SWAA991790 1 19991025 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED SERVICE CHECK, FOUND AFT EEPLS INOP. RECONNECTED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999110500107 19991105 00107 NM 1999 11 5 SWAA991791 1 19991025 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM BS 827,787&867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND 3 EACH FRAMES CRACKED, BS 827, BS 787, STRINGER 8L, AND BS 867, STRINGER 8R. REPAIRED F RAMES PER ER NR 99-6247. 2 L 7 2 4F RT A16WE 1999110500108 19991105 00108 NM 1999 11 5 SWAA991792 1 19991025 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 482,400&380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND 3 EACH FRAMES CRACKED, BS 482, BS 400, STRINGER 8L, AND BS 380, STRINGER 8R. REPAIRED F RAMES PER ER NR 99-6247. 2 L 7 2 4F RT A16WE 1999110500109 19991105 00109 NM 1999 11 5 SWAA991793 1 19991025 A 5311 6558280 FRAME BOEING 737 7375H4 138449D NM BS 299 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND DOORWAY FRAME CRACKED, BS 299, RBL 62. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999110500110 19991105 00110 NM 1999 11 5 SWAA991788 1 19991025 A 5314 6545409 KEEL BEAM BOEING 737 7375H4 138449D NM BS 482 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND KEEL BEAM LT LOWER CHORD CORRODED, BS 482B+4. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999110500111 19991105 00111 NM 1999 11 5 SWAA991776 1 19991023 A 2560 D31354 SLIDE BOEING 737 7373T5 NM PAX DOORWAY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 668SW 23060 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE GIRT SAGGING ON FLOOR. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999110500112 19991105 00112 NM 1999 11 5 SWAA991777 1 19991023 A 3350 07912 LENS BOEING 737 7373T5 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 668SW 23060 DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS BROKEN NEAR FWD END. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999110500113 19991105 00113 NM 1999 11 5 SWAA991778 1 19991024 A 3350 P4010021 BATTERY BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 LT FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999110500114 19991105 00114 NM 1999 11 5 SWAA991779 1 19991024 A 3350 65C27093 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOORWAY INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT A SSY PER MM. 2 L 7 2 4F A16WE 1999110500115 19991105 00115 NM 1999 11 5 SWAA991780 1 19991024 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 1140 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND STRINGER 5A LT CRACKED AT BS 1140. REPAIRED STRINGER SECTION PER SRM AND ER NR 99-6236P I. 2 L 7 2 4F RT A16WE 1999110500116 19991105 00116 NM 1999 11 5 SWAA991773 1 19991023 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM BS 930 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 930, STRINGER 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999110500117 19991105 00117 NM 1999 11 5 SWAA991774 1 19991023 A 5753 6573731 SKIN BOEING 737 7373H4 1384600 NM RT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING RON, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED ON INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 1999110500118 19991105 00118 NM 1999 11 5 SWAA991775 1 19991023 A 5314 6545866 KEEL BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM CRACKED AT 2 EACH PLACES, 1.5 FEET FROM FWD END AND 3 FEET FROM FWD END AT LT SIDE. REPAIRED BEAM PER TI-153-009. 2 L 7 2 4F RT A16WE 1999110500119 19991105 00119 NM 1999 11 5 SWAA991761 1 19991024 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369SW 26580 EEPLS WIRES EXPOSED IN TRACK BY OVERWING EXIT. REINSTALLED WIRING AND TRACKS PER MM. 2 L 7 2 4F RT A16WE 1999110500120 19991105 00120 NM 1999 11 5 SWAA991762 1 19991023 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 12-19 BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS INOP AT ROWS 12 TO 19. REPAIRED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999110500121 19991105 00121 NM 1999 11 5 SWAA991763 1 19991024 A 3350 07912 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 630WN 27705 EEPLS TRACK BROKEN IN SEVERAL PLACES. REPAIRED TRACK COVER ASSY PER MM. 2 L 7 2 4F RT A16WE 1999110500122 19991105 00122 NM 1999 11 5 SWAA991764 1 19991022 A 2170 1830104 COALESCER BOEING 737 7375H4 138449D NM A/C COMPT DIRTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 515SW 25154 OIL SMELL IN CABIN DURING TAKEOFF, CLIMB AND DESCENT. REMOVED AND REPLACE LT A/C WATER SEPARATOR PER MM. 2 L 7 2 4F RT A16WE 1999110500123 19991105 00123 NM 1999 11 5 SWAA991765 1 19991022 A 3230 65C16237 MODULE BOEING 737 737317 138447P NM E&E COMPT INOP A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 698SW 23176 AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED RELAY R276, AND M991 MODULE PER MM. 2 L 7 2 4F RT A16WE 1999110500124 19991105 00124 NM 1999 11 5 SWAA991766 1 19991022 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 EXTERNAL FUSELAGE SKIN CRACKED APPROX 8 INCHES AFT OF LT WING ILLUMINATION LIGHT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999110500125 19991105 00125 NM 1999 11 5 SWAA991767 1 19991022 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM SERVICE DOORWAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM. 2 L 7 2 4F RT A16WE 1999110500126 19991105 00126 NM 1999 11 5 SWAA991768 1 19991022 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12 AND RBL 7. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999110500127 19991105 00127 NM 1999 11 5 SWAA991769 1 19991022 A 5330 6545774 SKIN BOEING 737 7373T5 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 668SW 23060 DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCHES LONG CRACK ON FUSELAGE EXTERNAL SKIN, BS 727D, AND A 2.5 INCH LONG CRAC K ON BS 727E, BOTH ON STRINGER 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999110500128 19991105 00128 NM 1999 11 5 SWAA991770 1 19991022 A 5312 6516300 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999110500129 19991105 00129 NM 1999 11 5 SWAA991771 1 19991022 A 5320 6545410 BEAM BOEING 737 7375H4 138449D NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL CENTER WING BOX BEAM CRACKED, BS 663, RBL 25. REMOVED AND REPLACED BEAM SE CTION PER BAC DRAWING AND SRM. 2 L 7 2 4F RT A16WE 1999110500130 19991105 00130 NM 1999 11 5 SWAA991772 1 19991023 A 5320 6545807 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR UPPER FUSELAGE CUT OUT CENTER FWD FRAME CRACKED. REPAIRED FRAME PER S WA RA NR 1-353-2170. 2 L 7 2 4F RT A16WE 1999110500131 19991105 00131 NM 1999 11 5 SWAA991794 1 19991027 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS HAS EXPOSED WIRES. REPOSITIONED TRACK COVERS PER MM. 2 L 7 2 4F RT A16WE 1999110500132 19991105 00132 NM 1999 11 5 SWAA991795 1 19991026 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 637SW 27710 EEPLS LOOSE IN MID CABIN. REPAIRED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 1999110500133 19991105 00133 NM 1999 11 5 SWAA991796 1 19991026 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM PAX DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT BAR ATTACH BRACKETS (FWD AND AFT) LOOSE. TIGHTENED BOTH BRACKETS PER MM. 2 L 7 2 4F RT A16WE 1999110500134 19991105 00134 NM 1999 11 5 SWAA991797 1 19991027 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 16L CRACKED AT BS 420. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999110500135 19991105 00135 NM 1999 11 5 SWAA991798 1 19991027 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 397SW 27691 DURING SCHEDULED 1/2D CHECK, FOUND BS 986 FLOORBEAM UPPER FACE CORRODED ON RBL 31.5. REPAIRED BEAM PER SWA RA NR 1-353- 2172. 2 L 7 2 4F RT A16WE 1999110500136 19991105 00136 NM 1999 11 5 SWAA991799 1 19991027 A 5330 6545774 SKIN BOEING 737 7373T5 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 747, BETWEEN STRINGERS 22R-23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999110500137 19991105 00137 1999 11 5 SWAA991800 4 19991027 A 2565 2202290153 SLIDE BOEING 737 7372H4 138448C NM PAX DOORWAY FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 AFT ENTRY EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999110500138 19991105 00138 NM 1999 11 5 SWAA991801 1 19991027 A 3350 101114 BULB BOEING 737 7372H4 138448C NM LT EMER EXIT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 95SW 23054 LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F A16WE 1999110500139 19991105 00139 NM 1999 11 5 SWAA991802 1 19991027 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 22 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 601WN 27695 EEPLS INOP AT ROW 22. REPAIRED TRACK LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999110500140 19991105 00140 NM 1999 11 5 SWAA991803 1 19991026 A 3350 07912 COVER BOEING 737 7375H4 138449D NM ROW 4 CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 508SW 24185 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 4. REMOVED AND REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999110500141 19991105 00141 NM 1999 11 5 SWAA991804 1 19991026 A 5754 65C26686 SKIN BOEING 737 7373T5 NM LT LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED BELOW OUTBOARD TRACK CUT OUT. REPAIRED SKIN PER SWA RA NR1- A57-0691. 2 L 7 2 4F RT A16WE 1999110500142 19991105 00142 NM 1999 11 5 SWAA991805 1 19991028 A 5754 0570056 SKIN BOEING 737 7372H4 138448C NM LT LE SLAT DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 UPPER AFT SECTION OF NR 1 L/E SLAT TORN AND DELAMINATED. REMOVED AND REPLACED NR 1 L/E SLAT PER MM. 2 L 7 2 4F A16WE 1999110500143 19991105 00143 NM 1999 11 5 SWAA991806 1 19991027 A 5315 6546804 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND BS 344 FLOORBEAM UPPER FACE CORRODED, RBL 11-RBL 56. REPAIRED BEAM PER SRM. 2 L 7 2 4F A16WE 1999110500144 19991105 00144 NM 1999 11 5 SWAA991807 1 19991027 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 973-998 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 973-998. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999110500145 19991105 00145 NM 1999 11 5 SWAA991808 1 19991027 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND STRINGER 4L CRACKED, BS 727. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999110500146 19991105 00146 NM 1999 11 5 SWAA991810 1 19991027 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 1138 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND STRINGER 5R CRACKED, BS 1138. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999110500147 19991105 00147 NM 1999 11 5 SWAA991809 1 19991027 A 5320 6546578 DOUBLER BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND DOUBLER STRAP CRACKED, BS 1138, STRINGER 12L AND STRINGER 5R. REPAIRED DOUBLER PER SRM. 2 L 7 2 4F A16WE 1999110500148 19991105 00148 NM 1999 11 5 SWAA991811 1 19991027 A 5320 BAC1517 SPLICE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 360, STRINGER 11L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F A16WE 1999110500149 19991105 00149 NM 1999 11 5 TWAA9914601 1 19991029 A 3350 582243 BATTERY BOEING 767 767231 1385131 NM ROW 33-35 DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING PREFLIGHT, FOUND EGRESS LIGHTS INOP FROM SEAT 33 LT TO ROW 35 LT. REPLACED BATTERY. CC 10-24-99 LAX. 2 L 7 2 4F RT A1NM 1999110500150 19991105 00150 WP 1999 11 5 TWAA9914602 1 19991028 A 3350 0930197 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 917TW 49366 DURING PREFLIGHT, FOUND EGRESS LIGHTS INOP. REPLACED BATTERY PACK MFG PN 100865 AND POWER SUPPLY MFG PN 0930197. AC01 9 -10-99 DFW. 2 L 7 2 4F A6WE 1999110500151 19991105 00151 NE 1999 11 5 TWAA9914603 2 19991027 A 7314 3782017 FUEL PUMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D1 52044 NE RT ENGINE FAILED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 929L 47174 2107 ABORTED TAKEOFF ROLL, DUE TO RT ENG COMPRESSOR STALL. FOUND RT ENG FUEL PUMP OUT PUT SHAFT SHEARED. REPLACED FUEL PUMP ASSY. CC00 7-20-99 STL. 2 L 7 2 4F 4 F A6WE E2EA 1999110500152 19991105 00152 WP 1999 11 5 TWAA9914604 1 19991028 A 3350 408822101 BATTERY DOUG DC9 DC983 3022083 WP ROW 28L DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9305N 49395 DURING PREFLIGHT, FOUND OVERHEAD EMERGENCY LIGHTS INOP AT ROWS 28L AND 28R THROUGH ROWS 26L AND R AND 5 EACH INOP IN THE TAIL SECTION. REPLACED BATTERY. AC01 9-14-99 JFK. 2 L 7 2 4F RT A6WE 1999110500153 19991105 00153 WP 1999 11 5 TWAA9914605 1 19991026 A 2897 WIRE DOUG DC9 DC931 3022065 WP FUEL PANEL BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 WHILE THE AIRCRAFT WAS ON THE GROUND SPARKS WERE OBSERVED COMING FROM THE FUELING PANEL. REPLACED A BROKEN WIRE. CC00 9-4-99 STL. 2 L 7 2 4F A6WE 1999110500154 19991105 00154 WP 1999 11 5 TWAA9914606 1 19991029 A 3260 DS0775295 CONNECTOR DOUG DC9 DC932 3022066 WP LT MLG FAILED A TWAA K NONE O OTHER AP APPROACH 1 CE 05 998R 47030 DURING APPROACH, THE LEFT MAIN LANDING GEAR DOWN LOCK LIGHT FLICKERED. REPLACED SWITCH CONNECTOR MFG PN DS07-75295 AND SOCKET MFG PN 800-20-30-1. CC00 10-14-99, STL. 2 L 7 2 4F A6WE 1999110500155 19991105 00155 SO 1999 11 5 LR7A9962 1 19991021 A 5320 3483143 CROSS TIE LKHEED 382 382G 526414U SO BS 737 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 4590 DURING CARGO OFF LOADING AT WRG FS 737 CROSS TIE ASSY AFT FLANGE DENTED AT RBL 42.7 AND CRACKED AT LBL 42.7 DUE CARGO IM PACT. DAMAGE EVALUATED AND AIRCRAFT RELEASED FOR UNPRESSURIZED MAINTENANCE FERRY FLIGHT TO YXD FOR REPAIR PER COTNEY ED J51-1, REV IR. REPLACED CROSS TIE ASSY IAW DWG 348314-3. ACCOMPLISHED HFEC INSP ON ATTACH FTGS P/N 348314-7 AND -8. R EPLACED 2 ATTACHING DRAG BRACES P/N 356689-1L AND 1R. REPAIRED 3 ATTACHING DRAG SUPPORTS P/N 348405-3, -4 AND -5 PER SR M 51-140-22 PG 61. 2 H 7 4 4T A1SO 1999110500156 19991105 00156 NE 1999 11 5 9904369944 2 19991026 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LEFT FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 1309T 50676 7652 47316 666905 ON TAKEOFF, THE LEFT ENGINE LOST ALL OIL PRESSURE. THE LEFT ENGINE OIL PRESSURE DECREASE WAS NOTICED BY THE FLIGHT CREW DURING LANDING GEAR RETRACTION. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENG INE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1999110500157 19991105 00157 WP 1999 11 5 9904371235 1 19991024 A 5242 DOOR MECHANISM DOUG DC10 DC1040 3023508 WP E&E COMP NOT LATCHED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 235NW 46915 AVIONICS COMPARTMENT DOOR WARNING LIGHT ILLUMINATED AT ROTATION. LOUD WIND NOISE IN AIRCRAFT AND AIRCRAFT WOULD NOT PRE SSURIZE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENMANCE CLOSED AND LATCHED DOOR. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999110500158 19991105 00158 1999 11 5 9904381161 4 19991015 A 2565 SLIDE DOUG DC10 DC1040 3023508 WP 1L DOORWAY MALFUNCTIONED A NWAA K NONE O OTHER CR CRUISE 1 GL 01 161US 46770 DURING CRUISE DOOR 1L EMERGENCY EVACUATION SLIDE PARTIALLY INFLATED AND BROKE OUT OF THE COVER. THE SLIDE WAS PUNCTURED TO DEFLATE AND MOVED OUT OF GALLEY AREA. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TH E SLIDE, COVER, AND MANUAL LIFT BAR. REQUIRED INSPECTION COMPLETED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A22WE 1999110500159 19991105 00159 WP 1999 11 5 9904399949 1 19991020 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999110500160 19991105 00160 WP 1999 11 5 9904409951 1 19991021 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9347 45827 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY P ACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999110500161 19991105 00161 NM 1999 11 5 UPS99230995 1 19991027 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 19 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 ROW 19 EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999110500162 19991105 00162 NM 1999 11 5 UPS99230996 1 19991027 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM AFT AIRSTAIR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 AFT AIRSTAIR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999110500163 19991105 00163 NM 1999 11 5 UPS99230997 1 19991027 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 EMERGENCY LIGHT ABOVE AFT WORK STATION VERY DIM. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999110500164 19991105 00164 NM 1999 11 5 UPS99231000 1 19991028 A 3350 1000677 LIGHT BOEING 727 7272A1 138407F NM COCKPIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 213UP 21341 COCKPIT EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND TESTED PER MM 33-50-101. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999110500165 19991105 00165 NM 1999 11 5 UPS99430999 1 19991027 A 2611 SMOKE DETECTOR BOEING 747 747123 1384873 NM CARGO COMPT MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 673UP 20325 AFT LOWER CARGO FIRE WARINING ILLUMINATED DURING FLIGHT. DETERMINED TO BE FALSE WARNING. MEL'D AFT LWR CARGO FIRE WARN ING PER MEL 26-10-1-1, AND PLACARDED M 180936. 2 L 7 4 4F A20WE 1999110500166 19991105 00166 NM 1999 11 5 UPS99431001 1 19991028 A 8010 CONNECTOR BOEING 747 747121 1384871 NM NR 4 ENGINE CONTAMINATED A IPXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 691UP 19641 APPROX 2 HRS INTO FLIGHT, NR 4 START VALVE LIGHT CAME ON THE WENT OUT CAME ON AGAIN, THEN SHUT DOWN NR 4 ENGINE PER AOM. LIGHT WENT OUT. MX FOUND CONNECTORS AT START VALVE OIL SOAKED AND SHORTED. CLEANED CONNECTORS. SYSTEM OPS CHECK NOR MAL. THIS CLEARS M180958. 2 L 7 4 4F A20WE 1999110500167 19991105 00167 NM 1999 11 5 99FDEA00456 1 19991029 A 5210 MECHANISM BOEING 727 727227 1384078 NM L 1 DOOR NOT LATCHED A FDEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 25 478FE 21395 A/C LOST PRESSURIZATION ON CLIMB-OUT FROM COS, NO LIGHTS ILLUM ON DOOR PANEL. A/C BLOCKED IN FOUND L1 DOOR AFT SECTION WAS IN 2 INCHES. FWD SECTION WAS FLUSH. 2 L 7 3 4F A3WE 1999110500168 19991105 00168 EU 1999 11 5 RAIA9910036 1 19991027 A 2450 2105F PDU JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 567HK 41085 6124 - JFK - NON ESSENTIAL BUS SHED AND WON'T RESET. MAINTENANCE REPLACED RIGHT POWER DISTRIBUTION UNIT. 2 L 7 2 4T RT A41NM 1999110500169 19991105 00169 EU 1999 11 5 RAIA9910037 1 19991026 A 2434 8260121 GENERATOR AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LT ENGINE FAILED A RAIA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 722TE 1746 1746 220 124169R 7391 - XNA - LEFT GENERATOR INOP. MAINTENANCE REPLACED LEFT GENERATOR. 2 H 7 2 4T 4 T RT A53EU E2ONE 1999110500170 19991105 00170 SO 1999 11 5 RAIA9910038 1 19991026 A 2760 3604501001 VALVE EMB 145 EMB145ER SO SPOILER FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 2815 28715 145077 5780 - ORD - CHATTERING NOISE COMING FROM A/C ON LEFT SIDE. MAINTENANCE REPLACED GROUND SPOILER VALVE. 2 L 7 2 4F RT T00011AT 1999110500171 19991105 00171 WP 1999 11 5 TWA9914706 1 19991030 A 3350 BATTERY DOUG DC9 DC983 3022083 WP ROW 29DEF DISCHARGED A TWAA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 05 9404V 53140 DURING PREFLIGHT THE CABIN EGRESS LIGHTS WERE INOP AT ROW 29 D/E/F AND TAIL CONE EMERGENCY LIGHTS. INSTALLED A NEW MODU LE AND INSTALLED NEW BATTERY. 2 L 7 2 4F RT A6WE 1999110500172 19991105 00172 WP 1999 11 5 TWAA9914701 1 19991030 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN DIRTY A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 05 908TW 49169 PRIOR TO DEPARTURE FLT CREW REPORTED SMOKEY SMELL IN CABIN. CHANGED WATER SEPARATOR BAGS AND PERFORMED PACK BURN OUT. 2 L 7 2 4F A6WE 1999110500173 19991105 00173 WP 1999 11 5 TWAA9914702 1 19991029 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP RT MLG LOOSE A TWAA O OTHER N FALSE WARNING LD LANDING 1 CE 05 926L 47172 DURING LANDING, RIGHT GEAR SAFE LIGHT FLICKERED ON AND OFF. SECURED CONNECTOR ON THE RIGHT GEAR UPLOCK SWITCH. 2 L 7 2 4F A6WE 1999110500174 19991105 00174 NE 1999 11 5 TWAA9914703 2 19991030 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 909TW 30684 49170 01210 DURING CRUISE, THE LEFT ENGINE SHOWED VIBRATION, CREW SHUT DOWN THE ENG. REPLACED LEFT ENG AND PERFORMED ENG RUN. 2 L 7 2 4F 4 F A6WE E9NE 1999110500175 19991105 00175 WP 1999 11 5 TWAA9914704 1 19991030 A 3240 6002701 TEMP SENSOR DOUG DC9 DC983 3022083 WP BRAKE SYS CORRODED A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 9616G 53563 DURING CRUISE, THE SYSTEM BRAKE TEMP IND LIGHT CAME ON. REPLACED THE BRAKE TEMP SENSOR AND PERFORMED OPS CK AND TEST. 2 L 7 2 4F RT A6WE 1999110500176 19991105 00176 WP 1999 11 5 TWAA9914705 1 19991029 A 2150 ACM DOUG DC9 DC983 3022083 WP LT&RT OVERSERVICED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 9307R 49663 DURING ENG START UP SMOKE FILLED THE CABIN. LEFT AND RIGHT ACM'S WERE OVERSERVICED. SERVICED ACM'S TO PROPER LEVEL AND PERFORMED PACK BURNOUT. 2 L 7 2 4F RT A6WE 1999110500177 19991105 00177 WP 1999 11 5 TWAA9914707 1 19991030 A 5320 SPLICE DOUG DC9 DC982 3022082 WP BS 240 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925TW 49357 DURING LS, FOUND STATION 240 LONGERON L19 SPLICE IS CRACKED. INSTALLED NEW SPLICE IN ACCORDANCE WITH SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 1999110500178 19991105 00178 NM 1999 11 5 HNAA9900140 1 19991029 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO COMPT MALFUNCTIONED A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 927HA 117 BAGGAGE SMOKE WARNING LIGHT ILLUMINATED INFLIGHT AND EXTINGISHED ON LANDING. COULD NOT DUPLICATE PROBLEM ON GROUND. RE MOVED AND REPLACED NUMBER 1 SMOKE DETECTOR, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999110500179 19991105 00179 WP 1999 11 5 AT9900743 1 19991024 A 2910 HOSE DOUG DC9 DC932 3022066 WP RT MLG WW OUT OF POSITION A ZZDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 15 839AT 47089 DURING CLIMBOUT, THE GEAR DOOR OPEN LIGHT ILLUMINATED. RIGHT HYDRAULIC OVERFLOW BOTTLE HOSE WAS FOUND STUCK IN DOOR. R EPOSITIONED DRAIN HOSE FOR CLEARANCE. 2 L 7 2 4F A6WE 1999110500180 19991105 00180 WP 1999 11 5 AT9900747 1 19991012 A 5320 BRACKET DOUG DC9 DC932 3022066 WP FWD LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FORWARD LAVATORY WALL ATTACH L BRACKETS CORRODED. FABRICATED ANGLE REPAIR, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1999110500181 19991105 00181 WP 1999 11 5 AT9900748 1 19991013 A 5320 CUSP WEB DOUG DC9 DC932 3022066 WP BS 256 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND CUSP WEB AT BS 256 AND L18L CORRODED AT INTERSECTION OF SUBFLOOR AND SIDEWALL PANELS. REMOVED CORRODED AREA OF CU SP WEB AND REMOVED FRAME-TO-CUSP FITTING. FABRICATED REPAIR DOUBLER FOR CUSP WEB. REPLACED FRAME-TO-CUSP FITTING. INS TALLED REPAIR DOUBLER AND FRAME-TO-CUSP FITTING IAW DC9 SRM 51-10-3, 51-10-4, 51-30 AND MM 53-20-1. 2 L 7 2 4F A6WE 1999110500182 19991105 00182 WP 1999 11 5 AT9900749 1 19991013 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 389 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FORWARD CARGO DOOR CUTOUT UPPER WEB AT BS 389 HAD CORROSION UNDERNEATH WEB AT FLOORBEAM. REMOVED CORROSION FROM WEB, FA BRICATED REPAIR DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-30-2 AN D 53-01 FIG 2. 2 L 7 2 4F A6WE 1999110500183 19991105 00183 WP 1999 11 5 AT9900750 1 19991002 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 579-617 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND RT INBOARD FLOOR PANEL AT BS 579-617 CORRODED. FLOOR PANEL HAT SECTION CORRODED ON SQUARE ENDS AND ANGLED ENDS. MOST OF THE FASTENER HOLES ON THE TOP OF THE FLOOR PANEL HAVE CORROSION AND CIRCULAR WEAR GROOVES. REMOVED CORROSION F ROM AROUND FASTENER HOLES AND HAT SECTIONS. FABRICATED REPAIR DOUBLER, DRILLED, COUNTERSUNK AND INSTALLED IAW DC9 SRM 5 3-21-0 AND 51-10-4. 2 L 7 2 4F A6WE 1999110500184 19991105 00184 WP 1999 11 5 AT9900759 1 19991012 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 150 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND COCKPIT FLOOR SUPPORT FLANGE CORRODED BEYOND LIMITS. FABR ICATED FLOOR SUPPORT FLANGE AT BS 150 LBL 14 IAW SRM DC9 53-01 FIG 1, 51-10-02, 51-10-03 AND 51-30-03. 2 L 7 2 4F A6WE 1999110500185 19991105 00185 NM 1999 11 5 AT9900760 1 19991021 A 3350 LIGHT BOEING 737 7372L9 1384497 NM L2 DOORWAY LOOSE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 L-2 DOOR EMERGENCY EXIT LIGHT WILL NOT STAY IN PROPER POSITION. RESECURED L-2 DOOR EMERGENCY LIGHT IAW MM 25-50. 2 L 7 2 4F RT A16WE 1999110500186 19991105 00186 WP 1999 11 5 AT9900761 1 19990812 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT WING LEADING EDGE HAD THREE CRACKED REPAIR FRAMES/RIBS AT BS 445. REMOVED, FABRICATED AND INSTALLED REPAIR ANGLES IAW DC9 SRM 51-30-5, 57-01 FIGURE 3. 2 L 7 2 4F A6WE 1999110500187 19991105 00187 WP 1999 11 5 AT9900762 1 19990912 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT WING LEADING EDGE HAD TWO CRACKED REPAIR FRAMES/RIBS AT BS 383. FABRICATED AND INSTALLED REPAIR ANGLES/FRAM ES/RIBS IAW DC9 SRM 51-30-1, 51-30-2, 51-10-4, 57-22-1, 57-01 FIGURE 3. 2 L 7 2 4F A6WE 1999110500188 19991105 00188 WP 1999 11 5 AT9900763 1 19990906 A 5313 STRINGER DOUG DC9 DC932 3022066 WP BS 756 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND LEFT SIDE CABIN AT BS 756 STRINGER 2L WAS CRACKED AT ATTACH POINT. CUT OUT CRACKED SECTION, FABRICATED AND INSTAL LED REPAIR SECTION AND SPLICES IAW DC9 SRM 53-02 FIGURE 18, 51-30-2, 51-20-4, 51-10-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999110500189 19991105 00189 WP 1999 11 5 AT9900764 1 19990914 A 5313 76378133 LONGERON DOUG DC9 DC932 3022066 WP BS 680-699 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 LONGERON AT BS 680-699 L6R WAS FOUND CRACKED. CUT OUT CRACKED SECTION, FABRICATED LONGERON REPAIR AND SPLICE IAW DC9 SR M 53-02 FIGURE18, 51-10-3, 51-10-4, 51-30-5. 2 L 7 2 4F A6WE 1999110500190 19991105 00190 WP 1999 11 5 AT9900765 1 19990923 A 5313 2774922325000 LONGERON DOUG DC9 DC932 3022066 WP BS 148-178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND LONGERONS 3 AND 4 AT BS 148-178 CRACKED. REMOVED CRACKED SECTIONS, TRIMMED TO FIT AND INSTALLED NEW SECTIONS OF L ONGERONS 3 AND 4 WITH SPLICES IAW DC9 SRM 53-02 FIGURE 18. 2 L 7 2 4F A6WE 1999110500191 19991105 00191 WP 1999 11 5 AT9900766 1 19990911 A 5730 PANEL DOUG DC9 DC932 3022066 WP WS 383 DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND LEFT WING UPPER TRAILING EDGE PANEL INBOARD OF THE AILERON AT XRS 383 WAS DELAMINATED. CUT OUT DELAMINATED HONEYC OMB CORE, BONDED NEW CORE, DOUBLERS AND SKIN. REINSTALLED TRAILING EDGE PANEL IAW DC9 SRM 51-30-1, 51-30-2, TIMCO EO 99 -1309 REV DATED 10/12/99. 2 L 7 2 4F A6WE 1999110500192 19991105 00192 WP 1999 11 5 AT9900767 1 19990913 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT OUTBOARD FLOOR SUPPORT ABOUT 10 FROM SERVICE DOOR AT BS 160-200 WAS CORRODED. REMOVED FLOOR SUPPORT, FABRIC ATED, AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-30-4, 53-01 FIGURE 1, 51-10-2, 51-10-4, 51-30-5. 2 L 7 2 4F A6WE 1999110500193 19991105 00193 WP 1999 11 5 AT9900768 1 19990912 A 5712 99193054 RIB DOUG DC9 DC932 3022066 WP WS 241 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND RIGHT WING 5TH SLAT TRACK WAS CHAFING INTO XRS 241 LEADING EDGE RIB. BLENDED GOUGED AREA, TREATED AND PRIMED. RE MOVED AND REPLACED ROLLER BEARING IAW TIMCO EO 99-1294 REV DATED 10/05/99. 2 L 7 2 4F A6WE 1999110500194 19991105 00194 WP 1999 11 5 AT9900769 1 19991013 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 157 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR SUPPORT TO BE CORRODED BEYOND LIMITS. CLEANED CORRO SION AT BS 153, FABRICATED NEW FLOOR SUPPORT AND INSTALLED AT BS 157 IAW DC9 SRM 53-01 FIG 1, 51-10-03, 53-11-01 FIG 13, 51-30-02, AND CALIPER A-2542. 2 L 7 2 4F A6WE 1999110500195 19991105 00195 WP 1999 11 5 AT9900770 1 19991009 A 5743 FITTING DOUG DC9 DC932 3022066 WP LT MLG CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 811AT 47285 FOUND LEFT MAIN LANDING GEAR FIX STRUT ATTACH FITTING FORWARD AND AFT LUG FACES AND ID CORRODED. REAMED LUG HOLE TO 1.4 69 AND MECHANICALLY REMOVED CORROSION FROM, ID, FORWARD AND AFT, OF LUG FACES. FABRICATED NEW BUSHING AND SHIMS. INSTA LLED BUSHING AND SHIMS. PERFORMED MAG PARTICAL AND HFEC INSPECTION IAW EO 99-1324, DC9 MM 20-10-7. 2 L 7 2 4F A6WE 1999110500196 19991105 00196 WP 1999 11 5 AT9900771 1 19991026 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 246 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND 3.75 INCH CRACK ON LEADING EDGE OF RIGHT WING AT STA XOS 246. FABRICATED ONE INTERNAL AND ONE EXTERNAL DOUBLER AT STATION XOS 246 IAW EO 99-1597, DC9 SRM 51-10-02, 51-30-02, AND 51-30-04. 2 L 7 2 4F A6WE 1999110500197 19991105 00197 WP 1999 11 5 AT9900782 1 19991016 A 5320 PANEL DOUG DC9 DC932 3022066 WP BS 332-370 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND RT FORWARD CARGO SLANT PANEL AT BS 332-370 CORRODED OUT OF LIMITS ON UPPER SIDE AROUND FASTENER HOLES AND EDGE. R EMOVED CORROSION AROUND FASTENERS AND EDGES. FABRICATED NEW SLANT PANEL. TREATED, PRIMED AND REINSTALLED IAW DC9 SRM 5 3-01 FIG 1, 51-10-3 AND 51-10-2. 2 L 7 2 4F A6WE 1999110500198 19991105 00198 WP 1999 11 5 AT9900783 1 19991012 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-197 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FLOORBOARD SUPPORT CORRODED AT BS 160-197. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-3, 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999110500199 19991105 00199 WP 1999 11 5 AT9900784 1 19991015 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FLOOR SUPPORT ANGLE AT BS 160 CORRODED. REMOVED CORROSION FROM FLOOR SUPPORT ANGLE. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR SUPPORT ANGLE IAW DC9 SRM 51-10-3, 51-10-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999110500200 19991105 00200 WP 1999 11 5 AT9900785 1 19991018 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FORWARD FLOOR SUPPORT AT BS 200 AND RBL 24 TO RBL 42 CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, DRILL ED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 53-01 FIG 1, 51-30-3, 51-10-2 AND 53-11-1 FIG 13. 2 L 7 2 4F A6WE 1999110500201 19991105 00201 WP 1999 11 5 AT9900786 1 19991016 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 1039 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND SUPPORT ANGLE AT BS 1039 CORRODED FROM RBL 4 TO RBL 15. REMOVED CORROSION, FABRICATED STACKED ANGLE REPAIR, TREAT ED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 53-01 FIG 2, 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 1999110500202 19991105 00202 WP 1999 11 5 AT9900787 1 19991018 A 5320 HAT CHANNEL DOUG DC9 DC932 3022066 WP CABIN FLOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND HAT CHANNELS ON FLOOR PANEL NR 36 CORRODED AND CRACKED. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 53-2 1 FIG 3. 2 L 7 2 4F A6WE 1999110500203 19991105 00203 WP 1999 11 5 AT9900788 1 19991014 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 165-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FORWARD FLOOR SUPPORT AT BS 165-200 AND LBL 44 CORRODED. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, DRILLED, DEB URRED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-3 AND 51-30-5. 2 L 7 2 4F A6WE 1999110500204 19991105 00204 WP 1999 11 5 AT9900789 1 19990923 A 5260 STEP DOUG DC9 DC932 3022066 WP VENTRAL STAIRS CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND SECOND STEP FROM TOP OF VENTRAL STAIRS CORRODED. REMOVED STEP, REMOVED SUPPORT ANGLES, FABRICATED AND INSTALLED N EW SUPPORT ANGLES, PREPARED AND INSTALLED NEW STEP. FABRICATED AND INSTALLED REPAIR DOUBLER IAW TIMCO EO 99-1313, DC9 S RM 52-60-0 FIG 2, 51-30-1, 51-30-2, 51-10-2, 51-10-3 AND 52-63-0 FIG 802. 2 L 7 2 4F A6WE 1999110500205 19991105 00205 WP 1999 11 5 AT9900793 1 19991027 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND FUSELAGE TAIL INTERIOR FRAME AT BS 1143 CRACKED. INSTALLED NEW FRAME SECTION REPAIR AND SPLICES IAW TIMCO EO 99-1 292. 2 L 7 2 4F A6WE 1999110500206 19991105 00206 WP 1999 11 5 AT9900794 1 19991022 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 197-256 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND CABIN FLOOR SUPPORT AT BS 197-256 CORRODED OUT OF LIMITS ON SUPPORT AND 2 CRACKS ON SUBFLOOR. REMOVED AND REPLACE D FLOOR SUPPORT AT BS 197. FABRICATED AND INSTALLED REPAIR DOUBLER ON SUBFLOOR IAW DC9 SRM 53-20-1 AND 51-10-2. 2 L 7 2 4F A6WE 1999110500207 19991105 00207 WP 1999 11 5 AT9900795 1 19990912 A 2701 CONTROL COLUMN DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 812AT 47359 FOUND FIRST OFFICERS CONTROL COLUMN ON THE AFT LOWER SIDE BELOW THE MACH TRIM INDICATOR WAS CORRODED. TRIMMED OUT CRACK , MECHANICALLY REMOVED CORROSION. FABRICATED AND INSTALLED DOUBLER REPAIR IAW TIMCO EO 99-1301 REV DATE 10/13/99. 2 L 7 2 4F A6WE 1999110500208 19991105 00208 SO 1999 11 5 COMA9910169 1 19991029 A 3350 1013073 LIGHT EMB 120 EMB120RT SO CABIN INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 247CA 120225 FWD EMERGENCY FLOOR LIGHT WAS INOP. REPLACED LIGHT ASSY. 2 L 7 2 4T RT A31SO 1999110500209 19991105 00209 SO 1999 11 5 COMA9910170 1 19991028 A 3230 PINS EMB 120 EMB120RT SO LANDING GEAR NOT REMOVED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 264CA 120256 LANDING GEAR WILL NOT RETRACT. REMOVED LANDING GEAR DOWNLOCK PINS. RETRACT CHECK NORMAL. 2 L 7 2 4T RT A31SO 1999110500210 19991105 00210 EA 1999 11 5 COMA9960653 1 19991029 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 13579 7040 CRACK IN J CHANNEL ON FS 280 ON O/B SIDE OF RBL 9, CRACK IS 1.7 INCH LONG. REPAIRED AFT J ANGLE ON FS 280.0 O/B SIDE OF RBL 9 IAW WVAC EO 601R-53-0535. 2 L 7 2 4F RT A21EA 1999110500211 19991105 00211 EA 1999 11 5 COMA9960654 1 19991029 A 5315 601R31113767 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280-370 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 FLOOR SUPPORT BEAM CAP (P/N 601R31113-67) AT RBL 9 WAS CORRODED BETWEEN FS 280 TO FS 370. PERFORMED A MAJOR REPAIR BY R EPLACING CORRODED SECTION OF FLOORBEAM CAP (P/N 601R31113-67) AT RBL 9 BETWEEN FS 280 TO FS 409 IAW CRJ REO 601R-53-00-0 27 NC. 2 L 7 2 4F RT A21EA 1999110500212 19991105 00212 EA 1999 11 5 COMA9960655 1 19991027 A 5320 601R530479A ANGLE CNDAIR CL600 CL6002B19 EA PAX DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 PAX DOOR ENTRANCE FLOOR SUPPORT ANGLE HAD CORROSION (P/N 601R31527-46R). REMOVED AND INSTALLED PAX DOOR THRESHOLD ANGLE IAW WVAC EO 601R-53-0479A. 2 L 7 2 4F RT A21EA 1999110500213 19991105 00213 EA 1999 11 5 COMA9960656 1 19991031 A 5320 6003606032 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 AFT DOUBLER CRACKED AT FS 718.00 STR 11, LEFT AND RIGHT SIDE OF AIRCRAFT. REMOVED CRACKED DOUBLERS AND INSTALLED NEW DO UBLERS AT FS 718.00 STR 11 RHS IAW WVAC EO 601R-53-0543, AND AT FS 718.00, STR 11, LHS IAW WVAC EO 601R-53-0542. 2 L 7 2 4F RT A21EA 1999110500214 19991105 00214 EA 1999 11 5 COMA9960657 1 19991029 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 349 MISDRILLED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 933CA 13579 7040 FLOORBEAM CAP LBL 9 HAS A OVERSIZED HOLE AT FS 349. REAMED OVERSIZED HOLE AT FS 349 FLOORBEAM CAP LBL 9 TO ACCOMODATE F ASTENER H18P38-3 HI-LOK AND INSTALLED FASTENER IAW CRJ WVAC EO 601R-53-0516A. 2 L 7 2 4F RT A21EA 1999110500215 19991105 00215 EA 1999 11 5 COMA9960658 1 19991029 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 THE AFT J-ANGLE AT FS 380 AND RBL 9.0 WAS CRACKED. REMOVED CRACKED SECTION AND SPLICED NEW SECTION OF ANGLE (P/N 600-34 017-595) IAW WVAC EO 601R-53-0535. 2 L 7 2 4F RT A21EA 1999110500216 19991105 00216 EA 1999 11 5 COMA9960659 1 19991029 A 5320 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 13579 7040 SERVICE DOOR DOUBLER FORWARD OF DOOR HAD CORRODED AREA. REMOVED AND REPLACED DOUBLER FORWARD OF DOOR IAW WVAC EO 601R-5 3-0530. 2 L 7 2 4F RT A21EA 1999110500217 19991105 00217 EA 1999 11 5 COMA9960660 1 19991029 A 5320 601R3114879 SILL CNDAIR CL600 CL6002B19 EA SERVIC DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 THE FLOOR SILL FWD OF THE SERVICE DOOR P/N 601R31148-79 IS CORRODED.\NPERFORMED A MAJOR REPAIR BY REPLACING FLOOR SILL P /N 601R31148-79 FWD OF THE SERVICE DOOR IAW WVAC EO 601R-53-0531. 2 L 7 2 4F RT A21EA 1999110500218 19991105 00218 EA 1999 11 5 COMA9960661 1 19991029 A 5315 60034017351 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 13579 7040 THE FLOORBEAM AT FS 280 WAS CORRODED ON THE UPPER EDGE BETWEEN RBL 9 AND LBL 9. PERFORMED A MAJOR REPAIR TO CORRODED FL OORBEAM WEB AT FS 280 BETWEEN RBL 9 AND LBL 9 IAW WVAC EO 601R-53-0505. 2 L 7 2 4F RT A21EA 1999110500219 19991105 00219 EA 1999 11 5 COMA9960662 1 19991029 A 5320 601R38673 SUPPORT CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 FLOOR SUPPORT PLATES AT FS 349.0 (P/N'S 601R38673-17,-19,-21 AND -25) BETWEEN LBL 42 TO RBL 42 WERE CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING FLOOR SUPPORT PLATES (P/N 601R38673-17,--19,-21 AND -25) AT FS 349 BETWEEN LBL 42 TO RBL 42 IAW EVAC EO 601R-53-0515. 2 L 7 2 4F RT A21EA 1999110500220 19991105 00220 EA 1999 11 5 COMA9960663 1 19991028 A 5320 60034017723 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 13579 7040 VERTICAL L ANGLE FWD FS 280.0 AT LBL 9 IS CRACKED (P/N 600-34017-723). PERFORMED A MAJOR REPAIR. REMOVED CRACKED L ANG LE FWD OF FS 280 JUST O/B OF LBL 9 AND REPLACED WITH NEW ANGLE IAW WVAC EO 601R-53-0517. 2 L 7 2 4F RT A21EA 1999110500221 19991105 00221 EA 1999 11 5 COMA9960664 1 19991028 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA SERVICE DOORWAY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 SERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE WAS CORRODED (P/N 601R38303-105). REMOVED UNSERVICEABLE THRESHOLD ANGLE (P/N 601R38303-105) AND INSTALLED NEW SERVICEABLE ANGLE (P/N 3992T 7075 T6511) EXTRUSION IAW WVAC EO 601R-53-0478A. 2 L 7 2 4F RT A21EA 1999110500222 19991105 00222 EA 1999 11 5 COMA9960665 1 19991029 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280-356 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 FLOOR SUPPORT BEAM CAP (P/N 601R31113-67) AT RBL 27 WAS CORRODED BETWEEN FS 310 TO FS 349. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED SECTION OF FLOORBEAM CAP (P/N 601R31113-67) AT LBL 27 BETWEEN FS 280 TO FS 356 IAW CRJ 601R-53-00-027 NC AND WVAC EO 601R-53-0482A. 2 L 7 2 4F RT A21EA 1999110500223 19991105 00223 EA 1999 11 5 COMA9960666 1 19991025 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7718 7145 FRAME FLANGE AND FRAME DOUBLER AT FS 718.00 STR 11 LHS WAS CRACKED. PERFORMED A MAJOR REPAIR TO CRACKED FRAME FLANGE AN D FRAME AFT DOUBLER AT FS 718.0 STR 11 LHS IAW CRJ REO 601R-53-61-193 REVA AND WVAC EO 601R-53-0503. 2 L 7 2 4F RT A21EA 1999110500224 19991105 00224 EA 1999 11 5 COMA9960667 1 19991025 A 5320 601R9515544 SUPPORT CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7145 ACM SUPPORT BEAM ON RHS AT FS 718.0 WAS CRACKED. PERFORMED A MAJOR REPAIR TO CRACKED ACM SUPPORT BEAM AT FS 718.0 RHS I AW WVAC EO 601R-53-0495A. 2 L 7 2 4F RT A21EA 1999110500225 19991105 00225 NM 1999 11 5 99FDEA00453 1 19991028 A 5330 6517555 SKIN BOEING 727 7272S2F 1384O81 NM BS 1427 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 211FE 22933 DENT IN EXTERNAL SKIN AT BS 1427 6 O/B OF VERTICAL STABILIZER ON LT SIDE. *S/D* REPAIRED DENT, ALL WORK DONE IAW FEDEX EA NR 7-5430-47837. 2 L 7 3 4F A3WE 1999110500226 19991105 00226 WP 1999 11 5 ABXA9900754 1 19991028 A 2421 31229000 GENERATOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 4 DEFECTIVE A ABXA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 GL 23 808AX 2041 45954 643547 FAULT ON NR 4 GENERATOR. UNABLE TO RESET IAW ABNORMAL CHECKLIST. SECURED ENGINE, MAINTAINED POSITIVE ENGINE OIL PRESSU RE. INSPECTED MAIN OIL FILTER, FOUND NO CONTAMINATION. CHECKED OIL QUANTITY, RAN ALL ENGINES, ENGINE RUN WAS NORMAL. C HECKED AIRCRAFT WIRING AT GENERATOR RELAYS AND BUS TIE RELAYS. REPLACED NR 4 GENERATOR AND CSD. OPS AND LEAK CHECKED G OOD IAW DC8 MM 24-10 AND 24-20. 2 L 7 4 4F 4 F 4A25 1E8 1999110500227 19991105 00227 WP 1999 11 5 MWEA99744 1 19991030 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOORWAY LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 GALLEY DOOR EVACUATION SLIDE PACKWASS LOOSE ON DOOR. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE PACK. 2 L 7 2 4F A6WE 1999110500228 19991105 00228 WP 1999 11 5 MWEA99745 1 19991031 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOORWAY DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 400ME 45727 ATTACH PIN AT BOTTOM OF GALLEY DOOR SLIDE PACK HAS BECOME DETACHED -- MTC REINSTALLED GALLEY DOOR SLIDE COVER 2 L 7 2 4F A6WE 1999110500229 19991105 00229 WP 1999 11 5 MWEA99746 1 19991028 A 5240 59114071 DOUBLER DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 ACCOMPLISH SERVICE DOOR HOLD OPEN PIN SKIN CUTOUT REWORK. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500230 19991105 00230 WP 1999 11 5 MWEA99747 1 19991028 A 5240 49157601 PIN DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 SERVICE DOOR HOLD OPEN PIN WAS CRACKED. MTC DRILLED AND INSTALLED NEW PIN. 2 L 7 2 4F A6WE 1999110500231 19991105 00231 WP 1999 11 5 MWEA99748 1 19991028 A 5712 391225 RIB DOUG DC9 DC932 3022066 WP WS 446 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 CORROSION AROUND FASTENERS AND ON TRACK, LOWER RIB TRACK AT STATION 446 AT LONGERONS 29 LEFT TO 28 LEFT. CORROSION OUT OF LIMITS. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500232 19991105 00232 WP 1999 11 5 MWEA99749 1 19991028 A 5230 59101575 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 CRACK ON INNER DOOR PAN BELOW AFT LATCH ON AFT CARGO DOOR. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500233 19991105 00233 WP 1999 11 5 MWEA99750 1 19991028 A 5320 99124541 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 446 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO COMPARTMENT FRAME AT STATION 446, SHEAR TIE WAS CUT DURING REPAIR BETWEEN LONGERONS 26 RIGHT, 27 RIGHT. M TC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500234 19991105 00234 WP 1999 11 5 MWEA99751 1 19991028 A 5230 59101571 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT CARGO DOOR INNER PAN WAS BLENDED AROUND CUT OUT FOR HANDLE MECHANISM -- MTC FABRICATED AND INSTALLED DOUBLER 2 L 7 2 4F A6WE 1999110500235 19991105 00235 WP 1999 11 5 MWEA99752 1 19991028 A 5230 59101411 WEB DOUG DC9 DC932 3022066 WP CARGO DOOR CORODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FORWARD CARGO DOOR WEB HAD BEEN BLENDED DIRECTLY BELOW THE CARGO DOOR MECHANISM. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500236 19991105 00236 WP 1999 11 5 MWEA99753 1 19991028 A 5330 59114061 SKIN DOUG DC9 DC932 3022066 WP PAX DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FUSELAGE SKIN CRACKED AT PASSENGER DOOR JAMB UPPER FORWARD CORNER. MTC FABRICATED AND INSTALLED TITANIUM DOUBLER. 2 L 7 2 4F A6WE 1999110500237 19991105 00237 WP 1999 11 5 MWEA99754 1 19991101 A 5230 59101573 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 AFT CARGO DOOR HANDLE IS CHAFING INTO OUTER DOOR SKIN. MTC FABRICATED CHAFE DOUBLER. MTC INSTALLED CHAFE DOUBLER. 2 L 7 2 4F A6WE 1999110500238 19991105 00238 WP 1999 11 5 MWEA99755 1 19991101 A 5730 591216148 PANEL DOUG DC9 DC932 3022066 WP RT WING DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 RIGHT WING MOST INBOARD TRAILING EDGE PANEL (TRAP PANEL) HAD APPROX 120 SQUARE INCH OF DELAMINATION ON LOWER AFT SURFACE . MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500239 19991105 00239 WP 1999 11 5 MWEA99756 1 19991101 A 5512 5910402529 SKIN DOUG DC9 DC932 3022066 WP RT HORIZ STAB CORRODID A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 RIGHT HORIZONTAL STABILIZER HAD MODERATE CORROSION ON OUTBOARD HALF OF LEADING EDGE. CORROSION WAS OUT OF LIMITS. MTC FABRICATED AND INSTALLED DOUBLER ON RIGHT STABILIZER. 2 L 7 2 4F A6WE 1999110500240 19991105 00240 WP 1999 11 5 MWEA99757 1 19991101 A 5752 5910047501 TAB DOUG DC9 DC932 3022066 WP LT AILERON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 WATCH ITEM 3038 REPAIR LT AILERION CONTROL TAB, ORIGINAL REPAIR ACCOMPLISHED CORRECTLY. MTC REMOVED TAGGED AILERON. RE MOVED DAMAGED AREA THEN FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500241 19991105 00241 WP 1999 11 5 MWEA99758 1 19991101 A 5313 5920319504 LONGERON DOUG DC9 DC932 3022066 WP BS 387 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LIGHT CORROSION OF LONGERON 30 STATION 387. CORROSION WAS OUT OF LIMITS. MTC FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 1999110500242 19991105 00242 WP 1999 11 5 MWEA99759 1 19991101 A 5320 5911401195 DOUBLER DOUG DC9 DC932 3022066 WP BS 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FUSELAGE SKIN HAD CRACK AT STATION 200 BETWEEN LONGERON 20 AND 21 COMING OUT OF THE AIRSTAIR COMPARTMENT OPENING LOWER A FT CORNER. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999110500243 19991105 00243 WP 1999 11 5 MWEA99760 1 19991101 A 5320 593660095 SPLICE DOUG DC9 DC981 3022081 WP BS 1212 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT CARGO TIE DOWN TRACK SUPPORT SPLICE WAS CORRODED AT STATION 1212 TO 1231. MAINTENANCE FABRICATED AND INSTALLED SPL ICE REPAIR. 2 L 7 2 4F A6WE 1999110500244 19991105 00244 WP 1999 11 5 MWEA99761 1 19991101 A 5240 591008425 WEB DOUG DC9 DC981 3022081 WP SERVICE DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FORWARD GALLEY SERVICE DOOR CLOSE OUT WEB JUST BELOW BAYONET WAS CHAFED. MAINTENANCE FABRICATED AND INSTALLED REPAIR DO UBLER. 2 L 7 2 4F A6WE 1999110500245 19991105 00245 WP 1999 11 5 MWEA99762 1 19991101 A 5751 995757112 SKIN DOUG DC9 DC981 3022081 WP RT AILERON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 RIGHT AILERON SKIN UNDER UPPER CHAFE STRIP WAS CORRODED. MAINTENANCE FABRICATED AND INSTALLED SKIN REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999110500246 19991105 00246 WP 1999 11 5 MWEA99763 1 19991101 A 5522 593055717 SKIN DOUG DC9 DC981 3022081 WP LT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT ELEVATOR INBOARD TOP SKIN PANEL JUST AFT OF LEADING EDGE WAS CRACKED. MAINTENANCE FABRICATED AND INSTALLED SKIN PA NEL REPAIR. 2 L 7 2 4F A6WE 1999110500247 19991105 00247 NM 1999 11 5 DLM88992371 1 19991026 A 2910 O RING DOUG MD88 MD88 3023688 NM RT HYD SYS FAILED A DALA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 990DL 53342 ON APPROACH, RT HYD SYSTEM DROPPED TO 4 QTS. ACCOMPLISHED POM PROCEDURE. AFTER POM ACCOMPLISHED STABILIZED WITH 3 QUAR TS. NORMAL PRESSURE. FOUND PLUG ON RUDDER SHUTOFF VALVE LEAKING. REPLACED O-RING. 2 L 7 2 4F RT A6WE 1999110500248 19991105 00248 NM 1999 11 5 DL72S992375 1 19991027 A 7120 65312813 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 NR 2 ENG AFT MOUNT SUPPORT ANGLE LEFT HAND WAS CORRODED. REPLACED ANGLE. 2 L 7 3 4F A3WE 1999110500249 19991105 00249 NM 1999 11 5 DL72S992376 1 19991027 A 7120 65312814 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 NR 2 ENG AFT MOUNT LOWER CHORD WAS CORRODED. REPLACED CHORD. 2 L 7 3 4F A3WE 1999110500250 19991105 00250 NM 1999 11 5 DL733992377 1 19991026 A 2720 65C370537 PCU BOEING 737 737347 1384647 NM RUDDER FAILED A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 27 304WA 1583AC 23345 AT FL370, MACH .76 THE ACFT EXPERIENCED AN UNCOMMANDED YAW, (TWO SEPARATE SHARP INPUTS). YAW DAMPER SWITCH TURNED OFF. MTC IN PROGRESS REPLACING RUDDER PCU, YAW DAMP COUPLER AND WIRING CHECKOUT. 2 L 7 2 4F RT A16WE 1999110500251 19991105 00251 NM 1999 11 5 DLM11992378 1 19991027 A 3150 CAWS H05A003553 DOUG MD11 MD11 3023602 NM E/E INOP A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 806DE 43 48477 ATB AURAL WARNING WITH NO VISUAL CAUSE, UNABLE TO SILENCE HORN. REPLACED CAWS UNIT. 2 L 7 3 4F RT A22WE 1999110500252 19991105 00252 NM 1999 11 5 DL72S992379 1 19991024 A 4920 656740214 APU BOEING 727 727232 1384082 NM WHEE WELL INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 33422 21702 P36446 DURING HMV CK WORKING MCO 127703001, APU QUIT AT GATE BEFORE PUSHBACK. DURING T/S AND JIC OP 6009 FOUND APU FIRE TEST I NOP. ALSO, FOUND FIRE LOOP BROKEN WITH APPARENT HIGH HEAT INDICATION AND SOOT INSIDE APU SHROUD AT INNER EXHAUST DUCT C LAMP. REPLACED APU (S/N 36681). 2 L 7 3 4F A3WE 1999110500253 19991105 00253 NE 1999 11 5 DLL10992380 2 19991027 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 1 FAILED A DALA A UNSCHED LANDING C M J F.O.D. OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 1734D 42277 193C1225 10553 BIRD STRIKE ON NR 1 ENGINE AT LIFTOFF. ENGINE BEGAN TO VIB, SURGE, STALL AND TGT ROSE TO 900 DEGS FOR GREATER THAN 30 S ECS. REPLACED ENGINE. 2 L 7 3 4F 4 F A23WE E12EU 1999110500254 19991105 00254 NM 1999 11 5 DL73K992381 1 19991026 A 2120 AIR DIST BOEING 737 737232 1384475 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 318DL 23090 ELECTRICAL ODOR EMINATING FROM FWD CABIN (ROW 4 TO FWD GALLEY) SIMILAR TO VERY POTENT MATCH SMELL. INSPECTED ACFT ELECT SYS, GALLEY PWR, OVERHEAD AND SIDEWALL LIGHTS, ALL OK. RAN NR 1 AND NR 2 ENGINES, LOADED ELECT SYSYEMS NTF. RAN LT AN D RT PACKS, NO ODOR DETECTED. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 1999110500255 19991105 00255 NM 1999 11 5 DL72W992382 1 19991027 A 5320 ANGLE BOEING 727 727247 138408F NM BS 1253 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 TORQUE BOX Z ANGLE CRACKED LT SIDE STA 1253. REPAIRED PER SRM 51-40-3. 2 L 7 3 4F A3WE 1999110500256 19991105 00256 NM 1999 11 5 DLM88992383 1 19991027 A 2910 AS15308K0254 HOSE DOUG MD88 MD88 3023688 NM RT HYD SYS FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 936DL 49723 IN FLT PASSING APPROX 16,000 FT, GOT RT HYD PRESS LOW MESSAGE. HYD PRESS WAS 0 AND HYD QTY READ 6. RAN POM CHECKLIST ( 17-104 AND 17-106) HYD PRESS LOW AND HYD QTY DECREASING. TURNED OFF THE RIGHT HYD PUMP AND HAD TO USE ALT GEAR EXTEND P ROCEDURE. WITH RT ENG DRY SPIN FOUND RT HYD PRESS LINE LEAKING IN TAIL SECTION TO POWER MODULE. REMOVED AND REPLACED R T ENG HYD PRESS LINE. LEAK CHECKED OK. 2 L 7 2 4F RT A6WE 1999110500257 19991105 00257 NM 1999 11 5 DLM88992384 1 19991028 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM BS 218-229 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DL 49573 A DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN FS 218 AND 229 AND BETWEEN LONGERONS 18L AND 19L. THE DAMAGE WAS REMOVED WITH A 11 X 6 CUTOUT AND REPAIRED PER ERA 333708-14 AT HMV. 2 L 7 2 4F RT A6WE 1999110500258 19991105 00258 NM 1999 11 5 DL733992385 1 19991028 A 5330 654576987 SKIN BOEING 737 73735B NM FUSELAGE MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 221DL 23970 IMPROPER FASTENER SPACING WAS FOUND AT THE VHF ANTENNA RESULTING IN A 2.0 INCH DIAMETER HOLE FOR DAMAGE REMOVAL. TH E DAMAGE WAS REPAIRED PER ERA 333724-14 AT MV. 2 L 7 2 4F RT A16WE 1999110500259 19991105 00259 NM 1999 11 5 DL72S992388 1 19991007 A 5754 RIB BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 AT HMV, FOUND O/B RIB CRACKED ON NR 7 L/E SLAT AT ACTUATOR FITTING. REMOVED FASTENER AND DOUBLER, FABBED NEW DOUBLER PE R MM 57-54-0 FIG 804, AND INSTALLED. 2 L 7 3 4F A3WE 1999110500260 19991105 00260 NE 1999 11 5 DL72W992389 2 19991028 A 7310 O-RING BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT AP APPROACH 1 SO 27 292WA 22110 695302 NR 3 ENGINE FLAMED OUT ON APPROACH AT 6000 FEET. AT LEVEL OFF 6000 FEET DURING FINAL APPROACH SEGMENT NR 3 INSTRUMENTS INDICATED THE FOLLOWING FUEL FLOW 0 / 35 PERCENT N2 / EPR0 / N1 ZERO / NORMAL OIL PRESS, NORMAL OIL TEMP / THROTTLE MOVE MENT, NO EFFECT / NR 3 GEN LIGHT CAME ON APPROXIMENTLY 3-5 MINUTES AFTER INDICATIONS. TROUBLESHOT PER M/M, FOUND BAD O- RING ON FUEL CONTROL CONDENSATION TRAP BOWL. PERFORMED ENGINE RUN PER PREFLIGHT HANDBOOK, CHECKS OUT GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999110500261 19991105 00261 NM 1999 11 5 DL72S992390 1 19991028 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 543DA 22392 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPS CK OK. 2 L 7 3 4F A3WE 1999110500262 19991105 00262 NM 1999 11 5 DL72S992391 1 19991013 A 5520 WEB BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 DURING BUYBACK OF N/R 129, FOUND 1.5 INCH CRACK IN LT ELEVATOR I/B CLOSEOUT WEB AT ACCESS PLATE (MARKED). REPAIRED PER SRM 55-1-4 FIG 2. 2 L 7 3 4F A3WE 1999110500263 19991105 00263 NM 1999 11 5 DL72S992392 1 19991012 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 CORROSION AT FLOORBEAM STA 334 BL 0 TO LBL 46. REPAIRED PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1999110500264 19991105 00264 NM 1999 11 5 DLM88992393 1 19991029 A 5320 591214186 ANGLE DOUG MD88 MD88 3023688 NM BS 1474 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 949DL 49880 THE RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE WAS FOUND WITH A 1.5 CRACK ALONG THE I/B FASTENER ROW OF THE HOR IZONTAL FLANGE OF THE ANGLE. THE CRACKED AREA OF FLANGE WAS CUT AWAY AND REPAIRED WITH A STEEL REPAIR ANGLE PER ER/ A 368626-14, REV A. 2 L 7 2 4F RT A6WE 1999110500265 19991105 00265 WP 1999 11 5 DLL19992394 1 19991028 A 5320 1550830101 INTERCOSTAL LKHEED 1011 10113853 5265020 WP BS 1796 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 767DA 193H1209 THE L3 DOOR CUTOUT SURROUND STRUCTURE WAS FOUND WITH A TYPICAL CRACK IN THE BACK-UP INTERCOSTAL OF THE NR 2 DOOR ST OP ON THE FS 1796 DOOR CUTOUT FRAME. THE CRACK IS TYPICAL OF LAC S/B 93-53-270. THE CRACKED STRUCTURE WILL BE REPLACED PER THE REQUIREMENTS OF THE LAC S/B AND PER ER/A 368615-14. 2 L 7 3 4F A23WE 1999110500266 19991105 00266 NM 1999 11 5 DL72W992395 1 19991028 A 5312 BULKHEAD WEB BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 THE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH TYPICAL CRACK AT WL 178 AND LBL 8. THE CRACK IS TYPICAL OF BAC S/B 72 7-53-0175. THE CRACK WAS CUT OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER THE S/B AND ER/A 368608-14AD. TH E WEB WILL BE MODIFIED PER S/B REQUIREMENTS PRIOR TO 60K CYCLES. 2 L 7 3 4F A3WE 1999110500267 19991105 00267 NM 1999 11 5 DL73K992396 1 19991027 A 5313 6546877143 STRINGER BOEING 737 737232 1384475 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 THE STRINGER 18A WEB WAS FOUND WITH A CRACKED FASTENER HOLE AT FS 727 ON THE LT AND RT SIDES OF THE AIRCRAFT. THE CRACK S ARE TYPICAL OF THOSE NOTED IN BAC S/B 737-53-1066. THE CRACKS WERE REPAIRED WITH A NEW GUSSET CHANNEL SIMILAR TO THE S/B AND INSTALLED PER ER/A 368583-14. 2 L 7 2 4F RT A16WE 1999110500268 19991105 00268 NM 1999 11 5 DL72S992397 1 19991019 A 5720 BRACKET BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FOUND DURING MV2 CORROSION VISIT NRC 9 I/B AND O/B SLAT ACTUATOR ATTACH BRACKETS CRACKED AT NR 1 SLAT ACTUATOR. REPAIRE D PER M/M 57-20-21 PG 812. 2 L 7 3 4F A3WE 1999110500269 19991105 00269 NM 1999 11 5 DL72S992398 1 19991019 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FOUND DURING MV2 CORROSION VISIT NRC 8 SPAR STIFFENER CRACKED APPROX 1.25 INCH AT NR 2 SLAT O/B TRACK I/B STIFFENER. RE PLACED STIFFENER PER M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1999110500270 19991105 00270 NM 1999 11 5 DL72W992399 1 19991029 A 5320 WEB BOEING 727 727247 138408F NM BS 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 FOUND ON D-2 LETTER CK, .5 INCH CRACK ON LT LOWER TORQUE BOX LIGHTENING HOLE FWD END STA 1228. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999110500271 19991105 00271 NM 1999 11 5 DL72W992400 1 19991029 A 5330 SKIN BOEING 727 727247 138408F NM BS 1098 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 FOUND ON D-2 LETTER CK, 1 INCH CRACK LT SIDE OF STRINGER 1 STA 1098. REPAIRED PER SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1999110500272 19991105 00272 NM 1999 11 5 DL72S992402 1 19991029 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM ROW 2 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 404DA 21148 ROW 2 OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATT PACK, OPS CK OK. 2 L 7 3 4F A3WE 1999110500273 19991105 00273 NM 1999 11 5 DL76G992403 1 19991029 A 2913 PUMP BOEING 767 7673P6 1385105 NM LT HYD SYS FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 153DL 24985 LEFT HYD SYSTEM FLUID LOST AND SUBSEQUENT ADB FAILURE. REPLACED LT HYD PUMP, FLUSHED SYSTEM, CHANGED ALL ASSOCIATED FIL TERS. 2 L 7 2 4F RT A1NM 1999110500274 19991105 00274 WP 1999 11 5 DLL19992404 1 19991030 A 3350 LIGHT 5165741 LKHEED 1011 10113853 5265020 WP CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 753DA 10001 193W1189 ON L/O, FOUND L-2 EMERGENCY EXIT LIGHT AND L-2 EXTERIOR LIGHT INOP. 2 L 7 3 4F A23WE 1999110500275 19991105 00275 WP 1999 11 5 DLL10992405 1 19991031 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP 2L DOOR DISCHARGED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 735D 69459 193C1226 EMERGENCY BATTERY PACK ABOVE 2L DOOR FLIGHT ATTENDANT SEAT SMOKED. REPLACED BATTERY PACK, CHECKS GOOD. 2 L 7 3 4F A23WE 1999110500276 19991105 00276 NM 1999 11 5 DLM88992406 1 19991031 A 3246 WHEEL MD88M DOUG MD88 MD88 3023688 NM NR 3 MAIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 998DL DL1165A 53370 INSPECTED WHEELS FOR PASSENGER COMPLAINT OF FLAT TIRE. FOUND NR 3 MAIN WHEEL DAMAGED ON INSIDE. ALSO, RUBBING BRAKE. I NNER BEARING HUB FAILURE, AXLE HAD NO DAMAGE. REPLACED WHEEL AND BRAKE ASSY. 2 L 7 2 4F RT A6WE 1999110500277 19991105 00277 NM 1999 11 5 DL76S992407 1 19991030 A 5270 LIGHT BOEING 767 767332 1382001 NM 1R DOOR SHORTED A DALA O OTHER B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING TX TAXI/GRND HDL 1 SO 27 139DL 25984 INBOARD WRITE UP / ALL SLIDE LIGHTS INOP AFTER PUSHBACK. FOUND POPPED C/B. FOUND 1R DOOR CAUSING C/B T-35 (DOOR ARM WA RNING) TO POP. RESET C/B, SMELLED HEAVY ELECTICAL SMELL. MTC STILL IN WORK, FOUND LIGHT ASSY SHORTED AT 1R AND PSEU CA RD NR 6 FAULTY. REPLACED LIGHT ASSY AND CARD, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999110500278 19991105 00278 NE 1999 11 5 DL76L992408 2 19991031 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 182DN 22566 25987 724715 AT APPROX 160-170 KTS DURING TAKEOFF, RT ENG OVERTEMPED WITH ASSOCIATED VIBRATIONS. RT ENG SUBSEQUENTLY SHUTDOWN PER CH ECKLIST. LANDING WT APPROX 338K. TAKEOFF PWR WAS AT 35. FUEL DUMPING USED TO DECREASE LANDING WT. DUMPED APPROX 30K. MAINT IN PROGRESS, REPLACING ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999110500279 19991105 00279 NM 1999 11 5 DLM88992409 1 19991031 A 3350 P2070003001 FLASHLIGHT DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 988DL 53339 JUMPSEAT 2L FWD FLASHLIGHT SEAL MISSING/BROKEN. FOUND FLASHLIGHT NOT FLASHING. REPLACED FLASHLIGHT, CKS OK. 2 L 7 2 4F RT A6WE 1999110500280 19991105 00280 NE 1999 11 5 DL72L992410 2 19991031 A 7210 STUD BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MISSING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 508DA 50018 21310 700726 NR 1 ENG RAPID OIL LOSS, LOW OIL PRESS LT ILLUM AND QTY WENT TO ZERO. SHUTDOWN ENG PER POM. FOUND .25 INCH STUD MISSIN G FROM FRONT GEARBOX COVER. REINSTALLED STUD PER 727 M/M 72-61-02. 2 L 7 3 4F 4 F A3WE E2EA 1999110500281 19991105 00281 NM 1999 11 5 DLM88992411 1 19991031 A 2780 4952287505 SWITCH DOUG MD88 MD88 3023688 NM PEDESTAL INOP A DALA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 912DL DL89 49543 SLAT DISAGREE LIGHT FLICKERED DURING APPROACH THROUGH ALL FLAP SETTINGS. NO ROLLING TENDENCY. REPLACED FLAP/SLAT HAND LE POSITION SWITCH ASSY, ADJUSTED AND TESTED PER M/M 27-80-07-2. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1999110500282 19991105 00282 NM 1999 11 5 DL72S992413 1 19991031 A 2782 ACTUATOR 1U1110 BOEING 727 727232 1384082 NM NR 3 LE FLAP FAILED A DALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 SO 27 401DA 9717DFGKL 21145 NUMBER THREE LEADING EDGE FLAP INDICATION AND UNCOMMANDED ROLL. REPLACED NUMBER THREE LEADING EDGE FLAP ACTUATOR. 2 L 7 3 4F A3WE 1999110500283 19991105 00283 NE 1999 11 5 VNAA9910020 2 19991017 A 7320 3039242 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 430JS 10339 3044 DURING CLIMBOUT, THE FLIGHT CREW RECEIVED A RT ENGINE ELECTRONIC CONTROL UNIT FAIL MESSAGE. THE FLIGHT CREW RETURNED TO THE FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT NH SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 77-13-00. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500284 19991105 00284 EU 1999 11 5 RAIA9910039 1 19991029 A 7120 9505405 MOUNT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 552HK 41057 76083 STL- A/C VIBRATION JUST AFTER TAKEOFF. MAINTENANCE REPLACED RIGHT ENGINE REAR ENGINE MOUNT. 2 L 7 2 4T 4 T RT A41NM E18NE 1999110500285 19991105 00285 EU 1999 11 5 RAIA9910040 1 19991030 A 2150 5598C600 FLOW SELECTOR JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 550HK 41039 DCA- LEFT DUCT OVERTEMP LIGHT ON. MAINTENANCE REPLACED LEFT FLOW SELECTOR. 2 L 7 2 4T RT A41NM 1999110500286 19991105 00286 EU 1999 11 5 RAIA9910041 1 19991031 A 3320 5108WW BULB JETAIR JETSTM JETSTM4101 1500501 EU ROW 10BC FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 570HK 41089 JFK- OVERHEAD LIGHT AT 10 B & C APPEARS TO BE SHORTING OUT. MAINTENANCE REPLACED LIGHT BULB FOR SEAT 10 B & C. 2 L 7 2 4T RT A41NM 1999110500287 19991105 00287 WP 1999 11 5 TWAA9914801 1 19991021 A 5320 FORMER DOUG DC9 DC931 3022065 WP BS 937 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, THE AFT CARGO FORMER CAP ANCHOR NUT HOLE WAS CORRODED AT STA 937, LONGERON 28L. REMOVED AND R EPLACED FORMER CAP PER SRM 6-70-01. 2 L 7 2 4F A6WE 1999110500288 19991105 00288 WP 1999 11 5 TWAA9914802 1 19991023 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING CHECK-C MAINT, FOUND AT STA 996 THE END CAP FITTINGS AT LONGERON 23L, 24L, AND 25L WERE FOUND WITH CORROSION. R EMOVED AND REPLACED THE FITTINGS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1999110500289 19991105 00289 WP 1999 11 5 TWAA9914803 1 19991023 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING CHECK-C MAINT, FOUND SKIN PILLOWED/DENTED AND RIVETS POSSIBLY DISTRESSED ON LT FUSELAGE, NEAR THE PRESSURE DOME, FORWARD AND BELOW THE TR SELECTOR ACCESS. A SIX BY 8 INCH AREA. REPAIRED DAMAGED AREA PER ARA 13937. 2 L 7 2 4F A6WE 1999110500290 19991105 00290 EU 1999 11 5 JBXA9900110 1 19991102 A 2910 O RING FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE FAILED A JBXA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 108ML 11484 HYDRAULIC SYSTEM 1 LOW QUANTITY IN AIR. AIRCRAFT RETURNED TO RDU. FOUND SYSTEM NR 1 ENGINE NR 2 HYDRAULIC PUMP LEAKING AT OUTPUT LINE. QUICK DISCONNECT. REPLACED O-RING AND OPS CHECKED NR 1 SYSTEM HYDRAULIC PUMPS FOR ENGINE NR 1 AND NR 2. NO LEAKS FOUND IAW MM 29-11-01. 2 L 7 2 4F RT 1999110500291 19991105 00291 NM 1999 11 5 AWXA9900387 1 19991029 A 3350 831136 LIGHT BOEING 737 7373G7 1384595 NM ROW 13C INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 151AW 23219 EMERGENCY LIGHT ASSY AT 13C INOP. REPLACED EMERGENCY LT ASSY AT 13C, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1999110500292 19991105 00292 NM 1999 11 5 AWXA9900388 1 19991029 A 3397 BMS13131122 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 179AW 22646 EMERGENCY EXIT LT FORWARD OF L-1 DOOR INOP. REPAIRED BROKEN WIRE, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999110500293 19991105 00293 NM 1999 11 5 RAAA99B2056 1 19991029 A 3350 8621014 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 12ABC DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 EMERGENCY LIGHT AT ROW 12 A, B, C, WILL NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999110500294 19991105 00294 NM 1999 11 5 RAAA99B2057 1 19991029 A 3350 8621014 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 14ABC DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 EMERGENCY LIGHT AT ROW 14 ABC, WILL NOT TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999110500295 19991105 00295 NM 1999 11 5 RAAA99B2058 1 19991029 A 3350 8621014 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 14DEF DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 EMERGENCY LIGHT AT ROW 14 D, E, F, WILL NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999110500296 19991105 00296 NM 1999 11 5 RAAA99B2059 1 19991029 A 3350 873100212 LIGHT INTVLV 873100212 BOEING 727 72722C 138400F NM PAX DOORWAY INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AFT ENTRY EMERGENCY LIGHT WILL NOT TEST. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1999110500297 19991105 00297 NM 1999 11 5 RAAA99B2060 1 19991029 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 14 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 EMERGENCY LIGHT @ ROW 14 ( FLOOR PROXIMITY) WILL NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999110500298 19991105 00298 NM 1999 11 5 RAAA99B2061 1 19991101 A 3397 873100212 WIRE INTVLV 873100212 BOEING 727 72722C 138400F NM ROW 21 BROKEN A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 EMERGENCY LIGHT AT ROW 21 A, B, C, HAS BROKEN LENS AND WIRE DISCONNECTED FROM LIGHT. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1999110500299 19991105 00299 SO 1999 11 5 RAAA99E4075 1 19991030 A 3350 1000553 LIGHT GRIMES 1000553 LKHEED 188 188C 5262604 SO ROW 12 AB INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 EMERGENCY PULL DOWN LIGHT AT ROW 12 A & B, DID NOT TEST. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1999110500300 19991105 00300 SO 1999 11 5 RAAA99E4076 1 19991030 A 3350 1000553 LIGHT GRIMES 1000553 LKHEED 188 188C 5262604 SO COCKPIT INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 EMERGENCY PULL DOWN LIGHT AT FLIGHT STATION, DID NOT TEST. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1999110500301 19991105 00301 SO 1999 11 5 RAAA99E8056 1 19991029 A 3350 873100212 LIGHT INTVLV 873100212 LKHEED 188 188C 5262604 SO ROW 11AB INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY LIGHT @ ROW 11,A&B, FAILS SELF TEST. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1999110500302 19991105 00302 SO 1999 11 5 RAAA99E8057 1 19991029 A 3350 873100212 LIGHT INTVLV 873100212 LKHEED 188 188C 5262604 SO ROW 17AB INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY LIGHT AT ROW 17, A & B, FAILS SELF TEST. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1999110500303 19991105 00303 SO 1999 11 5 RAAA99E9031 1 19991030 A 3350 873100212 LIGHT INTVLV 873100212 LKHEED 188 188C 5262604 SO ROW 16 INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EMERGENCY LIGHT AT ROW 16 C, D, E, WILL NOT TEST. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1999110500304 19991105 00304 WP 1999 11 5 CALA9901439 1 19991031 A 3222 STRUT DOUG DC9 DC981 3022081 WP NOSE GEAR REQD SERVICE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 13881 48045 THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. QRH PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR STRUT AT 100 PSI. THE STRUT WAS SERVICED IAW MM 32-21-02. THE GEAR WAS SWUNG SEVERAL TIMES AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999110500305 19991105 00305 NM 1999 11 5 CALA9901440 1 19991027 A 5230 FRAME/BEAM BOEING 737 7373T0 1384582 NM FWD CARGO DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND A 1 INCH CRACK IN LOWER AFT FRAME AND A 2 INCH CRACK IN T-BEAM OF FORWARD CARGO DOOR LOWER FORWARD CORN ER. THE FRAME WAS REPLACED IAW SRM 51-10-02 AND 51-40-02. THE BEAM WAS REPAIRED IAW ECRA 5230-01491. 2 L 7 2 4F RT A16WE 1999110500306 19991105 00306 NM 1999 11 5 CALA9901441 1 19991027 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND FLOORBEAM CORRODED AT ATTACH HOLES, STA 328, RBL 13 TO RBL 49. REPAIRED FLOORBEAM IAW SRM 51-10-51, FI GURE 205. 2 L 7 2 4F RT A16WE 1999110500307 19991105 00307 NM 1999 11 5 CALA9901442 1 19991027 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, RBL 45 TO LBL 45. REPAIRED IAW ECRA 5310-03938. 2 L 7 2 4F RT A16WE 1999110500308 19991105 00308 NM 1999 11 5 CALA9901443 1 19991028 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 344-380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 344-380. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00-5 2. 2 L 7 2 4F RT A16WE 1999110500309 19991105 00309 WP 1999 11 5 CALA9901444 1 19991028 A 5754 STRIP DOUG DC10 DC1030 3023501 WP NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14079 46927 INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT O/B STRIP. PERFORMED REPAIR IAW SRM 57-10-00. 2 L 7 3 4F A22WE 1999110500310 19991105 00310 WP 1999 11 5 CALA9901445 1 19991029 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12510 47799 INSPECTION FOUND FUSELAGE SKIN DENTED AND SCRATCHED AT STA 229, STRINGER 18L. THE DAMAGED AREA WAS CUT OUT, A DOUBLER, FINGER DOUBLER, AND NEW SKIN WERE INSTALLED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1999110500311 19991105 00311 NM 1999 11 5 CALA9901446 1 19991029 A 5753 652163188 SKIN BOEING 727 727224 1384076 NM RT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND RIGHT I/B FOREFLAP O/B LEADING EDGE GOUGED. THE RIGHT I/B FOREFLAP WAS REMOVED AND REPLACED IAW MM 27- 51-1, PAGE 404 AND 406. 2 L 7 3 4F A3WE 1999110500312 19991105 00312 NM 1999 11 5 CALA9901447 1 19991029 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 45. A NEW FLOORBEAM WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999110500313 19991105 00313 NM 1999 11 5 CALA9901448 1 19991031 A 5320 FRAME BOEING 737 7373T0 1384582 NM R-1 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND A .5 INCH CRACK BETWEEN TWO FASTENERS OF FORWARD LOWER R-1 DOOR FRAME. A DOUBLER AND FILLERS WERE INST ALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 1999110500314 19991105 00314 NM 1999 11 5 CALA9901449 1 19991031 A 5240 65505734 GATE BOEING 737 7373T0 1384582 NM R-1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND R-1 DOOR LOWER GATE CORRODED AROUND STOPS. THE R-1 DOOR LOWER GATE ASSEMBLY WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1999110500315 19991105 00315 WP 1999 11 5 CALA9901450 1 19991101 A 5520 TIP DOUG DC10 DC1030 3023501 WP LT&RT ELEVATOR BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND THE LEFT AND RIGHT I/B ELEVATOR T/E TIPS BENT. THE BENT AREAS WERE TRIMMED OUT AND NEW EDGE PORTIONS W ERE INSTALLED IAW SRM 55-30-00, FIGURE 2 51-35-02, AND 51-31-01. 2 L 7 3 4F A22WE 1999110500316 19991105 00316 WP 1999 11 5 CALA9901451 1 19991101 A 5414 SKIN DOUG DC10 DC1030 3023501 WP NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON PRE-COOLER CUTOUT AT RT SIDE. THE CRACKED AREA WAS TRIMMED OUT AND REINFO RCED WITH A REPAIR ANGLE IAW ECRA 5450-01283. 2 L 7 3 4F A22WE 1999110500317 19991105 00317 NM 1999 11 5 CALA9901452 1 19991101 A 5755 SKIN BOEING 727 727224 1384076 NM NR 8 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1, PAGE 401 & 403. 2 L 7 3 4F A3WE 1999110500318 19991105 00318 EU 1999 11 5 9904413202 1 19991028 A 3260 TARGET AIRBUS 320 A320211 3930320 EU NLG OUT OF ADJUST A NWAA O OTHER N FALSE WARNING CR CRUISE 1 GL 01 302US 32 DURING CRUISE, RECEIVED L/G LGCIU 1 FAULT AND LGCIU 2 FAULT. ON APPROACH PERFORMED GRAVITY EXTENSION OF LANDING GEAR PE R COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR STRUT EXTENSION TARGET CLEARAN CES 24GA AND 25GA. LANDING GEAR FUNCTIONAL CHECKS NORMAL. 2 L 7 2 4F RT A28NM 1999110500319 19991105 00319 WP 1999 11 5 9904439138 1 19991025 A 3246 9560645 WHEEL DOUG DC9 DC915 3022036 WP NR 3 SEPERATED A NWAA O OTHER O OTHER LD LANDING 1 GL 01 9348 19648 115 45787 DURING LANDING, THE NR 3 MAIN WHEEL LIBERATED FROM THE AIRCRAFT. AIRCRAFT WAS TOWED TO GATE. MAINTENANCE REPLACED THE NR 3 MAIN WHEEL AND BRAKE ASSEMBLIES. ALSO, REPLACED THE NR 4 MAIN WHEEL AND BRAKE ASSEMBLIES AND RIGHT MAIN GEAR STRUT . REPAIRED RIGHT INBOARD FLAP FAIRING AND RIGHT ENGINE FAN BLADE DUE TO DAMAGE. 2 L 7 2 4F A6WE 1999110500320 19991105 00320 WP 1999 11 5 9904429911 1 19991028 A 4930 FUEL CONTROL GTCP8598DCA DOUG DC9 DC931 3022065 WP APU MALFUNCTIONED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 961N P28040DCA 47405 DURING CRUISE FLIGHT, CABIN AND FLIGHT CREW PERSONNEL SMELLED FUMES IN THE AIRCRAFT. CATPAIN AND FIRST OFFICER DONNED O XYGEN MASKS. AN UNEVENTFUL LANDING WAS MADE AT DESTINATION AIRPORT. MAINTENANCE FOUND THAT FUEL WAS BEING INGESTED INT O THE APU. SOURCE OF FUEL WAS FOUND TO BE A LEAK FROM APU FUEL CONTROL. REPLACED THE FUEL CONTROL. 2 L 7 2 4F A6WE 1999110500321 19991105 00321 NM 1999 11 5 99FDEA00457 1 19991101 A 5720 ARC0502506 BRACKET DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RT WING O/B TRAILING EDGE FLAP, AFT REMOVAL OF FWD FAIRING 635AL FOUND I/B HINGE BRACKET FWD O/B END CRACKED. *S/D* RE MOVED AND REPLACED PER MM 57-53-01 AND O/B FLAP ASSY REMOVED AND REPLACED PER MM 27-50-30-4. 2 L 7 3 4F RT A22WE 1999110500322 19991105 00322 NM 1999 11 5 102599 1 19991022 A 3411 PITOT SYS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT/RT COCKPIT MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 614UA 21875 CHRONIC PITOT-STATIC SYSTEM FAULTS. ALTIMETERS SPLIT. SPLIT IN INDICATIONS BECOME MORE APPARENT WITH INCREASING AIRSPE ED AND ALTITUDE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999110500323 19991105 00323 NM 1999 11 5 99UAL900419 1 19990829 A 3350 582233 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOP A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY EXIT LIGHTING WILL NOT TURN OFF IN BUSINESS SECTION. *S/D* REPLACED POWER SUPPLY M1553, OPS CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1999110500324 19991105 00324 NM 1999 11 5 99UAL900546 1 19991024 A 7930 BYPASS LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 WP 29 365UA 24534 FLIGHT CREW REPORTED, THE OIL FILTER BYPASS LIGHT ILLUMINATED ON THE NUMBER ONE ENGINE WHEN OIL PRESSURE AND TEMPERATURE ARE INDICATING NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999110500325 19991105 00325 NM 1999 11 5 99UAL900548 1 19991024 A 2530 94020147S2 CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY CORRODED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7251U 21398 AFT COFFEEMAKER CAUSED SMOKE, SMOKE STOPPED WHEN POT TURNED OFF. *S/D* SMOKE CAUSED BY CORRODED AND BURNED CONNECTOR O N AIRCRAFT SIDE. REPLACED CONNECTOR. THIS WAS AN ISOLATED INCIDENT. 2 L 7 3 4F 4 F A3WE E2EA 1999110500326 19991105 00326 NM 1999 11 5 99UAL900549 1 19991023 A 3350 3005931 LAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CARGO COMPT FAILED A UALA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 29 7252U 21399 EMERGENCY LIGHTS ACTIVATED ON LANDING WHEN AIRCRAFT WAS TOWED TO THE GATE. *S/D* OPERATIONALLY CHECKED OK EMERGENCY LI GHTS. ALL CHECKED GOOD EXCEPT FOR FORWARD LIGHT BULB ON AFT CARGO PIT DOOR. RELAMPED, OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1999110500327 19991105 00327 NM 1999 11 5 99UAL900550 1 19991023 A 2750 240863 MOTOR VICKERS, INC BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS LEAKING A UALA H DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 29 7252U 21399 SHORTLY AFTER DEPARTURE FROM COS, FLIGHT SUFFERED A COMPLETE LOSS OF SYSTEM A HYDRAULIC PRESSURE. FLIGHT CONTINUED TO D EN. DECLARED AMBER ALERT. LANDING WAS UNEVENTFUL, AIRCRAFT TOWED TO GATE. *S/D* REPLACED RIGHT FLAP DRIVE MOTOR. CH ECKED CASE DRAIN AND PRESSURE FILTERS PER MAINTENANCE MANUAL. FILTERS CLEAN, NO LEAKS NOTED. RAN FLAPS AND PRIMARY FLI GHT CONTROLS SEVERAL TIMES TO WORK AIR OUT OF SYSTEM. OPS CHECK OK. RAN ENGINES AND SERVICED HYDRAULIC SYSTEM. 2 L 7 3 4F 4 F A3WE E2EA 1999110500328 19991105 00328 EU 1999 11 5 99UAL900551 1 19991024 A 3243 C24703001 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PARKING BRAKE INTERMITTENT A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 422UA 503 ON ARRIVAL TO MEX, CAPTAIN SET PARKING BRAKE AND IT FAILED. AIRCRAFT ROLLED ABOUT 20 FEET BEFORE CAPTAIN WAS ABLE TO AP PLY BRAKES. AIRCRAFT CONTACTED JETWAY AT THE LEFT ENGINE COWL. *S/D* PERFORMED AN OPERATIONAL TEST OF THE PARKING BRA KE SYSTEM PER AMM TASK 32-45-00-710-001. FOUND PARKING BRAKE VALVE (72GG) TO BE INTERMITTENT. REPLACED VALVE AND OPS C HECK WAS NORMAL. TAXI TEST OF AIRCRAFT SHOWED BRAKE SYSTEM TO FUNCTION NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1999110500329 19991105 00329 NM 1999 11 5 99UAL900552 1 19991025 A 2621 80600031600U FIRE BOTTLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU BAY DISCHARGED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 316UA 23948 ON DESCENT, THE AUXILIARY POWER UNIT FIRE BOTTLE DISCHARGED WARNING LIGHT ILLUMINATED. *S/D* VISUAL INSPECTION NOTED T HE AUXILIARY POWER UNIT FIRE BOTTLE PRESSURE WAS AT APPROXIMATELY 250 PSI, THE THRESHOLD FOR LOW PRESSURE INDICATION. R EPLACED THE FIRE BOTTLE, AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999110500330 19991105 00330 NM 1999 11 5 99UAL900553 1 19991025 A 7930 BY PASS LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE ILLUNINATED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 365UA 24534 FLIGHT CREW REPORTED THAT THE OIL FILTER BYPASS LIGHT ILLUMINATED ON THE NUMBER ONE ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999110500331 20001010 00331 NM 2000 10 10 99UAL900554 1 19991025 A 7722 SOCKET BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 EGT IND LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7284U 21562 700141 NR 1 ENGINE REACHED 640 DEGREES EGT ON CLIMBOUT (30 SECONDS OVERTEMP) APPROXIMATELY 1.8 EPR - N1 99 PERCENT HAD TO PULL THROTTLE BACK 4 INCHES TO MAINTAIN TEMPERATURE IN NORMAL RANGE. RETURNED TO DEN. *S/D* THE EGT EXCEEDANCE WAS AN INDI CATION PROBLEM. TROUBLESHOOTING REVEALED FAULTY RETENTION AT SOCKET D374J POS L WHICH IS PART OF THE NR 1 EGT INDICATIO N SYSTEM. THE SOCKET WAS REPLACED, THE SYSTEM CALIBRATED AND THE EGT INDICATOR ALSO REPLACED AS A PRECAUTION. GROUND E NGINE RUNS CONFIRMED THE FIX. 2 L 7 3 4F 4 F A3WE E2EA 1999110500332 20001010 00332 EU 2000 10 10 99UAL900555 1 19991025 A 5610 WINDSHIELD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALA B EMER. DESCENT O OTHER CR CRUISE 1 WP 29 420UA 489 FLT EXPERIENCED A CRACKED OUTER WINDSHIELD ON THE CAPT SIDE AT FL390. FLT DESCENDED TO FL220 PER THE FLIGHT MANUAL. *S /D* WATER INGRESS THROUGH THE WEATHER SEAL REACHED THE WINDSHIELD''S BUSBAR, RESULTING IN ELECTRICAL ARCING AND SUBSEQU ENT CRACKING OF THE WINDSHIELD OUTER FACE PLY. CRACKING OF THE OUTER FACE PLY DOES NOT AFFECT STRUCTURAL INTEGRITY, HOW EVER THE WINDSHIELD WAS REPLACED PRIOR TO THE AIRCRAFT''S NEXT FLIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 1999110500333 19991105 00333 NM 1999 11 5 99UAL900556 1 19991024 A 5411 RIB BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 4 STRUT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 158UA 21054 DURING INSPECTION OF THE OUTBOARD STRUTS RIBS (OUTBOARD AND INBOARD) AT NAC STA 236.5, THE OUTBOARD RIB ON STRUT NR 4 WA S FOUND CRACKED UNDERNEATH THE 65B90150-3 BRACKET. THE APPROXIMATE LENGTH OF THE CRACK IS 6 INCHES. ALSO, THE BRACKET WAS FOUND CRACKED. (P/N 65B90308-3) RIB. ALSO, ON THE NR 1 AND NR 4 STRUTS INBOARD RIBS, THE BRACKETS WERE FOUND CRACK ED. 2 L 7 4 4F 4 F A20WE E20EA 1999110500334 19991105 00334 NM 1999 11 5 99UAL900557 1 19991025 A 3010 1552121321464 BLEED VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ANTI-ICE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7284U 21562 AFTER TAKEOFF, NR 1 ANTI-ICE BLEED VALVE WOULD NOT CLOSE. RETURNED TO DEN. *S/D* WING ANTI-ICE HIGH PRESSURE SHUT OFF VALVE (P/N 1552121) AND WING ANTI-ICE VALVE (P/N 32146451). REPLACED WING ANTI-ICE HP SOV AND WING ANTI-ICE VALVE PER MM, OPS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999110500335 20001010 00335 NE 2000 10 10 99UAL900558 2 19991021 A 7240 616318 DUCT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7445U 21899 700340 NR 3 ENGINE CASE CRACKED. REFERENCE NR 6 FAN DISCHARGE COMBUSTION SECTION OUTER DUCT HAS A DENT APPROXIMATELY .5 INCH D EEP AND TWO CRACKS 2 INCHES AND 2.5 INCHES LONG. *S/D* ENGINE CASE WAS CRACKED/DENTED DUE TO IMPACT WITH GROUND EQUIP MENT. THE CASE WAS NDT INSPECTED TO DETERMINE THE TRUE LENGTH OF THE CRACKS AND SUBSEQUENTLY PATCHED. A LONG TERM DEFE RRAL WAS CREATED TO CHECK THE INTEGRITY OF THE PATCH RIVETS AT AT C CHECK AND REPLACE THEM AT HMV. 2 L 7 3 4F 4 F A3WE E2EA 1999110500336 19991105 00336 NM 1999 11 5 99UAL900559 1 19991028 A 2730 ELEVATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WING FLUTTERED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 575UA 26689 FLIGHT DIVERTED TO ORD UNDER AMBER ALERT DUE TO A CONTROL FLUTTER PROBLEM. CONCURRENT REPORTING OF UNITED'S FINDINGS TO FAA IS ONGOING THROUGH UNITED'S FLIGHT SAFETY DEPARTMENT. ACTIONS ACCOMPLISHED PRIOR TO SUCCESSFUL TEST FLIGHT INCLUDE REPLACEMENT OF NUMEROUS ELEVATOR HINGE BEARINGS, ELEVATOR REACTION LINK BEARINGS, REACTION LINKS, AND REPLACEMENT OF EL EVATOR PCA'S. RE-RIGGING OF THE ELEVATOR SYSTEM AND RE-TENSION OF THE ELEVATOR CONTROL CABLES WERE ALSO ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 1999110500337 19991105 00337 1999 11 5 MWEA754 4 19991101 A 3425 2588369901 ADI DOUG DC9 DC932 3022066 WP LT COCKPIT INOP A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 501ME 47132 CAPTIANS HORIZON FAILED ON CLIMBOUT. MTC REMOVED AND REPLACED CAPTIANS ADI AND INSTRUMENT AMP. 2 L 7 2 4F A6WE 1999110500338 19991105 00338 1999 11 5 MWEA755 4 19991101 A 3421 258733511 VERT GYRO DOUG DC9 DC932 3022066 WP LT COCKPIT INOP A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 501ME 47132 CAPTAIN'S HORIZON FAILIED ON CLIMBOUT. MTC NR 1 VERTICAL GYRO. 2 L 7 2 4F A6WE 1999110500339 19991105 00339 WP 1999 11 5 MWEA756 1 19991102 A 3397 60030451 WIRE DOUG DC9 DC914 3022034 WP CABIN BROKEN A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 600ME 45725 FORWARD CABIN OVERHEAD EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN SELECTED. MTC REPLACED TERMINAL END ON BROKEN GROUND WI RE FROM BATTERY PACK. 2 L 7 2 4F A6WE 1999110500340 19991105 00340 WP 1999 11 5 MWEA757 1 19991102 A 5330 591142269 SKIN DOUG DC9 DC981 3022081 WP BS 1155 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 FOUND PREVIOUS REPAIR STATION 1155 BETWEEN LONGERON 7 LEFT AND 8 LEFT UNACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLE D PROPER REPAIR DOUBLER AND FILLER. 2 L 7 2 4F A6WE 1999110500341 19991105 00341 WP 1999 11 5 MWEA758 1 19991102 A 5311 991187723 FRAME DOUG DC9 DC981 3022081 WP BS 1474 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 FOUND PREVIOUS REPAIR ON FRAME STATION 1474 AT LONGERON 15 LEFT TO 16 LEFT UNACCEPTABLE. MAINTENANCE FABRICATED AND INS TALLED PROPER REPAIR. 2 L 7 2 4F A6WE 1999110500342 19991105 00342 WP 1999 11 5 MWEA759 1 19991102 A 5311 9912246197 FRAME DOUG DC9 DC981 3022081 WP BS 1380 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS REPAIR DOUBLER ON FRAME STATION 1380 BETWEEN LONGERON 4 LEFT AND 5 LEFT WAS CHAFED. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999110500343 19991105 00343 NM 1999 11 5 SCNA99740 1 19991018 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 385 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT INTERIOR FUSELAGE STA 385 BL 18R FLOOR SUPPORT. RE MOVED CORROSION IAW B727 511006. REMOVED FLOOR SUPPORT FROM BS 385 RBL 18 PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 15064417 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER MM 513002. 2 L 7 3 4F A3WE 1999110500344 19991105 00344 NM 1999 11 5 SCNA99741 1 19991018 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 420 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT INTERIOR FUSELAGE STA 420 BL 36R FLOOR SUPPORT. RE MOVED CORROSION IAW B727 511006. REMOVED FLOOR SUPPORT FROM BS 385 RBL 18 PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 15064417 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER MM 513002. 2 L 7 3 4F A3WE 1999110500345 19991105 00345 NM 1999 11 5 SCNA99742 1 19991015 A 5320 BRACKET BOEING 727 727259 138408J NM BS 1183 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT STA 1183 LBL 1783 WL 208 LOWER ATTACH BRACKET FOR V ERTICAL BEAM. REMOVED CORROSION IAW SRM 511006. REMOVED BRACKET IAW SRM 513002. FABRICATED NEW BRACKET PER SAMPLE FRO M 7075 T6 .032. TREATED AND PRIMED IAW SRM 51006, MM 512002. INSTALLED IAW SRM 513002. 2 L 7 3 4F A3WE 1999110500346 19991105 00346 NM 1999 11 5 DHL99706001 1 19991101 A 7933 10200002 TEMP BULB BOEING 727 72722C 138400F NM NR 1 ENGINE FAILED A DHLA A E UNSCHED LANDING ENGINE SHUTDOWN M N OVER TEMP FALSE WARNING CR CRUISE 1 SO 01 706DH 19192 NR 1 ENGINE OIL TEMP ROSE IN FLIGHT TO 131 REGARDLESS OF THRUST SETTING. ENGINE OIL TEMP WOULD NOT DECREASE. SHUT DOWN NR 1 ENGINE AFTER 15 MIN, TOTAL TIME TEMP AT 125, 25 MIN. REPLACED OIL TEMP BULB, REPLACED MAIN OIL SCREEN AND DRAINED AND REPLACED OIL. RAN ENG, OIL TEMP OK. 2 L 7 3 4F A3WE 1999110500347 19991105 00347 SO 1999 11 5 SWIA971585 1 19991015 A 2750 RETRACT MECH EMB 120 EMB120RT SO PWA 118 PW118 NE RT TE FLAPS DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 593SW 120191 FLAP DISAGREEMENT ON TAKEOFF WOULD NOT CLEAR. RETURNED TO RDM. CYCLED FLAPS MULTIPLE TIMES, COULD NOT DUPLICATE PROBLE M. INSPECTED AND CLEANED FLAP TRACKS AND ROLLERS. FOUND SOME OLD STICKY HYDRAULIC FLUID ON RIGHT INBOARD FLAP TRACK. S EALED RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG. REPLACED FCU IAW MM 27-00-00, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999110500348 19991105 00348 SO 1999 11 5 SWIA971586 1 19991017 A 2910 FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE BLUE HYD STS DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 290SW 120317 HYDRAULIC FILTER LIGHT ILLUMINATED AFTER TAKEOFF BLUE SYSTEM. RETURNED TO SFO. RESET BLUE HYDRAULIC RETURN IMPENDING B YPASS PIN AND REPLACED ENGINE AND ELECTRIC RETURN FILTERS. OPS CHECKS GOOD WITH NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999110500349 19991105 00349 EA 1999 11 5 SWIA971587 1 19991027 A 4990 OIL SYS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE APU REQD SERVICE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 EN ROUTE TO HLN CLIMBING THROUGH 28,000 FT, RECEIVED AN APU LOW OIL PRESSURE LIGHT ON EICAS ONE. RETURNED TO SLC. SERV ICED APU OIL TO CORRECT LEVEL. INSPECTED APU AND OBSERVED NO LEAKS OR OTHER ABNORMALITIES. OPS CHECKS GOOD AT THIS TIM E. 2 L 7 2 4F 4 F RT A21EA E15NE 1999110500350 19991105 00350 NE 1999 11 5 VNAA9910021 2 19991031 A 7321 8111803004 EEC DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 07 430JS 9656 3044 DURING CLIMB FLIGHT 4158 EXPERIENCED VARYING POWER LOSS IN THE RIGHT HAND ENGINE. THE FLIGHT CREW RETURNED TO THE FIELD . THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED THE INLET BLEED VALVE SERVO SCR EEN IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-31-04 AND REPLACED RIGHT HAND ELECTRONIC ENGINE CONTROL IN ACCORDAN CE WITH DORNIER MAINTENANCE MANUAL 73-21-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT RELEASED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500351 19991105 00351 NM 1999 11 5 VNAA9910022 1 19991031 A 3240 BRAKE SYS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT REQD SERVICE A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 426JS 3038 DURING TAXI, THE FLIGHT CREW REPORTED THE FIRST OFFICERS' LEFT HAND BRAKE PEDAL HAD NO RESPONSE WHEN ACTIVATED. AIRCRAF T WAS FERRIED TO PIT. MAINTENANCE INSPECTED AND BLED THE FIRST OFFICERS' BRAKE SYSTEMS IN ACCORDANCE WITH DORNIER MAINT ENANCE MANUAL 32-42-00. FUNCTION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500352 19991105 00352 NM 1999 11 5 VNAA9910023 1 19991031 A 2432 DTSP400L BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT DISCHARGED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 461PS 9007 72 3075 DURING THE APPROACH TO PIT, THE FLIGHT CREW EXPERIENCED A NR 1 BATTERY INDICATION WITH AN OVERHEAT INDICATION STAYING ON AFTER THE TEST BUTTON WAS RELEASED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO OVERHEAT CONDITION TO EXIST AND FE RRIED THE AIRCRAFT TO CAK. MAINTENANCE THEN REPLACED THE NUMBER ONE BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANU AL 24-32-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500353 19991105 00353 EU 1999 11 5 RAIA9911001 1 19991101 A 7931 1241013 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 926AE 1408 1408 926 4709- LAX RIGHT OIL PRESSURE WENT TO ZERO. MAINTENANCE REPLACED OIL PRESS TRANSDUCER FOR RIGHT ENGINE. 2 L 7 2 4T RT A56EU 1999110500354 19991105 00354 NM 1999 11 5 USAA990885 1 19990927 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 342US 37150 23511 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES BS 328, LBL 20, TO RBL 50 FLOORBEAM. CORROS ION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999110500355 19991105 00355 NM 1999 11 5 USAA990869 1 19990817 A 5320 BEAM BOEING 757 757225 1384959 NM BS 1661 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 42362 22210 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION VARIOUS SPOTS AT STATION 1661, RBL 3, LBL 45 UPPER CHORD BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-251-03. INSTALLED BEAM PER SRM 53-00-51 PAGE 219. (M) 2 L 7 2 4F RT A2NM 1999110500356 19991105 00356 NM 1999 11 5 USAA990868 1 19990817 A 5320 BEAM BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 42362 22210 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION VARIOUS SPOTS AT STATION 1640, RBL 10, LBL 40 UPPER SURFACE BE AM. CORROSION LEVEL 2. INSTALLED NEW T-CAP PER TR 53-15-01 AND EA 65254. (M) 2 L 7 2 4F RT A2NM 1999110500357 19991105 00357 NM 1999 11 5 USAA990872 1 19990817 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1560 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 42362 22210 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK ON FRAME AT STATION 1560, LBL 25. FABRICATED STRINGER, D OUBLER, TIE CLIP PER EA 65314. (M) 2 L 7 2 4F RT A2NM 1999110500358 19991105 00358 NM 1999 11 5 USAA990858 1 19990817 A 5320 SUPPORT BOEING 757 757225 1384959 NM BS 1510 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 42362 22210 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION UNDER NUTPLATES ON CARGO FLOOR SUPPORT STATIN 1510, RBL 11. C ORROSION LEVEL 1. INSTALLED SPLICE AND FILLER PER TR 53-10-01 REV A. (M) 2 L 7 2 4F RT A2NM 1999110500359 19991105 00359 NM 1999 11 5 USAA990870 1 19990817 A 5320 HAT CHANNEL BOEING 757 757225 1384959 NM BS 1380-1440 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 42362 22210 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND 1.5 INCH AREA OF CORROSION AT STATION 1380-1440, RBL 21.5 HAT CHANNEL. C ORROSION LEVEL 2. FABRICATED REPLACEMENT WEB PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1999110500360 19991105 00360 NM 1999 11 5 USAA990831 1 19990817 A 5330 SKIN BOEING 757 757225 1384959 NM BS 535 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 42362 22210 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH AT SKIN LOWER LOBE AT BL 0 STATION 535, CORROSION LEVEL 1. BLENDED PER SRM 51-10-00 AND 53-00-01. (M) 2 L 7 2 4F RT A2NM 1999110500361 19991105 00361 NM 1999 11 5 USAA990956 1 19990910 A 5311 146N10175 FRAME BOEING 757 757225 1384959 NM BS 1520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 1520, STRINGER 27L FRAME. INSTALLED DOUBLER PER EA 65446A. (M) 2 L 7 2 4F RT A2NM 1999110500362 19991105 00362 NM 1999 11 5 USAA990958 1 19990910 A 5320 TIE CLIP BOEING 757 757225 1384959 NM BS 1520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STATION 1520, STRINGER 26L TIE CLIP. REPAIRED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A2NM 1999110500363 19991105 00363 NM 1999 11 5 USAA990976 1 19990910 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 1460 TRANS ANGLE ATTACH POINT FRAME. INSTAL LED DOUBLER PER EA 65552. (M) 2 L 7 2 4F RT A2NM 1999110500364 19991105 00364 NM 1999 11 5 USAA990957 1 19990910 A 5311 146N1013 FRAME BOEING 757 757225 1384959 NM BS 1440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT BS 1440 AT 27.75, LBL 5 INCH ABOVE OUTBOARD OF STRINGE R 27L FRAME. INSTALLED SPLICE DOUBLER PER EA 65442B. (M) 2 L 7 2 4F RT A2NM 1999110500365 19991105 00365 NM 1999 11 5 USAA990949 1 19990910 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1400 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 3 INCH BY 2 INCH AT BS 1400 FORWARD SIDE OF FRAM E AT STRINGER 28L. CORROSION LEVEL 2. REPLACED STRAP PER BOEING DRAWING 146N3305. (M) 2 L 7 2 4F RT A2NM 1999110500366 19991105 00366 NM 1999 11 5 USAA990954 1 19990910 A 5313 STRINGER BOEING 757 757225 1384959 NM BS 1330 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON TOP OF CARGO FLOOR STRINGER STATION 1330 AT LBBL 15.5. COR ROSION LEVEL 2. INSTALLED REPAIR ANGLE PER TR 53-10-01. (M) 2 L 7 2 4F RT A2NM 1999110500367 19991105 00367 NM 1999 11 5 USAA990955 1 19990910 A 5313 STRINGER BOEING 757 757225 1384959 NM BS 1330 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON TOP OF CARGO FLOOR STRINGER STATION 1330 AT LBBL 3.0. CORR OSION LEVEL 2. INSTALLED REPAIR ANGLE PER TR 53-10-01. (M) 2 L 7 2 4F RT A2NM 1999110500368 19991105 00368 NM 1999 11 5 USAA990950 1 19990910 A 5330 SKIN BOEING 757 757225 1384959 NM R4 DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 46058 22203 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN DOOR RELEASE LEVER CLOSE OUT PANEL R4 FORWARD CUTOUT A T LOWER INBOARD CORNER FOR UPPER TORQUE TUBE WEB. INSTALLED DOUBLER PER EA 65505 AND SRM 51-40-02 AND SRM 51-20-05. (M ) 2 L 7 2 4F RT A2NM 1999110500369 19991105 00369 NE 1999 11 5 USAA109901 2 19991002 A 7314 3782017 PUMP BOEING 727 727254 138408L NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J X WARNING INDICATION ENGINE FLAMEOUT TO TAKEOFF 1 EA 19 913TS 20250 649456 FLT 6470 - DCA-LGA - ON TAKEOFF, DURING GEAR RETRACTION, NR 3 ENGINE FAILED. EMERGENCY DECLARED, RETURNED TO DCA. REPL ACED NR 3 ENGINE DRIVEN FUEL PUMP. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999110500370 19991105 00370 NM 1999 11 5 USAA990992 1 19990916 A 5240 SKIN BOEING 737 737201 1384454 NM SERV DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 51315 22018 TPA - DURING A CX-CHECK VISUAL INSPECTION, FOUND A .250 INCH LONG CRACK AT AFT SERVICE DOOR BOTTOM HINGE AFT CORNER DOOR SKIN. INSTALLED REPAIR DOUBLER PER TR 52-40-03A AND EA 65097. (M) 2 L 7 2 4F A16WE 1999110500371 19991105 00371 NM 1999 11 5 USAA991015 1 19990922 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 817 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 42468 23131 TPA - DURING A CX-6 CHEK VISUAL INSPECTION, FOUND A .25 INCH CRACK ON DOOR CUTOUT SKIN FOR HANDLE STATION 817, WL 178. I NSTALLED DOUBLER PER SRM 52-00-03 FIG 2. (M) 2 L 7 2 4F A16WE 1999110500372 19991105 00372 NM 1999 11 5 USAASB99238 1 19990927 A 5350 FAIRING BOEING 737 737301 1384611 NM WING/FUSELAGE MISSING A USAA A UNSCHED LANDING E D VIBRATION/BUFFET INFLIGHT SEPARATION CL CLIMB 1 EA 19 339US 23236 BOS - FLT 8053 - FLIGHT RETURNED TO FIELD AT BOS DUE TO A LOUD HIGH PITCH HUMMING NOISE AND VIBRATION AROUND CABIN WINDO W AT SEAT ROW 9ABC. VIBRATION AND HUMMING NOISE DECREASED UNDER 10,000 FT AND 220 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A SIX INCH SECTION OF THE LEFT WING-TO-BODY FAIRING AT SEAT ROW 9ABC MISSING SEALANT. RES EALED WING-TO-BODY FAIRING. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1999110500373 19991105 00373 NM 1999 11 5 P2EA99292 1 19990825 A 5720 BEAM BOEING 737 737247 138448D NM WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SPAN WISE BEAM NR 1 CRACKED AT STRINGER 9C BL 0. REPAIRED IAW COOPESA EO COO-3-57-520-99. (M) 2 L 7 2 4F A16WE 1999110500374 19991105 00374 NM 1999 11 5 P2EA99291 1 19990823 A 5315 FLOORBEAM BOEING 737 737247 138448D NM BS 578 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FLOORBEAM WEB CRACKED AT BS 578 BETWEEN RBL 55 AND RBL 55 AT WL 206. REPAIRED IAW SERVICE BULLETIN 737-53-1061 RE VISION 4. (M) 2 L 7 2 4F A16WE 1999110500375 19991105 00375 NM 1999 11 5 P2EA99290 1 19990820 A 5330 SKIN BOEING 737 737247 138448D NM BS 847-907 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - CORROSION, SKIN AND TEAR STRAP BOND SEPARATED, AT BS 847 TO BS 907 AND BETWEEN 20R AND 25R. REPAIRED SKIN FROM BS 855 TO BS 867 AND BETWEEN STRINGER 23R AND 25R IAW SRM 53-30-03 FIG 17. BONDED TEAR STRAP AS REQUIRED IAW SRM 53-30-03 . ALL CORROSION WITHIN LIMITS REMOVED AND TREATED IAW SRM 51-10-06. (M) 2 L 7 2 4F A16WE 1999110500376 19991105 00376 NM 1999 11 5 P2EA99293 1 19990924 A 5330 SKIN BOEING 737 737247 138448D NM BS 887 MISREPAIRED A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN REPAIR NOT IAW SRM AT BS 887 BETWEEN 21R AND 22R. REPAIRED IAW SRM 53-30-03 FIG 7. (M) 2 L 7 2 4F A16WE 1999110500377 19991105 00377 NM 1999 11 5 P2EA99294 1 19990924 A 5330 SKIN BOEING 737 737247 138448D NM BS 870 MISREPAIRED A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN REPAIR NOT IAW SRM AND BS 870 BETWEEN 20R AND 21R. REPAIRED IAW SRM 53-30-03 FIG 4. (M) 2 L 7 2 4F A16WE 1999110500378 19991105 00378 NM 1999 11 5 P2EA99301 1 19990924 A 5330 SKIN BOEING 737 737247 138448D NM BS 847 MISREPAIRED A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 204AU 19603 SJO - SKIN REPAIR NOT PER SRM AT BS 847 BETWEEN STRINGER 22R AND 24R. REPAIRED IAW COOPESA EO COO-3-53-551-99. (M) 2 L 7 2 4F A16WE 1999110500379 19991105 00379 NM 1999 11 5 P2EA99299 1 19990820 A 5311 FRAME BOEING 737 737247 138448D NM BS 947.5 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FRAME CRACKED AT BS 947.5 BETWEEN STRINGER 20L AND 21L. REPAIRED IAW SRM 51-10-01 PAGE 5. (M) 2 L 7 2 4F A16WE 1999110500380 19991105 00380 NM 1999 11 5 P2EA99300 1 19990824 A 5313 STRINGER BOEING 737 737247 138448D NM BS 787 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - STRINGER 16R CRACKED AT BS 787. REPAIRED IAW SRM 53-10-03 FIG 3. (M) 2 L 7 2 4F A16WE 1999110500381 19991105 00381 NM 1999 11 5 P2EA99302 1 19991008 A 2780 RETRACT MECH BOEING 737 737244 138448U NM NR 1 LE SLAT MALFUNCTIONED A P2EA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 05 620PC 19708 MCI - FLT 588 - NR 1 LEADING EDGE SLAT TRANSIT LIGHT ON. VISUALLY CONFIRMED INBOARD END OF SLAT NOT FULLY EXTENDED WITH SLATS IN MID EXTEND POSITION. SLAT EXTENDED NORMAL WITH SLATS SELECTED TO FULL EXTEND POSITION. LUBED NR 1 LEADING ED GE SLAT. OPS CHECKS GOOD PER MM 27-88-11. (M) 2 L 7 2 4F A16WE 1999110500382 19991105 00382 WP 1999 11 5 USAA991088 1 19991008 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP BS 636 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND 1 INCH BY 1 INCH CORROSION ON AND AROUND FASTENER HOLES, QTY 4, AT FLOOR SUPPORT STATION 63 6 BETWEEN LONGS 28L AND 29R. CORROSION TASK NR C51-53300, CORROSION LEVEL 2. REPLACED FLOOR SUPPORT PER EA 53012. (M) 2 L 7 2 4F A6WE 1999110500383 19991105 00383 WP 1999 11 5 USAA991086 1 19991014 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 542 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 48811 48092 PIT - DURING Q5 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 541, LONG 3 RIGHT. INSTALLED NEW SECTION PER SRM 53-02 , FIG 18. (M) 2 L 7 2 4F A6WE 1999110500384 19991105 00384 NM 1999 11 5 USAA990970 1 19990904 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 39386 23318 PHL - DURING RON, FOUND 1.5 INCH CRACK ON SKIN AT STATION 747 STRINGER 25R. REPAIRED WITH EXTERNAL DOUBLER PER SRM 53-0 0-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999110500385 19991105 00385 NM 1999 11 5 USAA109903 1 19991014 A 3260 656021132 ACCESSORY UNIT BOEING 727 727254 138408L NM E/E COMPT INOPERATIVE A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 916TS 20437 FLT 6050 - LGA-BOS - HAD TO USE GEAR TRIGGER TO RAISE GEAR. OIL COOLER CSD RETURNED TO NORMAL WHEN FLAPS RAISED FROM 5- 2 DEGREES. AURAL WARNING SOUNDED. HAD TO PULL C/B TO SILENCE HORN. ALL OTHER INDICATIONS NORMAL. T/S TO LANDING GEAR ACCESSORY UNIT, REPLACED SAME. CHECKS OK PER MM 32-09-121. LEVER LATCH. SOLENOID OPS CHECKS OK PER MM 32-31-12. (M) 2 L 7 3 4F A3WE 1999110500386 19991105 00386 NM 1999 11 5 USAA991042 1 19991008 A 5320 BEAM BOEING 757 7572B7 1384964 NM BS 160 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 623AU 19669 27244 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT 1640 UPPER CHORD RBL 36 BEAM. CORROSION L EVEL 1. CORROSION TASK NR C53-251-03. INSTALLED STRAPS AND ANGLES PER EA 65808, TR 53-15-02 AND SRM 53-00-51 FIG 203. (M) 2 L 7 2 4F RT A2NM 1999110500387 19991105 00387 NM 1999 11 5 USAA991083 1 19991011 A 5230 SKIN BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 46269 22753 TPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK LOWER AFT WEB OF CARGO DOOR STRUCTURE 6 INCHES FORWARD O F LOWER AFT STOP. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999110500388 19991105 00388 NM 1999 11 5 USAA991048 1 19991007 A 5330 SKIN BOEING 737 737201 1384454 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 45191 22796 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SKIN AFT ENTRY DOOR LOWER DOOR HINGE CUTOUT. INSTA LLED DOUBLER PER TR 53-30-10 REV B AND SRM 53-30-3 FIG 34. (M) 2 L 7 2 4F A16WE 1999110500389 19991105 00389 NM 1999 11 5 USAA991073 1 19991011 A 5330 SKIN BOEING 737 7372B7 1384560 NM L2 DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 286AU 42413 23133 TPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SKIN L-2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORN ER. INSTALLED DOUBLER PER REPAIR DOCUMENT 53-30-3 FIG 34 AND TR 53-30-10 REV A. (M) 2 L 7 2 4F A16WE 1999110500390 19991105 00390 NM 1999 11 5 USAA991072 1 19991011 A 5330 SKIN BOEING 737 7372B7 1384560 NM R2 DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 286AU 42413 23133 TPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN SKIN R-2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNE R. INSTALLED DOUBLER PER REPAIR DOCUMENT 53-30-3 FIG 33. (M) 2 L 7 2 4F A16WE 1999110500391 19991105 00391 NM 1999 11 5 GAIA99145 1 19990928 A 2611 302842 SMOKE DETECTOR BOEING 727 727251 138408H NM CARGO COMPT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278US 21157 DURING ROUTINE MAINTENANCE IN TOL, IT WAS DISCOVERED THAT THE NR 3 AND NR 5 SMOKE DETECTORS FAILED TO TEST. REMOVED AND REPLACED THE NR 3 AND NR 5 SMOKE DETECTORS. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500392 19991105 00392 NM 1999 11 5 GAIA99146 1 19990928 A 2611 302842 SMOKE DETECTOR BOEING 727 727251 138408H NM CARGO COMPT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 279US 21158 DURING ROUTINE MAINTENANCE AT TOL IT WAS DISCOVERED, THAT THE NR 2, NR 4, NR 5, AND NR 6 SMOKE DETECTORS WOULD NOT TEST. REMOVED AND REPLACED THE NR 2, NR 4, NR 5 AND NR 6 SMOKE DETECTORS. OPERATIONALLY CHECKS NORMAL. THE AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500393 19991105 00393 NM 1999 11 5 GAIA99156 1 19991014 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1090 MISDRILLED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 6806 19481 'NO FLIGHT', FOUND DURING C-CHECK AT AAR IN OKC. INSPECTION FOUND FRAME WITH MISDRILLED HOLES AT BS 1090, STRINGER 27R. REPAIRED BS 1090 FRAME IAW FLT VEHICLES, INC DRAWING 53-99447-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500394 19991105 00394 NM 1999 11 5 GAIA99157 1 19991014 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1110 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6806 19481 'NO FLIGHT', FOUND DURING C-CHECK AT AAR IN OKC. INSPECTION FOUND CORROSION NEXT TO EXISTING REPAIR AT BS 1110, FLOORBE AM, UPPER TEE CHORD AFT FLANGE. REPAIRED BS 1110 FLOORBEAM UPPER CHORD IAW FLT VEHICLES, INC DRAWING 53-99432-1. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500395 19991105 00395 NM 1999 11 5 GAIA99158 1 19991014 A 5320 BEAM BOEING 727 727223 1384074 NM BS 857.4 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6806 19481 'NO FLIGHT', FOUND DURING C-CHECK AT AAR IN OKC. INSPECTION FOUND 3 FT CRACK ON SEAT TRACK SUPPORT BEAM, LBL 45 AT BS 8 57.4. REPAIRED SEAT TRACK SUPPORT BEAM, LBL 45, AT BS 857.4, IAW FLT VEHICLES, INC DRAWING 53-99432-2. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500396 19991105 00396 NM 1999 11 5 GAIA99159 1 19991014 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1166 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6806 19481 'NO FLIGHT', FOUND DURING C-CHECK AT AAR IN OKC. CORROSION WAS FOUND ON FLOORBEAM LOWER CHORD FORWARD FLANGE AT BS 1166 , LBL 25. REPAIRED FLOORBEAM LOWER CHORD FORWARD FLANGE AT BS 1166, LBL 25, IAW FLT VEHICLES, INC DRAWING 53-99432-3. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500397 19991105 00397 NM 1999 11 5 GAIA99160 1 19991014 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 950 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6806 19481 'NO FLIGHT', FOUND DURING C-CHECK AT AAR IN OKC. CORROSION WAS FOUND BETWEEN RBL 24.5 AND RBL 45.5 AT BS 950, FLOORBEAM UPPER TEE CHORD HORIZONTAL FLANGE. REPAIRED FLOORBEAM UPPER TEE CHORD HORIZONTAL FLANGE BETWEEN RBL 24.5 AND RBL 45.5 AT BS 950, IAW FLT VEHICLES, INC DRAWING 53-99432-4. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500398 19991105 00398 NM 1999 11 5 GAIA99161 1 19991014 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 OUT OF POSITION A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6806 19481 'NO FLIGHT' FOUND DURING C-CHECK AT AAR IN OKC. INTERFERENCE FOUND BETWEEN EXISTING CHANNEL AND THE SEAT TRACK SCREW AT LBL 24.5 BS 1130. NOTCHED OUT UPPER EDGE OF CHANNEL AND SHIM, IAW FLT VEHICLES, INC DRAWING 53-99432-5. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500399 19991105 00399 SO 1999 11 5 ASOA99119 1 19991013 A 5320 12046158601 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORROSION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 227AS 120023 DURING C-CHECK, FOUND LEFT 3RD AFT BUTTSTRAP CORRODED. MAINTENANCE REMOVED AND REPLACED LEFT BUTTSTRAP IAW EMB SRM 51-2 5-00, 51-40-06, 51-40-02, 51-40-01 AND CPM 51-21-04. (M) 2 L 7 2 4T RT A31SO 1999110500400 19991105 00400 SO 1999 11 5 ASOA99118 1 19991013 A 5347 12029490003 SEAT TRACK EMB 120 EMB120RT SO FUSELAGE CORROSION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 227AS 120023 DURING C-CHECK, FOUND LEFT FORWARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED LEFT FORWARD SEAT TRACK IAW EM B 120 SRM 51-40-03. (M) 2 L 7 2 4T RT A31SO 1999110500401 19991105 00401 SO 1999 11 5 ASOA99117 1 19991013 A 5320 12027888003 BUTTSTRAP EMB 120 EMB120RT SO BS 5740-9964 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 227AS 120023 DURING C-CHECK, FOUND LEFT NR 2 BUTTSTRAP HAS CORROSION AT STATIONS APPROX 5740.0 TO 9964.5. MAINTENANCE REMOVED AND RE PLACED BUTTSTRAP. (M) 2 L 7 2 4T RT A31SO 1999110500402 19991105 00402 SO 1999 11 5 ASOA99116 1 19991013 A 5400 12037517002 STIFFENER EMB 120 EMB120RT SO NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 227AS 120023 DURING C-CHECK, FOUND RIGHT NACELLE AFT OUTBOARD STIFFENER IS CRACKED. MAINTENANCE REMOVED AND REPLACED RIGHT NACELLE S TIFFENER IAW EMB120 SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 1999110500403 19991105 00403 SO 1999 11 5 ASOA99115 1 19991013 A 5414 PANEL EMB 120 EMB120RT SO NACELLE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 227AS 120023 DURING C-CHECK, FOUND THE PANELS 121 DB AND 131 BB ARE CORRODED. MAINTENANCE REMOVED AND REPLACED PANELS 121 DB AND 131 BB IAW EMB 120 MM 34-42-02. LEAK CHECK GOOD. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1999110500404 19991105 00404 SO 1999 11 5 ASOA99114 1 19991008 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 239AS 120057 DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999110500405 19991105 00405 SO 1999 11 5 ASOA99113 1 19991008 A 2150 12039804001 MOUNT EMB 120 EMB120RT SO RT PACK FAILED A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 243AS 120072 FLT 4038 - SMOKE DETECTED IN CABIN DURING TAXI. AIRCRAFT SAFELY RETURNED TO THE GATE. MAINTENANCE PERFORMED GROUND OPE RATIONAL CHECK AND DETERMINED THE PROBLEM TO BE THE RIGHT PACK. MAINTENANCE REPLACED THE RIGHT PACK AND GROUND COOLING FAN. FURTHER INSPECTION SHOWED THE FEEDER PROTECTION RELAY MOUNT BURNED. (M) 2 L 7 2 4T RT A31SO 1999110500406 19991105 00406 SO 1999 11 5 ASOA99112 1 19991008 A 2160 9799901 VALVE EMB 120 EMB120RT SO CABIN INOPERATIVE A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 243AS 120072 CREW DETECTED SMOKE IN CABIN. AIRCRAFT SAFELY RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE TEMPERATURE C ONTROL VALVE. ENGINE WAS THEN RAN. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999110500407 19991105 00407 SO 1999 11 5 ASOA99111 1 19991007 A 2120 AIR DIST EMB 120 EMB120RT SO CABIN SMOKE A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 243AS 120072 CREW REPORTS SMOKE IN CABIN DURING TAXI. MAINTENANCE PERFORMED OPERATIONAL CHECK ON BOTH PACKS WITH BOTH ENGINES RUNNIN G APPROXIMATELY FORTY MINUTES. NO FAILURES OR SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999110500408 19991105 00408 NM 1999 11 5 BJNA991001 1 19991008 A 3350 582214 BATTERY PACK BOEING 737 737282 13844AT NM LT EMER EXIT DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 789TM 23046 LEFT EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE, INTERIOR. REMOVED AND REPLACED LEFT EMERGENCY OVERWING INTERIOR BATTER Y PACK, IAW BMM 33-51-01, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1999110500409 19991105 00409 NE 1999 11 5 BJNA991002 2 19991012 A 7250 TURBINE SECTION BOEING 737 737282 13844AT NM PWA JT8 JT8D17A 52049 NE ENGINE FAILED A BJNA C E ABORTED TAKEOFF ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 11 233TM 23043 709440 FLT 233, A REPOSITION FLIGHT, FROM KTVL TO KSFO, STARTUP, TAXI WERE ACCOMP W/O INCIDENT. AFTER BEING CLEARED FOR T/O, P OWER WAS ADVANCED TO T/O EPR OF 2.18. APPROX 2 TO 5 SECONDS AFTER BRAKE RELEASE THE CREW OBSERVED A LOUD BANG COMING FR OM THE REAR OF THE A/C. THE CREW FIRST THOUGHT IT WAS A MAIN TIRE BLOWOUT. THE CREW IMMEDIATELY RETRACED THE ENGINES T O IDLE. THE A/C WAS ONLY MOVING ABOUT 5 MPH. THE CREW OBSERVED EGT AT APPROX 650 DEGREES CENTAGRADE. ENGINE SHUT DOWN WAS ACCOMP AS PER THE 'ENGINE FIRE AND SEVERE DAMAGE OR SEPARATION' CHECKLIST. AFTER COMPLETION OF CHECKLIST THE CREW TAXIED TO THE HARDSTAND WITH EQUIP STANDING BY. NO FURTHER PROBLEMS. EXAMINATION OF ENGINE REVEILED A CONTAINED TURBIN 2 L 7 2 4F 4 F RT A16WE E2EA 1999110500410 19991105 00410 WP 1999 11 5 AALA996005 1 19990922 A 3830 11201005 TANK DOUG DC9 DC983 3022083 WP FWD LAV CRACKED A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 882RA 49949 LAS - AFTER TAKEOFF, INCURRED MULITPLE ELECT MALFUNCTIONS. RETURNED IN IMC FOR OVERWEIGHT LANDING. LAV LEAK FORWARD LA V FLUID LEAKING INTO E/E. CLEANED EXCESS FLUID IN E/E FOUND LAV TANK CRACKED. FWD LAV ALREADY ON DMI. REF DMI NR 1867 2. ACCOMP RTS CU BOTH SIDES. REPLACED NR 1 AND NR 2 ENG GCUS AND BUS CONTROL PANEL RAN ENGINES ELECT SYSTEM. INST AND WARN LIGHTS GROUND ON GOOD. NO OVERWEIGHT LANDING INSPECTION REQUIRED PER MM 05-51-04 PAGE NR 609. A/C REQUIRES A FUN CTIONAL CHECK FLT. FUNCTIONAL CHECK FLT REQUIRED BECAUSE OF MULTIPLE ELECTRICAL MALFUNCTIONS. A/C HAS BEEN INSPECTED A ND NO KNOWN CONDITIONS EXISTS THAT WOULD MAKE THIS A/C UNSAFE FOR A FUNCTIONAL CHECK FLT. ACCOMP INSPECTION OF A/C. NO 2 L 7 2 4F RT A6WE 1999110500411 19991105 00411 NM 1999 11 5 USAASB99249 1 19991015 A 2910 HYDRAUIC LINE BOEING 737 7372B7 1384560 NM LT MLG FAILED A USAA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 19 275AU 22887 BOS - FLT 2674 - FLT WAS ON 4 MILE FINAL INTO BOS WHEN COMPLETE LOSS OF SYSTEM 'A' HYDRAULICS OCCURRED AFTER GEAR WAS SE LECTED DOWN. CAPT DECLARED AN EMERGENCY AND ACCOMPLISHED GO-AROUND TO COMPLETE CHECKLIST. CABIN WAS PREPPED FOR AN EME RGENCY LANDING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE LANDING GEAR WAS PINNED AND THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED BOTH HYDRAULIC LINES TO THE LEFT MAIN LANDING GEAR RETRACT CYLINDER. DUE TO HYD RAULIC LOSS, MAINTEANCE ALSO REMOVED AND REPLACED BOTH ENGINE DRIVEN HYDRAULIC PUMPS AND FILTERS. SERVICED HYDRAULIC SY STEM. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999110500412 19991105 00412 CE 1999 11 5 99ZZZM733 1 19991014 A 3242 30204A BRAKE BEECH 1900 1900D 1154162 CE LT MLG LEAKING A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 831CA 240 UE20 NR 2 BRAKE SEEPING HYD FLUID. REPLACED NR 2 BRAKE ASSEMBLY IAW CLEVELAND MAINTENANCE MANUAL. (M) 2 L 7 2 4T RT A24CE 1999110500413 19991105 00413 WP 1999 11 5 HALA9900190 1 19990630 A 5753 SKIN DOUG DC9 DC951 3022051 WP RT TE FLAP CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 661HA 47796 MAE - RT WING T/E FLAP INBOARD END OUTER SKIN HAS CORROSION ON ENTIRE AREA AFT OF MOVEABLE VANE. REMOVED SKIN AND DOUBL ER AND REPLACED IAW 51-30-2 AND 51-10-4 AND EA 9-5750-19-A0460. (M) 2 L 7 2 4F RT A6WE 1999110500414 19991105 00414 WP 1999 11 5 HALA9900191 1 19990630 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 964 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 661HA 47796 AFT CARGO LONGERON 26L IS CRACKED AT STATION 964. REMOVED AND INSTALLED REPAIR TO LONGERON 26L IAW SRM 51-30-2 AND 51-3 0-5 AND EA 9-5314-19-A0469. (M) 2 L 7 2 4F RT A6WE 1999110500415 19991105 00415 WP 1999 11 5 HALA9900192 1 19990630 A 5753 PANEL DOUG DC9 DC951 3022051 WP LT TE FLAP CORRODED A HALA O OTHER O OTHER IN INSP/MAINT 1 WP 13 661HA 47796 MAE - LEFT WING TE FLAP LOWER SIDE AT PANEL 1523A, SKIN AND RIB ARE CORRODED. REMOVED AND REPLACED RIB, ANGLE, AND SKIN IAW SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 1999110500416 19991105 00416 WP 1999 11 5 HALA9900193 1 19990701 A 5320 SPLICE DOUG DC9 DC951 3022051 WP BS 1258 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 661HA 47796 MAE - FUSELAGE SKIN PRODUCTION SPLICE IS CRACKED JUST BELOW LONGERON 17R BETWEEN FS 1247 AND FS 1258. TRIM OUT OF PRODU CTION SPLICE BETWEEN LONGERON 17R AND 16R AND INSTALLED SPLICE DOUBLER PER EA 9-5333-19-A0455. (M) 2 L 7 2 4F RT A6WE 1999110500417 19991105 00417 WP 1999 11 5 HALA9900194 1 19990702 A 5620 WINDOW DOUG DC9 DC951 3022051 WP CABIN CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 661HA 47796 MAE - CABIN WINDOW NR 26 LEFT INTERNAL DOUBLER TOP FORWARD EDGE IS CRACKED AT STATION 693 LONGERON 12L. REPAIRED WINDOW RING PAN IAW EA 9-5310-19-A0458 AND SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 1999110500418 19991105 00418 WP 1999 11 5 HALA9900196 1 19990927 A 2460 BUS CONTROL DOUG DC10 DC1010 3022110 WP NR 2 GENERATOR FAILED A HALA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 125AA 46525 SEA - FLT 21 - NR 2 GEN OFF LIGHT ON. ISSUED MEL 24-01 AUTH NR 9-194C-B. DURING OVERNIGHT MAINTENANCE RREMOVED AND REP LACED BUS CONTROL UNIT CHECKS OK. REMOVED PLACARD CLEARED MIC SHEET. (M) 2 L 7 3 4F A22WE 1999110500419 19991105 00419 WP 1999 11 5 HALA9900195 1 19990924 A 3230 COTTER KEY DOUG DC9 DC951 3022051 WP NLG OUT OF POSITION A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 661HA 47796 FLT 113 - HNL - ON APPROACH TO LIH, WHEN GEAR HANDLE PLACED DOWN, BOTH MAINS CAME DOWN. NOSE GEAR DID NOT COME DOWN. F OLLOWED SOP. RETURNED HNL. GEAR CAME DOWN 3 GREEN. INSPECTED NOSE GEAR COND AND SECURITY CHECK GOOD WIRING CHECK GOOD . REPLACED L/G PROX CTL BITE CHECK GOOD, SERVICED NOSE STRUT PER MM 32-21-2. REPLACED SCHRADER VLV. REPLACED NOSE GEA R BUNGEE CYL PER MM 32-32-07 CONDITION SAME. FOUND COTTER KEY WEDGED IN BUNGEE CYL CUTOUT REPOSITIONED COTTER KEY. GEA R SWING OK. (M) 2 L 7 2 4F RT A6WE 1999110500420 19991105 00420 WP 1999 11 5 HALA9900199 1 19991014 A 3241 39249 VALVES DOUG DC9 DC951 3022051 WP ANTI-SKID SYSTEM INOPERATIVE A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 420EA 47689 HNL - LEFT OUTBOARD TIRE BLEW WHILE TURNING OFF RUNWAY. POSSIBLE ANTI-SKID FAILURE. DAMAGE TO FLAP ARTICULATING ELBOW AND FLYING GEAR DOOR. REPLACED NR 1 AND NR 2 MAIN TIRES. CDL FOR FLY DOOR AND MEL FOR ANTI-SKID FERRIED PLANE W/GEAR D OWN TO HNL. ON ARRIVAL AT HNL, REPLACED NR 1 ANTI-SKID TRANSDUCER, ANTI-SKID CONTROL BOX AND ALL 4 DUAL ANTI-SKID CONTR OL VALVES. ANTI-SKID TEST CHECKS OK. REPAIRED FLY DOOR, GEAR SWING GOOD. (M) 2 L 7 2 4F RT A6WE 1999110500421 19991105 00421 EU 1999 11 5 PLGA990923A 1 19990923 A 7712 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU RT TQ IND TRIPPED A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NE 05 365BE 340B299 LGA - FLT 4579 - DURING TAKEOFF ROLL OF FLIGHT 4579, LGA-SYR, THE RIGHT TORQUE GAUGE WOULD NOT COME UP. TAKEOFF WAS ABO RTED. MAINTENANCE PULLED AND RESET THE RT TORQUE INDICATION CIRCUIT BREAKER AND OPERATIONALLY CHECKED THE SYSTEM GOOD. (M) 2 L 7 2 4T RT A52EU 1999110500422 19991105 00422 EU 1999 11 5 PLGA991006 1 19991006 A 3020 6124300 DUCT SAAB SF340 340B 7860101 EU LEFT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 358BE 275 340B279 BOS-SYR - FLT 4776 - CREW NOTED THAT THE LEFT INTAKEO LIGHT ILLUMINATED WHEN SYSTEM WAS SELECTED ON. ATTEMPTS FAILED IN TRYING TO RESET THE SYSTEM PER THE CHECKLIST. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE DUCT PARTICLE SEPARATOR IN THE LEFT INTAKE SYSTEM. LEFT INTAKE HEAT SYSTEM WAS OPERATIONALLY CHECKED GOOD AND A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999110500423 19991105 00423 EU 1999 11 5 PLGA990928 1 19990928 A 2150 7769105 ACM SAAB SF340 SF340A 7850100 EU RIGHT FAILED A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 05 744BA 860514 340A105 BOS-PHL - FLT 4773 - DURING CLIMB-OUT, CREW NOTED A BURNING SMELL IN THE COCKPIT. THEY SHUTDOWN THE RIGHT BLEED SYSTEM AND THE SMELL WENT AWAY. A/C DIVERTED BACK TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT ACM AND PERFORMED ALL REQUIRED CHECKS SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999110500424 19991105 00424 CE 1999 11 5 PLGA990922 1 19990922 A 2161 7546911 SWITCH CESSNA 340 340A 2076405 CE LT BLEED SYSTEM FAILED A PLGA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 NE 05 339BE 340A044 BOS-YHZ - FLT 4693 - CREW NOTED LEFT OVERTEMP LIGHT HAD ILLUMINATED. CREW FOLLOWED CHECKLIST AND SHUT OFF THELEFT BLEED . AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT DUCT OVERTEMP SWITCH AND OPERATI ONALLY CHECKED THE SYSTEM GOOD. (M) 1 L 7 2 3O 3A25 1999110500425 19991105 00425 CE 1999 11 5 PLGA990923 1 19990923 A 3260 MS213212 SWITCH CESSNA 340 340A 2076405 CE RT MLG FAILED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 339BE 340A044 PQI-BOS - FLT 4680 - CREW NOTED THAT THE INTRANSIT LIGHT IN THE GEAR HANDLE STAYED ILLUMINATED EVEN THROUGH THE GEAR APP EARED TO BE UP AND LOCKED. CREW FOLLOWED THEIR CHECKLIST AND RETURNED TO PQI. AIRCRAFT LANDED WITHOUT INCIDENT. CONTR ACT MAINTENANCE WAS DISPATCHED AND MEL'D THE GEAR DOWN. AIRCRAFT REPOSITIONED TO ALB WHERE MAINTENANCE REPLACED THE RT UPLOCK SWITCH. ALL REQUIRED CHECKS WERE DONE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 3O 3A25 1999110500426 19991105 00426 NE 1999 11 5 99ZZZM734 2 19991007 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D1A 30020 NE NR 1 FAILED A RYNA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 CE 07 571SC 46645 451573 FLT 102 - LAX - NR 1 ENGINE EXHAUST GAS TEMPERATURE CAUTION LIGHT CAME ON EARLY ON CLIMB-OUT, NR 1 THRUST HAD TO BE REDU CED TO MAINTAIN EXHAUST GAS TEMPERATURE LIMITS. REPLACED NR 1 ENGINE DUE TO BOROSCOPE DAMAGE FOUND. (M) 2 L 7 3 4F 4 F A22WE E23EA 1999110500427 19991105 00427 NM 1999 11 5 EISA99188 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 700 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND CLIP CRACKED AT FS 700 STRINGER 20L. FABRICATED NEW CLIP PE R SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999110500428 19991105 00428 NM 1999 11 5 99ZZZM735 1 19991016 A 3610 CLAMP BOEING 727 72782C 1384026 NM LOWER AFT BODY LOOSE A RYNA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 528PC 19597 FLT 707 - DEN-IND - LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT OF DEN WITH WING AND ENGINE ANTI-ICE ON. FOUND LOOSE CLAMP ON OVERHEAT LOOP, RESECURED CLAMP, ALL OPERATIONS NORMAL. (M) 2 L 7 3 4F A3WE 1999110500429 19991105 00429 NM 1999 11 5 99ZZZM736 1 19990914 A 2612 18252800 FIRE LOOP BOEING 727 72777C 1380420 NM NR 3 ENGINE RECONFIGURED A RYNA K NONE N FALSE WARNING CR CRUISE 1 CE 07 526PC 20370 FLT 712 - IND - NR 3 ENGINE FIRE DETECTOR CIRCUIT GROUND LIGHT ON IN FLIGHT. RECONFIGURED LOOP, SYSTEM CHECKS NORMAL, N R 3 ENGINE FIRE DETECTION CIRCUIT. (M) 2 L 7 3 4F A3WE 1999110500430 19991105 00430 NM 1999 11 5 99ZZZM737 1 19990929 A 2612 18252800 FIRE LOOP BOEING 727 72777C 1380420 NM NR 3 ENGINE OUT OF POSITION A RYNA K NONE N FALSE WARNING CR CRUISE 1 CE 07 526PC 20370 FLT 710 - IND - NR 3 ENGINE FIRE DETECTOR CIRCUIT LIGHT ILLUMINATED. REPOSITIONED NR 3 ENGINE FIRE DETECTION LOOP. (M) 2 L 7 3 4F A3WE 1999110500431 19991105 00431 NM 1999 11 5 99ZZZM738 1 19991009 A 2613 356644400 OVERHEAT LIGHT BOEING 727 72777C 1380420 NM NR 3 STRUT ILLUMINATED A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 526PC 20370 FLT 611 - IND-EWR - NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FIGHT WITH ENGINE AND WING ANTI-ICE ON. TURNED OFF RIGHT WING ANTI-ICE VALVE AND NR 3 ENGINE STRUT OVERHEAT LIGHT REMAINS OUT FOR REMAINDER OF FLIGHT. TROUBLESHOT WITH SU PPLIED AIR AND WITH ENGINE RUNNING, WAS UNABLE TO DETECT OR DUPLICATE DISCREPANCY, NO AIR/PNEUMATIC LEAKS FOUND NEAR NR 3 STRUT. (M) 2 L 7 3 4F A3WE 1999110500434 19991105 00434 NM 1999 11 5 99ZZZM741 1 19990804 A 2611 302842 SMOKE DETECTOR BOEING 727 727222 1384073 NM CARGO COMP LOOSE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 7635U 19908 FLT 307 - JFK - NR 5 CARGO COMPARTMENT SMOKE DETECTOR FAILS TO TEST. FOUND SOCKET LOOSE ON TEST BULB, RE-SECURED SOCKET OPERATIONAL CHECKS NORMAL. (M) 2 L 7 3 4F A3WE 1999110500435 19991105 00435 NM 1999 11 5 99ZZZM742 1 19990819 A 2611 355 BULB BOEING 727 72721 1384003 NM SMOKE DETECTOR BURNED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 357QS 19259 FLT 701 - IND- NR 1 SMOKE DETECTOR WON'T SELF TEST. RELAMPED TEST BULBS. (M) 2 L 7 3 4F A3WE 1999110500436 19991105 00436 EU 1999 11 5 UF6A990910 1 19990921 A 5320 12D11186 INTERCOSTAL BAG ATP ATP EU STATION 289-308 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL BETWEEN STATION 289AS AND 308AS HAS EXCESSIVE CORROSION. MAINTENANCE FABRICATED INTERCOSTAL AND INSTA LLED. ALL WORK WAS DONE IAW BAE ATP SRM 51-40-03 AND 51-50-02. (M) 2 L 7 2 4T RT A27NM 1999110500437 19991105 00437 EU 1999 11 5 UF6A990819 1 19990823 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 317 2028 FORWARD EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REPLACED THE POWER SUPPLY. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500438 19991105 00438 NM 1999 11 5 P2EA99304 1 19991011 A 3244 314396 TIRE BOEING 737 737230 NM RT MLG FLAT A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 123NJ 22121 MCI - FLT 584 - CREW REPORTED RIGHT OUTBOARD MAIN TIRE IS FLAT. REPLACED NR 4 MAIN TIRE ASSY PER MM 32-45-11. REPLACED NR 3 MAIN TIRE ASSY PER MM 32-45-11. DEFERRED ANTI-SKID SYSTEM PER MEL 32-2 CI NR M123629 ASSIGNED BY MX CONTROL. (M) 2 L 7 2 4F RT A16WE 1999110500439 19991105 00439 1999 11 5 MASA99159 4 19990924 A 2210 26ET1T SWITCH BEECH 1900 1900D 1154162 CE YAW DAMPER MALFUNCTIONED A MASA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 135YV UE135 FLT 5347 - BOS-HYA - ON TAXI OUT, THE CREW HEAD A POPPING NOSE COMING FROM THE PEDESTAL. THE RUDDER BOOST YAW DAMP C/B POPPED WHEN THIS HAPPENED AND THIS CAUSED THERE TO BE SPARKS IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE AND MAIN TEANCE WAS CALLED OUT TO INSPECT FOR ANY DAMAGE. THERE WAS NO DAMAGE NOTED AND THE YAW DAMP RUDDER BOOST SYSTEM WAS DEA CTIVATED AND DEFERRED. THE FOLLOWING EVENING THE A/C WAS ROUTED TO REDDING MX WHERE THE YAW DAMP SWITCH WAS REMOVED AND REPLACED USING EO B1900D-27-0007. (M) 2 L 7 2 4T RT A24CE 1999110500440 19991105 00440 EA 1999 11 5 MASA99161 1 19991013 A 3350 GE1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7219 FLT 5799 - DCA-HSV - WHEN THE CREW WAS PERFORMING THEIR STANDARD PREFLIGHT CHECK THEY NOTED A CABIN EMERGENCY LIGHT IN T HE CEILING WAS INOPERATIVE. MAINTENANCE WAS CALLED OUT AND REMOVED AND REPLACED THE EMERGENCY LIGHT IN THE CEILING. OP S CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999110500441 19991105 00441 NM 1999 11 5 NOCA0999 1 19991002 A 3350 BULB BOEING 757 75728A 1384976 NM ROW 12 ABC FAILED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 DURING INSPECTION, FOUND E-PATH FLOOR LIGHT AT SEAT 12 ABC INOP. RELAMPED E-PATH LIGHT AT SEAT 12 ABC. OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A2NM 1999110500442 19991105 00442 NM 1999 11 5 USAASB99229 1 19990915 A 2750 MS9391130ZE DRIVE MOTOR BOEING 737 7372Q9 138448M NM TE FLAPS FAILED A USAA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 19 231US 52000 21976 MIA - FLT 2739 - CAPT REPORTED HE WAS EIGHT MILES ON FINAL APPROACH AND HAD JUST SET THE FLAPS TO A SETTING OF 1 DEGREE WHEN THE 'A' SYSTEM HYDRAULICS FAILED. CAPT PULLED OFF APPROACH, DECLARED AN EMERGENCY AND ACCOMPLISHED CHECKLIST FOR ' A' SYSTEM HYDRAULIC FAILURE. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT MIA AND WAS TOWED TO THE GATE. MAINTENANCE REMO VED AND REPLACED THE TRAILING EDGE FLAP DRIVE HYDRAULIC MOTOR. SERVICED HYDRAULICS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999110500443 19991105 00443 NM 1999 11 5 USAASB99244 1 19991008 A 5210 MECHANISM BOEING 737 7373B7 1384580 NM PAX DOOR LACK OF LUBE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 374US 22953 PHL - FLT 1908 - DURING CLIMB-OUT FROM PHL, CREW NOTICED AN AIR LEAK FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CLEANED AND LUBED THE FORW ARD MAIN ENTRY DOOR ROLLERS. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999110500444 19991105 00444 NM 1999 11 5 USAASB99242 1 19991008 A 3260 65446915 MODULAR ASSEMBLY BOEING 737 737401 1384701 NM LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 420US 23987 EWR - FLT 1056 - AFTER GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. WITH HANDLE IN 'OFF' POSI TION, THE LEFT MAIN GEAR EXTENDED DOWN AND LOCKED. CREW RECYCLED GEAR AND SAME PROBLEM OCURRED. FLIGHT RETURNED TO FIE LD AT EWR AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT MA IN LANDING GEAR MODULAR ASSEMBLY PER MM 32-32-61. OPS CHECK AND LEAK CHECK GOOD ON GROUND. (M) 2 L 7 2 4F RT A16WE 1999110500445 19991105 00445 NM 1999 11 5 USAASB99234 1 19990920 A 2120 658098724 DUCT BOEING 737 737301 1384611 NM COCKPIT FAILED A USAA A B UNSCHED LANDING EMER. DESCENT O OTHER CL CLIMB 1 EA 19 334US 23231 PIT - FLT 1840 - AFTER PASSING 7,000 FT, A VERY LOUD BANG OCCURRED FROM BEHIND THE INSTRUMENT PANEL. HIGH PRESSURE AIR RUSHED OUT AND BLEW INSULATION THROUGH OUT THE COCKPIT. COCKPIT WAS VERY LOUD. AUTOPILOT OPERATION WAS AFFECTED AND H AD TO BE TAKEN OFF LINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURT HER INCIDENT. MAINTENANCE VISUALLY INSPECTED THE COCKPIT EXTERIOR FOR DAMAGE. NO DAMAGE WAS FOUND. PERFORMED PITOT CH ECK OF PITOT SYSTEM. ALL CHECKS NORMAL. PRESSURIZED AIRCRAFT TO 3.5 PSI. NO LEAKS NOTED. INSPECTED AREA BEHIND INSTR UMENT PANEL AND FOUND THE COCKPIT AIR CONDITIONING SPLITTER DUCT CRACKED. REMOVED AND REPLACED DUCT ASSEMBLY. LEAK CHE 2 L 7 2 4F RT A16WE 1999110500446 19991105 00446 NM 1999 11 5 USAASB99245 1 19991009 A 2420 6130200502 HARNESS BOEING 737 737301 1384611 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 351US 23554 ORD - FLT 1817 - EN ROUTE FROM PHL/MSP, CAPTAIN REPORTED THE NR 2 AND NR 3 TRANSFORMER RECTIFIERS HAD TRIPPED AND THE C APTAIN'S WINDOW OVERHEAT LIGHT WAS ON. CAPTAIN RESET T/R'S, BUT THEY BOTH TRIPPED AGAIN. LOSS OF ELECTRIC TRIM, AUTOSP EED BRAKE AND RIGHT GENERATOR WAS NOTED. AN ELECTRICAL SMELL IN THE COCKPIT WAS ALSO NOTED. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE GENERATO R FEEDER HARNESS. RAN ENGINE. OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4F RT A16WE 1999110500447 19991105 00447 NM 1999 11 5 USAASB99243 1 19991002 A 3397 WIRE BOEING 737 737201 1384454 NM ROW 12C BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 234US 22274 TPA - MAINTENANCE FOUND THE AISEL EMERGENCY LIGHT AT SEAT ROW 12C INOPERATIVE. MAINTENANCE REPAIRED TWO BROKEN WIRES AT SEAT ROW 12C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999110500448 19991105 00448 WP 1999 11 5 USAAD99147 1 19991008 A 3350 408822101 BATTERY DOUG DC9 DC931 3022065 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 973VJ 47099 IND - THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD CABIN EMERGENCY LIGHT BATTE RIES. (M) 2 L 7 2 4F A6WE 1999110500449 19991105 00449 NM 1999 11 5 USAASB99237 1 19990925 A 5210 COVER BOEING 737 7373B7 1384580 NM PAX DOOR LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 507AU 23382 RIC - FLT 163 - DURING CLIMB-OUT FROM RIC, CREW REPORTED A LOUD AIR LEAK FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETUR NED TO FIELD AT RIC AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE LOWER MAIN E NTRY DOOR HINGE COVER LEAKING. REALIGNED/REPOSTIONED LOWER HINGE COVER. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999110500450 19991105 00450 NM 1999 11 5 USAABB99043 1 19990914 A 5270 SENSOR BOEING 767 767201 1385125 NM CARGO DOOR DAMAGED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 646US 23898 BOS - FLT 894 - AFTER TAKEOFF FROM PHL, CREW RECEIVED THE BULK CARGO DOOR LIGHT. FLIGHT DIVERTED TO BOS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE BULK CARGO DOOR LATCH SENSOR (S211) DAMAGED. AIRCRAFT WAS RELEASED ON MEL. (M) 2 L 7 2 4F RT A1NM 1999110500451 19991105 00451 EU 1999 11 5 USAAF99044 1 19990913 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 897US 11392 IND - FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 12 THROUGH 17. MAINTENANCE REPLACED THE NR 7 BATTERY PACK. (M) 2 L 7 2 4F RT 1999110500452 19991105 00452 EU 1999 11 5 USAAF99045 1 19990911 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 868US 11313 IND - FOUND AFT LAVATORY AREA AND AISLE LIGHT 6 INOPERATIVE. MAINTENANCE REPLACED THE NR 8 BATTERY PACK. (M) 2 L 7 2 4F RT A20EU 1999110500453 19991105 00453 EU 1999 11 5 USAAF99048 1 19990928 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 897US 11392 GSO - EMERGENCY LIGHT STRIP NEAR CENTER EXIT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1999110500454 19991105 00454 EU 1999 11 5 USAAF99049 1 19991002 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 854US 11282 IND - FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 10 AND 15 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (M ) 2 L 7 2 4F RT 1999110500455 19991105 00455 EU 1999 11 5 USAAF99050 1 19991003 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 866US 11310 IND - FOUND EXIT SIGN BETWEEN RIGHT OVERWING EXITS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (M) 2 L 7 2 4F RT 1999110500456 19991105 00456 NM 1999 11 5 USAABB99045 1 19991004 A 3320 0593910 BALLAST BOEING 757 757225 1384959 NM GALLEY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 602AU 22196 CLT - FLT 55 - ON CLIMB-OUT FROM CLT, CREW NOTED AN ELECTRICAL SMELL IN THE COCKPIT. IT SEEMED TO STOP WHEN THE UTILITY BUSSES WERE SECURED. FLIGHT RETUREND TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE AFT GALLEY FLUORESCENT LIGHT BALLAST. (M) 2 L 7 2 4F RT A2NM 1999110500457 19991105 00457 NE 1999 11 5 USAASB99239 2 19991001 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE RIGHT FAILED A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 259AU 41665 22806 709102 CLT - FLT 8028 - DURING CLIMB-OUT FROM CLT, THE CREW ENCOUNTERED A RIGHT ENGINE VIBRATION AT ALL AIR SPEEDS ABOVE 86 PER CENT N1. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSEMBLY PER JOB CARD. TRIMMED ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. NO VIBRATION NOTED ON NEWLY INSTALLED ENGINE. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999110500458 19991105 00458 NM 1999 11 5 USAASB99236 1 19990923 A 2823 BACC63BW14SC5S CONNECTOR BOEING 737 7372B7 1384560 NM RT WING DIRTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 283AU 23116 TPA - FLT 2642 - DURING CLIMB-OUT FROM TPA, THE NR 2 ENGINE FUEL SHUTOFF VLV CLOSED LIGHT BEGAN FLICKERING ON AND OFF TH EN ILLUMINATED STEADY. ENGINE INDICATIONS WERE NORMAL. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCI DENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CLEANED THE NR 2 ENGINE FUEL SHUTOFF VALVE CANNON PLUG. OPERATED VALVE N UMEROUS TIMES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999110500459 19991105 00459 NM 1999 11 5 TSAA9927444 1 19990922 A 5753 6546434159 SKIN BOEING 737 737230 NM LT TE FLAP SEPARATED A TSAA L ABORTED APPROACH D INFLIGHT SEPARATION AP APPROACH 1 WP 13 823AL 23154 FLT 246 - LIH-HNL - FELT 'THUMP' IN AIRFRAME DURING NORMAL CRUISE. DECLARED PRECAUTIONARY AND ADVISED TOWER OF INTENT T O EXTEND GEAR AND PERFORM FLY-BY OF TOWER. REQUESTED VISUAL OF TIRES SUSPECTING POSSIBLE TIRE BLOWOUT. TOWER REPORTED TIRES NORMAL. COMPLETED NORMAL LANDING WITH FIRE EQUIPMENT STANDING BY. GEARS PINNED BY MX. PERSONNEL AND A/C TAXIED TO TERMINAL WITH NO FURTHER PROBLEM. FOUND LEFT AFT INBOARD T/E FLAP COMPOSITE MATERIAL TORN OFF IN FLIGHT AND MISSING. REMOVED AND REPLACED THE LEFT AFT INBOARD T/E FLAP IAW MM 27-51-31, PAGE 401-405, OPERATIONAL AND RIG CHECK OK. REMOV ED GEAR PINS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999110500460 19991105 00460 EU 1999 11 5 REXA99029 1 19990927 A 3620 51533172 SENSOR LOOP SAAB SF340 SF340A 7850100 EU LT WING FAILED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 406BH 340A074 PILOT REPORTED LEFT BLEED LEAK, LIGHT REMAINED ON AND MADE INFLIGHT SHUTDOWN. REMOVED AND REPLACED LEFT WING BLEED AIR SENSOR LOOP IAW AMM 36-23-10. CHECK GOOD IAW AMM 36-23-00. (M) 2 L 7 2 4T RT A52EU 1999110500461 19991105 00461 CE 1999 11 5 PLGA990921 1 19990921 A 2910 L387106A HYD SWIVEL CESSNA 340 340A 2076405 CE RT MLG BROKEN A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 05 337BE 340A047 PWM - FLT 4629 - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP HYDRAULIC FLUID QTY INDICATOR DROPPED RAPIDLY. CREW FO LLOWED CHECKLIST AND SELECTED GEAR DOWN BY PULLING EMERGENCY LANDING GEAR RELEASE HANDLE. AIRCRAFT LANDED IN PWM WITHOU T INCIDENT. MAINTENANCE WAS DISPATCHED, THE GEAR AND TOW THE A/C IN. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOWN AND LOCK ACTUATOR SWIVEL ASSEMBLY. ALL REQUIRED TESTS ALONG WITH OTHER SYSTEMS RESET AND CHECKED GOOD. AIRCRAFT W AS RETURNED TO SERVICE. (M) 1 L 7 2 3O 3A25 1999110500462 19991105 00462 WP 1999 11 5 GAIA99147 1 19990929 A 5753 5912800501 SKIN DOUG DC9 DC915F 3022037 WP LT TE FLAP DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND NUMEROUS DENTS ON THE LEFT FLAP REMOVABLE PANEL TRAILING EDGE SKIN AT XFLS 65.5 TO XFLS 127.4. THE SKIN WAS REPLACED IAW KITTY HAWK EA D9-57-008, THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999110500463 19991105 00463 NM 1999 11 5 GAIA99148 1 19991004 A 3230 RETRACT MECH BOEING 727 727251 138408H NM NLG MALFUNCTIONED A GAIA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 252US 19971 FLT 27 - OKC-AUS - DURING APPROACH, EXTENDED THE GEAR AND THE NLG FAILED TO EXTEND. THE CREW RECYCLED THE GEAR AND GOT A NORMAL EXTENSION. THE AIRCRAFT LANDED AT AUS WITHOUT FURTHER DIFFICULTIES. JACKED NOSE GEAR AND PERFORMED SEVERAL EX TENSIONS AND RETRACTIONS. NO DEFECTS NOTED AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500464 19991105 00464 NM 1999 11 5 GAIA99149 1 19991005 A 5411 FRAME BOEING 727 727223 1384074 NM NR 2 ENGINE MISDRILLED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 6821 19496 MDT - DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT AT STATION 1342.4 RIGHT SIDE HAD LOOSE FASTENERS BETWEEN WL 260 ADN WL 195. REMOVED AND REPLACED SKIN PANEL IAW BOEING SRM ANS S/B 727-53-155. INSTALLED AN INTERNAL REPAIR STRAP IAW FVI DRAWING NUMBER 53-99527-1 AND 8110 DATED OCTOBER 4, 1999. THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500465 19991105 00465 NM 1999 11 5 GAIA99150 1 19991005 A 5720 BEAM BOEING 727 727223 1384074 NM LT MLG CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 858AA 21085 PHX - DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED DURING FUEL CELL REPAIR THAT THE LOWER TRAILING EDGE PANEL ATTACHMEN T TO THE LEFT MLG BEAM HAD CORROSION DAMAGE. REPAIRS WERE COMPLETED IAW FVI DRAWING NUMBER 57-99515-1 AND 8110 DATED OC TOBER 4, 1999. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500466 19991105 00466 NM 1999 11 5 GAIA99151 1 19991005 A 3350 10006779 LIGHT BOEING 727 727214 138407R NM BS 328 FAILED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751US 21513 DURING ROUTINE MAINTENANCE CHECK IN PHX, THE EMERGENCY EXIT LIGHTS SYSTEM FAILED SELF TEST. MAINTENANCE FOUND THE EMERG ENCY EXIT LIGHT SWITCH IN THE 'ON' POSITION. BOTH LIGHT ASSEMBLIES WHERE REPLACED AND OPERATIONAL CHECK CARRIED OUT GOO D. THE AIRCRAFT WAS RELEASED BACK TO SERVICE. (M) 2 L 7 3 4F A3WE 1999110500467 19991105 00467 NM 1999 11 5 GAIA99153 1 19991008 A 2750 MS9391130ZE4C FLAP MOTOR BOEING 727 727223 1384074 NM LT TE FLAP LEAKING A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 6812 19487 LAX-MHR - FLT 2007 - LOSS OF SYSTEM 'A' HYDRAULICS AFTER TAKEOFF. PERFORMED ABNORMAL CHECKLIST AND RETURNED TO AND LAND ED AT LAX. GEAR CRANKED DOWN AND ALTERNATE EXTENSION OF FLAPS WERE ACCOMPLISHED. AIRCRAFT MADE AN UNEVENTFUL LANDING A T LAX. REMOVED AND REPLACED LEFT OUTBOARD FLAP MOTOR. OPERATIONAL AND LEAK CHECKS PERFORMED GOOD. AIRCRAFT RETURNED T O SERVICE WITH NO ADDITIONAL PROBLEMS NOTED. (M) 2 L 7 3 4F A3WE 1999110500468 19991105 00468 WP 1999 11 5 GTIA9901105 1 19990908 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 13512 48111 ACY - FLT 391 - EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK GOOD IAW DC9 MM 33 -53-00. (M) 2 L 7 2 4F A6WE 1999110500469 19991105 00469 WP 1999 11 5 GTIA9901106 1 19990901 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 ACY - ONE RED STRIP AT EMERGENCY EXIT LIGHTING INOPERATIVE. REPAIRED WIRING AT EMERGENCY LIGHT STRIP IAW MM DC9 33-00-0 0. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999110500470 19991105 00470 WP 1999 11 5 GTIA9901145 1 19990927 A 3397 WIRE DOUG DC9 DC932 3022066 WP TAILCONE FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 MYR - ONE EMERGENCY 'WHITE' FLOOR TRACK LIGHTING INOPERATIVE IN TAILCONE. FOUND WIRES BAD AT DIGITAL. REMOVED AND REPL ACED AS NEEDED. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999110500471 19991105 00471 WP 1999 11 5 EISA99164 1 19990903 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP RT EMER EXIT DISCHARGED A EISA K NONE L NO TEST NR NOT REPORTED 1 SW 07 950VJ 47564 REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999110500472 19991105 00472 1999 11 5 EISA99167 4 19990917 A 2565 1133169 SLIDE BFGOODRICH DOUG DC9 DC931 3022065 WP R2 DOOR LOW PRESSURE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 7515P 47066 FORWARD R2 EMERGENCY SLIDE LOW PRESSURE. REMOVED AND REPLACED R2 EMERGENCY SLIDE IAW 25-60-0. (M) 2 L 7 2 4F A6WE 1999110500473 19991105 00473 1999 11 5 EISA99033 4 19990226 A 3421 258733513 GYRO COLLINS DOUG DC9 DC931 3022065 WP E/E COMP FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 943VJ 81022745 47058 AIR TURN BACK BUF, CAPTAIN ADI ERRATIC IN FIGHT AFTER TAKEOFF, BANK AND PITCH BOTH SHOW INCORRECT INDICATIONS. REPLACED CAPTAINS ADI AND VERTICAL GYRO, OPERATIONS CHECK GOOD PER MM 34-00. (M) 2 L 7 2 4F A6WE 1999110500474 19991105 00474 NM 1999 11 5 EISA99170 1 19990922 A 7170 493645 MOISTURE TRAP BOEING 727 7272M7 138407S NM NR 3 ENGINE FULL A EISA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 742RW 21952 NR 3 ENGINE EPR AND FUEL FLOW FLUCTUATING. ABORTED TAKEOFF. INSPECTED ENGINE AND DRAINED WATER TRAP. NO DEFECT NOTED PER 727 MM CHAPTER 73-00. (M) 2 L 7 3 4F A3WE 1999110500475 19991105 00475 NM 1999 11 5 EISA99172 1 19990924 A 2611 774001 SMOKE DETECTOR 5360112 BOEING 727 7272M7 138407S NM CARGO BAY FAILED A EISA K NONE N FALSE WARNING CL CLIMB 1 SW 07 721RW 3327 21200 ONCE DURING CLIMB AND ONCE DURING DESCENT, NR 4 SMOKE DETECTOR LIGHT ILLUMINATED BRIEFLY, NO SMOKE OBSERVED. REMOVED AN D REPLACED NR 4 SMOKE DETECTOR. OPS CHECK NORMAL IAW MM 26-17-1. (M) 2 L 7 3 4F A3WE 1999110500476 19991105 00476 NM 1999 11 5 EISA99169 1 19990910 A 2432 25582003 BATTERY MARATHON CA72720 BOEING 727 727223 1384074 NM E/E COMPT OVERHEATED A EISA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 6819 9601409 19494 FOUR MINUTES AFTER APU CONNECTED, SMOKE IN COCKPIT. CREW SHUTDOWN ALL POWER AND FIRE DEPARTMENT REMOVED SMOKING BATTERY . REMOVED AND REPLACED BATTERY IAW MM 24-40. (M) 2 L 7 3 4F A3WE 1999110500477 19991105 00477 NM 1999 11 5 EISA99144 1 19990516 A 2120 DUCT BOEING 727 727223 1384074 NM COCKPIT FAILED A EISA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 6819 19494 DURING PREFLIGHT, SMOKE IN COCKPIT COOLING DUCT COLLAPSED CAUSING NR 1 TRANSFORMER TO OVERHEAT. REPLACED NR 1 T/R. (M) 2 L 7 3 4F A3WE 1999110500478 19991105 00478 NM 1999 11 5 EISA99168 1 19990917 A 2150 PACK BOEING 727 727223 1384074 NM NR 1 MALFUNCTIONED A EISA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 313NE 19702 LEG NR 1 AIR TURN BACK DUE TO POOR RIGHT PACK OUTFLOW AND NO PRESSURIZATION. GROUND OPS CHECK PRESSURE SYSTEM PER MM 21 -31-00. NO DEFECTS NOTED OF FOR FURTHER FLIGHT. (M) 2 L 7 3 4F A3WE 1999110500479 19991105 00479 NM 1999 11 5 EISA99166 1 19990917 A 2150 5727571 SENSOR BOEING 727 727223 1384074 NM NR 1 PACK SHORTED A EISA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 313NE 19702 CREW REPORTED LOST NR 1 PACK. REMOVED AND REPLACED INLET TEMP SENSOR IAW MM 21-61-41. OPS CHECK NORMAL PER MM 21-31-00 . (M) 2 L 7 3 4F A3WE 1999110500480 19991105 00480 NM 1999 11 5 EISA99163 1 19990823 A 3350 1000679 LIGHT GRIMES BOEING 727 7272A7 138407K NM L1 DOOR INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310NE 20241 ON POST FLIGHT, L-1 DOOR EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND REPLACED L-1 EMERGENCY LIGHT PER MM 33-50-0. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999110500481 19991105 00481 NM 1999 11 5 EISA99171 1 19990924 A 5230 MS24586187 SPRING BOEING 727 72731 1384010 NM CARGO DOOR BROKEN A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 240NE 18906 FORWARD PIT DOOR LIGHT CAME ON AT TAKEOFF. REMOVED AND REPLACED DOOR HANDLE BELL CRANK SPRING. (M) 2 L 7 3 4F A3WE 1999110500482 19991105 00482 NM 1999 11 5 F3LA99127 1 19991011 A 3297 WIRE BOEING 737 7372L9 1384497 NM NLG CHAFED A F3LA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 03 271FL 22734 DEN - FLT 436 - FLIGHT CREW REPORTED RED NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED WITH LANDING GEAR RETRAC TED. RECYCLED LANDING GEAR AND INTRANSIT LIGHT EXTINGUISHED. MAINTENANCE REPAIRED CHAFED WIRING AT AFT RT SIDE OF NOSE WHEEL AT THE POINT THE HARNESS EXITS THE CONDUIT AND PASSES THROUGH THE FEED THROUGH. PERFORMED GEAR SWING AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999110500483 19991105 00483 SO 1999 11 5 ASOA99106 1 19990928 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 228AS 22534 120025 DURING INSPECTION, EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTE RY PACK. OPERATIONAL CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999110500484 19991105 00484 SO 1999 11 5 ASOA99107 1 19991001 A 3350 F0017 FUSE EMB 120 EMB120RT SO CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 275AS 120234 DURING INSPECTION, NR 1 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MCN MAINTENANCE REMOVED AND REPLACED THE FUSE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999110500485 19991105 00485 WP 1999 11 5 ARWA991001 1 19991016 A 2612 D5020 FIRE LOOP DOUG DC8 DC862 3021970 WP NR 1 ENGINE FAILED A ARWA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 19 802BN AK03786 45909 MIA - FLT 447 - AT 14,000 FT ALT, NR 1 ENGINE FIRE WARNING SOUNDED. ENGINE SHUTDOWN. OIL QTY AND OIL PRESSURE NORMAL A ND OIL TEMP HIGH AT 140 DEGREES. REMOVED AND REPLACED NR 1 ENGINE MAIN OIL SCREEN. NO CONTAMINATION FOUND. REMOVED DI SCHARGED FIRE BOTTLE AND REPLACED WITH SERVICEABLE UNIT. REMOVED AND REPLACED NR 1 ENGINE LOWER FIRE LOOP. OPS CHECK N ORMAL. (M) 2 L 7 4 4F 4A25 1999110500486 19991105 00486 EU 1999 11 5 UF6A991011 1 19991005 A 5411 JD711J0219001 FRAME BAG ATP ATP EU NR 1 NACELLE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE NR 1 MODULAR 6 IS CRACKED AT THE AFT FRAME ASSEMBLY. MAINTENANCE STOP DRILLED AND INSTALLED REPAIR. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-01 AND ENGINEERING REPORT NR 99-051. (M) 2 L 7 2 4T RT A27NM 1999110500487 19991105 00487 EU 1999 11 5 UF6A991009 1 19991004 A 5753 JD275J0035000 SKIN BAG ATP ATP EU LT TE FLAP DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 2029 SBN - DENT FOUND ON THE LEFT BOTTOM FLAP RIB STATION 149 AND 140. MAINTENANCE INSPECTED AND FOUND TO BE WITHIN LIMITS. DAMAGE REQUIRES REPAIR WITHIN 250 FLIGHT HOURS. (M) 2 L 7 2 4T RT A27NM 1999110500488 19991105 00488 EU 1999 11 5 UF6A991008 1 19991004 A 5753 JD275J0035000 SKIN BAG ATP ATP EU LT TE FLAP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 2029 SBN - DENT FOUND ON THE LEFT BOTTOM FLAP RIB STATION 122 AND 113. MAINTENANCE INSPECTED AND FOUND TO BE WITHIN LIMITS. DAMAGE REQUIRES REPAIR WITHIN 250 FLIGHT HOURS. (M) 2 L 7 2 4T RT A27NM 1999110500489 19991105 00489 EU 1999 11 5 UF6A991007 1 19991001 A 3310 JDSL4208250 RESISTOR BAG ATP ATP EU FLT DECK FAILED A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 853AW 2022 SBN - REQUEST INSPECTION OF SMOKE AND BURNING SMELL COMING FROM FIRST OFFICERS SIDE CONSOLE. MAINTENANCE INSPECTED AND FOUND FAULTY RESISTOR. RESISTOR WAS REMOVED AND REPLACED. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500490 19991105 00490 EU 1999 11 5 UF6A991006 1 19991002 A 5411 JD711J0219001 FRAME BAG ATP ATP EU NR 2 NACELLE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE NR 2 MODULAR 6 IS CRACKED AT THE 7 O'CLOCK POSITION. MAINTENANCE STOP DRILLED AND INSTALLED REPAIR. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-01 AND ENGINEERING REPORT NR 99-051. (M) 2 L 7 2 4T RT A27NM 1999110500491 19991105 00491 EU 1999 11 5 UF6A991005 1 19991002 A 5320 12D11186 INTERCOSTAL BAG ATP ATP EU BS 270-308 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - IN GALLEY AREA BY REAR BAGGAGE DOOR INTERCOSTAL BETWEEN STATIONS 270AS AND 308AS IS CORRODED. MAINTENANCE FABRICA TED INTERCOSTAL AND INSTALLED. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-03, 51-30-01, AND 51-50-02. (M) 2 L 7 2 4T RT A27NM 1999110500492 19991105 00492 EU 1999 11 5 UF6A991004 1 19991002 A 5250 890310903 DOOR BAG ATP ATP EU BS 325.5 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - TOP ANGLE STRIP ON THE BIFOLD DOOR IS DAMAGED. MAINTENANCE REMOVED AND REPLACED STRIP. (M) 2 L 7 2 4T RT A27NM 1999110500493 19991105 00493 EU 1999 11 5 UF6A991003 1 19991002 A 3397 58791 WIRE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 SBN - SECOND TO LAST FLOOR PROXIMITY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LEAD ASSEMBLY. (M) 2 L 7 2 4T RT A27NM 1999110500494 19991105 00494 EU 1999 11 5 UF6A991002 1 19991002 A 5753 JD575J0091000 SHROUD BAG ATP ATP EU LT TE FLAP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - LEFT FLAP TRACK SHROUD AT STATION 88.41 IS DAMAGED ON THE INBOARD SIDE OF THE SHROUD. MAINTENANCE REPAIRED SHROUD . ALL WORK WAS DONE IAW ENGINEERING REPORT NR 99-191. (M) 2 L 7 2 4T RT A27NM 1999110500495 19991105 00495 EU 1999 11 5 UF6A991001 1 19991002 A 5230 JD523J0063002 SKIN BAG ATP ATP EU CARGO DOOR DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - DENT ON AFT REAR BAGGAGE DOOR. MAINTENANCE REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER. ALL WORK WAS DONE IA W BAE ATP SRM 52-11-00. (M) 2 L 7 2 4T RT A27NM 1999110500496 19991105 00496 EU 1999 11 5 UF6A990958 1 19990930 A 5400 JD711J0598001 ANGLE BAG ATP ATP EU NR 2 NACELLE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 2032 SBN - THE RIGHT MODULAR 7 AFT SUPPORT ANGLE BRACKET IS BROKEN. MAINTENANCE REMOVED AND REPLACED BRACKET. (M) 2 L 7 2 4T RT A27NM 1999110500497 19991105 00497 EU 1999 11 5 UF6A990957 1 19990928 A 5320 240D11186 INTERCOSTAL BAG ATP ATP EU BS 325.5 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL ON THE RIGHT SIDE OF CABIN BETWEEN STATIONS 325.5AS AND 308AS IS DAMAGED. MAINTENANCE REPAIRED INTERC OSTAL. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999110500498 19991105 00498 EU 1999 11 5 UF6A990956 1 19990928 A 5320 240D11186 INTERCOSTAL BAG ATP ATP EU STATION 325.5-30 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL ON THE LEFT SIDE OF CABIN BETWEEN STATIONS 325.5AS AND 308AS IS DAMAGED. MAINTENANCE REPAIRED INTERCO STAL. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999110500499 19991105 00499 EU 1999 11 5 UF6A990955 1 19990928 A 5315 JD533J0244000 FLOORBEAM BAG ATP ATP EU BS 289 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE FLOORBEAM AT STATION 289AS IS GOUGED. MAINTENANCE REPAIRED AND TREATED FLOORBEAM. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-04. (M) 2 L 7 2 4T RT A27NM 1999110500500 19991105 00500 EU 1999 11 5 UF6A990954 1 19990928 A 5320 SUPPORT BAG ATP ATP EU BS 325.5-378 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE T-RAIL LOCATED IN THE AFT BAGGAGE COMPARTMENT IS CORRODED. MAINTENANCE REPAIRED AND TREATED T-RAIL PANEL SUPP ORT. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-13. (M) 2 L 7 2 4T RT A27NM 1999110500501 19991105 00501 EU 1999 11 5 UF6A990953 1 19990928 A 5320 JD533J0007001 INTERCOSTAL BAG ATP ATP EU BS 324-343 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE INTERCOSTAL BETWEEN STATIONS 324FS AND 343FS ON THE RIGHT SIDE IS BENT. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-04 FIGURE 4. (M) 2 L 7 2 4T RT A27NM 1999110500502 19991105 00502 EU 1999 11 5 UF6A990952 1 19990928 A 5347 592SS3075 SEAT TRACK BAG ATP ATP EU BS 180-234 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE SEAT TRACK LOCATED UNDER THE LEFT GALLEY IS CORRODED. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK. A LL WORK WAS DONE IAW BAE ATP SRM 51-10-13 FIGURE 12. (M) 2 L 7 2 4T RT A27NM 1999110500503 19991105 00503 EU 1999 11 5 UF6A990951 1 19990928 A 5320 BRACKET BAG ATP ATP EU BS 378 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE AFT PRESSURE BULKHEAD GILL LINER SUPPORT BRACKET IS CORRODED. MAINTENANCE CLEANED AND TREATED CORROSION. ALL WORK WAS DONE IAW BAE ATP SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999110500504 19991105 00504 EU 1999 11 5 UF6A990950 1 19990928 A 5320 104D11186 INTERCOSTAL BAG ATP ATP EU BS 378 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - OUTBOARD RIGHT INTERCOSTAL AT STATION 378AS IS CORRODED. MAINTENANCE CLEANED AND TREATED CORROSION. ALL WORK WAS DONE IAW BAE ATP SRM 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999110500505 19991105 00505 EU 1999 11 5 UF6A990949 1 19990928 A 5320 JD533J0079000 SUPPORT BAG ATP ATP EU BS 378 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE FLOOR SUPPORT AT STATION 378AS IS CORRODED. MAINTENANCE FABRICATED FLOOR SUPPORT AND INSTALLED. ALL WORK WAS DONE IAW BAE ATP SRM 51-40-00 AND 51-50-00. (M) 2 L 7 2 4T RT A27NM 1999110500506 19991105 00506 EU 1999 11 5 UF6A990948 1 19990928 A 5320 JD256J0064001 BRACKET BAG ATP ATP EU BS 324 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE AFT SLIDE ATTACHMENT BRACKET ON THE FORWARD PASSENGER DOOR IS CRACKED. MAINTENANCE REMOVED AND REPLACED BRACK ET. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-06. (M) 2 L 7 2 4T RT A27NM 1999110500507 19991105 00507 EU 1999 11 5 UF6A990946 1 19990928 A 5411 JD711J0371001 FRAME BAG ATP ATP EU NR 2 NACELLE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE RIGHT MODULAR 6 EXHAUST SHROUD HAS 2 CRACKS. MAINTENANCE STOP DRILLED CRACKS AND INSTALLED PATCH. ALL WORK W AS DONE IAW UFS SRM SUPPLEMENT 99-03 AND ENGINEERING ORDER 99-051. (M) 2 L 7 2 4T RT A27NM 1999110500508 19991105 00508 EU 1999 11 5 UF6A990945 1 19990928 A 5400 JD711J0349000 MODULAR BAG ATP ATP EU NR 1 NACELLE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - LEFT MODULAR 7 AFT INBOARD DIAPHRAGM IS CRACKED. MAINTENANCE STOP DRILLED CRACK AND REPAIRED. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-02 AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999110500509 19991105 00509 EU 1999 11 5 UF6A990944 1 19990928 A 5330 SKIN BAG ATP ATP EU BS 252 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - DENT ON THE RIGHT SIDE OF AIRCRAFT FORWARD OF AFT BAGGAGE DOOR. MAINTENANCE REMOVED PREVIOUS REPAIR AND INSTALLED PERMANENT REPAIR. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-00 AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999110500510 19991105 00510 EU 1999 11 5 UF6A990943 1 19990928 A 5330 SKIN BAG ATP ATP EU BS 288 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - DENT ON THE LEFT SIDE OF AIRCRAFT AFT OF FORWARD PASSENGER DOOR. MAINTENANCE REPAIRED DENT BY BLENDING AND INSTAL LING STIFFENER. ALL WORK WAS DONE IAW BAE ATP SRM 51-20-01, 51-30-01, AND 51-60-01. (M) 2 L 7 2 4T RT A27NM 1999110500511 19991105 00511 EU 1999 11 5 UF6A990942 1 19990927 A 5320 JF216J0001000 BRACKET BAG ATP ATP EU BS 90 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE RIGHT TEMP CONTROL VALVE SUPPORT BRACKET IS CRACKED. MAINTENANCE REPAIRED SUPPORT BRACKET. ALL WORK WAS DONE IAW BAE ATP SRM 51-40-00 AND 51-50-00. (M) 2 L 7 2 4T RT A27NM 1999110500512 19991105 00512 EU 1999 11 5 UF6A990941 1 19990927 A 5411 JD711J0007000 FRAME BAG ATP ATP EU NR 1 NACELLE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE UPPER AFT FRAME ON THE MODULAR 5 IS CRACKED. MAINTENANCE REPAIRED UPPER AFT FRAME. ALL WORK WAS DONE IAW BAE ATP SRM 54-10-00. (M) 2 L 7 2 4T RT A27NM 1999110500513 19991105 00513 EU 1999 11 5 UF6A990940 1 19990927 A 5530 JD553J0410001 ANGLE BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE ANGLE WHICH ATTACHES THE VERTICAL STABILIZER TO THE FUSELAGE IS CRACKED ON THE RIGHT SIDE. MAINTENANCE REPAIR ANGLE. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-184. (M) 2 L 7 2 4T RT A27NM 1999110500514 19991105 00514 EU 1999 11 5 UF6A990939 1 19990927 A 5320 BRACKETS BAG ATP ATP EU E/E COMPT CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE AFT AVIONICS CRATE IS CRACKED AT THE FORWARD LEFT AND RIGHT BRACKETS. MAINTENANCE FABRICATED AND INSTALLED BR ACKETS. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-03, 51-50-01, AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999110500515 19991105 00515 EU 1999 11 5 UF6A990938 1 19990927 A 5753 JD275J0036010 SKIN BAG ATP ATP EU BS 237.63 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE LEFT FLAP TAB IS DENTED AT APPROXIMATELY STATION 237.63. MAINTENANCE REPAIRED DAMAGED AREA. ALL WORK WAS DON E IAW BAE ATP SRM 57-50-01. (M) 2 L 7 2 4T RT A27NM 1999110500516 19991105 00516 EU 1999 11 5 UF6A990937 1 19990927 A 5753 JD275J0036010 SKIN BAG ATP ATP EU LT TE FLAP DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE LEFT FLAP IS OIL CANNING APPROXIMATELY 4.5 FT FROM INBOARD TRAILING EDGE. MAINTENANCE REPAIRED DAMAGED AREA. ALL WORK WAS DONE IAW BAE ATP SRM 57-50-01. (M) 2 L 7 2 4T RT A27NM 1999110500517 19991105 00517 EU 1999 11 5 UF6A990936 1 19990927 A 5753 JD275J0036010 SKIN BAG ATP ATP EU RT TE FLAP DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE RIGHT FLAP IS DENTED AT STATION 246.63. MAINTENANCE REPAIRED DAMAGE BY FABRICATION OF PATCH. ALL WORK WAS DO NE IAW BAE ATP SRM 57-60-01. (M) 2 L 7 2 4T RT A27NM 1999110500518 19991105 00518 EU 1999 11 5 UF6A990935 1 19990927 A 5330 SKIN BAG ATP ATP EU BS 360 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - DENT LOCATED AT STRINGER 360AS ON FUSELAGE SKIN. MAINTENANCE REPAIRED DAMAGED BY FABRICATION OF PATCH. ALL WORK WAS DONE IAW BAE ATP SRM 53-30-00 AND 51-20-00. (M) 2 L 7 2 4T RT A27NM 1999110500519 19991105 00519 EU 1999 11 5 UF6A990933 1 19990927 A 7921 JD716J0104000 BRACKET BAG ATP ATP EU NR 2 ENGINE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE RN 2 ENGINE MODULE 3 OIL COOLER BRACKET IS CRACKED. MAINTENANCE REMOVED AND REPLACED BRACKET. ALL WORK WAS D ONE BAE ATP MM 79-00-00. (M) 2 L 7 2 4T RT A27NM 1999110500520 19991105 00520 EU 1999 11 5 UF6A990932 1 19990927 A 5320 243D11186 INTERCOSTAL BAG ATP ATP EU BS 270-252 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL LOCATED BETWEEN STATION 270AS AND 252AS HAS CORROSION ON IT. MAINTENANCE FABRICATED AND INSTALLED INT ERCOSTAL. ALL WORK WAS DONE BAE ATP SRM 51-40-00 FIGURE 12. (M) 2 L 7 2 4T RT A27NM 1999110500521 19991105 00521 EU 1999 11 5 UF6A990931 1 19990927 A 5315 JD533J0244000 FLOORBEAM BAG ATP ATP EU BS 270-308 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - FLOORBEAM LOCATED BETWEEN STATION 270AS AND 308AS HAS CORROSION ON IT. MAINTENANCE FABRICATED AND INSTALLED FLOOR BEAM. ALL WORK WAS DONE BAE ATP SRM 51-30-01, 51-10-03, AND 51-40-00. (M) 2 L 7 2 4T RT A27NM 1999110500522 19991105 00522 EU 1999 11 5 UF6A990930 1 19990927 A 5320 10D11186 INTERCOSTAL BAG ATP ATP EU BS 270-289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL LOCATED BETWEEN STATION 270AS AND 289AS HAS CORROSION ON IT. MAINTENANCE REMOVED CORROSION AND APPLIE D PROTECTIVE TREATMENTS. ALL WORK WAS DONE BAE ATP SRM 51-30-00. (M) 2 L 7 2 4T RT A27NM 1999110500523 19991105 00523 SO 1999 11 5 C2XA99IA493 1 19990921 A 3350 1317 BULB EMB 145 EMB145 SO PAX DOORWAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14959 145091 IAH - DURING 2A INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999110500524 19991105 00524 SO 1999 11 5 C2XA99IA514 1 19990926 A 3350 3025103 LIGHT EMB 145 EMB145 SO LT EMER EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14960 145100 IAH - DURING MAINTENANCE INSPECTION, THE LEFT FORWARD EXTERNAL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-55-10, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999110500525 19991105 00525 EU 1999 11 5 C2XA99IA513 1 19990924 A 3350 301180 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 EFD - DURING MAINTENANCE INSPECTION, THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR42-320 MM 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500526 19991105 00526 EU 1999 11 5 C2XA99IA512 1 19990923 A 5347 S5367800123900 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK WAS FOUND TO BE CORRODED AT FRAME 36. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500527 19991105 00527 EU 1999 11 5 C2XA99IA511 1 19990923 A 5347 S5367800120200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 33-34 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE LEFT INBOARD SEAT TRACK WAS FOUND TO BE CORRODED BETWEEN FRAMES 33 AND 34. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500528 19991105 00528 EU 1999 11 5 C2XA99IA510 1 19990923 A 5321 S5317310820000 FLOOR AEROSP ATR42 ATR42320 8680930 EU COCKPIT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FLOOR PANEL 21FF WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECT ED FLOOR PANEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500529 19991105 00529 EU 1999 11 5 C2XA99IA509 1 19990923 A 5320 S5367121820200 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE LEFT FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500530 19991105 00530 EU 1999 11 5 C2XA99IA508 1 19990923 A 5320 S5368953400400 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE RIGHT CARGO WALL SUPPORT AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED WALL SUPPORT IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500531 19991105 00531 EU 1999 11 5 C2XA99IA507 1 19990923 A 5347 S5367800121000 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLIGHT ATTENDANT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999110500532 19991105 00532 EU 1999 11 5 C2XA99IA506 1 19990923 A 5347 S5367800121000 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLIGHT ATTENDANT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500533 19991105 00533 EU 1999 11 5 C2XA99IA505 1 19990923 A 5320 S5367800821602 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE RIGHT Z-CHANNEL WAS FOUND TO BE CORRODED AT FRAME 39. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED Z-CHANNEL IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500534 19991105 00534 EU 1999 11 5 C2XA99IA504 1 19990923 A 5315 S53672408202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED FLOORBEAM IAW ATR42-320 SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500535 19991105 00535 EU 1999 11 5 C2XA99IA503 1 19990923 A 5315 S53672406208202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED FLOORBEAM IN ACCORDANCE WITH ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999110500536 19991105 00536 EU 1999 11 5 C2XA99IA502 1 19990923 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED DOUBLER REPA IRS ON THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500537 19991105 00537 EU 1999 11 5 C2XA99IA501 1 19990923 A 5347 S5367800120202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 33-34 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 34. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500538 19991105 00538 EU 1999 11 5 C2XA99IA500 1 19990923 A 5315 S5367800920102 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD FLOORBEAM WAS FOUND TO BE CORRODED AT THE SERVICE DOOR THRESHOLD. M AINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500539 19991105 00539 EU 1999 11 5 C2XA99IA499 1 19990923 A 5320 S53671318280 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500540 19991105 00540 EU 1999 11 5 C2XA99IA498 1 19990923 A 5320 S53673000219 BEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE TOP OF THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 30 AND 40. MA INTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASEBEAM IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500541 19991105 00541 EU 1999 11 5 C2XA99IA497 1 19990923 A 5311 S53672406200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FRAME 36 RIGHT WAS FOUND TO BE CORRODED AT FLOOR LEVEL. MAINTENANCE REPAIRED THE AFFEC TED FRAME IAW ATR 42-320 SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999110500542 19991105 00542 EU 1999 11 5 C2XA99IA496 1 19990923 A 3350 7012210 BULB AEROSP ATR42 ATR42320 8680930 EU LT EXTERNAL LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE FORWARD LEFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REINSTALLED THE AFFECTED LIGHT BULB IAW ATR42-320 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999110500543 19991105 00543 EU 1999 11 5 C2XA99IA495 1 19990923 A 5320 S536712903460 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR THRESHOLD WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 1999110500544 19991105 00544 EU 1999 11 5 UF6A990820 1 19990822 A 3350 0L3071BPEGPL BULB BAG ATP ATP EU PAX DOORWAY FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 14982 2028 SBN - FORWARD PAX DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE REPLACED THE BULB. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500545 19991105 00545 EU 1999 11 5 UF6A990821 1 19990824 A 2422 ASH6641PB INVERTER BAG ATP ATP EU NR 2 FAILED A UF6A A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 31 858AW 10551 2035 ORD - FLT 5712 - NR 2 INVERTER DROPPED OFF LINE. MAINTENANCE REPLACED THE NR 2 INVERTER. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500546 19991105 00546 EU 1999 11 5 UF6A990822 1 19990830 A 2421 BA03304 GENERATOR BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 31 851AW 2020 CWA - FLT 5718 - AT 70 KNOTS THE CWP/GEN CWP ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AC GENERATOR. SYST EM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500547 19991105 00547 EU 1999 11 5 UF6A990904 1 19990913 A 3350 1317 BULB BAG ATP ATP EU LT EXTERIOR FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 2034 SBN - THE LEFT EXTERIOR EMERGENCY LIGHT BULT AT AFT POSITION IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500548 19991105 00548 EU 1999 11 5 UF6A990905 1 19990911 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - THE LEFT EXTERIOR EMERGENCY LIGHT BULB AT AFT POSITION IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500549 19991105 00549 EU 1999 11 5 UF6A990902 1 19990908 A 5230 DOOR BAG ATP ATP EU BAGGAGE COMP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - FLT 5756 - REQUEST INSPECTION OF AFT BAGGAGE DOOR. MAINTENANCE FOUND DENT TO BE WITHIN LIMITS AT STATION 308AS. R EINSPECTION REQUIRED EVERY 125 FLIGHT HOURS AND EVERY 2 YEARS FOLLOWING INITIAL INSPECTION. ALL WORK DONE IAW BAE ATP S RM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999110500550 19991105 00550 EU 1999 11 5 UF6A990908 1 19990920 A 5720 JD920J0163000 BRACKET BAG ATP ATP EU WS 534.83 CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE LEFT WING TIP FLUX VALVE MOUNTING BRACKET IS CRACKED. MAINTENANCE REPAIRED BRACKET. ALL WORK WAS DONE IAW BA E ATP SRM 57-30-00, FIGURE 1. (M) 2 L 7 2 4T RT A27NM 1999110500551 19991105 00551 EU 1999 11 5 UF6A990906 1 19990915 A 3350 1317 BULB BAG ATP ATP EU LT EXTERIOR FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 SBN - THE LEFT EXTERIOR EMERGENCY LIGHT BULB AT AFT POSITION IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500552 19991105 00552 EU 1999 11 5 UF6A990907 1 19990915 A 3350 013071BPE BULB BAG ATP ATP EU PAX DOORWAY FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 SBN - THE EMERGENCY LIGHT AT THE FORWARD PASSENGER DOOR IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYS TEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999110500553 19991105 00553 EU 1999 11 5 UF6A990913 1 19990921 A 5720 JD571J0047000 STIFFENER BAG ATP ATP EU WS 368.366 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - LEFT WING RIB STATION 368.366 HAS A CRACKED STIFFENER AT THE LOWER ATTACHMENT POINT. MAINTENANCE FABRICATED AND I NSTALLED STIFFENER. ALL WORK WAS DONE IAW BAE ATP SRM 57-40-01. (M) 2 L 7 2 4T RT A27NM 1999110500554 19991105 00554 EU 1999 11 5 UF6A990912 1 19990921 A 5753 JD275J0036010 TAB BAG ATP ATP EU RT TE FLAP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN RIGHT FLAP TAB TRAILING EDGE IS BUCKLED AT STATION 260.366. MAINTENANCE REPAIRED DAMAGED AREA. ALL WORK WAS DONE I AW BAE ATP SRM 57-50-01. (M) 2 L 7 2 4T RT A27NM 1999110500555 19991105 00555 EU 1999 11 5 UF6A990911 1 19990921 A 5280 JD528J0074001 SKIN BAG ATP ATP EU RT MLG DOOR DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - RIGHT NOSE GEAR DOOR HAS A DENT IN THE LEADING EDGE. MAINTENANCE DRESSED OUT DAMAGED AREA AND APPLIED A DOUBLER P ATCH. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-01. (M) 2 L 7 2 4T RT A27NM 1999110500556 19991105 00556 EU 1999 11 5 UF6A990909 1 19990921 A 5330 SKIN BAG ATP ATP EU BS 305-288 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - FOUND SHALLOW DENT ON THE LEFT FORWARD FUSELAGE BETWEEN STATION 305FS AND 288FS. MAINTENANCE INSPECTED DENT AND W AS FOUND TO BE WITHIN LIMITS. DAMAGE REQUIRES A REPETITIVE 2 YEAR REINSPECTION. ALL WORK WAS DONE IAW BAE ATP SRM 51-1 0-01. (M) 2 L 7 2 4T RT A27NM 1999110500557 19991105 00557 EU 1999 11 5 UF6A990914 1 19990921 A 3350 1317 BULB BAG ATP ATP EU LT EMER EXIT FAULTY A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 SBN - LEFT EXTERNAL OVERWING EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1999110500558 19991105 00558 EU 1999 11 5 UF6A990915 1 19990922 A 5753 JD275J0036001 SKIN BAG ATP ATP EU RT TE FLAP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - RIGHT FLAP TRAILING EDGE IS DAMAGED AT STATION 206.366. MAINTENANCE REPAIRED DAMAGE. ALL WORK WAS DONE IAW BAE A TP SRM 57-50-01. (M) 2 L 7 2 4T RT A27NM 1999110500559 19991105 00559 NE 1999 11 5 CA990514013 2 19990513 A 7320 FCU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 2 ENGINE FAILED W O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 807498 (CAN) LIGHTNING STRIKE ON RIGHT WING AREA. LOSS OF N2 ON RIGHT ENGINE FOR 45 SECONDS. HEAVY RAIN. NO FAULTS FOUND BY GROUND CREW. FCU REPLACED, PRECAUTIONARY. 2 L 7 2 4F 4 F RT A21EA E15NE 1999110500562 19991105 00562 SO 1999 11 5 CA990907007 2 19990816 A 8520 635832 CRANKSHAFT CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO MCAULY 3AF34C 3AF34C92 GL ENGINE FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 431 607002 751005 (CAN) NR 2 CON ROD FAILURE DUE TO OIL STARVATION. OIL JOURNAL INTEGRITY LOOSE WHICH COULD HAVE CAUSED THE ROD BEARING F AILURE. 1 L 7 2 3O 3 O A7CE E7CE 5 C P22EA 1999110500563 19991105 00563 EA 1999 11 5 CA990907017 2 19990819 A 8530 STF27ERRB CYLINDER PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE3Y HCE3YR2A GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 584 L58061 DJ9117A (CAN) CRACKED CYLINDER BETWEEN SPARK PLUG AND EXHAUST PORT. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999110500564 19991105 00564 SO 1999 11 5 CA990907018 1 19990819 A 8100 LW15952R MOUNT PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE3Y HCE3YR2A GL TURBOCHARGER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 25 RL223861 DJ9117A (CAN) TURBO MOUNT BROKEN. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999110500565 19991105 00565 SO 1999 11 5 CA990907019 2 19990821 A 8530 635448CPA1 CYLINDER CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO MCAULY 2A34C D2A34C58 GL NR 6 CRACKED W O OTHER O OTHER IN INSP/MAINT 1 CA 511 552882 777568 (CAN) NR 6 CYLINDER CRACKED NEAR EXHAUST VALVE. 1 H 7 1 3O 3 O 3A24 E5CE 5 C P3EA 1999110500566 19991105 00566 EA 1999 11 5 CA990907027 2 19990326 A 7322 IO5217R CARBURETOR FACET MR45PR CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA MCAULY 1C160 1C160DTM GL ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 3 DC0218 L161176T 733668 (CAN) CARBURETOR LEAKING FUEL IN CUT OFF. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999110500569 19991105 00569 GL 1999 11 5 CA990907042 3 19990826 A 6114 C58 HUB CESSNA 206 P206 2073304 CE CONT O520 IO520F 17032 SO MCAULY 2A34C D2A34C58 GL PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 912 15974570F 806598 (CAN) CRACK FOUND IN HUB THREADS THROUGH NDI PER REGULAR INSPECTION REQUIREMENTS. 1 H 7 1 3O 3 O A4CE E5CE 5 C P3EA 1999110500570 19991105 00570 SO 1999 11 5 CA990907044 2 19990521 A 8530 654962A2 SPRING CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL LT ENGINE BROKEN W A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 1588 811133R 971469 (CAN) STICKING VALVES AND BROKEN VALVE SPRING. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 1999110500571 19991105 00571 CE 1999 11 5 CA990907051 1 19990719 A 6120 CYLINDER CESSNA 180 180C 2072608 CE CONT O470 O470K 17026 SO HARTZL HCA2V BHCA2V* GL PROP CONTROL LEAKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 474336K Z751 (CAN) CYLINDER FOUND LOOSE ON PROPELLER AND GUIDE COLLAR. 1 H 7 1 3O 3 O 5A6 E273 5 C P24EA 1999110500573 19991105 00573 NE 1999 11 5 CA990907069 2 19990826 A 7261 FILTER BOEING 727 727225 1384077 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE CONTAMINATED W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 649507 (CAN) ENGINE OIL TEMPERATURE INCREASED FOLLOWED BY OIL FILTER BYPASS. FILTER FOUND CARBON CONGESTED. ENGINE BEING MON ITORED. 2 L 7 3 4F 4 F A3WE E2EA 1999110500574 19991105 00574 NE 1999 11 5 CA990907078 2 19990816 A 8530 16475 STUD DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HAMSTD 2D 2D30 NE NR 9 CYLINDER BROKEN W B EMER. DESCENT E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 1200 13357 130526 (CAN) CYLINDER STUDS BROKEN ALLOWING SEPARATION OF CYLINDER. 1 H 7 1 3R 3 R A806 5E1 5 C P206 1999110500575 19991105 00575 EA 1999 11 5 CA990907080 1 19990822 A 7931 1024PG TRANSMITTER FRCHLD F27 F27F 3373008 EA RROYCE DART DART5297E 54507 EU ROTOL R4304 R1934304 EU OIL PRESSURE MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 3223 13888 18460150 (CAN) OIL PRESSURE FLUCTUATIONS INDICATING. TRANSMITTER REPLACED. 2 H 7 2 4T 4 T 7A1 E297 6 C P899 1999110500576 19991105 00576 NE 1999 11 5 CA990907082 2 19990823 A 8530 327626 CYLINDER CNDAIR CL215 CL2151A10 EA PWA R2800 R2800* 52026 NE HAMSTD 43E 43E60 NE NR 4 CRACKED W E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA 100 P31506 208837 (CAN) NR 4 CYLINDER CRACKED AT EXHAUST VALVE. 2 H 7 2 4R 4 R A14EA 5E8 6 C P871 1999110500577 19991105 00577 1999 11 5 CA990907087 4 19990825 A 6122 F624L GOVERNOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL PROPELLER MALFUNCTIONED W C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 CA 532 L152368A DJ11310A (CAN) PROPELLER UNDERSPEED AT TAKEOFF, GOVERNOR SENT FOR TEAR DOWN. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999110500578 19991105 00578 EA 1999 11 5 CA990907092 1 19990716 A 6120 TSCU DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE PROP CONTROL FAILED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA 123176 86642923 (CAN) TSCU AND TORQUE SENSOR FAILED CAUSING 150 PERCENT OVERTORQUE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500579 19991105 00579 WP 1999 11 5 CA990915081 1 19990909 A 7810 COLLECTOR DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE HAMSTD 23E 23E50 NE EXHAUST SYSTEM CRACKED W E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 71514 NK122770 (CAN) HOLE IN EXHAUST COLLECTOR CAUSED HYDRAULIC LINES FOR THE HYDRAULIC COWL FLAP TO MELT CAUSING SMOKE. 2 L 7 2 4R 4 R A669 5E4 6 C P603 1999110500580 19991105 00580 NE 1999 11 5 CA990915082 2 19990909 A 8530 CYLINDER BEECH 18 E18S 1151006 CE PWA R985 R985* 52008 NE HAMSTD 22D 22D30 NE NR 4 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 367 4216116 E2248 (CAN) NR 4 CYLINDER CRACKED. 1 L 7 2 3R 3 R A765 5E1 5 C P736 1999110500581 19991105 00581 NE 1999 11 5 CA990916002 2 19990901 A 7200 ENGINE BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE NR 1 MALFUNCTIONED W O OTHER O OTHER NR NOT REPORTED 1 CA 30863 (CAN) OIL CONS. AND VIBRATION, 2 L 7 2 4F 4 F RT A2NM E12EU 1999110500582 19991105 00582 NE 1999 11 5 CA990916005 2 19990810 A 7200 807295 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 807211 (CAN) HIGH VIBRATIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 1999110500584 19991105 00584 NM 1999 11 5 CA990927091 1 19990831 A 4990 APU AIRBUS A319 A319114 NM GE CFM56 CFM565A 13802 NE TAIL LEAKING W O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 CA 731933 (CAN) SMOKE EMITTED FROM AIR CONDITIONING UNITS WHEN SELECTED TO APU BLEED. INVESTIGATION REVEALED SMALL OIL LEAK ON AP U. UNIT REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999110500585 19991105 00585 EA 1999 11 5 CA991007002 1 19990923 A 2897 WIRE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 123110 870626 (CAN) NR 2 ENGINE LOW FUEL PRESSURE LIGHT DOESN'T ALWAYS ILLUMINATE ON ENGINE SHUT DOWN. BROKEN WIRE FOUND AT CANNON PL UG BACKSHELL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500586 19991105 00586 NM 1999 11 5 CA991007003 1 19990923 A 2710 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CONTROL YOKE LOOSE W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 22745 121158 851115 (CAN) PILOT REPORTED CONSIDERABLE FREE PLAY IN CONTROL YOKE ROLL CONTROL. CABLE LOOP IN BOTH COLUMNS UNDERTENSIONED AND ADJUSTED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500587 19991105 00587 NM 1999 11 5 CA991007004 1 19990923 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN INOPERATIVE W K NONE L NO TEST IN INSP/MAINT 1 CA 3821 1450 120373 870601 (CAN) TWO EMERGENCY LIGHTS FOUND INOPERATIVE. POWER SUPPLY AT 3352 PS1 FOUND U/S. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500588 19991105 00588 EU 1999 11 5 CA991007005 1 19990925 A 3040 M500D4A RELAY BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE WINDSHIELD HEAT FAILED W O OTHER L NO TEST CR CRUISE 1 CA LF05629A (CAN) ICE FORMED ON PILOT'S OUTER 30 PERCENT OF WINDSHIELD. FAILURE OF RELAY 1HL14. RELAY REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999110500589 19991105 00589 EA 1999 11 5 CA991007006 1 19990818 A 3231 574205 SELECTOR VALVE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG STICKING W K NONE O OTHER IN INSP/MAINT 1 CA 4334 345 123113 901009 (CAN) DURING GROUND RUNS IT WAS DISCOVERED THAT THE LANDING GEAR DOORS WOULD NOT CLOSE AND NOSE WHEEL STEERING WOULD NOT OPERATE. LANDING GEAR SELECTOR VALVE FOUND STICKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500590 19991105 00590 NE 1999 11 5 CA991007007 2 19990925 A 7320 87600520001 CABLE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 2 ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 123113 901009 (CAN) DURING INSPECTION, THE NR 2 ENGINE LOWER CONDITION LEVER CABLE WAS FOUND BLENDED BEYOND LIMITS. CABLE RESTS ON A STAINLESS STEEL PULLEY FORWARD OF THE FIREWALL WHERE THE BLENDING TOOK PLACE. CABLE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500591 19991105 00591 EA 1999 11 5 CA991007009 1 19990929 A 3010 85510202003 BOOT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HORIZONTAL STAB DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 6617 CAP0104 123113 901009 (CAN) MAINTENANCE DISCOVERED LARGE AREA OF DELAMINATION OF THE DEICER BOOT FROM THE OUTBOARD TOP SECTION OF THE LEFT HOR IZONTAL STABILIZER LEADING EDGE. LEADING EDGE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500592 19991105 00592 NE 1999 11 5 CA991007011 2 19990927 A 7321 561964 VALVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FCU LEAKING W C ABORTED TAKEOFF K R FLUID LOSS PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA LF05542A (CAN) CREW UNABLE TO ACHIEVE N1, TEMP LIMITED. FCU POPPET VALVE FOUND LEAKING WHICH CONTROLS BLEED BAND OPERATION. 2 H 7 4 4F 4 F RT A49EU E6NE 1999110500593 19991105 00593 NM 1999 11 5 CA991007012 1 19990919 A 3020 8SC0041001 BOOT 1711002 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 3097 S2BHC0059 121165 891129 (CAN) INSPECTION OF NR 2 ENGINE INTAKE DEICER BOOT FOUND DISBONDING AT THE 3 AND 9 O'CLOCK POSITIONS. COWL REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500594 19991105 00594 NM 1999 11 5 CA991007013 1 19991001 A 2823 AV24B1319D3 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 20822 M60431 121165 891129 (CAN) DURING PRE-FLIGHT, CREW NOTICED FUEL LEAKING FROM SINGLE POINT ADAPTER MANIFOLD DRAIN. MASTER REFUEL/DEFUEL SHUT- OFF VALVE AND ACTUATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500595 19991105 00595 NE 1999 11 5 CA991007014 2 19990927 A 7250 230371302 SEAL BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 ENGINE LEAKING W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA LF05683A (CAN) CREW REPORTED OIL SMELL IN COCKPIT. NR 4 ENGINE, NR 9 SEAL AND FACEPLATE REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999110500596 19991105 00596 NE 1999 11 5 CA991007019 2 19990714 A 7532 9550158260 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE INTERMITTENT W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 4939 418 340 (CAN) INTERMITTENT CLOSING OF BLEED VALVE. 1 G 7 1 3U 3 U NC H9EU E19EU 1999110500597 19991105 00597 NE 1999 11 5 CA991007020 2 19990724 A 7414 SB9RU3 GEAR DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HARTZL HCB3R HCB3R304 GL MAGNETO FAILED W H DEACTIVATE SYST/CIRCUITS E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 730 JP203317 EMA1112 (CAN) INTERNAL GEAR FAILURE. 1 H 7 1 3R 3 R A806 5E1 5 C P28EA 1999110500598 19991105 00598 NE 1999 11 5 CA991007021 2 19990914 A 7230 RIVETS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE COMPRESSOR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 4113 PCEPS0151 GH851 (CAN) ITT SPLIT REPORTED. FIRST STAGE COMPRESSOR DAMAGE FOUND BEYOND FIELD REPAIR DATA PLATE RETAINING RIVET FAILURE SU SPECTED BY OPERATOR. NOTE: SUBMITTER STATED P&W ARE REVIEWING HARDWARE ATTACHMENT OF DATA PLATES ON THESE ENGINES POS SIBLE CHANGES TO COME IN 4TH QUARTER 2000. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1999110500599 19991105 00599 NE 1999 11 5 CA991007022 2 19990914 A 7230 RIVETS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE COMPRESSOR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 4721 PCEPS0135 HJ799 (CAN) FIRST STAGE COMPRESSOR DAMAGE FOUND FIELD REPAIR COMPLETED. DATA PLATE RETAINING RIVET FAILURE SUSPECTED BY OPERA TOR. NOTE: SUBMITTER STATED P&W ARE REVIEWING HARDWARE ATTACHMENT OF DATA PLATES ON THESE ENGINES. POSSIBLE CHANGES TO COME IN 4TH QUARTER 2000. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1999110500602 19991105 00602 SW 1999 11 5 CA991007026 1 19990123 A 6710 206062721011 ACTUATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR INTERMITTENT W K NONE O OTHER IN INSP/MAINT 1 CA 237 066A CAE820743 (CAN) N2 BEEP CHANGES AND OPERATES INTERMITTENTLY AND JAMS AT TIMES. WHEN THE LINEAR ACTUATOR WAS REMOVED, THE CONNECTI NG ROD FELL OUT OF THE ACTUATOR HOUSING. 1 G 7 1 3U 3 U H2SW E4CE 1999110500603 19991105 00603 WP 1999 11 5 CA991007027 1 19990130 A 3110 INDICATOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL COCKPIT MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE832104 (CAN) FUEL SHUT-OFF CABLE WAS HARD TO ACTUATE BECAUSE THE N1 AND TOT GAUGES WERE NOT INSTALLED CORRECTLY. GAUGES SUBSEQ UENTLY INSTALLED CORRECTLY. 1 G 7 1 3U 3 U H3WE E4CE 1999110500604 19991105 00604 EU 1999 11 5 CA991007028 1 19990211 A 6420 350A33105803 BUSHINGS SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE PITCH CONTROL DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 57 ACRO11 347 (CAN) ROUTINE INSPECTION REVEALED THAT BUSHINGS DEBONDED FROM THE TAIL ROTOR PITCH CHANGE LEVER WHICH CAUSED EXCESSIVE P LAY BETWEEN THE T/R GEARBOX CASTING AND THE PITCH CONTROL LEVER. SERVICEABLE PITCH CONTROL LEVER INSTALLED. 1 G 7 1 3U 3 U H9EU E19EU 1999110500605 19991105 00605 SW 1999 11 5 CA991007029 1 19990303 A 6720 206011022067 PITCH TUBE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA CAE802195BA (CAN) DURING INSPECTION OF FLIGHT CONTROLS, A RUBBING NOISE WAS HEARD. INVESTIGATION FOUND THAT THE PITCH TUBE WAS WORN BY THE CASEY HEATER HOSE. (2.015 INCH GROOVES APPROX 3 INCHES LONG). THE TUBE WAS REPLACED AND POSTIONED CORRECTLY. 1 G 7 1 3U 3 U H2SW E4CE 1999110500606 19991105 00606 GL 1999 11 5 CA991007030 2 19990222 A 7510 6856984 VALVE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ANTI ICE SYSTEM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE802195BA (CAN) PILOT REPORTED HIGHER THAN NORMAL TOT DURING CRUISE FLIGHT. SUBSEQUENT INVESTIGATION REVEALED THE ANTI-ICE BODY H AD CRACKED OFF BETWEEN THE JAM NUT AND THE MAIN BODY. UNIT WAS REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999110500607 19991105 00607 EU 1999 11 5 CA991007031 1 19990226 A 6220 350A31183106 BUSHING SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR DISPLACED W K NONE O OTHER IN INSP/MAINT 1 CA 2653 M15092 834 (CAN) BLADE PIN BUSHING FOUND LIFTED OUT OF SLEEVE. 1 G 7 1 3U 3 U H9EU E19EU 1999110500608 19991105 00608 EU 1999 11 5 CA991007032 1 19990307 A 2432 1656 BATTERY SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE BATTERY BAY DISCHARGED W K NONE O OTHER IN INSP/MAINT 1 CA 3399 45 45207 835 (CAN) BATTERY REPLACED AS A RESULT OF STARTING PROBLEMS (VOLTAGE WAS CHECKED AND SET TO 29.0 WITH NO SUCCESS). 1 G 7 1 3U 3 U H9EU E19EU 1999110500609 19991105 00609 GL 1999 11 5 CA991007033 2 19990301 A 7323 23065123 GOVERNOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TURBINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 911 22096 CAE832056 (CAN) BLUE GREASE VISIBLE ON OUTER TURBINE GOVERNOR HOUSING. GOVERNOR WAS SLUGGISH EVEN WITH THE UNIT RIGGED ALL TO THE MAXIMUM. GOVERNOR REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 1999110500610 19991105 00610 WP 1999 11 5 CA991007034 1 19990308 A 6710 369H7352903 COLLECTIVE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL LOOSE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA CAE832056 (CAN) PLAY FOUND ON THE COLLECTIVE STICK IN THE THROTTLE MECHANISM WHICH CAUSED THE IDLE POSITION TO BE INCONSISTENT. U NIT WAS REPAIRED AND REINSTALLED. 1 G 7 1 3U 3 U H3WE E4CE 1999110500611 19991105 00611 GL 1999 11 5 CA991007035 2 19990916 A 7323 23065123 GOVERNOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TURBINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 943 26481 CAE832056 (CAN) GOVERNOR NOT MAINTAINING ROTOR RPM AND GRADUALLY DEGRADING. UNIT HAD ONLY BEEN INSTALLED FOR 53 HOURS. UNIT REPL ACED. 1 G 7 1 3U 3 U H3WE E4CE 1999110500612 19991105 00612 EU 1999 11 5 CA991007036 1 19990313 A 7810 0292808690 TAILPIPE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE EXHAUST SYSTEM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 451 (CAN) TAILPIPE CRACKED AT 10 O'CLOCK POSITION BEGINNING NEAR AN ATTACH BOLT AND EXTENDING REARWARD ALONG A WELD LINE (AP PROX 60 MM). ROTORCRAFT HAD JUST FINISHED G INSPECTION 102 HOURS PREVIOUSLY. TAIL ROTOR DRIVESHAFT (SHORT) WAS OUT OF BALANCE AND MAY HAVE CAUSED THIS CRACK. 1 G 7 1 3U 3 U H9EU E19EU 1999110500613 19991105 00613 EU 1999 11 5 CA991007042 1 19990323 A 7540 0177555170 TACHOMETER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENG BLEED SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 2138B 4525 (CAN) TACHOMETER BOX FAILING TO PROVIDE POWER TO THE BLEED VALVE, TTSN 1575.3 HOURS. 1 G 7 1 3U 3 U NC H9EU E19EU 1999110500614 19991105 00614 WP 1999 11 5 CA991007043 1 19990323 A 6230 369D27609 SWASHPLATE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR VIBRATION W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA 8033 2510 02222C064 CAE830901 (CAN) WHEN MAINTENANCE RUNNING WITH BLADES OFF, A SEVERE STICK SHAKE (1.2 IPS) WAS NOTED. SWASHPLATE REPLACED AND SHAKE REDUCED TO 0.2 IPS. 1 G 7 1 3U 3 U H3WE E4CE 1999110500615 19991105 00615 SW 1999 11 5 CA991007044 1 19990421 A 7710 LINE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TORQUEMETER LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA CAE820289 (CAN) TORQUEMETER LINE FOUND LOOSE AND LEAKING ON THE AIRCRAFT. 1 G 7 1 3U 3 U H2SW E4CE 1999110500616 19991105 00616 WP 1999 11 5 CA991007045 1 19990427 A 6710 369A7304 BRACKET HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ROTOR CONTROL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 995 CAE830896 (CAN) DURING INSPECTION, THE UPPER BEARING RETAINER CAP WAS FOUND CRACKED IN TWO. PART REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 1999110500617 19991105 00617 SW 1999 11 5 CA991007046 1 19990506 A 6230 20601045113 SWASHPLATE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR OUT OF ADJUST W K NONE O OTHER IN INSP/MAINT 1 CA A19222 CAE801475BA (CAN) THE SWASHPLATE FRICTION WAS ADJUSTED AT THE 300 HOUR INSPECTION. WAS ADJUSTED TO THE HIGH SIDE. HOWEVER, WHEN TH E OUTSIDE TEMPERATURE WENT UP, SO DID THE FRICTION. UNIT WAS RE-ADJUSTED. 1 G 7 1 3U 3 U H2SW E4CE 1999110500618 19991105 00618 GL 1999 11 5 CA991007047 2 19990507 A 7323 23065123 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TURBINE STIFF W K NONE O OTHER IN INSP/MAINT 1 CA 697 19478 CAE801475BA (CAN) TURBINE GOVERNOR ARM WAS VERY STIFF TO MOVE. ENGINES OVERSPEEDS AND DROOPS EXCESSIVELY. UNIT REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999110500619 19991105 00619 1999 11 5 CA991007048 4 19990507 A 3421 500DCBELL INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 15 335 CAE801475BA (CAN) THE GYRO WILL NOT CAGE LEVEL. TOPPLES. GYRO REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999110500620 19991105 00620 SW 1999 11 5 CA991007050 1 19990511 A 5311 206032308103 FRAME BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE890130 (CAN) DURING A VISUAL EXAMINATION OF THE TAILBOOM TO FUSELAGE ATTACH STRUCTURE, A CRACK WAS FOUND ON THE FUSELAGE AFT BU LKHEAD LOCATED AT THE UPPER RIGHT INTERCOSTAL. 1 G 7 1 3U 3 U H2SW E1GL 1999110500621 19991105 00621 NE 1999 11 5 CA991007051 2 19990514 A 7532 0177555170 TACHOMETER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENG BLEED SYSTEM FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 1821 956 (CAN) TACHOMETER BOX TESTED AND FOUND FAULTY, 7.3 TSI. 1 G 7 1 3U 3 U H9EU E19EU 1999110500622 19991105 00622 SW 1999 11 5 CA991007052 1 19990527 A 5510 206020121101 FITTING 206020123004 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE821443 (CAN) RIGHT HORIZONTAL STABILIZER FITTING CRACKED. (P/N 206-020-121-010). 1 G 7 1 3U 3 U H2SW E4CE 1999110500623 19991105 00623 SW 1999 11 5 CA991007053 1 19990604 A 2120 CONTROL CABLE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL HEATER CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA CAE822647 (CAN) CASEY HEATER FIRE WALL SHUT-OFF FOUND NOT TO BE CONNECTED. CABLE WAS CHAFING ON THE ENGINE PAN LONGERON. 1 G 7 1 3U 3 U H2SW E4CE 1999110500624 19991105 00624 SW 1999 11 5 CA991007054 1 19990604 A 2821 FILTER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL SYSTEM MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE822647 (CAN) FUEL FILTER BOWL FOUND LOCKWIRED INCORRECTLY. CORRECTED. 1 G 7 1 3U 3 U H2SW E4CE 1999110500625 19991105 00625 SW 1999 11 5 CA991007055 1 19990604 A 7920 LINE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE OIL CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA CAE822647 (CAN) ENGINE OIL SYSTEM LINES FOUND TO BE CHAFING ON THE FUEL CONTROL SYSTEM LINES. LINES WERE THEN REPOSITIONED CORREC TLY. 1 G 7 1 3U 3 U H2SW E4CE 1999110500626 19991105 00626 GL 1999 11 5 CA991007056 2 19990604 A 7230 NUT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COMPRESSOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA CAE822647 (CAN) COMPRESSOR SCROLL JAM NUT FOUND LOOSE. RECTIFIED. 1 G 7 1 3U 3 U H2SW E4CE 1999110500627 19991105 00627 GL 1999 11 5 CA991007060 2 19991021 A 7323 23006259 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TURBINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 666 3AAD2118 CAE821010 (CAN) FUEL LEAK BEYOND LIMITS FROM GOVERNOR. UNIT CHANGED. 1 G 7 1 3U 3 U H2SW E4CE 1999110500628 19991105 00628 CE 1999 11 5 CA991007067 1 19990930 A 3230 EVE4001S1 MOTOR PRESTOLITE HYH5001 BEECH 76 76 1153005 CE LYC O360 O360A1G 41514 EA HARTZL HCM2Y HCM2YR GL MLG DAMAGED W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION AP APPROACH 1 CA 4330 CAC01 L2840736A FB1079A (CAN) GEAR WOULD NOT EXTEND TO DOWN AND LOCKED WHEN SELECTED. HAD TO USE EMERGENCY EXTENSION. UPON INVESTIGATION, HYD RAULIC POWER PACK ELECTRIC MOTOR ARMATURE WAS FOUND DAMAGED. 1 L 7 2 3O 3 O A29CE E286 5 C P43GL 1999110500629 19991105 00629 1999 11 5 CA991007069 4 19990922 A 3420 WIRE EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL COCKPIT COMPASS SHORTED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA PCE56782 BU8607 (CAN) DURING FLIGHT, PILOT REPORTED SMOKE AROUND MASTER COMPASS AND LOSS OF OTHER LIGHTING IN THE COCKPIT. COMPASS LIGH T WIRES FOUND SHORTED AT CONNECTOR AND INSULATION BURNT. CIRCUIT BREAKER DID NOT TRIP. 1 L 7 2 4T 4 T A21SO E4EA 6 C P15EA 1999110500631 19991105 00631 CE 1999 11 5 CA991007075 1 19991004 A 5610 5042006923 WINDSHIELD BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL COCKPIT CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA PCE51165 EAA1140M1 (CAN) DURING CLIMB THROUGH 10,000 FEET, THE CAPTAIN'S OUTER PANE WINDSHIELD CRACKED. AIRCRAFT WINDSHIELD REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 1999110500632 19991105 00632 CE 1999 11 5 CA991007077 1 19991004 A 3230 1CH25 SWITCH BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL LT & RT MLG OUT OF ADJUST W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA PCE41919 BU8250 (CAN) AIRCRAFT GEAR-IN-TRANSIT LIGHT REMAINED ON FOLLOWING LIFT OFF. UPON INVESTIGATION, MAINTENANCE FOUND THE LEFT AND RIGHT GEAR POSITION SWITCHES WERE ADJUSTED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999110500633 19991105 00633 CE 1999 11 5 CA991007078 1 19991004 A 2730 DRAIN BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL ELEVATOR PLUGGED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA PCE50392 BU5322 (CAN) AIRCRAFT WAS IN-FLIGHT AND CREW NOTICED THAT THE AIRCRAFT SEEMED TO BE TRIMMING ITSELF. MAINTENANCE FOUND THAT T HE ELEVATOR CABLES WERE STICKING IN ICE IN THE TAIL. ICE WAS REMOVED AND THE DRAIN HOLES UNPLUGGED. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999110500634 19991105 00634 EA 1999 11 5 CA991007080 1 19990924 A 2720 C3CF259LS4 BEARING DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE HARTZL HCB3T HCB3TN3 GL RUDDER PEDAL WORN W K NONE O OTHER IN INSP/MAINT 1 CA PCE35102 BUA19206 (CAN) DURING INSPECTION, RUDDER PEDALS FOUND TO HAVE PLAY UP AND DOWN. LEFT SUPPORT BRACKET, BEARING AND BOLT WERE FOUN D TO HAVE SIGNIFICANT AMOUNT OF WEAR. ALL PARTS REPLACED. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 1999110500635 19991105 00635 EA 1999 11 5 CA991007081 1 19990924 A 2750 C3CF5012 DETENT DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE HARTZL HCB3T HCB3TN3 GL FLAP SELECTOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA PCE35102 BUA19206 (CAN) FLAP SELECTOR DETENT HOLES FOUND WORN WHERE THERE IS NO POSITIVE DETENT FOR HANDLE POSITION. NEW SELECTOR INSTALL ED. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 1999110500636 19991105 00636 EA 1999 11 5 CA991007082 1 19990924 A 5523 C3TE1312 SERVO TAB DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE HARTZL HCB3T HCB3TN3 GL ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE35102 BUA19206 (CAN) DURING INSPECTION, ELEVATOR SERVO TAB WAS FOUND CRACKED. TAB REPLACED. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 1999110500637 19991105 00637 NM 1999 11 5 CA991007088 1 19990926 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 22481 361 123152 LH8415 (CAN) DURING TAXI, THE NWS FAILED. AFTER TAKEOFF, GEAR RETRACTED NORMALLY, BUT FAILED TO EXTEND WHEN SELECTED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500638 19991105 00638 NM 1999 11 5 CA991007089 1 19990926 A 2910 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24779 120329 870304 (CAN) HYDRAULIC FLUID FOUND LEAKING FROM NR 2 NACELLE WHILE AIRCRAFT PARKED. NR 2 EDP PRESSURE LINE FOUND LEAKING AT PR ESSURE MANIFOLD. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999110500639 19991105 00639 EA 1999 11 5 CA991007094 1 19990930 A 2761 2651001011 ACTUATOR DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL SPOILER CRACKED W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 106 PCE86302 237483 (CAN) DURING PRE-FLIGHT, PILOTS NOTICED THAT ROLL SPOILERS WOULD NOT STOW WITH INBOARD, OUTBOARD FAILURE INDICATION AND NO HYDRAULIC FLUID IN NR 2 SYSTEM. INVESTIGATION REVEALED THE HOUSING FOR THE ROLL SPOILER ACTUATOR WAS CRACKED COMPLET ELY AROUND ITS CIRCUMFERENCE NEAR WHERE THE TWO HALVES OF THE ACTUATOR BOLT TOGETHER. ONE ATTACHMENT BOLT WAS SHEARED. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 1999110500641 19991105 00641 EU 1999 11 5 CA991007096 1 19990929 A 3246 A32266 BOLT C20211160 AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE MLG WHEEL FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 11387 455332 (CAN) WHEEL TIE BOLTS STRETCHED AT 180 FEET/POUNDS TORQUE. REF: MESSIER BUGUATTI SL C20195-32-799. 2 L 7 2 4F 4 F RT A35EU E23EA 1999110500642 19991105 00642 EU 1999 11 5 CA991007097 1 19990929 A 3246 A32266 BOLT C20211160 AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE MLG WHEEL BROKEN W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 11646 455332 (CAN) WHEEL TIE BOLTS STRETCHED AT 180 FEET/POUNDS TORQUE. REF: MESSIER BUGUATTI SL C2 195-32-799. 2 L 7 2 4F 4 F RT A35EU E23EA 1999110500643 19991105 00643 EU 1999 11 5 CA991007098 1 19990929 A 3246 A32266 BOLT C20211160 AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE MLG WHEEL FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 11345 455827 (CAN) WHEEL TIE BOLTS STRETCHED AT 180 FEET/POUNDS TORQUE. REF: MESSIER BUGUATTI SL C2 195-32-799. 2 L 7 2 4F 4 F RT A35EU E23EA 1999110500644 19991105 00644 SO 1999 11 5 CA991008005 1 19990925 A 2750 4TL571 SELECTOR 41231 PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE2Y HCE2YR2 GL TE FLAP BROKE W A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 CA 8173 31363 L161761 CJ505 (CAN) WHEN ON APPROACH, PILOT SELECTED WING FLAPS, SELECTOR HANDLE BROKE OFF CLOSE TO PIVOT POINT. INSPECTION SHOWS 40 PERCENT DIAMETER OF STEM SHOWS INTERNAL CORROSION; THUS, WEAKENING THE STEM. KNOB P/N: 23943-00. PIPER SWITCH ASSY P /N: 487-839 REPLACED. MICROSWITCH P/N: 4TLS71. 1 L 7 2 3O 3 O A20SO E14EA 5 C P9EA 1999110500645 19991105 00645 NE 1999 11 5 CA991008012 2 19990913 A 7322 ECU AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE ENGINE FAULTY W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 741603 (CAN) UNSTABLE ENGINE POWER CAUSED BY ECU CHANNEL B FAULT, LOW PRESSURE TURBINE CLEARANCE VALVE AND T12 SENSOR ALSO CHAN GED. 2 L 7 4 4F 4 F RT A197 E37NE 1999110500646 19991105 00646 EU 1999 11 5 CA991008013 1 19990916 A 2610 FIRE LOOP AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 2 ENGINE MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 741496 (CAN) ON CLIMB-OUT, NR 2 ENGINE FIRE DETECT SYSTEM FAULT. NR 2 ENG FIRE LOOP B REPLACED. 2 L 7 4 4F 4 F RT A197 E37NE 1999110500647 19991105 00647 EU 1999 11 5 CA991008014 1 19990921 A 2913 PUMP AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE HYDRAULIC SYS FAULTY W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 741567 (CAN) GREEN SYSTEM HYDRAULIC LOSS OF PRESSURE AND QUANTITY. 2 L 7 4 4F 4 F RT A197 E37NE 1999110500648 19991105 00648 EU 1999 11 5 CA991008016 1 19990922 A 3260 SENSOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NLG FAULTY W A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 CA 731503 (CAN) AFTER TAKEOFF, LANDING GEAR ABSORBER FAULT ILLUMINATED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999110500649 19991105 00649 EU 1999 11 5 CA991008017 1 19990925 A 2420 CARBON SEAL AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE GENERATOR FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 731880 (CAN) INTEGRATED DRIVE GENERATOR CARBON SEAL FAILED CAUSING LOSS OF ENGINE OIL. 2 L 7 2 4F 4 F RT A28NM E29NE 1999110500650 19991105 00650 EA 1999 11 5 CA991008023 1 19990914 A 2750 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 807428 (CAN) FLAP FAILED ON DESCENT. BROKEN WIRE ON BPSU IN WHEELWELL. REPAIRED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999110500651 19991105 00651 EU 1999 11 5 CA991008029 1 19990819 A 7921 350A72032527 GUIDE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE RIVET HOLES SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 786 (CAN) DURING ROUTINE MAINTENANCE, OIL COOLER WHEEL AND BLOWER DUCT FOUND DAMAGED. FURTHER INSPECTION FOUND GUIDE MISSIN G WHICH WAS FOUND IN BOTTOM BELLY PANEL. 1 G 7 1 3U 3 U H9EU E19EU 1999110500652 19991105 00652 EU 1999 11 5 CA991008030 1 19990819 A 7921 95544576 BLOWER WHEEL SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE OIL COOLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 786 (CAN) DURING ROUTINE MAINTENANCE, THE OIL COOLER BLOWER WHEEL WAS FOUND TO HAVE MISSING BLADES. SUSPECT GUIDE (P/N 350A- 720-325-27) TO HAVE SEPARATED FROM ASSEMBLY AND GOT CAUGHT BETWEEN BLOWER WHEEL AND BLOWER DUCT. 1 G 7 1 3U 3 U H9EU E19EU 1999110500653 19991105 00653 EU 1999 11 5 CA991008031 1 19990819 A 7921 350A53106721 DUCT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE OIL COOLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 786 (CAN) DURING ROUTINE MAINTENANCE, FOUND BLOWER DUCT CRACKED. SUSPECT GUIDE P/N 350A-720-325-27 TO HAVE SEPARATED FROM A SSEMBLY AND GOT CAUGHT BETWEEN BLOWER WHEEL AND BLOWER DUCT. 1 G 7 1 3U 3 U H9EU E19EU 1999110500654 19991105 00654 SW 1999 11 5 CA991008032 1 19990913 A 7921 HOLE 41291013 ENSTRM 480 480TH28 SW ALLSN 250C 250C20 03013 GL OIL COOLER ELONGATED W K NONE O OTHER IN INSP/MAINT 1 CA CAE845007 (CAN) DURING INSPECTION, MOVEMENT BETWEEN ADAPTER AND OIL COOLER IMPELLER SHAFT WAS FOUND. ATTACHMENT IS BY TAPERED PIN WITH HOLES DRILLED IN SHAFT ADAPTER. UPON DISASSEMBLY, ALL DRILLED HOLES AND TAPERED PIN WAS FOUND WORN. 1 G 7 1 3O 3 U 0 H1CE E4CE 1999110500655 19991105 00655 NM 1999 11 5 TWAA9914901 1 19991103 A 3350 LIGHT BOEING 767 767231 1385131 NM ROW 11 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 601TW 22564 FOUND CABIN EGRESS LIGHTS INOPERATIVE AT ROW 11 RT SIDE AND ON THE RT SIDE BY THE OVERWING EXIT. FOUND BOTH BULBS WERE LOOSE. SECURED LOOSE CONNECTIONS. CHECK-C 9-26-99 LAX. 2 L 7 2 4F RT A1NM 1999110500656 19991105 00656 NM 1999 11 5 TWAA9914902 1 19991020 A 5730 SKIN BOEING 757 7572Q8 1384972 NM WS 300-360 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 704X 28163 FOUND CORROSION AROUND MANY FASTENERS AND ON RT WING SKIN SURFACE UNDER BLACK ICE DETECTION STRIPE, FRONT TO REAR SPAR, STA 300 TO 360. REMOVED BLACK ICE DETECTION STRIPE. CLEANED CORROSION FROM SURFACE OF WING SKIN. REMOVED AND REPLACED 235 FASTENERS AND CLEANED HOLES FROM SAME DUE TO CORROSION. PRIMER PAINTED WING SKIN SURFACE AND ALODINED. REPAIRED P ER 737-300 SRM 57-20-01, FIG 101 AND 104. CHECK-C 7-19-98 LAX. 2 L 7 2 4F RT A2NM 1999110500657 19991105 00657 NM 1999 11 5 TWAA9914903 1 19991020 A 5730 SKIN BOEING 757 7572Q8 1384972 NM WS 300-360 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 704X 28163 FOUND CORROSION ON LT WING SKIN SURFACE FROM FRONT TO REAR SPAR UNDER THE BLACK ICE DETECTION STRIPE, STA 300 TO 360. R EMOVED BLACK ICE DETECTION STRIPE. CLEANED CORROSION FROM SURFACE OF WING SKIN AND REPLACED TWO FASTENERS DUE TO CORROS ION. CLEANED HOLES FROM SAME. ALODINED AND PRIMER PAINTED WING SKIN SURFACE. REPAIRED PER 737-300 SRM 57-20-01, FIG 1 01 AND 102. CHECK-C 7-19-98 LAX. 2 L 7 2 4F RT A2NM 1999110500658 19991105 00658 WP 1999 11 5 TWAA9914904 1 19991024 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9405T 53141 DURING CHECK-C MAINT, FOUND THE AREA AROUND THE FORWARD CARGO DOOR OUTER DOOR HANDLE WITH SKIN BENT IN WITH A .375 INCH CRACK COMING OUT OF RADIUS. REMOVED CRACKED AREA AND STRAIGHTENED OUT DENT PER SRM 53-04, FIG 38. 2 L 7 2 4F RT A6WE 1999110500659 19991105 00659 WP 1999 11 5 TWAA9914905 1 19991102 A 5320 END CAP DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING CHECK-C MAINT, FOUND LONGERONS R2 AND L2 WITH THE END CAPS CRACKED AT STA 1076, EACH WITH APPROXIMATELY A 1.5 INC H CRACK. REPLACED EACH LONGERON SECTION PER SRM 53-02, FIG 8. 2 L 7 2 4F A6WE 1999110500660 19991105 00660 1999 11 5 MALA976619 4 19991008 A 2210 AUTO PILOT BAC 146 AVRO146RJ85A 1500097 EU E/E COMP TRIPPED OFF A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 503XJ E2310 AUTO THROTTLE, AUTO PILOT, AND FLIGHT DIRECTOR AS WELL AS THE ALTITUDE ALERTER AND TRP KICKED OFF LINE IN FLIGHT. RESET AND KICKED OFF LINE AGAIN ABOUT 20 MINUTES LATER. MAINTENANCE CYCLED POWER AND PERFORMED RETURN TO SERVICE TEST, ALL C HECKS GOOD IAW RJ 85 MM CH 34. 2 H 7 4 4F RT A49EU 1999110500661 19991105 00661 1999 11 5 MALA976620 4 19991008 A 3417 HC396H0485008 ADAU BAC 146 AVRO146RJ85A 1500097 EU E/E COMP MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 503XJ E2310 AUTO THROTTLE, AUTO PILOT, FLIGHT DIRECTOR, TRP, ALTITDE ALERTER KICKED OFF LINE IN FLIGHT. MAINTENANCE, FAULT CODES SH OWED NR 1 & NR 2 ADC'S INVALID FAULTS. COULD NOT DUPLICATE FAULT ON GROUND. REPLACED ADAU FOR PRECAUTIONS, SYSTEMS ALL CHECK GOOD IAW AVRO RJ-85 MM SECTIONS 34, 22, 76. 2 H 7 4 4F RT A49EU 1999110500662 19991105 00662 EU 1999 11 5 MALA976621 1 19991026 A 5311 FRAME SAAB SF340 SF340A 7850100 EU BS 694,710&733 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 48XJ 048 DURING HEAVY CHECK INSPECTION, FOUND CORROSION DAMAGE ON FRAMES AT STA 694, 710, AND 733. MAINTENANCE REPAIRED CORROSIO N DAMAGE PER SAAB STRUCTURAL REPAIR STATEMENT 72SDS1887 AND PER EO NR S53065. 2 L 7 2 4T RT A52EU 1999110500663 19991105 00663 EU 1999 11 5 MALA976622 1 19991030 A 2750 RETRACT MECH BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS LACK OF LUBE A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 511XJ E2326 WHEN SELECTING FLAPS FROM 18 TO 24 DEGREES, GOT A FLAP FAULT AND FLAP INOP. THE FLAPS DID NOT MOVE FROM 18 TO 24 DEGREE S. THE F/O REPORTED THE FLAP HANDLE DID NOT TRAVEL SMOOTHLY FROM 18 TO 24 DEGREES. MAINTENANCE PERFORMED FLAP FAULT RE SET AND SAFETY LANE 1 AND 2 RESET PROCEDURES IAW AVRO MM 27-50-00 PG 301. LUBRICATED SCREW JACK BALL NUTS. OPS CHECK O F FLAP GOOD. 2 H 7 4 4F RT A49EU 1999110500664 19991105 00664 EU 1999 11 5 MALA976623 1 19991030 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMP MALFUNCTIONED A MALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 GL 15 410XJ 410 CARGO SMOKE LIGHT ILLUMINATED ON SHORT FINAL TO ATW, MEMORY ITEMS AND QRH COMPLETED, FIRE EXTINGUISHER ACTIVATED. MAINT ENANCE REPLACED NR 1 SYSTEM RT AFT CARGO FIRE BOTTLE, PERFORMED OPS CHECKS, ALL CHECKS GOOD. CLEANED SMOKE DETECTOR AND CANNON PLUG AT DETECTORS, PERFORMED OPS CHECK OF SMOKE DETECTOR SYSTEM. CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999110500665 19991105 00665 EU 1999 11 5 MALA976624 1 19991101 A 7722 ITT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 102XJ 340A102 A 40 DEGREE SPLIT AT CHARTED TORQUE WITH ENGINE ANTI ICE ON, RIGHT ENGINE WAS AT 832 ITT WHILE LEFT ENGINE WAS AT 792. A IRCRAFT RETURNED TO DTW. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF INLET, NO DEBRIS FOUND. PERFORMED ALL CHECKS IA W 72-00-00 PAGE 167. TEMP/PARAMETERS ALL WITHIN LIMITS, MAX SPLIT FOUND WAS 12 DEGREES. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999110500666 19991105 00666 NM 1999 11 5 CALA9901454 1 19991101 A 3350 900835A BATTERY PACK AVIALL BOEING 727 727224 1384076 NM EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND THE LT AND RT AFT EXIT DOOR OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED, THE CONNECTOR WAS CLEANED, AND THE BATTERY PACK WAS RECHARGED. THE BATTERY PACK WAS REINSTALLED AND OPERATION CHECKED G OOD IAW MM 33-51-01, PAGES 5 & 6. 2 L 7 3 4F A3WE 1999110500667 19991105 00667 NM 1999 11 5 CALA9901455 1 19991101 A 3350 6104781 BATTERY PACK GRIMES BOEING 727 727224 1384076 NM GALLEY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND THE FORWARD GALLEY DOOR RT OUTSIDE EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS RECHARGED AND OPE RATION CHECKED GOOD IAW MM 33-50-0, PAGE 201. 2 L 7 3 4F A3WE 1999110500668 19991105 00668 NM 1999 11 5 CALA9901456 1 19991101 A 3350 900835A BATTERY PACK AVIALL BOEING 727 727224 1384076 NM EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND THE LT AND RT FORWARD EXIT DOOR OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVE D, THE CONNECTOR WAS CLEANED, AND THE BATTERY PACK WAS RECHARGED. THE BATTERY PACK WAS REINSTALLED AND OPERATION CHECKE D GOOD IAW M 33-51-01, PAGES 5 & 6. 2 L 7 3 4F A3WE 1999110500669 19991105 00669 NM 1999 11 5 CALA9901457 1 19991101 A 3350 BATTERY PACK BOEING 727 727224 1384076 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND THE CENTER OVERHEAD EMERGENCY EXIT LIGHTS ALL DIM OR INOPERATIVE. THE BATTERY PACK WAS REMOVED, THE CO NNECTORS WERE CLEANED AND THE BATTERY PACK WAS RECHARGED. THE BATTERY PACK WAS REINSTALLED AND OPERATION CHECKED GOOD I AW MM 33-51-01, PAGE 5. 2 L 7 3 4F A3WE 1999110500670 19991105 00670 NM 1999 11 5 CALA9901458 1 19991101 A 3350 BATTERY PACK BOEING 727 727224 1384076 NM ROW 17 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND EMERGENCY EXIT LIGHTS AT FORWARD ENTRY DOOR AND OVERHEAD AT ROW 17 INOPERATIVE. THE BATTERY PACKS WERE REMOVED, RECHARGED, AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE 201. 2 L 7 3 4F A3WE 1999110500671 19991105 00671 NM 1999 11 5 CALA9901459 1 19991101 A 5753 FITTING BOEING 737 7373T0 1384582 NM TE FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND A .5 INCH CRACK IN LT WING NR 3 FLAP TRACK FAIRING FORWARD FITTING AT FORWARD END OF FLAP TRACK I/B LOW ER CORNER. A NEW FITTING WAS INSTALLED IAW SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F RT A16WE 1999110500672 19991105 00672 NM 1999 11 5 CALA9901460 1 19991101 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 294, BL 0 TO LBL 45. A NEW T-CHORD AND SPLICES WERE INSTALLED IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 1999110500673 19991105 00673 NM 1999 11 5 CALA9901461 1 19991101 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 867-887 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 THE FORWARD DORSAL FIN FAIRING CAUSED CHAFING WEAR ON UPPER FUSELAGE SKIN IN TWO AREAS AT STA 867-887, RBL 1-11 AND LBL 1-11. THE WORN SECTIONS OF SKIN WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 1999110500674 19991105 00674 WP 1999 11 5 CALA9901462 1 19991101 A 5312 BULKHEAD TEE DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND ANGLE TEE ATTACHED TO PRESSURE BULKHEAD AT STA 2007, LBL 5 CORRODED. THE ANGLE TEE WAS REPAIRED IAW SR M 53-40-00, FIGURE 16. 2 L 7 3 4F A22WE 1999110500675 19991105 00675 NM 1999 11 5 CALA9901463 1 19991102 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947&967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 947, LBL 10 TO RBL 10 AND AT STA 967. NEW UPPER CHORDS WERE INSTALLED IAW SRM 53-00-51 AND ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999110500676 19991105 00676 WP 1999 11 5 9904449923 1 19990925 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 47 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 927RC 47469 DURING MAINTENANCE INSPECTION, NOSE LANDING GEAR JAMB BEAM AT FS 47 WAS FOUND CRACKED AT BOTH LEFT AND RIGHT DOOR JAMBS. REPAIRED PER EA 99-169112. 2 L 7 2 4F A6WE 1999110500677 19991105 00677 WP 1999 11 5 9904459923 1 19990917 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 148 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 927RC 47469 DURING MAINTENANCE INSPECTION, FOUND A DAMAGED HOLE IN AFT FACING FLANGE OF CABIN FLOORBEAM AT RIGHT SIDE OF FS 148. RE PAIRED PER EA 99-169153. 2 L 7 2 4F A6WE 1999110500678 19991105 00678 WP 1999 11 5 9904469758 1 19990902 A 5347 CARGO TRACK DOUG DC9 DC941 302207N WP BS 408-427 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING SCHEDULED INSPECTION, FOUND CORROSION ON THE OUTBOARD FLANGE OF THE CARGO TIE DOWN TRACK (S2922357), FS 408 - 427 . BLEND OUT WAS BELOW SRM LIMITS. REPAIRED PER EA 97-169116. 2 L 7 2 4F A6WE 1999110500679 19991105 00679 EU 1999 11 5 9904473212 1 19990918 A 5315 FLOORBEAM AIRBUS 320 A320211 3930320 EU BS 13-24 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 312US 152 DURING LINE CHECK, FOUND SOFT FLOOR IN FORWARD GALLEY AREA. FOUND CORROSION ON FLOORBEAMS AND SEAT TRACKS FROM FRAMES F S 13 TO 24. REPAIRED PER SRM 51-72-11 AND NW DWG SA 5346-01004-2. 2 L 7 2 4F RT A28NM 1999110500680 19991105 00680 WP 1999 11 5 9904481162 1 19990907 A 5320 ANGLE DOUG DC10 DC1040 3023508 WP BS 1741-1746 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING M-CHECK, FOUND CORROSION ON T ANGLE FROM FS 1741 TO 1746 BETWEEN LONGERON 42L AND 43L. REPAIRED PER EA 11-170503 . 2 L 7 3 4F A22WE 1999110500681 19991105 00681 WP 1999 11 5 9904491162 1 19990914 A 5711 RIB DOUG DC10 DC1040 3023508 WP WS 344 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING M-CHECK, FOUND CRACK IN RIGHT WING LEADING EDGE RIB AT WS XW344 RIGHT. REPAIRED PER EA 11-167483. 2 L 7 3 4F A22WE 1999110500682 19991105 00682 WP 1999 11 5 9904501230 1 19990930 A 5753 SKIN DOUG DC10 DC1030 3023501 WP LT TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 230NW 46552 DURING M-CHECK, FOUND CRACKS ON LEFT INBOARD FLAP UPPER SKIN 12 INCHES FORWARD OF MID SPAR 18 INCHES FROM OUTBOARD END. REPAIRED PER EA 12-170069. 2 L 7 3 4F A22WE 1999110500683 19991105 00683 NM 1999 11 5 DL757992414 1 19991030 A 2150 6806404 ACM BOEING 757 757232 1384965 NM LEFT INOP A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 625DL 22915 PILOT REPORTED SMOKE IN COCKPIT, AFTER T/R DEPLOYMENT ON TOUCHDOWN. LT PACK TRIPPED SHORTLY THEREAFTER. REPLACED L T ACM, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1999110500684 19991105 00684 NE 1999 11 5 DL76S992416 2 19991101 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE DAMAGED A DALA O OTHER C F.O.D. TX TAXI/GRND HDL 1 SO 27 116DL 23275 ON ARRIVAL FLT 1814 BOS, FOUND FOD DAMAGE TO MULTIPLE FAN BLADES AND ACCOUSTICAL LINER. REPLACED FAN. 2 L 7 2 4F 4 F RT A1NM E13NE 1999110500685 19991105 00685 1999 11 5 DLM11992417 4 19991101 A 2330 ENERTAINMENT SYS 1301273110R DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 815DE 9812001316 48624 INFLIGHT ENTERTAINMENT SYSTEM STOPPED AFTER 1.5 HOURS APPROX. QUIT TOTALLY WITH SMOKE ODOR SHORTLY AFTER SYSTEM SHUT DO WN. FOUND PAT AVU FAILED. NOTICED BURNED ODOR IN UNIT. REPLACED AVU. SYSTEM OPERATED NORMALLY AFTER REPLACEMENT. 2 L 7 3 4F RT A22WE 1999110500686 19991105 00686 NM 1999 11 5 DL72S992418 1 19991101 A 3350 6104789 BATTERY PACK BOEING 727 727232 1384082 NM EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 DURING L/O CHECK, FOUND R1 L1 EXT EMERG LIGHTS INOP. REPLACED BATTERY PACK, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999110500687 19991105 00687 NM 1999 11 5 DL72S992419 1 19991101 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 DURING L/O CHECK, FOUND LEFT AFT OVERWING EXTERNAL EMERGENCY LIGHT INOP. REPLACED BATTERY AND CHARGER, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999110500688 19991105 00688 NM 1999 11 5 DL72S992420 1 19991101 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 DURING L/O CHECK, FOUND RT FWD OVERWING EMERG LIGHT INOP. REPLACED BATTERY AND CHARGER, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999110500689 19991105 00689 NM 1999 11 5 DLM88992421 1 19991102 A 5330 5911406 SKIN DOUG MD88 MD88 3023688 NM BS 213-229 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 920DL 49644 DENTS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FS 213 AND 229 AND BETWEEN STRINGERS 16L AND 17L. THE DAMAGE WAS CUT OUT AND REPAIRED PER ERA 333730-14. 2 L 7 2 4F RT A6WE 1999110500690 19991105 00690 NM 1999 11 5 DL72S992422 1 19991102 A 5330 6518420404 SKIN BOEING 727 727232 1384082 NM BS 354 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 354 AT STRINGER 3R. THE DAMAGE WAS REMOVED WITH A 1.0 CUTOUT AND REPAIRED PER ERA 333754-14. 2 L 7 3 4F A3WE 1999110500691 19991105 00691 NE 1999 11 5 DLM11992423 2 19991101 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 1 BIRD STRIKE A DALA K NONE C F.O.D. LD LANDING 1 SO 27 801DE 29995 723874 48472 723874 ON WALK-AROUND, FOUND EVIDENCE OF BIRD STRIKE ON NR 1 ENG AND NR 1 PYLON AREA. PERFORMED BIRD STRIKE INSPECTION PER AMM 05-52-00 OF AIRCRAFT INCLUDING NR 2 ENG INLET. ALSO, PERFORMED BIRD STRIKE INSP OF NR 1 PER AMM 72-11-02-6-02 AND DUE TO EVIDENCE OF BIRD ENTERING CORE. PERFORMED BORO OF HPC PER AMM 72-00-07 TASK 290-869, ALL OK. 2 L 7 3 4F 4 F RT A22WE E24NE 1999110500692 19991105 00692 NM 1999 11 5 DL72W992425 1 19991102 A 2611 SMOKE DETECTOR 7213 BOEING 727 7272Q8 138407W NM LAVATORY ACTIVATED A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 831L 2829 21826 ON FINAL APPROACH, LAV SMOKE LIGHT ILLUMINATED, F/A SMELLED SMOKE IN RT AFT LAV. INSPECTED RT AFT LAV, NO EVIDENCE OF SMOKE. LIGHTS ALL CHECKED GOOD. REPLACED SMOKE DETECTOR AS A PRECAUTION, TEST GOOD. 2 L 7 3 4F A3WE 1999110500693 19991105 00693 NM 1999 11 5 DL72S992426 1 19991101 A 5320 WEB BOEING 727 727232 1384082 NM BS 1323 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 A .25 INCH CRACK AT LIGHTENING HOLE IN TORQUE BOX OF 48 SEC, STA 1323 LEFT SIDE. ROUTED OUT DAMAGED AREA PER M/M 53-11- 0, DYE CHECK OK. 2 L 7 3 4F A3WE 1999110500694 19991105 00694 NE 1999 11 5 DL73K992427 2 19991102 A 7230 COMPRESSOR BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE BIRD SRTIKE A DALA O OTHER C F.O.D. AP APPROACH 1 SO 27 313DL 40915 23085 709164 ON APPROACH BOS CREW REPORTED POSSIBLE BIRD STRIKE. INSPECTION FOUND DAMAGE TO NR 2 ENGINE FAN BLADES. DRESSED BLADES TO LIMITS OF 5 FLIGHTS FLY BACK LIMITS. RAN ENGINE TO TAKEOFF POWER. ALL PARAMETERS AND OPERATION NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 1999110500695 19991105 00695 NM 1999 11 5 DL72S992428 1 19991102 A 5320 FRAME BOEING 727 727232 1384082 NM R-1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 FOUND ON C2 LETTER CHECK, 1.5 INCH CRACK ON R-1 DOOR FWD FRAME AT THE LOWER STOP CASTING. REPAIRED PER ERA AND MM 52-1 2-0. 2 L 7 3 4F A3WE 1999110500696 19991105 00696 NM 1999 11 5 DL72S992429 1 19991102 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 A .125 INCH CRACK IN NR 2 L/E FLAP ACTUATOR SUPPORT BOX INBD LWR BRACKET. INSTALLED DOUBLER PER M/M 57-20-21. 2 L 7 3 4F A3WE 1999110500697 19991105 00697 NM 1999 11 5 DL777992430 1 19991102 A 2530 1105011 COFFEE MAKER BOEING 777 777232 1385232 NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 860DA 29951 LEFT COFFEEMAKER POPPED. RESETTING CENTER C/B CAUSES ARCING IN AFT COFFEEMAKER. ISOLATED PROBLEM TO NR 2 C/M IN LEFT A FT GALLEY. PULLED AND COLLARED POWER C/B FOR NR 2 C/M. FWD TO MCO AND PLACARD. C/M NASI LGW. 2 L 7 2 4F RT T00001SE 1999110500698 19991105 00698 NM 1999 11 5 VNAA9911001 1 19991101 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 441JS 10268 3815 3059 HL325 WHILE PREPARING TO TAXI, FLIGHT 4097 COULD NOT GET THE RIGHT HAND PROPELLER OUT OF FEATHER. MAINTENANCE INSPECTED AND R EPLACED THE PROPELLER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OPERATIONAL CHECKS WERE COMP LETED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500699 19991105 00699 NE 1999 11 5 VNAA9911002 2 19991101 A 7532 311995704 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 07 430JS 6180 3044 E116118 DURING FLIGHT THE AIRCRAFT HAD A 20 PERCENT TORQUE FLUCTUATION ON THE RIGHT HAND ENGINE. THE AIRCRAFT LANDED WITHOUT AN Y INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND INLET BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-31-01. OPERATIONAL CHECKS WERE COMPLETED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00 AND THE AIRC RAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999110500700 19991105 00700 NE 1999 11 5 S84A101 2 19991021 A 7261 COVER BOEING 727 727276 138408R NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A S84A A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 21 908PG 20951 DEPARTED ST LOUIS EN ROUTE MBJ, DIVERTED INTO MIAMI - FLT 301 - NR 3 ENGINE OIL QUANTITY HAD SLOW DROP, ENGINE SHUT DOW N AT ALTITUDE, 35 PSI OIL PRESSURE AFTER SHUT DOWN. FOUND MAIN OIL SCREEN GASKET DAMAGED AND COVER LEAKING. REMOVED AN D REPLACED OIL SCREEN, REPLACED GASKET IAW P & W MM 72-61-8. LEAK CHECKED GOOD. (X) 2 L 7 3 4F 4 F RT A3WE E2EA 1999110500701 19991105 00701 NM 1999 11 5 AALA991224 1 19990818 A 3350 SOCKET GRIMES BOEING 757 757223 1384957 NM RT EMRG EXIT CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AN 29425 ORD - DURING OVERNIGHT MAINTENANCE, RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. CLEANED CORRODED LIGHT SOCKET. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999110500702 19991105 00702 EU 1999 11 5 99ZZZX4163 1 19990925 A 2822 9A2045 CARTRIDGE GLOBE UROCOP EC135 EC135P1 8680990 EU FUEL PUMP INOPERABLE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 412 156 EC1350054 FUEL PUMP INOPERABLE. NO FUEL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999110500703 19991105 00703 EU 1999 11 5 99ZZZX4164 1 19990926 A 7714 56337078012 INDICATOR SEXTANT SNIAS 350 AS350B2 8680813 EU COCKPIT FLUCTUATES A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 256 991 2575 NG NEEDLE FLUCTUATES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999110500704 19991105 00704 NE 1999 11 5 99ZZZX4165 2 19990610 A 7321 0164248820 FCU SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE FUEL SYSTEM LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 473 48 C242B 2917 9431 FCU LEAKING FUEL BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 1999110500705 19991105 00705 EU 1999 11 5 99ZZZX4166 1 19990815 A 2840 1135020019 SWITCH SNIAS 350 AS350B2 8680813 EU FUEL PRESSURE INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 101LN 407 3926 3038 FUEL PRESSURE SWITCH OPERATES INTERMITTENTLY. FLICKERS IN-FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999110500706 19991105 00706 NE 1999 11 5 99ZZZX4167 2 19990908 A 7532 9550164960 BLEED VALVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 101LN 445 395 3038 9533 BLEED VALVE INOPERATIVE. CLOSES AT 98 PERCENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 1999110500707 19991105 00707 NM 1999 11 5 AALA991547 1 19991017 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 6E DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 681AA 25338 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON RIGHT SIDE AND AFT OF SEAT 6E INOPERATIVE. REPLACED EMERGEN CY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999110500708 19991105 00708 NM 1999 11 5 AALA991550 1 19991015 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 643AA 24601 DFW - DURING OVERNIGHT MAINTENANCE AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTING HAS A BULB INOPERATIVE. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHTING STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999110500709 19991105 00709 NM 1999 11 5 AALA991553 1 19991017 A 3397 WIRE BOEING 757 757223 1384957 NM ROW 8DEF BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 684AA 25341 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM SEAT ROW 8DEF TO 17DEF INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING WIRING AT MID-CABIN AREA. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999110500710 19991105 00710 NM 1999 11 5 AALA991554 1 19991018 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 25H DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385AM 27059 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTS AT SEAT ROW 25H INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT SEAT CONNECTOR AT SEAT ROW 25H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999110500711 19991105 00711 NM 1999 11 5 AALA991524 1 19991009 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661AA 25295 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING AND MOST OF MAIN CABIN INOPERATIVE. R EPAIRED FLAT WIRE FOR EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999110500712 19991105 00712 NM 1999 11 5 AALA991545 1 19991015 A 3397 WIRE BOEING 757 757223 1384957 NM ROW 27DEF LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 627AA 24585 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 27DEF INOPERATIVE. RE-SECURED WIRE TO EMERG ENCY EXIT FLOOR PATH LIGHT AT SEAT 27DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999110500713 19991105 00713 NM 1999 11 5 AALA991543 1 19991014 A 3350 1001191 LIGHT GRIMES BOEING 757 757223 1384957 NM L2 DOORWAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 626AA 24584 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT AT L2 DOORWAY INOPERATIVE. REPLACED PORTABLE EMERGENC Y EXIT LIGHT AT L2 DOORWAY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999110500714 19991105 00714 NM 1999 11 5 AALA991452 1 19990926 A 2711 652172642K TRIM TAB BOEING 727 727223 1384074 NM RT AILERON DEFECTIVE A AALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 07 869AA 21374 MIA - FLT 1360 - EN ROUTE MIA/DCA AT 30,000 FEET WITH AIRSPEED OF 305 KNOTS AND ECON CLIMB THERE WAS A NOTICEABLE FLUTTE R IN YOKE. INSPECTED AILERON IN-FLIGHT AND NOTICED RIGHT INBOARD AILERON FLUTTER APPROXIMATELY 3 SECONDS AFTER A TURN I N EITHER DIRECTION. AIR INTERRUPTED AND LANDED MCO WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CO NDITION FOR FERRY FLIGHT TO MIA FOR FURTHER EVALUATION OF AILERON FLUTTER. FERRY FLIGHT TO MIA AND LANDED WITHOUT INCID ENT. REPLACED RIGHT INBOARD AILERON TRIM TAB AND ADJUSTED PER MM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999110500715 19991105 00715 NM 1999 11 5 AALA991334 1 19990907 A 3610 39271611 VALVE BOEING 727 727223 1384074 NM NR 3 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 843AA P1220 20984 DFW - FLT 0092 - AFTER TAKEOFF DFW/EWR, CREW WAS UNABLE TO CONTROL PRESSURIZATION. AIRCRAFT RETURNED TO DFW, DUMPED FUE L, AND LANDED WITHOUT INCIDENT. REPLACED NR 3 ENGINE 13TH STAGE MODULATING VALVE. ACCOMPLISHED CHECK OF BLEED AND PRES SURIZATION SYSTEM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999110500716 19991105 00716 NM 1999 11 5 AALA991269 1 19990824 A 3260 MS250081 SWITCH BOEING 727 727223 1384074 NM LT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 875AA 21387 PHL - FLT 1845 - AFTER TAKEOFF PHL/MIA - ALL 3 RED GEAR WARNING LIGHTS AND TAIL SKID LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. AIRCRAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO LGA. REPLACED LANDING GEAR HANDLE DOWN SWITCH. ALSO, REPLACED LEFT MAIN LANDING GEAR DOWNLOCK PROXIMITY SENSOR. ACCOMPLISHED GEAR RETRACTION CHEC K. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999110500717 19991105 00717 NM 1999 11 5 AALA991266 1 19990824 A 3260 AAP2448A UNIT BOEING 727 727223 1384074 NM E/E COMP DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 875AA R00005R 21387 PHL - FLT 0880 - AFTER TAKEOFF MIA/PHL - GEAR AND TAIL SKID UNSAFE LIGHTS REMAINED ILLUMINATED WHEN GEAR HANDLE WAS IN U P AND OFF POSITION. GEAR OPERATION WAS NORMAL. AIRCRAFT LANDED PHL WITHOUT INCIDENT. REPLACED LANDING GEAR ACTUATION UNIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999110500718 19991105 00718 NM 1999 11 5 AALA991539 1 19991012 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 29B FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7375A 25202 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 29B INOPERATIVE. REPAIRED CONNECTOR TO EMER GENCY EXIT FLOOR PATH LIGHT AT SEAT 29B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999110500719 19991105 00719 WP 1999 11 5 AALA991488 1 19991002 A 2810 698640 SEAL DOUG DC10 DC1030 3023501 WP LT WING DEFECTIVE A AALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 07 143AA 46555 LAX - FLT 0143 - EN ROUTE DFW/HNL, 1-1/2 HRS INTO FLIGHT, A PASSENGER NOTICED A FUEL STREAM COMING FROM THE TOP LEFT WIN G WHICH WAS CONFIRMED. NO MEASUREABLE FUEL LOSS ACCORDING TO FUEL GAUGES. DUMPED FUEL, AIR INTERRUPTED, AND LANDED AT LAX WITHOUT INCIDENT. REPLACED SEAL ON INBOARD PANEL 531, LEFT WING. ACCOMPLISHED LEAK CHECK OF PANEL. NO LEAKS NOTED . TRANSFERRED 40,000 POUNDS OF FUEL TO LEFT TANK DURING TESTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1999110500720 19991105 00720 WP 1999 11 5 AALA991464 1 19990927 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 225AA 49175 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999110500721 19991105 00721 NE 1999 11 5 AALA991367 2 19990909 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 590AA 53253 725786 SJC - FLT 0740 - ON TAKEOFF SJC/DFW, BOTH LEFT AND RIGHT AIR CONDITIONING SUPPLY HIGH TEMPERATURE LIGHTS ILLUMINATED. H IGH PRESSURE BLEED AIR SUPPLY WAS SHUT OFF AND LIGHTS EXTINGUISHED. STRONG FUEL ODOR DETECTED IN CABIN. AIRCRAFT RETUR NED TO SJC AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F 4 F RT A6WE E9NE 1999110500722 19991105 00722 NE 1999 11 5 AALA991253 2 19990821 A 7250 TURBINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE FAILED A AALA L ABORTED APPROACH X ENGINE FLAMEOUT LD LANDING 1 SW 07 7550 53032 725773 MIA - FLT 1381 - DURING GO-AROUND FOR LANDING AT MIA, NR 2 ENGINE FAILED AND SPOOLED DOWN. RE-START WAS NOT ATTEMPTED. AIRCRAFT LANDED MIA WITHOUT INCIDENT. REPLACED NR 2 ENGINE. PERFORMED ENGINE RUN-UP. SYSTEM GROUND CHECKED, NORMAL O PERATION. (X) 2 L 7 2 4F 4 F A6WE E9NE 1999110500723 19991105 00723 NM 1999 11 5 AALA991497 1 19991001 A 5320 FITTING BOEING 727 727227 1384078 NM BS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STRINGER END FITTING CORRODED AFT OF THE LAVATORY PANEL, STR 22L, STA 1183. REMOVED AND REPLACED END FITTING PER SRM 51-10-01. TST: 73,038 HOURS. CYCLES: 48,641. (X) 2 L 7 3 4F A3WE 1999110500724 19991105 00724 NM 1999 11 5 AALA991508 1 19991002 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1166-1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STR 22L CORRODED FROM STA 1166 - STA 1183 AND STRINGER CLIPS AND END FITTING BELOW LAVATORY SERVICE PANEL. DESIGN LEAK. CUT OUT CORRODED PIECES OF STRINGER, REMOVED AND REPLACED STRINGER. INSTALLED SPLICE AND NEW END FITTING AND CL IPS PER SRM 53-10-3, FIG 1. TST: 73,038 HOURS. CYCLES: 48,641. (X) 2 L 7 3 4F A3WE 1999110500725 19991105 00725 NM 1999 11 5 AALA991473 1 19990925 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 910 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - H-FITTING CRACKED AT FORWARD LUG (UPLOCK SUPPORT FITTING) RIGHT MAIN LANDING GEAR WHEELWELL. REPLACED H-FITTING W ITH NEW PART. TST: 73,027 HOURS. CYCLES: 48,643. (X) 2 L 7 3 4F A3WE 1999110500726 19991105 00726 NM 1999 11 5 AALA991474 1 19990925 A 5320 WEB BOEING 727 727227 1384078 NM BS 913 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL- H-FITTING SUPPORT BOX AFT STRUCTURE CRACKED AT FASTENER HOLE (RIGHT MAIN GEAR WELL). REPLACED BOX STA 913 WEB WITH NEW PART. TST: 73,027 HOURS. CYCLES: 48,643. (X) 2 L 7 3 4F A3WE 1999110500727 19991105 00727 NM 1999 11 5 AALA991476 1 19990925 A 5312 BULKHEAD BOEING 727 727227 1384078 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CRACK ON 1183 BULKHEAD, RBL 10, 8 INCHES UP FROM LOWER FRAME. INSTALLED DOUBLER PER SRM 53-10-2, PAGE 28. TST: 7 3,027 HOURS. CYCLES: 48,643. (X) 2 L 7 3 4F A3WE 1999110500728 19991105 00728 WP 1999 11 5 AALA991470 1 19990924 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 711 - 698 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - CORROSION IN SEVERAL PLACES AT ROLLER TRAY STA 711 - STA 745, STA'S 698, 697, 678. SPLICED IN SECTION OF TRAY PE R SRM 53-70-00, PAGE 41. TST: 64,254 HOURS. CYCLES: 20548. (X) 2 L 7 3 4F A22WE 1999110500729 19991105 00729 NM 1999 11 5 AALA991537 1 19991005 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1110 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 871AA 21383 TUL - ONE INCH LONG CRACK IN FUSELAGE SKIN SIX FEET FORWARD OF TAIL SKID. SJU REPORTS CORROSION IN AREA OF CRACK. CRAC KED/CORRODED SKIN AND SHEAR TIE REMOVED AND REPLACED WITH NEW SHEAR TIE AND SKIN DOUBLER T3-2024-0.071 INCH PER REPAIR S RM 53-30-3, FIG 1. TST: 59,320 HOURS. CYCLES: 35,833. (X) 2 L 7 3 4F A3WE 1999110500730 19991105 00730 NM 1999 11 5 AALA991541 1 19991007 A 5330 SKIN BOEING 727 727223 1384074 NM BS 415 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 873AA 21385 TUL - LOWER AFT CORNER OF FORWARD GALLEY DOOR CUT-OUT FUSELAGE SKIN CRACKED. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SB 727-53-0188. TST: 59,297 HOURS. CYCLES: 35,868. (X) 2 L 7 3 4F A3WE 1999110500731 19991105 00731 NM 1999 11 5 AALA991536 1 19991008 A 5320 DOUBLER BOEING 727 727227 1384078 NM BS 1166-1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - EXFOLIATED CORROSION ON INTERNAL SKIN DOUBLER STR 22L, STA 1166 - STA 1183. INSTALLED DOUBLER REPAIR PER SRM 53-3 0-2, FIG 3A, AARD 51-20-01-5. TST: 73,038 HOURS. CYCLES: 48,641. (X) 2 L 7 3 4F A3WE 1999110500732 19991105 00732 EU 1999 11 5 C2XA99IA527 1 19991010 A 5311 S5317220820001 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, FRAME NINE LEFT WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF FRAME A ND INSTALLED A SPLICE REPAIR IAW ATR 42-320 SRM 53-11-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500733 19991105 00733 EU 1999 11 5 C2XA99IA528 1 19991010 A 5311 S5317220820101 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, FRAME NINE RIGHT WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF FRAME AND INSTALLED A SPLICE REPAIR IAW ATR 42-320 SRM 53-11-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT : 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500734 19991105 00734 EU 1999 11 5 C2XA99IA529 1 19991010 A 5320 S5367800920102 SUPPORT AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT UNDER THE PASSENGER DOOR THRESHOLD FROM FRAME 36 TO FRAME 38 WAS FOUN D CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500735 19991105 00735 EU 1999 11 5 C2XA99IA530 1 19991010 A 5320 S5367800826901 SUPPORT AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT UNDER THE PASSENGER DOOR THRESHOLD FROM FRAME 38 TO FRAME 39 WAS FOUN D CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500736 19991105 00736 EU 1999 11 5 C2XA99IA531 1 19991010 A 5347 S5367800124000 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK WAS FOUND CORRODED FROM FRAME 29 TO FRAME 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR 42-320 SRM 51-21-42, AND THE AIRCRAFT WAS RETURNED TO S ERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500737 19991105 00737 EU 1999 11 5 C2XA99IA532 1 19991010 A 5311 S53572500200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, FRAME 29 WAS FOUND CORRODED BETWEEN S20L AND S20R. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED SECTION OF FRAME 29 IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT T T: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500738 19991105 00738 EU 1999 11 5 C2XA99IA533 1 19991010 A 5320 S5367131827401 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 WAS FOUND CORRODED. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED FLOOR SUPPORT IAW ATR 42-320 SRM 51-25-02, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500739 19991105 00739 EU 1999 11 5 C2XA99IA534 1 19991010 A 5347 S53570201204 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 34 AND 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE ARICRAFT WAS APPROVED FOR R ETURN TO SERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500740 19991105 00740 EU 1999 11 5 C2XA99IA535 1 19991010 A 5347 S53570201204 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 34 AND 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500741 19991105 00741 EU 1999 11 5 C2XA99IA536 1 19991010 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER SEAT TRACK WAS FOUND CORRODED BETWEEN FRAMES 39 AND 40. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500742 19991105 00742 EU 1999 11 5 C2XA99IA537 1 19991010 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLIGHT ATTENDANT SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500743 19991105 00743 EU 1999 11 5 C2XA99IA538 1 19991010 A 5347 S5378001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FIGHT ATTENDANT SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. ACFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500744 19991105 00744 EU 1999 11 5 C2XA99IA522 1 19991006 A 3350 7012210 BULB AEROSP ATR42 ATR42320 8680930 EU PASSENGER DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 IAH - DURING MAINTENANCE INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999110500745 19991105 00745 EU 1999 11 5 C2XA99IA524 1 19991011 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING 2A INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999110500746 19991105 00746 EU 1999 11 5 C2XA99IA523 1 19991006 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT 18WL IAW ATR 42-320 MM 3351-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999110500747 19991105 00747 SO 1999 11 5 C2XA99CL110 1 19991017 A 3610 S2U2226 SEALS EMB 145 EMB145LR SO CARGO COMPT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 14953 145071 MCI - FLT 4108 - PILOT REPORTED A BAGGAGE SMOKE WARNING INDICATION WAS NOTED DURING FLIGHT. THE ACFT RETURNED TO MCI WT HOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND THE LEFT BLEED SYSTEM WAS FOUND LEAKING IN THE CARGO BAY. THE SE ALS ON THE BLEED TUBE GAMA JOINT WERE FOUND HARDENED AND BROKEN ALLOWING THE RETAINING SLEEVE TO FALL OUT OF POSITION. S UBSEQUENT DAMAGE OCCURRED TO WIRING GOING TO THE BLEED LEAK SENSOR AT THE GAMA JOINT. THE AIRCRAFT WAS FERRIED TO BTV W HERE MAINT REPLACED THE AFFECTED SEALS, GAMA JOINT CLAMP, AND PERFORMED REPAIRS TO THE WIRING DAMAGE. ACFT APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 1999110500748 19991105 00748 EU 1999 11 5 C2XA99IA526 1 19991010 A 5315 S53172206258 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME NINE WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTIO N OF FLOORBEAM AND INSTALLED A REPAIR DOUBLER IAW ATR 42-320 SRM 51-70-00 AND SRM 53-11-00, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. ACFT TT: 20,771.1. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999110500749 19991105 00749 EU 1999 11 5 PLGA990921A 1 19990921 A 7110 7271110604 COWL SAAB SF340 340B 7860101 EU LT NACELLE DAMAGED A PLGA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 NE 05 348BE 340B190 BOS - FLT 4859 - SHORTLY AFTER TAKEOFF, CREW NOTED THE LEFT INBOARD ENGINE COWLING OPENED IN-FLIGHT. CREW RETURNED TO B OS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE COWLING ASSEMBLY AND CHECKED FIT AND SECURITY, ALL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1999110500750 19991105 00750 NM 1999 11 5 TSAA9933437 1 19990918 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. TAT: 31,375. 7 HOURS. TAC: 37,575. (X) 2 L 7 2 4F A16WE 1999110500751 19991105 00751 WP 1999 11 5 USAA991106 1 19991008 A 5320 WEB DOUG DC9 DC981 3022081 WP BS 1338 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND 6 INCH BY 1 INCH AREA OF CORROSION AT WEB AT STA 1338 AT LONGERON 18R (RT AFT LAVATORY). C ORROSION TASK NR C58-53300. CORROSION LEVEL: 1. CUT OUT DAMAGED AREA OF THE WEB AND SPLICED IN NEW SECTION PER SRM 53 -01, FIG 2, AND SRM 53-14-3, FIG 7. (X) 2 L 7 2 4F A6WE 1999110500752 19991105 00752 WP 1999 11 5 USAA991107 1 19991008 A 5312 BULKHEAD DOUG DC9 DC981 3022081 WP BS 160 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND UPPER LEFT CUSP HANDLE 2 INCH BY 3 INCH CORRODED AT STA 160 AT AIRSTAIRS FORWARD BULKHEAD L EFT CORNER. INSTALLED DOUBLER PER EA 52924. (X) 2 L 7 2 4F A6WE 1999110500753 19991105 00753 WP 1999 11 5 USAA991108 1 19991008 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 160 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND .50 INCH CRACK AT FRAME ATTACH POINT AT STA 160 LONGERON 3 LEFT. INSTALLED SPLICE PER SRM 53-02, FIG 18. (X) 2 L 7 2 4F A6WE 1999110500754 19991105 00754 WP 1999 11 5 USAA991109 1 19991008 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 160 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND .50 INCH LONG CRACK AT FRAME ATTACH POINT AT STA 160. INSTALLED SPLICES PER SRM 53-02 FIG 18. (X) 2 L 7 2 4F A6WE 1999110500755 19991105 00755 WP 1999 11 5 USAA991110 1 19991008 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 160 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND 1 INCH CRACK AT FRAME STA 160 LONGERON 2 LEFT. INSTALLED SPLICES PER SRM 53-02 FIG 18. (X ) 2 L 7 2 4F A6WE 1999110500756 19991105 00756 WP 1999 11 5 USAA991111 1 19991008 A 5321 FLOOR DOUG DC9 DC981 3022081 WP BS 160-200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND 2 FOOT BY 3 FOOT CORRODED AREA AT SUB-FLOOR AT STA 160 - STA 200 AND BETWEEN CENTERLINE OF AIRCRAFT AND RT INBOARD SEAT TRACK. CORROSION TASK NR C46-53303 CORROSION LEVEL 1. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHT 3 PER SRM 53-01. (X) 2 L 7 2 4F A6WE 1999110500757 19991105 00757 NM 1999 11 5 USAASB99251 1 19991018 A 3350 20121 BATTERY CHARGER BOEING 737 737401 1384701 NM LT EMERG EXIT FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 CLT - MAINTENANCE FOUND THE LEFT AISLE EMERGENCY LIGHT ABOVE THE LEFT AFT EMERGENCY EXIT WINDOW INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999110500758 19991105 00758 NM 1999 11 5 USAASB99253 1 19991016 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 779AU 24996 EWR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT THE FORWARD MAIN ENTRY DOOR WOULD NOT ILLUMINATE. MAINTENANCE REMO VED AND REPLACED THE M1133 BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999110500759 19991105 00759 1999 11 5 USAASB99230 4 19990916 A 3417 HG480B42 ADC BOEING 737 7373B7 1384580 NM E/E COMPT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 389US 34850 23311 PIT - FLT 1764 - EN ROUTE FROM PIT TO PWM DURING CRUISE AT FL 370, THE CAPTAIN'S ALTIMETER, AIRSPEED INDICATOR AND VSI B ECAME INOPERABLE. NO CHANGE OCCURRED WITH CLIMB AND DESCENT FOR 15 MINUTES. FLIGHT RETURNED TO FIELD AT PIT AND WHILE ON DESCENT INTO PIT, INDICATORS BEGAN OPERATING INTERMITTENTLY. ON GROUND, INDICATORS OPERATED NORMAL. NO EMERGENCY WA S DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA COMPUTER. OPERATIONAL CHECK OF AIR DATA COMPUTER AND AS SOCIATED INDICATORS WAS NORMAL. (X) 2 L 7 2 4F RT A16WE 1999110500760 19991105 00760 EU 1999 11 5 USAASB99250 2 19991017 A 7230 TURBINE BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563B2 13802 EU LT ENGINE FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 19 423US 33180 3893 23990 720862 GSO - FLT 1046 - DURING CRUISE AT APPROXIMATELY FL 290, THE CREW HEARD A LOUD BANG FROM THE LEFT SIDE OF THE ACFT WITH F LUCTUATIONS OF THE LT ENGINE GAUGES. ENGINE INDICATIONS RETURNED TO NORMAL AND THE CREW CONTINUED FLIGHT. SHORTLY THER EAFTER, ANOTHER LOUD BAG WAS HEARD ACCOMPANIED WITH ENGINE VIBRATION AND ADDITIONAL ENGINE INDICATION FLUCTUATIONS. CAP TAIN ELECTED TO REDUCE THE LEFT ENGINE TO IDLE THRUST AND DIVERT TO GSO, THE NEAREST AIRPORT. FLIGHT LANDED WITHOUT FUR THER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE TURBINE SEIZED ON THE LEFT ENGINE ASSY. REMOVED AND R EPLACED THE LEFT ENGINE ASSEMBLY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F RT A16WE E21EU 1999110500761 19991105 00761 NM 1999 11 5 USAASB99227 1 19990910 A 2751 2061141 INDICATOR BOEING 737 737301 1384611 NM TE FLAP FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 573US 29535 23560 CLT - FLT 2250 - AFTER TAKEOFF WHEN FLAPS WERE RETRACTED FROM 5 DEGREES TO 1 DEGREE, FLAP TRAVEL STOPPED AT APPROXIMATEL Y 1-3/4 DEGREE POSITION WHILE LEADING EDGE REMAINED EXTENDED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND CLEANED CANNON PLUGS ON FLAP ASYMMETRY SWI TCH. CYCLED FLAPS SEVERAL TIMES UP AND DOWN. OPERATIONAL CHECK GOOD. NO FAULTS NOTED. (X) 2 L 7 2 4F RT A16WE 1999110500762 19991105 00762 NM 1999 11 5 USAABB99042 1 19990907 A 3244 TIRES BOEING 757 757225 1384959 NM RT MLG FAILED A USAA O OTHER A FLAME/FIRE LD LANDING 1 EA 19 602AU 22196 BOS - FLT 2325 - ON LANDING AT BOS, ALL FOUR RIGHT MLG TIRES BLEW. TOWER REPORTED TO THE CREW THAT THERE WAS A FIRE IN THE WHEEL WELL. CRASH CREWS MET THE AIRCRAFT AND THE PASSENGERS WERE DEPLANED ON THE RUNWAY. MAINTENANCE REPLACED NUME ROUS PARTS, MOST NOTABLY THE LOWER CYLINDER AND TRUCK ASSEMBLY. THE AIRCRAFT WAS FLYING WITH THE ANTI-SKID SYSTEM AND T HE RIGHT THRUST REVERSER ON MEL. THE CAUSE OF THE FIRE IS BELIEVED TO BE THAT ON THE WET RUNWAY UNDER THE SPECIFIC AIRC RAFT CIRCUMSTANCES, THAT THE RIGHT SIDE BRAKES LOCKED, CAUSING THE TIRES TO BLOW AND SUBSEQUENTLY CATCH FIRE. (M) 2 L 7 2 4F RT A2NM 1999110500763 19991105 00763 NM 1999 11 5 USAABB99046 1 19991006 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM ROW 29 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 PHL - FOUND AISLE EMERGENCY LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F RT A2NM 1999110500764 19991105 00764 NM 1999 11 5 USAASB99246 1 19991010 A 2410 731753 CSD BOEING 737 7372B7 1384560 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 267AU 36183 22879 MCO - FLT 2646 - FLIGHT DEPARTED MIA WITH THE NR 1 GENERATOR ON MEL. DURING CRUISE, THE NR 2 GENERATOR LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE NR 2 CSD AND DIVERTED TO MCO WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT . NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE CSD PER MM AND REMOVED AND REPLACED THE CSD OIL COOLER (P/N 6A47-000) AS PRECAUTIONARY. OPERATIONAL CHECK AND LEAK CHECK GOOD. LIKEWISE, MAINTENANCE CLEARED T HE MEL ON THE NR 1 ENGINE GENERATOR BY REMOVING AND REPLACING THE NR 1 ENGINE CSD AND THE OIL COOLER. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F A16WE 1999110500772 19991105 00772 CE 1999 11 5 99ZZZX4175 1 19990913 A 3244 10X55 TIRE GOODYEARAERO BEECH 99 99 1154002 CE MLG DAMAGED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 24BH 82090135 U67 A NEW TIRE WITH 151 CYCLES INSTALLED ON 9-13-99. DURING INSPECTION, FOUND TIRE TREAD SPLIT AND SEPARATED THE SAME DIREC TION AS TIRE GROOVES. 1 L 7 2 3T A14CE 1999110500773 19991105 00773 NE 1999 11 5 USAASA99007 2 19991013 A 7200 ENGINE AIRBUS A319 A319112 EU CFMINT CFM565 CFM565B6 13802 NE LEFT OVERSPEED A USAA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 EA 19 705UW 2811 0929 779436 DEN/PHL - FLT 140 - AFTER TAKEOFF, FLIGHT CREW WAS ALERTED TO A LEFT ENGINE N2 OVERSPEED. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD. 28 MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A28NM E37NE 1999110500774 19991105 00774 EU 1999 11 5 C2XA99IA525 1 19991008 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE INSPECTION, THE AFT SECTION OF EMERGENCY FLOOR LIGHTS WAS FOUND INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999110500775 19991105 00775 EU 1999 11 5 C2XA99IA539 1 19991010 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABLE DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT BATTERY PACK AT 30WL WAS FOUND DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR 42-320 JIC 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A CFT TT: 20,771.1 HOURS. CYCLES: 23,768. (X) 2 H 7 2 4T RT A53EU 1999111100001 19991111 00001 WP 1999 11 11 TWAA9915001 1 19991103 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP PAX DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING CHECK-C MAINT, FOUND 3 CRACKS IN INTERNAL SKIN DOUBLER AT FWD ENTRY DOOR CUTOUT. CRACKS WERE 3 INCHES, 1.75 IN, AND .75 IN. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR PER SRM 53-05, FIG 25A AND ARA 16407. 2 L 7 2 4F A6WE 1999111100002 19991111 00002 SO 1999 11 11 LR7A9963 1 19991101 A 2150 203430 PACK LKHEED 382 382G 526414U SO FS 215 FAILED A LR7A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 401LC 1126 4606 FLIGHT CREW NOTED SMOKE AND LOUD NOISE FROM FLT DECK AIR CONDITIONER PACK. TRANSFERRED TO DMI NR 00618 PER MEL 21-1. R EMOVED AND REPLACED FLT DECK COOLING TURBINE ASSY DUE FAILED IAW MM SMP 581-21-50-00, PG 206. OPS AND LEAK CHECKS GOOD. CLEARED DMI 00618 AT 28663 TAT. 2 H 7 4 4T A1SO 1999111100003 19991111 00003 1999 11 11 JBXA9900120 4 19991103 A 2300 COMM SYS FOKKER F28 F28MK0100 4990807 EU NR 1 &2 TRIPPED A JBXA O OTHER O OTHER CL CLIMB 1 SO 05 105ML 11475 FLIGHT 119 FROM FLL TO RDU, ON CLIMBOUT NR 1 AUDIO FAILED AND BACK-UP SYSTEM DID NOT WORK, COMPLETE COM FAILURE. RESET NR 1 AMU AND NR 2 AMU AND ALT AMU. PERFORMED OPERATIONAL CHECK IAW F-100 MM 23-51-00, OPERATIONAL CHECK GOOD. RESET NR 1 AND NR 2 VHF COMS AND PERFORMED OPERATIONAL CHECK IAW F-100 MM 23-12-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT 1999111100004 19991111 00004 EU 1999 11 11 AWXA9900389 1 19991101 A 2932 501310000 SWITCH AIRBUS 320 A320231 3930325 EU NR 1 HYD SYS MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION CL CLIMB 1 WP 28 631AW 077 AFTER TAKEOFF LAS, ECAM MSG ENG 1 HYD LOW PRESS HAD INDICATION NR 2 ENG LOW PRESS HYD PUMP. HOWEVER RETURNED TO NORMAL, OPS CHECK NORMAL REST OF FLIGHT. REPLACED GREEN SYS PRESS SW 1074GK, ON NR 1 ENG LEAK AND F/C GOOD PER AAM CHAPTER 29. HYD LINE CHANGED ON NR 2 ENG 09/09/99. 2 L 7 2 4F RT A28NM 1999111100005 19991111 00005 EU 1999 11 11 AWXA9900390 1 19991101 A 3411 5062010 PITOT AIRBUS 320 A320231 3930325 EU FUSELAGE MALFUNCTIONED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 28 627AW 66 CONDITION: ABORTED TAKE-OFF NO F/O AIRSPEED INDICATION LP 7552885DISCREPANCY: TAKE-OFF REJECTED @90KTS DUE TO NO AI RSPEED INDICATION ON FO SIDECORRECTIVE ACTION: R+R F/O PITOT PROBE PER AMM 13-11-15-109--PITOT STATIC LK CHECK NML AND PRBES R+R'D AIR DATA MODULE AS A PRECAUTION--CHECKED PITOT LINES FROM ADM AND PROBE--NO F AULT FOUNDCURRENT HISTORY: ATA 341 ONE UN-RELATED WRITE-UP IN 90 DAY LOOK BACKRECOMMENDATION: REMAIN OPEN PENDING TEAR DOWN REPORT 2 L 7 2 4F RT A28NM 1999111100006 19991111 00006 NM 1999 11 11 AWXA9900391 1 19991101 A 3297 W4920AAA WIRE BOEING 757 7572S7 1384962 NM RT MLG CHAFED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 905AW 23567 AFTER GEAR RETRACTION LANDING GEAR MONITOR EICAS MSG APPEARED. FOUND PROXIMITY SENSOR RT MLG INBOARD WIRING DOWN AND LO CK SENSOR HAD A CHAFED WIRE. REPAIRED WIRING PER MM CHAPTER 20 BITE OF THE PSEU, OPS CHECK GOOD RT MLG DOWNLOCK SENSOR . 2 L 7 2 4F RT A2NM 1999111100007 19991111 00007 NM 1999 11 11 AWXA9900392 1 19991102 A 7331 WIRE BOEING 737 7372U9 1384498 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL FLOW CHAFED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 149AW 22575 BOTH F/F INDICATORS STARTED FLUCTUATING BETWEEN 500-4000 PPH ON CLIMBOUT. CONTINUED THROUGHOUT REMAINDER OF FLIGHT. FO UND WIRE CHAFED AT F/F TRANSMITTER OF NR 1 ENG. REPAIRED AND REPOSITIONED WIRES TO PREVENT FURTHER CHAFING, OPS CK GOOD ON HI PWR ENG RUN. A/C HAS SIGNIFICANT HISTORY OF WIRE REPAIR ON LT & RT ENG. 2 L 7 2 4F 4 F RT A16WE E2EA 1999111100008 19991111 00008 NM 1999 11 11 AWXA9900393 1 19991103 A 2742 AR7077M3 ACTUATOR BOEING 737 7373Q8 1384670 NM HORZ STAB MALFUNCTIONED A AWXA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 28 327AW 29661 6787 23507 REF LOG SQUAWK UNCOMMANDED PITCH TRIM AS A CAUTION. MX REQUEST REPLACE STAB TRIM MOTOR. REPLACED STAB TRIM ACTUATOR MO TOR AS PER CARD R6C27001, OPS CK GOOD. TT 0102894 2 L 7 2 4F RT A16WE 1999111100009 19991111 00009 NM 1999 11 11 AWXA9900394 1 19991102 A 3397 BMS13131122 WIRE BOEING 737 737277 1384570 NM ROW 11 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 EMERGENCY AISLE LIGHTING ROW 11 INOP. REPAIRED BROKEN WIRE, CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1999111100010 19991111 00010 EA 1999 11 11 COMA9960668 1 19991102 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA RT EMER EXIT FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 963CA 7127 AFT OVERWING EMERGENCY EXIT LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999111100011 19991111 00011 EA 1999 11 11 COMA9960669 1 19991101 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA STAB TRIM MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 779CA 7306 STABILIZER TRIM, NOSE DOWN, DOES NOT REACH FULL TRAVEL. REPLACED THE STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 1999111100012 19991111 00012 NM 1999 11 11 UPS99231013 1 19991025 A 5320 ANGLE BOEING 727 72725C 138400H NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C SURFACE CORROSION ON BKLD BS 950 LWR CHORD LBL 6 TO RBL 6 IN AFT CAR GO BAY LWR CHORD ANGLE REMOVE D IAW SRM 51-30-02 LWR CHORD ANGLE REPLACED IAW DRAWING # 66-12639-0 ***CPCP*** 2 L 7 3 4F A3WE 1999111100013 19991111 00013 NM 1999 11 11 UPS99231014 1 19991021 A 5753 HINGE BOEING 727 72725C 138400H NM NR 4 TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, NR 4 FLAP TRACK, AFT HINGE FITTING FOR WING DOOR CRACKED. REPLACED AFT DOOR HINGE ON FLAP TRACK IAW SRM 51-10-01 AND 51-30-02. 2 L 7 3 4F A3WE 1999111100014 19991111 00014 NM 1999 11 11 UPS99231015 1 19991019 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1163 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1163 S20L & S22L. ALL CORROSION REMOVED FROM SKIN A REA IAW SRM 51-30-2 AND FOUND TO BE WITHIN LIMITS PER SRM 53-30-1. 2 L 7 3 4F A3WE 1999111100015 19991111 00015 NM 1999 11 11 UPS99231016 1 19991022 A 5320 INTERCOSTAL BOEING 727 72725C 138400H NM BS 1148 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, INTERCOSTAL CRACKED ON LWR LEG AT BS 1148 BENEATH LT TIE DOWN TRACK. REPAIRED INTERCOSTAL IAW SRM 51 -20-02. 2 L 7 3 4F A3WE 1999111100016 19991111 00016 NM 1999 11 11 UPS99231018 1 19991001 A 5320 SILL BOEING 727 72725C 138400H NM BS 480-620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING CUSTOMER CARD NR 997512 FOUND MAIN CARGO DOOR SILL WEB CORRODED FROM BS 480-620 LBL 70 , WL 207-200. REMOVED CORRODED MAIN CARGO DOOR SILL WEB AND REPLACED WITH NEW ONE IAW 51-30-02. 2 L 7 3 4F A3WE 1999111100017 19991111 00017 NM 1999 11 11 UPS99231019 1 19991020 A 5320 SILL BOEING 727 72725C 138400H NM BS 460 -640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, AREAS OF CORROSION AT MAIN CARGO DOOR SILL LBL 64 BETWEEN BS 460 - BS 640. REPAIR CARRIED OUT IAW SM RO EO 99-37-03 UPS ENGINEERING FILE NR 727-53-2194. 2 L 7 3 4F A3WE 1999111100018 19991111 00018 NM 1999 11 11 UPS99231020 1 19990825 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, FLOORBEAM IS EXFOLIATED BS 740, LBL 37, WL 208 AND CORROSION AT PREVIOUS REPAIR ANGLE BS 740, LBL 8- 22, WL 208 (C53-224-01.05-01). REPAIRED CORRODED FLOORBEAM IAW SRM 53-10-04, 51-30-02. 2 L 7 3 4F A3WE 1999111100019 19991111 00019 NM 1999 11 11 UPS99231021 1 19991101 A 5320 ANGLE BOEING 727 72725C 138400H NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, INTERCOSTAL SUPPORT BRACKET CORRODED BS 1166 LBL 65 WL 208. REMOVED AND REPLACED BRACKET. 2 L 7 3 4F A3WE 1999111100020 19991111 00020 NM 1999 11 11 UPS99231022 1 19991020 A 5320 FITTING BOEING 727 72725C 138400H NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, EVIDENCE OF CORROSION AND CRACK ON BS 740 RT FITTING LWR WEB VERTICAL FLANGE. FITTING REPLACED IAW E O B727-5310-7477-E. 2 L 7 3 4F A3WE 1999111100021 19991111 00021 NM 1999 11 11 UPS99231023 1 19991101 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, FLOORBEAM IS EXFOLIATED BS 640, LBL 34-44, WL 208 CORROSION BLEND OUT BEYOND ALLOWABLE LIMITS. REMO VED AND REPLACED FLOORBEAM UPPER CHORD PER TRAMCO ER 99-6134. 2 L 7 3 4F A3WE 1999111100022 19991111 00022 NM 1999 11 11 UPS99231024 1 19991021 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 294.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, CRACK AT BS 294.5 ON FLOORBEAM WEB RBL 44.5. REPAIRED CRACK IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 1999111100023 19991111 00023 NM 1999 11 11 UPS99231025 1 19991024 A 5330 M228308 SKIN BOEING 727 72725C 138400H NM BS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING EO NR 727-5310-1371E, DISCOVERED EXTERNAL SKIN TO HAVE MATERIAL LOSS AT BS 440, RLB 30 , WL 303. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED SKIN PATCH PER DRAWING 69-62161. 2 L 7 3 4F A3WE 1999111100024 19991111 00024 NM 1999 11 11 UPS99231026 1 19990823 A 5751 HINGE BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, LEFT WING O/B AILERON O/B HINGE HALF ATTACHED TO FIXED WING IS CORRODED. REMOVED AND REPLACED CORRO DED HINGE FITTING IAW SRM 51-30-05, 51-30-02. 2 L 7 3 4F A3WE 1999111100025 19991111 00025 NM 1999 11 11 UPS99231027 1 19991029 A 5755 651922226 FITTING BOEING 727 72725C 138400H NM NR 7 SPOILER CORODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING CUSTOMER CARD 997840 FOUND NR 7 SPOILER ATTACH FITTING ON T/E HAS CORRODED ACTUATOR MO UNT HOLES. REMOVED DISCREPANT FITTING AND INSTALLED NEW FITTING. 2 L 7 3 4F A3WE 1999111100026 19991111 00026 NM 1999 11 11 UPS99231028 1 19991021 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS B1110 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C WHILE INSTALLING SMOKE DETECTOR UNIT AT BS 1110 A SUSPECT CRACK FOUN D ON LWR CHORD OF FLOOR BEAM BS 1 110 LBL 19 APPROX REPAIR CARRIED OUT IAW SMRO EO. 99-37-005 UPS ENGINEERING FILE NO 727-53-2195 2 L 7 3 4F A3WE 1999111100027 19991111 00027 NM 1999 11 11 UPS99231029 1 19991022 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, FRAME AT BS 1010 LWR LEG CRACKED STR 29R. REPAIRED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1999111100028 19991111 00028 NM 1999 11 11 UPS99231030 1 19991022 A 5320 SUPPORT BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, CARGO FLOOR SUPPORT CRACKED AT BS 990 RBL 3 AFT CARGO BAY. CARGO FLOOR SUPPORT REPLACED IAW SRM 53-1 0-05 FIG 4. 2 L 7 3 4F A3WE 1999111100029 19991111 00029 NM 1999 11 11 UPS99231033 1 19991021 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1050 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, CORROSION FOUND ON FLOORBEAM LWR CAP AT BS 1050 BL 0 - RBL 20. REPAIR CARRIED OUT IAW SMRO EO 99-37- 004 UPS ENGINEERING FILE NR 77-53-2197. 2 L 7 3 4F A3WE 1999111100030 19991111 00030 NM 1999 11 11 UPS99231034 1 19991020 A 5320 BRACKET BOEING 727 72725C 138400H NM LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, LT WHEEL WELL, BRACKET CRACKED AT FWD FACE OF 940 FITTING. FABRICATED AND INSTALLED BRACKET IAW DRAW ING 65C15732. 2 L 7 3 4F A3WE 1999111100031 19991111 00031 NM 1999 11 11 UPS99231035 1 19991021 A 5320 WEB BOEING 727 72725C 138400H NM BS 275 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, 2 CRACKS CONFIRMED ON NOSE LANDING GEAR CEILING PRESSURE WEB AT BS 275 RBL 12 & LBL 16. PRESSURE WEB REPLACED IAW DRAWING NR 65-18416. 2 L 7 3 4F A3WE 1999111100032 19991111 00032 NM 1999 11 11 UPS99231036 1 19991029 A 5755 651922226 FITTING BOEING 727 72725C 138400H NM NR 8 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING CARD NR 998054 FOUND CORROSION ON I/B SIDE OF BOTH LUGS OF CENTER HINGE FITTING MOUNT OF NR 8 SPOILER. REMOVED DISCREPANT FITTING AND INSTALLED NEW FITTING. 2 L 7 3 4F A3WE 1999111100033 19991111 00033 NM 1999 11 11 UPS99231037 1 19991022 A 5311 FRAME BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, FRAME CRACKED AT BS 990 LWR LEG LBL 17. REPAIR CARRIED OUT IAW SRM 53-10-4 FIG 4. 2 L 7 3 4F A3WE 1999111100034 19991111 00034 NM 1999 11 11 UPS99231038 1 19991008 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, UPON GIVING OK TO CLOSE FLOORBOARD FOUND CORROSION AROUND SEVERAL NUT PLATES ON LOWER SURFACE OF SEA T TRACK RBL 65 BS 760 - BS 848. CUT OUT CORRODED AREA AND INSTALLED NEW SEAT TRACK. CORROSION WAS OUT OF LIMITS, ALL W ORK IN ACCORDANCE WITH SRM 53-10-1, 51-30-2, 51-30-5, 51-30-8, 51-20-4, 51-10-2. 2 L 7 3 4F A3WE 1999111100035 19991111 00035 NM 1999 11 11 UPS99231039 1 19991020 A 5320 BRACKET BOEING 727 72725C 138400H NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, RT WHEEL WELL, BRACKET CRACKED AT FWD SIDE OF BS 940 FITTING. FABRICATED AND INSTALLED BRACKET IAW D RAWING NR 65C15732. 2 L 7 3 4F A3WE 1999111100036 19991111 00036 NM 1999 11 11 UPS99231040 1 19991020 A 5230 PLATE BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:C, FWD CARGO DOOR AFT CORNER SCUFF PLATE CRACKED. SCUFF PLATE REPLACED IAW DRAWING NR 65-18621. 2 L 7 3 4F A3WE 1999111100037 19991111 00037 NM 1999 11 11 UPS99231041 1 19990920 A 5320 BEAM BOEING 727 72725C 138400H NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING CUST CARD NR 997322 FOUND OUTBOARD TAB ON UPPER CHORD OF LOWER LONGITUDINAL BEAM CRACK ED AND CORRODED RT SIDE. REMOVED AND REPLACED FABRICATED NEW REPLACEMENT CHORD AND INSTALLED PER IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1999111100038 19991111 00038 NM 1999 11 11 UPS99231042 1 19991030 A 5320 65344422 LINK BOEING 727 72725C 138400H NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, WHILE WORKING 870 FLOORBEAM REPAIR CUST CARD NR 997981 FOUND EXPANSION LINK TO BE CRACKED BS 870 RBL 25 WL 208. REMOVED CRACKED EXPANSION LINK, INSTALLED NEW LINK PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999111100039 19991111 00039 NM 1999 11 11 UPS99231043 1 19990823 A 5751 HINGE BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, LEFT WING O/B AILERON O/B CENTER HINGE HALF ATTACHED TO FIXED WING IS CORRODED. REMOVED AND REPLACE D LEF WING O/B AILERON O/B CENTER HINGE HALF ATTACHED TO FIXED WING IAW 51-30-02. 2 L 7 3 4F A3WE 1999111100040 19991111 00040 NM 1999 11 11 UPS99231044 1 19991103 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION AROUND FASTENER HOLES BS 360, WL 208 LBL 6 AND RBL 11. REMOVED AND REPLACED FLOORBEAM UPP ER CHORD. 2 L 7 3 4F A3WE 1999111100041 19991111 00041 NM 1999 11 11 UPS99231045 1 19990826 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION ON BS 870 FLOORBEAM TOP SURFACE RBL 20 TO RBL 50 WL 208. REPAIRED BS 870 FLOORBEAM IAW SB B727-53-0116 AND DRW NR 65C23231 SHEET 1 (REF NRC 997381). 2 L 7 3 4F A3WE 1999111100042 19991111 00042 NM 1999 11 11 UPS99231046 1 19990825 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON FLOORBEAM BS 680 RBL 20 AND LBL 33-54, WL 208. REMOVED AND REPLACED UPPER CHORD OF FLOORBEAM BS 680 LBL 65 TO RBL 65, WORK DONE IAW SRM'S 53-10-1, 51-30-2, 53-10-8 AND MM 51-20-151. 2 L 7 3 4F A3WE 1999111100043 19991111 00043 NM 1999 11 11 UPS99231048 1 19991104 A 3350 LIGHT BOEING 727 72722C 138400F NM CABIN MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT ROBBED FOR ACFT 910. INSTALLED FWD ENTRY DOOR EMERGENCY EXIT L IGHT, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999111100044 19991111 00044 NM 1999 11 11 UPS99231049 1 19991003 A 3350 1000679 LIGHT BOEING 727 72727C 138400J NM EMER EXIY INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 910UP 19117 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AT ENTRY DOOR INOP. REMOVED AND REPLACED EXIT LIGHT ASSY IAW 33-50-00. 2 L 7 3 4F A3WE 1999111100045 19991111 00045 NM 1999 11 11 UPS99431012 1 19991102 A 3040 6171545 CONTROL BOEING 747 747123 1384873 NM LT WINDSHIELD FAILED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 676UP 20101 INSPECTION TYPE:N/A, AFTER T/O CAPT'S WINDOW HEAT BEGAN TO EMIT WHITE SMOKE. TURNED HEAT OFF AND SMOKE STOPPED. REMOVE D AND REPLACED WINDOW HEAT CONTROLLER AND SECURED CONNECTORS ON WINDOW CONTACTS, OPS CK NORMAL. (P/N 617154-5), (S/N 07 9C-188) OFF, (S/N 026C-1904) ON. 2 L 7 4 4F A20WE 1999111100046 19991111 00046 NM 1999 11 11 UPS99531017 1 19991023 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 161-100 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 432UP 25463 INSPECTION TYPE:C, AFT CARGO LT FLOOR/SIDEWALL SUPPORT PLATE IS CRACKED AND IS GOUGED IN SEVERAL PLACES BS 1357-1349. R EMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED ALL WORK DONE IAW SRM'S 53-00-53, 51-70-13, 51-40-02 AND MM 25-50-02. 2 L 7 2 4F RT A2NM 1999111100047 19991111 00047 WP 1999 11 11 UPS99831031 1 19991025 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 93-99 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:SV, FWD LWR NOSE SKIN CREASE AND TORN STA -99 TO-93, L31R TO L28R. REMOVED DAMAGED SECTION OF SKIN AND DAMAGED FRAME, FABRICATED NEW SKIN SECTION AND DOUBLERS IAW REO -06765, LOCATED NEW FRAME SKIN SECTION AND DOUBLERS, DRI LLED UP IAW DC8 SRM 51-24. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1999111100048 19991111 00048 WP 1999 11 11 UPS99831032 1 19991025 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 80-85 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:SV, FWD LWR NOSE SKIN CREASED AND TORN STA -85 TO -80 L31L TO 28L CRACKED APRROX 15.0. REMOVED DAMAGE S ECTION OF SKIN, FABBED DOUBLER, FILLER AND SPLICE DOUBLER IAW REO-06778, INSTALLED DOUBLER, FILLER AND SPLICE DOUBLER IA W DC8 SRM 51-1-20D, 51-1-21 & 51-3-0. FILLET SEALED IAW DC8 SRM 51-1-15. 2 L 7 4 4F RT 4A25 1999111100049 19991111 00049 WP 1999 11 11 UPS99831047 1 19990829 A 5310 STRUCTURE DOUG DC8 DC871F 302199D WP NOSE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 INSPECTION TYPE:N/A, FUSELAGE NOSE SECTION, INTERM, REPAIR EO DC8 5300-11498A TO INCLUDE REMOVAL OF NOSE LANDING GEAR DO ORS, BOTH PAC'S INOP (REF DEFERRAL M- 177745) RT PNEUMATIC PRESSURE INDICATION INOP (REF DEFERRAL M-177744 ) REF INCIDEN T NUMBER RS99-288. COMPLIED WITH REPAIRS REF TIMCO REO NR'S 06734, 06743, 06756, 06765, 06767 REV B, 06776, 06778, 0679 1, 06797 REV B, 06800, 06802 REV A, 0 6820. 2 L 7 4 4F RT 4A25 1999111100050 19991111 00050 WP 1999 11 11 UPS99831050 1 19991102 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS DID NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY IAW MM 33- 50-00, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999111100051 19991111 00051 WP 1999 11 11 UPS99831051 1 19991101 A 3350 6012233 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP ON PRE-DEPARTURE CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-50-0 1 PAGE 202. 2 L 7 4 4F RT 4A25 1999111100052 19991111 00052 EU 1999 11 11 QXEA9902192 1 19991009 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CRACK IN FRAME 20075, STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5. 2 L 7 2 4F RT A20EU 1999111100053 19991111 00053 EU 1999 11 11 QXEA9902193 1 19991010 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CRACK IN FRAME 20075, STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999111100054 19991111 00054 EU 1999 11 11 QXEA9902194 1 19991005 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CRACK IN FRAME 17565, STRINGER 57. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601A. 2 L 7 2 4F RT A20EU 1999111100055 19991111 00055 EU 1999 11 11 QXEA9902195 1 19991005 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CRACK IN FRAME 17565, STRINGER 56. REPAIRED IAW FOKKER SRM 5302-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999111100056 19991111 00056 EU 1999 11 11 QXEA9902196 1 19991004 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - CRACK IN FRAME 17565, STRINGER 14. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999111100057 19991111 00057 EU 1999 11 11 QXEA9902197 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - RIGHT OUTBOARD SEAT TRACK, 3 INCHES FORWARD OF FRAME 6305 HAD TWO GOUGES ON CENTER FLANGE. REPAIRED IAW FOKKER SR M 51-10-04, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1999111100058 19991111 00058 EU 1999 11 11 QXEA9902198 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - RIGHT INBOARD SEAT TRACK JUST FORWARD OF FRAME 6805 HAD LIGHT SURFACE CORROSION IN CENTER FLANGE. REPAIRED IAW FO KKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100059 19991111 00059 EU 1999 11 11 QXEA9902199 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - RIGHT INBOARD SEAT TRACK APPROXIMATELY 10 AFT OF FRAME 6805 HAD LIGHT SURFACE CORROSION IN CENTER FLANGE. REPAIRE D IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100060 19991111 00060 EU 1999 11 11 QXEA9902200 1 19991011 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - RIGHT INBOARD SEAT TRACK JUST FORWARD OF FRAME 7805 HAD LIGHT SURFACE CORROSION IN CENTER FLANGE. REPAIRED IAW HO RIZON AIR EA 4-53-895. 2 L 7 2 4F RT A20EU 1999111100061 19991111 00061 EU 1999 11 11 QXEA9902201 1 19991007 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT INBOARD SEAT TRACK AT FRAME 13815 CENTER FLANGE HAD LIGHT SCRATCHES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1999111100062 19991111 00062 EU 1999 11 11 QXEA9902202 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION IN CENTER FLANGE APPROXIMATELY 12 AFT OF FRAME 13345. REPAIRE D IAW FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100063 19991111 00063 EU 1999 11 11 QXEA9902203 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME12875-13345 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT INBOARD SEAT TRACK HAD LIGHT SURFACE CORROSION AND LIGHT SCRATCHES BETWEEN FRAME 12875 AND 13345. REPAIRED I AW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100064 19991111 00064 EU 1999 11 11 QXEA9902204 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11405 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT OUTBOARD SEAT TRACK HAD TWO GOUGES TOP OUTBOARD FLANGE APPROXIMATELY 3 FORWARD OF FRAME 11405. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100065 19991111 00065 EU 1999 11 11 QXEA9902205 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT INBOARD SEAT TRACK HAD LIGHT SCRATCHES AT CENTER FLANGE APPROXIMATELY 6 AFT OF FRAME 11905. REPAIRED IAW FOK KER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100066 19991111 00066 EU 1999 11 11 QXEA9902206 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT OUTBOARD SEAT TRACK HAD LIGHT SCRATCHES AT CENTER FLANGE JUST AFT OF FRAME 10346. REPAIRED IAW FOKKER SRM 51 -10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100067 19991111 00067 EU 1999 11 11 QXEA9902207 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10546 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT OUTBOARD SEAT TRACK HAD TWO SMALL GOUGES ON TOP FLANGE JUST AFT OF FRAME 10546. REPAIRED IAW FOKKER SRM 51-1 0-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100068 19991111 00068 EU 1999 11 11 QXEA9902208 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT INBOARD SEAT TRACK HAD LIGHT SCRATCHES IN CENTER FLANGE AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, 2 AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100069 19991111 00069 EU 1999 11 11 QXEA9902209 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT OUTBOARD SEAT TRACK HAD A GOUGE ON TOP INBOARD FLANGE APPROXIMATELY 3 FORWARD OF FRAME 6305. REPAIRED IAW FO KKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, B, C AND SRM 51-10-4, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100070 19991111 00070 EU 1999 11 11 QXEA9902210 1 19991004 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6805 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT OUTBOARD SEAT TRACK HAD LIGHT SCRATCHES IN CENTER FLANGE BETWEEN FRAME 5805 AND 6805. REPAIRED IAW FOKKER SR M 51-10-4, PAGE 9, PARAGRAPH 4, B, C AND SRM 51-10-7, PAGE 8, PARAGRAPH 3, C, 4. 2 L 7 2 4F RT A20EU 1999111100071 19991111 00071 EU 1999 11 11 QXEA9902211 1 19991003 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 15205 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - TOOLING MARK ON FUSELAGE SKIN AT FRAME 15205 NEAR STRINGER 20. REPAIRED IAW FOKKER SRM 53-10-01, PARAGRAPH 3D, FI GURE 1. 2 L 7 2 4F RT A20EU 1999111100072 19991111 00072 EU 1999 11 11 QXEA9902212 1 19991022 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU LTEMER EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT AFT OVERWING EMERGENCY EXIT TOP AFT CORNER CHAFED/CRACKED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52 -02-03, PAGE 5. 2 L 7 2 4F RT A20EU 1999111100073 19991111 00073 EU 1999 11 11 QXEA9902213 1 19991022 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU LT EMER EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT AFT OVERWING EMERGENCY EXIT TOP FORWARD CORNER CHAFED/CRACKED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SR M 52-02-03, PAGE 5. 2 L 7 2 4F RT A20EU 1999111100074 19991111 00074 EU 1999 11 11 QXEA9902214 1 19991022 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU LT EMER EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT OVERWING EMERGENCY EXIT BOTTOM AFT CORNER CHAFED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52-01-01, P AGE 3, FIGURE 1 AND SRM 52-01-01, PAGE 9. 2 L 7 2 4F RT A20EU 1999111100075 19991111 00075 EU 1999 11 11 QXEA9902215 1 19991022 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU LT EMER EXIT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - LEFT AFT OVERWING EMERGENCY EXIT BOTTOM FORWARD CORNER CHAFED ON OUTSIDE SKIN FLANGE. REPAIRED IAW FOKKER SRM 52- 01-01, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1999111100076 19991111 00076 EU 1999 11 11 QXEA9902216 1 19991018 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 16660 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX- A .75 INCH LONG DENT IN LEFT FUSELAGE SKIN, FORWARD OF REAR PRESSURE BULKHEAD 4 AFT OF FRAME 16660, 1 ABOVE STRINGE R 6. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH 5A AND SRM 51-10-04, PAGE 9, PARAGRAPH 4BC. 2 L 7 2 4F RT A20EU 1999111100077 19991111 00077 EU 1999 11 11 QXEA9902217 1 19991013 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME15205-15635 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - RIGHT FUSELAGE SKIN LAP JOINT AT STRINGER 66 BETWEEN FRAMES 15205 AND 15635 HAD CHAFE DAMAGE FROM PANEL 92BD, LOOS E AND MISSING PAINT AND SURFACE CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PAGES 2-6. 2 L 7 2 4F RT A20EU 1999111100078 19991111 00078 EU 1999 11 11 QXEA9902218 1 19991015 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 2650 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - FORWARD FRAME AT STATION 2650 IN NOSEWHEEL BAY HAD BOTH LEFT AND RIGHT LOWER LIPS CRACKED OFF AT THE NUT PLATE SUP PORT BLOCKS. REPAIRED IAW HORIZON AIR EA 4-53-886. 2 L 7 2 4F RT A20EU 1999111100079 19991111 00079 EU 1999 11 11 QXEA9902219 1 19991006 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - FORWARD CARGO COMPARTMENT FRAME 9305 HAS CORROSION AROUND NUTPLATES BETWEEN STRINGERS 74 AND 1. REPAIRED IAW HORI ZON AIR EA 4-53-891. 2 L 7 2 4F RT A20EU 1999111100080 19991111 00080 EU 1999 11 11 QXEA9902220 1 19991013 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 3450-4150 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - FORWARD CARGO COMPARTMENT STRINGER 65 HAD SURFACE CORROSION BETWEEN FRAMES 3450 AND 4150. REPAIRED IAW FOKKER SRM 53-02-05, FIGURE 1F. 2 L 7 2 4F RT A20EU 1999111100081 19991111 00081 EU 1999 11 11 QXEA9902221 1 19990927 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - AFT CARGO PIT CRACK COMING OUT FROM UNDER WASHER ON PREVIOUSLY REPAIRED FRAME CLIP AT FRAME 13815A AND STRINGER 1. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999111100082 19991111 00082 EU 1999 11 11 QXEA9902222 1 19991003 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 481US 11230 PDX - AFT CARGO PIT CRACK IN PREVIOUS REPAIR TO FRAME CLIP ON FRAME 13815A AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-0 2-13, PAGE 4. 2 L 7 2 4F RT A20EU 1999111100083 19991111 00083 EU 1999 11 11 QXEA9902223 1 19991005 A 5350 FAIRING FOKKER F28 F28MK4000 4990810 EU RT WING/ FUS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - FUSELAGE HAD CHAFE DAMAGE FROM PANEL 91BD AFT RIGHT WING FAIRING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8, PARAGR APH 3C. 2 L 7 2 4F RT A20EU 1999111100084 19991111 00084 EU 1999 11 11 QXEA9902224 1 19991005 A 5350 FAIRING FOKKER F28 F28MK4000 4990810 EU LT WING/FUS CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - FUSELAGE HAS CHAFE DAMAGE FROM PANEL 92BD AFT LEFT WING FAIRING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRA PH 4. 2 L 7 2 4F RT A20EU 1999111100085 19991111 00085 EU 1999 11 11 QXEA9902225 1 19991014 A 2150 EXHAUST FOKKER F28 F28MK4000 4990810 EU RT ACM CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - RIGHT ACM EXHAUST HAS A SUSPECTED SMALL CRACK AT THE LOWER FORWARD CORNER. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999111100086 19991111 00086 EU 1999 11 11 QXEA9902226 1 19991015 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 104.33 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - TWO CRACKS LOCATED THROUGH THE RIGHT SIDE SKIN AT STATION 104.330 APPROXIMATELY WL 30.00. REPAIRED IAW HORIZON AI R EA 4-53-886. 2 L 7 2 4F RT A20EU 1999111100087 19991111 00087 EU 1999 11 11 QXEA9902227 1 19991010 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - FRONT PRESSURE BULKHEAD BEAM VI AT CENTERLINE HAD A CRACK ON PREVIOUS REPAIR AT TOP FLANGE IN RADIUS. REPAIRED IA W FOKKER SRM 53-02-18. 2 L 7 2 4F RT A20EU 1999111100088 19991111 00088 EU 1999 11 11 QXEA9902228 1 19991010 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX - FRONT PRESSURE BULKHEAD BEAM VI AT CENTER LINE HAD A CRACK IN PREVIOUS REPAIR AT BOTTOM FLANGE IN RADIUS. REPAIRE D IAW FOKKER SRM 53-02-18. 2 L 7 2 4F RT A20EU 1999111100089 19991111 00089 WP 1999 11 11 99FDEA00458 1 19991021 A 5753 MS2125014078 BOLT DOUG DC10 DC1030F 3023504 WP LT TE FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 LT WING INBD FLAP HINGE BOLT TO REAR SPAR FND LOOSE AND ABOUT A QTR OF THE NUT MATERIAL MISSING. 2 L 7 3 4F RT A22WE 1999111100090 19991111 00090 NM 1999 11 11 99FDEA00459 1 19991102 A 5510 AJC515501 FITTING DOUG MD11 MD11F 3023600 NM ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 EDDY CURRENT INSP CARRIED OUT ON NR 4 BANJO FITTING FOUND CRACKS. *S/D* REPAIRS CARRIED OUT PER FEDEX ENG AUTH 1-5530- 48154. 2 L 7 3 4F RT A22WE 1999111100091 19991111 00091 WP 1999 11 11 ABXA9900755 1 19991013 A 5620 3912039 WINDOW DOUG DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LEFT FORWARD EMERGENCY EXIT OUTER WINDOW PANE CRACKED COMPLETELY THROUGH. REPLACED WINDOW IAW DC9 MM. 2 L 7 2 4F A6WE 1999111100092 19991111 00092 WP 1999 11 11 ABXA9900756 1 19991026 A 5730 99579681 PANEL DOUG DOUG DC9 DC932 3022066 WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LEFT WING TRAILING EDGE PANEL 1507 DELAMINATED AT INTERIOR HINGE. REPLACED PANEL IAW DC9 SRM 51-3 0-1. 2 L 7 2 4F A6WE 1999111100093 19991111 00093 WP 1999 11 11 ABXA9900757 1 19991026 A 5530 9911840165 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH FITTING SHEAR-TIE AT STATION 1094 CRACKED. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999111100094 19991111 00094 WP 1999 11 11 ABXA9900758 1 19991026 A 5553 4918093501 FITTING DOUG DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND VERTICAL STABILIZER LEFT ATTACH FITTING CRACKED AT STATION 1094. REPLACED FITTING IAW DC9 SRM 51- 30-5. 2 L 7 2 4F A6WE 1999111100095 19991111 00095 WP 1999 11 11 ABXA9900759 1 19991026 A 5320 99196526 INTERCOSTAL DOUG DOUG DC9 DC932 3022066 WP BS 579-593 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND INTERCOSTAL CRACKED BETWEEN STATION 579-593 AT LONGERON 9 RIGHT. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999111100096 19991111 00096 WP 1999 11 11 MWEA99770 1 19991102 A 2560 100503119 SLIDE DOUG DC9 DC981 3022081 WP GALLEY DOORWAY DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 810ME 48072 AFT GALLEY SLIDE NEEDED TO BE RE-ATTACHED. MTC REINSTALLED AFT GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1999111100097 19991111 00097 WP 1999 11 11 MWEA99771 1 19991103 A 5220 3917853503 BEAM DOUG DC9 DC932 3022066 WP EMER EXIT DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT LOWER CORNER OF AFT EXIT DOOR WAS CHAFED. MAINTENANCE FITTED AND INSTALLED NEW BEAM. 2 L 7 2 4F A6WE 1999111100098 19991111 00098 WP 1999 11 11 MWEA99772 1 19991103 A 5730 59305035 SKIN DOUG DC9 DC981 3022081 WP WS 245 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS SKIN REPAIR ON BOTTOM OF LEFT WING AT XRS 245 WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED SKIN RE PAIR DOUBLER. 2 L 7 2 4F A6WE 1999111100099 19991111 00099 WP 1999 11 11 MWEA99773 1 19991103 A 5330 59360229 SKIN DOUG DC9 DC981 3022081 WP BS 1085 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS SKIN REPAIR AT STATION 1085, LONGERON 29 LEFT, WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED SKIN R EPAIR DOUBLER. 2 L 7 2 4F A6WE 1999111100100 19991111 00100 WP 1999 11 11 MWEA99774 1 19991103 A 5330 5936029 SKIN DOUG DC9 DC981 3022081 WP BS 1110 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS SKIN REPAIR AT STATION 1110, LONGERON 28 RIGHT WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED SKIN R EPAIR DOUBLER. 2 L 7 2 4F A6WE 1999111100101 19991111 00101 WP 1999 11 11 MWEA99775 1 19991103 A 5230 59101413 SKIN DOUG DC9 DC981 3022081 WP CARGO DOOR MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS REPAIR TO FORWARD CARGO SKIN AROUND DOOR HANDLE WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED REPAI R SCUFF PLATE. 2 L 7 2 4F A6WE 1999111100102 19991111 00102 WP 1999 11 11 MWEA99776 1 19991103 A 5313 593601020 LONGERON DOUG DC9 DC981 3022081 WP BS 1401 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS REPAIR SPLICE OF LONGERON 18 RIGHT AT STATION 1401 TO 1418 WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INST ALLED PROPER REPAIR SPLICE. 2 L 7 2 4F A6WE 1999111100103 19991111 00103 WP 1999 11 11 MWEA99777 1 19991103 A 5320 5936439509 FITTING DOUG DC9 DC981 3022081 WP BS 1340 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FOUND FITTING AT STATION 1340 CORRODED. MAINTENANCE FITTED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999111100104 19991111 00104 WP 1999 11 11 MWEA99778 1 19991103 A 5313 593601019 LONGERON DOUG DC9 DC981 3022081 WP BS 1401 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS LONGERON REPAIR SPLICE AT STATION 1401 TO 1418 LONGERON 18 LEFT WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED REPAIR SPLICE. 2 L 7 2 4F A6WE 1999111100105 19991111 00105 WP 1999 11 11 MWEA99779 1 19991103 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR UNLATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 216ME 47740 GALLEY DOOR ESCAPE SLIDE CONTAINER WAS UNLATCHED AT BOTTOM. MAINTENANCE RELATCHED LANYARD ON GALLEY DOOR ESCAPE SLIDE. 2 L 7 2 4F A6WE 1999111100106 19991111 00106 WP 1999 11 11 MWEA99780 1 19991104 A 5730 59305035 SKIN DOUG DC9 DC981 3022081 WP WS 170 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS SKIN REPAIR ON BOTTOM OF LEFT WING AROUND SLAT TRACK DRAIN AT STATION XRS 170 WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999111100107 19991111 00107 WP 1999 11 11 MWEA99781 1 19991104 A 5311 9911839244 FRAME DOUG DC9 DC981 3022081 WP BS 1463 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS REPAIR TO CANTED FRAME STATION 1463, LONGERON 15 LEFT TO 18 LEFT WAS NOT ACCEPTABLE. MAINTENANCE FABRICATED AN D INSTALLED FRAME REPAIR. 2 L 7 2 4F A6WE 1999111100108 19991111 00108 NM 1999 11 11 SCNA99743 1 19991018 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 410 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT SEAT TRACK FORWARD RT CABIN, STA 410, RBL 36. REMO VED CORROSION PER SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED PER SRM 511002. PRIMED P ER MM 512002. INSTALLED PER SRM 513002. 2 L 7 3 4F A3WE 1999111100109 19991111 00109 NM 1999 11 11 SCNA99744 1 19991019 A 5320 ANGLE BOEING 727 727259 138408J NM BS 1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON LONGITUDINAL FLOOR SUPPORT ANGLE, BETWEEN FS 1110 A ND 1130 BL 0. REMOVED CORROSION IAW SRM 511006. REMOVED SUPPORT IAW SRM 513002. FABRICATED NEW FLOOR SUPPORT FROM 707 5 T6 .032 PER SAMPLE. TREATED AND PRIMED IAW SRM 511002, MM 522002. INSTALLED IAW SRM 513002. 2 L 7 3 4F A3WE 1999111100110 19991111 00110 NM 1999 11 11 SCNA99745 1 19991024 A 5315 FLOORBEAM BOEING 727 727259 138408J NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON BOTTOM FWD FLANGE OF MAIN FLOOR T-CAP AROUND NUT CL IP HOLES, FS 1110 BL 0. REMOVED CORROSION IAW SRM 511006. REMOVED DAMAGED AREA, FABRICATED 2 ANGLES FROM BAC 14902831, FABRICATED 1 FILLER FROM 7075 T6 .125 IAW SRM 531008. TREATED AND PRIMED IAW SRM 511002, MM 512002. INSTALLED IAW SRM 531008 AND 513002. 2 L 7 3 4F A3WE 1999111100111 19991111 00111 NM 1999 11 11 SCNA99746 1 19991024 A 5320 ANGLE BOEING 727 727259 138408J NM BS 1050 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON LONGITUDINAL FLOORBOARD SUPPORT ANGLE, FS 1050 LBL 15. REMOVED CORROSION IAW SRM 511006. REMOVED FLOORBOARD SUPPORT IAW B727 SRM 513002. FABRICATED NEW FLOORBOARD SUPPO RT FROM BAC 15064417 PER SAMPLE. TREATED IAW B727 SRM 511002. PRIMED IAW B727 MM 512002. INSTALLED IAW B727 SRM 51300 2. 2 L 7 3 4F A3WE 1999111100112 19991111 00112 NM 1999 11 11 SCNA99747 1 19991018 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 385 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON FLOOR SUPPORT STRUCTURE, STA 385 BL 36R. REMOVED C ORROSION FROM FLOOR SUPPORT PER SRM 511006. REMOVED FLOOR SUPPORT PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 1506 4417 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER SRM 513002. 2 L 7 3 4F A3WE 1999111100113 19991111 00113 NM 1999 11 11 SCNA99748 1 19991018 A 5315 FLOORBEAM BOEING 727 727259 138408J NM BS 294-344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON FWD LAV FLOORBEAMS AT RT BS 294 TO BS 344. REMOVED CORROSION AT FS 294 TO 344 PER SRM 511006. REMOVED LAV FLOOR SUPPORT PER SRM 513002. FABRICATED NEW SUPPORT FROM BAC 1509100312 PER SAMPLE. TREATED PER SRM 511002. PRIMED PER MM 512002. INSTALLED PER SRM 513002. 2 L 7 3 4F A3WE 1999111100114 19991111 00114 NM 1999 11 11 VNAA9911003 1 19991102 A 3060 B6444 HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP HEAT FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 442JS 3060 HL17 WHILE EN ROUTE TO CLT, THE FLIGHT CREW RECEIVED A LEFT HAND PROPELLER HEAT FAIL CAS MESSAGE. THE FLIGHT CREW RETURNED T O CAK. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED 2 DE-ICE WIRING HARNESSES IN ACCORDANC E WITH HARTZELL MAINTENANCE MANUAL 61-00-60. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED TO SERVICE . 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111100115 19991111 00115 CE 1999 11 11 99ZZZX4176 1 19991015 A 2731 POTENTIOMETER BEECH 18 C45H 1151018 CE ELEV INDICATOR MALFUNCTIONED A KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 404CK AF297 ELEVATOR TRIM INDICATOR INACCURATE, ELEVATOR TRIM STIFF. REPLACED ELEVATOR TRIM INDICATOR POTENTIOMETER WITH NEW AND AD JUSTED TRIM INDICATOR PER MM. LUBED ELEVATOR TRIM ACTUATOR DRIVES, OPERATIONALLY CHECKS GOOD. 1 L 7 2 3R A765 1999111100116 19991111 00116 CE 1999 11 11 99ZZZX4177 1 19991015 A 2730 ELEVATOR TRIM BEECH 18 C45H 1151018 CE ELEVATOR LACK OF LUBE A KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 404CK AF297 ELEVATOR INOPERATIVE, WILL NOT ADJUST. LUBED ELEVATOR TRIM CHAINS AND ACTUATORS OPERATIONALLY CHECKED GOOD. 1 L 7 2 3R A765 1999111100127 19991111 00127 NE 1999 11 11 QKLA0000032 2 19990903 A 7210 350A32314306 GEAR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE REDUCTION GEARBX DAMAGED A QKLA K NONE O OTHER IN INSP/MAINT 1 WP 19 544AS 3300 ZF2141 2890 9403 GEAR SET REPLACED AT THE FIRST OVERHAUL. SECOND GEAR SET REPLACED AT THE FIRST OVERHAUL WITH NEW PART. PART TOTAL CYCL ES: 5,975. 1 G 7 1 3U 3 U H9EU E19EU 1999111100130 19991111 00130 CE 1999 11 11 99ZZZX4190 1 19990928 A 3230 1NE18 SWITCH LEAR 24 24D 5170311 CE RT MLG MALFUNCTIONED A KKFA O OTHER O OTHER NR NOT REPORTED 1 GL 23 80CK 309 LANDING GEAR WOULD NOT EXTEND FIRST TIME SELECTED, GEAR CAME DOWN WHEN SELECTED SECOND TIME. RIGHT DOWN AND LOCK MICROS WITCH FOUND FAULTY. REPLACED RIGHT MAIN GEAR DOWN AND LOCK MICROSWITCH WITH NEW AND ADJUSTED PER THE LEARJET MAINTENANC E SECTION 3-57. OPERATIONALLY CHECKED SATISFACTORY. 2 L 7 2 4J A10CE 1999111100132 19991111 00132 CE 1999 11 11 99ZZZX4192 1 19990809 A 3230 CIRCUIT BREAKER BEECH 200 200BEECH 1152920 CE MLG FAILED G O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 11 5UN BB697 AIRCRAFT, OPERATED BY EASTWAY AVIATION, INC., CERTIFICATE NR AOBA190C, LANDED AT KHPN AT APPROXIMATELY 0730. UPON LAND ING, THE MAIN LANDING GEAR COLLAPSED. THE CREW DID NOT HAVE ANY GREEN DOWN AND LOCKED LIGHTS OR RED LANDING GEAR UNSAFE LIGHTS, DID A FLY-BY THE TOWER, AND VISUALLY, THE LANDING GEAR APPEARED DOWN. AT THIS TIME, ALL THAT IS KNOW IS THE LA NDING GEAR MOTOR CIRCUIT BREAKER OPENED CAUSING THE LANDING GEAR NOT TO FUNCTION NORMALLY AND AN EMERGENCY EXTENSION WAS NOT ATTEMPTED. 1 L 7 2 4T A24CE 1999111100135 19991111 00135 SO 1999 11 11 99ZZZX4195 1 19990908 A 2130 672890001 VALVE GULSTM G1159 G1159A 3970109 SO CARGO BAY INOPERABLE A PJVA O OTHER O OTHER NR NOT REPORTED 1 EA 17 724DB 7340 04810742 372 EMERGENCY PRESSURIZATION SHUT-OFF VALVE FAILED IN THE OPEN POSITION CAUSING LOUD AIR NOISE IN BAGGAGE AREA, AND CAUSED C ABIN TO GET WARM (AMBIENT TEMP). VALVE WAS REMOVED AND REPLACED. 2 L 7 2 4F A12EA 1999111100147 19991111 00147 GL 1999 11 11 RAAA99E9032 2 19990208 A 7200 ENGINE LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 3 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 501219 NR 3 ENGINE COMPRESSOR INLET CASE HAS TWO INSERTS PULLED OUT AT LT INLET GUIDE VANE ANTI-ICE VALVE MOUNT PAD. REPLACED NR 3 ENGINE. 2 L 7 4 4T 4 T 4A22 E282 1999111100148 19991111 00148 GL 1999 11 11 RAAA99E9033 2 19990307 A 7200 ENGINE LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 2 LOW POWER A RAAA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 1968R 35131 188C2007 501397 APM 2.0 IN-FLT MONITORING INDICATES PAST 7 FLIGHTS PERCENT EFF AVG 89.3 PERCENT EQUALS .9 PERCENT BELOW ALERT LEVEL NR 2 ENGINE. REPLACED NR 2 ENGINE. 2 L 7 4 4T 4 T 4A22 E282 1999111100149 19991111 00149 WP 1999 11 11 9904549960 1 19991011 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 965 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING M CHECK, CORROSION WAS FOUND ON THE ANGLE WHICH ATTACHES TO THE FLOORBEAM AT FS 965, LBL 20. 2 L 7 2 4F A6WE 1999111100150 19991111 00150 WP 1999 11 11 9904559980 1 19991026 A 5320 TRAP PANEL DOUG DC9 DC931 3022065 WP MLG WW DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING M CHECK, -5 AND -6 STRAPS WERE INSTALLED ON THE FORWARD SIDE OF THE TRAPEZOIDAL PANEL. THE REPAIR DEVIATED FROM SRM 57-09, FIG 34, PG167. REPAIRED PER EA 99-169253. 2 L 7 2 4F A6WE 1999111100151 19991111 00151 WP 1999 11 11 9904569618 1 19991028 A 5414 SKIN DOUG DC9 DC932 3022066 WP NR 1 PYLON WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING INSPECTION, FOUND NUMBEROUS LOOSE FASTENERS ON NR 1 PYLON. REPAIRED PER EA 99-097710. 2 L 7 2 4F A6WE 1999111100152 19991111 00152 WP 1999 11 11 9904579980 1 19991019 A 5320 JAMB DOUG DC9 DC931 3022065 WP SERVICE DOORWAY GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47444 DURING M CHECK, A GOUGE WAS FOUND ON THE HORIZONTAL FLANGE IN THE LOWER FORWARD CORNER OF THE FORWARD SERVICE DOOR JAMB. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER EA 99-169244. 2 L 7 2 4F A6WE 1999111100153 19991111 00153 WP 1999 11 11 9904589963 1 19990922 A 5711 SPAR WEB DOUG DC9 DC931 3022065 WP WS 144 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING M CHECK, A .75 INCH CRACK WAS FOUND ON THE WINGS REAR SPAR WEB AT WS XRS144. THE CRACK EMANATED FROM A FASTENER HOLE COMMON TO THE END FASTENER OF THE AUXILIARY SPAR LOWER ANGLE. THE TRIM OUT WAS 1.25 WIDTH BY 2.5 LENGTH. INSTALLE D .080 STEEL DOUBLER WEB REPAIR PER EA 99-169163. 2 L 7 2 4F A6WE 1999111100154 19991111 00154 WP 1999 11 11 9904599980 1 19991001 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING M CHECK, FOUND .625 LONG BEND RADIUS CRACK ON THE 9958212-121 VERTICAL SUPPORT BEAM AT FS 756 AND X25. THE CRACK WAS STOPPED DRILLED AND .050 17-7 PH CORROSION RESISTANT STEEL ANGLES WERE INSTALLED AT EACH LEG PER EA 99-169205. 2 L 7 2 4F A6WE 1999111100155 19991111 00155 WP 1999 11 11 9904609981 1 19991006 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1038 WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING M CHECK, FOUND WEAR DAMAGE ON THE FORWARD FLANGE OF THE LOWER TEE CAP. THE DAMAGE WAS CAUSED BY A STEEL DOUBLER INSTALLED AT THE EDGE OF THE APU DOOR WHERE IT CONTACTED THE FRAME LOWER TEE CAP FORWARD FLANGE, FS 1038. THE DAMAGE WA S BLENDED OUT. REPAIRED PER EA 99-169206. 2 L 7 2 4F A6WE 1999111100156 19991111 00156 WP 1999 11 11 9904619977 1 19991028 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1060 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9341 47390 DURING M CHECK, FOUND 9 HOLES ELONGATED IN 5911432-69 SKIN, THESE HOLES WERE OVERSIZED TO .250. ALSO, THE SKIN WAS CRAC KED AT A FASTENER LOCATION COMMON TO THE -69 SKIN AND ATTACH ANGLE. REPAIRED PER EA 99-169299. 2 L 7 2 4F A6WE 1999111100157 19991111 00157 WP 1999 11 11 9904629980 1 19991013 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING M CHECK, ONE NUTPLATE ATTACH FASTENER HOLE IN THE ANGLE ABOVE LONGERON 18L WAS FOUND TO BE DAMAGED. THE SUBJECT HOLE WAS OPENED UP TOE .25 DIA IN ADDITION, CORROSION WAS BLENDED ON THE INBOARD FLANGE BELOW THE DAMAGED HOLE. REPAIRE D PER EA 99-169241. 2 L 7 2 4F A6WE 1999111100158 19991111 00158 WP 1999 11 11 9904639960 1 19991011 A 5320 SPLICE DOUG DC9 DC931 3022065 WP BS 937 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING M CHECK, FOUND 3 HOLES SEVERELY DAMAGED AT FRAME SPLICE NEAR 127, FS 937. REPAIRED PER EA 99-169211. 2 L 7 2 4F A6WE 1999111100159 19991111 00159 WP 1999 11 11 9904649758 1 19990819 A 5312 CHANNEL DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING APB INSPECTIONS, A 1.25 CRACK WAS FOUND IN THE UPPER INBOARD BEND RADIUS OF THE LEFT CHANNEL 5910130-9. REPAIRED PER EA 97-169048. 2 L 7 2 4F A6WE 1999111100160 19991111 00160 WP 1999 11 11 9904659963 1 19991007 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 STATIC DISCHARGE DAMAGE OCCURRED AT THE LEFT NR 8 AND NR 9 WINDOW BELT SKIN. DAMAGE WAS SEVERE ENOUGH TO NEED REPAIR. R EPAIRED PER EA 99-111035. 2 L 7 2 4F A6WE 1999111100161 19991111 00161 WP 1999 11 11 9904669963 1 19990922 A 5720 PRESS PANEL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING M CHECK, CORROSION REMOVED EXCEEDS LIMITS AT 5 FASTENER LOCATIONS ON THE FITH SLAT PRESSURE PANEL LOWER ATTACH AN GLE CAP. REPAIRED PER EA 99-169178. 2 L 7 2 4F A6WE 1999111100162 19991111 00162 WP 1999 11 11 9904679980 1 19991013 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING M CHECK, THE AFT PRESSURE BULKHEAD WAS INSPECTED FOR DAMAGE. A CRACK WAS FOUND AT THE BEND RADIUS OF THE VERTICA L FORWARD FACING FLANGE EXTENDING DOWN AND INBOARD ON THE LEFT AND RIGHT DOUBLER. CRACK LENGTH -9 WAS 1.125. CRACK LEN GTH -11 WAS .875. REPAIRED PER EA 99-169207. 2 L 7 2 4F A6WE 1999111100163 19991111 00163 WP 1999 11 11 9904689963 1 19991006 A 5720 DOUBLER DOUG DC9 DC931 3022065 WP WS 225-274 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING M CHECK, FOUND CORROSION ON LOWER FLANGE OF THE RIGHT WING FRONT SPAR LOWER TEE BETWEEN XFS=244 AND XFS=257. COR ROSION WAS ALSO FOUND ON THE RIGHT WING LEADING EDGE DOUBLER BETWEEN XFS =225 AND XFS=274. THE PRESENT REPAIR WAS DEVEL OPED AS AN ALTERNATIVE TO THE SRM SPLICE REPAIR OF THE FRONT SPAR LOWER TEE. REPAIRED PER EA 99-169182. MFG PART NUMBE R 5919153-2. 2 L 7 2 4F A6WE 1999111100164 19991111 00164 WP 1999 11 11 9904699980 1 19991014 A 5320 TEE DOUG DC9 DC931 3022065 WP KEELBEAM CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING M CHECK, CORROSION REMOVED BEYOND LIMITS ON SUBJECT KEEL BEAM REAR SPAR ATTACH TEE. REPAIRED PER EA 99-169249. 2 L 7 2 4F A6WE 1999111100165 19991111 00165 WP 1999 11 11 9904709957 1 19990812 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 200 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING L CHECK AND WITH COMPLIANCE WITH SB DC9-53-280 REV 1. A CRACK WAS NOTED ON THE FUSELAGE SKIN AFT OF THE FORWARD PASSENGER DOOR AT DOORSTOP NR 6. REPAIRED PER EA 99-167024. 2 L 7 2 4F A6WE 1999111100166 19991111 00166 WP 1999 11 11 9904719924 1 19991027 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 270 BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926RC 47473 DURING M CHECK, FOUND OUTBOARD FLANGE OF THE RIGHT OUTBOARD SEAT TRACK FS 270 BROKEN. REPAIRED PER EA 99-169290. 2 L 7 2 4F A6WE 1999111100167 19991111 00167 WP 1999 11 11 9904729980 1 19991013 A 5320 STRAP DOUG DC9 DC931 3022065 WP BS 1066 CUT A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING M CHECK, THE ANTI-ROTATION STRAPS AT LONGERON 2L AND 2R, FS 1066 HAD BEEN PREVIOUSLY CUT AS PART OF A LONGERON SP LICE. REPAIRED PER EA 99-169239. 2 L 7 2 4F A6WE 1999111100168 19991111 00168 NM 1999 11 11 9904515511 1 19991029 A 2751 TRANSMITTER BOEING 757 757251 1384970 NM TE FLAPS FAILED A NWAA K NONE N FALSE WARNING AP APPROACH 1 GL 01 511US 23199 DURING APPROACH AFTER FLAPS POSITION 1 SELECTED, RECEIVED TRAILING EDGE DISAGREE MESSAGE AND TRAILING EDGE LIGHT ILLUMIN ATED. EXTENDED FLAPS USING COM PROCEDURES TO FLAPS POSITION 20. DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 8 FLAP TRANSMISSION. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1999111100169 19991111 00169 WP 1999 11 11 9904529868 1 19991101 A 2780 RETRACT MECH DOUG DC9 DC951 3022051 WP LE FLAPS MALFUNCTIONED A NWAA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 01 777NC 47787 DURING APPROACH INTO DTW, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH A ROLL TO THE LEFT. FLIGHT CREW DECLARED AN EMERGENC Y AND NORMAL LANDING WAS ACCOMPLISHED USING FLAPS ONLY. MAINTENANCE RAN SLATS SEVERAL TIMES AND PROBLEM COULD NOT BE DU PLICATED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1999111100170 19991111 00170 WP 1999 11 11 9904539620 1 19991028 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 620NW 47533 DURING LINE MAINTENANCE INSPECTION, FOUND CENTER SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999111100171 19991111 00171 NM 1999 11 11 UPS99231053 1 19991105 A 3350 BATTERY PACK BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 EMERGENCY EXIT LIGHT OVER FOWARD ENTRY DOOR COMES ON INTERMITTENLY WITH CORRESPONDING OVERHEAD PANEL SWITCH IN ARM POSIT ION. REMOVED AND REPLACED BATTERY PACK IN UNIT OVER FORWARD ENTRY DOOR. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1999111100172 19991111 00172 NM 1999 11 11 UPS99231054 1 19991104 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM LT EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 2 EXIT LIGHTS IN OVER HEAD INOP LEFT WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999111100173 19991111 00173 NM 1999 11 11 UPS99531052 1 19991105 A 5230 SKIN BOEING 757 75724APF 1384969 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 426UP 25457 INSPECTION TYPE: N/A, AFT LOWER CARGO DOOR HAS SKIN CRACK OUT OF SRM LIMITS. *S/D* STOP DRILLED CRACK AND INSTALLED DO UBLER PER SRM 52-30-01. 2 L 7 2 4F RT A2NM 1999111100174 19991111 00174 NM 1999 11 11 99FDEA00460 1 19991101 A 5720 ARB2431512514 SUPPORT DOUG MD11 MD11F 3023600 NM RT WING CHAFFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 RIGHT WING TRAILING EDGE FLAP AFT REMOVAL FWD FAIR 635AL FOUND HINGE UNDRWING SUPPORT FITTING FWD SIDE I/B AND O/B EDGE WITH DEEP CHAFE MARK. INBD AND OTBD MATERIAL ORIG THICKNESS - 0.210 AFT BLEND-OUT, MATERIAL REMAIN - 0.096 FOR I/B & 0. 168 FOR O/B. *S/D* CHAFING MARK REMOVED PER SRM 57-00-01 VOL 1. REPAIRED SUPPORT FITTING PER ENG AUTH NR 1-5720-48152 . 2 L 7 3 4F RT A22WE 1999111100175 19991111 00175 NM 1999 11 11 SCNA99129 1 19991031 A 2150 56697 VALVE BOEING 727 7272J4 1384006 NM EQUIP COOLING INOP A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 285SC 21676 DURING CLIMB, THE CABIN PRESSURIZATION CONTINUED TO CLIMB BEYOND CABIN ALTITUDE SET. UNABLE TO CONTROL RATE OF CLIMB IN AUTO, STANDBY OR MANUAL MODES. REMOVED AND REPLACED THE FLOW CONTROL VALVE EQUIPMENT COOLING PER MM 215821. CABIN PRE SSURIZATION CONTROL SYSTEM TESTED NORMAL PER 21310. 2 L 7 3 4F RT A3WE 1999111100176 19991111 00176 NM 1999 11 11 SCNA99130 1 19991028 A 3350 SIGN BOEING 727 7272J4 1384006 NM RT EMER EXIT INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE AFT RIGHT OVERWING EMERGENCY EXIT SIGN INSIDE THE AIRCRAFT WAS FOUND TO BE INOPERAT IVE. FOUND WIRE DISCONNECTED BEHIND THE LIGHT ASSEMBLY. REPAIRED WIRE AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999111100177 19991111 00177 NM 1999 11 11 SCNA99131 1 19991031 A 8012 97925471 START VALVE BOEING 727 727227 1384078 NM NR 3 ENGINE INOP A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 275AF 22092 DURING THE TAKEOFF ROLL, THE NUMBER THREE ENGINE START VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED THE NUMBER THREE E NGINE START VALVE PER MM 801111. OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 3 4F A3WE 1999111100178 19991111 00178 NM 1999 11 11 DHL99727006 1 19991105 A 5230 602EN6026 SWITCH BOEING 727 727228 NM CARGO DOOR OUT OF ADJUST A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 727DH 20204 MAIN CARGO DOOR LIGHT CAME ON IN FLIGHT THEN WENT OUT. ADJUSTED AFT AUX LATCH PIN SWITCH PER PEMCO M 52-32-21 PRESSURIZ ED AIRCRAFT AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1999111100179 19991111 00179 NM 1999 11 11 VNAA9911005 1 19991104 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7LK DISCHARGED A VNAA K NONE L NO TEST NR NOT REPORTED 1 GL 07 432JS 7969 139 3045 THE FLIGHT CREW FOUND THE EMERGENCY EXIT SIGN LIGHT AT SEAT 11A WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111100180 19991111 00180 EU 1999 11 11 RAIA9911002 1 19991101 A 3240 AHA1835 BRAKE JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 554HK 41067 6140 - ORF - A/C PULLS TO LEFT DURING TAXI. MAINTENANCE REPLACED LEFT OUTBOARD BRAKE AND WHEEL ASSY. 2 L 7 2 4T RT A41NM 1999111100181 19991111 00181 EU 1999 11 11 RAIA9911003 1 19991101 A 3246 AHA1837 WHEEL ASSY JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 554HK 41067 6140 - OR F- A/C PULLS TO LEFT DURING TAXI. MAINTENANCE REPLACED LEFT OUTBOARD BRAKE AND WHEEL ASSY. 2 L 7 2 4T RT A41NM 1999111100182 19991111 00182 1999 11 11 RAIA9911004 3 19991102 A 6140 8659567 SWITCH BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 864AE 1892 1892 864 4793 - FAT - LEFT BETA LIGHT WOULD NOT ILLUMINATE IN BETA MODE. MAINTENANCE REPLACED LEFT BETA SWITCH. 2 L 7 2 4T RT A56EU 1999111100183 19991111 00183 EU 1999 11 11 RAIA9911005 1 19991102 A 3060 666000218 BRUSH BLOCK BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 430AM 880 7261 - SBN - LEFT ENGINE VIBRATIONS WITH DE-ICE PROP ON. VIBRAITION GOES AWAY AT 35 PERCENT TORQUE. MAINTENANCE REPLAC ED BRUSH BLOCK ON RIGHT ENGINE. 2 L 7 2 4T RT A56EU 1999111100184 19991111 00184 EU 1999 11 11 RAIA9911006 1 19991103 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RIGHT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 343TE 947 947 955 7336 - STL - RIGHT RPM INDICATOR FAILED. MAINTENANCE REPLACED TACH GENERATOR ON RIGHT ENGINE. 2 L 7 2 4T RT A56EU 1999111100185 19991111 00185 WP 1999 11 11 TWAA9915102 1 19991103 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP ROW 17 WORN A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 9407R 49400 THE CABIN EGRESS LIGHT WAS INOPERATIVE AT ROW 17. DEFERRED CORRECTION PER MEL. ON LAYOVER, THE BULB WAS REPLACED. CHE CK-C 5-1-99 STL. 2 L 7 2 4F RT A6WE 1999111100186 19991111 00186 WP 1999 11 11 TWAA9915103 1 19991104 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING CHECK-C MAINT, TWO SKIN CRACKS WERE FOUND ON THE FORWARD CARGO DOOR, LOWER AFT CORNER, FUSELAGE STA 427 AND LONGE RON 27R. CRACKS WERE 13/32 AND 5/32 IN LONG. REPAIRED PER SRM 53-05, FIG 105. 2 L 7 2 4F A6WE 1999111100187 19991111 00187 EA 1999 11 11 JBXA9900121 1 19991107 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A JBXA K NONE J WARNING INDICATION DE DESCENT 1 SO 05 582ML 7322 FLAPS FAIL MESSAGE IN FLIGHT AT INDICATION OF ZERO DEGREES. REMOVED AND REPLACED FECU, RIGGED AND OPERATIONAL CHECK IAW CL-65 MM 27-51-05. ALL CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 1999111100188 19991111 00188 EU 1999 11 11 JBXA9900122 1 19991108 A 3610 BLEED AIR FOKKER F28 F28MK0100 4990807 EU NR 1&2 FAILED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 105ML 11475 BLEED 1 AND BLEED 2 FAULTED ON TAKEOFF AT 60 KNOTS. ABORTED TAKEOFF. ACCOMPLISHED CHECK PER MM 36-00-5, OPS CK GOOD. 2 L 7 2 4F RT 1999111100189 19991111 00189 NM 1999 11 11 AWXA9900395 1 19991103 A 3510 RCF6708 REGULATOR AIRBUS A319 A319132 NM CREW OXYGEN SYS LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 802AW 3789 3783 924 DIVERT FOR CREW OXYGEN LOSS. CREW O2 750 PSI, DECREASED TO 570 IN FLT. REMOVED AND REPLACED O2 REGULATOR FOR LEAKS PER MM 35-13-15-401. NO LEAKS NOTED. SEE ALSO LPS 7349112, 113, 116, PLUS 110. ATA 35 NUMEROUS WRITE-UPS SINCE APRIL 99 , 9 MONTH LOOK BACK RECOMMENDATION. AIRCRAFT IS ON CRITICAL WATCH. 2 L 7 2 4F RT A28NM 1999111100190 19991111 00190 EU 1999 11 11 AWXA9900396 1 19991102 A 4990 OIL SYS AIRBUS 320 A320231 3930325 EU APU LEAKING A AWXA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 644AW 14509 1290 317 UPON ACCEPTING A/C IN LAS, SMELLED THE DIRTY SOCK SMELL FAIRLY STRONG. CLEANED AND REMOVED RESIDUAL OIL FROM APU INLET, SMELL CLEARED. APU OPS CK GOOD. SUSPECT SLOW EXTERNAL OIL SEEP CAUSING APU INLET. 2 L 7 2 4F RT A28NM 1999111100191 19991111 00191 NM 1999 11 11 AWXA9900397 1 19991103 A 3397 BMS13131122 WIRE BOEING 737 737277 1384570 NM ROW 6 BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 EMERGENCY PATH LIGHTING INOP AT ROW 6. REPAIRED BROKEN WIRES, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999111100192 19991111 00192 WP 1999 11 11 CALA9901464 1 19991104 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160-200, LBL 54. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-2, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999111100193 19991111 00193 NM 1999 11 11 CALA9901465 1 19991105 A 5414 PANEL BOEING 737 7373T0 1384582 NM NR 1 PYLON GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12318 23369 INSPECTION FOUND NR 1 ENGINE PYLON ACCESS PANEL NR 5727L CUTOUT GOUGED IN TWO PLACES. REPAIRED IAW ECRA 5430-01581. 2 L 7 2 4F RT A16WE 1999111100194 19991111 00194 WP 1999 11 11 CALA9901466 1 19991105 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND LONGERON 30 AT FS 110 CORRODED. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-10-01. 2 L 7 2 4F A6WE 1999111100195 19991111 00195 WP 1999 11 11 CALA9901467 1 19991105 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND FORWARD SERVICE DOOR CLOSEOUT PANEL LOWER ATTACH ANGLES CORRODED AT STA 160, RBL 52. THE ANGLES WERE R EMOVED AND REPLACED IAW SRM 51-10-4 AND 53-14-1, FIGURE 11. 2 L 7 2 4F A6WE 1999111100196 19991111 00196 WP 1999 11 11 CALA9901468 1 19991105 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1136-1240 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND LT CENTER SEAT TRACK CORRODED FROM STA 1136-1240, LBL 12. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TR ACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F, 51-10-3, 51-30-1, AND 51-30-5. 2 L 7 2 4F A6WE 1999111100197 19991111 00197 WP 1999 11 11 CALA9901469 1 19991105 A 5512 SKIN DOUG DC9 DC982 3022082 WP HORIZ STAB BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND UPPER LT HORIZONTAL STABILIZER BANANA PANEL SKIN AND DOUBLER BROKEN. THE DAMAGED AREA WAS REMOVED. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 55-03, FIGURE 17, 51-10-3, AND 51-10-4. 2 L 7 2 4F A6WE 1999111100198 19991111 00198 WP 1999 11 11 CALA9901470 1 19991105 A 5320 SUBFLOOR DOUG DC9 DC982 3022082 WP BS 148-158 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND SUBFLOOR CORRODED AT STA 148-158, RBL 44 TO RBL 54. THE CORRODED AREA WAS REMOVED IAW SRM 51-10-3, SHE ET 3. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-1, FIGURE 11, 51-30-5, AND 51-30-8. 2 L 7 2 4F A6WE 1999111100199 19991111 00199 WP 1999 11 11 CALA9901471 1 19991105 A 5542 SKIN DOUG DC9 DC982 3022082 WP RUDDER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND LT UPPER RUDDER SKIN DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 53-03. A DOUBLER REPAIR WAS INSTALLE D IAW SRM 55-03, FIGURE 11. 2 L 7 2 4F A6WE 1999111100200 19991111 00200 NM 1999 11 11 CALA9901472 1 19991107 A 5240 SKIN BOEING 737 7373T0 1384582 NM R-1 DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND R-1 DOOR SKIN GOUGED JUST ABOVE LOWER HINGE ARM. THE GOUGED AREA WAS REMOVED AND A REPAIR WAS INSTALLE D IAW SRM 52-00-01. 2 L 7 2 4F RT A16WE 1999111100201 19991111 00201 NM 1999 11 11 CALA9901473 1 19991107 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND CABIN FLOORBEAM CORRODED AROUND NUTPLATE HOLES AT BS 986.5. THE CORRODED UPPER PART OF BEAM WAS REMOVE D AND A REPAIR WAS INSTALLED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999111100202 19991111 00202 WP 1999 11 11 CALA9901474 1 19991106 A 3350 60030451 POWER SUPPLY GRIMES DOUG DC9 DC982 3022082 WP ROW 23-27 INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33805 49249 INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE AT ROWS 23-27. THE BATTERY POWER SUPPLY AT STATION 1150 IN RT O VERHEAD BIN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00. 2 L 7 2 4F A6WE 1999111100203 19991111 00203 WP 1999 11 11 CALA9901475 1 19991107 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A 1 CRACK IN ANGLE AT BASE OF LT LOWER AFT SIDE VERTICAL STABILIZER. FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-05, FIGURE 23A. 2 L 7 2 4F A6WE 1999111100204 19991111 00204 NM 1999 11 11 CALA9901476 1 19991107 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 942 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 23371 INSPECTION FOUND CABIN SEAT TRACK CORRODED AT BS 942, LBL 25. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 1999111100205 19991111 00205 NM 1999 11 11 CALA9901477 1 19991108 A 3350 110283 LIGHT GRIMES BOEING 727 727232 1384082 NM ROW 22 INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND INTERIOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 22. THE LIGHT ASSEMBLY WAS REMOVED AND REPLA CED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1999111100206 19991111 00206 WP 1999 11 11 CALA9901478 1 19991108 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 455&506 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14079 46927 INSPECTION FOUND RT WING LEADING EDGE LOWER SKIN CRACKED AT STA XORS 455 AND STA XORS 506. BOTH CRACKS WERE 1 LONG. RE PAIRS WERE INSTALLED IAW DRAWING ARB2933-46, DRAWING ARB2933-10, SRM 57-10-00, FIGURE 49 AND 51-31-01. 2 L 7 3 4F A22WE 1999111100207 19991111 00207 SO 1999 11 11 COMA9910171 1 19991104 A 5210 MECHANISM EMB 120 EMB120RT SO PAX DOOR LACK OF LUBE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 266CA 120258 DOOR WARNING DURING FLIGHT. CLEANED AND LUBED DOOR MECHANISM. 2 L 7 2 4T RT A31SO 1999111100208 19991111 00208 EA 1999 11 11 COMA9960670 1 19991107 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 712CA 7244 1 CABIN EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1999111100209 19991111 00209 EA 1999 11 11 COMA9960671 1 19991106 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA NR 1 MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 713CA 280 7245 TAKEOFF CONFIG WARNING, SPOILER CONFIG WARNING. REPLACED THE NR 1 SECU. 2 L 7 2 4F RT A21EA 1999111100210 19991111 00210 EA 1999 11 11 COMA9960672 1 19991105 A 2421 GENERATOR CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 01 995CA 7229 RIGHT ENGINE GENERATOR FAILED DURING TAKEOFF. TRANSFERRED DISCREPANCY TO DEFERRED LIST PER MEL. 2 L 7 2 4F RT A21EA 1999111100211 19991111 00211 EA 1999 11 11 COMA9960673 1 19991104 A 5210 601R383951 BUSHING CNDAIR CL600 CL6002B19 EA PAX DOOR WORN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 978CA 7158 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED BUSHING AT UPPER PIVOT ASSY. 2 L 7 2 4F RT A21EA 1999111100212 19991111 00212 EA 1999 11 11 COMA9960674 1 19991104 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 934CA 7410 7042 FLAPS FAILED AT 8 DEGREES. REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 1999111100213 19991111 00213 NM 1999 11 11 UPS99231055 1 19991102 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 344 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI WHILE WORKING CARD NR 010022 FOUND SHEAR TIE WITH 2 EA EXISTING HOLES WITH EXCESSIVE DIAMETER AT BS 3 44 ABOVE RT NOSE CHORD WL 156. REMOVED DAMAGED SHEAR TIE AND REPLACED WITH FABRICATED SHEAR TIE. 2 L 7 3 4F A3WE 1999111100214 19991111 00214 NM 1999 11 11 UPS99231056 1 19991102 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1030 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI AFT BAY FRAME DENTED BS 1030 LBL 25 WL 150. REMOVED DAMAGE AND REPAIRED PER SRM 51-40-3. 2 L 7 3 4F A3WE 1999111100215 19991111 00215 NM 1999 11 11 UPS99231057 1 19991023 A 5753 65216937 TRACK BOEING 727 72725C 138400H NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI L/W I/B AFT FLAP I/B TRACK ON MID-FLAP IS CORRODED. REMOVED CORRODED TRACK, INSTALLED NEW TRACK PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999111100216 19991111 00216 NM 1999 11 11 UPS99231058 1 19991102 A 5720 SUPPORT BOEING 727 72725C 138400H NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CRACKED, T/E UPPER PANEL SUPPORT L CHANNEL JUST ABOVE THE VERTICAL BULB, APPROX 1 FT FROM THE OB END OF THE I/B AILERON. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-20-1. 2 L 7 3 4F A3WE 1999111100217 19991111 00217 NM 1999 11 11 UPS99231059 1 19991101 A 5753 651859933 CARRIAGE BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION ON NR 4 FLAP CARRIAGE SPINDLE FWD SHIM MATING SURFACE ORDERED AND RECEIVED NEW NR 4 FLA P CARRIAGE AND INSTALLED PER MM 27-51-03. 2 L 7 3 4F A3WE 1999111100218 19991111 00218 NM 1999 11 11 UPS99231060 1 19991103 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION ON SEAT TRACK AT BS 940 RBL 45 WL 208. REPLACED SEAT TRACK SEGMENT FROM BS 870 TO 960 RBL 45 PER 727 SRM 51-30-5, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999111100219 19991111 00219 NM 1999 11 11 UPS99231061 1 19991104 A 5347 BAC15201434 SEAT TRACK BOEING 727 72725C 138400H NM BS 362&369 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION ON SEAT TRACK AT BS 362 AND 369 RBL 45, WL 208 OUT OF LIMITS. REPLACED SEAT TRACK FROM BS 340 TO 390 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999111100220 19991111 00220 NM 1999 11 11 UPS99231062 1 19991104 A 5753 651926913 TRACK BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 4 FLAP TRACK UPPER SURFACE AT MOUNT PADS. REPLACED FLAP TRACK PER 727 MM. 2 L 7 3 4F A3WE 1999111100221 19991111 00221 NM 1999 11 11 UPS99231063 1 19991105 A 5330 SKIN BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-111-03.00-01) BULGE IN FUSELAGE SKIN BS 344, LBL 16, LWL 148 AND LEVELING COMPOUND SEP ARATED FROM INTERIOR STRUCTURE HORIZ WALKWAY BEAM FROM BS 335-BS 351, LBL 16, WL 152. REMOVED DAMAGE AND REPAIRED PER S RM 53-30-3. 2 L 7 3 4F A3WE 1999111100222 19991111 00222 NM 1999 11 11 UPS99231064 1 19991026 A 5320 WEB BOEING 727 72725C 138400H NM BS 758 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI UPPER WEB CRACKED ON INTERCOSTAL, BS 758, LBL 35, WL 208. REMOVED AND REPLACED UPPER WEB SKIN ON INT ERCOSTAL PER SRM 53-10-1 SRM 51-10-2, SRM 51-30-2. 2 L 7 3 4F A3WE 1999111100223 19991111 00223 NM 1999 11 11 UPS99231065 1 19991023 A 5753 65216938 TRACK BOEING 727 72725C 138400H NM LT TE AFT FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI L/W I/B AFT FLAP, CENTER I/B TRACK ON MID FLAP IS CORRODED. CORRODED TRACK REMOVED AND NEW TRACK INS TALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999111100224 19991111 00224 NM 1999 11 11 UPS99231066 1 19991023 A 5320 65163517 FRAME BOEING 727 72725C 138400H NM E/E DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON FWD E/E DOOR FRAME LT AND RT SIDE OF FWD LATCH. REMOVED AND REPLACED FRAME PER SRM 51-30-2, SRM 51-10-1, SRM 51-10-3, SRM 51-10-02, MM 51-20-151, SRM 51-20-4 AND SRM 51-20-4 MM 51-20-00. 2 L 7 3 4F A3WE 1999111100225 19991111 00225 NM 1999 11 11 UPS99231067 1 19991021 A 5753 65192492 TRACK BOEING 727 72725C 138400H NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 3 FLAP TRACK LOWER SURFACE AROUND SPOILER BEAM MOUNT HOLES. REMOV ED AND REPLACED NR 3 FLAP TRACK. 2 L 7 3 4F A3WE 1999111100226 19991111 00226 EU 1999 11 11 QXEA9902232 1 19991106 A 3350 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU ROW 8 INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 GEG - BOTH EXIT SIGNS AT ROW 8 ARE INOPERATIVE. REMOVED AND REPLACED BOTH EXIT SIGN ASSEMBLIES. OPERATIONAL CHECK GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999111100227 19991111 00227 WP 1999 11 11 ABXA9900760 1 19991104 A 3260 313 BULB DOUG DC9 DC933F 302207A WP LDG GEAR DOOR FAILED A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 933AX 47291 AFTER GEAR RETRACTION, GEAR DOOR OPEN LIGHT ILLUMINATED. RECYCLED GEAR AND LIGHT WENT OUT. CHECKED LANDING GEAR DOORS AND SWITCHES, NO DEFECTS NOTED. RELAMPED THE OPEN DOOR LIGHT. 2 L 7 2 4F A6WE 1999111100228 19991111 00228 NM 1999 11 11 SCNA99749 1 19991101 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 1064 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT STA 1064 RBL 44, FLANGE BROKEN. REMO VED SEAT TRACK IAW SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAW SRM 51100 2, MM 512002. INSTALLED IAW SRM 513002. 2 L 7 3 4F A3WE 1999111100229 19991111 00229 NM 1999 11 11 SCNA99750 1 19991026 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 380 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON FLOORBOARD SUPPORT ANGLE BETWEEN STA 380 AND 420, R BL 26. REMOVED CORROSION IAW SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IA W SRM 511002, MM 512002. INSTALLED IAW SRM 513002. 2 L 7 3 4F A3WE 1999111100230 19991111 00230 NM 1999 11 11 SCNA99751 1 19991024 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 1050&1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK ANGLE BETWEEN FS 1050 AND 1070 RBL 26. R EMOVED CORROSION IAW SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAW SRM 511 002, MM 512002. INSTALLED IAW SRM 513002. 2 L 7 3 4F A3WE 1999111100231 19991111 00231 NM 1999 11 11 SCNA99132 1 19991106 A 3350 LIGHT BOEING 727 727225 1384077 NM RT EMER EXIT INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED BROKEN WIRES AT AISLE BY LIGHT ASSEMBLY IAW MM 33501. 2 L 7 3 4F A3WE 1999111100232 19991111 00232 NM 1999 11 11 SCNA99133 1 19991105 A 3350 086861 LIGHT BOEING 727 727225 1384077 NM ROW 16 INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, AN EMERGENCY FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT SEAT ROW 16. REMOVED AND REPLACED THE LIGHT LAMP HOOLDER ASSEMBLY. LIGHT OPERATIONALLY CHECKS GOOD REF MM 335900. 2 L 7 3 4F A3WE 1999111100233 19991111 00233 WP 1999 11 11 SCNA99134 1 19991104 A 2611 30231R17 SMOKE DETECTOR DOUG DC10 DC1015 3022118 WP CARGO COMPT INOP A SCNA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 153SY 48276 DURING FLIGHT, THE AFT CARGO FIRE INDICATION AND NR 2 AFT SMOKE DETECTOR WAS ON INTERMITTENTLY. FIRED NR 1 AND NR 2 BOT TLES AND COMPLIED WITH THE COM. REMOVED AND REPLACED THE NR 2 AFT CARGO SMOKE DETECTOR AND BOTH FIRE BOTTLES. OPERATIO NAL TEST WAS NORMAL. 2 L 7 3 4F A22WE 1999111100234 19991111 00234 NM 1999 11 11 VNAA9911006 1 19991104 A 7603 001A761A1010100 SWITCH RACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT CONTROL LEVER FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 459PS 3070 DURING THE TAKE ROLL, THE NOSE WHEEL STEERING FAILED. THE AIRCRAFT WENT LEFT. THE FLIGHT CREW REGAINED CONTROL AND TAX IED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT CONDITION LEVER MICROSWITCH RACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-05. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RE LEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111100235 19991111 00235 1999 11 11 TC8A99027 4 19991105 A 3422 WIRE BOEING 727 72721C 138400M NM NR 2 DG FAILED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 705A 19134 ON TAXI OUT, FLAGS APPEARED ON NR 2 AND NR 2 CDI. REPAIRED WIRE AT NR 2 DG AND SECURED WIRING HARNESS. NR 2 DG, RMI AN D CD, OPS CHECK NORMAL IAW B727 MM 34-21-0. NR 2 COMPASS SYSTEM NORMAL. 2 L 7 3 4F A3WE 1999111100236 19991111 00236 EU 1999 11 11 RAIA9911011 1 19991106 A 5330 SKIN JETAIR JETSTM JETSTM4101 1500501 EU FRAME 537 DAMAGED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 558HK 41071 STL - RIGHT AFT FUSELAGE SKIN AT FRAME 537 SUSTAINED DAMAGE DURING RAMP OPERATION. MAINTENANCE REPAIRED DAMAGE IAW EOJ4 100-53-006-1. 2 L 7 2 4T RT A41NM 1999111100237 19991111 00237 GL 1999 11 11 RAIA9911007 3 19991106 A 6110 PROP ASSY. JETAIR JETSTM JETSTM4101 1500501 EU MCAULY 5JFR C5JFR36C1102 GL RIGHT FAILED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 552HK 7744 3265 41057 7500 - STL - FELT STRONG VIBRATION IN THE FLIGHT DECK FLOOR/RUDDER PEDALS. MAINTENANCE REPLACED RIGHT PROP. 2 L 7 2 4T RT A41NM 5 C P15WE 1999111100238 19991111 00238 1999 11 11 RAIA9911008 4 19991106 A 3418 0771065 STICK SHAKER BAG JETSTM JETSTM3201 1500217 EU NR 2 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 425AM 870 7508 - STL - STICK SHAKER WENT OFF. MAINTENANCE REPLACED NR 2 SIGNAL SUMMING UNIT. 2 L 7 2 4T RT A56EU 1999111100239 19991111 00239 EU 1999 11 11 RAIA9911009 1 19991107 A 7714 AG34 TACH GEN BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 432AM 1300 1300 883 66179 7313 - BMI - LEFT RPM DROPPED TO ZERO. MAINTENANCE REPLACED TACH GENERATOR FOR LEFT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999111100240 19991111 00240 1999 11 11 RAIA9911010 4 19991107 A 3418 0020BN4MODSW2 COMPUTOR EMB 145 EMB145 SO E/E COMPT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 804HK 145082 6305 - BO - SPS 2 ADVANCE FAIL LIGHT ILLUMINATED. MAINTENANCE REPLACED STALL COMPUTER. 2 L 7 2 4F RT T00011AT 1999111100249 19991111 00249 CE 1999 11 11 99ZZZX4215 1 19991025 A 5712 082217579 RIB CESSNA 402 402B 207590P CE MLG WW CRACKED A S HBCA K NONE O OTHER IN INSP/MAINT 1 SW 11 5040Q 14960 402B0347 DURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE FORWARD PORTION OF RIB, CESSNA P/N 0822175-79. THE RIB HAD BEEN MODIFIED IAW CESSNA SK 414-8E APPROXIMATELY 4,303 HOURS AGO, WHICH, BY LOCATION, IS NOT AS SOCIATED WITH THE CRACK SHOWN IN THE DRAWING. 1 L 7 2 3O A7CE 1999111100250 19991111 00250 CE 1999 11 11 99ZZZX4216 1 19991025 A 5712 082217574 RIB CESSNA 402 402B 207590P CE MLG WW CRACKED A S HBCA K NONE O OTHER IN INSP/MAINT 1 SW 11 5040Q 14960 402B0347 DURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE FORWARD PORTION OF RIB, CESSNA P/N 0822175-74. THE RIB HAD BEEN MODIFIED IAW CESSNA SK 414-8E APPROXIMATELY 4,303 HOURS AGO, WHICH, BY LOCATION, IS NOT AS SOCIATED WITH THE CRACK SHOWN IN THE DRAWING. 1 L 7 2 3O A7CE 1999111100253 19991111 00253 SO 1999 11 11 99ZZZX4219 2 19991025 A 8530 646657 CYLINDER HEAD CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO NR 2 CYLINDER SEPARATED A HBCA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 11 5040Q 416 402B0347 183255R DURING THE COURSE OF NORMAL FLIGHT, THE PILOT NOTICED RIGHT ENGINE RUNNING ROUGH WITH A DROP IN ITS MANIFOLD PRESSURE. T HE AIRCRAFT LANDED WITHOUT EVENT. MAINTENANCE WAS ABLE TO DETERMINE THAT THE NR 2 CYLINDER HEAD HAD SEPARATED FROM THE BARREL OF THE CYLINDER. THE DAMAGE WAS CONFINED TO THE CYLINDER, THE UPPER DECK LINES, INJECTOR LINES, INTAKE AND EXHAU ST PIPES WERE ALL UNDAMAGED. 1 L 7 2 3O 3 O A7CE E8CE 1999111100263 19991111 00263 SO 1999 11 11 WVBA01299 1 19991013 A 2140 A23D0475 REGULATOR ELECTROSYS FR65D793EL PIPER PA31 PA31350 7103110 SO HEATER FUEL LEAKING A WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 4082T A99050D39 318152089 DURING A NORMAL AIRCRAFT INSPECTION, FORWARD FUEL PRESSURE REGULATOR WAS FOUND TO BE EXTREMELY STAINED FROM FUEL LEAKING BETWEEN BODY HALVES. TIME IN SERVICE ON THIS PARTICULAR REGULATOR IS UNKNOWN. THERE HAS BEEN APPROX 120 HOURS SINCE L AST INSPECTED AND 1,191.2 HOURS TIME IN SERVICE ON THE HEATER ASSY ITSELF. SUBMITTER SUGGESTED THAT PARTICULAR ATTENTIO N BE PAID TO INSPECTING THESE REGULATORS DUE TO EXCESSIVE FAILURES IDENTICAL TO THIS ONE. (X) 1 L 7 2 3O A20SO 1999111100264 19991111 00264 CE 1999 11 11 99ZZZX4229 1 19991025 A 5712 SK4148E RIB CESSNA 402 402B 207590P CE LT MLG WW CRACKED A HBCA K NONE O OTHER IN INSP/MAINT 1 SW 11 5040Q 4303 402B0347 DURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, MULTIPLE CRACKS WERE FOUND IN THE PRIMARY COMPONENTS THAT MAKE UP CESSNA SERVICE KIT SK414-83. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT RIBS, FILLERS, DOUBLERS, AND ANGLES. 1 L 7 2 3O A7CE 1999111100265 19991111 00265 CE 1999 11 11 99ZZZX4230 1 19991025 A 5712 SK4148E RIB CESSNA 402 402B 207590P CE RT MLG WW CRACKED A HBCA K NONE O OTHER IN INSP/MAINT 1 SW 11 5040Q 4303 402B0347 DURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, MULTIPLE CRACKS WERE FOUND IN THE PRIMARY COMPONENTS THAT MAKE UP CESSNA SERVICE KIT SK404-83. CRACKS WERE FOUND ON BOTH LEFT AND RIGHT RIBS, FILLERS, DOUBLERS, AND ANGLES. 1 L 7 2 3O A7CE 1999111100270 19991111 00270 CE 1999 11 11 99ZZZX4237 1 19991007 A 3240 551417543 BRAKE CESSNA 500 550 2076604 CE MLG MALFUNCTIONED A FVAA O OTHER J WARNING INDICATION AP APPROACH 1 NE 03 300PY 849 5500806 WHILE ON APPROACH TO SCHEDULED DESTINATION, ALN, CREW EXTENDED LANDING GEAR AND MASTER CAUTION' 'LOW BRAKE PRESSURE', AN D ANTI-SKID INOP' ANNUNCIATORS ILLUMINATED. CREW CYCLED SKID CONTROL BREAKER, NO CHANGE NOTED. UPON LANDING, NO NORMAL BRAKING ACTION AVAILABLE. CREW UTILIZED EMERGENCY BRAKING. NORMAL BRAKING PARTIALLY RESTORED ON TAXI. AN ON-SITE REP AIR STATION TROUBLESHOT, COULD NOT DUPLICATE FAULT. CONSULATION RESULTED THAT THE GROUND FOR THE POWER BRAKE MOTOR NOT MADE THROUGH PIN 'P' OF CONNECTOR P160 (LANDING GEAR LEVER). SUBMITTER STATED RECYCLING OF LANDING GEAR ON APPROACH MAY HAVE RESTORED NORMAL BRAKING. 1 L 7 2 4F A22CE 1999111100276 19991111 00276 NM 1999 11 11 TWAA9915201 1 19991108 A 2910 AE1008809H0310 LINE BOEING 727 727231 1384079 NM RT MLG DOOR ACT RUPTURED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 05 54353 21985 THE 'A' HYDRAULIC SYSTEM DEPLETED WHEN THE LANDING GEAR WAS LOWERED. WAS NECESSARY TO MANUALLY CRANK DOWN THE RT MAIN L ANDING GEAR. REPLACED FAILED HYDRAULIC LINE FOR THE RT GEAR DOOR ACTUATOR. CHECK-C 7-18-99 MCI. 2 L 7 3 4F A3WE 1999111100277 19991111 00277 NM 1999 11 11 TWAA9915202 1 19991109 A 3350 767 BULB BOEING 757 757231 1384950 NM R1 & R4 DOORS FAILRED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 721TW 29954 THE EXTERIOR EMERGENCY LIGHTS AT THE NUMBER 1 AND 4 DOORS, RT SIDE, WERE INOPERATIVE. REPLACED THE BULB IN EACH. 2 L 7 2 4F RT A2NM 1999111100278 19991111 00278 WP 1999 11 11 TWAA9915203 1 19991108 A 5330 SKIN DOUG DC9 DC932 3022066 WP SERVICE DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING CHECK-C MAINT, FOUND 2 CRACKS IN SKIN IN FWD UPPER CORNER OF THE RT SIDE FORWARD CABIN SERVICE DOOR JAM. CRACKS WERE .0625 IN AND .3125 IN LONG COMING OUT OF RIVETS, AND EDDY CURRENT SHOWED A CRACK THAT WAS UNDER .0625 INCHES IN LE NGTH. CUT OUT CRACKS IN SKIN AND INSTALLED DOUBLERS PER SRM 53-05, FIG 112, SHEET 3 AND ARA 16421. 2 L 7 2 4F A6WE 1999111100279 19991111 00279 WP 1999 11 11 AT9900756 1 19991028 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOORBEAM TO BE CORRODED AROUND NUT PLATE HOLE. CUT OUT C ORRODED SECTION AT BS 237 RBL 52 AND FABRICATED REPAIR ANGLE, FILLER, AND RUB STRIP IAW DC9 SRM 53-06 FIG 20A, 51-10-02, 51-10-03, 51-10-04, 51-10-05, AND 53-05 FIG 20A. 2 L 7 2 4F A6WE 1999111100280 19991111 00280 WP 1999 11 11 AT9900772 1 19991020 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FLOOR SUPPORT AT BS 160 TO BS 200. REMOVED A ND REPLACED FLOOR SUPPORT AT BS 160 TO BS 200 IAW DC9 SRM 53-11-01, 51-10-02, 51-10-03, 51-10-04, AND 51-30-02. 2 L 7 2 4F A6WE 1999111100281 19991111 00281 WP 1999 11 11 AT9900773 1 19991012 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 370-427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION AT BOTTOM OF FORWARD CARGO DOOR JAMB. FABRICAT ED AND INSTALLED FILLER, DOUBLER, AND TRIPLER AT BS 370-427 IAW DC9 SRM 51-10-03, 51-10-04, 51-10-05, 51-30-01, 51-30-02 , AND EO 99-1329. 2 L 7 2 4F A6WE 1999111100282 19991111 00282 WP 1999 11 11 AT9900774 1 19991105 A 2560 7270001 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 CHECK RIGHT SLIDE PACK AND COVER. REINSTALLED RIGHT SLIDE COVER IAW DC9 MM 25-60. 2 L 7 2 4F A6WE 1999111100283 19991111 00283 WP 1999 11 11 AT9900778 1 19991027 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 718 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND WEB SUPPORT AT BS 718 LBL 56 TO BE CORRODED. REMOVED CORR OSION AND FOUND OUT OF LIMITS. FORMED NEW WEB SUPPORTS AND INSTALLED IAW DC9 SRM 51-10-03, 53-01 FIG 1, 51-10-02, 51-10 -04, AND 51-30-02. 2 L 7 2 4F A6WE 1999111100284 19991111 00284 WP 1999 11 11 AT9900779 1 19991022 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR SUPPORTS FROM LEFT TO RIGHT SIDE AT BS 200 AND FORWA RD ENDS OF SEAT TRACKS TO HAVE CORROSION. REPLACED FLOOR SUPPORTS AND TREATED SEAT TRACKS IAW DC9 SRM 51-30-02 AND 51-1 0-03. 2 L 7 2 4F A6WE 1999111100285 19991111 00285 WP 1999 11 11 AT9900780 1 19991028 A 5320 59124921 JAMB DOUG DC9 DC932 3022066 WP R-1 DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND R-1 DOOR JAMB PAN TO HAVE CORROSION, HOLE, AND DENT IN AFT SIDE. REMOVED AND REPLACED TRANSITION PANEL, FLOOR SUPPORT, AND FORWARD SEAL ANGLE IAW DC9 SRM 51-10-04, 53-05 FIG 55, 51-10-2A, 51-10-03, 51-30-02, AND 51-30-01. 2 L 7 2 4F A6WE 1999111100286 19991111 00286 WP 1999 11 11 AT9900781 1 19991022 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOORBOARD SUPPORT HAT CHANNELS BETWEEN BS 200 AND BS 218 TO BE CORRODED. REMOVED AND REPLACED HAT CHANNELS IAW DC9 SRM 51-30-02. 2 L 7 2 4F A6WE 1999111100287 19991111 00287 WP 1999 11 11 AT9900790 1 19991020 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 229 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND CABIN FLOOR SUPPORT AT BS 229 AND LBL 14 CORRODED BEYOND LIMITS AND SUB-FLOOR SKIN CRACKED. REMOVED AND REPLACED FLOOR SUPPORT AT BS 229. FABRICATED AND INSTALLED REPAIR DOUBLER ON SUB-FLOOR IAW DC9 SRM 53-11-1, 53-01 FIG 2, 51-10-3 , 51-30-2, AND 51-10-4. 2 L 7 2 4F A6WE 1999111100288 19991111 00288 WP 1999 11 11 AT9900791 1 19991027 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 197 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND CABIN FLOOR SUPPORT AT BS 197 AND BL 0 TO LBL 44 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW DC9 SRM 51-10-2 , 51-30-5 AND 53-11-1 FIG 13. 2 L 7 2 4F A6WE 1999111100289 19991111 00289 WP 1999 11 11 AT9900792 1 19991025 A 5730 PANEL DOUG DC9 DC932 3022066 WP WS 434-486 DELAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND RT WING TRAILING EDGE PANEL UPPER AND LOWER SURFACES DELAMINATED AT WS 434-486. REMOVED UPPER SKIN, DOUBLER, HONE YCOMB CORE AND INNER SKIN. FABRICATED REPLACEMENT UPPER SKIN, UPPER SKIN EXTERNAL DOUBLER AND INNER SKIN. CUT AND FIT HONEYCOMB REPLACEMENT CORE. ACCOMPLISHED COMPOSITE REPAIR ON PANEL IAW TIMCO EO 99-1320 AND DC9 SRM 51-70-2. 2 L 7 2 4F A6WE 1999111100290 19991111 00290 WP 1999 11 11 AT9900798 1 19991022 A 5753 PANEL DOUG DC9 DC932 3022066 WP RT WING DISBONDED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND RT WING TRAILING EDGE PANEL DISBONDED. REMOVED UPPER SKIN, DOUBLER, CORE AND INNER SKIN. FABRICATED REPLACEMENT UPPER SKIN, UPPER SKIN EXTERNAL DOUBLER AND INNER SKIN. CUT AND FIT HONEYCOMB REPLACEMENT CORE. ACCOMPLISHED COMPOSITE REPAIR ON PANEL IAW TIMCO EO 99-1319 AND DC9 SRM 51-70-2. 2 L 7 2 4F A6WE 1999111100291 19991111 00291 WP 1999 11 11 AT9900799 1 19991101 A 3231 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG DOOR MALFUNCTIONED A ZZDA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 15 836AT 47397 AFTER TAKEOFF AND UPON GEAR RETRACTION A FLUTTER NOISE CAME FROM THE NOSE GEAR AREA. FOUND RIGHT NOSE GEAR DOOR OPEN. V ISUALLY INSPECTED NOSE GEAR DOORS AND WHEEL WELL. FOUND NOTHING ABNORMAL. CLOSED GEAR DOOR. OK FOR SERVICE PER MM 52- 80. 2 L 7 2 4F A6WE 1999111100292 19991111 00292 EU 1999 11 11 MALA976629 1 19991105 A 3320 6500110 SOCKET SAAB SF340 340B 7860101 EU ROW 1A FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 415XJ 340B415 FA NOTED SMOKE COMING FROM REAR OF FA PANEL. MAINTENANCE REPLACED FWD LIGHT SOCKET ON SEAT 1A SIDEWALL. OPS CHECKS GOO D. 2 L 7 2 4T RT A52EU 1999111100293 19991111 00293 EU 1999 11 11 MALA976630 1 19991104 A 3320 6500110 SOCKET SAAB SF340 340B 7860101 EU CABIN FAILED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 418XJ 418 FA REPORTS HAZE IN CABIN. RETURNED TO GATE. MAINTENANCE REPLACED SOCKET AND BALLAST. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999111100294 19991111 00294 EU 1999 11 11 MALA976631 1 19991104 A 3230 GA30 RELAY BAC 146 AVRO146RJ85A 1500097 EU LANDING GEAR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 502XJ E2307 CREW REPORTED DURING GEAR RETRACTION HAD TO USE OVERRIDE BUTTON. MAINTENANCE REPLACED RELAY AT GA30. COMPLETED OPS CHE CK OF LANDING GEAR CONTROL IAW ARJ 85 AMM 32-30-14. ALL CHECKS GOOD AT THIS TIME. 2 H 7 4 4F RT A49EU 1999111100295 19991111 00295 EU 1999 11 11 MALA976632 1 19991107 A 5270 INDICATION BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 505XJ E2313 AFTER TAKEOFF MAIN CABIN DOOR AND GALLEY SERVICE DOOR BECAME DISARMED. RETURNED TO RDU. MAINTENANCE PERFROMED OPS TEST ON CABIN DOOR AND GALLEY SERVICE DOOR IAW 52-11-00. FOUND NO DEFECT WITH DOOR RIGGING ON DOORS. PASSED ALL OPERATION CHECKS. NO DISCREPANCYS FOUND. 2 H 7 4 4F RT A49EU 1999111100296 19991111 00296 NM 1999 11 11 AWXA9900398 1 19991107 A 2131 21173886 CONTROLLER BOEING 757 757225 1384959 NM CABIN MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 915AW 39448 5763 22209 AIR-TURNBACK, AFTER T/O CABIN AUTO INOP MSG AND A/C WAS NOT PRESSURIZING WITH NR 1 SWITCHED TO AUTO CONT NR 2, NO CHANGE . MANUAL CONTROL OF OUTFLOW VALVE WORKED OK. RETURNED TO PHX. REMOVED AND REPLACED NR 1 AND NR 2 CABIN PRESS CONTROLL ERS IAW 21-31-04 AND CABIN PRESS OUTFLOW ACTUATOR IAW 21-31-04. TT FOR CONTROLS 0081408 S/N 02400-0008957, S/N 07766. T T OUTFLOW ACT 0083127, S/N 04758. (M) 2 L 7 2 4F RT A2NM 1999111100297 19991111 00297 NM 1999 11 11 AWXA9900399 1 19991107 A 3397 BMS13131122 WIRE BOEING 737 7373G7 1384595 NM ROW 18 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 SEAT MOUNTED EMERGENCY LIGHT INOP ROW 18. REPLACED SPLICES ON WIRE. 2 L 7 2 4F RT A16WE 1999111100298 19991111 00298 NM 1999 11 11 AWXA9900400 1 19991107 A 3397 BMS13131122 WIRE BOEING 737 7372M8 1384483 NM ROW 4 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 21955 EMERGENCY LIGHT INOP, ROW 4. REPAIRED BROKEN WIRE, OPS CK NML. 2 L 7 2 4F A16WE 1999111100299 19991111 00299 EU 1999 11 11 AWXA9900401 1 19991108 A 5320 D53472193200 SUPPORT AIRBUS 320 A320231 3930325 EU BS 765 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 CORROSION LEFT AND RIGHT FLOOR SUPPORT Y765 RT BETWEEN FRAMES 66 AND 68, CORROSION AROUND CLI P NUT (TOP AND BOTTOM). REPAIRED RT FLOOR SUPPORT AT FR 68 Y 765 AS PER ER 26-5341-99294-EYI. PRIMED AND PAINTED AS PE R SRM 51-75-17-2. REMOVED AND REPLACED DAMAGED LT FLOOR SUPPORT, FABRICATED REPLACEMENTS AND INSTALLED AS PER SRM 51-74 -00. 2 L 7 2 4F RT A28NM 1999111100300 19991111 00300 EU 1999 11 11 AWXA9900402 1 19991108 A 5347 531120922056 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 1292 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 628AW 67 RT INBD AND OUTBD SEAT TRACKS Y-1292 CORRODED AT FRAME 20. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACKS RT INBD AN D OUTBD Y 1292 AS PER DWG NR 53112092205 AND 206 RESPECTIVELY. 2 L 7 2 4F RT A28NM 1999111100301 19991111 00301 EU 1999 11 11 AWXA9900403 1 19991108 A 5315 D53112613200 TRACK AIRBUS 320 A320231 3930325 EU Y189 RH FR20 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 67 FLOOR PANEL SUPPORT RT 189 FR 20 CORRODED. FABRICATED NEW PART PER DWG D 53112613200. INSTALLED PER SRM 51-72-11, AND SRM 51-42-11. 2 L 7 2 4F RT A28NM 1999111100302 19991111 00302 EU 1999 11 11 AWXA9900404 1 19991108 A 5315 D53472090 SUPPORT FLOOR AIRBUS 320 A320231 3930325 EU Y1292RH @FR66 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 67 CORROSION ON RT FLOOR SUPPORT Y1292 RT AT FR 66. FABRICATED FLOOR SUPPORT PER DWG NR D 53472090 AND INSTALLED AS PER SR M 51-42-11. 2 L 7 2 4F RT A28NM 1999111100303 19991111 00303 EU 1999 11 11 AWXA9900405 1 19991108 A 5315 D53112087200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU Y254LH FR20-17 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 67 CORROSION AROUND A NUT HOLES B/T FR 20-17. FABRICATED AND INSTALLED FLOOR SUPPORT PER DWG NR D53112087 AND SRM 51-42-00 , SRM 51-72-00. 2 L 7 2 4F RT A28NM 1999111100304 19991111 00304 EU 1999 11 11 AWXA9900406 1 19991108 A 5315 D543772075001 SUPPORT AIRBUS 320 A320231 3930325 EU Y1732RH FR 65-66 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 67 CORROSION RT FLOOR SUPPORT Y1732 BTWN FR 65-66, CORROSION AROUND CLIP. NUT HOLES (TOP AND BOTTOM). REPLACED BEAM AS PE R DWG NR D534772075001 AND INSTALLED IAW A-320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 1999111100305 19991111 00305 NM 1999 11 11 RAAA99B2062 1 19991105 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 10DEF DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 EMERGENCY LIGHT AT ROW 10 D, E, F, DOES NOT TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999111100306 19991111 00306 NM 1999 11 11 RAAA99B2063 1 19991105 A 3350 873100112 SIGN INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN BROKEN A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 MID CABIN EXIT IDENTIFIER CASE IS BROKEN. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1999111100307 19991111 00307 NM 1999 11 11 RAAA99B2064 1 19991108 A 3350 S106 BATTERIES GRIMES 1102833 BOEING 727 72722C 138400F NM AIRSTAIR DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV NSN 19098 AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1999111100308 19991111 00308 1999 11 11 RAAA99E4080 4 19991105 A 2565 80181 MOUNT LKHEED 188 188C 5262604 SO PAX DOOR SLIDE STICKING A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 EMERGENCY EVACUATION SLIDE AT PAX ENTRY DOOR, STICKING IN FLOOR SLOT. LUBRICATED EVAC SLIDE MOUNTS, OPERATION CHECKED N ORMAL. 2 L 7 4 4T 4A22 1999111100309 19991111 00309 EA 1999 11 11 COMA9960675 1 19991107 A 5320 60034017587 STIFFENER CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 SUSIE: THIS IS A TEST ODR....HAD TO REDO THEM ON MY COMPUTER....CALL AND LET ME KNOW IF YOU RECEIVED THIS OK....LINDA 6 06-767-2708. 2 L 7 2 4F RT A21EA 1999111100310 19991111 00310 EA 1999 11 11 COMA9960676 1 19991107 A 5320 601R3111357 CLIP CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 15845 7011 FS 280 LBL9 HAS ZEA CLIPS P/N 601R31113-57 CRACKED. REMOVED CRACKED ANGLE AND REPLACED WITH NEW SERVICEABLE ANGLE P/N 6 01R31113-57 IAW WVAC EO 601R-53-0578A. 2 L 7 2 4F RT A21EA 1999111100311 19991111 00311 EA 1999 11 11 COMA9960677 1 19991104 A 5320 6004017351 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 15845 7011 THE FORWARD J ANGLE AT FS 280 BETWEEN LBL AND RBL 9.0 IS CORRODED. REMOVED AND REPLACED FORWARD J ANGLE AT FS 280 BETWE EN LBL 9.0 AND RBL 9.0 IAW WVAC EO 601R-53-0571. 2 L 7 2 4F RT A21EA 1999111100312 19991111 00312 EA 1999 11 11 COMA9960678 1 19991107 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 `912C 15845 7011 AFT J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED AND CRACKED. REPAIRED AFT J-ANGLE AT FS 280 BETWEEN LBL 9 .0 AND RBL 9.0 IAW WVAC EO 601R-53-0580A. 2 L 7 2 4F RT A21EA 1999111100313 19991111 00313 EA 1999 11 11 COMA9960679 1 19991107 A 5315 60034017 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 15845 7011 THE FLOOR WEB AT FS 280 IS CORRODED ON THE UPPER EDGE BETWEEN LBL 9.0 AND RBL 9.0. REPAIRED THE FLOORBEAM WEB AT FS 280 .00 BETWEEN LBL 9.0 AND RBL 9.0 IAW WVAC EO 601R-53-0581. 2 L 7 2 4F RT A21EA 1999111100314 19991111 00314 EA 1999 11 11 COMA9960680 1 19991107 A 5320 6003401717 SUPPORT CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 15845 7011 FLOOR MEMBER AT FS 280.00 IS CRACKED L/2-.75 INCH, APPROXIMATELY 1 TO THE RIGHT OF FLOOR SUPPORT AT RBL 9.0. REPAIRED F LOOR MEMBER AT FS 280.00 IAW WVAC EO 601R-53-0579. 2 L 7 2 4F RT A21EA 1999111100315 19991111 00315 EA 1999 11 11 COMA9960681 1 19991106 A 5320 6003603023 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 10013 7092 FS 718 RH5 AFT DOUBLER IS CRACKED BETWEEN STR 11-12. REPLACED CRACKED DOUBLER AT FS 718 RHS BETWEEN STR 11 AND 12 WITH NEW DOUBLERS IAW CRJ REO 601R-53-61-193. 2 L 7 2 4F RT A21EA 1999111100316 19991111 00316 NM 1999 11 11 QXEA9901605 1 19990720 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 268 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 PDX - LEFT INBOARD SEAT TRACK HAS TWO GAUGES AT X268. REPAIRED IAW DHC-8 SRM 51-26-26. 2 H 7 2 4T RT A13NM 1999111100317 19991111 00317 WP 1999 11 11 99FDEA00461 1 19991107 A 5753 FITTING DOUG DC10 DC1010F 3022111 WP LT TE FLAP MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 385FE 46619 SNRM 764 - LT WING O/B FLAP, I/B OF O/B FLAP VANE ATTACH FITTINGS TO VANE TRACK IS MISS 4 ATTACH BOLTS. REMOVED ALL BOL TS WITH NEW PER MM 27-50-03-2. ENCAPSULATED ALL BOLTS AND NUTS WITH SEALANT PER MM 57-10-00. OK FOR SERVICE. 2 L 7 3 4F A22WE 1999111100318 19991111 00318 NM 1999 11 11 99FDEA00462 1 19990910 A 5741 BOTTLE PIN BOEING 727 72722 1384002 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 RT FWD BOTTLE BOLT (SPAR TERMINAL PIN) HAS CORROSION. REMOVED AND REPLACED NEW BOTTLE BOLT PIN SEALED. 2 L 7 3 4F A3WE 1999111100319 19991111 00319 NM 1999 11 11 99FDEA00463 1 19990809 A 5412 FIREWALL BOEING 727 72722 1384002 NM NR 2 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 185FE 18871 LT FWD INTERNAL COMP OVERTOP CF NR 2 ENG HORZ FIREWALL/PYLON, 1 1/2 CRACK IN HORIZONTAL ANGLE RADIUS UPPER SECTION OF CO MP. REPLACED CRACKED CHORD ANGLE PER SRM 51-16-1. 2 L 7 3 4F A3WE 1999111100320 19991111 00320 NM 1999 11 11 99FDEA00464 1 19990922 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 1148-1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 STR 30 IS CORRODED BETWEEN BS 1148 AND 1166 IN AFT CARGO. REMOVED AND REPLACED STR 30 PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999111100321 19991111 00321 1999 11 11 99UAL900443 4 19990912 A 3414 AIR SPEED IND HONEYWELL 4039891906 BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT COCKPIT FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 664UA 98113970 29236 MACH AIRSPEED INDICATOR FAILURE. FIRST OFFICER MACH AIRSPEED FLAG IN VIEW AND INDICATOR FROZE AT 170KTS ON TAKEOFF, RE MAINED THAT WAY FOR APPROX 10 SEC. A TAP TO THE CASE RETURNED TO NORMAL. REPLACED FIRST OFFICER MACH AIRSPEED INDICATO R. SHOP FINDINGS, COMPONENT SENT TO THE MANUFACTURER IN WARRANTY. SECOND SHOP VISIT OF THIS UNIT, FAULT CONFIRMED, COU NTER BINDING, REPLACED THE DRIVER MOTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 1999111100322 19991111 00322 NM 1999 11 11 99UAL900561 1 19991029 A 2131 CONTROLLER HAMILTON STA 7638101 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7445U 21899 FLIGHT EXPERIENCED PRESSURIZATION PROBLEMS AFTER DEPARTING ORD. CABIN RATE OF DESCENT EXCESSIVE DURING ASCENT. RETURNE D TO ORD. *S/D* PROBABLE CAUSE WAS TRACED DOWN TO THE CABIN PRESSURE CONTROLLER. REPLACED CABIN PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 1999111100323 19991111 00323 NM 1999 11 11 99UAL900562 1 19991029 A 2130 SELECTOR PANEL HAMILTON STA 7110024 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7258U 21405 CABIN NOT CONTROLLABLE IN AUTO, STANDBY OR MANUAL MODE. RETURNED TO ORD. *S/D* NO OBVIOUS CAUSE OF PROBLEMS WERE DET ECTED DURING CHECK OF PRESSURIZATION SYSTEM DURING MAINTENANCE. REPLACED CABIN PRESSURE SELECTOR PANEL AS PRECAUTIONAR Y. 2 L 7 3 4F 4 F A3WE E2EA 1999111100324 19991111 00324 EU 1999 11 11 99UAL900563 1 19991030 A 3350 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT WING DISCONNECTED A UALA K NONE L J NO TEST WARNING INDICATION IN INSP/MAINT 1 WP 29 408UA 457 CABIN EMERGENCY LIGHTING SYSTEM TEST GIVES STATUS OF 'EXT LOADS EMER R' ON PTP DISPLAY. *S/D* 'EXT LOADS EMER R' WAS S HOWN DURING TEST ON PTP. CANNON PLUG WAS FOUND DISCONNECTED FROM RT WING AFT LIGHT ASSEMBLY (62WL). CANNON PLUG WAS RE CONNECTED AND CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 1999111100325 19991111 00325 NE 1999 11 11 99UAL900564 2 19991030 A 7230 COMPRESSOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE DAMAGED A UALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 29 933UA 26659 724415 DURING CLIMBOUT, THE NUMBER ONE ENGINE STALLED THREE TIMES. REDUCED POWER TO IDLE AND THE ENGINE STABILIZED. THE CREW REPORTED NO EXCEEDED LIMITS. *S/D* BORESCOPE THE ENGINE AND DISCOVERED THAT THE HIGH PRESSURE COMPRESSOR WAS DAMAGED B EYOND SERVICEABLE LIMITS. REPLACED THE ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111100326 20001011 00326 NM 2000 10 11 99UAL900565 1 19991101 A 2431 18550 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BATTERY BAY DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 659UA 27114 RTF WITH MAIN BATTERY EICAS MESSAGE. *S/D* REPLACED MAIN BATTERY, CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999111100327 19991111 00327 NM 1999 11 11 99UAL900566 1 19991102 A 3350 900835A BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7442U 21896 LEFT WING, LEFT FORWARD OVERWING EMERGENCY EXIT EXTERIOR LIGHT ASSEMBLY IS INOPERATIVE. *S/D* REPLACED BATTERY CARTRID GE. 2 L 7 3 4F 4 F A3WE E2EA 1999111100328 19991111 00328 NM 1999 11 11 99UAL900567 1 19991030 A 2120 AIR DIST BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 614UA 21875 OIL/ELECTRICAL SMELL IN CABIN. DIVERTED TO DEN. CREW REPORT ODOR IN CABIN AROUND AREA OF SEATS 1DE AND 2DE. ODOR REMA INS WITH CABIN LIGHTS AND ENTERTAINMENT SYSTEMS 'OFF'. 2 L 7 2 4F 4 F RT A1NM E3NE 1999111100329 19991111 00329 EU 1999 11 11 99UAL900568 1 19991101 A 2923 O-RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD PUMP FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 432UA 587 FLIGHT CREW ADVISED OVERHEAD MEMPHIS LOST YELLOW SYSTEM HYDRAULIC. ELECTED TO DIVERT TO DFW FOR REPAIRS. LANDED 6.8 OV ERWEIGHT AT 149,000 LBS. *S/D* FOUND O-RING AT BOTTOM OF YELLOW PUMP PRESSURE LINE TORN. REPLACED O-RING AND SERVICED YELLOW SYSTEM TO 2SVC TASK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999111100330 20001011 00330 NE 2000 10 11 99UAL900569 2 19991101 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WING STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 417UA 483 FLT CREW REPORTS SUSPECTED ENGINE STALL WHEN PULLING THROTTLE BACK TO NEAR IDLE IN ORDER TO SLOW ACFT. ALTITUDE WAS FL 350. IGNITION MSG DISPLAYED FOR APPROX 7 SECS. UNABLE TO DETERMINE WHICH ENG STALLED. *S/D* CHRONIC TOP-OF-DESCENT STALLS HAVE BEEN UNDER INVESTIGATION BY UA AND THE ENGINE MANUFACTURER IAE FOR SIX MONTHS. DURING THIS TIME FRAME INTER IM MEASURES HAVE BEEN IMPLEMENTED BY RECOMMENDING FLIGHT CREW USE OF ANTI-ICE BLEED WHEN MAKING SIGNIFICANT POWER REDUCT IONS ABOVE FLIGHT LEVEL 290. THIS HAS ELIMINATED ALL EVENTS OF STALLS SINCE THIS INCIDENT OCCURRED. A FINAL FIX FROM T HE MANUFACTURER IS EXPECTED BY MARCH 2000. 2 L 7 2 4F 4 F RT A28NM E40NE 1999111100331 19991111 00331 NM 1999 11 11 99UAL900570 1 19991103 A 2722 658D1003 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER TRIM FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 29 655UA 25393 RUDDER TRIM INOP. DIVERTED TO ORD. C/B RESET, NO HELP. *S/D* THE INOP CONDITION OF THE RUDDER TRIM SYSTEM WAS DUE TO AN INTERMITTENT INTERNAL FAULT OF THE OF THE RUDDER TRIM ACTUATOR. THE SUBJECT ACTUATOR WAS REPLACED PER MM 27-21-11 A ND ALL OPS CHECKS ARE NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999111100332 19991111 00332 NM 1999 11 11 99UAL900571 1 19991102 A 3230 3910028101 BYPASS VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NLG FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 205UA 28714 NOSE GEAR DISAGREE LIGHT ON. FLY-BY CONFIRMED NOSE GEAR NOT DOWN AND DOORS NOT OPEN. GEAR WAS EXTENDED BY ALTERNATE ME THOD. *S/D* NOSE LANDING GEAR FAILED TO EXTEND DUE TO A FAILURE OF THE NOSE LANDING GEAR SELECTOR BYPASS VALVE (391002 8-101). THE SELECTOR BYPASS VALVE WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999111100333 19991111 00333 NM 1999 11 11 99UAL900572 1 19991103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER CR CRUISE 1 WP 29 119UA 28812 ALL EMERGENCY LIGHTS CAME ON AT LEVEL OFF. CYCLING BOTH SWITCHES AND CB'S, NO HELP. 2 L 7 4 4F 4 F RT A20WE E24NE 1999111100334 19991111 00334 NM 1999 11 11 99UAL900573 1 19991104 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 183UA 25379 RT SIDE OVERWING EMERGENCY LIGHT IS INOP, MOST FWD LIGHT ASSEMBLY AFT LAMP ONLY. 2 L 7 4 4F 4 F RT A20WE E24NE 1999111100335 19991111 00335 WP 1999 11 11 ABXA9900761 1 19991103 A 5320 99220422 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 484 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FLOOR SUPPORT FITTING CRACKED AT STATION 484 AND LONGERON 23 RIGHT. REPAIRED IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999111100336 19991111 00336 WP 1999 11 11 ABXA9900762 1 19991103 A 5320 99220422 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 913 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D CHECK, FOUND VERTICAL FLOOR SUPPORT FITTING CORRODED AT STATION 813 AND LONGERON 23 RIGHT. REPLACED FITTING IA W DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999111100337 19991111 00337 WP 1999 11 11 ABXA9900763 1 19991103 A 5320 99220421 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 484 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FLOOR SUPPORT FITTING CRACKED AT STATION 484 AND LONGERON 23 LEFT. REPLACED FITTING IAW DC9 SRM 5 1-30-2. 2 L 7 2 4F A6WE 1999111100338 19991111 00338 WP 1999 11 11 ABXA9900764 1 19991103 A 5755 591005551 SKIN DOUG DOUG DC9 DC932F 3022067 WP RT SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND RIGHT INBOARD GROUND SPOILER DELAMINATED ON UPPER SURFACE. REPAIRED SPOILER IAW DC9 SRM 51-70-2. 2 L 7 2 4F A6WE 1999111100339 19991111 00339 WP 1999 11 11 ABXA9900765 1 19991103 A 5313 3753728501 LONGERON DOUG DOUG DC8 DC862 3021970 WP BS 1185 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 DURING C-CHECK, FOUND LONGERON 34 AND 36 RIGHT, STATION 1185 CRACKED AT PRODUCTION SPLICE. REPAIRED IAW ABX REA D853-33 152MR. 2 L 7 4 4F 4A25 1999111100340 19991111 00340 WP 1999 11 11 MWEA99782 1 19991103 A 2730 CONTROLS DOUG DC9 DC932 3022066 WP ELEVATOR MALFUNCTIONED A MWEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 31 215ME 47744 AT APPROX FL 200, ELEVATOR CONTROL ACTIVITY WAS LOST AND TRIM WAS USED TO SUSTAIN FLIGHT. MAINTENANCE REMOVED AND REINS TALLED PANELS 63084 AND 63104 ON HORIZONTAL STAB. INSPECTED FOR WATER AND DEBRIS BLOCKING DRAIN HOLES, NONE FOUND. OK FOR SERVICE AT THIS TIME. 2 L 7 2 4F A6WE 1999111100341 19991111 00341 WP 1999 11 11 MWEA99783 1 19991106 A 2560 113317 SLIDE DOUG DC9 DC914 3022034 WP GALLEY DOORWAY DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 GALLEY SERVICE DOOR EVACUATION SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999111100342 19991111 00342 WP 1999 11 11 MWEA99784 1 19991107 A 3350 60030431 BATTERY PACK DOUG DC9 DC914 3022034 WP ROW 9-11 DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 80ME 45795 EMERGENCY LIGHTS DID NOT ILLUMINATE ABOVE LEFT OVERWING EMERGENCY EXIT OR AT ROWS 9 TO 11 CEILING EMERGENCY LIGHTS. MAI NTENANCE REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1999111100343 19991111 00343 WP 1999 11 11 MWEA99785 1 19991105 A 5511 991841349 RIB DOUG DC9 DC932 3022066 WP HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 LEFT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION HAS A CRACK ON THE INBOARD RIB. MTC DRILLED UP AND INSTALLED NE W RIB WEB. 2 L 7 2 4F A6WE 1999111100344 19991111 00344 NM 1999 11 11 MWEA99786 1 19991105 A 3350 CONNECTOR DOUG MD88 MD88 3023688 NM CABIN LOOSE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 701ME 49760 FIVE CONSECUTIVE LIGHT SEGMENTS OF FLOOR TRACK LIGHTING INOPERATIVE. FOUND CONNECTOR OF AT L2-843, RECONNECTED CONNECTO R. OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 1999111100345 19991111 00345 WP 1999 11 11 MWEA99787 1 19991109 A 5730 99374983 SKIN DOUG DC9 DC981 3022081 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 LEFT WIND LEADING EDGE UPPER SKIN HAS A BULGE AT ANTI-ICE TELESCOPING DUCT. MAINTENANCE FABRICATED AND INSTALLED SKIN D OUBLER REPAIR. 2 L 7 2 4F A6WE 1999111100346 19991111 00346 WP 1999 11 11 MWEA99788 1 19991109 A 5311 9911839243 FRAME DOUG DC9 DC982 3022082 WP BS 1463 MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS REPAIR ON CANTED FRAME 1463 AT LONGERON 15 TO 18 LEFT IS NOT ACCEPTABLE. MAINTENANCE FABRICATED AND INSTALLED FRAME REPAIR. 2 L 7 2 4F A6WE 1999111100347 19991111 00347 WP 1999 11 11 MWEA99789 1 19991109 A 5311 9912249103 FRAME DOUG DC9 DC982 3022082 WP BS 1380 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FRAME AT STATION 1380 HAS ELONGATED HEAT EXCHANGER SUPPORT ROD HOLE BETWEEN LONGERON 12 AND 13 LEFT. MAINTENANCE FABRIC ATED AND INSTALLED HOLE REPAIR BUSHING. 2 L 7 2 4F A6WE 1999111100348 19991111 00348 WP 1999 11 11 MWEA99790 1 19991109 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP BS 522 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LOWER LEG OF FUSELAGE FRAME 522 HAS CORROSION AT LONGERON 30. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1999111100349 19991111 00349 WP 1999 11 11 MWEA99791 1 19991109 A 5320 49128171 FITTING DOUG DC9 DC932 3022066 WP BS 427 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FORWARD CARGO PIT AFT CARGO DOOR JAMB UPPER STRUT FITTING IS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1999111100350 19991111 00350 WP 1999 11 11 MWEA99792 1 19991109 A 5311 59114481 FRAME DOUG DC9 DC932 3022066 WP BS 503 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FUSELAGE FRAME 503 AT LONGERON 25 RIGHT IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999111100351 19991111 00351 WP 1999 11 11 MWEA99793 1 19991109 A 5320 5956028113 SUPPORT DOUG DC9 DC932 3022066 WP BS 332 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FORWARD BAG PIT LEFT SIDEWALL SUPPORT AT STATION 332 IS CRACKE. MAINTENANCE FABRICATED AND INSTALLED SUPPORT REPAIR SEC TION. 2 L 7 2 4F A6WE 1999111100352 19991111 00352 NM 1999 11 11 DHL99740006 1 19991109 A 2781 40174 SWITCH BOEING 727 7272Q9 138448M NM NR 5 LE FLAP FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 740DH 21930 NR 5 LEADING EDGE FLAP WOULD NOT RETRACT AFTER TAKEOFF. AMBER LIGHT ON FED PANEL DID NOT EXTINGUISH NOR LIGHT ON S/O PA NEL. REMOVED AND REPLACED INDICATING SWITCH. OPS CHECKED SYSTEM PER MM 27-82-0. 2 L 7 3 4F RT A3WE 1999111900001 19991119 00001 NM 1999 11 19 TWAA9915301 1 19991109 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 721TW 29954 THE EXTERIOR EMERGENCY LIGHT AT THE NUMBER 2 CABIN DOOR, RT SIDE, WAS FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND BULB, NO HELP. DEFERRED CORRECTIONS PER MEL. ON ARRIVAL AT THE NEXT STATION THE LIGHT WAS FOUND OPERATIVE. 2 L 7 2 4F RT A2NM 1999111900002 19991119 00002 NM 1999 11 19 TWAA9915302 1 19991107 A 3350 757 BULB BOEING 767 767231 1385131 NM EXTERIOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 606TW 22569 AN EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE, RT SIDE OF THE AIRCRAFT AFT OF THE REAR CARGO DOOR. REPLACED THE LAM P. CHECK-C 9-10-99 LAX. 2 L 7 2 4F RT A1NM 1999111900003 19991119 00003 NM 1999 11 19 TWAA9915303 1 19991110 A 5754 SKIN BOEING 767 767205 1385121 NM NR 11 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, THE NUMBER 11 LE SLAT HAD DELAMINATION AT LOWER INBD SURFACE, 6 INCHES FROM THE TE. INSTALLED MET AL HOT BOND REPAIR PER SRM 51-70-10, PER BOEING SERVICE BULLETIN 767-57A0057 REV 2. 2 L 7 2 4F RT A1NM 1999111900004 19991119 00004 NM 1999 11 19 TWAA9915304 1 19991107 A 5754 SKIN BOEING 767 767205 1385121 NM NR 3 LE SLAT MISREPAIRED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, THE LEFT WING NUMBER 3 LE SLAT, TOP SIDE AT OTBD END, FOUND THE PATCH COVER HAD COME OFF OF THE ME TAL SURFACE. INSTALLED A 3.5 INCH IN BY 5.5 IN HOT BOND REPAIR PER BOEING SERVICE BULLETIN 767-57A0057 REV 2, AND SRM 5 1-70-10. 2 L 7 2 4F RT A1NM 1999111900005 19991119 00005 WP 1999 11 19 IXXA9900030 1 19991109 A 3230 CONTROL VALVE DOUG DC8 DC871F 302199D WP NLG OUT OF ADJUST A IXXA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 829BX 81727 218 45994 EN ROUTE FROM IAH TO DFW, DURING THE GEAR UPLATCH CHECK THE NOSE GEAR FAILED AND EXTENDED. THE FLIGHT CREW CYCLED THE G EAR TO PERFORM A SECOND CHECK WITH NO SUCCESS. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSP ECTED THE NOSE LANDING GEAR CONTROL SYSTEM WHICH REVEALED DISCREPANCIES. MAINTENANCE RIG THE NOSE LANDING CONTROL VALVE LINKAGE IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND PERFORMED A SUCCESSFUL GEAR SWING. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 1999111900006 19991119 00006 NE 1999 11 19 9904739139 2 19991105 A 7321 FUEL CONTROL DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 GL 01 948L 47049 657547 AS POWER WAS INCREASED FOR TAKEOFF AND WITH EPR INDICATION BELOW 1.2, THE LEFT ENGINE FLAMED OUT. THE EGT INDICATION FO R THE LEFT ENGINE DECREASED AND THE N1 AND N2 INDICATIONS DECREASED TO ZERO. TAKEOFF WAS ABORTED AT LESS THAN 20 KNOTS AIRSPEED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL PUMP AND FUEL CONTROL UNITS ON THE LEFT ENGINE. OPERATIONAL C HECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1999111900007 19991119 00007 NE 1999 11 19 9904745519 2 19991108 A 7320 COMPRESSOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A NWAA C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 GL 01 519US 23207 716337 DURING TAKEOFF, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND SHUTDOWN. TAKEOFF WAS ABORTED AT 120 KNOTS. MAINTEN ANCE FOUND THAT THE PMA, ROTOR, AND STATOR HAD FAILED. THE PMA WAS REPLACED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1999111900008 19991119 00008 WP 1999 11 19 9904759955 1 19991102 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMP FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999111900009 19991119 00009 WP 1999 11 19 9904769917 1 19991102 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY P ACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999111900010 19991119 00010 WP 1999 11 19 9904779949 1 19991103 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL COMP DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999111900011 19991119 00011 WP 1999 11 19 9904781151 1 19991108 A 2420 FEEDER LINS DOUG DC10 DC1040 3023508 WP NR 2 GENERATOR SHORTED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 151US 46760 AFTER TAKEOFF, LOST NR 2 GENERATOR. RESET AND VOLTS AND FREQUENCIES WERE NORMAL. FIVE MINUTES LATER, FLIGHT ATTENDANTS NOTED HAZY SMOKE IN AFT GALLEY AREA AND GENERATOR OFF LIGHT ILLUMINATED AGAIN. FLIGHT DIVERTED TO GEG AND LANDED WITHO UT INCIDENT. FOUND GENERATOR FEEDER LINES SHORTED TO ANTI-ICE SUPPORT FORWARD OF FUEL/OIL COOLER. REPLACED GENERATOR F EEDER LINES AND GCU. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A22WE 1999111900012 19991119 00012 WP 1999 11 19 9904799907 1 19991103 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY ESCAPE PATH LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BA TTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999111900013 19991119 00013 NM 1999 11 19 UPS99231069 1 19991108 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI LOWER FLANGE OF BS 600 FLOORBEAM CORRODED BL 0-RBL 25 WL 200 CORROSION CLEAN UP BEYOND ACCEPTABLE LIMITS. REMOVED AND REPLACED LOWER CHORD LBL 18 TO RBL 31 PER ER 99-6268 AND SRM 53-10-1. 2 L 7 3 4F A3WE 1999111900014 19991119 00014 NM 1999 11 19 UPS99231070 1 19990918 A 5320 65C232314 FORGING BOEING 727 72725C 138400H NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON BS 870 FRAME RBL 63. REMOVED AND REPLACED RT 870 BODY FORGING AFTER FINDING CRACKS AND CORROSION OUT OF LIMITS, WORK DONE IAW ER NR 99-6228. 2 L 7 3 4F A3WE 1999111900015 19991119 00015 NM 1999 11 19 UPS99231071 1 19990901 A 5320 BEAM BOEING 727 72725C 138400H NM BS 540-580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:SI CORROSION ON MCD BEAM BS 540-580 LBL 65 WL 208. REMOVED AND REPLACED MCD BEAM IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1999111900016 19991119 00016 NM 1999 11 19 UPS99231072 1 19991109 A 5720 65216406 BRACKET BOEING 727 72727C 138400J NM WS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE:C RT WING AFT SPAR AT WS 380.0 THE NR 6 T/E FLAP JACKSCREW OUTBOARD ATTACH BRACKET HAS CORROSION ON LOWE R ATTACH POINT. REMOVED AND REPLACED BRACKET IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1999111900017 19991119 00017 NM 1999 11 19 UPS99231073 1 19991109 A 5320 FRAME BOEING 727 72727C 138400J NM EMER EXIT DRWAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE:C C/W PERMANENT REPAIR TO OVERWING EXIT FRAMES 783.95 RIGHT, 825.95 LEFT, 825.95 RIGHT, AND 848.95 RIGHT . INSTALLED PERMANENT REPAIRS TO OVERWING EXIT FRAMES BS783.95 RIGHT, 825.95 LEFT, 848.95 RIGHT AS PER UPS E0 B727-5310 -12010-A. 2 L 7 3 4F A3WE 1999111900018 19991119 00018 NM 1999 11 19 UPS99231074 1 19991109 A 5312 BLKHD STIFFENER BOEING 727 72727C 138400J NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE:C AFT CARGO COMPARTMENT, BS1183 BULKHEAD, VERTICAL STIFFENER, RBL 8 HAS CRACK INDICATION, TOP OF STRINGE R, OUTBOARD SIDE OF STIFFENER. HFEC INSPECTED AND VERIFIED CRACK INDICATION AT TOP OF STIFFENER RBL 8, BS 1183, LENGTH 1.25 INCH IAW NDT MANUAL PART 6, 51-00-00, FIG 4. REMOVED AND REPLACED VERTICAL STIFFENER RBL 8 AT AFT CARGO COMT BULKH EAD IAW BOEING TELEX UPS-MIA-99-0000214 AVITAS ENGINEERING RO 99AVHM.077RO-1 AND UPS E.O.727-53-2201. 2 L 7 3 4F A3WE 1999111900019 19991119 00019 NM 1999 11 19 UPS99231075 1 19991109 A 5730 SKIN BOEING 727 72727C 138400J NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE:C LEFT WING OUTBOARD FLAP-FOREFLAP LEADING EDGE SKIN CRACKED AT RIVET HEAD (NR 2 FOREFLAP CARRIAGE). PE RFORMED HFEC INSP OF CRACK AT L/W O/B FOREFLAP IAW NDT MANUAL PART 6, 51-00-00, FIG 4. VERIFIED CRACK EXTENDS FROM RIVE T HOLE TO SKIN EDGE. NO STOP DRILL REQUIRED. INSTALLED DOUBLER REPAIR AS PER B727 S RM 57-50-4 FIG 7. MATERIAL USED, 2024-T3, 0.063, 5 BY 8. 2 L 7 3 4F A3WE 1999111900020 19991119 00020 NM 1999 11 19 UPS99231076 1 19991109 A 5320 PRESSURE WEB BOEING 727 72727C 138400J NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE:C NOSE WHELL WELL CEILING PRESSURE WEB CRACKED AT BS277, WL194. CRACKS VERIFIED PER NDT PART 6, 51-00-0 0, HFEC. STOP DRILLED CRACKS ON CEILING PRESSURE WEB AT STA 277, WL 194. CRACKS END AT STOP DRILL. REMOVED AND REPLAC ED DAMAGED SECTION OF NOSE W/W CEILING PRESSURE WEB AS PER B727 SRM 53-10-2, FIG 2. MATERIAL USED 2024-T3, 0.040, 12 BY 12. 2 L 7 3 4F A3WE 1999111900021 19991119 00021 NM 1999 11 19 UPS99231077 1 19991109 A 5320 PRESSURE WEB BOEING 727 72727C 138400J NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE:C NOSE WHEEL WELL LEFT SIDEWALL PRESSURE WEB CRACKED AT BS259.5, WL190 (TWO INCHES BELOW CEILING). CRAC K VERIFIED PER NDT PART 6, 51-00-00 HFEC. STOP DRILLED CRACKS ON SIDEWALL PRESSURE WEB. CUT-OUT DAMAGED AREA AT NOSE WHEEL WELL LEFT SIDE WALL BS 259.5, WL190. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 FIG 1. MATERIAL USED 7075 -T6, 0.040, 6 BY 4.5. 2 L 7 3 4F A3WE 1999111900022 19991119 00022 NM 1999 11 19 UPS99231078 1 19991109 A 5320 PRESSURE WEB BOEING 727 72727C 138400J NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE:C NOSE WHEEL WELL RIGHT SIDEWALL PRESSURE WEB CRACKED AT BS235.8, WL17 0. (JUST BELOW PRESSURE PANEL) CR ACK VERIFIED PER NDT PART 6, 51-00-00 HFEC. STOP DRILLED CRACKS. T RIMMED OUT DAMAGED AREA. INSTALLED REPAIR ON RIGHT PRESSURE WEB BS23 5.8, WL170 IAW B727 SRM 51-40-2 FIG 1 MATERIAL USED 2024-T3, 0.050, 16 BY 9. 2 L 7 3 4F A3WE 1999111900023 19991119 00023 NM 1999 11 19 UPS99431068 1 19991109 A 2611 SMOKE DETECTOR BOEING 747 747121 1384871 NM CARGO COMPT INOP A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 691UP 19641 INTERMITTENT ZONE 5 MAIN CARGO DECK FIRE LIGHT ILLUMINATED DURING CLIMB-OUT OF PHL. DEFERRED PER MEL 26-11. REMOVED AN D REPLACED B SMOKE DETECTOR AND A8 SMOKE DETECTOR CARD. OP'S CHECK GOOD PER MM 26-10-00. POSITIONS 14 TO 15A VOID. RE FERENCE LOG PAGE 148290 ITEM 3 FOR OVERWEIGHT LANDING WHICH OCCURED DURING LANDING. 2 L 7 4 4F A20WE 1999111900024 19991119 00024 WP 1999 11 19 ABXA9900766 1 19991108 A 5230 59101413 SKIN DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND OUTER SKIN OF FORWARD LOWER CARGO DOOR CRACKED. REPAIRED CRACK IAW DC9 SRM 52-05. 2 L 7 2 4F A6WE 1999111900025 19991119 00025 WP 1999 11 19 ABXA9900767 1 19991108 A 5543 5910257503 TAB DOUG DOUG DC9 DC941 302207N WP RUDDER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND RUDDER TAB DELAMINATED. REPLACED RUDDER TAB IAW DC9 MM 27-20-2. 2 L 7 2 4F A6WE 1999111900026 19991119 00026 WP 1999 11 19 ABXA9900768 1 19991022 A 5320 59220791 SUPPORT DOUG DOUG DC9 DC932F 3022067 WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND RIGHT FLOOR SUPPORT STRUT CRACKED AT STATION 237. REPLACED STRUT IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999111900027 19991119 00027 WP 1999 11 19 ABXA9900769 1 19991022 A 5320 39141371 BRACKET DOUG DOUG DC9 DC932F 3022067 WP BS 756 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT SIDEWALL WINDOW STIFFENER BRACKET CRACKED AT STATION 756. REPLACED BRACKET IAW DC9 SRM 51-30 -5 AND DACO DWG 39141371. 2 L 7 2 4F A6WE 1999111900028 19991119 00028 WP 1999 11 19 ABXA9900770 1 19991108 A 5730 56429401 SKIN DOUG DOUG DC8 DC862 3021970 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 DURING C-CHECK, FOUND CRACK INDICATIONS IN LEFT WING UPPER AFT SKIN PANEL 505F. REPAIRED IAW ABX REA D857-33611MR. 2 L 7 4 4F 4A25 1999111900029 19991119 00029 WP 1999 11 19 DLL10992431 1 19991103 A 7603 THROTTLE 359360113 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE WORN A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 720DA 193C1136 010427 WHILE IN CRUISE NR 2 ENGINE POWER DECREASED AS THROTTLE WAS IN STATIONARY POSITION DURING APPROACH AT FL 100 THROTTLE WA S RETURNED TO IDLE STOP, BUT FUEL FLOW REMAINED AT 5000 LBS AND N2 WAS AT 79 PERCENT ENGINE WAS SHUT DOWN. FOUND THROT TLE RACK AND TELEX DOVETAIL WORN. REPLACED BOTH. 2 L 7 3 4F 4 F A23WE E12EU 1999111900030 19991119 00030 NM 1999 11 19 DL72W992432 1 19991103 A 2782 BRACKET BOEING 727 727247 138408F NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 INBD ATTACH BRACKET CRACKED NR 1 SLAT ACTUATOR BRKT. INSTALLED DOUBLER PER M/M 57-20-21. TPA F-1 LETTER CHECK. 2 L 7 3 4F A3WE 1999111900031 19991119 00031 NM 1999 11 19 DLM88992433 1 19991104 A 5330 5924802 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 920DL 49644 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 237 AND STRINGER 17L. THE DAMAGE WAS REPAIRED PER ERA 333751-14 AT HMV. 2 L 7 2 4F RT A6WE 1999111900032 19991119 00032 WP 1999 11 19 DLL14992434 1 19991103 A 5330 1503542107 SKIN LKHEED 1011 1011385115 5265015 WP BS 1615 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 FUSELAGE SKIN FS 1605-1625 STRINGER 33-35 HAS CORROSION REPAIR. THE FUSELAGE SKIN BETWEEN FS 1605 AND 1625 AND BETWEEN STRINGERS 33 (BL0) AND 35 WAS FOUND WITH AN AREA OF CORROSION UNDER AN EXISTING TEAR STRAP. THE CORROSION WAS CUTOUT OF THE SKIN WITH AN 8.25 BY 7.75 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 3 68651-14, REV A. 2 L 7 3 4F A23WE 1999111900033 19991119 00033 NM 1999 11 19 DL757992435 1 19991103 A 5315 146N51116 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 FUSELAGE FLOORBEAM FS 1681 UPPER CAP, HAS CORROSION REPAIR. THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION ALONG ITS LENGTH. THE ENTIRE UPPER CAP FLANGE WAS TRIMMED OFF TO REMOVE ALL OF THE CORROSION. A NEW SECTION OF UPPER CAP WAS FABRICATED FROM THE SAME EXTRUSION AS THE ORIGNAL BEAM AND INSTALLED PER ER/ A 368560-14, REV B. 2 L 7 2 4F RT A2NM 1999111900034 19991119 00034 NM 1999 11 19 DL76L992436 1 19991104 A 5270 DOOR WARNING BOEING 767 767332 1382001 NM RT EMER EXIT ACTIVATED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 196DN 28453 ATB FIRST FLIGHT DELAY, RT FWD EMERGENCY DOOR MSG CAME ON DURING CLIMB, WENT OUT ON ROLLOUT. FWD TO MCO. 2 L 7 2 4F RT A1NM 1999111900035 19991119 00035 NM 1999 11 19 DL757992437 1 19991104 A 2131 CONTROLLER BOEING 757 757232 1384965 NM CABIN MALFUNCTIONED A DALA G O2 MASK DEPLOYED G MULTIPLE FAILURE CR CRUISE 1 SO 27 618DL 22908 CABIN ALT MASTER WARNINGS ACTIVATED WHILE AT CRZ FL350. CREW REPORTS CABIN ALT CONTINUED TO CLIMB PAST 12K SO O2 MASKS DEPLOYED MANUALLY. SYSTEM SWITCHED TO MANUAL MODE AND OUTFLW VLV WENT TO FULL CLOSED AS COMMANDED DURING EMERGENCY DESC ENT INTO TYS. CREW REPORTED ATTEMPTS TO RETURN SYS TO AUTO MODE WERE UNSUCCESSFUL, BUT SHIP DID PRESS IN MANUAL MODE AN D CABIN ALT RETURNED TO NORMAL. FOUND CABIN PRESS CONTROLLER FAULTING A/C MOTOR ON AFT CABIN OUTFLOW VALVE. REPLACED S AME. AS PRECAUTION, REPLACED BOTH CABIN PRESS. CONTROL MODULES AND ALT CONTROL PANEL, PRESS OP CKS NORMAL. 2 L 7 2 4F RT A2NM 1999111900036 19991119 00036 NM 1999 11 19 DL72W992438 1 19991104 A 5320 FRAME BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 FOUND AT B-2 LETTER CK, AFT ENTRY DOOR LT CUTOUT FRAME CRACKED AT UPPER STOP FITTING STIFFENER. REPAIRED PER SRM 53-10- 9. 2 L 7 3 4F A3WE 1999111900037 19991119 00037 NM 1999 11 19 DL72W992440 1 19991104 A 5320 WEB BOEING 727 727247 138408F NM BS 1305 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 REF SHIP 569 TPA LTR CHK B-2 11-04-99, .5 INCH CRACK AT UPPER ROW OF RIVETS LT TORQUE BOX, VERT WEB STA 1305. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999111900038 19991119 00038 NM 1999 11 19 DL72W992441 1 19991104 A 5320 WEB BOEING 727 727247 138408F NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 REF SHIP 569 TPA LTR CHK B-2 11/04/99, .5 INCH CRACK AT LEFT TORQUE BOX VERT WEB LOWER LIGHTNING HOLE STA 1233. REP AIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999111900039 19991119 00039 NM 1999 11 19 DL76S992442 1 19991104 A 3350 LIGHT BPS73 BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 124DE 7651 23438 FOUR AISLE EMERGENCY LIGHTS INOP AFT RIGHT SIDE. REPLACED POWER SUPPLY, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999111900040 19991119 00040 1999 11 19 DLM11992443 4 19991104 A 3417 CADA 4059060901 DOUG MD11 MD11 3023602 NM NR 2 MALFUNCTION A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 803DE 92120522 48474 DURING CLIMB-OUT CADC2 SHOWED PLUS 100 KTS WITH OVERSPEED WARNING. REPLACED NR 2 CADC. OP CKS NORMAL. 2 L 7 3 4F RT A22WE 1999111900041 19991119 00041 NM 1999 11 19 DL72S992444 1 19991105 A 2150 VALVE 39608831 BOEING 727 727232 1384082 NM RT PACK FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 401DA P1233 21145 AFTER NR 3 ENG START AND RT PACK SELECTED ON, LOUD BANG WAS HEARD IN COCKPIT/CABIN. RT DUCT PRESS NEEDLE WENT TO ZERO A ND AFT FLT ATTENDANTS REPORTED FUEL SMELL. INSPECTED DUCTS AT NR 3 ENG/PYLON/AFT AIRSTAIR FOR DAMAGE/LEAKAGE, CK GOOD. CHECKED DUCTS AT RT PACK BAY CK OK. RAN NR 3 ENG AND RAN RT PACK OPS CK NML. REPLACED RT AFT PACK VLV PRECAUTIONARY. S YSTEM CK NORMAL. 2 L 7 3 4F A3WE 1999111900042 19991119 00042 NM 1999 11 19 DL757992445 1 19991105 A 2530 OVEN 831620403MO BOEING 757 757232 1384965 NM GALLEY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 6700 0214 30337 ELECTRICAL ODOR IN FIRST CLASS GALLEY. ELECTRICAL POWER REMOVED. FOUND ODOR TO BE COMING FROM F/C GALLEY AFT OVEN. TI MER CONTROL PANEL HOT TO TOUCH FORTY FIVE MIN AFTER POWER. REMOVED AND REPLACED OVEN, RAN NEW ONE ODOR GONE OVEN C KS GOOD. 2 L 7 2 4F RT A2NM 1999111900043 19991119 00043 NM 1999 11 19 DL72S992446 1 19991105 A 3231 MECHANISM 69295281 BOEING 727 727232 1384082 NM NLG DOOR FAILED A DALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 535DA 22048 LOUD BANG DURING INITIAL GEAR RETRACTION ON T/O FROM SJC. FOLLOWED BY EXCESSIVE VIBS. RED GEAR DOOR LIGHT ILLUMINATED. ON FRONT PNL AS WELL AS AMBER NOSE GEAR LIGHT ON S/O PNL. GEAR EXTENDED NORMALLY. PER EMERGENCY CK-OUT. UPON ARR IN TO SFO, MAINTENANCE FOUND FWD NOSE GEAR DOOR CONTROL ROD END SEPERATED FROM CONTROL ROD ASSY. REMOVED AND REPLACED CO NTROL ROD ASSY. OPS CK OK. 2 L 7 3 4F A3WE 1999111900044 19991119 00044 NM 1999 11 19 DL72S992447 1 19991105 A 3350 LIGHT 900542 BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 409DA 1210 21153 FWD CABIN OVERHEAD EMERGENCY LIGHT INOP. ON LAYOVER CK. REPLACED RACK. 2 L 7 3 4F A3WE 1999111900045 19991119 00045 NM 1999 11 19 DL72S992448 1 19991106 A 3350 334701744 BATTERY 900542 BOEING 727 727225A 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 8873Z 6591 21291 DURING STBY PWR CK, THE EMERGENCY EXIT LIGHTS OVER THE RT WING EXIT DOORS FLASHED ON/OFF CONTINUOSLY. REPLACED RACK AND BATTERY ASSY M1086 NOW CKS OK. 2 L 7 3 4F RT A3WE 1999111900046 19991119 00046 NM 1999 11 19 DL72S992449 1 19991106 A 2612 FIRE DETECTOR BOEING 727 727232 1384082 NM APU MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 494DA 40626 21074 0 APU FIRE WARNING WITH LIGHT AND BELL AT 100 KNOTS. REJECTEDTAKEOFF. STOPPED ACFT USING MODERATE, EVEN BRAKING. 16 DEG COAT 168,000 LBS. INSPECTED ACFT PER MM 05-52-121. NO DISCREPANCIES NOTED. FWD FIRE WARNING TO MCO PER MEL 26-00 -01B. PULLED AND COLLARED APU FIRE DETECTOR CB. NEEDS LOOP ASSY. 2 L 7 3 4F A3WE 1999111900047 19991119 00047 NM 1999 11 19 DL757992450 1 19991106 A 2740 TRIM 285T0015117 BOEING 757 757232 1384965 NM HORIZ STAB MALFUNCTIONED A DALA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 27 693DL D00133 29725 DISCONTINUED TAKEOFF AT 90K. RED STABILIZER WARNING MESSAGE APPEARED ON T/O. AT PWR APPLICATION TRIM WAS 4.1 AT 90K TR IM WAS DRIVING UNCOMMANDED THROUGH 6.5 NOSE UP TO A FINAL OF 8.0 UNITS. FOUND RT SAM MODULE FAULTED, REPLACED SAME. 2 L 7 2 4F RT A2NM 1999111900048 19991119 00048 NM 1999 11 19 DL72W992456 1 19991107 A 3350 LIGHT 900542 BOEING 727 727247 138408F NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2810W 4618 20648 FC AISLE EMERGENCY LIGHTS AFT OF LIFE RAFT COMPARTMENT INOP. REPLACED CHARGING RACK. 2 L 7 3 4F A3WE 1999111900049 19991119 00049 NM 1999 11 19 DLM88992457 1 19991108 A 5711 9930514501 SPAR CAP DOUG MD88 MD88 3023688 NM LT/RT WING OVERSIZED HOLES A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DL 49573 DURING INSTALLATION OF THE UPPER SURFACE HEATER BLANKETS FOR THE LEFT AND RIGHT WING THE HOLES COMMON TO THE UPPER CAP O F THE FRONT SPAR WERE NOT COLD WORKED. ERA 333738-14 ADDRESSED THE DISCREPANCY. 2 L 7 2 4F RT A6WE 1999111900050 19991119 00050 NM 1999 11 19 DLM88992458 1 19991108 A 5330 5924802 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 920DL 49644 A DENT WAS FOUND AT FS 237 AT LONGERON 17L. THE DAMAGE WAS REPAIRED PER ERA 333751-14 AT HMV. 2 L 7 2 4F RT A6WE 1999111900051 19991119 00051 NM 1999 11 19 DL72S992462 1 19991025 A 2497 BMS1331 WIRE BOEING 727 727232 1384082 NM NR 1 ENGINE SPLIT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 0 ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACE D CABLES FROM SPLICES IN LT 48SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SER- VICE LETTER 727-SL-24-026-A. 2 L 7 3 4F A3WE 1999111900052 19991119 00052 NM 1999 11 19 DLM11992463 1 19991108 A 2560 MEGAPHONE MV10 DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA K NONE O OTHER CR CRUISE 1 SO 27 814DE 9200995 48769 MEGAPHONE HAS CONTINOUS FEEDBACK. USED IN FLT DUE TO PA, FAILURE. REPLACED SAME. 2 L 7 3 4F RT A22WE 1999111900053 19991119 00053 NM 1999 11 19 DL72S992464 1 19991101 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 FOUND DURING D1 LETTER CHECK/SHUTTLE MOD NRC 69, NR 3 L/E SLAT SPAR STIFFENER CRACKED APPROX 1.5 INCH AT INBD TRACK OUTB D STIFFENER. REPLACED SPAR STIFFENER PER M/M 57-20-21 P 813. 2 L 7 3 4F A3WE 1999111900054 19991119 00054 NM 1999 11 19 DL757992466 1 19991108 A 2121 6457053 FAN 6457053 BOEING 757 757232 1384965 NM CARGO COMPT INOP A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 660DL 109567 24422 FLT ATTN REPORT RUBBER SMELL IN AFT CABIN ALONG WITH SMOKEY HAZE. PERFORM SMOKE IDENT AND REMOVAL CHECK LIST. SMOKE CL EARED. AFTER RE-ENERGIZING LT RECIR FAN LT RECIR FAN EICAS MSG CAME ON AND OFF SEVERAL TIMES FINALLY CAME ON AND STAYED ON. REPLACED LT RECIR FAN AND RESET 20 AMP C/B. OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1999111900055 19991119 00055 NM 1999 11 19 DL76G992468 1 19991109 A 2530 OVEN 828450407M0 BOEING 767 767324 NM GALLEY MALFUNCTIONED A DALA K NONE M OVER TEMP CR CRUISE 1 SO 27 394DL 728 27394 GALLEY MID CABIN CENTER OVEN OVERHEATS, TOP WILL NOT SHUT OFF. REPLACED OVEN, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1999111900056 19991119 00056 NM 1999 11 19 DL72S992469 1 19990426 A 5753 ANGLE BOEING 727 727225A 1384077 NM LT TE MID FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 47 FROM THE IB END OF THE MIDFLAP. THE ANGLE WAS RE PAIRED PER 727 MM 57-52-0, FIG 802. 2 L 7 3 4F RT A3WE 1999111900057 19991119 00057 NM 1999 11 19 DL72S992470 1 19990426 A 5753 ANGLE BOEING 727 727225A 1384077 NM LT TE MID FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 32 FROM THE IB END OF THE MIDFLAP. THE ANGLE WAS RE PAIRED PER 727 MM 57-52-0, FIG 802. 2 L 7 3 4F RT A3WE 1999111900058 19991119 00058 NM 1999 11 19 DL72S992471 1 19990426 A 5753 SKIN BOEING 727 727225A 1384077 NM LT TE MID FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND DENTED AND WORN 20 FROM OB END OF FLAP. THE SKIN WAS REPAIRED PER MM 57 -52-0, FIG 809. 2 L 7 3 4F RT A3WE 1999111900059 19991119 00059 NM 1999 11 19 DL75A992473 1 19991109 A 2120 AIR DIST BOEING 757 757212 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 751AT 23125 DIVERT TO DFW DUE TO FUMES IN CABIN NEAR MID GALLEY FUMES. RESEMBLED TURPENTINE/SOLVENT. INSPECTED LEFT AND RIGHT AC B AY FOR LEAKS. ALL CHECKS OK. INSPECTED FWD BAG BIN. BAG BIN CHECKS OK. INSPECTED PASSENGER CABIN ON ARRIVAL. NO FUM ES NOTED. RAN NR 1 AND NR 2 ENG W/2 PACKS. STILL NO FUMES. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 1999111900060 19991119 00060 NM 1999 11 19 DL72S992476 1 19990719 A 5753 SPAR BOEING 727 727232 1384082 NM RT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 AFT SPAR LWR CAP ANGLE, CRACKED 19 FROM INBD END. REPAIRED PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999111900061 19991119 00061 NM 1999 11 19 DL72S992477 1 19990811 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 HOLE IN COVE SKIN, 24 FROM I/B FROM I/B END OF FLAP, REPAIRED PER MM 57-52-0 FIG 809. 2 L 7 3 4F A3WE 1999111900062 19991119 00062 NM 1999 11 19 DL72S992490 1 19991110 A 5330 SKIN BOEING 727 727232 1384082 NM BS 384 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 4 INCH CRACK IN FUSELAGE SKIN AT FS 384 2 .5 INCH ABOVE STR 25R AND .25 INCH CRACK IN FUSE SKIN 2 INCH AFT OF ABOVE CRAC K. REPAIR PER SRM 53-30-3 TIME LIMITED. 2 L 7 3 4F A3WE 1999111900063 19991119 00063 NM 1999 11 19 DL72S992492 1 19991110 A 3350 LIGHT 900835A BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 493DA T3913 21062 LT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 1999111900064 19991119 00064 NM 1999 11 19 SCNA99135 1 19991108 A 3350 900835A BATTERY PACK 900542 BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC UA4721 20764 DURING A LINE MAINTENANCE CHECK, THE CENTER AISLE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE CENTER AISLE OVERWING EMERGENCY EXIT SIGN BATTERY PACK. OPERATIONALLY CHECKS GOOD PER MM 335022. 2 L 7 3 4F RT A3WE 1999111900065 19991119 00065 1999 11 19 RAIA9911012 4 19991109 A 2350 B692246 AUDIO PANEL BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 430AM 880 7478 - STL - F/O'S COCKPIT COMM SYSTEM POPPING C/B. MAINTENANCE REPLACED F/O'S AUDIO PANEL. 2 L 7 2 4T RT A56EU 1999111900163 19991119 00163 SW 1999 11 19 CA991007073 1 19990929 A 3040 140132100 MOTOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE WINDSHIELD WIPER OVERHEATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA P44663 881750 (CAN) AFTER TAKEOFF, THE CREW SMELLED SMOKE/BURNING SMELL. AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE INVEST IGATED AND FOUND THE WIPER MOTOR TOO HOT TO TOUCH. CREW REPORTED THAT ON THE PREVIOUS FLIGHT, THE WIPER SYSTEM CAME ON, THEN WENT OFF. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999111900164 19991119 00164 EU 1999 11 19 CA991007074 1 19991001 A 2910 HTE400005 VALVE BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL HYDRAULIC SYSTEM CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA P63311C DRG658087 (CAN) ON APPROACH, FLAPS WERE SELECTED AND THE CREW NOTICED HYDRAULIC PRESSURE AT ZERO PSI. EMERGENCY GEAR EXTENSION WA S CARRIED OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE INVESTIGATED AND FOUND FLUID IN BELLY POD AREA AND DETERMINED IT TO BE COMING FROM THE NR 2 NON-RETURN VALVE IN THE HYDRAULIC PUMP OUTLET CIRCUIT. 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C P61GL 1999111900165 19991119 00165 CE 1999 11 19 CA991007079 1 19990922 A 7800 MS21042L08 NUT ED8100 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE MCAULY 3AF34C 3GFR34C703 GL EXHAUST DISINTEGRATED W K NONE O OTHER IN INSP/MAINT 1 CA PCE19192 921619 (CAN) DURING INSPECTION OF EXHAUST DEFLECTOR INSTALLATION, THE NUTS ON THE RETAINER SCREWS WERE FOUND TO BE MISSING. N UTS SUPPLIED ARE NOT CORROSION RESISTANT AND HAD DISINTEGRATED. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 1999111900166 19991119 00166 CE 1999 11 19 CA991007083 1 19990929 A 7800 MS21042L08 NUT ED8100 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL EXHAUST DISINTEGRATED W K NONE O OTHER IN INSP/MAINT 1 CA PCEPC0486 970516 (CAN) DURING INSPECTION OF EXHAUST DEFLECTOR INSTALLATION, THE NUTS ON THE RETAINER SCREWS WERE FOUND TO BE MISSING. NU TS SUPPLIED ARE NOT CORROSION RESISTANT AND HAD DISINTEGRATED. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 1999111900167 19991119 00167 CE 1999 11 19 CA991007086 1 19990918 A 5330 24130003 SKIN CESSNA 172 172RG 2072438 CE LYC O360 O360F1A6 41514 EA MCAULY 2D34C B2D34C220 GL FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9954 L2417536A 807375 (CAN) DURING SCHEDULED MAINTENANCE, A CRACK WAS FOUND RUNNING HORIZONTALLY BEHIND THE FUELING STEP ON BOTH SIDES OF AIRC RAFT. 1 H 7 1 3O 3 O 3A17 E286 5 C P7EA 1999111900168 19991119 00168 EU 1999 11 19 CA991007093 1 19990930 A 2133 326C321 OUTFLOW VALVE AVIAC AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE7312 01518 WP FUSELAGE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 238 257 P73114C (CAN) AIRCRAFT FAILED TO PRESSURIZE, AIR CONDITIONING VALVE FAILED CLOSED. 2 L 7 2 4F 4 F A33EU E6WE 1999111900169 19991119 00169 EU 1999 11 19 CA991027002 1 19991005 A 5270 SWITCH AIRBUS 310 A310304 EU PASSENGER DOOR OUT OF ADJUST W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) CLIMBING THROUGH FL 280, NR 1 RT CABIN DOOR NOT CLOSED WARNING ILLUMINATED. DOOR SWITCHES ADJUSTED AND TESTED PE R AMM 52. NO FURTHER FAULT REPORTED. 2 L 7 2 4F RT A35EU 1999111900170 19991119 00170 EA 1999 11 19 CA991027011 1 19991007 A 6123 V319 SWITCH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE AUTOFEATHER FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 123110 870626 (CAN) DURING LINE CHECK, IT WAS DISCOVERED THAT NR 2 AUTOFEATHER SYSTEM MICROSWITCH WOULD NOT TEST. SWITCH REPLACED, SY STEM SERVICED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900171 19991119 00171 EA 1999 11 19 CA991027012 1 19991008 A 2710 82700565S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE WS 178 DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 123110 870626 (CAN) WHILE C/W SB 8-27-78, THE INBOARD UPPER LEFT AILERON CABLE WAS FOUND BLENDED BETWEEN PULLEYS AT STATION Y178. CAB LE REPLACED. SUBMITTER STATED NOT KNOWN IF ORIGINAL EQUIPMENT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900172 19991119 00172 NM 1999 11 19 CA991027013 1 19990930 A 5260 85210276101 BUSHING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AIRSTAIR WORN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 120648 881221 (CAN) AIRSTAIR WAS JAMMED. FORWARD HANDLE HAD WORN BUSHING THAT CAUSED RAIL TO FOUL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900173 19991119 00173 NM 1999 11 19 CA991027014 1 19991015 A 3010 153212A VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE SYSTEM STUCK W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 23679 RF3901 120648 881221 (CAN) DURING DE-ICE SYSTEM CHECK, RIGHT NR 4 BOOT WOULD NOT DEFLATE. DISTRIBUTOR VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900174 19991119 00174 EU 1999 11 19 CA991027015 1 19991001 A 5610 NF20216401 WINDSCREEN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT DELAMINATED W O OTHER O OTHER NR NOT REPORTED 1 CA 828 L277027 LF05464A (CAN) LARGE AREA OF CAPTAIN'S B-WINDOW DELAMINATED. WINDSCREEN REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999111900175 19991119 00175 EU 1999 11 19 CA991027016 1 19991019 A 5250 460248 SPRING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT DOOR BROKEN W O OTHER O OTHER NR NOT REPORTED 1 CA LF05464A (CAN) FLIGHT DECK DOOR REPORTED TO BE BINDING NEAR THE TOP. INVESTIGATION REVEALED A BROKEN DOOR SPIGOT SPRING. 2 H 7 4 4F 4 F RT A49EU E6NE 1999111900176 19991119 00176 NM 1999 11 19 CA991027017 1 19990930 A 7600 87600514001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 120083 901134 (CAN) DURING INSPECTION, NR 1 ENGINE CONTROL CABLE WAS FOUND WORN TO LIMITS IN AREA OF STEEL FIREWALL PULLEY. CABLE REP LACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900177 19991119 00177 NM 1999 11 19 CA991027018 1 19991015 A 2435 23088002B STARTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE STARTER/GEN FAILED W E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CA 5821 931 319 120083 901134 (CAN) NR 2 STARTER HAD TO BE DE-ELECTED MANUALLY. GCU REPLACED FOR TROUBLESHOOTING WITH NO RESULTS AND THEN STARTER REP LACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900178 19991119 00178 NM 1999 11 19 CA991027022 1 19991008 A 3010 8SC0029011 DEICE BOOT 85510203003 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HORIZONTAL STAB SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 9155 CAP241 120854 890709 (CAN) DURING ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT OUTBOARD DEICE BOOT ON THE HORIZONTAL STABILIZER WAS SE PARATING FROM THE LEADING EDGE. LEADING EDGE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900179 19991119 00179 NM 1999 11 19 CA991027023 1 19991005 A 3242 68728 SEAL BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 BRAKE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 442 0667 121165 891129 (CAN) NR 1 BRAKE FOUND LEAKING AT ACTUATOR PISTON. OPERATOR AWARE OF THIS PROBLEM WITH BRAKE AND IS ONLY OPERATOR USIN G THIS P/N. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900180 19991119 00180 NM 1999 11 19 CA991027024 1 19991005 A 3242 68728 SEAL BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 BRAKE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 896 1879 121165 891129 (CAN) NR 2 BRAKE FOUND LEAKING. ONLY OPERATOR USING THIS P/N BRAKE AND IS AWARE OF PROBLEMS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900181 19991119 00181 EA 1999 11 19 CA991027025 1 19991005 A 2761 82950010175 ACTUATOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE SPOILER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123133 920528 (CAN) HYDRAULIC LEAK WAS DISCOVERED IN THE AREA OF THE LEFT OUTBOARD ROLL SPOILER ACTUATOR. LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900182 19991119 00182 EA 1999 11 19 CA991027026 1 19991007 A 3350 6104791 POWER SUPPLY DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CABIN FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 10223 123132 901056 (CAN) ROUTINE INSPECTION FOUND TWO EMERGENCY FLOOR TRACK LIGHTS OUT. POWER SUPPLY BASE 3352-PS2 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900183 19991119 00183 NM 1999 11 19 CA991027027 1 19991010 A 2435 AJA4N CONTACTOR DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE STARTER/GEN MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS O OTHER IN INSP/MAINT 1 CA 123124 901161 (CAN) WHEN MAINTENANCE APPLIED GROUND POWER TO THE AIRCRAFT, THE NR 2 ENGINE BEGAN TO ROTATE. STARTER CONTACTOR 2431-K2 WAS REPLACED AS WELL AS STARTER/GENERATOR WHICH HAD EXCEEDED DUTY LIMITS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900184 19991119 00184 NM 1999 11 19 CA991027028 1 19991016 A 7602 87600518003 CABLE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 1 ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 123124 901161 (CAN) DURING INSPECTION, NR 1 ENGINE LOWER CONDITION LEVER CABLE WAS BLENDED TO LIMITS AT THE STEEL PULLEY FORWARD OF TH E FIREWALL. CABLE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900185 19991119 00185 EA 1999 11 19 CA991027029 1 19991016 A 3010 8SC0029028 DEICE BOOT 85720062006 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE RT WING SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 451 0060030 123116 900837 (CAN) CREW REPORTED THE RIGHT INBOARD L/E DEICE BOOT AS BEING DEFORMED. MAINTENANCE REVEALED WHEN INFLATED, THE BOOT HA D SEPARATED INTERNALLY ALONG STITCHING BETWEEN INFLATION TUBES. INFLATED AS A BUBBLE IN ONE AREA. LEADING EDGE WAS REP LACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900186 19991119 00186 NM 1999 11 19 CA991027030 1 19991018 A 3240 DSC252A40230 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 3 BRAKE LEAKING W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 120152 891130 (CAN) RIGHT BRAKE LINE BLEW OFF AS BRAKES WERE BEING APPLIED WHEN PARKING. LINE FAILED AT THE BRAKE UNIT END WHERE THE BRAIDED LINE ENTERS THE FITTING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900187 19991119 00187 NM 1999 11 19 CA991027031 1 19991018 A 3350 6104781 POWER SUPPLY GRIMES DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 5169 26 1414 120152 891130 (CAN) DURING INSPECTION, IT WAS NOTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. POWER SUPPLY REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900188 19991119 00188 EU 1999 11 19 CA991027032 1 19991013 A 3230 HTE210014 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG INTERMITTENT W O OTHER O OTHER AP APPROACH 1 CA 286GB136H LF05542A (CAN) ON EXTEND, SELECTION GEAR MOVEMENT DELAYED SIX SECONDS. GEAR SWINGS CONFIRMED FAULT AND LED TO REPLACEMENT OF LAN DING GEAR SELECTOR VALVE ACTUATOR. 2 H 7 4 4F 4 F RT A49EU E6NE 1999111900189 19991119 00189 SW 1999 11 19 CA991027033 1 19990929 A 6730 212076004003 SERVO BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA TAIL ROTOR LEAKING W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA 940 941 CPPS61861 (CAN) NR 1 HYDRAULIC SYSTEM GRADUALLY LOST PRESSURE, WARNING LIGHT CAME ON AND NR 1 SYSTEM WAS SHUT DOWN. POST-LANDING CHECK REVEALED HYDRAULIC FLUID LEAKING FROM T/R SERVO ACTUATOR. 1 G 7 1 4U 4 U H4SW E22EA 1999111900191 19991119 00191 SW 1999 11 19 CA991027035 1 19990930 A 5302 K934400002 SKIN KAMAN KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5499 LE81008 (CAN) CIRCUMFERENTIAL CRACK ON FIRST PANEL AFT OF MOUNTING BRACKET. LEFT SIDE CRACK APPROXIMATELY 1 INCH LONG. MANUFAC TURER CONTACTED AND REPAIR IMPLEMENTED. 1 G 7 1 4F 4 U NT TR7BO E17EA 1999111900192 19991119 00192 SW 1999 11 19 CA991027036 1 19991001 A 6310 206040205005 BEARING 206040230019 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FREEWHEEL UNIT FAILED W A UNSCHED LANDING O OTHER IN INSP/MAINT 1 CA 8039 1344 BLA2320 CAE821158 (CAN) POST-FLIGHT INSPECTION OF FREEWHEELING UNIT REVEALED THAT THE FORWARD CAP BEARING WAS FOUND IN PIECES. FREEWHEELI NG THROUGH SHAFT WAS SCORED/OVERHEATED. FOLLOWING DISASSEMBLY AT LABORATORY FOR METALLURGICAL TESTS, THE ENGINEERING RE PORT STATED THAT A SMALL PARTICLE OF A PRO-SEAL WAS BLOCKING THE OIL FITTING (206-040-254-001 OR 206-040-094-001). IT I S SUSPECTED THAT LACK OF OIL LUB CAUSED BEARING TO OVERHEAT AND FAIL. 1 G 7 1 3U 3 U H2SW E4CE 1999111900193 19991119 00193 1999 11 19 CA991027037 4 19991004 A 3422 HARNESS SPERRYFLT 258719343 SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE COCKPIT MISROUTED W A UNSCHED LANDING B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C NR NOT REPORTED 1 CA 78129660 295031 (CAN) WIRE CHAFING BETWEEN THE 26 VAC BUNDLE FOR INSTRUMENT LIGHTS AND COMPASS SYSTEM WIRE BUNDLES RESULTED IN A ELECTRI CAL SHORT AND SUBSEQUENT LOSS OF PILOT INSTRUMENT LIGHTS AND THE C-14 GYRO SYCRONIZER FOR THE COMPASS SYSTEMS. INVESTIG ATION REVEALED THAT WIRE BUNDLES WERE NOT ROUTED CORRECTLY AND WERE THUS RE-ROUTED CORRECTLY. A NEW C-14 GYRO WAS INSTA LLED AND ALL SYSTEMS ARE SERVICEABLE. 2 G 7 2 4U 4 U 1H15 1E3 1999111900194 19991119 00194 CE 1999 11 19 CA991027039 1 19991010 A 3221 NAS464P5A42 BOLT 12436001 CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO HARTZL HCJ3Y PHCJ3YF1 GL NLG SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 482 11041541 FP929A (CAN) DURING MAINTENANCE, NOSE GEAR DRAG LINK, AFT ATTACH BOLT FOUND WITH BOLT HEAD SHEARED OFF. 1 H 7 1 3O 3 O A4CE E5CE 5 C P36EA 1999111900195 19991119 00195 CE 1999 11 19 CA991027042 1 19991014 A 3260 MS2417101 RELAY BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL MLG CORRODED W O OTHER O OTHER LD LANDING 1 CA 7462 PCE32492 FWA2058 (CAN) ON APPROACH, THE LANDING GEAR WAS SELECTED DOWN BUT SYSTEM FAILED TO OPERATE. THE MANUAL EXTEND SYSTEM WAS USED A ND AN UNEVEVENTFUL LANDING WAS COMPLETED. UPON INSPECTION BY MAINTENANCE, THE RELAY CONTACTS FOR THE HYDRAULIC PUMP WER E FOUND TO HAVE SOME CONTACTS CORRODED. THE RELAY WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 1999111900196 19991119 00196 NE 1999 11 19 CA991027043 1 19991019 A 6320 S613520600046 DRIVE SHAFT SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE NR 1 ENGINE SEPARATED W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 CA A14013761027 295056 (CAN) DURING CLIMB AT 80 PERCENT TORQUE, NR 1 ENGINE LOST POWER AND ROTORCRAFT LANDED ON SINGLE ENGINE. POST-FLIGHT INV ESTIGATION REVEALED THAT NR 1 DRIVESHAFT HAD SEPARATED FROM THE TRANSMISSION INPUT DUE TO TRANSMISSION INPUT GEAR SEIZIN G. 2 G 7 2 4U 4 U 1H15 1E3 1999111900197 19991119 00197 GL 1999 11 19 CA991027045 2 19990928 A 7323 2520503 BEARING ALAA2 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL GOVERNOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 126 27245 CAE830901 (CAN) PT GOVERNOR LEVER BEARINGS ARE DEVELOPING FLAT SPOTS INTERNALLY AND EXTERNALLY WHICH DIRECTLY AFFECTS GOVERNOR SPR ING TENSION WHICH IN TURN THEN CAUSES THE GOVERNOR TO BLEED OFF EARLY. THE NET EFFECT IS DROOP. 1 G 7 1 3U 3 U H3WE E4CE 1999111900198 19991119 00198 EU 1999 11 19 CA991027047 1 19990717 A 6420 350A33200403 SPIDER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 5274 1462 M258 347 (CAN) T/R SPIDER ASSY BEARING FAILED THE ROTATIONAL DRAG TORQUE TEST (SB 05.00.29). THE BEARING WAS ALSO ROUGH WHEN ROTA TED. 1 G 7 1 3U 3 U H9EU E19EU 1999111900199 19991119 00199 WP 1999 11 19 CA991027048 1 19990801 A 6320 369D2570411 LINE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R GEARBOX CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA CAE830657 (CAN) OIL LEAK TRACED TO MGB OIL LINE WHICH WAS CHAFED THROUGH BY A CLAMP. 1 G 7 1 3U 3 U H3WE E4CE 1999111900200 19991119 00200 EU 1999 11 19 CA991027049 1 19990807 A 2435 BRUSHES AIRCRFTPRDTS 150SG122Q SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE STARTER/GEN BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 1277 6160 835 (CAN) INSPECTION OF THE STARTER/GENERATOR REVEALED 3 BROKEN BRUSHES AND A BROKEN ELECTRICAL WIRE. THE STARTER/GENERATOR STARTER SHAFT WAS ALSO BENT. 1 G 7 1 3U 3 U H9EU E19EU 1999111900201 19991119 00201 WP 1999 11 19 CA991027052 1 19990906 A 6420 BEARING 369D216009 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL TAIL ROTOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 4316 0022222190 CAE830926 (CAN) SUSPECT FAILURE OF ELASTOMETRIC FORK/HINGE BEARING AS T/R WAS DIFFICULT TO BALANCE. 1 G 7 1 3U 3 U H3WE E4CE 1999111900202 19991119 00202 EU 1999 11 19 CA991027053 1 19990906 A 6210 355A11002026 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5030 4120 879 (CAN) CRACK FOUND IN AREA C OF THE TRAILING EDGE (BETWEEN STA 590 AND STA 725). 1 G 7 1 3U 3 U NC H9EU E19EU 1999111900203 19991119 00203 NM 1999 11 19 CA991027067 1 19991008 A 3234 574205 SELECTOR VALVE DOWTY 83210001001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 12390 121399 880611 (CAN) LANDING GEAR WOULD NOT RETRACT. PANEL SHOWED 3 GREEN, 3 RED, AND 3 YELLOW TRANSIT LIGHTS ON. GEAR DOWN SELECTION MADE WITH 3 GREEN AND DOORS CLOSED. LANDING GEAR SELECTOR VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900204 19991119 00204 NM 1999 11 19 CA991027069 1 19991013 A 3232 10500103 ACTUATOR DOWTY 83210001001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG DOOR CRACKED W L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 26196 2368 120468 860512 (CAN) ON APPROACH, PILOTS HEARD A LOUD BANG FOLLOWED BY LOSS OF NR 2 HYDRAULIC QUANTITY. MAIN LANDING GEAR DOOR ACTUATO R REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900205 19991119 00205 EU 1999 11 19 CA991027070 1 19990924 A 5620 1379595C3 WINDOW BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110 01514 WP LT PAX WINDOW CRACKED W I CABIN DEPRESSURIZATION O OTHER CR CRUISE 1 CA 16087 P63111 (CAN) DURING CRUISE FLIGHT, THE LEFT HAND PASSENGER WINDOW EXTERNAL PANEL, CRACKED THROUGH. CABIN PRESSURE REDUCED TO 2 PSI FOR REMAINDER OF FLIGHT. 2 L 7 2 4T 4 T RT BA15CAA E4WE 1999111900206 19991119 00206 EU 1999 11 19 CA991027071 1 19990930 A 5620 1379595C3 WINDOW BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110 01514 WP LT PAX WINDOW CRACKED W I CABIN DEPRESSURIZATION O OTHER CR CRUISE 1 CA 16071 P63111 (CAN) DURING CRUISE FLIGHT, THE LEFT HAND NR 1 PASSENGER EXTERNAL WINDOW PANEL CRACKED. AIRCRAFT DEPRESSURIZED TO 2 PSI FOR REMAINDER OF FLIGHT. 2 L 7 2 4T 4 T RT BA15CAA E4WE 1999111900207 19991119 00207 SO 1999 11 19 CA991027073 1 19991005 A 2730 710563 SPRING PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA HARTZL HCE3Y HCE3YR2 GL ELEVATOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 488 L649461A DJ8142A (CAN) AD 98-08-18 ELEVATOR DOWN SPRING REPLACEMENT JULY 03/98 AT 14,302 TAFT. INSPECTION OF SPRING DURING NORMAL INSPEC TION REVEALED ODD WEAR/DAMAGE TO SPRING END. CAUSE UNKNOWN. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999111900208 19991119 00208 CE 1999 11 19 CA991027074 1 19991009 A 3221 12116011 FITTING CESSNA 206 U206E 2073350 CE CONT O520 IO520F 17032 SO LT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5400 175576R (CAN) DURING SCHEDULED MAINTENANCE, THE LEFT OUTBOARD MAIN LANDING GEAR FITTING WAS FOUND CRACKED AT THE AFT LOWER RADIU S. 1 H 7 1 3O 3 O A4CE E5CE 1999111900209 19991119 00209 CE 1999 11 19 CA991028008 1 19991006 A 7120 265102215 MOUNT RING CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5742 PCE19255 912967 (CAN) DURING SCHEDULED MAINTENANCE, THE ENGINE MOUNT RING WAS FOUND CRACKED AT THE TWO LOWEST PICK-UP SPIGOTS ON THE EXI STING WELDS. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 1999111900210 19991119 00210 CE 1999 11 19 CA991028009 1 19991018 A 3040 W20538100 RESISTOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL COCKPIT BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA PCE51808 BU17909 (CAN) PILOT REPORTED SMOKE IN THE CABIN FROM OVERHEAD PANEL. UPON INVESTIGATION FOUND WINDSHIELD WIPER MOTOR RESISITOR AND WIRE BURNT. BOTH ITEMS REPLACED. CIRCUIT BREAKER REPLACED AS A CAUTIONARY PRACTISE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999111900211 19991119 00211 SW 1999 11 19 CA991028010 1 19991018 A 2910 2781032079 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE HYDRAULIC SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 11404 P44436 9311170 (CAN) ALUMINUM HYDRAULIC LINE CRACKED AT CLAMP POINT IN FORWARD CONTAINMENT BAG. SUBMITTER SUGGESTED CLAMP WAS IMPROPER LY INSTALLED AT THE FACTORY. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999111900212 19991119 00212 CE 1999 11 19 CA991028011 1 19990910 A 5510 07123021 BRACKET CESSNA 180 180H 2072618 CE CONT O470 O470R 17026 SO MCAULY 2A34C 2A34C66 GL EMPENNAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 49041R 746179 (CAN) DURING SCHEDULED MAINTENANCE, STABILIZER APPEARED LOOSE. FURTHER INVESTIGATION REVEALED A CRACKED HINGE BRACKET. 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 1999111900213 19991119 00213 EU 1999 11 19 CA991028018 1 19991001 A 2720 RUDDER PEDAL AIRBUS 330 A330202 3930316 EU COCKPIT JAMMED W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 811148 (CAN) CREW REPORTED LIMITED RUDDER TRAVEL. MAINTENANCE REMOVED CELL PHONE FROM CAPTAIN'S PEDALS.........SYSTEM OPERATED NORMAL! 2 L 7 2 4F RT A46NM 1999111900214 19991119 00214 NM 1999 11 19 CA991028020 1 19990916 A 3010 85720013006 BOOT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT WING PUNCTURED W O OTHER C F.O.D. LD LANDING 1 CA 22646 0060082 120338 890605 (CAN) BIRD STRIKE ON NR 3 LEADING EDGE ON APPROACH. BOOT REPAIRED THEN REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900215 19991119 00215 NM 1999 11 19 CA991028021 1 19990930 A 5315 85310380 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 30437 120338 890605 (CAN) DURING INSPECTION, NLG WELL UPPER FRAME WAS FOUND CRACKED. CRACK RAN FROM THE LOWER FORWARD RADIUS TO THE BACK OF THE FRAME UNDER THE UPLOCK ACTUATOR FITTING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900216 19991119 00216 NM 1999 11 19 CA991028022 1 19991004 A 2820 82820077003 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL SYSTEM CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 22249 120584 LH1766 (CAN) FUEL WAS FOUND LEAKING FROM THE WING ON THE OUTBOARD SIDE OF THE NACELLE. FUEL SUPPY LINE FROM COLLECTOR BOX TO N ACELLE HAD TWO CHAFE MARKS IN IT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900217 19991119 00217 NM 1999 11 19 CA991028023 1 19991002 A 7930 82455020011 HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL PRESSURE SHORTED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA 22041 120249 LH646 (CAN) OIL PRESSURE DROPPED BETWEEN 5-8 PSI WHEN PROP SYNC SELECTED. SHORT BETWEEN PINS 6 AND 16 IN HARNESSES 9811P17 AN D 9811P29. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999111900222 19991119 00222 WP 1999 11 19 CA991028038 1 19991004 A 5230 1582113101 TORQUE TUBE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10284 (CAN) DURING INSPECTION LIFT TORQUE TUBES, FOUND CRACKED NEAR ENDS. FLEET CAMPAIGN INITIATED. 2 L 7 3 4F 4 F A23WE E12EU 1999111900223 19991119 00223 NM 1999 11 19 CA991028039 1 19990904 A 5610 WINDSHIELD AIRBUS A319 A319114 NM GE CFM56 CFM565A 13802 NE COCKPIT CRACKED W O OTHER O OTHER NR NOT REPORTED 1 CA 731902 (CAN) FIRST OFFICER'S OUTER PANE CRACKED. WINDSHIELD REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999111900224 19991119 00224 EA 1999 11 19 CA991028043 1 19991001 A 2750 SENSING UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 807380 (CAN) FLAPS FAIL ON APPROACH AT ZERO DEGREES. NR 5 FLEX SHAFT AND RIGHT BRAKE SENSOR REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900225 19991119 00225 NM 1999 11 19 CA991028045 1 19991005 A 7500 VALVE CFM565A5 AIRBUS A319 A319114 NM GE CFM56 CFM565A 13802 NE NR 1 ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 731921 731921 (CAN) AFTER NR 1 ENGINE BLEED AIR FAULT ILLUMINATED, AIRCRAFT LANDED DUE TO ICING CONDITION FORECAST. REPLACED PRESSURE REGULATOR VALVE AND TRANSDUCER 7HA1. 2 L 7 2 4F 4 F RT A28NM E29NE 1999111900226 19991119 00226 EA 1999 11 19 CA991028046 1 19991005 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 807380 (CAN) FLAPS FAILED ON APPROACH. NR 3 ACTUATOR AND NR 5 LEFT ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900227 19991119 00227 EA 1999 11 19 CA991028048 1 19991015 A 2752 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE WING FAILED W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA (CAN) FLAP FAIL CAUTION MESSAGE AT 16 DEGREES. ONGOING INVESTIGATION BY TC. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900229 19991119 00229 EA 1999 11 19 CA991028050 1 19991021 A 2752 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE WING FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) FLAPS FAIL AT 8 DEGREES. RIGHT OUTBOARD FLAP TWISTED AND NR 4 FLEXSHAFT BROKE. FLAP, NR 3, NR 4 RIGHT ACTUATORS AND NR 4 FLEXSHAFT REPLACED. PDU REPLACED DUE TO THREAD DAMAGE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900230 19991119 00230 CE 1999 11 19 CA991028052 1 19991005 A 5510 04320016 RIB 043200159 CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9138 L2371415 (CAN) HORIZONTAL STABILIZER RIGHT RIB CRACKED. 1 H 7 1 3O 3 O NT 3A19 E223 1999111900231 19991119 00231 CE 1999 11 19 CA991028053 1 19991005 A 5510 043200146 RIB 043200159 CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA LT ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9641 L1388615 (CAN) HORIZONTAL STABILIZER LEFT RIB CRACKED. 1 H 7 1 3O 3 O NT 3A19 E223 1999111900232 19991119 00232 EA 1999 11 19 CA991028055 1 19991018 A 2422 WIRE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL INVERTER SHORTED W C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 CA GG41829 BU15605 (CAN) INVERTER SYSTEM FAILED IN-FLIGHT. TROUBLESHOOTING FOUND WIRE FROM CVR INPUT SWITCH TO CIRCUIT BREAKER SHORTING T O ITS OWN SHIELDING. WIRE REPAIRED. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 1999111900233 19991119 00233 SO 1999 11 19 CA991028057 1 19991014 A 7160 BA15 AIR FILTER PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA HARTZL HCE2Y HCE2YR2 GL INTAKE CLOGGED W A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 35 L372748 BP8496 (CAN) AIRCRAFT FLEW IN RAIN APPROXIMATELY 45 MINUTES, AND THEN CAME OUT IN THE CLEAR AT 7,000 FEET, AND -5 DEGREES CEL SIUS. ENGINES FUEL FLOW DECREASED, ENGINES SLOWED DOWN. PILOT SELECTED ALTERNATE AIR ON AND RECOVERED POWER. RE-SELE CTED ALTERNATE AIR OFF AFTER A FEW MINUTES AND TERMINATED FLIGHT NORMALLY. BOTH ENGINES' AIR INTAKE FILTER ELEMENTS P/N BA15 FOUND SATURATED WITH WATER. SUBMITTER SUSPECTED WET ELEMENTS FROZE UP RESTRICTING AIRFLOW. 1 L 7 2 3O 3 O 1A10 1E4 5 C P9EA 1999111900234 19991119 00234 SW 1999 11 19 CA991028062 1 19991001 A 5541 442283 SPAR SLINDS GULSTM 112 112B 7630303 SW LYC O360 IO360C1D6 41514 EA HARTZL HCE2Y HCE2YR1 GL RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1912 L1658851A DK1854A (CAN) RUDDER SPAR CRACKED. 1 L 7 1 3O 3 O A12SO 1E10 5 C P9EA 1999111900235 19991119 00235 SO 1999 11 19 CA991028063 1 19991004 A 2140 44814000 HEATER PLATE DWG52551 PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL CABIN BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 12025 L586361A DJ11486A (CAN) REF: IPC FIG. 112A ITEM 2. NOTICED PLATE STOP DRILLED PREVIOUSLY. CRACKS HAD SINCE PROGRESSED IN 90 DEGREE BE NT LIP RADIUS TO PERMIT SCREWING PART TO FORMER AND TO REMOVEABLE PART OF FORMER. DESIGNED FOR EASIER HEATER REMOVAL/IN STALLATION. IT APPEARS PART WAS NOT ALWAYS REMOVED AT HEATER MAINTENANCE AND SEVERAL FORCING ASIDE FATIGUED ANGLE BEND AND EVENTUALLY FAILED. A DOUBLER WAS INSTALLED PENDING RECEIPT OF NEW PART. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999111900236 19991119 00236 EA 1999 11 19 CA991028064 1 19991007 A 3242 6008512381 BRAKE CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE RT MLG FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 1252 OCT940639 350173 (CAN) TECHNICIAN NOTICED THE RIGHT OUTBOARD MAIN WHEEL WAS FLAT. THE FUSE PLUG WAS FOUND MELTED AS WELL AS A LOCALIZED W EAR (FLAT SPOT) ON THE TIRE. IT WAS NOTICED THAT THE WHEEL HAD OVERHEATED AND SUFFERED PREMATURE WEAR CAUSED BY THE BRA KE WHICH WAS STUCK ON. THE BRAKE WAS NOT EQUALLY WORN AND WAS OUT OF LIMITS, HOWEVER, THE WEAR INDICATOR WAS OVER THE L IMITS. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900237 19991119 00237 CE 1999 11 19 CA991028067 1 19990926 A 2752 505212234 ACTUATOR BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL TE FLAP FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 2500 EAS130988 PCE51331 BU2556 (CAN) AFTER LANDING, OUTBOARD FLAP FAILED TO RETRACT. ACTUATOR MANUALLY RUN IN AND SYSTEM SECURED. AIRCRAFT FERRIED TO MAIN BASE. REPLACED ACTUATOR. THIS UNIT HAS A 10,000 CYCLE LIFE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999111900238 19991119 00238 CE 1999 11 19 CA991028068 1 19990921 A 2400 CONNECTOR BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL POWER INPUT CONTAMINATED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA PCE51331 BU2556 (CAN) SUSPECT WATER CAUSED SHORTING ON POWER INPUT PORTION OF CIRCUIT BREAKER PANEL - PERHAPS SOME WINDOW OPEN OR LEAK ( HIGH WINDS CAN FORCE SIDE WINDOW TO OPEN SLIGHTLY). ALSO NOTED SOME COPILOT INSTRUMENT LIGHTS, ALSO NOT WORKING ( A SEP ARATE PROBLEM). FOUND BURNT TRANSISITOR ON LIGHT DIMMER ASSY LOCATED ON BULKHEAD FORWARD OF COPILOT'S RUDDER PEDALS. A PLASTIC GASKET ON THE ASSY SEEMED TO HAVE CAUSED THE SMOKE AND SMELL. SUBMITTER STATED THE BURNT TRANSISTOR APPEARS TO HAVE BEEN CAUSED BY A SHORT COMING FROM A PUSHED IN POST LIGHT BULB ASSY ON THE COPILOT'S SIDE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999111900239 19991119 00239 CE 1999 11 19 CA991028070 1 19991017 A 3310 50524558 LIGHT 505245711 BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL COCKPIT SHORTED W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA PCE51331 BU2556 (CAN) AFTER TAKEOFF, NOTICED FUMES IN COCKPIT. NON-ESSENTIAL ELECTRICS WERE SHUT OFF AND EMERGENCY DECLARED. CREW REPO RTED THAT THEY HAD NOTICED WATER AROUND THE CIRCUIT BREAKER PANELS. ENGINEER INSPECTED THE AIRCRAFT AND FOUND SOURCE OF FUMES TO BE COMING FROM THE RUDDER TRIM LIGHTED PANEL WHICH HAD A SINGED LIGHT BULB WHICH HAD PREVIOUSLY SHORTED OUT. PANEL REMOVED. AIRCRAFT GROUND RUN FOR 45 MINUTES. ALL SYSTEMS WERE OK. CIRCUIT BREAKER PANELS WERE CHECKED FOR WA TER AND FOUND TO BE DRY. AIRCRAFT TTSN: 33,860.2 HRS. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999111900242 19991119 00242 EU 1999 11 19 99ZZZX4246 1 19991029 A 6120 89548122 PITCH CONTROL CASA C212 C212CC 2410204 EU NR 1 ENGINE FAILED A EHAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 423CA 2252 4109 240 TENDENCY FOR NR 1 ENGINE TO OVERSPEED WITH SPEED LEVERS SET FOR 96.5 PERCENT RPM AND TORQUE AT 45 PERCENT. ENGINE IN TH IS SETTING WOULD OVERSPEED TO 102.0 PERCENT RPM. THIS IS A RECURRENCE OF A SIMILAR INCIDENT IN JULY, 1999, ON THE SAME ENGINE. THE PROBLEM WAS SUSPECTED TO BE RIGGING, AND AFTER RE-RIGGING, THE PROBLEM WENT AWAY. AS THE CONTROLLING COMPO NENT AT THIS SETTING IS THE PROP PITCH CONTROL (PPC), THIS COMPONENT IS BEING REMOVED AND REPLACED. 2 H 7 2 4T A43EU 1999111900259 19991119 00259 NM 1999 11 19 TWAA9915401 1 19991109 A 3350 251005 FUSE BOEING 757 7572Q8 1384972 NM R1 DOORWAY BLOWN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 701TW 28160 THE RIGHT SIDE NUMBER 1 CABIN DOOR SLIDE LIGHT WAS INOPERATIVE. REPLACED FUSE AND IT BLEW AGAIN. REPOSITIONED THE LIGH T ASSEMBLY AND INSULATED THE CENTER BULB WIRE CONTACT, THEN REPLACED THE FUSE AGAIN. CHECK-C 7-31-99 LAX. 2 L 7 2 4F RT A2NM 1999111900260 19991119 00260 NM 1999 11 19 TWAA9915402 1 19991106 A 3350 582243 BATTERY CHARGER BOEING 767 7673Q8 NM CABIN INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 THE RT FORWARD COACH SECTION OF CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY CHARGER. CHECK-C 11-1-99 LA X. 2 L 7 2 4F RT A1NM 1999111900261 19991119 00261 WP 1999 11 19 TWAA9915403 1 19991101 A 5711 SPAR DOUG DC9 DC931 3022065 WP WS 353 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING OP 16 MAINT CHECK, FOUND RT WING REAR SPAR OTBD FLAP MOUNT HOLES AT XRS 353 HAD THE LOWER OTBD HOLE CRACKED 1.125 INCH LONG. REAR SPAR REPAIRED AT XRS 353 PER ARA 16334. 2 L 7 2 4F A6WE 1999111900262 19991119 00262 EU 1999 11 19 MALA976633 1 19991108 A 3230 L38710SA ACTUATOR SAAB SF340 SF340A 7850100 EU LANDING GEAR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 109XJ 340A109 AFTER TAKEOFF, THE HYDRAULIC CAUTION LIGHT ILLUMINATED, PERFORMED MEMORY ITEMS. CREW NOTED ONLY THE HYDRAULIC MAIN PRES SURE ACCUMULATOR AND HYDRAULIC QUANTITY INDICATOR BOTH READ ZERO AND IN THE RED ARK. ALL OTHER ACCUMULATORS AND GAUGES WERE NORMAL. WE PERFORMED THE QRH CHECKLIST AND DECLARED AN EMERGENCY AND RETURNED TO CRW. MAINTENANCE REPLACED DOWNLO CK RELEASE ACTUATOR SWIVEL, SERVICED HYDRAULIC SYSTEM. RESET EMERGENCY GEAR RELEASE SYSTEM, COMPLETE NECESSARY OPERATIO NAL CHECKS. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999111900263 19991119 00263 WP 1999 11 19 CALA9901479 1 19991109 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP WS 414.125 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14079 46927 INSPECTION FOUND A 3 CRACK IN RT WING FIXED L/E SUPPORT ANGLE AT STA XOS 414.125. A NEW ANGLE WAS INSTALLED IAW SRM 51- 31-01. 2 L 7 3 4F A22WE 1999111900264 19991119 00264 WP 1999 11 19 CALA9901480 1 19991109 A 7110 ANGLE DOUG DC10 DC1030 3023501 WP NR 1 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14079 46927 INSPECTION FOUND NR 1 ENGINE INTAKE EXTERNAL SIDE AFT SUPPORT ANGLES(2) CRACKED. THE CRACKS WERE 1 LONG. THE SUPPORT A NGLES WERE REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1999111900265 19991119 00265 NM 1999 11 19 CALA9901481 1 19991110 A 5320 JAMB BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND A 1.5 CRACK IN LT AFT ENTRY DOOR JAMB AT STA 1183, NEAR THE SECOND DOOR STOP DOWN FROM TOP. REPAIR WAS ACCOMPLISHED IAW DRAWING 365C15764 AND EA 5310-03567. 2 L 7 3 4F A3WE 1999111900266 19991119 00266 NM 1999 11 19 CALA9901482 1 19991111 A 5753 6521630173 SKIN BOEING 727 727232 1384082 NM LT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND LT I/B FOREFLAP I/B EDGE UPPER SKIN GOUGED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1. 2 L 7 3 4F A3WE 1999111900267 19991119 00267 WP 1999 11 19 CALA9901483 1 19991111 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND CABIN RT CENTER SEAT TRACK CORRODED AT STA 218, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SR M 51-30-1 AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999111900268 19991119 00268 WP 1999 11 19 CALA9901484 1 19991111 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A 3 CRACK AND CORROSION ON FORWARD CARGO FLOOR SUPPORT AT FORWARD BULKHEAD, STA 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999111900269 19991119 00269 WP 1999 11 19 CALA9901485 1 19991111 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 218 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A .5 INCH CRACK IN CUSP WEB AT STA 218. THE CRACK WAS STOP DRILLED IAW SRM 53-10, FIGURE 2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-10-4. 2 L 7 2 4F A6WE 1999111900270 19991119 00270 WP 1999 11 19 CALA9901486 1 19991111 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A 1 CRACK IN MID CARGO DOOR BRACKET AT LOWER END OF FORWARD STIFFENER. THE BRACKET WAS REMOVED AND A N EW BRACKET WAS INSTALLED IAW SRM 51-30-2 AND 52-33-0, FIGURE 1. 2 L 7 2 4F A6WE 1999111900271 19991119 00271 WP 1999 11 19 CALA9901487 1 19991112 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 286 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72821 49481 INSPECTION FOUND A 3 CRACK IN RT WING LEADING EDGE UPPER SKIN AT STA XOS 286. A DOUBLER WAS INSTALLED IAW ECRA 5720-017 73 AND A DIP WAS INITIATED TO REINSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 14 DAYS AND TO INSTALL A PERMANENT REPAIR WITHIN 12 MONTHS. 2 L 7 2 4F A6WE 1999111900272 19991119 00272 NM 1999 11 19 CALA9901488 1 19991112 A 5753 6521631324A SKIN BOEING 727 727232 1384082 NM RT TE FOREFLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND RT O/B FOREFLAP I/B T/E DELAMINATED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-57-11. 2 L 7 3 4F A3WE 1999111900273 19991119 00273 NM 1999 11 19 CALA9901489 1 19991112 A 5755 651734871 SKIN BOEING 727 727232 1384082 NM NR 5 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND LT WING NR 5 SPOILER UPPER SURFACE DELAMINATED AT I/B FORWARD CORNER. THE SPOILER WAS REMOVED AND REPL ACED IAW MM 27-61-1. 2 L 7 3 4F A3WE 1999111900274 19991119 00274 NM 1999 11 19 CALA9901490 1 19991112 A 5755 6517348108A SKIN BOEING 727 727232 1384082 NM NR 9 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND THE NR 9 SPOILER UPPER SURFACE DELAMINATED AT FORWARD I/B CORNER. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1. 2 L 7 3 4F A3WE 1999111900275 19991119 00275 EA 1999 11 19 COMA9960682 1 19991106 A 3350 100865 POWER SUPPLY CNDAIR CL600 CL6002B19 EA CABIN INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 958CA 7111 EXTERIOR OVERWING EMERGENCY EXIT LIGHTS ARE INOPERABLE. REPLACED THE NR 3 POWER SUPPLY. 2 L 7 2 4F RT A21EA 1999111900276 19991119 00276 NM 1999 11 19 UPS99231093 1 19991112 A 3350 BATTERY PACK BOEING 727 72751C 1384015 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 904UP 18946 FWD ENTRY DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED BATTERY PACK ON EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999111900277 19991119 00277 NM 1999 11 19 QXEA9902234 1 19991030 A 5400 ANGLE DHAV DHC8 DHC8102 2809003 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - ANGLE ATTACHMENT FOR OUTBOARD NACELLE SKIN TO WIG BOX, TO FROM MAIN LANDING GEAR FRAME. REPAIRED IAW HORIZON AIR EA 9-53-485. 2 H 7 2 4T RT A13NM 1999111900278 19991119 00278 NM 1999 11 19 QXEA9902235 1 19991013 A 5711 ANGLE DHAV DHC8 DHC8102 2809003 NM WING SPAR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - UPPER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN THE AREA FOR LEADING EDGE 613CR ATTACHMENT. REPAIRED IA W DHC-8-100 M/M 20-32-02. 2 H 7 2 4T RT A13NM 1999111900279 19991119 00279 NM 1999 11 19 QXEA9902236 1 19991013 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM WING SPAR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LOWER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN AREA FOR LEADING EDGE 613CR ATTACHMENT. REPAIRED IAW DH C-8-100 M/M 20-32-02. 2 H 7 2 4T RT A13NM 1999111900280 19991119 00280 NM 1999 11 19 QXEA9902237 1 19991013 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM WING SPAR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - UPPER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN THE AREA FOR LEADING EDGE 613AR. REPAIRED IAW DHC-8-100 M/M 20-32-02. 2 H 7 2 4T RT A13NM 1999111900281 19991119 00281 NM 1999 11 19 QXEA9902238 1 19991013 A 5720 ANGLE DHAV DHC8 DHC8102 2809003 NM WING SPAR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LOWER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN THE AREA FOR LEADING EDGE 613AR. REPAIRED IAW DHC-8-102 M/M 20-32-02. 2 H 7 2 4T RT A13NM 1999111900282 19991119 00282 NM 1999 11 19 QXEA9902239 1 19991015 A 5753 PATCH DHAV DHC8 DHC8102 2809003 NM LT TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - OUTBOARD FLAP UPPER SURFACE AT STATION YW232.200 PREVIOUS REPAIR CHAFE PATCH IS CHAFFED APPROXIMATELY .010. REPAI RED IAW RD 8-57-037. 2 H 7 2 4T RT A13NM 1999111900283 19991119 00283 NM 1999 11 19 QXEA9902240 1 19991014 A 5720 SKIN DHAV DHC8 DHC8102 2809003 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FRETTING CORROSION ON SURFACE THAT THE ANTI-FRET RING CONTACTS. REPAIRED IAW HORIZON AIR EA 9-57-457. 2 H 7 2 4T RT A13NM 1999111900284 19991119 00284 NM 1999 11 19 QXEA9902241 1 19991013 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT WING OUTBOARD FLAP CHAFFED .010 ON REPAIR PATCH. REPAIRED IAW RD 8-57-037. 2 H 7 2 4T RT A13NM 1999111900285 19991119 00285 NM 1999 11 19 QXEA9902242 1 19991013 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM LT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT WING INBOARD FLAP .015: DEEP CHAFFED DAMAGE TO REPAIR ON FLAP. REPAIRED IAW RD 8-57-037. 2 H 7 2 4T RT A13NM 1999111900286 19991119 00286 NM 1999 11 19 QXEA9902243 1 19991014 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM LT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT WING INBOARD FORWARD SPAR INBOARD END HAS SMALL FRETTING DAMAGE TO END. REPAIRED IAW RD 8-57-811, STEPS 5 TH ROUGH 7. 2 H 7 2 4T RT A13NM 1999111900287 19991119 00287 NM 1999 11 19 QXEA9902244 1 19991016 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WS 39&39.75 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT FORWARD CORNER OF LADDER PLATE FOR PANEL 521AT HAS TWO CORROSION PITS AT STATIONS YW39.00 AND 39.75. REPAIRE D IAW HORIZON AIR EA 9-57-459. 2 H 7 2 4T RT A13NM 1999111900288 19991119 00288 NM 1999 11 19 QXEA9902245 1 19991018 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LADDER PLATE FOR 522AT HAS CORROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EO 9-57-68D, PAGE 9 OF 19, DHC- 8 SRM 51-20-16 AND RD 8-57-114. 2 H 7 2 4T RT A13NM 1999111900289 19991119 00289 NM 1999 11 19 QXEA9902246 1 19991016 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LADDER PLATE 521AT HAS CORROSION AROUND SCREW HOLES. REPAIRED IAW SRM 51-20-36, RD 8-57-592 AND DHC-8 PSM 1-8-7A 51-00-06. 2 H 7 2 4T RT A13NM 1999111900290 19991119 00290 NM 1999 11 19 QXEA9902247 1 19991008 A 5330 PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - PANEL 521AT HAS FRETTING CORROSION ON INSIDE MATING SURFACE AT INBOARD AND OUTBOARD EDGES. REPAIRED IAW DHC-8 SRM 51-20-16, RD 8-57-617 AND -8 PSM 1-8-7A 51-00-04. 2 H 7 2 4T RT A13NM 1999111900291 19991119 00291 NM 1999 11 19 QXEA9902248 1 19991008 A 5330 PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - PANEL 521AT HAS TWO DEEP CORROSION GOUGES ON LEFT MATING SURFACE EDGE. REPAIRED IAW DHC-8 SRM 51-20-16. 2 H 7 2 4T RT A13NM 1999111900292 19991119 00292 NM 1999 11 19 QXEA9902249 1 19991030 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FORWARD SIDE OF OUTBOARD MAIN LANDING GEAR FRAME, TWO DRILL MARKS, JUST AFT OF ENGINE BAY FIREWALL. REPAIRED IAW HORIZON AIR EA 9-54-221. 2 H 7 2 4T RT A13NM 1999111900293 19991119 00293 NM 1999 11 19 QXEA9902250 1 19991029 A 5412 FIREWALL DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - THERE IS A CRACK IN THE AFT FIREWALL OF THE NR 2 ENGINE, OUTBOARD SIDE, AT BEND IN MATERIAL JUST ABOVE FIRE DETECT ION LOOP BRACKET. REPAIRED IAW HORIZON AIR EA 9-54-219 AND RD 8-54-430. 2 H 7 2 4T RT A13NM 1999111900294 19991119 00294 NM 1999 11 19 QXEA9902251 1 19991022 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT NACELLE UPPER DECK FOR EXHAUST FINGERNAIL IS CORRODED AND HAS SEVERAL AREAS WITH DEEP CHAFE MARKS. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900295 19991119 00295 NM 1999 11 19 QXEA9902252 1 19991023 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT NACELLE EXHAUST FINGERNAIL DECK HAS DEEP CHAFE MARKS AT STATION XN 224.76. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 THROUGH 4. 2 H 7 2 4T RT A13NM 1999111900296 19991119 00296 NM 1999 11 19 QXEA9902253 1 19991023 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT NACELLE EXHAUST FINGERNAIL DECK HAS 1 .5 BY .75 HOLE CHAFED THROUGH AT STATION XN 224.76. REPAIRED IAW DHC- 8 SRM 51-40-00, PAGE 1 THROUGH 4. 2 H 7 2 4T RT A13NM 1999111900297 19991119 00297 NM 1999 11 19 QXEA9902254 1 19991014 A 5400 WEB DHAV DHC8 DHC8102 2809003 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT NACELLE AFT WALL OF WHEEL WELL IS CHAFED WHERE LOWER PORTION OF GRAVEL GUARD ATTACHES. REPAIRED IAW RD 8-54 -041. 2 H 7 2 4T RT A13NM 1999111900298 19991119 00298 NM 1999 11 19 QXEA9902255 1 19991028 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM LT NACELLE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - DENT ON INBOARD SIDE OF LEFT NACELLE AT APPROXIMATELY XN 155.30 AND ZN 24.25. REPAIRED IAW SRM 54.30.21, PAGE 2, FIGURE 2. 2 H 7 2 4T RT A13NM 1999111900299 19991119 00299 NM 1999 11 19 QXEA9902256 1 19991020 A 5412 FIREWALL DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - THERE IS A CRACK IN THE AFT FIREWALL OF THE NR 1 ENGINE, ON THE INBOARD SIDE, AT THE BEND IN MATERIAL JUST ABOVE T HE FIRE DETECTION LOOP BRACKET. REPAIRED IAW RD 8-54-806. 2 H 7 2 4T RT A13NM 1999111900300 19991119 00300 NM 1999 11 19 QXEA9902257 1 19991009 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FINGERNAIL DECK HAS A CHAFE ON UPPER SURFACE AT CENTERLINE OF NACELLE AT STATION XN 240. REPAIRED IAW DHC-8-100 S RM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900301 19991119 00301 NM 1999 11 19 QXEA9902258 1 19991021 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM LT MLG WW CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - PITTING CORROSION ON TOP HOLE OF LEFT MAIN LANDING GEAR FRAME WHERE MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHME NT FITTING IS MOUNTED. REPAIRED IAW HORIZON AIR EA 9-54-213. 2 H 7 2 4T RT A13NM 1999111900302 19991119 00302 NM 1999 11 19 QXEA9902259 1 19991018 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 653 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT SIDE REAR FUSELAGE SKIN HAS DENT APPROXIMATELY .500 IN DIAMETER AND .045 DEEP AT APPROXIMATELY STATION 653.34 9. REPAIRED IAW RD 8-53-2181 AND SRM 53-30-24, PAGE 1. 2 H 7 2 4T RT A13NM 1999111900303 19991119 00303 NM 1999 11 19 QXEA9902260 1 19991014 A 5311 CASTELLATION DHAV DHC8 DHC8102 2809003 NM FRAME 2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - REAR FUSELAGE FRAME CASTELLATION AT FRAME 3 AND AT APPROXIMATELY TOP 12 O'CLOCK POSITION IS CRACKED. REPAIRED IAW SRM 53-20-21, PAGE 5. 2 H 7 2 4T RT A13NM 1999111900304 19991119 00304 NM 1999 11 19 QXEA9902261 1 19991014 A 5522 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - TRAILING RUDDER TOP LEFT EDGE OF SKIN HAS CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 55-40-16, TABLE 2 AND SRM 51-20-11 . 2 H 7 2 4T RT A13NM 1999111900305 19991119 00305 NM 1999 11 19 QXEA9902262 1 19991018 A 5522 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FORE RUDDER UPPER LEADING EDGE, NEAR RUDDER RIB 11A LOCATION, HAS LOCATIONS OF HEAVY CHAFE DAMAGE TO LEFT SIDE OF LEADING EDGE. REPAIRED IAW DHC-8 SRM 55-40-28, FIGURE 2 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900306 19991119 00306 NM 1999 11 19 QXEA9902263 1 19991018 A 5540 STRIP DHAV DHC8 DHC8102 2809003 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FORE RUDDER TOP LEADING EDGE CHAFE STRIP HAS HEAVY CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900307 19991119 00307 NM 1999 11 19 QXEA9902264 1 19991014 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - THERE ARE TWO DENTS IN RIGHT EXTERNAL FUSELAGE SKIN AT STRINGER 2 AND STATION X600. REPAIRED IAW RD 8-53-436. 2 H 7 2 4T RT A13NM 1999111900308 19991119 00308 NM 1999 11 19 QXEA9902265 1 19991103 A 5350 FAIRING DHAV DHC8 DHC8102 2809003 NM FUSELAGE DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - THERE ARE NUMEROUS DELAMINATED AREAS ON COMPOSITE AERODYNAMIC FAIRING AROUND ACCESS PANEL 261AT. REPAIRED IAW HOR IZON AIR EA 9-53-492, STEPS 13-20, AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900309 19991119 00309 NM 1999 11 19 QXEA9902266 1 19991022 A 5320 THRESHOLD DHAV DHC8 DHC8102 2809003 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - MAIN CABIN DOOR THRESHOLD BEAM AND NUTPLATES HAVE CORROSION TOP SIDE AND UNDER SIDE X224 TO X248 Z100. REPAIRED I AW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900310 19991119 00310 NM 1999 11 19 QXEA9902268 1 19991019 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - NUMEROUS CORROSION DISCREPANCIES ON RIGHT OUTBOARD FORWARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999111900311 19991119 00311 NM 1999 11 19 QXEA9902269 1 19991022 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - NUMEROUS CORROSION AND DAMAGE DISCREPANCIES ON RIGHT CENTER SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999111900312 19991119 00312 NM 1999 11 19 QXEA9902270 1 19991031 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - NUMEROUS CORROSION DISCREPANCIES ON LEFT INBOARD CENTER SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999111900313 19991119 00313 NM 1999 11 19 QXEA9902271 1 19991102 A 5320 SUPPORT DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - INBOARD AND OUTBOARD FLOOR SUPPORTS FOR WARDROBE ARE CORRODED ALONG UPPER SURFACE. REPAIRED IAW HORIZON AIR EA 9- 53-483. 2 H 7 2 4T RT A13NM 1999111900314 19991119 00314 NM 1999 11 19 QXEA9902272 1 19991028 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FRAME 4885 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - CORROSION ON FORWARD SIDE OF FRAME 4885 FROM STRINGER 32P TO STRINGER 32S. REPAIRED IAW HORIZON AIR EA 9-53-487. 2 H 7 2 4T RT A13NM 1999111900315 19991119 00315 NM 1999 11 19 QXEA9902273 1 19991028 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FRAME 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FRAME 531.5 HAS CORROSION ON AFT SIDE JUST OUTBOARD OF STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-489 AND DHC -8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900316 19991119 00316 NM 1999 11 19 QXEA9902274 1 19991028 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FRAME 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FRAME 545.00 HAS CORROSION ON FORWARD SIDE JUST OUTBOARD OF STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-486 AN D DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900317 19991119 00317 NM 1999 11 19 QXEA9902275 1 19991029 A 5310 STRUCTURE DHAV DHC8 DHC8102 2809003 NM FRAME 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - THERE IS CORROSION ON SKIN AND FRAME FORWARD OF 531.500 AT STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-489 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999111900318 19991119 00318 NM 1999 11 19 QXEA9902276 1 19991029 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FRAME 510 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FORWARD SIDE OF FRAME 510.00 HAS CORROSION AT OUTBOARD SIDE OF STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-490 . 2 H 7 2 4T RT A13NM 1999111900319 19991119 00319 NM 1999 11 19 QXEA9902277 1 19991018 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 510 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - THERE IS CORROSION AT THE TOP OF FRAME 510 BETWEEN FLOOR SUPPORT Y9.250 RIGHT AND FRAME. REPAIRED IAW PSM CHAPTER 4. 2 H 7 2 4T RT A13NM 1999111900320 19991119 00320 NM 1999 11 19 QXEA9902278 1 19991014 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 467-488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - STRINGER 31S IS CORRODED BETWEEN FRAME 467 AND 488.5. CLEANED AREA AND FOUND CRYSTALLIZED HARDCOAT. NO CORROSION FOUND. REAPPLIED HARDCOAT AS NECESSARY. 2 H 7 2 4T RT A13NM 1999111900321 19991119 00321 NM 1999 11 19 QXEA9902279 1 19991028 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FRAME 488.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FORWARD SIDE OF FRAME 488.5 IS CORRODED AT STRINGER 341S. REPAIRED IAW HORIZON AIR EA 9-53-487. 2 H 7 2 4T RT A13NM 1999111900322 19991119 00322 NM 1999 11 19 QXEA9902280 1 19991028 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FRAME 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FORWARD SIDE OF FRAME 467 HAS CORROSION AT STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-488. 2 H 7 2 4T RT A13NM 1999111900323 19991119 00323 NM 1999 11 19 QXEA9902281 1 19991018 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FRAME 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - FRAME 467 HAS CORROSION ALONG TOP OF FRAME BETWEEN FLOOR SUPPORT Y9.250R AND FRAME. REPAIRED IAW PSM CHAPTER PARA GRAPH 9B. 2 H 7 2 4T RT A13NM 1999111900324 19991119 00324 NM 1999 11 19 QXEA9902282 1 19991025 A 5320 SUPPORT DHAV DHC8 DHC8102 2809003 NM BS 9.25 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - THE VERTICAL FLOOR SUPPORT WEB AT Y9.250 RIGHT IS BUCKLED APPROXIMATELY .090 AT THE TOP JUST AFT OF X601 TO ABOUT X611. REPAIRED IAW HORIZON AIR EA 9-53-478. 2 H 7 2 4T RT A13NM 1999111900325 19991119 00325 NM 1999 11 19 QXEA9902283 1 19991020 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - AFT LOWER TCAS ANTENNA HAS CORROSION AROUND ANTENNA MOUNT HOLES UNDER DOUBLER. REPAIRED IAW DHC-8 SRM 53-00-16, P AGE 3, TABLE 1. 2 H 7 2 4T RT A13NM 1999111900326 19991119 00326 NM 1999 11 19 QXEA9902284 1 19991015 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 387 MISINSTALLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT OUTBOARD CABIN SEAT TRACK HAS FOUR IMPROPER AN TYPE BOLTS ATTACHING SEAT TRACK TO FUSELAGE FRAMES AT STATION 387.350 AND STATION 426.974. REPLACED BOLTS IAW IAC 53-41-00, FIGURE 10, ITEM 50. 2 H 7 2 4T RT A13NM 1999111900327 19991119 00327 NM 1999 11 19 QXEA9902285 1 19991013 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 333 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT OUTBOARD CABIN SEAT TRACK BETWEEN STATION 333.300 AND 387.350 HAS CORROSION ON TOP SURFACE AND INSIDE CHANNE L. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900328 19991119 00328 NM 1999 11 19 QXEA9902286 1 19991013 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 291.4 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT OUTBOARD CABIN SEAT TRACK AT STATION 291.400 HAS TOOL GOUGE MARKS ON TOP SURFACE. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900329 19991119 00329 NM 1999 11 19 QXEA9902287 1 19991013 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 265 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT OUTBOARD CABIN SEAT TRACK AT STATION 265.000 HAS CORROSION ON TOP SURFACE AND AROUND SEAT PEG HOLE. REPLACE D SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900330 19991119 00330 NM 1999 11 19 QXEA9902288 1 19991022 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 597 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK AT STATION 597.000 HAS CORROSION ON TOP SURFACE AROUND TIE DOWN PEG HOLES. REPAIRE D IAW DHC-8 SRM 51-40-00, TABLE 4. 2 H 7 2 4T RT A13NM 1999111900331 19991119 00331 NM 1999 11 19 QXEA9902289 1 19991013 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 545-597 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK BETWEEN STATION 545.000 AND 597.600 HAS CORROSION ON TOP SURFACE OF OUTBOARD FLANGE . REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900332 19991119 00332 NM 1999 11 19 QXEA9902290 1 19991013 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 510-545 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK BETWEEN STATION 510.000 AND 545.000 HAS GOUGE MARKS ON TOP SURFACE WITH CORROSION A ND INSIDE CHANNEL HAS CORROSION. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900333 19991119 00333 NM 1999 11 19 QXEA9902291 1 19991013 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 246-488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK BETWEEN STATION 426.974 AND 488.500 HAS CORROSION AND GOUGE MARKS ON TOP SURFACE AN D INSIDE CHANNEL. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900334 19991119 00334 NM 1999 11 19 QXEA9902292 1 19991010 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 387 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK AT STATION 387.350 HAS GOUGE MARKS ON TOP SURFACE WITH CORROSION TO INCLUDE INSIDE CHANNEL. REPLACED RIGHT FORWARD INBOARD SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900335 19991119 00335 NM 1999 11 19 QXEA9902293 1 19991010 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 312-370 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK BETWEEN STATION 312.360 AND 370.800 HAS CORROSION ON TOP SURFACE AND INSIDE CHANNEL . REPLACED RIGHT FORWARD INBOARD SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900336 19991119 00336 NM 1999 11 19 QXEA9902294 1 19991010 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 267-312 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 267.000 AND 312.360 HAS CORROSION ON TOP SURFACE AND INSID E CHANNEL. REPLACED RIGHT FORWARD INBOARD SEAT TRACK. 2 H 7 2 4T RT A13NM 1999111900337 19991119 00337 NM 1999 11 19 QXEA9902295 1 19991022 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 182.5-240.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT INBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 182.500 AND 240.500 HAS CORROSION ON TOP SURFACE AND AROUN D 4 SCREW HOLES. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999111900338 19991119 00338 NM 1999 11 19 QXEA9902300 1 19991031 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 597.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT INBOARD CABIN SEAT TRACK AT FUSELAGE STATION 597.500 HAS CORROSION ON TOP SURFACE. REPAIRED IAW DHC-8 SRM 51 -40-00. 2 H 7 2 4T RT A13NM 1999111900339 19991119 00339 NM 1999 11 19 QXEA9902301 1 19991007 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - CORROSION FOUND ON AIRCRAFT SKIN UNDER AFT DME ANTENNA. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 5, STEP 3, SRM 53-0 0-16, PAGE 3, TABLE 1, SHEET 2. 2 H 7 2 4T RT A13NM 1999111900340 19991119 00340 NM 1999 11 19 QXEA9902338 1 19991110 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 363PH 481 520 SEA - TWO EACH RED EMERGENCY EGRESS FLOOR LIGHTS INOP. REMOVED AND REPLACED BATTERY AND POWER SUPPLY. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999111900341 19991119 00341 NM 1999 11 19 99FDEA00465 1 19990927 A 5311 BELLFRAME BOEING 727 72722 1384002 NM BS 1050 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 NR 685 - DENTS IN UPPER FLANGE RADIUS OF BELLFRAME AT BS 1050 ABOVE STR 26L IN AFT CARGO. CUT OUT DAMAGED AND INSTALL F ILLER AND DOUBLER PER SRM 53-10-4 AND EA 7-5310-45407. 2 L 7 3 4F A3WE 1999111900342 19991119 00342 NM 1999 11 19 99FDEA00466 1 19990921 A 5341 CASTING BOEING 727 72722 1384002 NM BS 870 SCORED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 NR 999 - LT WING BS 870 FWD AND AFT BOTTLE PIN CASTINGS ARE SCORED, AFT CASTING HAS 2 PREVIOUSLY BLENDED (DISHED OUT) AR EAS (MARKED). REMOVED SCORING AND BLENDING. INSTALL TERMINAL PIN BUSHINGS IAW S/B 727-57-0175 NSC01, EA 7521045399 AND SRM 5240-1. 2 L 7 3 4F A3WE 1999111900343 19991119 00343 WP 1999 11 19 99FDEA00467 1 19990921 A 2910 AJK7004589 LINE DOUG DC10 DC1010 3022110 WP BS 1989 CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N 3478 - HYD LINE PN AJK7004-589 IS CRACKED AND LEAKING, LOCATED IN AFT PIT AT BS 1989 LT SIDE. REPAIRED HYD LINE IAW D C10 MM 20-10-01-2 AND DRS 3-80-10. 2 L 7 3 4F A22WE 1999111900344 19991119 00344 WP 1999 11 19 99FDEA00468 1 19990920 A 2910 LINE DOUG DC10 DC1010 3022110 WP NR 2 HYD SYS CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N3472 NR 2 HYD SYS RETURN LINE CRACKED. LOCATED IN AFT CARGO COMP RT SIDE AT SM 2.000. REPAIRED HYD LINE IAW DC10 MM 2 0-10-01-5 AND DPS 3.80-10. 2 L 7 3 4F A22WE 1999111900345 19991119 00345 WP 1999 11 19 99FDEA00469 1 19990922 A 2910 AFK7002541 LINE DOUG DC10 DC1010 3022110 WP BS 1720 CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N3483 - HYD LINE P/N AFK7002-541 IS CRACKED AND LEAKING LOCATED IN LT CTR CARGO TUNNEL AREA AT BS 1720. REPAIRED HYD LI NE IAW DC10 MM 20-10-01-2 AND DPS 3.80-10. 2 L 7 3 4F A22WE 1999111900346 19991119 00346 WP 1999 11 19 99FDEA00470 1 19991019 A 2910 APK7002536 LINE DOUG DC10 DC1010 3022110 WP LT MLG WW CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N3477 - HYD LINE PN APK7002-536 IS CRACKED AND LEAKING LOCATED IN LT WHEEL WELL, NR 3 SYS TO MLG. REPAIRED HYD LINE IAW DC10 MM 20-10-01-2 AND DPS 3.80-10. 2 L 7 3 4F A22WE 1999111900347 19991119 00347 WP 1999 11 19 99FDEA00471 1 19991109 A 2910 AJK70111 LINE DOUG DC10 DC1010 3022110 WP BS 1960 CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N3671 - HYD SYS NR 2 PRESSURE LINE PN AJK7011-1 CRACKED AND LEAKING LOCATED AT BS 1960 IN AFT CARGO TUNNEL AREA. REPAIR ED IAW DC10 MM 20-10-01-2 AND DPS 3.80-10. 2 L 7 3 4F A22WE 1999111900348 19991119 00348 WP 1999 11 19 99FDEA00472 1 19990921 A 2910 AGK7002513 LINE DOUG DC10 DC1010 3022110 WP BS 1721 CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N3481 - HYD LINE SYS 2 PN AGK7002-513 CRACKED AND LEAKING LOCATED AT BS 1721 LT SIDE. REPAIRED IAW DC10 MM 20-10-01-2 A ND 3.80-10. 2 L 7 3 4F A22WE 1999111900349 19991119 00349 WP 1999 11 19 99FDEA00473 1 19991108 A 2910 AGK7002514 LINE DOUG DC10 DC1010 3022110 WP BS 1995-2004 CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N3668 - SYS 2 HYD LEAK DETECT PRESSURE LINE, PN AGK7002-514, RUPTURED. LOCATED BETWEEN BS 1995 AND 2004 LT SIDE. REPAI RED IAW DC 10 MM 20-10-01-2 AND DPS 3.20-10. 2 L 7 3 4F A22WE 1999111900350 19991119 00350 WP 1999 11 19 99FDEA00474 1 19990923 A 2910 APK7002518 LINE DOUG DC10 DC1010 3022110 WP BS 1278 CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 N3489 - SYS NR 3 HYD LINE PN APK7002-518 IS CRACKED AND LEAKING LOCATED ON LT SIDE AT STA 1278 IN ACCESS AREA BETWEEN ML G W/W. REPAIRED IAW DC 10 MM 20-10-01-2 AND DPS 3.80-10. 2 L 7 3 4F A22WE 1999111900351 19991119 00351 WP 1999 11 19 99FDEA00475 1 19990921 A 2910 AGK7002565 LINE DOUG DC10 DC1010 3022110 WP BS 1995 CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 25 373FE 46611 HYD LINE P/N AGK7002-565, CRACKED AND LEAKING AT BS 1995 IN AFT WASTE COMP TUNNEL AREA ON LT SIDE. REPAIRED IAW DC10 MM 20-10-01-2 AND DPS 3.80-10. 2 L 7 3 4F A22WE 1999111900352 19991119 00352 NM 1999 11 19 99FDEA00476 1 19990920 A 5314 KEEL BEAM BOEING 727 72722 1384002 NM BS 954 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 NR 794 - KEEL BEAM LWR LT CHORD CRACKED IN RADIUS AT BS 954. STOP DRILLED CRACK AND INSTALL DOUBLER PER EA NR7-53104539 1 DATED 15 SEP 99. 2 L 7 3 4F A3WE 1999111900353 19991119 00353 NM 1999 11 19 99FDEA00477 1 19990921 A 5720 COVER BOEING 727 72722 1384002 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 NR 782 - RT WING RT STUB TANK PLATE LAND NEEDS RESIDUE REMOVED FWD SPAR ACCESS. CORROSION REMOVED AND REPLACED AREA PER EA NR 75710-45413 DATED 9-29-99 SEEN NR 782 AND JPF AREA ON REVERSE SIDE. 2 L 7 3 4F A3WE 1999111900354 19991119 00354 NM 1999 11 19 99FDEA00478 1 19990921 A 5320 SPLICE BOEING 727 72722 1384002 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 190FE 19083 NR 118 - UPPER LOBE BS 344 LBL 45- LBL 60 CORROSION AROUND FLOORBOARD ATTACH HOLES UPPER LEG OF FLOORBEAM. INSTALLED UP PER CHORD SPLICE PER DRAWING SR 27-53-007 PG 14. 2 L 7 3 4F A3WE 1999111900355 19991119 00355 NM 1999 11 19 99FDEA00479 1 19991111 A 5610 5893543110 WINDOW BOEING 727 727233 138408A NM RT COCKPIT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 NR 42 F/O'S R1 WINDOW CRACKED IN FLIGHT. *S/D* REMOVED AND REPLACED NR 1 F/O'S WINDOW IAW FEDEX MM 56-11-011-4. WINDO W HEAT CKS GOOD IAW FEDEX MM 30-41-002-5 STEP 3. 2 L 7 3 4F RT A3WE 1999111900356 19991119 00356 WP 1999 11 19 ABXA9900771 1 19991108 A 5230 99576645 INTERCOSTAL DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL WEB CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999111900357 19991119 00357 WP 1999 11 19 ABXA9900772 1 19991108 A 5521 99184443 RIB DOUG DOUG DC9 DC941 302207N WP LT ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND LEADING EDGE RIB CRACKED ON LEFT ELEVATOR. REPLACED RIB IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999111900358 19991119 00358 WP 1999 11 19 ABXA9900773 1 19991108 A 5230 3926046505 FITTING DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL TEE FITTING CRACKED AT LOWER AFT STOP. REPLACED TEE FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999111900359 19991119 00359 WP 1999 11 19 ABXA9900774 1 19991108 A 5530 591214129 ANGLE DOUG DOUG DC9 DC941 302207N WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND VERTICAL STABILIZER, LOWER LEFT ATTACH ANGLE CRACKED AT AFT END. REPAIRED IAW ABX REA D953-34140M R. 2 L 7 2 4F A6WE 1999111900360 19991119 00360 WP 1999 11 19 ABXA9900775 1 19991108 A 5230 591014167 PAN DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR OUTER PAN CRACKED. REPAIRED IAW DC9 SRM 52-03. 2 L 7 2 4F A6WE 1999111900361 19991119 00361 NE 1999 11 19 ABXA9900776 2 19991109 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 3 LOW POWER A ABXA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 23 801AX 46077 642913 DURING FUNCTIONAL CHECK FLIGHT (FCF), ON INITIAL LEVEL-OFF, WHEN POWER WAS REDUCED TO IDLE, NR 3 ENGINE N1 WAS LOWER TH AN OTHER ENGINES. WHEN THROTTLES WERE ADVANCED, NR 3 ENGINE DID NOT ACCELERATE. LOW OIL PRESSURE LIGHT ILLUMINATED. I NDICATED OIL PRESSURE WAS 33-35 PSI. ENGINE WAS SECURED. ENGINE WINDMILLED FOR 27 MIN WITH POSITIVE OIL PRESSURE. PER FORMED INSPECTION OF NR 3 ENGINE IAW PRATT AND WHITNEY JT3D MM 79-20-7. INSPECTED AND REPLACED MAIN OIL FILTER. NO DEF ECTS WERE NOTED. OPS CHECKED GOOD ON ENGINE RUN-UP. 2 L 7 4 4F 4 F 4A25 1E8 1999111900362 19991119 00362 WP 1999 11 19 ABXA9900777 1 19991108 A 5313 39132091 FITTING DOUG DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LONGERON END FITTING CRACKED AT LONGERON 27 RIGHT. REPLACED FITTING IAW DC9 51-30-2. 2 L 7 2 4F A6WE 1999111900363 19991119 00363 WP 1999 11 19 ABXA9900778 1 19991108 A 5280 59175331 PAN DOUG DOUG DC9 DC931 3022065 WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LEFT LANDING GEAR INBOARD DOOR PAN CRACKED. REPLACED DOOR PAN IAW DC9 SRM 51-30-8. 2 L 7 2 4F A6WE 1999111900364 19991119 00364 WP 1999 11 19 ABXA9900779 1 19991108 A 5220 59131951 PAN DOUG DOUG DC9 DC931 3022065 WP EMER EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LEFT FORWARD EMERGENCY EXIT PAN CRACKED. REPLACED DOOR ASSEMBLY. 2 L 7 2 4F A6WE 1999111900365 19991119 00365 WP 1999 11 19 ABXA9900780 1 19991108 A 5220 59131951 PAN DOUG DOUG DC9 DC931 3022065 WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LEFT AFT EMERGENCY EXIT DOOR PAN CRACKED. REPLACED DOOR ASSEMBLY. 2 L 7 2 4F A6WE 1999111900366 19991119 00366 WP 1999 11 19 ABXA9900781 1 19991108 A 5220 59131951 PAN DOUG DOUG DC9 DC931 3022065 WP EMER EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND RIGHT FORWARD OVERWING EXIT DOOR PAN CRACKED. REPLACED DOOR ASSEMBLY. 2 L 7 2 4F A6WE 1999111900367 19991119 00367 WP 1999 11 19 ABXA9900782 1 19991027 A 5753 591735425 ANGLE DOUG DOUG DC9 DC932F 3022067 WP LTTE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE FITTING INTERIOR ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30- 1 AND 51-30-2. 2 L 7 2 4F A6WE 1999111900368 19991119 00368 WP 1999 11 19 ABXA9900783 1 19991027 A 5400 995815958 STIFFNER DOUG DOUG DC9 DC932F 3022067 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND NR 1 PYLON INTERIOR WEB STIFFENER BETWEEN 8TH AND 13TH DUCT CRACKED AT END. REPLACED STIFFENER IA W DC9 SRM 54-10-0. 2 L 7 2 4F A6WE 1999111900369 19991119 00369 WP 1999 11 19 ABXA9900784 1 19991027 A 2720 5616068501 BRACKET DOUG DOUG DC9 DC932F 3022067 WP COCKPIT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND FORWARD, INBOARD FOOT OF THE RUDDER PEDAL ASSEMBLY ATTACH BRACKET CORRODED. REPLACED BRACKET ASSE MBLY IAW DC9 MM 20-16-0. 2 L 7 2 4F A6WE 1999111900370 19991119 00370 WP 1999 11 19 ABXA9900785 1 19991028 A 5230 9957664513 INTERCOSTAL DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INTERNAL INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999111900371 19991119 00371 WP 1999 11 19 ABXA9900786 1 19991008 A 5312 5910163108 BULKHEAD CLIP DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 AFT PRESSURE BULKHEAD RADIAL STIFFENER 16 LEFT ATTACH CLIP CRACKED ADJACENT TO LONGERON 18 LEFT. REPLACED CLIP IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999111900372 19991119 00372 WP 1999 11 19 MWEA99794 1 19991111 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY SERV DOOR DISLODGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 GALLEY SERVICE DOOR EVACUATION SLIDE COVER WAS KNOCKED OFF. MAINTENANCE RE-INSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999111900373 19991119 00373 WP 1999 11 19 MWEA99795 1 19991111 A 5311 99118435 FRAME DOUG DC9 DC932 3022066 WP AFT FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FRAME AT TAILCONE MATING SURFACE ON FUSELAGE IS CHAFED. MAINTENANCE FITTED AND INSTALLED NEW -5 AND -6 FRAMES. 2 L 7 2 4F A6WE 1999111900374 19991119 00374 WP 1999 11 19 MWEA99796 1 19991111 A 5241 9911577 BRACKET DOUG DC9 DC932 3022066 WP GALLEY DOOR BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 GALLEY DOOR GRAB HANDLE ATTACH BRACKET IS BROKEN. MAINTENANCE FITTED AND INSTALLED NEW ATTACH BRACKET. 2 L 7 2 4F A6WE 1999111900375 19991119 00375 WP 1999 11 19 MWEA99797 1 19991111 A 5313 527779221 LONGERON DOUG DC9 DC932 3022066 WP BS 718 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LONGERON 3 LEFT AT STATION 718 IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED LONGERON REPAIR. 2 L 7 2 4F A6WE 1999111900376 19991119 00376 WP 1999 11 19 MWEA99798 1 19991111 A 5312 5910130307 CHANNEL DOUG DC9 DC932 3022066 WP AFT PRESS BKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 VENTRAL DOOR CHANNEL RIGHT UPPER CORNER FOUND CRACKED. MAINTENANCE FITTED AND INSTALLED NEW CHANNEL. 2 L 7 2 4F A6WE 1999111900377 19991119 00377 WP 1999 11 19 MWEA99799 1 19991111 A 5347 2914913 SEAT TRACK DOUG DC9 DC932 3022066 WP LT COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 PILOTS AFT OUTBARD SEAT TRACK WORN BEYOND LIMITS. MAINTENANCE FITTED AND INSTALLED NEW SEAT TRACK. 2 L 7 2 4F A6WE 1999111900378 19991119 00378 WP 1999 11 19 MWEA99800 1 19991111 A 5320 3913577404 INSTERCOSTAL DOUG DC9 DC932 3022066 WP BS 465 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 INTERCOSTAL BENEATH FLOORBOARDS AT STATION 465 AFT ATTACH POINT IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED INTERC OSTAL REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999111900379 19991119 00379 WP 1999 11 19 MWEA99801 1 19991111 A 5312 5910130232 BLKHD DOUBLER DOUG DC9 DC932 3022066 WP AFT PRESS BKHD MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 602ME 48133 FINGER DOUBLER ON RIGHT SIDE OF AFT PRESSURE BULKHEAD, HALF WAY UP VENTRAL DOOR OPENING DAMAGED DURING PREVIOUS REPAIR. MAINTENANCE FITTED AND INSTALLED NEW FINGER DOUBLER. 2 L 7 2 4F A6WE 1999111900380 19991119 00380 WP 1999 11 19 MWEA99802 1 19991111 A 5320 99100875 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 1157 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 INTERCOSTAL AT STATION 1157 AND AFT CANTED FRAME HAS A CRACK IN THE BEND RADIUS. MAINTENANCE FABRICATED AND INSTALLED I NTERCOSTAL REPAIR. 2 L 7 2 4F A6WE 1999111900381 19991119 00381 WP 1999 11 19 MWEA99803 1 19991111 A 5320 49128191 FITTING DOUG DC9 DC932 3022066 WP BS 427 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FORWARD CARGO COMPARTMENT AFT CARGO DOOR JAMB STRUT FITTING, LOWER, IS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW FI TTING. 2 L 7 2 4F A6WE 1999111900382 19991119 00382 WP 1999 11 19 MWEA99804 1 19991111 A 5320 9957710 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 917 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 INTERCOSTAL AT STATION 917, FUSELAGE CENTERLINE IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL REPAIR. 2 L 7 2 4F A6WE 1999111900383 19991119 00383 WP 1999 11 19 MWEA99805 1 19991111 A 3350 6011779 BATTERY PACK DOUG DC9 DC915 3022036 WP CARGO COMPT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 900ME 45841 RIGHT OVERWING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING TEST. MAINTENANCE CHARGED EMERGENCY EXIT LIGHT BATTERY P ACK. 2 L 7 2 4F A6WE 1999111900384 19991119 00384 WP 1999 11 19 MWEA99806 1 19991112 A 5320 992948017 ANGLE DOUG DC9 DC932 3022066 WP VENTRAL DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 AFT VENTRAL DOOR LOWER BEAM ANGLE RIGHT SIDE IS CRACKED IN RADIUS. MAINTENANCE FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 1999111900385 19991119 00385 WP 1999 11 19 MWEA99807 1 19991112 A 5320 59174637 FRAME DOUG DC9 DC932 3022066 WP VENTRAL DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT SIDE OF AFT VENTRAL DOOR JAMB FRAME IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOOR JAMB FRAME DOUBLER REPA IR. 2 L 7 2 4F A6WE 1999111900386 19991119 00386 WP 1999 11 19 MWEA99808 1 19991112 A 5330 5910228 SKIN DOUG DC9 DC932 3022066 WP BS 1163 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FUSEALGE SKIN IS CRACKED, LEFT SIDE, AFT OF EMERGENCY EXIT PULL HANDLE AT STATION 1163. MAINTENANCE FABRICATED AND INST ALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999111900387 19991119 00387 WP 1999 11 19 MWEA99809 1 19991112 A 5320 59175795 WEB DOUG DC9 DC932 3022066 WP VENTRAL DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT UPPER VENTRAL DOOR FRAME WEB HAS CRACKS AT FORWARD EDGE. MAINTENANCE FABRICATED AND INSTALLED WEB REPAIR. 2 L 7 2 4F A6WE 1999111900388 19991119 00388 NM 1999 11 19 SCNA99136 1 19991111 A 3350 90054 BATTERY CHARGER BOEING 727 727225 1384077 NM CARGO DOORWAY INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECK, THE AFT CARGO DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED T HE BATTERY PACK CHARGER. OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999111900389 19991119 00389 EA 1999 11 19 SWIA971588 1 19991031 A 7603 POWER LEVER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTIONED A SWIA E ENGINE SHUTDOWN F FLT CONT AFFECTED DE DESCENT 1 NM 07 411SW 7067 LEFT ENGINE POWER LEVER UNABLE TO RETARD TO IDLE OR CUT OFF. SHUT LEFT ENG DOWN USING LEFT FIRE PUSH BUTTON. LANDED AT SLC UNEVENTFUL. N1 STUCK AT 90 DEGREES. REMOVED AND REPLACED LEFT ENGINE GEAR BOX ASSY FOR POWER THROTTLE LEVER PER M M 76-11-17. PERFORMED ENGINE ASSURANCE RUNS PER MM 71-00-00. OPS CHECKS OF THROTTLE LINKAGE GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900390 19991119 00390 SO 1999 11 19 SWIA971589 1 19991031 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 576SW 120345 THE CARGO DOOR LIGHT CAME ON DURING FLIGHT. RETURNED TO LAX. ADJUSTED CARGO DOOR MICROSWITCH ROCKER ARM TONGUE IAW 52- 72-02. OPS CHECKS GOOD. RESET CARGO DOOR WARNING CB. 2 L 7 2 4T 4 T RT A31SO E20NE 1999111900391 19991119 00391 SO 1999 11 19 SWIA971590 1 19991101 A 5270 SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE FUEL DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 137H 120137 SERVICE DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO PDX. ADJUSTED SINGLE POINT REFUELING DOOR MICROSWITCH AS NEC ESSARY. LIGHT OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999111900392 19991119 00392 NE 1999 11 19 SWIA971591 2 19991103 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 2 LOW POWER A SWIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 07 403SW 7028 CLIMBING THROUGH 33,000 N2 VIB WARNING ON N2 GAUGE ILLUMINATED (NR 2 ENGINE). REDUCED POWER UNTIL VIB WARNING CLEARED ( 84 PERCENT N1). DESCENDED TO 27,000 TO MAINTAIN FLYABLE AIRSPEED. ADVANCED NR 2 ENGINE POWER AND VIB WARNING CAME ON AG AIN AT 80 PERCENT N1. REDUCED POWER, VIB LIGHT EXTINGUISHED AT 78 PERCENT N1. RETURNED TO SLC. PERFORMED INTERNAL ENG INE WASH ON RIGHT ENGINE IAW GE MM TASK 72-00-00 -170-001. ENGINE RESTORED TO NORMAL. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900393 19991119 00393 EA 1999 11 19 SWIA971592 1 19991107 A 3010 DE-ICE SYS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT WING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 ANTI-ICE DUCT MESSAGE WITH -A/I+ ON LEFT WING LEADING EDGE RED ON ANTI-ICE SYNOPTIC PAGE. RETURNED TO SLC. LEFT WING SU FFICIENT OVERHEAT SENSOR CHANGED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999111900394 19991119 00394 NM 1999 11 19 VNAA9911007 1 19991110 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7A DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 434JS 8580 1534 3051 THE FLIGHT CREW FOUND THE EMERGENCY LIGHT AT SEAT 7A DID NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BAT TERY AT THE L03 POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111900395 19991119 00395 EU 1999 11 19 RAIA9910042 1 19991014 A 3010 14155090404 DE- ICE SYS JETAIR JETSTM JETSTM4101 1500501 EU RT WING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 550HK 41039 6128 - BWI - FAULT LIGHT ILLUMINATED ON DE-ICE SYSTEM - CCT1. MAINTENANCE REPLACED RIGHT HORIZONTAL STAB LEADING EDGE. 2 L 7 2 4T RT A41NM 1999111900396 19991119 00396 EU 1999 11 19 RAIA9910043 1 19991015 A 3320 EO33601 SOCKET AEROSP ATR72 ATR72202 8680940 EU ROW 5AB FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 03 722TE 220 732 4- STL - FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL NEAR SEAT 7A/B. MAINTENANCE REPLACED LIGHT SOCKET AT SEAT 5A/B. 2 H 7 2 4T RT A53EU 1999111900397 19991119 00397 EU 1999 11 19 RAIA9910044 1 19991016 A 3010 3D354701 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU AIRFRAME FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 563HK 41079 7492 - ST L- AUTO CYCLE FOR AIRFRAME DE-ICE FAULTING ON CCT3. MAINTENANCE REPLACED DE-ICE PRESS SWITCH. 2 L 7 2 4T RT A41NM 1999111900398 19991119 00398 1999 11 19 RAIA9910045 4 19991019 A 3452 96072107 COMM UNIT JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 568HK 41086 6190 - PIT - BOTH RMU'S GIVING AN ATC NR 2 WARNING. MAINTENANCE REPLACED NR 2 COMM UNIT. 2 L 7 2 4T RT A41NM 1999111900399 19991119 00399 EU 1999 11 19 RAIA9910046 1 19991019 A 3610 832491226 0-RING JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 555HK 41072 6129 - ORF - LET FLOW AT SETTING NR 5 GETS DUCT FAIL LIGHT. MAINTENANCE REPLACED GAMMA DUCT O-RING ON LEFT SIDE. 2 L 7 2 4T RT A41NM 1999111900400 19991119 00400 SO 1999 11 19 RAIA9910047 1 19991020 A 7830 XD4N RELAY EMB 145 EMB145 SO RT TR UNIT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 801HK 145053 5797 - TRI-ENGINE NR 22 REV DISAGREE LIGHT ON. MAINTENANCE REPLACED D22 RELAY FOR RIGHT THRUST REVERSER. 2 L 7 2 4F RT T00011AT 1999111900401 19991119 00401 EU 1999 11 19 RAIA9910048 1 19991023 A 3320 8ES0055800 TRANSFORMER AEROSP ATR72 ATR72202 8680940 EU ROW 4CD FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 03 723TE 283 7327 - BMI - STRONG ODOR IN AIRCRAFT. MAINTENANCE REPLACED TRANSFORMER FOR LIGHT AT SEAT 4C/D. 2 H 7 2 4T RT A53EU 1999111900402 19991119 00402 SO 1999 11 19 RAIA9910049 1 19991024 A 7830 XD4N RELAY EMB 145 EMB145 SO NR 2 TR UNIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 801HK 145053 5785 - SBN - NR 2 THRUST REVERSER DISAGREE. MAINTENANCE REPLACED T/R RELAY NR D23. 2 L 7 2 4F RT T00011AT 1999111900403 19991119 00403 EU 1999 11 19 RAIA9910050 1 19991028 A 2160 7252C000 VALVE BAG JETSTM JETSTM3201 1500217 EU NR 1 TEMP CONTL FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 973JX 973 4756 - FAT- NR 1 OVERTEMP CAP ILLUMINATED, STAYS ON UNTIL FLOW WAS TURNED OFF. MAINTENANCE REPLACED NR 1 TEMP CONTROL V ALVE. 2 L 7 2 4T RT A56EU 1999111900404 19991119 00404 EU 1999 11 19 RAIA9910051 1 19991031 A 2844 1103P0645 SWITCH BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 422AM 856 7318 - STL - RIGHT FUEL CAP ILLUMINATED. MAINTENANCE REPLACED RIGHT FUEL LOW PRESS SWITCH. 2 L 7 2 4T RT A56EU 1999111900405 19991119 00405 1999 11 19 RAIA9911013 2 19991110 A 7320 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 432AM 883 9431 - STL - LEFT TTL SYSTEM TEST FAILED. MAINTENANCE REPLACEDTOQUE LIMITING BYPASS VALVE FOR LEFT ENGINE. 2 L 7 2 4T RT A56EU 1999111900406 19991119 00406 NM 1999 11 19 SWAA991836 1 19991102 A 2560 D31591 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOORWAY DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 367SW 26578 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900407 19991119 00407 NM 1999 11 19 SWAA991837 1 19991102 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 EEPLS INOP ON MID CABIN. RECONNECTED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999111900408 19991119 00408 NM 1999 11 19 SWAA991838 1 19991102 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 14 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361SW 26572 EEPLS INOP AND COVER MISSING AT ROW 14. RELAMPED AND REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999111900409 19991119 00409 NM 1999 11 19 SWAA991839 1 19991102 A 2560 D31354 SLIDE BOEING 737 7375H4 138449D NM PAX DOORWAY DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 FWD ENTRY DOOR EVACUATON SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900410 19991119 00410 NM 1999 11 19 SWAA991840 1 19991102 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND CRACKED FUSELAGE FRAME, BS 440, WL 166 AND WL 170. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999111900411 19991119 00411 NM 1999 11 19 SWAA991841 1 19991101 A 5312 963820 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 RT SIDE CHORD CRACKED AT STA 178, RBL 26. REMOVED AND REPLACED CHORD SECTION PER SRM. 2 L 7 2 4F A16WE 1999111900412 19991119 00412 NM 1999 11 19 SWAA991842 1 19991102 A 5754 6573714 SKIN BOEING 737 7375H4 138449D NM NR 2 LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 1999111900413 19991119 00413 NM 1999 11 19 SWAA991843 1 19991102 A 5320 6552988 SPLICE BOEING 737 7372H4 138448C NM BS 910 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER SPLICE 23R, BS 910. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F A16WE 1999111900414 19991119 00414 NM 1999 11 19 SWAA991844 1 19991103 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOORWAY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 656SW 28401 AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900415 19991119 00415 NM 1999 11 19 SWAA991845 1 19991103 A 3350 P4010021 BATTERY BOEING 737 7373L9 1384470 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 658SW 23332 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999111900416 19991119 00416 NM 1999 11 19 SWAA991846 1 19991103 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM RT EMER EXIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND CHARGER P ER MM. 2 L 7 2 4F A16WE 1999111900417 19991119 00417 NM 1999 11 19 SWAA991847 1 19991103 A 5753 6547901 TRACK BOEING 737 7372H4 138448C NM RT TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND RT OUTBOARD AFT FLAP INBOARD CENTER AND OUTBOARD TRACKS CORRODED. REMOVED AND REPLACED TRACKS PER OHM. 2 L 7 2 4F A16WE 1999111900418 19991119 00418 NM 1999 11 19 SWAA991848 1 19991103 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 869-876 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND EXTERNAL FUSELAGE SKIN CREASED FROM BS 869 TO BS 876, BETWEEN STRINGERS 24R-25R. REPAIR ED SKIN PER SRM. 2 L 7 2 4F A16WE 1999111900419 19991119 00419 NM 1999 11 19 SWAA991849 1 19991103 A 5330 6545769 SKIN BOEING 737 7373Q8 1384670 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 312, BETWEEN STRINGERS 25L-26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999111900420 19991119 00420 NM 1999 11 19 SWAA991824 1 19991030 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM ROW 10 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610WN 27696 EEPLS MISSING TRACK COVER AT ROW 10. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999111900421 19991119 00421 NM 1999 11 19 SWAA991825 1 19991030 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CARGO COMPT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND LT OUTER OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F A16WE 1999111900422 19991119 00422 NM 1999 11 19 SWAA991826 1 19991030 A 5753 6546435235 SKIN BOEING 737 7372H4 138448C NM LT TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND LT OUTBOARD AFT FLAP DELAMINATED IN SEVERAL AREAS. REMOVED AND REPLACED FLAP ASSY PER MM. 2 L 7 2 4F A16WE 1999111900423 19991119 00423 NM 1999 11 19 SWAA991827 1 19991030 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 18. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999111900424 19991119 00424 NM 1999 11 19 SWAA991828 1 19991031 A 3350 BR2013 LGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 EEPLS INOP NEAR OVERWING DOOR. REPAIRED WIRING AND RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999111900425 19991119 00425 NM 1999 11 19 SWAA991829 1 19991031 A 2560 D31354 SLIDE BOEING 737 7377H4 NM PAX DOORWAY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 709SW 27843 FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY SAGGING. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900426 19991119 00426 NM 1999 11 19 SWAA991830 1 19991101 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 094SW 23053 AIR TURNBACK, BIRD STRIKE DURING TAKEOFF ABOVE CAPT'S L-1 WINDOW. C/W BIRD STRIKE INSPECTION PER MM. NO DAMAGE NOTED. 2 L 7 2 4F A16WE 1999111900427 19991119 00427 NM 1999 11 19 SWAA991831 1 19991031 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AFT OF OVERWING DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999111900428 19991119 00428 NM 1999 11 19 SWAA991832 1 19991031 A 3350 D31354 SLIDE BOEING 737 7372H4 138448C NM PAX DOORWAY OUT OF POSITION A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PE R MM. 2 L 7 2 4F A16WE 1999111900429 19991119 00429 NM 1999 11 19 SWAA991833 1 19991031 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 18-20 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 18-20. RECONNECTED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999111900430 19991119 00430 NE 1999 11 19 SWAA991834 2 19991101 A 7230 COMPRESSOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SW 07 628SW 27703 858348 AIR TURNBACK, MULTIPLE BIRD STRIKES DURING TAKEOFF. PERFORMED BIRD STRIKE INSPECTION ON AIRFRAME. NO DEFECT NOTED. LA TER DISCOVERED 3 EA NR 1 ENG FAN BLADES BENT. REMOVED AND REPLACED FAN BENT FAN BLADES AND PERFORMED BORESCOPE INSPECT ION ON BOTH ENGS. NO OTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900431 19991119 00431 NM 1999 11 19 SWAA991835 1 19991101 A 3150 TO WARNING BOEING 737 7373H4 1384600 NM COCKPIT SOUNDED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING IN INSP/MAINT 1 SW 07 373SW 26581 ABORTED TAKEOFF, UPON ADVANCING THROTTLES FOR TAKEOFF WARNING HORN SOUNDED. (FLAPS AND SPEEDBRAKED CORRECTLY SET). INS PECTED AND OPERATED TAKEOFF WARNING SYSTEM. NO DEFECTS NOTED LATER ON PERFORMED TAKEOFF WARNING TEST PER MM. NO DEFECT S NOTED. 2 L 7 2 4F RT A16WE 1999111900432 19991119 00432 NM 1999 11 19 SWAA991812 1 19991028 A 3350 07912 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 1999111900433 19991119 00433 NM 1999 11 19 SWAA991813 1 19991028 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED C3 CHECK, FOUND EEPLS SECTION LOOSE ON AFT END. REINSTALLED LIGHT SECTION PER MM. 2 L 7 2 4F A16WE 1999111900434 19991119 00434 NM 1999 11 19 SWAA991814 1 19991028 A 5753 654643089 SKIN BOEING 737 7372H4 138448C NM LT TE FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED 1/4D CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP ASSY PER MM. 2 L 7 2 4F A16WE 1999111900435 19991119 00435 NM 1999 11 19 SWAA991815 1 19991028 A 3220 6580005113 DRAG BRACE BOEING 737 7372H4 138448C NM NLG CRACKED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 102SW 23108 AIR TURNBACK, UPON GEAR RETRACTION FELT AND HEARD A LOUD BANG BELOW RUDDER PEDALS, FOLLOWED BY A VIBRATION WHICH INCREAS ED AS AIRSPEED WENT UP. FOUND NLG DRAG BRACE CRACKED ON UPPER LT SIDE WHERE NLG DOOR ACTUATING ARM CONNECTS. REMOVED A ND REPLACED DRAG BRACE ASSY PER MM. 2 L 7 2 4F A16WE 1999111900436 19991119 00436 NM 1999 11 19 SWAA991816 1 19991030 A 3350 6113211 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 EEPLS INOP ON FWD END. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999111900437 19991119 00437 1999 11 19 SWAA991817 4 19991029 A 2565 1061323468 SLIDE BOEING 737 7373T5 NM PAX DOORWAY DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 FWD ENTRY DOOR EVACUATION SLIDE INADVENTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900438 19991119 00438 NM 1999 11 19 SWAA991818 1 19991029 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS TRACK COVER LOOSE BY OVERWING EXIT. REINSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 1999111900439 19991119 00439 NM 1999 11 19 SWAA991819 1 19991029 A 5523 183A81004 BUSHING BOEING 737 7377H4 NM RT ELEVATOR FAILED A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 07 700GS 27835 AIRCRAFT VIBRATION AT 295 KNOTS AND ABOVE DURING LEVEL FLIGHT AND NO BANKS. REMOVED AND REPLACED RT ELEVATOR TAB ASSY A ND HINGE ATTACH FITTING BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 1999111900440 19991119 00440 NM 1999 11 19 SWAA991820 1 19991029 A 5311 6516323 FRAME BOEING 737 7372H4 138448C NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D CHECK, FOUND BS 348 FRAME CRACKED, LBL 64, WL 208. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999111900441 19991119 00441 NM 1999 11 19 SWAA991821 1 19991029 A 3350 65C27075 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND SERVICE DOORS EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999111900442 19991119 00442 NM 1999 11 19 SWAA991822 1 19991029 A 3350 10885 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED RON CHECK, FOUND EEPLS FWD AND AFT SECTIONS INOP. REMOVED AND REPLACED BATTERY PACKS AND CHARGERS PER MM. 2 L 7 2 4F RT A16WE 1999111900443 19991119 00443 NM 1999 11 19 SWAA991823 1 19991030 A 2751 1817381 TRANSMITTER BOEING 737 7373Q8 1384670 NM RT TE FLAP ERRATIC A SWAA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 688SW 23254 AIR TURNBACK, AFTER TAKEOFF T/E FLAPS WOULD NOT FULLY RETRACT. REPAIRED WIRE AT 5C ON FLAP ASYMMETRY SWITCH. REMOVED A ND REPLACED FLAP POSITION INDICATOR. REMOVED AND REPLACED R123 RELAY AND REMOVED AND REPLACED RT FLAP TRANSMITTER PER M M. 2 L 7 2 4F RT A16WE 1999111900444 19991119 00444 NM 1999 11 19 SWAA991850 1 19991104 A 3350 P207001 FLASHLIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999111900445 19991119 00445 NM 1999 11 19 SWAA991851 1 19991104 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOORWAY DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED RON, FOUND FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900446 19991119 00446 NM 1999 11 19 SWAA991852 1 19991104 A 3350 07912 LIGHT BOEING 737 7373H4 1384600 NM ROW 13 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 631SW 27706 EEPLS TRACK LOOSE AT ROW 13. SECURED FLOOR TRACK PER MM. 2 L 7 2 4F RT A16WE 1999111900447 19991119 00447 NM 1999 11 19 SWAA991853 1 19991104 A 3350 65C27095 BATTERY BOEING 737 7372H4 138448C NM SERVICE DOORWAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999111900448 19991119 00448 NM 1999 11 19 SWAA991854 1 19991104 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 1006-1012 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON STRINGER 27L, BS 1006-1012. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999111900449 19991119 00449 NM 1999 11 19 SWAA991855 1 19991104 A 3350 100031 LIGHT BOEING 737 7372H4 138448C NM CABIN. LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND AFT CABIN EMERGENCY EXIT LIGHT LOSSE. TIGHTENED LOWER SCREWS PER MM. 2 L 7 2 4F A16WE 1999111900450 19991119 00450 NM 1999 11 19 SWAA991856 1 19991104 A 5312 6516300 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, LBL 10. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999111900451 19991119 00451 NM 1999 11 19 SWAA991857 1 19991104 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 26R CORRODED, BS 1006-1016. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 1999111900452 19991119 00452 NM 1999 11 19 SWAA991858 1 19991104 A 5313 6552988 STRINGER BOEING 737 7375H4 138449D NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED D CHECK, FOUND STRINGER 4R CRACKED, BS 907. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 1999111900453 19991119 00453 NM 1999 11 19 SWAA991859 1 19991104 A 2560 BR2013 SLIDE BOEING 737 7375H4 138449D NM PAX DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT DRAGGING ON THRESHOLD AND PRESS INDICATOR WINDOW L OOSE. REINSTALLED SLIDE AND WINDOW ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999111900454 19991119 00454 NM 1999 11 19 SWAA991865 1 19991105 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS LOOSE. TIGHTENED AND SECURED BRAKETS PER MM. 2 L 7 2 4F RT A16WE 1999111900455 19991119 00455 NM 1999 11 19 SWAA991866 1 19991105 A 5320 6516323 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR TIE, BS 360, STRINGER 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F A16WE 1999111900456 19991119 00456 NE 1999 11 19 SWAA991867 2 19991104 A 7200 CFM563 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 POWER LOSS A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 603SW 27954 ABORTED TAKEOFF, UNABLE TO ATTAIN TAKEOFF POWER AT 90 KNOTS ON NR 1 ENG. PERFORMED ENG RUN. OPS CK GOOD IN ALL PARAMET ERS PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900457 19991119 00457 1999 11 19 SWAA991868 2 19991106 A 7532 3214552 BLEED VALVE BOEING 737 7373H4 1384600 NM NR 2 ENGINE MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 395SW 27689 AIR TURNBACK, ACFT WOULD NOT MAINTAIN CABIN PRESS AT 27,000 FEET. C/W PRESS DECAY CHECK AND FOUND NR 2 ENG PNEU BLEED P RESS LOW AT IDLE, UNLOCKED NR 2 ENG HIGH STAGE PRESS BLEED VALVE AND OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999111900458 19991119 00458 NE 1999 11 19 SWAA991869 2 19991106 A 7321 8063208 MEC BOEING 737 7375H4 138449D NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE ERRATIC A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 526SW 26568 856175 AIR TURNBACK, IN FLIGHT SHUT DOWN, NR 2 ENG WOULD NOT GET OUT OF FULL POWER. REMOVED AND REPLACED NR 2 ENG T2 AND T12 S ENSORS AND REMOVED AND REPLACED NR 2 ENG MEC PER MM.. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900459 19991119 00459 NE 1999 11 19 SWAA991870 2 19991106 A 7230 COMPRESSOR BOEING 737 7375H4 138449D NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE STALLED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 520SW 25319 857632 AIR TURNBACK, IN FLIGHT SHUT DOWN, NR 1 ENG COMPRESSOR STALLED AT 27,000 FEET AND THEN AGAIN AT 16,000 FEET FOLLOWED BY OIL PRESS IND DECREASE AND ENG VIBRATION. REMOVED AND REPLACED NR 1 ENG PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900460 19991119 00460 NM 1999 11 19 SWAA991860 1 19991106 A 2560 65C16820 GIRT BOEING 737 7377H4 NM EMER EXIT OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 742SW 29278 DURING SCHEDULED SERVICE CHECK, FOUND ALL FOUR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASS Y'S PER MM. 2 L 7 2 4F RT A16WE 1999111900461 19991119 00461 NM 1999 11 19 SWAA991861 1 19991106 A 2560 65C16820 GIRT BOEING 737 7377H4 NM EMER EXIT OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 703SW 27837 DURING SCHEDULED SERVICE CHECK, FOUND ALL FOUR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASS Y'S PER MM. 2 L 7 2 4F RT A16WE 1999111900462 19991119 00462 NM 1999 11 19 SWAA991862 1 19991106 A 2560 65C16820 GIRT BOEING 737 7373H4 1384600 NM PAX DOORWAY OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 628SW 27703 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. A DJUSTED SLIDE ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999111900463 19991119 00463 NM 1999 11 19 SWAA991863 1 19991106 A 2560 65C16820 GIRT BOEING 737 7373H4 1384600 NM DOORS OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. A DJUSTED SLIDE ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999111900464 19991119 00464 NM 1999 11 19 SWAA991864 1 19991106 A 2560 65C16820 GIRT BOEING 737 7373H4 1384600 NM FWD SRVCE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 384SW 26590 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900465 19991119 00465 NM 1999 11 19 SWAA991871 1 19991108 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOORWAY DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900466 19991119 00466 NM 1999 11 19 SWAA991872 1 19991108 A 5330 6545773 SKIN BOEING 737 7373H4 1384600 NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED APPROX BS 807, STRINGER 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999111900467 19991119 00467 NM 1999 11 19 SWAA991873 1 19991107 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SRVCE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLI DE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900468 19991119 00468 NM 1999 11 19 SWAA991874 1 19991107 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED SERVICE CHECK, FOUND LAST FOUR EEPLS INOP. REMOVED AND REPLACED TRACK LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900469 19991119 00469 1999 11 19 SWAA991875 4 19991107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD SRVCE DOOR OUT OF POSITI0N A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 617SW 27700 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVCUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLID E ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900470 19991119 00470 NM 1999 11 19 SWAA991876 1 19991107 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 5. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999111900471 19991119 00471 NM 1999 11 19 SWAA991877 1 19991107 A 2560 D31354 SLIDE BOEING 737 7373Q8 1384670 NM SRVCE DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 23401 DURING SCHEDULED SERVICE CHECK, FOUND BOTH SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED BOTH SLIDES PER MM. 2 L 7 2 4F RT A16WE 1999111900472 19991119 00472 NM 1999 11 19 SWAA991878 1 19991107 A 2560 D31354 SLIDE BOEING 737 7377H4 NM PAX DOORWAY SAGGING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 741SA 29277 DURING SCHEDULED SERVICE CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED BO TH SLIDES PER MM. 2 L 7 2 4F RT A16WE 1999111900473 19991119 00473 NM 1999 11 19 SWAA991879 1 19991107 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 510SW 24187 EEPLS FWD END LOOSE. REINSTALLED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999111900474 19991119 00474 1999 11 19 SWAA991889 4 19991111 A 3417 LINE BOEING 737 7373G7 1384595 NM AIR DATA COMP LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 684WN 23941 AIR TURNBACK, AFTER TAKEOFF, LOST AIRSPEED, ALTITUDE INDICATIONS. WARNING HORN WENT OFF. FOUND LINE TO AIR DATA COMPUT ER LOOSE. REINSTALLED LINE PER MM. 2 L 7 2 4F RT A16WE 1999111900475 19991119 00475 NM 1999 11 19 SWAA991890 1 19991111 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 12 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 EEPLS INOP AT ROW 12. RECONNECTED WIRES AND OPS CHECKED GOOD. LATER ON AT PHX, REMOVED AND REPLACED TRACK COVER PER MM . 2 L 7 2 4F RT A16WE 1999111900476 19991119 00476 NM 1999 11 19 SWAA991891 1 19991111 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOORWAY LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 FWD ENTRY DOOR EVACUATION SLIDE LOOSE INSIDE COVER. REINSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999111900477 19991119 00477 NM 1999 11 19 SWAA991892 1 19991111 A 3350 07912 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 615SW 27698 EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999111900478 19991119 00478 NM 1999 11 19 SWAA991893 1 19991110 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOORWAY OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY/SERVICE AND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999111900479 19991119 00479 NM 1999 11 19 SWAA991894 1 19991110 A 2560 D31354 SLIDE BOEING 737 7373H4 1384600 NM DOORS OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED SERVICE CHECK, FOUND BOTH SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999111900480 19991119 00480 NM 1999 11 19 SWAA991895 1 19991110 A 5315 6546804 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM BS 312, LBL 1- RBL 21. REPAIRED BEAM PER TYPICAL REPAIR NR TI -353-007. 2 L 7 2 4F RT A16WE 1999111900481 19991119 00481 NM 1999 11 19 SWAA991896 1 19991110 A 5320 6545409 WEB BOEING 737 7373Y0 1384671 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED 1/2D CHECK, FOUND PRESS WEB CRACKED, BS 663, LBL 32. REPAIRED WEB PER TI-353-046. 2 L 7 2 4F RT A16WE 1999111900482 19991119 00482 NM 1999 11 19 SWAA991897 1 19991110 A 2560 D31354 SLIDES BOEING 737 7375H4 138449D NM PAX DOORWAY OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND BOTH ENTRY DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SL IDE ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999111900483 19991119 00483 NM 1999 11 19 SWAA991880 1 19991109 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 3 EACH MOST FWD EEPLS LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999111900484 19991119 00484 NM 1999 11 19 SWAA991881 1 19991109 A 3350 BR2013 LIGHT BOEING 737 7377H4 NM ROW 17-19 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701GS 27836 EEPLS INOP BETWEEN ROWS 17-19. REPAIRED LIGHT SYSTEM PER MM. 2 L 7 2 4F RT A16WE 1999111900485 19991119 00485 NM 1999 11 19 SWAA991882 1 19991109 A 2560 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT SRVCE DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999111900486 19991119 00486 NM 1999 11 19 SWAA991883 1 19991109 A 3350 BR2013 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT MID CABIN. RELAMPED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999111900487 19991119 00487 NM 1999 11 19 SWAA991884 1 19991109 A 5312 6516300 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD HAS 3 EACH CRACKS, LBL 5- RBL 7. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999111900488 19991119 00488 NM 1999 11 19 SWAA991885 1 19991109 A 5320 65C27314 CLIP BOEING 737 7373T5 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED, BS 380, STRINGER 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 1999111900489 19991119 00489 NM 1999 11 19 SWAA991886 1 19991109 A 5754 65C26686 SKIN BOEING 737 7373T5 NM NR 5 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED. REPAIRED SLAT PER SWA RA NR A57-0691 AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 1999111900490 19991119 00490 NM 1999 11 19 SWAA991887 1 19991110 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 15 INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS INOP AT ROW 15. RECONNECTED PULLED WIRES PER MM. 2 L 7 2 4F RT A16WE 1999111900491 19991119 00491 NM 1999 11 19 SWAA991888 1 19991111 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 EXTERNAL FUSELAGE SKIN CRACKED, BS 500C, STRINGER 11L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999111900492 19991119 00492 NM 1999 11 19 SWAA991898 1 19991111 A 2560 D31354 SLIDES BOEING 737 7372H4 138448C NM EMER EXIT OUT OF POSITION A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 BOTH AFT EVACUATION SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSY'S PER MM. 2 L 7 2 4F A16WE 1999111900493 19991119 00493 NM 1999 11 19 SWAA991899 1 19991111 A 3350 65C27093 LIGHTS BOEING 737 7372H4 138448C NM EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C1 CHECK, FOUND BOTH FWD DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2 L 7 2 4F A16WE 1999111900494 19991119 00494 NM 1999 11 19 SWAA991900 1 19991111 A 3350 6104789 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F A16WE 1999111900495 19991119 00495 NM 1999 11 19 SWAA991901 1 19991111 A 3350 6104789 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED LT OVERWING EXIT LIGHT BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999111900496 19991119 00496 NM 1999 11 19 TWAA9915501 1 19991111 A 3397 WIRE BOEING 767 76733AER 1385230 NM BS 1085 FAILED A TWAA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 CE 05 637TW 25403 AIRCRAFT RETURNED TO THE GATE FROM TAXI FOR A NAVIGATION SYSTEM PROBLEM. DURING TROUBLESHOOTING SOME POPPED CIRCUIT BRE AKERS FOR LIGHTING FOUND POPPED IN THE LOWER ELECTRONIC COMPARTMENT, WOULD NOT RESET. MINUTES LATER A PASSENGER REPORT ED A POPPING NOISE ABOVE SEAT ROW 29, LEFT SIDE OF CABIN. A MECHANIC CHECKING THE SOUND OPENED THE COVE LIGHT PANEL AND FOUND SMOKE. FANNING THE AREA TO CLEAR THE SMOKE, A SMALL FLAME DEVELOPED. THE MECHANIC USED HIS HAND TO EXTINGUISH THE FLAME. PASSENGERS WERE DEPLANED. SOME 19 WIRES WERE DAMAGED AT STA 1085, LBL 53, WL 305, BUNDLE 6035. REPLACED SE CTION OF DAMAGED WIRES PER STD PRACTICES 20-41-01 AND 20-51-01. CHECK-C 10-29-99. 2 L 7 2 4F RT A1NM 1999111900497 19991119 00497 WP 1999 11 19 TWAA9915502 1 19991114 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOP A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 981Z 47345 TWO FORWARD CABIN OVERHEAD EMERGENCY LIGHTS REMAINED ON AFTER ALL ELECTRICAL POWER WAS OFF. REPLACED THE POWER SUPPLY, (P/N 60030451LB) AND BATTERY (P/N 408822101). CHECK-C 8-29-99 MCI. 2 L 7 2 4F A6WE 1999111900498 19991119 00498 NM 1999 11 19 TWAA9915503 1 19991112 A 2910 LINE BOEING 727 727231 1384079 NM NR 1 HYD SYS FAILED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 05 64339 20844 THE NUMBER 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT AND THE -A- HYDRAULIC SYSTEM QUANTITY WENT TO ZE RO. IT WAS NECESSARY TO MANUALLY EXTEND THE LANDING GEAR. THE NUMBER 1 ENGINE PUMP PRESSURE LINE HAD RUBBED THROUGH AT THE PYLON PASS THROUGH TO THE FUSELAGE. REMOVED THE LINE AND ACCOMPLISHED A RING LOCK REPAIR PER MM 20-10-5. CHECK-C 5-20-99 JFK. 2 L 7 3 4F A3WE 1999111900499 19991119 00499 WP 1999 11 19 TWAA9915504 1 19991113 A 3350 58222 BATTERY PACK DOUG DC9 DC931 3022065 WP ROW 16-21 DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 976Z 47248 THE EGRESS LIGHTS ILLUMINATED FROM ROWS 16 TO 21 WITH THE SWITCH IN ARM POSITION. REPLACED THE BATTERY PACK. CHECK-C 1 0-2-99 STL. 2 L 7 2 4F A6WE 1999111900500 19991119 00500 WP 1999 11 19 TWAA9915505 1 19991113 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP ROW 16-21 INOP A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 976Z 47248 THE EGRESS LIGHTS FROM ROW 16 THROUGH 21 ILLUMINATED INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 10-2-99 STL. 2 L 7 2 4F A6WE 1999111900501 19991119 00501 NM 1999 11 19 HNAA990014 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 214 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED 4.75 RIGHT OF CENTER STA X214. REPAIRED IAW EO8-53-99-397. 2 H 7 2 4T RT A13NM 1999111900502 19991119 00502 NM 1999 11 19 HNAA9900141 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 212.7 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED.5 LEFT OF CENTER STA X212.7. REPAIRED IAW EO8-53-99-397. 2 H 7 2 4T RT A13NM 1999111900503 19991119 00503 NM 1999 11 19 HNAA9900143 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 212.5 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED .5 LEFT OF CENTER, STA X212.5. REPAIRED IAW E08-53-99-397. 2 H 7 2 4T RT A13NM 1999111900504 19991119 00504 NM 1999 11 19 HNAA9900144 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 210 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED 2 RIGHT OF CENTER, STA X210. REPAIRED IAW EO8-53-99-397. 2 H 7 2 4T RT A13NM 1999111900505 19991119 00505 NM 1999 11 19 HNAA9900145 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 220 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED 3.5 LEFT OF CENTER, STA X220. REPAIRED IAW EO8-53-99-397. 2 H 7 2 4T RT A13NM 1999111900506 19991119 00506 NM 1999 11 19 HNAA9900146 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 213.5 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED 4 RIGHT OF CENTER, STA X213.5. REPAIRED IAW EO8-53-99-397. 2 H 7 2 4T RT A13NM 1999111900507 19991119 00507 NM 1999 11 19 HNAA9900147 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 215 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED 6.5 RIGHT OF CENTER, STA X215. REPAIRED IAW EO8-53-99-397. 2 H 7 2 4T RT A13NM 1999111900508 19991119 00508 NM 1999 11 19 HNAA9900148 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 BELLY SKIN SPLICE BURNED BY LIGHTNING. PIT BLENDED .005 DEEP AND PIT REMAINS. INFO SENT TO ENGINEERING. VERIFIED BETW EEN BLEND AND RIVETS. ALODINE, PRIME AND PAINT AND SEAL. C'D/W ABOVE DISPOSITION. 2 H 7 2 4T RT A13NM 1999111900509 19991119 00509 NM 1999 11 19 HNAA9900149 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 575 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 BELLY SKIN SPLICE BURNED AT STA X575. BLENDED OUT BURN MARK. VERIFIED ON RIVETS. VERIFIED STRAP WAS CRACK FREE. PERF ORMED EDDY CURRENT INSP, DAMAGED AREA SHOWS INDICATION OF POSSIBLE CRACK OR A DEEP PIT. SEE SEQ 67 (END RESULT WAS ONLY A PIT). 2 H 7 2 4T RT A13NM 1999111900510 19991119 00510 NM 1999 11 19 HNAA9900150 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 615 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED AT STA X615 I/B OF STR 31. DAMAGE PARTIALLY BLENDED .008 DEEP, PIT STILL VISABLE. INFO SENT TO ENGINEERING . BLEND OUT BURN AND REPAIR PER ESR8-53-92-025. C'D/W ABOVE DISPOSITION. 2 H 7 2 4T RT A13NM 1999111900511 19991119 00511 NM 1999 11 19 HNAA9900151 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 531 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN JOINT BURNED ON EDGE AT STA X531 BETWEEN STR 31P AND 32P. BLEND OUT BURNED AREA MAINTAIN ED ON RIVETS, ALODINE, PR IME, AND PAINT. C'D/W ABOVE DISPOSITION. 2 H 7 2 4T RT A13NM 1999111900512 19991119 00512 NM 1999 11 19 HNAA9900152 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 615 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED AT STA X615 I/B OF STR 31 NEXT TO RIVET. BLEND OUT BURN AND REPAIR PER ESR8-53-92-025. C'D/W ABOVE DISPOSI TION. 2 H 7 2 4T RT A13NM 1999111900513 19991119 00513 NM 1999 11 19 HNAA9900153 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN SPLICE ON BELLY HAS BURN MARK AT FRAME NR 2. BLEND BURN AREA LEAVING ED ON RIVETS. ALODINE PRIME, PAINT AND SEAL. C'D/W ABOVE DISPOSITION. 2 H 7 2 4T RT A13NM 1999111900514 19991119 00514 NM 1999 11 19 HNAA9900154 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 165 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED ON CENTER LINE, STA X165 (BETWEEN RIVETS). BLEND OUT PIT TO MAX .006, ALODINE PRIME AND PAINT. C'D/W ABOVE DISPOSITION. 2 H 7 2 4T RT A13NM 1999111900515 19991119 00515 NM 1999 11 19 HNAA9900155 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 181.7 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED 1 LEFT OF CENTER, 3 FROM EDGEOF SKIN JOINT STA X181.7. BLEND AREA UP TO .006 DEEP. ALODINE, PRIME, AND PAI NT. C'D/W ABOVE DISPOSITION. 2 H 7 2 4T RT A13NM 1999111900516 19991119 00516 NM 1999 11 19 HNAA9900156 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 203 DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 SKIN BURNED AND RIVET BURNED 3 LEFT OF CENTER STA X203. DRILLED OUT AND INSTALLED NEW RIVET. CHECK INSTALLATION OF NEW RIVET FOR ANY PTTING. IF AREA IS PIT FREE, ALODINE, PRIME AND PAINT. C'D/W ABOVE DISPOSITION. 2 H 7 2 4T RT A13NM 1999111900517 19991119 00517 NM 1999 11 19 HNAA9900157 1 19991115 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 926HA 114 C/W REPAIR TO DENT AND STRUCTURE BELOW F/O WINDSCREEN (DENT ON SKIN TO NOSE BAY STRAP) 6 ABOVE PANEL 212BL. THIS DMT IS CLEARED PER EO8-53-99-394. 2 H 7 2 4T RT A13NM 1999111900518 19991119 00518 NM 1999 11 19 CALA9901491 1 19991113 A 3234 1FA011342 SELECT. VALVE BOEING 737 737824 13844BZ NM LANDING GEAR INOP A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 18223 2542 28932 THE RT MLG EXTENDED WHILE IN CRUISE AT FL 290 AND 300 KTS INDICATED AIRSPEED. BOTH RED AND GREEN GEAR LIGHTS FOR THE RI GHT GEAR WERE ILLUMINATED. THE ACFT WAS SLOWED TO 260 KTS AND ALL GEAR WERE FULLY EXTENDED, THEN RETRACTED. THE ACFT W AS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE RT MLG ASSEMBLY AND UPLOCK WERE INSPECTED WITH NO DEFECTS NOTE D. A GEAR RETRACTION WAS PERFORMED IAW MM 32-32-00 AND NO FAULTS WERE FOUND. THE RT MLG UPLOCK AND DOWNLOCK SENSORS WE RE CHECKED FOR PROPER CLEARANCE IAW MM 32-61-21 AND BOTH CHECKED GOOD. THE LANDING GEAR SELECTOR VALVE WAS REMOVED AND REPLACED IAW MM 32-31-51. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1999111900519 19991119 00519 WP 1999 11 19 CALA9901492 1 19991112 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND G-2 GALLEY FITTING CORRODED AFTER REMOVAL OF RT O/B SEAT TRACK AT STA 218. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1999111900520 19991119 00520 WP 1999 11 19 CALA9901493 1 19991112 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND AFT CARGO DOOR OUTER SKIN AFT EDGE DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1, 52- 32-0, AND 51-10-3. 2 L 7 2 4F A6WE 1999111900521 19991119 00521 WP 1999 11 19 CALA9901494 1 19991112 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A 1 INCH CRACK IN INTERNAL SUPPORT BRACKET AT FORWARD CARGO DOOR LOWER FORWARD DOOR STOP. THE SUPPORT BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999111900522 19991119 00522 WP 1999 11 19 CALA9901495 1 19991112 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN DOOR NR 1 BEAM FORWARD END. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGUR E 31. 2 L 7 2 4F A6WE 1999111900523 19991119 00523 NM 1999 11 19 CALA9901496 1 19991112 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND UPPER ATTACH ANGLE CORRODED AT FS 1166 FALSE BULKHEAD, BL 0. THE CORRODED AREA WAS REMOVED IAW SRM 51- 40-3. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1999111900524 19991119 00524 WP 1999 11 19 CALA9901497 1 19991114 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 475 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 87070 48292 INSPECTION FOUND FORWARD AVIONICS BAY CROSS BEAM CORRODED AT STA Y475, LT SIDE. REPAIRED IAW ECRA 5312-01015 AND FLS DR AWING 90-53-1057. 2 L 7 3 4F A22WE 1999111900525 19991119 00525 WP 1999 11 19 CALA9901498 1 19991114 A 3397 WIRE DOUG DC10 DC1030 3023501 WP ROW 2KL BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13067 47866 INSPECTION FOUND FORWARD EMERGENCY LIGHT AT SEAT 2KL INOPERATIVE. INSPECTION REPAIRED BROKEN WIRE AT SEAT 2KL AND OPERA TION CHECKED GOOD. 2 L 7 3 4F A22WE 1999111900526 19991119 00526 EA 1999 11 19 COMA9960683 1 19991114 A 5751 691R39310152 PANEL CNDAIR CL600 CL6002B19 EA RT AILERON CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 709CA 3966 7235 RIGHT HAND OUTBOARD LOWER COVER PANEL ON RIGHT HAND AILERON CHAFED BEYOND LIMITS. FABRICATED NEW PANEL AND INSTALLED AN AILERON IAW WVAC EO 601R-57-0619. 2 L 7 2 4F RT A21EA 1999111900527 19991119 00527 EA 1999 11 19 COMA9960684 1 19991114 A 5730 601R10045 PLATE CNDAIR CL600 CL6002B19 EA WS 76.1612 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 TWO CRACKS IN LOWER HORIZONTAL SURFACE OF LEFT HAND LOWER WING ACCESS HOLE AT 540 CB. BLENDED OUT DAMAGED, ROTO PEENED AFFECTED AREAS AND ALODINED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999111900528 19991119 00528 EA 1999 11 19 COMA9960685 1 19991114 A 5730 601R10045 PLATE CNDAIR CL600 CL6002B19 EA WS 188 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 THREE CRACKS IN LOWER HORIZONTAL SURFACE OF LEFT HAND LOWER WING ACCESS HOLE AT 550 BB. BLENDED OUT DAMAGE, ROTO PEENED AFFECTED AREAS AND ALODINED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999111900529 19991119 00529 EA 1999 11 19 COMA9960686 1 19991114 A 5730 601R10045 PLATE CNDAIR CL600 CL6002B19 EA WS 76.161 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 CRACK IN LOWER HORIZONTAL SURFACE OF RIGHT HAND LOWER WING ACCESS HOLE AT 640 CB. BLENDED OUT DAMAGE, ROTO-PEENED AFFEC TED AREA AND ALODINED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999111900530 19991119 00530 EA 1999 11 19 COMA9960687 1 19991114 A 5320 6003663031 DOUBLER CNDAIR CL600 CL6002B19 EA FS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 708CA 3966 7235 FS 718.00 FRAME DOUBLERS ARE CRACKED AT LHS 7 RHS OF FRAME, STR 10-12. REMOVED CRACKED DOUBLERS AND REPLACED WITH NEW D OUBLERS IAW CANADAIR REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 1999111900531 19991119 00531 EA 1999 11 19 COMA9960688 1 19991109 A 5320 RIVET CNDAIR CL600 CL6002B19 EA BS 409 MISINSTALLED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 916CA 15913 70147 FS 409.0 + 123 HAS A RIVET NOT FILLING HOLE, JUST ABOVE STRINGER A15. DISCOVERED DURING ACCOMPLISHMENT OF TASK CARD 003- 53-900-602. REMOVED AND REPLACED RIVET AT FS 409 + 128 JUST ABOVE STRINGER 15 IAW WVAC EO 601R-53-0596A. 2 L 7 2 4F RT A21EA 1999111900532 19991119 00532 EA 1999 11 19 COMA9960689 1 19991110 A 5320 601R50134 BRACKET CNDAIR CL600 CL6002B19 EA BS 114.5 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 NEED PROVISIONS FOR THE FDR MODIFICATION. PERFORMED BRACKET ALTERATION FOR FDR MODIFICATION IAW WVAC EO 601R-53-0594A. 2 L 7 2 4F RT A21EA 1999111900533 19991119 00533 EA 1999 11 19 COMA9960690 1 19991113 A 2170 DRAIN CNDAIR CL600 CL6002B19 EA LT & RT CLOGGED A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 999CA 7230 LEFT AND RIGHT AC PACKS TRIPPED OFF DURING CRUISE FLIGHT. REPLACED WATER SEPARATOR DRAIN ORIFICE. 2 L 7 2 4F RT A21EA 1999111900534 19991119 00534 EA 1999 11 19 COMA9960691 1 19991113 A 3220 LINK CNDAIR CL600 CL6002B19 EA NLG DISCONNECTED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 781CA 7312 LANDING GEAR DISAGREE WARNING. NLG TORQUE LINKS NOT CONNECTED. CONNECTED TORQUE LINKS AND RETRACT CHECKS NORMAL. 2 L 7 2 4F RT A21EA 1999111900535 19991119 00535 EA 1999 11 19 COMA9960692 1 19991114 A 3260 INDICATION CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 986CA 7174 CREW REPORTED LANDING GEAR INDICATION WAS IN ERROR. LANDING GEAR RETRACTION CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 1999111900536 19991119 00536 NM 1999 11 19 UPS99231094 1 19991108 A 5753 652165113 SUPPORT BOEING 727 72762C 138402C NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE AD V LEFT SUPPORT ASSY I/B FLAP TRACK FWD CORRODED. LEFT I/B FLAP TRACK FWD SUPPORT ASSY REPLACED IAW M M 27-51-31. 2 L 7 3 4F A3WE 1999111900537 19991119 00537 NM 1999 11 19 UPS99231095 1 19991023 A 5313 BAC1498138 STRINGER BOEING 727 72725C 138400H NM BS 450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON RT STRINGER BS 450, STR 28R, E & E COMPL. REMOVED CORRODED SECTION OF STRINGER, INSTAL LED NEW STRINGER AND SPLICE PER SRM 51-30-6, 51-30-5 AND 53-10-3. 2 L 7 3 4F A3WE 1999111900538 19991119 00538 NM 1999 11 19 UPS99231096 1 19991023 A 5320 66118099 CLIP BOEING 727 72725C 138400H NM BS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI STRINGER CLIP CORRODED AT STR 28R, BS 460 REPLACED STRINGER CLIP PER SRM 51-30-2 ***CPCP*** 2 L 7 3 4F A3WE 1999111900539 19991119 00539 NM 1999 11 19 UPS99231097 1 19991110 A 5320 65163516 FRAME BOEING 727 72725C 138400H NM E/E DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) ON AFT E & E DOOR FRAME AFT SIDE AT BS 451. REMOVED FRAME AND REPLACED WITH NEW FRAME. 2 L 7 3 4F A3WE 1999111900540 19991119 00540 NM 1999 11 19 UPS99231098 1 19991110 A 5347 BAC15201331 SEAT TRACK BOEING 727 72725C 138400H NM BS 379 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK AT BS 379, LBL 1, WL 208. REMOVED CORROSION ON SEAT TRACK, FOUND TO BE OUT OF LIMITS PER SRM 51-10-6 AND SRM 53-10-1. REMOVED CORRODED SEAT TRACK FROM BS 360 TO 545, BL 0 AND INSTALLED NEW SEAT TRACK PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999111900541 19991119 00541 NM 1999 11 19 UPS99231099 1 19991108 A 5347 659927173 SEAT TRACK BOEING 727 72725C 138400H NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 740, RBL 45, WL 208. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK FRO M BS 660 TO 745, RBL 45, PER SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F A3WE 1999111900542 19991119 00542 NM 1999 11 19 UPS99231100 1 19991023 A 5313 BAC1498138 STRINGER BOEING 727 72725C 138400H NM BS 450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORRODED STRINGER 28L BS 450, E & E COMPL. REMOVED CORRODED SECTION OF STRINGER AND INSTALLED NEW S ECTION W STRINGER SPLICE PER SRM 53-10-3. 2 L 7 3 4F A3WE 1999111900543 19991119 00543 NM 1999 11 19 UPS99231101 1 19991029 A 5315 HFAB53AN011 FLOORBEAM BOEING 727 72725C 138400H NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) FLOORBEAM TOP CHORD BS 680 RBL 51, WL 208. REMOVED AND REPLACED TOP CH ORD PER SRM 53-10-1, SRM 53-10-8, OHM 20-41-02, SRM 51-30-2. 2 L 7 3 4F A3WE 1999111900544 19991119 00544 NM 1999 11 19 UPS99231102 1 19991027 A 5751 FITTING BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, WHILE WORKING CARD 010635 (WINGS 277) FOUND LT WING O/B, AILERON O/B AND O/B CENTER HINGE SUPPORT FI TTINGS CORRODED, AILERON SIDE. REMOVED AND REPLACED HINGE FITTINGS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999111900545 19991119 00545 NM 1999 11 19 UPS99231103 1 19991104 A 5311 FRAME BOEING 727 72725C 138400H NM BS 680 PUNCTURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, FWD BAY FRAME UPPER FLANGE PUNCTURED BS 680 RBL 23 (BELOW RT FLOOR TO SIDEWALL SUPPORT NUTPLATE). R EMOVED DAMAGE AND REPAIRED PER SRM. 2 L 7 3 4F A3WE 1999111900546 19991119 00546 NM 1999 11 19 UPS99231104 1 19991108 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 739 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION ON LOWER SURFACE OF SEAT TRACK BS 739 LBL 63 WL 208 REPLACED SEAT TRACK SEGMENT FROM BS 660 TO BS 740 LBL 65 PER 727 SRM 53-10-5 AND 51-30-2 ***CPCP*** 2 L 7 3 4F A3WE 1999111900547 19991119 00547 NM 1999 11 19 UPS99231105 1 19991108 A 5730 SKIN BOEING 727 72725C 138400H NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON INNER SURFACE OF BOOST PUMP CAVITY 7302 AT THE 6 O'CLOCK POSITION. REPAIRED PER ER 99- 6318. 2 L 7 3 4F A3WE 1999111900548 19991119 00548 NM 1999 11 19 UPS99231106 1 19991027 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 780/825 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK AT BS 780 AND BS 825 TO BS 840, LBL 63 WL 208. REMOVED AND REPLACED SEAT TR ACK PER SRM 53-10-1, SRM 51-30-5, SRM 51-20-151, SRM 51-40-3, SRM 51-30-2. 2 L 7 3 4F A3WE 1999111900549 19991119 00549 NM 1999 11 19 UPS99231107 1 19991108 A 5320 65159791 CHORD BOEING 727 72725C 138400H NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI WHILE WORKING NRC 010078 FUSE 157, 870 LOWER CHORD IS CRACKED LBL 10 WL 138 (870 BULKHEAD AIR COND BA Y SIDE). CUT OUT DAMAGED SECTION OF CHORD AND REPAIRED PER SRM 51-40-4 BY SPLICING IN A NEW SECTION. 2 L 7 3 4F A3WE 1999111900550 19991119 00550 NM 1999 11 19 UPS99231108 1 19991105 A 5347 BAC15201430 SEAT TRACK BOEING 727 72725C 138400H NM BS 882 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK AT BS 882, LBL 1, WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS AND REPLA CED THE SEAT TRACK FROM BS 870 - BS 958, BL 0, WL 208, ON CUSTOMER ID 010795 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999111900551 19991119 00551 NM 1999 11 19 UPS99231109 1 19991108 A 5311 FRAME BOEING 727 72725C 138400H NM BS 680 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, FWD CARGO BAY FRAME UPPER FLANGE PUNCTURED BS 680 LBL 23 WL 148.5. CUT OUT DAMAGED AREA 1 X 3 ON FR AME CROWN AT BS 680 LBL 23 WL 148.5, FABRICATED REPAIR DOUBLER, HEAT TREATED & INSTALLED ALL WORK ACCOMPLISHED IAW SRM 5 3-10-1, SRM 51-30-2, MM 51-20-21 AND MM 50-21-151 AND SRM 51-40-3. 2 L 7 3 4F A3WE 1999111900552 19991119 00552 NM 1999 11 19 UPS99231110 1 19991108 A 5730 SKIN BOEING 727 72725C 138400H NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON INNER SURFACE OF BOOST PUMP CAVITY 7302 AT THE 3 O'CLOCK POSITION. REPAIRED PER ER NR 99-6318. 2 L 7 3 4F A3WE 1999111900553 19991119 00553 NM 1999 11 19 UPS99231111 1 19991022 A 5347 659927173 SEAT TRACK BOEING 727 72725C 138400H NM BS 326/329 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON SEAT TRACK UNDER NUTPLATE AT BS 326 AND 329 RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 340 - 390 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999111900554 19991119 00554 NM 1999 11 19 UPS99231112 1 19991111 A 5330 SKIN BOEING 727 72725C 138400H NM BS 295-312 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-100-01.07-04) BULGING SKIN AND ONE SHEARED RIVET BELOW THE FORWARD LAV SERVICE PANEL B S 295 TO BS 312 STR 20R. REMOVED DAMAGE AND REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1999111900555 19991119 00555 NM 1999 11 19 UPS99231113 1 19991111 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 236 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION (C53-221-01.01-01) ON FLOOR STRUCTURE AT BS 236 WL 208, LBL 32. REMOVED DAMAGE AND REPLAC ED PER SRM. 2 L 7 3 4F A3WE 1999111900556 19991119 00556 NM 1999 11 19 UPS99231114 1 19991112 A 5313 69144925 STRINGER BOEING 727 72725C 138400H NM BS 445 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI, CORROSION ON STRINGER SPLICE AT BS 445, STR 20R. DAMAGE BEYOND LIMITS. REMOVED AND REPLACED STRING ER SPLICE PER BAC DWG 65-18215. 2 L 7 3 4F A3WE 1999111900557 19991119 00557 NM 1999 11 19 UPS99231115 1 19991113 A 5230 65C170883 FITTING BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 944UP 19103 INSPECTION TYPE:AD V AFT CARGO DOOR NR 2 AFT DOOR STOP FITTING CRACKED. FITTING REPLACED IAW B727-5230-0032 APPENDIX C & D. 2 L 7 3 4F A3WE 1999111900558 19991119 00558 WP 1999 11 19 ABXA9900787 1 19991027 A 5753 591735426 ANGLE DOUG DOUG DC9 DC932F 3022067 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND THE LEFT OUTBOARD FLAP HINGE FITTING INTERIOR ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51 -30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999111900559 19991119 00559 WP 1999 11 19 ABXA9900788 1 19991027 A 5320 9922042506 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 794 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING AT STATION 794 CRACKED ON THE RIGHT SIDE. REPLACED FITTING IAW DC9 SRM 5 1-30-5. 2 L 7 2 4F A6WE 1999111900560 19991119 00560 WP 1999 11 19 ABXA9900789 1 19991027 A 5320 9922042505 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 867 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LEFT VERTICAL SUPPORT FITTING AT STATION 869 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999111900561 19991119 00561 WP 1999 11 19 ABXA9900790 1 19991027 A 5311 5912285513 FRAME DOUG DOUG DC9 DC932F 3022067 WP BS 579 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND CABIN WINDOW RETAINER FRAME CRACKED AT STATION 579, FORWARD LOWER CORNER. REPAIRED IAW ABX REA D9 53-33951. 2 L 7 2 4F A6WE 1999111900562 19991119 00562 WP 1999 11 19 ABXA9900791 1 19991027 A 5311 5912285513 FRAME DOUG DOUG DC9 DC932F 3022067 WP BS 794 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND CABIN WINDOW RETAINER FRAME CRACKED AT STATION 794, AFT LOWER CORNER. REPAIRED IAW ABX REA D953-3 3951. 2 L 7 2 4F A6WE 1999111900563 19991119 00563 NM 1999 11 19 SCNA99137 1 19991113 A 3350 LIGHT BOEING 727 7272J4 1384006 NM ROW 32D INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE WHITE FLOOR TRACK EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE AT SEAT ROW 32D. INS TALLED A NEW LAMP AT POSITION 32D, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999111900564 19991119 00564 NE 1999 11 19 SCNA99138 2 19991114 A 7310 FUEL LINE BOEING 727 7272J4 1384006 NM PWA JT8 JT8D217C 52053 NE NR 2 ENGINE LEAKING A SCNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 288SC 20765 UPON LEVEL OFF AT CRUISE ALTITUDE THE NUMBER TWO ENGINE SHUTDOWN. ALL INDICATIONS LOW. UPON INSPECTION FOUND FUEL LEAK AT THE PRESSURIZATION AND DUMP VALVE LINE RUNNING TO THE FUEL/OIL HEATHER. REMOVED AND REPLACED PACKINGS AND THE LINE, RAN ENGINE AS REQUIRED. LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 3 4F 4 F RT A3WE E9NE 1999111900565 19991119 00565 NM 1999 11 19 DHL99742003 1 19991112 A 2782 ACTUATOR BOEING 727 727225 1384077 NM NR 1 LE SLAT LOOSE A DHLA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 SO 01 742DH 21290 NR 1 L/E SLAT WOULD NOT RETRACT. FOUND NR 1 L/E SLAT ACTUATOR LOOSE IN MOUNT. TIGHTENED 4 MOUNT BOLTS, PERFORMED SYST EM ADJ AND TEST. LIGHTS OPS CHECK GOOD PER MM 27-82-0. 2 L 7 3 4F A3WE 1999111900566 19991119 00566 NM 1999 11 19 VNAA9911008 1 19991016 A 2435 8160121 STARER GEN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 430JS 8510 1434 3044 116118 DURING CLIMBOUT, THE FLIGHT CREW RECEIVED AN ECU FAIL CAS MESSAGE, THEN THE RIGHT HAND STARTER GENERATOR CAME ON AND OFF RAPIDLY AND CONTINUOUSLY. THE AIRCRAFT RETURNED TO THE FIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENA NCE INSPECTED AND CLEANED THE ELECTRONIC ENGINE CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-21-01. OP ERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS FERRIED TO PITTSBURGH WHERE MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND STARTER GENERATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-31-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111900567 19991119 00567 WP 1999 11 19 RAIA9911014 2 19991112 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT FAILED A RAIA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 CE 03 860AE 14392 1830 860 66128 LAX- RIGHT ENGINE LOSE OIL PRESS. ENGINE WAS SHUT DOWN. MAINTENANCE REPLACED RIGHT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999111900568 19991119 00568 EU 1999 11 19 RAIA9911015 1 19991113 A 2731 TRIM JETAIR JETSTM JETSTM4101 1500501 EU ELEVATOR MALFUNCTIONED A RAIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 03 561HK 41077 JFK- ELEVATOR TRIM JAMMED MOMENTARILY ON APPROACH. MAINTENANCE INSPECTED ELEVATOR TRIM TAB, MANUALLY RAN TRIM BACK & FO RTH SEVERAL TIMES, ELECTRICALLY RAN TRIM FULL TRAVEL. 2 L 7 2 4T RT A41NM 1999111900569 19991119 00569 1999 11 19 RAIA9911016 4 19991113 A 2210 AUTOPILOT JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPT DISCONNECTED A RAIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 CE 03 561HK 41077 JFK- AUTO PILOT DISCONNECTED UNCOMMANDED DURING DESCENT. MAINTENANCE CYCLED AUTO PILOT CIRCUIT BREAKER, PERFORMED OPERA TIONAL CHECK. 2 L 7 2 4T RT A41NM 1999111900570 19991119 00570 SO 1999 11 19 RAIA9911017 1 19991114 A 3010 329445 VALVE EMB 145 EMB145 SO WING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 807HK 145119 BOS-URING DEICE TEST, DID NOT GET A WING OPEN LIGHT. MAINTENANCE REPLACED WING ANTI-ICE VALVE. 2 L 7 2 4F RT T00011AT 1999111900571 19991119 00571 SO 1999 11 19 LR7A9964 1 19991115 A 7931 ST104A TRANSMITTER LKHEED 382 382G 526414U SO NR 4 ENGINE FAILED A LR7A A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CR CRUISE 1 AL 03 405LC 401 5025 FLIGHT CREW REPORTED NR 4 ENGINE DEVELOPED A RGB OIL PRESSURE FLUCUATION OF 30 PSI, 1.5 HOURS OUT OF BOS EN ROUTE TO CDC . DUMPED 9000 LBS OF FUEL, RETURNED TO BOS PRECAUTIONARY AND LANDED WITHOUT INCIDENT. INSPECTED RGB MAG PLUGS AND PRES SURE FILTER FOR METAL CONTAMINATION, NONE FOUND. REPLACED RGB OIL PRESSURE TRANSMITTER IAW SMP 581 CHAPTER 79-30, PG 20 2B AND 203. OPS CHECK GOOD IAW CHAPTER 71. 2 H 7 4 4T A1SO 1999111900572 19991119 00572 SO 1999 11 19 LR7A9965 1 19991115 A 5313 LONGERON LKHEED 382 382G 526414U SO BS 924 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 DURING SCHEDULED A CHECK, FOUND RT SLOPING LONGERON BUMPER BENT AND CRACKED AT FS 922-926. REMOVED FASTENERS, ACCOMPLIS HED HFEC INSPECTION TO VERIFY CRACKED TERMINAL ENDS. REPAIRED IAW SRM 583-53-50-22. 2 H 7 4 4T A1SO 1999111900573 19991119 00573 EA 1999 11 19 COMA9960693 1 19991114 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 783CA 5629 7315 NWS CAUTION MESSAGE DURING FLIGHT. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1999111900574 19991119 00574 EA 1999 11 19 COMA9960694 1 19991109 A 3350 20131A BATTERIES CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 960CA 4509 7117 EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY BATTERIES. 2 L 7 2 4F RT A21EA 1999111900575 19991119 00575 NM 1999 11 19 UPS99231116 1 19991108 A 5753 65216514 SUPPORT BOEING 727 727180C 138406G NM RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE: AD, RT SUPPORT ASSEMBLY INBOARD FLAP TRACK FORWARD CORRODED. SUPPORT ASSEMBLY REPLACED IAW BOEING DRAW ING NR 65 19297, SHEET 3, REV E. 2 L 7 3 4F A3WE 1999111900576 19991119 00576 NM 1999 11 19 UPS99231117 1 19991108 A 3211 658595926 LINK BOEING 727 727180C 138406G NM RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE: AD, RT MLG TRUNNION LINK HAS PITTING CORROSION ON FORWARD BEARING SURFACE. REPLACED TRUNNION LINK ASSE MBLY. INSTALLED IAW MM 32-11-01. 2 L 7 3 4F A3WE 1999111900577 19991119 00577 NM 1999 11 19 UPS99231118 1 19991115 A 3350 LIGHT BOEING 727 72727C 138400J NM CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE: N/A, EMERGENCY EXIT LIGHT FWD ENTRY DOOR INTERMIT (REPEAT ITEM). ACCOMPLISHED VOLTAGE CHECK IAW MM 33- 50-01, OPS CHECK GOOD. REPLACED LIGHT MOUNT, DISCOVERED A POOR CONTACT. 2 L 7 3 4F A3WE 1999111900578 19991119 00578 NM 1999 11 19 99UAL900575 1 19991105 A 5210 SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 340UA 24244 AIRCRAFT CABIN WAS UNABLE TO BE PRESSURIZED. *S/D* THE 2L SLIDING WINDOW AND THE 1L DOOR SEALS LEAK. REPLACED THE 2L SLIDING WINDOW SEAL AND REPAIRED THE DOOR 1L PRESSURE SEAL. PRESSURIZED THE AIRCRAFT, NO LEAKS. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900579 19991119 00579 NM 1999 11 19 99UAL900576 1 19991107 A 2130 MODULE BOEING 654531458 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT LOOSE A UALA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 WP 29 339UA 24243 CABIN ALTITUDE RISE ABOVE 10 PSI. *S/D* DELTA P MODULE WAS NOT CORRECTLY SEATED IN ITS SOCKET. REPLACED THE DELTA P M ODULE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900580 19991119 00580 NM 1999 11 19 99UAL900577 1 19991106 A 2131 CONTROLLER HAMILTON STA 7638101 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 908UA 91120003 25008 AIRCRAFT ENCOUNTERED CABIN PRESSURIZATION PROBLEM AFTER TAKEOFF. *S/D* THE CABIN PRESSURE CONTROLLER FAILED. REPLACED THE CABIN PRESSURE CONTROLLER. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900581 19991119 00581 NE 1999 11 19 99UAL900578 2 19991106 A 7321 ECU WOODWARD GOV MR73204 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE LEAKING A UALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 933UA 43859 26659 725367 NUMBER TWO ENGINE FAILURE INDICATION ILLUMINATED DUE TO COMPRESSOR STALL. *S/D* NO DAMAGE FOUND ON THE BORESCOPE INSPE CTION. THE MAIN ENGINE CONTROL LEAKS. REPLACED THE MAIN ENGINE CONTROL AND FUEL PUMP. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900582 19991119 00582 NM 1999 11 19 99UAL900579 1 19991103 A 3020 VALVE WHITTAKER 1726257 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ENGINE ANTI-ICE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 381UA 2038 24656 THE COWL VALVE OPEN LIGHT REMAINED BRIGHT WHEN THE NUMBER TWO ENGINE ANTI-ICE VALVE SWITCHED TO THE ON POSITION. *S/D* REPLACED THE ENGINE ANTI-ICE VALVE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900583 19991119 00583 NE 1999 11 19 99UAL900580 2 19991102 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 MALFUNCTIONED A UALA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 29 938UA 26671 725718 AT 120 KNOTS, THE EXHAUST GAS TEMPERATURE ON NUMBER TWO ENGINE EXCEEDED 1000 0 C. *S/D* REMOVED AND SENT THE ENGINE TO THE TURBINE SHOP. AFTER REVIEWING THE FLIGHT RECORDER DATA, THE ENGINE EXHAUST GAS TEMPERATURE EXCEEDED THE 930 0 C LI MIT FOR 45 SECONDS. REPLACED THE ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900584 19991119 00584 NM 1999 11 19 99UAL900581 1 19991107 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7452U 21906 FORWARD GALLEY UPPER EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1999111900585 19991119 00585 NM 1999 11 19 99UAL900582 1 19991107 A 3350 582214 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7254U 21401 LAST SECTION OF EEL STRIP AND AFT AIR STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. *S/D* CAUSE ATTRIBUTED TO POWER SUPPLY. REPLACED POWER SUPPLY FOR AFT SECTION OF EEL STRIP, OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1999111900586 19991119 00586 1999 11 19 99UAL900583 4 19991109 A 3460 COMPUTER SMITH INDUST 1689250601 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 29 389UA 0001069 24664 ON TAKEOFF, ALL ENGINE FAN SPEED INDICATIONS WERE LOST ON THE FLIGHT MANAGEMENT COMPUTER. *S/D* REPLACED THE FLIGHT MA NAGEMENT COMPUTER. THE DIGITAL FLIGHT COMPUTER SYSTEM TESTED, OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999111900587 19991119 00587 NM 1999 11 19 99UAL900584 1 19991105 A 5310 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AFT FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 26951 MAJOR REPAIR TO AFT LOWER FUSELAGE DUE TO TAIL CONTACTING RUNWAY AT TAKEOFF. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999111900588 19991119 00588 NM 1999 11 19 99UAL900585 1 19991107 A 2497 299112005014 WIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 31G FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 779UA 26941 EN ROUTE MUC-IAD, SPARKS OBSERVED AT SEAT CONTROL BOX UNDER SEAT 31G. *S/D* POWER CABLE FOR SEAT VIDEO UNIT CHAFED AGA INST THE SHROUD DOOR THAT PROTECTS THE SVU (SEAT VIDEO UNIT) AND CABLE CONECTION. CAUSE ATTRIBUTED TO CABLE ROUTING FRO M THE FLOOR TO THE SVU RESULTING IN PINCHED CABLE BETWEEN THE SVU DOOR AND THE FLOOR. THE METAL DOOR CUT THROUGH THE CA BLE INSULATION RESULTING IN AN ELECTRICAL SHORT. ENGINEERING ISSUED A FLEET INSPECTION TO CHECK FOR PROPER ROUTING AND CORRECT AS REQUIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999111900589 19991119 00589 NM 1999 11 19 99UAL900586 1 19991109 A 2910 1121S21095 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAP LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 7271U 21418 ON FLAP EXTENSION FROM 2 TO 5 LOST HYDRAULIC SYSTEM A FLUID. AIRCRAFT TOWED TO GATE. *S/D* REPLACED FLAP FLOW LIMITIN G VALVE PER MAINTENANCE MANUAL. LEAK CHECKED OK. SERVICED HYDRAULIC SYSTEM. RETURNED AIRCRAFT BACK TO NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999111900590 19991119 00590 NM 1999 11 19 99UAL900587 1 19991110 A 5610 WINDOW BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT UNSECURED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 661UA 27158 CAPTAIN'S WINDOW OPENED DURING TAKEOFF ROLL. RTO AT 120 KTS IAS. *S/D* FLIGHT DECK RT SLIDING WINDOW WAS NOT SECURED I N THE LOCKED POSITION. ACCOMPLISHED VISUAL CHECK OF THE WINDOW. 2 L 7 2 4F 4 F RT A1NM E24NE 1999111900591 19991119 00591 NM 1999 11 19 99UAL900588 1 19991109 A 5511 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HORIZ STAB MISDRILLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7453U 21907 DURING HEAVY MAINTENANCE A FASTENER HOLE COMMON TO THE RIGHT HAND HORIZONTAL STABILIZER ELEVATOR HINGE RIB WAS MISDRILL ED RESULTING IN A DOUBLE HOLE CONDITION. THE DISCREPANT HOLE WAS OVERSIZED TO A CLEAN ROUND CONDITION AND A FREEZE PLUG WAS INSTALLED PER TIMCO REPAIR INSTRUCTIONS. THIS REPAIR WAS APPROVED WITH AN 8110-3 BY TIMCO'S DER. 2 L 7 3 4F 4 F A3WE E2EA 1999111900592 19991119 00592 NE 1999 11 19 99UAL900589 2 19991111 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7447U 21901 SHUT DOWN NR 3 ENGINE DUE LOSS OF ENGINE OIL QUANTITY AND PRESSURE. 2 L 7 3 4F 4 F A3WE E2EA 1999111900593 19991119 00593 EU 1999 11 19 99UAL900590 1 19991110 A 3260 BOLT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 425UA 508 CREW REPORTED, UNABLE TO RETRACT GEAR AFTER TAKEOFF. RECEIVED LANDING GEAR NOT UPLOCKED AND SHOCK ABSORBER ECAM FAULTS. *S/D* TIGHTENED NLG BARREL FITTING BOLT FOR PROX SENSORS REF IPC 32-21-11-13 ITEM 60. SECURED WITH LOCK WASHER, OPER ATED LANDING GEAR, ALL INDICATIONS NORMAL. COA 403250 INITIATED TO CORRECT THIS PROBLEM. HOWEVER, IT WAS NOT ACCOMPLIS HED ON THIS AIRCRAFT TO DATE. A SECONDARY LOCKING FEATURE WAS INCLUDED WITH THE BOLT TO PREVENT THE BOLT FROM LOOSENING . 2 L 7 2 4F 4 F RT A28NM E40NE 1999111900594 19991119 00594 WP 1999 11 19 ABXA9900792 1 19991014 A 5753 5652287505N VANE DOUG DOUG DC8 DC862 3021970 WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT FLAP VANE ASSEMBLY WAS 50 PERCENT DELAMINATED. REPAIRED UNIT COMPLETE. 2 L 7 4 4F 4A25 1999111900595 19991119 00595 WP 1999 11 19 ABXA9900793 1 19991115 A 7921 15144051 VALVE DOUG DC8 DC861 3021952 WP NR 4 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 23 846AX 446 46158 NR 4 OIL TEMPERATURE WAS 150 DEGREES FOR 10 MINUTES. SHUT NR 4 ENGINE DOWN. AFTER ENGINE SHUT DOWN OIL TEMPERATURE AND QUANTITY DECREASED. OIL PRESSURE WAS 15 PSI AFTER SHUT DOWN. REPLACED NR 4 ENGINE OIL COOLER BYPASS VALVE. OPS AND L EAK CHECKED GOOD. 2 L 7 4 4F 4A25 1999111900596 19991119 00596 WP 1999 11 19 MWEA99810 1 19991116 A 5330 59114081 SKIN DOUG DC9 DC915 3022036 WP BS 435-158 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 DENT IN FUSELAGE AT STATION 435 BETWEEN LONGERON 6-7. ALSO, DENT IN FUSELAGE AT STATION 158 BETWEEN LONGERON 25-26. MT C FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1999111900597 19991119 00597 WP 1999 11 19 MWEA99811 1 19991116 A 5330 5911422 SKIN DOUG DC9 DC915 3022036 WP BS 389 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 REPAIR DOUBLER INSTALLED IN FUSELAGE SKIN, NO FILLER INSTALLED IN CUTOUT AT STATION 389 LEFT SIDE OF LONGERON. MTC REMO VED OLD DOUBLER AND FABRICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 1999111900598 19991119 00598 WP 1999 11 19 MWEA99812 1 19991116 A 5523 SKIN DOUG DC9 DC915 3022036 WP LT ELEV TAB DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT HAND ELEVATOR GEARED TAB HAS SMALL DENT ON TOP SURFACE. MTC FABRICATED AND INSTALLED DOUBLER FOR THE LEFT HAND ELE VATOR GEARED TAB. 2 L 7 2 4F A6WE 1999111900599 19991119 00599 WP 1999 11 19 MWEA99813 1 19991116 A 5320 991150020 STIFFENER DOUG DC9 DC915 3022036 WP BS 37 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 STIFFENER CRAKCED FUSELAGE STATION 37 UPPER RIGHT HAND CORNER AT THE 2 O'CLOCK POSITION. MTC REMOVED ANGLE THEN FABRICA TED AND INSTALLED NEW STIFFENER. 2 L 7 2 4F A6WE 1999111900600 19991119 00600 WP 1999 11 19 MWEA99814 1 19991116 A 5512 59121612 SKIN DOUG DC9 DC915 3022036 WP HORIZ STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 HORIZONTAL STABILIZER TO VERTICAL STABILIZER FAIRING ON RIGHT HAND SIDE UPPER WAS CHAFED AT AFT END, FAIRING SKIN WAS DA MAGED (OUT OF LIMITS). MTC REMOVED DAMAGED SKIN THEN DRILLED AND INSTALLED NEW SKIN. 2 L 7 2 4F A6WE 1999111900601 19991119 00601 WP 1999 11 19 MWEA99815 1 19991112 A 3350 100865 BATTERY PACK DOUG DC9 DC914 3022034 WP ROW 2-11 DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 700ME 45696 EMERGENCY FLOOR PATH LIGHTING INOPEATIVE BETWEEN ROW 2 TO ROW 11. MTC REMOVED AND REPLACED BATTER PACK. 2 L 7 2 4F A6WE 1999111900602 19991119 00602 WP 1999 11 19 MWEA99816 1 19991105 A 7711 LG80E1 EPR TRANSMITTER DOUG DC9 DC981 3022081 WP LT ENGINE FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 803ME 48029 LEFT EPR GAUGE FLAGGED AND FROZE IN PLACE AT 1.89. MTC REMOVED AND REPLACED LEFT EPR TRANSMITTER. 2 L 7 2 4F A6WE 1999111900603 19991119 00603 NM 1999 11 19 DL76L992486 1 19991110 A 3350 HARNESS BOEING 767 767332 1382001 NM ROW 22FG BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 SEAT MOUNTED PROX LIGHTING SYSTEM INOP AT 22FG. FOUND BROKEN WIRE AT SEAT HARNESS TO SIDEWALL CONECTOR. FWD TO MCO AND PLACARD PER MEL 33-51-03B. 2 L 7 2 4F RT A1NM 1999111900604 19991119 00604 NM 1999 11 19 DL76L992487 1 19991110 A 3350 LENS BOEING 767 767332 1382001 NM ROW 6AB MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 25143 SEAT MOUNTED PROXIMITY LIGHTING AT 6AB MISSING 1 LENS (WHITE) AND BOTH BULBS. RELAMPED LIGHT AND REPLACED MISSING BULBS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 1999111900605 19991119 00605 NM 1999 11 19 DL76L992488 1 19991110 A 2120 AIR DIST BOEING 767 767332 1382001 NM COCKPIT ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 198DN 28455 ABOUT ONE HOUR INTO FLIGHT THE SMELL (FAINT SMELL) OF PLASTIC BURNING WAS LOCATED IN THE AREA OF THE REAR OF THE AUX PANEL (BEHIND F/O'S SEAT) IT CONTINUED FOR ABOUT 5 MINS AND STOPPED. THERE WAS NO SMOKE FLT CNTRL NOTIFIED. REST O F FLIGHT OK. INSPECTED P61 AND P6 PANELS, INSIDE AND BEHIND. INSPECTED REMAINDER OF FLIGHT DECK. INSPECTED MAIN EQUIP MENT CENTER AND FWD EQUIPMENT CENTER. FOUND NO EVIDENCE OF OVERHEAT OR BURNING OF ANY MATERIAL. 2 L 7 2 4F RT A1NM 1999111900606 19991119 00606 NM 1999 11 19 DL72W992494 1 19991111 A 7331 POWER SUPPLY 8TJ88GAP4 BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 295WA DL0343 22532 FLIGHT ABORTED TAKEOFF DUE TO 115 VOLT AC. FUEL FLOW CIRCUIT BREAKER POPPED DURING TAKEOFF ROLL. REPLACED FUEL FLOW PO WER SUPPLY, PRECAUTIONARY. CHECKED OK ON ENGINE RUN. 2 L 7 3 4F 4 F A3WE E2EA 1999111900607 19991119 00607 NM 1999 11 19 DL72E992496 1 19991111 A 5754 WEB BOEING 727 727247 138408F NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FWD WEB CRACKED INSIDE NR 3 L/E SLAT AT ANTI-ICE DUCT. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS PER M/M 57-40-0 F IG 802 A. OK TO INSTALL. INSTALLED DOUBLER PER M/M 57-40-0 FIG 802 A. 2 L 7 3 4F A3WE 1999111900608 19991119 00608 NM 1999 11 19 DL72S992497 1 19991111 A 5320 WEB BOEING 727 727225 1384077 NM BS 1235 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 VERT WEB OF LT LOWER TORQUE BOX IN 48 SECTION CRACKED AT STA 1235 AT UPPER RIVET ROW .25 INCH. INSTALLED DOUBLER PER M/ M 53-11-0- NR 19, A-1 LETTER CHECK. 2 L 7 3 4F A3WE 1999111900609 19991119 00609 NM 1999 11 19 DL76G992499 1 19991111 A 2530 CHILLER 3488 BOEING 767 7673P6 1385105 NM GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 SO 27 1501P 24983 MID GALLEY CHILLER FAULT LIGHT ILLUMINATED, WALL BEHIND SEAT 10C SEAMED VERY HOT. TURNED OFF, WALL COOLED. CLEANED OUT LET AND VENT PORTS OF CHILLER, OPS CK OK. NO FAULT LIGHT OCCURRED. 2 L 7 2 4F RT A1NM 1999111900610 19991119 00610 1999 11 19 DLM88992500 4 19991112 A 3417 001048101 SWITCHING UNIT DOUG MD88 MD88 3023688 NM E/E COMP GOOD A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 909DL 1194 49540 ABORTED T/O AT 60 KTS DUE CAPTS A/S IND GOING TO ZERO WITH RED FLAGS APPEARING. REPLACED INST SWITCHING UNIT. CKD WIRI NG FROM NR 1 CADC TO SWITCHING UNIT, CKS GOOD. PERFORMED PITOT SYS TEST NR 1 CADC. ALL SYS CKS GOOD. 2 L 7 2 4F RT A6WE 1999111900611 19991119 00611 NM 1999 11 19 DL76G992501 1 19991112 A 3350 BATTERY PACK 20131A BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1501P 24983 LEFT EMERGENCY ESCAPE LIGHT DID NOT TEST WITH TEST SWITCH ON P-61 PANEL. REPLACED ASSOCIATED BATTERY PACK, ALL TEST OK. LOG B537394 ITEM 002. 2 L 7 2 4F RT A1NM 1999111900612 19991119 00612 NM 1999 11 19 DL72S992502 1 19991112 A 5754 65162221 SKIN BOEING 727 727232 1384082 NM LT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 SKIN CRACKED AT CORNER OF T DUCT HOLE. REPAIRED SKIN PER M/M 57-54-0, FIG 802A. 2 L 7 3 4F A3WE 1999111900613 19991119 00613 NM 1999 11 19 DL72S992503 1 19991112 A 5754 65162221 RIB BOEING 727 727232 1384082 NM LT LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 NR 8 RIB CRACKED IN CORNER OF RADIUS. REPAIRED RIB PER M/M 57-54-0, FIG 814. 2 L 7 3 4F A3WE 1999111900614 19991119 00614 NM 1999 11 19 DL72S992504 1 19991112 A 5754 65162221 RIB BOEING 727 727232 1384082 NM LT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 NR 11 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999111900615 19991119 00615 NM 1999 11 19 DL72S992505 1 19991112 A 5754 65162221 RIB BOEING 727 727232 1384082 NM LT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 OUTBOARD RIB CRACKED. REPAIRED PER M/M 57-54-0 FIG 814. 2 L 7 3 4F A3WE 1999111900616 19991119 00616 NM 1999 11 19 DLM88992506 1 19991112 A 2530 OVEN 50459 DOUG MD88 MD88 3023688 NM GALLEY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 912DE 49997 CREW REPORTED, BURNING SMELL FROM FWD PORTION OF CABIN, NO SMOKE. UNABLE TO DETERMINE LOCATION/ORIGIN OF FUMES. INSPEC TED CABIN OVHD AND GALLEY AREAS, STATIC PORT HEATERS, APU INLET AND OIL LEVEL. RAN PACKS WITH BOTH ENGINES. ONLY ODOR CAME FROM THE FWD GALLEY OVEN AREA. SUSPECT MEAL CARRIER MAY HAVE HAD PLASTIC DEBRIS MELTED TO EXTERIOR OF UNIT. UNPLU GGED CANNON PLUG AND PULLED/COLLARED C/B FOR OVEN. FWD TO MCO/PLAC PER MEL. 2 L 7 2 4F RT A6WE 1999111900617 19991119 00617 NM 1999 11 19 DL72L992507 1 19991112 A 5400 65312813 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 ON HEAVY WEIGHT HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT SUPPORT LT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT CH ORD ANGLE WITH ONE OF NEW MFG. 2 L 7 3 4F A3WE 1999111900618 19991119 00618 NM 1999 11 19 DL72L992508 1 19991113 A 5400 65312814 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 ON HEAVY WEIGHT HUSH-KIT MOD, FOUND RT AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ON E OF NEW MFG. 2 L 7 3 4F A3WE 1999111900619 19991119 00619 NM 1999 11 19 DLM88992509 1 19991113 A 2530 50459 OVEN DOUG MD88 MD88 3023688 NM GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 968DL 53161 IN FLIGHT FWD AND AFT OVENS GENERATED SMOKE WHEN USED. REMOVED FOOD CARRIER FROM FWD OVEN WITH INTRACOMPANY SHIPPING OR DER NR N 132323 TAPED TO SIDE OF CARRIER AND CLEANED FOOD DEBRIS FROM AFT OVEN. SHIPPING TICKET SHOWED EVIDENCE OF BURN ING. 2 L 7 2 4F RT A6WE 1999111900620 19991119 00620 NM 1999 11 19 DLM88992510 1 19991114 A 2530 50459 OVEN DOUG MD88 MD88 3023688 NM GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 985DL 53312 ELECTRICAL / PLASTIC FUMES. SUSPECTED SOURCE FORWARD GALLEY OVEN WAS NOT ON AT THE TIME. FOUND PLASTIC SHIPPING TAG ST ILL ON FWD GALLEY OVEN LINER. REMOVED LINER, RAN OVENS. CHECKS OK. 2 L 7 2 4F RT A6WE 1999111900621 19991119 00621 NM 1999 11 19 DL72S992512 1 19991114 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 6734 21432 ON L/O, FOUND LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT STROBING. REPLACED BATTERY PACK, CKS OK. 2 L 7 3 4F A3WE 1999111900622 19991119 00622 NM 1999 11 19 DL72K992513 1 19991114 A 3350 SIGN 900835A BOEING 727 727232 1384082 NM GALLEY INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 526DA 1297 21586 FWD EMER EXIT SIGN DOES NOT ILLUMINATE DURING TEST. 2 L 7 3 4F A3WE 1999111900623 19991119 00623 NM 1999 11 19 DL72S992514 1 19991114 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 7735 21470 FOUND ON LAYOVER AFT EMERGENCY CEILING LIGHT STROBING. REPLACED BATTERY CHARGER AND BATTERY. 2 L 7 3 4F A3WE 1999111900624 19991119 00624 NM 1999 11 19 DL76L992516 1 19991114 A 2610 MONITOR BOEING 767 767332 1382001 NM CABIN INOP A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 171DN 24759 BULKHEAD MONITOR AT 1A CAME ON BY ITSELF IN FLT, WOULD NOT SHUT OFF, GAVE ELEC SMELL WHEN IT FIRST CAME ON. SYSTEM TES TED.NIL ELECTICAL SMELL. MONITOR VERIFIED UNABLE TO SWITCH OFF. MONITOR TESTED IN OTHER LOCATION. FAULT STAYS WITH MO NITOR. MCC INFORMED REQUEST DEACTIVATION OF MONITOR 1A. ALSO, CONFIRM DEACTIVATION OF MONIOTR 1A, VERIFIED WITH MCC. 2 L 7 2 4F RT A1NM 1999111900625 19991119 00625 NM 1999 11 19 DHL99742004 1 19991116 A 2780 CONNECTOR BOEING 727 727225 1384077 NM NR 1 LE SLAT LOOSE A DHLA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 742DH 21290 ON FLAP RETRACTION , NR 1 SLAT LIGHT AND L/E FLAPS LIGHT AMBER AT FLAPS 2. RESEATED CANNON PLUG ON NR 1 SLAT ACUATOR. C YCLED FLAPS SEVERAL TIMES, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1999111900626 19991119 00626 NM 1999 11 19 VNAA9911009 1 19991112 A 7714 3033509 NL PROBE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 426JS 3038 116110 DURING CLIMBOUT, THE FLIGHT CREW RECEIVED A CAS MESSAGE INDICATING AN ENGINE MISCOMPARE. THE AIRCRAFT RETURNED TO THE F IELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NL PROBE SENSOR IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 77-14-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111900627 19991119 00627 NM 1999 11 19 VNAA9911010 1 19991113 A 3250 FAIL MESSAGE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING ACTIVATED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 461PS 3075 FLIGHT 4032 WAS ON FINAL WHEN THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND A NOSE WHEEL POWER UP FAIL CA S MESSAGE. THE CREW EXECUTED A GO-AROUND. WHEN THE GEAR WAS RETRACTED THE CAS MESSAGES CLEARED. FLIGHT 4032 EXECUTED A SECOND APPROACH AND LANDED WITHOUT FURTHER INCIDENT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111900628 19991119 00628 EU 1999 11 19 RAIA9911018 1 19991106 A 2121 M4941Z1A FAN BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 860AE 860 4756-FAT RECIRC FAN INOP. MAINTENANCE REPLACED RECIRC FAN. 2 L 7 2 4T RT A56EU 1999111900629 19991119 00629 1999 11 19 UF6A990101 4 19990101 A 3420 3085003206 SLEEVE BAG ATP ATP EU EFIS SHORTED A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 851AW 2020 ORD - FLT 5700 - REQUEST INSPECTION OF BURNING SMELL IN COCKPIT. MAINTENANCE INSPECTED AND REPLACED SHORTED PBSI SLEEVE ON NR 1 EFIS RECONFIGURATION PANEL. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999111900630 19991119 00630 EU 1999 11 19 UF6A990402 1 19990410 A 2926 JD290J0047002 RESERVOIR BAG ATP ATP EU NLG WW UNDERSERVICED A UF6A A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 GL 31 855AW 14657 2029 ORD - FLT 5764 - HYDRAULIC LOW LEVEL CWP WITH MAIN LEGEND INDICATION ILLUMINATED. MAINTENANCE BLED AUXILIARY RESERVOIR AND SERVICED SYSTEM. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999111900631 19991119 00631 NE 1999 11 19 UF6A990317 2 19990325 A 7320 CONNECTOR BAG ATP ATP EU PWA PW120 PW126A NE EEC CONTAMINATED A UF6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 859AW 2036 124242 ORD - FLT 5742 - NR 1 ENGINE TORQUE NH AND NL OCCILATES DURING CLIMB. MAINTENANCE INSPECTED THE NR 1 ENGINE RIGGING AN D CLEANED THE EEC CONNECTIONS. PERFORMED POWER ASSURANCE RUNS. NO DEFECTS NOTED. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999111900632 19991119 00632 NE 1999 11 19 UF6A990201 3 19990201 A 6111 786350R4D BLADE BAG ATP ATP EU HAMSTD 5500 65500F1 NE NR 2 ENGINE DAMAGED A UF6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 859AW 2036 GRB - FLT 5764 - PROP DE-ICE CWP WITH NR 2 PROP PBSI ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AND NR 6 BL ADE ON THE NR 2 ENGINE DUE TO LOW RESISTANCE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 6 C P13NE 1999111900633 19991119 00633 EU 1999 11 19 UF6A990309 1 19990310 A 2420 TRU BAG ATP ATP EU E/E BAY FAILED A UF6A O OTHER O OTHER NR NOT REPORTED 1 GL 31 857AW 2034 ORD - FLT 5712 - NR 1 TRU AND INVERTER FAILED IN FLIGHT. MAINTENANCE PERFORMED OPS CHECK OF SYSTEM. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999111900635 19991119 00635 EU 1999 11 19 VTZA1999019 1 19990630 A 2120 UNKNOWN BAG JETSTM JETSTM3201 1500217 EU COCKPIT SMOKE A VTZA A C UNSCHED LANDING ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 474UE 849 FLT 7324 - IAD-ROC - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO SMOKE IN CABIN. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND CHECKED FLOWS. MAINTENANCE COULD NOT D UPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900636 19991119 00636 EA 1999 11 19 VTZA9909427 1 19990618 A 3234 7179015 SELECTOR CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 627BR 7233 FLT 7719 - IAD-JAX - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR DISAGREE LIGHT ILLUMINATED. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED GEAR SELECTOR CONTROL. MAI NTENANCE PERFORMED GEAR SWINGS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999111900638 19991119 00638 EU 1999 11 19 VTZA9909429 1 19990620 A 7720 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE CONTAMINATED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 477UE 890 FLT 7400 - RIC-IAD - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE EGT ONLY MADE 450 DEGREES. AIRCRAFT RE TURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND LEANED ZONE 2 CANNON PLUG. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900639 19991119 00639 EA 1999 11 19 VTZA990192 1 19990622 A 3150 860D10018 EICAS CNDAIR CL600 CL6002B19 EA E/E BAY FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 639BR 7313 FLT 7804 - ORD-CRW - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AND DIVERTED TO CVG DUE TO FLAP FAIL MESSAGE ON EICAS. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLAP COMPUTER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999111900640 19991119 00640 EA 1999 11 19 VTZA990193 1 19990624 A 5610 601B330334 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A VTZA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 632BR 7268 FLT 7791 - IAD-SAV - DURING CRUISE, AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO CAE DUE TO SMOKE IN COCKPIT. CREW DE PLOYED OXYGEN MASKS. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND RIGHT SIDE WINDOW CRACKED AND WINDOW HEAT TERMINAL BLOCK SMELLED LIKE SMOKE. MAINTENANCE REMOVED AND REPLACED RIGHT SIDE WIND OW AND TEMP CONTROLLER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999111900641 19991119 00641 EA 1999 11 19 99ZZZM751 1 19990624 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A VTZA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 632BR 7268 FLT 7791 - IAD-SAV - DURING CRUISE, AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO CAE DUE TO SMOKE IN COCKPIT. CREW DE PLOYED OXYGEN MASKS. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND RIGHT SIDE WINDOW CRACKED AND WINDOW HEAT TERMINAL BLOCK SMELLED LIKE SMOKE. MAINTENANCE REMOVED AND REPLACED RIGHT SIDE WIND OW AND TEMP CONTROLLER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999111900642 19991119 00642 EA 1999 11 19 VTZA990204 1 19990704 A 5270 DOOR CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 627BR 7233 FLT 7186 - SGF-ORD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NLG DOOR WARNING LIGHT ILLUMINATED. AI RCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED CYCLED NLG DOORS AND FOUND NO DEFECT S. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999111900643 19991119 00643 EU 1999 11 19 VTZA990203 1 19990702 A 3242 BRAKES BAG JETSTM JETSTM3201 1500217 EU MLG MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 EA 27 496UE 900 FLT 7445 - MDT-IAD - DURING TAKEOFF, CREW ABORTED TAKEOFF DUE TO AIRCRAFT VEERING LEFT DURING TAKEOFF DISPITE FULL RIGHT RUDDER AND TILLER INPUTS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CHECKED BRAKE S AND SERVICED TIRES AND PERFORMED HIGH SPEED TAXI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900644 19991119 00644 EU 1999 11 19 VTZA990202 1 19990702 A 2910 AN82416D TEE BAG JETSTM JETSTM3201 1500217 EU COCKPIT LEAKING A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 482UE 897 FLT 7650 - IAD-SYR - DURING APPROACH, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS BOTH HYDRAULICS SYSTEM DRO PPED TO 0 PSI UPON LANDING GEAR EXTENSION. AIRCRAFT LANDED WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTE D AND REMOVED AND REPLACED TEE FITTING AND TWO CHECK VALVES UNDERNEATH RT ACM PANEL. OPS CHECK OK. AIRCRAFT RELEASED A ND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900645 19991119 00645 EU 1999 11 19 99ZZZM752 1 19990702 A 2910 HTE400004 VALVE BAG JETSTM JETSTM3201 1500217 EU COCKPIT LEAKING A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 482UE 897 FLT 7650 - IAD-SYR - DURING APPROACH, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS BOTH HYDRAULICS SYSTEM DRO PPED TO 0 PSI UPON LANDING GEAR EXTENSION. AIRCRAFT LANDED WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTE D AND REMOVED AND REPLACED TEE FITTING AND TWO CHECK VALVES UNDERNEATH RT ACM PANEL. OPS CHECK OK. AIRCRAFT RELEASED A ND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900646 19991119 00646 EU 1999 11 19 99ZZZM753 1 19990702 A 2910 400005 TEE BAG JETSTM JETSTM3201 1500217 EU COCKPIT LEAKING A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 482UE 897 FLT 7650 - IAD-SYR - DURING APPROACH, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS BOTH HYDRAULICS SYSTEM DRO PPED TO 0 PSI UPON LANDING GEAR EXTENSION. AIRCRAFT LANDED WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTE D AND REMOVED AND REPLACED TEE FITTING AND TWO CHECK VALVES UNDERNEATH RT ACM PANEL. OPS CHECK OK. AIRCRAFT RELEASED A ND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900648 19991119 00648 EU 1999 11 19 VTZA990200 1 19990630 A 3220 NLG BAG JETSTM JETSTM3201 1500217 EU NOSE MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 493UE 805 FLT 7317 - IAD-CHO - DURING TAKEOFF, AIRCRAFT RETURNED TO IAD AND MADE AN UNSCHEDULED LANDING DUE TO NOSE LANDING GEAR N OT LOCKING IN THE UP POSITION. MAINTENANCE SERVICED NOSE STRUT AND PERFORMED NUMEROUS GEAR SWINGS. OPS CHECK GOOD. AI RCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900649 19991119 00649 EU 1999 11 19 VTZA990215 1 19990708 A 3240 S214161K INDICATOR BAG JETSTM JETSTM3201 1500217 EU BRAKE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 471UE 821 FLT 7324 - IAD-ROC - DURING LANDING, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS WITH BRAKES APPLIED BRAKE P RESSURE GAUGE READ ZERO. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED D MI 45651, MEL 32-1. MAINTENANCE CLOSED DMI 45651 ON 7-9-99 BY REMOVING AND REPLACING PRESSURE INDICATOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999111900650 19991119 00650 1999 11 19 EISA99174 4 19991006 A 2565 13621224 SLIDE BFGOODRICH 300117225 DOUG DC9 DC931 3022065 WP TAILCONE FAILED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 8003 47066 TAILCONE SLIDE DEPLOYMENT BOTTLE LOW PRESSURE. REPLACED SLIDE. (M) 2 L 7 2 4F A6WE 1999111900651 19991119 00651 NM 1999 11 19 EISA99177 1 19991008 A 2612 655449915 FIRE WARNING BOEING 727 727225 1384077 NM COCKPIT FAILED A EISA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 07 352PA R00414 20616 FIRE BELL DOES NOT SOUND IN EITHER ENGINE FIRE OR APU FIRE TEST. REMOVED AND REPLACED FIRE AND OVERHEAT ACCESSORY PANEL . NO HELP. REMOVED AND REPLACED AURAL WARNING BOX FIRE TEST IAW MM 26-14-11. (M) 2 L 7 3 4F A3WE 1999111900652 19991119 00652 NM 1999 11 19 EISA99190 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 480 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 19L. FABRICATED NEW CLI P PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999111900653 19991119 00653 NM 1999 11 19 EISA99189 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 500 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 500 STRINGER 19R. FABRICATED NEW CLI P PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999111900654 19991119 00654 NM 1999 11 19 A6WA9900116 1 19991014 A 3320 325310 BALLAST DORNER DO32 DO328100 2996000 NM ROW 9A FAILED A A6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 328PH 3006 FLT 7069 - DEN-GJT - STRONG ODOR AND HAZE/SMOKE IN CABIN. INSPECTED CABIN AND FOUND BALLAST UNIT ABOVE SEAT 9A HAD FAIL ED. REMOVED BALLAST UNIT BECAUSE OF STRONG ODOR AND MEL'D INTERIOR LIGHT. (M) 2 H 7 2 4T RT A45NM 1999111900655 19991119 00655 EU 1999 11 19 A6WA9900118 1 19991013 A 4930 B-NUT BAG BAE146 BAE146200A 1500266 EU APU LOOSE A A6WA O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS IN INSP/MAINT 1 GL 31 608AW E2049 AT GATE BEFORE DEPARTURE, WHEN CREW DID PREFLIGHT, STRONG FUEL SMELL IN CABIN AND COCKPIT WITH APU BLEED AIR ON. FOUND APU FUEL SOLENOID B-NUT LOOSE, LEAKING FUEL, TIGHTENED PERFORMED PACK BURNOUT. NO SMELL NOTED. (M) 2 H 7 4 4F RT A49EU 1999111900656 19991119 00656 EA 1999 11 19 A6WA9900117 1 19991015 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 401AW 7280 FLT 5617 - MEM - PASSENGER DOOR LATCH CAUTION CASS, FOLLOWED BY PASSENGER DOOR WARNING CASS. PERFORMED OPS CHECK NUMERO US TIMES, COULD NOT DUPLICATE. (M) 2 L 7 2 4F RT A21EA 1999111900657 19991119 00657 SO 1999 11 19 ASOA99110 1 19991003 A 2150 22045402 ACM EMB 120 EMB120RT SO CABIN INOPERATIVE A ASOA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 11 243AS 120072 FLT 4219 - ON TAKEOFF, SMOKE FILLED THE CABIN. CREW REMOVED BATTERY FROM SMOKE DETECTOR TO SILENCE ALARM AND RETURNED T O THE GATE. MAINTENANCE REMOVED AND REPLACED THE ACM AND GROUND COOLING FAN. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999111900658 19991119 00658 SO 1999 11 19 ASOA99108 1 19990929 A 3620 WARNING LIGHT EMB 120 EMB120RT SO RT BLEED AIR ILLUMINATED A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN N J FALSE WARNING WARNING INDICATION CL CLIMB 1 SO 11 215AS 120010 FLT 4241 - APPROX 15 MINUTES AFTER DEPARTING ATL AND 30 NM WEST THE RIGHT ENGINE BLEED AIR 'DUCT LEAKAGE' WARNING LIGHT ILLUMINATED. WE WENT THROUGH THE 'DUCT LEAK LIGHT ILLUMINATED' CHECKLIST WHILE BEING VECTORED BACK TO ATL. THE LIGHT F AILED TO EXTINGUISH, SO CAPTAIN SHUTDOWN THE RIGHT ENGINE. AS A PRECAUTION, CREW REQUESTED THAT THE FIRE EQUIPMENT STAN DBY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN ENGINE THREE TIMES, BUT COULD NOT DUPLICATE DISCREPANCY. MTC CHECKED THE DUCT LIGHT SENSORS ON THE LEADING EDGE AND SIDE PANEL. ALL SENSORS WERE GOOD. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1999111900659 19991119 00659 1999 11 19 99ZZZM754 4 19991011 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT MALFUNCTIONED A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 101UX UE101 CAPTAINS ALTIMETER WAS REPORTED TO BE 100 TO 200 FEET OFF AT ALL ALTITUDES. REMOVED AND REPLACED ALTIMETER. SYSTEM TES TS SATISFACTORY. SUBSEQUENT BENCH TESTS FOUND THAT THE ALTIMETER WAS INDICATING 100 FEET HIGH AND THAT THE MILIBAR INDI CATION DID NOT COINCIDE WITH THE INCHES OF MERCURY DICATION. THIS WAS A SECOND SUCH FAILURE OF THIS INSTRUMENT IN THE P AST 6 MONTHS OF OPERATION. (M) 2 L 7 2 4T RT A24CE 1999111900660 19991119 00660 NM 1999 11 19 MASA99164 1 19990913 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 FLT 6258 - PHX-PSP - DURING STANDARD PREFLIGHT CHECK, THE CREW NOTED THE FORWARD EMERGENCY EXIT LIGHT WAS INOPERATIVE. M AINTENANCE WAS CALLED OUT AND REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999111900661 19991119 00661 1999 11 19 99ZZZM755 4 19991003 A 6122 8210410 PROP GOVERNOR BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 845CA 2701268 UE47 RIGHT PROP RPM SURGED TO 1800 RPM AT TAKEOFF SETTING. UNIT REPLACED, GROUND RUN AND TEST FLIGHT PERFORMED. (M) 2 L 7 2 4T RT A24CE 1999111900662 19991119 00662 EU 1999 11 19 REXA99031 1 19991001 A 2421 J221P147 O-RINGS SAAB SF340 SF340A 7850100 EU LT ENGINE DAMAGED A REXA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 25 403BH 340A060 DECLARED EMERGENCY FOR LEFT OIL PRESSURE. HAD CWP AND GAUGE WARNING. REMOVED AND REPLACED LEFT ENGINE ALTERNATOR O-RIN G DUE TO CUT, GROUND RAN CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1999111900663 19991119 00663 EU 1999 11 19 REXA99030 1 19991002 A 2913 4018502 PUMP SAAB SF340 SF340A 7850100 EU HYD SYSTEM FAILED A REXA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 25 112PX AH93432 340A025 LOSS OF ELECTRIC HYDRAULIC PUMP MANUAL AND OVERRIDE. EMERGENCY LANDING. SWAPPED INTO 401. REMVOED AND REPLACED ELECTR IC HYDRAULIC PUMP IAW AMM 29-10-00. NO LEAKS NOTED. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1999111900664 19991119 00664 EU 1999 11 19 C2XA99BT095 1 19991005 A 3297 D231970000 WIRE HARNESS AEROSP ATR72 ATR72212 EU LANDING GEAR FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 69902 385 EWR - FLT 3421 - CRWE REPORTED LANDING GEAR TAKES 30 PLUS SECONDS TO RETRACT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND AND REPAIRED A BROKEN WIRE AT PIN A OF CANNON PLUG 51GB AND REPAIRED BROKEN WIRE AT PIN C OF CANNON PLUG 50GB. REMOVED AND REPLACED LEFT MAIN LANDING GEAR SYSTEM ONE PROXIMITY SWITCH WOW HARNESS. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999111900665 19991119 00665 SO 1999 11 19 C2XA99BT093 1 19991005 A 2611 CONNECTOR EMB 145 EMB145ER SO BAGG COMP CORRDOED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 14943 145040 EWR - FLT 4130 - CREW REPORTED BAGGAGE SMOEK EICAS MESSAGE IN FLIGHT. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE CLEANE D CORROSION AT CANNON PLUG OF NR 2 SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999111900666 19991119 00666 SO 1999 11 19 C2XA99BT092 1 19990929 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 EWR - FLT 4145 - DURING SERVICE CHECK, FOUND REAR PORTION OF EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK. OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999111900667 19991119 00667 SO 1999 11 19 C2XA99IA517 1 19990930 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14974 145161 IAH - DURING A-CHECK INSPECTION, THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 33-50-50, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999111900668 19991119 00668 SO 1999 11 19 C2XA99IA516 1 19990929 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14974 145161 CLE - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999111900669 19991119 00669 EU 1999 11 19 C2XA99IA515 1 19990929 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17448 506 EFD - DURING MAINTENANCE INSPECTION, THE AFT CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR42-500 MM 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999111900670 19991119 00670 GL 1999 11 19 C2XA99TY001 2 19990913 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 15941 5177 145035 CAE310020 EWR - FLT 4133 - CREW REPORTED THAT THEY ABORTED TAKEOFF DUE TO HIGH OIL PRESSURE ON THE RIGHT ENGINE. THE AIRCRAFT WAS MAINTENANCE FERRIED TO TYS AND THE RIGHT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL CHECK WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999111900671 19991119 00671 NM 1999 11 19 AALA991364 1 19990908 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 540 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND SHEAR TIE CORRODED STATION 540 BETWEEN STRINGER 27R AND 28R. REMOVED AND REPLACED SHEAR TIE AT STATION 540 PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1999111900672 19991119 00672 NM 1999 11 19 AALA991363 1 19990908 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 540 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - SHEAR TIE CORRODED AT STATION 540 OUTBOARD OF STRINGER 27R. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-1 PAGE 4 . (M) 2 L 7 3 4F A3WE 1999111900673 19991119 00673 NM 1999 11 19 AALA991362 1 19990909 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 541-560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON STRINGER 28R 541 TO 560. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED STRINGER REPAIRS PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999111900674 19991119 00674 NM 1999 11 19 AALA991361 1 19990908 A 5320 FITTING BOEING 727 727227 1384078 NM BS 540 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND STRINGER TIE FITTING CORRODED STATION 540 STRINGER 26R. REMOVED AND REPLACED FITTING PER SRM 51-10-1 PAGE 4 AT STATION 540 STRINGER 26R. (M) 2 L 7 3 4F A3WE 1999111900675 19991119 00675 NM 1999 11 19 AALA991352 1 19990831 A 5260 WEB BOEING 727 727227 1384078 NM VENTRAL STAIRS CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - VENTRAL STAIRS, RIGHT LOWER TORQUE BOX, CRACK IN WEB AT LIGHTING HOLE, STATION 1223. INSTALLED DOUBLER PER SRM 51 -40-02. DOUBLER .050 2024T3. INSTALLED WITH 13 .5/32 D-RIVETS. (M) 2 L 7 3 4F A3WE 1999111900676 19991119 00676 NM 1999 11 19 AALA991351 1 19990831 A 5260 WEB BOEING 727 727227 1384078 NM VENTRAL STAIRS CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - VENTRAL STAIRS, LEFT LOWER TORQUE BOX, CRACK IN WEB AT LIGHTING HOLE, STATION 1243. INSTALLED DOUBLER PER SRM 51- 40-2. DOUBLER .050 2024T3, INSTALLED WITH 14 5/32 D-RIVETS. (M) 2 L 7 3 4F A3WE 1999111900677 19991119 00677 NM 1999 11 19 AALA991350 1 19990908 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - LEFT LOWER WING SKIN HAS CORROSION IN AREA OF 4C, LBL 30/38/40, ABOVE PRIMARY HEAT EXCHANGER. REMOVED CORROSION, TREATED AND PRIMED. INSTALLED DOUBLER REPAIR PER SRM 57-30-3 FIG 6, SH 2. (M) 2 L 7 3 4F A3WE 1999111900678 19991119 00678 NM 1999 11 19 AALA991349 1 19990903 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 5300-5800 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON TOP OF FLOORBEAM AT 1127L, STATION 5300 TO 5800. REMOVED CORROSION AND INSTALLED T-ANGLE REPLA CEMENT PER SRM 53-12-10-1. (M) 2 L 7 3 4F A3WE 1999111900679 19991119 00679 NM 1999 11 19 AALA991348 1 19990907 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION STRINGER 28 RIGHT STATION 700. FABRICATED AND INSTALLED REPAIR STRINGER AND SPLICES PER SRM 53-10 -3. (M) 2 L 7 3 4F A3WE 1999111900680 19991119 00680 NM 1999 11 19 AALA991347 1 19990908 A 5315 STRINGER BOEING 727 727227 1384078 NM BS 481-482 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON STRINGER 28L STATION 481-482. CUT AND REMOVED 3 INCH SECTION OF STRINGER 28L. INSTALLED STRIN GER SPLICE REPAIR PER ESO 11697, DATED 9-1-99. (M) 2 L 7 3 4F A3WE 1999111900681 19991119 00681 NM 1999 11 19 AALA991346 1 19990908 A 5320 SPLICE BOEING 727 727227 1384078 NM BS 480-486 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON STRINGER SPLICE STRINGER 28L STATION 480 TO 486. REMOVED STRINGER SPLICE AND INSTALLED STRINGE R SPLICE REPAIR PER ESO 11697, DATED 9-1-99. (M) 2 L 7 3 4F A3WE 1999111900682 19991119 00682 NM 1999 11 19 AALA991345 1 19990908 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720-740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON 23 LEFT STATION 720F - STATION 740. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999111900683 19991119 00683 NM 1999 11 19 AALA991344 1 19990907 A 5330 SKIN BOEING 727 727227 1384078 NM BS 696-704 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND FUSELAGE SKIN GOUGED BELOW STRINGER 28R STATION 696-704. BLENDED, INSTALLED DOUBLER OVER DAMAGED AREA PER S RM 53-30-3. (M) 2 L 7 3 4F A3WE 1999111900684 19991119 00684 NM 1999 11 19 AALA991343 1 19990908 A 5330 SKIN BOEING 727 727227 1384078 NM BS 685-690 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND STATION 685-690 STRINGER 25L FUSE SKIN BULGING AT SEVERAL RIVETS. CUTOUT CORRODED SECTION OF SKIN. INSTALL ED DOUBLER PER SRM 53-30-3 FIGURE 3A. (M) 2 L 7 3 4F A3WE 1999111900685 19991119 00685 NM 1999 11 19 AALA991342 1 19990908 A 5330 SKIN BOEING 727 727227 1384078 NM BS 695 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND STATION 695, STRINGER 24L, SKIN BULGING AT RIVET. CUTOUT CORRODED SECTION OF SKIN. INSTALLED DOUBLER PER S RM 53-30-3 FIG 3A. (M) 2 L 7 3 4F A3WE 1999111900686 19991119 00686 NM 1999 11 19 AALA991341 1 19990908 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND FUSELAGE SKIN CRACKED (BULGED) AT RIGHT RAM AIR ROD, STATION 720B PLUS 5 INCHES, BELOW STRINGER 28R. CUT OU T DAMAGE IN SKIN 2 INCHES BY 4 INCHES. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999111900687 19991119 00687 NM 1999 11 19 AALA991340 1 19990830 A 5330 SKIN BOEING 727 727227 1384078 NM BS 235-250 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND SKIN CRACKED AROUND FASTENER HEADS AT SECOND FASTENER ROW BELOW LEFT NR 3 COCKPIT WINDOWS STATION 235-STATIO N 250. INSTALLED REPAIR DOUBLER PER ESO 11697 (M) 2 L 7 3 4F A3WE 1999111900688 19991119 00688 NM 1999 11 19 AALA991339 1 19990908 A 5330 SKIN BOEING 727 727227 1384078 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND SKIN BULGED FASTENER HEADS POPPED STATION 480-482 FROM STRINGER 28L TO 2 INCHES OUTBOARD. CUT AND REMOVED C ORRODED SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3A. (M) 2 L 7 3 4F A3WE 1999111900689 19991119 00689 NM 1999 11 19 AALA991441 1 19990915 A 5330 SKIN BOEING 727 727223 1384074 NM BS 999-1003 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 870AA 21382 TUL - FOUND BULGE IN SKIN LAP 26L FROM BS 990 PLUS 9 INCHES TO 990 PLUS 13 INCHES. REMOVED CORRODED PORTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999111900690 19991119 00690 NM 1999 11 19 AALA991440 1 19990917 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 870AA 21382 TUL - FOUND BELTFRAME DRILLED INTO 4 PLACES UPPER LEG STATION 560 BETWEEN STRINGER 28R AND 27R. INSTALLED DOUBLERS PER AARD 51-40-1. (M) 2 L 7 3 4F A3WE 1999111900691 19991119 00691 NM 1999 11 19 AALA991439 1 19990917 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 870AA 21382 TUL - FOUND DEEP GOUGE IN SKIN AT STATION BETWEEN STRINGERS 1 AND 2R. CUT OUT DAMAGED AREA AND INSTALLED DOUBELR PER SR M 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900692 19991119 00692 NM 1999 11 19 AALA991438 1 19990917 A 5330 SKIN BOEING 727 727223 1384074 NM BS 660 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 870AA 21382 TUL - FOUND GOUGE IN SKIN AT STATION 660 BETWEEN STRINGER 1 AND 2R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900693 19991119 00693 NM 1999 11 19 AALA991437 1 19990917 A 5711 SPAR BOEING 727 727223 1384074 NM WS 519 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 870AA 21382 TUL - FOUND CORROSION ON LOWER SPAR CHORD BELOW NR 6 SLAT ACTUATOR. INSTALLED REPAIR STRAP IAW AARD 57-30-00-2 PAGES 1- 3. (M) 2 L 7 3 4F A3WE 1999111900694 19991119 00694 WP 1999 11 19 AALA991496 1 19990924 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 655 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - FOUND MAIN CABIN FLOORBEAM HAS WORN AREA STATION 655 RIGHT 1 INCH. BLENDED DAMAGE FROM BOTTOM OF FLOORBEAM STATIO N 655, FABRICATED REPAIR ANGLE AND INSTALLED PER AARD 53-20-00-21. (M) 2 L 7 2 4F A6WE 1999111900695 19991119 00695 WP 1999 11 19 AALA991495 1 19990920 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 794 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - FOUND NR 3 SEAT TRACK CORRODED AT STATION 794. CUT OUT DAMAGED SEAT TRACK FROM STATION 755 AND 815. INSTALLED NE W SEAT TRACK PER SRM 53-5 FIG 4F-1, 4F-2. (M) 2 L 7 2 4F A6WE 1999111900696 19991119 00696 WP 1999 11 19 AALA991494 1 19990920 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - FOUND LONGERON 4L CRACKED AT BELLFRAME 160. REPAIRED LONGERON PER SRM 53-02 PAGE 48 FIG 18. (M) 2 L 7 2 4F A6WE 1999111900697 19991119 00697 WP 1999 11 19 AALA991493 1 19990924 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 733 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - NR 3 SEAT TRACK HAS CORROSION STATION 733. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 PART 1 FIG 4A. (M) 2 L 7 2 4F A6WE 1999111900698 19991119 00698 WP 1999 11 19 AALA991492 1 19990924 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 792-795 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - FOUND SEAT TRACK NR 6 HAS CORROSION STATION 792-795. SPLICED SEAT TRACK AT STATION 730 PER SRM 53-05 PART 1 FIG 4 F SHEET 2 THROUGH 11 PAGE 10K THROUGH 10. (M) 2 L 7 2 4F A6WE 1999111900699 19991119 00699 WP 1999 11 19 AALA991491 1 19990924 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1203 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - FOUND NR 2 SEAT TRACK HAS CORROSION IN CHANNEL. REPAIRED TRACK WITH 3 LIP PLUG REPAIR PER SRM 53-05 PART 1 PAGE 8 C SHEET 1 FIG 4A. (M) 2 L 7 2 4F A6WE 1999111900700 19991119 00700 WP 1999 11 19 AALA991462 1 19990827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 609 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND NR 6 SEAT TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999111900701 19991119 00701 WP 1999 11 19 AALA991461 1 19990827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 579 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND NR 6 SEAT TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999111900702 19991119 00702 WP 1999 11 19 AALA991459 1 19990827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 484 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND NR 6 SEAT TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999111900703 19991119 00703 WP 1999 11 19 AALA991458 1 19990827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 547 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND NR 6 SEAT TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999111900704 19991119 00704 WP 1999 11 19 AALA991457 1 19990827 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 517 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND NR 6 SEAT TRACK CORRODED. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999111900705 19991119 00705 NM 1999 11 19 MZZA99151 1 19990802 A 5752 SKIN BOEING 727 727227 1384078 NM LT ELEV TAB DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY 1 INCH DELAMINATION WAS FOUND ON LEFT ELEVATOR TAB SKIN AT LEFT ELEV STATION 117. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAP 51-40-06. (M) 2 L 7 3 4F A3WE 1999111900706 19991119 00706 NM 1999 11 19 MZZA99150 1 19990805 A 5753 SKIN BOEING 727 727227 1384078 NM RT TE MIDFLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.75 INCH BY .875 INCH AREA CORROSION WAS FOUND ON RIGHT INBO ARD MIDFLAP SKIN. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 57-50-04 FIG 2. (M) 2 L 7 3 4F A3WE 1999111900707 19991119 00707 NM 1999 11 19 MZZA99149 1 19990731 A 5753 SKIN BOEING 727 727227 1384078 NM RT TE FOREFLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2.5 INCH LONG CRACK WAS FOUND ON RIGHT OUTBOARD FOREFLAP NOSE SKIN AT WBL 442. THE CRACK END WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 57-50-04 FIG 7. (M) 2 L 7 3 4F A3WE 1999111900708 19991119 00708 NM 1999 11 19 MZZA99147 1 19990804 A 5320 STIFFENER BOEING 727 727227 1384078 NM BS 920 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WS FOUND ON LEFT MLG WW STIFFENER AT BS 920. THE COR RODED AREA WAS CLEANED UP AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900709 19991119 00709 NM 1999 11 19 MZZA99146 1 19990730 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1273 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON RIGHT LOWER TORQUE BOX ANGLE A T BS 1274. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-04 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900710 19991119 00710 NM 1999 11 19 MZZA99145 1 19990804 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1173 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON ANGLE ATTACHED TO RIGHT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1173. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-10-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900711 19991119 00711 NM 1999 11 19 MZZA99144 1 19990804 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH CORROSION WAS FOUND ON BS 950D FRAME FORWARD FL ANGE AT S30 RT. THE CORRODED AREA WAS CLEANED UP AND REPAIRED PER B727 SRM CHAPTER 53-10-04 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900712 19991119 00712 NM 1999 11 19 MZZA99174 1 19990818 A 2760 BACC2A3A05800EG CABLES BOEING 727 727224 1384076 NM LT SPOILER RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, THREE SPOILER CONTROL CABLES WERE FOUND RUSTED IN LEFT WING TE CAVITY. THE DAMAGED CABLES WERE REMOVED AND REPLACED WITH NEW ONES PER B727 MM CHAPTER 27-61-00 AND OPERATIONAL CHECK N ORMALLY. (M) 2 L 7 3 4F A3WE 1999111900713 19991119 00713 NM 1999 11 19 99ZZZM756 1 19990818 A 2760 BACC2A3A06738EG CABLES BOEING 727 727224 1384076 NM LT SPOILER RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, THREE SPOILER CONTROL CABLES WERE FOUND RUSTED IN LEFT WING TE CAVITY. THE DAMAGED CABLES WERE REMOVED AND REPLACED WITH NEW ONES PER B727 MM CHAPTER 27-61-00 AND OPERATIONAL CHECK N ORMALLY. (M) 2 L 7 3 4F A3WE 1999111900714 19991119 00714 NM 1999 11 19 99ZZZM757 1 19990818 A 2760 BACC2A3A02795EG CABLES BOEING 727 727224 1384076 NM LT SPOILER RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, THREE SPOILER CONTROL CABLES WERE FOUND RUSTED IN LEFT WING TE CAVITY. THE DAMAGED CABLES WERE REMOVED AND REPLACED WITH NEW ONES PER B727 MM CHAPTER 27-61-00 AND OPERATIONAL CHECK N ORMALLY. (M) 2 L 7 3 4F A3WE 1999111900715 19991119 00715 NM 1999 11 19 MZZA99173 1 19990818 A 2710 BACC2A4B00492FG CABLES BOEING 727 727224 1384076 NM LT AILERON RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO INBOARD AILERON TAB CONTROL CABLES WERE FOUND RUSTED IN LEF T MLG WW. THE DAMAGED CABLES WERE REMOVED AND REPALCED WITH NWE ONES PER B727 MM CHAPTER 27-10-00 AND OPERATIONAL CHECK NORMALLY. (M) 2 L 7 3 4F A3WE 1999111900716 19991119 00716 NM 1999 11 19 99ZZZM758 1 19990818 A 2710 BACC2A4B00587FG CABLES BOEING 727 727224 1384076 NM LT AILERON RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO INBOARD AILERON TAB CONTROL CABLES WERE FOUND RUSTED IN LEF T MLG WW. THE DAMAGED CABLES WERE REMOVED AND REPALCED WITH NWE ONES PER B727 MM CHAPTER 27-10-00 AND OPERATIONAL CHECK NORMALLY. (M) 2 L 7 3 4F A3WE 1999111900717 19991119 00717 NM 1999 11 19 MZZA99172 1 19990817 A 7603 6132155D3KH1702 CONTROL CABLE BOEING 727 727224 1384076 NM NR 2 ENGINE FRAYED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FRAYED NR 2 ENGINE CONTROL CABLE (ESS2A) WAS FOUND AT BS 1204 . THE DAMAGED CABLE WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM CHAPTER 76-11-11 AND OPERATIONAL CHECK NORMALLY . (M) 2 L 7 3 4F A3WE 1999111900718 19991119 00718 NM 1999 11 19 MZZA99170 1 19990818 A 5711 FRONT SPAR BOEING 727 727224 1384076 NM LT WING CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 6 INCH BY 1.5 INCH AREA CORROSION WAS FOUND ON LEFT WING FRON T SPAR LOWER CHORD PLATE UPPER SURFACE BETWEEN FSS 551 AND FSS 557. THE CORRODED SECTION WAS TRIMMED OUT AND REPAIRED P ER ECRA NR 5710-01969. (M) 2 L 7 3 4F A3WE 1999111900719 19991119 00719 NM 1999 11 19 MZZA99169 1 19990817 A 7603 6132155D3KJ2496 CONTROL CABLE BOEING 727 727224 1384076 NM NR 1 ENGINE FRAYED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FRAYED NR 1 ENGINE CABLE (ESS1A) WAS FOUND AT BS 1186. THE D AMAGED CABLE WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM CHAPTER 76-11-11 AND OPERATIONAL CHECK NORMALLY. (M) 2 L 7 3 4F A3WE 1999111900720 19991119 00720 NM 1999 11 19 MZZA99168 1 19990818 A 5711 CHORD PLATE BOEING 727 727224 1384076 NM FSS 513-516 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY 1.28 INCH AREA CORROSION WAS FOUND ON LEFT WING FRO NT SPAR LOWER CHORD PLATE UPPER SURFACE BETWEEN FSS 513 AND FSS 516. THE CORODED SECTION WAS TRIMMED OUT AND REPAIRED P ER ECRA NR 5710-01969. (M) 2 L 7 3 4F A3WE 1999111900721 19991119 00721 NM 1999 11 19 MZZA99167 1 19990819 A 5330 SKIN BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 5 INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN AT S TRINGER 29R BETWEEN BS 950 PLUS 11 AND BS 950A. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER ECRA 5330-02865. (M ) 2 L 7 3 4F A3WE 1999111900722 19991119 00722 NM 1999 11 19 MZZA99166 1 19990818 A 2612 10608777 FIRE DETECTOR BOEING 727 727224 1384076 NM APU DAMAGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, APU FIRE DETECTOR SENSOR EXTERIOR INSULATOR WAS FOUND STRIPPED. THE DAMAGED APU FIRE DETECTOR SENSOR WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM 26-10-0 AND OPERATIONAL CHECK NORMALLY. (M) 2 L 7 3 4F A3WE 1999111900723 19991119 00723 NM 1999 11 19 MZZA99165 1 19990817 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 1340 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AIR ASIA, A .25 INCH LONG CRACK WAS FOUND ON ANGLE WHICH IS ATTACHED TO RIGH T LOWER TORQUE BOX VERTICAL WEB AT BS 1340. THE DAMAGED ANGLE WAS REMOVED AND REPLACED PER B727 SRM CHAPTER 51-30-02 FI G 1-4. (M) 2 L 7 3 4F A3WE 1999111900724 19991119 00724 NM 1999 11 19 MZZA99164 1 19990823 A 5320 GUSSETT BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON GUSSET WHICH IS ATTACHED TO BS 950 BU LKHEAD LOWER T-CHORD AND S29R. THE CORRODED GUSSET WAS REMOVED AND REPLACED PER SRM 51-30-2 FIG 1-4. (M) 2 L 7 3 4F A3WE 1999111900725 19991119 00725 NM 1999 11 19 MZZA99163 1 19990823 A 5312 BULKHEAD TEE BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-CHORD BETWEEN S30 AND S29R. THE CORRODED LOWER T-CHORD WAS REMOVED AND REPLACED PER B727 CHAPTER 51-30-02 FIG 1-4. (M) 2 L 7 3 4F A3WE 1999111900726 19991119 00726 NM 1999 11 19 MZZA99162 1 19990819 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON L-ANGLE WHICH ATTACH WITH S29R (KEEL BEAM) SPLICE AND BS 950 BULKHEAD WEB IN RIGHT MLG WW. THE CORRODED L ANGLE WAS REMOVED AND REPLACED EPR SRM 51-30-02 FI G 1-4. (M) 2 L 7 3 4F A3WE 1999111900727 19991119 00727 NM 1999 11 19 MZZA99161 1 19990819 A 5312 BULKHEAD WEB BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON T-STIFFENER JUST ATTACHED TO BS 950 P RESSURE BULKHEAD WEB FORWARD SIDE IN RT MLG WW/ THE CORRODED T-STIFFENER WAS REMOVED AND REPLACED PER SRM 51-30-2 FIGUR E 1-4. (M) 2 L 7 3 4F A3WE 1999111900728 19991119 00728 NM 1999 11 19 MZZA99160 1 19990819 A 5314 KEEL BEAM BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3.5 INCH BY .5 INCH WIDTH BY .122 INCH DEPTH CORROSION WAS FO UND ON RT FUSELAGE KEEL BEAM RADIUS AT BS 950 PLUS 11. THE CORRODED KEEL BEAM WAS BLENDED OUT AND REPAIRED PER ECRA 531 0-03908. (M) 2 L 7 3 4F A3WE 1999111900729 19991119 00729 NM 1999 11 19 MZZA99159 1 19990816 A 5313 655848826 STRINGER BOEING 727 727224 1384076 NM BS 943 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DUIRNG S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO 3.1 AND 1.68 INCH LONG CRACKS WERE FOUND ON RT FUSELAGE S-1 8A VERTICAL FLANGE AT BS 943. THE DAMAGED SECTION WAS TRIMMED OUT AND REPAIRED PER ECRA NR 5310-03914. (M) 2 L 7 3 4F A3WE 1999111900730 19991119 00730 NM 1999 11 19 MZZA99158 1 19990816 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1218 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .25 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN AT BS 1218. T HE CRACKED SKIN WAS STOP DRILLED AND REPAIRED PER B727 SRM 53-30-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900731 19991119 00731 NM 1999 11 19 MZZA99157 1 19990819 A 5310 BULKHEAD TEE BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH AREA CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-C HORD FORWARD SURFACE AT STRINGER 29R. THE CORRODED AREA WAS BLENDED OUT AND REPAIRED PER ECRA 5310-03910. (M) 2 L 7 3 4F A3WE 1999111900732 19991119 00732 NM 1999 11 19 MZZA99156 1 19990817 A 5320 CHANNEL BOEING 727 727224 1384076 NM BS 1273 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON U-CHANNEL WHICH IS ATTACHED TO RIGHT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED U-CHANNEL WAS REMOVED AND REPLACED PER B727 SRM CHAPTER 51-40-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900733 19991119 00733 NM 1999 11 19 MZZA99155 1 19990817 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 1263 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON RIGHT LOWER TORQUE BOX ANGLE AT BS 1 263. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 1. (M) 2 L 7 3 4F A3WE 1999111900734 19991119 00734 NM 1999 11 19 MZZA99154 1 19990812 A 3610 DUCT BOEING 727 727264 138408M NM NR 2 ENGINE LOOSE A MZZA A J UNSCHED LANDING DUMP FUEL M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 13 625DH 20780 SIN - FLT 878 - NR 2 FIRE WARNING ILLUMINATED IN FLIGHT. LIGHT EXTINGUISHED WITH POWER REDUCTION TO IDLE, FIRE TEST SYS TEM NORMAL, L/P 7904361. MAINTENANCE OPEN NR 2 ENGINE COWLS. INSPECTED ENGINE AND FIRE DETECTION AND SENSORS FOR IRREG ULARITIES, NONE NOTED. RAN ENGINE WITH HIGH POWER SETTINGS. NOTICED 2 PNEUMATIC LEAKS NEAR LOOP AND OH SENSOR. RECLAM P ENGINE PURGE BLEED LINE AND REPLACED FORWARD CSD PNEUMATIC TUBE GASKET. AS PRECAUTION, REPLACED ENG LOOP PER MM 26-11 -22. ALL CHECKS NORMAL. RELEASED AIRCRAFT FOR SERVIEC WITH NO FURTHER INCIDENT. (M) 2 L 7 3 4F A3WE 1999111900735 19991119 00735 NM 1999 11 19 MZZA99153 1 19990811 A 2612 CONNECTOR BOEING 727 727264 138408M NM NR 2 ENGINE CONTAMINATED A MZZA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 625DH 20780 SIN - FLT 877 - NR 2 FIRE WARNING LIGHT FLASHED WITH MOMENTARY BELL. REDUCED THRUST NR 2 ENGINE AND SYMPTOMS DID NOT RE OCCUR IAW AFM, PROCEDURES, FIRE WARNING SYSTEM CHECKED OK, L/P NR 7904359. MAINTENANCE OPENED NR 2 ENGINE COWL, INSPECT ION NR 2 ENGINE FIRE LOOP. REMOVED AND CLEANED OILED CONNECTORS AT BOTH SYSTEM A/B CONNECTORS. RESECURED CONNECTORS, R AN ENGINE UP TO 70 PERCENT. NO LEAKS NOTED. ENGINE COWL SECURED. SYSTEM GROUND TEST NORMAL AND WITH ENGINE AT IDLE PO WER MM REF 26-11-0. REQUEST FURTHER CREW COMMENTS. RELEASED AIRCRAFT FOR SERVICE. (M) 2 L 7 3 4F A3WE 1999111900736 19991119 00736 NM 1999 11 19 MZZA99171 1 19990829 A 3610 07212030251 CLAMPS BOEING 727 727264 138408M NM NR 3 STRUT LOOSE A MZZA A J UNSCHED LANDING DUMP FUEL M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 13 625DH 20780 FLT 879 - MNL - WITH TAKEOFF POWER SET NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT REMAINED ILLUMINATED UNTIL NR 3 THR OTTLE RETARDED. MAINTENANCE T/S SYSTEM AND FOUND 5 CLAMP LOOSE AND PNEUMATIC DUCTING INSIDE NR 3 STRUT ACCESS PANEL. R E-TIGHTENED ALL CLAMPS PER MM 36-00-1. PERFORMED ENGINE RUN PER MECHANIC CHECKLIST. LEAK ON PRE-COOLER MANIFOLD REF IP C 36-10-0-9 ITEM 340. REPLACED 2 CLAMP M/E 07-2120-3-0251. RAN ENGINE AT TAKEOFF POWER OPS AND LEAK CHECK OK. PANELS SECURED AND RELEASED AIRCRAFT FOR SERVICE. (M) 2 L 7 3 4F A3WE 1999111900737 19991119 00737 NM 1999 11 19 99ZZZM759 1 19990928 A 3610 BACC10DU450ABE CLAMP BOEING 727 727222 1384073 NM RT BLEED SYSTEM LOOSE A RYNA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 CE 07 7642U 19915 FLT 308 - EN ROUTE TO JFK, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. RAN CHECKLIST, LIGHT EXTINGUISHED WITH NR 1 BLEED PACK VALVE CLOSED. FOUND AIR LEAK AT CLAMP ON DUCTING BEHIND PANEL OF THE RIGHT KEEL BEAM IN THE RIGHT WHEEL WELL. SECURED SAME. TEST NORMAL. (M) 2 L 7 3 4F A3WE 1999111900738 19991119 00738 NM 1999 11 19 99ZZZM760 1 19990921 A 2611 BULB BOEING 727 727222 1384073 NM CABIN FAILED A RYNA K NONE L NO TEST CR CRUISE 1 CE 07 7645U 20039 FLT 215 - DAY - NR 6 SMOKE DETECTOR IS INOPERATIVE. RELAMPED BEACON LAMP ON NR 6 SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 1999111900739 19991119 00739 NM 1999 11 19 99ZZZM761 1 19990914 A 7931 62413140106 HOSE BOEING 727 727222 1384073 NM NR 2 ENGINE PLUGGED A RYNA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 07 7635U 19908 FLT 319 - OMA - NR 2 ENGINE OIL PRESSURE EXCEEDED NORMAL LIMITS (61 PSI) AND WOULD NOT RETURN TO NORMAL PRESSURE RANGE, NR 2 ENGINE WAS SHUT DOWN IN ACCORDANCE PROCEDURES AND CHECKLISTS. REPLACED OIL PRESSURE RELIEF VALVE, REPLACED OIL PRE SSURE TRANSMITTER. REPLACED PLUGGED HOSE AT TRANSMITTER. (M) 2 L 7 3 4F A3WE 1999111900740 19991119 00740 NM 1999 11 19 99ZZZM762 1 19991003 A 2612 18252800 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 429EX 19100 FLT 9001 - MKE-DAY - ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT INTERMITTENT IN FLIGHT. FOUND FIRE LOOP TOUCHING CONSTAN T SPEED DRIVE OIL COOLER EXHAUST DUCT, REPOSITIONED LOOP. (M) 2 L 7 3 4F A3WE 1999111900741 19991119 00741 NM 1999 11 19 99ZZZM763 1 19990821 A 2611 355 BULB BOEING 727 72721 1384003 NM CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 329QS 19038 FLT 613 - GSO - SERVICE CHECK FOUND ONE SMOKE DETECTOR LAMP INOPERATIVE (LOWER DETECTOR). RELAMPED. (M) 2 L 7 3 4F A3WE 1999111900742 19991119 00742 NM 1999 11 19 99ZZZM764 1 19990908 A 2611 308 BULB BOEING 727 727151C 138404V NM CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 433EX 19868 FLT 719 - IND - DURING TRANSIT CHECK, LOWER WINDOWS OF SMOKE DETECTORS APPEAR TO HAVE NO OR AT LEAST IN SUFFICIENT BACKG ROUND LIGHTING. RELAMPED LOWER BULBS ON FLIGHT ENGINEERS SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 1999111900743 19991119 00743 NM 1999 11 19 99ZZZM765 1 19990905 A 2611 308 BULB BOEING 727 727151C 138404V NM CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 433EX 19868 FLT 643 - SAN - DURING SERVICE CHECK, BOTH UPPER LEFT AND RIGHT SMOKE DETECTORS LIGHT INOPERATIVE. RELAMPED SMOKE DETEC TORS. (M) 2 L 7 3 4F A3WE 1999111900744 19991119 00744 NM 1999 11 19 99ZZZM766 1 19990928 A 2611 308 BULB BOEING 727 727134C 138404H NM CABIN FAILED A RYNA K NONE L NO TEST CR CRUISE 1 CE 07 424EX 20042 FLT 718 - ORD-IND - LOWER RIGHT SMOKE DETECTOR BACKGROUND LIGHT INOPERATIVE. RELAMPED LOWER RIGHT SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 1999111900745 19991119 00745 NM 1999 11 19 99ZZZM767 1 19991005 A 2611 308 BULB BOEING 727 727151C 138404V NM CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 432EX 19867 FLT 613 - GSO SERVICE CHECK, MAIN CABIN SMOKE DETECTOR LIGHT IS OUT. RELAMPED MAIN CABIN SMOKE DETECTOR LIGHT. (M) 2 L 7 3 4F A3WE 1999111900746 19991119 00746 NM 1999 11 19 99ZZZM768 1 19991005 A 2613 356802255 OVERHEAT LOOP BOEING 727 72722C 138400F NM LWR AFT BODY OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 428EX 19097 FLT 9002 - MIA-IND - LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED AFT BODY CIRCUIT. (M) 2 L 7 3 4F A3WE 1999111900747 19991119 00747 NM 1999 11 19 99ZZZM769 1 19990922 A 2612 1825280037525 FIRE LOOP BOEING 727 72782C 1384026 NM NR 1 ENGINE GROUNDED A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 528PC 19597 FLT 648 - DFW-OMA - NR 1 FIRE DETECTION LIGHT ON INTERMITTENTLY. REPOSITIONED FIRE LOOP AWAY FROM A TUBE. (M) 2 L 7 3 4F A3WE 1999111900748 19991119 00748 NM 1999 11 19 99ZZZM770 1 19991007 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 428EX 19097 FLT 9001 - PIT-IND - NR 3 ENGINE FIRE DETECTOR GROUND FAULT LIGHT CAME ONE IN FLIGHT, WENT OUT ON FINAL. REPOSITIONED N R 3 ENGINE GRUOND FAULT LOOP. (M) 2 L 7 3 4F A3WE 1999111900749 19991119 00749 NM 1999 11 19 99ZZZM771 1 19991005 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 428EX 19097 FLT 9002 - MIA-IND - NR 3 GROUND FAULT CIRCUIT FLICKERED IN FLIGHT. REPOSITIONED FAULT CIRCUIT. (M) 2 L 7 3 4F A3WE 1999111900750 19991119 00750 NM 1999 11 19 99ZZZM772 1 19991010 A 2613 35664400 OVERHEAT ELEMENT BOEING 727 72777C 1380420 NM NR 3 STRUT OUT OF ADJUSTED A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 526PC 20370 FLT 711 - EWR-IND - NR 3 ENGINE STRUT OVERHEAT LIGHT FLICKERS WITH ENGINE AND WING ANTI-ICE ON. LIGHT COMES ON WITH TEM PERATURE GAUGE SHOWING BETWEEN 200 DEGREES CELSIUS, 225 DEGREES CELSIUS. TURNED OFF RIGHT WING ANTI-ICE AND THE NR 3 EN GINE STRUT LIGHT REMAINED OUT FOR REST OF FLIGHT. ADJUSTED OVERHEAT SENSING LOOP. (M) 2 L 7 3 4F A3WE 1999111900751 19991119 00751 NM 1999 11 19 99ZZZM773 1 19991022 A 2612 18252800 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF ADJUST A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 428EX 19097 FLT 705 - BWI-IND - FIRE PROTECTION SYSTEM NR 3 ENGINE GROUND DETECTOR SYSTEM LIGHT ILLUMINATED. ADJUSTED FIRE PROTECTI ON LOOP. (M) 2 L 7 3 4F A3WE 1999111900752 19991119 00752 EU 1999 11 19 SIMA992913 1 19991018 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AE 340B298 ABI - FOUND NON STANDARD REPAIR TO THE LT FUSELAGE SKIN BETWEEN STATION 608 AND 618.5, AND SL 1520 AND 1522. REMOVED EX ISTING DOUBLER. REMOVED DAMAGED SECTION OF SKIN FROM DAMAGE AREA AND REFORMED DAMAGE TO NORMAL SKIN CONTOUR. PERFORMED A DYE PENETRANT INSPECTION. NO INDICATIONS OF CRACKS NOTED. FABRICATED AN EXTERNAL REPAIR DOUBLER .063 THICK, 10.75 B Y 7.5. TREATED ALL REPAIR SURFACES. WET INSTALLED FASTENERS. RIVETS IN FIELD OF REPAIR. WORK DONE IAW SAAB REPAIR ST ATEMENT 72SDS1850 AND STANDARD PRACTICES OF SAAB 340 SRM72LKS 3079 REV 34. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999111900753 19991119 00753 EU 1999 11 19 SIMA992912 1 19991018 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 MISDRILLED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 298AE 340B298 ABI - FOUND NONSTANDARD REPAIR TO RT FUSELAGE SKIN BETWEEN FRAMES STATIONS 339 AND 363, AND BETWEEN STRINGERS SL 1616 AN D SL 1620. ALSO, FOUND ONE MISDRILLED HOLE. PERFORMED DYE PENETRANT INSPECTION. NO CRACKS FOUND. FABRICATED EXTERNAL REPAIR DOUBLER .063 THICK 13.25 BY 7.25. WET INSTALLED ALL FASTENERS. THE MISDRILLED HOLE WAS PLUGGED WITH A WET INST ALLED DOUBLER COUNTERSUNK RIVET. ALL EXISTING HOLES DRILLED FOR THE LARGER NON-STANDARD REPAIR WERE DRILLED OUT OT ACCE PT AN AF138AD5 RIVET AND THOSE RIVET WERE INSTALLED WET. WORK DONE STANDARD SAAB 340 SRM 72LKS 3079 REV 34 PRACTICES. A IRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999111900754 19991119 00754 EU 1999 11 19 SIMA992732 1 19990930 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 204NE 340B204 ABI - AFTER REMOVAL OF LEFT AFT WING TO FUSELAGE FAIRING THREE ELONGATED HOLES WERE DISCOVERED IN THE CABIN SKIN PANEL A T STATION 584, 591.85 AND 593. REAMED ELONGATED HOLES. INSTALLED MS 20470A8 RIVETS WET WITH SEALANT. WORK DONE IAW SA AB REPAIR STATEMENT 72SDS1798, SAAB 340 SRM 72LKS3079, 51-40-21 PAGE 1 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SER VICE. (M) 2 L 7 2 4T RT A52EU 1999111900755 19991119 00755 EU 1999 11 19 SIMA992731 1 19990930 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 567 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 204NE 340B204 ABI - DENT FOUND ON THE LEFT FUSELAGE SKIN PANEL AT STATION 567 JUST BELOW SL 1520. RETURNED SKIN TO NORMAL CONTOUR. P ERFORMED EDDY CURRENT INSPECTION OF RECONTOURED AREA WITH NO INDICATIONS OF CRACKS. PREPARED REPAIR PLATE .050 THICK, F ORMED TO CONTOUR OF SKIN AND CHAMFERED EDGES. CLEANED REPAIR PLATE AND APPLIED ALODINE AND EPOXY PRIMER. APPLIED FAY S EALANT TO PLATE, POSITIONE DPLATE AND INSTALLED ALL FASTENER WET. FAIRED EDGES OF REPAIR PLATE. APPLIED EPOXY PRIMER T O INTERIOR AND EXTERIOR SURFACES AND RESTORED TOP COAT. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1798, SAAB 340 SRM 72L KS3079, 53-70-10 PARA 4 PAGE 215 FIG 209 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999111900756 19991119 00756 EU 1999 11 19 SIMA992673 1 19990924 A 5330 SAAB SF340 340B 7860101 EU UNKNOWN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 204NE 340B204 ABI - DENT WAS FOUND ON BOTTOM OF TAILCONE BETWEEN STA 827 AND 839 AND BETWEEN STRINGERS 1528 AND 1624 THAT REQUIRED REP AIR. CLEANED AREA AND CHECKED THAT DAMAGED AREA DID NOT EXCEED LIMITATIONS. REMOVED DAMAGED AREA WITH A 2 INCH DIAMETE R CIRCULAR CUT OUT. FABRICATED A SPACER .025 THICK. CHECKED THE GAP BETWEEN THE SKIN AND SPACER WHICH IS TO BE .08 INC H PLUS/MINUS .04 INCH. ALSO, FABRICATED A PLATE .025 THICK. APPLIED CHROMATING TO THE BARE METAL SURFACES AND FR PRIME R TO THE TREATED SURFACES OF THE SKIN, THE SPACER AND THE PLATE. FAY SEALED THE PLATE, POSITIONED THE SPACER AND THE PL ATE, AND INSTALLED THE FASTENER WET. FILLET SEALED THE GAP BETWEEN THE SPACER AND THE SKIN. APPLIED TOPCOAT AND CORRO 2 L 7 2 4T RT A52EU 1999111900757 19991119 00757 WP 1999 11 19 AALA996021 1 19991007 A 2560 D29985107 EMERGENCY SLIDE DOUG DC9 DC983 3022083 WP GALLEY DOOR LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880RA 53186 SJC - AFT GALLEY SLIDE PACK CAME OUT, BUT DID NOT INFLATE, AFTER DOOR WAS OPENED WITHOUT DISARMING FOR CATERING. REINST ALLED AFT GALLEY SLIDE ON DOOR. (M) 2 L 7 2 4F RT A6WE 1999111900758 19991119 00758 WP 1999 11 19 AALA996007 1 19990903 A 5320 JAMB DOUG DC9 DC983 3022083 WP PAX DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 882RA 49949 OKC - JUST AFT OF FORWARD ENTRANCE DOOR JAM HAS CORROSION. BLENDED OUT OF LIMITS IAW DC-9 SRM 51-01 MAT LOSS .030 FABRI CATED NEW THRESHOLD DOOR JAM IAW DC-9 SRM 51-1002. TREATED AND PRIMED IAW DC-9 SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 1999111900759 19991119 00759 EU 1999 11 19 SIMA992653 1 19990922 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 608 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 359SB 340B359 ABI - DENT ON LEFT FUSELAGE STATION 608 WL 73.5. CLEANED REPAIR AREA AND CUT OUT DAMAGE. FABRICATED REPAIR PLATE .050 THICK. CLEANED REPAIR PLATE AND APPLIED A PROTECTIVE COAT OF ALODINE AND ONE COAT OF EPOXY PRIMER. APPLIED FAY SEALANT TO THE CONTRACT SURFACE OF THE REPAIR PLATE, REPOSITIONED, AND INSTALLED FASTENERS WET. APPLIED FILLET SEALANT AROUND PER REPAIR PLATE EDGE STEP. CLEANED REPAIR AREA, APPLIED ONE COAT OF EPOXY PRIMER AND ONE COAT OF TOP COAT TO THE INTER IOR AND EXTERIOR SURFACE AND RESTORED PAINT FINISH. WORK DONE IAW SAAB SRM 53-70-10 PAGE 215 AND STANDARD SRM PROCEDURE S. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1999111900760 19991119 00760 EU 1999 11 19 SIMA992952 1 19991022 A 3350 650006BR6303121 SOCKET SAAB SF340 340B 7860101 EU ROW 3B FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 256AE 340B256 JFK - FLT 5163 - STRONG ELECTRICAL ODOR COMING FROM ABOVE SEAT 3B. REMOVED AND REPLACED OVERHEAD LAMP ASSEMBLY AT SEAT 3B. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999111900761 19991119 00761 EU 1999 11 19 SIMA992951 1 19991022 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AT 1372 420 SGF - SEVERAL FORWARD CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED A POWER SUPPLY BATTERY PACK. OPER ATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999111900762 19991119 00762 EU 1999 11 19 SIMA992941 1 19991021 A 3350 EO38321 FUSE AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 249AT 0249 MIA - FLT 5208 - PASSENGER DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BLOWN FUSE IN EMERGENCY LIGHT POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999111900763 19991119 00763 WP 1999 11 19 USAA991176 1 19991016 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 420, 370, 408 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 48811 48092 PIT - DURING Q-5 CHECK, FOUND .125 INCH CRACK AND .5 INCH CRACK, TWO IN LONGERON AT STATION 420 STATION 370 AND STATION 408. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-02 FIG 18 SHT 1. (M) 2 L 7 2 4F A6WE 1999111900764 19991119 00764 WP 1999 11 19 USAA991175 1 19991016 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 160 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 48811 48092 PIT - DURING Q-5 CHECK, FOUND .5 INCH CRACK AT LONGERON 31 AT STATION 160 ATTACH POINT. CUT OUT DAMAGED SECTION AND SPL ICED IN NEW PER SRM 53-02. (M) 2 L 7 2 4F A6WE 1999111900765 19991119 00765 WP 1999 11 19 USAA991174 1 19991016 A 5320 CUSP DOUG DC9 DC981 3022081 WP BS 1297 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 812US 48811 48092 PIT - DURING Q-5 CHECK, FOUND 2 INCH CRACK 3 INCHES FORWARD OF STATION 1297 LEFT SIDE CUSP MEMBRANE AT LONGERON 18L. CU T OUT DAMAGED SECTION AND INSTALLED NEW FROM 7075 T-6 .032 INCH PER SRM 53-04. (M) 2 L 7 2 4F A6WE 1999111900766 19991119 00766 WP 1999 11 19 USAAD99149 1 19991019 A 3350 408822101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 807US 48039 CLT - THE EMERGENCY LIGHTS IN THE FIRST CLASS SECTION OF THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999111900767 19991119 00767 NM 1999 11 19 USAA109907 1 19990811 A 3350 256005 FUSE BOEING 727 727225 1384077 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS 20447 FLT 6181 - BOS-LGA - FOUND ON L/S, CENTER PORTION OF FLOOR TRACK EPL LIGHTING INOPERATIVE. REPLACED BLOWN FUSE IN AFT E PL BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999111900768 19991119 00768 NM 1999 11 19 USAA109905 1 19991015 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM RT EMER EXIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 926TS 20774 FLT 6530 - DCA-LGA - FOUND ON L/S, RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKS OK. (M) 2 L 7 3 4F A3WE 1999111900769 19991119 00769 NM 1999 11 19 USAA109904 1 19991015 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 18 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS P3014 21244 FLT 6141 - BOS-LGA - FOUND ON L/S, EMERGENCY EXIT SIGN AT ROW 18 INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999111900770 19991119 00770 WP 1999 11 19 USAAD99148 1 19991019 A 3350 86210151 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 IND - THE LOW LEVEL LIGHTING DID NOT TEST. MAINTENANCE REPLACED THE AFT CONTROL MODULE BATTERY. (M) 2 L 7 2 4F A6WE 1999111900771 19991119 00771 WP 1999 11 19 USAAD99152 1 19991023 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP ROW 9-13 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 983VJ 48159 IND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 9 TO 13 WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. ( M) 2 L 7 2 4F A6WE 1999111900772 19991119 00772 NE 1999 11 19 USAAD99151 2 19991023 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LEFT FAILED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 965VJ 47374 655101 PHL-CLT- FLT 61 - ON TAKEOFF, THE LEFT ENGINE EGT WAS HIGHER THAN NORMAL. ATTEMPTS TO MATCH ENGINE PARAMETERS WERE UNSU CCESSFUL WITHOUT SIGNIFICANT THROTTLE STAGGER. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED THE LEFT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999111900773 19991119 00773 NM 1999 11 19 USAABB99047 1 19991023 A 7830 ETPU10002C PRESSURE UNIT BOEING 757 7572B7 1384964 NM RT TR UNIT FAULTY A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 621AU 22789 27200 BOS - FLT 38 - DESCENDING INTO BOS AT FL270, THE RIGHT ENGINE FLAMED OUT. THE ENGINE WAS SUCCESSFULLY RESTARTED AT FL21 0. FLIGHT CONTINUED TO BOS. CREW REPORTED THAT THE RIGHT THRUST REVERSER WAS SLOW TO DEPLOY. MAINTENANCE FOUND THE TR ANSIENT PRESSURE UNIT WITH A FAULT CODE 'BF' AND REPLACED IT. (M) 2 L 7 2 4F RT A2NM 1999111900774 19991119 00774 WP 1999 11 19 USAAD99150 1 19991021 A 3230 39358603 FITTING DOUG DC9 DC981 3022081 WP LT MLG WW BROKEN A USAA L ABORTED APPROACH K FLUID LOSS AP APPROACH 1 EA 19 809US 48041 EWR-PIT - FLT 760 - DURING LANDING GEAR EXTENSION PRIOR TO LANDING THE RIGHT HYDRAULIC SYSTEM WENT TO ZERO. THERE GEAR INDICATION LIGHTS WERE GREEN, BUT THE CREW ELECTED TO FLYBY THE TOWER FOR CONFIRMATION. ALL APPEARED NORMAL AND THE AIR CRAFT LANDED WITHOUT INCIDENT. AFTER THE AIRCRAFT STOPPED ON THE RUNWAY, MAINTENANCE PINNED THE GEAR AND TOWED THE AIRC RAFT TO THE GATE. MAINTENANCE FOUND THE LEFT MAIN GEAR RETRACT CYLINDER ATTACH FITTING BROKEN, CAUSING DAMAGE TO THE RE TRACT CYLINDER. THE RETRACT CYLINDER AND ATTACH FITTING WERE REPLACED. (M) 2 L 7 2 4F A6WE 1999111900775 19991119 00775 NE 1999 11 19 TSAA9972466 2 19991020 A 7532 658385B1 BLEED VALVE BOEING 737 7372T4 1384492 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A TSAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 13 807AL 23443 687825 FLT 263 - HNL-LIH - COMPRESSOR STALL NR 2 ENGINE THROTTLE UP OFF OF IDLE. ABORTED TAKEOFF. RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE BLEED CONTROL VALVE. SYSTEM LEAK CHECK AND OPS CHECK GOOD PER MM 75-31-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999111900776 19991119 00776 NM 1999 11 19 TSAA9953468 1 19991022 A 5330 65737461 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 FOUND FUSELAGE SKIN CRACK NOTED APPROXIMATELY .5 INCH LONG AT BS 727A STRINGER 17L, CONFIRMED WITH HFEC. REPAIRED IAW S RM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999111900777 19991119 00777 NM 1999 11 19 TSAA9933470 1 19991024 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 2 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999111900778 19991119 00778 NM 1999 11 19 TSAA9933469 1 19991024 A 3350 963100211 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 2 FLOOR LIGHT ASSY DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999111900779 19991119 00779 NM 1999 11 19 TSAA9933467 1 19991022 A 3350 1000679 LIGHT BOEING 737 7372S5C 1384499 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED CONTROL CABIN EXIT EMERGENCY LIGHT ASSY DUE TO NOT TURNING OFF. OPS CHECK OK. AIRCRAFT RETURNED TO SERICE. ( M) 2 L 7 2 4F RT A16WE 1999111900780 19991119 00780 WP 1999 11 19 SABA990069 2 19991024 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A SABA E A ENGINE SHUTDOWN UNSCHED LANDING B Y SMOKE/FUMES/ODORS/SPARKS ENGINE STOPPAGE CR CRUISE 1 SO 33 913AE 913 C66308 LWB - FLT 5163 - DURING CRUISE FLIGHT 20 MINUTES OUT OF LWB, LEFT ENGINE HAD A SUDDEN FAILURE AND THERE WAS SMOKE IN THE COCKPIT AND CABIN. AN INFLIGHT EMERGENCY WAS DECLARED. EMERGENCY CHECKLIST WERE FOLLOWED. EMERGENCY VEHICLES WERE DE PLOYED. THE SMOKE WAS EVACUATED FROM THE AIRCRAFT, AND THE AIRCRAFT LANDED SAFELY AT LWB WITH NO OTHER PROBLEMS. AIRCR AFT TAXIED TO THE GATE TO DEPLANE PASSENGERS. MAINTENANCE FROM CLT REMOVED AND REPLACED THE LEFT ENGINE. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999111900781 19991119 00781 WP 1999 11 19 AALA996009 1 19990928 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROW 10 UNSERVICEABLE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 882RA 49949 SJC - EMERGENCY LIGHTS IN CABIN FROM SEAT ROW 10 ALL THE WAY FORWARD ARE ON. WE CANNOT EXTINGUISH THEM. REPLACED FORWA RD ENTRY DOOR EMERGENCY LIGHT POWER SUPPLY. SYSTEM GROUND CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 1999111900782 19991119 00782 WP 1999 11 19 AALA996010 1 19990915 A 3320 PA21499 SOCKET DOUG DC9 DC983 3022083 WP SEAT 32D BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881RA 49941 LAX - EMERGENCY EXIT TRACK LIGHT AT SEAT 32D BROKEN. REINSTALLED LIGHT SOCKET ON SEAT 32D BROKEN. REINSTALLED LIGHT SO CKET ON SEAT TRIM AT 32D. OPS CHECK NORMALS. (M) 2 L 7 2 4F RT A6WE 1999111900783 19991119 00783 WP 1999 11 19 AALA996008 1 19990928 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP ROW 26-32 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881RA 49941 SJC - 'E' PATH LIGHTS IN ROW 26 THROUGH 32 INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD. ( M) 2 L 7 2 4F RT A6WE 1999111900784 19991119 00784 NM 1999 11 19 AALA996017 1 19990930 A 3350 6011779 POWER SUPPLY DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 901RA 53489 EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE IN FIRST CLASS. REPLACED B5-240 POWER SUPPLY, CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999111900785 19991119 00785 NM 1999 11 19 AALA996011 1 19990921 A 3350 59306431 BATTERY DOUG MD90 MD9030 3023690 NM ROW 28 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 905RA 53573 SJC - EMERGENCY ESCAPE LIGHTS ROWS 28 AND AFT INOPERATIVE. REMOVED AND REPLACED AFT BATTERY PACK PER MM, OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A6WE 1999111900786 19991119 00786 WP 1999 11 19 AALA996012 1 19990919 A 3350 59306431 BATTERIES DOUG DC9 DC983 3022083 WP ROW 5DF DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 882RA 49949 RNO - FIRST CLASS 5DF AISLE EMERGENCY LIGHTS AND FORWARD GALLEY LIGHTS ARE 'ON' WITH ALL POWER OFF. REMOVED AND REPLACE D EMERGENCY LIGHT BATTERIES, OPS CHECKED GOOD SEVERAL TIMES. (M) 2 L 7 2 4F RT A6WE 1999111900787 19991119 00787 WP 1999 11 19 AALA996014 1 19990923 A 3350 60050451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751RA 49779 SJC - EMPENNAGE 'E' PATH LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999111900788 19991119 00788 WP 1999 11 19 AALA996019 1 19991010 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP EMPENNAGE DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751RA 49779 RNO - EMERGENCY LIGHT IN EMPENNAGE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999111900789 19991119 00789 WP 1999 11 19 AALA996015 1 19990926 A 3350 6011779 POWER SUPPLY DOUG DC9 DC987 3022087 WP BS 1113 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 752RA 49780 RNO - O/H EMERGENCY LIGHTS OUT AT STATION 1113. REMOVED AND REPLACED POWER SUPPLY R5-27, OPS CHECK GOOD. ALL WORK DONE PER MM. (M) 2 L 7 2 4F RT A6WE 1999111900790 19991119 00790 WP 1999 11 19 AALA996013 1 19990926 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 9 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 833RA 53045 ROW NR 9 EMERGENCY LIGHT INOPERATIVE. RECONNECTED CONNECTOR, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999111900791 19991119 00791 NM 1999 11 19 ASAA9910243 1 19990928 A 5210 GUIDE ARM BOEING 737 7372Q8C 138448S NM L2 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 741AS 21959 ANC - PRIOR TO FLIGHT 146, THE L2 DOOR WAS FOUND TO BE DIFFICULT TO CLOSE AND LATCH. ADJUSTED GUIDE ARM AND DOOR OPERAT ED NORMALLY. (M) 2 L 7 2 4F A16WE 1999111900792 19991119 00792 EU 1999 11 19 PLGA991017 1 19991017 A 2530 COFFEE POT SAAB SF340 340B 7860101 EU GALLEY FAILED A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 05 357BE 340B277 MHT - FLT 4814 - THE FLIGHT ATTENDANT NOTICED BURNING SMELL IN THE CABIN. THE PILOT WAS NOTIFIED AND THE AIRCRAFT DIVER TED INTO MHT AND LANDED WITHOUT INCIDENT. MAINTENANCE LOOKED AT AND FOUND THE COFFEE URN AND PLUG TO BE AT FAULT. THE SYSTEM WAS DEACTIVATED AND THE AIRCRAFT WAS FERRIED TO BGR. IN BGR, MAINTENANCE REPLACED THE AFFECTED ITEMS, PERFORMED ALL REQUIRED CHECKS AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999111900793 19991119 00793 WP 1999 11 19 TWAA9915601 1 19991116 A 3350 1315 BULB DOUG DC9 DC931 3022065 WP CABIN INCORRECT A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 986Z 47589 THE FIRST CLASS CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. FOUND INCORRECT BULBS INSTALLED. REPLACED THE BULBS. CHECK-C 8-28-99 MCI. 2 L 7 2 4F A6WE 1999111900794 19991119 00794 WP 1999 11 19 IXXA9900031 1 19991116 A 3310 LIGHT DOUG DC8 DC863F 302198F WP COCKPIT FAILED A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 786AL 46121 EN ROUTE FROM NGU TO RTA, SMOKE WAS NOTICE EMITTING FROM THE ALTERNATE LONG TRIM LIGHT PANEL WHEN THE CENTER PEDESTAL LI GHTING WAS TURNED ON. THE FLIGHT CREW TURNED THE LIGHTING SYSTEM OFF AND THE FLIGHT CONTINUED TO RTA. A COMPANY REPRES ENTATIVE INSPECTED THE LIGHTING SYSTEM AND CENTER PEDESTAL WITH NO DISCREPANCIES NOTED. A SUCCESSFUL OPERATIONAL TEST W AS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999111900795 19991119 00795 WP 1999 11 19 9904801230 1 19991013 A 5315 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1273 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 230NW 46552 DURING M-CHECK, FOUND CRACK ON FLOOR SUPPORT BEAM AT FS 1273, LBL 108. REPAIRED PER EA 11-168622. 2 L 7 3 4F A22WE 1999111900796 19991119 00796 NM 1999 11 19 9904816635 1 19991015 A 5311 FRAME BOEING 747 747227B 1384888 NM BS 1265 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING M-CHECK, FOUND CRACK ON FASTENER HOLE A TO EDGE OF FRAME WEB. REPAIRED PER EA 66-171515. 2 L 7 4 4F A20WE 1999111900797 19991119 00797 NM 1999 11 19 9904826635 1 19991008 A 5711 SPAR WEB BOEING 747 747227B 1384888 NM WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING M-CHECK, FOUND CRACK IN MID SPAR WEB INSIDE TANK. REPAIRED PER EA 66-168400. 2 L 7 4 4F A20WE 1999111900798 19991119 00798 NM 1999 11 19 9904836635 1 19990928 A 5711 SPAR WEB BOEING 747 747227B 1384888 NM WS 1018 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING M-CHECK, FOUND CORROSION ON FRONT SPAR LOWER CHORD. REPAIRED PER EA 66-167487. 2 L 7 4 4F A20WE 1999111900799 19991119 00799 NM 1999 11 19 9904846635 1 19991022 A 5320 SUPPORT BOEING 747 747227B 1384888 NM BS 520-560 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING M-CHECK, FOUND CORROSION ON MAIN DECK FLOOR SUPPORT FS 520 - 560, RBL 116. REPAIRED PER EA 66-171514. 2 L 7 4 4F A20WE 1999111900800 19991119 00800 NM 1999 11 19 9904856635 1 19991015 A 5315 FLOORBEAM BOEING 747 747227B 1384888 NM BS 1280-1304 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING M-CHECK, FOUND FLOORBEAM UPPER FLANGE CORRODED AT FS 1280 - 1304, RBL 34. REPAIRED PER EA 66-171511. 2 L 7 4 4F A20WE 1999111900801 19991119 00801 NM 1999 11 19 9904866635 1 19991015 A 5347 SEAT TRACK BOEING 747 747227B 1384888 NM BS 1333-1349 DEFORMED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING M-CHECK, FOUND 5 HOLES ELONGATED IN RIGHT FLANGE OF SEAT TRACK FS 1333 - 1349, LBL 75. REPAIRED PER EA 66-171508 . 2 L 7 4 4F A20WE 1999111900802 19991119 00802 NM 1999 11 19 9904876635 1 19991022 A 5347 SEAT TRACK BOEING 747 747227B 1384888 NM BS 488-492 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING M-CHECK, FOUND CORROSION ON SEAT TRACK FLANGE FS 488 - 492, LBL 34. REPAIRED PER EA 66-171513. 2 L 7 4 4F A20WE 1999111900803 19991119 00803 NM 1999 11 19 9904886637 1 19991020 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 700 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 637US 23548 DURING PERIODIC CHECK, FOUND CRACK IN FORWARD CARGO FLOORBEAM UPPER 'T' CHORD FS 700, LBL 26. REPAIRED PER EA 66-171312 . 2 L 7 4 4F A20WE 1999111900804 19991119 00804 WP 1999 11 19 9904899753 1 19991110 A 3510 292617EA1 REGULATOR DOUG DC9 DC941 302207N WP COCKPIT SHORTED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 753NW 25654 491 47117 AFTER TAKEOFF, CREW OBSERVED SMOKE COMING FROM OXYGEN REGULATOR IN COCKPIT. CREW DECLARED A RED EMERGENCY AND FLIGHT WA S RETURNED TO FSD. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OXYGEN LIGHT PLATE SHORTED OUT. REPLACED OBSER VER'S OXYGEN REGULATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999111900805 19991119 00805 WP 1999 11 19 9904909753 1 19991109 A 2910 LINE DOUG DC9 DC941 302207N WP RT ENGINE LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 753NW 47117 LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY ON APPROACH INTO MEM. CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AS A PRECAU TION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED HYDRAULIC LINE AT RIGHT ENGINE, LEAK CHECK NORMAL. 2 L 7 2 4F A6WE 1999111900806 19991119 00806 WP 1999 11 19 9904919139 1 19991106 A 3242 BRAKES DOUG DC9 DC914 3022034 WP NR 4 CONTAMINATED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 01 948L 47049 TOWER REPORTED SMOKE FROM RIGHT MAIN GEAR AREA ON LANDING. EMERGENCY EQUIPMENT WAS CALLED AS A PRECAUTION. MAINTENANCE I NSPECTED NR 4 BRAKE AND FOUND WETNESS ON TWO PUCKS. CLEANED AND NO LEAKAGE WAS FOUND. 2 L 7 2 4F A6WE 1999111900807 19991119 00807 NM 1999 11 19 UPS99231119 1 19991105 A 2810 FITTING BOEING 727 727180C 138406G NM LT WING LEAKING A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:AD FUEL LEAK AT LT WING BEHIND LANDING GEAR TRUNNION FITTING. THIS MRR RESUBMIT TO INCLUDE TRUNNION FU EL LEAK. REPAIRED IAW SMRO EO 99-35-01 TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE. 2 L 7 3 4F A3WE 1999111900808 19991119 00808 NM 1999 11 19 UPS99231120 1 19991105 A 2810 FITTING BOEING 727 727180C 138406G NM RT WING LEAKING A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE:AD, FUEL LEAK AT RT WING BEHIND LANDING GEAR TRUNNION FITTING, ONLY STAINS. THIS MRR RESUBMITTED TO INC LUDE TRUNNION FITTING, FUEL LEAK REPAIRED IAW SMRO EO 99-35-001. TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICA L DAMAGE. 2 L 7 3 4F A3WE 1999111900809 19991119 00809 NM 1999 11 19 UPS99231121 1 19991116 A 2751 18129932 INDICATOR BOEING 727 72727C 138400J NM TE FLAPS INOP A IPXA K NONE N FALSE WARNING AP APPROACH 1 SO 01 939UP 19532 INSPECTION TYPE: N/A, ON FLAP SELECTION NO O/B FLAP MOVEMENT, SPLIT FLAP COND. PERFORMED SPLIT FLAP AND ALT USE FLAP EX TENTION CHECKLIST. NORMAL LANDING. REMOVED AND REPLACED O/B FLAP POSITION INDICATOR PER MM 27-52-21 AND ADJUSTED RIGHT O/B FLAP POSITION TRANSMITTER PER MM 27-52-13, OPS CHECK GOOD. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999111900810 19991119 00810 NM 1999 11 19 UPS99231122 1 19991110 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM EXTERNAL DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: SI, LEFT SIDE UPPER EXTERNAL EMERGENCY LIGHT OUT. VERIFIED WIRES AND LIGHTS GOOD PER WDM 33-51-01. RE MOVED AND REPLACED EMERGENCY BATTERY PACK AND FUNCTIONALLY TESTED PER MM 33-50-101, MM 33-50-11, MM 33-50-81. 2 L 7 3 4F A3WE 1999111900811 19991119 00811 NM 1999 11 19 UPS99231123 1 19991110 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM EXTERNAL BISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: SI, RIGHT SIDE LOWER EXTERNAL EMERGENCY LIGHT OUT. VERIFIED WIRES AND LIGHT GOOD. REMOVED AND REPLACE D BATTERY PACK AND PERFORMED FUNCTIONAL CHECK PER MM 33-50-101, MM 33-50-22. 2 L 7 3 4F A3WE 1999111900812 19991119 00812 NM 1999 11 19 99FDEA00484 1 19991117 A 2612 FIRE LOOP BOEING 727 7272S2F 1384O81 NM NR 3 ENGINE OUT OF POSITION A FDEA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 25 211FE 22933 INTERMITTENT FIRE WARN LIGHT AND BELL ON NR 3 ENG. REPOSITIONED FIRE LOOP INSIDE NR 3 ENGINE COWLING. CLOSED ENGINE CO WLING AND COMPLETED FIRE TEST, OPER NORM AS PER 727-200 MM SECTION 26. 2 L 7 3 4F A3WE 1999111900813 19991119 00813 WP 1999 11 19 MWEA99817 1 19991116 A 5753 5912596502 BUSHING DOUG DC9 DC932 3022066 WP RT TE FLAP WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT HAND WING OUTBOARD FLAP ATTACH FITTING NEEDS TO BE REWORKED DUE TO DAMAGE AT HINGE POINT. MTC REMOVED DAMAGE BY R EAMING HOLE AND INSTALLING BUSHING. 2 L 7 2 4F A6WE 1999111900814 19991119 00814 WP 1999 11 19 MWEA99818 1 19991116 A 5320 59121648 TRAP PANEL DOUG DC9 DC932 3022066 WP RIGHT DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT HAND TRAP PANEL HAS AREAS OF DELAMINATION. MTC REMOVED, DRILLED, COUNTER SUNK, RELAMINATED AND REINSTALLED PANEL. 2 L 7 2 4F A6WE 1999111900815 19991119 00815 WP 1999 11 19 MWEA99819 1 19991116 A 5320 5910137 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 351 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FLOORBEAM STRUCTURE AND ATTACHED SIDE WALL STRUCTURE AT STATION 351, LEFT HAND SIDE HAD A TOOL MARKS THAT WERE OUT OF LI MITS. MTC FABRICATED AND INSTALLED TWO ANGLE REPAIRS IAW 53-01 FIG 2. 2 L 7 2 4F A6WE 1999111900816 19991119 00816 WP 1999 11 19 MWEA99820 1 19991116 A 5220 5910186 FRAME DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 VENTRAL DOOR FRAME LOWER RIGHT HAND CORNER HAD A CRACK. MTC REPAIRED CRACKED MEMBER IAW DC9- SRM 53-01 FIG 2 SHEET NR 4 . 2 L 7 2 4F A6WE 1999111900817 19991119 00817 WP 1999 11 19 MWEA99822 1 19991116 A 5321 5910348 FLOOR DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 REMOVED CENTER FLOOR BETWEEN LAVS FOM SEVERAL OF THE HAT CHANNELS ON THE FLOORBOARD WERE CRACKED. MTC FABRICATED AND IN STALLED NEW CENTER FLOOR. 2 L 7 2 4F A6WE 1999111900818 19991119 00818 WP 1999 11 19 MWEA99823 1 19991113 A 5330 591140659 SKIN DOUG DC9 DC932 3022066 WP BS 200 HOLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 HOLE IN AIRCRAFT SKIN AFT OF PAX DOOR STATION 200 LONGERON 17. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999111900819 19991119 00819 WP 1999 11 19 MWEA99824 1 19991117 A 5330 59114071 SKIN DOUG DC9 DC915 3022036 WP BS 205 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 DENT IN RIGHT HAND SIDE FUSELAGE AT STATION 205 BETWEEN LONGERON 18-19R. MTC FABRICATED AND INSTALLED DOUBLER IAW SRM 5 3-04 FIG 30 SHEET 10. 2 L 7 2 4F A6WE 1999111900820 19991119 00820 WP 1999 11 19 SCNA99139 1 19991112 A 3397 WIRE DOUG DC10 DC1015 3022118 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 153SY 48276 DURING A LINE MAINTENANCE CHECK, THE AFT EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE FIRST HALF OF THE AF T CABIN. FOUND SHORTED WIRE ON THE RIGHT SIDE OF THE AIRCRAFT. REPLACED THE WIRE WITH A NEW WIRE. EMERGENCY LIGHTS OP ERATIONALLY CHECK GOOD. 2 L 7 3 4F A22WE 1999111900821 19991119 00821 NE 1999 11 19 VNAA9911011 2 19991115 A 7532 311671504 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 459PS 10039 3070 116150 THE FLIGHT CREW RECEIVED A RIGHT HAND ELECTRONIC ENGINE CONTROL UNIT FAIL CAS MESSAGE DURING TAKEOFF AND ABORTED THE TAK EOFF. THE AIRCRAFT TAXIED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE RIGHT HAND INLET BLEED VALVE. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999111900822 19991119 00822 EU 1999 11 19 RAIA9911019 1 19991116 A 2913 PV304426 PUMP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 433AM 15994 442 885 7069-STL LEFT HYDRAULIC PUMP PRESSURE DROPPED TO ZERO. MAINTENANCE REPLACED HYDRAULIC PUMP ON LEFT ENGINE. 2 L 7 2 4T RT A56EU 1999112500124 19991125 00124 WP 1999 11 25 TWAA9915701 1 19991117 A 3350 58222 POWER SUPPLY DOUG DC9 DC941 302207N WP ROW 8-14 INOP A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 935L 47603 THE FWD SECTION OF COACH CABIN EGRESS LIGHTING WAS INOPERATIVE. REPLACED THE POWER SUPPLY FOR ROWS 8 THRU 14. CHECK-C 9-28-98 STL. 2 L 7 2 4F A6WE 1999112500125 19991125 00125 NM 1999 11 25 TWAA9915702 1 19991117 A 3350 6100928 LAMP BOEING 767 767330 NM ROW 44 WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 THE EGRESS FLOOR LIGHTS WERE INOPERATIVE AT ROW 37 AND 44, RT SIDE OF CABIN. SECURED LOOSE LIGHT SOCKET TO THE LIGHT AS SY AT ROW 37 RH, AND REPLACED THE LAMP AT ROW 44 ON RT SIDE. CHECK-C 6-8-99 MCI. 2 L 7 2 4F RT A1NM 1999112500126 19991125 00126 WP 1999 11 25 TWAA9915703 1 19991117 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP ROW 15-22 WORN A TWAA K NONE O OTHER CR CRUISE 1 CE 05 980Z 47344 THE EGRESS LIGHTS ON LEFT SIDE OF CABIN, ROWS 15 TO 22, FLASHED DURING FLIGHT WITH THE SWITCH IN THE ARM POSITION. REPL ACED THE POWER SUPPLY FOR ROWS 15 TO 22. CHECK-C 9-23-99 STL. 2 L 7 2 4F A6WE 1999112500127 19991125 00127 WP 1999 11 25 CALA9901499 1 19991116 A 3234 SAFETY WIRE DOUG DC10 DC1030 3023501 WP GEAR HANDLE OUT OF POSITION A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 14079 46927 CREW RECEIVED RED GEAR WARNING LIGHTS WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND GEAR WAS EXTENDED MANUALLY. ALL GEAR LIGHTS WERE GREEN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR CONTROL HAND LE WAS NOT MAKING CONTACT WITH SWITCH. MAINTENANCE FOUND SAFETY WIRE ON LANDING GEAR CONTROL CABLE AT HANDLE ASSEMBLY B INDING TO FRAME. THE SAFETY WIRE WAS REMOVED AND REPOSITIONED. THE HANDLE ASSEMBLY WAS CLEANED AND LUBRICATED. A GEAR SWING WAS PERFORMED IAW MM 32-00. GEAR OPERATION AND INDICATIONS CHECKED NORMAL. 2 L 7 3 4F A22WE 1999112500128 19991125 00128 NM 1999 11 25 CALA9901500 1 19991115 A 5755 651734866 SKIN BOEING 727 727232 1384082 NM NR 8 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND THE NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REPLACED IAW MM 27-62-1. 2 L 7 3 4F A3WE 1999112500129 19991125 00129 WP 1999 11 25 CALA9901501 1 19991115 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND FORWARD BAGGAGE BIN DOOR JAMB PAN CORRODED AT STA 370-427. THE CORRODED PAN SECTION WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 1999112500130 19991125 00130 NM 1999 11 25 CALA9901502 1 19991116 A 3350 BATTERIES BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND SELF CONTAINED FIXED EMERGENCY LIGHT INOPERATIVE IN FORWARD CABIN. THE LIGHT ASSEMBLY WAS REMOVED, THE BATTERIES WERE REPLACED, AND THE LIGHT WAS REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-101, PAGE 203. 2 L 7 3 4F A3WE 1999112500131 19991125 00131 NM 1999 11 25 CALA9901503 1 19991116 A 3350 BATTERY BOEING 727 727232 1384082 NM R2 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND R-2 DOOR EXIT IDENTIFIER INOPERATIVE. THE BATTERY PACK WAS REMOVED, CHARGED AND REINSTALLED. OPERATIO N CHECKED GOOD IAW MM 33-50-22, PAGE 401. 2 L 7 3 4F A3WE 1999112500132 19991125 00132 NM 1999 11 25 CALA9901504 1 19991116 A 3350 BATTERY BOEING 727 727232 1384082 NM RT EMER EXIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND THE RT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, CHARGED, AND REINSTA LLED. OPERATION CHECKED GOOD IAW MM 33-50-22, PAGE 401. 2 L 7 3 4F A3WE 1999112500133 19991125 00133 WP 1999 11 25 CALA9901505 1 19991116 A 7110 5930645501ASB716 COWL DOUG DC9 DC982 3022082 WP NR 2 ENGINE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND CORROSION ON INLET SKIN OF NR 2 NOSE COWL INSIDE FRONT ACCESS. THE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01. 2 L 7 2 4F A6WE 1999112500134 19991125 00134 WP 1999 11 25 CALA9901506 1 19991116 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1791 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON SKIN AND AROUND LONGERON 48L AT STA 1791 INSIDE CENTER CARGO COMPARTMENT BELOW FLOOR. THE CORRODED AREA WAS REPAIRED IAW EA 10-5332-2-A0505. 2 L 7 3 4F A22WE 1999112500135 19991125 00135 WP 1999 11 25 CALA9901507 1 19991116 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 229-237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 229-237. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1999112500136 19991125 00136 WP 1999 11 25 CALA9901508 1 19991117 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 THE INTERIOR AND EXTERIOR TAIL CONE RELEASE HANDLES REQUIRED EXCESS FORCE TO DEPLOY TAIL CONE. THE TAIL CONE CABLES WER E ADJUSTED IAW MM 53-53-01. 2 L 7 2 4F A6WE 1999112500137 19991125 00137 WP 1999 11 25 CALA9901509 1 19991117 A 5730 SKIN DOUG DC9 DC982 3022082 WP LT WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND THE LT WING LOWER SKIN SURFACE ADJACENT TO FUEL PANEL 1373C GOUGED. THE SKIN WAS REPAIRED IAW EA 9-573 1-2-A0530 AND ECRA 5730-01669. 2 L 7 2 4F A6WE 1999112500138 19991125 00138 WP 1999 11 25 CALA9901510 1 19991117 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP LT COCKPIT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND CAPTAIN'S RT AFT SEAT TRACK I/B SIDE CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-0 1. 2 L 7 2 4F A6WE 1999112500139 19991125 00139 WP 1999 11 25 CALA9901511 1 19991118 A 3350 60030431 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS ABOVE BOTH LEFT AND RIGHT DOORS INOPERATIVE DURING EMERGENCY LIG HT TEST. THE POWER SUPPLY BATTERY PACK WAS REMOVED AND REPLACED. OPERATION CHECKED GOOD IAW MM 33-53-00, PAGE 407. 2 L 7 2 4F A6WE 1999112500140 19991125 00140 WP 1999 11 25 CALA9901512 1 19991118 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND AFT CARGO DOOR SEAL FLANGE GOUGED AND BENT AT STOPS. AN ANGLE REPAIR WAS INSTALLED ON AFT CARGO DOOR A FT EDGE OF PAN IAW ECRA 5230-01494. 2 L 7 2 4F A6WE 1999112500141 19991125 00141 WP 1999 11 25 CALA9901513 1 19991118 A 5754 SLAT DOUG DC9 DC982 3022082 WP RT LE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND RT WING NR 0 SLAT END LEADING EDGE DENTED AT STA XFS 55. THE DENT WAS BLENDED OUT AND REPAIRED WITH FI LLER IAW SRM 57-03, FIGURE 14B. 2 L 7 2 4F A6WE 1999112500142 19991125 00142 WP 1999 11 25 CALA9901514 1 19991118 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND AFT FUSELAGE LOWER SKIN CORRODED AT AREA UNDER LOWER ANTENNA, FS 1155. THE AREA WAS REPAIRED IAW SRM 5 1-10-3 AND 53-04, FIGURE 38A. 2 L 7 2 4F A6WE 1999112500143 19991125 00143 WP 1999 11 25 CALA9901515 1 19991118 A 5754 SKIN DOUG DC9 DC982 3022082 WP RT LE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND RT WING NR 3 FLAP LEADING EDGE BULL NOSE GOUGED. REPAIRED IAW ECRA 5750-03318 AND INSTALLED NEW CHAFE STRIP IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999112500144 19991125 00144 WP 1999 11 25 CALA9901516 1 19991118 A 5247 SKIN DOUG DC9 DC982 3022082 WP APU DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A 2 INCH CRACK WITH GOUGE IN APU DOOR OUTER SKIN. A DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 2, 51- 10-3, AND 52-10, FIGURE 2. 2 L 7 2 4F A6WE 1999112500145 19991125 00145 SO 1999 11 25 COMA9910173 1 19991116 A 5270 WARNING EMB 120 EMB120RT SO CARGO DOOR ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 257CA 120248 CARGO DOOR WARNING DURING TAKEOFF. DEFERRED DOOR WARNING, AIRCRAFT CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1999112500146 19991125 00146 EA 1999 11 25 COMA9960695 1 19991116 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR NOT LATCHED A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 SO 01 915CA 7013 CABIN DOOR LATCH CAUTION MESSAGE. PERFORMED OPERATIONAL CHECK OF CABIN DOOR LATCH WARNING SYSTEM. NO DEFECTS NOTED. S USPECT HANDLE NOT IN FULLY CLOSED POSITION. 2 L 7 2 4F RT A21EA 1999112500147 19991125 00147 EA 1999 11 25 COMA9960696 1 19991115 A 2120 196305 FILTER CNDAIR CL600 CL6002B19 EA E/E COMPT DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 938CA 7046 DISPLAY COOL CAUTION MESSAGE. REPLACED DIRTY AIR FILTER. 2 L 7 2 4F RT A21EA 1999112500148 19991125 00148 EA 1999 11 25 COMA9960697 1 19991115 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 CABIN DOOR WARNING. ADJUSTED DOOR LATCHING MECHANISM. 2 L 7 2 4F RT A21EA 1999112500149 19991125 00149 EA 1999 11 25 COMA9960698 1 19991115 A 3620 356024310 ELEMENT CNDAIR CL600 CL6002B19 EA LT FALSE WARNING A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 964CA 7129 LEFT 14TH STAGE BLEED AIR DUCT LEAK WARNING. REPLACED THE LEFT PYLON BLEED AIR LEAK DETECTION LOOP. 2 L 7 2 4F RT A21EA 1999112500150 19991125 00150 EA 1999 11 25 COMA9960699 1 19991117 A 5320 601R40122 BRACKET CNDAIR CL600 CL6002B19 EA COCKPIT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 15743 7012 THE NUT PLATE MOUNTING BRACKET FOR DADO PANEL 241DLW WAS FOUND BROKEN AT THE CLIP NUT PLATE SLOT. PERFORMED A MAJOR REP AIR BY REPLACING NUT PLATE. MOUNTING BRACKET FOR DADO PANEL 241DLW IAW WVAC EO 601R-53-0620. 2 L 7 2 4F RT A21EA 1999112500151 19991125 00151 EA 1999 11 25 COMA9960700 1 19991117 A 3230 PIN CNDAIR CL600 CL6002B19 EA NLG NOT REMOVED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 977CA 7157 NLG DID NOT RETRACT. REMOVED DOWNLOCK SAFETY PIN FROM NLG. 2 L 7 2 4F RT A21EA 1999112500152 19991125 00152 NM 1999 11 25 QXEA9902345 1 19991112 A 3350 SWITCH DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 831PH 328 PDX- FLIGHT ATTENDANTS LIGHTING PANEL EMERGENCY LIGHT SWITCH INTERMITTANT. REMOVED AND REPLACED LIGHT SWITCH, OPERATION AL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999112500153 19991125 00153 NM 1999 11 25 QXEA9902346 1 19991116 A 5210 CABLE DHAV DHC8 DHC8102 2809003 NM PAX DOOR OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 YYJ- UNABLE TO OPEN MAIN CABIN DOOR. INSPECTED AND FOUND CABLE OFF PULLEY. DISCONNECTED DOOR CABLE. DOOR COUNTER BALA NCE INOPERATIVE. FERRIED AIRCRAFT TO PDX. REMOVED AND REPLACED BOTH LEVER CABLES, OPERATION CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999112500154 19991125 00154 NM 1999 11 25 99FDEA00483 1 19991114 A 2910 HYDRAULIC LINE DOUG MD11 MD11 3023602 NM LT MLG DISCONNECTED A FDEA A J UNSCHED LANDING DUMP FUEL J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 SO 25 584FE 48436 ON DEPARTURE, GEAR HANDLE WAS RAISED, LEFT MAIN WAS UNSAFE, RAN CKLIST. RECYCLED THEN GOT A HYD SYS 3 FAIL. *S/D* REM OVED AND REPLACED HYD FILTERS AND NR 3 LWR HYD PUMP, TRIM CYLINDER, HYD LINE, BRACKETS, CONDUIT AND HARNESS. 2 L 7 3 4F RT A22WE 1999112500155 19991125 00155 WP 1999 11 25 ABXA9900794 1 19991116 A 3350 MP701 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP COCKPIT FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 982AX 47317 EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHTING 5 AMP CIRCUIT BREAKER IAW DC9 MM 33-53, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999112500156 19991125 00156 WP 1999 11 25 ABXA9900795 1 19991115 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 966AX 47510 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1999112500157 19991125 00157 WP 1999 11 25 ABXA9900796 1 19991108 A 5730 56429402 SKIN DOUG DOUG DC8 DC862 3021970 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 DURING C-CHECK, CRACK INDICATIONS WERE FOUND IN SEVERAL RIGHT WING UPPER AFT SKIN PANEL 505F ATTACH HOLES. REPAIRED IAW ABX REA D857-33607MR. 2 L 7 4 4F 4A25 1999112500158 19991125 00158 WP 1999 11 25 ABXA9900797 1 19991111 A 5320 992230D1 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT VERTICAL SUPPORT FITTING CRACKED AT STATION 980. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51 -30-5. 2 L 7 2 4F A6WE 1999112500159 19991125 00159 WP 1999 11 25 ABXA9900798 1 19991111 A 5321 99578275 FLOOR DOUG DOUG DC9 DC932F 3022067 WP BS 140-160 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND COCKPIT FLOOR PANEL CORRODED FROM STATION 140-160 AND RBL 10-48. REPLACED FLOOR PANEL IAW DC9 SRM 53-21-0. 2 L 7 2 4F A6WE 1999112500160 19991125 00160 WP 1999 11 25 ABXA9900799 1 19991111 A 5320 991015163 WEB DOUG DOUG DC9 DC932F 3022067 WP BS 614 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 614. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999112500161 19991125 00161 WP 1999 11 25 ABXA9900800 1 19991112 A 5753 59121682 SKIN DOUG DOUG DC9 DC931 3022065 WP RT TE FLAP VANE DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND RIGHT WING MOVABLE VANE DELAMINATED. REPLACED RIGHT FORWARD MOVABLE VANE IAW DC9 MM 27-51-2. 2 L 7 2 4F A6WE 1999112500162 20010117 00162 WP 2001 1 17 MWEA99825 1 19991108 A 2420 91415074 RELAY DOUG DC9 DC932 3022066 WP E/E BAY FAILED A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 206ME 47791 MCI - FLT 580 - SMELLED ELECTRICAL SMOKE IN COCKPIT PRIOR TO DEPARTURE. MTC DEFERRED APU AND REMOVED AND REPLACED LEFT APU POWER RELAY. (X) 2 L 7 2 4F A6WE 1999112500163 19991125 00163 NM 1999 11 25 VNAA9911012 1 19991115 A 3610 4067B000002 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 441JS 7676 3059 116124 THE FLIGHT CREW RECEIVED A LEFT HAND LOW PRESSURE BLEED VALVE FAIL CAS MESSAGE DURING THE TAKEOFF ROLL. WHILE TALKING T O MAINTENANCE CONTROL THE CAS MESSAGE CLEARED. THE FLIGHT CREW AGAIN ATTEMPTED TO TAKEOFF AND RECEIVED THE SAME LEFT HA ND LOW PRESSURE BLEED VALVE FAIL CAS MESSAGE. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITH NO FURT HER INCIDENT. MAINTENANCE INSPECTED AND REPLACED LEFT HAND LOW PRESSURE BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENA NCE MANUAL 36-11-03. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999112500164 19991125 00164 NM 1999 11 25 VNAA9911013 1 19991104 A 3250 MS3476W1419P CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 459PS 3070 DURING TAKEOFF, THE NOSE WHEEL STEERING FAILED. THE FLIGHT CREW REGAINED CONTROL AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE NOSE WHEEL STEERING CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-51-06. OPER ATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999112500165 19991125 00165 NE 1999 11 25 VNAA9911014 2 19991117 A 7321 311888804 FUEL CONTROL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 437JS 9203 3055 116145 DURING TAKEOFF, THE FLIGHT CREW RECEIVED A RIGHT HAND ENGINE ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE. THE CREW ABORTED TAKE OFF. THE CREW CYCLED THE ELECTRONIC ENGINE CONTROL UNIT ON THE RAMP AND IT RESET. PERFORMED A STATIC RUN UP AND IT REMAINED GOOD. THE CREW THEN PROCEEDED BACK TO THE RUNWAY FOR ANOTHER TAKEOFF. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999112500166 19991125 00166 NE 1999 11 25 VNAA9911015 2 19991117 A 7321 311995704 FUEL CONTROL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 437JS 9203 3055 116145 DURING TAKEOFF, THE FLIGHT CREW RECEIVED A RIGHT HAND ENGINE ELECTRONIC CONTROL UNIT FAIL CAS MESSAGE AND THE CREW ABORT ED TAKEOFF. THE CREW THEN FERRIED THE AIRCRAFT TO DAY WHERE MAINTENANCE INSPECTED AND CLEANED THE IBV AND ITS CANNON PL UG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-00-00. FUNCTION CHECKS WERE PERFORMED IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 71-01-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999112500167 19991125 00167 WP 1999 11 25 CA991027001 1 19991005 A 2432 3S2060DM169A1 BATTERY CHARGER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE E/E BAY FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 45311 19142 455154 (CAN) AT CRUISE, BATTERY AND LEFT EMERGENCY AC BUS WERE PULSATING. RESET BATTERY CHARGER CIRCUIT BREAKER, PROBLEM STILL EVIDENT. CHARGING STOPPED COMPLETELY, VOLTAGE DROPPED TO 20 VOLTS. AFTER STARTING DIVERSION CHARGING STARTED TO CYCLE FOR APPROXIMATELY 5 MINUTES, THEN PEGGED AT 50 AMPS AND BATTERY CHARGER CIRCUIT BREAKER TRIPPED. LANDED OK. REPLACED BATTERY CHARGER, BATTERIES, CIRCUIT BREAKER. 2 L 7 3 4F 4 F A22WE E23EA 1999112500168 19991125 00168 1999 11 25 CA991027006 4 19991015 A 3414 2083081 INDICATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE COCKPIT FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 47826 702782 (CAN) CAPTAIN'S MACH AIRSPEED INDICATOR CYCLING ZERO TO 450 FTS, CIRCUIT BREAKER RESET, INDICATION NORMAL. ON TAKEOFF R OLL, AIRSPEED WENT U/S AGAIN, TAKEOFF ABANDONED, RETURNED TO RAMP. MACH AIRSPEED INDICATOR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999112500169 19991125 00169 NM 1999 11 25 CA991027008 1 19991018 A 2917 7209 VALVE BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE HYD PRESSURE FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 9658 378 709396 (CAN) ON DESCENT, NR 1 HYDRAULIC SYSTEM PUMP FAILED, HALFWAY THROUGH CHECK LIST, NR 2 A-PUMP LOW PRESSURE LIGHT CAME ON, WITH CORRESPONDING DROP OF A-SYSTEM PRESSURE. LOSS OF A-SYSTEM PRESSURE CHECK LIST CARRIED OUT , NR 1 AND NR 2 ENGINE CASE DRAIN FILTERS CHECKED PER WORK CARD 1124-1 AND -2. NO FAULTS FOUND. HYDRAULIC SYSTEM PRESSURE REGULATOR REPLACE D. 2 L 7 2 4F 4 F A16WE E2EA 1999112500170 19991125 00170 NM 1999 11 25 CA991027009 1 19991019 A 3244 26088115 TIRE BOEING 767 767375 NM GE CF6 CF680C2B6 30025 NE LT MLG FAILED W C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 CA 30163 8608 690221 (CAN) AFTER LANDING, MAINTENANCE REPORTED SEVERE AIRCRAFT DAMAGE DUE NR 6 TIRE TREAD BLOWN. SEVERE DAMAGE TO LEFT INBO ARD FLAP, LEFT MAIN FLAP, AND NR 6 SPOILER. PARTS REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 1999112500171 19991125 00171 EA 1999 11 25 CA991027038 2 19991008 A 7230 ROTOR BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA NR 1 ENGINE DAMAGED W E ENGINE SHUTDOWN E VIBRATION/BUFFET NR NOT REPORTED 1 CA 10342 4391 CPPS60514 (CAN) POSSIBLE STATOR AND ROTOR DAMAGE. FOD - ENGINE TEAR DOWN RQUIRED TO CONFIRM. 1 G 7 1 4U 4 U H4SW E22EA 1999112500172 19991125 00172 SO 1999 11 25 CA991027040 2 19991010 A 8520 631716 CRANKSHAFT CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO HARTZL HCJ3Y PHCJ3YF1 GL ENGINE FAILED W A UNSCHED LANDING E VIBRATION/BUFFET AP APPROACH 1 CA 4972 1535 870096 247559R FP929A (CAN) CRANKSHAFT FAILED - THERE ARE MAINTENANCE LOG ENTRIES OF PREVIOUS PROP STRIKE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P36EA 1999112500173 19991125 00173 EA 1999 11 25 CA991027051 2 19990824 A 7531 3029266 COVER BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA COMPRESSOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA CPPS6058 (CAN) P3 FILTER SPINNING IN THE COVER CAUSING INTERNAL WEAR OF THE UNIT. 1 G 7 1 4U 4 U H4SW E22EA 1999112500174 19991125 00174 NE 1999 11 25 CA991027054 2 19990815 A 7532 0177555170 TACH BOX SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COMPRESSOR FAILED W A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 CA 1071B 956 (CAN) TACHOMETER BOX DOES NOT HAVE OUTPUT TO CLOSE BLEED VALVE. 1 G 7 1 3U 3 U H9EU E19EU 1999112500175 19991125 00175 SW 1999 11 25 CA991027056 1 19990604 A 6310 20604023025 SEAL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FREEWHEEL ASSY FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 997 BLA2677 CAE820651 (CAN) FORWARD SEAL FAILED AT 60 HOURS AFTER INSTALLATION. 1 G 7 1 3U 3 U H2SW E4CE 1999112500176 19991125 00176 SW 1999 11 25 CA991027057 1 19990806 A 5210 ROLL PIN BELL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN DOOR WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE801518BA (CAN) DOOR HANDLE CAME OFF SEVERAL TIMES. IT WAS DISCOVERED THAT THE WRONG PIN WAS INSTALLED. PROPER PIN INSTALLED. 1 G 7 1 3U 3 U H2SW E4CE 1999112500177 19991125 00177 GL 1999 11 25 CA991027059 2 19990717 A 7240 23031260 COMBUSTION CASE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE CRACKED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA 6870992J CAE830542 (CAN) CRACK FOUND IN ARMPIT OF THE OUTER COMBUSTION CASE. CRACK WAS ABOUT 2 INCHES LONG. 1 G 7 1 3U 3 U H2SW E4CE 1999112500178 19991125 00178 SW 1999 11 25 CA991027061 1 19990722 A 6320 206040002025 DRAG PIN BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R TRANSMISSON FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1574 B1299 CAE830542 (CAN) STAKING ON THE DRAG PIN FAILED 35.6 HOURS AFTER INSTALLATION. 1 G 7 1 3U 3 U H2SW E4CE 1999112500179 19991125 00179 SW 1999 11 25 CA991027062 1 19990208 A 2810 206063668001 HOSE BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL FUEL CELL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA CAE830144 (CAN) FORWARD FUEL TANK VENT HOSE LEAKED SLIGHTLY WHEN FULL. THE MANUFACTURER DATE ON THE HOSE WAS 7-76. 1 G 7 1 3U 3 U H2SW E4CE 1999112500180 19991125 00180 EU 1999 11 25 CA991027063 1 19990628 A 6720 PEDAL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TAILROTOR STIFF W K NONE O OTHER IN INSP/MAINT 1 CA CAE836260 (CAN) PILOT NOTED THAT TAIL ROTOR PEDALS WERE STIFF ON PRE-FLIGHT CHECK. TAIL ROTOR PITCH CHANGE SYSTEM CHECKED AND CLE ANED. AIRCRAFT RETURNED TO SERVICE. 1 G 7 2 3U 3 U H3EU E4CE 1999112500181 19991125 00181 WP 1999 11 25 CA991027064 1 19990914 A 7921 369D25630 BLOWER HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL OIL COOLER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 8089 287 V1010 CAE830926 (CAN) OIL COOLER BLOWER VIBRATING EXCESSIVELY AND ALSO SHOWED SIGNS OF GREASE LOSS. 1 G 7 1 3U 3 U H3WE E4CE 1999112500182 19991125 00182 WP 1999 11 25 CA991027065 1 19990910 A 7714 369D24518 INDICATOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL DUAL TACH INACCURATE W K NONE O OTHER IN INSP/MAINT 1 CA 61 400D CAE830926 (CAN) 16 PERCENT TACH NEEDLE SPLIT AT THE HIGH END OF THE RANGE. 1 G 7 1 3U 3 U H3WE E4CE 1999112500183 19991125 00183 SW 1999 11 25 CA991027066 1 19990927 A 7931 206040088005 PISTON BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL PRESS REGULATOR WORN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA CAE831866 (CAN) OIL PRESSURE REGULATOR WAS FOUND TO HAVE THE PISTON INSTALLED UPSIDE DOWN. UNIT WAS REPLACED BECAUSE OF INTERNAL WEAR. 1 G 7 1 3U 3 U H2SW E4CE 1999112500184 19991125 00184 EU 1999 11 25 CA991027068 1 19990930 A 3010 SWITCH FOKKER F28 F28MK1000 4990808 EU ANTI ICING SYS FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) ON TAKEOFF, DUCT LIGHT CAME ON WITH SELECTION OF THE AIRFOIL ANTI-ICE. THE WING ANTI-ICE PRIMARY OVERHEAT LIGHT CA ME ON AND THE SHUT-OFF VALVE BEGAN TO CYCLE. AIRCRAFT RETURNED TO BLOCKS. REPLACED DUCT LEAK SENSING SWITCH. TEST FL IGHT INDICATED SERV HOWEVER THE PRIMARY OVERHEAT STILL ON. REPLACED THIRD LT INBOARD LEADING EDGE. 2 L 7 2 4F RT A20EU 1999112500185 19991125 00185 WP 1999 11 25 CA991027072 2 19991003 A 7321 89778021 FCU BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110UG 01514 WP ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 4529 1944711 P63111 (CAN) POWER SETTING COULD NOT BE ALTERED USING POWER LEVER. FCU CHANGED. 2 L 7 2 4T 4 T RT BA15CAA E4WE 1999112500186 19991125 00186 SW 1999 11 25 CA991027075 1 19991009 A 5210 205030245037 BRACKET 205030245183 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE PASSENGER DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA LEO7194X (CAN) DURING DOOR PANEL REPLACEMENT, THE DOOR POST SUPPORT WAS FOUND CRACKED WHICH HOLDS THE MAIN LATCH FOR THE CREW DOO R. FURTHER INVESTIGATION REVEALED THAT THE LT DOOR SUPPORT WAS ALSO CRACKED. SUBMITTER STATED IF LEFT LONGER, THE SUPP ORTS WOULD HAVE FAILED AND POSSIBLY RESULTED IN FAILURE OF THE DOORS. 1 G 7 1 4U 4 U H1SW E17EA 1999112500187 19991125 00187 SW 1999 11 25 CA991027077 1 19991014 A 6710 471402525 BEARING 204010925009 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE MAIN ROTOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA LE07158X (CAN) DURING DAILY INSPECTION, THE BEARING WAS FOUND UNSERVICEABLE. THE BEARING IS HELD IN THE ROD END BY SWAGING AND F AILED ALLOWING THE BEARING TO SLIDE OUT OF THE ROD END. REPLACED. 1 G 7 1 4U 4 U H1SW E17EA 1999112500188 19991125 00188 NM 1999 11 25 CA991027078 1 19991018 A 2910 6517644140 LINE BOEING 727 727116C NM PWA JT8 JT8D7B 52053 NE BS 1253 FAILED W H DEACTIVATE SYST/CIRCUITS F K FLT CONT AFFECTED FLUID LOSS DE DESCENT 1 CA 649375 (CAN) ON DESCENT, CREW NOTICED THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT ON FOLLOWED BY A TOTAL LOSS OF ALL A-SYSTEM OIL . AIRCRAFT LANDED BY ALT MEANS AND TOWED OFF RUNWAY. A-SYSTEM RETURN LINE IN AFT AIRSTAIR AREA HAD FAILED, NEW LINE INSTALLED. 2 L 7 3 4F 4 F A3WE E2EA 1999112500190 19991125 00190 SW 1999 11 25 CA991027080 1 19990915 A 6320 206040002015 GEARBOX BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL MAIN ROTOR MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 1319 CAE821945F (CAN) MAGNETIC CHIP PLUG WAS CONTAMINATED WITH FERROUS METAL FROM MAIN GEARBOX. 1 G 7 1 3U 3 U H2SW E4CE 1999112500192 19991125 00192 EU 1999 11 25 CA991028002 1 19990923 A 6710 0292928150 HMU SNIAS AS350 AS350B3 8680954 EU ENGINE FAILED W H DEACTIVATE SYST/CIRCUITS E VIBRATION/BUFFET AP APPROACH 1 CA 485 192B (CAN) HMU FAILED WITH RED 'GOV' LIGHT ON CAUTION PANEL. 1 G 7 1 3U NC H9EU 1999112500194 19991125 00194 EA 1999 11 25 CA991028013 2 19990927 A 8540 LW11053C CRANK CASE O360A1A PIPER PA23 PA23160 7102304 SO LYC O360 O360A1A 41514 EA HARTZL HCC2Y HCC2YK2 GL ENGINE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1942 L1525936A L1525936A BC202 (CAN) CRACK FOUND IN VICINITY OF STARTER PAD. 1 L 7 2 3O 3 O 1A10 E286 5 C P920 1999112500195 19991125 00195 EU 1999 11 25 CA991028019 1 19991011 A 2910 5316JM301 VALVE AIRBUS 330 A330202 3930316 EU HYD MANIFOLD LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) COMPLETE LOSS OF YELLOW SYSTEM HYDRAULIC FLUID. INVESTIGATION REVEALED A FAULTY O-RING ON CHECK VALVE 5316JM301. 2 L 7 2 4F RT A46NM 1999112500196 19991125 00196 1999 11 25 CA991028026 4 19991015 A 3457 KLN90B0660403111 RECEIVER PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE GPS MALFUNCTIONED W O OTHER O OTHER CR CRUISE 1 CA 2770 25924 PCEPR0050 (CAN) UNIT SUCCESSFULLY COMPLETED ITS SELF-TEST AND ACQUIRED ENOUGH SATELLITES TO ENTER NAV 'D' MODE WITH THE INCORRECT DATE. 1 L 7 1 3T 4 T RT A78EU E26NE 1999112500197 19991125 00197 NE 1999 11 25 CA991028027 2 19991005 A 8520 8760 WASHER 399353 BEECH 18 E18S9700 1151008 CE PWA R985 R985AN14B 52008 NE HAMSTD 22D 22D30 NE EXHAUST VALVE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 541 436714 E2248 (CAN) CRACK ON EXHAUST VALVE GUIDE SPRING RETAINER WASHER CAUSING LOW EXHAUST VALVE. 1 L 7 2 3R 3 R A765 5E1 5 C P736 1999112500198 19991125 00198 EU 1999 11 25 CA991028030 1 19991013 A 7830 AS78301011 THRUST REVERSER ISRAEL 1125 ASTRASPX 4500205 EU LT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 915 DHC0011 (CAN) CRACK FOUND ON LEFT TAIL ROTOR ASSY INSIDE TAILPIPE ON LEFT UPPER EDGE APPROXIMATELY 2 INCHES IN LENGTH. 2 L 7 2 4F RT A16NM 1999112500199 19991125 00199 1999 11 25 CA991028032 4 19991008 A 6122 582855 HOUSING LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE PROP VALVE FAILED W E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA 2216 C5514 500934 N212585 (CAN) TORQUE DECAY AND DROPPING RPM EXIBITED. THE GOVERNOR EXIBITED FAILURE AT PROP VALVE HOUSING REMOVAL. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1999112500201 19991125 00201 NE 1999 11 25 CA991028040 2 19990902 A 7250 BEARING BOEING 767 767333 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE LEAKING W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA P724730 (CAN) ON TAKEOFF, SMOKE DETECTED IN CENTER LAVATORY MS2 ACTIVATED, ELECTRICAL SMELL REPORTED NEAR MIDDLE GALLEY, BUSSES TURNED OFF, SMELL DISSIPATED. NR 1 ENG BEARING LEAKING, REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999112500202 19991125 00202 NE 1999 11 25 CA991028044 2 19991005 A 7320 FADEC AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE FAILED W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA 731301 (CAN) NR 2 FADEC B FAULT, ENGINE REMOVED, TEAR DOWN TO FOLLOW. 2 L 7 2 4F 4 F RT A28NM E29NE 1999112500204 19991125 00204 SO 1999 11 25 CA991028054 1 19991012 A 3710 442GW6 PUMP PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL RT ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CA 575 L159368A DJ11486A (CAN) INSTALLED 99-01-05. ALL HOSES FROM FIREWALL TO PUMP THEN REPLACED AND P/N B3-5-1 AIR INLET FILTER REPLACED AND C HANGED AT EACH 100 HR INTERVALS. FAILED PUMP THEN REPLACED WITH OVERHAULED PUMP FROM BRIDGEMARK AEROSPACE LTD. ADDITIO NAL INFORMATION FROM NAMEPLATE: VVFAA REF. 004189; PMA PART NO: 82-50122-2; SERIAL NR: A1035. THIS IS A REPEATED TYP E OF FAILURE FROM THIS SUPPLY SOURCE. PUMP REPLACED WITH ZERO HRS. UNIT FROM DIFFERENT CERTIFIED SUPPLIER. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999112500206 19991125 00206 SO 1999 11 25 CA991028061 1 19991014 A 8120 LW31S444 BOLT TIO540J2BD PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL LT ENGINE SHEARED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 1485 L586361A L586361A DJ11486A (CAN) BOLT FAILURE AT TURBOCHARGER MOUNT. OPERATOR SUSPECTS IMPROPER INSTALLATION FROM OVERHAULER. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999112500207 19991125 00207 SW 1999 11 25 CA991028071 1 19991012 A 7810 6853511 EXHAUST STACK BELL 206 206L 1181522 SW ALLSN 250C 250C20J 03013 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4181 7133 CAE270419 (CAN) CRACK WAS FOUND IN THE AREA OF THE EXHAUST STACK RETAINING CLAMP. 1 G 7 1 3U 3 U H2SW E4CE 1999112500210 19991125 00210 SO 1999 11 25 CA991103001 2 19991013 A 8520 LIFTER TSIO520C CESSNA 182 182N 2072730 CE CONT O520 TSIO520C 17040 SO MCAULY D3A34 D3A34C401 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1596 1780269CR 1780269CR 961512 (CAN) HYDRAULIC LIFTERS FAILING TO KEEP CONTACT WITH CAMS. NEW P/N INSTALLED. 1 H 7 1 3O 3 O NT 3A13 E8CE 5 C P47GL 1999112500211 19991125 00211 NM 1999 11 25 CA991103002 1 19991020 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 8741 8286 02900520 02900520 870537 (CAN) OIL TEMPERATURE NEAR MAX. OIL COOLER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999112500212 19991125 00212 EU 1999 11 25 CA991103007 1 19991025 A 3233 104626002 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NLG CORRODED W C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 CA 27133 1837 DRG927886 LF05542A (CAN) FLIGHT CREW REPORTED A CLUNKING NOISE COMING FROM THE NLG WELL. INVESTIGATION REVEALED A LOSS OF SEALANT AROUND T HE NOSE GEAR ACTUATOR ROD END. ROD END HAD LOST MOST OF ITS LOCKING. ACTUATOR REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999112500213 19991125 00213 WP 1999 11 25 CA991103012 1 19990921 A 7920 105HBG312 OIL PUMP 5602300 HILLER UH12 UH12E 4360122 WP ALLSN 250C 250C20B 03013 GL TRANSMISSION SEIZED W E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CA 10 117 CAE833503 (CAN) TRANSMISSION OIL PUMP HAD FAILED, FAILING TO LUBRICATE THE LOWER MAIN ROTOR TRANSMISSION RGB CAUSING IT TO SEIZE. TEAR DOWN TO FOLLOW. 1 G 7 1 3O 3 U 4H11 E4CE 1999112500214 19991125 00214 EA 1999 11 25 CA991103017 2 19991014 A 7532 PISTON FLANGE 3033063 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA BLEED VALVE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 2758 CPPS62075 (CAN) ENGINE SURGING EXPERIENCED. BLEED VAVE HAS HISTORY OF CAUSING SIMILAR PROBLEMS ON OTHER AIRCRAFT. REF: PT6 SB 5 274R3 FOR IMPROVED BLEED VALVE CLOSING OPS. 1 G 7 1 4U 4 U H4SW E22EA 1999112500215 19991125 00215 EU 1999 11 25 CA991103023 1 19991018 A 3260 622800200 SWITCH BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL MLG FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA P63174C DRG138781 (CAN) GEAR WAS SLECTED DOWN ON APPROACH AND THE CREW FAILED TO GET A NOSE GEAR DOWN AND LOCKED (GREEN) LIGHT. GEAR IN T RANSIT (RED ) LIGHT REMAINED ILLUMINATED. AFTER A LOW PASS FOR GROUND OBSERVATION, THE AIRCRAFT LANDED SAFELY. MAINTEN ANCE FOUND THE NOSE GEAR DOWN AND LOCKED MICROSWITCH FAILED IN THE OPEN POSITION. 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C P61GL 1999112500217 19991125 00217 EU 1999 11 25 CA991103045 1 19991023 A 7830 NAS161228 O-RING 70M00339 AIRBUS 330 A330322 3930325 EU PWA 4168 PW4168 NE THRUST REVERSER CRACKED W H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 733336 (CAN) THRUST REVERSER HYDRAULIC FILTER ASSY O-RING WAS FOUND CUT AND EXTRUDED. 2 L 7 2 4F 4 F RT A46NM E36NE 1999112500218 19991125 00218 EA 1999 11 25 CA991103056 2 19991014 A 7314 GASKET ROMEC RG9080J7A PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL FUEL PUMP LEAKING W A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA C8234 L320561A DJ9946A (CAN) FUEL LEAKING AT FLANGE AND ON DRIVE SIDE OF PUMP. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999112500220 19991125 00220 NM 1999 11 25 CA991103058 1 19991026 A 2432 29069 BATTERY BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE E/E BAY FAILED W H DEACTIVATE SYST/CIRCUITS B H J SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 4150 665392 (CAN) ON ARRIVAL WITH LOW BATTERY VOLTAGE DEFECT WRITTEN UP IN THE LOG BOOK. THE BATTERY WAS BEING CHARGED BY ELECTRICA L BATTERY CHARGER ON GROUND SERVICE. GROOMING CREW NOTICED FUMES AND SMOKE IN THE CABIN AND EVACUATED AIRCRAFT. BATTER Y REMOVED. BATTERY CHARGER HAD TRIPPED THE CIRCUIT BREAKER AND WAS ALSO UNSERVICEABLE. THE BATTERY AND BATTERY CHARGER WERE REPLACED AND SYSTEM SERVICEABLE. BATTERY HAD UNSERVICEABLE CELL'S ' AND BEYOND REPAIR. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999112500221 19991125 00221 CE 1999 11 25 CA991103059 1 19991017 A 3211 0541153 U BOLT CESSNA 172 172I 2072426 CE LYC O320 O320E2D 41508 EA MCAULY 1C172 1C172* GL LT MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 3221 L2269127A E10406 (CAN) DURING PRE-LIGHT INSPECTION, LEFT MAIN LANDING GEAR LEG FAIRING WAS FOUND DISPLACED (STICKING OUT). U-BOLT FOUND BROKEN, AFT END. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999112500223 19991125 00223 EU 1999 11 25 CA991103065 1 19990520 A 6130 FE1595006 BRAKE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE PROPELLER FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 336 120678 871242 (CAN) PROPELLER BRAKE FAILED DUE FAILURE OF COMPONENT, PN FE1595006. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999112500224 19991125 00224 EU 1999 11 25 CA991103066 1 19990926 A 7920 SEAL 3038450 AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE OIL PUMP CUT W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 153 2483391 120619 890429 (CAN) HP OIL PUMP SEAL CUT AND EXTRUDED CAUSING OIL LEAK AND LOW PRESSURE. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999112500225 19991125 00225 EU 1999 11 25 CA991103070 1 19991025 A 2530 24E507009G03 WATER HEATER AIRBUS 330 A330243 3930330 EU GALLEY OVERHEATED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) BURNT SMELL REPORTED BY CREW. THROUGH INVESTIGATION BY MAINTENANCE REVEALED BURNT SMELL COMING FROM SPILLED COFFE E ON HOT PLATE. 2 L 7 2 4F RT A46NM 1999112500226 19991125 00226 WP 1999 11 25 CA991103090 1 19991019 A 2841 INDICATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE FUEL QUANTITY FAILED W C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA P657724D (CAN) SHORTLY AFTER TAKEOFF, RIGHT WING FUEL GAUGE INDICATED 6200, WAS 9100 AT TAKEOFF. RIGHT FUEL QUANTITY INDICATOR R EPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1999112500227 19991125 00227 NM 1999 11 25 CA991103091 1 19991014 A 3244 TIRE BOEING 747 747433 NM PWA 4056 PW4056 NE MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 CA P724345 (CAN) DURING WALK-AROUND, FOUND NR 11 TIRE TREAD PEELED OFF CAUSING DAMARE TO SEVERAL PANELS AND HARNESS DAMAGE. TIRE RE PLACED, PANELS AND HARNESS REPAIRED. 2 L 7 4 4F 4 F RT A20WE E24NE 1999112500228 19991125 00228 1999 11 25 CA991103093 4 19991015 A 2310 TRANSDUCER BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE HF COMM FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA P707548 (CAN) BOTH HF RADIOS U/S. COULD BE HEARD BUT NOT RECEIVED. LEFT CONTROL PANEL, LEFT COUPLER AND LEFT TRANSDUCER REPLA CED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999112500229 19991125 00229 NM 1999 11 25 CA991103094 1 19991004 A 7714 TACH GEN BOEING 767 767275 1385155 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA P709606 (CAN) RIGHT ENGINE N2 ANALOG AND N2 READING ZERO AT ENGINE RUNNING. N2 TACHOMETER/GENERATOR REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999112500230 19991125 00230 NM 1999 11 25 CA991103095 1 19991015 A 2530 OVEN FAN BOEING 767 767275 1385155 NM PWA JT9 JT9D7R4D 52054 NE GALLEY BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P709688 (CAN) IN CRUISE, SMOKE COMING FROM AREA NEAR CENTER OVEN REAR GALLEY. ALL OVENS SHUT OFF, CIRCUIT BREAKERS PULLED. S MOKE DISSIPATED, OVENS LEFT OFF FOR DURATION OF FLIGHT. NR 2 RIGHT FAN BURNT AND SEIZED, REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999112500231 19991125 00231 CE 1999 11 25 CA991104007 1 19991028 A 8120 C1650020102 CONTROLLER ROTOMASTER C1650020102 CESSNA 335 335 2075601 CE CONT O520 TSIO520EB 17040 SO TURBOCHARGER SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA C104986 510526 (CAN) AFTER REPLACEMENT OF TURBO CONTROLLER, ADJUSTMENTS TO ENGINE POWER COULD NOT BE MADE DUE TO SEIZED ADJUSTMENT SCRE W. SUBMITTER STATES UNIT RECEIVED FROM SUPPLIER AS A FACTORY (RAJAY) OVERHAUL. 1 L 7 2 3O 3 O 3A25 E8CE 1999112500232 19991125 00232 1999 11 25 CA991112008 4 19991104 A 3423 2589419901 FLUX VALVE BOEING 737 737204 1384458 NM PWA JT8 JT8D15 52051 NE HSI STICKING W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA P688672 (CAN) DURING FLIGHT, CAPTAIN'S HSI WAS DETERMINED TO BE GIVING WRONG HEADING INFORMATION. FLIGHT RETURNED TO BASE. DI RECTIONAL GYRO SWAPPED AND MAG FLUX VALVE INOPERATIVE, REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999112500234 19991125 00234 WP 1999 11 25 TWAA9915802 1 19991108 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 180 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9414W 53189 DURING CHECK-C MAINT, THE FORWARD GALLEY FLOORBEAM WAS FOUND CORRODED AT STA 180, RBL 6 IN TO RBL 40 INCHES. REPLACED T HE PART PER SPM 6-70-01, PAGE 2. 2 L 7 2 4F RT A6WE 1999112500235 19991125 00235 WP 1999 11 25 TWAA9915803 1 19991108 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9414W 53189 DURING CHECK-C MAINT THE FORWARD GALLEY FLOOR FRAME WAS FOUND CORRODED AT STA 200, RBL 6 IN TO RBL 42 INCHES. REMOVED F LOORBEAM AND FABRICATED PART FROM TWA STOCK. ALODINED AND PAINTED. REINSTALLED FLOORBEAM WITH RIVETS AND ORIGINAL HI-L OKS PER SPM 6-70-01. 2 L 7 2 4F RT A6WE 1999112500236 19991125 00236 WP 1999 11 25 TWAA9915804 1 19991108 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 579 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LONGERON 29L AFT OF STA 579, WITH ABOUT A 6 INCH CRACK IN THE I/B SIDE OF FLANGE OF LONG ERON. INSTALLED LONGERON END AND SPLICE PER SRM 53-02, FIG 14 AND ARA 16211B. 2 L 7 2 4F A6WE 1999112500237 19991125 00237 WP 1999 11 25 TWAA9915805 1 19991108 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 579 - 598 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND AN EIGHT INCH CRACK AT STA 579 TO 598, LONGERON 29L, AT THE CENTER OF THE LONGERON AT SP LICE JOINT. INSTALLED NEW FITTING PER SPM 6-70-1. 2 L 7 2 4F A6WE 1999112500238 19991125 00238 NM 1999 11 25 TWAA9915806 1 19991110 A 5754 SKIN BOEING 767 767205 1385121 NM LE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, FOUND AT LOWER O/B SURFACE OF NUMBER 8 SLAT, THE T/E WEDGE HAD DELAMINATION 6 INCHES FROM THE T/E. INSTALLED HOT BOND REPAIR PER SRM 51-70-10, A 3 INCH BY 5 INCH PATCH. 2 L 7 2 4F RT A1NM 1999112500239 19991125 00239 WP 1999 11 25 TWAA9915807 1 19991103 A 5754 SPAR DOUG DC9 DC931 3022065 WP LE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND A CRACK ON RT WING INSIDE THE I/B TOP HOLE FOR THE I/B FLAP HINGE CASTING UPPER SPAR ARE A AT 11 O'CLOCK POSITION. REAMED OUT HOLE AND INSTALLED BUSHING AND DOUBLER REPAIR PER J060271 AND ARA 16217. 2 L 7 2 4F A6WE 1999112500240 19991125 00240 WP 1999 11 25 TWAA9915808 1 19991024 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9405T 53141 DURING CHECK-C MAINT, FOUND AREA AROUND THE FORWARD CARGO DOOR HANDLE HAD SKIN BENT IN WITH A .375 INCH CRACK COMING OUT OF RADIUS. REMOVED CRACKED AREA AND STRAIGHTENED OUT DENT PER MD80 SRM 53-04 FIG 38. 2 L 7 2 4F RT A6WE 1999112500241 19991125 00241 NM 1999 11 25 HNAA9900160 1 19991121 A 3350 LIGHT DHAV DHC8 DHC8201 2809001 NM CABIN MALFUNCTIONED A HNAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 07 986HA 421 F/A'S EMERGENCY CALL AND ATT LIGHTS STAY ON ALL THE TIME. FLIGHT DECK EMERGENCY AND CALL LIGHTS STAY ON. SYSTEMS WORK BUT LIGHT STAYS ON. REF: LOG PAGE 37752. REMOVED AND REPLACED PA ELECTRONICS UNIT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999112500242 19991125 00242 NM 1999 11 25 HNAA9900161 1 19991119 A 5210 CABLE DHAV DHC8 DHC8102 2809003 NM PAX DOOR LOOSE A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 924HA 105 PAX DOOR WILL NOT OPEN. FOUND LOWER CABLE OFF PULLEY. REPOSITIONED CABLE ON PULLEY, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999112500243 19991125 00243 EU 1999 11 25 MALA976634 1 19991117 A 7930 4052T9P01 CHIP DETECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 106XJ 106 RIGHT CHIP DETECT LIGHT ON OVERHEAD PANEL ILLUMINATED WITH ASSOCIATED CWP ENGINE LIGHT, CONDITIONS AT THE TIME OF INCIDE NT 12,000 FT/-14DEGREES C/ TRQ 80 PERCENT. ALL OTHER ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND CHIP DETECTOR SHORTED INTERNALLY. REPLACED CHIP DETECTOR, GE MM CHAPTER 79. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999112500244 19991125 00244 EU 1999 11 25 MALA976635 1 19991118 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 430XJ 430 AIRCRAFT HAD A BAD ODOR IN COCKPIT AND CABIN. NO VISIBLE SMOKE IN EITHER, RECIRC FAN TURNED OFF, SMELL WAS REDUCED, BUT NOT COMPLETELY. AIRCRAFT RETURNED TO DTW. MAINTENANCE RAN AIRCRAFT AND VERFIED ODOR, SUSPECT COMP WASH FLUID. RAN AI RCRAFT WITH BLEEDS ON FOR 15 MINUTES AND SMELL WENT AWAY. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999112500245 19991125 00245 NM 1999 11 25 AWXA9900407 1 19991110 A 2131 7638102 CONTROLLER BOEING 737 737277 1384570 NM CABIN PRESSURE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 184AW 37254 8824 22651 A/C CABIN ALTITUTE CLIMBED ABOVE 10,000 FT WHEN CLIMBING THRU FL 27,000. PRESSURIZATION CONTROL WAS REGAINED AFTER SELE CTING MAN DC MODE. REPLACED CABIN PRESSURE CONTROLLER IAW 21-31-21 PG 401, TT 0099110. ALSO, OUTFLOW VALVE WAS REPLAC ED (SEE LP 7558125 & 7558124) TT 0101252. 2 L 7 2 4F RT A16WE 1999112500246 19991125 00246 NM 1999 11 25 AWXA9900408 1 19991110 A 5320 6547959 INTERCOSTAL BOEING 737 7373S3 1384711 NM BS 787 - 793 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 C-CHECK, AFT PIT STA 787-793, STR 25R INTERCOSTAL HAD CORROSION ON UPPER FLANGE AT NUT PLATE ATTACH AREAS. REMOVED CORR ODED INTERCOSTAL, FABRICATED, TREATED, AND PRIMED REPAIR PART AND INSTALLED PER SRM 53-60-15, 51-40-12 AND 51-10-1. 2 L 7 2 4F RT A16WE 1999112500247 19991125 00247 NM 1999 11 25 AWXA9900409 1 19991110 A 5330 42297A00635 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 C-CHECK, CRACK IN FUSLAGE SKIN AT LWR AFT CORNER OF R1 DOOR HAD CRACKS EXTENDING FROM 2 FASTENER HOLES. REMOVED FASTENE RS AND REAMED HOLES TO .25 IAW SRM 53-10-01, HFEC REVEALED INTERIOR CRACKS, EXTERIOR CRACKS ARE CONTAINED AT FASTENER HO LES. INSTALLED FLUSH WASHERS AND FABRICATED DOUBLERS FROM 2024 .063 R681615, FABRICATED SHIMS FROM 7075T .100R707582. T REATED, PRIMED AND INSTALLED WET PER SRM 53-10-1. 2 L 7 2 4F RT A16WE 1999112500248 19991125 00248 NM 1999 11 25 AWXA9900410 1 19991111 A 5753 032301CRES SKIN BOEING 737 7373S3 1384711 NM TE FLAP GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 C-CHECK, RIGHT O/B MID FLAP AT I/B TRACK IS GOUGED ON LWR L/E SURFACE. REMOVED DAMAGED AREA, FABRICATED REPLACEMENT DOU BLER FROM .032301 CRES 1/2 HARD MATERIAL, IAW SRM 57-53-01. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED DOUBLER IAW SRM 57-53-01. 2 L 7 2 4F RT A16WE 1999112500249 19991125 00249 NM 1999 11 25 AWXA9900411 1 19991111 A 5330 65C35768 SKIN BOEING 737 7373S3 1384711 NM BS 380 CREASED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 C-CHECK, TWO SMALL DENTS 5 FEET FWD OF FWD CARGO DOOR, FS 380 STR 24R. CREASE IN BOTTOM OF DENTS OUT OF LIMITS. REMOV ED DAMAGE, NDT REVEALED NO CRACKS. FABRICATED REPAIR PARTS FROM 2024T3 X.063 R699111 2024T3 X.050 R697963. INSTALLED C ONICAL WASHERS, ALODINED AND PRIMED IAW SRM 51-40-02, 51-20 -02 AND 53-00-01. 2 L 7 2 4F RT A16WE 1999112500250 19991125 00250 NM 1999 11 25 AWXA9900412 1 19991111 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373S3 1384711 NM BS 500B - 500D CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 C-CHECK, CORROSION ON SEAT TRACK AT RIGHT OUTBD FS 500B-500D OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02 , FABRICATED SEAT TRACK FROM BAC 1520-792/7178T6 PER SRM 53-30-52 R659935, TREATED AND PRIMED PER SRM 51-20-01 AND INST ALLED PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999112500251 19991125 00251 NM 1999 11 25 AWXA9900413 1 19991111 A 5312 6545409245 BULKHEAD BOEING 737 7373S3 1384711 NM BS 644 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 C-CHECK, CABIN STA 663.75 LBL 32, WHEEL WELL PRESSURE DECK HAD 1 .4375 CRACK. HFEC VERIFIED CRACK. REMOVED DAMAGED ARE A, FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED PARTS PER ER 03-5310-99288-EY1. FABRICATED REPAIR DOUBLER FROM 20 24T3 X .050 R700212, FILLER FROM 2024T3 X .050 R700212, ANGLE FROM 7075T6 X .063 R699452. 2 L 7 2 4F RT A16WE 1999112500252 19991125 00252 EU 1999 11 25 AWXA9900414 1 19991115 A 3260 69743532 BRACKET AIRBUS 320 A320231 3930325 EU LT MLG BROKEN A AWXA O OTHER N FALSE WARNING AP APPROACH 1 WP 28 644AW 317 EMERGENCY LANDING, ON SHORT FINAL GOT ECAM MSG INDICATING DOOR PROXIMITY. NOSE AND RT MLG INDICATED GREEN, LT MLG INDIC ATED RED. FOUND LT MLG DOWNLOCK TARGET AND BRACKET MISSING. INSTALLED TARGET AND BRACKET PER AAM 32-31-73 401. ADJUST ED PER AMM 32-31-73. 2 L 7 2 4F RT A28NM 1999112500253 19991125 00253 EU 1999 11 25 AWXA9900415 1 19991117 A 2120 VFT300A1 VALVE AIRBUS 320 A320232 3930326 EU FUSELAGE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 655AW 564 555 1075 ABORTED TAKEOFF, AT LOW GROUND SPEED HAD A VENT SKIN VALVE FAULT. REMOVED AND REPLACED SKIN AIR EXT VALVE PER 21-26-53. 2 L 7 2 4F RT A28NM 1999112500254 19991125 00254 EU 1999 11 25 AWXA9900416 1 19991117 A 3260 69743532 BRACKET AIRBUS 320 A320231 3930325 EU MLG WORN A AWXA O OTHER N FALSE WARNING LD LANDING 1 WP 28 624AW 55 EMERGENCY LANDING - LGCIU 1AND 2 FAULTED. RESET CIRCUIT BREAKERS, NO HELP. MANUALLY EXTENDED GEAR MLG FOR LANDING. R EMOVED AND REPLACED WORN TARGET SUPPORT PER AMM 32-21-27-991. 2 L 7 2 4F RT A28NM 1999112500255 19991125 00255 NM 1999 11 25 AWXA9900417 1 19991117 A 3397 BMS13131122 WIRE BOEING 737 7373G7 1384595 NM ROW 5 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 311AW 24712 NON-ROUTINE LINE, EMERGENCY LIGHTING ROW 5 EMERGENCY LIGHT INOP. REPAIRED WIRES AT SEAT TO TRACK CONNECTION, OPS CK NOR MAL. 2 L 7 2 4F RT A16WE 1999112500256 19991125 00256 NM 1999 11 25 AWXA9900418 1 19991111 A 3397 BMS13131122 WIRE BOEING 737 737277 1384570 NM SEAT 19 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 NON-ROUTINE LINE, EMERGENCY EXIT LIGHT INOP AT SEAT 19. SPLICED BROKEN WIRE, OPS CK NORMAL. 2 L 7 2 4F RT A16WE 1999112500257 19991125 00257 EU 1999 11 25 AWXA9900419 1 19991117 A 4920 38002784 APU AIRBUS 320 A320231 3930325 EU TAIL SECTION SATURATED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 28 637AW 19265 1055 099 CABIN HAD STRONG ODOR LIKE DIRTY SOCKS SMELL, ALL AREAS ESPECIALLY DURING DESCENT. APU WASH CARD Z6D49301 COMPLIED WITH , NO SMELLS NOTED. 2 L 7 2 4F RT A28NM 1999112500258 19991125 00258 NM 1999 11 25 AWXA9900420 1 19991120 A 2751 WARNING LIGHT BOEING 757 7572S7 1384962 NM TE FLAP ILLUMINATED A AWXA O OTHER J WARNING INDICATION AP APPROACH 1 WP 28 904AW 23566 EMERGENCY LANDING-- ON APPROACH WHEN SELECTING FLAPS, TRAILING EDGE ASYMMETRY MESSAGE CAME ON UPPER EICAS. PERFORMED CK PER FIM 27-51-00. BITE C/W NO FAULTS NOTED, OPS CK OF FLAPS WAS NORMAL. 2 L 7 2 4F RT A2NM 1999112500259 19991125 00259 WP 1999 11 25 CALA9901517 1 19991121 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DEFLATED A CALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 09 938AS 49365 THE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION DEPARTING DEN AND THE AIRCRAFT WOULD NOT PRESSURIZE UNTIL P ULLING THE RIGHT GROUND CONTROL RELAY. THE ABNORMAL CHECKLIST WAS COMPLETED AND THE NOSE GEAR LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT UNDER INFLATED. A COMP LETE NOSE STRUT SERVICING WITH FLUID AND NITROGEN WAS PERFORMED. THE GEAR WAS RETRACTED IAW MM 32-30-09 AND GROUND CHEC K WAS NORMAL. 2 L 7 2 4F A6WE 1999112500260 19991125 00260 NM 1999 11 25 CALA9901518 1 19991118 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND A 1 INCH CRACK AT LIGHTENING HOLE OF C-1 DOOR INTERNAL SKIN. REPAIRED IAW ECRA 5230-01500. 2 L 7 2 4F RT A16WE 1999112500261 19991125 00261 NM 1999 11 25 CALA9901519 1 19991118 A 5240 DOOR BOEING 737 737724 NM SERVICE DOOR OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24715 28786 THE R-2 EMERGENCY EXIT/GALLEY DOOR WOULD NOT OPEN PROPERLY PAST 90 DEGREES OF FUSELAGE. THE DOOR WAS RIGGED IAW MM 52-4 1-00 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999112500262 19991125 00262 NM 1999 11 25 CALA9901520 1 19991120 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14325 23455 INSPECTION FOUND LOWER SURFACE OF FLOORBEAM AT NUT PLATE FOR R-2 DOOR GIRT BAR LATCH, STA 986.5 CORRODED. A STRAP REPAI R WAS INSTALLED IAW ECRA 5360-01030 AND SRM 53-00-51, FIGURE 203. 2 L 7 2 4F RT A16WE 1999112500263 19991125 00263 WP 1999 11 25 CALA9901521 1 19991120 A 5320 SCUFF PLATE DOUG DC9 DC982 3022082 WP BS 1133 - 1191 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND AFT PIT DOOR SCUFF PLATE TORN AT ONE CORNER AND EDGES DAMAGED AT FS 1133-1192, LONGERON 27R. THE DAMAG ED AREA WAS TRIMMED OUT IAW SRM 51-10-4. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 2, 51-30-2, AND ECRA 5310 -03947. 2 L 7 2 4F A6WE 1999112500264 19991125 00264 NM 1999 11 25 CALA9901522 1 19991120 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 312, LBL 30. A REPAIR DOUBLER AND FLOOR SUPPORT WERE INSTAL LED IAW SRM 53-10-8, 51-30-1, AND 51-30-2. 2 L 7 3 4F A3WE 1999112500265 19991125 00265 NM 1999 11 25 CALA9901523 1 19991120 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 380 - 420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND SEAT TRACK CORRODED AT STA 380-420, RBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999112500266 19991125 00266 NM 1999 11 25 CALA9901524 1 19991120 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 848 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 848, BL 0 TO RBL 25. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999112500267 19991125 00267 NM 1999 11 25 CALA9901525 1 19991120 A 5210 PAN BOEING 727 727232 1384082 NM PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF UPPER AFT CORNER OF L-1 DOOR PAN. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999112500268 19991125 00268 NM 1999 11 25 CALA9901526 1 19991120 A 5320 WEB BOEING 727 727232 1384082 NM BS 400 - 420 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN WEB ANGLE AT STA 400-420, RBL 45. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4, 51-30-0, PAGE 3, 51-20-0, AND 51-10-2. 2 L 7 3 4F A3WE 1999112500269 19991125 00269 NM 1999 11 25 CALA9901527 1 19991120 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 620 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND AN 8 INCH CRACK IN INTERCOSTAL UNDER FLOOR SUPPORT FITTING AT FS 620. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2. 2 L 7 3 4F A3WE 1999112500270 19991125 00270 NM 1999 11 25 CALA9901528 1 19991120 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 420 - 440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND SEAT TRACK CORRODED AT STA 420-440, RBL 50. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999112500271 19991125 00271 WP 1999 11 25 CALA9901529 1 19991122 A 3350 AD4002P BATTERY MATHEWS DOUG DC9 DC982 3022082 WP ROW 22 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16806 49260 THE CEILING EMERGENCY LIGHTS AT ROW 23-32, EXIT SIGNS AT AFT SERVICE DOOR, LEFT AFT LAV WALL, AND THE CATWALK WOULD NOT TEST. THE BATTERY AT OVERHEAD BINS 25 AND 29 WAS REPLACED. REPLACED BLOWN FUSE AT AFT BATTERY CHARGER. REPAIRED WIRE AT AFT SERVICE DOOR SIGN. OPERATION OF ALL EMERGENCY LIGHTS CHECKED GOOD. 2 L 7 2 4F A6WE 1999112500272 19991125 00272 SO 1999 11 25 COMA9910174 1 19991119 A 3320 5108WW BULB BC10047005 EMB 120 EMB120RT SO ROW 9 FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 249CA 120230 WHILE PERFORMING A MAINTENANCE SERVICE CHECK, THE MECHANIC NOTED A CABIN LIGHT DIM AT SEAT 9A-UPPER ROW. AFTER GAINING ACCESS TO FIXTURE, MECH FOUND CEILING LINING WITH 2 BURN MARKS AT CLOSE PROXIMITY TO LAMP ENDS. ALSO, BULB FELT HOT AT ENDS. REMOVED AND REPLACED BRUCE LIGHT FIXTURE AND BULB IAW COMAIR EO 33-012. REPAIRED CEILING LINING IAW EMB FAX SST- 1145/97-1. 2 L 7 2 4T RT A31SO 1999112500273 19991125 00273 SO 1999 11 25 COMA9910175 1 19991118 A 5246 WARNING LIGHT EMB 120 EMB120RT SO FUEL DOOR ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 268CA 120262 SERVICE DOOR WARNING AFTER TAKEOFF. SECURED SIGNAL POINT FUEL SERVICE DOOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999112500274 19991125 00274 EA 1999 11 25 COMA9960701 1 19991118 A 2750 TE FLAP CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 709CA 7238 FLAPS WILL NOT RETRACT, FLAPS STUCK AT 26 DEGREES. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999112500275 19991125 00275 EA 1999 11 25 COMA9960702 1 19991121 A 3210 VIBRATION CNDAIR CL600 CL6002B19 EA MLG DETECTED A COMA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 710CA 7241 VIBRATION FELT DURING GEAR RETRACTION. CND A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999112500276 19991125 00276 EA 1999 11 25 COMA9960703 1 19991120 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 EA RT MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 918CA 7018 LANDING GEAR DISAGREE WARNING. RIGHT HAND MLG DID NOT INDICATE UPLOCK TIGHTENED LOOSE UPLOCK TARGET ON RIGHT HAND MLG. 2 L 7 2 4F RT A21EA 1999112500277 19991125 00277 EU 1999 11 25 QXEA9902348 1 19991116 A 3350 5515900004 EXIT SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 GEG - THE AISLE EMERGENCY EXIT SIGN IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN CIRCUIT BOARD, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999112500278 19991125 00278 NM 1999 11 25 SCNA99752 1 19991112 A 3350 900835A BATTERY PACK BOEING 727 727259 138408J NM BS 480 DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE EMERGENCY BATTERY PACK FOR THE EXIT LIGHT AT STA 480 WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW B727 MM 335071, OPERATIONALLY CHECKS GOOD IAW B727 MM 335001. 2 L 7 3 4F A3WE 1999112500279 19991125 00279 NM 1999 11 25 SCNA99753 1 19991112 A 3350 616033054 EXIT SIGN BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE LEFT FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN FAILS BRIGHTNESS INSPEC TION. REPLACED LEFT FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031. 2 L 7 3 4F A3WE 1999112500280 19991125 00280 NM 1999 11 25 SCNA99754 1 19991112 A 3350 616033054 EXIT SIGN BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE LEFT AFT OVERWING EXIT DOOR SELF LUMINESECNT PULL SIGN FAILS BRIGHTNESS INSPECTION . REMOVED AND REPLACED AFT OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031. 2 L 7 3 4F A3WE 1999112500281 19991125 00281 NM 1999 11 25 SCNA99755 1 19991112 A 3350 616033054 EXIT SIGN BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN FAILS BRIGHTNESS INSPE CTION. REMOVED AND REPLACED FORWARD OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031. 2 L 7 3 4F A3WE 1999112500282 19991125 00282 NM 1999 11 25 SCNA99756 1 19991112 A 3350 616033054 EXIT SIGN BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK THE RIGHT AFT OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN FAILS BRIGHTNESS INSPECTION . REPLACED THE RIGHT AFT OVERWING EXIT DOOR SELF LUMINESCENT PULL SIGN IAW B727 MM 335031. 2 L 7 3 4F A3WE 1999112500283 19991125 00283 NM 1999 11 25 SCNA99757 1 19991112 A 3350 EXIT SIGN BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK THE RIGHT AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN FAILS BRIGHTNESS INSPE CTION. REMOVED AND REPLACED THE AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN IAW B727 MM 335031. 2 L 7 3 4F A3WE 1999112500284 19991125 00284 NM 1999 11 25 SCNA99758 1 19991112 A 3350 EXIT SIGN BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE LEFT AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN FAILS BRIGHTNESS INSPE CTION. REMOVED AND REPLACED THE AFT OVERWING EXIT DOOR SELF LUMINESCENT EMERGENCY SIGN IAW B727 MM 335031. 2 L 7 3 4F A3WE 1999112500285 19991125 00285 NM 1999 11 25 SCNA99759 1 19991104 A 5311 65317731 FRAME BOEING 727 727259 138408J NM BS 1183 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE AFT ENTRY DOOR LOWER RIGHT SIDE AT THE FLOOR LEVEL EXHIBITS A LARGE AREA OF CORROS ION AT STA 1183. REMOVED CORROSION, REPAIRED DAMAGED FRAME AND FRAME SPLICE IAW SRM 51302. 2 L 7 3 4F A3WE 1999112500286 19991125 00286 NM 1999 11 25 SCNA99760 1 19991104 A 5320 BRACKET BOEING 727 727259 138408J NM BS 1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE RIGHT AFT LAVATORY FLOORBEAM AT STA 1130 WAS FOUND TO EXHIBIT A CORRODED BRACKET. REMOVED CORROSION IAW SRM 51106. MATERIAL CORRODED OUT OF LIMITS. FABRICATED A NEW ANGLE FROM 7075 T6. TREATED AND IN STALLED NEW BRACKET PER 51302 AND 51202. 2 L 7 3 4F A3WE 1999112500287 19991125 00287 NM 1999 11 25 SCNA99761 1 19991104 A 5315 FLOORBEAM BOEING 727 727259 138408J NM BS 1166 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE LEFT AFT LAVATORY AT FLOORBEAM STA 1166 HAD ELONGATED HOLE IN THE LAVATORY FLOOR S TRUCTURE. REMOVED DAMAGED AREA IAW SRM 51402. FABRICATED DOUBLER IAW SRM 51402 FROM 7075 T6 .063. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER IAW SRM 51102 AND MM 51202. 2 L 7 3 4F A3WE 1999112500288 19991125 00288 NM 1999 11 25 SCNA99762 1 19991105 A 5315 FLOORBEAM BOEING 727 727259 138408J NM BS 1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND AROUND THE NUT CLIP HOLE AT THE BOTTOM OF THE MAIN CABIN FLOOR T C AP AT STA 1130 BETWEEN LBL 15 AND RBL 15 IN THE AFT CARGO COMPARTMENT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLES AND FILLER FROM 7075 T6. TREATED, PRIMED AND INSTALLED PER SRM 51102 AND MM 51202. 2 L 7 3 4F A3WE 1999112500289 19991125 00289 NM 1999 11 25 VNAA9911016 1 19991120 A 3260 870004MODA SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG FAILED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 328JS 8506 3142 3030 DURING FLIGHT, WITH GEAR UP THE CREW RECEIVED THREE RED AND THREE GREEN INDICATIONS INTERMITTENTLY. MAINTENANCE INSPECT ED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-61-01. OPERATIONA L CHECKS AND A VERIFICATION FLIGHT WAS FLOWN AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999112500307 19991125 00307 EU 1999 11 25 99ZZZX4317 1 19991026 A 2131 22201D071700 PRESS CONTROLLER AMD FALC50 FALCON50MYST 2730106 EU COCKPIT FAILED A FVAA O OTHER O OTHER NR NOT REPORTED 1 NE 03 163WW 490 344 052 PRESSURIZATION CONTROLLER FAILED TO MAINTAIN CABIN PRESSURE. REPLACEMENT OF CONTROLLER WITH REPAIRED UNIT AND OPS CHECK ED SYSTEM PER WORK CARD 84.0 TO BE GOOD. 2 L 7 3 4F A46EU 1999112500317 19991125 00317 EU 1999 11 25 PLGA991019 1 19991019 A 3260 SWITCH SAAB SF340 SF340A 7850100 EU RT MLG LACK OF LUBE A PLGA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 NE 05 342BE 340A096 BOS - FLT 4662 - ON DESCENT, WHEN CREW SELECTED GEAR DOWN, RIGHT GEAR DOWN AND LOCKED LIGHT WOULD NOT COME ON. CREW PER FORMED CHECKLIST AND EXECUTED A MISSED APPROACH INTO BOS. GEAR WAS CYCLED ONCE TO OBTAIN ALL DOWN AND LOCKED LIGHTS, AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBRICATED THE RIGHT MAIN GEAR UP AND DOWN LOCK MICROSWITCHES. ALL REQUIRED GEAR SWINGS AND CHECKES WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999112500318 19991125 00318 EU 1999 11 25 PLGA991016 1 19991016 A 2910 MS24142D1 RELAY SAAB SF340 SF340A 7850100 EU HYD SYSTEM FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NE 05 346BE 340A150 BOS - FLT 4704 - DURING INBOUND FLIGHT, CREW HAD TO PUMP THE GEAR DOWN DUE TO THE HYDRAULIC PUMP WOULD NOT COME ON LINE. CREW PERFORMED EMERGENCY EXTENSION OF THE GEAR, UNTIL GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED THE POWER RELAY FOR THE HYDRAULIC PUMP. REQUIRED OPERATIONAL CHECKS WERE PERFORMED. THE GEAR WAS ME L'D DOWN FOR A REPOSITION FLIGHT TO ALBANY FOR REPLACEMENT OF THE EXPLOSIVE BOLTS AND GEAR SWING. MAINTENANCE REPLACED THE EXPLOSIVE BOLTS AND PERFORMED ALL REQUIRED CHECKS. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999112500319 19991125 00319 NM 1999 11 25 P2EA99307 1 19991024 A 2150 20405011 ACM BOEING 737 737205 NM RIGHT FAILED A P2EA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 412CE 165 1623709 20412 MCI - FLT 584 - AFTER SHUT DOWN OF NR 1 ENGINE A BURNING ODOR WAS NOTICE FOLLOWED, A FEW SECONDS LATER, BY SMOKE IN THE COCKPIT AND FORWARD CABIN. REMOVED AND REPLACED RIGHT PACK AIR CYCLE MACHING PER MM 21-51-11. OPERATION NORMAL. (M) 2 L 7 2 4F A16WE 1999112500320 19991125 00320 NM 1999 11 25 P2EA99305 1 19991012 A 5753 FLAP BOEING 737 737230 NM LT TE AFT FLAP BIRDSTRIKE A P2EA A UNSCHED LANDING C F.O.D. CL CLIMB 1 CE 05 123NJ 22121 MCI - FLT 588 - EMERGENCY DECLARED AS PRECAUTIONARY. LANDING UNEVENTFUL. MADE PRECAUTIONARY EMERGENCY LANDING AT MCI. SUSPECTED A BLOWN MAIN OR NOSE TIRE. INSPECTED ALL 4 MAIN TIRES FOR DAMAGE, NO DAMAGE FOUND. TIRE PRESSUERS ALL CHECK ED NORMAL. INSPECTED NOSE TIRES, NO DAMAGE. FOUND TIRE PRESSURES NORMAL. FOUND BIRD STRIKE AT LEFT INBOARD AFT FLAP. ACCOMPLISHED BIRD STRIKE INSPECTION PER MM 5-51-201, NO DAMAGE TO FLAP FOUND. ACCOMPLISHED ENGINE RUN PER MM 71-09, AL L PARAMETERS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 1999112500321 19991125 00321 NM 1999 11 25 P2EA99306 1 19991013 A 7910 529452 OIL LINE BOEING 737 737247 138448D NM NR 1 ENGINE CRACKED A P2EA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 05 912MP 29452 19607 FLT 736 - CVG - NR 1 ENGINE OIL QTY WENT TO ZERO AND PRESSURE FLUCTUATING PLUS/MINUS PSI. NR 1 ENGINE SECURED (SHUT DOW N) IN FLIGHT. TEMPS WITHIN LIMITS, 13 MINUTES OF WINDMILLING, POSITIVE OIL PRESSURE THROUGHOUT LANDING. REPLACED CRACK ED OIL PRESSURE LINE AT FUEL/OIL COOLER PER MM 79-21-0. REMOVED OIL FILTER AND INSPECTED FOR METAL DUE TO INFLIGHT SHUT DOWN PER PWA MM 72-00, NONE NOTED. REPLACED OIL FILTER. REPLACED NR 1 ENGINE GEARBOX BECAUSE HELICOIL STRIPPED OUT OF GEAR BOX WHILE INSTALLING BRACKET ON NEW OIL LINE. (M) 2 L 7 2 4F A16WE 1999112500322 19991125 00322 WP 1999 11 25 HALA9900202 1 19991019 A 2170 COALESCER BAGS DOUG DC10 DC1010 3022110 WP CABIN DIRTY A HALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 119AA 46519 FLT 2 - HNL - STRONG ODOR IN CABIN SERVICE AREA MOSTLY BURNING OIL SMELL, BUT ALSO LIGHT PLASTIC SMELL. REMOVED AND REP LACED ALL 3 WATER SEPARATOR SOCKS. PURGED AIR CONDITION SYSTEM PER TAFI 21-50-00 PAGE 120. OPS CHECK OK. (M) 2 L 7 3 4F A22WE 1999112500323 19991125 00323 NM 1999 11 25 TWRA9966 1 19991021 A 3610 8988061 REG VALVE BOEING 747 7472F6B 1384807 NM NR 4 ENGINE INOPERATIVE A TWRA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 EA 15 623FF 1230 22382 DURING TAKEOFF AT 142 KNOTS AND PRIOR TO V1 NR 4 ENGNE FIRE WARNING LIGHT AND BELL CAME ON CAPTAIN ABORTED TAKEOFF AND B OTH BELL AND LIGHT WENT OUT AS CAPTAIN INDICATED THE ABORT. REMOVED AND REPLACED NR 4 OVER PRESSURE VALVE AND NR 4 ENGI NE BLEED REGULATOR VALVE. PERFORMED R/U PER MM 71-00-00, TEST 4 ALL, LEAKS CHECKED OK. (M) 2 L 7 4 4F A20WE 1999112500324 19991125 00324 NM 1999 11 25 99ZZZM774 1 19991021 A 3610 A111857 RELIEF VLV BOEING 747 7472F6B 1384807 NM NR 4 ENGINE INOPERATIVE A TWRA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 EA 15 623FF 298 22382 DURING TAKEOFF AT 142 KNOTS AND PRIOR TO V1 NR 4 ENGNE FIRE WARNING LIGHT AND BELL CAME ON CAPTAIN ABORTED TAKEOFF AND B OTH BELL AND LIGHT WENT OUT AS CAPTAIN INDICATED THE ABORT. REMOVED AND REPLACED NR 4 OVER PRESSURE VALVE AND NR 4 ENGI NE BLEED REGULATOR VALVE. PERFORMED R/U PER MM 71-00-00, TEST 4 ALL, LEAKS CHECKED OK. (M) 2 L 7 4 4F A20WE 1999112500325 19991125 00325 NM 1999 11 25 UIEA9991 1 19991019 A 5711 SPAR WEB BOEING 747 7472D3B 1384805 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 74272 21251 RIGHT WING MID SPAR UPPER CHORD FOUND WEB CRACKS. INDICATIONS VERIFIED USING HFEC INSPECTION, BETWEEN MSS 563.24 AND 59 2.45. AT MSS 575 THE WEB AT THE TWO CRACKED FASTENER HOLES WERE TRIMMED OUT AND A PERMANENT REPAIR WAS ACCOMPLISHED USI NG FILLERS, A DOUBLER AND A STIFFENER REF 8110-3. (M) 2 L 7 4 4F RT A20WE 1999112500326 19991125 00326 NM 1999 11 25 UIEA9994 1 19991019 A 5711 SPAR WEB BOEING 747 7472D3B 1384805 NM WS 1241 CORROSION A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 74272 21251 WING CENTER SECTION, BS 1241 REAR SPAR WEB CORROSION. CORROSION REMOVED FROM WEB AND REWORKED, THIS IS AN APPROVED ALTE RNATE METHOD OF COMPLIANCE REF 8110-3. (M) 2 L 7 4 4F RT A20WE 1999112500327 19991125 00327 NM 1999 11 25 UEIA9993 1 19991019 A 5730 SKIN BOEING 747 7472D3B 1384805 NM WS 1241 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 74272 21251 LEFT WING STATION 1241 SPLICE STRAP AND SKIN FOUND CRACKED IN FORWARD HOLE, VERIFIED WITH HFEC INSPECTION. FAIL/SAFE ST RAP WAS REMOVED AND REPLACED AND CRACKED SKIN WAS TRIMMED OUT AND REPAIRED. THIS IS AN APPROVED ALTERNATE METHOD OF COM LIANCE REF 8110-3. (M) 2 L 7 4 4F RT A20WE 1999112500328 19991125 00328 NM 1999 11 25 UIEA9992 1 19991019 A 5720 BACB30US14K BOLT BOEING 747 7472D3B 1384805 NM WS 1241 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 74272 21251 LEFT WING REAR SPAR STATION 1241, LOWER SPLICE PLATE AND KICK FITTING INBOARD BOLT AND BOLT HOLE HAS CRACK INDICATIONS, VERIFIED WITH HFEC INSPECTION. OVERSIZED KICK FITTING AND REAR SPAR LOWER CHORD BOLT HOLE TO .975 INCH. VERIFIED HOLE IS CRACK FREE WITH HIGH FREQ EDDY CURRENT INSPECTION. REPLACED BOLT. (M) 2 L 7 4 4F RT A20WE 1999112500329 19991125 00329 NM 1999 11 25 USAA991045 1 19991007 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 45191 22796 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN SKIN AT STATION 727A STRINGER 19R. INSTALLED DOUBLER P ER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999112500330 19991125 00330 NM 1999 11 25 USAA109906 1 19991024 A 2611 824PY SMOKE DETECTOR BOEING 727 727225 1384077 NM AFT LAV FAILED A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 918TS 20445 FLT 6141 - BOS-LGA - FOUND ON L/S, AFT LAV SMOKE DETECTOR TEST WILL NOT SHUT OFF. REPLACED AFT LAV SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 1999112500331 19991125 00331 NM 1999 11 25 TSAA9933460 1 19991019 A 3350 8731002511 LIGHT BOEING 737 7372S2C 138448G NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED LEFT FORWARD EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999112500332 19991125 00332 NM 1999 11 25 TSAA9933461 1 19991017 A 3350 8731002511 LIGHT ASSY BOEING 737 7372Q9 138448M NM CABIN BROKEN A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED AFT ENTRY EXIT IDENTIFIER LIGHT ASSY DUE TO BEING BROKEN AND CRACKED. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1999112500333 19991125 00333 NM 1999 11 25 TSAA9933462 1 19991019 A 3350 6013211 BATTERY PACK BOEING 737 7372Q9 138448M NM PAX CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD ENTRY AND SERVICE DOOR SLIDE LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1999112500334 19991125 00334 NM 1999 11 25 TSAA9933463 1 19991018 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED EMERGENCY FLOOR LIGHT BATTERY PACKS IN POSITIONS 1-6 DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A16WE 1999112500335 19991125 00335 NM 1999 11 25 TSAA9933464 1 19991015 A 3350 8731002511 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999112500336 19991125 00336 NM 1999 11 25 TSAA9933465 1 19991015 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 2 FLOOR BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999112500337 19991125 00337 NM 1999 11 25 TSAA9953459 1 19991018 A 5330 65737461 SKIN BOEING 737 7372Q9 138448M NM BS 744 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 POSSIBLE CRACK NEAR BS 727B-747 AT STRINGER 17R. VERIFIED FUSELAGE SKIN CRACK AT BS 744 STRINGER 17R USING HFEC. CUTOU T CRACK IAW SRM 53-30-03 AND VERIFIED WITH HFEC CRACK WAS COMPLETELY REMOVED. REPAIRED IAW SRM 53-30-03. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999112500338 19991125 00338 1999 11 25 ARWA991003 4 19991028 A 3417 2592800901 ADC DOUG DC8 DC862 3021970 WP E/E COMP FAILED A ARWA A J UNSCHED LANDING DUMP FUEL G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 19 8969U 0990146 46070 MIA - FLT 431 - MODE C INOPERATIVE BOTH TRANSPONDERS. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. PERFORMED OPS CHECK , TESTED AND INSPECTED BOTH ATC TRANSPONDERS. FOUND TO COMPLY WITH FAR 43 APPENDIX 'E' PAR SMALL "C" OPS NORMAL. PERFO RMED PITOT STATIC LEAK CHECK IAW ARROW AIR JC 34-01. NO LEAKS NOTED. 37.0 FUEL DUMPED AIR TURNBACK. (M) 2 L 7 4 4F 4A25 1999112500339 19991125 00339 NE 1999 11 25 EIA990286 2 19991015 A 7200 ENGINE BOEING 747 747131 1384881 NM PWA JT9 JT9D7AH 52054 NE NR 1 BIRD STRIKE A EIAA O OTHER C F.O.D. CL CLIMB 1 NM 09 472EV 20320 HNL - NR 1 ENGINE 'N1' INDICATOR HAD INTERMITTENT FLUCT PLUS/MINUS 5 PERCENT ON CLIMB-OUT. FLUCT AT CRUISE PEGGED OVERS PEED INDICE AT 112 PERCENT. RESET INDICE AND INDICATOR OPERATED NORMALLY FOR REMAINDER OF FLT. ON POST FLT, FOUND 'C1' DISC AND '1'STATOR' GUIDE VANES DAMAGED FROM APPARENT BIRD STRIKE. PERFORMED BIRD STRIKE INSPECTION PER MM 72-00-00. F OUND 4 BLADES DAMAGED AND 7 EXIT VANES DAMAGED. REMOVED AND REPLACED 8 FAN BLADES PER WORK CARD F7208. BOROSCOPE ACCOM PLISHED PER MM 72-00-00. REPLACED BLADES NR 45, 22, 23, 1, 24, 2, AND 25. RAN ENGINE AT PART POWR PER MM 71-00-00. AL L PARAMETERS CHECKED NORMAL. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999112500340 19991125 00340 WP 1999 11 25 VTZA990194 2 19990624 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT SHUTDOWN A VTZA A UNSCHED LANDING X Y J ENGINE FLAMEOUT ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 27 488UE 907 FLT 7319 - SYR TO IAD - DURING CLIMB, A/C MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE SHUTDOWN IN FLT. A/C RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE COMPLETE FUEL SYSTEM FOR CONTAMINATION BY INSPECTING FUEL LIN ES AND FILTERS. PERFORMED OPS CHECK OF FUEL SHUT OFF VALVES AND PERFORMED GRUOND RUNS TO CHECK POWER SETTING FROM GROUN D IDLE TO MAX POWER. MX ACCEPATANCE FLT WAS PERFORMED WITH NO FAULTS FOUND. AIRCRAF WAS REPOSITIONED TO IAD. AT IAD M X DE-FUELED AIRCRAFT AND OPENED WING FUEL PANELS TO INSPECTED FOR FOREIGN OBJECTS IN FUEL TANKS. NO DEFECTS NOTED. MAI NTENANCE PERFORMED MORE GROUND RUNS ON THE FUEL SYSTEM PARAMETERS AND NO FAULTS FOUND. OPS CHECK OK. AIRCRAFT WAS RELE 2 L 7 2 4T 3 T RT A56EU E3WE 1999112500341 19991125 00341 WP 1999 11 25 99ZZZM775 2 19990709 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT MALFUNCTIONED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 482UE 897 FLT 7546 - IAD-EWR - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE NOT MAKING TORQUE. AIRCRAFT RETURNE D TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED LEFT TSC AND EGT COMPENSATOR. OPS CHECK OK. AI RCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999112500342 19991125 00342 NE 1999 11 25 MZZA99152 2 19990806 A 7230 FAN BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .5 INCH LONG CRACK WAS FOUND ON NR 1 ENGINE FIRST STAGE COMPR ESSOR BLADE LEADING EDGE SURFACE. THE STAGE 1 COMPRESSOR DISC P/N 817401 WAS REMOVED AND REPLACED WITH A NEW ONE PER JT 8D MM SECT 72-30 PARA 1.B. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999112500343 19991125 00343 EU 1999 11 25 UF6A990916 1 19990922 A 5320 281D11186 INTERCOSTAL BAG ATP ATP EU BS 289 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - INTERCOSTAL BY REAR PASSENGER DOOR IS CORRODED. MAINTENANCE REMOVED CORROSION AND WAS FOUND TO BE NEGLIGIBLE. AL L WORK WAS DONE IAW BAE ATP SRM 51-10-01. (M) 2 L 7 2 4T RT A27NM 1999112500344 19991125 00344 EU 1999 11 25 UF6A991018 1 19991021 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 855AW 2029 SBN - AFT EMERGENCY LIGHT BULB IS INOPERATIVE ON THE RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1999112500345 19991125 00345 NE 1999 11 25 UF6A991016 2 19991012 A 7321 324484112141819 FUEL CONTROL BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE FAILED A UF6A A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 31 859AW 10178 2036 124242 SBN - FLT 5751 - DURING CRUISE, THE NR 1 ENGINE TORQUE BEGAN TO SURGE PLUS/MINUS 5 PERCENT. TORQUE PEAKED AT 120 PERCEN T FOR 1 SECOND THEN ROLLED BACK TO 0 PERCENT. ENGINE WAS SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE NR 1 MFC. POW ER ASSURANCE RUNS WERE PERFORMED AND ALL PARAMETERS WERE FOUND TO BE WITHIN LIMITS. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999112500346 19991125 00346 EU 1999 11 25 UF6A991017 1 19991017 A 5330 SKIN BAG ATP ATP EU BS 289 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE BAGGAGE DOOR SURROUND HAS A CUT AT THE AFT LOWER CORNER. MAINTENANCE REPAIRED DAMAGED AREA. ALL WORK WAS DON E ENGINEERING REPORT NR 99-201. (M) 2 L 7 2 4T RT A27NM 1999112500347 19991125 00347 EU 1999 11 25 UF6A991015 1 19991011 A 2120 AIR DIST BAG ATP ATP EU GALLEY ODOR A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 857AW 2034 AZO - FLT 5704 - ELECTRICAL BURNING SMELL IN AFT GALLEY. MAINTENANCE RAN ENGINES, INSPECTED LIGHTING, AND DOORS. NO DE FECTS OR UNUSUAL SMELL NOTED. (M) 2 L 7 2 4T RT A27NM 1999112500348 19991125 00348 EU 1999 11 25 UF6A991014 1 19991011 A 5330 SKIN BAG ATP ATP EU BS 360 DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 ORD - DENT ON FUSELAGE BELOW LAVATORY SERVICING DOOR. MAINTENANCE FOUND DENT TO BE SHALLOW AND REQUIRES REINSPECTION EV ERY TWO YEARS. (M) 2 L 7 2 4T RT A27NM 1999112500349 19991125 00349 NE 1999 11 25 UF6A991010 2 19991003 A 7261 3034505 FILTER BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE DIRTY A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 31 851AW 2020 124015 ORD - FLT 5715 - ON TAKEOFF ROLL, THE NR 1 ENGINE OIL FILTER CWP ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE LP A ND HP FILTERS. POWER ASSURANCE RUNS WERE PERFORMED AND ALL PARAMETERS WERE FOUND TO BE WITHIN LIMITS. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999112500350 19991125 00350 EU 1999 11 25 UF6A990923 1 19990923 A 5530 JD553J0410000 FAIRING BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE TOP ANGLE WHICH ATTACHES THE VERTICAL STABILIZER TO THE FUSELAGE ON THE LEFT SIDE IS CRACKED AT THE FORWARD SE CTION. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-184. (M) 2 L 7 2 4T RT A27NM 1999112500351 19991125 00351 EU 1999 11 25 UF6A990922 1 19990923 A 5530 JD553J0410001 FAIRING BAG ATP ATP EU VERT STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE ANGLE WHICH ATTACHES THE VERTICAL STABILIZER TO THE FUSELAGE ON THE LEFT SIDE IS CRACKED AT THE AFT SECTION. M AINTENANCE REPAIRED CRACKED. ALL WORK WAS DONE IAW ENGINEERING ORDER 99-184. (M) 2 L 7 2 4T RT A27NM 1999112500352 19991125 00352 EU 1999 11 25 SIMA992833 1 19991010 A 3350 LP1670 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 423MQ 030 ORD - FLT 9752 - TWO EMERGENCY FLOOR PROXIMITY EXIT LIGHTS DO NOT ILLUMINATE AT SEAT ROW 5 AND 10. REMOVED AND REPLACED BULBS FOR FLOOR PROXIMITY LIGHTS. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999112500353 19991125 00353 EU 1999 11 25 SIMA992873 1 19991014 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 293AT 6343 293 SAW - DURING PS-2 INSPECTION FOUND SEVERAL CABIN EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LI GHT BATTERY PACK AT LOCATION 3WL IAW JIC 335121-RAI-10000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500354 19991125 00354 EU 1999 11 25 SIMA992832 1 19991010 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU ROW 5 DISCHARGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 47AE 047 ORD - FLT 4057 - LOWER EMERGENCY EXIT SIGNS AT BOTH FORWARD EXIT LOCATIONS AND THE FLOOR PROXIMITY LIGHT AT ROW 5 DOES N OT ILLUMINATE. REPLACED NR 2 BATTERY PACK AND THE CONNECTOR AT 35WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500355 19991125 00355 EU 1999 11 25 99ZZZM776 1 19991010 A 3350 E0052R10B65NE CONNECTOR AEROSP ATR42 ATR42300 8680920 EU ROW 5 FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 47AE 047 ORD - FLT 4057 - LOWER EMERGENCY EXIT SIGNS AT BOTH FORWARD EXIT LOCATIONS AND THE FLOOR PROXIMITY LIGHT AT ROW 5 DOES N OT ILLUMINATE. REPLACED NR 2 BATTERY PACK AND THE CONNECTOR AT 35WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500356 19991125 00356 EU 1999 11 25 SIMA992821 1 19991009 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 142DD 4204 040 SAW - DURING PS-2 INSPECTION, FOUND SOME EMERGENCY FLOOR PROXIMITY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION 30 WL IAW JIC 33500-RAI-10000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500357 19991125 00357 EU 1999 11 25 SIMA992781 1 19991005 A 3350 1013073 SOCKET AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURNIG PS-2 INSPECTION, FOUND ONE EMERGENCY FLOOR LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY FL OOR LIGHT SOCKET. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999112500358 19991125 00358 EU 1999 11 25 SIMA992881 1 19991015 A 5400 S5421020000000 MOUNT AEROSP ATR42 ATR42300 8680920 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING PS-2 INSPECTION, FOUND THE LEFT ENGINE BLEED AIR SHUTOFF VALVE HAD CHAFED THROUGH THE AFT OUTBOARD ZEE MOUN T. REMOVED AND REPLACED THE ZEE MOUNT IAW JIC 542161-RAI-1000-007. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500359 19991125 00359 EU 1999 11 25 SIMA992782 1 19991005 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 250AE 340B250 DFW - FLT 3252 - FLOOR PROXIMITY LIGHT AT ROW 9 DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 1999112500360 19991125 00360 EU 1999 11 25 SIMA992843 1 19991011 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 906AE 340B348 DFW - FLT 3304 - FLOOR PROXIMITY LIGHT AT 9B DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4T RT A52EU 1999112500361 19991125 00361 EU 1999 11 25 SIMA992872 1 19991014 A 5313 S5337120221002 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING PS-2 INSPECTION, FOUND A .375 INCH HOLE IN THE FUSELAGE BETWEEN FRAMES 22 AND 23 AT STRINGER 7. REPAIRED S TRINGER 7 IAW SRM 53-00-00 FIGURE 426 AND REPAIRED THE FUSELAGE SKIN IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500362 19991125 00362 EU 1999 11 25 99ZZZM777 1 19991014 A 5330 S5337120320405 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 135 SAW - DURING PS-2 INSPECTION, FOUND A .375 INCH HOLE IN THE FUSELAGE BETWEEN FRAMES 22 AND 23 AT STRINGER 7. REPAIRED S TRINGER 7 IAW SRM 53-00-00 FIGURE 426 AND REPAIRED THE FUSELAGE SKIN IAW SRM 53-00-00 FIGURE 405. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500363 19991125 00363 SO 1999 11 25 SIMA992811 1 19991008 A 3350 3025101 LIGHT EMB 145 EMB145LR SO RT EMER EXIT BROKEN A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 628AE 145124 ORD - FLT 4134 - RIGHT OVERWING EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. (M) 2 L 7 2 4T RT T00011AT 1999112500364 19991125 00364 EU 1999 11 25 SIMA992842 1 19991011 A 2611 FR3123 SMOKE DETECTOR AEROSP ATR72 ATR72212 EU LAVATORY FAILED A SIMA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 21 533AT 588 533 AFT SMOKE DETECTOR WARNING ILLUMINATED. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED LAVATORY SMOKE DETECTO R. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500365 19991125 00365 NM 1999 11 25 TSAA9933450 1 19991005 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999112500366 19991125 00366 NM 1999 11 25 TSAA9933454 1 19991007 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999112500367 19991125 00367 NM 1999 11 25 TSAA9933451 1 19991010 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999112500368 19991125 00368 NM 1999 11 25 TSAA9933452 1 19991008 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999112500369 19991125 00369 NM 1999 11 25 TSAA9953453 1 19991007 A 5753 6570947188 SKIN BOEING 737 7372X6C 1384552 NM RT TE FOREFLAP DAMAGE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 FOREFLAP ON RIGHT WING ABOVE BEARING TRACK DAMAGED. REPAIRED PYLON SKIN PER ECO 3025. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999112500370 19991125 00370 NM 1999 11 25 TSAA9951459 1 19991011 A 5330 6554837503 SKIN BOEING 737 737282C 13844AU NM FUSELAGE TORN A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 826AL 23051 TEAR IN AFT FUSELAGE SKIN FORWARD OF APU DOOR ON LEFT SIDE IN NON-PRESSURIZED AREA. REPAIRED IAW ECO 3029. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999112500371 19991125 00371 WP 1999 11 25 ARWA991002 1 19991024 A 3231 SWITCH DOUG DC8 DC862 3021970 WP MLG DOOR FAILED A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 810BN 45905 MIA - FLT 751 - AIR TURNBACK, ON GER RETRACT DOOR NOT LATCHED. LIGHT REMAINS ILLUMINATED. PERFORMED ABNORMAL CHECKLIST 4 TIMES. LIGHT REMAINS ON. TROUBLESHOT, FOUND LEFT MAIN GEAR DOOR SWITCH FAULTY. REMOVED AND REPLACED SWITCH. OPS C HECK NORMAL IAW MM 32-60-0. (M) 2 L 7 4 4F 4A25 1999112500372 19991125 00372 NM 1999 11 25 EISA99187 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND NR 5 SEAT TRACK GOUGED FROM FS 720D TO 720E. DAMAGE OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 222136-1-1 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-1 0-2 AND MM 51-20-2. INSTALLED NEW TRACK FROM FS 720D TO 720E PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500373 19991125 00373 NM 1999 11 25 EISA99186 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 640 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARAD FOUND NR 4 SEAT TRACK CORRODED AT FS 640. MATERIAL OUT OF LIMIT S. FABRICATED NEW SECTION OF TRACK FROM BAC 222136-1-1 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2 A ND MM 51-20-2. INSTALLED NEW TRACK FROM FS 620 TO 660 PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500374 19991125 00374 NM 1999 11 25 EISA99185 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1110 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 1 SEAT TRACK CORRODED AT FS 1110. MATERIAL OUT OF LIMI TS. FABRICATED NEW SECTION OF TRACK FROM BAC 1520 -792 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2 A ND MM 51-20-2. INSTALLED NEW TRACK FROM FS 1070 TO 1130 PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500375 19991125 00375 NM 1999 11 25 EISA99184 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1070 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 1070. MATERIAL OUT OF LIMITS . FABRICATED NEW SECTION OF TRACK FROM BAC 1520-792 EXTRUSION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW TRACK FROM FS 1060 TO 1130 PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500376 19991125 00376 NM 1999 11 25 EISA99183 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 870 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 870. REMOVED CORROSION, MA TERIAL OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 1520-792 EXTRUSION. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW TRACK FROM FS 870 TO 950 PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500377 19991125 00377 NM 1999 11 25 EISA99182 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 760-850 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK, LBL 24, CORRODED FROM FS 760 TO 850. MAT ERIAL LOSS OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK FROM BAC 1520-792 EXTRUSION. TREATED AND PRIMED PER SRM 51-1 0-2 AND MM 51-20-2. INSTALLED NEW TRACK FROM FS 760-850 PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500378 19991125 00378 NM 1999 11 25 EISA99181 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND NR 2 SEAT TRACK CORRODED AT FS 720C. CORROSION OUT OF LIMIT S. FABRICATED NEW SECTION OF TRACK PER SRM 53-10-05. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW TRACK FROM FS 460 TO 690 PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500379 19991125 00379 NM 1999 11 25 EISA99180 1 19990914 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 460-680 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND NR 1 SEAT TRACK CORRODED FROM FS 460 TO 690 LBL 42. CORRO SION OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK PER SRM 53-10-05. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20- 2. INSTALLED NEW TRACK FROM FS 460 TO 690 PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500380 19991125 00380 NM 1999 11 25 EISA99179 1 19991007 A 5730 SKIN BOEING 727 727223 1384074 NM WS 491-505 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON RIGHT WING LOWER SURFACE OF AT WS 491.5 TO 50 5 BETWEEN STRINGER 5 AND 6. REMOVED CORROSION PER SRM 51-10-6. FABRICATED AND INSTALLED DOUBLER PER FLIGHT VEHICLES CO NSULTING INC EO NR 57-99455 AND SRM 51-30-4. (M) 2 L 7 3 4F A3WE 1999112500381 19991125 00381 NM 1999 11 25 EISA99178 1 19991007 A 5730 SKIN BOEING 727 727223 1384074 NM WS 460 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON LOWER SURFACE OF RIGHT WING AT WS 460 BETWEEN STRINGER 8 AND 9. REMOVED CORROSION PER SRM 51-10-6. MATERIAL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DO UBLER PER FLIGHT VEHICLES CONSULTING INC EO NR 57-99455 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999112500382 19991125 00382 NM 1999 11 25 EISA99145 1 19990602 A 5270 69189101 SWITCH BOEING 727 72731 1384010 NM CARGO DOOR OUT OF ADJUST A EISA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 240NE 18906 LIGHT ILLUMINATED FOR LOWER FORWARD PIT DOOR. ADJUSTED DOOR SWITCH. (M) 2 L 7 3 4F A3WE 1999112500383 19991125 00383 NE 1999 11 25 AALA991251 2 19990821 A 7230 840001 BALDE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE BROKEN A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 721AA 20729 665339 ORD - FLT 1590 - AFTER TAKEOFF ORD/MCO, NR 2 ENGINE EPR ROLLED BACK AND VIBRATION NOTED. ENGINE WAS SHUT DOWN AND AIRCR AFT LANDED AT ORD WITHOUT INCIDENT. REPLACED NR 2 ENGINE. PERFORMED ENGINE RUN-UP. SYSTEM GROUND CHECKED, NORMAL OPER ATION. A 1ST STAGE HPT BLADE FAILED AT THE AIRFOIL. THE FRACTURE IS THE RESULT OF STRESS RUPTURE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1999112500384 19991125 00384 NE 1999 11 25 99ZZZM778 2 19990903 A 7250 304418301 TURBINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A JJBA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 01 841CA 4932 UE40 114078 EN ROUTE BETWEEN ROC AND HPN LEFT ENGINE SUFFERED LOSS OF TORQUE FOLLOWED BY HIGH INTERNAL TURBINE TEMPERATURE INDICATIO NS, ENGINE WAS THEN SHUT DOWN IN FLIGHT, AIRCRAFT DIVERTED TO BGM FOR EMERGENCY LANDING. LEFT ENGINE WAS REPLACED IN BG M IAW PRATT AND WHITNEY CANADA AND RAYTHEON MAINTENANCE MANUALS. OPERATIONAL LEAK CHECK AND GROUND PERFORMANCE RUN SATI SFACTORY IAW CHAMPLAIN ENTERPRISES, INC APPROVED WORK CARDS. BLADE FAILURE ON NR 1 POWER TURBINE DISK IS SUSPECTED IN F AILURE OF ENGINE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999112500385 19991125 00385 NE 1999 11 25 F3LA99129 2 19991013 A 7510 577957 HEAT DUCT BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CRACKED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 214AU 20214 20214 MLI - DURING CLIMB-OUT FROM MDW, FLIGHT CREW REPORTED THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT WAS DIVERTED TO MOLINE, IL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CRACKED FUEL HEAT DUCT AND CHECKED OK. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999112500386 19991125 00386 NE 1999 11 25 AALA991329 2 19990904 A 7310 1777M18G01 MANIFOLD BOEING 767 767223 1385123 NM GE CF680 CF680A2 NE RT ENGINE DEFECTIVE A AALA E ENGINE SHUTDOWN K FLUID LOSS TX TAXI/GRND HDL 1 SW 07 324AA 22325 GIG - FLT 972 - ON INITIAL ENGINE START UP ON RAMP DURING PUSH OUT, FUEL LEAK NOTED FROM RIGHT ENGINE. ENGINE WAS SHUTD OWN WITHOUT FURTHER INCIDENT. FOUND RIGHT ENGINE UPPER FUEL NOZZLE MANIFOLD LEAKING. REPLACED RIGHT ENGINE UPPER FUEL NOZZLE MANIFOLD AND SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 1999112500387 19991125 00387 NE 1999 11 25 AALA991295 2 19990830 A 7230 840001 BLADE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 725AA 20732 666359 IAH - FLT 1428 - AFTER TAKEOFF IAH/ORD, NR 2 ENGINE N1 DECREASED TO 50 PERCENT AND EGT INCREASED TO 600 DEGREES. VIBRAT ION FELT THROUGHOUT AIRCRAFT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE. PERFORMED ENGINE RUN-UP. SYSTEM GROUND CHECKED, NORMAL OPERATION. A 1ST STAGE HPT BLADE FAILED AT THE AI RFOIL APPROXIMATELY 2.3125 INCHES FROM THE ROOT. THE FRACTURE IS THE RESULT OF STRESS RUPTURE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1999112500388 19991125 00388 NE 1999 11 25 RAIA990817 2 19990814 A 7310 DH8975131 FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 566HK 41084 76039R FLT 7570 - ORF - LEFT FUEL FILTER LIGHT ON. MAINTENANCE REPLACED FUEL FILTER ON LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999112500389 19991125 00389 NE 1999 11 25 RAIA990815 2 19990813 A 7310 1153P0094 FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 566HK 41084 FLT 7788 - ORF - RIGHT FUEL FILTER LIGHT ON. MAINTENANCE REPLACED FUEL PRESSURE SWITCH ON RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999112500390 19991125 00390 NE 1999 11 25 99ZZZM779 2 19990712 A 7510 470962 TUBE BOEING 727 7272Q6 138407V NM PWA JT8 JT8D17 52049 NE LT ANTI-ICE SYS INOPERATIVE A AMTA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 11 782AT 21972 DURING LEVEL CRUISE AT 310, THE NR 1 ENGINE FIRE WARNING ANNUNCIATOR CAME ON. ACCOMPLISHED ENGINE FIRE SHUTDOWN PROCEDU RE, FIRE HANDLE PULLED, LIGHT IMMEDIATELY EXTINGUISHED. REPLACED LEFT FRONT ANTI-ICING TUBE AS REQUIRED. NO LEAKS NOTE D AT THIS TIME, OK FOR SERVICE. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 1999112500391 19991125 00391 NE 1999 11 25 USAASB99192 2 19990805 A 7320 LACKOFLUBE FUEL CONTROL BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE UNKNOWN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 223US LTRTENGINE 21665 PIT - FLT 1279 - APPROXIMATELY 100 MILES EAST OF PIT, FLIGHT WAS CLEARED TO FL350 FROM FL290. CAPTAIN REPORTED A THROTT LE SPLIT WITH A 5 KNOT DIFFERENCE IN ENGINE THRUST DURING CLIMB. FLIGHT RETURNED TO FL290 AND THEN DIVERTED TO PIT WHER E THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED THE LEFT AND RIGHT ENGINE P2 AND P7 SYSTEMS FOR LEAKS. CHECKED THROTTLE RIGGING AND LUBED FUEL CONTROL ASSEMBLIES. ON GROUND RUN, CHECKED LEFT AND RIGHT BLEED VAVLE OPERATION. CHECKED GOOD. TRIMMED ENGINES PER MM. ALL PARAMETERS NORMAL. NO THROTTLE SPREADS NO TED. THROTTLE MOVEMENTS CHECK NORMAL. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999112500392 19991125 00392 NE 1999 11 25 TSAA9977401 2 19990727 A 7250 840001 BLADE BOEING 737 737297 1384480 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 666682 NR 1 ENGINE EGT AT LIMIT ON START, RUNS 40-100 DEGREES ABOVE NR 2 DEPENDING ON FLT CONDITION. SECURED ENGINE AT 400 DEG REE BOROSCOPE FOUND NR 1 ENGINE T-1 DAMAGE BEYOND LIMITS. REMOVED AND REPLACED NR 1 ENGINE TEARDOWN FOUND FORWARD OCC C ASE RETAINING BOLT SHEARED HEAD AS CAUSE OF T-1 BLADE FRACTURE. BOLT IS P/N 772568QQ. LEAK AND OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999112500393 19991125 00393 NE 1999 11 25 USAASB99199 2 19990811 A 7230 COMPRESSOR BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE RT ENGINE STALLED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 268AU 22880 BOS - FLT 2851 - AT ROTATION, CREW HEARD AND FELT A LOUD BANG. ALL ENGINE INDICATIONS WERE NORMAL. FLAMES OR A FLASH W ERE LATER REPORTED BY A PASSENGER OFF THE RIGHT SIDE OF THE AIRCRAFT. AT APPROXIMATELY 5,000 FT. CAPTAIN DECLARED AN E MERGENCY AND PREPPED THE CABIN. FLIGHT RETURNED TO FIELD TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENA NCE ACCOMPLISHED A BOROSCOPE INSPECTION OF THE RIGHT ENGINE COMPRESSOR AND HOT SECTION PER MAINTENANCE MANUAL CHAPTER 7 2. NO DEFECTS NOTED. ACCOMPLISHED POWER RUN PER MM 71-09-200. ALL PARAMETERS CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999112500394 19991125 00394 NE 1999 11 25 AALA990998 2 19990701 A 7230 MS9408258 RIVET BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A AALA A UNSCHED LANDING R B J PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 6823 19701 666211 ORD - FLT 374 - CLIMBING THROUGH 27,000 FEET, NR 1 ENGINE COMPRESSOR STALLED. EGT FLUCTUATED FROM 1.92 TO 1.97. OTHER ENGINE INSTRUMENT REMAINED STEADY AT N1 89 PERCENT, EGT 500 DEGREES, N2 92 PERCENT. COMPRESSOR STALL CAUSED A SMOKY SME LL TO ENTER COCKPIT, ENGINE BLEEDS SWITCHED BY OPENING BLEED NR 2 AND CLOSING BLEED NR 1 RESULTING IN SMOKY SMELL DISSIP ATION AND STABLE ENGINE OPERATION. LANDED ORD WITHOUT INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECKED, NORMAL O PERATION. A 1ST STAGE STATOR RIVET WAS FOUND MISSING ON THE AFT INNER FLANGE AT THE 6:00 O'CLOCK POSITION. THE DEPARTI NG RIVET DAMAGED ALL STAGES OF THE COMPRESSOR. (X) 2 L 7 3 4F 4 F A3WE E2EA 1999112500395 19991125 00395 NE 1999 11 25 AALA991151 2 19990806 A 7230 84001 BLADE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A AALA A UNSCHED LANDING R B J PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 861AA 21088 666224 IAH - FLT 1752 - AFTER TAKEOFF IAH WHILE CLIMBING THROUGH 5,500 FEET, CREW NOTICED A SEVERE VIBRATION THEN HEARD A NOISE . NR 2 ENGINE N1 DROPPED TO 48 PERCENT AND OIL TEMPERATURE WAS AT 130 DEGREES CELSIUS. RETARDED NR 2 THROTTLE AND FOLL OWED EMERGENCY ENGINE FAILURE/SHUTDOWN CHECKLIST. NR 1 CFR ADVISED NR 1 ENGINE WAS SMOKING AFTER LEAVING RUNWAY, BUT TH EY FELT IT TO BE NORMAL. CREW SHUTDOWN NR 1 ENGINE ALSO. RETURNED AND LANDED IAH WITHOUT FURTHER INCIDENT. REPLACED N R 2 ENGINE. SYSTEM GROUND CHECKED, NORMAL OPERATION. A 1ST STAGE HPT BLADE FAILED AT THE AIRFOIL APPROXIMATELY 2 INCHE S FROM THE ROOT. THE FRACTURE IS THE RESULT OF STRESS RUPTURE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1999112500396 19991125 00396 NE 1999 11 25 AALA990953 2 19990625 A 7261 7581193 FILTER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE DEFECTIVE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 144AA 47848 HNL - FLT 72 - DURING CLIMB-OUT, NR 2 ENGINE STRAINER CLOG LIGHT ILLUMINATED INTERMITTENTLY AND THEY STAYED ON. FLIGHT CREW ACCOMPLISHED SHUT DOWN PROCEDURES CHECKLIST AND RETURNED AND LANDED HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSP ECTED NR 2 ENGINE OIL SYSTEM WITH NO CONTAMINATION FOUND. REPLACED NR 2 ENGINE OIL FILTER AND GROUND RAN ENGINE WITH NO LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A22WE E23EA 1999112500397 19991125 00397 NE 1999 11 25 MASA99146 2 19990823 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT DEER STRIKE A MASA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 SW 07 93ZV UE93 FLT 6450 - IN DSM, DURING TAKEOFF ROLL, THE AIRCRAFT STRUCK A DEER. THE AIRCRAFT DEPLANED ON THE TAXIWAY. MAINTENANCE FOUND THE RIGHT PROP HAD LOST THREE BLADES. THERE WAS A HOLE IN THE LOWER RIGHT SIDE OF FUSELAGE. THE ENGINE AND NACEL LE WERE PUSHED AFT AND THE OUTBOARD DE-ICE BOOT WAS TORN. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999112500398 19991125 00398 CE 1999 11 25 MASA99143 1 19990819 A 7712 1293800043 TORQUE GAUGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE FAILED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 65YV UE65 FLT 5977 - PIT-ART - AFTER DEPARTURE FROM PIT, THE CAPTAIN REPORTED THAT THE NR 2 ENGINE TORQUE AND FUEL FLOW WERE FLUCT UATING IN FLIGHT. THE AIRCRAFT DIVERTED TO DUJ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE TORQUE GAUGE AND THE FUEL FLOW GAUGE. THE PROPS WERE THEN BALANCED, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999112500399 19991125 00399 CE 1999 11 25 99ZZZM780 1 19990819 A 7331 1303800101 FUEL FLOW GAUGE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 ENGINE FAILED A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 65YV UE65 FLT 5977 - PIT-ART - AFTER DEPARTURE FROM PIT, THE CAPTAIN REPORTED THAT THE NR 2 ENGINE TORQUE AND FUEL FLOW WERE FLUCT UATING IN FLIGHT. THE AIRCRAFT DIVERTED TO DUJ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE TORQUE GAUGE AND THE FUEL FLOW GAUGE. THE PROPS WERE THEN BALANCED, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999112500400 19991125 00400 GL 1999 11 25 C2XA99CL084 2 19990818 A 7532 23052650 BLEED VALVE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 09 13935 FF3662 145022 ATL-CLE - FLT 4016 - THE CREW REPORTED THAT ON TAKEOFF THE NR 1 ITT WENT TO 921C, THE AIRCRAFT LANDED IN CLEVELAND WITHO UT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE COMPRESSOR ACCELERATION BLEED CONTROL VALVE IAW E MB145 MM 75-31-02 AND PERFORMED OPERATIONAL CHECKS IAW ALLISON MM 72-00-00, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999112500401 19991125 00401 GL 1999 11 25 RAIA990811 2 19990812 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 1 FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 801HK 8230 145053 310172 FLT 5776 - ORD - NR 1 ENGINE OIL PRESS HIGH. MAINTENANCE REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999112500402 19991125 00402 NE 1999 11 25 RAIA990709 2 19990703 A 7532 32897041 BLEED VALVE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 03 426TE 228 FLT 7400 - STL - RIGHT BLEED FAULTED. MAINTENANCE REPLACED NR 2 BLEED VALVE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999112500403 19991125 00403 NE 1999 11 25 ORJA99252 2 19990808 A 7321 76960611 FUEL CONTROL DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE OUT OF ADJUST A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 751RA 49779 RNO - RETURN TO GATE ABORTED TAKEOFF AT ABOUT 30 KNOTS RIGHT ENGINE SLOW TO SPOOL. T/S PER 72-00-04 FIG 114, FOUND BOTH ENGINE IDLES LOW. RETRIM BOTH ENGINE PER 72-00-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1999112500404 19991125 00404 GL 1999 11 25 C2XA99T4001 2 19990913 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 15941 5178 145035 CAE310020 EWR - FLT 4133 - CREW REPORTED THAT THEY ABORTED TAKEOFF DUE TO HIGH OIL PRESSURE ON THE RIGHT ENGINE. AIRCRAFT WAS MAI NTENANCE FERRIED TO TYS AND THE RIGHT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPE RATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999112500405 19991125 00405 NM 1999 11 25 99ZZZM781 1 19990621 A 2710 654476112 PCU BOEING 737 7372L9 1384497 NM AILERON FAILED A F3LA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 03 270FL 4014A 22733 DEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, FIRST OFFICER INITIATED A RIGHT TURN TO FINAL COURSE. AILE RON CONTROL BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS O F FORCE. CAPTAIN ASSISTED FIRST OFFICER AND ROLLED AIRCRAFT TO LEVEL FLIGHT. MAINTENANCE REPLACED A AND B SYSTEM AILER ON PCUS AS A PRECAUTION ADN R 2 FLIGHT SPOILER ACTUATOR DUE TO CHATTERING AND INTERNAL BYPASSING. PERFORMED GENERAL VIS UAL INSPECTION OF FLAP TRACKS, CARRIAGES, TOGGLES, SPINDLES AND AILERON CABLES, AND QUADRANTS, WITH NO DISCREPANCIES NOT ED. EXTERNAL LEAKAGE, SEAL MATERIAL WORN. ELECT HYD SERVO DEFECTIVE. SOLENOIDS SCRATCHED/PITTED/CORROSION. UNIT WAS 2 L 7 2 4F RT A16WE 1999112500406 19991125 00406 NM 1999 11 25 99ZZZM782 1 19990621 A 2761 654456113 PCU BOEING 737 7372L9 1384497 NM SPOILER MALFUNCTIONED A F3LA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 03 270FL 2179 22733 DEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, FIRST OFFICER INITIATED A RIGHT TURN TO FINAL COURSE. AILE RON CONTROL BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS O F FORCE. CAPTAIN ASSISTED FIRST OFFICER AND ROLLED AIRCRAFT TO LEVEL FLIGHT. MAINTENANCE REPLACED A AND B SYSTEM AILER ON PCUS AS A PRECAUTION ADN R 2 FLIGHT SPOILER ACTUATOR DUE TO CHATTERING AND INTERNAL BYPASSING. PERFORMED GENERAL VIS UAL INSPECTION OF FLAP TRACKS, CARRIAGES, TOGGLES, SPINDLES AND AILERON CABLES, AND QUADRANTS, WITH NO DISCREPANCIES NOT ED. UNIT WAS RETURNED WITH 'NO TROUBLE FOUND'. (M) 2 L 7 2 4F RT A16WE 1999112500407 19991125 00407 SO 1999 11 25 C2XA99IA547 1 19991012 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT SO FRAME 33 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM CORRODED AT FRAME 33. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999112500408 19991125 00408 SO 1999 11 25 C2XA99IA546 1 19991012 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO FRAME 34-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE, LT BUTTSTRAP CORRODED BETWEEN FRAMES 34/39. REMOVED AND REPLA CED BUTTSTRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999112500409 19991125 00409 EU 1999 11 25 C2XA99IA556 1 19991026 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING 2A INSPECTION, THE EMERGENCY LIGHT BATTERY LIGHT BATTERY AT 10WL WAS FOUND TO HAVE LOW VOLTAGE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR42-320 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500410 19991125 00410 EU 1999 11 25 C2XA99IA557 1 19991026 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING 2A INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500411 19991125 00411 EU 1999 11 25 C2XA99IA558 1 19991018 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING MAINTENANCE INSPECTION, THE NR 3 EMERGENCY LIGHT POWER SUPPLY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED POWER SUPPLY BATTERY PACK IN ACCORDANCE WITH ATR42-320 MM 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500412 19991125 00412 EU 1999 11 25 C2XA99IA559 1 19991018 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING MAINTENANCE INSPECTION, THE NR 5 EMERGENCY LIGHT POWER SUPPLY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED POWER SUPPLY BATTERY PACK IAW ATR42-320 MM 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500413 19991125 00413 EU 1999 11 25 C2XA99BT098 1 19991022 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 21837 202 BTV - FLT 3680 - MAINTENANCE FOUND PASSENGER DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999112500414 19991125 00414 SO 1999 11 25 C2XA99BT097 1 19991022 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 EWR - FLT 4264 - CREW REPORTED THAT THE AFT EMERGENCY EXIT LIGHT FLOOR STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE NR 4 BATTERY PACK AND OPS CHECKED THE SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999112500415 19991125 00415 SO 1999 11 25 C2XA99IA544 1 19991001 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO FUSELAGE DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16718 120136 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CABIN EMERGENCY LIGHTING INOPERATIVE. 'ARMED' SYSTEM, ALLOWED TO RECHARGE. P ERFORMED FUNCTIONAL CHECK IAW AMM 33-50-00, ALL CHECKS GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999112500416 19991125 00416 SO 1999 11 25 C2XA99IA545 1 19991001 A 5411 120540036 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW EC5410- 01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999112500417 19991125 00417 EU 1999 11 25 C2XA99BT096 1 19991022 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU EXTERIOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 BDL - FLT 3336 - CREW REPORTED AFT EMERGENCY EXTERIOR LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED AFT EXT ERIOR LIGHT BULB AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999112500418 19991125 00418 EU 1999 11 25 C2XA99IA543 1 19991014 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW ATR42-500 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999112500419 19991125 00419 SO 1999 11 25 C2XA99IA542 1 19991014 A 3350 7287550503 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16951 145063 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST SECTION OF EMERGENCY AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999112500420 19991125 00420 SO 1999 11 25 C2XA99IA541 1 19991013 A 3350 F02A250V1A FUSE EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE EXTERIOR EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999112500421 19991125 00421 CE 1999 11 25 C2XA99IA540 1 19991015 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE RT MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 47542 UE198 IAH - DURING FLIGHT 3449, THE CREW REPORTED A GEAR UNSAFE LIGHT DURING EXTENSION AND RETRACTION. THE CREW MANUALLY EXTE NDED THE LANDING GEAR AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK SWITC H IAW B1900-D MM 32-61-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999112500422 19991125 00422 CE 1999 11 25 C2XA99CL119 1 19991020 A 3260 1143610441 HARNESS BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 87557 UE246 THE PILOT REPORTED THE RIGHT GEAR NEEDED TO BE CYCLED ONCE TO GET A DOWN AND LOCKED INDICATION LIGHT ON APPROACH. THE A IRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT DOWN AND LOCKED SQUAT SWITCHES AND HARNESS IAW BEECHCRAFT MM 32-60-05, GEAR RETRACTION WAS GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999112500423 19991125 00423 WP 1999 11 25 TWAA9915901 1 19991121 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROWS 1 - 5 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9412W 53187 THE AFT OVERWING EMERGENCY EXIT LIGHTS AND THE EGRESS LIGHTS AT ROWS 1 TO 5 WERE INOPERATIVE. REPLACED THE BATTERY POWE R SUPPLY B5-23. CHECK-C 9-2-99 MCI. 2 L 7 2 4F RT A6WE 1999112500424 19991125 00424 WP 1999 11 25 TWAA9915902 1 19990925 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 965.091 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND RT STA 965.091 BULKHEAD CRACKED 3 PLACES BETWEEN 220 AND 225. REPLACED RT STA 965.091 B ULKHEAD ANGLE CHORD PER DRAWING JO60119 AND DRAWING 5936993. 2 L 7 2 4F A6WE 1999112500425 19991125 00425 WP 1999 11 25 TWAA9915903 1 19990915 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 & 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LONGERON 4L WITH 2 INCH CRACK AT STA 160 AND 200. REPLACED LONGERON PER SPM 6-70-01, PA GE 2. 2 L 7 2 4F A6WE 1999112500426 19991125 00426 WP 1999 11 25 TWAA9915904 1 19990925 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.55 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, CENTER FRAME ANGLE 5912350-17 WAS CRACKED APPROX 1.5 IN RADIUS AT I/B END, STA 83.55 X=10.00, Z=42 IN LT SIDE. REPLACED ANGLE PER SRO9530268 DRAWING AND EMLR 70039. 2 L 7 2 4F A6WE 1999112500427 19991125 00427 WP 1999 11 25 TWAA9915905 1 19990924 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83.55 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, CENTER FRAME ANGLE 5912350-17 WAS CRACKED APPROX 1.75 INCHES IN RADIUS AND 1.5 IN AT ATTACH RI VETS AT I/B END, STA 83.55, X=-10 IN, Z=42, RT SIDE. REPLACED ANGLE PER SRO 9530268 DRAWING AND EMLR 70039. 2 L 7 2 4F A6WE 1999112500428 19991125 00428 WP 1999 11 25 TWAA9915906 1 19990928 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND FUSELAGE FRAME (P/N 9911505-7) CRACKED 2 PLACES AT STA 83, APPROX 1.25 INCH CRACK. REPL ACED FRAME PER SRO 9530268 DRAWING AND EMLR 70039. 2 L 7 2 4F A6WE 1999112500429 19991125 00429 WP 1999 11 25 TWAA9915907 1 19990920 A 5711 SPAR DOUG DC9 DC931 3022065 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LEFT WING HAD CRACK APPROX 1 INCH LONG AT LOWER I/B HOLE ON FACE OF REAR SPAR AT I/B FLA P HINGE AREA, 5 O'CLOCK POSITION. STOP DRILLED CRACK PER DWG JO60271. REPAIRED LT WING REAR SPAR AT I/B FLAP HINGE ARE A PER DOUGLAS PRINT NUMBER JO60271. 2 L 7 2 4F A6WE 1999112500430 19991125 00430 WP 1999 11 25 IXXA9900032 1 19991123 A 2120 FAN DOUG DC8 DC862 3021970 WP A/C BAY FAILED A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 728PL 978 45918 EN ROUTE FROM QPG TO NKW, AN ELECTRICAL ODOR WAS SENSED IN THE COCKPIT WHEN THE RIGHT RECIRCULATING FAN WAS TURNED ON. T HE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO NKW. MAINTENANCE INSPECTED THE FAN AND WAS FOUND DEFECTIVE AND WAS PLACED ON DEFERRAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1999112500431 19991125 00431 EA 1999 11 25 COMA9960707 1 19991122 A 5320 VANE CAP CNDAIR CL600 CL6002B19 EA FUSELAGE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 709CA 7238 LEFT HAND AND RIGHT HAND INBOARD CAPS CHAFED LEFT HAND .027 RIGHT HAND .028. REMOVED CHAFED INBOARD FLAP VANE INBOARD C APS AND INSTALLED NEW CAPS IAW WVAC EO 601R-57-0632A. 2 L 7 2 4F RT A21EA 1999112500432 19991125 00432 EA 1999 11 25 COMA9960706 1 19991120 A 2780 601R1480341 VANE CAP CNDAIR CL600 CL6002B19 EA TE FLAP CHAFFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 7151 LEFT INBOARD FLAP MOVEABLE VANE INBORAD CAP WAS CHAFED BEYOND LIMITS AT .027 DEEP. REMOVED CHAFED VANE CAP AND INSTALLE D NEW VANE CAP (P/N 601R14803-41) IAW AERODESIGN REPORT NR 1286-1, REV IR, DATED 9/27/94. 2 L 7 2 4F RT A21EA 1999112500433 19991125 00433 EA 1999 11 25 COMA9960705 1 19991120 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 188.040 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 CRACK IN LOWER HORIZONTAL SURFACE OF LEFT HAND LOWER WING ACCESS HOLE AT 550BB. BLENDED OUT DAMAGE, ROTO-PEENED, AND AL ODINED IAW BOMBARDIER REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999112500434 19991125 00434 EA 1999 11 25 COMA9960704 1 19991120 A 5330 6003603032 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 709CA 7238 AFT DOUBLER (P/N 600-36030-32) AT FS 718 RWS STR 11-12 WAS CRACKED. PERFORMED A MAJOR REPAIR BY REPLACING AFT DOUBLER ( P/N 600-36030-32) AT FS 718 RHS STR 11-12 IAW CRJ REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 1999112500435 19991125 00435 NM 1999 11 25 UPS99231137 1 19991122 A 3350 3706701 BATTERY BOEING 727 727172C 1384058 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY LIGHTS INOP. REPLACED BATTERIES, OPS CHECK OK. 2 L 7 3 4F A3WE 1999112500436 19991125 00436 NM 1999 11 25 UPS99431139 1 19991121 A 3150 COMPUTER BOEING 747 747123F NM TE FLAP INOP A IPXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 01 677UP 20391 INSPECTION TYPE:N/A, AFTER TAKEOFF WHEN SELECTING FLAPS UP FROM FLAPS 1, CREW GOT WARNING HORN. AIR TURNBACK DUE TO WAR NING HORN. REMOVED AND REPLACED AURAL WARNING CONTROL LOGIC MODULE. OPS CHECK GOOD. 2 L 7 4 4F A20WE 1999112500437 19991125 00437 NM 1999 11 25 UPS99431140 1 19991123 A 3350 90085 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:N/A, CREW SERVICE DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CREW SERVICE DOOR EMERGENCY LIGHT BA TTERY POWER PACK. 2 L 7 4 4F A20WE 1999112500438 19991125 00438 1999 11 25 UPS99431141 2 19991122 A 7532 BLEED VALVE BOEING 747 747212B 1384886 NM NR 4 ENGINE FAILED A IPXA E C ENGINE SHUTDOWN ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 522UP 21936 INSPECTION TYPE:N/A, AT 1000 FEET ENGINE NR 4 SHOWED ENGINE FIRE. SHUT ENGINE DOWN PER UPS OPERATING PROCEDURES. REMOV ED AND REPLACED NR 4 ENGINE HIGH STAGE BLEED VALVE AND CONTROLLER PER MM 36-11-17 AND 36-11-06, OPS CHECKS NORMAL PER MM 71-00-00. INSPECTED TIRES AND BRAKES AFTER COOL DOWN, CKS NORMAL. 2 L 7 4 4F A20WE 1999112500439 19991125 00439 1999 11 25 UPS99431143 2 19991120 A 7200 JT9D7Q ENGINE BOEING 747 747212B 1384886 NM NR 3 FAILED A IPXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 520UP 21943 INSPECTION TYPE:N/A, NR 3 ENGINE IN-FLIGHT SHUT DOWN DUE TO LOW OIL PRESSURE AND QUANTITY. ENGINE OIL QUANTITY WAS FULL AT TAKEOFF, AS FLIGHT PROGRESSED QUANTITY CONSUMPTION GREATER THAN 1 QUART PER HOUR. OIL PRESSURE DROPPED INTO YELLOW BAND. SHUT DOWN ENGINE AS PER AOM. REMOVED AND REPLACED NR 3 ENGINE IAW UPS TC 5000. OPS AND LK CHECKS GOOD. 2 L 7 4 4F A20WE 1999112500440 19991125 00440 NM 1999 11 25 UPS99531138 1 19991122 A 7100 RB211535E437 ENGINE BOEING 757 75724APF 1384969 NM NR 2 FAILED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 450UP 25472 INSPECTION TYPE:N/A, PACK SMELL DURING FLIGHT, MOSTLY ON LEFT PACK. RIGHT PACK FREE OF SMELL IN FLIGHT. REMOVED AND RE PLACED RIGHT ENGINE PER TC NR 5001. 2 L 7 2 4F RT A2NM 1999112500441 19991125 00441 EU 1999 11 25 QXEA9902351 1 19991116 A 3241 BRAKE FOKKER F28 F28MK4000 4990810 EU ANTI SKID SYSTEM MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 484US 11234 SEA - DURING LANDING ROLL, BREAKING EFFECTIVNESS DIMINISHED NOTICEABLY. INSPECTED ANTI SKID SYSTEM. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999112500442 19991125 00442 NM 1999 11 25 99FDEA00485 1 19991123 A 3231 VALVE BOEING 727 727233 138408A NM MLG DOOR FAILED A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 257FE 20939 DURING GEAR RETRACT RED DOORS LIGHT AND AMBER GEAR DOOR LIGHT (2ND OFF PNL) REMAIN ILLUM. RECYCLED GEAR. *S/D* REMOVE D AND REPLACED NOSE SCHRADER VALVE AND RESERVICE PER MM 12-15-025-2. CHECKED 6 HRS LATER, NO LEAKS AND PRESSURE THE SAM E. 2 L 7 3 4F RT A3WE 1999112500443 19991125 00443 WP 1999 11 25 ABXA9900805 1 19991122 A 7931 CONNECTOR DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE CONTAMINATED A ABXA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 23 828AX 45999 671397 WHEN THROTTLE WAS RETARDED FOR DESCENT, NR 1 LOW OIL PRESSURE LIGHT CAME ON. THROTTLE WAS PULLED BACK TO IDLE, LOW OIL PRESSURE LIGHT STAYED ON. OIL PRESSURE WAS 41 PSI, TEMP 75 DEGREES AND QUANTITY WAS 4.2 GALLONS. SHUT ENGINE DOWN IAW ABNORMAL PROCEDURES. OIL PRESSURE REMAINED ABOVE 10 PSI. INSPECTED NR 1 ENGINE OIL FILTER, NO CONTAMINATION FOUND. CL EANED CANNON PLUG AT OIL PRESSURE SWITCH. RAN ENGINE AT SEVERAL POWER SETTINGS. NO FURTHER DISCREPANCIES NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1999112500444 19991125 00444 WP 1999 11 25 MWEA99837 1 19991121 A 7931 4201091A SWITCH DOUG DC9 DC932 3022066 WP RT ENGINE LEAKING A MWEA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 31 401ME 47133 RIGHT ENGINE OIL QUANTITY DROPPING, OIL PRESSURE AND TEMPS WITHIN LIMITS. MTC REMOVED AND REPLACED DIFFERENTIAL OIL PRE SSURE SWITCH. 2 L 7 2 4F A6WE 1999112500445 19991125 00445 NM 1999 11 25 SCNA99142 1 19991120 A 3350 BATTERY PACK BOEING 727 727259 138408J NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE VERY DIM. FOUND AFT TWO BATTERY PAC KS NOT WIRED TO FLOOR TRACK. INSTALLED MISSING WIRE FROM PACKS AT 19ABC AND 24ABC. ALSO, REPLACED BATTERY PACK AT 24AB C. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999112500446 19991125 00446 NM 1999 11 25 SCNA99143 1 19991120 A 3350 BATTERY PACK BOEING 727 727259 138408J NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE MIDDLE OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE ON THE LEFT SI DE OF THE AIRCRAFT. REPAIRED CHAFED WIRE TO THE LIGHT ASSEMBLY AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOO D. 2 L 7 3 4F A3WE 1999112500447 19991125 00447 NM 1999 11 25 SCNA99144 1 19991120 A 3350 1002833 LIGHT BOEING 727 727259 138408J NM AIRSTAIR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, AN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE IN THE AFT AIRSTAIR AREA. REMOVED AND R EPLACED THE EMERGENCY LIGHT ASSEMBLY IN THE AFT AIRSTAIR AREA IAW MM 335061. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999112500448 19991125 00448 NM 1999 11 25 SCNA99145 1 19991122 A 2131 7638101 CONTROLLER BOEING 727 7272J4 1384006 NM CABIN PRESSURE FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 285SC 12355 21676 DURING CLIMB, UNABLE TO CONTROL THE CABIN ALTITUDE. LEAK CHECKED AIR CONDITIONING SYSTEM, NO LEAKS NOTED. PRESSURIZED AIRCRAFT TO 3.0 PSI AND NO LEAKS NOTED. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER PER MM 21310. SYSTEM OPERATIONA LLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1999112500449 19991125 00449 NM 1999 11 25 VNAA9911017 1 19991121 A 2161 5413C000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN TEMP FAILED A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 457PS 9696 3048 DURING FLIGHT, THE LEFT HAND PACK TEMPERATURE WAS UNCONTROLLABLE AND CAUSED SMOKE TO ENTER THE FLIGHT DECK. THE CREW TU RNED THE LEFT HAND PACK OFF AND THE SMOKE CLEARED THE FLIGHT DECK. THE AIRCRAFT LANDED AT PIT WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE TEMPERATURE CONTROL VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-63-0 6. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999112500450 19991125 00450 EU 1999 11 25 RAIA9911021 1 19991120 A 3260 7177283 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU MLG FAILED A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 567HK 41085 JFK- LEFT MAIN LANDING GEAR LIGHT OUT. MAINTENANCE REPLACED MAIN LANDING GEAR INDICATOR. 2 L 7 2 4T RT A41NM 1999112500451 19991125 00451 EU 1999 11 25 RAIA9911022 1 19991120 A 2840 6839 BULB BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 972JX 972 FAT- FUEL CROSSFEED LIGHT INOP. MAINTENANCE REPLACED LIGHT BULB FOR FUEL CROSSFEED LIGHT. 2 L 7 2 4T RT A56EU 1999120400001 19991204 00001 WP 1999 12 4 TWAA9916101 1 19991123 A 3260 SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 903TW 49154 AFTER TAKEOFF, NOSE GEAR RED LIGHT WAS ON. CYCLED THE GEAR AND THE LIGHT WENT OUT BRIEFLY THEN CAME BACK ON. WENT OUT AFTER 2 HRS OF FLIGHT AND STAYED OUT. ADJUSTED NOSE GEAR LOCK POSITION SENSOR AND ACCOMPLISHED GEAR SWING. AC-00, NO S TATION NO DATE. 2 L 7 2 4F A6WE 1999120400002 19991204 00002 WP 1999 12 4 TWAA9916102 1 19991124 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9304C 49530 EGRESS LIGHT TRACK BROKEN AT MOST AFT PART OF EGRESS STRIP BY THE AFT LAVS. REPAIRED BROKEN WIRE AND SECURED TRACK. AC -IN-VA-LD. 2 L 7 2 4F RT A6WE 1999120400003 19991204 00003 WP 1999 12 4 AT9900817 1 19991024 A 5330 1A537981 PANEL DOUG DC9 DC932 3022066 WP BS 705 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON OVERWING PRESSURE PANEL AT BS 705 LBL 50 BLEN DING CAUSED OUT OF LIMITS. REMOVED CORROSION AND INSTALLED FILLER AND DOUBLER AT BS 705 LBL 50 IAW EO 99-1348. 2 L 7 2 4F A6WE 1999120400004 19991204 00004 WP 1999 12 4 AT9900818 1 19991112 A 5330 SKIN DOUG DC9 DC932 3022066 WP ROW 21 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT CABIN WINDOW 21. BLENDED LIGHTNING ST RIKE, FABRICATED, AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 111 AND EO 99-1338. 2 L 7 2 4F A6WE 1999120400005 19991204 00005 WP 1999 12 4 AT9900819 1 19991112 A 5330 SKIN DOUG DC9 DC932 3022066 WP ROW 25 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT CABIN WINDOW 25. BLENDED LIGHTNING ST RIKE, FABRICATED, AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 111 AND EO 99-1339. 2 L 7 2 4F A6WE 1999120400006 19991204 00006 WP 1999 12 4 AT9900820 1 19991112 A 5330 SKIN DOUG DC9 DC932 3022066 WP ROW 33 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT CABIN WINDOW 33. BLENDED LIGHTNING ST RIKE, FABRICATED, AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 111 AND EO 99-1340. 2 L 7 2 4F A6WE 1999120400007 19991204 00007 WP 1999 12 4 AT9900821 1 19991112 A 5330 SKIN DOUG DC9 DC932 3022066 WP ROW 36 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT CABIN WINDOW 36. BLENDED LIGHTNING ST RIKE, FABRICATED, AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 111 AND EO 99-1342. 2 L 7 2 4F A6WE 1999120400008 19991204 00008 WP 1999 12 4 AT9900822 1 19991112 A 5330 SKIN DOUG DC9 DC932 3022066 WP ROW 42 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT CABIN WINDOW 4. BLENDED LIGHTNING STR IKE, FABRICATED, AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 111 AND EO99-1343. 2 L 7 2 4F A6WE 1999120400009 19991204 00009 WP 1999 12 4 AT9900823 1 19991112 A 5330 SKIN DOUG DC9 DC932 3022066 WP ROW 32 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT CABIN WINDOW 32. BLENDED LIGHTNING ST RIKE, FABRICATED, AND INSTALLED DOUBLER IAW DC9 SRM 53-05 FIG 111 AND EO 99-1341. 2 L 7 2 4F A6WE 1999120400010 19991204 00010 WP 1999 12 4 AT9900824 1 19991115 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 945 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENT AT BS 945. FABRICATED AND INSTALLED SKIN REPAIR AT B S 945 IAW RES 07441 AND EO 99-1364. 2 L 7 2 4F A6WE 1999120400011 19991204 00011 WP 1999 12 4 AT9900825 1 19991117 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT FRAME ATTACH FITTING CORRODED BEYOND LIMITS AT FLOOR LEVEL. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 51-10-03, 51-30, AND EO 99-1357. 2 L 7 2 4F A6WE 1999120400012 19991204 00012 NM 1999 12 4 AT9900827 1 19991117 A 3350 900542 POWER SUPPLY BOEING 737 7372L9 1384497 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 FOUND FORWARD INTERIOR OVERHEAD EMERGENCY LIGHT, EXIT SIGN, INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW 737 MM 3 3-51-81. 2 L 7 2 4F RT A16WE 1999120400013 19991204 00013 NM 1999 12 4 AT9900828 1 19991117 A 3350 1000679 LIGHT BOEING 737 7372L9 1384497 NM COCKPIT INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 FOUND COCKPIT EMERGENCY LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW 737 MM 33-00. 2 L 7 2 4F RT A16WE 1999120400014 19991204 00014 WP 1999 12 4 AT9900829 1 19991109 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 811AT 47285 FOUND AFT EMERGENCY CEILING LIGHTS DIM. REMOVED AND REPLACED BATTERY PACKS AND BATTERIES B5-28, B5-25, B5-26, B5-27 IAW 737 MM 33-53-0. 2 L 7 2 4F A6WE 1999120400015 19991204 00015 NM 1999 12 4 AT9900830 1 19991114 A 3230 893601 PSEU BOEING 717 717200 1383700 NM E/E BAY FAILED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 943AT 55006 FOUND AFTER TAKEOFF AT 200-300FT PSEU FAIL ON EAD. AFTER GEAR EXTENSION, NO GREEN LIGHT ON LEFT MAIN GEAR, SECONDARY IN DICATIONS ALL GREEN. REMOVED AND REPLACED PSEU IAW 717 MM 32-61-01 PAGE 401-405. 2 L 7 2 4F TR A6WE 1999120400016 19991204 00016 WP 1999 12 4 AT9900831 1 19991115 A 3520 PSU DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 848AT 47559 FOUND OXYGEN MASK INSPECTION FAILED DROP TEST, 5 PANELS DID NOT DEPLOY, ROW 24, SEAT: A-C, ROW 25, SEAT: D,E,F, ROW 4, SEAT: A-C, FORWARD FLIGHT ATTENDANT PANEL, ROW 23, SEAT: D,E,F. ADJUSTED PANEL DOOR AND REPOSITIONED LANYARD IAW DC9 MM 35-20-2, 35-20-3. 2 L 7 2 4F A6WE 1999120400017 19991204 00017 WP 1999 12 4 AT9900832 1 19991111 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 FOUND FUSELAGE SKIN CORRODED AT BS 954 BETWEEN L26R- S29R. REMOVED CORRODED SECTION OF SKIN, FABRICATED AND INSTALLED R EPAIR DOUBLER AND TRIPLER IAW DC9 SRM 51-30-2, 51-10-3, 53-05, TIMCO EO 99-1369 REV IR. 2 L 7 2 4F A6WE 1999120400018 19991204 00018 WP 1999 12 4 AT9900833 1 19991111 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 930 - 958 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 818AT 47320 FOUND AFT CARGO COMPARTMENT LONGERON 30 AT BS 930-958 HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED LONGERON 30 AT BS 930-958 IAW DC9 SRM 53-02 FIGURE 14. 2 L 7 2 4F A6WE 1999120400019 19991204 00019 WP 1999 12 4 AT9900834 1 19991116 A 5310 STRUCTURE DOUG DC9 DC932 3022066 WP BS 37 DAMAGED A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 806AT 47379 LEFT SIDE OF NOSE SECTION AND FORWARD BULKHEAD WERE DAMAGED BY BAGGAGE CART. REPAIRED LEFT NOSE SECTION AND FORWARD BUL KHEAD AT BS 37 IAW DC9 SRM 53-01 FIG 4, 53-01 FIG 2, RES 99-1628, RES 99-1629, RES 99-1630, AND RES 99-1651. 2 L 7 2 4F A6WE 1999120400020 19991204 00020 WP 1999 12 4 AT9900835 1 19991106 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 227 - 285 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 FOUND LONGERON 20R AT BS 227 TO 285 CORRODED. CUT OUT CORRODED SECTION OF LONGERON. FABRICATED NEW LONGERON SECTION AN D SPLICES. INSTALLED REPAIR IAW DC9 SRM 53-10-2, 51-30-2, 51-10-3 AND 51-10-4. 2 L 7 2 4F A6WE 1999120400021 19991204 00021 WP 1999 12 4 AT9900836 1 19991121 A 3520 PSU DOUG DC9 DC932 3022066 WP CABIN OUT OF ADJUST A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 837AT 45774 FOUND WHILE ACCOMPLISHING WO55322 PER EO9-3520-29-E1461 REV A, THE RIGHT AFT LAVATORY OXYGEN MASK COMPARTMENT AND THE FO RWARD FLIGHT ATTENDANT OXYGEN MASK COMPARTMENT DOORS DID NOT DEPLOY. CLEANED AND ADJUSTED DOORS AS REQUIRED. 2 L 7 2 4F A6WE 1999120400022 19991204 00022 WP 1999 12 4 CALA9901530 1 19991123 A 5230 DOOR PAN DOUG DC9 DC982 3022082 WP CARGO DOOR WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND MAIN BAGGAGE BIN DOOR INNER PAN WORN THROUGH AT AFT LOCKING CAM. A DOUBLER WAS INSTALLED IAW ECRA 5230 -01502. 2 L 7 2 4F A6WE 1999120400023 19991204 00023 WP 1999 12 4 CALA9901531 1 19991123 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 206 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND A 2 CRACK IN LT WING LEADING EDGE LOWER SKIN FOUR INCHES OUTBOARD OF NR 2 SLAT CENTER TRACK CUTOUT AT S TA XFS 206. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5730-01670. A DIP WAS INITIATED TO PERMANEN TLY REPAIR THE AREA WITHIN 21 DAYS. 2 L 7 2 4F A6WE 1999120400024 19991204 00024 NM 1999 12 4 UPS99431144 1 19991123 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM GALLEY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 UPPER DECK EMERGENCY LIGHT (2) IN CEILING AFT OF CREW GALLEY ARE INOP. THE LIGHTS COME ON AND THEN GO OUT IMMEDIATLY. F OUND CEILING BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 4 4F A20WE 1999120400025 19991204 00025 NM 1999 12 4 UPS99431145 1 19991123 A 3350 90085 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 CREW SERVICE DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CREW SERVICE DOOR EMERGENCY LIGHT BATTERY POWER PACK. O PS CHECK NORMAL. 2 L 7 4 4F A20WE 1999120400026 19991204 00026 WP 1999 12 4 UPS99831146 1 19991122 A 3350 5708458503 LIGHT DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779UP 45979 EMERGENCY EXIT LIGHTS FAILED TO COME ON DURING PREFLIGHT CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PN O N 5208458-503, PN OFF 570845 8-503 SN ON 976 SN OFF 2054, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999120400027 19991204 00027 WP 1999 12 4 UPS99831147 1 19991124 A 2930 GAUGE DOUG DC8 DC873F 302199F WP HYD SYSTEM INOP A IPXA O OTHER N FALSE WARNING LD LANDING 1 SO 01 810UP 46001 REVERSER HYDRALIC PRESS GAUGE INDICATES ZERO WITH HYD S/O SWITCH OFF WITH SWITCH IN THE OPEN POSITION ABLE TO GET ALL 4 REVERSORS ON LANDING ROLL. REPLACED HYD PRESS GAUGE AND TRANSMITTERS. OPS CHECK OK, NO LEAKS. 2 L 7 4 4F RT 4A25 1999120400028 19991204 00028 WP 1999 12 4 UPS99831148 1 19991124 A 7110 COWL DOUG DC8 DC871F 302199D WP NR 3 & 4 ENGINE DAMAGED A IPXA O OTHER O OTHER LD LANDING 1 SO 01 703UP 45939 INSPECTION TYPE:N/A, UPON LANDING NUMBER 3 AND 4 ENGINE COWLS CONTACTED RUNWAY. *S/D* REMOVED AND REPLACED NUMBER 3 AN D 4 ENGINE AND DAMAGED FAN COWLS PER MM 71-10-02 AND TC 9071-1, 9071-2. PERFORMED ENGINE RUNS PER TC 9071-2 AND 9071- 3 . REFER TO LOG PAGES 371266 TO LOG PAGES 371273, OPERATIONAL CHECKS. 2 L 7 4 4F RT 4A25 1999120400029 19991204 00029 NM 1999 12 4 99FDEA00486 1 19991124 A 3231 DOOR BOEING 727 727233 138408A NM NLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 257FE 20939 RED DOOR LIGHTS AND S/O AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUM'D AFTER GEAR RETRACTION W/HANDLE UP. CREW FELT/HEARD NOSE GEAR DOOR NOT FULLY CLOSED. ACCOMPLISHED RED TABS. AFTER GEAR WAS RECYCLED CREW FELT/HEARD SUBSTANTIALLY LESS NOI SE AIRSPEED LIMITED TO 270 KNOTS OR LESS. LIGHT WENT OUT AT 6000 MSL 190 KNOTS. 2 L 7 3 4F RT A3WE 1999120400030 19991204 00030 NM 1999 12 4 99FDEA00487 1 19991124 A 2120 UNKNOWN BOEING 727 727233 138408A NM CABIN ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 285FE 22622 DURING T/O A BURNING RUBBER ODOR AND SMOKY HAZE BEGAN TO FILL THE COCKPIT AND CARGO AREA. RED TABS FOLLOWED AND A/C INI TIATED RETURN TO BASE. INSP'D FOLLOWING AREAS FOR PROBLEMS, BOTH E & E BAYS, A/C PACK BAYS, AFT AIRSTAIRS, GEARWELLS, S NAKE PIT IN FWD BELLY, CAPTS, & F/O INSTRUMENT PANELS COCKPIT OVERHEAD, PEDESTAL, C/B RACKS & RUBBER PEDAL AREA. CK'D G ASPER FAN OPS, W/APU RUNNING. OPS BOTH PACKS, RAN ALL ENG & C/W PNEU & A/C CKS, AIR CLEANER SYS CK, PNEU SYS CK, PRESS CONT SYS CK TEST, AUTO PACK TRIP CK, SIMULATED T/O & CLIMB PWR SETTINGS & PACK OPS NO DEFECT/PROBLEMS. ONLY CK NOT DUP WAS T/O. 2 L 7 3 4F RT A3WE 1999120400031 19991204 00031 WP 1999 12 4 DHL99805002 1 19991124 A 3222 STRUT DOUG DC8 DC873F 302199F WP NLG DISCHARGED A DHLA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 805DH 46125 AFTER TAKEOFF, LANDING GEAR HANDLE JAMMED IN DOWN POSITION. COMPLETED ABNORMAL PROCEDURES RETURNED TO CVG. RESERVICED NOSE STRUT WITH HYDRAULIC FLUID AND NITROGEN. PERORMED GEAR SWING AND OPS CHECKED GOOD PER DC-8 M/M. 2 L 7 4 4F RT 4A25 1999120400032 19991204 00032 NM 1999 12 4 VNAA9911018 1 19991122 A 7603 001A761A1010100 SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CONDITION LEVER FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 459PS 3070 DURING FINAL APPROACH, THE RIGHT ELECTRONIC ENGINE CONTROL UNIT FAILED WHEN CONDITION LEVERS WERE MOVED FROM MINIMUM TO MAXIMUM. THE CREW WAS ABLE TO RESET THE UNIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACE D THE RIGHT CONDITION LEVER MICROSWITCH RACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-05. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999120400033 19991204 00033 NE 1999 12 4 VNAA9911019 2 19991122 A 7532 311995704 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 437JS 9247 3055 116103 DURING FINAL APPROACH, THE RIGHT ELECTRONIC ENGINE CONTROL UNIT FAILED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENA NCE INSPECTED AND CLEANED THE RIGHT INTERCOMP BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-00-00. OPERA TIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999120400034 19991204 00034 NE 1999 12 4 VNAA9911020 2 19991123 A 7532 311995704 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 458PS 10230 3068 116144 DURING CLIMB-OUT, THE LEFT ELECTRONIC ENGINE CONTROL UNIT FAILED. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER IN CIDENT. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND INTERCOMP BLEED VALVE CANNON PLUG AND SCREEN IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999120400035 19991204 00035 EU 1999 12 4 RAIA9911023 1 19991125 A 3060 ANN60 FUSE JETAIR JETSTM JETSTM4101 1500501 EU PROP DEICE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 570HK 41089 6225 - JFK - LEFT PROP DE-ICE FAILED. MAINTENANCE REPLACED FUSE FOR LEFT PROP. 2 L 7 2 4T RT A41NM 1999120400036 19991204 00036 EU 1999 12 4 RAIA9911024 1 19991125 A 3320 LT52A BALLAST BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 427AM 876 7348 - STL - ELECTRICAL SMELL IN AIRCRAFT. MAINTENANCE REPLACED LIGHTING BALLAST AT POSITION 1LH7 IN CABIN. 2 L 7 2 4T RT A56EU 1999120400037 19991204 00037 NM 1999 12 4 SWAA991952 1 19991121 A 5314 6545866 KEEL BEAM BOEING 737 7375H4 138449D NM BS 717 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM CRACKED AT LOWER SKIN, BS 717. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999120400038 19991204 00038 1999 12 4 SWAA991953 4 19991122 A 2565 D31354 INDICATOR BOEING 737 7372H4 138448C NM SLIDE MOVED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999120400039 19991204 00039 NM 1999 12 4 SWAA991954 1 19991122 A 3213 26078251 AXLE BOEING 737 7373H4 1384600 NM NLG SHEARED A SWAA O OTHER O OTHER NR NOT REPORTED 1 SW 07 335SW 23939 ON ARRIVAL TO GATE, FOUND RT NLG TIRE/WHEEL ASSY MISSING. FOUND NLG RT AXLE SHEARED JUST OUTBOARD OF INNER BEARING. R EMOVED AND REPLACED LOWER STRUT ASSY AND REMOVED AND REPLACED BOTH NLG TIRE/WHEEL ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999120400040 19991204 00040 NM 1999 12 4 SWAA991955 1 19991122 A 5751 6546454 SKIN BOEING 737 7372H4 138448C NM AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING WALK ARROUND INSP, FOUND RT AILERON DELAMINATED. REMOVED AND REPLACED AILERON PER MM. 2 L 7 2 4F A16WE 1999120400041 19991204 00041 NM 1999 12 4 SWAA991956 1 19991122 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 057SW 21722 DURING RON, FOUND FWD ENTRY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999120400042 19991204 00042 NM 1999 12 4 SWAA991957 1 19991122 A 2560 P4010021 BATTERY BOEING 737 7372H4 138448C NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SPECIAL VISIT, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F A16WE 1999120400043 19991204 00043 NM 1999 12 4 SWAA991958 1 19991122 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM BS 500B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 500B, STRINGER 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F A16WE 1999120400044 19991204 00044 NM 1999 12 4 SWAA991959 1 19991122 A 5315 6516323 FLOORBEAM BOEING 737 7372H4 138448C NM BS 259 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND BS 259 FLOORBEAM UPPER SURFACE CORRODED, LBL 9 TO RBL 9. REPAIRED BEAM PER SRM. 2 L 7 2 4F A16WE 1999120400045 19991204 00045 NM 1999 12 4 SWAA991960 1 19991122 A 3350 101114 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999120400046 19991204 00046 1999 12 4 SWAA991961 4 19991120 A 2565 D31354 SLIDE BOEING 737 7373T5 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999120400047 19991204 00047 NM 1999 12 4 SWAA991962 1 19991122 A 3020 2703200 CLAMP BOEING 737 7373H4 1384600 NM NR 1 ENGINE LOOSE A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 395SW 27689 AIR TURNBACK, NR 1 ENG OVERHEAT LIGHT ILLUMINATED DURING CLIMB AFTER NOSE COWL ANTI-ICE VALVE WAS TURNED ON. REPLACED F WD ATTACH ANTI-ICE VALVE CLAMP. 2 L 7 2 4F RT A16WE 1999120400048 19991204 00048 NM 1999 12 4 SWAA991963 1 19991123 A 2131 7110025 CONTROLLER BOEING 737 7373H4 1384600 NM COCKPIT INOP A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 357SW 26594 AIR TURNBACK, AIRCRFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REMOVED AND REPLACED PRESSURE CONTROLLER PANEL PER MM. 2 L 7 2 4F RT A16WE 1999120400049 19991204 00049 1999 12 4 SWAA991936 4 19991118 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999120400050 19991204 00050 NM 1999 12 4 SWAA991937 1 19991118 A 5311 6546533 FRAME BOEING 737 7372H4 138448C NM BS 490 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR CUT OUT FRAME CRACKED, BS 490, WL 183-189. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999120400051 19991204 00051 1999 12 4 SWAA991938 4 19991118 A 2565 D31354 INDICATOR BOEING 737 7372H4 138448C NM PAX DOOR MOVED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 AFT ENRTY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999120400052 19991204 00052 NM 1999 12 4 SWAA991939 1 19991117 A 5753 6573732 SKIN BOEING 737 7373G7 1384595 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691WN 23781 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SWA RA NR 1-35 7-0769. 2 L 7 2 4F RT A16WE 1999120400053 19991204 00053 NM 1999 12 4 SWAA991940 1 19991118 A 2781 WIRE BOEING 737 7373Q8 1384670 NM FLAP INDICATOR FAILED A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 688SW 23254 ABORTED TAKEOFF, TAKE-OFF WARNING HORN SOUNDED AND NR 4 L/E FLAP TRANSIT LIGHT INOP. REPAIRED WIRING CONNECTING TO NR 4 L/E FLAP DOWN POS INDICATOR SWITCH PER MM. 2 L 7 2 4F RT A16WE 1999120400054 19991204 00054 NM 1999 12 4 SWAA991933 1 19991116 A 7830 R8963P01 LINE BOEING 737 7373H4 1384600 NM NR 2 ENGINE RUPTURED A SWAA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 07 661SW 23173 LOSS OF B-SYSTEM HYD PRESS DURING FLIGHT. LOW PRESS LIGHT ILLUMINATED AND HYD QTY IND DECREASED TO 1/8 FULL. DISCOVERE D RUPTURED NR 2 ENG T/R LOCKING ACTUATOR PRESS LINE. REMOVED AND REPLACED FLEX LINE PER MM. LEAK AND OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999120400055 19991204 00055 NM 1999 12 4 SWAA991934 1 19991117 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 611SW 27697 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 1999120400056 19991204 00056 NM 1999 12 4 SWAA991935 1 19991117 A 5311 6516323 FRAME BOEING 737 7373Y0 1384671 NM BS 304 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED 1/2D CHECK, FOUND BS 304 FRAME CRACKED, STRINGER 4L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999120400057 19991204 00057 NM 1999 12 4 SWAA991941 1 19991120 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 612SW 27930 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 1999120400058 19991204 00058 NM 1999 12 4 SWAA991942 1 19991120 A 3230 BACH8B04NN166T LINE BOEING 737 7373Q8 1384670 NM NLG RUPTURED A SWAA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 689SW 23387 AIR TURNBACK, NLG FAILED TO RETRACT DURING TAKEOFF. FOUND RUPTURED NLG DOWNLOCK ACTUATOR HYDRAULIC PRESS LINE. REMOVED AND REPLACED LINE PER MM. 2 L 7 2 4F RT A16WE 1999120400059 19991204 00059 1999 12 4 SWAA991943 4 19991120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 618WN 28034 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999120400060 19991204 00060 NM 1999 12 4 SWAA991944 1 19991120 A 5320 65C27314 CLIP BOEING 737 7372H4 138448C NM BS 663 & BS 534 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND THROUGH HFEC INSPECTION 2 EACH STRINGER TIE CLIPS CRACKED, BS 663, STR 7R, AND BS 534, S TR 4R. REMOVED AND REPLACED TIE CLIPS PER SRM. 2 L 7 2 4F A16WE 1999120400061 19991204 00061 NM 1999 12 4 SWAA991945 1 19991120 A 5313 6546546 STRINGER BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND THROUGH HFEC INSPECTION STRINGER CHORD 18A LT CRACKED, BS 727. REPAIRED PER ACO 651-53. 2 L 7 2 4F A16WE 1999120400062 19991204 00062 NM 1999 12 4 SWAA991946 1 19991120 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 480 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND FUSELAGE EXTERNAL SKIN CORRODED, BS 480, STRINGER 4R. REMOVED AND REPLACED SKIN PANEL B S 360-BS 520 PER ACO 6717-53. 2 L 7 2 4F A16WE 1999120400063 19991204 00063 NM 1999 12 4 SWAA991947 1 19991120 A 5330 6545769 SKIN BOEING 737 7372H4 138448C NM BS 468 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND FUSELAGE EXTERNAL SKIN CORRODED, BS 468, WL 148. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999120400064 19991204 00064 NM 1999 12 4 SWAA991948 1 19991120 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SWA RA NR 1-353-2176. 2 L 7 2 4F RT A16WE 1999120400065 19991204 00065 NM 1999 12 4 SWAA991949 1 19991120 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED AT 9 EACH PLACES. REPAIRED BULKHEAD PER DALFORT XEA X2-53-26 7. 2 L 7 2 4F RT A16WE 1999120400066 19991204 00066 1999 12 4 SWAA991950 4 19991120 A 2565 D31354 INDICATOR BOEING 737 7373H4 1384600 NM SLIDE MOVED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 612SW 27930 FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999120400067 19991204 00067 1999 12 4 SWAA991951 4 19991120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999120400068 19991204 00068 EU 1999 12 4 CA990513012 1 19990504 A 2430 10200311 GCU AEROSP ATR42 ATR42300 8680920 EU PWA PW121 PW121 52124 NE HAMSTD 14SF 14SF5 NE DC SYSTEM FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 21523 5100113 120423 MFG870702 (CAN) DURING CLIMB, NR 1 DC POWER WAS LOST. NR 1 GCU REPLACED. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999120400069 19991204 00069 SO 1999 12 4 CA991027076 1 19991012 A 2910 1934 LINE AIRESRCH LW10098 PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL HYD SYSTEM CRACKED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 740 L767261A DJ11279A (CAN) HOSE DOES NOT STAND UP TO HEAT IN AREA OF CONTROLLER. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999120400070 19991204 00070 SW 1999 12 4 CA991027081 1 19990915 A 5315 204030163325 FLOORBEAM 204200013001 BELL 204 204B 1181404 SW LYC T53 T5311B 41549 NE CABIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13298 2004 LE13064 (CAN) DURING REMOVAL OF FLOORBOARDS DURING SCHEDULED MAINTENANCE, THE LEFT MAIN BEAM WEB WAS FOUND CRACKED. REPAIR CARR IED OUT IAW BELL DATA. SUBMITTER SUSPECTED CRACK WAS CAUSED DUE TO HEAVY INTERNAL CARGO. 1 G 7 1 4U 4 U H1SW E1EA 1999120400073 19991204 00073 EU 1999 12 4 CA991028031 1 19991007 A 6420 60102RSIMT33CA BEARING 350A33200505 SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE T/R SPIDER ROUGH W K NONE O OTHER IN INSP/MAINT 1 CA 1450 M2098 9190 (CAN) DURING COMPLIANCE WITH DGAC AD 99-085-076(A)R1, FOUND T/R PITCH CHANGE SPIDER BEARING WAS VERY ROUGH/DRY. BEARING REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 1999120400075 19991204 00075 SW 1999 12 4 CA991028058 1 19991019 A 5302 206032409001 FITTING BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL TAIL BOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 81 CAE800420F (CAN) LEFT UPPER TAIL BOOM/FUSELAGE ATTACHMENT FITTING FOUND CRACKED DURING A CAMPAIGN NOTICE (DATED OCT 12/99). 1 G 7 1 3U 3 U H2SW E4CE 1999120400076 19991204 00076 SW 1999 12 4 CA991028065 1 19991018 A 2550 204072915103 CARGO HOOK BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA SLING LOAD FAILED W H DEACTIVATE SYST/CIRCUITS O OTHER HO HOVERING 1 CA AEL16936 CPPS61075 (CAN) WHILE IN THE HOVER, IT WAS NOTED THAT THE CARGO HOOK WOULD NOT ELECTRICALLY CLOSE. THIS WAS CAUSED BY THE LOAD RI NG ENDING UP BETWEEN THE CARGO HOOK AND THE HOOK SECURITY LATCH. SUBMITTER STATED THE CREW WAS THEN UNABLE TO OPEN OR C LOSE THE CARGO HOOK (ELECTRICALLY/MANUALLY) WHICH COULD HAVE HAD SERIOUS CONSEQUENCES IN AN IN-FLIGHT EMERGENCY. 1 G 7 1 4U 4 U H4SW E22EA 1999120400077 19991204 00077 EU 1999 12 4 CA991028066 1 19991018 A 3213 112335114 ANGLE BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL SKID TUB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE835693 (CAN) DURING SCHEDULED INSPECTION OF SKID GEAR, A CRACKED ANGLE WAS FOUND ON THE LEFT AFT SKID TUBE. SUBMMITTER SUSPECT ED CRACK WAS CAUSED BY NORMAL IN-SERVICE OPERATIONS, HOWEVER, SERIOUS DAMAGE COULD HAVE OCCURRED IF BEAR PAW HAD DEPARTE D SKIDS DURING FLYING. BEAR PAW ANGLES WERE REPLACED. 1 G 7 2 3U 3 U H3EU E4CE 1999120400079 19991204 00079 SW 1999 12 4 CA991028073 1 19991018 A 6730 412076620101 UNIVERSAL BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA COLLECTIVE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 2196 CPPS60495 (CAN) DURING REPLACEMENT OF THE RIGHT CYCLIC SERVO (FOR TIME), THE UNIVERSAL JOINT ON THE OUTPUT RAM WAS FOUND TO HAVE S EIZED (LOWER BEARING), AND THE INNER RACE WAS TURNING ON THE ATTACHMENT BOLT (P/N 20-057-5-24D). THE BOLT WAS ALSO CORR ODED AND HAD WEAR STEPS. 1 G 7 1 4U 4 U H4SW E22EA 1999120400080 19991204 00080 SW 1999 12 4 CA991103009 1 19991027 A 2435 230791281 BRUSH LUCAS 230790002 FRCHLD SA227 SA227CC SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE STARTER/GEN CRACKED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 479 97010 P44168 931191 (CAN) 5 MINUTES AFTER TAKEOFF, THE RIGHT GENERATOR WENT OFF-LINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENA NCE DETERMINED THAT THE STARTER/GENERATOR BRUSHES HAD CRACKED AND THE LEADS HAD SEPARATED FROM THE REMAINING BRUSH MATER IAL. 2 L 7 2 4T 4 T RT A18SW E4WE 6 C 3PNE 1999120400084 19991204 00084 EU 1999 12 4 CA991103018 1 19991020 A 6210 350A11001006 BLADE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2968 571A 4495 (CAN) M/R BLADE CHORDWISE CRACK (90 MM LONG) DETECTED DURING SCHEDULED MAINTENANCE. CRACK WAS ON UNDERSIDE OF BLADE AT 179 MM FROM LEADING EDGE AND AT BLADE STATION 1160 MM. THERE WAS ALSO DEBONDING ON THE STAINLESS STEEL LEADING EDGE OF THE BLADE. 1 G 7 1 3U 3 U H9EU E19EU 1999120400085 19991204 00085 WP 1999 12 4 CA991103019 1 19991020 A 6710 369A7304 BRACKET HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ROTOR CONTROL FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 5439 CAE830905 (CAN) DURING ROUTINE INPSPECTION (UNDER THE FRONT MIDDLE SEAT), THE BEARING CAP WAS FOUND BROKEN ON THE FORWARD SIDE ON THE COLLECTIVE/CYCLIC ASSEMBLY. 1 G 7 1 3U 3 U H3WE E4CE 1999120400086 19991204 00086 CE 1999 12 4 CA991103020 1 19991005 A 5280 HINGE BEECH 90 C90 1152913 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL MLG DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13554 PCE50546 BU3119 (CAN) AT INSPECTION IT WAS NOTICED THAT THE DOOR HINGE WAS CRACKED AT A FEW LOCATIONS ON THE DOOR SIDE OF THE HINGE. TH E HINGE WAS REPLACED ON BOTH SIDES C/W NEW HINGE PIN. 1 L 7 2 3T 4 T 3A20 E4EA 6 C P15EA 1999120400087 19991204 00087 SO 1999 12 4 CA991103025 1 19991005 A 3233 94951 ACTUATOR PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1G5 41532 EA HARTZL HCC2Y HCC2YK1 GL MLG CRACKED W O OTHER K FLUID LOSS NR NOT REPORTED 1 CA 2509 286 L1617348A CH30593A (CAN) ACTUATOR HOUSING CRACKED AT FITTING PORT. SUBMITTER STATED REPLACEMENT PART ACTUATOR HAS IMPROVED DESIGN WITH A S TRONGER PORT. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 1999120400088 19991204 00088 CE 1999 12 4 CA991103029 1 19991024 A 5610 10138402522 WINDSHIELD BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCB3T HCB3TN3 GL COCKPIT SHATTERED W G A O2 MASK DEPLOYED UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA 801 97118H5259 PCE81062 BUA22063 (CAN) BEFORE WINDSHILED CRACKED IN-FLIGHT, THE GLASS WAS DELAMINATING AT APPROXIMATELY 4 SQUARE INCHES IN THE LEFT BOTTO M CORNER. DELAMINATION AND LACK OF SEAL IN WINDOW FRAME MAY HAVE CONTRIBUTED TO OVERSTRESS IN TIME. SUBMITTER SUGGESTE D FACTS TO REDUCE POSSIBLE RECURRENCE, WHEN WINDOW DOESN'T SIT 100 PERCENT IN PLACE, NEVER OVERTORQUE WINSHIELD SCREWS A ND BE SURE TO PROVIDE PROPER SEALS AND SUFFICIENT SEALANT. 1 L 7 2 4T 4 T A24CE E4EA 6 C P15EA 1999120400089 19991204 00089 CE 1999 12 4 CA991103031 1 19991014 A 5610 10138402515 WINDSHIELD BEECH B300 B300 1159232 CE PWA PT6 PT6A60A 52043 NE HARTZL HCB4M HCB4MP3 GL COCKPIT CRACKED W G A O2 MASK DEPLOYED UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA 842 95144H8607 PCE95500 FW991 (CAN) AT FL 260 AND WINDSHIELD HEAT HAD BEEN ON FOR APPROXIMATELY 45 MINUTES IN 'LOW' POSITION, THE LEFT WINDSHIELD WAS OBSERVED TO SHATTER BUT REMAINED INTACT. NO POINT OF ORIGIN COULD BE DETERMINED. WINDSHIELD REPLACED. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 1999120400090 19991204 00090 CE 1999 12 4 CA991103048 1 19991027 A 3234 CONTACT HARTMAN MC815AS1 BEECH 100 A100 1152915 CE PWA PT6 PT6A34 52043 EA HARTZL HCB4T HCB4TN3 GL MLG SELECTOR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 340 CC38604 PCE57492 EAA1075 (CAN) AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT THE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO BASE. TROUBLES HOOTING REVEALED THAT A SET OF POINTS IN THE LANDING GEAR CONTROLLER WELDED TOGETHER. THE MOTOR WAS REPLACED. THIS IS T HE FOURTH PROBLEM WITH THESE CONTROLLERS. SUBMITTER STATED NOW REQUIRING THE VENDOR TO OVERHAUL THE UNIT IN ADDITION T O POLISHING THE POINTS. THESE UNITS WERE ONLY BEING SENT FOR POINTS POLISHING IN THE PAST. ADDITIONALLY, IT HAS BEEN D ETERMINED THAT THE CONNECTING CABLES TO THE MOTOR CONTROLLER CAN ROTATE THE STUD WHEN TIGHTENING. INSIDE THE CONTROLLER THE STUD IS SQUARE AND IF IT ROTATES, WILL BRING IT CLOSER TO THE CONTACTS, WHICH COULD CAUSE A PROBLEM AS WELL. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 1999120400091 19991204 00091 SO 1999 12 4 CA991103050 1 19991013 A 5310 4521504 DOOR FRAME PIPER PA31T PA31T2 7103127 SO PWA PT6 PT6A135 52043 NE HARTZL HCB3T HCB3TN3 GL FUSELAGE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 10422 PCE92434 BUA21235 (CAN) DOOR FRAME (BULKHEAD) BROKE AT SNUBBER UPPER ATTACHMENT POINT. 1 L 7 2 3T 4 T RT A8EA E4EA 6 C P15EA 1999120400092 19991204 00092 CE 1999 12 4 CA991103051 1 19991127 A 3213 50810323 TORQUE KNEE 115810000653 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL RT & LT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 887 342R PCE50228 EAA1113 (CAN) WHILE MOVING AXLE TO CHECK FOR EXCESSIVE PLAY, MOVEMENT WAS NOTICED IN THE TORQUE KNEE UPPER AND LOWER BUSHINGS (B OTH MAIN GEAR). LEFT AND RIGHT LANDING GEAR TORQUE KNEES REMOVED TO INSTALL NEW BUSHINGS. DURING BUSHING REPLACEMENT, A SMALL CRACK WAS NOTICED IN THE RADIUS OF SINGLE BOLT HOLE. UNIT L.P.I'D CONFIRMED CRACK. TWO OUT OF FOUR TORQUE KNE ES FOUND CRACKED. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 1999120400093 19991204 00093 CE 1999 12 4 CA991103052 1 19990902 A 3230 50810336 BOLT BEECH 100 100BEECH 1152916 CE GARRTT TPE331 TPE3316252B 01514 WP HARTZL HCB4T HCB4TN5 GL DRAG BRACE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 383 P27185 CDA3702 (CAN) PILOT FOUND THE BOLT HEAD MISSING ON THE LEFT LOWER DRAG BRACE TO GEAR ATTACHMENT. CLOSER INSPECTION REVEALED THA T THE BOLT HAD FAILED AT THE DRILL HOLES IN THE CENTER OF THE SHANK. INSPECTED TWO OTHER FASTENERS ON THE LEFT DRAG BRA CE AND ALL THREE ON THE RIGHT SIDE. THOSE INSTALLED IN THE RIGHT SIDE DID NOT HAVE THE SAME BOLT. SUBMITTER SUSPECTED THAT THE WRONG P/N BOLT HAD NOT BEEN INSTALLED DURING PREVIOUS MAINTENANCE ACTIVITY. 1 L 7 2 3T 4 T A14CE E2WE 6 C P40EA 1999120400095 19991204 00095 EA 1999 12 4 CA991103069 2 19991021 A 7230 BEARING EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL COMPRESSOR FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 21972 7498 56760101 56760101 BYA20862 (CAN) OIL FOUND CONTAMINATED, SUSPECT NR 1 BEARING. 1 L 7 2 4T 4 T A21SO E4EA 6 C P15EA 1999120400097 20010315 00097 NE 2001 3 15 CA991103088 2 19991020 A 7230 BEARING AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 3 ENGINE SPALLED W A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 CA 741810 (CAN) COMPRESSOR STALLED. REPORT TO FOLLOW. NR 4 BEARING FAILURE EXPERIENCED. TH E OUTER RACE WAS SPALLED. 2 L 7 4 4F 4 F RT A197 E37NE 1999120400098 20010315 00098 NE 2001 3 15 CA991103089 2 19991021 A 7230 BEARING AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 1 ENGINE SPALLED W E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 CA 741608 (CAN) N1 FAN SEIZED. REPORT TO FOLLOW. NR 4 BEARING FAILURE EXPERIENCED. 2 L 7 4 4F 4 F RT A197 E37NE 1999120400099 19991204 00099 NM 1999 12 4 CA991103096 1 19991004 A 7830 THRUST REVERSER BOEING 767 767275 1385155 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED W O OTHER J WARNING INDICATION LD LANDING 1 CA P709688 P709688 (CAN) SEPARATION OF THRUST REVERSER SLEEVE. MODIFIED SLEEVES INSTALLED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999120400100 19991204 00100 EA 1999 12 4 CA991104004 1 19991105 A 7931 601505197 TRANSDUCER CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE OIL PRESSURE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 59577532 (CAN) OIL PRESSURE INDICATION ON EICAS AND ENGINE OIL AURAL MESSAGE ANNUNCIATED. TRANSDUCER FAILED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999120400101 19991204 00101 GL 1999 12 4 CA991104013 2 19991020 A 7230 23064577D SCROLL BELL 407 407 SW ALLSN 250C 250C47B GL COMPRESSOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1679 CAE847124 CAE847124 (CAN) BRAIDED REINFORCED AREA OF SCROLL FOUND CRACKED. REINFORCEMENT AREA OF SCROLL FOUND CRACKED. REINFORCEMENT AREA ALSO DELAMINATED. THESE ITEMS PRESENTLY BEING ACTIONED BY ALLISON. 1 G 7 1 3U 3 U O H2SW E1GL 1999120400102 19991204 00102 SO 1999 12 4 CA991104014 1 19991021 A 3231 487933 SWITCH PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE3Y HCE3YR2 GL LT MLG DOOR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA L134861 DJ8071A (CAN) AFTER TAKEOFF, THE LANDING GEAR WAS SELECTED UP, THE GEAR HANDLE RETURNED TO NEUTRAL, BUT THE RED UNSAFE LIGHT REM AINED ILLUMINATED. THE LEFT DOOR MICROSWITCH WAS FOUND DEFECTIVE. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999120400104 19991204 00104 SO 1999 12 4 CA991104016 1 19991027 A 2710 09012007T265 BELLCRANK AYRES S2 S2RT34NORMAL 0970106 SO PWA PT6 PT6A34AG 52053 NE HARTZL HCB3T HCB3TN3 GL AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2480 PCE56682 BU10976 (CAN) CRACK FOUND IN AILERON BELLCRANK. BELLCRANK REPLACED. SUBMITTER STATED THIS IS THE THIRD OCCURRENCE FOR THE SAME BELLCRANK. 1 L 7 1 3T 4 T A3SW E4EA 6 C P15EA 1999120400105 19991204 00105 CE 1999 12 4 CA991112003 1 19991028 A 2720 07331151 BELLCRANK CESSNA 180 180J 2072622 CE CONT O470 O470R 17026 SO MCAULY 2A34C 2A34C203 GL RUDDER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 12347 451290 740807 (CAN) SEVERE CORROSION FOUND ON BOTTOM OF BELLCRANK UNDER THE CABLE ATTACHMENT CLEVIS. SUBMITTER STATED AIRCRAFT OPERAT ED IN SALT WATER ENVIRONMENT FOR OVER 12,000 HOURS. 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 1999120400106 19991204 00106 SO 1999 12 4 CA991112005 1 19991027 A 5280 466522 HINGE 4752930 PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL LT MLG DOOR BROKEN W O OTHER O OTHER LD LANDING 1 CA 7070 L723761A DJ8153A (CAN) WHEN LANDING GEAR WAS LOWERED CREW HEARD LOUD BANG! GEAR WAS INSPECTED AND FORWARD HINGE ON LEFT INBOARD GEAR DOO R WAS FOUND BROKEN. PART WAS THE NEW IMPROVED HINGE THAT PIPER PRODUCED TO REPLACE ORIGINAL HINGE S/B 682.AD 80-26-05 A ND S/B 682 C/W. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999120400107 19991204 00107 SO 1999 12 4 CA991112006 2 19991028 A 8530 653446A6 CYLINDER CESSNA 206 U206E 2073350 CE CONT O520 IO520F 17032 SO MCAULY 3A32C D3A32C90 GL ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1152 574060 574060 870232 (CAN) CYLINDER BORE EXIBITED EXCESSIVE WEAR RIDGE, OPERATOR SUSPECTS OVERHEAT IN THE PAST. 1 H 7 1 3O 3 O A4CE E5CE 5 C P21EA 1999120400108 19991204 00108 CE 1999 12 4 CA991112012 1 19991021 A 5511 0532001202 SPAR CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160DTM GL HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16804 RL3258827A 725226 (CAN) DURING SCHEDULED MAINTENANCE, THE HORIZONTAL STABILIZER FORWARD SPAR WAS FOUND CRACKED AROUND THE CENTER LIGHTENIN G HOLE. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999120400109 19991204 00109 CE 1999 12 4 CA991112013 1 19991028 A 2434 FIELD ROTOR FORD C6115010204 CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO SNSNCH 69CK 69CK EA ALTERNATOR SHEARED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 212 11685 11018A P9049 (CAN) DURING FLIGHT, THE CHARGING SYSTEM FAILED AND WOULD NOT RESET. AFTER LANDING, MAINTENANCE PERSONNEL DETERMINED TH AT THE ALTERNATOR FIELD ROTOR HAD SHEARED AFT OF THE FORWARD (DRIVE END) BEARING. 1 H 7 1 3O 3 O 3A19 E252 5 N P9045 1999120400110 19991204 00110 CE 1999 12 4 CA991112014 1 19991102 A 5711 MS20470AD5 RIVETS CESSNA 172 172P 2072436 CE LYC O320 O320D2J 41508 EA MCAULY 1C160 1C160DTM GL WING SPAR SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 9845 L1701539A FB050 (CAN) AFTER REMOVAL OF FUEL TANK, TWO RIVETS WERE FOUND SHEARED ON THE FRONT SPAR. THE RIVETS WERE LOCATED AT THE SPAR ANGLE (PN 0523017-14) AND THE INBOARD RIB (PN 0523010-14). 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999120400111 19991204 00111 CE 1999 12 4 CA991112017 1 19991101 A 7601 5485066 ACTUATOR WOODWARD CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ENGINE FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 3613 2481233J 71747 (CAN) ACTUATOR HAD EXCESSIVE DEAD BAND RANGE. 1 L 7 2 4F 4 F A22CE E1NE 1999120400112 19991204 00112 CE 1999 12 4 CA991112018 1 19991101 A 7601 5485066 ACTUATOR WOODWARD CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ENGINE FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 3493 245610H 71719 (CAN) ACTUATOR HAD EXCESSIVE DEAD BAND RANGE. 1 L 7 2 4F 4 F A22CE E1NE 1999120400113 19991204 00113 CE 1999 12 4 CA991112019 1 19991104 A 2730 556555026 SUPPORT ARM CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3613 71747 (CAN) DURING SCHEDULED MAINTENANCE, BOTH CONTROL COLUMN BOBWEIGHT SUPPORT ARMS FOUND DAMAGED. ONE ARM WAS FOUND CRACKED .3750 INCH FROM THE TOP FLANGE AND .50 INCH FORWARD OF THE ATTACH BOLT CENTERLINE. THE OTHER ARM WAS FOUND DEFORMED 1. 1250 INCHES FORWARD OF THE ATTACH BOLT AND WITH A SMALL .1250 INCH CRACK IN THE UPPER FLANGE. 1 L 7 2 4F 4 F A22CE E1NE 1999120400114 19991204 00114 CE 1999 12 4 CA991112020 1 19991031 A 7603 THROTTLE CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO MCAULY 1A102 1A102OCM GL ENGINE FAILED W B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 CA 3076 676657A 676657A QA002 (CAN) THROTTLE CONTROL HAD NO EFFECT ON RPM. OPERATOR COULD NOT FIND FAULT ON GROUND. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 1999120400115 19991204 00115 CE 1999 12 4 CA991112022 1 19991014 A 3233 ACTUATOR PHOENIX BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 7802 GGMPS0054 (CAN) AFTER SELECTING THE GEAR DOWN, THE NOSE GREEN LIGHT INDICATION DID NOT ILLUMINATE AND THE RED GEAR HANDLE INTRANSI T LIGHT ILLUMINATED. THE CREW COMPLETED AN EMERGENCY PROCEDURE AND THE AIRCRAFT LANDED SAFELY. AFTER INVESTIGATION, FO UND THE ACTUATOR TO BE THE PROBLEM. 2 L 7 2 4T 4 T RT A24CE E26NE 1999120400116 19991204 00116 CE 1999 12 4 CA991112023 1 19991016 A 3060 MS24166D1 RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PROP DEICE FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 8212 GGM114476 (CAN) AFTER THE ENGINE SHUTDOWN , THE RE-FUELER SAW SMOKE COMING OUT FROM ONE OF THE DE-ICER BOOTS ON THE NR TWO PROPELL ER. HE ADVISED THE CREW ABOUT THE SITUATION. THE CAPTAIN EXTINGUISHED THE FLAME WHILE THE COPILOT INITIATED THE EMERGE NCY PROCEDURE. MAINTENANCE REPLACED THE NR TWO PROPELLER ASSEMBLY AND THE FOLLOWING PARTS: K1 RELAY P/N 109-381002; K 2 RELAY P/N 24166-D1; AND THE PRESSURE SWITCH KS-9 (P/N 50-389121-51). SUBMITTER SUSPECTED K2 RELAY TO BE THE SOURCE O F THE PROBLEM. 2 L 7 2 4T 4 T RT A24CE E26NE 1999120400117 19991204 00117 SO 1999 12 4 CA991112025 1 19991101 A 2140 487898 SWITCH PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE2Y HCE2YR2 GL HEATER FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 8223 L161761 CJ505 (CAN) WHILE ON GROUND AND ENGINES RUNNING, HEATER WAS SELECTED ON. SMOKE AND SMELL EMANATED FROM UNDER THE INSTRUMENT P ANEL. MASTER SWITCH TURNED OFF-NO SMOKE. RE-ATTEMPT MASTER ON - HEATER FAN STARTED BY ITSELF WITH HEATER SWITCH TURN ED OFF PILOT FELT SWITCH TO BE HOT. UNPOPPED CIRCUIT BREAKER PULLED, MASTER ON, AIRCRAFT RETURNED TO BASE. SWITCH REPL ACED AND PROPERLY WIRED USING AM 36152 TERMINALS. 1 L 7 2 3O 3 O A20SO E14EA 5 C P9EA 1999120400118 19991204 00118 CE 1999 12 4 CA991112028 1 19991029 A 2701 24151521 CONTROL COLUMN LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P74114C (CAN) DURING SCHEDULED MAINTENANCE, A 2 INCH LONG CRACK WAS FOUND ON THE CONTROL COLUMN YOKE ASSEMBLY. THE CRACK RUNS F ROM THE BASE OF THE COVER, PN 2415165-1, DOWN THE INBOARD SIDE OF THE LEFT SIDE OF THE YOKE ASSEMBLY. 2 L 7 2 4F 4 F A10CE E6WE 1999120400119 19991204 00119 EA 1999 12 4 CA991112034 2 19991027 A 8530 LW12987 PISTON RING PARTEN P68 P68C 6780105 EU LYC O360 IO360A1B6 41514 EA HARTZL HCC2Y HCC2YK2 GL RT ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 961 49551 L2371751A AU7570 (CAN) RIGHT ENGINE PISTON RING FAILED. 1 H 7 2 3O 3 O A31EU 1E10 5 C P920 1999120400120 19991204 00120 CE 1999 12 4 CA991112035 1 19991101 A 3030 7270515 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PITOT HEATER FAILED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 80 PCEPS0276 (CAN) CREW REPORTED BURNING ODOR IN THE COCKPIT WHICH WOULD DISSIPATE AFTER A FEW MOMENTS. IT WAS NOTED THAT THE LEFT P ITOT HEATER CIRCUIT BREAKER HAD TRIPPED. INVESTIGATION FOUND ONE TERMINAL ON THE SELECTOR SWITCH WAS LOOSE AND SHOWED S IGNS OF EXCESSIVE HEAT. SWITCH REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 1999120400121 19991204 00121 CE 1999 12 4 CA991116002 1 19991104 A 3230 MS24171D1 RELAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG PITTED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 7699 4976 PCEPS0128 (CAN) THE LANDING GEAR WOULD NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN. MANUAL EXTENSION SELECTED, ALL GEAR LOCKS INDIC ATING GREEN. INSPECTION FOUND THE LANDING GEAR RELAY CONTACTS WERE PITTED AND ARCED. RELAY REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 1999120400122 19991204 00122 CE 1999 12 4 CA991116006 1 19991102 A 2720 8A08000032 CONTROL CABLE CESSNA 208 208 2073702 CE PWA PT6 PT6A114 52043 NE MCAULY 3AF34C 3GFR34C703 GL RUDDER FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 92 PCEPC0597 981667 (CAN) DURING DAILY INSPECTION, 4 WATER RUDDER CABLES WERE FOUND FRAYED. THE DAMAGE WAS ISOLATED TO THE AREA ABOVE THE S PREADER BAR WHERE THE CABLES TRANSITION TO THE AIRCRAFT FUSELAGE. SUBMITTER STATED THEY CONTACTED THE MANUFACTURER AND STATED A NUMBER OF OTHER OPERATORS HAD THE SAME PROBLEM AND SUSPECTED A BAD BATCH CABLE FROM THE VENDOR. 1 H 7 1 3T 3 T NT A37CE E4EA 5 C P60GL 1999120400123 19991204 00123 EA 1999 12 4 CA991116009 2 19991109 A 8530 LW11775 PISTON PLUG CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA MCAULY 1C160 1C160DTM GL ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 152 L57476T L57476T BE143 (CAN) METAL FLAKING OFF PISTON PIN PLUG. SIL 1267C ADDRESSES THIS ISSUE. NEW PART 72198. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999120400124 19991204 00124 EU 1999 12 4 CA991116010 1 19991102 A 3213 5321012175R STRUT PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE RT MLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1006 IL025 PCEPR0078 (CAN) THE RIGHT SHOCK DEVELOPED AN INTERNAL NITROGEN LEAK THAT WAS CAUSED BY A FEELER GAUGE BEING LEFT IN THE SHOCK STRU T DURING THE ASSEMBLY/MANUFACTURING PROCESS. 1 L 7 1 3T 4 T RT A78EU E26NE 1999120400125 20010307 00125 NM 2001 3 7 CA991116011 1 19991104 A 7921 PLATE PWA 6A47000 BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE OIL COOLER MISSING W O OTHER O OTHER NR NOT REPORTED 1 CA 0495 (CAN) PLATE SEPARATED FROM CSD OIL COOLER AT START UP.THIS WAS AN ACESS PANEL WE RE THE HINGED PORTION HAD BROKEN ALLOWI NG SEPARATION. 2 L 7 2 4F 4 F A16WE E2EA 1999120400126 19991204 00126 EU 1999 12 4 CA991116012 1 19991113 A 2920 762973 BLADE AIRBUS 330 A330322 3930325 EU PWA 4168 PW4168 NE RAM AIR TURBINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15836 0202 733336 (CAN) DURING ROUTINE INSPECTION OF RAM AIR TURBINE, SCRATCH FOUND ON BLADE ROOT. FURTHER INVESTIGATION REVEALED A CRACK . THE SUBMITTER INDICATED THAT THERE IS NO SPECIFIC INSPECTION TASK CALLING UP THE INSPECTION OF THE RAM BLADES. 2 L 7 2 4F 4 F RT A46NM E36NE 1999120400127 19991204 00127 NM 1999 12 4 CA991116013 1 19991112 A 2120 396401 FLOW VALVE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE RT PACK FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 30886 (CAN) AIRCRAFT RETURNED DUE UNABLE TO PRESSURIZE. AFT CABIN DOOR SEAL FOUND ADRIFT. LEFT PACK UNDER MEL UNABLE TO PRES SURZIZE. REPLACED RIGHT PACK FLOW CONTROL VALVE. 2 L 7 2 4F 4 F RT A2NM E12EU 1999120400128 19991204 00128 NE 1999 12 4 CA991116014 2 19991104 A 7220 NR 1 BEARING LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE LEAKING W C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CA 10459 10459 (CAN) ENGINE EXPERIENCED HIGH VIBRATIONS ON TAKEOFF. OIL FOUND IN SPINNER. OPERATOR SPECIFIED THAT THIS IS A KNOWN PRO BLEM BUT HAPPENS VERY INFREQUENTLY. OIL IS PROPAGATING FROM NR 1 BEARING UNDER CERTAIN CONDITIONS. 2 L 7 3 4F 4 F A23WE E12EU 1999120400129 19991204 00129 NM 1999 12 4 CA991116021 1 19991103 A 3230 CONNECTOR BOEING 737 7372E1 138448F NM PWA JT8 JT8D9A 52048 NE AGU CONTAMINATED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 654487 (CAN) LEFT MLG GREEN LIGHT REMAINED ON AFTER RETRACTION. AIRCRAFT RETURNED. SUBMITTER SUSPECTED SNOW ON ACCESSORY GEAR UNIT CONNECTOR. DRIED OUT AND CLEANED. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1999120400130 19991204 00130 NM 1999 12 4 CA991116022 1 19991103 A 2130 SENSE LINE BOEING 737 7372A9C 1384495 NM PWA JT8 JT8D9A 52048 NE CABIN PRESSURE LOOSE W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 674318 (CAN) CABIN ALTITUDE WARNING HORN WAS ON DURING FLIGHT AND THE CABIN CLIMBED TO 10,000 FEET WITH 5.0 PSID. THE DUCT PRE SSURE WAS 24 AND 26 PSID. AIRCRAFT RETURNED. SENSE LINE LOOSE AT LEFT PACK CONTROL VALVE. TIGHTENED LINE. AIRCRAFT S ERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1999120400131 19991204 00131 NM 1999 12 4 CA991116023 1 19991103 A 2910 65468581103 LINE BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 648850 (CAN) LOSS OF ALL NR 2 HYDRAULIC FLUID IN-FLIGHT. PIN HOLE IN LINE AT PYLON UNDER CLAMP. REPLACED NR 2 HYDRAULIC PUMP AND CASE DRAIN FILTER REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999120400132 19991204 00132 CE 1999 12 4 CA991116024 1 19991108 A 2701 55655026 ARM CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BOBWEIGHT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2939 71721 (CAN) DURING SCHEDULED MAINTENANCE, THE CONTROL COLUMN BOBWEIGHT SUPPORT ARM WAS FOUND CRACKED. INSPECTION CARRIED OUT PER COMPANY CAMPAIGN NOTICE ISSUED IN RESPECT OF 3 PREVIOUS OCCURRENCES. 1 L 7 2 4F 4 F A22CE E1NE 1999120400133 19991204 00133 EU 1999 12 4 CA991116026 1 19991104 A 2540 PANEL AIRBUS 310 A310304 EU LAVATORY LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) PANEL FORWARD OF RIGHT ACU INTAKE FOUND DAMAGED. SUBMITTER SUSPECTED ICE BUILD-UP FROM LAVATORY SERVICE PANEL WHI CH WAS LEAKING AT ONE DROP PER SECOND. LEAK REPAIRED, PANEL REPAIRED. 2 L 7 2 4F RT A35EU 1999120400134 19991204 00134 EU 1999 12 4 CA991116027 1 19990515 A 2430 10200311 GCU AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE ENGINE FAILED W H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 CA 813115 120788 890218 (CAN) GCU CONTACTOR FAILED. REPLACED. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999120400135 19991204 00135 NM 1999 12 4 TWAA9916001 1 19991125 A 3350 6104783 BATTERY PACK BOEING 727 727231 1384079 NM AIRSTAIR DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54345 21632 THE AFT AIRSTAIR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 8-8-99 MCI. 2 L 7 3 4F A3WE 1999120400136 19991204 00136 NM 1999 12 4 TWAA9916002 1 19991124 A 3350 LIGHT BOEING 767 767231 1385131 NM CABIN CONTAMINATED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 607TW 22570 FOUND EGRESS LIGHTS DIM AT THE MID GALLEY CROSSOVER AND THE FORWARD RT SIDE OF COACH. FOUND WATER IN THE EGRESS STRIP. DRIED AREA AND REPLACED WET BULBS AND STRIP. CHECK-C 10-20-99 LAX. 2 L 7 2 4F RT A1NM 1999120400137 19991204 00137 WP 1999 12 4 TWAA9916003 1 19991105 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 184 - 228 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING OP 16 MAINT CHECK, THE FWD SERVICE DOOR CUSP ANGLE WAS CORRODED BETWEEN STA 190 TO 220. INSTALLED NEW SECTION OF CUSP ANGLE FROM STA 184 TO FACTORY SPLICE AT STA 228 PER SPM 6-70-01. INSTALLED SPLICE REPAIR AT STA 184 PER SRM 53-05 . 2 L 7 2 4F A6WE 1999120400138 19991204 00138 WP 1999 12 4 TWAA9916004 1 19991105 A 5320 TIE DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING OP 16 MAINT CHECK, FOUND CORRODED FORMER TIE AT STA 200, FORMER TO LONGERON 18R. INSTALLED NEW FORMER TIE FITTIN G AT STA 200 PER SPM 6-70-01. 2 L 7 2 4F A6WE 1999120400139 19991204 00139 WP 1999 12 4 TWAA9916005 1 19991110 A 5744 FITTING DOUG DC9 DC931 3022065 WP WS 164 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING OP 16 MAINT CHECK ON RT WING THE I/B FLAP HINGE CASTING AREA XRS 164 HAD LOWER O/B HOLE CRACKED AT 12 O'CLOCK POS ITION. CRACK WAS STOP DRILLED AND NDT CHECKED FOR CRACK CONTAINMENT. DOUBLERS INSTALLED PER DOUGLAS DRAWING JO 60271. 2 L 7 2 4F A6WE 1999120400140 19991204 00140 WP 1999 12 4 TWAA9916006 1 19991110 A 5744 FITTING DOUG DC9 DC931 3022065 WP WS 164 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING OP 16 MAINT CHECK, THE RT WING I/B FLAP HINGE CASTING AREA XRS 164, I/B LOWER HOLE IN REAR SPAR HAD 2 CRACKS APPR OXIMATELY 1.25 AND .5 INCH LONG. CRACKS WERE STOP DRILLED AND NDT CHECKED FOR CRACK CONTAINMENT. DOUBLERS WERE INSTALL ED PER DOUGLAS DRAWING JO 60271. 2 L 7 2 4F A6WE 1999120400141 19991204 00141 WP 1999 12 4 CALA9901532 1 19991124 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG DISCHARGED A CALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 09 14880 48044 THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR WAS EXTENDED AND ALL THREE GEAR GREEN LIGHTS WERE INDI CATED. THE AIRCRAFT WAS RETURNED TO EWR. CREW NOTICED GEAR HANDLE RELEASE BUTTON WAS IN. THE BUTTON POPPED OUT WITH N OSE GEAR TOUCHDOWN. A FULL NOSE GEAR STRUT SERVICING WAS PERFORMED IAW MM 32-21-02. IN ADDITION, THE NOSE GEAR UPPER T ORQUE LINK WAS REPLACED DUE TO WEAR AND THE GROUND SENSING CABLES WERE ADJUSTED IAW MM 32-23-01. THE GEAR WAS SWUNG AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999120400142 19991204 00142 WP 1999 12 4 CALA9901533 1 19991124 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R AT BELTFRAME 1418. REPAIRED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1999120400143 19991204 00143 WP 1999 12 4 CALA9901534 1 19991124 A 5311 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16892 49391 INSPECTION FOUND A 1.125 CRACK IN LONGERON 2L AT BELTFRAME 1418. REPAIRED IAW ECRA 5310-03950. 2 L 7 2 4F A6WE 1999120400144 19991204 00144 NM 1999 12 4 CALA9901535 1 19991125 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 294.5, RBL 54 TO LBL 24. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999120400145 19991204 00145 NM 1999 12 4 CALA9901536 1 19991127 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 211 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13331 23569 INSPECTION FOUND A .5 INCH CRACK IN SKIN OF CAPTAIN'S SLIDING WINDOW FORWARD UPPER FRAME AT STA 211. A DOUBLER REPAIR W AS INSTALLED IAW ECRA 5330-02833. 2 L 7 2 4F RT A16WE 1999120400146 19991204 00146 NM 1999 12 4 CALA9901537 1 19991128 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND RT AND LT AFT LAV FLOORBEAMS CORRODED AT STA 1016, RBL 6.5 AND LBL 28. THE FLOORBEAM UPPER CHORD SECTI ONS WERE REPLACED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999120400147 19991204 00147 NM 1999 12 4 CALA9901538 1 19991124 A 5330 SKIN BOEING 737 7373T0 1384582 NM WINDOW FRAME CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND A 1 INCH CRACK IN CAPTAIN'S L-1 WINDOW FRAME SKIN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02833. 2 L 7 2 4F RT A16WE 1999120400148 19991204 00148 NM 1999 12 4 CALA9901539 1 19991128 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 344 FROM RBL 18 TO LBL 48. A NEW FLOORBEAM UPPER CHORD WAS INSTALLED I AW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1999120400149 19991204 00149 NM 1999 12 4 CALA9901540 1 19991129 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328 - 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 328-344, RBL 42. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52, FIGURE 202 AND 51-40-02. 2 L 7 2 4F RT A16WE 1999120400150 19991204 00150 EU 1999 12 4 QXEA9902356 1 19991121 A 3350 6008903 POWER SUPPLY GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 497US 11167 BOI- EXIT SIGNS IN GALLEY AND CABIN ARE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN POWER SUPPLIES, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999120400151 19991204 00151 WP 1999 12 4 ABXA9900806 1 19991126 A 3260 6222262060 SWITCH DOUG DC8 DC863 302198A WP RT MLG CORRODED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 813AX 46136 RIGHT MAIN LANDING GEAR DOWN LIGHT (GREEN) DID NOT ILLUMINATE AFTER GEAR EXTENSION. RED UNSAFE LIGHT DID NOT ILLUMINATE . RECYCLED LANDING GEAR, RIGHT GEAR LIGHT CAME ON. REPLACED MAIN GEAR DOWNLOCK SWITCH IAW DC8 MM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999120400152 19991204 00152 WP 1999 12 4 DLL19992546 1 19991118 A 2120 UNKNOWN LKHEED 1011 10113853 5265020 WP CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 755DL 193Y1184 NUMEROUS COMPLAINTS OF SMOKE ODOR IN CABIN. INSPECTED CABIN AND GALLEYS FOR FAULTS AND FOUND NONE. OPERATED AIR CONDIT IONING SYSTEM FOR 30 MINUTES WITH NO FAULTS. UNABLE TO IDENTIFY SOURCE OF ODOR. ALL CHECKS NORMALLY. 2 L 7 3 4F A23WE 1999120400153 19991204 00153 NM 1999 12 4 DL72S992550 1 19991118 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 534DA 22047 R-1 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NOW OK. 2 L 7 3 4F A3WE 1999120400154 19991204 00154 NM 1999 12 4 DL767992553 1 19991120 A 2910 V730144 MODULE BOEING 767 767232 1385132 NM RT MLG WW CRACKED A DALA O OTHER K FLUID LOSS LD LANDING 1 SO 27 101DA 730144R28 22213 ON TOUCHDOWN, LOST CTR HYD SYS AND INTERMITTENT BRAKE VLV LIGHT WITH ALT SELECTED. RES BRAKE VLV EICAS MSG. CTR HYD SY S SHOWS .09 RF. NO RES BRAKE OR OR STEERING. BRAKE SOURCE LIGHT ON. C/ MTC IN PROG. RAT MODULE REPLACED. 2 L 7 2 4F RT A1NM 1999120400155 19991204 00155 NE 1999 12 4 DL757992554 2 19991120 A 7240 ENGINE PW2037RTC BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 27 667DN 20370308 25035 716544 ON CLIMBOUT, HEARD LOUD BANG ON LEFT SIDE OF A/C. THE LEFT ENGINE HAD TEMP ROLLBACK THEN ALL ENGINE INDICATION RETURNED TO NORMAL. THE FLT ATTENDANTS SAW A YELLOW FLASH DOWN THE LEFT SIDE OF THE A/C. INSPECTED AND RUN TESTED ENGINE. REP LACED EEC. 2 L 7 2 4F 4 F RT A2NM E17NE 1999120400156 19991204 00156 NM 1999 12 4 DL73K992555 1 19991120 A 4950 BLEED LINE BOEING 737 737232 1384475 NM APU LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 325DL 23097 SOLID WING BODY OVERHEAT LIGHT PASSING 1,500 FT, AFTER TAKEOFF. AFTER COMPLETING PROCEDURES, LIGHT REMAINED ON. RETURN ED TO DEPARTURE AIRPORT AND LANDED. A/C GROSS WEIGHT UPON LANDING 112,000 LBS. FOUND BLEED LEAK FWD OF APU BLEED VALV E. REPLACED GASKETS, CLEANED SENSE LOOP. 2 L 7 2 4F RT A16WE 1999120400157 19991204 00157 1999 12 4 DL757992556 4 19991120 A 3160 43467410312257 LIGHT BOEING 757 757232 1384965 NM COCKPIT FAILED A DALA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 633DL 23614 ELECTRICAL SMELL IN COCKPIT FOLLOWED BY SMOKE COMING FROM FWD GLARESHIELD. PWR REMOVED FROM AIRCRAFT WHICH CAUSED SMOKE TO DISSIPATE. FOUND BRAKE SOURCE LIGHT ASSY BURNED. REPLACED WIRE CONNECTORS AND LIGHT ASSY. NO DAMAGE TO SURROUNDIN G ASSYS. LIGHT OPS CKS NORMAL. MRR PARTS SENT AND PARTS ROUTED TO ATL DEPT 595 FAA LAISON. 2 L 7 2 4F RT A2NM 1999120400158 19991204 00158 NM 1999 12 4 DLM11992557 1 19991121 A 3397 WIRE DOUG MD11 MD11 3023602 NM SEAT 13 A FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 802DE 48473 SLIGHT ARCING WITH FIRE SEAT 13A CAUSED BY PINCHED READING LIGHT CABLE UNDER SEAT CUSHION PAN. REMOVED PWR FROM CABLE T O LIGHT RENDERED LIGHT INOP. FOUND BY MTC. 2 L 7 3 4F RT A22WE 1999120400159 19991204 00159 NE 1999 12 4 DL767992558 2 19991121 A 7200 ENGINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE RIGHT FAILED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 115DA 24724 8433 580400 22227 580400 ON TAKOFF ROLL, RT ENG COMPRESSOR STALL AND EGT WENT TO 1081 DEG CELSIUS. ICING CONDITIONS PRESENT, ANTI ICE ON. ENGIN E HAD METAL IN TAILPIPE ON GATE RETURN. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 1999120400160 19991204 00160 NM 1999 12 4 DL72W992559 1 19991121 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2821W 21059 AFT CABIN DOOR EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999120400161 19991204 00161 NM 1999 12 4 DL72W992560 1 19991121 A 3350 S106 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2821W 21059 R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1999120400162 19991204 00162 NM 1999 12 4 DL72W992561 1 19991121 A 3350 S106 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2821W 21059 ROW 28 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1999120400163 19991204 00163 NM 1999 12 4 DL733992563 1 19991121 A 2130 CONTROLLER BOEING 737 737301 1384611 NM CABIN PRESSURE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 948WP 23259 PRESSURIZATION LOST AFTER T/O FROM COS. UNABLE TO REGAIN PRESSURATION ANY CONFIGURATION. CHECKED ALL DOORS, RAN ENGS A ND PACKS ON GROUND. ACFT PRESSURIZATION NORMAL. 2 L 7 2 4F RT A16WE 1999120400164 19991204 00164 WP 1999 12 4 DLL10992564 1 19991121 A 2910 FILTER MODULE 15056006139 LKHEED 1011 10113851 5265010 WP HYD SYSTEM LEAKING A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 1732D 0943 193C1213 ON TAXI, IN BRAKE PRESSURE LOST B SYSTEM PRESSURE LOW AND QTY LESS THAN 1/4 NORMAL BRAKES ACCUMULATOR PRESSURE LOW. FOU ND HIGH PRESSURE FILTER MODULE LEAKING FROM WEEP HOLE. REPLACED HI PRESS FILTER MOD PER M/M (P/N 297001913) (S/N 0943) OFF (S/N 0715) LOG NUMBER C346311001. 2 L 7 3 4F A23WE 1999120400165 19991204 00165 NM 1999 12 4 DL76S992565 1 19991115 A 5330 143T322110 SKIN BOEING 767 767332 1382001 NM BS 500 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 138DL 25409 DAMAGE TO SKIN AND TEAR STRAP AT STA 500 BETWEEN STRINGERS 38L AND 39L. DAMAGE CONSISTS OF DENTS AND GOUGES BEYOND SRM LIMITS. ERA 333770-14 REV A. 2 L 7 2 4F RT A1NM 1999120400166 19991204 00166 NM 1999 12 4 DL76S992566 1 19991115 A 5330 146T33414 SKIN BOEING 767 767332 1382001 NM BS 1560 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 138DL 25409 SKIN DENTED BEYOND SRM LIMITS AT STA 1560 BETWEEN STRINGERS 20L AND 21L. ERA 333757-14 REV A. 2 L 7 2 4F RT A1NM 1999120400167 19991204 00167 NM 1999 12 4 DL76S992567 1 19991118 A 5330 141T32316 SKIN BOEING 767 767332 1382001 NM BS 368 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 138DL 25409 SKIN AND STRINGER DAMAGED AT STA 368 AND STRINGER 33R. DAMAGE CONSISTS OF DENTED SKIN AND CRACKED STRINGER. ERA 333785 -14. 2 L 7 2 4F RT A1NM 1999120400168 19991204 00168 NM 1999 12 4 DL72S992568 1 19991116 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 A .375 INCH CRACK LT VERTICAL TORQUE BOX WEB AT UPPER END STA 1223 (MARKED). REPAIRED PER MM 53-11-0 PAGE 832. 2 L 7 3 4F A3WE 1999120400169 19991204 00169 NM 1999 12 4 DLM88992569 1 19991122 A 5330 29525001 SKIN DOUG MD88 MD88 3023688 NM BS 313 - 351 DENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 919DL 49584 THREE DENTS WERE FOUND IN THE FUSELAGE SKIN FROM FS 313 TO 351 BETWEEN L21R AND L22R. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333828-14. 2 L 7 2 4F RT A6WE 1999120400170 19991204 00170 NM 1999 12 4 DL72E992570 1 19991122 A 5532 65174633 SKIN BOEING 727 727247 138408F NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 THE SKIN OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FUSELAGE CREASE LINE AND STRINGER 10L. THE DAMAGE WAS FOUN D AT HMV AND REPAIRED PER ERA 333830-14AD. 2 L 7 3 4F A3WE 1999120400171 19991204 00171 NM 1999 12 4 DLM88992571 1 19991122 A 5330 592480296 SKIN DOUG MD88 MD88 3023688 NM BS 229 - 245 DENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 922DL 49646 THE FUSELAGE SKIN WAS FOUND DENTED AT FROM FS 229 TO 245 BETWEEN L16L AND L18L. THE DAMAGE WAS FOUND AT HMV AND REPAIRE D PER ERA 333836-14. 2 L 7 2 4F RT A6WE 1999120400172 19991204 00172 NM 1999 12 4 DL72E992572 1 19991122 A 5532 65237489 SKIN BOEING 727 727247 138408F NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 A CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN, LEFT HAND SIDE, WHERE THE SKIN MEETS THE UPPER TORQUE BOX AT APPROX F S 1210. THE DAMAGE WAS FOUND DURING HMV AND REPAIRED PER ERA 333807-14. 2 L 7 3 4F A3WE 1999120400173 19991204 00173 NM 1999 12 4 DL72E992573 1 19991122 A 5330 651768339 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 A 1.5 CRACK WAS FOUND IN THE L1 DOOR SURROUND STRAP. THE DAMAGE WAS FOUND DURING HMV AND REPAIRED PER ERA 333818-14. 2 L 7 3 4F A3WE 1999120400174 19991204 00174 NM 1999 12 4 DL72S992574 1 19991120 A 5320 6516350380 BEAM BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 THE RBL 17.8 VERTICAL DOOR BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A SMALL CRACK IN A FASTENER HOLE COMMON TO AN EXI STING REPAIR. THE CRACK WAS REMOVED BY OVERSIZING THE .0625 INCH FASTENER HOLE TO .296 DIA WITH AN ADDITIONAL .0625 OVE RSIZE. THE CRACK WAS FOUND WITH A BOLT HOLE EDDY CURRENT INSPECTION AND IS OUTSIDE THE CRACK AREA OF AD 99-18-05. THE HOLE WAS BUSHED AND REPAIR RE-INSTALLED PER ER/A 368793-14. 2 L 7 3 4F A3WE 1999120400175 19991204 00175 NM 1999 12 4 DL72W992575 1 19991120 A 5753 6519270 SHIM BOEING 727 727247 138408F NM RH FLAP TRACK LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 DURING INSPECTIONS OF THE I/B FLAP TRACK FOR THE RT I/B FLAP REQUIRED PER AD 90-07-05, THE EXISTING LAMINATED SHIM WAS F OUND TO HAVE MIGRATED .375 INCH. THE SHIM WAS REMOVED AND REPLACED PER THE REQUIREMENTS OF BAC S/B 727-57-0178 AND THEA D. THE WORK WAS ACCOMPLISHED PER ER/A 368797-14AD. 2 L 7 3 4F A3WE 1999120400176 19991204 00176 WP 1999 12 4 DLL14992576 1 19991119 A 5330 1608989163 SKIN LKHEED 1011 1011385115 5265015 WP BS 1715 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 737D 193C1228 THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION BETWEEN FS 1710 & 1720 AT STRINGER 39. THE CORROSION WAS CENTERED AROUND THE EXISTING TITANIUM TEAR STRAP. THE CORROSION WAS CUT OUT OF THE SKIN WITH A 8 X 4 CUTOUT AND REPAIRED WITH A N EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 368769-14, REV A. 2 L 7 3 4F A23WE 1999120400177 19991204 00177 NM 1999 12 4 DL76G992577 1 19991122 A 2121 FAN BOEING 767 7673P6 1385105 NM CARGO BAY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 156DL 25354 FWD EQUIP EX FAN STATUS MSG PRECEDED BY SOUND OF MOTOR WINDING DOWN AND SMOKE IN COCKPIT. C/B H-20 OPENED/POPPED. SMOK E DISSIPATED. 2 L 7 2 4F RT A1NM 1999120400178 19991204 00178 NM 1999 12 4 DL72S992578 1 19991122 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 4 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 COVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999120400179 19991204 00179 NM 1999 12 4 DL72S992579 1 19991122 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 COVE SKIN ANGLE CRACKED NR 3 SLAT I/B OF ACTUATOR ROD END REPAIR PER MM 57-54-0. 2 L 7 3 4F A3WE 1999120400180 19991204 00180 NM 1999 12 4 DL757992580 1 19991122 A 4920 331200 APU BOEING 757 757232 1384965 NM APU BAY FAILED A DALA O OTHER Y ENGINE STOPPAGE AP APPROACH 1 SO 27 664DN 31790 25012 P137 APU SHUT DOWN ON APPROACH. RT ENGINE GENERATOR INOP AND ON MCO. ALSO, HAD APU OIL QTY STATUS MSG DURING FLIGHT. SERVI CED APU OIL QUANTITY AND LEAK CHECKED APU. 2 L 7 2 4F RT A2NM 1999120400181 19991204 00181 NM 1999 12 4 DL72S992582 1 19991122 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 LOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 6 SLAT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812 & ERA 368813-14. 2 L 7 3 4F A3WE 1999120400182 19991204 00182 NM 1999 12 4 DL72L992584 1 19991123 A 5330 655456512 SKIN BOEING 727 727232 1384082 NM BS 500 & 520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 CORROSION WAS FOUND IN THE STR 26R LAP JOINT BETWEEN FS 500 AND 520. THE DAMAGE WAS REPAIRED PER ERA 333773-14AD AT HMV . 2 L 7 3 4F A3WE 1999120400183 19991204 00183 NM 1999 12 4 DL73E992585 1 19991123 A 2130 REGULATOR VALVE 363001144 BOEING 737 737247 138448D NM NR 2 ENGINE FAILED A DALA I CABIN DEPRESSURIZATION J WARNING INDICATION CL CLIMB 1 SO 27 377DL 3266 23604 WHILE PASSING THROUGH FL230 CABIN ALT WAS NOTED TO BE APPROX 10,000 FT AND CLIMBING 1,000 FT/SEC. A/C LEVELED AT FL230 WITH CABIN CLIMBING. DESCENDED A/C AND SWD TO MAN DC CONTROL. OUTFLOW VLV INDICATED FULL CLOSED. MAN CONTROL CLOSED O NE MORE NEEDLE WIDTH TO FULL CLOSED AND CABIN CONTROL WAS REGAINED. WHILE T/S FOUND CK VLV AND HP REG VLV BAD, NR 2 ENG . BOTH ITEMS REPLACED AND PERFORMED CK OUT PER MM 21-11-0 PG 504. ALL OPS AND INDICATIONS NORMAL. 2 L 7 2 4F A16WE 1999120400184 19991204 00184 NM 1999 12 4 DL76G992586 1 19991123 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1602 29694 FIRST SECTION OF COACH RT SIDE EMERGENCY TRACK LIGHTS INOP. FOUND WIRE SHORTED AT ROW 30. REPAIRED WIRE, OPS NORMAL. 2 L 7 2 4F RT A1NM 1999120400185 19991204 00185 NM 1999 12 4 DL72W992587 1 19991123 A 5720 STIFFENER BOEING 727 727247 138408F NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 A 1 INCH CRACK WING L/E SPAR STIFFENER O/B SIDE OF I/B TRACK BOX NR 4 SLAT. REPLACED SPAR STIFFENER PER MM 57-20-21. 2 L 7 3 4F A3WE 1999120400186 19991204 00186 WP 1999 12 4 DLL19992588 1 19991123 A 3350 LIGHT 5165741 LKHEED 1011 10113853 5265020 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 37062 193H1216 C-ZONE EMERGENCY LIGHT FAILED L/O TEST. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1999120400187 19991204 00187 NM 1999 12 4 DL72W992589 1 19991123 A 5754 STIFFENER BOEING 727 727247 138408F NM SLAT TRACK CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 L/E SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK I/B STIFFENER. REPLACED PER M/M 57-20-21 PG 813 {NR 6 SLAT}. 2 L 7 3 4F A3WE 1999120400188 19991204 00188 NM 1999 12 4 DL72S992591 1 19991123 A 3350 10617844 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 3315 21223 DURING L/O CHECK, FOUND SVL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTS AND PACKS, ALL CHECK OK. 2 L 7 3 4F A3WE 1999120400189 19991204 00189 NM 1999 12 4 DL72S992592 1 19991121 A 3350 LIGHT 10617839 BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 495DA 1912 21075 EMERGENCY EXIT SIGN TOO DIM TO SEE ON EMERGENCY PWR TEST. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1999120400190 19991204 00190 NM 1999 12 4 DL72S992593 1 19991121 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 516DA 8837 21432 AFT CABIN EMERGENCY EXIT SIGN OVERHEAD INOP DURING LIGHTS TEST. REPLACED BATTERY PACK, OPS GOOD. 2 L 7 3 4F A3WE 1999120400191 19991204 00191 NM 1999 12 4 DL72W992594 1 19991008 A 5753 652163585 SKIN BOEING 727 727247 138408F NM TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 INBOARD L/E DENTED AND WORN. REPAIRED ON SHOP ORDER 927514 PER M/M 57-52-0 FIG 803 {FLAP SHOP}. 2 L 7 3 4F A3WE 1999120400192 19991204 00192 NM 1999 12 4 DL757992595 1 19991124 A 3350 CONTROLLER 233T321028 BOEING 757 757232 1384965 NM EMERGENCY LIGHTS MALFUNCTIONED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 601DL D00207 22808 CABIN EMERGENCY EXIT LIGHT CAME ON INTERMITTENTLY. REPLACED CONTROL PANEL. 2 L 7 2 4F RT A2NM 1999120400193 19991204 00193 NM 1999 12 4 DL757992596 1 19991124 A 2120 SMOKE ODOR BOEING 757 757232 1384965 NM E/E BAY DETECTED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 610DL 22817 PASSING APPROX 10,000 FT FWD EQUIPMENT SMOKE EICAS, NOTICED CAUSTIC ELECTRICAL SMELL, BEGAN SMOKE AND FIRE PROCEDURE. E QUIPMENT OVERHEAT CAME ON IMMEDIATLY. DECLARED AN EMERGENCY AND REQUESTED APPROACH CLEARANCE. WENT TO EQUIP COOLING AL T, COMPLIED WITH PROCEDURE. NO VISABLE SMOKE, SMELL ONLY. SMOKE LIGHT ON OVERHEAD ALSO CAME ON. REPLACED SMOKE DETECT ORS. 2 L 7 2 4F RT A2NM 1999120400194 19991204 00194 1999 12 4 DL76G992597 4 19991123 A 2565 SQUIB BOEING 767 7673P6 1385105 NM SLIDE FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1501P 24983 DURING L/O CHECK, RT OVERWING SLIDE SQUIB FAILED TO TEST. DURING T/S SLIDE WAS BLOWN. A/C WAS FERRIED ON FLT 9933/24 T O REPLACE SLIDE AND WORK ON SQUIB SYS. 2 L 7 2 4F RT A1NM 1999120400195 19991204 00195 NM 1999 12 4 DLM88992599 1 19991124 A 2150 SEPARATOR BAG 20495061 DOUG MD88 MD88 3023688 NM CABIN COOLING FAULTY A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 902DL 3512163 49533 STRONG SMOKE ODOR IN AIRCRAFT. AFT SMOKE DET WENT OFF. REPLACED RT ACM PER M/M, PERFORMED DUCT BURN OUT. REPLACED WAT ER SEPARATOR BAG, LEAK CKS GOOD. 2 L 7 2 4F RT A6WE 1999120400196 19991204 00196 NE 1999 12 4 DL76L992600 2 19991125 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RIGHT STALLED A DALA C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 SO 27 183DN 25786 27110 724691 FLT 47 ARN/JFK AIR TURNBACK, DUE RT ENG STALLED TWICE ON ROTATION A/C LANDED HEAVY. FUEL WAS NOT DUMPED. RT FWD BRAKE O VERHEATED AND HAD A SMALL FIRE. FIRE WENT OUT BY ITSELF WITH NO DAMAGE TIRES DID NOT DEFLATE. RT ENG EGT WENT TO 758 FOR 17 SECS. ENG CHANGE WAS CALLED. ETOPS CATEGORY 'C': UNC OMMANDED PWR CHANGES,SURGES,OR STALLS 2 L 7 2 4F 4 F RT A1NM E24NE 1999120400197 19991204 00197 NM 1999 12 4 DL72S992601 1 19991125 A 2530 OVEN BOEING 727 727232 1384082 NM GALLEY CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 403DA 21147 FORWARD GALLEY WORK LIGHT C/B POPPED. F/A REPORTED LIGHT PLASTIC SMELL. NO SMOKE NOTED. BREAKER WAS NOT RESET. ON CHE CK, FOUND GALLEY WORK LIGHT C/B POPPED AND COLLARED BY PREVIOUS ENG ORDER. CHKD OPS OF OVENS, COFFEEMAKER. ALL ELEC OP ERATIONS NORMAL. FOUND MASKING TAPE ON OVEN INSERT/CARRIER. REMOVED CARRIER AND OPD OVEN AGAIN, NO ODOR NOTED. AGAIN ALL ELECTRIC OPERATION WAS NORMAL. 2 L 7 3 4F A3WE 1999120400198 19991204 00198 NE 1999 12 4 DL72W992604 2 19991123 A 7200 ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 MALFUNCTIONED A DALA J A DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 2812W 68005 20868 687512 DURING T/O, NR 1 THROTTLE HAD TO BE ADVANCED BEYOND NORMAL POS TO ATTAIN T/O EPR, EGT AND N2 WERE IN CAUTION RANGE FOR N R 1 ENG & N1 WAS LOWER THAN NR 2 & NR 3 ENG. DUCT PRESS ON LT SIDE WAS 30 PSI ON RT 68 PSI. AFT F/A HEARD WHAT SOUNDE D LIKE A BACKFIRE ON T/O. DUMPED FUEL TO 21,000 LBS TO NEEDED WT. ON SHORT FINAL HEARD POPPING SOUNDS AGAIN. ENG REPL ACED. 2 L 7 3 4F 4 F A3WE E2EA 1999120400199 19991204 00199 1999 12 4 DLM88992605 4 19991125 A 3460 COMPUTER HG1103BA01 DOUG MD88 MD88 3023688 NM FLIGHT MANAGE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 917DE 104 49958 CLIMBOUT OF EWR TOTAL IRU FAIL LIGHTS. LOSS OF NAVIGATION PLATFORM, NO HEADING. REPLACED NR 1 IRU, ALIGNED BOTH IRUS. SYS CK GOOD PER MM. 2 L 7 2 4F RT A6WE 1999120400200 19991204 00200 NM 1999 12 4 DL72S992607 1 19991125 A 5210 SEAL BOEING 727 727225 1384077 NM PAX DOOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 805EA 22436 AIRCRAFT WOULD NOT HOLD SCHEDULED CABIN PRESSURE WITH SINGLE PACK OPS AT FL 210. CABIN WAS 8000 FT, CLIMBING 500-700 FE ET PER MIN. DESCENDED TO 15,000 TO HOLD LEVEL AT 8000 FEET CABIN PRESSURE. PRESSURIZED ACFT. FOUND AIR LEAKS AT L-1 A ND R-1 DOOR SCUFF PLATES. REPAIRED PLATES AND SEALS ON BOTH DOORS. REPLACED RIGHT PNEUMATIC HIGH PRESSURE REGULATOR AS PRECAUTION. 2 L 7 3 4F A3WE 1999120400201 19991204 00201 NM 1999 12 4 DL72S992609 1 19991127 A 2730 10609265003 POWER PACK BOEING 727 727232 1384082 NM ELEVATOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 404DA 630 21148 SYS A QTY RAPIDLY DECREASED ON GEAR RETRACTION. FOUND RT ELEV POWER PACK LEAKING. REPLACED RT ELEV POWER PACK. 2 L 7 3 4F A3WE 1999120400202 19991204 00202 NM 1999 12 4 DLM88992610 1 19991127 A 2560 BATTERY 61020 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 980DL 53267 FLASHLIGHT AT AFT F/A JUMP SEAT DID NOT FLASH. REPLACED BATTERY. 2 L 7 2 4F RT A6WE 1999120400203 19991204 00203 WP 1999 12 4 DLL10992613 1 19991127 A 2780 COMPARATOR 472085119M LKHEED 1011 10113851 5265010 WP LE FLAP MALFUNCTIONED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 730DA 891J 193C1199 AFTER TAKEOFF, FLAP/SLAT LIGHT ILLUMINATED ON S/O PANEL. FLAPS CAME UP RETRACTED BUT SLATS LOCKED IN EXTENDED POSITION. FOUND BOTH ASYMMETRY BRAKES TRIPPED. RESET LT AND RT BRAKES. REPLACED L/E ASYMMETRY COMPARATOR. FLAP/SLAT OPN NORMA L. 2 L 7 3 4F A23WE 1999120400204 19991204 00204 NM 1999 12 4 DLM88992614 1 19991128 A 5610 WINDOW DOUG MD88 MD88 3023688 NM COCKPIT OUT OF ADJUST A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 CAPT'S ESCAPE WINDOW WILL NOT OPEN. ADJUSTED CAPT'S SLIDING WINDOW, OPS CK OK. 2 L 7 2 4F RT A6WE 1999120400205 19991204 00205 WP 1999 12 4 DLL10992615 1 19991128 A 3310 LIGHT 26446 LKHEED 1011 10113851 5265010 WP COCKPIT FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 1731D 193C1200 DURING PREFLIGHT, COCKPIT FILLED UP WITH SMOKE AND FUMES FROM CAPT FLOOD LIGHT. REMOVED AND REPLACED CAPT FLOOD LIGHT R HEOSTAT, GROUND TEST NML. 2 L 7 3 4F A23WE 1999120400206 19991204 00206 NM 1999 12 4 DL733992616 1 19991128 A 2410 GENERATOR 735511A BOEING 737 737347 1384647 NM NR 1 ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 313WA B0509 23599 NR 1 ENGINE DRIVEN GENERATOR TRIPPED OFF ON CLIMBOUT. APU ON PREVIOUS MCO. REPLACED CSD. 2 L 7 2 4F RT A16WE 1999120400207 19991204 00207 NM 1999 12 4 P5CA9900788 1 19991128 A 3232 1U11986 ACTUATOR BOEING 747 747123 1384873 NM NLG DOOR FAILED A P5CA O OTHER J WARNING INDICATION AP APPROACH 1 WP 23 859FT 20326 ON APPROACH NOSE GEAR DOOR WARNING BOTH PRIMARY AND ALTERNATE. REPLACED NOSE LANDING GEAR DOOR ACTUATOR PER MAINTENANCE MANUAL 32-34-14 PAGE 201. 2 L 7 4 4F A20WE 1999120400208 19991204 00208 NM 1999 12 4 P5CA9900789 1 19991122 A 5753 SKIN BOEING 747 747123 1384873 NM TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DELAMINATION RIGHT INBOARD TRAILING EDGE AFT FLAP INBOARD OF NR 6 CANOE AREA. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1999120400209 19991204 00209 NM 1999 12 4 P5CA9900790 1 19991122 A 5730 PANEL BOEING 747 747123 1384873 NM RIGHT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DAMAGED RIGHT WING TIP HF PANEL COVER. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1999120400210 19991204 00210 NM 1999 12 4 P5CA9900791 1 19991122 A 3233 1387T1003 ACTUATOR BOEING 747 747123 1384873 NM LT MLG INTERMITTENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 INTERMITTENT OPERATION OF THE LEFT WING GEAR ALTERNATE EXTENTION ACTUATOR (DURING SCHEDULED OPERATIONAL CHECK). REPLACE D ACTUATOR PER BOEING MAINTENANCE MANUAL 32-35-01. 2 L 7 4 4F A20WE 1999120400211 19991204 00211 NM 1999 12 4 P5CA9900792 1 19991122 A 5330 SKIN BOEING 747 747123 1384873 NM BS 2650 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 CRACK IN FUSELAGE SKIN JUST ABOVE LEFT ELEVATOR BS 2650. REPAIRED PER BOEING SRM 53-30-03. 2 L 7 4 4F A20WE 1999120400212 19991204 00212 NM 1999 12 4 P5CA9900793 1 19991122 A 3233 1387T1003 ACTUATOR BOEING 747 747123 1384873 NM RT MLG INOPERATIVE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 INOPERATIVE RIGHT WING LANDING GEAR ALTERNATE EXTENSION MOTOR. REPLACED PER BOEING MAINTENANCE MANUAL 32-35-01. 2 L 7 4 4F A20WE 1999120400213 19991204 00213 NM 1999 12 4 P5CA9900794 1 19991122 A 5280 DOOR BOEING 747 747123 1384873 NM LT MLG DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DAMAGED LEFT BODY LANDING GEAR WHEEL WELL DOOR FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-03. 2 L 7 4 4F A20WE 1999120400214 19991204 00214 NM 1999 12 4 P5CA9900795 1 19991122 A 4980 MUFFLER BOEING 747 747123 1384873 NM APU CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 CRACKED APU EXHAUST MUFFLER AT 8 AND 12 O'CLOCK POSITIONS. REPAIRED PER BOEING MAINTENANCE MANUAL 49-21-03. 2 L 7 4 4F A20WE 1999120400215 19991204 00215 NM 1999 12 4 TWAA9916202 1 19991117 A 5754 SKIN BOEING 767 767330 NM LE FLAP DISBONDED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 691LF 25137 DURING CHECK-C MAINT, FOUND A 1.5 INCH BY 2 INCH DISBONDED AREA ON UPPER SURFACE NEAR THE O/B TRAILING EDGE AREA OF THE NUMBER 11 LEADING EDGE SLAT ON THE RT WING. AN INTERIM REPAIR WAS PREVIOUSLY INSTALLED. REPAIRED PER 767-300 SRM 51-70 -10 AND BOEING SERVICE BULLETIN 767-57A0057. 2 L 7 2 4F RT A1NM 1999120400216 19991204 00216 WP 1999 12 4 TWAA9916203 1 19991122 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 598 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND CORROSION ON THE FORMER FOOT AT STA 598, BETWEEN LONGERON 29L AND 30L. REMOVED VISIBLE CORROSION PER SPM 6-80-01 AND SRM 51-10-3. INSTALLED NEW FORMER FOOT PER SRM 53-03, FIG 3. 2 L 7 2 4F A6WE 1999120400217 19991204 00217 WP 1999 12 4 TWAA9916204 1 19991122 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 598 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND CORROSION ON THE FORMER FOOT AT STA 598, RT SIDE OF LONGERON 30. REMOVED VISIBLE CORROS ION PER SPM 6-80-1 AND SRM 51-10-03. INSTALLED NEW FORMER FOOT PER SRM 53-03 FIG 3. 2 L 7 2 4F A6WE 1999120400218 19991204 00218 NM 1999 12 4 HNAA9900162 1 19991128 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM LAVATORY ODOR A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 938HA 152 HEAVY FUEL ODOR IN LAV. INSPECTED AND FOUND UNIDENTIFIED FLUID IN LAV. DRAINED LAV AND PLACED ON MEL 25-7 (INOP AND NO USE). 2 H 7 2 4T RT A13NM 1999120400219 19991204 00219 EU 1999 12 4 MALA976636 1 19991118 A 3230 MLG BAC 146 AVRO146RJ85A 1500097 EU RIGHT MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 504XJ E2311 CREW HAD TO USE GEAR OVER RIDE TO RETRACT GEAR. MAINTENANCE INSPECTED LT AND RT MLG, NO DEFECTS NOTED. LUBRICATED AND CLEANED SHOCK STRUCT. NO LEAKAGE NOTED. 2 H 7 4 4F RT A49EU 1999120400220 19991204 00220 EU 1999 12 4 MALA976637 1 19991118 A 3230 643500300 CONTROL HANDLE BAC 146 AVRO146RJ85A 1500097 EU COCKPIT FAILED A MALA O OTHER O OTHER CL CLIMB 1 GL 15 504XJ E2311 AFTER 35 SECONDS THE GEAR HANDLE WOULD NOT RELEASE TO RETRACT THE GEAR, HAD TO USE OVERRIDE. MAINTENANCE REPLACED THE G EAR CONTROL HANDLE. OPS CHECKS GOOD PER 32-30-14. PERFORMED GEAR SWINGS. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999120400221 19991204 00221 EU 1999 12 4 MALA976638 1 19991124 A 3230 HP848430621 CONTROL VALVE SAAB SF340 SF340A 7850100 EU MLG MALFUNCTIONED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 106XJ 106 UPON SELECTING GEAR DOWN THE INTRANSIT LIGHT ILLUMINATES WITHOUT THE GEAR GREEN LIGHTS. RECYCLING THE GEAR HANDLE REQUI RES THE DOWNLOCK RELEASE BUTTON TO BE PUSHED AND CIRCUIT F7 WAS FOUND TO BE TRIPPED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR CONTROL VALVE. OPS AND LEAK CHECKS GOOD, ALL WORK DONE IAW 32-31-15 SAAB AMM. 2 L 7 2 4T RT A52EU 1999120400222 19991204 00222 EU 1999 12 4 MALA976639 1 19991126 A 7600 531706 CONTROL LEVER SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 412XJ 340B412 FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED ON LIFT OFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED CONTROL QUADRANT. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999120400223 19991204 00223 NE 1999 12 4 MALA976640 2 19991121 A 7261 3065T25P01 SCAVENGE PUMP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A MALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 445XJ 445 JUST AFTER TAKEOFF THE RIGHT ENGINE OIL PRESSURE CWP ILLUMINATED AND RIGHT OIL PRESSURE GUAGE WENT TO ZERO. RAN QRH AND SHUT DOWN ENGINE. RETURNED TO ELM. MAINTENANCE REPLACED SCAVENGE PUMP, PRESSURE SWITCH (P/N IPTE119-1000-200D1) AND D IFFERENITIAL PRESSURE SWITCH (P/N 8346-5). OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1999120400224 19991204 00224 1999 12 4 MALA976641 2 19991122 A 7320 219333008 HMA BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE FAILED A MALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 GL 15 528XJ E2353 NR 3 ENGINE FAILED IN FLIGHT (CRUISE) 24,000 FEET APPROXIMATELY 15 MINUTES BEFORE LANDING IN XNA. QRH FOLLOWED. MAINTE NANCE REPLACED HMA. OPS AND FUNCTION CHECKED GOOD AT THIS TIME IAW 73-20-01. RAN AC, ALL POWER SETTINGS FOR AN HOUR. 2 H 7 4 4F RT A49EU 1999120400225 19991204 00225 WP 1999 12 4 IXXA9900033 1 19991124 A 2810 FUEL CELL DOUG DC8 DC871F 302199D WP FUSELAGE CONTAMINATED A IXXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 822BX 790 45813 EN ROUTE FROM ONT TO SAN, THE NUMBER ONE ENGINE FLAMED OUT AT THE TOP OF CLIMB. THE FLIGHT CREW RELIT THE ENGINE FOLLOW ING COMPANY PROCEDURES, THE FLIGHT CONTINUED TO SAN FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE IN ACCO RDANCE WITH THE CFM MAINTENANCE MANUAL WHICH REVEALED MOISTURE IN THE NUMBER ONE MAIN FUEL TANK AND FILTER ASSEMBLY. MA INTENANCE REMOVED THE MOISTURE AND REPLACED THE MAIN FUEL FILTER AS PRECAUTIONARY. MAINTENANCE PERFORMED A MAXIMUM POWE R ASSURANCE CHECK IN ACCORDANCE WITH THE COMPANY JRH BOOK WITH NO DISCREPANCIES NOTED. 2 L 7 4 4F RT 4A25 1999120400226 19991204 00226 NM 1999 12 4 CALA9901541 1 19991129 A 2150 65771 FAN BOEING 737 7373T0 1384582 NM E/E BAY FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 70352 40321 23590 A BURNING ODOR ENTERED THE COCKPIT AND CABIN ON CLIMBOUT FROM ABQ. THE AIRCRAFT WAS RETURNED TO ABQ WHERE IT LANDED WIT HOUT INCIDENT. MAINTENANCE FOUND THE AVIONICS COOLING FAN INOPERATIVE. THE AVIONICS COOLING FAN WAS REMOVED AND REPLAC ED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1999120400227 19991204 00227 WP 1999 12 4 CALA9901542 1 19991130 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 395 - 475 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND FLOOR SUPPORT CORRODED AT UPPER LOBE CABIN FLOOR AT STA 395-457, RBL 28-33 AND STA 420-475, LBL 27. TH E FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999120400228 19991204 00228 WP 1999 12 4 CALA9901543 1 19991130 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 495 - 615 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND FLOOR SUPPORT CRACKED AT UPPER LOBE CABIN FLOOR STA 495-615, RBL 14. THE CRACKED AREA OF FLOOR SUPPORT WAS TRIMMED OUT. A NEW SECTION WAS INSTALLED IAW SRM 51-31-01 AND 51-21-01. 2 L 7 3 4F A22WE 1999120400229 19991204 00229 WP 1999 12 4 9904929867 1 19991114 A 4990 APU GARRTT GPTCP8598DCA DOUG DC9 DC951 3022051 WP APU BAY LEAKING A NWAA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 776NC P159DCA 47786 AFTER TAKEOFF AFT LEFT LAV SMOKE DETECTOR SOUNDED AND SMOKE APPARENT IN LAV. MAINTENANCE FOUND OIL LEAK FROM THE APU WA S BEING INGESTED INTO THE AC PNEUMATIC SYSTEM. APU AND WATER SEPARATORS REPLACED. 2 L 7 2 4F RT A6WE 1999120400230 19991204 00230 WP 1999 12 4 9904939867 1 19991114 A 2150 ACM DOUG DC9 DC951 3022051 WP AIR DISTRIBUTION CONTAMINATED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 GL 01 776NC 47786 AFTER TAKEOFF SMOKE ALARMS IN 3 LAVS SOUNDED AND FUMES WERE PRESENT IN THE CABIN. AIRCRAFT RETURNED TO DEPARTURE AIRPOR T. MAINTENANCE RAN ENGINES AT TAKEOFF POWER WITH PACKS ON TO BURN OUT RESIDUAL OIL FROM A PREVIOUS APU OIL LEAK. ACM A ND WATER SEPARATORS WERE REPLACED. 2 L 7 2 4F RT A6WE 1999120400231 19991204 00231 NM 1999 12 4 9904946314 1 19991122 A 3320 BALLAST BOEING 747 747451 1384940 NM ROW 12 FAILED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 674US 30269 DURING CRUISE, AN ELECTRICAL ODOR AND SMOKE WAS NOTICED COMING FROM THE OVERHEAD LIGHTS IN CABIN ZONE 'B'. TURNED CABIN LIGHTS OFF AND THE ODOR AND SMOKE DISSIPATED. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDNET. REPLACED BALLAST AT ROW 12JK. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999120400232 19991204 00232 WP 1999 12 4 9904959156 1 19991112 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8915E 45832 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999120400233 19991204 00233 WP 1999 12 4 9904969868 1 19991113 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 FORWARD CABIN EMERGENCY LIGHTS REMAIN ON WITH SWITCH IN OFF POSITION. MAINTENANCE REPLACED POWER SUPPLIES AND BATTERIES AT MAIN CABIN DOOR AND GALLEY DOOR. 2 L 7 2 4F RT A6WE 1999120400234 19991204 00234 WP 1999 12 4 9904979907 1 19991114 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMPARTMENT FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999120400235 19991204 00235 WP 1999 12 4 9904989969 1 19991114 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK MOUNTED EMERGENCY LIGHTS AND INTERIOR TAIL CONE RELEASE HANDLE LIGHT I NOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999120400236 19991204 00236 NE 1999 12 4 9904999611 2 19991124 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE RIGHT FAILED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 01 611NA 43248 8344 47435 657515 DURING CLIMBOUT PASSING 10,000 FEET, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. THE FLIGHT CREW INITIATED EMERGENCY CHEC K LIST PROCEDURES, RETURNED TO MKE, AND LANDED WITHOUT INCIDENT. THE FLIGHT CREW NOTED THERE WERE NO RELIGHT OF THE RIG HT ENGINE AND AN OVERWEIGHT LANDING (102,000 POUNDS) WAS ACCOMPLISHED WITH A NORMAL SINK RATE OF 200 FEET PER MINUTE. M AINTENANCE REPLACED THE RIGHT ENGINE AND CONDUCTED AN OVERWEIGHT LANDING INSPECTION, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1999120400237 19991204 00237 WP 1999 12 4 9905009980 1 19991117 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG DISCHARGED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9344 47440 GROUND SHIFT FAILURE AFTER TAKEOFF. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED NOSE GEAR STRUT TO PROPER LEVELS. ALSO RIGGED GROUND SHIFT LINKAGE AND RETENSIONED CABLES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999120400238 19991204 00238 EA 1999 12 4 COMA990708 1 19991117 A 5230 H2912A SPRING CNDAIR CL600 CL6002B19 EA CARGO DOOR BROKEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 937CA 7044 CARGO DOOR MESSAGE ON EICAS. REPLACED BROKEN SPRING ON DOOR HANDLE LATCH. 2 L 7 2 4F RT A21EA 1999120400239 19991204 00239 EA 1999 12 4 COMA9960709 1 19991123 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 CABIN DOOR WARNING. ADJUSTED DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1999120400240 19991204 00240 EA 1999 12 4 COMA9960710 1 19991123 A 2750 TE FLAPS CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 739CA 7273 FLAPS FAILED AT 37 DEGREES. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999120400241 19991204 00241 SO 1999 12 4 COMA9910177 1 19991129 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 263CA 120255 EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN. 2 L 7 2 4T RT A31SO 1999120400242 19991204 00242 EA 1999 12 4 COMA9960711 1 19991126 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 EA E/E BAY FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 946CA 7072 LEFT HAND PITOT, STATIC AND AOA HEAT CAUTION MESSAGE. REPLACED THE LEFT ADSHC. 2 L 7 2 4F RT A21EA 1999120400243 19991204 00243 EA 1999 12 4 COMA9960712 1 19991128 A 7714 6047T55P01 INDICATOR CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A COMA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 01 710CA 7241 RIGHT ENGINE N2 INDICATION WAS INOPERABLE. REPLACED THE ENGINE ALTERNATOR STATOR ASSY. 2 L 7 2 4F RT A21EA 1999120400244 19991204 00244 EA 1999 12 4 COMA60713 1 19991128 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA TE FLAP MALFUNCTIONED A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 739CA 191 10 7273 FLAPS FAILED AT 45 DEGREES. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999120400245 19991204 00245 EA 1999 12 4 COMA9960714 1 19991128 A 2750 TE FLAPS CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 981CA 7163 FLAPS FAILED AT ZERO. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999120400246 19991204 00246 EA 1999 12 4 COMA9960715 1 19991128 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA TE FLAP ILLUMINATED A COMA O OTHER O OTHER NR NOT REPORTED 1 SO 01 933CA 7040 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM PER AD98 20 01. 2 L 7 2 4F RT A21EA 1999120400247 19991204 00247 EA 1999 12 4 COMA9960716 1 19991129 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 981CA 5300 2300 7163 FLAPS FAILED AT ZERO. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1999120400248 19991204 00248 EA 1999 12 4 COMA9960717 1 19991129 A 3260 162255 BRACKET CNDAIR CL600 CL6002B19 EA NLG DAMAGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 945CA 7069 NLG DID NOT RETRACT. REPLACED THE NLG WOW AND CENTERED PROXIMITY BRACKET. 2 L 7 2 4F RT A21EA 1999120400249 19991204 00249 EA 1999 12 4 COMA9960718 1 19991125 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 920CA 13197 7022 FLAPS FAIL MESSAGE. FLAPS STUCK AT 0 DEGREES. COULD NOT DUPLICATE. FECU SHOWS LEFT HAND BPSU AT FAULT. REPLACED LEF T HAND BPSU. 2 L 7 2 4F RT A21EA 1999120400250 19991204 00250 NE 1999 12 4 COMA9960719 2 19991126 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 2 MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 971CA 7145 DURING TAKEOFF, NR 2 ENGINE N1 HUNG AT 38 DEGREES. COULD NOT DUPLICTE. ACCELERATION TEST WAS NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 1999120400251 19991204 00251 EA 1999 12 4 COMA9960720 1 19991126 A 5720 601R140341 VANE CAP CNDAIR CL600 CL6002B19 EA WS 53.60 CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 THE LEFT AND RIGHT INBOARD FLAP MOVEABLE VANE CAPS AT WS 53.60 ARE CHAFED BEYOND LIMITS. REPLACED LEFT AND RIGHT INBOAR D FLAP VANE CAPS AT WS 53.60 IAW WVAC EO 601R-57-0643. 2 L 7 2 4F RT A21EA 1999120400252 19991204 00252 EA 1999 12 4 COMA9960721 1 19991127 A 5315 601R311341 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 295 - 310 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 FLOORBEAM WEB ON INBOARD SIDE OF RBL 9 AT FS 295-310 HAS ELONGATED HOLE PREVIOUSLY PLUGGED WITH IMPROPER FASTENER. REPL ACED DAMAGED WEB WITH NEW WEB IAW WVAC E. 601R-53-0646. 2 L 7 2 4F RT A21EA 1999120400253 19991204 00253 EA 1999 12 4 COMA9960722 1 19991027 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7091 THE FWD J-ANGLE FS 280.00 BETWEEN LBL 9.0 AND RBL 9.0 WAS CORRODED. REPLACED J-ANGLE AT FS 280.00 BETWEEN LBL 9.0 AND R BL 9.0 WITH NEW J-ANGLE IAW WVAC EO 601R-53-0642. 2 L 7 2 4F RT A21EA 1999120400254 19991204 00254 EA 1999 12 4 COMA9960723 1 19991112 A 5315 601R3867317 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 TOP PLATES AT FS 349.00 CORRODED BEYOND LIMITS. REPLACED CORRODED PLATES WITH NEW PLATES IAW WVAC EO 601R-53-0640. 2 L 7 2 4F RT A21EA 1999120400255 19991204 00255 EA 1999 12 4 COMA9960724 1 19991127 A 5320 601R3152746 ANGLE CNDAIR CL600 CL6002B19 EA BS 300 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 PAX DOOR THRESHOLD ANGLE FOUND CORRODED BEYOND LIMITS. REPLACED CORRODED PAX DOOR THRESHOLD ANGLE IAW WVAC EO 601R-53-0 639. 2 L 7 2 4F RT A21EA 1999120400256 19991204 00256 EA 1999 12 4 COMA9960725 1 19991127 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 SERVICE DOOR THRESHOLD FLOOR SUPPORT ANGLE FOUND TO BE CORRODED BEYOND LIMITS. REPLACED CORRODED ANGLE WITH NEW ANGLE I AW WVAC EO 601R-53-0631, REV B. 2 L 7 2 4F RT A21EA 1999120400257 19991204 00257 EA 1999 12 4 COMA9960726 1 19991128 A 5320 601R31135758 CLIP CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 THE CLIPS AT FS 280.00 AT LBL 9.0 AND RBL 9.0 INBOARD AND OUTBOARD WERE CRACKED. REMOVED OLD CLIPS AND INSTALLED NEW CL IPS AT FS 280.00 (LBL 9.0 AND RBL 9.0) IAW WVAC EO 601R-53-0641. 2 L 7 2 4F RT A21EA 1999120400258 19991204 00258 EA 1999 12 4 COMA9960727 1 19991127 A 5311 600360303132 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 975CA 7150 FS 718.00 LEFT HAND AND RIGHT HAND FRAMES AND AFT DOUBLERS WERE CRACKED STR 10-12. REPAIRED LEFT HAND AND RIGHT HAND FR AMES AND AFT DOUBLER IAW CANADAIR REO 601R-53-61-193A. 2 L 7 2 4F RT A21EA 1999120400259 19991204 00259 EA 1999 12 4 COMA9960728 1 19991128 A 5320 601R3111367 SUPPORT CNDAIR CL600 CL6002B19 EA BS 310 - 358 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 FLOOR SUPPORT BEAM CAPS LBL 9, RBL 9 AND RBL 27 FOUND CORRODED BEYOND LIMITS OF REO 601R-53-00-005 IN AREAS FROM FS 310. 00 TO FS 355.00. REMOVED CORRODED SECTIONS OF FLOOR SUPPORT BEAM CAPS AND INSTALLED NEW BEAM CAPS IAW CANADAIR REO 601R -53-00-027 AND WVAC EO 601R-53-0647, 601R-53-0651, 601R53-0652. 2 L 7 2 4F RT A21EA 1999120400260 19991204 00260 NM 1999 12 4 UPS99231150 1 19991125 A 3260 SWITCH BOEING 727 72725C 138400H NM LT MLG DOOR INOP A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, LEFT MAIN GEAR DOOR INDICATION UNSAFE FWD AND AFT. NO AIRFRAME VIBRATION NOTED. DEFERRED PER MEL 32-1. SWITCH AT FAULT INDICATION ONLY. REMOVED AND REPLACED LEFT MLG DOOR WARNING SWITCH IAW MM 32-62-11, OPS CHECK G OOD. 2 L 7 3 4F A3WE 1999120400261 19991204 00261 NM 1999 12 4 UPS99231151 1 19991124 A 3350 LIGHT BOEING 727 72727C 138400J NM COCKPIT LOOSE A IPXA O OTHER L NO TEST CR CRUISE 1 SO 01 914UP 19246 INSPECTION TYPE:N/A, COCKPIT DOOR EMERGENCY EXIT LIGHT FELL OFF ITS MOUNT DURING FLIGHT. RESECURED LIGHT, OPS CHECKS NO RMAL. 2 L 7 3 4F A3WE 1999120400262 19991204 00262 WP 1999 12 4 UPS99831152 1 19991124 A 2821 FUEL FILTER DOUG DC8 DC873F 302199F WP NR 4 ENGINE CONTAMINATED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 802UP 46100 INSPECTION TYPE:N/A, NR 4 ENGINE FLAME-OUT FL350 1717Z OIL PRESS ZERO FLAME-OUT. INFLIGHT ENGINE START AND INFLIGHT ENG INE SHUTDOWN ACCOMPLISHED, MX CONTROL NOTIFIED. FL 310 RE-ATTEMPTED ENG START 1728Z OIL PRESS ZERO. ALL ENG PARAMETERS NORMAL, NO LIGHT OFF. ACCOMPLISHED TASKS ON ENGINE FLAME-OUT, TROUBLESHOOT ER 71-00-00, REMOV ED AND REPLACED FUEL PUM P FILTER ASSY PER 73-10-02. RUN AND LEAK CKS GOOD. ACFT REQUIRES HIGH POWER RUN 51265 REFERENCE LOG PAGE 348432 ITEM. 2 L 7 4 4F RT 4A25 1999120400263 19991204 00263 WP 1999 12 4 UPS99831153 1 19991115 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A, NO EMERGENCY LIGHTS ON BISE TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01 PG 2 02. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 1999120400264 19991204 00264 WP 1999 12 4 UPS99831154 1 19991126 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:N/A, ON PREFLIGHT EMERGENCY LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY P ACK, OPS CK GOOD. 2 L 7 4 4F RT 4A25 1999120400265 19991204 00265 EU 1999 12 4 QXEA9902358 1 19991127 A 3350 6008905 POWER SUPPLY GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU COCKPIT DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 1883 1883 11230 BOI- OVERHEAD EXIT SIGN ABOVE FLIGHT COMPARTMENT DOOR IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN POWER SUPPLY. O PERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999120400266 19991204 00266 WP 1999 12 4 99FDEA00488 1 19991124 A 2130 TERMINAL DOUG DC10 DC1010F 3022111 WP PRESS CONTROLLER FAILED A FDEA O OTHER O OTHER CL CLIMB 1 SO 25 367FE 46605 AC WOULD NOT PRESSURIZE. ALL DOORS CLOSED. REPAIRED TERMINAL END IAW SMP. IND LIGHT WORKS NORM, SYS CK NORM. 2 L 7 3 4F A22WE 1999120400267 19991204 00267 NM 1999 12 4 99FDEA00489 1 19991126 A 3260 LIGHT BOEING 727 72725 1384006 NM MLG INDICATOR INOP A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 152FE 18285 WHEN LANDING GEAR LOWERED NORM THERE WAS NO LT MAIN DOWN & LOCK IND. GEAR LIGHT TEST LT MAIN LIGHT INOP. 2 L 7 3 4F A3WE 1999120400268 19991204 00268 NM 1999 12 4 99FDEA00490 1 19991129 A 3260 ACCESSORY UNIT BOEING 727 727233 138408A NM MLG INOP A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 219FE 21102 DURING GEAR EXT, 3 GRN LIGHT+3 RED GEAR LIGHT+TAILSKID LIGHT WERE ILLUMINATED. REMOVED AND REPLACED L/G ACCESSORY UNIT PER MM 32-09-122 & TEST OK. 2 L 7 3 4F RT A3WE 1999120400269 19991204 00269 WP 1999 12 4 ABXA9900807 1 19991123 A 2133 20219741 OUTFLOW VALVE DOUG DC9 DC931 3022065 WP AFT FUSELAGE FAILED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 23 945AX 1714 47551 AUTO-PRESSURIZATION WAS INOPERATIVE. AIRCRAFT WOULD NOT DEPRESSURIZE UNTIL LANDING. OBSERVED STRONG ELECTRICAL SMELL. REPLACED OUTFLOW VALVE ACTUATOR. 2 L 7 2 4F A6WE 1999120400270 19991204 00270 WP 1999 12 4 MWEA99838 1 19991123 A 3350 59341391 LIGHT DOUG DC9 DC915 3022036 WP FUSELAGE FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 900ME 45841 RIGHT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE TROUBLESHOT AND REPAIRED GROUND FROM LIGHT BRACKET TO A IRFRAME. 2 L 7 2 4F A6WE 1999120400271 19991204 00271 WP 1999 12 4 MWEA99839 1 19991129 A 5230 591015740 BEAM DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND CORROSION ON AFT CARGO DOOR UNDER NUT PLATE BELOW NR 2 BEAM, AFT BAY. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999120400272 19991204 00272 WP 1999 12 4 MWEA99840 1 19991129 A 5753 99577733 STIFFENER DOUG DC9 DC932 3022066 WP TE FLAP CRACKED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 602ME 48133 LT FLAP OUTBOARD LEADING EDGE STIFFENER/DOUBLER WAS CRACKED AND HAD MISDRILLED RIVET HOLE. MAINTENANCE FITTED AND INSTA LLED NEW DOUBLER. 2 L 7 2 4F A6WE 1999120400273 19991204 00273 WP 1999 12 4 MWEA99841 1 19991129 A 5753 99577755 RIB DOUG DC9 DC932 3022066 WP TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT FLAP HAD CRACKED NOSE RIB AT STATION Z 88. MAINTENANCE FITTED AND INSTALLED NEW NOSE RIB. 2 L 7 2 4F A6WE 1999120400274 19991204 00274 WP 1999 12 4 MWEA99842 1 19991129 A 5753 59121241 SPAR DOUG DC9 DC932 3022066 WP WS 113.5 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND CORROSION ON LEFT FLAP, AFT SPAR UPPER TEE CAP AT STATION XFLS 113.5. MAINTENANCE FABRICATED AND INSTALLED SPAR C AP REPAIR. 2 L 7 2 4F A6WE 1999120400275 19991204 00275 WP 1999 12 4 MWEA99843 1 19991129 A 5753 5910134 SKIN DOUG DC9 DC932 3022066 WP WS 69 - 127 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND CORROSION ON INNER SURFACE OF LEFT FLAP LOWER SKIN PANEL, STATION XFLS 69 TO 127. MAINTENANCE FITTED AND INSTALLE D NEW SKIN PANEL. 2 L 7 2 4F A6WE 1999120400276 19991204 00276 WP 1999 12 4 MWEA99844 1 19991129 A 5753 5910134143 SKIN DOUG DC9 DC932 3022066 WP TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND LEFT FLAP UPPER INBOARD SKIN PANEL CORRODED. MAINTENANCE FITTED AND INSTALLED NEW SKIN PANEL. 2 L 7 2 4F A6WE 1999120400277 19991204 00277 WP 1999 12 4 MWEA99845 1 19991129 A 5753 99576131 DOUBLER DOUG DC9 DC932 3022066 WP TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND LEFT FLAP UPPER INBOARD SKIN PANEL AFT DOUBLER CORRODED. MAINTENANCE FITTED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 1999120400278 19991204 00278 WP 1999 12 4 MWEA99846 1 19991129 A 5753 9958000 ANGLE DOUG DC9 DC932 3022066 WP WS 65 - 127 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND LEFT FLAP INBOARD AFT BOTTOM T ANGLE CORRODED AT STATION XFLS 65 TO 127. MAINTENANCE FITTED AND INSTALLED NEW T A NGLE. 2 L 7 2 4F A6WE 1999120400279 19991204 00279 WP 1999 12 4 MWEA99847 1 19991129 A 5330 99581561 SKIN DOUG DC9 DC932 3022066 WP BS 305 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT SIDE FUSELAGE WINDOW BELT SKIN AT STATION 305 HAD A TOOL MARK. MAINTENANCE FABRICATED AND INSTALLED SKIN DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999120400280 19991204 00280 WP 1999 12 4 MWEA99848 1 19991129 A 3211 5919289517 TRUNNION DOUG DC9 DC932 3022066 WP LT MLG CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT MAIN LANDING GEAR FITTING ASSEMBLY (TRUNNION) WAS FOUND CORRODED. MAINTENANCE FITTED AND INSTALLED NEW FITTING ASS EMBLY. 2 L 7 2 4F A6WE 1999120400281 19991204 00281 NM 1999 12 4 SCNA99146 1 19991128 A 2110 2041853 VALVE BOEING 727 7272J4 1384006 NM AC COMPARTMENT FAILED A SCNA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 15 288SC 3684 20765 TAKEOFF WAS ABORTED JUST SHY OF V1 DUE TO SMOKE IN THE COCKPIT. NO SMOKE NOTICED IN THE CABIN. REMOVED AND REPLACED FL OW MULTIPLIER PER MM 211211. RAN ALL ENGINES AND PRESSURIZED WITH ALL PACKS RUNNING. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999120400282 19991204 00282 NM 1999 12 4 DHL99708001 1 19991109 A 3221 TRUNNION BOEING 727 72725 1384006 NM NLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 LEFT AND RIGHT NOSE LANDING GEAR TRUNNION HAD CORROSION AND PITTING AT BEARING MATING SURFACES. MACHINED LEFT AND RIGHT TRUNNIONS, CORROSION REMOVED AND WITHIN LIMITS PER SRM 53-40-1. 2 L 7 3 4F A3WE 1999120400283 19991204 00283 NM 1999 12 4 DHL99708002 1 19991109 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 BS 560 FLOOR BEAM UPPER CHORD HAS FLOOR BEAM REPAIR AND CORROSION FROM LBL 4 TO LBL 14.REMOVED OLD REPAIR AND INSTALLE D NEW REPAIR PER SRM 53-10-8 , SUPPORT ANGLE 11 , AND 7 N/R 3885 2 L 7 3 4F A3WE 1999120400284 19991204 00284 NM 1999 12 4 DHL99708003 1 19991109 A 5320 STRAP BOEING 727 72725 1384006 NM BS 1110 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 STABILITY STRAP AT RBL 23 HAS PREVIOUS REPAIR LOCATED FWD SIDE OF BS 1110 FLOOR NOT IN CONFORMANCE WITH SRM. REPLACED R EPAIR PER SRM 53-10-8 3 X 26. 2 L 7 3 4F A3WE 1999120400285 19991204 00285 NM 1999 12 4 DHL99708004 1 19991115 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 804.5 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 REMOVED AND REPLACED WEB AT BS 804.5 OF FLOORBEAM RBL 51 PREV REPAIRED. REMOVED AND INSTALLED NEW WEB PER SRM 53-10-1, 24 X 9. 2 L 7 3 4F A3WE 1999120400286 19991204 00286 NM 1999 12 4 DHL99708005 1 19991111 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 708 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 CABIN SEAT TRACK AT BS 708 LBL 24.5 CORRODED BEYOND LIMITS ON I/B FLANGE. REPLACED SECTION OF SEAT TRACK FROM BS 680 TO 740 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1999120400287 19991204 00287 NM 1999 12 4 DHL99708006 1 19991111 A 5320 STRAP BOEING 727 72725 1384006 NM BS 420 MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 FLOORBEAM STABILITY STRAP FROM BS 420 TO BS 400 BL 0 HAD NUMEROUS HOLES DRILLED IN TO IT. REPLACED STRAP 3 X 63 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999120400288 19991204 00288 NM 1999 12 4 DHL99708007 1 19991111 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 380 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 FLOORBEAM STABILITY STRAP REPAIR AT BS 380 BL 0 DID NOT CONFORM TO SRM. REPLACED SECTION OF STRAP PER SRM 53-10-8, 3 X 63. 2 L 7 3 4F A3WE 1999120400289 19991204 00289 NM 1999 12 4 DHL99708008 1 19991117 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 560 MISREPAIR A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 REPAIR AT BS 560 FLOORBEAM LBL 44 BOTH ANGLES, MATERIAL NOT IN CONFORMANCE. REPLACED BOTH SUPPORT ANGLES PER SRM 53-10- 8 MATERIAL 1490-2831 AND 2785. 2 L 7 3 4F A3WE 1999120400290 19991204 00290 NM 1999 12 4 DHL99708009 1 19991117 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 560 MISREPAIR A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 REPAIR AT BS 560 FLOORBEAM RBL 3 TO RBL 21 HAD BOTH REPAIR ANGLES OF MATERIAL NOT IN CONFORMANCE. REPLACED BOTH SUPPORT ANGLES PER SRM 53-10-8 BAC 1490-2785 AND 2831. 2 L 7 3 4F A3WE 1999120400291 19991204 00291 NM 1999 12 4 DHL99708010 1 19991109 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 620 MISREPAIR A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 BS 620 FLOORBEAM REPAIR UPPER CHORD FROM LBL 2 TO 31 DID NOT CONFORM PER SRM. CUT OUT DAMAGED UPPER CHORD, INSTALLED FL OORBEAM REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999120400292 19991204 00292 NM 1999 12 4 DHL99708011 1 19991109 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 BS 360 FLOORBEAM CORRODED ON UPPER CHORD FLANGE RBL 30. CUT OUT DAMAGED AREA FROM RBL 24 TO RBL 68. INSTALLED FLOORBEA M PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999120400293 19991204 00293 NM 1999 12 4 DHL99708012 1 19991109 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 660 MISREPAIR A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 BS 660 FLOORBEAM REPAIR UPPER CHORD OF RBL 14 TO RBL 22 DID NOT CONFORM TO SRM. CUT OUT DAMAGED AREA FROM RBL 16 TO 36. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999120400294 19991204 00294 NM 1999 12 4 DHL99708013 1 19991109 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 680 MISREPAIR A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 BS 680 FLOORBEAM REPAIR UPPER CHORD OF LBL 6 TO 30 DID NOT CONFORM TO SRM. CUT OUT DAMAGED AREA. INSTALLED FLOORBEAM R EPAIR BETWEEN LBL 36 AND 12 PER SM 53-10-8. 2 L 7 3 4F A3WE 1999120400295 19991204 00295 NM 1999 12 4 DHL99708014 1 19991109 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 BS 480 FLOORBEAM CORROSION LOWER SIDE OF UPPER CAP FWD SIDE OF LBL 45. CUT OUT DAMAGED AREA AT STA 480 RBL 35, INSTALLE D FLOORBEAM REPAIR FROM RBL 35 TO 65 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999120400296 19991204 00296 NM 1999 12 4 DHL99708015 1 19991110 A 5320 STRAP BOEING 727 72725 1384006 NM BS 1090 MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 STABILITY STRAP HAS DRILL MARKS BL 0 BS 1090 AND 1070. INSTALLED PLUG FASTENERS PER SRM 51-30-2. REMOVED SECTION OF ST AB STRAP AT BOTTOM OF FLOORBEAM BETWEEN STA 1070 AND 1090. INSTALLED NEW SECTION PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999120400297 19991204 00297 NM 1999 12 4 K4HA99087 1 19991120 A 5720 PANEL BOEING 747 747132 1384882 NM LE FLAP SEPARATED A K4HA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 GL 23 709CK 20247 FLAP PANEL ON RT WING FOUND MISSING ON POST FLIGHT (FLAP PANEL NR 7). INSPECTED L/E FLAP AREA FOUND DAMAGE TO L/E FLAP PANEL NR 19 AND I/B LEFT AND RIGHT ROTORY ACTUATORS. REPLACED NR 19 L/E FLAP PANEL ASSY PER MM 27-81-02. REMOVED AND R EPLACED LEFT AND RIGHT I/B ROTARY ACTUATORS. 2 L 7 4 4F A20WE 1999120400298 19991204 00298 EU 1999 12 4 RAIA9911025 1 19991127 A 7400 3037885 EXITER BOX AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 423TE 119 120970R STL- NR 1 ENGINE WOULD NOT START. MAINTENANCE REPLACED EXITER BOX FOR NR 1 ENGINE. 2 H 7 2 4T 4 T RT A53EU E20NE 1999120400301 19991204 00301 1999 12 4 99ZZZX4334 4 19990915 A 3417 MC9610 SWITCH SNIAS AS350 AS350B3 8680954 EU AIR DATA INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 103LN 182 053 3128 SWITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U NC H9EU 1999120400302 19991204 00302 1999 12 4 99ZZZX4335 4 19990918 A 3417 MC9610 SWITCH SNIAS AS350 AS350B3 8680954 EU AIR DATA INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 104LN 016 3134 SWITCH INOPERATIVE UPON INSTALLATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U NC H9EU 1999120400303 19991204 00303 GL 1999 12 4 99ZZZX4336 2 19990811 A 7320 1564T1005 ACTUATOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL FUEL CONTROL INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 206 2331 S754 FUEL CONTROL ACTUATOR INOPERATIVE. WILL NOT MOVE IN EITHER DIRECTION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H3EU E4CE 1999120400304 19991204 00304 EU 1999 12 4 R7MA0000786 1 19991013 A 6420 109813102125 HUB ASSY AGUSTA A109 A109K2 0260502 EU TAIL ROTOR DAMAGED A P R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 2679 078 10018 DURING PRE-FLIGHT INSPECTION, PILOT NOTED THE FLAPPING OF THE TAIL ROTOR BLADES TO BE TIGHTER THA NORMAL AND FELT TO BE ROUGH. MAINTENANCE REMOVED AND INSPECTED TAIL ROTOR ASSEMBLY. THE TAIL ROTOR TRUNNION WAS FOUND SCORED WITH TWO AREAS THAT APPEARED TO BE PITS IN THE FIRST AREA WAS .75 INCHES LONG AND .25 INCHES WIDE AT THE WIDEST POINT. THE SECOND AREA WAS .6 INCHES LONG. THE AREAS ARE APROXIMATELY .050 INCH. THE TAIL ROTOR HUB BUSHING REFLECTED THE SAME PITTING TYPE DAMAGE. (X) 1 G 7 2 3U RT H7EU 1999120400305 19991204 00305 EU 1999 12 4 R7MA0000793 1 19991015 A 2400 MS245471 SWITCH AGUSTA A109 A109K2 0260502 EU ELECTRICAL SYS INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 10018 SWITCH INTERMITTENTLY INOPERATIVE. (X) 1 G 7 2 3U RT H7EU 1999120400306 19991204 00306 NM 1999 12 4 USAA990997 1 19991018 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER TIE CLIP AT BS 616, S-1, S-5L, S-8L. INSTALLE D NEW TIE CLIP PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400307 19991204 00307 NM 1999 12 4 USAA990996 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 312, STR 5L FRAME. INSTALLED DOUBLER PER SRM 5 3-00-07. (X) 2 L 7 2 4F RT A16WE 1999120400308 19991204 00308 NM 1999 12 4 USAA990990 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 827, SR 9L FRAME. INSTALLED FILLER AND REPAIR A NGLE PER EA 65542. (X) 2 L 7 2 4F RT A16WE 1999120400309 19991204 00309 NM 1999 12 4 USAA990989 1 19991018 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT LOWER FASTENER HOLE OF INNER CHORD BS 616, FUSELAGE FR AME WL 203 LEFT SIDE. INSTALLED FILLER AND DOUBLER PER SRM 3-10-23 AND EA 65562. (X) 2 L 7 2 4F RT A16WE 1999120400310 19991204 00310 NM 1999 12 4 USAA990988 1 19991018 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 616 RBL 62, WL 202, INBOARD CHORD ANGLE. INSTAL LED REPAIR ANGLES PER EA 65562. (X) 2 L 7 2 4F RT A16WE 1999120400311 19991204 00311 NM 1999 12 4 USAA990987 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 887, STR 9L FRAME. INSTALLED DOUBLER PER EA 655 42 AND SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999120400312 19991204 00312 NM 1999 12 4 USAA990986 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK AT STA 480 STR 9L FRAME. INSTALLED DOUBLER PER SRM 5 3-00-07 AND E 65542. (X) 2 L 7 2 4F RT A16WE 1999120400313 19991204 00313 NM 1999 12 4 USAA990985 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 400 STR 9L FRAME. INSTALLED DOUBLER PER SRM 5 3-00-07 AND EA 65542. (X) 2 L 7 2 4F RT A16WE 1999120400314 19991204 00314 NM 1999 12 4 USAA990984 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 480 STR 9R FRAME. INSTALLED DOUBLER PER SRM 5 3-00-07 AND EA 65542. (X) 2 L 7 2 4F RT A16WE 1999120400315 19991204 00315 NM 1999 12 4 USAA990951 1 19991018 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 663 STR 10R TIE CLIP. INSTALLED TIE CLIP PER SR M 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400316 19991204 00316 NM 1999 12 4 USAA990948 1 19991018 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STA 616 STR 4R TIE CLIP. REPAIRED PER SRM 51-10-02. ( X) 2 L 7 2 4F RT A16WE 1999120400317 19991204 00317 NM 1999 12 4 USAA990940 1 19991018 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 663 STR 10L TIE CLIP. REPAIRED PER SRM 51-10- 02. (X) 2 L 7 2 4F RT A16WE 1999120400318 19991204 00318 NM 1999 12 4 USAA990939 1 19991018 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 639 STR 4R TIE CLIP. REPAIRED PER SRM 51-10-0 2. (X) 2 L 7 2 4F RT A16WE 1999120400319 19991204 00319 NM 1999 12 4 USAASB99258 1 19991024 A 2751 2061141 INDICATOR BOEING 737 737301 1384611 NM TE FLAPS MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 352US 33045 23555 BWI - FLT 2438 - AFTER TAKEOFF, THE FLAPS WOULD NOT RETRACT FROM THE FIVE DEGREE POSITION. FLAP HANDLE WOULD NOT MOVE F LAPS UP OR DOWN. FLIGHT DIVERTED TO BWI AND AN EMERGENCY WAS DECLARED. ALTERNATE FLAP EXTENSION WAS USED TO POSITION F LAPS TO 15 DEGREES FOR LANDING. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED FLAP SURFACES AND MECHANISMS. F LAPS EXTENDED ON ALTERNATE TO 40 DEGREES THEN RETRACTED HYDRAULICALLY TO ZERO DEGREES. ACCOMPLISHED LUBRICATION OF FLAP S AND MECHANISMS AND PERFORMED OPERATIONAL CHECK AND ASYMMETRY TEST PER MM. REMOVED AND REPLACED FLAP POSITION INDICATO R AS PRECAUTIONARY. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4F RT A16WE 1999120400320 19991204 00320 NM 1999 12 4 USAA990737 1 19990715 A 5230 6547952166M SKIN BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 525AU 35680 23860 TPA - DURING CX-1 CHECK, FOUND .25 INCH CRACK AT AFT CARGO DOOR OUTER SKIN AT UPPER AFT CORNER OF DOOR HANDLE CUT-OUT. I NSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-30-03. (X) 2 L 7 2 4F RT A16WE 1999120400321 19991204 00321 NM 1999 12 4 USAA990738 1 19990719 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727E CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 42842 22956 TPA - DURING WALK-AROUND FOUND 1.9 INCH SKIN CRACK AT BS 727E PLUS 2 INCHES AND S18R. INSTALLED DOUBLER MADE OF .090 IN CH 2024T3 PER SRM 53-00-01 FIG 202. (X) 2 L 7 2 4F RT A16WE 1999120400322 19991204 00322 NM 1999 12 4 USAA990739 1 19990719 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 743-754 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 42842 22956 TPA - DURING WALK-AROUND FOUND 1.9 INCH SKIN CRACK AND 1 INCH CRACK IN SKIN AT BS 743 AND S19R AND BS 754.5 AND S19R. I NSTALLED DOUBLER MADE OF .090 INCH 2024T3. BOTH CRACKS REPAIRED WITH SAME DOUBLER PER SRM 53-00-01 FIG 202. (X) 2 L 7 2 4F RT A16WE 1999120400323 19991204 00323 NM 1999 12 4 USAA990672 1 19990708 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 40186 22957 CLT - DURING WALK-AROUND CHECK VISUAL INSPECTION, FOUND A 2.25 INCH CRACK AT STA 727D PLUS 2 INCHES TO 727D PLUS 4.25 IN CHES JUST BELOW AND PARALLEL TO STR 23R FUSELGE SKIN. FABRICATED AND INSTALLED REPAIR FILLER AND EXTERNAL DOUBLER PER T R 53-60-03. (X) 2 L 7 2 4F RT A16WE 1999120400324 19991204 00324 NM 1999 12 4 USAA990087 1 19990214 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 374US 41365 22953 CLT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK IN EXTERNAL SKIN AT STA 380 AND BL 3 LEFT E/E COOLING DUCT EXHAUST CUT-OUT. INSTALLED DOUBLER PER SRM 53-30-07. (X) 2 L 7 2 4F RT A16WE 1999120400325 19991204 00325 NM 1999 12 4 USAA990725 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STA 639 STR 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-4 0-02. (X) 2 L 7 2 4F RT A16WE 1999120400326 19991204 00326 NM 1999 12 4 USAA990726 1 19990729 A 5320 FRAME BOEING 737 737301 1384611 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT ENTRY DOOR CUT-OUT FRAME UPPER FORWARD SECTION AT BOT TOM HOLE FORWARD EDGE FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (X) 2 L 7 2 4F RT A16WE 1999120400327 19991204 00327 NM 1999 12 4 USAA990727 1 19990729 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANG LE. REPAIRED PER BOEING DWG NR 69-48985/51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400328 19991204 00328 NM 1999 12 4 USAA990728 1 19990729 A 5320 FRAME BOEING 737 737301 1384611 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .500 INCH CRACK MAIN ENTRY DOORWAY UPPER HINGE H-STRAP DOORWAY FRAME. FABRICATED AND INSTALLED NEW H-STRAP PER SRM 51-10-02 AND BOEING DWG 90-7822. (X) 2 L 7 2 4F RT A16WE 1999120400329 19991204 00329 NM 1999 12 4 USAA990729 1 19990729 A 5311 FRAME BOEING 737 737301 1384611 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK FRAME 312 AT STR 5L. CRACK TRIMMED OUT AND DOUBLER INS TALLED PER SRM 53-00-07 FIG 202 AND EA 65075. (X) 2 L 7 2 4F RT A16WE 1999120400330 19991204 00330 NM 1999 12 4 USAA990681 1 19990729 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X) 2 L 7 2 4F RT A16WE 1999120400331 19991204 00331 NM 1999 12 4 USAA990682 1 19990729 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD RBL1 W/L 188 SKIN. INSTALLED REPAI R DOUBLER PER SRM 53-10-08 FIG 203. (X) 2 L 7 2 4F RT A16WE 1999120400332 19991204 00332 NM 1999 12 4 USAA990683 1 19990729 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER TR 53-10-07. (X) 2 L 7 2 4F RT A16WE 1999120400333 19991204 00333 NM 1999 12 4 USAA990684 1 19990729 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 195 SKIN. INSTALLED DOUB LER PER TR 53-10-07. (X) 2 L 7 2 4F RT A16WE 1999120400334 19991204 00334 NM 1999 12 4 USAA990719 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 500C CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 500C STR 7R TIE CLIP. INSTALLED NEW TIE CLIP PE R SRM 51-40-02. (X) 2 L 7 2 4F RT A16WE 1999120400335 19991204 00335 NM 1999 12 4 USAA990755 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 787 BETWEEN STR 8 AND STR 9R. INSTALLED DOUBLER PER EA 65040. (X) 2 L 7 2 4F RT A16WE 1999120400336 19991204 00336 NM 1999 12 4 USAA990756 1 19990803 A 5312 BKHD INTERCOSTAL BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 2 5, WL 195 INTERCOSTAL. REPAIRED PER TR 53-10-18. (X) 2 L 7 2 4F RT A16WE 1999120400337 19991204 00337 NM 1999 12 4 USAA990757 1 19990803 A 5312 BULKHEAD WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5 WL 200 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (X) 2 L 7 2 4F RT A16WE 1999120400338 19991204 00338 NM 1999 12 4 USAA990758 1 19990803 A 5312 BULKHEAD WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 0 2, WL 190 WEB. (X) 2 L 7 2 4F RT A16WE 1999120400339 19991204 00339 NM 1999 12 4 USAA990759 1 19990803 A 5312 BULKHEAD WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, RBL 0 2, WL190 WEB. INSTALLED DOUBLER PER TR 53-10-08 FIG 203. (X) 2 L 7 2 4F RT A16WE 1999120400340 19991204 00340 NM 1999 12 4 USAA990762 1 19990803 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 773 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 21 INCH BY 1 INCH AREA OF CORROSION AT STA 773, RBL 14 FLOORBEAM AFT CARGO. CORROSION LEVEL 2. INSTALLED NEW SECTION OF FLOORBEAM AND SPLICE PER SRM 53-00-53. (X) 2 L 7 2 4F RT A16WE 1999120400341 19991204 00341 NM 1999 12 4 USAA990800 1 19990803 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT- DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 639 AND STR 2L TIE CLIP. REPAIRED PER RM 51-10-0 2. (X) 2 L 7 2 4F RT A16WE 1999120400342 19991204 00342 NM 1999 12 4 USAA990801 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 807 STR 8 AND 9L FUSELAGE FRAME AT FASTENER HOLE. REPAIRED PER SRM 53-00-07 FIG 202. (X) 2 L 7 2 4F RT A16WE 1999120400343 19991204 00343 NM 1999 12 4 USAA990802 1 19990803 A 5312 BKHD INTERCOSTAL BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURENT INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 195, RBL 25, AFT SIDE PRESS URE BULKHEAD INTERCOSTAL. INSTALLED ACCESS COVER PER SRM 53-10-08. (X) 2 L 7 2 4F RT A16WE 1999120400344 19991204 00344 NM 1999 12 4 USAA990803 1 19990803 A 5312 BULKHEAD WEB BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 204, RBL 5, PRESSURE BULKH EAD WEB. REPAIRED PER TR 53-10-07, REV A. (X) 2 L 7 2 4F RT A16WE 1999120400345 19991204 00345 NM 1999 12 4 USAA990804 1 19990803 A 5320 WEB BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK AT STA 18A SHEAR BEAM WEB LEFT SIDE 1 INCH FORWARD OF STA 727, LBL 60, WL 188.5. REPAIRED PER SRM 53-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400346 19991204 00346 NM 1999 12 4 USAA990805 1 19990803 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 663 STR 14L TIE CLIP. REMOVED AND REPAIRED PER SR M 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400347 19991204 00347 NM 1999 12 4 USAA990806 1 19990803 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 663 STR 14R TIE CLIP. REMOVED AND REPLACED PER SR M 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400348 19991204 00348 NM 1999 12 4 USAA990807 1 19990803 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT STA 706 STR 1 TIE CLIP. REPLACED PER SRM 51-10-02. ( X) 2 L 7 2 4F RT A16WE 1999120400349 19991204 00349 NM 1999 12 4 USAA990808 1 19990803 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 639 STR 4L TIE CLIP. REMOVED AND REPLACED PER R M 51-10-02 AND SRM 51-40-01. (X) 2 L 7 2 4F RT A16WE 1999120400350 19991204 00350 NM 1999 12 4 USAA990809 1 19990803 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37131 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 639 STR 5L TIE CLIP. REMOVED AND REPLACED PER S RM 51-10-02 AND SRM 51-40-03. (X) 2 L 7 2 4F RT A16WE 1999120400351 19991204 00351 NM 1999 12 4 USAA990810 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK BOTTOM END OF FRAME STA 616 INBOARD CHORD ANGLE RT SIDE FRAME. INSTALLED FILLER AND DOUBLER PER SB 737-53-1182 AND EA 64972. (X) 2 L 7 2 4F RT A16WE 1999120400352 19991204 00352 NM 1999 12 4 USAA991021 1 19991013 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 480, BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER ANGLE PER EA 65618 AND SRM 53-00-07 FIG 202. (X) 2 L 7 2 4F RT A16WE 1999120400353 19991204 00353 NM 1999 12 4 USAA991020 1 19991013 A 5311 FRAME BOEING 737 737301 1384611 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 887, BETWEEN STR 8L AND STR 9L FRAME. INTALLED D OUBLER ANGLE PER EA 65618. (X) 2 L 7 2 4F RT A16WE 1999120400354 19991204 00354 NM 1999 12 4 USAA991029 1 19991013 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT BS 907, STR 9L STRINGER TIE CLIP. REPAIRED WITH I DENTICAL PART PER SRM 51-10-2. (X) 2 L 7 2 4F RT A16WE 1999120400355 19991204 00355 NM 1999 12 4 USAA991081 1 19991013 A 5240 6551674501 FITTING BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT FORWARD SERVICE DOOR LOWER AFT DOOR STOP FITTING ASSEM BLY. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400356 19991204 00356 NM 1999 12 4 USAA991090 1 19991013 A 5330 SKIN BOEING 737 737301 1384611 NM BS 5332 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 EACH .50 INCH CRACKS AT BS 5332, RBBL 60, WL 21.5 SKIN ASSEMBLY. INST ALLED REPAIR PLATES PER SRM 53-10-01 FIG 202. (X) 2 L 7 2 4F RT A16WE 1999120400357 19991204 00357 NM 1999 12 4 USAA991123 1 19991016 A 5240 SKIN BOEING 737 7373B7 1384580 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT FORWARD SERVICE DOOR LOWER HINGE CUT-OUT UPPER CORN ER SKIN. INSTALLED EXTERNAL DOUBLER PER EA 65883. (X) 2 L 7 2 4F RT A16WE 1999120400358 19991204 00358 NM 1999 12 4 USAA991126 1 19991016 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 778AU 25020 24980 CLT - DURING A RON CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND A 2 INCH CRACK AT BS 500, RBL 1, BETWEEN STR 28L AND STR 28R FRAME. INSTALLED FABRICATED REPAIR PER EA 65887. (X) 2 L 7 2 4F RT A16WE 1999120400359 19991204 00359 NM 1999 12 4 USAA991125 1 19991016 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 778AU 25020 24980 CLT - DURING A RON CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND 4 CRACKS 2 INCHES, 3.50 INCHES, 3 INCHES, AND 2.50 INCHES BETWEEN BS 500 AND BS 500A, BETWEEN STR 28L AND STR 28R SKIN. INSTALLED REPAIR FASTENERS IN DOUBLER PER EA 65887. (X) 2 L 7 2 4F RT A16WE 1999120400360 19991204 00360 NM 1999 12 4 USAA991124 1 19991016 A 5320 FRAME BOEING 737 7373B7 1384580 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK ON SKIN AT LOWER AFT CORNER OF SERVICE DOOR CUT-OUT SKI N. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-10-01. (X) 2 L 7 2 4F RT A16WE 1999120400361 19991204 00361 NM 1999 12 4 USAA991122 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 480 BETWEEN STR 8L AND STR 9L FRAME. INSTALLE D REPAIR ANGLE AND FILLER PER EA 65705. (X) 2 L 7 2 4F RT A16WE 1999120400362 19991204 00362 NM 1999 12 4 USAA991121 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 907 BETWEEN STR 8L AND STR 9L FRAME. INSTALLE D REPAIR ANGLE AND FILLER PER EA 65705. (X) 2 L 7 2 4F RT A16WE 1999120400363 19991204 00363 NM 1999 12 4 USAA991120 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 927 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRAACK AT STA 927 BETWEEN STR 8R AND STA 9R FRAME. INSTALL ED REPAIR ANGLE AND FILLER PER EA 65705. (X) 2 L 7 2 4F RT A16WE 1999120400364 19991204 00364 NM 1999 12 4 USAA991119 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 847 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D REPAIR ANGLE AND FILLER PER EA 65705. (X) 2 L 7 2 4F RT A16WE 1999120400365 19991204 00365 NM 1999 12 4 USAA991118 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 827 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D REPAIR ANGLE AND FILLER PER EA 65705. (X) 2 L 7 2 4F RT A16WE 1999120400366 19991204 00366 NM 1999 12 4 USAA991117 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK AT STA 480 BETWEEN STR 8R AND STR 9R FRAME. INSTALLE D REPAIR ANGLE AND FILLER PER EA 65705. (X) 2 L 7 2 4F RT A16WE 1999120400367 19991204 00367 NM 1999 12 4 HNAA9900163 1 19991201 A 3230 858601 PSEU DHAV DHC8 DHC8201 2809001 NM LT MLG FAILED A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 969HA 468 LT MLG DOOR AMBER LIGHT ILLUMINATED UPON RETRACTION CYCLE GEAR AND UPON 2ND REACTION SAME LT ILLUMINATED ALONG WITH LAND ING GEAR CAUTION LIGHT. PERFORMED MANUAL EXTENSION. FOUND PSEU DRIVER 53 FLAG. REMOVED AND REPLACED PSEU AND RETRACTE D GEAR, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999120400368 19991204 00368 NM 1999 12 4 AWXA9900421 1 19991122 A 5411 BACB30MY12K FASTENER BOEING 757 7572S7 1384962 NM RT PYLON SHEARED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING ENGINE CHANGE SEVERAL FASTENERS ON THE PYLON ATTACH FITTING, WHERE THE DIAGONAL WING BRACE ATTACHES WERE LOOSE AN D 2 WERE SHEARED. ACTION IS CURRENTLY BEING EVALUATED FOR DISPOSITION AND REPAIR. 2 L 7 2 4F RT A2NM 1999120400369 19991204 00369 NM 1999 12 4 AWXA9900422 1 19991123 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 STA 344 BL 0 LIGHT CORROSION AT CLIP-NUT HOLE ON BOTTOM OF FLOORBEAM T CAP FLANGE. CORROSION REMOVED, MATERIAL LOSS IS BEYOND LIMITS. REPAIRED PER SRM 53-10-51 FIG 206. 2 L 7 2 4F RT A16WE 1999120400370 19991204 00370 NM 1999 12 4 AWXA9900423 1 19991123 A 5320 654580T8 WEB BOEING 737 7373B7 1384580 NM BS 277 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 WEB CRACKED AT STA 277 STR 14R. REPAIRED PER ER 03-5310-99309-EY1, FPI PER BOEING 20-20-02 PAINTED PER M/M 51-21-00. 2 L 7 2 4F RT A16WE 1999120400371 19991204 00371 NM 1999 12 4 AWXA9900424 1 19991123 A 5751 656346110 ANGLE BOEING 737 7373B7 1384580 NM WS 537 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 RT AILERON HINGE ATTACH FITTING ON WING, O/B SUPPORT LOWER ANGLE CRACKED AT 2ND I/B HINGE. FABRICATED AND INSTALLED NEW ATTACH ANGLE FITTING AS PER DWG NR 65-63461 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 1999120400372 19991204 00372 NM 1999 12 4 AWXA9900425 1 19991123 A 5751 65C2591117A SKIN BOEING 737 7373B7 1384580 NM AILERON DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 LOWER FLANGE OF LT AILERON FWD SPAR WAS DAMAGED IN 2 SPOTS, 1 AT I/B END AND 2 AT 24 FROM I/B END. REPAIRED LOWER FLA NGE OF AILERON AS PER ER 03-5751-99306-EY1. 2 L 7 2 4F RT A16WE 1999120400373 19991204 00373 NM 1999 12 4 AWXA9900426 1 19991123 A 5320 693535214 CLIP BOEING 737 7373B7 1384580 NM BS 616 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 STR 3L CLEAT CRACKED AT FRAME STA 616. REPLACED CLIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999120400374 19991204 00374 NM 1999 12 4 AWXA9900427 1 19991123 A 5751 65C2591118A HINGE BOEING 737 7373B7 1384580 NM RT AILERON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 328AW 23377 RT AILERON FRONT SPAR LOWER FLANGE DELAMINATED, FIBER MISSING AT I/B HINGE AREA AT I/B END. ALSO, CRACKED AT 2ND I/B HI NGE. REPAIRED PER ER 03-5751-99306-EYI. 2 L 7 2 4F RT A16WE 1999120400375 19991204 00375 NM 1999 12 4 AWXA9900428 1 19991123 A 2131 7638101 CONTROLLER BOEING 737 737301 1384611 NM CABIN PRESSURE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 324AW 41563 24731 23261 IN AUTO PRESS, SYSTEM FAILED TO MAINTAIN CABIN PRESS, STANDBY AND MANUAL MODE FAILED, DUCT PRESS NML AT ALL PWR SETTINGS . INSPECTED DOOR SEALS AND PRESSURIZED CABIN WITH NO DEFECTS NOTED. REPLACED CABIN PRESS CONTROLLER AS PRECAUTION DUE TO PREVIOUS HISTORY PER BMM 21-31-21, TT 0050444. CURRENT HISTORY: 18 NOV AUTO PRESSURIZATION PROB OPS CK'D NO FAULT FOUND PER MM 21-31-00. 21 NOV TROUBLESHOT SYS PLACED ON MEL. RECOMMENDATION: MONITOR CLOSE AFTER PENDING REVIEW OF TE ARDOWN REPORTS. 2 L 7 2 4F RT A16WE 1999120400376 19991204 00376 NM 1999 12 4 AWXA9900429 1 19991124 A 2932 ST107R TRANSMITTER BOEING 737 737112 1384412 NM HYD SYSTEM MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 708AW 19771 ON DEPARTURE, B SYS PRESS INDICATOR WENT TO 500 PSI, NO LOW PRESS LIGHT. CLEANED TRANSMITTER, LK AND OPS CK NORMAL PER MM 29-12-00 AND 29-31-11. 2 L 7 2 4F A16WE 1999120400377 19991204 00377 NM 1999 12 4 AWXA9900430 1 19991127 A 3350 831862 BATTERY PACK BOEING 737 7372E3 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 EMERGENCY EXIT LIGHTS REMAIN ON WITH SWITCH IN ARMED POSITION. REPLACED BATTERY PACKS AT ROW 3L, 11L, AND 17L. 2 L 7 2 4F RT A16WE 1999120400378 19991204 00378 NM 1999 12 4 AWXA9900431 1 19991128 A 3350 831862 BATTERY PACK BOEING 737 7372E3 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 EMERGENCY LIGHTS OUT LAST 6 SEAT ROWS. REPLACED BATTERY PACK AT ROW 18L. CURRENT HISTORY: SEVERAL WRITE-UPS EXPERIENC ED IN LAST FEW FLIGHT HRS. 2 L 7 2 4F RT A16WE 1999120400379 19991204 00379 NM 1999 12 4 AWXA9900432 1 19991128 A 3150 WARNING SYSTEM BOEING 737 7373S3 1384711 NM COCKPIT ACTIVATED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 312AW 24060 TAKEOFF CONFIGURATION WARNING DURING T/O ROLL, ABORTED T/O PRIOR TO 70KTS. AIRCRAFT CONFIG WAS NML FOR T/O CONDITIONS. ACCOMPLISHED TAKEOFF WARNING SYS TEST, NO DEFECTS NOTED. SAME PROBLEM OCCURED 4 NOV 99 AT DFW. CYCLED FLIGHT CONTROLS , CHECKED GOOD. NO PRIOR HISTORY. RECOMMENDATION: IN DEPTH LOOK, TECH SUPPORT CONTACTED. 2 L 7 2 4F RT A16WE 1999120400380 19991204 00380 1999 12 4 AWXA9900433 4 19991128 A 3415 2083111 INDICATOR BOEING 737 7373G7 1384595 NM COCKPIT FAILED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 151AW 31586 292 23219 ON DEPARTURE, HIGH SPEED CLACKER SOUNDED AT APPROXIMATELY 95 KTS. T/O ABORTED. REPLACED F/O'S AIRSPEED INDICATOR TT 00 43116, OPS CK GOOD. CURRENT HISTORY: THIS IS THIRD OCCURANCE OF PROBLEM SINCE 25 NOV, REF LP'S 7569746 AND 7569735. R ECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT. 2 L 7 2 4F RT A16WE 1999120400381 19991204 00381 1999 12 4 AWXA9900434 4 19991128 A 2210 422081100 TRANSDUCER AIRBUS A319 A319132 NM AUTO PILOT FAILED A AWXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 28 658AW 166 162 1110 AMBER FLT CONT ELAC 2 PITCH FAULT MSG ON UPPER ECAM. REPLACED TRIMMABLE HORIZONTAL STABILIZER TRANSDUCER, OPS CK GOOD. CURRENT HISTORY: 27 NOV A/C WAS WRITTEN FOR PITCH FAULT WITH NO FAULT FOUND. REPLACED ELAC2, TEST GOOD. RECOMMENDAT ION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT. 2 L 7 2 4F RT A28NM 1999120400382 19991204 00382 NM 1999 12 4 AWXA9900435 1 19991130 A 3397 13131122 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 156AW 23778 ROW TWO EMERGENCY LIGHT INOP ON SEAT. RE-SPLICED WIRE, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999120400383 19991204 00383 NM 1999 12 4 AWXA9900436 1 19991130 A 3397 13131122 WIRE BOEING 737 7373S3 1384711 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 312AW 24060 ROW 8L EMERGENCY AISLE LIGHT INOP. REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A16WE 1999120400384 19991204 00384 NM 1999 12 4 UPS99231155 1 19991130 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY LIGHT AT FWD ENTRY ABOVE EMERGENCY FLASHLIGHTS WAS INOP. REPLACED BATT AND BULB, OP CHEC KS GOOD. 2 L 7 3 4F A3WE 1999120400385 19991204 00385 NM 1999 12 4 UPS99231156 1 19991130 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF RT AFT OVERWING EMERGENCY EXIT WAS DIM. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999120400386 19991204 00386 NM 1999 12 4 UPS99231157 1 19991130 A 3350 BATTER PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT AFT OF LT FWD OVERWING EXIT WAS DIM. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999120400387 19991204 00387 NM 1999 12 4 UPS99231158 1 19991130 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF LT AFT OVERWING EMERGENCY EXIT INOP. REMOVED AND REPLACED BATTERY PACK AT L T AFT OVERWING EXIT, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999120400388 19991204 00388 NM 1999 12 4 UPS99231159 1 19991130 A 3350 96310322 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, EMERGENCY LIGHT AFT OF FWD RT OVERWING EMERGENCY EXIT INOP, LENS BROKEN. REMOVED AND REPLACED LIGH T ASSY AND BATTERY PACK, OPS CHECK GOOD. LIGHT ASSY (P/N 96-3-1032-2), BATTERY PACK (P/N 96-2-1015). 2 L 7 3 4F A3WE 1999120400389 19991204 00389 EU 1999 12 4 QXEA9902359 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB JUNCTION FITTING UPPER LEFT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169. 2 L 7 2 4F RT A20EU 1999120400390 19991204 00390 EU 1999 12 4 QXEA9902360 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB JUNCTION FITTING LOWER LEFT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169. 2 L 7 2 4F RT A20EU 1999120400391 19991204 00391 EU 1999 12 4 QXEA9902361 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB JUNCTION FITTING LOWER RIGHT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169 . 2 L 7 2 4F RT A20EU 1999120400392 19991204 00392 EU 1999 12 4 QXEA9902362 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB JUNCTION FITTING UPPER RIGHT-HAND LUG HAD PITTING/CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169 . 2 L 7 2 4F RT A20EU 1999120400393 19991204 00393 EU 1999 12 4 QXEA9902363 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB DRIVE FITTING LEFT-HAND UPPER AFT LUG CORRODED. REPAIRED IAW HORIZON AIR EA 4-55-169. 2 L 7 2 4F RT A20EU 1999120400394 19991204 00394 EU 1999 12 4 QXEA9902364 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB DRIVE FITTING AFT LEFT-HAND LOWER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169. 2 L 7 2 4F RT A20EU 1999120400395 19991204 00395 EU 1999 12 4 QXEA9902365 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB DRIVE FITTING AFT RIGHT-HAND UPPER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169. 2 L 7 2 4F RT A20EU 1999120400396 19991204 00396 EU 1999 12 4 QXEA9902366 1 19991117 A 5510 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZONTAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - HORIZONTAL STAB DRIVE FITTING AFT RIGHT-HAND LOWER LUG HAD CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-169. 2 L 7 2 4F RT A20EU 1999120400397 19991204 00397 EU 1999 12 4 QXEA9902367 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4850 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LEFT-HAND OUTBOARD CABIN SEAT TRACK WAS CHAFED AT STATION 4850. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAP H 4. 2 L 7 2 4F RT A20EU 1999120400398 19991204 00398 EU 1999 12 4 QXEA9902368 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4850 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LEFT-HAND INBOARD SEAT TRACK AT STATION 4850 WAS CHAFED AND GOUGED. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARA GRAPH 4. 2 L 7 2 4F RT A20EU 1999120400399 19991204 00399 EU 1999 12 4 QXEA9902369 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 1305 & 9805 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LEFT-HAND INBOARD SEAT TRACK HAD GROOVES WORN IN TRACK BETWEEN STATION 1305 AND 9805. REPAIRED IAW FOKKER SRM 51- 10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400400 19991204 00400 EU 1999 12 4 QXEA9902370 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13551 - 13853 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LEFT-HAND INBOARD SEAT TRACK HAD LIGHT CORROSION PITTING BETWEEN STATION 13551 AND 13853. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400401 19991204 00401 EU 1999 12 4 QXEA9902371 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 6805 - 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT-HAND INBOARD SEAT TRACK HAD LIGHT CORROSION PITTING BETWEEN STATION 6805-8305. REPAIRED IAW FOKKER SRM 51-1 0-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400402 19991204 00402 EU 1999 12 4 QXEA9902372 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 8305 - 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT-HAND INBOARD SEAT TRACK HAD LIGHT PITTING CORROSION AT STATION 8305-9305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400403 19991204 00403 EU 1999 12 4 QXEA9902373 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 10253 - 10753 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT-HAND INBOARD SEAT TRACK HAD LIGHT PITTING CORROSION BETWEEN STATION AF4910253 AND 10753. REPAIRED IAW FOKKE R SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400404 19991204 00404 EU 1999 12 4 QXEA9902374 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4900 - 5805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAD PITTING CORROSION BETWEEN FRAMES 4900-5805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400405 19991204 00405 EU 1999 12 4 QXEA9902375 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9805 - 10253 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS LIGHT PITTING CORROSION BETWEEN STATION 9805 AND 10253. REPAIRED IAW FOKKER SR M 51-10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400406 19991204 00406 EU 1999 12 4 QXEA9902376 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 14793 - 15263 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAD PITTING CORROSION AT STATION 14793 TO 15263. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400407 19991204 00407 EU 1999 12 4 QXEA9902377 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400408 19991204 00408 EU 1999 12 4 QXEA9902378 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400409 19991204 00409 EU 1999 12 4 QXEA9902379 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400410 19991204 00410 EU 1999 12 4 QXEA9902380 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400411 19991204 00411 EU 1999 12 4 QXEA9902381 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400412 19991204 00412 EU 1999 12 4 QXEA9902382 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16660 AND STRINGER 24. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400413 19991204 00413 EU 1999 12 4 QXEA9902383 1 19991109 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - VERTICAL STIFFENER/BRACKET ON LEFT-HAND FORWARD SIDE OF REAR PRESSURE BULKHEAD WAS CRACKED AND HAD TWO POPPED RIVE TS. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999120400414 19991204 00414 EU 1999 12 4 QXEA9902384 1 19991108 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CRACKS IN RADIUS OF FUSELAGE SKIN TO REAR PRESSURE BULKHEAD STIFFENER/ANGLE, BETWEEN STRINGER 48 AND 49. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400415 19991204 00415 EU 1999 12 4 QXEA9902385 1 19991107 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 16660 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS CHAFING DAMAGE TO FRAME 16660 AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 9, VIEW C-C. 2 L 7 2 4F RT A20EU 1999120400416 19991204 00416 EU 1999 12 4 QXEA9902386 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400417 19991204 00417 EU 1999 12 4 QXEA9902387 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400418 19991204 00418 EU 1999 12 4 QXEA9902388 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400419 19991204 00419 EU 1999 12 4 QXEA9902389 1 19991110 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU BS 3820 - 4610 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - MINOR PITTING CORROSION ON TOP OF FLOORBEAM 600L BETWEEN FRAME 3820 AND 4610. REPAIRED IAW FOKKER SRM 51-10-04, P AGE 9. 2 L 7 2 4F RT A20EU 1999120400420 19991204 00420 1999 12 4 QXEA9902390 4 19991120 A 3451 MOUNT FOKKER F28 F28MK4000 4990810 EU DME ANTENNA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AIR FRAME MOUNTING SURFACE FOR DME 2 ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1999120400421 19991204 00421 1999 12 4 QXEA9902391 4 19991111 A 3451 MOUNT FOKKER F28 F28MK4000 4990810 EU DME ANTENNA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AIR FRAME MOUNTING SURFACE FOR DME 1 ANTENNA IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999120400422 19991204 00422 1999 12 4 QXEA9902392 4 19991105 A 3416 MOUNT FOKKER F28 F28MK4000 4990810 EU ALT ANTENNA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AIR FRAME MOUNTING SURFACE FOR AFT RAD ALT ANTENNA IS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 1999120400423 19991204 00423 1999 12 4 QXEA9902393 4 19991111 A 3434 MOUNT FOKKER F28 F28MK4000 4990810 EU M/B ANTENNA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AIR FRAME MOUNTING SURFACE FOR MARKER BEACON ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARA GRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400424 19991204 00424 1999 12 4 QXEA9902394 4 19991105 A 3416 MOUNT FOKKER F28 F28MK4000 4990810 EU ALT ANTENNA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AIR FRAME MOUNTING SURFACE FOR FORWARD RAD ALT ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9. 2 L 7 2 4F RT A20EU 1999120400425 19991204 00425 1999 12 4 QXEA9902395 4 19991111 A 3452 MOUNT FOKKER F28 F28MK4000 4990810 EU ATC ANTENNA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AIR FRAME MOUNTING SURFACE FOR LOWER ATC ANTENNA WAS CORRODED. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAP H 4 B&C. 2 L 7 2 4F RT A20EU 1999120400426 19991204 00426 EU 1999 12 4 QXEA9902436 1 19991112 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU BS 2650 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - LEFT-HAND ACM BAY INNER WALL HAD 4 GOUGE MARKS APPROXIMATELY .25 INCH LONG AND RANGE FROM APPROXIMATELY .003 - .00 5 DEEP AT FUSELAGE STATION 2650, 13 INCHES FROM BOTTOM OF WALL. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B &C. 2 L 7 2 4F RT A20EU 1999120400427 19991204 00427 EU 1999 12 4 QXEA9902437 1 19991112 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - RIGHT-HAND ACM BAY INNER WALL HAD 2 DENTS JUST FORWARD OF LOWER/AFT ACM MOUNT. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B&C. 2 L 7 2 4F RT A20EU 1999120400428 19991204 00428 EU 1999 12 4 QXEA9902438 1 19991113 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 9305B CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FORWARD CARGO BAY CORROSION UNDER TWO NUT PLATES ON FRAME 9305B ABOVE STRINGER 74. REPAIRED IAW FOKKER SRM 51-10- 04, PAGE 8 FIGURE 3. 2 L 7 2 4F RT A20EU 1999120400429 19991204 00429 EU 1999 12 4 QXEA9902439 1 19991111 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 9305A CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FORWARD CARGO BAY CORROSION UNDER NUT PLATES AND ON FLANGE OF FRAME 9305A BETWEEN STRINGERS 74 AND 1. REPAIRED IA W FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH 3. 2 L 7 2 4F RT A20EU 1999120400430 19991204 00430 EU 1999 12 4 QXEA9902440 1 19991118 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FORWARD CARGO BAY CORROSION ON UNDERSIDE OF UPPER FLANGE OF FRAME 9305 ABOVE STRINGER 2, UNDER AND AROUND NUT PLAT E. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1999120400431 19991204 00431 EU 1999 12 4 QXEA9902441 1 19991114 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 17565 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE SKIN IS DENTED IN FOUR AREAS JUST FORWARD OF FRAME 17565, BETWEEN STRINGERS 55-59. REPAIRED IAW FOKKER S RM 53-02-02, FIGURE 1. 2 L 7 2 4F RT A20EU 1999120400432 19991204 00432 EU 1999 12 4 QXEA9902442 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE WAS A CRACKED CLIP AT FRAME 16060 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999120400433 19991204 00433 EU 1999 12 4 QXEA9902443 1 19991116 A 5210 HINGE FOKKER F28 F28MK4000 4990810 EU PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - PASSENGER DOOR HINGE IS WORN TO LIMITS. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999120400434 19991204 00434 NM 1999 12 4 99FDEA00491 1 19991130 A 2613 OVERHEAT LOOP BOEING 727 72722C 138400F NM NR 1 ENGINE INOP A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 104FE 19198 NR 1 ENG STRUT FLICKERED ON T/O ROLL MOMENTARILY AND THEN EXTINGUISH AT 4,000' ALT, LIGHT ILLUM STEADY. *S/D* REMOVED AND REPLACED OVERHEAT LOOP PER MM 26-14-1, LEAK CK NORMAL. LIGHT OPER CK NORM. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999120400435 19991204 00435 1999 12 4 MWEA99849 4 19991123 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP SERVICE DOOR LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 GALLEY SERVICE DOOR EMERGENCY ESCAPE SLIDE WAS DETACHED FROM HOUSING. MAINTENANCE REINSTALLED SLIDE. 2 L 7 2 4F A6WE 1999120400436 19991204 00436 1999 12 4 MWEA99850 4 19991129 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP SERVICE DOOR LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 THE FORWARD GALLEY DOOR EMERGENCY EVACUATION SLIDE CAME OUT OF ITS COVER. MAINTENANCE REINSTALLED SLIDE AND COVER. 2 L 7 2 4F A6WE 1999120400437 19991204 00437 WP 1999 12 4 MWEA99851 1 19991129 A 2120 UNKNOWN DOUG DC9 DC932 3022066 WP COCKPIT ODOR A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 401ME 47133 FLIGHT CREW DETECTED STRONG PRESENTS OF HOT ELECTRICAL ODOR. MTC INSPECTED COCKPIT, GLARESHIELD, CIRCUIT BREAKER PANELS , E/E COMPARTMENT, NOSE AREA, RADIO RACK FAN FOR OPERATION, ACCM. OIL AND OPERATION. ALL FOUND NORMAL RAN NR 1 ENGINE A ND RIGHT AIR CONDITIONING PACK. NO ODOR NOTED. 2 L 7 2 4F A6WE 1999120400438 19991204 00438 NE 1999 12 4 MWEA99852 2 19991130 A 7230 500361301 BLADE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE COMPRESSOR DAMAGED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 301ME 47190 ON CLIMBOUT AFTER TAKEOFF, LEFT ENGINE BEGAN TO COMPRESSOR STALL. MAINTENANCE FOUND FOREIGH OBJECT DAMAGE TO 13 STAGE C OMPRESSOR BLADES. REPLACED ENGINE WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1999120400439 19991204 00439 1999 12 4 SWIA971601 4 19991114 A 3454 6226137001 TRANSCEIVER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE VOR SYSTEM INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 203SW 120240 NR 2 NAV RADIO INOP DURING FLIGHT. RETURNED TO SFO. INSTALLED SERVICEABLE NR 2 NAV RECEIVER, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999120400440 19991204 00440 SO 1999 12 4 SWIA971602 1 19991117 A 3260 SENSOR EMB 120 EMB120RT SO PWA 118 PW118 NE MLG FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 161CA 120143 AFTER TAKEOFF, CYCLED GEAR AND IT DID NOT RETRACT. CYCLED GEAR 4 TIMES AND IT STILL DID NOT WORK. RETURNED TO SEA. IN STALLED NEW LEFT MAIN GEAR A UPLOCK SENSOR PER EMB 120 MM 32-61-01. PERFORMED GEAR SWING, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999120400441 19991204 00441 SO 1999 12 4 SWIA971603 1 19991117 A 3610 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PNEUMATIC SYSTEM MALFUNCTIONED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 203SW 120240 RIGHT DUCT LEAK LIGHT ILLUMINATED ON CLIMBOUT BUT WENT OUT AFTER CLOSING BLEED. INSTALLED 31 PSI REGULATING VALVE FOR R IGHT HAND SIDE. RAN ENGINE AT FULL AND CRUISE POWER FOR 20 MINUTES, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1999120400442 19991204 00442 SO 1999 12 4 SWIA971604 1 19991117 A 3010 DEICE BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE VERTICAL STAB FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 294SW 120321 OUTBOARD, MIDDLE LEFT WING AND VERTICAL STABILIZER DEICE BOOTS FAILED. RETURNED TO SLC. REMOVED AND REPLACED DEICE MON ITOR IAW 30-00-01, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999120400443 19991204 00443 SO 1999 12 4 SWIA971605 1 19991120 A 3230 MLG EMB 120 EMB120RT SO PWA 118 PW118A NE LEFT MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 270YV 120270 WHEN LANDING GEAR HANDLE SELECTED TO UP POSITION AFTER TAKEOFF, RIGHT MAIN UPLOCK BUT WOULD NOT RETRACT. LEFT MAIN NOSE GEAR RETRACTED NORMALLY. A LOUD RATTLING NOISE WAS CONTINUOUSLY HEARD WHEN GEAR RETRACTION WAS ATTEMPTED. ALL 3 GEARS DID DOWNLOCK NORMALLY. RETURNED TO LAX. INSPECTED RIGHT MAIN GEAR, OPERATED GEAR UP AND DOWN MANY TIMES. NO NOISE WA S HEARD AND NO DISCREPANCY NOTED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999120400444 19991204 00444 SO 1999 12 4 SWIA971606 1 19991117 A 5270 SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE SERVICE DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 137H 120137 SERVICE DOOR LIGHT CAME ON AT ROTATION. RETURNED TO FIELD. FOUND OUTBOARD FUEL SERVICE DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED MICROSWITCH, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999120400445 19991204 00445 NM 1999 12 4 VNAA9911021 1 19991125 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 07 425JS 9793 3037 THE FLIGHT CREW FOUND EMERGENCY LIGHTS 4, 5, 6, AND 7 NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPEC TED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK LOCATION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPER ATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999120400446 19991204 00446 NM 1999 12 4 VNAA9911022 1 19991127 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 07 461PS 6351 238 3075 THE FLIGHT CREW FOUND EMERGENCY LIGHTS AT THE 4LK POSITION NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENC Y BATTERY AT THE 4LK LOCATION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999120400447 19991204 00447 NE 1999 12 4 VNAA9911024 2 19991129 A 7322 311703603 HMU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 438JS 7880 3056 116122 DURING TAKEOFF, THE RIGHT HAND ENGINE WOULD ONLY PRODUCE 86 PERCENT TORQUE. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECTED AND REPLACED THE HYDRO MECHANICAL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-22-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED F OR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999120400448 19991204 00448 1999 12 4 VNAA9911025 4 19991130 A 6113 001A716E1000010 SPINNER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE BIRD STRIKE A VNAA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 GL 07 437JS 9045 3055 116145 DURING TAKEOFF, THE RIGHT HAND ENGINE SUSTAINED A BIRD STRIKE. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE FIELD W ITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE PROPELLER SPINNER IN ACCORDANCE WITH DORNIER MAINTENANC E MANUAL 61-13-00 AND THE INTAKE ASSEMBLY IN ACCORDANCE DORNIER MAINTENANCE MANUAL 71-63-00. OPERATIONAL CHECKS WERE PE RFORMED AND THE AIRCRAFT WAS FERRIED TO DAYTON WHERE MAINTENANCE PERFORMED A BORESCOPE INSPECTION IN ACCORDANCE WITH DOR NIER MAINTENANCE MANUAL 72-00-00. THE INSPECTION SHOWED NO INJESTATION AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999120400449 19991204 00449 EU 1999 12 4 AALA991450 1 19990921 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59081 639 MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH TRACK LIGHTING AT ROW 21B INOPERATIVE. REPAIRED WIRE SPLIC E AT ROW 21B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999120400450 19991204 00450 EU 1999 12 4 AALA991421 1 19990920 A 3350 P4010051124 CHARGER UNIT AIRBUS 300 A300B4605R 3930308 EU ROW 6G DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 1084 615 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM SEAT ROW 6G TO 18G INOPERATIVE. REPLACED PO WER SUPPLY UNIT TO EMERGENCY EXIT FLOOR PATH LIGHTING FROM SEAT ROWS 6G TO 18G. SYSTEM GROUND CHECKED, NORMAL OPERATION . (X) 2 L 7 2 4F RT A35EU 1999120400451 19991204 00451 EU 1999 12 4 AALA991376 1 19990911 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ROWS 24-25 MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70079 619 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP BETWEEN SEATS 24B AND 25B MISSING. REPLACE D EMERGENCY EXIT FLOOR PATH LIGHTING STRIP BETWEEN SEATS 24B AND 25B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999120400452 19991204 00452 EU 1999 12 4 AALA991377 1 19990911 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70079 619 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT AFT CABIN CROSS AISLE INOPERATIVE. REPL ACED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT AFT CABIN CROSS AISLE. SYSTEM GROUND CHECKED, NORMAL OPER ATION. (X) 2 L 7 2 4F RT A35EU 1999120400453 19991204 00453 EU 1999 12 4 AALA991370 1 19990910 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 19059 469 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT R1 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999120400454 19991204 00454 NM 1999 12 4 AALA991667 1 19991108 A 2530 8609010000 OVEN BOEING 767 767323 1385205 NM GALLEY DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 378AN 25447 MAD - FLT 0068 - EN ROUTE MIA/MAD, NR 2 FIRST CLASS GALLEY OVEN EMITTED SMOKE AND SPARKS. CIRCUIT BREAKER PULLED AND AI RCRAFT CONTINUED TO MAD AND LANDED WITHOUT INCIDENT. CLEANED DIRT AND FOOD RESIDUE FROM NR 2 FIRST CLASS CABIN OVEN AND FAN. OVEN OPERATED FOR 20 MINUTES AT ALL POWER SETTINGS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999120400455 19991204 00455 NM 1999 12 4 AALA6027 1 19991027 A 3010 12294411 ANTI-ICE VALVE DOUG MD90 MD9030 3023690 NM LT MLG WW FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 902RA 53490 SJC - DURING CLIMB-OUT, AIR FOIL ANTI-ICE WAS TURNED ON. CABIN IMMEDIATLEY STARTED A CLIMB. FLOW LIGHT CAME ON, AND CA BIN AIR BECAME HOT AND SMOKEY. LEVELLED AT 21,000 FEET AND SYSTEM RETURNED TO NORMAL. PERFORMED HIGH POWER ENGINE RUN. FOUND WING ANTI-ICE VALVE INOPERATIVE. REMOVED AND REPLACED THE WING ANTI-ICE SHUTOFF VALVE PER MM 30-11-01. (X) 2 L 7 2 4F RT A6WE 1999120400456 19991204 00456 EU 1999 12 4 REXA99032 1 19991031 A 2910 GPP125012 SWITCH SAAB SF340 340B 7860101 EU HYDRAULIC SYSTEM FAILED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 367PX 340B271 PILOT REPORTED LOSS OF HYDRAULIC PRESSURE. PERFORMED EMERGENCY EXTENSION OF THE LANDING GEAR AND DECLARED AN IN-FLIGHT EMERGENCY. REMOVED AND REPLACED THE HYDRAULIC PRESSURE SWITCH. REMOVED AND REPLACED THE EXPLOSIVE BOLTS ON LEFT AND RI GHT MLG DOORS AND PERFORMED FUNCTIONAL/OPERATIONAL CHECK OF LANDING GEAR. SYSTEM CHECKED GOOD. (X) 2 L 7 2 4T RT A52EU 1999120400457 19991204 00457 NM 1999 12 4 P2EA99308 1 19991016 A 2810 65507532 FITTING BOEING 737 737244 138448U NM RT WING CRACKED A P2EA O OTHER K FLUID LOSS IN INSP/MAINT 1 CE 05 620PC 55424 19708 MCI - RUNNING FUEL LEAK AT RIGHT WING ROOT, LOWER SURFACE AT WING-TO-BODY AREA NEAR SUMP DRAIN. PRESSURE CHECKED. CLEA NED AND SEALED LEAK AREA. LEAK NOW CLASSIFIED AS STAIN PER MM 28-11-0. FOUND TIE FITTING CRACKED IN RADIUS, BL 70.85. STRINGER S9R WING LOWER SURFACE. REPLACED RT WING LOWER TIE FITTING AND FEED-THROUGH TUBE, BL 70.85, STR S9 PER SRM 51- 30-2 AND BAC DRAWING 65-45414. PART TC: 59,093. (X) 2 L 7 2 4F A16WE 1999120400458 19991204 00458 NM 1999 12 4 P2EA99309 1 19991031 A 2780 DETENT ARM BOEING 737 737222 1384473 NM LE SLAT OUT OF ADJUST A P2EA O OTHER O OTHER AP APPROACH 1 CE 05 208AU 19547 MDW - FLT 277 - FLAPS 1 THROUGH 25 SELECTED, NR 6 LEADING EDGE SLAT EXTENDS CROOKED. FLAPS 30 THROUGH 40 SELECTED, NR 6 LEADING EDGE SLAT GOES TO FULL EXTEND. ADJUSTED DETENT ARMS ON NR 6 L/E SLAT PER MM 27-81-0A. OPS CHECKS NORMAL. (X) 2 L 7 2 4F A16WE 1999120400459 19991204 00459 WP 1999 12 4 GAIA99165 1 19991102 A 5330 5910934 SKIN DOUG DC9 DC915F 3022037 WP BS 340 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING B-CHECK INSPECTION, FOUND A DENT ABOVE THE FORWARD BAGGAGE BIN. THE SKIN WAS REPAIRED IAW DC-9 SRM. THE AIRCRAF T WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F A6WE 1999120400460 19991204 00460 WP 1999 12 4 GAIA99164 1 19991102 A 5330 5910593 SKIN DOUG DC9 DC915F 3022037 WP BS 110 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING B-CHECK INSPECTION, FOUND A DENT BELOW THE RIGHT COCKPIT SLIDING WINDOW. THE SKIN WAS REPAIRED IAW DC-9 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F A6WE 1999120400461 19991204 00461 WP 1999 12 4 GAIA99162 1 19991105 A 5320 991557815 INTERCOSTAL DOUG DC9 DC915F 3022037 WP BS 710 TO 718 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE INTERCOSTAL FROM STA 710 TO STA 718 BETWEEN L29L TO L30. THE INTERCOS TAL WAS REPLACED IAW DC-9 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F A6WE 1999120400462 19991204 00462 NM 1999 12 4 GAIA99163 1 19991028 A 3020 ANTI-ICE VALVE BOEING 727 727223 1384074 NM NR 3 ENGINE LOOSE A GAIA K NONE M OVER TEMP CL CLIMB 1 SW 07 6811 19486 DEN/MHR - FLT 2015 - FOUR MINUTES AFTER TAKEOFF DURING CLIMB-OUT PASSING THROUGH 10,000 FEET, THE NR 3 ENGINE STRUT OVER HEAT LIGHT ILLUMINATED WITH 42 PSI DUCT PRESSURE. RAN ABNORMAL CHECKLIST AND LIGHT REMAINED EXTINGUISHED AT CRUISE THRU ST. THE AIRCRAFT CONTINUED ON TO MHR AND MADE A ROUTINE LANDING. MAINTENANCE TIGHTENED BOLTS ON 13TH STAGE ANTI-ICE VA LVE, REPOSITIONED CLAMP ON ANTI-ICE DUCTING. RAN ENGINE AT TAKEOFF POWER FOR 5 MINUTES. LEAKED CHECKED OKAY. STRUT OVE RHEAT LIGHT REMAINED EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999120400463 19991204 00463 NM 1999 12 4 GAIA99167 1 19991108 A 3260 106122615 SENSOR BOEING 727 727251 138408H NM RT MLG OUT OF ADJUST A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 252US 19971 CLT/PHL - FLT 2811 - DURING CLIMB-OUT, RETRACTED THE LANDING GEAR AND THE RIGHT MAIN LANDING GEAR LIGHT REMAINED ON WITH THE GEAR RETRACTED AND THE GEAR HANDLE IN THE UP POSITION. WHEN THE GEAR HANDLE WAS SELECTED TO THE OFF POSITION, THE RIGHT MAIN GEAR LIGHT WENT FROM ON TO OFF IN APROXIMATELY ONE MINUTE. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT FURTHER DIFFICULTIES. THE AIRCRAFT MAINTENANCE FERRIED TO INT FOR A GEAR RETRACTION TEST. TROUBLESHOOTING REVEALED THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR WAS OUT OF ADJUSTMENT. ADJUSTED THE RIGHT MLG UPLOCK SENSOR PER B727 MM 32-61-81 . OPERATIONALLY CHECKED GOOD PER B727 MM 32-61-0. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999120400464 19991204 00464 NM 1999 12 4 GAIA99166 1 19991108 A 3260 INDICATION BOEING 727 727251 138408H NM LANDING GEAR MALFUNCTIONED A GAIA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 252US 19971 ATL/CLT - FLT 518 - DURING CLIMB-OUT, RETRACTED THE LANDING GEAR AND THE RIGHT MAIN LANDING GEAR LIGHT REMAINED ON WITH THE GEAR RETRACTED AND THE GEAR HANDLE IN THE UP POSITION. WHEN THE GEAR HANDLE WAS SELECTED TO THE OFF POSITION, THE R IGHT MAIN GEAR LIGHT WENT FROM ON TO OFF. THE AIRCRAFT CONTINUED TO CLT AND LANDED WTHOUT FURTHER DIFFICULTIES. PERFOR MED A LANDING GEAR ELECTRIC MODULE TEST PER B727 MM 32-09-121. OPERATIONALLY CHECKED GOOD ON GROUND AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999120400465 19991204 00465 NM 1999 12 4 UIEA9996 1 19991104 A 5753 BACB30LM58P BOLT BOEING 747 7472D7B 1384803 NM NR 2 TE AFT FLAP LOOSE A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 60910 11888 22472 INSPECTION OF NR 2 INBOARD AFT FLAP TRACK CARRIAGE BOGIE PIN ASSY REVEALED SAFETY BOLT MIGRATED OVER .50 INCH. NO PIN MI GRATION DUE PIN HELD IN PLACE BY ROLLER SUPPORT ROD. THIS CONFIGURATION DOES NOT REQUIRE SAFETY WIRE FROM BOLT TO PIN. REMOVED BOLT, INSPECTED, FOUND OK. RE-INSTALLED AND TORQUED TO 240 INCHES - 260 INCHES PER BOEING RECOMMENDATION. RE- TORQUED REMAINING SEVEN POSITIONS PRECAUTIONARY. ATLAS AIR IS CURRENTLY PROCESSING AN FCD TO INSPECT THE REMAINDER OF T HE -200 FLEET. ATLAS WILL ALSO CREATE A TASK CARD TO ROUTINELY RE-TORQUE SAFETY BOLT DURING A-CHECKS UNTIL THE PIN AND BOLT COMBINATION CAN BE REPLACED WITH A DRILLED ASSEMBLY. (X) 2 L 7 4 4F RT A20WE 1999120400466 19991204 00466 NM 1999 12 4 99ZZZX4337 1 19991030 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 429EX 19100 CLT/GSO - FLT 613 - ENGINE NR 3 FIRE PROTCTION SYSTEM ENGINE DETECTOR LIGHT COMES ON INTERMITTENTLY IN-FLIGHT. REPOSITI ONED NR 3 ENGINE FIRE DETECTION LOOP. (X) 2 L 7 3 4F A3WE 1999120400467 19991204 00467 NM 1999 12 4 99ZZZX4338 1 19991027 A 2120 AIR DISTRIBUTION BOEING 727 72721 1384003 NM COCKPIT ODOR A RYNA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 359QS 19007 CLT/IND - FLT 713 - FUEL ODOR SMELL IN COCKPIT WITH PACK(S) OPERATING. OPERATED PACKS FOR SEVERAL MINUTES, FUEL ODOR DI SSIPATED, ALL OPERATIONS NORMAL. (X) 2 L 7 3 4F A3WE 1999120400468 19991204 00468 NM 1999 12 4 99ZZZX4339 1 19991026 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 428EX 19097 MCI/STL - FLT 716 - NR 3 DETECTOR CIRCUIT GROUND ILLUMINATED AFTER TAKEOFF, LIGHT GOES OUT WHEN THROTTLE IS REDUCED. (D EFERRED IN STL, CLEARED IN TPA). VISUALLY INSPECTED FIRE LOOP AND FOUND LOOP GROUNDING ON BRACKET JUST FORWARD OF DRAIN BOX, REPOSITIONED LOOP. (X) 2 L 7 3 4F A3WE 1999120400469 19991204 00469 NM 1999 12 4 99ZZZX4340 1 19991026 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 421EX 19099 MSY/IND - FLT 708 - NR 3 ENGINE FIRE DETECTION GROUND FAULT LIGHT IS ILLUMINATED. (DEFERRED IN IND, CLEARED IN EWR). F OUND FIRE LOOP RESTING ON LOWER ENGINE COWLING. RE-POSITIONED FIRE LOOP. 2 L 7 3 4F A3WE 1999120400470 19991204 00470 NM 1999 12 4 99ZZZX4341 1 19991024 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 421EX 19099 EWR/IND - FLT 711 - NR 3 GROUND FAULT LIGHT ILLUMINATED ALL OF THE TIME. (DEFERRED IN IND, CLEARED IN IAH). REPOSITION ED FIRE LOOP. (X) 2 L 7 3 4F A3WE 1999120400471 19991204 00471 NM 1999 12 4 99ZZZX4342 1 19991023 A 2611 308 BULB BOEING 727 72722C 138400F NM SMOKE DETECTOR FAILED A RYNA O OTHER P NO WARNING INDICATION CR CRUISE 1 CE 07 429EX 19100 DSM/MCI - FLT 635 - LOWER SMOKE DETECTOR LIGHTS INOPERATIVE. RE-LAMPED LOWER SMOKE DETECTOR LIGHTS. 2 L 7 3 4F A3WE 1999120400472 19991204 00472 EU 1999 12 4 99ZZZX4343 1 19991022 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A RYNA O OTHER L NO TEST IN INSP/MAINT 1 CE 07 GSUEE 363 SFO - FLT 8162 - FORWARD EMERGENCY EXIT LIGHTS, NO ILLUMINATION. REPLACED BATTERY TO POWER SUPPLY UNIT. 2 L 7 2 4F RT A28NM 1999120400473 19991204 00473 1999 12 4 ARWA991101 4 19991109 A 3442 20675680501 ANTENNA DOUG DC8 DC863F 302198F WP WX RADAR FAILED A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 661AV 1527 45969 MIA - FLT 517 - AIR TURNBACK, DURING CLIMB-OUT OF MIAMI, LOST WEATHER RADAR, TEST GOOD ON GROUND. REMOVED AND REPLACED RADAR ANTENNA. CLEANED CONNECTORS ON VIDEO CABLE AND RADAR SCOPE. RETURN AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1999120400474 19991204 00474 SO 1999 12 4 ASOA99140 1 19991102 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 241AS 18346 120065 DURING INSPECTION, FOUND NR 2 EMERGENCY BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY BATTERY. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400475 19991204 00475 SO 1999 12 4 ASOA99139 1 19991101 A 3010 D55201001 MONITOR EMB 120 EMB120RT SO WING DE-ICE INOPERATIVE A ASOA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 266AS 11075 28 120188 FLT 4328 - DE-ICE BOOTS AND PROPELLER HEAT FAILED AT 19,000 FEET IN LIGHT TO MODERATE ICE. BOTH BOOTS FAILED. CREW DEC LARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED THE DE-ICE MONITOR. OPERATIONAL CHECKS WERE GOOD. N O DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999120400476 19991204 00476 SO 1999 12 4 ASOA99138 1 19991031 A 5311 FRAME EMB 120 EMB120RT SO FRAME 22 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 273AS 120222 DURING INSPECTION, MAINTENANCE FOUND CORROSION AT FRAME 22. MAINTENANCE REPAIRED CORROSION IAW EO 120-53-0123. OPERATI ONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400477 19991204 00477 SO 1999 12 4 ASOA99137 1 19991030 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 247AS 120113 DURING INSPECTION, FOUND NR 1 EMERGENCY BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400478 19991204 00478 SO 1999 12 4 ASOA99136 1 19991029 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 267AS 120198 DURING INSPECTION, FOUND NR 1 EMERGENCY BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400479 19991204 00479 NM 1999 12 4 USAA990918 1 19990824 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727E CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 40461 22957 CLT - DURING RON CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK JUST BELOW STR 18R AT STA 727E PLUS 1.5 INCHES TO 727E PLUS 4 INCHES FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (X) 2 L 7 2 4F RT A16WE 1999120400480 19991204 00480 NM 1999 12 4 USAA990928 1 19990817 A 5320 FRAME BOEING 737 737301 1384611 NM R1 DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40865 23514 PIT - DURING RON, FOUND .8750 INCH CRACK IN RADIUS OF Z-ANGLE DOOR FRAME AT R1 ABOVE BOTTOM HINGE CUT-OUT IN DOOR OPENIN G. STOP DRILLED CRACK, INSTALLED TITANIUM DOUBLER PER SRM 53-10-15, FIG 3, SH 2/ER 07-07-90/EA 52711. (X) 2 L 7 2 4F RT A16WE 1999120400481 19991204 00481 NM 1999 12 4 USAA990715 1 19990729 A 5311 65C25229 FRAME BOEING 737 737301 1384611 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN FRAME AT STA 727D, RBL 2. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-00-07 AND EA 65131 PAGES 1 AND 2. (X) 2 L 7 2 4F RT A16WE 1999120400482 19991204 00482 NM 1999 12 4 USAA990716 1 19990729 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 306 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN STRINGER AT STA 306 STR 4L. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-15. (X) 2 L 7 2 4F RT A16WE 1999120400483 19991204 00483 NM 1999 12 4 USAA990718 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 600 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 600 STR 8L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X) 2 L 7 2 4F RT A16WE 1999120400484 19991204 00484 NM 1999 12 4 USAA990797 1 19990803 A 5321 FLOORPAN BOEING 737 737301 1384611 NM BS 1024 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION 2 INCH BY 2 INCH AT STA 1024, RBL 6, WL 208 FLOORPAN. CORROSION LEVEL 1, CORROSION NR C53-107-02. FABRICATED NEW STRAP PER DRAWING 6546812 AND SRM 51-10-02. (X0 2 L 7 2 4F RT A16WE 1999120400485 19991204 00485 NM 1999 12 4 USAA990799 1 19990803 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 908 STR 9L. REPAIRED PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400486 19991204 00486 NM 1999 12 4 USAA990793 1 19990803 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 1020 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES STA 1020, LBL 9, WL 208 INTERCOSTAL. CO RROSION LEVEL 1, CORROSION NR C53-107-02. REPLACED CAP PER SRM 53-10-51. (X) 2 L 7 2 4F RT A16WE 1999120400487 19991204 00487 NM 1999 12 4 USAA990796 1 19990803 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 1010 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES STA 1010, LBL 12, WL 208 INTERCOSTAL. C ORROSION LEVEL 1, CORROSION NR C53-107-02. (X) 2 L 7 2 4F RT A16WE 1999120400488 19991204 00488 NM 1999 12 4 USAA990763 1 19990803 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 773 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 74131 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION FOUND A 4 INCH BY 1 INCH AREA OF CORROSION AT STA 773, LBL 3 FLOORBEAM AFT CA RGO. CORROSION LEVEL 2. CUT OUT CORROSION, INSTALLED REPAIR ANGLE, DOUBLER PER TR 53-10-06, SRM'S 51-30-09, 51-10-02, 5 1-20-01/05. (X) 2 L 7 2 4F RT A16WE 1999120400489 19991204 00489 NM 1999 12 4 USAA990764 1 19990803 A 5330 SKIN BOEING 737 737301 1384611 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH SKIN ATTACH CHORD CRACK STA 1016 BETWEEN STR 3R AND STR 4L. F ABRICATED, SPLICE ANGLES PER EA 65021. (X) 2 L 7 2 4F RT A16WE 1999120400490 19991204 00490 NM 1999 12 4 USAA990657 1 19990803 A 5320 65353522 TIE CLIP BOEING 737 737301 1384611 NM BS 1006 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 1006 AT FIRST STRINGER ABOVE FLOOR LEVEL ON RT SI DE TIE CLIP. REPLACED WITH IDENTICAL PART. (X) 2 L 7 2 4F RT A16WE 1999120400491 19991204 00491 NM 1999 12 4 USAA990658 1 19990803 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 616 STR 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400492 19991204 00492 NM 1999 12 4 USAA990659 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 807 BETWEEN STR 8 AND STR 9R IN FUSELAGE FRAME AT FASTENER HOLE. INSTALLED DOUBLER PER SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999120400493 19991204 00493 NM 1999 12 4 USAA990660 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STR 8 AND STR 9R IN FUSELAGE FRAME AT FASTENER HOLE. FABRICATED REPAIR ANGLE AND FILLER INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (X) 2 L 7 2 4F RT A16WE 1999120400494 19991204 00494 NM 1999 12 4 USAA990661 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STR 8 AND STR 9L IN FUSELAGE FRAME AT FASTENER HOLE. INSTALLED DOUBLER. (X) 2 L 7 2 4F RT A16WE 1999120400495 19991204 00495 NM 1999 12 4 USAA990674 1 19990803 A 5320 WEB BOEING 737 737301 1384611 NM BS 305.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK SHEAR WEB LOWER CHORD STA 305.5 STR 4L. INSTALLED DOUB LER PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 1999120400496 19991204 00496 NM 1999 12 4 USAA990675 1 19990803 A 5320 BEAM BOEING 737 737301 1384611 NM BS 712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK LOWER WEB OF RBL 25 AT STA 712 WL 203 BEAM. INSTALLED DOUBLER PER SRM 51-70-13. (X) 2 L 7 2 4F RT A16WE 1999120400497 19991204 00497 NM 1999 12 4 USAA990676 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 480 BETWEEN STR 8 AND STR 9L. CUT-OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (X) 2 L 7 2 4F RT A16WE 1999120400498 19991204 00498 NM 1999 12 4 USAA990677 1 19990803 A 5330 6547952524M SKIN BOEING 737 737301 1384611 NM CARGO DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 DLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK UPPER AFT CORNER OF CUT-OUT FOR ACCESS TO EXTERNAL DO OR HANDLE AFT CARGO DOOR EXTERIOR SKIN. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 52-00-3. (X) 2 L 7 2 4F RT A16WE 1999120400499 19991204 00499 NM 1999 12 4 USAA990678 1 19990803 A 5320 WEB BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT LBL 25 WEB AT HOLES 707, 708, 709, 710, AND 713, W L 203. INSTALLED DOUBLER PER SRM 51-70-13. (X) 2 L 7 2 4F RT A16WE 1999120400500 19991204 00500 NM 1999 12 4 USAA990679 1 19990803 A 5311 FRAME BOEING 737 737301 1384611 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 400 BETWEEN STR 8R AND STR 9R. INSTALLED DOUBLER PER SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1999120400501 19991204 00501 NM 1999 12 4 USAA990706 1 19990803 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK 1.5 INCHES AFT OF STA 663.75 AT BL ZERO BEAM (FRAME). I NSTALLED FLOORBEAM REPAIR PER EA 64999 AND BOEING SB 737-57-1210 FIG 4 AND 8. (X) 2 L 7 2 4F RT A16WE 1999120400502 19991204 00502 NM 1999 12 4 USAA990707 1 19990803 A 5330 SKIN BOEING 737 737301 1384611 NM BS 324 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK FORWARD SERVICE DOOR AFT LOWER CUT-OUT BS 324, WL 211 SKIN. INSTALLED DOUBLER AND FILLERS PER SRM 53-10-01. (X) 2 L 7 2 4F RT A16WE 1999120400503 19991204 00503 NM 1999 12 4 USAA990708 1 19990803 A 5320 693535214 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 616 STR 1 TIE CLIP. INSTALLED NEW CLIP PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1999120400504 19991204 00504 NM 1999 12 4 USAA990709 1 19990803 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA VARIOUS SIZES AND PLACES ON Z-ANGLE/GIRT BAR MOUNTS FORW ARD ENTRY DOOR AT BS 312 TO BS 344. INSTALLED NEW Z-ANGLE AND GIRT BAR MOUNTS PER SRM 51-40-02 AND SRM 53-10-15. (X) 2 L 7 2 4F RT A16WE 1999120400505 19991204 00505 NM 1999 12 4 USAA990711 1 19990803 A 5320 CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT STRINGER TIE CLIP STA 616 STR 2R. INSTALLED DOUBLER PER SRM 53-00-03. (X) 2 L 7 2 4F RT A16WE 1999120400506 19991204 00506 NM 1999 12 4 USAA990751 1 19990803 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .75 INCH CRACK AND 5 INCH CRACK IN SKIN AROUND PANEL 5724L. INSTALLED DOUBLER PER TR 54-40-040. (X) 2 L 7 2 4F RT A16WE 1999120400507 19991204 00507 NM 1999 12 4 USAA990752 1 19990803 A 5312 BULKHEAD ANGLE BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5 .7, WL 181 T-ANGLE. FABRICATED 2 ANGLES AND 1 STRAP PER SRM 53-10-08 FIG 205 SHEET 12. (X) 2 L 7 2 4F RT A16WE 1999120400508 19991204 00508 NM 1999 12 4 USAA990753 1 19990803 A 5312 BULKHEAD ANGLE BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5 .5, WL 188 T-ANGLE. FABRICATED 2 ANGLES AND 1 STRAP PER SRM 53-1-08 FIG 205, SHEET 12. (X) 2 L 7 2 4F RT A16WE 1999120400509 19991204 00509 SO 1999 12 4 C2XA99CL118 1 19991017 A 3620 OVERTEMP IND EMB 145 EMB145ER SO BLEED AIRSYSTEM ACTIVATED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 13929 145009 FLT 4115 - THE PILOT REPORTED, GOT A DAUL BLEED OVERTEMP DURING ICING CONDITIONS DURING CLIMB. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE BLEED SYSTEM IAW EMB145 MM 36-20-00 . NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999120400510 19991204 00510 WP 1999 12 4 EIA990268 1 19990703 A 5711 SPAR DOUG DC9 DC933F 302207A WP WS 169 BENT A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 DURING C-CHECK, THE LOWER HORIZONTAL FLANGE OF THE LEFT LOWER REAR SPAR CHORD AT XRS 169 WAS FOUND BENT. REPAIRED BY IN STALLING FILLER PER ECRA 942-57-073-2. (M) 2 L 7 2 4F A6WE 1999120400511 19991204 00511 CE 1999 12 4 C2SA99CL117 1 19991014 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE RT MLG FAILED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 87557 1426AB UE246 THE PILOT REPORTED, ON FINAL APPROACH DID NOT GET A DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR. THE AIRCRAFT LA NDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW BEECHC RAFT MM 32-60-00 AND 32-30-00 OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999120400512 19991204 00512 SO 1999 12 4 C2XA99CL115 1 19991006 A 3231 12012347003 LATCH EMB 120 EMB120RT SO LT MLG FAILED A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 09 15732 120195 FLT 3348 - THE CRWE REPORTED THE LEFT MAIN GEAR DOOR WOULD NOT CLOSE. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD OUTBOARD GEAR DOOR LATCH AND PERFORMED OPERATIONAL CHECKS I AW EMB120 MM 32-12-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400513 19991204 00513 SO 1999 12 4 C2XA99CL114 1 19991003 A 3150 CIRCUIT BREAKER EMB 120 EMB120RT SO AURAL WARNING TRIPPED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 09 15732 120195 FLT - 3297 - THE CREW REPORTED THEY GOT THE AURAL WARNING 'TAKEOFF TRIM' WITH THE ELEVATORS IN THE GREEN ARC, THE AIRCRA FT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE AURAL WARNING C/B AND PERFO RMED OPERATIONAL CHECKS WITH THE ENGINES RUNNING IAW EMB120 MM 71-00-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400514 19991204 00514 CE 1999 12 4 C2XA99CL113 1 19991001 A 2432 40576 BATTERY BEECH 1900 1900D 1154162 CE BATTERY COMP DISCHARGED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 17541 4533 082067 UE203 FLT 3075 - PILOT REPORTED THAT THE BATTERY CHARGE LIGHT WOULD NOT GO OUT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FU RTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MAIN BATTERY IAW BEECHCRACT 1900D MM 24-32-00. THE AIRCRAFT WAS R ELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999120400515 19991204 00515 CE 1999 12 4 C2XA99CL112 1 19991001 A 6123 WARNING LIGHT BEECH 1900 1900D 1154162 CE AUTOFEATHER SYS ILLUMINATED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 17541 UE203 FLT 3213 - PILOT REPORTED, THE AUTOFEATHER OFF AMBER CAUTION ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. THE AIRCRAFT ABOR TED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 61-3/3 PLACARD NUMBER 116062. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999120400516 19991204 00516 SO 1999 12 4 C2XA99CL111 1 19991001 A 2740 CONTROL UNIT EMB 145 EMB145 SO HORIZ STAB TRIPPED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 14938 145029 FLT 3965 - PILOT REPORTED THEY GOT A TAKEOFF CONFIG WARNING WITH THE PITCH TRIM AT THE TOP OF THE GREEN ARC. THE AIRCRA FT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE HORIZONTAL STABILIZER CONTR OL UNIT AND OPERATIONAL CHECKED THE SYSTEM GOOD IAW EMB145 MM 27-40-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999120400517 19991204 00517 WP 1999 12 4 EIA990272 1 19990802 A 5270 SKIN DOUG DC9 DC933F 302207A WP RT MLG DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, CRACKS WERE FOUND ON THE RIGHT INBOARD MLG DOOR INNER SKIN PANEL. REPAIRED BY CUTTING AWAY INNER SKIN SECTION FORWARD OF STATION 746.027 AND SPLICING IN A NEW SECTION PER ECRA 942-52-005-2. (M) 2 L 7 2 4F A6WE 1999120400518 19991204 00518 WP 1999 12 4 EIA990271 1 19990723 A 7830 PANEL DOUG DC9 DC933F 302207A WP NR 1 TR UNIT CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE NR 1 ENGINE THRUST REVERSER INBOARD ACTUATOR PANEL WAS FOUND CRACKED. REPAIRED BY INSTALLING REPAIR DOUBLER PER DOUGLAS INSTRUCTION AND ECRA 942-78-098-2. (M) 2 L 7 2 4F A6WE 1999120400519 19991204 00519 WP 1999 12 4 EIA990270 1 19990506 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 1066 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A 1 INCH CRACK WAS FOUND AT THE NR 5 TAILCONE RECEPTICLE SHEAR PIN ON THE LEFT SIDE OF THE STATION 1066 CANTED FRAME. REPAIRED BY INSTALLING REPAIR SPLICES PER ECRA 942-53-085-2. (M) 2 L 7 2 4F A6WE 1999120400520 19991204 00520 WP 1999 12 4 EIA990267 1 19990729 A 5320 ANGLE DOUG DC9 DC933F 302207A WP BS 756-832 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, OVERSIZE FASTENER HOLES WERE FOUND AT STATION 756 TO 832, STRINGER 18R TO 26R. FOUND AFTER REMOVA L OF JATO MOUNT BRACKETS. REMOVED DAMAGED RIB ANGLES, FABRICATED AND INSTALLED RIB ANGLES, DOUBLERS AND STRAPS PER ECRA 942-53-097-2. (M) 2 L 7 2 4F A6WE 1999120400521 19991204 00521 WP 1999 12 4 EIA990266 1 19990729 A 5320 ANGLE DOUG DC9 DC933F 302207A WP BS 756-832 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, OVERSIZE FASTENER HOLES WERE FOUND AT STATION 756 TO 832, STRINGER 18L TO 26L. FOUND AFTER REMOVA L OF JATO MOUNT BRACKETS. REMOVED DAMAGED RIB ANGLES, FABRICATED AND INSTALLED RIB ANGLES, DOUBLERS AND STRAPS PER ECRA 942-53-100-2. (M) 2 L 7 2 4F A6WE 1999120400522 19991204 00522 WP 1999 12 4 EIA990265 1 19990611 A 5520 99184513 WEB DOUG DC9 DC933F 302207A WP LT ELEVATOR DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE LEFT ELEVATOR REAR SPAR WEB WAS FOUND TO HAVE ELONGATED FASTENER HOLES. REPAIRED BY CUTTING O UT DAMAGE AND INSTALLING REPAIR SPLICE AND CHANNEL PER ECRA 942-55-072-2. (M) 2 L 7 2 4F A6WE 1999120400523 19991204 00523 WP 1999 12 4 EIA990264 1 19990611 A 5330 LONGERON DOUG DC9 DC933F 302207A WP BS 1095 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, DURING SKIN REPLACEMENT, NUMEROUS HOLES IN THE UPPER SKIN AND LONGERON AT STATION 1095, LONGERON 2 5R, WERE FOUND ELONGATED. REPAIRED BY TRIMMING THE ELONGATED HOLES AND INSTALLING REPAIR FILLERS AND DOUBLERS. (M) 2 L 7 2 4F A6WE 1999120400524 19991204 00524 WP 1999 12 4 EIA990263 1 19990530 A 5411 AMS4911 RIB DOUG DC9 DC933F 302207A WP RT PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A 6 INCH CRACK WAS FOUND ON THE RIGHT TRAILING EDGE PYLON 2ND RIB INBOARD. REPAIRED BY TRIMMING R IB AND INSTALLING NEW SPLICE AND REPAIR DOUBLERS PER ECRA 942-55-020-2. (M) 2 L 7 2 4F A6WE 1999120400525 19991204 00525 WP 1999 12 4 EIA990262 1 19990507 A 5320 PRESS PANEL DOUG DC9 DC933F 302207A WP BS 699 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A PRESSURE PANEL AT STATION 699 WAS FOUND TO HAVE EXFOLIATION CORROSION. REPAIRED BY TRIMMING PRE SSURE PANEL AND NDT'ING AREA PER ECRA 942-53-049-2. (M) 2 L 7 2 4F A6WE 1999120400526 19991204 00526 WP 1999 12 4 EIA990261 1 19990507 A 5320 DOUBLER DOUG DC9 DC933F 302207A WP CARGO DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A CRACK WAS FOUND IN THE FORWARD LOWER CARGO DOOR CUTOUT DOUBLER. CRACKED DOUBLER REPAIRED, ONE D OUBLER AND 2 FILLERS WERE INSTALLED PER ECRA 942-53-016-2. (M) 2 L 7 2 4F A6WE 1999120400527 19991204 00527 WP 1999 12 4 EIA990260 1 19990507 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 332-370 MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, SKIN REPAIRS BETWEEN STATION 332 TO 370, LONGERON 21R TO 26R, WERE FOUND TO BE UNACCEPTABLE. REMO VED AND RE-REPAIRED SKIN SECTION PER ECRA 942-53-008-2. (M) 2 L 7 2 4F A6WE 1999120400528 19991204 00528 WP 1999 12 4 EIA990259 1 19990506 A 4980 TAIL PIPE DOUG DC9 DC933F 302207A WP APU CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE APU TAIL TO EMPENNAGE WELD WAS FOUND CRACKED. PART WAS NDT'D AND STOP DRILLED PER DOUGLAS SRM 08-00-07. WELD WAS REPAIRED BY REPAIR STATION NR J3WR275J. ALL WORK ACCOMPLISHED WITH INSTRUCTIONS FROM ECRA942-49-00 6-2 AND BOEING ENGINEERING. (M) 2 L 7 2 4F A6WE 1999120400529 19991204 00529 WP 1999 12 4 EIA990258 1 19990505 A 5743 5924841409 FITTING DOUG DC9 DC933F 302207A WP LT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE LEFT MAIN LANDING GEAR FITTING SIDE BRACE ATTACH LUG WAS FOUND CORRODED ON AFT FACE. REMOVED CORROSION AND REPAIRED PER ECRA 942-57-003-2. (M) 2 L 7 2 4F A6WE 1999120400530 19991204 00530 WP 1999 12 4 EIA990257 1 19990505 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 446-465 MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A FUSELAGE SKIN REPAIR BETWEEN STATION 446 TO 465, LONGERON 23L TO 26L, WAS EVALUATED AND FOUND TO BE AN UNACCEPTABLE REPAIR. REMOVED EFFECTED SECTION OF SKIN, COMPLETED REWORK OF SKIN REPAIR PER ECRA 942 53-1-0211 AN D REINSTALLED. (M) 2 L 7 2 4F A6WE 1999120400531 19991204 00531 WP 1999 12 4 EIA990256 1 19990504 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 737-756 MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A FUSELAGE SKIN REPAI AT STATION 737 TO 756, LONGERON 19R, WAS EVALUATED AND FOUND TO BE AN UNACCE PTABLE REPAIR. REMOVED EXISTING REPAIR, NDT'D AREA AND INSTALLED NEW FABRICATED DOUBLER PER ECRA 942-53-0111-2. (M) 2 L 7 2 4F A6WE 1999120400532 19991204 00532 WP 1999 12 4 EIA990255 1 19990506 A 5320 WEB DOUG DC9 DC933F 302207A WP BS 420 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, THE MAIN CABIN CUSP WEB, LOCATED AT STATION 420R, WAS FOUND CRACKED. REPAIRED CUSP WEB BY FABRICA TING AND INSTALLING A REPAIR DOUBLER PER SRM 53-01 AND 51-30-1. (M) 2 L 7 2 4F A6WE 1999120400533 19991204 00533 WP 1999 12 4 EIA990274 1 19990720 A 5522 9918480112 SKIN DOUG DC9 DC933F 302207A WP RT ELEVATOR HOLE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 942F 47408 MZJ - DURING C-CHECK, A HOLE WAS FOUND IN THE RIGHT ELEVATOR LOWER SURFACE OUTBOARD END. REPAIRED BY REPLACING RIGHT EL EVATOR OUTBOARD LOWER SKIN PER DOUGLAS DRAWING NR 9918480 AND ECRA 942-55-083-2 AND SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999120400534 19991204 00534 WP 1999 12 4 EIA990276 1 19990913 A 5350 5910066515 FILLET DOUG DC9 DC932F 3022067 WP LT WING/FUS CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK, ELONGATED HOLES AND CRACKS WERE FOUND ON THE UPPER LEFT WING TO FUSELAGE FILLET. REPAIRED BY TRIM MING ELONGATED HOLES, FABRICATED AND INSTALLED REPAIR DOUBLER PER ECRA 932-53-049-2. (M) 2 L 7 2 4F A6WE 1999120400535 19991204 00535 WP 1999 12 4 EIA990275 1 19990915 A 5320 991073415 WEB DOUG DC9 DC932F 3022067 WP BS 240 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK, A CRACK WAS FOUND IN THE CUSP WEB AT RIGHT STATION 240, RBL 54.50. REPAIRED BY STOP DRILLING CRAC K AND INSTALLING REPAIR DOUBLER PER ECRA 932-53-053-2. (M) 2 L 7 2 4F A6WE 1999120400536 19991204 00536 NM 1999 12 4 EIA990285 1 19990721 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 880 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - SWELLING AND OPEN HOLES ON FAIRING SUPPORT AT LOWER FUSELAGE STATION 880 BETWEEN AREA RBL 15 TO RBL 27. SWOLLEN A REA TRIMMED OUT AND DEBURRED. REINFORCED AREA WITH 2 SUPPORTS(7075 T60 .080 THK) PER SRM 53-50-04, FIG 1. ALODINED AND EP PRIMER PROTECTED PER SRM 51-10-01. INSTALLED REPAIR WITH RIVETS PER SRM 51-30-02. (M) 2 L 7 4 4F A20WE 1999120400537 19991204 00537 NM 1999 12 4 EIA990284 1 19990721 A 5320 FITTING BOEING 747 747128 1384894 NM BS 1480 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - FOUND CORROSION ON THE OUTER CHORD SPLICE FITTING AT STATION 1480 LEFT SIDE. REPAIR STRAP INSTALLED IAW IAI EO MF -MAN-B47-53-88841 REV A DATED 9-9-99. (M) 2 L 7 4 4F A20WE 1999120400538 19991204 00538 NM 1999 12 4 EIA990283 1 19990721 A 5312 BULKHEAD BOEING 747 747128 1384894 NM BS 140 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - FOUND CRACKS ON PRESSURE BULKHEAD STATION 140 FORWARD SIDE, WL 305 APPROX L AND R BL 33. CRACKED AREA TRIMMED OUT . REINFORCED AREA WITH DOUBLERS AND FILLER 2024-T3 .050 PLUS .032 THK PER SRM 53-10-04 FIG 8D ALODINED AND EP PRIMER PR OTECTED PER SRM 51-10-02 AND RIVETED PER SRM 51-30-00. (M) 2 L 7 4 4F A20WE 1999120400539 19991204 00539 NM 1999 12 4 EIA990282 1 19990917 A 5330 SKIN BOEING 747 747128 1384894 NM BS 660-700 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - SWELLING ON EXTERNAL FUSELAGE WITH SHEARED RIVET BETWEEN STATION 660-700 BETWEEN STRINGER 41-43R. REPAIR DOUBLER INSTALLED IAW EO MF-MAN-B47-53-00-88832 REF, BOEING FAX MESSAGE M-7200-99-06866 DATED 8/5/99 AND SRM 53-30-03 FIG 1. (M ) 2 L 7 4 4F A20WE 1999120400540 19991204 00540 NM 1999 12 4 EIA990281 1 19990917 A 5711 SKIN BOEING 747 747128 1384894 NM WS 1360 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - SWELLING ON RIGHT WING UPPER SKIN, UPPER SURFACE ABOVE FRONT SPAR AT WS 1360. PERFORMED REPAIR PER EO MF-MAN-B47- 57-88838 NEW REF BOEING SERVICE ENGINEERING MESSAGE M-7200-99-07260 DATED AUGUST 16, 1999. INSTALLED DOUBLER. (M) 2 L 7 4 4F A20WE 1999120400541 19991204 00541 NM 1999 12 4 EIA990280 1 19990917 A 5720 112U50261 CHORD BOEING 747 747128 1384894 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - FOUND CRACK IN THE RADIUS OF THE UPPER CHORD OF LEFT WING STATION 669.5 INTERIOR FUEL TANK. CRACKED UPPER CHORD R EMOVED. INSTALLED NEW UPPER CHORD IAW SB 57-2273-R2. (M) 2 L 7 4 4F A20WE 1999120400542 19991204 00542 NM 1999 12 4 EIA990279 1 19990917 A 5311 FRAME BOEING 747 747128 1384894 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - FOUND CRACK IN FRAME INNER CHORD AT STATION 1265 LEFT BELOW FLOOR LINE. WEB REPAIR PERFORMED AND INSTRUCTION DETA ILED OF THIS WORK ARE NOTED IN EO MF-MAN-B47-53-88847 NEW REF BOEING SERVICE ENG MESSAGE M-7200-99-02111 8/12/99 AND M72 00-99-07861 8/30/99. (M) 2 L 7 4 4F A20WE 1999120400543 19991204 00543 NM 1999 12 4 EIA990278 1 19990917 A 5311 FRAME BOEING 747 747128 1384894 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - FOUND CRACK IN FRAME WEB AT STATION 1265 RIGHT JUST ABOVE FLOOR LINE. WEB REPLACEMENT PERFORMED AND INSTRUCTION O F THIS WORK NOTED IN JOB CARD NR 366-53-035M REF IAI SB 366-53-035. DRAWING R05366-53-15-15196-006. (M) 2 L 7 4 4F A20WE 1999120400544 19991204 00544 NM 1999 12 4 EIA990277 1 19990917 A 5711 SPAR WEB BOEING 747 747128 1384894 NM LT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 3203Y 19751 TLV - DURING THE ACCOMPLISHMENT OF THE TERMINATING OF THE SB 747-57A2266 REV 6 CRACK FOUND AT FASTENER HOLES IN THE FRON T SPAR WEB STATION 660, COMMON TO THE LOWER CHORD. PERFORMED REPAIR IAW IAI EO MF MAN B47-57-88849 AND AS APPROVED BY F AA REPAIR 8110-3 ATTACHED. WEB REPAIR ACCOMPLISHED. (M) 2 L 7 4 4F A20WE 1999120400545 19991204 00545 WP 1999 12 4 EIAA990251 1 19990824 A 3010 3919532505 DUCT DOUG DC9 DC933F 302207A WP LT WING BENT A EIAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 933F 47191 SYR - WITH FLAPS AND SLATS SELECTED UP, CONTROL WHEEL REQUIRED 45 DEGREES RIGHT TURN TO MAINTAIN STRAIGHT AND LEVEL FLIG HT UNTIL LOUD BANGING SOUND, THEN CONTROL WHEEL WOULD BE CENTERED AND NORMAL (REQUIRED 4-5 SECONDS). MAINTENANCE CREWS FOUND LEFT WING AIRFOIL TELESCOPING DUCT BINDING AND HANGING UP. MAINTENANCE REMOVED AND REPLACED LEFT WING AIRFOIL OUT ER TELESCOPING DUCT AND ASSOCIATED HARDWARE IAW MM 30-10-07. SYSTEM CHECKS NORMAL WITH NO BINDING OR HANGING UP. (M) 2 L 7 2 4F A6WE 1999120400546 19991204 00546 WP 1999 12 4 EIA990287 1 19990929 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 89 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47279 SEA - DURING PREFLIGHT, FOUND 11 INCH CRACK IN LEFT SIDE OF AIRCRAFT AT STATION 89, ALSO, FOUND FUSELAGE FRAME CRACKED AT STATION 83, LEFT SIDE. REPAIRED DAMAGED SKIN AREA PER SRM 51-10-03 AND SRM 51-30-02. REMOVED AND REPLACED DAMAGED F RAME WITH NEW PART PER SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1999120400547 19991204 00547 WP 1999 12 4 99ZZZM783 1 19990929 A 5330 FRAME DOUG DC9 DC933F 302207A WP BS 83 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47279 SEA - DURING PREFLIGHT, FOUND 11 INCH CRACK IN LEFT SIDE OF AIRCRAFT AT STATION 89, ALSO, FOUND FUSELAGE FRAME CRACKED AT STATION 83, LEFT SIDE. REPAIRED DAMAGED SKIN AREA PER SRM 51-10-03 AND SRM 51-30-02. REMOVED AND REPLACED DAMAGED F RAME WITH NEW PART PER SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1999120400548 19991204 00548 EU 1999 12 4 99ZZZM784 1 19991018 A 2497 WIRE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DAMAGED A A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 487UE 906 FLT 206 - FLIGHT CREW NOTICED A SMELL OF SMOKE IN THE COCKPIT AND RETURNED TO THE GATE. A FERRY PERMIT WAS ISSUED AND T HE AIRCRAFT RETURNED TO IAD. MAINTENANCE FOUND A WIRE WITH SIGNS OF HEAT DAMAGE. THIS WIRE RUNS FROM THE LEFT ENGINE S TART GENERATOR TO THE LEFT ENGINE START CONTACTOR. A DETAILED INSPECTION FOUND A BUTT SPLICE INSTALLED ON WIRE KN130 WH EN THIS SPLICE WAS INSTALLED THE WIRE SHIELD WAS DAMAGED . (M) 2 L 7 2 4T RT A56EU 1999120400549 19991204 00549 WP 1999 12 4 99ZZZM785 1 19991005 A 2750 KRP5024V7 BEARING DOUG DC9 DC932 3022066 WP LT TE FLAP VANE WORN A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 35 930BB 47521 DURING WALK AROUND INSPECTION IN GPT, MECHANIC FOUND LEFT AFT FLAP VANE CABLE PROTRUDING FROM TOP OF LEFT FLAP. AIRCRAF T WAS FERRIED TO MOBILE AEROSPACE IN MOBILE, ALABAMA. LEFT FLAP MOVEABLE VANE SYSTEM WAS RERIGGED IAW MM 27-51-2. LEFT FLAP WOULD NOT RETRACT TO FULL UP POSITION. PROBLEM WAS T/S TO WORN AND FROZEN MOVEABLE VANE TRACK BEARINGS. LEFT VAN E TRACK WAS REMOVED INSPECTED AND REINSTALLED. VANE TRACK BEARINGS WERE RMOVED AND REPLACED, FLAP VANE SYSTEM WAS OPERA TIONS CHECKED OK IAW MM 27-51-2 AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999120400550 19991204 00550 NM 1999 12 4 USAA990754 1 19990803 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 37413 23510 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5 , WL 204 WEB. FABRICATED DOUBLER AND FILLERS PER SRM 53-10-07 AND 08. (M) 2 L 7 2 4F RT A16WE 1999120400551 19991204 00551 NM 1999 12 4 USAA991163 1 19991023 A 5330 SKIN BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 407US 32316 23877 CLT - DURING RON VISUAL INSPECTION, FOUND A 1.250 INCH SKIN CRACK JUST BELOW STRINGER 23L AND 3 INCH AFT OF STATION 727D . INSTALLED REPAIR DOUBLER PER EA 65983 AND TR 53-60-03. (M) 2 L 7 2 4F RT A16WE 1999120400552 19991204 00552 NM 1999 12 4 USAA991160 1 19991024 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 40217 23380 CLT - DURING WALK AROUND VISUAL INSPECTION, FOUND A .875 INCH CRACK SEC 46 FUSELAGE SKIN JUST BELOW STRINGER 23L, BS 727 D PLUS 2 INCHES. CUTOUT CRACKED AREA AND INSTALLED FILLER AND DOUBLER PER TR 53-60-003. (M) 2 L 7 2 4F RT A16WE 1999120400553 19991204 00553 NM 1999 12 4 USAA991092 1 19991018 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 540, STRINGER 22R SUPPORT ANGLE RAM AIR INLET SUP PORT. FABRICATED AND INSTALLED REPLACEMENT REPAIR ANGLE PER 53-50-03. (M) 2 L 7 2 4F RT A16WE 1999120400554 19991204 00554 NM 1999 12 4 USAA991091 1 19991018 A 5414 SKIN BOEING 737 737301 1384611 NM LT PYLON CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LOWER AFT CORNER OF PANEL NR 5727L CUTOUT LEFT PYLON SK IN. INSTALLED DOUBLER PER EA 65815 AND TR 54-30-07. (M) 2 L 7 2 4F RT A16WE 1999120400555 19991204 00555 NM 1999 12 4 USAA991077 1 19991018 A 5330 SKIN BOEING 737 737301 1384611 NM BS 379 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 379, LBS 3.5 SKIN. INSTALLED REPAIR DOUBLER PER TR-53-30-07 AND BAC DRWG 65C33930. (M) 2 L 7 2 4F RT A16WE 1999120400556 19991204 00556 NM 1999 12 4 USAA991076 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0125 INCH CRACK AT BS 827 STRINGER 9R AT FASTENER HOLE FRAME. INSTAL LED DOUBLER PER EA 65542, SRM 53-00-07 AND SRM 53-30-07. (M) 2 L 7 2 4F RT A16WE 1999120400557 19991204 00557 NM 1999 12 4 USAA991075 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 295.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT FORWARD SERVICE DOOR CUTOUT FRAME STATION 295.5, RBL 54, WL 208.5. FABRICATED REPAIR ANGLE PER SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F RT A16WE 1999120400558 19991204 00558 NM 1999 12 4 USAA991074 1 19991018 A 5330 SKIN BOEING 737 737301 1384611 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 CRACKS, 1 AT 1.25 INCH LONG AND 1 AT .0675 INCH LONG EMANATING FROM RI VETS IN FUS AT LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED DOUBLER PER SRM 53-10-01. (M) 2 L 7 2 4F RT A16WE 1999120400559 19991204 00559 NM 1999 12 4 USAA991071 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .250 INCH BY .250 INCH AREA OF CORROSION AT BS 344, LBL 51, RBL 15 FLO ORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-01. INSTALLED T-CAP PER EA 65749 AND SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999120400560 19991204 00560 NM 1999 12 4 USAA991059 1 19991018 A 5320 SHEAR BEAM BOEING 737 737301 1384611 NM BS 726 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 726, STRINGER 18A RIGHT, RBL 61, WL 188 SHEA R BEAM WEB. INSTALLED NEW WEB AND GUSSETT PLATE PER EA 65576 AND SB 737-53-1170. (M) 2 L 7 2 4F RT A16WE 1999120400561 19991204 00561 NM 1999 12 4 USAA991056 1 19991018 A 5320 CHANNEL BOEING 737 737301 1384611 NM BS 359 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 359 STRINGER 14L IN TIE CHANNEL TO STRINGER. I NSTALLED NEW CHANNEL PER EA 65686. (M) 2 L 7 2 4F RT A16WE 1999120400562 19991204 00562 NM 1999 12 4 USAA991055 1 19991018 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT UPPER OUTBOARD CORNER OF CO-PILOTS NR 1 WINDOW SKIN. INSTALLED DOUBLER PER EA65643 AND SRM 53-30-3 FIG 11. (M) 2 L 7 2 4F RT A16WE 1999120400563 19991204 00563 NM 1999 12 4 USAA991054 1 19991018 A 5320 SPLICE BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 907 STRINGER 4L, AT FASTENER HOLE STRINGER SPLIC E. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400564 19991204 00564 NM 1999 12 4 USAA990717 1 19990729 A 5313 LONGERON BOEING 737 737301 1384611 NM BS 277 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH LONGERON CRACK AT FORWARD L/B CORNER STATION 277 STRINGER 14R . FABRICATED NEW LONGERON WEB AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999120400565 19991204 00565 NM 1999 12 4 USAA990721 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 520 STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400566 19991204 00566 WP 1999 12 4 USAA991105 1 19991008 A 5240 SERVICE DOOR DOUG DC9 DC981 3022081 WP BS 205 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48971 48042 PIT - DURING Q2 CHECK, FOUND CORROSION AT STATION 205 AT AFT SIDE OF SERVICE DOOR 2 INCH BY 3 INCH AT STATION 205 LONG 1 8 CUSP AREA. CORROSION LEVEL 1, CORROSION TASK NR C46-53301. INSTALLED NEW CUSP MEMBRANE AND SPLICED DOOR PAN PER SRM 53-05 SIG 55 AND EA 53042. 2 L 7 2 4F A6WE 1999120400567 19991204 00567 WP 1999 12 4 USAA991179 1 19991025 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 50376 48037 PIT - DURING RON, FOUND 1 INCH LONG CRACK IN FUSELAGE SKIN AT FORWARD AIRSTAIR DOOR CUT OUT LOWER AFT CORNER AT STATION 200. INSTALLED EXTERNAL DOUBLERS PER SRM 53-05 FIG 57A. (M) 2 L 7 2 4F A6WE 1999120400568 19991204 00568 WP 1999 12 4 USAA991180 1 19991021 A 5320 DOUBLER DOUG DC9 DC981 3022081 WP STA 1155-1162 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 50946 48034 PIT - DURING C-3 CHECK, FOUND 7 INCH BY 7 INCH CORRODED AREA AT WEB DOUBLER STATION 1155-1162 LONGERON 29R TO 27R. CORR OSION LEVEL 1, CORROSION TASK NR C57-53300. CUT OUT DAMAGED WEB SECTION, MANUFACTURED NEW, INSTALLED WITH DOUBLERS (SPL ICES) PER EA 53135. (M) 2 L 7 2 4F A6WE 1999120400569 19991204 00569 WP 1999 12 4 USAA991177 1 19991026 A 3210 3935860501 BOTTLE PIN DOUG DC9 DC981 3022081 WP LT MLG SHEARED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 49015 48041 PIT - PILOT REPORT INDICATED THREADS OF BOTTLE PIN FOR THE LEFT MAIN LANDING GEAR SHEARED 100 PERCENT. DEFECTIVE PART R EPLACED WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F A6WE 1999120400570 19991204 00570 WP 1999 12 4 USAA991178 1 19991026 A 3210 3935860501 LASTING DOUG DC9 DC981 3022081 WP RT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 49015 48041 PIT - DURING RON AND EA 53181, FOUND 100 PERCENT CORROSION OF ALL BUSHING AREA OF BOTTLE PIN FOR THE RIGHT MLG. DEFECTI VE PART REPLACED WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F A6WE 1999120400571 19991204 00571 NM 1999 12 4 USAA990723 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 616 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400572 19991204 00572 NM 1999 12 4 USAA990724 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 639 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400573 19991204 00573 NM 1999 12 4 USAA990768 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 6L TIE CLIP. INSTALLED NEW TIE CL IP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400574 19991204 00574 NM 1999 12 4 USAA990769 1 19990729 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 957 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 957 AND 987, LBL 45, WL 208 CREASEBEAM INNER CHORD ANGLE . CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. INSTALLED NEW CHORD ANGLE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400575 19991204 00575 NM 1999 12 4 USAA990770 1 19990729 A 3210 655223536 STABILIZER LINK BOEING 737 737301 1384611 NM RT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION RIGHT GEAR STABILIZER LINK ATTACH POINTS. CORROSION LEVEL 2. REMOVED AND REPLACED STABILIZER LINK PER MM 32-32-93 AND 32-13-21. (M) 2 L 7 2 4F RT A16WE 1999120400576 19991204 00576 NM 1999 12 4 USAA990779 1 19990729 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND TIE CLIP CRACKED IN HALF. ALSO, FOUND STRINGER CRACKED BELOW CLIP LOCATION, STATION 616, S -4L. INSTALLED STRINGER DOUBLER PER SRM 53-00-03 FIG 204 AND FABRICATED TIE CLIP AND INSTALLED PER SRM 51-10-1. (M) 2 L 7 2 4F RT A16WE 1999120400577 19991204 00577 NM 1999 12 4 USAA990780 1 19990729 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DUIRNG Q-3 CHECK, FOUND .25 INCH CRACK IN FRAME AT BS 480 S9R. INSTALLED DOUBLER PER EA 65009. (M) 2 L 7 2 4F RT A16WE 1999120400578 19991204 00578 NM 1999 12 4 USAA990781 1 19990729 A 5311 FRAME BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND .125 INCH CRACK IN FRAME AT STATION 616 RBL 64 WL 201 INBOARD CHORD ANGLE. INSTALLED REPAI R FILLER AND STIFFENING ANGLE PER EA 65007 TR 53-10-23 (737-200). (M) 2 L 7 2 4F RT A16WE 1999120400579 19991204 00579 NM 1999 12 4 USAA990782 1 19990729 A 5320 65516989 SPLICE BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4RT. REPLACED STRINGER SPLICE WITH IDE NTICAL PART. (M) 2 L 7 2 4F RT A16WE 1999120400580 19991204 00580 NM 1999 12 4 USAA990783 1 19990729 A 5320 65516989 SPLICE BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4LT. REPLACED STRINGER SPLICE WITH IDEN TICAL PART. (M) 2 L 7 2 4F RT A16WE 1999120400581 19991204 00581 NM 1999 12 4 USAA990784 1 19990729 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CREASE BEAM INNER CHORD ANGLE BS 294.5 RBL 45 WL 208. INSTALLED CHORD ANGL E PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400582 19991204 00582 NM 1999 12 4 USAA990785 1 19990729 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK, FOUND .5 INCH CRACK E/E COOLING DUCT OUTLET INNER FUSELAGE FUSELAGE SKIN AT BS 380 BL 0. INSTAL LED EXTERNAL FUSELAGE SKIN DOUBLER 23 INCH BY 40 INCH PER TR 53-30-07 AND BOEING DWG NR 65C33930. (M) 2 L 7 2 4F RT A16WE 1999120400583 19991204 00583 NM 1999 12 4 USAA990786 1 19990729 A 5320 69353522 CLIP BOEING 737 737301 1384611 NM STATION 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND .25 INCH CRACK AT TIE CLIP AT STATION 663 S10L. REPLACED WITH IDENTICAL PART PER SRM 51-10 -2. (M) 2 L 7 2 4F RT A16WE 1999120400584 19991204 00584 NM 1999 12 4 USAA990787 1 19990729 A 5754 SKIN BOEING 737 737301 1384611 NM NR 1 LE SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND 3 CRACKS ONE 1.375 INCH, TWO .5 INCH ON SKIN AT NR 1 L/E SLAT. INSTALLED REPAIR DOUBLER PE R TYPICAL REPAIR 57-50-01 REV 'H'. (M) 2 L 7 2 4F RT A16WE 1999120400585 19991204 00585 NM 1999 12 4 USAA990788 1 19990729 A 5320 POST BOEING 737 737301 1384611 NM LT WINDSHIELD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CAPTAINS UPPER O/B CORNER OF EXTERIOR WINDSHIELD (POST). INSTALLED EXTERNA L DOUBLER PER EA 64979. (M) 2 L 7 2 4F RT A16WE 1999120400586 19991204 00586 NM 1999 12 4 USAA990789 1 19990729 A 5320 67203802 INTERCOSTAL BOEING 737 737301 1384611 NM STATION 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT STATION 178, 195 INTERCOSTAL RT SIDE. REPLACED WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F RT A16WE 1999120400587 19991204 00587 NM 1999 12 4 USAA990790 1 19990729 A 5311 65479576 FRAME BOEING 737 737301 1384611 NM BS 605-845 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND VARIOUS 1 INCH AREAS OF CORROSION AT NUTPLATE HOLES IN FRAME/WEB AT BS 605 TO 845 STRINGER 25R TOP FLANGE. REPLACED WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F RT A16WE 1999120400588 19991204 00588 NM 1999 12 4 USAA990791 1 19990729 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q3 CHECK, FOUND .75 INCH CRACK AT BS 727 STRINGER 18A WEB S18AL. REPAIRED WITH REPLACEMENT REF SB 737-53-1 170. (M) 2 L 7 2 4F RT A16WE 1999120400589 19991204 00589 NM 1999 12 4 USAA990883 1 19990820 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 353US 35311 23556 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK FLOORBEAM AT BS 807 AFT CARGO COMPT. INSTALLED DOUBLER PER EA 65091 SRM 51-70-10/53-00-51 SECT 41, 43 PAGE 201 AND 202. (M) 2 L 7 2 4F RT A16WE 1999120400590 19991204 00590 NM 1999 12 4 USAA990862 1 19990808 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 41337 22958 PIT - DURING CX 3 CONV CHECK, FOUND CRACK APPROX .500 INCH FLOORBEAM AT FS 344 AT LBL 11. REPAIRED PER SRM 53-10-51 AND EA 52604. (M) 2 L 7 2 4F RT A16WE 1999120400591 19991204 00591 NM 1999 12 4 USAA990884 1 19990820 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 860 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 353US 35311 23556 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION AFT CARGO FLOOR SUPPORT STATION 860. CORROSION LEVEL 1. INSTALLED ANGLE PER TR 53-10-06. (M) 2 L 7 2 4F RT A16WE 1999120400592 19991204 00592 NM 1999 12 4 USAA990863 1 19990808 A 5230 SKIN BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 41337 22958 PIT - DURING CX3 CONV CHECK, FOUND CRACK APPROX .500 INCH IN AFT CARGO DOOR, FLAPPER DOOR CUT OUT (A/C SKIN) UPPER AFT C ORNER. REPAIRED PER TYPICAL REPAIR 52-10-01 'A' FIG 1. (M) 2 L 7 2 4F RT A16WE 1999120400593 19991204 00593 NM 1999 12 4 USAA990864 1 19990808 A 5320 6545834525 STIFFENER BOEING 737 7373B7 1384580 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 385US 41337 22958 PIT - DURING CX3 CONV CHECK, FOUND .5 INCH CRACK IN STIFFENER AT STATION 344 INTERCOSTAL. REPLACED ANGLES PER EA 52604. (M) 2 L 7 2 4F RT A16WE 1999120400594 19991204 00594 NM 1999 12 4 USAA990680 1 19990729 A 5240 ANGLE BOEING 737 737301 1384611 NM SERVICE DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AFT RT Z-ANGLE AT AFT SERV DOOR. CORROSION LEVEL 2. REPLACED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400595 19991204 00595 NM 1999 12 4 USAA990722 1 19990729 A 5414 SKIN BOEING 737 737301 1384611 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT NR 1 ENGINE PYLON SKIN AT ACCESS PANEL NR 5727 CUTOU T LOWER AFT CORNER. INSTALLED DOUBLER PER TR 54-30-07. (M) 2 L 7 2 4F RT A16WE 1999120400596 19991204 00596 NM 1999 12 4 USAA991053 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 887, STRINGER 9R AT FASTENER HOLE FRAME. INSTAL LED DOUBLER AND FILLER PER EA 65542, SRM 53-00-07 AND SRM 53-30-07. (M) 2 L 7 2 4F RT A16WE 1999120400597 19991204 00597 NM 1999 12 4 USAA991052 1 19991018 A 5320 SHEAR BEAM BOEING 737 737301 1384611 NM BS 726 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT BS 726, LBL 61, WL 188 STRINGER 18A SHEAR BEAM WEB. FABRICATED REPAIR ANGLES, AND INSTALLED PER EA 65576, SRM 51-40-05 AND SB 737-53-1170. (M) 2 L 7 2 4F RT A16WE 1999120400598 19991204 00598 NM 1999 12 4 USAA991003 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 907 STRINGER 9R AT FASTENER HOLE FRAME. INSTALL ED FILLER AND REPAIR ANGLE PER EA 65542. (M) 2 L 7 2 4F RT A16WE 1999120400599 19991204 00599 NM 1999 12 4 USAA990998 1 19991018 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER TIE CLIP AT BS 597 AT , S-1, S-8L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400600 19991204 00600 NM 1999 12 4 99ZZZM786 1 19991118 A 2780 69396351 PULLEY BOEING 727 727264 138408M NM LE FLAP SEIZED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 764AT 22984 DURING C-CHECK, FOUND THE AFT FLAP CABLE FRAYING AGAINST THE INBOARD FLAP PULLEY. THE INBOARD FLAP OUTBOARD CABLE PULLE Y WAS FOUND WITH THE SWIVEL POINT CONTAMINATED WITH CIC COMPOUND AND DIRTY CAUSING TO SEIZE IN ONE POSITION. REPLACED F LAP CABLE AND BOTH INBOARD AND OUTBOARD CABLES AND PULLEY. SWIVEL POINT WAS ALSO REPLACED. (M) 2 L 7 3 4F A3WE 1999120400601 19991204 00601 NM 1999 12 4 99ZZZM787 1 19991102 A 2120 UNKNOWN BOEING 757 75723N 1384973 NM ROW 23/24 ODOR A AMTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 519AT 27975 DURNG CRUISE ELECTRICAL ODOR WAS SENSED BY THE FLIGHT CREW NEAR ROWS 23-24. CHECK LIST WAS ACCOMPLISHED THEN THE ODOR D ISSIPATED. PERFORMED AN UNSCHEDULED LANDING IN NASSAU. A/C WAS INSPECTED FOR MAINTENANCE FERRY FLIGHT. RAN BOTH ENGIN ES AT POWER AND PRESSURIZED A/C, POWERED UP GALLEYS AND ALL ELECTRICAL SYSTEM IN THE CABIN AND NO ELECTRICAL ODOR NOTED. A/C RETURN TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1999120400602 19991204 00602 1999 12 4 99ZZZM788 4 19991102 A 2564 R0202A207 RAFT LKHEED 1011 10113851 5265010 WP EMERGENCY EXIT ACTIVATED A AMTA H DEACTIVATE SYST/CIRCUITS O OTHER DE DESCENT 1 GL 11 192AT 193C1057 DURING DESCENT, THE 3L RAFT INFLATED, HAD TO PUNCTURE TO CLEAR THE EMERGENCY EXIT. INSTALLED SERVICEABLE LIFE RAFT PER MM 25, SECURED LIFE RAFT IN PLACE. (M) 2 L 7 3 4F A23WE 1999120400603 19991204 00603 WP 1999 12 4 ASAA9980173 1 19990814 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 PDX - FLT 503 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPER ATIVE. RECONNECTED CONNECTOR IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400604 19991204 00604 WP 1999 12 4 ASAA9980174 1 19990817 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE AFT HALF OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE DIM. REPLACED TWO AF T BATTERIES IN EMERGENCY PACKS AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400605 19991204 00605 WP 1999 12 4 ASAA9980175 1 19990818 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 3 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - FLT 158 - PRIOR TO DEPARTURE, THE FIRST SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE IN THE FIRST CLASS SECTION. REPAIRED WIRING AT ROW 3 AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400606 19991204 00606 WP 1999 12 4 ASAA9980176 1 19990819 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - FLT 198 - PRIOR TO DEPARTURE CREW REPORTED SOME EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE IN OPERATIVE. FOUND APPROXIMATELY A SIX INCH SECTION OF THE MOUNTING TRACK MISSING FORWARD OF ROW 1 D-F. PERFORMED INTERI M REPAIR TO THE TRACK COVER, RECONNECTED THE CONNECTOR IN THE FLOOR TRACK AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400607 19991204 00607 WP 1999 12 4 ASAA9980177 1 19990820 A 3350 LIGHT DOUG DC9 DC983 3022083 WP ROWS 19-22 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19 THROUGH 22. REPLAC ED PACK BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400608 19991204 00608 WP 1999 12 4 ASAA9980179 1 19990825 A 3350 BATTERY DOUG DC9 DC983 3022083 WP ROWS 14-17 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 14-17 WERE FOUND TO BE INOPERATIVE. REPLACED BATT ERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400609 19991204 00609 WP 1999 12 4 ASAA9980180 1 19990828 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - PRIOR TO DEPARTURE OF FLIGHT 434, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400610 19991204 00610 WP 1999 12 4 ASAA9980181 1 19990830 A 3350 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROWS 18-22 FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 18 TO 22 WERE FOUND INOPERATIVE. REPLACED THE P OWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400611 19991204 00611 WP 1999 12 4 ASAA9980182 1 19990830 A 3350 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POW ER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400612 19991204 00612 WP 1999 12 4 ASAA9980183 1 19990831 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400613 19991204 00613 WP 1999 12 4 ASAA9980186 1 19990904 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 OAK - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400614 19991204 00614 WP 1999 12 4 ASAA9980187 1 19990905 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING MAINTENANCE CHECK, THE TWO EMERGENCY FLOOR TRACK RED LIGHTS FOR THE L2 DOOR EXIT WERE FOUND INOPERATIVE. R EPLACED THE WIRING IN THE FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999120400615 20000703 00615 NM 2000 7 3 ASAA9940160 1 19991104 A 2560 61768101 BOTTLE BOEING 737 737490 1384715 NM ESCAPE SLIDE LEAKING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 799AS 29270 PDX - DURING MAINTENANCE CHECK, THE R2 DOOR EVAC SLIDE GAUGE WAS FOUND TO BE IN THE RED. REPLACED THE R2 DOOR EVAC SLID E. AIR CRUISERS INSPECTED THE BOTTLE AND FOUND IT TO BE LEAKING FROM THE GAUGE ADAPTER O-RING. REPAIRED BY AIR CRUISER S, REFILLED, LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999120400616 19991204 00616 WP 1999 12 4 AALA996026 1 19991013 A 3350 BR9661106 EXIT SIGN DOUG DC9 DC983 3022083 WP ROW 20 LOOSE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 872RA 49793 RNO - EMERGENCY EXIT SIGN AT ROW 20 ON RT, TORN FROM WALL. RESECURED EXIT SIGN AS REQUIRED. (M) 2 L 7 2 4F RT A6WE 1999120400617 19991204 00617 NM 1999 12 4 AALA996030 1 19991021 A 3320 5D03911 LIGHTS DOUG MD90 MD9030 3023690 NM SEATS 9 A/C FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 903RA 53551 SNA - READING LIGHTS SEAT 9AC EXTREMELY HOT, AND SMOKE OBSERVED BY FLT ATTENDANT. REPLACED 9A AND 9C READING LIGHTS. O PS CHECK NORMAL. NO SMOKE NOTED. (M) 2 L 7 2 4F RT A6WE 1999120400618 19991204 00618 WP 1999 12 4 AALA996037 1 19991102 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 22-26 DISCHARGED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 754RA 49641 RNO - ROW 22-26 EMERGENCY LIGHTS INOPERATIVE. REPLACED LEFT AFT EXIT BATTERY PACK PER MM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999120400619 19991204 00619 WP 1999 12 4 AALA996033 1 19991102 A 3350 BC50447907 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833RA 53045 FORWARD OVERWING OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING OVERHEAD EMERGENCY EXIT LIGHT . OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999120400620 19991204 00620 WP 1999 12 4 AALA996034 1 19991102 A 3397 WIRE DOUG DC9 DC983 3022083 WP SEAT 9DEF DISCONNECTED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833RA 53045 EMERGENCY PATH LIGHT AT 9DEF INOPERATIVE. RECONNECTED WIRE. CONNECTOR ON EMERGENCY PATH LIGHT AT 9DEF. OPS CHECK GOOD . (M) 2 L 7 2 4F RT A6WE 1999120400621 19991204 00621 WP 1999 12 4 AALA996032 1 19991030 A 3350 BR9661105 BATTERY PACK DOUG DC9 DC983 3022083 WP SEAT 1 DEF DISCHARGED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832RA 53044 SJC - EMERGENCY LIGHTS INOPERATIVE AT SEAT 1 D-F. REMOVED AND REPLACED FORWARD ENTRY BATTERY PACK. OPS CHECK GOOD. (M ) 2 L 7 2 4F RT A6WE 1999120400622 19991204 00622 NM 1999 12 4 AALA996028 1 19990717 A 3397 WIRE DOUG MD90 MD9030 3023690 NM CABIN PINCHED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 901RA 53489 OKC - EMERGENCY FLOOR TRACK LIGHTING FAILED STEP H 1. REPAIRED PINCHED WIRE IN FLOOR TRACK SYSTEM. OPS CHECK NORMAL IA W MD-90 MM 20-10-03. OPS CHECK GOOD IAW C-CHECK CARD 1C-114 STEP H. 1. (M) 2 L 7 2 4F RT A6WE 1999120400623 19991204 00623 NM 1999 12 4 AALA996029 1 19990717 A 3397 WIRE DOUG MD90 MD9030 3023690 NM ROW 1 BROKEN A AALA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 901RA 53489 OKC - EMERGENCY FLOOR TRACK LIGHTING FAILED STEP B.1 WIRES BROKEN AT LIGHT ASSY ROW 1 FORWARD LIGHT. REPLACED BULB AND REPAIRED BROKEN WIRES IAW MD-90 MM 20-50-01. OPS CHECK GOOD IAW C-CHECK CARD NR 1C-114 STEP B.1. (M) 2 L 7 2 4F RT A6WE 1999120400624 19991204 00624 WP 1999 12 4 AALA996031 1 19991018 A 3350 59306431 BATTERY DOUG DC9 DC983 3022083 WP FWD/AFT GALLEY DISCHARGED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 882RA 49949 SJC - EMERGENCY BATTERY PACKS ON FORWARD GALLEY AND AFT GALLEY INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS ON FORWA RD GALLEY AND AFT GALLEY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999120400625 19991204 00625 NM 1999 12 4 AALA996025 1 19991013 A 3350 1001191 CHARGER DOUG MD90 MD9030 3023690 NM CABIN FAILED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 901RA 53489 SNA - 1ST CLASS FLOOR E-LIGHTS INOPERATIVE. REMOVED AND REPLACED E-PACK CHARGING UNIT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999120400626 19991204 00626 NM 1999 12 4 AALA996024 1 19991014 A 3350 1001191 BATTERY PACK DOUG MD90 MD9030 3023690 NM CABIN DISCHARGED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 901RA 53489 SNA - MAIN ENTRANCE EMERGENCY EXIT SIGN LIGHT OUT, BATTERY CHARGER INOPERATIVE. REPLACED BATTERY PACK POWR SUPPLY. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999120400627 19991204 00627 1999 12 4 AALA996020 4 19991008 A 2565 D29985103 EVAC SLIDE DOUG DC9 DC982 3022082 WP GALLEY OPEN A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 823RA 49889 RNO - AFT GALLEY SLIDE PACKS NEEDS TO BE STOWED. REINSTALLED SLIDE COVER IN AFT GALLEY PER MM. (M) 2 L 7 2 4F A6WE 1999120400628 19991204 00628 NM 1999 12 4 BJNA110199 1 19991112 A 3350 CONNECTOR BOEING 737 737282 13844AT NM CABIN CONTAMINATED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 233TM 23043 CENTER SECTION OF EMERGENCY LIGHT WON'T COME ON WITH MASTER SWITCH. CLEANED CONNECTOR MATING ON EL LAMP, TESTED EMERGEN CY LIGHT SYSTEM, PER LOCTITE MAINTENANCE MANUAL. OPS TEST OK. (M) 2 L 7 2 4F RT A16WE 1999120400629 19991204 00629 1999 12 4 99ZZZM789 4 19991021 A 6122 311849601 PROP GOVERNOR WOODWARD BEECH 1900 1900D 1154162 CE RT ENGINE FLUCTUATING A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 834CA 12734 2488895 UE25 RIGHT PROP RPM AND TORQUE FLUCTUATING. REPLACED RIGHT ENGINE PROP GOVERNOR, REVERSING ARM AND BETA BLOCK. AIRCRAFT TES T FLOWN AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999120400630 19991204 00630 EU 1999 12 4 C2XA99IA566 1 19991024 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS LEFT AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400631 19991204 00631 EU 1999 12 4 C2XA99IA567 1 19991024 A 5320 S53678008216300 CHANNEL AEROSP ATR42 ATR42300 8680920 EU FRAME 39-41 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE RIGHT 'Z' CHANNEL WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED 'Z' CHANNEL IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. (M) 2 H 7 2 4T RT A53EU 1999120400632 19991204 00632 EU 1999 12 4 C2XA99IA568 1 19991024 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS FORWARD RIGHT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999120400633 19991204 00633 EU 1999 12 4 C2XA99IA569 1 19991024 A 5347 S53678001240 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FRAME 34-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK WAS FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 36. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400634 19991204 00634 EU 1999 12 4 C2XA99IA570 1 19991024 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER RE PAIR ON THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400635 19991204 00635 EU 1999 12 4 C2XA99IA571 1 19991024 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS LEFT FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 1999120400636 19991204 00636 EU 1999 12 4 C2XA99IA572 1 19991024 A 5320 S53572804200 STRAP AEROSP ATR42 ATR42300 8680920 EU FRAME 27 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE OUTER STRAP AT FRAME 27 LEFT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRAC K IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING REPAIR AUTHORIZATION EC5340-01041, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400637 19991204 00637 SO 1999 12 4 C2XA99IA574 1 19991103 A 5411 12003857001 FRAME EMB 120 EMB120RT SO LEFT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT AND RIGHT NACELLE NR 1 FRAMES CRACKED. REMOVED AND REPLACED LEFT AND RIG HT ENGINE NACELLE NR 1 FRAMES IAW SRM 51-25-00 AND 54-10-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400638 19991204 00638 SO 1999 12 4 99ZZZM790 1 19991103 A 5411 12003857001 FRAME EMB 120 EMB120RT SO RIGHT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT AND RIGHT NACELLE NR 1 FRAMES CRACKED. REMOVED AND REPLACED LEFT AND RIG HT ENGINE NACELLE NR 1 FRAMES IAW SRM 51-25-00 AND 54-10-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999120400639 19991204 00639 SO 1999 12 4 C2XA99CL120 1 19991110 A 2120 BWT138001 NOISE ATTENUATOR EMB 145 EMB145ER SO CABIN LOOSE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 13929 145009 CLE - FLT 4041 - THE CREW REPORTED SMOKE IN THE AIRCRAFT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE PACK SYSTEM AND FOUND THE LEFT NOISE ATTENUATOR AND CLAMP HAD COME LOOSE. MAINTENANCE RESECU RED THE NOISE ATTENUATOR AND CLAMP AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED IAW EMB145 MM 21-20-04 AND 2 1-20-00. REFERENCE EMB145 IPC 21-24-01 FOR LOCATION OF PARTS. (M) 2 L 7 2 4F RT T00011AT 1999120400640 19991204 00640 SO 1999 12 4 99ZZZM791 1 19991110 A 2120 NAS192204501H CLAMP EMB 145 EMB145ER SO CABIN LOOSE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 13929 145009 CLE - FLT 4041 - THE CREW REPORTED SMOKE IN THE AIRCRAFT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE PACK SYSTEM AND FOUND THE LEFT NOISE ATTENUATOR AND CLAMP HAD COME LOOSE. MAINTENANCE RESECU RED THE NOISE ATTENUATOR AND CLAMP AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED IAW EMB145 MM 21-20-04 AND 2 1-20-00. REFERENCE EMB145 IPC 21-24-01 FOR LOCATION OF PARTS. (M) 2 L 7 2 4F RT T00011AT 1999120400641 19991204 00641 EU 1999 12 4 C2XA99IA588 1 19991108 A 3610 311489201 VALVE AEROSP ATR42 ATR42500 EU NR 2 ENGINE FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 16450 510 IAH - DURING FLIGHT 3557, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE AIR SWITCHING VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400642 19991204 00642 SO 1999 12 4 C2XA99CL121 1 19991103 A 2510 SEAT EMB 145 EMB145 SO COCKPIT MALFUNCTIONED A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 09 13956 145078 CLE - FLT 4234 - THE CREW REPORTED THAT ON TAKEOFF ROLL, THE CAPTAINS SEAT SLIDED BACK. THE AIRCRAFT ABORTED TAKEOFF AN D RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE CAPTAINS SEAT TRACKS AND INSPECTED T HE SEAT, NO DEFECTS WERE NOTED WORK WAS DONE IAW EMB145 MM 25-11-00. (M) 2 L 7 2 4F RT T00011AT 1999120400643 19991204 00643 CE 1999 12 4 C2XA99CL122 1 19991108 A 7722 3034857 THERMOCOUPLE BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 09 87552 MR16441 UE216 CLE - FLT 3439 - THE CREW REPORTED THAT AFTER TAKEOFF THE RIGHT ITT WENT TO 810C WITH ALL OTHER INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE TRIM THERMO COUPLE IAW P/W MM 77-20-01. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999120400644 19991204 00644 SO 1999 12 4 C2XA99CL123 1 19991110 A 2752 3633001017 ACTUATOR EMB 145 EMB145LR SO TE FLAP FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14952 00259 145067 CLE - FLT 3973 - THE CREW REPORTED THAT AFTER TAKEOFF, THE FLAPS GOT STUCK AT THE 4 DEGREE POSITION. THE AIRCRAFT RETUR NED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMB145 MM 27-51-09. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999120400645 19991204 00645 SO 1999 12 4 C2XA99BT102 1 19991109 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 EWR - FLT 4184 - CREW REPORTED REAR EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY PACK AND OPS CH ECKED THE SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999120400646 19991204 00646 EU 1999 12 4 UF6A991107 1 19991113 A 3242 ACA2100 VALVE DUNLOP BAG ATP ATP EU BRAKE SYSTEM FAILED A UF6A A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 31 853AW 562 LE505 2022 CWA - FLT 5735 - BRAKE LOW PRESSURE CWP ILLUMINATED DURING THE TOP OF DESCENT. OUTER BRAKE PRESSURE INDICATED ZERO. MA INTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999120400647 19991204 00647 EU 1999 12 4 UF6A991108 1 19991113 A 5751 JD5760001000W AILERON BAG ATP ATP EU WS 518.830 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 SBN - LEFT AILERON IS DAMAGED ON THE TRAILING EDGE. MAINTENANCE REPAIRED DAMAGE. ALL WORK WAS DONE IAW ATP SRM 57-60-0 1. (M) 2 L 7 2 4T RT A27NM 1999120400648 19991204 00648 EU 1999 12 4 C2XA99IA576 1 19991030 A 5720 S57210535200 ANGLE AEROSP ATR42 ATR42320 8680930 EU LT WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT WING FORWARD SPAR, LOWER SPAR CAP AT RIB 19. REMOVED CORROS ION, FABRICATED REPAIR ANGLE AND INSTALLED IAW DER REPORT NR 99-209 DER SO423, STRUCTURES. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400649 19991204 00649 EU 1999 12 4 C2XA99IA578 1 19991030 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36/40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 40. REMOVED AND REPLACED CORRO DED SECTION OF SEAT TRACK IAW SRM 51-31-31, 51-32-40, 53-00-00, 53-63-00, 51-25-00, 51-25-04, 51-21-17 AND 51-21-28. AI RCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400650 19991204 00650 EU 1999 12 4 C2XA99IA577 1 19991030 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36/40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 40. REMOVED AND REPLACED CORR ODED SECTION OF SEAT TRACK IAW SRM 51-31-31, 53-00-00, 53-63-00, 51-25-00, 51-21-17 AND 51-21-31. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400651 19991204 00651 EU 1999 12 4 C2XA99IA579 1 19991030 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND SEAT TRACK AT LBL 37 CORRODED AT FRAME 36. REMOVED AND REPLACED CORRODED SECT ION OF SEAT TRACK IAW SRM 53-00-00, 51-21-25, 51-25-00, 51-25-04 AND 51-21-17 AND 51-21-18. AIRCRAFT APPROVED FOR RETUR N TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400652 19991204 00652 EU 1999 12 4 C2XA99IA580 1 19991030 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND SEAT TRACK AT LBL 13 CORRODED AT FRAME 36. REMOVED AND REPLACED CORRODED SECT ION OF SEAT TRACK IAW SRM 53-00-00, 51-25-00, 51-21-17 AND 51-21-27. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400653 19991204 00653 EU 1999 12 4 C2XA99IA581 1 19991030 A 5311 S53672108200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON FRAME 36. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOU BLERS IAW CONTINENTAL EXPRESS EC5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400654 19991204 00654 EU 1999 12 4 C2XA99IA582 1 19991030 A 5311 S53672409200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON FRAME 40. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOU BLERS IAW CONTINENTAL EXPRESS EC5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400655 19991204 00655 EU 1999 12 4 C2XA99IA583 1 19991030 A 5311 S53672308200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON FRAME 38. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOU BLERS IAW CONTINENTAL EXPERSS EC5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400656 19991204 00656 EU 1999 12 4 C2XA99IA584 1 19991030 A 5311 S53672408200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON FRAME 39. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOU BLERS IAW SRM 51-31-31 AND 51-21-28. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400657 19991204 00657 EU 1999 12 4 C2XA99IA585 1 19991030 A 5311 S53672409200 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON FRAME 40. REMOVED CORROSION, FABRICATED AND INSTALLED REINFORCEM ENT STRAPS IAW CONTINENTAL EXPRESS EC5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400658 19991204 00658 EU 1999 12 4 C2XA99IA586 1 19991030 A 5320 S5367800920102 ANGLE AEROSP ATR42 ATR42320 8680930 EU FRAME 36/38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON SUPPORT ANGLE BELOW RIGHT THRESHOLD, FRAME 36 AND 38. REMOVED AN D REPLACED ANGLE IAW SRM 51-25-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400659 19991204 00659 EU 1999 12 4 C2XA99IA587 1 19991030 A 5320 S5367800820002 ANGLE AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT FLOOR SILL SUPPORT ANGLE AT FRAME 39. REMOVED AND REPLACED ANGLE IAW SRM 51-25-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999120400660 19991204 00660 WP 1999 12 4 VTZA990248 2 19990721 A 7320 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 317UE 41031 FLT 7602 - IAD-BGM - AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT ENGINE ONLY MADE 94 PERCENT TORQUE. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED RIGHT ENGINE MAX FUEL FLOW, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999120400661 19991204 00661 WP 1999 12 4 VTZA990245 2 19990718 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP NR 1 ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 495UE 818 FLT 7486 - IAD-BUF - DURING TAKEOFF, CREW ABORTED TAKEOFF DUE TO NR 1 ENGINE RPM ROLLED BACK TO 99.5 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED X-SCREW, OPS CHECK OK. AIRCRAFT WAS RELE ASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999120400662 19991204 00662 WP 1999 12 4 VTZA990243 2 19990716 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP NR 2 ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 489UE 908 FLT 7439 - IAD-GSO - CREW ABORTED TAKEOFF DUE TO NR 2 ENGINE RPM DROPPED TO 99.5 PERCENT ON TAKEOFF ROLL. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED X-SCREW, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999120400663 19991204 00663 NE 1999 12 4 REXA99028 2 19990904 A 7261 4074T58P0904 O-RING SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE DETERIORATED A REXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 922MA 340A077 IN FLIGHT SHUTDOWN OF RIGHT ENGINE DUE TO CWP WARNING LIGHT AND OIL PRESSURE BELOW 30 PSI. REMOVED AND REPLACED 'C' SUM P COVER O-RING AND STRUT O-RINGS ON RT ENGINE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999120400664 19991204 00664 NE 1999 12 4 99ZZZM792 2 19990216 A 7230 COMPRESSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 ENGINE DAMAGED A A6WA O OTHER E Y VIBRATION/BUFFET ENGINE STOPPAGE CR CRUISE 1 GL 31 607AW E2052 NR 1 ENGINE VIBRATION 2.5 AIRBORN ENGINE SHUTDOWN BY EMERGENCY CHECKLIST. INSPECTED AND FOUND BLADES MISSING FROM NR 3 AND NR 4 WHEEL AND DAMAGE TO NR 2 WHEEL AND SUSPECT DAMAGE TO NR 1 WHEEL. AIRCRAFT TO BE FERRIED TO ATW. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1999120400665 19991204 00665 NE 1999 12 4 UF6A990532 2 19990506 A 7310 158P36394 TUBE BAG ATP ATP EU PWA PW120 PW126A NE LEFT DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT AND RIGHT FUEL SUPPLY TUBES HAS SEVERAL DENTS. MAINTENANCE REMOVED AND REPLACED TUBES. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999120400666 19991204 00666 NE 1999 12 4 99ZZZM793 2 19990506 A 7310 154P3694 TUBE BAG ATP ATP EU PWA PW120 PW126A NE RIGHT DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 2034 SBN - LEFT AND RIGHT FUEL SUPPLY TUBES HAS SEVERAL DENTS. MAINTENANCE REMOVED AND REPLACED TUBES. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999120400667 19991204 00667 EU 1999 12 4 UF6A990934 1 19990927 A 5414 JD711J0016000 PANEL BAG ATP ATP EU NR 2 ENGINE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2701265R3 2035 SBN - THE RIGHT OUTBOARD IGNITER PANEL IS CRACKED. MAINTENANCE REPAIRED PANEL. ALL WORK WAS DONE IAW ENGINEERING ORDER 98-210. (M) 2 L 7 2 4T RT A27NM 1999120400668 19991204 00668 NE 1999 12 4 C2XA99CL116 2 19991013 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT MALFUNCTIONED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 69549 UE194 FLT 3173 - THE CREW REPORTED THE RIGHT ENGINE LOST POWER. THE AIRCRAFT RETURNED TO ERI WITHOUT FURTHER INCIDENT. MAINT ENANCE RAN THE NR 2 ENGINE, CHECKED ALL ENGINE RIGGING AND PERFORMED ENGINE RUNS. NO DEFECTS WERE NOTED IAW BEECHCRAFT MM 76-10-00. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999120400669 19991204 00669 NE 1999 12 4 99ZZZM794 2 19991105 A 7310 1082853 LINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE MISINSTALLED A AMTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 11 518AT 11851 27974 DURING A RELIABILITY RESEARCH, FOUND THE HP SHUTOFF FLEX HOSE CHAFING AGAINST THE C-DUCT ACTUATOR ON THE RIGHT ENGINE. F URTHER RESEARCH REVEALED THAT THE FLEX HOSE WAS IMPROPERLY INSTALLED AT MANUFACTURER. THE ADEL CLAMPS WERE ALSO FOUND I NSTALLED ON THE FLEX LINE INSTEAD OF THE RIGID TUBING. REPLACED THE CHAFED FLEX LINE AND INSTALLED PER BOEING DWG NR 31 2N5309. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1999120400670 19991204 00670 NM 1999 12 4 USAA991116 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 45.5 IN RADIUS FORWARD SIDE OF FLOORBEAM. INSTALLED DOUBLER, FILLER AND REPAIR ANGLES PER EA 65721 AND S/B 737-53-1120. (M) 2 L 7 2 4F RT A16WE 1999120400671 19991204 00671 NM 1999 12 4 USAA991115 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, LBL 24.75 IN RADIUS FORWARD SIDE OF FLOORBEAM. INSTALLED DOUBLER, FILLER AND REPAIR ANGLES PER EA 65721 AND SB 737-53-1120. (M) 2 L 7 2 4F RT A16WE 1999120400672 19991204 00672 NM 1999 12 4 USAA991114 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 520, RBL 45.5 IN RADIUS FORWARD SIDE OF FLOORBEAM. INSTALLED DOUBLER, FILLER AND REPAIR ANGLES PER EA 65721 AND S/B 737-57-1120. (M) 2 L 7 2 4F RT A16WE 1999120400673 19991204 00673 NM 1999 12 4 USAA991113 1 19991016 A 5320 CLIP BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 847, STRINGER 25L TIE CLIP. INSTALLED NEW STRINGER TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400674 19991204 00674 NM 1999 12 4 USAA991112 1 19991016 A 5320 CLIP BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727B, STRINGER 25L TIE CLIP. REPLACED WITH IDENTIC AL PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999120400675 19991204 00675 NM 1999 12 4 USAA991104 1 19991016 A 5320 CLIP BOEING 737 7373B7 1384580 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 827, STRINGER 25L TIE CLIP. REPLACED WITH IDENTICA L PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999120400676 19991204 00676 NM 1999 12 4 USAA991102 1 19991013 A 5510 ANGLE BOEING 737 737301 1384611 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT HORIZONTAL STAB CENTER SECTION THRUST BEAM ATTACH ANGL E. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400677 19991204 00677 NM 1999 12 4 USAA991046 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STATION 400 BETWEEN STRINGER 8R AND STRINGER 9R FRA ME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 65705. (M) 2 L 7 2 4F RT A16WE 1999120400678 19991204 00678 NM 1999 12 4 USAA991041 1 19991016 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN STRINGER TIE CLIP AT STATION 847 AND STRINGER 25L. I NSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400679 19991204 00679 NM 1999 12 4 USAA990824 1 19990903 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SHEAR TIE STATION 639 STRINGER 7R AND 8R. REPAIRED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400680 19991204 00680 NM 1999 12 4 USAA990926 1 19990903 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 251 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH FORWARD OF STATION 251 FRAME, RBL 16, WL 157 ALONG INBO ARD ROW OF FASTENERS RIGHT LOWER CHORD ANGLE. CORROSION LEVEL 2. REPLACED RIGHT LOWER CHORD ANGLE IN NLG WHEEL WELL PE R SRM 51-70-12 FIG 1, BAC DWG 65-45819 AND EA 65426. (M) 2 L 7 2 4F RT A16WE 1999120400681 19991204 00681 NM 1999 12 4 USAA990910 1 19990903 A 5320 CHORD BOEING 737 737301 1384611 NM BS 270 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 270, RBL 2.5 - LBL 2.5 Z-CHORD. CORROSION LEVEL 1. REPAIRED REPLACEMENT 'Z' CHORD PER EA 65414 AND TR 53-20-04. (M) 2 L 7 2 4F RT A16WE 1999120400682 19991204 00682 NM 1999 12 4 USAA990882 1 19990903 A 5320 WEB BOEING 737 737301 1384611 NM MLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK SHEAR BEAM WEB SHELF 18A AFT WW BULKHEAD. INSTALLED DOU BLER PER EA 65323. (M) 2 L 7 2 4F RT A16WE 1999120400683 19991204 00683 NM 1999 12 4 USAA990875 1 19990903 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION LBL 21, 28, 35, 42 AND 45, BS 344, WL 208.1 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW SECTION OF T-CAP WITH REPAIR ANGLES PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999120400684 19991204 00684 NM 1999 12 4 USAA990876 1 19990903 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH AREA OF CORROSION STATIO N1006, LBL 26 FLOORBEAM. CORROSION LEVEL 1. INSTALLED REPAIR STRAP PER EA 65360 AND SRM 53-00-51 FIG 203. (M) 2 L 7 2 4F RT A16WE 1999120400685 19991204 00685 NM 1999 12 4 USAA990877 1 19990903 A 5240 SKIN BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT SERVICE DOOR FORWARD EDGE 30 INCH BELOW TOP SKIN. IN STALLED DOUBLER PER SRM 52-10-01. (M) 2 L 7 2 4F RT A16WE 1999120400686 19991204 00686 NM 1999 12 4 USAA990855 1 19990903 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 289.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACK AT BS 289.5 STRINGER 10R WEB ANGLE. INSTALLED NEW WEB ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400687 19991204 00687 NM 1999 12 4 USAA990838 1 19990903 A 5320 SPLICE BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 5R SPLICE. REPLACED SPLICE PE R SRM 51-00-02. (M) 2 L 7 2 4F RT A16WE 1999120400688 19991204 00688 NM 1999 12 4 USAA990839 1 19990903 A 5311 FRAME BOEING 737 737301 1384611 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 887, STRINGER 9L FRAME. INSTALLED DOUBLER P ER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999120400689 19991204 00689 NM 1999 12 4 USAA990840 1 19990903 A 5320 CLIP BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 727D STRINGER 4R. REPLACED CLIP PER SRM 51-10-02 . (M) 2 L 7 2 4F RT A16WE 1999120400690 19991204 00690 NM 1999 12 4 USAA990841 1 19990903 A 5320 CLIP BOEING 737 737301 1384611 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 663.75 AT STRINGER 10R. REPLACED CLP PER SRM 51- 10-02. (M) 2 L 7 2 4F RT A16WE 1999120400691 19991204 00691 NM 1999 12 4 USAA990842 1 19990903 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 616, STRINGER 4R TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400692 19991204 00692 NM 1999 12 4 USAA990843 1 19990903 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616, STRINGER 8L TIE CLIP. REPLACED CLIP PER SR M 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400693 19991204 00693 NM 1999 12 4 USAA990837 1 19990903 A 5320 SPLICE BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 907, STRINGER 4L SPLICE. REPLACED SPLICE PE R SRM 51-00-02. (M) 2 L 7 2 4F RT A16WE 1999120400694 19991204 00694 NM 1999 12 4 USAA990821 1 19990903 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 5L TIE CLIP. INSTALLED NEW TIE CL IP PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999120400695 19991204 00695 NM 1999 12 4 USAA990822 1 19990903 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 3R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400696 19991204 00696 NM 1999 12 4 USAA990823 1 19990903 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 38542 23236 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727D STRINGER 7R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999120400697 19991204 00697 NM 1999 12 4 USAA990685 1 19990729 A 5320 ANGLE BOEING 737 737301 1384611 NM BS480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT BS 480 STRINGER 9L BAG BIN ATTACH ANGLE. FABRICATE D NEW REPAIR DOUBLER PER SRM 53-00-07 AND EA 650009. (M) 2 L 7 2 4F RT A16WE 1999120400698 19991204 00698 WP 1999 12 4 USAA991217 1 19991029 A 5320 JAMB DOUG DC9 DC931 3022065 WP PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 982VJ 43129 48158 PIT - DURING RON, FUOND 1.5 INCH CRACK ON SKIN AND DOUBLER AT FORWARD PASS ENTRANCE DOOR JAMB UPPER FORWARD CORNER. INS TALLED DOUBLERS PER SRM 53-05 FIG 26. (M) 2 L 7 2 4F A6WE 1999120400699 19991204 00699 NM 1999 12 4 USAASB99266 1 19991106 A 5240 10604764 SEAL BOEING 737 737201 1384454 NM RT SERVICE DOOR OUT OF POSITION A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 247US 22754 TPA - FLT 2733 - FLT DEPARTURED IAD, EN ROUTE TO FLL, OPERATING WITH MEL 26-12. AIRCRAFT BEGAN OT EXPERIENCED CABIN PRE SSURE FLUCTUATIONS. AIRCRAFT HAD BEEN FLYING AT FL240 DUE TO MEL RESTRICTION WHEN THE CABIN ALTITUDE ROSE TO 8,500 FEET AND A PRESSURE DIFFERENTIAL OF 5.2. PRESSURIZATION STABILIZED FOR A SHORT TIME BEFORE CLIMBING TO 9,000 FEET WITH A DI FFERENTIAL OF 5.0. CAPTAIN DESCENDED TO FL180 AND THE CABIN STABILIZED IN STANDBY MODE FOR A WHILE UNTIL THE CABIN ALTI TUDE BEGAN TO CLIMB AGAIN. CAPTAIN DESCENDED TO FL100 AND THE CABIN STABILIZED. FLIGHT DIVERTED TO TPA AND LANDED WITH OUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REINSTALLED THE DOOR SEAL AT THE LOWER FORWARD CORNER OF 2 L 7 2 4F A16WE 1999120400700 19991204 00700 WP 1999 12 4 USAAD99155 1 19991105 A 3260 1D32140571 SENSOR DOUG DC9 DC931 3022065 WP NLG LOOSE A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 977VJ 48155 PIT-YYZ - FLT 1750 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THE FLIGHT CREW FELT A VIBRATION IN THE NOSE GEAR WELL AR EA AS IF THE NOSE WHEELS WERE STILL SPINNING. ALSO, THE GEAR UNSAFE LIGHT STAYED ON. THE LANDING GEAR WAS EXTENDED AND THE NOSE GEAR GREEN LIGHT WAS VERY SLOW TO ILLUMINATE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR UPLOCK SENSOR LOOSE. THE SENSOR WAS ADJUSTED AND THE NOSE WHEEL BRAKE BARS WERE REPLA CED. (M) 2 L 7 2 4F A6WE 1999120400701 19991204 00701 NM 1999 12 4 USAASB99201 1 19990813 A 3610 32895624 CONTROL VALVE BOEING 737 7373B7 1384580 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 531AU 22928 24478 CLT - FLT2250 - AIRCRAFT DEPARTED CLT WITH LEFT PACK ON MEL. ON CLIMB-OUT AT APPROXIMATELY 8,000 FEET, CREW LOST THE RI GHT PACK AS THE RIGHT PACK FAIL LIGHT ILLUMINATED. CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT AND DECIDED TO RETURN TO FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCDIENT. NO EMEGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLA CED THE NR 2 ENGINE PRECOOLER CONTROL VALVE. RIGHT PACK OPERATIONAL CHECK GOOD. PRESSURIZATION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999120400702 19991204 00702 NM 1999 12 4 USAASB99205 1 19990819 A 3260 INDICATION BOEING 737 7373B7 1384580 NM LANDING GEAR MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 371US 22950 CLT - FLT 432 - AFTER TAKEOFF AND GEAR RETRACTION FROM CHS, BOTH THE LEFT AND RIGHT MAIN LANDING GEAR UNSAFE LIGHTS REMA INED ILLUMINATED WHILE THE NOSE LANDING GEAR INDICATED UP AND DOORS CLOSED. CREW RECYCLED THE GEAR AND RECEIVED NORMAL INDICATION. FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE JACKED AIRCRAFT AND SWUNG THE GEA R SIX TIMES. UNABLE TO DUPLICATE PROBLEM. CYCLE TIMES CHECKED GOOD PER MM 32-32-00. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1999120400703 19991204 00703 NM 1999 12 4 USAASB99207 1 19990820 A 5610 5717623115 WINDOW BOEING 737 737301 1384611 NM LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 576US 29629 23741 TPA - FLT 2335 - EN ROUTE FROM FLL TO CLT, THE CAPTINS L2 SLIDING WINDOW CRACKED. FLIGHT DIVERTED TO TPA AND LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS L2 SLIDING WINDOW AND THE WINDOW HEAT CONTROLLER ( P/N 231-2). OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 1999120400704 19991204 00704 NM 1999 12 4 USAASB99175 1 19990718 A 3260 189929 UPLOCK SENSOR BOEING 737 7373B7 1384580 NM RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 395US 23317 CLT - FLT 249 - DURING CLIMB-OUT FROM CLT, THE RIGHT MLG UNSAFE LIGH TILLUMINATED WITH THE GEAR UP. FLIGHT RETUREND TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGH T MLG UPLOCK SENSOR. OPERATIONAL CHECK GOOD PER MM 32-61-21. (M) 2 L 7 2 4F RT A16WE 1999120400705 19991204 00705 NM 1999 12 4 USAASB99177 1 19990719 A 3020 1726256 ANTI-ICE VALVE BOEING 737 7373B7 1384580 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 516AU 39865 23702 PIT - FLT 620 - EN ROUTE FROM LAS TO PHL, DURING CRUISE, THE NR 1 ENGINE COWL ANTI-ICE LIGHT ILLUMINATED WHEN SELECTED O N. CREW REDUCED POWER AND LIGHT EXTINGUISHED. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A16WE 1999120400706 19991204 00706 NM 1999 12 4 USAASB99179 1 19990720 A 2740 50556011 CHAIN BOEING 737 7373B7 1384580 NM FLIGHT COMPAR OUT OF ADJUST A USAA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 EA 19 525AU 23860 PIT - FLT 1217 - DURING CLIMB-OUT FROM PIT, CREW NOTICED A VIBRATION THAT CONTINUED AFTER RETRACTING THE GEAR AND THE FL APS. VIBRATION EVEN REGISTERED ON THE AVM GAUGE FOR THE NR 1 ENIGNE. CREW LEVELED OFF AT FL 230 AND STATED THAT THE VI BRATION WAS MOST NOTICEABLE WHEN CONTROLLING THE STABILIZER TRIM. AFTER CONSULTING WITH MAINTENANCE CONTROL, THE CREW E LECTED TO RETURN TO FIELD AT PIT RATHER THAN CONTINUING ON TO DFW. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DE CLARED. MAINTENANCE FOUND THE FORWARD STABILIZER CONTROL MECHANISM CHAIN DRIVE OUT OF ADJUSTMENT. ADJUSTED SAME PER MM 27-41-41. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999120400707 19991204 00707 NM 1999 12 4 USAASB99247 1 19991012 A 3244 6558256275 TIRE BOEING 737 737301 1384611 NM LT MLG FAILED A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 591US 384 23936 LAS - FLT 606 - AFTER T/O AND GEAR ACTUATION, THE 'A' HYD SYS LOW PRESSURE LIGHTS ILLUMINATED AND THE HYD QTY WENT TO ZE RO. CREW COULD NOT GET THE GEAR TO RETRACT. AN EMERGENCY WAS DECLACED. FLIGHT RETURNED TO FIELD AT LAS AND LANDED WIT HOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED TO THE GATE DUE TO LOSS OF NOSE WHEEL STEERING. MAINTENANCE FOUND THE LEFT M LG NR 2 TIRE RECAP HAD COME OFF AND DAMAGED HYDRAULIC LINES TO THE LEFT MLG HYD MODULE. REPLACED HYD LINES AND A CABLE GUIDE THAT WAS BROKEN OFF NEXT TO THE HYD MODULE. REMOVED AND REPLACED THE LEFT WING INBOARD T/E AFT FLAP THAT WAS FOUN D DAMAGED FROM DEBRIS. REPLACED THE NR 2 TIRE ASSY. AS PRECAUTIONARY, REPLACED THE NR 1 TIRE ASSEMBLY. SERVICED RESER 2 L 7 2 4F RT A16WE 1999120400708 19991204 00708 EU 1999 12 4 USAAF99052 1 19991022 A 2150 LT PACK FOKKER F28 F28MK0100 4990807 EU AC BAY LEAKING A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 884US 11338 CLT - FLT 945 - AFTER TAKEOFF, A BURNING ODOR WAS NOTICED IN THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAK IN LEFT AIR CONDITIONING PACK. (M) 2 L 7 2 4F RT 1999120400709 19991204 00709 NM 1999 12 4 USAASB99252 1 19991018 A 2130 7110025 SELECTOR PANEL BOEING 737 737301 1384611 NM FLT COMPART FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 585US 23930 CLT - FLT 858 - ON CLIMB-OUT FROM CLT, THE AIRCRAFT WOULD NOT PRESSURIZE. CAPTAIN COULD NOT CONTROL PRESSURIZATION IN A UTO, STANDBY OR MANUAL MODE. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DEC LARED. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE SELECTOR PANEL PER MM 21-31-00. ALSO, REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER (P/N 763810-1) AND THE AFT OUTFLOW VALVE (P/N 711003-3). OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999120400710 19991204 00710 NM 1999 12 4 USAASB99222 1 19990907 A 5230 10608214 SEAL BOEING 737 7373B7 1384580 NM CARGO DOOR TORN A USAA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 EA 19 393US 23315 TPA - FLT 1469 - EN ROUTE FROM CLT TO TPA, ABOVE GAINESVILLE FLORIDA AT FL310, FLIGHT LOST PRESSURIZATION. THE CREW FEL T A THUMP IN THE CABIN ALONG WITH A RISE IN CABIN ALTITUDE OF 4,000 FEET PER MINUTE. CREW DECLARED AN EMERGENCY AND QUI CKLY DESCENDED TO 10,000 FEET, CREW REQUESTED A SLOW DESCENT FROM ATC. FLIGHT LANDED AT TPA WITHOUT FURTHER INCIDENT. A FTER ARRIVING AT GATE, MAINTENANCE DISCOVERED THAT THE AFT CARGO DOOR SEAL HAD BLOWN. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO DOOR SEAL AS IT WAS FOUND TORN. REPLACED OXYGEN GENERATORS AND CLEANED AND STOWED OXYGEN MASKS PER MM 35- 22-31. PRESSURIZATION CHECK OF AIRCRAFT GOOD. (M) 2 L 7 2 4F RT A16WE 1999120400711 19991204 00711 NM 1999 12 4 USAASB99260 1 19991027 A 2150 106050616 ACM BOEING 737 7372B7 1384560 NM LT A/C BAY WEAK A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 269AU 22881 BWI - FLT 2741 - FLT ON MX DELAY IN BDL, WHEREAS MX PLACED THE RT PACK ON MEL. FLT DEPARTED BDL AND WHILE FLYING OVER P HL, THE LT PACK WOULD ONLY HOLD CABIN PRESSURE TO 9,500 FT. CAPT ELECTED TO DIVERT TO BWI WHERE THE FLT LANDED W/O FURT HER INCIDENT. NO EMERGENCY WAS DECLARED. MX CLEARED THE RT PACK MEL BY REMOVING AND REPLACING THE RT PACK VLV (P/N 396 064-1-1). OPS CHECK GOOD. RAN BOTH ENG'S AND PRESSURIZED A/C TO FIVE PSI. PRESSURIZATION CHECK AND LEAK CHECK OF A/C GOOD. DUCT PRESSURES GOOD. FURTHERMORE, A TECH SERVICE ITEM WAS ISSUED FOR FOLLOWUP WHEREAS MX REMOVED AND REPLACED TH E LT ACM AND THE LT WATER SEPARATOR BAG (P/N V121-1). PERFORMED LEAK CHECK AND OPS CHECK. A/C PRESSURIZED TO 3 PSI WIT 2 L 7 2 4F A16WE 1999120400712 19991204 00712 NM 1999 12 4 USAABB99048 1 19990909 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AU 27201 MCO - THE LOW LEVEL AISLE EMERGENCY LIGHTS DID NOT TEST PROPERLY, BUT DID OPERATE NORMALLY. THE SITUATION WAS REMEDIED BY REPLACING THE BATTERY PACKS. (M) 2 L 7 2 4F RT A2NM 1999120400713 19991204 00713 NM 1999 12 4 EISA99175 1 19991004 A 2782 6516209 ACTUATOR BOEING 727 727231 1384079 NM RT LE SLAT MALFUNCTIONED A EISA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 74318 1115 20051 ON TAKEOFF, WHEN FLAPS AND LEADING EDGE DEVICES WERE RETRACTING, NR 7 SLAT FAILED TO RETRACT, RECYCLED BUT REMAINED EXTE NDED. AIR TURN BACK TO (VIT). UPON LANDING FLAPS WERE RETRACTED AND NR 7 SLAT RETRACTED. INSPECTED SLAT, NO DEFECTS N OTED. (M) 2 L 7 3 4F A3WE 1999120400714 19991204 00714 NM 1999 12 4 EISA99173 1 19991004 A 2782 6516209 ACTUATOR BOEING 727 727231 1384079 NM RT LE SLAT MALFUNCTIONED A EISA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 74318 1115 20051 ON TAKEOFF, WHEN FLAPS AND LEADING EDGE DEVICES WERE RETRACTING, NR 7 SLAT FAILED TO RETRACT, RECYCLED BUT REMAINED EXTE NDED. AIR TURN BACK TO (VIT). UPON LANDING FLAPS WERE RETRACTED AND NR 7 SLAT RETRACTED. INSPECTED SLAT, NO DEFECTS N OTED. (M) 2 L 7 3 4F A3WE 1999120400715 19991204 00715 NM 1999 12 4 EISA99211 1 19991016 A 3310 1500265 LIGHT BOEING 727 727223 1384074 NM P-6 PANEL FAILED A EISA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 316NE 19475 SMELLED ELECTRICAL BURNING SMELL IN COCKPIT. NOT DETECTABLE IN CARGO AREA, COULD NOT SEE SMOKE. SMELL STRINGER TOWARD BACK OF COCKPIT. INSPECTED AREA FOR SMELL FOUND PANEL ARCHING AT BULB TRANSFERRED LIGHT TO MEL 463 IAW B-727 MEL 33-1, BULB REMOVED. (M) 2 L 7 3 4F A3WE 1999120400716 19991204 00716 1999 12 4 EISA99207 4 19991018 A 3417 CADC HONEYWELL BOEING 727 72725 1384006 NM LT COCKPIT FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 290NE A1006 18972 BOTH ALTIMETERS (ELECTRIC) ON CAPTAINS SIDE INOPERATIVE. AIR TURN BACK TO BSL. REMOVED AND REPLACED CADC, OPS CHECK GO OD. (M) 2 L 7 3 4F A3WE 1999120400717 19991204 00717 NM 1999 12 4 EISA99133 1 19990713 A 7830 NAS1104SM BOLT BOEING 727 727223 1384074 NM NR 1 T/R UNIT MISSING A EISA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 6819 6537874 19494 NR 1 T/R LIGHT ON IN FLIGHT AIR ABORT, RETURN TO BRU. TROUBLE SHOT, FOUND BOLT ON SWITCH MISSING. INSTALLED BOLT. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999120400718 19991204 00718 NM 1999 12 4 EISA99210 1 19991028 A 5751 6521766211 AILERON BOEING 727 727223 1384074 NM LEFT DAMAGED A EISA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 07 6819 19494 AIRCRAFT HAS VIBRATION IN FLIGHT. REMOVED AND REPLACED LEFT OUTBOARD AILERON IAW MM REF 27-10, FUNCTIONAL CHECK GOOD. ( M) 2 L 7 3 4F A3WE 1999120400719 19991204 00719 NM 1999 12 4 EISA99212 1 19991027 A 5210 507945114 MECHANISM BOEING 727 727225 1384077 NM L1 DOOR OUT OF ADJUST A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 352PA 20616 L-1 DOOR WARNING LIGHT ILLUMINATED ON CLIMB-OUT, DOOR NOT IN CLOSED POSITION. AIRCRAFT WOULD NOT PRESSURIZE. RIGGED L- 1 DOOR OPERATION CHECK, PRESSURE CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999120400720 19991204 00720 NM 1999 12 4 AALA991538 1 19991006 A 3350 BATTERY BOEING 727 727223 1384074 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 878AA 21390 TUL - LIGHT INOPERATIVE, BATTERY WILL NOT HOLD CHARGE. INSTALLED NEW LIGHT ASSY, OPS CHECK OK MM 35-50-001-6. (M) 2 L 7 3 4F A3WE 1999120400721 19991204 00721 NM 1999 12 4 AALA991205 1 19990830 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 869AA 21374 TUL - FORWARD GALLEY 36 INCH LENGTH OF SEALED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED SECTION OF LIGHT ASSEMBLY, FOU ND BROKEN WIRE (E583053872). (M) 2 L 7 3 4F A3WE 1999120400722 19991204 00722 NM 1999 12 4 AALA991203 1 19990813 A 3350 LIGHT BOEING 727 727223 1384074 NM PAX DOORWAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 891AA 22007 TUL - EMERGENCY LIGHT ASSY IN AFT ENTRY OVERHEAD LIGHT WILL NOT COME ON WHEN AFT ATTENDANTS LIGHT SWITCH IS TURNED ON. I NSTALLED SERVICEABLE LIGHT LIGHT ASSY. (M) 2 L 7 3 4F A3WE 1999120400723 19991204 00723 NM 1999 12 4 AALA991204 1 19990810 A 3350 LIGHT BOEING 727 727227 1384078 NM PAX DOORWAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999120400724 19991204 00724 WP 1999 12 4 AALA991606 1 19991013 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - LONGERON 4L CRACKED AT STATION 160 OUTBOARD LEG AND INBOARD RADIUS. REMOVED CRACKED LONGERON SECTION OF LONGERON AND ACCOMPLISHED REPAIR PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999120400725 19991204 00725 WP 1999 12 4 AALA991607 1 19991019 A 5320 FRAME DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - FOUND CORROSION ON LONGERON 28R AT DOOR FRAME (CARGO AFT) FROM BS 1155-1212. BLENDED CORROSION PER SRM 51-10-3. I NSTALLED DOUBLER AT STATION 1172 PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 1999120400726 19991204 00726 NM 1999 12 4 AALA991048 1 19990716 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720AA 20613 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT SIGN IN FIRST CLASS SECTION INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999120400727 19991204 00727 NM 1999 12 4 AALA991132 1 19990803 A 3350 AAP2661 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 717AA 7350 20610 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT STAIRWELL INOPERATIVE. REPLACED AFT STAIRWELL EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999120400728 19991204 00728 NM 1999 12 4 AWXA9900437 1 19991129 A 5220 146610011 DOOR BOEING 757 7572G7 1384963 NM PAX DOOR OUT OF ADJUST A AWXA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 909AW 24522 AFT ENTRY DOOR EICAS MESSAGE DURING CLIMB. CABIN DOOR HANDLE COULD NOT BE LATCHED UNTIL A/C WAS DEPRESSURIZED PER QRH P ROCEDURE WAS ACCOMPLISHED. ADJUSTED L4 PASSENGER DOOR IAW MM 52-11-00, OPS CK GOOD. 2 L 7 2 4F RT A2NM 1999120400729 19991204 00729 EU 1999 12 4 AWXA9900438 1 19991129 A 2120 UNKNOWN AIRBUS 320 A320231 3930325 EU CABIN ODOR A AWXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 632AW 81 STRONG ODOR OF SMOKE IN AFT CABIN. RAN ENGINES AND APU ON BOTH PACKS TO ISOLATE MALFUNCTION. NO ODOR NOTED DURING ENG RUN OR AFTER SHUTDOWN. 2 L 7 2 4F RT A28NM 1999120400730 19991204 00730 NM 1999 12 4 AWXA9900440 1 19991201 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 EMERGENCY SEAT LIGHTS INOP ROW 15-20. REPLACED BATTERY PACK, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999120400731 19991204 00731 NM 1999 12 4 RAAA99B1027 1 19991019 A 5320 65C232312 FITTING BOEING 727 72722C 138400F NM BS 870 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING COMPLIANCE WITH AD91-24-11, FOUND FITTING CRACKED AT FS 870 RT ROW 2 IN SECOND AND THIRD HOLES BELOW S-9R ROW 1 A T TOP HOLE AND ROW 2 AT 5TH HOLE BELOW S-9R. REPLACED BODY TERMINAL FITTING IAW S/B 727-53-0116 DWG 65C23231. 2 L 7 3 4F A3WE 1999120400732 19991204 00732 NE 1999 12 4 RAAA99B1028 2 19991126 A 7200 JT8D7B ENGINE BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 2 STALLED A RAAA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION IN INSP/MAINT 1 AL 03 831RV 49977 779 19093 653555 DURING ENGINE TRIM RUN, NR 2 ENG BEGAN COMPRESSOR STALLING AT APPROXIMATELY 1.94 EPR 20 SECONDS. RETARDED THRUST LEVER, ENGINE CONTINUED TO STALL. SHUTDOWN ENGINE. FOUND 12 AND 13 HPC DISC DAMAGED. REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1999120400733 19991204 00733 NM 1999 12 4 RAAA99B2065 1 19991124 A 3520 4566M37B042NM PBE BOEING 727 72722C 138400F NM CABIN OPEN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 FWD RT CABIN OVERHEAD BIN PBE INDICATOR PROTRUDING. REPLACED PBE DUE POUCH VACUUM LOST. 2 L 7 3 4F A3WE 1999120400734 19991204 00734 NM 1999 12 4 RAAA99B2066 1 19991201 A 3520 4566M37B042NM PBE BOEING 727 72722C 138400F NM ROW 2 OPEN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 ROW 2, PBE INDICATOR PROTRUDING ON SERVICE CHECK. REPLACED PBE. 2 L 7 3 4F A3WE 1999120400735 19991204 00735 SO 1999 12 4 RAAA99E8058 1 19991129 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY AISLE LIGHT AT ROW 11 CDE INOP. REPLACED BATTERY PACK, OPS CHECKED OK. 2 L 7 4 4T 4A22 1999120400736 19991204 00736 WP 1999 12 4 9905019924 1 19991105 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 604 BULGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47473 DURING LINE MAINTENANCE INSPECTION, FOUND BULGE IN LOWER FUSELAGE SKIN ADJACENT TO FS 604 BULKHEAD 'T' CAP. REPAIRED PE R EA 99-153395. 2 L 7 2 4F A6WE 1999120400737 19991204 00737 WP 1999 12 4 9905029140 1 19991114 A 5530 ANGLE DOUG DC9 DC914 3022034 WP VERTICAL STAB PITTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 930RC 45729 DURING M-CHECK, FOUND LEFT LEADING EDGE ATTACH ANGLE FOR LEADING EDGE NR 6321 PITTED. REPAIRED PER EA 91-169335. 2 L 7 2 4F A6WE 1999120400738 19991204 00738 WP 1999 12 4 9905039982 1 19991115 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 982US 45790 DURING LINE CHECK, FOUND FASTENER HOLES OUT OF ROUND AT BEAUTY BAND FORWARD SKIN, 3 FASTENERS BELOW LONGERON 5L, 6 FASTE NERS BETWEEN LONGERON 4L AND 5L, 6 EA AT LONGERON 5L. REPAIRED PER EA 99-169622. 2 L 7 2 4F A6WE 1999120400739 19991204 00739 WP 1999 12 4 9905049760 1 19991115 A 5312 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING M-CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD FORWARD UPPER LEFT CORNER -9 DOUBLER. REPAIRED PER EA 97-171705. 2 L 7 2 4F A6WE 1999120400740 19991204 00740 WP 1999 12 4 9905059982 1 19991110 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 982US 45790 DURING LINE CHECK, FOUND FUSELAGE SKIN FS 996 BETWEEN LONGERONS 7 AND 8, 4 EA FASTENERS, BETWEEN LONGERONS 8 AND 9, 2 EA FASTENER HOLES CRACKED IN ROW NR 1. REPAIRED PER EA 99-169624. 2 L 7 2 4F A6WE 1999120400741 19991204 00741 NM 1999 12 4 9905062287 1 19991016 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 1070 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 287US 21375 DURING H-CHECK, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM FS 1070, LBL 47. REPAIRED PER EA 22-170706. 2 L 7 3 4F A3WE 1999120400742 19991204 00742 NM 1999 12 4 9905072287 1 19991015 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 287US 21375 DURING H-CHECK, FOUND CORROSION ON UPPER FLANGE SURFACE OF THE FLOORBEAM FS 1130, WL 208, LBL 11 - LBL 16. REPAIRED PER EA 22-170714. 2 L 7 3 4F A3WE 1999120400743 19991204 00743 NM 1999 12 4 9905082287 1 19991020 A 5531 SPAR BOEING 727 727251 138408H NM VERTICAL STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 287US 21375 DURING H-CHECK, FOUND CRACKS EMITTING IN LEFT VERTICAL STABILIZER SKIN AT REAR SPAR CHORD. REPAIRED PER EA 22-170717, R EV A. 2 L 7 3 4F A3WE 1999120400744 19991204 00744 SO 1999 12 4 COMA9910178 1 19991113 A 2731 WIRE EMB 120 EMB120RT 3260202 SO ELEVATOR DAMAGED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 269CA 120263 TAKEOFF TRIM AURAL WARNING. REPAIRED DAMAGED WIRE SPLICE AT THE ELEVATOR TRIM PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1999120400745 19991204 00745 EA 1999 12 4 COMA9960732 1 19991201 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 EA RT MLG UPLOCK LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 951CA 7091 RIGHT HAND MLG DID NOT RETRACT. TIGHTENED LOOSE TARGET ON RIGHT HAND MLG UPLOCK. 2 L 7 2 4F RT A21EA 1999120400746 19991204 00746 EA 1999 12 4 COMA9960730 1 19991201 A 2750 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 989CA 7215 FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE RIGHT HAND OUTBOARD FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 1999120400747 19991204 00747 EA 1999 12 4 COMA9960729 1 19991127 A 5320 601R31113 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 295 - 310 MISREPAIRED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 951CA 7091 FLOORBEAM WEB ON I/B RBL 9 FS 295 - FS 310 HAD AN ELONGATED HOLE PREVIOUSLY PLUGGED WITH AN IMPROPER FASTENER. PERFORM ED A MAJOR REPAIR BY REPLACING FLOORBEAM WEB AT RBL9 I/B FS 295 - FS 310 IAW WVAC EO 601R-53-0646. 2 L 7 2 4F RT A21EA 1999120400748 19991204 00748 NM 1999 12 4 QXEA9902444 1 19991125 A 3350 82410191009 SWITCH DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS FAILED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 814PH 43 SEA- EMERGENCY LIGHTS CIRCUIT BREAKER POPS EVEN WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED FLIGHT ATTENDENTS EME RGENCY LIGHTING SWITCH AND EMERGENCY LIGHTING CONTROL BOX, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999120400749 19991204 00749 EU 1999 12 4 QXEA9902447 1 19991129 A 2824 VALVE CELCIUS 3M31 FOKKER F28 F28MK4000 4990810 EU FUEL CROSSFEED FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 497US FTRR336 11167 PDX- DURING FLIGHT, RIGHT HAND FUEL CROSSFEED VALVE WOULD NOT OPEN. REMOVED AND REPLACED CROSSFEED VALVE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999120400750 19991204 00750 NM 1999 12 4 99FDEA00492 1 19991201 A 3260 656021132 ACCESSORY UNIT BOEING 727 727233 138408A NM E/E BAY MALFUNCTIONED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 219FE 21102 WHEN LANDING GEAR EXTENDED, BOTH GROUND AND RED IND LIGHTS WERE PRESENT ON FRONT IND. REMOVED AND REPLACED LANDING GEAR ASSY UNIT AND CLEANED ELECTRICAL CONNECTORS ON THE RACK WITH CONTACT CLEANER MM 32-01-122, TEST OK ON GROUND. 2 L 7 3 4F RT A3WE 1999120400751 19991204 00751 NM 1999 12 4 99FDEA00493 1 19991201 A 3260 656021132 UNIT BOEING 727 727247 138408F NM E/E BAY FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 237FE 21331 RT MLG IND UNSAFE ON EXTENSION. WHILE WORK CKLIST GEAR LATER WENT DOWN AND LOCKED IND FOR NO REASON. *S/D* REPLACED L AND GEAR ASSY BOX PRECAUTIONARY. OPER CK PER ENG AUTH 7-3209-4087-1 REVISION A AND MM 32-09-122-5 STEPS 5A-E. 2 L 7 3 4F A3WE 1999120400752 19991204 00752 WP 1999 12 4 99FDEA00494 1 19991201 A 3010 WARNING LIGHT DOUG DC10 DC1030F 3023504 WP COCKPIT ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 310FE 48299 NR 3 PNEUMATIC FAIL LIGHT ILLUM. COMPLETED RED TABS. 2 L 7 3 4F RT A22WE 1999120400753 19991204 00753 NE 1999 12 4 99UAL900606 2 19991120 A 7200 ENGINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 381UA 24656 AIRCRAFT ABORTED TAKEOFF AT 90 KNOTS WHEN THE NR 2 ENGINE WITH AUTO THROTTLES ON WILL NOT ACCELERATE BEYOND 80.1 PERCENT . 2 L 7 2 4F 4 F RT A16WE E2GL 1999120400754 19991204 00754 NM 1999 12 4 99UAL900607 1 19991121 A 3810 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE POTABLE WATER MALFUNCTIONED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 521UA 24891 DIVERTED TO MCI DUE TO VIBRATION IN AFT GALLEY AREA. *S/D* POTABLE WATER FILL/SHUTOFF VALVE WAS FOUND OPEN, CAUSING PR ESSURE TO VENT AND MAKE WATER LINE VIBRATE. VALVE WAS MOVED TO CLOSED POSITION AND VIBRATION WENT AWAY. 2 L 7 2 4F 4 F RT A2NM E17NE 1999120400755 20001016 00755 NM 2000 10 16 99UAL900608 1 19991120 A 2741 160000 CONTROLLER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE STABILIZER TRIM FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 610UA 11696 21871 ON APPROACH, STAB-TRIM WENT NOSE-UP. CREW SUCCESSFUL IN RESETTING CIRCUIT-BREAKER. EMERGENCY DECLARED. FLIGHT LANDED WITH NO FURTHER INCIDENT. *S/D* AN INTERNAL FAILURE IN THE LEFT STABILIZER TRIM CONTROL MODULE (STCM) INHIBITED MOVEM ENT OF THE HORZ STABILIZER. THE LEFT STCM WAS REPLACED PER 767-222 MM. ALL FINAL OPS CHECKS WERE GOOD. DUE TO THE POS SIBILITY OF A DUAL FAILURE, THE RIGHT STCM WAS REPLACED AND OPS CHECKED PER 767-222 MM AND ALL CHECKED GOOD. ALSO THE STABILIZER TRIM HYDRAULIC SHUTOFF SWITCHES WERE OPERATIONALLY CHECKED AND TESTED PER 767-222 MM AND SWITCHES OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E3NE 1999120400756 19991204 00756 NM 1999 12 4 99UAL900609 1 19991123 A 3030 DEICE SYSTEM BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE PITOT STATIC INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 611UA 21872 F/O PITOT HEAT INOP. CAPTAIN DETERMINED FLIGHT COULD NOT AVOID ICING CONDITIONS. MEL RESTRICTIONS DETERMINED NEED TO RTF. OVERWEIGHT LANDING. 2 L 7 2 4F 4 F RT A1NM E3NE 1999120400757 19991204 00757 WP 1999 12 4 ABXA9900808 1 19991022 A 5320 3914025502N FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND INTERCOSTAL FITTING CRACKED IN UPPER AFT CORNER OF AFT LOWER CARGO DOOR. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999120400758 19991204 00758 WP 1999 12 4 ABXA9900809 1 19991025 A 5311 59203472N FRAME DOUG DOUG DC9 DC932F 3022067 WP BS 579 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND RIGHT SIDEWALL FRAME FOOT CRACKED AT STATION 579 AND LONGERON 18 RIGHT. REPLACED FOOT IAW DC9 SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1999120400759 19991204 00759 WP 1999 12 4 ABXA9900810 1 19991105 A 5321 99578275 FLOOR PANEL DOUG DOUG DC9 DC932F 3022067 WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND COCKPIT FLOOR PANEL CRACKED AT STATION 132 AND RBL 4.0. REPLACED FLOOR PANEL IAW DC9 SRM 53-21-0 AND DACO DWG 9957827. 2 L 7 2 4F A6WE 1999120400760 19991204 00760 WP 1999 12 4 ABXA9900811 1 19991105 A 5320 99220422 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 869 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND RIGHT VERTICAL SUPPORT FITTING CRACKED AT STATION 869. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 5 1-30-5. 2 L 7 2 4F A6WE 1999120400761 19991204 00761 WP 1999 12 4 ABXA9900812 1 19991105 A 5320 99220422 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 813 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND RIGHT VERTICAL SUPPORT FITTING AT STATION 813 CRACKED IN TWO PLACES. REPLACED FITTING AW DC9 SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1999120400762 19991204 00762 WP 1999 12 4 ABXA9900813 1 19991130 A 3310 BA170MODB BALLAST DOUG DC8 DC863 302198A WP COCKPIT FAILED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 813AX 798 46136 COCKPIT INSTRUMENT LIGHTS FAILED AND BURNING ODOR WAS NOTICED. PULLED CIRCUIT BREAKER AND SMELL DISSIPATED. REPLACED LIGHTING BALLAST IAW DC8 MM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999120400763 19991204 00763 WP 1999 12 4 MWEA99853 1 19991122 A 2740 95906 MOTOR DOUG DC9 DC915 3022036 WP STAB TRIM INOPERATIVE A MWEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 300ME 45718 INFLIGHT NR 2 COMM WAS INOP. ALSO, ON APPROACH INTO MKE PRIMARY TRIM WENT INOP. FOUND ANTENNA CONNECTOR LOOSE AT E & E . RECONNECTED THE CONNECTOR AND REMOVED AND REPLACED PRIMARY TRIM MOTOR. 2 L 7 2 4F A6WE 1999120400764 19991204 00764 WP 1999 12 4 MWEA99854 1 19991129 A 5753 99581056 RIB DOUG DC9 DC932 3022066 WP TE FLAP GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 INBOARD RIB/WEB OF LEFT FLAP AT TRAILING EDGE HAD GOUGES. MAINTENANCE FABRICATED AND INSTALLED WEB REPAIR SECTION. 2 L 7 2 4F A6WE 1999120400765 19991204 00765 WP 1999 12 4 MWEA99855 1 19991129 A 5753 99577755 STIFFENER DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND CORROSION ON LEFT FLAP LEADING EDGE STIFFENER/ DOUBLER. MAINTENANCE FITTED AND INSTALLED NEW STIFFENER/DOUBLER. 2 L 7 2 4F A6WE 1999120400766 19991204 00766 WP 1999 12 4 MWEA99856 1 19991129 A 5753 99580035 RIB DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LOWER CHANNEL OF LEFT FLAP RIB LOCATED AT STATION XFLS 127, FORWARD END, WAS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 1999120400767 19991204 00767 WP 1999 12 4 MWEA99857 1 19991201 A 5753 5910134141 SPAR DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT FLAP REAR SPAR WEB AT STATION XFLS 69 TO XFLS 127 WAS CORRODED. MAINTENANCE FITTED AND INSTALLED NEW WEB SECTION. 2 L 7 2 4F A6WE 1999120400768 19991204 00768 WP 1999 12 4 MWEA99858 1 19991201 A 5753 99577737 DOUBLER DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT FLAP LOWER FORWARD SKIN DOUBLER WAS CORRODED. MAINTENANCE FITTED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 1999120400769 19991204 00769 WP 1999 12 4 MWEA99859 1 19991201 A 5753 5913560501 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND CRACK ON LEFT FLAP LEADING EDGE AT STATION XRS 270. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999120400770 19991204 00770 WP 1999 12 4 MWEA99860 1 19991202 A 5711 59305035 SPAR DOUG DC9 DC981 3022081 WP WS 111.5 MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 SEVERAL PREVIOUS BLEND OUTS ON BOTTOM OF LEFT WING, BOTTOM OF AFT SPAR FROM STATION XRS 111.5 AND XRS 120 ARE NOT ACCEPT ABLE. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999120400771 19991204 00771 1999 12 4 MWEA99861 4 19991202 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP SERVICE DOOR LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 GALLEY SERVICE DOOR EMERGENCY ESCAPE SLIDE COVER WAS LOOSE AND DETACHED FROM BOTTOM OF DOOR. MAINTENANCE RE-ATTACHED SL IDE TO COVER. 2 L 7 2 4F A6WE 1999120400772 19991204 00772 WP 1999 12 4 MWEA99862 1 19991202 A 5753 99577752 RIB DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT FLAP, LEADING EDGE SECTION NUMBER 5 RIB WAS CRACKED. MAINTENANCE FABRICATED AND INSTALLED RIB REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999120400773 19991204 00773 WP 1999 12 4 MWEA99863 1 19991202 A 5720 9913440511 ANGLE DOUG DC9 DC932 3022066 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT WING TRAPAZOIDAL PANEL ANGLE BRACKET AT FORWARD BOTTOM CORNER WAS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW AN GLE. 2 L 7 2 4F A6WE 1999120400774 19991204 00774 1999 12 4 MWEA99864 2 19991202 A 7230 5910297501 SPINNER DOUG DC9 DC932 3022066 WP RT ENGINE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT ENGINE INLET NOSE BULLET HAD AREA OF NICKS AND TWO DEEP SCRATCHES. MAINTENANCE REPLACED NOSE BULLET WITH SERVICEA BLE UNIT. 2 L 7 2 4F A6WE 1999120400775 19991204 00775 WP 1999 12 4 MWEA99865 1 19991202 A 5753 99580614 RIB DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT FLAP, TRAILING EDGE PANEL NUMBER ONE, THE FIFTH RIB FROM OUTBOARD END WAS CRACKED. MAINTENANCE FITTED AND INSTALL ED NEW RIB. 2 L 7 2 4F A6WE 1999120400776 19991204 00776 WP 1999 12 4 DHL99801003 1 19991201 A 2910 2400000000405334 LINE DOUG DC8 DC873F 302199F WP HYD SYSTEM LEAKING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 EXPERIENCED HYDRAULIC QUANTITY LOSS. FOUND PRESSURE LEAKING AT STBY HYDRAULIC PUMP. REMOVED AND REPLACED FLEX PRESSURE LINE, OPS AND LEAK CHECK GOOD. 2 L 7 4 4F RT 4A25 1999120400777 19991204 00777 EU 1999 12 4 RAIA9910052 1 19991014 A 3320 13181A SOCKET BAG JETSTM JETSTM3201 1500217 EU SEAT 3 A FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 343TE 955 STL- SMOKE SMELL IN COCKPIT IN FLIGHT. MAINTENANCE REPLACED LIGHT SOCKET ASSY AT SEAT 3A FOR THE OVERHEAD LIGHT. 2 L 7 2 4T RT A56EU 1999120400778 19991204 00778 NE 1999 12 4 RAIA9911028 2 19991130 A 7210 310430211 DIAPHRAM JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT ENGINE G/B FAILED A RAIA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 572HK 41091 75109 JFK- SET POWER LEVERS TO FLIGHT, LEFT TORQUE FLUCTUATING. MAINTENANCE REPLACED INTERMEDIATE GEARBOX DIAPHRAM. 2 L 7 2 4T 4 T RT A41NM E18NE 1999121000002 19991210 00002 EA 1999 12 10 JBXA9900109 1 19991027 A 5240 MECHANISM CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE SERVICE DOOR NOT LATCHED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 583ML 7327 ON CLIMBOUT OF RDU ON FLIGHT NR 222 TO MEM, CREW RECEIVED A SERVICE DOOR AMBER FAULT. FLIGHT ATTENDANT (AFTER A/C HAD P ULLED OFF RUNWAY) RESET SERVICE DOOR HANDLE AND FAULT CLEARED. CREW TURNED BACK ONTO RUNWAY AND TOOK OFF WITH NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121000003 19991210 00003 NM 1999 12 10 99UAL900560 1 19991029 A 2150 8102093 ACM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT PACK FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 767UA 26918 CREW REPORTED SMOKE IN COCKPIT AND AFT CABIN AREAS DURING FLIGHT. *S/D* LEFT HAND AIR CYCLE MACHINE (ACM PN:810209-3) WAS REPLACED PRECAUTIONARY. AIRCRAFT WENT BACK TO REVENUE SERVICE WITHOUT FURTHER SMOKE INCIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999121000004 19991210 00004 NE 1999 12 10 CALA9901453 2 19991031 A 7200 COMPRESSOR BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE LEAKING A CALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 09 12114 27556 31319 SEVERAL EICAS MESSAGES AND TAT PROBE CAME ON DURING TAKEOFF ROLL. A STRONG SMELL ENTERED THE CABIN AND THE PACKS OVERHE ATED AFTER LIFT OFF. ALSO, A RUMBLING NOISE WAS HEARD. THE SMELL IN CABIN KEPT GETTING STRONGER AND AT 11,000 FEET THE CAPTAIN DECIDED TO RETURN TO EWR. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE NR 1 ENGINE LEAKING OIL AT COMPRESSOR. THE NR 1 ENGINE WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999121000006 19991210 00006 1999 12 10 VNAA9911004 4 19991102 A 3160 7015327901 FLIGHT DIRECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 431JS 7352 3028 DURING CRUISE, THE TOUCH CONTROL SWITCH ON PRIMARY FLIGHT DISPLAY CAME ON BY ITSELF. THE AUTO PILOT DID NOT DISCONNECT BUT WAS OFF LINE. THE AIRCRAFT DID NOT FOLLOW THE FLIGHT DIRECTOR. MAINTENANCE INSPECTED AND REPLACED THE FLIGHT DIREC TOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 22-11-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELE ASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121000007 19991210 00007 NM 1999 12 10 TWAA9915101 1 19991108 A 3350 20131A BATTERY BOEING 767 7673Q8 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 636TW 30301 THE EMERGENCY EGRESS LIGHTS ON THE RIGHT SIDE OF THE CABIN, ROW 25 GOING AFT, WAS INOPERATIVE. REPLACED THE BATTERY CHA RGER, MFG 2012-1, AND THE BATTERY PACK. 2 L 7 2 4F RT A1NM 1999121000011 19991210 00011 NE 1999 12 10 DLL19992439 2 19991104 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 3 FAILED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 754DL 69770 193Y1181 014756 NR 3 MOTOR SUFFERED CONTINOUS INFLIGHT STALLS JUST AFTER LIFTOFF. REPORTED AGL WAS APPROX 400 FT. ENG PARAMETERS WAS F LUCUATING WITH STALLS. STALLS WERE VERY LOUD AND NOTICABLE IN AIRCRAFT STRUCTURE. UPON INSPECTION OF ENG INLET AND EXH AUST, METAL SHAVINGS WERE FOUND IN TAIL PIPE AND RT CORE COWL. BLOWOUT PANEL WAS FOUND IN THE OPEN POSITION. INFLIGHT SHUT DOWN REPORT WAS FILLED OUT AND FORWARDED. REPLACED NR 3 ENG. 2 L 7 3 4F 4 F A23WE E12EU 1999121000012 19991210 00012 NM 1999 12 10 DL72S992451 1 19991107 A 3244 TIRE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 4 MAIN GEAR FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 527DA 70708 21587 687423 NR 4 MAIN TIRE RECAP CAME APART. DAMAGED RT OUTBOARD GEAR DOOR FLAP ASSY AND FOD NR 3 ENG. REPLACED NR 3 ENGINE. REPL ACED FLAP ASSY. REPLACED NR 4 WHEEL. 2 L 7 3 4F 4 F A3WE E2EA 1999121000013 19991210 00013 NM 1999 12 10 DL72E992459 1 19991108 A 5330 SKIN BOEING 727 727247 138408F NM BS 1030-1050 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 A CRACK WAS FOUND IN THE STRINGER 4L LAP JOINT BETWEEN FS 1030 AND 1050 DURING INSPECTIONS PER AD 99-04-22. ERA 333766- 14 REPAIRED THE DAMAGE AT HMV. 2 L 7 3 4F A3WE 1999121000014 19991210 00014 NM 1999 12 10 DL72E992460 1 19991103 A 5312 6516350 BLKHD STIFFENER BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 THE LBL 36.83 VERTICAL STIFFENER OF THE 1183 BULKHEAD WAS FOUND CRACKED AT HMV. ERA 333764-14 REPAIRED THIS CONDITION. 2 L 7 3 4F A3WE 1999121000015 19991210 00015 NM 1999 12 10 DL72E992461 1 19991108 A 5330 SKIN BOEING 727 727247 138408F NM BS 620-640 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 THE FUSELAGE SKIN WAS FOUND CRACKED AT THE STRINGER 4R LAP JOINT BETWEEN FS 620 AND 640. THE DISCREPANCY WAS REPAIRED B Y ER/A 333765-14 AT HMV. 2 L 7 3 4F A3WE 1999121000016 19991210 00016 NM 1999 12 10 DL72E992465 1 19991108 A 5712 65162222 RIB BOEING 727 727247 138408F NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 ACTUATOR RIB CRACKED. REPAIRED RIB PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999121000017 19991210 00017 NM 1999 12 10 DLM90992474 1 19991109 A 3350 8039251 POWER SUPPLY DOUG MD90 MD9030 3023690 NM R1 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DA 53389 R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 1999121000018 19991210 00018 NM 1999 12 10 DL72L992475 1 19991110 A 3350 LIGHT 0201984006 BOEING 727 727232 1384082 NM R1 DOOR BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 21306 EXIT LIGHT FORWARD OF R-1 DOOR IS UNSECURED/LOOSE. REPLACED SAME. 2 L 7 3 4F A3WE 1999121000019 19991210 00019 NM 1999 12 10 DL72E992478 1 19991110 A 5330 SKIN BOEING 727 727247 138408F NM BS 540-560 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 THE FUSELAGE SKIN LAP WAS FOUND CRACKED AT STRINGER 4R BETWEEN FS 540 AND FS 560. THE DAMAGE WAS REPIARED PER ERA 33376 3-14 DURING HMV. 2 L 7 3 4F A3WE 1999121000020 19991210 00020 NM 1999 12 10 DL72L992479 1 19991110 A 5312 6516350339 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 THE VERTICAL STIFFENERS AT LBL AND RBL 36.83 ON THE FORWARD SIDE OF THE FS 1183 BULKHEAD WERE FOUND CRACKED BETWEEN WL 2 30 AND WL 270. THE DAMAGE WAS REPIARED PER ERA 333759-14 AT MV. 2 L 7 3 4F A3WE 1999121000021 19991210 00021 NM 1999 12 10 DL72L992480 1 19991104 A 5330 6518219 SKIN BOEING 727 727232 1384082 NM BS 380 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 SKIN DENTED AT STA 380 AND STR 17L AND STA 387 BETWEEN S 17L AND 18L. DAMAGE TRIMMED OUT AND REPAIRED WITH AN EXTERNAL DOUBLER. ERA 333767-14 REV B. 2 L 7 3 4F A3WE 1999121000022 19991210 00022 NM 1999 12 10 DL72E992481 1 19991102 A 5754 RIB BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 AT HMV2, FOUND NR 2 L/E SLAT, RIB CRACKED I/B SIDE OF ACT FITTING. STOPPED DRILLED CRACK PER MM 57-54-0 FIG 804. FAB'D DOUBLER PER SAME, AND INSTALLED. 2 L 7 3 4F A3WE 1999121000023 19991210 00023 NM 1999 12 10 DL72E992482 1 19991102 A 5754 RIB BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 AT HMV2, FOUND NR 2 L/E SLAT, RIB TEMP REPAIR STOP DRILLED CRACK, I/B SIDE OF ACT FITTING. STOP DRILLED CRACK PER MM 57 -54-0 FIG 804, FAB'D DOUBLER PER SAME, INSTALLED. 2 L 7 3 4F A3WE 1999121000024 19991210 00024 NM 1999 12 10 DL72E992483 1 19991102 A 5754 RIB BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 AT HMV2, FOUND RIB CRACKED ON O/B SIDE OF ACT FITTING ON NR 2 L/E SLAT. STOP DRILLED CRACK PER MM 57-54-0 FIG 804. FAB RICATED DOUBLER PER SAME, INSTALLED. 2 L 7 3 4F A3WE 1999121000025 19991210 00025 NM 1999 12 10 DL72E992484 1 19991102 A 5754 RIB BOEING 727 727247 138408F NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 AT HMV2, FOUND RIB CRACKED INSIDE NR 3 L/E SLAT ON O/B SIDE OF I/B TRACK. TRIMMED OUT DAMAGE, AND REPAIR ANGLE PER MM 5 7-54-0 FIG 811. INSTALLED DOUBLER PER SAME. 2 L 7 3 4F A3WE 1999121000026 19991210 00026 NM 1999 12 10 DL72E992485 1 19991102 A 5754 RIB BOEING 727 727247 138408F NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 AT HMV2 FOUND NR 3 L/E SLAT, RIB CRACKED I/B SIDE OF I/B TRACK. REMOVED FASTENERS, STOPPED DRILLED CRACK. FABRICATED D OUBLER PER MM 54-57-0 FIG 811. INSTALLED DOUBLER PER SAME. 2 L 7 3 4F A3WE 1999121000027 19991210 00027 NM 1999 12 10 DL72E992493 1 19991026 A 5753 SKIN BOEING 727 727247 138408F NM RT TE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 COVE SKIN WORN 34 FROM INBD END, REPAIRED PER MM 57-52-0 FIG 809, ON SHOP ORDER 877885. 2 L 7 3 4F A3WE 1999121000030 19991210 00030 NM 1999 12 10 QXEA9902267 1 19991027 A 5347 SEAT RACK DHAV DHC8 DHC8102 2809003 NM CABIN CORODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - NUMEROUS CORROSION DISCREPANCIES ON LEFT INBOARD FORWARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999121000031 19991210 00031 NM 1999 12 10 QXEA9902296 1 19991029 A 5320 CHANNEL DHAV DHC8 DHC8102 2809003 NM BS 182 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - RIGHT FORWARD DRAIN CHANNEL ATTACHED TO RIGHT INBOARD CABIN SEAT TRACK HAS FRETTING CORROSION AND IS CRACKED AROUN D FORWARD ATTACH RIVET HOLES AT STATION 182.000. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999121000032 19991210 00032 NM 1999 12 10 QXEA9902297 1 19991022 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 291.4-366 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT OUTBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 291.400 AND 366.000 HAS CORROSION ON TOP SURFACE AND INSID E CHANNEL. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999121000033 19991210 00033 NM 1999 12 10 QXEA9902298 1 19991022 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 436.5-456.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT OUTBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 436.500 AND 456.500 HAS CORROSION ON TOP SURFACE AND INSID E CHANNEL. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999121000034 19991210 00034 NM 1999 12 10 QXEA9902299 1 19991019 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 467-513.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 275 PDX - LEFT OUTBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 467.000 AND 513.500 HAS CORROSION ON TOP SURFACE AND INSID E CHANNEL. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1999121000035 19991210 00035 NM 1999 12 10 99UAL900574 1 19991104 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOP A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 161UA 21352 EEL STRIP AT BOTTOM OF CIRCULAR STAIR IS INTERMITTENT ON AND OFF NEAR 1ST CLASS GALLEY. *S/D* CYCLED EMERGENCY LIGHT S WITCH AND CHECKED LIGHT OPERATION. LIGHTS CHECKED OK. SYSTEM HAS BEEN FUNCTIONING NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1999121000036 19991210 00036 NE 1999 12 10 UIEA9975 2 19990916 A 7421 CH31785 IGNITOR BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE ERODED A UIEA K NONE X ENGINE FLAMEOUT DE DESCENT 1 EA 15 523MC 21782 FLT 2087 - ANC-KIX - DURING DESCENT THROUGH 4000 FT, NR 1 ENGINE FLAMED OUT. FLIGHT CRWE DID NOT ATTEMPT TO RE-START EN GINE. AIRCRAFT LANDING AT KIX UNEVENTFUL. MAINTENANCE PERFORMED TROUBLESHOOTING AS PER MM 71-00-42. NO FAULTS FOUND. BOTH IGNITERS WERE REPLACED. REMOVED IGNITERS SHOWED SIGNS OF HEAVY EROSION. MPA PERFORMED ON NR 1 AND NR 4 ENGINES. ACCELERATION/DECELERATION NORMAL. (M) 2 L 7 4 4F 4 F RT A20WE E23EA 1999121000037 19991210 00037 NM 1999 12 10 MZZA99148 1 19990930 A 5754 65162252 FITTING BOEING 727 727227 1384078 NM NR 4 LE FLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURNG S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON NR 4 L/E FLAP CENTER HINGE MOUNT FITTING OUTB OARD LUG. THE DAMAGED FLAP WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM CHAPTER 27-81-0 AND OPERATIONAL CHECK FO UND TO BE SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999121000038 19991210 00038 WP 1999 12 10 MWEA99821 1 19991116 A 5753 5919218504 FITTINGS DOUG DC9 DC932 3022066 WP RT TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT WING, I/B AND MIDDLE FLAP HINGE FITTING NEEDS TO HAVE BEARINGS REPLACED (LOWER PIVOT POINTS). FOUND CORROSION OUT OF LIMITS ON BOTH INBOARD AND MIDDLE ATTACH HOLES. MTC REMOVED AND REPLACED NEW I/B AND MIDDLE ATTACH FITTINGS. 2 L 7 2 4F A6WE 1999121000040 19991210 00040 NM 1999 12 10 CA991027007 1 19991018 A 5210 SENSOR BOEING 737 7372T2 1384491 NM PWA JT8 JT8D17 52049 NE PASSENGER DOOR OUT OF ADJUST W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA 708801 (CAN) FORWARD ENTRY DOOR WARNING LIGHT CAME ON PRIOR TO 80 KNOTS ON TAKEOFF ROLL, AIRCRAFT RETURNED TO BLOCKS. DOOR OP ERATION AND RIGGING CHECKED OK. DOOR WARNING PROXIMITY SENSOR ADJUSTED PER MM 52-71-0. 2 L 7 2 4F 4 F RT A16WE E2EA 1999121000041 19991210 00041 EA 1999 12 10 CA991028035 2 19991006 A 8550 CH48110 FILTER O360A1H6 PIPER PA44 PA44180 7104402 SO LYC O360 O360A1H 41514 EA OIL SYSTEM MISMANUFACTURED W K NONE O OTHER IN INSP/MAINT 1 CA 20 L58371A L58371A (CAN) QUALITY CONTROL PROBLEM OF ONE FILTER IN STOCK BATCH. 1 L 7 2 3O 3 O A19S0 E286 1999121000043 19991210 00043 WP 1999 12 10 MWEA99836 1 19991123 A 3350 60080451 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 80ME 45795 LEFT OVERWING EMERGENCY EXIT IDENTIFIER SIGN BATTERY PACK IS DISCHARGED. MAINTENANCE REPLACED BATTERY PACK 2 L 7 2 4F A6WE 1999121000044 19991210 00044 NM 1999 12 10 UPS99230998 1 19991027 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM GALLEY DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 EMERGENCY LIGHT AT GALLEY SERVICE DOOR INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999121100001 19991211 00001 EU 1999 12 11 AALA991507 1 19991001 A 5320 CPN405663 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAMES 29-33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100002 19991211 00002 EU 1999 12 11 AALA991518 1 19991005 A 5320 4086773 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAMES 77-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. STRAP REPAIR PER AARD 53-20-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100003 19991211 00003 EU 1999 12 11 AALA991517 1 19991005 A 5320 4043373 BEAM AIRBUS 300 A300B4605R 3930308 EU GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100004 19991211 00004 EU 1999 12 11 AALA991516 1 19991005 A 5320 A5327920620800 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAMES 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100005 19991211 00005 EU 1999 12 11 AALA991515 1 19991005 A 5320 A5327920720451 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAMES 79-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100006 19991211 00006 EU 1999 12 11 AALA991514 1 19991005 A 5320 CPN4060652 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-74-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100007 19991211 00007 EU 1999 12 11 AALA991513 1 19991005 A 5320 4086773 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAMES 77-79 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. STRAP REPAIRED PER AARD 53-29-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100008 19991211 00008 EU 1999 12 11 AALA991512 1 19991006 A 5320 A53278466200 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAMES 75-76 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. STRAP REPAIRED PER AARD 53-20-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100009 19991211 00009 EU 1999 12 11 AALA991511 1 19991005 A 5347 A53779862701 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAMES 28-31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. SECTION SPLICE PER SRM 53-10-16. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100010 19991211 00010 EU 1999 12 11 AALA991532 1 19991007 A 5320 A53274618200 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100011 19991211 00011 EU 1999 12 11 AALA991531 1 19991007 A 5320 A53274262202 BEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100012 19991211 00012 EU 1999 12 11 AALA991534 1 19991009 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU BS 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION ON STRINGER SPLICE AT STR 57 AND AFT SIDE OF FRAME 65. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53- 10-14. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100013 19991211 00013 EU 1999 12 11 AALA991533 1 19991007 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION ON FRAME BETWEEN STR 49L TO STR 49R. INSTALLED DOUBLER REPAIR PER SRM 53-10-13. TST: 31,677 HOURS. C YCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100014 19991211 00014 EU 1999 12 11 AALA991563 1 19991016 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 54.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION ON STR 55R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100015 19991211 00015 EU 1999 12 11 AALA991566 1 19991018 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - FLOOR SUPPORT AT FRAME 56 HAS CORROSION ON TOP SIDE. INSTALLED FLOOR SUPPORT SECTION PER SRM 53-10-15. TST: 31, 677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100016 19991211 00016 EU 1999 12 11 AALA991565 1 19991016 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 54.1 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION ON STR 53R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100017 19991211 00017 EU 1999 12 11 AALA991564 1 19991016 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 54.1 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION ON STR 55R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100018 19991211 00018 EU 1999 12 11 AALA991569 1 19991013 A 5313 A5391308020490 STRINGER AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL- STR 45R CORRODED - FRAME FITTING. REPLACED STRINGER AND FRAME FITTING PER SRM 53-17-18. TST: 31,677 HOURS. CYCL ES: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100019 19991211 00019 WP 1999 12 11 AALA991628 1 19991028 A 5230 30602283 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 466AA 49596 TUL - CARGO DOOR PAN CORRODED FORWARD CARGO. REMOVED AND REPLACED SECTION OF DOOR PAN PER SRM 53-05. TST: 33,663 HOURS . CYCLES: 18,069. (X) 2 L 7 2 4F A6WE 1999121100020 19991211 00020 EU 1999 12 11 AALA991590 1 19991012 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - CORROSION ON FRAME 58 BETWEEN STR 55L AND STR 55R. INSTALLED DOUBLER PER SRM 51-10-13. TST: 31,677 HOURS. CYCLE S: 12,770. (X) 2 L 7 2 4F RT A35EU 1999121100021 19991211 00021 NM 1999 12 11 AALA994172 1 19990930 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 286 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - FLOORBEAM AT STA 286 RBL 49 HAD CORROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. REPAIRED PER MRB 767-1959. F ABRICATED STRAP OUT OF 301 1/2H 55 .050 INCH THICK. ALODINED ALL BARE ALUMINUM PRIME PARTS WITH 2 COATS BMS 10-11 PRIME R FILLED BLENDS WITH BMS 5-92. INSTALLED STRAP BELT WITH BMS 5-92 SEALANT. TST: 56,505 HOURS. CYCLES: 16,666. (X) 2 L 7 2 4F RT A1NM 1999121100022 19991211 00022 NM 1999 12 11 AALA994169 1 19991006 A 5730 SKIN BOEING 767 767223 1385123 NM WS 798.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - RIGHT WING UPPER SURFACE SKIN HAS CORROSION AND INTERGRANULAR CORROSION AT FASTENER LOCATION. REPAIRED PER MRB 76 7-1960. DRILLED OUT THE CORRODED FASTENERS AND BLENDED OUT CORROSION ON WING SKIN SURFACE. ALODINED ALL BARE ALUMINUM. INSTALLED FREEZE PLUG WET WITH BMS 5-95. INSTALLED STRAP/WASHER 7075T-56 MINIMUM OVERLAP OF .125 INCH PAST THE FREEZE PLUG. 2 L 7 2 4F RT A1NM 1999121100023 19991211 00023 NM 1999 12 11 AALA994170 1 19991001 A 5330 SKIN BOEING 767 767223 1385123 NM BS 718-712 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - FUSELAGE SKIN AT S2R STA 718 HAD CORROSION BLENDED BEYOND LIMITS. REPAIRED PER MRB 767-1962. REMOVED CORROSION P ER 767-200 SRM 53 FIG 101. REPLACED FASTENERS IN BLENDED AREA WITH BACR15FV6KE RIVETS. APPLIED ALODINED 1000 TO BLENDE D AREA. TST: 56,505 HOURS. CYCLES: 16,666. (X) 2 L 7 2 4F RT A1NM 1999121100024 19991211 00024 NM 1999 12 11 AALA994182 1 19991015 A 5312 BULKHEAD STRAP BOEING 767 767223 1385123 NM BS 955 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - FAIL SAFE STRAP ON LEFT WHEELWELL REAR SPAR BULKHEAD IS CRACKED. SHORED AN BRACED AIRCRAFT. DISASSEMBLED REAR SP AR AND INSTALLED NEW FAIL SAFE STRAP. RE-ASSEMBLED PER BOEING SRM. PERMANENT REPAIRS COMPLETED. TST: 55,772 HOURS. CYCLES: 16,441. (X) 2 L 7 2 4F RT A1NM 1999121100025 19991211 00025 NM 1999 12 11 AALA994181 1 19991029 A 5730 SKIN BOEING 767 767223 1385123 NM LT/RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - LEFT/RIGHT WINGS UPPER SKIN HAS CORROSION BLENDOUTS. CORROSION BLENDED, FASTENERS REPLACED, AREA CHECKED FOR CRAC KS. RE-FINISHED PER MB 767-196. TST: 55,772 HOURS. CYCLES: 16,441. (X) 2 L 7 2 4F RT A1NM 1999121100026 19991211 00026 NM 1999 12 11 AALA991622 1 19991028 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 21 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 381AN 25450 DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT SEAT LIGHTS AT SEAT 21 AB INOPERATIVE. REPAIRED WIRE TO EMERGENCY E XIT SEAT LIGHTS AT 21 AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999121100027 19991211 00027 NM 1999 12 11 AALA991621 1 19991024 A 3350 CONNECTOR BOEING 767 767223 1385123 NM ROWS 9-19 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 302AA 22308 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS FROM 9H TO 19H ON RIGHT SIDE OF AIRCRAFT INOPERATIVE. SE CURED POWER SUPPLY CONNECTOR TO EMERGENCY EXIT SEAT LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999121100028 19991211 00028 NM 1999 12 11 AALA991625 1 19991029 A 3350 417T50961D LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379AA 25448 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY, EXIT LIGHT ASSEMBLY BY FS3 LAVATORY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BY FS3 LAVATORY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999121100029 19991211 00029 NM 1999 12 11 AALA991614 1 19991027 A 3350 CONNECTOR BOEING 757 757223 1384957 NM ROW 29DEF LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 631AA 24589 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SIDE OF SEAT 29DEF WOULD NOT TEST. RECONNECTED SEAT TO WALL CONNECTOR FOR SEAT 29DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999121100030 19991211 00030 NM 1999 12 11 AALA991617 1 19991027 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN OPEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645AA 24603 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED WIRE ON EMERG ENCY EXIT FLOOR PATH LGIHTS IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999121100031 19991211 00031 NM 1999 12 11 AALA991650 1 19991102 A 3350 LIGHT BOEING 767 767223 1385123 NM L2 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 322AA 22323 SFO - DURING OVERNIGHT MAINTENANCE, L2 LOWER EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED 1.2 LOWER EMERGENCY EXIT S IGN LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999121100032 19991211 00032 NM 1999 12 11 AALA991651 1 19991103 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 28H BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352AA 24033 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 28H INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT SEAT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999121100033 19991211 00033 NM 1999 12 11 AALA001652 1 19991103 A 3350 LIGHT BOEING 757 757223 1384957 NM ROWS 9-17 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 663AM 25297 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 9-17 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP BETWEEN ROWS 9-17. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999121100034 19991211 00034 NM 1999 12 11 AALA991644 1 19991030 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 612AA 24488 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED FORWARD EMERGENCY EX IT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999121100035 19991211 00035 NM 1999 12 11 AALA991645 1 19991030 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 612AA 24488 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT HAND OVER WING LOWER EXIT SIGN INOPERATIVE. REPAIRED RIGHT HAND OVER WING LOW ER EXIT SIGN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999121100036 19991211 00036 NM 1999 12 11 AALA991627 1 19991020 A 5511 SPAR CHORD BOEING 727 727227 1384078 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - SKIN BULGED AT AFT SPAR RT HORIZONTAL STABILIZER UPPER SURFACE JUST FORWARD OF ACTUATOR ACCESS PANEL. FABRICATED AND INSTALLED DOUBLER PER ESO 11697 DATED 10-19-99. TST: 74,272, HOURS. CYCLES: 49,986. (X) 2 L 7 3 4F A3WE 1999121100037 19991211 00037 NM 1999 12 11 AALA991643 1 19991030 A 3260 LIGHT BOEING 767 767223 1385123 NM RT MLG DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 330AA 22330 ORD - FLT 0067 - ON APPROACH, RIGHT MAIN GEAR GREEN GEAR DOWN LIGHT DID NOT ILLUMINATE. CYCLED GEAR THREE TIMES, RECEIV ED NORMAL GEAR DOWN INDICATION. LANDED ORD WITHOUT INCIDENT. REPLACED DOWNLOCK LIGHT CAPSULE ASSY. SYSTEM GROUND CHEC KED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1999121100038 19991211 00038 NE 1999 12 11 AALA991626 2 19991028 A 7510 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE BLOWN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 410AA 49321 BOS - FLT 2039 - DURING CLIMB-OUT, EN ROUTE BOS/ORD, RIGHT ENGINE FIRE LOOP B ILLUMINATED IMMEDIATELY FOLLOWED BY LOOP-A AND ENGINE FIRE WARNING. ACCOMPLISHED ENGINE FIRE CHECK LIST. RETURNED AND LANDED BOS WITHOUT INCIDENT. INSPECTED EN GINE WITH NO FIRE NOTED. REPLACED BLOWN ANTI-ICE TUBE DUCT ASSEMBLY AT 12 O'CLOCK POSITION. INSPECTED ASSOCIATED WIRIN G AND DUCTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X0 2 L 7 2 4F 4 F A6WE E9NE 1999121100039 19991211 00039 NM 1999 12 11 AALA991618 1 19991027 A 3350 LIGHT DOUG MD11 MD11 3023602 NM ROW 15 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT 15D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100040 19991211 00040 WP 1999 12 11 AALA991639 1 19991030 A 3222 59104475071 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 7532A 49924 DFW - FLT 1869 - NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED AND LANDED DFW WITHOUT INCIDENT. RE-PACKED NOSE L ANDING GEAR STRUT PER MM. AIRCRAFT FLEW FUNCTIONAL CHECK FLIGHT AND NOSE LANDING GEAR OPERATED NORMAL. SYSTEM GROUND C HECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999121100041 19991211 00041 EU 1999 12 11 AALA991666 1 19991107 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU ROWS 29-37 SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14056 463 SJU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE FROM ROWS 29 TO 37. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROWS 29 TO 37. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999121100042 19991211 00042 NM 1999 12 11 AALA991659 1 19991102 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE ON RIGHT HAND SIDE OF FIRST CLASS CABIN . REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP ON RIGHT HAND SIDE OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMA L OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100043 19991211 00043 NM 1999 12 11 AALA991245 1 19990822 A 3397 WIRE DOUG MD11 MD11 3023602 NM ROWS 21-38 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM SEATS 21G TO 38G INOPERATIVE. REPAIRED BROK EN WIRE SPLICE TO EMERGENCY EXIT FLOOR PATH LIGHTING AT SEATS 21G TO 38G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100044 19991211 00044 NM 1999 12 11 AALA991424 1 19990920 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FRONT OF LAVATORY DD INOPERATIVE. REPLACED EM ERGENCY EXIT FLOOR PATH LIGHTING STRIP IN FRONT OF LAVATORY DD. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100045 19991211 00045 NM 1999 12 11 AALA991405 1 19990917 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM ROW 34G BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1764B 48554 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FLICKERS WHEN STEPPED ON AFT OF 34G. REPLACED FL AT CONNECTOR AT 34G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100046 19991211 00046 NM 1999 12 11 AALA991288 1 19990826 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM ROW 38G DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1765B 48596 DFW - DURING OVERNIGHT MAINTENANCE, FOUND ONE BULB ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 38G INOPERATIVE. RE PLACED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 38G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100047 19991211 00047 NM 1999 12 11 AALA991199 1 19990816 A 3350 LIGHT DOUG MD11 MD11 3023602 NM ROW 35C DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1764B 48554 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 35C INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT STRIP AT SEAT 35C. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100048 19991211 00048 NM 1999 12 11 AALA991198 1 19990816 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM ROWS 26-28 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1764B 48554 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 26C AND 28C INOPERATIVE. REPLACED CO NNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 26C AND 28C. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100049 19991211 00049 NM 1999 12 11 AALA991173 1 19990814 A 3350 LIGHT DOUG MD11 MD11 3023602 NM ROWS 8-13 DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN SEATS 8D AND 13D INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHTING STRIP BETWEEN SEATS 8D AND 13D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100050 19991211 00050 NM 1999 12 11 AALA990975 1 19990629 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM ROW 4AB LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BETWEEN SEAT ROWS 23C THROUGH 34C. RE-SEATED CON NECTOR AT SEAT 34C. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100051 19991211 00051 NM 1999 12 11 AALA991042 1 19990714 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST CR CRUISE 1 SW 07 1763 48553 DFW - FLT 158 - EN ROUTE KIX/DFW - EMERGENCY EXIT LIGHTS RIGHT AISLE OF COACH ILLUMINATED FOR 20 MINUTES, THEN EXTINGUIS HED. LANDED DFW WITHOUT INCIDENT. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED, NORMAL O PERATION. (X) 2 L 7 3 4F RT A22WE 1999121100052 19991211 00052 NM 1999 12 11 AALA991302 1 19990901 A 2120 AIR DISTRIBUTION DOUG MD11 MD11 3023602 NM CABIN ODOR A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1764B 48554 LHR - FLT 0056 - EN ROUTE MIA/LHR, SLIGHT ELECTRICAL SMELL NOTED IN AFT GALLEY. GALLEY EQUIPMENT AND RE-CIRCULATING FA NS TURNED OFF AND SMELL MOVED TO MID-BUSINESS CLASS AREA AND DISSIPATED AFTER APPROXIMATELY ONE MINUTE. AIRCRAFT CONTIN UED TO LHR AND LANDED WITHOUT INCIDENT. EXAMINED AND TESTED AIR CONDITIONING PACKS. RE-CIRCULATION FANS, GALLEY EQUIPM ENT, AND VIDEO UNITS. NO FAULTS NOTED. NO SMELL OR SMOKE DETECTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1999121100053 19991211 00053 WP 1999 12 11 AALA991656 1 19991101 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 20 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90511 49805 YYC - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 20 INOPERATIVE. RE-CONNECTED EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 20. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999121100054 19991211 00054 WP 1999 12 11 AALA991658 1 19991102 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 473AA 49648 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 11 INOPERATIVE. REPLACED EMERGENCY EXIT FLO OR PATH LIGHTS STRIP AT ROW 11. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999121100055 19991211 00055 WP 1999 12 11 AALA991642 1 19991029 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP TAIL COMPT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 290AA 49302 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD TAIL COMPARTMENT EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED OVERHEAD TAIL COMPARTMENT EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999121100056 19991211 00056 WP 1999 12 11 AALA991641 1 19991029 A 3397 WIRE DOUG DC9 DC983 3022083 WP TAIL CONE BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 598AA 53288 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOD LIGHTS IN TAIL CONE INOPERATIVE. REPAIRED HOT WIRE TO EMERGENC Y EXIT FLOOD LIGHT SYSTEM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1999121100057 19991211 00057 WP 1999 12 11 AALA991653 1 19991103 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP AFT STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 443AA 49469 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT L IGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999121100058 19991211 00058 WP 1999 12 11 AALA991649 1 19991101 A 3350 P2010031303 LIGHT DOUG DC9 DC982 3022082 WP ROW 33D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 479AA 49654 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROW 33D INOPERATIVE. REPLACED EMERGENCY EXIT FLO OR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999121100059 19991211 00059 NM 1999 12 11 AALA991648 1 19991031 A 3350 CONNECTOR BOEING 727 727223 1384074 NM GALLEY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 870AA 21382 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ABOVE AFT GALLEY IS BLINKING ON AND OFF WITH LIGHT SWITCH IN THE ON POSITION. RE-SEATED EMERGENCY EXIT SIGN CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1999121100060 19991211 00060 EU 1999 12 11 AALA991660 1 19991103 A 2120 AIR DISTRIBUTION FOKKER F28 F28MK0100 4990807 EU ROWS 18-20 ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1457B 11469 STL - FLT 1520 - EN ROUTE SAT/ORD - UNKNOWN BURNING SMELL NOTED IN CABIN AT SEAT ROWS 18-20. AIRCRAFT DIVERTED AND LAND ED STL WITHOUT INCIDENT. PERFORMED VISUAL INSPECTION OF AIRCRAFT INTERIOR, CABIN LIGHTING, PSU PANELS, CARGO COMPARTMEN TS, AND ELECTRONIC BAYS. NO OPEN CIRCUIT BREAKERS WERE NOTED. RAN AIR CONDITIONING PACKS AND RE-CIRCULATION FANS. COU LD NOT DUPLICATE SMELL OR ODOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1999121100061 19991211 00061 EU 1999 12 11 AALA991624 1 19991029 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU ROW 34G BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14065 508 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT 34G INOPERATIVE. REPAIRED WIRE FOR EMERGENCY EXI T FLOOR PATH LIGHT AT 34G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999121100062 19991211 00062 EU 1999 12 11 AALA991529 1 19991007 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU ROW 10G DEFECTIVE A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 70073 516 EGLL - FLT 0109 - GROUND INTERRUPTED AT LHR, RETURNED TO GATE. WIRE ARCING AT SEAT 10G. REPLACED INDIVIDUAL VIDEO SYST EM CABLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999121100063 19991211 00063 EU 1999 12 11 AALA991519 1 19991008 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 40064 507 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING ON RIGHT HAND SIDE OF FIRST CLASS INOPERATIVE. R EPAIRED RIBBON CONNECTOR AT RIGHT HAND SIDE OF FIRST CLASS ON EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED , NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1999121100064 19991211 00064 NM 1999 12 11 SWAA991998 1 19991202 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING WALK ARROUND INSP, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 767, STRINGER 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999121100065 19991211 00065 1999 12 11 SWAA991999 4 19991202 A 2565 22D22900 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE ASS Y PER MM. 2 L 7 2 4F A16WE 1999121100066 19991211 00066 NM 1999 12 11 SWAA992000 1 19991202 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOP. RELAMPED LIGHT ASSY PER MM . 2 L 7 2 4F RT A16WE 1999121100067 19991211 00067 NM 1999 12 11 SWAA992001 1 19991202 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND BS 312 FLOORBEAM UPPER SURFACE CORRODED, LBL 1 TO LBL 19. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999121100068 19991211 00068 NM 1999 12 11 SWAA991987 1 19991203 A 3230 273A14012 MANIFOLD BOEING 737 7377H4 NM NLG FAILED A SWAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 712SW 27846 DECLARED EMERGENCY, NLG WOULD NOT EXTEND. MANUAL EXTENSION PROCEDURES USED. REMOVED AND REPLACED NLG LOCK ACTUATOR REL IEF MODULE PER MM. 2 L 7 2 4F RT A16WE 1999121100069 19991211 00069 NM 1999 12 11 SWAA991988 1 19991203 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 11 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 EEPLS LENS MISSING AT ROW 11. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100070 19991211 00070 NM 1999 12 11 SWAA991989 1 19991203 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND BS 328 FLOORBEAM CORRODED ON UPPER SURFACE, LBL 27 TO RBL 49. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 1999121100071 19991211 00071 NM 1999 12 11 SWAA991990 1 19991201 A 2780 6554402 SWITCH BOEING 737 7373H4 1384600 NM LE FLAP OUT FO ADJUST A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 343SW 24151 AIR TURNBACK, RT WING L/E FLAP INDICATED PARTIALLY EXTENDED AFTER FLAP RETRACTION. QRH PROCEDURED C/W WITH NO CHANGE. A DJUSTED RT L/E FLAP TARGET RETRACT SWITCH PER MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1999121100072 19991211 00072 NM 1999 12 11 SWAA991991 1 19991201 A 5753 6546429 TRACK BOEING 737 7372H4 138448C NM TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED C4 CHECK, FOUND NR 7 T/E FLAP TRACK CRACKED AT INBD SIDE. REMOVED AND REPLACED FLAP TRACK ASSY PER MM. 2 L 7 2 4F A16WE 1999121100073 19991211 00073 NM 1999 12 11 SWAA991992 1 19991201 A 5320 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AROUND STOPS NR 3 AND NR 4. REMOVED AND REPLACED DOOR ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100074 19991211 00074 NM 1999 12 11 SWAA991993 1 19991201 A 5314 6545866 KEEL BEAM BOEING 737 7372H4 138448C NM BS 500A + 7" CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED, BS 500A+7, RBL 6.5. REPAIRED KEEL BEAM PER ER 99-6252. 2 L 7 2 4F A16WE 1999121100075 19991211 00075 NM 1999 12 11 SWAA991994 1 19991201 A 3350 6104791 POWER SUPPLY BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM. 2 L 7 2 4F A16WE 1999121100076 19991211 00076 NM 1999 12 11 SWAA991995 1 19991201 A 5210 6512353 HINGE COVER BOEING 737 7373H4 1384600 NM PAX DOOR LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 331SW 23695 AIR TURNBACK, DURING CLIMB, A VERY LOUD PRESS LEAK NOISE OUT OF FWD ENTRY DOOR UPPER HINGE AREA. READJUSTED UPPER DOO R HINGE COVER. 2 L 7 2 4F RT A16WE 1999121100077 19991211 00077 1999 12 11 SWAA991996 4 19991201 A 2565 D31354 INDICATOR BOEING 737 7372H4 138448C NM SLIDE DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 FWD SERVICE DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999121100078 19991211 00078 NM 1999 12 11 SWAA991997 1 19991201 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 EEPLS TRACK DAMAGED BY OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100079 19991211 00079 NM 1999 12 11 SWAA991985 1 19991129 A 5311 6546569 FRAME BOEING 737 7373H4 1384600 NM BS 1048 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND BS 1048 FRAME CRACKED BETWEEN STRINGERS 2R-3R. REMOVED AND REPLACED FRAME SECTION PE R SRM. 2 L 7 2 4F RT A16WE 1999121100080 19991211 00080 NM 1999 12 11 SWAA991986 1 19991129 A 5753 6546435277 SKIN BOEING 737 7373A4 1384585 NM TE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT FLAP CRACKED ON LOWER SKIN. REPAIRED FLAP PER SWA RA NR 1-357-077 1. 2 L 7 2 4F RT A16WE 1999121100081 19991211 00081 1999 12 11 SWAA991977 4 19991129 A 2565 D31354 INDICATOR BOEING 737 7372H4 138448C NM SLIDE DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 68SW 22357 AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999121100082 19991211 00082 NM 1999 12 11 SWAA991978 1 19991129 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FLANGE, BS 986, RBL 35.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999121100083 19991211 00083 NM 1999 12 11 SWAA991979 1 19991129 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 398SW 27692 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER FLANGE, BS 328, RBL 49. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 1999121100084 19991211 00084 1999 12 11 SWAA991980 4 19991128 A 2565 61621 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 614SW 28033 DURING SCHEDULED SPECIAL VISIT FOUND, AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY TORN. REMOVED AND REPLACED SLIDE ASSY P ER MM. 2 L 7 2 4F RT A16WE 1999121100085 19991211 00085 NM 1999 12 11 SWAA991981 1 19991129 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600WN 27694 EEPLS LIGHT ASSY BROKEN AT ROW 16. REMOVED AND REPLACED TRACK SECTION PER MM. 2 L 7 2 4F RT A16WE 1999121100086 19991211 00086 NM 1999 12 11 SWAA991982 1 19991129 A 5311 6546529 FRAME BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED, BS 360, STRINGER 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999121100087 19991211 00087 NM 1999 12 11 SWAA991983 1 19991129 A 5320 6545772 SPLICE BOEING 737 7372H4 138448C NM BS 727A - 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED, BS 727A-727B, STRINGER 5R. REPAIRED SPLICE PER SRM. 2 L 7 2 4F A16WE 1999121100088 19991211 00088 NM 1999 12 11 SWAA991984 1 19991129 A 5320 BAC1503 STIFFENER BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD BOTH VERTICAL STIFFENER CRACKED, LBL 28.5 AND RBL 28.5. REMOVED AND REPLACED VERTICAL STIFFENERS PER SRM. 2 L 7 2 4F RT A16WE 1999121100089 19991211 00089 NE 1999 12 11 SWAA991964 2 19991125 A 7230 9527M99P11 BLADE BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE BIRD STRIKE A SWAA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SW 07 509SW 24186 ABORTED TAKEOFF, BIRD STRIKE ON NR 1 ENG INLET. FOUND 4 FAN BLADES DAMAGED. REMOVED AND REPLACED NR 1 ENG FAN BLADES P ER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121100090 19991211 00090 1999 12 11 SWAA991965 4 19991126 A 2565 D31354 INDICATOR BOEING 737 7377H4 NM SLIDE DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 733SA 27865 AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100091 19991211 00091 NM 1999 12 11 SWAA991966 1 19991128 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 EEPLS LIGHTS INOP NEAR OVERWING EXIT. RESECURED EEPLS LIGHTS PER MM. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999121100092 19991211 00092 NM 1999 12 11 SWAA991967 1 19991127 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 4 EEPLS LIGHTS INOP. REINSTALLED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999121100093 19991211 00093 NM 1999 12 11 SWAA991968 1 19991126 A 2720 65C370539 PCU BOEING 737 7373H4 1384600 NM RUDDER ERRATIC A A SWAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 07 361SW 26572 DURING DESCENT, YAW DAMPER KICKED HARD TO THE LEFT AND DISCONNECTED. AIRCRAFT FLEW NORMALLY THE REST OF THE FLIGHT WITH YAW DAMPER DISCONNECTED. REMOVED AND REPLACED RUDDER PCU AND RUDDER STANDBY PCU. 2 L 7 2 4F RT A16WE 1999121100094 19991211 00094 NM 1999 12 11 SWAA991969 1 19991124 A 5330 6545773 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 727, BELOW NR 21 AND NR 22 WINDOWS. REPAIRED S KIN PER SRM. 2 L 7 2 4F A16WE 1999121100095 19991211 00095 1999 12 11 SWAA991970 4 19991124 A 2565 D22901 SLIDE BOEING 737 7372T4 1384492 NM PAX DOOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT VELCRO WORN. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999121100096 19991211 00096 NM 1999 12 11 SWAA991971 1 19991124 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 EEPLS TRACK PULLED UP AT OVERWING EXIT. RESECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100097 19991211 00097 1999 12 11 SWAA991972 4 19991124 A 2565 D31354 SLIDE BOEING 737 7373T5 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100098 19991211 00098 NM 1999 12 11 SWAA991973 1 19991127 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROW 14 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS INOP AT ROW 14. REPAIRED WIRING PER MM. 2 L 7 2 4F RT A16WE 1999121100099 19991211 00099 1999 12 11 SWAA991974 4 19991127 A 2565 6567380 BRACKET BOEING 737 7373H4 1384600 NM SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 622SW 27932 FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR AFT MOUNT BRACKET LOOSE. REMOVED AND REPLACED BRACKET ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100100 19991211 00100 NM 1999 12 11 SWAA991975 1 19991127 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FWD SECTION INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999121100101 19991211 00101 NM 1999 12 11 SWAA991976 1 19991122 A 5240 6552873 SEAL BOEING 737 7373H4 1384600 NM SERVICE DOOR LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 07 662SW 23255 DIVERSION VERY LOUD PRESSURIZATION LEAK NOISE IN AFT SERVICE DOOR. (DIVERTED TO PHX). ADJUSTED AFT SERVICE DOOR PER MM. 2 L 7 2 4F RT A16WE 1999121100102 19991211 00102 NM 1999 12 11 SPAA00008 1 19991202 A 3350 900542 BATTERY CHARGER BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE FORWARD AISLE EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE ASSOCIATED SYSTEM BATTERY C HARGER WAS REPLACED. SUBSEQUENT SYSTEM TEST WAS SATISFACTORY PER BMM 33-51-81. 2 L 7 2 4F A16WE 1999121100103 19991211 00103 NM 1999 12 11 HNAA9900164 1 19991203 A 5210 DOOR DHAV DHC8 DHC8201 2809001 NM CABIN BINDING A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 966HA 452 PAX DOOR BINDING WILL NOT OPEN. REINSTALLED AIRSTAIR DOOR CABLE 2 H 7 2 4T RT A13NM 1999121100104 19991211 00104 EU 1999 12 11 MALA976642 1 19991123 A 2613 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 413XJ 413 RIGHT TAILPIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF. CREW REDUCED POWER 20-30 PERCENT AFTER 5-7 MINUTES LIGHT EXTINGUISH ED. ALL OTHER ENGINE PARAMETERS NORMAL. RETURNED TO CWA. MAINTENANCE OPERATED RIGHT ENGINE, SUSPECT MOISTURE FROM HEA VY RAIN STORM, WHICH CAUSED FALSE INDICATION. ALL INDICATIONS NORMAL. 2 L 7 2 4T RT A52EU 1999121100105 19991211 00105 EU 1999 12 11 MALA976643 1 19991126 A 5415 WX2598 SEAL BAC 146 AVRO146RJ85A 1500097 EU PYLON FAILED A MALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 15 511XJ E2326 WHILE AT LEVEL CRUISE 31,000 AP-ON A/T ON .7 MACH CREW NOTICED THRUST LEVERS 1,3,4 MOVING TOWARD IDLE, TRIED MOVING NR 2 BUT IT WAS STUCK SELECTED A/T OFF NR 2 ENGINE STILL STUCK. 91 PERCENT N1 TURNED ON NR 2 ENGINE ANTI-ICE AND AFTER 2 MI NUTES, 30 SECONDS REGAINED CONTROL OF 32 THRUST LEVER. MAINTENANCE RESEALED SUSPECTED AREA, PYLON TO WING CONNECTION AN D LOWER EDGE TO WING INBOARD. 2 H 7 4 4F RT A49EU 1999121100106 19991211 00106 EU 1999 12 11 MALA976644 1 19991126 A 7603 POWER LEVER BAC 146 AVRO146RJ85A 1500097 EU NR 1 ENGINE JAMMED A MALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 15 524XJ E2349 DURING DESCENT OUT OF 28,000 AS THE POWER LEVERS RETARDED, THE NR 1 POWER LEVER STOPPED AT 78 PERCENT. CREW DISENGAGED THE AUTO THROTTLES AND THE NR 1 POWER LEVER WAS JAMMED, WOULD NOT RETARD. IT WOULD HOWEVER MOVE FORWARD. AS WE DESCEND ED INTO WARMER TEMP POWER LEVER FREED UP. MAINTENANCE REMOVED NR 1 ENGINE POWER LEVER INSPECTION PANEL, INSPECTED DUAL LEVER CABLES. NO EVIDENCE OF MOISTURE OR CANTAMINATION NOTED, EXERCISED CONTROL CABLES-MOVED FREELY. PERFORMED AUTO TH ROTTLE SERVO CHECK AND RTS CHECK. SYSTEM OPERATES NORMALLY. UNABLE TO DUPLICATE DISCREPANCY. 2 H 7 4 4F RT A49EU 1999121100107 19991211 00107 EU 1999 12 11 AWXA9900444 1 19991203 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 26699 19088 082 EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED MID CABIN RT POWER SUPPLY AND BATTERY. OPS CK NML. 2 L 7 2 4F RT A28NM 1999121100108 19991211 00108 NM 1999 12 11 AWXA9900445 1 19991203 A 5330 6545800 SKIN BOEING 737 73733A 1384673 NM FS 348 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 R-1 DOOR JAMB AFT LWR CORNER HAS 3 CRACKS, ALL START FROM EDGE TWO 1/4 CRACKS STOP AT FASTENERS ONE EXTENDS PAST FASTENE R. CUT OUT DAMAGED AREA, ACCOMPLISHED HFEC. NO CRACKS NOTED. FABRICATED OUTER DOUBLER FROM .100 2024T3 - R641191 BOTH MIDDLE AND INNER DOUBLERS FROM .063 2024T - R700214 PER SRM 53-10-01 FIG 202. INSTALLED REPAIR WASHERS AND SHIMMED AS REQUIRED, INSTALLED REPAIR DOUBLERS AND SHIMS PER SRM 53-10-01 FIG 202. 2 L 7 2 4F RT A16WE 1999121100109 19991211 00109 NM 1999 12 11 AWXA9900446 1 19991203 A 5330 6545877 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 L-1 DOOR JAMB AFT LWR CORNER HAS 1 CRACK .25 LONG COMING OUT OF FASTENER .125 INCH ON EACH SIDE OF FASTENER. REPAIRED L -1 DOOR JAMB AFT LWR CORNER FUSELAGE SKIN CRACKS PER ER 03-5330-99314-EY5. FABRICATED REPAIR FILLER USING MAT'L 2024T3 - .071 QQA250/5 R700681+ KIT PN 65C27257-30 R732516RECOMMENDATION. 2 L 7 2 4F RT A16WE 1999121100110 19991211 00110 NM 1999 12 11 AWXA9900447 1 19991203 A 5320 69144691 TIE CLIP BOEING 737 73733A 1384673 NM BS 1040 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 REMOVED DAMAGED PART PER 737-300 SRM 51-40-02, FABRICATED REPLACEMENT PART FROM 7075T6 - .032 QQA250/13 R682523 IAW SRM 51-30-01 TREATED AND PRIMED PART IAW SRM 51-20-01. INSTALLED REPLACEMENT PART I AW SRM 51-40-02 RECOMMENDATION. 2 L 7 2 4F RT A16WE 1999121100111 19991211 00111 NM 1999 12 11 AWXA9900448 1 19991203 A 5320 69144691 TIE CLIP BOEING 737 73733A 1384673 NM BS 1040 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 STRINGER CLIP CRACKED STR 15L STA 1040. REMOVED DAMAGED PART PER SRM 51-40-02, FABRICATED REPLACEMENT PART FROM 7075T6 .032 QQA 250/134 R682523 IAW SRM 51-30-01, TREATED AND PRIMED REPLACEMENT PART IAW 51-20-01. INSTALLED PART IAW SRM 51 -40-02 RECOMMENDATION. 2 L 7 2 4F RT A16WE 1999121100112 19991211 00112 CE 1999 12 11 PNSA991101 1 19991121 A 2450 CM358915 CIRCUIT BREAKER CESSNA 441 441 2076020 CE COCKPIT FAILED A PNSA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 AL 03 441LL 441139 WHILE CLIMBING-OUT PILOT NOTICED SMOKE COMING FROM THE RECOGNITION LIGHT SWITCH-BREAKER. SYSTEM WAS TURNED OFF, SMOKE S TOPPED. LANDING WAS NORMAL. SWITCH BREAKER WAS REPLACED. 1 L 7 2 3T RT A28CE 1999121100113 19991211 00113 CE 1999 12 11 PNSA991102 1 19991127 A 7921 99103431 COOLER CESSNA 441 441 2076020 CE OIL SYSTEM CRACKED A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 441LL 441139 EN ROUTE FROM BFI TO ANC, RT OIL PRESSURE BEGAN TO FLUCTUATE, DIVERTED TO SIT. ON FINAL, LOST RT OIL PRESSURE COMPLETEL Y SECURED ENGINE AND LANDED. OIL COOLER WAS LEAKING ALONG MOUNTING FLANGE. REPLACED COOLER. LEAK CHECK OK. 1 L 7 2 3T RT A28CE 1999121100114 19991211 00114 EU 1999 12 11 PNSA991103 1 19991121 A 2430 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A PNSA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 685PA 212 LT GENERATOR OVERHEAT LIGHT CAME ON AFTER TAKEOFF. RETURNED TO BASE. NO FAULT FOUND REPLACED STARTER GENERATOR AS A PR ECAUTIONARY PROCEDURE. 2 L 7 2 4T RT A52EU 1999121100115 19991211 00115 SW 1999 12 11 PNSA991104 1 19991101 A 5230 VALVE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR CONTAMINATED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 41NE AC741B AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO BASE. PURGED WATER FROM CARGO DOOR INFLATION VALVE. OPS CHECK OK. 2 L 7 2 4T RT A8SW 1999121100116 19991211 00116 EU 1999 12 11 PNSA991105 1 19991101 A 2430 WARNING LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A PNSA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 685PA 212 LEFT START GENERATOR OVER HEAT LIGHT ILLUMINATED DURING CLIMB. RETURNED TO BASE. NO FAULT FOUND. REPLACED WEU AS A PRE CAUTIONARY MEASURE. 2 L 7 2 4T RT A52EU 1999121100117 19991211 00117 NE 1999 12 11 9905091156 2 19991126 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 MALFUNCTIONED A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 01 156US 46765 686129 DURING DESCENT AT 12,000 FEET WHILE IN TURBULENCE, THE NR 2 ENGINE FLAMED OUT. THE RESTART ATTEMPT WAS SUCCESSFUL WITH ENGINE OPERATION NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER THE TAFI MANUAL WITH NO DE FECTS NOTED. ADDITIONAL MAINTENANCE ACTION WAS DEFERRED FOR 5 CYCLES. 2 L 7 3 4F 4 F A22WE E20EA 1999121100118 19991211 00118 WP 1999 12 11 9905109998 1 19991126 A 2910 BRAKE FUSE DOUG DC9 DC931 3022065 WP MLG LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 8934E 47143 LEFT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO AFTER TAKEOFF. CREW DECLARED A YELLOW EMERGENCY AND FLIGHT WAS RETURNED TO YYZ. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT LOWER BRAKE FUSE LEAKING. REPLACED BRA KE FUSE. LEAK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999121100119 19991211 00119 WP 1999 12 11 9905119620 1 19991129 A 2612 FIRE LOOP DOUG DC9 DC932 3022066 WP RT ENGINE MALFUNCTIONED A NWAA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 620NW 47533 RIGHT ENGINE B LOOP LIGHT ILLUMINATED AS POWER WAS SET FOR TAKEOFF. TAKEOFF WAS ABORTED AND NR 2 FIRE BOTTLE WAS BLOWN. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT ENGINE A AND B LOOPS FAILED. REPLACED RIGHT ENGI NE HARNESS/LOOP ASSEMBLY. ALSO, REPLACED NR 2 ENGINE FIRE BOTTLE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F A6WE 1999121100120 19991211 00120 WP 1999 12 11 9905129983 1 19991125 A 2161 60714621 CONTROLLER DOUG DC9 DC932 3022066 WP CABIN TEMP FAILED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 983US 62522 885 45790 AFTER TAKEOFF FROM MSP, CABIN TEMPERATURE WAS 150 DEGREES AND ACCOMPANIED BY SMOKE AND FUMES. THE RIGHT SIDE AUTOMATIC CABIN TEMPERATURE CONTROL VALVE WAS AT FULL HOT. FLIGHT CREW DISABLED AUTO TEMPERATURE CONTROL SYSTEM PER MAINTENANCE C ONTROL AND CONTINUED MEL 21-03A. AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT AUTO TEMPER ATURE CONTROLLER. OPERATIONAL CHECK GOOD AND REMOVED FROM MEL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999121100121 19991211 00121 NM 1999 12 11 UPS99431161 1 19991203 A 7110 COWL BOEING 747 747123F NM NR 3 ENGINE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 NR 3 ENGINE COWL DAMAGED ON INBOARD SIDE PUNCTURED. PERFORMED TEMP REPAIR PER EO AND DEFERRED INCIDENT RS99-409 DEFFER AL D182831. 2 L 7 4 4F A20WE 1999121100122 19991211 00122 NM 1999 12 11 UPS99431162 1 19991202 A 2780 TORQUE TUBE BOEING 747 747121 1384871 NM LE FLAP BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 NR 4 L/E PANEL RIGHT DROOPED AND SPLIT FROM INBD TO OUTBOARD SEGMENT. REMOVED AND REPLACED NR 4 L/E TORQUE TUBE IAW MM 27-81-05. FUNCTIONAL TEST OF L/E DEVIC ES PERFORMED. OPS CHECK NORMAL. 2 L 7 4 4F A20WE 1999121100123 19991211 00123 NM 1999 12 11 UPS99531163 1 19991203 A 2761 ACTUATOR BOEING 757 75724APF 1384969 NM SPOILER LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 424UP 25369 PILOT REPORT, CENTER HYD QTY LOSS IN FLIGHT. REMOVED AND REPLACED NR 1 SPOILER ACTUATOR. 2 L 7 2 4F RT A2NM 1999121100124 19991211 00124 WP 1999 12 11 ABXA9900814 1 19991130 A 3040 WB0320 TERMINAL BLOCK DOUG DC8 DC861 3021952 WP COCKPIT FAILED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 844AX 45848 AT TOP OF DESCENT WHEN THE ANTI-FOG CIRCUIT BREAKER WAS PUSHED, THERE WAS SMOKE IN THE UPPER RIGHT HAND CORNER OF THE RI GHT WINDSHIELD. PULLED ANTI-FOG CIRCUIT BREAKER, SMOKE STOPPED. *S/D* REPLACED TERMINAL BLOCK IAW MM, OPS CHECKS GOOD . 2 L 7 4 4F 4A25 1999121100125 19991211 00125 1999 12 11 MWEA99866 4 19991202 A 2565 100503117 SLIDE DOUG DC9 DC982 3022082 WP SERVICE DOOR LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 THE AFT GALLEY SIDE SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1999121100126 19991211 00126 NE 1999 12 11 RAIA9912001 2 19991201 A 7260 310430712 GEARBOX JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE CONTAMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 550HK 41039 75090 6113 - BOS - RIGHT OIL CONTAM LIGHT ON. MAINTENANCE REPLACED GEAR BOX FOR RIGHT ENGINE. 2 L 7 2 4T 4 T RT A41NM E18NE 1999121100127 19991211 00127 EU 1999 12 11 RAIA9912002 1 19991202 A 7332 41SG107100G14 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP FUEL PRESSURE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 342TE 954 66079 7477 - STL - LEFT FUEL PRESSURE GAUGE FLUCTUATING. MAINTENANCE REPLACED FUEL PRESS TRANSDUCER FOR LEFT ENGINE. 2 L 7 2 4T 4 T RT A56EU E4WE 1999121100128 19991211 00128 EU 1999 12 11 RAIA9912003 1 19991202 A 3060 845081B TIMER JETAIR JETSTM JETSTM4101 1500501 EU PROP HEAT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 559HK 41075 7458 - STL - NR 2 PROP HEAT INOP. MAINTENANCE REPLACED PROP HEAT TIMER FOR NR 2 ENGINE. 2 L 7 2 4T RT A41NM 1999121100129 19991211 00129 NE 1999 12 11 RAIA9912004 2 19991202 A 7322 350A52005009 MFC AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE NR 1 FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 722TE 220 7408 - STL - DC GEN NR 1 FAULT LIGHT ON. MAINTENANCE REPLACED NR 1 MULTI-FUNCTION COMPUTOR. 2 H 7 2 4T 4 T RT A53EU E2ONE 1999121100223 19991211 00223 SW 1999 12 11 HEEA064661 1 19991004 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DAMAGED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 447PH 2944 53114 RUBBER ON MAIN ROTOR GEARBOX MOUNT EXTRUDING. 1 G 7 1 3U O H2SW 1999121100224 19991211 00224 SW 1999 12 11 HEEA064662 1 19991004 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DAMAGED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 447PH 2944 53114 RUBBER ON MAIN ROTOR GEARBOX MOUNT EXTRUDING. 1 G 7 1 3U O H2SW 1999121100403 19991211 00403 SW 1999 12 11 HEEA064932 1 19991102 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DAMAGED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 437PH 53072 MAIN ROTOR GEARBOX MOUNT HAD RUBBER SEPARATION. 1 G 7 1 3U O H2SW 1999121100650 19991211 00650 NM 1999 12 11 RAAA99B1029 1 19991125 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 ROW 14 AISLEWAY EGRESS LIGHT, DOES NOT TEST. REPLACED BATTERY PACK, OPS OK. 2 L 7 3 4F A3WE 1999121100651 19991211 00651 NM 1999 12 11 RAAA99B1030 1 19991125 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 AFT ENTRY EMERGENCY EXIT ID LIGHT DOES NOT TEST. REPLACED BATTERY PACK OPS OK. 2 L 7 3 4F A3WE 1999121100652 19991211 00652 NM 1999 12 11 RAAA99B1031 1 19991125 A 3510 4566M37B042NM PBE ESSEX BOEING 727 72722C 138400F NM COCKPIT INFLATED A RAAA K NONE J WARNING INDICATION IN INSP/MAINT 1 AL 03 831RV 19093 COCKPIT PBE INDICATOR PIN PROTRUDING FROM CASE. REPLACED PBE. 2 L 7 3 4F A3WE 1999121100653 19991211 00653 NM 1999 12 11 RAAA99B1032 1 19991203 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 EMERGENCY AISLE LIGHT AT ROW 17 DEF WILL NOT TEST. REPLACED BATTERY, OPS CHECK OK. 2 L 7 3 4F A3WE 1999121100654 19991211 00654 WP 1999 12 11 CALA9901544 1 19991204 A 3222 VALVE DOUG DC9 DC982 3022082 WP NLG LEAKING A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 92874 49122 THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE SIF LIGHT AND AUTOSPOILER DO NOT USE LIGHT WERE ILLUMINATED . THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX FOUND THE SHRADER VALVE LEAKING. THE SCHRADER VALVE AND O-RING WERE REPLACED AND THE STRUT WAS SERVICED IAW MM 32-21-02. A GEAR RETRACTION WAS PERFORMED IAW MM 32-3 0-00 WITH ALL INDICATIONS AND OPERATION CHECKING GOOD. 2 L 7 2 4F A6WE 1999121100655 19991211 00655 WP 1999 12 11 CALA9901545 1 19991201 A 5511 SPAR DOUG DC10 DC1010 3022110 WP HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER SPAR CRACKED AT UPPER 11B MOUNTING HOLE FOR I/B L/E SECTION. THE AREA W AS REPAIRED IAW ECRA 5510-01473 AND EA 10-5510-2-A0514. 2 L 7 3 4F A22WE 1999121100656 19991211 00656 NM 1999 12 11 CALA9901546 1 19991202 A 5320 DOOR FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69311 23362 INSPECTION FOUND A 5 CRACK IN FORWARD CARGO DOOR AFT LOWER CORNER AND A 2 CRACK WAS LOCATED AT THE FORWARD LOWER CORNER. BOTH THE FORWARD AND AFT LOWER CORNERS OF DOOR FRAME WERE REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1999121100657 19991211 00657 WP 1999 12 11 CALA9901547 1 19991202 A 3350 60030431 BATTERY PACK GRIMES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16808 49262 INSPECTION FOUND THE FIRST CLASS OVERHEAD EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE OVERHEAD LIGHTING CHECKED GOOD. 2 L 7 2 4F A6WE 1999121100658 19991211 00658 NM 1999 12 11 CALA9901548 1 19991203 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND C-1 DOOR EXTERNAL SKIN DENTED. THE DENTED AREAS WERE CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW SR M 52-00-01, FIGURE 203. 2 L 7 2 4F RT A16WE 1999121100659 19991211 00659 NM 1999 12 11 CALA9901549 1 19991203 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 867 - 907 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND FUSELAGE CROWN SKIN WORN BY DORSAL FIN AT STA 867-907. THE WORN AREA WAS REMOVED AND A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 1999121100660 19991211 00660 WP 1999 12 11 CALA9901550 1 19991205 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1660 - 1680 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND CENTER CARGO COMPARTMENT LOWER FRAME CORRODED FROM STA 1660-1680, LONGERON 51L - 51R. THE CORRODED ARE A WAS TRIMMED OUT AND REINFORCED WITH SHEAR CLIP AND SPLICE IAW SRM 53-30-00, FIGURE 10 AND SRM 51-31-01. 2 L 7 3 4F A22WE 1999121100661 19991211 00661 WP 1999 12 11 CALA9901551 1 19991205 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1780 & 1841 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND CENTER CARGO COMPARTMENT LOWER FRAME CORRODED AT STA 1780 BETWEEN LONGERON 50L - 50R AND AT STA 1841, L 49R - 50L. THE CORRODED AREAS WERE TRIMMED OUT AND REINFORCED WITH SHEAR CLIPS AND SPLICES IAW SRM 53-30-00, FIGURES 9 AND 10, AND SRM 51-31-01. 2 L 7 3 4F A22WE 1999121100662 19991211 00662 WP 1999 12 11 CALA9901552 1 19991205 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 460 - 515 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND CABIN FLOORBEAM SUPPORT CORRODED BETWEEN STA 460 AND 515, LBL 33. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999121100663 19991211 00663 WP 1999 12 11 CALA9901553 1 19991205 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 785 - 789 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED BETWEEN STA 785 AND 789, RBL 47. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-70-00, FIGURE 13 AND 51-31-01. 2 L 7 3 4F A22WE 1999121100664 19991211 00664 NM 1999 12 11 CALA9901554 1 19991205 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500C CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND A 1 CRACK IN STRINGER 16R AT STA 500C. THE STRINGER SECTION WAS REPLACED IAW SRM 53-00-03, FIGURE 201. 2 L 7 2 4F RT A16WE 1999121100665 19991211 00665 NM 1999 12 11 CALA9901555 1 19991205 A 5314 KEELBEAM BOEING 737 7373T0 1384582 NM BS 500D CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13331 23569 INSPECTION FOUND KEEL BEAM CORRODED AT STA 500D, S28R. REPAIRED IAW SRM 53-30-12. 2 L 7 2 4F RT A16WE 1999121100666 19991211 00666 NM 1999 12 11 CALA9901556 1 19991205 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 312 FROM RBL 36 TO LBL 18. THE CORRODED SECTION OF FLOORBEAM WAS REPLAC ED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999121100667 19991211 00667 NM 1999 12 11 CALA9901557 1 19991205 A 5320 WEB BOEING 737 7373T0 1384582 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND A 2 CRACK IN WEB BELOW R-2 DOOR ASSIST HANDLE AT STA 950, S11R AND A 2 CRACK WAS FOUND IN WEB BELOW L-2 DOOR ASSIST HANDLE AT STA 950, S11L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 1999121100668 19991211 00668 NM 1999 12 11 CALA9901558 1 19991124 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND FLOORBEAM CAP IN AFT LEFT LAV AREA CORRODED AT STA 986. REPAIRED IAW ECRA 5310-03851. 2 L 7 2 4F RT A16WE 1999121100669 19991211 00669 WP 1999 12 11 9905139976 1 19991123 A 5711 SPAR DOUG DC9 DC931 3022065 WP WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9340 47389 DURING M CHECK, FOUND CRACK AT NBR 4 FLAP HING OUTBOARD BOLT HOLE AT BOTTOM APPROXIMATEY 3.8 INCH ON WING SPAR. REPAIRE D PER EA 99-169349. 2 L 7 2 4F A6WE 1999121100670 19991211 00670 WP 1999 12 11 9905149760 1 19991117 A 5711 SPAR DOUG DC9 DC941 302207N WP WS 267 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING M CHECK, LEFT WING REAR SPAR CAP HAS CORROSION AFT SIDE STA. XRS 267, NR 3 FLAP HINGE FITTING UPPER STUD HOLES. R EPAIRED PER EA 97-171707. 2 L 7 2 4F A6WE 1999121100671 19991211 00671 WP 1999 12 11 9905159986 1 19991124 A 5311 SPAR DOUG DC9 DC932 3022066 WP WING DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING M CHECK, LEFT UPPER REAR SPAR CAP MOD STEP 8 REVEALED HOLES 1-22 AT OR EXCEEDING .2797 LIMIT. REPAIRED PER EA 99 -171572. 2 L 7 2 4F A6WE 1999121100672 19991211 00672 WP 1999 12 11 9905169986 1 19991117 A 5753 HINGE DOUG DC9 DC932 3022066 WP TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING M CHECK, NR 3 FLAP HINGE LEFT OUTER HOLE HAS CRACK ABOVE HOLE AT APPROXIMATELY 12:00 POSITION. REPAIRED PER EA 9 9-169621. 2 L 7 2 4F A6WE 1999121100673 19991211 00673 WP 1999 12 11 9905179996 1 19991117 A 5320 DOOR FRAME DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47441 DURING L CHECK, FOUND FORWARD CARGO DOOR CUTOUT AFT EDGE CRACKED AND GOUGED. REPAIRED PER EA 99-169362. 2 L 7 2 4F A6WE 1999121100674 19991211 00674 WP 1999 12 11 9905189989 1 19991119 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1038 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING SVI, AFT ACCESSORY COMPARTMENT FS 1038 LEFT FRAME HAS FASTENER HOLE ELONGATED TO .310 AT HOLE NR 22 FOR UPPER REA R SPAR CAP. REPAIRED PER EA 99-169369. 2 L 7 2 4F A6WE 1999121100675 19991211 00675 WP 1999 12 11 9905199976 1 19991124 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 180 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9340 47389 DURING M CHECK, FOUND ELONGATED HOLE IN FLOORBEAM FS 180, 22 INCHES INBOARD OF CUSP AT PASSENGER ENTRANCE DOOR. REPAIRE D PER EA 99-169386. 2 L 7 2 4F A6WE 1999121100676 19991211 00676 WP 1999 12 11 9905209986 1 19991124 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 155 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING M CHECK, FOUND CRACK AT CANTED INTERCOSTAL AT FS 155, LONGERON 12R. REPAIRED PER EA 99-172600. 2 L 7 2 4F A6WE 1999121100677 19991211 00677 NM 1999 12 11 9905216303 1 19991205 A 5330 SKIN BOEING 747 747451 1384940 NM BS 760 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND CRACK IN FUSELAGE SKIN FORWARD BOTTOM OF DOOR 2L LBL 199.8. REPAIRED PER EA 63-160583. 2 L 7 4 4F RT A20WE 1999121100678 19991211 00678 SO 1999 12 11 COMA9910179 1 19991203 A 5240 DOOR EMB 120 EMB120RT SO FUEL SERVICE OPEN A COMA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 SO 01 249CA 120230 SERVICE DOOR WARNAING DURING TAKEOFF. FUEL SERVICE DOOR FOUND OPEN. SECURED DOOR, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1999121100679 19991211 00679 SO 1999 12 11 COMA9910180 1 19991202 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 264CA 120256 EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999121100680 19991211 00680 EA 1999 12 11 COMA9960733 1 19991130 A 5210 100805 STRIKER CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 017CA 7017 CABIN DOOR WARNING. REWORKED DOOR SEAL STRIKER IAW REO 601R52-11-103. FLIGHT CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 1999121100681 19991211 00681 EA 1999 12 11 COMA9960734 1 19991204 A 3350 100805 BATTERY CHARGER CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 958CA 7111 EMERGENCY LIGHT SYSTEM INOP. REPLACED THE NR 3 EMERGENCY BATTERY CHARGER. 2 L 7 2 4F RT A21EA 1999121100682 19991211 00682 EA 1999 12 11 COMA9960735 1 19991204 A 5315 601R3111329 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 15727 7018 FLOORBEAM WEB AT LBL9 AT FS 280.00 TO FS 295 AT OUTBOARD SIDE HAS CRACK 1.4 LONG AT APT SIDE OF L ANGLE AT FS280.00. RE MOVED CRACK WEB AND INSTALLED NEW FABBED WEB IAW WVAC EO 601R-53-0666. 2 L 7 2 4F RT A21EA 1999121100683 19991211 00683 EA 1999 12 11 COMA9960736 1 19991203 A 5320 60031535 STRIKER CNDAIR CL600 CL6002B19 EA BS 310 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 4889 7204 PAX DOOR SEAL STRIKER AT FS 310.00 STR 15-16 HAS PREVIOUS REPAIR DAMAGED IE SEALANT CRACKED AND DOUBLER BENT, DUE TO CON TACT WITH PASSENGER DOOR PIN. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR SEAL STRIKER AT FS 310.00 STR 15-16 LHS IAW CR J REO 601R-52-11-008 REV B. 2 L 7 2 4F RT A21EA 1999121100684 19991211 00684 EA 1999 12 11 COMA9960737 1 19991203 A 5330 601R31109 SKIN CNDAIR CL600 CL6002B19 EA BS 310 DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 4889 7204 FUSELAGE SKIN AT FS 31.00 STR 15-16 LHS DAMAGED BY CONTACT WITH PASSENGER DOOR BTM PIN. PERFORMED A MAJOR REPAIR TO FUS ELAGE SKIN AT FS 310.00 STR 15-16 LHS IAW CRJ REO 601R-53-21-180 REV NC. 2 L 7 2 4F RT A21EA 1999121100685 19991211 00685 EA 1999 12 11 COMA9960738 1 19991203 A 5320 601R31527176 ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 15727 7018 PAX DOOR THRESHOLD SUPPORT ANGLE DUE REPAIR PER DMI Z07472. REMOVED AND REPLACED THRESHOLD ANGLE IAW WVAC EO 601R-53-06 64B. 2 L 7 2 4F RT A21EA 1999121100686 19991211 00686 EA 1999 12 11 COMA9960739 1 19991204 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 15727 7018 FWD J ANGLE AT FS 280.00 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED BEYOND REPAIR. REMOVED CORRODED ANGLE AND INSTALLED NE W J ANGLE IAW WVAC EO 601R-52-0667. 2 L 7 2 4F RT A21EA 1999121100687 19991211 00687 EA 1999 12 11 COMA9960740 1 19991204 A 5320 60034017373 CLIP CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 15727 7018 ANGLE CLIP AT FS 280.00 INSIDE CBP1 ON INBOARD SIDE CRACKED. REMOVED CRACKED CLIP AND INSTALL NEW FABBER ANGLE CLIP IAW WVAC EO 601R-53-0668, REV A. 2 L 7 2 4F RT A21EA 1999121100688 19991211 00688 EA 1999 12 11 COMA9960741 1 19991204 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 15727 7018 AFT J ANGLE AT FS 280.00 IS CRACKED APPROXIMATELY 1.0 ON THE OUTBOARD SIDE OF RBL9. RETURNED CRACKED ANGLE AND INSTALLE D NEW ANGLE IAW WVAC EO 601R-53-0670. 2 L 7 2 4F RT A21EA 1999121100689 19991211 00689 EA 1999 12 11 COMA9960742 1 19991204 A 5320 601R3111357 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 15727 7018 FORWARD L ANGLES AT FS 280.00 AND LBL 9.00 ARE CRACKED. REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES FS 280.00 AND L BL 9.0 IAW WVAC EO 601R-53-0669, REV A. 2 L 7 2 4F RT A21EA 1999121100690 19991211 00690 EA 1999 12 11 COMA9960743 1 19991204 A 5311 6003603031 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 988CA 4889 7204 FRAME AT FS 718.0 LHS STR 10-12 HAS AFT DOUBLER P/N 600-36030-31 IS CRACKED. PERFORMED A MAJOR REPAIR TO FRAME AFT DOUB LER AT FS 718.0 LHS STR 10-12 BY REPLACING DOUBLER IAW CRJ REO 601R-53-61-193A. 2 L 7 2 4F RT A21EA 1999121100691 19991211 00691 EA 1999 12 11 COMA9960744 1 19991205 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 640 CRACK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 LOWER HORIZONTAL SURFACE OF RIGHT LOWER WING ACCESS HOLE AT 640DB CRACKED. BLENDED OUT DAMAGE, ROTO-PEENED, AND ALODINE D IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999121100692 19991211 00692 NM 1999 12 11 UPS99231164 1 19991123 A 5730 7075T6 SKIN BOEING 727 72725C 138400H NM WS 867 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI DISCOVERED CORROSION ON LOWER SURFACE OF UPPER WING CENTER SECTION SKIN AT BS 867 RBL 66 AND LBL 66. REPAIRED IAW BFG ER 99-6346 (UPS FILE NR B727-5710-12093). 2 L 7 3 4F A3WE 1999121100693 19991211 00693 NM 1999 12 11 UPS99231165 1 19991118 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 463 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION ON STRINGER AT BS 463 STR 21R. REPAIRED STRINGER PER SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999121100694 19991211 00694 NM 1999 12 11 UPS99231166 1 19991118 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI SHEAR TIE AT BS 480 STR 20-21 RT IS CRACKED AND CORRODED. FABRICATED AND REPLACE SHEAR TIE PER SRM 5 3-10-4 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999121100695 19991211 00695 NM 1999 12 11 UPS99231167 1 19991118 A 5330 SKIN BOEING 727 72725C 138400H NM BS 355 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI BULGING SKIN AT BS 355, STR 27R, WL 156. REPAIRED BULGING SKIN AT BS 355, STR 27R, WL 156 IAW ER 99- 6374 AND SRM 53-30-03 FIG 3A AND ER 99-6412. 2 L 7 3 4F A3WE 1999121100696 19991211 00696 NM 1999 12 11 UPS99231170 1 19991205 A 2131 CONTROLLER BOEING 727 72725C 138400H NM COCKPIT INOP A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 949UP 19717 PRESSURIZATION INOP IN MANUAL AND AUTO MODE. 2 L 7 3 4F A3WE 1999121100697 19991211 00697 NM 1999 12 11 UPS99231176 1 19991203 A 3350 LIGHT BOEING 727 72725C 138400H NM ROW 11 & 19 INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 EMERGENCY LIGHT AT ROW 11 AND 19 INOP. REMOVED AND REPLACED BATTERY PACK IN ROW 11 AND 19, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1999121100698 19991211 00698 NM 1999 12 11 UPS99431169 1 19991204 A 2150 FAN BOEING 747 747212B 1384886 NM COCKPIT INOP A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 520UP 1 CREW PREFLIGHT, ELECTRIC ODOR UPPER DECK EQUIP COOLING FAN INOP. SWAPPED LEFT MAIN EQUIP COOL FAN WITH UPPER DECK AND D EFERRED. 2 L 7 4 4F A20WE 1999121100699 19991211 00699 NM 1999 12 11 UPS99431171 1 19991206 A 5730 PANEL BOEING 747 747212B 1384886 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A, CRACK UPPER WING PANEL L/E RIGHT WING. *S/D* REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1999121100700 19991211 00700 NM 1999 12 11 UPS99431172 1 19991205 A 5754 SKIN BOEING 747 747212B 1384886 NM LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 523UP 22381 4 INCH CRACK AFT OF NR 13 KRUGER FLAP. 2 L 7 4 4F A20WE 1999121100701 19991211 00701 NM 1999 12 11 UPS99431175 1 19991204 A 5311 FRAME BOEING 747 747123F NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 FRAME DAMAGED AT PANEL 192, SUPPLEMENTAL MRR, TRANSFERRED TO C CHECK VISIT 1006 FLS AEROSPACE DUBLIN NRC 017. 2 L 7 4 4F A20WE 1999121100702 19991211 00702 WP 1999 12 11 UPS99831174 1 19991205 A 2760 LINK DOUG DC8 DC873F 302199F WP NR 1 SPOILER BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:N/A, LEFT NR 1 SPOILER HAD 2 BROKEN LINKS. *S/D* REMOVED AND REPLACED BOTH NR 1 GROUND SPOILER PANEL C RANKS IAW 27-61-01. PERFORMED INSP/CHECK OF SPOILER ACT SYSTEM IAW 27-61-01, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999121100703 19991211 00703 NM 1999 12 11 99FDEA00495 1 19991203 A 7932 41809104 TRANSMITTER DOUG MD11 MD11F 3023600 NM NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 616FE 48747 99-279 - DURING CLIMB, NR 1 ENG OIL PRESS DROPPED TO 0. REMOVED AND REPLACED NR 1 ENG OIL PRESS TRANSMITTER PER MM 79-3 3-01-4. OPS CK SATISFACTORY. 2 L 7 3 4F RT A22WE 1999121100704 19991211 00704 NM 1999 12 11 99FDEA00497 1 19991126 A 5530 AJC7515501 FITTING DOUG MD11 MD11F 3023600 NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 582FE 48420 WHILE ACCOMPLISHING EO 1-5510-7-3304 PART 2 AT RT AFT MOST BOTTOM HOLE, WHILE REAMING TO CLEAR-OFF CRACK FOUND A SLEEVE BUSHING ON THE HOLE SKIN SIDE. (SLEEVE BUSHING HAD COME OUT DURING REAMING PROCESS). RT AFT MOST BOTTOM HOLE REPAIR CA RRIED OUT AS PER FED EX ENG AUTH NR 1-5530-48153. 2 L 7 3 4F RT A22WE 1999121100705 19991211 00705 WP 1999 12 11 ABXA9900815 1 19991203 A 3350 5708458 BATTERY PACK DOUG DC8 DC862 3021970 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805AX 45906 DURING PREFLIGHT, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC8 MM 33-50-01. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999121100706 19991211 00706 WP 1999 12 11 ABXA9900816 1 19991203 A 3260 2714425 SPRING DOUG DC8 DC861 3021952 WP LT MLG WW WEAK A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 843AX 46017 DURING CLIMB-OUT, LANDING GEAR UNSAFE LIGHT ILLUMINATED. LEFT GEAR DOOR LIGHT INDICATED UNSAFE. RECYCLED GEAR, LIGHT D ID NOT GO OUT. LIGHT WENT OUT DURING CRUISE. REPLACED LEFT MAIN LANDING GEAR DOOR UPLATCH TENSION SPRING. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999121100707 19991211 00707 NM 1999 12 11 SCNA99147 1 19991203 A 3350 38931002 BATTERY BOEING 727 7272J4 1384006 NM AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIRS EMERGENCY OVERHEAD LIGHT WAS FOUND VERY DIM. REMOVED AND REPLACED TH E EMERGENCY OVERHEAD LIGHT BATTERIES. OPERATIONALLY CHECKS GOOD PER MM 335061. 2 L 7 3 4F RT A3WE 1999121100708 19991211 00708 NM 1999 12 11 SCNA99148 1 19991203 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM LT OVERWING DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REMOVED AND REPLACED LEFT O VERWING EMERGENCY LIGHTS BATTERY PACK. OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1999121100709 19991211 00709 NM 1999 12 11 VNAA9912001 1 19991205 A 7110 001A711E1400008 DOOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COWL UNLATCHED A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 432JS 11625 3045 116061 DURING CLIMB, THE FLIGHT CREW FELT A VIBRATION ON THE LEFT SIDE. THE CREW TURNED ON THE WING LIGHT AND NOTICED THE LEFT ENGINE OUTBOARD COWLING FLAPPING IN FLIGHT. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE AT PIT INSPECTED AND REPOSITIONEDTHE DOOR COWLING AND THE AIRCRAFT WAS FERRIED TO CAK FOR FURTHER MAINTENANCE. MAINTENA NCE AT CAK INSPECTED AND REPLACED THE LEFT OUTBOARD ENGINE COWLING DOOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71 -10-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR FLIGHT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121100710 19991211 00710 NM 1999 12 11 VNAA9912002 1 19991205 A 3251 2318000002 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 458PS 8993 3068 THE AIRCRAFT WAS TAKING THE RUNWAY FOR TAKEOFF WHEN THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE. THE AIRCR AFT WAS DIFFICULT TO CONTROL SO THE CREW BROUGHT THE AIRCRAFT TO A STOP. THE FLIGHT CLEARED THE RUNWAY AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A TAXI CHECK IN ACCORDANCE WITH DORNIER MAINTENA NCE MANUAL 32-50-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121100711 19991211 00711 WP 1999 12 11 K4HA99088 1 19990616 A 3260 CONTROL CABLE LKHEED 1011 1011385115 5265015 WP MLG FAILED A K4HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 106CK 293C1211 UNSAFE GEAR INDICATION. REPLACE CABLE. 2 L 7 3 4F A23WE 1999121100712 19991211 00712 EU 1999 12 11 RAIA9911029 1 19991118 A 3620 6411343 SWITCH AEROSP ATR42 ATR42300 8680920 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 426TE 228 7108 - STL - LEFT BLEED OVERHEAT LIGHT ON. MAINTENANCE REPLACED BLEED OVERTEMP SWITCH FOR LEFT SYSTEM. 2 H 7 2 4T RT A53EU 1999121100713 19991211 00713 EU 1999 12 11 RAIA9912005 1 19991118 A 3620 6411343 SWITCH AEROSP ATR42 ATR42300 8680920 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 426TE 228 7108 - STL - NR 1 BLEED OVERHEAT LIGHT ON. MAINTENANCE REPLACED BLEED OVERTEMP SWITCH FOR LEFT BLEED SYSTEM. 2 H 7 2 4T RT A53EU 1999121100714 19991211 00714 EU 1999 12 11 R7MA0000789 1 19991010 A 2435 160SG137Q STARTER AGUSTA A109 A109K2 0260502 EU STARTER/GEN MALAFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 810 1016 10016 STARTER INTERMITTENTLY WILL NOT TURN OVER. WHEN ENGINE IS HOT, STARTER WILL NOT TURN. WHEN AIRCRAFT COOLS FOR 30 MINUT ES, ENGINE WILL START. SUBMITTER SUSPECTED BEARINGS IN STARTER/GENERATOR TO BE THE PROBLEM. (X) 1 G 7 2 3U RT H7EU 1999121100715 19991211 00715 EU 1999 12 11 R7MA0000801 1 19991026 A 6220 709010118105 ROD ENDS AGUSTA A109 A109K2 0260502 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 10016 UPPER ROD END WORN BEYOND LIMITS. (X) 1 G 7 2 3U RT H7EU 1999121100716 19991211 00716 EU 1999 12 11 R7MA0000800 1 19991025 A 2913 807712 COUPLING AGUSTA A109 A109K2 0260502 EU HYDRAULIC PUMP WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 10016 SPLINES WORN BEYOND LIMITS. (X) 1 G 7 2 3U RT H7EU 1999121100721 19991211 00721 NM 1999 12 11 99ZZZX4349 1 19991117 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 950F-970 CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 70755 21366 DURING A C-CHECK, CORROSION WAS NOTED ON STR 28L STA 950F - STA 970. 2 L 7 3 4F A3WE 1999121100749 19991211 00749 NM 1999 12 11 HNAA9900165 1 19991206 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8201 2809001 NM CABIN INOP A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 990HA 428 LEFT FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED 3352-P2 POWER SUPPLY BASE AND 3351-PS3 POWER SUPPLY. 2 H 7 2 4T RT A13NM 1999121100750 19991211 00750 WP 1999 12 11 AT9900837 1 19991124 A 3350 OL3071PBE LIGHT DOUG DC9 DC932 3022066 WP CABIN MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 845AT 47238 AFT SECTION FLOOR EMERGENCY PATHWAY LIGHT AND LENS MISSING. INSTALLED MISSING LIGHT AND LENS IAW MM 33-21-27. 2 L 7 2 4F A6WE 1999121100751 19991211 00751 WP 1999 12 11 AT9900838 1 19991128 A 3520 OXYGEN MASK DOUG DC9 DC932 3022066 WP SEAT 28 DEF FAILED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 836AT 47397 DURING OXYGEN MASK INSPECTION TO COMPLY WITH EO 9-3520-29-E1461, PASSENGER OXYGEN MASKS ABOVE SEAT POSITION 28-DEF AND A FT F/A STATION DID NOT DEPLOY. CLEANED EXCESSIVE PAINT OFF DOOR OF AFT F/A O2 MASK COMPARTMENT. RE-ATTACHED LOOSE HOSE TO MANIFOLD IN PSU ABOVE SEAT 28DEF IAW MM 35-20. 2 L 7 2 4F A6WE 1999121100752 19991211 00752 WP 1999 12 11 AT9900839 1 19991117 A 3520 OXYGEN MASK DOUG DC9 DC932 3022066 WP ROW 18 DEF FAILED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 822AT 47274 DURING OXYGEN MASK INSPECTION TO COMPLY WITH EO 9-3520-29-E1461, PASSENGER OXYGEN MASKS ABOVE SEAT 18DEF DID NOT DEPLOY. PERFORMED OPERATIONAL CHECK OF OXYGEN MASK DROP AT ROW 18 DEF PER MM 35-20. RESULTS GOOD PER MM 35-20. 2 L 7 2 4F A6WE 1999121100753 19991211 00753 1999 12 11 AT9900840 4 19991126 A 2565 11611143 SLIDE BOEING 737 737222 1384473 NM PAX DOOR LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 468AT 19074 FOUND L1 DOOR EMERGENCY SLIDE PACK LOOSE. SECURED L1 DOOR EMERGENCY SLIDE PACK IAW B737 MM 25-61. 2 L 7 2 4F A16WE 1999121100754 19991211 00754 WP 1999 12 11 AT9900841 1 19991026 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND AFT PIT AFT BULKHEAD RIGHT HAND PANEL WAS CORRODED. REMOVED CORROSION FROM STRAP MATT LOSS OF 50 PERCENT OUT OF L IMITS. FABRICATED STRAP, TREATED, PRIMED IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 53-01 FIGURE 1. 2 L 7 2 4F A6WE 1999121100755 19991211 00755 WP 1999 12 11 AT9900842 1 19991106 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 389 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND FORWARD PIT FLOOR SUPPORT AT BS 389 HAS TWO EACH CRACKS. REMOVED, WEILDED AND REINSTALLED FLOOR SUPPORT IAW EA 1 2-5321-29-C1362 AND DC9 SRM 51-10-03, 51-30-2. 2 L 7 2 4F A6WE 1999121100756 19991211 00756 WP 1999 12 11 AT9900843 1 19991111 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 870 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND FLOORBEAM CHAFED 8 INCH AREA AT BS 870 BETWEEN LBL 5 - LBL 15, CHAFED AREA OUT OF LIMITS. FABRICATED AND INSTALLE D REPAIR ANGLE AND STAINLESS STEEL WRAP STRIP IAW DC9 SRM 53-05 FIGURE 20A. 2 L 7 2 4F A6WE 1999121100757 19991211 00757 WP 1999 12 11 AT9900845 1 19991026 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND UPPER SKIN LOOSE AND CORROSION ALONG AFT EDGE OF FLOOR PANEL NR 4695. REMOVED, FABRICATED AND INSTALLED UPPER SKI N AND HAT SECTIONS IAW DC9 SRM 53-01, 51-10-31, 53-21-0, 51-30-3, DC9 MM 25-11-0. 2 L 7 2 4F A6WE 1999121100758 19991211 00758 WP 1999 12 11 AT9900847 1 19991105 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 908 - 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND RIGHT HAND AFT CABIN AT BS 908-965 RBL 50, FLOOR SUPPORT WEB WAS CRACKED AND CORRODED. REMOVED CORROSION, STOP DR ILLED CRACK, FABRICATED, INSTALLED REPAIR IAW DC9 SRM 53-01, 51-10-3, 51-30-1. 2 L 7 2 4F A6WE 1999121100759 19991211 00759 WP 1999 12 11 AT9900848 1 19991121 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 688 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND RIGHT HAND MAIN FRAME AT FRAME NR 718 HAD 2 CRACKS. REMOVED AND REPLACED RIGHT HAND MAIN FRAME AT BS 699 IAW DC9 SRM 51-30-2, 51-30-5, EO 1253-11-29-B1044. 2 L 7 2 4F A6WE 1999121100760 19991211 00760 WP 1999 12 11 AT9900849 1 19991121 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 737 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND LEFT HAND MAIN FRAME NR 737 HAD 2 CRACKS. REMOVED AND REPLACED LEFT HAND MAIN FRAME NR 737 IAW DC9 SRM 51-30-2, 5 1-30-5 AND EO 1253-1129-B1044. 2 L 7 2 4F A6WE 1999121100761 19991211 00761 WP 1999 12 11 AT9900850 1 19991112 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND RIGHT HAND FRAME AT BS 699 HAD 4 CRACKS. REMOVED AND REPLACED RIGHT HAND MAIN FRAME AT BS 699 IAW DC9 SRM 51-30-2 , 51-30-5 AND EO 1253-1129-B1044. 2 L 7 2 4F A6WE 1999121100762 19991211 00762 WP 1999 12 11 AT9900851 1 19991028 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND LEFT HAND MAIN FRAME AT BS 699 HAD 3 CRACKS. REMOVED AND REPLACED LEFT HAND MAIN FRAME AT BS 699 IAW DC9 SRM 51-3 0-2, 51-30-5 AND EO 1253-1129-B1044. 2 L 7 2 4F A6WE 1999121100763 19991211 00763 WP 1999 12 11 AT9900852 1 19991028 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 915 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND FLOORBEAM CHAFED AT BS 915. BLENDED AND FABRICATED REPAIR ANGLE AND FILLERS, TREATED, PRIMED, INSTALLED REPAIR IA W DC9 SRM 53-01 FIGURE 1, 51-30-1, 53-05 FIGURE 20A, 51-10-3, 51-30-5. 2 L 7 2 4F A6WE 1999121100764 19991211 00764 WP 1999 12 11 AT9900853 1 19991101 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 160 - 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND FLOOR PANEL NR 4692A WAS CORRODED. GAINED ACCESS, REMOVED HAT SECTIONS, FABRICATED NEW FLOOR PANEL, TREATED, PRIM ED INSTALLED HAT SECTIONS AND PANEL IAW DC9 SRM 51-30-2, 57-10-2, 51-10-3, 51-70-2 AND DC9 MM 53-20-1. 2 L 7 2 4F A6WE 1999121100765 19991211 00765 WP 1999 12 11 AT9900854 1 19991103 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 887 - 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 838AT 47442 FOUND FLOOR PANEL CRACKED (HAT SECTION) AND CORRODED AROUND SCREW HOLE. FABRICATED PANEL REPAIR, FABRICATED 5 REPAIR HA T SECTIONS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED REPAIR AND HAT SECTIONS IAW DC9 SRM 51-10-4, 51-10-3, 51-3 0-2, AND DC9 MM 25-11-0. 2 L 7 2 4F A6WE 1999121100766 19991211 00766 WP 1999 12 11 ATT9900855 1 19991124 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 809AT 47322 EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK POWER SUPPLY. 2 L 7 2 4F A6WE 1999121100767 19991211 00767 1999 12 11 LR7A9967 2 19991205 A 7530 321372221 VALVE LKHEED 382 382G 526414U SO NR 2 ENGINE LEAKING A LR7A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 AL 03 403LC 3068 4590 EN ROUTE BJX, NR 2 NACELLE OVERHEAT WARNING ILLUMINATED. SHUTDOWN NR 2 ENGINE IAW LYNDEN PROCEDURES. FOUND NR 2 BLEED AIR REGULATING VALVE LEAKING. CHANGED VALVE IAW MM 36-10-20B. LEAK CHECK AND OPS CHECK NORMAL. PERFORMED LEAK CHECK ON ENGINE PNEUMATIC DUCTING AND NO LEAKS NOTED. 2 H 7 4 4T A1SO 1999121100768 19991211 00768 NM 1999 12 11 AWXA9900449 1 19991206 A 2824 6563 VALVE BOEING 737 7372E3 NM NR 1 ENGINE FAILED A AWXA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 28 138AW 37288 15953 22792 NR 1 ENG START SEQUENCE NORMAL THROUGH IDLE, AFTER SEVERAL SECONDS FF SURGED AND ENGINE FLAMED OUT. FOUND NR 1 SPAR VAL VE MOTOR NOT OPENING VALVE. REPLACED VALVE AND ACTUATOR LK AND OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999121100769 19991211 00769 NM 1999 12 11 AWXA9900450 1 19991206 A 3350 831136 LIGHT BOEING 737 737112 1384412 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 EMERGENCY EXIT FLOOR LIGHT ON END OF SEAT 3C, ONE WIRE BROKEN. REPLACED LIGHT ASSY, OPS CK GOOD. 2 L 7 2 4F A16WE 1999121100770 19991211 00770 NM 1999 12 11 AWXA9900451 1 19991206 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM BS 787 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 STA 787 LOWER SKIN BL 0 CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA IAW SRM 53-00-01, FABRICATED REPAIR DOUBLER FRM 20 24-T3 .071 R700681, ALODINED AND PRIMED PER SRM 53-00-01, INSTALLED PART PER SRM, 51-40-01. 2 L 7 2 4F RT A16WE 1999121100771 19991211 00771 NM 1999 12 11 AWXA9900452 1 19991206 A 5330 6545877 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 154AW 23776 HFEC INSP DETECTED CRACK APPROX 1 INCH LENGTH AT LOWER AFT CORNER OF THE FWD SERVICE DOOR CUTOUT. ALSO, MIDDLE LAYER CR ACKED. TRIMMED SKIN AS REQUIRED TO ELIMINATE CRACK IN THE OUTER AND MIDDLE LAYERS, VERIFIED DAMAGED AREA, REMOVED, INS TALLED CONICAL REP WASHERS PER SRM 53-10-01. FABRICATED FILLER FROM 2024T3 .100 R641191 FILL FROM T3 .071, .160, AND .100. TREATED AND PRIMED PER SRM 51-20-01. INSTALLED PART PER SRM 53-10-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 1999121100772 19991211 00772 NM 1999 12 11 AWXA9900453 1 19991206 A 5310 143N1009 FRAME BOEING 757 7572S7 1384962 NM BS 600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 FRAME CRACKED IN UPPER FLANGE OF FWD CARGO DOOR CUTOUT FS 600 BETWEEN STR 24L AND 26 L. REMOVED DAMAGED SECTION OF FRAM E IAW SRM 53-00-07 FIG 201, FABRICATED REPLACEMENT FRAME SECTION AND SPLICE CHANN EL IAW SRM 53-00-07 FIG 201. INSTALLED REPLACEMENT FRAME SECTION AND INSTALLED REPLACEMENT PART IAW 53-00-07. 2 L 7 2 4F RT A2NM 1999121100773 19991211 00773 NM 1999 12 11 AWXA9900454 1 19991206 A 5311 14N1008 FRAME BOEING 757 7572S7 1384962 NM BS 1340 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 STA 1340 STR 23R JUST BELOW FACTORY SPLICE, FRAME DENTED AND CRACKED. CUT OUT DAMAGED AREA AT STA 1340 BETWEEN 23-24 R PER SRM 53-00-07 FIG 201. ALODINED AND PRIMED CUTOUT IAW SRM 51-20-01 AND AMM 51-21. INSULATION AND PANEL INSTALLED PE R 20-12-00. 2 L 7 2 4F RT A2NM 1999121100774 19991211 00774 WP 1999 12 11 CALA9901559 1 19991206 A 3234 GEAR HANDLE DOUG DC10 DC1030 3023501 WP COCKPIT BINDING A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 37078 46926 WHEN THE LANDING GEAR WAS EXTENDED ON APPROACH TO EWR, NO GREEN GEAR SAFE LIGHTS ILLUMINATED. THE GEAR WAS CYCLED THREE TIMES BEFORE RECEIVING GREEN DOWN AND LOCKED INDICATIONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED BITE ON PROX BOX AND ALL GEAR AND INTEGRITY TESTS PASSED. THE GEAR HANDLE ASSEMBLY WAS CLEANED AND LUBRICATED WITH NO OTHER DEFECTS NOTED. 2 L 7 3 4F A22WE 1999121100775 19991211 00775 WP 1999 12 11 CALA9901560 1 19991206 A 5350 FAIRING DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14090 46553 INSPECTION FOUND A 1 INCH CRACK IN LT WING I/B FLAP FAIRING O/B SIDE PANEL 549AL. A REPAIR WAS INSTALLED IAW SRM 57-00- 01. 2 L 7 3 4F A22WE 1999121100776 19991211 00776 WP 1999 12 11 CALA9901561 1 19991206 A 5730 SKIN DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14090 46553 INSPECTION FOUND A 2 INCH CRACK AND DELAMINATION IN RT WING I/B FLAP VANE T/E SKIN. THE VANE WAS REMOVED AND REPLACED I AW MM 27-50-00. 2 L 7 3 4F A22WE 1999121100777 19991211 00777 WP 1999 12 11 CALA9901562 1 19991206 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 370 - 427 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR JAMB LOWER SECTION OF SKIN CORRODED FROM STA 370-427. THE DOOR JAMB PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 53-05, FIGURE 44, 51-10-01, 51-10-02, AND 51-10-04. 2 L 7 2 4F A6WE 1999121100778 19991211 00778 WP 1999 12 11 CALA9901563 1 19991206 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1850 - 1890 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND LAV SUPPORTS CORRODED AT STA 1860-1887, RBL 47 AND AT STA 1850-1890, LBL 47. THE SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999121100779 19991211 00779 WP 1999 12 11 CALA9901564 1 19991207 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP BS 1079 - 1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 1079-1309. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999121100780 19991211 00780 WP 1999 12 11 CALA9901565 1 19991207 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 237 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND A .5 INCH CRACK AT LOWER FASTENER HOLE OF LONGERON 17L AT STA 237. A NEW SECTION OF LONGERON WAS INSTA LLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1999121100781 19991211 00781 WP 1999 12 11 CALA9901566 1 19991207 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 222 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN NEAR FORWARD LAV ON LT SIDE AT STA 222. REPAIRED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1999121100782 19991211 00782 WP 1999 12 11 CALA9901567 1 19991207 A 5320 ANGLE DOUG DC9 DC982 3022082 WP CARGO BAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND A 6 INCH CRACK IN MID CARGO COMPARTMENT FORWARD FALSE BULKHEAD FRAME LOWER PANEL SUPPORT ANGLE. THE AN GLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 2 4F A6WE 1999121100783 19991211 00783 WP 1999 12 11 CALA9901568 1 19991207 A 5532 PANEL DOUG DC10 DC1030 3023501 WP VERTICAL STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14090 46553 INSPECTION FOUND VERTICAL STABILIZER LOWER REAR CENTER PANEL DELAMINATED. A REPAIR WAS INSTALLED IAW ECRA 5533-01002. 2 L 7 3 4F A22WE 1999121100784 19991211 00784 EA 1999 12 11 COMA9960745 1 19991205 A 7931 INDICATOR CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 940CA 7048 AFTER T/O, NR 2 ENGINE OIL PRESSURE ROSE TO 130 PSI, STAYED THERE FOR 10 SECONDS THEN DROPPED TO 55 PSI. ALL OTHER ENGI NE PARAMETERS WERE NORMAL. BAGGED DRAINS, AGB PAD PLUGS, EXAMINED OIL QUANTITY AT TANK, PERFORMED VARIOUS POWER SETTING GROUND RUNS. COULD NOT ACHIEVE EXCESSIVE OIL PRESSURE AT ANYTIME. MAINTENANCE IAW AMM-00-00-710-812/868-809/710-810/7 90-801/710-802/710-808. 2 L 7 2 4F RT A21EA 1999121100785 19991211 00785 EA 1999 12 11 COMA9960746 1 19991205 A 2760 SPOILER CNDAIR CL600 CL6002B19 EA WING MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 967CA 7134 ABORTED T/O FOR SPOILER CON FIG MSG WHITE SPOLER FAULT STATUS MSG. RESET SPOILERS AND PERFORMED REJECTED T/O INSP. 2 L 7 2 4F RT A21EA 1999121100786 19991211 00786 EA 1999 12 11 COMA9960747 1 19991204 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA ROWS 2C - 5C INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779CA 7306 EMERGENCY FLOOR LIGHTS AT ROWS 2C-5C AND 8A WERE INOPERABLE. REPLACED FLOOR LIGHT STRIP. 2 L 7 2 4F RT A21EA 1999121100787 19991211 00787 NM 1999 12 11 QXEA9902535 1 19991205 A 2611 734386B SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 353PH 2213 496 PDX- EN ROUTE FROM EUG TO SEA, SMOKE WARNING LIGHT FLASHED THREE TO FOUR TIMES THEN WENT OUT. THIS OCCURED TWO SEPARATE TIMES. FLIGHT THEN DIVERTED TO PDX. LANDED WITHOUT INCIDENT. MX INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REMOVED AND REPLACED BOTH FWD AND AFT CARGO PIT SMOKE DETECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NUMBER TWO SMOKE DETECTOR SERIAL NUMBER 0936. TIME SINCE REPAIR 545 HOURS, 761 CYCLES. 2 H 7 2 4T RT A13NM 1999121100788 19991211 00788 NM 1999 12 11 99FDEA00498 1 19991204 A 2420 GENERATOR BOEING 727 727227 1384078 NM AC SYSTEM INOP A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 485FE 21488 DURING CLIMB LOST NR 1 GEN AND BUS ACCOMPLISHED ELECTRICAL SYS MALFUNCTION CKLIST AND GENERATOR FIELD/GENERATOR BREAKER TRIP CK LIST AND CSD DISC. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT AND VOLTAGE REGULATOR. REMOVED AND REPLACE D NR 2 VOLTAGE REGULATOR, ALL CK GOOD. 2 L 7 3 4F A3WE 1999121100789 19991211 00789 WP 1999 12 11 ABXA9900817 1 19991206 A 5320 59101577N PAN DOUG DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 DURING C-CHECK, FOUND OUTER DOOR PAN CRACKED. REPAIRED DOOR PAN IAW ABX REA D952-34585. 2 L 7 2 4F A6WE 1999121100790 19991211 00790 WP 1999 12 11 ABXA9900818 1 19991026 A 5230 49123171 ROD DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR LOCK ROD FLANGE CRACKED. REPAIRED LOCK ROD IAW DC9 MM 52-30-1. 2 L 7 2 4F A6WE 1999121100791 19991211 00791 WP 1999 12 11 ABXA9900819 1 19991028 A 5320 99222951 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 889 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING CRACKED, LEFT SIDE AT STATION 889. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999121100792 19991211 00792 WP 1999 12 11 ABXA9900820 1 19991022 A 5313 591142517 LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 982 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LONGERON 30 CRACKED AT STATION 982. REPAIRED IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999121100793 19991211 00793 WP 1999 12 11 ABXA9900821 1 19991012 A 5320 99577397 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1021, LONGERON 15 AND 16 RIGHT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30 -2. 2 L 7 2 4F A6WE 1999121100794 19991211 00794 WP 1999 12 11 ABXA9900822 1 19991012 A 5313 S27779224 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 1041. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1999121100795 19991211 00795 WP 1999 12 11 MWEA99867 1 19991205 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 DURING TEN MINUTE TEST EMERGENCY LIGHTS, LAST 3 CEILING IN CABIN, AFT ATTENDANT OVERHEAD AND LEFT/RIGHT VENTRAL STAIR, W ERE DIM. MAINTENANCE REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1999121100796 19991211 00796 WP 1999 12 11 MWEA99868 1 19991205 A 5230 3926046501 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 TEE FITTING ON FORWARD CARGO DOOR AT LOWER AFT STOP PAD SUPPORT WAS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW TEE F ITTING. 2 L 7 2 4F A6WE 1999121100797 19991211 00797 1999 12 11 MWEA99869 4 19991205 A 2565 113377 SLIDE DOUG DC9 DC932 3022066 WP SERVICE DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE CAME OFF DOOR. MAINTENANCE REINSTALLED SLIDE AND COVER. 2 L 7 2 4F A6WE 1999121100798 19991211 00798 1999 12 11 MWEA99870 4 19991206 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP CABIN DEPLOYED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47794 CATERING INADVERTENTLY OPENED GALLEY DOOR BEFORE DISCONNECTING THE SLIDE, PULLING SLIDE AND SLIDE COVER PARTIALLY OUT. M TC REINSTALLED SLIDE AND SLIDE COVER. 2 L 7 2 4F A6WE 1999121100799 19991211 00799 WP 1999 12 11 MWEA99871 1 19991206 A 5520 5910413504 TAB DOUG DC9 DC932 3022066 WP ELEVATOR DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 BOTTOM SIDE OF RIGHT ELEVATOR CONTROL TAB HAD AREA OF DELAMINATION. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER . 2 L 7 2 4F A6WE 1999121100800 19991211 00800 NM 1999 12 11 SCNA99149 1 19991201 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE LOWER AFT LIGHT IN THE EMERGENCY LIGHT ASSEMBLY OVER THE L2 AND R2 DOOR WERE INOPER ATIVE. MAINTENANCE RELAMPED THE EMERGENCY LIGHT ASSEMBLY OVER L2 AND R2 DOOR PER MM 335001. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999121100801 19991211 00801 WP 1999 12 11 RRXA991587 1 19991125 A 3260 SWITCH DOUG DC8 DC873F 302199F WP MLG MALFUNCTIONED A RRXA O OTHER N FALSE WARNING AP APPROACH 1 WP 15 791FT 46045 LM GEAR DOWN (GREEN) LIGHT WILL NOT ILLUMINATE GEAR WARNING (RED) LIGHTS NORMAL RECYCLED GEAR. NO HELP LIGHT CAME ON DU RING FINAL APPROACH. REMOVED AND REPLACED LT MAIN LANDING GEAR SWITCH OP'S CHECK NORMAL ON GROUND AS PER MM 32-60-00. 2 L 7 4 4F RT 4A25 1999121100802 19991211 00802 WP 1999 12 11 RRXA991588 1 19991128 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 ON WALKAROUND, FOUND CORROSION HOLE ON LOWER BELLY AFT OF ADF ANTENNA LT SIDE. ACFT PREPARED FOR FERRY FLIGHT. THIS A CFT INSPECTED AND FOUND IT SAFE FOR THE FLIGHT INTENDED. 2 L 7 4 4F RT 4A25 1999121100803 19991211 00803 WP 1999 12 11 RRXA991589 1 19991204 A 2612 D5025D5030D502 FIRE DETECTOR DOUG DC8 DC863 302198A WP NR 4 ENGINE MALFUNCTIONED A RRXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 796AL 46054 HAD FIRE WARNING NR 4 ENGINE WHEN SETTING CLIMB POWER. COMPLETED QRH EMERG FIRE PROCEDURE. FIRED INBOARD AGENT. ATTEM PTED TO FIRE OUTBOARD BUT NO INDICATION OF DISCHARGE NR 3 LIGHT TESTS, NR 4 LIGHT NO-TEST. REMOVED AND REPLACED NR 4 EN GINE AFT UPPER, FORWARD UPPER, AND LOWER FIRE SENSING ELEMENTS. ALSO, REPAIRED BROKEN WIRE ON AT CONNECTOR OF LOW PRESS URE SWITCH. REPLACED BOTH INBOARD AND OUTBOARD FIRE BOTTLES. 2 L 7 4 4F 4A25 1999121100804 19991211 00804 1999 12 11 RAIA9912006 4 19991206 A 3445 6229614003 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU TCAS FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 926AE 23918 1582 926 FAT- BOTH TRANSPONDERS FAILED, REPORTED BY ATC. MAINTENANCE REPLACED TCAS CONTROL. 2 L 7 2 4T RT A56EU 1999121100805 19991211 00805 EU 1999 12 11 RAIA9912007 1 19991206 A 3040 ANN50 FUSE JETAIR JETSTM JETSTM4101 1500501 EU WINDSHIELD HEAT FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 568HK 41086 JFK- LEFT OUTBOARD WINDSHIELD HEAT INOP. MAINTENANCE REPLACED FUSE FOR LEFT OUTBOARD WINDSHIELD. 2 L 7 2 4T RT A41NM 1999121100806 19991211 00806 NM 1999 12 11 HNAA9900158 1 19991118 A 3350 DHAV DHC8 DHC8201 2809001 NM UNKNOWN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 998HA 509 PAX DOOR OVERHEAD EXIT LIGHT AND LT FWD EXTERIOR EGRESS LIGHT INOP. REMOVED AND REPLACED BASE ASSY AND POWER SUPPLY 335 1-PS1 NO FIX. FOUND PIN PUSHED BACK ON CONNECTOR TO BASE ASSY. RE-SEATED PIN SECURED CANNON PLUG OPS NORMAL. 2 H 7 2 4T RT A13NM 1999121100807 19991211 00807 NM 1999 12 11 HNAA9900159 1 19991116 A 3350 DHAV DHC8 DHC8102 2809003 NM UNKNOWN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 984HA 377 AFT INTERIOR EMERGENCY LIGHTS INTERMITTENT. REPLACED EMERGENCY LIGHTS BATTERIES, POSITION 5/6 (PS3 AND PS4). OPS. CHEC K GOOD. 2 H 7 2 4T RT A13NM 1999121100808 19991211 00808 WP 1999 12 11 AT9900755 1 19990917 A 5315 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 200-238 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND PANEL SUPPORT AT BS 200-238, LBL 13 CORRODED OUT OF LIMITS. REMOVED AND FABRICATED REPAIR SECTION ON SUPPORT. AL ODINED AND PRIMED REPAIR. INSTALLED REPAIR SECTION IAW DC9 SRM 51-30-2, 51-10-3, 53-01 FIGURE 2. 2 L 7 2 4F A6WE 1999121100809 19991211 00809 WP 1999 12 11 AT9900775 1 19990806 A 5321 WEB DOUG DC9 DC932 3022066 WP BS 955-960 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND 4 CRACK AT BS 955-960, LBL 48-52 IN CUSP WEB AND CORROSION OUT OF LIMITS. FABRICATED REPAIR IAW DC9 SRM 53-05 FIG URE 97, 51-10-3, 51-30-1, 51-30-2, AND DC9 MM 53-20-1. 2 L 7 2 4F A6WE 1999121100810 19991211 00810 WP 1999 12 11 AT9900776 1 19990729 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 936-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND CUSP WEB AT BS 945-965 WITH EXFOLIATED CORROSION. FABRICATED REPAIR WEB IAW DC9 SRM 53-05 FIGURE 97, 51-10-3, 51- 30-1, 51-30-2, AND DC9 MM 53-20-1. 2 L 7 2 4F A6WE 1999121100811 19991211 00811 WP 1999 12 11 AT9900777 1 19990724 A 5330 591141899N SKIN&LONGERON DOUG DC9 DC932 3022066 WP BS 658-756 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 LOWER KEEL BEAM SKIN AT BS 658-756 HAS A BULDGING AREA OF CORROSION THAT HAS PUSHED OUT AND CRACKED THE SKIN. REMOVED C ORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED SKIN AT BS 658-756 AND LONGERON AT 29L AND 29R IAW DC9 SRM 53-04 FIGUR E 42, 52-05 FIGURE 48, 51-30-1, 51-30-2. 2 L 7 2 4F A6WE 1999121100812 19991211 00812 WP 1999 12 11 AT9900796 1 19990929 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 340 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND MILLED DOUBLERS CORRODED BEYOND LIMITS AT BS 340 LONGERON 30. REMOVED AND REPLACED WITH NEW DOUBLERS IAW DC9 SRM 51-10-3, 51-30-1, 51-30-2. 2 L 7 2 4F A6WE 1999121100813 19991211 00813 WP 1999 12 11 AT9900797 1 19990922 A 5330 FUSELAGE SKIN DOUG DC9 DC932 3022066 WP BS 299-408 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 835AT 47534 FOUND RIGHT FUSELAGE SKIN DENTED OUT OF LIMITS AT BS 229-408. REMOVED AND REPLACED SKIN PANEL AT BS 229-408, LONG 18-26 IAW DC9 SRM 51-10-3, 51-10-2, 51-30-2, AND TIMCO EO 99-1258 APPROVED BY 8110-3. 2 L 7 2 4F A6WE 1999121100814 19991211 00814 WP 1999 12 11 AT9900800 1 19991108 A 3350 EMERGENCY LIGHTS DOUG DC9 DC932 3022066 WP OVERWING INTERMITTENT A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 815AT 47443 WITH EMERGENCY EXIT LIGHTS SELECTED OFF AND BATTERY SWITCH OFF. THE OVERWING EXIT LIGHTS REMAIN ILLUMINATED WITH SWITCH (BATT) ON ALL EMERGENCY EVAC LIGHTS ARE OUT/OFF. POWERED DOWN AIRCRAFT, THE REPOWERED EMERGENCY LIGHTS CHECKED NORMAL IAW DC9 MM 33-53. 2 L 7 2 4F A6WE 1999121100815 19991211 00815 WP 1999 12 11 AT9900801 1 19991108 A 5270 WSP0299509 HANDLE DOUG DC9 DC932 3022066 WP TAIL CONE UNSERVICEABLE A ZZDA K NONE O OTHER LD LANDING 1 SO 15 831AT 47674 TAILCONE UNSAFE LIGHT ON AFTER LANDING ROLL. RECONNECTED EXTERIOR HANDLE LINKAGE AND PERFORMED TAIL CONE DROP CHECK IAW DC9 MM 53-50-3. 2 L 7 2 4F A6WE 1999121100816 19991211 00816 WP 1999 12 11 AT9900802 1 19991108 A 3350 5224280104 BATTERY DOUG DC9 DC932 3022066 WP FWD CABIN DISCHARGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 848AT 47559 EMERGENCY EVACUATION LIGHTS IN COCKPIT AND FORWARD PASSENGER CABIN INOPERATIVE. REMOVED AND REPLACED BATTERY IAW DC9 MM 33-40. 2 L 7 2 4F A6WE 1999121100817 19991211 00817 WP 1999 12 11 AT9900804 1 19990718 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 218-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND RIGHT INBOARD SEAT TRACK AT BS 218-965 WITH NICKS, SCRATCHES AND CORROSION. REPLACED SEAT TRACK IAW DC9 SRM 53-05 FIGURE 4, 51-30-2, 51-10-3. 2 L 7 2 4F A6WE 1999121100818 19991211 00818 WP 1999 12 11 AT9900805 1 19990725 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 870-955 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 803AT 47261 FOUND AFT PIT LONGERON AT BS 870-965 CORRODED. INSTALLED LONGERON REPAIR BETWEEN BS 870-955 IAW DC9 SRM 53-03 FIGURE 2A , 51-10-2, 51-10-4, 51-30-2, 51-70-2, 53-02 FIGURE 14. 2 L 7 2 4F A6WE 1999121100819 19991211 00819 WP 1999 12 11 AT9900806 1 19991108 A 5311 99196182R FRAME DOUG DC9 DC932 3022066 WP BS 718 RIGHT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK OUT OF LIMITS IN MAIN FRAME AT BS 718 RIGHT. REMOVE D AND REPLACED MAIN FRAME AT BS 718 RIGHT IAW DC9 SB 53-131. 2 L 7 2 4F A6WE 1999121100820 19991211 00820 WP 1999 12 11 AT9900807 1 19991108 A 5311 99196482R FRAME DOUG DC9 DC932 3022066 WP BS 718 LEFT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK OUT OF LIMITS IN MAIN FRAME AT BS 718 LEFT. REMOVED AND REPLACED MAIN FRAME AT BS 718 LEFT IAW DC9 SB 53-131. 2 L 7 2 4F A6WE 1999121100821 19991211 00821 WP 1999 12 11 AT9900808 1 19991102 A 5320 1A538421 DOUBLER DOUG DC9 DC932 3022066 WP BS 718 LEFT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND UPPER PRESSURE WEB DOUBLER AT BS 718 LEFT CORRODED BEYOND LIMITS. REMOVED, FORMED, AND INSTALLED NEW DOUBLER AT BS 718 LEFT IAW DC9 SRM 53-01 FIG 1, 51-10-02, 51-10-02A, 51-10-0 3, AND 51-10-04. 2 L 7 2 4F A6WE 1999121100822 19991211 00822 WP 1999 12 11 AT9900809 1 19991027 A 5320 CUSP WEB DOUG DC9 DC932 3022066 WP BS 238 RIGHT CORRODED/CRACK A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CUSP WEB AT BS 238 RIGHT TO BE CORRODED AND CRACKED. REMO VED DAMAGED AREA FABRICATED REPAIR AND INSTALLED DOUBLER IAW DC9 SRM 53-01 FIG 4, 51-10-03, AND 51-30-02. 2 L 7 2 4F A6WE 1999121100823 19991211 00823 WP 1999 12 11 AT9900810 1 19991012 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP XRS 387-400 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON RIGHT WING AFT SPAR UPPER CAP AT XRS 387-400. FABRICATED AND INSTALLED REPAIR STRAP AT XRS 387-400 IAW DC9 SRM 57-09 FIG 12, 51-10-03, 51-30, AND EO 99-1344. 2 L 7 2 4F A6WE 1999121100824 19991211 00824 WP 1999 12 11 AT9900811 1 19991104 A 5320 DOUBLER/LONGERON DOUG DC9 DC932 3022066 WP BS 230 LONG 21 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK AT BS 230 LONGERON 21 LEFT. FABRICATED AND INSTALLE D FILLER, DOUBLER, AND LONGERON SPLICE IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30, 51-30-02, 51-30-05, 25-52, AND E O 99-1335. 2 L 7 2 4F A6WE 1999121100825 19991211 00825 WP 1999 12 11 AT9900812 1 19991111 A 5610 WINDOW FRAME DOUG DC9 DC932 3022066 WP PILOT'S WINDOW GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND GOUGES IN PILOT'S SLIDING WINDOW FRAME. BLENDED OUT GOUGE S IN PILOT'S SLIDING WINDOW FRAME IAW EO 991367. 2 L 7 2 4F A6WE 1999121100826 19991211 00826 WP 1999 12 11 AT9900813 1 19991105 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 227-408 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, THE RIGHT FUSELAGE SKIN HAD NUMEROUS DENTS AT BS 227-408. R EMOVED AND FABRICATED NEW SKIN IAW AT BS 227-408 EO 99-1328. 2 L 7 2 4F A6WE 1999121100827 19991211 00827 WP 1999 12 11 AT9900814 1 19991105 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 120-200 RIGHT CRACK A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 120-200 RIGHT. REMOVED AND REPAIRED CRACK AT BS 120-200 RIGHT IAW EO 99-1332. 2 L 7 2 4F A6WE 1999121100828 19991211 00828 WP 1999 12 11 AT9900815 1 19991105 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 323-380 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND CORROSION AT BS 323-380 AND AT STATIC PORT TO BE OUT OF LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER BS 323-380 IAW EO 99-1332 AND DC9 SRM 53-00. 2 L 7 2 4F A6WE 1999121100829 19991211 00829 WP 1999 12 11 AT9900816 1 19991106 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 617 RIGHT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FLORIDA, FOUND FRAME AT BS 617 RIGHT TO HAVE TEMPORARY REPAIR. REMO VED AND REPLACED FRAME AT BS 617 RIGHT IAW DC9 SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F A6WE 1999121100830 19991211 00830 SO 1999 12 11 LR7A9966 1 19991118 A 2612 3108KA161S CONNECTOR LKHEED 382 382G 526414U SO FS 500.5 CONTAMINATED A LR7A E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 AL 03 401LC 4606 EN ROUTE DLG TO ANC NR 2 ENGINE FIRE WARNING ILLUMINATED. SHUTDOWN NR 2 ENGINE IAW SHUTDOWN PROCEDURES AND DISCHARGED F IRE BOTTLE AT 0023Z AND 0053Z RESPECTIVELY. REPLACED P414 HORSCOLLAR CONNECTOR DUE SUSPECTED CONTAMINATION. REPLACED N ORMAL FIRE EXTINGUISHER AGENT BOTTLE AND SQUIB IAW SMP 581 26-20. REPLACED FIRE DETECTION CONTROL UNIT PRECAUTIONARY. 2 H 7 4 4T A1SO 1999121100831 19991211 00831 NM 1999 12 11 UPS99231125 1 19991117 A 5310 STRINGER BOEING 727 72725C 138400H NM 12-1 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION ON STRINGER BS 360 TO 380, STR 26L. REMOVED AND REPLACED STRINGER SEGMENT PER SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1999121100832 19991211 00832 NM 1999 12 11 UPS99231126 1 19991112 A 2710 AILERON BOEING 727 72725C 138400H NM 81-5 DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI LT O/B AILERON T/E WEDGE IS DELAMINATED AND SATURATED WITH OIL ON THE O/B AFT END. REMOVED A 1 HALF INCH AREA OF DELAMINATED SKIN AT O/B AFT CORNER UPPER AND LOWER SURFACES AND REMOVED CONTAMINATED POTTING COMPOUND. FAB RICATED REPAIR PLUGS AND INSTALLED WITH REPAIR PLUGS SANDED AND APPLIED FINISH COAT REBALANCE OF AILERON NOT REQUIRED. 2 L 7 3 4F A3WE 1999121100833 19991211 00833 NM 1999 12 11 UPS99231127 1 19991112 A 5310 7075T6 SUPPORT BOEING 727 72725C 138400H NM 13-1 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-111-01.00-02) ON SIDEWALL/BULKHEAD SUPPORT AT BS 680 LBL 31-45 WL 159-166. REMOVED SU PPORT AND REPLACED PER SRM. 2 L 7 3 4F A3WE 1999121100834 19991211 00834 NM 1999 12 11 UPS99231128 1 19991112 A 5310 7075T6 ANGLE BOEING 727 72725C 138400H NM 23-2 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) CORROSION ON AFT EDGE OF L-ANGLE AT BS 297, RBL 12-RBL 54, WL 208. REMO VED L-ANGLE AND REPLACED. 2 L 7 3 4F A3WE 1999121100835 19991211 00835 NM 1999 12 11 UPS99231129 1 19991112 A 5310 2024T3 L-ANGLE BOEING 727 72725C 138400H NM 23-2 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) CORROSION ON FLOOR STRUCTURE L-ANGLE AND WEB AT STA 298 RBL 13, WL 208. REMOVED DAMAGED AND REPAIRED PER SRM. 2 L 7 3 4F A3WE 1999121100836 19991211 00836 NM 1999 12 11 UPS99231130 1 19991112 A 5310 651822035 STRINGER BOEING 727 72725C 138400H NM 12-1 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STRINGER AT BS 360 TO BS 400 STR 27L. REMOVED CORRODED SECTION AND R EPLACED PER SRM. 2 L 7 3 4F A3WE 1999121100837 19991211 00837 NM 1999 12 11 UPS99231131 1 19991112 A 5740 FITTING BOEING 727 72725C 138400H NM 35-1 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI WHILE WORKING TASK CARD NR 1249 FOUND THE NR 4 FLAP TRACK FITTING THAT ATTACHES TO FWD LANDING GEAR T RUNION BEARING TO BE CORRODED. REPLACED FITTING PER SRM 51-30-4. 2 L 7 3 4F A3WE 1999121100838 19991211 00838 NM 1999 12 11 UPS99231132 1 19991112 A 5330 STIFFNER BOEING 727 72725C 138400H NM 31-1 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON SIDES OF E/E DOOR WARNING SWITCH COVER HOUSING. REPLACED STIFFENER B S 450-452 LBL 10 TO RBL 13 AND DOOR SWITCH HOUSING SAME BS LBL 2 TO RBL 6 PER 727 SRM 51-30-2, 51-20-1, 51-30-5, 51-20-1 51 AMD MM 52-40-11. 2 L 7 3 4F A3WE 1999121100839 19991211 00839 NM 1999 12 11 UPS99231133 1 19991027 A 5310 BEAM BOEING 727 72725C 138400H NM 24-2 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION ON UPPER FLANGE OF LONGITUDINAL BEAM BS 825 AND BS 845 LBL WL 208. REMOVED CORRODED UPPER FLANGE ON LONGITUDINAL BEAM. FABRICATED NEW UPPER BEAM AND INSTALL NEW REPLACEMENT PART AND SPLICE PER SRM 51-30-2, 51- 30-. 2 L 7 3 4F A3WE 1999121100840 19991211 00840 NM 1999 12 11 UPS99231134 1 19991022 A 5310 STIFFNER BOEING 727 72725C 138400H NM 35-1 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION AT TOP OF STA 870 STIFFENER AT LBL 25 WL 198. REMOVED CORRODED STIFFENER AT STA 870 FABRIC ATED NEW REPLACEMENT PART AND INSTALLED IAW SRM 51-30-2, 51-30-6. 2 L 7 3 4F A3WE 1999121100841 19991211 00841 NM 1999 12 11 UPS99231135 1 19991116 A 5310 65C1576443 BEAM BOEING 727 72725C 138400H NM 24-2 CRACK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CRACK IN VERTICAL BEAM AT BS 1183, LB 18.5, WL 275. REMOVED DAMAGE AND REPAIRED PER UPS EO B727-5310 -7267 APPX B. 2 L 7 3 4F A3WE 1999121100842 19991211 00842 NM 1999 12 11 UPS99231136 1 19991116 A 5310 7075T6 ANGLES BOEING 727 72725C 138400H NM 13-1 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:SI CORROSION (C53-111-01.03-02) ON FWD CARGO BAY CEILING BEAM AROUND 2 EACH FASTENER HOLES BS 580-BS 600 , BL 0, WL 200. REMOVED DAMAGE AND REPAIRED PER ERO 99-6278. 2 L 7 3 4F A3WE 1999121100843 19991211 00843 WP 1999 12 11 UPS99831124 1 19991112 A 5730 #4 PYLON DOUG DC8 DC871F 302199D WP R/W #4 PYLONG LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:SV FUEL LEAKING AT NR 4 PYLON AREA FROM FWD SPAR TO REAR SPAR, LOWER SURFACE OF WING. REMOVED I/B AND O /B SKATE ANGLES, T-DOUBLERS, L/E SKIN PANEL, INTERNAL FITTINGS LOCATED AT CANT BLKHDS STA 495 AND 508. INJECTED FRONT S PAR, CTR SPAR AND STRINGERS IAW DC8 51-1-12. REINSTALL I/B AND O/B SKATE ANGLES AND DRAG ANGLES AND LEADING EDGE SKIN D OUBLER AND T DOUBLER IAW DC 8 SRM 51-1-20D AND REO 06862 REV A. 2 L 7 4 4F RT 4A25 1999121100844 19991211 00844 EU 1999 12 11 QXEA9902342 1 19991111 A 5610 20412222451 RADAR INDICATOR GRIMES RADARINDICA FOKKER F28 F28MK4000 4990810 EU COCKPIT INOPERATIVE A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 486US 5007 1471 3683 11237 SEA - ELECTRICAL BURNING SMELL IN COCKPIT. NO VISABLE SMOKE. FOUND WEATHER RADAR CONTAMINATED WITH WATER. RESEALED W INDSHIELD POST AND REPLACED WEATHER INDICATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999121100845 19991211 00845 NM 1999 12 11 QXEA9902347 1 19991117 A 3350 10005511 EMERG EXIT LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - COCKPIT OVERHEAD EMERGENCY LIGHT DOES NOT TEST OR ILLUMINATE WHEN REMOVED. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999121100846 19991211 00846 WP 1999 12 11 ABXA9900801 1 19991110 A 5315 9922042505 FITTING DOUG DOUG DC9 DC932F 3022067 WP AFT LOWER CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT VERTICAL SUPPORT FITTING CRACKED AT STATION 794. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51 -30-5. 2 L 7 2 4F A6WE 1999121100847 19991211 00847 WP 1999 12 11 ABXA9900802 1 19991110 A 5315 99220422 FITTING DOUG DOUG DC9 DC932F 3022067 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND RIGHT VERTICAL SUPPORT FITTING CRACKED AT STATION 332. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 5 1-30-5. 2 L 7 2 4F A6WE 1999121100848 19991211 00848 WP 1999 12 11 ABXA9900803 1 19991110 A 5315 99220422 FITTING DOUG DOUG DC9 DC932F 3022067 WP AFT LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND RIGHT VERTICAL SUPPORT FITING CRACKED IN TWO PLACES AT STATION 832. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1999121100849 19991211 00849 WP 1999 12 11 ABXA9900804 1 19991110 A 5312 591016326 STIFFNER DOUG DOUG DC9 DC932F 3022067 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND AFT PRESSURE BULKHEAD, NR 2 RADIAL STIFFENER CRACKED. REPLACED STIFFENER IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999121100850 19991211 00850 WP 1999 12 11 MWEA99826 1 19991119 A 5280 59134213 SKIN DOUG DC9 DC981 3022081 WP NOSE LNDNG GEAR UNACCEPTABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 PREVIOUS REPAIR AT LEFT AFT NOSE LANDING GEAR DOOR AFT HINGE CUT OUT SKIN. MTC FABRICATED AND INSTALLED NEW DOUBLER REP AIR. 2 L 7 2 4F A6WE 1999121100851 19991211 00851 WP 1999 12 11 MWEA99827 1 19991119 A 5210 49157473 TUBE DOUG DC9 DC915 3022036 WP FWD CABIN CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 THE FORWARD SERVICE DOOR HOLD OPEN HOOK PUSH-PULL TUBE IS CHAFED. MAINTENANCE REMOVED AND REPLACED TUBE ASSEMBLY. 2 L 7 2 4F A6WE 1999121100852 19991211 00852 WP 1999 12 11 MWEA99828 1 19991119 A 5750 59121482 FLAP DOUG DC9 DC915 3022036 WP RIGHT WING DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 RIGHT FLAP OUTBOARD EDGE HAS A DEEP DENT. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999121100853 19991211 00853 WP 1999 12 11 MWEA99829 1 19991119 A 5240 591008427 WEB DOUG DC9 DC915 3022036 WP FWD CABIN MISDRILLED HOLES A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 GALLEY SERVICE DOOR HAS NUMEROUS MISDRILLED HOLES IN WEB. MTC FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 1999121100854 19991211 00854 WP 1999 12 11 MWEA99830 1 19991119 A 5750 3913194505 FITTING DOUG DC9 DC915 3022036 WP STATION XTE251 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 RIGHT WING TRAILING EDGE RIB AT STATION XTE 251 HAS A CRACKED FITTING. MAINTENANCE FABRICATED AND INSTALLED NEW FITTING . 2 L 7 2 4F A6WE 1999121100855 19991211 00855 WP 1999 12 11 MWEA99831 1 19991119 A 5240 991158133 FRAME DOUG DC9 DC915 3022036 WP FWD CABIN MISDRILLED HOLES A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 GALLEY SERVICE DOOR NR 3 FRAME HAS SEVERAL MISDRILLED HOLES. MAINTENANCE FABRICATED AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 1999121100856 19991211 00856 WP 1999 12 11 MWEA99832 1 19991119 A 5750 99194752 RIB DOUG DC9 DC915 3022036 WP RIGHT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 RIGHT WING TRAILING EDGE RIB IS CRACKED BETWEEN INBOARD AND OUTBOARD SPOILER PANELS. MAINTENANCE FABRICATED AND INSTALL ED NEW RIB. 2 L 7 2 4F A6WE 1999121100857 19991211 00857 WP 1999 12 11 MWEA99833 1 19991119 A 5230 59114111 SKIN DOUG DC9 DC915 3022036 WP FWD CARGO CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FUSELAGE SKIN IS CRACKED IN 2 PLACES AT FORWARD CARGO DOOR LOWER AFT CORNER. MAINTENANCE FABRICATED AND INSTALLED NEW D OUBLER. 2 L 7 2 4F A6WE 1999121100858 19991211 00858 WP 1999 12 11 MWEA99834 1 19991119 A 5240 5910084115 WEB DOUG DC9 DC915 3022036 WP FWD CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LOWER LEFT CORNER OF SERVICE DOOR IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED NEW WEB. 2 L 7 2 4F A6WE 1999121100859 19991211 00859 WP 1999 12 11 MWEA99835 1 19991119 A 5610 59529654 DOUBLER DOUG DC9 DC915 3022036 WP COCKPIT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 F/O'S AND CAPTIANS SLIDING WINDOW FRAME HAS CRACK ON INSIDE UPPER AFT CORNER. MAINTENANCE FABRICATED AND INSTALLED NEW DOUBLER AND RETAINER. 2 L 7 2 4F A6WE 1999121100860 19991211 00860 NM 1999 12 11 DL76G992517 1 19991113 A 5330 146T32311 SKIN BOEING 767 7673P6 1385105 NM FS1425, S-34&35L GOUGED/DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 153DL 24985 FUSELAGE SKIN FS 1425, STRG 34L-35L, DENT/GOUGE REPAIR. THE FUSELAGE SKIN WAS DENTED AND GOUGED AT FS 1425 OVER STRINGE RS 34L AND 35L BY GROUND EQUIPMENT. THERE WAS NO DAMAGE TO THE UNDERLYING STRUCTURE. THE SKIN DAMAGE WAS REMOVED WI TH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 368748-14. 2 L 7 2 4F RT A1NM 1999121100861 19991211 00861 NM 1999 12 11 DL76L992519 1 19991113 A 5330 143T3321 SKIN BOEING 767 767332 1382001 NM FS 654, S-26L CREASED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 FUSELAGE SKIN FS 654, STRINGER 25L-26L, CREASE REPAIR. THE FUSELAGE SKIN WAS FOUND WITH A DEEP CREASE JUST ABOVE THE ST RINGER 26L LAP JOINT AT FS 654. THE DAMAGED AREA WAS CUTOUT WITH A 13 LONG BY 1.1 HIGH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 368729-14. 2 L 7 2 4F RT A1NM 1999121100862 19991211 00862 1999 12 11 DL76K992520 4 19991112 A 3450 8221152002 BOEING 767 767332 1382001 NM FWD E AND E COMP FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 177DZ 117431 29698 TWENTY MINUTES INTO FLIGHT GOT CAPT LOC AND GS FLAGS ON ADI AND EICAS MSG LGPS WITH C/B 10E MMR POPPED. RESET C/B ONCE PER MTC COORD SUGGESTION. C/B POPPED AGAIN. COULD SMELL SLIGHT ELEC ODOR BRIEFLY. CAPT OPERATED IN ALTNEFI. ALSO, NO LAND NR ON ASA AND NO ILS IDENT. FWD TO MCO AND PLAC PER MEL 34-60-03. NO SOURCE OF ODOR NOTED SUSPECT MMR P/N 341002 525 NASI MIA. 2 L 7 2 4F RT A1NM 1999121100863 19991211 00863 NM 1999 12 11 DL72E992521 1 19991105 A 5754 ATTACH BOLT BOEING 727 727247 138408F NM #5 L/E SLAT CRACKS A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 AT HMV2, FOUND NR 5 L/E SLAT 2 CRACKS AT FENCE ATTACH BOLT HOLES AT L/E. MFR REPAIR DOUBLER PER MM 57-54-0 FIG 813, REP AIRED PER SAME. 2 L 7 3 4F A3WE 1999121100864 19991211 00864 NM 1999 12 11 DL73E992522 1 19991115 A 2780 NBR 2 SLAT BOEING 737 737247 138448D NM NBR 2 SLAT DAMAGED A DALA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SO 27 244WA 23518 ON T/O FROM MSY, GOT NR 2 L/E SLAT LIGHT ON. CREW REPORTED SLAT HANGING OUT. OFF LANDED IN JAN. FOUND SLAT MOUNTS BRO KEN. REPLACED SLAT ASSY, REPAIRED SHEET METAL DAMAGE TO AIRCRAFT. 2 L 7 2 4F A16WE 1999121100865 19991211 00865 NE 1999 12 11 DL72W992523 2 19991115 A 7230 ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE #1 ENGINE DAMAGED A DALA K NONE T ENGINE CASE PENETRATION IN INSP/MAINT 1 SO 27 295WA 55735 22532 700016 FOUND PIECE OF METAL IN BOTTOM OF COWL. FOUND 4-6 INCH HOLE IN OUTER CASE APPROX 4 FT AFT OF NOSE COWL ATTACH FLANGE. R EPLACED NR 1 ENG. 2 L 7 3 4F 4 F A3WE E2EA 1999121100866 19991211 00866 NM 1999 12 11 DL72E992524 1 19991102 A 5754 RIB BOEING 727 727247 138408F NM #3 L/E SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 AT HMV2, FOUND DOUBLER CRACKED ON RIB LOC I/B SIDE OF ACTUATOR FITTING ON NR 3 L/E SLAT. STOP DRILLED CRACK PER MM 57-5 4-0. FABRICATED DOUBLER, FOUND SECOND RIB CRACK, DRILLED SECOND RIB, FABRICATED ANOTHER DOUBLER, CUT AND REMOVED RIBS. INSTALLED DOUBLERS PER 51-40-3 AND 57-54-0 FIG 804. CPONTN N/R 1086, REPAIRED RIB/SKIN SPLICE PER MM 57-54-0 FIG 804, 8 01, SRM 51-40-3. 2 L 7 3 4F A3WE 1999121100867 19991211 00867 NM 1999 12 11 DLM88992525 1 19991115 A 4910 6054578 DOUG MD88 MD88 3023688 NM AFT FAN SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 909DE 718956 53418 ATL WORKING APU INOP FROM BURNING SMELL IN CABIN AT BTR. REF LOG C042035 ITEM 002. WHILE WORKING WRITEUP, FOUND AFT RE CIRCULATION FAN BEARINGS GONE AND FAN SEIZED. SMELL CAME FROM FAN AT LIFTOFF IN BTR. AIR TURNBACK BTR. REPLACED FAN. 2 L 7 2 4F RT A6WE 1999121100868 19991211 00868 NM 1999 12 11 DL733992528 1 19991115 A 5330 6545800 SKIN BOEING 737 7373B7 1384580 NM C-D WINDOW POST CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947WP 23376 FUSELAGE SKIN L1 COCKPIT WINDOW, C-D POST CRACK REPAIR. THE SKIN AT THE UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW (C- D POST) WAS FOUND WITH A .25 CRACK. THE UNDERLYING GUSSET WAS ALSO CRACKED. THE CRACKED AREA WAS TRIMMED OUT AND A STE EL REPAIR DOUBLER AND ALUMINUM REPAIR TRIPLER. INSTALLED TO REPAIR THE DAMAGE PER ER/A 368758-14, REV A. 2 L 7 2 4F RT A16WE 1999121100869 19991211 00869 NM 1999 12 11 DL72K992529 1 19991115 A 5330 SKIN BOEING 727 727232 1384082 NM FS 440, S-21R PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 FUSELAGE SKIN FS 440-460, STRG 20R-21R, CUTOUT REPAIR. THE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 440 AND 460 AND BETWE EN STRINGERS 20R AND 21R. THE SKIN SPLICE STRAP AT FS 440 WAS SEVERED. THE SKIN DAMAGE WAS REMOVED WITH A 12 BY 8 CUTO UT AND THE DAMAGED SECTION OF SPLICE STRAP WAS CUT OUT. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND THE SPLICE STRAP WAS REPAIRED WITH AN INTERNAL TITANIUM STRAP PER ER/A 368750-14. 2 L 7 3 4F A3WE 1999121100870 19991211 00870 NM 1999 12 11 DL72L992531 1 19991116 A 2760 651622161 SLAT BOEING 727 727232 1384082 NM L/H WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 SKIN CRACKED AT FENCE ATTACH HOLES. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999121100871 19991211 00871 WP 1999 12 11 DLL19992533 1 19991116 A 2560 D30170559 LKHEED 1011 10113853 5265020 WP R-2 DOOR UNSERV A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 754DL 3582 193Y1181 WHILE TRYING TO CRANK R-2 DOOR SHUT DOOR SLIDE DEPLOYED. REPLACED SLIDE. 2 L 7 3 4F A23WE 1999121100872 19991211 00872 NM 1999 12 11 DL73E992535 1 19991116 A 2700 65503286 BOEING 737 7372S3 NM NO.8 POS DAMAGED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 369DL 21776 RT WING OUTBOARD FLAP JACKSCREW DAMAGED. REPLACED NR 8 JACKSCREW TRANSMISSION ASSY. 2 L 7 2 4F RT A16WE 1999121100873 19991211 00873 NM 1999 12 11 DL72L992536 1 19991117 A 5330 65545914 BEARSTRAP BOEING 727 727232 1384082 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 THE FORWARD EDGE OF THE BEARSTRAP OF THE C-1 CARGO DOOR WAS FOUND DAMAGED. THE DAMAGE WAS CLEANED UP WITH A .5 BY .3 A ND REPAIRED PER ERA 333761-14 AT MV. 2 L 7 3 4F A3WE 1999121100874 19991211 00874 NM 1999 12 11 DL757992538 1 19991115 A 2740 BOEING 757 757232 1384965 NM PEDESTAL CABLE FRAYED A DALA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 27 632DL 23613 STAB TRIM LEVERS MOVE WHEN SPEEDBRAKE IS DEPLOYED APPEARS THAT THE LEFT STAB TRIM LEVER BINDS ACTS AS IF THE SPRING IS B ROKEN. FOUND STAB TRIM CABLE STB1/STB2 MISROUTED AROUND SPOILER, NO BRAKE CLUTCH ASSY BENEATH STAB TRIM HANDLES CABLE F RAYED. CABLES REPLACED ON ROUTINE OPN 2000 RC NR 1 CABLES RIGGED IAW MM REF 27-41-00-05. 2 L 7 2 4F RT A2NM 1999121100875 19991211 00875 NM 1999 12 11 DL757992539 1 19991116 A 3040 WIPER MOTOR BOEING 757 757232 1384965 NM BELOW CAPT WINDS WIRING BAD A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 629DL 22919 CAPTS WINDSHIELD WIPER CB POPPED WOULD NOT RESET. REPLACED WIPER MOTOR. 2 L 7 2 4F RT A2NM 1999121100876 19991211 00876 NM 1999 12 11 DL72L992540 1 19991116 A 2910 39483 ANTISKID MODULE BOEING 727 727232 1384082 NM RT SPLIT A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 511DA 21313 WHILE STOPPED ON THE TAXI WAY DURING TAXI OUT WITH BRAKES SET. A/C STARTED TO ROLL. S/O NOTED 'B' SYSTEM PRESSURE DRO PPING TO ZERO WITH BOTH HYD B LIGHTS ON. FOUND RT ANTI-SKID MODULE CASE BROKEN IN TWO AT FILTER CASE. REPLACED MODULE. 2 L 7 3 4F A3WE 1999121100877 19991211 00877 NM 1999 12 11 DL72S992542 1 19991117 A 5700 RIB BOEING 727 727232 1384082 NM #2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FOUND ON D1 LETTER CK, 1 INCH CRACK NR 2 SLAT NOSE RIB I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999121100878 19991211 00878 NM 1999 12 11 DL72S992543 1 19991117 A 5300 FSLG SKIN BOEING 727 727232 1384082 NM STA 1090 CRKD A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FUSELAGE SKIN CRACKED FS1090 BELOW STRINGER 17L. REPAIRED PER SRM 53-30-3 FIG 26. 2 L 7 3 4F A3WE 1999121100879 19991211 00879 NM 1999 12 11 DL72L992544 1 19991117 A 3350 900835A BOEING 727 727232 1384082 NM STA 950D OVERHD BAD A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 514DA 21430 RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY, CKS GOOD. 2 L 7 3 4F A3WE 1999121100880 19991211 00880 NM 1999 12 11 DL72S992545 1 19991117 A 5300 SKIN BOEING 727 727232 1384082 NM STR 22R STA 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 3/4 CRACK IN FUSELAGE SKIN STR 22R STA 1233. REPAIRED PER SRM 53-30-3 FIG 25. 2 L 7 3 4F A3WE 1999121100881 19991211 00881 NM 1999 12 11 SCNA99140 1 19991118 A 3350 EMER EXIT LIGHT BOEING 727 7272J4 1384006 NM R2 EXIT DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A SCHEDULED MAINTENANCE CHECK, A FUNCTIONAL TEST OF THE EMERGENCY LIGHTS REVEALED THE AFT RIGHT R2 CABIN DOOR EXI T SIGN DID NOT ILLUMINATE. FOUND A BENT PIN ON BATTERY PACK CONNECTOR. STRAIGHTENED PIN AND LIGHT OPERATIONALLY CHECKS GOOD PER MM 335071. 2 L 7 3 4F RT A3WE 1999121100882 19991211 00882 NM 1999 12 11 SCNA99141 1 19991118 A 3350 900542 BATTERY PACK BOEING 727 7272J4 1384006 NM AFT ENTRY SIGN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A SCHEDULED MAINTENANCE CHECK, A FUNCTIONAL TEST OF THE EMERGENCY LIGHTS REVEALED THE AFT ENTRY DOOR CEILING EXIT SIGN LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD REF MM 335071. 2 L 7 3 4F RT A3WE 1999121100883 19991211 00883 SO 1999 12 11 SWIA971593 1 19991106 A 2750 12042642507 EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE UNKNOWN A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 299SW 120329 FLAP DISAGREEMENT AFTER TAKEOFF. RETURNED TO PSP REPLACED FLAP SELECTOR HANDLE. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100884 19991211 00884 SO 1999 12 11 SWIA971594 1 19991106 A 3610 38E966A EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE UNKNOWN A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CL CLIMB 1 NM 07 235SW 120310 LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED INFLIGHT. SHUTDOWN LEFT ENGINE PER QRH PROCEDURES AND RETURNED FOR LANDING. PE RFORMED EXTENSIVE GROUND RUN AT HIGH POWER SETTINGS, DUPLICATED DISC ISOLATED FAULT TO PRESS REGULATOR VALVE IN LEFT WIN G. INSTALLED SERVICEABLE VALVE. PERFORMED EXTENSIVE GROUND RUN AND NO LIGHTS OR LEAKS NOTED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100885 19991211 00885 SO 1999 12 11 SWIA971595 1 19991108 A 3010 EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE UNKNOWN A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 393SW 120330 OUTBOARD LEFT AND RIGHT STABILIZER AND MIDDLE AND OUTBOARD RIGHT WING BOOTS FAIL BOTH TIMERS AND CYCLES. FAILURE OCCURE D EN ROUTE BLI. RETURNED TO SEA. REPLACED MIDDLE WING BOOT EJECTOR FLOW CONTROL VALVE IAW MM 30-70-04. REPLACED RIGHT ENGINE PRESSURE REG IAW MM 30-00-00. PERFORMED ENGINE RUNS, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100886 19991211 00886 SO 1999 12 11 SWIA971596 1 19991108 A 3010 EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE UNKNOWN A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 393SW 120330 DE-ICE BOOT FAILURE LEADING EDGE DEVICES LEFT AND RIGHT OUTBOARD STABILIZER ALSO HAD LEFT AND RIGHT MIDDLE AND OUTBOARD WING FAILURE IN FLIGHT. RETURNED TO SEA. TIGHTENED PNEUMATIC LINE ON DE-ICE MANIFOLD. INSTALLED SERVICEABLE STABILIZE R EJECTOR VALVE. ALL BOOTS OPS CHECKS GOOD EMB 120 MM 30-10-05. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100887 19991211 00887 SO 1999 12 11 SWIA971597 1 19991109 A 3010 EMB 120 EMB120RT SO PWA 118 PW118A NE UNKNOWN A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 284YV 120284 MIDDLE LEFT WING, INBOARD RIGHT WING AND INBOARD LEFT STABILIZER BOOTS FAILED IN FLIGHT. RETURNED TO SEA. REMOVED AND REPLACED LEFT MIDDLE WING DE-ICE PRESSURE SWITCH IAW MM30-10-05. REMOVED AND REPLACED INBOARD WING AND STABILIZER EJECT OR VALVE IAW MM30-10-0. REMOVED AND REPLACED MIDDLE WING EJECTOR IAW MM 30-10-04. RAN ENGINES AND OPS CHECK DE-ICE BOO TS ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100888 19991211 00888 SO 1999 12 11 SWIA971598 1 19991109 A 5270 EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE UNKNOWN A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 581SW 120349 SERVICE LIGHT ILLUMINATED IN FLIGHT. RETURNED TO FIELD. FOUND FORWARD CAM LOCK ON OUTBOARD REFUEL DOOR UNLOCKED. FAST ENED CAM LOCK. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100889 19991211 00889 EA 1999 12 11 SWIA971599 1 19991110 A 7732 CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE UNKNOWN A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 403SW 7028 EN ROUTE CLIMB THROUGH FL340 N2 VIB ICON CAME ON. WOULD NOT GO OUT UNTIL N1 REDUCED TO 80 PERCENT. ON DESCENT, N2 ICON AGAIN CAME ON AT FL300. REDUCED N1 TO 79 PERCENT. N2 VIB ICON OUT. RETURNED TO SLC. REPLACED ENGINE VIBRATION TRANS DUCER RIGHT ENGINE AND MEGGED WIRING AT ENGINE COMPARTMENT. GROUND RUN UP CHECKS GOOD AT ALL POWER SETTINGS. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121100890 19991211 00890 SO 1999 12 11 SWIA971600 1 19991111 A 3020 EMB 120 EMB120RT SO PWA 118 PW118A NE UNKNOWN A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 284YV 120284 LEFT ENGINE INLET DE-ICE BOOT FAILS AFTER 2 MINUTES. RETURNED TO FIELD. FOUND SIGNIFICANT AIR LEAKAGE AT LEFT PRESSURE REGULATOR VALVE FITTING. SECURED LOOSE FITTING. OPS CHECKS GOOD PER MM 30-10-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100891 19991211 00891 EU 1999 12 11 RAIA9911020 1 19991117 A 3610 6411344 SWITCH AEROSP ATR42 ATR42300 8680920 EU #1 FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 426TE 228 7108 - ST L- NR 1 BLEED FAULTING. MAINTENANCE REPLACED NR 1 BLEED OVERTEMP SWITCH. 2 H 7 2 4T RT A53EU 1999121100892 19991211 00892 1999 12 11 SWAA991920 4 19991115 A 2565 D31354 SLIDES BOEING 737 7373H4 1384600 NM DOORS SAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE AND BOTH AFT DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. A DJUSTED SLIDE ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999121100893 19991211 00893 1999 12 11 SWAA991921 4 19991115 A 2565 D31354 SLIDES BOEING 737 7373H4 1384600 NM DOORS SAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLID ES PER MM. 2 L 7 2 4F RT A16WE 1999121100894 19991211 00894 1999 12 11 SWAA991922 4 19991115 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY IND OUT OF VIEW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999121100895 19991211 00895 1999 12 11 SWAA991923 4 19991114 A 2565 6557463 BRACKETS BOEING 737 7373Y0 1384671 NM CABIN FLOOR CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM. 2 L 7 2 4F RT A16WE 1999121100896 19991211 00896 1999 12 11 SWAA991924 4 19991114 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM FWD ENTRY SAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 367SW 26578 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 1999121100897 19991211 00897 1999 12 11 SWAA991925 4 19991114 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT ENTRY TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT FABRIC TORN. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999121100898 19991211 00898 NM 1999 12 11 SWAA991926 1 19991115 A 5751 65C25911 AILERON BOEING 737 7372H4 138448C NM LH WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND LT WING AILERON LOWER SURFACE DELAMINATED NEXT TO 3RD HINGE POINT. REMOVED AND R EPLACED AILERON PER MM. 2 L 7 2 4F A16WE 1999121100899 19991211 00899 NM 1999 12 11 SWAA991927 1 19991115 A 2613 894091 LOOP ELEMENT BOEING 737 7372H4 138448C NM PWA JT8 JT8* 52044 NE #2 ENG ERRATIC A SWAA D E RETURN TO BLOCK ENGINE SHUTDOWN J N WARNING INDICATION FALSE WARNING CL CLIMB 1 SW 07 086SW 22827 707328 AIR TURNBACK INFLIGHT ENGINE SHUTDOWN, DURING CLIMB NR 2 ENG OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES, S HUT NR 2 ENG DOWN AND OVERHEAT LIGHT WENT OUT. NR 2 ENG OVERHEAT SYSTEM WAS PREVIOUSLY PLACED ON MEL. REMOVED OVERHEAT LIGHT BULBS PER MEL 26-2, NOTE C. LATER ON DURING RON REMOVED AND REPLACED NR 2 ENG LOWER FIRE LOOP ELEMENT. 2 L 7 2 4F 4 F A16WE E2EA 1999121100900 19991211 00900 NM 1999 12 11 SWAA991928 1 19991115 A 3244 2606671 TIRE BOEING 737 7373H4 1384600 NM LH MLG SEPARATED A SWAA D RETURN TO BLOCK F S FLT CONT AFFECTED AFFECT SYSTEMS TO TAKEOFF 1 SW 07 322SW 23343 AIR TURNBACK, AFTER TAKEOFF, DURING GEAR RETRACTION NR 2 MLG TIRE SEPARATED, DAMAGING ALL THREE INBD T/E FLAPS, INBD GRO UND SPOILER AND GEAR UPLOCK ACTUATOR HYD LINE. REMOVED AND REPLACED NR 1 AND NR 2 MLG TIRE/WHEEL ASSY'S, ALL THREE INBD FLAPS, INBD GROUND SPOILER AND HYD LINE PER MM. 2 L 7 2 4F RT A16WE 1999121100901 19991211 00901 1999 12 11 SWAA991929 4 19991116 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM AFT SERVICE DOOR OUT OF VIEW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 068SW 22357 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999121100902 19991211 00902 NM 1999 12 11 SWAA991930 1 19991116 A 5315 6546804 BEAM BOEING 737 7373H4 1384600 NM AFT CARGO COMPT CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 860, RBL 8. REPAIRED BEAM PER SWA RA NR 1-A 53-2021. 2 L 7 2 4F RT A16WE 1999121100903 19991211 00903 NM 1999 12 11 SWAA991931 1 19991116 A 5312 963820 CHORD BOEING 737 7373H4 1384600 NM FUSELAGE NOSE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 SIDE CHORD CRACKED, LT SIDE, WL 207. REMOVED AND REPLACED CHORD SECTION PER S RM. 2 L 7 2 4F RT A16WE 1999121100904 19991211 00904 NM 1999 12 11 SWAA991932 1 19991116 A 2560 A170033 STRAP BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND FWD EMERGENCY FLASHLIGHT STRAP BROKEN. REMOVED AND REPLACED STRAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100905 19991211 00905 NM 1999 12 11 SWAA991919 1 19991115 A 5540 65C2584151 RUDDER BOEING 737 7375H4 138449D NM TAIL DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND RT SIDE OF RUDDER DELAMINATED JUST BELOW CENTER HINGE NEAR L/E. REMOVED AND REPLA CED RUDDER ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121100906 19991211 00906 NM 1999 12 11 SWAA991904 1 19991112 A 5310 6545765 SKIN BOEING 737 7372H4 138448C NM FEW FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING WALK ARROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 420, STRINGER 4R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999121100907 19991211 00907 1999 12 11 SWAA991905 4 19991112 A 2565 6557463 BRACKETS BOEING 737 7373H4 1384600 NM AFT ENTRY INCORRECT INSTAL A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 395SW 27689 AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR RETAINING BRACKETS INCORRECTLY INSTALLED. REINSTALLED BRACKETS PER MM. 2 L 7 2 4F RT A16WE 1999121100908 19991211 00908 NM 1999 12 11 SWAA991906 1 19991111 A 5310 6545840 WEB BOEING 737 7373Q8 1384670 NM NLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED RON, NLG WEB CRACKED INBD AFT RADIUS OF LT SIDE ACCESS PANEL. REMOVED AND REPLACED WEB ASSY PER TR NR T1-253-001. 2 L 7 2 4F RT A16WE 1999121100909 19991211 00909 NM 1999 12 11 SWAA991907 1 19991113 A 2612 894091 DETECTOR BOEING 737 7372H4 138448C NM #1 ENG INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 RIGHT AFTER LANDING, NR 1 ENG FIRE WARNING LIGHT AND BELL SOUNDED, SHUT ENG DOWN, AND FIRED BOTH FIRE EXTINGUISHER BOTTL E. WARNING STOPPED. REMOVED AND REPLACED UPPER FIRE LOOP ELEMENT PER MM. 2 L 7 2 4F A16WE 1999121100910 19991211 00910 NM 1999 12 11 SWAA991908 1 19991112 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED RON, FOUND AFT EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999121100911 19991211 00911 NM 1999 12 11 SWAA991909 1 19991112 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM UPPER FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 EXTERNAL FUSELAGE SKIN CRACKED, APPROX BS 540, STRINGER 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999121100912 19991211 00912 1999 12 11 SWAA991910 4 19991112 A 2565 61620468 SLIDE ASSY BOEING 737 7373H4 1384600 NM FWD SERVC DOOR RING PULLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR CHAIN ATTACH RING PULLED APPART. REMOVED AN D REPLACED SLIDE ASSY. 2 L 7 2 4F RT A16WE 1999121100913 19991211 00913 1999 12 11 SWAA991911 4 19991112 A 2565 D31354 SLIDE ASSY BOEING 737 7373H4 1384600 NM DOORS SAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDED OUT OF LIMITS . ADJUSTED BOTH SLIDE ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999121100914 19991211 00914 1999 12 11 SWAA991912 4 19991112 A 2565 D31354 SLIDE ASSY BOEING 737 7373H4 1384600 NM FWD DOORS SAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 642WN 27715 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLID E ASSY'S PER MM. 2 L 7 2 4F RT A16WE 1999121100915 19991211 00915 NM 1999 12 11 SWAA991902 1 19991112 A 2150 106054711 FAN BOEING 737 7373H4 1384600 NM E&E COPMT BURNED A SWAA A B UNSCHED LANDING EMER. DESCENT O OTHER CR CRUISE 1 SW 07 387SW 26602 DURINNG FLIGHT A STRONG BURNING SMELL ENTERED THE CABIN AND COCKPIT. (LAX TO MCI). FOUND EQUIPMENT COOLING FAN BURNED O UT. REMOVED AND REPLACED COOLING FAN PER MM. 2 L 7 2 4F RT A16WE 1999121100916 19991211 00916 1999 12 11 SWAA991903 4 19991112 A 3425 39B1681B HORZ IND BOEING 737 7373H4 1384600 NM COCKPIT INOP A SWAA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SW 07 385SW 26600 STANDBY HORIZON INDICATOR INOP. (PHX TO ONT). REMOVED AND REPLACED STATIC INVERTER AND STANDBY HORIZON INDICATOR. 2 L 7 2 4F RT A16WE 1999121100917 19991211 00917 NM 1999 12 11 SWAA991913 1 19991112 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR, EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTER Y PACK PER MM. 2 L 7 2 4F RT A16WE 1999121100918 19991211 00918 NM 1999 12 11 SWAA991914 1 19991112 A 5230 6545871 FRAME BOEING 737 7373T5 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR CRACKED AT LOWER FRAME NEAR AFT END. REMOVED AND REPLACED DOOR ASSY P ER MM. 2 L 7 2 4F RT A16WE 1999121100919 19991211 00919 NM 1999 12 11 SWAA991915 1 19991112 A 5230 6545871 FRAME BOEING 737 7373T5 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR CRACKED AT LOWER FRAME NEAR AFT END. REMOVED AND REPLACED DOOR ASSY P ER MM. 2 L 7 2 4F RT A16WE 1999121100920 19991211 00920 1999 12 11 SWAA991916 4 19991113 A 2565 D31354 SLIDES BOEING 737 7373H4 1384600 NM FWD DOORS SAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLID ES PER MM. 2 L 7 2 4F RT A16WE 1999121100921 19991211 00921 1999 12 11 SWAA991917 4 19991113 A 2565 D31354 SLIDES BOEING 737 7377H4 NM DOORS SAGGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 707SA 27841 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMI TS. ADJUSTED SLIDES PER MM. 2 L 7 2 4F RT A16WE 1999121100922 19991211 00922 NM 1999 12 11 SWAA991918 1 19991113 A 5315 6546804 BEAM BOEING 737 7373Y0 1384671 NM FWD GALLEY CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 344. REMOVED AND REPLACED UPPER T-CAP FROM RBL 38 TO LBL 67 PER SRM. 2 L 7 2 4F RT A16WE 1999121100923 19991211 00923 EU 1999 12 11 MALA976645 1 19991008 A 5330 SKIN SAAB SF340 SF340A 7850100 EU BS 357 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 48XJ 048 DURING HEAVY CHECK INSPECTION, DENT IN SKIN/STRINGER AT STA 357, LT FUSELAGE, STRINGER 1520. MAINTENANCE REPAIRED IAW M AL GENERIC EO NR S53057. 2 L 7 2 4T RT A52EU 1999121100924 19991211 00924 EU 1999 12 11 MALA976646 1 19991120 A 5347 SEAT TRACK SAAB SF340 SF340A 7850100 EU BS 297 - 357 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING HEAVY CHECK INSPECTION, FOUND CENTER FORWARD SEAT TRACK CORRODED FROM STA 297 TO 357. MAINTENANCE REPAIRED BY CO MPLETING SEAT TRACK SPLICE REPAIR PER IAW EO NR S53060. 2 L 7 2 4T RT A52EU 1999121100925 19991211 00925 EU 1999 12 11 MALA976647 1 19991201 A 5414 SKIN SAAB SF340 SF340A 7850100 EU LT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING HEAVY CHECK INSPECTION FOUND CHAFED SKIN ON LEFT INBOARD NACELLE SKIN. MAINTENANCE PERFORMED PERMANENT REPAIR IA W EO NR S54021. 2 L 7 2 4T RT A52EU 1999121100926 19991211 00926 EU 1999 12 11 MALA976648 1 19991201 A 5414 SKIN SAAB SF340 SF340A 7850100 EU RT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING HEAVY CHECK INSPECTION FOUND RIGHT INBOARD NACELLE SKIN CHAFED. MAINTENANCE PERFORMED PERMENANT REPAIR IAW EO NR S54022. 2 L 7 2 4T RT A52EU 1999121100927 19991211 00927 EU 1999 12 11 MALA976649 1 19991202 A 3230 S2700003 RELAY BAC 146 AVRO146RJ85A 1500097 EU MLG FAILED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 512XJ E2328 AFTER TAKEOFF, THE LANDING GEAR WILL NOT RETRACT WITHOUT USING THE OVERRIDE SWITCH, TRIED SEVERAL TIMES TO RAISE THE GEA R NORMALLY. MAINTENANCE REPLACED RELAY GA30 AND LT STRUT TO BE UNDERSERVICED IN LOWER CHAMBER, SERVICED IAW AVRO MM 32- 10-14. LUBRICATED ALL GREASE FITTINGS, VERIFIED NORMAL OPERATION OF SQUAT SYSTEMS AND LANDING GEAR HANDLE. GOOD FOR CO NTINUED SERVICE. 2 H 7 4 4F RT A49EU 1999121100928 19991211 00928 EU 1999 12 11 MALA976650 1 19991202 A 3213 STRUT BAC 146 AVRO146RJ85A 1500097 EU RT MLG DISCHARGED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 517XJ E2335 DEPARTING DLH GEAR SELECTED UP, OVERRIDE HAD TO BE USED. ALSO, AUTO THROTTLE FAILED, FD ALSO, BUT CAME BACK DURING FLIG HT. MAINTENANCE FOUND RIGHT LEG DOLLS EYE ILLUMINATED, JACKED AC FOUND RIGHT SHOCK ABSORBER NOT EXTENDING ALL OF THE WA Y, LOWER AC AND SERVICED RT SHOCK ABSORBER IAW 32-10-14. JACKED AC COMPRESSED STRUT AND RELEASE STRUT, EXTENDS FULLY, P ERFORMED GEAR SWINGS. ALL CHECKS GOOD IAW 32-30-00. PERFORMED RESET OF AUTO THROTTLE, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1999121100929 19991211 00929 1999 12 11 MALA976651 4 19991203 A 3420 6226190113 COMPUTER SAAB SF340 SF340A 7850100 EU AVIONICS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 68XJ 068 DURING CLIMB, 31 EADI DISPLAYED BLACK SKELETON SCREEN WITH RED ATT, FD, VOR, AND HDG FLAGS. RETURNED TO MSP. MAINTENAN CE REPLACED NR 1 AHRS COMPUTER. SYSTEM OPS CHECKS GOODS IAW SF340 MM. 2 L 7 2 4T RT A52EU 1999121100930 19991211 00930 EU 1999 12 11 MALA976652 1 19991204 A 5610 7256100502 WINDSHIELD SAAB SF340 SF340A 7850100 EU COCKPIT CRACKED A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 119XJ 119 CRACK IN RIGHT FRONT WINDSHIELD. MAINTENANCE REPLACED NR 2 FRONT WINDOW IAW SF340 MM 56-10-05, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999121100931 19991211 00931 EU 1999 12 11 MALA976653 1 19991207 A 3020 44730501 MODULE SAAB SF340 340B 7860101 EU DEICE CONTROL FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 412XJ 340B412 RIGHT INTAKE ANNUNCIATOR ILLUMINATED IN FLIGHT, RESET SWITCH IT REMAINED ILLUMINATED UNTIL CREW RETURNED BACK TO MSP. M AINTENANCE REPLACED DEICE CONTROL MODULE, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999121100932 19991211 00932 EU 1999 12 11 MALA976654 1 19991204 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 414XJ 340B414 AFTER TAKEOFF WHEN LP BLEEDS WERE PLACED IN AUTO A STRONG METALLIC OR POWDERY ODOR WAS EMITED FROM DUCTS AND ODOR WAS ST RONGER IN THE COCKPIT. ODOR PERSISTED AND ONLY DECREASED BY SHUTING OFF THE RECIRCULATION FAN. RETURNED TO DTW. MAINT ENANCE GROUND RAN AC WITH LP AND HP BLEEDS ON AT VARIOUS TEMP SETTINGS. NO ODOR NOTED. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999121100933 19991211 00933 EU 1999 12 11 MALA976655 1 19991204 A 3260 INDICATOR SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A MALA O OTHER N FALSE WARNING LD LANDING 1 GL 15 418XJ 418 ON FINAL APPROACH TO DTW, LOWERED GEAR, RIGHT MAIN DID NOT ILLUMINATE. RAISED AND LOWERED GEAR A SECOND TIME, RIGHT GEA R LIGHT STILL WAS OUT. CHECKED GEAR LIGHTS, RIGHT MAIN STILL OUT, THEN OUT OF THE BLUE THE LIGHT CAME ON WHILE GEAR WAS DOWN. MAINTENANCE RELAMPED RIGHT GEAR GREEN DOWNLOCK LIGHTS AND CLEANED DOWNLOCK INDICATION CANNON PLUGS. PERFORMED G EAR SWINGS AND OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999121100934 19991211 00934 EU 1999 12 11 MALA976656 1 19991203 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS BAY MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 425XJ 425 AVIONICS SMOKE WARNING LIGHT CAME ON AFTER TAKEOFF. NO SMOKE NOTED. RETURNED TO TVC. MAINTENANCE REPLACED AVIONICS SM OKE DETECTOR IAW AMM 26-13-05-4, OPS CHECKS GOOD IAW 26-13-00-5. 2 L 7 2 4T RT A52EU 1999121100935 19991211 00935 EU 1999 12 11 MALA976657 1 19991207 A 3320 LIGHT SAAB SF340 340B 7860101 EU ROW 1A FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 418XJ 418 CREW REPORTED SMOKE COMING FROM ROW 1A OVERHEAD FLOOD LIGHT. MAINTENANCE REPLACED SOCKET AT ROW 1A, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999121100936 19991211 00936 WP 1999 12 11 CALA9901569 1 19991207 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP CARGO BAY DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND AFT CARGO DOOR THRESHOLD DENTED AND GOUGED. A STRAP REPAIR WAS INSTALLED IAW ECRA 5310-03954. 2 L 7 2 4F A6WE 1999121100937 19991211 00937 WP 1999 12 11 CALA9901570 1 19991207 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1136 - 1117 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1136-1117, LBL 56. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999121100938 19991211 00938 WP 1999 12 11 CALA9901571 1 19991207 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1180 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND A 6 INCH CRACK IN CUSP WEB AT FS 1180, LBL 44. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999121100939 19991211 00939 WP 1999 12 11 CALA9901572 1 19991207 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 190 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND CUSP WEB PUNCTURED AT FS 190, LBL 6. THE PUNCTURED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1999121100940 19991211 00940 WP 1999 12 11 CALA9901573 1 19991207 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND LT SIDE OF AFT AIRSTAIRS LOWER SEGMENT SKIN CRACKED AT ROLLER BEARINGS. THE CRACK WAS ROUTED OUT AND S TOP DRILLED IAW SRM 53-01, FIGURE 1. A REPAIR PATCH WAS INSTALLED IAW SRM 52-60-0, FIGURE 3, 51-10-4, 51-30-1, AND 51-3 0-5. 2 L 7 2 4F A6WE 1999121100941 19991211 00941 WP 1999 12 11 CALA9901574 1 19991207 A 5280 DOOR PAN DOUG DC9 DC982 3022082 WP RT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND RT MAIN GEAR DOOR OUTBOARD AFT PAN CRACKED ON CORNER. THE DOOR PAN WAS REMOVED AND REPLACED IAW SRM 51 -10-3. 2 L 7 2 4F A6WE 1999121100942 19991211 00942 WP 1999 12 11 CALA9901575 1 19991207 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP COCKPIT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND COCKPIT FLOORBOARD BETWEEN TWO LOWER FIRST OFFICER'S SEAT TRACKS CORRODED. THE FLOORBOARD WAS REMOVED AND A NEW FLOORBOARD WAS INSTALLED IAW SRM 53-05, FIGURE 1. 2 L 7 2 4F A6WE 1999121100943 19991211 00943 WP 1999 12 11 CALA9901576 1 19991207 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP BS 636 - 693 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND OUTBOARD LIP OF MID PIT DOOR THRESHOLD PANEL TORN AT FS 636-693. THE AREA WAS ROUTED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5310-03952, SRM 53-01, FIGURE 2, AND 51-30-2. 2 L 7 2 4F A6WE 1999121100944 19991211 00944 WP 1999 12 11 CALA9901577 1 19991207 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP CARGO BAY DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND FORWARD CARGO DOOR THRESHOLD DENTED. REPAIRED IAW ECRA 5310-03953. 2 L 7 2 4F A6WE 1999121100945 19991211 00945 WP 1999 12 11 CALA9901578 1 19991208 A 5730 PANEL DOUG DC10 DC1030 3023501 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14090 46553 INSPECTION FOUND A 1 INCH CRACK IN LT WING UPPER LEADING EDGE PANEL NR 517CT. THE PANEL WAS REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999121100946 19991211 00946 NM 1999 12 11 UPS99231178 1 19991207 A 3350 1000677 LIGHT BOEING 727 72730C 1384009 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:N/A, REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY (P/N 10-0067-7) (S/N 20261) OFF, REF IPC 33-50-00-20 -15. REMOVED EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999121100947 19991211 00947 NM 1999 12 11 UPS99231181 1 19991206 A 3350 1000677 LIGHT BOEING 727 72730C 1384009 NM CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE:N/A, BORROWED PART INSTALLED IN EMERGENCY EXIT LIGHT L1 POSITION. REMOVED AND REPLACED EMERGENCY EXIT L IGHT IN L1 POSITION (P/N 10-0067-9) ON, (P/N 10- 0067-7) OFF, (S/N 2151) ON, (S/N 20261) OFF. 2 L 7 3 4F A3WE 1999121100948 19991211 00948 NM 1999 12 11 UPS99231182 1 19991207 A 3260 SWITCH BOEING 727 727108C 1384039 NM MLG OUT OF ADJUST A IPXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 936UP 19503 INSPECTION TYPE:N/A, AFTER GEAR RETRACTION, RED DOORS LIGHT REMAINED ILLUMINATED, CYCLED GEAR, LIGHT WENT OUT. PERFORME D ADJ/TEST OF LANDING GEAR DOOR WARNING SWITCHES PER AMM 32- 62-11 PG 501. ALL INDICATORS LIGHTS CK GOOD PER MM REFEREN CE. 2 L 7 3 4F A3WE 1999121100949 19991211 00949 NM 1999 12 11 UPS99231183 1 19991206 A 3350 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:N/A, EMERGENCY LIGHT AT MAIN ENTRY DOOR INOP. REPLACED BATTERIES, OPS CK GOOD. 2 L 7 3 4F A3WE 1999121100950 19991211 00950 NM 1999 12 11 UPS99431180 1 19991206 A 2824 MA11A1194 ACTUATOR BOEING 747 747123F NM NR 4 ENGINE FAILED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 677UP 20391 INSPECTION TYPE:N/A, NR 4 ENG IN FLIGHT SHUTDOWN DUE TO S/O VLV CLOSED AND C/B POPPED. REPAIRED PIN CONNECTOR D2316J AN D REMOVED AND REPLACED S/O VLV. 2 L 7 4 4F A20WE 1999121100951 19991211 00951 NM 1999 12 11 UPS99631184 1 19991208 A 2150 3964961 VALVE BOEING 767 76734AF 1385212 NM LT PACK INOPERATIVE A IPXA O OTHER O OTHER UK UNKNOWN 1 SO 01 316UP 27744 INSPECTION TYPE:ETOP PIREP- LT PACK O/TEMPS. REPLACED LEFT PACK FLOW CONTROL VALVE. RAN PACKS AND FOUND SAME TO OPERAT E NORMALLY. CLEARED ITEM (P/N 396496-1) (S/N 116) ON, (P/N 396496-1) (S/N 309) OFF. 2 L 7 2 4F RT A1NM 1999121100952 19991211 00952 NM 1999 12 11 99UAL900597 1 19991113 A 2460 FC3400D CONNECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 GENERATOR FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 316UA 23948 AFTER TR-2 AND TR-3 CIRCUIT BREAKERS POPPED, NUMBER TWO GENERATOR TRIPPED OFF LINE AND COULD NOT BE RESET. *S/D* CONTA CTS IN CONNECTOR D5126 PLUG AND JACK WERE BURNT. THE NR 2 ENGINE GENERATOR FEEDERS DISCONNECTED AT THE PYLON TO WING. R EPLACED THE CONTACTS AND THE CONNECTOR D5126 PLUG AND JACK. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121100953 19991211 00953 NM 1999 12 11 99UAL900610 1 19991126 A 3350 BATTERY PACK BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 954UA 26739 AFT CABIN SECTION OF EEL LIGHTING WAS FOUND TO BE INOPERATIVE. THE EEL LIGHTING BATTERY PACK WAS REPLACED, OPS CHECK WA S GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121100954 20001016 00954 EU 2000 10 16 99UAL900611 1 19991124 A 2750 D5757030500251 ROD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE TE FLAPS OUT OF ADJ A UALA O OTHER F FLT CONT AFFECTED LD LANDING 1 WP 29 424UA 506 DURING APPROACH THE T/E FLAPS DID NOT FULLY DEPLOY. L/E SLATS OPERATED NORMALLY. *S/D* AN INSPECTION FOUND THE ACTUA TING (ADJUSTMENT) ROD INSIDE THE INTERCONNECTING STRUT BETWEEN THE LT I/B AND O/B FLPS HAD ORIGINALLY BEEN ADJUSTED ALMO ST OUT OF LIMIT, CAUSING THE PROX SENSOR OUT OF TARGET WHILE EXTENDINGG FLAP TO HIGHER SETTING. THE ROD WAS FINALLY EXT ENDED TO ALLOW MORE MARGIN IN THE PROX TARGET RANGE. 2 L 7 2 4F 4 F RT A28NM E40NE 1999121100955 19991211 00955 NM 1999 12 11 99UAL900612 1 19991126 A 3397 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 357UA 24378 EEL LIGHTING WAS INOPERATIVE FROM ROW 16 AFT. THE AFT 18 FEET OF EEL CONDUIT CABLE ASSEMBLY WAS REPLACED. OPS CHECK WA S GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121100956 19991211 00956 NM 1999 12 11 99UAL900613 1 19991126 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 107UA 26900 EMERGENCY LIGHTS EICAS ADVISORY MESSAGE DISPLAYED. EMERGENCY LIGHTS SWITCH NOT IN ARMED POSITION AND EMERGENCY LIGHTS T URNED ON BY FLIGHT ATTENDANT SWITCH. 2 L 7 4 4F 4 F RT A20WE E24NE 1999121100957 19991211 00957 NM 1999 12 11 99UAL900614 1 19991128 A 2613 355644310 DETECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WING TO BODY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 380UA 24655 THE RIGHT-HAND WING-BODY OVERHEAT LIGHT CAME ON DURING FLIGHT. *S/D* REPLACED THE RIGHT-HAND M1204 BLEED AIR DUCT LEAD ING EDGE OVERHEAT DETECTOR. RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121100958 19991211 00958 EU 1999 12 11 99UAL900615 1 19991129 A 2121 BLOWER VF4957, TECH EVT3454GOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 451UA 3488 865 A LOUD NOISE WAS HEARD UNDER FLIGHT DECK AND F/A SMELLED ELECTRICAL ODOR. PROBLEM WAS POSIBLE AVIONICS COOLING SYSTEM. AFTER OVERRIDING SYSTEM, SMELL DISSIPATED AND NOISE STOPPED. ALL SYSTEMS REPORTING NORMAL. FLIGHT CONTINUED TO DESTIN ATION. *S/D* THE AVIONICS VENTILATION BLOWER WAS FAULTED ON THIS FLIGHT. THE BLOWER FAN (FIN 20HQ) FAILED AND WAS REP LACED DECEMBER 1 IN SAN FRANCISCO PER AMM 21-26-51 DURING C-CHECK. THERE HAS BEEN NO FURTHER OCCURRANCES. 2 L 7 2 4F 4 F RT A28NM E40NE 1999121100959 19991211 00959 EU 1999 12 11 99UAL900616 1 19991129 A 3350 POWER SUPPLY DIEHL GMBH & 321454 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 444UA 1494 824 EMERGENCY LIGHT TEST FAILS EPSU COM L. *S/D* EMERGENCY POWER SUPPLY UNIT (11WL) WAS FOUND FAULTED DURING TEST WITH MES SAGE EPSU COM L SHOWN. THE UNIT WAS REPLACED AND CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1999121100960 19991211 00960 NM 1999 12 11 99UAL900617 1 19991124 A 3350 900835A BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7256U 21403 RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1999121100961 19991211 00961 NM 1999 12 11 99UAL900618 1 19991129 A 2910 1121S21072 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE HYDRAULIC SYS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 7275U 21422 ON SHORT APPROACH, LOST SYSTEM A HYDRAULIC PRESSURE AND FLUID. TOWED TO GATE. *S/D* REPLACED LEAKING HYDRAULIC FLOW L IMITING VALVE. ALSO, REPLACED NR 1 & NR 2 ENG HYDRAULIC PUMPS AND CASE DRAIN FILTERS. BLEED AND TESTED PUMPS FOR LEAKS . JACKED AIRCRAFT AND CYCLED LANDING GEAR TO BLEED AIR OUT OF SYSTEM AND LEAK CHECK REPLACEMENT FLOW LIMITING VALVE. N O LEAKS NOTED. SERVICED HYDRAULIC SYSTEM. 2 L 7 3 4F 4 F A3WE E2EA 1999121100962 19991211 00962 NM 1999 12 11 99UAL900619 1 19991130 A 5270 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR ACTIVATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 376UA 24641 FLIGHT ABORTED TAKEOFF AT APPROXIMATELY 100 KNOTS DUE TO A PASSENGER DOOR 1 LEFT WARNING INDICATION. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121100963 19991211 00963 NM 1999 12 11 99UAL900620 1 19991201 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 199UA 28717 EMERGENCY LIGHTS EICAS ADVISORY MESSAGE DISPLAYED. EMERGENCY LIGHTS SWITCH NOT IN ARMED POSITION, OR SWITCH IN ARMED P OSITION ON AND EMERGENCY LIGHTS TURNED ON BY FLIGHT ATTENDANT SWITCH. 2 L 7 4 4F 4 F RT A20WE E24NE 1999121100964 20001016 00964 NE 2000 10 16 99UAL900621 2 19991129 A 7200 ENGINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 2 FAILED A UALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 158UA 21054 685788 NUMBER TWO ENGINE STALLED, BACK FIRED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 120 KTS. EGT AMBER LIGHT CAME ON AS CAPTIAN REDUCED THRUST. *S/D* COMPRESSOR FAILED AND THE ENGINE SURPLUSED, IT WAS NOT DISASSEMBLED. 2 L 7 4 4F 4 F A20WE E20EA 1999121100965 19991211 00965 NM 1999 12 11 99UAL900622 1 19991201 A 2150 8102082 HEAT EXCHANGER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT PACK FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 26931 ON GROUND, AC PACK NOISE FOLLOWED BY SUBSEQUENT PACK SHUT DOWN AND EICAS MESSAGE RT DUCT LEAK. *S/D* FOUND RIGHTHAND H EAT EXCHANGER (P/N 810208-2 ) PRIMARY INLET TORN, INITIAL EXAM REVEALED THAT THE DAMAGE STARTED FROM THE V-NOTCH AREA. T HE RT HEAT EXCHANGER WAS REPLACED. UNDER INVESTIGATION BY MANUFACTURER. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999121100966 19991211 00966 NM 1999 12 11 99UAL900623 1 19991201 A 2150 213W31201 DOOR ASSY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT RAM INLET DAMAGED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 770UA 26925 CREW REPORTED AIRFRAME VIBRATION LEFT SIDE OF AIRCRAFT DURING CLIMBOUT FROM FRA EN ROUTE ORD. DIVERTED TO LHR. *S/D* FOUND LEFTHAND PACK RAM AIR INLET DOOR ASSY (AFT PANEL (P/N 213W3120-1) DAMAGED. AFT PANEL DOOR ASSY WAS REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999121100967 19991211 00967 WP 1999 12 11 ABXA9900823 1 19991026 A 5320 99576643 INTERCOSTAL DOUG DOUG DC9 DC932 3022066 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND FORWARD LOWER CARGO COMPARTMENT DOOR INTERNAL INTERCOSTAL AT LOWER DOOR STOP CRACKED. REPLACED IN TERCOSTAL IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1999121100968 19991211 00968 WP 1999 12 11 ABXA9900824 1 19991026 A 5230 59101415 PAN DOUG DOUG DC9 DC932 3022066 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT THIRD STOP FROM TOP AFT FLANGE. REPAIRED PAN IAW DC 9 SRM 52-05. 2 L 7 2 4F A6WE 1999121100969 19991211 00969 WP 1999 12 11 ABXA9900825 1 19991026 A 5230 59101577 PAN DOUG DOUG DC9 DC932 3022066 WP FWD LWR CARGO CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR OUTER PAN CRACKED IN 6 PLACES. REPAIRED IAW ABX REA D952-337 73. 2 L 7 2 4F A6WE 1999121100970 19991211 00970 WP 1999 12 11 ABXA9900826 1 19991026 A 5712 991707210 RIB DOUG DOUG DC9 DC932 3022066 WP RIGHT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE PANEL INBOARD RIB CRACKED OUTBOARD OF MAIN LANDING GEAR. REPLACED RIB IA W DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999121100971 19991211 00971 WP 1999 12 11 ABXA9900827 1 19991026 A 5313 49125151 END CAP DOUG DOUG DC9 DC932 3022066 WP AFT LWR CARGO CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 30 END CAP CORRODED AT STATION 986 TO 996. REPLACED END CAP IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999121100972 19991211 00972 WP 1999 12 11 MWEA99872 1 19991208 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP AFT CABIN DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT AND RIGHT NACELLE EMERGENCY LIGHTS WENT OUT DURING TEN MINUTE TEST. MAINTENANCE REPLACED NACELLE EMERGENCY LIGHTS BATTERY PACK. 2 L 7 2 4F A6WE 1999121100973 19991211 00973 WP 1999 12 11 MWEA99873 1 19991208 A 5310 5911401123 LONGERON DOUG DC9 DC932 3022066 WP STATION 158 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CORROSION ON LONGERON 22 RIGHT AT STATIONS 158 TO 218 IN ELECTRICAL / ELECTRONICS COMPARTMENT. MAINTENANCE FITTED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 1999121100974 19991211 00974 WP 1999 12 11 MWEA99874 1 19991208 A 5230 59101573 SKIN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND AN AREA OF CHAFING ON AFT CARGO DOOR LOWER FORWARD SKIN. MAINTENANCE FABRICATED AND INSTALLED SKIN DOUBLER REPAIR . 2 L 7 2 4F A6WE 1999121100975 19991211 00975 WP 1999 12 11 MWEA99875 1 19991208 A 5230 59101573 SKIN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND AREAS OF CHAFING ON BOTTOM EDGE OF AFT CARGO DOOR SKIN. MAINTENANCE FABRICATED AND INSTALLED SKIN REPAIRS. 2 L 7 2 4F A6WE 1999121100976 19991211 00976 WP 1999 12 11 MWEA99876 1 19991208 A 5210 995575855 BEAM DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND PASSENGER DOOR NUMBER SEVEN BEAM CRACKED ON FORWARD SIDE IN RADIUS. MAINTENANCE FABRICATED AND INSTALLED REPAIR D OUBLER. 2 L 7 2 4F A6WE 1999121100977 19991211 00977 WP 1999 12 11 MWEA99877 1 19991208 A 5210 995575213 BEAM DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND PASSENGER DOOR NUMBER ONE BEAM CRACKED ON FORWARD AND AFT ENDS. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBL ERS. 2 L 7 2 4F A6WE 1999121100978 19991211 00978 WP 1999 12 11 MWEA99878 1 19991208 A 5210 995575745 BEAM DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND PASSENGER DOOR NUMBER SIX BEAM CRACKED ON FORWARD SIDE. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999121100979 19991211 00979 WP 1999 12 11 MWEA99879 1 19991208 A 3350 6011777 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 BOTH SIDES OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MTC REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK. 2 L 7 2 4F A6WE 1999121100980 19991211 00980 WP 1999 12 11 DHL99801004 1 19991208 A 3231 H654 SWITCH DOUG DC8 DC873F 302199F WP LEFT MAIN DOOR UNSERVICABLE A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 AFTER GEAR RETRACTION, DOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LEFT MA IN GEAR DOOR POSITION SWITCH PER MM 32-60-0, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999121100981 19991211 00981 SO 1999 12 11 SWIA971607 1 19991122 A 2750 FLAPS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE WINGS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 301YV 120301 AFTER TAKEOFF, INBOARD FLAP DISAGREEMENT. CYCLED FLAPS BUT THEY WOULD NOT RETRACT. RETURNED FOR LANDING USING FLAPS 25 . FLAPS RETRACTED NORMALLY ON GROUND. REPLACED FLAP ANNUNCIATOR PANEL, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100982 19991211 00982 SO 1999 12 11 SWIA971608 1 19991122 A 3230 RETRACT SYSTEM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG CONTAMINATED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 209SW 120269 LEFT MAIN GEAR WOULD NOT RETRACT. RETURNED TO FIELD. JACKED AIRCRAFT AND CYCLED GEAR WITH GROUND POWER AND GREEN SYSTE M ONLY. FAULT FREE CYCLES. SUSPECT SNOW AND SLUSH CONDITION TO BE THE FAULT. GEAR OPERATION TESTED OK IAW MM 32. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100983 19991211 00983 SO 1999 12 11 SWIA971609 1 19991123 A 3610 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PNEUMATIC SYSTEM ILLUMINATED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 578SW 120346 DUCT LEAK RIGHT SIDE ILLUMINATED. RETURNED TO SEA. SECURED DRAIN FOR DEICE REGULATOR, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100984 19991211 00984 SO 1999 12 11 SWIA971610 1 19991123 A 3610 WARNING LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PNEUMATIC SYSTEM ILLUMINATED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 578SW 120346 RIGHT DUCT LEAK LIGHT ILLUMINATED AT 800 FEET AFTER TAKEOFF. ISOLATED BLEED WITH CROSSBLEED OFF AND BLEED OFF AND STILL STAYED ILLUMINATED OVER 3 MINUTES. RETURNED TO SEA. SECURED RIGHT DEICE DRAIN LINE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100985 19991211 00985 SO 1999 12 11 SWIA971611 1 19991124 A 2722 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER FAILED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 293SW 120320 RIGHT RUDDER STUCK JUST PAST HALF TRAVEL. SHUT OFF BLUE RUDDER SYSTEM AND RUDDER TRAVEL BECAME FREE. RETURNED TO SLC. INSTALLED SERVICEABLE RUDDER ACTUATOR FOR BLUE SYSTEM IAW 27-20-00. NO LEAKS NOTED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100986 19991211 00986 SO 1999 12 11 SWIA971612 1 19991126 A 5297 WIRE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DOOR WARNING BROKEN A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 288SW 120316 PASSENGER DOOR LIGHT CAME ON AFTER TAKEOFF. RETURNED TO SEA. REPAIRED BROKEN WIRE AT DOOR HINGE, OPS CHECK GOOD IAW 52 . 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100987 19991211 00987 1999 12 11 SWIA971613 4 19991126 A 3417 7858062 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE AIR DATA MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 410SW 7066 PITOT BASE OVERHEAT WARNING ILLUMINATED AFTER TAKEOFF. RETURNED TO FIELD. POWERED AIRCRAFT DOWN AND BACK UP. NO DEFEC TS NOTED AT THIS TIME. AIRCRAFT GOOD FOR CONTINUED SERVICE. REMOVED AND REPLACED AIR DATA SENSOR CONTROLLER AFTER ARRI VAL IN SLC. OPS CHECKS GOOD IN OVERWEIGHT ON WHEELS CONFIGURATION. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121100988 19991211 00988 SO 1999 12 11 SWIA971614 1 19991128 A 2722 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 UNABLE TO APPLY NORMAL RIGHT RUDDER AFTER TAKEOFF. LEFT RUDDER WORKED OK AND SYSTEM WORKED NORMALLY ON DESCENT. REPLAC ED BLUE SYSTEM RUDDER ACTUATOR. NO LEAKS NOTED. GROUND FUNCTIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100989 19991211 00989 SO 1999 12 11 SWIA971615 1 19991128 A 3260 UPLOCK EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 196CA 120196 UPON GEAR RETRACTION THE RIGHT MAIN GEAR RED A LIGHT WORLD NOT EXTINGUISH. ALSO HEARD BANGING SOUNDS AND FELT VIBRATION . RETURNED TO FAT. ADJUSTED RIGHT MLG UPLOCK INDICATION PLUNGER SCREW IAW 32-61-01. ALL GEAR SWING CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100990 19991211 00990 SO 1999 12 11 SWIA971616 1 19991129 A 3610 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE PNEUMATIC SYSTEM LOOSE A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 561SW 120335 ON TAKEOFF DURING CLIMBOUT DUCT LEAK LIGHT CAME ON BUT WENT OFF WHEN RESPECTIVE BLEED WAS CLOSED. RETURNED TO LAX. LIG HT CAME BACK ON DURING APPROACH. LIGHT WENT OFF AFTER ENGINE WAS SHUTDOWN DURING TAXI. FOUND PRESSURE REGULATOR OVERBO ARD DRAIN OFF OF LEFT SIDE. REPOSITIONED PRESSSURE REGULATOR AND REPLACED CLAMP. RAN ENGINE AND NO LEAKS WERE NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121100991 19991211 00991 EA 1999 12 11 SWIA971617 1 19991130 A 3260 TARGET CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE MLG UPLOCK LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 416SW 7089 AFTER GEAR RETRACTION GEAR DISAGREE WARNING ON LEFT MAIN GEAR. RETURNED TO SLC. NOTED FAULT IN PSEU FOR LEFT GEAR UPLO CK, (FAR). TIGHTENED UPLOCK TARGET AND CHECKED GAP PER MM 32-32-05. CYCLED GEAR NORMALLY AND PEFORMED FREE FALL CHECK. GEAR INDICATIONS CHECKS GOOD. CLEARED PSEU MEMORY. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121100992 19991211 00992 EU 1999 12 11 99ZZZX4377 1 19991028 A 7933 1409611 CONNECTOR SNIAS 350 AS350B2 8680813 EU OIL TEMPERATURE LOOSE A A HCMA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 13 982BH 2876 DURING A TOUR FLIGHT WITH 6 PASSENGERS ON BOARD, THE PILOT NOTICED THE ENGINE OIL TEMPERATURE GAUGE JUMP FROM 90 DEGREES CELCIUS TO BEING PEGGED OUT AT 130 DEGREES CELCIUS. THE PILOT PERFORMED A PRECAUTIONARY LANDING IN A PASTURE IN HANA. WHEN THE MECHANIC ARRIVED 30 MINUTES LATER, THE ENGINE OIL TEMPERATURE GAUGE INDICATED A NORMAL 45 DEGREES CELCIUS. TH E SPADE TERMINAL ELECTRICAL CONNECTOR AT THE OIL TEMPERATURE PROBE WAS CHANGED DUE TO POSSIBLE LOOSENESS OF THE CRIMP CO NNECTION OR BROKEN WIRE STRANDS AT THE TERMINAL. 1 G 7 1 3U H9EU 1999121100993 19991211 00993 CE 1999 12 11 R7MA0000780 1 19991007 A 2130 F7513 CONTROLLER BEECH 200 200BEECH 1152920 CE FLOW PACK INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 301HC 3K00170 BB1219 INTERMITTENT FLOW PACK OPERATION. 1 L 7 2 4T A24CE 1999121100995 19991211 00995 SW 1999 12 11 HEEA064977 1 19991105 A 6510 407040302101 DRIVESHAFT BELL 407 407 SW TAIL ROTOR CONTAMINATED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 407PH 4473 A15 53003 ROYCO 13 AND MOBILE 28 MIXED IN TAIL ROTOR DRIVESHAFT. (X) 1 G 7 1 3U O H2SW 1999121101011 19991211 01011 EU 1999 12 11 GXPA99004 1 19991029 A 2120 UNKNOWN HAMFLU HFB320 HFB320 4071204 EU COCKPIT SMOKE A GXPA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 171GA 1039 SMOKE IN COCKPIT AFTER TAKEOFF FROM LITTLE ROCK, ARKANSAS. RETURNED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AI RCRAFT AND INSPECTED AIRCRAFT SYSTEMS AND PERFORMED FULL POWER ENGINE RUN FOR 30 MINUTES. COULD NOT DUPLICATE SMOKE IN COCKPIT. (X) 2 L 7 2 4J A14EU 1999121101012 19991211 01012 CE 1999 12 11 99ZZZX4394 1 19991028 A 3010 5E1319 BOOT BEECH 99 99A 1154003 CE DEICE SYSTEM FAILED A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 955AA U128 LIP DEICE BOOT TRIPPED CIRCUIT BREAKER IN-FLIGHT. POST-FLIGHT INSPECTION REVEALED DEICER BURNED UP LEAVING EXPOSED WIRE S AND CHARING ON COWL. DEICER WAS THEN REPLACED FOLLOWING REPAIRS TO COWL. SEVERAL THINGS COULD HAVE CONTRIBUTED TO TH E PROBLEM INCLUDING AN IMPACT DAMAGE OR AGE OF THE BOOT ALLOWING HEATING ELEMENT WIRES TO BE EXPOSED AND SUBSEQUENTLY SH ORTING. 1 L 7 2 3T A14CE 1999121101013 19991211 01013 1999 12 11 99ZZZX4395 4 19991027 A 6122 8210002AD PROP GOVERNOR WOODWARD BEECH 99 B99 1154004 CE RT ENGINE ERRATIC A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 99TH 1208905 U155 PROPELLER GOVERNOR OPERATED SLUGGISHLY REGARDING PROPELLER RPM CHANGES FROM HIGH POWER SETTINGS TO IDLE ON SHORT FINAL. THE PROPELLER GOVERNOR WAS CHANGED FOR TROUBLESHOOTING PURPOSES AND CONSEQUENTLY ALLEVIATED THE DISCREPANCY. THE PILOT VALVE MAY HAVE BEEN STUCK IN THE CLOSED POSITION NOT ALLOWING OIL TO DRAIN FROM THE HUB AND FORCING THE PROPELLER BLADE S TO REMAIN IN A FLAT PITCH. THIS, IN TURN, WOULD CAUSE A YAW TOWARD THE DIRECTION OF THE PROP WITH THE FLAT BLADE PITC H. 1 L 7 2 3T A14CE 1999121101024 19991211 01024 CE 1999 12 11 99ZZZX4406 1 19991116 A 2140 B4500 HEATER CESSNA 340 340A 2076405 CE COCKPIT DIRTY A K5LA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 EA 05 45TF 367 A96120020 340A1507 SMOKE AND FUMES IN COCKPIT WHEN HEATER TURNED TO FULL INCREASE. HEATER OVERHEAT ANNUNCIATOR DISPLAYED. POSSIBLE CAUSE: DUST OR DIRT IN THE SYSTEM. MECHANIC RESET CIRCUIT BREAKER AND OPERATIONALLY TESTED FOR 30 MINUTES WITH NO DEFECT OR MALFUNCTION. 1 L 7 2 3O 3A25 1999121101027 19991211 01027 GL 1999 12 11 99ZZZX4409 2 19991105 A 7321 23069251 FCU CHNDLREVANS BELL 407 407 SW ALLSN 250C 250C47B GL FUEL SYSTEM LEAKING A B65A K NONE K FLUID LOSS IN INSP/MAINT 1 GL 13 407CR 407 UGALM00496 53254 CAE847279 FUEL CONTROL LEAKING AT AMBIENT AIR PASSAGE. 1-2 DROPS AFTER START. INTERNAL LEAKAGE. 1 G 7 1 3U 3 U O H2SW E1GL 1999121101028 19991211 01028 SW 1999 12 11 99ZZZX4410 1 19991104 A 2435 23081018 STARTER/GEN LUCAS BELL 407 407 SW ENGINE FAILED A B65A K NONE O OTHER IN INSP/MAINT 1 GL 13 407CR 406 98012 53254 STARTER/GENERATOR FAILED WITH 405.6 HOURS TT. BRUSH LENGTH FAIR TO GOOD. NOT OIL OR FUEL SOAKED. BEARINGS OK. SUBMIT TER SUGGESTED POSSIBLE INTERNAL SHORTING. 1 G 7 1 3U O H2SW 1999121101034 19991211 01034 CE 1999 12 11 99ZZZX4416 1 19991118 A 3233 23271001 ACTATOR LEAR 25 25 5170506 CE LT MLG LEAKING A DQIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 45BK 13860 14639 317 036 AIRCRAFT WAS ON FINAL APPROACH TO LAND WHEN GEAR WAS SELECTED DOWN. CREW REALIZED NO HYDRAULIC PRESSURE. DECLARED AN E MERGENCY. BLEW THE GEAR DOWN. LANDED WITHOUT INCIDENT. LOCAL MAINTENANCE DETERMINED WHEN GEAR WAS RETRACTED, HYDRAULI C FLUID LEAKED PAST SEALS IN LEFT MAIN GEAR ACTUATOR. 2 L 7 2 4J A10CE 1999121101040 19991211 01040 NE 1999 12 11 99ZZZX4423 2 19991111 A 8500 ENGINE DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE RIGHT MAKING METAL A VLLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 9923S 5927 930 25964 67946 AFTER DEPARTURE FROM MWO, RIGHT ENGINE OIL TEMPERATURE INCREASED AND OIL PRESSURE DROPPED TO REDLINE. AIRCRAFT RETURNED TO MWO. METAL FOUND IN OIL SCREEN. SUBMITTER SUSPECTED A FAILED MASTER ROD BEARING. 2 L 7 2 4R 4 R A669 5E4 1999121101043 19991211 01043 NE 1999 12 11 99ZZZX4426 1 19991013 A 2611 303267 AMPLIFIER SKRSKY S76 S76A 8143006 NE SMOKE DETECTOR MALFUNCTIONED A ALGA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 03 769AL 760048 IN-FLIGHT, SMOKE DETECTOR BAGGAGE LIGHT ILLUMINATED. AIRCRAFT DIVERTED AND LANDED WITH NO INCIDENT. NO FIRE OR SMOKE W AS NOTED. REPLACED SMOKE AMP. 1 G 7 2 3U H1NE 1999121101044 19991211 01044 SW 1999 12 11 99ZZZX4427 1 19991021 A 6510 407340340101 DISC PACK BELL 407 407 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL 25 RNFS3349 53264 DURING 25-HOUR AD INSPECTION. DURING DAILY INSPECTION. DISC PACK FOUND CRACKED WITH CRACK FACING AFT TOWARDS TAIL ROTO R IN NR 3 POSITION, CAUSE NOT KNOWN. ONLY ONE SEGMENT WAS FOUND CRACKED. 1 G 7 1 3U O H2SW 1999121101047 19991211 01047 CE 1999 12 11 99ZZZX4430 1 19991008 A 3230 08421022 BELLCRANK CESSNA 310 310P 2074238 CE NLG FAILED A S A XG9A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 5768M 3315 310P0068 AFTER TAKEOFF, PILOT RETRACTED GEAR. HE HEARD A LOUD BANG UNDER HIS FEET, AND SELECTED GEAR DOWN. HE NOTICED IN THE MI RROR THE NOSE GEAR WAS NOT DOWN AND LOCKED. AFTER NUMEROUS ATTEMPTS TO BRING THE GEAR DOWN, HE MADE A SUCCESSFUL LANDIN G, BUT THE NOSE GEAR COLLAPSED ON TOUCH DOWN. PART HAD 3,315.2 HOURS TT. PART HAD 78 HOURS SINCE IT WAS VISUALLY INSPE CTED AT ANNUAL. SUBMITTER RECOMMENDED REMOVAL AND NDI EVERY 500 HOURS; REPLACEMENT AT 2,500 HOURS. 1 L 7 2 3O 3A10 1999121101051 19991211 01051 CE 1999 12 11 99ZZZX4434 1 19991108 A 5540 541248118 BRACKET LEAR 55 55LEAR 5170702 CE RUDDER CRACKED A A EXOA K NONE O OTHER IN INSP/MAINT 1 SO 17 59HJ 6627 027 DURING REPLACEMENT OF A YAW DAMPENER SERVO, LOWER RUDDER SUPPORT BRACKET WAS FOUND CRACKED AT BOTH LIGHTENING HOLES. TH E CRACKS HAD PROGRESSED ALMOST TO TORQUE TUBE BEARING FITTING. SUBMITTER SUSPECTED LACK OF USE OF RUDDER GUST LOCK AS C AUSE, AS THIS IS AREA WHERE PRIMARY RUDDER STOPS ARE LOCATED. 2 L 7 2 4F A10CE 1999121101061 19991211 01061 CE 1999 12 11 99ZZZX4444 1 19991025 A 7931 ST4H TRANSMITTER LEAR 35 35A 5170602 CE LT ENGINE FLUCTUATED A BSYA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 07 684HA 17954 113 CMH - LEFT RING OIL PRESSURE FLUCTUATING. RETURNED TO COLUMBUS. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. OPS CH ECKED GOOD. 2 L 7 2 4F A10CE 1999121101062 19991211 01062 CE 1999 12 11 99ZZZX4445 1 19991117 A 2910 FITTING LEAR 25 25D 5170514 CE HYDRAULIC SYSTEM LEAKING A KKFA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 23 75CK 256 AFTER AN UNEVENTFUL LANDING, THE FLIGHT CREW NOTED HYDRAULIC FLUID LEAKING FROM THE AIRCRAFT BELLY. MAINTENANCE PERSONN EL DISCOVERED A LOOSE JAM NUT ON A FITTING ON THE INBOARD GEAR DOOR SELECTOR VALVE. JAM NUT WAS TIGHTENED, SYSTEM LEAK CHECK WAS SATISFACTORY. RESERVOIR SERVICED AND HYDRAULIC SYSTEM TESTED. 2 L 7 2 4J A10CE 1999121101063 19991211 01063 NM 1999 12 11 AALA991503 1 19991005 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 716AA 20608 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101064 19991211 01064 NM 1999 12 11 AALA991434 1 19990922 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM SERVICE DOORWAY DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729AA 20736 IAH - DURING OVERNIGHT CHECK, FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD SERVICE DOOR EMER GENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101065 19991211 01065 NM 1999 12 11 AALA991589 1 19991021 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT RIGHT AFT LAVATORY INOPERATIVE. REPLACED WIRE ON RIGHT AFT LAVATORY EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101066 19991211 01066 NM 1999 12 11 AALA991397 1 19990915 A 3350 1001141 LIGHT GRIMES BOEING 727 727227 1384078 NM AFT AIRSTAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 8952 20611 TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EXI T LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101067 19991211 01067 EA 1999 12 11 ASOA99128 1 19991026 A 3350 0L3071BPEGPL LAMP CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 820AS 7188 DURING INSPECTION, CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY CEILING LIGHTING SYSTEM LAMP. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999121101068 19991211 01068 NM 1999 12 11 USAASB99259 1 19991026 A 5610 PPG5893543110 WINDSHIELD BOEING 737 737301 1384611 NM FLT COMPARTMENT CRACKED A USAA A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 EA 19 336US 23233 CLT - FLT 1217 - EN ROUTE FROM PIT TO DFW, AT FL350, CREW HEARD A LOUD POPPING NOISE. CAPTAIN NOTICED THE FIRST OFFICER S NR 1 WINDSHIELD HAD MULTIPLE CRACKS AND WAS ARCING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO E MERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS NR 1 WINDSHIELD PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999121101069 19991211 01069 WP 1999 12 11 USAAD99153 1 19991026 A 3350 14597101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 CLT - THE FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999121101070 19991211 01070 NM 1999 12 11 USAASB99257 1 19991022 A 2751 INDICATION BOEING 737 7372B7 1384560 NM TE FLAPS MALFUNCTIONED A USAA O OTHER N FALSE WARNING DE DESCENT 1 EA 19 270AU 22882 TPA - FLT 2637 - UPON SELECTING FIVE DEGREES FLAP SETTING ON APPROACH, THE FLAP INDICATOR NEEDLES SPLIT AND THE FLAPS FR OZE AT ONE DEGREE FLAPS. AN EMERGENCY WAS DECLARED. FLIGHT LANDED AT A HIGHER THAN NORMAL LANDING SPEED BUT OTHERWISE HAD A NORMAL LANDING IN TPA. MAINTENANCE CHECKED AND RAN FLAPS SEVERAL TIMES. UNABLE TO DUPLICATE CONDITION. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1999121101071 19991211 01071 NM 1999 12 11 USAA991173 1 19991019 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 47003 22755 BOS - DURING WALKAROUND, FOUND 3 INCH SKIN CRACK AT STATION 727B AT SIDE AT WL 208 FLOORBEAM. INSTALLED DOUBLER AT STAT ION 727 A/B AND WL 208 PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999121101072 19991211 01072 NM 1999 12 11 USAA991161 1 19991023 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1050 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 46674 22754 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A CRACKED STRINGER AT STATION 1050 STRINGER 9L. ACCOMPLISHED REPAIR PE R SRM 53-10-3 FIG 2. (M) 2 L 7 2 4F A16WE 1999121101073 19991211 01073 NM 1999 12 11 USAA991162 1 19991023 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 46674 22754 TPA - DURING CX-3 CHECK EDDY CURRENT INSPECTION, FOUND 6 SMALL CRACKS EXTENDING FROM RIVETS IN AFT FASTENERS ROW PRESSUR E BULKHEAD WEB STATION 1016 STRINGER 6L. ACCOMPLISHED REPAIR PER EA 65955. (M) 2 L 7 2 4F A16WE 1999121101074 19991211 01074 NM 1999 12 11 USAASB99256 1 19991022 A 2913 6507506 PUMP BOEING 737 737201 1384454 NM NR 2 ENGINE FAILED A USAA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 EA 19 223US 10911 21665 CLT - FLT 929 - EN ROUTE FROM ORF-CLT, CREW REPORTED THEY HAD LOST 'A' SYSTEM HYDRAULICS AS LOW PRESSURE HYDRAULIC LIGHT S ILLUMINATED AND ZERO HYD QTY WAS INDICATED. CREW ACCOMP CHECKLIST AND PROCEEDED ONTO CLT. FLI LANDED WITHOUT INCIDEN T AND TAXIED OFF THE RUNWAY WITH NO PROBLEMS. AIRCRAFT WAS THEN TOWED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTEN ANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-11-32. REPLACED 'A' SYSTEM PRESSURE AND RETUR N FILTERS AND CASE DRAIN FILTERS. ALSO, REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYD PUMP AND STANDBY PUMP FILTERS. NO METAL NOTED. SERVICED RESERVOIR. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999121101075 19991211 01075 NM 1999 12 11 USAA109908 1 19991029 A 2781 H1010271 SWITCH BOEING 727 727227 1384078 NM NR 8 SLAT INOPERATIVE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 927TS 20837 FLT 6431 - LGA-DCA - DURING FLAP RETRACTION TO 0 DEGREES, LEADING EDGE FLAP AMBER DISAGREEMENT LIGHT STAYS ON. NR 8 SLA T INDICATED EXTENDED AT 0 DEGREES AND 2 DEGREES FLAP SETTINGS. REPLACED NR 8 FLAP EXTEND POSITION SWITCH. OPS CHECKS O K PER MM 27-81-32 PAGE 407. (M) 2 L 7 3 4F A3WE 1999121101076 19991211 01076 NM 1999 12 11 TWRA9969 1 19991025 A 3350 3004181A LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 624FF 2206 21439 DURING 'A' CHECK, FOUND R1, R2, R4, R5 DOOR BUSTLE LIGHTS NEED TO BE CHECKED WHEN INSTALLED. R1, R4, R5 BUSTLE LIGHTS C HECKED OK. R2 REMOVED AND REPLACED BUSTLE LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (M) 2 L 7 4 4F A20WE 1999121101077 19991211 01077 NM 1999 12 11 TWRA9968 1 19991025 A 3350 3004083 LIGHT BOEING 747 747212B 1384886 NM EMER EXIT INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 624FF 62701 21439 DURING 'A' CHECK, FOUND OVERWING LIGHT LEFT SIDE SECOND FROM TOP BULB OUT. REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1999121101078 19991211 01078 NM 1999 12 11 UIEA9989 1 19991011 A 2612 FIRE WARNING BOEING 747 7472D7B 1384803 NM APU ACTIVATED A UIEA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 527MC 22471 FLT GT394 - CTS-ANC - DURING CRUISE, APU 'A' LOOP FIRE WARNING ILLUMINATED INTERMITTENTLY, WARNIGN HORN DID NOT SOUND. A PU FIRE WARNING WAS SELECTED TO THE BOTH POSITION. SYSTEM CHECK WAS PERFORMED AND 'B' LOOP FAILED TEST. 'A' LOOP WAS S ELECTED AND TESTED OK, HOWEVER, LATER THE APU FIRE WARNING ONCE AGAIN SOUNDED VERY BRIEFLY. CREW PERFORMED APU FIRE CHE CKLIST AND DISCHARGED APU FIRE BOTTLE. ATC NOTIFIED. NO FIRE HAD ACTUALLY OCCURRED. ANC MAINTENANCE WAS UNABLE TO DUP LICATE DISCREPANCY. APU FUEL VALVE LOCKED CLOSED AND ITEM DEFERRED AS MEL ITEM 49-1 AND 26-08. REPLACED FIRE EXTINGUIS HER BOTTLE AND SQUIB AND RESEATED FIRE WARNING CARD. REACTIVATED FUEL VALVE. APU AND APUF FIRE WARNIGN SYSTEM OPERATI 2 L 7 4 4F RT A20WE 1999121101079 19991211 01079 NM 1999 12 11 UIEA9988 1 19991008 A 2611 SMOKE DETECTOR BOEING 747 74747UF 1384949 NM CABIN INOPERATIVE A UIEA C H ABORTED TAKEOFF DEACTIVATE SYST/CIRCUITS N FALSE WARNING TO TAKEOFF 1 EA 15 494MC 29255 FLT GT3573 - REJECTED TAKEOFF, AT APPROX 80 KNOTS, A MAIN DECK FIRE WARNING ALERT WAS ANNUNCIATED. THE CENTRAL MAINTENA NCE COMPUTER (CMC) SHOWED NR 1 ZONE MAIN DECK SMOKE DETECTORS 'A' AND 'B' AT FAULT. BOM, MAINTENANCE DEACTIVATED NR 1 Z ONE MAIN DECK SMOKE DETECTORS 'A' AND 'B' BY REMOVING THE ELECTRICAL CONNECTORS PER FLT CREW AND ATLAS AIR MAINTENANCE C ONTROL, JFK REQUEST. DISCREPANCY WAS DEFERRED PER MEL ITEM NR 26-14-1 AND AIRCRAFT RELEASE. REPLACED BOTH 'A' AND 'B' NR 1 ZONE SMOKE DETECTORS AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F RT 1384945 1999121101080 19991211 01080 NM 1999 12 11 UIEA9995 1 19991022 A 2750 1267629 PDU BOEING 747 74747UF 1384949 NM LT TE FLAP FAILED A UIEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 15 491MC 29252 FLT FX076 - HKG-ANC - ON DEPARTURE FROM HKG AT FL290, AUTO-PILOT AND AUTO-THROTTLE DISENGAGED AND WOULD NOT RE-ENGAGE. T RIED BOTH FMC'S, BUT NO HELP. RETURNED TO HKG AND ON APPROACH THERE WAS NO FLAP POSITION INDICATION. TRIED TO CONFIRM FLAP POSITION VISUALLY. FLAPS WERE NOT MOVING EXTENDED FLAP USING ALTERNATE METHOD. BOTH FLIGHT DIRECTORS DISENGAGED R EPEATEDLY. FLEW RAW DATA APPROACH. MAINTENANCE FOUND NR 3 LT PDU INOPERATIVE. REPLACED PDU AND PERFORMED FCU, FCC, FL IGHT DIRECTOR, AUTO PILOT AND FMC CHECKS AND ALL OPERATIONS NOW NORMAL. LOSS OF FLAPS BELIEVED DUE TO CYCLING OF ALTERN ATE FLAPS. DISCREPANCIES CLEARED AND AIRCRAFT RELEASED FOR DISPATCH. (M) 2 L 7 4 4F RT 1384945 1999121101081 19991211 01081 NM 1999 12 11 MZZA99188 1 19991028 A 2530 99259990001 OVEN BOEING 727 727224 1384076 NM AFT GALLEY FAILED A MZZA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 79743 22252 FLT 972 - AFTER PUSHBACK AIRCRAFT RETURN TO GATE DUE TO OVEN SMOKING IN THE AFT GALLEY. MAINTENANCE INSPECTED OVEN AND PLACARDED AFT GALLEY AFT FACING OVEN INOPERATIVE AND CIRCUIT BREAKER PULLED. RELEASED AIRCRAFT FOR SERVICE AND REDISPAT CHED. GUAM MAINTENANCE FOUND OVEN LEFT CAVITY FAN SEIZED UP. REMOVED AND REPLACED OVEN PER MM 25-31-07. OPS CHECKED N ORMAL. RELEASED AIRCRAFT FOR SERVICE. (M) 2 L 7 3 4F A3WE 1999121101082 19991211 01082 NM 1999 12 11 MZZA99185 1 19991005 A 3232 20704090101 ANTENNA BOEING 727 727264 138408M NM RADAR FAILED A MZZA A UNSCHED LANDING L NO TEST CL CLIMB 1 WP 13 624DH 20709 FLT 891 - MNL - RADAR FAILED IN FLIGHT CRWE RESET CIRCUIT BREAKERS IN FLIGHT, NO EFFECT. INDICATOR SHOW MANY SMALL DOTS ON SCREEN. DUMP FUEL AND AIR RETURN TO MANILLA. GOT GOOD TEST PATTERN ON THE GROUND. MAINTENANCE T/S SYSTEM AND FOUN D RADAR ANTENNA AT FAULT. REMOVED AND REPLACED RADAR ANTENNA AS PER MM 34-41-23. FUNCTIONAL CHECK SATISFACTORY AS PER 34-41-02. AIRCRAFT RELEASE FOR SERVICE WITH NO FURTHER INCIDENT. (M) 2 L 7 3 4F A3WE 1999121101083 19991211 01083 WP 1999 12 11 GTIA9901159 1 19991014 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947ML 47514 MLB - DURING DAILY, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BULB AND LENSE AND ROW 4. OPERATION CHECK NORMAL IAW 33-53-0. (M) 2 L 7 2 4F A6WE 1999121101084 19991211 01084 WP 1999 12 11 GTIA9901160 1 19991013 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 DTW - FLOOR TRACK LIGHTING INOPERATIVE, RED STRIP NEAR FORWARD GALLEY. RECONNECTED FLOOR TRACK LIGHTING NEAR FORWARD GA LLEY. SYSTEM OPERATION CHECKS GOOD IAW MM 33-53-00. (M) 2 L 7 2 4F A6WE 1999121101085 19991211 01085 WP 1999 12 11 GTIA9900118 1 19991029 A 3350 SA251 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 7140 47326 DTW - LEFT FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED B5-32 BATTERY PACK IAW MM 24-30-0. OPS CHEC K GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 1999121101086 19991211 01086 1999 12 11 99ZZZM795 4 19991012 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LEFT FAILED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 118UX 4551 UE118 CAPTAINS ALTIMETER REPORTED TO HAVE FLAGGED AND GONE INOPERATIVE. REMOVED AND REPLACED ALTIMETER. SUBSEQUENT BENCH TES T RESULTED IN 'NO FAULT FOUND'. (M) 2 L 7 2 4T RT A24CE 1999121101087 19991211 01087 NM 1999 12 11 F3LA99135 1 19991107 A 5312 BULKHEAD ANGLE BOEING 737 7372P6 NM BS 1016 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED AFT PRESSURE BULKHEAD ANGLE FOR FLOOR SEAL CRACKED ON LEFT SIDE AT STATION 1 016. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, FIG 1, SHEET 1-3. (M ) 2 L 7 2 4F RT A16WE 1999121101088 19991211 01088 NM 1999 12 11 F3LA99134 1 19991107 A 3230 RETRACT MECH BOEING 737 737317 138447P NM NLG OUT OF ADJUST A F3LA O OTHER J WARNING INDICATION AP APPROACH 1 NM 03 EICHH 23177 DEN - UPON ARRIVAL, FLIGHT CREW REPORTED NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN. RECYCLED GEAR HANDLE AND NOSE GEAR EXTENDED. MAINTENANCE RESHIMMED NLG LOCK MECHANISM, PERFORMED EXTENSION AND RETRACTION TEST, LUBRICATED N OSE LANDING GEAR AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999121101089 19991211 01089 NM 1999 12 11 EISA99149 1 19990801 A 2611 66233901 SMOKE SENSOR BOEING 727 72725 1384006 NM CABIN DIRTY A EISA K NONE N FALSE WARNING AP APPROACH 1 SW 07 290NE 18972 CARGO SMOKE ANNUNCIATOR ILLUMINATED IN FLIGHT, FALSE INDICATION. PURGED SYSTEM WITH DRY NITROGEN IAW MM 26-10. (M) 2 L 7 3 4F A3WE 1999121101090 19991211 01090 1999 12 11 EISA99148 4 19990729 A 3442 RADAR COLLINS BOEING 727 72731 1384010 NM COCKPIT FAILED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 240NE 18906 WEATHER RADAR WOULD NOT PAINT. WEATHER RADAR COMPONENTS REMOVED AND BENCHED CHECKED. REINSTALLED COMPONENTS, CHECKS OK PER MM 3440-20 REF EAGLE ONE WO ITEM 2.1.44. (M) 2 L 7 3 4F A3WE 1999121101091 19991211 01091 NM 1999 12 11 EISA99156 1 19990821 A 2611 302842 SMOKE DETECTOR BOEING 727 72725 1384006 NM NR 3 POSITION DEFECTIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 290NE 18972 REMOVED AND REPLACED NR 3 SMOKE DETECTOR. OPS CHECK GOOD PER MM CHAPTER 26. (M) 2 L 7 3 4F A3WE 1999121101092 19991211 01092 NM 1999 12 11 EISA99155 1 19990820 A 3350 1000679 LIGHT BOEING 727 7272A7 138407K NM COCKPIT DEFECTED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310NE 20241 REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT IAW MM 33-50. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999121101093 19991211 01093 NM 1999 12 11 EISA99153 1 19990808 A 2611 774001 DETECTOR BOEING 727 7272M7 138407S NM NR 4 ILLUMINATED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 721RW 3181 21200 SMOKE DETECTOR ILLUMINATES IN FLIGHT. REMOVED AND REPLACED NR 4 SMOKE DETECTOR IAW MM CHAPTER 26-10. NO DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 1999121101094 19991211 01094 NM 1999 12 11 EISA99150 1 19990803 A 3260 MS250111 SWITCH BOEING 727 72725 1384006 NM TAIL SKID SERVICEABLE A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 TAIL SKID WARNING ILLUMINATED IN FLIGHT AND WOULD NOT GO OUT. COMPLIED WITH EEMP SECTION. (M) 2 L 7 3 4F A3WE 1999121101095 19991211 01095 NM 1999 12 11 A6WA9900121 1 19991024 A 2430 220GC02Y02 1VE PANEL DORNER DO32 DO328100 2996000 NM COCKPIT FAILED A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 328PH 3006 FLT 7084 - GUC-DEN - ON TAXI, LEFT DC GENERATOR FAILED, SMOKE ENTERED CABIN. REMOVED AND AND REPLACED 1VE PANEL. (M) 2 H 7 2 4T RT A45NM 1999121101096 19991211 01096 NM 1999 12 11 A6WA9900120 1 19991025 A 2150 PACK DORNER DO32 DO328100 2996000 NM LEFT FAILED A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 338PH 3029 FLT 7119 - DEN-RAP - LEFT PACK FAIL, SOME LAV CAS MESSAGE, PACK OVERHEAR SMOKE/ODOR IN CABIN. REMOVED AND REPLACED NR 1 ENVIRONMENTAL CONTROL UNIT AND 87HB RELAY. (M) 2 H 7 2 4T RT A45NM 1999121101097 19991211 01097 WP 1999 12 11 AALA991608 1 19991007 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1214 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - NR 6 SEAT TRACK CORRODED AT STATION 1214. REPAIRED SEAT TRACK OF SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4A. (M ) 2 L 7 2 4F A6WE 1999121101098 19991211 01098 WP 1999 12 11 AALA991610 1 19991012 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 640-642 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - FOUND CORROSION ON NR 1 SEAT TRACK AT STATION 640-642. REMOVED CORRODED SECTION OF TRACK AND INSTALLED REPAIR PLU G PER SRM 53-05 PART 1, FIG 4A, SHEET 1. (M) 2 L 7 2 4F A6WE 1999121101099 19991211 01099 WP 1999 12 11 AALA991609 1 19991015 A 5320 CASTING DOUG DC9 DC982 3022082 WP BS 1155 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - AFT CARGO DOOR CUTOUT FORWARD LOWER CASTING CRACKED, STATION 1155 LONGERON 28R. REPLACED CASTING WITH NEWS CASTIN G PER SRM 51-01 PAGE 2. (M) 2 L 7 2 4F A6WE 1999121101100 19991211 01100 NM 1999 12 11 AALA991603 1 19991022 A 5712 RIB BOEING 727 727227 1384078 NM WS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - HFEC INDICATES CRACK IN RIB CHORD RADIUS INBOARD SIDE AT STATION 760R AT EDGE OF REPAIR DOUBLER. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SB 727-57-0112, DWG 65C33202 AND ESO 11697 DATED 10-20-99. (M) 2 L 7 3 4F A3WE 1999121101101 19991211 01101 NM 1999 12 11 AALA991602 1 19991021 A 5730 SKIN BOEING 727 727227 1384078 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - LOWER WING SKIN ABV RT PRIMARY HEAT EXCHANGE HAS AREA OF CORROSION FORWARD OF PREVIOUS REPAIR. INSTALLED DOUBLER/ TRIPLER PER SRM 57-30-3. (M) 2 L 7 3 4F A3WE 1999121101102 19991211 01102 NM 1999 12 11 AALA991601 1 19991021 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FOUND LOWER WING SKIN ABV LEFT PRIMARY HEAT EXCHANGER HAS AREA OF CORROSION. INSTALLED DOUBLER/TRIPLER PER SRM 57 -30-3. (M) 2 L 7 3 4F A3WE 1999121101103 19991211 01103 NM 1999 12 11 AALA991600 1 19991022 A 5712 RIB BOEING 727 727227 1384078 NM BS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - LEFT RIB CHORD CRACKED IN RADIUS UNDER DOUBLER STATION 760L. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLE D IAW SB 727-57-0112 DWG 65C3302 ESO 11697 DATED 10-20-99. (M) 2 L 7 3 4F A3WE 1999121101104 19991211 01104 NM 1999 12 11 AALA991599 1 19991022 A 5330 SKIN BOEING 727 727227 1384078 NM BS 680-695 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FUSELAGE SKIN BULGING BETWEEN FASTENERS ON SKIN LAP STRINGER 19R FS 680-695. CUTOUT CORRODED SKIN AND INSTALLED D OUBLER PER SRM 53-30-3 PAGE 1. (M) 2 L 7 3 4F A3WE 1999121101105 19991211 01105 EU 1999 12 11 UF6A991101 1 19991101 A 2421 BA03304 GENERATOR BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 31 859AW 12109 2036 GRB - FLT 5738 - DURING TAKEOFF ROLL, THE NR 1 GENERATOR FAILED WITH 'GEN 1' CWP ILLUMINATED. MAINTENANCE REMOVED AND R EPLACED THE NR 1 GENERATOR. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999121101106 19991211 01106 EU 1999 12 11 UF6A991102 1 19991102 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 12109 2035 ORD - THE LEFT EXTERIOR EMERGENCY EXIT LIGHT IS INOP. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999121101107 19991211 01107 NE 1999 12 11 UF6A991103 2 19991104 A 7261 3034508 FILTER BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE DIRTY A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 858AW 2035 124394 CAK - FLT 5712 - THE NR 1 ENGINE OIL FILTER CWP ILLUMINATED DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE OIL PR ESSURE AND SCAVENGE FILTERS. POWER ASSURANCE RUNS WERE PERFORMED AND ALL PARAMETERS WERE FOUND TO BE WITHIN LIMITS. ( M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1999121101108 19991211 01108 NM 1999 12 11 MASA99165 1 19991013 A 5210 85210127051 CABLE DHAV DHC8 DHC8202 2809007 NM AIRSTAIR DOOR OUT OF POSITION A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 454YV 454 FLT 6360 - PHX-TEX - THE AIRCRAFT HAD AN AIRSTAIR DOOR THAT WOULD NOT OPEN AFTER ARRIVAL IN PHX. MAINTENANCE WAS CALLED OUT AND THEY OPENED THE DOOR AND THEN REINSTALLED THE COUNTER BALANCE CABLE BACK ON THE PULLEY. OPS CHECKED GOOD AND T HE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999121101109 19991211 01109 EU 1999 12 11 AALA991605 1 19991023 A 2150 A42713429 PANEL FOKKER F28 F28MK0100 4990807 EU COCKPIT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1467A FBE0015 11499 CLT - FLT 803 - FIVE MINUTES AFTER DEPARTURE CLT A STRONG MOMENTARY SMELL OF ELECTRICAL FIRE ACCOMPANIED BY A PUFF OF SM OKE WAS NOTICED BY CREW. APPROXIMATELY TWO MINUTES LATER ANOTHER MOMENTARY SMELL OF ELECTRICAL FIRE WAS NOTED. NO INDI CATIONS ON MFDU, NO CIRCUIT BREAKER POPPED. NO ABNORMAL INDICATIONS WERE NOTED. RETURNED TO CLT. SMELL DID NOT RETURN FOR LAST TEN MINUTES OF FLIGHT. LANDED CLT WITHOUT INCIDENT. INSPECTED AIRCRAFT AND CONDUCTED FERRY FLIGHT TO ORD WIT HOUT INCIDENT. REPLACED AIR CONDITIONING CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999121101110 19991211 01110 NM 1999 12 11 AALA991612 1 19991026 A 3350 CONNECTOR BOEING 757 757223 1384957 NM ROW 16D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 637AM 24595 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SIDE OF SEAT 16D WILL NOT TEST. RECONNECTED SEAT TO WALL CO NNECTOR FOR SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999121101111 19991211 01111 NM 1999 12 11 AALA991613 1 19991026 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 9H LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380AN 25449 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON SIDE OF SEAT 9H INOPERATIVE. RESEATED SEAT EMERGENCY EXIT L IGHT CONNECTOR FOR SEAT 9H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121101112 19991211 01112 NM 1999 12 11 AALA991595 1 19991023 A 3350 P4010051112 LIGHT BOEING 767 767323 1385205 NM ROW 23B INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 376AN 25445 SFO - DURING OVERNIGHT MAINTENANCE, SEAT 23B EMERGENCY EXIT SEAT PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SEAT L IGHT ASSEMBLY AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121101113 19991211 01113 NM 1999 12 11 AALA991596 1 19991024 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 679AN 29589 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS SECTION INOPERATIVE. REPAIRED EME RGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999121101114 19991211 01114 NM 1999 12 11 AALA991581 1 19991020 A 3350 SOCKET BOEING 757 757223 1384957 NM ROW 16-25 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 629AA 24587 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM 16D TO 25D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999121101115 19991211 01115 NM 1999 12 11 AALA991585 1 19991020 A 3350 P2070001213 FLASHLIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358AA 24039 SFO - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT 3L DOOR INOPERATIVE. REPLACED FLIGHT ATTEN DANT EMERGENCY FLASHLIGHT AT 3L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121101116 19991211 01116 NM 1999 12 11 AALA991586 1 19991021 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 32B BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AA 25196 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 32B THROUGH 41B INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT 38B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121101117 19991211 01117 NM 1999 12 11 AALA991587 1 19991021 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 32D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 693AA 26973 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 32D EMERGENCY EXIT PATH LIGHTING INOPERATIVE. REPLACED SEAT 32D EMERGENCY EXIT PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999121101118 19991211 01118 NM 1999 12 11 AALA991299 1 19990828 A 3350 CONNECTOR BOEING 727 727227 1384078 NM CABIN MISWIRED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 726AA 20733 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT F LOOR PATH LIGHTING CONNECTOR THAT WAS FOUND INSTALLED WITH REVERSE POLARITY. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 3 4F A3WE 1999121101119 19991211 01119 WP 1999 12 11 AALA991623 1 19991028 A 3222 6F2314 VALVE DOUG DC9 DC982 3022082 WP NLG STRUT LEAKING A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 7532A 49924 DFW - FLT 1966 - AFTER TAKEOFF, EN ROUTE AUS-DFW, NOSE GEAR DID NOT RETRACT. CYCLED NOSE GEAR ONCE WITHOUT SUCCESS. LE FT THE NOSE WHEEL GEAR DOWN AND MAIN GEAR RETRACTED FOR REST OF THE FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE STRUT SCHRADER VALVE AND SEAL, SERVICED NOSE STRUT, AND ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (M) 2 L 7 2 4F A6WE 1999121101120 19991211 01120 WP 1999 12 11 AALA991593 1 19991002 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 494AA 49732 PHX - DURING OVERHEAT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 8 THROUGH 20 INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121101121 19991211 01121 WP 1999 12 11 AALA991592 1 19991022 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 07 403A 49314 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD FLIGHT ATTENDANT PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD FLI GHT ATTENDANT PORTABLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121101122 19991211 01122 WP 1999 12 11 AALA991598 1 19991024 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 27D BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 416AA 49327 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM SEAT 27D TO AFT OF AIRCRAFT INOPERATIVE. REPA IRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121101123 19991211 01123 WP 1999 12 11 AALA991597 1 19991024 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 442AA 49468 BOS - DURING OVERNIGHT MAINTENANCE, SEAT 3E FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. TIGHTENED FORWARD E MERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121101124 19991211 01124 WP 1999 12 11 AALA991582 1 19991020 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP AFT STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 461AA 49566 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD AFT AIRSTA IRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121101125 19991211 01125 WP 1999 12 11 AALA991583 1 19991020 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505AA 49799 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY FLIGHT ATTENDANT PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWA RD ENTRY LIGHT ATTENDANT PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121101126 19991211 01126 WP 1999 12 11 AALA991584 1 19991020 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY FLIGHT ATTENDANT PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWA RD ENTRY FLIGHT ATTENDANT PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121101127 19991211 01127 NM 1999 12 11 AALA990881 1 19990616 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 712AA 22468 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT EXIT ROW 18 INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 3 4F A3WE 1999121101128 19991211 01128 NM 1999 12 11 AALA991430 1 19990622 A 3350 1000679 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 869AA 11035 21374 TPA - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR DOES NOT TEST. REPLACED EMERGENCY EXIT LI GHT ABOVE AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101129 19991211 01129 NM 1999 12 11 AALA991076 1 19990722 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 709AA 23427 22466 LGA - FLT 1886 - DURING LANDING AT LGA COCKPIT EMERGENCY EXIT LIGHTS ILLUMINATED AND REMAINED ILLUMINATED WITH SWITCH TU RNED OFF. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101130 19991211 01130 NM 1999 12 11 AALA991075 1 19990722 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 707AA 22464 MIA - DURING OVERNIGHT MAINTENANCE, EMERGNCY EXIT FLOOR PATH LIGHTING FROM ROWS 25 TO 28 DEF INOPERATIVE. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101131 19991211 01131 NM 1999 12 11 AALA991086 1 19990725 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 886AA 21525 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWELL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIRWELL EMERGENCY EX IT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101132 19991211 01132 NM 1999 12 11 AALA991105 1 19990727 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 850AA 20991 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. RESECURED WIRE TO EMERGENCY EXIT FL OOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101133 19991211 01133 NM 1999 12 11 AALA991139 1 19990804 A 3397 WIRE BOEING 727 727223 1384074 NM ROW 9 OUT OF POSITION A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 892AA 22008 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERHEAD AISLE LIGHT AT ROW 9 INOPERATIVE. REPOSITIONED WIRE ON BATTERY T ABS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101134 19991211 01134 NM 1999 12 11 AALA991271 1 19990822 A 3350 CONNECTOR BOEING 727 727223 1384074 NM AFT AIRSTAIR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 TUL - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED CONNECTOR TO AFT A IRSTAIR EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101135 19991211 01135 NM 1999 12 11 AALA991290 1 19990827 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 890AA 22006 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 17D, 20D, AND 24D INOPERATIVE. REPLACED C ONNECTORS TO EMERGENCY EXIT FLOOR PATH LIGHTS STRIPS AT SEATS 17D, 20D, AND 24D. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 3 4F A3WE 1999121101136 19991211 01136 NM 1999 12 11 AALA991292 1 19990828 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 894AA 22010 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BY AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101137 19991211 01137 NM 1999 12 11 AALA991304 1 19990901 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 715AA 22470 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE FROM AFT OF FIRST CLASS CABIN TO FORWAR D OVERWING EXIT DOOR. REPLACED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN FIRST CLASS CABIN AND FORWARD OV ERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101138 19991211 01138 NM 1999 12 11 AALA991331 1 19990907 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT AIRSTAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 865AA 5533 21370 TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS OVE RHEAD EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101139 19991211 01139 NM 1999 12 11 AALA991353 1 19990908 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 889AA 21527 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EXI T LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101140 19991211 01140 NM 1999 12 11 AALA991374 1 19990911 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 850AA 20991 TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN CABIN INOPERATIVE. REPAIRED WIRING FROM BATTERY PACK TO EMERGENCY EXIT FLOOR PATH LIGHTS AT BULKHEAD FORWARD OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 3 4F A3WE 1999121101141 19991211 01141 NM 1999 12 11 AALA991378 1 19990911 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 879AA 21391 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT MID CABIN CABIN INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHTING STRIP AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101142 19991211 01142 NM 1999 12 11 AALA991380 1 19990912 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 892AA 22008 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT LIGHTING IN CABIN INOPERATIVE. RECONNECTED WIRING T O EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101143 19991211 01143 NM 1999 12 11 AALA991386 1 19990913 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843AA 20984 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. REPLACED CONNECTOR TO EMERGENCY FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101144 19991211 01144 NM 1999 12 11 AALA991388 1 19990913 A 3350 LIGHT BOEING 727 727223 1384074 NM VENTRAL STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 709AA 22466 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHT AT VENTRAL STAIRS INOPERATIVE. CLEANED AND ADJUSTED E LECTRICAL CONTACTS OF BATTERY/CHARGER TO EMERGENCY EXIT OVERHEAD LIGHT AT VENTRAL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101145 19991211 01145 NM 1999 12 11 AALA991401 1 19990915 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 849AA 20990 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. RESECURED CONNECTOR TO E MERGENCY FLOOR PATH LIGHTING IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101146 19991211 01146 NM 1999 12 11 AALA991403 1 19990918 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT STAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 705AA 22462 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101147 19991211 01147 NM 1999 12 11 AALA991427 1 19990921 A 3350 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT FUSELAGE DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 884AA 21523 MIA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED ELECTRICAL CONTACTS TO BATT ERY FOR AFT AIRSTAIRS EMERGNCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101148 19991211 01148 NM 1999 12 11 AALA991443 1 19990921 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN EMERGENCY EXIT ROWS INOPERATIVE. REPAIR ED EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101149 19991211 01149 NM 1999 12 11 AALA991479 1 19991001 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT STAIRS FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 871AA 8430 21383 TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS THRESHOLD EMERGENCY EXIT LIGHT WOULD NOT TEST. REPLACED AFT AIRSTAIRS THRESHOLD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101150 19991211 01150 NM 1999 12 11 AALA991510 1 19991006 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 18 DEF THROUGH 20 DEF INOPERATIVE. REPAIR ED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101151 19991211 01151 NM 1999 12 11 AALA991528 1 19991012 A 3350 A3060720101 CONDUCTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 867AA 21372 MIA - AISLE EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN FIRST CLASS AND COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING FLAT CONDUCTOR BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101152 19991211 01152 NM 1999 12 11 AALA991591 1 19991023 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR VENTRAL EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIR VENTRAL EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101153 19991211 01153 NM 1999 12 11 AALA991594 1 19991024 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 703AA 22461 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR VENTRAL EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIR VENTRAL EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101154 19991211 01154 NM 1999 12 11 AALA991611 1 19991025 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 847AA 20988 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. RECONNECTED EMERGENC Y EXIT FLOOR PATH LIGHT CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999121101155 19991211 01155 NM 1999 12 11 EISA99147 1 19990728 A 5210 MECHANISM BOEING 727 72725 1384006 NM PAX DOOR NOT LATCHED A EISA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 300NE 18974 FORWARD ENTRY DOOR NOT CLOSED PROPERLY, COULD NOT PRESSURIZE AIRCRAFT. OPENED DOOR AND CLOSED PROPERLY. (M) 2 L 7 3 4F A3WE 1999121101156 19991211 01156 NM 1999 12 11 EISA99140 1 19990625 A 3260 ZZBAC171624P CONNECTOR BOEING 727 727223 1384074 NM RT MLG DIRTY A EISA K NONE N FALSE WARNING LD LANDING 1 SW 07 6826 CM159 19704 UPON GEAR EXTENSION THE RIGHT MAIN GEAR (RED) WARNING LIGHT ILLUMINATED. PERFORMED ABNORMALS SECTION 3 PAGE 50 PROCEDUR E UNEVENTFUL LANDING. CLEANED AND REPOSITIONED CONNECTOR TO LANDING GEAR ACCY BOX AND PERFORMED TEST IAW MM 32-61-01. O PS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999121101157 19991211 01157 1999 12 11 EISA99142 4 19990713 A 3442 20871790501 ANTENNA BENDIX BOEING 727 72725 1384006 NM FWD FUSELAGE OUT OF ADJUST A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 300NE 2005 18974 RADARS SPOKING AND WOULD NOT PAINT TARGETS. REPLACED CONTROL PANEL, REPLACED RADOME INSTALLED WAVE GUIDE WINDOW. CHECK ED AND ADJUSTED ANTENNA PITCH. CLEANED RADOME BONDING WIRE TO AIRCRAFT. (M) 2 L 7 3 4F A3WE 1999121101158 19991211 01158 WP 1999 12 11 EISA99206 1 19991011 A 2560 11331DGDME SLIDE BFGOODRICH DOUG DC9 DC931 3022065 WP GALLEY DOOR LOOSE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 GALLEY DOOR SLIDE PACK FELL OFF OF DOOR. REINSTALLED AND SECURED SLIDE PACK TO RIGHT FORWARD GALLEY DOOR IAW 25-62-00, PATE 201-204. (M) 2 L 7 2 4F A6WE 1999121101159 19991211 01159 NM 1999 12 11 EISA99208 1 19991020 A 3397 WIRE BOEING 727 727231 1384079 NM COCKPIT DAMAGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 74318 20051 ALL EMERGENCY LIGHTS INOPERATIVE. REPAIRED DAMAGED WIRES BEHIND CONTROL PANEL, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1999121101160 19991211 01160 NM 1999 12 11 EISA99209 1 19991019 A 5210 MECHANISM BOEING 727 727223 1384074 NM L1 DOOR FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6813 19488 AIRCRAFT LOST PRESSURIZATION, DIVERTED TO BRU AT 0200Z) UNABLE TO OPEN L1 DOOR. (M) 2 L 7 3 4F A3WE 1999121101161 19991211 01161 NM 1999 12 11 EISA99205 1 19990914 A 5530 65168024 FITTING BOEING 727 727223 1384074 NM VERT STAB CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND 1 INCH CRACK IN VERTICAL FIN SPAR TERMINAL FITTING RIGHT SIDE . REMOVED DAMAGED FITTING REPLACED WITH NEW FITTING PER SB 55-0060 AND BAC BLUEPRINT 65-89361. (M) 2 L 7 3 4F A3WE 1999121101162 19991211 01162 NM 1999 12 11 EISA99204 1 19991005 A 5530 65168023 FITTING BOEING 727 727223 1384074 NM VERT STAB MISDRILLED A EISA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 315NE 20190 DURING REPLACEMENT OF VERTICAL FIN FRONT SPAR UPPER RIGHT TERMINAL FITTING AND SUBSEQUENT REMOVAL OF PREVIOUS REPAIR FOU ND MIS-DRILLED HOLES IN LEFT HAND TERMINAL FITTING. REMOVED AND REPLACED LEFT TERMINAL FITTING PER SB 55-0060 AND BAC D RAWING 65-89361. (M) 2 L 7 3 4F A3WE 1999121101163 19991211 01163 NM 1999 12 11 EISA99203 1 19991005 A 5730 SKIN BOEING 727 727223 1384074 NM WS 460-650 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON RIGHT WING LOWER SURFACE FROM WS 460 TO 650 AROUND FASTENERS. REMOVED CORROSION AND MATERIAL LOSS OUT OF LIMITS PER SRM 57-30-1, FABRICATED AND INSTALLED DOUBLER PER FLI GHT VEHICLES CONSULTING, INC EO NR 57-99455 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121101164 19991211 01164 NM 1999 12 11 EISA99202 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 348 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 348, STRINGER 25R. FABRICATED NEW TIE C LIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121101165 19991211 01165 NM 1999 12 11 EISA99201 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 277 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 277, STRINGER 25R. FABRICATED NEW TIE C LIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121101166 19991211 01166 NM 1999 12 11 EISA99200 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 400 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 400 STRINGER 26L. FABRICATED NEW TIE CL IP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121101167 19991211 01167 NM 1999 12 11 EISA99199 1 19990914 A 5753 SKIN BOEING 727 727223 1384074 NM RT TE AFT FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND DELAMINATION AT TRAILING EDGE OF RIGHT INBOARD AFT FLAP. REM OVED DAMAGED AREA. INSTALLED NEW HONEYCOMB CORE PER SRM 51-40-6 AND FIBERGLASS OVERLAY PER SRM 51-40-6. PRIMED AND PAI NTED PER MM 51-20-151. (M) 2 L 7 3 4F A3WE 1999121101168 19991211 01168 NM 1999 12 11 EISA99198 1 19990914 A 5753 SKIN BOEING 727 727223 1384074 NM RT TE MID FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND RIGHT INBOARD MID FLAP DELAMINATED AT TRAILING EDGE AT WBL 20 0. REMOVED DAMAGED SKIN PER SRM 51-40-6. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. (M) 2 L 7 3 4F A3WE 1999121101169 19991211 01169 NM 1999 12 11 EISA99197 1 19990914 A 5753 SKIN BOEING 727 727223 1384074 NM RT TE FOREFLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CRACK AT INBOARD OF RIGHT INBOARD FOREFLAP. REMOVED DAMAGED AREA, REPAIRED INBOARD TIP WITH POTTING COMPOUND PER SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1999121101170 19991211 01170 NM 1999 12 11 EISA99196 1 19990914 A 5730 SKIN BOEING 727 727223 1384074 NM BS 805 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 2 FUEL TANK LOWER SURFACE AT FS 800 RBL 18. R EMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS PER SRM 57-10-1. FABRICATED REPAIR DOUBLER PER SRM 57-30-3. TREATED AND PRIMED REPAIR PARTS PER SRM 51-10-2 AND MM 51-20-2. INSTALLED DOUBLER PER SRM 57-30-3, FIG 4. (M) 2 L 7 3 4F A3WE 1999121101171 19991211 01171 NM 1999 12 11 EISA99195 1 19990914 A 5330 SUPPORT BOEING 727 727223 1384074 NM BS 805 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION AT FS 805 WING CENTER FUEL TANK ABOVE AFT END OF RI GHT HEAT EXCHANGER ON STRUCTURE SUPPORT OUTBOARD SURFACE. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. FABRICATED D OUBLER PER SRM 51-40-2. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1999121101172 19991211 01172 NM 1999 12 11 EISA99194 1 19990914 A 5730 SKIN BOEING 727 727223 1384074 NM BS 805 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND CORROSION ON NR 2 FUEL TANK LOWER SURFACE AT FS 805, LBL 18. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS PER SRM 57-10-1. FABRICATED REPAIR PER SRM 57-30-3, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED REPAIR PER SRM 57-30-3 FIG 4. (M) 2 L 7 3 4F A3WE 1999121101173 19991211 01173 NM 1999 12 11 EISA99193 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 480 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 23L. FABRICATED NEW TIE CL IP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121101174 19991211 01174 NM 1999 12 11 EISA99192 1 19990914 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 480 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 22L. FABRICATED NEW TIE CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121101175 19991211 01175 NM 1999 12 11 EISA99191 1 19990914 A 3350 TIE CLIP BOEING 727 727223 1384074 NM BS 480 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORKCARD, FOUND TIE CLIP CRACKED AT FS 480 STRINGER 20L. FABRICATED NEW CLIP PER SAMPLE, TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED NEW CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121101176 19991211 01176 WP 1999 12 11 EISA99146 1 19990718 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 950VJ 47564 MISSING EMERGENCY FLOOR BULB AND COVER. REPLACED BULB AND LENS. (M) 2 L 7 2 4F A6WE 1999121101177 19991211 01177 1999 12 11 MASA99170 4 19991022 A 3422 6226136002 GYRO COLLINS BEECH 1900 1900D 1154162 CE LT/RT FAILED A MASA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SW 07 133YV UE133 FLT 5415 - PHL-LEB - AFTER TAKEOFF FROM BOS, THE CREW NOTED THAT BOTH DIRECTIONAL GYROS WERE DRIFTING AT AN EXTREME RATE . THE CREW NOTIFIED THE TOWER THEY WERE RETURNING TO BOS AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BOTH DIRECTIONAL GYROS. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999121101178 19991211 01178 EA 1999 12 11 MASA99172 1 19991024 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5774 - CLT-LIT - DURING PREFLIGHT, THE CREW FOUND THE FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999121101179 19991211 01179 NM 1999 12 11 MASA99171 1 19991023 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM ROW 1 LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 6346 - PSP-PHX - DURING PREFLIGHT, THE CREW FOUND THE EMERGENCY LIGHTS INOPERATIVE AT ROW 1. MAINTENANCE OPENED UP THE FLOOR BOARD AND RESECURED THE CONNECTOR. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE (M) 2 H 7 2 4T RT A13NM 1999121101180 19991211 01180 EU 1999 12 11 UF6A990947 1 19990928 A 5320 37E3333 ANGLE BAG ATP ATP EU FUSELAGE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE ATTACHMENT FLANGE FOR ACCESS PANEL 531AB IS CRACKED. MAINTENANCE FABRICATED FLANGE AND INSTALLED. ALL WORK W AS DONE IAW BAE ATP SRM 51-10-01 AND 51-30-01. (M) 2 L 7 2 4T RT A27NM 1999121101181 19991211 01181 WP 1999 12 11 WXOA99022 1 19991016 A 5230 SUPPORT DOUG DC9 DC921 302205A WP CARGO DOOR CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION OF FORWARD CARGO DORO PER OPS 4.735 DE TECTED CRACKED AT AFT SIDE OF INTERCOSTAL ANGLE SUPPORT LOCATED AFT SIDE OF FORWARD STOP. REMOVED CRACKED ANGLE SUPPORT . FABRICATED REPAIR ANGLE SUPPORT IAW DC-9 SRM 51-10-1. ALODINED AND PRIMED REPLACEMENT SUPPORT PER DC-9 SRM 51-10-3. INSTALLED REPAIR ANGLE SUPPORT IAW DC-9 SRM 51-30-00 AND 51-30-02. (M) 2 L 7 2 4F A6WE 1999121101182 19991211 01182 WP 1999 12 11 WXOA99023 1 19991016 A 5320 SHEAR TIE DOUG DC9 DC921 302205A WP BS 766 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED AND APPROXIMATE 2 INCH LONG C RACK ON SHEAR TIE BETWEEN LONGERON L14 AND L15 AT FUSELAGE STATION 766. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR SH EAR TIE (REF W/C A134, B03, W073). INSTALLED REPAIR SHEER TIE IAW DC-9 SRM 51-10-2, 51-10-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121101183 19991211 01183 WP 1999 12 11 WXOA99024 1 19991020 A 5540 DOUBLER DOUG DC9 DC921 302205A WP RUDDER CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND INTERNAL DOUBLER EDGE OF RUDDER BROKEN AT REFERENCE ZR99. REMOVED DAMAGED INTERNAL DOUBLER. FABRICATED REPLACEMENT DOUBLER IAW DC-SRM 51-10-1. INSTALLED REPAIR DOUBLER I AW DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999121101184 19991211 01184 WP 1999 12 11 WXOA99025 1 19991022 A 5320 INTERCOSTAL DOUG DC9 DC921 302205A WP FUSELAGE CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND INTERCOSTAL CRACKED AT FORWARD AREA OF AFT CARGO DOO R JAMB. REMOVED DAMAGED INTERCOSTAL AND REPLACED IAW EA M-7200-99-09504. (M) 2 L 7 2 4F A6WE 1999121101185 19991211 01185 WP 1999 12 11 WXOA99026 1 19991022 A 5311 FRAME DOUG DC9 DC921 302205A WP BS 859 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN AFT ACCESSORY COMPARTMENT RIGHT SIDE OF FRA ME 859 AT LONGERON 13R NEAR LIGHTNING HOLE. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC-9 SRM 5 3-01, 51-10-2, 51-10-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121101186 19991211 01186 WP 1999 12 11 WXOA99027 1 19991022 A 5311 FRAME DOUG DC9 DC921 302205A WP BS 737 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND 3.5 INCH CRACK IN RADIUS OF FUSELAGE FRAME STATION 7 37 AT LONGERON 17L. REMOVED DAMAGED SECTION OF FRAME. FABRICATED ANGLE, FILLER AND DOUBLER (RED W/C A134, B03, W063). INSTALLED REPAIR PARTS IAW DC-9 SRM 53-03 FIG 32, 51-10-2, 51-10-3 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1999121101187 19991211 01187 WP 1999 12 11 WXOA99028 1 19991022 A 5311 FRAME DOUG DC9 DC921 302205A WP BS718 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND THREE CRACKES ON FUSELAGE FRAME STATION 718 AT STRIN GER 17L. REMOVED DAMAGED MATERIAL. PERFORMED HFEC INSPECTION IAW OPS 4.751. NO EVIDENCE OF CRACKS EXTENDING FROM CUT OUT AREA. FABRICATED REPAIR PARTS PER DC-9 SRM 53-03 PAGE 4 FIG 32. HEAT TREATED REPAIR PARTS PER AMS-H-6088. ALODINE D AND PRIMED PARTS PER DC-9 SRM 51-10-3 AND INSTALLED REPAIR ANGLES PER DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999121101188 19991211 01188 WP 1999 12 11 WXOA99029 1 19991022 A 5240 BEAM DOUG DC9 DC921 302205A WP SERVICE DOOR CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND CRACK IN GALLEY SERVICE DOOR HORIZONTAL BEAM AFT EDG E. CRACK REPORTED APPROXIMATELY .240 INCH LONG, EXTENDING FROM FASTENER HOLE. FABRICATED DOUBLER PER DC-9 SRM 52-05 FI GURE 25, SHEET 7 AND 9. (M) 2 L 7 2 4F A6WE 1999121101189 19991211 01189 WP 1999 12 11 WXOA99030 1 19991022 A 5320 ANGLE DOUG DC9 DC921 302205A WP AIRSTAIRS CORRODED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND LEVEL 1 CORROSION ON AFT STAIR ANGLE. REMOVED CORRO DED ANGLE. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-9 SRM 51-10-2, 51-10-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121101190 19991211 01190 WP 1999 12 11 WXOA99031 1 19991113 A 5754 5922532503 SLAT DOUG DC9 DC921 302205A WP LT WING DENTED A WXOA O OTHER C F.O.D. DE DESCENT 1 WP 17 127NK 47361 AMA - BIRD STRIKE REPORTED TO LEFT WING AT 8500 FT DURING DESCENT FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. BIRD STRIKE INSPECTION ACCOMPLISHED IAW DC-9 MM 05-56. FOUND LEFT WING NR 2 OUTBOARD LEADING EDGE SLAT TO HAVE SUSTAINED BIR D STRIKE DAMAGE. DENT DIMENSIONS APPROXIMATELY 12 INCH BY 6 INCH, WITH A MEASURED DEPTH OF 1.4 INCH. AIRCRAFT FERRIED TO MVH FOR REPAIRS. REMOVED AND REPLACED LEFT WING NR 2 SLAT IAW DC-9 MM 27-80-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999121101191 19991211 01191 CE 1999 12 11 C2XA99IA573 1 19991103 A 6123 MS252531 SWITCH BEECH 1900 1900D 1154162 CE AUTOFEATHER OUT OF RIG A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 09 17534 UE141 IAH - FLT 3695 - THE CREW ABORTED TAKEOFF DUE TO THE AUTO FEATHER SYSTEM NOT ARMING. MAINTENANCE ADJUSTED THE AFFECTED PEDESTAL MICROSWITCH IAW BEECHCRAFT 1900D MM 61-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999121101192 19991211 01192 SO 1999 12 11 C2XA99BT101 1 19991108 A 4930 4501968 LINE EMB 145 EMB145 SO FUEL DRAIN CLOGGED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 16963 145116 EWR - FLT 8081 - CREW REPORTED AFTER TAKEOFF IN CLIMB AT 3000 FEET, SMELL IN AIRCRAFT SMOKE OR FUEL, AIR RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SMELL DOWN TO FAULTY APU. APU PLACED ON MEL AND RETURNED TO SERV ICE. FOUND APU FUEL DRAIN LINE CLOGGED.. MAINTENANCE UNCLOGGED DRAIN LINE OPERATIONALLY CHECKED APU GOOD. NO FUEL SME LL OR SMOKE NOTED. AIRCRAFT REMOVED FROM MEL AND RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999121101193 19991211 01193 SO 1999 12 11 C2XA99BT100 1 19991107 A 3350 1317 BULB EMB 145 EMB145 SO FUSELAGE FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14959 145091 BTV - FLT 4218 - DURING 3A INSPECTION MAINTENANCE, FOUND BOTH OVERWING EMERGENCY EXTERIOR LIGHTS INOPERATIVE. REMOVED A ND REPLACED BOTH BULBS AND OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999121101194 19991211 01194 EU 1999 12 11 C2XA99BT099 1 19991104 A 3350 167006 BULB AEROSP ATR42 ATR42320 8680930 EU FUSELAGE FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14834 193 BTV - FLT 3680 - MAINTENANCE FOUND EMERGENCY EXIT AISLE PATH LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999121101195 19991211 01195 NE 1999 12 11 C2XA99IA560 2 19991022 A 7200 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE RIGHT MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 86842 22483 286 LFT-IAH - FLT 3743 - THE CREW REPORTED OVERTEMP CONDITION ON NUMBER 2 ENGINE AT CRUISE. THE AIRCRAFT LANDED AT IAH WITH OUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999121101196 19991211 01196 SO 1999 12 11 C2XA99IA589 1 19991103 A 3230 12043270501 RELAY BOX EMB 120 EMB120RT SO MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 47722 120166 IAH - FLT 3455, THE CREW REPORTED THAT THE LANDING GEAZR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED TO IAH WHERE IT LAND ED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX IAW EMB120 MM 32-31-02, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121101197 19991211 01197 SO 1999 12 11 C2XA99IA575 1 19991103 A 5320 12030479015 HOUSING EMB 120 EMB120RT SO DISCHARGE VALVE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LAVATORY DISCHARGE VALVE HOUSING. REMOVED AND REPLACED DISCHARGE VALVE HOUSING IAW CPM 51-14-00, 51-14-04, 51-14-05 AND SRM 51-25-00. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121101198 19991211 01198 SO 1999 12 11 C2XA99BT103 1 19991111 A 3350 3025101 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13956 145078 BTV - FLT 3944 - DURING 4A INSPECTION MAINTENANCE, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT TO BE INOPERATIVE IN ALL MOD ES. REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999121101199 19991211 01199 NM 1999 12 11 F3LA99137 1 19991112 A 5320 ANGLE BOEING 737 7372P6 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED RIGHT FORWARD SERVICE DOOR INBOARD THRESHOLD SUPPORT ANGLE CORRODED. MAINTE NANCE FABRICATED AND REPAIRED RIGHT FORWARD SERVICE DOOR INBOARD THRESHOLD SUPPORT ANGLE PER SRM 51-40-3. (M) 2 L 7 2 4F RT A16WE 1999121101200 19991211 01200 EU 1999 12 11 C2XA99IA565 1 19991024 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS RIGHT AFT SEAT TRACKS WERE FOUND TO BE CORRODED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (M) 2 H 7 2 4T RT A53EU 1999121101201 19991211 01201 EU 1999 12 11 C2XA99IA564 1 19991024 A 5313 S53671407209 STRINGER AEROSP ATR42 ATR42300 8680920 EU FRAME 29/34 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, STRINGER 17 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 29 AND 34. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED STRINGER IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999121101202 19991211 01202 EU 1999 12 11 C2XA99IA563 1 19991024 A 5280 GA62103 FITTING AEROSP ATR42 ATR42300 8680920 EU NLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD NOSE LANDING GEAR DOOR ACTUATING ROD ATTACHMENT WAS FOUND TO BE CRACKE D. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOOR ATTACHMENT IAW ATR42-320 MM 32-21-00, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 1999121101203 19991211 01203 NM 1999 12 11 P2EA99311 1 19991112 A 7711 LG80A6 TRANSMITTER BOEING 737 737281 138448P NM NR 2 ENGINE INOPERATIVE A P2EA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 05 219US P55 20414 FLT 588 - MCI - ABORTED TAKEOFF, NO EMERGENCY DECLARED. DURING TAKEOFF ROLL, NR 2 EPR GAUGE READS ZERO. REPLACED NR 2 EPR TRANSMITTER AND NR 2 EPR INDICATOR PER MM 77-11-21, OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1999121101204 19991211 01204 NM 1999 12 11 P2EA99312 1 19991113 A 2751 CONTROL CABLE BOEING 737 737247 138448D NM FLAP INDICATOR BROKEN A P2EA O OTHER O OTHER AP APPROACH 1 CE 05 912MP 19607 MSP - FLT 703 - EMERGENCY DECLARED, LANDING UNEVENTFUL. FLAP ASYMMETRY LOCKOUT AND INDICATOR SPLIT OCCURRED WHEN FLAPS WERE SELECTED DURING APPROACH. WHEN FLAPS 5 WERE SELECTED, NO LEADING EDGE FLAP TRANSIT LIGHT CAME ON AND NO MOVEMENT O F FLAP POSITION INDICATOR. REFERRED TO QRH AND ELECTRICALLY LOWERED FLAPS (ALTERNATE). FOUND LEFT FLAP POSITION INDICA TOR CABLE BROKEN. FABRICATED AND INSTALLED LEFT FLAP POSITION INDICATOR CABLE FAC-1, FAC-4 PER MM 27-51-221 AND BAC 500 2, SECTION 8-11. REMOVED PINS F-1, F-2, F-3 AFTER RIG, SAFETIED TURNBUCKLES. FLAPS OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999121101205 19991211 01205 EU 1999 12 11 PLGA991102 1 19991102 A 3230 HARNESS SAAB SF340 340B 7860101 EU MLG FAILED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 348BE 340B190 BGR - DURING C-CHECK INSPECTION MX WAS PERFORMING MRB TASK 323106, FUNCTIONAL CHECK OF EMERG EXTENSION OF L/G. DURING P ERFORMANCE OF THE FUNCTIONAL CHECK EXTREME FORCE HAD TO BE USED TO PULL THE RELEASE HANDLE. WHEN THE HANDLE WAS PULLED THE RT EMERG RELEASE C/B POPPED. FURTHER T/S IDENTIFIED THAT THE RT AND LT L/G EXPLOSIVE BOLT HARNESSES FAILED ELECT CH ECKS. MX FOUND SEVERAL BROKEN WIRES AT HARNESS CONNECTOR FOR THE EXPLOSIVE BOLT ON LT MLG. THE CONNECTOR WAS REPLACED AND WIRES IN THE HARNESS WERE REPAIRED. MX ALSO FOUND A COUPLE SHORTED WIRES ON RT MLG EXPLOSIVE BOLT HARNESS. THOSE W IRES WERE REPAIRED. MX CLEANED AND LUBED THE RELEASE HANDLE AND OPERATED THE HANDLE THRU SEVERAL CYCLES TO RELIEVE THE 2 L 7 2 4T RT A52EU 1999121101206 19991211 01206 EU 1999 12 11 PLGA991104 1 19991104 A 3060 MS2740017 RELAY SAAB SF340 340B 7860101 EU LT PROP DE-ICE FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 350BE 340B197 BOS - FLT 4682 - THE LEFT PROP DI-ICE LIGHT ILLUMINATED AFTER 45 SECONDS. ALL ATTEMPTS TO RESET BY THE CHECKLIST FAILED . FLIGHT CONTROL CHOSE TO HAVE AIRCRAFT RETURN TO BOS WHERE IT LANDED WITHOUT INCIDENT. BOS MAINTENANCE REPLACED THE L EFT PROP DE-ICE RELAY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999121101207 19991211 01207 NE 1999 12 11 99ZZZM796 2 19991105 A 7200 3044800 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LEFT SEIZED A JJBA O OTHER J WARNING INDICATION IN INSP/MAINT 1 EA 01 852CA UE55 UPON A NORMAL ENGINE START AT GATE, LEFT ENGINE EMITTED AN ABNORMAL PITCH NOISE FOLLOWED BY A DROP IN N1 SPEED AND A RIS E IN ITT INDICATION. OTHER ENGINE INDICATIONS ALSO, INDICATED ABNORMAL INDICATIONS. ENGINE WAS REPLACED. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999121101208 19991211 01208 NM 1999 12 11 F3LA99136 1 19991119 A 3350 LIGHT BOEING 737 7372L9 1384497 NM CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 270FL 22733 DURING SERVICE CHECK, MAINTENANCE FOUND AFT EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING TO EMERGE NCY TRACK LIGHTS AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999121101209 19991211 01209 NM 1999 12 11 F3LA99138 1 19991028 A 5320 ANGLE BOEING 737 7372P6 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED R-1 MAIN ENTRY THRESHOLD ANGLE CORROSION. MAINTENANCE REPAIRED AND REPLACED R-1 MAIN ENTRY THRESHOLD SUPPORT ANGLE PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999121101210 19991211 01210 NM 1999 12 11 USAA991143 1 19991029 A 5312 BULKHEAD BOEING 737 737301 1384611 NM STA 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .075 INCH CRACK AT STATION 178 BULKHEAD LBL. 5, WL 188 WEB. CUTOUT DA MAGE AREA AND INSTALLED DOUBLER PER SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999121101211 19991211 01211 NM 1999 12 11 TSAA9933479 1 19991109 A 3350 86210066 BATTERY BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 3, 4, 5, AND 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1999121101212 19991211 01212 NM 1999 12 11 TSAA9933471 1 19991026 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 3 EMERGENCY FLOOR BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999121101213 19991211 01213 NM 1999 12 11 TSAA9933477 1 19991103 A 3350 9221009 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED AFT SERVICE EMERGENCY EXIT LIGHT POWER PACK DUE TO FLICKERING. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F A16WE 1999121101214 19991211 01214 NM 1999 12 11 TSAA9933478 1 19991105 A 3350 6013211 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED LEFT OVERWING SLIDE LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999121101215 19991211 01215 NM 1999 12 11 TSAA9933472 1 19991030 A 3350 8731002511 LIGHT BOEING 737 737297 1384480 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED AFT SERVICE DOOR IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999121101216 19991211 01216 NM 1999 12 11 TSAA9933473 1 19991027 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED EMERGENCY FLOOR BATTERY PACKS FOR POSITIONS 3 AND 5 DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F A16WE 1999121101217 19991211 01217 NM 1999 12 11 99ZZZM797 1 19991102 A 2611 302842 SMOKE DETECTOR BOEING 727 727222 1384073 NM CARGO BAY NO TEST A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 7640U 19913 FLT 243 - CAE-DAY - NR 2 CARGO SMOKE DETECTOR WILL NOT TEST. REPLACED NR 2 CARGO SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 1999121101218 19991211 01218 NM 1999 12 11 99ZZZM798 1 19991111 A 2612 18252800 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF ADJUST A RYNA O OTHER N FALSE WARNING DE DESCENT 1 CE 07 429EX 19100 FLT 720 - DTW-IND - NR 3 FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED ON DESCENT, ALL OTHER INDICATION NORMAL AND LIG HT EXTINGUISHED BEFORE LANDING. ADJUSTED FIRE LOOP AWAY FROM ENGINE. (M) 2 L 7 3 4F A3WE 1999121101219 19991211 01219 WP 1999 12 11 USAAD99164 1 19991112 A 3350 41B001TD05G1 BATTERY DOUG DC9 DC981 3022081 WP CARGO BAY DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 48041 THE NACELLE EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE NACELLE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999121101220 19991211 01220 WP 1999 12 11 99ZZZM799 1 19991112 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 48041 THE PASSENGER CABIN LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE PASSENGER CABIN LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999121101221 19991211 01221 WP 1999 12 11 USAAD99163 1 19991116 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP GALLEY DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 48145 DTW - THE GALLEY DOOR EVACUATION SLIDE EMERGENCY LIGHT WAS DIM. REPLACED THE GALLEY DOOR EVACUATION SLIDE EMERGENCY LIG HT BATTERY. (M) 2 L 7 2 4F A6WE 1999121101222 19991211 01222 WP 1999 12 11 99ZZZM800 1 19991116 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 48145 THE FIRST CLASS AREA OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE FIRST CLASS ARE OVERHEAD EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999121101223 19991211 01223 WP 1999 12 11 USAAD99162 1 19991115 A 3350 8732030153 CONTROL MODULE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 19 800US 48034 CLT - DURING TAXI, THE LOW LEVEL EMERGENCY LIGHTS FLASHED ON AND OFF. MAINTENANCE REPLACED THE FORWARD CONTROL MODULE A ND ALL THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999121101224 19991211 01224 NM 1999 12 11 USAA991139 1 19991029 A 5312 BULKHEAD BOEING 737 737301 1384611 NM STATION 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 178 BULKHEAD RBL 4.75, WL 201 SKIN. INSTALLED FILLERS AND DOUBLER PER SRM 51-10-02 AND TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999121101225 19991211 01225 NM 1999 12 11 USAA991138 1 19991029 A 5320 SPLICE BOEING 737 737301 1384611 NM STATION 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .01 INCH CRACK AROUND TWO RIVETS AT STATION 908 AND STRINGER 4L STRING ER SPLICE. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999121101226 19991211 01226 NM 1999 12 11 USAA991137 1 19991029 A 5414 SKIN BOEING 737 737301 1384611 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT ACCESS PANEL OUTBOARD EDGE CUTOUT PYLON SKIN. INSTAL LED DOUBLER PER TR 54-30-07. (M) 2 L 7 2 4F RT A16WE 1999121101227 19991211 01227 NM 1999 12 11 USAA991136 1 19991029 A 5320 SPLICE BOEING 737 737301 1384611 NM STATION 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .01 INCH CRACK STATION 908, STRINGER 4R IN STRINGER SPLICE. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999121101228 19991211 01228 NM 1999 12 11 USAA991135 1 19991029 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM STATION 291.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK BETWEEN STRINGERS 10 AND 11 AND STATION 291.5 SHEAR TI E. REPLACED WITH IDENTICAL PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999121101229 19991211 01229 EU 1999 12 11 AWXA9900455 1 19991207 A 5347 ASNA2223 SEAT TRACK AIRBUS 320 A320231 3930325 EU FRAME 20 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SEAT TRACK NR 4 CORRODED AT FRAME 20. FABRICATED SEAT TRACK AS PER SRM 53-11-15. ALODINED, PRIMED AND PAINTED AS PER S RM 51-75-00. INSTALLED NR 4 SEAT TRACK PER SRM 53-11-15. 2 L 7 2 4F RT A28NM 1999121101230 19991211 01230 EU 1999 12 11 AWXA9900456 1 19991207 A 5347 ASNA2223 SEAT TRACK AIRBUS 320 A320231 3930325 EU FRAME 20 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 SEAT TRACK NR 3 CORRODED AT FRAME 20. FABRICATED SEAT TRACK REPAIR AS PER DWG 53-00-15. INSTALLED REPAIR PER SRM 53-00 -15 FIG 201. TRACK SPLICES PO NR C1012005729. 2 L 7 2 4F RT A28NM 1999121101231 19991211 01231 NM 1999 12 11 AWXA9900457 1 19991207 A 5311 143N1009 FRAME BOEING 757 7572S7 1384962 NM BS600 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 FWD CARGO FS 600 BETWEEN STR 24L AND 26L FRAME IS CRACKED IN UPPER FLANGE. REMOVED DAMAGED SECTION OF FRAME BS 600 BETW EEN 24L-26L. FABRICATED AND INSTALLED REPLACEMENT FRAME SECTION AND SPLICE CHANNEL IAW 53-00-07 FIG 201. 2 L 7 2 4F RT A2NM 1999121101232 19991211 01232 NM 1999 12 11 AWXA9900458 1 19991207 A 5320 143N5140 ANGLE BOEING 757 7572S7 1384962 NM BS 660 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 INTERCOSTAL CRACKED AT RADIUS AT RT STA 660 AND RBL 26. REMOVED AND FABRICATED INTERCOSTAL FWD ATTACH ANGLE PER SRM 53- 30-51. INSTALLED IAW SRM 53-00-51 FIG 20. 2 L 7 2 4F RT A2NM 1999121101233 19991211 01233 NM 1999 12 11 AWXA9900459 1 19991207 A 5311 146N1008 FRAME BOEING 757 7572S7 1384962 NM BS 1340 CRACK A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 FRAME DENTED AND CRACKED JUST BELOW FACTORY SPLICE AT STA 1340 STR 23R. TRIMMED OUT DAMAGED FRAME IAW SRM 53-00-07 FIG 201. FABRICATED REPAIR PARTS PER SRM 53-00-07, 7075-0 .071 R710334. ALODINED AND PRIMED CUTOUT IAW SRM 51-20-01. INS TALLED REPAIR PART AND ACCESS TREATED WITH LPS3. 2 L 7 2 4F RT A2NM 1999121101234 19991211 01234 NM 1999 12 11 AWXA9900460 1 19991208 A 5320 DHM42281C01291 CLIP BOEING 737 73733A 1384673 NM BS 334 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 STRINGER TO FRAME TIE CLIP CRACKED AT STRINGER 11R FS 334. REMOVED CRACKED TIE CLIP PER SRM 51-40-02. FABRICATED TIE C LIP FRM MAT'L 7075 T6 .032 QQA250/13 R700673 PER 53-10-15. TREATED AND PRIMED PER SRM 51-20-01. INSTALLED PER SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 1999121101235 19991211 01235 NM 1999 12 11 AWXA9900461 1 19991208 A 5320 NOTAVAIL CHANNEL BOEING 737 73733A 1384673 NM BS 948 - 1000 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 CABIN FLOOR STRUCTURE CHANNEL AT L-2 DOOR HAS CORROSION FROM STA 948 TO 1000 WL 208. REMOVED AND REPLACED CHANNEL AT L- 2 DOOR PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999121101236 19991211 01236 NM 1999 12 11 AWXA9900462 1 19991208 A 5320 NOTAVAIL CHANNEL BOEING 737 73733A 1384673 NM BS 947 - 1000 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 CABIN FLOOR STRUCTURE CHANNEL AT R-2 DOOR HAD CORROSION FROM STA 947-STA 1000 WL 208. REMOVED AND REPLACED CHANNEL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999121101237 19991211 01237 NM 1999 12 11 AWXA9900463 1 19991208 A 5210 DHM42281A00421 SKIN BOEING 737 73733A 1384673 NM PAX DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 CRACK ON AFT LWR CORNER OF R-1 DOOR FROM RADIUS OF CUTOUT TO FASTENER HOLE. REAMED HOLE .025 AND PLUGGED IAW 51-10-02. FABRICATED REPAIR DOUBLERS PER SRM 51-30-01. FABRICATED FILLERS PER SRM 53-10-01. TREATED AND PRIMED IAW SRM 51-20-0 1 AND INSTALLED DOUBLERS 2024T3 .063 QQA 250/5 R687660 FILLERS 2024T3 .025 QQA 250/5 R706895. 2 L 7 2 4F RT A16WE 1999121101238 19991211 01238 NM 1999 12 11 AWXA9900464 1 19991208 A 5313 DHM42281LD13L1 STRINGER BOEING 737 73733A 1384673 NM BS 337 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 STRINGER 8R CRACKED AT FS 337 FWD SERVICE DOORWAY AFT FRAME. REMOVED DAMAGED PART AT BS 333 PER SRM 51-30-2. FABRICATE D REPLACEMENT STRINGER OF BAC 1498-151/70 TG QQA250/13 R642745 IAW 53-10-03. TREATED AND PRIMED PER SRM 51-20-2. 2 L 7 2 4F RT A16WE 1999121101239 19991211 01239 NM 1999 12 11 99FDEA00499 1 19991208 A 3260 SWITCH BOEING 727 727233 138408A NM RT MLG DOOR FAILED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 271FE 22036 RT MAIN DOOR LIGHT STAY ON WITH GEAR HANDLE IN OFF POS. REMOVED AND REPLACED RT MAIN GEAR DOOR LOCK SWITCH PLUG (D752) PER STAND MAINT PRACT AND REF WIRING DIAGRAM MANUAL 32-62-01. OPER CK WARN SWITCH REF MM 32-62-011-5. OPER CK NORM. O K FOR SERVICE. 2 L 7 3 4F RT A3WE 1999121101240 19991211 01240 EU 1999 12 11 99FDEA00500 1 19991209 A 3260 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU MLG ILLUMINATED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 665FE 769 LANDING GEAR DOWN NR 3 WAS UNSAFE WARNING AFT MISSED APPROACH, GOT THREE GROUND LIGHTS (BOTH PNLS SAME) LEVEL. RECYCLED THE GEAR AND ALL OK. INSP RT GEAR ALL LINKS, SWITCHES NORM. PER PROX BOX TEST PER TSM 32-61-00 101 THRU 105. NO FAUL TS DISPLAYED. MEMORY CLEAR. 2 L 7 2 4F RT A35EU 1999121101241 19991211 01241 WP 1999 12 11 ABXA9900828 1 19991208 A 3260 H1410051 SWITCH DOUG DC9 DC933F 302207A WP LT MLG WW MALFUNCTIONED A ABXA O OTHER N FALSE WARNING TO TAKEOFF 1 GL 23 933AX 47291 AFTER TAKEOFF, THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR, LIGHT EXTINGUISHED. REPLACED LEFT GEAR DOOR SWITCH. 2 L 7 2 4F A6WE 1999121101242 19991211 01242 WP 1999 12 11 ABXA9900829 1 19991206 A 3350 60030451 POWER SUPPLY DOUG DC9 DC933F 302207A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 932AX 5737 47465 ON PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1999121101243 19991211 01243 WP 1999 12 11 ABXA9900830 1 19991206 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 962AX 1530 47768 EMERGENCY LIGHTS INOPERATIVE INTERMITTENTLY. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1999121101244 19991211 01244 WP 1999 12 11 RRXA991590 1 19991208 A 2400 RELAY DOUG DC8 DC871F 302199D WP E/E BAY MALFUNCTIONED A RRXA O OTHER J WARNING INDICATION LD LANDING 1 WP 15 8091U 45995 NO SPOILER PRESSURE WHEN GEAR EXTENDED OR SPOILER SW HELD IN OVERRIDE. WHEN SPOILER PUMP SWITCH WAS PLACED TO OVERRIDE A STRONG ODOR LIKE ELECTRICAL WIRING OVERHEATING WAS NOTICED. REMOVED AND REPLACED RELAY R2-217. SPOILER SYSTEM OP CHE CKS NORMAL ON GROUND FUNCTION TEST. NO DEFECT NOTICED. 2 L 7 4 4F RT 4A25 1999121101245 19991211 01245 NM 1999 12 11 VNAA9912003 1 19991206 A 2435 8160121 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE STARTER/GEN FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 9311 3068 116120 DURING THE TAKEOFF ROLL, THE FLIGHT CREW EXPERIENCED A LEFT HAND GENERATOR FAILURE. THE CREW ABORTED TAKEOFF AND EXITED THE RUNWAY. THE CREW PERFORMED THE QUICK REFERENCE PROCEDURES AND ATTEMPTED ANOTHER TAKEOFF. THE FLIGHT TOOK OFF WITH OUT FURTHER INCIDENT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121101246 19991211 01246 NE 1999 12 11 VNAA9912004 2 19991207 A 7321 8111804004 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 8498 3068 116120 DURING THE TAKEOFF ROLL, THE FLIGHT CREW EXPERIENCED A LEFT HAND ELECTRONIC ENGINE CONTROL UNIT FAIL CAS MESSAGE. THE C REW ABORTED TAKEOFF. THE CREW RESET THE ELECTRONIC ENGINE CONTROL UNIT AND THE AIRCRAFT CHECKED GOOD. MAINTENANCE CONT ROL CLEARED THE AIRCRAFT FOR ANOTHER TAKEOFF ATTEMPT. THE AIRCRAFT TOOK OFF WITHOUT FURTHER INCIDENT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121101247 19991211 01247 NE 1999 12 11 VNAA9912005 2 19991207 A 7321 8111804004 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE CONTAMINATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 8498 3068 116120 DURING THE TAKEOFF ROLL, THE FLIGHT CREW EXPERIENCED A LEFT HAND ELECTRONIC ENGINE CONTROL UNIT FAIL CAS MESSAGE. THE C REW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND CLEANED THE CANNON PLUGS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 7 5-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121101248 19991211 01248 NM 1999 12 11 VNAA9912006 1 19991208 A 7603 001A761A1021003 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 328JS 3030 DURING THE TAKEOFF ROLL, THE CREW ADVANCED THE POWER LEVERS BUT THEY FAILED TO FULLY RELEASE. THE CREW ABORTED TAKEOFF AND PROCEEDED TO CHECK THE SYSTEM. AFTER GROUND CHECKS WERE COMPLETED THE AIRCRAFT WAS CLEARED TO ATTEMPT ANOTHER TAKEO FF. THE AIRCRAFT TOOK OFF AND DEPARTED WITHOUT FURTHER INCIDENT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121101249 19991211 01249 1999 12 11 RAIA9912008 4 19991206 A 2320 7511001945 AUDIO PANEL JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 572HK 9331 9331 41091 JFK- UNABLE TO TRANSMIT ON NR 2 COM. MAINTENANCE REPLACED NR 2 AUDIO CONTROL PANEL. 2 L 7 2 4T RT A41NM 1999121500001 19991215 00001 NM 1999 12 15 TWAA9916301 1 19991201 A 3350 767 LIGHT BOEING 757 757231 1384950 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 709TW 28168 THE EMERGENCY LIGHT AT THE FORWARD LEFT CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-24-8 LAX. 2 L 7 2 4F RT A2NM 1999121500002 19991215 00002 EU 1999 12 15 JBXA9900127 1 19991202 A 2760 60042752 TRANSDUCER MESSIERDOWT FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE MLG FAILED A JBXA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 05 103ML 11444 RDU - LIFT-DUMPER UNSAFE FAULT ON LEFT MFDU AT 75 KTS (ABORTED TAKEOFF). REMOVED AND REPLACED RT INBOARD WHEEL SPEED SE NSOR (TRANSDUCER) IAW F-100 AMM 32-45-02. OPERATIONAL TEST GOOD. 2 L 7 2 4F 4 F RT E25NE 1999121500003 19991215 00003 WP 1999 12 15 TWAA9916401 1 19991201 A 2150 DUCT DOUG DC9 DC982 3022082 WP LT PACK CONTAMINATED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 05 917TW 49366 APPROXIMATELY ONE MINUTE BEFORE TOUCHDOWN SMOKE APPEARED THROUGHOUT THE CABIN. SMOKE DISSIPATED WHEN THE PACKS WERE SHU T DOWN. FOUND OIL IN THE LT PACK DUCT AFTER THE ACM. PLACARDED THE ACM PER MEL. CHECK-C 7-13-99 STL. 2 L 7 2 4F A6WE 1999121500004 19991215 00004 NM 1999 12 15 TWAA9916501 1 19991201 A 3242 BRAKE BOEING 767 767330 NM MLG FAILED A TWAA O OTHER A J FLAME/FIRE WARNING INDICATION LD LANDING 1 CE 05 691LF 25137 DURING LANDING USING AUTO BRAKES THE BRAKE TEMP LIGHT ILLUMINATED. NO ANTI-SKID RELEASE DURING NORMAL BRAKING. MANUAL BRAKING COMMENCED AT ABOUT 100 KTS WITH RESERVE APPLIED. RAMP PERSONNEL REPORTED FLAMES IN BRAKE AREA WHICH WAS EXTINGU ISHED. REPLACED THE NUMBER 2 REAR WHEEL AND BRAKE. CHECK-C 6-8-99 MCI. 2 L 7 2 4F RT A1NM 1999121500005 19991215 00005 NM 1999 12 15 TWAA9916601 1 19991206 A 3350 3020433 LIGHT BOEING 757 757231 1384950 NM PAX DOOR INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 717TW 28485 THE RIGHT SIDE NUMBER 4 CABIN DOOR EMERGENCY SLIDE LIGHT WAS INOPERATIVE. FOUND SOLDER FLUX ON THE SOLDERED CONNECTION OF THE LIGHT ASSEMBLY. CLEANED THE CONNECTION ON LIGHT ASSY AND RESOLDERED CONTACT ON THE LAMP. CHECK-C 3-14-99 LAX. 2 L 7 2 4F RT A2NM 1999121500006 19991215 00006 NM 1999 12 15 TWAA9916704 1 19991130 A 5330 SKIN BOEING 727 727231 1384079 NM FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54348 21967 DURING CHECK-C MAINT, THE FORWARD LT CABIN ENTRY DOOR, LOWER HINGE CUTOUT WAS CRACKED GOING FORWARD, 1.5 INCHES LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-1, PAGE 6. I NSTALLED REPAIR DOUBLER PER SSRM 53-10-219, DETAIL 3. 2 L 7 3 4F A3WE 1999121500007 19991215 00007 NM 1999 12 15 TWAA9916705 1 19991130 A 5330 SKIN BOEING 727 727231 1384079 NM FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54348 21967 DURING CHECK-C MAINT, THE FORWARD LEFT CABIN ENTRY DOOR, UPPER HINGE CUTOUT WAS CRACKED, GOING FORWARD 1.375 INCH LONG I N FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED CRACK 0.250 INCH PER SRM 51-10-1, PAGE 6 TO 8. INSTALLED REPAIR DOUBLER PER SSRM 53-10-219, DETAIL IV. 2 L 7 3 4F A3WE 1999121500008 19991215 00008 WP 1999 12 15 TWAA9916706 1 19991130 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 1079 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND FORMER FOOT CORRODED AROUND FASTENERS AT STA 1079, BETWEEN LONGERON 29L AND 28L. REMOVED CO RROSION PER STANDARD PROCESSES MANUAL 6-80-01 AND TREATED AND PRIMED AREA PER SRM 51-10-3 PARAGRAPH 22. 2 L 7 2 4F RT A6WE 1999121500009 19991215 00009 WP 1999 12 15 TWAA9916803 1 19991130 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 604 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND SECTION OF STA 604 BULKHEAD TEE CHORD FROM O/B OF LONGERON 29L TO O/B OF 29R HAD CORROSI ON. REPLACED LOWER SECTION OF STA 604 TEE CHORD BECAUSE OF OUT OF LIMIT CORROSION BETWEEN L28L TO L28R PER ARA 16470. 2 L 7 2 4F A6WE 1999121500010 19991215 00010 WP 1999 12 15 TWAA9916804 1 19991130 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 579 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LARGE FASTENER HOLES IN FUSELAGE SKIN AT LONGERON 29L, STA 579 AREA. INSTALLED SKIN REP AIR AT LONGERON 29L, STA 579, TO REPAIR LARGE FASTENER HOLES PER ARA 16470 AND SRM 53-04, FIG 12B. 2 L 7 2 4F A6WE 1999121500011 19991215 00011 WP 1999 12 15 TWAA9916805 1 19991130 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 427 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND AT STA 427 AND LONGERON 29R, HAD BLIND FASTENER PULLED AND SKIN PILLOWING, AND SKIN DENT ED 7 IN BY 1 IN BY 0.10 DEEP. FOUND NO CRACK PER SRM 53-603 PART 6. REPAIRED DENT IN SKIN PER ARA 16217 AND SRM 53-05 FIG 105 AND PILLOWED AREA WAS TRIMMED OUT. 2 L 7 2 4F A6WE 1999121500012 19991215 00012 NM 1999 12 15 TWAA9916801 1 19991212 A 3350 LIGHT BOEING 727 727231 1384079 NM ROW 30 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64346 21633 THE LAST SECTION OF CABIN EGRESS LIGHTS AT ROW 30 WERE INOPERATIVE. REPAIRED THE TRACK FEEDER CABLE. CHECK-C 9-8-99 MC I. 2 L 7 3 4F A3WE 1999121500013 19991215 00013 WP 1999 12 15 TWAA9916802 1 19991208 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9307R 9307R THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 21 TO 29. REPLACED BATTERIES IN BATTERY PACK. CHECK-C 10-28-99 STL. 2 L 7 2 4F A6WE 1999121500014 19991215 00014 EU 1999 12 15 JBXA9900128 1 19991213 A 2760 60042752 TRANSDUCER FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE NR 4 MLG FAILED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 109ML 11485 FLT 9 RDU - BOS, ON TAKEOFF AT APPROX 75 KTS HAD LIFT DUMPER FAULT ON LEFT MFDU. ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED OPS CHECK OF PSEU, NO FAULT NOTED. LIFT DUMPERS CHECKED GOOD IAW AMM 31-41-01. REMOVED AND REPLACED NR 4 WH EEL SPEED TRANSDUCER. OPS CHECK GOOD IAW AMM 32-45-02. 2 L 7 2 4F 4 F RT E25NE 1999121500015 19991215 00015 EA 1999 12 15 JBXA9900129 1 19991213 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A JBXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 05 584ML 7330 FLIGHT 211 RDU TO SWF HAD FLAP FAIL MESSAGE AND FLAPS LOCKED AT 8 DEGREES ON DEPARTURE. REMOVED AND REPLACED RT BPSU AS SY IAW AMM 27-51-10, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1999121500016 19991215 00016 NM 1999 12 15 PCAA9900062 1 19991213 A 3260 ROD END DHAV DHC8 DHC8102 2809003 NM MLG DOOR OUT OF ADJUST A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 805EX 228 BGM-FLIGHT 3576, RETURNED TO THE FIELD AFTER THE RIGHT MAIN LANDING GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. M AINTENANCE INSPECTED AND FOUND THE RIGHT FORWARD GEAR DOOR ACTUATOR ROD END REQUIRING ADJUSTMENT. MAINTENANCE ADJUSTED THE ROD END IAW DHC M/M CHAPTER 32, OPERATIONAL CHECK PROVED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999121700001 19991217 00001 NM 1999 12 17 DLM90992583 1 19991122 A 3350 LIGHT DOUG MD90 MD9030 3023690 NM SEATS 32-37 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 905DA 53385 EMERGENCY TRACK LIGHTING AT SEATS 32-37 INOP. FOUND FAULTY WIRE SPLICES AT SEAT 33. INSTALLED PROPER SPLICE, OPS CK GO OD. 2 L 7 2 4F RT A6WE 1999121700002 19991217 00002 WP 1999 12 17 TWAA9916201 1 19991128 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP ROW 19 & 24 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9403W 53139 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROW ONE, FORWARD LT CABIN DOOR, ROW 19 AND ROW 24. REPLACED THE WIRE SEGMEN TS AT EACH LOCATION. CHECK-C 9-25-99 STL. 2 L 7 2 4F RT A6WE 1999121700003 19991217 00003 NM 1999 12 17 AWXA9900439 1 19991201 A 3350 831136 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 168AW 23629 EMERGENCY ESCAPE PATH LIGHT AT ROW 5 AND 13 INOP. REWIRED ROW 5 AND REPLACED LIGHT ASSY. RELAMPED ROW 13. 2 L 7 2 4F RT A16WE 1999121700004 19991217 00004 NM 1999 12 17 AWXA9900441 1 19991202 A 5330 6552988 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 CRACK IN FUSELAGE SKIN AT THE UPPER CORNER OF L-2 DOOR HINGE CUTOUT. DAMAGED MATERIAL REMOVED, FABRICATED REPAIR DOUBLE R OF 301 1/2 HARD 2660361 AND FILLER 2024-T3 .071 QQA250/5 R700681. INSTALLED REPAIR IAW 53-69-01. 2 L 7 2 4F RT A16WE 1999121700005 19991217 00005 NM 1999 12 17 AWXA9900442 1 19991201 A 5311 6546533 FRAME BOEING 737 73733A 1384673 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 UPPER PART OF FRAME 500 HAD A CRACK APPROXIMATELY 1.5 INCH LONG AT BL 0 IN THE FWD CARGO COMPARTMENT. STOP DRILLED CRAC K, FABRICATED A REPAIR DOUBLER PER 737 SRM 53-00-07 FIG 201 OF QQA 250/13 T6 .05 R698980. TREATED, PRIMED AND INSTAL LED IAW 737 SRM 53-00-07 FIG 201, PER 51-40-02. 2 L 7 2 4F RT A16WE 1999121700006 19991217 00006 WP 1999 12 17 TWAA9916702 1 19991130 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 579 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND LARGE FASTENER HOLES IN FUSELAGE SKIN AT LONGERON 29L, STA 579 AREA. INSTALLED SKIN REP AIR AT LONGERON 29L AT STA 579 TO REPAIR LARGE FASTENER HOLES PER ARA 16470 AND SRM 53-04, FIG 12B. 2 L 7 2 4F A6WE 1999121700007 19991217 00007 WP 1999 12 17 TWAA9916703 1 19991130 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 570 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, LONGERON 30 WAS CRACKED AT STA 570, APPROXIMATELY 4 INCHES LONG, LEFT AND RIGHT SIDE OF LONGER ON. INSTALLED SPLICE REPAIR PER SRM 53-02, FIG 14. 2 L 7 2 4F A6WE 1999121700008 19991217 00008 WP 1999 12 17 TWAA9916701 1 19991129 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING OP 16 MAINT CHECK, FOUND CRACK INDICATION USING LFEC AT LOWER AFT CORNER OF THE FORWARD CARGO DOOR OPENING. CRAC K CONTAINED PER SRM 51-00-03, PART 6. REPAIRED PER SRM 53-05. 2 L 7 2 4F A6WE 1999121800043 19991218 00043 CE 1999 12 18 99ZZZX4488 1 19991019 A 3230 99100023 MOTOR CESSNA 310 310R 2074245 CE MLG MALFUNCTIONED A BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 37223 310R0963 ONT - GEAR WOULD NOT EXTEND AT ONTARIO, CALIF. HAND CRANKED GEAR DOWN AND LANDED WITH NO PROBLEMS. JACKED AIRCRAFT, CO ULD NOT DUPLICATE PROBLEM, CHANGED GEAR MOTOR FOR PRECAUTIONARY MEASURES. 1 L 7 2 3O 3A10 1999121800046 19991218 00046 CE 1999 12 18 99ZZZX4491 1 19991118 A 5711 1011100303 SPAR BEECH 200 200BEECH 1152920 CE LT WING CORRODED A DQIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SJ 10006 BB290 WHILE INVESTIGATING POSSIBLE SURFACE CORROSION ON THE LEFT WING TO FORWARD SPAR HINGE CAP DURING THE 12-MONTH SPAR CAP I NSPECTION PER CHAPTER 5 OF THE MM, AN APPROXIMATE 2.6 INCH CRACK WAS FOUND AT APPROXIMATELY WS 153.735. 1 L 7 2 4T A24CE 1999121800069 19991218 00069 EU 1999 12 18 99ZZZX4514 1 19991022 A 2435 150SG10095 BRUSHES 150SG1220 SNIAS 350 AS350B2 8680813 EU STARTER/GEN WORN A R7MA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NM 11 101LN 442 8330 3038 IN CRUISE, FUEL BOOST PUMP LIGHT ILLUMINATED WITH CORRESPONDING DROP IN FUEL PRESSURE. LIGHTS AND RADIOS THEN BEGAN FAI LING. AS THE LIGHTS WERE DIMMING, FIRE WARNING LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT AIRPORT WITHOUT FURTHER INCID ENT. GENERATOR FAIL LIGHT DID NOT ILLUMINATE. THE STARTER/GENERATOR BRUSHES WERE REPLACED AND A FUNCTIONAL TEST OF THE STARTER/GENERATOR SYSTEM WAS SATISFACTORILY PERFORMED. 1 G 7 1 3U H9EU 1999121800075 19991218 00075 1999 12 18 SWAA992033 4 19991209 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM SLIDE MISLOCATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY AND SERVICE DOORS EVACUATION SLIDE RELEASE CABLES OUT OF POSITION. REROUTED CABLES PER MM. 2 L 7 2 4F A16WE 1999121800076 19991218 00076 NM 1999 12 18 SWAA992034 1 19991209 A 3350 07912 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED A2 CHECK, FOUND EEPLS LIGHT LENS MISSING AT MID CABIN. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 1999121800077 19991218 00077 NM 1999 12 18 SWAA992035 1 19991209 A 3350 07912 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS MISSING AT MID CABIN. REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121800078 19991218 00078 NM 1999 12 18 SWAA992036 1 19991209 A 5320 65C27314 CLIP BOEING 737 7375H4 138449D NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED, BS 400, STRINGER 15L, AND BS 277, STRINGER 15R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2 L 7 2 4F RT A16WE 1999121800079 19991218 00079 NM 1999 12 18 SWAA992037 1 19991209 A 2820 714810 VALVE BOEING 737 7372H4 138448C NM NR 1 ENGINE LEAKING A SWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 059SW 21811 ABORTED TAKEOFF, POWER LOSS AT NR 1 ENGINE DURING TAKEOFF ROLL. FOUND NR 1 ENG P/D VALVE LEAKING FUEL. REMOVED AND REP LACED NR 1 ENG P/D VALVE PER MM. 2 L 7 2 4F A16WE 1999121800080 19991218 00080 NM 1999 12 18 SWAA992038 1 19991209 A 5270 284A0133 SWITCH BOEING 737 7373H4 1384600 NM CARGO DOOR OUT OF ADJUST A SWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 754SW 29849 AIR TURNBACK, AFT CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF AND CABIN PRESSURE RATE OF CLIMB SLOW. ADJUSTED AND LUBRI CATED AFT CARGO DOOR LIGHT SWITCH PER MM. PRESSURIZED ACFT, NO LEAKS NOTED. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999121800081 19991218 00081 NM 1999 12 18 SWAA992025 1 19991204 A 3230 6973169 BOLT BOEING 737 7373H4 1384600 NM LT MLG SHEARED A SWAA O OTHER O OTHER LD LANDING 1 SW 07 661SW 23173 LT MLG TORQUE LINK BOLT SHEARED IMMEDIATELY AFTER LANDING. SHIMMY DAMPER DEPARTED FROM GEAR, WALKING BEAM OUTBD ATTACH FITTING CRACKED, OUTER CYL TRUNION ATTACH LUGS CHAFED. MX FERRY TO DAL. REPLACED LT MLG TORQUE LINK BOLT. REPLACED SH IMMY DAMPER. REMOVED AND REPLACED WALKING BEAM OUTBOARD ATTACH FITTING, C/W 12K NR 1 PYLON INSPECTION. REPAIRED OUTER CYL TRUNION ATTACH LUGS PER SWA RA NR 1-332-0023, REV 1. 2 L 7 2 4F RT A16WE 1999121800082 19991218 00082 1999 12 18 SWAA992026 4 19991208 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 FWD SERVICE DOOR EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999121800083 19991218 00083 NM 1999 12 18 SWAA992027 1 19991208 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY P ER MM. 2 L 7 2 4F RT A16WE 1999121800084 19991218 00084 NM 1999 12 18 SWAA992028 1 19991208 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND BS 270 FLOORBEAM UPPER SURFACE CORRODED, LBL 11-RBL 11. REMOVED AND REPLACED UPPER CHOR D SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999121800085 19991218 00085 NM 1999 12 18 SWAA992029 1 19991208 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND BS 616 FUSELAGE FRAME CRACKED, LBL 64. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999121800086 19991218 00086 NM 1999 12 18 SWAA992030 1 19991208 A 5754 6573714 SKIN BOEING 737 7375H4 138449D NM LE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND NR 3 L/E SLAT INBOARD END DELAMINATED. REPAIRED SLAT PAR ER NR 99-6418 AND SRM. 2 L 7 2 4F RT A16WE 1999121800087 19991218 00087 NM 1999 12 18 SWAA992031 1 19991209 A 3350 07912 LIGHT BOEING 737 7373H4 1384600 NM ROW 10 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 619SW 28035 EEPLS TRACK PULLED UP AT ROW 10. SECURED TRACK ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121800088 19991218 00088 NM 1999 12 18 SWAA992032 1 19991209 A 3350 65C27095 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED C3 CHECK, FOUND CABIN OVERHEAD EMERGENCY AISLE LIGHTS INOP. REMOVCED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1999121800089 19991218 00089 NM 1999 12 18 SWAA992002 1 19991203 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 747 - 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED RON, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 747-767, BETWEEN STRINGERS 19R-20R. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 1999121800090 19991218 00090 1999 12 18 SWAA992003 4 19991204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121800091 19991218 00091 NM 1999 12 18 SWAA992004 1 19991203 A 3150 6545756 WARNING SYSTEM BOEING 737 7373H4 1384600 NM COCKPIT ACTIVATED A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 360SW 26571 ABOTED TAKEOFF, TAKEOFF WARNING SOUNDED. ALL CONTROLS IN NORMAL POSITION. C/W TAKEOFF WARNING TEST. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999121800092 19991218 00092 NM 1999 12 18 SWAA992005 1 19991204 A 5330 6545774 SKIN BOEING 737 7372H4 138448C NM BS 805 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING WALKAROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED BS 805, STRINGER 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999121800093 19991218 00093 NM 1999 12 18 SWAA992006 1 19991205 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 611SW 27697 EEPLS WIRES EXPOSED AT OVERWING EXIT. REPAIRED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999121800094 19991218 00094 NM 1999 12 18 SWAA992007 1 19991203 A 3350 101073 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED D CHECK, FOUND BOTH FWD EMERGENCY EVACUATION SLIDE LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM. 2 L 7 2 4F A16WE 1999121800095 19991218 00095 NM 1999 12 18 SWAA992008 1 19991203 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED SERVICE CHECK, FOUND RT FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM . 2 L 7 2 4F RT A16WE 1999121800096 19991218 00096 NM 1999 12 18 SWAA992009 1 19991203 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 312, STRINGER 6L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999121800097 19991218 00097 NM 1999 12 18 SWAA992010 1 19991204 A 5330 6545767 SKIN BOEING 737 7372T4 1384492 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED RON, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 520, STRINGER 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 1999121800098 19991218 00098 1999 12 18 SWAA992011 4 19991204 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR DISCHARGED A SWAA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SL IDE ASSY. 2 L 7 2 4F RT A16WE 1999121800099 19991218 00099 NM 1999 12 18 SWAA992012 1 19991204 A 5312 6516300 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED AT 5 EACH PLACES, BETWEEN LBL 7 AND RBL 7. REPAIRED BULKHEAD PE R SRM. 2 L 7 2 4F RT A16WE 1999121800100 19991218 00100 EU 1999 12 18 AWXA9900465 1 19991209 A 3397 131122 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 635AW 092 EMERGENCY EXIT LT OUT, AT AFT MOST LT SEAT ROW. REPAIRED BROKEN WIRE AT AFT SEAT. 2 L 7 2 4F RT A28NM 1999121800101 19991218 00101 NM 1999 12 18 AWXA9900466 1 19991209 A 3350 864705 POWER SUPPLY BOEING 737 7372U9 1384498 NM SEATS 6 - 14 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 EMERGENCY EXIT PATH LIGHTING INOP SEATS 6-14. REMOVED AND REPLACED LIGHTING AMP. 2 L 7 2 4F RT A16WE 1999121800102 19991218 00102 NM 1999 12 18 AWXA9900467 1 19991209 A 3397 131122 WIRE BOEING 737 7372U9 1384498 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 EMERGENCY ESCAPE LIGHT INOP. REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A16WE 1999121800103 19991218 00103 NM 1999 12 18 AWXA9900468 1 19991209 A 5320 BAC1509100146 SUPPORT BOEING 737 73733A 1384673 NM BS 858 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 CORROSION ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT, AFT CARGO BAY, O/B OF STRINGER 27R FS 858. REMOVED DAMAGE. FABR ICATED REPAIR ANGLES FRM 5HT 7075, 0.071 R710334 AND SHT 7075 0.080 R71036. HEAT TREATED TO T6 IAW SRM 53-00-53. ALO DINED AND PRIMED PER SRM 51-20-01 AND INSTALLED WET PER SRM 53-00-53 FIG 201 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999121800104 19991218 00104 NM 1999 12 18 AWXA9900469 1 19991209 A 5315 654681143 FLOORBEAM BOEING 737 73733A 1384673 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 TOP OF MAIN CABIN FLOORBEAM STA 986, INSIDE R-2 DOOR HAS CORROSION ON TOP SIDE. REMOVED AND REPLACED T- CAP. FABRICATE D CAP FRM 7075-T BAC/ 1505. STRAP .063 7075-T6 AND .071 7075-T6. SUPPORT ANGLES 7075T6 0.63 AND 7075T6 .071 PER SRM 53-00-51. ALONDINED AND PRIMED IAW SRM 53-20-01. INSTALLED PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 1999121800105 19991218 00105 NM 1999 12 18 AWXA9900470 1 19991209 A 5315 BAC150510067 FLOORBEAM BOEING 737 73733A 1384673 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 MAIN CABIN FLOORBEAM STA 947 HAS CORROSION ON TOP SURFACE. REMOVED DAMAGE, FABRICATED T CAP FRM MAT'L 1505-100617 R696 03 7075-T73 ANGLE FRM BAC 1490-2865 7075-T6, STRAPS 7075-T6 .071 AND 7075-T6 .063 PER SRM 53-60-51 FIG 202. TREATED AND PRIMED PER SRM 51-20-01. 2 L 7 2 4F RT A16WE 1999121800106 19991218 00106 NM 1999 12 18 AWXA9900471 1 19991209 A 5347 6546813 SEAT TRACK BOEING 737 73733A 1384673 NM BS 328 - 480 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 SEAT TRACK OUT OF LIMITS AND CRACKED STA 328-480 RBL 45.5. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52. TREATED AND PRIMED PER S1-20-01. 2 L 7 2 4F RT A16WE 1999121800107 19991218 00107 NM 1999 12 18 AWXA9900472 1 19991209 A 5754 6546431 SKIN BOEING 737 7373S3 1384711 NM LE FLAP GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 RIGHT WING OTBD FORE FLAP GOUGED AT INBD UPPER SURFACE. REMOVED EXISTING DAMAGED REPAIR. FABRICATED REPAIR DOUBLER PER SRM 57-33-01 FRM .032 301 1/2 HARD R602099--CAD PLATED PER SOPM 20-42-01. INSTALLED REPAIR PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999121800108 19991218 00108 NM 1999 12 18 AWXA9900473 1 19991209 A 5313 BAC1498151 STRINGER BOEING 737 7373S3 1384711 NM BS 344 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 FWD CABIN FS 344 STR 8A RT CRACKED. REMOVED DAMAGED SECTION PER SRM 51-40-02. FABRICATED REPLACEMENT PART FRM CLAD 707 5T6 QQA250/13 R642745 PER SRM 53-10-30 FIG 1. TREATED AND PRIMED PER 51-20-02. INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999121800109 19991218 00109 NM 1999 12 18 AWXA9900474 1 19991209 A 5347 6546813 SEAT TRACK BOEING 737 7373S3 1384711 NM BS 520 - 634 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 SEAT TRACK STA 520-634 WENT OUT OF LIMITS LBL 45. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02. FABRICATED AND INSTALL ED REPLACEMENT PER SRM 53-00-52 MAT'L BAC 1520841 7178T6511 QQA-200/13C R65996, TREATED AND PRIMED. 2 L 7 2 4F RT A16WE 1999121800110 19991218 00110 WP 1999 12 18 9905221154 1 19991111 A 2530 OVEN DOUG DC10 DC1040 3023508 WP GALLEY FIRE A NWAA F D ACTIVATE FIRE EXT. RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 154US 46763 AFTER PUSHBACK, FLIGHT ATTENDANT REPORTED FIRE IN AFT GALLEY. ONE HALON BOTTLE WAS DISCHARGED. AIRCRAFT RETURNED TO GA TE. FIRE WAS CAUSED BY PAPER/TRASH BEHIND THE OVENS AND COFFEEMAKER. AFTER CLEANUP, GALLEY EQUIPMENT WAS CHECKED FOR P ROPER OPERATION. CHECKED OK. 2 L 7 3 4F A22WE 1999121800111 19991218 00111 NM 1999 12 18 9905236718 1 19991203 A 2612 FIRE LOOP BOEING 747 747251F 1384898 NM NR 4 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 618US 21122 DURING CRUISE, THE NR 4 ENGINE NACELLE FIRE DETECTION FAULT LIGHT ILLUMINATED. THE FIRE DETECTION LIGHT ILLUMINATED INT ERMITTENTLY AND THE 'A' AND 'B' NACELLE TEMP INDICATORS INTERMITTENTLY INDICATED HIGH. AIRCRAFT DIVERTED TO DTW AND LAN DED WITHOUT INCIDENT. REPLACED THE LOWER AFT LOOP DETECTOR AND BLEED ELEMENT SENSING LINE DUE TO LINE TOUCHING THE UPPE R AFT LOOP LINE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999121800112 19991218 00112 NM 1999 12 18 9905245514 1 19991207 A 3350 LIGHT BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 514US 23202 DURING INTERIOR CHECK, MAINTENANCE FOUND FORWARD SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE DUE TO BROKEN WIRE AT EL ECTRICAL CONNECTOR. REPLACED THE ELECTRICAL CONNECTOR. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1999121800113 19991218 00113 EU 1999 12 18 9905253248 1 19991130 A 5210 B5211084620000 BUSHING AIRBUS 320 A320212 EU PAX DOOR LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 348NW 410 AFTER ARRIVING AT THE GATE AND DEPLANING PASSENGERS. CATERING CREW FOUND THAT THEY WERE UNABLE TO OPEN DOOR 2L. MAINTE NANCE FOUND THE DOOR UPPER SAFETY PIN GUIDE BUSHINGS HAD MIGRATED OUT OF THE FITTING NOT ALLOWING FOR FULL RETRACTION OF THE SAFETY PIN REQUIRED FOR DOOR OPENING. BUSHINGS WERE CEMENTED IN PROPER POSITION AND DOOR OPERATIONALLY CHECK NORMA L. 2 L 7 2 4F RT A28NM 1999121800114 19991218 00114 NE 1999 12 18 9905269758 2 19991204 A 7314 378200 PUMP DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE RT ENGINE FAILED A NWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 758NW 41689 47286 676231 DURING CRUISE FLIGHT, THE RIGHT ENGINE FLAMED OUT AT FL350; SMOOTH AIR, NO VIBRATION, AND NO RELIGHT. THE RIGHT ENGINE WAS WINDMILLED AT 17-22 PERCENT AND POSITIVE OIL PRESSURE WAS MAINTAINED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DIVE RTED FLIGHT TO BUF, AND LANDED WITHOUT INCIDENT. THE RIGHT ENGINE OIL TEMPERATURE WAS 120C AT TOUCHDOWN. LANDING WEIGH T AT TOUCHDOWN WAS 94,000 LBS WITH A SINK RATE LESS THAN 200 FEET PER MINUTE. MAINTENANCE REPLACED THE MAIN FUEL PUMP O N THE RIGHT ENGINE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1999121800115 19991218 00115 1999 12 18 9905276633 4 19991208 A 2330 20072F PROJECTOR BOEING 747 747227B 1384888 NM CABIN FAILED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 633US 21991 EN ROUTE TO KIX, MOVIE PROJECTOR BR PRODUCED SMOKE AND SPARKS. POWER WAS TURNED OFF AND AIRCRAFT CONTINUED TO KIX AND L ANDED WITHOUT INCIDENT. REPLACED PROJECTOR. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999121800116 19991218 00116 SO 1999 12 18 COMA9910181 1 19991206 A 3250 STEERING UNIT EMB 120 EMB120RT SO NLG MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 258CA 120247 AIRCRAFT VEERED LEFT SHARPLY DURING TAKEOFF ROLL. COULD NOT DUPLICTE. NO DEFECTS FOUND IN STEERING SYSTEM. 2 L 7 2 4T RT A31SO 1999121800117 19991218 00117 SO 1999 12 18 COMA9910182 1 19991206 A 2150 AIR CONDITIONING EMB 120 EMB120RT SO RT PACK FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 261CA 120254 RIGHT AIR CONDITIONING FAILED. COULD NOT DUPLICATE. SYSTEM FUNCTION CHECK NORMAL. 2 L 7 2 4T RT A31SO 1999121800118 19991218 00118 EA 1999 12 18 COMA9960748 1 19991206 A 3260 864807 PSEU CNDAIR CL600 CL6002B19 EA MLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 710CA 4140 2678 7241 LANDING GEAR DISAGREE WARNING WHEN SELECTED UP. REPLACED THE PSEU, RETRACT CHECKS SATISFACTORY. 2 L 7 2 4F RT A21EA 1999121800119 19991218 00119 NE 1999 12 18 COMA9960749 2 19991205 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT LACK OF LUBE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 713CA 7245 807532 RIGHT ENGINE LOW OIL PRESSURE WARNING IFSD. REPLACED RIGHT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800120 19991218 00120 EU 1999 12 18 QXEA9902501 1 19991115 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - TOP LAYER OF FUSELAGE SKIN, IMMEDIATELY AFT OF RADOME IS ROLLED BACK OVER AND AREA OF .375 BY 5 WIDE. REPAIRED IA W FOKKER SRM 53-02-02, PAGE 2. 2 L 7 2 4F RT A20EU 1999121800121 19991218 00121 EU 1999 12 18 QXEA9902502 1 19991117 A 5321 FLOOR PANEL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - BL33.0 WL22.047 CORROSION IN SEVERAL PLACES, NEAR AFT WALL 3 OUTBOARD OF CO-PILOTS RIGHT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999121800122 19991218 00122 EU 1999 12 18 QXEA9902503 1 19991117 A 5321 FLOOR PANEL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CORROSION ON CO-PILOTS FLOOR, 11 FORWARD OD COCKPIT AFT WALL, JUST OUTBOARD OF CO-PILOTS RIGHT SEAT TRACK. REPAIR ED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999121800123 19991218 00123 EU 1999 12 18 QXEA9902504 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CORROSION UNDER PILOTS LEFT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999121800124 19991218 00124 EU 1999 12 18 QXEA9902505 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CORROSION UNDER PILOTS RIGHT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999121800125 19991218 00125 EU 1999 12 18 QXEA9902506 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CORROSION UNDER CO-PILOTS LEFT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999121800126 19991218 00126 EU 1999 12 18 QXEA9902507 1 19991117 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CORROSION UNDER CO-PILOTS RIGHT SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999121800127 19991218 00127 EU 1999 12 18 QXEA9902508 1 19991128 A 5610 POST FOKKER F28 F28MK4000 4990810 EU COCKPIT WINDOW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - TYPE A CRACK ON RIGHT SIDE NR 3 WINDOW POST. REPAIRED IAW HORIZON AIR EA 4-53-56B. 2 L 7 2 4F RT A20EU 1999121800128 19991218 00128 EU 1999 12 18 QXEA9902509 1 19991118 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FUSELAGE SKIN UNDER AFT EDGE OF PANEL 91BC IS CHAFFED. REPAIRED IAW HORIZON AIR EA 4-53-931. 2 L 7 2 4F RT A20EU 1999121800129 19991218 00129 EU 1999 12 18 QXEA9902510 1 19991115 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACK IN THE ANGLE/BRACKET WHICH ATTACHES THE SHORT FLOORBEAM TO THE AFT PRESSURE BULKHEAD, AT BL330 RH . REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A. 2 L 7 2 4F RT A20EU 1999121800130 19991218 00130 EU 1999 12 18 QXEA9902511 1 19991113 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACK IN THE ANGLE/BRACKET WHICH ATTACHES THE SHORT FLOORBEAM TO THE AFT PRESSURE BULKHEAD AT BL320LH. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A. 2 L 7 2 4F RT A20EU 1999121800131 19991218 00131 EU 1999 12 18 QXEA9902512 1 19991116 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815B CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO PIT CRACKED FRAME CLIP AT FRAME 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999121800132 19991218 00132 EU 1999 12 18 QXEA9902513 1 19991124 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815A CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - AFT CARGO PIT CRACKED FRAME CLIP AT FRAME 13815A AND STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGUR E 2. 2 L 7 2 4F RT A20EU 1999121800133 19991218 00133 EU 1999 12 18 QXEA9902514 1 19991129 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - ANGLE AND BULKHEAD CHAFFED IN RIGHT WHEELWELL WHERE AFT OUTBOARD EDGE OF GEAR DOOR CONTACTS. REPAIRED IAW HORIZON AIR EA 4-57-328. 2 L 7 2 4F RT A20EU 1999121800134 19991218 00134 EU 1999 12 18 QXEA9902515 1 19991110 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - TOOLING DAMAGE TO PLATE ON TOP OF FRAME 8305 AT CENTER CARGO DOOR LOWER TORSION BOX. REPAIRED IAW FOKKER SRM 51-3 1-01, PAGE 13, PARAGRAPH 7A, SRM 51-31-05 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999121800135 19991218 00135 EU 1999 12 18 QXEA9902516 1 19991130 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8805 MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE ARE TWO DRILLED HOLES IN FRAME 8805 ABOVE STRINGER 67IN THE FORWARD CARGO BAY. REPAIRED IAW HORIZON AIR EA 4-53-921. 2 L 7 2 4F RT A20EU 1999121800136 19991218 00136 EU 1999 12 18 QXEA9902517 1 19991105 A 4910 DUCT FOKKER F28 F28MK4000 4990810 EU APU CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - APU FUSELAGE INTAKE DUCT IS CRACKED AT AFT LOWER CORNER. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999121800137 19991218 00137 EU 1999 12 18 QXEA9902518 1 19991112 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A GROOVE CHAFFED INTO LUG, IN SUPPORT STRUCTURE, DIRECTLY UNDER LEFT SPEED BRAKE PANEL SUPPORT LINK, LOWE R ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4-53-936. 2 L 7 2 4F RT A20EU 1999121800138 19991218 00138 EU 1999 12 18 QXEA9902519 1 19991115 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 58.5 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - CRACK IN CLIP AT AFT SIDE OF FRAME 58.5-2, ABOVE STRINGER 46. REPAIRED IAW FOKKER MM 53-10-05. 2 L 7 2 4F RT A20EU 1999121800139 19991218 00139 EU 1999 12 18 QXEA9902520 1 19991116 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACKED CLIP AT AFT SIDE OF FRAME 50-2 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1999121800140 19991218 00140 EU 1999 12 18 QXEA9902521 1 19991114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACKED CLIP AT FRAME 50-2 AND STRINGER 24. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-30-02 AND SRM 53- 10-05. 2 L 7 2 4F RT A20EU 1999121800141 19991218 00141 EU 1999 12 18 QXEA9902522 1 19991108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACKED CLIP AT FRAME 19976 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 4, SCHEME 1 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999121800142 19991218 00142 EU 1999 12 18 QXEA9902523 1 19991116 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACKED CLIP AT FRAME 19976 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6, FIGURE 4 AND FO KKER MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999121800143 19991218 00143 EU 1999 12 18 QXEA9902524 1 19991115 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACKED CLIP AT FRAME 20075 AND STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6, FIGURE 4, REPAI R SCHEME 1. 2 L 7 2 4F RT A20EU 1999121800144 19991218 00144 EU 1999 12 18 QXEA9902525 1 19991119 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU BS 19775 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS SEVERE CHAFFING DAMAGE INTO VERTICAL BEAM TENSION MEMBER WEBBING, AT BL425R, JUST AFT OF STATION 19775, R EPAIRED IAW HORIZON AIR EA 4-53-932. 2 L 7 2 4F RT A20EU 1999121800145 19991218 00145 EU 1999 12 18 QXEA9902526 1 19991116 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - SEVERAL RIVET HEADS AND NUT PLATE SURROUNDS ON FUSELAGE SKIN UNDER APU HEAT SHIELD, HAVE LIGHT SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999121800146 19991218 00146 EU 1999 12 18 QXEA9902527 1 19991124 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 50 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - THERE IS A CRACK ON THE CORNER CUTOUT FOR STRINGER 27 ON FRAME 50-2. REPAIRED IAW HORIZON AIR EA 4-53-934. 2 L 7 2 4F RT A20EU 1999121800147 19991218 00147 EU 1999 12 18 QXEA9902528 1 19991124 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - FRAME 32-2 AND STRINGER 25 HAS THREE CRACKS AROUND BOTTOM RIVET OF CLIP. REPAIRED IAW FOKKER SRM 51-31-01, 51-30- 02 AND FOKKER MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1999121800148 19991218 00148 EU 1999 12 18 QXEA9902529 1 19991116 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - PANEL APERTURE AND PANEL 72A HAVE PITTING/FRETTING CORROSION AROUND HOLES FOR FASTENERS. REPAIRED IAW 57-01-01, P AGE 5. 2 L 7 2 4F RT A20EU 1999121800149 19991218 00149 EU 1999 12 18 QXEA9902530 1 19991116 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - PANEL 74D ACCESS PANEL APERTURE HAS FRETTING CORROSION AROUND FASTENER HOLES. REPAIRED IAW 57-01-01, PAGE 5. 2 L 7 2 4F RT A20EU 1999121800150 19991218 00150 EU 1999 12 18 QXEA9902531 1 19991116 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - PANEL 74C AND ACCESS PANEL APERTURE HAS FRETTING CORROSION AROUND FASTENER HOLES. REPAIRED IAW 57-01-01, PAGE 5. 2 L 7 2 4F RT A20EU 1999121800151 19991218 00151 EU 1999 12 18 QXEA9902532 1 19991116 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - PANEL 74B AND ACCESS PANEL APERTURE HAS FRETTING CORROSION AROUND THE FASTENERS. REPAIRED IAW 57-01-01, PAGE 5. 2 L 7 2 4F RT A20EU 1999121800152 19991218 00152 EU 1999 12 18 QXEA9902533 1 19991116 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - PANEL APERTURE AND PANEL 74A HAS CORROSION AROUND THE FASTENER HOLES. REPAIRED IAW 57-01-01, PAGE 5. 2 L 7 2 4F RT A20EU 1999121800153 19991218 00153 EU 1999 12 18 QXEA9902534 1 19991124 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU WS 4700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 PDX - Z STRINGERS 2.13 AND 2.10 ARE CRACKED ON LEFT WING AT APPROXIMATELY STATION 4700. REPAIRED IAW HORIZON AIR EA 4-5 7-327. 2 L 7 2 4F RT A20EU 1999121800154 19991218 00154 NM 1999 12 18 QXEA9902541 1 19991208 A 3350 2T1C106 RELAY DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 345PH 476 PDX - EMERGENCY TRACK LIGHTING ILLUMINATES INTERMITTANTLY. REPLACED K3 AND K4 RELAYS ON EMERGENCY LIGHT CONTROL BOX. O PERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. K3 RELAY PART NUMBER DSC-76-2. 2 H 7 2 4T RT A13NM 1999121800155 19991218 00155 NM 1999 12 18 99FDEA00501 1 19991210 A 5610 B275600102A WINDOW BOEING 727 727233 138408A NM COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 286FE 22623 99-284 - R2 WINDOW STARTED ARCING. SHUT R2 OFF COMPLIED WITH RED TABS. REMOVED AND REPLACED NR 2 SLIDING WINDOW. ADJU STED PER MM 56-12-011-5. 2 L 7 3 4F RT A3WE 1999121800156 19991218 00156 WP 1999 12 18 ABXA9900831 1 19991105 A 5311 99118593 FRAME DOUG DOUG DC9 DC932F 3022067 WP BS 1104 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND CANTED FRAME AT STATION 1104 CRACKED AT LONGERONS 15, 16 AND 20 LEFT AND LONGERONS 5, 14 AND 18 R IGHT. REPLACED THREE FRAME SECTIONS IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999121800157 19991218 00157 WP 1999 12 18 ABXA9900832 1 19991105 A 5311 59135956 FRAME DOUG DOUG DC9 DC932F 3022067 WP BS 1076 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FRAME CRACKED AT STATION 1076 AND LONGERON 19 RIGHT. REPLACED FRAME IAW DC9 SRM 51-30-2 AND 51-30 -5. 2 L 7 2 4F A6WE 1999121800158 19991218 00158 WP 1999 12 18 ABXA9900833 1 19991105 A 5311 99115023 FRAME DOUG DOUG DC9 DC932F 3022067 WP BS 58 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FUSELAGE FRAME CRACKED AT STATION 58 AND 12 O'CLOCK POSITION. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1999121800159 19991218 00159 WP 1999 12 18 ABXA9900834 1 19991018 A 5511 565208612 SPAR DOUG DOUG DC8 DC863F 302198F WP HORIZONTAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 RIGHT HORIZONTAL STABILIZER SPAR WEB CRACKED AT LOWER LIP OF LIGHTENING HOLE AT STATION XE 79.000. REPAIRED IAW ABX REA D855-33601 MR. 2 L 7 4 4F 4A25 1999121800160 19991218 00160 WP 1999 12 18 ABXA9900835 1 19991021 A 5730 57537361 SKIN DOUG DOUG DC8 DC863F 302198F WP WS 76 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 THE FORWARD END OF LOWER LEFT WING SKIN DOUBLER WAS CORRODED. REPAIRED LEFT WING SKIN DOUBLER AT XRS 76 AND STRINGER 58 IAW ABX REA D857-33115MR. 2 L 7 4 4F 4A25 1999121800161 19991218 00161 WP 1999 12 18 MWEA99880 1 19991208 A 7997 WIRE DOUG DC9 DC914 3022034 WP RT ENGINE CHAFED A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 80ME 45795 MASTER CAUTION LIGHT AND RIGHT OIL STRAINER CLOGGING LIGHT CAME ON. FOUND CHAFED WIRE IN WIRE BUNDLE IN DIFFERENTIAL PR ESSURE SENSOR ON RIGHT ENGINE AND REPAIRED. 2 L 7 2 4F A6WE 1999121800162 19991218 00162 WP 1999 12 18 MWEA99881 1 19991123 A 5330 591140659 SKIN DOUG DC9 DC982 3022082 WP BS 221 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 DENT IN FUSELAGE SKIN AT STATION 221 BETWEEN LONGERON17L AND 18L. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999121800163 19991218 00163 WP 1999 12 18 MWEA99882 1 19991203 A 5713 59121563 STRINGER DOUG DC9 DC932 3022066 WP WS 232 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 DAMAGE TO FORWARD STRINGER AT STATION XRS 232 ON LEFT WING. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1999121800164 19991218 00164 WP 1999 12 18 MWEA99883 1 19991128 A 3211 5935812509 FITTING DOUG DC9 DC982 3022082 WP LT MLG CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FOUND CORROSION IN CUP AREA OF LEFT MAIN LANDING GEAR FITTING BOTTLE BOLT AREA. MTC REMOVED CORROSION, REMANUFACTURED O VERSIZE BUSHING AND INSTALLED. 2 L 7 2 4F A6WE 1999121800165 19991218 00165 WP 1999 12 18 MWEA99884 1 19991210 A 5753 5910040513 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LEADING EDGE SKIN OF LEFT FLAP, BOTTOM MOVEABLE VANE, OUTBOARD END, IS CHAFED. MAINTENANCE FABRICATED AND INSTALLED SKI N REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999121800166 19991218 00166 WP 1999 12 18 MWEA99885 1 19991210 A 2760 9919474503 RIB DOUG DC9 DC932 3022066 WP SPOILER CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LEFT INBOARD SPOILER, INBOARD TRAILING EDGE RIB IS CHAFED. MAINTENANCE FITTED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 1999121800167 19991218 00167 WP 1999 12 18 MWEA99886 1 19991210 A 5720 5919289510 FITTING DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CORROSION AROUND TWO LOWER ATTACH BOLTS OF RIGHT MAIN LANDING GEAR TRUNNION FITTING, LOWER OUTBOARD FLANGE. MAINT ENANCE REWORKED HOLES PER MIDWEST EXPRESS AND BOEING ENGINEERING INSTRUCTIONS. 2 L 7 2 4F A6WE 1999121800168 19991218 00168 WP 1999 12 18 MWEA99887 1 19991210 A 5320 995821471 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 897 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 SHEAR TIE AT STATION 897, LONGERON 24 LEFT HAS GOUGE AROUND FASTENER HOLE FOR FLOOR SUPPORT. MAINTENANCE FITTED AND INS TALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 1999121800169 19991218 00169 WP 1999 12 18 MWEA99888 1 19991210 A 5315 995821437 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 897 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT BAGGAGE PIT FLOORBEAM SUPPORT AT STATION 897, LONGERON 24 LEFT, HAS CORROSION. MAINTENANCE FITTED AND INSTALLED NEW FLOORBEAM SUPPORT. 2 L 7 2 4F A6WE 1999121800170 19991218 00170 WP 1999 12 18 MWEA99889 1 19991210 A 5210 991556533 FRAME DOUG DC9 DC932 3022066 WP PAX DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT ENTRANCE DOOR FRAME HAS A CHAFE FORWARD AND BELOW LEFT SHOULDER HARNESS ATTACH POINT. MAINTENANCE FABRICATED AND IN STALLED FRAME REPAIR. 2 L 7 2 4F A6WE 1999121800171 19991218 00171 WP 1999 12 18 MWEA99890 1 19991210 A 5210 995575965 BEAM DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 PASSENGER DOOR, NUMBER EIGHT BEAM IS CRACKED ON FORWARD SIDE IN RADIUS. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOU BLER. 2 L 7 2 4F A6WE 1999121800172 19991218 00172 WP 1999 12 18 MWEA99891 1 19991210 A 5753 5910040513 DOUBLER DOUG DC9 DC932 3022066 WP TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LEFT LOWER MOVEABLE VANE IS CHAFED JUST BELOW INBOARD FORWARD STOP. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER . 2 L 7 2 4F A6WE 1999121800173 19991218 00173 WP 1999 12 18 MWEA99892 1 19991210 A 5752 5910047501 CONTROL TAB DOUG DC9 DC932 3022066 WP LT AILERON DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 BOTTOM TRAILING EDGE OF LEFT AILERON CONTROL TAB HAS A DENT. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1999121800174 19991218 00174 WP 1999 12 18 MWEA99893 1 19991210 A 5320 99196373 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 408 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND ELONGATED HOLE IN CENTER AFT FLANGE OF INTERCOSTAL AT STATION 408. MAINTENANCE FABRICATED AND INSTALLED REPAIR AN GLE. 2 L 7 2 4F A6WE 1999121800175 19991218 00175 WP 1999 12 18 MWEA99894 1 19991210 A 5315 9911544507 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 CHAFING DAMAGE FOUND ON LOWER LEG OF FLOORBEAM AT STATION 389 AND STATION 408, IN FORWARD CARGO COMPARTMENT. MAINTENANC E FABRICATED AND INSTALLED BEAM REPAIR. 2 L 7 2 4F A6WE 1999121800176 19991218 00176 WP 1999 12 18 MWEA99895 1 19991210 A 5210 995575015 INTERCOSTAL DOUG DC9 DC932 3022066 WP PAX DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 PASSENGER DOOR INTERCOSTAL FLANGE BETWEEN BEAM SIX AND BEAM SEVEN IS BENT DOWN AND DISTORTED. MAINTENANCE FABRICATED AN D INSTALLED INTERCOSTAL REPAIR. 2 L 7 2 4F A6WE 1999121800177 19991218 00177 NM 1999 12 18 VNAA9912007 1 19991209 A 3350 321230 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 434JS 8872 1211 3051 THE FLIGHT CREW FOUND THE EMERGENCY LIGHTS 7, 8, AND 9 NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPE CTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-O1. OPE RATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121800178 19991218 00178 NM 1999 12 18 VNAA9912008 1 19991209 A 2435 8160121 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE STARTER/GEN FAILED A VNAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 07 438JS 7214 342 3056 116122 DURING CRUISE, FLIGHT 4168 EXPERIENCED A RIGHT GENERATOR FAILURE. THE AIRCRAFT WAS 20 MILES FROM CAK, SO MAINTENANCE CO NTROL DIVERTED THE AIRCRAFT TO CAK. MAINTENANCE INSPECTED AND REPLACED THE RIGHT STARTER GENERATOR IN ACCORDANCE WITH D ORNIER MAINTENANCE MANUAL 29-31-01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED AND CONTINUED ON TO AZO WITHOUT FURTHER INCIDENT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121800179 19991218 00179 NE 1999 12 18 VNAA9912009 2 19991209 A 7321 8111803004 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ENGINE FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 459PS 10022 3070 116150 DURING TAKEOFF, THE RIGHT ELECTRONIC ENGINE CONTROL UNIT FAILED. THE CREW ABORTED TAKEOFF AND CLEARED THE RUNWAY. THE CREW PERFORMED THE QUICK REFERENCE HANDBOOK PROCEDURES AND RESET THE ELECTRONIC ENGINE CONTROL UNIT AND WAS RELEASED FOR ANOTHER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121800180 19991218 00180 NE 1999 12 18 VNAA9912010 2 19991209 A 7321 8111803004 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ENGINE FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 459PS 10022 3070 116150 DURING TAKEOFF, THE RIGHT ELECTRONIC ENGINE CONTROL UNIT FAILED. THE CREW ABORTED TAKEOFF AND CLEARED THE RUNWAY. MAIN TENANCE INSPECTED AND CLEANED THE ELECTRONIC ENGINE CONTROL UNIT AND INTERCOMP BLEED VALVE CANNON PLUGS IN ACCORDANCE WI TH DORNIER MAINTENANCE MANUAL 73-21-01. OPERATIONAL CHECKS AND GROUND RUNS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999121800181 19991218 00181 1999 12 18 RAIA9912009 3 19991208 A 6140 31056294 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PROPELLER FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 566HK 2925 2925 41084 6209 - JFK - LEFT BETA LIGHT INOP. MAINTENANCE REPLACED LEFT BETA SWITCH. 2 L 7 2 4T RT A41NM 1999121800182 19991218 00182 NE 1999 12 18 RAIA9912013 2 19991209 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RIGHT LEAKING A RAIA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 559HK 7243 7243 41075 7144-STL - RIGHT ENGINE WAS SHUT DOWN INFLIGHT FOR LOW OIL PRESSURE. MAINTENANCE RE-TORQUED RT ENGINE UPPER OUTBOARD OI L COOLER FITTING. 2 L 7 2 4T 4 T RT A41NM E18NE 1999121800185 19991218 00185 SW 1999 12 18 99ZZZX4522 1 19991209 A 5302 407023800118 SUPPORT 407030801101 BELL 407 407 SW TAILBOOM CRACKED A A NXTA K NONE O OTHER IN INSP/MAINT 1 SW 19 147CF 696 53281 53281 PILOT FOUND CRACK ON PRE-FLIGHT CHECK NEAR FORWARD END OF HORIZONTAL STABILIZER MOUNTING BRACKET (UPPER). THIS OEM INST ALLED BRACKET WAS LOADED WHEN INSTALLED. MFG SUPPLIED APPROVED DATA AND BRACKET WAS REPLACED. THIS BRACKET WAS ON THE RIGHT HAND SIDE OF TAILBOOM. 1 G 7 1 3U O H2SW 1999121800192 19991218 00192 NE 1999 12 18 99ZZZX4529 2 19991101 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NACELLE MALFUNCTIONED A PCAA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 EA 13 831EX 19977 160 910306 ENGINE REMOVED FROM AIRCRAFT DUE TO MODERATE VIBRATION AT 900 RPM. 2 H 7 2 4T 4 T RT A13NM E20NE 1999121800193 19991218 00193 NE 1999 12 18 99ZZZX4530 2 19991101 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NACELLE MALFUNCTIONED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 832EX 19977 280 890116 ENGINE REMOVED FROM AIRCRAFT DUE TO MODERATE VIBRATION AT 1,050 RPM, SLIGHT AT 900 RPM. 2 H 7 2 4T 4 T RT A13NM E20NE 1999121800194 19991218 00194 NE 1999 12 18 99ZZZX4531 2 19991101 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NACELLE MALFUNCTIONED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 836EX 19977 297 940603 ENGINE REMOVED FROM AIRCRAFT DUE TO VIBRATION AT 1,050 RPM. 2 H 7 2 4T 4 T RT A13NM E20NE 1999121800199 19991218 00199 CE 1999 12 18 99ZZZX4536 1 19991029 A 2133 1304061 VALVE AIRESRCH LEAR 35 35A 5170602 CE FUSELAGE CRACKED A A J7EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 317TT 6766 1212018 317 AS A RESULT OF A RECENT PRESSURE VESSEL INSP, FOUND THE SAFETY VALVE, PN 130406-1, SN 121-2018, DATED 12-22-81 BY LEAR, WAS FOUND TO HAVE A CRACKED NR 1 BOSS. BY DATE AND S/N, THIS VALVE IS NOT AFFECTED BY AD 95-20-03 (LEARJET SB 35-21-19) . TO LOCATE CRACK, 'AN' FITTING WAS REMOVED. PRESSURIZATION SYS WAS WORKING NORMALLY, WITH NO INDICATION OF A CRACK. LEARJET CONFIRMED CRACKS NOT ACCEPTABLE AND VALVE REPLACED. SINCE BOTH OUTFLOW VALVE AND SAFETY VALVE HAVE SAME P/N, BO TH VALVES WERE CHECKED. NO CRACKS FOUND IN THE OUTFLOW VALVE. CRACK WAS APPARENTLY CAUSED BY OVERTORQUE SITUATION, OR, OVER A PERIOD OF TIME, CAUSED BY EXTREME TEMP CHANGES. SUBMITTER SUSPECTED OVERTQORQUE POSSIBILITY FIRST. 2 L 7 2 4F A10CE 1999121800208 19991218 00208 CE 1999 12 18 99ZZZX4545 1 19991108 A 3010 993800093 DEICER BEECH 99 B99 1154004 CE HORZONTIAL STAB CONTAMINATED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 950AA U159 ROUTINE CHECK OF SURFACE DEICERS REVEALED WATER SPRAYING FROM HOLES IN THE TAIL SURFACE DEICERS. REPLACED BOTH SURFACE DEICERS. OPS CHECK OF OTHER BOOTS REVEALED NO WATER AND PROPER OPERATION. 1 L 7 2 3T A14CE 1999121800218 19991218 00218 CE 1999 12 18 99ZZZX4555 1 19991112 A 2730 115610010 TAPER PINS BEECH 99 99 1154002 CE TORQUE TUBE LOOSE A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 14MV U59 INSPECTION OF ELEVATOR TORQUE TUBE REVEALED LOOSE TAPER PINS ATTACHING THE TUBE TO THE COLLAR. ENTIRE TORQUE TUBE ASSEM BLY WAS REPLACED WITH A SERVICEABLE UNIT. THE MM PROVIDES LIMITED CRITERIA FOR RESTORING ORIGINAL SECURITY BETWEEN TUBE AND COLLAR. PERHAPS USING A TAPERED REAMER TO REMOVE A SMALL QUANTITY OF MATERIAL COULD RETURN TUBE ASSEMBLY TO ORIGIN AL SECURITY. 1 L 7 2 3T A14CE 1999121800222 19991218 00222 EA 1999 12 18 99ZZZX4559 2 19991209 A 7414 1068291018 BEARING BENDIX PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA MAGNETO FAILED A WVBA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 AL 01 59764 1645 30280 317652037 L209468A PILOT RETURNED TO BASE CITING ENGINE FAILURE. ENGINE WOULD NOT START WHEN ATTEMPTED ON GROUND. FURTHER INVESTIGATION R EVEALED THE DUAL MAGNETO EXPERIENCED TOTAL BEARING FAILURE. MAGNETO WAS REPLACED AND A FULL GROUND RUN AND LEAK CHECK ACCOMPLISHED. GROUND CHECK APPEARS NORMAL. NOTE: SEVERAL SINGLE ENGINE AIRCRAFT ALSO USE THIS DUEL MAGNETO. 1 L 7 2 3O 3 O A20SO E14EA 1999121800225 19991218 00225 GL 1999 12 18 99ZZZX4562 2 19990805 A 7321 23070264 ECU BELL 407 407 SW ALLSN 250C 250C47B GL ENGINE FAILED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 973AA 53167 THE ECU, SN JG7ALK0380 FAILED AND WENT INTO THE MANUAL MODE. ATTEMPTS WERE MADE TO DOWNLOAD INFORMATION FROM THE ECU WI TH NO RESULTS. REMOVED THE DEFECTIVE ECU. INSTALLED SERVICEABLE ECU. GROUND RAN AIRCRAFT. ALL SYSTEMS FUNCTIONALLY C HECKED OK. GROUNDED AIRCRAFT, AND SENT DEFECTIVE UNIT TO CHANDLER EVANS FOR EVALUATION UNTIL RECORDING DATA COULD BE RE TRIEVED TO DETERMINE ANY EXCEEDENCES. 1 G 7 1 3U 3 U O H2SW E1GL 1999121800226 19991218 00226 SW 1999 12 18 99ZZZX4563 1 19991021 A 6510 407340340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL 25 RNFS3349 53264 DURING 25-HOUR AD INSPECTION. DURING DAILY INSPECTION. DISC PACK FOUND CRACKED WITH CRACK FACING AFT TOWARDS TAIL ROTO R IN NR 3 POSITION. CAUSE NOT KNOWN. ONLY ONE SEGMENT WAS FOUND CRACKED. 1 G 7 1 3U O H2SW 1999121800227 19991218 00227 SW 1999 12 18 99ZZZX4564 1 19991012 A 6510 407340340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL RNFS2976 53284 DURING 25-HOUR AD INSPECTION, FOUND NR 7 TAILROTOR DISC CRACKED. 1 G 7 1 3U O H2SW 1999121800228 19991218 00228 SW 1999 12 18 99ZZZX4565 1 19991009 A 6720 406312103101 BEARING 407012101105 BELL 407 407 SW PITCH LINK WORN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 417AL A456 53054 ON DAILY INSPECTION, FOUND OUTER RACE OF PITCH CHANGE LINK SPHERICAL BEARING WORN THROUGH BY BALL ALLOWING LINK TO CONTA CT PITCH HORN CAUSING DAMAGE TO BOTH REQUIRING SCRAPPING. 1 G 7 1 3U O H2SW 1999121800229 19991218 00229 SW 1999 12 18 99ZZZX4566 1 19991012 A 6510 407340340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL RNF29 53141 DURING 25-HOUR AD INSPECTION, FOUND NR 7 TAILROTOR DISC CRACKED IN TWO PLACES. 1 G 7 1 3U O H2SW 1999121800230 19991218 00230 SW 1999 12 18 99ZZZX4567 1 19990925 A 6510 407340340101 DISC PACK 407040302103 BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 627AL 77 A1199 53284 DURING 25-HOUR AD INSPECTION, FOUND CRACKED 1ST FORWARD SEGMENT. 1 G 7 1 3U O H2SW 1999121800231 19991218 00231 SW 1999 12 18 99ZZZX4568 1 19990925 A 6510 407340340101 DISC PACK 407040325101 BELL 407 407 SW T/R DRVIE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 547AL A542 53240 DURING 25-HOUR AD INSPECTION, FOUND AFT DISC IN PACK CRACKED IN HALF. 1 G 7 1 3U O H2SW 1999121800245 19991218 00245 SW 1999 12 18 99ZZZX4582 1 19991005 A 6510 407340340101 DISC PACK BELL 407 407 SW TAIL ROTOR CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL RNFS2104 53141 DURING 25-HOUR AD INSPECTION. 50-HOUR PMI LAST 50-HOUR INSPECTION DONE AT 2,867.5 HOURS. AFT LAMINATE OF NR 6 DISC PAC K CRACKED. 1 G 7 1 3U O H2SW 1999121800253 19991218 00253 SW 1999 12 18 99ZZZX4590 1 19991018 A 6322 206061432121 HOUSING 407040303105 BELL 407 407 SW COOLER BLOWER CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 497AL 308 A272 53172 DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING. 1 G 7 1 3U O H2SW 1999121800260 19991218 00260 SW 1999 12 18 99ZZZX4597 1 19991111 A 6520 212040054013 CASE 412040002105 BELL 412 412 1182202 SW M/R GEARBOX CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 169EH 12096 1748 A1203375 33064 MAIN SUPPPORT CASE AFT LEFT MOUNTING EAR IS CORRODED AND CRACKED ACROSS MOUNT BOLT BUSHING. 1 G 7 2 4U H4SW 1999121800262 19991218 00262 SW 1999 12 18 99ZZZX4599 1 19990826 A 6510 406040340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL F5091390511 53264 DURING 25-HOUR AD INSPECTION, FOUND CRACK AT FORWARD SEGMENT AT THE DISC PACK, NR 3 POSITION. 1 G 7 1 3U O H2SW 1999121800263 19991218 00263 SW 1999 12 18 99ZZZX4600 1 19990930 A 6510 406040340101 DISC PACK 407040303101 BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL AFS670 53230 DURING 25-HOUR AD INSPECTION, NR 3 DISC PACK CRACKED AT FORWARD DISC. IT IS CRACKED IN ONLY ONE LOCATION. 1 G 7 1 3U O H2SW 1999121800265 19991218 00265 SO 1999 12 18 RAAA99E8059 1 19991211 A 3350 37067001 BATTERY PACK GRIMES 1102833 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY EXIT INDICATOR CEILING LIGHT INOP AT ROW 12. REPLACED BATTERY AND OPS CHECKED IAW RAA GMM. 2 L 7 4 4T 4A22 1999121800266 19991218 00266 SO 1999 12 18 RAAA99E8060 1 19991211 A 3350 86210066 BATTERY PACK INTVLV 87310012 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EMERGENCY AISLE LIGHT AT ROW 13 C,D,E INOP. REPLACED BATTERY AND OPS CHECKED IAW RAA GMM. 2 L 7 4 4T 4A22 1999121800267 19991218 00267 EA 1999 12 18 COMA9960750 1 19991212 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT SHATTERED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 934CA 9894 7042 PILOT FORWARD WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED PILOT FORWARD WINDSHIELD. 2 L 7 2 4F RT A21EA 1999121800268 19991218 00268 EA 1999 12 18 COMA9960751 1 19991212 A 5730 601R10045 PANEL CNDAIR CL600 CL6002B19 EA WS 136.676 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 LOWER HORIZONTAL SURFACE OF RIGHT HAND LOWER WING ACCESS HOLES AT 640FB AND 650EB CRACKED. BLENDED OUT DAMAGE, ROTO PEE NED AND ALODINED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 1999121800269 19991218 00269 WP 1999 12 18 UPS99831192 1 19991211 A 2752 ACTUATOR DOUG DC8 DC871F 302199D WP TE FLAP LEAKING A IPXA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 715UP 45915 INSPECTION TYPE:N/A, AFTER LANDING WHEN PULLING INTO PARKING RES PRESSURE LIGHT ILLUMINATED AND THEN FLIGHT CONTROL MANU AL LIGHTS. ONLY HAD ACCUMULATOR PRESSURE TO STOP AIRCRAFT. FLAPS DID NOT RETRACT. REMOVED AND REPLACED INBOARD LT FLA P ACTUATOR, OPS CK AND FUNCTIONAL CHECK NORMAL. NO LEAKS NOTED IAW MM 27-51-09 PAGE 410. 2 L 7 4 4F RT 4A25 1999121800270 19991218 00270 WP 1999 12 18 UPS99831193 1 19991210 A 2730 57025792 SKIN DOUG DC8 DC873F 302199F WP ELEVATOR TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A, RT ELEVATOR CONTROL TAB DELAMINATED BOTTOM SIDE. REMOVED AND REPLACED RIGHT ELEVATOR GEARED TAB IA W MM 27-30-03. 2 L 7 4 4F RT 4A25 1999121800271 19991218 00271 WP 1999 12 18 UPS99831194 1 19991209 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:N/A, PUNCTURE IN LT HORIZONTAL STABILIZER LEADING EDGE. *S/D* REMOVED DAMAGED SECTION OF L/E SKIN PER SRM 55-2-1 BPT 92716 PC 1565 0. FABRICATED AND DRILLED REPAIR DOUBLER PER SRM 55-2-1. BAT 92716 12-13-99. INSTALLED DO UBLER PER SRM 55-2-1. 2 L 7 4 4F RT 4A25 1999121800272 19991218 00272 1999 12 18 SCNA99150 2 19991207 A 7532 PRBC BOEING 727 7272J4 1384006 NM NR 2 ENGINE LACK OF LUBE A SCNA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 GL 15 288SC 20765 ON FINAL APPROACH, THE NUMBER TWO COMPRESSOR STALLED WHEN POWER WAS ADDED. LUBRICATED PRBC VALVE IAW MM 720000. OPERAT IONAL CHECK ON VALVE OK. 2 L 7 3 4F RT A3WE 1999121800273 19991218 00273 NM 1999 12 18 HNAA9900166 1 19991210 A 3350 82425110001 HARNESS DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 975HA 37814 176 FIRST THREE WHITE FLOOR EMERGENCY LIGHTS INOP. INSPECTED EMERGENCY LIGHT AND FOUND BROKEN WIRE AT LIGHT SOCKET. ALSO, FOUND LOOSE PIN AT 3352 P-1. RE-SECURED PIN, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999121800274 19991218 00274 NM 1999 12 18 HNAA9900167 1 19991210 A 3230 82910010107 LINE DHAV DHC8 DHC8102 2809003 NM NLG LEAKING A HNAA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 07 909HA 018 AFTER REAR RETRACTION LOUD RUSHING AIR NOISE, BURNING SMELL AND NOTICED SMOKE UNDER RIGHT C/B PNL. FOUND HYD LEAK IN NL G DOWN LINE UNDER COCKPIT FLOOR. INSTALLED SPLICE IN LINE USING QUICK FIT HYD REPAIR KIT LEAK AND OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1999121800275 19991218 00275 WP 1999 12 18 CALA9901579 1 19991208 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP BS 218 - 256 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA 218-256. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53- 05, FIGURE 4F. 2 L 7 2 4F A6WE 1999121800276 19991218 00276 WP 1999 12 18 CALA9901580 1 19991209 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND THE FORWARD ENTRY DOOR EXTERNAL SKIN DENTED AT LOWER EDGE. THE DENTED AREA WAS REMOVED SRM 52-05, FIGU RE 37. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 37, 51-10-04, 51-10-03, AND 51-30-02. 2 L 7 2 4F A6WE 1999121800277 19991218 00277 NM 1999 12 18 CALA9901581 1 19991209 A 3350 1000679 LIGHT GRIMES BOEING 727 727232 1384082 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT AFT ENTRY INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND OPERATION CHECK ED IAW MM 33-50-01. 2 L 7 3 4F A3WE 1999121800278 19991218 00278 NM 1999 12 18 CALA9901582 1 19991209 A 5510 SKIN BOEING 737 737524 1384721 NM HORIZONTAL STAB PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16650 28911 INSPECTION FOUND A PUNCTURE IN LT I/B HORIZONTAL STABILIZER LEADING EDGE AT STA 70. A FLUSH DOUBLER REPAIR WAS INSTALLE D IAW SRM 55-10-01. 2 L 7 2 4F RT A16WE 1999121800279 19991218 00279 NM 1999 12 18 CALA9901583 1 19991210 A 3350 20131A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND THE L-1 AND L-2 DOOR EXIT SIGNS INOPERATIVE. THE BATTERY PACK FOR EACH SIGN WAS REMOVED, RECHARGED, RE INSTALLED AND OPERATION CHECKED GOOD IAW MM 33-51-01. 2 L 7 3 4F A3WE 1999121800280 19991218 00280 NM 1999 12 18 CALA9901584 1 19991210 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN CHAFED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND THE LT OVERWING EMERGENCY LIGHTS IN MID AND AFT POSITIONS INOPERATIVE. MAINTENANCE FOUND A CHAFED WIRE BEHIND WHEEL WELL FAIRING PANEL AREA. THE WIRE WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6. 2 L 7 3 4F A3WE 1999121800281 19991218 00281 NM 1999 12 18 CALA9901585 1 19991210 A 3350 20131A BATTERY RADIANT BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND MID CABIN FIXED EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CH ECKED GOOD IAW MM 33-51-00, PAGE 6. 2 L 7 3 4F A3WE 1999121800282 19991218 00282 NM 1999 12 18 CALA9901586 1 19991210 A 3350 20131A BATTERY PACK RADIANT BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 THE RT OVERWING EMERGENCY EXIT LIGHTS IN THE MID AND AFT POSITIONS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED , RECHARGED, REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6. 2 L 7 3 4F A3WE 1999121800283 19991218 00283 NM 1999 12 18 CALA9901587 1 19991210 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND THE EMERGENCY PATH LIGHTS IN SECTION 3 AND 4 INOPERATIVE. BROKEN WIRES AT SECTION 3 AND 4 WERE REPAIRE D IAW MM 33-10-00 AND OPERATIONAL CHECK WAS GOOD. 2 L 7 3 4F A3WE 1999121800284 19991218 00284 NM 1999 12 18 CALA9901588 1 19991210 A 3350 20131A BATTERY PACK RADIANT BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND THE EMERGENCY LIGHT AT AFT AIRSTAIR INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, REINSTALLED, OPERATION CHECKED GOOD IAW MM 33-51-01, PAGE 6. 2 L 7 3 4F A3WE 1999121800285 19991218 00285 NM 1999 12 18 CALA9901589 1 19991213 A 3350 20121 CHARGER MATHEWS BOEING 757 757224 1384958 NM ROWS 15 - 25 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17122 27564 INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 15-25. THE BATTERY CHARGER WAS REPLACED AND OPERATION CHECKED GOO D IAW MM 33-51-07. 2 L 7 2 4F RT A2NM 1999121800286 19991218 00286 NM 1999 12 18 QXEA9902592 1 19991209 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 814PH 14341 21 43 PDX- COCKPIT EMERGENCY LIGHT ILLUMINATED WHEN EMERGENCY LIGHTS WERE ARMED. REPLACED COCKPIT LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999121800287 19991218 00287 NM 1999 12 18 QXEA9902595 1 19991213 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 356PH 502 SEA- COCKPIT OVERHEAD EMERGENCY PORTABLE LANTERN WAS NOT CHARGED TO NORMAL BRIGHTNESS. REPLACED COCKPIT EMERGENCY LIGHT , OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999121800288 19991218 00288 WP 1999 12 18 99UAL900600 1 19991112 A 2150 22155696 SEAL DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 PACK CRACKED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1849U 46939 FLIGHT ATTENDANTS REPORT ODOR OF BURNT RUBBER IN CABIN AFTER T/O WHEN PACKS TURNED ON. ALSO, NOSE GEAR RUMBLING AFTER R ETRACTIONS. *S/D* REPLACED DAMAGED SEAL ON NR 3 PACK HEAT EXCHANGER, IN AIR CONDITIONING COMPARTMENT. THERE HAS BEEN NO REOCCURANCE SINCE REPAIR. 2 L 7 3 4F 4 F A22WE E23EA 1999121800289 20001016 00289 NE 2000 10 16 99UAL900624 2 19991203 A 7320 7791005 FUEL CONTROL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 591UA 19307 1390 28142 727195 RETURNED TO THE FIELD AT ORD DUE TO ENGINE INDICATION. *S/D* THE FUEL CONTROL UNIT WAS REPLACED FOR FLUCTUATING ENGINE PARAMETERS. THE FUEL CONTROL UNIT HAD A LEAKING MAIN PRESSURE SHUTOFF VALVE (MPSOV). 2 L 7 2 4F 4 F RT A2NM E17NE 1999121800290 19991218 00290 1999 12 18 99UAL900625 4 19991204 A 2565 S283T00610 SENSOR ELDEC CORP S283T00610 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WING SLIDE DIRTY A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 576UA 26690 RETURNED TO EWR DUE TO EICAS WING SLIDE MESSAGE. LEFT OFF-WING SLIDE COMPARTMENT DOOR FOUND CLOSED. DOOR SENSOR S283T0 06-10 WAS FOUND TO BE DIRTY. SENSOR WAS CLEANED, AND TESTED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 1999121800291 19991218 00291 NM 1999 12 18 99UAL900626 1 19991205 A 7931 6131506531 HARNESS BOEING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE CHAFED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 363UA 7300 24532 724288 AT 120 KNOTS THE AIRCRAFT ABORTED AT TAKEOFF DUE TO NR 1 ENGINE LOW OIL PRESSURE INDICATION. *S/D* DURING TROUBLESHOOT ING, THE LOW OIL PRESSURE CONNECTOR WIRES WERE SHORTED. REPAIRED EACH WIRE AND RAN THE ENGINE. THE ENGINE LOW OIL PRES SURE INDICATION SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121800292 20001016 00292 2000 10 16 99UAL900627 4 19991205 A 2210 AFCS BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 924UA 26645 ON CLIMBOUT THE AIRCRAFT EXPERIENCED UNCOMMANDED YAW AND THE AUTOPILOT DISCONNECTED. *S/D* PINS 25 AND 26 SHORTED TO P IN 24 IN CONNECTOR 4079J OF THE E1-3 SHELF. REMOVED THE SHORT, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121800293 19991218 00293 1999 12 18 99UAL900628 4 19991203 A 2565 LIGHT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE SLIDE INOPERATIVE A UALA O OTHER L NO TEST NR NOT REPORTED 1 WP 29 1858U 46987 THE 3L SLIDE PRESS TO TEST LIGHT INOP. 2 L 7 3 4F 4 F A22WE E23EA 1999121800294 20001016 00294 NM 2000 10 16 99UAL900629 1 19991205 A 2612 18252 ELEMENT 18252 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7261U 21408 NR 1 ENGINE DOES NOT PASS FIRE TEST (WHEN SELECTED TO ENGINE & WHEEL WELL TEST). *S/D* REPLACED NR 1 ENG FIRE DETECTIO N ELEMENT M447. SYSTEM OPERATIONAL CHECK NORMAL NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1999121800295 19991218 00295 NM 1999 12 18 99UAL900630 1 19991204 A 5300 UNKNOWN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG WW SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7287U 21565 CREW REPORTED, SMOKE IN THE RIGHT MAIN LANDING GEAR WHEEL WELL. FOUND RESIDUAL GLYCOL AT RIGHT MAIN LANDING GEAR WHEEL WELL, APU EXHAUST DUCT EVAPORATING WITH APU OPERATION. CLEANED AREA, CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1999121800296 19991218 00296 NM 1999 12 18 99UAL900631 1 19991204 A 2530 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY MALFUNCTIONED A UALA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 613UA 21874 AIRCRAFT RETURNED TO BLOCKS, SPARKS IN AFT GALLEY OVEN AREA. 2 L 7 2 4F 4 F RT A1NM E3NE 1999121800297 20001016 00297 NM 2000 10 16 99UAL900632 1 19991204 A 3233 273T11005 ACTUATOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE MLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 614UA 21875 INBOUND TO SFO AND JFK, WHEN EXTENDING GEAR GOT NORMAL INDICATIONS FROM NOSE AND RIGHT GEAR. GOT EICAS GEAR DISAGREE ME SSAGE AND NO LEFT GEAR INDICATION FOR APPROX 5 SECONDS. FINALLY LEFT GEAR GREEN AND EICAS MESSAGE WENT AWAY. *S/D* R EPLACED LEFT MAIN GEAR RETRACT ACTUATOR. (PART OFF WAS MR32387-11). 2 L 7 2 4F 4 F RT A1NM E3NE 1999121800298 19991218 00298 NM 1999 12 18 99UAL900633 1 19991205 A 3260 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 643UA 25093 HALF OF THE NOSE GEAR, RIGHT MAIN AND ALL LEFT MAIN GEAR LIGHTS REMAINED ILLUMINATED DIM AFTER RETRACTION. GEAR DID SEE M UP. FLIGHT RETURNED TO SFO. 2 L 7 2 4F 4 F RT A1NM E24NE 1999121800299 19991218 00299 NM 1999 12 18 99UAL900634 1 19991206 A 2421 GENERATOR HAMILTON SUN 729825G BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 547UA C0687 25368 AIRCRAFT RETURNED TO ORD, DUE TO LEFT ENGINE GENERATOR PROBLEM. REPLACED LEFT (NR 1) INTEGRATED DRIVE GENERATOR (IDG). THE IDG HAD AN INTERNAL DIODE FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999121800300 19991218 00300 NM 1999 12 18 99UAL900635 1 19991203 A 5320 SILL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 990 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7462U 21916 DURING A HEAVY MAINTENANCE VISIT, CORROSION DAMAGE WAS FOUND IN TWO FASTENER HOLES COMMON TO THE AFT CARGO DOOR LOWER SI LL OUTBOARD CHORD AT STATION 990. THE DISCREPANT HOLES WERE OVERSIZED TO .400 INCH DIAMETER TO REMOVE ALL THE DAMAGE AN D FREEZE PLUGS. INSTALLED PER SRM 51-10-07. THIS REPAIR IS CONSIDERED MAJOR AND WAS APPROVED BY AN 8110-3 BY BOEING'S DER. 2 L 7 3 4F 4 F A3WE E2EA 1999121800301 20001016 00301 NE 2000 10 16 99UAL900636 2 19991206 A 7230 6A4254 BLADE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 WP 29 812UA 5361 0 850 V10378 LOST NR 2 ENGINE ON CLIMBOUT PASSING 17,000 FT. LOUD BANG AND HIGH EGT. SHUTDOWN ENGINE. *S/D* STAGE 4 BLADE FAILED IN FATIGUE IN ROOT ATTACHMENT AREA, LIBERATING AIRFOIL AND PLATFORM AND CAUSING EXTENSIVE DOWNSTREAM DAMAGE. THE MANUFA CTURER HAS ISOLATED THE CAUSE TO A VSV SCHEDULE INTRODUCED WITH EEC SOFTWARE CHANGE NR 11. EEC SOFTWARE WILL BE REVISED TO REVERT TO PREVIOUS VSV SCHEDULE. A SERVICE BULLETIN IS EXPECTED IN APRIL. 2 L 7 2 4F 4 F RT A28NM E40NE 1999121800302 20001016 00302 NE 2000 10 16 99UAL900637 2 19991207 A 7230 STATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COMPRESSOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 590UA 8015 8015 28708 727248 DIVERTED TO DEN DUE TO NR 1 ENGINE COMPRESSOR STALLS. *S/D* AFTER LANDING AT DEN METAL WAS FOUND IN THE TAILPIPE AND T HE ENGINE WAS REPLACED AND SENT TO THE SHOP FOR INVESTIGATION AND REPAIR. SHOP DISASSEMBLY FINDING WAS A FAILED 10TH ST AGE STATOR THIS FAILURE MODE IS UNDER INDUSTRY INVESTIGATION BY PWA EAST HARTFORD. 2 L 7 2 4F 4 F RT A2NM E17NE 1999121800303 19991218 00303 NM 1999 12 18 99UAL900638 1 19991208 A 2150 BLOWER BOEING 10605471 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E BAY FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 395UA 00160997 24670 THE EQUIPMENT COOLING EXHAUST FAN CIRCUIT BREAKER POPPED, CAUSING AN ELECTRICAL SMELL. *S/D* THE EQUIPMENT BLOWER MOTO R MAIN BEARING FAILED. REPLACED THE EQUIPMENT BLOWER MOTOR AND RESET THE EQUIPMENT COOLING EXHAUST FAN CIRCUIT BREAKER. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121800304 19991218 00304 NM 1999 12 18 99UAL900639 1 19991208 A 2120 ODOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 347UA 24251 FLIGHT CREW REPORTED KEROSENE ODOR. EXECUTED SMOKE-FUMES-ODOR PROCEDURE IN FLIGHT MANUAL. OPERATED BOTH ENGINES AND PA CKS. NO FUMES OR ODOR NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999121800305 19991218 00305 NM 1999 12 18 99UAL900640 1 19991130 A 3320 CQCRA21WA4P CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 774UA 26936 AFT CABIN LIGHTING COULD NOT BE CONTROLLED THROUGH ANY OF THE CACP. FOUND C/B ON P110 POSITION G2 OEU TRANSFER BUSS POP PED, COULD NOT RESET. FOUND CONNECTOR ABOVE DOOR 3 LT SHORTED. *S/D* PIN 1 ON CONNECTOR D6535P SHORTED TO PIN 2. PI N 1 IS 115 VAC AND PIN 2 IS AC GROUND. THE SHORT DAMAGED BOTH THE PLUG & SOCKET CONNECTORS. WIRE WAS DAMAGED ON THE PL UG SIDE. EVIDENCE OF WATER ON THE CONNECTOR AND OTHER COMPONENTS MOUNTED ON THE OVERDOOR PANEL. POSSIBLE WATER DRIPPIN G ON THE CONNECTOR CAUSED THE SHORT. DOES NOT APPEAR TO HAVE BEEN ANY FAILURE OF THE CONNECTOR THAT WOULD HAVE ALLOWED THE 2 PINS TO MAKE CONTACT. THE CONNECTOR WAS REPLACED WITH AN ENVIRONMENTAL PLUG THAT RESISTS MOISTURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999121800306 19991218 00306 WP 1999 12 18 ABXA9900836 1 19991210 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 956AX 9049 47620 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY SUPPLY. 2 L 7 2 4F A6WE 1999121800307 19991218 00307 WP 1999 12 18 ABXA9900837 1 19991209 A 2170 21D101 COALESCER BAG DOUG DC9 DC941 302207N WP ACCESSORY COMP CONTAMINATED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 953AX 47608 ON TAKEOFF WITH EPR SET AT 2.07, SMELL OF BURNING RUBBER WAS NOTICED. SMELL DISSIPATED WHEN THROTTLES WERE REDUCED TO 1 .7 EPR FOR CLIMBOUT. ALL ENGINE INSTRUMENTS WERE NORMAL. GROUND RAN BOTH ENGINES WITH AIR CONDITIONING PACKS ON. NO S MELL WAS NOTICED. INSPECTED AND CLEANED THE SEAL TO THE ACCESSORY DOOR ABOVE THE NOSE LANDING GEAR. REPLACED COALESCER BAGS. 2 L 7 2 4F A6WE 1999121800308 19991218 00308 WP 1999 12 18 MWEA99896 1 19991213 A 5320 575468828 DOUBLER DOUG DC9 DC932 3022066 WP COCKPIT WINDOW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 42324 FOUND FIRST OFFICER'S WINDOW STAINLESS STEEL DOUBLER WAS CRACKED. MAINTENANCE FITTED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 1999121800309 19991218 00309 1999 12 18 MWEA99897 4 19991210 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 GALLEY DOOR SLIDE COVER LOOSE. MTC SECURED LOOSE SLIDE COVER. 2 L 7 2 4F A6WE 1999121800310 19991218 00310 1999 12 18 DLM88992619 2 19991129 A 7200 JT8D219 ENGINE JT8D219 DOUG MD88 MD88 3023688 NM NR 2 DAMAGED A DALA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 27 967DL 53116 AFTER TAKEOFF, HEARD LOUD NOISE, LOSS OF AIR CONDITIONING AND A FLOW LIGHT ILLUMINATED. RECEIVED FIRE WARNING ON THE NR 2 ENGINE. FOLLOWED ENGINE FIRE PROCEDURES. THE FIRE WARNING WENT OUT AT IDLE THRUST. TESTED THE FIRE WARNING SYSTEM AND TESTED GOOD. RETURNED TO ATL. REPLACED DAMAGED ENGINE COWL AND APRON. 2 L 7 2 4F RT A6WE 1999121800311 19991218 00311 WP 1999 12 18 DLL10992620 1 19991129 A 3610 PNEU DUCT LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE FAILED A DALA C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 1732D 193C1213 010657 WHILE ADVANCING PWR FOR A NO PACK T/O, A LOUD BANG WAS HEARD FOLLOWED BY A CABIN PRESSURE SURGE. J-AREA OVERHEAT, POM PROCEDURES COMPLETED. RETURNED TO GATE. MTC FOUND NR 2 DUCT BLOWN BEHIND AFT B/B WALL ON LEFT SIDE OF LAV TANK. 2 L 7 3 4F 4 F A23WE E12EU 1999121800312 19991218 00312 NM 1999 12 18 DL72S992621 1 19991116 A 5512 PANEL BOEING 727 727232 1384082 NM HORIZONTAL STAB WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 FOUND DURING MV2 CORROSION VISIT NRC 165, A .75 INCH HOLE IN NR 4 BALANCE BOARD CLOSURE PANEL. REPAIRED PER SRM 55-20-3 . 2 L 7 3 4F A3WE 1999121800313 19991218 00313 NM 1999 12 18 DL757992622 1 19991129 A 3350 GE767 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 697DL 30318 EMERGENCY LIGHTS INOP AT C2 DOOR AND R4 DOOR. RELAMPED BOTH, OPS CK GOOD. 2 L 7 2 4F RT A2NM 1999121800314 19991218 00314 NM 1999 12 18 DL72W992623 1 19991130 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2814W 20870 ON PREFLIGHT CHECKLIST, CREW FOUND RIGHT REAR EMERGENCY OVERWING LIGHT INOP IN EMERGENCY MODE ON TEST. FOUND CANNON PLU G DISCONNECTED ON ASSOCIATED BATTERY PACK. RECONNECTED CANNON PLUG, LIGHT TESTS GOOD IN EMERGENCY MODE ON CHECK OUT. 2 L 7 3 4F A3WE 1999121800315 19991218 00315 WP 1999 12 18 DLL14992625 1 19991130 A 3240 BRAKE 2136720PT1 LKHEED 1011 1011385115 5265015 WP LT MLG LEAKING A DALA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 SO 27 1739D 2234 193C1237 ON TAKEOFF, ANOTHER AIRCRAFT ON THE GROUND REPORTED SOME SMOKE COMING FROM THE LEFT MAIN LANDING GEAR. FOUND NR 2 REAR BRAKE LEAKING. REPLACED BRAKE ASSY, LEAK CHECKS OK. 2 L 7 3 4F A23WE 1999121800316 19991218 00316 NM 1999 12 18 DL72W992627 1 19991130 A 2170 COALESCER BOEING 727 727247 138408F NM ACCESSORY BAY CONTAMINATED A DALA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 2812W 20868 SMOKE ENTERED CABIN AFTER START, PACKS WERE ON BUT NOT OVERHEATED. PNEUMATIC SOURCE WAS APU ON ENGINE NR 1. REPLACED A PU FLOW-MULTIPLIER AND COALESCER BAGS. SERVICED APU TO PROPER LEVEL, OP CKS GOOD. 2 L 7 3 4F A3WE 1999121800317 19991218 00317 NM 1999 12 18 DL757992628 1 19991130 A 2910 296201054 LINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE RUPTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 675DL 25980 716458 DURING CLIMBOUT, L HYD QTY LIGHT ILLUMINATED, FOLLOWED BY SYS PRESS LIGHT. STATUS PAGE SHOWS L HYD SYS 0.00RF. FOUND E DP PRESS LINE RUPTURED. CHECKED EDP PRESS AND CASE DRAIN FILTERS, BOTH CLEAN. REPLACED BOTH FILTERS AND EDP AS PRECAUT ION. REPLACED LINE AND SERVICED HYD SYS. RAN ENG AND CHECKED EDP PER MM. PRESS AND LEAK CK OK. RE-CHECKED FILTERS, B OTH CLEAN. 2 L 7 2 4F 4 F RT A2NM E17NE 1999121800318 19991218 00318 NM 1999 12 18 DL72K992629 1 19991129 A 3350 BATTERY 38931002 BOEING 727 727232 1384082 NM BS 370 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA D896D898 21232 EMERGENCY LIGHT AT COCKPIT DOOR INOP. REPLACED BATTERY, CKS OK. 2 L 7 3 4F A3WE 1999121800319 19991218 00319 WP 1999 12 18 DLL10992630 1 19991130 A 3350 LIGHT 5165741 LKHEED 1011 10113851 5265010 WP CABIN INTERMITTENT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 64382 193C1173 L1 EVACUATION LIGHT OPERATES INTERMITTENTLY. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1999121800320 19991218 00320 NM 1999 12 18 DL767992631 1 19991130 A 5330 146T02005 SKIN BOEING 767 767232 1385132 NM BS 1197 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 110DL 22222 THE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 1197 & 1219 AND BETWEEN STRINGERS 36L & 38L. STRINGERS 36L & 37L WERE CRACK ED AND THE O/B SKIN FLANGE OF STRINGER 38L WAS CRACKED. THE DAMAGED SKIN WAS CUT OUT WITH A 10 X 18 CUTOUT AND THE DAMA GED FLANGE OF STR 38L WAS TRIMMED OUT. THE STRINGERS WERE REPAIRED PER B767 SRM, THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUM DOUBLER PER ER/A 368828-14, REV A. 2 L 7 2 4F RT A1NM 1999121800321 19991218 00321 NM 1999 12 18 DL72S992632 1 19991201 A 5754 ANGLE BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FOUND ON D1 LETTER CK, NR 6 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B STOP PAD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999121800322 19991218 00322 NM 1999 12 18 DL72K992633 1 19991201 A 3350 LIGHT 900835A BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 495DA 14445 21075 AFT CARGO DOOR EMERG LIGHT INOP. REPLACED BATTERY AT RACK M957, CHECKS GOOD. 2 L 7 3 4F A3WE 1999121800323 19991218 00323 NM 1999 12 18 DL72S992634 1 19991201 A 3350 900542 POWER SUPPLY BOEING 727 727232 1384082 NM BS 800 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 21020 RT FWD EMERG EXIT HATCH EMERGENCY LT INOP. FOUND FUSE BROKEN OFF IN SOCKET OF PWR SUPPLY. REPLACED SAME. 2 L 7 3 4F A3WE 1999121800324 19991218 00324 NM 1999 12 18 DL72S992635 1 19991116 A 5320 WEB BOEING 727 727232 1384082 NM BS 1213 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 A .125 INCH CRACK LT VERTICAL TORQUE BOX WEB AT UPPER END STA 1213L (MARKED). MANUFACTURED AND INSTALLED FILLER PER MM 53-11-0 PG 832. 2 L 7 3 4F A3WE 1999121800325 19991218 00325 NM 1999 12 18 DLM88992636 1 19991201 A 2520 CARPET DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 926DL 49713 AIRCRAFT DIVERTED TO PIT DUE TO ODOR REPORTED AROUNFD ROW 29 AND AFT. AIRCRAFT WAS THEN MAINTENANCE FERRIED TO CVG FOR INSPECTION/REPAIR. CVG REPLACED ALL UNDERSEAT CARPETS IN COACH CABIN. 2 L 7 2 4F RT A6WE 1999121800326 19991218 00326 NM 1999 12 18 DLM88992638 1 19991202 A 3244 TIRE M88M DOUG MD88 MD88 3023688 NM LT MLG FAILED A DALA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SO 27 979DL DL1074 53266 NR 2 MAIN TIRE RECAP SEPARATED FROM CASING. REPLACED NR 2 MAIN WHEEL ASSY. INSPECTED NR 1 ENG INTAKE, NO DAMAGE. REP LACED LEFT GEAR FLYING DOOR STRUT, NO OTHER DAMAGE NOTED. 2 L 7 2 4F RT A6WE 1999121800327 19991218 00327 NM 1999 12 18 DL76L992640 1 19991203 A 3320 331101733 BALLAST BOEING 767 767332 1382001 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 199DN 28456 ELECTRICAL ODOR WAS NOTICED AROUND SEAT 3A. THE BUSINESS CLASS BALLAST LIGHTS WERE TURNED OFF AND THE ODOR DISSIPATED . FOUND BALLAST FOR 3A SIDEWALL LIGHTS EXTREMELY HOT. REPLACED SAME, OPS CHECK GOOD. NO ELECTRICAL ODOR NOTED. 2 L 7 2 4F RT A1NM 1999121800328 19991218 00328 NM 1999 12 18 DLM11992642 1 19991203 A 2530 OVEN DOUG MD11 MD11 3023602 NM GALLEY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 809DE 48480 DURING FLIGHT, SMOKE WAS IN THE AFT SECTION OF THE A/C. TURNING OFF THE AFT GALLEY AND THE VCC/ADB SWITCH, SMOKE STOPPE D. FOUND PLASTIC IN ONE OF THE OVENS CREATING ODOR. 2 L 7 3 4F RT A22WE 1999121800329 19991218 00329 NM 1999 12 18 DL72S992643 1 19991203 A 2133 CONTROL VALVE 32167431 BOEING 727 727225A 1384077 NM LEFT PACK FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 8873Z P2686 21291 LOST CABIN ALTITUDE WHILE CRUISING AT FLIGHT LEVEL 250. LOSS OF CABIN PRESSURE PROCEDURES ACCOMPLISHED. CHANGED LT PAC K CONTROL VALVE PER MM, LEAKS CKS GOOD. 2 L 7 3 4F RT A3WE 1999121800330 19991218 00330 NM 1999 12 18 DL73K992644 1 19991203 A 5330 PANEL R6200M311 BOEING 737 737232 1384475 NM FUSELAGE LOOSE A DALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 27 312DL 831001 23084 LOUD NOISE COMING FROM RT REAR OF AIRCRAFT, FELT VIBRATION ON PEDALS DURING CRUISE AT FL 150 AND 240. NO AIRCRAFT CONTR OL PROBLEMS NOTICED. NO SIGNIFICANT PRESSURIZATION PROBLEMS NOTICED. INSPECTED A/C PER MM 5-51-281. FOUND DEBRIS ON A FT PRESS RELIEF VALVE AND LOOSE INSULATION AROUND SAME. REMOVED DEBRIS AND SECURED INSULATION. ALSO, FOUND LT RAM AIR DOOR SEAL TORN, KEEL BEAM AFT W/W PANEL LOOSE AND APU RAM AIR INLET DOOR LOOSE. SECURED PANELS, REPLACED APU INLET DOOR ACT AND HARDWARE, DEFERRED LT RAM AIR INLET DOOR SEAL. 2 L 7 2 4F RT A16WE 1999121800331 19991218 00331 NM 1999 12 18 DL72E992645 1 19991204 A 2752 ACTUATOR 2690021017 BOEING 727 727247 138408F NM LE FLAP FAILED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 831WA DL686X 21483 AFTER TAKEOFF, NR 7 SLAT WOULD NOT RETRACT UNTIL BACK ON GROUND. REPLACED NR 7 SLAT ACTUATOR AND EXTEND SWITCH, CHECKS OK. 2 L 7 3 4F A3WE 1999121800332 19991218 00332 NM 1999 12 18 DLM88992646 1 19991204 A 2121 6054578 FAN DOUG MD88 MD88 3023688 NM AIR DISTRIBUTION SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 931DL 49718 UNIDENTIFIED FUMES IN CABIN. FOUND FUMES COMING FROM CEASED CABIN AIR RECIR FAN. PULLED AND COLLARED C/B'S, FWD RECIR FAN TO MCO AND PLAC PER MEL 21-00-43. 2 L 7 2 4F RT A6WE 1999121800333 19991218 00333 NM 1999 12 18 DLM88992647 1 19991204 A 4990 APU DOUG MD88 MD88 3023688 NM APU LEAKING A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 911DL 7507 P80510 49542 DURING FLT, BURNING ODOR WAS NOTICED IN CABIN AND AFT LAV SMOKE DETECTOR WENT OFF. A/C RETURNED TO DEN. SUSPECT LEAK I N APU SYSTEM. DEACTIVATED APU. PERFORMED DUCT BURN-OUT PER MM. REPLACED COALESCER BAGS. 2 L 7 2 4F RT A6WE 1999121800334 19991218 00334 NM 1999 12 18 DL72W992649 1 19991204 A 3350 LIGHT 900542 BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 33165 22533 FWD AND AFT RT OVERWING EMERGENCY LIGHTS INOP. REPLACED RACK, OP CKS GOOD. 2 L 7 3 4F A3WE 1999121800335 19991218 00335 NM 1999 12 18 DLM88992650 1 19991204 A 2120 DUCT DOUG MD88 MD88 3023688 NM CABIN AIR ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 934DL 49721 ON SHORT FINAL 600 AGL, F/A REPORT SMOKE IN CABIN. PERFORMED POM AND SMOKE CLEARED. SMOKE SMELLED LIKE BLEED AIR. SMO KE CLEARED AFTER A/C PACKS TURNED OFF. BOTH PACK OIL LEVEL CHECK OK. COALESCER BAGS, NO CONTAMINATION AND CLEAN. ENG BLEED DUCT CHECKED, NO CONTAMINATION. BOTH PACKS OPS WITH APU, NO FAULTS. DUCT BURN-OUT PROCEDURE C/W PACK OPERATING W ITH ENG RUNNING NORMAL. 2 L 7 2 4F RT A6WE 1999121800336 19991218 00336 NM 1999 12 18 DL73K992651 1 19991204 A 3350 LIGHT BPS73 BOEING 737 737232 1384475 NM ROWS 1 - 3 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 302DL 6277 23047 EMERGENCY EXIT LIGHTING INOP ROWS 1 THRU 3. REPLACED PWR SUPPLY AND FOUND WIRES SHORTED AT ROW 4 D, E, F. REPAIRED SAM E, OPS CKS NORMAL. 2 L 7 2 4F RT A16WE 1999121800337 19991218 00337 NM 1999 12 18 DLM88992652 1 19991205 A 2721 TRIM TAB 95906 DOUG MD88 MD88 3023688 NM RUDDER SEIZED A DALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 27 947DL 2940 49878 PRIMARY TRIM INTERMITTENTLY FAILS. REPLACED PRIMARY TRIM ACTUATOR, ALL CKS NORMAL. 2 L 7 2 4F RT A6WE 1999121800338 19991218 00338 NM 1999 12 18 DL72K992653 1 19991205 A 2750 MS391130ZE MOTOR BOEING 727 727232 1384082 NM RT WHEEL WELL FAILED A DALA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 27 491DA 21060 AFTER T/O, O/B FLAPS FROZE AT 15 FOR A FEW SECONDS THEN WENT TO 5. O/B FLAPS DID NOT EXTEND FOR LANDING. PER PILOT REP ORT AN EMERGENCY WAS DECLARED. FOUND O/B FLAP HYD DRIVE MOTOR AT FAULT. MOTOR AND CASE DRAIN CHECK VALVE WERE REPLACED PER M/M. 2 L 7 3 4F A3WE 1999121800339 19991218 00339 WP 1999 12 18 DLL19992654 1 19991205 A 2530 OVEN LKHEED 1011 10113853 5265020 WP GALLEY DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 767DA 193H1209 INBOUND PILOT REPORT, OVENS IN ALL GALLEYS GET VERY HOT AND CREATE A LOT OF SMOKE THROUGHOUT A/C. OVENS NEED CLEANING T O REMOVE OLD FOOD. OVENS CLEANED BY CABIN SERVICE. 2 L 7 3 4F A23WE 1999121800340 19991218 00340 NE 1999 12 18 DL73K992655 2 19991206 A 7250 JT8D15AHK TURBINE WHEEL BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE DAMAGED A DALA E C ENGINE SHUTDOWN ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SO 27 329DL 37273 23101 709175 AT APPROX 400 FT AGL, LOUD BANG, NR 1 ENGINE FAILED 700 DEGREES EGT, WINDMILLING N1 AND N2 WAS BLOF T/O DUE TO GROSS WT. FOUND 3RD STAGE OF LPT DAMAGED. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2EA 1999121800341 19991218 00341 NM 1999 12 18 DL76G992656 1 19991206 A 3350 20131A BATTERY BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 24984 DURING SQUIB TEST, FOUND EMERGENCY ESCAPE SQUIBS NOT TESTING PROPERLY. FOUND MODULE M08962 BATTERY BAD. REPLACED SAME, ALL CKS OK. 2 L 7 2 4F RT A1NM 1999121800342 19991218 00342 NM 1999 12 18 DL767992658 1 19991206 A 3233 273T11027 ACTUATOR BOEING 767 767232 1385132 NM MLG CRACKED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 111DN MHB045 22223 A LOUD THUMP HEARD ON GEAR RETRACTION. AFTER GEAR WAS PUT TO THE DOWN POS THE LEFT GEAR GREEN LIGHTS WERE NOT ON AND HA D A GEAR DISAGREE AND DOORS DISAGREE LIGHTS. CREW LANDED UNEVENTFUL. MTC FOUND THE LT GEAR SIDE BRACE CRACKED AND THE BRACE BEYOND OVER CENTER. ALSO, FOUND MAIN LANDING GEAR ACTUATOR ROD SHEARED AT GEAR SIDE. REPLACED AFFECTED COMPONENT S. 2 L 7 2 4F RT A1NM 1999121800343 19991218 00343 NM 1999 12 18 DL72W992659 1 19991206 A 5755 SKIN BOEING 727 727247 138408F NM SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 LTR CHK C-1 12/6/99, NR 3 SPOILER DELAMINATED UPPER O/B SIDE. REPAIRED PER SRM 57-50-6. 2 L 7 3 4F A3WE 1999121800344 19991218 00344 NM 1999 12 18 DL72S992660 1 19991206 A 3350 1680X BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 419DA 21272 ON SVC CHECK, FOUND RT R1 EMERGENCY LIGHT INOP. REPLACED BULB, OPS CK GOOD. 2 L 7 3 4F A3WE 1999121800345 19991218 00345 NM 1999 12 18 DL72W992662 1 19991207 A 2150 VALVE 39854021 BOEING 727 727247 138408F NM LT PACK FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 290WA 22108 AT 37,000 FT CARGO VALVE LIGHT ON, UNABLE TO CONTROL CABIN ALTITUDE. REPLACED LT PACK FLOW CONTROL VALVE, OP CKS GO OD. 2 L 7 3 4F A3WE 1999121800346 19991218 00346 NM 1999 12 18 DL72K992663 1 19991206 A 5311 651592526 FRAME BOEING 727 727232 1384082 NM BS 440 - 460 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 THE FUSELAGE WAS BADLY DAMAGED BY GROUND EQUIPMENT RESULTING IN DENTING AND CRACKING OF THE FS 440 & FS 460 FRAMES BETWE EN STRINGERS 22R & 26R. THE DAMAGED SECTIONS OF FRAMES WERE CUT OUT AND NEW SECTIONS INSTALLED WITH NEW FORMED SHE ET ALUMINUM SPLICES PER ER/A 368848-14, REV B. 2 L 7 3 4F A3WE 1999121800347 19991218 00347 NM 1999 12 18 DL72K992664 1 19991206 A 5330 655456953 SKIN BOEING 727 727232 1384082 NM BS 416 - 484 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 THE FUSELAGE SKIN WAS BADLY DAMAGED BY CONTACT WITH GROUND EQUIPMENT. THE SECTION OF SKIN BETWEEN FS 416 & FS 484 AND BELOW STRINGER 22R WAS CUTOUT. NEW SECTIONS OF SKIN WERE INSTALLED WITH AN EXTERNAL ALUMINUM SPLICE STRAP PER ER/A 36 8846-14AD, REV A. 2 L 7 3 4F A3WE 1999121800348 19991218 00348 NM 1999 12 18 DL72S992665 1 19991204 A 5311 FRAME BOEING 727 727232 1384082 NM BS 560 CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 THE WEB OF THE FS 560 C1 DOOR JAMB FRAME WAS FOUND WITH 2 SMALL CRACKS AT EXISTING FASTENER HOLES BELOW THE UPPER SILL . THE CRACKS WERE ROUTED OUT OF THE WEB AND A TITANIUM DOUBLER INSTALLED TO REPAIR THE DAMAGE AND ENABLE INSTALLATION U NDER THE EXISTING UPPER FRAME SPLICES. THE REPAIR WAS ACCOMPLISHED PER ER/A 368792-14AD. 2 L 7 3 4F A3WE 1999121800349 19991218 00349 WP 1999 12 18 DLL19992666 1 19991207 A 2120 UNKNOWN LKHEED 1011 10113853 5265020 WP CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 765DA 193H1206 ODOR APPEARED IN CABIN DURING LAST 5 - 10 MINUTES OF FLIGHT PRIMARILY IN THE REAR OF B-ZONE. FORWARD TO MCO AND PLAC PE R MEL 25-99-06. FLIGHT ATTENDANTS REPORTED AN ELECTRICAL ODOR. CHECKED CABIN LIGHTING SYS, ALL OK. CHECKED MID AND AF T GALLEY EQUIPMENT. NO ODOR NOTED. CHECKED PA AND CABIN INTERPHONE SYS AND VIDEO SYS OPERATION, ALL OK. NO ODOR NOT ED IN CABIN. PERFORMED PSS/PES SYS TEST. PSS TEST OK, PES SYS FAILED ALL SEAT ROWS AFT OF ROW 28 B-ZONE. DISABLED PSS /PES SYS, PULLED AND CLAMPED C/B 2D11 AND C/B F14 AT CABIN OVERHEAD PNL (CB4). 2 L 7 3 4F A23WE 1999121800350 19991218 00350 NM 1999 12 18 DL72L992667 1 19991130 A 5531 STRINGER BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2, FOUND STRINGER 5R CRACKED AT RIB NR 9 VERT STAB INTERIOR. DYE CHECKED AND FOUND CRACK EXTENDS TO EDGE OF MATER IAL. CHEM TREATED PER PS 900-2-4-1 NR 2, FABRICATED REPAIR PER MM 55-30-0 PG 803, AND INSTALLED PER SAME. 2 L 7 3 4F A3WE 1999121800351 19991218 00351 NM 1999 12 18 DL72L992668 1 19991130 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DISBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2, FOUND RT ELEVATOR I/B TRAILING EDGE DISBONDED. REPAIRED PER MM 55-20-0 PG 801 NR 2. 2 L 7 3 4F A3WE 1999121800352 19991218 00352 NM 1999 12 18 DL72L992669 1 19991130 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2, FOUND LT ELEVATOR T/E DELAMINATED I/B AND O/B OF TAB. REPAIRED PER MM 55-20-0 PG 801 NR 2. 2 L 7 3 4F A3WE 1999121800353 19991218 00353 NM 1999 12 18 DL72L992670 1 19991130 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DISBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2, FOUND RT ELEV T/E DISBONDED BETWEEN UPPER AND LWR SKIN SEVERAL AREA'S FROM I/B TO O/B AREA. REPAIRED PER MM 55 -20-0 PG 801 NR 2. 2 L 7 3 4F A3WE 1999121800354 19991218 00354 NM 1999 12 18 DL72L992671 1 19991201 A 5754 RIB BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2, FOUND NR 8 SLAT RIB'S CRACKED, NR 4, 14 (MARKED). REMOVED I/B SLTRK AND STOP DRILLED CRACK PER MM 57-40-0 FIG 809, FABRICATED REPAIR PARTS PER MM 57-54-00 FIG 809. 2 L 7 3 4F A3WE 1999121800355 19991218 00355 NM 1999 12 18 DL72W992672 1 19991207 A 5754 BRACKET BOEING 727 727247 138408F NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 NR 5 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED TOP AND BOTTOM RADIUS. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999121800356 19991218 00356 NM 1999 12 18 DL76G992673 1 19991208 A 3350 LIGHT 20131 BOEING 767 7673P6 1385105 NM SEAT 11 - 27 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 1898 24984 EMERGENCY EXIT LIGHTS FROM SEAT 11 TO 27 OVERHEAD AISLE RT LIGHTS INOP. 2 L 7 2 4F RT A1NM 1999121800357 19991218 00357 NM 1999 12 18 DL72L992675 1 19990812 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 COVE SKIN CRACKED 36 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0, FIG 809, ON SHOP ORDER 847111. 2 L 7 3 4F A3WE 1999121800358 19991218 00358 NM 1999 12 18 DL72L992676 1 19990812 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 REPAIR ANGLE CRACKED I/B SPAR CAP 18 INCHES I/B TO 23 INCHES O/B. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 84711 1. 2 L 7 3 4F A3WE 1999121800359 19991218 00359 NM 1999 12 18 DL72S992678 1 19991208 A 5754 ANGLE BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 COVE SKIN ANGLE CRACKED 15 INCHES O/B OF NR 7 SLAT ACTUATOR ROD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999121800360 19991218 00360 NM 1999 12 18 DL72S992679 1 19991208 A 5754 STIFFENER BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 VERTICAL SPAR STIFFENER CRACKED NR 7 SLAT O/B SIDE OF I/B TRACK. REPLACED SPAR STIFFENER PER MM 57-20-21. 2 L 7 3 4F A3WE 1999121800361 19991218 00361 NM 1999 12 18 DL72S992680 1 19991208 A 5230 BEAM BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 C-2 DOOR HORIZONTAL BEAM WEB DAMAGED AT LIGHTNING HOLE AT DOOR HANDLE SNUBBER SRM 52-30-2D FIG 802D. 2 L 7 3 4F A3WE 1999121800362 19991218 00362 NM 1999 12 18 DL757992681 1 19991207 A 2120 UNKNOWN BOEING 757 757232 1384965 NM COCKPIT ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 671DN 25332 STRONG ELECTRICAL ODOR IN COCKPIT. DECLARED EMERGENCY, ACCOMP SMOKE IDENTIFICATION/REMOVEL CHECKLIST. UNABLE TO DETERM INE CAUSE OF ODOR. ISOLATED TO COCKPIT, ODOR DID NOT GO AWAY. REMOVED ALL CAPT AND F/O INSTRUMENTS, INSPECTED BEHIND P ANEL, INSPECTED LOWER E/E COMPARTMENTS, NTF RAN ENGINES AND ALL SYS OPN CHECKED NORMAL WITH NO ELECTRICAL ODORS FOUND. CLEANED COFFEE SPILL AT F/O BRIEF CASE AREA. 2 L 7 2 4F RT A2NM 1999121800363 19991218 00363 NM 1999 12 18 DL72S992682 1 19991208 A 5754 SKIN BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 A .5 INCH CRACK AT FWD LWR SIDE OF NR 2 MIDFLAP AT I/B AFT FLAP ACTUATING ROD CUTOUT. REPAIRED PER MM 57-52-0 AND ER A 368899-14. 2 L 7 3 4F A3WE 1999121800364 19991218 00364 NM 1999 12 18 DL72S992683 1 19991208 A 2782 BRACKET BOEING 727 727232 1384082 NM LE FLAP ACTUATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 NR 1 LEADING EDGE SLAT I/B AND O/B ACTUATOR MOUNT BRACKETS CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999121800366 19991218 00366 NM 1999 12 18 DL76S992685 1 19991209 A 5270 85 LAMP BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 137DL 25306 LEFT AFT DOOR ARMED LIGHT ON LT FWD ATTND PANEL FAILED TO TEST. RELAMPED, OPS CKS GOOD. 2 L 7 2 4F RT A1NM 1999121800367 19991218 00367 NE 1999 12 18 DLM11992687 2 19991208 A 7200 PW44603 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 FAILED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 807DE 20949 723915 48478 723915 NR 3 ENG SURGE ON T/O ROLL. T/O ABORTED. MTC FOUND METAL EQUIP SWAP WITH ACFT 803, ACFT 807 NR 3 ENG CHANGE. 2 L 7 3 4F 4 F RT A22WE E24NE 1999121800368 19991218 00368 NM 1999 12 18 DL72S992688 1 19991209 A 3310 LIGHT S106 BOEING 727 727232 1384082 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 407DA 21151 FLIGHT DECK EMERGENCY PORTABLE EXIT IDENTIFIER LIGHT WOULD NOT TEST. REPLACED BATTERY PACK, OP CKS GOOD. 2 L 7 3 4F A3WE 1999121800369 19991218 00369 NM 1999 12 18 DL72S992689 1 19991011 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 DURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 20 FROM I/B END. THE ANGLE WAS REPAIRED BY INSTALLIN G A DOUBLER PER MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1999121800370 19991218 00370 NM 1999 12 18 DL72S992690 1 19991117 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 55 FROM I/B END OF FLAP. THE CHORD ANGLE WAS REPAI RED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1999121800371 19991218 00371 NM 1999 12 18 DL72E992691 1 19991209 A 5754 ANGLE BOEING 727 727247 138408F NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 DOUBLER CRACKED AT NR 2 L/E SLAT COVE SKIN ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1999121800372 19991218 00372 NM 1999 12 18 DL72S992692 1 19991209 A 2910 65178444017 LINE BOEING 727 727232 1384082 NM HYDRAULIC SYS LEAKING A DALA O OTHER K FLUID LOSS CL CLIMB 1 SO 27 538DA 22076 DURING CLIMBOUT OF STL, A SYS QTY DROPPED TO 1.2 GAL AFTER GEAR RETRACTION. ONCE AT CRUISE ATL, A SYS QTY SLOWLY DROPP ED TO .2 GAL. A SYS LOSS PROCEDURES WERE FOLLOWED. LANDING GEAR WAS LOWERED NORMALLY AND FLAPS WERE LOWERED BY ALT MET HOD. LOW PRESS LIGHTS DID NOT ILLUMINATE. REPLACED A SYS HYD PRESS LINE FROM NR 2 ENG IN 48 SECTION. 2 L 7 3 4F A3WE 1999121800373 19991218 00373 NM 1999 12 18 DL72E992693 1 19991209 A 2132 0000 SENSOR BOEING 727 727247 138408F NM LT PACK FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 831WA 21483 DURING CRUISE AT FL 290, A PASSENGER NOTICED THE AREA APPROXIMATELY 10 INCHES BELOW THE WINDOWS AT SEATS 16E & 17E WAS H OT TO THE TOUCH AND A SLIGHT BURNING ODOR WAS PRESENT. AFTER RT PACK TURNED OFF AND DESCENDED TO FL240, THE AREA COOLED IMMEDIATELY AND ODOR DISSIPATED. CONTINUED ON LT PACK ONLY. CLEANED 35 DEG VALVE SENSOR AND C/P, OPS CHECK OF PACK ON GROUND OK. UNABLE TO DUPLICATE ITEM AT SEATS. 2 L 7 3 4F A3WE 1999121800374 19991218 00374 NM 1999 12 18 DL72E992694 1 19991209 A 5754 BRACKET BOEING 727 727247 138408F NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 NR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999121800375 19991218 00375 1999 12 18 DLL10992696 2 19991209 A 7200 RB21122B02 ENGINE 21SN0426J LKHEED 1011 10113851 5265010 WP NR 2 MALFUNCTIONED A DALA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 27 730DA D127B 193C1199 STEADY FILTER PRESSURE LIGHT NR 2 ENGINE, LEVEL AT 11,000 FT 250 KTS. POWER UP ON ENGINES, LIGHT WENT OUT WHEN ENGINE P ULLED TO IDLE. ENGINE SHUTDOWN. CHECKD FILTER AND CHIP DETECTORS, NO PROBLEMS NOTED. REPLACED DIFF PRESSURE SWITCH. 2 L 7 3 4F A23WE 1999121800376 19991218 00376 NM 1999 12 18 DL73K992697 1 19991210 A 5313 STRINGER BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE RIGHT STR 18A HAD A CRACK IN THE SHEAR WEB SIMILAR TO THAT OF S/B 737-53-1170. DAMAGE WAS FOUND AT AMV IN ATL. D AMAGE WAS REPAIRED PER ERA 333859-14. 2 L 7 2 4F A16WE 1999121800377 19991218 00377 NM 1999 12 18 DL73K992698 1 19991208 A 5343 654654320 FITTING BOEING 737 737232 1384475 NM BS 685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 THE STRUT ATTACH LUG OF THE RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE LU G BORE AND ON THE LUG FACES. THE BORE WAS OVERSIZED AND THE LUG FACES MACHINED TO REMOVE THE CORROSION. A REPAIR BUS HING WAS INSTALLED AND THE INSTALLATION RE-ASSEMBLED PER ER/A 368888-14, REV A. 2 L 7 2 4F RT A16WE 1999121800378 19991218 00378 NM 1999 12 18 DL76L992699 1 19991209 A 4990 000001232 O-RING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE OIL CAP FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 27 1201P 10751 28458 P1927 ATTEMPTED APU START AT 22,000. APU FAILED TO START WITH ASSOC APU FAULT EICAS MSG. ATTEMPTED 2ND START ON GROUND AT CV G. 2ND START SUCCESSFUL. FOUND APU BITE MSG EGT 293 - RPM 95 PERCENT - AUTO EVENT ECU BITE SHOWS LAST SHUTDOWN NORMAL. SHUTDOWN NR 2 LOP - 3 & 4, NO DATA. SUMMARY FAULTS - FAN VALVE/ MINI FLAGS READ 18. APU LOW ON OIL, CAP O-RING BAD. REMOVED AND REPLACED O-RING, SVCD APU OIL TO FULL. NORMAL START & OPN. ATL MCC NOTIFIED. 2 L 7 2 4F 4 F RT A1NM E24NE 1999121800379 19991218 00379 NM 1999 12 18 DL72S992700 1 19991209 A 5320 651750425 SHEAR CLIP BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 THE SHEAR CLIP FOR THE FS 1263 FRAME BETWEEN STRINGERS 13L AND 14L WAS FOUND WITH A 1 INCH CRACK IN THE SKIN FLANGE RAD IUS. THE SKIN FLANGE WAS TRIMMED OFF TO REMOVE THE CRACK. THE SHEAR CLIP WAS RESTORED BY INSTALLING AN ALUMINUM REPAIR ANGLE PER ER/A 368904-14, REV A. 2 L 7 3 4F A3WE 1999121800380 19991218 00380 NM 1999 12 18 DL73K992701 1 19991210 A 5312 65163007 BULKHEAD BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 TWO CRACKS WERE FOUND IN THE FS 178 BULKHEAD WEB. THE DAMAGE WAS FOUND AT MV IN ATL AND REPAIRED PER ERA 333854-14 . 2 L 7 2 4F A16WE 1999121800381 19991218 00381 NM 1999 12 18 DL73K992702 1 19991210 A 5330 6545767531 SKIN BOEING 737 737247 138448D NM BS 425 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 425 BETWEEN STR 14L AND 15L. THE DAMAGE WAS FOUND AT MV IN ATL AND REPAIRED PE R ERA 333892-14. 2 L 7 2 4F A16WE 1999121800382 19991218 00382 NM 1999 12 18 DL72W992703 1 19991209 A 5330 651842011 SKIN BOEING 727 727247 138408F NM BS 312 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 THE FUSELAGE SKIN BELOW THE LAVATORY SERVICE PANEL WAS FOUND WITH AN AREA OF SKIN CORROSION AT STRINGER 20R BETWEEN FS 3 00 & FS 312. THE CORROSION WAS REMOVED WITH AN 8 X 2 SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMIN UM DOUBLER PER ER/A 368892-14, REV A. 2 L 7 3 4F A3WE 1999121800383 19991218 00383 NM 1999 12 18 DLM88992704 1 19991210 A 4990 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU BAY LEAKING A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 934DL 7250 49721 WITH ENG A/I ON AND PNEUMATIC X-FFED CLOSED, GOT SMOKE AND FUMES IN CABIN. BOTH AFT LAV SMOKE DETECTORS WENT OFF. E NG A/I ON FOR APPROX 20 MINS. A/C WAS ON APPROACH WITH ENG PWR AT 1.3 EPR, ALT BELOW 10K FT. PERFORMED DUCT BURN-OUT P ER MM. REPLACED WATER SEP BAGS. FOUND APU LEAKING OIL. PLACED ON MCO. 2 L 7 2 4F 4 F RT A6WE E9NE 1999121800384 19991218 00384 NM 1999 12 18 DL72S992706 1 19991210 A 2782 BRACKET BOEING 727 727232 1384082 NM LE FLAP ACTUATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 A 1.25 INCH CRACK NR 8 SLAT ACTUATOR I/B AFT ATTACH BRACKET. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1999121800385 19991218 00385 NM 1999 12 18 DL76S992707 1 19991210 A 2560 MV10 MEGAPHONE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 119DL 23278 ON L/O, FOUND FWD CLOSET MEGAPHONE BROKEN. REPLACED MEGAPHONE. 2 L 7 2 4F RT A1NM 1999121800386 19991218 00386 1999 12 18 DL733992709 4 19991210 A 2565 61620468 SLIDE BOEING 737 737301 1384611 NM PAX DOOR DEPLOYED A DALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 27 948WP 23259 WHILE REPOSITIONING A/C TO GATE FOR FIRST FLIGHT DEPARTURE, R1 SLIDE WAS INADVERTENTLY DEPLOYED DUE TO GIRT BAR APPARENT LY SHIFTED AND WHEN OPS ATTEMPTED TO BOARD A/C GIRT BAR GOT CAUGHT ON DOOR FRAME AND DEPLOYED WHEN DOOR WAS OPENED FULLY . MTC FERRY A/C TO SLC FOR SLIDE REPLACEMENT. REPLACED SLIDE. 2 L 7 2 4F RT A16WE 1999121800387 19991218 00387 NM 1999 12 18 DL76L992710 1 19991211 A 2570 HARNESS BOEING 767 767332 1382001 NM SEAT 4 ARCING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 197DN 28454 ELECTRICAL BURNING SMELL AT SEATS 4C AND E. SEATS DEACTIVATED. REPLACED WIRE BUNDLE. 2 L 7 2 4F RT A1NM 1999121800388 19991218 00388 NM 1999 12 18 DL733992711 1 19991211 A 3320 SOCKET BV03112033 BOEING 737 737347 1384647 NM ROW 13 FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 306WA 23347 ELECTRICAL SMELL IN CABIN. FOUND FLUORESCENT OVERHEAD LIGHT TUBE FWD SOCKET AT 13 A, B, C MELTING. REMOVED LIGHT TUBE AND REPLACED SOCKET. 2 L 7 2 4F RT A16WE 1999121800389 19991218 00389 NM 1999 12 18 DL733992712 1 19991211 A 2611 WIRE BOEING 737 737347 1384647 NM SMOKE DETECTOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304WA 23345 FIRST CLASS LAV SMOKE DETECTOR INOP. REPLACED BROKEN WIRES AT SWITCH DETECTOR. 2 L 7 2 4F RT A16WE 1999121800390 19991218 00390 NM 1999 12 18 DLM88992713 1 19991211 A 2432 947F9463 BPU 947F9463 DOUG MD88 MD88 3023688 NM E & E BAY FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 927DA TL1090 49714 CLIMBING THROUGH 20K FT OVHD PANEL LIGHTS AND NUMEROUS OTHER COCKPIT LIGHTS BEGAN TO FLICKER. APPROX 5 SECS LATER ELECT ICAL FAILURE OCCURED FOR APPROX 15 SEC, THEN PWR CAME BACK ON. THEN FOR APPROX 3-5 SECS PWR WOULD GO OFF THEN ON. WHEN PWR WENT OFF THE 1ST TIME THE EMER PWR SWITCH WAS TURNED ON AND THE APU WAS PLACED TO START. AFTER 5 SECS PWR CAME ON AND REMAINED ON AND THE FLICKERING STOPPED. A WINDSHIELD OVT LIGHT REMAINED ON THE OAP AND THE AUTO THROTTLES WOULD NOT ENGAGE. BOTH THE CAPTS AND F/OS PFDS AND NDS WENT BLANK. REPLACED BPU AND R2-50, RAN AND LOADED GENS SWAPPED PWR OK. 2 L 7 2 4F RT A6WE 1999121800391 19991218 00391 NM 1999 12 18 DL73K992714 1 19991211 A 2612 89638305 FIRE DETECTOR BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE E & E BAY MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 27 309DL 30948 23081 APU FIRE INDICATION AFTER START AT 12,000 FT. PULLED FIRE HANDLE AND THE LIGHT REMAINED ON. AFTER FIRING THE BOTTLE TH E FIRE HANDLE LIGHT WENT OUT IN ABOUT 2 SEC. APU HAD BEEN RUNNING FOR ABOUT 1 MIN WHEN THE FIRE INDICATION CAME ON. TR OUBLESHOOT SYSTEM, NO TROUBLE FOUND. 2 L 7 2 4F 4 F RT A16WE E2EA 1999121800392 19991218 00392 NM 1999 12 18 DL757992716 1 19991211 A 3230 273N20873 SWITCH BOEING 757 757232 1384965 NM MLG FAILED A DALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 27 637DL 23760 INBOUND PILOT REPORT, GEAR FAILED TO RETRACT NORMALLY AFTER T/O. GEAR HANDLE LOCKED IN THE OFF POSITION. LOCK OVERRIDE USED TO RAISE GEAR. REPLACED RT AND LT MLG TILT PRESSURE SWITCH. REPLACED THE SHUTTLE VLV. ALSO, REPLACED THE LT TIL T ACT. ALL CHECKED NORMAL DURING LANDING GEAR SWING. 2 L 7 2 4F RT A2NM 1999121800393 19991218 00393 NM 1999 12 18 DL757992717 1 19991212 A 2120 ODOR BOEING 757 757232 1384965 NM COCKPIT DETECTED A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 699DL 29970 STRONG HYD FLUID ODOR IN COCKPIT AT TAKEOFF. INSP PACK INLETS AND EXHAUST, INSP AIR COND BAYS, INSP BELLY SKIN AND ENGS , ALL OK AND NO LKS. RAN PACKS FULL HOT AND COLD BOTH OK. NO ODOR NOTED, HYS QTY OK. 2 L 7 2 4F RT A2NM 1999121800394 19991218 00394 NM 1999 12 18 DL767992718 1 19991212 A 3350 BPS73 BATTERY PACK BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 108DL 22220 DURING LAYOVER, FOUND NR 1 SQUIB TEST INOP. LEFT OVERWING ESCAPE SLIDE. REPLACED BATTERY AND BATTERY PACK, OPERA TION NOW NORMAL. 2 L 7 2 4F RT A1NM 1999121800395 19991218 00395 NM 1999 12 18 DL73K992719 1 19991210 A 5330 6545768295 SKIN BOEING 737 737247 138448D NM BS 440 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 FUSELAGE SKIN JUST FWD OF C-1 DOOR CUTOUT AT BS 440 WAS FOUND CRACKED IN TWO PLACES BETWEEN S-22R AND 24R. REPAIR ENLAR GED TO ENCOMPASS STATIC PORT, ER/A 333852-14 REV A. 2 L 7 2 4F A16WE 1999121800396 19991218 00396 NM 1999 12 18 DL73K992722 1 19991213 A 5330 6545768158 SKIN BOEING 737 737247 138448D NM BS 492 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE FUSELAGE SKIN WAS GOUGED AT THE C-1 DOOR, FS 492 AND STR 23R. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 3339 02-14. 2 L 7 2 4F A16WE 1999121800397 19991218 00397 NM 1999 12 18 DL72L992723 1 19990812 A 5753 652163261 FASTENERS BOEING 727 727232 1384082 NM LE FLAP MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 ANGLE REPAIR AFT SPAR, LWR.ANGLE 32 TO 37 INCHES FROM I/B HAD MISSING FASTENERS. REMOVED I/B SECTION OF SPAR RAIL, FABR ICATED REPLACEMENT SECTIONS AND INSTALLED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 847111. 2 L 7 3 4F A3WE 1999121800398 19991218 00398 NM 1999 12 18 DL72L992724 1 19991213 A 7120 65312813 ANGLE BOEING 727 727232 1384082 NM ENGINE MOUNT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 ON HUSH-KIT MOD, FOUND LT NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT AFT MOUNT SUPPORT C HORD ANGLE WITH ONE OF NEW MFG. 2 L 7 3 4F A3WE 1999121800399 19991218 00399 NM 1999 12 18 DL72L992725 1 19991210 A 7120 65312814 ANGLE BOEING 727 727232 1384082 NM ENGINE MOUNT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 ON HUSH-KIT MOD, FOUND RT NR 2 ENG AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH O NE OF NEW MFG. 2 L 7 3 4F A3WE 1999121800400 19991218 00400 NM 1999 12 18 DL72L992727 1 19991201 A 5754 RIB BOEING 727 727232 1384082 NM LE FLAP CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2, FOUND NR 4 SLAT RIB (MARKED) CRACKED. FABRICATED DOUBLER PER MM 57-54-0 FIG 804. DYE CHECKED END OF CRACK PER FIG 504. CHEM TESTED PER PS 900-2-4-1 NR 2. REPAIRED RIB PER MM 57-54-0. 2 L 7 3 4F A3WE 1999121800401 19991218 00401 1999 12 18 DL72W992728 4 19991213 A 3440 RADAR 20671570153 BOEING 727 727247 138408F NM COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 296WA 7162 22533 AIRBORNE THE RADAR WOULD NOT PAINT ANY GROUND OR WX, BUT WOULD OCCASIONALLY SPIKE. REPLACED RT UNIT. 2 L 7 3 4F A3WE 1999121800402 19991218 00402 NM 1999 12 18 DL72E992730 1 19991213 A 5320 WEB BOEING 727 727247 138408F NM TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 TWO CRACKS AT LIGHTENING HOLES RT TORQUE BOX VERT WEB STA 1223 AT UPPER LIGHTENING HOLE AND STA 1233 AT LOWER LIGHTENING HOLE. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999121800403 19991218 00403 NM 1999 12 18 DL72E992731 1 19991213 A 5320 WEB BOEING 727 727247 138408F NM TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 A .25 INCH CRACK AT LT TORQUE BOX VERT WEB LWR LIGHTENING HOLE STA 1233. TWO .1875 INCH CRACKS AT LT TORQUE BOX VERT WEB UPPER LIGHTENING HOLE STA 1223. BOTH REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1999121800404 19991218 00404 NM 1999 12 18 DLM11992732 1 19991213 A 5610 WINDSHIELD NBA6045501 DOUG MD11 MD11 3023602 NM COCKPIT SHATTERED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 803DE 0436 48474 AT 25,000 FT, CAPT OUTER WINDSHIELD CRACKED. ON INSP, TOTAL AREA FOUND TO BE SHATTERED AT OUTER PANE. REPLACED WIN DSHIELD AND CONTROLLER. 2 L 7 3 4F RT A22WE 1999121800405 19991218 00405 NM 1999 12 18 DL73K992733 1 19991214 A 5313 STRINGER BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE LT STR 18A HAD A CRACK RUNNING FWD AND AFT SIMILIAR TO THOSE NOTED IN S/B 737-53-1170 AND 737-53-1066. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 333890-14. 2 L 7 2 4F A16WE 1999121800406 19991218 00406 EU 1999 12 18 RAIA9912014 1 19991211 A 3230 QA03043 FILTER JETAIR JETSTM JETSTM4101 1500501 EU MLG FAILED A RAIA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 557HK 41074 6183-JFK- LANDING GEAR WOULD NOT RETRACT AFTER T/O. MAINTENANCE REPLACED LANDING GEAR RELEASE VALVE FILTER ELEMENT. 2 L 7 2 4T RT A41NM 1999121800407 19991218 00407 WP 1999 12 18 AT9900844 1 19991126 A 5711 5911301501 SPAR DOUG DC9 DC932 3022066 WP WS 477.35 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT WING LOWER AFT SPAR FLANGE TO BE CORRODED AT BS 477.3 5. FABRICATED AND INSTALLED SPAR IAW EO 99-1384. 2 L 7 2 4F A6WE 1999121800408 19991218 00408 WP 1999 12 18 AT9900856 1 19991124 A 5711 1A545891 SPAR DOUG DC9 DC932 3022066 WP WS 550 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT WING AFT SPAR FLANGE CORRODED BEYOND LIMITS AT BS 550 . FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 51-30-02, 51-30-03, AND 51-30-05. 2 L 7 2 4F A6WE 1999121800409 19991218 00409 WP 1999 12 18 AT9900857 1 19991114 A 5532 PANEL DOUG DC9 DC932 3022066 WP VERTICAL STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON VERTICAL STABILIZER AFT SPAR PANEL NR 6408 TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW DC9 SRM 55-31 FIG 9 AND 51-30-02. 2 L 7 2 4F A6WE 1999121800410 19991218 00410 WP 1999 12 18 AT9900858 1 19991115 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FIVE CRACKS IN RIGHT WING OUTBOARD RIBS. STOP DRILLED CRA CKS AND FABRICATED ANGLES IAW DC9 SRM 57-01 FIG 3, 51-10-03, AND 51-30-02. 2 L 7 2 4F A6WE 1999121800411 19991218 00411 WP 1999 12 18 AT9900859 1 19991119 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR PANEL BS 237 RBL 47 CORRODED BEYOND LIMITS. R EMOVED AND REPLACED FLOOR PANEL AT BS 237 RBL 47 IAW DC9 SRM 51-20-02, 51-10-04, 51-10-02, 51-30-02, AND 51-21. 2 L 7 2 4F A6WE 1999121800412 19991218 00412 WP 1999 12 18 AT9900860 1 19991120 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 579 - 680 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CABIN FLOOR PANEL BS 579-680 TO BE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-03, 51-10-04, 51-30-02, AND 53-21. 2 L 7 2 4F A6WE 1999121800413 19991218 00413 WP 1999 12 18 AT9900861 1 19991118 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 313 - 332 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON CUSP WEB BETWEEN STATION BS 332 AND BS 313 AT LONGERON 18R TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-03, 53-01 FIG 1, 51-30. 2 L 7 2 4F A6WE 1999121800414 19991218 00414 WP 1999 12 18 AT9900862 1 19991121 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN SKIN AT BS 1038 ABOVE LONGERON 14R. CUT OUT CRAC K AND INSTALLED DOUBLER IAW DC9 SRM 51-30-02, 51-10-03, AND 53-04 FIG 18. 2 L 7 2 4F A6WE 1999121800415 19991218 00415 WP 1999 12 18 AT9900863 1 19991116 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 794 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON CUSP WEB TO BE OUT OF LIMITS AT BS 794 LONGER ON 18R. FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 53-02 FIG 1, 53-01 FIG 2, 51-10-02, 51-10-03, 51-10-04, AND 51-30- 02. 2 L 7 2 4F A6WE 1999121800416 19991218 00416 WP 1999 12 18 AT9900864 1 19991202 A 3350 43 LAMP DOUG DC9 DC932 3022066 WP CABIN FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 813AT 47318 FOUND L1 DOOR OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. RELAMPED, OPS CHECK NORMAL IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 1999121800417 19991218 00417 WP 1999 12 18 AT9900865 1 19991120 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 237 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENT DIMENSIONS IN SKIN TO BE OUT OF LIMITS AT BS 237. FA BRICATED AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1999121800418 19991218 00418 WP 1999 12 18 AT9900866 1 19991204 A 3397 WIRE DOUG DC9 DC932 3022066 WP ROWS 10 - 12 BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 832AT 47451 FOUND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE, BETWEEN ROWS 10-12. REPAIRED BROKEN WIRE IAW DC9 MM 20-50-1. 2 L 7 2 4F A6WE 1999121800419 19991218 00419 WP 1999 12 18 AT9900867 1 19991122 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 160 - 200 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR PANEL CRACKED AND CORRODED AT BS 160-200. FABRICATE D AND INSTALLED FLOOR PANEL AND HAT CHANNELS IAW DC9 SRM 53-21 FIG 20, 51-10-02, 51-10-04, 51-10-03, AND 51-30-03. 2 L 7 2 4F A6WE 1999121800420 19991218 00420 WP 1999 12 18 AT9900868 1 19991124 A 5414 SKIN DOUG DC9 DC932 3022066 WP NR 1 PYLON CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION AROUND SCREW HOLES ON NR 1 ENGINE PYLON L/E PANE L, MATERIAL LOSS WAS MORE THAN 20 PERCENT, THIS IS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 5 4-30 FIG 1, 51-10-04, 51-30-09, 51-10-03, AND 51-30-02. 2 L 7 2 4F A6WE 1999121800421 19991218 00421 WP 1999 12 18 AT9900869 1 19991115 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 614 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN SKIN AT BS 614 LONGERON 2R. REMOVED CRACK AND IN STALLED DOUBLER IAW DC9 SRM 53-04 FIG 38, 51-10-04, AND 51-10-03. 2 L 7 2 4F A6WE 1999121800422 19991218 00422 WP 1999 12 18 AT9900870 1 19991123 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160 - 180 HOLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND HOLE DRILLED IN THE E & E COMPARTMENT BETWEEN BS 160 AND 1 80 LONGERON 27R. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-02, 53-02 FIG 18, 51-10-04, 51-10-03, AND 51-30-05. 2 L 7 2 4F A6WE 1999121800423 19991218 00423 WP 1999 12 18 AT9900871 1 19991126 A 5320 4911383INI FITTING DOUG DC9 DC932 3022066 WP BS 794 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FRAME FITTING AT BS 794 LONGERON 18L TO BE CORRODED. INS TALLED NEW FITTING IAW DC9 SRM 51-30-05, 51-10-03, AND 51-10-02. 2 L 7 2 4F A6WE 1999121800424 19991218 00424 WP 1999 12 18 AT9900873 1 19991122 A 5320 4911383INI FITTING DOUG DC9 DC932 3022066 WP BS 237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FRAME FITTING AT BS 237 LONGERON 18L CORRODED BEYOND LIMIT S. INSTALLED FRAME FITTING IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 1999121800425 19991218 00425 WP 1999 12 18 AT9900874 1 19991121 A 5320 STIFFENER DOUG DC9 DC932 3022066 WP BS 699 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND ANGLE STIFFENER CORRODED AT BS 699. REMOVED AND REPLACED STIFFENER IAW DC9 SRM 51-10-04 AND 51-30-02. 2 L 7 2 4F A6WE 1999121800426 19991218 00426 WP 1999 12 18 AT9900875 1 19991128 A 5320 4911381INI CLIP DOUG DC9 DC932 3022066 WP BS 541 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FRAME CLIP CORRODED OUT OF LIMITS AT BS 541 LONGERON 18L. FABRICATED AND INSTALLED FRAME CLIP IAW DC9 SRM 53-01 FIG 1, 51-10-04, 51-30-01, AND 51-30-05. 2 L 7 2 4F A6WE 1999121800427 19991218 00427 WP 1999 12 18 AT9900876 1 19991128 A 5320 4911383INI CLIP DOUG DC9 DC932 3022066 WP BS 446 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FRAME CLIP TO BE CORRODED OUT OF LIMITS AT BS 446 LONGERON 18L. FABRICATED AND INSTALLED FRAME CLIP IAW DC9 SRM 51-30-01, 51-30-05, 53-01 FIG 1, AND 51-10-04. 2 L 7 2 4F A6WE 1999121800428 19991218 00428 WP 1999 12 18 AT9900877 1 19991119 A 5512 SKIN DOUG DC9 DC932 3022066 WP HORIZONTAL STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT HORIZONTAL STABILIZER WING TIP UPPER SKIN CORRODED B EYOND LIMITS. FABRICATED AND INSTALLED UPPER SKIN IAW DC9 SRM 51-10-04, 55-11 FIG 1, 55-03 FIG 4, AND 51-10-03. 2 L 7 2 4F A6WE 1999121800429 19991218 00429 WP 1999 12 18 AT9900878 1 19991122 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON CUSP WEB TO BE OUT OF LIMITS AT BS 579 LONGER ON 18R. FABRICATED AND INSTALLED WEB REPAIR IAW DC9 SRM 53-01 FIG 2, 51-10-04, 51-10-03, AND 51-30-02. 2 L 7 2 4F A6WE 1999121800430 19991218 00430 WP 1999 12 18 AT9900879 1 19991129 A 5230 FRAME DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND THREE CRACKS IN THE FORWARD CARGO DOOR BS 420. STOP DRILL ED CRACKS AND INSTALLED REPAIR IAW DC9 SRM 51-30-02, 51-10-04, 51-10-03, AND 52-03. 2 L 7 2 4F A6WE 1999121800431 19991218 00431 WP 1999 12 18 AT9900880 1 19991202 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 541 - 484 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON CUSP WEB BS 541-484 LONGERON 18L OUT OF LIMIT S. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 53-01 FIG 1, 53-01 FIG 2, 51-10-03, 51-10-04, 51-10-02, AND 51- 30-01. 2 L 7 2 4F A6WE 1999121800432 19991218 00432 WP 1999 12 18 AT9900881 1 19991203 A 3350 41B004AD073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 836AT 47397 FOUND BOTH SIDES FORWARD UPPER CABIN EMERGENCY EXIT DOOR, EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW DC9 MM 33-53-0. 2 L 7 2 4F A6WE 1999121800433 19991218 00433 WP 1999 12 18 AT9900882 1 19991202 A 5246 ANGLE DOUG DC9 DC932 3022066 WP FUEL DOOR CHAFFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND HINGE PIN AT THE MAIN RE-FUELING DOOR CHAFED INTO ADJACENT SUPPORT ANGLE (OUT OF LIMITS). INSTALLED A STACKED ANGLE REPAIR IAW DC9 SRM 57-21 FIG 2, 51-10-02, 51-10-2A, 57-01 FIG 3, 51-10-04, 51-10-03, 51-30, AND 57-01 FIG 1. 2 L 7 2 4F A6WE 1999121800434 19991218 00434 WP 1999 12 18 AT9900883 1 19991129 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CHAFFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FORWARD CARGO DOOR OUTER SKIN CHAFED BEYOND LIMITS AT BS 4 00. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 52-05 FIG 30, 51-10-04, AND 51-30-02. 2 L 7 2 4F A6WE 1999121800435 19991218 00435 WP 1999 12 18 AT9900884 1 19991203 A 2150 RT PACK DOUG DC9 DC932 3022066 WP AC BAY OVERHEAT A ZZDA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 15 814AT 47486 FOUND RIGHT AIR CONDITIONING PACK WENT TO FULL HOT IN FLIGHT, APPROXIMATELY 5 MINUTES AFTER TAKEOFF. DEFERRED PER MEL 2 1-1, PROBLEM COULD NOT BE DUPLICATED. 2 L 7 2 4F A6WE 1999121800436 19991218 00436 WP 1999 12 18 AT9900885 1 19991208 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 - 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR SUPPORT AT BS 160-218 TO BE CORRODED. FABRICATED AN D INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-03, 51-10-04, 51-30-05, AND 53-11-01 FIG 13. 2 L 7 2 4F A6WE 1999121800437 19991218 00437 NM 1999 12 18 AT9900887 1 19991211 A 3350 CONNECTOR BOEING 717 717200 1383700 NM SEAT 17 LOOSE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 945AT 55008 SEAT 17 EMERGENCY PATH LIGHTING WOULD NOT ILLUMINATE. RE-SEATED CONNECTOR AT INBOARD SEAT LEG IAW MM 20-31-0, OPERATION AL CHECK NORMAL. 2 L 7 2 4F TR A6WE 1999121800438 19991218 00438 WP 1999 12 18 AT9900888 1 19991210 A 3350 43 LAMP DOUG DC9 DC932 3022066 WP CABIN FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 835AT 47534 OVERHEAD EMERGENCY LIGHT AT L1 DOOR WOULD NOT ILLUMINATE. RELAMPED OVERHEAD EMERGENCY LIGHT IAW MM 33-50, OPS CHECK NOR MAL. 2 L 7 2 4F A6WE 1999121800439 19991218 00439 WP 1999 12 18 AT9900889 1 19991210 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 802AT 47177 FWD ENTRY DOOR EMERGENCY LIGHT DID NOT ILLUMINATE DURING SERVICE CHECK. REMOVED AND REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 1999121800440 19991218 00440 1999 12 18 AT9900890 4 19991209 A 2565 156110162 SLIDE BOEING 737 7372L9 1384497 NM PAX DOOR LOOSE A ZZDA O OTHER O OTHER NR NOT REPORTED 1 SO 15 464AT 21278 AFT CABIN DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REPLACED L-2 DOOR EVACUATION SLIDE IAW MM 25-61 AND RES 99-9330. 2 L 7 2 4F RT A16WE 1999121800441 19991218 00441 NM 1999 12 18 AT9900886 1 19991210 A 3397 WIRE BOEING 737 737284 138448R NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 470AT 21501 EMERGENCY PATH LIGHTING IN FORWARD CABIN INOPERATIVE. RE-SPLICED BROKEN WIRE UNDER E-PATH WIRE COVERS. 2 L 7 2 4F A16WE 1999121800442 19991218 00442 NM 1999 12 18 AWXA9900475 1 19991214 A 2430 GCU BOEING 737 7373Y0 1384671 NM NR 2 MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 329AW 41188 7698 23500 ON CLIMBOUT NR 2 & 3 TR C/B POPPED FOLLOWED BY NR 2 GENERATOR TRIPPED OFF THE BUS. INSPECTED CONNECTIONS AT NR 2 ENG AN D ENG DISCONNECT, CHECKED OK. REPLACED NR 2 ENG GEN BREAKER PER M/M 24-21-41 TT 0049807. REPLACED NR 2 GEN CONT UNIT, TT 0043009 (P/N 948F458-3) (S/N OK2413). GCU WAS REPLACED TWICE, NO FIX. CURRENT HISTORY: SHORT HISTORY OF NR 2 GEN PROBLEMS 9 DEC 99. A/C IS ON CRITICAL ALERT. RECOMMENDATION: SDR WILL REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT. NOTE: A/C IS CURRENTLY OUT OF SERVICE, MORE INFO TO FOLLOW. 2 L 7 2 4F RT A16WE 1999121800443 19991218 00443 SO 1999 12 18 RAAA99E4081 1 19991213 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 EMERGENCY AISLE LIGHT AT ROW 14 C, D, E INOP. REPLACED BATTERY PACK AND OPS CHECKED IAW RAA GMM. 2 L 7 4 4T 4A22 1999121800444 19991218 00444 SO 1999 12 18 RAAA99E4082 1 19991213 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 EMERGENCY AISLE LIGHT AT ROW 19 D, E INOP. REPLACED BATTERY PACK AND OPS CHECKED IAW RAA GMM. 2 L 7 4 4T 4A22 1999121800445 19991218 00445 EA 1999 12 18 COMA9960752 1 19991213 A 5311 6003603031 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 LEFT HAND SIDE OF FRAME FS 718.0 STR 10-12 HAD A CRACKED DOUBLER ON AFT SIDE OF FRAME. REMOVED LEFT HAND DOUBLER AT STA 718 AND REPLACED IT WITH (P/N 600-36030-31) IAW REO 601R-53-61-153 REV A. 2 L 7 2 4F RT A21EA 1999121800446 19991218 00446 EA 1999 12 18 COMA9960754 1 19991213 A 5311 6003603032 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 RIGHT HAND SIDE OF FRAME FS 718.00 ON STR 10-12 HAD CRACKED DOUBLER ON AFT SIDE OF FRAME. REMOVED RIGHT HAND DOUBLER AT STA 718 AND REPLACED IT WITH (P/N 600-36030-32) IAW REO 601R-53-61-193A. 2 L 7 2 4F RT A21EA 1999121800447 19991218 00447 EA 1999 12 18 COMA9960753 1 19991213 A 5330 SKIN CNDAIR CL600 CL6002B19 EA BS 310 DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 FUSELAGE SKIN IS DAMAGED BY PAX DOOR PIN AT FS 310.00 STR 16-17 LEFT HAND SIDE. REPAIRED IAW CRJ EO 601R-53-21-180 REV NC. 2 L 7 2 4F RT A21EA 1999121800448 19991218 00448 EA 1999 12 18 COMA9960755 1 19991213 A 5210 SWITCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 931CA 7037 CABIN DOOR OUTER HANDLE MESSAGE. ADJUSTED HANDLE SWITCH NR S2MB. 2 L 7 2 4F RT A21EA 1999121800449 19991218 00449 EA 1999 12 18 COMA9960756 1 19991211 A 4900 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY SMOKE A COMA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 783CA 7315 FIRE DEPARTMENT NOTIFIED CREW OF WHITE SMOKE COMING FROM THE RIGHT HAND ENGINE AREA. CREW REPORTED ALL INDICATIONS IN C OCKPIT WERE NORMAL. CREW HAD JUST STARTED THE APU. INSPECTION OF APU AND ENGINE FOUND NO PROBLEM. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A21EA 1999121800450 19991218 00450 EA 1999 12 18 COMA9960757 1 19991211 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 716CA 7250 AIRCRAFT VEERED TO THE RIGHT DURING TAKEOFF ROLL. COULD NOT DUPLICATE. INSPECTED STEERING SYSTEM, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999121800451 19991218 00451 EA 1999 12 18 COMA9960758 1 19991211 A 3010 6243843 SENSOR CNDAIR CL600 CL6002B19 EA ANTI-ICE SYSTEM MALFUNCTIONED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 920CA 935 7022 LEFT WING ANTI-ICE MESSAGE. REPLACED THE LEFT WING TEMP SENSOR. 2 L 7 2 4F RT A21EA 1999121800452 19991218 00452 EA 1999 12 18 COMA9960759 1 19991210 A 3040 WINDOW HEAT CNDAIR CL600 CL6002B19 EA COCKPIT INOPERATIVE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 948CA 7079 LEFT WINDOW HEAT INOPERABLE. SWITCHED WIRE TERMINALS TO THE BACK UP TERMINAL BLOCK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 1999121800453 19991218 00453 EA 1999 12 18 COMA9960760 1 19991210 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 EA FUSELAGE OPEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 979CA 7159 LOUD HIGH PITCH NOISE ON RIGHT HAND SIDE OF COCKPIT. SECURED O2 SERVICE DOOR CLOSED. 2 L 7 2 4F RT A21EA 1999121800454 19991218 00454 EA 1999 12 18 COMA9960761 1 19991211 A 5210 H2912A SPRING CNDAIR CL600 CL6002B19 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 931CA 7037 CABIN DOOR OUTER HANDLE MESSAGE. REPLACED OUTER HANDLE LATCH SPRING. 2 L 7 2 4F RT A21EA 1999121800455 19991218 00455 EA 1999 12 18 COMA9960762 1 19991213 A 2750 FLAPS CNDAIR CL600 CL6002B19 EA LT & RT WING FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 984CA 7171 FLAPS FAILED. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999121800456 19991218 00456 EA 1999 12 18 COMA9960763 1 19991212 A 3040 CAUTION LIGHT CNDAIR CL600 CL6002B19 EA AOA SYSTEM ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 779CA 7306 RIGHT HAND AOA CAUTION MESSAGE. COULD NOT DUPLICATE. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1999121800457 19991218 00457 NM 1999 12 18 UPS99231195 1 19991213 A 3350 BATTERY BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:N/A, EMERENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS OK. 2 L 7 3 4F A3WE 1999121800458 19991218 00458 NM 1999 12 18 UPS99231197 1 19991215 A 2611 SMOKE DETECTOR BOEING 727 72727C 138400J NM CARGO BAY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:N/A, LT LWR SMOKE DETECTOR INOP. RELAMPED SMOKE DETECTOR. 2 L 7 3 4F A3WE 1999121800459 19991218 00459 NM 1999 12 18 UPS99231198 1 19991203 A 5753 65192029 FLAPTRACK BOEING 727 72725C 138400H NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, LT WING O/B FLAP NR 2 MIDFLAP CARRIAGE HAD RUST INSIDE. REPLACED THE NR 2 FLAP CARRIAGE WITH A NEW ASSY. 2 L 7 3 4F A3WE 1999121800460 19991218 00460 NM 1999 12 18 UPS99231199 1 19991213 A 5330 2024T3 SKIN BOEING 727 72725C 138400H NM BS 259.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, LFEC INSP EXHIBITS GREATER THAN 10 PERCENT MATERIAL LOSS AT BS 259.5 STR 23L TO STR 24L FWD SIDE OF SPLICE. REPAIRED SKIN AT 259.5 STR 23L TO STR 24L IAW UPS EO B727-5310-1371E APP 8.5 AND DWG 69-62161. 2 L 7 3 4F A3WE 1999121800461 19991218 00461 NM 1999 12 18 UPS99231200 1 19991212 A 5320 ANGLE BOEING 727 72725C 138400H NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORRODED FLOOR SUPPORT STRUCTURE BS 351, RBL W 168.5. REMOVED, FABRICATED AND INSTALLED MISC ANGLES AND WEBS PER SRM 51-40-2. 2 L 7 3 4F A3WE 1999121800462 19991218 00462 NM 1999 12 18 UPS99231201 1 19991210 A 5540 65167911 HINGE BOEING 727 72725C 138400H NM RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, UPPER RUDDER, UPPER RUDDER TAB HINGE IS LOOSE AND CORRODED ON INNER HINGE CLEVIS. REMOVED AND REPLA CED UPPER RUDDER, UPPER HINGE PER MM 27-20-11. 2 L 7 3 4F A3WE 1999121800463 19991218 00463 NM 1999 12 18 UPS99231202 1 19991212 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1044 - 1050 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORRODED FLOORBEAM AT BS 1044-1050, LBL 2, WL 148.5. CORROSION CLEAN UP BEYOND ACCEPTABLE LIMITS. R EMOVED, FABRICATED, AND REPLACED FLOORBEAM SEGMENT FROM BS 950-1050 SRM 53-10-5 FIG 4. 2 L 7 3 4F A3WE 1999121800464 19991218 00464 NM 1999 12 18 UPS99231203 1 19991212 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1050 - 1044 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORRODED FLOORBEAM AT BS 1050-1044 RBL 9 WL 148.5. CORROSION CLEAN UP BEYOND ACCEPTABLE LIMITS. RE MOVED, FABRICATED AND REPLACED FLOORBEAM SEGMENT FROM BS 950-1050 PER SRM 53-10-5 FIG 4. 2 L 7 3 4F A3WE 1999121800465 19991218 00465 NM 1999 12 18 UPS99231204 1 19991209 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 538 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION AT FWD CARGO BAY SEAT TRACK BS 538 RBL 14 WL 148.5. REMOVED AND REPLACED SEAT TRACK BS ST A 480-588, RLB 14 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999121800466 19991218 00466 NM 1999 12 18 UPS99231205 1 19991210 A 5311 FRAME BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, FWD LWR CARGO DOOR CUTOUT AFT DOOR FRAME WEB AT LWR STOP PAD FITTING CRACKED. REPAIRED PER SRM 51-4 0-2 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999121800467 19991218 00467 NM 1999 12 18 UPS99231206 1 19991209 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 294.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION AT BS 294.5, LBL 10.5 NOSE WHEEL UPPER LEFT CORNER ON STIFFENER. FABRICATED STIFFENER AND REPLACED PER SRM 51-20-1, SRM 51-30-2. 2 L 7 3 4F A3WE 1999121800468 19991218 00468 NM 1999 12 18 UPS99231207 1 19991206 A 5320 FLOORBEAM BOEING 727 72725C 138400H NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION ON FLOORBEAM BS 312, WL 200, RBL 60. REPAIRED CORRODED FLOORBEAM BS 312, WL 220, RBL 60, IAW SRM 53-10-08. 2 L 7 3 4F A3WE 1999121800469 19991218 00469 NM 1999 12 18 UPS99231208 1 19991206 A 5320 WEB BOEING 727 72725C 138400H NM BS 277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, WEB CRACKED AT BS 277 STRINGER 16 RT SIDE. REPAIRED PER SRM 51-40-2 FIG 1 PG 2. 2 L 7 3 4F A3WE 1999121800470 19991218 00470 NM 1999 12 18 UPS99231210 1 19991206 A 5347 M269367 SEAT TRACK BOEING 727 72725C 138400H NM BS 343 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON SEAT TRACK, BS 343, LBL 24 WL 208. REPLACED SEAT TRACK AT BS 344-48 0, LBL 24, WL 208 PER SRM 51-10-6, 53-10-1, 51-30-2. 2 L 7 3 4F A3WE 1999121800471 19991218 00471 NM 1999 12 18 UPS99231211 1 19991214 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM BS 328 LBL 20 WL 208. REPLACED FLOORBEAM FROM LBL 21 TO R BL 16, BS 328 WL 208 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999121800472 19991218 00472 NM 1999 12 18 UPS99231212 1 19991206 A 5315 7075T6 FLOORBEAM BOEING 727 72725C 138400H NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM AT UNDERSIDE OF THE AFT UPPER FLANGE, BS 312, RBL 11, WL 2 08. REPLACED FLOORBEAM FROM RBL 1 TO RBL 65, BS 312, WL 208 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1999121800473 19991218 00473 NM 1999 12 18 UPS99231213 1 19991205 A 5315 7075T6 FLOORBEAM BOEING 727 72725C 138400H NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION ON FLOORBEAM AT BS 720, RBL 46 TO RBL 50 WL 208. REMOVED AREA OF CORROSION IN A AREA OF 1 .0 X 1.0 AND 1.0 X .75, REMOVED MAX .141 FROM ORIG OF .151 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED UPPER SEC TION OF FLOORBEAM FROM BS 720 RBL 0 TO RBL 70. FABRICATED NEW SECTION AND REPAIR SPLICES FILLERS. INSTALLED ALL PER SR M 53-10-8, 51-30-5, 51-30-6, 51-30-2. 2 L 7 3 4F A3WE 1999121800474 19991218 00474 NM 1999 12 18 UPS99231214 1 19991122 A 5320 274353 SILL BOEING 727 72725C 138400H NM BS 312 - 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON MOP SILL ANGLE BS 312 BS 344 LBL 58 WL 208. REMOVED, REPLACED MOP S ILL PER SRM 51-30-2, 53-10-1. 2 L 7 3 4F A3WE 1999121800475 19991218 00475 WP 1999 12 18 UPS99831196 1 19991215 A 2120 UNKNOWN DOUG DC8 DC871F 302199D WP COCKPIT SMOKE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A, DURING PREFLIGHT INSPECTION CREW REPORTED SMOKE IN COCKPIT. 2 L 7 4 4F RT 4A25 1999121800476 19991218 00476 WP 1999 12 18 UPS99831209 1 19991215 A 2720 RUDDER DOUG DC8 DC871F 302199D WP TAIL OUT OF RIG A IPXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 718UP 46018 INSPECTION TYPE:N/A, PILOT REPORT, RUDDER WENT FULL RT DEFLECTION ON APPROACH. COMPLETED ECA 04957 FOUND RUDDER CONTROL SYSTEM OUT OF RIG. RIGGED PER ECA. OPS CHECKS GOOD PER MM 22-10-00. 2 L 7 4 4F RT 4A25 1999121800477 19991218 00477 EU 1999 12 18 RAIA9912015 1 19991212 A 3250 190600 CONTROL CABLE JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 551HK 41040 7514-STL- NOSE WHEEL STEERING DID NOT STEER TO THE LEFT. MAINTENANCE REPLACED NOSE WHEEL STEERING CABLE ASSEMBLY. 2 L 7 2 4T RT A41NM 1999121800478 19991218 00478 NM 1999 12 18 USAA991142 1 19991029 A 5312 BULKHEAD BOEING 737 737301 1384611 NM STATION 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 178 RBL 4.75, WL 198 SKIN. INSTALLED FILLER S AND DOUBLER PER SRM 51-10-02 AND TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999121800479 19991218 00479 NM 1999 12 18 USAA119908 1 19991115 A 3350 900885A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 21244 FLT 6328 - LGA-BOS - FOUND ON L/S CHECK, BOTH RIGHT WING EXTERIOR EMERGENCY EXIT LIGHTS FLASHING. REPLACED BATTERY PAC K, OPS CHECKS OK. (M) 2 L 7 3 4F A3WE 1999121800480 19991218 00480 NM 1999 12 18 USAA119903 1 19991113 A 3310 532TS13 SWITCH HONEYWELL BOEING 727 727225 1384077 NM COCKPIT FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 919TS 20447 FLT 6311 - BOS-LGA - SMOKE SEEN FROM RUNWAY TURNOFF LIGHT SWITCHES, WHEN SWITCHES PLACED TO ON POSITION. INSPECTED WIRI NG AT SWITCHES, FOUND ALL WIRES OK. REPLACED LEFT AND RIGHT RUNWAY TURNOFF LIGHT SWITCHES, OPERATIONAL CHECK NORMAL. ( M) 2 L 7 3 4F A3WE 1999121800481 19991218 00481 NM 1999 12 18 USAA119904 1 19991112 A 3350 1102833 LIGHT BOEING 727 727254 138408L NM AIRSTAIRS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 916TS 20437 OVERNIGHT L/S DCA - AFT AIRSTAIR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS ASSEMBLY. OPERATION AL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1999121800482 19991218 00482 NM 1999 12 18 USAA119905 1 19991112 A 3350 08165 LIGHT BOEING 727 727254 138408L NM AIRSTAIRS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 912TS 20438 FLT 6364 - DCA-LGA - ESCAPE PATH LIGHTING AT SEAT 10D INOPERATIVE. INSTALLED EPL LIGHT ASSEMBLY, OPERATIONAL CHECK NORM AL. (M) 2 L 7 3 4F A3WE 1999121800483 19991218 00483 NM 1999 12 18 USAA119906 1 19991112 A 3350 LIGHT BOEING 727 727254 138408L NM OVERWING EXIT CORRODED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 916TS 20437 OVERNIGHT L/S DCA- EMERGENCY LIGHT INOPERATIVE RIGHT OVERWING EXIT. CLEANED CORROSION FROM LIGHT SOCKETS. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1999121800484 19991218 00484 NM 1999 12 18 USAASB99255 1 19991020 A 2420 BOEING 737 737201 1384454 NM UNKNOWN A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 233US 22273 GSO - FLT 2660 - UPON PUSHBACK, THE NR 1 TRU C/B TRIPPED. THE NR 1 ENG GEN READ ZERO AMPS AND ZERO VOLTS. CREW RESET T HE NR 1 TRU C/B ALONG WITH THE NORMAL EQUIP BLOWER C/B'S THAT HAD ALSO TRIPPED AND THE NR 1 GEN CAME ON LINE. HOWEVER, EN ROUTE FROM ATL TO BWI AT CRUISE ALT, THE NR 1 TRU C/B TRIPPED AGAIN AND AN ELECTRICAL ODOR WAS NOTED IN THE FLT COMPA RTMENT. CREW SHIFTED BUS NR 1 TO APU GEN AND ODOR WENT AWAY. FLT DIVERTED TO GSO AND LANDED W/O FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX FOUND THR NR 1 ENG FIREWALL CONNECTOR D41O CORRODED. REMOVED AND REPLACED CONNECTOR AND PIN S. RAN NR 1 ENG GEN SYSTEM. OP'S CHECK GOOD. AS FOR THE NORMAL EQUIP BLOWER C/B'S TRIPPING, MX REMOVED AND REPLACED T 2 L 7 2 4F A16WE 1999121800485 19991218 00485 NM 1999 12 18 USAASB99254 1 19991022 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 22797 CMH - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E BATTERY PACK AT STATION 390. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999121800486 19991218 00486 NM 1999 12 18 USAA991246 1 19991106 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 22891 22891 TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT FORWARD EDGE OF LOW ER HINGE CUTOUT OF MAIN ENTRY DOOR. INSTALLED DOUBLER PER SRM 53-30-3 FIG 31. (M) 2 L 7 2 4F A16WE 1999121800487 19991218 00487 NM 1999 12 18 USAA991247 1 19991106 A 5210 SKIN BOEING 737 7372B7 1384560 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 22891 22891 TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK IN FORWARD ENTRY DOOR UPPER HINGE CU TOUT DOOR SKIN. INSTALLED DOUBLER PER TR 52-10-05 AND EA 65479. (M) 2 L 7 2 4F A16WE 1999121800488 19991218 00488 NM 1999 12 18 USAA991216 1 19991025 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 40016 23379 PIT - DURING CX2 CHECK, FOUND 1.5 INCH CRACK IN SKIN AT BS 380 BL 0 AFT EDGE E/E COOLING DUCT CUTOUT. INSTALLED DOUBLER PER EA 53160 BOEING SB 737-53-1117. (M) 2 L 7 2 4F RT A16WE 1999121800489 19991218 00489 WP 1999 12 18 USAAD99161 1 19991115 A 3350 79137451206 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 PHL - THE LOW LEVEL EMERGENCY INDICATOR LIGHTS WERE BLINKING. MAINTENANCE REPLACED THE CONTROL MODULE BATTERIES AND THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999121800490 19991218 00490 WP 1999 12 18 USAAD99159 1 19991114 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 PHL - THE EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT WITH THE EMERGENCY SWITCH IN THE ARMED POSITION. WITH THE SWITCH I N THE OFF POSITION THE EMERGENCY LIGHTS IN FIRST CLASS FLICKER. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE MID FORWA RD CEILING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1999121800491 19991218 00491 WP 1999 12 18 USAAD99160 1 19991113 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 966VJ 47420 IND - THE MAIN ENTRY DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999121800492 19991218 00492 WP 1999 12 18 USAAD99158 1 19991112 A 3260 INDICATOR DOUG DC9 DC931 3022065 WP MLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 983VJ 48159 ORD-PIT - FLT 1272 - AFTER LANDING GEAR EXTENSION ALL THREE RED GEAR INDICATION LIGHTS REMAINED LIT. THE LANDING GEAR W AS CYCLED AND ALL THE LIGHTS INDICATED GREEN. MAINTENANCE INSPECTED ALL THE GEAR INDICATION SENSORS, JACKED THE AIRCRAF T AND PERFORMED MULTIPLE GEAR SWINGS. THE INDICATION PROBLEM COULD NOT BE DUPLICATED. (M) 2 L 7 2 4F A6WE 1999121800493 19991218 00493 WP 1999 12 18 USAAD99157 1 19991109 A 3260 DS077S059 CONNECTOR DOUG DC9 DC931 3022065 WP NLG CORRODED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 991VJ 47310 PIT-ROC - FLT 218 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THE NOSE GEAR UNSAFE LIGHT REMAINED ON. THE LANDING GEAR WAS EXTENDED AND ALL THREE GREEN LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED A CORRODED ELECTRICAL CONNECTOR AT THE NOSE GEAR UPLOCK SWITCH. (M) 2 L 7 2 4F A6WE 1999121800494 19991218 00494 NM 1999 12 18 USAA119907 1 19991115 A 3350 081691 SOCKET BOEING 727 727254 138408L NM ROW 5 MISSING A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 912TS 20438 FLT 6359 - LGA-DCA - FOUND ON POST FLIGHT INSPECTION, ON WHITE EPL LIGHT MISSING AT ROW 5 DEF. REPLACED EPL LIGHT SOCKE T ASSEMBLY AND LENS ASSEMBLY. (M) 2 L 7 3 4F A3WE 1999121800495 19991218 00495 NM 1999 12 18 99ZZZM801 1 19991115 A 3350 0791217023 LENS BOEING 727 727254 138408L NM ROW 5 MISSING A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 912TS 20438 FLT 6359 - LGA-DCA - FOUND ON POST FLIGHT INSPECTION, ON WHITE EPL LIGHT MISSING AT ROW 5 DEF. REPLACED EPL LIGHT SOCKE T ASSEMBLY AND LENS ASSEMBLY. (M) 2 L 7 3 4F A3WE 1999121800496 19991218 00496 WP 1999 12 18 USAAD99156 1 19991109 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 MCO - THE EMERGENCY LIGHTS WERE REMAINING ON AFTER THE AIRCRAFT WAS SHUTDOWN. MAINTENANCE REPLACED THE FORWARD EXIT WIN DOW BATTERY POWER SUPPLY, THE LOW LEVEL LIGHTING CONTROL MODULE, AND THE LOW LEVEL LIGHTING BATTERIES. (M) 2 L 7 2 4F A6WE 1999121800497 19991218 00497 NM 1999 12 18 USAA991132 1 19991029 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 303-294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STRINGER SUPPORT BETWEEN STATION 303.3 - 294.5 HORIZONTAL SUPPORT. INSTALLED NEW FABRICATED SUPPORT PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999121800498 19991218 00498 NM 1999 12 18 USAA991133 1 19991029 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 277 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STRINGER NR 14 STATION 277 SHEAR TY WEB. REMOVED AND R EPLACED WEB PER ARM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999121800499 19991218 00499 NM 1999 12 18 USAA991100 1 19991029 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 312-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURIGN Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 2 INCH BY 32 INCH AT LBL 55 STATION 312 TO 344 FLOORBEA M LEFT Z ANGLE. CORROSION LEVEL 2, CORROSION TASK NR C53-107-01. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999121800500 19991218 00500 NM 1999 12 18 USAA991200 1 19991029 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 480 STRINGER 9R BELTFRAME. INSTALLED DOUBLER PER S RM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999121800501 19991218 00501 NM 1999 12 18 USAA991199 1 19991029 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 706 AT STRINGER 11L ANGLE. REPLACED WITH IDENT ICAL PART 6623574. (M) 2 L 7 2 4F RT A16WE 1999121800502 19991218 00502 NM 1999 12 18 USAA991094 1 19991029 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 967-986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CORRODED AREA AFT SERVICE DOOR Z-ANGLE STATION 967 TO 986.5, WL 208. CORROSION LEVEL 1. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999121800503 19991218 00503 NM 1999 12 18 USAA991140 1 19991029 A 5312 BULKHEAD BOEING 737 737301 1384611 NM STATION 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT STATION 178 LBL 4.75, WL 201 SKIN. INSTALLED FILLERS AND DOUBLER PER SRM 51-10-02 AND TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999121800504 19991218 00504 1999 12 18 USAASB99167 4 19990709 A 3460 BACC45FN18315 CONNECTOR BOEING 737 737301 1384611 NM FLT MANAGMENT FAILED A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 574US 23739 IAH - FLT 1185 - FLIGHT WAS APPROX 150 MILES FROM IAH WHEN THE A/C LOST THE WEATHER RADAR, CAPTAINS HSI, BOTH AUTOPILOTS AND THE CAPTAINS ATTITUDE INDICATOR. CAPTAIN DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL DUE TO THUNDERSTORMS 55 MI LES NORTHEAST OF IAH. THE F/O HAND FLEW THE AIRCRAFT AS AIR TRAFFIC CONTROL VECTORED THEM SOUTH OF THE WEATHER. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT IAH. MAINTENANCE REMOVED AND REPLACED THE NAV DATA TRANSFER CANNON PLUG D1907. ALS O, REMOVED AND REPLACED FMCS COMPUTER (P/N 166805-14-01) PER MM 34-62-21. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1999121800505 19991218 00505 NM 1999 12 18 USAASB99264 1 19991102 A 3260 189929 SENSOR BOEING 737 737301 1384611 NM MLG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 346US 23515 CHS - FLT 542 - DURING CLIMB-OUT FROM CHS, FLIGHT EXPERIENCED A FAILURE OF BOTH ATC TRANSPONDERS AND THE LEFT NAV FUNCTI ON OF THE AUTOPILOT. FLIGHT RETURNED TO FIELD AT CHS AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT THEN TAXIED TO THE GA TE. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AIR GROUND SENSOR S105 AT FAULT. REPLACED S105 SENSOR PER MM. O PERATIONAL CHECK OF BOTH ATC TRANSPONDERS AND LEFT NAV FUNCTION OF AUTOPILOT GOOD. (M) 2 L 7 2 4F RT A16WE 1999121800506 19991218 00506 1999 12 18 USAASB99263 4 19991031 A 3417 HG480B13 ADC BOEING 737 737201 1384454 NM E/E BAY FAILED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 245US 33798 22751 PIT - FLT 2659 - EN ROUTE FROM CLE TO BWI, CRUISING AT FL 290, THE AIRCRAFT TOOK AN UNCOMMANDED ROLL TO THE RIGHT. ROLL WAS A FULL DEFLECTION, STOPPING AT 35 TO 45 DEGREES. CAPTAIN TOOK CONTROL AND RETURNED AIRCRAFT TO LEVEL FLIGHT. THE AUTOPILOT WAS DISCONNECTED AND THE PROBLEM CEASED. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMER GENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA COMPUTER. FUNCTIONAL TEST GOOD. ACCOMPLISHED S ATISFACTORY TEST FLIGHT. AUTOPILOT CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1999121800507 19991218 00507 NM 1999 12 18 USAA991131 1 19991029 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 291.5 AND BS CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 11 AND 12 AND STATION 291.5 AND 277 SH EAR TIE. REPLACED WITH IDENTICAL PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999121800508 19991218 00508 NM 1999 12 18 USAA991209 1 19991101 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 38606 23935 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 380, DIRECTLY AFT OF EQUIPMENT COOLING DUCT O UTLET FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 1999121800509 19991218 00509 NM 1999 12 18 USAA991201 1 19991029 A 5311 FRAME BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 907 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65850. (M) 2 L 7 2 4F RT A16WE 1999121800510 19991218 00510 NM 1999 12 18 USAA991164 1 19991029 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT FORWARD SERVICE DOOR CUTOUT LOWER AFT CORNER DOOR FR AME SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999121800511 19991218 00511 NM 1999 12 18 USAA991144 1 19991029 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 178 BULKHEAD RBL .5, WL 188 WEB. CUTOUT DAM AGE AREA AND INSTALLED DOUBLER PER SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999121800512 19991218 00512 NM 1999 12 18 USAA991148 1 19991029 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 616 STRINGER 2R TIE CLIP. REPLACED PER SRM 51 -40-02. (M) 2 L 7 2 4F RT A16WE 1999121800513 19991218 00513 NM 1999 12 18 USAA991147 1 19991029 A 5311 FRAME BOEING 737 737301 1384611 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 887 STRINGER 9L BELT FRAME. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M) 2 L 7 2 4F RT A16WE 1999121800514 19991218 00514 NM 1999 12 18 USAA991145 1 19991029 A 5311 FRAME BOEING 737 737301 1384611 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 827 STRINGER 9R BELT FRAME. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M) 2 L 7 2 4F RT A16WE 1999121800515 19991218 00515 NM 1999 12 18 USAA991146 1 19991029 A 5311 FRAME BOEING 737 737301 1384611 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 827 STRINGER 9L BELT FRAME. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M) 2 L 7 2 4F RT A16WE 1999121800516 19991218 00516 NM 1999 12 18 USAA991165 1 19991029 A 5313 BAC1498108 STRINGER BOEING 737 737301 1384611 NM BS 303.3 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER 4 JUST AFT OF STATION 303.3. INSTALLED REPAIR ZEE AND FILLER PER SRM 53-00-03 AND EA 65951. (M) 2 L 7 2 4F RT A16WE 1999121800517 19991218 00517 NM 1999 12 18 USAA991093 1 19991029 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION STATION 344 FLOORBEAM UPPER FLANGE LBL 12 TO RBL 10. CORROSION LEVEL 1. NEW SECTION SPLICED IN PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999121800518 19991218 00518 NM 1999 12 18 USAA991084 1 19991029 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 8 INCH AT FLOORBEAM BS 986.5, LBL 44 TO RBL 44 BEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED CORRODED AREA PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999121800519 19991218 00519 NM 1999 12 18 USAA991082 1 19991029 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1/CX-6 CHECK VISUAL INSPECTION, FUOND A .25 INCH CRACK AT STATION 706, STRINGER 11L AFT SIDE OF FRAME ATT ACH ANGLE. FABRICATED NEW ANGLE PER DRAWING 66-23574. (M) 2 L 7 2 4F RT A16WE 1999121800520 19991218 00520 NM 1999 12 18 USAA991044 1 19991029 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CRACK .25 INCH AT STATION 663 STRINGER 10R TIE CLIP. REPLACED WITH ID ENTICAL PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999121800521 19991218 00521 NM 1999 12 18 USAA991043 1 19991029 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 CRACKS EACH .25 INCH AT STATION 663 STRINGER 10L. REPLACED WITH IDENT ICAL PART PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1999121800522 19991218 00522 NM 1999 12 18 USAA991150 1 19991029 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO .75 INCH AREAS OF CORROSION AT STATION 328, BL 0, AND LBL 28 FLOORBE AM. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. INSTALLED T-CAP AND DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999121800523 19991218 00523 NM 1999 12 18 USAA991149 1 19991029 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 480 STRINGER 9L FRAME. INSTALLED DOUBLER PE R SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999121800524 19991218 00524 NM 1999 12 18 USAA991101 1 19991029 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND 7.25 INCH AT FLOORBOARD FASTENERS HOLES FLOORBEAM 312 L BL 11 TO RBL 11. CORROSION LEVEL 2. INSTALLED 'T' CAP AND DOUBLER EPR SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999121800525 19991218 00525 NM 1999 12 18 USAA991134 1 19991029 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 291.5/BS 277 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGERS 12 AND 13 AND BETWEEN STATION 291.5 A ND 277 SHEAR TIE. REPLACED WITH IDENTICAL PART PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999121800526 19991218 00526 NM 1999 12 18 USAA991141 1 19991029 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FUOND A .75 INCH CRACK AT STATION 178 LBL 4.78, WL 198 SKIN. INSTALLED FILLER S AND DOUBLERS PER SRM 51-10-02 AND TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999121800527 19991218 00527 NM 1999 12 18 F3LA99133 1 19991103 A 5347 SEAT TRACK BOEING 737 7372P6 NM BS 344-360 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK INSPECTION REPORTED CORROSION IN FORWARD SEAT TRACK EDGE, LEFT INBOARD TRACK, BETWEEN STATION 344 AND 360. MAINTENANCE REPAIRED PER SRM 53-10-5, PAGE 3-5, FIGURE 2, SHEETS 1-3. (M) 2 L 7 2 4F RT A16WE 1999121800528 19991218 00528 NM 1999 12 18 BJNA991003 1 19991021 A 3260 6552811109 ACCESSORY UNIT BOEING 737 737282 13844AT NM LANDING GEAR MALFUNCTIONED A BJNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 11 789TM 23046 ABNORMAL GEAR RETRACTION. VISUALLY CHECKED ALL LANDING GEAR, UPLOCK AND DOWNLOCK SENSORS AND WIRING. REPLACED LANDING GEAR ACCESSORY UNIT AND TESTED IAW BMM 32-09-100. ALL TESTS WERE NORMAL JACKED AIRCRAFT AND PERFORMED EXT/RET TEST IAW BMM 7-11-11. ALL TESTS NORMAL. AIRCRAFT CHECK FLIGHT COMPLETED. NO DISCREPANCIES NOTED. (M) 2 L 7 2 4F RT A16WE 1999121800529 19991218 00529 WP 1999 12 18 AALA991530 1 19991007 A 2613 JAM NUT DOUG DC9 DC982 3022082 WP TAIL COMP LOOSE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 450AA 49476 DFW - FLT 2221 - EN ROUTE ORD-DFW - TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMB-OUT. ACCOMPLISHED EMER GENCY CHECKLIST, LIGHT STAYED ILLUMINATED. BEGAN EXPANDED CHECKLIST, DETERMINED LIGHT EXTINGUISHED WHEN LEFT THROTTLE W AS BELOW 1.65 EPR. CONTINUED FLIGHT FOR 15 MINUTES, FIRE AGENT NUMBER 2 LOW LIGHT ILLUMINATED. 15 MINUTES LATER FIRE A GENT NUMBER 1 LOW LIGHT ILLUMINATED. DIVERTED AND LANDED STL WITHOUT INCIDENT. INSPECTED AND FOUND SAFE FOR FERRY FLIG HT TO DFW FOR REPAIR. SECURED JAM NUT TO 13 SM-65 SENSE LINE LEFT TAIL SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F A6WE 1999121800530 19991218 00530 1999 12 18 AALA991578 4 19991020 A 2210 6224717004 PANEL BOEING 767 767223 1385123 NM COCKPIT DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 328AA 1761 22328 LHR - FLT 66 - EN ROUTE LHR - APPROXIMATELY 20 MINUTES PRIOR TO LANDING A BURNING ELECTRICAL SMELL WAS NOTICED IN COCKPI T. LANDED WITHOUT INCIDENT. REPLACED AUTO FLIGHT MODE CONTROL SELECT PANEL AND CAPTAINS DME/VOR PANEL. ACCOMPLISHED M CDP TEST 40. INSPECTED WINDOW HEAT CONNECTIONS AND COOLING DUCTS. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A1NM 1999121800531 19991218 00531 WP 1999 12 18 AALA991540 1 19991011 A 2930 90G621A SWITCH DOUG DC9 DC982 3022082 WP RT HYD SYSTEM DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 266AA 3509 49291 DFW - FLT 527 - EN ROUTE DFW-SLC, RIGHT SYSTEM HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. EMERGENCY DECLARED AND AIRCRAF T RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND NO HYDRAULIC LEAKS AND BOTH HYDRAULIC RESERVOIRS WERE FULL. REPLA CED RIGHT HYDRAULIC SYSTEM LOW PRESSURE SWITCH. ALSO, REPLACED RIGHT HYDRAULIC PRESSURE TRANSMITTER. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800532 19991218 00532 WP 1999 12 18 AALA991544 1 19991014 A 3241 CONNECTOR DOUG DC9 DC982 3022082 WP MLG LOOSE A AALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 581AA 53158 SAT - FLT 1636 - DURING TAKEOFF ROLL, MAIN LANDING GEAR WHEEL NOT TURNING ANNUNCIATOR LIGHT ILLUMINATED. TAKEOFF ABORTE D AND AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. RESECURED LOOSE CONNECTOR TO NR 1 MAIN LANDING GEAR ANTI-SKID TRANSDU CER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800533 19991218 00533 WP 1999 12 18 AALA991559 1 19991018 A 5248 CABLE DOUG DC9 DC982 3022082 WP TAIL CONE LOOSE A AALA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 439AA 49457 ORD - FLT 1427 - TAIL CONE LIGHT ILLUMINATED AFTER LANDING ORD. RESECURED LOCKING CABLE AND INSPECTED INTEGRITY OF ENTI RE TAIL CONE RELEASE SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800534 19991218 00534 WP 1999 12 18 AALA991555 1 19991015 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP APU COMP LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 3515 P80487 49892 BOS - FLT 1527 - AFTER TAKEOFF BOS CREW NOTICED SMOKE IN CABIN. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. CHANGED A PU AND REPLACED BOTH WATER SEPARATOR BAGS. CLEANED INSIDE OF WATER SEPARATOR AND ACCOMPLISHED PACK BURNOUT OF HIGH PRES SURE DUCTING. ALL WORK ACCOMPLISHED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800535 19991218 00535 WP 1999 12 18 AALA991562 1 19991018 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 415AA 49326 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT STRIP IN FORWARD GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800536 19991218 00536 WP 1999 12 18 AALA991561 1 19991018 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP AFT STAIRWAY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 574AA 53151 SFO - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED AFT STAIRWAY OV ERHEAD EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800537 19991218 00537 WP 1999 12 18 AALA991551 1 19991017 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70404 49315 DFW - DURING OVERNIGHT MAINTENANCE, BOTH TAIL COMPARTMENT OVERHEAD EMERGENCY EXIT LIGHTS AND TAIL CONE SLIDE EMERGENCY E XIT LIGHTS INOPERATIVE. REPAIRED OPEN CONNECTION ON EMERGENCY EXIT LIGHT SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (M) 2 L 7 2 4F A6WE 1999121800538 19991218 00538 WP 1999 12 18 AALA991549 1 19991015 A 3350 L202011 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 226AA 49176 PHX - DURING OVERNIGHT MAINTENANCE FORWARD CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD CEILING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800539 19991218 00539 WP 1999 12 18 AALA991525 1 19991009 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 480AA 49655 DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING AND MAIN CABIN INOPERATIVE. REPLACED JUMPER WIRE FOR EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800540 19991218 00540 WP 1999 12 18 AALA991523 1 19991008 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7537A 49991 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHTING SIGN INOPERATIVE. REPLACED CONNEC TOR PIN ON FORWARD GALLEY EMERGENCY EXIT FLOOR PATH LIGHTING SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800541 19991218 00541 NM 1999 12 18 99ZZZM802 1 19991019 A 3260 656021132 MODULE BOEING 727 727227 1384078 NM LT MLG DEFECTIVE A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 308AS 22002 FLT 127 KOKC-KDAY - AFTER TAKEOFF AND UPON PLACING GEAR HANDLE IN UP POSITION LEFT MLG SHOWED GREEN AND RED LIGHTS ON CE NTER PANEL. SECONDARY LIGHTS EXTINGUISHED. CYCLED GEAR HANDLE TO OFF, LIGHTS REMAINED GREEN AND RED. CYCLED GEAR HAND LE TO DOWN SAFE IND CENTER AND SECONDARY. RETURNED TO KOKC WITHOUT FURTHER INCIDENT. INSTALLED SERVICEABLE LANDING GEA R ACCESSORY MODULE. OPERATIONAL CHECK OF LEFT MLG LOCK AND POSITION INDICATING SYSTEM CHECKED GOOD IAW B727 MM 32-19-12 1. RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999121800542 19991218 00542 WP 1999 12 18 AALA991556 1 19991015 A 2721 49558711 BOLT DOUG DC9 DC982 3022082 WP RUDDER TAB MISSING A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 493AA 49731 DFW - FLT 465 - RIGHT AFTER T/O DFW WITH FLAP RETRACTION A/C TRIED TO ROLL RIGHT. THE RUDDER FELT AS IF IT WAS LOCKED U P WHEN TRYING TO PUSH IT LEFT. PUSHING IT RIGHT SEEMED TO WORK. AT ONE POINT THE RUDDER PEDALS WERE FELT TO MOVE BACK AND FORTH SLIGHTLY ON THEIR OWN. THE AUTOPILOT WAS NOT ON. THE PROBLEM WAS WORSE AT HIGHER SPPEDS. WHEN THE DFGS WAS MOVED FROM NR 1 TO NR 2 PER THE MANUAL THE RUDDER SEEMED TO UNLOCK AND THE A/C THEN TRIED TO ROLL THE OTHER DIRECTIONS. GOING TO MANUAL RUDDER CAUSED YAWING AND ROLL IN NEW DIRECTIONS. RETURNED DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. TOUCHDOWN WAS NORMAL. INSTALLED RUDDER TAB CRANK ARM BOLT AND CHECKED RUDDER RIG. SYS GROUND CHECKED NORMAL OP'S. AC 2 L 7 2 4F A6WE 1999121800543 19991218 00543 WP 1999 12 18 WXOA99007 1 19991011 A 5400 99122439 ANGLE DOUG DC9 DC921 302205A WP LT PYLON CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, PERFORMED NDT HFEC INSPECTION PER OPS 4.735. RESULTS OF I NSPECTION DETECTED CRACK ON ANGLE P/N 9912243-9 AT THE LEFT PYLON LOWER FRONT SPAR STATION Y781/Z20. REMOVED CRACKED AT TACH ANGLE AND INSTALLED NEW ANGLE PER DC-9 SERVICE BULLETIN DC9-53-150 AND DC-9 SRM 51-30-1, 51-30-2 AND 51-20-0. (M) 2 L 7 2 4F A6WE 1999121800544 19991218 00544 WP 1999 12 18 WXOA99006 1 19991006 A 5311 FRAME DOUG DC9 DC921 302205A WP BS 859 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, AFT ACCESSORY COMPARTMENT FRAME 859 AT LONGERON L13 IS CRA CKED BY LIGHTNING HOLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-9 SRM 53-01 PAGE 9, 51-10-2, 51-10- 3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121800545 19991218 00545 WP 1999 12 18 WXOA99005 1 19991006 A 2120 DUCT DOUG DC9 DC921 302205A WP BS 261 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACK DETECTED IN COOLING EXHAUST DUCT AT FUSELAGE STATION 261 AND LONGERON L21. WELDED CRACKS TWO PER REPAIR STATION PROCEDURES IAW FAA AC 43.13 1A. (M) 2 L 7 2 4F A6WE 1999121800546 19991218 00546 WP 1999 12 18 WXOA99004 1 19991006 A 5720 BRACKET DOUG DC9 DC921 302205A WP LT WING CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEFT WING SLAT TRACK NR 2 FORWARD LOWER PANEL BRACKET CRAC KED AND OUTBOARD BRACKET HOLE ELONGATED. REMOVED TWO DAMAGED BRACKETS, FABRICATED REPAIR BRACKETS AND INSTALLED REPAIR BRACKETS IAW DC-9 SRM 51-10-2, 51-10-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121800547 19991218 00547 WP 1999 12 18 WXOA99003 1 19990923 A 2730 5913832503 BRACKET DOUG DC9 DC951 3022051 WP BS 1273 CORRODED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 414EA 47746 FAT - DURING AIRCRAFT CONFORMITY INSPECTION, PRIOR TO PLACING AIRCRAFT ON AIRLINE OPERATIONS SPECIFICATIONS, LEVEL 1 COR ROSION DETECTED ON ELEVATOR CABLE PULLEY BRACKET BY MEANS OF VISUAL INSPECTION. BRACKET LOCATED IN TAILCONE AREA. REMO VED AND REPLACED BRACKET. (M) 2 L 7 2 4F RT A6WE 1999121800548 19991218 00548 NM 1999 12 18 P2EA99316 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM CRACKED AT BS 727, WL 202 INCH AND RBL 24.5. REPAIRED FLOORBEAM BETWEEN BS 721 AND BS 7 37 IAW SERVICE BULLETIN 737-57-1210, PART III FIG 7, DATED APRIL 4, 1991. (M) 2 L 7 2 4F A16WE 1999121800549 19991218 00549 NM 1999 12 18 P2EA99315 1 19991110 A 5320 65C3176612 FITTING BOEING 737 737297 1384480 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FITTING AT BS 727, BL 0, WL 202 INCH CRACKED. REPLACED FITTING IAW SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999121800550 19991218 00550 NM 1999 12 18 P2EA99314 1 19991102 A 5320 BEAM BOEING 737 737297 1384480 NM BS 726 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, LEFT WHEEL WELL AT BS 726, WL 192 LBL 66 INCH STRINGER 18A SHEAR BEAM CRACKED. FABRICATED SHEAR B EAM IAW SRM 51-20-1 AND REPLACED SHEAR BEAM IAW SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1999121800551 19991218 00551 NM 1999 12 18 P2EA99313 1 19991103 A 5754 6546421222 FASTENERS BOEING 737 737297 1384480 NM NR 6 SLAT WRONG PART A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, NR 6 SLAT REPAIRED WITH TEMPORARY FASTENERS. REPAIRED IAW SRM 57-50-3 FIG 4. (M) 2 L 7 2 4F A16WE 1999121800552 19991218 00552 NM 1999 12 18 P2EA99318 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DUIRNG C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 727, WL 202 INCH AND LBL 24.5 INCH. REPAIRED FLOORBEAM LOWER CHORD FROM BS 721.5 TO BS 738.5 IAW SERVICE BULLETIN 737-57-1210, PART III FIG 7, DATED APRIL 4, 1991. (M) 2 L 7 2 4F A16WE 1999121800553 19991218 00553 NM 1999 12 18 P2EA99317 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 726 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 DURING C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 726, BL 0 AND WL 202 INCH. REPAIRED FLOORBEAM LOWER CHORD FROM BS 7 21 TO BS 738 IAW SB 737-57-1210, PART III FIG 7, DATED APRIL 4, 1991. (M) 2 L 7 2 4F A16WE 1999121800554 19991218 00554 SO 1999 12 18 ASOA99151 1 19991115 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 233AS 17429 120031 DURING INSPECTION, FOUND NR 1 AND 3 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND 3 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800555 19991218 00555 SO 1999 12 18 ASOA99152 1 19991116 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 242AS 25990 120069 DURING INSPECTION, FOUND NR 2 EMERGENCY BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY BATTERY. O PS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800556 19991218 00556 SO 1999 12 18 ASOA99153 1 19991116 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 285AS 20609 120265 DURING INSPECTION, FOUND NR 3 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY B ATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800557 19991218 00557 SO 1999 12 18 ASOA99132 1 19991018 A 5410 12003851004 FRAME EMB 120 EMB120RT SO RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 269AS 120210 DURING INSPECTION, FOUND RIGHT NACELLE FRAME NR 1 CRACKED. MAINTENANCE REPAIRED CRACK IAW EO 120-54-0034 AND S/B 120-54 -0036. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800558 19991218 00558 SO 1999 12 18 ASOA99133 1 19991018 A 5410 12003851003 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 269AS 120210 DURING INSPECTION, FOUND LEFT NACELLE FRAME NR 1 CRACKED. MAINTENANCE REPAIRED CRACK IAW EO 120-54-0034 AND S/B 120-54- 0036. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800559 19991218 00559 SO 1999 12 18 ASOA99130 1 19991018 A 5400 12016079001 STIFFENER EMB 120 EMB120RT SO LT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 269AS 120210 DURING INSPECTION, FOUND LEFT NACELLE FLAP TOP SKIN STIFFENER HAS A CRACK. MAINTENANCE REPAIRED STIFFENER IAW EMB 120 S RM 54-20-02. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 2 4T RT A31SO 1999121800560 19991218 00560 SO 1999 12 18 ASOA99131 1 19991018 A 5330 12022788017 SKIN EMB 120 EMB120RT SO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 269AS 120210 DURING INSPECTION, FOUND SKIN EDGE CRACK AT THE LATERAL POST. MAINTENANCE REPAIRED CRACK IAW EO 120-53-0119. OPERATION AL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800561 19991218 00561 NM 1999 12 18 EISA99165 1 19990910 A 2432 25502003 BATTERY BOEING 727 727223 1384074 NM E/E BAY OVERHEATED A EISA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 6819 MARATHON 19494 FOUR MINUTES AFTER APU CONNECTED, SMOKE IN COCKPIT. CREW SHUT DOWN ALL POWER. FIRE DEPARTMENT REMOVED SMOKING BATTERY. REMOVED AND REPLACED BATTERY. (M) 2 L 7 3 4F A3WE 1999121800562 19991218 00562 NM 1999 12 18 EISA99213 1 19991106 A 2823 AV16E1167C VALVE BOEING 727 727223 1384074 NM FUEL SO FAILED A EISA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 07 316NE 19475 AT APPROXIMATELY LEVEL OFF AT FLIGHT LEVEL 280, APU FIRE WARNING LIGHT AND HORN SOUNDED. APU FIRE CHECK, LIST ACCOMPLIS HED IAW AIRCRAFT OPERATION MANUAL PROCEDURES. FIRE BOTTLE DISCHARGED. APU FAILED TO SHUT DOWN AND WAS RUNNING IN FLIGH T, CAUSING AN OVER TEMPERATURE CONDITION. REMOVED AND REPLACED THE FUEL SHUTOFF VALVE AND 3-SPEED SWITCH. (M) 2 L 7 3 4F A3WE 1999121800563 19991218 00563 NM 1999 12 18 EISA99217 1 19991116 A 5240 652555527 DOOR BOEING 727 727223 1384074 NM FUSELAGE MISSING A EISA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 SW 07 312NE 20193 B-SYSTEM SERVICE DOOR MISSING. PER MAINTENANCE THERE IS SHEET METAL DAMAGE, TO AIRFRAME, HINGE IS MISSING AND RIVETS PUL LED. REPLACED DOOR ASSEMBLEY, DALFORT COMPLETED STRUCTURAL REPAIR PER 727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999121800564 19991218 00564 NM 1999 12 18 F3LA99140 1 19991104 A 5320 INTERCOSTAL BOEING 737 7372P6 NM BS 344-360 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON WEB BETWEEN FLOORBEAMS 344 AND 360. MAINTENANCE FABRICATED AND REPLACED INTERCOSTAL BETWEEN 344 AND 360 PER SRM 53-10-2, FIG 7, AND EA NR 53-737-047. (M) 2 L 7 2 4F RT A16WE 1999121800565 19991218 00565 NM 1999 12 18 F3LA99139 1 19991024 A 5531 RIB BOEING 737 7372P6 NM VERTICAL STAB CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON RIGHT VERTICAL STABILIZER RIB CAPS AROUD NUTPLATES AT BS 58. MAINTEN ANCE REPLACED UPPER AND LOWER CHORDS PER SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A16WE 1999121800566 19991218 00566 NM 1999 12 18 F3LA99142 1 19991104 A 5320 INTERCOSTAL BOEING 737 7372P6 NM BS 328-344 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL BETWEEN BS 328 AND 344, 12 INCHES RIGHT OF BBL 0. M AINTENANCE FABRICATED AND REPLACED INTERCOSTAL PER SRM 53-10-2, FIG 7 AND EA NR 53-737-047. (M) 2 L 7 2 4F RT A16WE 1999121800567 19991218 00567 NM 1999 12 18 F3LA99143 1 19991108 A 5313 STRINGER BOEING 737 7372P6 NM BS 360 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STRINGER 28L AT BS 360 INSIDE E/E COMPARTMENT. MAINTENANCE REP LACED STRINGER PER 53-10-3, FIG 1 DETAIL 7. (M) 2 L 7 2 4F RT A16WE 1999121800568 19991218 00568 NM 1999 12 18 F3LA99144 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT BS 967, RBL 32, 36 AND 40. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-6, 51-10-9, 51-20-1, 51-22-99, 51-30-2 AND 51-30-3. (M) 2 L 7 2 4F RT A16WE 1999121800569 19991218 00569 NM 1999 12 18 F3LA99146 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM NUT PLATE HOLES AT BS 967, RBL 14 TO RBL 48. MAINTENANCE F ABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-9, FIG 2, PAGE 10 A. (M) 2 L 7 2 4F RT A16WE 1999121800570 19991218 00570 NM 1999 12 18 F3LA99147 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 312-328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM, BS 312 TO BS 328. MAINTENANCE FABRICATED REPLACEMEN T PARTS PER SRM 53-10-2, DETAIL I, AND EA 53-737-047, AND REPAIRED PER SRM 53-10-9, FIG 7. (M) 2 L 7 2 4F RT A16WE 1999121800571 19991218 00571 NM 1999 12 18 F3LA99148 1 19991108 A 5320 INTERCOSTAL BOEING 737 7372P6 NM BS 277-294 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL BETWEEN FLOORBEAMS 277 AD 294. MAINTENANCE FABRICA TED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-2, FIG 7, AND EA 53-737-047. (M) 2 L 7 2 4F RT A16WE 1999121800572 19991218 00572 NM 1999 12 18 F3LA99149 1 19991108 A 5320 WEB BOEING 737 7372P6 NM BS 294-312 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON WEB BETWEEN FLOORBEAMS 294 AND 312, LT OF BBL 0. MAINTENANCE F ABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-2, FIG 7, AND EA 53-737-047. (M) 2 L 7 2 4F RT A16WE 1999121800573 19991218 00573 NM 1999 12 18 F3LA99150 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 294 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON TOP CHORD OF FLOORBEAM, BS 294. MAINTENANCE FABRICATED REPLACE MENT PARTS AND REPAIRED PER SRM 53-10-1, 51-30-2, 51-10-2, PAGES 1-3, AND SRM 51-10-9 FIG 1. (M) 2 L 7 2 4F RT A16WE 1999121800574 19991218 00574 NM 1999 12 18 F3LA99151 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 312 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURNG C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP 312, BBL 0 TO BBL 16. MAINTENANCE FABRICATED REPL ACEMENT PARTS AND REPAIRED PER SRM 53-10-9, FIG 7, AND SRM 53-10-2, DETAIL 1, FIG 7. (M) 2 L 7 2 4F RT A16WE 1999121800575 19991218 00575 NM 1999 12 18 F3LA99152 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 312 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM 312, BBL 0 TO RT SIDE END. MAINTENANCE FABRICATED RE PLACEMENT PARTS AND REPAIRED PER SRM 53-10-9, FIG 7, AND SRM 53-10-2, DETAIL 1, FIG 7. (M) 2 L 7 2 4F RT A16WE 1999121800576 19991218 00576 NM 1999 12 18 F3LA99153 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON TOP CHORD OF FLOORBEAM 328, BBL 6-12 LT. MAINTENANCE FABRICATED REPL ACEMENT PARTS AND REPAIRED PER SRM 53-10-9 FIG 1. (M) 2 L 7 2 4F RT A16WE 1999121800577 19991218 00577 NM 1999 12 18 F3LA99154 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON TOP CHORD OF FLOORBEAM 328, BBL 0 TO 50 INCHES RT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-0, FIG 7 AND SRM 53-10-2, FIG 7 DETAIL 1. (M) 2 L 7 2 4F RT A16WE 1999121800578 19991218 00578 NM 1999 12 18 F3LA99155 1 19991108 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 344 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK INSPECTION, REPORTED CORROSION ON TOP CAP OF FLOORBEAM 344. MAINTENANCE FABRICATED REPLACEMENT P ARTS AND REPAIRED PER SRM 53-10-9, FIG 1, AND SRM 53-10-2 FIG 7. (M) 2 L 7 2 4F RT A16WE 1999121800579 19991218 00579 NM 1999 12 18 F3LA99156 1 19991104 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL BETWEEN FLOORBEAMS 328 AND 344 LT. MAINTENANCE FAB RICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-2, FIG 7, AND EA 53-737-047. (M) 2 L 7 2 4F RT A16WE 1999121800580 19991218 00580 NM 1999 12 18 F3LA99157 1 19991122 A 5512 SKIN BOEING 737 7372P6 NM HORIZONTAL STAB CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK INSPECTION, REPORTED FORWARD TIP OF RIGHT STABILIZER CORRODED. MAINTENANCE FABRICATED REPLACEMEN T PARTS AND REPAIRED PER EA NR 55-737-010. (M) 2 L 7 2 4F RT A16WE 1999121800581 19991218 00581 NM 1999 12 18 F3LA99158 1 19991108 A 5540 WEB BOEING 737 7372P6 NM RUDDER CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON WEB INVERTICAL STABILIZER AT RUDDER BS 45. MAINTENANCE FABRICA TED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND EO NR 53-737-044. (M) 2 L 7 2 4F RT A16WE 1999121800582 19991218 00582 NM 1999 12 18 F3LA99159 1 19991108 A 5347 SEAT TRACK BOEING 737 7372P6 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED FORWARD SEAT TRACK EDGES CORRODED ON RIGHT INBOARD GALLEY FLOOR. MAINTENANC E FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999121800583 19991218 00583 NM 1999 12 18 F3LA99160 1 19991025 A 5320 SUPPORT BOEING 737 7372P6 NM FRAME 394-312 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FORWARD LAVATORY FLOOR SUPPORT BETWEEN FLOORBEAMS 294 AND 312. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, FIG 7, AND EA NR 53-737-047. (M) 2 L 7 2 4F RT A16WE 1999121800584 19991218 00584 NM 1999 12 18 F3LA99161 1 19991025 A 5347 SEAT TRACK BOEING 737 7372P6 NM BS 340/350 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TRACK AT BS 340 AND 350. MAINTENANCE FABRICATED REPLACEM ENT PARTS AND REPAIRED PER SRM 53-10-5, FIG 2, AND SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1999121800585 19991218 00585 NM 1999 12 18 F3LA99162 1 19991108 A 5320 INTERCOSTAL BOEING 737 7372P6 NM BS 987.5-1006 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON DIAGONAL, INTERCOSTAL BETWEEN BS 1006 AND 987.5. MAINTENANCE F ABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999121800586 19991218 00586 NM 1999 12 18 F3LA99163 1 19991108 A 5313 STRINGER BOEING 737 7372P6 NM BS 960-970 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSON ON STRINGER 26L, BS 960 - BS 970. MAINTENANCE FABRICATED REPLACEME NT PARTS AND REPAIRED PER SRM 53-10-3, FIG 1, DETAIL 7. (M) 2 L 7 2 4F RT A16WE 1999121800587 19991218 00587 NM 1999 12 18 F3LA99164 1 19991121 A 5313 STRINGER BOEING 737 7372P6 NM BS 987-987.5 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26R, BS 987 TO BS 987.5. MAINTENANCE FABRICATED REPLA CEMENT PARTS AND REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 1999121800588 19991218 00588 NM 1999 12 18 F3LA99165 1 19991024 A 5523 BRACKET BOEING 737 7372P6 NM ELEVATOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED RT ELEVATOR TOP OUTBOARD HINGE COVER BRACKET CRACKED. MAINTENANCE FABRICATE D REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2 AND 51-40-3. (M) 2 L 7 2 4F RT A16WE 1999121800589 19991218 00589 WP 1999 12 18 GTIA9900120 1 19991115 A 7830 WARNING LIGHT DOUG DC9 DC987 3022087 WP T/R ACCUMULATOR ILLUMINATED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 750RA 49777 DTW - FLT 712 - LEFT REVERSER ACCUMULATOR LOW LIGHT CAME ON DURING CRUISE. COMPLIED WITH QRH AND LIGHT CAME BACK ON AFT ER 45 MINUTES. PERFORM OPS CHECK ON THRUST REVERSER. PRE-CHANGE IS AT 1000 PSI. CLEANED CANNON PLUG ON SWITCH. OPS C HECKED GOOD, NO DEFECTS NOTED AT THIS TIME IAW MM 78-31-00. (M) 2 L 7 2 4F RT A6WE 1999121800590 19991218 00590 NM 1999 12 18 GAIA99168 1 19991122 A 2121 5007024620 GASPER FAN BOEING 727 727224 1384076 NM BS 720 OVERHEATED A GAIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 69740 20668 FLT 2032 - DEN-MHR - DURING CRUISE, THE GASPER FAN OVERHEATED, SMELL SMOKE, SHORTLY THEREAFTER THE GASPER FAN CIRCUIT BR EAKER TRIPPED. THE AIRCRAFT CONTINUED ON TO MHR AND MADE A SAFE LANDING. REMOVED INOPERATIVE GASPER FAN. INSTALLED NE WLY OVERHAULED GASPER FAN. OPERATIONAL CHECK CARRIED OUT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999121800591 19991218 00591 WP 1999 12 18 GAIA99152 1 19991007 A 3241 DC26F1210S CONNECTOR DOUG DC9 DC915F 3022037 WP BRAKE DIRTY A GAIA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 563PC 47055 FLT 563 - EWR-DFW - AFTER LANDING AT DFW ON ROLL OUT THE LEFT BRAKE WOULD NOT APPLY. THE BRAKE OPERATED NORMALLY WITH T HE ANTI-SKID OFF. THE AIRCRAFT TAXIED TO PARKING WITHOUT INCIDENT. CLEANED CANNON PLUG ON BOTH DUAL SERVO VALVES IN LE FT WHEEL WELL. OPS CHECK ON GROUND SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999121800592 19991218 00592 WP 1999 12 18 GTIA9901206 1 19991112 A 3260 WARNING HORN DOUG DC9 DC932 3022066 WP MLG SOUNDED A GTIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 12536 47113 ACY - FLT 880 - UPON MOVING THE L/G HANDLE TO THE UP POSITION THE L/G WARNING HORN SOUNDED AND WOULD NOT SILENCE. L/G R ETRACTED CORRECTLY WITH L/G EXTENDED ALL WARNING LIGHTS AND HORN WAS EXTINGUISHED. RETURNED TO ACY NO FURTHER PROBLEMS. (M) 2 L 7 2 4F A6WE 1999121800593 19991218 00593 WP 1999 12 18 GTIA9900119 1 19991103 A 2600 CONNECTOR DOUG DC9 DC941 302207N WP WARNING LIGHT DISCONNECTED A GTIA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 GL 23 130NK 47604 MYR - FLT 257 - LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND CANNON PLUG UNATTACHED FROM BATTERY PACK. LOCK ED CANNON PLUG ON BATTERY. OPS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1999121800594 19991218 00594 WP 1999 12 18 GTIA9901194 1 19991109 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 DTW - FLT 605 - EMERGENCY FLOOR LIGHTING INOPERATIVE. REPAIR TRACK LIGHT WIRING AT ROW NR 9, OPS CHECKED GOOD IAW DC-9 MM 33-50. (M) 2 L 7 2 4F A6WE 1999121800595 19991218 00595 WP 1999 12 18 GTIA9901198 1 19991106 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP ROW 2/4 DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 MYR - FLT 257 - OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 2 AND 4. REMOVED AND REPLACED BATTERY PACK AT B5-24 IAW M M 33-53-0, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999121800596 19991218 00596 WP 1999 12 18 GTIA9901199 1 19991107 A 3350 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 750RA 49777 DTW - BOTH FORWARD OVERWING EMERGENCY EXITS LIGHTS INOPERATIVE. REPLACED EMERGENCY POWR SUPPLY, OPS CHECK GOOD PER MM 3 3-51-00. (M) 2 L 7 2 4F RT A6WE 1999121800597 19991218 00597 WP 1999 12 18 GTIA9901204 1 19991111 A 3350 LIGHT DOUG DC9 DC931 3022065 WP ROW 9/21 LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 132NK 47202 MCO - FLT 729 - TRANSFERRED FROM CABIN LOG CONTROL NR 12034 AISLE PATH LIGHTING STRIPS TORN LOOSE AT ROW 9 AND 21. RE-I NSTALLED AND SECURED FLOOR PATH LIGHTING AT ROW 9 AND 21. OPS CHECK GOOD IAW MM 33-51-00. (M) 2 L 7 2 4F A6WE 1999121800598 19991218 00598 WP 1999 12 18 AALA991577 1 19991019 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 285AA 49297 DFW - DURING OVERNIGHT MANTENANCE, AFT CEILING EMERGENCY EXIT LIGHT INOPERATIVE. SPLICED WIRES TO AFT CEILING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800599 19991218 00599 WP 1999 12 18 AALA991579 1 19991019 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT STAIRS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 513AA 49890 IAH - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY ESCAPE PATH MARKING EXIT LIGHT INOPERATIVE. REPAIRED AFT STAIR EMERGENCY ESCAPE PATH MARKING EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800600 19991218 00600 WP 1999 12 18 AALA991575 1 19991019 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 20D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 208AA 49159 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHING AT SEAT 20D INOPERATIVE. RECONNECTED EMERGENCY EX IT FLOOR PATH LIGHTING CONNECTOR AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800601 19991218 00601 WP 1999 12 18 AALA991580 1 19991014 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 459AA 49564 TUL - FOUND SKIN CRACKED ON EDGE OF CUTOUT FOR ANTENNA PLUG AT 380 STATION ON BELLY. INSTALLED DOUBLER PER SRM 53-04 FI G 12. (M) 2 L 7 2 4F A6WE 1999121800602 19991218 00602 WP 1999 12 18 AALA991535 1 19990924 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 182-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49258 TUL - EXFOLIATED CORROSION BELOW CABIN FLOOR AT APPROX STATION 182-200, LBL 44-55. NOTE EXFOLIATED CORROSION ABOVE CABI N FLOOR ALSO. REPAIRED CORROSION DAMAGE PER AARD 53-00-00-02 AND SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 1999121800603 19991218 00603 WP 1999 12 18 AALA991568 1 19990929 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 483 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 469AA 49599 TUL - FOUND CORROSION ON NR 6 SEAT TRACK. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999121800604 19991218 00604 NM 1999 12 18 AALA991520 1 19991008 A 5320 FORGING BOEING 727 727227 1384078 NM BS 870 CRACKING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION AND A CRACK ON THE OUTBOARD FLANGE AND INBOARD. OUTBOARD WEB OF THE LEFT BS 870 FORGING UPPER POR TION AT SPLICES ANGLES ABOVE STRINGER 96. INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 9/29/99. (M) 2 L 7 3 4F A3WE 1999121800605 19991218 00605 1999 12 18 99ZZZM803 4 19991003 A 2210 75130 SOLENOID VALVE BOEING 727 727227 1384078 NM RUDDER FAILED A AMTA H DEACTIVATE SYST/CIRCUITS F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 11 768AT 21996 IN FLT AT FL310, THE AIRCRAFT ROLLED ABRUPTLY TO THE RIGHT. AUTO PILOT DISENGATED AND TRIMMED A/C TO HOLD WINGS LEVEL A ND HOLD HEADING REQUIRED 2.2* LT RUDDER TRIM AND .5* AILERON TRIM. ON APPROACH UPPER RUDDER WENT OT NEUTRAL AND LOW RUD DER WENT HARD LEFT TO AGREE WITH TRIM KNOB. LANDED WITHOUT INCIDENT. REPLACED TRANSFER VALVE SOLENOID IN LOWER RUDDER UNIT PER MM 22-11-31, OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1999121800606 19991218 00606 NM 1999 12 18 99ZZZM804 1 19991002 A 2761 65C163001 ACTUATOR BOEING 727 727227 1384078 NM SPOILER FAILED A AMTA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 GL 11 768AT 21996 ABRUPT LEFT ROLL WHEN SPEED BRAKES APPLIED. B-SYSTEM OFF, NO ROLL. A-SYSTEM OFF, ABRUPT LEFT ROLL. LANDED WITHOUT INC IDENT. FOUND THE NR 14 SPOILER ACTUATOR BYPASSING. REPLACED ACTUATOR IAW MM 27-61-81, OPS CHECKED NORMAL, LEAK CHECKED OK. (M) 2 L 7 3 4F A3WE 1999121800607 19991218 00607 WP 1999 12 18 AALA991703 1 19991112 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROWS 3-6 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 477AA 49652 ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 3D THROUGH 6D INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT CONDUCTOR AT ROWS 3D THROUGH 6D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800608 19991218 00608 WP 1999 12 18 AALA991704 1 19991112 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 516AM 49893 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AFT OF EMERGENCY EXIT WINDOWS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800609 19991218 00609 WP 1999 12 18 AALA991711 1 19991114 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 31 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 560AA 53090 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 31 INOPERATIVE. REPLACED EMERGENCY EXIT FLO OR PATH LIGHT STRIP AT SEAT 31. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800610 19991218 00610 WP 1999 12 18 AALA991689 1 19991110 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 17/24 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 246AA 49258 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD AISLE EMERGENCY EXIT LIGHTS AT ROWS 17 AND 24 INOPERATIVE. SECURED OVERHEA D AISLE EMERGENCY EXIT LIGHT GROUND WIRES. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800611 19991218 00611 EU 1999 12 18 AALA991714 1 19991115 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 90070 513 LHR - DURING OVERNIGHT MAINTENANCE, FIRST CLASS NR 1 OVEN EMITS A STRONG BURNING ODOR. CLEANED FIRST CLASS NUMBER 1 OVE N. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999121800612 19991218 00612 WP 1999 12 18 AALA991737 1 19991117 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP AIRSTAIRS MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 586AA 53249 ORD - FLT 1105 - AFTER SHUTDOWN AT MAINTENANCE HANGAR DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHTS I LLUMINATED AND WOULD NOT TURN OFF. RESET AFT AIRSTAIR EMERGENCY EXIT LIGHT CIRCUIT BREAKERS. SYSTEM GROUND CHECK NORMA L OPERATION. (M) 2 L 7 2 4F A6WE 1999121800613 19991218 00613 WP 1999 12 18 AALA991750 1 19991120 A 3320 BV04055N0156 HOLDER BRUCE DOUG DC9 DC982 3022082 WP GALLEY DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 236AA 49251 ORD - DURING OVERNIGHT MAINTENANCE, ELECTRICAL BURNING SMELL NOTED IN THE AFT GALLEY DOOR AREA. REPLACED UPPER SIDEWALL LIGHT SOCKET IN AFT GALLEY AREA. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800614 19991218 00614 EU 1999 12 18 AALA990698 1 19990511 A 2722 30513136 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU RUDDER MALFUNCTIONED A A AALA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SW 07 7082A 2011 643 MIA - FLT 916 - DURING APPROACH AFTER GEAR EXTENSION, A/C EXPERIENCED UNCOMMANDED RUDDER INPUTS. FLT CREW DECIDED TO GO AROUND TO RESOLVE PROBLEM. YAW DAMPERS WERE CYCLED W/NO HELP AND LEFT OFF UNTIL APPROACH. DURING GO AROUND RUDDER INP UTS BECAME VIOLENT AND A/C YAWED. CREW RETURNED TO MIA. PILOT WRITE UP REPORTED RUDDER PEDALS STIFF DURING APPROACH AN D NOSE WHEEL STEERING OP'S NORM ON THE GRD. HDY PRESS AND QUANTITIES NORM DURING ENTIRE INCIDENT. ENGAGE SOLENOID IN T HE NR 1 AUTOPILOT HALF OF THE ACT FAILED TO DISENGAGE DUE TO MANF DEBRIS IN THE SOLENOID. THE FLT CONTROL COMPUTER DETE CTED FAILURE BUT COULD NOT REMOVE HYD PRESS TO THE ACT MECH. THE NR 1 PRESS S/O SOLENOID DID NOT OPERATE BECAUSE NR 1 S 2 L 7 2 4F RT A35EU 1999121800615 19991218 00615 WP 1999 12 18 AALA991692 1 19991111 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP LT MLG FAILED A AALA O OTHER N FALSE WARNING LD LANDING 1 SW 07 223AA 49173 IAD - FLT 1438 - DURING LANDING WITH GEAR HANDLE DOWN, LEFT MAIN GEAR INDICATOR NOT DOWN AND LOCKED. ACCOMPLISHED ABNOR MAL CHECKLIST. LEFT MAIN GEAR VISUALLY VERIFIED DOWN AND LOCKED. LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR DOW N LOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800616 19991218 00616 WP 1999 12 18 AALA991677 1 19991109 A 2820 7938343 TUBE DOUG DC9 DC982 3022082 WP NR 1 ENGINE LEAKING A AALA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SW 07 70404 49315 SJC - FLT 701 - AIRCRAFT ARRIVED AT GATE WITH A NR 1 ENGINE FUEL LEAK. REPLACED FUEL SYSTEM TUBE. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800617 19991218 00617 WP 1999 12 18 AALA991674 1 19991105 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 237 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 465A 49595 TUL - FOUND NR 4 CABIN TIE DOWN TRACK CORRODED AT STATION 237. CUTOUT DAMAGED AREA IN NR 4 TRACK. INSTALLED PLUG REPAI R PER SRM 53-05 FIG 6A. (M) 2 L 7 2 4F A6WE 1999121800618 19991218 00618 WP 1999 12 18 AALA991678 1 19991106 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 927-946 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 465A 49595 TUL - FOUND CORROSION AROUND LIGHTING HOLES IN LEFT CUSP BETWEEN STATION 927 TO 946. CUTOUT CORRODED SECTION OF LEFT CU SP. INSTALLED REPAIR DOUBLER PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F A6WE 1999121800619 19991218 00619 WP 1999 12 18 AALA991673 1 19991105 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 794 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 465A 49595 TUL - NR 4 CABIN TIE DOWN TRACK CORRODED AT STATION 794. CUTOUT DAMAGED SECTION OF TRACK. SPLICED IN SECTION PER SRM 5 3-05 PART 1. (M) 2 L 7 2 4F A6WE 1999121800620 19991218 00620 NM 1999 12 18 AALA991662 1 19991104 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39365 24046 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS ON BUSINESS CLASS GALLEY WALL INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT LIGHTS ON BUSINESS CLASS GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121800621 19991218 00621 WP 1999 12 18 WXOA99008 1 19991012 A 5400 CLIPS DOUG DC9 DC921 302205A WP RT PYLON CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACKS DETECTED IN TWO CLIPS ON RIGHT ENGINE LOWER APRON. REMOVED CRACKED CLIPS, FABRICATED REPAIR CLIPS PER DC-9 SRM 51-10-2 AND SAMPLE, ALODINE AND PRIMED CLIPS PER DC-9 SRM 5 1-10-3, AND INSTALLED PER DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999121800622 19991218 00622 WP 1999 12 18 WXOA99009 1 19991014 A 5320 SUPPORT DOUG DC9 DC921 302205A WP BS 786-826 CORRODED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTON AT REPAIR STATION, LEVEL 1 SURFACE CORROSION DETECTED AT THREE PLACES IN AFT R IGHT LAV FLOOR SUPPORT FRAME, STATIONS 786 TO 826, RBL PLUS/MINUS 16. REMOVED CORRODED PARTS FROM FLOOR SUPPORT FRAME. FABRICATED 2 'L' MEMBERS AND 2 FILLERS AND 1 DOUBLER PER DC-9 SRM 51-10-02 AND 53-01 FIG 2 ALODINED, PRIMERED AND FABRI CATED PER DC-9 SRM 51-10-3. INSTALLED FABRICATED REPAIR PARTS PER DC-9 SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1999121800623 19991218 00623 WP 1999 12 18 WXOA99010 1 19991014 A 5311 FRAME DOUG DC9 DC921 302205A WP BS 766 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION AT STATION 766 RIGHT SIDE, BETWEEN LON GERON 15 AND 16, DETECTED CRACK IN RADIUS AT 3RD FASTENER BELOW LONGERON 15. REMOVED DAMAGED SECTION OF FORMER, FABRICA TED REPAIR FORMER AND DOUBLER, AND INSTALLED REPAIR PARTS IAW DC-9 SRM 51-10-2, 51-10-3, 51-30-2, 51-30-5 AND 53-03 FIG 3. (M) 2 L 7 2 4F A6WE 1999121800624 19991218 00624 WP 1999 12 18 WXOA99011 1 19991014 A 5530 DUCT DOUG DC9 DC921 302205A WP VERTICAL STAB CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, VERTICAL STABILIZER AIR INTAKE DUCT AT 12 O'CLOCK POSITION HAS A CRACK APPROXIMATELY .25 INCHES LONG. REPAIRED CRACK IAW BOEING EA M-7200-99-09364. (M) 2 L 7 2 4F A6WE 1999121800625 19991218 00625 WP 1999 12 18 WXOA99012 1 19991014 A 5532 PANEL DOUG DC9 DC921 302205A WP VERTICAL STAB CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, VERTICAL STABILIZER ACCESS PANEL 3806 HAS CRACK PROPOGATIN G FROM EXISTING STOP DRILL. STOP DRILLED NEW CRACK, FABRICATED DOUBLER AND INSTALLED REPAIR DOUBLER IAW DC-9 SRM 51-10- 2, 51-10-3, 51-30-2 AND 55-01 FIG 2. (M) 2 L 7 2 4F A6WE 1999121800626 19991218 00626 WP 1999 12 18 WXOA99013 1 19991014 A 5313 LONGERON DOUG DC9 DC921 302205A WP BS 786 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED CRACK INDICATION AT LONGERON 16, FUSELAGE STATION 786 RIGHT. CRACK EVIDENT ON LONGERON AT CONNECTION POINT OF 'L' BRACKET ON AFT SIDE OF BULKHEAD. R EMOVED DAMAGED AREA OF LONGERON 16. INSTALLED REPAIR PARTS IAW DC-9 SRM 53-02 PAGE 48-52, 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1999121800627 19991218 00627 WP 1999 12 18 WXOA99014 1 19991014 A 5230 ANGLE DOUG DC9 DC921 302205A WP CARGO DOOR CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED CRACK INDICATION ON FORWARD C ARGO DOOR AT FORWARD SIDE OF LOWER AFT DOOR STOP, FORWARD SIDE OF INTERCOSTAL FITTING. REMOVED CRACKED ANGLE, FABRICATE D REPAIR ANGLE AND INSTALLED IAW DC-9 SRM 51-10-2, 51-10-3, 51-30-1 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121800628 19991218 00628 WP 1999 12 18 WXOA99015 1 19991014 A 5230 DOOR PAN DOUG DC9 DC921 302205A WP CARGO DOOR CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACK DETECTED AT PAN AND INTERCOSTAL INTERSECTION OF TOP FORWARD CORNER OF FORWARD CARGO DOOR. FABRICATED REPAIR DOUBLER, STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW DC -9 SRM 51-10-2, 51-10-3, 52-01, 52-03 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121800629 19991218 00629 WP 1999 12 18 WXOA99016 1 19991015 A 5230 ANGLE DOUG DC9 DC921 302205A WP CARGO DOOR CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION PERFORMED PER OPS 4.735 AT FORWARD CAR GO DOOR. INDICATION OF CRACK NOTED ON INTERCOSTAL ANGLE FITTING, LOCATED AFT SIDE OF LOWER FORWARD DOOR STOP. REMOVED EXISTING ANGLE AND FABRICATED REPAIR ANGLE FITTING IAW DC-9 SRM 51-10-1. APPLIED ALODINE AND PRIMER TO REPLACEMENT PART S IAW DC-9 SRM 51-10-2. INSTALLED REPAIR ANGLE PER DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1999121800630 19991218 00630 WP 1999 12 18 WXOA99017 1 19991015 A 5400 99198641 FITTING DOUG DC9 DC921 302205A WP LT PYLON CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTIN PERFORMED PER OPS 4.751 OF LEFT PYLON ' BATH TUB' FITTING. INDICATION OF CRACK NOTED AT FAIL/SAFE STRAP INBOARD UPPER RIVET. DIMENSION OF CRACK APPROXIMATELY 2.5 INCH IN LENGTH. REMOVED AND REPLACED LEFT PYLON BATH TUB FITTING PER DC-9 SRM 51-30-5 AND 51-30-1. (M) 2 L 7 2 4F A6WE 1999121800631 19991218 00631 WP 1999 12 18 WXOA99018 1 19991015 A 5542 SKIN DOUG DC9 DC921 302205A WP RUDDER DENTED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, DENT DISCOVERED ON RIGHT SIDE OF RUDDER BETWEEN RIBS 23 AN D 24, LOCATED APPROXIMATELY 18 INCH FROM TRAILING EDGE. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR EXTERNAL DOUBLER I AW DC-9 SRM 55003, PAGE 18, FIG 4. APPLIED ALODINE AND PRIMER PER DC-9 SRM 55-03, 51-30-1 AND 51-20-0. (M) 2 L 7 2 4F A6WE 1999121800632 19991218 00632 WP 1999 12 18 WXOA99019 1 19991015 A 5400 991224310 ANGLE DOUG DC9 DC921 302205A WP FS 786 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC DETECTED A CRACK ON ANGLE P/N 9912243-10 AT THE R IGHT PYLON BULKHEAD LOWER FRONT SPAR (F/S 786) EXTENDING FROM FASTENER HOLE APPROX .400 INCH LONG. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-01, 51-20-0, 51-30-5 AND MM 20-16-0. (M) 2 L 7 2 4F A6WE 1999121800633 19991218 00633 WP 1999 12 18 WXOA99020 1 19991015 A 5280 SKIN DOUG DC9 DC921 302205A WP LT MLG CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACK DETECTED AT UPPER AFT AREA OF LEFT MLG DOOR NEAR HIN GE. STOP DRILLED CRACK, INSTALLED DOUBLER P/N J060256-23 IAW SRM 52-05 AND EA HM-7200-99-09402. (M) 2 L 7 2 4F A6WE 1999121800634 19991218 00634 WP 1999 12 18 WXOA99021 1 19991015 A 5320 SHEAR TIE DOUG DC9 DC921 302205A WP BS 766 CRACKED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 MHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, NDT HFEC INSPECTION DETECTED CRACK OF APPROXIMATELY 2 INCH LONG ON SHEER CLIP BETWEEN LONGERON L15 AND L16 AT FUSELAGE STATION 766. FABRICATED REPAIR SHEER CLIP. REMOVED CRACKE D SHEER CLIP AND INSTALLED REPAIRED SHEERCLIP IAW DC-9 SRM 51-10-1, 51-10-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1999121800635 19991218 00635 WP 1999 12 18 AALA996036 1 19991104 A 2750 WHEEL DOUG DC9 DC982 3022082 WP TE FLAP OUT OF ADJUST A AALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 824RA 53017 SNA - ON TAKEOFF ROLL, TAKEOFF WARNING HORN. ABORT FLAP TAKEOFF SEL 24 DEGREES. SLAT WENT FROM TAKEOFF TO LAND RETURNE D TO GATE.. FLAPS 24 CG 11.4 STAB 8. FOUND DIAL A FLAP WHEEL ADJUSTMENT TOO SENSITIVE CAUSING FLAP MOVEMENT. ASSIGNED DMI NR 20214 ENTERED ON DMI SHEET. PLACARDED. CLEANED DEBRIS FROM DIAL A FLAP MECHANISM. OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1999121800636 19991218 00636 NM 1999 12 18 AALA991671 1 19991108 A 3350 A3060972 LIGHT BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 672AA 25337 TUL - FLT 1998 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM ROW 9 TO ROW 17 INOPERATIVE. REP LACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999121800637 19991218 00637 NM 1999 12 18 AALA991681 1 19991109 A 3350 021975 HARNESS BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 307AA 22313 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING HARNESS AT SEATS 26AB BROKEN. REPLACED EMERGENCY EXIT SEAT PATH LIGHTING HARNESS AT SEAT 26AB. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121800638 19991218 00638 EU 1999 12 18 AALA991713 1 19991112 A 2120 6451101 FAN FOKKER F28 F28MK0100 4990807 EU ACM BAY FAILED A AALA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1449D 11458 DFW - FLT 458 - AFTER TAKEOFF FROM DFW, DURING CLIMB-OUT, ELECTRICAL BURNING SMELL NOTICED IN COCKPIT AND CABIN. EMERGE NCY DECLARED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED PACK RECIRCULATING FAN. SYSTEM GROUND CH ECK NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999121800639 19991218 00639 EU 1999 12 18 AALA991695 1 19991110 A 3230 FPTN304758R3 SENSOR ELDEC AIRBUS 300 A300B4605R 3930308 EU LT MLG FAILED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 11060 470 MIA - FLT 881 - ON FINAL MIA, UNABLE TO EXTEND LANDING GEAR HYDRAULICALLY. EXTENDED LANDING GEAR MANUALLY AND LANDED MI A WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999121800640 19991218 00640 NM 1999 12 18 AALA991687 1 19991109 A 3350 CONNECTOR BOEING 767 767323 1385205 NM SEAT 28H FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379AA 25448 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 28H EMERGENCY EXIT FLOOR PATH LIGHT WAS INOPERATIVE. REPLACED EMERGENCY EXIT F LOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121800641 19991218 00641 NM 1999 12 18 AALA991690 1 19991112 A 3350 1000679 LIGHT BOEING 767 767223 1385123 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 323AA 22324 ORD - FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY. SYSTE M GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121800642 19991218 00642 NM 1999 12 18 AALA991710 1 19991114 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAULTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 619AA 24577 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT NEAR AFT LAVATORY INOPERATIVE. REPLACED FAULTY WIRE FROM 4R DO OR TO THE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999121800643 19991218 00643 NM 1999 12 18 AALA991709 1 19991114 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 34H INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY EXIT SEAT LIGHT AT SEAT 34H. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121800644 19991218 00644 NM 1999 12 18 AALA991708 1 19991113 A 3350 CONTACT BOEING 767 767323 1385205 NM EXIT LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361AA 24042 DFW - DURING OVERNIGHT MAINTENANCE, 1L DOOR JAM EMERGENCY EXIT LIGHT FAILED LIGHT TEST. CLEANED BULB CONTACT. SYSTEM G RUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999121800645 19991218 00645 NM 1999 12 18 AALA991706 1 19991112 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 638AA 24596 LAX - DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTS INOPERATIVE. REPAIRED WIRE ON 4L DOOR E MERGENCY EXIT SIGN. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999121800646 19991218 00646 WP 1999 12 18 AALA991701 1 19991111 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 27D BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 513AA 49890 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROW 27D INOPERATIVE. REPLACED EMERGENCY EXIT PAT H LIGHT STRIP AT SEAT ROW 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800647 19991218 00647 WP 1999 12 18 AALA991702 1 19991112 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 25D FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 494AA 49732 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 25D THROUGH 28D INOPERATIVE. REPAIRED EMERG ENCY EXIT FLOOR PATH LIGHT AT ROWS 25D. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999121800648 19991218 00648 SO 1999 12 18 ASOA99155 1 19991118 A 3350 1317 BULB EMB 120 EMB120RT SO FUSELAGE FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 273AS 120222 DURING INSPECTION, FOUND AFT OUTSIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800649 19991218 00649 SO 1999 12 18 ASOA99141 1 19991104 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 266AS 120188 DURING INSPECTION, FOUND NR 3 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY BATTERY. OPE RATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800650 19991218 00650 SO 1999 12 18 ASOA99142 1 19991105 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 261AS 120141 DURING INSPECTION, FOUND NR 1 AND 2 EMERGENCY BATTERY PACKS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND 2 EMERGENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800651 19991218 00651 SO 1999 12 18 ASOA99143 1 19991105 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 243AS 120072 DURING INSPECTION, FOUND NR 1 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY B ATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800652 19991218 00652 SO 1999 12 18 ASOA99144 1 19991106 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 242AS 25949 120069 DURING INSPECTION, FOUND NR 1 EMERGENCY BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY. O PERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800653 19991218 00653 SO 1999 12 18 ASOA99145 1 19991106 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR LOOSE A ASOA I CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 SO 11 269AS 120210 FLT 4003 - WHILE CRUISING AT 15,000 FT, THE FLIGHT ATTENDANT REPORTED A HISSING SOUND COMING FROM THE AFT BULKHEAD AREA. FIVE MINUTES LATER, THE CABIN DEPRESSURIZED. CREW COMPLETED THE EMERGENCY PROCEDURES AND LEVELED OFF AT 10,000 FEET, WHILE THE CABIN CLIMBED TO 8.000. AIRCRAFT PROCEEDED TO ABY AND SAFELY LANDED. MAINTENANCE RESECURED CARGO DOOR SEAL I AW EMB120MM 52-30. PRESSURIZATION AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800654 19991218 00654 SO 1999 12 18 ASOA99146 1 19991106 A 2120 EVAC2322C2 COOLING FAN EMB 120 EMB120RT SO ACM BAY INOPERATIVE A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 246AS 19839 120100 FLT 4028 - AFTER TAKEOFF, CREW SMELLED SOMETHING BURNING. CAPTAIN TURNED AUTOPILOT ON AND TURNED ON COCKPIT READING LIG HTS AND SAW THIN WHITE SMOKE. F/A REPORTED BURNING SMELL, BUT SAW NO SMOKE IN CABIN AFTER INSPECTION. CREW UNABLE TO I DENTIFY SOURCE OF BURNING SMELL. CAPTAIN TURNED RECIRCULATING AND GASPER FANS OFF AND CLOSED EYEBALL VENTS. CREW DECLA RED EMERGENCY AND RETURNED TO ATL WHERE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK GROUND C OOLING FAN. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800655 19991218 00655 SO 1999 12 18 ASOA99147 1 19991108 A 6120 78249046 PCU EMB 120 EMB120RT SO RT ENGINE INOPERATIVE A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 285AS 22692 120265 IN CLIMB-OUT, CREW NOTICED RIGHT NP BEGAN SHOWING OUT OF LIMITS. NP THEN BEGAN TO SURGE AND FLUCTUATE UP TO APPROXIMATE LY 102 PERCENT. CREW FOLLOWED QRH PROCEDURES, WHICH REQUIRED FEATHERING RIGHT PROPELLER. CREW DECLARED EMERGENCY, DIVE RTED TO AGS, AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE PCU IAW EMB120 MM 61-00-00. LEAK AND OPE RATIONAL CHECKS WERE GOOD ON GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800656 19991218 00656 1999 12 18 RU3A99012 4 19991118 A 3425 80956861001 INDICATOR BEECH 300 300BEECH 1152930 CE EFHSI INOPERATIVE A RU3A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 83 FF18 THE CREW REPORTED THE PILOTS EFHSI IND FLICKERED THEN TURNED OFF WITH THE SMELL OF ELECTRICAL SMOKE JUST BEFORE IT WENT OUT. TRIED TO COPY TO THE CO-PILOTS EFHSI AND THE SAME PROBLEM OCCURRED. REPLACED THE PILOTS EFHSI AND THE SYSTEM CHEC KED FINE ON THE GROUND. THE A/C WAS RELEASED, DURING A/C ROLL FOR T/O THE PILOTS EFHSI AGAIN FLICKERED AND REDUCED IN S IZE HORIZONTALLY TO THE RT HALF OF THE DISPLAY. COPY DOWN WAS THE SAME DISPLAY. THE CO-PILOTS EFHSI WAS OK. THE CREW CONTINUED ON TO BTL. THIS PROBLEM DOESN'T APPEAR RELATED TO THE ONE DETAILED IN ARR BN 29-7, WHICH CONCERNED THE CO-PIL OTS EFHSI. AVIONICS BELIEVES THIS PROBLEM TO BE POSSIBLY A SYMBOL GENERATOR OR WIRING PROBLEM. THE SYMBOL GENERATOR WA 2 L 7 2 4T A24CE 1999121800657 19991218 00657 EU 1999 12 18 UF6A991109 1 19991122 A 7740 636044004 NP GAUGE BAG ATP ATP EU COCKPIT FAILED A UF6A O OTHER O OTHER NR NOT REPORTED 1 GL 31 858AW 16127 2035 ORD - FLT 5723 - THE NR 1 NP GAUGE IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE GAUGE. SYSTEM OPS CHECKED GOOD . (M) 2 L 7 2 4T RT A27NM 1999121800658 19991218 00658 NE 1999 12 18 99ZZZM805 2 19991006 A 7530 C8E389 CONTROL BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE FAILED A N8TA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 19 757NA 24567 30721 DURING TRANSITION FROM HIGH CLIMB POWER TO CRUISE POWER LT ENGINE APPEARED TO SURGE. ALL ENGINE INDICATIONS WERE NORMAL PRIOR TO AND AFTER SURGE EVENT. REMOVED BLVL CONTROL C8E38-9 AND INSTALLED BLVL CONTROL C8E38-12, OPERATIONAL CHECK NO RMAL. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1999121800659 19991218 00659 EA 1999 12 18 UHLA991087 1 19991014 A 3350 82410162003 LIGHT DHAV DHC8 DHC8311 1386006 EA COCKPIT INOPERATIVE A UHLA K NONE L NO TEST IN INSP/MAINT 1 NE 03 803SA 15947 221 ISP-TNN - DURING PREFLIGHT, UNABLE TO ACTIVATE EMERGENCY LIGHTS FROM COCKPIT OR FLIGHT ATTENDANT PANEL. FERRIED AIRCRAF T TO BUF. REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROLLER, OPS CHECKS GOOD. (M) 2 H 7 2 4T RT A13NM 1999121800660 19991218 00660 NE 1999 12 18 99ZZZM806 2 19991015 A 7250 TURBINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A JJBA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 01 835CA 12128 UE30 114060 RIGHT ENGINE POWER LOSS ON TAKEOFF ROLL PRIOR TO FULL POWER. TAKEOFF ABORTED WITHOUT INCIDENT. LOUD 'BANG' HEARD BY CR EW PRIOR TO POWER LOSS. ENGINE WAS REMOVED AND REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999121800661 19991218 00661 NM 1999 12 18 99ZZZM807 1 19991026 A 3260 189929 SENSOR BOEING 737 7372Y5 1384554 NM LT MLG UPLOCK INTERMITTENT A TSAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 810AL 24031 FLT 101 - OGG-HNL - LEFT MAIN GEAR RED UNSAFE GEAR LIGHT COMES ON INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED UP LOCK SENSOR LEFT GEAR PER MM 32-61-21 AND ALSO CHECKED UPLOCK MECHANISM PER MM 32-32-31. ALL OK, OPS OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1999121800662 19991218 00662 SO 1999 12 18 C2XA99IA554 1 19991012 A 5411 120540036KIT FRAME EMB 120 EMB120RT SO NR 1 NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT ENGINE NACELLE NR 1 FRAME CRACKED. REMOVED AND REPLACED NR 1 FRAME IAW SB 120-54-0036 AND EC5410-01034. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800663 19991218 00663 SO 1999 12 18 C2XA99IA552 1 19991012 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT SO FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM CORRODED AT FRAME 36. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE (M) 2 L 7 2 4T RT A31SO 1999121800664 19991218 00664 SO 1999 12 18 C2XA99IA551 1 19991012 A 5320 12006962001 CROSSBEAM EMB 120 EMB120RT SO FRAME 16 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800665 19991218 00665 SO 1999 12 18 C2XA99IA550 1 19991012 A 5330 12019230003 SKIN EMB 120 EMB120RT SO FUSELAGE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE SKIN WORN INTO BY SCREWS FROM PANELS 191 AND 192. FABRICATED R EPAIR DOUBLER AND INSTALLED IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800666 19991218 00666 SO 1999 12 18 C2XA99IA549 1 19991012 A 5320 12046963001 BUTTSTRAP EMB 120 EMB120RT SO FRAME 14-21 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE, LT BUTTSTRAP CORRODED BETWEEN FRAMES 14 AND 21. REMOVED CORRO DED SECTION OF BUTTSTRAP AND SPLICED IN NEW SECTION IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800667 19991218 00667 SO 1999 12 18 C2XA99IA548 1 19991012 A 5320 12007089603 BUTT STRAP EMB 120 EMB120RT SO FRAME 13-16 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CENTER BUTT STRAP CORRODED BETWEEN FRAMES 13 AND 16. REMOVED A ND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999121800668 19991218 00668 NM 1999 12 18 GAIA99211A 1 19991126 A 2612 652244421 DUCT BOEING 727 7272J0 138407E NM NR 1 ENGINE RUPTURED A GAIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 281KH 21105 DURING CLIMB-OUT FROM TOL, HAD A NR 1 ENGINE FIRE WARNING. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANED WITHOUT FURTHER PROBLEMS. FOUND THE 8TH STAGE BLEED AIR SUPPLY DUCT RUPTURED. ALSO, FOUND A PIECE OF TH E DUCT STUCK IN THE THROTTLE LINKAGE. REMOVED AND REPLACED THE 8TH STAGE BLEED AIR SUPPLY DUCT. RAN ENGINE, OPERATIONA LLY CHECKED THE THROTTLE, AND LEAK CHECKED THE THROTTLE, AND LEAK CHECKED THE NEW DUCT. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 1999121800669 19991218 00669 WP 1999 12 18 GAIA99210 1 19991119 A 3260 H146 SWITCH DOUG DC9 DC915F 3022037 WP LT MLG LOOSE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 561PC 47014 FLT 805 - DEN-SLC - AFTER TAKEOFF, THE LEFT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. THE FLIGHT CREW ELE CTED TO RETURN TO DEN. AN UNEVENTFUL LANDING WAS MADE. INSPECTION FOUND THE LEFT GEAR UPLOCK SWITCH SPACER BOLT AND NU T MISSING. THE MISSING HARDWARE WAS REPLACED AND THE SYSTEM OPERATIONAL CHECK WAS PERFORMED PER THE DC-9 MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999121800670 19991218 00670 WP 1999 12 18 HALA9900225 1 19991117 A 3231 CONTROL CABLE DOUG DC9 DC951 3022051 WP NLG DOOR FAILED A HALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 13 649HA 47715 FLT 103 - HNL - AIR TURN BACK, UPON GEAR RETRACTION LOUD VIBRATION FROM NOSE WHEEL AREA, DID NOT STOP TILL GEAR WAS EXTE NDED. FOUND RT NOSE GEAR FORWARD DOOR ASSIST CABLE AND ACT BROKEN, HA 3472. REPLACED DOOR ACT AND CABLE ASSY PER MM 32 -22-1. OPS CHECK GOOD. GEAR WING CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999121800671 19991218 00671 EA 1999 12 18 MASA99169 1 19991021 A 2780 WARNING LIGHT CNDAIR CL600 CL6002B19 EA COCKPIT ILLUMINATED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 77195 7195 FLT 5766 - SWF-PHL - THE AIRCRAFT RETURNED TO THE FIELD SHORTLY AFTER TAKEOFF DUE TO A SPOILER FAULT MESSAGE DURING TAKE OFF ROLL. MAINTENANCE DEPOWERED AND REPOWERED THE AIRCRAFT AND PERFORMED AN OPS CHECK OF THE SYSTEM AND FOUND NO DEFECT S OR FAILURES IN THE SYSTEM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999121800672 19991218 00672 EA 1999 12 18 MASA99168 1 19991014 A 5270 SWITCH CNDAIR CL600 CL6002B19 EA CARGO DOOR MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 77302 7302 FLT 6009 - PHX-DSM - AFTER TAKEOFF, THE AIRCRAFT RETURNED TO THE FIELD DUE TO A CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATIN G. THERE WAS NO LOSS OF CABIN PRESSURIZATION. MAINTENANCE INSPECTED AND THE ITEM WAS DEFERRED PER MEL NR 52704. THE A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999121800673 19991218 00673 NM 1999 12 18 MZZA99189 1 19990928 A 3270 65579348 FITTING BOEING 727 727232 1384082 NM TAIL SKID CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON TAIL SKID ACTUATOR RIGHT HINGE ARM INBOARD SUPPORT BRACKET IN TAIL SKID BAY. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW (P/N 65-57934-8) PER B727 SR M CHAPTER 51-10-01, 51-30-02. (M) 2 L 7 3 4F A3WE 1999121800674 19991218 00674 NM 1999 12 18 MZZA99190 1 19991011 A 3270 652561411 FITTING BOEING 727 727232 1384082 NM TAIL SKID CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON TAIL SKID DRAG LEFT HINGE FITTING I N TAIL SKID BAY. THE CORRODED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-25614-11) PER B727 SRM CHAPTER 51 -10-01 AND 51-30-02. (M) 2 L 7 3 4F A3WE 1999121800675 19991218 00675 NM 1999 12 18 MZZA99191 1 19990929 A 5210 SKIN BOEING 727 727232 1384082 NM PAX DOOR DAMAGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH BY 1 INCH AREA DAMAGE WAS FOUND ON L2 CABIN DOOR SKI N FORWARD LOWER CORNER. THE DAMAGED AREA WAS TRIMMED AND REPAIRED PER B727 SRM CHAP 52-40-02. (M) 2 L 7 3 4F A3WE 1999121800676 19991218 00676 NM 1999 12 18 MZZA99192 1 19990923 A 5230 SKIN BOEING 727 727232 1384082 NM CARGO DOOR CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH LONG IG CORROSION WAS FOUND ON NR 3 CARGO DOOR FORWA RD EDGE BETWEEN NR 3 AND NR 4 STOP FITTING. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-0 3 FIG 1. (M) 2 L 7 3 4F A3WE 1999121800677 19991218 00677 NM 1999 12 18 MZZA99193 1 19990923 A 5230 65577686 FITTING BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AIR ASIA, CRACK WAS FOUND ON C3 DOOR FORWARD LOWER CORNER STOP FITTING. TH E DAMAGED STOP FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-57768-6) PER CMI EA NR 5230-0185. (M) 2 L 7 3 4F A3WE 1999121800678 19991218 00678 NM 1999 12 18 MZZA99194 1 19991006 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .625 INCH LONG CRACK WAS FOUND ON BS 1183 BULKHEAD WEB FORWAR D SIDE REINFORCEMENT BEAM OUTBOARD FLANGE AT LBL 37 AND WL 250. THE DAMAGED SECTION WAS REPAIRED PER CMI EC/RA NR 5310- 03930 USING KIT NR 65C34406-12 AND DWG 65C34406. (M) 2 L 7 3 4F A3WE 1999121800679 19991218 00679 NM 1999 12 18 MZZA99195 1 19991006 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.125 INCH LONG CRACK WAS FOUND ON BS 1183 BULKHEAD WEB FORWA RD SIDE REINFORCEMENT BEAM INBOARD FLANGE AT LBL 36 AND WL 250. THE CORRODED SECTION WAS REPAIRED PER CMI EC/RA NR 5310 -03930 USING KIT NR 65C34406-12 AND DWG NR 65C34406. (M) 2 L 7 3 4F A3WE 1999121800684 19991218 00684 CE 1999 12 18 99ZZZX4606 1 19991008 A 8120 4709449013 WASTEGATE CESSNA 402 402C 207590R CE RT ENGINE LACK OF LUBE A GULC C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NE 01 407BK CC1983 402C0238 THE RIGHT ENGINE DID NOT DEVELOP FULL POWER FOR TAKEOFF. INSPECTED ENGINE AND CONTROLLER AND WASTEGATE. LUBED WASTEGAT E VALVE SHAFT. GROUND RUN-UP CHECKED GOOD. NO OCCURRENCE SINCE THEN. 1 L 7 2 3O A7CE 1999121800686 19991218 00686 NE 1999 12 18 GXPA99007 2 19991122 A 7321 FCU AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE NR 1 ENGINE OUT OF ADJUST A GXPA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 614GA 6891 3914 94 304369B NR 1 ENGINE FLAMED OUT AT ALTITUDE. FLAMED OUT ABOVE 29,000 FEET. ADJUSTED FUEL DENSITY, GROUND RUN AND TEST FLIGHT. C HECKED GOOD. (X) 2 L 7 2 4F 4 F RT A7EU E7EA 1999121800687 19991218 00687 CE 1999 12 18 99ZZZX4608 1 19991129 A 5210 9942002457 HINGE BEECH 99 99A 1154003 CE PASSENGER DOOR CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 955AA U128 CREW DOOR MISALIGNED WHEN PILOT ATTEMPTED TO SECURE. INSPECTION REVEALED FORWARD HINGE CRACKED AT HINGE PIN REGION. HI NGE HALF WAS REPLACED WITH SERVICEABLE HINGE HALF. AN INFORMAL INSPECTION OF ALL COMPANY AIRCRAFT RESULTED IN NO OTHER DISCREPANCIES. 1 L 7 2 3T A14CE 1999121800688 19991218 00688 SW 1999 12 18 GXPA99006 1 19991115 A 3240 212033 BRAKE BFGOODRICH SWRNGN SA226 SA226AT 8780405 SW LT MLG SEIZED A GXPA O OTHER O OTHER LD LANDING 1 GL 23 615GA AT009 AIRCRAFT DEPARTED SDF EN ROUTE TO S24 (SANDUSKY COUNTRY REGIONAL). UPON LANDING, LEFT BRAKES WERE LOCKED CAUSING BOTH L EFT WHEEL ASSEMBLIES TO SKID AND CAUSE AIRCRAFT TO RUN OFF RUNWAY ON LEFT SIDE. WATER APPEARS TO HAVE ENTERED BRAKES AN D FROZE CAUSING BRAKES TO SEIZE. (X) 2 L 7 2 4T RT A5SW 1999121800705 19991218 00705 SO 1999 12 18 COMA9910183 1 19991211 A 2731 ATG120TR SENSOR EMB 120 EMB120RT SO ELEVATOR OUT OF ADJUST A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 269CA 120263 TRIM WARNING DURING TAKEOFF. ADJUSTED THE ELEVATOR TRIM PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1999121800706 19991218 00706 SO 1999 12 18 COMA9910184 1 19991214 A 3060 SM600BA60N1 RCCB EMB 120 EMB120RT SO COCKPIT FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 247CA 120225 RIGHT HAND PROPELLER DEICE FAIL WARNING. REPLACED RCCB (CB0226). 2 L 7 2 4T RT A31SO 1999121800707 19991218 00707 SO 1999 12 18 COMA9910185 1 19991214 A 3350 3071BPEGPL LAMP EMB 120 EMB120RT SO GALLEY FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 463CA 120267 EMERGENCY LIGHTS INOP. FOUND ONLY ONE LAMP INOP. REPLACED FLOOR PATH LIGHT BULB AT GALLEY AREA. ALL EMERGENCY LIGHTS OPERATE NORMAL. 2 L 7 2 4T RT A31SO 1999121800708 19991218 00708 SO 1999 12 18 COMA9910186 1 19991206 A 3241 21585 BRAKE ROTOR EMB 120 EMB120RT SO MLG BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 20868 120247 LEFT INBOARD BRAKE MAKING LOUD NOISE DURING TOWING. FOUND BRAKE ROTOR BROKEN, LEFT INBOARD BRAKE. INSTALLED SERVICEABL E BRAKE. 2 L 7 2 4T RT A31SO 1999121800709 19991218 00709 1999 12 18 COMA9910187 3 19991216 A 6111 RFC11016A BLADE EMB 120 EMB120RT SO RT PROPELLER DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 21304 120259 FOUND NR 4 BLADE RIGHT PROP HAD TIP DAMAGE. REMOVED AND REPLACED NR 4 BLADE RIGHT PROP. 2 L 7 2 4T RT A31SO 1999121800710 19991218 00710 NE 1999 12 18 COMA9960764 2 19991214 A 7261 FILTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE OIL SYSTEM CLOGGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 948CA 7079 807316 RIGHT HAND ENGINE OIL PRESSURE AT 130 PSI. REPLACED CLOGGED OIL FILTER, AND CLEANED THE OIL PUMP SCAVENGE SCREENS. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800711 19991218 00711 EA 1999 12 18 COMA9960765 1 19991213 A 3020 12681 SWITCH CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 966CA 8461 7132 RIGHT HAND ENGINE COWL ANTI-ICE CAUTION MESSAGE. REPLACED COWL ANTI-ICE SWITCH. 2 L 7 2 4F RT A21EA 1999121800712 19991218 00712 EA 1999 12 18 COMA9960766 1 19991213 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 971CA 7145 PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1999121800713 19991218 00713 EU 1999 12 18 QXEA9902596 1 19991209 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 PDX- FORWARD OVERHEAD EXIT SIGN ABOVE GALLEY HAS MOST 28V LAMPS INOPERATIVE. REMOVED AND REPLACED GALLEY OVERHEAD EMERG ENCY EXIT SIGN CIRCUIT BOARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1999121800714 19991218 00714 EU 1999 12 18 QXEA9902598 1 19991214 A 3350 551590004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 SEA- TRIM FELL OFF AROUND EMERGENCY EXIT SIGN IN GALLEY. REPLACED CIRCUIT BOARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1999121800715 19991218 00715 WP 1999 12 18 ABXA9900838 1 19991116 A 5220 99577355 BRACKET DOUG DOUG DC9 DC932F 3022067 WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND INTERIOR BRACKET IN LOWER LEFT CORNER OF THE RIGHT FORWARD EMERGENCY EXIT DOOR CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1999121800716 19991218 00716 WP 1999 12 18 ABXA9900839 1 19991116 A 5315 9958190501 FLOORBEAM DOUG DOUG DC9 DC932F 3022067 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-DHECK, FOUND LEFT FLOORBEAM CRACKED AT STATION 737 OUTBOARD LOWER FLANGE. REPAIRED IAW ABX REA D953-34148-MR. 2 L 7 2 4F A6WE 1999121800717 19991218 00717 WP 1999 12 18 ABXA9900840 1 19991116 A 5320 991015164 CUSP DOUG DOUG DC9 DC932F 3022067 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND RIGHT CUSP WEB CRACKED AT STATION 617. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999121800718 19991218 00718 WP 1999 12 18 ABXA9900841 1 19991116 A 5315 9922047501 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 579 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FLOOR SUPPORT FITTING AT STATION 579 AND LONGERON 23 LEFT CRACKED. REPLACED FITTING IAW DC9 SRM 5 1-30-5. 2 L 7 2 4F A6WE 1999121800719 19991218 00719 WP 1999 12 18 MWEA99898 1 19991213 A 3260 833702 SENSOR DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 808ME 48070 AFTER DEPARTURE AT SLAT RETRACT, THE STALL INDICATION FAILURE ANNUNCIATOR CAME ON. MTC REMOVED AND REPLACED RIGHT GEAR WOW SENSOR. 2 L 7 2 4F A6WE 1999121800720 19991218 00720 WP 1999 12 18 MWEA99899 1 19991214 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 FOUND EMERGENCY LIGHTS IN AFT ACCESSORY COMPARTMENT ARE DIM. MAINTENANCE REPLACED THE AFT ACCESSORY COMPARTMENT LIGHTS BATTERY PACK. 2 L 7 2 4F A6WE 1999121800721 19991218 00721 NM 1999 12 18 SCNA99764 1 19991007 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, LEFT FORWARD OVERWING EXIT, LOWER RIGHT EMERGENCY EXIT LIGHT INOP. RELAMPED IAW B727 MM 3350121, OPS CK NORMAL IAW B727 MM 3350121. 2 L 7 3 4F A3WE 1999121800722 19991218 00722 NM 1999 12 18 SCNA99765 1 19991007 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, EMERGENCY EXIT LIGHT AT LOWER LEFT R1 DOOR INOP. RELAMPED IAW B727 MM 3350121, OPS CHEC K NORMAL IAW B727 MM3350121. 2 L 7 3 4F A3WE 1999121800723 19991218 00723 NM 1999 12 18 SCNA99766 1 19991007 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, RIGHT FORWARD OVERWING EXIT, LOWER LEFT EMERGENCY EXIT LIGHT INOP. RELAMPED IAW B727 MM 3350121, OPS CHECK NORMAL IAW B727 MM 3350121. 2 L 7 3 4F A3WE 1999121800724 19991218 00724 NM 1999 12 18 SCNA99767 1 19991007 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, EMERGENCY EXIT LIGHT AT LOWER RIGHT L1 DOOR INOP. RELAMPED IAW B727 MM 3350121, OPS CHE CK NORMAL IAW B727 MM 3350121. 2 L 7 3 4F A3WE 1999121800725 19991218 00725 NM 1999 12 18 SCNA99768 1 19991007 A 5320 ANGLE BOEING 727 7272M7 138407S NM BS 166 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, STA 166 GILLINER AFT BULKHEAD SUPPORT L ANGLE WAS CORRODED OUT OF LIMITS AT LBL 36 AND A TTACH POINT TOP LOWER L ANGLE. REMOVED L ANGLE IAW B727 SRM 513002. FABRICATED NEW ANGLE PER SAMPLE FROM AND 101401024 AND 7075 T6 .026. TREATED AND PRIMED IAW SRM 511002, MM 512002. INSTALLED IAW SRM 513002. 2 L 7 3 4F A3WE 1999121800726 19991218 00726 NM 1999 12 18 SCNA99769 1 19991010 A 5313 STRINGER BOEING 727 7272M7 138407S NM BS 620 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, FORWARD CARGO PIT FS 620, STR 27R HAD CORROSION OUT OF LIMITS ON I/B FLANGE AT PREVIOUS REPAIR. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED STRINGER REPAIR FROM BAC 1498147 IAW B727 SRM 531003. TREAT ED AND PRIMED IAW B727 SRM 511022 MM 512002. INSTALLED REPAIR IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1999121800727 19991218 00727 NM 1999 12 18 SCNA99770 1 19991016 A 5320 ANGLE BOEING 727 7272M7 138407S NM BS 700 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT APPROX BETWEEN FS 700 AND 804 LBL 10 JUST FWD OF AI R CONDITION COMPARTMENT ON PANEL INSTL ANGLE. REMOVED CORROSION IAW SRM 511006. ROUTED OUT DAMAGE AND FABRICATED 2 ANG LES AND 1 FILLER FROM BAC 14902865 IAW SRM 514003. TREATED AND PRIMED IAW MM 512002 AND SRM 511002. INSTALLED REPAIR I AW SRM 514003 AND 513002. 2 L 7 3 4F A3WE 1999121800728 19991218 00728 NM 1999 12 18 SCNA99771 1 19991011 A 5320 SHEAR TIE BOEING 727 7272M7 138407S NM BS 720E CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT FORWARD PIT RIGHT STRINGER, BETWEEN 26 AND 27 SHEAR TIE AT BS 720E. REMOVED CORROSION IAW SRM 511006. REMOVED CORRODED SHEAR TIE IAW SRM 513002. FABRICATED SHEAR TIE FR OM ALC 2024 T3 PER SAMPLE. TREATED AND PRIMED IAW 511002 AND MM 512002. 2 L 7 3 4F A3WE 1999121800729 19991218 00729 NM 1999 12 18 SCNA99773 1 19991007 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, THE EMERGENCY LIGHT ON AFT CARGO DOOR WAS FOUND INOP. REPAIRED AND REPLACED BATTERY PAC K. 2 L 7 3 4F A3WE 1999121800730 19991218 00730 NM 1999 12 18 SCNA99772 1 19991005 A 5320 SHEAR TIE BOEING 727 7272M7 138407S NM BS 302 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT SHEAR TIE IN THE NOSE LANDING GEAR WHEEL WELL BS 30 2 LBL 16 LWR FRAME AT SKIN ATTACHMENT INSIDE CUTOUT. TRIMMED OUT DAMAGED AREA AND FABRICATED DOUBLER FROM 0.050 7075 T6 IAW SRM 514002. TREATED AND PRIMED AREA AND DOUBLER IAW SRM 511002 AND MM 512002. INSTALLED REPAIR IAW SRM 514002 AND 513002. 2 L 7 3 4F A3WE 1999121800731 19991218 00731 NM 1999 12 18 SCNA99774 1 19991007 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, R2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999121800732 19991218 00732 NM 1999 12 18 SCNA99775 1 19991007 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, L2 DOOR EMERGENCY EXIT LIGHT OVER DOOR INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999121800733 19991218 00733 NM 1999 12 18 SCNA99776 1 19991007 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, L2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999121800734 19991218 00734 NM 1999 12 18 SCNA99763 1 19991206 A 3350 6013211 BATTERY PACK BOEING 727 7272M7 138407S NM BATTERY PACK DISCHARGED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 294SC 21202 DURING HEAVY MAINTENANCE CHECK, EMERGENCY LIGHT BATTERY PACK M9802 WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK I AW B727 MM 335023. OPS CHECK NORMAL IAW B727 MM 335023. 2 L 7 3 4F A3WE 1999121800735 19991218 00735 1999 12 18 RAIA9912016 4 19991213 A 3420 258719343 GYRO BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 430AM 16198 474 880 7045-STL- CAPTAINS RMI AND FIRST OFFICERS HSI FAILED DURING TAXI. MAINTENANCE REPLACED NR 2 DIRECTIONAL GYRO. 2 L 7 2 4T RT A56EU 1999121800736 19991218 00736 WP 1999 12 18 RAIA9912017 2 19991213 A 7321 89737525 FCU BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CE 03 423AM 2633 2633 858 7071-STL- RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT ENGINE FUEL CONTROL. 2 L 7 2 4T 4 T RT A56EU E4WE 1999121800737 19991218 00737 EU 1999 12 18 RAIA9912018 1 19991214 A 3230 00A702956 O-RING BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 427AM 876 7322-STL- LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPLACED NOSE LANDING GEAR SCHRADER VALVE O-RING. 2 L 7 2 4T RT A56EU 1999121800738 19991218 00738 CE 1999 12 18 CA991007064 1 19990924 A 3310 CIRCUIT BOARD TFM138 CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE LIGHTING PANEL MELTED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA F0249 PCE76344 (CAN) THE LIGHTING CIRCUIT BOARD MELTED ON THE FM RT. DISCUSSIONS WITH THE OPERATOR AND MANUFACTURER REVEALED NO OTHER F AILURES SUCH AS THIS. THERE IS A NEW PART P/N 983378-1 FROM TECHTRONICS. 1 L 7 2 4F 4 F A22CE E1NE 1999121800739 19991218 00739 NM 1999 12 18 CA991103003 1 19991024 A 2910 82970010561 LINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123124 901161 (CAN) WHILE INVESTIGATING A HYDRAULIC LEAK IN THE NR 2 ENGINE NACELLE AREA, MAINTENANCE FOUND A DAMAGED FLARE ON THE HYD RAULIC LINE TO THE SPOILER UNLOADING VALVE. THE LINE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800740 19991218 00740 EA 1999 12 18 CA991103004 1 19991108 A 3250 87005 ECU DOWTY 8700 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NLG STEERING FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 32530 85088 123113 901009 (CAN) DURING TAXI, THE CREW FOUND THE NOSE GEAR STEERING PULLING TO THE LEFT, REQUIRING RIGHT TILLER INPUT TO KEEP THE A IRCRAFT STRAIGHT. MAINTENANCE FOUND THE NOSE GEAR STEERING ELECTRONIC CONTROL UNIT WOULD NOT RESPOND TO A BITE TEST. T HE ECU WAS REPLACED, 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800741 19991218 00741 EA 1999 12 18 CA991103005 1 19991025 A 3510 90070003659 O2 MASK SCOTT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE COCKPIT FAILED W K NONE L J NO TEST WARNING INDICATION IN INSP/MAINT 1 CA 9680 12 181 123113 901009 (CAN) DURING PRE-FLIGHT TEST, THE CAPTAIN'S OXYGEN MASK INDICATED FLOW WARNING. MASK REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800742 19991218 00742 EA 1999 12 18 CA991103006 1 19991025 A 2611 3023143 SMOKE DETECTOR KIDDE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CARGO BAY MALFUNCTIONED W O OTHER N FALSE WARNING CR CRUISE 1 CA 16734 10966 0149 123113 901009 (CAN) CREW REPORTED INTERMITTENT WARNING SYSTEM INDICATION OF THE BAGGAGE COMPARTMENT SMOKE WARNING. MAINTENANCE SUGGES TED POSSIBLE IMPACT DAMAGE. SMOKE DETECTOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800743 19991218 00743 NM 1999 12 18 CA991103008 1 19991025 A 2841 10013000002 INDICATOR SIMMONDS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL QUANTITY FLUCTUATED W O OTHER O OTHER CR CRUISE 1 CA 19007 206 228 120854 890709 (CAN) FLIGHT CREW REPORTED THAT THE NR 1 FUEL GAUGE WAS INTERMITTENTLY INDICATING 400 TO 500 POUNDS HIGH. MAINTENANCE R EPLACED THE GAUGE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800744 19991218 00744 EA 1999 12 18 CA991103010 1 19991028 A 3010 8SC0029029 DEICE BOOT 85720063003 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE WING SPLIT W K NONE L NO TEST IN INSP/MAINT 1 CA 3055 0050012 123133 920528 (CAN) FLIGHT CREW REPORTED THE DEICE BOOT OUTBOARD OF THE NR 1 ENGINE WAS INOPERABLE. THE DEICE BOOT HAD ONE SPLIT INFL ATION TUBE. THE LEADING EDGE ASSY WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800745 19991218 00745 EA 1999 12 18 CA991103021 1 19991020 A 3233 DSC252B40124 HOSE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE MLG ACTUATOR LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 123112 900701 (CAN) DURING CLIMB AS THE GEAR WAS SELECTED UP, HYDRAULIC PRESSURE BEGAN TO FLUCTUATE AND THE QUANTITY IN THE NR 2 SYST EM BEGAN TO DROP. AFTER THE AIRCRAFT LANDED, MAINTENANCE FOUND THE NOSE GEAR DRAG STRUT ACTUATOR HYDRAULIC SUPPLY HOSE RUPTURED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800746 19991218 00746 WP 1999 12 18 CA991103028 1 19991025 A 3210 369H921333 SPRING 369D26301111 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL GEAR DAMPER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1326 CAE831009 (CAN) SPRING COIL (DAMPER) CRACKED APPROXIMATELY HALF WAY THROUGH WIRE. 1 G 7 1 3U 3 U H3WE E4CE 1999121800748 19991218 00748 NM 1999 12 18 CA991103033 1 19991003 A 2910 82940010115 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 25331 120382 LH1896 (CAN) DURING PRE-FLIGHT, HYDRAULIC FLUID WAS FOUND TO BE LEAKING FROM THE RIGHT HAND WING ROOT AREA. THE NR 2 SYSTEM PRE SSURE LINE WAS FOUND LEAKING WHERE IT RUNS THROUGH THE OVERWING AREA. THE DAMAGED SECTION OF LINE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800749 19991218 00749 EA 1999 12 18 CA991103034 1 19991006 A 2923 731840 PUMP DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE HYDRAULIC SYS FAILED W H DEACTIVATE SYST/CIRCUITS A J FLAME/FIRE WARNING INDICATION IN INSP/MAINT 1 CA 18904 MX514447 123144 LH750 (CAN) WHILE RUNNING THE AIRCRAFT TO INVESTIGATE A PILOT REPORTED SNAG WITH THE NR 2 STANDBY HYDRAULIC PUMP HOT CAUTION L IGHT, THE SUBJECT CAUTION LIGHT ILUMINATED AND THE STANDBY PUMP FAILED. WHEN THE PUMP FAILED, THE MAINTENANCE CREW NOTI CED SMOKE THEN FLAME, AT WHICH TIME THE PUMP WAS SELECTED OFF. WHEN THE PUMP WAS SELECTED OFF, THE FLAMES WENT OUT. THE STANDBY PUMP WAS REPLACED AND THE SURROUNDING STRUCTURE WAS INSPECTED FOR DAMAGE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800750 19991218 00750 NM 1999 12 18 CA991103035 1 19991010 A 2120 78279016 ACM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AC BAY SEIZED W O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA 25770 2700 860827 121075 LH532 (CAN) DURING FLIGHT, THE FLIGHT ATTENDANT NOTICED A LOUD HUMMING SOUND ACCOMPANIED BY VIBRATION. THIS COULD BE HEARD AN D FELT NEAR THE REAR OF THE CABIN IN THE CABIN FLOOR. THE SOUND AND VIBRATION WAS ACCOMPANIED BY AN OILY/ ELECTRICAL SME LL IN THE COCKPIT. AFTER LANDING, THE AIR CYCLE MACHINE WAS FOUND TO BE SEIZED AND LEAKING OIL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800751 19991218 00751 NM 1999 12 18 CA991103036 1 19991011 A 2910 82920010227 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 25141 121075 LH532 (CAN) A HYDRAULIC FLUID LEAK WAS NOTICED ON THE AIRCRAFT BELLY RT SIDE UNDER ROW 2 SEATS. A HYDRAULIC LINE WAS FOUND LE AKING AT THE PERMASWAGE FITTING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800752 19991218 00752 NM 1999 12 18 CA991103037 1 19991011 A 2910 82910010209 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24107 120795 LH955 (CAN) DURING PRE-FLIGHT, MAINTENANCE NOTICED HYDRAULIC FLUID LEAKING FROM THE NOSE WHEELWELL. THE NOSE GEAR DOWN PRESSU RE HYDRAULIC LINE WAS FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800753 19991218 00753 NM 1999 12 18 CA991103039 1 19991015 A 3231 83231014003 ROD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG DOOR BROKEN W O OTHER O OTHER AP APPROACH 1 CA 22814 120843 LH697 (CAN) UPON ARRIVAL, THE LEFT HAND CENTER AND AFT MAIN LANDING GEAR DOORS REMAINED OPEN WITH NO CORRESPONDING WARNING. M AINTENANCE FOUND THE DOOR CONNECTING ROD FROM THE DOOR ACTUATOR BELLCRANK TO THE LEFT/AFT DOOR HAD BROKEN JUST ABOVE THE LOWER SWAGE. THE EXTENSION SPRING TO THE LEFT HAND AFT DOOR WAS ALSO FOUND BROKEN. CRACKING WAS ALSO FOUND ON THE NAC ELLE ANGLE, PN 85411581-101, IN THE AREA OF THE CENTER DOOR HINGE BRACKET. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800754 19991218 00754 NM 1999 12 18 CA991103040 1 19991016 A 2910 82970410123 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 7429 120816 LH640 (CAN) DURING SCHEDULED MAINTENANCE, HYDRAULIC FLUID WAS FOUND TO BE LEAKING FROM THE FRONT OF THE RIGHT HAND WHEELWELL A REA. THE STAINLESS STEEL CASE DRAIN AND FLUID SUPPLY LINE FOR THE ENGINE DRIVEN PUMP WERE FOUND LEAKING FROM CHAFING WE AR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800755 19991218 00755 NM 1999 12 18 CA991103042 1 19991016 A 3020 83010056127 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE SYSTEM CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 26799 120816 LH640 (CAN) DURING MAINTENANCE, THE PRESSURE LINE FOR THE RIGHT ENGINE AIR INLET DEICE BOOT WAS FOUND CHAFED AGAINST STRUCTURE . LINE REPLACED AND SECURED TO PREVENT CONTACT WITH STRUCTURE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800756 19991218 00756 EA 1999 12 18 CA991103044 1 19991027 A 2731 C3CF4187 ROD DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE HARTZL HCB3T HCB3TN3 GL ELEVATOR TAB WORN W K NONE O OTHER IN INSP/MAINT 1 CA 846 PCE92418 BUA19022 (CAN) DURING INSPECTION, THE PUSH/PULL ROD FOR THE ELEVATOR TRIM TAB WAS SEVERELY WORN. THE WEAR SPOT OCCURRED WHERE TH E ROD RUNS THROUGH THE BULKHEAD AND CONTACTS THE TWO ROLLERS WHICH IT RIDES ON. RODS REPLACED. ROLLERS HAD WORN THROUG H THE ROD. 1 H 7 1 3R 4 T A815 E4EA 6 C P15EA 1999121800759 19991218 00759 EA 1999 12 18 CA991103053 1 19991027 A 3320 BV501261 SOCKET CNDAIR CL600 CL600* EA LYC ALF502 ALF502L2 41580 NE CABIN FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) CONDENSATION ACCUMULATING ON TOP OF FLUORESCENT LIGHT FIXTURE CAUSING SHORT CIRCUIT POSSIBLY LEADING TO SHOCK/FIR E. CONDENSATION OCCURS FROM THE USE OF VARIOUS KITCHEN APPLIANCES USED IN THE PROXIMITY TO LIGHTING FIXTURE. 2 L 7 2 4F 4 F RT A21EA E6NE 1999121800760 19991218 00760 EA 1999 12 18 CA991103055 1 19991009 A 3213 1602234A AXLE CNDAIR CL215 CL2156B11415 EA PWA PW120 PW123 NE LT MLG SCORED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 139 (CAN) DURING INSPECTION LEFT AND RIGHT MAIN WHEELS, UPON REMOVAL, FOUND MAIN WHEEL NUTS ON BOTH SIDES DID NOT HAVE ANY T ORQUE VALUE. REAR BEARING WAS FOUND ON AN ANGLE WITH SCORING AND REPAIRED IAW PSP495. SUBMITTER SUGGESTED IMPROPER TOR QUING BY MANUFACTURER AT ASSEMBLY. MANUAL TO BE AMENDED. 2 H 7 2 4T 4 T RT A14EA E20NE 1999121800761 19991218 00761 SW 1999 12 18 CA991103067 1 19990906 A 5320 212030161001 FITTING BELL 212030156005 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CPPS60310 (CAN) LOWER LEFT FITTING WAS FOUND CRACKED. TT 15,524 HOURS AND WAS POSSIBLY THE ORIGINAL FITTING. CRACK EXTENDED FROM FORWARD MOST RIVET HOLE .6250 INCH TO THE UPPER EDGE AND .75 INCH TO THE RADIUS OF THE 90 DEGREE ANGLE. 1 G 7 1 4U 4 U H4SW E22EA 1999121800762 19991218 00762 EA 1999 12 18 CA991103073 1 19991007 A 2750 ECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807173 (CAN) DURING TAXI FLAPS FAIL MESSAGE CAME ON. UNABLE TO RESET. FECU REPLACED AND BPSU. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800763 19991218 00763 EA 1999 12 18 CA991103074 1 19991005 A 2750 TE FLAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WING FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 807267 (CAN) FLAP FAIL ON APPROACH. RESET CARRIED OUT SERV. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800764 19991218 00764 EA 1999 12 18 CA991103075 1 19991012 A 2750 FLEX SHAFT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP DAMAGED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 807267 (CAN) FLAP FAIL ON APPROACH AT 190 KNOTS. ZERO DEGREES FLAP LANDING. POWER DRIVE UNIT CHANGED DUE TO HIGH CURRENT DRAW . RIGHT NR 4 FLEXSHAFT DAMAGED. REPLACED. LEFT NR 5 CONDUIT ASSY REPLACED. AD 98-14R1 C/W. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800765 19991218 00765 EA 1999 12 18 CA991103076 1 19991020 A 2750 11508202 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 807281 (CAN) FLAP FAIL IN-FLIGHT AT 8 DEGREES. INDICATION ZERO. CHANGE BPSU. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800766 19991218 00766 1999 12 18 CA991103077 4 19991023 A 3417 ADC CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 807380 (CAN) FLAP FAIL WHEN SELECTING FLAPS TO 45 DEGREES. FLAPS STOPPED AT 40 DEGREES AT 168 IAS. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800767 19991218 00767 EA 1999 12 18 CA991103078 1 19991024 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 807385 (CAN) ON APPROACH, CAPTAIN'S WINDSHIELD SHATTERED. NEW WINDSHIELD INSTALLED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800768 19991218 00768 NE 1999 12 18 CA991103092 2 19991004 A 7321 FCU BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE ENGINE FLUCTUATED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA P707529 (CAN) ENGINE EXPERIENCED EPR FLUCTUATIONS UP TO 21 EPR. N2 REMAINED STEADY, N1 FLUCTUATED UP TO 5 DEGREES. EEC'S REPLA CED INDESCRIMINENTLY, SUBMITTER STATED FAILURE WAS DUE TO FCU TRIM CONTROL MAIN OVERRIDE PX. 2 L 7 2 4F 4 F RT A1NM E3NE 1999121800769 19991218 00769 EA 1999 12 18 CA991104002 1 19991105 A 2910 AE2464219EO164 LINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE WS 47.61 CHAFED W K NONE K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA 807024 (CAN) SEVERAL SPOILER HYDRAULIC LINES FOUND CHAFING ON LEFT AND RIGHT FRAMES WS 47.61 APPROX FS 5444. THE CHAFING WAS C OMPOUNDED BY THE FIBERGLASS COVERING. 2 L 7 2 4F 4 F RT A21EA E15NE 1999121800770 19991218 00770 EA 1999 12 18 CA991104005 1 19991105 A 7603 M640631 TROTTLE 2100140003 CNDAIR CL600 CL6002B19 EA LT ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 618 (CAN) CREW REPORTED THE LEFT POWER LEVER UNABLE TO RETARD TO IDLE OR CUTOFF. ENGINE SHUTDOWN BY FIRE PUSH BUTTON. THRO TTLE GEARBOX REPLACED. 2 L 7 2 4F RT A21EA 1999121800771 19991218 00771 EA 1999 12 18 CA991104006 1 19991105 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA TE FLAP FAILED W B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA 1002A (CAN) FLAPS FAILED AT 8 DEGREES ON APPROACH. BPSU REPLACED. 2 L 7 2 4F RT A21EA 1999121800772 19991218 00772 EA 1999 12 18 CA991104008 1 19991007 A 2913 65WED1042 PUMP CNDAIR CL215 CL2156B11415 EA PWA PW120 PW123 NE HYDRAULIC SYS WORN W K NONE O OTHER IN INSP/MAINT 1 CA 938 BO70 109047 930402 (CAN) ON 100-HOUR INSPECTION, FOUND PREMATURE WEAR ON THE DRIVE SHAFT OF HYDRAULIC PUMP ON INTERNAL SPLINES. WEAR WAS T O THE POINT OF THE SHAFT SHEARING. THE PROBLEM OCCURRED WITH ONLY 037 HOURS OF OPERATION ON THE PUMP. THE REPLACEMENT PUMP SHOWED THE SIMILAR PROBLEM. 2 H 7 2 4T 4 T RT A14EA E20NE 1999121800774 19991218 00774 EU 1999 12 18 CA991104010 1 19991019 A 6220 E1T254901 ADAPTER 350A31000005 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R HEAD DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA M339 786 (CAN) DURING SCHEDULED MAINTENANCE, 2 OF THE 3 FREQUENCY ADAPTERS WERE FOUND TO HAVE A BLISTER ON THE TRAILING EDGE SIDE OF THE UNIT. 1 G 7 1 3U 3 U H9EU E19EU 1999121800775 19991218 00775 EU 1999 12 18 CA991104011 1 19991019 A 6210 350A11001003 BLADE 350A11001003 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 4124 3094 786 (CAN) ALL 3 MAIN ROTOR BLADES WERE FOUND TO HAVE DELAMINATION OF THE STAINLESS STEEL LEADING EDGE STRIPS. DELAMINATION FOUND AT BLADE ROOT AREA AND AT OVERLAP AREA OF THE INBOARD AND OUTBOARD EDGE STRIPS. 1 G 7 1 3U 3 U H9EU E19EU 1999121800776 19991218 00776 EU 1999 12 18 CA991104012 1 19991019 A 6220 350A3118317 SLEEVE 350A31000005 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R BLADE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3234 M339 786 (CAN) DURING ROUTINE MAINTENANCE, 2 OF THE UPPER SLEEVES OF THE MAIN ROTOR HEAD HAD CRACKS IN THE BLADE BOLT AREA. THE BLADE BOLT BUSHINGS (OF THE SLEEVE) WERE ALSO FOUND TO BE LOOSE. 1 G 7 1 3U 3 U H9EU E19EU 1999121800777 19991218 00777 EA 1999 12 18 CA991112001 1 19991026 A 5510 C2TP57 SPAR DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE HARTZL HCB3R HCB3R304 GL HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3441 SA800 5127 EM332 (CAN) TAILPLANE FRONT SPAR WAS FOUND CRACKED UNDER LEFT PICK-UP BRACKET AT UPPER BOLT HOLE. CRACK WAS NOT VISIBLE WITHO UT PICK-UP BRACKET REMOVED. AD 91-42 REPEAT WAS NOT DUE UNTIL MAY 2000. AD DOES NOT REQUIRE REMOVAL OF THE BRACKETS. 1 H 7 1 3R 3 R A806 5E1 5 C P28EA 1999121800778 19991218 00778 SW 1999 12 18 CA991112002 1 19991027 A 6320 2060405325 RING GEAR BELL 206040004101 BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL TRANSMISSION CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1437 BMC45194 CAE890788 (CAN) ELEVEN TEETH WERE FOUND CRACKED ON 1,500-HOUR INSPECTION. 1 G 7 1 3U 3 U H2SW E1GL 1999121800779 19991218 00779 NE 1999 12 18 CA991112004 1 19991030 A 6320 S613520600046 BEVEL GEAR SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE M/R GEARBOX BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 450 A1H2666211 295089 (CAN) DURING SERVICING REMOVAL OF COARSE SCREEN, ENGINEER NOTICED SEVERAL SMALL PIECES OF NON-FERROUS METAL WHICH WAS FO UND IN PART OF THE BEVEL GEAR TOOTH . 2 G 7 2 4U 4 U 1H15 1E3 1999121800780 19991218 00780 NM 1999 12 18 CA991112010 1 19991021 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT FAILED W O OTHER N FALSE WARNING DE DESCENT 1 CA 16598 297 120816 LH640 (CAN) AFTER THE CREW SELECTED LANDING GEAR DOWN, THE WEIGHT ON -ON-WHEELS CAUTION LIGHT REMAINED ON. THE CREW CARRIED O UT AN ALTERNATE GEAR EXTENSION AND LANDED SAFELY. THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU) WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800781 19991218 00781 NM 1999 12 18 CA991112011 1 19991026 A 2910 82910010175 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS LEAKING W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 22889 120843 LH697 (CAN) HYDRAULIC FLUID FOUND LEAKING FROM A PIN HOLE IN THE LINE TO THE NOSE GEAR DOOR ACTUATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800782 19991218 00782 1999 12 18 CA991112015 4 19991104 A 2215 C6R16071 CONTROL CABLE COLLINS SMT65 DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL AFCS BROKEN W O OTHER O OTHER NR NOT REPORTED 1 CA 5464 4737 PCE42181 BU5043 (CAN) PILOT REPORTED AUTOPILOT NOT ENGAGING NORMALLY. AILERON SERVO CABLE FOUND BROKEN AT THE ENTRY INTO UPPER AILERON CABLE CLAMP. DUE TO LOSS OF TENSION , CABLES JUMPED OUT OF THEIR TRACKS, TWISTED AND JAMMED UNDER THE CABLE GUARD. BOT H CABLES EXHIBIT CRUSHING WHERE CABLES ENTERED THE CABLE CLAMP. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 1999121800783 19991218 00783 1999 12 18 CA991112024 4 19991021 A 2210 6229968002 ACTUATOR CNDAIR CL600 CL6002B19 EA YAW DAMPER FAILED W A O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 681 (CAN) NR 2 YAW DAMPER DISENGAGED IN-FLIGHT AND WOULD NOT RE-ENGAGE, THEN NR 1 YAW DAMPER DISENGAGED. NR 1 CAME BACK ON- LINE AND NR 2 WAS UNABLE TO RESET. ACTUATOR REPLACED FOR INDICATING RUDDER INPUT. 2 L 7 2 4F RT A21EA 1999121800784 19991218 00784 EA 1999 12 18 CA991112030 1 19991105 A 5230 B17806R COUNTERBALANCE CNDAIR CL600 CL6002B19 EA CARGO DOOR FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) CABLE FOR CARGO DOOR COUNTERBALANCE BROKE FALLING ON HANDLER'S ARM. 2 L 7 2 4F RT A21EA 1999121800786 19991218 00786 EA 1999 12 18 CA991112032 1 19990719 A 2822 85198 TERMINAL BLOCK ADEL 85816 DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL BOOST PUMP FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 4623 H348A PCE40240 BUA20047 (CAN) NR 1 AFT BOOST PUMP WAS REPORTED AS INOPERABLE. ON INSPECTION OF THE CANISTER TYPE PUMP, THE TERMINAL BLOCK ON TH E PUMP WAS FOUND SEVERELY BURNT AND MELTED AT THE PLUS TERMINAL. ABOUT ONE-HALF INCH OF THE A/C POWER WIRE INSULATION H AD ALSO BURNT OFF. TB WAS REPLACED, DRAW TO THE PUMP CHECKED, AND AIRCRAFT RETURNED TO SERVICE. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 1999121800787 19991218 00787 NM 1999 12 18 CA991112033 1 19991027 A 6120 7901012 ACTUATOR HAMSTD 7901802 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROPELLER LEAKING W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 25245 7112 880910 120175 1814 (CAN) PROPELLER ACTUATOR LEAK INVESTIGATED AND REVEALED CHROME PLATING ON THE INSIDE OF THE DOME HAD PEELED BACK APPROXI MATELY .75 INCH IN LENGTH AND .1685 INCH IN WIDTH. THIS DAMAGED O-RING, CAUSED DOME TO PRESSURIZE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800788 19991218 00788 NM 1999 12 18 CA991116001 1 19991103 A 2750 DRIVE SHAFT 745581A DHAV DHC8 DHC8101 2809002 NM TE FLAP SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA E097 (CAN) FLAP SECONDARY DRIVE SHAFT SWAGED END FOUND SEPARATED FROM BRAIDED END OF DRIVE SHAFT. THIS END CONNECTS THE DRIV E SHAFT TO THE TRANSFER GEARBOX. 2 H 7 2 4T RT A13NM 1999121800789 19991218 00789 SO 1999 12 18 CA991116003 1 19991109 A 2913 65WE002241 PUMP EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL HYDRAULIC SYS FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 2248 A1678C1 56864 BU13608 (CAN) RIGHT HYDRAULIC PUMP FAILED AFTER TAKEOFF. PUMP REPLACED. LINES FLUSHED, FILTERS REPLACED. 1 L 7 2 4T 4 T A21SO E4EA 6 C P15EA 1999121800791 19991218 00791 EA 1999 12 18 CA991116007 1 19991102 A 5220 85220282001 SEAL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE EMERGENCY EXIT DISPLACED W I CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 CA 19087 123144 LH750 (CAN) IN CRUISE FLIGHT AT 8,000 FEET, CABIN PRESSURE WAS LOST AND AIR COULD BE HEARD EXITING FROM THE EMERGENCY EXIT DOO R AREA. MAINTENANCE FOUND A SMALL SECTION OF DOOR SEAL DISPLACED FROM ITS TRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800794 19991218 00794 EA 1999 12 18 CA991116017 1 19991113 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA TE FLAP FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA 526 (CAN) FLAPS FAILED AT ZERO DEGREES ON DESCENT. FECU REPLACED. 2 L 7 2 4F RT A21EA 1999121800795 19991218 00795 EA 1999 12 18 CA991116018 1 19991113 A 2750 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAP JAMMED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA 830 (CAN) UPON SELECTION OF FLAPS TO 45 DEGREES ON APPROACH, FLAPS FAILED AT 23 DEGREES. NR 4 RIGHT ACTUATOR WAS FOUND HAR D JAMMED. NEW ACTUATOR INSTALLED. 2 L 7 2 4F RT A21EA 1999121800798 19991218 00798 EU 1999 12 18 CA991116025 1 19991102 A 6120 7901802 ACTUATOR HAMSTD 14SF5 AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE PROPELLER LEAKING W E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA 21401 5963 890217 120719 890217 (CAN) EVIDENCE OF OIL LEAKING FROM PROPELLER ACTUATOR, O-RING AND ACTUATOR REPLACED. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999121800799 19991218 00799 EA 1999 12 18 CA991208001 1 19991028 A 3010 3D147211 TIMER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE DEICE SYSTE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 123110 870626 (CAN) FLIGHT CREW REPORTED THE LEFT AND RIGHT NR 5 DEICE BOOTS WOULD NOT INFLATE IN AUTO MODE BUT OPERATED IN MANUAL. M AINTENANCE REPLACED A FAULTY DEICE TIMER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800800 19991218 00800 EA 1999 12 18 CA991208002 1 19991107 A 3610 7821004 SWITCH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE DEICE SYSTEM STUCK W O OTHER J WARNING INDICATION DE DESCENT 1 CA 960582 123110 870626 (CAN) THE FLIGHT CREW REPORTED THAT THE DEICE PRESSURE DROPPED FROM 18 PSI WHEN THE POWER WAS REDUCED ON DESCENT, AND TH AT THE DEICE BOOTS WOULD NOT INFLATE. MAINTENANCE REPLACED THE NR 2 HP BLEED SWITCH. SUBMITTER STATED THAT THESE SWITC HES ARE COMMONLY CONTAMINATED WITH WATER, WHICH CAUSES THEM TO FAIL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800801 19991218 00801 EA 1999 12 18 CA991208003 1 19991114 A 2760 82950010271 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE ROLL SPOILER CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA 123110 870626 (CAN) ON FINAL APPROACH, ALL HYDRAULIC FLUID WAS LOST FROM THE NR 1 HYNR 1 SYSTEM. MAINTENANCE FOUND A CRACKED HYDRAULI C LINE TO THE ROLL SPOILER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800802 19991218 00802 NM 1999 12 18 CA991208006 1 19991111 A 2421 31708001A AC GENERATOR LUCAS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 8509 720 120373 870601 (CAN) THE FLIGHT CREW REPORTED THE NR 2 AC GENERATOR FAILED AND WOULD NOT RESET. MAINTENANCE REPLACED THE NR 2 AC GENER ATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800803 19991218 00803 NM 1999 12 18 CA991208008 1 19991103 A 3320 BR63031021 RECEPTACLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 120064 860404 (CAN) WHILE REPLACING A CABIN OVERHEAD LIGHT, MAINTENANCE FOUND THE AFT TUBE RECEPTACLE TO BE BURNT. THE ENTIRE FIXTURE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800804 19991218 00804 NM 1999 12 18 CA991208009 1 19991106 A 3242 68728 SEAL BFGOODRICH 224664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE ASSY LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 772 1108 120064 860404 (CAN) DURING SCHEDULED MAINTENANCE, THE NR 2 BRAKE WAS FOUND TO BE LEAKING. THE PROBLEM WAS TRACED TO A DAMAGED BACK-UP RING ON A BRAKE PISTON. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800805 19991218 00805 NM 1999 12 18 CA991208010 1 19991101 A 2435 23088002A GENERATOR LUCAS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE STARTER/GEN FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 3936 887 399 120648 881221 (CAN) THE NR 2 GENERATOR FAILED AND WOULD NOT RESET. MAINTENANCE REPLACED THE S/G. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800806 19991218 00806 NM 1999 12 18 CA991208011 1 19991108 A 3010 3D147211 TIMER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE DEICE SYSTEM FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 6137 G046 120648 881221 (CAN) FLIGHT CREW REPORTED THAT THE DEICE BOOTS WOULD NOT DEFLATE AFTER THE INFLATION CYCLE. MAINTENANCE REPLACED THE D EICE TIMER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800807 19991218 00807 NM 1999 12 18 CA991208012 1 19991109 A 2435 23088002A GENERATOR LUCAS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE STARTER/GEN OVERHEAT W H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA 6515 48 806 120648 881221 (CAN) DURING FLIGHT, THE CREW GOT A 'NR 2 GEN HOT' LIGHT AND SELECTED THE GENERATOR OFF. MAINTENANCE REPLACED THE START ER/GENERATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800808 19991218 00808 NM 1999 12 18 CA991208014 1 19991114 A 3242 214664 BRAKE ASSY BFGOODRICH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG VIBRATION W D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 14026 2072 1769 120648 881221 (CAN) DURING TAXI ,THE AIRCRAFT EXPERIENCED SEVERE VIBRATION DURING BRAKING. MAINTENANCE REPLACED THE NR 4 BRAKE ASSY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800809 19991218 00809 NM 1999 12 18 CA991208015 1 19991119 A 2910 82970010319 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 120229 870537 (CAN) HYDRAULIC LINE CHAFED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800810 19991218 00810 NM 1999 12 18 CA991208016 1 19991122 A 2420 M817142AC1 TERMINAL BLOCK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 GENERATOR LOOSE W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 18023 120229 870537 (CAN) CREW REPORTED AN INTERMITTENT NR 2 AC GENERATOR FAIL SNAG. WHILE TROUBLESHOOTING, A PIN WAS FOUND TO BE NOT LOCK ED IN TERMINAL BLOCK 2422-TB2. THE TERMINAL BLOCK WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800811 19991218 00811 NM 1999 12 18 CA991208017 1 19991126 A 3010 8SC0029030 DEICE BOOT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 3 LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 6172 120229 870537 (CAN) FLIGHT CREW REPORTED THAT THE RIGHT NR 3 LEADING EDGE DEICE BOOT WOULD NOT INFLATE. MAINTENANCE FOUND THE DEICE B OOT TO BE INTERNALLY CONTAMINATED WITH WATER. SUBMITTER SUGGESTED WATER ENTERED THROUGH A NUMBER OF HOLES INCLUDING ONE HOLE WHICH HAD BEEN PATCHED WHERE THE PATCH WAS MISSING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800812 19991218 00812 EA 1999 12 18 CA991208018 1 19991110 A 2420 51539008C GCU LUCAS DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 1 FAILED W D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 CA 14648 7634 123116 900837 (CAN) DURING TAXI, THE CREW NOTED THAT THE NR 1 GENERATOR CAUTION LIGHT CAME ON. AN ELECTRICAL SMELL WAS ALSO EVIDENT I N THE COCKPIT AND CABIN. MAINTENANCE REPLACED A DEFECTIVE GCU. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800813 19991218 00813 NE 1999 12 18 CA991208020 2 19991129 A 7510 82110848001 DUCT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BLEED AIR LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 123116 900837 (CAN) FLIGHT CREW REPORTED THAT THE STATIC AIR TEMPERATURE WAS READING 10 DEGREES TOO HIGH IN-FLIGHT AND ON THE GROUND. MAINTENANCE FOUND A LEAKING BLEED AIR DUCT IN THE AREA OF THE RIGHT WING ROOT. THE DUCT ASSY WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800814 19991218 00814 EA 1999 12 18 CA991208021 1 19991101 A 5210 85321986001 SEAL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PAX DOOR LEAKING W O OTHER K FLUID LOSS CR CRUISE 1 CA 3002 123113 901009 (CAN) FLIGHT CREW REPORTED DOOR SEAL LEAKING AT CABIN PRESSURES EXCEEDING 4.8 PSID. MAINTENANCE FOUND ICE/WATER IN LOWE R PART OF SEAL. AFTER THE WATER WAS REMOVED, THE SEAL WAS FOUND TO BE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800815 19991218 00815 EA 1999 12 18 CA991208022 1 19991126 A 3242 68728 SEAL BFGOODRICH 21517 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BRAKE ASSY LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 402 0345 123113 901009 (CAN) BRAKE ASSY FOUND TO BE LEAKING WHILE PARKING BRAKE WAS APPLIED. THE CAUSE OF THE LEAK WAS DETERMINED TO BE A DEFE CTIVE BACK-UP RING ON ONE OF THE BRAKE PISTONS WHICH WAS FOLDED OVER THE PISTON. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800816 19991218 00816 NM 1999 12 18 CA991208023 1 19991108 A 7600 87600520001 CABLE PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CONDITION LEVER DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 120854 120854 890709 (CAN) DURING SCHEDULED MAINTENANCE, THE CONDITION LEVER CABLE WAS FOUND WORN TO SERVICE LIMITS WHERE IT RIDES ON THE STE EL PULLEY FORWARD OF THE FIREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800817 19991218 00817 NM 1999 12 18 CA991208024 1 19991110 A 7500 82110144003 PIPE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BLEED AIR CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 1 120854 890709 (CAN) THE FLIGHT CREW COMPLAINED OF FEELING LIGHT HEADED WITH ASSOCIATED HEADACHES. MAINTENANCE DETERMINED THE SMELL TO BE COMING FROM THE BLEED AIR SYSTEM. A NEW BLEED AIR PIPE WAS INSTALLED THE PREVIOUS NIGHT. SUBMITTER FELT THE PIPE M AY HAVE BEEN TREATED WITH A COATING THAT BURNED OFF WITH THE HOT BLEED AIR PASSING THROUGH THE NEW ASSY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800818 19991218 00818 NM 1999 12 18 CA991208025 1 19991120 A 3350 6104781 POWER SUPPLY GRIMES DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 5639 186 AAD19 120854 890709 (CAN) DURING SCHEDULED MAINTENANCE, AN EMERGENCY LIGHTING POWER SUPPLY WAS FOUND TO BE UNSERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800819 19991218 00819 NM 1999 12 18 CA991208026 1 19991128 A 3260 82455023015 HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NLG DAMAGED W K NONE L NO TEST IN INSP/MAINT 1 CA 120854 890709 (CAN) DURING SCHEDULED MAINTENANCE, THE NOSE GEAR ALTERNATE INDICATION LIGHT WAS FOUND TO BE INOPERATIVE. THE LIGHT HARN ESS HAD BEEN DAMAGED IN THE AREA OF THE NOSE GEAR STRUT. THE HARNESS WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800820 19991218 00820 NM 1999 12 18 CA991208027 1 19991107 A 5230 SWITCH DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CARGO DOOR STUCK W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA 123124 901161 (CAN) DURING THE TAKEOFF ROLL, THE CREW NOTICED THE BAG DOOR WARNING LIGHT COME ON AND ABORTED THE TAKEOFF. MAINTENANCE DETERMINED THE BAGGAGE DOOR PROXIMITY SWITCHES TO STICK (COMPRESSED) BEYOND THEIR NORMAL DOOR CLOSED POSITION, EVEN WHE N THE DOOR WAS OPENED. THE SWITCH SLIDES WERE CLEANED AND LUBRICATED AND TESTED OK. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800821 19991218 00821 NM 1999 12 18 CA991208030 1 19991103 A 5210 85321986001 SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PAX DOOR LEAKING W O OTHER O OTHER DE DESCENT 1 CA 4328 121165 891129 (CAN) THE CREW REPORTED A LOUD SQUEAL COMING FROM THE PASSENGER DOOR DURING DESCENT. MAINTENANCE FOUND THE INFLATABLE D OOR SEAL TO BE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800822 19991218 00822 NM 1999 12 18 CA991208032 1 19991109 A 2760 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ROLL SPOILER BROKEN W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA 121165 891129 (CAN) DURING TAXI, THE NR 1 ROLL SPOILER PUSH-OFF LIGHT ILLUMINATED. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT TH E RIGHT ROLL SPOILER CLUTCH MICROSWITCH. THE SUBMITTER STATES THAT DEHAVILLAND HAS ISSUED ASYD TO ADDRESS THIS ISSUE, W HICH THE SUBMITTER STATES IS FAIRLY COMMON. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800823 19991218 00823 NM 1999 12 18 CA991208033 1 19991120 A 5711 857400052 BRACKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ACTUATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 121165 891129 (CAN) DURING AN INSPECTION REQUIRED BY SB 8-57-7, A CRACK WAS FOUND IN THE RIGHT AILERON TAB ACTUATOR ARM BRACKET. A RE PLACEMENT TRIM TAB WAS INSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800824 19991218 00824 EA 1999 12 18 CA991208034 1 19991031 A 3242 68728 O-RING BFGOODRICH 21517 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE BRAKE FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 5512 259 0481 123132 901056 (CAN) DURING SCHEDULED MAINTENANCE, THE NR 2 BRAKE ASSY WAS FOUND TO BE LEAKING. MAINTENANCE REVEALED THAT AN O-RING ON A BRAKE PISTON WAS LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800825 19991218 00825 EA 1999 12 18 CA991208036 1 19991128 A 3040 SYLZ50970 CONTROLLER BARBERCOL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE WINDSHIELD FAILED W O OTHER O OTHER CR CRUISE 1 CA 23800 623C 123132 901056 (CAN) DURING CRUISE FLIGHT, THE PILOTS WINDSCREEN FROSTED OVER ON THE INSIDE. THE AC POWER MONITOR SHOWED NO LOAD WHEN THE POWER WAS TURNED ON. MAINTENANCE DETERMINED THE FAULT TO LIE WITH THE WINDSHIELD HEAT CONTROLLER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800826 19991218 00826 EA 1999 12 18 CA991208037 1 19991028 A 5210 8SC0156 ASSIST STRUT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PASSENGER DOOR OVERSERVICED W A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 CA 123132 901056 (CAN) WHILE CLIMBING THROUGH FL 210, THE PASSENGER DOOR WARNING LIGHT CAME ON. THE AIRCRAFT RETURNED TO BASE WHERE THE MAINTENANCE CREW ADJUSTED THE DOOR PROXIMITY SENSOR. ON THE NEXT FLIGHT WHILE DESCENDING THROUGH FL 210, THE DOOR HANDL E DISLODGED FROM THE LOCKED POSITION. THIS CAUSED THE DOOR SEAL TO DEFLATE AND THE CABIN ALTITUDE TO CLIMB. THE FLIGHT ATTENDANT PULLED THE HANDLE BACK TO THE LOCKED POSITION AND THE DOOR RESEALED. AFTER AN UNEVENTFUL LANDING, MAINTENANC E FOUND THE DOOR MECHANISM OVER CENTER ASSIST STRUT TO BE UNSERVICEABLE AND REPLACED IT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800827 19991218 00827 EA 1999 12 18 CA991208038 1 19991129 A 3244 314801OPT3 TIRE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE LT MLG FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 123132 901056 (CAN) BOTH TIRES ON THE LEFT MAIN GEAR FAILED DURING TAXI. BOTH TIRES WERE THOMPSON RECAPS AND BOTH FAILED IN THE SIDEW ALL AREA. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800828 19991218 00828 NM 1999 12 18 CA991208039 1 19991123 A 5210 85321986001 SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PAX DOOR LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 120083 901134 (CAN) DURING CRUISE FLIGHT, THE INFLATABLE DOOR SEAL STARTED TO LEAK. MAINTENANCE REPLACED THE DOORSEAL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999121800829 19991218 00829 EU 1999 12 18 CA991208040 1 19991103 A 2731 CHAIN DRIVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ELEVATOR TRIM BINDING W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA 28665 LF05464A (CAN) FLIGHT CREW REPORTED ELEVATOR TRIM GRINDING AND BINDING IN BOTH MANUAL AND ELECTRIC MODES. TRIM SYSTEM LUBRICATED AND OPERATED NORMAL. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800830 19991218 00830 EU 1999 12 18 CA991208041 1 19991108 A 2530 8201014000 CONTROLLER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE GALLEY OVEN STICKING W O OTHER O OTHER NR NOT REPORTED 1 CA 17415 88070342 LF05464A (CAN) OVEN TIMER STICKING. OVEN CONTROLLER REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800831 19991218 00831 EU 1999 12 18 CA991208042 1 19991118 A 5610 NF20216526 HEATER BRAERO BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE WINDSCREEN FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 11663 L210940 LF05683A (CAN) RIGHT PILOTS WINDSCREEN HEAT NOT WORKING. WINDSCREEN REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800832 19991218 00832 EU 1999 12 18 CA991208043 1 19991130 A 3010 TAS202001 SENSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ANTI-ICE SYSTEM SHORTED W O OTHER J WARNING INDICATION CR CRUISE 1 CA A160 LF05465A (CAN) AIR LOW TEMP WARNING LIGHT ON IN-FLIGHT WITH WING DEICE SELECTED ON. NR 4 DUCK OVERTEMP SWITCH SHORTED CAUSING A IR VALVE TO CLOSE RESULTING IN LOW PRESSURE. OVERTEMP SWITCH REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800833 19991218 00833 EU 1999 12 18 CA991208044 1 19991201 A 5710 FASTENERS BRAERO BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE RT WING UNDERTORQUED W K NONE W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 CA LF05465A (CAN) FUEL LEAK FOUND IN RIGHT REAR WING ROOT AREA. SEVERAL SUSPECT FASTENERS TIGHTENED IAW HC536H9043 AND THE LEAK SUB SIDED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800834 19991218 00834 EU 1999 12 18 CA991208046 1 19991115 A 5710 FASTENERS BRAERO BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE RT WING LOOSE W K NONE K S FLUID LOSS AFFECT SYSTEMS IN INSP/MAINT 1 CA LF05629A (CAN) FUEL LEAK FOUND IN RIGHT REAR WING ROOT AREA. SEVERAL SUSPECT FASTENERS TIGHTENED IAW HC536H9043 AND THE LEAK SUB SIDED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800835 19991218 00835 EU 1999 12 18 CA991208047 1 19991130 A 2530 6201231 RECEPTACLE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE GALLEY FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 28778 LF05629A (CAN) ELECTRICAL BURNING SMELL REPORTED IN FORWARD GALLEY. INVESTIGATION REVEALED A BURNT RECEPTICAL ON THE COFFEE MAK ER. RECEPTICAL REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800836 19991218 00836 EU 1999 12 18 CA991208049 1 19991028 A 2910 HTE210014 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE HYDRAULIC SYS FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 389GB285H LF05629A (CAN) LOW PRESSURE HYDRAULIC SYSTEM GREEN LIGHT ON AT PUSHBACK AFTER ENGINE START. GREEN SYS ISOLATION VALVE REPLACED. TOTAL TIME ON PART 28,506 HOURS. 2 H 7 4 4F 4 F RT A49EU E6NE 1999121800837 19991218 00837 EU 1999 12 18 CA991208050 1 19991126 A 2433 Y0052 TRU AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE E/E BAY FAULTY W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 1654 731762 (CAN) ELECTRICAL BURNING SMELL REPORTED APPARENTLY COMING FROM AIR CONDITIONING PACKS. INVESTIGATION REVEALED NR 2 TRU FAILED. UNIT REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999121800838 19991218 00838 EU 1999 12 18 CA991208051 1 19991130 A 2121 FAN AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE CABIN FAILED W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 23739 17435 731586 (CAN) STRONG SMELL BURNING PLASTIC, VIBRATION AND SMOKE IN COCKPIT AND ECAM MASSAGE VENT EXTRACT FAN. AIRCRAFT LANDED, VENT FAN REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1999121800839 19991218 00839 1999 12 18 CA991208052 4 19991202 A 3460 FMGC1 DATA AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE E/E BAY FAULTY W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 731474 (CAN) ECAM REPORTED FMGC 1 FAULT. NR 1 FMGC RESET. 2 L 7 2 4F 4 F RT A28NM E29NE 1999121800840 19991218 00840 NM 1999 12 18 CA991208053 1 19991115 A 3520 OXYGEN MASKS BOEING 747 747475 NM CABIN FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) DURING INSPECTION, OXYGEN MASKS DID NOT DEPLOY PROPERLY FROM PASSENGER CONTROL UNITS. MASKS INCORRECTLY PACKED. ALL MASKS PACKED PER MM. 2 L 7 4 4F RT A20WE 1999121800841 19991218 00841 NM 1999 12 18 CA991208054 1 19991102 A 2701 DUST SHIELD BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE CONTROL COLUMN OVERTORQUED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 708805 (CAN) REPORT OF ELEVATOR FEEL NOT NORMAL. THIS SNAG GENERATED AFTER FIRST FLIGHT AFTER HEAVY MAINTENANCE VISIT. ELEVATO R FEEL BREAKOUT TORQUE WITHIN LIMITS. WAS PREVIOUS SAME SNAG. ELEVATOR COMPUTER REPLACED AND ELEVATOR CABLES CHECKED F OR PROPER TENSION. HINGE BEARINGS GREASED. LIGHT TEST ACCOMPLISHED, PILOT REPORTED ELEVATORS WERE NORMAL. NEXT FLIGHT CREW REPORTED HEAVY ELEVAROT, WITH A DEAD BAND IN CENTER OF TRAVEL. TROUBLESHOOTING FOUND BINDING WHEN CONTROL COLUMN OPERATING FORE AND AFT. CONTROL COLUMN DUST SHIELDS ADJUSTED TOO TIGHT. FOD FOUND, SPLIT PIN TRAPPED UNDER F/OS DUST S HIELD. CONTROL COLUMN DUST SHIELDS ADJUSTED PER MM. SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1999121800842 19991218 00842 NM 1999 12 18 CA991208055 1 19991126 A 7933 INDICATOR BOEING 737 737275C NM PWA JT8 JT8D9A 52048 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 707356 (CAN) CREW REPORTED NR 1 ENGINE OIL TEMPERATURE INDICATOR HAD FAILED AFTER TAKEOFF. AIRCRAFT RETURNED FOR REPAIRS. REP LACED NR 1 OIL TEMPERATURE BULB AND RUN-UP CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1999121800843 19991218 00843 NM 1999 12 18 CA991208056 1 19991202 A 2410 699647C CSD BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NR 1 ENGINE FAILED W G C O2 MASK DEPLOYED ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 CA 48246 33211 702782 (CAN) ON TAKEOFF, NR 1 GENERATOR DROPPED OFF-LINE WHEN POWER APPLIED FOR TAKEOFF. TAKEOFF REJECTED DUE NR 2 GEN US AND ON MEL, APU TOOK OVER POWER ELECTRONICS. NR 1 GENERATOR ON BUS WHEN RESET. NR 1 ENGINE RUN-UP CARRIED OUT AND TAKEOFF POWER WAS COMPLETED, NR 1 GENERATOR DROPPED OFF THE BUS AND CSD LOW OIL PRESSURE LIGHT CAME ON, CSD DISCONNECTED. NR 1 CSD REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999121800844 19991218 00844 1999 12 18 CA991208057 4 19990907 A 3444 GPS155XL GPS SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE COCKPIT FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 95000800 280227AC (CAN) DURING TAXI, THE GARMIN GPS DROPPED OFF- LINE AND THEN PERFORMED AN AUTOMATIC RE-BOOT. 2 G 7 2 4U 4 U 1H15 1E3 1999121800845 19991218 00845 1999 12 18 CA991208058 4 19990908 A 3444 GPS155XL GPS SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE COCKPIT FAILED W O OTHER O OTHER CR CRUISE 1 CA 95000798 295119C (CAN) DURING CRUISE, THE GPS DROPPED OFF-LINE AND PERFORMED AN AUTOMATIC RE-BOOT. 2 G 7 2 4U 4 U 1H15 1E3 1999121800846 19991218 00846 WP 1999 12 18 CA991208061 1 19991109 A 2840 HARNESS DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUEL QUANTITY SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 84830 517958 (CAN) FUEL QUANTITY INDICATION BLINKING. FUEL QUANTITY WIRES IN UPPER AUXILIARY TANK HAVE INSULATION SEPARATION. WIRES DAMAGED LOCATED BETWEEN FUEL QUANTITY JUNCTION PROBE AND AFT FUEL TANK BULKHEAD. WIRES REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1999121800847 19991218 00847 SW 1999 12 18 CA991208066 1 19991118 A 2910 2781032756 LINE SWRNGN SA226 SA226AT 8780405 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL HYDRAULIC SYS CRACKED W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 8306 P54184C BU8497 (CAN) WHILE TAXIING TO THE PARKING AREA AFTER LANDING, THE HYDRAULIC PRESSURE WARNING LIGHTS ILLUMINATED AND NOSE WHEEL STEERING BECAME DIFFICULT. MAINTENANCE FOUND TOTAL LOSS OF HYDRAULIC SYSTEM FLUID CAUSED BY A CRACKED HYDRAULIC LINE IN THE RIGHT HAND WING LEADING EDGE. LINE AND BOTH HYDRAULIC PUMPS REPLACED. 2 L 7 2 4T 4 T RT A5SW E4WE 6 C P15EA 1999122100001 19991221 00001 NM 1999 12 21 EISA99295 1 19991006 A 2611 774001 SMOKE DETECTOR BOEING 727 7272M7 138407S NM CARGO COMP ACTIVATED A EISA K NONE N FALSE WARNING DE DESCENT 1 SW 07 721RW 21200 NR 4 CARGO COMPARTMENT SMOKE SENSOR ILLUMINATED ON DESCENT. FOUND GAP BETWEEN AFT ENTRY DOOR AND CEILING PANELS. SECUR ED PANELS AND RE-TAPED IT. SYSTEM OPS CHECK PER MM 26-13-0. (M) 2 L 7 3 4F A3WE 1999122200001 19991222 00001 SO 1999 12 22 C2XA99IA553 1 19991012 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT SO FRAME 40 SCORED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 DURING CONTINENTAL EXPRESS C-CHECK, FOUND LOWER FUSELAGE CROSSBEAM SCORED AT FRAME 40. REMOVED AND REPLACED CROSSBEAM I AW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999122300002 19991223 00002 NE 1999 12 23 A6WA990004 2 19990219 A 7320 3039692 PY LINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE NR 1 ENGINE CRACKED A A6WA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 31 334PH 3012 DURING CRUISE, NR 1 ENGINE TORQUE DROPPED TO ZERO, ITT FELL 200 - 300 DEGREES, SHUT DOWN PER CHECKLIST. AIR START ATTEM PTED. NO GOOD. NOTE: AIRCRAFT FLT 7133 WAS EN ROUTE DEN/MTJ AND DIVERTED TO GUC. FOUND PY LINE BROKEN. REMOVED AND REPLACED PY LINE. GROUND RAN AIRCRAFT. OSP CHECK GOOD. ALSO C/W P&W SB 21583. (X) 2 H 7 2 4T 4 T RT A45NM E20NE 1999122300003 19991223 00003 NE 1999 12 23 UF6A990804 3 19990809 A 6111 78650R5D BLADE HAMSTD BAG ATP ATP EU HAMSTD 5500 65500F1 NE NR 1 ENGINE FAILED A UF6A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 GL 31 856AW 10960 4867 864011 2032 DWA - FLT 5718 - DE-ICE CWP ILLUMINATED WITH THE NR 1 PROPELLER LEGEND. MAINTENANCE REMOVED AND REPLACED THE NR 1 PROPE LLER BLADE ON THE NR 1 SIDE. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 6 C P13NE 1999122300004 19991223 00004 NM 1999 12 23 AALA991419 1 19990920 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AN 29425 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS CABIN INOPERATIVE. REPAIRED EMERG ENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1999122300005 19991223 00005 SO 1999 12 23 ASOA99109 1 19991005 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 131AM 22434 120158 DURING INSPECTION, EMERGENCY BATTERY PACK FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PAC K. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1999122300006 19991223 00006 NM 1999 12 23 TSAA9933483 1 19991127 A 3350 1000679 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY DUE TO DIM LIGHTS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4F RT A16WE 1999122300007 19991223 00007 NM 1999 12 23 TSAA9933484 1 19991127 A 3350 86210151 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED AFT EMERGENCY CONTROL UNIT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999122300008 19991223 00008 NM 1999 12 23 TSAA9933485 1 19991127 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED 1 THROUGH 6 FLOOR LIGHT EMERGENCY BATTERY PACKS DUE TO BEING INOPERABLE IN TEST. OPS CHECK OK. AIRCRAFT RETUR NED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999122300009 19991223 00009 NM 1999 12 23 TSAA9933486 1 19991128 A 3350 900835A BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED LEFT AND RIGHT CENTER PASSENGER EMERGENCY BATTERY CARTRIDGE DUE TO INOPERABLE. OPS CHECK OKAY. AIRCRAFT RETUR NED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999122300010 19991223 00010 NM 1999 12 23 TSAA9933482 1 19991127 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED BATTERY PACK FOR NR 5 POSITION FLOOR LIGHT DUE TO INOPERABLE. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4F RT A16WE 1999122300011 19991223 00011 NM 1999 12 23 ASAA9910250 1 19991020 A 3397 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE R1 OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RE-CONNECTED R-1 OVERHEAD L IGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300012 19991223 00012 NM 1999 12 23 ASAA9910251 1 19991021 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 11 AND 13 WERE ONLY PICKING UP ONE RECEIVE R INDICATION. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300013 19991223 00013 NM 1999 12 23 ASAA9910252 1 19991024 A 3350 873100211 LIGHT BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBL Y AND THE LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300014 19991223 00014 NM 1999 12 23 ASAA9940148 1 19990916 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF THE EMERGENCY EXIT FLOOR TRACK LIGHT WIRING WAS FOUND DISCONNECTE D. RE-CONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300015 19991223 00015 NM 1999 12 23 ASAA9940149 1 19990918 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, ONE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE BETWEEN AFT LAVS. REPLACED L IGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300016 19991223 00016 NM 1999 12 23 ASAA9940150 1 19990920 A 3397 WIRE BOEING 737 7374Q8 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - PRIOR TO FLT 364, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 20-24. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300017 19991223 00017 NM 1999 12 23 ASAA9940151 1 19990926 A 3350 8100022601 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-17. REPLACED LI GHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300018 19991223 00018 NM 1999 12 23 ASAA9940152 1 19990928 A 3397 WIRE BOEING 737 7374Q8 NM CABIN FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 YVR - PRIOR TO FLT 684, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-15. CONTRACT MAINTENANC E REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300019 19991223 00019 NM 1999 12 23 ASAA9940153 1 19990928 A 3397 WIRE BOEING 737 7374Q8 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 PDX - PRIOR TO FLT 440 SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE MID-CABIN AREA. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300020 19991223 00020 NM 1999 12 23 ASAA9940154 1 19991005 A 3350 8100022601 LIGHT BOEING 737 737490 1384715 NM CABIN INOPERABLE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 797AS 28892 SEA - DURING MAINTENANCE CHECK THE AFT EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERABLE. REPLACED LIGHT ASSEMBLY A ND THE LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300021 19991223 00021 NM 1999 12 23 ASAA9940155 1 19991012 A 3397 WIRE BOEING 737 737490 1384715 NM ROW 19 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 792AS 28887 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE AT ROWS 15-19. RECONNECTED WIRING AND LIGHTS AT ROW 19 AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300022 19991223 00022 NM 1999 12 23 ASAA9940156 1 19991012 A 3397 WIRE BOEING 737 7374Q8 NM ROW 21 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - PRIOR TO FLT 394, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE AND LENSES MISSING AT ROWS 21 AND 22 . REPLACED LENSES AT ROWS 21 AND 22. RELAMPED LIGHT AT ROW 22, LIGHT OPERATED NORMALLY. EMERGENCY EXIT FLOOR TRACK LI GHT AT ROW 21 WAS STILL INOPERABLE. RELEASED PER ME 33-33-19C. SUBSEQUENTLY, RECONNECTED WIRING/LIGHT AT ROWS 21 AND L IGHT OPERATED NORMALLY. REF: OPER CONTROL NR 99ZZZX4626. (X) 2 L 7 2 4F RT A16WE 1999122300023 19991223 00023 NM 1999 12 23 99ZZZX4626 1 19991012 A 3350 LENS BOEING 737 7374Q8 NM ROWS 21 & 22 MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - PRIOR TO FLT 394, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE AND LENSES MISSING AT ROWS 21 AND 22 . REPLACED LENSES AT ROWS 21 AND 22. RELAMPED LIGHT AT ROW 22, LIGHT OPERATED NORMALLY. EMERGENCY EXIT FLOOR TRACK LI GHT AT ROW 21 WAS STILL INOPERABLE. RELEASED PER ME 33-33-19C. SUBSEQUENTLY, RECONNECTED WIRING/LIGHT AT ROWS 21 AND L IGHT OPERATED NORMALLY. REF: OPER CONTROL NR ASAA9940156. 2 L 7 2 4F RT A16WE 1999122300024 19991223 00024 NM 1999 12 23 ASAA9940157 1 19991021 A 3350 S283T0143 BATTERY PACK BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 760AS 25098 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN OPERATED NORMALLY INITIAL LY AND THEN BECAME INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300025 19991223 00025 NM 1999 12 23 ASAA9940161 1 19991102 A 3397 WIRE BOEING 737 7374Q8 NM ROWS 20 & 23 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 PDX - PRIOR TO FLT 602, THE FLOOR TRACK LIGHT COVER WAS FOUND LOOSE AT ROW 20. MAINTENANCE INSPECTED AND FOUND LIGHTS T O BE INOPERATIVE. RECONNECTED WIRING AT ROWS 20 AND 23. LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300026 20000609 00026 NM 2000 6 9 ASAA9940162 1 19991111 A 2450 HARNESS BOEING 737 7374Q8 NM FUSELAGE FAILED A ASAA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 NM 01 772AS 25105 PDX-ATB OF F500 DUE TO MULTIPLE CIRCUIT BREAKERS POPPED. AIRCRAFT RETURNED TO PDX. PDX MAINTENANCE INSPECTED AND FOUND A FAILURE OF THE WIRE BUNDLE INSULATION AT BS 410, WL 203, RBL 58 (BEHIND LINER IN FORWARD CARGO COMPARTMENT AFT OF E/E BULKHEAD AND FORWARD OF THE FORWARD CARGO DOOR). MAINTENANCE REPLACED THE WIRING ON A/C 772. THERE WERE NO SYSTEM PRO BLEMS FOUND DURING THE REPAIR OR SUBSEQUENT SYSTEM CHECKS THAT WOULD HAVE CAUSED THE WIRING TO OVERLOAD. EO 2400-01047 WAS ACCOMPLISHED ON THE 737-400 FLEET WITH NO EVIDENT SYSTEM FINDINGS. BASED ON THESE FINDINGS IT WOULD INDICATE THAT T HE DISCREPANCY ON A/C 772 WAS AN ISOLATED OCCURANCE OF WIRE CHAFING. (M) 2 L 7 2 4F RT A16WE 1999122300027 19991223 00027 NM 1999 12 23 ASAA9940163 1 19991113 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 PDX - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE. RECONNECTED WIRI NG AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300028 19991223 00028 WP 1999 12 23 ASAA9980189 1 19990907 A 3350 014597101 BATTERY MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERABLE. REPLACED THE BAT TERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999122300029 19991223 00029 WP 1999 12 23 ASAA9980190 1 19990908 A 3350 1001191 LIGHT MIDLANDROSS DOUG DC9 DC982 3022082 WP CABIN INOPERABLE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 28474 11945 0653 49235 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERABLE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. PART TC: 17,240. (X) 2 L 7 2 4F A6WE 1999122300030 19991223 00030 WP 1999 12 23 ASAA9980191 1 19990909 A 3350 014597101 BATTERY MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERABLE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999122300031 19991223 00031 WP 1999 12 23 ASAA9980192 1 19990913 A 3350 0105606003 LAMP GULTON DOUG DC9 DC983 3022083 WP ROW 23 FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 23 WAS FOUND INOPERATIVE. REPLACED DEFECTIVE LAM P MODULE AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999122300032 19991223 00032 WP 1999 12 23 ASAA9980194 1 19990922 A 3350 FUSE DOUG DC9 DC982 3022082 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE FUSE IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999122300033 19991223 00033 WP 1999 12 23 ASAA9980195 1 19990922 A 3350 8039111 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 PHX - DURING C-CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 13 THROUGH 20. REPLACED PACK BA TTERIES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999122300034 19991223 00034 WP 1999 12 23 ASAA9980196 1 19990927 A 3350 60030431 POWER SUPPLY MIDLANDROSS DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE PWOER USPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1999122300035 19991223 00035 WP 1999 12 23 ASAA9980198 1 19990930 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 PHX - PRIOR TO DEPARTURE OF FLT 721, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1999122300036 19991223 00036 NM 1999 12 23 USAASB99282 1 19991128 A 2910 SEAL BOEING 737 737201 1384454 NM PCU FAILED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 255AU 22797 MKE - FLT 2745 - ABOUT 15 MINUTES OUT FROM MKE, THE B-HYDRAULIC SYSTEM LOST PRESSURE AND A-HYDRAULIC SYSTEM QUANTITY DRO PPED TO 1.25 GALLONS. THE LOW PRESS AND LOW QTY LIGHTS ILLUMINATED. CAPTAIN TURNED OFF B-PUMPS WITHIN 15 SECONDS OF LO W PRESS LIGHTS ILLUMINATING. CAPTAIN DECLARED AN EMERGENCY AND MADE A NORMAL LANDING AT MKE. AIRCRAFT TAXIED TO THE G ATE UNDER ITS OWN POWER. MAINT FOUND A SEAL ON THE B-SYSTEM AILERON POWER CONTROL UNIT BAD. REMOVED AND REPLACED AILER ON POWER CONTROL UNIT (PN 65-44761-17) IN ASSOCIATION WITH MM 27-11-71. INSPECTED ALL HYD FILTERS FOR CONTAMINANTS. N O CONTAMINANTS FOUND. REPLACED FILTERS. SERVICED AIRCRAFT HYD SYSTEMS. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F A16WE 1999122300037 19991223 00037 NM 1999 12 23 USAASB99284 1 19991130 A 3260 DT2RA7 SWITCH BOEING 737 737201 1384454 NM E/E BAY MISADJUSTED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 248US 22755 TPA - FLT 8030 - AFTER TAKEOFF DURING LANDING GEAR RETRACTION, THE LANDING GEAR WARNING HORN AND ALL THREE RED GEAR LIGH TS ILLUMINATED AND REMAINED ON. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WTHOUT FURTHER INCIDENT. NO EMERGENCY WAS D ECLARED. MAINTENANCE ADJUSTED THE S139 THRUST LEVER ACTUATED LANDING GEAR WARNING HORN SWITCH PER MM. OPERATIONAL CHEC K GOOD PER MM. FUNCTIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION GOOD PER MM. (X) 2 L 7 2 4F A16WE 1999122300038 19991223 00038 NM 1999 12 23 USAA991300 1 19991121 A 5330 SKIN BOEING 737 737201 1384454 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 53027 21818 CLT - DURING RON, FOUND .8750 INCH CRACK IN FUSELAGE SKIN AT BS 787 STR 18R. DAMAGE CUT OUT. INSTALLED REPAIR DOUBLER (12 INCHES BY 6.5 INCHES) PER SRM 53-00-01 FIG 201. (X) 2 L 7 2 4F A16WE 1999122300039 19991223 00039 NM 1999 12 23 USAASB99285 1 19991130 A 2131 7638101 CONTROLLER BOEING 737 7372B7 1384560 NM E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 271AU 29404 22883 BDL - FLT 2743 - AIRCRAFT DEPARTED BDL WITH MEL 21-14A APPLIED, CABIN PRESSURE CONTROL SYSTEM AUTOMATIC MODE INOPERABLE. AFTER TAKEOFF, THE CAPTAIN REPORTED THE STANDBY MODE WOULD NOT WORK AND THE AIRCRAFT WOULD NOT PRESSURIZE PROPERLY. F LIGHT RETURNED TO FIELD AT BDL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. OPERATIONAL CHECK GOOD. CLEARED MEL 21-14A. (X) 2 L 7 2 4F A16WE 1999122300040 19991223 00040 NM 1999 12 23 USAA991342 1 19991129 A 5330 SKIN BOEING 737 737201 1384454 NM STA 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 239US 49024 22354 PIT - DURING RON VISIT, FOUND 1.50 INCH CRACK IN SKIN AT STA 727B, STR 16L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 1. ( X) 2 L 7 2 4F A16WE 1999122300041 19991223 00041 NM 1999 12 23 USAA991245 1 19991122 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 48642 22198 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT FLOORBEAM T-CAP FORWARD SURFACE STA 1640, RBL 9, CORROSION LEVEL 2. INSTALLED NEW T-CAP PER TR 53-15-01. (X) 2 L 7 2 4F RT A2NM 1999122300042 19991223 00042 NM 1999 12 23 USAA991249 1 19991122 A 5311 FRAME BOEING 757 757225 1384959 NM BS 1580 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 48642 22198 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A .250 INCH FRAME CRACK AROUND RIVET AT BS 1580, LBL 23. TRIMMED OUT DA MAGE AND INSTALLED DOUBLER PER TR 53-60-01. (X) 2 L 7 2 4F RT A2NM 1999122300043 19991223 00043 EU 1999 12 23 USAAF99055 1 19991201 A 2120 UNKNOWN FOKKER F28 F28MK0100 4990807 EU NR 2 PACK ODOR A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 882US 11334 ORD - FLT 1999 - STRONG OIL BURNING ODOR DETECTED DURING TAKEOFF AND CLIMB-OUT. ODOR WENT AWAY ONCE THE NR 2 PACK WAS T URNED OFF. MAINTENANCE OPS CHECKED NR 2 PACK FOR OIL ODOR, BUT DID NOT DETECT ANY ODOR. PACK OK FOR SERVICE. (X) 2 L 7 2 4F RT 1999122300044 19991223 00044 NM 1999 12 23 USAASB99276 1 19991121 A 3350 3114981 SOCKET BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 TPA - MAINTENANCE FOUND THE RIGHT FUSELAGE EMERGENCY EGRESS LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE SOCK ET ASSEMBLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1999122300045 19991223 00045 NM 1999 12 23 USAASB99281 1 19991129 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 265AU 22962 CLE - MAINTENANCE FOUND BOTH AFT DOOR EXTERIOR EMERGENCY LIGHTS AND INTERIOR LOWER EXIT SIGN LIGHTS INOPERABLE. MAINTEN ANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1999122300046 19991223 00046 NM 1999 12 23 USAASB99280 1 19991119 A 3350 900835A BATTERY BOEING 737 737201 1384454 NM COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 265AU 22962 ALB - MAINTENANCE FOUND THE COCKPIT EMERGENCY EXIT SIGN INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OP ERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1999122300047 19991223 00047 EA 1999 12 23 MASA99174 1 19991027 A 3350 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5803 - PHL-HPN - DURING STANDARD PRE-FLIGHT CHECK, THE CREW NOTED AN EMERGENCY LIGHT INOPERATIVE LOCATED ON THE OUTS IDE FUSELAGE NEAR THE PASSENGER DOOR. MAINTENANCE WAS CALLED OUT AND REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHE CKED GOOD AND THE AIRCRAFT WAS READY FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 1999122300048 19991223 00048 EA 1999 12 23 MASA99179 1 19991123 A 3350 GE1317 LAMP BRUCE CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37218 7218 PHL/MKE - FLT 5807 - DURING A STANDARD PRE-FLIGHT INSPECTION, THE CREW NOTED A CABIN OVERHEAD EMERGENCY LIGHT WAS INOPER ABLE. MAINTENANCE WAS CALLED OUT AND REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT. OPS CHECKED GOOD AND THE AIRCR AFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999122300049 19991223 00049 NM 1999 12 23 MASA99180 1 19991123 A 3350 6038443 BATTERY PACK BRUCE DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 PHX/BFL - FLT 6337 - IN PHX DURING STANDARD PRE-FLIGHT CHECK, THE CREW NOTED THE EMERGENCY LIGHTS IN 6A WERE INOPERABLE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE EMERGENCY BATTERY PACKS. OPS CHECKED GOOD AND THE AIRCRAFT WAS RET URNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1999122300050 19991223 00050 WP 1999 12 23 USAAD99169 1 19991201 A 3350 P2010014 LIGHT DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918VJ 48138 LGA - THE FORWARD ENTRY DOOR EMERGENCY SLIDE LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGEN CY SLIDE LIGHT ASSEMBLY. (X) 2 L 7 2 4F A6WE 1999122300051 19991223 00051 WP 1999 12 23 USAAD99168 1 19991128 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP FUSELAGE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 974VJ 47130 IND - THE TAIL CONE ACTIVATED EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (X) 2 L 7 2 4F A6WE 1999122300052 19991223 00052 NM 1999 12 23 ASAA9910237 1 19990904 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER STROBE LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERAT ED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300053 19991223 00053 NM 1999 12 23 ASAA9910238 1 19990904 A 3350 6104781 BATTERY GRIMES BOEING 737 737210C 1384459 NM ROW 14 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK THE EMERGENCY EXIT LIGHTS AT ROW 14 AND THE SMOKE BARRIER SIGN WOULD NOT TEST PROPERLY. R EPLACED BATTERIES AT ROW 14 AND SMOKE BARRIER, LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR 99ZZZX4627. (X) 2 L 7 2 4F A16WE 1999122300054 19991223 00054 NM 1999 12 23 99ZZZX4627 1 19990904 A 3350 86210144 BATTERY INTVLV BOEING 737 737210C 1384459 NM SIGN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK THE EMERGENCY EXIT LIGHTS AT ROW 14 AND THE SMOKE BARRIER SIGN WOULD NOT TEST PROPERLY. R EPLACED BATTERIES AT ROW 14 AND SMOKE BARRIER, LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR ASAA9910238. 2 L 7 2 4F A16WE 1999122300055 19991223 00055 NM 1999 12 23 ASAA9910239 1 19990907 A 3350 86210144 BATTERY PACK INTVLV BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK THE R2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300056 19991223 00056 NM 1999 12 23 ASAA9910241 1 19990910 A 3350 8821004 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ON PALLET 8-7. REPLACED BAT TERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300057 19991223 00057 NM 1999 12 23 ASAA9910242 1 19990920 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND INOPERATIVE AT PALLETS 3-10 AND 7-4. REPLACED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300058 19991223 00058 NM 1999 12 23 ASAA9910240 1 19990907 A 3350 873203041 TRANSMITTER INTVLV BOEING 737 7372X6C 1384552 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - PRIOR TO FLT 63, THE EMERGENCY FLOOR TRACK LIGHTING AND THE R1 AND L2 DOOR RECEIVERS WERE FOUND INOPERATIVE. REPL ACED THE EMERGENCY FLOOR TRACK LIGHTING MID-CABIN TRANSMITTER, THE R1 DOOR RECEIVER BATTERIES, AND THE L2 DOOR RECEIVER. ALL LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NRS 99ZZZX4628 AND 99ZZZX4629. (X) 2 L 7 2 4F RT A16WE 1999122300059 19991223 00059 NM 1999 12 23 99ZZZX4628 1 19990907 A 3350 86210144 RECEIVER INTVLV BOEING 737 7372X6C 1384552 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - PRIOR TO FLT 63, THE EMERGENCY FLOOR TRACK LIGHTING AND THE R1 AND L2 DOOR RECEIVERS WERE FOUND INOPERATIVE. REPL ACED THE EMERGENCY FLOOR TRACK LIGHTING MID-CABIN TRANSMITTER, THE R1 DOOR RECEIVER BATTERIES, AND THE L2 DOOR RECEIVER. ALL LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NRS ASAA9910240 AND 99ZZZX4629. 2 L 7 2 4F RT A16WE 1999122300060 19991223 00060 NM 1999 12 23 99ZZZX4629 1 19990907 A 3350 873100211 BATTERY INTVLV BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - PRIOR TO FLT 63, THE EMERGENCY FLOOR TRACK LIGHTING AND THE R1 AND L2 DOOR RECEIVERS WERE FOUND INOPERATIVE. REPL ACED THE EMERGENCY FLOOR TRACK LIGHTING MID-CABIN TRANSMITTER, THE R1 DOOR RECEIVER BATTERIES, AND THE L2 DOOR RECEIVER. ALL LIGHTS OPERATED NORMALLY. REF: OPER CONTROL NRS ASAA9910240 AND 99ZZZX4628. 2 L 7 2 4F RT A16WE 1999122300061 19991223 00061 NM 1999 12 23 ASAA9910244 1 19991002 A 3350 883200312 RECEIVER INTVLV BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 18 WOULD NOT TEST. REPLACED RECEIVER AND LI GHTS TESTED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300062 19991223 00062 NM 1999 12 23 ASAA9910245 1 19991005 A 3350 8731002142 SIGN INTVLV BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - PRIOR TO FLT 65, THE EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER WAS FOUND INOPERATIVE. REPLACED THE EXIT IDENTIFIE R AND THE LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300063 19991223 00063 NM 1999 12 23 ASAA9910246 1 19991008 A 3350 883200312 RECEIVER INTVLV BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - PRIOR TO FLIGHT 41, THE EMERGENCY EXIT FLOOR PROXIMITY LIGHTS WERE FOUND INOPERATIVE AT PALLET 7-4. REPLACED RECE IVER AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. REF: OPER CONTROL 99ZZZX4630. (X) 2 L 7 2 4F A16WE 1999122300064 19991223 00064 NM 1999 12 23 99ZZZX4630 1 19991008 A 3350 8821004 BATTERY INTVLV BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - PRIOR TO FLIGHT 41, THE EMERGENCY EXIT FLOOR PROXIMITY LIGHTS WERE FOUND INOPERATIVE AT PALLET 7-4. REPLACED RECE IVER AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. REF: OPER CONTROL ASAA9910246. 2 L 7 2 4F A16WE 1999122300065 19991223 00065 NM 1999 12 23 ASAA9910247 1 19991016 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING ON SEAT PALLET 4-9 WAS FOUND INOPERATIVE. REPL ACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999122300066 19991223 00066 NM 1999 12 23 ASAA9910249 1 19991020 A 3350 88210144 BATTERY INTVLV BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, R1 DOOR LOWER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OP ERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999122300067 19991223 00067 NM 1999 12 23 SWAA992061 1 19991212 A 5330 6545835 SKIN BOEING 737 7375H4 138449D NM FUSELAGE BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 524SW 26566 AIR TURNBACK, SEVERAL BIRD STRIKES DURING CLIMB OUT. C/W BIRD STRIKE INSPECTION AND FOUND DAMAGED NOSE RADOME, RADAR AN TENNA, NR 2 KRUGER FLAP BELL CRANK ARM, AND FUSELAGE SKIN STRUCTURE DAMAGED FWD OF E/E DOOR. NO ENGINE INGESTION NOTED . REMOVED AND REPLACED NOSE RADOME, RADAR ANTENNA, NR 2 KRUGER FLAP BELL CRACK ARM AND REPAIRED FUSELAGE SKIN STRUCTURE . 2 L 7 2 4F RT A16WE 1999122300068 19991223 00068 NM 1999 12 23 SWAA992062 1 19991214 A 5210 507945 SEAL BOEING 737 7373G7 1384595 NM PAX DOOR LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 690SW 23783 AIR TURNBACK, LOUD PRESSURIZATION AIR LEAK AROUND FWD ENTRY DOOR LOWER HINGE COVER PLATE AREA. REPOSITIONED FWD ENTRY D OOR LOWER HINGE SECTION OF DOOR FRAME SEAL PER MM. C/W PHASE 1 OVERWEIGHT LANDING INSPECTON. NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1999122300069 19991223 00069 NM 1999 12 23 SWAA992063 1 19991214 A 5753 6546430 SKIN BOEING 737 7372T4 1384492 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D CHECK, FOUND LT AND RT WING T/E INBOARD FORE FLAPS DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACE D BOTH FORE FLAP ASSY'S PER MM. 2 L 7 2 4F A16WE 1999122300070 19991223 00070 NM 1999 12 23 SWAA992064 1 19991214 A 5320 65C27314 CLIP BOEING 737 7375H4 138449D NM E/E BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED, BS 312, STRINGER 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 1999122300071 19991223 00071 NM 1999 12 23 SWAA992065 1 19991214 A 2530 832210 COFFEEMAKER BOEING 737 7372H4 138448C NM GALLEY FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 64SW 22062 BURNING ELECTRICAL SMELL IN AFT GALLEY. SMELL COMING FROM UPPER COFFEE MAKER HEATING BLANKET WHICH HAD RESIDUAL MOISTUR E. REMOVED MOISTURE FROM HEATING BLANKET. OPS CK GOOD. 2 L 7 2 4F A16WE 1999122300072 19991223 00072 NM 1999 12 23 SWAA992066 1 19991215 A 5320 149A76562 PANEL BOEING 737 7377H4 NM MLG WW MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 714CB 27848 DURING SCHEDULED SERVICE CHECK, FOUND 9 INCHES OF FILLET PANEL MISSING AFT OF RT MLG WHEEL WELL CUT OUT. REPAIRED PANEL PER SWA RA NR 1-753-2186, REV 1. 2 L 7 2 4F RT A16WE 1999122300073 19991223 00073 NM 1999 12 23 SWAA992067 1 19991215 A 3350 D717001100 BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 714CB 27848 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND BATTERY C HARGER PER MM. 2 L 7 2 4F RT A16WE 1999122300074 19991223 00074 NM 1999 12 23 SWAA992068 1 19991215 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 609SW 27929 EEPLS LIGHT INOP AT OVERWING EXIT. REPAIRED TRACK WIRING PER MM. 2 L 7 2 4F RT A16WE 1999122300075 19991223 00075 NM 1999 12 23 SWAA992069 1 19991215 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT OUTBOARD T/E FLAPS DELAMINATED AT INBOARD ENDS. REMOVED AND REPLACED T/ E FLAPS PER MM. 2 L 7 2 4F RT A16WE 1999122300076 19991223 00076 NM 1999 12 23 SWAA992070 1 19991215 A 5730 65C26714 SKIN BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED C2 CHECK, FOUND RT WING L/E CRACKED AT NR 4 SLAT ACTUATOR CUT OUT. REPAIRED SKIN PER SWA RA NR 1-257-0 782. 2 L 7 2 4F A16WE 1999122300077 19991223 00077 NM 1999 12 23 SWAA992071 1 19991215 A 3320 6558220 LENS BOEING 737 7373H4 1384600 NM GALLEY LIGHT MELTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 AFT GALLEY HAS A BURNING ODOR. FOUND AFT GALLEY WORK LIGHT BULB MELTING LENS ASSY. PULLED/COLLARED WORKLIGHT C/B AND D EFERRED PER MEL. 2 L 7 2 4F RT A16WE 1999122300078 19991223 00078 NM 1999 12 23 SWAA992072 1 19991215 A 7930 332A1041 INDICATOR BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 364SW 26575 AIR TURNBACK, AFTER TAKEOFF, NR 2 ENG LOW OIL PRESS LIGHT ILLUMINATED SEVERAL TIMES. OIL PRESS INDICATOR OPERATED NORMA L. FOUND FAULTY NR 2 ENG LOW OIL PRESS LIGHT SOCKET. ALL ENG INDICTORS NORMAL. DEFERRED LIGHT PER MEL. 2 L 7 2 4F RT A16WE 1999122300079 19991223 00079 1999 12 23 SWAA992057 4 19991213 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 615SW 27698 AFT SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999122300080 19991223 00080 NM 1999 12 23 SWAA992058 1 19991213 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 615SW 27698 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 1999122300081 19991223 00081 NM 1999 12 23 SWAA992059 1 19991213 A 3260 3186301001036 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 07 392SW 27379 ON FINAL APPROACH, RT MLG GREEN INDICATOR LIGHT FAILED TO ILLUMINATE. ABORTED THE APPOACH AND ALTERNATE GEAR EXTENSION WAS USED. REMOVED AND REPLACED RT MLG KORRY LIGHT ASSY. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999122300082 19991223 00082 NM 1999 12 23 SWAA992060 1 19991213 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM BS 400 - 420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN HAS A 7.25 INCHES LONG CRACK, BS 400-420, JUST ABOVE SKIN L AP, STRINGER 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999122300083 19991223 00083 NM 1999 12 23 SWAA992050 1 19991212 A 3350 101073 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720WN 27854 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999122300084 19991223 00084 NM 1999 12 23 SWAA992051 1 19991212 A 5320 6969854 DOOR FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FAME CRACKED ON AFT LOWER GUSSET. REPAIRED FRAME PER BOEING DRAW ING. 2 L 7 2 4F RT A16WE 1999122300085 19991223 00085 NM 1999 12 23 SWAA992052 1 19991212 A 3397 BR2013 WIRE BOEING 737 7373H4 1384600 NM ROW 12 DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 EEPLS INOP. RECONNECTED WIRING AT ROW 12 PER MM. 2 L 7 2 4F RT A16WE 1999122300086 19991223 00086 NM 1999 12 23 SWAA992053 1 19991212 A 5754 65C26602311A SKIN BOEING 737 7373Q8 1384670 NM LE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 317WN 24068 DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DISBONDED ON OUTBOARD END. REPAIRED SLAT PER SWA RA NR 1-357-0779. 2 L 7 2 4F RT A16WE 1999122300087 19991223 00087 NM 1999 12 23 SWAA992054 1 19991213 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 616, RBL 64, WL 201. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999122300088 19991223 00088 NM 1999 12 23 SWAA992055 1 19991213 A 5311 6546546 FRAME BOEING 737 7372T4 1384492 NM BS 727B CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED, BS 727B, RBL 12, WL 150. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999122300089 19991223 00089 NM 1999 12 23 SWAA992056 1 19991213 A 3350 6104879 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 68SW 22357 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP ON BOTH AFT CABIN DOORS. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM. 2 L 7 2 4F A16WE 1999122300090 19991223 00090 1999 12 23 SWAA992039 4 19991210 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999122300091 19991223 00091 1999 12 23 SWAA992040 4 19991211 A 2565 6567380 LENS BOEING 737 7373H4 1384600 NM EVAC SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 648SW 27718 AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LENS LOOSE. SECURED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999122300092 19991223 00092 NM 1999 12 23 SWAA992041 1 19991210 A 3233 6546109 CLEVIS BOEING 737 7373H4 1384600 NM RT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED SERVICE CHECK, FOUND THROUGH ULTRASONIC INSPECTION, RT MLG WALKING BEAM ARM CLEVIS CRACKED ON AFT LUG. REMOVED AND REPLACED RT MLG BEAM ARM CLEVIS PER MM. 2 L 7 2 4F RT A16WE 1999122300093 19991223 00093 1999 12 23 SWAA992042 4 19991210 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR SHIFTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 93SW 22965 AFT ENTRY DOOR EVACUATON SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999122300094 19991223 00094 NM 1999 12 23 SWAA992043 1 19991210 A 5753 65C30462 SKIN BOEING 737 7372T4 1384492 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D CHECK, FOUND LEFT INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2 L 7 2 4F A16WE 1999122300095 19991223 00095 NM 1999 12 23 SWAA992044 1 19991210 A 5312 963820 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LEFT AND RIGHT OUTBOARD CHORDS CRACKED AT WL 207. REMOVED AND REPLAC ED BOTH CHORD SECTIONS PER SRM. 2 L 7 2 4F RT A16WE 1999122300096 19991223 00096 NM 1999 12 23 SWAA992045 1 19991210 A 3350 65C34691 LENS BOEING 737 7373H4 1384600 NM ROW 5 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY LIGHT LENS MISSING AT ROW 5DEF. REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 1999122300097 19991223 00097 NM 1999 12 23 SWAA992046 1 19991210 A 5320 6557463 BRACKET BOEING 737 7373H4 1384600 NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED A ND REPLACED BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 1999122300098 19991223 00098 NM 1999 12 23 SWAA992047 1 19991211 A 5320 6560552 ANGLE BOEING 737 7375H4 138449D NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED D CHECK, FOUND FUSELAGE INNER SKIN WEB ANGLES CRACKED, BS 291, BETWEEN STRINGERS 10R-12R. REMOVED AND REPLACED ANGLES PER SRM. 2 L 7 2 4F RT A16WE 1999122300099 19991223 00099 NM 1999 12 23 SWAA992048 1 19991211 A 5320 6546559 SHEAR TIE BOEING 737 7375H4 138449D NM BS 967 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED, BS 967, STRINGER 6L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 1999122300100 19991223 00100 NM 1999 12 23 SWAA992049 1 19991211 A 5320 65C27314 CLIP BOEING 737 7375H4 138449D NM BS 685 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED, BS 685, STRINGER 11L, AND BS 706, STRINGERS 11L AND 11R. REMOVE D AND REPLACED CLIPS PER SRM. 2 L 7 2 4F RT A16WE 1999122300101 19991223 00101 NM 1999 12 23 SWAA992013 1 19991206 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 611SW 27697 EEPLS TRACK ASSY PULLED UP FWD OF OVERWING EXITS. SECURED TRACK ASSY PER MM. 2 L 7 2 4F RT A16WE 1999122300102 19991223 00102 1999 12 23 SWAA992014 4 19991205 A 2565 D31354 RELEASE RING BOEING 737 7373H4 1384600 NM EVAC SLIDE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE RELEASE RING MISSING SOLDER. SOLDERED RING PER MM. 2 L 7 2 4F RT A16WE 1999122300103 19991223 00103 NM 1999 12 23 SWAA992015 1 19991205 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED C2 CHECK, FOUND LEFT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED ON INBOARD SIDE. REMOVED AND REP LACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999122300104 19991223 00104 NM 1999 12 23 SWAA992016 1 19991205 A 3350 610478 BATTERY BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY AISLE EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999122300105 19991223 00105 NM 1999 12 23 SWAA992017 1 19991205 A 5313 6552988 STRINGER BOEING 737 7375H4 138449D NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES CRACKED, BS 907, STRINGERS 4L AND 4R. REPAIRED SPLICES PER SRM. 2 L 7 2 4F RT A16WE 1999122300106 19991223 00106 NM 1999 12 23 SWAA992018 1 19991205 A 5320 6557463 BRACKET BOEING 737 7375H4 138449D NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR BOTH EVACUATION SLIDE ATTACH FLOOR BRACKETS CORRODED. REMOVED AND REPLAC ED BOTH BRACKETS PER SRM. 2 L 7 2 4F RT A16WE 1999122300107 19991223 00107 NM 1999 12 23 SWAA992019 1 19991207 A 5330 6518420 SKIN BOEING 737 7375H4 138449D NM BS 183 - 188 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND FUSELAGE EXTERNAL SKIN CREASED BETWEEN BS 183-188, WL 190 RH SIDE. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 1999122300108 19991223 00108 NM 1999 12 23 SWAA992020 1 19991206 A 5320 6567380 BRACKET BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 605SW 27956 FWD ENTRY DOOR EVACUATION SLIDE LEFT GIRT BAR HOLDER LOOSE. TIGHTENED HOLDER PER MM. 2 L 7 2 4F RT A16WE 1999122300109 19991223 00109 NM 1999 12 23 SWAA992021 1 19991205 A 5311 AND10138 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 HORIZONTAL CHORD CRACKED, RBL 28. REMOVED AND REPLACED CHORD SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999122300110 19991223 00110 NM 1999 12 23 SWAA992022 1 19991206 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 1999122300111 19991223 00111 NM 1999 12 23 SWAA992023 1 19991207 A 5311 AND10138 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD HORIZONTAL CHORD CRACKED, LBL 28. REPAIRED CHORD PER SWA RA NR 1-353 -2184. 2 L 7 2 4F RT A16WE 1999122300112 19991223 00112 NM 1999 12 23 SWAA992024 1 19991206 A 5315 6553844 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 794 FLOORBEAM CORRODED, RBL 8. REPAIRED BEAM PER SWA RA NR 1-353-2182. 2 L 7 2 4F RT A16WE 1999122300113 19991223 00113 NM 1999 12 23 AWXA9900476 1 19991216 A 7932 SEL0C4W INDICATOR BOEING 737 7373S3 1384711 NM COCKPIT FAILED A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 312AW 41165 100 24060 AIR TURN-BACK, NR 1 ENG OIL PRESS BELOW 20 PSI, OIL TEMP NML. RETURNED TO PHX PER MX. REPLACED OIL PRESS INDICATOR PER BMM 79-32-02 P401 LK AND OPS CK GOOD. OTHER PARTS CHANGED, UNIT, LUBRICATING. A/C HAS EXPERIENCED SEVERAL OIL PRESS F LUX PROBLEMS, 3 OIL PRESS TRANSMITTERS AND A PRESS INDICATOR HAVE BEEN CHANGED SINCE 11 AUG 99. 2 L 7 2 4F RT A16WE 1999122300114 19991223 00114 NM 1999 12 23 AWXA9900477 1 19991216 A 3350 900835A BATTERY PACK BOEING 737 7372M8 1384483 NM ROW 6 - 14 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 21955 ROW 6-14 EMERGENCY EXIT LIGHTS DID NOT WORK DURING TEST. BATTERY CHARGED BY CONTRACT MAINTENANCE PREVIOUS FLIGHT. REPL ACED AFT EMERGENCY LIGHT BATTERY PACK IN DROP CEILING. OPS CK GOOD RECOMMENDATION. NO RELATED HISTORY. 2 L 7 2 4F A16WE 1999122300115 19991223 00115 NM 1999 12 23 AWXA9900478 1 19991216 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DOOR L-2 OVERHEAD EMERGENCY EXIT LIGHT DOES NOT COME ON WHEN ARMED FROM COCKPIT. REPLACED LIGHT ASSY. OPS CK NORMAL. 2 L 7 2 4F RT A16WE 1999122300116 19991223 00116 NM 1999 12 23 AWXA9900479 1 19991217 A 5315 6545810128 FLOORBEAM BOEING 737 7373G7 1384595 NM FS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 REMOVED DAMAGED T CHORD IAW B737 SRM 51-40-02. FABRICATED T CAP MAT BAC 1505100246 R709117 AND 3 SPLICES MAT 7075 T6 . 063 R73168 IAW B737 SRM 53-10-51 FIG 205. TREATED AND PRIMED ALL PARTS IAW B737 SRM 51-20-01. INSTALLED PARTS IAW B73 7 SRM 50-10-51 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 1999122300117 19991223 00117 NM 1999 12 23 AWXA9900480 1 19991217 A 5315 6545812 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 CABIN FLOORBEAM STA 328 RBL 12 TO RBL 55 ON UPPER CHORD CORRODED BEYOND LIMITS. REMOVED DAMAGED PART PER B737 SRM 53-00 -51. FABRICATED REPLACEMENT FLOORBEAM PER B737 SRM 53-10-51. INSTALLED PER B737 SRM 53-00-51. 2 L 7 2 4F RT A16WE 1999122300118 19991223 00118 NM 1999 12 23 AWXA9900481 1 19991217 A 5315 101362401 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 294 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 CABIN FLOORBEAM STA 294.5 RBL 17 TO 60 CORRODED BEYOND LIMITS ON UPPER CAP. REMOVED DAMAGED AREA AT UPPER T CAP PER B73 7 SRM 51-40-02. FABRICATED PARTS, FROM 10136-2401/7075 -T6 IAW B737 SRM 53-10-51. TREATED AND PRIMED IAW B737 SRM 51- 20-01. 2 L 7 2 4F RT A16WE 1999122300119 19991223 00119 WP 1999 12 23 CALA9901596 1 19991216 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND A 2 AND .125 INCH CRACK IN CANTED BELTFRAME WEB AT LEFT SIDE, STA 1463. THE WEB WAS REMOVED AND REPLAC ED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1999122300120 19991223 00120 WP 1999 12 23 CALA9901597 1 19991215 A 5320 ANGLE DOUG DC9 DC981 3022081 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND ANGLE CORRODED AT STA 1338, LONGERON 18L. A NEW SECTION OF ANGLE WAS SPLICED IN IAW SRM 53-03, FIGURE 14. 2 L 7 2 4F A6WE 1999122300121 19991223 00121 WP 1999 12 23 CALA9901598 1 19991215 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND CENTER CARGO COMPARTMENT LEFT CHANNEL CORRODED UNDER OMNI ROLLERS. A NEW CHANNEL WAS INSTALLED IAW SRM 53-42-01. 2 L 7 3 4F A22WE 1999122300122 19991223 00122 WP 1999 12 23 CALA9901599 1 19991215 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1860 - 1889 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND LAV SUPPORT CORRODED AT STA 1860-1889, BL 0. THE LAV SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALL ED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1999122300123 19991223 00123 WP 1999 12 23 CALA9901600 1 19991215 A 5511 SPAR DOUG DC10 DC1030 3023501 WP HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND A 3 INCH CRACK IN LEFT HORIZONTAL STABILIZER PANEL SIDE UPPER CHORD. THE CHORD WAS REMOVED AND A REPAI R WAS INSTALLED IAW SRM 51-33-01. 2 L 7 3 4F A22WE 1999122300124 19991223 00124 NM 1999 12 23 CALA9901601 1 19991215 A 5320 STRAP BOEING 727 727232 1384082 NM BS 328 - 344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2.5 CRACK IN STRAP UNDER FLOORBEAM IN FORWARD CABIN AREA AT STA 328-344, LBL 50. THE STRAP WAS REPAI RED BY INSTALLING A DOUBLER IAW SRM 51-30-2 AND 51-40-3. 2 L 7 3 4F A3WE 1999122300125 19991223 00125 NM 1999 12 23 CALA9901602 1 19991215 A 5320 BRACKET BOEING 727 727232 1384082 NM BS 1193 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN VERTICAL SUPPORT LOWER END ATTACH BRACKET AT STA 1193, LBL 20. THE BRACKET WAS REMOV ED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300126 19991223 00126 NM 1999 12 23 CALA9901603 1 19991215 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND ATTACH ANGLE CUT AND CORRODED AT C-1 DOOR CUTOUT LOWER FORWARD SECTION, STA 540, STRINGER 26R. THE ANG LE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300127 19991223 00127 NM 1999 12 23 CALA9901604 1 19991215 A 5320 BRACKET BOEING 727 727232 1384082 NM BS 720C CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .75 INCH CRACK IN BRACKET AT FS 720C, S27R. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300128 19991223 00128 NM 1999 12 23 CALA9901605 1 19991215 A 5320 BRACKET BOEING 727 727232 1384082 NM BS 700B CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND BRACKET CORRODED AT FS 700B, S27R. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300129 19991223 00129 NM 1999 12 23 CALA9901606 1 19991216 A 5532 SKIN BOEING 727 727232 1384082 NM VERTICAL STAB DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LEADING EDGE ACCESS PANEL SKIN OF VERTICAL STABILIZER WITH FASTENERS PULLING THROUGH AT STA 134. A DOU BLER WAS INSTALLED IAW SRM 55-30-7, 51-10-6, 51-20-0, AND 51-30-2. 2 L 7 3 4F A3WE 1999122300130 19991223 00130 NM 1999 12 23 CALA9901607 1 19991216 A 5512 PANEL BOEING 727 727232 1384082 NM HORIZONTAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT HORIZONTAL STABILIZER LE PANEL 9202 CORRODED. A NEW PANEL WAS INSTALLED IAW SRM 51-10-5, 51-10-2, A ND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300131 19991223 00131 NM 1999 12 23 CALA9901608 1 19991216 A 5730 SKIN BOEING 727 727232 1384082 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN RT I/B FLAP TRACK FAIRING SKIN. A DOUBLER WAS INSTALLED IAW SRM 51-30-0, 51-10-2, 51 -30-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300132 19991223 00132 NM 1999 12 23 CALA9901609 1 19991216 A 5210 SKIN BOEING 727 727232 1384082 NM PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN L-1 DOOR INNER SKIN AT CUTOUT FOR HANDLE ON LOWER FORWARD SIDE. THE CRACK WAS STOP D RILLED IAW SRM 51-10-1, PAGE 6D, 51-40-2, AND 51-30-1. 2 L 7 3 4F A3WE 1999122300133 19991223 00133 NM 1999 12 23 CALA9901610 1 19991216 A 5720 BRACKET BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN SUPPORT BRACKET AT LEFT WING L/E PANEL NR 6215. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300134 19991223 00134 NM 1999 12 23 CALA9901611 1 19991216 A 5720 ANGLE BOEING 727 727232 1384082 NM BS 760 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB SUPPORT ANGLE CORRODED AT WING CENTER SECTION, STA 760 LOWER TORQUE BOX KEEL AREA. THE ANGLE WAS R EMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1999122300135 19991223 00135 NM 1999 12 23 CALA9901612 1 19991216 A 5541 RIB BOEING 727 727232 1384082 NM RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 CRACK IN UPPER RUDDER AFT UPPER LEFT T/E RIB. A DOUBLER WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999122300136 19991223 00136 NM 1999 12 23 CALA9901613 1 19991216 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 1148 - 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 1148-1166, L26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300137 19991223 00137 NM 1999 12 23 CALA9901614 1 19991216 A 5280 ANGLE BOEING 727 727232 1384082 NM LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN LEFT MLG WING DOOR ANGLE AT T/E LOWER CORNER. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300138 19991223 00138 NM 1999 12 23 CALA9901615 1 19991216 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 780 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LOWER WEB SUPPORT ANGLE CORRODED AT FS 780. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300139 19991223 00139 NM 1999 12 23 CALA9901616 1 19991216 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN STIFFENER AT STA 1183, LBL 60. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INS TALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300140 19991223 00140 NM 1999 12 23 CALA9901617 1 19991216 A 5311 FRAME BOEING 727 727232 1384082 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FRAME BENT AND CRACKED AT UPPER FLANGE, STA 540, L25L. THE FRAME WAS REFORMED AND THE CRACKED AREA WAS TRIMMED OUT IAW SRM 51-40-4. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1999122300141 19991223 00141 NM 1999 12 23 CALA9901618 1 19991216 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 660 - 800 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 660-800, RBL 12. SUPPORT ANGLES WERE INSTALLED IAW SRM 51-40-4 AND 51-30- 3. 2 L 7 3 4F A3WE 1999122300142 19991223 00142 NM 1999 12 23 CALA9901619 1 19991216 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1.4 INCH CRACK IN STIFFENER AT STA 1183, LBL 35. REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-30-2, 51- 10-2, MM 51-20-0, AND ECRA 5310-01600. 2 L 7 3 4F A3WE 1999122300143 19991223 00143 NM 1999 12 23 CALA9901620 1 19991216 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1050 - 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT ANGLES AT FS 1070-1050, LBL 55 AND AT FS 1130, BL 0 CORRODED. THE FLOOR SUPPORT ANGLES W ERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-30-2, 51-10-2, AND 51-20-02. 2 L 7 3 4F A3WE 1999122300144 19991223 00144 NM 1999 12 23 CALA9901621 1 19991216 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 555 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FS 555 BETWEEN STRINGER 23L AND 27L. A NE W FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300145 19991223 00145 NM 1999 12 23 CALA9901622 1 19991216 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 580 - 600 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 4R AT STA 580-600. THE CRACKED SECTION OF STRINGER WAS CUTOUT AND A REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-10-2, 53-10-3, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300146 19991223 00146 NM 1999 12 23 CALA9901623 1 19991216 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 480 - 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN INTERCOSTAL AT STA 480-500, S28L. THE CRACKED AREA WAS REMOVED AND A DOUBLER WAS INS TALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1999122300147 19991223 00147 NM 1999 12 23 CALA9901624 1 19991216 A 5321 FLOOR PANEL BOEING 727 727232 1384082 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND AFT PIT FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM 51-30-5, 51-10-2, AND MM 51-20-0 . 2 L 7 3 4F A3WE 1999122300148 19991223 00148 NM 1999 12 23 CALA9901625 1 19991216 A 5720 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .25 INCH CRACK IN SUPPORT ANGLE FOR BODY TO FUSELAGE FAIRING AT RT WING AFT VERY I/B T/E PANEL. THE SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-3. 2 L 7 3 4F A3WE 1999122300149 19991223 00149 NM 1999 12 23 CALA9901626 1 19991216 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 950A - 950B CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND AFT CARGO INTERCOSTAL CORRODED UNDER AND ON TOP OF NUTPLATES AT FS 950A-950B, S26R-27R. A REPAIR WAS I NSTALLED IAW SRM 51-30-1. 2 L 7 3 4F A3WE 1999122300150 19991223 00150 NM 1999 12 23 CALA9901627 1 19991216 A 5320 WEB BOEING 727 727232 1384082 NM BS 800 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB CORRODED AROUND FASTENERS ON LEFT AND RIGHT SIDES AT WING CENTER SECTION FS 800 LOWER TORQUE BOX KE EL AREA, S29L-29R. THE WEB WAS CUT OUT AND A NEW WEB SECTION AND SPLICE WERE INSTALLED IAW SRM 51-40-2, FIGURE 1, 51-30 -6, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300151 19991223 00151 NM 1999 12 23 CALA9901628 1 19991216 A 5320 WEB BOEING 727 727232 1384082 NM BS 790 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB OUTER SURFACE CORRODED AROUND FASTENERS ON LEFT AND RIGHT SIDES AT WING CENTER SECTION, FS 790 LOWE R TORQUE BOX AT KEEL AREA. THE CORRODED WEB SECTION WAS CUT OUT AND A NEW WEB SECTION WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999122300152 19991223 00152 NM 1999 12 23 CALA9901629 1 19991216 A 5320 WEB BOEING 727 727232 1384082 NM BS 760 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB OUTER SURFACE CORRODED AROUND FASTENERS AT WING CENTER SECTION, FS 760 LOWER TORQUE BOX KEEL AREA. THE CORRODED WEB SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999122300153 19991223 00153 NM 1999 12 23 CALA9901630 1 19991216 A 5320 CUSP BOEING 727 727232 1384082 NM BS 1090 - 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND CUSP WEB SECTION CORRODED ON BOTTOM SIDE AT FS 1090-1110, RBL 58. THE CUSP WEB WAS REMOVED AND A NEW W EB WAS INSTALLED IAW 51-10-1, 53-10-2, 51-10-6, 51-30-0, AND MM 51-20-2. 2 L 7 3 4F A3WE 1999122300154 19991223 00154 NM 1999 12 23 99FDEA00502 1 19991217 A 2750 65404493 CONTROL VALVE BOEING 727 72725 1384006 NM RT MLG WW FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 154FE 18287 99-285 - ON FLAP RETRACT UP TO FLAPS 2, BOTH INBD AND OTBD NEEDLES STUCK BETWEEN 2 AND 5. ALL LED'S IND EXT. REMOVED A ND REPLACED O/B FLAP CONTROL VALVE PER MM 27-51-00. LUBED I/B FLAP CONTROL DRUM RIGGED CK GOOD PER 27-51-00-5. 2 L 7 3 4F A3WE 1999122300155 19991223 00155 NE 1999 12 23 MWEA99905 2 19991215 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LEFT FAILED A MWEA A UNSCHED LANDING E X J VIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 31 701ME 49760 LEFT ENGINE FAILED AT 33,000 FT DURING CRUISE INDICATIONS WERE SEVERE VIBRATION AND TOTAL LOSS OF OIL PRESSURE AND QUANT ITY. REMOVED AND REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999122300156 19991223 00156 NM 1999 12 23 MWEA99906 1 19991215 A 2170 21D101 COALESCER BAG DOUG MD88 MD88 3023688 NM ACM BAY CONTAMINATED A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 701ME 49760 SMOKE WAS OBSERVED BEING DISHARGED FROM THE OVERHEAD VENTS. MTC INSPECTED, REMOVED AND REPLACED THE WATER SEPERATOR BAG S. 2 L 7 2 4F RT A6WE 1999122300157 19991223 00157 1999 12 23 MWEA99907 4 19991216 A 2565 113317 COVER DOUG DC9 DC932 3022066 WP EVAC SLIDE LOOSE A MWEA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 204ME 47680 SLIDE ON GALLEY DOOR NEEDS TO BE REINSTALLED. MTC REINSTALLED SLIDE ON GALLEY DOOR. 2 L 7 2 4F A6WE 1999122300158 19991223 00158 WP 1999 12 23 MWEA99908 1 19991217 A 5320 591218820 ANGLE DOUG DC9 DC932 3022066 WP BS 1070 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DORSAL FIN LEFT AND RIGHT ATTACH ANGLES ARE CRACKED AT STATION 1070. MAINTENANCE FITTED AND INSTALLED NEW ATTACH ANGLES . 2 L 7 2 4F A6WE 1999122300159 19991223 00159 WP 1999 12 23 RRXA991592 1 19991214 A 2612 8990892 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 2 ENGINE MALFUNCTIONED A RRXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 603AL 46003 FIRE INDICATION NR 2 ENGINE PER QRH CHECKLIST ALL NR 2 SYSTEMS SHUT DOWN, OUTBOARD AGENT WOULD NOT DISCHARGE, DISCHARGED INBOARD. FOUND BOTH BOTTLES DISCHARGED OUTBOARD BOTTLE HAD BROKEN WIRE AT AGENT LOW LIGHT SWITCH REPAIRED WIRE. REMOV ED AND REPLACED LEFT SIDE INBD AND OUTBOARD FIRE BOTTLES. NR 2 FIRE WARNING WOULD NOT TEST. REPLACED RT AFT FIRE LOOP, NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1999122300160 19991223 00160 NM 1999 12 23 VNAA9912011 1 19991215 A 2161 4068B000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PACK FAILED A VNAA O OTHER M OVER TEMP CR CRUISE 1 GL 07 436JS 11567 3052 116125 WHILE EN ROUTE TO CLARKSBURG, THE LEFT PACK OVERHEATED. THE FLIGHT CREW WAS INSTRUCTED TO RETURN TO THE FIELD. THE AIR CRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLOW CONTROL AND SHUT OFF VALVE IN ACCORD ANCE WITH DORNIER MAINTENANCE MANUAL 21-61-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERV ICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999122300161 19991223 00161 WP 1999 12 23 RAIA9912026 2 19991216 A 7314 8974007 FUEL PUMP BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE LEAKING A RAIA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 875JX 1840 1840 875 4710 - SAN - LEFT ENGINE FUEL PUMP FILTER BOWL LEAKING FUEL. MAINTENANCE REPLACED LEFT ENGINE FUEL PUMP. 2 L 7 2 4T 4 T RT A56EU E4WE 1999122300162 19991223 00162 EU 1999 12 23 RAIA9912027 1 19991216 A 7330 1103P0645 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 973JX 2400 2400 973 4756 - FAT - RIGHT ENGINE FUEL LOW PRESSURE CAPTION ILLUMINATED. MAINTENANCE REPLACED RIGHT ENGINE FUEL PRESSURE SWITC H. 2 L 7 2 4T RT A56EU 1999122300163 19991223 00163 EU 1999 12 23 MALA976658 1 19991212 A 3020 47301 DEICE MODULE SAAB SF340 SF340A 7850100 EU RT INTAKE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 79XJ 079 ON CLIMBOUT, RIGHT INTAKE LIGHT ILLUMINATED. CONTINUOUS CYCLE OF 5 SECONDS ON, 22 SECONDS OFF. QRH (CYCLING ANTI ICE R T ENGINE) SWITCH HAD NO EFFECT. AFTER 10 MINUTES OF CONTINUOUS CYCLING, INTAKE LIGHT WENT OUT. RETURNED TO DTW. MAINT ENANCE PERFORMED RT INTAKE TEST, FOUND RT DEICE MODULE HAD A BAD LOAD MONITOR. REPLACED RIGHT DEICE MODULE, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999122300164 19991223 00164 EU 1999 12 23 MALA976659 1 19991216 A 2421 51634002 GCU SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 89XJ 089 AFTER TAKEOFF EXPERIENCED LEFT AC GENERATOR FAILURE WITH ASSOCIATED INTAKE, WINDSHIELD HEAT FAILURE. PERFORMED QRH ITEM S WITH UNSUCCESSFUL OUTCOME. RETURNED TO DTW. MAINTENANCE REPLACED LT AC GCU & AC GEN. ALL WORK DONE IAW SF 340 MM CH APTER 24. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999122300165 19991223 00165 EU 1999 12 23 MALA976660 1 19991214 A 3020 447301 DEICE MODULE SAAB SF340 340B 7860101 EU LT INTAKE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 413XJ 413 LEFT INTAKE CAUTION LIGHT ILLUMINATED, CYCLES EVERY 5 MINUTES AFTER SWITCH WAS RESET. MAINTENANCE REPLACED LT DEICE MOD ULE IAW SAAB MM. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999122300166 19991223 00166 EU 1999 12 23 MALA976661 1 19991212 A 3020 44730501 DEICE MODULE SAAB SF340 340B 7860101 EU LT INTAKE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 426XJ 426 INTERMITTENT ILLUMINATION OF LEFT INTAKE CAUTION LIGHT ON CLIMBOUT FROM DTW. LIGHT CYCLES ON FOR 2 - 7 SEC, THEN OFF 5 - 15 SEC, LIGHT DID NOT CYCLE ON DESCENT BACK INTO DTW. MAINTENANCE REPLACED LEFT DEICE CONTROL MODULE. PERFORMED OPER ATIONAL CHECK OF LT INTAKE. OPS CHECK GOOD IAW SAAB AMM 30-20. 2 L 7 2 4T RT A52EU 1999122300167 19991223 00167 NE 1999 12 23 MALA976662 2 19991208 A 7200 20030401 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE NR 3 MALFUNCTIONED A MALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 15 528XJ E2353 NR 3 ENGINE LOST POWER IN FLIGHT AT FL330, FUEL FLOW 2.2 N143, EGT AND N2 NORMAL, UNABLE TO CONTROL ENGINE WITH THROTTLE . TURNED ALL ICE ON AND TURNED OFF FADEC WITH NO SUCCESS. MAINTENANCE REPLACED NR 3 ENGINE IAW TASK CARD 7100-502 AND COMPLETED WORK PACKAGE DATED 12/8/99. PERFORMED POWER ASSURANCE CHECK IAW TASK CARD 7100-501 REF 409 CARD 079953 AND WP DATED 12/8/99. OPS CHECK GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 1999122300168 19991223 00168 EU 1999 12 23 MALA976663 1 19991213 A 3320 LIGHT SAAB SF340 340B 7860101 EU ROW 5A FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 435XJ 435 SMOKE WAS SEEN COMING FROM THE WINDOW LIGHTS AT 5A ALONG WITH SOME TINY SPARKS. THERE WAS ALSO A STRONG ODOR OF BURNT W IRES IN THE CABIN. MAINTENANCE REPLACED SIDE WALL LIGHT AND SOCKET AT ROW 5A. 2 L 7 2 4T RT A52EU 1999122300169 19991223 00169 EU 1999 12 23 MALA976664 1 19991215 A 3020 44730501 DEICE MODULE SAAB SF340 340B 7860101 EU LT INTAKE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 404XJ 340B404 LEFT ENGINE ANTI ICE LIGHT ILLUMINATED. MAINTENANCE REPLACED LT DEICE CONTROL MODULE. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999122300170 19991223 00170 EU 1999 12 23 MALA976665 1 19991209 A 3260 D49412001 CONTROLLER SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 GL 15 418XJ 418 LEFT MAIN GEAR INDICATOR LIGHT INTERMITTENT. ON APPROACH RECYCLED GEAR, THIS DIDN'T CORRECT THE PROBLEM. MAINTENANCE R EPLACED LANDING GEAR CONTROL IN COCKPIT. COMPLETED SEVERAL GEAR SWINGS, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999122300171 19991223 00171 EU 1999 12 23 MALA976666 1 19991207 A 2120 UNKNOWN BAC 146 AVRO146RJ85A 1500097 EU CABIN SMOKE A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 518XJ E2337 HAZE AND PLASTIC ODOR WAS DETECTED BY REAR FLIGHT ATTENDANT AFTER 3 MINUTES OF COMPLETING CHECKLIST (SHUTDOWN CHECK). A PU WAS SHUTDOWN, EXTERNAL POWER USED AND EXTERNAL HEAT WAS TURNED ON. MAINTENANCE INSPECTED AIRCRAFT FOR POSSIBLE SMOKE . INSPECTED AFT SECTION (CARGO, APU, GALLEY, AVIONICS BAY) NO DEFECTS NOTED, NO SMOKE OR SMELL NOTED. 2 H 7 4 4F RT A49EU 1999122300172 19991223 00172 NM 1999 12 23 AWXA9900482 1 19991220 A 5312 DHM4229600092 BULKHEAD BOEING 737 737277 1384570 NM BS 178 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 VERTICAL INTERCOSTAL WEB HAD NINE 4 INCH CRACKS ON AFT SIDE OF STA 178 PRESSURE BULKHEAD LBL 18, WL 172. REMOVED DAMAGE D WEB PER SRM B737 51-40-02, HFEC INSP FOR CRACKS, FABRICATED WEB FROM 7075 T6 .020 R699797, DOUBLER FROM 7075 T6 .032 R 700673 PER SRM B737 51-40-02. TREATED AND PRIMED PER SRM B737 51-10-2. INSTALLED PARTS PER SRM B737 51-30-2. 2 L 7 2 4F RT A16WE 1999122300173 19991223 00173 NM 1999 12 23 AWXA9900483 1 19991220 A 5330 6573746 SKIN BOEING 737 737277 1384570 NM BS 760 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 FUSELAGE SKIN CRACKED STA 760 STR 18. REMOVED EXISTING DOUBLER PER SRM 51-30-2, HFEC AROUND CUTOUT PER B737 NTM PT 6 5 1-00-00 FIG 23. NO CRACKS NOTED. FABRICATED DOUBLER FROM 2024 T3 .090. TREATED AND PRIMED PER B737 SRM 53-30-3. INST ALLED DOUBLER PER B737 SRM 51-30-2. 2 L 7 2 4F RT A16WE 1999122300174 19991223 00174 NM 1999 12 23 AWXA9900484 1 19991220 A 5320 6546526 SHEAR TIE BOEING 737 737277 1384570 NM BS 400 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 FRAME CLIP CRACKED AT STA 400 STR 22L FWD SIDE. REMOVED DAMAGED SHEAR TIE PER B737 SRM 53-10-4, FABRICATED REPAIR PART PER SRM 53-10-4, MAT'L 7075 T6 .050 R659586. INSTALLED REPAIR PART PER SRM B737 SRM 53-10-4 FIG 8. 2 L 7 2 4F RT A16WE 1999122300175 19991223 00175 NM 1999 12 23 RAAA99B1033 1 19991216 A 2750 TE FLAP BOEING BOEING 727 72722C 138400F NM WING MALFUNCTIONED A RAAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 AL 03 831RV 19093 INBOARD FLAPS WOULD NOT RETRACT AFTER DEPARTURE. VISUALLY INSPECTED INBOARD FLAP ASSEMBLIES, PERFORMED OPS CHECK. (EL ECT AND HYD IAW 27-51-0 PG 201) SEVERAL TIMES AND NO DISCREPANCIES WERE NOTED. OK FOR SERVICE. C/W OVERWEIGHT LANDING INSPECTION FOR LOW TO MODERATE SINK IAW C1-5-51-61 AND 61A, NO DISCREPANCIES NOTED. 2 L 7 3 4F A3WE 1999122300176 19991223 00176 NM 1999 12 23 RAAA99B1034 1 19991216 A 2750 TE FLAP BOEING BOEING 727 72722C 138400F NM WING MALFUNCTIONED A RAAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 AL 03 831RV 19093 INBOARD FLAPS WOULD NOT RETRACT AFTER DEPARTURE. INSPECTED FLAP SYSTEM, NO DEFECTS NOTED. LUBED LT AND RT INBOARD FLAP CARRIAGES AND ALL ROLLERS OPS CHECKED OK FOR SERVICE. RELEASED FOR TEST FLIGHT. C/W OVERWEIGHT LANDING INSPECTION FOR LOW TO MODERATE SINK IAW C1-5-51-61 AND 61A. NO DISCREPANCIES WERE NOTED. ACCOMPLISHED TEST FLIGHT. TEST FLIGHT OK. 2 L 7 3 4F A3WE 1999122300177 19991223 00177 SO 1999 12 23 RAAA99E4083 1 19991217 A 3350 1000553 LIGHT GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN WON'T TEST A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 AFT EMERGENCY EXIT PULL DOWN LIGHT DOES NOT TEST. REPLACED PULL DOWN LIGHT, OPS CHECK GOOD PER RAA ECO NR 86-24. 2 L 7 4 4T 4A22 1999122300178 19991223 00178 SO 1999 12 23 RAAA99E4084 1 19991217 A 3350 1000553 LIGHT GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN WON'T TEST A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 MAIN CABIN DOOR EMERGENCY PULL DOWN LIGHT DOES NOT TEST. REPLACED PULL DOWN LIGHT, OPS CK GOOD PPER RAA ECO NR 86-24. 2 L 7 4 4T 4A22 1999122300179 19991223 00179 NM 1999 12 23 CALA9901631 1 19991216 A 5320 WEB BOEING 727 727232 1384082 NM BS 1090 - 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND AFT DOOR AFT TORQUE BOX WEB CORRODED WITH A 1 INCH CRACK AT RIVET, FS 1090-1130, S27R. THE CORROSION W AS REMOVED IAW SRM 51-10-6. A WEB AND NUT PLATES WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 53-10-4. 2 L 7 3 4F A3WE 1999122300180 19991223 00180 NM 1999 12 23 CALA9901632 1 19991216 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 950 - 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 950-990, LBL 24 AND FROM STA 1070-1110, LBL 24. THE SEAT TRACK SEC TIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-0, AND 51-10-2. 2 L 7 3 4F A3WE 1999122300181 19991223 00181 NM 1999 12 23 CALA9901633 1 19991216 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .5 INCH CRACK IN O/B FLOOR SUPPORT AT RT FUSELAGE WALL FS 760. THE FLOOR SUPPORT WAS REMOVED AND A N EW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300182 19991223 00182 NM 1999 12 23 CALA9901634 1 19991216 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 750 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LOWER WEB ATTACH ANGLE CORRODED AT STA 750. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SR M 51-30-2 AND 51-30-1, PAGE 7. 2 L 7 3 4F A3WE 1999122300183 19991223 00183 NM 1999 12 23 CALA9901635 1 19991216 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1070 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN FLOORBOARD SUPPORT ANGLE AT STA 1070, LBL 28. THE FLOOR SUPPORT WAS REMOVED AND A NE W SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, MM 51-20-0. 2 L 7 3 4F A3WE 1999122300184 19991223 00184 NM 1999 12 23 CALA9901636 1 19991216 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 660 - 800 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 660-800, LBL 12. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-40-4 AND 51- 30-0. 2 L 7 3 4F A3WE 1999122300185 19991223 00185 NM 1999 12 23 CALA9901637 1 19991216 A 5410 SUPPORT BOEING 727 727232 1384082 NM NR 2 ENG COWL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN SECOND FRAME SUPPORT FROM AFT OF LT FORWARD NR 2 ENGINE COWL. THE FRAME SUPPORT WAS REMOVED AND A NEW FRAME SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-10-1. 2 L 7 3 4F A3WE 1999122300186 19991223 00186 NM 1999 12 23 CALA9901638 1 19991216 A 5330 PANEL BOEING 727 727232 1384082 NM BS 620 - 800 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND TRANSITION PANELS AT FS 620-660, S24R AND AT STA 660-800, S23L CORRODED. THE PANELS WERE REMOVED AND N EW PANELS WERE INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999122300187 19991223 00187 NM 1999 12 23 CALA9901639 1 19991215 A 5320 STRAP BOEING 727 727232 1384082 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 6 INCH CRACK IN TRANSITION PANEL STRAP AT FS 720, RT FORWARD PIT. A NEW STRAP WAS INSTALLED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 1999122300188 19991223 00188 NM 1999 12 23 CALA9901640 1 19991216 A 5330 PANEL BOEING 727 727232 1384082 NM BS 990 - 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LT AND RT TRANSITION PANELS AT FS 990-1030, S27L AND RT TRANSITION PANEL AT FS 1030-1070 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-01. 2 L 7 3 4F A3WE 1999122300189 19991223 00189 NM 1999 12 23 CALA9901641 1 19991216 A 5330 PANEL BOEING 727 727232 1384082 NM BS 1030 - 1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LT TRANSITION PANELS AT FS 1030-1065 AND FS 1065-1090 CORRODED. THE PANELS WERE REMOVED AND REPLACED I AW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300190 19991223 00190 NM 1999 12 23 CALA9901642 1 19991215 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBEAM CORRODED AT STA 360, BL 0 TO RBL 35. REPAIR ANGLES, FILLER, AND EXTRUSION WERE INSTALLED IAW SRM 53-10-8, FIGURE 8. 2 L 7 3 4F A3WE 1999122300191 19991223 00191 NM 1999 12 23 CALA9901643 1 19991216 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBEAM GOUGED AT STA 344, RBL 45. A REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-20-4, 51-30-2, MM 51-2 0-0, ECRA 5310-03955, AND EA 27-5310-2-A0532. 2 L 7 3 4F A3WE 1999122300192 19991223 00192 NM 1999 12 23 CALA9901644 1 19991216 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND CABIN FLOORBEAM UPPER CHORDS CORRODED AT FS 1030 FROM LBL 12 TO RBL 40. A REPAIR WAS INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-1, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300193 19991223 00193 WP 1999 12 23 CALA9901645 1 19991217 A 5230 PAN DOUG DC9 DC982 3022082 WP CARBO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR INNER PAN AROUND AFT LOCKING CAM. THE CRACKED AREA WAS BLENDED OUT, T REATED, AND PRIMED IAW SRM 52-01, FIGURE 1, 51-10-3, AND 51-01, FIGURE 1. 2 L 7 2 4F A6WE 1999122300194 19991223 00194 WP 1999 12 23 CALA9901646 1 19991217 A 5511 SPAR DOUG DC9 DC982 3022082 WP HORIZONTAL STAB BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND RT HORIZONTAL STABILIZER REAR SPAR U-CHANNEL BENT BETWEEN HINGE NR 4 AND NR 5. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-02 AND 51-30-08. 2 L 7 2 4F A6WE 1999122300195 19991223 00195 NM 1999 12 23 CALA9901647 1 19991218 A 5753 6521634131A SKIN BOEING 727 727232 1384082 NM TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND THE LT INBOARD T/E FLAP DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-2, PAGE 405. 2 L 7 3 4F A3WE 1999122300196 19991223 00196 NM 1999 12 23 CALA9901648 1 19991217 A 3350 20121 CHARGER MATHEWS BOEING 737 7373T0 1384582 NM GALLEY DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12322 23373 INSPECTION FOUND FORWARD GALLEY SERVICE DOOR SLIDE LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE FOUND CHARGER ASSEMBLY INOPE RATIVE. THE CHARGER ASSEMBLY WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1999122300197 19991223 00197 WP 1999 12 23 9905289989 1 19991209 A 2130 2075301AA CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE FAILED A NWAA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8945E 47181 CABIN PRESSURE AUTO FAIL LIGHT ILLUMINATED CLIMBING THROUGH 14,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN AN D FLIGHT WAS RETURNED TO DFW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH CABIN PRESSURE CONTROLLERS, OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999122300198 19991223 00198 WP 1999 12 23 9905299869 1 19991209 A 3260 301350201 PSEU DOUG DC9 DC951 3022051 WP MLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 778NC 4066 3127 48100 DURING FINAL APPROACH, ALL THREE GREEN DOWN AND LOCK LIGHTS INTERMITTENTLY ILLUMINATED AND EXTINGUISHED. FLIGHT CREW DE CLARED YELLOW EMERGENCY AND GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. LOG PAGE IN DICATES BITE CHECK NOT ACCOMPLISHED. MAINTENANCE REPLACED PROXIMITY SYSTEM ELECTRONIC UNIT, OPERATIONAL CHECK NORMAL. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1999122300199 19991223 00199 NM 1999 12 23 9905302292 1 19991213 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 292US 21503 DURING OVERNIGHT INTERIOR CHECK, MAINTENANCE FOUND AFT SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE REPL ACED BATTERY PACK, ALL OPERATIONAL CHECKS OK. 2 L 7 3 4F A3WE 1999122300200 19991223 00200 NM 1999 12 23 9905312288 1 19991214 A 3250 PIN BOEING 727 727251 138408H NM NLG STEERING MISSING A NWAA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 01 288US 21376 UPON LANDING, CREW EXPERIENCED SHIMMY FROM NOSE GEAR AREA AND DIFFICULTY IN STEERING. AIRCRAFT COMPLETED LANDING WITHOU T INCIDENT. MSP MAINTENANCE INSTALLED MISSING STEERING PIN AND AIRCRAFT TAXIED TO GATE. MAINTENANCE INSPECTED NOSE LAN DING GEAR AREA, ALL CHECKED OK. 2 L 7 3 4F A3WE 1999122300201 19991223 00201 WP 1999 12 23 9905329911 1 19991216 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 47405 DURING LINE MAINTENANCE INSPECTION, FOUND VENTRAL STAIR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AT POWER SUPPL Y B5-28, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999122300202 19991223 00202 WP 1999 12 23 9905339971 1 19991207 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTS IN COACH CLASS DIM AND/OR INOPERATIVE. REPLACED WIRE SPLICE UNDER SEAT 7 D, E, F AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999122300203 19991223 00203 WP 1999 12 23 9905349969 1 19991124 A 3397 WIRE DOUG DC9 DC931 3022065 WP TAIL CONE DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. RECONNECTED GROUND ABOVE LEFT LAVATORY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999122300204 19991223 00204 WP 1999 12 23 9905359907 1 19991125 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK AND OTHER TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999122300205 19991223 00205 WP 1999 12 23 9905369914 1 19991117 A 2910 82205 SOLENOID VALVE DOUG DC9 DC931 3022065 WP HYDRAULIC SYS LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 964N 44001 10119 47416 LOSS OF LEFT HYDRAULIC SYSTEM QUANTITY AND PRESSURE OCCURRED DURING APPROACH INTO DFW. LANDING WAS UNEVENTFUL. MAINTEN ANCE REPLACED ALTERNATE HYDRAULIC PUMP SOLENOID VALVE, OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999122300206 19991223 00206 WP 1999 12 23 9905379937 1 19991211 A 2780 CONTROL VALVE DOUG DC9 DC931 3022065 WP RT WING FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 908H 47517 DURING APPROACH INTO JAX, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE RIGHT ON SLAT EXTENSION. SUCCESSFUL LAND ING WAS ACCOMPLISHED USING FLAPS ONLY. MAINTENANCE FOUND BUILD-UP OF LUBE ON RIGHT T-DUCT. CLEANED LUBE AREA. ALSO, R EPLACED RESTRICTOR VALVE AT SLAT CONTROL VALVE. OPERATIONAL CHECK NORMAL ON SLAT CYCLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999122300207 19991223 00207 SO 1999 12 23 COMA9910188 1 19991216 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 258CA 120247 EXIT SIGN AT ROW 5 WAS INOPERATIVE. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999122300208 19991223 00208 SO 1999 12 23 COMA9910189 1 19991216 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO ROW 4 DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 248CA 23193 120228 EMERGENCY LIGHTS FWD OF ROW 4 WERE INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4T RT A31SO 1999122300209 19991223 00209 SO 1999 12 23 COMA9910190 1 19991215 A 6120 CONTROLLER EMB 120 EMB120RT SO RT PROPELLER MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 247CA 120225 RT PROPELLER RPM WAS 99.2 TO 99.6 AFTER TAKEOFF. GROUND RUNS SHOWED PROPELLER RPM TO BE IN LIMITATIONS. 2 L 7 2 4T RT A31SO 1999122300210 19991223 00210 SO 1999 12 23 COMA9910191 1 19991215 A 7720 SEL0C19EG INDICATOR EMB 120 EMB120RT SO COCKPIT ERRATIC A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 269CA 22059 120263 RT ENGINE T6 INDICATOR FLUCTUATED FULL SCALE. REPLACED T6 INDICATOR GAUGE. 2 L 7 2 4T RT A31SO 1999122300211 19991223 00211 SO 1999 12 23 COMA9910192 1 19991215 A 3240 396512 CONTROL VALVE EMB 120 EMB120RT SO BRAKE SYS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 264CA 21636 120256 WHEN BRAKES WERE SLAMMED ON, THE RT SYSTEM PRESSURE MOMENTARILY LOW ENOUGH TO TRIGGER THE LOW PRESSURE WARNING. REPLACE D THE BLUE SYSTEM BRAKE CONTROL VALVE. 2 L 7 2 4T RT A31SO 1999122300212 19991223 00212 EA 1999 12 23 COMA9960771 1 19991215 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 EA FUSELAGE OPEN A COMA A UNSCHED LANDING W N INADEQUATE Q C FALSE WARNING CL CLIMB 1 SO 01 759CA 7279 STALL FAIL MESSAGE AND LOUD NOISE THAT INCREASED WITH SPEED. FOUND 02 SERVICE DOOR OPEN, CLOSED DOOR. 2 L 7 2 4F RT A21EA 1999122300213 19991223 00213 EA 1999 12 23 COMA9960770 1 19991215 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 EA FUSELAGE CONTAMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 804CA 7352 AIRCRAFT DID NOT PRESSURIZE. REMOVED PAPER FROM OUTFLOW VALVE. A/C PRESSURIZED NORMAL. 2 L 7 2 4F RT A21EA 1999122300214 19991223 00214 EA 1999 12 23 COMA9960769 1 19991216 A 5320 MS20426AD5 RIVET CNDAIR CL600 CL6002B19 EA FUSELAGE LIGHTNING STRIKE A COMA O OTHER O OTHER CR CRUISE 1 SO 01 959CA 7116 DURING LIGHTNING STRIKE INSPECTION, FOUND FOUR RIVETS ON RIGHT LOWER PORTION OF FUSELAGE THAT NEEDED TO BE OVERSIZED TO A NAS1097AD6 RIVET. REPLACED AFFECTED RIVET. 2 L 7 2 4F RT A21EA 1999122300215 19991223 00215 EA 1999 12 23 COMA9960768 1 19991215 A 4920 38760016 SWITCH CNDAIR CL600 CL6002B19 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 957CA 7109 APU OIL PRESSURE CAUTION MESSAGE. REPLACED OIL PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 1999122300216 19991223 00216 EA 1999 12 23 COMA9960767 1 19991215 A 4920 APU CNDAIR CL600 CL6002B19 EA APU BAY LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 957CA 7109 APU OIL PRESSURE CAUTION MESSAGE. ADDED 1 QT OF OIL TO APU. 2 L 7 2 4F RT A21EA 1999122300217 19991223 00217 NM 1999 12 23 QXEA9902599 1 19991213 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 367PH 511 SEA- SMOKE WARNING AND MASTER CAUTION LIGHT ILLUMINATED FOR 10 SECONDS DURING FINAL APPROACH. INSPECTED BOTH SMOKE DETE CTORS IN BAGGAGE PIT. NO DEFECTS NOTED. PERFORMED BAGGAGE COMPARTMENT SMOKE DETECTOR SYSTEM TEST. NO FURTHER DEFECTS. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999122300218 19991223 00218 EU 1999 12 23 99FDEA00503 1 19991216 A 7830 32052213 PILOT VALVE AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 679FE 793 NR 2 ENGINE REVERSER PRESSURE ON T/O ROLL. REMOVED AND REPLACED NR 2 DIRECTIONAL PILOT VALVE PER AMM 78-31-06-2. 2 L 7 2 4F RT A35EU 1999122300219 19991223 00219 WP 1999 12 23 ABXA9900847 1 19991208 A 5313 591142425 LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 945 - 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LONGERON 22 RIGHT CORRODED BETWEEN STATION 945 AND 980. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1999122300220 19991223 00220 WP 1999 12 23 ABXA9900848 1 19991208 A 5320 991073417 CUSP DOUG DOUG DC9 DC932F 3022067 WP BS 218 - 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 218. REPLACED CUSP WEB FROM STATION 218 TO 237 IAW DC9 SRM 51-30 -2. 2 L 7 2 4F A6WE 1999122300221 19991223 00221 WP 1999 12 23 ABXA9900849 1 19991208 A 5753 5910041504 VANE DOUG DOUG DC9 DC932F 3022067 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND RIGHT FLAP, INBOARD FIXED VANE DELAMINATED ON LOWER SURFACE. REPLACED FIXED VANE IAW DC9 MM 27-51 -3. 2 L 7 2 4F A6WE 1999122300222 19991223 00222 NM 1999 12 23 SCNA99151 1 19991216 A 2131 7248272 VALVE BOEING 727 727259 138408J NM CABIN PRESSURE FAILED A SCNA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 289SC 234 22475 APPROXIMATELY FIVE MINUTES AFTER LEVEL OFF AT 31,000 FEET, CABIN BEGAN TO DEPRESSURIZE RAPIDLY. CABIN RATE INDICATOR PE GGED AT MAXIMUM RATE OF CLIMB, SWITCHED TO MANUAL OUTFLOW VALVE INDICATOR AT FULL CLOSED POSITION RATE OF CLIMB CONTINUE D AT MAXIMUM RATE OF CLIMB. PERFORMED RAPID DEPRESSURIZATION CHECKLIST AND COULD NOT STABILIZE CABIN ALTITUDE. PERFORM ED RAPID DESCENT CHECKLIST AND LANDED. REMOVED AND REPLACED SAFETY OVERPRESSURE VALVE. PRESSURIZED AIRCRAFT TO 9.4 DIF FERENTIAL. OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999122300223 19991223 00223 NM 1999 12 23 SCNA99152 1 19991210 A 3350 900835A BATTERY PACK BOEING 727 727259 138408J NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE L2 EMERGENCY OVERHEAD DOOR LIGHT FLASHES WHEN TESTED. REMOVED AND REPLACED THE L2 EMERGENCY DOOR LIGHT BATTERY PACK, OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999122300224 19991223 00224 NM 1999 12 23 SCNA99153 1 19991218 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT SIGN ABOVE THE R2 DOOR WAS FOUND NOT ILLUMINATING. REMOVED AND REPL ACED THE BATTERY PACK FOR THE EMERGENCY EXIT SIGN ABOVE THE R2 DOOR. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999122300225 19991223 00225 NM 1999 12 23 VNAA9912012 1 19991217 A 6120 APS3D10001000A SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PROPELLER FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 436JS 11592 3052 116015 DURING CLIMBOUT FROM PIT, THE FLIGHT CREW RECEIVED A RIGHT HAND PROPELLER OIL PRESSURE CAS MESSAGE. MAINTENANCE CONTROL INSTRUCTED THE CREW TO RETURN TO THE FIELD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND R EPLACED THE OIL PRESSURE SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANAUL 61-21-12. MAINTENANCE ALSO SERVICED THE O IL. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999122300226 19991223 00226 1999 12 23 RAIA9912028 2 19991204 A 7310 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CE 03 972JX 1425 1425 972 6702-LAX- DURING TAKEOFF ROLL, LEFT ENGINE TORQUE FLUCTUATED BETWEEN 60 PERCENT AND 100 PERCENT. MAINTENANCE DEFERRED PER MEL 12/05/99. MAINTENANCE REPLACED LEFT ENGINE FUEL BY-PASS VALVE. 2 L 7 2 4T RT A56EU 1999122300242 19991223 00242 SW 1999 12 23 HEEA065295 1 19991124 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX CRACKED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 404PH 633 53188 CRACKS IN MAIN ROTOR GEARBOX ELASTOMER ARE BEYOND LIMITS. 1 G 7 1 3U O H2SW 1999122300243 19991223 00243 SW 1999 12 23 HEEA065296 1 19991124 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX CRACKED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 404PH 633 53188 CRACKS IN MAIN ROTOR GEARBOX ELASTOMER ARE BEYOND LIMITS. 1 G 7 1 3U O H2SW 1999122300329 19991223 00329 SO 1999 12 23 LR7A9968 1 19991217 A 5320 3528962 FITTING LKHEED 382 382G 526414U SO BS 946 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 91 4590 DURING SCHEDULED A CHECK INSPECTION, FOUND FS 946 RT BUTTERFLY FITTING CRACKED AT APPROX WL 280. REPLACED FITTING IAW S MP 583 51-10, PARA G AND 51-70, PARA D. 2 H 7 4 4T A1SO 1999122300330 19991223 00330 SO 1999 12 23 LR7A9969 1 19991217 A 2421 288589B GENERATOR LKHEED 382 382G 526414U SO NR 2 ENGINE FAILED A LR7A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 AL 03 405LC 444 5025 FLIGHT CREW REPORTED NR 2 GENERATOR BEARING FAILURE LIGHT ILLUMINATED 57 MIN OUT OF SKP. NR 2 ENGINE SHUTDOWN AT 1600Z. CONTINUED TO NSY AND LANDED WITHOUT INCIDENT. REMOVED NR 2 GENERATOR, REMOVED DRIVE SHAFT AND REINSTALLED GENERATOR P ER SMP 581 24-20-220 AND MEL 24-5. DEFERRED NR 2 GENERATOR PER MEL 24-5, CAT C DMI NR 00131. 2 H 7 4 4T A1SO 1999122300331 19991223 00331 NM 1999 12 23 AWXA9900485 1 19991221 A 3397 BMS13131122 WIRE BOEING 757 757225 1384959 NM ROW 7 CUT A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 913AW 22207 WIRES NEED REPAIR LT SIDE EMERGENCY LIGHT AT ROW 7. REPAIRED WIRES IAW MM 33-51-00, OPS CK GOOD. 2 L 7 2 4F RT A2NM 1999122300332 19991223 00332 NM 1999 12 23 AWXA9900486 1 19991221 A 3397 13131122 WIRE BOEING 737 7373G7 1384595 NM ROW 6 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 305AW 24012 EMERGENCY LIGHT AT ROW 6 A, B, C SIDE OF SEAT INOP. FOUND AND REPAIRED BROKEN WIRE, OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1999122300333 19991223 00333 NM 1999 12 23 AWXA9900487 1 19991221 A 3350 831136 LIGHT BOEING 737 737301 1384611 NM SEAT 12 - 22 INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 EMERGENCY EXIT LIGHT ASSY AT SEATS 12 AND 22 LT SIDE INOP. REPLACED LIGHT ASSY AT SEAT 12, REPAIRED BROKEN WIRE AT SEA T 22 AND OPS CHECKED GOOD. WIRE (P/N BMS 13-13-1/1-22) 2 L 7 2 4F RT A16WE 1999122300334 19991223 00334 NM 1999 12 23 AWXA9900488 1 19991221 A 3397 13131122 WIRE BOEING 737 737277 1384570 NM ROW 17 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 181AW 22648 SEAT EMERGENCY EXIT LIGHT INOP AT ROW 17 LT. REPAIRED BROKEN WIRE UNDER SEAT, OPS CK NORMAL. 2 L 7 2 4F RT A16WE 1999122300335 19991223 00335 NM 1999 12 23 AWXA9900489 1 19991221 A 5330 6573746 SKIN BOEING 737 737277 1384570 NM BS 747A CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 FUSELAGE SKIN CRACK AT STA 747A STR 17R, TEMP REPAIR INSTALLED. REMOVED EXISTING DOUBLER PER B737 SRM 51-30-02, HFEC AR OUND CUTOUT PER B737 NTM PT 6 51-00-00 FIG 23. NO CRACK NOTED. FABRICATED DOUBLER 2024 T3 .09 R665790. TREATED AND P RIMED PER B737 SRM 53-30-03. INSTALLED DOUBLER PER 51-30-02. 2 L 7 2 4F RT A16WE 1999122300336 19991223 00336 NM 1999 12 23 AWXA9900490 1 19991221 A 5752 6546471 INTERCOSTAL BOEING 737 737277 1384570 NM AILERON CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 INTERCOSTAL CRACKED AT LT O/B MID FLAP. REMOVED INTERCOSTAL PER B737 SRM 51-30-02. FABRICATED INTERCOSTAL FROM 2024 .0 50 HT TO T42 PER DWG 65-4647, BAC 5602R 699109 T AND PER B737 SRM 51-10-02. INSTALLED INTERCOSTAL PER B737 SRM 51-30-02 . 2 L 7 2 4F RT A16WE 1999122300337 19991223 00337 NM 1999 12 23 AWXA9900491 1 19991221 A 5313 657374413 STRINGER BOEING 737 737277 1384570 NM BS 420 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 INTERIOR STRUCTURE BD 420 STR 26R CRACKED AND BULGING CORROSION. REMOVED STRINGER IAW B737 SRM 51-30-2. REMOVED CORROS ION ON ATTACH ANGLE IAW SRM 51-10-2. NDT VERIFIED NO CRACKS USING HFEC PER B737 NTM PT 6 51-00-00 FIG 23. TREATED AND PRIMED AREA PER B737 51-10-02. INSTALLED STRINGER AND SPLICE IAW B737 SRM 51-30-02. 2 L 7 2 4F RT A16WE 1999122300338 20000616 00338 NE 2000 6 16 CALA9901649 2 19991217 A 7200 LINER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE FAILED A CALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14074 46911 455994 THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMBOUT. THE FIRE WARNING LIGHT WAS ACCOMPANIED BY EGT GOING FUL L SCALE. THE ENGINE THROTTLE WAS RETARDED AND THE FIRE LIGHT WENT OUT. AN ATTEMPT TO THROTTLE UP WAS MADE, BUT N1 WOUL D NOT ACCELERATE. THE NR 2 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUN D METAL IN THE NR 2 ENGINE TAILPIPE. NO EVIDENCE OF FIRE WAS FOUND. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* INVESTIGATION CONCLUDED THAT THE TMF LINER HAD FAILED ALLOWING HOT GAS TO REACH THE HPT STAGE 2 BLADE RETAINER WHICH SUB SEQUENTLY BROKE INTO SEVERAL PIECES, ONE OF WHICH PUNCTURED THE TMF. 2 L 7 3 4F 4 F A22WE E23EA 1999122300339 19991223 00339 NM 1999 12 23 CALA9901650 1 19991220 A 2430 39B1681C INVERTER BOEING 737 737524 1384721 NM E/E BAY BURNT A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14628 14577 27532 THE CABIN CREW REPORTED FUMES HAVING A HOT PLASTIC SMELL IN THE CABIN AND COCKPIT WHILE EN ROUTE FROM CLE TO PHL. THE A IRCRAFT WAS DIVERTED TO MDT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE STATIC INVERTER AT FAULT. THE STAT IC INVERTER WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1999122300340 19991223 00340 WP 1999 12 23 CALA9901651 1 19991220 A 5320 BEAM DOUG DC9 DC981 3022081 WP CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND Z-BEAM CORRODED BENEATH CENTER THRESHOLD PLATE IN MID CARGO BIN. THE Z-BEAM WAS REPLACED IAW SRM 53-05 , FIGURE 63. 2 L 7 2 4F A6WE 1999122300341 19991223 00341 WP 1999 12 23 CALA9901652 1 19991220 A 5350 LATCH DOUG DC9 DC981 3022081 WP TAIL CONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16884 48074 TAIL CONE PULL FROM INSIDE HANDLE WAS EXCESSIVE. THE TAIL CONE WOULD NOT DEPLOY FROM THE AFT SERVICE DOOR. THE TAIL CO NE LATCHES WERE ADJUSTED AND OPERATIONAL CHECKS WERE GOOD IAW MM 53-53-00. 2 L 7 2 4F A6WE 1999122300342 19991223 00342 NM 1999 12 23 CALA9901653 1 19991221 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 950 - 1038 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LT O/B SEAT TRACK CORRODED FROM STA 950-1038. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INST ALLED IAW SRM 51-30-2, 51-10-4, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 1999122300343 19991223 00343 NM 1999 12 23 CALA9901654 1 19991221 A 5230 FITTING BOEING 727 727232 1384082 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND CENTER CARGO DOOR FORWARD PRESSURE RELIEF DOOR SKIN FITTING CORRODED. THE FITTING WAS REMOVED AND REPL ACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300344 19991223 00344 NM 1999 12 23 CALA9901655 1 19991221 A 5414 SKIN BOEING 727 727232 1384082 NM COWL DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND BOTTOM OF NR 3 ENGINE COWL SKIN DENTED AND SCRATCHED BETWEEN STIFFENERS 9 & 10. THE DAMAGED AREA WAS C UT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 54-30-3. 2 L 7 3 4F A3WE 1999122300345 19991223 00345 NM 1999 12 23 CALA9901656 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 848 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK ON EACH END OF FLOOR SUPPORT AT STA 848, BL 0 AND LBL 25. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300346 19991223 00346 NM 1999 12 23 CALA9901657 1 19991221 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 344, LBL 20 TO LBL 60. A REPAIR WAS INSTALLED IA W SRM 53-10-8, FIGURE 9. 2 L 7 3 4F A3WE 1999122300347 19991223 00347 NM 1999 12 23 CALA9901658 1 19991221 A 5280 FRAME BOEING 727 727232 1384082 NM NLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .75 INCH CRACK IN LT FORWARD NLG DOOR SIXTH FRAME. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALL ED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300348 19991223 00348 NM 1999 12 23 CALA9901659 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 810 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB SUPPORT ANGLE CORRODED AT WING CENTER SECTION LOWER TORQUE BOX AT KEEL AREA, FS 810. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-10-2. 2 L 7 3 4F A3WE 1999122300349 19991223 00349 NM 1999 12 23 CALA9901660 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 790 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB SUPPORT ANGLE CORRODED WING CENTER SECTION FS 790 LOWER TORQUE BOX AT KEEL AREA. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 7. 2 L 7 3 4F A3WE 1999122300350 19991223 00350 NM 1999 12 23 CALA9901661 1 19991221 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN AFT CARGO DOOR JAMB UPPER AFT WEB. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED I AW SRM 51-30-2 AND 51-20-1. 2 L 7 3 4F A3WE 1999122300351 19991223 00351 NM 1999 12 23 CALA9901662 1 19991221 A 5410 STIFFENER BOEING 727 727232 1384082 NM COWL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN NR 3 ENGINE COWL NR 10 STIFFENER. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51- 20-1 AND 51-30-2. 2 L 7 3 4F A3WE 1999122300352 19991223 00352 NM 1999 12 23 CALA9901663 1 19991221 A 5311 FRAME BOEING 727 727232 1384082 NM BS 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 380, LONGERON 8R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4. A REPA IR WAS INSTALLED IAW SRM 53-10-4, FIGURE 1. 2 L 7 3 4F A3WE 1999122300353 19991223 00353 NM 1999 12 23 CALA9901664 1 19991221 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND SKIN OF RT ACCESS PANEL AT FUSELAGE BELLY BETWEEN HEAT EXCHANGERS CORRODED WITH PULLED RIVETS. THE SKI N WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1999122300354 19991223 00354 NM 1999 12 23 CALA9901665 1 19991221 A 5350 SUPPORT BOEING 727 727232 1384082 NM FAIRING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT LOWER BODY FAIRING SUPPORT NR 10 CORRODED. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300355 19991223 00355 NM 1999 12 23 CALA9901666 1 19991221 A 5311 FRAME BOEING 727 727232 1384082 NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1.25 INCH CRACK IN RT FUSELAGE FRAME AT STA 312, LONGERON 13R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4, FIGURE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-0. 2 L 7 3 4F A3WE 1999122300356 19991223 00356 NM 1999 12 23 CALA9901667 1 19991221 A 5210 PAN BOEING 727 727232 1384082 NM PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 4 INCH CRACK IN L-1 DOOR INNER PAN FORWARD LOWER CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5265-01005. 2 L 7 3 4F A3WE 1999122300357 19991223 00357 NM 1999 12 23 CALA9901668 1 19991221 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB CORRODED AT AFT CARGO DOOR JAMB. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 A ND 51-20-1. 2 L 7 3 4F A3WE 1999122300358 19991223 00358 NM 1999 12 23 CALA9901669 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 560 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND ATTACH ANGLE FOR RT TRANSITION WEB AT FS 560, LONGERON 27R BELOW TORQUE BOX BROKEN OFF. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1999122300359 19991223 00359 NM 1999 12 23 CALA9901670 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 720F CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL ATTACH ANGLE AT STA 720F, BL 0. THE ANGLE WAS REMOVED AND A NEW ANGLE W AS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300360 19991223 00360 NM 1999 12 23 CALA9901671 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 420, RBL 12-25. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTA LLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999122300361 19991223 00361 NM 1999 12 23 CALA9901672 1 19991221 A 5320 WEB BOEING 727 727232 1384082 NM BS 720E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT WING ROOT L/E TO BODY LOWER SUPPORT WEB CRACKED AT NUT PLATE HOLE, FS 720E, STRINGER 21R. THE CRACK WAS 1 INCH LONG. THE CRACKED AREA WAS CUT OUT, FILLER AND DOUBLER WAS INSTALLED IAW SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1999122300362 19991223 00362 NM 1999 12 23 CALA9901673 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1110 - 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1110-1130, LBL 15. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-0, PAGE 3. 2 L 7 3 4F A3WE 1999122300363 19991223 00363 NM 1999 12 23 CALA9901674 1 19991221 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND SHEAR TIE CORRODED AT STA 480, LONGERON 27R-27L. THE SHEAR TIE WAS REMOVED AND A REPAIR WAS INSTALLED I AW SRM 53-10-4, FIGURE 12. 2 L 7 3 4F A3WE 1999122300364 19991223 00364 NM 1999 12 23 CALA9901675 1 19991221 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 1050 - 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 1050-1070, LONGERON 27L. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANG LE WAS INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1999122300365 19991223 00365 SO 1999 12 23 COMA9910193 1 19991217 A 3240 21585 BRAKE EMB 120 EMB120RT SO MLG WORN A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 249CA 23785 120230 ANTI SKID WARNING DURING TAKEOFF. REPLACED THE NR 4 BRAKE ASSY. 2 L 7 2 4T RT A31SO 1999122300366 19991223 00366 1999 12 23 COMA9910194 2 19991217 A 7200 ENGINE EMB 120 EMB120RT SO RIGHT MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 463CA 120267 RT ENGINE T6 INDICATION WENT FULL SCALE DURING TAKEOFF. CAME BACK TO NORMAL AFTER ABORT. REPAIRED LOOSE WIRE TERMINALS AT T6 BUS BAR. 2 L 7 2 4T RT A31SO 1999122300367 19991223 00367 EA 1999 12 23 COMA9960772 1 19991218 A 3250 COMPUTER CNDAIR CL600 CL6002B19 EA NLG STEERING MALFUNCTIONED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 804CA 7352 WHEN TAKE-OFF POWER APPLIED, FULL LEFT RUDDER NEEDED TO KEEP A/C STRAIGHT.\NCOULD NOT DUPLICATE. TAXI CHECK NORMAL. NO F AULT CODES IN STEERING COMPUTER. 2 L 7 2 4F RT A21EA 1999122300368 19991223 00368 EA 1999 12 23 COMA9960773 1 19991218 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTION A COMA C ABORTED TAKEOFF F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 954CA 6220 1945 7100 CONFIG SPOILERS WARNING DURING TAKEOFF. REPLACED NR 2 SECU. 2 L 7 2 4F RT A21EA 1999122300369 19991223 00369 EA 1999 12 23 COMA9960775 1 19991216 A 2750 TE FLAP CNDAIR CL600 CL6002B19 EA WING FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 965CA 7131 FLAPS FAILED AT 8 DEGREES DURING APPROACH. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 1999122300370 19991223 00370 EA 1999 12 23 COMA9960776 1 19991217 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 739CA 2763 7273 COPILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1999122300371 19991223 00371 EA 1999 12 23 COMA9960777 1 19991218 A 7920 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE EDP FAILED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 962CA 7123 807393 LEFT ENGINE OIL PRESSURE WARNING. REPLACED AGB DRIVE SEALS FOR THE EDP AND ATS. 2 L 7 2 4F 4 F RT A21EA E15NE 1999122300372 19991223 00372 NM 1999 12 23 UPS99231225 1 19991122 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 760 - 848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) MAIN DECK LONGITUDINAL BEAM BS 760-848 LBL 45 WL 208 RT FLANGE SEVERAL PLACES. REPAIRED PER SRM 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 1999122300373 19991223 00373 NM 1999 12 23 UPS99231226 1 19991122 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, MAIN DECK SEAT TRACK HAS CORROSION ON TOP OF TRACK, BS 760 AND BS 780 RBL 63 WL 208. REMOVED CORROD ED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 53-10-1, SRM 51-30-5, SRM 51-10-2 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1999122300374 19991223 00374 NM 1999 12 23 UPS99231227 1 19991220 A 5320 FITTING BOEING 727 72725C 138400H NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI, THE STR 29L BATH TUB FITTING COMMON TO BS 1183 IS CRACKED (INBD FITTING). FITTING WAS REPLACED PER SRM 51-30-2 AND MM 53-11-0. 2 L 7 3 4F A3WE 1999122300375 19991223 00375 NM 1999 12 23 UPS99431229 1 19991220 A 5753 SKIN BOEING 747 747121 1384871 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE:N/A, LEFT O/B TRAILING EDGE FLAP WHEEL END HAD 10 INCH CRACK. REMOVED AND REPLACED AFT O/B TRAILING EDG E FLAP PER 747 MM 27-51-06, OPS CHECK GOOD. 2 L 7 4 4F A20WE 1999122300376 19991223 00376 WP 1999 12 23 UPS99831228 1 19991216 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. CHARGED BATTERY, OPS OK. 2 L 7 4 4F RT 4A25 1999122300377 19991223 00377 EU 1999 12 23 99FDEA00504 1 19991221 A 3230 MLG AIRBUS 300 A300F4605R 3930327 EU FUSELAGE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 679FE 793 99-287 - LAND GEAR WOULD NOT RETRACT AFTER T/O IN SYSTEM NR 1 OR NR 2. RETURN TO ORD. REMOVED AND REPLACED LAND GEAR S EL VLV I/A AMM 32-31-12-4. OPS CK NORM WITH NO LEAKS. PERF SEVERAL SUCCESSFUL GEAR SWINGS. JACK PAD ACCESS PNL REINST ALL. 2 L 7 2 4F RT A35EU 1999122300378 19991223 00378 WP 1999 12 23 ABXA9900850 1 19991129 A 5320 9910164163 DOUBLER DOUG DOUG DC9 DC932F 3022067 WP BS 696 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND KEEL WEB DOUBLER AT STATION 696 CRACKED. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999122300379 19991223 00379 WP 1999 12 23 ABXA9900851 1 19991129 A 5320 991075513 WEB DOUG DOUG DC9 DC932F 3022067 WP BS 813 - 832 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 813 - 832. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1999122300380 19991223 00380 WP 1999 12 23 ABXA9900852 1 19991129 A 5320 99155503 INTERCOSTAL DOUG DOUG DC9 DC932F 3022067 WP BS 980 - 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND INTERCOSTAL BETWEEN STATIONS 980 - 996 AND LONGERONS N27 AND 28 LEFT CORRODED AROUND NUT PLATES. R EPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999122300381 19991223 00381 WP 1999 12 23 ABXA9900853 1 19991129 A 5320 59248443 FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FITTING BELOW FORWARD SPAR OF CENTER WING TANK AT LONGERON 24 LEFT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999122300382 19991223 00382 WP 1999 12 23 ABXA9900854 1 19991129 A 5320 59248444 FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FITTING BELOW FORWARD SPAR OF CENTER WING TANK AT LONGERON 24 RIGHT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999122300383 19991223 00383 WP 1999 12 23 MWEA99909 1 19991219 A 2822 6550934 PUMP DOUG DC9 DC982 3022082 WP FUEL BOOST FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 809ME 48071 CENTER FORWARD FUEL BOOST PUMP POPPED CIRCUIT BREAKERS. MTC REMOVED AND REPLACED FORWARD CENTER BOOST PUMP. 2 L 7 2 4F A6WE 1999122300384 19991223 00384 NE 1999 12 23 DL76L992726 2 19991213 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MAKING METAL A DALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 27 186DN 29185 27962 724145 FOUND METAL ON NR 1 AND 1.5 CHIP DETECTORS. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999122300385 19991223 00385 NM 1999 12 23 DL72L992735 1 19991116 A 5753 65192709 FLAP TRACK BOEING 727 727232 1384082 NM WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 INB'D FLAP / INB'D TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS, WEAR AT FWD LUGS, WEAR AT MLG DOOR HINGE F ITTING HOLES, WEAR AT SPACER BAR HOLES AND WEAR AT TOGGLE DETENT HOLE. AUTHORIZED BUSHING AND BLEND REPAIRS. 2 L 7 3 4F A3WE 1999122300386 19991223 00386 NE 1999 12 23 DL757992736 2 19991214 A 7200 ENGINE 7836001807 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 FAILED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 662DN 20370116 24991 716525 LOST NR 1 ENG EPR IND ON EICAS THEN ENG ROLLED BACK WITH AUDIBLE POP. F/A AND PASS REPORT FLAME FROM TAILPIPE. SHUTDOW N ENG AND DIVERTED TO CPR. REPLACED EEC. 2 L 7 2 4F 4 F RT A2NM E17NE 1999122300387 19991223 00387 NM 1999 12 23 DL76L992738 1 19991214 A 2910 LINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 27 190DN 28447 724741 RT HYD QUANTITY DECREASED TO .33. EDP DEPRESSURIZED AND ACMP OFF, QTY CONTINUED TO DECREASE. FOUND CASE RETURN LINE AT AFT END OF PYLON CHAFED THROUGH. REMOVED LINE AND INSTALLED INTERIM FLEX HOSE PER MM 20-10-09-2 AND ERA 227766-14. 2 L 7 2 4F 4 F RT A1NM E24NE 1999122300388 19991223 00388 NM 1999 12 23 DLM88992740 1 19991214 A 3350 BATTERY PACK 20131A DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 946DL 72125 49819 ON LAYOVER, FOUND F/C EMERGENCY SEAT TRACK LIGHTING INOP. REPLACED BATTERY PACK DELTA (P/N 337101963) (S/N 72125) OFF, (S/N 65889) ON. TRACK LIGHTING OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 1999122300389 19991223 00389 NM 1999 12 23 DLM11992742 1 19991210 A 5753 ARC74602 SKIN DOUG MD11 MD11 3023602 NM TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805DE 48476 RIGHT I/B FLAP VANE LOWER SKIN, TIRE DAMAGE 24 X 22 DAMAGE TO LOWER SKIN AND CORE OF FLAP VANE. AUTHORIZED PREPREG CARB ON FIBER COMPOSITE REPAIR. 2 L 7 3 4F RT A22WE 1999122300390 19991223 00390 NM 1999 12 23 DL73K992743 1 19991211 A 5230 6547952524 BEAM BOEING 737 737232 1384475 NM CARGO DOOR CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 AFT CARGO DOOR / NR 2 STOP BEAM / OUTER CHORD: AD 98-11-04, R1 CRACK FOUND IN TYPICAL POSITION ON NR 2 STOP BEAM OUTER CHORD AS ADDRESSED IN SUBJECT AD (I.E. LOCATED AT FWD END OF BEAM ADJACENT TO STOP FITTING). AUTHORIZED ANGLE REPAIR. 2 L 7 2 4F RT A16WE 1999122300391 19991223 00391 NM 1999 12 23 DL72L992744 1 19991212 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 INBOARD FLAP / NR 5 INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS, AND WEAR AT FWD ATTACH LUGS AND M LG DOOR HINGE FITTING HOLES. AUTHORIZED BLEND REPAIRS AND OVERSIZED FASTENERS. 2 L 7 3 4F A3WE 1999122300392 19991223 00392 NM 1999 12 23 DL72L992745 1 19991102 A 5753 651927015 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 INBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS. AUTHORIZED BUSHING REPAIR. 2 L 7 3 4F A3WE 1999122300393 19991223 00393 NM 1999 12 23 DL72L992746 1 19991102 A 5753 651927015 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 INBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG BEAM ATTACH PAD. AUTHORIZED BLEND AND BUSHING REPAIR. 2 L 7 3 4F A3WE 1999122300394 19991223 00394 NM 1999 12 23 DL72L992747 1 19991116 A 5753 651927010 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 INBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD LUGS. AUTHORIZED BLEND AND BUSHING REPAIR. 2 L 7 3 4F A3WE 1999122300395 19991223 00395 NM 1999 12 23 DL72L992748 1 19991116 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 INBOARD FLAP / INBOARD TRACK - TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS, WEAR AT FWD LUGS, WEAR AT MLG DOOR HIN GE FITTING HOLES, WEAR AT SPACER BAR HOLES, WEAR AT TOGGLE DETENT HOLE. AUTHORIZED BLEND AND BUSHING REPAIRS. 2 L 7 3 4F A3WE 1999122300396 19991223 00396 NM 1999 12 23 DL72S992751 1 19991215 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 FOUND ON C1 LETTER CK, .375 INCH CRACK ON SKIN AT THE LOWER I/B FASTENER OF THE L4 WINDOW CUTOUT. REPAIRED PER SRM 53-3 0-3. 2 L 7 3 4F A3WE 1999122300397 19991223 00397 NM 1999 12 23 DLM88992752 1 19991215 A 3260 H141016 SWITCH DOUG MD88 MD88 3023688 NM NLG FAILED A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 946DL 49819 NOSE GEAR LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. NO RE-INDICATION, AND COCKPIT NOSE GEAR PIN EXTENDED. LIGHTS T ESTED NORMALLY. NOSE GEAR LIGHT ILLUMINATED ON TAXI IN. REPLACED NOSE GEAR DOWN SWITCH S1-412. 2 L 7 2 4F RT A6WE 1999122300398 19991223 00398 NM 1999 12 23 DL76L992753 1 19991214 A 2570 HARNESS 12583901 BOEING 767 767332 1382001 NM SEAT 10 WORN A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 185DN 27961 WHILE TROUBLESHOOTING SEAT 10A SNAKE LIGHT INOP ITEM, FOUND SCU TO BE EXTREMELY HOT. FURTHER T/S FOUND SNAKE LIGHT SHOR T HARNESS WHICH CONNECTS SNAKE LIGHT TO SEAT MAIN HARNESS WORN THROUGH AND ARCED TO SEAT BACK FRAME. THE HARNESS AT THI S POINT WAS ALSO EXTREMELY HOT. DEACTIVATED SNAKE LIGHT UNTIL PROBLEM CAN BE RECTIFIED. 2 L 7 2 4F RT A1NM 1999122300399 19991223 00399 NM 1999 12 23 DL72K992754 1 19991215 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CARGO BAY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 495DA 21075 EMERGENCY LIGHTS ON AFT CARGO DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1999122300400 19991223 00400 NM 1999 12 23 DL73E992755 1 19991215 A 7711 TRANSMITTER 774001004 BOEING 737 737247 138448D NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 380DL H0816 23607 717162 RIGHT ENGINE EPR IND INOP AFTER T/O, ALL OTHER ENGINE INDICATIONS NORMAL 30 MINS LATER. REPLACED NR 2 EPR TRANSMITTER, OPS CK OK ON ENGINE RUN. 2 L 7 2 4F 4 F A16WE E2EA 1999122300401 19991223 00401 NM 1999 12 23 DLM88992756 1 19991216 A 3397 WIRE RPS1 DOUG MD88 MD88 3023688 NM ROW 1 BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 905DL 3813 49536 ON PREFLIGHT CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS NOT WORKING. FOUND WIRE BROKEN IN SEAT TRACK AT ROW 1 C, D. RE PAIRED WIRE. REPLACED POWER SUPPLY AND BATTERY PACK. 2 L 7 2 4F RT A6WE 1999122300402 19991223 00402 NM 1999 12 23 DL72L992758 1 19991202 A 5330 655458041 SKIN BOEING 727 727232 1384082 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 GOUGE FOUND IN THE SKIN AT THE AFT EDGE OF THE C-2 DOOR CUTOUT AT FS 990. THE DAMAGE AREA IS LOCATED JUST BELOW STR 24R . DAMAGE IN SKIN, DOUBLER AND TRIPLER BUT NOT THE INTERNAL BEAR STRAP ER/A 333860-14 REV A. 2 L 7 3 4F A3WE 1999122300403 19991223 00403 1999 12 23 DLL10992759 2 19991215 A 7261 PUMP LKHEED 1011 10113851 5265010 WP NR 1 ENGINE WEAK A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 1731D 22249 193C1200 10662 A/C RETURNED FROM FLIGHT WITH A NR 1 ENGINE VIBRATION. FOUND THAT ENGINE WAS HIDING OIL IN GEAR CASE RESULTING IN A VIB RATION AT HIGHER POWER SETTINGS. GROUND RAN ENGINE AT HIGHER POWER SETTINGS UNTIL OIL SCAVENGED FROM GEAR CASE AND DRAI NED OFF EXCESS AS ENGINE WAS OVER SERVICED DUE TO HIDDEN OIL. ALSO, REPORTS OF SMOKE IN CABIN DUE TO OIL VAPOR IN CABIN FROM OVER SERVICED ENGINE. REPLACED ENGINE. 2 L 7 3 4F A23WE 1999122300404 19991223 00404 NM 1999 12 23 DL72L992760 1 19991216 A 5530 651754248 WEB BOEING 727 727232 1384082 NM VERTICAL STAB DENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 THE NR 4 RIB OF THE VERTICAL STABILIZER HAS A DENT IN THE WEB THAT RESULTED IN A 1 INCH DIAMETER CUTOUT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333924-14. 2 L 7 3 4F A3WE 1999122300405 19991223 00405 NM 1999 12 23 DL72S992761 1 19991216 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 380 CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 A .75 INCH LONG CRACK WAS FOUND EMANATING FROM A FASTENER HOLE NEAR THE UPPER FORWARD CORNER OF THE R1 DOOR CUTOUT (FS 3 80). THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 368954-14, REV A. 2 L 7 3 4F A3WE 1999122300406 19991223 00406 NM 1999 12 23 DL72S992762 1 19991215 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 THE WEB OF THE FS 1183 BULKHEAD WAS FOUND WITH A .75 INCH LONG TYPICAL CRACK AT RBL 26 AND WL 169. THE CRACK IS TYPICA L OF BOEING S/B 727-53-0215. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED PER THE S/B AS DOCUMENTED IN ER/A 368897- 14. 2 L 7 3 4F A3WE 1999122300407 19991223 00407 NM 1999 12 23 DL76L992763 1 19991216 A 2133 60683221 OUTFLOW VALVE BOEING 767 767332 1382001 NM FUSELAGE MALFUNCTIONED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 180DN 25985 DURING CLIMB, CABIN AUTO INOP CAUTION CAME ON EICAS. CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 STATUS MESSAGES. OPN NORMAL IN MANUAL. REMOVED AND REPLACED OUTFLOW VLV PER M/M, CKS GOOD. 2 L 7 2 4F RT A1NM 1999122300408 19991223 00408 NM 1999 12 23 DL76L992764 1 19991216 A 3350 0201804001 LENS BOEING 767 767332 1382001 NM ROW 1 MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 180DN 25985 SEAT 1AB MISSING 2 EMERGENCY ESCAPE PATH LIGHTING LENSES (WHITE) AND BULBS. REPLACED MISSING LENSES AND REPLACED BULBS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 1999122300409 19991223 00409 NM 1999 12 23 DL72W992765 1 19991216 A 5754 651622370 RIB BOEING 727 727247 138408F NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 NR 11 RIB CRACKED. REPAIRED PER M/M 57-54-0 FIG 804. 2 L 7 3 4F A3WE 1999122300410 19991223 00410 NM 1999 12 23 DL72W992766 1 19991216 A 5754 651622370 RIB BOEING 727 727247 138408F NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 NR 12 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0 FIG 804. 2 L 7 3 4F A3WE 1999122300411 19991223 00411 WP 1999 12 23 DLL10992767 1 19991216 A 3244 L1011N TIRE LKHEED 1011 10113851 5265010 WP NLG FAILED A DALA O OTHER O OTHER DE DESCENT 1 SO 27 729DA 193C1180 THUMP HEARD DURING DESCENT THROUGH 15,000 FT, FELT LIKE IT WAS UNDER COCKPIT LT SIDE. FOUND LT NOSE TIRE WITH BLOW OUT UNDER RETREAD CAUSING SEPARATION. REPLACED WHEEL ASSY. 2 L 7 3 4F A23WE 1999122300412 19991223 00412 NM 1999 12 23 DL72K992768 1 19991216 A 3350 61020 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 491DA 21060 FORWARD OUTBOARD FLIGHT ATTENDANT FLASHLIGHT NO TEST. REPLACED BATTERY. FLASHLIGHT NOW OPS NORMAL. 2 L 7 3 4F A3WE 1999122300413 19991223 00413 NM 1999 12 23 DL72S992769 1 19991216 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 498DA 21142 ON MTC LAYOVER, LT OUTSIDE EMERGENCY EGRESS LIGHTING INOP. REPLACED FWD LIGHT POWER SUPPLY. REPLACED BULBS FOR MID LIG HT AND REPLACED BATTERY PACK ON AFT LIGHT, OPER NOW NORMAL. 2 L 7 3 4F A3WE 1999122300414 19991223 00414 NM 1999 12 23 DL76S992770 1 19991201 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 STRINGER 39L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAG E WAS FOUND ON THE STRINGER. 2 L 7 2 4F RT A1NM 1999122300415 19991223 00415 NM 1999 12 23 DL76S992771 1 19991201 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 STRINGER 38L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAG E TO THE STRINGER WAS FOUND. 2 L 7 2 4F RT A1NM 1999122300416 19991223 00416 NM 1999 12 23 DL76S992772 1 19991201 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 STRINGER 37L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAG E TO THE STRINGER WAS FOUND. 2 L 7 2 4F RT A1NM 1999122300417 19991223 00417 NM 1999 12 23 DL76S992773 1 19991201 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 STRINGER 34L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAG E TO THE STRINGER WAS FOUND. 2 L 7 2 4F RT A1NM 1999122300418 19991223 00418 NM 1999 12 23 DL76S992774 1 19991201 A 5320 140T011516 SPLICE BOEING 767 767332 1382001 NM BS 434 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 STRINGER 37R SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAG E TO THE STRINGER WAS FOUND. 2 L 7 2 4F RT A1NM 1999122300419 19991223 00419 NM 1999 12 23 DL76S992775 1 19991206 A 5311 146T122330 FRAME BOEING 767 767332 1382001 NM BS 1562 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 FS 1562 FRAME FAIL-SAFE CHORD WAS FOUND CORRODED BETWEEN STR 38L AND STR 38R. THE (P/N 146T1223-30) CHORD WAS REPLACE D PER DWG 146T1223. 2 L 7 2 4F RT A1NM 1999122300420 19991223 00420 NM 1999 12 23 DL76S992776 1 19991201 A 5320 140T210223 SHEAR TIE BOEING 767 767332 1382001 NM BS 1562 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 THE FUSELAGE SKIN TO FRAME SHEAR TIE LOCATED ON THE AFT SIDE OF FRAME STA 1562 WAS FOUND CORRODED. THE (P/N 140T2102-23 ) SHEAR TIE WAS REPLACED PER DWG 146T1223. THE SHEAR TIE IS LOCATED BETWEEN STR 38L AND STR 38R. 2 L 7 2 4F RT A1NM 1999122300421 19991223 00421 NM 1999 12 23 DL76S992777 1 19991201 A 5320 140T2102656 SHEAR TIE BOEING 767 767332 1382001 NM BS 1562 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 THE FUSELAGE TO FRAME SHEAR TIE AT STA 1562 LOCATED ON THE FWD SIDE OF THE FRAME BETWEEN STR 38L AND 38R WAS FOUND CORRO DED. THE (P/N 150T2102-656) SHEAR TIE WAS REPLACED PER DWG 146T1223. 2 L 7 2 4F RT A1NM 1999122300422 19991223 00422 NM 1999 12 23 DL73K992779 1 19991216 A 2612 FIRE LOOP BOEING 737 737232 1384475 NM APU BAY MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 27 309DL 23081 ATTEMPTED APU START PRIOR TO LANDING, HAD INDICATION OF APU FIRE (LIGHTS AND BELLS). FIRE HANDLE PULLED, BOTTLE DISCHAR GED AND LIGHT EXTINGUISHED. INSPECTED APU AREA AND EXHAUST, SUSPECT FALSE INDICATION. REPLACED LOOP. 2 L 7 2 4F RT A16WE 1999122300423 19991223 00423 NM 1999 12 23 DL73K992781 1 19991217 A 5320 654587545 ANGLE BOEING 737 737247 138448D NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 242WA 23516 THE INNER CHORD ANGLE OF THE R1 DOOR SILL WAS FOUND CORRODED. A 1.5 X 1.0 CUTOUT WAS USED TO REMOVE THE DAMAGE. THIS W AS FOUND AT MV AND REPAIRED PER ERA 333863-14. 2 L 7 2 4F A16WE 1999122300424 19991223 00424 NM 1999 12 23 DL72L992782 1 19991201 A 5754 RIB BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2 FOUND NR 3 SLAT RIBS CRACKED. REPAIR AT RIB MARKED NR 3, RIB MKD NR 10, RIB MKD NR 17. CORROSION - DYE CKD AS PER PS 900-6-3 AND NO CRACKS. FABRICATED DOUBLER PER MM 57-54-0 PG 807. INSTALLED DOUBLER PER SAME, DYE CHECKED RIB N R 17 PER PS 900-6-3 STOP DRILLED CRACK, FABD DOUBLER PER MM 57-54-00 PG 813, CHEM TREAT PER PS 900-2-4-1 NR 02, FABD SHI MS PER MM 57-54-00 PG 813A, PAIT/TREAT, AND INSTALLED PER MM 57-54-00. 2 L 7 3 4F A3WE 1999122300425 19991223 00425 NM 1999 12 23 DL72L992783 1 19991130 A 5522 SKIN BOEING 727 727232 1384082 NM ELEVATOR TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 AT HMV2 ELEVATOR T/E CHIPPED/TORN LT ELEVATOR EXTREME O/B END. BUSHED AREA AND FOUND TO BE WITHIN LIMITS PER SRM 55-20- 1 FIG 161, INSTALLED FASTENERS. 2 L 7 3 4F A3WE 1999122300426 19991223 00426 NE 1999 12 23 DL76L992784 2 19991217 A 7220 BLADE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 179DN 36527 25144 724138 UPON ARRIVAL FOUND NUMBER 1 ENGINE WITH FAN BLADE DAMAGE AND FAN CASE DAMAGE. MTC FERRY TO ATL FOR REPAIR. REPLACED DA MAGED FAN BLADES AND 3 FAN EXIT GUIDE VANES BECAUSE OF DAMAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999122300427 19991223 00427 NM 1999 12 23 DLM11992785 1 19991217 A 3520 MC1004101 O2 MASK DOUG MD11 MD11 3023602 NM CABIN WON'T TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 802DE 48473 F/O O2 MASK WILL NOT TEST. REPLACED O2 MASK. 2 L 7 3 4F RT A22WE 1999122300428 19991223 00428 NM 1999 12 23 DL72S992786 1 19991217 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z WA6807 21291 EMERGENCY LIGHT ABOVE R2 DOOR INOP. REPLACED BATTERY PACK, OPS NORMAL. 2 L 7 3 4F A3WE 1999122300429 19991223 00429 NM 1999 12 23 DLM88992787 1 19991217 A 4910 APU 38005041 DOUG MD88 MD88 3023688 NM APU BAY CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 912DL P80530 49543 ON FINAL INTO CLE ON FLT 1156/17 AT 1000 FT, THE AFT FLT ATTN REPORTED AN OILY ODOR AND HAZE INDICATIONS IN CABIN. TAI L ANTI ICE WAS ON, LAV SMOKE ALARMS SOUNDED. ENG ANTI ICE WAS ALSO ON. INSPECTED ENG PNEU DUCTS, CHECKED GOOD. INSPEC TED A/C FOR HYD LEAK, NONE FOUND. REPLACED WATER SEPARATOR BAGS AND PERFORMED DUCT BURNOUT PROCEDURE, CHECKS GOOD. FOU ND OIL IN APU INLET DEACTIVATED APU PER MEL 49-00-01A. 2 L 7 2 4F RT A6WE 1999122300430 19991223 00430 NE 1999 12 23 DLM88992789 2 19991218 A 7321 76960615 FCU 38430110 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 27 916DL 9559 49591 718141 NR 1 ENGINE FLUCTUATIONS AND EVENTUAL SHUTDOWN. RETURNED TO CVG FLT 971. ENGINE SHUT DOWN ON ITS OWN AFTER 45 SECONDS OF FLUCTUATIONS FROM CLIMB POWER TO NEAR IDLE. RAN ENGINE TO T/O AND POWER SETTINGS BELOW ALL CKS OK, NO FLUX. PERFORM ED ACCELERATION CHECK. FAILED CHECK. REMOVED FUEL CONTROL AND FUEL PUMP. REINSTALLED FUEL PUMP. INSTALLED FUEL CONTR OL. LEAK CK OF FUEL CONTROL AND PUMP GOOD. RAN ENGINE PER PFHB, ALL PARAMETERS CK GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 1999122300431 19991223 00431 NM 1999 12 23 DL733992790 1 19991218 A 2750 TRANSMITTER 1817389 BOEING 737 73735B NM TE FLAP MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 27 221DL 3926 23970 SPLIT FLAP INDICATION AT 1 DEGREE FLAPS DURING DESCENT. MADE 1 DEGREE FLAP LANDING. REPLACED LEFT FLAP POSITION TRANSM ITTER. PERFORMED CHECK OUT PER M/M CHAP 27. FLAPS OPERATE NORMAL AND ALL INDICATIONS CHECK OK. 2 L 7 2 4F RT A16WE 1999122300432 19991223 00432 NM 1999 12 23 DLM88992791 1 19991219 A 7603 THROTTLE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE BINDING A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 936DL 21151 49723 726052 AFTER T/O, LEVELING AT 6,000 FEET, LEFT THROTTLE WOULD NOT MOVE BACK. STUCK AT F/F APPROX 6000 PPH. MOVING LEFT THROTT LE TOOK EXCESSIVE FORCE. COULD SEE LEFT FUEL CONTROL LEVER MOVING AS ATTEMPT WAS MADE TO MOVE LEFT THROTTLE. RETURNED CVG UNEVENTFULL LANDING. TURNING FINAL APPROACH, LEFT THROTTLE STARTED WORKING NORMALLY. THROTTLE AND FUEL CONTROL AT ENGINE, FUEL CONT CROSSOVER SHAFT-TELEFLEX CK NORMAL. RECONNECTED THROTTLE AND FUEL CONTROL. RAN ENGINE TO TAKEOFF PW R, NO TROUBLE FOUND. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999122300433 19991223 00433 NM 1999 12 23 DLM88992792 1 19991219 A 2170 WATER SEPARATOR 97968011 DOUG MD88 MD88 3023688 NM ACM BAY FAILED A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 906DL 994 49537 ON CLIMBOUT, TAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER LT ENG BROUGHT BACK TO IDLE/LT PACK O FF. F/A COMPLAINED OF SMOKE SMELL IN CABIN, THEN UNABLE TO MAINTAIN CABIN PRESSON RT PACK. REPLACED RT WATER SEPARATOR ANTI ICE VALVE. 2 L 7 2 4F RT A6WE 1999122300434 19991223 00434 NM 1999 12 23 DLM88992793 1 19991219 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 980DL 53267 PRIOR TO DEPARTURE CREW FOUND F/C EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS POWER SUPPLY. 2 L 7 2 4F RT A6WE 1999122300435 19991223 00435 NM 1999 12 23 DLM88992794 1 19991219 A 3244 MD88N TIRE DOUG MD88 MD88 3023688 NM NLG WORN A DALA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CL CLIMB 1 SO 27 902DL 49533 ON T/O, EXCESSIVE NOSE WHEEL SHIMMY FOLLOWED BY VIBRATION WHEN NOSE WHEEL SLOWED AGAINST SNUBBERS, BURNING RUBBER SMELL WAS EVIDENT FOR 3-5 MIN ON CLIMBOUT. CLEANED NOSE WHEEL SNUBBERS AND REPLACED NOSE WHEEL ASSY. 2 L 7 2 4F RT A6WE 1999122300436 19991223 00436 NM 1999 12 23 DL75A992796 1 19991218 A 3350 RPS1 PWR SUPPLY BOEING 757 757212 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750AT 23126 FWD CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A2NM 1999122300437 19991223 00437 WP 1999 12 23 DLL10992798 1 19991202 A 2780 LE FLAP 7000393 LKHEED 1011 10113851 5265010 WP WINGS MALFUNCTIONED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 730DA 344 193C1199 FLAP/SLAT LOCK LIGHT ILLUMINATED IMMEDIATELY AFTER TAKEOFF. PRIOR TO FLAP RETRACTION FLAPS RETRACTED OK BUT SLATS STAYE D AT FULL DOWN AND LOCKED. REPLACED LT SLAT BRAKE, CHECKS GOOD PER MM. WHEN THE STROBE LIGHT SWITCH WAS TURNED ON, ALL 3 SLAT COMPARTOR LIGHTS FLASH AND FLAP/SLAT LOCK ANNUN. ALSO, FAINT CRACKING SOUND WAS HEARD ON SER INTERPHNE. REPLAC ED STROBE FLASHER AND ALL OK. 2 L 7 3 4F A23WE 1999122300438 19991223 00438 EU 1999 12 23 RAIA9912029 1 19991214 A 2430 153LCA8 AMMETER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FLUCTUATED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 343TE 379 379 955 7470-STL- RIGHT AMMETER FLUCTUATES 20 TO 30 AMPS. MAINTENANCE DEFERRED AMMETER IAW MEL 24-1 CAT B. MAINTENANCE REPLA CED RIGHT AMMETER. 2 L 7 2 4T RT A56EU 1999122300439 19991223 00439 1999 12 23 RAIA9912030 2 19991210 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 428AM 874 874 877 7531-LEX- LEFT EGT GAUGE FLUCTUATED BETWEEN 400 AND FULL SCALE. MAINTENANCE DEFERRED PER MEL 76-2 CAT C. MAINTENANCE REPLACED LEFT ENGINE FUEL BYPASS VALVE. 2 L 7 2 4T RT A56EU 1999122300440 19991223 00440 EU 1999 12 23 RAIA9912031 1 19991220 A 7921 SYLC522454 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 560HK 6359 6359 41076 6150- JFK- ON TAXI OUT, NR 2 ENG OIL TEMP INCREASED. MAINTENANCE REPLACED NR 2 ENGINE OIL COOLER FLAP ACTUATOR. 2 L 7 2 4T RT A41NM 1999122300441 19991223 00441 NM 1999 12 23 TWRA9971 1 19991112 A 5210 65B100022 ROD BOEING 747 747130 1384880 NM PAX DOOR BROKEN A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FUOND L-1 DOOR GIRT BAR SUPPORT ROD TO LIFTER BROKEN. REMOVED AND REPLACED SUPPORT ROD, PER MM 52-1 1-07. REMOVED AND REPLACED SUPPORT ROD, PER MM 52-11-07. (M) 2 L 7 4 4F A20WE 1999122300442 19991223 00442 NM 1999 12 23 MZZA99215 1 19990928 A 5712 RIB BOEING 727 727232 1384082 NM WS 738.5 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING INSPAR WS 738.5 RIB UPPER FLANG E ATTACHED TO UPPER STRINGER 12. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 57-10-05 FIG 5. (M) 2 L 7 3 4F A3WE 1999122300443 19991223 00443 NM 1999 12 23 MZZA99216 1 19990928 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 629 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING UPPER STRINGER S-13 ATTACHED T O WS 629 RIB. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA NR 5762-01050. (M) 2 L 7 3 4F A3WE 1999122300444 19991223 00444 NM 1999 12 23 MZZA99217 1 19990922 A 5711 SPAR BOEING 727 727232 1384082 NM WS 221 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION OWAS FOUND ON LEFT WING FRONT SPAR WEB ABOVE FUEL BYP ASS VALVE ACTUATOR. THE DAMAGED AREA WAS BLENDED OUT AND REPAIRED PER CMI EC/RA NR 5710-01978. (M) 2 L 7 3 4F A3WE 1999122300445 19991223 00445 NM 1999 12 23 MZZA99218 1 19990928 A 5320 GUSSET BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AN IG CORROSION WAS FOUND ON GUSSET ATTACHED TO BS 950 BULKHEAD LOWER TEE CHORD AND STRINGER 29R INBOARD FLANGE. THE CORRODED GUSSET WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 SRM CHAPTER 51-10-01 AND 51-30-02. (M) 2 L 7 3 4F A3WE 1999122300446 19991223 00446 NM 1999 12 23 MZZA99219 1 19990928 A 5720 69139004 FITTING BOEING 727 727232 1384082 NM LT WING CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON LEFT WING BOTTLE PIN. THE CORRODED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE POWER SRM 53-30-02. (M) 2 L 7 3 4F A3WE 1999122300447 19991223 00447 NM 1999 12 23 MZZA99220 1 19991005 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1183 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO 2 INCH AND 1.5 INCH LONG CRACKS WERE FOUND ON BS 1183 BULKH EAD FRAME INBOARD AND OUTBOARD FLANGE AT RBL 36 AND WL 238. THE DAMAGED SECTION WAS REPAIRED PER CMI EC/RA NR 5310-0393 0 USING KIT NR 65C34406-12 AND DWG 65C34406. (M) 2 L 7 3 4F A3WE 1999122300448 19991223 00448 NM 1999 12 23 MZZA99221 1 19990928 A 5320 GUSSET BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON GUSSET ATTACHED TO BS 950 LOWER TEE C HORD AND STRINGER 29L IN FLANGE. THE CORRODED GUSSET WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-10-01 AND 51-30-0 2. (M) 2 L 7 3 4F A3WE 1999122300449 19991223 00449 NM 1999 12 23 MZZA99222 1 19990928 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO CRACKS WERE FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB LIG HTENING HOLES AT BS 1223. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02. (M) 2 L 7 3 4F A3WE 1999122300450 19991223 00450 NM 1999 12 23 MZZA99223 1 19991012 A 5320 FRAME BOEING 727 727232 1384082 NM BS 303 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 5 INCH AREA IG CORROSION WAS FOUND ON NLG BAY FUSEL AGE FRAME AT BS 303 BETWEEN STRINGER 25L AND STRINGER 26L. THE CORRODED FRAME WAS TRIMMED AND REPAIRED PER B727 SRM CHA PTER 53-30-03. (M) 2 L 7 3 4F A3WE 1999122300451 19991223 00451 NM 1999 12 23 MZZA99224 1 19991008 A 5320 TEE BOEING 727 727232 1384082 NM BS 294-312 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON NOSE WHEEL WELL TEE CHORD BETWEEN BS 294-312 AT STRINGER 26L. THE CORRODED T-CHORD WAS TRIMMED AND REPAIRED PER CMI EC/RA NR 5310-03937. (M) 2 L 7 3 4F A3WE 1999122300452 19991223 00452 NM 1999 12 23 MZZA99225 1 19990922 A 7603 CONTROL CABLE BOEING 727 727232 1384082 NM BS 1186 FRAYED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AIR ASIA, NR 1 ENGINE START CONTROL CABLE (ESS1A) WAS FOUND FRAYED AT BS 118 6. THE FRAYED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 76-12-01 AND OPERATIONAL CHECK FOUND NORMAL. (M) 2 L 7 3 4F A3WE 1999122300453 19991223 00453 NM 1999 12 23 MZZA99226 1 19991017 A 7603 CONTROL CABLE BOEING 727 727232 1384082 NM BS 1070 FRAYED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT ASIA, NR 3 ENGINE CONTROL CABLE (T3B) WAS FOUND FRAYED AT BS 1070. THE FRAY ED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 76-12-01 AND OPERATIONAL CHECK FOUND NORMAL. (M) 2 L 7 3 4F A3WE 1999122300454 19991223 00454 NM 1999 12 23 MZZA99227 1 19991004 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 920 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT KEEL BEAM STIFFENER LOWER END AT BS 920. THE CORRODED STIFFENER SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M) 2 L 7 3 4F A3WE 1999122300455 19991223 00455 NM 1999 12 23 MZZA99228 1 19991004 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 930 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT KEEL BEAM STIFFENER LOWER END AT WS 930. THE CORRODED STIFFENER SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M) 2 L 7 3 4F A3WE 1999122300456 19991223 00456 NM 1999 12 23 NOCA1199 1 19991116 A 3340 767 LAMP BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE FUSELAGE INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 DURING INSPECTION, EMERGENCY EXTERIOR LIGHTS AT 4L AND 4R INOPERATIVE. RELAMPED 4L AND 4R EMERGENCY EXTERIOR LIGHTS. O PS CHECK NORMAL. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1999122300457 19991223 00457 NM 1999 12 23 NOCA1099 1 19991116 A 2560 P4010021 FLASHLIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 DURING INSPECTION, EMERGENCY FLASHLIGHT AT R4 DOOR FLIGHT ATTENDANT JUMP SEAT FOUND INOPERATIVE. FLASHLIGHT AT R4 DOOR REPLACED, OPS CHECK OK. (M) 2 L 7 2 4F RT A2NM 1999122300458 19991223 00458 EU 1999 12 23 USAAF9053 1 19991104 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 858US 11291 CLT - THE COCKPIT EMERGENCY EXIT FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD BATTERY PACK. OPS CHECK ED NORMAL. (M) 2 L 7 2 4F RT 1999122300459 19991223 00459 NM 1999 12 23 USAASB99274 1 19991118 A 5210 SEAL BOEING 737 737201 1384454 NM PAX DOOR CONTAMINATED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 264AU 22961 CLT - FTL 2703 - EN ROUTE FROM BWI TO MIA, A LOUD SQUEALING NOISE BEGAN COMING FROM THE AFT LEFT ENTRY DOOR. NOISE WAS LOUD ENOUGH TO SCARE PASSENGERS AND IT WAS ALSO HARD TO COMMUNICATE. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED DEBRIS AND LUBRICATED THE AFT LEFT ENTRY DOOR SEAL WITH SOAPS TONE. PRESSURIZED AIRCRAFT. LEAK CHECK SATISFACTORY. (M) 2 L 7 2 4F A16WE 1999122300460 19991223 00460 NM 1999 12 23 USAA991297 1 19991118 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 22752 22752 BOS - DURING RON, FOUND .75 INCH CRACK ON SKIN AT STATION 767 ON STRINGER 21L. VISUAL CONFIRMED BY EDDY CURRENT AND DYE PENETRANT. INSTALLED DOUBLER AT STATION 767 ON STRINGER 21L PER SRM 53-30-3 FIG 6, PAGES 11 TO 12B, SHEETS 1 TO 4. (M ) 2 L 7 2 4F A16WE 1999122300461 19991223 00461 NM 1999 12 23 USAA991194 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.2 5INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999122300462 19991223 00462 NM 1999 12 23 USAA991193 1 19991111 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 663 STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300463 19991223 00463 NM 1999 12 23 USAA991218 1 19991111 A 5320 ANTENNA BASE BOEING 737 737301 1384611 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 12 INCH AREA OF CORROSION BETWEEN STRINGER 28 LT AND RT AFT OF STATION 500 ANTENNA BASE, CORROSION LEVEL 2. REPLACED ANTENNA BASE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300464 19991223 00464 NM 1999 12 23 USAA991215 1 19991111 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 420 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 420 STRINGER 4 LEFT SHEAR TIE. REMOVED AND REP LACED PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999122300465 19991223 00465 NM 1999 12 23 USAA991214 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500 RIGHT STRINGER 15 SHEAR TIE DAMAGE AT STRIN GER AND FRAME. REMOVED AND REPLACED PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999122300466 19991223 00466 NM 1999 12 23 USAA991213 1 19991111 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 2 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999122300467 19991223 00467 NM 1999 12 23 USAA991212 1 19991111 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 3 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999122300468 19991223 00468 NM 1999 12 23 USAA991211 1 19991111 A 5414 SKIN BOEING 737 737301 1384611 NM NR 2 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON NR 2 ENGINE PYLON AT ACCESS PANEL NR 5824R UPPER FORWA RD CORNER SKIN. INSTALLED DOUBLER PER EA 65982 AND TR 54-50-04D. (M) 2 L 7 2 4F RT A16WE 1999122300469 19991223 00469 NM 1999 12 23 USAA991210 1 19991111 A 5210 ANGLE BOEING 737 737301 1384611 NM PAX DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 10 INCH AREA OF CORROSION AT AFT ENTRY DOOR FLOOR Z-ANGLE, C ORROSION LEVEL 1. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300470 19991223 00470 NM 1999 12 23 USAA991208 1 19991111 A 5320 T-CAP BOEING 737 737301 1384611 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TEN 1 INCH BY 1 INCH AREAS OF CORROSION ON UPPER CAP OF T-CAP STATION 96 7, CORROSION LEVEL 2. REPLACED T-CAP PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999122300471 19991223 00471 NM 1999 12 23 USAA991207 1 19991111 A 5210 ANGLE BOEING 737 737301 1384611 NM PAX DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT AFT ENTRY DOOR Z-ANGLE (CHANNEL), CORROSIO N LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED AFT ENTRY DOOR Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300472 19991223 00472 NM 1999 12 23 USAA991206 1 19991111 A 5240 ANGLE BOEING 737 737301 1384611 NM SERVICE DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 20 INCH AREA OF CORROSION AT RT AFT SERVICE DOOR Z-ANGLE (FL OOR), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300473 19991223 00473 NM 1999 12 23 USAA991205 1 19991111 A 5347 SEAT TRACK BOEING 737 737301 1384611 NM BS 727B-947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AT BS 727B-947 SEAT TRACK, CORROSIO N LEVEL 2. INSTALLED SEAT TRACK PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 1999122300474 19991223 00474 NM 1999 12 23 USAA991204 1 19991111 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH MULTIPLE AREA OF CORROSION AT BS 986.5, RBL 44 - LBL 45, FLOORBEAM T-CAP. CORROSION LEVEL 2. REPLACED FLOORBEAM T-CAP PER TR 53-60-01 AND SRM 53-00-51 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999122300475 19991223 00475 NM 1999 12 23 USAA991198 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 908 STRINGER 9L BELT FRAME. INSTALLED DOUBLER P ER TR 53-10-14 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999122300476 19991223 00476 NM 1999 12 23 USAA991197 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999122300477 19991223 00477 NM 1999 12 23 USAA991196 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 867 STRINGER 9R BELT FRAME. INSTALLED DOUBLER P ER EA 65950 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999122300478 19991223 00478 NM 1999 12 23 USAA991195 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 827 STRINGER 9L BELT FRAME. INSTALLED DOU BLER PER EA 65950 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999122300479 19991223 00479 NM 1999 12 23 USAA991192 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STRINGER 8 AND 9L FRAME. INSTALLED D OUBLER PER TR 53-10-14 AND EA 65950. (M) 2 L 7 2 4F RT A16WE 1999122300480 19991223 00480 NM 1999 12 23 USAA991191 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727 STRINGER 14L OUTER CHORD ANGLE. REPAIRED DOUBL ER AND TRIPLER PER EA 65952. (M) 2 L 7 2 4F RT A16WE 1999122300481 19991223 00481 NM 1999 12 23 USAA991190 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK IN FUSE FRAME AT FASTENER HOLE BS 480 BETWEEN STRINGE R 8 AND 9R. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M) 2 L 7 2 4F RT A16WE 1999122300482 19991223 00482 NM 1999 12 23 USAA991189 1 19991111 A 5312 BULKHEAD BOEING 737 737301 1384611 NM STATION 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACKS IN 2 PLACES STATION 178 WEB A AND WEB B, LBL 1 AND RB L 1 SKIN. INSTALLED DOUBLER PER SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 1999122300483 19991223 00483 NM 1999 12 23 USAA991188 1 19991111 A 5330 SKIN BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS AT BS 663, LBL 32 CEILING PRESSURE DECK. INSTALLED DO UBLER PER TR 53-60-04 AND SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1999122300484 19991223 00484 NM 1999 12 23 USAA991187 1 19991111 A 5330 SKIN BOEING 737 737301 1384611 NM BS 111-166 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RIGHT HORIZONTAL STABILIZER LOWER SURFACE STATION 111- 166 SKIN. INSTALLED DOUBLER AND FILLER PER SRM 55-10-01 AND TR 55-10-07A. (M) 2 L 7 2 4F RT A16WE 1999122300485 19991223 00485 NM 1999 12 23 USAA991186 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK THROUGH RIVET HOLE BS 847, STRINGER 9R BELT FRAME. INST ALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999122300486 19991223 00486 NM 1999 12 23 USAA991185 1 19991111 A 5320 TIE CLIP BOEING 737 737301 1384611 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .250 INCH CRACK AT BS 727B STRINGER 4L TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300487 19991223 00487 NM 1999 12 23 USAA991184 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 807 STRINGER 9R BELT FRAME. INSTALLED DOU BLER PER EA 65950 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999122300488 19991223 00488 NM 1999 12 23 USAA991183 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 887 STRINGER 91 BELT FRAME. INSTALLED DOU BLER PER EA 65950 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999122300489 19991223 00489 NM 1999 12 23 USAA991182 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 787 STRINGER 9R BELT FRAME. INSTALLED DOU BLER PER EA 65950 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999122300490 19991223 00490 NM 1999 12 23 USAA991181 1 19991111 A 5320 BEAM BOEING 737 737301 1384611 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES T-CAP STATION 967 BEAM. REPAIRED DOUBLER AND T -CAP PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999122300491 19991223 00491 NM 1999 12 23 USAA991168 1 19991111 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 178, 5 INCHES BELOW FLOOR AT STIFFENER 3 SKIN. INSTALLED DOUBLER PER TR 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999122300492 19991223 00492 NM 1999 12 23 USAA991167 1 19991111 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 178, 5 INCHES BELOW FLOOR AT STIFFENER 2, SKIN . INSTALLED DOUBLER PER TR 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1999122300493 19991223 00493 NM 1999 12 23 USAA991166 1 19991111 A 5311 FRAME BOEING 737 737301 1384611 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 867 STRINGER 9R BELT FRAME. INSTALLED DOU BLER PER EA 65950. (M) 2 L 7 2 4F RT A16WE 1999122300494 19991223 00494 NM 1999 12 23 USAA991159 1 19991111 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH AREA OF CORROSION AT STATION 312, LBL 21 TO RBL 22 FLOORBEAM. C ORROSION LEVEL 2. CORROSION TASK NR C53-107-02. SPLICED IN NEW CAP SECTION PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999122300495 19991223 00495 NM 1999 12 23 USAA991158 1 19991111 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 597 STRINGER 1 SHEAR TIE SPLICE. INSTALLED SHE AR TIE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300496 19991223 00496 NM 1999 12 23 USAA991157 1 19991111 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .500 INCH WIDE AREA OF CORROSION AT STATION 360, CORROSION LEVEL 2. I NSTALLED STRAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1999122300497 19991223 00497 NM 1999 12 23 USAA991156 1 19991111 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK STATION 500 STRINGER 15R SHEAR TIE. INSTALLED SHEAR T IE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300498 19991223 00498 NM 1999 12 23 USAA991155 1 19991111 A 5320 SPLICE BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 908 STRINGER 4L SPLICE. INSTALLED NEW SPLICE PE R SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1999122300499 19991223 00499 NM 1999 12 23 USAA991154 1 19991111 A 5320 CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616 STRINGER 2L CLIP. INSTALLED TIE CLIP PER SR M 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999122300500 19991223 00500 NM 1999 12 23 MZZA99196 1 19990923 A 5320 TEE BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T EE CHORD BETWEEN STRINGER 29R AND S29L. THE CORRODED SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-10-01 AND 51-30-02. (M) 2 L 7 3 4F A3WE 1999122300501 19991223 00501 NM 1999 12 23 MZZA99197 1 19990923 A 5320 TEE BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 1 INCH AREA CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-CHORD AT RIGHT SIDE OF STRINGER 29R. THE CORRODED T-CHORD WAS TRIMMED AND REPAIRED PER CMI EC/RA NR 5310-3928. ( M) 2 L 7 3 4F A3WE 1999122300502 19991223 00502 NM 1999 12 23 MZZA99198 1 19990923 A 5314 KEEL BEAM BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY .5 INCH AREA CORROSION WAS FOUND S-29L KEEL BEAM OU TBOARD FLANGE AT BS 950 PLUS 14. THE CORRODED KEEL BEAM OUTBOARD FLANGE WAS TRIMMED AND REPAIRED PER B727 SB 53-0179. ( M) 2 L 7 3 4F A3WE 1999122300503 19991223 00503 NM 1999 12 23 MZZA99199 1 19991026 A 5320 T-CHORD BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER TEE OF STRINGER 29L. THE CORRODED T-CHORD SECTION WAS TRIMMED AND REPAIRED PER CMI EC/RA NR 5310-0397. (M) 2 L 7 3 4F A3WE 1999122300504 19991223 00504 NM 1999 12 23 MZZA99200 1 19990923 A 5314 KEEL BEAM BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY .5 INCH AREA IG CORROSION WAS FOUND ON STRINGER29R KEEL BEAM OUTBOARD FLANGE AT BS 950 PLUS 14. THE CORRODED T-CHORD SECTION WAS TRIMMED AND REPAIRED PER B727 SB 53-0179. (M) 2 L 7 3 4F A3WE 1999122300505 19991223 00505 NM 1999 12 23 MZZA99201 1 19990920 A 5320 652665117 FITTING BOEING 727 727232 1384082 NM AIRSTAIR CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON AFT AIRSTAIR LEFT LOWER STRUT END TO AIRST AIR FITTING. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-26651-17) PER B727 SRM CHAPTER 51-10-0 1. (M) 2 L 7 3 4F A3WE 1999122300506 19991223 00506 NM 1999 12 23 MZZA99202 1 19990920 A 5320 652665118 FITTING BOEING 727 727232 1384082 NM AIRSTAIR CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON AFT AIRSTAIR RIGHT LOWER STRUT END TO AIRS TAIR FITTING. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-26651-18) PER B727 SRM CHAPTER 51-10- 01. (M) 2 L 7 3 4F A3WE 1999122300507 19991223 00507 NM 1999 12 23 MZZA99203 1 19991006 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 740 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPE R CHORD AT BS 740. THE CORRODED SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 53-30-02 AND 51-10-01. (M) 2 L 7 3 4F A3WE 1999122300508 19991223 00508 NM 1999 12 23 MZZA99204 1 19990929 A 5311 FRAME BOEING 727 727232 1384082 NM BS 783.9 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON FUSELAGE FRAME BETWEEN STRINGE R 16R AND 17R AT BS 783.9. THE DAMAGED SECTION WAS TRIMMED AND REPAIRED PER BOEING DRAWING NR 65C36280 USING REPAIR KIT NR 65C36280-24. (M) 2 L 7 3 4F A3WE 1999122300509 19991223 00509 NM 1999 12 23 MZZA99205 1 19990923 A 5330 SKIN BOEING 727 727232 1384082 NM BS 730-734 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN AT STRINGER 17R BETWEEN BS 730 AND BS 734. THE DAMAGED SECTION WAS TRIMMED AND REPAIRED PER CML ECRA NR 5330-2891. (M) 2 L 7 3 4F A3WE 1999122300510 19991223 00510 NM 1999 12 23 MZZA99206 1 19991006 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 740 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPE R CHORD AT BS 740 AND LBL 25. THE CORRODED SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M) 2 L 7 3 4F A3WE 1999122300511 19991223 00511 NM 1999 12 23 MZZA99207 1 19991005 A 5320 WEB BOEING 727 727232 1384082 NM BS 1184 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON TAIL SKID DRAG FORWARD WEB AT BS 1184. T HE CORRODED WEB WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-03. (M) 2 L 7 3 4F A3WE 1999122300512 19991223 00512 NM 1999 12 23 MZZA99208 1 19991005 A 5210 BRACKET BOEING 727 727232 1384082 NM PAX DOOR CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AN IG CORROSION WAS FOUND ON L2 CABIN DOOR FORWARD STOP FITTING SUPPORT BRACKET. THE CORRODED FITTING WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M) 2 L 7 3 4F A3WE 1999122300513 19991223 00513 NM 1999 12 23 MZZA99209 1 19990922 A 5520 BEAM BOEING 727 727232 1384082 NM ELEVATOR CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON LEFT STABILIZER UPPER T /E BEAM AT ELEV STAB 146. THE CORRODED AREA WAS REMOVED AND REPAIRED PER B727 SRM CHAP 55-10-06. (M) 2 L 7 3 4F A3WE 1999122300514 19991223 00514 NM 1999 12 23 MZZA99210 1 19990922 A 5542 SKIN BOEING 727 727232 1384082 NM RUDDER BULGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 4 INCH AREA BULGE WAS FOUND ON UPPER RUDDER SKIN AT FIN STATION 213. THE BULGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-40-02 FIG 1 AND 55-20-03 FIG 1. (M) 2 L 7 3 4F A3WE 1999122300515 19991223 00515 NM 1999 12 23 MZZA99211 1 19990928 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223-1243 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUR CRACKS WERE FOUND ON RIGHT LOWER TORQUE BOX VERTICAL WEB L IGHTENING HOLES BETWEEN BS 1223 AND BS 1243. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02. (M ) 2 L 7 3 4F A3WE 1999122300516 19991223 00516 NM 1999 12 23 MZZA99212 1 19990922 A 5542 SKIN BOEING 727 727232 1384082 NM RUDDER BULGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTIN ON AIRCRAFT AT AIR ASIA, A 7 INCH BY 3 INCH AREA BULGE WAS FOUND ON UPPER RUDDER SKIN AT FIN STATION 270. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-40-02, 55-20-03. (M) 2 L 7 3 4F A3WE 1999122300517 19991223 00517 NM 1999 12 23 MZZA99213 1 19990922 A 5711 BAC15141688 SPAR BOEING 727 727232 1384082 NM WS 401 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD VE RTICAL LEG AT FSS 401. THE CORRODED SECTION WAS CLEANED UP AND REPAIRED PER CMI EC/RA NR 5710-01975. (M) 2 L 7 3 4F A3WE 1999122300518 19991223 00518 NM 1999 12 23 MZZA99214 1 19990928 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 629 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING UPPER STRINGER S-9 ATTACHED TO WS 629 RIB. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA NR 5762-01050. (M) 2 L 7 3 4F A3WE 1999122300519 19991223 00519 SO 1999 12 23 C2XA99BT109 1 19991120 A 2120 UNKNOWN EMB 145 EMB145 3260210 SO COCKPIT SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 14947 145054 YHZ - FLT 4309 - CREW REPORTED SMOKE IN CABIN FROM APU. A/C RELEASED IAW MEL NR 49-00-00 CAT C PLACARD NR 211420. RETU RNED TO SERVICE. AFTER ARRIVING EWR CO3982, MAINTENANCE REAN APU WITH BLEED AND PACKS ON AND AIRCRAFT CLOSED UP. NO SM OKE NOTED IN CABIN. CLEARED MEL AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999122300520 19991223 00520 SO 1999 12 23 C2XA99CL124 1 19991118 A 5210 14525311401 SEAL EMB 145 EMB145ER SO PAX DOOR FAILED A C2XA B A EMER. DESCENT UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 09 14945 145049 CLE - FLT 4234 - THE CREW REPORTED THAT THE MAIN CABIN DOOR DEVELOPED A LEAK AND THEY LOST PRESSURE. THE AIRCRAFT RETUR NED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN MAIN DOOR SEAL IAW EMB145 MM 52-1 8-04. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999122300521 19991223 00521 NM 1999 12 23 P2EA99324 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 695 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 695, RBL 45.5 INCH AND WL 202 INCH. REPAIRED FLOORBEAM LOWER CHORD FROM BS 689.5 TO BS 701.5. (M) 2 L 7 2 4F A16WE 1999122300522 19991223 00522 NM 1999 12 23 P2EA99323 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 673 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 673, RBL 45.5 INCH AND WL 20 INCH. REPAIRED FLOORBEAM LOWER C HORD FROM BS 667.5 TO BS 683. (M) 2 L 7 2 4F A16WE 1999122300523 19991223 00523 NM 1999 12 23 P2EA99322 1 19991103 A 5320 BEAM BOEING 737 737297 1384480 NM BS 704 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, PRESSURE DECK LOWER BEAM IN LEFT WHEEL WELL CRACKED AT BS 704, LBL 30 INCH AND L 0. FABRICATED BE AM USING EXTRUSION AND 10140-2002 IAW SRM 51-20-1 AND INSTALLED IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999122300524 19991223 00524 NM 1999 12 23 P2EA99321 1 19991110 A 5311 RIB BOEING 737 737297 1384480 NM BS 695 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, RIB CRACKED AT BS 695, LBL 45.5 AND WL 206 INCH. FABRICATED WEB IAW SRM 51-20-2 AND INSTALLED IAW 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999122300525 19991223 00525 NM 1999 12 23 P2EA99320 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 707 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM CRACKED AT BS 707, BL 0 AND WL 204. REPAIRED FLOORBEAM FROM BS 698 AND BS 717 IAW SERVI CE BULLETIN 737-57-1210 PART III FIG 5, DATED APRIL 4, 1999. REPAIRED IN CONJUNCTION WITH NON-ROUTINE 697. (M) 2 L 7 2 4F A16WE 1999122300526 19991223 00526 NM 1999 12 23 P2EA99319 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 712 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM WEB CRACKED AT BS 712, BL 0 AND WL 204 INCH. REPAIRED FLOORBEAM FROM BS 698 AND BS 717 IAW SERVICE BULLETIN 737-57-1210 PART III FIG 5. REPAIRED IN CONJUNCTION WITH NON-ROUTINE 700. (M) 2 L 7 2 4F A16WE 1999122300527 19991223 00527 WP 1999 12 23 99ZZZM808 2 19991118 A 7250 30723111 BLADE BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R 01518 WP LP TURBINE BROKEN A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 270KA NA0307 ENGINE WAS DISASSEMBLED FOR SCHEDULED MPI. DISCOVERED A FIRST STAGE LOW PRESSURE TURBINE BLADE FAILURE. THE SINGLE BLA DE HAD FAILED AT THE MID-POINT OF THE BLADE. ALL OF THE FIRST STAGE AND 2ND STAGE LPT BLADES SUFFERED DAMAGE AND WILL B E REPLACED. 10 OF THE THIRD STAGE LPT BLADES HAD DAMAGE. THE FIRST STAGE LOW PRESSUER TURBINE NOZZLE WILL BE REPLACED DUE TO FOD. (M) 2 L 7 2 4F 4 F A3EU E6WE 1999122300528 19991223 00528 NM 1999 12 23 AALA994186 1 19991104 A 5730 SKIN BOEING 767 767223 1385123 NM LT/RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 305AA 22311 AFW - LEFT AND RIGHT WING UPPER SURFACE HAS CORROSION REMOVAL AS SHOWN ON SKETCH. BLEND OUT CORROSION. PERFORMED HFEC BLENDED AREA FOR CRACKS, ROTO PEEN PER SRM. APPLY ALODINE AND PRIMER TO REWORKED AREA. (M) 2 L 7 2 4F RT A1NM 1999122300529 19991223 00529 EU 1999 12 23 AALA991655 1 19991028 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - THIRD SEAT TRACK INBOARD FROM L2 DOOR, JUST FORWARD OF LAV L CORRODED. TEMP REPAIR INSTALLED PER ESO 30595 DATED 10-28-99. (M) 2 L 7 2 4F RT A35EU 1999122300530 19991223 00530 EU 1999 12 23 AALA991668 1 19991105 A 5754 RIB AIRBUS 300 A300B4605R 3930308 EU LE FLAP CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70079 619 TUL - FORMER RIB CRACKED BETWEEN RIVETS TOP FLANGE OUTBOARD OF L/E KRUEGER FLAP ACTUATOR. STOP DRILLED AND INSTALLED RE PAIR DOUBLER FITTING PER ESO 30595, DATED 11/05/99. (M) 2 L 7 2 4F RT A35EU 1999122300531 19991223 00531 EU 1999 12 23 AALA991698 1 19991112 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 54.1-54.3 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - LEVEL 2 CORROSION BEYOND LIMITS. REMOVED AND REPLACED STRINGER SECTION FROM STATION 54.1 TO 54.3 AS PER SRM 53-10 -14. (M) 2 L 7 2 4F RT A35EU 1999122300532 19991223 00532 EU 1999 12 23 AALA991686 1 19991110 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - LEVEL 2 CORROSION BEYOND LIMITS. COMPLETED A STRINGER SPLICE IAW SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1999122300533 19991223 00533 EU 1999 12 23 AALA991680 1 19991109 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - LEVEL 2 WIDESPREAD CORROSION ON FITTING AND FRAME. REMOVED AND REPLACED FITTING PER 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999122300534 19991223 00534 EU 1999 12 23 AALA991679 1 19991109 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - LEVEL 2 WIDESPREAD CORROSION ON FITTING AND FRAME. REMOVED AND REPLACED FITTING PER 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999122300535 19991223 00535 EU 1999 12 23 AALA991808 1 19991122 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU BS 38.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND CORROSION ON AFT SIDE OF FLOORBEAM AT FRAME 38.2 BETWEEN NR 4 AND NR 5 ROLLER TRAYS. REMOVED AND REPLACED F LOORBEAM AT FRAME 38.2 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999122300536 19991223 00536 EU 1999 12 23 AALA991809 1 19991129 A 5320 STIFFENER AIRBUS 300 A300B4605R 3930308 EU BS 13-14 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - VERTICAL STIFFENERS IS CRACKED ON RIGHT CONNECTING FITTING IN NLG BAY BET FRAME 13A AND FRAME 14. BLENDED CRACK W ITHIN MAX BLEND DEPTH OF .314, RESULTANT BLEND IS ACCEPTALE FOR AN ADDITIONAL 3.300 FC BEFORE PERMANENT REPAIRS ARE REQ IAW S/B 53-6102 AND ESO 30595 DATED 11/29/99. (M) 2 L 7 2 4F RT A35EU 1999122300537 19991223 00537 EU 1999 12 23 AALA991810 1 19991129 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU B 56-58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - CORROSION ON BOTTOM NR 5 ROLLER TRAY FRAMES 56 AND 58. REMOVED AND REPLACED NR 5 ROLLER TRAY FROM FRAME 56 TO FRA ME 63 IAW SRM 57-72-10. (M) 2 L 7 2 4F RT A35EU 1999122300538 19991223 00538 EU 1999 12 23 AALA991811 1 19991129 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 58-63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND CORROSION ON BOTTOM OF NR 3 ROLLER TRAY AT FRAME 58. REMOVED AND REPLACED NR 3 ROLLER TRAY FROM FRAME 58 TO FRAME 63 IAW SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999122300539 19991223 00539 EU 1999 12 23 AALA991812 1 19991129 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 58-63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND CORROSION ON BOTTOM OF NR 1 ROLLER TRAY AT FRAME 58 IN AFT CARGO COMPARTMENT. REMOVED CORRODED ROLLER TRAY AND INSTALLED NEW ROLLER TRAY FROM FRAME 58 TO FRAME 63 IAW SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1999122300540 19991223 00540 EU 1999 12 23 AALA991806 1 19991123 A 5320 SILL AIRBUS 300 A300B4605R 3930308 EU BS 59-63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND CORROSION ON AFT CX DOOR JAMB LOWER SILL BEAM FROM FRAME 59 TO FRAME 63. REMOVED CORROSION INSTALLED SILL B EAM REPAIR AT FRAME 60 IAW SRM 53-17-18 AND ESO 30595 DATED 11-17-99 AND DATED 11-22-99, OTHER BLENDOUTS THAT WERE OUT O F LIMITS PER SRM ARE OK PER ESO 30595 DATED 11-22-99 AFTER TREATING, PRIMING, PAINTING, AND APPLY A CORR PRSV COMPOUND. (M) 2 L 7 2 4F RT A35EU 1999122300541 19991223 00541 EU 1999 12 23 AALA991807 1 19991123 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 60-62 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - STRINGER 50R IS CORRODED FROM FRAME 60 TO FRAME 62. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER SRM 53-10-14 AND ESO30595 DATED 11-22-99. (M) 2 L 7 2 4F RT A35EU 1999122300542 19991223 00542 EU 1999 12 23 AALA991786 1 19991126 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND CORROSION ON BOTTOM AND TOP OUTBOARD AFT CORNER OF NR 5 ROLLER TRAY AT FRAME 58. REMOVED CORROSION AND SPLI CED IN NEW SECTION OF ROLLER TRAY IAW 51-74-01 AND 53-10-15-2 BOTH OF THE SRM. (M) 2 L 7 2 4F RT A35EU 1999122300543 19991223 00543 EU 1999 12 23 AALA991763 1 19991119 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 64 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND STRINGER 52L IS CORRODED BELOW FRAME 64. REMOVED CORROSION AND INSTALLED REPAIR SPLICE IAW SRM 53-10-14. ( M) 2 L 7 2 4F RT A35EU 1999122300544 19991223 00544 EU 1999 12 23 AALA991760 1 19991121 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 62 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND CORROSION ON STRINGER 52L AT FRAME 62. INSTALLED NEW REPAIR STRINGER ON 52L AT FRAME 62 PER ESO 30595, DATE D 11-19-99. (M) 2 L 7 2 4F RT A35EU 1999122300545 19991223 00545 EU 1999 12 23 AALA991753 1 19991118 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU BS 72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FOUND CORROSION ON STRINGER SPLICES AT STRINGER 45L, 46L, AND 47L IN AREA OF FRAME 72. REMOVED AND REPLACED STRIN GER SPLICES AT STRINGER 45L, 46L, AND 47L AT FRAME 72. (M) 2 L 7 2 4F RT A35EU 1999122300546 19991223 00546 WP 1999 12 23 AALA991725 1 19991103 A 5313 STRINGER DOUG DC9 DC982 3022082 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - STRINGER 4L CRACKED AT STATION 160 LEFT. REPLACED DAMAGED SECTION AND INSTALLED SPLICE PER 53-02. (M) 2 L 7 2 4F A6WE 1999122300547 19991223 00547 WP 1999 12 23 AALA991726 1 19991102 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 518 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - FOUND CORROSION ON NR 1 SEAT TRACK AT STATION 518. REMOVED DAMAGED AREA. INSTALLED PLUG IN SEAT TRACK PER AARD 5 3-20-00-10. (M) 2 L 7 2 4F A6WE 1999122300548 19991223 00548 WP 1999 12 23 AALA991727 1 19991117 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1155-1250 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - NR 1 SEAT TRACK CORROSION STATION 1214 DOME NUT 20 EACH SEAT TRACK LUGS CORROSION. INSTALLED NEW SEAT TRACK FROM STATION 1155-1309 SRM 51-01. (M) 2 L 7 2 4F A6WE 1999122300549 19991223 00549 WP 1999 12 23 AALA991728 1 19991110 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 826 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - INBOARD LUG ON NR 4 SEAT TRACK WORN STATION 826. CUTOUT DAMAGED AREA AND INSTALLED SEAT TRACK PLUG REPAIR PER AAR D 53-20-00-10. (M) 2 L 7 2 4F A6WE 1999122300550 19991223 00550 WP 1999 12 23 AALA991729 1 19991103 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1307 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - SHEAR TIE CRACKED AT STATION 1307, L16, LEFT. REMOVED CRACKED SHEAR TIE FS 1307 STRINGER 16 LEFT. INSTALLED NEW SERVICEABLE SHEAR TIE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 1999122300551 19991223 00551 WP 1999 12 23 AALA991730 1 19991102 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1429 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - SHEAR TIE CRACKED JUST INBOARD OF VERTICAL STABILIZER SPAR FITTING RIGHT, AFT SIDE OF STATION 1429. REPLACED SHEA R TIE JUST INBOARD OF VERTICAL STABILIZER SPAR FITTING RIGHT, AFT SIDE OF STATION 1429 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 1999122300552 19991223 00552 WP 1999 12 23 AALA991731 1 19991116 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174-1200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - FOUND CORROSION ON SEAT TRACK STATION 1174 TO 1200 TRACK NR 3. REMOVED CORROSION AND INSTALLED REPAIR 2 PLACES PE R SRM AND 1 PLACE PER ESO 80559. (M) 2 L 7 2 4F A6WE 1999122300553 19991223 00553 WP 1999 12 23 AALA991732 1 19991110 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - REF E58 NR 0141593, CORROSION ON LEFT CUSP AT STATION 1231 (UNDER SEAT TRACK). INSTALLED NEW CUSP STATION 1174 TO 1250 PER SRM 51-01. (M) 2 L 7 2 4F A6WE 1999122300554 19991223 00554 WP 1999 12 23 AALA991733 1 19991110 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - FOUND CORROSION ON LEFT CUSP AND EXTENDING UNDER DOUBLER AT STATION 1271 APPROX LBL 48. INSTALLED NEW CUSP FROM S TATION 1250-1305 SRM 51-01. (M) 2 L 7 2 4F A6WE 1999122300555 19991223 00555 WP 1999 12 23 AALA991734 1 19991104 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 305 DAMAGED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 294AA 49306 TUL - TOOLING DAMAGE IN SKIN T STATION 305, LONG 3R. ACCOMPLISHED REPAIR PER GUIDELINES OF SRM 53-04 FIG NR 38 ALONG WI TH THE FOLLOWING, AT THE AFT END OF DOUBLER OVERLAP EXISTING INTERNAL DOUBLER ONE ROW MINIMUM AND OMIT FINGERS AT THE OV ERLAPPED DOUBLER PER ESO80559, DATED 11/3/99. (M) 2 L 7 2 4F A6WE 1999123000001 19991230 00001 WP 1999 12 30 TWAA9916901 1 19991214 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 4 - 16 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 914TW 49185 THE CABIN EGRESS LIGHTS WERE INOPERATIVE FROM ROW 4 TO 16. FOUND FEEDER CABLE BROKEN AND SPLICED CABLE TOGETHER. CHECK -C 2-13-99 MCI. 2 L 7 2 4F A6WE 1999123000002 19991230 00002 1999 12 30 TWAA9917001 4 19991215 A 2312 G1977 VHF RADIO DOUG DC9 DC982 3022082 WP COCKPIT CONTAMINATED A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 914TW 49185 THE NUMBER 1 AND 2 VHF COMM RADIOS WERE INOPERATIVE AFTER TAKEOFF. STATIC WAS TRANSMITTED ON ANY FREQUENCY SELECTED. F LIGHT RETURNED TO STL. FOUND MOISTURE IN THE CAPTAINS AUDIO SELECTOR PANEL AND REPLACED THE PANEL. CHECK-C 2-13-99 MCI . 2 L 7 2 4F A6WE 1999123000003 19991230 00003 WP 1999 12 30 TWAA9917002 1 19991215 A 2134 LINE DOUG DC9 DC982 3022082 WP OUTFLOW VALVE LOOSE A TWAA G B A O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 917TW 49366 CRUISING AT FL310 CABIN PRESSURIZATION WAS LOST. PASSENGER OXYGEN MASKS DEPLOYED. MADE AN UNSCHEDULED LANDING AT RNO. TIGHTENED A LOOSE SENSE LINE AT THE LEFT FLOW CONTROL VALVE. CHECK-C 7-13-99 STL. 2 L 7 2 4F A6WE 1999123000004 19991230 00004 EA 1999 12 30 JBXA9900130 1 19991216 A 5210 WARNING LIGHT CNDAIR CL600 CL6002B19 EA PAX DOOR ILLUMINATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 579ML 7224 PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE CAME ON IN FLIGHT. APPLIED QRH PROCEDURE ABNORMAL 5-5 AND LIGHT DID NOT GO OUT. RETURNED TO MCO. ASSIGNED TO DMI NR 07328 PER MIDWAY MOC LS 11026, RELEASED PER MEL 52-70-1. 2 L 7 2 4F RT A21EA 1999123000005 19991230 00005 NM 1999 12 30 SCNA99777 1 19991211 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING A HEAVY MAINTENANCE CHECK THE LEFT AFT GALLEY OUTBOARD SEAT TRACK TIE DOWNS WERE FOUND TO BE CORRODED OUT OF LIMI TS. FABRICATED NEW SEAT TRACK FROM STA 1070 TO STA 1110. TREATED, PRIMED AND INSTALLED NEW SEAT TRACK PER SRM 51302 AND 51202. 2 L 7 3 4F A3WE 1999123000006 19991230 00006 WP 1999 12 30 TWAA9917101 1 19991216 A 2150 20495052 ACM DOUG DC9 DC982 3022082 WP AIR DISTRIBUTION LEAKING A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 917TW 49366 SHORTLY AFTER TAKEOFF SMOKE APPEARED IN THE COCKPIT AND CABIN, LIGHT IN NATURE. FLIGHT RETURNED TO STL. FOUND RIGHT AIR CYCLE MACHINE LEAKING OIL INTO DUCT. REPLACED THE ACM. CHECK-C 7-13-99 STL. ---CLOSED---- 2 L 7 2 4F A6WE 1999123000007 19991230 00007 NM 1999 12 30 TWAA9917102 1 19991216 A 3350 20131A BATTERY BOEING 767 767205 1385121 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 650TW 23057 THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE ON RT SIDE OF CABIN, ROW 22 AFT. REPLACED POWER SUPPLY. CHECK-C 11-7-99 LAX. 2 L 7 2 4F RT A1NM 1999123000008 19991230 00008 EU 1999 12 30 QXEA9902621 1 19991219 A 3310 561408B212 BALLAST GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT OVERHEATED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 493US 11161 SEA - ELECTRICAL SMELL ON FIRST OFFICERS SIDE FLOOD LIGHTING. MAINTENANCE INSPECTED AND FOUND SOURCE OF SMELL TO BE FRO M LIGHTING BALLAST. REMOVED AND REPLACED BALLAST, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999123000009 19991230 00009 EU 1999 12 30 QXEA9902620 1 19991217 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 PDX - FOWARD CABIN EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999123000010 19991230 00010 EU 1999 12 30 QXEA9902619 1 19991217 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 3053 3053 11229 SEA- OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999123000011 19991230 00011 WP 1999 12 30 TWAA9917201 1 19991220 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 913TW 49184 THE AFT SECTION OF CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 12-20-99. 2 L 7 2 4F A6WE 1999123000012 19991230 00012 NM 1999 12 30 QXEA9902622 1 19991217 A 5610 SYL250970 CONTROLLER PPG DHAV DHC8 DHC8102 2809003 NM WINDSCREEN MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 827PH 13201 8633 93216H2849 275 PDX- ON APPROACH, A STRONG SMELL WAS NOTED IN THE COCKPIT. AFTER LANDING AND ENGINE SHUT DOWN, SMELL LINGERED. SMOKE A ND SMELL WAS NOTED IN THE COCKPIT ONLY, NOT THE CABIN. MAINTENANCE REPLACED THE PILOT'S WINDSHIELD AND WINDSHIELD HEAT CONTROLLER. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999123000013 19991230 00013 NM 1999 12 30 QXEA9902602 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 500 - 545 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND INBOARD SEAT TRACK CHAFED AT APPROXIMATELY STATION 500 TO 520 AND 545. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000014 19991230 00014 NM 1999 12 30 QXEA9902600 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 445 - 470 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND INBOARD SEAT TRACK CHAFED AT APPROXIMATELY STATION 445, 456 AND 470. REPAIRED IAW DHC-8 SRM 51-20-16 AN D 51-21-36. 2 H 7 2 4T RT A13NM 1999123000015 19991230 00015 NM 1999 12 30 QXEA9902601 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 488 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND INBOARD SEAT TRACK CHAFED AT STATION 488 AND LUG LIP WORN. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-2 0-36. 2 H 7 2 4T RT A13NM 1999123000016 19991230 00016 EU 1999 12 30 QXEA9902624 1 19991219 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 PDX- THE SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING LIGHTS ON ROWS 1-4 CAME ON AND WOULD NOT RESET. MAI NTENANCE FOUND A LOOSE CONNECTION UNDER SEAT 1A. RESEATED CONNECTION AND REPLACED BATTERY PACK. OPERATIONAL CHECKS GOO D. 2 L 7 2 4F RT A20EU 1999123000017 19991230 00017 EU 1999 12 30 QXEA9902623 1 19991219 A 3350 XB864041 LIGHT ASSY FOKKER F28 F28MK4000 4990810 EU ROW 8 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 481US 11230 PDX- SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROW 8AB BROKEN. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1999123000018 19991230 00018 NM 1999 12 30 SCNA99778 1 19991213 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 1070 - 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING A HEAVY MAINTENANCE CHECK, THE RIGHT FORWARD GALLEY INBOARD SEAT TRACK TIE DOWNS WERE FOUND TO BE CORRODED OUT OF LIMITS. FABRICATED NEW SEAT TRACK FROM STA 1070 TO STA 1110. TREATED, PRIMED AND INSTALLED NEW SEAT TRACK PER SRM 513 02 AND 51202. 2 L 7 3 4F A3WE 1999123000019 19991230 00019 NM 1999 12 30 PCAA9900063 1 19991222 A 5210 GAS STRUT DHAV DHC8 DHC8102 2809003 NM PAX DOOR FAILED A PCAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 13 830EX 155 PIT- FLIGHT 3774- PRIOR TO DEPARTURE THE CABIN DOOR WAS FOUND DIFFICULT TO CLOSE. MAINTENANCE INSPECTED, OPERATED DOOR , NO DEFECTS FOUND. SUBSEQUENT MAINTENANCE REPLACED THE FORWARD DOOR GAS STRUT IAW DHC MAINTENANCE MANUAL PROCEDURES, O PERATIONAL CHECK PROVED SATISFACTORY. 2 H 7 2 4T RT A13NM 1999123000020 19991230 00020 NM 1999 12 30 QXEA9902665 1 19991220 A 3350 10005511 LAMP ASSY DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 363PH 2639 520 PDX - OVERHEAD EMERGENCY LIGHT CAME ON. REPLACED OVERHEAD EMERGENCY LANTERN ASSEMBLY. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1999123000021 19991230 00021 NM 1999 12 30 QXEA9902603 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 500 - 520 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED FROM APPROXIMATELY STATION 500 TO 520. REPAIRED IAW DHC-8 SRM 51-20-36 AND S RM 51-20-16. 2 H 7 2 4T RT A13NM 1999123000022 19991230 00022 NM 1999 12 30 QXEA9902604 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 456 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED AND NICKED AT APPROXIMATELY STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000023 19991230 00023 NM 1999 12 30 QXEA9902605 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 436 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED IN BOTTOM OF TRACK APPROXIMATELY 10 FROM STATION 436. REPAIRED IAW DHC08 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000024 19991230 00024 NM 1999 12 30 QXEA9902639 1 19991212 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION AROUND RIVET LEFT-HAND SIDE OF STRINGER 33 AT FRAME STATION 488. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999123000025 19991230 00025 NM 1999 12 30 QXEA9902640 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 456 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT-HAND INBOARD SEAT TRACK CHAFED AND NICKED AT APPROXIMATELY STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000026 19991230 00026 EA 1999 12 30 JBXA9900132 1 19991225 A 5210 WARNING LIGHT CNDAIR CL600 CL6002B19 EA PAX DOOR ILLUMINATED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 587ML 7346 PAX DOOR WARNING AFTER TAKEOFF. CLEANED DOOR SWITCHES AND REGREASED PAX DOOR IAW AMM 12-20-52. DOOR OPS CHECKED NORMAL LY IAW AMM 52-11-02. 2 L 7 2 4F RT A21EA 1999123000027 19991230 00027 EA 1999 12 30 JBXA9900133 1 19991225 A 5242 DOOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE FUSELAGE OPEN A JBXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 573ML 7227 AIR NOISE COMING FROM FUSELAGE NOSE SECTION, F/O SIDE ON TAKEOFF. CLOSED GROUND POWER CONNECTION DOOR AS REQUIRED, NO D AMAGE FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 1999123000028 19991230 00028 NM 1999 12 30 PCAA9900064 1 19991224 A 5210 CABLE DHAV DHC8 DHC8102 2809003 NM PAX DOOR KINKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 828EX 392 FLIGHT 3715- UPON ARRIVAL INTO BOS THE CREW COULD NOT OPEN THE PASSENGER DOOR. PASSENGERS WERE DEPLANED THROUGH THE RIG HT FORWARD EMERGENCY EXIT. MAINTENANCE INSPECTED AND FOUND THE DOOR CABLE WAS KINKED AND BOUND AROUND THE LOWER PULLEY. MAINTENANCE REMOVED AND REPLACED THE DOOR GAS STRUTS AND DOOR CABLES. OPERATIONAL CHECKED PROVED SATISFACTORY. 2 H 7 2 4T RT A13NM 1999123000029 19991230 00029 WP 1999 12 30 TWAA9917301 1 19991220 A 5730 PLATE DOUG DC9 DC931 3022065 WP NR 1305 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 990Z 47136 THE LEFT WING FUEL TANK PLATE NUMBER 1305 DOUBLER WAS CRACKED 1.75 INCH LONG AT THE 8 O'CLOCK POSITION. REPAIRED CRACKE D DOUBLER PER ARA 16436 AT LT WING FUEL TANK DOUBLER NUMBER 1305. CHECK-C 9-21-98 STL. 2 L 7 2 4F A6WE 1999123000030 19991230 00030 WP 1999 12 30 TWAA9917303 1 19991226 A 3350 0105601003PA57 LIGHT DOUG DC9 DC983 3022083 WP ROW 11 DISCONNECTED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9409F 53121 THE EGRESS LIGHTING AT SEAT ROW 11 WAS DISCONNECTED. REPLACED BROKEN TRACK LIGHTING COVER AND RECONNECTED THE LIGHT. C HECK-C 5-18-99 STL. 2 L 7 2 4F RT A6WE 1999123000031 19991230 00031 NM 1999 12 30 TWAA9917304 1 19991222 A 3350 LIGHT BOEING 757 757231 1384950 NM ROWS 1 & 2 DISCONNECTED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 703TW 27620 THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROWS 1 AND 2. FOUND LOOSE CONNECTION. RECONNECTED LAMPS. CHECK-C 9-12-99 LAX. 2 L 7 2 4F RT A2NM 1999123000032 19991230 00032 NE 1999 12 30 TWAA9917302 2 19991220 A 7314 37820178 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LT ENGINE FAILED A TWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 CE 05 987Z 47137 2116 THE LEFT ENGINE SPOOLED DOWN JUST AFTER TAKEOFF, PRIOR TO FLAP RETRACTION. FLIGHT RETURNED TO STL. REPLACED THE ENGINE FUEL PUMP. CHECK-C 4-26-99 MCI. 2 L 7 2 4F 4 F A6WE E2EA 1999123000033 19991230 00033 NM 1999 12 30 QXEA9902641 1 19991210 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CLIP CORROSION BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 467. REPAIRED IAW DHC-8 SRM 53-20-21, FIGUR E 1. 2 H 7 2 4T RT A13NM 1999123000034 19991230 00034 NM 1999 12 30 QXEA9902642 1 19991216 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 445 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CLIP CORROSION BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGUR E 1. 2 H 7 2 4T RT A13NM 1999123000035 19991230 00035 NM 1999 12 30 QXEA9902643 1 19991216 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 445 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CLIP CORROSION BETWEEN LEFT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1. 2 H 7 2 4T RT A13NM 1999123000036 19991230 00036 NM 1999 12 30 QXEA9902644 1 19991215 A 3010 CONNECTOR DHAV DHC8 DHC8102 2809003 NM DEICE SYSTEM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - INSPECT DEICE DISTRIBUTOR CANNON PLUGS AND PRESSURE SWITCHES FOR CORROSION AND SERVICEABILITY. REMOVED AND REPLAC ED PRESSURE SWITCHES. (S/N 6503, 3509, 7020 AND 6951). 2 H 7 2 4T RT A13NM 1999123000037 19991230 00037 NM 1999 12 30 QXEA9902645 1 19991210 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND FORWARD CONNECTION ANGLE WAS CRACKED THROUGH THE OUTBOARD RADIUS. REPAIRED IAW HORIZON AIR EA 9-53-348A . 2 H 7 2 4T RT A13NM 1999123000038 19991230 00038 NM 1999 12 30 QXEA9902646 1 19991210 A 5320 BRACKET DHAV DHC8 DHC8102 2809003 NM BS 636 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - A .25 INCH CHAFE MARK ON TIE IN BRACKET AT FRAME X636.0 AND STRINGER 22S. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 1999123000039 19991230 00039 NM 1999 12 30 QXEA9902647 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 405.737 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL AT STATION 405.737. REPAIRED IAW DHC-8 SRM 51-20 -16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000040 19991230 00040 NM 1999 12 30 QXEA9902648 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL BETWEEN STRINGER 467.000 AND 445.500, LESS THAN 1 INCH LONG. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000041 19991230 00041 NM 1999 12 30 QXEA9902649 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 467 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL 4 AFT OF STATION 467.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000042 19991230 00042 NM 1999 12 30 QXEA9902650 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 488.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAD LIGHT CORROSION INSIDE CHANNEL AT STATION 488.500. REPAIRED IAW DHC-8 SRM 51-20 -16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000043 19991230 00043 NM 1999 12 30 QXEA9902651 1 19991218 A 5321 FLOOR PANEL DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - MAIN ENTRY THRESHOLD WHERE FLOOR PANEL ATTACHES HAD NUMEROUS SPOTS OF CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1999123000044 19991230 00044 EU 1999 12 30 QXEA0992666 1 19991222 A 3350 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX - MID CABIN FORWARD FACING EXIT SIGN WAS REPORTED AS INOPERATIVE. THE AFFECTED SIGN WAS REMOVED AND REPLACED, OPERA TIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999123000045 19991230 00045 NM 1999 12 30 QXEA9902653 1 19991216 A 5320 SPLICE DHAV DHC8 DHC8102 2809003 NM BS 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON STRINGER SPLICE AT STATION 531 AND STRINGER 30 RT. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-40-11 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000046 19991230 00046 NM 1999 12 30 QXEA9902654 1 19991211 A 5320 SPLICE DHAV DHC8 DHC8102 2809003 NM BS 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON STRINGER SPLICE AT STATION 531 AND STRINGER 29 RT. REPAIRED IAW PSM 1-GEN-5, CHAPTER 4, PAGE 4-21, P ARAGRAPH 8D AND DHC-8 SRM 53-00-16, PAGE 4, TABLE 2. 2 H 7 2 4T RT A13NM 1999123000047 19991230 00047 NM 1999 12 30 QXEA9902655 1 19991211 A 5320 SPLICE DHAV DHC8 DHC8102 2809003 NM BS 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - MINOR CORROSION ON TOP FLANGE OF STRINGER SPLICE AT STATION 531 AND STRINGER 28 RT. ACID ETCHED, ALODINED, AND PR IMED. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW DHC-8 SRM 53-00-16, PAGE 4, TABLE 2. 2 H 7 2 4T RT A13NM 1999123000048 19991230 00048 NM 1999 12 30 QXEA9902656 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 540 - 543 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - PITTING CORROSION AND NICKS ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 540-543. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123000049 19991230 00049 NM 1999 12 30 QXEA9902657 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - MINOR CORROSION ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 531. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-3 6. 2 H 7 2 4T RT A13NM 1999123000050 19991230 00050 NM 1999 12 30 QXEA9902658 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 471 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - MINOR CORROSION ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 471. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-3 6. 2 H 7 2 4T RT A13NM 1999123000051 19991230 00051 NM 1999 12 30 QXEA9902659 1 19991210 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 456 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - MINOR CORROSION ON RIGHT-HAND OUTBOARD SEAT TRACK AT STATION 456. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-3 6. 2 H 7 2 4T RT A13NM 1999123000052 19991230 00052 NM 1999 12 30 QXEA9902660 1 19991219 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION INBOARD SIDE OF RIGHT-HAND STRINGER 32 AT FRAME STATION 488. INSTALLED NEW STRINGER SPLICE IAW DHC-8 SR M 51-40-11. 2 H 7 2 4T RT A13NM 1999123000053 19991230 00053 NM 1999 12 30 QXEA9902661 1 19991211 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CLIP HAS CORROSION BETWEEN RIGHT-HAND STRINGER 31 AND 32 AT FRAME STATION 531. REPAIRED IAW DHC-8 SRM 51-20-11, P AGE 1-2, PARAGRAPH 1 AND 2 AND SRM 51-20-11, PAGE 6, PARAGRAPH 2C. 2 H 7 2 4T RT A13NM 1999123000054 19991230 00054 NM 1999 12 30 QXEA9902662 1 19991210 A 5320 CLIP DHAV DHC8 DHC8102 2809003 NM BS 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CLIP HAS CORROSION OUTBOARD END BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 531. REPAIRED IAW PSMI-GEN- 5, CHAPTER 4, PART 2, PARAGRAPH 3, 1, PAGE 4-4. 2 H 7 2 4T RT A13NM 1999123000055 19991230 00055 NM 1999 12 30 QXEA9902663 1 19991221 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 550 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - SMALL GOUGE IN LEFT-HAND STRINGER 31 AT APPROXIMATELY STATION 550. REPAIRED IAW HORIZON AIR EA 9-53-532. 2 H 7 2 4T RT A13NM 1999123000056 19991230 00056 NM 1999 12 30 QXEA9902664 1 19991214 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 242 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT OUTBOARD SEAT TRACK HAS CHAFING PITS ON INBOARD LIP APPROXIMATELY STATION 242. REPAIRED IAW DHC-8 SRM 51-20- 16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 1999123100001 19991231 00001 EA 1999 12 31 CA991103071 1 19991031 A 2120 601R952162 DUCT ASSY CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE AIR DIST DEFECTIVE W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) CABIN ALT WARNING AT FL 330. IMPOSSIBLE TO CONTROL CABIN PRESSURE IN MANUAL MODE. PROGRESSIVE RETURN TO NORMAL P ASSING THROUGH FL 220. PRESSURE REGULATOR AND RELIEF VALVES REPLACED. NEXT FLIGHT EXPERIENCED SAME MALFUNCTION. AIR I NLET DUCT FOUND DEFECTIVE AND REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999123100002 19991231 00002 NM 1999 12 31 CA991208005 1 19991107 A 2823 42828DB FUEL VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE WING LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 121158 851115 (CAN) DURING SCHEDULED MAINTENANCE, FUEL WAS OBSERVED DRIPPING FROM THE FUEL-DEFUEL VALVE SCUPPER DRAIN LINE. THE VALVE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100003 19991231 00003 NM 1999 12 31 CA991208013 1 19991112 A 3397 33422D20AT WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NAV LIGHTS CHAFED W K NONE L NO TEST IN INSP/MAINT 1 CA 30917 120648 881221 (CAN) DURING PRE-FLIGHT, IT WAS DISCOVERED THAT THE PORT NAV LIGHTS WERE NOT ILLUMINATING. THE PROBLEM WAS TRACED TO AN OPEN CIRCUIT IN THE NAV LIGHT WIRING IN THE PORT WING LEADING EDGE. THE WIRE APPEARED TO HAVE CHAFED THE EDGE OFTHE WI RE CONDUIT WHERE IT EXITED THE CONDUIT BEHIND THE NR 4 LEADING EDGE PANEL. THE SUBMITTER SUGGESTED THAT THE WIRE SHORTE D OUT OFTEN ENOUGH TO BURN THROUGH THE CONDUCTOR COMPLETELY. NO REPORTS OF TRIPPED CIRCUIT BREAKERS WERE SUBMITTED BY ANY FLIGHT CREW MEMBERS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100004 19991231 00004 EA 1999 12 31 CA991208019 1 19991124 A 3320 BV0330012150 RECEPTACLE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CABIN FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 123116 900837 (CAN) DURING REPLACEMENT OF AN INOPERATIVE CABIN OVERHEAD FLUORESCENT LIGHT, THE AFT TUBE RECEPTACLE WAS FOUND IN A BURN ED/MELTED CONDITION. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100005 19991231 00005 NM 1999 12 31 CA991208028 1 19991123 A 2530 1095BL COFFEE WARMER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE GALLEY FAILED W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 1401 123124 901161 (CAN) THE FLIGHT CREW REPORTED AN ELECTRICAL SMELL IN THE CABIN DURING TAKEOFF AND RETURNED TO THE AIRPORT. MAINTENANCE INVESTIGATION REVEALED THE COFFEE WARMER TO BE MALFUNCTIONING AND REPLACED IT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100006 19991231 00006 1999 12 31 CA991208059 4 19990911 A 3457 GPS155XL GPS SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE COCKPIT FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 95000775 280327KL (CAN) AFTER LANDING ON DECK, THE GARMIN GPS DROPPED OFF-LINE AND PERFORMED AN AUTOMATIC RE-BOOT. 2 G 7 2 4U 4 U 1H15 1E3 1999123100007 19991231 00007 CE 1999 12 31 CA991208065 1 19991110 A 3260 1CH16 SWITCH 23171005 LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP NLG FAILED W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA 2390 P89721 (CAN) WHEN THE GEAR WAS SELECTED DOWN ON APPROACH, THE NOSE GEAR FAILED TO INDICATE DOWN AND LOCKED. THE EMERGENCY EXTE NSION SYSTEM WAS USED AND THE AIRCRAFT LANDED SAFELY. THE NOSE GEAR DOWN AND LOCKED SWITCH ON THE NOSE GEAR WAS DIAGNOS ED TO BE AT FAULT. 2 L 7 2 4F 4 F A10CE E6WE 1999123100008 19991231 00008 SW 1999 12 31 CA991208070 1 19991103 A 5302 4070238001178 SUPPORT 407023800101 BELL 407 407 SW ALLSN 250C 250C47B GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1978 53022 CAE847023 (CAN) FOLLOWING OVERTORQUE INSPECTION (113 PERCENT FOR .1 SEC), CRACKS WERE NOTICED (3) IN THE BEND RADIUS OF THE HORIZ ONTAL STABILIZER UPPER SUPPORTS. PARTS WERE REPLACED IAW BELL REPAIR SCHEME. NO OTHER DEFECTS NOTED. REPAIR SCHEME INCLUDES INSTRUCTIONS ON SHIMMING SUPPORTS (FOUND WITHOUT SHIMS FROM BELL). SUBMITTER STATED SHIMMING INFO NOT FOUND IN MAINTENANCE MANUALS. 1 G 7 1 3U 3 U O H2SW E1GL 1999123100009 19991231 00009 EU 1999 12 31 CA991208078 1 19991102 A 3297 WIRE BAG JETSTM JETSTM3212 1500217 EU GARRTT TPE331 TPE33110UG 01514 WP ROTOL R333 R333482F12 GL MLG BROKEN W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA P63174C DRG138781 (CAN) WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH, THE INTRANSIT AND GEAR DOWN LIGHTS FAILED TO ILLUMINATE. THE CREW FOUND THE GEAR INDICATION CIRCUIT BREAKER TRIPPED AND RESET IT, AT WHICH TIME THE LIGHTS OPERATED NORMALLY. MA INTENANCE TRACED THE PROBLEM TO A CHAFED/SHORTED WIRE IN THE LANDING GEAR INDICATION CIRCUIT. 2 L 7 2 4T 4 T RT BA15CAA E4WE 6 C P61GL 1999123100010 19991231 00010 SO 1999 12 31 CA991208080 1 19991110 A 3297 487862 WIRE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2A GL LT MLG BROKEN W L ABORTED APPROACH H N ELECT. POWER LOSS-50 PC FALSE WARNING AP APPROACH 1 CA 13907 L775961A DJ11100A (CAN) ON APPROACH TO DESTINATION AIRPORT, PILOT SELECTED GEAR DOWN AND FAILED TO GET INDICATION THAT THE MAIN GEAR WAS D OWN AND LOCKED. THE GEAR WAS SELECTED SEVERAL TIMES WITH THE FAILED LEFT MAIN DOWN AND LOCKED INDICATION STAYING EXTING UISHED. INSPECTION BY MAINTENANCE REVEALED THE GEAR WAS LOCKED, BUT A BROKEN WIRE CAUSED THE GREEN LAMP TO FAIL. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1999123100011 19991231 00011 SW 1999 12 31 CA991208087 1 19991122 A 7603 205060751003 BELLCRANK T5313B BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE POWER LEVER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA LE07569X LE07569X (CAN) BELLCRANK FAILED ON POWER LEVER. 1 G 7 1 4U 4 U H1SW E17EA 1999123100012 19991231 00012 WP 1999 12 31 CA991208092 1 19991125 A 2435 PW203PP BEARING LUCAS 23032027 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL STARTER/GEN WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 10836 (CAN) AMO RECEIVED SG AND FOUND THE A.D.E. BEARING TO BE NOISY AND ROUGH AND ALSO UNAPPROVED. PROPER OEM BEARINGS INSTA LLED P/N 03-6009-23. ARMATURE WAS THEN RESURFACED, BALANCED AND BRUSHES WERE SEATED. UNAPPROVED BEARINGS WERE QUARANTI NED. 1 G 7 1 3U 3 U H3WE E4CE 1999123100013 19991231 00013 EU 1999 12 31 CA991208093 1 19991125 A 2435 230321423 BEARING 150S6122Q SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE STARTER/GEN WRONG PART W O OTHER K FLUID LOSS IN INSP/MAINT 1 CA 1382 5875 4002 (CAN) ADE BEARING SUPPORT ASSY FOUND AT OVERHAUL TO HAVE LUCAS P/N WHICH IS NOT APPROVED ON APC SG'S. IT REQUIRED REPAI R TO THE BEARING LINER AND REPLACEMENT OF ITS CIRCUIT BOARD ASSY BEFORE IT CAN BE RE-USED ON IT LUCAS 23032-018 SG. SUB SEQUENTLY, A NEW ASSY, APC P/N 150SG 1153 WAS PROCURED AND INSTALLED. THE SUPPORT ASSY IS QUARANTINED. 1 G 7 1 3U 3 U H9EU E19EU 1999123100014 19991231 00014 EA 1999 12 31 CA991209001 2 19990929 A 7414 K3984 CAPACITOR SLICK 4370 CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA MCAULY 1C160 1C160CTM GL MAGNETO FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 49 86100124 L3226127A 726350 (CAN) MAGNETO SNAGGED AS U/S ON AIRCRAFT BUT TESTED OK ON THE TEST BENCH. THE MAGNETO WAS DISASSEMBLED FOR INSPECTION A ND WHEN THE CAPACITOR WAS TESTED, IT SHOWED EXCESSIVE CURRENT LEAKAGE TO GROUND. THE SUBMITTER STATES THAT THE SUBJECT C APACITOR TESTED OK AT THE PREVIOUS OVERHAUL. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999123100015 19991231 00015 SW 1999 12 31 CA991209004 1 19990928 A 5510 2060201214 FITTING 2060201234 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820310 (CAN) HORIZONTAL STABILIZER FITTING FOUND CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 1999123100016 19991231 00016 EU 1999 12 31 CA991209008 1 19990930 A 6520 BEARING 350A33200401 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R GEARBOX FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 9604 831 M205 4294 (CAN) UNIT FAILED THE ROTATIONAL DRAG TORQUE CHECK SET OUT IN DGAC AD 1999-085-076(A)R2. 1 G 7 1 3U 3 U NC H9EU E19EU 1999123100017 19991231 00017 NE 1999 12 31 CA991209009 2 19991030 A 7532 9550158260 BLEED VALVE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 304 453 4294 (CAN) ENGINE BLEED AIR BUTTERFLY VALVE WOULD NOT CLOSE AT 97 PERCENT. TACHOMETER BOX OPERATION VERIFIED AND VALVE REPLA CED. NOW SERVICEABLE. 1 G 7 1 3U 3 U NC H9EU E19EU 1999123100018 19991231 00018 EU 1999 12 31 CA991209010 1 19990930 A 6520 350A33020004 GEARBOX SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 7693 831 M923 4294 (CAN) UNIT MAKING METAL (GENEROUS AMOUNTS). 1 G 7 1 3U 3 U NC H9EU E19EU 1999123100019 19991231 00019 NM 1999 12 31 CA991209015 1 19991111 A 7330 282111D20 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL PRESSURE CHAFED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 120255 880520 (CAN) DURING CLIMB, THE CREW NOTICED THE FUEL PRESSURE WARNING LIGHT FLICKER. THE BOOST PUMP WAS TURNED ON AND HAD NO E FFECT ON THE WARNING LIGHT. THE FLIGHT RETURNED TO THE AIRPORT FOR LANDING. MAINTENANCE FOUND A CHAFING/SHORTING WIRE IN THE FUEL PRESSURE WARNING CIRCUIT. THE WIRE WAS CHAFING ON THE AFT SIDE OF THE ENGINE FUEL HEATER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100020 19991231 00020 CE 1999 12 31 CA991209019 1 19991120 A 7921 AE3663163K0600 HOSE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE OIL COOLER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 22961 PC0554 (CAN) HOSE FOUND LEAKING AT SWAGED ON END FITTINGS. 1 H 7 1 3T 3 T A37CE E4EA 1999123100021 19991231 00021 CE 1999 12 31 CA991209022 1 19991122 A 3260 903610373 SWITCH BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA HARTZL HCB3T HCB3TN3 GL LT MLG BROKEN W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA PCE25222 BU22221 (CAN) C90A KINGAIR EN ROUTE FROM WINNIPEG TO EDMONTON. ON ARRIVAL EDMONTON, GEAR SELECTED DOWN, CREW OBSERVED 2 GREEN L IGHTS AND A RED LIGHT IN HANDLE. CREW SELECTED GEAR UP AND PROCEEDED TO CALGARY DUE TO WEATHER CONDITIONS. GEAR SELECT ED DOWN IN CALGARY. FIELD AVIATION IN CALGARY REPLACED LEFT HAND GEAR DOWNLOCK SWITCH, P/N 90-361037-3. 1 L 7 2 3T 4 T RT 3A20 E4EA 6 C P15EA 1999123100022 19991231 00022 1999 12 31 CA991209027 4 19991102 A 2312 7926657003 TRANSCEIVER COLLINS VHF20 LEAR 25 25B 5170511 CE GE CJ610 CJ6108 30006 NE AVIONICS BAY MALFUNCTIONED W O OTHER O OTHER AP APPROACH 1 CA 9568 2890 211361A (CAN) AFTER FLYING THROUGH RAIN ON APPROACH, COMMUNICATION RADIOS BECAME GARBLED/UNREADABLE. BENCH CHECK OF UNITS REVEAL ED TRANSCEIVER UNITS TO BE INTERNALLY CONTAMINATED WITH WATER. NO LEAKS IN THE NOSE CONE COULD BE FOUND. 2 L 7 2 4J 4 J A10CE 1E16 1999123100023 19991231 00023 SW 1999 12 31 CA991209029 1 19991022 A 3231 222031194101 LINK DOOR BELL 222 222 1182122 SW LYC LTS101 LTS101650C3 41560 NE NLG DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA LE41151AE (CAN) DURING INSPECTION, A VISIBLE CRACK WAS FOUND AT ROD END ATTACHMENT HOLE. THE PART SEPARATED IN HALF DURING REMOVA L. NOTE: THIS IS A PLASTIC PART. 1 G 7 2 3U 3 U H9SW E5NE 1999123100024 19991231 00024 CE 1999 12 31 CA991209030 1 19991110 A 2720 03101965 SPRING CESSNA 172 172I 2072426 CE LYC O320 O320E2D 41508 EA MCAULY 1C172 1C172MTM GL RUDDER PEDAL BROKEN W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 5554 L4718527A E9810 (CAN) DURING TAXI, THE PILOT HEARD A SNAP AND COULD NO LONGER EXECUTE RIGHT TURNS. MAINTENANCE FOUND THE LEFT RUDDER PE DAL RETURN SPRING BROKEN. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1999123100026 19991231 00026 1999 12 31 CA991209047 4 19991209 A 2350 506111 CONTROL HEAD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE COCKPIT FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 120063 860117 (CAN) DURING PRE-FLIGHT INSPECTION, MAINTENANCE PERSONNEL NOTICED A BURNING SMELL COMING FROM THE RIGHT AUDIO PANEL. IN VESTIGATION REVEALED THAT THE LIGHTING CIRCUIT IN THE SUBJECT CONTROL HEAD HAD SHORTED DUE TO WATER CONTAMINATION. THE SUBMITTER DETERMINED THAT THE WATER CAME FROM A LEAKING EMERGENCY ESCAPE HATCH SEAL. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100028 19991231 00028 CE 1999 12 31 CA991209050 1 19991119 A 7110 18559212 BRACKET 4141859011 BEECH 18 E18S9700 1151008 CE PWA R985 R985AN14B 52008 NE HAMSTD 22D 22D30 NE LT ENGINE BROKEN W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 436714 E2248 (CAN) AIRCRAFT WAS ON FLIGHT FROM DAYTON TO OSHAWA. IN THE CLIMB THROUGH 6,500 FEET, THE LEFT COWL CAME FORWARD AT THE TOP 304 INCHES. THE CREW DECIDED TO RETURN TO DAYTON AND LANDED UNEVENTFULLY. TWO BRACKETS ON THE UPPER PART OF THE CO WL WERE FOUND BROKEN. 1 L 7 2 3R 3 R A765 5E1 5 C P736 1999123100029 19991231 00029 NM 1999 12 31 CA991209052 1 19991107 A 2761 A44700009 ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SPOILER LEAKING W A UNSCHED LANDING K F FLUID LOSS FLT CONT AFFECTED TO TAKEOFF 1 CA 28192 0409 120421 LH714 (CAN) AFTER TAKEOFF, SUBSTANTIAL RIGHT AILERON INPUT WAS REQUIRED TO KEEP THE AIRCRAFT LEVEL. MAINTENANCE FOUND THE RIG HT HAND SPOILER ACTUATOR TO HAVE AN INTERNAL LEAK. THE SPOILER ACTUATOR WAS REPLACED AND A TEST FLIGHT WAS CARRIED OUT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100030 19991231 00030 NM 1999 12 31 CA991209053 1 19991108 A 2910 82950010193 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 25612 120581 LH9917 (CAN) DURING TAXI, HYDRAULIC FLUID WAS SEEN LEAKING FROM THE RIGHT ENGINE NACELLE AREA. MAINTENANCE FOUND A LEAK IN THE HYDRAULIC LINE FOR THE NR 2 SPOILER UNLOADING VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100031 19991231 00031 NM 1999 12 31 CA991209054 1 19991024 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG MALFUNCTIONED W O OTHER N FALSE WARNING DE DESCENT 1 CA 17267 137 121075 LH532 (CAN) DURING DESCENT, THE LEFT LANDING GEAR DOWN AND LOCKED LIGHT (GREEN) CAME ON INTERMITTENTLY UNTIL THE LANDING GEAR WAS SELECTED DOWN. MAINTENANCE REPLACED THE PSEU AND GROUND CHECKED THE SYSTEM WITH NO FURTHER FAULTS FOUND. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100032 19991231 00032 NM 1999 12 31 CA991209055 1 19991107 A 7920 DSC2831 HOSE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ENGINE OIL LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 30736 120338 890605 (CAN) DURING PRE-FLIGHT INSPECTION, OIL WAS NOTICED DRIPPING FROM THE NR 2 ENGINE LOWER COWLING. MAINTENANCE FOUND THE OIL SUPPLY HOSE BETWEEN THE OIL FILTER HOUSING AND THE OIL COOLER WAS LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100033 19991231 00033 NM 1999 12 31 CA991209056 1 19991110 A 3250 MS21250H03006 BOLT 86005 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NLG STEERING FAILED W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 25546 DCL1178798 120273 LH10007 (CAN) DURING TAXI, LOUD NOISE WAS HEARD, FOLLOWED BY A LOSS OF NR 2 SYSTEM HYDRAULIC PRESSURE. MAINTENANCE FOUND 2 FAIL ED BOLTS ON THE STEERING MANIFOLD COMPENSATOR CAP. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999123100034 19991231 00034 CE 1999 12 31 CA991209057 1 19991115 A 3244 650X106 TIRE GOODYEAR BEECH 100 A100 1152915 CE PWA PT6 PT6A34 52043 EA HARTZL HCB4T HCB4TN3 GL MLG FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 91501128 PCE57492 EAA1075 (CAN) ON TAKEOFF, THE LEFT INBOARD MAIN WHEEL ASSEMBLY SHED ITS ENTIRE TREAD. ALTHOUGH THIS WAS A RECAPPED TIRE, THE TR EAD DID NOT SEPARATE AT THE RECAP. IN THIS CASE, THE RETREAD LAYER AND THE LAYER OF THE RUBBER FROM THE RETREAD TO THE FIRST LAYER OF CORD SEPARATED FROM THE REST OF THE TIRE. THE TREAD DAMAGED THE GEAR DOOR AS IT CAME APART, BUT DID NOT CAUSE ENOUGH DAMAGE TO THE GEAR TO AFFECT ITS OPERATION. THE AIRCRAFT LANDED WITHOUT INCIDENT, THE TIRE WAS CHANGED. T HE TIRE REMAINED INFLATED EVEN THOUGH ITS TREAD WAS MISSING. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 1999123100035 19991231 00035 CE 1999 12 31 CA991209058 1 19991123 A 2750 100384040 MOTOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA TE FLAP OVERHEATED W O OTHER B F SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED NR NOT REPORTED 1 CA 72 2295 PCE50438 (CAN) THE AIRCRAFT WAS PARKED AND THE ENGINES SHUT DOWN, WHEN, WITH THE BATTERY STILL ON, THE CABIN FILLED WITH SMOKE. I NVESTIGATION REVEALED THE FLAP MOTOR HAD OVERHEATED, SEIZED AND BEGAN TO SMOKE. THE CAUSE WAS THE UPLIMIT SWITCH NOT MA KING CONTACT WHEN THE FLAPS WERE RETRACTED AFTER LANDING. THIS KEPT POWER ON THE MOTOR WHICH WAS UNABLE TO ROTATE CAUSI NG IT TO OVERHEAT AND SMOKE. THE FLAP MOTOR AND GEARBOX WERE REPLACED, THE UPLIMIT SWITCH ADJUSTED, FLAPS RIGGED, THE A IRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 1999123100036 19991231 00036 CE 1999 12 31 CA991209059 1 19991129 A 3297 WIRE 1003810061 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA INDICATOR BROKEN W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA PCE50411 (CAN) AIRCRAFT WAS ON APPROACH WHEN AFTER SELECTING GEAR DOWN , THE LEFT MAIN GEAR DOWN AND LOCKED INDICATION LIGHT FAIL ED TO ILLUMINATE. THE GEAR WAS CYCLED SEVERAL TIMES, BUT DID NOT HELP. THE GEAR INTRANSIT LIGHTS WERE EXTINGUISHED AFT ER THE COMPLETION OF EACH ATTEMPT. A MANUAL GEAR EXTENSION WAS CARRIED OUT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. I NVESTIGATION REVEALED A BROKEN WIRE AT THE DOWN LIMIT SWITCH. DURING TROUBLESHOOTING, THE BROKEN WIRE WAS MOMENTARILY C ONNECTED TO THE SWITCH AND THE GEAR DOWN AND LOCKED INDICATION LIGHT ILLUMINATED. THE SWITCH WAS REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 1999123100038 19991231 00038 CE 1999 12 31 CA991209066 1 19991104 A 2750 MS264755 CIRCUIT BREAKER BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL COCKPIT FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA PCE41562 BU16552 (CAN) AFTER TAKEOFF, FLAPS WOULD NOT RETRACT FROM THE TAKEOFF POSITION TO THE FULL UP. AIRCRAFT RETURNED TO BASE AND TH E FLAP SYSTEM WAS INSPECTED. CIRCUIT BREAKER WAS RESET AND THE SYSTEM OPERATED PER MANUFACTURE'S PARAMETERS. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 1999123100039 20010307 00039 CE 2001 3 7 CA991209069 1 19991110 A 3213 50810318605 STRUT BEECH 115810000651 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5383 AMA1135 PCE41920 EAA1123M1 (CAN) AFTER REMOVAL FROM AIRCRAFT FOR TIMEX ON A TIME TRIAL, IT WAS INSPECTED AND THE FOLLOWING FOUND:LPI INDICATIONS OF CRACKS ON THE TORQUE KNEE LUG. THE CRACKS WERE IN THE RADIUS OF THE LUG ON THE BOTTOM SIDE. PART WAS REJECTED. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 1999123100040 19991231 00040 CE 1999 12 31 CA991209086 1 19990828 A 2160 12938000113 VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE RT ENGINE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 4207 PCE114131 HJ448 (CAN) AS THE CREW WAS ON TAKEOFF ROLL DOWN THE RUNWAY AND THE POWER LEVERS WERE ADVANCED TO FULL POWER, THEY RECEIVED A RT ENVIRONMENTAL FAIL INDICATION LIGHT. THEY REJECTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE WAS ADVISED AND UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT THE PRE-COOLER BYPASS VALVE HAD FAILED WHICH GENERATED THE LIGHT. THE VALVE WAS REPLACED AND THE AIRCRAFT GROUND RUN WITH THE SYSTEM TESTING SERVICEABLE. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1999123100041 19991231 00041 CE 1999 12 31 99ZZZX4631 1 19990722 A 3260 1008200191 SWITCH BEECH 1900 1900C 1154161 CE NLG OUT OF ADJUST A YADA O OTHER N FALSE WARNING AP APPROACH 1 AL 01 5632C UC81 NOSE GEAR DOWN AND LOCKED LIGHTS FAILED TO ILLUMINATE WITH LANDING GEAR SELECTED DOWN FOR LANDING AT NOME, ALASKA. AN U NEVENTFUL LANDING WAS PERFORMED AT NOME. THE PILOT VISUALLY INSPECTED THE GEAR AFTER LANDING AND AFTER WIGGLING THE NOS E GEAR DOWN AND LOCKED SWITCH, GOT DOWN AND LOCKED INDICATION. AIRCRAFT RETURNED TO ANCHORAGE AND MAINTENANCE ADJUSTED THE DOWNLOCK SWITCH. SYSTEM OPERATION CHECKED GOOD. 2 L 7 2 4T RT A24CE 1999123100052 19991231 00052 EU 1999 12 31 99ZZZX4642 1 19991122 A 7931 350A67402301AA CONNECTOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE OIL PRESSURE CONTAMINATED A A HCMA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 13 532BH 2494 4004 ON 11-22-99 AT APPROX 09:45 A.M., THE AIRCRAFT ENGINE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. THE PILOT MADE A PREC AUTIONARY LANDING AT THE ROYAL GARDENS ON THE ISLAND OF HAWAII. A MECHANIC WAS FLOWN TO THE SITE AND INSPECTED THE AIRC RAFT. A GROUND RUN-UP SHOWED THE ENGINE OIL PRESSURE AND OIL TEMPERATURE GAUGES WERE IN THE NORMAL OPERATING RANGE. TH E LOW PRESSURE LIGHT WAS NOT ILLUMINATED AT THIS TIME. FURTHER INVESTIGATION FOUND MOISTURE IN THE CANNON PLUG. THE PLU G AND SENDING UNIT WERE CLEANED WITH NO FURTHER INCIDENT. 1 G 7 1 3U 3 U NC H9EU E19EU 1999123100064 19991231 00064 1999 12 31 99ZZZX4654 4 19991103 A 3454 AK950KLN90B ANNUNCIATOR AMERIKING BEECH 1900 1900C 1154161 CE GPS FAILED A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 01 45GL 1035 91031 UC45 FAILURE OF NON-FIELD REPLACEABLE IFR GPS 'LEG' ANNUNCIATION. THIS COMPONENT IS THE INDICATOR/SWITCHING UNIT OF A CERTIF IED IFR GPS NAVIGATION SYSTEM. 2 L 7 2 4T RT A24CE 1999123100073 19991231 00073 EU 1999 12 31 99ZZZX4663 1 19991027 A 6330 L633M2001105 MOUNT UROCOP EC135 EC135P1 8680990 EU TRANSMISSION WEAK A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 382 973935 0054 MOUNT WEAK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999123100075 19991231 00075 NE 1999 12 31 99ZZZX4665 2 19991205 A 7230 BEARING BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE ENGINE FAILED A GDMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 28JH 30006 LE07631 DURING OPERATION, PILOT EXPERIENCED AN ENGINE CHIP. OIL SYSTEM PRELIMINARY INVESTIGATION SUGGESTED NR 2 BEARING FAILURE 1 G 7 1 4U 4 U H1SW E17EA 1999123100076 19991231 00076 1999 12 31 AT9900895 4 19991221 A 3432 GLIDE SLOPE DOUG DC9 DC932 3022066 WP NR 2 INOPERATIVE A ZZDA O OTHER O OTHER CL CLIMB 1 SO 15 866AT 47168 DURING CLIMB-OUT, NR 2 NAV BECAME INOPERATIVE AND ALL FLOURESCENT LIGHTS FLICKERED. RESEATED NR 2 NAV CONTROL PANEL IAW DC9 MM 34-32 AND TESTED LIGHTING IAW DC9 MM 33-10. 2 L 7 2 4F A6WE 1999123100077 19991231 00077 1999 12 31 AT9900910 4 19991216 A 2210 65C370539 PCU BOEING 737 7372L9 1384497 NM AFCS MALFUNCTIONED A ZZDA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 15 465AT 21528 DURING CRUISE, EXPERIENCED RUDDER HARDOVER. AIRPLANE ROLLED LEFT THEN RIGHT APPROX 30 DEGREE BANK WITH AUTOPILOT ON. R EMOVED AND REPLACED FLIGHT DATA RECORDER, COCKPIT VOICE RECORDER, YAW DAMPER COUPLER, RUDDER AUXILIARY POWER CONTROL UNI T, RUDDER MAIN POWER CONTROL UNIT, AUTOPILOT ROLL CONTROL CHANNEL AND AUTOPILOT ACCESSORY UNIT. ACCOMPLISHED CONTINUITY CHECK OF WIRING FROM RUDDER POWER CONTROL UNIT TO YAW DAMPER COUPLER AND AUTOPILOT ACCESSORY UNITS. WORK DONE IAW B737 MM 23-71, 27-41, 27-21, 22-15, 22-11 AND BOEING ENGINEERING RECOMMENDATIONS NR VAU-ORL-99-002194. 2 L 7 2 4F RT A16WE 1999123100078 19991231 00078 EU 1999 12 31 MALA976667 1 19991217 A 3230 L387105A SWIVEL SAAB SF340 SF340A 7850100 EU MLG BROKEN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 31XJ 031 AFTER TAKEOFF, ON GEAR RETRACTION, HYDRAULIC CAUTION LIGHT ILLUMINATED, COMPLETED MEMORY ITEMS, HYD MAIN PRESSURE LOW AN D QUANTITY LOW. EMERGENCY ACCUMULATOR PRESURE NORMAL. COMPLETED QRH SELECTED GEAR DOWN, LEFT MAIN GEAR WAS NOT DOWN AN D LOCKED, PULLED EMERGENCY GEAR EXTENSION HANDLE, ALL THREE GEARS WERE THEN INDICATING DOWN AND LOCKED. MAINTENANCE REP LACED BROKEN SWIVEL AND SERVICE HYD. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999123100079 19991231 00079 EU 1999 12 31 MALA976668 1 19991220 A 5610 7256100501 WINDSHIELD SAAB SF340 SF340A 7850100 EU COCKPIT CRACKED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 115XJ 340A115 LEFT FRONT WINDSHIELD CRACKED ON CLIMB-OUT. MAINTENANCE REPLACED LEFT WINDSHIELD IAW SF AMM 56-10-05. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999123100080 19991231 00080 EU 1999 12 31 MALA976669 1 19991220 A 2612 CONNECTOR SAAB SF340 340B 7860101 EU RT ENGINE CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 422XJ 422 SHORTLY AFTER ROTATION, THE RIGHT TAIL PIPE HOT LIGHT CAME ON, FOLLOWED QRH. MAINTENANCE INSPECTED TAIL PIPE FOUND NO D EFECTS AT THIS TIME, CLEANED CANNON PLUGS AND GROUND RAN ENGINE FOR 30 MINUTES, HAD NO PROBLEMS WITH TAIL PIPE HOT. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999123100081 19991231 00081 NM 1999 12 31 AWXA9900492 1 19991223 A 3397 13131122 WIRE BOEING 737 7372E3 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 EMERGENCY LIGHTS STAY ON INFLIGHT. RESPLICED WIRE AT SEAT 13A, OPS CK GOOD. A/C HAS 4 SDR'S GENERATED FOR EMERGENCY L IGHTING, NONE RELATED. 2 L 7 2 4F RT A16WE 1999123100082 19991231 00082 1999 12 31 AWXA9900493 4 19991223 A 3417 HG1150AC05 ADC AIRBUS 320 A320231 3930325 EU E/E BAY MALFUNCTIONED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 625AW 30332 725 064 ON TAKEOFF ROLL AT APPROX 80 KNOTS, RECEIVED SPD LIM WARNING ON ECAM. TAKEOFF REJECTED. REPLACED NR 2 AIR DATA (IRU) T T 0096655. CURRENT HISTORY: NR 2 IRU WAS REPLACED 10/11/99 FOR SIMILAR PROBLEM BOTH TIMES IT WAS ASSOCIATED WITH TAT P ROBE HEAT ON. 2 L 7 2 4F RT A28NM 1999123100083 19991231 00083 NE 1999 12 31 CALA9901676 2 19991219 A 7200 ENGINE BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 1 FAILED A CALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SW 09 16301 23352 857914 THE NR 1 ENGINE AUTO SHUTDOWN WITH NO ABNORMAL INDICATIONS WHILE ON APPROACH TO ATL. AN ENGINE RESTART WAS ATTEMPTED. U PON ENGINE SPOOL UP THE OIL PRESSURE AND QUANTITY BEGAN TO DECREASE. THE RESTART WAS ABORTED AND THE ENGINE WAS SECURED . THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE ACCESSORY GEARBOX HAD FAILED WITH RES ULTANT DAMAGE TO THE O/B FAN COWL. THE NR 1 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION REVEALED AN ANTI-ROTATION P IN ON THE CORE ANTI-ROTATION TOOLING SHEARED OFF AND FELL INTO GEARBOX AT LAST SHOP VISIT. 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100084 19991231 00084 NM 1999 12 31 CALA9901677 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1193 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT FS 1193, RBL 20. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100085 19991231 00085 NM 1999 12 31 CALA9901678 1 19991221 A 5320 WEB BOEING 727 727232 1384082 NM BS 770 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND WEB CORRODED AT WING CENTER SECTION, FS 770 LOWER TORQUE BOX AT KEEL AREA. THE CORRODED SECTION OF WEB WAS CUT OUT AND A NEW WEB SECTION WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100086 19991231 00086 NM 1999 12 31 CALA9901679 1 19991221 A 5532 PANEL BOEING 727 727232 1384082 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND VERTICAL STABILIZER RT ACCESS PANEL NR 5216 AND STIFFENER CORRODED. A NEW PANEL AND NUT PLATES WERE IN STALLED IAW SRM 51-20-1, FIGURE 7, 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100087 19991231 00087 NM 1999 12 31 CALA9901680 1 19991221 A 5280 SKIN BOEING 727 727232 1384082 NM MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN LEFT MLG O/B DOOR SKIN INNER SURFACE. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1999123100088 19991231 00088 NM 1999 12 31 CALA9901681 1 19991221 A 5753 SKIN BOEING 727 727232 1384082 NM TE FLAP WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND THE RT I/B FOREFLAP UPPER SKIN WORN THROUGH. THE FOREFLAP WAS REPAIRED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1999123100089 19991231 00089 NM 1999 12 31 CALA9901682 1 19991221 A 3350 900542 POWER SUPPLY IDDAEROSPACE BOEING 727 727232 1384082 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND THE RT AND LT SERVICE DOOR EMERGENCY SLIDE LIGHTS INOPERATIVE. THE POWER SUPPLY HAD FAILED AND A SHORT ED WIRE WAS FOUND. THE POWER SUPPLY WAS REPLACED AND THE WIRE WAS REPAIRED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50- 00, PAGE 401. 2 L 7 3 4F A3WE 1999123100090 19991231 00090 NM 1999 12 31 CALA9901683 1 19991221 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND THE LT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. A BROKEN WIRE AT CONNECTOR ON POWER SUPPLY WAS RE PAIRED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-22, PAGE 401. 2 L 7 3 4F A3WE 1999123100091 19991231 00091 NM 1999 12 31 CALA9901684 1 19991221 A 3350 20131 BATTERY PACK BOEING 727 727232 1384082 NM ROW 23 - 30 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND EMERGENCY LIGHTS FROM ROW 23-30 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-50-01 , PAGE 501. 2 L 7 3 4F A3WE 1999123100092 19991231 00092 NM 1999 12 31 CALA9901685 1 19991221 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND EMERGENCY EXIT SIGNS AT L2 AND R2 DOORS INOPERATIVE. THE BATTERY WAS REMOVED AND REPLACED IAW MM 33-50 -22. 2 L 7 3 4F A3WE 1999123100093 19991231 00093 NM 1999 12 31 CALA9901686 1 19991221 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 700 - 750 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND STRINGER 26R CORRODED FROM STA 700-750. A REPAIR WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100094 19991231 00094 NM 1999 12 31 CALA9901687 1 19991221 A 5230 69455552 FITTING BOEING 727 727232 1384082 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND C1 CARGO DOOR LOWER FORWARD SILL FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30- 2. 2 L 7 3 4F A3WE 1999123100095 19991231 00095 NM 1999 12 31 CALA9901688 1 19991221 A 5311 FRAME BOEING 727 727232 1384082 NM BS 560 BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FRAME UPPER FLANGE BENT AT STA 560, LONGERON 25L. THE BENT AREA WAS REMOVED AND AN ANGLE WAS INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1999123100096 19991231 00096 NM 1999 12 31 CALA9901689 1 19991221 A 5755 65192227 FITTING BOEING 727 727232 1384082 NM SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND NR 6 SPOILER CENTER HINGE POINT LEFT AND RIGHT FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLAC ED IAW SRM 51-30-2 AND 51-20-3, PAGE 5. 2 L 7 3 4F A3WE 1999123100097 19991231 00097 NM 1999 12 31 CALA9901690 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1148 - 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND TRANSITION PANEL ATTACH ANGLE AT STA 1148-1166 IN AFT PIT. THE ATTACH ANGLE WAS REMOVED AND REPLACED I AW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100098 19991231 00098 NM 1999 12 31 CALA9901691 1 19991221 A 5330 PANEL BOEING 727 727232 1384082 NM BS 1110 - 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LEFT TRANSITION PANEL CORRODED AT FS 1110-1166 IN AFT PIT. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100099 19991231 00099 NM 1999 12 31 CALA9901692 1 19991221 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 950B - 1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT O/B SEAT TRACKS CORRODED AT STA 990-1030 AND 950B-970. THE SEAT TRACK SECTIONS WERE REMOVED AND REP LACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100100 19991231 00100 NM 1999 12 31 CALA9901693 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN FLOOR SUPPORT AT FS 760, RBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-2, AND 51-20-0. 2 L 7 3 4F A3WE 1999123100101 19991231 00101 NM 1999 12 31 CALA9901694 1 19991221 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1030 - 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT O/B SEAT TRACK CORRODED FROM STA 1030-1070. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 . 2 L 7 3 4F A3WE 1999123100102 19991231 00102 NM 1999 12 31 CALA9901695 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 303 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH IN COCKPIT FLOOR SUPPORT ANGLE AT FS 303, LBL 5. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 5 1-30-2 AND 51-20-1. 2 L 7 3 4F A3WE 1999123100103 19991231 00103 NM 1999 12 31 CALA9901696 1 19991221 A 5330 PANEL BOEING 727 727232 1384082 NM BS 480 - 1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT TRANSITION PANELS AT FS 480-560 AND FS 1070-1090 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-1, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100104 19991231 00104 NM 1999 12 31 CALA9901697 1 19991221 A 5330 PANEL BOEING 727 727232 1384082 NM BS 950E CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 950E. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE PANEL WAS RE MOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-6, AND 51-40-3. 2 L 7 3 4F A3WE 1999123100105 19991231 00105 NM 1999 12 31 CALA9901698 1 19991221 A 5330 PANEL BOEING 727 727232 1384082 NM BS 540 - 670 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LT TRANSITION PANEL AT FS 540-670 CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100106 19991231 00106 NM 1999 12 31 CALA9901699 1 19991221 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND STRINGER 28L CORRODED AT STA 480. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-10-2, 51-30-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100107 19991231 00107 NM 1999 12 31 CALA9901700 1 19991221 A 5320 WEB BOEING 727 727232 1384082 NM BS 1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND AFT CARGO C-3 DOOR CUTOUT FORWARD WEB LOWER SURFACE CORRODED AROUND NUT PLATES FROM STRINGER 27R TO 19R AT FS 1090. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-10-1, 51-20-1, AND 51-30-2. 2 L 7 3 4F A3WE 1999123100108 19991231 00108 NM 1999 12 31 CALA9901701 1 19991221 A 5754 WEB BOEING 727 727232 1384082 NM TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN LEFT WING SLAT NR 1 O/B TRACK TO SLAT WEB. THE SLAT AND TRACK WERE REMOVED IAW MM 27 -81-11. A NEW WEB, TRACK FITTING, AND LOWER SKIN WERE INSTALLED IAW SRM 51-30-2. THE SLAT AND TRACK WERE INSTALLED IAW MM 27-81-11. 2 L 7 3 4F A3WE 1999123100109 19991231 00109 NM 1999 12 31 CALA9901702 1 19991221 A 5311 FRAME BOEING 727 727232 1384082 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 540, S27R. THE CRACKED SECTION OF FRAME WAS REMOVED AND A REPAIR DOUB LER, FRAME, AND ANGLE WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 1999123100110 19991231 00110 NM 1999 12 31 CALA9901703 1 19991221 A 5755 BEAM BOEING 727 727232 1384082 NM SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN BEAM BEHIND WEB AFTER REMOVAL OF NR 8 SPOILER FITTING. THE CRACK WAS STOP DRILLED IA W SRM 51-10-1, PAGE 6A. A REPAIR WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100111 19991231 00111 NM 1999 12 31 CALA9901704 1 19991221 A 5751 SKIN BOEING 727 727232 1384082 NM AILERON GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LEFT O/B AILERON LOWER EDGE GOUGED. THE GOUGED AREA WAS REPAIRED IAW SRM 57-50-5, FIGURE 2 AND 51-20-0 . 2 L 7 3 4F A3WE 1999123100112 19991231 00112 NM 1999 12 31 CALA9901705 1 19991221 A 5311 FRAME BOEING 727 727232 1384082 NM BS 930 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .75 INCH CRACK IN LT FRAME AT FS 930 BELOW WINDOW. REPAIRED IAW ECRA 5310-01397. 2 L 7 3 4F A3WE 1999123100113 19991231 00113 NM 1999 12 31 CALA9901706 1 19991221 A 5350 SKIN BOEING 727 727232 1384082 NM FAIRING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LEFT LOWER BODY FAIRING 3341 SKIN AND NR 7 SUPPORT CORRODED. THE SKIN WAS REMOVED AND NEW SKIN, DOUBLE R, AND STRAPS WERE INSTALLED IAW SRM 53-30-3 AND 51-20-4. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100114 19991231 00114 WP 1999 12 31 CALA9901707 1 19991222 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG DISCHARGED A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 14880 48044 THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. THE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR WAS CYCLED AND R ETRACTION WAS SUCCESSFUL WITH ALL GEAR INDICATION LIGHTS GREEN. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. A NO SE STRUT FULL SERVICE WAS PERFORMED IAW MM 32-21-02, PAGE 301-304A. A NOSE GEAR EXTENSION AND RETRACTION CHECK WAS PERF ORMED IAW MM 32-30-00, PAGE 201-206 AND NOSE GEAR OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1999123100115 19991231 00115 NM 1999 12 31 CALA9901708 1 19991221 A 5350 SKIN BOEING 727 727232 1384082 NM FAIRING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT BODY FAIRING 3441 INNER SKIN AND SUPPORT NR 22 CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. THE SUPPORT WAS REMOVED AND A DOUBLER AND BRA CKET WERE INSTALLED IAW SRM 51-10-6, 51-30-2, AND 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 1999123100116 19991231 00116 NM 1999 12 31 CALA9901709 1 19991221 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 380 - 1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND SEAT TRACK SECTIONS CORRODED AT STA 380-420, RBL 40 AND STA 990-1030, RBL 48. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100117 19991231 00117 NM 1999 12 31 CALA9901710 1 19991221 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 277 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBEAM CORRODED AT FS 277, RBL 12. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS I NSTALLED USING SUPPORT ANGLES AND STIFFENERS IAW SRM 51-30-2 AND 51-40-4, FIGURE 1. 2 L 7 3 4F A3WE 1999123100118 19991231 00118 NM 1999 12 31 CALA9901711 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 623 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN NUT PLATE STRIP ANGLE AT STA 623, LONGERON 23R. THE ANGLE WAS REMOVED AND A NEW ANGL E WAS INSTALLED IAW SRM 51-30-2 AND 53-10-2. 2 L 7 3 4F A3WE 1999123100119 19991231 00119 NM 1999 12 31 CALA9901712 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 216 - 219 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND TWO ATTACH ANGLES CORRODED FROM FS 216-219, RBL 15, L27R. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100120 19991231 00120 NM 1999 12 31 CALA9901713 1 19991221 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 380 - 420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND R-1 DOOR THRESHOLD ATTACH ANGLES CORRODED AT STA 380-420. THE CORROSION WAS REMOVED IAW SRM 51-10-6. T HE ATTACH ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-10-2, 51-20-1, 51-40-3, FIGURE 1, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100121 19991231 00121 NM 1999 12 31 CALA9901714 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 400 - 420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 420, RBL 20-40 AND AT STA 400-420, RBL 10. THE FLOOR SUPPORTS WERE REMO VED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100122 19991231 00122 NM 1999 12 31 CALA9901715 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN FLOOR SUPPORT AT FS 760, RBL 3. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100123 19991231 00123 NM 1999 12 31 CALA9901716 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 660 - 800 BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AND BENT AT FS 660-800, BL 0. THE CORROSION WAS REMOVED IAW SRM 53-10-1. THE B ENT SECTION OF FLOOR SUPPORT WAS REMOVED AND REPLACED USING SPLICES IAW SRM 51-40-2 AND 51-30-1. 2 L 7 3 4F A3WE 1999123100124 19991231 00124 NM 1999 12 31 CALA9901717 1 19991221 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 950D - 990 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 950D-990, BL 0. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A REPAIR WAS INSTALLED IAW SRM 51-10-4, FIGURE 3. 2 L 7 3 4F A3WE 1999123100125 19991231 00125 WP 1999 12 31 CALA9901718 1 19991221 A 2560 P2070003001 FLASHLIGHT DME DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND TWO EACH EMERGENCY PORTABLE FLASHLIGHTS INOPERATIVE. THE FLASHLIGHTS WERE REPLACED AND TESTED IAW MM 2 5-60-00. 2 L 7 3 4F A22WE 1999123100126 19991231 00126 NE 1999 12 31 9905389875 2 19991219 A 7200 JT8D17 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LEFT FAILED A NWAA C ABORTED TAKEOFF E X J VIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 GL 01 784NC 50097 1672 48109 696690 DURING TAKEOFF, THE LEFT ENGINE FAILED AT ABOUT 100 KNOTS AIRSPEED WITH AN ASSOCIATED EPR INDICATION OF 1.0, A DECREASE OF N1 AND N2 RPM SPEED, AND A NOTICEABLE ENGINE VIBRATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND THE FLIGHT RETURNED TO BLOCKS. MAINTENANCE REPLACED THE LEFT ENGINE. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1999123100127 19991231 00127 WP 1999 12 31 9905399951 1 19991220 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9347 45827 DURING PERIODIC CHECK, FOUND FORWARD CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999123100128 19991231 00128 WP 1999 12 31 9905409963 1 19991219 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999123100129 19991231 00129 NM 1999 12 31 UPS99631232 1 19991221 A 3230 GEAR LEVER BOEING 767 76734AF 1385212 NM COCKPIT MALFUNCTIONED A IPXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 315UP 27743 GEAR LEVER WOULD NOT MOVE TO UP POS INFLT WAS FREE TO MOVE TO UP POS WHEN LOCK OVRH PUSHER. FLIGHT RETURNED TO SDF PER AMC. AIR TURN BACK, FOUND LEVER LOCK CIRCUIT BREAKER NOT COMPLETELY IN. RESET BREAKER AND OPS CHECKED LANDING GEAR CON TROL PER MM 32-31-00. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 1999123100130 19991231 00130 1999 12 31 UPS99831230 4 19991223 A 2565 SLIDE DOUG DC8 DC873F 302199F WP CABIN LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 LOAD SUPERVISOR OPENED MAIN ENTERANCE DOOR AND SLIDE FELL OUT. REINSTALLED EVAC SLIDE IAW MM 25-60-01 PG 202-204. 2 L 7 4 4F RT 4A25 1999123100131 19991231 00131 WP 1999 12 31 UPS99831231 1 19991221 A 3350 LIGHT DOUG DC8 DC871F 302199D WP COCKPIT INTERMITTENT A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 EMERGENCY EXIT LIGHT DOES NOT REMAIN ILLUMINATED AFTER DISARM CHECK ON SHUTDOWN CHECKLIST. CYCLED EMERGENCY LIGHT SWITC H. LIGHT OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1999123100132 19991231 00132 NM 1999 12 31 99FDEA00505 1 19991221 A 7603 THROTTLE DOUG MD11 MD11F 3023600 NM COCKPIT FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 601FE 48401 99-288 - ON T/O FROM LFPG, MISC DISPLAY IND NO AUTOLAND AND AUTOPILOT 1 AND 2 WOULD NOT ENGAGE. GOT AILERON DISAGREE AL ERT. PERF FCC NR 1 AND 2 RTS PER MM 22-00-00-5, (TASK 22-00-00-701-801). ALL RTS PASSED DUE TO PREVIOUS HISTORY. CAT 2 PRECAUTIONARY AND DEFERRED AILERON IND INOP. 2 L 7 3 4F RT A22WE 1999123100133 19991231 00133 NM 1999 12 31 99FDEA00506 1 19991222 A 2612 FIRE DETECTOR BOEING 727 7272S2F 1384O81 NM NR 2 ENGINE MALFUNCTIONED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 203FE 22925 99-289 - FIRE WARNING BELL RANG 1 TIME AND BOTH FIRE LIGHTS ON GLARE SHIELD ILLUMINATED MOMENTARY AS PWR WAS APPLIED. D ID NOT SEE OR HEAR ANY OTHER ABNORMAL IND (ONE DING ONLY). REMOVED AND REPLACED FIRE DETECTION ASSY UNIT RAN NR 2 ENG A S WAS STILL ABLE TO DUPLICATE PROBLEM AT OR AROUND 70 PERCENT N2 TRIED TO ISOLATE TO EITHER SYS A AND B FOUND SYSTEM. 2 L 7 3 4F A3WE 1999123100134 19991231 00134 NM 1999 12 31 99FDEA00507 1 19991222 A 2130 CONTROLLER BOEING 727 727233 138408A NM CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 258FE 20940 CLIMB THRU FLT LEVEL 180 CABIN PRESS START TO DECREASE AT 1200 RPM (4.8 PSID & DECREASING). PERFORMED CABIN PRES CKLIST , NO HELP. *S/D* ACCOMPLISH EXCESS CABIN PRESS LEAKAGE CONDITION, REF B727 MM 05-51-101-2, TEST OK. NO DEFECTS NOTED AT THIS TIME, A/C OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1999123100135 19991231 00135 NM 1999 12 31 99FDEA00508 1 19991222 A 7930 INDICATOR BOEING 727 72725 1384006 NM NR 3 ENGINE MALFUNCTIONED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 508FE 18279 99-291 - OIL PRESS ON NR 3 ENG DROP BELOW 30 PSI. MAIN OIL FILTER WAS REMOVED AND CK PER 727 MM 79-00-000-2. FOUND CLE AN, REINSTALL. NO LEAKS NOTED. COULD NOT DUPLICATE ON GRD. OK FOR SERVICE. 2 L 7 3 4F A3WE 1999123100136 19991231 00136 EU 1999 12 31 99FDEA00509 1 19991222 A 2910 WARNING SYSTEM AIRBUS 310 A310203 EU HYDRAULIC SYS ACTIVATED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 408FE 257 99-292 - ON T/O YELLOW SYSTEM LOW PRESS ECAM WARNING. REJECTED TO AT 83 KTS. YELLOW SYS RECOVERED TO NORM CLEAR RUNWAY . 2 L 7 2 4F RT A35EU 1999123100137 19991231 00137 EU 1999 12 31 99FDEA00510 1 19991222 A 3030 E0065Z01W01B RELAY AIRBUS 310 A310203 EU PITOT HEAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 412FE 360 99-293 - ON DEPT GDL, F/O PITOT HEAT FAILED, THEN NR 1 ATS TRIPPED. WOULD NOT RESET. REMOVED AND REPLACED NOSE GEAR RE LAY 153GB IAW MM. ALL CK GOOD, OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1999123100138 20001016 00138 NM 2000 10 16 99UAL900641 1 19991210 A 3350 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHTS STAY ON WITH COCKPIT SWITCH OFF. AUTOMATIC FUNCTION WORKS NORMALLY WITH SWITCH ARMED. *S/D* REPLACED 1 RT DOOR EMERGENCY LIGHT SWITCH AND SWITCH GARD (CH7724). BOEING IS IN THE PROCESS OF DETERMINING A SOLUTION TO THE F AULTY CARD SWITCH. A RESPONSE IS EXPECTED FROM BOEING IN THE NEAR FUTURE. REF TELEX UAL-OAK 99-00798H. 2 L 7 4 4F 4 F RT A20WE E24NE 1999123100139 20001016 00139 NM 2000 10 16 99UAL900642 1 19991210 A 3110 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 656UA 25394 OVERHEAD INDICATION PANEL: ENTRY, EMER DOORS, CARGO DOORS, AND ACCESS DOORS ILLUMINATE WITH ASSOCIATED DOORS CLOSED. N O EICAS MESSAGES. STARTING LEFT ENG EXTINGUISHES INDICATOR LIGHTS. UPON ENG SHUT DOWN, ALL ABNORMALITIES RESUME. *S/D * TEST OF THE OVERHEAD INDICATION PANEL FOUND A FAULT IN THE F/O PITOT ANN CAPSULE. REPLACED F/O PITOT ANN CAPSULE. D EFECT HAS NOT BEEN NOTED SINCE REPLACEMENT WAS MADE. 2 L 7 2 4F 4 F RT A1NM E24NE 1999123100140 20001016 00140 2000 10 16 99UAL900643 4 19991212 A 2565 SLIDE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE PAX DOOR DEPLOYED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 7293U 21571 DOOR NR 2 RIGHT HAND SLIDE PACKAGE DEPLOYMENT CABLE SEVERED. *S/D* LATCH CABLE WAS FOUND FRAYED, NOT SEVERED. REPLACE D SLIDE ASSY PER MAINTENANCE MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 1999123100141 20001016 00141 NE 2000 10 16 99UAL900644 2 19991210 A 7230 5A0017 CONE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE NR 2 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 4507 882 V10411 NR 2 ENG HAS INLET CONE FAIRING CRACKED AROUND BOLT HOLE. *S/D* THE CAUSE OF THE INLET CONE CRACKING IS VIBRATION OF T HE INLET CONE FAIRING AGAINST THE INLET CONE SEATING. THE MANUFACTURER ISSUED SERVICE BULLETIN V2500-ENG-72-0318 WHICH MODIFIED THE FAIRINGS WITH A SEAL TO REDUCE VIBRATION. THIS SERVICE BULLETIN WAS IN PROCESS OF INCORPORATION BY COA R-9 039-0/1. 2 L 7 2 4F 4 F RT A28NM E40NE 1999123100142 20001016 00142 NE 2000 10 16 99UAL900645 2 19991213 A 7261 LINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 GENERATOR LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 315UA 23947 THE NR 1 GENERATOR TRIPPED OFF LINE TWICE. *S/D* LEAK FOUND ON OIL RETURN LINE. REPLACED O-RING. 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100143 20001016 00143 NM 2000 10 16 99UAL900646 1 19991213 A 2611 21198356 DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CARGO BAY MALFUNCTIONED A UALA F C ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING NR NOT REPORTED 1 WP 29 771UA 2100 26932 AFTER ENGINE START, RECEIVED AFT CARGO WARNING MESSAGE. DISCHARGED AFT FIRE BOTTLES. WARNING WENT AWAY AFTER 2 - 3 MI NUTES. *S/D* INITIAL CAUSE WAS THOUGHT TO BE INADVERTENT DETECTION DUE TO FUMIGATION OR MOISTURE BECAUSE OF NO SYSTEM FAULTS PRESENT. WHEN SAME EVENT OCCURRED 7 DAYS LATER IN FRA, THE AFT CARGO SMOKE DETECTOR (P/N:2119835-6 / S/N:34-A003 5) WAS REPLACED AND SENT TO VENDOR FOR TEARDOWN. NO FURTHER EVENTS HAVE OCCURRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999123100144 20001016 00144 NM 2000 10 16 99UAL900647 1 19991214 A 5270 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PAX DOOR OUT OF ADJ A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 572UA 26682 ABORTED TAKEOFF AT 130 KNOTS DUE TO LEFT AFT ENTRY DOOR EICAS MESSAGE. *S/D* DOOR WARNING SENSOR WAS OUT OF ADJUSTMENT . ADJUSTED DOOR WARNING SENSOR. DEFECT HAS NOT BEEN NOTED SINCE ADJUSTMENT WAS MADE. 2 L 7 2 4F 4 F RT A2NM E17NE 1999123100145 19991231 00145 WP 1999 12 31 99UAL900648 1 19991214 A 2120 ODOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DETECTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1845U 48261 OIL SMELL IN CABIN, DEBRIEF CREW ON ARRIVAL. HAD UNCOMFORTABLE SMELL THROUGHOUT AIRCRAFT FOR 15-20 AFTER T/O, LIKE A BU RNED OIL SMELL POSSIBLY IN NR 2 PNEU SYSTEM. ALL TEMPS, NORMAL. NO SMELL ON APU. 2 L 7 3 4F 4 F A22WE E23EA 1999123100146 19991231 00146 NM 1999 12 31 99UAL900649 1 19991214 A 5270 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CARGO DOOR ACTIVATED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 665UA 29237 FWD CARGO DOOR CAUTION MESSAGE ON EICAS CLIMBING OUT AFTER T/O FROM OGG, ABOUT 11K. FOLLOWED PROC, DIVERTED TO HNL. OV ERWEIGHT LANDING. LANDING WEIGHT 316.0. 2 L 7 2 4F 4 F RT A1NM E24NE 1999123100148 19991231 00148 NM 1999 12 31 99UAL900651 1 19991214 A 5710 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING DAMAGED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 344UA 24248 WHILE TAXIING THE AIRCRAFT FOR MAINTENANCE, THE LEFT-HAND WING HIT A BLAST FENCE, SHEARING OFF THE WING TIP ASSEMBLY AND DAMAGING THE FRONT SPAR LOWER CHORD, LOWER WING SKIN AND THE OUTBOARD FIXED LEADING EDGE SKIN. *S/D* REPLACED THE WIN G TIP ASSEMBLY AND FIXED LEADING EDGE. REPAIRED THE FRONT SPAR LOWER CHORD AND THE WING SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100149 19991231 00149 WP 1999 12 31 ABXA9900855 1 19991220 A 3260 INDICATOR DOUG DC8 DC862 3021970 WP MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 805AX 45906 DURING CLIMB, RED GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. DURING UPLATCH CHECK, THE LEFT GEAR DOOR LIGHT ILLUMINATE D WHEN SELECTED. AFTER GEAR RECYCLE, BOTH LIGHTS EXTINGUISHED. CHECKED MAIN GEAR DOOR SWITCHES IAW DC8MM. NO DEFECTS NOTED. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999123100150 19991231 00150 WP 1999 12 31 ABXA9900856 1 19991214 A 3350 5708458503 POWER PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 820AX 46155 EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN ELECTRICAL POWER WAS LOST. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 MM 33-5 0-00. 2 L 7 4 4F 4A25 1999123100151 19991231 00151 WP 1999 12 31 ABXA9900857 1 19991221 A 2510 5925379517ABX1 SEAT DOUG DC9 DC931 3022065 WP COCKPIT WORN A ABXA O OTHER O OTHER NR NOT REPORTED 1 GL 23 947AX 3476 47004 CAPTAIN'S SEAT VERTICAL MOVEMENT ADJUSTMENT RELEASES INADVERTENTLY. SEAT SLIDES TO FLOOR WITHOUT ACTUATION. REPLACED C APTAIN'S SEAT. 2 L 7 2 4F A6WE 1999123100152 19991231 00152 1999 12 31 MWEA99910 4 19991219 A 2565 113317 SLIDE DOUG DC9 DC982 3022082 WP CABIN LOOSE A MWEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 806ME 48032 FORWARD PASSENGER DOOR ESCAPE SLIDE PULLED FROM COVER. MTC REPACKED FORWARD DOOR SLIDE. 2 L 7 2 4F A6WE 1999123100153 19991231 00153 WP 1999 12 31 MWEA99911 1 19991222 A 2120 5930859 DUCT DOUG DC9 DC981 3022081 WP LT PACK DAMAGED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 806ME 48032 CREW WAS UNABLE TO MAINTAIN CABIN PRESSURE AT 3,4000 FT, CREW THAN INITIATED DECENT AND WERE THEN ABLE TO STABLIZE CABIN PRESSURE AT 18,000 FT. MAINTENANCE REINSTALLED FLEX DUCTS ON LEFT PACK AT AIR CYCLE MACHINE AND HOT AIR DISCHARGE DUCT . 2 L 7 2 4F A6WE 1999123100154 19991231 00154 NM 1999 12 31 SCNA99154 1 19991221 A 3243 VALVE BOEING 727 7272K3 138400D NM PARKING BRAKE LEAKING A SCNA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 291SC 22770 WHILE THE AIRCRAFT WAS PARKED AT THE GATE SMOKE WAS NOTICED IN THE CABIN. MAINTENANCE FOUND THE PARKING BRAKE VALVE LEA KING. REMOVED AND REPLACED PARK BRAKE VALVE PER MM 324421. OPERATIONALLY AND LEAK CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999123100155 19991231 00155 NM 1999 12 31 VNAA9912013 1 19991222 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 442JS 9941 3060 THE FLIGHT CREW NOTICED THAT THE EMERGENCY CABIN LIGHTING WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERG ENCY BATTERY IN THE 6LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE PERFOR MED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999123100156 19991231 00156 1999 12 31 RAIA9912032 4 19991220 A 3416 B4515210004 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 432AM 14554 9 883 7470 - STL- FIRST OFFICERS ALTIMETER IS INOPERATIVE. MAINTENANCE REPLACED FIRST OFFICERS ALTIMETER. 2 L 7 2 4T RT A56EU 1999123100157 19991231 00157 EU 1999 12 31 RAIA9912033 1 19991221 A 2432 A848KH CONTACTOR BAG JETSTM JETSTM3201 1500217 EU BS 130 FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 871JX 17081 871 4723 - SFO- NR1 BATTERY CAPTION ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED NR 1 BATTERY CONTACTOR. 2 L 7 2 4T RT A56EU 1999123100158 19991231 00158 NE 1999 12 31 MALA976670 2 19991225 A 7510 WARNING SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE COCKPIT ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 76XJ 076 RIGHT AIR VALVE LIGHT ILLUMINATED. MAINTENANCE RAN AIRCRAFT TO SF340 MM AND POM ICE CHECK AND OTHER MAINTENANCE CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1999123100159 19991231 00159 EU 1999 12 31 MALA976671 1 19991223 A 7810 EXHAUST NOZZLE SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 107XJ 340A107 LEFT INTAKE LIGHT CAME ON IN FLIGHT. QRH DIDN'T CORRECT THE PROBLEM. RETRUNED TO CWA. MAINTENANCE TROUBLESHOT SYSTEM, RESECURED EXHAUST NOZZLE ENVIROMENTAL SPLICED ON LEFT ENGINE. OPS CHECK GOOD IAW SAAB 340 AMM 30-20-00. 2 L 7 2 4T RT A52EU 1999123100160 19991231 00160 1999 12 31 MALA976672 4 19991224 A 3425 AHRS SAAB SF340 340B 7860101 EU NR 1 MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 420XJ 420 DURING INITIAL CLIMB BOTH NR 1 AND NR 2 EHSI SHOWED 30 OFF FROM ATC. RED FLAG ON NR 1'S RMI CYCLED ON/OFF, THEN NR 1 EH SI HAD RED HEADING FLAG AND NR 2 RMI HAD RED FLAG CYCLED ON/OFF THEN YELLOW HEADING FLAG COMPARATOR CYCLED ON/OFF. IT E XTINGUISHED WITHOUT CREW ACTION AND DURING TURN TO FINAL BOTH NR 1 AND NR 2 EHSI AND RMI ROTATED TO CORRECT HEADING. MA INTENANCE REINITALIZED NR 1 AHRS SYSTEM. ALL CHECKS GOOD IAW SAAB MM CH 34. 2 L 7 2 4T RT A52EU 1999123100161 19991231 00161 EU 1999 12 31 MALA976673 1 19991225 A 7930 4053T7P01 PROBE SAAB SF340 340B 7860101 EU OIL TEMP FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 434XJ 434 RIGHT PGB OIL TEMP INDICATING TO THE UPPER/HOTTEST LIMIT. MAINTENANCE REPLACED OIL TEMP PROBE, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999123100162 19991231 00162 WP 1999 12 31 CALA9901719 1 19991223 A 2530 810128000B OVEN DOUG DC10 DC1030 3023501 WP GALLEY INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 13067 28176 47866 SMOKE BEGAN COMING OUT OF THE AFT GALLEY OVEN CONTROL PANEL WHILE EN ROUTE TO EWR. THE SMOKE STOPPED WHEN OVEN WAS TURN ED OFF. THE FLIGHT CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE AFT GALLEY OVEN WAS REMOVED AND REPLACED. OPERATION OF THE OVEN CHECKED GOOD. NO OTHER DEFECTS WERE FOUND. 2 L 7 3 4F A22WE 1999123100163 19991231 00163 NM 1999 12 31 CALA9901720 1 19991223 A 5320 STIFFENER BOEING 727 727232 1384082 NM PANEL 1104 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK AT EACH END OF PANEL 1104 STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100164 19991231 00164 NM 1999 12 31 CALA9901721 1 19991224 A 5330 DOUBLER BOEING 727 727232 1384082 NM BS 259 - 303 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND DOUBLER GOUGED AT FS 259-303, S24L. THE GOUGED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5330-02912 AND BOEING DRAWING 65-18420. 2 L 7 3 4F A3WE 1999123100165 19991231 00165 NM 1999 12 31 CALA9901722 1 19991226 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34315 23366 INSPECTION FOUND FLOORBEAM CORRODED AT FASTENER HOLES, STA 344, LBL 18-RBL 10. A CHORD WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1999123100166 19991231 00166 NM 1999 12 31 CALA9901723 1 19991227 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1148, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1999123100167 19991231 00167 NM 1999 12 31 CALA9901724 1 19991227 A 5752 HINGE BOEING 727 727232 1384082 NM AILERON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A .5 INCH CRACK IN CENTER HINGE BRACKET OF RT WING I/B AILERON TAB. THE HINGE WAS REMOVED AND REPLACED IAW SRM 57-50-01. 2 L 7 3 4F A3WE 1999123100168 19991231 00168 NM 1999 12 31 CALA9901725 1 19991227 A 5321 FLOOR PANEL BOEING 727 727232 1384082 NM BS 290 - 300 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND BLUE WATER STAINS AND CORROSION ON FLOOR PANEL AT STA 290-300. THE PANEL WAS REMOVED AND A NEW PANEL W AS INSTALLED IAW SRM 51-10-4, PAGE 4, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100169 19991231 00169 NM 1999 12 31 CALA9901726 1 19991227 A 5330 SKIN BOEING 727 727232 1384082 NM BS 348 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FUSELAGE SKIN GOUGED AT FS 348, S26L. THE GOUGED AREA WAS CUT OUT, REPAIR FILLER AND DOUBLER WERE INST ALLED IAW SRM 53-30-3, FIGURE 24, 51-30-2, 51-20-4. 2 L 7 3 4F A3WE 1999123100170 19991231 00170 NM 1999 12 31 CALA9901727 1 19991227 A 5280 RIB BOEING 727 727232 1384082 NM NLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF RIB AT RT FORWARD NLG DOOR FORWARD UPPER EDGE, SIX INCHES BELOW THE DOOR LA TCH. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-10, FIGURE 1, 52-10-2, 51-30-1, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100171 19991231 00171 NM 1999 12 31 CALA9901728 1 19991227 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 600 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT FS 600, LBL 12. THE CRACK WAS STOP DRILLED AND REPAIR PARTS WERE IN STALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1999123100172 19991231 00172 NM 1999 12 31 CALA9901729 1 19991227 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 312 - 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312-344, LBL 30. THE UPPER STRAP OF FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT STRAP WAS INSTALLED IAW SRM 51-30-2 AND 53-10-2. 2 L 7 3 4F A3WE 1999123100173 19991231 00173 NM 1999 12 31 CALA9901730 1 19991227 A 5313 LONGERON BOEING 727 727232 1384082 NM BS 560 - 600 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LONGERON 20L CORRODED AT FS 560-600. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-3, FIGURE 2, 51-10-2, AND 51-20-3. 2 L 7 3 4F A3WE 1999123100174 19991231 00174 NM 1999 12 31 CALA9901731 1 19991227 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1075 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND AFT CARGO FLOOR SUPPORT CORRODED AT FS 1075, RBL 12. THE CORRODED AREA WAS CUT OUT, NEW PARTS AND NUT PLATES WERE INSTALLED IAW SRM 51-40-4, 51-30-1, 51-10-2, 51-20-0, AND 51-20-4. 2 L 7 3 4F A3WE 1999123100175 19991231 00175 NM 1999 12 31 CALA9901732 1 19991227 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1130, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTAL LED IAW SRM 53-10-1, 51-10-2, 51-30-2, AND MM 51-20-2. 2 L 7 3 4F A3WE 1999123100176 19991231 00176 NM 1999 12 31 CALA9901733 1 19991227 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FRAME CORRODED ON TOP LEG IN AFT CARGO AREA AT STA 1070, S27R. THE CORRODED DOUBLER, GUSSET, AND STIFF ENER WERE REMOVED IAW SRM 51-30-2. A NEW DOUBLER, GUSSET, AND STIFFENER WERE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1999123100177 19991231 00177 NM 1999 12 31 CALA9901734 1 19991227 A 5414 SKIN BOEING 727 727232 1384082 NM NR 2 ENG COWL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN UPPER FORWARD CORNER SKIN OF LT AFT NR 2 ENGINE COWL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FILLER WERE INSTALLED IAW SRM 54-30-3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1999123100178 19991231 00178 EA 1999 12 31 COMA9960781 1 19991218 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 965CA 7131 RIGHT HAND THRUST REVERSER UNLOCK MESSAGE. DEACTIVATED AND DEFERRED THE RIGHT HAND THRUST REVERSER. 2 L 7 2 4F RT A21EA 1999123100179 19991231 00179 EA 1999 12 31 COMA9960780 1 19991219 A 3610 20035008067 CONTROLLER CNDAIR CL600 CL6002B19 EA ANTI ICE SYSTEM MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 938CA 9418 7046 REO ANTI ICE DUCT MESSAGE. REPLACED THE LEFT AND RIGHT BLEED AIR CONTROLLERS. 2 L 7 2 4F RT A21EA 1999123100180 19991231 00180 EA 1999 12 31 COMA9960779 1 19991219 A 7931 601509197 TRANSDUCER CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 940CA 348 7048 RIGHT ENGING OIL PRESURE INDICATED 130 PSI. REPLACED THE OIL PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 1999123100181 19991231 00181 EA 1999 12 31 COMA9960778 1 19991220 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 CABIN DOOR OUTER HANDLE MESSAGE AND OVERBOARD COOL MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR WARNING SYS TEM NORMAL. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1999123100182 19991231 00182 SO 1999 12 31 COMA9910196 1 19991219 A 2731 WIRE EMB 120 EMB120RT 3260202 SO TRIM SENSOR BROKEN A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 259CA 120252 TAKEOFF TRIM WARNING. REPAIRED BROKEN WIRE AT ELEVATOR TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1999123100183 19991231 00183 SO 1999 12 31 COMA9910195 1 19991221 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 8 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 249CA 120230 EXIT SIGN AT ROW 8 WAS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1999123100184 19991231 00184 NM 1999 12 31 UPS99231235 1 19991224 A 3510 O2 BOTTLE BOEING 727 72727C 138400J NM COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE:N/A, CREW O2 BOTTLE READS LOW. REMOVED AND REPLACED BOTTLE. 2 L 7 3 4F A3WE 1999123100185 19991231 00185 NM 1999 12 31 UPS99431234 1 19991227 A 2610 SWITCH BOEING 747 747123 1384873 NM CARGO BAY MALFUNCTIONED A IPXA F ACTIVATE FIRE EXT. N FALSE WARNING UK UNKNOWN 1 SO 01 673UP 20325 INSPECTION TYPE:N/A, AFT CARGO FIRE WARNING. REMOVED AND REPLACED FIRE BOTTLES AND DISCHARGE SWITCH, SYSTEM TESTS NORMA L. 2 L 7 4 4F A20WE 1999123100186 19991231 00186 WP 1999 12 31 UPS99831233 1 19991223 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:N/A, EMER EXIT LIGHTS FAILED TO DISARM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. S YSTEM OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 1999123100187 19991231 00187 1999 12 31 UPS99831236 4 19991227 A 2565 SLIDE DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A, L-1 DOOR EVAC SLIDE INOP REF M183941. 2 L 7 4 4F RT 4A25 1999123100188 19991231 00188 WP 1999 12 31 UPS99831237 1 19991227 A 5320 FITTING DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A, 9G NET ATTACH FITTINGS CORRODED BEYOND REPAIR. 2 L 7 4 4F RT 4A25 1999123100189 19991231 00189 WP 1999 12 31 ABXA9900858 1 19991221 A 3260 STRIKER DOUG DC8 DC862 3021970 WP MLG DOOR LOOSE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 805AX 45906 RED GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP AT 1700 FT. PERFORMED GEAR UPLATCH CHECK. DISCRIMINATOR PANEL NOT LATCH ED LIGHT ILLUMINATED IN LEFT LANDING GEAR DOOR POSITION. RECYCLED GEAR AND RED UNSAFE LIGHT WENT OUT. LEFT UPLATCH SWI TCH STRIKER WAS HITTING FUSELAGE FRAME. RESHIMMED ROLLER SWITCH STRIKER TO OBTAIN REQUIRED CLEARANCE. OPS CHECKED GOOD IAW DC8 MM 32-31-4. 2 L 7 4 4F 4A25 1999123100190 19991231 00190 WP 1999 12 31 ABXA9900859 1 19991223 A 3350 1864 BULB DOUG DC8 DC863 302198A WP COCKPIT FAILED A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 817AX 45928 EMERGENCY FAIL LIGHT WAS INOPERATIVE. UNABLE TO CONFIRM LIGHTS DISARMED. RELAMPED ANNUNCIATOR BULB, OPS CHECKED GOOD I AW DC8 MM 33-50. 2 L 7 4 4F 4A25 1999123100191 19991231 00191 1999 12 31 MWEA99912 4 19991225 A 2565 113317 SLIDE DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 GALLEY DOOR EVACUATION SLIDE PRESSURE LOW. MAINTENANCE REPLACED GALLEY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1999123100192 19991231 00192 WP 1999 12 31 MWEA99913 1 19991225 A 2560 GIRT BAR DOUG DC9 DC981 3022081 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FORWARD GALLEY DOOR EVACUATION SLIDE GIRT BAR NOT ATTACHED TO SLIDE ASSEMBLY. MAINTENANCE RE-ATTACHED GIRT BAR TO COVER . 2 L 7 2 4F A6WE 1999123100193 19991231 00193 WP 1999 12 31 MWEA99914 1 19991224 A 2560 4125A MEGAPHONE DOUG DC9 DC981 3022081 WP CABIN MALFUNCTIONED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 806ME 48032 FORWARD FLIGHT ATTENDANT'S MEGAPHONE WAS SCRATCHY. MAINTENANCE REPLACED MEGAPHONE WITH SERVICEABLE UNIT. 2 L 7 2 4F A6WE 1999123100194 19991231 00194 NM 1999 12 31 DHL99712002 1 19991201 A 5347 SEAT TRACK BOEING 727 72729 1384007 NM BS 540 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 CRACKED SEAT TRACK LBL 45.5 BS 540. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM 480 TO 620 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1999123100195 19991231 00195 NM 1999 12 31 DHL99712003 1 19991201 A 5315 FLOORBEAM BOEING 727 72729 1384007 NM BS 540 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 CRACKED REPAIR OF FLOORBEAM UPPER CAP BS 540 LBL 45.5. REMOVED OLD REPAIR AND INSTALLED FLOORBEAM REPAIR PER SRM 53-10- 8, 3 X 17. 2 L 7 3 4F A3WE 1999123100196 19991231 00196 NM 1999 12 31 DHL99712004 1 19991201 A 5320 SPLICE BOEING 727 72729 1384007 NM BS 660 - 680 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 712DH 19401 FWD CARGO FLOORBEAM STABILITY STRAP SPLICE AT BL 0 BS 660-680 DID NOT CONFORM TO SRM. REMOVED SECTION OF STABILITY STRA P, FOUND CRACKED SUPPORT ANGLE AT BL 0 STA 680 TO 700. REPLACED SECTION OF STABILITY STRAP 640 TO 680 PER SRM 53-10-8, 3 X 46. REPLACED SUPPORT ANGLE PER SRM 53-40-3 . 2 L 7 3 4F A3WE 1999123100197 19991231 00197 EU 1999 12 31 RAIA9912034 1 19991223 A 3060 R333482F12 PROP HEAT BAG JETSTM JETSTM3201 1500217 EU ROTOL R333 R333482F12 GL LT PROPELLER FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 424AM 11823 5755 865 DRG1065390 7027-STL- LEFT PROPELLER HEAT WAS INOPERATIVE. MAINTENANCE REPLACED LEFT PROPELLER ASSEMBLY. 2 L 7 2 4T RT A56EU 6 C P61GL 1999123100198 19991231 00198 NM 1999 12 31 SWAA992107 1 19991221 A 3350 07912 EEL COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 387SW 26602 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS AFT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 1999123100199 19991231 00199 NM 1999 12 31 SWAA992108 1 19991221 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED ON OUTBOARD LOWER CORNER. REPAIRED FLAP PER SWA R A NR 1-357-0785. 2 L 7 2 4F RT A16WE 1999123100200 19991231 00200 NM 1999 12 31 SWAA992109 1 19991221 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED ON OUTBOARD UPPER AND LOWER END. REMOVED AND REPL ACED FLAP ASSY PER MM. 2 L 7 2 4F RT A16WE 1999123100201 19991231 00201 1999 12 31 SWAA992110 4 19991221 A 2565 D31354 INDICATOR BOEING 737 7373H4 1384600 NM ESCAPE SLIDE MOVED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE A SSY PER MM. 2 L 7 2 4F RT A16WE 1999123100202 19991231 00202 NM 1999 12 31 SWAA992098 1 19991220 A 5311 6546536 FRAME BOEING 737 7372T4 1384492 NM BS 639 & BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D-CHECK, FOUND 2 FUSELAGE FRAMES CRACKED, BS 639, STRINGER 17R AND BS 303, STRINGER 18L. REPAIRED FRAM ES PER SRM. 2 L 7 2 4F A16WE 1999123100203 19991231 00203 NM 1999 12 31 SWAA992099 1 19991220 A 3350 07912 EEL COVER BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT COVERS LOOSE AT ROW 17 AND AFT END. RESECURED COVERS PER MM. 2 L 7 2 4F A16WE 1999123100204 19991231 00204 NM 1999 12 31 SWAA992100 1 19991220 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389SW 26592 EEPLS INOP AT OVERWING EXIT. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1999123100205 19991231 00205 NM 1999 12 31 SWAA992101 1 19991221 A 5610 5893543109 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT LEAKING A SWAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 320SW 23341 AIR TURNBACK- DURING CLIMB HEARD A LOUD PRESS LEAK NOISE FROM L1 WINDOW. RESEALED LT SIDE OF L1 WINDOW PER MM, LEAK CH ECKED GOOD. 2 L 7 2 4F RT A16WE 1999123100206 19991231 00206 1999 12 31 SWAA992102 4 19991221 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999123100207 19991231 00207 1999 12 31 SWAA992103 4 19991221 A 2565 65C19901 CABLE BOEING 737 7372H4 138448C NM ESCAPE SLIDE MISINSTALLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE RELEASE CABLE OUT OF POSITION. RE-ROUTED CABLE PER M M. 2 L 7 2 4F A16WE 1999123100208 19991231 00208 NM 1999 12 31 SWAA992104 1 19991221 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F A16WE 1999123100209 19991231 00209 NM 1999 12 31 SWAA992089 1 19991217 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER SURFACE CORRODED, BS 986, LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER RE N R 99-6451. 2 L 7 2 4F RT A16WE 1999123100210 19991231 00210 NM 1999 12 31 SWAA992090 1 19991217 A 5311 6546546 FRAME BOEING 737 7375H4 138449D NM BS 747 - 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D-CHECK, FOUND 6 FUSELAGE FRAME CRACKS, BS 747, LBL 60, BS 827, LBL 60 AND RBL 60, BS 867 LBL 60 AND RB L 60, AND BS 907, LBL 60. REPAIRED FRAMES PER ER NR 99-6438. 2 L 7 2 4F RT A16WE 1999123100211 19991231 00211 NM 1999 12 31 SWAA992091 1 19991217 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 360 - 386 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED, BS 360-386. SPLICED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 1999123100212 19991231 00212 NM 1999 12 31 SWAA992092 1 19991217 A 5511 6547500 SPAR BOEING 737 7375H4 138449D NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB FRONT SPAR CHORD CRACKED, STA 57.93. REPAIRED SPAR CHORD PER ER NR 9 9-6467. 2 L 7 2 4F RT A16WE 1999123100213 19991231 00213 NM 1999 12 31 SWAA992093 1 19991220 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS INOP. REPAIRED WIRING PER WDM. 2 L 7 2 4F RT A16WE 1999123100214 19991231 00214 NM 1999 12 31 SWAA992094 1 19991218 A 5311 6517583 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND LT AND RT SIDE BS 178 SIDE CHORDS CRACKED LBL 26 AND RBL 26. REPAIRED CHORDS PER SRM . 2 L 7 2 4F RT A16WE 1999123100215 19991231 00215 NM 1999 12 31 SWAA992095 1 19991218 A 5311 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED IN AFT LOWER CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999123100216 19991231 00216 NM 1999 12 31 SWAA992096 1 19991218 A 5312 6516300 BULKHEAD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 7. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F A16WE 1999123100217 19991231 00217 1999 12 31 SWAA992097 4 19991220 A 2565 D31354 SLIDE BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 1999123100218 19991231 00218 NM 1999 12 31 SWAA992084 1 19991227 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 EEPLS INOP AT ROW 24. REPAIRED TRACK LIGHTING PER MM. 2 L 7 2 4F RT A16WE 1999123100219 19991231 00219 NM 1999 12 31 SWAA992085 1 19991217 A 5311 6546546 FRAME BOEING 737 7372T4 1384492 NM BS 767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D-CHECK, FOUND FRAME CORRODED, BS 767, WL 150. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 1999123100220 19991231 00220 NM 1999 12 31 SWAA992086 1 19991217 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED LBL 7 AND RBL 5. REPAIRED BULKHEAD PER SRM AND SWA RA NR 1-3 53-2187. 2 L 7 2 4F RT A16WE 1999123100221 19991231 00221 NM 1999 12 31 SWAA992087 1 19991217 A 5311 6516323 FRAME BOEING 737 7375H4 138449D NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 291, BETWEEN STRINGERS 12R-13R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999123100222 19991231 00222 NM 1999 12 31 SWAA992088 1 19991217 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED D-CHECK, FOUND STRINGER SPILCE 4L CRACKED, BS 907. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 1999123100223 19991231 00223 NM 1999 12 31 SWAA992073 1 19991216 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED RON, FOUND AFT EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE AT PIN CONNECTOR D2966 PER MM. 2 L 7 2 4F RT A16WE 1999123100224 19991231 00224 NM 1999 12 31 SWAA992074 1 19991217 A 2781 6971787 SWITCH BOEING 737 7373H4 1384600 NM LE FLAP CONTAMINATED A SWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 302SW 22942 ABORTED TAKEOFF, L/E FLAP/SLAT TRANSIT LIGHTS ILLUMINATED AND TAKEOFF WARNING HORN SOUNDED UPON THROTTLE ADVANCEMENT. C LEANED KRUEGER FLAP POSITION INDICATOR SWITCHES. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 1999123100225 19991231 00225 NM 1999 12 31 SWAA992075 1 19991219 A 7312 577957 DUCT BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE CRACKED A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 93SW 22965 AIR TURNBACK, NR 1 ENG OVERHEAT LIGHT ILLUMINATED. FOUND NR 1 ENG UPPER FUEL HEAT DUCT CRACKED. REMOVED AND REPLACED D UCT PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1999123100226 19991231 00226 NM 1999 12 31 SWAA992076 1 19991218 A 2170 COALESCER BOEING 737 7375H4 138449D NM A/C BAY CONTAMINATED A SWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 515SW 25154 AIR TURNBACK, FWD LAV SMOKE ALARM SOUNDED FOLLWED BY A STRONG ODOR THROUGH OUT CABIN. RESET FWD LAV SMOKE DETECTOR C/B. OPS CK GOOD. REMOVED AND REPLACED BOTH A/C WATER SEPARATOR'S COALESCER BAGS. 2 L 7 2 4F RT A16WE 1999123100227 19991231 00227 1999 12 31 SWAA992077 4 19991218 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999123100228 19991231 00228 NM 1999 12 31 SWAA992078 1 19991216 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR LOWER FUSELAGE SKIN CUTOUT CRACKED AT DOUBLER. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1999123100229 19991231 00229 NM 1999 12 31 SWAA992079 1 19991216 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 787 & 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 787, STRINGER 19L AND BS 480, STRINGER 10R. RE PAIRED FUSELAGE SKIN PER SRM. 2 L 7 2 4F RT A16WE 1999123100230 19991231 00230 NM 1999 12 31 SWAA992080 1 19991216 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 772, LBL 18 TO RBL 14. REPAIRED BEAM PER SW A RA NR 1-A53-2021. 2 L 7 2 4F RT A16WE 1999123100231 19991231 00231 NM 1999 12 31 SWAA992081 1 19991216 A 5320 141A880 POST BOEING 737 7375H4 138449D NM COCKPIT WINDOW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D-CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED, UPPER LT SECTION. REPAIRED PER SWA RA NR 1-A53-1156. 2 L 7 2 4F RT A16WE 1999123100232 19991231 00232 NM 1999 12 31 SWAA992082 1 19991216 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED SPECIAL VISIT, FOUND EEPLS INOP, ROWS 6 TO 13. REPAIRED WIRING PER WDM. 2 L 7 2 4F RT A16WE 1999123100233 19991231 00233 NM 1999 12 31 SWAA992083 1 19991216 A 3350 D717001 BATTERY BOEING 737 7377H4 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 714CB 27848 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 1999123100234 19991231 00234 NM 1999 12 31 SWAA992112 1 19991222 A 2751 65C46990 INDICATOR BOEING 737 7373Q8 1384670 NM COCKPIT MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 672SW 23406 AIR TURNBACK, T/E FLAP POSITION INDICATION OF FLAPS NOT RETRACTING BETWEEN 2 AND 5 DEGREES. RESET T/E FLAP POSITION IND ICATOR C/B, RESEATED T/E FLAP POSITION TRANSMITTER CONNECTOR. OPERATED T/E FLAPS, OPS CK GOOD. LATER DURING RON AT BWI REMOVED AND REPLACED T/E FLAP POSITION INDICATOR FOR MX CONVENIENCE. 2 L 7 2 4F RT A16WE 1999123100235 19991231 00235 NM 1999 12 31 SWAA992113 1 19991222 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 605SW 27956 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED, BS 807, BETWEEN STRINGERS 27L-28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 1999123100236 19991231 00236 NM 1999 12 31 SWAA992114 1 19991222 A 3350 BATTER PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 614SW 28033 EEPLS INOP BETWEEN ROWS 14 AND 19. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 1999123100237 19991231 00237 1999 12 31 SWAA992115 4 19991222 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 AFT ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 1999123100238 19991231 00238 NM 1999 12 31 SWAA992117 1 19991222 A 3350 BR2013 LIGHT BOEING 737 7375H4 138449D NM ROW 14 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK CRACKED AT ROW 14. REMOVED AND REPLACED TRACK SECTION PER MM. 2 L 7 2 4F RT A16WE 1999123100239 19991231 00239 NM 1999 12 31 SWAA992118 1 19991222 A 2750 6546428 FLAP TRACK BOEING 737 7372T4 1384492 NM TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D-CHECK, FOUND PITTING CORROSION AT NR 1 AND NR 8 T/E FLAP TRACKS AFT MOUNTING SURFACES. REMOVED AND R EPLACED FLAP TRACKS PER MM AND ACO. 2 L 7 2 4F A16WE 1999123100240 19991231 00240 NM 1999 12 31 SWAA992111 1 19991222 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 FLOORBEAM UPPER SURFACE CORRODED, RBL 31-RBL 35. REPAIRED BEAM PER SWA RA NR 1-353-2188. 2 L 7 2 4F RT A16WE 1999123100241 19991231 00241 SO 1999 12 31 LR7A9970 1 19990519 A 3211 3884932 BEAM LKHEED 382 382G 526414U SO BS 597 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION PER HST5319 (ST-19) FOUND FS 597 RT MLG BEAM CORRODED AT WL 146. REMOVED CORROSION, TREA TED AND REPAIRED IAW SRM 583 53-40-31. DRC-0020-SM. 2 H 7 4 4T A1SO 1999123100242 19991231 00242 SO 1999 12 31 LR7A9971 1 19990503 A 5320 3896801 ANGLE LKHEED 382 382G 526414U SO BS 517 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION PER HST5316 (ST-16) FOUND LT MLG WHEEL WELL FS 517 CHINE CORRODED AT WL 146, LBL 61.6. N DI ACCOMPLISHED, NO DEFECTS NOTED. CORROSION REMOVED AND TREATED PER SRM 583-53. REPAIRED PER MEA 382-53-99-109. DRC 0070-SM. 2 H 7 4 4T A1SO 1999123100243 19991231 00243 SO 1999 12 31 LR7A9972 1 19990424 A 5320 3561824 FITTING LKHEED 382 382G 526414U SO BS 817E CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION PER SB 382-53-53, FOUND RT FS 817E BULKHEAD FITTING CRACKED AT WL 143. REPLACED FITTING IAW SB 382-53-53 R2. DRC-0079-SM. 2 H 7 4 4T A1SO 1999123100244 19991231 00244 SO 1999 12 31 LR7A9973 1 19990428 A 5720 WEB LKHEED 382 382G 526414U SO WS 542 - 562 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION LT WING OWS 545 TO 562 FWD SPAR WEB DUE REPLACEMENT TO CORRECT DAMAGE FROM INCIDENT 6/27/ 98 AND TERMINATE REPETITIVE INSPECTION REQUIREMENT. WEB REPLACED FROM OWS 545 TO 562 IAW SRM 583-57-30-22. DRC-0001-SM . 2 H 7 4 4T A1SO 1999123100245 19991231 00245 SO 1999 12 31 LR7A9974 1 19990504 A 3211 38848212 BEAM LKHEED 382 382G 526414U SO BS 577 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION PER HSP5369 (SP-69) FOUND FS 577 RT MLG VERTICAL BEAM CORRODED AT WL 179 AT OUTER CAP END . REPAIRED IAW SRM 583-53-40-09. DRC-110-SM. 2 H 7 4 4T A1SO 1999123100246 19991231 00246 SO 1999 12 31 LR7A9975 1 19990507 A 7120 360015 TRUSS MOUNT LKHEED 382 382G 526414U SO NR 3 ENGINE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION PER HST5409 FOUND NR 3 I/B TRUSS MONT LOWER ATTACHMENT BARREL NUT CAVITY CRACKED. REPLAC ED TRUSS MOUNT IAW SRM 583-54-30-06. (P/N 360015-19) INSTALLED. DRC-0009 AND 0138-SM. 2 H 7 4 4T A1SO 1999123100247 19991231 00247 SO 1999 12 31 LR7A9976 1 19990504 A 5320 3914878 BEAM LKHEED 382 382G 526414U SO BS 599 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION PER HST5316 (ST-16) FOUND RT FS 599 VERTICAL BEAM CORRODED AT WL 146. NDI INSPECTION, NO CRACKS. REPAIRED IAW MEA 382-53-99-108. 2 H 7 4 4T A1SO 1999123100248 19991231 00248 SO 1999 12 31 LR7A9977 1 19990503 A 5320 BEAM LKHEED 382 382G 526414U SO BS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING SCHEDULED C1 INSPECTION PER HSP5369 (SP-69) FOUND FS 517 LT MLG VERTICAL BEAM CRACKED AT WL 256.5 IN THE FLANGE A REA. REPAIRED PER SRM SMP 583-53-40-17. DRC 0021-SM. 2 H 7 4 4T A1SO 1999123100249 19991231 00249 WP 1999 12 31 IXXA9900034 1 19991224 A 3297 WIRE DOUG DC8 DC871F 302199D WP LT MLG DOOR BROKEN A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 829BX 81970 461 45994 EN ROUTE FROM ICT TO GDL, THE LANDING GEAR DOOR UNSAFE LIGHT ILLUMIATED AFTER A SUCCESSFUL LANDING GEAR UPLATCH CHECK WA S ACCOMPLISHED. THE FLIGHT CREW CYCLED THE GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED T O GDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTION THE LANDING GEAR LOCATING A BROKEN WIRE ON THE LEFT GEAR DOOR W ARNING SWITCH. THE WIRING WAS REPAIRED AND A SUCCESSFUL OPERATIONAL TEST WAS PERFORMED. 2 L 7 4 4F RT 4A25 1999123100250 19991231 00250 WP 1999 12 31 IXXA9900035 1 19991227 A 3260 CONNECTOR DOUG DC8 DC871F 302199D WP LT MLG DOOR FAILED A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 829BX 45994 AFTER TAKEOFF FROM GDL TO TOL, WHEN THE LANDING GEAR WAS RETRACTED THE LANDING GEAR DOOR UNSAFE LIGHT WAS INTERMITTENTLY FLASHING THEN EXTINGUISHED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND THE FLIGHT CONTINUED TO TOL FOR AN UNEVENT FUL LANDING. MAINTENANCE INSPECTION THE LANDING GEAR WARNING SYSTEM LOCATING A DEFECTIVE CANNON PLUG ON THE LEFT GEAR D OOR WARNING SWITCH. THE CANNON PLUG WAS REPLACED AND A SUCCESSFUL OPERATIONAL TEST WAS PERFORMED. 2 L 7 4 4F RT 4A25 1999123100251 19991231 00251 NM 1999 12 31 CALA9901735 1 19991227 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 420 - 440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 420-440, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALL ED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1999123100252 19991231 00252 WP 1999 12 31 CALA9901736 1 19991227 A 5730 PANEL DOUG DC10 DC1030 3023501 WP RT WING DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12089 46550 INSPECTION FOUND RT WING TRAILING EGDE PANEL 641JB DELAMINATED. THE PANEL WAS REPLACED IAW MM 20-50-02. 2 L 7 3 4F A22WE 1999123100253 19991231 00253 WP 1999 12 31 CALA9901737 1 19991227 A 5753 PANEL DOUG DC10 DC1030 3023501 WP TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12089 46550 INSPECTION FOUND RT WING O/B HINGE O/B FLAP PANEL 636DL DELAMINATED. THE PANEL WAS REPLACED IAW MM 20-50-02. 2 L 7 3 4F A22WE 1999123100254 19991231 00254 EA 1999 12 31 COMA9960782 1 19991222 A 3246 50105711 WHEEL LORAL CNDAIR CL600 CL6002B19 EA MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA MAY960895 7134 MECHANIC FOUND BOTH MAIN WHEELS FROM AIRCRAFT DUE RT/DB TIRE FLAT. DURING VISUAL LEAK CHECK IN TIRE SHOP FOUND WHEEL SU BASSEMBLY WAS CRACKED AT BOTTOM OF KEY BOSS AREA. CRACK WAS FOUND TO BE ABOUT 1 INCH LONG. WHEEL SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS. 2 L 7 2 4F RT A21EA 1999123100255 19991231 00255 EA 1999 12 31 COMA9960783 1 19991212 A 5315 601R3111367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 - 409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 FLOORBEAM CAPS LBL 27, LBL 9, RBL 9, AND RBL 27 IN AREAS FROM FS 280.00 TO FS 409 FOUND TO BE CORRODED BEYOND LIMITS. R EMOVED CORRODED SECTIONS OF FLOORBEAM CAPS AND SPLICED IN NEW SECTIONS IAW REO 601R-53-00-027 AND WVAC EO 601R-53-0719. 2 L 7 2 4F RT A21EA 1999123100256 19991231 00256 EA 1999 12 31 COMA9960784 1 19991218 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 7080 FS 718 RIGHT SIDE FRAME AND DOUBLER CRACKED IN RADIUS BETWEEN STR 10-12. REPAIRED FS 718 RIGHT SIDE FRAME AND DOUBLER I AW REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 1999123100257 19991231 00257 EA 1999 12 31 COMA9960785 1 19991218 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 710CA 7241 FUSELAGE FRAME AT FS 718 STR 11-12 LHS IS CRACKED IN FWD FRAME. REPAIRED FRAME AT FS 718 STR 11-12 IAW SRM 6-1R-53-61-1 93 REV A. 2 L 7 2 4F RT A21EA 1999123100258 19991231 00258 EA 1999 12 31 COMA9960786 1 19991218 A 5320 6003603031 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 949CA 7080 FS 718 LEFT SIDE DOUBLER CRACKED IN RADIUS. REPAIRED FS 718 LEFT SIDE DOUBLER IAW REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 1999123100259 19991231 00259 EA 1999 12 31 COMA9960787 1 19991218 A 5270 SEAL STRIKER CNDAIR CL600 CL6002B19 EA BS 310 BENT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 710CA 7241 PAX DOOR SEAL STRIKER AT FS 310 DAMAGED BY LOWER DOOR PIN. TRIMMED OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED, FINISHED OUT REPAIR IAW CANADAIR REO 601R-52-11-008 REPAIR A. 2 L 7 2 4F RT A21EA 1999123100260 19991231 00260 EA 1999 12 31 COMA9960788 1 19991221 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA BS 480 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 THE ATTACH ANGLES AT FS 484 AT RBL 27 AND LBL 36 WERE CRACKED. INSTALLED NEW BRACKETS IAW WVAC EO 601R-53-07628. 2 L 7 2 4F RT A21EA 1999123100261 19991231 00261 EA 1999 12 31 COMA9960789 1 19991212 A 5320 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA BS 310 & 319 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 DOUBLER PLATE CORRODED BETWEEN FS 310.00 AND FS 319.00 AT RBL 42 BEYOND REPAIRABLE LIMITS. REMOVED CORRODED DOUBLER AND INSTALLED NEW SERVICEABLE DOUBLER (P/N 601R38669-49) IAW WVAC EO 601R-53-0748. 2 L 7 2 4F RT A21EA 1999123100262 19991231 00262 EA 1999 12 31 COMA9960790 1 19991215 A 5320 601R38303253 THRESHOLD CNDAIR CL600 CL6002B19 EA BS 317 - 342 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 THRESHOLD SUPPORT HAD DEEP CORROSION RBL 40 FS 317-FS 342 (SERVICE DOOR THRESHOLD). INSTALLED NEW THRESHOLD SUPPORT ANG LE IAW WVAC EO 601R-53-0709B. 2 L 7 2 4F RT A21EA 1999123100263 19991231 00263 EA 1999 12 31 COMA9960791 1 19991213 A 5311 FRAME CNDAIR CL600 CL6002B19 EA BS 324.5 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 SERVICE DOOR FRAME HAD DEEP GOUGES BY 2 ANCHOR NUTS AND CORROSION RBL 44 FS 324.5 AT FS 326. REPAIRED CORRODED AREAS ON LOWER SILL OF SERVICE DOOR IAW WVAC EO 601R-53-0718A. 2 L 7 2 4F RT A21EA 1999123100264 19991231 00264 EA 1999 12 31 COMA9960792 1 19991218 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 THE FLOORBEAM WEB AT FS 280 IS CORRODED IN THE UPPER EDGE BETWEEN RBL 9 AND LBL 9 APPROXIMATELY 3 X .5 AT BL 0. REPAIRE D FLOORBEAM WEB IAW WVAC EO 601R-53-0712. 2 L 7 2 4F RT A21EA 1999123100265 19991231 00265 EA 1999 12 31 COMA9960793 1 19991218 A 5320 601R31527131 CLEAT CNDAIR CL600 CL6002B19 EA BS 349 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 THE CLEAT ATTACHING TO BRACKET ASSY 601R31527-149 AT FS 349 IS CORRODED. REMOVED CRACKED CLEAT, FABRICATED NEW CLEAT AN D INSTALLED CLEAT IAW WVAC EO 601R53-0714. 2 L 7 2 4F RT A21EA 1999123100266 19991231 00266 EA 1999 12 31 COMA9960794 1 19991212 A 5320 6003401737337 CLIP CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 ANGLE CLIPS INSIDE CBP1 AND CBP2 UTB OUTBOARD OF RBL 9.0 AND LBL 9.0 AT FS 280.00 WERE CRACKED. REMOVED CRACKED ANGLE C LIPS, FABRICATED NEW ANGLE CLIPS PER SAMPLER AND INSTALLED CLIPS IAW WVAC EO 601R-53-0706. 2 L 7 2 4F RT A21EA 1999123100267 19991231 00267 EA 1999 12 31 COMA9960795 1 19991212 A 5320 601R311135758 CLIP CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 ANGLE CLIPS AT FS 280.00 AT LBL 9.0 AND RBL 9.0 ARE CRACKED. REMOVED CRACKED CLIPS, FABRICATED NEW CLIPS, AND INSTALLED CLIPS IAW WVAC EO 601R-53-0707. 2 L 7 2 4F RT A21EA 1999123100268 19991231 00268 EA 1999 12 31 COMA9960796 1 19991212 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 THE FORWARD J ANGLE AT FS 280.00 BETWEEN LBL 9.0 AND RBL 9.0 WAS CORRODED. REMOVED CORRODED ANGLE AND INSTALLED NEW ANG LE (P/N 600-34017-351) IAW WVAC EO 601R-53-0705. 2 L 7 2 4F RT A21EA 1999123100269 19991231 00269 EA 1999 12 31 COMA9960797 1 19991212 A 5315 6003401717 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 THE FLOOR MEMBER AT FS 280.00 WAS CRACKED .5 - .75 APPROXIMATELY 1 INCH TO THE RIGHT OF FLOOR SUPPORT AT RBL 9.0. REPAI RED FLOOR MEMBER IAW WVAC EO 601R-53-0708. 2 L 7 2 4F RT A21EA 1999123100270 19991231 00270 EA 1999 12 31 COMA9960798 1 19991212 A 5320 601R38303105 ANGLE CNDAIR CL600 CL6002B19 EA BS 317 - 342 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 SERVICE DOOR THRESHOLD ANGLEWAS CORRODED AT FS 317.00 TO FS 342.00 BEYOND REPAIRABLE LIMITS. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE IAW WVAC EO 601R-53-0702. 2 L 7 2 4F RT A21EA 1999123100271 19991231 00271 EA 1999 12 31 COMA9960799 1 19991212 A 5320 601R352746 ANGLE CNDAIR CL600 CL6002B19 EA BS 310 - 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 PAX DOOR SUPPORT THRESHOLD WAS CORRODED BEYOND REPAIRABLE LIMITS FS 310.00 FS 349.00. REMOVED CORRODED ANGLE AND INSTAL LED NEW ANGLE IAW WVAC EO 601R-53-0703, REV A. 2 L 7 2 4F RT A21EA 1999123100272 19991231 00272 EA 1999 12 31 COMA9960800 1 19991212 A 5320 601R31527181 ANGLE CNDAIR CL600 CL6002B19 EA BS 310 - 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 PAX DOOR THRESHOLD TOP ANGLE CORRODED BEYOND REPAIRABLE LIMITS AT FS 310.00 TO FS 349.00. REMOVED CORRODED ANGLE AND IN STALLED NEW ANGLE IAW WVAC EO 601R-53-0704. 2 L 7 2 4F RT A21EA 1999123100273 19991231 00273 EA 1999 12 31 COMA9960801 1 19991212 A 5320 601R3867314 TOP PLATE CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 7031 TOP PLATES AT FS 349 OUTBOARD OF LBL 9, RBL 9 AND RBL 27 ARE ALL CORRODED BEYOND REPAIRABLE LIMITS. REMOVED CORRODED TO P PLATES AT LBL 9 (601R38673-19), RBL 9 (601R38673-21) AND AT RBL 27 (601R38673-25) AND REPLACED WITH NEW BEAM CAPS OF S AME PART NUMBER IAW WVAC EO 601R-53-0701, REV A. 2 L 7 2 4F RT A21EA 1999123100274 19991231 00274 EA 1999 12 31 COMA9960802 1 19991212 A 5315 601R311367 FLOORBEAM CNDAIR CL600 CL6002B19 EA BS 280 - 409 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 927CA 14734 7031 FLOORBEAM CAPS LBL 27, LBL 9, RBL 9 AND RBL 27 IN AREAS FROM FS 280.00 TO FS 409 FOUND TO BE CORRODED BEYOND LIMITS. RE MOVED CORRODED SECTIONS OF FLOORBEAM CAPS AND SPLICED IN NEW SECTIONS IAW REO 601R-53-00-027 AND WVAC EO 601R-53-0719. 2 L 7 2 4F RT A21EA 1999123100275 19991231 00275 EA 1999 12 31 COMA9960803 1 19991223 A 5320 60034017373 STIFFENER CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 VERTICAL STIFFENESS CRACKED AT FS 28 DEGREES BELOW CBP-1 AND CBP-2 AT LBL 12 AND RBL 12. INSTALLED NEW STIFFENERS IAW W VAC EO 601R-53-0759. 2 L 7 2 4F RT A21EA 1999123100276 19991231 00276 EA 1999 12 31 COMA9960804 1 19991222 A 5320 601R3866949 DOUBLER CNDAIR CL600 CL6002B19 EA BS 310 - 319 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 DOUBLER PLATE AT RBL 42 FS 310 - FS 319 (P/N 601R38669-49) WAS CORRODED. INSTALLED NEW DOUBLER PLATE AT RBL 42 FS 310 - 319 IAW WVAC EO 601R-53-0778. 2 L 7 2 4F RT A21EA 1999123100277 19991231 00277 EA 1999 12 31 COMA9960805 1 19991222 A 5320 601R3111317 WEB CNDAIR CL600 CL6002B19 EA BS 307 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 OUTBOARD WEB AT LBL 27 FS 307 HAD ELONGATED HOLE .27 DEGREES DIAMETER (P/N 601R31113-17). INSTALLED NEW WEB IAW WVAC EO 6501R-53-0772. 2 L 7 2 4F RT A21EA 1999123100278 19991231 00278 EA 1999 12 31 COMA9960806 1 19991222 A 5320 601R38303105 THRESHOLD CNDAIR CL600 CL6002B19 EA BS 317 - 342 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 SERVICE DOOR THRESHOLD TOP ANGLE (P/N 601R38303 105) WAS CORRODED FS 317 - FS 342. INSTALLED NEW THRESHOLD TOP ANGLE IA W WVAC EO 601R-53-0757. 2 L 7 2 4F RT A21EA 1999123100279 19991231 00279 EA 1999 12 31 COMA9960807 1 19991222 A 5320 601R3152746 THRESHOLD CNDAIR CL600 CL6002B19 EA BS 310 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 PAX DOOR THRESHOLD TOP ANGLE (P/N 601R31527-46) WAS CORRODED. INSTALLED NEW PAX DOOR THRESHOLD ANGLE IAW WVAC EO 601R-5 3-0757. 2 L 7 2 4F RT A21EA 1999123100280 19991231 00280 EA 1999 12 31 COMA9960808 1 19991226 A 5320 60034017587 WEB CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 FS 280.00 WEB (P/N 600-34017-587) CORRODED. REMOVED FORWARD J ANGLE TO ACCESS WEB, TRIMMED OUT DAMAGED AREA FAB FILLER AND REPAIR DOUBLER, INSTALLED, REINSTALLED FWD J ANGLE IAW WVAC EO 601R-53-0773. 2 L 7 2 4F RT A21EA 1999123100281 19991231 00281 EA 1999 12 31 COMA9960809 1 19991226 A 5320 601R3111357 CLIP CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 FS 280.00 LBL 9 HAD CRACKED FLOOR SUPPORT ANGLE. REMOVED DAMAGED ANGLE AND FABED NEW ANGLE, INSTALLED IAW WVAC EO 601R- 53-0760. 2 L 7 2 4F RT A21EA 1999123100282 19991231 00282 EA 1999 12 31 COMA9960810 1 19991226 A 5320 60034017595 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 14413 7035 FS 280.00 AFT J ANGLE (P/N 600-34017-595) WAS CORRODED. TRIMMED OUT DAMAGED AREA OF J ANGLE AND FABED NEW SECTION, INST ALLED IAW WVAC EO 601R-53-0774. 2 L 7 2 4F RT A21EA 1999123100283 19991231 00283 EA 1999 12 31 COMA9960811 1 19991226 A 5320 60034017351 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 929CA 7035 FS 280.00 FWD J ANGLE (P/N 600-34017-351) IS CORRODED. REMOVED DAMAGED J ANGLE AND REPLACED IAW WVAC EO 601R-53-0758. 2 L 7 2 4F RT A21EA 1999123100284 19991231 00284 EA 1999 12 31 COMA9960812 1 19991218 A 5311 6003603014 FRAME CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 710CA 7241 FUSELAGE FRAME AT FS 718.0 STR 11-12 RHS AFT DOUBLER CRACKED. PERFORMED A MAJOR REPAIR BY REPLACING AFT DOUBLER ON FUSE LAGE FRAME AT FS 718.0 STR 11-12 RHS IAW CRJ REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 1999123100285 19991231 00285 WP 1999 12 31 99FDEA00511 1 19991223 A 3234 LEVER DOUG DC10 DC1010F 3022111 WP MLG STICKING A FDEA O OTHER O OTHER AP APPROACH 1 SO 25 367FE 46605 LOWERED GEAR DIDN'T GET LIGHT ON EITHER PNL. WHEN GEAR ALT HANDLE IS STOW AFT LAND RED LIGHTS ILLUM. LUBED LANDING GEA R CONTROL LEVER MECHANISM. OPS CK GOOD. GROUND LIGHT ON BOTH POS. 2 L 7 3 4F A22WE 1999123100286 19991231 00286 EU 1999 12 31 99FDEA00512 1 19991224 A 7830 THRUST REVERSER AIRBUS 310 A310222 3930315 EU NR 3 ENGINE INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 450FE 162 NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUM ON T/O ROLL. NR 2 ENG THRUST REVERSER DEACTIVATED PER MEL 78-1. ITEM TO BE SCHEDULED FOR REPAIRS 2 L 7 2 4F RT A35EU 1999123100287 19991231 00287 EU 1999 12 31 99FDEA00513 1 19991228 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 669FE 774 ON T/O, ECAM SOUNDED AND DISPLAY NR 2 REV PRESSURIZED. THROTTLE PLACED AT IDLE, RETURN TO DEPART. T/REV DEFERRED PER M EL 78-1 NR 2 REVERSER LOCKED OUT. 2 L 7 2 4F RT A35EU 1999123100288 19991231 00288 NM 1999 12 31 99UAL900592 1 19991026 A 5315 6546808 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF T HE WEB AND THE UPPER CAP OF THE I-BEAM. *S/D* REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM . 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100289 19991231 00289 NM 1999 12 31 99UAL900593 1 19991021 A 5315 6546808 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF T HE WEB AND THE UPPER CAP OF THE I-BEAM. *S/D* REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM . 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100290 19991231 00290 NM 1999 12 31 99UAL900594 1 19991117 A 5315 6546808 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF T HE WEB AND THE UPPER CAP OF THE I-BEAM. *S/D* REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM . 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100291 19991231 00291 NM 1999 12 31 99UAL900595 1 19991108 A 5315 6546808 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF T HE WEB AND THE UPPER CAP OF THE I-BEAM. *S/D* REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM . 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100292 19991231 00292 NM 1999 12 31 99UAL900596 1 19991111 A 5315 6546808 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF T HE WEB AND THE UPPER CAP OF THE I-BEAM. *S/D* REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM . 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100293 19991231 00293 NM 1999 12 31 99UAL900603 1 19991117 A 5315 6546808 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF T HE WEB AND THE UPPER CAP OF THE I-BEAM. *S/D* REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM . 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100294 19991231 00294 NM 1999 12 31 99UAL900652 1 19991217 A 2930 WARNING LIGHT BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE HYD SYSTEM ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 990UA 21980 THE CREW REPORTED THE 'A' HYDRAULIC SYSTEM QUANTITY INDICATION OF 1.9 GALLONS ALONG WITH THE ILLUMINATION OF THE LOW QUA NTITY LIGHT FOR THE STANDBY HYDRAULIC SYSTEM. 2 L 7 2 4F 4 F A16WE E2EA 1999123100295 19991231 00295 NM 1999 12 31 99UAL900653 1 19991219 A 3244 TIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 383UA 24658 ON TAKEOFF, THE CREW SUSPECTED THAT THE NOSE TIRES WERE BLOWN. REPLACED BOTH NOSE TIRES. INSPECTED ALL GEAR STRUTS, WI NG LOWER SURFACES AND FLAPS, NO DAMAGES NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100296 20001016 00296 NM 2000 10 16 99UAL900654 1 19991214 A 2120 UNKNOWN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN SMOKE A UALA G O2 MASK DEPLOYED B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7444U 21898 ON LANDING WHILE ENGINES WERE IN REVERSE SMOKE APPEARED IN CABIN. ENGINE BLEEDS AND PACKS WERE SHUT OFF PROBLEM WENT AW AY. *S/D* UNKNOWN CAUSE. SEATTLE MAINTENANCE TRIED TO DUPLICATE PROBLEM BY RUNNING ALL ENGINES AND PACKS, AND CYCLEIN G REVERSERS. PROBLEM COULD NOT BE DUPLICATED. 2 L 7 3 4F 4 F A3WE E2EA 1999123100297 20001016 00297 NM 2000 10 16 99UAL900655 1 19991216 A 5297 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE PAX DOOR BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7462U 21916 UNABLE TO PRESSURIZE AIRCRAFT. NOISE FROM NOSE OF AIRCRAFT, OUTFLOW FULLY CLOSED. TRIED AUTO, STANDBY AND MANUAL ALL D OOR LIGHTS OFF AND TEST OK. FLIGHT DIVERTED TO SFO. *S/D* BROKEN WIRE ON DOOR WARNING SENSOR. RELUGGED WIRE CHECK S YSTEM IN ALL MODES, NO PROBLEMS FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1999123100298 19991231 00298 NM 1999 12 31 99UAL900656 1 19991217 A 2782 1U1110 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE FLAP LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7265U 21412 FLIGHT RETURNED TO MIA DUE TO LOSS OF A SYSTEM HYDRAULIC FLUID. *S/D* REPLACED NR 5 LEADING EDGE FLAP ACTUATOR PER MAI NTENANCE MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 1999123100299 20001016 00299 NM 2000 10 16 99UAL900657 1 19991218 A 2597 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SEAT 6 CHAFED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7278U 21425 SPARKS AND FRAYED WIRE AT SEAT 6E. *S/D* CABLE WIRES LOCATED UNDER SEAT ASSY RUBBED OR CHAFED CREATING SPARKS. WIRES WERE TAPED AND THE AFFECTED PASSENGER ENTERTAINMENT SEAT HARNESS WAS REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999123100300 20001016 00300 NM 2000 10 16 99UAL900658 1 19991218 A 3320 6013211LB POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7450U 21904 FORWARD GALLEY EXTERIOR EMERGENCY LIGHTING SYSTEM SLIDE LIGHT INOP. *S/D* EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PA CK. REPLACED EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK. OPERATIONAL TEST CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1999123100301 20001016 00301 NM 2000 10 16 99UAL900659 1 19991216 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FIRE A UALA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 WP 29 656UA 25394 OVEN FIRE IN FLIGHT. DISCHARGED HALON EXTINGUISHER. *S/D* PAPER DEBRIS ON OVEN INSERT CAUSED SMALL FLAME-UP IN FLT. THE FIRE WAS EXTINGUISHED BY CREW USING HALON EXTINGUISHER. CHECKED OVEN AND GALLEY SURROUNDING AREA FOR DAMAGED, NO DA MAGE FOUND. CLEANED OVEN AND FAN SCREEN. RAN OVEN AT VARIOUS TIME SETTING, NO DISCREPANCY FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 1999123100302 20001016 00302 NM 2000 10 16 99UAL900660 1 19991220 A 2612 FIRE LOOP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE OUT OF POSITION A UALA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 WP 29 7451U 21905 696554 ENGINE 1 STRUT OVERHEAT LIGHT CAME ON. COMPLETED IN FLIGHT ENGINE SHUTDOWN, LIGHT REMAINED ON. *S/D* THE STRUT OVERHE AT LIGHT ILLUMINATION IN-FLIGHT WAS AN INDICATION PROBLEM. ALL DUCTS WERE FOUND INTACT. THE OVERHEAT LOOP WAS FOUND RE STING ON THE 13TH STAGE DUCT AND WAS RESPOITIONED. 2 L 7 3 4F 4 F A3WE E2EA 1999123100303 20001016 00303 EU 2000 10 16 99UAL900661 1 19991220 A 4930 4500039D FUEL CONTROL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU LEAKING A UALA F D ACTIVATE FIRE EXT. RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 401UA 3079 3079 435 1087 ON TAXI OUT AN AMERICAN AIRLINES CREW REPORTED FLAMES FROM THE APU EXHAUST. CREW SHUT DOWN THE APU AND RETURNED TO THE GATE. MM RESTARTED THE APU AND FLAMES RETURNED. FIRE BOTTLE WAS BLOWN AND FIRE DEPARTMENT CALLED TO STANDBY. *S/D* T HE CAUSE OF THE FAILURE HAS BEEN ATTRIBUTED TO A PARTIALLY STUCK SOLENOID VALVE ON THE FUEL CONTROL UNIT. THIS PERMITTE D FUEL TO ENTER THE COMBUSTOR FOLLOWING APU SHUTDOWN. THE APU SEIZURE OCCURRED AFTER THE FAILURE EVENT AND CAN BE ATTRI BUTED TO THE CORROSION IN THE GEARBOX AND INGESTED EXTINGUISHING AGENT IN THE LOAD COMPRESSOR AND POWER SECTION. ROTATI NG COMPONENTS WERE NOT RUBBED. CORROSION HAS BEEN ATTRIBUTED TO INGESTION OF WATER AND CHEMICAL EXTINGUISHING AGENT. 2 L 7 2 4F 4 F RT A28NM E40NE 1999123100304 19991231 00304 NM 1999 12 31 99UAL900662 1 19991221 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7446U 21900 RIGHT EXTERIOR OVERWING EMERGENCY LIGHTS INOP. 2 L 7 3 4F 4 F A3WE E2EA 1999123100305 19991231 00305 NM 1999 12 31 99UAL900663 1 19991130 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 927 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 DISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF T HE WEB AND THE UPPER CAP OF THE I-BEAM. REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 1999123100306 20001016 00306 2000 10 16 99UAL900664 4 19991216 A 2310 7926140001 COUPLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HF RADIO FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 772UA 26930 EN ROUTE CDG-IAD, LOST RIGHT HIGH FREQUENCY RADIO. DIVERTED TO LHR. *S/D* FAULT, INTERNAL TO THE HIGH FREQUENCY ANTEN NA COUPLER (P/N: 792-6140-001) CAUSED THE COUPLER TO RECEIVE BUT NOT TRANSMIT. UNIT WAS REPLACED AND FULL SYSTEM FUNCTI ONALITY WAS RESTORED. TESTING VERIFIED REPORT OF RECEIVE BUT NOT TRANSMIT FUNCTION AND ADDITIONAL UNIT ANALYSIS IS SCHE DULED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999123100307 20001016 00307 NM 2000 10 16 99UAL900665 1 19991221 A 2131 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 777UA 26916 EN ROUTE ORD-LHR, FAILURE OF BOTH AUTO-PRESSURIZATION CONTROLLERS. CREW ELECTED TO DIVERT TO JFK. *S/D* AT JFK, NO EX ISTING FAULTS WERE FOUND. MAINTENANCE ACCESS TERMINAL GROUND TEST ON CABIN PRESSURE CONTROL WAS PERFORMED PER AMM 21-31 -00. PRESSURIZATION SYSTEM PASSED OPERATIONAL CHECK. AIRCRAFT WAS RETURNED TO REVENUE SERVICE WITHOUT FURTHER INCIDENT . THE QAR (QUICK ACCESS RECORDER) CONTAINING DATA FROM THE AIRPLANE CONDITION MONITORING SYSTEM WAS SENT TO BOEING FOR FURTHER ANALYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999123100308 19991231 00308 WP 1999 12 31 ABXA9900860 1 19991227 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 971AX 47497 EMERGENCY LIGHTS WERE INOPERATIVE. REPAIRED SHORTED WIRE AT EMERGENCY BATTERY PACK AND REPLACED BATTERY POWER SUPPLY. 2 L 7 2 4F A6WE 1999123100309 19991231 00309 WP 1999 12 31 ABXA9900861 1 19991227 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 955AX 47619 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERIES. 2 L 7 2 4F A6WE 1999123100310 19991231 00310 WP 1999 12 31 ABXA9900862 1 19991227 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 986AX 47543 EMERGENCY LIGHTING WOULD NOT TEST. REPLACED EMERGENCY LIGHTS BATTERY PACK. 2 L 7 2 4F A6WE 1999123100311 19991231 00311 WP 1999 12 31 ABXA9900863 1 19991227 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932F 3022067 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 930AX 47363 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1999123100312 19991231 00312 NM 1999 12 31 SCNA99155 1 19991226 A 3350 900835A BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC 21202 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS OVER THE AISLE AT SEAT 5 AND THE OVERWING LIGHTS ABOVE THE LEFT OV ERWING EXITS WERE FOUND INOPERATIVE. RELAMPED 5 SOCKETS AT AISLE SEAT 5 WITH 328 LAMPS. REMOVED AND REPLACED BATTERY P ACK FOR THE LEFT OVERWING EXIT LIGHTS. OPERATIONALLY CHECKS GOOD IAW MM 345022. 2 L 7 3 4F A3WE 1999123100313 19991231 00313 NM 1999 12 31 SCNA99156 1 19991226 A 3350 900835A BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS AT THE OVERWING EXITS WERE FOUND INOPERATIVE. FOUND BATTERY PACK AT M1090 TO BE LOW OF CHARGE. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD IAW MM 335071. 2 L 7 3 4F RT A3WE 1999123100314 19991231 00314 NM 1999 12 31 SCNA99779 1 19991223 A 3211 651628911 FITTING BOEING 727 727225 1384077 NM LT MLG CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING A HEAVY MAINTENANCE CHECK, THE LEFT MAIN LANDING GEAR BEAM OUTBOARD SUPPORT FITTING WAS FOUND TO BE CRACKED. REM OVED AND REPLACED THE LEFT MAIN LANDING GEAR BEAM SUPPORT FITTING IAW SB 72757167. 2 L 7 3 4F A3WE 1999123100324 19991231 00324 SW 1999 12 31 99ZZZX4675 1 19991228 A 7721 8974764 RESISTOR SWRNGN SA227 SA227AC 8780603 SW LT ENGINE FAILED A OZCA O OTHER O OTHER NR NOT REPORTED 1 SO 19 821BC 8913097 AC642 WHEN CAPTAIN REPORTED PULLING POWER, LT ENGINE STARTED TO NTS. THE CAPTAIN ADVANCED LT POWER LEVER WITH NO RESPONSE FRO M THE ENGINE. AT THAT POINT, THE CAPTAIN PER THE AFM, STARTED SINGLE ENGINE LANDING PROCEDURES. THE POSSIBLE CAUSE OF THE LT ENGINE NOT RESPONDING TO POWER LEVER MOVEMENT WAS FUEL BYPASS. AT THIS TIME, IT IS NOT KNOWN WHY THE ENGINE BYPA SSED FUEL. THE TEMP LIMITER WAS DEFERRED BY MEL 77-1-3 WHICH DISABLES THE BYPASS FROM THE FUEL SYSTEM. 2 L 7 2 4T RT A8SW 1999123100331 19991231 00331 CE 1999 12 31 99ZZZX4682 1 19991106 A 3260 358250944 PLUNGER BEECH 58 58 1152740 CE NLG BROKEN A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 858LG TH518 CMH - NO NOSE GEAR DOWN AND LOCK LIGHT COMING INTO CMH. FOUND FORK END ON PLUNGER ASSY BROKEN. REMOVED AND REPLACED PL UNGER ASSY. OPS CHECKED GOOD. 1 L 7 2 3O 3A16 1999123100332 19991231 00332 SO 1999 12 31 99ZZZX4683 1 19991103 A 3260 SWITCH PIPER PA31 PA31350 7103110 SO RT MLG DIRTY A BSYA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 07 35551 318052063 AGC - RT MAIN GEAR DOWN AND LOCK LIGHT INTERMITTENT. JACKED AIRCRAFT, CYCLED GEAR, COULD NOT DUPLICATE. CLEANED AND LU BED SWITCH, CYCLED GEAR AGAIN. OPS CHECKED GOOD. 1 L 7 2 3O A20SO 1999123100335 19991231 00335 NE 1999 12 31 99ZZZX4686 2 19991126 A 7200 ENGINE DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE RIGHT MALFUNCTIONED A VLLA K NONE O OTHER IN INSP/MAINT 1 GL 05 932H 17800 805 34368 351666 EN ROUTE FROM MWO/BAK - RIGHT ENGINE OIL TEMP AND OIL PRESSURE WENT TO RED LINE. RETURNED TO GWO. SUSPECT MASTER ROD H EAVILY FAILURE. 2 L 7 2 4R 4 R A669 5E4 1999123100342 19991231 00342 EU 1999 12 31 GXPA99009 1 19991205 A 2810 350012A FUEL CAP AMD FALC20 FALCON 2720302 EU RIGHT WING MISSING A GXPA O OTHER O OTHER NR NOT REPORTED 1 GL 23 175GA 45 DEPARTED OMA AND DETERMINED RIGHT FUEL CAP CAME OFF. RETURNED TO OMA AND REPLACED CAP WITH SERVICEABLE ONE. (X) 2 L 7 2 4F A7EU 1999123100350 19991231 00350 EA 1999 12 31 99ZZZX4700 2 19991001 A 7532 310082903 BLEED VALVE BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA COMPRESSOR LEAKING A TIMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 99TH B0084 U155 PCE40522 ENGINE TEMPERATURE, N1 HIGH, TORQUE LOW, AND FUEL FLOW HIGH. INSPECTED FIRST STAGE COMPRESSOR SECTION BLADES FOR DAMAGE AND P3 LINES FOR CHAFED SECTIONS AND LOOSE FITTINGS. REPLACED BLEED VALVE FOR TROUBLESHOOTING PURPOSES. ALL ELSE CHECK ED GOOD. PERFORMED JET-CAL ON ALL ENGINE INSTRUMENTS AND PERFORMED DPS RUN BEFORE AND AFTER WORK PERFORMED. POST-DPS R UN NUMBERS CHECKED GOOD. SUBMITTER STATED IT WAS NOT DETERMINED WHAT CAUSED BLEED VALVE TO MALFUNCTION. 1 L 7 2 3T 4 T A14CE E4EA 1999123100353 19991231 00353 CE 1999 12 31 99ZZZX4703 1 19991013 A 5751 991300003 SKIN BEECH 99 99 1154002 CE RT AILERON CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 14MV U59 INSPECTION REVEALED TOP SIDE SKIN OF RIGHT AILERON CRACKED. REPLACED AILERON WITH SERVICEABLE AILERON WHILE ORIGINAL IS REPAIRED. SUBMITTER STATED IT APPEARED THE CRACK MAY HAVE BEEN THE RESULT OF AN IMPROPERLY INSTALLED OR SECURED EXISTI NG SURFACE DOUBLER. BEECHCRAFT RECOMMENDED THE APPLICATION OF SURFACE STRUCTURAL EPOXY WHEN APPLYING DOUBLERS TO AILERO NS (EA 9309). 1 L 7 2 3T A14CE 1999123100358 19991231 00358 EU 1999 12 31 AWXA9900494 1 19991227 A 2120 0MP25052 FITTING AIRBUS 320 A320231 3930325 EU AIR DISTRIBUTION LEAKING A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 640AW 448 DURING CLIMBOUT NOTICED VERY STRONG DIRTY SOCKS ODOR IN COCKPIT. REMOVED AND REPLACED LEAKING SERVICE OVERFLOW FITTING, WASHED OIL FROM APU INLET AND AIRCRAFT INLET. 2 L 7 2 4F RT A28NM 1999123100359 19991231 00359 NM 1999 12 31 AWXA9900495 1 19991227 A 2150 6450552 FAN MOTOR BOEING 737 73733A 1384673 NM COOLING FAILED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 166AW 23627 FLT ATTENDANTS REPORT STRONG ODOR FROM AIR CONDITIONING. ISOLATED PROBLEM TO NORMAL EQUIPMENT COOLING EXHAUST FAN MOTOR BAD (VIBRATES EXCESSIVELY). PLACED ON MEL. 2 L 7 2 4F RT A16WE 1999123100360 19991231 00360 1999 12 31 AWXA9900496 4 19991227 A 2565 D30665105 SLIDE AIRBUS 320 A320231 3930325 EU PAX DOOR DEPLOYED A AWXA O OTHER O OTHER NR NOT REPORTED 1 WP 28 632AW 13534 1002 81 DOOR L-2 SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED L-2 DOOR SLIDE. 2 L 7 2 4F RT A28NM 1999123100361 19991231 00361 NM 1999 12 31 AWXA9900498 1 19991227 A 3350 864705 POWER SUPPLY BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22647 LEFT AND RIGHT FWD EMERGENCY EXIT DOOR LIGHTS AND CEILING LIGHT STARTED FLASHING AFTER 1 MINUTE. REPLACED FWD BATTERY P ACK AND POWER SUPPLY, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999123100362 19991231 00362 NM 1999 12 31 AWXA9900499 1 19991227 A 5315 654681143 FLOORBEAM BOEING 737 73733A 1384673 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509AW 23636 FLOORBEAM FS 986.5 LBL 0 TO LBL 54 CORRODED OUT OF LIMITS. REMOVED DAMAGE FROM FLOORBEAM, FABRICATED REPLACEMENT OF BAC 1505-100617 R69033 AND 2 REPAIR STRAPS 7075 T6 QQA250/13 .063 R208344 AND .071 R698634 IAW 737 SRM 53-00-51 FIG 202. I NSTALLED BEAM REPAIR IAW 737 SRM 53-00-51 FIG 202. 2 L 7 2 4F RT A16WE 1999123100363 19991231 00363 NM 1999 12 31 CALA9901738 1 19991229 A 3350 BATTERY PACK BOEING 727 727243 138408D NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE IN CABIN AND AT OVERWING EXITS, BOTH SIDES. MAINTENANCE REPLACED A BAD FUSE. THE BATTERY PACKS WERE REMOVED, RECHARGED, AND REINSTALLED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-01, PAGE 201. 2 L 7 3 4F RT A3WE 1999123100364 19991231 00364 WP 1999 12 31 MWEA99915 1 19991228 A 3350 6011777 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 400ME 45727 RIGHT AFT NACELLE LIGHT INOP IN EMERGENCY MODE. MAINTENANCE REPLACED NACELLE LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1999123100365 19991231 00365 1999 12 31 MWEA99916 4 19991229 A 2565 113317 SLIDE COVER DOUG MD88 MD88 3023688 NM GALLEY DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FORWARD ENTRY DOOR SLIDE COVER CAME OFF. MTC REINSTALLED ENTRY DOOR SLIDE COVER AS REQUIRED. 2 L 7 2 4F RT A6WE 1999123100366 19991231 00366 WP 1999 12 31 MWEA99917 1 19991221 A 3350 1315 BULB DOUG DC9 DC932 3022066 WP CABIN FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 AFT OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MTC RELAMPED AFT OVERHEAD EMERGENCY EXIT LIGHT. 2 L 7 2 4F A6WE 1999123100367 19991231 00367 WP 1999 12 31 MWEA99918 1 19991229 A 5753 99576003 RETAINER DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FOUND LEFT FLAP OUTBOARD HINGE RETAINERS (2 EACH) WERE CRACKED INSIDE OF FLAP. MAINTENANCE FITTED AND INSTALLED NEW RET AINERS. 2 L 7 2 4F A6WE 1999123100368 19991231 00368 WP 1999 12 31 MWEA99919 1 19991229 A 5230 59101419 ANGLE DOUG DC9 DC932 3022066 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD CARGO DOOR HAD GOUGE ON INNER PAN NEAR AFT LOCKING TORQUE TUBE. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANG LE. 2 L 7 2 4F A6WE 1999123100369 19991231 00369 NM 1999 12 31 DLM11992799 1 19991220 A 2120 UNKNOWN DOUG MD11 MD11 3023602 NM CABIN SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 804DE 48475 CREW REPORTED SMOKE IN CABIN AND TRACES OF SMOKE IN COCKPIT. CREW TURNED OFF CABIN BUS AND DIVERTED TO RDU. INSPECTED AIRCRAFT, CLEANED DUCTS AND NO TROUBLE FOUND. 2 L 7 3 4F RT A22WE 1999123100370 19991231 00370 NE 1999 12 31 DL73K992800 2 19991220 A 7230 795722 SEAL BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE SEPARATED A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 302DL 23047 717159 NR 1 ENG HAD MULTIPLE COMPRESSOR STALLS AT FL310 AS THROTTLES RETARDED FROM CLIMB EPR TO CRUISE EPR OF 1.96. COMPRESSOR STALLS STOPPED AS THROTTLES WERE PULLED TO IDLE THE ENG WAS NOT SHUTDOWN AND OPERATED NORMALLY AT IDLE. REPLACED C2 FA N FOR SEAL LIBERATION. 2 L 7 2 4F 4 F RT A16WE E2EA 1999123100371 19991231 00371 NM 1999 12 31 DL72S992803 1 19991221 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 680 - 740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS. INTERNAL MFEC INSPE CTION OF THE 4R LAP SPLICE BETWEEN FS 680 & 740 CONFIRMED 7 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN ALONG T HE LENGTH OF THE PANEL. THE SKIN LAP WAS CUT OUT OVER THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER P ER ER/A 368980-14AD. 2 L 7 3 4F A3WE 1999123100372 19991231 00372 NM 1999 12 31 DL72S992804 1 19991221 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 360 - 480 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS IN THE LOWER SKIN OF THE LOWER FASTENER ROW. INTERNAL MFEC INSPECTION OF THE SKIN PANEL BETWEEN FS 360 & 480 CONFIRMED A TOTAL OF 4 CRACKS I N ALONG THE SKIN LENGTH. THE ENTIRE LAP JOINT WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 36897 9-14AD. 2 L 7 3 4F A3WE 1999123100373 19991231 00373 NM 1999 12 31 DL72S992805 1 19991221 A 5330 65545672 SKIN BOEING 727 727232 1384082 NM BS 480 - 680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION OF THE SKIN PANEL BETWEEN FS 480 & 680 CONFIRMED CRACKS IN CONSECUTIVE FRAME BAYS. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 368977-14AD. 2 L 7 3 4F A3WE 1999123100374 19991231 00374 NM 1999 12 31 DL72L992806 1 19991214 A 5311 651766445 FRAME BOEING 727 727232 1384082 NM BS 580,600 & 660 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 FRAMES DAMAGED AT STA 580, 600, 660 AND 700 AT STRINGER 22L. NEW SECTIONS BEING SPLICED IN ER/A 333911-14 REV A. 2 L 7 3 4F A3WE 1999123100375 19991231 00375 NM 1999 12 31 DL76S992807 1 19991216 A 5311 143T35214 FRAME BOEING 767 767332 1382001 NM BS 615 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 EXISTING REPAIR REMOVED AT C-1 DOORWAY AFT EDGE. REVEALING DAMAGE TO SKIN BEARSTRAP AND FRAME OUTER CHORD. DAMAGE LOCA TED BETWEEN STR-31R AND 32R AT STA 615. SKIN AND BEARSTRAP WERE GOUGED, CUTOUT AND THE FRAME WAS DENTED. ER/A 333883-1 4 REV A. 2 L 7 2 4F RT A1NM 1999123100376 19991231 00376 NM 1999 12 31 DL72S992808 1 19991208 A 5230 BRACKET BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 C2 DOOR (S/N 634) HAD 2 BRACKETS BROKEN, ROD BENT, WEB DAMAGED AT LIGHTNING HOLE. REPAIRED PER SRM 52-30-20, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999123100377 19991231 00377 NM 1999 12 31 DLM88992809 1 19991221 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 49543 EMERGENCY LIGHTS INOP IN COCKPIT OVER ENTRY DOOR AND UNDER GLARESHIELD. REPLACED BATTERIES IN BATTERY PACK, CKS GOOD. 2 L 7 2 4F RT A6WE 1999123100378 19991231 00378 NM 1999 12 31 DL73K992810 1 19991217 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 HFEC INSP OF FWD GALLEY DOOR CUT OUT LOWER AFT CORNER REVEALS .125 INCH LONG CRACK AT 2 FASTENER LOCATIONS. ROUTED OUT DAMAGED AREA PER SRM 53-30-3. HFEC INSP ROUTED AREA NO INDICATIONS. FABRICATED DOUBLER DRILLED UP DOUBLER AND INSTALLE D DOUBLER PER SRM 53-30-3. 2 L 7 2 4F A16WE 1999123100379 19991231 00379 NM 1999 12 31 DL72L992812 1 19991207 A 5753 TRACK 651626920 BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 2520 21314 DURING OVERHAUL THE I/B FLAP, I/B TRACK ASSY (P/N 65-19270-12) CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PA D AREAS AND WEAR WAS FOUND AT THE FWD ATTACH LUGS AND THE MLG DOOR HINGE FITTING ATTACH HOLES AND THE TOGGLE DETENT HO LE. SUBJECT PART WAS REPAIRED PER BFG ER 23-0511. 2 L 7 3 4F A3WE 1999123100380 19991231 00380 NM 1999 12 31 DL72L992813 1 19991207 A 5753 TRACK 651926918 BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 1468 21314 DURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY, (P/N 65-19269-18), CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTA CH PAD AREAS AND WEAR AT THE FWD ATTACH LUG. PART WAS REPAIRED PER ER/A 372298-14AD REVISION B. 2 L 7 3 4F A3WE 1999123100381 19991231 00381 1999 12 31 DL738992814 4 19991222 A 2562 TETHER BOEING 737 737832 13844CF NM RADIO BEACON FRAYED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 371DA 038C1751 29619 TETHER LINE ON RADIO BEACON FRAYED, POSSIBLY TORN OR BROKE. REMOVED AND REPLACED ELT. 2 L 7 2 4F RT A16WE 1999123100382 19991231 00382 NM 1999 12 31 DL72K992815 1 19991222 A 3260 324001046 ACCESSORY UNIT BOEING 727 727232 1384082 NM NLG MALFUNCITONED A DALA A UNSCHED LANDING N FALSE WARNING LD LANDING 1 SO 27 415DA R00696 21257 AFTER GEAR EXT, NOSE GEAR GREEN DOWN AND LOCK FAILED TO ILLUM. DIVERTED INTO JFK. REPLACED LANDING GEAR ACCESSORY UNIT. 2 L 7 3 4F A3WE 1999123100383 19991231 00383 NM 1999 12 31 DL72S992816 1 19991222 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 STR 18A CRACKED AT STA 940 AFT SIDE OF RADIUS BLOCK AT AFT LOWER BOLT. REPAIRED PER M/M 53-12-0 PG 816, LEVEL II TIME LIMITED REPAIR. 2 L 7 3 4F A3WE 1999123100384 19991231 00384 NM 1999 12 31 DL72S992817 1 19991222 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 NR 2 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED STIFFENER PER M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1999123100385 19991231 00385 NM 1999 12 31 DL757992818 1 19991217 A 5754 RIB 114N4002148 BOEING 757 757232 1384965 NM LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 674DL A20529 25979 DURING B757 L/E SLAT T/E WEDGE CHANGE PER EO 6-74595-3AD, THE NR 10 L/E SLAT I/B END RIB HAD ONE HOLE OVERSIZED IN THE I /B END RIB AT OSS 707. PER ER/A 387211-14AD THE SUBJECT PART WAS REPAIRED BY OVERSIZING THE DISCREPANT HOLE TO ACCOMODA TE A .25 DIA BLIND BOLT. 2 L 7 2 4F RT A2NM 1999123100386 19991231 00386 NM 1999 12 31 DL72S992822 1 19991221 A 5311 FRAME BOEING 727 727232 1384082 NM BS 560 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 THE FWD JAMB FRAME OF THE C1 DOOR CUTOUT FS 560 WAS FOUND WITH A 1 INCH CRACK IN THE FRAME WEB JUST BELOW THE NR 6 DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A DOUBLER PER ER/A 368895-14AD. 2 L 7 3 4F A3WE 1999123100387 19991231 00387 NM 1999 12 31 DL72S992823 1 19991222 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 294.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 THE FS 294.5 FLOORBEAM WEB AT LBL 40 WAS FOUND WITH A 7 INCH LONG CRACK RUNNING FROM A CABLE PASS THROUGH HOLE TO THE LOWER EDGE OF THE WEB AND THROUGH THE LOWER CHORD. THE LOWER CHORD WAS REPLACED. THE DAMAGED SECTION OF WEB WAS REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 368915-14, REV A. 2 L 7 3 4F A3WE 1999123100388 19991231 00388 NM 1999 12 31 DLM88992824 1 19991223 A 2530 OVEN 50459 DOUG MD88 MD88 3023688 NM GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 974DL 15 53242 FWD GALLEY OVEN BEGAN TO SMOKE AND EMIT AUDIBLE CRACKLE AFTER T/O. CONTINUED WITH C/B PULLED AND GALLEY POWER OFF. REP LACED OVEN. 2 L 7 2 4F RT A6WE 1999123100389 19991231 00389 NE 1999 12 31 DLM88992825 2 19991224 A 7261 FILTER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE CONTAMINATED A DALA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 27 967DL 21852 53116 726021 ON DESCENT INTO GRR, GOT LEFT ENG OIL STRAINER CLOG MSG. PERFORMED POM PROCEDURES, LIGHT DID NOT EXTINGUISH. PERFORMED POM PROCEDURES AND SHUT LEFT ENG DOWN AND DECLARED EMERGENCY. FOUND CARBON IN FILTER. REPLACED AND PERFORMED ENGINE R UN-UP, NO ADDITIONAL CARBON FOUND. 2 L 7 2 4F 4 F RT A6WE E9NE 1999123100390 19991231 00390 NM 1999 12 31 DL733992827 1 19991224 A 3246 BEARING B737M BOEING 737 737347 1384647 NM MLG WHEEL WRONG PART A DALA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 SO 27 305WA DL4081 23346 ON TAKEOFF, NR 3 MAIN WHEEL ASSY DEPARTED A/C. FOUND WRONG INNER BEARING INSTALLED IN THE WHEEL ASSEMBLY. REPLACED WHE EL AND AXLE. 2 L 7 2 4F RT A16WE 1999123100391 19991231 00391 NM 1999 12 31 DLM88992829 1 19991224 A 3234 HANDLE DOUG MD88 MD88 3023688 NM MLG OUT OF RIG A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 928DL 49715 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT COME UP. ADJUSTED TURNBUCKLE ON GEAR HANDLE RELEASE CABLE. SERVICED STRUT S. 2 L 7 2 4F RT A6WE 1999123100392 19991231 00392 NM 1999 12 31 DLM88992830 1 19991224 A 3222 STRUT 5920629 DOUG MD88 MD88 3023688 NM NLG DISCHARGED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 979DL 53266 AFTER TAKEOFF WHEN GEAR HANDLE RAISED, NLG WOULD NOT RETRACT. AUTO SPLR FAIL, STALL IND FAIL, NO ACARS OFF TIMES. SERV ICED NOSE STRUT. 2 L 7 2 4F RT A6WE 1999123100393 19991231 00393 NM 1999 12 31 DLM88992831 1 19991226 A 2910 LINE AS15308K025 DOUG MD88 MD88 3023688 NM HYDRAULIC SYS RUPTURED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 986DL 53313 APPROXIMATELY 30 MINUTES BEFORE ARRIVING ATL, THE RIGHT HYD SYSTEM DECREASED TO 3 QUARTS AND ZERO HYD PRESS FOLLOWED BY APU SHUTDOWN. RAN THE EMERG PROCEDURES IAW POM. UPON GEAR EXTEND THE GEAR WENT DOWN BUT THE GEAR DOORS DID NOT C OME BACK UP. REPLACED RUPTURED FLEX LINE AT CASE DRAIN FILTER. 2 L 7 2 4F RT A6WE 1999123100394 19991231 00394 1999 12 31 DL767992832 4 19991217 A 2565 BATTERY 900835A BOEING 767 767232 1385132 NM SLIDE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 108DL 7866 22220 DURING SQUIB TEST, LT ESCQPE SLIDE DID NOT ILL WHILE PRESSING TEST 1 AND RT ESCAPE SLIDE DID NOT ILL WHILE PRESSING TEST 2. REPLACED LT OVERWING SLIDE POWER SUPPLY AND BATTERY. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1999123100395 19991231 00395 NM 1999 12 31 DL76G992833 1 19991226 A 2120 UNKNOWN BOEING 767 767332 1382001 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 16065 30199 BURNING OR SMOKE ODOR IN REAR CABIN ON LANDING (DIFFERENT FROM BOMBAY SMOKE ODOR). DISSIPATED BY THE TIME A/C ARRIVED A T GATE. CHECKED AREA, NO EVIDENCE OF SMOKE OR BURNING. 2 L 7 2 4F RT A1NM 1999123100396 19991231 00396 NE 1999 12 31 DLM11992835 2 19991227 A 7200 PW44603 ENGINE 7911006084 DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 UNRESPONSIVE A DALA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 SO 27 813DE 40000806 48600 723875 NR 3 ENGINE APPEARED TO FLAME-OUT DURING DESCENT. DID NOT RESPOND WHEN PWR INCREASE. CREW SHUTDOWN ENG. REPLACED EEC . 2 L 7 3 4F 4 F RT A22WE E24NE 1999123100397 19991231 00397 NM 1999 12 31 DL72E992837 1 19991103 A 5754 652163362 SKIN BOEING 727 727247 138408F NM LE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 DURING SHOP INSPECTION, THE LOWER L/E SKIN WAS FOUND WORN APPROX 1 INCH LENGTH AT THE O/B END OF THE FLAP. THE L/E W AS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1999123100398 19991231 00398 NM 1999 12 31 DL757992838 1 19991227 A 2622 892480 EXTINGUISHER BOEING 757 757232 1384965 NM CABIN LEAKING A DALA O OTHER O OTHER CR CRUISE 1 SO 27 671DN 25332 FWD H2O EXTINGUISHER USED, SEAL BROKEN. FOUND SEAL BROKEN ON H2O EXTINGUISHER AND EXTINGUISHER LEAKING. BOTTLE WAS NOT USED. REPLACED H2O EXTINGUISHER. (P/N 267701883) (S/N DL2591) OFF, (S/N DL2207). 2 L 7 2 4F RT A2NM 1999123100399 19991231 00399 WP 1999 12 31 DLL19992839 1 19991227 A 2821 KB27161 O-RING LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 2 ENGINE CUT A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 768DL 193H1216 014623 ON WALKAROUND, FOUND FUEL LEAKING FROM NR 2 ENG FUEL FILTER BOWL. REPLACED ONE HELI-COIL AND O-RING ON FUEL FILTER ASSY . 2 L 7 3 4F 4 F A23WE E12EU 1999123100400 19991231 00400 NM 1999 12 31 DL72S992840 1 19991227 A 5230 BEAM 655692711 BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 51 22047 B727 AFT CARGO DOOR, NR 5 PRESSURE STOP BEAM WAS FOUND DAMAGED. THE OUTER T-CHORD OF THE STOP BEAM WAS FOUND CRACKED AT ATA 1095. REPAIRED PER ER/A 372942-14AD. 2 L 7 3 4F A3WE 1999123100401 19991231 00401 NM 1999 12 31 DLM88992841 1 19991228 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM TAIL SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 912DL 49543 ON SHORT FINAL WITH ENG AND AIRFOIL ANTI ICE ON, A BURNING SMELL WAS NOTICED THRU OUT A/C. SMOKE DETECTOR IN AFT LT L AV WENT OFF. F/A CHECKED LAV AND TRASH BIN, ALL WAS NORMAL. PERFORMED DUCT BURNOUT AND PNEU SYS CK OUT PER M/M, OPS NO RMAL. NO SMELL NOTED. 2 L 7 2 4F RT A6WE 1999123100402 19991231 00402 NM 1999 12 31 DLM88992842 1 19991228 A 3397 WIRE RPS1 DOUG MD88 MD88 3023688 NM ROW 24 - 30 BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 978DL 5616 53259 EMERGENCY LIGHTS INOP BETWEEN ROWS 24-30. REPAIRED WIRES BROKEN AT WALL SPLICE AND REPLACED BAD PWR SUPPLY LIGHTS, NOW CK GOOD. 2 L 7 2 4F RT A6WE 1999123100403 19991231 00403 NM 1999 12 31 SCNA99157 1 19991228 A 3350 106178316 BATTERY PACK 10617842 BOEING 727 7272M7 138407S NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 294SC T4088 21202 DURING A LINE MAINTENANCE CHECK, THE CENTER AISLE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. FOUND LIGHT ASSEMBLY INOPERA TIVE AND BATTERY PACK INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AND BATTERY PACK, OPERATIONALLY CHECKS GOOD IAW 335001. 2 L 7 3 4F A3WE 1999123100404 19991231 00404 1999 12 31 RAIA9912035 4 19991228 A 2300 CAU2583 RCAU AEROSP ATR42 ATR42300 8680920 EU AVIONICS RACK FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 423TE 1092 4 119 7108-STL- CAPTAINS AUDIO CUT OUT DURING TAXI. MAINTENANCE REPLACED REMOTE AUDIO UNIT. 2 H 7 2 4T RT A53EU 1999123100405 19991231 00405 WP 1999 12 31 AALA991715 1 19991114 A 2530 2510000308 OVEN DOUG DC9 DC982 3022082 WP GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 450AA 49476 IAD - FLT 775 - AFTER TAKEOFF FROM DCA, COCKPIT AND CABIN FILLED WITH SMOKE. DIVERTED AND LANDED IAD WITHOUT INCIDENT. REPLACED OVEN IN FIRST CLASS GALLEY. RAN APU AND ENGINE WITH BOTH PACKS IN FULL OPERATION. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100406 19991231 00406 WP 1999 12 31 AALA991721 1 19991115 A 4910 5940405503 APU DOUG DC9 DC982 3022082 WP TAIL LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 434AA 49452 DFW - FLT 1837 - ON CLIMB-OUT FROM DFW, THE CABIN FILLED WITH WHITE SMOKE AND AN ACRID SMELL. AIR INTERRUPTED AND RETUR NED TO DFW. ON DESCENT, THE SMOKE CLEARED AND THE SMELL DECREASED. LANDED DFW WITHOUT INCIDENT. REPLACED AUXILLARY PO WER UNIT. REPLACED COALESCER BAGS AND ACOMPLISHED PACK BURNOUT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100407 19991231 00407 NM 1999 12 31 AALA991795 1 19991125 A 3310 342648 LIGHT GRIMES BOEING 767 767323 1385205 NM COCKPIT FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 369AA 25196 LHR - FLT 100 - EN ROUTE JFK-LHR, FIRST OFFICERS GRIMES UTILITY LIGHT SHORTS OUT AND CAUSED SPARKS WHEN TOUCHED TO A MET AL OBJECT. POPPED UTILITY P31 CIRCUIT BREAKER ON OVERHEAD PANEL. REPLACED FIRST OFFICERS GRIMES UTILITY LIGHT. GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999123100408 19991231 00408 NM 1999 12 31 AALA991748 1 19991120 A 3350 0201820001 LIGHT BOEING 767 767223 1385123 NM SEAT 30B INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325AA 22326 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLIGHT AT SEAT 30B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEA T 30B. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999123100409 19991231 00409 NM 1999 12 31 AALA991749 1 19991119 A 3350 0201820001 LIGHT BOEING 767 767323 1385205 NM SEAT 34H INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34H INOPERATIVE. REPAIRED WIRING AT EMERGENCY EXIT LIG HT AT SEAT 34H. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999123100410 19991231 00410 1999 12 31 AALA991696 4 19991108 A 2565 106622318 GIRT BAR BFGOODRICH BOEING 767 767223 1385123 NM PAX DOOR BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA BBCNHSZ 22316 SFO - DURING OVERNIGHT MAINTENANCE, RIGHT SLIDE PACK RELEASE BAR BRACKETS BROKEN. REPLACED RIGHT SLIDE PACK. SYSTEM GR OUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999123100411 19991231 00411 WP 1999 12 31 AALA991752 1 19991119 A 2133 ACTUATOR DOUG DC9 DC982 3022082 WP OUTFLOW VALVE FAILED A AALA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 07 445AA 49471 DFW - FLT 701 - EN ROUTE LGA-DFW, JUST PRIOR TO DESCENT OUT OF 35,000 FT CABIN WARNIGN CAME ON AT 9500 FEET CABIN ALTITU DE. DESCENDED TO 24,000 FT AND CABIN ALTITUDE WENT TO 14,000 FT AND PASSENGER OXYGEN MASKS DEPLOYED. AFTER SWITCHING T O STANDBY CONTROLLER, PRESSURE STARTED TO DESCEND SLOWLY. CONTINUED TO DEPRESSURIZE TO LANDING. NO RED WARNING CABIN A LTITUDE MASTER CAUTION LIGHT ILLUMINATED. PACK FLOW INDICATION NORMAL. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED OUT FLOW VALVE ACTUATOR ASSEMBLY AND BOTH CABIN PRESSURE CONTROLLERS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100412 19991231 00412 WP 1999 12 31 AALA991768 1 19991123 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7512A 49806 PHX - FLT 2084 - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED CONNE CTOR FOR FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100414 19991231 00414 WP 1999 12 31 AALA991775 1 19991123 A 3350 LIGHT GRIMES DOUG DC9 DC982 3022082 WP SEAT 11D MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 458AA 49563 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 11D MISSING. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 11D. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100415 19991231 00415 WP 1999 12 31 AALA991799 1 19991126 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 237AA 49523 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT IN AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100416 19991231 00416 WP 1999 12 31 AALA991801 1 19991126 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 20D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7518A 49895 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 20D INOPERATIVE. REPLACED EMERGENCY EXIT FLO OR PATH LIGHT STRIP AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100417 19991231 00417 WP 1999 12 31 AALA991802 1 19991126 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7518A 49895 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT FROM FRONT ENTRY TO FIRST CLASS INOPERATIVE. REPLAC ED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR FOR FRONT ENTRY TO FIRST CLASS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100418 19991231 00418 WP 1999 12 31 AALA991769 1 19991123 A 2430 6RW176YN3 RECTIFIER DOUG DC9 DC982 3022082 WP E/E BAY FAILED A AALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 07 285AA 49297 ORD - FLT 2378 - EN ROUTE DFW-ORD, NUMBER ONE LOAD INDICATOR READ ZERO LOAD AND NUMBER TWO LOAD INDICATOR READ .8 LOAD. BURNING SMELL NOTED AND DC BUS TIE WAS CLOSED. SMELL DISSIPATED AND K1 CIRCUIT BREAKER WAS POPPED. REPLACED NUMBER 1 TRANSFORMER RECTIFIER. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100419 19991231 00419 WP 1999 12 31 AALA991797 1 19991125 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7518A 49895 SAN - FLT 310 - AFTR TAKEOFF, ON INITIAL CLIMB-OUT STRONG ELECTRICAL FUMES IN AFT CABIN. AIRCRAFT RETURNED TO SAN AND L ANDED WITHOUT FURTHER INCIDENT. NO DISCREPANCIES FOUND. REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100420 19991231 00420 WP 1999 12 31 AALA991813 1 19991128 A 2120 UNKNOWN DOUG DC9 DC982 3022082 WP CABIN ODOR A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 70524 49916 ORD - FLT 1387 - DURING TAXI, ODOR OF OVERHEATED ELECTRICAL CIRCUITS REPORTED. RETURNED TO GATE ORD. ODOR CONTINUED AN D MAINTENANCE VERIFIED ODOR. AFTER EXTENSIVE INSPECTION AND CLEANING NO ODORS WERE NOTED. COULD NOT DUPLICATE ODOR. S YSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999123100421 19991231 00421 WP 1999 12 31 AALA991803 1 19991126 A 2170 1808492 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 432AA 49350 DFW - FLT 1488 - AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED WHITE VAPOR OR FOG IN CABIN. AIRCRAFT RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED COALESCER BAGS AND PERFORMED PACK BURNOUT. AFTER BURNOUT WAS ACCOMPLISHED. PACKS WERE OPE RATED WITH NO LEAKS, ODOR, OR SMOKE NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1999123100422 19991231 00422 EU 1999 12 31 SIMA993131 1 19991109 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 269AT 11719 269 SAW - DURING PS-1 INSPECTION, FOUND SEVERAL FLOOR PROXIMITY LIGHT BULBS DID NOT ILLUMINATE. REMOVED AND REPLACED THE EM ERGENCY LIGHT BATTERY PACK AT LOCATION 3WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100423 19991231 00423 EU 1999 12 31 SIMA993151 1 19991111 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 283AE 340B283 DFW - FLT 3366 - FLOOR PROXIMITY LIGHTS AT ROW 7BC AND 8A DO NOT ILLUMINATE. FOUND BLOWN FUSE 73WL AND WIRE LN131-22N S HORTED TO GROUND. REINSULATED WIRE AND REMOVED AND REPLACED FUSE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 1999123100424 19991231 00424 EU 1999 12 31 SIMA993002 1 19991027 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 16057 045 SAW - DURING PS-2 INSPECTION, FOUND THE EMERGENCY FLOOR PROXIMITY LIGHTS BETWEEN SEATS 1AB AND 5AB DID NOT ILLUMINATE. R EMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS AT LOCATION 3WL AND 29WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100425 19991231 00425 EU 1999 12 31 99ZZZM809 1 19991027 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 16630 045 SAW - DURING PS-2 INSPECTION, FOUND THE EMERGENCY FLOOR PROXIMITY LIGHTS BETWEEN SEATS 1AB AND 5AB DID NOT ILLUMINATE. R EMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS AT LOCATION 3WL AND 29WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100426 19991231 00426 EU 1999 12 31 SIMA993143 1 19991110 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 431AT 1324 431 DFW - FLT 3505 - FROM ROW TWELVE FORWARD, EVERY OTHER EMERGENCY FLOOR PROXIMITY LIGHT AND TWO CENTER EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACK ABOVE SEAT 5AB. OPERATIONAL CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100427 19991231 00427 EU 1999 12 31 SIMA993142 1 19991110 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 1160 540 DFW - FLT 3724 - SEVERAL RANDOM EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED ONE EMERGENCY POWER SUPPL Y BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100428 19991231 00428 EU 1999 12 31 SIMA993281 1 19991124 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 238AE 340B238 DFW - FLT 3285 - SEVEN EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BULBS FOR FLOOR PROXIMI TY LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100429 19991231 00429 EU 1999 12 31 SIMA993282 1 19991124 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343SB 340B343 TWO EMERGENCY FLOOR LIGHTS AT SEAT 7BC DO NOT ILLUMINATE. REMOVED AND REPLACED BULBS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999123100430 19991231 00430 EU 1999 12 31 SIMA993291 1 19991125 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 191AE 9102 340B191 DFW - FLT 3906 - LAVATORY SMOKE WARNING LIGHT COMES ON INTERMITTENTLY. VERIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100431 19991231 00431 EU 1999 12 31 SIMA993292 1 19991125 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 241AE 340B241 JFK - FLT 5024 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROW 3, 5 AND 11 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999123100432 19991231 00432 EU 1999 12 31 SIMA993293 1 19991125 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 339SB 340B339 LAX - FLIGHT ATTENDANTS EMERGENCY LIGHT 'ARMED' INDICATOR DOES NOT ILLUMINATE. REMOVED AND REPLACED ARM LIGHT BULB. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100433 19991231 00433 EU 1999 12 31 SIMA993294 1 19991125 A 3350 3011180 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AE 17786 243 MIA - FLT 5278 - SEVERAL EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED ONE EMERGENCY BATTERY PACK AND REPAIR ED TWO FLOOR PROXIMITY TRACK LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100434 19991231 00434 EU 1999 12 31 SIMA993311 1 19991127 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 244AE 340B244 DFW - FLT 3554 - FLIGHT ATTENDANTS EMERGENCY LIGHT 'ARMED' INDICATOR DOES NOT ILLUMINATE. REMOVED AND REPLACED ARM LIGH T BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100435 19991231 00435 EU 1999 12 31 SIMA993342 1 19991130 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 317AE 340B317 LAX - FLT3034 - EMERGENCY LIGHT ABOVE SEAT 8 BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 1999123100436 19991231 00436 EU 1999 12 31 SIMA993343 1 19991130 A 3350 43741 SIGN SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 312AE 340B312 LAX - FLT 3200 - EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANTS SEAT IS LOOSE. RESECURED EXIT SIGN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100437 19991231 00437 EU 1999 12 31 SIMA993344 1 19991130 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 320AE 340B320 SAN - FLT 3023 - FLT ATTENDANTS EMERGENCY LIGHTS ARMED INDICATOR DOES NOT ILLUMINATE. REMOVED AND REPLACED ARM LIGHT BU LB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100438 19991231 00438 EU 1999 12 31 SIMA993261 1 19991122 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AE 18458 340B306 SAN - FLT 3003 - EMERGENCY FLOOR PROXIMITY LIGHTS FAIL INTERMITTENTLY. FERRIED AIRCRAFT TO LAX AND EMERGENCY POWER SUPP LIES WERE REPLACED AT LOCATIONS 21LN, 20LN, 22LN, 23LN AND 24LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100439 19991231 00439 EU 1999 12 31 99ZZZM810 1 19991122 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AE 18209 340B306 SAN - FLT 3003 - EMERGENCY FLOOR PROXIMITY LIGHTS FAIL INTERMITTENTLY. FERRIED AIRCRAFT TO LAX AND EMERGENCY POWER SUPP LIES WERE REPLACED AT LOCATIONS 21LN, 20LN, 22LN, 23LN AND 24LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100440 19991231 00440 EU 1999 12 31 99ZZZM811 1 19991122 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AE 19451 340B306 SAN - FLT 3003 - EMERGENCY FLOOR PROXIMITY LIGHTS FAIL INTERMITTENTLY. FERRIED AIRCRAFT TO LAX AND EMERGENCY POWER SUPP LIES WERE REPLACED AT LOCATIONS 21LN, 20LN, 22LN, 23LN AND 24LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100441 19991231 00441 EU 1999 12 31 99ZZZM812 1 19991122 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AE 11148 340B306 SAN - FLT 3003 - EMERGENCY FLOOR PROXIMITY LIGHTS FAIL INTERMITTENTLY. FERRIED AIRCRAFT TO LAX AND EMERGENCY POWER SUPP LIES WERE REPLACED AT LOCATIONS 21LN, 20LN, 22LN, 23LN AND 24LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100442 19991231 00442 EU 1999 12 31 99ZZZM813 1 19991122 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AE 340B306 SAN - FLT 3003 - EMERGENCY FLOOR PROXIMITY LIGHTS FAIL INTERMITTENTLY. FERRIED AIRCRAFT TO LAX AND EMERGENCY POWER SUPP LIES WERE REPLACED AT LOCATIONS 21LN, 20LN, 22LN, 23LN AND 24LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100443 19991231 00443 EU 1999 12 31 SIMA993271 1 19991123 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 306AE 340B306 LAX - FLT 3212 - FLOOR PROXIMITY LIGHT ADJACENT TO SEAT 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY LI GHT BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999123100444 19991231 00444 EU 1999 12 31 SIMA993272 1 19991123 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 244AE 340B244 DFW - FLT 3798 - EMERGENCY FLOOR PROXIMITY LIGHT ADJACENT TO SEAT 11A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999123100445 19991231 00445 EU 1999 12 31 SIMA993192 1 19991115 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 305AE 340B305 JFK - FLT 5064 - EMERGENCY LIGHTS ABOVE SEATS 5C, 7A, 8C AND 10C DO NOT ILLUMINATE. REMOVED AND REPLACED BULB AT SEAT 5 C. REMOVED AND REPLACED FUSE AT LOCATION 72 LN FOR LIGHTS 7A, 8C AND 10C. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100446 19991231 00446 EU 1999 12 31 99ZZZM814 1 19991115 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 305AE 340B305 JFK - FLT 5064 - EMERGENCY LIGHTS ABOVE SEATS 5C, 7A, 8C AND 10C DO NOT ILLUMINATE. REMOVED AND REPLACED BULB AT SEAT 5 C. REMOVED AND REPLACED FUSE AT LOCATION 72 LN FOR LIGHTS 7A, 8C AND 10C. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100447 19991231 00447 SO 1999 12 31 SIMA993263 1 19991122 A 2530 CBC16707 SOCKET EMB 145 EMB145LR SO GALLEY FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 616AE 145092 DFW - FLT 3663 - FLIGHT ATTENDANT REPORTS MILD BURNING ODOR IN THE GALLEY AREA. PULLED ALL THREE GALLEY CIRCUIT BREAKER S AND THE ODOR WENT AWAY. REMOVED AND REPLACED ONE AIRCRAFT SIDE HOT JUG SOCKET. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999123100448 19991231 00448 EU 1999 12 31 SIMA993141 1 19991110 A 3350 SM400D41 CONTACTOR AEROSP ATR72 ATR72212 EU STARTER/GEN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 260AE 263 MCO - EMERGENCY LIGHTS REMAIN ILLUMINATED WITH SWITCH IN THE ARM POSITION. REMOVED AND REPLACED NR 1 ENGINE START/GEN C ONTACTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100449 19991231 00449 EU 1999 12 31 SIMA993161 1 19991112 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AE 18590 340B232 RDU - FLT 5148 - ALL EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED ALL FIVE EMERGENCY POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100450 19991231 00450 EU 1999 12 31 99ZZZM815 1 19991112 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AE 19173 340B232 RDU - FLT 5148 - ALL EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED ALL FIVE EMERGENCY POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100451 19991231 00451 EU 1999 12 31 99ZZZM816 1 19991112 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AE 19481 340B232 RDU - FLT 5148 - ALL EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED ALL FIVE EMERGENCY POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100452 19991231 00452 EU 1999 12 31 99ZZZM817 1 19991112 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AE 17619 340B232 RDU - FLT 5148 - ALL EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED ALL FIVE EMERGENCY POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100453 19991231 00453 EU 1999 12 31 99ZZZM818 1 19991112 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AE 340B232 RDU - FLT 5148 - ALL EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED ALL FIVE EMERGENCY POWER SUPPLIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100454 19991231 00454 SO 1999 12 31 C2XA99CL125 1 19991122 A 3610 S2U2226 SEAL EMB 145 EMB145 SO CARGO BAY FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15941 145035 YUL - FLT 4005 - THE CREW REPORTED THAT DURING CLIMB THROUGH ICING CONDITIONS THE F/A HEARD A 'LOUD BANG' NE THE LAV ARE A, THE APU WAS ALREADY SHUTDOWN AND BLEED LEAK 1-2 WAS NOTED. BLEED LEAK 1 CLEARED AFTER ABOUT 1 MIN BLEED LEAK 2 REMAI NED. ENGINE NR 2 WAS SHUTDOWN PER THE QRH. THE AIRCRAFT LANDED BACK TO YUL UNDER WEIGHT AND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE O-RING ON GAMAH JOINT ON THE NR 2 BLEED DUCT BY THE RADIO ALTIMETER IN THE LOW AFT WING FAIRING IAW EMB145MM 36-11-09, LEAKS AND OPS CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999123100455 19991231 00455 EU 1999 12 31 C2XA99B1108 1 19991116 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 BTV - FLT 4371 - CREW REPORTED SEVERAL EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. MAINTENANCE REMOVED AND REPLACED EMER GENCY LIGHT POWER SUPPLY AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999123100456 19991231 00456 SO 1999 12 31 C2XA99BT106 1 19991117 A 3350 110049 POWER SUPPLY EMB 145 EMB145ER SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15948 145056 BTV - 3944 - DURING 2A INSPECTION MAINTENANCE, FOUND EMERGENCY LIGHTS OUT AT ROW 17 (OVERHEAD) AND SERVICE DOOR EXTERNAL . REMOVED AND REPLACED POWER SUPPLY. OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999123100457 19991231 00457 SO 1999 12 31 C2XA99BT105 1 19991118 A 3350 20131A POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 EWR - MAINTENANCE REPORTED LAST STRIP OF EMERGENCY LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED AFT EMEREGNCY LIGHT B ATTERY POWER SUPPLY. OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1999123100458 19991231 00458 SO 1999 12 31 C2XA99BT104 1 19991122 A 3320 BULB EMB 145 EMB145 SO CABIN FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 17928 145007 PIT - FLT 4299 - CREW REPORTED SMOKE FROM SIDEWALL LIGHT SEAT 4B, TROUBLESHOT AND FOUND BURNED BULB SOCKET AT 4D SIDEWAL L LIGHT, SYSTEM RELEASED UNDER MEL 32-20-00 CAT C CONTROL NUMBER 211401. AIRCRAFT RETURNED TO SERVICE. CLE, MAINTENANC E REMOVED AND REPLACED BULB AND LIGHT ASSY. OPS CHECKED LIGHTS GOOD. NO SMOKE NOTED. MEL REMOVED AND AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999123100459 19991231 00459 EU 1999 12 31 C2XA99IA593 1 19991115 A 5260 S52176404200 PANEL AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR STEP STRUCTURE FORWARD SIDE PANEL WAS FOUND TO BE CRACKED AT THE BOT TOM STEP. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED SIDE PANEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100460 19991231 00460 EU 1999 12 31 C2XA99IA594 1 19991115 A 3350 NSA937910EA2000 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY EXIT LIGHT ON PANEL 256CW WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAI RED THE CONNECTOR ON THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100461 19991231 00461 SO 1999 12 31 C2XA99IA591 1 19991114 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145 SO CARGO BAY DEFECTIVE A C2XA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14960 145100 IAH - DURING FLIGHT 3919, THE CRWE REPORTED THE LAVATORY AND BAGGAGE SMOKE WARNING ILLUMINATED AFTER TAKEOFF. THE CREW DISCHARGED THE BAGGAGE FIRE BOTTLES AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE CARGO SMOKE DETECTOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999123100462 19991231 00462 SO 1999 12 31 C2XA99IA590 1 19991112 A 2121 AE1711AA0 FAN EMB 120 EMB120RT SO GROUND COOLING FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 27716 120128 IAH - DURING FLT 3718 - THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT GROUND COOLING FAN TO HAVE A POOR ELECTRICAL CO NNECTION. MAINTENANCE CLEANED THE AFFECTED CONNECTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999123100463 19991231 00463 NE 1999 12 31 GAIA99228 2 19991127 A 7314 371900 FUEL PUMP DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A GAIA E A ENGINE SHUTDOWN UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 07 564PC 47062 665275 FLT 7302 - LRD-FWA - IN CRUISE AT FL330, THE NR 1 ENGINE FLAMED OUT. THE CREW COULD NOT RESTART THE ENGINE. THE AIRCRA FT DIVERTED TO DFW WHERE AN UNEVENTFUL LANDING WAS MADE. AFTER TROUBLESHOOTING, THE ENGINE THE FUEL PUMP AND FUEL CONTR OL WERE REPLACED PER THE MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999123100464 19991231 00464 NM 1999 12 31 GAIA99213 1 19991130 A 2781 CONNECTOR BOEING 727 727223 1384074 NM LE FLAP LOOSE A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 6806 19481 EN ROUTE FROM OKC TO STL, FLIGHT 717, ON APPROACH TO STL WHEN FLAPS WERE SET TO 2 DEGREES, POSITION PANEL SHOWED AMBER L EADING EDGE SLAT NR 2 INDICATION. USED 'ONE LEADING EDGE DEVICE INOP' EMERGENCY CHECKLIST. AIRCRAFT MADE AN UNEVENTFUL LANDING IN STL. A VISUAL CHECK INDICATES NR 2 SLAT WAS WORKING PROPERLY. FOUND CANNON PLUG ON NR 2 SLAT ACTUATOR LOOS E. CLEANED AND SECURED CANNON PLUG. OPERATIONALLY TESTED GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999123100465 19991231 00465 EU 1999 12 31 SIMA993011 1 19991028 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 541AT 1083 541 DFW - FLT 3617 - EMERGENCY LIGHTS DO NOT ILLUMINATE IN SEVERAL LOCATIONS. REMOVED BATTERY PACK AT 61WL AND 62WL. OPERA TIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999123100466 19991231 00466 EU 1999 12 31 SIMA992991 1 19991026 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 536AT 1124 536 HOU - FLT 3548 - EXIT SIGNS FOR BOTH FORWARD EMERGENCY DOORS AND FIVE ALTERNATING FLOOR PROXIMITY LIGHTS DO NOT ILLUMINA TE. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999123100467 19991231 00467 EU 1999 12 31 SIMA993092 1 19991105 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 254AE 18173 340B254 SBP - FLT 3077 - RANDOM EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT LOCATION 22LN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999123100468 19991231 00468 EU 1999 12 31 SIMA993091 1 19991103 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AE 340B198 DFW - FLT 3668 - EMERGENCY LIGHT BULB AT SEAT 11A DOES NOT ILLUMINATED. REMOVED AND REPLACED BULB. OPERATIONAL CHECK G OOD. (M) 2 L 7 2 4T RT A52EU 1999123100469 19991231 00469 EU 1999 12 31 SIMA993081 1 19991104 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 238AE 340B238 DFW - FLT 3520 - EMERGENCY LIGHT ABOVE SEAT 11 DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999123100470 19991231 00470 NM 1999 12 31 P2EA99331 1 19991110 A 5311 RIB BOEING 737 737297 1384480 NM BS 537 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, RIB CRACKED AT BS 537, WL 156 INCH BETWEEN LBL 52 INCH AND LBL 62 INCH, INSIDE THE LEFT FORWARD WI NG TO BODY FAIRING. FABRICATED ANGLE IAW COOPESA EO COO-3-53-663-99 AND REPAIRED RIB IAW SERVICE BULLETIN 737-53-1098 P ART III FIG 3, REVISION 3, DATED JANUARY 2, 1999. PART THAT WAS FABRIATED WAS NOT AVAILABLE. (M) 2 L 7 2 4F A16WE 1999123100471 19991231 00471 NM 1999 12 31 P2EA99325 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 706 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - FLOORBEAM LOWER CHORD CRACKED AT BS 706, RBL 24.5 INCH AND WL 202 INCH. REPAIRED FLOORBEAM LOWER CHORD FROM BS 70 1 TO BS 712.5 IAW COOPESA EO NR COO-3-57-643-99, DATED 11/11/99. (M) 2 L 7 2 4F A16WE 1999123100472 19991231 00472 NM 1999 12 31 P2EA99326 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 706 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 706, LBL 24.5 INCH AND WL 202 INCH. REPAIRED FLOORBEAM LOWER CHORD FROM BS 698 TO BS 714 IAW COOPESA EO NR COO-3-57-643-99, DATED 11/11/99. (M) 2 L 7 2 4F A16WE 1999123100473 19991231 00473 NM 1999 12 31 P2EA99327 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 674 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 674, LBL 45.5 AND WL 202. REPAIRED FLOORBEAM LOWER CHORD FROM BS 668 TO BS 681 IAW COOPESA EO NR COO-3-57-643-99, DATED 11/11/99. (M) 2 L 7 2 4F A16WE 1999123100474 19991231 00474 NM 1999 12 31 P2EA99328 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 695 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 695, LBL 45.5 AND WL 202. REPAIRED FLOORBEAM LOWER CHORD FROM BS 688.5 TO BS 700 IAW COOPESA EO NR COO-3-57-643-99, DATED 11/11/99. (M) 2 L 7 2 4F A16WE 1999123100475 19991231 00475 NM 1999 12 31 P2EA99329 1 19991110 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 707 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, FLOORBEAM LOWER CHORD CRACKED AT BS 707, BL 0 AND WL 202. REPAIRED FLOORBEAM LOWER CHORD FROM BS 700 TO BS 713 IAW COOPESA EO NR COO-3-57-643-99, DATED 11/11/99. (M) 2 L 7 2 4F A16WE 1999123100476 19991231 00476 NM 1999 12 31 P2EA99330 1 19991108 A 5754 654645151 SKIN BOEING 737 737297 1384480 NM SPOILER CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, SPOILER NR 8, P/N 65-46451-51 DELAMINATED AND FITTING IN SPOILER CORRODED. FABRICATED FITTING IAW COOPESA EO COO-3-57-657-99, DATED 11/16/99 AND REPAIRED SPOILER IAW COOPESA EO COO-CMP-3-57-649-99, DATED 11/13/99 SPOI LER REMOVED AND REPLACED ON VAM100 NR 514 COOPESA W/O M11071-6-75. (M) 2 L 7 2 4F A16WE 1999123100477 19991231 00477 NM 1999 12 31 USAA991153 1 19991111 A 5320 CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 639 STRINGER 2L CLIP. INSTALLED TIE CLIP PER SR M 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999123100478 19991231 00478 NM 1999 12 31 USAA991152 1 19991111 A 5320 CLIP BOEING 737 737301 1384611 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 639 STRINGER 1L CLIP. INSTALLED TIE CLIP PER SR M 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999123100479 19991231 00479 NM 1999 12 31 USAA991151 1 19991111 A 5320 CLIP BOEING 737 737301 1384611 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 40945 23514 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 616 STRINGER 1L CLIP. INSTALLED TIE CLIP PER SR M 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999123100480 19991231 00480 NM 1999 12 31 USAA991269 1 19991107 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727E CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 40758 23703 PIT - DURING RON IN CLE, FOUND 3 INCH LONG CRACK ON SKIN AT STATION 727E FUSELAGE BELLY CENTER LINE AT NR 3 COMM ANTENNA MOUNT AREA. REMOVED CRACK, INSTALLED DOUBLER AND FILLER PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999123100481 19991231 00481 NM 1999 12 31 USAA991271 1 19991108 A 5320 BAC1498168 STIFFENER BOEING 737 7373B7 1384580 NM BS 727E CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 40758 23703 PIT - DURING OTHER REPAIR FOUND 3 CRACKS TOTALING 12.5 INCH W/2.5 INCH BY .5 INCH BROKENOUT AREA ON RADIUS. CORROSION O N CONTACT SURFACE MOST OF LENGTH, LEVEL 1. FOUND AT NR 3 COMM ANTENNA ATTACH POINT STIFFENER APPROX STATION 727E. REMO VED CRACKED AND CORRODED STIFFENER CHANNEL. MADE AND INSTALLED NEW STIFFENER EXTRUSION OF BAC 1498-168 7075-T6 MATERIAL PER 65-65 DWG AND SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1999123100482 19991231 00482 1999 12 31 USAABB99051 2 19991106 A 7520 7929304 PRECOOLER BOEING 767 7672B7 1385107 NM LEFT ENGINE FAILED A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 19 655US 25257 PHL - FLT 126 - APPROXIMATELY FORTY MINUTES OUT OF PHL, THE CREW RECEIVED THE E/M 'L BLD OVHT'. CREW CLOSED THE LEFT BL EED AND SECURED THE LEFT PACK. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LE FT ENGINE PRECOOLER. (M) 2 L 7 2 4F RT A1NM 1999123100483 19991231 00483 NM 1999 12 31 TSAA9933481 1 19991116 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999123100484 19991231 00484 NM 1999 12 31 USAA119901 1 19991106 A 3350 1000677 BATTERY PACK GRIMES BOEING 727 727254 138408L NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913TS 20250 EMERGENCY EXIT LIGHTS AT L-1 DOOR AND COCKPIT DOOR WON'T TEST. REPLACED EMERGENCY EXIT LIGHTS (S/N 2019 AND 4459) AT L- 1 DOOR AND COCKPIT DOOR. (M) 2 L 7 3 4F A3WE 1999123100485 19991231 00485 EU 1999 12 31 USAA991233 1 19991101 A 5320 FITTING FOKKER F28 F28MK0100 4990807 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 897US 18123 11392 PIT - DURING RON VISIT, FOUND 1.125 INCH CRACK IN T-FITTING (W/O JOGGLE) AT BOTTOM END OF T-FITTING AFT SIDE APBH BL 102 7L. STOP DRILLED CRACK PER CD. REINSTALLED BLIND FASTENERS PER CD 53F00703. (M) 2 L 7 2 4F RT 1999123100486 19991231 00486 WP 1999 12 31 USAAD99167 1 19991122 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812US 48092 CLT - THE LOW LEVEL EMERGENCY LIGHT INDICATORS WERE FLASHING RED AND GREEN. MAINTENANCE REPLACED THE LOW LEVEL EMERGENC Y LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1999123100487 19991231 00487 NM 1999 12 31 USAASB99273 1 19991118 A 3350 500000043 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 224US 21666 CLT - PILOT REPORTED THAT THE EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY WITH SWITCH IN AUTO POSITION OR OFF POSITION. M AINTENANCE FOUND THE AFT FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH STICKING. REPLACED SAME. OPS CHECK NORMAL. BUF, PIL OT REPORTED LATER IN THE DAY THAT THE EMERGENCY EXIT AISLE LIGHTS FROM ROW 7 THROUGH 14 FLICKER ON AND OFF IN FLIGHT REG ARDLESS OF POSITION OF SWITCH. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK (P/N 9008-3-5-A) UNDER SEAT ROW 11. OPERATIONAL CHECK OF LIGHTS NORMAL. (M) 2 L 7 2 4F A16WE 1999123100488 19991231 00488 NM 1999 12 31 USAA991270 1 19991105 A 5753 7319544 FORK BOEING 737 737301 1384611 NM TE FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 40219 23560 PIT - DURING CX6 CHECK, FOUND ROD END CORROSION AND FITTING THREADS STRIPPED (SPHERICAL FORK END AND ATTACH CASTING) AT RIGHT WING OUTBOARD AFT TRAILING EDGE FLAP CONTROL ROD FITTING. REPLACED FOR END AND ATTACH CASTING. (M) 2 L 7 2 4F RT A16WE 1999123100489 19991231 00489 NM 1999 12 31 99ZZZM819 1 19991105 A 5753 1131697 CASTING BOEING 737 737301 1384611 NM TE FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 40219 23560 PIT - DURING CX6 CHECK, FOUND ROD END CORROSION AND FITTING THREADS STRIPPED (SPHERICAL FORK END AND ATTACH CASTING) AT RIGHT WING OUTBOARD AFT TRAILING EDGE FLAP CONTROL ROD FITTING. REPLACED FOR END AND ATTACH CASTING. (M) 2 L 7 2 4F RT A16WE 1999123100490 19991231 00490 NM 1999 12 31 USAA991258 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 601 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK THROUGH 2 FASTENER HOLES ON INNER CHORD OF FRAME BS 601 , WL 208 LEFT SIDE. INSTALLED CHORD ANGLE REPAIR PER EA 66021. (M) 2 L 7 2 4F RT A16WE 1999123100491 19991231 00491 NM 1999 12 31 USAA991257 1 19991118 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 665 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 665, LBL 31 PRESSURE DECK BELOW CABIN FLOOR B ULKHEAD. INSTALLED DOUBLER PER TR 53-60-04. (M) 2 L 7 2 4F RT A16WE 1999123100492 19991231 00492 NM 1999 12 31 USAA991256 1 19991118 A 5754 SKIN BOEING 737 737401 1384701 NM LE FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT INBOARD LOWER T/E NR 2 SLAT SKIN. INSTALLED DOUBLE R PER BOEING DWG 65C30133. (M) 2 L 7 2 4F RT A16WE 1999123100493 19991231 00493 NM 1999 12 31 USAA991255 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 907 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED D OUBLER PER TR 53-10-14 AND EA 66037. (M) 2 L 7 2 4F RT A16WE 1999123100494 19991231 00494 NM 1999 12 31 USAA991254 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 907 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED D OUBLER PER TR 53-10-14 AND EA 66037. (M) 2 L 7 2 4F RT A16WE 1999123100495 19991231 00495 NM 1999 12 31 USAA991253 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 827 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED D OUBLER PER TR 53-10-14 AND EA 66037. (M) 2 L 7 2 4F RT A16WE 1999123100496 19991231 00496 NM 1999 12 31 USAA991252 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727F CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 727F BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66037. (M) 2 L 7 2 4F RT A16WE 1999123100497 19991231 00497 NM 1999 12 31 USAA991251 1 19991118 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION FOUND CORROSION AT CLIPNUT HOLES UPPER FLANGE BS 947, RBL 16. CORROSION LEVEL 1. INSTALLED FLOORBEAM REPAIR PER TR 53-60-02. (M) 2 L 7 2 4F RT A16WE 1999123100498 19991231 00498 NM 1999 12 31 USAA991250 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION NUMEROUS AREAS .500 INCH FLOORBEAM BS 986 UPPER SURFACE OF T-C AP UPPER CHORD. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED REPLACEMENT T-CAP PER TR 53-60-01. (M) 2 L 7 2 4F RT A16WE 1999123100499 19991231 00499 NM 1999 12 31 USAA991244 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 787 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED R EPAIRED ANGLE PER TR 53-10-14 AND EA 66040 AND SRM 53-60-07. (M) 2 L 7 2 4F RT A16WE 1999123100500 19991231 00500 NM 1999 12 31 USAA991243 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 787 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED D OUBLER PER TR 53-10-14 AND EA 66040 AND SRM 53-60-07. (M) 2 L 7 2 4F RT A16WE 1999123100501 19991231 00501 NM 1999 12 31 USAA991242 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 867 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED D OUBLER PER TR 53-10-14 AND EA 66037. (M) 2 L 7 2 4F RT A16WE 1999123100502 19991231 00502 NM 1999 12 31 USAA991241 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT BS 867 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOU BLER PER TR 53-10-14 AND EA 66037. (M) 2 L 7 2 4F RT A16WE 1999123100503 19991231 00503 NM 1999 12 31 USAA991240 1 19991118 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 199, LBL 4.5 BULKHEAD WEB. INSTALLED DOUBL ER PER EA 66072. (M) 2 L 7 2 4F RT A16WE 1999123100504 19991231 00504 NM 1999 12 31 USAA991239 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 480 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED L ARGER FASTENER PER SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1999123100505 19991231 00505 NM 1999 12 31 USAA991238 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 500A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 500A BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED REPAIR DOUBLER PER EA 66037 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999123100506 19991231 00506 NM 1999 12 31 USAA991236 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 747 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED D OUBLER PER TR 53-10-14 AND EA 66037. (M) 2 L 7 2 4F RT A16WE 1999123100507 19991231 00507 NM 1999 12 31 USAA991235 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 727D BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED FRAME REPAIR PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999123100508 19991231 00508 NM 1999 12 31 USAA991234 1 19991118 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION FOUND 3 AREAS OF CORROSION 2 INCH BY 4 INCH AT STATION 294.5, RBL 54 Z ANGLE. C ORROSION LEVEL 2. INSTALLED NEW Z-ANGLE PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999123100509 19991231 00509 NM 1999 12 31 USAA991232 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURIGN Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY .5 INCH BS 344, LBBL 50 - RBBL 24 EXTRUSION UPPER C HORD. CORROSION LEVEL 2. CORROSON TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999123100510 19991231 00510 NM 1999 12 31 USAA991231 1 19991118 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIPNUT HOLE ON TOP OF FLOORBEAM 1 INCH BY 1 INCH BS 967, R BL 15, WL 208. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 1999123100511 19991231 00511 NM 1999 12 31 USAA991230 1 19991118 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 178, WL 199, RBL 4.5 BULKHEAD WEB. INSTALLED DOUBL ER PER TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1999123100512 19991231 00512 NM 1999 12 31 USAA991229 1 19991118 A 5320 TIE CLIP BOEING 737 737401 1384701 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A . 5 INCH CRACK AT BS 663 STRINGER 10R TIE CLIP. INSTALLED NEW CLIP PE R SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999123100513 19991231 00513 NM 1999 12 31 USAA991228 1 19991118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 727D BETWEEN STRINGER 8 AND 9R FRAME. INSTALLED D OUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999123100514 19991231 00514 NM 1999 12 31 USAA991227 1 19991118 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 294.3 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT T-CAP 1 INCH BY 1 INCH 12 PLACES STATION 294.3, RBL 0-52. C ORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999123100515 19991231 00515 NM 1999 12 31 USAA991203 1 19991118 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT NUTPLATE HOLE ON FLOORBEAM T-CAP BS 312, LBL 26, WL 208. C ORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED T-CAP PER SRM 53-10-51 FIG 205. (X) 2 L 7 2 4F RT A16WE 1999123100516 19991231 00516 NM 1999 12 31 USAA991262 1 19991113 A 5330 SKIN BOEING 737 737296 1384486 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 22398 22398 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A SECTION OF SKIN REMOVED TO GAIN ACCESS TO AFT PRESSURE BULKHEAD SKIN. INSTALLED DOUBLER PER BOEING DWG 65C28106 SHEET 1. (M) 2 L 7 2 4F RT A16WE 1999123100517 19991231 00517 NM 1999 12 31 USAA991261 1 19991113 A 5312 BULKHEAD BOEING 737 737296 1384486 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 22398 22398 TPA - DURIGN CX-2 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA AFT PRESSURE BULKHEAD STATION 1016, LOWER CENTER FUSELA GE WEB AND STIFFENERS, CORROSION LEVEL 2. REPAIRED PER EA 65691 AND SB 737-53A1075 BOEING DWG 65C28106. (M) 2 L 7 2 4F RT A16WE 1999123100518 19991231 00518 NM 1999 12 31 USAA991248 1 19991113 A 5330 SKIN BOEING 737 737296 1384486 NM BS 1156 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 22398 22398 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH SKIN CRACK STATION 1156 BETWEEN STRINGER 2L AND 3L. INSTALLED DOUBLER PER SB 737-53-1095. (M) 2 L 7 2 4F RT A16WE 1999123100519 19991231 00519 NM 1999 12 31 USAA119902 1 19991112 A 3350 0791217023 LENS BRUCE BOEING 727 727254 138408L NM ROW 10 MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 912TS 20438 FLT 6376 - DCA-LGA - EMERGENCY PATH LIGHTING HAS ONE LIGHT OUT ADJACENT TO ROW 10. REPLACED MISSING LENS. (M) 2 L 7 3 4F A3WE 1999123100520 19991231 00520 NM 1999 12 31 USAA991276 1 19991114 A 5320 BEAM BOEING 737 737401 1384701 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 10 INCH AREA OF CORROSION RIGHT CREASEBEAM INNER CHORD 1.5 INCH AFT OF STATION 294.5 TO 3.25 INCH FORWARD OF 360 CHORD. CORROSION LEVEL 1. INSTALLED NEW PART PER SRM 53-10-15. (M) 2 L 7 2 4F RT A16WE 1999123100521 19991231 00521 NM 1999 12 31 USAA991275 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25INCH CRACK STATION 827, BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-10-14 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999123100522 19991231 00522 NM 1999 12 31 USAA991274 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 787, BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999123100523 19991231 00523 NM 1999 12 31 USAA991272 1 19991114 A 5330 SKIN BOEING 737 737401 1384701 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK LOWER INNER RADIUS OF FORWARD SERVICE DOOR FORWARD FRAM E STATION 294.5, RBL 54.25 DOOR CUTOUT FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1999123100524 19991231 00524 NM 1999 12 31 USAA991219 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8R AND 9R AT BS 907 FRAME. INSTALLED DOUBLER AND FILLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999123100525 19991231 00525 NM 1999 12 31 USAA991268 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 907 AT RIVET IN PSU SUPPORT AT STRINGER 8R FRAM E. DAMAGED REMOVED AND INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202 AND SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999123100526 19991231 00526 NM 1999 12 31 USAA991267 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 907 AT RIVET IN PSU SUPPORT AT STRINGER 8L FRAM E. DAMAGED REMOVED AND INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202 AND SRM 51-10-02. (M0 2 L 7 2 4F RT A16WE 1999123100527 19991231 00527 NM 1999 12 31 USAA991266 1 19991114 A 5320 TIE CLIP BOEING 737 737401 1384701 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 706 AT TIE CLIP STRINGER 10R STRINGER TIE CLIP. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999123100528 19991231 00528 NM 1999 12 31 USAA991265 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME 520 AT PSU SUPPORT STRINGER 8R FRAME. INSTALLE D REPAIR DOUBLER PER SRM 53-00-07 FIG 202 AND SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999123100529 19991231 00529 NM 1999 12 31 USAA991264 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME STATION 616, RBL 54 INNER CHORD ANGLE. INSTALL ED REPAIR ANGLE AND FILLER PER TR 53-62-01. (M) 2 L 7 2 4F RT A16WE 1999123100530 19991231 00530 NM 1999 12 31 USAA991263 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME STATION 616, LBL 54 INNER CHORD ANGLE. INSTALL ED REPAIR ANGLE AND FILLER PER TR 53-62-01. (M) 2 L 7 2 4F RT A16WE 1999123100531 19991231 00531 NM 1999 12 31 USAA991220 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L AT BS 907 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999123100532 19991231 00532 NM 1999 12 31 USAA991221 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L AT BS 827 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 1999123100533 19991231 00533 NM 1999 12 31 USAA991222 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8R AND 9R AT BS 867 FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000010400001 20000104 00001 WP 2000 1 4 MWEA99900 1 19991215 A 5753 5910041503 VANE DOUG DC9 DC932 3022066 WP TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LEFT NUMBER ONE FLAP FIX VANE IS CHAFED ON INBOARD LEADING EDGE. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2000010400002 20000104 00002 WP 2000 1 4 MWEA99901 1 19991215 A 5753 5910134 SKIN DOUG DC9 DC932 3022066 WP TE FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND TOOL MARK ON UPPER OUTBOARD END OF RIGHT FLAP SKIN NEXT TO TRAILING EDGE MOUNTING FLANGE. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 2000010400003 20000104 00003 WP 2000 1 4 MWEA99902 1 19991215 A 5210 5910084 SKIN DOUG DC9 DC932 3022066 WP PAX DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 UPPER AFT CORNER, EXTERIOR SKIN OF FORWARD PASSENGER DOOR IS BENT. MAINTENANCE FABRICATED AND INSTALLED CORNER REPAIR. 2 L 7 2 4F A6WE 2000010400004 20000104 00004 WP 2000 1 4 MWEA99903 1 19991215 A 5347 5956027521 TIEDOWN RAIL DOUG DC9 DC932 3022066 WP BS 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RIGHT CARGO TIE DOWN RAIL WAS CORRODED FROM STATION 218 TO 248 IN FORWARD CARGO BIN. MAINTENANCE FITTED AND INSTALLED N EW TIE DOWN RAIL. 2 L 7 2 4F A6WE 2000010400005 20000104 00005 WP 2000 1 4 MWEA99904 1 19991215 A 5347 5956027519 TIEDOWN RAIL DOUG DC9 DC932 3022066 WP BS 396 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LEFT CARGO TIE DOWN RAIL WAS CORRODED FROM STATION 396 TO 510 AND FROM STATION 510 AFT. MAINTENANCE FITTED AND INSTALLE D NEW TIE DOWN RAIL. 2 L 7 2 4F A6WE 2000010700001 20000107 00001 NM 2000 1 7 ASAA9940145 1 19990901 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 13-15 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 708AS 28895 PDX - DURING MAINTENANCE CHECK,THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13-15 WERE FOUND INOPERATIVE. RE-CONNECTED WIRI NG AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 2000010800001 20000108 00001 NM 2000 1 8 RAAAB1035 1 19991223 A 3350 873100212 SIGN INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN MALFUNCTIONED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 MID-CABIN DOOR EMERGENCY EXIT LIGHT COMES ON WHEN EXIT LIGHTS PLACED IN ARMED POSITION. REPLACED MID-CABIN DOOR EMERGEN CY EXIT LIGHT ASSY PER RAA GMM. 2 L 7 3 4F A3WE 2000010800002 20000108 00002 SO 2000 1 8 COMA9910197 1 19991223 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 261CA 23696 120254 EMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES. 2 L 7 2 4T RT A31SO 2000010800003 20000108 00003 SO 2000 1 8 COMA9910198 1 19991225 A 3350 SIGN EMB 120 EMB120RT SO ROW 8 INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 247CA 120255 EMERGENCY EXIT SIGN AT ROW 8 IS INOPERABLE. REPAIRED DAMAGED WIRES AT EXIT SIGN. 2 L 7 2 4T RT A31SO 2000010800004 20000108 00004 SO 2000 1 8 COMA9910199 1 19991227 A 2916 3182001003 RESERVOIR EMB 120 EMB120RT SO HYD SYSTEM LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 259CA 24639 11558 120252 HYDRAULIC RESERVOIR LOW LEVEL WARNING. QUANTITY INDICATED EMPTY. REPLACED THE RIGHT HAND HYDRAULIC RESERVOIR ASSY. 2 L 7 2 4T RT A31SO 2000010800005 20000108 00005 EA 2000 1 8 COMA9960813 1 19991226 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SMOKE A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 924CA 7026 SMOKE IN CABIN AND COCKPIT WHEN BLEED AIR SOURCE SWITCHED FROM ENGINES TO APU. SECURED AND DEFERRED THE APU PER MEL. 2 L 7 2 4F RT A21EA 2000010800006 20000108 00006 EA 2000 1 8 COMA9960814 1 19991226 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 EA LT PACK DIRTY A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 934CA 7042 FUMES AND OCCASIONAL SMOKE FROM THE LEFT HAND ACM. REPLACED THE LEFT ACM COALESCER SOCK. 2 L 7 2 4F RT A21EA 2000010800007 20000108 00007 EA 2000 1 8 COMA9960815 1 19991227 A 5730 601R10045 PANEL CNDAIR CL600 CL6002B19 EA WS 116 - 136 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 RIGHT HAND LOWER WING ACCESS HOLES AT 640 EB WS 116.366, 640FB WS 136.676 AND 650 DB WS 230 CRACKED. BLENDED OUT DAMAGE AREAS, ROTO-PEENED AND ALODINED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2000010800008 20000108 00008 EA 2000 1 8 COMA9960816 1 19991223 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 806CA 7359 ANTI-ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED SYSTEM, NO DEFECTS FOUND. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A21EA 2000010800009 20000108 00009 EA 2000 1 8 COMA9960817 1 19991222 A 2750 TE FLAPS CNDAIR CL600 CL6002B19 EA WINGS FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 965CA 7131 FLAPS FAILED AT 20 DEGREES DURING APPROACH. RESET FLAP SYSTEM PER AD 98-20-01. 2 L 7 2 4F RT A21EA 2000010800010 20000108 00010 EA 2000 1 8 COMA9960818 1 19991227 A 3010 32022321 CHECK VALVE CNDAIR CL600 CL6002B19 EA BLEED AIR MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 912CA 7011 RIGHT WING ANTI-ICE CAUTION MESSAGE. REPLACED THE RIGHT HAND BLEED AIR CHECK VALVE. 2 L 7 2 4F RT A21EA 2000010800011 20000108 00011 EU 2000 1 8 99FDEA00514 1 19991229 A 2842 COMPUTER AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E 52054 NE FUEL QUANTITY INOPERATIVE A FDEA C ABORTED TAKEOFF W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 SO 25 449FE 217 99-297 - ECAM AND MASTER SHOW CHECK FUEL MGMT. REMOVED AND REPLACED FUEL QTY COMPUTER PERFORM BITE CK. 2 L 7 2 4F 4 F RT A35EU E3NE 2000010800012 20000108 00012 NM 2000 1 8 SCNA99158 1 19991225 A 3350 SIGN BOEING 727 727225 1384077 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22559 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT IDENTIFIERS AT THE RT OVERWING DOORS WERE FOUND INOPERATIVE. REPAIR ED SPLICES FOR RT OVERWING EXIT IDENTIFIERS PER WPM 203012. LIGHTS OP CHECKED GOOD PER MM 33590. 2 L 7 3 4F A3WE 2000010800013 20000108 00013 EU 2000 1 8 RAIA9912037 1 19991219 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU POD FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 574HK 7296 7296 41093 7459 - BHM - POD SMOKE CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE DEFERRED POD SMOKE DETECTOR IAW MEL 26-3 CAT C. MAIN TENANCE REPLACED POD SMOKE DETECTOR. 2 L 7 2 4T RT A41NM 2000010800014 20000108 00014 EU 2000 1 8 RAIA9912038 1 19991221 A 3610 S2L226 SEAL JETAIR JETSTM JETSTM4101 1500501 EU CROSS BLEED FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 560HK 41076 6160 - PHL- LEFT DUCT FAIL CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE DEFERRED PER MEL 21-18. MAINTENANCE REPLA CED DUCT BLEED SEALS. 2 L 7 2 4T RT A41NM 2000010800015 20000108 00015 NM 2000 1 8 SWAA992119 1 19991223 A 5230 6547952 SKIN BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND FWD CARGO DOOR OUTER SKIN, FWD LOWER CORNER CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2000010800016 20000108 00016 NM 2000 1 8 SWAA992120 1 19991224 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM ROWS 10 & 11 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS LIGHTS LOOSE AT ROWS 10 AND 11. SECURED LIGHTS PER MM. 2 L 7 2 4F RT A16WE 2000010800017 20000108 00017 2000 1 8 SWAA992121 4 19991224 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 FWD ENTRY DOOR EVACUATION SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2000010800018 20000108 00018 NM 2000 1 8 SWAA992122 1 19991224 A 5210 507945 DOOR BOEING 737 7377H4 NM PAX DOOR UNSECURED A SWAA C ABORTED TAKEOFF W P INADEQUATE Q C NO WARNING INDICATION CL CLIMB 1 SW 07 737JW 27869 AIR TURNBACK, PRESSURIZATION LEAK AT FWD ENTRY DOOR. UNABLE TO CONTROL MANUALLY THE ACFT PRESSURIZATION. DOOR APPEARED NOT BEING COMPLETELY CLOSED, DOOR ANNUNCIATOR DID NOT ILLUMINATE. C/W GROUND PRESS LEAK CK. OPS CK GOOD, DOOR OPS CK GOOD. 2 L 7 2 4F RT A16WE 2000010800019 20000108 00019 NM 2000 1 8 SWAA992123 1 19991225 A 5210 6545849 GATE BOEING 737 7373T5 NM SERVICE DOOR LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 667SW 23063 DIVERSION, LOUD NOISE AND VIBRATON AROUND AFT SERVICE DOOR. DURING DESCENT AT 7000 FEET, CABIN CLIMB RATE WENT TO 2000 FEET FOR ABOUT 10 SECONDS. ADJUSTED AFT SERVICE DOOR LOWER GATE. INSTALLED PRESS SEAL FILLER AROUND AFT SERVICE DOOR F WD THRESHOLD PLATE EDGE, AND REMOVED AND REPLACED AFT OUTFLOW VALVE AND PRESS RELIEF VALVES. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2000010800020 20000108 00020 NM 2000 1 8 SWAA992124 1 19991225 A 5210 808000 DOOR BOEING 737 7372H4 138448C NM AIRSTAIR OPEN A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 92SW 22964 AIR TURNBACK, AIRSTAIR LIGHT ILLUMINATED AND CABIN WOULD NOT PRESSURIZE NEITHER AUTO NOR STANDBY. FOUND AIRSTAIR DOOR A JAR. OPERATED AIRSTAIR SEVERAL TIMES AND OPS CK GOOD PER MM. 2 L 7 2 4F A16WE 2000010800021 20000108 00021 NM 2000 1 8 SWAA992125 1 19991227 A 3350 BR2013 LIGHT ASSY BOEING 737 7373H4 1384600 NM CABIN FLOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 EEPLS COVER LOOSE AND INOP IN AFT SECTION. SECURED LOOSE COVER AND LIGHT ASSY. OPS CK GOOD. 2 L 7 2 4F RT A16WE 2000010800022 20000108 00022 NM 2000 1 8 SWAA992126 1 19991222 A 5230 6545871 FRAME BOEING 737 7375H4 138449D NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND FWD CARGO DOOR AFT LOWER T-FRAME CRACKED. REMOVED AND REPLACED CARGO DOOR ASSY PE R MM. 2 L 7 2 4F RT A16WE 2000010800023 20000108 00023 2000 1 8 SWAA992127 4 19991223 A 2565 D31354 INDICATOR BOEING 737 7372H4 138448C NM ESCAPE SLIDE MOVED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 94SW 23053 AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F A16WE 2000010800024 20000108 00024 NM 2000 1 8 SWAA992128 1 19991223 A 3350 100031 POWER SUPPLY BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED C2 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY ASSY P ER MM. 2 L 7 2 4F A16WE 2000010800025 20000108 00025 NM 2000 1 8 SWAA992129 1 19991223 A 5313 BAC1498 STRINGER BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 15L CRACKED, BS 540. REPAIRED STRINGER PER SRM. 2 L 7 2 4F A16WE 2000010800026 20000108 00026 NM 2000 1 8 SWAA992130 1 19991223 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 DURING SCHEDULED 1/2D CHECK, FOUND BS 987 FLOORBEAM CORRODED AT FWD FACE BETWEEN LBL 43 AND RBL 43. REPAIRED BEAM PER S WA 1-453-037. 2 L 7 2 4F RT A16WE 2000010800027 20000108 00027 NM 2000 1 8 SWAA992131 1 19991224 A 3350 07912 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 603SW 27954 EEPLS TRACK LOOSE AT ROW 12. SECURED TRACK PER MM. 2 L 7 2 4F RT A16WE 2000010800028 20000108 00028 NM 2000 1 8 SWAA992132 1 19991224 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 EEPLS INOP. REPAIRED BROKEN WIRE PER MM. 2 L 7 2 4F RT A16WE 2000010800029 20000108 00029 2000 1 8 SWAA992133 4 19991225 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM PAX DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2000010800030 20000108 00030 NM 2000 1 8 SWAA992136 1 19991227 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED, BS 747, WL 208. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2000010800031 20000108 00031 NM 2000 1 8 SWAA992137 1 19991227 A 3350 07912 LIGHT COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 13. SECURED TRACK COVER PER MM. 2 L 7 2 4F RT A16WE 2000010800032 20000108 00032 NM 2000 1 8 SWAA992138 1 19991227 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600WN 27694 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 FLOORBEAM CORRODED ON UPPER SURFACE, RBL 31-36. REPAIRED BEAM PER SWA RA NR A1-353-2188. 2 L 7 2 4F RT A16WE 2000010800033 20000108 00033 NM 2000 1 8 SWAA992139 1 19991227 A 3350 300432 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505SW 24182 DURING SCHEDULED D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REPAIRED WIRING AT LIGHT'S PIN CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2000010800034 20000108 00034 NM 2000 1 8 SWAA992140 1 19991227 A 3350 100003 LIGHT BOEING 737 7377H4 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 712SW 27846 DURING SCHEDULED SERVICE CHECK, FOUND AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 2000010800035 20000108 00035 NM 2000 1 8 SWAA992141 1 19991228 A 5311 963820 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 SIDE CHORD CRACKED, RBL 26. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2000010800036 20000108 00036 NM 2000 1 8 SWAA992142 1 19991228 A 3350 BR2013 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 EEPLS LIGHTS INOP AT MID CABIN AND TRACK COVER MISSING. REPAIRED LIGHTS AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2000010800037 20000108 00037 NM 2000 1 8 SWAA992143 1 19991228 A 5330 6545773 SKIN BOEING 737 7372H4 138448C NM BS 747 & 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED BS 747 AND 767, STRINGER 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F A16WE 2000010800038 20000108 00038 2000 1 8 SWAA992144 4 19991228 A 2565 D31354 INDICATOR BOEING 737 7372H4 138448C NM PAX DOOR MOVED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASS Y PER MM. 2 L 7 2 4F A16WE 2000010800039 20000108 00039 NM 2000 1 8 SWAA992145 1 19991229 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 847 - 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 847-867, STRINGER 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2000010800040 20000108 00040 NM 2000 1 8 SWAA992146 1 19991229 A 3350 6574550 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR EVACUATION SLIDE LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F A16WE 2000010800041 20000108 00041 NM 2000 1 8 SWAA992147 1 19991229 A 5311 6546537 FRAME BOEING 737 7372T4 1384492 NM BS 578 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED, BS 578, LBL 60 AND LBL 63. REPAIRED STUB FRAME PER SRM. 2 L 7 2 4F A16WE 2000010800042 20000108 00042 NM 2000 1 8 SWAA992148 1 19991229 A 5311 6546558 FRAME BOEING 737 7372T4 1384492 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 907, STRINGER 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F A16WE 2000010800043 20000108 00043 NM 2000 1 8 SWAA992134 1 19991227 A 3260 284A0301 SENSOR BOEING 737 7377H4 NM COCKPIT MALFUNCTIONED A SWAA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 755SA 27871 DURING APPROACH, CYCLED THE GEARS TWICE TO GET A GREEN LIGHT NOSE GEAR INDICATION, PSEU LIGHT ILLUMINATED AFTER. C/W PS EU BITE CHECK, RESET MSG D9082 AT PIN NR 9, SENSOR S0846. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 2000010800044 20000108 00044 SO 2000 1 8 LR7A99100 1 19990923 A 5311 352896 FITTING LKHEED 382 382G 526414U SO BS 946 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 550 4606 DURING SCHEDULED B2 INSPECTION PER HB0505 FOUND L AND R FS 946 BUTTERFLY FITTINGS CRACKED AT WL 250. REPLACED FITTINGS PER SRM 583-51-10, PG 4(G). NR 2009. 2 H 7 4 4T A1SO 2000010800045 20000108 00045 SO 2000 1 8 LR7A99101 1 19990926 A 5330 PANEL LKHEED 382 382G 526414U SO BS 1067 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 550 4606 DURING SCHEDULED B2 INSPECTION PER HB0502 FOUND FS 1067 SKIN BUTT SPLICE CORRODED BL 0 TO RBL 36. REMOVED PANEL AND CLE ANED CORROSION. REPAIRED LOWER CAP PER SRM SMP 583-55-20-04, ITEM 04. REPAIRED SKIN PANEL PER SRM SMP 583-55-20-06. N R 3002. 2 H 7 4 4T A1SO 2000010800046 20000108 00046 SO 2000 1 8 LR7A99102 1 19990411 A 5320 3556713 FITTING LKHEED 382 382G 526414U SO BS 617 - 717 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP5297, FOUND FS 617 RT AND FS 717 RT 25K TIE DOWN END FITTINGS CRACKED. REPLAC ED FITTINGS IAW SMP 583-51-70. NR 323. 2 H 7 4 4T A1SO 2000010800047 20000108 00047 SO 2000 1 8 LR7A99103 1 19990411 A 5320 339394 FITTING LKHEED 382 382G 526414U SO BS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HST5302, FOUND FS 617 BULKHEAD SIDE SUPPORT FITTING CRACKED AT RBL 61. REPLACED FITTING IAW SMP 583-51-70, NR 350. 2 H 7 4 4T A1SO 2000010800048 20000108 00048 SO 2000 1 8 LR7A99104 1 19990411 A 5413 36250214 LONGERON LKHEED 382 382G 526414U SO NACELLE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP7180 FOUND NR 3 QEC RT UPPER SLOPING LONGERON CORRODED. REPLACED LONGERON IAW SRM 583-54-20-08 AND SB 382-71-12, REV 92. NR 349 AND 959. 2 H 7 4 4T A1SO 2000010800049 20000108 00049 SO 2000 1 8 LR7A99105 1 19990411 A 5320 3759996 PRESS PANEL LKHEED 382 382G 526414U SO BS 593 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC3208, FOUND RMLG FS 593 SIDE PRESSURE PANEL DENTED BEYOND LIMITS AT WL 150. RE PLACED PANEL IAW SMP 583-51-70 AND DWG 3311015. NR 360. 2 H 7 4 4T A1SO 2000010800050 20000108 00050 SO 2000 1 8 LR7A99106 1 19990411 A 5320 WEB LKHEED 382 382G 526414U SO BS 583 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP57108, FOUND RMLG FS 583 ACCESS PANEL OPENING DENTED BEYOND LIMITS AT WL 155. REPAIRED IAW SMP 583 51-140-17. 2 H 7 4 4T A1SO 2000010800051 20000108 00051 SO 2000 1 8 LR7A99107 1 19990411 A 5312 3759995 PANEL LKHEED 382 382G 526414U SO BS 593 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC3209, FOUND LMLG FS 593 PRESSURE PANEL DENTED BEYOND LIMITS AT WL 150. REPLACE D PRESSURE PANEL IAW SMP 583-51-70 AND DWG 3311015. NR 362. 2 H 7 4 4T A1SO 2000010800052 20000108 00052 SO 2000 1 8 LR7A99108 1 19990411 A 5320 FITTING LKHEED 382 382G 526414U SO BS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 880 BULKHEAD END FITTING CAP CRACKED AT LBL 61. REPLACED CAP I AW SMP 583-51-70 AND DWG 342582. NR 365. 2 H 7 4 4T A1SO 2000010800053 20000108 00053 SO 2000 1 8 LR7A99109 1 19990411 A 5320 FITTING LKHEED 382 382G 526414U SO BS 817 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND LT SLOPING LONGERON FWD ATTACH FITTING CORRODED AT FS 817. REPLACED FITTING I AW SMP 583-53-10-10. NR 381. 2 H 7 4 4T A1SO 2000010800054 20000108 00054 SO 2000 1 8 LR7A99110 1 19990411 A 5320 ANGLE LKHEED 382 382G 526414U SO BS 687 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND FS 687 LT CHINE ANGLE CORRODED. REPAIRED IAW SMP 583-53-40-26. NR 382. 2 H 7 4 4T A1SO 2000010800055 20000108 00055 SO 2000 1 8 LR7A99111 1 19990411 A 5320 35625019 CAP LKHEED 382 382G 526414U SO BS 777 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 777 CARGO COMPARTMENT LOWER CAP CRACKED. REPLACED CAP IAW DWG 376954, 356250 AND MPP L100-404-99-057. DRC 386. 2 H 7 4 4T A1SO 2000010800056 20000108 00056 SO 2000 1 8 LR7A99112 1 19990411 A 5320 CAP LKHEED 382 382G 526414U SO BS 797 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 797 CARGO COMPARTMENT LOWER BEAM CAP CRACKED BETWEEN LBL 11.0 A ND RBL 5.0. REPAIRED IAW MPP L100-404-99-017. NR 387. 2 H 7 4 4T A1SO 2000010800057 20000108 00057 SO 2000 1 8 LR7A99113 1 19990411 A 5320 CAP LKHEED 382 382G 526414U SO BS 817 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 817 CARGO COMPARTMENT LOWER CAP CRACKED. REPLACED CAP IAW SMP 583-51-70 AND DWG 356251. NR 388 2 H 7 4 4T A1SO 2000010800058 20000108 00058 SO 2000 1 8 LR7A99114 1 19990411 A 5320 BEAM LKHEED 382 382G 526414U SO BS 597 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HST5319, FOUND FS 597L VERTICAL BEAM CORRODED AT WL 144. REPLACED BEAM IAW SMP 5 83-53-30. NR 389. 2 H 7 4 4T A1SO 2000010800059 20000108 00059 SO 2000 1 8 LR7A99115 1 19990411 A 5320 BEAM LKHEED 382 382G 526414U SO BS 597 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HST5319, FOUND FS 597R VERTICAL BEAM SHEARED DUE CORROSION AT WL 200. REPLACED B EAM IAW SMP 583-53-30. NR 390. 2 H 7 4 4T A1SO 2000010800060 20000108 00060 SO 2000 1 8 LR7A99116 1 19990411 A 5320 337508R FITTING LKHEED 382 382G 526414U SO BS 697 - 817 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND RT LONGERON FITTING CORRODED AND DRILLED FS 697 TO 817. REPLACED FITTING IAW DWG 3305049 AND SMP 583-51-70. NR 393. 2 H 7 4 4T A1SO 2000010800061 20000108 00061 SO 2000 1 8 LR7A99117 1 19990411 A 3221 3700319 FITTING LKHEED 382 382G 526414U SO BS 196 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND NLG DRAG BRACE ATTACH FITTING CRACKED AT FS 196. REPLACED FITTING IAW SMP 583-51-70. NR 398. 2 H 7 4 4T A1SO 2000010800062 20000108 00062 SO 2000 1 8 LR7A99118 1 19990411 A 5320 WEB LKHEED 382 382G 526414U SO BS 200 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND FS 200 NWW AFT PRESSURE WEB CRACKED AT WL 126, LBL 9 TO RBL 9. REPAIRED IAW M PP L100-404-99-016. NR 400. 2 H 7 4 4T A1SO 2000010800063 20000108 00063 SO 2000 1 8 LR7A99119 1 19990411 A 5320 FITTING LKHEED 382 382G 526414U SO BS 817 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND RT SLOPING LONGERON FITTING CRACKED AT FS 817. REPLACED FITTING IAW SMP 583-51-70 AND DWG 356198. NR 402. 2 H 7 4 4T A1SO 2000010800064 20000108 00064 SO 2000 1 8 LR7A99120 1 19990411 A 5320 DOUBLER LKHEED 382 382G 526414U SO BS 817 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND RT SLOPING LONGERON DOUBLER CORRODED, CHIPPED AND HOLED AT FS 817 . REPLACED DOUBLER IAW SMP 583-51-70 AND DWG 340033. NR 403. 2 H 7 4 4T A1SO 2000010800065 20000108 00065 SO 2000 1 8 LR7A9978 1 19990322 A 5320 34004328R CHANNEL LKHEED 382 382G 526414U SO BS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 477 C CHANNEL CRACKED AT RBL 25. REPLACED CHANNEL PER DW G 340043. 2 H 7 4 4T A1SO 2000010800066 20000108 00066 SO 2000 1 8 LR7A9979 1 19990322 A 5320 3759431R FITTING LKHEED 382 382G 526414U SO BS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 477 UPPER BULKHEAD SPLICE CRACKED AT RBL 20. REPLACED PE R DWG 340043-12. 2 H 7 4 4T A1SO 2000010800067 20000108 00067 SO 2000 1 8 LR7A9980 1 19990322 A 5320 3393943 FITTING LKHEED 382 382G 526414U SO BS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HSP5372 (SP-72), FOUND FS 617 RT STRUT SUPPORT FITTING CRACKED AT WL 150. REPLACED F ITTING IAW SRM SMP 583-53-40-01 AND DWG 339394-3. 2 H 7 4 4T A1SO 2000010800068 20000108 00068 SO 2000 1 8 LR7A9981 1 19990323 A 5315 3642421 FLOORBEAM LKHEED 382 382G 526414U SO BS 257 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2382 4606 DURING SCHEDULED C1 INSPECTION PER HSP53161, FOUND FS 257 FLOORBEAM CAP CORRODED AROUND ANCHOR NUT LOCATION AT WL 146, R BL 43. REPLACED FLOORBEAM CAP IAW SMP 583-53-40-01. 2 H 7 4 4T A1SO 2000010800069 20000108 00069 SO 2000 1 8 LR7A9982 1 19990324 A 5714 WEB LKHEED 382 382G 526414U SO WINGBOX CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2382 4606 DURING SCHEDULED C1 INSPECTION PER HC2704, FOUND FWD CENTER WING WEB CRACKED 1.25 INCH AT RBL 20 RADIATING FROM FASTENER HOLE UNDER SUPPORT FITTING. REPAIRED PER MPP 401-1999-L100-57-107. 2 H 7 4 4T A1SO 2000010800070 20000108 00070 SO 2000 1 8 LR7A9983 1 19990322 A 5320 ANGLE LKHEED 382 382G 526414U SO BS 490 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 490 UPPER PRESSURE FAIRING CAP ANGLE CRACKED AT RBL 61. R EPAIRED IAW SRM SMP 583-53-40-35B. 2 H 7 4 4T A1SO 2000010800071 20000108 00071 SO 2000 1 8 LR7A9984 1 19990322 A 5320 ANGLE LKHEED 382 382G 526414U SO BS 490 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 490 UPPER PRESSURE FAIRING CAP ANGLE CRACKED AT LBL 61. R EPAIRED IAW SRM SMP 583-53-40-35B. 2 H 7 4 4T A1SO 2000010800072 20000108 00072 SO 2000 1 8 LR7A9985 1 19990322 A 5400 3638011 FITTING LKHEED 382 382G 526414U SO NR 2 NACELLE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HSP71189, FOUND NR 2 ENGINE SUPPORT FITTING CRACKED. REPLACED FITTING PER SRM 583-54 -20-10 USING P/N 3331795-3. 2 H 7 4 4T A1SO 2000010800073 20000108 00073 SO 2000 1 8 LR7A9986 1 19990322 A 5400 3638011 FITTING LKHEED 382 382G 526414U SO NR 4 NACELLE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HSP71189, FOUND NR 4 ENGINE SUPPORT FITTING CRACKED. REPLACED FITTING IAW SRM SMP 58 3-54-20-10 USING P/N 3331795-3. 2 H 7 4 4T A1SO 2000010800074 20000108 00074 SO 2000 1 8 LR7A9987 1 19990322 A 5320 39820425 ANGLE LKHEED 382 382G 526414U SO BS 817 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2328 4606 DURING SCHEDULED C1 INSPECTION PER HC5303, FOUND FS 817 CHINE CRACKED AT WL 146, LBL 60. REPAIRED IAW SRM SMP 583-53-40 -26/27. 2 H 7 4 4T A1SO 2000010800075 20000108 00075 SO 2000 1 8 LR7A9988 1 19991228 A 5320 342718 GUSSET LKHEED 382 382G 526414U SO BS 858 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 153 4590 DURING SCHEDULED A CHECK, FOUND LT AND RT FS 858 UPPER GUSSETS CRACKED AT BL 61, WL 256. REPLACED GUSSETS IAW SRM 583-5 1-10, PG 4. 2 H 7 4 4T A1SO 2000010800076 20000108 00076 SO 2000 1 8 LR7A9989 1 19990424 A 5320 34004233R CHANNEL LKHEED 382 382G 526414U SO BS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 1772 4590 DURING SCHEDULED B1 INSPECTION, FOUND FS 477 BULKHEAD CHANNEL CRACKED AT RBL 40, WL 250. REPAIRED PER SRM SMP 583-51-14 0-19. 2 H 7 4 4T A1SO 2000010800077 20000108 00077 SO 2000 1 8 LR7A9990 1 19990424 A 5320 WEB LKHEED 382 382G 526414U SO BS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 1773 4590 DURING SCHEDULED B1 INSPECTION, FOUND FS 497 WEB CRACKED AT RBL 61, WL 254.4. REPAIRED PER SRM SMP 583 53-40-04, ITEM 1 2 FIG 53-40-35A FASTENER SUBSTITUTION APPROVED BY EDG 88-1, REV IR, DATED 4/22/99. DRC 0050. 2 H 7 4 4T A1SO 2000010800078 20000108 00078 SO 2000 1 8 LR7A9991 1 19990424 A 5330 SKIN LKHEED 382 382G 526414U SO BS 228 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 1773 4590 DURING SCHEDULED B1 INSPECTION PER HB0502, FOUND CRACK IN SKIN PANEL ABOVE CREW ENTRANCE DOOR AT FS 228 AT WL 200. REPA IRED IAW SRM SMP 583-51-140-12 AND 53-30-30. DRC 0001, 0008 AND 0012. 2 H 7 4 4T A1SO 2000010800079 20000108 00079 SO 2000 1 8 LR7A9992 1 19990424 A 5523 BEAM LKHEED 382 382G 526414U SO RT ELEVATOR TAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 1773 4590 DURING SCHEDULED B1 INSPECTION FOUND RT ELEVATOR TAB BEAM CRACKED, APPROX 7 INCH AT INBD END AND 4 INCH CRACK IN LE SKIN AT HSS 92. BEAM CRACK CUT OUT AND REPAIRED PER EDG 88-R01, REV IR, DATED 4/20/99. LE SKIN REPLACED IAW SRM SMP 583-51 -140-10. DRC 0034. 2 H 7 4 4T A1SO 2000010800080 20000108 00080 SO 2000 1 8 LR7A9993 1 19990708 A 5320 3700279 WEB LKHEED 382 382G 526414U SO BS 196 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 590 4606 DURING SCHEDULED B1 INSPECTION PER HB0506, FOUND FS 196 NOSE WHEEL WELL BULKHEAD CRACKED AT RT REAR HINGE FITTING MOUNT. REPLACED WEB IAW SRM SMP 583-51-70 AND DWG 370027. NR 1005. MEA 382-53-99-021. 2 H 7 4 4T A1SO 2000010800081 20000108 00081 SO 2000 1 8 LR7A9994 1 19990817 A 5320 INTERCOSTAL LKHEED 382 382G 526414U SO BS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2361 4590 DURING SCHEDULED C1 INSPECTION PER HSP5369 (SP-69), FOUND LMLG FS 477 INTERCOSTAL BEAM CRACKED AT WL 200 FASTENER HOLE. REPLACED BEAM PER SRM 583-53-40-02. DRC 2046. 2 H 7 4 4T A1SO 2000010800082 20000108 00082 SO 2000 1 8 LR7A9995 1 19990817 A 5320 341973R FITTING LKHEED 382 382G 526414U SO BS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2361 4590 DURING SCHEDULED C1 INSPECTION PER HSP5369 (SP-69) FOUND RMLG FS 497 UPPER BOW BEAM END FITTING CRACKED AT WL 250. REPL ACED FITTING PER SRM SMP 583-53-40-02. DRC 2034. 2 H 7 4 4T A1SO 2000010800083 20000108 00083 SO 2000 1 8 LR7A9996 1 19991009 A 5320 3800744 WEB LKHEED 382 382G 526414U SO BS 522 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2361 4590 DURING SCHEDULED C1 INSPECTION PER HSP53108, FOUND FS 522 RMLG ACCESS OPENING CRACKED AT WL 184. REPAIRED IAW DWG R99-0 016-1 AND MEA 382-53-99-178. DRC 2139. 2 H 7 4 4T A1SO 2000010800084 20000108 00084 SO 2000 1 8 LR7A9997 1 19990816 A 5320 3800743 WEB LKHEED 382 382G 526414U SO BS 522 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2361 4590 DURING SCHEDULED C1 INSPECTION PER HSP53108, FOUND FS 522 LMLG ACCESS OPENING CRACKED AT WL 184. REPAIRED IAW DWG R99-0 016-1 AND MEA 382-53-99-177. DRC 2031. 2 H 7 4 4T A1SO 2000010800085 20000108 00085 SO 2000 1 8 LR7A9998 1 19990905 A 5712 33261242 RIB LKHEED 382 382G 526414U SO WS 293 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 4590 DURING SCHEDULED C1 INSPECTION PER SB 382-57-75, FOUND RT RIB FORMER CRACKED AT OWS 293R. REPLACED RIB FORMER IAW SRM 5 83-57-50-02. DRC 2173. 2 H 7 4 4T A1SO 2000010800086 20000108 00086 SO 2000 1 8 LR7A9999 1 19990905 A 5320 375943 FITTING LKHEED 382 382G 526414U SO BS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2361 4590 DURING SCHEDULED C1 INSPECTION PER HSP53224, FOUND LEFT AND RIGHT FS 477 CIRCUMFERENTIAL SPLICE FITTINGS CRACKED AT BL 2 0 LONGERON CUTOUTS. REPLACED FITTINGS PER SMP 583-53-40-04 DRC 2093 AND 2094. 2 H 7 4 4T A1SO 2000010800087 20000108 00087 2000 1 8 9905413218 4 19991221 A 2210 SC47003 YAW DAMPER AIRBUS 320 A320211 3930320 EU VERTICAL STAB LEAKING A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 318US 23694 5912 206 DURING DESCENT, RECEIVED HYD G RSVR LOW LVL ECAM MESSAGE. FOLLOWED COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED LEAKING YAW DAMPER 3CC1. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2000010800088 20000108 00088 NM 2000 1 8 9905426642 1 19991226 A 3350 BATTERY BOEING 747 747212B 1384886 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 642NW 21942 DURING LINE CHECK, FOUND B ANC C ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY ON POWER SUPPLY. OPERA TIONAL CHECK GOOD. 2 L 7 4 4F A20WE 2000010800089 20000108 00089 NM 2000 1 8 9905436303 1 19991226 A 2612 RELAY BOEING 747 747451 1384940 NM WHEEL WELL FAILED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 665US 23820 DURING TAKEOFF, THE WHEEL WELL FIRE WARNING ACTIVATED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. REPLACED R8048 RELAY. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 2000010800090 20000108 00090 WP 2000 1 8 9905449601 1 19991226 A 2910 LINE DOUG DC9 DC932 3022066 WP HYD SYSTEM CHAFED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 601NW 47038 DURING DESCENT INTO DTW, THE RIGHT HYDRAULIC QUANTITY DROPPED TO TWO GALLONS WITH LOW PRESSURE LIGHT ILLUMINATED. FLIGH T CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TEMPERATUREFLEX LINE CHAFED. REPL ACED LINE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2000010800091 20000108 00091 WP 2000 1 8 9905459906 1 19991228 A 2612 473925 ECU DOUG DC9 DC931 3022065 WP CARGO BAY FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 956N 1895 1895 47252 DURING TAXI INTO IAD, FORWARD CARGO SMOKE DETECTOR LIGHT ILLUMINATED. FLIGHT CREW ACTIVATED FORWARD CARGO BAY FIRE BOTT LE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE DAMAG E. REPLACED NR 1 CARGO ELECTRONICS UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2000010800092 20000108 00092 EU 2000 1 8 99FDEA00515 1 19991230 A 7932 INDICATOR AIRBUS 300 A300F4605R 3930327 EU OIL QUANTITY LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 685FE 803 99-298 - NR 2 ENG OIL QTY BEFORE START WAS 17 QTS, AFT START AND T/C WAS 13 QTS. AFTER 1 HR CR 10 QT. THEN LOSS OF A Q T 20 MIN 7 QTS. SWAPPED OIL QUAN IND PER MEM MOCC. RAN ENGINE, FOUND NO LEAKS. ENG IND 17 QTS. 2 L 7 2 4F RT A35EU 2000010800093 20000108 00093 NM 2000 1 8 99FDEA00516 1 19991229 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 618FE 48754 SNRM 403,0404, 467 - MAIN DECK CARGO COMP BS 635, LBL 47 CRACK IN LWR -403, MAIN DECK CARGO COMP BS 635, RBL 8.5 CRACK I N LWR -404, MAIN DECK CARGO COMP BS 635, LBL 27 CRACK IN LWR - 467. SEAT TRACKS REPAIRED PER SRM 53-70-00 FIG VOL 1. 2 L 7 3 4F RT A22WE 2000010800098 20000108 00098 SW 2000 1 8 2000ZZZX5 1 19991119 A 6720 206301052103 ACTUATOR BELL 206 206L4 1182110 SW TAIL ROTOR FAILED A WIPA K NONE O OTHER IN INSP/MAINT 1 WP 05 3310 1689 0062 52094 REMOVAL OF FAILED ACTUATOR. THIS IS THE THIRD ACTUATOR THAT HAS FAILED. 1 G 7 1 3U NC H2SW 2000010800103 20000108 00103 SO 2000 1 8 ASOA99154 1 19991117 A 3350 1013073 BULB EMB 120 EMB120RT SO ROWS 1 & 9 FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 269AS 120210 DURING INSPECTION, FOUND EMERGENCY LIGHTS AT ROWS 1 AND 9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY L IGHT BULBS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 2000010800104 20000108 00104 SO 2000 1 8 AD6A99004 1 19991008 A 2612 WIRE LKHEED 382 382G 526414U SO NR 2 NACELLE LOOSE A AD6A H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 03 82178 5048 ON TAXI OUT, NR 2 ENGINE NACELLE OVERHEAT LIGHT ILLUMINATED. RETURNED TO MAINTENANCE. FOUND WIRES LOOSE ON DETECTORS. WIRES TIGHTENED BY MAINTENANCE. OPS CHECKED OK. CONTINUED WITH FLIGHT. (X) 2 H 7 4 4T A1SO 2000010800105 20000108 00105 SO 2000 1 8 AD6A99003 1 19990908 A 3297 WIRE LKHEED 382 382G 526414U SO NLG BROKEN A AD6A O OTHER N FALSE WARNING AP APPROACH 1 SO 03 82178 5048 ON APPROACH, NOSE LANDING GEAR SHOWED INTRANSIT. VERIFIED GEAR DOWN AND LOCKED BY VISUAL THROUGH INSPECTION WINDOW. LA NDED WITH NO OCCURRENCES. MAINTENANCE TROUBLESHOOTING FOUND BROKEN GROUND WIRE. REPAIRED WIRE. (X) 2 H 7 4 4T A1SO 2000010800106 20000108 00106 EA 2000 1 8 ASOA99135 1 19991030 A 7931 602509197 TRANSMITTER CNDAIR CL600 CL6002B19 EA LEFT ENGINE INOPERATIVE A ASOA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 11 833AS 3117 7246 FLT 4739 - IN CRUISE AT FL 410, CREW RECEIVED LEFT ENGINE OIL PRESSURE MESSAGE AS WELL AS LEFT ENGINE OIL PRESSURE LESS THAN 25 PSI AND 'RED' IN COLOR. CREW PROCEEDED WITH LEFT ENGINE OIL PRESSURE MESSAGE EMERGENCY CHECKLIST. WITH ADVANCE MENT OF LEFT TRUST LEVER, THERE WAS NO CHANGE IN OIL PRESSURE. CREW COMPLETED SINGLE ENGINE PROCEDURES, DECLARED AN EME RGENCY, AND REQUESTED FIRE TRUCKS AND EMERGENCY EQUIPMENT. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REPLACED THE LEF T ENGINE OIL PRESSURE TRANSMITTER. LEAK AND OPERATIONAL CHECK WERE GOOD AFTER GROUND RUNS. AIRCRAFT RETURNED TO SERVIC E. (X) 2 L 7 2 4F RT A21EA 2000010800107 20000108 00107 EA 2000 1 8 ASOA99129 1 19991026 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS INOPERATIVE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 846AS 688 7328 FLT 4503 - AFTER DEPARTING HTL ON FLAP RETRACTION, FLAP FAIL MESSAGE CAME ON EICAS. CREW LEVELED OFF AT 6,000 FEET AND PERFORMED AFTER TAKEOFF CHECK LIST. CREW THEN MAINTAINED 200 KNOTS, PERFORMED FLAP FAIL CHECK LIST AND CALLED MAINTENAN CE CONTROL. CREW DECLARED AN EMERGENCY. FLIGHT RETURNED TO ATL AND SAFELY LANDED. MAINTENANCE REMOVED AND REPLACED LT BPSU. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 2000010800108 20000108 00108 CE 2000 1 8 2000ZZZX10 1 19991115 A 2121 26193873 BLOWER LEAR 35 35A 5170602 CE CABIN INOPERATIVE A AIOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 11 235AC 88 676 SMOKE CAME FROM VENTS ON APPROACH, 8 MILES FROM DESTINATION. TURNED OFF COCKPIT BLOWER, WENT ON OXYGEN, AND DECLARED EM ERGENCY. GROUND RUN DETERMINED BLOWER WAS SMOKING. MEL'D AND RETURNED TO BASE. FOUND BLOWER MOTOR DEFECTIVE. 2 L 7 2 4F A10CE 2000010800109 20000108 00109 NM 2000 1 8 AALA991573 1 19991016 A 2421 LINE BOEING 777 777223 1385213 NM BACKUP GENERATOR LOOSE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 770AN 29578 TUL - FLT 61 - ELECTRICAL BACK-UP GENERATOR RIGHT, OIL PRESSURE LOW. FOUND OVERFLOW LINE LEAK. RETORQUED LINE, SERVI CED BACKUP GENERATOR. RAN ENGINE FOR 10 MINUTES. NO LEAKS, NORMAL TEMP, NORMAL OPS, CHECKS OK. (X) 2 L 7 2 4F RT T00001SE 2000010800110 20000108 00110 NM 2000 1 8 AALA991542 1 19991011 A 2421 GENERATOR BOEING 777 777223 1385213 NM RT ENGINE FAILED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 770AN 29578 SEA - FLT 154 - ELECTRICAL BACK-UP GENERATOR RIGHT STATUS MESSAGE ILLUMINATED. REPLACED RIGHT ENGINE BACK-UP GENERATOR. ACCOMPLISHED ENGINE RUN TEST AND MATERIALS CHECK. BOTH NORMAL. LEAK CHECK NORMAL. (X) 2 L 7 2 4F RT T00001SE 2000010800111 20000108 00111 NM 2000 1 8 AALA991705 1 19991114 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AN 29590 MIA - DURING OVERNIGHT MAINTENANCE, AFT SECTION IN FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED W IRING TO THE AFT SECTION IN FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATI ON. (X) 2 L 7 2 4F RT A2NM 2000010800112 20000108 00112 NM 2000 1 8 AALA991604 1 19991025 A 3397 WIRE BOEING 757 757223 1384957 NM ROW 5EF BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AN 29590 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 5EF INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE AT SEAT 5EF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000010800113 20000108 00113 NM 2000 1 8 AALA991739 1 19991116 A 3350 7024092007 LIGHT BOEING 777 777223 1385213 NM SEAT 33 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 780AN 29956 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH EXIT LIGHT AT SEAT 33G INOPERATIVE. REPLACED EMERGENCY EX IT FLOOR PATH EXIT LIGHT ASSEMBLY AT SEAT 33G. SYSTEM GROUND CHECK, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 2000010800114 20000108 00114 NM 2000 1 8 AALA991738 1 19991116 A 3350 SOCKET BOEING 777 777223 1385213 NM COCKPIT INTERMITTENT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 780AN 29956 DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT IS INTERMITTENT. REPOSITIONED EMERGENCY EXIT LIGHT SOC KET FOR POSITIVE CONTACT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 2000010800115 20000108 00115 NM 2000 1 8 AALA991570 1 19991018 A 3350 CIRCUIT BREAKER BOEING 777 777223 1385213 NM COCKPIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 778AN 29587 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN FIRST CLASS ILLUMINATED WITH THE SWITCH IN THE ARMED POSITI ON. REPLACED EMERGENCY EXIT LIGHT CIRCUIT BREAKER FOR FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 2000010800116 20000108 00116 NM 2000 1 8 AALA991254 1 19990823 A 2161 TEMP CONTROL BOEING 737 737823 13844BZ NM LEFT INOPERATIVE A AALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 905AN 29507 ORD - FLT 1875 - AFTER TAKEOFF ORD-SAN, ELECTRICAL SMOKE NOTED IN COCKPIT. EMERGENCY DECLARED AND AIRCRAFT LANDED ORD W ITHOUT INCIDENT. ACCOMPLISHED RUN-UP OF BOTH LEFT AND RIGHT ENGINES. REPLACED LEFT TEMPERATURE CONTROLLER THAT HAD BEE N PREVIOUSLY PLACARDED INOPERATIVE PER MEL. OPERATED BOTH AIR CONDITIONING PACKS. NO FAULTS FOUND AND COULD NOT DUPLIC ATE DISCREPANCY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A16WE 2000010800117 20000108 00117 EU 2000 1 8 2000ZZZX11 1 19991222 A 3220 NLG MENASCO STBROS SD3 SD330 8100602 EU NOSE MALFUNCTIONED A DATA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 13 938MA SH3046 FLYING INTO WILMINGTON, THE CREW EXPERIENCED AN UNSAFE NOSE GEAR INDICATION. CREW TRIED TO HAVE TOWER VERIFY NOSE GEAR POSITION, BUT UNABLE TO. CREW TRIED NUMEROUS TIMES TO VERIFY POSTION BY MEANS OF EMERGENCY CHECKLIST. NONE OF THESE WE RE SUCCESSFUL. AN EMERGENCY WAS DECLARED BY THE CREW. LANDING WAS MADE SUCCESSFULLY WITH NO PROBLEMS OR DAMAGE. AIRCR AFT WAS TAXIED UNDER ITS OWN POWER CLEAR OF THE RUNWAY AND TO ITS ASSIGNED PARKING SPOT. THE MECHANIC PINNED THE GEAR A ND IT HAS BEEN MEL'D. 2 H 7 2 4T A41EU 2000010800119 20000108 00119 EU 2000 1 8 2000ZZZX13 1 19991206 A 2436 10590139 VOLT REGULATOR BOLKMS 105 BO105CBS 5626008 EU JUNCTION BOX FAILED A ALGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 493HL 5634 S809 IN CRUISE FLIGHT, SMOKE IN COCKPIT. SMOKE EMANATING FROM MAST MOMENT INDICATOR. AIRCRAFT DIVERTED TO ICY FOR MAINTENAN CE, OVER-VOLTAGE CAUSED BY THE VOLTAGE REGULATOR. 1 G 7 2 3U NC H3EU 2000010800120 20000108 00120 SW 2000 1 8 2000ZZZX14 1 19991124 A 6510 407340339103 BEARING 407040303107 BELL 407 407 SW MAIN ROTOR FAILED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 527AL 84 K981322 53211 FOUND ON AIRCRAFT SHUTDOWN. (STRANGE NOISES). FORWARD BEARING COMPLETE FAILURE, BEARING IS NOT RUNNING TRUE (OFF CENTE R) CAUSING BEARING TO RUN HOTTER AND SLINGING ALL OF ITS GREASE BEFORE NEXT SCHEDULED SERVICING (100 HOURS). 1 G 7 1 3U O H2SW 2000010800122 20000108 00122 SW 2000 1 8 2000ZZZX16 1 19991130 A 6510 407340340101 DISC PACK 407040302103 BELL 407 407 SW T/R DRIVE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 607AL RNFS3037 53264 DURING 25-HOUR AD INSPECTION, FOUND NR 7 DISC PACK CRACKED ON LAST AFT LAMINATE. (X) 1 G 7 1 3U O H2SW 2000010800124 20000108 00124 EU 2000 1 8 GXPA99008 1 19991203 A 3210 MLG AMD FALC20 FALCON 2720302 EU FUSELAGE MALFUNCTIONED A GXPA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 175GA 45 AIRCRAFT DEPARTED (ADS) ADDISON, TEXAS, EN ROUTE TO (ADU) RALEIGH DURHAM, NC. LANDING GEAR WOULD NOT EXTEND. USED EMER GENCY EXTENSION AND LANDED WITHOUT INCIDENT AT RDV. FERRIED AIRCRAFT GEAR DOWN TO (SDF) LOUISVILLE, KY FOR REPAIRS. (X ) 2 L 7 2 4F A7EU 2000010800172 20000108 00172 NM 2000 1 8 2000ZZZX24 1 19990907 A 5711 SPAR BOEING 727 727260 NM WS 124-152 CORRODED A S84A K NONE O OTHER IN INSP/MAINT 1 EA 21 901PG 39275 21978 SJO - REPAIRED LEFT WING FRONT SPAR LOWER CHORD PLATE LEADING EDGE BETWEEN FSS 124 AND FSS 152 DUE TO WEAR AND CORROSION IAW COOPESA EO COO-2-57-549-99 DATED 9-22-99, AND, BOEING FAX NR COO-5J0-99-00306 H, DATED 9-22-99, AND BOEING FAX NR M -7200-99-08778 DATED 9-26-99, DOCUMENTED ON FAA FORM 8110-3, APPROVED AND SUBMITTED BY FAA DER. 2 L 7 3 4F RT A3WE 2000010800175 20000108 00175 CE 2000 1 8 2000ZZZX27 1 19991207 A 3230 SWITCH RKWELL NA265 NA26560 7630106 CE LT MLG OUT OF RIG A UUKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 66GE 30699 CREW EXTENDED LANDING GEAR ON APPROACH TO SUS. NO GREEN DOWN AND LOCKED LIGHT ON LT SIDE. LANDING GEAR WAS CYCLED WITH SAME RESULTS. CREW PERFORMED EMERGENCY EXTENSION PROCEDURES AND DID FLY-BY OF TOWER AT SUS. TOWER REPORTED GEAR APPEA RED DOWN AND LOCKED. AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. AS AIRCRAFT TAXIED TO RAMP, LT DOWNLOCK LIGHT ILLUM INATED. LT DOWNLOCK SWITCH WAS FOUND RIGGED FOR MINIMUM TRAVEL. RE-RIGGED SWITCH IAW THE SABRE 60 MM., CHAPTER 32-60-0 1. FUNCTIONALLY CHECKED OK. 2 L 7 2 4J RT A2WE 2000010800178 20000108 00178 NE 2000 1 8 2000ZZZX31 2 19991010 A 7261 LINE BOEING 727 727276 138408R NM PWA JT8 JT8D15 52051 NE ENGINE OIL LEAKING A S84A A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 EA 21 908PG 20951 NR 3 ENGINE LOSING OIL (LANDED WITH 2 GALLONS LEFT). FOUND NR 4 BEARING VENT LINE 'B' NUT LOOSE (ONE FULL TURN). NO CH ANGE IN OIL PRESSURE. TIGHTENED NR 4 BEARING VENT LINE 'B' NUT, RE-SAFTETIED, RAN ENGINE AND OPS CHECKED GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 2000010800180 20000108 00180 2000 1 8 2000ZZZX33 4 19991216 A 6113 1250909K201 SPINNER CESSNA 207 207A 2073604 CE PROPELLER SEPARATED A P FWRA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 AL 01 9996M 207600779 DURING CRUISE FLIGHT, SPINNER SEPARATED FROM AIRCRAFT. INSPECTION REVEALED SPINNER CRACKED MIDWAY BETWEEN BACKING PLATE AND FORWARD SUPPORT. 1 H 7 1 3O A16CE 2000010800189 20000108 00189 SO 2000 1 8 2000ZZZX43 1 19991216 A 3240 3083A BRAKE ASSEMBLY PARKERHANFIN PIPER PA32 PA32R300 7103213 SO RT MLG FAILED A GSBA O OTHER O OTHER NR NOT REPORTED 1 AL 05 1392H 2514 32R7780156 BRAKES BINDED AND WORE BRAKE PADS DOWN TO THE METAL AND CONTINUED TO WEAR. THE HEAT AND WEAR RUINED THE BRAKE DISC AND BRAKE PAD BACKING PLATE. THE BACKING PLATE WARPED CAUSING THE BRAKES TO BIND AND THE HEAT DEFORMED THE O-RINGS IN THE B RAKE CALIPER. BRAKE FLUID WAS LOST. THE HEAT RUINED THE TIRE AND THE WHEEL. 1 L 7 1 3O A3SO 2000010800196 20000108 00196 WP 2000 1 8 UPS00831248 1 19991230 A 2610 TERMINAL DOUG DC8 DC873F 302199F WP CORE COWL BROKEN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 NR 3 ENG FIRE WARNING NO TEST. REPAIRED TERMINAL UNDER CORE COWL. 2 L 7 4 4F RT 4A25 2000010800197 20000108 00197 NM 2000 1 8 UPS99531240 1 19991229 A 2150 COOLING FAN BOEING 757 75724APF 1384969 NM COCKPIT OVERHEAT A IPXA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SO 01 404UP 23726 PILOT REPORT, SMOKE IN FLT DECK ON LANDING. WITH EQUIP COOLING MSG OVERHEAT LIGHT ILLUMINATED EICAS MSG CLG FAN DISPLAYE D. OVHT LGT EXT IN WHEN ALT WAS SELECTED. RESET 3 PHASE FWD COOLING FAN 1 ON P6. RAN FAN ON GROUND 1.5 HRS, OPS NORMA L, NO HISTORY. 2 L 7 2 4F RT A2NM 2000010800198 20000108 00198 2000 1 8 UPS99531243 2 19991231 A 7532 BLEED VALVE BOEING 757 75724APF 1384969 NM LT ENGINE INOPERATIVE A IPXA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 01 410UP 23732 AIR TURN BACK, EICAS MSG CABIN ALTITUDE DISPLAYED. CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUMINATED. ALSO, L ENG BLEED OFF MSG ON EICAS ALONG WITH L ENG BLEED AIR LIGHT ON. DUCT PRESSURE AT ZERO. DEFERRED LEFT ENGINE BLEED PER MEL 36-77- 7. PERFORMED BITE TEST PER 21-30-00, FIGURE 103, OF CABIN PRESSURE CONTROLLER WITH NO FAILURE NOTED. 2 L 7 2 4F RT A2NM 2000010800199 20000108 00199 WP 2000 1 8 UPS99831242 1 19991230 A 2720 3760963501 MECHANISM DOUG DC8 DC871F 302199D WP RUDDER BINDING A IPXA C ABORTED TAKEOFF F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 715UP 45915 RUDDER BINDING DURING TAKEOFF ROLL, NORMAL OPERATION UNTIL AFTER LANDING AND TAXI. RUDDER BINDS LIMITING TRAVEL TO 3 IN CH RUDDER PEDAL MOVEMENT PROBLEM WITH RUDDER IS SPORADIC. REF LOG PAGE 138103. REMOVED AND REPLACED LOAD FEEL MECHINISM . SYSTEM OPS CHECKS GOOD IAW DC8MM27-23-01, P/N OFF 3760963-501, S/N OFF UPO4627, P/N ON 3760963-501, S/N ON OA2175. 2 L 7 4 4F RT 4A25 2000010800200 20000108 00200 NE 2000 1 8 99FDEA00517 2 19991231 A 7230 COMPRESSOR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 3 ENGINE STALLED A FDEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 25 607FE 48547 99-299, COMPRESSOR STALLS NR 3 ENG, FLT LEVEL 320. 2 L 7 3 4F 4 F RT A22WE E31N3 2000010800201 20000108 00201 NM 2000 1 8 SWAA992152 1 19991231 A 2781 6544760287 SWITCH BOEING 737 7373T5 NM LE FLAP INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 696SW 23064 AIR TURNBACK, NR 2 L/E SLAT TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 L/E SLAT ROD END SWITCH PER MM. 2 L 7 2 4F RT A16WE 2000010800202 20000108 00202 NM 2000 1 8 SWAA992153 1 19991230 A 2560 P4010021 BATTERY BOEING 737 7377H4 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729SW 27861 AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2000010800205 20000108 00205 NM 2000 1 8 SWAA992149 1 19991230 A 2782 65445516 ACTUATOR BOEING 737 7373Y0 1384671 NM LE FLAP INOPERATIVE A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 682SW 23496 AIR TURNBACK, NR 3 KRUGER FLAP WOULD NOT FULLY RETRACT, TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 KRUGER FLA P ACTUATOR. 2 L 7 2 4F RT A16WE 2000010800206 20000108 00206 NM 2000 1 8 SWAA992150 1 19991230 A 3230 A42006028305 SOLENOID BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 068SW 22357 AIR TURNBACK, GEAR LEVER WOULD NOT MOVE UP AFTER TAKEOFF. REMOVED AND REPLACED GEAR LEVER LOCK SOLENOID ASSY PER MM. 2 L 7 2 4F A16WE 2000010800207 20000108 00207 2000 1 8 SWAA992151 4 19991230 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 506SW 24183 AFT SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 2000010800208 20000108 00208 NM 2000 1 8 SCNA99159 1 19991229 A 2822 CIRCUIT BREAKER BOEING 727 7272M7 138407S NM BOOST PUMP FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 294SC 21202 AIR RETURN DUE TO ALL CIRCUIT BREAKERS FOR TANK NUMBER TWO FUEL BOOST PUMPS POPPED. FOUND NUMBER TWO FWD RT CIRCUIT BRE AKER PHASE B AFT RT CIRCUIT BREAKER PHASE A AND AFT LEFT CIRCUIT BREAKERS PHASE A INTERMITTENTLY OPENING. REMOVED AND R EPLACED CIRCUIT BREAKERS. DURING TROUBLESHOOTING INTERCHANGED THE NUMBER TWO RT FWD AND RT AFT BOOST PUMPS. OPERATION ALLY CHECKS GOOD. 2 L 7 3 4F A3WE 2000010800209 20000108 00209 SO 2000 1 8 LR7A99121 1 19990411 A 5320 WEB LKHEED 382 382G 526414U SO BS 657 BUCKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND FS 657 CARGO FLOOR BULKHEAD WEB BUCKLED AND CHANNEL CRACKED. REP LACED WEB AND CHANNEL IAW DWG 356119. NR 440. 2 H 7 4 4T A1SO 2000010800210 20000108 00210 SO 2000 1 8 LR7A99122 1 19990411 A 5320 CHANNEL LKHEED 382 382G 526414U SO BS 517 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND FS 517 4 VERTICAL BULKHEAD CHANNELS CRACKED AT TOP END AT RBL 7, L BL 7, RBL 9 AND LBL 9. REPLACED VERTICAL CHANNELS IAW DWG R99-0002-2 REV A AND MPP L100-404-99-012. NR410. 2 H 7 4 4T A1SO 2000010800211 20000108 00211 SO 2000 1 8 LR7A99123 1 19990411 A 5320 WEB LKHEED 382 382G 526414U SO BS 677 BUCKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUNDFS 677 CARGO FLOOR BULKHEAD WEB BUCKLED, STIFFENER BENT AND CHANNE L CRACKED. REPLACED WEB, STIFFENER AND CHANNEL PER DWG 356245. NR 441. 2 H 7 4 4T A1SO 2000010800212 20000108 00212 SO 2000 1 8 LR7A99124 1 19990411 A 5320 WEB LKHEED 382 382G 526414U SO BS 697 BUCKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND FS 697 CARGO FLOOR BULKHEAD WEB BUCKLED AND CHANNEL BENT. REPLAC ED WEB AND CHANNEL PER DWG 356250. NR 442. 2 H 7 4 4T A1SO 2000010800213 20000108 00213 SO 2000 1 8 LR7A99125 1 19990411 A 5320 WEB LKHEED 382 382G 526414U SO BS 717 BUCKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND FS 717 CARGO FLOOR BULKHEAD WEB BUCKLED AND CHANNEL BENT. REPLAC ED WEB AND CHANNEL PER DWG 356250. NR 443. 2 H 7 4 4T A1SO 2000010800214 20000108 00214 SO 2000 1 8 LR7A99126 1 19990411 A 5320 ANGLE LKHEED 382 382G 526414U SO BS 597 - 737 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND CARGO COMPARTMENT CHINE ANGLE CORRODED AND CRACKED FS 597 TO 737. REPLACED CHINE ANGLE IAW SMP 583 AND DWG 372326. NR 458. 2 H 7 4 4T A1SO 2000010800215 20000108 00215 SO 2000 1 8 LR7A99127 1 19990411 A 5320 ANGLE LKHEED 382 382G 526414U SO BS 576 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC3208, FOUND LOWER CHINE ANGLE CRACK AT FS 576, LBL 61.6. REPAIRED IAW SMP 583 53-40-27 AND MPP L100-404-99-059. NR 478. 2 H 7 4 4T A1SO 2000010800216 20000108 00216 SO 2000 1 8 LR7A99128 1 19990411 A 5315 FLOORBEAM LKHEED 382 382G 526414U SO BS 657 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND CARGO COMPARTMENT FLOOR FS 657 UPPER BEAM CAP CORRODED AT RLB 20. REPAIRED BEAM CAP IAW MPP L100 404-99-019. NR 921 2 H 7 4 4T A1SO 2000010800217 20000108 00217 SO 2000 1 8 LR7A99129 1 19990411 A 5315 FLOORBEAM LKHEED 382 382G 526414U SO BS 597 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND CARGO LOWER STRUCTURE FS 597 UPPER BEAM CAP CORRODED AT RBL 40. R EPLACED CAP IAW SMP 583 53-40. NR 924. 2 H 7 4 4T A1SO 2000010800218 20000108 00218 SO 2000 1 8 LR7A99130 1 19990411 A 5714 BEAM LKHEED 382 382G 526414U SO WING BOX CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION NR 420 WORK, FOUND CENTER WING BOX BEAM UPPER REAR CAP CORRODED AT CWS 61R. REPAIRED IAW SMP S83 AND MPP L100-404-99-060. NR 981. 2 H 7 4 4T A1SO 2000010800219 20000108 00219 SO 2000 1 8 LR7A99131 1 19990411 A 5413 3625018 LONGERON LKHEED 382 382G 526414U SO NR 2 NACELLE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP7180, FOUND NR 2 ENGINE QEC S/N 3769-24 LOWER RT LONGERON CRACKED AND CORRODED AT FWD INNERFLANGE FIRESHIELD HOLE. REPLACED LONGERON IAW DWG 362501 AND SB 382-71-12. NR 944. 2 H 7 4 4T A1SO 2000010800220 20000108 00220 SO 2000 1 8 LR7A99132 1 19990411 A 5413 36250214 LONGERON LKHEED 382 382G 526414U SO NR 3 NACELLE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP7180, FOUND NR 3 QEC S/N LMG 1369-31 UPPER RT SLOPING LONGERON CORRODED. REPL ACED LONGERON IAW SMP 583 54-20-03, HSPO7180, AND SB 382-71-12, REV 92. NR 959. 2 H 7 4 4T A1SO 2000010800221 20000108 00221 SO 2000 1 8 LR7A99133 1 19990411 A 5320 CAP LKHEED 382 382G 526414U SO BS 946 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION, FOUND FS 946 LT INBD CAP CRACKED BEHIND SLOPING LONGERON. REPLACED CAP IAW DWG 3425 85. NR 1011. 2 H 7 4 4T A1SO 2000010800222 20000108 00222 SO 2000 1 8 LR7A99134 1 19990411 A 5311 FRAME LKHEED 382 382G 526414U SO BS 297 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND FS 297 RT RING SEGMENT CORRODED AT WL 166 TO 190. REPAIRED IAW SM P 583 51-70 AND MPP L100-404-99-005. NR 500. 2 H 7 4 4T A1SO 2000010800223 20000108 00223 SO 2000 1 8 LR7A99135 1 19990411 A 5530 WEB LKHEED 382 382G 526414U SO VERTICAL STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HST5505, FOUND FS 1095 VERTICAL STAB WEB CRACKED AT VSS 9 TO 12. REPAIRED IAW DW G R99-0002-8 AND MPP L100-404-99-061. NR 545. 2 H 7 4 4T A1SO 2000010800224 20000108 00224 SO 2000 1 8 LR7A99136 1 19990411 A 5320 WEB LKHEED 382 382G 526414U SO BS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 4763 DURING C CHECK/BRIDGING INSPECTION PER HSP53224, FOUND FS 477 UPPER BULKHEAD WEB CRACKED AT RBL 20 TO RBL 61. REPAIRED IAW SRM 583 53-40-33A. NR 585 2 H 7 4 4T A1SO 2000010800225 20000108 00225 EA 2000 1 8 COMA0060001 1 19991230 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 188.040 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 LEFT LOWER WING ACCESS HOLES 550-CBW.S.209.040, 550BB-WS 188.040 AND 550AB-WS 163.000 CRACKED. BLENDED OUT DAMAGE, ROTO PEENED AND ALODINED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2000010800226 20000108 00226 EA 2000 1 8 COMA0060002 1 19991230 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 EA WS 163 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 RIGHT LOWER WING ACCESS HOLES 650BB-WS 188.040, 650AB -WS 163.000, 640FB-WS 136.676, 640 EB-WS 116-.366, 640CB-WS 76.161 AND 640AB-WS 54.681 CRACKED. BLENDED OUT DAMAGE, ROTO PEENED, AND ALODINED IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2000010800228 20000108 00228 WP 2000 1 8 TWAA9917402 1 19991224 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING CHECK-C MAINT, THE AFT END OF LONGERON 2L WAS CRACKED AT STA 1076. COMPLETED LONGERON SPLICE PER SRM 53-02, FIG 8. 2 L 7 2 4F A6WE 2000010800229 20000108 00229 WP 2000 1 8 TWAA9917403 1 19991223 A 5530 ANGLE DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING CHECK-C MAINT, THE FUSELAGE TO VERTICAL STAB ATTACH ANGLE WAS CRACKED .875 INCH LONG AT RT SIDE, STA 1121. CRACK IS BEYOND STOP DRILLED HOLES OF LOWER LEG CRACK. REPAIRED PER SRM 53-05, FIG 230. DOUBLER INSTALLED. 2 L 7 2 4F A6WE 2000010800230 20000108 00230 WP 2000 1 8 TWAA9917405 1 19990929 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 69 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND ANGLE CRACKED, AFT SIDE OF STA 69, LBL 13. REMOVED AND REPLACED PART PER TWA STANDARD P RACTICES MANUAL 6-70-01. 2 L 7 2 4F A6WE 2000010800231 20000108 00231 WP 2000 1 8 TWAA9917406 1 19990929 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 63 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND T ANGLE CRACKED, FORWARD SIDE OF STA 63, RBL 13. REMOVED AND REPLACED PART PER TWA STAN DARD PROCESSES MANUAL 6-70-01. 2 L 7 2 4F A6WE 2000010800232 20000108 00232 WP 2000 1 8 TWAA9917407 1 19991018 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 610 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND FUSELAGE TO WING ATTACH ANGLE CRACKED INBD OF LE OF LT WING, STA 610. REPLACED ANGLE WI TH MFG PN 5910006-43. REINSTALLED HI-LOCKS PER SRM 51-30-5. INSTALLED BOLTS, NUTS AND WASHERS PER TWA SPM 6-30-07. 2 L 7 2 4F A6WE 2000010800233 20000108 00233 WP 2000 1 8 TWAA9917409 1 19991110 A 5400 STIFFENER DOUG DC9 DC932 3022066 WP NR 2 NACELLE WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, THE SIDE COWL PANEL VERTICAL STIFFENER HAD WORN THROUGH AT REPAIR AND METAL HAD NOT BEEN ROUTED OUT TO PREVENT FURTHER CRACKING. ACCOMP EDDY CURRENT INSPECTION PER NDT 51-00-03 AND FOUND CRACK CO NTAINED. REPAIRED PER SRM 54-01, FIG 1. REPLACED DOUBLER. 2 L 7 2 4F A6WE 2000010800234 20000108 00234 WP 2000 1 8 TWAA9917410 1 19991022 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND LONGERON 2 LEFT CRACKED AT TIE BOLTS, STA 200. REMOVED AND REPLACED WITH NEW LONGERON F ROM STA 148 TO APPROX STA 230 PER TWA SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800235 20000108 00235 WP 2000 1 8 TWAA9917408 1 19991006 A 5320 STIFFENER DOUG DC9 DC932 3022066 WP BS 69 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND TOP FOOT OF VERTICAL STIFFENER CRACKED AT STA 69, RBL X-10. CRACK IS .25 IN LONG AND IN AFT END OF FOOT RADIUS. REMOVED AND REPLACED CRACKED STIFFENER PER SPM 6-70-01. INSTALLED HILOCKS PER SRM 51-30-05. 2 L 7 2 4F A6WE 2000010800236 20000108 00236 WP 2000 1 8 TWAA9917411 1 19991020 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 408 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND AT STA 408, FLOORBEAM TOP CHORD WORN AT LBL 0-10 IN. BLENDED OUT WEAR MARKS PER SRM 53- 05, FIG 20. INSTALLED 0.025 S/S WEAR STRIP PER SRM 53-05. 2 L 7 2 4F A6WE 2000010800237 20000108 00237 WP 2000 1 8 TWAA9917412 1 19991020 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 427 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND AT STA 427, THE FLOORBEAM TOP CHORD WAS WORN AT LBL 0-10 IN. BLENDED OUT WEAR MARKS PER SRM 53-05, FIG 20. INSTALLED 0.025 S.S WEAR STRIP PER SRM 5305. 2 L 7 2 4F A6WE 2000010800238 20000108 00238 WP 2000 1 8 TWAA9917413 1 19990929 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 83 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK AT STA 83 FORMER WAS CRACKED AT RBL 10. STOP DRILLED CRACK AND HIGH FREQ EDDY CURRENT STOP DRI LL PER NDT PART 6. CRACK CONTAINED PER 51-00-03. CRACK REPAIRED PER SRM 53-03, FIG 34. 2 L 7 2 4F A6WE 2000010800239 20000108 00239 WP 2000 1 8 TWAA9917414 1 19990929 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 83 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK AT STA 83 FORMER CRACKED AT LBL 10. STOP DRILLED CRACK. HFEC STOP DRILL PER TWA NDT PART 6-51 -00-03, CRACK CONTAINED. REPAIRED CRACK PER SRM 53-03, FIG 34. 2 L 7 2 4F A6WE 2000010800240 20000108 00240 WP 2000 1 8 TWAA9917415 1 19991224 A 5320 DOOR FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING CHECK-C MAINT, FOUND A FORWARD LT PASSENGER DOOR STOP HOLE, FOURTH HOLE FROM THE TOP ON THE AFT SIDE AND FIFTH FR OM THE BOTTOM, AFT SIDE. THE DOOR STOP HOLE HAD A .75 IN CRACK. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND INSTALLE D DOUBLER PER EMLR 96500. 2 L 7 2 4F A6WE 2000010800241 20000108 00241 WP 2000 1 8 TWAA9917401 1 19991224 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT STA 1076. REPAIRED LONGERON 2R AT STA 1076 PER SRM 53-02, FIG 8. 2 L 7 2 4F A6WE 2000010800242 20000108 00242 WP 2000 1 8 TWAA9917404 1 19990919 A 5400 CLIP DOUG DC9 DC932 3022066 WP NR 2 PYLON BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK AT STA 944, THE LOWER SIDE OF NUMBER 2 PYLON DOUBLER ANGLE CLIP WAS BROKEN. REPLACED DOUBLER P ER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800243 20000108 00243 NM 2000 1 8 QXEA9902675 1 19991222 A 3350 8252097701 LIGHT DHAV DHC8 DHC8202 2809007 NM ROW 8 INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 359PH 514 PDX - ROW 8 EMERGENCY PATH LIGHTING INOP. MAINTENANCE REPLACED THE PATH LIGHTING ASSEMBLY FOR ROW 8. OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2000010800244 20000108 00244 NM 2000 1 8 QXEA9902676 1 19991225 A 3350 10005511 LIGHT DHAV DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 826PH 16305 7944 24710 PDX - FLIGHT DECK EMERGENCY OVERHEAD LIGHT DEAD. MAINTENANCE REPLACED EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2000010800245 20000108 00245 NM 2000 1 8 QXEA9902677 1 19991226 A 5210 CABLE DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 827PH 275 PDX - MAIN CABIN DOOR HARD TO OPEN. MAINTENANCE LUBRICATED THE MAIN CABIN DOOR CABLE. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2000010800246 20000108 00246 NM 2000 1 8 QXEA9902667 1 19991211 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 653.349 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION NUMEROUS PLACED AROUND RIVETS ON TOP OF FRAME X653.349, BETWEEN STRINGER 23S AND 23P. REPAIRED IAW DHC- 8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2, SRM 51-20-11, PAGE 6, PARAGRAPH 2C AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800247 20000108 00247 NM 2000 1 8 QXEA9902668 1 19991215 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 618 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - GOUGE AT FRAME X618.0, BETWEEN STRINGERS 21S AND 20S. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800248 20000108 00248 NM 2000 1 8 QXEA9902669 1 19991221 A 5320 BRACKET DHAV DHC8 DHC8102 2809003 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION IN ANGLE BRACKET AT FRAME X600.0 AND STRINGER 21S. REPAIRED IAW HORIZON AIR EA 9-53-536. 2 H 7 2 4T RT A13NM 2000010800249 20000108 00249 NM 2000 1 8 QXEA9902670 1 19991210 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 636 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON FRAME X636.0 AT STRINGER 22P. REPAIRED IAW DHC-8 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2000010800250 20000108 00250 NM 2000 1 8 QXEA9902671 1 19991210 A 5320 BRACKET DHAV DHC8 DHC8102 2809003 NM BS 636 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON UPPER AND LOWER ANGLE BRACKETS, FRAME X636.0, STRINGER 22P. REPAIRED IAW DHC-8 SRM 51-20-41, SRM 51- 20-16 AND SRM 51-20-26. 2 H 7 2 4T RT A13NM 2000010800251 20000108 00251 NM 2000 1 8 QXEA9902672 1 19991215 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 262.400 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CHAFE DAMAGE AT STATION 262.400 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT, IT IS APPROXIMATELY .003 DEEP. REMOVA L WAS .001. FOUND TO BE WITHIN LIMITS IAW DHC-8 SRM PAGE 4, TABLE 2. 2 H 7 2 4T RT A13NM 2000010800252 20000108 00252 NM 2000 1 8 QXEA9902673 1 19991221 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 242.20 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CHAFE DAMAGE AT STATION 242.20 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT. IT IS APPROXIMATELY .035 DEEP. REPAIR ED IAW HORIZON AIR EA 9-53-535. 2 H 7 2 4T RT A13NM 2000010800253 20000108 00253 NM 2000 1 8 QXEA9902674 1 19991223 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 507 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - 4 DENT ON OUTER SKIN AT STATION 507, WL100, BL40RH. REPAIRED IAW HORIZON AIR EA 9-53-531. 2 H 7 2 4T RT A13NM 2000010800254 20000108 00254 NM 2000 1 8 QXEA9902606 1 19991129 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - LEFT FORWARD SEAT RAIL FLOOR BOARD ATTACH TABS CORRODED. REPAIRED IAW RD 8-53-3074 AND DHC-8 SRM 51-40-11, PAGES 1-4. 2 H 7 2 4T RT A13NM 2000010800255 20000108 00255 NM 2000 1 8 QXEA9902607 1 19991119 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 245 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION ON FLOOR BOARD ATTACH TABS AND DRILL DAMAGE ON UPPER SURFACE OF SEAT TRACK AT X245.0. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-26 AND SRM 51-40-11, PAGES 1-4. 2 H 7 2 4T RT A13NM 2000010800256 20000108 00256 NM 2000 1 8 QXEA9902608 1 19991126 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - LEFT INBOARD FLAP CONTACTING WINT TRAILING EDGE SHROUD IN CENTER AREA OF FLAP. POSSIBLE CHAFING ON FLAP UPPER SKI N. REPAIRED IAW RD 8-57-1022, PAGE 3, RD 8-57-1022, PAGE 3 (6 AND 7). 2 H 7 2 4T RT A13NM 2000010800257 20000108 00257 NM 2000 1 8 QXEA9902609 1 19991126 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - RIGHT WING INBOARD FLAP UPPER SURFACE IS CHAFED AT STATION YW87.0 AND STATION YW98.0. REPAIRED IAW RD 8-57-1022, PAGE 3, PARAGRAPH 5-7. 2 H 7 2 4T RT A13NM 2000010800258 20000108 00258 NM 2000 1 8 QXEA9902610 1 19991126 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX - RIGHT WING OUTBOARD FLAP UPPER SURFACE IS CHAFED AT STATION YW209.0-219.0 AND YW227.0-233.0. REPAIRED IAW RD 8-57 -1022, PAGE 3, PARAGRAPH 5-7. 2 H 7 2 4T RT A13NM 2000010800259 20000108 00259 NM 2000 1 8 QXEA9902611 1 19991130 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - CARGO DOOR UPPER SILL STRUCTURE IS DAMAGED AT TWO LOCATIONS. REPAIRED IAW RD 8-53-4654, DHC-8 SRM 51-20-16 AND SR M 51-20-36. 2 H 7 2 4T RT A13NM 2000010800260 20000108 00260 NM 2000 1 8 QXEA9902612 1 19991201 A 5320 WEB DHAV DHC8 DHC8202 2809007 NM BS 369 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - DAMAGE FOUND ON WEB AT X369 - PANEL 261FT ATTACH STRUCTURE. REPAIRED IAW HORIZON AIR EA 01-99177. 2 H 7 2 4T RT A13NM 2000010800261 20000108 00261 NM 2000 1 8 QXEA9902613 1 19991130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 598 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - CORROSION FOUND AT TIE DOWN LOCATION ON AFT END LEFT INBOARD SEAT TRACK STATION 598. REPAIRED IAW DHC-8 SRM 51-20 -16 AND RD 8-53-4657. 2 H 7 2 4T RT A13NM 2000010800262 20000108 00262 NM 2000 1 8 QXEA9902614 1 19991130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 598 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - CORROSION FOUND AT TIE DOWN LOCATION ON AFT RIGHT INBOARD SEAT TRACK, X598.0. REPAIRED IAW RD8-53-4657. 2 H 7 2 4T RT A13NM 2000010800263 20000108 00263 NM 2000 1 8 QXEA9902615 1 19991126 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - LEFT INBOARD FLAP TOP SURFACE HAS A CHAFE MARK 1 FROM INBOARD EDGE. REPAIRED IAW RD8-57-1541. 2 H 7 2 4T RT A13NM 2000010800264 20000108 00264 NM 2000 1 8 QXEA9902616 1 19991129 A 5400 HEAT SHIELD DHAV DHC8 DHC8202 2809007 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - LEFT NACELLE HEAT SHIELD HAS CHAFFING DAMAGE ON TOP SIDE AT STATION XN255.00. REPAIRED IAW RD8-54-177. 2 H 7 2 4T RT A13NM 2000010800265 20000108 00265 NM 2000 1 8 QXEA9902617 1 19991129 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - BAGGAGE DOOR OUTER SKIN GOUGED IN THE AFT UPPER CORNER AREA. REPAIRED IAW DHC-8 SRM 51-20-16M SRM 51-20-36 AND RD 8-52-418. 2 H 7 2 4T RT A13NM 2000010800266 20000108 00266 NM 2000 1 8 QXEA9902618 1 19991130 A 5210 SKIN DHAV DHC8 DHC8202 2809007 NM PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 YXX - PASSENGER DOOR OUTER SKIN HAS DENTS AT STATION X227.155, X229.03 AND X233.53. REPAIRED IAW RD8-52-417 AND DHC-8 S RM 51-40-00, PAGE 3, TABLE 2. 2 H 7 2 4T RT A13NM 2000010800267 20000108 00267 EU 2000 1 8 QXEA9902678 1 19991226 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU EVAC LIGHT FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 SEA- THE NR 1 EMERGENCY EVACUATION LIGHT WAS FOUND INOPERATIVE DURING INSPECTION. REMOVED AND REPLACED THE NR 1 EMERGEN CY LIGHT CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000010800268 20000108 00268 NM 2000 1 8 QXEA9902625 1 19991213 A 5230 STOP DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - DRESS OUT CONTACT AREA OF UPPER AND LOWER BAGGAGE DOOR STOPS AT LOCATIONS 7, 8, 9 AND 10. REPAIRED IAW RD8-53-104 , MM PSM 1-8-2, CHAPTER 52-30-00, PAGE 210. 2 H 7 2 4T RT A13NM 2000010800269 20000108 00269 NM 2000 1 8 QXEA9902626 1 19991209 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - RIGHT OUTBOARD FLAP TOP SURFACE AT YW176 AND 18 FORWARD OF THE TRAILING EDGE IS CHAFFED. REPAIRED IAW DHC-8 SRM 5 7-50-16, TABLE 1 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2000010800270 20000108 00270 NM 2000 1 8 QXEA9902627 1 19991213 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - RIGHT OUTBOARD FLAP TOP SURFACE AT YW232-242 AND 20 FORWARD OF TRAILING EDGE IS CHAFFED FROM SHROUD. REPAIRED IAW RD8-57-1022 AND RD8-57-1241. 2 H 7 2 4T RT A13NM 2000010800271 20000108 00271 NM 2000 1 8 QXEA9902628 1 19991208 A 5400 HEAT SHIELD DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - RIGHTHEATSHIELD HAS CHAFE DAMAGE AT XN245.0. REPAIRED IAW DHC-8 RD8-54-866. 2 H 7 2 4T RT A13NM 2000010800272 20000108 00272 NM 2000 1 8 QXEA9902629 1 19991207 A 5350 SKIN DHAV DHC8 DHC8202 2809007 NM TAIL CONE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - COMPOSITE TAIL CONE LOWER SKIN CRACKED JUST AFT OF INSPECTION PANEL OPENING, RIGHT OF CENTER. REPAIRED IAW DHC-8 SRM 51-70-00, PAGES 11-19 AND 601. 2 H 7 2 4T RT A13NM 2000010800273 20000108 00273 NM 2000 1 8 QXEA9902630 1 19991214 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 598 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - CORROSION FOUND ON RIGHT INBOARD SEAT TRACK AT X598.0 AT TIE DOWN IN BAGGAGE AREA. REPAIRED IAW RD8-53-4697. 2 H 7 2 4T RT A13NM 2000010800274 20000108 00274 NM 2000 1 8 QXEA9902631 1 19991214 A 5300 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 598 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - CORROSION FOUND ON LEFT INBOARD SEAT TRACK AT X598.0 AT TIE DOWN IN BAGGAGE AREA. REPAIRED IAW RD8-53-4697 AND HO RIZON AIR EA 2-53-122. 2 H 7 2 4T RT A13NM 2000010800275 20000108 00275 NM 2000 1 8 QXEA9902632 1 19991213 A 5230 STRAP DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - BAGGAGE DOOR UPPER SILL STRAPS AND FORWARD PRESSURIZATION STOP DAMAGED BY CONTACT WITH DOOR FITTINGS DURING CLOSIN G. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2000010800276 20000108 00276 NM 2000 1 8 QXEA9902633 1 19991212 A 5400 HEAT SHIELD DHAV DHC8 DHC8202 2809007 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - LEFT NACELLE DISHED HEAT SHIELDS HAVE CHAFE DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-20-36 AND RD8-54-1442 . 2 H 7 2 4T RT A13NM 2000010800277 20000108 00277 NM 2000 1 8 QXEA9902634 1 19991209 A 5400 HEAT SHEILD DHAV DHC8 DHC8202 2809007 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - LEFT HEATSHIELD TO FINGERNAIL ATTACH TABS AT XN280 IS CRACKED ON OUTBOARD TAB. REPAIRED IAW RD8-54-163 AND DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800278 20000108 00278 NM 2000 1 8 QXEA9902635 1 19991208 A 5400 HEAT SHILED DHAV DHC8 DHC8202 2809007 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - RIGHT OUTBOARD DISHED HEAT PANEL HAS CHAFE DAMAGE ON INBOARD SIDE AT XN223. REPAIRED IAW RD8-54-194. 2 H 7 2 4T RT A13NM 2000010800279 20000108 00279 NM 2000 1 8 QXEA9902636 1 19991211 A 7500 LINE DHAV DHC8 DHC8202 2809007 NM BLEED AIR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - LEFT CENTER WING BLEED PIPE MOUNT FLANGE CRACKED. REPAIRED IAW DHC-8 RD8-21-028. 2 H 7 2 4T RT A13NM 2000010800280 20000108 00280 NM 2000 1 8 QXEA9902637 1 19991215 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM LT NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - LEFT FORWARD LOWER NACELLE STRUCTURE ADJACENT TO LOWER COWL HINGE POINTS DAMAGED. REPAIRED IAW RD8-54-063. 2 H 7 2 4T RT A13NM 2000010800281 20000108 00281 NM 2000 1 8 QXEA9902638 1 19991209 A 5730 SCREW DHAV DHC8 DHC8202 2809007 NM WING PANEL STRIPPED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 YXX - STRESS PANEL 622AT, UPON REMOVAL OF PANEL ONE SCREW WAS FOUND STRIPPED HEAD AND SEIZED. REPAIRED IAW RD8-57-1420. 2 H 7 2 4T RT A13NM 2000010800282 20000108 00282 NM 2000 1 8 QXEA9902679 1 19991227 A 3350 RELAY DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 345PH 476 PDX - EMERGENCY LIGHTS IN CABIN FLICKERING ON AND OFF IN FLIGHT. REMOVED AND REPLACED XP4N AND YCD4N RELAY ON EMERGENCY LIGHTS CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2000010800283 20000108 00283 EU 2000 1 8 QXEA9902680 1 19991228 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 1985 1984 11169 BOI - CEILING EVACUATION LIGHTS INOP ABOVE ROWS 8-10. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000010800284 20000108 00284 NM 2000 1 8 QXEA9902682 1 19991218 A 5320 SPLICE DHAV DHC8 DHC8102 2809003 NM BS 488.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5, STRINGER 29RH. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800285 20000108 00285 NM 2000 1 8 QXEA9902681 1 19991210 A 5320 BRACKET DHAV DHC8 DHC8102 2809003 NM BS 618 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION IN AND AROUND NUT PLATE AND BRACKET AT FRAME X618.0, STRINGER 21S. REMOVED SURFACE CORROSION AROUND BRA CKET AND IN NUT PLATE. FOUND TO BE WITHIN LIMITS OF DHC-8 SRM 53-00-16, PAGE 4, TABLE 2. 2 H 7 2 4T RT A13NM 2000010800286 20000108 00286 NM 2000 1 8 QXEA9902683 1 19991218 A 5320 SPLICE DHAV DHC8 DHC8102 2809003 NM BS 488.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5 AND STRINGER 30RH. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800287 20000108 00287 NM 2000 1 8 TWAA9917501 1 19991228 A 5210 80330035 BOTTLE BOEING 757 757231 1384950 NM PAX DOOR DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 715TW 28483 THE FORWARD LEFT CABIN DOOR ASSIST BOTTLE PRESSURE WAS FOUND TO BE ZERO. REPLACED THE BOTTLE. CHECK-C 4-24-99 LAX. 2 L 7 2 4F RT A2NM 2000010800288 20000108 00288 WP 2000 1 8 TWAA9917506 1 19991123 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR ATTACH ANGLE STA 160 TO 200, LBL 45. REMOVED AND REPLACED SUPP ORT PER SPM 6-70-1, PAGE 3. 2 L 7 2 4F A6WE 2000010800289 20000108 00289 WP 2000 1 8 TWAA9917507 1 19991027 A 5310 WINDOW FRAME DOUG DC9 DC932 3022066 WP BS 794 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND IN LT CABIN STA 794 UPPER AFT CORNER OF WINDOW FRAME WITH A CRACK AT A FASTENER. REMOVE D CRACKED AREA OF WINDOW PAN AND INSTALLED C ANGLE REPAIR PER SSRM 53-10-114. 2 L 7 2 4F A6WE 2000010800290 20000108 00290 WP 2000 1 8 TWAA9917508 1 19991110 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 160 - 200 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR AT STA 160 TO 200, RBL 0 TO 50 IN, THE FLOOR PANEL MEMBRANE WITH A HEAVY WOR N DEEP AREA IN MEMBRANE FROM FLOOR PANEL CHAFING WORN ALMOST THROUGH. REMOVED AND REPLACED MEMBRANE FROM STA 160 TO 200 , RBL 0 TO 50, PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800291 20000108 00291 WP 2000 1 8 TWAA9917509 1 19991110 A 5321 PANEL DOUG DC9 DC931 3022065 WP BS 160 - 200 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR AT STA 160 TO 200, LBL 0 TO LBL44, FLOOR PANEL MEMBRANE WITH DEEP WORN AREAS FROM CHAFING FLOOR PANEL WORN ALMOST THROUGH IN 22 PLACES. REMOVED AND REPLACED MEMBRANES FROM STA 160 TO 200, BLB 0 T O LBL 44, PER STD PROCESSES MANUAL 6-70-01. 2 L 7 2 4F A6WE 2000010800292 20000108 00292 WP 2000 1 8 TWAA9917510 1 19991110 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 160 - 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915L 47357 DURING OP 16 MAINT CHECK,THE CABIN FLOOR AT STA 160 TO 200 HAD HEAVY CORROSION ON FLOOR PANEL ATTACH ANGLE RBL 45 IN. R EMOVED AND REPLACED SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800293 20000108 00293 WP 2000 1 8 TWAA9917511 1 19991110 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 197 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR AT STA 197, LBL 0 TO 57 IN WITH CORROSION ON FLOOR PANEL ATTACH ANGLES. REM OVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800294 20000108 00294 WP 2000 1 8 TWAA9917502 1 19991130 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 917 - 965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, THE CABIN FLOOR MEMBRANE AND FORMER FOOT WAS CORRODED AT STA 929, APPROX RBL 58. REMOVED CORR OSION AT FORMER FOOT AND ATTACH AREA SRM 51-10-3. REINSTALLED FORMER FOOT AND NEW FAB MEMBRANES PER SRM 51-30/51-10-4/5 3-05 FIG 97 AT STA 917 TO 965. 2 L 7 2 4F A6WE 2000010800295 20000108 00295 WP 2000 1 8 TWAA9917503 1 19991130 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 917 - 965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND THE CABIN FLOOR MEMBRANE AND FORMER FOOT AT LONGERON 18R, STA 945, APPROX RBL 58 WAS COR RODED. REMOVED CORROSION AT FORMER FOOT AND ATTACH AREA PER SRM 51-10-3. REINSTALLED FORMER FOOT AND NEW FAB MEMBRANE PER SRM 51-30/51-1-4/ AND 53-05, FIG 97, AT STA 917 TO 965. 2 L 7 2 4F A6WE 2000010800296 20000108 00296 WP 2000 1 8 TWAA9917504 1 19991130 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND ON THE RT WING A CRACK APPROXIMATELY 1 IN LONG WAS FOUND IN REPAIR DOUBLER OF WING L.E. RIB, 13 IN OTBD OF INBD END OF NUMBER 4 SLAT. INSTALLED NEW DOUBLER AND SHIM PER SRM 57-06A, FIG 5, SHEET 1 AND 4. 2 L 7 2 4F A6WE 2000010800297 20000108 00297 WP 2000 1 8 TWAA9917505 1 19991129 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1221 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND THE LEFT AFT FUSELAGE SKIN AT STA 1221, OTBD AT FWD CORNER OF VERT LOUVERS THE FWD OTBD ATTACH CLIP ANGLE WAS CRACKED THROUGH ON THE FWD SIDE. REPLACED CLIP AT STA 1221 PER SRM 53-05, FIG 66. FABRICATED LOW ER CLIP OUT OF 2024-O, 0.080, HEAT TREATED TO 2024T4 PER SPM 6-70-01, PAGE 2 AND 3. REPLACED CLIP PER SRM 53-05, FIG 66 . 2 L 7 2 4F A6WE 2000010800298 20000108 00298 NM 2000 1 8 QXEA9902684 1 19991211 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 510 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON FRAME FLANGE AT STATION 510 BETWEEN STRINGERS 30 AND 31 RT. REPAIRED IAW 20-32-02, PAGE 2, PARAGRAPH A, B AND C. 2 H 7 2 4T RT A13NM 2000010800299 20000108 00299 NM 2000 1 8 QXEA9902685 1 19991211 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 531 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON FRAME FLANGE AT STATION 531 BETWEEN STRINGERS 30 AND 31 RT. REMOVED LIGHT CORROSION IAW PSM 1-GEN-5, CHAPTER 4, PAGE 4-21, PARAGRAPH 8D. FOUND WITHIN LIMITS IAW DHC-8 SRM 53-00-16, PAGE 4, TABLE 2. 2 H 7 2 4T RT A13NM 2000010800300 20000108 00300 NM 2000 1 8 QXEA9902686 1 19991214 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 377 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - SMALL GOUGE IN BOTTOM OF LEFT INBOARD SEAT TRACK, APPROXIMATELY STATION 377. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2000010800301 20000108 00301 NM 2000 1 8 QXEA9902687 1 19991216 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 282 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT APPROXIMATELY STATION 282. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2000010800302 20000108 00302 NM 2000 1 8 QXEA9902688 1 19991214 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 330 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT INBOARD SEAT TRACK CHAFFED IN BOTTOM OF TRACK APPROXIMATELY AT STATION 330. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2 H 7 2 4T RT A13NM 2000010800303 20000108 00303 NM 2000 1 8 QXEA9902689 1 19991214 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 300 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT STATION 300. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36 . 2 H 7 2 4T RT A13NM 2000010800304 20000108 00304 NM 2000 1 8 QXEA9902690 1 19991215 A 5320 SILL DHAV DHC8 DHC8102 2809003 NM CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - NICKS BELOW CARGO DOOR SILL. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2. 2 H 7 2 4T RT A13NM 2000010800305 20000108 00305 NM 2000 1 8 QXEA9902691 1 19991217 A 5320 THRESHOLD DHAV DHC8 DHC8102 2809003 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - MINOR SURFACE CORROSION AROUND NUT PLATES UNDER MAIN CABIN DOOR THRESHOLD. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 6, PARAGRAPH 2C. 2 H 7 2 4T RT A13NM 2000010800306 20000108 00306 NM 2000 1 8 QXEA9902693 1 19991212 A 5347 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM BS 387 - 405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LIGHT SURFACE CORROSION ON RIVET HEADS AND WEB PLATE FROM RIGHT-HAND OUTBOARD SEAT TRACK TO STRINGER 23, BETWEEN F RAMES 387.350 AND 405.737. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800307 20000108 00307 NM 2000 1 8 QXEA9902694 1 19991219 A 5413 STRINGER DHAV DHC8 DHC8102 2809003 NM NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - EXHAUST DECK AFT LATERAL STRINGER HAS ONE CRACK. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800308 20000108 00308 NM 2000 1 8 QXEA9902696 1 19991221 A 5414 GUARD DHAV DHC8 DHC8102 2809003 NM NACELLE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - INBOARD MIDDLE GRAVEL GUARD ATTACH POINT WORN EXCESSIVELY THIN. REPAIRED IAW RD8-54-41. 2 H 7 2 4T RT A13NM 2000010800309 20000108 00309 NM 2000 1 8 QXEA9902697 1 19991219 A 5413 STRINGER DHAV DHC8 DHC8102 2809003 NM NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - HOLE IN STRINGER XN176.5 AT STATION ZN17.04. REPAIRED IAW HORIZON AIR EA 9-54-238, FIGURE 2. 2 H 7 2 4T RT A13NM 2000010800310 20000108 00310 NM 2000 1 8 QXEA9902698 1 19991219 A 5400 WEB DHAV DHC8 DHC8102 2809003 NM NACELLE PUNCTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - AFT NACELLE TOP DECK HAS A PUNCTURE HOLE AT APPROXIMATELY STATION X236.00 AND YW139.900. REPAIRED IAW HORIZON AIR EA 9-54-237. 2 H 7 2 4T RT A13NM 2000010800311 20000108 00311 NM 2000 1 8 QXEA9902699 1 19991223 A 5400 WEB DHAV DHC8 DHC8102 2809003 NM RT NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN280.0 0. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800312 20000108 00312 EA 2000 1 8 JBXA9900134 1 19991230 A 3230 46193 VALVE CNDAIR CL600 CL6002B19 EA MLG FAILED A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 579ML 7277 GEAR DISAGREE MESSAGE ON RETRACTION, NOSE UP MAINS DOWN. REMOVED AND REPLACED MAIN LANDING GEAR PRIORITY VALVE IAW AMM 32-32-15. GEAR RETRACTION NORMAL IAW AMM 32-30-00. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2000010800313 20000108 00313 WP 2000 1 8 TWAA9917607 1 19991117 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 1038 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND AFT INTERIOR AREA OF AFT ACCESSORY COMPT, STA 1038, THE LT ENG MOUNT INTERNAL TAIL STRUC TURE WEB WITH A 4 INCH CRACK. REPAIRED CRACK IN WEB STRUCTURE. STOP DRILLED HOLE, REPLACED DOUBLER PER SRM 53-01, FIG 2 SHEET 3. 2 L 7 2 4F A6WE 2000010800314 20000108 00314 WP 2000 1 8 TWAA9917608 1 19991202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 - 229 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON CABIN FLOOR TRACK CLIP NUT ATTACH, STA 200 TO 229, LBL 45. REMOVED C ORRODED TRACK FROM STA 200 TO 229, AND SPLICED IN NEW PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2000010800315 20000108 00315 WP 2000 1 8 TWAA9917611 1 19991124 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 165 - 185 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON LT FWD ENTRY DOOR FLOOR SILL ATTACH ANGLE AT SCREW HOLES APROX STA 16 5 TO 185, LBL 59. CUT OUT CORRODED DOOR SILL. REPLACED DOOR SILL CUSP FROM MIDDLE OF ENTRY DOOR TO STA 229, PER ARA 16 316. 2 L 7 2 4F A6WE 2000010800316 20000108 00316 WP 2000 1 8 TWAA9917613 1 19991110 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 180 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION ON TOP OF CABIN FLOOR PANEL ATTACH ANGLE, STA 180, RBL 0 TO 44 IN. REMOVED CO RROSION PER SPM 6-80-01. REINSTALLED SUPPORT PER SPM 6-30-07. TREATED PER SRM 51-10-3. 2 L 7 2 4F A6WE 2000010800317 20000108 00317 WP 2000 1 8 TWAA9917614 1 19991118 A 5711 SPAR DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND ON LT WING, 2 CRACKS AT TOP BOLT HOLES, OTBD APROX .375 IN LONG, INBD APPROX .25 IN LONG , ON REAR SPAR FACE AT CENTER FLAP HINGE SUPPORT, 1 O'CLOCK POSITION. STOP DRILLED CRACKS AROUND ATTACH BOLT HOLES PER SERVICE REWORK DRAWING JO60272. EDDY CURENT STOP DRILLED. REPAIRED DAMAGE TO REAR SPAR AT CENTER HINGE SUPPORT BOLT HO LES PER DRAWING JO602272. 2 L 7 2 4F A6WE 2000010800318 20000108 00318 WP 2000 1 8 TWAA9917601 1 19991110 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 160 - 220 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK AT STA 160 TO 220 FOUND CABIN FLOOR PANEL ATTACH ANGLE WITH CORROSION. REMOVED AND REPLACED FL OOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800319 20000108 00319 WP 2000 1 8 TWAA9917602 1 19991110 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 216 - 229 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON CABIN FLOOR SUPPORT ANGLE AT BL 0, STA 216 TO 229. REMOVED AND REPLA CED FLOOR SUPPORT ANGLE PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800320 20000108 00320 WP 2000 1 8 TWAA9917603 1 19991110 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION ON TOP OF CABIN FLOOR PANEL ATTACH ANGLE, STA 160, LBL 0 TO 13 IN. REMOVED AN D REPLACED FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800321 20000108 00321 WP 2000 1 8 TWAA9917604 1 19991110 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR ATTACH ANGLE, STA 160, RBL 0 TO 53 IN. REMOVED AND REPLACED FL OOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000010800322 20000108 00322 WP 2000 1 8 TWAA9917605 1 19991103 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 598 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR MEMBRANE AT STA 598, APPROX RBL 55 IN, WAS CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-01, FIG 4, SHEET 3, PAGE 19. 2 L 7 2 4F A6WE 2000010800323 20000108 00323 WP 2000 1 8 TWAA9917606 1 19991112 A 5350 FAIRING DOUG DC9 DC932 3022066 WP BS 813 - 816 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND RT WING LOWER EDGE OF FAIRING WAS WORN INTO FUSELAGE, STA 813 TO 816, FAIRING NUMBER 220 7A. METAL HAD THICKNESS IND OF 0.048 AT STA 813, LONGERON 26R. REMAINDER OF AREA WAS OK. INSTALLED DOUBLER PER SRM 53 -04, FIG 53, SHEET 1. 2 L 7 2 4F A6WE 2000010800324 20000108 00324 WP 2000 1 8 TWAA9917609 1 19991129 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 200, ON BOTH SIDES OF FORMER AT FLOOR LINE, FORWARD LEFT CABIN DOOR. C UT OUT CORRODED SECTION PER SPM 6-80-01. REMOVED AND REPLACED SUPPORT FROM MIDDLE OF FORWARD LEFT ENTRY DOOR TO STA 229 , PER ARA 16316. 2 L 7 2 4F A6WE 2000010800325 20000108 00325 WP 2000 1 8 TWAA9917610 1 19991129 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 195 - 204 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION ON LOWER AFT CORNER OF DOOR FRAME AND CABIN FLOOR WEB, APPROX STA 195 TO 204, LBL 59 IN. CUT OUT CORRODED SECTION PER SPM 6-80-01. REPLACED CUSP PER ARA 16316 FROM MIDDLE OF ENTRY DOOR TO STA 229. REPLACED MEMBRANE. 2 L 7 2 4F A6WE 2000010800326 20000108 00326 WP 2000 1 8 TWAA9917612 1 19991124 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND STA 200 CABIN FLOORBEAM OUTER EDGE CORRODED LBL 52 TO 55. CUT OUT CORRODED SECTION PER SPM 6-80-01. REPAIRED BEAM CAP PER ARA 16316. 2 L 7 2 4F A6WE 2000010800327 20000108 00327 WP 2000 1 8 TWAA9917615 1 19991118 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 813 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND WING TO FUSELAGE PANEL HAD WORN DEEPLY INTO THE SKIN ON LEFT SIDE, STA 813, LONGERON 26L . ACCOMP NDT INSP AND FOUND TOP SKIN EQUALS 0.022 MATERIAL LOSS AND BOTTOM SKIN 0.030 MATERIAL LOSS. REPAIRED, INSTALL ED DOUBLER PER SRM 53-04, FIG 53. 2 L 7 2 4F A6WE 2000010800328 20000108 00328 NM 2000 1 8 PCAA0001001 1 19991230 A 5210 85210263101 GAS STRUT DHAV DHC8 DHC8102 2809003 NM PAX DOOR BROKEN A PCAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 13 825EX 388 FLIGHT 3692 IN PHL- PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. PASSENGERS WERE DEPLANED NORMALLY. MAINTENAN CE INSPECTED AND FOUND THE AFT DOOR STRUT BROKEN. REMOVED AND REPLACED FORWARD AND AFT STRUTS IAW DHC PROCEDURES. DOOR OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2000010800329 20000108 00329 NM 2000 1 8 QXEA9902700 1 19991219 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT NACELLE EXTERIOR INBOARD SKIN HAS 1.5 CRACK AT STATION XN127.5 AND YW139.200, JUST AFT OF PANEL 425AL TOP ED GE. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2000010800330 20000108 00330 NM 2000 1 8 QXEA9902701 1 19991223 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM RT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT NACELLE EXTERIOR OUTBOARD SKIN HAS .250 CRACK FROM RIVET HOLE TO SKIN PANEL EDGE AT STATION XN122.00 AND YW1 71.200, ALSO HAS LOOSE WORKING RIVET IN SAME AREA JUST AFT OF PANEL 426AR. REPAIRED IAW HORIZON AIR EA 9-54-239. 2 H 7 2 4T RT A13NM 2000010800331 20000108 00331 EU 2000 1 8 QXEA9902702 1 19991227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 4150 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - MAIN LANDING GEAR DOORS ALTERNATE RETRACTION CABLE AT WINCH IS CHAFFING INTO FRAME 4150, TOP CENTER. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 2000010800332 20000108 00332 EU 2000 1 8 QXEA9902703 1 19991226 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 8805 SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT FUSELAGE EXTERIOR SKIN HAS (3) 1/2 LENGTH SCRATCHES LOCATED 3 AFT OF CENTER CARGO DOOR AFT SIDE APERTURE AT STRINGER 63 AND FRAME 8805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B, C. 2 L 7 2 4F RT A20EU 2000010800333 20000108 00333 EU 2000 1 8 QXEA9902704 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 7805 & 8305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - GOUGES IN LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 7805 AND 8305. REPAIRED IAW F-28 SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000010800334 20000108 00334 EU 2000 1 8 QXEA9902705 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 8305 - 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION IN SEVERAL PLACES ON LEFT OUTBOARD SEAT TRACK FLANGE BETWEEN FRAMES 8305 AND 8805. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000010800335 20000108 00335 EU 2000 1 8 QXEA9902706 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 8205 - 8805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - SEVERAL GOUGES IN CENTER OF LEFT OUTBOARD CABIN SEAT TRACK BETWEEN FRAMES 8205 AND 8805. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000010800336 20000108 00336 EU 2000 1 8 QXEA9902707 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305C CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON BOTTOM SIDE OF FLANGE, LEFT INBOARD SEAT TRACK, FORWARD OF FRAME 9305C. REPAIRED IAW FOKKER SRM 51-1 0-4. 2 L 7 2 4F RT A20EU 2000010800337 20000108 00337 EU 2000 1 8 QXEA9902708 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305C - 9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION IN CENTER OF LEFT OUTBOARD SEAT TRACK BETWEEN 9305C AND 9805. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000010800338 20000108 00338 EU 2000 1 8 QXEA9902709 1 19991221 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUEL PANEL 73F HAS FRETTING AROUND SEVERAL SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PARAGRAPH 3D. 2 L 7 2 4F RT A20EU 2000010800340 20000108 00340 NM 2000 1 8 QXEA9902710 1 19991227 A 3350 XD4N RELAY DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA O OTHER O OTHER CR CRUISE 1 NM 09 345PH 476 PDX - EMERGENCY LIGHTS IN THE CABIN FLICKERING ON AND OFF IN FLIGHT. MAINTENANCE REPLACED THE 3351-K3 AND 3351-K4 RELAY S. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2000010800341 20000108 00341 NM 2000 1 8 QXEA9902711 1 19991230 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 354PH 15196 228 498 SEA- 2 CEILING EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED THE PS3 BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 2000010800342 20000108 00342 EU 2000 1 8 QXEA0992712 1 19991229 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 GEG - EMERGENCY EXIT SIGN OVER ROW 9 WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT CIRCUIT BOARD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000010800343 20000108 00343 EU 2000 1 8 QXEA0992714 1 19991229 A 3350 551500004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU LIGHT FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 SEA - OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED CIRCUIT BOARD ON OVERHEAD EMERGENCY LIGHT. OPERATIONA L CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000010800344 20000108 00344 EU 2000 1 8 QXEA0992715 1 19991231 A 3350 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 GEG - FORWARD OVERHEAD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000010800345 20000108 00345 EU 2000 1 8 QXEA9902716 1 19991228 A 3350 6008905 BATTERY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 1984 1984 11169 PDX - OVERHEAD EXIT SIGNS INOPERATIVE OVER ROW 8 AND 9. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK G OOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000010800346 20000108 00346 EU 2000 1 8 QXEA9902717 1 19991229 A 3350 551500004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU SIGN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 BOI- FORWARD OVERHEAD EMERGENCY SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT CIRCUIT BOARD. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000010800347 20000108 00347 NM 2000 1 8 USAA991223 1 19991114 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK IN ANGLE RADIUS .5 INCH AFT OF STATION 294.5, RBL 54.2 5 ANGLE.. INSTALLED DOUBLER AND FILLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2000010800348 20000108 00348 NM 2000 1 8 USAA991224 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727F CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK IN FRAME STATION 727F BETWEEN STRINGER 8L AND 9L INST ALLED DOUBLER PER SRM 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000010800349 20000108 00349 NM 2000 1 8 USAA991225 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK IN FRAME STATION 787 BETWEEN STRINGER 8R AND 9R. INSTAL LED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000010800350 20000108 00350 NM 2000 1 8 USAA991226 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK IN FRAME STATION 827 BETWEEN STRINGER 8R AND 9R. INSTAL LED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000010800351 20000108 00351 NM 2000 1 8 USAA991273 1 19991114 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727F CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 31198 23989 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 727F, BETWEEN STRINGER 8L AND STRINGER 9L FRAM E. INSTALLED DOUBLER PER SRM 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000010800352 20000108 00352 NM 2000 1 8 USAABB99053 1 19991110 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM ROW 18 MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 606AU 22202 CLT - FOUND FLOOR EMERGENCY LIGHT AT ROW 18 ILLUMINATED WITH THE SWITCH OFF. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2000010800353 20000108 00353 NM 2000 1 8 USAABB99049 1 19990916 A 3350 873100151REV9 LIGHT BOEING 757 7572B7 1384964 NM ROW6 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 LAX - FOUND ROW 6 AISLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 2000010800354 20000108 00354 NM 2000 1 8 USAABB99050 1 19991019 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 26 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 PHL - FOUND BATTERY DEAD ON LOW LEVEL EMERGENCY LIGHT AT ROW 26. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2000010800355 20000108 00355 2000 1 8 USAABB99055 4 19991103 A 3452 071015031501 ATC BOEING 767 767201 1385125 NM COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 648US 27941 23900 PHL-LGW - FLT 126 - CREW RECEIVED THE EICAS MESSAGE 'ATC FAULT' AND THE ASSOCIATED LIGHT. BOTH TRANSPONDERS WERE REPORT ED TO BE INOPERATIVE. AFTER CONFERRING WITH MAINTENANCE, THE FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER PROBLEMS . MAINTENANCE REPLACED THE ATC CONTROL PANEL. (M) 2 L 7 2 4F RT A1NM 2000010800356 20000108 00356 NM 2000 1 8 USAASB99272 1 19991117 A 2430 GCU BOEING 737 7372B7 1384560 NM E/E BAY MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 286AU 23133 TPA - FLT 2674 - FLIGHT LOST THE NR 1 TRANSFER BUS AND ALL INSTRUMENTS ON BOTH SIDES DURING ROTATION. CREW RESET THE NR 1 TRANSFER BUS CIRCUIT BREAKER WHICH BROUGHT BACK ALL INSTRUMENTS EXCEPT THE MACH AIRSPEED INDICATION. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCIDENT. NOEMERGENCY WAS DECLARED. MAINTENANCE RAN ENGINES AND EXERCISED BUS TRANSFER. COULD NOT DUPLIATE PROBLEM. RERACKED GCU. NO DEFECTS NOTED. AIRCRAFT OK FOR SER VICE. (M) 2 L 7 2 4F A16WE 2000010800357 20000108 00357 NM 2000 1 8 USAASB99269 1 19991106 A 3350 S106 BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 TPA - PILOT REPORTED THAT THE RIGHT AFT SERVICE DOOR EMERGENCY LIGHT REMAINS ILLUMINATED DURING FLIGHT. MAINTENANCE FOU ND THE LIGHT ASSEMBLY UNPLUGGED CAUSING THE LIGHT TO REMAIN ILLUMINATED. CONNECTED LIGHT ASSEMBLY AND FOUND THAT IT WOU LD NOT CHARGE. REPLACED BATTERY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2000010800358 20000108 00358 NM 2000 1 8 USAASB99270 1 19991108 A 3350 LIGHT BOEING 737 737301 1384611 NM ROWS 17/19C INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 353US 23556 TPA - MAINTENANCE FOUND THE EMERGENCY LIGHTING INOPERATIVE AT SEAT ROWS 17C AND 19C. MAINTENANCE REPAIRED BROKEN WIRES AT SEAT ROWS 17C AND 19C. OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 2000010800359 20000108 00359 NM 2000 1 8 USAASB99271 1 19991114 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 525AU 23860 ALB - MAINTENANCE FOUND THE BULLNOSE EMERGENCY EVACUATIONLIGHTS AT SEAT ROWS 11 AND 18 RIGHT, 13, 16 AND 20 LEFT, AND BO TH EXTERIOR EMERGENCY EVACUATION LIGHTS BELOW FLAPS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY PACK AT SEAT ROW 17. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2000010800360 20000108 00360 WP 2000 1 8 USAA991299 1 19991112 A 5210 DOOR PAN DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918VJ 44135 48138 PIT - DURING C-1 CHECK, FOUND APPROX 9 INCH CRACK ON PANEL ASSEMBLY UPPER FORWARD DOOR OF MED DOOR PAN. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 95269. (M) 2 L 7 2 4F A6WE 2000010800361 20000108 00361 WP 2000 1 8 USAA991298 1 19991112 A 5210 DOOR PAN DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918VJ 44135 48138 PIT - DURING C-1 CHECK, FOUND SMALL CRACK APPROX .25 INCH LONG AT FORWARD DOOR PAN AREA JUST ABOVE HINGE CLEARANCE CUT O UT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 95269. (M) 2 L 7 2 4F A6WE 2000010800362 20000108 00362 NM 2000 1 8 USAA119909 1 19991120 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS WA7282 21244 AISLE OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 2000010800363 20000108 00363 WP 2000 1 8 USAAD99165 1 19991121 A 3350 20131ALP BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959VJ 47352 DTW - THE FLOOR TRACK LIGHTING FROM SEAT ROW 15 AFT WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR TRACK LIGHT BAT TERY PACK.. (M) 2 L 7 2 4F A6WE 2000010800364 20000108 00364 WP 2000 1 8 AALA991664 1 19991106 A 3260 59516395001 BUNGEE DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 297AA EE13060 49309 EN ROUTE LGA-ORD - FLT 317 - NOSE GEAR RED WARNING LIGH TILLUMINATED DURING CRUISE BUT WNE TOUT WHEN HYDRAULIC PUMPS WER E SET TO HIGH. AIRCRAFT CONTINUED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR BUNGEE CYLINDER. PERFORMED N OSE GEAR RETRACTION CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000010800365 20000108 00365 NM 2000 1 8 USAABB99054 1 19991117 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AU 27201 PHL - FOUND R-4 DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 2000010800366 20000108 00366 NM 2000 1 8 USAASB99268 1 19991111 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISC HARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245US 22751 MCO - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS ATSEAT ROWS 8 THROUGH 16, LEFT SIDE, FAILED TO TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2000010800367 20000108 00367 SO 2000 1 8 ASOA990998 1 19990915 A 2120 UNKNOWN EMB 120 EMB120RT 3260202 SO COCKPI T SMOKE A ASOA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 502AS 120274 TEN MILES FROM MEL, SMOKE EVIDENT IN COCKPIT. CRWE REQUESTED PRIORITY TO LAND AND FIRE EQUIPMENT. SMOKE CLEARED FROM A IRCRAFT. UPON SHUTDOWN, FIRE CREW AND STATION AGENTS OBSERVED SMOKE 'BELLOWING' NEAR LEFT ACM. THE TEARDOWN REPORT STA TES THAT OBSERVED DAMAGE AND REASON FOR REMOVAL COULD HAVEBEEN CAUSED BY A HARD LANDING IN COMBINATION WITH NORMAL WEAR AT AND TEAR OVER THE TIME IN SERVICE SINCE PREVIOUS SHOP VISIT. MAINTENANCE SERVICED AIRCRAFT WIT H 5 QUARTS OF OIL. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000010800368 20000108 00368 NM 2000 1 8 WRLA99021 1 19991026 A 2500 TP4429X32930 PRINTER DOUG MD11 MD11 3023602 NM COCKPIT JAMMED A WRLA O OTHER M OVER TEMP CR CRUISE 1 EA 27 275WA 48631 DURING CRUISE, THE FIRST OFFICER FELT A HOT SPOT ON THE CONSOLENEAR THE MULTI-PURPOSE PRINTER. INVESTIGATION REVEALED B LACKENED PAPER AT THE PRINTER FEED. CIRCUIT BREAKERS WERE PULLED AND THE PAPER WAS REMOVED. THE FLIGH T CONTINUED TO DESTINATION WITHOUT FURTHER PROBLEMS AND ALL OPERATIONSNORMAL. MAINTENANCE COLLARED THE PRINTER CIRCUIT BREAKERS AND DEA CTIVATED THE PRINTER AN D ASSIGNED A DEFERRED MAINTENANCE ITEM. DMI 310C26-43. (M) 2 L 7 3 4F RT A22WE 2000010800369 20000108 00369 2000 1 8 USAASB99248 4 19991012 A 3425 172938001 RELAY BOEING 737 7373B7 1384580 NM E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 515AU 23701 PHL - FLT 346 - AFTER TAKEOFF THE CREW REPORTED THAT EVERYTIME THE STAB TRIM SWITCH WAS ACTUATED FROM EITHER YOKE, THE F IRST OFFICERS HSI HEADING FLAGS APPEARED. RELEASING THE SWITCH CAUSES THE FLAGS TO DISAPPEAR. DECISION WAS MADE TO RET URN TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX R & R THE NR 2 COMPASS TR ANSFER RELAY. OPS CHECK NORM. (M) 2 L 7 2 4F RT A16WE 2000010800370 20000108 00370 WP 2000 1 8 USAAD99166 1 19991121 A 2170 WATER SEPARATOR DOUG DC9 DC931 3022065 WP CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 939VJ 48120 AFTER TAKEOFF, THE FLT ATTENDANT REPORTED SMOKE AND FUME SMELL IN THE CABIN. THE ACFT RETURNED TO THE FIELD. MX CHECKE D BOTH AIR CYCLE MACHINES FOR FREE OPERATION. NO SMOKE OR SMELL WAS EVIDENT. THE AIR CONDITIONING WATER SEPARATOR BAG S WERE REPLACED AS PRECAUTION. (M) 2 L 7 2 4F A6WE 2000010800371 20000108 00371 EU 2000 1 8 USAAF99054 1 19991122 A 3350 6104789 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 16 866US 11310 FOUND EMERGENCY LIGHTS ONLY COME ON FOR 5 SECONDS AND THEN GO OUT. MX REPLACED THE BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT 2000010800372 20000108 00372 NM 2000 1 8 WRLA99020 1 19991027 A 3350 0105606203 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A WRLA K NONE L NO TEST IN INSP/MAINT 1 EA 27 271WA 48518 DURING ROUTINE MAINTENANCE, NOTICED EMERGENCY FLOOR LIGHTING INOPERATIVE IN 'B' ZONE. MX PERSONNEL REMOVED AND REPLACED LIGHT SEGMENTS. OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2000010800373 20000108 00373 WP 2000 1 8 G60A039 1 19991124 A 3350 EMBS1392 BATTERY DOUG DC10 DC1030 3023501 WP COCKPIT DISCHARGED A G6OA K NONE L NO TEST IN INSP/MAINT 1 EA 27 606GC 47929 EMERGENCY LIGHTS CIRCUIT WILL NOT TEST IN ARM POSITION. TRANSFERRED TO MEL/CDL LOG IAW GAC MEL 33-17-4, MEL CONTROL NR M606-3677, PLACARD NR 011108. (M) 2 L 7 3 4F A22WE 2000010800374 20000108 00374 WP 2000 1 8 G60A038 1 19991107 A 5520 NLC6041505 ELEVATORS DOUG DC10 DC1030F 3023504 WP LT WING DAMAGED A G6OA O OTHER F FLT CONT AFFECTED CL CLIMB 1 EA 27 602GC 47923 TCAS MADE CONTACT WHILE FLT GCO7580 WAS DEPARTING PHNL, AT APPROXIMATELY 3800 FT. FLIGHT CREW INITIATED EVASIVE MANEUVE R WHICH RESULTED IN STRUCTURAL DAMAGE TO BOTH LT AND RT ELEVATORS. (M) 2 L 7 3 4F RT A22WE 2000010800375 20000108 00375 WP 2000 1 8 2000ZZZM12 1 19991107 A 5520 NLC6041506 ELEVATORS DOUG DC10 DC1030F 3023504 WP RT WING DAMAGED A G6OA O OTHER F FLT CONT AFFECTED CL CLIMB 1 EA 27 602GC 47923 TCAS MADE CONTACT WHILE FLT GCO7580 WAS DEPARTING PHNL, AT APPROXIMATELY 3800 FT. FLIGHT CREW INITIATED EVASIVE MANEUVE R WHICH RESULTED IN STRUCTURAL DAMAGE TO BOTH LT AND RT ELEVATORS. (M) 2 L 7 3 4F RT A22WE 2000010800376 20000108 00376 WP 2000 1 8 G6OA037 1 19991012 A 3231 DOOR DOUG DC10 DC1030F 3023504 WP NLG LOOSE A G6OA O OTHER E VIBRATION/BUFFET CL CLIMB 1 EA 27 600GC 46965 ON GEAR RETRACTION ON DEPARTURE FROM KLAX, FELT SEVERE VIBRATIONIN NOSE GEAR AREA. ON ARRIVAL AT KSAN, FOUND RIGHT NOSE GEAR DOOR OPEN. INSPECTED NOSE GEAR DOORS AND LOCKING MECHANISMS IAW MM 32-21-00. RESECURED NOSE GEAR DOORS AND LOCKI NG MECHANISMS. NOSE LANDING GEAR DOORS FUNCTION CHECKS GOOD ON TEST FLIGHT. (M) 2 L 7 3 4F RT A22WE 2000010800377 20000108 00377 WP 2000 1 8 WRLA99019 1 19991027 A 5610 NBA60452 WINDSHIELD DOUG DC10 DC1030F 3023504 WP COCKPIT CRACKED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 107WA 46836 DURING CRUISE FLIGHT CREW NOTICE CRACK IN F/O WINDSCREEN STARTED SLIGHT 'ARCING' W/RIGHT ANTI-ICE IN NORM ABOUT 2 MIN AF TER START OF DESCENT. FLIGHT CREW SECURED RIGHT WINDSHIELD ANTI-ICE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. (M) MA INTENANCE PERSONNEL REMOVED AND REPLACED WINDSHIELD AND ANTI-ICE CONTROLLER. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 2000010800378 20000108 00378 NM 2000 1 8 USAA119911 1 19991129 A 5330 SKIN BOEING 727 727227 1384078 NM BS 345-380 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 SKIN EXTERIOR BETWEEN STRINGER 5L AND 7L STATION 345 TO 380 HAS DENTS AND GOUGES. INSTALLED FUSELAGE EXTERIOR SKIN REPA IR FROM BS 345 TO BS 380, STRINGER 5 TO STRINGER 7 LEFT. MATERIAL USED 2024-T3, .063 INCH, 13.75 INCH BY 7.75 INCH. RE PAIR ACCOMPLISHED IAW B727 SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 2000010800379 20000108 00379 NM 2000 1 8 USAA119912 1 19991129 A 5320 STIFFENER BOEING 727 727227 1384078 NM BS 1183 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FOUND DURING C-CHECK, AFT CARGO COMPARTMENT STATION 1183 BULKHEAD CRACK INDICATION AT WEB VERTICAL STIFFENER LOWER END L BL 8 INCHES WL 181. INSTALLED REPAIR KIT, P/N 65C29080-1, AT VERTICAL BEAM LOWER END BS 1183, LBL 8, WL 181 IAW BOEING SB 727-53-0175. (M) 2 L 7 3 4F A3WE 2000010800380 20000108 00380 NM 2000 1 8 USAA119913 1 19991129 A 5754 SKIN BOEING 727 727227 1384078 NM LE FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FOUND DURING C-CHECK, RIGHT WING OUTBOARD FLAP, FORE FLAP DOUBLER, ON FORE FLAP HAS LOOSE RIVETS AND CRACKED AREA OUTBOA RD FLAP TOGGLE CARRIAGE. INSTALLED DOUBLER REPAIR AT RIGHT WING OUTBOARD FLAP, FORE FLAP IAW SRM 57-50-4 FIG 1. MATERI AL USED, 2024-T3, 0.050 INCH, 10 INCH BY 7 INCH. (M) 2 L 7 3 4F A3WE 2000010800381 20000108 00381 NM 2000 1 8 USAA119914 1 19991129 A 5312 BULKHEAD BOEING 727 727227 1384078 NM BS 870 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FOUND DURING C-CHECK, RIGHT MAIN WHEEL WELL STATION 870, PRESSUER WEB HAS 3 INCH CRACK JUST OUTBOARD OF KEEL BEAM. INST ALLED WEB REPAIR AT RIGHT MAIN WHEEL WELL RIGHT OF STATION 870, LOWER WEB INBOARD. MATERIAL USED, 2024-T3, .040 INCH, 1 4 INCH BY 6 INCH. REPAIR ACCOMPLISHED IAW SRM 53-10-9 FIG 4. INSTALLED ALSO REPAIR DOUBLERS AT RIGHT WHEEL WELL STATIO N 870 PRESSURE WEB, RIGHT APU CUTOUT. MATERIAL USED, 15-5PH STEEL, .050 INCH, 12 INCH BY 6 INCH, 21 INCH BY 18.5 INCH. REPAIR ACCOMPLISHED IAW SRM 53-10-9 FIG 5. 9M0 2 L 7 3 4F A3WE 2000010800382 20000108 00382 NM 2000 1 8 USAA119915 1 19991129 A 5320 STIFFENER BOEING 727 727227 1384078 NM BS 1183 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 VERTICAL BEAM AT AFT PRESSURE BULKHEAD STATION 1183 LBL 18, HAS SPOT OF CORROSION AT TOP END. ACCOMPLISHED BS 1183 BULK HEAD, LBL 17.8 VERTICAL BEAM CORROSION BLEND OUT IAW BOEING TELEX TSI-MIA-00001H. (M) 2 L 7 3 4F A3WE 2000010800383 20000108 00383 NM 2000 1 8 USAA119916 1 19991129 A 5320 STIFFENER BOEING 727 727227 1384078 NM BS 1183 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 AFT CARGO COMPARTMENT AFT BULKHEAD STATION 1183, VERTICAL STIFFENER CRACKED AT LOWR END, LBL 8 AND RBL 8. INSTALLED KIT REPAIR AT BS 1183, LBL 8 AND RBL 8, VERTICAL BEAMS, LOWER END, IAW BOEING SERVICE BULLETIN 727-53-0175. KIT P/N 65CC90 80-1 AND 65C29080-2 INSTALLED. (M) 2 L 7 3 4F A3WE 2000010800384 20000108 00384 NM 2000 1 8 USAA119917 1 19991129 A 5330 SKIN BOEING 727 727227 1384078 NM BS 203 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FOUND DURING C-CHECK, EXTERIOR SKIN STATION AT 203 ACROSS STRINGER 19R LAP SEAM HAS ELONGATED DENT. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR AT BS 203, STRINGER 19 RIGHT IAW BOEING TELEX TSI-MIA-99-00002H, 8110-3 DATED NOV 22, 1999 ISSUED. MATERIAL USED , 2024-T3, .080 INCH, 9 INCH BY 14 INCH. (M) 2 L 7 3 4F A3WE 2000010800385 20000108 00385 NM 2000 1 8 USAA119918 1 19991129 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1130 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FOUND CORROSION AT STATION 1130 FLOORBEAM LOWER CHORD FROM AT RBL 48 TO BL 0. INSTALLED REPAIR AT STATION 1130 FLOORBEA M LOWER CHORD, FROM RBL 20 TO RBL 52. MATERIAL USED, 7075-T6, 090 INCH, 39 INCH LONG, P/N BAC1490-2831, 35 INCH LONG. A LSO, STATION 1130, RBL 1. MATERIAL USED, 7075-T6, .090 INCH, 20 INCH LONG, P/N BAC1490-2831, 16 INCH LONG. REPAIR ACCO MPLISHED IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM.078RO-1, REV 1R 8110-3 DATED NOVE 23, 1999 ISSUED. (M) 2 L 7 3 4F A3WE 2000010800386 20000108 00386 NM 2000 1 8 USAA119919 1 19991129 A 5720 65742844 BRACKET BOEING 727 727227 1384078 NM RT WING CHAFFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 RIGHT WING AFT SPAR AREA SPOILER BRACKET, FOUND AILERON CABLE CHAFFING INTO BRACKET JUST FORWARD OF INBOARD AILERON AT W ING STATION 410. ACCOMPLISHED REWORK OF RIGHT WING AFT SPAR SPOILER BRACKET, P/N 65-74284-4 IAW AVITAS ENGINEERING REPA IR ORDER 99 AVHM.081RO-1, REV 1R, 8110-3 DATED NOV 23, 1999 ISSUED. (M) 2 L 7 3 4F A3WE 2000010800387 20000108 00387 NM 2000 1 8 USAA99169 1 19991026 A 5320 STIFFENER BOEING 757 757225 1384959 NM BS 1360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 46040 22192 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2 INCH CORRODED AREA AT BS 1360, RBL 7 STIFFENER. CORROSION LEVEL 2. REPLACED STIFFENER PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2000010800388 20000108 00388 NM 2000 1 8 USAA991172 1 19991026 A 5320 TIE CLIP BOEING 757 757225 1384959 NM BS 1460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 46040 22192 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A ..5 INCH CRACK AT STATION 1460 STRINGER 2R AND STRINGER 3R TIE CLIP. R EPLACED TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2000010800389 20000108 00389 NM 2000 1 8 USAA991171 1 19991026 A 5320 TIE CLIP BOEING 757 757225 1384959 NM BS 1460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 46040 22192 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A ..2 5INCH CRACK AT BS 1460 STRINGER 1460 STRINGER 5R TIE CLIP. REPLAC ED TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2000010800390 20000108 00390 NM 2000 1 8 USAA991170 1 19991026 A 5320 TIE CLIP BOEING 757 757225 1384959 NM BS 1460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 46040 22192 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK AT BS 1460 STRINGER 5L TIE CLIP. REPLACED TIE CLIP PE R SRM 51-10-02. (M) 2 L 7 2 4F RT A2NM 2000010800391 20000108 00391 NM 2000 1 8 USAA119910 1 19991127 A 2611 824PY UNKNOWN BOEING 727 727227 1384078 NM LAVATORY SMOKE A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 927TS 20837 FOUND ON L/S CHECK, FORWARD LAVATORY SMOKE DETECTOR SOUNDS FOR NO REASONS. REPLACED FORWARD LAV SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 2000010800392 20000108 00392 WP 2000 1 8 GTIA9901200 1 19991108 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 MYR - FLT 538 - PATH LIGHT UP ROW 14. REATTACHED PATH LIGHTING TRACK. NO DEFECTS NOTED IAW DC9 MM 33-50-00. (M) 2 L 7 2 4F A6WE 2000010800393 20000108 00393 SO 2000 1 8 C2XA99BT111 1 19991121 A 3350 20157A POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 EWR - FLT 4145 - REAR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY POWR SUPPLY AND OPS CHECKED THE SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 2000010800394 20000108 00394 SO 2000 1 8 C2XA99BT110 1 19991121 A 4920 ENGINE EMB 145 EMB145 SO APU FAILED A C2XA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 09 14947 145054 EWR - FLT 4023 - CREW REPORTED SPARKS AND HOT METAL DEPARTING THE TAILPIPE OF APU SMOKE FILLED CABIN AND COCKPIT. EVACU ATION PERFORMED. AIRCRAFT APU PLACED ON MEL 49-00-00 AND RETURNED TO SERVICE. AWAITING APU CHANGE. (M) 2 L 7 2 4F RT T00011AT 2000010800395 20000108 00395 NM 2000 1 8 P2EA99355 1 19991130 A 5330 SKIN BOEING 737 737281 138448P NM BS 727-727A CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 727 TO BS 727A BETWEEN STRINGER 14 RT AND 16 RT. DEFECT SIZE LENGTH 1.75 I NCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 727 TO BS 727A PLUS 9.9, BETWEEN STRINGER 16 AND 20 RT PER BOEING FAX COO-S JO-990060 DATED DECEMBER 6, 1999 AND COOPESA EO COO-3-53-710-99 DATED DECEMBER 6, 1999. (M) 2 L 7 2 4F A16WE 2000010800396 20000108 00396 NM 2000 1 8 P2EA99354 1 19991203 A 5315 FLOORBEAM BOEING 737 737281 138448P NM BS 259.5 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, FLOORBEAM WEB CORRODED AT BS 259.5, FROM WL 208.5 TO WL 206, BETWEEN LBL 13 INCH TO RBL 13 INCH. DEFECT SIZE, LENGTH 16 INCHES, WIDTH 5 INCHES. REPAIRED FLOORBEAM WEB AT BS 259.5 BETWEEN LBL 17 INCH AND RBL 14.5 INCH FROM W L 208.5 TO WL 193. (M) 2 L 7 2 4F A16WE 2000010800397 20000108 00397 NM 2000 1 8 P2EA99352 1 19991201 A 5712 RIB BOEING 737 737281 138448P NM RT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK ITEM, SUPPORT RIB CRACKED AT RT WING SLAT STATION 25. DEFECT SIZE, LENGTH .75 INCH. REPLACED SLAT TRACK SUPPORT RIB AT SLAT STATION 25 PER SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 2000010800398 20000108 00398 NM 2000 1 8 P2EA99351 1 19991203 A 5315 FLOORBEAM BOEING 737 737281 138448P NM BS 259.5 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, FLOORBEAM CORROSION AT BS 259.5, WL 208.5, BETWEEN LBL 20 AND RBL 15 INCHES. DEFECT SIZE, LENGTH 14 INCH ES, WIDTH 4 INCHES. REPAIRED FLOORBEAM ANGLE AT BS 259 FROM LBL 23 INCHES TO RBL 21.5 INCHES WL 208. ALSO, REPLACED FL OOR BEAM UPPER ANGLE AT BS 259 FROM LBL 23.5 TO RBL 23.5, WL 208. (M) 2 L 7 2 4F A16WE 2000010800399 20000108 00399 NM 2000 1 8 P2EA99350 1 19991203 A 5320 ANGLE BOEING 737 737281 138448P NM BS 270 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, FLOOR SUPPORT ANGLE CORRODED AT BS 270, WL 208.5, BETWEEN RBL 17 INCHE LBL 10 INCH. DEFECT SIZE, LENGTH 10 INCH, WIDTH 2 INCH. REPAIRED FLOOR SUPPORT ANGLE AT BS 270, WL 208.5, BETWEEN LBL 54 INCH TO RBL 25.5 INCH PER COOPE SA EO COO-3-53-714-99 DATED DECEMBER 8, 1999. (M) 2 L 7 2 4F A16WE 2000010800400 20000108 00400 NM 2000 1 8 P2EA99348 1 19991203 A 5753 65719301 SKIN BOEING 737 737222 1384473 NM LT WING DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - LEFT WING OUTBOARD FLIPPER FLAPPER DELAMINATED. DEFECT SIZE, LENGTH 9 INCH, WIDTH 7.25 INCH. REPAIRED FLIPPER FL APPER PER COOPESA EO COO-CMP-3-57-711-99, DATED DECEMBER 7, 1999. (M) 2 L 7 2 4F A16WE 2000010800401 20000108 00401 NM 2000 1 8 P2EA99347 1 19991130 A 5230 FRAME BOEING 737 737222 1384473 NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - FORWARD CARGO DOOR FRAME CRACKED AT AFT FRAME, DEFECT SIZE, LENGTH .750 INCH. REPAIRED FORWARD CARGO DOOR BETWEEN BEAM NR 1 AND BEAM NR 3 PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 2000010800402 20000108 00402 NM 2000 1 8 P2EA99346 1 19991130 A 5711 RIB BOEING 737 737222 1384473 NM RT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - SLAT TRACK RIB CRACKED AT RIGHT WING FRONT SPAR SS356. DEFECT SIZE, LENGTH 1.5 INCH, WIDTH .32 INCH. REPLACED RI B AT SS 356 OUTBOARD TRACK PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000010800403 20000108 00403 NM 2000 1 8 P2EA99345 1 19991201 A 5242 SKIN BOEING 737 737281 138448P NM E/E DOOR DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, E/E DOOR HAS A DENT OUT OF LIMITS, DEFECT SIZE, LENGTH 1.75 INCH, WIDTH 1.5 INCH, DEPTH .045 INCH. REPLA CED DOOR SKIN PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000010800404 20000108 00404 NM 2000 1 8 P2EA99349 1 19991214 A 2420 941D3391 TRANSFORMER BOEING 737 737247 138448D NM E/E BAY FAILED A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK O S OTHER AFFECT SYSTEMS TO TAKEOFF 1 CE 05 912MP 19607 FLT 612 - MCI - NR 1 GENERATOR AND ASSOCIATED BUS DROPPED OFF LINE DURING TAKEOFF. TAKEOFF ABORTED AT APPROX 50 KTS.. R ETURNED TO GATE. DEFERRED NR 1 GENERATOR PER MEL 24-1. REMOVED AND REPLACED CURRENT TRANSFORMER PER MM. OPERATION NOR MAL. (M) 2 L 7 2 4F A16WE 2000010800405 20000108 00405 NM 2000 1 8 P2EA99344 1 19991203 A 5311 FRAME BOEING 737 737222 1384473 NM BS 967 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - C-CHECK, FRAME CRACKED AT BS 967, BETWEEN STRINGER 20/21LT. DEFECT SIZE, LENGTH 3.5 INCH, WIDTH .16 INCH, DEPTH . 63 INCH. REPAIRED FUSELAGE SECTION AT BS 967, BETWEEN STRINGER 19 AND 21 LEFT PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 2000010800406 20000108 00406 WP 2000 1 8 HALA9900241 1 19991123 A 2430 TRU DOUG DC10 DC1010 3022110 WP E/E BAY FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 171AA 46906 LAX - (ATB) APPROXIMATELY ONE HOUR AFTER TAKEOFF LAX, LOST DC BUS 1 AND L EMERGENCY DC BUS. RESET T/R 1 OUTPUT AND T/R 1 INPUT. OPS BACK TO NORMAL. NR 1 T/R. UNIT OPS CHECKED NORMAL. SYSTEM OK FOR SERVICE. (X) 2 L 7 3 4F A22WE 2000010800407 20000108 00407 NM 2000 1 8 AALA991890 1 19991210 A 3350 0105924005 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 777AN 29585 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT NEAR FORWARD LEFT BULKHEAD INOPERATIVE. REPLACED EMERGENCY EXI T LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 2000010800408 20000108 00408 NM 2000 1 8 AALA991823 1 19991201 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 679AN 29589 DFW - DURING OVERNIGHT MAINTENANCE, AISLE EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 12-18D INOPERATIVE. RECONNECTE D EMERGENCY EXIT FLOOR PATH LIGHTING WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION.. (M) 2 L 7 2 4F RT A2NM 2000010800409 20000108 00409 NM 2000 1 8 AALA991858 1 19991206 A 3350 SWITCH BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 696AN 26976 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS TEST SWITCH AT FORWARD ATTENDANT PANEL DOES NOT ILLUMINATE. REPLAC ED EMERGENCY LIGHT TEST SWITCH AT FORWARD ATTENDANT PANEL. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2000010800410 20000108 00410 NM 2000 1 8 AALA991852 1 19991204 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 657AM 24615 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS NEAR AFT LAVATORY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEAR AFT LAVATORY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2000010800411 20000108 00411 NM 2000 1 8 AALA991877 1 19991207 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 376AN 25445 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT BEHIND SECOND CLASS GALLEY BROKEN. REPLACED EMERGENCY EXI T PATH LIGHT STRIP BEHIND SECOND CLASS GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2000010800412 20000108 00412 NM 2000 1 8 AALA991876 1 19991207 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 376AN 25445 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 9AB INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 9AB CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2000010800413 20000108 00413 NM 2000 1 8 AALA991873 1 19991207 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39365 24046 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTS AT SEAT 36B INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 2000010800414 20000108 00414 NM 2000 1 8 AALA991894 1 19991213 A 2530 8609010000 OVEN BOEING 767 767323 1385205 NM GALLEY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 379AA 25448 LHR - FLT 136 - DURING FLIGHT FIRST CLASS OVEN SMOKES. CLEANED DEBRIS FROM FIRST CLASS OVEN. SYSTEM GROUND CHECK NORMA L OPERATION. (M) 2 L 7 2 4F RT A1NM 2000010800415 20000108 00415 WP 2000 1 8 AALA991889 1 19991212 A 3350 P4010051111 CONTROLLER DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 413AA 49324 SAN - FLT 692 - DURING TEST EMERGENCY EXIT FLOOR PATH LIGHTS FORWARD OF WING INOPERATIVE. REPLACED AISLE PATH LIGHTING CONTROL MODULE. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000010800416 20000108 00416 WP 2000 1 8 AALA991888 1 19991211 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 598AA 53288 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT PATH FLOOR LIGHTS OVERWING EXIT TO AFT DOOR INOPERATIVE. REPAIRED WIR ING TO EMERGENCY EXIT PATH FLOOR LIGHTS OVERWING EXIT TO AFT DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2000010800417 20000108 00417 WP 2000 1 8 AALA991887 1 19991210 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 579AA 53156 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT STAIRWAY INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CONNECTOR IN AFT STAIRWAY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000010800418 20000108 00418 WP 2000 1 8 AALA991893 1 19991213 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 426AA 49338 DFW - DURING OVERNIGHT MAINTENANCE, TAILCONE EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE TO TAILCONE EMEREGNCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000010800419 20000108 00419 WP 2000 1 8 AALA991896 1 19991114 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 426AA 49338 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN CEILING JUST FORWARD OF AFT STAIR DOOR INOPERATIVE. REPAIRE D WIRING FOR EMERGENCY EXIT LIGHT IN CEILING JUST FORWARD OF AFT STAIR DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000010800420 20000108 00420 WP 2000 1 8 AALA991900 1 19991205 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 826 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 467AA 49597 TUL - SEAT TRACK CORRODED NR 6 STATION 826. REMOVED AND REPLACED SEAT TRACK SECTION STATION 795 THROUGH STATION 1030 PE R SRM 51-10 PAGE 1. (M) 2 L 7 2 4F A6WE 2000010800421 20000108 00421 WP 2000 1 8 AALA991899 1 19991206 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 218-237 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 467AA 49597 TUL - FOUND CORROSION ON SEAT TRACK NR 5 BETWEEN STATION 218 AND STATION 237. INSTALLED NEWS TRACK PER SRM 51-10 PAGE 1 . (M) 2 L 7 2 4F A6WE 2000010800422 20000108 00422 SO 2000 1 8 2000ZZZM13 1 19991203 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN FAILED A GLBA K NONE L NO TEST IN INSP/MAINT 1 CE 01 71GL 120071 INTERIOR EMERGENCY EXIT LIGHT NEAR PASSENGER DOOR INOPERATIVE. REPAIRED GROUND WIRE AT LIGHT ASSEMBLY. (M) 2 L 7 2 4T RT A31SO 2000010800423 20000108 00423 NM 2000 1 8 SCNA00001 1 19991228 A 3350 HARNESS BOEING 727 727259 138408J NM ROWS 1 - 15 INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 20765 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR PATH LIGHTING FROM ROWS 1 THROUGH 15 WAS FOUND INOPERATIVE. REMOVE D AND REPLACED ELECTRICAL HARNESS AT 3A. ALL EMERGENCY LIGHTS CHECK GOOD. 2 L 7 3 4F A3WE 2000010800437 20000108 00437 EA 2000 1 8 COMA0060003 1 19990102 A 5320 DOUBLER CNDAIR CL600 CL6002B19 EA BS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 712CA 3915 7244 RIGHT FRAME AT FS 718, STR 11, HAS A CRACKED DOUBLER ON AFT SIDE. REPAIRED IAW REO 601R-53-61-193 REV A. 2 L 7 2 4F RT A21EA 2000010800439 20000108 00439 EA 2000 1 8 COMA0060005 1 19991227 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 964CA 7129 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 2000010800440 20000108 00440 EA 2000 1 8 COMA0060006 1 19991228 A 2613 356024310 DETECTOR CNDAIR CL600 CL6002B19 EA LT ENGINE MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 963CA 7127 LEFT 14TH STAGE BLEED AIR DUCT LEAK WARNING. REPLACED FAULTY BLEED AIR LEAK DETECTOR. 2 L 7 2 4F RT A21EA 2000010800441 20000108 00441 EA 2000 1 8 COMA0060007 1 19991227 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 975CA 7150 LEFT WINDOW HEAT CAUTION MESSAGE. COULD NOT DUPLICATE, OPERATIONAL CHECK OF WINDOW HEAT SATISFACTORY. 2 L 7 2 4F RT A21EA 2000010800442 20000108 00442 EA 2000 1 8 COMA0060008 1 19991227 A 3010 AL00102 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 EA RUDDER MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 01 806CA 13957 7359 RIGHT WING ANTI-ICE DUCT WARNING. REPOSITIONED WIRE TERMINAL AT T/B 44WK THAT WAS SHORTED TO GROUND. 2 L 7 2 4F RT A21EA 2000010800443 20000108 00443 EA 2000 1 8 COMA0060009 1 19991228 A 2721 AL00102 TRIM ACTUATOR CNDAIR CL600 CL6002B19 EA RUDDER MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 933CA 13957 7040 RUDDER TRIM INDICATOR SHOWED FULL SCALE LEFT DEFLECTION. REPLACED THE RUDDER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 2000010800444 20000108 00444 NM 2000 1 8 9905436305 1 19991226 A 2612 RELAY BOEING 747 747451 1384940 NM MLG WW FAILED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 665US 23820 DURING TAKEOFF, THE WHEEL WELL FIRE WARNING ACTIVATED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDE NT. REPLACED R8048 RELAY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2000010800446 20000108 00446 NM 2000 1 8 UPS00231254 1 19991229 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 490 - 550 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI CRACKED FASTENER HOLES IN STR 1 BETWEEN BS 490 AND BS 540. REMOVED STRINGER 1 FROM BS 490 TO BS 550. FABRICATED NEW STRINGER AND REPAIR PARTS AND INSTALLED PER SRM 53-10-2 SRM 51-30-2, SRM 53-10-1 SRM 53-10-3. 2 L 7 3 4F A3WE 2000010800447 20000108 00447 NM 2000 1 8 UPS00231255 1 19991227 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 490 - 540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI CRACKED FASTENER HOLES IN STR 3 RT BETWEEN BS 490 AND BS 540. CUT OUT DAMAGED STRINGER FROM BS 490 T O BS 550, STR 3 RT. FABRICATED NEW STRINGER COLD FORMED NEW STRINGER AT JOGGLED AREAS AND FABRICATED STRINGER REPAIR SP LICES ALODINED PRIMED AND INSTALLED ALL PARTS IAW SRM 5 3-10-3, SRM 51-30-2, SRM 51-10-2. 2 L 7 3 4F A3WE 2000010800450 20000108 00450 NM 2000 1 8 CALA9901740 1 19991231 A 2530 8201110000A OVEN SELL BOEING 737 737724 NM GALLEY INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 13750 2117 28941 THE NR 2 OVEN IN FORWARD GALLEY BEGAN TO PRODUCE SMOKE WITH AN ELECTRICAL ODOR WHILE EN ROUTE TO IAH. THE OVEN CIRCUIT BREAKER WAS PULLED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO IAH WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE FORWARD GALLEY NR 2 OVEN WAS REMOVED AND REPLACED. THE OVEN WAS OPERATED FOR SEVERAL MINUTES WI TH NO FAULTS FOUND. NO OTHER DEFECTS WERE NOTED. 2 L 7 2 4F RT A16WE 2000010800451 20000108 00451 NM 2000 1 8 CALA9901742 1 19991229 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 380 - 400 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 380-400, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WA S INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2000010800452 20000108 00452 NM 2000 1 8 CALA9901743 1 19991229 A 5350 FAIRING SUPPORT BOEING 727 727232 1384082 NM BS 720F CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT LOWER BODY FAIRING 3441 SUPPORT NR 7 CORRODED AT STA 720F, S26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 2000010800453 20000108 00453 NM 2000 1 8 CALA9901745 1 19991229 A 5315 BULKHEAD BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 4 CRACK IN WEB AT AFT PRESSURE BULKHEAD STA 1183, STRINGER 2L FITTING. THE CRACK WAS STOP DRILLED IA W ECRA 5310-03958 AND A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY 3000 CYCLES. 2 L 7 3 4F A3WE 2000010800454 20000108 00454 NM 2000 1 8 CALA9901746 1 19991230 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 643 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT ANGLE CORRODED UNDER NUTPLATES AT STA 643, LBL 9. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT AND ANGLES WERE INSTALLED IAW SRM 51-40-4 AND 51-30-2. 2 L 7 3 4F A3WE 2000010800455 20000108 00455 NM 2000 1 8 CALA9901747 1 19991230 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 650 BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT BENT AT STA 650, LBL 3. THE BENT SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-40-4, FIGURE 1. 2 L 7 3 4F A3WE 2000010800456 20000108 00456 NM 2000 1 8 CALA9901748 1 19991230 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1110 - 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND SEAT TRACK CORRODED AT FS 1110-1130, RBL 22. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 2000010800457 20000108 00457 NM 2000 1 8 CALA9901749 1 19991230 A 5210 DOOR PAN BOEING 727 727232 1384082 NM PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 1 INCH CRACK IN L-2 CABIN DOOR AT UPPER PAN AREA NEAR HINGE FITTING. THE AREA WAS REPAIRED IAW SRM 5 1-40-2. 2 L 7 3 4F A3WE 2000010800458 20000108 00458 NM 2000 1 8 CALA9901750 1 19991230 A 5311 FRAME BOEING 727 727232 1384082 NM BS 640 BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FRAME BENT AT FS 640 BETWEEN LONGERON 26 AND 27R. THE FRAME WAS REPAIRED IAW EA 27-5311-2-A0538 AND EC RA 5310-03968. 2 L 7 3 4F A3WE 2000010800459 20000108 00459 NM 2000 1 8 CALA9901751 1 19991230 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER T-CHORD AT STA 1130, BL 0 TO O/B RT SIDE. THE FLOORBEAM WAS REPAIRED IAW E CRA 5310-03965 AND EA 27-5310-2-A0548. 2 L 7 3 4F A3WE 2000010800460 20000108 00460 NM 2000 1 8 CALA9901752 1 19991230 A 5320 WEB BOEING 727 727232 1384082 NM BS 1188 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 4 INCH CRACK IN CUSP WEB AT TOP OF BULKHEAD AT VERTICAL SUPPORT, FS 1188, RBL 20. THE CUSP WEB WAS R EMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2000010800461 20000108 00461 NM 2000 1 8 CALA9901753 1 19991230 A 5311 FRAME BOEING 727 727232 1384082 NM BS 880 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT FS 880 BETWEEN STRINGER 18R AND 17R. THE CRACK WAS STOP DRILLED IAW SRM 51- 10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 2000010800462 20000108 00462 NM 2000 1 8 CALA9901755 1 19991230 A 5320 SUPPORT BOEING 727 727232 1384082 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND RT AFT LAV FORWARD WALL FLOOR SUPPORT CORRODED. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 2000010800463 20000108 00463 NM 2000 1 8 CALA9901756 1 19991230 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FLOORBEAM UPPER T-CHORD CORRODED AT STA 1166, BL O TO O/B RT SIDE. THE CORROSION WAS REMOVED IAW SRM 5 1-10-6. AN ANGLE REPAIR WAS INSTALLED IAW ECRA 5310-03961. 2 L 7 3 4F A3WE 2000010800464 20000108 00464 NM 2000 1 8 CALA9901757 1 19991230 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 643 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT ANGLE CORRODED UNDER NUTPLATE AT FS 643, LBL 13. THE FLOOR SUPPORT ANGLE W AS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-4, AND MM 51-20-0. 2 L 7 3 4F A3WE 2000010800465 20000108 00465 NM 2000 1 8 CALA9901758 1 19991230 A 5755 651734866 PANEL BOEING 727 727232 1384082 NM SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND LT WING NR 6 SPOILER PANEL UPPER SURFACE CORRODED. THE SPOILER PANEL WAS REMOVED, REPAIRED, AND REINST ALLED IAW SRM 57-50-6 AND MM 27-62-1. 2 L 7 3 4F A3WE 2000010800466 20000108 00466 NM 2000 1 8 CALA9901759 1 19991230 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 113 0 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33785 20640 INSPECTION FOUND A 3 INCH CRACK IN RT FLOOR SUPPORT ANGLE AT CUSP WEB, FS 1130, STRINGER 17R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 2000010800467 20000108 00467 NM 2000 1 8 AWXA9900500 1 19991229 A 3246 26010452 WHEEL BOEING 737 7372E3 NM NLG UNBALANCED A AWXA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 WP 28 138AW 350 22792 EMERGENCY LANDING DECLARED, AT V1 PHX, THE NOSE WHEEL FELT OUT OF BALANCE, SUSPECT FLAT TIRE. REMOVED AND REPLACED BOTH NLG WHEEL AND TIRE ASSEMBLIES (LT S/N 3248 TOT 22044, RT S/N 6128 TOT 68142). WHEELS WERE REPLACED 13 NOV 99. A/C ALS O HAS HISTORY OF NLG STRUT BOTTOMING ON TAKEOFF AND LANDING. 2 L 7 2 4F RT A16WE 2000010800468 20000108 00468 NM 2000 1 8 AWXA9900501 1 19991229 A 5320 6546595 TIE BOEING 737 73733A 1384673 NM BS 727A CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509AW 23636 AFT CARGO BAY AT STA 727A, STR 25L CRACKED SUPPORT. REMOVED STRINGER TIE BRACKET PER B737 SRM 51-40-02. FABRICATED REP LACEMENT BRACKET PER B737 SRM 51-30-01 AND INSTALLED PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2000010800469 20000108 00469 NM 2000 1 8 AWXA9900502 1 19991229 A 5320 65C807351 MOP SILL BOEING 737 73733A 1384673 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509AW 23636 SURFACE CORROSION ON O/B FLOOR SUPPORT FROM R-2 DOOR CUT-OUT TO R-2 CUT-OUT AFT PAST STA BEAM 986.5 (MOP SILL). REMOVED AND REPLACED R-2 MOP SILL IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2000010800474 20000108 00474 NM 2000 1 8 VNAA9912014 1 19991229 A 3020 001A716AE1000010 DEICE SYSTEM DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 457PS 9814 3048 DURING TAKEOFF, THE CREW RECEIVED A LEFT ENGINE INTAKE DE-ICE FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND CLEARED TH E RUNWAY. THE CREW COULD VISUALLY VERIFY THAT THE DE-ICE BOOT WAS INDEED INFLATING. THE CREW CONTACTED MAINTENANCE CON TROL AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4026 DEPARTED THE FIELD AND CONTINUED TO PIT WITHOUT ANY FURTH ER INCIDENTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2000010800475 20000108 00475 NM 2000 1 8 VNAA9912015 1 19991229 A 2430 8160121 GENERATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 458PS 7928 29 3068 DURING TAKEOFF, THE CREW RECEIVED A LEFT GENERATOR FAIL MESSAGE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. TH E CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RESET THE GENERATOR. MAINTENANCE CONTROL CLEARED THE AIRCRAFT FOR ANOT HER TAKEOFF ATTEMPT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2000010800476 20000108 00476 NM 2000 1 8 TWAA0000101 1 19991230 A 3350 767 LAMP BOEING 757 757231 1384950 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 720TW 30319 THE EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE AT THE LEFT SIDE NUMBER 3 DOOR AND THE RIGHT SIDE NUMBER 1 DOOR. REPLACE D THE LAMP AT BOTH LOCATIONS. NO CHECK-C. 2 L 7 2 4F RT A2NM 2000010800478 20000108 00478 WP 2000 1 8 TWAA0000103 1 19991231 A 3350 LAMP DOUG DC9 DC983 3022083 WP ROW 20 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 982TW 53632 THE EGRESS LIGHTING WAS INOPERATIVE AROUND CABIN ROW 20. SECURED A LOOSE LAMP IN THE CONNECTOR. NO CHECK-C. 2 L 7 2 4F RT A6WE 2000010800479 20000108 00479 WP 2000 1 8 TWAA0000104 1 19991014 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 503 GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND A 2 INCH BY 2 1/2 INCH GOUGE AND TEAR IN THE FUSELAGE SKIN AT STA 503, LONGERON 20R. CU T OUT DAMAGED SKIN AND REPAIRED PER SRM 53-04, FIG 12B, SHEET 5. 2 L 7 2 4F A6WE 2000010800480 20000108 00480 WP 2000 1 8 TWAA0000105 1 19991019 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 1019 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD, STA 1019 LT SIDE JUST BELOW APU POWER LINE FEED THROUGH. REMOVED CORROSION PER SPM 6-80-01. 2 L 7 2 4F A6WE 2000010800481 20000108 00481 WP 2000 1 8 TWAA0000106 1 19991014 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 1017 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CORROSION AROUND THE AFT PRESSURE BULKHEAD. CORROSION WAS ON THE FINGER DOUBLER ON BULK HEAD AT STA 1017, LBL 25 INCHES. REMOVED CORROSION PER SPM 6-80-01. 2 L 7 2 4F A6WE 2000010800482 20000108 00482 WP 2000 1 8 TWAA0000107 1 19991006 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND INTERNAL STRUCTURE INBD OF WINDSHIELD WIPER MOTOR ACCESS WITH MFG PN 9911505-7 FRAME WIT H 1 1/2 INCH LONG CRACK IN RADIUS AT X=+1, STA 83.5. REMOVED AND REPLACED FRAME PER MO 72N37. 2 L 7 2 4F A6WE 2000010800483 20000108 00483 WP 2000 1 8 TWAA0000108 1 19991006 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 83.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND RT NOSE SECTION INTERNAL STRUCTURE, AS VIEWED INSIDE WINDSHIELD WIPER MOTOR ACCESS, HAD MFG PN 9911505-7 FRAME CRACKED AT X=-10, 1 1/2 INCHES LONG IN RADIUS AND 1 1/2 IN LONG BETWEEN 3 RIVETS AT STA 83.5. TW O EACH PLACES. REMOVED AND REPLACED FRAME PER MO 72N37. 2 L 7 2 4F A6WE 2000010800485 20000108 00485 WP 2000 1 8 TWAA0000110 1 19991230 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 639 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 924L 47324 DURING CHECK-C MAINT, FOUND IN THE FUSELAGE INTERIOR, BOTH FLANGES OF LONGERON 5L AT STA 639 WERE CRACKED APPROX 1/2 INC H LONG. REMOVED THE DAMAGED SECTION OF LONGERON AND FABRICATED A SECTION OF NEW LONGERON. LONG SPLICED AND INSTALLED P ER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 2000010800486 20000108 00486 WP 2000 1 8 TWAA0000112 1 19991215 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP BS 1380 CHAFED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 913TW 49184 DURING CHECK-C MAINT, THE AFT ACCESSORY COMPARTMENT AT STA 1380 BULKHEAD, HAD WORN AREA THROUGH WEB BELOW LONGERON 4L. R EPAIRED BULKHEAD PER SRM 53-01, FIG 2 SHEET 3 PAGE 9. DOUBLER TREATED AND PRIMED PER SRM 51-10-03, PAGE 16 AND 18. 2 L 7 2 4F A6WE 2000010800487 20000108 00487 NM 2000 1 8 TWAA0000111 1 19991129 A 5754 PATCH BOEING 767 767231 1385131 NM LE FLAP LOOSE A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 610TW 22573 DURING CHECK-C MAINT, THE PATCH ON THE LEFT WING NUMBER 6 LE SLAT, TOWARD THE OTBD END, WAS COMING LOOSE AT THE EDGES. I NSTALLED A 4 1/2 IN DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10. ALSO SEALED EDGES. 2 L 7 2 4F RT A1NM 2000010800488 20000108 00488 NM 2000 1 8 QXEA9902718 1 19991223 A 5400 WEB DHAV DHC8 DHC8102 2809003 NM RT NACELLE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN286.0 . REPAIRED IAW DHC-8 SRM 51-40-4. 2 H 7 2 4T RT A13NM 2000010800489 20000108 00489 NM 2000 1 8 QXEA9902719 1 19991216 A 3233 FITTING DHAV DHC8 DHC8102 2809003 NM MLG ACTUATOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - LEFT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER. REPAIRED IAW HORIZON AIR E A 9-54-233 AND EA 9-54-233A. 2 H 7 2 4T RT A13NM 2000010800490 20000108 00490 NM 2000 1 8 QXEA9902720 1 19991216 A 3233 FITTING DHAV DHC8 DHC8102 2809003 NM MLG ACTUATOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER MOUNTING PADS. REPAIRED IA W HORIZON AIR EA 9-54-233 AND EA 9-54-233A. 2 H 7 2 4T RT A13NM 2000010800491 20000108 00491 EU 2000 1 8 QXEA9902721 1 19991219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU 16660 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 16660 HAS NICKS AND GOUGES ON UPPER FLANGE BETWEEN STRINGERS 33 AND 36. REPAIRED IAW FOKKER SRM 51-10-4, PA RAGRAPH 4B AND 3C. 2 L 7 2 4F RT A20EU 2000010800492 20000108 00492 EU 2000 1 8 QXEA9902722 1 19991230 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - BRACKET FOR NR 1 DC IGNITION UNIT BETWEEN STRINGERS 26 AND 27 IS CRACKED AT THE FORWARD END. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2000010800493 20000108 00493 EU 2000 1 8 QXEA9902724 1 19991219 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 16660 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 16660 HAS A CHAFE ON THE TOP FLANGE AT STRINGER 27. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 A- C. 2 L 7 2 4F RT A20EU 2000010800494 20000108 00494 EU 2000 1 8 QXEA9902725 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 8305 - 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON INBOARD FLANGE OF LEFT INBOARD SEAT TRACK BETWEEN FRAME 8305 AND 8805. REPAIRED IAW FOKKER SRM 51-10 -4. 2 L 7 2 4F RT A20EU 2000010800495 20000108 00495 EU 2000 1 8 QXEA9902726 1 19991225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 8805 - 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRETTING CORROSION ON INBOARD FLANGE OF LEFT SEAT TRACK BETWEEN FRAMES 8805 AND 9305. REPAIRED IAW FOKKER SRM 51- 10-4 AND HORIZON AIR EA 4-53-946. 2 L 7 2 4F RT A20EU 2000010800496 20000108 00496 EU 2000 1 8 QXEA9902727 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305 - 9305A CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON INBOARD FLANGE OF LEFT INBOARD SEAT TRACK BETWEEN FRAMES 9305 AND 9305A. 2 L 7 2 4F RT A20EU 2000010800497 20000108 00497 EU 2000 1 8 QXEA9902728 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305B CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON INBOARD FLANGE OF LEFT INBOARD SEAT TRACK JUST FORWARD OF FRAME 9305B. REPAIRED IAW FOKKER SRM 51-10 -4. 2 L 7 2 4F RT A20EU 2000010800498 20000108 00498 EU 2000 1 8 QXEA9902729 1 19991230 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305B CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACK IN VERTICAL SUPPORT INBOARD SIDE FOR LEFT INBOARD SEAT TRACK AT FRAME 9305B. REPAIRED IAW FOKKER SRM 51-31- 01. 2 L 7 2 4F RT A20EU 2000010800499 20000108 00499 EU 2000 1 8 QXEA9902730 1 19991225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 10746 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - NUMEROUS CORRODED SPOTS ON INBOARD FLANGE OF LEFT INBOARD SEAT TRACK BETWEEN FRAMES 10746 THROUGH 14755. REPAIRED IAW HORIZON AIR EA 4-53-946. 2 L 7 2 4F RT A20EU 2000010800500 20000108 00500 EU 2000 1 8 QXEA9902731 1 19991222 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU BS 4805 - 5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON TOP OF CENTER BEAM BETWEEN FRAMES 4805 AND 5305. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2000010800501 20000108 00501 EU 2000 1 8 QXEA9902732 1 19991226 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4610 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - NUT PLATE CORRODED ON OUTBOARD FLANGE OF RIGHT INBOARD SEAT TRACK, AFT OF FRAME 4610. REPAIRED IAW FOKKER SRM 51- 31-01. 2 L 7 2 4F RT A20EU 2000010800517 20000108 00517 NM 2000 1 8 S84A990006 1 19991202 A 3350 MS1557081 BULB BOEING 727 727251 138408H NM CABIN FAILED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 20289 FORWARD EXTERIOR REAR EXIT LIGHT OUT (LEFT SIDE). RELAMPED. OPS CHECKED OK. (X) 2 L 7 3 4F A3WE 2000010800518 20000108 00518 NM 2000 1 8 S84A9900005 1 19990102 A 3350 1315 BULB BOEING 727 727251 138408H NM CABIN FAILED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 267US 20289 R1 DOOR EMERGENCY EXIT LIGHT INOPERABLE (OVER DOOR). RELAMPED. OPS CHECKED GOOD. (X) 2 L 7 3 4F A3WE 2000010800519 20000108 00519 NM 2000 1 8 S84A9900004 1 19991203 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A S84A K NONE O OTHER IN INSP/MAINT 1 EA 21 267US 20289 RIGHT AFT EMERGENCY EXIT LIGHT OUT (EXTERIOR). (X) 2 L 7 3 4F A3WE 2000010800531 20000108 00531 NE 2000 1 8 2000ZZZX71 2 19991013 A 7260 M61171 HOUSING BOMBDR BD700 BD7001A10 1390006 GL RROYCE BR700 BR700710A220 09500 NE ACCY GEARBOX CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 89 12111 (CAN) CRACK FOUND ADJACENT TO HYDRAULIC PUMP MOUNTING POSITION FORWARD FACE ON ACCESSORY GEARBOX. PART TOTAL CYCLES: 3 4. (X) 2 L 7 2 4F 4 F RT T00003NY E00061EN 2000010800538 20000108 00538 2000 1 8 R7MA0000827 4 19990913 A 3455 FACEPLATE AGUSTA A109 A109K2 0260502 EU ADF SWITCH DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 123RX 10018 FACEPLATE DAMAGED AND UNREADABLE. P/N 58410A2B2C2D2F4L9N2. (X) 1 G 7 2 3U RT H7EU 2000010800540 20000108 00540 2000 1 8 R7MA0000824 4 19991103 A 3413 1013800059 TRANSDUCER BEECH 200 200BEECH 1152920 CE COCKPIT MALFUNCTIONED A R7MA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 11 501HC 3860 3398 BB1306 TRANSDUCER INDICATES WARNING 25-30 KNOTS EARLY. (X) 1 L 7 2 4T A24CE 2000010800541 20000108 00541 2000 1 8 R7MA0000828 4 19990913 A 3455 FACEPLATE AGUSTA A109 A109K2 0260502 EU ADF SWITCH DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 109RX 10016 FACEPLATE DAMAGED AND UNREADABLE. P/N 58410A2B2C2D2F4L92. (X) 1 G 7 2 3U RT H7EU 2000010800552 20000108 00552 WP 2000 1 8 AALA991898 1 19991205 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 475-795 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 467AA 49597 TUL - FOUND SEAT TRACK CORRODED, RIGHT OUTBOARD TRACK.. REMOVED AND REPLACED SEAT TRACK SECTION STATION 475-795 PER SRM 51-01 PAGE 1. (M) 2 L 7 2 4F A6WE 2000010800553 20000108 00553 WP 2000 1 8 AALA991897 1 19991205 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 965 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 467AA 49597 TUL - FOUND SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK SECTION STATION 795 THROUGH STATION 1030 PER SRM 51-01 PAGE 1. (M) 2 L 7 2 4F A6WE 2000010800554 20000108 00554 WP 2000 1 8 AALA991891 1 19991209 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 279AA 49295 TUL - FOUND CORROSION AROUND SEVERAL FASTENERS ON FORWARD SIDE OF STATION 1338 PRESSURE BULKHEAD RIGHT SIDE ABOVE VAULT DOOR JAMB, JUST BELOW RIGHT A/C DUCT. REMOVED DAMAGE BY BLENDING. INSTALLED DOUBLER PER ESO 80559, DATED 12-10-99. (M ) 2 L 7 2 4F A6WE 2000010800555 20000108 00555 WP 2000 1 8 AALA991892 1 19991210 A 5310 SKIN DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 462AA 49592 TUL - RUST EMITTING FROM FASTENER HOLES ON LOWER AREA OF FORWARD CARGO LOWER DOOR SILL AND DOOR FRAME CUTOUT STATION 370 AND 427. REMOVED CORRODED LOWER SILL PAN. SPLICED IN REPAIR SECTION PER SRM 53-05 PART 1 FIG 44. (M) 2 L 7 2 4F A6WE 2000010800556 20000108 00556 WP 2000 1 8 AALA991910 1 19991209 A 5320 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 864 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - INBOARD OF NR 3 SEAT TRACK FLOORBEAM WORN AT FS 864. BLENDED OUT AREA DYE CHECKED. INSTALLED ODUBLER PER ESO 805 59. (M) 2 L 7 2 4F A6WE 2000010800557 20000108 00557 WP 2000 1 8 AALA991911 1 19991209 A 5320 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 845 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - INBOARD OF NR 3 SEAT TRACK FLOORBEAM WORN AT FS 845. BLENDED OUT WEAR DYE CHECKED FOR WEAR. INSTALLED DOUBLER PE R ESO 80559 REV 118. (M) 2 L 7 2 4F A6WE 2000010800558 20000108 00558 WP 2000 1 8 AALA991912 1 19991208 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 245-249 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - A 4 INCH DENT BETWEEN STATION 245 AND 249, 1 INCH BELOW LONGERON 17 LEFT AND 1 INCH DENT AT STRINGER 244, 3 INCHES ABOVE LONGERON 18 LEFT. (M) 2 L 7 2 4F A6WE 2000010800559 20000108 00559 WP 2000 1 8 AALA991913 1 19991207 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1212 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - AFT CARGO FRAME WEB CRACKED FROM LIGHTNING HOLE STATION 1212, LONGERON 27R. REMOVED OLD WEB. INSTALLED NEW WEB A ND FASTENERS PER AARD 53-10-00-24. (M) 2 L 7 2 4F A6WE 2000010800560 20000108 00560 WP 2000 1 8 AALA991914 1 19991123 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 234-237 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - NR 4 SEAT TRACK TANG CORRODED. REPAIRED SEAT TRACK PER SRM 53-05 PART 1 FIG 4A. (M) 2 L 7 2 4F A6WE 2000010800561 20000108 00561 WP 2000 1 8 AALA991915 1 19991123 A 5320 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 576-582 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - NR 6 SEAT TRACK CORRODED STATION 576-582. REPAIRED SEAT TRACK PER AARD 53-20-00-10 SEAT TRACK PLUG. (M) 2 L 7 2 4F A6WE 2000010800562 20000108 00562 WP 2000 1 8 AALA991916 1 19991123 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 824-828 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - NR 6 SEAT TRACK CORRODED STATION 824-828. SEAT TRACK PLUG PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 2000010800563 20000108 00563 WP 2000 1 8 AALA991917 1 19991124 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 670-674 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - NR 6 SEAT TRACK CORRODED STATION 670-674. REMOVED CORROSION CUTOUT DAMAGED AREA AND INSTALLED PLUG PER AARD 53-20 -00-10 PAGES 1-3. (M) 2 L 7 2 4F A6WE 2000010800564 20000108 00564 WP 2000 1 8 AALA991918 1 19991201 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 824-828 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - NR 6 SEAT TRACK CORRODED STATION 824-828. REMOVED OUT OF LIMITS AREA AND INSTALLED PLUG PER AARD 53-20-00-10. (M ) 2 L 7 2 4F A6WE 2000010800565 20000108 00565 WP 2000 1 8 AALA991919 1 19991201 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1287 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 288AA 49300 TUL - FOUND DOUBLE DRILLED HOLE ON FUSELAGE FRAME BELOW LONGERON 7L, AFT SIDE OF FS 1287. INSTALLED DOUBLER AT FS 1287, STRINGER 7L TO 8L PER SRM 53-03, PAGE 129. (M) 2 L 7 2 4F A6WE 2000010800566 20000108 00566 WP 2000 1 8 AALA991920 1 19991202 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP BS 148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - FOUND CORROSION ON COCKPIT FLOORBOARD, STATION 148 BETWEEN SEAT TRACKS, RIGHT SIDE RBL 23-27. INSTALLED NEW FLOOR BOARD PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2000010800567 20000108 00567 WP 2000 1 8 AALA991921 1 19991202 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174-1278 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - FOUND CORROSION ON SEAT TRACK NR 1 AT STATION 1174, 1231, 1250, 1265 AND 1278. REPLACED CORRODED SEAT TRACK WITH NEW ONE PER SRM 51-01. (M) 2 L 7 2 4F A6WE 2000010800568 20000108 00568 EU 2000 1 8 AALA991834 1 19991202 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 91050 423 TUL - FOUND CORROSION ON STRINGER 52R AT FRAME 59. INSTALLED REPAIR DOUBLER PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 2000010800569 20000108 00569 EU 2000 1 8 AALA991833 1 19991202 A 5320 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU FRAME 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 91050 423 TUL - SHEAR TIE HAS CORROSION AT FRAME 59 AND BETWEEN STRINGER 53R AND 54R. INSTALLED MANUFACTURED SHEAR TIE PER SRM 51 -75-10. (M) 2 L 7 2 4F RT A35EU 2000010800570 20000108 00570 EU 2000 1 8 AALA991832 1 19991130 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU FRAME 80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 91050 423 FOUND CORROSION ON STRINGER 51L AND FITTING AT FRAME 80. INSTALLED NEW STRINGER END FITTING PER SRM 51-75-10. (M) 2 L 7 2 4F RT A35EU 2000010800571 20000108 00571 EU 2000 1 8 AALA991870 1 19991203 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FRAME 32-34 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 91050 423 TUL - STRINGER SPLICE CORRODED ON STRINGER 54 LEFT BETWEEN FRAMES 32 AND 34. REPLACED STRINGER SPLICE PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2000010800572 20000108 00572 EU 2000 1 8 AALA991871 1 19991203 A 5320 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU FRAME 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 91050 423 TUL - FOUND CORROSION ON SHEAR TIE AT FRAME 59 AND BETWEEN STRINGER 46R AND 47R. INSTALLED NEW SHEAR TIE PER SRM 51-74- 10. (M) 2 L 7 2 4F RT A35EU 2000010800573 20000108 00573 EU 2000 1 8 AALA991822 1 19991130 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 91050 423 TUL - FOUND CORROSION ON STRINGER SPLICE 39 LEFT AT FRAME 58. INSTALLED NEW SPLICE PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2000010800574 20000108 00574 EU 2000 1 8 AALA991821 1 19991130 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 91050 423 TUL - FOUND CORROSION ON STRINGER SPLICE 37L AT FRAME 58. INSTALLED NEW STRINGER SPLICE PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 2000010800575 20000108 00575 WP 2000 1 8 AALA991895 1 19991214 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP STAIRWAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 208AA 49159 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIR FORWAR D EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000010800576 20000108 00576 WP 2000 1 8 AALA991878 1 19991209 A 2410 CSD DOUG DC9 DC982 3022082 WP LT ENGINE FAILED A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 07 574AA BBFRLLF 53151 DFW - FLT 817 - AFTER TAKEOFF AIRCRAFT EXPERIENCED LOSS OF ELECTRICAL POWER. LEFT GENERATOR OFF LIGHT AND AC CROSS TIE LOCKOUT LIGHT ILLUMINATED. ACCOMPLISHED REQUIRED PROCEDURE AND DISCONNECTED LEFT CONSTANT SPEED DRIVE. RETURNED AND LA NDED DFW WITHOUT INCIDENT. LOUD BANG HEARD FROM LEFT ENGINE DURING DESCENT. REPLACED LEFT CONSTANT SPEED DRIVE. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000010800577 20000108 00577 EA 2000 1 8 MASA99176 1 19991113 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA AVIONICS BAY INOPERATIVE A MASA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 7291Z 7291 FLT 6023 - PHX-FAT - DURING CRUISE ALTITUDE THE CREW NOTED THE AIRCRAFT INDICATED IT HAD THE FLIGHT SPOILERS, GROUND SPO ILERS AND SPOILERONS INDICATING AS INOPERATIVE IN FLIGHT. ONCE THE AIRCRAFT ARRIVED IN FAT MAINTENANCE INSPECTED AND PE RFORMED AN SECU TEST PER BOMBARDIER SERVICE LETTER 27001E. NO DEFECTS OR DISCREPANCIES WERE FOUND. OPS CHECKED GOOD AN D THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2000010800578 20000108 00578 WP 2000 1 8 G60A040 1 19991207 A 5230 NCA608037 SEAL DOUG DC10 DC1030 3023501 WP CARGO DOOR LEAKING A G6OA B A EMER. DESCENT UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 605GC 47925 CABIN ALTITUDE COULD NOT BE CONTROLLED IN AUTO, SEMI-AUTO, STANDBY, OR MANUAL POSITION. PERFORMED RAPID DEPRESSURIZATIO N/EMERGENCY DESCENT TO 11,000 FT, DUMPED FUEL AND RETURNED TO SBKP. DURING TROUBLESHOOTING, FOUND MAIN CARGO DOOR SEAL AFT AND FORWARD OF TRACK UNSECURED FROM FRAME DUE TO CARGO LOADING IMPACT. RESECURED SEAL AND PERFORMED PRESSURIZATION CHECK IAW MM 21-30-00. (M) 2 L 7 3 4F A22WE 2000010800579 20000108 00579 SO 2000 1 8 C2XA99BT113 1 19991207 A 3610 8166241 SENSOR EMB 145 EMB145 SO NR 1 NACELLE INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15932 145015 EWR - FLT 4027 - CREW REPORTED SMELL OF SMOKE IN FLIGHT AT FULL CLIMB POWER. FOUND SMOKE SMELL CAUSED BY PRECOOLER SENS OR INOPERATIVE. REMOVED AND REPLACED PRECOOLER SENSOR, OPERATIONALLY CHECKED AND TEST FLOWN SATISFACTORY. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000010800580 20000108 00580 NM 2000 1 8 USAA990902 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 380 BETWEEN STRINGER 8R AND 9R FRAME. INSTAL LED DOUBLER PER SRM 53-30-07. (M) 2 L 7 2 4F RT A16WE 2000010800581 20000108 00581 NM 2000 1 8 USAA990903 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 787 FRAME AT STRINGER 9L OVERHEAD BIN ATTACH POINT. INSTALLED DOUBLER AND REPAIR ANGLE PER EA 65193. (M) 2 L 7 2 4F RT A16WE 2000010800582 20000108 00582 NM 2000 1 8 USAA990895 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FUOND .125 INCH CRACK STATION 787 FRAME, STRINGER OVERHEAD BIN ATTACH POINT. I NSTALLED REPAIR ANGLE AND FILLER PER EA 65193 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2000010800583 20000108 00583 NM 2000 1 8 USAA990896 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 807 FRAME, STRINGER 9R OVERHEAD BIN ATTACH PO INT. INSTALLED REPAIR ANGLE AND FILLER PER EA 65193 AND SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2000010800584 20000108 00584 NM 2000 1 8 USAA990897 1 19990829 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..5 INCH CRACK STRINGER TIE CLIP STATION 663.75, STRINGER 10R. REMOVE D CRACKED TIE CLIP INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000010800585 20000108 00585 NM 2000 1 8 USAA990898 1 19990829 A 5320 STRAP BOEING 737 7373B7 1384580 NM BS 774-855 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION IN VARIOUS LOCATIONS STATION 774-855, RBL 19 STRAP. CORROSION LEVEL 1. REMOVED AND REPLACED WITH NEW STRAP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000010800586 20000108 00586 NM 2000 1 8 USAA990899 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 1064 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH BY 2 INCH CHAFFED AREA AT STATION 1064, BL 0 FRAME. DAMAGED BLENDED AND INSTALLED REPAIR DOUBLER PER TR 53-80-02. (M) 2 L 7 2 4F RT A16WE 2000010800587 20000108 00587 NM 2000 1 8 USAA990900 1 19990829 A 5320 SPLICE BOEING 737 7373B7 1384580 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 907 PLUS 1/2 AT STRINGER 4L. INSTALLED NEW ST RINGER SPLICE PER SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 2000010800588 20000108 00588 NM 2000 1 8 USAA990878 1 19990829 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 178, RBL 22, WL 196 INTERCOSTAL. INSTALLED DOUBL ER PER TR 53-10-15 AND SRM 53-10-08. (M) 2 L 7 2 4F RT A16WE 2000010800589 20000108 00589 NM 2000 1 8 USAA990879 1 19990829 A 5313 STRINGER BOEING 737 7373B7 1384580 NM BS 1007 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION BS 1007, STRINGER 23R, CORROSION LE VEL 1. INSTALLED STRINGER SPLICE PER SRM 53-00-03. (M) 2 L 7 2 4F RT A16WE 2000010800590 20000108 00590 NM 2000 1 8 USAA990871 1 19990829 A 5320 ANGLE BOEING 737 7373B7 1384580 NM BS 312-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 312 TO 344 LBL 45 Z-ANGLE. CORROSION LEVEL 2. REPAIRED PER 53-10-15 AND 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000010800591 20000108 00591 NM 2000 1 8 USAA990852 1 19990829 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES BY 2 INCHES AT STATION 344 FLOORBEAM LBL 45 - RBL 15 . CORROSION LEVEL 1. CORROSION TASK NR C 53-107-01. INSTALLED NEW SECTION OF UPPER CHORD WITH REPAIR DOUBLER PER SRM 51-70-12 AND EA 65239. (M) 2 L 7 2 4F RT A16WE 2000010800592 20000108 00592 NM 2000 1 8 USAA990853 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 726 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..1 INCH CRACK AT BS 726 STRINGER 18A RIGHT CHORD ANGLE. INSTALLED NE W PART PER EA 65273A. (M) 2 L 7 2 4F RT A16WE 2000010800593 20000108 00593 NM 2000 1 8 USAA990854 1 19990829 A 5530 ANGLE BOEING 737 7373B7 1384580 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTINO, FOUND A ..25 INCH CRACK AT DRAG ANGLE VERT FIN ATTACH FITTING. INSTALLED DOUB LER AND FILLERS PER EA 65234 AND 65234A. (M) 2 L 7 2 4F RT A16WE 2000010800594 20000108 00594 NM 2000 1 8 USAA990844 1 19990829 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION BS 1016, BBL 0, LBL 12, WL 208 FLOORBEAM. CORROSION LEVEL 1. INSTALLED COMPLETE T-CAP PER SRM 53-10-05 AND EA 65232. (M) 2 L 7 2 4F RT A16WE 2000010800595 20000108 00595 NM 2000 1 8 USAA990845 1 19990829 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 278 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A ..75 INCH CRACK BS 278 STRINGER 14R IN RADIUS OF INTERCOSTAL. INSTALL ED REPAIR DOUBLER PER SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F RT A16WE 2000010800596 20000108 00596 NM 2000 1 8 USAA990832 1 19990829 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM BS 887-947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT SEAT TRACK STATION 887 TO 947, LBL 48. CO RROSION LEVEL 1. REPAIRED DOUBLER/SHIMS PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 2000010800597 20000108 00597 NM 2000 1 8 USAA990833 1 19990829 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION AT STATION 360, RBL 12 FLOORBEAM. C ORROSION LEVEL 1. REPAIRED ANGLES PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2000010800598 20000108 00598 NM 2000 1 8 USAA990834 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 305 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK BS 305, STRINGER 4L FRAME. INSTALLED NEW PART PER SRM 51 -10-02.. (M) 2 L 7 2 4F RT A16WE 2000010800599 20000108 00599 NM 2000 1 8 USAA990835 1 19990829 A 5320 BRACKET BOEING 737 7373B7 1384580 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK IN ANGLE RIGHT BS 616 STRINGER 7 AND STRINGER 8 BRACKE T. REPLACED BRACKET, FABRICATED NEW PART PER SRM 51-30-01 FIG 2 PG 14. (M) 2 L 7 2 4F RT A16WE 2000010800600 20000108 00600 NM 2000 1 8 USAA990836 1 19990829 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM BS 666 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 666, LBBL 32.5 PRESSURE DECK. INSTALLED DOUBLER PER EA 65231. (M) 2 L 7 2 4F RT A16WE 2000010800601 20000108 00601 NM 2000 1 8 USAA990829 1 19990829 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTINO, FOUND A ..5 INCH BY .5 INCH AREA OF CORROSION STATION 1016, BL 0 TO LBL 12 FLO ORBEAM. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER EA 65232. (M) 2 L 7 2 4F RT A16WE 2000010800602 20000108 00602 NM 2000 1 8 USAA990830 1 19990829 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 24 INCH BY 24 INCH AREA OF CORROSION STATION 312, LBL 12, RBL 12 FLOOR BEAM. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000010800603 20000108 00603 NM 2000 1 8 USAA990825 1 19990829 A 5313 STRINGER BOEING 737 7373B7 1384580 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 908 PLUS 1/2 STRINGER 4R. INSTALLED NEW STRIN GER SPLICE PER SRM 51-10-00. (M) 2 L 7 2 4F RT A16WE 2000010800604 20000108 00604 NM 2000 1 8 USAA990812 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 TO 1.5 INCH CRACK STATION 807 STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 2000010800605 20000108 00605 NM 2000 1 8 USAA990813 1 19990829 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM BS 663.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..5 INCH CRACK STATION 663.75 STRINGER 10L TIE CLIP. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000010800606 20000108 00606 NM 2000 1 8 USAA990814 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK STATION 480 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLE D REPAIR ANGLE PER EA 65193. (M) 2 L 7 2 4F RT A16WE 2000010800607 20000108 00607 NM 2000 1 8 USAA990815 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 480 BETWEEN STRINGER 8L AND 9L FRAME. INSTAL LED REPAIR ANGLE PER EA 65193. (M) 2 L 7 2 4F RT A16WE 2000010800608 20000108 00608 NM 2000 1 8 USAA990816 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 867 STRINGER 9L OVERHEAD BIN ATTACH POINT FRA ME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 AND EA 65193. (M) 2 L 7 2 4F RT A16WE 2000010800609 20000108 00609 NM 2000 1 8 USAA990817 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 807 STRINGER 9L OVERHEAD BIN ATTACH POINT FRAM E. INSTALLED DOUBLER PER EA 65193. (M) 2 L 7 2 4F RT A16WE 2000011500001 20000115 00001 EU 2000 1 15 C2XA99IA598 1 19991128 A 5320 S5337122301200 FITTING AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR FORWARD LATCH FITTING FORWARD LUG WAS FOUND CRACKED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED LATCH FITTING IAW ATR 42-320 JIC 53-37-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. AIRCRAFT TT: 22,917.4 HOURS CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500002 20000115 00002 EU 2000 1 15 FJT99129221 1 19991214 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A FJTA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 03 922CX 4 922 MQY - FLT 7921 - THE AIRCRAFT WAS ON A FUNCTIONAL TEST FLIGHT FOR RELASE TO SERVICE FROM A HEAVY CHECK. SELECTING GEAR DOWN, THE NOSE LANDING GEAR TRANSIT LIGHT REMAINED ON. THE GEAR WAS CYCLED SEVERAL TIMES AND AN EMERGENCY EXTENSION WAS ATTEMPTED, BUT TO NO AVAIL. THE TRANSIT LIGHT REMAINED ON. THE CAPTAIN DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WI THOUT INCIDENT. INSPECTION REVEALED THE NOSE LANDING GEAR DOWNLOCK SWITCH HAD INTERNALLY FAILED. THE SWITCH WAS REPLAC ED AND A FUNCTIONAL CHECK PERFORMED AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 2000011500003 20000115 00003 WP 2000 1 15 2000ZZZX89 1 19991013 A 3350 60030451 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 12532 11418 45791 DURING ACCOMPLISHMENT OF B-CHECK WORK CARD 0617, DISCOVERED WHEN THE EMERGENCY LIGHTS WERE SELECTED TO THE ON POSITION, THE AFT EMERGENCY LIGHTS ABOVE THE TALL CONE SLIDE DID NOT ILLUMINATE. TROUBLESHOOTING PROCEDURES DETERMINED THE BATTER Y POWER SUPPLY WAS AT FAULT. THE POWER SUPPLY WAS REPLACED AND THE SYSTEM WAS OPERATIONAL CHECKED IAW DC-9 MM 33-53-0 AND FOUND TO BE OK FOR SERVICE. (X) 2 L 7 2 4F A6WE 2000011500004 20000115 00004 WP 2000 1 15 AALA991661 1 19991103 A 2170 1808492 COALESCER BAGS DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 484AA 49677 JAX - FLT 0758 - EN ROUTE MIA/BDL, FUEL ODOR DETECTED IN CABIN. AIRCRAFT DIVERTED TO JAX AND LANDED WITHOUT INCIDENT. R EPLACED COALESCER BAGS AND ACCOMPLISHED AIR CONDITIONING PACK BURN OUT PROCEDURE. SYSTEM GROUND CHECKED, NORMAL OPERATI ON. (X) 2 L 7 2 4F A6WE 2000011500005 20000115 00005 WP 2000 1 15 AALA991857 1 19991204 A 2120 S210N70121 FILTER DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 432AA 49350 DFW - FLT 0584 - AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. SMOKE WAS ALSO IN COCKPIT. PROBLEM ARRESTED AT 7,000 FEET. RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED BOTH PACK FILTERS AND ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECK NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000011500006 20000115 00006 NM 2000 1 15 AALA991764 1 19991118 A 3610 212T311615 DUCT BOEING 767 767223 1385123 NM APU FAILED A AALA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 303AA 22309 PSP - FLT 0160 - EN ROUTE SAN/JFK, AIRCRAFT EXPERIENCED LOW RUMBLE FOLLOWED BY CENTER DUCT LEAK LIGHT. CLOSED ISOLATION VALVE AND APU BLEED. CABIN CONTINUED TO CLIMB AT MAXIMUM RATE. ACCOMPLISHED EMERGENCY DESCENT TO 10,000 FEET. INSULA TION BLEW THROUGH AFT CABIN FROM RIGHT SIDE NEAR ROW 27. CREW AND PASSENGER OXYGEN MASKS DEPLOYED. EMERGENCY DECLARED, DIVERTED TO PSP AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU AIR SUPPLY DUCT ASSEMBLY. SYSTEM GROUND CHECKED, NO RMAL OPERATION. APU AIR SUPPLY DUCT WELD BROKE. (X) 2 L 7 2 4F RT A1NM 2000011500007 20000115 00007 WP 2000 1 15 AALA991818 1 19991129 A 3397 WIRE DOUG DC9 DC982 3022082 WP SEATS 3 AND 6 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 485AA 49678 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 3E AND 6E INOPERATIVE. REPAIRED SPLICE FO R EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 3E AND 6E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000011500008 20000115 00008 NM 2000 1 15 AALA991816 1 19991129 A 3350 CIRCUIT BREAKER BOEING 757 757223 1384957 NM COCKPIT TRIPPED A AALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 07 184AN 29594 CLO - FLT 0960 - DURING TAXI, EMERGENCY EXIT FLOOR PATH LIGHTS AND DOOR LIGHTS ILLUMINATED FROM FORWARD CABIN EXITS TO R OW 17. RETURNED TO GATE WITHOUT FURTHER INCIDENT. RESET BREAKERS ON FLIGHT ATTENDANT'S PANEL AND OVERHEAD PANEL EMERGE NCY SWITCH IN COCKPIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500009 20000115 00009 NM 2000 1 15 AALA991814 1 19991128 A 3350 CONNECTOR BOEING 757 757223 1384957 NM ROWS 1 AND 6 DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7667A 25301 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 1E AND 6E INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT CONNECTOR AT ROW 1E. SYSTEM GROUND CHECKED, NORMAL OPERRATION. (X) 2 L 7 2 4F RT A2NM 2000011500010 20000115 00010 NM 2000 1 15 AALA991815 1 19991129 A 3350 233T321033 CONTROLLER BOEING 767 767223 1385123 NM COCKPIT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 329AA D00251 22329 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT AND RIGHT OF AIRCRAFT INOPERATIVE ON TEST. REPLACED EMERGE NCY EXIT LIGHT CONTROL PANEL ON PILOTS OVERHEAD PANEL. SYSTEM GROUND CHECKED, NORMAL OPERATED. (X) 2 L 7 2 4F RT A1NM 2000011500011 20000115 00011 NM 2000 1 15 AALA991817 1 19991129 A 3397 WIRE BOEING 767 767223 1385123 NM SEAT 30 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 329AA 22329 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT MOUNTED PATH LIGHT AT SEATS 30H - 30J INOPERATIVE. REPAIRED SHO RTED WIRES ON EMERGENCY EXIT SEAT MOUNTED PATH LIGHT AT SEATS 30H - 30J. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000011500012 20000115 00012 NM 2000 1 15 AALA991820 1 19991130 A 3397 WIRE BOEING 767 767323 1385205 NM ROWS 24 AND 37 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7375A 25202 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTS AT 37B AND 24H INOPERATIVE. REPAIRED WIRE FOR EMERG ENCY EXIT SEAT PATH LIGHTS AT 37B AND 24H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000011500013 20000115 00013 NM 2000 1 15 USAASB99289 1 19991206 A 3234 HANDLE BOEING 737 737301 1384611 NM COCKPIT MALFUNCTIONED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 336US 23233 PIT - FLT 705 - DURING LOWERING OF LANDING GEAR, INBOUND TO PIT, CREW RECEIVED ALL 6 GEAR INDICATION LIGHTS (3 RED AND 3 GREEN). CREW RECYCLED GEAR AND INDICATION WAS NORMAL. FLIGHT LANDED AT PIT WITHOUT FURTHER INCIDENT. NO EMERGENCY WA S DECLARED. MAINTENANCE CLEANED AND LUBED THE LANDING GEAR HANDLE ASSEMBLY. PERFORMED GEAR SWING SEVERAL TIMES WITH AL L INDICATIONS NORMAL. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4F RT A16WE 2000011500014 20000115 00014 NM 2000 1 15 USAA991339 1 19991205 A 5512 SKIN BOEING 737 7373B7 1384580 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 528AU 36425 24410 CLT - DURING AN OVERNIGHT CHECK VISUAL AND EDDY CURRENT, FOUND A 1.8 INCH CRACK RT HORIZONTAL STABILIZER LOWER SKIN AT R EAR SPAR STA 125-126.8 SKIN. INSTALLED REPAIR DOUBLER PER TR 55-10-07 REV A. (X) 2 L 7 2 4F RT A16WE 2000011500015 20000115 00015 NM 2000 1 15 USAA991202 1 19991029 A 5320 SPLICE BOEING 737 737301 1384611 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 559AU 40914 23513 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 0.01 INCH CRACK STA 908 STR 4R STRINGER SPLICE. REPLACED WITH IDENTIC AL PART C/C 1122424. (X) 2 L 7 2 4F RT A16WE 2000011500016 20000115 00016 NM 2000 1 15 USAA990908 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 1040 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH SLIT WORN INTO FUSELAGE FRAME. BLENDED OUT DAMAGE, INSTALLED R EPAIR DOUBLER PER TR 53-80-02. (X) 2 L 7 2 4F RT A16WE 2000011500017 20000115 00017 NM 2000 1 15 USAA990909 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .1250 INCH CRACK STA 847 FRAME AT STR 9R OVERHEAD BIN ATTACH POINT. I NSTALLED FILLER AND REPAIR ANGLE PER EA 65193 AND SRM 53-00-07 FIG 202. (X) 2 L 7 2 4F RT A16WE 2000011500018 20000115 00018 NM 2000 1 15 USAA990904 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 723 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 723 STR 18A, LT CHORD ANGLE. REMOVED AND REPLACED PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 2000011500019 20000115 00019 NM 2000 1 15 USAA990905 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 726 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 726 STR 18A LT CHORD ANGLE. REMOVED AND REPLACED PER SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 2000011500020 20000115 00020 NM 2000 1 15 USAA990906 1 19990829 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK AT STRINGER TIE CLIP STA 616 AT STR 4L. REMOVED AND REPLACED PE R SRM 53-00-03. (X) 2 L 7 2 4F RT A16WE 2000011500021 20000115 00021 NM 2000 1 15 USAA990907 1 19990829 A 5320 ANGLE BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK LT RAM AIR INLET UPPER AFT ANGLE AT BS 520, STR21L. INST ALLED REPAIR FILLER AND DOUBLER PER TR 53-50-03. (X) 2 L 7 2 4F RT A16WE 2000011500022 20000115 00022 NM 2000 1 15 USAA990901 1 19990829 A 5320 SPLICE BOEING 737 7373B7 1384580 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STA 907 + 1/2 AT STR 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-00. (X) 2 L 7 2 4F RT A16WE 2000011500023 20000115 00023 NM 2000 1 15 TWRA9976 1 19991205 A 3350 RP51B CHARGER BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 624FF 3480 21439 EMERGENCY EGRESS LIGHTS C-ZONE INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 2000011500024 20000115 00024 NM 2000 1 15 AALA991758 1 19991118 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 871AA 21383 TUL - LOWER WING SKIN INSIDE PLENUM ARM, STR S5L, BUTT SPLICE AFT SKI SECTION, RBL 27-28 HAS SKIN EXFOLIATED AROUND RIVE TS. INSTALLED FILLER, DOUBLER AND TRIPLER PER SRM 57-30-3, AND ESO 11697 DATED NOVEMBER 18, 1999. TST: 59,603 HOURS. CYCLES: 35,983. (X) 2 L 7 3 4F A3WE 2000011500025 20000115 00025 NM 2000 1 15 AALA991757 1 19991116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1140 CREASED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 871AA 21383 TUL - SKIN DENTED AND CREASED OVER STR 21L AT BS 1140. CUT OUT 3 INCH BY 3 INCH SECTION OF SKIN, DID AN INTERNAL INSPEC TION OF SURROUNDING STRUCTURE, NO ADDITIONAL DEFECTS FOUND. REPAIRED SKIN WITH SOLID RIVET REPAIR PER SRM 53-30-3 FIG 3 . TST: 59,603 HOURS. CYCLES: 35,983. (X) 2 L 7 3 4F A3WE 2000011500026 20000115 00026 NM 2000 1 15 AALA991756 1 19991119 A 5320 6516200184 STIFFENER BOEING 727 727223 1384074 NM BS 184.8 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 871AA 21383 TUL - OUTBOARD LOWER VERTICAL STIFFENER, CORROSION BELOW TANK STUB PLATE. DRILLED UP AND INSTALLED NEW STIFFENER PER ES O 11697 DATED 11/18/99, SEALED FASTENERS INTERNALLY; LEAK CHECKED. STIFFENER, OK, TANK CLEAR, CLOSE, LEAK CHECK. (X) 2 L 7 3 4F A3WE 2000011500027 20000115 00027 NM 2000 1 15 AALA991759 1 19991117 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 871AA 21383 TUL - AFT SIDE 1166 FRAME/SHEAR TIE LOWER LEG CORRODED FROM STR 28L - STR 27L. REMOVED AND REPLACED SHEAR TIE FROM STR 28L - STR 27 AT STA 1166 PER SRM 51-10-1. TST: 59,603 HOURS. CYCLES: 35,983. (X) 2 L 7 3 4F A3WE 2000011500028 20000115 00028 NM 2000 1 15 AALA991754 1 19991108 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 1183 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 859AA 21086 TUL - VERTICAL STIFFENER AT 1183 BULKHEAD FORWARD SIDE RBL 8 INCHES. REMOVED AND REPLACED VERTICAL STIFFENER, REF SRM 5 1-10-1, PG 4. TST: 63, 374 HOURS. CYCLES: 39,840. (X) 2 L 7 3 4F A3WE 2000011500029 20000115 00029 NM 2000 1 15 AALA991785 1 19991123 A 5712 RIB BOEING 727 727223 1384074 NM WS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 848AA 20989 TUL - LEFT 760.95 RIB CHORD ANGLE CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR KIT PER SB 57-0112. TST: 63,311 HO URS. CYCLES, 40,510. (X) 2 L 7 3 4F A3WE 2000011500030 20000115 00030 NM 2000 1 15 AALA991779 1 19991121 A 5510 BEAM BOEING 727 727227 1384078 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 722AA 20730 TUL - HEAVY CORROSION ON TOP OF LEFT HORIZONTAL STABILIZER UPPER REAR T/E BEAM. INSTALLED DOUBLER OVER DAMAGED AREA PER 55-10-6. TST: 72,812 HOURS. CYCLES: 47,830. (X) 2 L 7 3 4F A3WE 2000011500031 20000115 00031 NM 2000 1 15 AALA991780 1 19991117 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 208 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 722AA 20730 TUL - HEAVY CORROSION ON STRUCTURE NOSE WHEELWELL JUST OUTBOARD OF LEFT TRUNNION CAP S70 208 WL 178 LBL 20-23. REMOVED/ TREATED CORROSION, INSTALLED DOUBLER AARD 51-20-01.5 S58 NR 3091337. TST: 72,812 HOURS. CYCLES: 47,830. (X) 2 L 7 3 4F A3WE 2000011500032 20000115 00032 NM 2000 1 15 AALA991781 1 19991119 A 5330 SKIN BOEING 727 727227 1384078 NM BS 572-580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 722AA 20730 TUL - CORROSION ON BILGE SIDE OF SKIN OUTBOARD OF STR 28L STA 572 - STA 580. INSTALLED EXTERNAL DOUBLER PER SRO 53-30-3 . TST: 72,812.33 HOURS. CYCLES: 47,830. (X) 2 L 7 3 4F A3WE 2000011500033 20000115 00033 NM 2000 1 15 AALA991782 1 19991123 A 5510 CASTING BOEING 727 727227 1384078 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 722AA 20730 TUL - HORIZONTAL STABILIZER HINGE LUGS RIGHT SIDE, BOTH INBOARD AND OUTBOARD HAS CORROSION. REMOVED CORROSION PER SRM 5 5-10-2. FABRICATED NEW BUSHING PER 55-10-2. TST: 72,812.33 HOURS. CYCLES: 47,830. (X) 2 L 7 3 4F A3WE 2000011500034 20000115 00034 NM 2000 1 15 AALA991783 1 19991123 A 5510 CASTING BOEING 727 727227 1384078 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 722AA 20730 TUL - HORIZONTAL STABILROSION ON BORES, LEFT SIDE. REMOVED CORROSION ER SRM 55-10-2 AND FABRICATED NEW BUSHING PER 55-10 -2. TST: 72,812.33 HOURS. CYCLES: 47,830. (X) 2 L 7 3 4F A3WE 2000011500035 20000115 00035 NM 2000 1 15 AALA991784 1 19991123 A 5510 CASTING BOEING 727 727227 1384078 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 722AA 20730 TUL - VERTICAL FIN - HORIZONTAL STABILIZER ATTACH LUGS HAD CORROSION IN BORE, BOTH LEFT AND RIGHT. REMOVED CORROSION ON RIGHT LUG PER SB 727-55-7 AND SRM 55-30-6. REMOVED CORROSION ON LEFT LUG PER ESO 11697 DATED 11-22-99. (X) 2 L 7 3 4F A3WE 2000011500036 20000115 00036 NM 2000 1 15 AALA991761 1 19991119 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - TOP OF FLOOR SUPPORT CORRODED AT STA 400 GI GALLEY AREA. INSTALLED NEWLY FABRICATED FLOOR SUPPORT AT STA 400 G1 G ALLEY PER MD-11 AARD 51-10-00-1. TST: 26,813 HOURS. CYCLES: 4,044. (X) 2 L 7 3 4F RT A22WE 2000011500037 20000115 00037 WP 2000 1 15 AALA991699 1 19991107 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1000 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - CORROSION ON ANGLE BEAM ON AFT FORWARD CARGO DOOR FRAME. REPAIR COVERED BY ESO 7349. BLENDED OUT CORROSION PER S RM 51-21-01 VOL II. TST: 101,286.36 HOURS. CYCLES: 18,805. (X) 2 L 7 3 4F A22WE 2000011500038 20000115 00038 WP 2000 1 15 AALA991697 1 19991109 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 859-899 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - CORROSION ON LOWER FORWARD SUPPORT ANGLE. REPAIR COVERED ON ESO 7349 DATE 11-9-99. REMOVED CORROSION AND REPAIRE D PER ESO 7349, S/N 47847, DATED 11-8-99. TST: 101,286.36 HOURS. CYCLES: 18,805. (X) 2 L 7 3 4F A22WE 2000011500039 20000115 00039 NM 2000 1 15 AALA991670 1 19991028 A 5330 SKIN BOEING 727 727227 1384078 NM BS 410 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 730AA 20737 TUL - SHARP DENT FROM WITHIN IN FUSELAGE SKIN AT BS 410 BETWEEN STR 22 AND STR 23R. CUT OUT DAMAGE AND INSTALLED DOUBLE R PER SRM 53-30-3, PAGE 7. TST: 72,099.47 HOURS. CYCLES: 46,524. (X) 2 L 7 3 4F A3WE 2000011500040 20000115 00040 NM 2000 1 15 AALA991669 1 19991102 A 5330 SKIN BOEING 727 727227 1384078 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 730AA 20737 TUL- CRACK STA 580, STR 27L, FUSELAGE SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 11. TST: 72 ,099.47 HOURS. CYCLES: 46,542. (X) 2 L 7 3 4F A3WE 2000011500041 20000115 00041 NM 2000 1 15 AALA991685 1 19991111 A 5320 WEB BOEING 727 727223 1384074 NM BS 294.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 859AA 21086 TUL - STA 294.5 WEB CRACK, RBL 23 INCHES FROM CENTER JUST ABOVE AND INBOARD OF RIGHT TUNNEL IN CHAMPAGNE LOUNGE. INSTAL LED DOUBLER PER SRM 51-40-2. TST: 63,374 HOURS. CYCLES: 39,840. (X) 2 L 7 3 4F A3WE 2000011500042 20000115 00042 NM 2000 1 15 AALA991724 1 19991111 A 5530 LUG BOEING 727 727223 1384074 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 848AA 20989 TUL - RIGHT OUTBOARD AND INBOARD LUGS FOR THE HORIZONTAL STABILIZER PIVOT BEARING CORRODED. BORED AND SPOT FACED, MANUF ACTURED AND INSTALLED NEW BUSHINGS PER ESO 11697 DATED 11-11-99. TST: 63,321 HOURS. CYCLES: 40,522. (X) 2 L 7 3 4F A3WE 2000011500043 20000115 00043 EU 2000 1 15 AALA991849 1 19991206 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 18066 509 LHR - DURING OVERNIGHT MAINTENANCE, FIRST CLASS NR 2 OVEN SMOKED. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NOR MAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000011500044 20000115 00044 EU 2000 1 15 AALA991848 1 19991206 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 18066 509 LHR - FLT 0106 - DURING OVERNIGHT MAINTNENANCE, FIRST CLASS NR 1 OVEN SMOKED. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000011500045 20000115 00045 NE 2000 1 15 AALA991751 2 19991118 A 7200 ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 2 STALLED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 1756 48491 702445 MIA - FLT 1769 - ON CLIMB-OUT FROM MIA, NR 2 ENGINE COMPRESSOR STALLS PASSING 12,000 FOOT CLIMB POWER. AIRCRAFT RETURNE D AND LANDED MIA WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL WITH ENGINE AT IDLE FOR THREE MINUTES PRIOR TO ENGINE SHUTDOWN. AIRCRAFT FERRIED TO DFW FOR ENGINE CHANGE. ARRIVED AND LANDED DFW T9551/19 WITHOUT INCIDENT. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F 4 F RT A22WE E31N3 2000011500046 20000115 00046 NM 2000 1 15 AALA991766 1 19991122 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 26 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357AA 24038 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT/ROW 26AB INOPERATIVE. REPLACED WIRING FOR EMERGE NCY EXIT PATH LIGHT AT SEAT/ROW 26AB SYSTEM GROUND CHECK, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000011500047 20000115 00047 NM 2000 1 15 AALA991771 1 19991123 A 3350 LIGHT BOEING 757 757223 1384957 NM SEAT 11 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 664AA 25298 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 11D INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT STRIP AT SEAT 11D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500048 20000115 00048 NM 2000 1 15 AALA991774 1 19991123 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 1 DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 691AA 25697 SFO -DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS IN ROW ONE DISCONNECTED. RECONNECTED FI RST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS IN ROW ONE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500049 20000115 00049 NM 2000 1 15 AALA991790 1 19991124 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 647AM 24605 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT IN MOST AFT OF AIRCRAFT INOPERATIVE. REPLACED EMERGE NCY FLOOR PATH LIGHT STRIP AT MOST AFT OF AIRCRAFT. SYSTEM GROUND CHECKED, NOMRAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500050 20000115 00050 NM 2000 1 15 AALA991791 1 19991124 A 3397 WIRE BOEING 767 767323 1385205 NM SEAT 40 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39365 24046 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 40H HAD BROKEN WIRE AT CONNECTOR. REPAIRED EMERGE NCY EXIT SEAT LIGHT CONNECTOR AT SEAT 40H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000011500051 20000115 00051 NM 2000 1 15 AALA991792 1 19991124 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697AN 26977 BOS - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS HAVE WIRE TERMINAL ENDS BROKEN. REPAIR ED FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500052 20000115 00052 NM 2000 1 15 AALA991794 1 19991125 A 3350 P2010031303 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 641AA 24599 TPA - DURING OVERNIGHT MAINTENANCE, BULKHEAD EMERGENCY EXIT LIGHT AFT OF DOOR R4 BROKEN. REPLACED BULKHEAD EMERGENCY EX IT LIGHT ASSEMBLY AFT OF DOOR R4. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500053 20000115 00053 NM 2000 1 15 AALA991800 1 19991126 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661AA 25295 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 9-17 INOPERATIVE. REPAIRED EMERGENCY EXIT F LOOR PATH LIGHT WIRING AT MID-GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500054 20000115 00054 NM 2000 1 15 AALA991819 1 19991129 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7667A 25301 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 1E AND FORWARD OF 9E INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTORS AT 1E AND 9E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500055 20000115 00055 NM 2000 1 15 AALA991838 1 19991202 A 2120 UNKNOWN BOEING 767 767323 1385205 NM LAVATORY ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 352AA 24033 PHX - FLT 2238 - DURING FLIGHT, STRONG ELECTRICAL BURNING ODOR IN LEFT BUSINESS CLASS M1 LAVATORY. REMOVED AND CLEANED SEALANT FROM M1 LAVATORY DOOR SEAL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000011500056 20000115 00056 NM 2000 1 15 AALA991856 1 19991204 A 2120 COALESCER BAG BOEING 767 767323 1385205 NM CABIN AIR ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 358AA 24039 LAX - FLT 0002 - RIGHT AFTER TAKEOFF, CABIN AND COCKPIT CREW NOTICED A BURNING RUBBER/PLASTIC ODOR. MAINTENANCE ACCOMPL ISHED OPERATIONS CHECK OF ELECTRICAL EQUIPMENT. UNABLE TO DUPLICATE ELECTRICAL SMOKE ODOR. AS A PRECAUTION, CHANGED CO ALESCER BAGS. OPERATED PACKS WITH ENGINES AND APU WITH NO SMOKE OR ELECTRICAL ODOR NOTED. SYSTEM GROUND CHECKED, NORMA L OPERATION. (X) 2 L 7 2 4F RT A1NM 2000011500057 20000115 00057 NM 2000 1 15 AALA991744 1 19991118 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 644AA 24602 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED FORWARD EMERGENCY EXI T FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000011500058 20000115 00058 WP 2000 1 15 HALA9900249 1 19991127 A 5280 BOLT DOUG DC9 DC951 3022051 WP RT MLG DOOR LOOSE A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 709HA 47764 HNL - FLT 203 - (ATB) AFTER TAKEOFF AND GEAR RETRACTION, THE RIGHT GEAR UNSAFE LIGHT WOULD EXTINGUISH. RECYCLED WITH NO CHANGE. ALSO, GEAR OPEN LIGHT REMAINED ON WITH GEAR DOWN. ALSO, SPOILERS WOULD NOT ARM. FOUND RIGHT MAIN GEAR DOOR LATCH MECHANISM HOLD-DOWN BOLTS LOOSE. REPLACED BOTH BOLTS AND NUTS. CLEARANCE CHECK GOOD. DOOR OPS CHECKED OK PER MM 32-31-4. CODE 3. (X) 2 L 7 2 4F RT A6WE 2000011500059 20000115 00059 WP 2000 1 15 HALA9900248 1 19991127 A 3297 WIRE DOUG DC9 DC951 3022051 WP NLG LOCK SENSOR BROKEN A HALA O OTHER N FALSE WARNING AP APPROACH 1 WP 13 709HA 47764 HNL - FLT 361 - CHECK NOSE GEAR DOWN LATCH AND INDICATION SYSTEM. GREEN NOSE GEAR DOWN LIGHT SLOW TO ACTIVATE THEN INTE RMITTENT WITH GEAR WARNING HORN. FOUND BROKEN WIRES ON NLG LOCK SENSOR. REPLACED LOCK SENSOR. PROXIMITY CONTROL BOX B ITE CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 2000011500060 20000115 00060 WP 2000 1 15 HALA9900250 1 19991127 A 2420 RAM AIR TURB DOUG DC9 DC951 3022051 WP AUX POWER INOPERATIVE A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 669HA 47654 HNL - FLT 512 -(RTR) RAT AND TRI INOPERATIVE. PLACARDED TRI INOPERABLE ALL MPCW. REF: OPERATOR CONTROL NR 99ZZZX90. (X) 2 L 7 2 4F RT A6WE 2000011500061 20000115 00061 WP 2000 1 15 2000ZZZX90 1 19991127 A 7712 TRI DOUG DC9 DC951 3022051 WP COCKPIT INOPERATIVE A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 669HA 47654 HNL - FLT 512 -(RTR) RAT AND TRI INOPERATIVE. PLACARDED TRI INOPERABLE ALL MPCW. REF: OPERATOR CONTROL NR HALA990025 0. 2 L 7 2 4F RT A6WE 2000011500062 20000115 00062 WP 2000 1 15 HALA9900251 1 19991126 A 3244 TIRE DOUG DC9 DC951 3022051 WP MLG FAILED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 649HA 47715 HNL - FLT 45 - NR 3 TIRE BLEW OUT DURING TAXI FOR TAKEOFF. REMOVED AND REPLACED NR 3 MAIN TIRE AND PRECAUTIONARY CHANGE D NR 4 MAIN TIRE ASSY. BRAKE VISUAL CHECK OK. TIRE PRESSURE CHECKED OK. (X) 2 L 7 2 4F RT A6WE 2000011500063 20000115 00063 WP 2000 1 15 HALA9900233 1 19991119 A 2910 HOUSING DOUG DC10 DC1010 3022110 WP HYD SYSTEM CRACKED A HALA K NONE K FLUID LOSS AP APPROACH 1 WP 13 125AA 46525 HNL - FLT 939 - HYDRAULIC SYSTEM 3 LEVEL OFF LIGHT ON. SYSTEM 3 HYDRAULIC QUANTITY ZERO, IT HAPPENED ON FINAL APPROACH AFTER ALL FLAPS OUT. PUMPS WERE TURNED OFF BEFORE 0. FOUND TRIM CYL INTERLOCK FUSE HOUSING CRACKED. REMOVED AND REPLA CED FUSE PER MM 32-31-06.. OPS LEAK CHECK OK. RESERVICED QUANTITIES. (M) 2 L 7 3 4F A22WE 2000011500064 20000115 00064 GL 2000 1 15 HALA9900235 2 19991119 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF6* 30020 GL NR 1 VIBRATION A HALA K NONE E VIBRATION/BUFFET CR CRUISE 1 WP 13 119AA 46519 NR 1 ENGINE IN CRUISE FL360, 1 HOUR OUT OF LAX HAD NOTICEABLE VIBRATION ABOVE 88.9 PCT, N2 94.0 PCT, NR 1 CSD TEMP 30 DE GREES CELSIUS RISE 60 DEGREES CELSIUS BELOW 89 PCT N2 VIBRATION WAS LESS FELT IN AIRFRAME AND N1 FUEL LEVER. REPLACED E NGINE PER MCM SECT 12 CARD DR 719401. POWER ASSURANCE CHECK OK PER MCM SECTION 12 719578. OPS AND LEAK CHECKS OK. ACC OMPLISHED PYLON INSPECTION PER MCM. (M) 2 L 7 3 4F 4 F A22WE E23EA 2000011500065 20000115 00065 WP 2000 1 15 HALA9900234 1 19991120 A 2420 GCU DOUG DC10 DC1010 3022110 WP NR 2 MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 122AA 46522 NR 2 AC BUS TIE ISOL LIGHT CAME ON IN FLIGHT PERFORMED PROCEDURES IN FCOM, LIGHT REMAINED ON. REMOVED AND REPLACED NR 2 GCU AND BCU. GROUND RUN CHECK OK. (M) 2 L 7 3 4F A22WE 2000011500066 20000115 00066 WP 2000 1 15 HALA9900237 1 19991122 A 2133 OUTFLOW VALVE DOUG DC9 DC951 3022051 WP CABIN PRESSURE MALFUNCTIONED A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 662HA 47742 HNL - FLT 131 - DURING ROLLOUT, OUTFLOW VALVE STARTS TO CLOSE, PRESSURIZING CABIN, THEN ABRUPTLY OPENS. GROUND CHECK, F ORWARD CONT AMP FAILED TO OPEN. REPLACED CONT AMP, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 2000011500067 20000115 00067 WP 2000 1 15 HALA9900245 1 19991124 A 2130 53895811 SENSOR DOUG DC9 DC951 3022051 WP CABIN PRESSURE MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 672MC 161230 47661 HNL - FLT 515 - CABIN PRESSURE CONTROL, ON TAKEOFF, CABIN DESCENDS 1800 FEET/MINUTE (PEGS OUT). THEN CLIMBS 500 FEET/MI NUTE. THEN OSCILATES IN CLIMB 200-800 FEET/MINUTE. ON DESCENT, CABIN CLIMBS 500 FEET/MINUTE, THEN DOWN 1,000 FEET/MINUT E. REPLACED DIFFERENTIAL PRESSURE SENSOR, TESTED OK. (X) 2 L 7 2 4F RT A6WE 2000011500068 20000115 00068 NM 2000 1 15 TSAA9933489 1 19991204 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 1 EMERGENCY FLOOR BATTERY PACK DUE TO INOPERABLE. OPS CHECKED OK, AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 2000011500069 20000115 00069 NM 2000 1 15 TSAA9933490 1 19991204 A 3350 8731002511 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD SERVICE DOOR EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SE RVICE. (X) 2 L 7 2 4F RT A16WE 2000011500070 20000115 00070 NM 2000 1 15 TSAA9933492 1 19991204 A 3350 8731002511 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD SERVICE DOOR LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 2000011500071 20000115 00071 NM 2000 1 15 TSAA9933491 1 19991204 A 3350 6013211 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD AND AFT EXTERIOR EMERGENCY SLIDE LIGHT BATTERY PACKS DUE TO INOPERABLE. OPS CHECKED OK. AIRCRAFT RETU RNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 2000011500072 20000115 00072 NM 2000 1 15 TSAA9933495 1 19991202 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED BATTERY PACK FOR NR 4 AND NR 6 POSITION FLOOR LIGHT DUE TO LOW. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 2000011500073 20000115 00073 NM 2000 1 15 TSAA9933494 1 19991204 A 3350 6012311 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARAGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD SERVICE AND ENTRY DOOR OUTSIDE EMERGENCY LIGHT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRA FT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 2000011500074 20000115 00074 NM 2000 1 15 TSAA9933493 1 19991204 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 2000011500075 20000115 00075 EU 2000 1 15 REXA99035 1 19991202 A 3234 WIRE SAAB SF340 340B 7860101 EU COCKPIT FAILED A REXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 363PX 340B260 LFT - FLT 5756 - ON CLIMB-OUT, RECEIVED CONFLICTING GEAR INDICATION. THROUGH COMMUNICATIONS WITH DISPATCH AND MAINT CON TROL, FLT 5756 WAS INSTRUCTED TO CONTINUE TO MEMPHIS. AT APPROX 60 NAUTICAL MILES S/W OF MEMPHIS, CREW RECEIVED A DIFFE RENT FALSE INDICATION OF LANDING GEAR POSITION. EMERG DECLARED, OVER FLIGHT OF TOWER TO CONFIRM STATUS OF LANDING GEAR . ACFT LANDED, DISCOVERED NOSE WHEEL STEERING SYS NOT WORKING. ACFT WAS STOPPED ON RUNWAY WITHOUT INCIDENT PAX DEPLANE D. UPON INSP, A POOR ELECT CONNECTION BETWEEN WIRE HARNESS AND LANDING GEAR CONTROL HANDLE WAS CAUSE OF THE CONFLICTIN G GEAR IND AND NOSE WHEEL STEERING FAILURE. (X) 2 L 7 2 4T RT A52EU 2000011500076 20000115 00076 EU 2000 1 15 REXA99034 1 19991106 A 3240 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU BRAKE LEAKING A REXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 346AM 340A032 LOSS OF MAIN HYDRAULIC PRESSURE WITH ASSOCIATED FLUID LOSS. EMERGENCY EXTENSION OF THE LANDING GEAR WAS PERFORMED AND A N EMERGENCY WAS DECLARED. FOUND SWIVEL LEAKING. REMOVED AND REPLACED SWIVEL AND LANDING GEAR EXPLOSION BOLTS. PERFORM ED FUNCTIONAL CHECK OF LANDING GEAR WITH NO FURTHER DISCREPANCIES NOTED. (X) 2 L 7 2 4T RT A52EU 2000011500077 20000115 00077 NE 2000 1 15 UF6A991201 2 19991204 A 7261 3036281 OIL CAP BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE DISLODGED A UF6A E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 859AW 2036 124451 ORD - FLT 5712 - THE NR 2 ENGINE LOW PRESSURE ILLUMINATED AND PRESSURE DROPPED BELOW RED LINE. NR 2 ENGINE WAS SHUT DOW N. MAINTENANCE INSPECTED AND FOUND OIL CAP DISLODGED. OIL CAP WAS REPLACED. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T 4 T RT A27NM E2ONE 2000011500078 20000115 00078 EU 2000 1 15 UF6A991112 1 19991125 A 3350 0L3071BPEGPL BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 ORD - FLT 5709 - WHITE EMERGENCY LIGHT INOPERABLE AT FORWARD PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED BULB. SY STEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 2000011500079 20000115 00079 EU 2000 1 15 UF6A991111 1 19991127 A 7931 648846062 INDICATAOR BAG ATP ATP EU COCKPIT FAILED A UF6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 857AW 9007 245 2034 ORD - FLT 5703 - NR 1 ENGINE FLUCTUATING OIL PRESSURE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE TRIPLE INDICATO R. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 2000011500080 20000115 00080 WP 2000 1 15 K4HA99091 1 19991122 A 5730 SKIN DOUG DC8 DC863F 302198F WP WING CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 PERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND SPOTS OF CORROSION. STA XFS-195000 . (X) 2 L 7 4 4F 4A25 2000011500081 20000115 00081 WP 2000 1 15 K4HA99090 1 19991118 A 5730 SKIN DOUG DC8 DC863F 302198F WP WING CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 PERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND SPOTS OF CORROSION ALONG LEADING ED GE. (X) 2 L 7 4 4F 4A25 2000011500082 20000115 00082 WP 2000 1 15 K4HA99093 1 19991126 A 5720 FLANGE DOUG DC8 DC863F 302198F WP WING CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 PERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND SPOTS OF CORROSION ALONG LEADING ED GE FLANGE. CORROSION DAMAGE ON INNER WING CENTER EXTENDED LEADING EDGE. LT/RT SIDE BL, WL, STRINGER, FRAME, BULKHEAD, ETC., STA XW-257000 TO XFS-429000. (X) 2 L 7 4 4F 4A25 2000011500083 20000115 00083 WP 2000 1 15 K4HA99092 1 19991127 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CRACKED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 803CK 46085 PERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP CARDS, FOUND RT CENTER WING AREA UPPER SKIN SURFACE C RACK, 1.25 INCH CRACK. RT CENTER WING AREA UPPER SURFACE SKIN AT STA WFS 65000. CUT OUT DAMAGED AREA, FABRICATED FILLE R AND DOUBLER AND INSTALLED IAW SRM 51-1-20D. WORK ACCOMPLISHED UNDER A1A FORM M-40 CONTROL NR 26719. (X) 2 L 7 4 4F 4A25 2000011500084 20000115 00084 WP 2000 1 15 K4HA99089 1 19991118 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 803CK 46085 PERU - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND CORROSION ON STUB WING NR 2 AT STA XRS-220.00 TO XRS-260.00. SPOTS OF CORROSION ALONG LEADING EDGE OF STUB WING. (X) 2 L 7 4 4F 4A25 2000011500085 20000115 00085 EA 2000 1 15 ASOA99165 1 19991214 A 3350 363782 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 832AS 7243 DURING INSPECTION, RIGHT OVERWING EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING SYSTEM BUL B. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 2000011500086 20000115 00086 SO 2000 1 15 ASOA99166 1 19991214 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 236AS 4679 2019 120049 DURING INSPECTION, NR 2 EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERG ENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 2000011500087 20000115 00087 SO 2000 1 15 ASOA99160 1 19991202 A 5411 12003852001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 263AS 120157 UPON INSPECTION, FOUND LT NACELLE UPPER FRAME NR 1 CRACKED. MAINTENANCE COMPLIED WITH EO 120-54-0034. OPERATIONAL CHEC KS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 2000011500088 20000115 00088 SO 2000 1 15 ASOA99161 1 19991204 A 3350 1013073 FUSE EMB 120 EMB120RT SO CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 266AS 120188 DURING INSPECTION, FOUND EMERGENCY FORWARD TRACK LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE FUSE FOR THE EMERGENCY TRACK LIGHTING. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 2000011500089 20000115 00089 NM 2000 1 15 F3LA99167 1 19991217 A 4920 COMPRESSOR 38042842 BOEING 737 7372L9 1384497 NM APU DAMAGED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 271FL 7222 79 P35605C 22734 ABQ - UPON DEPARTURE, FLIGHT CREW REPORTED APU AUTO SHUTDOWN AT 11,000 FEET. MAINTENANCE FOUND DAMAGE TO APU COMPRESSOR , TURBINE, MUFFLER, AND FIRE LOOP. MAINTENANCE REPLACED APU, MUFFLER AND FIRE LOOP AND CHECKED OKAY. REF: OPER CONTRO L NR 2000ZZZX91 THROUGH 2000ZZZX93. CYCLES: 4,481. (X) 2 L 7 2 4F RT A16WE 2000011500090 20000115 00090 NM 2000 1 15 2000ZZZX91 1 19991217 A 4920 TURBINE 38042842 BOEING 737 7372L9 1384497 NM APU DAMAGED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 271FL 7222 79 P35605C 22734 ABQ - UPON DEPARTURE, FLIGHT CREW REPORTED APU AUTO SHUTDOWN AT 11,000 FEET. MAINTENANCE FOUND DAMAGE TO APU COMPRESSOR , TURBINE, MUFFLER, AND FIRE LOOP. MAINTENANCE REPLACED APU, MUFFLER AND FIRE LOOP AND CHECKED OKAY. REF: OPER CONTRO L NR F3LA99167, 2000ZZZX92 AND 2000ZZZX93. CYCLES: 4,481. 2 L 7 2 4F RT A16WE 2000011500091 20000115 00091 NM 2000 1 15 2000ZZZX92 1 19991217 A 4920 FIRE LOOP 38042842 BOEING 737 7372L9 1384497 NM APU DAMAGED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 271FL 7222 79 P35605C 22734 ABQ - UPON DEPARTURE, FLIGHT CREW REPORTED APU AUTO SHUTDOWN AT 11,000 FEET. MAINTENANCE FOUND DAMAGE TO APU COMPRESSOR , TURBINE, MUFFLER, AND FIRE LOOP. MAINTENANCE REPLACED APU, MUFFLER AND FIRE LOOP AND CHECKED OKAY. REF: OPER CONTRO L NR F3LA99167, 2000ZZZX91 AND 2000ZZZX93. CYCLES: 4,481. 2 L 7 2 4F RT A16WE 2000011500092 20000115 00092 NM 2000 1 15 2000ZZZX93 1 19991217 A 4920 MUFFLER 38042842 BOEING 737 7372L9 1384497 NM APU BAY DAMAGED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 271FL 7222 79 P35605C 22734 ABQ - UPON DEPARTURE, FLIGHT CREW REPORTED APU AUTO SHUTDOWN AT 11,000 FEET. MAINTENANCE FOUND DAMAGE TO APU COMPRESSOR , TURBINE, MUFFLER, AND FIRE LOOP. MAINTENANCE REPLACED APU, MUFFLER AND FIRE LOOP AND CHECKED OKAY. REF: OPER CONTRO L NR F3LA99167, 2000ZZZX91 AND 2000ZZZX92. CYCLES: 4,481. 2 L 7 2 4F RT A16WE 2000011500093 20000115 00093 2000 1 15 2000ZZZX94 4 19991216 A 3416 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 01 96UX 1672 4082 UE96 CAPTAIN'S ALTIMETER FAILED ON TAKEOFF. REMOVED AND REPLACED NR 1 ALTIMETER. TESTED OK. COMPONENT P/N KEA3460663-3062- 00. (X) 2 L 7 2 4T RT A24CE 2000011500094 20000115 00094 NM 2000 1 15 GAIA99236 1 19991214 A 5311 FRAME BOEING 727 727223 1384074 NM BS 227.8 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6816 19491 'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). FRAME WEB AT BS 227.8 WL 208.1 TO WL 224 CORRODED OUT OF SRM LIMITS. CUT OUT CORROSION DAMAGED AREAS IAW ENGINEERING DEVIATION REQUEST B2-07307. APPLIED PROTECTIVE TREATMENT PER B 727 SRM 51-10-2. FABRICATED REPAIR DOUBLER AND REPLACEMENT WEB IAW EDR, B 2-07307. INSTALLED ALL REPAIR PARTS IAW EDR, B2-07307. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000011500095 20000115 00095 NM 2000 1 15 GAIA99235 1 19991214 A 5531 SPAR BOEING 727 727223 1384074 NM VERTICAL STAB CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6816 19491 'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). VERTICAL STABILI ZER FORWARD SPAR CORRODED AT FS 55R. REMOVED DAMAGED AREA IAW ENGINEERING DEVIATION REQUEST B2-07305. PERFORMED HFEC A ND LIGHT INSPECTION IAW B 727 NDT MANUAL PART 6 FIG 23. NO DEFECTS NOTED. FABRICATED REPAIR ANGLES AND FILLERS AND INS TALLED IAW EDR B2-07305. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000011500096 20000115 00096 NM 2000 1 15 GAIA99234 1 19991214 A 5530 TEE BOEING 727 727223 1384074 NM VERTICAL STAB WORN A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6816 19491 'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). VERTICAL STABLIZ ER LEFT SIDE T-CHORD WORN AT PANEL NR 9601. REMOVED DAMAGE IAW ENGINEERING DEVIATION REQUEST (EDR B2-07298). PERFORMED HFEC IAW B 727 NDT MANUAL PART 6 FIG 23. NO CRACKS NOTED. FABRICATED REPAIR PARTS IAW EDR B2-07298. INSTALLED REPAIR PARTS IAW EDR B2-07298. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000011500097 20000115 00097 WP 2000 1 15 GTIA9901209 1 19991123 A 3350 LENS DOUG DC9 DC981 3022081 WP ROW 8 MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 981SB 48058 LGA - FLT 722A - EMERGENCY FLOOR PATH LIGHTS OF ROW 8 MISSING LENS. INSTALLED MISSING LENS. OPS CHECK OK IAW MM 33 53 01. (X) 2 L 7 2 4F A6WE 2000011500098 20000115 00098 WP 2000 1 15 GTIA9901210 1 19991121 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 CLE - FLT 541 - LEFT EXTENSION EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY PACK. OPS CK GOOD. (X) 2 L 7 2 4F A6WE 2000011500099 20000115 00099 WP 2000 1 15 GTIA9901212 1 19991126 A 3350 SPLICE DOUG DC9 DC931 3022065 WP ROW 12 FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 ACY - FLT 880 - AISLE PATH LIGHTING FORWARD OF ROW 12 IS INOPERABLE. REPAIRED SPLICE, OPS CHECK GOOD. IAW MM 33-21-0. (X) 2 L 7 2 4F A6WE 2000011500100 20000115 00100 NM 2000 1 15 GAIA99233 1 19991214 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 950F CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6816 19491 'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). FLOOR BEAM UPPE R CHORD AFT FLANGE CORRODED AND CRACKED AT FASTENER HOLE. (BS 950F, RBL 62.0). REMOVED DAMAGED AREA IAW B 727 SRM 53-1 0-8. FABRICATED DOUBLERS PER B 727 SRM 51-10-2. INSTALLED REPAIR IAW B 727 SRM 53-10-8 AND EDR B2-07313. AIRCRAFT RET URNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000011500101 20000115 00101 NM 2000 1 15 GAIA99232 1 19991214 A 5320 WEB BOEING 727 727223 1384074 NM BS 848 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6816 19491 'NO FLIGHT', FOUND DURING 'HEAVY 2 MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (OSCODA MI). WEB CRACKED AT F LOOR SUPPORT, BS 848.0, RBL 50.0. STOP DRILLED CRACK IAW B727 SRM 51-10-1. PERFORMED HFEC IAW 727 NDT MANUAL PART 651- 00-00 FIG 11 AND FIG 23. FABRICATED NEW PARTS IAW ENGINEERING DEVIATION REQUEST (EDR B2-07306). INSTALLED REPAIR PARTS IAW EDR B2-07306. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000011500102 20000115 00102 NM 2000 1 15 GAIA99231 1 19991210 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A GAIA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 07 6806 19481 PRIOR TO DEPARTURE FOR IAH, THE COCKPIT EMERGENCY EXIT LIGHT WAS DETERMINED TO BE INOPERATIVE. THE EMERGENCY LIGHT IN T HE COCKPIT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000011500103 20000115 00103 EU 2000 1 15 C2XA99IA607 1 19991128 A 5311 S53672111200 FRAME AEROSP ATR42 ATR42320 8680930 EU NR 42 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH- DURING C-CHECK INSPECTION, THE LOWER PORTION OF FRAME 42 WAS FOUND CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAI R IAW ATR 42-320 SRM 51-21-42 AND SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 22,9 17.4 HOURS. CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500104 20000115 00104 EU 2000 1 15 C2XA99IA606 1 19991128 A 5315 S53672406208100 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 36 WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF FLOORBEAM AND PERFORMED A SPLICE REPAIR IAW ATR 42-320 SRM 51-25-09 AND SRM 53-61-40, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 22,917.4 HOURS. CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500105 20000115 00105 EU 2000 1 15 C2XA99IA605 1 19991128 A 5343 S5367800124002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAMES 32-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK WAS FOUND CORRODED FROM FRAME 32 TO FRAME 36. MAINTENANCE REMOVED AND REPLCED THE AFFECTED SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. AIRCRAFT TT: 22,917.4 HOURS. CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500106 20000115 00106 EU 2000 1 15 C2XA99IA604 1 19991128 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAMES 32-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK WS FOUND CORRODED FROM FRAME 32 TO FRAME 36. MAINTENANCE REMOVED AND REPLACED THE AFECTED SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. (X) 2 H 7 2 4T RT A53EU 2000011500107 20000115 00107 EU 2000 1 15 C2XA99IA603 1 19991128 A 5315 S5367240820302 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF FLOORBEAM AND PERFORMED A SPLICE REPAIR IAW ATR 42-320 SRM 51-25-02, SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 22,917.4 HOURS. CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500108 20000115 00108 EU 2000 1 15 C2XA99IA602 1 19991128 A 5320 S5367126120001 CHORD AEROSP ATR42 ATR42320 8680930 EU FRAMES 38-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR THRESHOLD CHORD WAS FOUND CORRODED FROM FRAME 38 TO FRAME 39. MAINTEN ANCE REMOVED AND REPLACED THE AFECTED CHORD IAW ATR 42-320 SRM 51-21-42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. AIRCRAFT TT: 22,917.4 HOURS. CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500109 20000115 00109 EU 2000 1 15 C2XA99IA601 1 19991128 A 5347 S5367800124002 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAMES 36-41 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH- DURING C-CHECK INSPECTION, THE LEFT SEAT TRACK WAS FOUND CORRODED FROM FRAMES 36 TO 41. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED SEAT TRACK IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRA FT TT: 22,917.4 HOURS. CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500110 20000115 00110 EU 2000 1 15 C2XA99IA600 1 19991128 A 5320 S5367127210 WEB AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED THRESHOLD IAW ATR 42-SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 22,917.4 H OURS. CYCLES: 24,865. (X) 2 H 7 2 4T RT A53EU 2000011500111 20000115 00111 EU 2000 1 15 C2XA99IA599 1 19991128 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAMES 36-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, THE RIGHT SEAT TRACK WAS FOUND CORRODED FROM FRAMES 36 TO 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW ATR 42-SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 22,917.4 HOURS. FRAMES 36-40. (X) 2 H 7 2 4T RT A53EU 2000011500112 20000115 00112 SO 2000 1 15 P77A9902726 2 19991108 A 8500 ENGINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RIGHT MAKING METAL A P77A K NONE O OTHER IN INSP/MAINT 1 EA 25 30LT 1491 402C0259 811165R RIGHT ENGINE SHUT DOWN AFTER TURNING ONTO TAXIWAY AFTER LANDING. PILOT COULD NOT RESTART ENGINE. AFTER PARKING, PILOT NOTICED OIL ON COWLING AND WING. INSPECTION FOUND OIL LEAK IN VICINITY OF CYLINDERS 2 AND 4. ALSO, FOUND HEAVY METAL C ONTAMINATION IN OIL. CRANKSHAFT IS HARD TO ROTATE WITHOUT ANY SPARK PLUGS IN. SUBMITTER STATED CAUSE OF THIS ENGINE FA ILURE IS STILL UNKNOWN. (X) 1 L 7 2 3O 3 O A7CE E8CE 2000011500113 20000115 00113 2000 1 15 AALA991740 4 19991117 A 2330 RDAA80171 DISPLAY AIRBUS 300 A300B4605R 3930308 EU CABIN FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 25071 200582 514 LHR - FLT 0108 - EN ROUTE BOS/LHR, MASTER DISPLAY UNIT AND AIRSHOW PORTION SMELLED OF SMOKE AND THEN WENT BLANK. REPLAC ED CMT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000011500131 20000115 00131 NM 2000 1 15 VNAA9912017 1 19991230 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 432JS 9932 247 3045 THE CREW NOTICED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT WORKING AT THE 7LK POSITION. MAINTENANCE INSPECTED AND REPLA CED THE EMERGENCY BATTERY AT THE 7LK POSITION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECK S PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2000011500132 20000115 00132 NM 2000 1 15 VNAA9912016 1 19991230 A 5210 001A524A1153000 BOLT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PAX DOOR FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 424JS 3033 WHILE EN ROUTE, THE FLIGHT CREW RECEIVED A RED WARNING PANEL DOORS ALERT AND A MAIN CABIN DOOR CAS MESSAGE. MAINTENANCE CONTROL INSTRUCTED THE CREW TO RETURN TO THE FIELD WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INS PECTED AND CLEANED THE SHOOT BOLT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-0O THERE WERE NO FURTHER DEFECTS N OTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 2000011500133 20000115 00133 SO 2000 1 15 COMA0010001 1 19991230 A 5270 WARNING SYSTEM EMB 120 EMB120RT SO SERVICE DOOR ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 152CA 120152 SERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND SECURED SIGNLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 2000011500135 20000115 00135 SO 2000 1 15 COMA0010003 1 19991220 A 3260 922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO RT MLG FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 259CA 120252 RIGHT MLG DISAGREE INDICATION WHEN GEAR RETRACTED. REPLACED THE UPLOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 2000011500136 20000115 00136 SO 2000 1 15 COMA0010004 1 19990104 A 3350 M610628023 RELAY EMB 120 EMB120RT SO E/E BAY INTERMITTENT A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 257CA 120248 EMERGENCY LIGHTS, ARMED INDICATOR, IS INTERMITTENT. REPLACED RELAY KO201. 2 L 7 2 4T RT A31SO 2000011500140 20000115 00140 EA 2000 1 15 COMA0060013 1 19991230 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 967CA 8690 8690 7134 FLAPS FAILED AFTER TAKE OFF. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 2000011500141 20000115 00141 EA 2000 1 15 COMA0060014 1 19991229 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTIONED A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 937CA 6318 7044 DID NOT RECEIVE TAKEOFF CONFIG OK MESSAGE.. REPLACED THE NR 2 SECU. 2 L 7 2 4F RT A21EA 2000011500143 20000115 00143 EA 2000 1 15 COMA0060016 1 19991228 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAP MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 797CA 488 7344 FLAPS FAILED AT 37 DEGREES DURING LANDING APPROACH. REPLACED LEFT WING NR 3 FLAP ACTUATOR. 2 L 7 2 4F RT A21EA 2000011500153 20000115 00153 WP 2000 1 15 AT9900891 1 19991129 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK ON FORWARD CARGO DOOR PAN BETWEEN BEAM 1 AND BEAM 2 AT BS 280. STOP DRILLED CRACK THEN FABRICATED AND INSTALLED DOUBLER REPAIR AT BS 280 IAW DC9 SRM 52-05, 51-10-03, 51-10 -04, AND 51-30-02. 2 L 7 2 4F A6WE 2000011500154 20000115 00154 WP 2000 1 15 AT9900892 1 19991205 A 2730 SKIN DOUG DC9 DC932 3022066 WP ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LEFT ELEVATOR UPPER SKIN AT XRS 218.8 CORRODED BEYOND LIMI TS. REMOVED, FABRICATED, AND REPLACED SKIN ON LEFT ELEVATOR AT XRS 218.8 IAW DC9 SRM 51-10-03, 55-03 FIG 14, AND 51-30. 2 L 7 2 4F A6WE 2000011500155 20000115 00155 WP 2000 1 15 AT9900893 1 19991227 A 5711 J0601654 SPAR DOUG DC9 DC932 3022066 WP RT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN RIGHT WING REAR SPAR LOWER CAP. REMOVED AND REPL ACED CRACKED SPAR SECTION IAW DC9 SRM 51-30-01, 51-30-05, 51-30-02, 57-40-01, AND DRAWING J060165.. 2 L 7 2 4F A6WE 2000011500156 20000115 00156 WP 2000 1 15 AT9900896 1 19991217 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 589 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT RIGHT WINDOW 20 BS 589 BLENDED DAMAGE AND FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 589 IAW EO 99-1399, DC9 SRM 53-05 FIG 111, AND DC9 MM 56-20. 2 L 7 2 4F A6WE 2000011500157 20000115 00157 WP 2000 1 15 AT9900897 1 19991217 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 551 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT RIGHT WINDOW 18 BS 551, BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 551 IAW EO 99-1399, DC9 SRM 53-05 FIG 111 , AND DC9 MM 56-20. 2 L 7 2 4F A6WE 2000011500158 20000115 00158 WP 2000 1 15 AT9900898 1 19991217 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 494 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT RIGHT WINDOW 15 BS 494, BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AT BS 494 IAW EO 99-1399, DC9 SRM 53-05 FIG 111, AND D C9 MM 56-20. 2 L 7 2 4F A6WE 2000011500159 20000115 00159 WP 2000 1 15 AT9900899 1 19991217 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 474 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT WINDOW 14 BS 474, BLENDED DAMAGE AND F OUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AT BS 474 IAW EO 99-1399, DC9 SRM 53-05 FIG 111, AND DC9 MM 56-20. 2 L 7 2 4F A6WE 2000011500160 20000115 00160 WP 2000 1 15 AT9900900 1 19991217 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 456 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT WINDOW 13 BS 456, BLENDED DAMAGE AND F OUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AT BS 456 IAW EO 99-1399, DC9 SRM 53-05 FIG 111, AND DC9 MM 56-20. 2 L 7 2 4F A6WE 2000011500161 20000115 00161 WP 2000 1 15 AT9900901 1 19991217 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 649 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT WINDOW 23 BS 649, BLENDED DAMAGE AND F OUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AT BS 649 IAW EO 99-1399, DC9 SRM 53-05 FIG 111, AND DC9 MM 56-20. 2 L 7 2 4F A6WE 2000011500162 20000115 00162 WP 2000 1 15 AT9900902 1 19991217 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND AFT CARGO DOOR WEB JAMB CORRODED BEYOND LIMITS AT BS 935. REMOVED AND REPLACED WEB JAMB AT BS 935 IAW DC9 SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F A6WE 2000011500163 20000115 00163 2000 1 15 AT9900903 4 19991223 A 2565 SLIDE BOEING 737 7372L9 1384497 NM PAX DOOR LOOSE A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 464AT 21278 R-1 SLIDE NEEDS TO BE SECURED IN COMPARTMENT. REMOVED R-1 DOOR SLIDE AND RESECURED IAW 737 MM 25-61-30. 2 L 7 2 4F RT A16WE 2000011500164 20000115 00164 WP 2000 1 15 AT9900904 1 19991217 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 484 - 502 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND A DENT WITH A CREASE AT BS 484-502 LONGERON 28L. CUT OUT SKIN AND LONGERON SPLICED IN NEW SKIN AND LONGERON AT BS 484-502 LONGERON 28L IAW EO 99-1431, DC9 SRM 53-02 FIG 1B,51-10 -04, 51-30-01, 51-30-02, 51-10-05, AND 53-04 FIG 12B. 2 L 7 2 4F A6WE 2000011500165 20000115 00165 WP 2000 1 15 AT9900905 1 19991218 A 5320 DOOR PAN DOUG DC9 DC932 3022066 WP BS 897 - 937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON LOWER SECTION OF AFT CARGO DOOR JAMB PAN AT B S 897-937. CORROSION REMOVAL RESULTED IN 100 PERCENT MATERIAL LOSS. REMOVED AND REPLACED LOWER SECTION OF AFT CARGO DO OR JAMB PAN AND INSTALLED NEW ANGLES BS 897-937 IAW DC9 SRM 53-11-03 FIG 3A, 51-10-03, 53-05 FIG44, 51-30-01, 51-30-02, 51-30-05, AND 51-10 2A. 2 L 7 2 4F A6WE 2000011500166 20000115 00166 WP 2000 1 15 AT9900906 1 19991216 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 474 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LIGHTNING STRIKE AT LEFT WINDOW 14 BS 474. AFTER BLEND OU T FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND WINDOW ASSEMBLY AT BS 474 IAW EO 99-1398, DC9 SRM 53- 05 FIG 111, AND MM 56-20. 2 L 7 2 4F A6WE 2000011500167 20000115 00167 WP 2000 1 15 AT9900907 1 19991218 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 310 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND DENT AT BS 310 LONGERON 27R-28L. REMOVED DAMAGED AREA, FA BRICATED AND INSTALLED DOUBLERS AND REPAIR AT BS 310 IAW EO 99-1419, DC9 SRM 51-30-01, AND 51-30-02. 2 L 7 2 4F A6WE 2000011500168 20000115 00168 WP 2000 1 15 AT9900908 1 19991220 A 5720 9919369502N CAP DOUG DC9 DC932 3022066 WP BS 605 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON RIGHT LOWER WING T-CAP BS 605. REMOVED AND R EPLACED RIGHT LOWER WING T-CAP AT BS 605 IAW DC9 SB 57-98 REV 8. 2 L 7 2 4F A6WE 2000011500169 20000115 00169 WP 2000 1 15 AT9900909 1 19991220 A 5720 9919369501N CAP DOUG DC9 DC932 3022066 WP BS 605 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON LEFT LOWER WING T-CAP BS 605. REMOVED AND RE PLACED LEFT LOWER WING T-CAP AT BS 605 IAW DC9 SB 57-98 REV 8. 2 L 7 2 4F A6WE 2000011500170 20000115 00170 WP 2000 1 15 AT9900911 1 19991208 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 - 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FLOOR SUPPORT AT BS 160 - 218 AND BL 0 CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, TRIMMED, FORMED, DRI LLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT. WORK DONE IAW SRM 51-30-5, 51-10-4, 53-11-1 FIG 13 AND 51-30-5. 2 L 7 2 4F A6WE 2000011500171 20000115 00171 WP 2000 1 15 AT9900912 1 19991213 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND CORROSION AROUND FASTENER HOLES ON FLOOR PANEL NR 71. FABRICATED AND INSTALLED REPAIR IAW SRM 53-3 AND 51-30-2. 2 L 7 2 4F A6WE 2000011500172 20000115 00172 WP 2000 1 15 AT9900913 1 19991223 A 5330 SKIN DOUBLER DOUG DC9 DC932 3022066 WP BS 900 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND INTERNAL DOUBLER CORRODED AT BS 900 BETWEEN LONGERONS 21L AND 22L. CUTOUT CORRODED AREA. FABRICATED AND INSTALLE D REPAIR DOUBLER AND FILLER IAW TIMCO EO 99-1441 AND RES 05858. 2 L 7 2 4F A6WE 2000011500173 20000115 00173 WP 2000 1 15 AT9900914 1 19991223 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 536 LIGHTING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND LIGHTNING STRIKE AT FS 536 BETWEEN LONGERON 21R AND 22R ON FUSELAGE SKIN. CUTOUT STRIKE AREA. FABRICATED AND INS TALLED DOUBLER REPAIR IAW TIMCO EO 99-1445, RES 06665, SRM 51-10-1 FIG 36, 51-10-3, 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2000011500174 20000115 00174 WP 2000 1 15 AT9900917 1 19991212 A 5411 RIB DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 RIGHT ENGINE PYLON LEADING EDGE HAS CRACKED RIB ANGLE. STOP DRILLED CRACK IAW DC9 SRM 57-01. 2 L 7 2 4F A6WE 2000011500175 20000115 00175 WP 2000 1 15 AT9900919 1 19991212 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 DURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND 2 CRACKS IN FORWARD AND 2 CRACKS IN AFT SIDE OF LEFT FUSELAGE FRAME AT BS 1038. INSTALLED REPAIR AT BS 1038 IAW DC9 SRM 51-30-02 AND 53-03. 2 L 7 2 4F A6WE 2000011500176 20000115 00176 WP 2000 1 15 AT9900920 1 19991212 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 DURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND CRACK IN RIGHT FUSELAGE FRAME AT BS 1038. INSTALLED REPAIR AT BS 1038 IAW DC9 SRM 53-04. 2 L 7 2 4F A6WE 2000011500177 20000115 00177 WP 2000 1 15 AT9900922 1 19991212 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 79 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 DURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND DENT TO HAVE A CRACK AT LEFT FUSELAGE BS 79 LONGERON 20 LEFT. INSTALLED DOUBLER IAW DC9 SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 2000011500180 20000115 00180 NM 2000 1 15 CALA9901739 1 19991227 A 4920 380428101 APU GARRETT BOEING 737 737524 1384721 NM TAIL FAILED A CALA F ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 SW 09 17627 6318 27531 THE APU FIRE WARNING LIGHT ILLUMINATED AFTER STARTING APU ON APPROACH TO IAH. THE APU WAS SHUT DOWN AND THE FIRE BOTTLE WAS DISCHARGED. THE FIRE WARNING LIGHT WENT OUT AND THE A/C LANDED AT IAH W/O INCIDENT. MX FOUND THE TAILPIPE FIRELOO P WIRING BURNED. MX ALSO FOUND A HOLE BURNED IN THE APU SHROUD FUEL DRAIN. THE APU LOWER SHROUD HEAT SHIELD INNER RADI US WAS SCORCHED AND COVERED WITH A SOOT RESIDUE. THE APU, TAILPIPE FIRELOOP, AND APU FIRE BOTTLE WERE REMOVED AND REPLA CED. ENGINEERING DETERMINED THAT THE DAMAGE WAS CAUSED BY FUEL POOLING IN A HEAT SHIELD PORTION OF THE REMOVABLE APU LO WER SHROUD. THE FUEL PROBABLY ENTERED THE AREA THROUGH A WEEP HOLE IN BOTTOM OF THE A/C MOUNTED EXHAUST PIPE. 2 L 7 2 4F RT A16WE 2000011500193 20000115 00193 EU 2000 1 15 QXEA9902733 1 19991230 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 18575 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - SHEARED RIVET WITH CRACK PROPAGATING FROM HOLE IN EXTERIOR SKIN AT FRAME 18575 AND STRINGER 61. REPAIRED IAW HORI ZON AIR EA 4-53-952 AND FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000011500194 20000115 00194 WP 2000 1 15 TWAA0000204 1 19991005 A 5523 SKIN DOUG DC9 DC982 3022082 WP ELEVATOR TAB DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND LT ELEVATOR CONTOL TAB WITH DELAMINATION AT THE INBD AREA. CONTROL TAB SENT TO SHOP FOR OVERHAUL. DELAMINATION REPAIRED PER SRM 55-04, PAGE 5 TO 7. 2 L 7 2 4F A6WE 2000011500195 20000115 00195 WP 2000 1 15 TWAA0000205 1 19991018 A 5320 WEB DOUG DC9 DC982 3022082 WP DOOR FRAME CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CRACK AT INTERIOR OF AFT CARGO DOOR AT AFT LOWER DOOR STOP CASTING AND INTERCOSTAL. REP LACED CRACKED WEB AND STIFFENER PER SPM 6-70-07, PAGE 2 AREA 4B. 2 L 7 2 4F A6WE 2000011500196 20000115 00196 WP 2000 1 15 TWAA0000206 1 19991022 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1155 - 1390 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN CHAIR TRACK AT LBL 50, STA 1155 TO 1390. REPLACED BAD TRACK PER SRM 53-05, FIG 4F. 2 L 7 2 4F A6WE 2000011500197 20000115 00197 WP 2000 1 15 TWAA0000207 1 19991023 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1260 - 1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 15 MAINT CHECK, FOUND CORROSION ON FLOOR TRACK, UNDERSIDE, AT STA 1260 TO 1271, LBL 24. INSTALLED NEW TRACK F ROM STA 1220 TO 1322, PER SRM 53-05 FIG 4G. 2 L 7 2 4F A6WE 2000011500198 20000115 00198 WP 2000 1 15 TWAA0000208 1 19991021 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1231 - 1304 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN CHAIR TRACK AT LBL 28, STA 1231 TO 1304. REPLACED TRACK PER SPM 6-70 -00. 2 L 7 2 4F A6WE 2000011500199 20000115 00199 WP 2000 1 15 TWAA0000209 1 19991017 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CORROSION ON STA 1309 FORMER, FROM LONGERON 20L TO 28L. REPLACED FORMER FROM L18L TO L2 8L, PER SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 2000011500200 20000115 00200 WP 2000 1 15 TWAA0000210 1 19991013 A 5320 CASTING DOUG DC9 DC982 3022082 WP DOOR FRAME CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND MID CARGO DOOR UPPER FORWARD INTERIOR DOOR STOP CASTING CRACKED, APPROX 3 IN BELOW TOP O F DOOR, AFT OF FWD EDGE. INSTALLED NEW CASTING PER SPM 6-70-01, PAGE 3. 2 L 7 2 4F A6WE 2000011500201 20000115 00201 WP 2000 1 15 TWAA0000201 1 19991024 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1170 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR MEMBRANE BELOW THE AFT SERVICE DOOR, AFT GIRT BAR FLOOR FITTING, STA 1170. REMOVED CORROSION PER SPM 6-80-01, PAGE 123. REPAIRED MEMBRANE PER SRM 53-01, PAGE 918. 2 L 7 2 4F A6WE 2000011500202 20000115 00202 WP 2000 1 15 TWAA0000202 1 19991020 A 5320 SILL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND IN FORWARD CARGO COMPT, BOTTOM DOOR SILL AREA HAD CORROSION AND WAS DIRTY. REPAIRED LOW ER DOOR SILL PER SRM 53-05 FIG 44. 2 L 7 2 4F A6WE 2000011500203 20000115 00203 WP 2000 1 15 TWAA0000203 1 19991007 A 5320 WINDOW FRAME DOUG DC9 DC982 3022082 WP BS 946 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CABIN WINDOW FRAME CRACKED AT STA 946, LONGERON 12R, UPPER FORWARD CORNER. REMOVED MATE RIAL AND INSTALLED DOUBLER REPAIR PER SRM 53-10-114. 2 L 7 2 4F A6WE 2000011500204 20000115 00204 WP 2000 1 15 ABXA9900867 1 19991221 A 3350 LIGHT DOUG DC8 DC863 302198A WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 826AX 46061 EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN TURNED ON. RELAMPED IAW DC8 MM 33-10-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2000011500205 20000115 00205 WP 2000 1 15 ABXA9900864 1 19991213 A 3231 DOOR DOUG DC8 DC863 302198A WP RT MLG OUT OF ADJUST A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 817AX 45928 AFTER TAKEOFF, THERE WAS A LOUD BANG ON GEAR RETRACTION. AS AIRCRAFT ACCELERATED, NOSE GEAR APPEARED TO BE VIBRATING SE VERELY. RECYCLED GEAR, NO HELP. JACKED AIRCRAFT, FOUND NOSE GEAR DOORS NOT FAIRED AND RIGHT GEAR DOOR ADJUSTMENT VERY TIGHT. ADJUSTED DOORS IAW DC8 MM 32-22-01. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2000011500206 20000115 00206 WP 2000 1 15 ABXA9900865 1 19991228 A 5610 5613217507 WINDOW DOUG DC8 DC861 3021952 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED UPPER GUIDE PIN. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 2000011500207 20000115 00207 WP 2000 1 15 ABXA9900866 1 19991216 A 5610 5613217508 WINDOW DOUG DC8 DC862 3021970 WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 FIRST OFFICER'S WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT HOOK IAW DC8 MM. 2 L 7 4 4F 4A25 2000011500209 20000115 00209 WP 2000 1 15 MWEA99933 1 19991223 A 5311 9910078 FRAME DOUG DC9 DC932 3022066 WP BS 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 AREAS OF THE FLOOR SUPPORT ANGLE AND FRAME ARE CORRODED AT STATION 200 BETWEEN CENTER BEAM AND NR 4 SEAT TRACK. MAINTEN ANCE FABRICATED AND INSTALLED NEW ANGLE AND FRAME ON THE FLOOR SUPPORT. 2 L 7 2 4F A6WE 2000011500213 20000115 00213 WP 2000 1 15 MWEA99934 1 19991222 A 5320 9910078873 BEAM DOUG DC9 DC932 3022066 WP BS 160 - 273 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CENTER SUPPORT BEAM HAS AREAS OF BARE METAL AND LIGHT CORROSION FROM STATION 160 TO STATION 237. MAINTENANCE FABRICATED AND INSTALLED NEW SUPPORT BEAM. 2 L 7 2 4F A6WE 2000011500214 20000115 00214 WP 2000 1 15 MWEA99935 1 19991223 A 2730 99184983 RIB DOUG DC9 DC932 3022066 WP ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CRACKED RIB ON LEADING EDGE OF RIGHT ELEVATOR. MAINTENANCE DRILLED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 2000011500215 20000115 00215 WP 2000 1 15 MWEA99936 1 19991222 A 5320 9910078 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 198 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 2 CRACKS IN SUB FLOOR JUST FWD OF SEAT TRACK NR 3 AT STATION 198. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000011500216 20000115 00216 WP 2000 1 15 MWEA99937 1 19991230 A 5350 S2274640 CLIP DOUG DC9 DC932 3022066 WP TAIL CONE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 EXTERIOR TAIL CONE RELEASE HANDLE FAILED PULL TEST. AFT CLIP IS CRACKED. MAINTENANCE REMOVED AND REPLACED AFT HANDLE R ETATINER CLIP. 2 L 7 2 4F A6WE 2000011500221 20000115 00221 WP 2000 1 15 TWAA0000305 1 19991007 A 5530 RIB DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND VERTICAL STABILIZER DORSAL FIN WITH RIBS CRACKED AT LOWER END, NUMBER 1 AND 5 ON LT SIDE AND 4, 7, AND 8 ON RT SIDE. REPAIRED RIBS 1, 5, 4, 7 PER SRM 55-02 FIG 19. REPLACED NUMBER 8 PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000011500222 20000115 00222 WP 2000 1 15 TWAA0000306 1 19991007 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 180 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK FOUND CABIN FLOOR PANEL SUPPORT, STA 180, WITH CORROSION, RBL 10 TO 43. REPLACED FLOOR PANEL S UPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000011500223 20000115 00223 WP 2000 1 15 TWAA0000307 1 19991006 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND GOUGE IN FWD ENTRY DOOR OUTER SKIN AT GUST LOCK CUTOUT, .5 IN BY .25 IN. BLENDED DAMAGE D AREA AND INSTALLED REPAIR DOUBLER TO OUTER SKIN PER SRM 52-05, FIG 20. 2 L 7 2 4F A6WE 2000011500224 20000115 00224 WP 2000 1 15 TWAA0000308 1 19991004 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1212 - 1287 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR PANEL SUPPORT (CHAIR TRACK) AT STA 1212 TO 1287, LBL 54. REPLACED SU PPORT TRACK PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000011500225 20000115 00225 WP 2000 1 15 TWAA0000309 1 19991005 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 160 - 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AT RBL 6, STA 160 TO 200. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01. 2 L 7 2 4F A6WE 2000011500226 20000115 00226 NM 2000 1 15 TWAA0000312 1 19991103 A 5320 FASTENERS BOEING 767 7673Y0 NM BS 456 WRONG A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING OP 16 MAINT CHECK, FOUND BLIND FASTENERS INSTALLED IN METAL REPAIR ON RT FUSELAGE AT STA 456, STRINGER 25R. MANU FACTURED DOUBLER FROM ALUM SHEET AND INSTALLED ON ACFT PER SRM 53-00-01, PAGES 201 TO 206. 2 L 7 2 4F RT A1NM 2000011500227 20000115 00227 NM 2000 1 15 TWAA0000313 1 19991112 A 5320 SUPPORT BOEING 767 7673Y0 NM BS 317 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT LBL 52 IN AT STA 317 WITH CORROSION. INSTALLED NEW SUPPORT PER SRM 51-40- 02, PAGE 9 PARA 6A AND 6B. HILOCK INSTALLED AND SRM 51-20-01 PAGE 6 PARA 4 FAYING SURFACE SEALING AND SRM 51-20-01 PAGE 7 PARA 5 AND FASTENER SEALING. 2 L 7 2 4F RT A1NM 2000011500228 20000115 00228 NM 2000 1 15 TWAA0000314 1 19991102 A 5322 FLANGE BOEING 767 7673Y0 NM FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING OP 16 MAINT CHECK, FOUND FWD CARGO FLANGES CRACKED ON DOUBLER FOR POWER DRIVE 5L, STA 513 AND 521, LBL 25. FABRI CATED AND INSTALLED NEW DOUBLER PER TWA STANDARD PROCESSES MANUAL 6-70-01, AND SRM 51-40-02. 2 L 7 2 4F RT A1NM 2000011500229 20000115 00229 NM 2000 1 15 TWAA0000315 1 19991102 A 5322 MOUNT FRAME BOEING 767 7673Y0 NM BS 513 - 520 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING OP 16 MAINT CHECK, FOUND FWD CARGO CORROSION UNDER NUT PLATES FOR MOUNT BOLTS OF POWER UNIT 5C, STA 513 TO 520, R BL 6. FABRICATED AND REPLACED MOUNT FRAME PER SPM 6-70-01 AND RIVETS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2000011500230 20000115 00230 WP 2000 1 15 TWAA0000310 1 19991005 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT AT STA 200, LBL 14, RBL 53 WAS CORRODED. REPLACED SUPPORT MEMBER PE R SPM 6-70-01. 2 L 7 2 4F A6WE 2000011500232 20000115 00232 WP 2000 1 15 TWAA0000311 1 19991004 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 522 CUT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 DURING OP 16 MAINT CHECK, FOUND 2 DEEP CUTS IN FORMER, INNER FLANGE AT STA 522, ABOVE LONGERON 6L. REPAIRED DAMAGED ARE A PER SRM 53-03, PAGE 5. 2 L 7 2 4F A6WE 2000011500238 20000115 00238 WP 2000 1 15 ABXA0000001 1 19991230 A 3260 313 BULB DOUG DC9 DC941 302207N WP COCKPIT FAILED A ABXA O OTHER N FALSE WARNING LD LANDING 1 GL 23 967AX 47509 ON LANDING, WHEN GEAR WAS LOWERED, THE GEAR DOOR OPEN LIGHT WOULD NOT ILLUMINATE. PRESS TO TEST WAS OK. REPLACED GEAR DOOR OPEN LIGHT BULB. 2 L 7 2 4F A6WE 2000011500239 20000115 00239 NM 2000 1 15 TWAA0000402 1 19991205 A 5751 SKIN BOEING 767 767231 1385131 NM AILERON SEPARATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 603TW 22566 DURING CHECK-C MAINT, THE LT WING OTBD AILERON, OTBD END CAP HAD APPROX 2.5 INCHES SEPARATION AT BOTTOM EDGE, LOCATED 5 IN FROM LE. SEALED SEPARATED END CAP PER SRM 51-10-00. 2 L 7 2 4F RT A1NM 2000011500240 20000115 00240 NM 2000 1 15 TWAA0000403 1 19991205 A 5751 SEAL BOEING 767 767231 1385131 NM AILERON MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 603TW 22566 DURING CHECK-C MAINT, THE LT WING OTBD AILERON, OTBD TE WEDGE HAD MISSING FILLER SEALANT APPROX 5 INCHES LONG, FROM THE TE TIP.. REPLACED MISSING SEALANT PER SRM 51-10-00. 2 L 7 2 4F RT A1NM 2000011500241 20000115 00241 WP 2000 1 15 TWAA0000404 1 19991206 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 218 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9626F 53596 THE RING FORMER SUPPORT ASSY WAS DAMAGED BY GROUND EQUIPMENT AT FUSESAGE STA 218, STR 21R. INSTALLED RING FORMER REPAIR PER SRM 53-03, FIG 3. CHECK-C 10-2-99 STL. 2 L 7 2 4F RT A6WE 2000011500242 20000115 00242 WP 2000 1 15 TWAA0000405 1 19991206 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 218 PUNCTURED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9626F 53596 PUNCTURE IN FUSELAGE SKIN CAUSED BY GROUND EQUIPMENT 3.5 IN BY 3 IN AT STA 218, STR 21. CLASS 3 REPAIR INSTALLED. REMO VED CLASS 3 REPAIR AND INSTALLED CLASS 2 REPAIR PER DRM 53-04, FIG 12. CHECK-C 10-2-99 STL. 2 L 7 2 4F RT A6WE 2000011500243 20000115 00243 NM 2000 1 15 TWAA0000406 1 19991205 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 1111 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54348 21967 DURING CHECK-C MAINT, FOUND CORROSION ON LOWER OTBD EDGE OF STRINGER 29R AT STA 1111. REPLACED S29R FROM STA 1110 TO 11 30 PER SRM 53-10-3. 2 L 7 3 4F A3WE 2000011500244 20000115 00244 WP 2000 1 15 TWAA0000408 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 446 - 465 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND UNDERSIDE OF FLOOR WEB CORRODED AROUND LIGHTING HOLE BETWEEN STA 446 TO 465 LEFT. REMOVED C ORROSION PER SRM 51-10-3 ITEM 35. APPLIED ALODINE AND PRIMER PER 51-10-3 ITEM 30 AND ITEM 23. REPAIRED PER SRM 53-01 P AGE 18, FIG 4. 2 L 7 2 4F RT A6WE 2000011500245 20000115 00245 WP 2000 1 15 TWAA0000409 1 19991216 A 5320 TIE STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND TIE STRAP CRACKED AT AFT END OF LT AND RT MAIN GEAR WELL AT KEEL BEAM. REMOVED AND REPLACED TIE STRAP. SEALED WITH PRC 142A. ATTACHED WITH ORIGINAL TYPE FASTENERS PER SRM 51-30-5/ 51-30-01. DOUGLAS DRAWING 59 36395. 2 L 7 2 4F RT A6WE 2000011500246 20000115 00246 WP 2000 1 15 TWAA0000410 1 19991209 A 5320 BRACKET DOUG DC9 DC983 3022083 WP BS 1429 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND RAM AIR DUCT HANGER BRACKET, CEILING AREA, STA 1429, 0BL, WAS CRACKED. REPLACED BRACKET PER SPM 6-70-01, PAGE 3, PAR 4(B). 2 L 7 2 4F RT A6WE 2000011500247 20000115 00247 WP 2000 1 15 TWAA0000411 1 19991220 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 522 - 541 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND WEB CORROSION AT STA 522 TO 541. REMOVED CORROSION PER SRM 51-10-3, PAGE 21 THRU 35. ALODI NED AND PRIMED PER SRM 51-10-3, PAGE 18 ITEM 30, AND 51-10-3 PAGE 16 ITEM 23. REPAIRED PER SRM 53-01, P18 FIGURE 4. 2 L 7 2 4F RT A6WE 2000011500248 20000115 00248 NM 2000 1 15 TWAA0000412 1 19991222 A 5755 RIB BOEING 727 727231 1384079 NM SPOILER CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54350 21969 DURING CHECK-C MAINT, FOUND LT WING NUMBER 3 SPOILER RIB ATTACHED TO OTBD CASTING WAS CRACKED. REPLACED PART PER SRM 57 -10-1 AND 51-30-2 FASTENER INSTALLATION. - 2 L 7 3 4F A3WE 2000011500249 20000115 00249 WP 2000 1 15 TWAA0000407 1 19991216 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 484 - 496 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND WEB CORROSION AT STA 484 TO 496, AROUND LIGHTENING HOLE UNDERSIDE OF WEB. CLEANED CORROSION FROM UNDERSIDE OF WEB LIGHTENING HOLE PER SRM 51-10-3. REPAIR COMPLETED PER SRM 53-11-2 AND SRM 53-01 PAGE 18. 2 L 7 2 4F RT A6WE 2000011500250 20000115 00250 NM 2000 1 15 TWAA0000401 1 19991205 A 5751 SKIN BOEING 767 767231 1385131 NM AILERON SEPARATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 603TW 22566 DURING CHECK-C MAINT, THE LT WING OTBD AILERON TE HAD SEPARATION/ROUGH EDGES APPROX 6 INCHES LONG, APPROX 5 IN FROM OTBD END. DRESSED OUT AREA, FILLED WITH FIBERGLAS RISEN, SEALED, PRIMED AND PAINTED PER SRM 57-60-02. 2 L 7 2 4F RT A1NM 2000011500251 20000115 00251 WP 2000 1 15 TWAA0000413 1 19991219 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND CORROSION ON FWD OTBD END OF TRACK, RBL 22 AROUND BLANK HOLE. REMOVED CORROSION 0.020, WHIC H WAS WITHIN SRM 53-05 LIMITS, FROM BLANK HOLE AT END OF TRACK PER SPM 6-80-1 AND TREATED OUTER FLANGE HOLE PER SRM 51-1 0-3, PARA 3D. FINISHED PER SRM 51-10-3, PARA 23. 2 L 7 2 4F RT A6WE 2000011500252 20000115 00252 WP 2000 1 15 TWAA0000414 1 19991221 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1155 - 1306 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, THE AFT CARGO COMPT FLOOR WEB WAS CORRODED ON LOWER SIDE OF WEB, STA 1155 TO 1306, RT SIDE. REMOV ED AND REPLACED WEB MEMBRANE PER SRM 53-05, VIEW D AND E. 2 L 7 2 4F RT A6WE 2000011500253 20000115 00253 NM 2000 1 15 TWAA0000415 1 19991102 A 5320 STUD BOEING 767 7673Y0 NM BS 544 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING OP 16 MAINT CHECK, FOUND FWD CARGO CORROSION AT GROUND STUD ON FLOOR SUPPORT AT STA 544, LBL 10. REPLACED FLOOR SUPPORT PANEL PER STD PROCESSING MANUAL 6-70-01, AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2000011500254 20000115 00254 NM 2000 1 15 TWAA0000416 1 19991112 A 5315 FLOORBEAM BOEING 767 7673Y0 NM BS 325 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING OP 16 MAINT CHECK, FOUND FLOORBEAM CAP CORRODED AT APPROX STA 325, LBL 52. INSTALLED A FLOORBEAM UPPER CHORD REP AIR PER SRM 53-00-51, FIG 201 SHEET 3. 2 L 7 2 4F RT A1NM 2000011500255 20000115 00255 NM 2000 1 15 TWAA0000417 1 19991130 A 5330 SKIN BOEING 727 727231 1384079 NM FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54348 21967 DURING OP 16 MAINT CHECK, THE FWD ENTRY DOOR LOWER HINGE CUT-OUT WAS CRACKED OUT, FWD 1.5 IN LONG IN FUSELAGE SKIN. ACC OMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-1, PAGE 6. INSTALLED REPAIR DO UBLER PER SSRM 53-10-219, DETAIL III. 2 L 7 3 4F A3WE 2000011500391 20000115 00391 NM 2000 1 15 USAA990818 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 887 STRINGER 9L OVERHEAD BIN ATTACH POINT FRA ME. REMOVED AND REINSTALLED BRACKET PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 2000011500392 20000115 00392 NM 2000 1 15 USAA990819 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCHCRACK STATION 847 STRINGER 9L OVERHEAD BIN ATTACH POINT FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 65193. (M) 2 L 7 2 4F RT A16WE 2000011500393 20000115 00393 NM 2000 1 15 USAA990820 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 907 STRINGER 9L OVERHEAD BIN ATTACH POINT FRA ME. INSTALLED REPAIRED ANGLE PER EA 65193. (M) 2 L 7 2 4F RT A16WE 2000011500394 20000115 00394 NM 2000 1 15 USAA990792 1 19990829 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 500D CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING A Q-2 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION AT FS 500D, LBBL 17 FRAME. CORROSION LEVEL 2. REPA IRED ANGLES FABRICATED PER SRM 53-00-07 FIG 203. (M) 2 L 7 2 4F RT A16WE 2000011500395 20000115 00395 NM 2000 1 15 USAA990771 1 19990729 A 5320 ANGLE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 6 SQUARE INCH OF CORROSION MED Z-ANGLE UPPER SURFACE. CORROSION LEVEL 2 . REPLACED Z-ANGLE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000011500396 20000115 00396 NM 2000 1 15 USAA990772 1 19990729 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 727A CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 338US 38294 23234 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH AREA OF CORROSION AT STATION 727A PLUS 14 INCHES, STRINGER 26L. C ORROSION TASK NR C53-202-01, CORROSION LEVEL 2. INSTALLED FABRICATED STRINGER REPAIR CHANNEL ANDRADIUS FILLERS PER SRM 53-00-03 FIG 201. (M) 2 L 7 2 4F RT A16WE 2000011500397 20000115 00397 NM 2000 1 15 USAA990765 1 19990829 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM BS 500A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 500A STRINGER 16R TIE CLIP. REPLACED PART PE R SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000011500398 20000115 00398 NM 2000 1 15 USAA990766 1 19990829 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK STATION 639 STRINGER 4R TIE CLIP. REPLACED PART PER SRM 51-10-0 2. (M) 2 L 7 2 4F RT A16WE 2000011500399 20000115 00399 NM 2000 1 15 USAA990767 1 19990829 A 5320 TIE CLIP BOEING 737 7373B7 1384580 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 397US 38495 23319 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK STATION 616 STRINGER 4R TIE CLIP. REPLACED PART PER SRM 51-10-0 2. (M) 2 L 7 2 4F RT A16WE 2000011500400 20000115 00400 NM 2000 1 15 USAA990462 1 19990522 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 30191 23986 CLT - DURING Q-2 CHECK, FOUND .75 INCH IN FUSELAGE FRAME AT FAST HOLE AT BS 747 BETWEEN STRINGER 8/STRINGER 9L. REMOVED CRACKED AND INSTALLED DOUBLER PER SRM 53-00-07 AND EA 54536. (M) 2 L 7 2 4F RT A16WE 2000011500401 20000115 00401 NM 2000 1 15 USAA991283 1 19991130 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION IN NUT PLATE HOLES BL 0 TO RBL 56, 12 EACH 1 INCH BY 1 INCH FL OORBEAM. CORROSINLEVEL 2. REPLACED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000011500402 20000115 00402 NM 2000 1 15 USAA991282 1 19991130 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK AT BS 867 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED R EPAIR DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000011500403 20000115 00403 NM 2000 1 15 USAA991281 1 19991130 A 5312 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..750 INCH CRACK AT STATION 178, LBL 4.75, WL 198 BULKHEAD. INSTALLED REPAIR DOUBLER PER TR 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 2000011500404 20000115 00404 NM 2000 1 15 USAA991280 1 19991130 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A ..5 INCHCRACK AT STATION 380 BETWEEN STRINGER 8 AND 9L FRAME. INSTALL ED DOUBLER PER EA 66083 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000011500405 20000115 00405 NM 2000 1 15 USAA991279 1 19991130 A 5311 FRAME BOEING 737 737401 1384701 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727D RIGHT, BETWEEN STRINGER 8 AND 9 FRAME. INSTAL LED DOUBLER PER EA66083 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000011500406 20000115 00406 NM 2000 1 15 USAA991278 1 19991130 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 747 LEFT, BETWEEN STRINGE R8 AND 9 FRAME. INSTALLE D DOUBLER PER EA 66083 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000011500407 20000115 00407 NM 2000 1 15 USAA991277 1 19991130 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 747 RIGHT, BETWEEN STRINGER 8 AND 9 FRAME. INSTALL ED DOUBLER PER EA 66083 AND TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000011500408 20000115 00408 NM 2000 1 15 USAA991259 1 19991130 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 31054 23988 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND ONE INCH AREA OF CORROSION TOP SURFACE AROUND CLIPNUT HOLE STATION 967 R BL 30 FLOORBEAM. CORROSION LEVEL 2. INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 2000011500409 20000115 00409 NM 2000 1 15 USAA991289 1 19991208 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 44382 22888 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 20 INCH BY 2 FT AT STATION 344, LBL 10 RBL 10 T-CAP. CORROSIO N LEVEL 2. FABRICATED NEW T-CAP PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 2000011500410 20000115 00410 NM 2000 1 15 USAA991284 1 19991208 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 500B CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 44382 22888 CLT - DURNG Q-6 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY4 INCH AREA OF CORROSION AT STATION 500B STRINGER 27R SKIN. C ORROSION LEVEL 2. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2000011500411 20000115 00411 NM 2000 1 15 USAA991294 1 19991208 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 324 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 44382 22888 CLT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND A 2.25 INCH CRACK AT BS 324 STRINGER 17R SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 26. (M) 2 L 7 2 4F A16WE 2000011500412 20000115 00412 NM 2000 1 15 USAA991293 1 19991208 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 806 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 44382 22888 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A ..250 INCH CRACK AT BS 806 STRINGER 13L LOWER HINGE CUTOUT SKIN. INST ALLED FILLER AND DOUBLER PER SRM 53-30-03. (M) 2 L 7 2 4F A16WE 2000011500413 20000115 00413 NM 2000 1 15 USAA991292 1 19991208 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 44382 22888 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK AT BS 727B STRINGER 2-23 TIE CLIP. REMOVED AND REPLAC ED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000011500414 20000115 00414 NM 2000 1 15 USAA991291 1 19991208 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 44382 22888 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT RIGHT AFT SERVICE DOOR UPPER HINGE CUTOUT SKIN. INSTA LLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2000011500415 20000115 00415 NM 2000 1 15 USAA991290 1 19991208 A 5320 FITTING BOEING 737 7372B7 1384560 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 44382 22888 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT BS 1016, STRINGER 20R TIE FITTING. CORROS ION LEVEL 1. REMOVED CORROSION AND PRIMED PER SRM 51-10-06. (M) 2 L 7 2 4F A16WE 2000011500416 20000115 00416 NM 2000 1 15 USAASB99291 1 19991209 A 2720 65C370539 PCU BOEING 737 7372B7 1384560 NM RUDDER FAILED A USAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 EA 19 283AU 10202 23116 MCO - FLT 2611 - CAPTAIN REPORTED THAT 40 MILES NORTH OF MCO, AT FL120, THEY EXPERIENCED A POSSIBLE LEFT UNCOMMANDED RUD DER MOVEMENT. ROLL DISCONTINUED WHEN AUTOPILOT WAS DISENGATED. THE FIRST OFFICER OBSERVED THE AIRCRAFT ROLLED 25 DEGRE ES. FLIGHT CONTINUED AND LANDED AT MCO WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RE PLACED THE RUDDERPOWER CONTROL UNIT PER MM 27-21-9. RIGGING AND OPERATIONAL CHECK GOOD. COMPLIED WITH WORK CARD J227- 21-00. (M) 2 L 7 2 4F A16WE 2000011500417 20000115 00417 WP 2000 1 15 USAAD99170 1 19991202 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 823US 49142 CLT - THE CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FROM OVERHEAD BINS FIVE R IGHT AND TEN RIGHT. OPS CHECKED OK. (M) 2 L 7 2 4F A6WE 2000011500418 20000115 00418 WP 2000 1 15 USAAD99175 1 19991209 A 3350 87310272 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 PHL - THE LEFT AFT OVERWING EXIT IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT AFT OVERWING EXIT IDEN TIFIER LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2000011500419 20000115 00419 EU 2000 1 15 2000ZZZM14 1 19991026 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 21 262AT 0262 EMERGENCY BATTERY LOW VOLTAGE AT STATION 10WL, 10WL, 15WL, AND 29WL. REMOVED AND REPLACED BATTERY PACK 10WL, 18WL, 15WL AND 29WL AS PER MM 33-50-00. (M) 2 H 7 2 4T RT A53EU 2000011500420 20000115 00420 EU 2000 1 15 2000ZZZM15 1 19991008 A 5320 S5367800826801 SUPPORT AEROSP ATR72 ATR72212 EU FRAME 36-38 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 451AT 451 FLOOR SUPPORT CORRODED OUT BETWEEN FRAMES 36 AND 38. BLENDED AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED A ND REPLACED FLOOR SUPPORT IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500421 20000115 00421 EU 2000 1 15 2000ZZZM16 1 19991008 A 5347 EPNE95300013020 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29-36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 451AT 451 LEFT OUTBOARD AFT SEAT TRACK, CORRODED BETWEEN FRAMES 32 AND 33, OVER 29, 30, 33, 34 AND 35. BLENDED OUT AND FOUND TO B E OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED TRACK IAW EO NR E9-5300-013 R4 PART B. (M) 2 H 7 2 4T RT A53EU 2000011500422 20000115 00422 EU 2000 1 15 2000ZZZM17 1 19991008 A 5320 S53589536200 BRACKET AEROSP ATR72 ATR72212 EU FRAME 25 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 451AT 451 AIR CONDITIONER LINE ATTACHMENT BRACKET ON STRINGER 21L ATFRAME 25 IS CORRODED. FABRICATED ATTACHMENT BRACKET IAW SRM 5 3-51-26, FIG 102. INSTALLED BRACKET IAW SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2000011500423 20000115 00423 EU 2000 1 15 2000ZZZM19 1 19991008 A 5347 S5357020320202 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 27-33 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 451AT 451 LEFT OUTBOARD AFT MID SEAT TRACK, CORRODED BETWEEN FRAMES 28B AND 28C. BLENDED OUT OAN FOUND TO BE OUT OF LIMITS IAW SR M 53-00-00 FIG 304SHEET 2. BETWEEN F/A SEAT TRACKS IN TWO PLACES. BLENDED OUT AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW TRACK BETWEEN FRAMES 27 AND 33, IAW SRM 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000011500424 20000115 00424 EU 2000 1 15 2000ZZZM20 1 19991008 A 5347 EPNE95300013020 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29-36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 451AT 451 LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 32 AND 33OVER 33, 34, 29 AND 30. BLENDED OUT IAW SRM 53-00-00 AND FOUN D TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK BETWEEN FRAMES IAW EO NR E9-5300-013-020, PART B. (M) 2 H 7 2 4T RT A53EU 2000011500425 20000115 00425 EU 2000 1 15 2000ZZZM21 1 19991008 A 5315 S53672450620801 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 451AT 451 FLOORBEAM 36 IS CORRODED BETWEEN F/A SEAT TRACKS IN TWO PLACES. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21 -58. REMOVED AND REPLACED IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500426 20000115 00426 EU 2000 1 15 2000ZZZM22 1 19991028 A 5320 SUPPORT AEROSP ATR72 ATR72212 EU FRAME 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 448AM 448 PAX DOOR SIDE, FLOOR SUPPORTS, BETWEEN FRAMES 36 AND 39 HAVE CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-00.REMOVED AND INSTALLED SUPPORT IAW SRM 52-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500427 20000115 00427 EU 2000 1 15 2000ZZZM24 1 19991028 A 5320 S5367121729801 SUPPORT AEROSP ATR72 ATR72212 EU FRAME 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 448AM 448 PASSENGER DOOR, SIDE PLATE, HAS CORROSION ON DRAIN TRACK. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW SRM 53-6 1-00. REMOVED AND INSTALLED DRAIN TRACK IAW SRM 52-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500428 20000115 00428 EU 2000 1 15 2000ZZZM25 1 19991028 A 5320 SUPPORT AEROSP ATR72 ATR72212 EU FRAME 36-39 CORRO DED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 448AM 448 SERVICE DOOR SIDE, FLOOR SUPPORT, BETWEEN FRAME 36 AND 39,HAS CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMIT S, IAW SRM 51-00-00. REMOVED AND INSTALLED FLOOR SUPPORT IAW SRM 52-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500429 20000115 00429 EU 2000 1 15 2000ZZZM26 1 19991028 A 5347 EPNE95300013022 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 31-35 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 448AM 448 CORROSION ON LEFT AFT INBOARD SEAT TRACK, FROM FRAME 31 TO35. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW SRM 51-21-42. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9-5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000011500430 20000115 00430 EU 2000 1 15 2000ZZZM27 1 19991208 A 5320 S53670600820002 ZEE AEROSP ATR72 ATR72212 EU FRAME 39-40 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 LEFT Z-MEMBER IS CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW ATR 72 SRM 53-61-00. REMOVED AND INSTALLED Z- MEMBER IAW SRM 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000011500431 20000115 00431 EU 2000 1 15 2000ZZZM28 1 19991208 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29/36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 LEFT AFT INBOARD SEAT TRACK HAS CORROSION. BLENDED OUT AND FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED LEFT AFT I NBOARD SEAT TRACK IAW EO NR E9-5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000011500432 20000115 00432 EU 2000 1 15 2000ZZZM29 1 19991208 A 5320 S52176204402 FLOOR PAN AEROSP ATR72 ATR72212 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 NUMEROUS AREAS OF PASSENGER DOOR PAN HAVE SURFACE CORROSION. BLENDED OUT CORROSION IAW ATR-72 SRM 51-21-58. REMOVED A ND REPLACED DAMAGED SECTION OF PAX DOOR UPPER PANE IAW ATR-72 SRM 52-11-00. (M) 2 H 7 2 4T RT A53EU 2000011500433 20000115 00433 EU 2000 1 15 2000ZZZM30 1 19991108 A 5320 S53671290422 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME 38/39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 AFT FLOOR SUPPORT CHANNEL ON PAX DOOR SILL PLATE IS CORRODED, IAW SRM 51-21-58. REMOVED AND INSTALLED NEW AFT FLOOR SUPP ORT BETWEEN FRAME 38 AND 39 LEFT IAW ATR 42RM. (M) 2 H 7 2 4T RT A53EU 2000011500434 20000115 00434 EU 2000 1 15 2000ZZZM31 1 19991108 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FRAME 39/40 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 AFT FLIGHT ATTENDANT SEAT TRACK FOUND CORROSION. WHERE DOOR POST MOUNT ATTACHES. SEAT TRACK OUT OF LIMITS AFTER CORROS ION REMOVAL IAW SRM 53-00-00. REMOVED AND INSTALLED NEW SEAT TRACK IAW EO E9-5300-013R4. (M) 2 H 7 2 4T RT A53EU 2000011500435 20000115 00435 EU 2000 1 15 2000ZZZM32 1 19991108 A 5315 S53672409218 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FRAME 40 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 FLOORBEAM NR 40 HAS CORROSION (AFT CARGO AND LAVATORY AREA). FOUND TO BE OUT OF LIMITS IAW 53-61-00. FLOORBEAM NR 40 REPAIRED IAW 53-61-40, FIG 413. (M) 2 H 7 2 4T RT A53EU 2000011500436 20000115 00436 NM 2000 1 15 USAA991344 1 19991208 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 22888 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM APPROX 6 FT FORWARD CABIN STATION 328 - RBL 51. C ORROSION LEVEL. INSTALLED DOUBLER PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 2000011500437 20000115 00437 EU 2000 1 15 2000ZZZM18 1 19991008 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29 - 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 451AT 451 LEFT INBOARD AFT SEAT TRACK, CORRODED BETWEEN FRAMES 19, 30, 31, 32 AND 33. BLENDED OUT AND FOUND TO BE OUT OF LIMITS I AW SRM 53-00-00. REMOVED AND REPLACED TRACK BETWEEN FRAMES IAW EO E9-5300-013 R4 PART B. (M) 2 H 7 2 4T RT A53EU 2000011500438 20000115 00438 EU 2000 1 15 2000ZZZM23 1 19991028 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 448AM 448 FLOORBEAM 38 HAS CORROSION AROUND SCREW HOLES UPPER AND LOWER SURFACES. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-42. REMOVED AND INSTALLED FLOORBEAM IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500439 20000115 00439 EU 2000 1 15 2000ZZZM33 1 19991108 A 5320 S53678008216702 ZEE AEROSP ATR42 ATR42300 8680920 EU FRAME 39/41 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 Z-MEMBER RIGHT OF AFT CARGO HAS CORROSION AND WAS FOUND TO BE OUT OF LIMITS WHEN CORROSION WAS REMOVED IAW SRM 51-61-00. REPLACED Z-MEMBER IAW SRM 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000011500440 20000115 00440 EU 2000 1 15 2000ZZZM34 1 19991108 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 RIGHT OUTBOARD SPLICE ON FLOORBEAM 36 HAS CORROSION FROM SPLICE TO FRAME 36. BLENDED IAW SRM 51-21-58 AND FOUND BEAM CO RROSION BEYOND LIMITS IN TWO AREAS. REPAIRED FLOORBEAM IAW SRM 53-00-00 FIG 438. (M) 2 H 7 2 4T RT A53EU 2000011500441 20000115 00441 EU 2000 1 15 2000ZZZM35 1 19991108 A 5347 S53375001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FRAME 13/23 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 FOUND CORROSION ON LEFT INBOARD SEAT TRACK FORWARD CARGO AREA. CLEANED TRACK AND FOUND TO BE BEYOND LIMITS IAW 53-00-00 SRM PAGE 315. EO NR E9-5300-013 R4 PART B WAS SATISFACTORILY ACCOMPLISHED. (M) 2 H 7 2 4T RT A53EU 2000011500442 20000115 00442 EU 2000 1 15 2000ZZZM36 1 19991108 A 5320 S5367800826901 SILL PLATE AEROSP ATR42 ATR42300 8680920 EU FRAME 38/39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 SERVICE DOOR SILL PLATE, AFT SUPPORT, BETWEEN FRAME 38 AND 39, HAS CORROSION ON BOTTOM SIDE, BY NUTPLATES. REMOVED, BLE NDED AND FOUND TO BE BEYOND LIMITS IN SRM 53-16-15. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500443 20000115 00443 EU 2000 1 15 2000ZZZM37 1 19991108 A 2842 S7667962 FUEL PROBE AEROSP ATR72 ATR72212 EU LT WING CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 TOP OF LEFT WING, HIGH LEVEL SENSOR HAS FLOORING PAINT AND CORROSION. BLENDED CORROSION IAW ATR SRM 53-14-12. REMOVED AND REPLACED LEFT MAIN OUTBOARD TANK PROBE PER JIC 28-42-72 RA/10000-001. (M) 2 H 7 2 4T RT A53EU 2000011500444 20000115 00444 EU 2000 1 15 2000ZZZM38 1 19991108 A 5714 52105 PANEL AEROSP ATR72 ATR72212 EU WING BOX CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 CENTER WING DRY BAY PAREL NR 52105 HAS CORROSION, UNIT TRANSFERED FROM CRIC NR 7860. BLENDED CORROSION IAW ATR SRM 53-1 4-12. INSTALLED NEW CENTER WING DRY BAY PANEL IAW ATR 72 AMM/JIC 57-00-00 OAC. (M) 2 H 7 2 4T RT A53EU 2000011500445 20000115 00445 EU 2000 1 15 2000ZZZM39 1 19991108 A 5730 PANEL AEROSP ATR72 ATR72212 EU RT WING CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 RIGHT FEEDER TANK PANEL NR 622CT HAS CORROSION ON IT TRANSFERED FROM CRIC NR 7873. BLENDED CORROSION IAW ATR SRM 53-14- 12. INSTALLED NEW RIGHT FEEDER TANK PANEL IAW ATR72 AMM/JIC 57-00-00 OAC. (M) 2 H 7 2 4T RT A53EU 2000011500446 20000115 00446 EU 2000 1 15 2000ZZZM40 1 19991108 A 5730 PANEL AEROSP ATR72 ATR72212 EU LT WING CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 LEFT FEEDER TANK ACCESS PANEL NR 622CT HAS CORROSION ON IT TRANSFERRED FROM CRIC NR 7858. BLENDED CORROSION IAW ATR SRM 53-14-12. INSTALLED NEW LEFT FEEDER TANK PANEL IAW ATR72 AMM/JIC 57-00-00 OAC. (M) 2 H 7 2 4T RT A53EU 2000011500447 20000115 00447 EU 2000 1 15 2000ZZZM41 1 19991108 A 5730 PANEL AEROSP ATR72 ATR72212 EU LT WING CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 LEFT OVERWING REFUELING PANEL HAS CORROSION. INSTALLED NEW PANEL IAW ATR72 AMM/JIC 57-00-00 OAC. (M) 2 H 7 2 4T RT A53EU 2000011500448 20000115 00448 EU 2000 1 15 2000ZZZM42 1 19991108 A 5315 S53680021602 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 RIGHT AFT CARGO Z-MEMBER BY FLOORBEAM 39 CORRODED AROUND PLATE NUTS. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IA W SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW ATR72 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500449 20000115 00449 EU 2000 1 15 2000ZZZM43 1 19991108 A 5347 S5367001212 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 RIGHT F/A SEAT TRACK CORRODED. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9-5300-013. (M) 2 H 7 2 4T RT A53EU 2000011500450 20000115 00450 EU 2000 1 15 2000ZZZM44 1 19991108 A 5347 S5367001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 RIGHT F/A SEAT TRACK CORRODED. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9-5300-013. (M) 2 H 7 2 4T RT A53EU 2000011500451 20000115 00451 EU 2000 1 15 2000ZZZM45 1 19991108 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 RIGHT AFT INBOARD SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALL ED SEAT TRACK IAW EO NR E9 5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000011500452 20000115 00452 EU 2000 1 15 2000ZZZM46 1 19991108 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 FLOORBEAM, FRAME 36, DAMAGED. REMOVED DAMAGED FLOORBEAM. REPLACED SECTION IAW SRM 53-00-00 FIG 435. (M) 2 H 7 2 4T RT A53EU 2000011500453 20000115 00453 EU 2000 1 15 2000ZZZM47 1 19991108 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 38 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 FRAME 38, CORRODED AROUND NTU PLATED. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND IN STALLED FLOORBEAM SECTION AND PERFORMED SPLICE IAW SRM 53-00-00 FIG 435. (M) 2 H 7 2 4T RT A53EU 2000011500454 20000115 00454 EU 2000 1 15 2000ZZZM48 1 19991108 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 LEFT F/A SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT T RACK IAW EO NR E9 5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000011500455 20000115 00455 EU 2000 1 15 2000ZZZM49 1 19991108 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 LEFT AFT INBOARD SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLE D SEAT TRACK IAW EO NR E9 5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000011500456 20000115 00456 EU 2000 1 15 2000ZZZM50 1 19991108 A 5347 S53672407252 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 LEFT AFT SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT T RACK IAW EO NR E9 5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000011500457 20000115 00457 EU 2000 1 15 2000ZZZM51 1 19991108 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 29 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 369AT 369 RIGHT AFT INBOARD SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALL ED SEAT TRACK IAW EO NR E9 5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000011500458 20000115 00458 EU 2000 1 15 2000ZZZM52 1 19991210 A 5320 S5367800920102 SUPPORT AEROSP ATR72 ATR72212 EU FRAME 36-38 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 RIGHT CHANNEL, FLOOR SUPPORT, BETWEEN FRAMES 36 AND 38 CORRODED. BLENDED OUT OT BEYOND MANUAL LIMITS. INSTALLED NEW FL OOR SUPPORT BETWEEN FRAME 36 AND 38, IAW ATR 72 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2000011500459 20000115 00459 EU 2000 1 15 2000ZZZM53 1 19991210 A 5347 S53678001212 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 39-40 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 CORROSION AROUND SCREW HOLES TO SEAT TRACK. BLENDED OUT CORROSION TO SEAT TRACK IAW ATR72 SRM 51-21-42. EO NR E9-5300- 015 R7 PART 'B' WAS SATISFACTORILY ACCOMPLISHED. (M) 2 H 7 2 4T RT A53EU 2000011500460 20000115 00460 EU 2000 1 15 2000ZZZM54 1 19991210 A 5320 S5367800821602 ZEE AEROSP ATR72 ATR72212 EU FRAME 39-41 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 FOUND CORROSION ON RIGHT Z-MEMBER IN AFT CARGO. BLENDED OUT CORROSION IAW SRM 51-21-58. REMOVED AND INSTALLED MEMBER I AW ATR SRM 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000011500461 20000115 00461 EU 2000 1 15 2000ZZZM55 1 19991210 A 5320 S5367800821602 ZEE AEROSP ATR72 ATR72212 EU FRAME 39-41 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 FOUND CORROSION ON LEFT Z-MEMBER IN LAV BLENDED OUT CORROSION IAW SRM 51-21-58. FOUND TO BE BEYOND LIMITS. REMOVED AND INSTALLED MEMBER IAW ATR SRM 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000011500462 20000115 00462 EU 2000 1 15 2000ZZZM56 1 19991210 A 5315 S5367240825402 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 FLOORBEAM NR 39 HAS CORROSION AROUND SEVERAL HOLES, UPPER AND LOWER SURFACE AT FLANGE. BLENDED CORRODED AREAS IAW SRM 5 1-21-58. REMAINING THICKNESS .053 INCH. REMOVED AND INSTALLED NEW FLOORBEAM NR 39 IAW ATR SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500463 20000115 00463 EU 2000 1 15 2000ZZZM57 1 19991210 A 5320 S5367240620601 STANCHION AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 FLOORBEAM NR 36 LEFT STANCHION HAS CORROSION AROUND GROUND SCREW HOLE. BLENDED CORRODED AREAS IAW SRM 51-21-58. REMOVE D AND INSTALLED STANCHION IAW ATR SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500464 20000115 00464 EU 2000 1 15 2000ZZZM58 1 19991210 A 5320 S5367240725201 STANCHION AEROSP ATR72 ATR72212 EU FRAME 38 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 FLOORBEAM NR 38 LEFT STANCHION HAS CORROSION AROUND SEVERAL HOLES. BLENDED CORRODED AREAS IAW ATR-72 SRM 51-2158, REMAI NING THICKNESS .053 INCH. REMOVED AND INSTALLED NEW FLOORBEAM NR 38 IAW ATR SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500465 20000115 00465 EU 2000 1 15 2000ZZZM59 1 19991210 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 FLOORBEAM NR 36 HAS CORROSION AROUND SEVERAL HOLES UPPER AND LOWER SURFACE AT FLANGE. BLENDED CORRODED AREAS IAW ATR-72 SRM 51-21-58, REMAINING THICKNESS .054. REMOVED AND INSTALLED NEW FLOORBEAM NR 36 IAW ATR SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000011500466 20000115 00466 EU 2000 1 15 2000ZZZM60 1 19991210 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 34-36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 LEFT AFT OUTBOARD SEAT TRACK HAS CORROSION BETWEEN FLOORBEAMS 34 TO 36. BLENDED CORRODED AREAS IAW ATR-72 SRM 51-21-42. REMOVED AND INSTALLED NEW LEFT OUTBOARD SEAT TRACK IAW ATR-72 SRM 51-25-04. (M) 2 H 7 2 4T RT A53EU 2000011500467 20000115 00467 EU 2000 1 15 2000ZZZM61 1 19991210 A 5320 BRACKET AEROSP ATR72 ATR72212 EU FRAME 36-38 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 PASSENGER DOOR, TOP TWO FAIRING BRACKETS CORRODED. REMOVED CORROSION IAW ATR-72 SRM 51-25-42. MFG P/N S53689609016 AND S5389609014. REMOVED CORROSION, CLEANED AND TREATED PANEL AND PAINTED IAW SRM 51-25-42. (M) 2 H 7 2 4T RT A53EU 2000011500468 20000115 00468 EU 2000 1 15 2000ZZZM62 1 19991210 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 34-36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 LEFT AFT INBOARD SEAT TRACK HAS CORROSION AREAS FROM FLOORBEAM 34 TO 36. BLENDED CORROSION IAW ATR-72 SRM 51-21-42. CO MPLIED WITH EO NR E9-5300-013 R4, PART 'B' WAS SATISFACTORY ACCOMPLISHED. (M) 2 H 7 2 4T RT A53EU 2000011500469 20000115 00469 EU 2000 1 15 C2XA99BT112 1 19991205 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69902 385 BTV - FLT 3655 - FOUND STAIRWAY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED GROUND ILLUMINATION LIGHT INSIDE CABIN DOOR. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 2000011500470 20000115 00470 EU 2000 1 15 C2XA99IA608 1 19991201 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING A-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-320 JIC 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500471 20000115 00471 SO 2000 1 15 C2XA99IA610 1 19991204 A 4910 4951327 CLAMP EMB 145 EMB145 SO APU BROKEN A C2XA H DEACTIVATE SYST/CIRCUITS O OTHER TX TAXI/GRND HDL 1 SW 09 27962 145110 GSP - FLIGHT 4205 - APU WILL NOT START, PILOT PLACED ON MEL, AND CONTINUED NORMAL FLIGHTS. DURING TROUBLESHOOTING, MAIN TENANCE FOUND THE APU COMBUSTION HOUSING V-BAND CLAMP BROKEN. THE APU WAS REMOVED AND REPLACED, AND THE AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000011500472 20000115 00472 EU 2000 1 15 C2XA99IA609 1 19991205 A 3350 3013017 BATTERY AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE VISIT, NR 2 THE AFT CABIN AND GALLEY AREA EMERGENCY LIGHTS FAILED TO OPERATE. MAINTENANCE FOUN D THE POWER SUPPLY LOCATED AT NR 62WL TO HAVE A DISCHARGED BATTERY PACK. REPLACED BATTERY PACK AND PERFORMED OPERATIONA L TEST OF EMERGENCY LIGHTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500473 20000115 00473 EU 2000 1 15 C2XA99IA595 1 19991121 A 3350 3101210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING MAINTENANCE INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-320 MM 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500474 20000115 00474 GL 2000 1 15 C2XA99IA596 2 19991124 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT LEAKING A C2XA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 14960 2529 145100 CAE311086 IAH - DURING FLIGHT 3998, THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE CREW RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2000011500475 20000115 00475 EU 2000 1 15 C2XA99IA619 1 19991128 A 5347 S53678001214 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 39-41 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 DURING CONTINENTAL EXPRESS AIRLINES C-CHECKS, FOUND CORROSION ON SEAT TRACK LBL 5 FROM FRAME 39 TO 41. REMOVED AND REPL ACED SEAT TRACK IAW SRM 51-25-02, 51-25-04, 51-21-17 AND 51-21-27. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500476 20000115 00476 EU 2000 1 15 C2XA99IA617 1 19991128 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 34 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND CORROSION ON SEAT TRACK RBL 13 AT FRAME 34. REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 51-21-42, 53-00-00, 51-25-02, 51-21-17 AND 51-21-27. AIRCRAFT APPROVE D FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500477 20000115 00477 EU 2000 1 15 C2XA99IA618 1 19991128 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND CORROSION ON SEAT TRACK LBL 5 FROM FRAME 36 TO 39. REMOVED AND REPLA CED SEAT TRACK IAW SRM 51-25-04 AND 51-21-31. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500478 20000115 00478 EU 2000 1 15 C2XA99IA616 1 19991128 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND CORROSION ON SEAT TRACK RBL 9 FROM FRAME 36 TO 39. REMOVED AND REPLA CED SEAT TRACK IAW SRM 51-25-02, 51-25-04 AND 51-21-31. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500479 20000115 00479 EU 2000 1 15 C2XA99IA615 1 19991128 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 39-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND CORROSION ON SEAT TRACK RBL 9 FROM 39 TO 40. REMOVED AND REPLACED SE AT TRACK IAW SRM 51-25-02, 51-25-04, 51-21-17, 51-21-18, 51-21-28 AND 51-21-31. AIRCRAFT APPROVED FOR RETURN TO SERVICE . (M) 2 H 7 2 4T RT A53EU 2000011500480 20000115 00480 EU 2000 1 15 C2XA99IA614 1 19991128 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FRAME 34/36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 DURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND CORROSION ON SEAT TRACK RBL 37 BETWEEN FRAMES 34 AND 36. REMOVED COR RODED SECTION AND SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 51-21-42, 53-00-00, 51-25-00 AND 51-25-04. AIRCRAFT APPR OVED FOR RETURN FOR RETURN TO SERVICE.. (M) 2 H 7 2 4T RT A53EU 2000011500481 20000115 00481 SO 2000 1 15 C2XA99IA613 1 19991114 A 5330 12019229001 SKIN EMB 120 EMB120RT SO FRAME 29 CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FUSELAGE SKIN CHAFED AT FRAME 29, STRINGER 18L. REPAIRED IAW SRM 53-00-01. A IRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000011500482 20000115 00482 SO 2000 1 15 C2XA99IA612 1 19991114 A 5330 12017416041 SKIN EMB 120 EMB120RT SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FUSELAGE SKIN DENTED AFT OF LAV SERVICE PORT. REPAIRED IAW SRM 53-00-01. AIR CRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000011500483 20000115 00483 SO 2000 1 15 C2XA99IA611 1 19991114 A 5315 1204449001 FLOORBEAM EMB 120 EMB120RT SO FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 DURING CONTINENTAL EXPRESS C-CHECK, FOUND FLOOR CROSSBEAM AT FRAME 38 CORRODED. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000011500484 20000115 00484 SO 2000 1 15 C2XA99IA628 1 19991201 A 3350 1011103 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16723 120169 CLE - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REM OVED AND REINSTALLED THE AFFECTED LIGHT ASSEMBLY IAW EMB120 MM 3-52-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A31SO 2000011500485 20000115 00485 SO 2000 1 15 C2XA99IA627 1 19991203 A 3350 1317 BULB EMB 120 EMB120RT SO FUSELAGE FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 22727 120177 CLE - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT REAR EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB,AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000011500486 20000115 00486 EU 2000 1 15 C2XA99IA597 1 19991123 A 3350 E0062D1S4BJ0A SWITCH AEROSP ATR42 ATR42500 EU COCKPIT FAILED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 09 15447 505 IAH - FLT 3521 - THE CREW REPORTED THAT THE EMERGENCY LIGHTS ILLUMINATED IN THE CABIN AND THE EMERGENCY EXIT ANNUNCIATOR FAILED TO ILLUMINATE WHEN PUSHED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED S WITCH 2WL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500487 20000115 00487 SO 2000 1 15 C2XA99IA622 1 19991115 A 2910 MILH5606 HYD SYSTEM EMB 120 EMB120RT SO NACELLE LOW A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 09 15732 120195 CLE - FLT 3392 - THE CREW REPORTED THAT AFTER GEAR RETRACTION, ALL THREE 'B' SYSTEM RED LIGHTS REMAINED ILLUMINATED FOR 45 SECONDS AFTER GEAR WAS APPARENTLY UP. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE GREEN HYDRAULIC SYSTEM TO BE LOW. MAINTENANCE SERVICED THE AFFECTED HYDRAULIC SYSTEM, AND PERFORMED GEAR EXTENSION/RETRACTION IAW EMB120 MM 32-32-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000011500488 20000115 00488 SO 2000 1 15 C2XA99IA621 1 19991117 A 3350 2514115 LIGHT EMB 120 EMB120RT SO CABIN MISINSTALLED A C2XA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 SW 09 16724 120171 ALB - DURING PRE-FLIGHT INSPECTION, THE CRWE REPORTED THAT THE AISLE PATH EMERGENCY LIGHTING DID NOT HAVE RED LIGHTS AT ROW 6. MAINTENANCE REPOSITIONED THE AFFECTED LIGHTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000011500489 20000115 00489 SO 2000 1 15 C2XA99IA620 1 19991123 A 3350 1367 BULB EMB 120 EMB120RT SO FUSELAGE FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16710 120106 CLE - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000011500490 20000115 00490 CE 2000 1 15 C2XA99CL127 1 19991203 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE LT GEAR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 87557 1230 0927A UE246 CLE - FLT 3009 - AFTER TAKEOFF FROM CLE, THE LANDING GEAR WOULD NOT RETRACT. GREEN INDICATION LIGHTS REMAINED ON WITH N O INTRANSIT LIGHT. AIRCRAFT RETURNED TO CLE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDI NG GEAR ACTUATOR IAW BEECH MM 32-30-10. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2000011500491 20000115 00491 EU 2000 1 15 C2XA99IA624 1 19991205 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE VISIT INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 2000011500492 20000115 00492 EU 2000 1 15 C2XA99IA623 1 19991205 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE VISIT INSPECTION, THE GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500493 20000115 00493 CE 2000 1 15 C2XA99IA626 1 19991203 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 87557 UE246 CLE - FLT 3009, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR IAW BEECH MM 32-30-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2000011500494 20000115 00494 EU 2000 1 15 C2XA99IA625 1 19991207 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK AT 10 WL IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000011500495 20000115 00495 SW 2000 1 15 CA990614020 1 19990527 A 6310 205040001101 TRANSMISION BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE MAIN ROTOR MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA LE07560A (CAN) MAIN TRANSMISSION MAKING ROARING NOISE. AFTER SHUTDOWN THE TRANSMISSION WAS MAKING A CLICKING NOISE. INSPECTION FOUND METAL IN THE FILTERS AND CHIP DETECTORS. TRANSMISSION AND MAST ASSEMBLY WERE REPLACED. TRANSMISSION GEAR SENT TO TSB LABS FOR ANALYSIS ON 29 DEC 99. 1 G 7 1 4U 4 U H1SW E17EA 2000011500496 20000115 00496 GL 2000 1 15 CA991028060 2 19991022 A 7320 23056915 CONNECTOR 23060274 BELL 407 407 SW ALLSN 250C 250C47B GL FADEC FAILED W H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 CA 949 JG7ALK0421 CAE847153 (CAN) ITEM SENT FOR TRANSLATION. ONE TIME FAILURE IND NR 3 AND AND 8 RESTART SYSTEM. HUMIDITY WITHIN CONNECTOR SPECIF IED TO BE THE PROBLEM ASSOCIATED TO THE WRONG INDICATION ON THE CIT THAT CAUSED THE FIXED FAIL OF THE FADEC. 1 G 7 1 3U 3 U O H2SW E1GL 2000011500497 20000115 00497 NE 2000 1 15 CA991208004 2 19991101 A 7321 7898426009 ECU PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 16139 3880 121158 121158 851115 (CAN) TORQUE AND POWER REDUCTION REPORTED. MANUAL MODE SELECTED AND ENGINE STABILIZED. EEC FAILURE ESTABLISHED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000011500498 20000115 00498 NE 2000 1 15 CA991208007 2 19991110 A 7210 RGB120322 GEARBOX PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE REDUCTION G/B CONTAMINATED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 13381 120373 120373 870601 (CAN) RGB CHIP FLAGGED. MATERIAL WAS BEARING DEBRIS. BEARING PART NUMBER NOT SPECIFIED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000011500499 20000115 00499 NE 2000 1 15 CA991208029 2 19991128 A 7530 310848501 VALVE PWA PW123 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE NR 1 ENGINE STUCK W O OTHER O OTHER NR NOT REPORTED 1 CA 123124 123124 901161 (CAN) MIST IN CABIN REPORTED AFTER SELECTING NR 1 BLEED ON. ENG P2.5-3 AIR SWITCH STUCK IN P3 POSITION CAUSING OIL TO BE FORCED PAST THE SEALS AND INTO COMPRESSOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000011500500 20000115 00500 NE 2000 1 15 CA991208031 2 19991104 A 7321 7863916 FCU PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE FAILED W H DEACTIVATE SYST/CIRCUITS R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA 121165 121165 891129 (CAN) TORQUE ROLLBACK WITH LARGE WF FLUCTUATIONS EXPERIENCED, MANUAL MODE SELECTED WHICH REDUCED FLUCTUATIONS. HMU AND EEC INSPECTED AND FOUND FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000011500501 20000115 00501 EA 2000 1 15 CA991208035 1 19991122 A 7921 45E041 VALVE PWA PW123 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE OIL COOLER STUCK W O OTHER J WARNING INDICATION CR CRUISE 1 CA 123132 123132 901056 (CAN) OIL TEMPERATURE REGISTERING VERY LOW. TEMPERATURE CONTROL VALVE FOUND STUCK IN OIL COOLER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000011500502 20000115 00502 NE 2000 1 15 CA991208045 2 19991107 A 7230 230371302 SEAL LYC ALF502R5 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 3 ENGINE LEAKING W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 1750 LF05629A LF05629A (CAN) ODOR IN CABIN WITH ENGINE AIR SELECTED. ACM SELECTED OFF, MAINTENANCE FOUND THAT OIL WAS POOLING AT THE NR 9 SEAL LOCATION OF THE NR 3 ENGINE. SEAL AND FACEPLATE WERE REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 2000011500503 20000115 00503 EA 2000 1 15 CA991208060 2 19991014 A 7532 3033063 BLEED VALVE PWA PT6T3 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA NR 2 ENGINE SURGING W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 2758 CPPS62075 CPPS62075 (CAN) BLEED VALVE SPECIFIED TO HAVE HISTORY OF CAUSING SIMILAR ENGINE SURGING ON OTHER OPERATORS' A/C. SB 5274 R3 FOR P OSSIBLE IMPROVED BLEED VALVE CLOSING OPS. 1 G 7 1 4U 4 U H4SW E22EA 2000011500504 20000115 00504 SO 2000 1 15 CA991208062 2 19991104 A 8530 CN635444EC CYLINDER CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO MCAULY 2A34C D2A34C58 GL NR 2 SEPARATED W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA 675 646652CF 15966770DAB 777568 (CAN) ROUGH ENGINE ON TAKEOFF EXPERIENCED. INSPECTION REVEALED NR 2 CYLINDER SEPARATED AND CRACKED FROM EXHAUST PORT T HROUGH BOTH SPARK PLUGS AND COOLING FINS. 1 H 7 1 3O 3 O 3A24 E5CE 5 C P3EA 2000011500505 20000115 00505 CE 2000 1 15 CA991208064 1 19991111 A 6120 GUIDE COLLAR HARTZL HCB4MP3A BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL PITCH CHANGE FAILED W E C ENGINE SHUTDOWN ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA FW838 PCE32044 FW838 (CAN) THE PITCH CHANGE GUIDE COLLAR WAS CHANGED DUE TO A CLOSE TOLERANCE FIT (STILL WITHIN LIMITS) FAILURE. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2000011500506 20000115 00506 SO 2000 1 15 CA991208068 1 19991123 A 5521 4595106 SPAR PIPER 5501602 PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11403 PCE51482 BU5496 (CAN) INSPECTION AS INDICATED IN PIPER S/B 1032. LEADING EDGE SKIN REMOVED AND FOUND 2 CRACKS ON OUTBOARD END OF SPAR. ONE CRACK WAS ON TOP IN THE BEND RADIUS AND EXTENDING 1 INCH INBOARD BEHIND THE HINGE. THE OTHER CRACK EXTENDED 1 INCH INBOARD ON THE LOWER SPAR FLANGE AT THE HINGE. INSTALLED SPAR MODIFICATION KIT (PIPER P/N 766-655) REFERENCE DRAWING: 88258 PAGES 1-6. FACTORS: AIRCRAFT TTSN AND MORE PROP WASH ON THE LEFT SIDE OF AIRCRAFT. 1 L 7 2 3T 4 T A8EA E4EA 6 C P15EA 2000011500507 20000115 00507 SO 2000 1 15 CA991208071 1 19991022 A 2460 587886 MASTER SWITCH PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL COCKPIT FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA RL609561A DJ9088A (CAN) MASTER SWITCH TURNS ON BY ITSELF USUALLY AT NIGHT AND HIGH MOISTURE. SITUATION CAUSING DEAD BATTERIES. THIS HAS BEEN RECURRING ON SEVERAL DIFFERENT A/C OVER THE PAST 8 YEARS. SUBMITTER STATED COMPANY POLICY IS TO REPLACE WITH A NEW SWITCH EACH TIME, BUT THIS HAS NOT SOLVED THE PROBLEM. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2000011500508 20000115 00508 SO 2000 1 15 CA991208072 1 19991022 A 7920 LINE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA HARTZL HCE2Y HCE2YR2 GL OIL PRESSURE LOOSE W C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA RL103161 CJ242 (CAN) OIL PRESSURE LINE LOOSE AFTER TAKEOFF AS NOTED BY OIL ON LEFT COWLING. AIRCRAFT RETURNED FOR LANDING (APPROXIMATE LY 3 MINUTE FLIGHT). ENGINE SHUT DOWN AFTER LANDING. 1 L 7 2 3O 3 O A20SO E14EA 5 C P9EA 2000011500509 20000115 00509 NE 2000 1 15 CA991208074 2 19990424 A 7250 597602 BLADE PWA JFTD12A4A SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE TURBINE SECTION BROKEN W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION HO HOVERING 1 CA 4962 1057 672481 672481 (CAN) OPERATOR HAS IMPOSED A LIMIT OF 36 GRAMS MINIMUM WEIGHT ON ALL THE BLADES AT INSTALLATION. A PERIODIC STRUM CHECK IS ALSO IMPOSED. 2 G 7 2 4U 4 U H4EA E15EA 2000011500510 20000115 00510 NE 2000 1 15 CA991208075 2 19991114 A 7322 VALVE PWA JFTD12A4A SKRSKY S64 S64E 8142604 NE PWA JFTD12 JFTD12A4A 52047 NE FUEL SYSTEM WORN W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 CA 767 672523 672523 (CAN) ENGINE EXPERIENCED A SOFT STALL; POWER LOSS AND AN INCREASE IN ITT. THIS IS DUE TO AN OVERFUEL OR INADEQUATE AIR CONDITION IN THE COMBUSTOR. CORRECTIVE ACTIONS WERE DEVELOPED BY AIR CRANE AND P&W. HPX FUEL PUMP GEAR DESIGN CHANGE ELIMINATING THE MATERIAL THAT WAS ON THE SURFACE OF THE GEARS, WHICH, WHEN PARTED CAUSED THE P&D TO FAIL. FCU WEAR IMPR OVEMENTS AND AN AUTO IGNITION SYSTEM TO PREVENT THE RAPID ITT RISE WERE ALSO UNDER DEVELOPEMENT. 2 G 7 2 4U 4 U H4EA E15EA 2000011500511 20000115 00511 EA 2000 1 15 CA991208076 2 19991026 A 7200 ENGINE PWA PT6A28 BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL LEFT FAILED W E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CA PCE50063 PCE50063 BUA20609 (CAN) NEW OVERHAULED ENGINE INSTALLED, OIL PRESSURE LOW AND NOT DUE TO POWER SECTION OR PRESSURE RELIEF VALVE. ENGINE RETURNED. 1 L 7 2 3T 4 T A14CE E4EA 6 C P15EA 2000011500512 20000115 00512 SO 2000 1 15 CA991208079 2 19991110 A 7414 IMPULSE COUPLING SLICK 6310 CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO HARTZL HCC3Y PHCC3YF1 GL MAGNETO WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1229 93040127 293213R EE2789A (CAN) IMPULSE COUPLING WORN PAST LIMITS. DISTRIBUTOR DRIVE GEAR BUSHES WEAR WAS EXCESSIVE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P25EA 2000011500513 20000115 00513 SO 2000 1 15 CA991208082 1 19991125 A 8011 MZ4222R STARTER PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA HARTZL HCC2Y HCC2YK1 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 140 RL923348 CH11122 (CAN) FOUR SEPARATE OCCURRENCES OF STARTER FAILURE EXPRESSED BY OPERATOR ALL RELATING TO THE BENDIX DRIVE GEAR EITHER NO T ENGAGING OR WILL NOT DISENGAGE DURING START SEQUENCE. 1 L 7 1 3O 3 O A3SO 1E4 5 C P920 2000011500514 20000115 00514 CE 2000 1 15 CA991208083 1 19991128 A 3233 HFR6M ROD END 1053840021 BEECH 76 76 1153005 CE LYC O360 O360A1G 41514 EA HARTZL HCM2Y HCM2YR GL RT MLG FAILED W O OTHER O OTHER CR CRUISE 1 CA L2641636A FB941 (CAN) IN CRUISE, RT MAIN GEAR EXTENDED AND LOCKED DOWN. THE LEFT MAIN AND NOSE GEARS WERE LOWERED AND THE LANDING WAS C OMPLETED WITHOUT EVENT. THE RIGHT ACTUATOR CYLINDER (P/N 105-384002-1) FAILED AT ROD END (P/N HFR6M). SERVICE DIFFICUL TY REPORTED TO TSB AND TSD INSPECTION COMPLETED AND WILL REPORT ON DEFECT PART CONDITION. 1 L 7 2 3O 3 O A29CE E286 5 C P43GL 2000011500515 20000115 00515 GL 2000 1 15 CA991208086 3 19991119 A 6114 57A18517 BEARING HARTZL HCB3TN3DY DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL PROP HUB CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 823 BU10148 PCE50230 BU10148 (CAN) CORROSION FOUND ON ALL THREE BLADE THRUST BEARINGS IN HUB AREA. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 2000011500516 20000115 00516 SO 2000 1 15 CA991208089 1 19991110 A 3297 WIRE PIPER PA34 PA34200T 7103406 SO CONT O360 LTSIO360E 17025 SO HARTZL HCC2Y BHCC2YF2 GL LT MLG BROKEN W A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 CA 304562 AN1137 (CAN) LEFT LANDING GEAR DOWN AND LOCKED LIGHT MICROSWITCH WIRE BUNDLE BROKE AT TOP OF GEAR LEG CAUSING UNSAFE INDICATION OF LEFT GEAR. AIRCRAFT LANDED WITH BOTH ENGINES FEATHERED. 1 L 7 2 3O 3 O A7SO E9CE 5 C P920 2000011500519 20000115 00519 GL 2000 1 15 CA991209005 2 19991021 A 7321 23061824 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 138 3AAC2476 CAE801483BA (CAN) ENGINE WAS FAILING DECEL CHECKS. 1 G 7 1 3U 3 U H2SW E4CE 2000011500520 20000115 00520 SW 2000 1 15 CA991209006 1 19991020 A 7714 206062627003 SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL TACH GENERATOR SHEARED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 151796 CAE832831 (CAN) TACHOMETER/GENERATOR SHAFT SHEARED, CAUSING THE ENGINE OUT WARNING SYSTEM TO COME ON DURING THE TAKEOFF ROLL. 1 G 7 1 3U 3 U H2SW E4CE 2000011500521 20000115 00521 GL 2000 1 15 CA991209007 2 19991112 A 7532 23053176 BLEED VALVE ALLSN BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL COMPRESSOR FAILED W L ABORTED APPROACH E VIBRATION/BUFFET AP APPROACH 1 CA 773 FF44889 CAE831866 (CAN) COMPRESSOR STALLS WHEN POWER APPLIED AT ALT. 1 G 7 1 3U 3 U H2SW E4CE 2000011500522 20000115 00522 EU 2000 1 15 CA991209012 1 19991128 A 2910 A17662405 LINE MENASCO 1070121 FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU HYD SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 9084 (CAN) ON CLIMB, CREW NOTICED THAT THE FLIGHT CONTROL MASTER CAUTION LIGHT CAME ON AND THE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE HAD DROPPED TO ZERO. ALL ASSOCIATED NR 2 SYSTEM CAUTION LIGHTS WERE NOW ON. AIRCRAFT RETURNED AND LANDE D OK. PRESSURE LINE TO THE RIGHT AILERON ACTUATOR HAD BURST. LINE REPLACED. A/C SERVICEABLE. 2 L 7 2 4F 4 F RT A20EU E2EU 2000011500525 20000115 00525 SW 2000 1 15 CA991209020 1 19991119 A 3310 2719033073 LIGHTING PANEL SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP HARTZL HCB3T HCB3TN5 GL COCKPIT MELTED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 9873418 P03551C BV4226 (CAN) A DAMAGED LIGHT BULB IN THE PILOT'S LOWER SWITCH PANEL BACKLIGHTING CAUSED A SHORT WHICH MELTED PART OF THE PANEL RESULTING IN SOME SMOKE AND FUMES IN THE COCKPIT. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2000011500526 20000115 00526 WP 2000 1 15 CA991209021 2 19991125 A 7210 31011442 SUNGEAR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL REDUCTION G/B MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 9P42893 P54143 BV3970 (CAN) OIL ANALYSIS SHOWED TRACES OF ALUMINUM AND CARBON STEEL. RGB PLANETARY GEARS P/N 358268-1 SHOWED METAL DAMAGE. L OCKS P/N 866523-1 SHOWED ALUMINUM FRETTING FROM VIBRATION CAUSED FROM ABOVE PARTS RUNNING UNDER LOAD. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2000011500527 20000115 00527 EA 2000 1 15 CA991209024 1 19991117 A 5312 BULKHEAD CNDAIR CNDAIR CL215 CL2151A10 EA PWA R2800 R2800* 52026 NE HAMSTD 43E 43E60 NE BS 371 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2786 55397 N177731 (CAN) WATERBOMB SYSTEM UNLATCHING JACK, THE MOUNTING LUG HAD LOOSENED IN SERVICE CAUSING ELONGATION OF THE MOUNTING LUG BOLT HOLES. THE BULKHEAD THAT THE ACTUATOR IS ATTACHED WAS ALSO CRACKED BETWEEN THE HOLES. BOTH LT AND RT HAVE SAME D EFECTS. 2 H 7 2 4R 4 R A14EA 5E8 6 C P871 2000011500528 20000115 00528 EA 2000 1 15 CA991209025 1 19991115 A 5312 BULKHEAD CNDAIR CNDAIR CL215 CL2151A10 EA PWA R2800 R2800* 52026 NE HAMSTD 43E 43E60 NE BS 371 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3263 1122 N193564 (CAN) AFTER REMOVAL OF THE UNLATCHING JACK MOUNTING SPIGOT, THE BULKHEAD AT FS 371 WAS CRACKED. THE CRACKS RUN BETWEEN THE TWO MOUNTING HOLES. BOTH LT AND RT MOUNTING HOLES HAD CRACKS. 2 H 7 2 4R 4 R A14EA 5E8 6 C P871 2000011500529 20000115 00529 NM 2000 1 15 CA991209031 1 19990724 A 3246 31070 WHEEL BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE NLG DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 942999 695337 (CAN) RIGHT NOSE WHEEL INNER RIM DAMAGED AROUND ENTIRE CIRCUMFERENCE. WHEEL REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 2000011500530 20000115 00530 NM 2000 1 15 CA991209032 1 19990930 A 3230 651637113 TORSION LINK BOEING 727 72727C 138400J NM PWA JT8 JT8D7B 52053 NE NLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 653499 (CAN) LOWER NLG TORSION LINK HAS A CRACK AT CENTER PIVOT POINT LT LUG. TORSION LINK REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2000011500531 20000115 00531 NM 2000 1 15 CA991209033 1 19991020 A 3510 11442621 OXYGEN MASK BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE COCKPIT LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 533510264 695337 (CAN) S/O OXYGEN MASK LEAKING AROUND BASE OF MASK WHEN ON EMERGENCY. 2 L 7 3 4F 4 F RT A3WE E2EA 2000011500532 20000115 00532 NM 2000 1 15 CA991209034 1 19991021 A 3242 26011825 BRAKE BENDIX 26011825 BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE MLG FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 896 4279 688128 (CAN) BRAKES CAUSING A/C TO SHUDDER AT TAXI SPEEDS RT SIDE IS WORSE THAN LEFT SIDE ANTI-SKID ON OR OFF. NR 4 BRAKE REPL ACED. 2 L 7 3 4F 4 F RT A3WE E2EA 2000011500533 20000115 00533 NM 2000 1 15 CA991209035 1 19991027 A 2781 H1010262 SWITCH BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE LE FLAP FAILED W O OTHER N FALSE WARNING CR CRUISE 1 CA 297 688128 (CAN) NR 6 LE FLAP IN-TRANSIT LIGHT ON WITH UNIT RETRACTED. UNIT REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 2000011500534 20000115 00534 NM 2000 1 15 CA991209036 1 19991027 A 2751 2061131 INDICATOR BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE TE FLAP FAILED W O OTHER F FLT CONT AFFECTED CL CLIMB 1 CA 1626 4277 689961 (CAN) COULD NOT RETRACT INBOARD FLAPS PAST 2, USED ALTERNATE FLAPS TO RETRACT, CONTINUED FLIGHT AND AT LANDING USED NORM AL SYSTEM WITHOUT INCIDENT, ON GROUND CYCLED TWICE NORMALLY. REPLACED FLAP POSITION INDICATOR PER MM. 2 L 7 3 4F 4 F RT A3WE E2EA 2000011500535 20000115 00535 NM 2000 1 15 CA991209037 1 19991101 A 7120 65187228 FITTING BOEING BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 35678 P689955 (CAN) NR 3 FORWARD ENGINE SUPPORT FITTING CRACKED, REPLACED. REF 97-05-08. 2 L 7 3 4F 4 F RT A3WE E2EA 2000011500536 20000115 00536 NM 2000 1 15 CA991209038 1 19991106 A 3241 LINE BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE RT MLG MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA P689955 (CAN) ON ONE OCCASION BRAKE CHATTER APPEARS ON RT SIDE. FOUND TWO HYDRAULIC LINES CROSSED, REPAIRED. 2 L 7 3 4F 4 F RT A3WE E2EA 2000011500537 20000115 00537 2000 1 15 CA991209039 4 19991215 A 6122 B3124 CONTROL SHAFT HARTZL E52 PIPER PA46 PA46310P 7104605 SO HARTZL HCC2Y BHCC2YF1 GL PROP GOVERNOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5125SJ AM2747 (CAN) DURING INSPECTION NDT PROCESS REVEALED A CRACK IN THE CONTROL SHAFT. 1 L 7 1 3O RT A25SO 5 C P920 2000011500538 20000115 00538 EA 2000 1 15 CA991209046 1 19991113 A 2752 60093000116 ACTUATOR CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 5102 94469 350143 (CAN) OCCASIONALLY FLAPS FAILED IN COLD WEATHER. NR 3 ACTUATOR REPLACED AND PROBLEM WENT AWAY. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500539 20000115 00539 NE 2000 1 15 CA991209051 2 19991119 A 8520 12081 STUD PWA R985AN14B BEECH 18 E18S9700 1151008 CE PWA R985 R985AN14B 52008 NE HAMSTD 22D 22D30 NE NR 3 CYLINDER BROKEN W E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA 747 436714 436714 E2248 (CAN) NR 3 CYLINDER FLANGE STUDS BROKEN. 1 L 7 2 3R 3 R A765 5E1 5 C P736 2000011500540 20000115 00540 EU 2000 1 15 CA991209063 1 19991124 A 2610 D890 FIRE DETECTOR BRAERO 748 HS7482B 1500248 EU RROYCE DART DART5352 54509 NE ROTOL R4304 R2124304 EU NR 1 ENGINE FAILED W E F D ENGINE SHUTDOWN ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA 16249 DRG22868 (CAN) ON TAXI, NR 1 ENGINE FIRE WARNING ILLUMINATED. INVESTIGATION REVEALED FAILED FIRE WIRE AND FERRULE. PARTS REPLAC ED. 2 L 7 2 3T 4 T A24EU E297 6 C P899 2000011500541 20000115 00541 GL 2000 1 15 CA991209064 3 19991215 A 6114 57A2433 BOLT HARTZL BHCC2YF1BF PIPER PA46 PA46310P 7104605 SO HARTZL HCC2Y BHCC2YF1 GL PROP HUB WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 1350 AM2747 AM2747 (CAN) ONE BOGUS PART (HUB BOLT) FOUND. 1 L 7 1 3O RT A25SO 5 C P920 2000011500542 20000115 00542 NE 2000 1 15 CA991209067 2 19991110 A 7230 3040911 BLADE PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE HARTZL HCE4A HCE4A3I NE ENGINE BROKEN W E C ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 1698 PCEPR0093 PCEPR0093 HJ1053 (CAN) ENGINE CT BLADES HAD HEAVY CONTACT WITH SEGMENTS AND PILOT REPORTED HIGH ITT1000 DEGREES CELSIUS. 1 L 7 1 3T 4 T RT A78EU E26NE 5 C P10NE 2000011500543 20010307 00543 EU 2001 3 7 CA991209068 1 19991110 A 2434 60CR132903 BRUSH BLOCK PILATS 524321215 PILATS PC12 PC1245 EU PWA PT6 PT6A67B 52043 NE BRUSHES WORN W O OTHER J WARNING INDICATION CR CRUISE 1 CA 592 100032 PCEPR0050 (CAN) DURING CRUISE FLIGHT, THE CREW GOT A GEN 2 FAIL LIGHT. MAINTENANCE FOUND THE ALTERNATOR BRUSHES WORN TO THE POINT OF BRUSH FAILURE. 1 L 7 1 3T 4 T RT A78EU E26NE 2000011500544 20000115 00544 EU 2000 1 15 CA991209079 1 19991118 A 2750 5275012003 TE FLAP PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE WINGS CONTAMINATED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 576 239 PCEPR0095 (CAN) ON APPROACH, THE PILOT SELECTED FLAPS AND THE COMPUTER SENSED A FAULT. A FLAPLESS LANDING WAS CARRIED OUT. THE SUBMITTER BELIEVES THAT A SMALL AMOUNT OF WATER, EVIDENT ON THE LEFT UPPER FLAP SKIN, HAD FROZEN AND CAUSED THE FLAP TO STICK IN THE RETRACTED POSITION. 1 L 7 1 3T 4 T RT A78EU E26NE 2000011500545 20000115 00545 EA 2000 1 15 CA991209083 1 19991129 A 2435 MS245105 CIRCUIT BREAKER DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL COCKPIT INTERMITTENT W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA PCE41110 BU8184 (CAN) START FAILURES RESOLVED WITH 5 AMP GENERATOR. RESET CIRCUIT BREAKER SHOWING AN INTERMITTENT OPEN CIRCUIT CONDITIO N. REPLACED. 1 H 7 2 3T 4 T RT A9EA E4EA 6 C P15EA 2000011500546 20000115 00546 EU 2000 1 15 CA991209084 1 19991107 A 2752 951D10011 ACTUATOR 5275012003 PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE TE FLAP SEIZED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 135 239 PCEPR0095 (CAN) AFTER FLYING 3 HOURS AT HIGH ALTITUDE WITH AN OAT OF MINUS 45 DEGREES CELSIUS, THE CREW SELECTED FLAPS ON APPROAC H AND GOT A FLAPS FAIL CAUTION LIGHT. MAINTENANCE GOT AN E13 ERROR FROM THE COMPUTER. MAINTENANCE REMOVED ALL THE FLAP ACTUATORS AND AFTER COLD SOAKING THEM IN A FREEZER FOR TWO HOURS, FOUND THE LEFT INBOARD ACTUATOR SEIZED. IT REQUIRED OVER 100 POUNDS/INCHES OF TORQUE TO ROTATE THE DRIVE PINION. THE OTHER ACTUATORS ONLY REQUIRED 2 POUNDS/INCHES OF TORQU E TO ROTATE. 1 L 7 1 3T 4 T RT A78EU E26NE 2000011500547 20000115 00547 EU 2000 1 15 CA991209085 1 19991202 A 2752 951D10011 ACTUATOR PILATS PC12 PC12 7090550 EU PWA PT6 PT6A67B 52043 NE TE FLAP MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA 104 1073A PCEPR0141 (CAN) WHILE PERFORMING A SCHEDULED CHECK ON THE FLAP ACTUATOR BACKLASH, THE ACTUATOR WAS FOUND BEYOND SERVICE LIMITS. AC TUATOR REPLACED WITH OVERHAULED UNIT. 1 L 7 1 3T 4 T RT A78EU E26NE 2000011500548 20000115 00548 SO 2000 1 15 CA991209087 1 19990907 A 3260 MS272402 SWITCH EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA HARTZL HCB3T HCB3TN3 GL NLG OUT OF ADJUST W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA PCE56688GG BU11331 (CAN) AFTER TAKEOFF WHEN GEAR SELECTED UP, CREW DIDN'T GET NOSE GEAR UP INDICATION THAT THE NOSE GEAR HAD MOVED. GEAR CYCLED WITH NO INDICATION. RETURNED HANDL E TO DOWN POSITION WITH 3 GREEN LIGHTS. NOSE GEAR CENTERING ACCUMULATOR WAS BELOW MINIMUM PRESSURE AND NOSE STEERING MICROSWITCH WAS OUT OF ADJUSTMENT. 1 L 7 2 4T 4 T A21SO E4EA 6 C P15EA 2000011500549 20000115 00549 WP 2000 1 15 CA991209089 2 19991101 A 7250 30720141 BLADE GARRTT TFE7312 AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE7312 01518 WP TURBINE SECTION MISSING W E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 10539 P73114C P73114C (CAN) ENGINE AT OVERHAUL FACILITY, REPORT TO FOLLOW. 2 L 7 2 4F 4 F A33EU E6WE 2000011500550 20000115 00550 EA 2000 1 15 CA991209091 2 19991122 A 7414 K5277 ROTOR SLICK 4761 ZLIN 242 Z242L 9970204 EU LYC O360 AEIO360A1B6 41514 EA MAGNETO BROKEN W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 494 99021040 L2662451A (CAN) EXCESSIVE MAG DROP WAS EXIBITED AND COULD NOT BE TIMED. ONE-HALF OF THE CAM/ROTOR GEAR ATTACH POINT WAS BROKEN AT ROTOR SHAFT. THIS AREA IS TO BE CHECKED AT SB 2-80C (500 HR INSP). 1 L 7 1 3O 3 O 0 A76EU 1E10 2000011500551 20000115 00551 EA 2000 1 15 CA991209092 1 19991204 A 2610 70017M00000 CONNECTOR 600572891 CNDAIR CL600 CL600* EA LYC ALF502 ALF502L2 41580 NE NR 1 ENGINE WORN W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) ON CLIMB-OUT, NR 1 ENGINE FIRE FAULT FLICKERING. A/C LEVELED AND NR 1 ENGINE FIRE FAULT ON STEADY. ON APPROACH, FIRE BELL AND FIRE WARNING CAME ON. ENGINE SECURED AND A/C LANDED WITHOUT INCIDENT. ENGINE AFT FIRE WIRE CONNECTOR FOUND WORN. REPLACED. 2 L 7 2 4F 4 F RT A21EA E6NE 2000011500552 20000115 00552 CE 2000 1 15 CA991209093 1 19990406 A 2510 AN2450A CLEVIS BOLT CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA SNSNCH 72C 72CK EA PILOTS SEAT FAILED W O OTHER O OTHER CR CRUISE 1 CA (CAN) BOLTS FOUND CRACKED AFTER AIRCRAFT DESTROYED IN ACCIDENT. 1 H 7 1 3O 3 O NT 3A19 E223 5 N P9045 2000011500553 20000115 00553 EU 2000 1 15 CA991210002 1 19991022 A 5347 SHACKLE SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A2 41560 NE CARGO LOAD FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA LE43021E (CAN) WHILE TESTING A SKISMIC BIRD, THE PILOT FELT THE LOAD RELEASE FROM THE AIRCRAFT. THE CARGO HOOK WAS FUNCTIONALLY TESTED BEFORE AND AFTER THE FLIGHT AND FOUND TO OPERATE CORRECTLY. SUBMITTER STATED INDICATIONS APPEAR THAT THE CUSTOM ER SUPPLIED SLING SHACKLE MAY NOT HAVE BEEN PROPERLY LOCKED. 1 G 7 1 3U 3 U H9EU E5NE 2000011500554 20000115 00554 NE 2000 1 15 CA991210003 1 19990501 A 2140 7650007901103 BLOWER JANITROL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL HEATER FAILED W O OTHER O OTHER CR CRUISE 1 CA 2 110950 CAE890138S (CAN) DURING FLIGHT, THE PILOT TURNED ON HEAT-VENT BLOWER AND REPORTED HEARING AN UNUSUAL HIGH PITCHED WHINE AND UNUSUAL SMELL AND THEN SHUT OFF THE UNIT. MAINTENANCE PERSONNEL COULD NOT DUPLICATE THE NOISE, BUT DID SMELL AN ODOR. UNIT W AS REPLACED AND CARBON WAS FOUND IN THE UNIT FROM THE BRUSHES WHICH WERE WORN TO HALF-LIFE. 1 G 7 2 3U 3 U H1NE E1GL 2000011500555 20000115 00555 SO 2000 1 15 CA991210014 1 19991105 A 3710 SHAFT AIRBORNE 441CC7 PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA HARTZL HCE3Y HCE3YR2 GL VACUUM PUMP SHEARED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 924 086040 L586361A DJ11486A (CAN) NO VACUUM WARNING LIGHT CAME ON DURING CRUISE FOR LT SIDE AND STAYED ON. PILOT REPORTED IN LOG AT ARRIVAL. FOUND PUMP DRIVE SHEARED AT UNUSUAL POINT. PUMP SEIZED. OVERHAUL INSTALLED AUG 15/98 AT 1116.7 AFTT. REMOVED AT 12090.7 A FTT. PART T.B.O. IS 1000 HRS. PART T.S.O. IS 924.0 HRS. SUBMITTER SUSPECTS CAUSE TO BE POOR COOLING DESIGN, THEREFO RE, INEFFICIENT HEAT REMOVAL. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 2000011500556 20000115 00556 SO 2000 1 15 CA991210015 1 19991111 A 3222 31811000 COLLAR 31767000 PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA HARTZL HCE2Y HCE2YR2 GL NLG BROKEN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 7066 L372748 BP8496 (CAN) DAMAGE CAUSED BY OVERSTEERING BY PILOT WHEN TOWING AIRCRAFT TO HANGAR WITH TRACTOR. REPLACED COLLARS (P/N 31811- 000; P/N 1781-000) AND HARDWARE. LINKS (SCISSORS) INSPECTED AS WELL AS THE INTERCONNECTING STEERING MECHANISM. 1 L 7 2 3O 3 O 1A10 1E4 5 C P9EA 2000011500557 20000115 00557 SO 2000 1 15 CA991210016 1 19991117 A 3411 3021603 PITOT TUBE PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA HARTZL HCE2Y HCE2YR2 GL LT WING FROZEN W O OTHER O OTHER CR CRUISE 1 CA 7072 L372748 BP8496 (CAN) THE PRE-TAKEOFF RUN UP AND TAKEOFF WAS DURING WET SLUSHY RUNWAY CONDITIONS DURING SNOW. AFTER CLIMB IN CRUISE, T HE A.S.I. WAS LOST. THE PILOT HAD PUT PITOT HEAT ON AT TAKEOFF, NOT DURING RUN UPS AND TAXIING. AIRSPEED CAME ON DURIN G DESCENT TO SEPT-ISLES. ON RETURN FLIGHT, A.S.I. JUMPED TO 250 MPH AND BACK TO 150 MPH, BUT REMAINED OK FOR THE REST OF THE TRIP. MAINTENANCE DISCONNECTED THE LINE TO THE A.S.I. AND FOUND WATER DROPLETS INSIDE. SUBMITTER STATED THE PI TOT TUBE IS LOW ON THIS AIRCRAFT, THEREFORE, SHOULD HAVE HEAT ON RIGHT FROM START. 1 L 7 2 3O 3 O 1A10 1E4 5 C P9EA 2000011500558 20000115 00558 SO 2000 1 15 CA991210017 1 19991118 A 2140 1933105 BRACKET JANITROL PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA HARTZL HCE2Y HCE2YR2 GL HEATER CABLE BROKEN W O OTHER M OVER TEMP CR CRUISE 1 CA 367 1492251 L372748 BP8496 (CAN) HEATER OVERHEAT SWITCH POPPED. INVESTIGATION FOUND PILOT HAD PULLED HEATER DOOR OPEN, BUT THE CABLE WAS STIFF AND THE CABLE BRACKET BROKEN. THE RESULT WAS THE HANDLE TOOK OUT THE PLAY GIVING THE IMPRESSION THE DOOR WAS OPEN. THE SU BMITTER REMARKED THAT THERE IS NO BRACKET SHOWING IN THE I.P.C. 1 L 7 2 3O 3 O 1A10 1E4 5 C P9EA 2000011500563 20000115 00563 NM 2000 1 15 CA991210024 1 19991122 A 3230 FRF6327PW08 CONNECTOR BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E437 54555 NE NLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 30680 (CAN) DURING ROUTINE INSPECTION, HARNESS BRACKET ALD393 AND CONNECTOR D40488P FOUND CONTAMINATED WITH WATER ON 25 PERCEN T OF THE CONNECTOR AREA. CAUSED WIRES TO BECOME BRITTLE AT CRIMPED AREA. ALSO, THE BACKSHELL OF THE CONNECTOR WAS SE IZED DUE TO CORROSION. CONNECTOR PLUG, BACKSHELL, AND RECEPTACLE PLUG REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 2000011500564 20010307 00564 NM 2001 3 7 CA991210025 1 19991203 A 2910 312N510146 LINE VICKERS 3508807 BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE HYD SYSTEM LOOSE W H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE LH HYD QTY DECREASED TO ZERO QTY PRESSURE LIGHT ON AND SYS DEACTIVATED. FOUND PRESSURE LINE JUST BEF ORE FILTER MODULE AND BRACKET BROKEN. LINE TIGHTENED. PUMP SEIZED AND REPLACED. UNDER INVESTIGATION. PMUP WENT DRY AND T HEN FAILED, UNIT FROZE DUE TO METAL CONTAMINATION, DAMAGED PACKINGS AND BACKUP SEALS. 2 L 7 2 4F 4 F RT A2NM E12EU 2000011500566 20000115 00566 EA 2000 1 15 CA991210027 1 19991112 A 3320 T96W2B28LELE LIGHT CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343B1 NE CABIN OVERHEATED W K NONE L NO TEST IN INSP/MAINT 1 CA 389 (CAN) WHILE PERFORMING INTERIOR WORK,THE ACCENT LIGHTS AROUND THE CABIN FLOOR LEVEL HAD SOME OVERHEAT SPOTS ON THE PLAST IC TUBES ESPECIALLY THE LONGEST ASSY. BOMBARDIER NOTIFIED AND SYSTEM DISABLED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500567 20000115 00567 EA 2000 1 15 CA991210028 1 19991023 A 5730 SKIN GE CF343A1 CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT WING LIGHTNING STRIKE W K NONE O OTHER IN INSP/MAINT 1 CA 807389 807389 (CAN) LIGHTNING STRIKE ON LEFT SIDE OF FUSLAGE. FOUND LEFT ICE DETECTOR TRAILING EDGE DAMAGE AND EVERY 9-10 INCHES RIVE T HEAD BURNT ALL THE WAY BACK TO LEFT WING. BURNS WITHIN LIMITS EXCEPT UNDER WINSHIELD. RIVETS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500568 20010307 00568 EA 2001 3 7 CA991210029 1 19991026 A 2751 INDICATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAP FAIL MESSAGE WHEN SELECTING FLAPS FROM 35 TO 45 DEG. SYSTEM RESET. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500569 20000115 00569 NM 2000 1 15 CA991210034 1 19991028 A 2460 D414 CONNECTOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE LT GENERATOR CHAFED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA P707553 (CAN) DURING TAKEOFF, LT GENERATOR FAILED FOLLOWED BY BUS TRIP. NO INSTRUMENT ON CAPTAIN'SED 3 INCHES FROM CONNECTOR D 414. REPAIRED SYS SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 2000011500570 20000115 00570 EA 2000 1 15 CA991210037 1 19991030 A 2120 PIN CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE VENT DOOR SHEARED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 807195 (CAN) ON CLIMB-OUT, UNABLE TO PRESSURIZE AIRCRAFT. PASSENGER DOOR FLAPPER DOOR OPENED WITH SHEAR PINS ON VENT DOOR SHEA RED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500571 20000115 00571 EA 2000 1 15 CA991210038 1 19991101 A 2760 4916405 ECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE SPOILER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807211 (CAN) DURING CRUISE , CAUTION MESSAGE FLIGHT SPOILER AND SPOILERONS. NR 2 SECU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500572 20000115 00572 EA 2000 1 15 CA991210041 1 19991102 A 2750 TE FLAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WING FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807380 (CAN) FLAPS FAIL AT 38 DEGREES ON APPROACH. SYSTEM RESET. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500573 20000115 00573 EA 2000 1 15 CA991210042 1 19991103 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807380 (CAN) FLAPS FAIL AT 40 DEGREES DURING TAXI. LEFT NR 5 FLEX SHAFT CLEANED AND LUBED AND LT BPSU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500574 20000115 00574 EA 2000 1 15 CA991210043 1 19991104 A 3040 MNP16591 CONTROLLER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WINDSHIELD FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807335 (CAN) LEFT WINDSHIELD HEAT MESSAGE WITH BURNING SMELL IN COCKPIT. WINDSHIELD TEMPERATURE CONTROLLER REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500575 20000115 00575 EA 2000 1 15 CA991210044 1 19991107 A 2750 MPN865D1007 DRIVE UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807267 (CAN) FLAP FAIL AT ZERO. ZERO FLAP LANDING CARRIED OUT. FLPA PDU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500576 20000115 00576 EA 2000 1 15 CA991210045 1 19991117 A 2750 TE FLAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WING FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807267 (CAN) FLAP FAIL MESSAGE ON APPROACH. SYSTEM RESET. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500577 20000115 00577 EA 2000 1 15 CA991210046 1 19991117 A 2750 TE FLAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WING FAULTY W O OTHER O OTHER AP APPROACH 1 CA 807267 (CAN) FLAP FAIL ON APPROACH. RESET CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500578 20000115 00578 EA 2000 1 15 CA991210047 1 19991117 A 2752 853D1009 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER O OTHER AP APPROACH 1 CA 807267 (CAN) FLAPS FAIL ON APPROACH. NR 1AND NR 2 LT ACTUATORS, NR'S1, 3, 4 FLEX SHAFTS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500579 20000115 00579 EA 2000 1 15 CA991210048 1 19991108 A 3260 PSEU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE MLG FAILED W A UNSCHED LANDING N FALSE WARNING IN INSP/MAINT 1 CA 807399 (CAN) AFTER TAKEOFF, MLG INDICATED UNSAFE AFTER GEAR UP SELECTION. PROX IMITY TARGET ADJUSTED AND PSU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500580 20000115 00580 EA 2000 1 15 CA991210049 1 19991108 A 5210 H341433 HANDLE CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR WORN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 807365 (CAN) AFTER TAKEOFF, EXPERIENCED A BANG TYPE NOISE AND PASSENGER DOOR MESSAGE. EXCESSIVE WEAR ON PASSENGER DOOR HANDLE. HANDLE REPLACED AND PRESSURE CHECK CARRIED OUT. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500581 20000115 00581 EA 2000 1 15 CA991210050 1 19991117 A 5210 LATCH CAM CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807365 (CAN) UNABLE TO OPEN PASSENGER DOOR ON ARRIVAL. DOOR LATCH MECHANISM CAM AND HOUSING RELOCATED, DOOR RIGGING CARRIED O UT AND DOOR SEAL CHANGED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500582 20000115 00582 EA 2000 1 15 CA991210051 1 19991111 A 2750 855D1007 SENSING UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807267 (CAN) FLAP FAILED AT 8 DEGREES ON APPROACH. BPSU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500583 20000115 00583 EA 2000 1 15 CA991210052 1 19991118 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER O OTHER AP APPROACH 1 CA 807385 (CAN) FLAPS FAIL ON APPROACH AT 8 DEGREES. RT BPSU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500584 20000115 00584 EA 2000 1 15 CA991210053 1 19991120 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE SPOILER FAILED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 807373 (CAN) ON DESCENT, FLIGHT SPOILERS DEPLOYED, IMMEDIATE SHARP BANK TO THE RIGHT. SPOILERS RETRACTED. NR 2 SPOILER ECU RE PLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000011500585 20000115 00585 WP 2000 1 15 CA991210061 1 19991122 A 2131 MPN2075301AA CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESSURE FAILED W O OTHER O OTHER DE DESCENT 1 CA P653454D (CAN) ON DESCENT AT 8,000 FEET, CABIN PRESSURE AUTO FAIL LIGHT CAME ON AND CABIN WAS CLIMBING AT 2,000 FEET PER MINUTE. REPLACED NR 2 CABIN PRESSURE CONTROLLER. 2 L 7 2 4F 4 F A6WE E2EA 2000011500586 20000115 00586 WP 2000 1 15 CA991210062 1 19991124 A 2133 2075401AA OUTFLOW VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESSURE INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA P653454D (CAN) CABIN AUTO PRESSURIZATION SYSTEM INOPERATIVE. REPLACED OUTFLOW VALVE. 2 L 7 2 4F 4 F A6WE E2EA 2000011500587 20000115 00587 WP 2000 1 15 CA991210063 1 19991122 A 2120 DUCT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE WATER SEPARATOR FAILED W O OTHER O OTHER CR CRUISE 1 CA P657261D (CAN) CREW REPORTED LACK OF OXYGEN AND DIZZEYNESS. LT WATER SEPARATOR AFT DUCT REPLACED. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 2000011500588 20000115 00588 GL 2000 1 15 CA991210090 2 19991110 A 7323 8613M25 ACTUATOR CAMAIR 480 480 1890102 SO ALLSN 250C 250C20 03013 GL TURBINE GOVERNOR FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 95110012 CAE845007 (CAN) ON TAKEOFF, THE NR, N2 DECREASED AND WOULD NOT RESPOND TO BEEP INPUT. 1 L 7 2 3O 3 U 2A2 E4CE 2000011500589 20000115 00589 SW 2000 1 15 CA991210091 1 19991112 A 2910 124044E0234C200 HOSE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA HYD SYSTEM RUPTURED W O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 CA CPPS60495 (CAN) BRAIDED HYDRAULIC HOSE (PRESSURE) LOCATED FORWARD BULKHEAD OF TRANSMISSION COMPARTMENT FOUND TO BE RUBBING ON THE AIRFRAME AND RUPTURED ON START-UP. 1 G 7 1 4U 4 U H4SW E22EA 2000011500642 20000115 00642 CE 2000 1 15 2000ZZZX114 1 19991126 A 2910 2307006101 LINE LEAR 23 23LEAR 5170102 CE NLG LEAKING A KKFA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 49CK 23009 AIRCRAFT LOST HYDRAULIC PRESSURE. UNEVENTFUL LANDING EXECUTED. REPLACED LEAKING NOSE GEAR RETRACT LINE. REPLACED BOTH ENGINE DRIVEN HYDRAULIC PUMPS AS A PRECAUTIONARY MEASURE. REPLACED HYDRAULIC SYSTEM FILTERS. SERVICED EMERGENCY AIR B OTTLE. C/W RETRACTION CHECKS. RAN ENGINES, BLED SYSTEM AND LEAKED CHECKED. ALL WORK ACCOMPLISHED IAW LEARJET MODEL 23 SM. 1 L 7 2 4J A5CE 2000011500645 20000115 00645 2000 1 15 WVBA01699 4 19991222 A 2200 065501100 SWITCH KA132 PIPER PA31 PA31350 7103110 SO AFCS FAILED A WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 4082T 1104 X3489 318152089 PILOT REPORTED AUTOPILOT WOULD DIS-ENGAGE IN FLIGHT AND WOULD NOT RE-ENGAGE. SYSTEM WAS CHECKED ON GROUND PER A/C P.O.H. ACCELEROMETER SWITCH WOULD NOT TEST IN THE UP POSITION AND WAS INTERMITTENT IN THE DOWN POSITION. SWITCH WAS REMOVED FROM SERVICE. (X) 1 L 7 2 3O A20SO 2000011500648 20000115 00648 NE 2000 1 15 2000ZZZX119 2 19991227 A 7321 301037290 P2 LINE 0164248800 SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE FCU FAILED A A HCMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 13 194BH 2827 C952B 2903 9402 DURING FLIGHT, PILOT EXPERIENCED LOW MAIN ROTOR SPEED CONDITION WITH AURAL WARNING. PILOT THEN LOWERED COLLECTIVE CONTRO L AND MAINTAINED OPERATING SPEED OF ROTOR SYSTEM. AT THAT TIME, HE ELECTED TO TAKE GOVERNOR OUT OF THE AUTO POSITION AN D INTO MANUAL OVERRIDE. HE WAS THEN ABLE TO MAINTAIN OPERATING SPEED OF THE ROTOR SYS AND FLEW BACK TO BASE. EMERGENCY LANDING DECLARED, ACFT LANDED WITH SLIGHT FORWARD RUN WITH NO DAMAGE OR INJURIES. EXAM OF ENGINE FOUND BROKEN P2 PIPE AND WAS REPLACED. POSSIBLE CAUSE UNKNOWN AND INCREASED INSP TO PREVENT RECURRENCE. 1 G 7 1 3U 3 U H9EU E19EU 2000011500650 20000115 00650 CE 2000 1 15 2000ZZZX121 1 19991214 A 3260 1SE1 SWITCH CESSNA 402 402B 207590P CE MLG FAILED A OZCA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 901BC 402B0379 REF: FLIGHT LOG PG 1341. LEFT GEAR LIGHT DID NOT SHOW DOWN AND LOCK AND WOULD NOT RETRACT EITHER. TROUBLESHOT SYSTEM AND FOUND DIRTY CONTACT ON LEFT GEAR DOWNLOCK MICROSWITCH. CLEANED MICROSWITCH, RETRACTED GEAR SEVERAL TIMES, AND CHECK ED EMERGENCY MANUAL EXTENSION. ALL SYSTEMS FOUND TO BE WORKING CORRECTLY PER CE MM, SECTION 4-1. 1 L 7 2 3O A7CE 2000011500667 20000115 00667 CE 2000 1 15 2000ZZZX138 1 19991214 A 3710 442CW12 PUMP BEECH 58 58 1152740 CE VACUUM SYSTEM FAILED A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 38CL 191 84718 TH829 VACUUM/PRESSURE PUMP FAILED AFTER 191.0 HOURS (OVERHAULED PUMP). 1 L 7 2 3O 3A16 2000011500708 20000115 00708 WP 2000 1 15 ABXA000002 1 19991215 A 3350 6012231 POWER PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 820AX 46155 EMERGENCY LIGHTS WOULD NOT COME ON WHEN ELECTRICAL POWER WAS LOST. REPLACED EMERGENCY LIGHT PACK ASSY. OPS CHECKED GOO D. 2 L 7 4 4F 4A25 2000011500711 20000115 00711 WP 2000 1 15 TWAA0000504 1 19991206 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 1155 - 1174 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE BETWEEN STA 1155 TO 1174 RT SIDE, 58 IN RBL. REMOVED SURFACE COROSION ON MEMBRANE STA 1155 TO 1174, RT SIDE, PER SPM 6-80-01, PAGE 1, AND SRM 51-10-03. PRIMED INST FASTENERS PER SRM 53-30- 0 PAGE 1 THAT WERE REMOVED IN REMOVING FIBERGLAS ANGLE. 2 L 7 2 4F RT A6WE 2000011500712 20000115 00712 WP 2000 1 15 TWAA0000505 1 19991206 A 4900 DEFLECTOR DOUG DC9 DC983 3022083 WP APU CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND CORROSION IN 3 EA PLACES AROUND APU WATER DEFLECTOR, STA 1338. REMOVED CORROSION AS REQUIRE D PER TWA SPM 6-80-01. TREATED AND PRIMED PER SRM 51-10-3, PAGE 16 AND 17. REMOVED AND REINSTALLED WATER DEFLECTOR PER SPM 6-70-01, PAGE 4B. 2 L 7 2 4F RT A6WE 2000011500713 20000115 00713 WP 2000 1 15 TWAA0000507 1 19991203 A 2520 SUPPORT DOUG DC9 DC983 3022083 WP BS 1257 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND CORROSION ON SIDEWALL SUPPORT 25L, STA 1257. REMOVED SUPPORT AND REMOVED CORROSION PER SPM 6-80-01. TREATED AND PAINTED PER SRM 51-10-03, PARA 21. INSTALLED SUPPORT WITH SAME TYPE FASTENERES REMOVED PER SRM 51 -30-2. 2 L 7 2 4F RT A6WE 2000011500714 20000115 00714 WP 2000 1 15 TWAA0000508 1 19991208 A 5320 DOOR SILL DOUG DC9 DC983 3022083 WP BS 1155 - 1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND CORROSION ON INSIDE OF LOWER DOOR SILL AREA, AFT CARGO BIN, FROM STA 1155 TO 1212, RT SIDE. MAPPED MATERIAL THICKNESS AND FOUND MATERIAL REMOVED 0.042 IN, 0.294 ORIGINAL THICKNESS. REPLACED INSIDE OF LOWER SILL AREA STA 1155 TO 1212 IN ACCORDANCE WITH SRM 53-05, PAGE 174, FIG 63 SHEET 2. 2 L 7 2 4F RT A6WE 2000011500715 20000115 00715 WP 2000 1 15 TWAA0000509 1 19991215 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 439 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 939AS 49657 DURING CHECK-C MAINT, FOUND CORROSION AND PILLOWING AT STA 439, LONGERON 18L MEMBRANE. REMOVED CORRODED SECTIONS OF MEM BRANE PER SPM 6-80-01, PAGE 1. REPAIRED PER SRM 53-01, PAGE 18. 2 L 7 2 4F RT A6WE 2000011500716 20000115 00716 WP 2000 1 15 TWAA0000510 1 19991215 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 1102 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 939AS 49657 DURING CHECK-C MAINT, FOUND CORROSION AT STA 1102R, LONGERON 18. CORRECTED PER SRM 53-01. TREATED AND PAINTED PER 51-1 0-B. 2 L 7 2 4F RT A6WE 2000011500717 20000115 00717 WP 2000 1 15 TWAA0000511 1 19991215 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 57 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 939AS 49657 DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT STA 57R, LONGERON 18. CORROSION REMOVED PER SRM 53-01. INSTALLED DOUBLER PER 53-01. 2 L 7 2 4F RT A6WE 2000011500718 20000115 00718 WP 2000 1 15 TWAA0000512 1 19991217 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 1031 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 939AS 49657 DURING CHECK-C MAINT, FOUND CORROSION AT STA 1031R, LONGERON 18. REMOVED CORROSION PER SRM 6-80-01. INSTALLED DOUBLER PER SRM 53-01, FIG 4. 2 L 7 2 4F RT A6WE 2000011500719 20000115 00719 WP 2000 1 15 TWAA0000513 1 19991220 A 5320 FLOOR PAN DOUG DC9 DC983 3022083 WP BS 1107 - 1149 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 939AS 49657 DURING CHECK-C MAINT, FOUND CORROSION AT MEMBRANE FLOOR PAN ALONG LONGERON 18L, FROM STA 1107 THROUGH 1149. REMOVED LIG HT AND MODERATE CORROSION ON THE LT FLOOR MEMBRANE, LONGERON 18L FROM STA 1107 TO 1149 PER SPM 6-80-01, PAGE 1-3. REPAI RED AREA STA 1118 TO 1123 PER SRM 53- 01, FIG 4 SHEET 3 PAGE 18. TREATED AREA FROM STA 1107 TO 1149 LONGERON 18L FLOOR MEMBRANE PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 2000011500720 20000115 00720 WP 2000 1 15 TWAA0000514 1 19991215 A 5320 FLOOR PAN DOUG DC9 DC932 3022066 WP BS 218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION AT CABIN FLOOR PAN STA 218, LONGERON 18R. REMOVED AND REPLACED FLOOR PA N PER SPM 6-70-01, PART A AND B. 2 L 7 2 4F A6WE 2000011500721 20000115 00721 WP 2000 1 15 TWAA0000506 1 19991206 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 636 - 655 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE BETWEEN STA 636 TO 655, 58 IN LRL ON LT SIDE. REPAIRED DAMAGED AREA P ER SRM 53-01, FIG 4 PAGE 18. 2 L 7 2 4F RT A6WE 2000011500722 20000115 00722 WP 2000 1 15 TWAA0000515 1 19991215 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND STA 200, RBL 0 TO 57 IN, WITH CORROSION ON CABIN FLOOR ATTACH ANGLE. REMOVED AND REPLAC ED FLOOR ATTACH ANGLE PER SPM 6-70-01, PART A AND B. 2 L 7 2 4F A6WE 2000011500725 20000115 00725 WP 2000 1 15 TWAA0000503 1 19991203 A 5320 SILL DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 912TW 49183 DURING CHECK-C MAINT, THE LOWER FRAME AT THE AFT CARGO DOOR SILL HAD CORROSION GROUND BEYOND LIMITS. REPLACED THE FRAME PER SPM 6-70-01, PAGE 1. 2 L 7 2 4F A6WE 2000011500726 20000115 00726 NM 2000 1 15 RAAA00B2001 1 19991231 A 3350 8621014 BATTERY INTVLV BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FWD EXIT IDENTIFIER WON'T TEST. REPLACED BATTERY PACK OPS OK. 2 L 7 3 4F A3WE 2000011500736 20000115 00736 EU 2000 1 15 QXEA0992713 1 19991226 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11233 SEA - EMERGENCY LIGHTS IN NR 1 EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT CIRCUIT BOARD. OPERATI ONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000011500737 20000115 00737 EU 2000 1 15 QXEA9902734 1 19991230 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 20075 CASTELLATION IS CRACKED AT STRINGER 38. REPAIRED IAW HORIZON AIR EA 4-53-956 AND FOKKER SRM 53-10-05, PAGE 601A. 2 L 7 2 4F RT A20EU 2000011500756 20000115 00756 WP 2000 1 15 AT0000010 1 19991126 A 5320 INTERCOASTAL DOUG DC9 DC932 3022066 WP BS 917 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 DURING A ROUTINE INSPECTION AT AVBORNE IN MIAMI FL, FOUND INTERCOASTAL CORRODED AT BS 917 RIGHT FUSELAGE FRAME. FABRICA TED AND INSTALLED NEW INTERCOASTAL AT BS 917 RIGHT FUSELAGE FRAME IAW DC9 SRM 51-00. 2 L 7 2 4F A6WE 2000011500757 20000115 00757 WP 2000 1 15 AT0000011 1 19991119 A 3520 PSU DOUG DC9 DC932 3022066 WP CABIN FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 810AT 47277 WHILE ACCOMPLISHING WORK ORDER 55311, SEVERAL PSU OXYGEN DOORS DID NOT DEPLOY WHEN SYSTEM WAS ACTIVATED. SEVERAL OXYGEN MASKS WERE FOUND UNSERVICEABLE. REPAIRED OR REPLACED THE AFFECTED PSU'S AND REPLACED ALL UNSERVICEABLE MASKS IAW EO 9- 3520-29-E1461 REV A. 2 L 7 2 4F A6WE 2000011500770 20000115 00770 EA 2000 1 15 COMA0060032 1 19990107 A 5320 601R3111358 ANGLE CNDAIR CL600 CL6002B19 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 13640 7042 O/B FLOORBEAM CLIP IS CRACKED AT FS 280 RBL9. REMOVED CRACKED ANGLE AND REPLACED WITH NEW ANGLE IAW WVAC EO 601R-53-078 6.. 2 L 7 2 4F RT A21EA 2000011500779 20000115 00779 EU 2000 1 15 00FDEA00009 1 19991222 A 2781 SWITCH AIRBUS 300 A300F4605R 3930327 EU LE FLAP OUT OF ADJUST A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 679FE 793 00-9 - IN FLT, AFT SLAT RETRACTION SPD LIMIT ZIPPER DID NOT GO AWAY AS IT SHOULD HAVE. RECYCLED SLATS, NO HELP. FOUND VMO/MMO SWITCH IN FWD AVIONICS COMP. IN THE ALT POS. REPOSITIONED SWITCH TO NORM POS. CKS NORMAL. 2 L 7 2 4F RT A35EU 2000012100001 20000121 00001 NM 2000 1 21 AWXA9900443 1 19991203 A 3397 13131122 WIRE AIRBUS A319 A319132 3930340 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 808AW 1088 EMERGENCY LIGHT AT 10 DEF INOP. REPAIRED WIRING OPS CK GOOD. 2 L 7 2 4F RT A28NM 2000012100006 20000121 00006 WP 2000 1 21 DLL14992515 1 19991115 A 7800 RB211 LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE #2 ENGINE PUNCTURED/CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 014716 FOUND ON SERVICE CHECK 13, NR 2 ENGINE BLOCKER DOORS AT 1:00 AND 3:00 POSTION DAMAGED. ACTUATING RODS FOR BLOCKER DOORS CAUSED A 3 INCH HOLE IN THE ENGINE EXHAUST NOZZLE AT 1:00 POSITION, AND A 4-5 IN CRACK AT THE 3:00 POSITION. WILL REQU IRE ENGINE CHANGE/EXHAUST SLEEVE REPLACEMENT. REPLACED NR 2 ENGINE. OP CKS GOOD. 2 L 7 3 4F 4 F A23WE E12EU 2000012100007 20000121 00007 NM 2000 1 21 DL757992518 1 19991115 A 2400 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE #1 ENGINE WIRES BURNT A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 608DA 22815 726710 ON TO ROLL AT APPROXIMATELY 30 KIAS LEFT ENG GEN FAILED. ABORTED T/O AND RETURN TO GATE. FOUND PHASE B WIRE CHAFED IN PYLON. REPAIRED SAME. 2 L 7 2 4F 4 F RT A2NM E17NE 2000012100008 20000121 00008 NE 2000 1 21 DL72L992526 2 19991115 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE #1 ENGINE UNRESPONSIVE A DALA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 27 508DA 50108 21310 700726 NR 1 ENG THROTTLE DID NOT RESPOND TO CONTROL. RECONNECTED THROTTLE ROD LINKAGE, RAN ENG PER PFHB. OP CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 2000012100010 20000121 00010 EU 2000 1 21 C2XA99IA561 1 19991024 A 5320 S52176404206 SIDE PANEL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOR STEP STRUCTURE FORWARD SIDE PANEL WAS FOUND TO BE CRACKED. MAINTENAN CE PERFORMED A DOUBLER REPAIR ON THE AFFECTED PANEL IAW ATR42-320 SRM 52-11-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000012100012 20000121 00012 EA 2000 1 21 COMA9960774 1 19991216 A 2752 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAP BINDING A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 984CA 186 2 7171 FLAPS FAIL MESSAGE DURING APPROACH. REPLACED LEFT I/B FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 2000012100013 20000121 00013 NM 2000 1 21 DLM90992757 1 19991214 A 5414 PANEL 2900003539 DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE SEPARATED A DALA O OTHER D INFLIGHT SEPARATION DE DESCENT 1 SO 27 911DA DL010 53391 020016 ON ARRIVAL DFW FOUND NR 2 ENGINE C-DUCT ACCESS PANEL BLOWOUT DOOR MISSING. UPPER C-DUCT COWL DAMAGED BY DOOR. REPLACED UPPER REVERSER HALF AND RIGGED PER MM 78-32-00. REPLACED AND ADJUSTED BLOWOUT DOOR. 2 L 7 2 4F 4 F RT A6WE E40NE 2000012100014 20000121 00014 EU 2000 1 21 CA991209061 1 19991124 A 2430 AZS5 CIRCUIT BREAKER ZLIN 242 Z242L 9970204 EU LYC O360 AEIO360A1B6 41514 EA COCKPIT FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 2992 L2640851A (CAN) AS PART OF AN INSP OF AIRCRAFT, WIRING AND PROTECTIVE DEVICES, FOUND THAT 3 CCT BREAKER SWITCHES FAILED TO PERFOR M INTENDED FUNCTION. BREAKER SWITCHES WERE TESTED FROM 2 TO 5 TIMES- RATED CURRENT (10-25 AMPS) AND WOULD NOT OPEN AT ALL. EACH SWITCH WAS ALLOWED TO RUN AT 2 TIMES- RATING FOR A PERIOD OF 5 MINUTES. SWITCHES APPEAR TO BE NON-MIL SPEC; HOWEVER, THE REMAINING 11 BREAKER SWITCHES (VARIOUS CURRENT RATINGS) PERFORMED INTENDED FUNCTION. ALL BREAKER SWITCHES ARE TO BE REPLACED BY MS24509-B-X MIL SPEC CIRCUIT BREAKER SWITCHES. NOTE: NORMALLY CCT BREAKERS AND SWITCHES ARE ON CONDITION AND ARE NOT TESTED UNDER CIRCUMSTANCES AS PART OF NORMAL MAINT PRACTICES. 1 L 7 1 3O 3 O 0 A76EU 1E10 2000012100015 20000121 00015 WP 2000 1 21 AT9900894 1 19991219 A 3350 L2245 LIGHT DOUG DC9 DC932 3022066 WP BS 669 INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 803AT 47261 DURING SERVICE CHECK, LEFT AFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT AT BS 669 WAS INOPERATIVE. TIGHTENED NUT ON GRO UND TERMINAL OF LIGHT FIXTURE L2-245 AT BS 669 IAW DC9 MM 33-53. 2 L 7 2 4F A6WE 2000012100016 20000121 00016 SO 2000 1 21 SIMA993171 1 19991103 A 2133 D38999926FA98SN CONNECTOR EMB 145 EMB145LR SO OUTFLOW VALVE FAILED A SIMA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 626AE 145117 DFW - FLT 3681 - AFTER CLIMBING THROUGH 21,000 FT, CABIN DIFFERENTIAL PRESS WARNING LIGHT ILLUMINATED. CABIN PRESS REAC HED 15,000 FT AND THE CABIN 02 MASKS DEPLOYED. UNABLE TO CONTROL CABIN PRESS IN AUTO OR MANUAL. CREW FOLLOWED ALL CHEC KLISTS, THE PACK 1 CLOSED IND CAME ON DURING DESCENT, BUT WORKED NORM AFTER THE APU WAS STARTED. A/C RETURNED TO DFW. F OUND BAD CANNON PLUG (P0079) ON THE REAR BULKHEAD OUTFLOW VALVE. REMOVED AND REPLACED CANNON PLUG. ALSO, REPAIRED SOME LEAKAGE AT THE CAPTAINS DV WINDOW AND BAGGAGE DOOR FRAME SEAL. AS A PRECAUTIONARY MEASURE, THE DIGITAL PRESSURE CONTRO LLER WAS ALSO REPLACED PER THE ADVICE OF THE EMBRAER TECHNICAL REPRESENTATIVE. DISCHARGED OXYGEN GENERATORS WERE ALSO 2 L 7 2 4T RT T00011AT 2000012100017 20000121 00017 NM 2000 1 21 USAA991237 1 19991108 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 31191 23984 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED F RAME REPAIR PER EA 66032. (M) 2 L 7 2 4F RT A16WE 2000012200001 20000122 00001 NE 2000 1 22 2000ZZZX139 2 19990909 A 7497 3038221 WIRE DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE IGNITER CHAFED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1930 90000012 PCE206018 UNITS EXCESSIVELY CHAFED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 2000012200002 20000122 00002 NM 2000 1 22 2000ZZZX140 1 19990412 A 6230 900C2010183107 LINK DOUG MD900 MD900 3027375 NM MAIN ROTOR LOOSE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 226 198541 90000012 LINK HAD EXCESSIVE PLAY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2000012200003 20000122 00003 NM 2000 1 22 2000ZZZX141 1 19991204 A 7933 900D3658007101 THERMAL VALVE DOUG MD900 MD900 3027375 NM OIL COOLER FLUCTUATED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 154 257 90000012 OIL TEMP FLUCTUATION TO VALVE (NOT SEATING). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2000012200004 20000122 00004 NM 2000 1 22 2000ZZZX142 1 19990726 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 551 0206040546 90000012 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2000012200005 20000122 00005 NM 2000 1 22 2000ZZZX143 1 19990728 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 867 0206040622 90000012 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2000012200006 20000122 00006 NM 2000 1 22 2000ZZZX144 1 19990830 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 654 0206040530 90000012 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2000012200007 20000122 00007 EU 2000 1 22 2000ZZZX145 1 19991204 A 6330 L633M2001105 MOUNT UROCOP EC135 EC135P1 8680990 EU TRANSMISSION LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 224 WI266 EC1350054 MOUNT LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2000012200008 20000122 00008 EU 2000 1 22 2000ZZZX146 1 19991204 A 6330 L633M2001106 MOUNT UROCOP EC135 EC135P1 8680990 EU TRANSMISSION LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 135SJ 79 WI302 EC1350054 MOUNT LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2000012200009 20000122 00009 NE 2000 1 22 2000ZZZX147 2 19991012 A 7412 304393701 EXCITER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 752 9752308 EC1350054 PCEBB0049 EXCITER OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2000012200010 20000122 00010 NE 2000 1 22 2000ZZZX148 2 19990925 A 7421 312088001 IGNITER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 713 EC1350054 PCE550045 IGNITER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2000012200011 20000122 00011 NE 2000 1 22 2000ZZZX149 2 19990928 A 7421 312088001 IGNITER UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 720 EC1350054 PCEBB0049 IGNITER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2000012200012 20000122 00012 EU 2000 1 22 2000ZZZX150 1 19991020 A 7332 312263701 SWITCH UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 771 AM0061 EC1350054 PCEBB0045 SWITCH INOPERATIVE. OIL FILTER CAUTION LIGHT ILLUMINATED AND REMAINED ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 2000012200013 20000122 00013 NM 2000 1 22 2000ZZZX151 1 19990728 A 6210 900R3100001101 BOLT DOUG MD900 MD900 3027375 NM M/R BLADE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 378 0098841468 90000012 NOT SEIZED ON SHAFT THREADS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 2000012200014 20000122 00014 WP 2000 1 22 GTIA9901213 1 19991201 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - FLT 880 - AFT EMERGENCY EXIT (OVER WING) SIGNS (UPPER) WILL NOT LIGHT LEFT AND RIGHT. REPLACED BATTERIES IN EMERG ENCY POWER PACK AT BS-25. OPS CHECK GOOD. REF: MD 80 MM 33-53-00. (X) 2 L 7 2 4F A6WE 2000012200015 20000122 00015 NM 2000 1 22 AALA991619 1 19991022 A 3520 CABLE BOEING 737 737823 13844BZ NM CABIN PSU MISRIGGED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 907AN 29509 ORD - FLT 1025 - DURING PRE-FLIGHT, OXYGEN MASKS WERE INADVERTENTLY DEPLOYED BY FLIGHT CREW. OXYGEN CANISTER WAS NOT RI GGED PROPERLY. PROPERLY RIGGED CABLES TO OXYGEN CANISTER AT SEAT 20 DEF AND RESTOWED ALL OTHE MASKS. SYSTEM GROUND CHE CKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A16WE 2000012200016 20000122 00016 SO 2000 1 22 C2XA99BT094 1 19991008 A 3350 1317 BULB EMB 145 EMB145 SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13969 145141 BTV - FL 3944 - MAINTENANCE FOUND DURING 2A INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPL ACED LAMP. OPS CHECKED, SYSTEM GOOD. (X) 2 L 7 2 4F RT T00011AT 2000012200017 20000122 00017 SO 2000 1 22 C2XA99IA555 1 19991018 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR SO CABIN INOPERABLE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13975 145163 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE FOWARD EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REM OVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-01, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 2000012200018 20000122 00018 GL 2000 1 22 2000ZZZX152 2 19991109 A 7240 6870992 COMBUSTION CASE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE CRACKED A CYXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 206AW 10418 387 2861 CAE830502 PILOTS REPORTED LOW POWER AND HIGH TOT. TROUBLESHOOTING FOUND A LARGE CRACK IN THE ARM PIT AREA WHERE IT IS REINFORCED WITH A BRAZED ON SCREEN, RIGHT SIDE. PART REMOVED AND SENT IN FOR POSSIBLE REPAIR. POSSIBLE CAUSE, METAL FATIGUE. 1 G 7 1 3U 3 U H2SW E4CE 2000012200019 20000122 00019 GL 2000 1 22 2000ZZZX153 2 19991116 A 7230 CAC44186 NR 2 BEARING BELL 407 407 SW ALLSN 250C 250C47B GL COMPRESSOR MAKING METAL A CYXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 407LG 456 53143 CAE847161 ENGINE CHIP LIGHT CAME ON. CHIP PLUGS INSPECTED AND FOUND EXCESSIVE METAL PARTICLES ON BOTH PLUGS. ENGINE REMOVED AND SENT IN FOR REPAIR. CAUSE UNKNOWN AT THIS TIME. 1 G 7 1 3U 3 U O H2SW E1GL 2000012200020 20000122 00020 SW 2000 1 22 2000ZZZX154 1 19991115 A 2842 407375016101 SIGNAL CONDITION BELL 407 407 SW FUEL SYSTEM MALFUNCTIONED A CYXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 01 407LG 531 53143 PILOTS REPORTED AN INTERMITTENT PROBLEM WITH THE RIGHT FUEL TRANSFER CAUTION LIGHT COMING ON AND THE FUEL QUANTITY GAUGE GOING BLANK. SUBMITTER STATED PROBLEM WAS IN P/N 407-375-016-101 SIGNAL CONDITIONER. DEFECT CAUSE UNKNOWN. 1 G 7 1 3U O H2SW 2000012200021 20000122 00021 SW 2000 1 22 2000ZZZX155 1 19991109 A 6230 406040036107 BEARING BELL 407 407 SW M/R MAST MAKING METAL A CYXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 01 407LG 462 53143 PILOTS REPORTED MAIN ROTOR TRANSMISSION CHIP LIGHT CAME ON. CHIP PLUGS INSPECTED AND FOUND METAL PARTICLES ON UPPER CHI P DETECTOR. HELICOPTER FLOWN AGAIN AND AFTER A FEW HOURS, THE LIGHT CAME ON AGAIN. CHIP PLUGS INSPECTED AND FOUND MET AL ON UPPER PLUG. MAST ASSY REPLACED. CAUSE FAULTY BEARING. 1 G 7 1 3U O H2SW 2000012200022 20000122 00022 WP 2000 1 22 EIAA990273 1 19990819 A 5320 DOUBLER DOUG DC9 DC933F 302207A WP BS 718 DEBONDED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - DURING C-CHECK, A FINGER DOUBLER, LOCATED BELOW WINDOW BELT AT STA 718 RIGHT, WAS FOUND DEBONDED. REMOVED DAMAGED DOUBLER AND INSTALLED NEW FABRICATED REPAIR DOUBLER PER SRM 51-30-2. (X) 2 L 7 2 4F A6WE 2000012200023 20000122 00023 NM 2000 1 22 F3LA99124 1 19991002 A 3350 20121 BATTERY CHARGER BOEING 737 7373L9 1384470 NM BS 975 FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 310FL 20 3399 26440 DEN - DURING SERVICE CHECK, INSPECTION REPORTED THE RT WING LOWER AFT WING-TO-BODY EMERGENCY EXIT LIGHT INOPERATIVE. MA INTENANCE REPLACED BATTERY CHARGER AT BS 975R (M1157) AND SYSTEM CHECKED OKAY. CYCLES: 10. (X) 2 L 7 2 4F RT A16WE 2000012200024 20000122 00024 NM 2000 1 22 F3LA99122 1 19990923 A 3244 0397812 TIRE BOEING 737 7373L9 1384470 NM NR 4 MAIN FAILED A F3LA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 NM 03 312FL 638 7232P00153R4 24569 DEN - UPON ARRIVAL IN BOS, FLIGHT CREW REPORTED NR 4 MAIN TIRE RECAP MISSING. TIRE REMAINED INFLATED. MAINTENANCE IN B OS REPLACED NR 4 MAIN TIRE AND WHEEL ASSY AND PERFORMED TEMPORARY REPAIRS NECESSARY TO FERRY AIRCRAFT TO DEN. UPON ARRI VAL IN DEN, MAINTENANCE REPLACED THE NR 3 MAIN TIRE AND WHEEL ASSY AS A PRECAUTION; REPLACED THE RT INBOARD FORE FLAP, M ID-FLAP AND AFT FLAP ASSEMBLIES; REMOVED THE RT LOWER MAIN LANDING GEAR DOOR AND INSTALLED PLACARD PER CDL 32-10-4; AND REPAIRED RT WING PANEL NR 8501 PER EA 57-737-026. INSPECTED DENT ON THE LEADING EDGE OF THE RT HORIZONTAL STABILIZER. C YCLES: 277. (X) 2 L 7 2 4F RT A16WE 2000012200025 20000122 00025 CE 2000 1 22 2000ZZZX156 1 19991016 A 3320 903640829 BALLAST BEECH 90 F90 1152909 CE CABIN FAILED A FUKA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 03 44882 LA102 DURING FLIGHT, THE PASSENGER IN THE LEFT AFT SEAT NOTED SMOKE COMING FROM BEHIND THE WINDOW SHADE. THE CREW SECURED THE LIGHTING SYSTEM BY SECURING THE CIRCUIT BREAKER. THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION, THE LIGHT BAL LAST WAS FOUND MELTED. THE BALLAST WAS REPLACED AND THE SYSTEM CHECKED GOOD. INSPECTION OF ALL AIRCRAFT IN THE FLEET F OUND NO FURTHER PROBLEMS. (X) 1 L 7 2 4T A31CE 2000012200026 20000122 00026 WP 2000 1 22 GTIA9901170 1 19991025 A 3350 60030431 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY EXIT DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 13405 48087 DTW - LIGHTS OVER EMERGENCY OVERWING EXITS DO NOT ILLUMINATE WHEN EMERGENCY LIGHTS SWITCH IS PLACED TO ON. REMOVED AND REPLACED BATTERIES IN BATTERY PACK B5-33 AND B5-25. REMOVED AND REPLACED BATTERY PACK ASSY B5-33. OPS CHECK GOOD ON RA MP AT THIS TIME IAW MM 33-50-0. (X) 2 L 7 2 4F A6WE 2000012200027 20000122 00027 WP 2000 1 22 GTIA9901171 1 19991023 A 3350 60030431 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 803NK 9987 48087 DTW - OVERWING EMERGENCY EXIT SIGNS AFT POSITION, BOTH LEFT AND RIGHT, WILL NOT LIGHT. REMOVED AND REPLACED BATTERY PAC K AT POSITION B5-25. OPS CHECK GOOD PER 33-53-00. (X) 2 L 7 2 4F A6WE 2000012200028 20000122 00028 2000 1 22 2000ZZZX157 4 19991101 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LEFT MALFUNCTIONED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 179GL 1381 UE179 CAPTAIN'S ALTIMETER HAS INTERMITTENT INVALID ENCODER IN-FLIGHT. REMOVED AND REPLACED ALTIMETER. SUBSEQUENT BENCH TEST VERIFIED THAT ENCODER WAS INTERMITTENTLY INOPERABLE. P/N KEA-346/066-0362-0008. (X) 2 L 7 2 4T RT A24CE 2000012200029 20000122 00029 2000 1 22 2000ZZZX158 4 19991029 A 3416 ALIMETER BEECH 1900 1900D 1154162 CE LEFT MALFUNCTIONED A GLBA K NONE O OTHER CR CRUISE 1 CE 01 151UX 2958 UE151 CAPTAIN'S ALTIMETER REPORTED AS INOPERATIVE IN-FLIGHT. REMOVED AND REPLACED ALTIMETER. SUBSEQUENT BENCH TEST RESULTED IN 'NO FAULT FOUND'. P/N KEA-346/066-0362-0008. 2 L 7 2 4T RT A24CE 2000012200030 20000122 00030 2000 1 22 2000ZZZX159 4 19991008 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT FAILED A GLBA O OTHER J WARNING INDICATION DE DESCENT 1 CE 01 195GL 254 4526 UE195 CAPTAIN'S ALTIMETER FLAGGED DURING DESCENT. REMOVED AND REPLACED ALTIMETER. SYSTEM TESTS SATISFACTORY. SUBSEQUENT BEN CH TESTS WERE UNABLE TO CONFIRM PROBLEM. THIS WAS THE THIRD SUCH FAILURE OF THIS INSTRUMENT IN THE PAST 9 MONTHS (714 H OURS) OF OPERATION. P/N KEA-346/066-03062-0008. 2 L 7 2 4T RT A24CE 2000012200031 20000122 00031 2000 1 22 2000ZZZX160 4 19991026 A 3422 DIRECTIONAL GYRO COLLINS BEECH 1900 1900D 1154162 CE LEFT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 228GL 1 4006 UE228 CAPTAIN'S RMI FLAGS AND CARD DO NOT TURN. (CAPTAIN'S DG FROZE). REMOVED AND REPLACED NR 1DGS-65. P/N DGS-65/622-6136- 002. 2 L 7 2 4T RT A24CE 2000012200032 20000122 00032 2000 1 22 2000ZZZX161 4 19991019 A 3422 DIRECTIONAL GYRO COLLINS BEECH 1900 1900D 1154162 CE LEFT INOPERABLE A GLBA K NONE O OTHER CR CRUISE 1 CE 01 228GL 7 950 UE228 CAPTAIN'S DIRECTIONAL GYRO INOPERABLE. REMOVED AND REPLACED NR 1 DGS-65 GYRO. P/N DGS-65/622-6136-002. (X) 2 L 7 2 4T RT A24CE 2000012200033 20000122 00033 2000 1 22 2000ZZZX162 4 19991013 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT FAILED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 240GL 2513 4592 UE240 CAPTAIN'S ALTIMETER FLAGGED IMMEDIATELY FOLLOWING TAKEOFF. THE SCHEDULED FLIGHT WAS ABORTED AND AIRCRAFT RETURNED TO TH E STATION. UPON LANDING, ALTIMETER BEGAN TO FUNCTION. THE ALTIMETER WAS REMOVED AND REPLACED. P/N KEA-346/066-03062-0 0. 2 L 7 2 4T RT A24CE 2000012200034 20000122 00034 NM 2000 1 22 GAIA99194 1 19991123 A 5711 SPAR BOEING 727 727287 1384020 NM WS 464-491 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT WING BETWEEN WS 464 AND WS 491 BELOW NR 11 SPOILER LOWER AFT SPAR CHORD CRACK. INSTALLED REPAIR BETWEEN RIGHT WS 464 AND WS 491 BELOW NR 11 SPOILER AT THE LOWER AFT SPAR CHORD. REPAIR ACCOMPLISHED IAW BOEING TELEX KHC-MIA-99-0002H, 8110-3 DATED OCTOBER 15, 1999 ISSUED. REF: N/R 3106 AND 3031. (X) 2 L 7 3 4F RT A3WE 2000012200035 20000122 00035 NM 2000 1 22 GAIA99195 1 19991123 A 5347 SEAT TRACK BOEING 727 727287 1384020 NM BS 960-1080 WORN A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 SEAT TRACK AT BS 1080 APPROXIMATELY LBL 45 LOCKING HOLES WORN. REPLACED SECTION OF CABIN SEAT TRACK FROM BS 960 TO BS 1 80, LBL 45. REPAIRED IAW SRM 53-10-5 FIG 7. REF: N/R 5326. (X) 2 L 7 3 4F RT A3WE 2000012200036 20000122 00036 NM 2000 1 22 GAIA99196 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 COCKPIT EXTERIOR, NR 1 WINDOW CUT OUT HAS CRACK AT OUTBOARD UPPER CORNER. VERIFIED BY NDT. INSTALLED DOUBLER REPAIR AT COCKPIT EXTERIOR, NR 1 WINDOW CUT-OUT OUTBOARD UPPER CORNER. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 8. REF: N/R 372 5. (X) 2 L 7 3 4F RT A3WE 2000012200037 20000122 00037 NM 2000 1 22 GAIA99208 1 19991123 A 3230 TRUNNION BOEING 727 727287 1384020 NM RT MLG CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTINGS INSIDE FACES ARE CORRODED. ACCOMPLISHED REPAIR TO LEFT AND RI GHT LANDING GEAR FORWARD TRUNNION REAR SPAR ATTACH FITTINGS IAW BOEING TELEX PSS-MIA-99-00007H. 8110-3 DATED 9/3/99 ISS UED. REF: N/R'S 7428, 7431, 7434, AND 7435. (X) 2 L 7 3 4F RT A3WE 2000012200038 20000122 00038 NM 2000 1 22 GAIA99207 1 19991123 A 5280 HINGE BOEING 727 727287 1384020 NM RT MLG LOOSE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT MAIN LANDING GEAR WING DOOR HAS PLAY AT THE FORWARD HINGE. ACCOMPLISHED REPAIR, RIGHT MAIN LANDING GEAR DOOR FRON T SPAR HINGE CLEVIS IAW BOEING TELEX PSS-MIA-99-00005H. 8110-3 DATED 8-3-99 ISSUED. REF: N/R 7344. (X) 2 L 7 3 4F RT A3WE 2000012200039 20000122 00039 NM 2000 1 22 GAIA99193 1 19991123 A 5751 SKIN BOEING 727 727287 1384020 NM AILERON DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT, OUTBOARD AILERON LOWER SKIN DENTED AT TWO LOCATIONS. INSTALLED DOUBLER REPAIR AT RIGHT OUTBOARD AILERON LOWER SKI N. REPAIR ACCOMPLISHED IAW SRM 57-50-5 FIG 1. REF: N/R 3121. (X) 2 L 7 3 4F RT A3WE 2000012200040 20000122 00040 NM 2000 1 22 GAIA99192 1 19991123 A 5313 STRINGER BOEING 727 727287 1384020 NM BS 351-360 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 E/E COMPARTMENT, RIGHT SIDE. CORROSION AT STR 25R BETWEEN STA 351 - STA 360, FORWARD APH POWER SUPPLY. INSTALLED STRI NGER REPAIR BETWEEN STA 351 AND STA 360 AT STR 25 RIGHT. REPAIR ACCOMPLISHED IAW SRM 53-10-3 FIG 1. REF: N/R 3947. ( X) 2 L 7 3 4F RT A3WE 2000012200041 20000122 00041 NM 2000 1 22 GAIA99191 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 1015-1025 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 10 INCH HOLE IN RIGHT SIDE FUSELAGE, STA 1015 TO STA 1025, STR 26 RIGHT. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR FROM S TA 1015 TO STA 1025, STR 26 RIGHT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. REF: N/R 3036. (X) 2 L 7 3 4F RT A3WE 2000012200042 20000122 00042 NM 2000 1 22 GAIA99190 1 19991123 A 5313 STRINGER BOEING 727 727287 1384020 NM BS 1020 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 AFT CARGO, STR 26 RIGHT DAMAGED, STA 1020. INSTALLED REPAIR AT AFT CARGO COMPARTMENT STR 26 RT, STA 1020. REPAIR ACCOM PLISHED IAW SRM 53-10-3 FIG 1. REF: N/R 3038. (X) 2 L 7 3 4F RT A3WE 2000012200043 20000122 00043 NM 2000 1 22 GAIA99189 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 203.8 - 228.8 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 DEEP SCRATCH AND DENT ON BODY SKIN LOCATED BETWEEN BS 203.8 AND BS 228.8, STR 19 LT AND 24 LT, 13 INCH BOTTOM LT. INSTA LLED FUSELAGE SKIN REPAIR BETWEEN BS 203.8 AND BS 228.8 BETWEEN STR 19 LT AND STR 24 LT. REPAIR ACCOMPLISHED IAW SRM 53 -30-3 FIG 15A. REF: N/R 3052. (X) 2 L 7 3 4F RT A3WE 2000012200044 20000122 00044 NM 2000 1 22 GAIA99188 1 19991123 A 5347 SEAT TRACK BOEING 727 727287 1384020 NM BS 910-930 MECHANICAL DAMAG A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 SEAT TRACK RBL 45.5 BETWEEN BS 910 AND BS 930. THREE LOCKING HOLES UPPER SURFACE WITH TOOL MARKINGS. REPLACED SECTION OF CABIN SEAT TRACK BETWEEN BS 870 AND BS 950, RBL 45.5. REPAIR ACCOMPLISHED IAW SRM 53-10-5 FIG 7. REF: N/R 3305. ( X) 2 L 7 3 4F RT A3WE 2000012200045 20000122 00045 NM 2000 1 22 GAIA99187 1 19991123 A 5512 SKIN BOEING 727 727287 1384020 NM HORIZONTAL STAB DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 LEFT HORIZONTAL STABILIZER L/E HAS SKIN DENT, APPROXIMATELY 15 INCHES FROM INBOARD END. INSTALLED DOUBLER REPAIR AT LEF T HORIZONTAL STABILIZER LEADING EDGE. REPAIR ACCOMPLISHED IAW SRM 55-10-3 FIG 1. REF: N/R 4315. (X) 2 L 7 3 4F RT A3WE 2000012200046 20000122 00046 NM 2000 1 22 GAIA99186 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 387 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 FUSELAGE LEFT SIDE EXTERIOR SKIN HAS TEMPORARILY FILLED DENT, STA 387, STR 18 LT. INSTALLED DOUBLER REPAIR AT FUSELAGE LEFT SIDE EXTERIOR SKIN STA 387, STR 18 LT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. REF: N/R 3347. (X) 2 L 7 3 4F RT A3WE 2000012200047 20000122 00047 NM 2000 1 22 GAIA99185 1 19991123 A 5311 FRAME BOEING 727 727287 1384020 NM BS 930 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 FS 930 LOWER FRAME IS CRACKED AT STR 14 LT. VERIFIED BY NDT INSPECTION. INSTALLED REPAIR AT FS 930, LOWER FRAME AT STR 14 LT. REPAIR ACCOMPLISHED IAW SRM 53-10-4 FIG 1. REF: N/R 5095. (X) 2 L 7 3 4F RT A3WE 2000012200048 20000122 00048 NM 2000 1 22 GAIA99184 1 19991123 A 5713 STRINGER BOEING 727 727287 1384020 NM WS 656.5 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT UPPER STR 10 CRACKED AT RIB STA 656.5. INSTALLED ANGLE REPAIR AT RIGHT WING UPPER STR 10 AT RIB STA 656.5. REPAI R ACCOMPLISHED IAW SB 727-57-0159. REF: N/R 2449. (X) 2 L 7 3 4F RT A3WE 2000012200049 20000122 00049 NM 2000 1 22 GAIA99183 1 19991123 A 5311 FRAME BOEING 727 727287 1384020 NM BS 312 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 CABIN CIRCUMFERENTIAL TRACK AT BS 312 BELOW STR 13. INSTALLED REPAIR AT BS 312 BELOW STR 13 RIGHT CABIN CIRCUMFERENTIAL . REPAIR WAS ACCOMPLISHED IAW SRM 53-10-4 DETAIL 1. REF: N/R 3921. (X) 2 L 7 3 4F RT A3WE 2000012200050 20000122 00050 NM 2000 1 22 GAIA99182 1 19991123 A 5315 FLOOR BEAM BOEING 727 727287 1384020 NM BS 400 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 CABIN FLOOR BEAM BS 400 FROM LBL 12 TO RBL 24 EVIDENCE OF CORROSION AT UPPER SECTION. INSTALLED CABIN FLOOR BEAM REPAIR AT BS 400, FROM LBL 12 TO RBL 64. REPAIR ACCOMPLISHED IAW SRM 53-10-8 PAGE 21. REF: N/R 3933. (X) 2 L 7 3 4F RT A3WE 2000012200051 20000122 00051 NM 2000 1 22 GAIA99181 1 19991123 A 5754 RIB BOEING 727 727287 1384020 NM LE FLAP CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 NR 2 L/E SLAT INBOARD TRACK OUTBOARD MOUNT RIB IS CRACKED AT UPPER FLANGE BEINDING RADIUS APPROXIMATELY 1.50 INCHES AFT FROM SLAT FRONT SPARE. INSTALLED REPAIR AT THE NR 2 LEADING EDGE SLAT INBOARD TRACK OUTBOARD MOUNT RIB UPPER FLANGE. R EPAIR ACCOMPLISHED IAW SRM 57-50-3 FIG 9. REF: N/R 1864. (X) 2 L 7 3 4F RT A3WE 2000012200052 20000122 00052 NM 2000 1 22 GAIA99180 1 19991123 A 5315 FLOOR BEAM BOEING 727 727287 1384020 NM BS 1070 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 FLOOR BEAM AT BS 1070 ACCESS THROUGH AFT BAGGAGE COMPARTMENT. UPPER FLANGE LOWER SECTION AT APPROXIMATELY LBL 70.5 HAS EVIDENCE OF CORROSION. REPLACED SECTION OF FLOOR BEAM FROM BLR 39 TO BLR 70.5 AT BS 1070. REPAIR ACCOMPLISHED IAW SRM 53-10-8 FIG 3. REF: N/R 5251. (X) 2 L 7 3 4F RT A3WE 2000012200053 20000122 00053 NM 2000 1 22 GAIA99175 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 380-400 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 FUSELAGE SKIN DENTED LOCATED BETWEEN BS 380 AND BS 400 JUST BELOW STR 19R. INSTALLED FUSELAGE SKIN DOUBLER REPAIR BETWE EN BS 380 AND BS 400 JUST BELOW STR 19R. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. REF: N/R 3582. (X) 2 L 7 3 4F RT A3WE 2000012200054 20000122 00054 NM 2000 1 22 GAIA99174 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 1070 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 916PG 21690 CHECKED INTEGRITY OF FLUSH REPAIR PREVIOUSLY MADE AT BS 1070 STR 24R AND STR 25R. INSTALLED FLUSH REPAIR AT BS 1070 BET WEEN STR 25R AND STR 24R. REPAIRED ACCOMPLISHED IAW SRM 53-30-3 FIG 2. REF: AIRBOURNE N/R 3586. (X) 2 L 7 3 4F RT A3WE 2000012200055 20000122 00055 NM 2000 1 22 GAIA99197 1 19991123 A 5210 TORQUE BOX BOEING 727 727287 1384020 NM PASSENGER DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 MAIN ENTRY DOOR AFT FRAME CORNER TORQUE BOX EIVDENCE OF CRACK AT LOWER AFT CORNER. REPLACED SECTION OF WEB AT MAIN DOOR LOWER AFT FRAME CORNER TORQUE BOX. REPAIR ACCOMPLISHED IAW SRM 51-40-2, FIG 1. REF: N/R 3924. (X) 2 L 7 3 4F RT A3WE 2000012200056 20000122 00056 NM 2000 1 22 GAIA99198 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 1342 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 DENT AT BS 1342 AFT SKIN JUST BELOW STR 15 RIGHT. INSTALLED DOUBLER REPAIR AT BS 1342 AFT SKIN JUST BELOW STR 14 RIGHT . REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 2. REF: N/R 3572. (X) 2 L 7 3 4F RT A3WE 2000012200057 20000122 00057 NM 2000 1 22 GAIA99199 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 1342 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 SEVERAL DENTS PUSHED OUT OF SKIN AT BS 1342 AFT SKIN PANEL BETWEEN STR 16R AND STR 26R. INSTALLED DOUBLER REPAIR AT BS 1342 AFT SKIN PANEL BETWEEN STR 16 AND STR 26 RIGHT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 2. REF: N/R 3573. (X) 2 L 7 3 4F RT A3WE 2000012200058 20000122 00058 NM 2000 1 22 GAIA99200 1 19991123 A 5712 RIB BOEING 727 727287 1384020 NM WS 686.5 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT WING DAMAGED AT RIB LOWER FLANGE STA 686.5 AND STR 6. REPLACED FLANGE AT LOWER RIGHT WING RIB, STA 686.5, STR 6 I AW SRM 51-30-2. REF: N/R 2448. (X) 2 L 7 3 4F RT A3WE 2000012200059 20000122 00059 NM 2000 1 22 GAIA99201 1 19991123 A 3340 HOUSING BOEING 727 727287 1384020 NM LIGHT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 LEFT WING TIP LOGO LIGHT HOUSING CRACK ON INBOARD SIDE. ACCOMPLISHED LEFT WING TIP LOGO LIGHT HOUSING CRACK REPAIR IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM,049R0-1 REV 1R. 8110-3 DATED 7-20-99 ISSUED. REF: N/R 1879. (X) 2 L 7 3 4F RT A3WE 2000012200060 20000122 00060 NM 2000 1 22 GAIA99202 1 19991123 A 5720 TUBE BOEING 727 727287 1384020 NM WS 601.5 CHAFED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 LEFT WING NR 1 TANK, VENT TUBE IS CHAFED ON LOWER SIDE. LOCATED ON TOP OF WING RIB AT WS 601.50. ACCOMPLISHED LEFT WIN G VENT LINE CHAFING REPAIR AT STA 601.5 IAW WITH AVITAS ENGINEERING REPAIR ORDER 99AVHM.052R0-1 RIV IR. 8110-3 DATED 7-2 2-99 ISSUED. REF: N/R 1852. (X) 2 L 7 3 4F RT A3WE 2000012200061 20000122 00061 NM 2000 1 22 GAIA99203 1 19991123 A 5753 BUSHING BOEING 727 727287 1384020 NM TE FLAP DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 LEFT OUTBOARD FLAP OUTBOARD MECHANISM FOR AFT FLAG SEGMENT DRUM SUPPORT QUADRANT BUSHING HOLES ELONGATED. ACCOMPLISHED LEFT OUTBOARD MIDFLAP DRUM SUPPORT BUSHING REPAIR IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM.084R0-1 REV IR. 8110-3 DATE D 9-26-99 ISSUED. REF: N/R 1879. (X) 2 L 7 3 4F RT A3WE 2000012200062 20000122 00062 NM 2000 1 22 GAIA99204 1 19991123 A 5754 LUG BOEING 727 727287 1384020 NM LE FLAP WORN A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 NR 2 L/E FLAP INBOARD BULLNOSE BEARING LUG WORN TOO LARGE FOR BEARING INSTALLATION AND LUG CORRODED AND PITTED. ACCOMPL IHSHED NR 2 LEADING EDGE FLAP BULLNOSE REPAIR IAW BOEING TELEX KHC-MIA-99-00003H, DATED 9-7-99. 8110-3 DATED 9-14-99 IS SUED. REF: N/R 1886. (X) 2 L 7 3 4F RT A3WE 2000012200063 20000122 00063 NM 2000 1 22 GAIA99205 1 19991123 A 5730 SKIN BOEING 727 727287 1384020 NM RT WING GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT WING L/E UPPER SURFACE EXTERIOR SKIN HAS OLD GOUGE (PAINTED) OVER NR 6 L/E SLAT INBOARD TRACK. INSTALLED DOUBLER REPAIR AT RIGHT WING LEADING EDGE UPPER SURFACE EXTERIOR SKIN. REPAIR ACCOMPLISHED IAW SRM 57-30-4 FIG 4. REF: N/R 23 64 AND 2365. (X) 2 L 7 3 4F RT A3WE 2000012200064 20000122 00064 NM 2000 1 22 GAIA99206 1 19991123 A 5314 KEEL BEAM BOEING 727 727287 1384020 NM BS 870 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 RIGHT WW BS 870.00 RBL ZERO KEEL BEAM AREA DENTED AND CRACKED. ACCOMPLISHED KEEL BEAM CHORD REPAIR AT STA 870 IAW AVITA S ENGINEERING REPAIR ORDER 99AVH.086R0-1, REV IR. 8110-3 DATED 10-21-99 ISSUED. REF: N/R 3071. (X) 2 L 7 3 4F RT A3WE 2000012200065 20000122 00065 SO 2000 1 22 2000ZZZX163 2 19990818 A 7314 6395082 FUEL PUMP PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360E 17025 SO LT ENGINE BROKEN A JIBA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NE 03 797MT 808 347870433 307645 AIRCRAFT WAS EN ROUTE FROM OWA TO HTO, CRUISE AT 4,500 MSL. EXPERIENCED ENGINE AND FUEL FLOW FLUCTUATIONS, THEN COMPLET E LOSS OF POWER. WAS CLOSE TO WST, SECURED LEFT ENGINE AND LANDED. REEVES AIR INSPECTED AND FOUND LEFT ENGINE DRIVEN F UEL PUMP INOPERABLE. INSTALLED OVERHAULED UNIT AND AIRCRAFT RETURNED TO SERVICE 8-19-99. (X) 1 L 7 2 3O 3 O A7SO E9CE 2000012200066 20000122 00066 EA 2000 1 22 JBXA9900123 1 19991117 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A JBXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 05 582ML 0870A 7322 FLAPS FAILED ON TAKEOFF DURING FLAP RETRACTION FROM 20 DEGREES TO 8 DEGREES. FLAPS FAIL AMBER MESSAGE APPEARED, AND FL AP INDICATION REMAINED AT 20 DEGREES. (FERRIED AIRCRAFT IAW CRJ CONCESSION/INSTRUCTION LETTER NR C095-1379 FROM PHL TO RDU WITH FLAPS AT 20 DEGREES PER GMM). REMOVED AND REPLACED RT FLAP BPSU (BRAKE POSITION SENSING UNIT) IAW DRJ AMM 27-5 1-10. PERFORMED OPERATIONAL TEST OF FLAP SYSTEM IAW CRJ AMM 27-54-0, NO FAULTS AT THIS TIME. SUBSEQUENT DISCREPANCY: F LAPS HALFSPEED MESSAGE AT 30 DEGREES. REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) IAW CRJ AMM 27-51-05. CH ECKS GOOD AT THIS TIME. FECU MPN: 860D100-18, S/N 572. (X) 2 L 7 2 4F RT A21EA 2000012200067 20000122 00067 EA 2000 1 22 JBXA9900124 1 19991119 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A JBXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 05 586ML 7341 FLIGHT ATTENDANT SMELLED GASOLINE IN THE FORWARD GALLEY AREA "NOT NOTICEABLE IN COCKPIT". HOWEVER, EMERGENCY WAS DECLAR ED AND LANDED IN RDU. (FLIGHT FROM ATL TO RDU). PERFORMED GENERAL INSPECTION OF CABIN INTERIOR IN AND AROUND GALLEY AR EA. NO SMELL OF GASOLINE NOTED. (X) 2 L 7 2 4F RT A21EA 2000012200068 20000122 00068 NE 2000 1 22 MASA99137 2 19990811 A 7230 COMPRESSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE STALLED A MASA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 47239 7239 RDU/LGA - FLT 5830 - DURING TAKEOFF, CAPTAIN HEARD A LOUD BANG AND BELIEVED IT WAS A BLOWN TIRE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE TIRES AND AIRCRAFT, NO DAMAGE WAS NOTED. THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F RT A21EA E15NE 2000012200069 20000122 00069 NE 2000 1 22 PLGA9909238 2 19990923 A 7420 6058T27P01 WIRE HARNESS SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A PLGA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 NE 05 338BE GJW80603 340A034 GEE367337 BOS - FLT 4658 - ON APPROACH OF FLT 4658 PSI TO BOS, APPROXIMATELY 7 MILES OUT, THE LT ENGINE SHUT DOWN UNCOMMANDED. T HE AIRCRAFT LANDED AT BOS WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE. REPLACED THE ENGINE CONTROL UNIT FUEL FI LTER AND OVERSPEED AND DRAIN VALVE. UPON FURTHER TROUBLESHOOTING, FOUND THE YELLOW HARNESS FAILING SOME OF THE ELECTRIC AL CHECKS. MAINTENANCE REPLACED THE YELLOW HARNESS AND PERFORMED ALL REQUIRED CHECKS. ALL CHECKS WERE GOOD. A TEST FL IGHT WAS PERFORMED. RESULTS WERE FOUND SATISFACTORY AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE6 2000012200070 20000122 00070 CE 2000 1 22 RU3A99011 1 19990928 A 2422 501132901 INVERTER BEECH 300 300BEECH 1152930 CE NR 1 BURNT A RU3A H DEACTIVATE SYST/CIRCUITS B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 21 69 FF4 LOST NR 1 INVERTER AND ASSOCIATED AVIONICS. USED EMERGENCY CHECK LIST AND SWITCHED TO NR 2 INVERTER. REPLACED CURRENT LIMITER AND NR 1 INVERTER. (X) 2 L 7 2 4T A24CE 2000012200071 20000122 00071 EU 2000 1 22 2000ZZZX164 1 19991014 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU LT EMER EXIT DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GYJBM 362 SFO - FLT 8168 - LEFT OVERWING EMERGENCY BATTERY GETTING FAULT WHEN TESTED. REPLACED EMERGENCY BATTERY. (X) 2 L 7 2 4F RT A28NM 2000012200072 20000122 00072 EU 2000 1 22 2000ZZZX165 1 19990812 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERABLE A RYNA K NONE L NO TEST CR CRUISE 1 CE 07 GYJBM 362 SFO - FLT 8188 - EMERGENCY EXIT LIGHTS AT CENTER CABIN AND LEFT NR 2 RIGHT NR 2 DOORS ARE INOPERATIVE IN-FLIGHT. RE-SET CABIN INTERCOMMUNICATION DATA SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2000012200073 20000122 00073 EU 2000 1 22 SIMA992831 1 19991010 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY FAILED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 345SB A2737 340B345 MIA - FLT 5257 - LAVATORY SMOKE WARNING LIGHT ILLUMINATED TWICE IN-FLIGHT FOR APPROXIMATELY THREE SECONDS EACH TIME. VE RIFIED EVENT AS A FALSE WARNING. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 2000012200074 20000122 00074 EU 2000 1 22 SIMA992921 1 19991019 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 358RZ 340B358 ABI - SEAT TRACK BL ZERO AND 18.3L CORRODED. REMOVED FASTENERS AND EXISTING SEAT TRACK. DRILLED FASTENER HOLES ON NEW SEAT TRACK EXTRUSION AND TREATED. INSTALLED NEW SEAT TRACK AND SECURED. APPLIED DINOTROL TO SEAT TRACK AND SUPPORTS. W ORK DONE IAW SAAB 340 SRM 53-70-60 AND SAAB 340 AMM 20-10-00. AIRCRAFT OK FOR SERVICE. REF: OPER CONTROL NR 2000ZZZX1 66. (X) 2 L 7 2 4T RT A52EU 2000012200075 20000122 00075 EU 2000 1 22 2000ZZZX166 1 19991019 A 5347 7253725193 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 358RZ 340B358 ABI - SEAT TRACK BL ZERO AND 18.3L CORRODED. REMOVED FASTENERS AND EXISTING SEAT TRACK. DRILLED FASTENER HOLES ON NEW SEAT TRACK EXTRUSION AND TREATED. INSTALLED NEW SEAT TRACK AND SECURED. APPLIED DINOTROL TO SEAT TRACK AND SUPPORTS. W ORK DONE IAW SAAB 340 SRM 53-70-60 AND SAAB 340 AMM 20-10-00. AIRCRAFT OK FOR SERVICE. REF: OPER CONTROL NR SIMA99292 -1. 2 L 7 2 4T RT A52EU 2000012200076 20000122 00076 SO 2000 1 22 SIMA992953 1 19991022 A 3350 GE1317 BULB EMB 145 EMB145LR SO EXTERIOR FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 618AE 145097 ORD - FLT 4389 - RIGHT FORWARD EXTERIOR EMERENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED RIGHT FORWARD EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKED GOOD. (X) 2 L 7 2 4T RT T00011AT 2000012200077 20000122 00077 SO 2000 1 22 SIMA992911 1 19991018 A 3350 20131A BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 619AE 68861 145101 ORD - FLT 4211 - FIRST TWO CABIN EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED ONE EMERGENCY BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 2000012200078 20000122 00078 SO 2000 1 22 SIMA992841 1 19991011 A 3350 7287580J01 LIGHT EMB 145 EMB145LR SO CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 632AE 145143 ORD - FLT 4045 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROWS 8 AND 9 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY FLO OR LIGHT STRIP AT ROWS 8 AND 9. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 2000012200079 20000122 00079 SO 2000 1 22 SIMA992981 1 19991025 A 3230 852701 SWITCH EMB 145 EMB145LR SO RT MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 635AE A10473 145158 ORD - FLT 4387 - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED TWO RIGHT MAIN LANDING GEAR PROXIMITY SWITCHES. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 2000ZZZX167. (X) 2 L 7 2 4T RT T00011AT 2000012200080 20000122 00080 SO 2000 1 22 2000ZZZX167 1 19991025 A 3230 852701 SWITCH EMB 145 EMB145LR SO RT MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 635AE A10971 145158 ORD - FLT 4387 - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED TWO RIGHT MAIN LANDING GEAR PROXIMITY SWITCHES. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA99298-1. 2 L 7 2 4T RT T00011AT 2000012200081 20000122 00081 SO 2000 1 22 SIMA992962 1 19991023 A 3350 RPS113 BATTERY PACK EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 637AE 13672 145170 ORD - FLT 4233 - FORWARD CABIN EEMRGENCY LIGHTS DO NOT ILUMINATE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 2000012200082 20000122 00082 SO 2000 1 22 SIMA992871 1 19991014 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR SO CABIN INOPERABLE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 638AE 60649 145172 ORD - FLT 4296 - CABIN EMERGENCY LIGHTS ON WITH NO POWER ON AIRCRAFT. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT POWER S UPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 2000012200083 20000122 00083 SO 2000 1 22 SIMA993001 1 19991027 A 3230 22270100001 SOLENOID EMB 145 EMB145LR SO NLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 639AE 210 145182 ORD - FLT 4245 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR VALVE UP SOLENOID. AI RCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 2000012200084 20000122 00084 NM 2000 1 22 TWRA9963 1 19991014 A 3610 VALVE BOEING 747 747237B NM NR 3 ENGINE CRACKED A TWRA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 15 104TR 21446 AFTER TAKEOFF AT APPROXIMATELY 200 FEET AGL, NR 3 ENGINE FIRE WARNING ILLUMINATED. AFTER COMPLETION OF TOWER AIR PROCED URES, LIGHT EXTINGUISHED. WRITE-UP ENGINE WINDMILLING TIME APPROXIMATELY 6 MINUTES, OIL PRESSURE APROXIMATELY 10 PSI RE MAINDER OF FLIGHT. NO FUEL DUMPED. LANDING WEIGHT 515.000. UPON PNEUMATIC LEAK INSP, FOUND HIGH STAGE VALVE CRACKED. REMOVED AND REPLACED HIGH STAGE VALVE PER MM 36-11-05. OPS CHECK OK PER MM 36-11 00 NORMAL. PERFORMED WINDMILLING INS PECTION PER MM 72-00-00. FOUND NO ABNORMALITIES. ALSO PERFORMED VISUAL INSPECTION ON ENGINE FOR HEAT DAMAGE. NO DAMAG E NOTED. (X) 2 L 7 4 4F A20WE 2000012200085 20000122 00085 EA 2000 1 22 2000ZZZX168 1 19991105 A 3231 864202 SWITCH 83232311101 DHAV DHC8 DHC8311 1386006 EA RT MLG WW CONTAMINATED A UHLA O OTHER N FALSE WARNING CR CRUISE 1 NE 03 802SA 16309 250 UHLA6401 - BUF/BDL - FLT 222 - DURING CRUISE, RIGHT MAIN HYD GEAR DOOR OPENED. SLOWED TO GEAR SPEED. FLIGHT COMPLETED WITHOUT FURTHER INCIDENT. WHEN GEAR SELECTED DOWN, DOOR CLOSED AND OPERATED NORMALLY FOR EXTENSION CYCLE. FOUND GEAR D OOR PROXIMITY SENSOR DIRTY. CLEANED PROXIMITY SENSOR GEAR DOOR. GROUND OPERATION AND INDICATION NORMAL. (X) 2 H 7 2 4T RT A13NM 2000012200086 20000122 00086 EA 2000 1 22 2000ZZZX169 1 19991030 A 7312 3035817 FILTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 ENGINE WRONG PART A UHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NE 03 805SA 9502 274 TM123222 WHILE COMPLETING ACCEPTANCE INSPECTION, NOTED THE WRONG FUEL FILTER INSTALLED AT THE NR 1 FUEL OIL HEATER RESULTING IN D AMAGE TO THE FILTER HOUSING AND MOUNTING LUGS. DAMAGE WAS DISCOVERED WHILE AIRCRAFT WAS IN MAINTENANCE AND NO FURTHER I NCIDENTS WERE REPORTED, MAINTENANCE REMOVED AND REPLACED FUEL OIL HEAT IAW P&WC MM 72-01-00. OPS LEAK CHECKED GOOD. N O DEFECTS NOTED AT THIS TIME. 2 H 7 2 4T 4 T RT A13NM E20NE 2000012200087 20000122 00087 EU 2000 1 22 USAASA99004 1 19990913 A 3350 32145410 POWER SUPLY AIRBUS A319 A319112 EU CABIN INOPERABLE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 701UW 0890 TPA - THE LEFT WING EMERGENCY EXIT OVERHEAD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE LEFT WING EMERGENCY EXIT. (X) 2 L 7 2 4F RT A28NM 2000012200088 20000122 00088 EU 2000 1 22 USAASA99006 1 19990923 A 3350 BATTERY PACK AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 710UW 1019 SFO - THE AFT EXIT EMERGENCY LIGHTS FOR SEAT 21 WERE INOPERATIVE. MAINTENANCE REPLACED THE EXIT LIGHT BATTERY PACK. (X ) 2 L 7 2 4F RT A28NM 2000012200089 20000122 00089 EU 2000 1 22 USAASA99008 1 19991106 A 5610 NP1653116 WINDSHIELD AIRBUS A319 A319112 EU COCKPIT CRACKED A USAA G A O2 MASK DEPLOYED UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 723UW 17 1109 JAX - FLT 1464 - WHILE AT FL 370, THE FIRST OFFICER'S WINDSHIELD CRACKED. THE FLIGHT CREW DONNED THEIR OXYGEN MASKS AND DESCENEDED TO FL 100. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO JAX WHERE A ROUTINE LANDING WAS MADE. MAIN TENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. (X) 2 L 7 2 4F RT A28NM 2000012200090 20000122 00090 NM 2000 1 22 UIEA99076 1 19990920 A 5753 69B141035 PIN BOEING 747 74747UF 1384949 NM TE AFT FLAP LOOSE A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 4816 1090 29253 DURING C1 CHECK AT FRA, FOUND OUTBOARD FLAP CARRIAGE AFT BOGIE PIN ASSEMBLY L/S NR 2 POS WITH BROKEN SAFETY WIRE AND BOT H BOLT SAFETY PIN AND PIN ASSY MIGRATED OUTWARD OVER .50 INCH. PER BOEING TELEX AND ATLAS AIR EO 4427A001, RESEATED PIN ASSY, TORQUE RETAINER BOLT, DRILLED PIN ASSY HEX (FLAT TO FACE), SAFETY WIRED BOLT. NR 2 L/S BOGIE FOUND STRETCHED WIR E, TORQUE BOLT, DRILLED PIN, REPLACED SAFETY WIRE PER ATLAS AIR EO 4427A001. NR 7 R/S BOGIE FOUND BROKEN WIRE, NO MIGRA TION OF PIN OR BOLT, DRILLED PIN AND REPLACED SAFETY WIRE PER EO. ALL OTHER POSITIONS DRILLED PIN ASSY AND SAFETY WIRED PER ATLAS AIR EO 4427 A001. (X) 2 L 7 4 4F RT 1384945 2000012200091 20000122 00091 NM 2000 1 22 UIEA99077 1 19990920 A 5753 69B112593 RETAINING NUT BOEING 747 74747UF 1384949 NM TE MIDFLAP LOOSE A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 4816 1090 29253 DURING C1 CHECK AT FRA, FOUND ALL MID-FLAP CARRIAGE FITTING (SPINDLE) POSITION RETAINING NUTS BELOW ZERO TORQUE. FOUND ALL RETAINER PLATES INSTALLED. INSPECTED AREA, FOUND NO ABNORMALITIES. RE-TORQUED ALL EIGHT POSITIONS TO MM LIMITS PER 27-51-23 (INBOARD) AND 27-51-28 (OUTBOARD). (X) 2 L 7 4 4F RT 1384945 2000012200092 20000122 00092 EU 2000 1 22 USAA991301 1 19991124 A 5720 D57541499208 ANGLE AIRBUS A319 A319112 EU LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 712US 1448 1038 TPA - DURING A-4 CHECK, FOUND 3 INCH CRACK AT INBOARD SUPPORT ANGLE AT LT WING UNDER AILERON CLOSE OUT PANE NR Z57S. IN STALLED ANGLE, FABRICATED FROM 301 1/2 HARD .032 INCH STAINLESS STEEL PER EA 94088. (X) 2 L 7 2 4F RT A28NM 2000012200094 20000122 00094 WP 2000 1 22 MWEA99938 1 19991228 A 5320 9910078871 DOUBLER DOUG DC9 DC932 3022066 WP BS 217, 218, 229 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47744 SUB - FLOOR IS CRACKED AT FUSELAGE STATION 217 AND 229 UNDER NR 4 SEAT TRACK. ALSO, CRACKED AT STATION 218 AT THE CENTE RLINE. MAINTENANCE FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2000012200095 20000122 00095 WP 2000 1 22 MWEA99939 1 19991221 A 5320 575468827 DOUBLER DOUG DC9 DC932 3022066 WP COCKPIT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47744 LEFT AND RIGHT COCKPIT WINDOW DOUBLER AND SHIM PLATE HAVE CRACK INDICATIONS. MAINTENANCE REMOVED CRACKED DOUBLERS, THEN FABRICATED AND INSTALLED NEW DOUBLERS. 2 L 7 2 4F A6WE 2000012200096 20000122 00096 WP 2000 1 22 MWEA99943 1 19991221 A 5330 59100681 SKIN DOUG DC9 DC932 3022066 WP BS 506 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47744 DENT AT FUSELAGE STATION 506, JUST ABOVE LONGERON 23 LEFT. MAINTENANCE FABRICTED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000012200097 20000122 00097 WP 2000 1 22 MWEA99940 1 19991222 A 5320 9910078 RIVET DOUG DC9 DC932 3022066 WP CABIN MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47744 TWO RIVET HEADS MISSING ON SUB-FLOOR IN FORWARD ENTRY. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000012200098 20000122 00098 WP 2000 1 22 MWEA99941 1 19991230 A 5320 9910078 WEB DOUG DC9 DC932 3022066 WP BS 150 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47744 CORROSION ON GALLEY SUB-FLOOR AROUND PLUMBING HOLES AT STATION 150. MAINTENANCE CUT AWAY CORROSION, THEN FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000012200099 20000122 00099 WP 2000 1 22 MWEA99942 1 19991230 A 5320 9910078 WEB DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47744 SUB-FLOOR FOR GALLEY NR 2 INBOARD FORWARD AND AFT FLOOR MOUNTS HAVE CORROSION ON THEM. MAINTENANCE REMOVED CORROSION, T HEN FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000012200102 20000122 00102 WP 2000 1 22 TWAA0000609 1 19991227 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 MISREPAIRED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND IN RT LAV AT STA 980 FORMER RING BETWEEN LONGERON 15 AND 16 AN INCORRECT REPAIR INSTALLE D. CUT FORMER RING BETWEEN STRINGER 10 AND 11 AND INSTALLED NEW BOEING RING PN 9958238-7. INSTALLED SPLICE PER SRM 53- 03, FIG 32, SHEET 2 AND 3. DOUBLER MADE FROM 7075-O, 0.063 IN, HEAT TREATED TO T6. INSTALLED CLIPS PER MO 72J14H AT ST RINGER 13, 14, 16, AND 17. 2 L 7 2 4F A6WE 2000012200103 20000122 00103 WP 2000 1 22 TWAA0000610 1 19991229 A 5720 BRACKET DOUG DC9 DC932 3022066 WP LT WING DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK ON LT WING TE NEED INSTALL RIB ASSEMBLY OTBD OF CENTER, FLAP HINGE ASSEMBLY, AFTER FLAP HINGE B RACKET INSTALLED. REINSTALLED HI-LOCKS IN RIB ASSEMBLY PER SRM 51-30-5, PAGE 12 AND 13, PARAGRAPH 7 A AND B. REINSTALL ED RIB PER SRM 51-30-2. 2 L 7 2 4F A6WE 2000012200104 20000122 00104 WP 2000 1 22 TWAA0000611 1 19991228 A 5720 HINGE DOUG DC9 DC932 3022066 WP LT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND ON LT WING, CENTER FLAP HINGE SUPPORTS HAD RUST EMITTING FROM HINGE TO REAR SPAR ATTACH BOLTS. ACCOMP HIGH FREQ EDDY CURRENT TO HOLES AND AREA PER TWA NDT 51-00-3, PART 6. INSTALLED NEW STUDS AND FLAP HINGE FITTING PER MM 57-40-1. 2 L 7 2 4F A6WE 2000012200105 20000122 00105 WP 2000 1 22 TWAA0000612 1 19991229 A 5720 BOLT DOUG DC9 DC932 3022066 WP RT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND ON RT WING TE, RUST EMITTING FROM TOP INBD BOLT OF CENTER FLAP HINGE CASTING AT REAR SPA R. ACCOM HIGH FREQ EDDY CURRENT OF HOLES AND AREA PER TWA NDT 51-00-03, PART 6, AND 2 EA CRACKS FOUND. INSTALLED 4 EA NEW STUDS AND ONE FLAP HINGE FITTING PER MM 57-40-1. 2 L 7 2 4F A6WE 2000012200106 20000122 00106 WP 2000 1 22 TWAA0000613 1 19991228 A 5720 BRACKET DOUG DC9 DC932 3022066 WP LT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND ON LT WING TE THE INBD FLAP HINGE SUPPORT BRACKET HAD RUST EMITTING FROM BETWEEN HINGE S UPPORT BRACKET TO ATTACH BOLT. ACCOMP HIGH FREQ EDDY CURRENT OF HOLES IN AREA PER TWA NDT 51-00-03 PART 6. INSTALLED N EW STUDS AND FLAP HINGE FITTING PER MM 57-40-1. 2 L 7 2 4F A6WE 2000012200107 20000122 00107 WP 2000 1 22 TWAA0000614 1 19991230 A 5720 BRACKET DOUG DC9 DC932 3022066 WP RT WING MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, RT WING TE NEED INSTALL RIB ASSEMBLY OTBD OF CENTER FLAP HINGE ASSEMBLY AFTER FLAP BRACKET INS TALLED. INSTALLED RIB ASSEMBLY USING HI-LOCKS PER SRM 51-30-5 AND RIVETS PER SRM 51-30-2. 2 L 7 2 4F A6WE 2000012200108 20000122 00108 WP 2000 1 22 TWAA0000607 1 19991209 A 5320 PANEL DOUG DC9 DC932 3022066 WP BS 698 GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND IN RT WHEEL WELL RT TRAPAZOIDAL PANEL AREA AT STR 20R, ABOVE RT TRAP PANEL, HAD 3.5 IN G OUGE BY 0.015 IN DEEP, STA 698. BLENDED GOUGE PER SRM 53-01, FIG 1 PAGE 6 LIMITS, AND 51-10-03 PROCESS. TREATED ON NON -ROUTINE CARD. 2 L 7 2 4F A6WE 2000012200109 20000122 00109 WP 2000 1 22 TWAA0000601 1 19991215 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 216 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CABIN ATTACH ANGLE AND MEMBRANE WITH CORROSION AT RBL 55 IN, STA 216. REMOVED AND REPLA CED MEMBRANE AND FLOOR ATTACH ANGLE PER SPM 6-70-01, PART A AND B. ANGLE REPLACED ON SEPARATE NON ROUTINE. 2 L 7 2 4F A6WE 2000012200110 20000122 00110 WP 2000 1 22 TWAA0000602 1 19991215 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 - 229 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR TRACK WITH CORROSION AT RBL 45 IN, STA 200 TO 229. REMOVED OLD PART OF TRAC K AND INSTALLED NEW PIECE PER SRM 53-05, FIG 4. 2 L 7 2 4F A6WE 2000012200111 20000122 00111 WP 2000 1 22 TWAA0000603 1 19991216 A 5711 SPAR DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND ON RT WING 2 EA SURFACE CRACKS AT TOP OF REAR SPAR, INBD HOLE 3/8 IN LONG, OTBD HOLE .5 IN LONG, AT CENTER FLAP HINGE AREA. STOP DRILLED CRACKS PER DOUGLAS REPAIR DOCUMENT JO60272. REPAIRED CRACKS AT TOP OF REAR SPAR RT WING AT CENTER FLAP HINGE PER JO60272. SUBSTITUTED HL325-6 FOR HLT59-6 PER SRM 51-60-0, FIG 4, PARAGRAPH 33. 2 L 7 2 4F A6WE 2000012200112 20000122 00112 WP 2000 1 22 TWAA0000604 1 19991216 A 5753 SKIN DOUG DC9 DC932 3022066 WP TE FLAP DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND RT WING FLAP LOWER SKIN AND DOUBLER WITH BAD HOLES BY OTBD HINGE CASTING. FABRICATED SK IN AND DOUBLER PER SRM 57-50-9. REPLACED SKIN AND FILLER SECTION PER SRM 51-10-01. 2 L 7 2 4F A6WE 2000012200113 20000122 00113 WP 2000 1 22 TWAA0000605 1 19991214 A 5521 SPAR DOUG DC9 DC932 3022066 WP ELEVATOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND RT ELEVATOR FRONT SPAR CRACKED APPROX 120 IN FROM INBD END. REPAIRED PER DWG 5934866-50 3. 2 L 7 2 4F A6WE 2000012200114 20000122 00114 WP 2000 1 22 TWAA0000606 1 19991215 A 5521 SPAR DOUG DC9 DC932 3022066 WP ELEVATOR LIGHTNING STRIKE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND LT ELEVATOR REAR SPAR LOWER SURFACE APPROX 14 IN FROM OTBD END WITH SKIN BURNED FROM LIG HTNING STRIKE. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 55-03, FIG 15 PAGE 32. 2 L 7 2 4F A6WE 2000012200115 20000122 00115 WP 2000 1 22 TWAA0000608 1 19991227 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 MISREPAIRED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, FOUND AN INCORRECT REPAIR ON FUSELAGE FRAME AT STA 980, BETWEEN LONGERON 14L AND 16L. CUT OLD ER SECTION OF FORMER RING BETWEEN STA 10 AND 11, AND INSTALLED NEW RING PN 9958238-7. INSTALLED SPLICE FABRICATED FROM 0.063, 7075-0 HEAT TREAT TO T6 PER SRM 53-05, FIG 32, SHEET 2 AND 3. 2 L 7 2 4F A6WE 2000012200121 20000122 00121 NM 2000 1 22 TWAA0000701 1 19991130 A 5330 SKIN BOEING 727 727231 1384079 NM FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54348 21967 DURING CHECK-C MAINT, THE FWD ENTRY DOOR LOWER HINGE CUT OUT WAS CRACKED, FWD 1 1/2 INCHES IN FUSELAGE SKIN. ACCOMP HIG H FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-01, PAGE 6. INSTALLED REPAIR DOUBLER PER SSRM 53-10-219, DETAIL III. 2 L 7 3 4F A3WE 2000012200122 20000122 00122 WP 2000 1 22 TWAA0000702 1 19991227 A 5320 MEMBRANE DOUG DC9 DC983 3022083 WP BS 608 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING OP 16 MAINT CHECK, FOUND CABIN MEMBRANE WITH AREA CUTOUT FOR CORROSION REMOVAL AND LIGHTING HOLE ON RT SIDE, STA 608. ALODINED AND PRIMED PER SRM 51-10-3, PAGE 18, AND 51-10-3 PAGE 16. REPAIRED PER SRM 53-01, AGE 18 F4. 2 L 7 2 4F RT A6WE 2000012200123 20000122 00123 WP 2000 1 22 TWAA0000703 1 19991228 A 5230 FLANGE DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING OP 16 MAINT CHECK, FOUND CRACK IN FWD CARGO DOOR FLANGE ON AFT SIDE NEXT TO DOOR HOLD OPEN LATCH. ACCOMP HIGH FR EQ EDDY CURRENT PER 51-00-03 FOR CRACK CONTAINMENT. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 52-05, PAGE 110A, FIG 26A, VIEW C-C. 2 L 7 2 4F RT A6WE 2000012200124 20000122 00124 WP 2000 1 22 TWAA0000704 1 19991228 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 200 - 218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING OP 16 MAINT CHECK, FOUND CORROSION ON TRACK FROM STA 200 TO 218, RBL 44. REPLACED FLOOR TRACK PER SRM 53-05, PAG E 10G AND H, FIG 4F. 46 INCHES OF TRACK REPLACED. 2 L 7 2 4F RT A6WE 2000012200128 20000122 00128 WP 2000 1 22 MWEA99944 1 19991218 A 5320 SRO953013711 SPLICE DOUG DC9 DC932 3022066 WP BS 407 - 419 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD CARGO COMPARTMENT CORROSION ON LONGERON 30 DOUBLER AT STATION 407 TO 419. MAINTENANCE REMOVED CORROSION AND FOU ND CRACK AT LONGERON 30 SPLICE. MAINTENANCE FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F A6WE 2000012200129 20000122 00129 WP 2000 1 22 MWEA99945 1 19991218 A 5320 59203192 SPLICE DOUG DC9 DC932 3022066 WP BS 375 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DUE TO NRI 18870 AND 18909, SPLICE IS REQUIRED ON LONGERON 30 AT STATION 375. MAINTENANCE FABRICATED AND INSTALLED NEW LONGERON SPLICE. 2 L 7 2 4F A6WE 2000012200130 20000122 00130 WP 2000 1 22 MWEA99946 1 19991216 A 5313 591142351 LONGERON DOUG DC9 DC932 3022066 WP BS 995 MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 CORROSION ON END OF TIE CLIP AT FUSELAGE STATION 995, LONGERON 22 LEFT. LONGERON 22 LEFT BLENDED OUT OF LIMITS. MAINTE NANCE FABRICATED AND INSTALLED SPLICE FITTING AND LONGERON. 2 L 7 2 4F A6WE 2000012200131 20000122 00131 WP 2000 1 22 MWEA99947 1 19991218 A 5311 3921813505 FRAME DOUG DC9 DC932 3022066 WP BS 333 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD CARGO COMPARTMENT CORROSION ON TOP OF FRAME UNDER FLOOR SUPPORT AND UNDER NUTPLATES AT STATION 333. MAINTENANCE FABRICATED AND INSTALLED NEW PLATE FOR REPAIR STATION. 2 L 7 2 4F A6WE 2000012200132 20000122 00132 WP 2000 1 22 MWEA99948 1 19991216 A 5315 99581851 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 917 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FLOORBEAM CHAFFED THROUGH AT FUSELAGE STATION 917. MAINTENANCE FABRICATED AND INSTALLED FLOORBEAM. 2 L 7 2 4F A6WE 2000012200133 20000122 00133 WP 2000 1 22 MWEA99949 1 19991216 A 5315 99115441 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 HEAVY CHAFING ON FLOORBEAM ABOVE FORWARD CARGO DOOR STATION 389. MAINTENANCE FABRICATED AND INSTALLED FLOORBEAM. 2 L 7 2 4F A6WE 2000012200134 20000122 00134 WP 2000 1 22 MWEA99950 1 19991214 A 5730 591214426 SKIN DOUG DC9 DC932 3022066 WP BS 164 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LEFT WING LOWER SURFACE INBOARD OF STATION 164 AFT OF REAR SPAR, THE SKIN IS CRACKED. MAINTENANCE FABRICATED AND INSTAL LED PANEL, SKIN AND BUET DOOR. 2 L 7 2 4F A6WE 2000012200135 20000122 00135 WP 2000 1 22 MWEA99951 1 19991220 A 5313 99155504 LONGERON DOUG DC9 DC932 3022066 WP BS 980 - 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 INTERCOSTAL LONGERON 28 RIGHT STATION 980-996 CORROSION OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED NEW LONGERO N. 2 L 7 2 4F A6WE 2000012200136 20000122 00136 WP 2000 1 22 MWEA99952 1 19991220 A 5315 595603345 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 917 - 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 NUMEROUS NUT PLATES HAVE CORROSION ON UNDERSIDE ON THE FORWARD AND AFT GILLINER SUPPORT STRUTS AT FUSELAGE 917 TO 996 AN D 943-996. SUPPORT BETWEEN FUSELAGE 917 TO 945 OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F A6WE 2000012200139 20000122 00139 WP 2000 1 22 ABXA000006 1 19991123 A 5320 49559771 BRACKET DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND RT MLG INBD DOOR FWD JAMB ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 2000012200140 20000122 00140 WP 2000 1 22 MWEA99953 1 19991221 A 5230 0952008945 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 AFT CARGO DOOR OUTER PAN HAS GOUGES ON THE FORWARD END OF THE NR 1, 3, AND 4 DOOR STOPS. MAINTENANCE DRILLED AND INSTAL LED NEW OUT PAN.. 2 L 7 2 4F A6WE 2000012200141 20000122 00141 WP 2000 1 22 MWEA99954 1 19991222 A 5347 2772660 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 - 237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 NR 3 SEAT TRACK IS MODERATELY CORRODED FROM STATION 200 TO STATION 237. MAINTENANCE DRILLED AND INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 2000012200142 20000122 00142 WP 2000 1 22 MWEA99955 1 19991222 A 5347 2914913 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 - 237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 NR 4 SEAT TRACK IS CORRODED FROM STATION 200 TO STATION 237. MAINTENANCE DRILLED AND INSTALLED NEW TRACK. 2 L 7 2 4F A6WE 2000012200143 20000122 00143 WP 2000 1 22 MWEA99956 1 19991222 A 5347 995787117 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FIRST OFFICERS AFT SEAT RAILS ARE WORN. MAINTENANCE FABRICATED AND INSTALLED NEW RAILS. 2 L 7 2 4F A6WE 2000012200144 20000122 00144 WP 2000 1 22 MWEA99957 1 19991222 A 5347 995787111 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CAPT'S AFT SEAT RAILS ARE WORN. MX FABRICATED AND INSTALLED NEW RAILS. 2 L 7 2 4F A6WE 2000012200145 20000122 00145 WP 2000 1 22 MWEA99958 1 19991220 A 5330 5911401 SKIN DOUG DC9 DC932 3022066 WP BS 80 CREASED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CREASE IN FUSELAGE SKIN AT STATION 80 LONGERON 20 LEFT. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000012200146 20000122 00146 WP 2000 1 22 MWEA99959 1 19991221 A 5330 5911410 SKIN DOUG DC9 DC932 3022066 WP BS 225, 291, 307 LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 3 AREAS OF LIGHTNING STRIKE DAMAGE AT FUSELAGE STATIONS 225, 291, 307 BELOW LONGERON 23. REMOVED CORROSION FOUND THAT S TATION 307 NEEDS DOUBLER. MX FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000012200147 20000122 00147 WP 2000 1 22 MWEA99960 1 19991228 A 5320 9910078 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FLOORBOARD J CHANNEL SUPPORT HAS MODERATE CORROSION AT STATION 160 AT CENTERLINE. MX FABRICATED AND INSTALLED NEW J-CHA NNEL. 2 L 7 2 4F A6WE 2000012200148 20000122 00148 WP 2000 1 22 TWAA0000813 1 19991117 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 218 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9626F 53596 THE RT FUSELAGE EXTERNAL DOUBLER WAS REMOVED TO GAIN ACCESS TO DAMAGE AT STA 218, LONGERON 21R. INSTALLED DOUBLER PER S RM 53-04, FIG 12B. CHECK-C 10-2-99 STL. 2 L 7 2 4F RT A6WE 2000012200149 20000122 00149 WP 2000 1 22 TWAA0000810 1 19991231 A 5730 SKIN DOUG DC9 DC983 3022083 WP RT WING SCRATCHED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9626F 53596 RT WING LE CAP WAS SCUFFED ON LOWER SURFACE, 6 IN BY 4 INCHES OFF OF NUMBER 4 SLAT. REMOVED AND REINSTALLED SERVICEABLE NUMBER 4 LE CAP PER DOUGLAS BLUE PRINT 5937523, SHEET 1. CHECK-C 10-2-99 STL. 2 L 7 2 4F RT A6WE 2000012200150 20000122 00150 WP 2000 1 22 TWAA0000811 1 19991231 A 5730 SKIN DOUG DC9 DC983 3022083 WP RT WING TORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9626F 53596 RT WING LE SKIN WAS TORN AND DENTED DUE TO GROUND DAMAGE BETWEEN 2 OTBD TRACKS FOR NUMBER 3 SLAT, RT WING, 37 IN LONG. R EPLACED LE CAP PER DOUGLAS BLUE PRINT 5937513 SHEET 1. 2 L 7 2 4F RT A6WE 2000012200151 20000122 00151 WP 2000 1 22 TWAA0000803 1 19991230 A 5230 FLANGE DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 11OHM 49787 DURING OP 16 MAINT CHECK, FOUND CRACK IN THE FORWARD CARGO DOOR FLANGE ON FWD SIDE NEXT TO DOOR HOLD OPEN LATCH. STOP D RILLED CRACK AND INSTALLED CARGO DOOR PAN CRACK REPAIR PER SRM 52-05, PAGE 110A TO 110C, VIEW C-C. 2 L 7 2 4F RT A6WE 2000012200153 20000122 00153 WP 2000 1 22 TWAA0000806 1 19991221 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 1149 - 1169 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 939AS 49657 DURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE BETWEEN STA 1149L AND 1169L, AT LONGERON 18L. ACCOMP NDT PER 51 -00-01 PART 4.. REMOVED LIGHT AND MODERATE CORROSION ON LT FLOOR MEMBRANE BETWEEN STA 1149 AND 1169 AT LONGERON 18, PER SPM 6-80-01 PAGE 1 TO 3. REPAIRED AREA AT 1155-115 PER SRM 53-01, FIG 4 SHEET 3 PAGE 18 DOUBLER REPAIR. TREATED AREA FROM STA 1145L TO 1169L AT LONGERON 18 PER SRM 51-10-3(C)(1)AND (3), PAGE 45 AND 46. 2 L 7 2 4F RT A6WE 2000012200154 20000122 00154 NM 2000 1 22 TWAA0000807 1 19991228 A 5320 RETAINER BOEING 727 727231 1384079 NM FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54350 21969 DURING CHECK-C MAINT, FOUND THE FWD RT EMERGENCY EXIT, FWD RT EMERGENCY EXIT BOTTOM SEAL RETAINER HAD CORROSION FROM FWD BOTTOM STOP TO AFT BOTTOM STOP. REMOVED CORROSION BY SANDING PER SRM 51-16-6, PAGE 147.. ALODINED AND PRIMED PER SRM 51-16-2, PAGE 1. 2 L 7 3 4F A3WE 2000012200155 20000122 00155 NM 2000 1 22 TWAA0000808 1 19991228 A 5220 FLANGE BOEING 727 727231 1384079 NM OVERWING EXIT CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54350 21969 DURING CHECK-C MAINT, FOUND RT AFT OVERWING EMERGENCY EXIT, PRESSURE SEAL FLANGE BOTTOM SIDE WITH CORROSION FROM 6 INCHE S UP ON EACH SIDE TO BOTTOM. REMOVED CORROSION BY SANDING PER SRM 51-10-6, PAGE 147. ALODINED AND PRIMED BARE AREA PER SRM 51-10-2 PAGE 1. 2 L 7 3 4F A3WE 2000012200156 20000122 00156 NM 2000 1 22 TWAA0000809 1 19991228 A 5311 FRAME BOEING 727 727231 1384079 NM BS 1273 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54350 21969 DURING CHECK-C MAINT, FOUND CRACK ON UPPER CORD OF VENTRAL STAIRWELL, AT STA 1273 RT SIDE. INSTALLED REPAIR ANGLE PER S SRM 53-80-211. 2 L 7 3 4F A3WE 2000012200157 20000122 00157 WP 2000 1 22 TWAA0000812 1 19991206 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 218 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9626F 53596 THE FORMER SUPPORT ASSY RECEIVED GROUND DAMAGE AT FUSELAGE STA 218, STRINGER 21R. INSTALLED RING FORMER REPAIR PER SRM 53-03, FIG 3 CHECK-C 10-2-99 STL. 2 L 7 2 4F RT A6WE 2000012200160 20000122 00160 WP 2000 1 22 TWAA0000804 1 19991230 A 5312 BULKHEAD DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING OP 16 MAINT CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD AT BOTTOM CENTER END TIE AND BULKHEAD. REMOVED CORRO SION IN ACCORDANCE WITH SRM 51-10-3, PAGE 21-22 AND SPM 6-80-01, PAGE 1 AND 2. 2 L 7 2 4F RT A6WE 2000012200183 20000122 00183 WP 2000 1 22 9905619961 1 19991224 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 924RW 47185 DURING PERIODIC CHECK, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 2000012200189 20000122 00189 WP 2000 1 22 UPS00831274 1 19991228 A 5730 3612572 ACCESS PANEL DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E AT THE ACCESS PANEL 518A INTERNAL DOUBLER HAS HEAVY EXFOLIATION CORROSION UNDER THE NUTPL ATE CHANNEL. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IWA DWG 3641257 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2000012200190 20000122 00190 WP 2000 1 22 UPS00831275 1 19991228 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 598 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E LWR SKIN AT XFS 598 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED THE CRACK AND REPAIRED TH E SKIN IAW EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 2000012200191 20000122 00191 WP 2000 1 22 UPS00831276 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 597.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200192 20000122 00192 WP 2000 1 22 UPS00831278 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XILD .7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE R IB IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200193 20000122 00193 WP 2000 1 22 UPS00831279 1 19991228 A 5730 576989117 SKIN DOUG DC8 DC871F 302199D WP WS 429 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E LWR SKIN, INTERNAL DOUBLER AT XS 429 IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE I NTERNAL DOUBLER IAW DWG 5769891 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200194 20000122 00194 WP 2000 1 22 UPS00831280 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 379 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 379.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RI B IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200195 20000122 00195 WP 2000 1 22 UPS00831281 1 19991228 A 5730 56412522 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED, AND REPL ACED THE DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2000012200196 20000122 00196 WP 2000 1 22 UPS00831282 1 19991228 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED THE SKIN IAW EO DC8-5740-4087. 2 L 7 4 4F RT 4A25 2000012200197 20000122 00197 WP 2000 1 22 UPS00831283 1 19991228 A 5320 47504191 FITTING DOUG DC8 DC871F 302199D WP BS 1260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LONGERON 19R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 1260. REMOVED AND REPLACED THE FIT TING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200198 20000122 00198 WP 2000 1 22 UPS00831284 1 19991229 A 5320 37502571 SPLICE DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LONGERON SPLICE FITTING CRACKED AT FS 1050 AND LONGERON 31R. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200201 20000122 00201 WP 2000 1 22 UPS00831287 1 19991226 A 5320 577327558 FITTING DOUG DC8 DC871F 302199D WP BS 683 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 683 AT RBL 24, THE FLOOR SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTIN G IAW DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200202 20000122 00202 WP 2000 1 22 UPS00831288 1 19991227 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 310.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LT WING L/E UPPER SKIN AT XFS 310.25 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1, FIG 38. 2 L 7 4 4F RT 4A25 2000012200203 20000122 00203 WP 2000 1 22 UPS00831289 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 360.2 - 366.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 360.25 AND 366.5 ARE CRACKED AT THE AFT UPPER FASTENERS. STOP DRILLED THE CR ACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200204 20000122 00204 WP 2000 1 22 UPS00831290 1 19991228 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 310.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LT WING L/E LWR SKIN IS CRACKED AT THE FASTENER HOLE AT XFS 310.25. STOP DRILLED THE CRACK AND REPAI RED THE SKIN IAW EO DC8-5740-4087. 2 L 7 4 4F RT 4A25 2000012200205 20000122 00205 WP 2000 1 22 UPS00831291 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 297 - 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 297 AND 304 ARE CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED THE CRACKS A ND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200206 20000122 00206 WP 2000 1 22 UPS00831292 1 19991228 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 THE SHEAR TIE AT FS 640 BETWEEN LONGERON 26R AND 27R IS CRACKED. CUT DAMAGED SHEAR TIE AND REPAIRED IAW SRM 53-2-0, FIG 2B. 2 L 7 4 4F RT 4A25 2000012200207 20000122 00207 WP 2000 1 22 UPS00831293 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 467.2 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE R IB IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200208 20000122 00208 WP 2000 1 22 UPS00831294 1 19991231 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 336 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XFS 336 IS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200211 20000122 00211 WP 2000 1 22 UPS00831297 1 19991227 A 5320 58026779 FITTING DOUG DC8 DC871F 302199D WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LT W/W FITTING AT FS 879 ABOVE LONGERON 24 HAS HEAVY CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0, FIG 8. 2 L 7 4 4F RT 4A25 2000012200212 20000122 00212 WP 2000 1 22 UPS00831298 1 19991228 A 5320 37799872 FITTING DOUG DC8 DC871F 302199D WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 781 AT LONGERON 18R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200213 20000122 00213 WP 2000 1 22 UPS00831299 1 19991228 A 5320 37502571 FITTING DOUG DC8 DC871F 302199D WP BS 440 - 460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 440 TO 460 AT LONGERON 31R, THE LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE FITT ING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200214 20000122 00214 WP 2000 1 22 UPS00831300 1 19991228 A 5320 37502571 FITTING DOUG DC8 DC871F 302199D WP BS 600 - 620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 600 TO 620 AT LONGERON 31R, THE LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE FITT ING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200215 20000122 00215 WP 2000 1 22 UPS00831301 1 19991228 A 5313 UNK LONGERON DOUG DC8 DC871F 302199D WP BS 920 & 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LONGERONG 24L IS CRACKED BETWEEN FS 920 AND 940. STOP DRILLED CRACK AND REPAIRED THE LONGERON IAW SR M 53-2-2, FIG 5. 2 L 7 4 4F RT 4A25 2000012200216 20000122 00216 WP 2000 1 22 UPS00831302 1 19991228 A 5320 47504192 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 1200 AT LONGERON 17R THE INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED THE FITTIN G IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200217 20000122 00217 WP 2000 1 22 UPS00831303 1 19991229 A 5320 37592221 FITTING DOUG DC8 DC871F 302199D WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LONGERON 34R SPLICE FITTING AT FS 1270 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 5 1-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2000012200218 20000122 00218 WP 2000 1 22 UPS00831304 1 19991228 A 5320 97540241 FITTING DOUG DC8 DC871F 302199D WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 280, ABOVE LONGERON 27R, THE FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED THE FITTI NG IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 2000012200219 20000122 00219 WP 2000 1 22 UPS00831305 1 19991228 A 5320 47504232 FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 857 AT LONGERON 19R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DH SK702-997 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200220 20000122 00220 WP 2000 1 22 UPS00831306 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 227.335 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XS 227.335 IS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED T HE RIB IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200221 20000122 00221 WP 2000 1 22 UPS00831307 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 467.232 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE R IB IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200222 20000122 00222 WP 2000 1 22 UPS00831308 1 19991228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 442.185 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 RT WING L/E RIB AT XS 442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE R IB IAW SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000012200223 20000122 00223 WP 2000 1 22 UPS00831309 1 19991228 A 5320 47504191 FITTING DOUG DC8 DC871F 302199D WP BS 1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 1230 AT LONGERON 18R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED TH E FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200224 20000122 00224 WP 2000 1 22 UPS00831310 1 19991229 A 5320 3750257503 FITTING DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 THE LONGERON SPLICE FITTING AT FS 1050, LONGERON 31L IS CRACKED. REMOVED AND REPLACED THE SPLICE FIT TING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2000012200225 20000122 00225 WP 2000 1 22 UPS00831311 1 19991228 A 5751 5763132512 WEIGHT DOUG DC8 DC871F 302199D WP AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 THE RT OTBD AILERON INBD BALANCE WEIGHT HAS MODERATE CORROSION ON AND UNDER THE WEIGHT. REMOVED AND REPLACED THE RT OTBD AILERON IAW M/M 27-10-02. 2 L 7 4 4F RT 4A25 2000012200226 20000122 00226 WP 2000 1 22 UPS00831312 1 19991228 A 5320 47516432 FITTING DOUG DC8 DC871F 302199D WP BS 742 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 742 AT LONGERON 12L, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200227 20000122 00227 WP 2000 1 22 UPS00831313 1 19991228 A 5320 47504201 FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 857 AT LONGERON 18L, THE INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED THE FITTIN G IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200228 20000122 00228 WP 2000 1 22 UPS00831314 1 19991229 A 5320 37592221 FITTING DOUG DC8 DC871F 302199D WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 THE LONGERON 36 SPLICE FITTING AT FS 1270 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SR M 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200229 20000122 00229 WP 2000 1 22 UPS00831315 1 19991231 A 5315 1418898 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 CABIN FLOORBEAM AT FS 980, LBL 54, UPPER FLANGE IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH SK702-314. 2 L 7 4 4F RT 4A25 2000012200230 20000122 00230 WP 2000 1 22 UPS00831316 1 19991229 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 1160 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 FS 1160 AT LONGERON 28R, THE PRESSURE WEB LIGHTENING HOLE COVER HAS 4 OPEN HOLES. REPAIRED WEB IAW D H SK702-183. 2 L 7 4 4F RT 4A25 2000012200231 20000122 00231 WP 2000 1 22 SCNA99606 1 19991231 A 5347 GALLEY TRACK DOUG DC10 DC1015 3022118 WP BS 879 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD PIT STATION 879 OUTBOARD RT GALLEY TRACK WAS FOUND CORRODED. REMOVED CORR ODED SECTION OF THE TRACK AND FABRICATED REPAIR SPLICE FOR THE NEW TRACK SECTION IAW DC10 SRM 537000 VOL 1. ALODINED AN D PRIMED SPLICE OF NEW SECTION IAW DC10 SRM 512101 VOL 2 AND INSTALLED IAW DC10 SRM 513501 AND 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200232 20000122 00232 WP 2000 1 22 SCNA99607 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 855 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, STATION 855 FLOOR SUPPORT RBL 40 WAS FOUND CORRODED. REMOVED FLOOR SUPPORT PER DC10 5 31201 VOL 2 MATERIAL IAW DC10 SRM 511001. FABRICATED IAW DC10 SRM 531201 VOL 3. ALODINED AND PRIMED IAW DC10 SRM 51200 1 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200233 20000122 00233 WP 2000 1 22 SCNA99608 1 19991231 A 5320 FLANGE DOUG DC10 DC1015 3022118 WP BS 715 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD PIT RT OUTBOARD GALLEY TRACK INBOARD FLANGE WAS FOUND CORRODED AT STATION 715. REMOVED CORROSION IAW DC10 SRM 512101 VOL 2. MATERIAL LOSS WAS FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER IA W DC10 SRM 537000 VOL 1. ALODINED AND PRIMED IAW DC10 SRM VOL 2. INSTALLED IAW DC10 SRM 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200234 20000122 00234 WP 2000 1 22 SCNA99609 1 19991231 A 5320 FITTING DOUG DC10 DC1015 3022118 WP BS 875 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD PIT STATION 875 INBOARD LT GALLEY TRACK STOP FITTING WAS FOUND CORRODED. R EMOVED AND REPLACED STOP TRACK FITTING IAW DC10 SRM 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200235 20000122 00235 WP 2000 1 22 SCNA99610 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 791 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD PIT AT STATION 791 FLOOR SUPPORT LBL WAS FOUND CORRODED. REMOVED FLOOR SU PPORT IAW DC10 SRM 513501 VOL 2. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC10 SRM 530001 VOL 1. MATERIAL ID FO R FABRICATION OF NEW SUPPORT IAW DC10 SRM 531301 VOL 3. FABBED AND INSTALLED NEW SUPPORT IAW DC10 SRM 513501 VOL 2.. 2 L 7 3 4F A22WE 2000012200236 20000122 00236 WP 2000 1 22 SCNA99611 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 715 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD PIT STATION 715 FLOORBOARD SUPPORT RBL 20 WAS FOUND CORRODED. REMOVED DAM AGED FLOORBOARD SUPPORT IAW DC10 SRM 513101 VOL 2. FABRICATED SUPPORT IAW DC10 530001 VOL 1. ALODINED AND PRIMED IAW D C10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200237 20000122 00237 WP 2000 1 22 SCNA99612 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1910 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 1910 LT VERY OUTBOARD AT LAVATORY ATTACH POINT WAS FOUND TO HAVE CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC10 SRM 530001. MATERIAL ID FOR NEW TRACK IAW IPC 53 4215. LOCATED DRILLED DEBURRED AND INSTALLED TRACK IAW DC10 SRM 537000 VOL 1. MATERIAL ID FOR SHEET AND SPLICE HAT EXT RUSION AND FABBED IAW DC10 SRM 537000 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 537000 VOL 1. 2 L 7 3 4F A22WE 2000012200238 20000122 00238 WP 2000 1 22 SCNA99613 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND ON FLOORBOARD SUPPORT INTERCOSTAL STATION 1887 LBL28 TO 33. MATER IAL ID FOR THE SUPPORT AND FABRICATION IAW DC10 SRM 531601 VOL 3. ALODINED AND PRIMED FLOOR SUPPORT IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200239 20000122 00239 WP 2000 1 22 SCNA99614 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND ON FLOORBOARD SUPPORT INTERCOSTAL STATION 1887 LBL 39 TO 57. MATE RIAL ID FOR FLOOR SUPPORT AND FABRICATED FLOOR SUPPORT IAW DC10 SRM 531601 VOL 3. ALODINED AND PRIMED IAW DC10 SRM 512 101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200240 20000122 00240 WP 2000 1 22 SCNA99615 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1861 - 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK FROM STATION 1861 TO 1887 RBL 58 WAS FOUND TO HAVE CORROSION. MATERIAL ID IAW DC10 SRM 537000 VOL 1. FABRICATE IAW DC10 SRM 537000 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. IN STALLED IAW DC10 SRM 537000 VOL 1. 2 L 7 3 4F A22WE 2000012200241 20000122 00241 WP 2000 1 22 SCNA99616 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1986 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBOARD SUPPORT INTERCOSTAL AT STATION 1986 LBL 60 TO 71 WAS FOUND TO BE CRACKE D AND CORRODED. REMOVED SUPPORT EXTRUSION MATERIAL ID SUPPORT AND FABRICATED IAW DAC DWG AGA7091. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200242 20000122 00242 WP 2000 1 22 SCNA99617 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1910 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBOARD SUPPORT AT STATION 1910 LBL 59 TO 86 WAS FOUND TO HAVE CORROSION. FABR ICATED NEW FLOOR SUPPORT IAW DAC DWG AGA3814. ALODINED AND PRIMED AND INSTALLED FLOORBOARD SUPPORT. 2 L 7 3 4F A22WE 2000012200243 20000122 00243 WP 2000 1 22 SCNA99618 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 421 - 459 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 421 TO 459 RBL 84 WAS FOUND TO HAVE CORROSION. REMOVED CORR OSION FOUND TO BE OUT OF LIMITS IAW DC10 SRM 530001 VOL 1. INSTALLED NEW SEAT TRACK IAW DC10 SRM 513101 VOL 2 AND DC10 SRM 513301 VOL 2 AND DC10 SRM 537000 VOL 3. 2 L 7 3 4F A22WE 2000012200244 20000122 00244 WP 2000 1 22 SCNA99619 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBOARD SUPPORT INTERCOSTAL AT STATION 1887 LBL 61 TO 90 WAS FOUND CORRODED. R EMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC10 SRM 530001 VOL 2. MATERIAL ID IAW DC10 SRM 531601 VOL 3. FABRICATE D SUPPORT IAW DAC DWG AGA3814. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 512501 VOL 2.. 2 L 7 3 4F A22WE 2000012200245 20000122 00245 WP 2000 1 22 SCNA99620 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 855 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE AT STATION 855 STRINGER 47 RT TO 48 RT WAS FOUND TO BE CORRODED. REMOVE D CORRODED SHEAR TIE AND FABRICATED SHEARTIE IAW DC10 SRM 531301 VOL 3. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2 A ND INSTALLED IAW DC10 SRM 513501 AND 513300 VOL 2. 2 L 7 3 4F A22WE 2000012200246 20000122 00246 WP 2000 1 22 SCNA99621 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 855 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE AT STATION 1099 BETWEEN STRINGER 52 RT TO 51 RT WAS FOUND TO BE CORRODED . REMOVED CORROSION IAW DC10 SRM 512101 VOL 2 FOUND TO BE OUT OF LIMITS. CUT OUT SECTION OF SHEAR TIE IAW DC10 SRM 533 000 VOL 1. MATERIAL ID AND FABRICATION IAW DC10 SRM 531301 VOL 2. HEAT TREAT REPAIR IAW SRM VOL 2. ALODINED AND PRIME D IAW DC10 SRM 512101 VOL 2. INSTALLED REPAIR IAW DC10 SRM 533000. 2 L 7 3 4F A22WE 2000012200247 20000122 00247 WP 2000 1 22 SCNA99622 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 1059 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE IN THE FORWARD PIT AT STATION 1059 BETWEEN 52 RT AND 52 LT WAS FOUND COR RODED. REMOVED DAMAGED SHEAR TIE IAW DC10 SRM 513101 VOL 2. MATERIAL ID FOR SPLICE AND SHEARTIE IAW DC10 SRM 531301 VO L 3. FABRICATED SHEAR TIE ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 3. 2 L 7 3 4F A22WE 2000012200248 20000122 00248 WP 2000 1 22 SCNA99623 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 1059 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE IN THE FORWARD PIT AT STATION 1059 BETWEEN LGR 51L TO 52L WAS FOUND TO B E CORRODED. REMOVED DAMAGED SHEAR TIE IAW DC10 SRM 513101 VOL 2. FABRICATED SHEAR TIE IAW DC10 SRM 533001 VOL 1. ALOD INED AND PRIMED IAW DC10 SRM 512101 VOL 2. 2 L 7 3 4F A22WE 2000012200249 20000122 00249 WP 2000 1 22 SCNA99624 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 1039 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE IN THE FORWARD PIT AT STATION 1039 LGR 51L TO 52L WAS FOUND TO BE CORROD ED. REMOVED DAMAGED SHEAR TIE IAW DC10 SRM 513101 VOL 2. FABRICATED SHEAR TIE IAW DC10 SRM 533010 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. 2 L 7 3 4F A22WE 2000012200250 20000122 00250 WP 2000 1 22 SCNA99625 1 19991231 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP E/E BAY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD E AND E BAY SUPPORT FRAME ABOVE ACCESS DOOR WAS FOUND CORRODED ACROSS THE TOP AND RT FRAME. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC10 SRM 512101. FABRICATED REPAIR STRAP AND REMOVED VERTICAL SUPPORT TO GAIN ACCESS. CLEANED ALODINED AND PRIMED AREA AND STRAP PER SRM 512101. INSTALLED STRAP AND SHIM REINSTALLED VERTICAL SUPPORT IAW SRM 513401 AND 513501 AND 514101 VOL 2.. 2 L 7 3 4F A22WE 2000012200251 20000122 00251 WP 2000 1 22 SCNA99626 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 979 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE IN THE FORWARD CARGO PIT AT STATION 979 BETWEEN LGR 43 LEFT TO 44 LEFT W AS FOUND CORRODED. REMOVED OLD SHEAR TIE FABRICATED SHEAR TIE SPLICE AND SPLICE DOUBLER IAW DC10 SRM 531301 FIG 8C VOL 3 AND 533000 FIG 10 VOL 1. ALODINED AND PRIMED BOTH SPLICE AND DOUBLER IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 S RM 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200252 20000122 00252 WP 2000 1 22 SCNA99627 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 1801 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE IN THE CENTER CARGO PIT AT STATION 1801 LGR 50 LFT TO 49 RT WAS FOUND CO RRODED. REMOVED CORROSION FROM SHEAR TIE FOUND TO BE OUT OF LIMITS IAW DC10 SRM 530001 VOL 2. REMOVED OLD SHEAR TIE AN D LOCATED DRILLED DEBURRED AND INSTALLED NEW SHEAR TIE IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200253 20000122 00253 WP 2000 1 22 SCNA99628 1 19991231 A 5320 FITTING DOUG DC10 DC1015 3022118 WP BS 855 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD PIT AT STATION 855 LGR 43R AFT SIDE OF FORWARD TORQUE BOX FITTING WAS FOUN D CORRODED. REMOVED CORRODED FITTING IAW DC10 SRM 512101 VOL 2. DRILLED AND INSTALLED NEW FITTING IAW DC10 SRM 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200254 20000122 00254 WP 2000 1 22 SCNA99629 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 457 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOORBEAM SUPPORT AT STATION 457 LBL 59 TO LBL 75 WAS FOUND TO BE CORRODED. REMOV ED CORROSION FOUND TO BE OUT OF LIMITS IAW DC10 SRM 530001. MATERIAL ID EXTRUSION AND FABRICATION IAW DAC DWG VZA7006. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200255 20000122 00255 WP 2000 1 22 SCNA99630 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 454 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 454 LBL 56 AT FLANGE SCREW HOLE UPPER AND LOWER SURFACES WAS FOUND TO BE CORRODED. REMOVED SEAT TRACK IAW DC10 SRM 537000 VOL 1. INSTALLED SEAT TRACK IAW DC10 SRM 513301 AND DC10 SRM 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200256 20000122 00256 WP 2000 1 22 SCNA99631 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 457 - 465 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 457 TO 465 RBL 57 WAS FOUND TO BE CORRODED. REMOVED SEAT TR ACK IAW DC10 SRM 513301 VOL 2. INSTALLED NEW SEAT TRACK IAW DC10 SRM 513501 VOL 2 AND 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200257 20000122 00257 WP 2000 1 22 SCNA99632 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 460 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 460 LBL 58 WAS FOUND TO BE CORRODED. REMOVED SEAT TRACK IAW DC10 SRM 537000 VOL 1. MATERIAL ID AND INSTALLED SEAT TRACK IAW DC10 SRM 513301 VOL 2 AND 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200258 20000122 00258 WP 2000 1 22 SCNA99633 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1915 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STATION 1915 LBL 28 TO 54 FLOOR SUPPORT UPPER AND LOWER SURFACES AT SCREW HOLES WAS FOUND CORRODED. REMOVED SUPPORT EXTRUSION MATERIAL ID AND FABRICATED IAW DAC DWG AGA7090. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200259 20000122 00259 WP 2000 1 22 SCNA99634 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1915 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STATION 1915 LBL 25 TO RBL 25 UPPER AND LOWER SURFRACES AT SCREW HOLES WERE FOUND CORRODED. FABRICATED FLOOR SUPPORT IAW DWG AGA7085. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. I NSTALLED SUPPORT IAW DC10 SRM 532415 VOL 1. 2 L 7 3 4F A22WE 2000012200260 20000122 00260 WP 2000 1 22 SCNA99635 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1303 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, EQUIPMENT TIE DOWN TRACK AT STATION 1303 RBL 25 WAS FOUND CORRODED ON THE INSIDE OF TH E TRACK.. TRACK WAS FOUND TO BE OUT OF LIMITS IAW DC10 SRM 537000 VOL 1. SEAT TRACK SPLICE REPAIR WAS ACCOMPLISHED. 2 L 7 3 4F A22WE 2000012200261 20000122 00261 WP 2000 1 22 SCNA99636 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP STA 870 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE AFT ELEVATOR SUPPORT AND FLOORBEAM IN THE MAIN CABIN AT STATION 870 RBL 25 WAS FOU ND CORRODED. REMOVED FLOORBOARD SUPPORT IAW DC10 SRM 513501 VOL 2. FABRICATED SUPPORT IAW DAC DC10 DWG ADA7605. ALODI NED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED SUPPORT IAW DC10 SRM 513501 VOL 3. 2 L 7 3 4F A22WE 2000012200262 20000122 00262 WP 2000 1 22 SCNA99637 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1278 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR BOARD SUPPORT ANGLE AT STATION 1278 RBL 40 TO 65 WAS FOUND CORRODED. REMOVE D CORROSION IAW DC10 SRM 512101 VOL 2 FOUND TO BE OUT OF LIMITS IAW DC10 SRM 511001 VOL 2. REMOVED SUPPORT IAW DC10 SRM 513501 VOL 2. EXTRUSION MATERIAL ID IAW DC10 SRM 531401 VOL 3. FABRICATED SUPPORT IAW DAC DWG ADA3615. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513601 VOL 2. 2 L 7 3 4F A22WE 2000012200263 20000122 00263 WP 2000 1 22 SCNA99638 1 19991231 A 5311 FRAME DOUG DC10 DC1015 3022118 WP BS 959 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FRAME IN THE FORWARD PIT AT STATION 959 LGR 48R WAS FOUND CORRODED. REMOVED LGR 4 8R FROM STATION 919 TO 979 PER DC10 SRM 533301 VOL 2 AND 513501 VOL 2. FABRICATED REPAIR SECTION PER DC10 SRM 513501 VO L 2. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 533301 VOL 2 AND 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200264 20000122 00264 WP 2000 1 22 SCNA99639 1 19991231 A 5311 FRAME DOUG DC10 DC1015 3022118 WP BS 979 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FRAME IN THE FORWARD PIT AT STATION 979 LGR 49L TO 49R WAS FOUND CORRODED. REMOVE D SECTION OF FRAME AND FABRICATED NEW FRAME IAW DAC DWG ADA0070. FABRICATED NEW SPLICE IAW DC10 SRM 533000 VOL 1. ALOD INED AND PRIMED IAW DC10 SRM 512101 VOL 2 AND INSTALLED IAW DC10 SRM 513501 VOL 2 AND 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200265 20000122 00265 WP 2000 1 22 SCNA99640 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 438 - 450 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 438 TO 450 LBL 27 WAS FOUND CORRODED. REMOVED SEAT TRACK FA BRICATED SPLICE HAT AND PLATE IAW DC10 SRM 537000 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED SEAT TRACK IAW DC10 SRM 537000 VOL 1. 2 L 7 3 4F A22WE 2000012200266 20000122 00266 WP 2000 1 22 SCNA99641 1 19991231 A 3150 AURAL WARNING DOUG DC10 DC1015 3022118 WP COCKPIT FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, CABIN ALTITUDE PRESSURE WARNING SWITCH WARNING HORN FAILED TO SOUND WHEN CABIN ALTITUD E AND MASTER WARNING LIGHTS ILLUMINATED. WIRE RING OUT CHECKED GOOD IAW DC10 WDM 213303. REMOVED AND REPLACED AURAL WA RNING UNIT IAW DC10 MM 315102. OPS CHECK CABIN ALTITUDE PRESSURE WARNING HORN GOOD IAW DC10 MM 213303. 2 L 7 3 4F A22WE 2000012200267 20000122 00267 WP 2000 1 22 SCNA99642 1 19991231 A 5320 SHEAR TIE DOUG DC10 DC1015 3022118 WP BS 635 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SHEAR TIE IN THE FORWARD PIT AT STATION 635 LGR 43R WAS FOUND CRACKED. REMOVED SH EAR TIE IAW DC10 SRM 513501 VOL 2. DYE PENETRATED SHEAR TIE AND NO CRACKS FOUND. ALODINED AND PRIMED IAW 512101 VOL 2. REINSTALLED SHEAR TIE IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200268 20000122 00268 WP 2000 1 22 SCNA99643 1 19991231 A 5320 STIFFENER DOUG DC10 DC1015 3022118 WP FUSELAGE CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, TWO STIFFENERS WERE FOUND CRACKED IN THE RT MLG WHEEL WELL AT STATION XCW118 IN THE AF T PORTION OF THE WHEEL WELL. MATERIAL ID HEAT TREAT AND FABRICATE IAW DAC DWG ANB7203. ALODINED AND PRIMED IAW DC10 SR M 512101 VOL 2. LOCATED AND DRILLED IAW DAC DWG ANB7203 AND DC10 SRM 513101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2 AND 513502 VOL 2. 2 L 7 3 4F A22WE 2000012200269 20000122 00269 WP 2000 1 22 SCNA99644 1 19991231 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 421 BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK THE FLOOR SUPPORT AT STATION 421 LBL 10 WAS FOUND BROKEN OFF. REMOVED SUPPORT MATERIAL ID AND FABRICATED SUPPORT IAW DAC DWG ACA3763. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200270 20000122 00270 WP 2000 1 22 SCNA99645 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 450 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK FLANGE AT STATION 450 LBL 7 WAS FOUND CRACKED. FABRICATED FILLER AND T WO STRAPS IAW DC10 SRM 537000 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2.. INSTALLED FILLER AND STRAPS IAW D C10 SRM 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200271 20000122 00271 WP 2000 1 22 SCNA99646 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 495 GOUGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 495 RBL 28 WAS FOUND GOUGED ON THE OUTBOARD FLANGE. REMOVED TRACK SECTION IAW DC10 SRM 537000 VOL 1. FABRICATED TRACK SPLICE HAT AND PLATE IAW DC10 SRM 517000 VOL 1. ALODINED AN D PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED TRACK SPLICE HAT AND PLATE IAW DC10 SRM 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200272 20000122 00272 WP 2000 1 22 SCNA99647 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 495 GOUGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 495 LBL 8 WAS FOUND TO HAVE GOUGES AND SCRATCHES. REMOVED S EAT TRACK SECTION IAW DC10 SRM 513301 VOL 2. FABRICATED TRACK SPLICE HAT AND SPLICE PLATE IAW DC10 SRM 537000 VOL 1. A LODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED SEAT TRACK SECTION IAW DC10 SRM 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200273 20000122 00273 WP 2000 1 22 SCNA99648 1 19991231 A 5320 ANGLE DOUG DC10 DC1015 3022118 WP BS 1977 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE RT SUPPORT ANGLE CUSP AT STATION 1977 WAS FOUND CRACKED. REMOVED SUPPORT ANGLE FR OM STATION 1977 RT IAW DC10 SRM 513301 AND 513501. MATERIAL ID IAW DC10 SRM 531001.. FABRICATED BRACKET IAW DC10 SRM 5 31601. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. 2 L 7 3 4F A22WE 2000012200274 20000122 00274 WP 2000 1 22 SCNA99649 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1986 WORN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STATION 1986 RBL 2 TO 18 WAS FOUND TO HAVE ELONGATED HOLES AND FO RWARD LIP OF THE LOWER SIDE ON THE GROUND DOWN. REMOVED PANEL SUPPORT STATION 1986 RBL 2 MATERIAL ID PER DC10 SRM 53160 1 VOL 3. FABRICATED FLOOR SUPPORT IAW DC10 DAC DWG AGA7090. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200275 20000122 00275 WP 2000 1 22 SCNA99650 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1986 WORN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT AT STATION 1986 LBL 2 TO 18 HAS ELONGATED HOLES ON THE FORWARD LOWER SIDE OF THE LIP GROUND DOWN. MATERIAL ID AND FABRICATION FOR FLOOR SUPPORT IAW DC10 SRM 531600 VOL 3. ALODINED AND PR IMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 518501 VOL 2. 2 L 7 3 4F A22WE 2000012200276 20000122 00276 WP 2000 1 22 SCNA99651 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1964 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT VERTICAL FLANGE AT STATION 1964 LBL 2 WAS FOUND CRACKED. REMOVED FL OOR SUPPORT MATERIAL ID AND FABRICATED IAW DAC DWG AGA7091. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED I AW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200277 20000122 00277 WP 2000 1 22 SCNA99652 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1902 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT VERTICAL LEG AT STATION 1902 LBL 12 WAS FOUND CRACKED. REMOVED FLOO R SUPPORT MATERIAL ID FOR FLOOR SUPPORT. FABRICATED FLOOR SUPPORT IAW DAC DWG AGA7090. ALODINED AND PRIMED IAW DC10 SR M 512101 VOL 2 AND INSTALLED IAW DC10 SRM 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200278 20000122 00278 WP 2000 1 22 SCNA99653 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1853 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FLOOR SUPPORT VERTICAL FLANGE AT STATION 1853 LBL 75 WAS FOUND CRACKED. MATERIAL ID AND FABRICATION OF FLOOR SUPPORT IAW DAC DWG AGA3814. ALODINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513501 VOL 2. 2 L 7 3 4F A22WE 2000012200279 20000122 00279 WP 2000 1 22 SCNA99654 1 19991231 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 857 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE SEAT TRACK AT STATION 857 RBL 28 WAS FOUND GOUGED BEYOND LIMITS. REMOVED SEAT TRA CK SECTION IAW DC10 SRM 513101 VOL 2. FABRICATED SEAT TRACK HAT SPLICE AND SPLICE PLATE IAW DC10 SRM 537000 VOL 1. ALO DINED AND PRIMED IAW DC10 SRM 512101 VOL 2. INSTALLED SEAT TRACK IAW DC10 SRM 513101 VOL 2. 2 L 7 3 4F A22WE 2000012200280 20000122 00280 WP 2000 1 22 SCNA99655 1 19991231 A 5320 INTERCOSTAL DOUG DC10 DC1015 3022118 WP BS 1904 - 1921 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE INTERCOSTAL AT STATION 1904 TO 1921 LBL 6 WAS FOUND TO HAVE A CRACK ON TOP. REMVO ED CRACKED INTERCOSTAL FABRICATED IAW DAC DWG AGA7751. HEAT TREATED LOCATED DRILLED DEBURRED ALODINED AND PRIMED IAW DC 10 SRM 512101 AND INSTALLED IAW DC10 SRM 513301 VOL 2. 2 L 7 3 4F A22WE 2000012200281 20000122 00281 WP 2000 1 22 SCNA99656 1 19991231 A 3350 EMBS1392 BATTERY PACK DOUG DC10 DC1015 3022118 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE OVERWING EMERGENCY POWER SUPPLY FAILED FROM THE COCKPIT TEST PANEL. REMOVED AND R EPLACED EMERGENCY BATTERY SUPPLY PACK AT OVERWING STATION IAW DC10 MM 335101. BATTERY PACK TESTS GOOD IAW DC10 MM 33510 1. 2 L 7 3 4F A22WE 2000012200282 20000122 00282 WP 2000 1 22 SCNA99657 1 19991231 A 3520 O2 SYSTEM DOUG DC10 DC1015 3022118 WP CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE AFT LEFT LAVATORY OXYGEN MASKS DID NOT DROP DURING TEST. TS AND CONNECTED WIRES F OR AFT LEFT LAV E OXYGEN CONTROL WIRING AT S3 824 TERMINAL STRIP IAW DC10 MM 223000 AND DC10 WD 352201. OPERATIONALLY C HECKS GOOD IAW DC10 MM 352101. 2 L 7 3 4F A22WE 2000012200283 20000122 00283 WP 2000 1 22 SCNA99658 1 19991231 A 3510 O2 SYSTEM DOUG DC10 DC1015 3022118 WP COCKPIT FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE OVERWING LEFT ATTENDANT OXYGEN MASK DID NOT OPEN DURING TEST. RESET LATCHING MECH ANISM IAW DC10 MM 352000. PERFORMED SUCCESSFUL OPERATIONAL CHECK IAW DC10 MM 352000. 2 L 7 3 4F A22WE 2000012200284 20000122 00284 WP 2000 1 22 SCNA99659 1 19991231 A 3520 O2 SYSTEM DOUG DC10 DC1015 3022118 WP ROW 13 FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, ROW 13 CENTER OXYGEN MASK DID NOT OPEN DURING TEST. RESET LATCHING MECHANISM IAW DC10 MM 352000. PERFORMED SUCCESSFUL OPERATIONAL CHECK IAW DC10 MM 352000. 2 L 7 3 4F A22WE 2000012200285 20000122 00285 WP 2000 1 22 SCNA99660 1 19991231 A 3520 O2 MASK DOUG DC10 DC1015 3022118 WP CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE L2 AND R2 ATTENDANT PANEL OXYGEN MASKS DID NOT DEPLOY DURING TEST. TS AND REPLACE D RELEASE SWITCH. ADJUSTED SPRING HEIGHT ON DOOR PER DC10 MM 352101. REINSTALLED DOOR. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 2000012200286 20000122 00286 WP 2000 1 22 SCNA99661 1 19991231 A 3520 O2 MASK DOUG DC10 DC1015 3022118 WP LAVATORY FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE LAV A AND LAV B OXYGEN MASKS DID NOT DEPLOY DURING TEST. TS AND CONNECTED WIRES F OR LAVS A AND B IAW DC10 MM 203000 AND IAW DC10 WD 352201. OPERATIONALLY CHECKS GOOD IAW DC10 MM 352101. 2 L 7 3 4F A22WE 2000012200287 20000122 00287 WP 2000 1 22 SCNA99662 1 19991231 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 979 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD PIT STATION 979 FLOOR SUPPORT AT LBL 50 WAS FOUND CRACKED. REMOVED DAMAGE D FLOOR SUPPORT IAW DC10 SRM 513501 VOL 2. FABRICATED FLOOR SUPPORT IAW DAC DWG ADA3626. ALODINED AND PRIMED FLOOR SUP PORT IAW DC10 SRM 512101 VOL 2. INSTALLED IAW DC10 SRM 513301. 2 L 7 3 4F A22WE 2000012200302 20000122 00302 NM 2000 1 22 AALA991298 1 19990829 A 3340 30083713 LIGHT GRIMES BOEING 727 727223 1384074 NM FUSELAGE FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 885AA 132 21524 CCS - FLT 2142 - AFTER TAKEOFF CCS-MIA, FUMES WITH SMELL OF BURNING RUBBER NOTED IN FORWARD AREA OF COACH CABIN. NO VIS IBLE SMOKE DETECTED. AIRCRAFT RETURNED TO CCS AND LANDED WITHOUT INCIDENT. SMELL TRACKED TO UPPER FUSELAGE ANTI-COLLIS IONS STROBE LIGHT. UPPER FUSELAGE ANTI-COLLISION STROBE LIGHT PLACARDED INOPERATIVE PER MEL. REPLACED UPPER FUSELAGE A NTI-COLLISION STROBE LIGHT AT IAH ON 8/30/99. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200303 20000122 00303 NM 2000 1 22 AALA991629 1 19991029 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM STAIRWELL INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 874AA 21386 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT STAIRWELL INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMLBY IN AFT STAIRWELL. YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200304 20000122 00304 NM 2000 1 22 AALA991640 1 19991029 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 712AA 22468 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR OVERHEAD EM ERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200305 20000122 00305 NM 2000 1 22 AALA991646 1 19991031 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 884AA 21523 DFW - DURING OVERNIGHT MAINTENANCE, SEAT 6D AND 8D EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200306 20000122 00306 NM 2000 1 22 AALA991657 1 19991102 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 21387 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LI GHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200307 20000122 00307 NM 2000 1 22 AALA991688 1 19991110 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 TUL - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EME RGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200308 20000122 00308 NM 2000 1 22 AALA991707 1 19991113 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 893AA 22009 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP CLOSE TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200309 20000122 00309 NM 2000 1 22 AALA991853 1 19991205 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 874AA 21386 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH FLOOR LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXI T PATH FLOOR LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200310 20000122 00310 NM 2000 1 22 AALA991773 1 19991123 A 3350 1000679 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844AA 20985 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT FORWARD EMERGENCY EX IT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200311 20000122 00311 NM 2000 1 22 AALA991720 1 19991115 A 3350 1000679 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 710AA 22467 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT GALLEY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT AFT G ALLEY DOOR OVERHEAD EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200312 20000122 00312 NM 2000 1 22 AALA991718 1 19991115 A 3350 CONNECTOR BOEING 727 727223 1384074 NM ROW 22-30 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6835 20188 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT FROM ROW 22 TO 30 INOPERATIVE. REPLACED CONNECTORS ON EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 22 AND 30. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000012200313 20000122 00313 NM 2000 1 22 AALA991837 1 19991201 A 3350 95246508 RELAY LEACH BOEING 727 727233 138408A NM CABIN FAILED A AALA O OTHER O OTHER CR CRUISE 1 SW 07 866AA 21371 TPA - FLT 811 - DURING FLIGHT WITH EMERGENCY EXIT LIGHT SWITCH IN ARM POSITION EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINA TE. REPLACED EMERGENCY EXIT LIGHT RELAY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F RT A3WE 2000012200314 20000122 00314 EU 2000 1 22 AALA991747 1 19991120 A 3397 WIRE GRIMES FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1413A 11376 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERHEAD CEILING EXIT LIGHT HAS BROKEN WIRES. REPAIRED EMEREGNCY OVERHEAD CEILING EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200315 20000122 00315 EU 2000 1 22 AALA991719 1 19991115 A 3350 502A LIGHT KORRY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1417D 11396 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD EMERGENCY EXIT LIGHT BROKEN. REPLACED RIGHT FORWARD EMERGENCY EXIT LI GHT.. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200316 20000122 00316 EU 2000 1 22 AALA991851 1 19991205 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1451N 11460 DFW - DURING OVERNIGHT MAINTENANCE, MAIN CABIN EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPAIRED WIRE SPLICE ON FLOOR STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200317 20000122 00317 EU 2000 1 22 AALA991842 1 19991202 A 2560 P2070001213 FLASHLIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1414D 11377 ATL - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY FL ASHLIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200318 20000122 00318 EU 2000 1 22 AALA991616 1 19991027 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1450A 11459 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FORWARD GALLEY INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200319 20000122 00319 EU 2000 1 22 AALA991306 1 19990831 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU E/E BAY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1403M 11354 DFW - DURING OVERNIGHT MAINTENANCE, ELECTRICAL EMERGENCY LIGHT DC BUS MESSAGE ILLUMINATED ON MULTI-FUNCTION DISPLAY UNIT . TIGHTENED LOOSE WIRE TO THE DC BUS RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200320 20000122 00320 EU 2000 1 22 AALA991418 1 19990920 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1444N 11447 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE FROM ROW 13 TO 15. REPLACED WIRING T O EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS FROM ROW 13 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200321 20000122 00321 EU 2000 1 22 AALA991417 1 19990920 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1410E 11368 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT FORWARD GALLEY HAS ONE LIGHT OUT. REPLA CED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000012200322 20000122 00322 WP 2000 1 22 AALA991886 1 19991211 A 3230 59104475071 NLG DOUG DC9 DC982 3022082 WP NOSE LACK OF LUBE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 33414 49325 LGA - FLT 693 - AFTER TAKEOFF RED NOSE GEAR LIGHT REMAINED ILLUMINATED. LOUD AIR NOISE. RECYCLED GEAR NO HELP. RETURN ED AND LANDED LGA WITHOUT INCIDENT. SERVICED NOSE STRUT AND ACCOMPLISHED GEAR SWING SEVERAL TIMES. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000012200323 20000122 00323 WP 2000 1 22 AALA991880 1 19991209 A 5230 BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 279AA 49295 TUL - FOUND CORROSION ON AFT CARGO DOOR BEAM. INSTALLED DOUBLER PER ESO80559 12/7/99 AND AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 2000012200324 20000122 00324 WP 2000 1 22 AALA991828 1 19991130 A 3320 BV04055N0156 LAMP HOLDER BRUCE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA O OTHER A FLAME/FIRE NR NOT REPORTED 1 SW 07 7506 49800 RDU - FLT 2146 - AT THE GATE, SMOEK AND FLAME GENERATED FROM ROW 3EF PASSENGER SERVICE UNIT. AIRPORT FIRE DEPARTMENT AR RIVED AND PUT FIRE OUT WITH WATER FROM FIRE HOSE. NO WATER DAMAGED NOTED. FORWARD END OF SECOND FLORESCENT LIGHT IN FI RST CLASS CABIN ROW 3EF HAS BEEN IDENTIFIED AS THE PROBABLE SOURCE OF THE FIRE. (M) 2 L 7 2 4F A6WE 2000012200325 20000122 00325 WP 2000 1 22 AALA991839 1 19991202 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP TAIL CONE BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 592AA 53255 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT TAIL CONE RELEASE FLOOR LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT T AIL CONE RELEASE FLOOR LIGHT CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 2000012200326 20000122 00326 WP 2000 1 22 AALA991850 1 19991206 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 586AA 53249 PHX - DURING OVERNIGHT MAINTENANCE, RIGHT AFT BOTTOM OVERWING DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED WIRES ON R IGHT AFT BOTTOM OVERWING DOOR EMERGENCY EXIT SIGN CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000012200327 20000122 00327 WP 2000 1 22 AALA991841 1 19991202 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 573AA 53092 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS NEAR FORWARD ENTRY INOPERATIVE. SECURED EMERGENCY EXIT FLOORPATH LIGHT CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000012200328 20000122 00328 WP 2000 1 22 AALA991843 1 19991202 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7514A 49891 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT ROW 22 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR P ATH LIGHT STRIP ROW 22. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000012200329 20000122 00329 WP 2000 1 22 AALA991844 1 19991202 A 3350 BULB DOUG DC9 DC982 3022082 WP CABIN WRONG PART A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 410AA 49321 ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT SEAT 5DF INOPERATIVE ON DIM. WRONG BULBS INSTALLED. REPL ACED BULBS. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 2000012200330 20000122 00330 WP 2000 1 22 AALA996041 1 19991118 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 1/2 DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 880RA 53186 SNA - E-LIGHTS AT 1/2 INOPERATIVE. FOUND A OPEN AT PLUG CONNECTOR, RE-PLUGGED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2000012200331 20000122 00331 NM 2000 1 22 AALA996044 1 19991124 A 3350 08163074126 LIGHT DOUG MD90 MD9030 3023690 NM ROW 28D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 905RA 53573 RNO - ROW 28D EMERGENCY PATH LIGHT INOPERATIVE TRACK P/N 08163-0741-26. REPLACED LIGHT SOCKET. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2000012200332 20000122 00332 WP 2000 1 22 AALA996046 1 19991122 A 3350 60030451 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 751RA 49779 RNO - EMERGENCY EXIT LIGHTS ON RIGHT SIDE BY EMERGENCY EXIT SIGNS OUT. REMOVED AND REPLACED EMERGENCY LIGHT PACK AT AFT RIGHT EXIT ROW. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2000012200333 20000122 00333 WP 2000 1 22 AALA996043 1 19991121 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC983 3022083 WP SEAT 2 D/F DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 880RA 53186 SJC - SEAT E-LIGHTS DO NOT STAY LIGHTED FORWARD MOST BIN (SEAT 2 D, F) NEED P/N 41B004AD07G3. CHARGED BATTERY PACKS, OP S CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2000012200334 20000122 00334 WP 2000 1 22 AALA996042 1 19991119 A 3350 41B004AD0763 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 882RA 49949 SJC - BATTERY PACK AT RIGHT AFT 'E' EXIT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FROM AFT AUX CHARGER PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2000012200335 20000122 00335 2000 1 22 AALA996047 4 19990623 A 2565 D29982107 PIN DOUG DC9 DC982 3022082 WP EVAC SLIDE LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 821RA 49931 OKC - NR 8000-0019, R-1 DOOR EMERGENCY SLIDE DEPLOY PIN LOOSE. REMOVED AND REPLACED R-1 DOOR EMERGENCY ESCAPE SLIDE IAW MD80 MM 25-60-00. (M) 2 L 7 2 4F A6WE 2000012200336 20000122 00336 NE 2000 1 22 AALA996045 2 19991130 A 7200 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE RIGHT MALFUNCTIONED A AALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 SW 07 904RA 53570 SNA - FLT 2827 - SJC-SNA - STARTING DESCENT FROM FL370, FELT SEVERAL JOLTS AS THE THROTTLES CAME BACK (COMPRESSOR STALLS ). ALSO, FLIGHT ATTENDANTS REPORTED LOUD BANGS HEARD FROM THE RIGHT ENGINE. ALL ENGINE INSTRUMENTS INDICATED NORMAL. R EMOVED ENGINE P/N V2528-D5, S/N V20120. INSTALLED ENGINE P/N V2528-D5 S/N V20040. AIRCRAFT RETURNS TO SERVICE. (M) 2 L 7 2 4F 4 F RT A6WE E40NE 2000012200337 20000122 00337 NM 2000 1 22 P2EA99310 1 19991102 A 5313 STRINGER BOEING 737 737297 1384480 NM BS 985.5 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - DURING C-CHECK, SKIN AT BS 980, STRINGER 27R BULGING. REPAIRED STRINGER 27R FROM BS 986.5 TO 969 IAW SRM 53-10-03 FIG 1. (M) 2 L 7 2 4F A16WE 2000012200338 20000122 00338 WP 2000 1 22 USAA990494 1 19990604 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 48114 PIT - DURING Q-4 CHECK, FOUND 2.25 INCH CRACK AT ATTACH ANGLE AT STATION 965 BETWEEN 15R AND 16R. DEFECTIVE PART REPLAC ED WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F A6WE 2000012200339 20000122 00339 WP 2000 1 22 USAA990189 1 19990227 A 5320 CLIP DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK IN SKIN CLIP STATION 945 BETWEEN LONGERON 15R AND 14R. REPLACED SKIN CLIP, NEW PART NR 1197928. (M) 2 L 7 2 4F A6WE 2000012200340 20000122 00340 WP 2000 1 22 USAA990163 1 19990227 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK LONGERON 15L AT HI-LOCK AT STATION 945. SPLICED IN SECTION OF LONGERON PER SRM 53-11-3. (M) 2 L 7 2 4F A6WE 2000012200341 20000122 00341 WP 2000 1 22 USAA990162 1 19990227 A 5313 27779224 LONGERON DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937VJ 47737 48117 PIT - DURING Q-1 CHECK, FOUND .5 INCH LONGERON CRACK AT HI-LOCK AT LONGERON 17L STATION 945. SPLICED IN SECTION OF LONG ERON PER SRM 53-11-3. (M) 2 L 7 2 4F A6WE 2000012200342 20000122 00342 NM 2000 1 22 2000ZZZM67 1 19991223 A 2752 MOTOR BOEING 727 727227 1384078 NM HYD SYSTEM LEAKING A AMTA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 767AT 22001 FLL-IND - FLT 476 - DURING CRUISE, THE 'A' HYDRAULIC SYSTEM QTY SLOWLY DECREASED, RAN AOM PROCEDURE, WAS UNABLE TO ISOLA TE LEAK. LANDING GEAR WAS EXTENDED USING MANUAL PROCEDURES, LANDED AT IND WITHOUT FURTHER INCIDENT. REMOVED AND REPLAC ED LEFT FLAP POWER UNIT HYDRAULIC MOTOR IAW MM 27-51-62. ADDITIONAL ITEMS WERE REPLACED, NR 1 AND NR 2 ENGINE HYDRAULIC PUMPS, CASE DRAIN FILTERS AND SYSTEM 'A' FILTERS, CHECKED FOR LEAKS AND FOUND SERVICEABLE. (M) 2 L 7 3 4F A3WE 2000012200343 20000122 00343 NM 2000 1 22 2000ZZZM68 1 19991026 A 2760 V3L2228 SWITCH BOEING 727 727208 138407W NM SPOILER MALFUNCTIONED A AMTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 780AT 22295 JFK - AIRCRAFT ABORTED TAKEOFF DUE TO A TAKEOFF WARNING HORN SOUNDING ON ROLL, A/C RETURNED TO RAMP. REMOVED AND REPLAC ED FLIGHT SPOILER HANDLE SWITCH, IAW MM 31-26-26, OPS CHECK NORMAL. (M) 2 L 7 3 4F RT A3WE 2000012200344 20000122 00344 NE 2000 1 22 2000ZZZM69 2 19991203 A 7530 LINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE LOOSE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 515AT 27598 31396 MDW-PHX - FLT 577 - DURING CRUISE, THE RIGHT ENGINE WAS SHUTDOWN DUE TO LOW ENGINE PARAMETERS. CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. FOUND THE P-1 AIR TUBE CHECK VALVE TO BE LOOSE AT FITTING. INSPECTED SAME FOR FRETTING AND CONTAMINATION, RESECURED FITTING, ENGINE RUN UP CHECKED OK. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 2000012200345 20000122 00345 2000 1 22 BJNA991201 4 19991211 A 3417 ADC BOEING 737 737282 13844AT NM COCKPIT MALFUNCTIONED A BJNA O OTHER J WARNING INDICATION CR CRUISE 1 WP 11 789TM 23046 DURING CRUISE, SEVERAL ABNORMAL INDICATIONS OCCURRED, AS FOLLOWS, NR 1 ALTIMETER WITH OFF FLAGS AND SPINNING, MACH TRIM FAIL LIGHT, NR 1 AIRSPEED WITH FLAGS WITH BARBER POLE REDUCED TO 260 KNOTS, GROUND PROX INOPERATIVE, EPR INOPERATIVE, AN D PDC WENT INTO TEST MODE. RE-RACKED AIR DATA COMPUTER PER 34-12-0. OPERATION OF EFFECTED SYSTEM CHECK OK. (M) 2 L 7 2 4F RT A16WE 2000012200346 20000122 00346 NM 2000 1 22 BJNA991202 1 19991230 A 2910 106056340 LINE BOEING 737 737282 13844AT NM HYD SYSTEM CHAFED A BJNA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 11 233TM 23043 AFTER DEPARTING IND, PILOT NOTICED LOW 'A' SYSTEM HYDRAULIC QTY. SOON AFTER LOW PRESSURE OF NR 1 HYD PUMP 'A' SYSTEM MA STER CAUTION WARNING FOLLOWED BY NR 2 HYD PUMP 'A' SYSTEM MASTER CAUTION WARNING.. CREW IMPLEMENTED QHR PROCEDURE AND L ANDED AT STL. UPON INSPECTION ON GROUND, NR 1 ENGINE 'A' PUMP PRESSURE LINE WAS EXCESSIVELY CHAFED. NR 1 ENGINE 'A' PU MP PRESSURE LINE WAS REPLACED. AIRCRAFT WAS REPOSITIONED TO EKO WITHOUT FURTHER PROBLEMS. (M) 2 L 7 2 4F RT A16WE 2000012200347 20000122 00347 EU 2000 1 22 C2XA99IA629 1 19991209 A 3350 3013017 POWER SUPPLY AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16450 510 EFD - DURING MAINTENANCE INSPECTION, THE CENTER AND AFT AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW ATR42-500 MM 33-51-21, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000012200348 20000122 00348 WP 2000 1 22 2000ZZZM70 1 19991021 A 3350 111397507 LENS GRIMES DOUG DC9 DC932 3022066 WP TAIL COMPART MISSING A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 930BB 47521 DURING THE ACCOMPLISHMENT OF B-CHECK CARD 0617, REQUIRING THE OPERATIONAL TEST AND INSPECTION OF THE EMERGENCY LIGHTS SY STEM, THE EMERGENCY LIGHT IN THE TAIL COMPARTMENT WAS WRITTEN UP AS HAVING A MISSING LENS. THE LENS COVER WAS REPLACED. THE LIGHT ASSEMBLY WAS OPERATIONALLY CHECKED OK IAW THE MCDONNELL DOUGLAS DC9 MM 33-53-0. (M) 2 L 7 2 4F A6WE 2000012200349 20000122 00349 WP 2000 1 22 2000ZZZM71 1 19991021 A 3350 1315 LAMP DOUG DC9 DC932 3022066 WP CABIN FAILED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 930BB 47521 DURING ACCOMPLISHMENT OF B-CHECK CARD 0617, REQUIRING THE OPERATIONAL TEST OF THE EMEREGNCY LIGHTING SYSTEM THE EMERGENC Y LIGHT AT THE L1 DOOR FAILED TO ILLUMINATE. THIS DISCREPANCY WAS TROUBLE SHOT TO A BURNED OUT LAMP. THE LAMP WAS REPL ACED AND OPERATIONAL CHECKED OK IAW MCDONNELL DOUGLAS DC0 MM REF 33-53-0. (M) 2 L 7 2 4F A6WE 2000012200350 20000122 00350 WP 2000 1 22 2000ZZZM72 1 19991021 A 3350 OL3071BPEGPL LAMP BRUCE 086861 DOUG DC9 DC932 3022066 WP SEAT 16 FAILED A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 930BB 47521 DURING THE ACCOMPLISHMENT OF B-CHECK CARD 0617, REQUIRING THE OPERATIONAL TEST OF THE EMERGENCY FLOOR PATH LIGHTING SYST EM THE EMERGENCY LIGHT AT SEAT POSITION 16 CDE FAILED TO ILLUMINATE. THIS DISCREPANCY WAS TROUBLE SHOT TO A BURNED OUT LAMP. THE LAMP WAS REPLACED AND OPERATIONAL CHECK OK IAW MCDONNELL DOUGLAS DC0 MM REFERENCE 33-53-01. (M) 2 L 7 2 4F A6WE 2000012200351 20000122 00351 WP 2000 1 22 2000ZZZM73 1 19991021 A 3350 60030431 BATTERY GRIMES DOUG DC9 DC932 3022066 WP CABIN DIRTY A A4JA K NONE L NO TEST IN INSP/MAINT 1 SO 35 930BB 8821 47521 DURING THE ACCOMPLISHMENT OF B-CHECK CARD 0617, REQUIRING THE OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM THE EMERGEN CY LIGHTS IN THE FORWARD OVERHEAD CEILING PANEL FAILED TO ILLUMINATE. THIS DISCREPANCY WAS TROUBLE SHOT TO A BAD BATTER Y PACK CHARGER ASSEMBLY. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKED IAW MCDONNELL DOUGLAS DC9 MM REFERENCE 3 3-53-0. (M) 2 L 7 2 4F A6WE 2000012200352 20000122 00352 WP 2000 1 22 GAIA99230 1 19991203 A 2421 976J252 GENERATOR DOUG DC9 DC915F 3022037 WP NR 1 ENGINE FAILED A GAIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 07 562PC 47012 FLT 805 - DEN-SLC - AFTER DEPARTURE FROM DEN THE FLIGHT CREW NOTICED THE COCKPIT INSTRUMENTATION LIGHTING AND INDICATORS STARTED FLICKERING AND READING ERRATIC. THE A/C CROSSTIE LOCKOUT ILLUMINATED, NR 1 GENERATOR TRIPPED OFF LINE AND THE LEFT A/C BUS FAILED. THE APU WAS STARTED AND A/C POWER RESTORED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEN. A N UNEVENTFUL LANDING WAS MADE. INVESTIGATION FOUND THE NR 1 GENERATOR NOT PRODUCING VOLTAGE. THE CSD WAS DISCONNECTED AND THE GENERATOR WAS DEFERRED PER THE MEL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2000012200536 20000122 00536 NM 2000 1 22 UPS00231327 1 19990114 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 ROW 19 EMERGENCY LIGHT FAILED TEST. REPLACED BATTERY. CHECKS GOOD 2 L 7 3 4F A3WE 2000012200539 20000122 00539 NM 2000 1 22 UPS00231333 1 19990114 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 EMERGENCY LIGHT AREA LIGHT BY AFT LEFT LAV FAILED TEST. REPLACED BATTERY. CHECKS GOOD. 2 L 7 3 4F A3WE 2000012200540 20000122 00540 WP 2000 1 22 UPS00831317 1 19991229 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 STA 1680 AT RT CUSP LWR SURFACE, THE FRAME IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000012200541 20000122 00541 WP 2000 1 22 UPS00831318 1 19991228 A 5320 37799782 FITTING DOUG DC8 DC871F 302199D WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 759 STR 18R. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200542 20000122 00542 WP 2000 1 22 UPS00831319 1 19991228 A 5320 37540251 FITTING DOUG DC8 DC871F 302199D WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 STA 280 ABOVE STR 27R, THE BACK-UP FITTING FOR THE FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED, FA BRICATED AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200543 20000122 00543 WP 2000 1 22 UPS00831320 1 19991228 A 5320 47504232 FITTING DOUG DC8 DC871F 302199D WP BS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 902 STR 18L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4750423 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200544 20000122 00544 WP 2000 1 22 UPS00831323 1 19991228 A 5320 4750419501 FITTING DOUG DC8 DC871F 302199D WP BS 742 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 LONGERON 11L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 742. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012200546 20000122 00546 WP 2000 1 22 UPS00831331 1 19991228 A 5320 36410042N FITTING DOUG DC8 DC871F 302199D WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 STA 879 AT STR 24R, SUPPORT FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 364100 4 AND SRM 53-2-0 FIG 8. 2 L 7 4 4F RT 4A25 2000012200561 20000122 00561 WP 2000 1 22 AT9900924 1 19991226 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1145 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND A CRACK UNDER THE VENTRAL STAIR ACTUATOR ON THE FRAME AT B S 1145R. CUT OUT AND REMOVED CRACKED SECTION OF FRAME AND FABRICATED FRAME SPLICE AT BS 1145R IAW EO 99-1405, DC9 SRM 5 1-1 0-02, AND DC9 MM 52-63. 2 L 7 2 4F A6WE 2000012200571 20000122 00571 NM 2000 1 22 RAAA00B2002 1 19991231 A 3350 86210066 BATTERY INTVLV BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FLOOR EMERGENCY LIGHT WON'T TEST ROW 15. REPLACED BATTERY PACK. OPS OK 2 L 7 3 4F A3WE 2000012200572 20000122 00572 NM 2000 1 22 RAAAB2002 1 19991231 A 3350 86210066 BATTERY INTVLV BOEING 727 72722C 138400F NM ROW 15 DISCHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FLOOR EMERGENCY LIGHT WON'T TEST ROW 15. REPLACED BATTERY PACK. OPS OK. 2 L 7 3 4F A3WE 2000012200574 20000122 00574 NM 2000 1 22 RAAAB002003 1 19991231 A 3350 86210066 BATTERY INTVLV BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FLOOR EMERGENCY LIGHT WON'T TEST ROW 17. REPLACED BATTERY PACK. OPS OK. 2 L 7 3 4F A3WE 2000012200582 20000122 00582 WP 2000 1 22 TWAA0000914 1 19991202 A 5730 SKIN DOUG DC9 DC983 3022083 WP RT WING GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9626F 53596 THE RT WING LOWER SURFACE SKIN HAD 3 GOUGES JUST AFT OF OTBD TRACK FOR NUMBER 3 SLAT, CAUSED BY GROUND EQUIPMENT DAMAGE. LENGTHS OF GOUGES 5 IN, 4.5 INCH, AND 2 INCH. DEEPEST DEPTH 0.050. BLENDED GOUGES PER SRM 57-01, FIG 1 SHEET 3. ALO DINE AREA PER SRM 51-10-3, PARAGRAPH 30. EDDY CURRENT ACCOMP AND NO DEFECTS. AREAS ALSO COVERED BY ARA 16489 AND ARA 1 6488. CHECK-C 10-2-99 STL. 2 L 7 2 4F RT A6WE 2000012200617 20000122 00617 WP 2000 1 22 MWEA99961 1 19991229 A 5313 59203191 LONGERON DOUG DC9 DC932 3022066 WP BS 337 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 FORWARD CARGO PIT, LONGERON 29 LEFT, HAS MODERATE CORROSION AT STATION 337. MAINTENANCE FABRICATED AND INSTALLED NEW SE CTION OF LONGERON. 2 L 7 2 4F A6WE 2000012200618 20000122 00618 WP 2000 1 22 MWEA99962 1 19991213 A 5311 J0602385 FRAME DOUG DC9 DC932 3022066 WP EMERGENCY EXIT CHAFFING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 LEFT FORWARD OVERWING EXIT FRAME CHAFFING AT CENTER TOP WHERE DOOR LATCHES. MAINTENANCE FABRICATED AND INSTALLED DOUBLE R. 2 L 7 2 4F A6WE 2000012200619 20000122 00619 WP 2000 1 22 MWEA99963 1 19991214 A 5320 59100066 STRUCTURE DOUG DC9 DC932 3022066 WP BS 91 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 REMOVE TEMPORARY REPAIR STRAP AND FASTENER FROM DAMAGED HOLE AT XRS 91.000. MX REMOVED TEMPORARY REPAIR, THEN FABRICATE D AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000012200621 20000122 00621 WP 2000 1 22 MWEA99964 1 19991216 A 5320 991960315 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 897 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 CORROSION ON SHEARTIE AT STATION 897 ABOVE LONGERON 30. MX DRILLED AND INSTALLED SHEARTIE. 2 L 7 2 4F A6WE 2000012200622 20000122 00622 WP 2000 1 22 MWEA99965 1 19991223 A 5320 59203192 SPLICE DOUG DC9 DC932 3022066 WP BS 351 - 370 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 MODERATE CORROSION AROUND RIVETS IN CHANNEL OF LONGERON 30, STATION 351-370. MAINTENANCE FABRICATED AND INSTALLED NEW S PLICE. 2 L 7 2 4F A6WE 2000012200638 20000122 00638 NM 2000 1 22 EISA99238 1 19991018 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 1050 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND CORROSION ON FLOORBEAM T-CAP AT FS 1050 LBL 20 MAIN CABIN FLOOR STRUCT URE. REMOVED CORROSION AND MATERIAL LOSS OUT OF LIMITS. SRM 53-10-1, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 A ND SRM 51-30-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200639 20000122 00639 NM 2000 1 22 EISA99237 1 19991112 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED A CRACK IN FUSELAGE EXTERNAL SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUT-OUT. TRIMMED DAMAGED AREA PER SB 727-53-0198. FABRICATED AND INSTALLED DOUBLER PER SB 727-53-0198. TT: 65,345 :17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200640 20000122 00640 NM 2000 1 22 EISA99236 1 19991104 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED A CRACK IN FUSELAGE SKIN AT UPPER HINGE CUT-OUT AT FORWARD ENTRY DO OR. TRIMMED DAMAGED AREA PER SB 727-53-0198. FABRICATED AND INSTALLED DOUBLER PER SB 727-53-0198. TT: 65,345:17 HOUR S. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200641 20000122 00641 NM 2000 1 22 EISA99235 1 19991104 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 950-1030 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON MAIN CABIN SEAT TRACK AT LBL 45 FROM BS 950 AFT TO BS 1030. REMOVED CORROSION AND MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED SEAT TRACK AND REPLACED WITH NEW SECT ION FABRICATED PER SAMPLE FROM BS 1130 PER SRM 51-30-2 AND SRM 51-10-1. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200642 20000122 00642 NM 2000 1 22 EISA99234 1 19991104 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 1166-1183 GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION OF FLOOR SUPPORT IN MAIN CABIN BETWEEN BS 1166 AND AND BS 1183 LBL 19. REMOVED DAMAGED AREA PER SRM 51-10-6, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-50-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200643 20000122 00643 NM 2000 1 22 EISA99233 1 19991104 A 5754 SKIN BOEING 727 727225 1384077 NM LE FLAP GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED LEFT OUTBOARD FOREFLAP WS 417 GOUGED UNDER LEADING EDGE. REMOVED D AMAGED AREA PER SRM 51-10-1, FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4. TT: 65,345:17 HOURS. TC: 43,816. ( X) 2 L 7 3 4F A3WE 2000012200644 20000122 00644 NM 2000 1 22 EISA99232 1 19991104 A 5754 SKIN BOEING 727 727225 1384077 NM LE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED AREA OF DELAMINATION ON RIGHT WING OUTBOARD FOREFLAP, INBOARD TRAIL ING EDGE. REPAIRED TRAILING EDGE WITH FIBERGLASS REPAIR PER SRM 51-40-6. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200645 20000122 00645 NM 2000 1 22 EISA99231 1 19991021 A 5320 ANGLE BOEING 727 727225 1384077 NM BS 1148 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK INSPECTION WORK CARD REVEALED CORROSION ON FLOORBEAM ANGLE IN AFT BAGGAGE COMPARTMENT AT FS 1148, LBL 8 TO RBL 8. REMOVED CORROSION IAW SRM 51-10-6 OUT OF LIMITS. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE IAW SRM 53-10-8. INSTALLED REPAIR IAW SRM 53-10-8 AND SRM 51-30-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200646 20000122 00646 NM 2000 1 22 EISA99230 1 19991110 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 608-740 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND CORROSION ON MAIN CABIN SEAT TRACK AT BS 680 TO BS 740, RBL 45. REMOV ED CORROSION PER SRM 51-10-6. MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED TRACK SECTION AND FABRICATED NEW SE CTION PER SAMPLE. INSTALLED NEW SECTION FROM BS 680 TO BS 740 PER SRM 51-10-1 AND SRM 51-30-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200647 20000122 00647 NM 2000 1 22 EISA99229 1 19991019 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 480 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND CORROSION ON FLOORBEAM UPPER T-CAP AT BS 480, BL ZERO AND RBL 120. RE MOVED CORROSION PER SRM 51-10-6, MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGED AREA PER SRM 53-10-8. FAB RICATED AND INSTALLED T-CAP REPAIR PER SRM 53-10-8. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200648 20000122 00648 NM 2000 1 22 EISA99228 1 19991027 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 950C CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON LOWER SURFACE OF MAIN CABIN FLOORBEAM AT BS 950C LBL 2 5. REMOVED CORROSION AND MATERIAL LOSS OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA. FABRICATED REPAIR ANGLES AND FILLER PER SRM 53-10-8. TREATED AND PRIMED PER SRM 51-10-2 AND MM 51-20-2. INSTALLED REPAIR PER SRM 53-10-8 AND SRM 51 -30-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200649 20000122 00649 NM 2000 1 22 EISA99227 1 19991027 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 950 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON STR 24L AT BS 950. REMOVED CORROSION AND MATERIAL LOS S OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 AND SRM 51-30-2. TT: 65,345:1 7 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200650 20000122 00650 NM 2000 1 22 EISA99226 1 19991111 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 1030 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON BS 1030 FLOORBEAM T-CAP AT BL ZERO. REMOVED CORROSION AND MATERIAL LOSS OF LIMITS PER SRM 53-10-3. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200651 20000122 00651 NM 2000 1 22 EISA99224 1 19991112 A 5753 SKIN BOEING 727 727225 1384077 NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED DELAMINATION OF LEFT OUTBOARD AFT FLAP TRAILING EDGE AT INBOARD COR NER. REPAIRED DELAMINATION WITH FIBERGLASS AND POTTING REPAIR PER SRM 57-50-4 AND SRM 51-40-6. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200653 20000122 00653 NM 2000 1 22 EISA99222 1 19991112 A 2721 SKIN BOEING 727 727225 1384077 NM RUDDER TAB DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED AREA OF DELAMINATION ON LOWER RUDDER TAB, UPPER TRAILING EDGE, LEFT CENTER AND UPPER LEFT SIDE AND LOWER SURFACE. ACCOMPLISHED HONEYCOMB REPAIR TO ALL AREAS PER SRM 51-40-6. TT: 65,3 45:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012200654 20000122 00654 NM 2000 1 22 EISA99221 1 19991116 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 1130 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHEMNT OF A ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON FLOORBEAM UPPER AND LOWER CHORDS AT BS 1130 LBL TO R BL 16 MAIN CABIN. AFTER CORROSION REMOVAL, MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED UPPER AND LOWER CHORDS PER SRM 51-30-2 AND FLIGHT VEHICLES CONSULTING EA DRAWING 53-99537-1. TT: 65,345:17 HOURS. TC: 43,81 6. (X) 2 L 7 3 4F A3WE 2000012200655 20000122 00655 NM 2000 1 22 2000ZZZX214 1 19990930 A 7910 693905 OIL CAP DOUG DC10 DC1040F 3023507 NM NR 1 ENGINE MISSING A CLCA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 19 140WE 46920 KMIA/SEQU - FLT 85 AT 17:45 Z - DISCREPANCY AFTER TAKEOFF FROM MIA, EXPERIENCED LOSS OF OIL QUANTITY, ENGINE NR 1 FROM 1 1 GALLONS TO SIX GALLONS WHERE IT THEN STABILIZED. RETURNED TO MIA. NO FUEL DUMPED, LANDING AT 389,000 POUNDS, LANDIN G UNEVENTFUL. FOUND OIL CAP NOT INSTALLED ON OIL TANK. INSTALLED OIL CAP AND SERVICED TANK TO FULL. RELEASED AIRCRAFT FOR REVENUE SERVICE. 2 L 7 3 4F RT A22WE 2000012200656 20000122 00656 NM 2000 1 22 2000ZZZX215 1 19991001 A 2910 AS11504K0232 LINE BOEING 757 75723APF 1384966 NM LT MLG RUPTURED A CLCA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 572CA 24868 KMIA/KSAL - FLT 067 AT 21:30 Z - LEFT HYDRAULIC QUANTITY INDICATOR DECREASED TO 0.03 GALLON. ENGINE DRIVEN PUMP DEPRESS URIZED AND ELECTRIC PUMP OFF, QUANTITY INDICATION CONTINUED TO DECREASE. AIR TURN BACK TO MIA. NO FUEL DUMPED, NO OVER WEIGHT LANDING, LANDING UNEVENTFUL. FOUND LEFT DOWNLOCK ACTUATOR HYDRAULIC FLEX LINE RUPTURED. REPLACED FLEX LINE, LEA K CHECKED, NO LEAKS NOTED. RELEASED AIRCRAFT FOR REVENUE SERVICE. 2 L 7 2 4F RT A2NM 2000012200657 20000122 00657 NM 2000 1 22 AALA991957 1 19991220 A 5751 SKIN BOEING 767 767323 1385205 NM AILERON CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 355AA 24036 LAX - DURING B-CHECK, THE RIGHT OUTBOARD TRAILING EDGE FLAP ASSEMBLY JUST INBOARD OF OUTBOARD AILERON HAD 12 INCH CRACK. REPAIRED UPPER AND LOWER SIDE RIGHT OUTBOARD TRAILING EDGE FLAP ASSEMBLYJUST INBOARD OF OUTBOARD AILERON. SYSTEM GROU ND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000012200658 20000122 00658 WP 2000 1 22 AALA991966 1 19991224 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 498AA 49736 ATL - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPAIRED EMERGENCY EXI T FLOOR PATH LIGHT WIRING IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012200659 20000122 00659 WP 2000 1 22 AALA991960 1 19991221 A 3350 HPD54053859 LIGHT DOUG DC9 DC982 3022082 WP SEAT 5 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 424AA 49336 LAX - DURING OVERNIGHT MAINTENANCE, L2 EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. REPLACED L2 EMERGENCY EXIT LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012200660 20000122 00660 WP 2000 1 22 AALA991961 1 19991222 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROWS 19-20 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 553AA 53083 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHT AT ROWS 19-20 INOPERATIVE. TIGHTENED LOOSE CONNECTOR ON EMERGENCY EXIT OVERHEAD LIGHT BATTERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012200661 20000122 00661 NM 2000 1 22 AALA991926 1 19991214 A 5510 CASTING BOEING 727 727223 1384074 NM HORIZ STABILIZER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - RIGHT STABILIZER HINGE CASTING CRACKED. ABOUT 1.50 INCHES LONG. REMOVED CRACKED AREA PER SRM 55-10-4. INSTALLED DOUBLER PLATE PER SRM 55-10-4. TST: 62,106 HOURS. CYCLES: 37,887. (X) 2 L 7 3 4F A3WE 2000012200662 20000122 00662 NM 2000 1 22 AALA991925 1 19991209 A 5320 STRINGER BOEING 727 727223 1384074 NM BS 950 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - STRINGER 18A CRACKED OUTBOARD SIDE OF LEFT MLG WHEELWELL. CUT STR 18A 36 INCHES FORWARD OF STA 950 AND REPAIRED P ER SB 727-53-0172 IAW SRM 53-30-3 SB REPAIRS. TST: 62,106 HOURS. CYCLES: 37,884. (X) 2 L 7 3 4F A3WE 2000012200663 20000122 00663 NM 2000 1 22 AALA991923 1 19991214 A 5330 SKIN BOEING 727 727223 1384074 NM BS 320 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - APPROXIMATE STA 320 CROWN SKIN GOUGED AT STR 4L. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-30-3 FIG 14. (DOUB LER AND FILLER). AUTHORIZED BY ESO 11697 DATED 12-14-99. TST: 62,106 HOURS. CYCLES: 37,884. (X) 2 L 7 3 4F A3WE 2000012200664 20000122 00664 NM 2000 1 22 AALA991922 1 19991213 A 5532 SKIN BOEING 727 727223 1384074 NM VERT STABILIZER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - CRACK IN VERTICAL STABILIZER SKIN LEFT AT BOTTOM APPROXIMATE STA 1343. STOP DRILLED CRACK AND INSTALLED DOUBLER P ER SB 727-55-82 AND ESO 11697 DATED 12-10-99. TST: 62,106 HOURS. CYCLES: 37,884. (X) 2 L 7 3 4F A3WE 2000012200665 20000122 00665 NM 2000 1 22 AALA991931 1 19991213 A 5532 SKIN BOEING 727 727227 1384078 NM VERT STABILIZER DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - VERTICAL STABILIZER DENT IN SKIN 34 INCHES AFT OF RIGHT AMERICAN FLAG IN SKIN STA 1223 WITH CRACK IN DENT. INSTAL LED DOUBLER PER SRM 54-10-3. TST: 72,089.43 HOURS. CYCLES: 46,585. (X) 2 L 7 3 4F A3WE 2000012200666 20000122 00666 NM 2000 1 22 AALA991930 1 19991212 A 5311 FRAME BOEING 727 727227 1384078 NM BS 783 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CRACK IN FRAME AT STA 783 LEFT FRAME. INSTALLED REPAIR ANGLES PER DWG 65C36280 AND PER SB 727-53-0197. TST: 72, 089.5 HOURS. CYCLES: 46,585. (X) 2 L 7 3 4F A3WE 2000012200667 20000122 00667 NM 2000 1 22 AALA991929 1 19991213 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION ON SHEAR TIES BETWEEN BL ZERO AND STR 26L. INSTALLED REPAIRS BETWEEN STR 28L AND STR 27L PER SRM 53-10-4 FIG 15 SHEET 3 REPAIR 3. INSTALLED NEW SHEAR TIE BETWEEN STR 27L AND STR 26L PER SRM 51-10-1. TST: 72,089 HOURS. CY CLES: 46,585. (X) 2 L 7 3 4F A3WE 2000012200668 20000122 00668 NM 2000 1 22 AALA991927 1 19991210 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - SHEAR TIE IN FORWARD CARGO CORRODED STA 720 STR 28L TO STR 28R. REMOVED CORRODED SHEAR TIE AND FABRICATED AND INS TALLED NEW SHEAR TIE SRM 51-10-1. TST: 72,089.43 HOURS. CYCLES: 46,585. (X) 2 L 7 3 4F A3WE 2000012200669 20000122 00669 EU 2000 1 22 AALA991935 1 19991215 A 5315 FLOORBEEAM AIRBUS 300 A300B4605R 3930308 EU BS 4574 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - CORROSION ON FLOOR SUPPORT BETWEEN SEAT TRACKS 'E' RIGHT AND 'D' RIGHT, LOCATED BETWEEN FRAMES 71 1/2 AND 74. REM OVED AND REPLACED FLOOR SUPPORT FROM FRAME 71 1/2 TO FRAME 74 BETWEEN TRACK 'E' RIGHT, AND 'D' RIGHT PER SRM 51-72-10-0. ALODINED, PRIMED, PAINTED PER SRM 51-21-00. TST: 32,241.11 HOURS. CYCLES: 12,979. (X) 2 L 7 2 4F RT A35EU 2000012200670 20000122 00670 NM 2000 1 22 AALA991905 1 19991217 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - STA 990 AFT SIDE OF FRAME BETWEEN 28R AND 29R SHEAR TIE UPPER LEG CORRODED. ALODINED AND PRIMED SKIN AREA IAW SRM 51-20-0, INSTALLED FASTENERS, INSTALLED NEW SHEAR TIE. TST: 59,544 HOURS. CYCLES: 36,249. (X) 2 L 7 3 4F A3WE 2000012200671 20000122 00671 NM 2000 1 22 AALA991906 1 19991214 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1010 - 1050 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL- LEFT SIDE OF STR 30 CORRODED FORWARD OF FRAME STA 1030. INSTALLED STRINGER REPAIR PER SRM 53-10-3 AND SKIN DOUBLER PER SRM 53-30-3 FIG 3A. TST: 59,544 HOURS. CYCLES: 36,749. (X) 2 L 7 3 4F A3WE 2000012200672 20000122 00672 NM 2000 1 22 AALA991907 1 19991214 A 5330 SKIN BOEING 727 727223 1384074 NM BS 383.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - FUSELAGE SKIN CRACKED AT RIVET STA 383.5 STR 8R FORWARD UPPER CORNER OF FORWARD GALLEY DOOR CUT-OUT. INSTALLED DO UBLER PER SRM 53-30-3. TST: 59,544 HOURS. CYCLES: 36,249. (X) 2 L 7 3 4F A3WE 2000012200673 20000122 00673 NM 2000 1 22 AALA991908 1 19991214 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1010-1020 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON SKIN BELOW STR 30 BS 1010 - BS 1030. REMOVED CORROSION INSTALLED DOUBLER ON SKIN PER SRM 53-30-3 FIG 3A. TST: 59,544 HOURS. CYCLES: 36,249. (X) 2 L 7 3 4F A3WE 2000012200674 20000122 00674 NM 2000 1 22 AALA991909 1 19991214 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1085 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - REMOVED TEMPORARY REPAIR AND RE-INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. TST: 59,544 HOURS. CYCLES: 36,249. ( X) 2 L 7 3 4F A3WE 2000012200675 20000122 00675 NM 2000 1 22 AALA991928 1 19991211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - STA 600 FRAME CRACKED AT UPPER FASTENER FOR INTERCOSTAL OF STR 28L (MARKED). STOP DRILLED CRACK, INSTALLED 2 INCH BY 1 INCH BY .063 INCH 7075T6 REPAIR ANGLE WITH 43.1875 INCH HILOCKS PER SRM 51-40-3. TST: 59,544 HOURS. CYCLES: 36 ,249. (X) 2 L 7 3 4F A3WE 2000012200676 20000122 00676 EU 2000 1 22 AALA991854 1 19991203 A 2120 6451101 FAN GARRTT FOKKER F28 F28MK0100 4990807 EU ACM BAY FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1441A 701199 11436 DFW - FLT 0600 - AFTER TAKEOFF FROM DFW, SMELL OF SMOKE IN COCKPIT. FLIGHT ATTENDANT REPORTED SMELL AND HAZE IN CABIN. DECLARED EMERGENCY, RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED LEFT PACK RECIRCULATING FAN. SYSTEM GR OUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 2000012200677 20000122 00677 NM 2000 1 22 AALA991924 1 19991210 A 5511 SPAR BOEING 727 727223 1384074 NM VERT STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - CORROSION AT LEFT REAR SPAR CAP 2 PLACES BETWEEN NR 4 AND NR 5 HINGES. INSTALLED REPAIR IAW ESO 11697 DATED 12-8- 99. TST: 62,106 HOURS. CYCLES: 37,884. (X) 2 L 7 3 4F A3WE 2000012200678 20000122 00678 EU 2000 1 22 AALA991772 1 19991123 A 2611 HOSE FOKKER F28 F28MK0100 4990807 EU CABIN BLOCKED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1418A 11397 DSM - FLT 2042 - AFTER TAKEOFF, RIGHT AFT LAVATORY SMOKE DETECTOR ALARM SOUNDED. RETURNED AD LANDED DSM WITHOUT FUTHER INCIDENT. SUCTION HOSE COLLAPSED. REPOSITIONED AND CLEANED SUCTION HOSE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X ) 2 L 7 2 4F RT 2000012200679 20000122 00679 EU 2000 1 22 AALA991947 1 19991221 A 3260 SCREW FOKKER F28 F28MK0100 4990807 EU LT MLG MISSING A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 1457B 11469 IAH - FLT 2031 - DURING FLIGHT, LEFT LANDING GEAR DOORLOCK SWITCH ILLUMINATED. REPLACED MISSING SCREW IN LEFT MAIN GEAR DOOR UPLOCK TARGET. SYSTEM GROUND CHECKED, NORMAL OEPRATION. (X) 2 L 7 2 4F RT 2000012200680 20000122 00680 NM 2000 1 22 AALA991904 1 19991214 A 3260 AAP2448A GEAR ACCY UNIT BOEING 727 727223 1384074 NM LT MLG MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 846AA 20987 ORD - FLT 1021 - AFTER TAKEOFF UPON GEAR RETRACTION, RED LEFT GEAR WARNING LIGHT REMAINED ILLUMINATED. ALL OTHER INDICA TIONS AND FUNCTIONS NORMAL. JACKED AIRCRAFT, OPERATED GEAR SEVERAL TIMES. UNABLE TO DUPLICATE PROBLEM. REPLACED LANDI NG GEAR ACCESSORY UNIT AS PRECAUTION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200681 20000122 00681 NM 2000 1 22 AALA991682 1 19991108 A 3220 6929527 ROD BOEING 727 727223 1384074 NM NLG DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 882AA 21521 MIA - FLT 0941 - AFTER TAKEOFF MIA EN ROUTE TO PHL, LANDING GEAR WAS RETRACTED AND A LOUD BANG WAS HEARD. GEAR CAME UP AND 3 GREEN LIGHTS ILLUMIANATED. GEAR DOOR LIGHTS REMAINED RED. AIRCRAFT RETURNED TO MIA. GEAR WAS LOWERED AND AIRCRA FT LANDED WITHOUT INCIDENT MIA. REPLACED ROD ASSY AND BRACKET. ACCOMPLISHED NOSE GEAR RETRACTION. SYSTEM GROUND CHECK ED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200682 20000122 00682 NE 2000 1 22 AALA991676 2 19991108 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D1 52044 NE NR 1 MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 728AA 20735 66617B CCS - FLT 2140 - EN ROUTE CCS/MIA - NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMB. WOULD NOT EXTINGUISH. A IRCRAFT RETURNED TO CCS AND LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF ALL DUCTS AT NR 1 ENGINE PYLON AND LOOP. A CCOMPLISHED ENGINE RUN-UP AT TKAEOFF POWER. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X ) 2 L 7 3 4F 4 F A3WE E2EA 2000012200683 20000122 00683 NM 2000 1 22 AALA991827 1 19991128 A 3260 2314143 SWITCH BOEING 727 727223 1384074 NM RT MLG FAILED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 895AA 22011 PHL - FLT 0274 - AFTER TAKEOFF, MIA/PHL, RIGHT GEAR DURING RETRACTION INDICATED UNSAFE INDICATION. RIGHT GEAR DOOR LIGH T ON FLIGHT ENGINEER'S PANEL WAS ILLUMINATED. RECYCLED GEAR, STILL HAD GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL ILLUMI NATED. 25 MINUTES INTO FLIGHT, LIGHT EXTINGUISHED. REPLACED RIGHT GEAR DOOR SWITCH. ACCOMPLISHED SUCCESSFUL GEAR SWIN G. GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200684 20000122 00684 NM 2000 1 22 AALA991560 1 19991018 A 2820 AAP3043A VALVE BOEING 727 727223 1384074 NM FUEL TANK DEFECTIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 844AA 6269 20985 MIA - FLT 1562 - EN ROUTE MIA/MCO, NR 3 FUEL CROSSFEED VALVE CLOSED IN-FLIGHT. FUEL WOULD NOT CROSSFEED FROM OR TO THE NR 3 FUEL TANK. LANDED MCO WITHOUT INCIDENT. SECURED NR 3 CROSSFEED VALVE IN OPEN POSITION AND RETURNED TO MIA WITHOU T INCIDENT. REPLACED NR 3 CROSSFEED VALVE ACCORDING TO MM. LEAK CHECK VALVE AND SYSTEM GROUND CHECKED, NORMAL OPERATIO N. (X) 2 L 7 3 4F A3WE 2000012200685 20000122 00685 NM 2000 1 22 AALA991798 1 19991126 A 3260 656021132 CONTROL UNIT BOEING 727 727227 1384078 NM LT MLG FAILED A AALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 729AA 20736 DFW - FLT 0876 - DURING APPROACH TO DFW ON GEAR EXTENSION, LEFT MAIN LANDING GEAR SHOWED UNSAFE. RECYCLED GEAR WITH NO HELP. GEAR MANUALLY EXTENDED AND VERIFIED LOCKED. GEAR LIGHT STILL SHOWED UNSAFE. LANDED DFW WITHOUT INCIDENT. REPLA CED LANDING GEAR ACCESSORY UNIT AND ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200686 20000122 00686 NM 2000 1 22 AALA991665 1 19991106 A 3240 AAP2401B BRAKE BOEING 727 727223 1384074 NM LT MLG OVERSERVICED A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 863AA 21090 IAH - FLT 1878 - ON TAXI OUT, LEFT BRAKES WERE WEAK ON STOPPING AIRCRAFT. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. N R 1 AND NR 2 BRAKE ASSEMBLIES WERE BLED. ALL BRAKE BOOSTERS WERE CHECKED AND FOUND TO BE IN THE GREEN BAND. SYSTEM GRO UND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200687 20000122 00687 NM 2000 1 22 AALA991694 1 19991110 A 2610 738001 CONTROLLER BOEING 727 727223 1384074 NM COCKPIT MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 703AA 456 22461 CUN - FLT 0940 - EN ROUTE TO MIA, NR 3 ENGINE FIRE DETECTION SYSTEM INOPERATIVE. AIRCRAFT LANDED CUN WITHOUT INCIDENT. REPLACED NR 3 ENGINE FIRE DETECTOR MODULE CONTROL. SYSTEM GORUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200688 20000122 00688 NM 2000 1 22 AALA991776 1 19991121 A 3222 MS28775015 O-RING BOEING 727 727223 1384074 NM NLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6835 20188 IAD - FLT 1239 - AFTER TAKEOFF FROM IAD WHEN GEAR HANDLE WAS RAISED, THE NOSE GEAR RED LIGHT ON THE FORWARD INSTRUMENT P ANEL REMAINED ILLUMINATED. NOSE GEAR DOOR LIGHT ON THE FLIGHT ENGINEER PANEL WAS ALSO ILLUMINATED. RETURNED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED SCHRAEDER VALVE O-RING AND SERVICED STRUT WITH FLUID AND AIR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200689 20000122 00689 NM 2000 1 22 AALA991879 1 19991209 A 2130 ST106AB TRANSMITTER AMETEK BOEING 727 727223 1384074 NM ACM BAY MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 874AA 21386 ORD - FLT 1214 - DURING CLIMB, CABIN RATE OF CLIMB EXCEEDED 700 FEET PER MINUTE. CABIN CONTINUED TO CLIMB WITH CONTROL FULL CLOCKWISE. RETURNED AND LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED LEFT PACK AIR PRESSURE TRANSMITTER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200690 20000122 00690 NM 2000 1 22 AALA991804 1 19991126 A 2131 AAP1032E CONTROLLER GARRTT BOEING 727 727223 1384074 NM CABIN PRESSURE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 844AA 20985 MIA - FLT 1578 - DURING CLIMB-OUT FROM MIA EN ROUTE TO ATL, UNABLE TO CONTROL CABIN PRESSURIZATION. AIRCRAFT RETURNED T O MIA AND LANDED WITHOUT INCIDENT. REPLACED CONTROLLER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 2000012200691 20000122 00691 NM 2000 1 22 AALA991826 1 19991125 A 3260 2314143 SWITCH BOEING 727 727223 1384074 NM RT MLG FAILED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 895AA 22011 TPA - FLT 1486 - DURING LANDING WHEN GEAR WAS EXTENDED, THE LEFT GEAR DOOR ANNUNCIATED ON THE FLIGHT ENGINEER'S PANEL AN D THE RED DOOR LIGHT REMAINED ILLUMINATED. REPLACED LEFT GEAR DOOR SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 3 4F A3WE 2000012200692 20000122 00692 NM 2000 1 22 AALA991902 1 19991214 A 3350 0105924005 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 775AN 29584 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT NEAR FORWARD GALLEY LEFT CORNER BROKEN. REPLACED EMERGENCY EXI T LIGHT NEAR FORWARD GALLEY LEFT CORNER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT T00001SE 2000012900001 20000129 00001 WP 2000 1 29 AALA991989 1 19991228 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 205AA 49155 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM FORWARD BULKHEAD TO FORWARD GALLEY INOPERATIVE . REPLACED EMERGENCY EXIT FLOOR PATH LIGHTS FROM FORWARD BULKHEAD TO FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPE RATION. (X) 2 L 7 2 4F A6WE 2000012900002 20000129 00002 WP 2000 1 29 AALA991956 1 19991222 A 2150 20495061 ACM GARRTT DOUG DC9 DC982 3022082 WP AC BAY MALFUNCTIONED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 07 295AA 0214679 49307 BDL - FLT 1180 - ON ARRIVAL BDL, CABIN FILLED WITH SMOKE. LANDED BDL WITHOUT INCIDENT. REPLACED RIGHT AIR-CONDITIONING AIR CYCLE MACHINE. ALSO, REPLACED COALESCER BAGS AND ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED, NORMAL OPERAT ION. (X) 2 L 7 2 4F A6WE 2000012900003 20000129 00003 WP 2000 1 29 AALA991973 1 19991226 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90511 49805 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 15D INOPERATIVE. REPAIRED EMERGENCY EXIT F LOOR PATH LIGHT WIRING AT SEAT 15D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012900004 20000129 00004 WP 2000 1 29 AALA991943 1 19991218 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 494AA 49732 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY FLOOR PA TH LIGHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012900005 20000129 00005 WP 2000 1 29 AALA991940 1 19991218 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3515 49892 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. OVERWING EMERGENCY EXIT LIGHT ASSEMBLY SHORTED TO SIDEWALL GRILL. REPLACED OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED , NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012900006 20000129 00006 WP 2000 1 29 AALA991986 1 19991229 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278AA 49294 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIG HT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012900007 20000129 00007 WP 2000 1 29 AALA991975 1 19991228 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 431AA 49343 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AFT OF FORWARD GALLEY INOPERATIVE. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHT STRIP AFT OF FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012900008 20000129 00008 NE 2000 1 29 AALA991992 2 19991230 A 7310 FUEL TRANSFER FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE CENTER FUEL TANK MALFUNCTIONED A AALA A UNSCHED LANDING B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CL CLIMB 1 SW 07 1401G 11352 SDF - FLT 1827 - SHORTLY AFTER TAKEOFF, CENTER FUEL TANK FUEL OF APPROXIMATELY 700 POUNDS WENT TO ZERO POUNDS. RIGHT WI NG TANK READING 700 POUNDS HIGHER THAN LEFT. SLIGHT FUEL SMELL IN COCKPIT. ACCOMPLISHED AUTOMATIC AND MANUAL CENTER FU EL AUTOFEED. COULD NOT DUPLICATE COMPLAINT. SYSTEM GROUND CHECKED, NORMAL OPERATION. RESIDUAL FUEL AT LEFT WING VENT. (X) 2 L 7 2 4F 4 F RT E25NE 2000012900009 20000129 00009 NE 2000 1 29 AALA991987 2 19991229 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 2 MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 561AA 53091 LAS - FLT 0696 - AFTER TAKEOFF, EXPERIENCED FIRE WARNING INDICATION ON NR 2 ENGINE. CREW SHUT DOWN ENGINE AND DISCHARGE D BOTH FIRE BOTTLES AS A PRECAUTION. EMERGENCY DECLARED, RETURNED AND LANDED LAS WITHOUT INCIDENT. REPLACED BOTH FIRE BOTTLES, RAN ENGINES AND NO DISCREPANCIES FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F 4 F A6WE E9NE 2000012900010 20000129 00010 WP 2000 1 29 AALA991968 1 19991015 A 3231 LATCH DOUG DC9 DC982 3022082 WP MLG DOOR DIRTY A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 469AA 49599 ORD - FLT 0066 - AFTER TAKEOFF, LEFT GEAR DOOR LIGHT (RED) ILLUMINATED. PROCEDURE FOLLOWED AND FLIGHT CONTINUED IN MANU AL. DURING CRUISE, THE AMBER GEAR DOOR LIGHT ILLUMINATED WITH ASSOCIATED NOISE AND YAW. INCREASED HYDRAULIC PRESSURE TO EXTINGUISH THE AMBER DOOR OPEN LIGHT. RED LEFT GEAR LIGHT REMAINED ILLUMINATED. CLEANED DEBRIS FROM LEFT MAIN GEAR DOOR LATCH. LUBRICATED LATCH MECHANISM ON BOTH GEAR DOORS. CYCLED GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED, NORMAL O PERATION. (X) 2 L 7 2 4F A6WE 2000012900011 20000129 00011 WP 2000 1 29 AALA991937 1 19991218 A 3234 GEAR HANDLE DOUG DC9 DC982 3022082 WP COCKPIT LACK OF LUBE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 7520A 49897 DFW - FLT 0899 - DURING APPROACH AFTER GEAR EXTENSION, ONLY THREE RED LIGHTS ILLUMINATED. ACCOMPLISHED EMERGENCY EXTENS ION CHECKLIST, GAVE THREE GREEN LIGHTS AND GEAR DOOR LIGHT EXTINGUISHED WHEN HANDLE WAS STOWED. LANDED DFW WITHOUT FURT HER INCIDENT. LUBRICATED GEAR HANDLE AND ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000012900012 20000129 00012 NM 2000 1 29 AALA991990 1 19991229 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AA 25196 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN RIGHT SIDE OF COACH CLASS INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT FLOOR PATH LIGHTS IN RIGHT SIDE OF COACH CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X ) 2 L 7 2 4F RT A1NM 2000012900013 20000129 00013 NM 2000 1 29 AALA991976 1 19991227 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 613AA 24489 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN ROWS 9 AND 12 INOPERATIVE. RESECURED EMERG ENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000012900014 20000129 00014 NM 2000 1 29 AALA991974 1 19991227 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 658AA 24616 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT IN FORWARD CABIN UNDER EXIT SIGN INOPERATIVE. REPLA CED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000012900018 20000129 00018 NM 2000 1 29 AALA991952 1 19991220 A 3350 43467410312113 LIGHT KORRY BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621AM 24579 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT ASSEMBLY AT SEAT 18D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000012900019 20000129 00019 NM 2000 1 29 AALA991946 1 19991219 A 3350 CONNECTOR BOEING 767 767323 1385205 NM SEAT 37 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 37H INOPERATIVE. REPAIRED EMERGENCY EXIT SEA T PATH LIGHT CONNECTOR AT SEAT 37H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000012900020 20000129 00020 NM 2000 1 29 AALA991944 1 19991219 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 336AA 22334 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT 22H INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT WIRE AT SEAT 22H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000012900021 20000129 00021 NM 2000 1 29 AALA991941 1 19991218 A 3397 WIRE BOEING 767 767323 1385205 NM SEAT 36 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 381AN 25450 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 36H INOPERATIVE. REPAIRED WIRING AT SEAT 36H . SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000012900022 20000129 00022 NM 2000 1 29 AALA991967 1 19991224 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 368AA 25195 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 35A INOPERATIVE. REPAIRED EMERGENCY EXIT SEA T PATH LIGHT CONNECTOR AT SEAT 35A. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000012900023 20000129 00023 NM 2000 1 29 AALA991963 1 19991224 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 656AA 24614 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN MID-GALLEY AREA INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000012900024 20000129 00024 NM 2000 1 29 AALA991901 1 19991214 A 3350 0201922001 SOCKET BOEING 767 767223 1385123 NM SEATS 7 AND 28 FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 304AA 22310 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEATS 7B AND 28B INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT SOCKET AT SEATS 7B AND 28B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000012900025 20000129 00025 EU 2000 1 29 AALA991969 1 19991225 A 2133 VST165D OUTFLOW VALVE TECHNOFAN AIRBUS 300 A300B4605R 3930308 EU ACM BAY MALFUNCTIONED A AALA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 07 7062A 474 MIA - FLT 1901 - DURING CRUISE AT FL 330, PRESSURE WARNING WITH DIFFERENTIAL PRESSURE OF 9.4 PSI IN AUTO MODE. CREW MAN UALLY DEPLOYED OXYGEN MASKS AND EXECUTED EMERGENCY DESCENT. REPOSITIONED OVEBOARD VALVE PRESSURE. SYSTEM GROUND CHECKE D, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000012900026 20000129 00026 EU 2000 1 29 AALA991951 1 19991215 A 5320 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU BS 56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL- CTR CX FLOORBEAM AT FR 56 CORRODED AROUND FLOORBOARD ATTACH HOLE BETWEEN NR 5 AND NR 6 ROLLER TRAY. CUT OUT CORRO DED SECTION OF FLOORBEAM AND SPLICED IN NEW SECTION IAW SRM 53-10-15-2. TST: 32,184 HOURS. CYCLES: 12,777. (X) 2 L 7 2 4F RT A35EU 2000012900027 20000129 00027 WP 2000 1 29 AALA991950 1 19991216 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1871 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - LAVATORY SUPPORT CORRODED AT AFT RIGHT SUPPORT TIE SUPPORT LAV 'E', STA 1871. INSTALLED NEW SUPPORT PER AARD 51-0 1-00-05 PAGE 1. TST: 96,475.29 HOURS. CYCLES: 19,001. (X) 2 L 7 3 4F A22WE 2000012900028 20000129 00028 WP 2000 1 29 AALA991984 1 19991221 A 5400 WEB DOUG DC10 DC1030 3023501 WP NR 3 PYLON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - NR 3 PYLON AFT UPPER WEB HAS FRETTING CORROSION ON BOTH INBOARD AND OUTBOARD EDGES IN 2 AREAS OF LAST 12 INCHES OF ONE AREA INBOARD SIDE OF AFT LIGHTENING HOLE. TREATED AND REPAIRED PER SRM 54-20-00 FIG 34 (VOL I). INSTALLED DOUBLER PER SRM 54-20-00 FIG 24 VOL I. TST: 96,475.29 HOURS. CYCLES: 19,001. (X) 2 L 7 3 4F A22WE 2000012900037 20000129 00037 EU 2000 1 29 AALA2000022 1 19991229 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - CORROSION BEYOND LIMITS. AFT CARGO AREA, FRAME 59R STR 44R. INSTALLED SHOP FABRICATED FITTING. TST: 32,184 HOU RS. CYCLES: 12,777. (X) 2 L 7 2 4F RT A35EU 2000012900039 20000129 00039 EU 2000 1 29 AALA2000020 1 19991229 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 61 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - FITTING HAD CORROSION ON TOP SIDE. REMOVED AND REPLACED FITTING PER SRM 51-72-10. TST: 32,184 HOURS. CYCLES: 12,777. (X) 2 L 7 2 4F RT A35EU 2000012900041 20000129 00041 EU 2000 1 29 AALA2000018 1 19991229 A 5320 BEAM AIRBUS 300 A300B4605R 3930308 EU DOOR SILL CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - DOOR SILL BEAM AT FRAME 63 HAD CORROSION BEYOND LIMITS. REPLACED DAMAGED SECTION OF DOOR SILL BEAM PER SRM 53-17- 18. TST: 32,184 HOURS. CYCLES: 12,777. (X) 2 L 7 2 4F RT A35EU 2000012900042 20000129 00042 EU 2000 1 29 AALA2000017 1 19991231 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 38.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - FITTING HAD CORROSION AT FRAME 38.2 RIGHT AFT END OF FORWARD CARGO STR 40R TO STR 44R. INSTALLED NEW FLOOR SUPPOR T FITTINGS PER SRM 53-10-14. ALODINED, PRIMED AND PAINTED PER 51-23-10. (X) 2 L 7 2 4F RT A35EU 2000012900043 20000129 00043 EU 2000 1 29 AALA2000016 1 19991230 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - AFT OF FRAME 65 STRINGER END CORRODED. STR 56L. REMOVED CORRODED SECTION, INSTALLED REPAIR SPLICE PER SRM 53-10- 14. TREATED, PRIMED AND PAINTED AREA. TST: 32,184 HOURS. CYCLES: 12,777. (X) 2 L 7 2 4F RT A35EU 2000012900044 20000129 00044 EU 2000 1 29 AALA2000015 1 19991207 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 70 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - CORROSION ON SKIN DOUBLER AT FRAME 70 BETWEEN LONGERONS 46L AND 47L. INSTALLED NEW DOUBLER PER SRM 51-72-10. TST : 32,184 HOURS. CYCLES: 12,777. (X) 2 L 7 2 4F RT A35EU 2000012900045 20000129 00045 EU 2000 1 29 AALA991994 1 19991210 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU BS 19-21 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - CORROSION ON LONGERONS 51LT THROUGH 50RT AT FRAMES 19 THROUGH 21. REPLACED LONGERON SECTIONS WITH NEW MATERIAL PE R ESO 30595 NR 50-531314-344 AND -347. TST: 32,184 HOURS. CYCLES: 12,777. (X) 2 L 7 2 4F RT A35EU 2000012900046 20000129 00046 NM 2000 1 29 AALA991787 1 19991126 A 3230 FITTING DOUG MD11 MD11 3023602 NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - RIGHT MLG TRAPEZOID FITTING CORRODED AT GEAR MOUNT HOLE. (INBOARD HORIZONTAL HOLE FOR BARREL NUT). TRAPEZOIDAL F ITTING REPAIR PER ESO 41000 11-24-99. DETAILS OF REPAIR ON BACK OF E58-11 016651. (X) 2 L 7 3 4F RT A22WE 2000012900047 20000129 00047 WP 2000 1 29 AALA991934 1 19991216 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 2001 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - CORROSION ON T-ANGLE RIGHT OF CENTER 18 INCHES TO 60 INCHES STA 2007. REPLACED T-ANGLE FROM NR 8 TRACK TO CENTER OF 2007 BULKHEAD PER SRM 53-40-00 VOL I. TST: 94,675.29 HOURS. CYCLES: 19,001. (X) 2 L 7 3 4F A22WE 2000012900048 20000129 00048 NM 2000 1 29 USAA991377 1 19991225 A 5315 BEAM BOEING 737 7372B7 1384560 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK IN RADIUS OF FLOOR SUPPORT ANGLE STA 294.5 RBL 54. REMOV ED AND REPLACED ANGLE PER SRM 51-40-1. (X) 2 L 7 2 4F A16WE 2000012900049 20000129 00049 NM 2000 1 29 USAA991376 1 19991225 A 5315 65C34537910 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 663, BL ZERO FLOORBEAM. INSTALLED REPAIR SECTION O F FLOORBEAM PER TR 57-10-04. (X) 2 L 7 2 4F A16WE 2000012900050 20000129 00050 NM 2000 1 29 USAA991374 1 19991225 A 5320 WEB BOEING 737 7372B7 1384560 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 1 INCH DAMAGED FASTENER HOLE CUTOUT AT BS 294.5, WL 208, RBL 21-RBL 25 WEB. INSTALLED DOUBLER PER SRM 51-40-2. (X) 2 L 7 2 4F A16WE 2000012900051 20000129 00051 NM 2000 1 29 USAA991372 1 19991225 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 300 - 333 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES IN Z-ANGLE, STA 300 TO STA 333, RBL 55 T O RBL 60, WL 208.1 CREASE BEAM INNER CHORD ANGLE. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED NEW Z-AN GLE PER SRM 51-10-1. (X) 2 L 7 2 4F A16WE 2000012900052 20000129 00052 NM 2000 1 29 EISA99244 1 19991021 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 400 RBL 10 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ROUTINE C-CHECK INSPECTION CARD REVEALED CORROSION ON MAIN CABIN FLOORBEAM T-CAP AT BS 400 RBL 10. REMOVED CORROSION PE R SRM 51-10-6, FABRICATED AND INSTALLED REPAIR PER SRM'S 51-10-8 AND 51-30-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012900053 20000129 00053 NM 2000 1 29 EISA99243 1 19991116 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 116 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON LOWER SURFACE OF UPPER FLOORBEAM CHORD AT BS 1166 LBL 28. REMOVED CORROSION AND MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLES AND INSTALLED REPAIR PER S RM 53-10-8 AND SRM 51-30-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012900054 20000129 00054 NM 2000 1 29 EISA99242 1 19991104 A 5755 SKIN BOEING 727 727225 1384077 NM SPOILER DELAMINATED A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED DELAMINATION ON TOP SURFACE OF NR 2 SPOILER PANEL. REPAIRED TOP LE FT CORNER OF PANEL WITH FIBERGLASS REPAIR PER SRM 57-50-6 PAGE 611. TT: 65,345:17 HOURS. TC: 43,816. (X 2 L 7 3 4F A3WE 2000012900055 20000129 00055 NM 2000 1 29 EISA99241 1 19991112 A 5210 SKIN BOEING 727 727225 1384077 NM PASSENGER DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED INTERIOR SKIN ON FORWARD ENTRY DOOR IS BENT AND CRACKED AT TORQUE T UBE CUTOUT. STOP DRILLED CRACK PER SRM 51-10-1, RESHAPED DEFORMED AREA PER SRM 51-30-10. FABRICATED AND INSTALLED WEB REPAIR PER SRM'S 51-40-2 AND 52-10-1. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000012900056 20000129 00056 EU 2000 1 29 AALA2000012 1 19991230 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 32-33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - SKIN UNDER ANTENNA CORRODED. INSTALLED DOUBLER PER SRM 53-10-12. TST: 32,241.11 HOURS. CYCLES: 12,979. (X) 2 L 7 2 4F RT A35EU 2000012900061 20000129 00061 WP 2000 1 29 UPS00831348 1 19991228 A 5320 3750229502 FITTING DOUG DC8 DC871F 302199D WP BS 640 - 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1, STA 640-660 STR 1 SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 37502 71 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000012900074 20000129 00074 WP 2000 1 29 UPS00831365 1 19991228 A 5313 37796571 LONGERON DOUG DC8 DC871F 302199D WP BS 640 - 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C1 SAT 640-660 LONGERON 1 IS CRACKED. FABRICATED AND REPLACED LONGERON 1 FROM STA 640-680 IAW DWG 63779 657 AND SRM 53-4-1 FIG 41. 2 L 7 4 4F RT 4A25 2000012900105 20000129 00105 WP 2000 1 29 9905621150 1 19991123 A 5713 LONGERON DOUG DC10 DC1040 3023508 WP WS 344 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 150US 46759 DURING L CHECK, FOUND CRACK ON STR 41 ON RIGHT WING FRONT SPAR AT XORS 344. REPAIRED PER EA 11-150363. 2 L 7 3 4F A22WE 2000012900106 20000129 00106 WP 2000 1 29 9905631153 1 19991109 A 5320 STIFFENER DOUG DC10 DC1040 3023508 WP BS 1521 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING M CHECK, FOUND CRACK ON HORIZONTAL T STIFFENER AT FS1521 BULKHEAD AT X=40, Z=97.350. REPAIRED PER EA 12-171336. 2 L 7 3 4F A22WE 2000012900107 20000129 00107 NM 2000 1 29 9905646626 1 19991115 A 5711 SPAR BOEING 747 747251B 1384892 NM WS 1445 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 626US 21708 DURING M CHECK, FOUND CORROSION ON LOWER SPAR CAP OF WING LEADING EDGE CAVITY AT FSSI 1445. REPAIRED PER EA 66-173191. 2 L 7 4 4F A20WE 2000012900108 20000129 00108 NM 2000 1 29 9905656303 1 19991122 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM BS 840 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING M CHECK, FOUND CORROSION ON MAIN DECK FLOORBEAM UPPER CHORD FS 840, RBL 108. REPAIRED PER EA 63-171521. 2 L 7 4 4F RT A20WE 2000012900109 20000129 00109 NM 2000 1 29 9905666626 1 19991111 A 5347 FLANGE BOEING 747 747251B 1384892 NM BS 1170 - 1220 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 626US 21708 DURING M CHECK, FOUND CORROSION ON SEAT TRACK INBOARD FLANGE AT FS 1170 - 1220, RBL 98. REPAIRED PER EA 66-171435. 2 L 7 4 4F A20WE 2000012900110 20000129 00110 NM 2000 1 29 9905676303 1 19991122 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM BS 840 - 846 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING M CHECK, FOUND CORROSION ON SEAT TRACK AT FS 840 - 846, RBL 39. REPAIRED PER EA 63-172896. REPAIRED PER EA 63-1 72896. 2 L 7 4 4F RT A20WE 2000012900154 20000129 00154 WP 2000 1 29 ABXA000011 1 19991108 A 5320 5956034505 FITTING DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND FLOOR SUPPORT FITTING CRACKED AT STATION 965 AND LONGERON 28 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2000012900155 20000129 00155 WP 2000 1 29 ABXA000012 1 19991108 A 5313 39132091 LONGERON DOUG DC9 DC931 3022065 WP BS 804 - 897 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LONGERON 30 STATION 804-897 CORRODED. REPLACED STRAP DOUBLER IAW DC9 SRM 51-30-01. 2 L 7 2 4F A6WE 2000012900156 20000129 00156 WP 2000 1 29 ABXA000013 1 19991108 A 5280 5910557107 SKIN DOUG DC9 DC931 3022065 WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND OUTBOARD LEFT MAIN LANDING GEAR DOOR CRACKED. REPLACED DOOR IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2000012900157 20000129 00157 WP 2000 1 29 ABXA000014 1 19991108 A 5320 39132091 FITTING DOUG DC9 DC931 3022065 WP CARGO BAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LONGERON END FITTING CRACKED IN FWD CARGO COMP. REPLACED LONGERON END FITTING IAW DC9 SRM 51-30-2 . 2 L 7 2 4F A6WE 2000012900158 20000129 00158 WP 2000 1 29 ABXA000015 1 19991108 A 5330 59114273 SKIN DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED AT STATION 996 AND LONGERON 14 LEFT. REPAIRED IAW ABX REA 33998-MR. 2 L 7 2 4F A6WE 2000012900200 20000129 00200 WP 2000 1 29 AT0000018 1 19991213 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 598 CHAFFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FLOORBEAM AT BS 598 LBL 12 HAS 5 CHAFFED SPOTS. FABRICATED AND INSTALLED 1 DOUBLER, 3 SHIMS, 3 WEAR STRIPS IAW TIMCO EO 99-1415. 2 L 7 2 4F A6WE 2000012900201 20000129 00201 WP 2000 1 29 AT0000019 1 19991221 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND LIGHTNING STRIKES AT LT CABIN WINDOW CUTOUT NR 17. FABRICATED AND INSTALLED WINDOW CUTOUT DOUBLER IAW TIMCO EO 99 -1432 AND SERVICE REWORK DRAWING SR09530053. 2 L 7 2 4F A6WE 2000012900202 20000129 00202 WP 2000 1 29 AT0000020 1 19991220 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 900 - 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 RT INBOARD SEAT TRACK CORRODED AT BS 900 TO 965. REMOVED AND REPLACED SEAT TRACK FROM BS 878 TO 965 IAW DC9 SRM 51-10-3 , 53-05 FIG 4 AND 53-20-1. 2 L 7 2 4F A6WE 2000012900203 20000129 00203 WP 2000 1 29 AT0000021 1 19991224 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 897 - 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND SURFACE CORROSION AND SEVERAL CRACKS IN LT CUSP WEB OUTBOARD EDGE AT BS 897 TO BS 965. REMOVED SECTION OF CUSP WE B AT BS 889-965. INSTALLED NEW CUSP WEB IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 2000012900204 20000129 00204 WP 2000 1 29 AT9900915 1 19991208 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 FOUND RIGHT WING, OUTBOARD SECTION OF TRAILING EDGE, TOP AND BOTTOM SKIN TO HAVE CORROSION AND FOUND RIB CRACKED ON RIGH T WING. REMOVED CORROSION AND INSTALLED DOUBLER ON RIB. 2 L 7 2 4F A6WE 2000012900205 20000129 00205 WP 2000 1 29 AT9900916 1 19991212 A 5754 BRACKET DOUG DC9 DC932 3022066 WP LE FLAP CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 FOUND CRACKED SUPPORT BRACKET ON RIGHT WING LEADING EDGE. FABRICATED AND REPLACED CRACKED BRACKET. 2 L 7 2 4F A6WE 2000012900206 20000129 00206 WP 2000 1 29 AT9900918 1 19991223 A 5712 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 FOUND LEFT WING OUTBOARD TRAILING EDGE INSIDE RIB NR 2 TOP AND BOTTOM CRACKED. INSTALLED DOUBLERS ON TOP AND BOTTOM OF NR 2 RIB. 2 L 7 2 4F A6WE 2000012900207 20000129 00207 WP 2000 1 29 AT9900921 1 19991212 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 917 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 834AT 47488 FOUND AFT CARGO COMPARTMENT LOWER CUT-OUT INTERCOSTAL CORRODED AT BS 917. FABRICATED AND INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F A6WE 2000012900242 20000129 00242 CE 2000 1 29 2000ZZZX228 1 19991207 A 3230 508103381 DOWNLOCK 50810335 BEECH 99 B99 1154004 CE LT MLG BROKEN A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 99CA U127 LEFT MAIN GEAR DOWNLOCK BROKEN. PROBLEM OCCURRED UNDER NORMAL CONDITIONS. DOWNLOCK HOOK SHOWED SIGNS OF WEAR ON THE IN SIDE OF THE HOOK THAT COULD BE CONDUCIVE TO TIGHT DOWNLOCK ENGAGEMENT. SUBMITTER STATED DOWNLOCK SHOULD NOT BE LOOSE AS TO CAUSE AN UNSAFE CONDITION, BUT SHOULD HAVE A SMALL AMOUNT OF PLAY AND SHOULD ALWAYS BE RIGGED IAW APPROPRIATE MM. 1 L 7 2 3T A14CE 2000012900245 20000129 00245 2000 1 29 2000ZZZX231 4 19991218 A 3422 4000B12 DIRECTIONAL GYRO AIRSCIENCES BEECH 99 99A 1154003 CE PITOT SYSTEM BROKEN A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 326CA A3227E U135 DIRECTIONAL GYRO BECAME INOPERABLE. CHECK OF PITOT SYSTEM FOUND BROKEN CONNECTOR ON BACK OF GYRO. UPON REMOVAL OF GYRO , FOUND ALL THREE LINE CONNTIONS BROKEN. 1 L 7 2 3T A14CE 2000012900360 20000129 00360 WP 2000 1 29 RRXA991001 1 19990324 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND CORROSION, RIGHT WING, AROUND SCREW HOLD RIGHT WING I/B L/E UPPER SURFACE AT XFS 20. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER IAW D C8 SRM 57-2-1 FIG 37 AND INSTALLED IAW DC8 SRM 57-2-1 FIT 37, 51-1-21, 51-1-20D AND 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900361 20000129 00361 WP 2000 1 29 RRXA991003 1 19990315 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FRAME TO MEMBRANE ATTACH ANGLE AT STA 1540 LONGERON 21 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW AND INSTALLED ATTAC H ANGLE IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900362 20000129 00362 WP 2000 1 29 RRXA991004 1 19990305 A 5320 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND CRACK, R-2 DOOR, FWD LOWER CORNER FRAME. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE D DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC8 SRM 51-3-0, 51-1-20, 51-1- 21. 2 L 7 4 4F RT 4A25 2000012900363 20000129 00363 WP 2000 1 29 RRXA991005 1 19990322 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1580 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND WEAR, FUSELAGE, MAIN CARGO COMPARTMENT NR 17 SEAT TRACK ROW NR 2 WORN STA 1580 APPROX. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW AND INSTALLED C HANNEL AND PLUG IAW DC8 SRM 53-2-3 FIG 6D. 2 L 7 4 4F RT 4A25 2000012900364 20000129 00364 WP 2000 1 29 RRXA991006 1 19990322 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1600 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND WEAR, FUSELAGE, MAIN CARGO COMPT NR 17 SEAT TRACK WORN AT STA 1600. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW CHANNEL AND PLUG AND INSTALLED IAW DC8 SRM 53-2-3 FIG 6D. 2 L 7 4 4F RT 4A25 2000012900365 20000129 00365 WP 2000 1 29 RRXA991007 1 19990322 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1690 & 1700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, LONGERON 24 RIGHT BETWEEN STA 1690 AND STA 1700. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC8 SR M 51-1-21 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900366 20000129 00366 WP 2000 1 29 RRXA991008 1 19990316 A 5720 FASTENER DOUG DC8 DC871F 302199D WP WS 58 SHEARED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND SHEARED, WING, HI-LOCK SHEARED IN SKATE ANGLE NR 4 ALT TANK 508 CONT AT STA 58. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW FAA AP PROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO-99-060. 2 L 7 4 4F RT 4A25 2000012900367 20000129 00367 WP 2000 1 29 RRXA991009 1 19990322 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1580 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND DAMAGE, FUSELAGE, FRAME AT STA 1580 RT DAMAGED AT UPPER CUSP LINE. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER, FILLERS AND SPLICE AND INST ALLED IAW DC8 SRM 53-2-0 FIG 2, 51-1-20D. 2 L 7 4 4F RT 4A25 2000012900368 20000129 00368 WP 2000 1 29 RRXA991010 1 19990322 A 5320 NUT DOUG DC8 DC871F 302199D WP BS 35 & 55 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, UNDER DOME NUTS BETWEEN STA 55 AND STA 35, LONGERON 30 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO- 99-53-0327-1. (CORROSION DAMAGE RECORDED IN EWA CORROSIO N PROGRAM). 2 L 7 4 4F RT 4A25 2000012900370 20000129 00370 WP 2000 1 29 RRXA991017 1 19990104 A 5320 ANGLE DOUG DC8 DC873 302199C WP BS 857 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, SPAR CAP, AT STA 857, BETWEEN BL 13 RIGHT AND BL 18 RIGHT. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC8 SRM 53-2-5 FIG 16, 51-1-20D, 51-3-0, AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900371 20000129 00371 WP 2000 1 29 RRXA991018 1 19990118 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1360 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND SCRAPE, CENTER FUSELAGE, SKIN/PLATE, AT STA 1360, LONGERON 23 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AREA IAW DC8 SRM 51-1-0, TREATED AND P RIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2000012900372 20000129 00372 WP 2000 1 29 RRXA991019 1 19990204 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1843 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, LT FRAME STA 1843 TW0 FEET ABOVE HORIZ STAB. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO 99-011 AND 8110-3 DATED 01/27/99. (CORROSION DAMAGE RECORDED IN EW A CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900373 20000129 00373 WP 2000 1 29 RRXA991020 1 19990114 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 7.50 - 32.5 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, L/E SKIN, LEFT WING L/E UPPER SURFACE UNDER SCREW HEADS FR OM XFS 7.50 TO XFS 32.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABR ICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO 99-004 AND DC8 SRM 51-1-20. ( CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900374 20000129 00374 WP 2000 1 29 RRXA991021 1 19990126 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 640 - 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, SKIN/PLATING, MARKER BEACON ON MOUNTING SKIN BETWEEN STA 6 40 AND STA 660, BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AREA FLAP PEEN, REWORKED AREA PROTECT AREA IAW DC8 SRM 51-1-8 AND FILL TO EN SURE SMOOTH CONTOUR IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO 99-008 AND 8110-3 DATED 01/20/99. (COR ROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900376 20000129 00376 WP 2000 1 29 RRXA991023 1 19990121 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP COCKPIT CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CRACK, CENTER FUSELAGE, SHIELD BULKHEAD, C-PIT FWD BULKHEAD, BENT, CRACKED. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PARTITION AND ATTACH ANGLE IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO- 99-017. PAINTED IAW DAC DWG NR 51-20-0. 2 L 7 4 4F RT 4A25 2000012900377 20000129 00377 WP 2000 1 29 RRXA991024 1 19990121 A 7110 CHANNEL DOUG DC8 DC871F 302199D WP ENGINE COWL CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, NOSE COWL CHANNEL 5:30 POSITION AFT SIDE OF CANTED BULKHEAD. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED U CHANNEL IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO 99-005 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA COR ROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900378 20000129 00378 WP 2000 1 29 RRXA991025 1 19990121 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, FWD PIT, AT STA 120, BETWEEN LONGERONS 33 RIGHT AND LONGERON 30 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLE DOUBLER AND INSTALLED IAW DC8 SRM 53-2-0 AND 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900379 20000129 00379 WP 2000 1 29 RRXA991026 1 19990115 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME ATTACH ANGLE, FWD PIT, AT STA 140, LONGERON 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATT ACH ANGLE IAW DC8 SRM 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900380 20000129 00380 WP 2000 1 29 RRXA991027 1 19990129 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, UPPER CUSP MEMBRANE, AT STA 560. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS AND INSTALLED IAW FAA APPROVED TEN NESSEE TECH DER ENGINEERING SKETCH NR EO 99-010 WITH 8110-3 DATED 01-25-99. (CORROSION DAMAGE RECORDED IN EWA CORROSIO N PROGRAM). 2 L 7 4 4F RT 4A25 2000012900381 20000129 00381 WP 2000 1 29 RRXA991028 1 19990210 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, FWD ACCESSORY COMPARTMENT FRAME AT STA 70, BETWEEN LONGERONS 33 LEFT AND LONGERON 31 LEFT, FRAME LOWER CHORD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TRE ATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLERS IAW DC8 SRM 53-2-5 AND INSTALLED IAW DC8 SRM 51-1-21 AND 51- 1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900382 20000129 00382 WP 2000 1 29 RRXA991029 1 19990114 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1306 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, AT STA 1306 UPPER CAP UNDER NUT PLATES AND WEB BETW EEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC -8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 53-02-0. (CORROSION DAMAGE RECORDED IN EWA CORR OSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900383 20000129 00383 WP 2000 1 29 RRXA991030 1 19990126 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, BILGE CORROSION FRAME AT STA 1040 BETWEEN LONGERONS 28 LEF T AND LONGERON 33 LEFT AT NUT PLATES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION P ROGRAM). 2 L 7 4 4F RT 4A25 2000012900384 20000129 00384 WP 2000 1 29 RRXA991031 1 19990114 A 5320 FRAME DOUG DC8 DC871F 302199D WP BS 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, DOOR FRAME, R2 FWD FRAME INSIDE WEB AT STA 1680. DAMAGE E XCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED FITTINGS IAW DC8 SRM 51-2-0 AND 53-4-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900385 20000129 00385 WP 2000 1 29 RRXA991032 1 19990211 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, FWD PIT AT STA 160, LOWER CAP, BETWEEN LONGERONS 3 4 RIGHT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED IAW DC8 SRM 53-2-0 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900386 20000129 00386 WP 2000 1 29 RRXA991033 1 19990114 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 13.750 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, WING, L/E SKIN, UNDER FASTENER RIGHT WING L/E UPPER SURFACE AT STA XFS 13.7 50 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900387 20000129 00387 WP 2000 1 29 RRXA991034 1 19990112 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, AFT COMPT AT STA 660 ATTACH POINT, LONGERON 34 LEF T. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED F ILLER AND DOUBLER IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900388 20000129 00388 WP 2000 1 29 RRXA991035 1 19990112 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 1620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, CUSP ANGLE, LT, AT STA 1620, L2 DOOR FRAME FITTING AND L ONGITUDIAL ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED L2 DOOR FRAME FITTING IAW DC8 SRM 51-1-3, 51-3-2, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSI ON PROGRAM). 2 L 7 4 4F RT 4A25 2000012900389 20000129 00389 WP 2000 1 29 RRXA991036 1 19990205 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME, BILGE CORROSION UNDER NUT PLATES TOP CAP AND AFT FA CE OF WEB FRAME AT STA 1260 BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMO VED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE TECH DER EN GINEERING SKETCH NR EO 99-002 AND 8110-3 DATED 01-18-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900390 20000129 00390 WP 2000 1 29 RRXA991037 1 19990111 A 5720 FITTING DOUG DC8 DC871F 302199D WP WS 3.125 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT, FOUND A CRACK, EXTENDING FROM BOLT HOLE RT I/B FLAP I/B HINGE ATTACH FITTING AT XW 3.125. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. MACHINE REPAIRED FITTING AND IN STALLED IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO 99-024 AND DC8 SRM 51-3-0. (CORROSION DAMAGE RECOR DED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900392 20000129 00392 WP 2000 1 29 RRXA991040 1 19990119 A 5320 3755847502 FITTING DOUG DC8 DC873 302199C WP BS 1151 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FORWARD HORIZONTAL FLANGE OF THE FITTING AT FS 1151, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED REPAIR ANGLE AND DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06124. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900393 20000129 00393 WP 2000 1 29 RRXA991041 1 19990114 A 5315 S2614462 FLOORBEAM DOUG DC8 DC873 302199C WP BS 8 - 70 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, DOUBLE DRILLED HOLES AND HOLES IN BEAM RADIOUS, FUSELAGE, MAIN CABIN FL OORBEAMS, UPPER FLANGES BETWEEN STA 8 AND STA 70 AT BL 46.5 RIGHT AND BL 46.5 LEFT. DAMAGE WAS CAUSED FROM A PREVIOUS M OD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FLOORBEAMS EXTRUSIONS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 53-0351, REV A AND DC8 SRM 51-1-21, 5 1-3-0, FIG 1F. 2 L 7 4 4F RT 4A25 2000012900394 20000129 00394 WP 2000 1 29 RRXA991042 1 19990119 A 5720 5751181 FITTING DOUG DC8 DC873 302199C WP WING WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND ATTACH FITTING WORN, RT I/B FLAP I/B ATTACH FITTING WORN AREA IS GREATER THAN 20 PERCE NT OF THE MATERIAL THICKNESS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06133. 2 L 7 4 4F RT 4A25 2000012900395 20000129 00395 WP 2000 1 29 RRXA991043 1 19990120 A 5315 561520259 FLOORBEAM DOUG DC8 DC873 302199C WP BS 857 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, FUSELAGE, FLOORBEAM, AT FS 857, AT BL 0 AND RL 20 RIGHT. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND DO UBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06137. 2 L 7 4 4F RT 4A25 2000012900396 20000129 00396 WP 2000 1 29 RRXA991045 1 19990120 A 5751 57631335 SKIN DOUG DC8 DC873 302199C WP WS 608 - 630 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND DAMAGE, SKIN, RT O/B UPPER SKIN RT O/B AILERON AT FWD AREA BETWEEN STA XA 630.250 AND 608.634. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06140. 2 L 7 4 4F RT 4A25 2000012900397 20000129 00397 WP 2000 1 29 RRXA991046 1 19990120 A 5320 561306481 ANGLE DOUG DC8 DC873 302199C WP BS 70 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND CRACK, AT A FASTENER HOLE, FUSELAGE, AFT 'L' ANGLE, AT FS70 AT LONGERON 36 IS CRACKE D OUT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 991045. 2 L 7 4 4F RT 4A25 2000012900398 20000129 00398 WP 2000 1 29 RRXA991047 1 19990120 A 5751 57631335 SKIN DOUG DC8 DC873 302199C WP AILERON DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND DAMAGE, UPPER SKIN, RT O/B AILERON AT STA XW 698. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM . REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO D ER ENGINEERING SKETCH NR REO- 06144. 2 L 7 4 4F RT 4A25 2000012900399 20000129 00399 WP 2000 1 29 RRXA991048 1 19990120 A 5720 5614372501 FITTING DOUG DC8 DC873 302199C WP WS 97.9 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND GOUGE, LT WING, CANOE FITTING, AT STA 97.906, ON OUTBD AFT EDGE. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AND REPAIRED IAW FAA APPROVED TIMCO DER EN GINEERING SKETCH NR REO- 06145. 2 L 7 4 4F RT 4A25 2000012900400 20000129 00400 WP 2000 1 29 RRXA991049 1 19990121 A 5315 2614462 FLOORBEAM DOUG DC8 DC873 302199C WP BS 70 & 200 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, DOUBLE DRILLED HOLES AND HOLES, FUSELAGE, MAIN CABIN FLOOR BEAMS AT VARI OUS LOCATIONS BETWEEN STA 70 AND STA 200. DAMAGE WAS CAUSED FROM A PREVIOUS MOD.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED FLOORBEAMS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-06148. 2 L 7 4 4F RT 4A25 2000012900401 20000129 00401 WP 2000 1 29 RRXA991050 1 19990121 A 5720 5751181 FITTING DOUG DC8 DC873 302199C WP WS 3 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND WORN AREA, WING, LT I/B FLAP ATTACH FITTING AT STA 3 WORN GREATER THAN 20 PERCENT OF T HE MATERIAL THICKNESS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDE D AND REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06151. 2 L 7 4 4F RT 4A25 2000012900402 20000129 00402 WP 2000 1 29 RRXA991051 1 19990122 A 5315 5613301503 FLOORBEAM DOUG DC8 DC873 302199C WP BS 960 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, FUSELAGE, FLOORBEAM AT FS 960 IN THE CAP AND VERTICAL FLANGE. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE A ND DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06152. 2 L 7 4 4F RT 4A25 2000012900403 20000129 00403 WP 2000 1 29 RRXA991052 1 19990123 A 5320 3750539501 NUTPLATE DOUG DC8 DC873 302199C WP BS 500 - 520 MISINSTALLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND NUTPLATES INSTALLED WHICH ARE NOT BEING USED, FUSELAGE, BETWEEN STA 500 AND STA 520, B ETWEEN LONGERONS 35 LEFT AND 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAP AND DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06161 . 2 L 7 4 4F RT 4A25 2000012900404 20000129 00404 WP 2000 1 29 RRXA991053 1 19990122 A 5711 56536221 SPAR DOUG DC8 DC873 302199C WP WS 97 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND CORROSION, WING, LT I/B FLAP REAR SPAR UPPER CAP AT STA XW 97. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SECTION OF SPAR , REPAIR ANGLES, AND EXTERNAL STRAP IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06163. (CORROSION DAMAGE RECO RDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900405 20000129 00405 WP 2000 1 29 RRXA991054 1 19990125 A 5320 37558442 FITTING DOUG DC8 DC873 302199C WP FUSELAGE MISMANUFACTURED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND P/N: 3755894-2 FITTING, FUSELAGE, MADE FROM P/N: 3755894-4 7075-T6 FORGING (MATERIAL S UBSTITUTION). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. SHOT PEEN FABRI CATED AND INSTALLED IAW DPS 4.999 OR DC8 SRM 51-1-4A, FINISH PART PER DAC DWG 3755844, ALL IAW FAA APPROVED TIMCO DER EN GINEERING SKETCH NR REO-06175. 2 L 7 4 4F RT 4A25 2000012900406 20000129 00406 WP 2000 1 29 RRXA991055 1 19990125 A 5315 3610417532 FLOORBEAM DOUG DC8 DC873 302199C WP BS 380 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND DOUBLE DRILLED, FUSELAGE, FLOORBEAM SUPPORT AT STA 380. DAMAGE EXCEEDED LIMITS IAW DC -8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06180. 2 L 7 4 4F RT 4A25 2000012900407 20000129 00407 WP 2000 1 29 RRXA991056 1 19990125 A 5311 56402323 FRAME DOUG DC8 DC873 302199C WP BS 1460 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND GOUGE, FUSELAGE, FRAME AT STA 1460 BETWEEN LONGERONS 35 LEFT AND LONGERON 34 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06178. 2 L 7 4 4F RT 4A25 2000012900408 20000129 00408 WP 2000 1 29 RRXA991057 1 19990125 A 5320 39250 DOOR FRAME DOUG DC8 DC873 302199C WP BS 465 - 495 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CRACK, MAIN CARGO DOOR FRAMES AT FS 465 AND FS 495 LOWER LATCH MOUNTS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR CHANNEL IAW F AA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06181. 2 L 7 4 4F RT 4A25 2000012900409 20000129 00409 WP 2000 1 29 RRXA991058 1 19990126 A 5511 565174762 PANEL DOUG DC8 DC873 302199C WP HORIZ STAB DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DELAMINATION, LT HORIZ STAB LOWER T/E PANEL APPROX STA XE 149.155. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HORIZ STAB LOWER T/E PANEL IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06191. 2 L 7 4 4F RT 4A25 2000012900410 20000129 00410 WP 2000 1 29 RRXA991059 1 19990126 A 5511 565174764 PANEL DOUG DC8 DC873 302199C WP HORIZ STAB DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DELAMINATION, LT HORIZ STAB LOWER T/E PANEL APPROX STA XE 221.227. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HORIZ STAB LOWER T/E PANEL IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06192. 2 L 7 4 4F RT 4A25 2000012900411 20000129 00411 WP 2000 1 29 RRXA991060 1 19990126 A 5511 565174766 PANEL DOUG DC8 DC873 302199C WP HORIZ STAB DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DELAMINATION, LT HORIZ STAB LOWER T/E PANEL APPROX STA XE 272.280. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HORIZ STAB LOWER T/E PANEL IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06193. 2 L 7 4 4F RT 4A25 2000012900412 20000129 00412 WP 2000 1 29 RRXA991061 1 19990203 A 5531 3651630 FITTING DOUG DC8 DC873 302199C WP RUDDER SPAR MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR 61.156 HAS OVERSIZED ATTACH HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW OVERSIZ ED BUSHING IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06194. 2 L 7 4 4F RT 4A25 2000012900413 20000129 00413 WP 2000 1 29 RRXA991062 1 19990202 A 5315 97537662 FLOORBEAM DOUG DC8 DC873 302199C WP BS 160 - 180 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE, FLOORBEAM, AT STA 160 AND STA 180, CRACKED AT APPROX BL 40 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS, ANGLES, AND DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06195. 2 L 7 4 4F RT 4A25 2000012900414 20000129 00414 WP 2000 1 29 RRXA991063 1 19990202 A 5315 97537662 FLOORBEAM DOUG DC8 DC873 302199C WP BS 160 - 180 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE, FLOORBEAM AT STA 160 AND STA 180, BL 40 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS, ANGLES, AND DOUBLER S IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06195. 2 L 7 4 4F RT 4A25 2000012900415 20000129 00415 WP 2000 1 29 RRXA991064 1 19990126 A 5330 5613861371 SKIN DOUG DC8 DC873 302199C WP BS 70 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DRILL DAMAGE, FUSELAGE, SKIN PANEL, JUST FWD OF STA 70 BETWEEN LONGERONS 21 LEFT AND LO NGERON 23 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AN D INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06199. 2 L 7 4 4F RT 4A25 2000012900416 20000129 00416 WP 2000 1 29 RRXA991065 1 19990128 A 5730 576954590 SKIN DOUG DC8 DC873 302199C WP WS 716.250 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DAMAGE, RIGHT WING, O/B L/E LWR SIDE SKIN AT APPROX STA XFS 716.250. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH #REO- 06200. 2 L 7 4 4F RT 4A25 2000012900417 20000129 00417 WP 2000 1 29 RRXA991066 1 19990210 A 5720 MOUNT DOUG DC8 DC873 302199C WP NR 4 PYLON MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND NUMEROUS OVERSIZED HOLES, NR 4 PYLON MOUNT AREA. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06204. 2 L 7 4 4F RT 4A25 2000012900418 20000129 00418 WP 2000 1 29 RRXA991067 1 19990128 A 5320 57112835141379 FITTING DOUG DC8 DC873 302199C WP FUSELAGE MISMANUFACTURED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND MATERIAL SUBSTITUTION, P/N: 5711283-514-1379 FITTING IS MADE FROM P/N: 4710626-7075-T6 FORGING. REQUEST TO FAB FROM ALUMINUM BAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC -8 SRM 51-1-8. FABRICATED AND INSTALLED SHOT PEEN IAW DPS 4.999 OR DC8 SRM 51-1-4A, ALL IAW FAA APPROVED TIMCO DER ENGI NEERING SKETCH NR REO-06206. 2 L 7 4 4F RT 4A25 2000012900419 20000129 00419 WP 2000 1 29 RRXA991068 1 19990129 A 5320 FITTING DOUG DC8 DC873 302199C WP BS 510 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CRACKED SPLICE FITTING AT STA 510, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW FAA APPROVED TIMCO DE R ENGINEERING SKETCH NR REO- 06218. 2 L 7 4 4F RT 4A25 2000012900420 20000129 00420 WP 2000 1 29 RRXA991069 1 19990201 A 5720 36161123 FITTING DOUG DC8 DC873 302199C WP WING MISMANUFACTURED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND MATERIAL SUBSTITUTION, P/N: 3616112-3 FITTING IS MADE FROM P/N: 3616111 7075-T6 FORGIN G. REQUEST TO FAB FROM ALUMINUM BAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED AND INSTALLED SHOT PEEN IAW DPS 4.999 OR DC8 SRM 51-1-4A, ALL IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-06223. 2 L 7 4 4F RT 4A25 2000012900421 20000129 00421 WP 2000 1 29 RRXA991070 1 19990201 A 5315 97537661 FLOORBEAM DOUG DC8 DC873 302199C WP BS 21 - 25 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND A TRIM OUT, FUSELAGE, LONGITUDINAL FLOORBEAM AT BL 11.5 RIGHT FROM STA 21 TO STA 25 IN THE UPPER HORIZONTAL FLANGE AND A BLEND OUT IN THE VERTICAL FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAG ED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06226. 2 L 7 4 4F RT 4A25 2000012900422 20000129 00422 WP 2000 1 29 RRXA991071 1 19990215 A 5711 5597838501 SPAR DOUG DC8 DC873 302199C WP NR 1 PYLON MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED, WING, FWD LWR SPAR CAP AT PYLON NR 1, STA XW 467.0, ONE EACH HOLE DOUBL E DRILLED IN SPAR, INTERNAL DOUBLER, AND LOWER WING SKIN IN TEE DOUBLER OUT OF ROUND, PAST 3RD OVERSIZE. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06228. 2 L 7 4 4F RT 4A25 2000012900423 20000129 00423 WP 2000 1 29 RRXA991072 1 19990204 A 5315 97510691 FLOORBEAM DOUG DC8 DC873 302199C WP BS 680 MISREPAIRED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND TWO CUTOUTS, FUSELAGE, FLOORBEAM, UPPER FORWARD FLANGE, AT STA 680. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPRO VED TIMCO DER ENGINEERING SKETCH NR REO- 06242. 2 L 7 4 4F RT 4A25 2000012900424 20000129 00424 WP 2000 1 29 RRXA991073 1 19990204 A 5315 9750472511 FLOORBEAM DOUG DC8 DC873 302199C WP BS 1140 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DAMAGE, FUSELAGE, FLOORBEAM AT STA 1140, BL 0.0, NO SRM. DAMAGE EXCEEDED LIMITS IAW DC -8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SHIM, ANGLE, AND DOUBLER IA W FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06249. 2 L 7 4 4F RT 4A25 2000012900425 20000129 00425 WP 2000 1 29 RRXA991074 1 19990204 A 5311 97510691 FRAME DOUG DC8 DC873 302199C WP BS 1140 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLE, FUSELAGE, FRAME AT STA 1140, LONGERON 35 LEFT AT AN INTERCOSTAL LOCAT ION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06244. 2 L 7 4 4F RT 4A25 2000012900426 20000129 00426 WP 2000 1 29 RRXA991075 1 19990208 A 5320 577263917 DOOR PAN DOUG DC8 DC873 302199C WP FUSELAGE MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND MISDRILLED, AFT SERVICE DOOR, AFT LWR DOOR PAN, IN TWO PLACES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE, FILLER, AND DO UBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06271. 2 L 7 4 4F RT 4A25 2000012900427 20000129 00427 WP 2000 1 29 RRXA991076 1 19990209 A 5315 S2640868 FLOORBEAM DOUG DC8 DC873 302199C WP BS 660 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND MISDRILLED, FLOORBEAM, AT STA 660, UPPER FLANGES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-0627 3 AND DC08-53-0351, REV A. 2 L 7 4 4F RT 4A25 2000012900428 20000129 00428 WP 2000 1 29 RRXA991077 1 19990209 A 5315 S459047 FLOORBEAM DOUG DC8 DC873 302199C WP BS 52 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND GOUGE, FLOORBEAM, FUSELAGE, AT STA 52, UPPER AFT FLANGE HAS DEEP TOOL GOUGE AT BL 36 LE FT ON UNDERSIDE OF FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RE PAIRED IAW FAA APPROVED TIMCO DER ENGINERING SKETCH NR REO-06277 AND DC08-53-0351,REV A. 2 L 7 4 4F RT 4A25 2000012900429 20000129 00429 WP 2000 1 29 RRXA991078 1 19990209 A 5320 S4594047 JAMB DOUG DC8 DC873 302199C WP BS 1660 - 1666 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED IN VARIOUS LOCATIONS, L-2 ENTRY DOOR AFT JAMB AT STA 1666 AND STA 1660. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPA IR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06279 2 L 7 4 4F RT 4A25 2000012900430 20000129 00430 WP 2000 1 29 RRXA991079 1 19990211 A 3230 57591201 BORE DOUG DC8 DC873 302199C WP MLG LINK OVERSIZED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND BORE OVERSIZED, MAIN LANDING GEAR LINK BORE, AND HAS ONE LOCATION OF LOCAL BLENDING. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR BUSHINGS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO- 06288. 2 L 7 4 4F RT 4A25 2000012900431 20000129 00431 WP 2000 1 29 RRXA991080 1 19990212 A 5541 3651630 FITTING DOUG DC8 DC873 302199C WP RUDDER DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND AN OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR=61.156. DAMAGE EXCEEDED LIMITS IAW DC -8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR BUSHING IAW FAA APPROVED TIM CO DER ENGINEERING SKETCH NR REO- 06298. 2 L 7 4 4F RT 4A25 2000012900432 20000129 00432 WP 2000 1 29 RRXA991081 1 19990602 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 360, AFT SIDE ABOVE LONGERONS 31 RIGHT AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED REPAIR ANGLE IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110-3, D ATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900433 20000129 00433 WP 2000 1 29 RRXA991082 1 19990602 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 702 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM FUSELAGE SKIN AT STA 702, LONGERON 36. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROV ED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110-3 DATED MAY 21, 1999. (CORROSION DAM AGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900434 20000129 00434 WP 2000 1 29 RRXA991083 1 19990602 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 717 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM SKIN AT STA 717, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW D C-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESS EE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDE D IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900435 20000129 00435 WP 2000 1 29 RRXA991084 1 19990602 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 680 - 702 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, BOTTOM OF FUSELAGE BEACON ANTENNA FROM BASE AND AROUND SKIN BETWEEN STA 680 AND STA 702. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IN STALLED DOUBLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900436 20000129 00436 WP 2000 1 29 RRXA991085 1 19990602 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LAV SERVICE DOOR FROM HINGE AT STA 80, LONGERON 24 RIGHT, FUSELAGE SKIN UND ER HINGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED DOUBLER IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900437 20000129 00437 WP 2000 1 29 RRXA991086 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 878.750 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, O/B L/E O/B SEGMENT LOWER SURFACE AT XFS 878.750. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900438 20000129 00438 WP 2000 1 29 RRXA991087 1 19990602 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CHAFFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND PANEL 86 RUBBING ON FUSELAGE LT SIDE OF LOWER RUDDER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED OUT IAW DC8 SRM 51-1-8, LIMITS ACCEPTABLE PER FAA APP ROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900439 20000129 00439 WP 2000 1 29 RRXA991088 1 19990602 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DELAMINATION, RUDDER TUB DELAMINATED LT SIDE AFT OF LOWER HINGE. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED RUDDER TAB IAW DC8 M/M 27-21- 1. 2 L 7 4 4F RT 4A25 2000012900440 20000129 00440 WP 2000 1 29 RRXA991090 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 7.50 - 26.25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN XFS 7.50 TO XFS 26. 250.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D FILLERS AND DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110- 3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900441 20000129 00441 WP 2000 1 29 RRXA991091 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 7.50 - 26.25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN XFS 7.50 AND XFS 26 .250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND D OUBLER IAW DC8 SRM 57-2-1 AND INSTALLED IAW DC9 SRM 57-2-1 AND 51-1-12. (CORROSION DAMAGE RECORDED IN EWA CORROSION PRO GRAM). 2 L 7 4 4F RT 4A25 2000012900442 20000129 00442 WP 2000 1 29 RRXA991092 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B L/E O/B SEGMENT I/B EDGE AT STA XFS 710. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 57-2-1 AND INSTALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900443 20000129 00443 WP 2000 1 29 RRXA991093 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A .25 INCH CRACK, RIGHT WING, EXTENDING FROM SCREW HOLE RIGHT WING O/B L/E I/B SEGMENT O/B EDGE AT STA XFS 710. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABR ICATED FILLER AND DOUBLER IAW DC8 SRM 51-2-1 AND INSTALLED IAW DC8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2000012900444 20000129 00444 WP 2000 1 29 RRXA991096 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 878.75 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION AND CRACKS, RIGHT WING, I/B L/E O/B SEGMENT LOWER SURFACE AT XFS 878.750. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND FILLER IA W DC8 SRM 57-2-1 AND INSTALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900445 20000129 00445 WP 2000 1 29 RRXA991097 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 566.25 - 603 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION AND CRACKS, RIGHT WING, O/B L/E I/B SEGMENT UPPER SURFACE BETWEEN STA XFS 566 .250 TO XFS 603.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED FILLER AND DOUBLER IAW DC8 SRM 57-2-1 AND INSTALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900446 20000129 00446 WP 2000 1 29 RRXA991098 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 491 & 503 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CRACKS, RIGHT WING, L/E JUST FWD O/B SLOT AT STA XFS 503.789 AND STA XFS 491.193. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. CRACKS ACCEPTABLE AS IS PER FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKET CH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900447 20000129 00447 WP 2000 1 29 RRXA991099 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 193.675 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACE AT XFS 193.675. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 57-2-1 AND INS TALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900448 20000129 00448 WP 2000 1 29 RRXA991100 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND SCREWS MISSING, RIGHT WING, L/E DOUBLER O/B END OF O/B SLOT, MISSING, LOOSE, AND PULLIN G THROUGH. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED DOUBLER IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900449 20000129 00449 WP 2000 1 29 RRXA991101 1 19990602 A 5522 PANEL DOUG DC8 DC873F 302199F WP ELEVATOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, AREA UNDER PANEL 69 LT ELEV INSIDE THROUGHOUT AREA BETWEEN XE 32.937 TO XE 50.000 FWD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED CORROSIO N IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 199 9. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900450 20000129 00450 WP 2000 1 29 RRXA991102 1 19990602 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1726 - 1745 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 36 BETWEEN STA 1726 AND STA 1745. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR SPLICE IAW DC8 SRM 53-2-1 AND 51-1- 21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900451 20000129 00451 WP 2000 1 29 RRXA991103 1 19990602 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT UPPER CUSP FRAME 560 AT STA 560 ATTACH ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ATTACH ANGLE IAW DC8 SRM 51-1-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900452 20000129 00452 WP 2000 1 29 RRXA991104 1 19990602 A 5720 FLANGE DOUG DC8 DC873F 302199F WP WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, NR 2 STUB WING, 9.75 LEFT WING NR 2 STUB WING I/B FLANGE. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900453 20000129 00453 WP 2000 1 29 RRXA991105 1 19990602 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DAMAGE, NR 1 LT FLAP WEDGE LOWER SKIN. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED D AMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES D ER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900454 20000129 00454 WP 2000 1 29 RRXA991106 1 19990602 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 8 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 33 RIGHT END TIE FITTING IN FWD ACCESSORY BAY AT STA 8.00 . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FI TTING IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900455 20000129 00455 WP 2000 1 29 RRXA991107 1 19990602 A 5753 FLANGE DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, RIGHT WING, O/B FLAP, NR 3 WEDGE I/B LOWER MOUNTING FLANGE. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NUT PLATE IAW FAA APPR OVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900456 20000129 00456 WP 2000 1 29 RRXA991108 1 19990602 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, LEFT WING, O/B FLAP LOWER SURFACE SKIN BULGED AND 2 CRACK 3 BELOW L/E, JUST UN DER CENTER HINGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900457 20000129 00457 WP 2000 1 29 RRXA991109 1 19990602 A 5754 SKIN DOUG DC8 DC873F 302199F WP LE FALP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING L/E, IMPROPER REPAIR LEFT WING O/B L/E O/B SECTION LWR SURFACE BET WEEN STA 822.50 TO XFS 841.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 . FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGR AM). 2 L 7 4 4F RT 4A25 2000012900458 20000129 00458 WP 2000 1 29 RRXA991110 1 19990602 A 5320 GUARD DOUG DC8 DC873F 302199F WP BS 210 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, CABIN, LONG SECTION OF MAIN CARGO SEAL GUARD BUMP RAIL AT STA 210 (EO). DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. WELDED CRACKED AREA IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3 DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900459 20000129 00459 WP 2000 1 29 RRXA991111 1 19990602 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE, C/D PIT DIVIDER AND SUPPORT FORMER CRACKED AND TORN. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PARTITION IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900460 20000129 00460 WP 2000 1 29 RRXA991112 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 95 -101.25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING L/E, TANK UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 95.000 AND XFS 101.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKET CH #EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900461 20000129 00461 WP 2000 1 29 RRXA991113 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 151 - 157 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING L/E, I/B L/E TANK UPPER SURFACE AROUND SCREW HOLES BETWEEN XFS 15 1.205 AND XFS 157.500. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WIT H APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900462 20000129 00462 WP 2000 1 29 RRXA991114 1 19990602 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 280 CRACK A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE A PIT FRAME DOOR BETWEEN BOLTS AT STA 280, BETWEEN LONGERONS 26 RIGHT AND LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED FRAME PER DWG NR 2772795 AND INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2000012900463 20000129 00463 WP 2000 1 29 RRXA991115 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 304 - 397 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING L/E, AROUND SCREW HOLES LEFT WING L/E CENTER SECTION UPPER SURFACE BETWEEN XFS 304.000 TO XFS 397.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900464 20000129 00464 WP 2000 1 29 RRXA991116 1 19990602 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS, AT STA 1680, BL 14 LEFT. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW SUPPORT AND INSTALLED IAW DC8 SR M 51-1-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900465 20000129 00465 WP 2000 1 29 RRXA991117 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 227.335 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, NR 3 STUB WING, UPPER SURFACE EMANATING FROM RIVET 2 FWD OF FRONT SPAR AT STA XS 227.335. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IN STALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8 110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900466 20000129 00466 WP 2000 1 29 RRXA991118 1 19990602 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1680 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS, AT STA 1680 BL 35 LEFT. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51- 1-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900467 20000129 00467 WP 2000 1 29 RRXA991119 1 19990602 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION CRACKS, FUSELAGE, FLOOR SUPPORTS AT STA 1700 BL 29 LEFT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1 -21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900468 20000129 00468 WP 2000 1 29 RRXA991120 1 19990602 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT AT STA 1726, BL 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900469 20000129 00469 WP 2000 1 29 RRXA991121 1 19990602 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1746 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT UNDER CLIP NUTS AT STA 1746 BETWEEN BL 1-1/2 LEFT AN D 20-1/2. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED H CHANNEL AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900471 20000129 00471 WP 2000 1 29 RRXA991123 1 19990602 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, FUSELAGE, LOWER ATTACH FITTING IN BOX FRAME AT STA 280, LONGERON 27 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-8 AND 51-1-21. 2 L 7 4 4F RT 4A25 2000012900472 20000129 00472 WP 2000 1 29 RRXA991124 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 385 - 388 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, L/E BETWEEN NR 3 AND NR 4 ENG JUST O/B OF STALL WARNING TRANSDUC ER BETWEEN XSF 385 AND XFS 388. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 . FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99 -085 WITH APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900473 20000129 00473 WP 2000 1 29 RRXA991125 1 19990602 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM UNDER SEAT TRACK 3 ABOVE LONGERON 32 LEFT AT STA 1700. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110-3, DATED MAY 21 , 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900474 20000129 00474 WP 2000 1 29 RRXA991126 1 19990602 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1746 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN, JUST FWD OF TAIL SKID AT STA 1746, LONGERON 36. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-1, INSTALLED FILLER AND DOUBLER IAW DC8 SRM 51-1-21 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2000012900475 20000129 00475 WP 2000 1 29 RRXA991127 1 19990528 A 2810 FLOAT BOX DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, LEFT WING, NR 1 ALT FLOAT BOX 2.5 CRACK IN WELD. DAMAGE EXCEEDED LIMITS IAW D C-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED FLOAT BOX, WELDED CRACK SECTION IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999, INSTALLED FLOAT B OX IAW DC8 M/M 28-21-14. 2 L 7 4 4F RT 4A25 2000012900476 20000129 00476 WP 2000 1 29 RRXA991128 1 19990602 A 2810 FLOAT BOX DOUG DC8 DC873F 302199F WP RT WING TWISTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND TUBE TWISTED, RIGHT WING, NR 4 A FLOAT BOX WELDED TUBE TWISTED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED FLOAT BOX, WELDED TUBE IN PLACE IAW FAA APPR OVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999, INSTALLED FLO AT BOX IAW DC8 SRM 28-21-14. 2 L 7 4 4F RT 4A25 2000012900477 20000129 00477 WP 2000 1 29 RRXA991129 1 19990602 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 460 - 480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, B-PIT LEFT FWD BETWEEN STA 460 AND STA 480 LEFT AT LONGERON 31 LEF T. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED F ILLERS AND DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3, D ATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900478 20000129 00478 WP 2000 1 29 RRXA991130 1 19990602 A 5720 FASTENER DOUG DC8 DC873F 302199F WP WS 463 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND DAMAGE, RIGHT WING, FASTENER DAMAGED INSIDE NR 4 ALT FUEL TANK BY NR 4 PYLON AT XW 463 STR 58 LOWER SURFACE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. FASTENER OK AS IS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO- 99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900479 20000129 00479 WP 2000 1 29 RRXA991131 1 19990602 A 5415 ANGLE DOUG DC8 DC873F 302199F WP NR 1 PYLON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND A CRACK, NR 1 PYLON, I/B TRIPLER (ANGLE) CRACKED 1.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ANGLES IAW DC8 SRM 51-1-6 AND 51-1-7, 51 -1-20D. 2 L 7 4 4F RT 4A25 2000012900480 20000129 00480 WP 2000 1 29 RRXA991132 1 19990602 A 5520 FITTING DOUG DC8 DC873F 302199F WP ELEVATOR GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND GOUGE, RIGHT ELEV, RT GEAR TAB ASSY, I/B FITTING GOUGED. DAMAGE EXCEEDED LIMITS IAW DC -8 SRM. BLENDED GEARED TAB I/B FITTING IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WIT H APPROVED 8110-3 DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900481 20000129 00481 WP 2000 1 29 RRXA991133 1 19990602 A 3230 PIN DOUG DC8 DC873F 302199F WP LT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG, RETRACT CYL A-PIN REPAIR PER CUSTOMER REQUEST IAW MA A13210-01:03 S/ B 32-102 REF. AD 71-25-09. ACCOMPLISHED INSPECTION FOUND CORROSION IN PIN BOSS.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING S KETCH NR EO- 99-085 WITH APPROVED 8110-3, DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900482 20000129 00482 WP 2000 1 29 RRXA991134 1 19990602 A 3230 PIN DOUG DC8 DC873F 302199F WP RT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG, RETRACT CYL. A PIN REPAIR PER CUSTOMER REQUEST IAW MA AI 3210-01:03 S/B 32-102, REF AD 71-25-09. ACCOMPLISHED INSPECTION, FOUND CORROSION, IN PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 S RM. REMOVED DAMAGED, TREATED AREA IAW DC8 SRM 51-1-8. REPAIRED IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERIN G SKETCH NR EO-99-085 WITH APPROVED 8110-3 DATED MAY 21, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900483 20000129 00483 WP 2000 1 29 RRXA991135 1 19990602 A 3230 PIN DOUG DC8 DC873F 302199F WP LT MLG DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND SPIRALED TOP AND BOTTOM HOLES, LEFT MLG RETRACT PIN BOSS THROUGH BOLT HOLE. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. SMOOTHED BORE, FLAP PEENED HOLE IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITH APPROVED 8110-3 DATED MAY 21, 1999. 2 L 7 4 4F RT 4A25 2000012900484 20000129 00484 WP 2000 1 29 RRXA991136 1 19990102 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN AT APPROX STA 1680, BETWEEN LONGERON 18 LEFT TO LONGERON 18 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED DOUBLER AND FILLER IAW DC8 SRM 53-2-1, FIG 7. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900485 20000129 00485 WP 2000 1 29 RRXA991137 1 19990108 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 1228 & 1292 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON, AFT CARGO COMPARTMENT, LONGERON 34 RIGHT, BETWEEN STA 12 28 AND STA 1292, UNDERNEATH DOOR THRESHOLD PLATE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA I AW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED COMMODORE DER ENGINEERING SKETCH NR EAF-MIA-99-00 10RR. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900486 20000129 00486 WP 2000 1 29 RRXA991138 1 19990101 A 5730 SKIN DOUG DC8 DC863 302198A WP BS 960 - 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WHEEL WELL PRESS DECK SKIN FROM FS 980 TO FS 960 AND I/B FIST HAT SECTI ON STIFFENER AND AROUND FITTING AT FS 960, BETWEEN LONGERON 24 LEFT AND CEILING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 53-2-0 PG 1B. (CORROSI ON DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900487 20000129 00487 WP 2000 1 29 RRXA991139 1 19990129 A 5741 FITTING DOUG DC8 DC863 302198A WP WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT W/W OVERHEAD O/B SIDE STUB FITTING AT LONGERON 24 LEFT. DAMAGE E XCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0 PG 43/44. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900488 20000129 00488 WP 2000 1 29 RRXA991140 1 19990104 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP BS 1700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FLOORBEAM, AT STA 1700, BL 20 LEFT, WL -2. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-0 AND 51-1-20D. (COR ROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900489 20000129 00489 WP 2000 1 29 RRXA991141 1 19990104 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP BS 1702 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FLOORBEAM, AT LIGHTING HOLE, STA 1702, BL 24 RIGHT, WL -6. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW FAA APPROVE D COMMODORE DER ENGINEERING SKETCH NR EAF-MIA-99-0004RR. 2 L 7 4 4F 4A25 2000012900490 20000129 00490 WP 2000 1 29 RRXA991142 1 19990106 A 5320 BRACKET DOUG DC8 DC863 302198A WP BS 620 - 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, BRACKET, CABIN FLOOR TRACK BRACKET BETWEEN STA 620 AND STA 660 AT BL 59 LEFT , WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED NEW SEAT TRACK SECTION IAW DC8 SRM 51-3-0 PG1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900491 20000129 00491 WP 2000 1 29 RRXA991143 1 19990105 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 480 - 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 480 AND STA 520, BL 44 LEFT, WL 0. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW SEAT TRACK SECTI ON AND INSTALLED SEAT TRACK AND FLOOR PANELS IAW DC8 SRM 51-3-0 PG 1 AND 53-1-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900492 20000129 00492 WP 2000 1 29 RRXA991144 1 19990106 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 920 - 960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 920 AND STA 960, BL 59 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW SEAT TRACK SECTION AN D INSTALLED IAW DC8 SRM 51-3-0 PG 1 AND 53-1-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900493 20000129 00493 WP 2000 1 29 RRXA991145 1 19990106 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1300 - 1360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1300 AND STA 1360 AT BL 59 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEC TION OF SEAT TRACK IAW DC8 SRM 51-3-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900494 20000129 00494 WP 2000 1 29 RRXA991146 1 19990106 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1180 - 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1180 AND STA 1200 AT BL 59 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEA T TRACK SECTION IAW DC8 SRM 53-1-0 PG 1 AND 51-3-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900495 20000129 00495 WP 2000 1 29 RRXA991147 1 19990106 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1300 - 1320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1300 AND STA 1320, BL 44 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW DC8 SRM 53-1-0 PG 1 AND 51-3-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900496 20000129 00496 WP 2000 1 29 RRXA991148 1 19990106 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1280 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1280 AND STA 1300 AT BL 59 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEA T TRACK SECTION IAW DC8 SRM 51-3-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900497 20000129 00497 WP 2000 1 29 RRXA991149 1 19990106 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1280 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1280 AND STA 1300 AT BL 44 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEA T TRACK SECTION IAW DC8 SRM 51-3-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900498 20000129 00498 WP 2000 1 29 RRXA991150 1 19990126 A 5315 FLOORBEAM DOUG DC8 DC863 302198A WP BS 1727 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOORBEAM LOWER ATTACHING CHORD AT STA 1727, BETWEEN BL 24 R IGHT AND BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACHING CHORD IAW DC8 SRM 51-1-21 PG.1, 51-1-9 PG1, 51-1-8 PG 1, 51-1-21 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900499 20000129 00499 WP 2000 1 29 RRXA991151 1 19990106 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1380 - 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 1380 AND STA 1440 AT BL 59 LEFT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED N EW SEAT TRACK SECTION IAW DC8 SRM 53-1-0 PG 1 AND 51-3-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900500 20000129 00500 WP 2000 1 29 RRXA991152 1 19990104 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 240 - 329 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK AT BL 44 LEFT, BETWEEN STA 240 AND STA 329. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900501 20000129 00501 WP 2000 1 29 RRXA991154 1 19990623 A 5270 SWITCH DOUG DC8 DC863 302198A WP CARGO DOOR OUT OF ADJUST A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 797AL 46163 PASSING FL 10.0 AT DIFF PRESS 4 PSI MAIN CARGO DOOR WARNING LIGHT IN THE COCKPIT AND BY THE DOOR ILLUMINATED DEPRESSURIZ ED THE CABIN AT 2 1/2 DIFF PRESS WARNING LIGHT GOES OUT. ADJUSTED CARGO DOOR CLOSED SWITCH AND ADJUSTED TENSION ON GANG BAR IAW ROSENBALM AVIATION MM PG 5-3 PRESSURIZED AIRCRAFT TO 6.5 PSI DIFF PRESS NO LIGHTS NOTED DOOR CLOSES AND LATCHES CORRECTLY AT THIS TIME. 2 L 7 4 4F 4A25 2000012900502 20000129 00502 WP 2000 1 29 RRXA991155 1 19990105 A 5753 5653509501 SPAR DOUG DC8 DC873 302199C WP TE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING OUT-BOARD FLAP REAR SPAR CAP BETWEEN XF=404 TO XF=405, D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR S PLICE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-06126. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900503 20000129 00503 WP 2000 1 29 RRXA991156 1 19990105 A 5753 5653509501 SPAR DOUG DC8 DC873 302199C WP TE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, OUT-BOARD FLAP, SPAR CAP AT XF=410, DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPR OVED TIMCO DER ENGINEERING SKETCH REO-06123. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900504 20000129 00504 WP 2000 1 29 RRXA991157 1 19990119 A 5311 FRAME DOUG DC8 DC873 302199C WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 70 BETWEEN LONGERONS 21 LEFT TO 34 RIGHT, DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-06199. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900505 20000129 00505 WP 2000 1 29 RRXA991158 1 19990118 A 5753 5653509501 SPAR DOUG DC8 DC873 302199C WP TE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, OUTBOARD FLAP, REAR SPAR CAP AT XW=220, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-06125. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900506 20000129 00506 WP 2000 1 29 RRXA991159 1 19990121 A 5753 5653509502 SPAR DOUG DC8 DC873 302199C WP TE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD FLAP, REAR SPAR CAP AT XF=225, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-06154. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900507 20000129 00507 WP 2000 1 29 RRXA991160 1 19990129 A 5313 975491334 LONGERON DOUG DC8 DC873 302199C WP BD 260 - 300 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT FOUND A CRACK AND CORROSION, FUSELAGE, LONGERON 36 BETWEEN STA 260 AND STA 300. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SECTION OF LONGERON IAW DAC DWG NR 9754913 AND DC8 SRM 53-2-2 FIG 10, SHT 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) . 2 L 7 4 4F RT 4A25 2000012900508 20000129 00508 WP 2000 1 29 RRXA991161 1 19990203 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 230 - 270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN FINGER DOUBLER BETWEEN STA 230 TO 270 AND LONGERON 21 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED NEW FINGER DOUBLER IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900509 20000129 00509 WP 2000 1 29 RRXA991162 1 19990201 A 5311 FRAME DOUG DC8 DC862F 3021972 WP BS 220 - 235 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME ALONG LONGERON ATTACHMENT POINTS BETWEEN STA 220 TO 235 BETWE EN LONGERONS 25 RIGHT TO 26 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51 -1-8. FABRICATED AND INSTALLED REPAIR DOUBLER SPLICE IAW FAA APPROVED COMMODOR DER ENGINEERING SKETCH 18R5311076. (COR ROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900511 20000129 00511 WP 2000 1 29 RRXA991164 1 19990127 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 330 - 390 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 330 TO STA 390 AND BL 48 RIGHT, DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER SPLICE IAW DC-8 SRM 53-2-3 FIGURE 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900512 20000129 00512 WP 2000 1 29 RRXA991165 1 19990218 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 250 - 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL AND SEAT TRACK BETWEEN STA 250 TO STA 300 AND BL 44 LEF T, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3 FIGURE 13. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900513 20000129 00513 WP 2000 1 29 RRXA991166 1 19990110 A 3230 FITTING DOUG DC8 DC862F 3021972 WP LT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SUPPORT FITTING IN LEFT MAIN LANDING GEAR AREA AT STA 920 AND LONGE RON 24 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW S UPPORT FITING AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900514 20000129 00514 WP 2000 1 29 RRXA991167 1 19990110 A 3230 FITTING DOUG DC8 DC862F 3021972 WP LT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SUPPORT FITTING IN LEFT MAIN LANDING GEAR AREA AT STA 940 AND LONGE RON 24 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW S UPPORT FITING AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900515 20000129 00515 WP 2000 1 29 RRXA991176 1 19990406 A 5320 ANGLE DOUG DC8 DC862F 3021972 WP BS 879 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE, RT W/W AT STA 879, BL 0, WL 16 RIGHT. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC8 SRM 51-1-4 (PAGE 1); FABRICATED AND INSTALLED 2 EACH SHIMS WITH BRACKET IAW DC8 SRM 51-1-2 AND 51-1-20 (PAGE 1). (CORR OSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900516 20000129 00516 WP 2000 1 29 RRXA991177 1 19990312 A 5315 FLOOR BEAM DOUG DC8 DC862F 3021972 WP BS 940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TOP SIDE OF PRESSURE WEB AND FLOOR BEAM JOINT AT STA 940, BL 67 RI GHT.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D REPAIR DOUBLER IAW BOEING DRAWING NR SRO 8530026. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900517 20000129 00517 WP 2000 1 29 RRXA991178 1 19990312 A 5315 FLOOR BEAM DOUG DC8 DC862F 3021972 WP BS 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TOP SIDE OF PRESSURE WEB AND FLOOR BEAM JOINT AT STA 920, BL 67 RI GHT.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D REPAIR DOUBLER IAW FAA APPROVED COMMODORE DER ENGINEERING SKETCH NR EAF-MIA 99-0016-44 AND DC8 SRM 51-1-20. (CORROSIO N DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900518 20000129 00518 WP 2000 1 29 RRXA991179 1 19990306 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT FUSELAGE SKIN AT STA 270 AND LONGERON 30 RIGHT. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-3-2 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900519 20000129 00519 WP 2000 1 29 RRXA991180 1 19990314 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 857 & 879 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN INT UNDER FLOOR PLANK TOP OF MLG W/W BETWEEN STA 857 AND STA 879 AT BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED COMMODORE DER ENGINEERING SKETCH NR EAF-MIA--99-0016RR. (CORROSION DAMAGE REC ORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900520 20000129 00520 WP 2000 1 29 RRXA991181 1 19990314 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 879 - 902 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN INT UNDER FLOOR PLANK TOP OF MLG W/W BETWEEN STA 879 TO STA 902 AT BL 69 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED COMMODORE DER ENGINEERING SKETCH #EAF-MI - 99-001644. (CORROSION DAMAG E RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900521 20000129 00521 WP 2000 1 29 RRXA991182 1 19990314 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN INT UNDER FLOOR PLANK TOP OF MLG W/W AT STA 980, BL 45 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FIT TING IAW DC8 SRM 53-01-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900522 20000129 00522 WP 2000 1 29 RRXA991183 1 19990315 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 902 - 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN TOP OF W/W UNDER FLOOR BETWEEN STA 902 AND STA 920 AT BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPA IR DOUBLER IAW EAF-MIA-99-0016RR AND DC8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900523 20000129 00523 WP 2000 1 29 RRXA991184 1 19990315 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 857 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CENTER TANK AFT TOP SKIN PANEL AT STA 857, BL 46 RIGHT, 2 FORWARD OF REAR SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED COMMODORE DER ENGINEERING SKETCH NR EAF-MIA- 99-03-17-002 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900524 20000129 00524 WP 2000 1 29 RRXA991185 1 19990315 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 1118 - 1165 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE,FUSELAGE SKIN BETWEEN STA 1118 AND STA 1165 BETWEEN LONGERONS 32 RI GHT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-1 FIG 21 AND 51-1-8 PAGE 16 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900525 20000129 00525 WP 2000 1 29 RRXA991186 1 19990418 A 5320 FITTING DOUG DC8 DC862F 3021972 WP BS 500 - 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD CARGO COMP C-2 DOOR CUT-OUT BETWEEN STA 500 AND STA 560, BL 34 RIGHT AT FITTINGS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW AND INSTALLED FITTINGS IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900526 20000129 00526 WP 2000 1 29 RRXA991188 1 19990306 A 5313 LONGERON DOUG DC8 DC862F 3021972 WP BS 500 - 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON NR 34 RIGHT, FWD CARGO COMPARTMENT FROM STA 500 TO STA 52 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED L ONGERON SECTION IAW DC8 SRM 51-1-21 PAGE 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900527 20000129 00527 WP 2000 1 29 RRXA991189 1 19990324 A 5320 WEB DOUG DC8 DC862F 3021972 WP BS 480 - 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB, CABIN RT TOP OF LOWER CARGO DOOR BETWEEN STA 480 AND STA 520 AT BL 53 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AN D INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 53-2-0 PAGE 165 FIG 23. (CORROSION DAMAGE RECORDED IN EWA CORROSION P ROGRAM). 2 L 7 4 4F 4A25 2000012900528 20000129 00528 WP 2000 1 29 RRXA991190 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 260 - 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 260 AND STA 300 AT BL 20 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900529 20000129 00529 WP 2000 1 29 RRXA991191 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 260 - 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 260 AND STA 300 AT BL 12 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 51-1-8 AND 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900530 20000129 00530 WP 2000 1 29 RRXA991192 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 260 - 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 260 AND STA 300 AT BL 4 LEFT. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW DC8 SRM 53-2-3 PAGES 30/40.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900531 20000129 00531 WP 2000 1 29 RRXA991193 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 260 - 330 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 260 AND STA 330 AT BL 12 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER AND FILLER IAW DC8 SRM 53-2-3 PAGES 30/40 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900532 20000129 00532 WP 2000 1 29 RRXA991194 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 320 AND BL 54 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM 1-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 FIG 10 PAGES 39/40. (CORROSION DAMA GE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900533 20000129 00533 WP 2000 1 29 RRXA991195 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 500 AND BL 42 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 S RM 53-2-3 PAGES 39/40 AND 53-2-3 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900534 20000129 00534 WP 2000 1 29 RRXA991196 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 560 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 560 AND BL 56 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 S RM 53-2-3 PAGES 30/40 FIG. 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900535 20000129 00535 WP 2000 1 29 RRXA991197 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 540 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 540 AND BL 42 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 S RM 53-2-3 PAGES 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900536 20000129 00536 WP 2000 1 29 RRXA991199 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 640 & 720 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 640 AND STA 720 AT BL 36 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 51-1-8 PG 17-20 AND 53-2-3 FIG 10 PGS 30/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900537 20000129 00537 WP 2000 1 29 RRXA991200 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 720 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANT AT STA 720 AND BL 20 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 S RM 53-2-3 FIG 10 PGS 39/40 AND 53-2-3 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900538 20000129 00538 WP 2000 1 29 RRXA991201 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 717 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 717 AND STA 730 AT BL 36 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABARICATED AND INSTALLED DOUBLER IAW DC8 SRM 52-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900539 20000129 00539 WP 2000 1 29 RRXA991202 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 730 & 760 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 730 AND STA 760 AT BL 36 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 51-1-8 PGS 17 AND 20 AND 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRA M). 2 L 7 4 4F 4A25 2000012900540 20000129 00540 WP 2000 1 29 RRXA991203 1 19990311 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 730 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 730 AND BL 54 RIGHT, WL 0. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-8 PAGE 17 AND 53-2-3 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900541 20000129 00541 WP 2000 1 29 RRXA991204 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 640 AND BL 28 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 S RM 51-1-8 PG 1, 53-2-0 FIG 1F, AND 53-2-3 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900542 20000129 00542 WP 2000 1 29 RRXA991205 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 880, BL 35 RIGHT AND WL 0. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SR M 53-2-3 PAGES 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900543 20000129 00543 WP 2000 1 29 RRXA991206 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1420 & 1460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1420 AND STA 1460 AT BL 6 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900544 20000129 00544 WP 2000 1 29 RRXA991207 1 19990306 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 1480 AND BL 34 LEFT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2 -3 PAGES 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900545 20000129 00545 WP 2000 1 29 RRXA991208 1 19990304 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 1360 AND BL 12 LEFT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 S RM 53-2-3 PAGES 39/40 FIG 10 AND 51-1-8 PG 17. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900546 20000129 00546 WP 2000 1 29 RRXA991209 1 19990304 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 1340 AND BL 12 RIGHT. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53- 2-3 PAGES 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900547 20000129 00547 WP 2000 1 29 RRXA991210 1 19990304 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1300 AND STA 1340 AT BL 6 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR I AW DC8 SRM 53-2-3 PAGES 39/40 AND 51-1-8 PAGES 17,20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900548 20000129 00548 WP 2000 1 29 RRXA991211 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN SEAT TRACK AT STA 1100 AND BL 59 LEFT. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK AND SPLICES IAW DC8 SRM 53-2-3 PGS 49/50. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900549 20000129 00549 WP 2000 1 29 RRXA991212 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 1230 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN SEAT TRACK AT STA 1230 AND BL 59 LEFT. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK SECTION AND SPL ICES IAW DC8 SRM 53-2-3 PAGES 49/50.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900550 20000129 00550 WP 2000 1 29 RRXA991213 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN SEAT TRACK AT STA 980 AND BL 45 RIGHT. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IAW DC8 SRM 53-2-3 PAGE 51 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900551 20000129 00551 WP 2000 1 29 RRXA991214 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 880 & 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 880 AND STA 920 AT BL 45 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECT ION OF SEAT TRACK IAW DC8 SRM 53-2-3 PAGE 51 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900552 20000129 00552 WP 2000 1 29 RRXA991215 1 19990304 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 740 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 740 AND BL 49 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1 -8 AND 53-2-3 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900553 20000129 00553 WP 2000 1 29 RRXA991216 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR TRACK AT STA 1000, BETWEEN BL 45 LEFT AND 49 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TR ACK SECTION AND SPLICE REPAIRS IAW DC8 SRM 53-3-2 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).. 2 L 7 4 4F 4A25 2000012900554 20000129 00554 WP 2000 1 29 RRXA991217 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 780 - 840 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 780 AND STA 840 AT BL 59 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECT ION TRACK AND SPLICE IAW DC8 SRM 53-2-3 PG 49 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).. 2 L 7 4 4F 4A25 2000012900555 20000129 00555 WP 2000 1 29 RRXA991218 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR TRACK AT STA 600, BL 0, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW DC8 SRM 53-2-3 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900556 20000129 00556 WP 2000 1 29 RRXA991220 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 600 - 690 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK BETWEEN STA 600 AND STA 690 AT BL 45 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTI ON OF TRACK IAW DC8 SRM 53-2-3 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900557 20000129 00557 WP 2000 1 29 RRXA991221 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR TRACK AT STA 1000, BL 59 LEFT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK SECTION AND SPLICES IAW DC8 SRM 53-2-3 PAGES 49/50. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900558 20000129 00558 WP 2000 1 29 RRXA991222 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR TRACK AT STA 600, BL 59 LEFT AND WL O. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK SECTION IAW DC8 SRM 53-2-3 PG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900559 20000129 00559 WP 2000 1 29 RRXA991223 1 19990313 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1300 - 1430 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1300 AND STA 1430 AT BL 4 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC8 SRM 51-1-8 PGS 17-20 AND 53-3-2 PGS 39/40 FIG. 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM ). 2 L 7 4 4F 4A25 2000012900560 20000129 00560 WP 2000 1 29 RRXA991224 1 19990401 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1500 - 1520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1500 AND STA 1520 AT BL 36 LEF. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900561 20000129 00561 WP 2000 1 29 RRXA991225 1 19990405 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 680 - 700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, LT CABIN FLOOR BETWEEN STA 680 AND STA 700 AT BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900562 20000129 00562 WP 2000 1 29 RRXA991226 1 19990401 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR PLANK AT STA 1460 AND BL 6 LEFT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 S RM 51-1-8 PGS 16 AND 20 AND 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900563 20000129 00563 WP 2000 1 29 RRXA991227 1 19990329 A 5315 FFLOORBEAM DOUG DC8 DC862F 3021972 WP BS 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSEALAGE, CABIN FLOOR PLANK BETWEEN STA 580 AND STA 700 AT BL 36 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-8 PG 20 AND 53-2-0 PG 28 AND 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900564 20000129 00564 WP 2000 1 29 RRXA991228 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 420 - 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 420 AND STA 520 AT BL 12 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 51-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900565 20000129 00565 WP 2000 1 29 RRXA991229 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 600 - 740 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 600 AND STA 740 AT BL 6 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLERS IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900566 20000129 00566 WP 2000 1 29 RRXA991230 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 760 - 800 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 760 AND STA 800 AT BL 32 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLERS IAW DC8 SRM 51-1-8 PGS 16 AND 20 AND 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGR AM). 2 L 7 4 4F 4A25 2000012900567 20000129 00567 WP 2000 1 29 RRXA991231 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 580 - 700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 580 AND STA 700 AT BL 28 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900568 20000129 00568 WP 2000 1 29 RRXA991232 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1360 - 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1360 AND STA 1440 AT BL 12 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900569 20000129 00569 WP 2000 1 29 RRXA991233 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1360 - 1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 1360 AND STA 1420 AT BL 22 RIGHT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900570 20000129 00570 WP 2000 1 29 RRXA991234 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1270 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1270 AND STA 1300 AT BL 54 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900571 20000129 00571 WP 2000 1 29 RRXA991235 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1460 - 1500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1460 AND STA 1500 AT BL 26 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 51-1-8 PG 20 AND 53-2-3 PGS 39/40 FIG 10 AND 51-01-20 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900572 20000129 00572 WP 2000 1 29 RRXA991236 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1000 - 1160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1000 AND STA 1160 AT BL 54 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLERS IAW DC8 SRM 51-1-8 PG 16 AND 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900573 20000129 00573 WP 2000 1 29 RRXA991237 1 19990329 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1160 - 1270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1160 AND STA 1270 AT BL 54 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-8 PGS 16-20 AND 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) . 2 L 7 4 4F 4A25 2000012900574 20000129 00574 WP 2000 1 29 RRXA991238 1 19990325 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1100 - 1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1100 AND STA 1120 AT BL 32 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 52-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900575 20000129 00575 WP 2000 1 29 RRXA991239 1 19990325 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1040 - 1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1040 AND STA 1060 AT BL 32 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 FIG 10 AND 51-1-8 PGS 16 AND 20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900576 20000129 00576 WP 2000 1 29 RRXA991240 1 19990325 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1120 - 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1120 AND 1140 AT BL 12 RIGHT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER I AW DC8 SRM 53-2-3 FIG 10 PGS 39/40 AND 51-1-21, 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900577 20000129 00577 WP 2000 1 29 RRXA991241 1 19990325 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION , FUSELAGE, CABIN FLOOR PLANK AT STA 1220 AND BL 18 RIGHT. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900578 20000129 00578 WP 2000 1 29 RRXA991242 1 19990325 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 1240 - 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE,CABIN FLOOR PLANK BETWEEN STA 1240 AND STA 1280 AT BL 12 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FAB RICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-8 PG 16 & 20 AND 53-2-3 FIG. 10 PGS 39/40. (CORROSION DAMAGE RECO RDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900579 20000129 00579 WP 2000 1 29 RRXA991243 1 19990324 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 717 - 759 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 717 AND STA 759 AT BL 36 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900580 20000129 00580 WP 2000 1 29 RRXA991244 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL AT STA 880, BL 38 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 5 3-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900581 20000129 00581 WP 2000 1 29 RRXA991245 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 1400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 1400, BL 12 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 52-2-3 PGS 39/40 FIG 10 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900582 20000129 00582 WP 2000 1 29 RRXA991246 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 1460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1460 AND STA 1480 AT BL 12 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900583 20000129 00583 WP 2000 1 29 RRXA991247 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 1460 - 1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 1460 AND STA 1480 AT BL 12 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900584 20000129 00584 WP 2000 1 29 RRXA991248 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL AT STA 700 BL 36 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FILLER AND ANGLE IAW DC8 SRM 51-1-8 PG 16 AND 20 AND 53-2-0 (FIG 1B). (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900585 20000129 00585 WP 2000 1 29 RRXA991249 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 900 - 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 900 AND STA 920 AT BL 54 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 2000012900586 20000129 00586 WP 2000 1 29 RRXA991250 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 460 - 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 460 AND STA 540 AT BL 12 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900587 20000129 00587 WP 2000 1 29 RRXA991251 1 19990324 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 700 - 822 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 700 AND STA 822 AT BL 49 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900588 20000129 00588 WP 2000 1 29 RRXA991252 1 19990322 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 800 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 800, BL 54 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DC8 S RM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900589 20000129 00589 WP 2000 1 29 RRXA991253 1 19990322 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 840 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 840, BL 4 LEFT. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51 -1-8 PG 16 AND 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900590 20000129 00590 WP 2000 1 29 RRXA991254 1 19990322 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 660 - 680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL BETWEEN STA 660 AND STA 680 AT BL 20 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 53-2-3 PG 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900591 20000129 00591 WP 2000 1 29 RRXA991255 1 19990322 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 600 - 620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 600 AND STA 620 AT BL 8 RIGHT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 51-1-8 PG 20 AND 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020400001 20000204 00001 WP 2000 2 4 K4HA99106 1 19991127 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 803CK 46085 PERU - LEFT WING LEADING EDGE SURFACE SKIN CORROSION. ATTACHMENT POINTS WS 485.000 TO WS 710.000. REMOVED L/E SKIN, FA BRICATED NEW SKIN AND INSTALLED IAW SRM 51-2-21. REF: AIA EA: D8-57-078 . WORK ACCOMPLISHED UNDER AIA FORM M-40 CONT ROL NR 26719. (X) 2 L 7 4 4F 4A25 2000020500004 20000205 00004 WP 2000 2 5 HALA000004 1 19991230 A 2612 CONNECTOR DOUG DC9 DC951 3022051 WP NR 2 ENGINE FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 HNL - MAINTENANCE ENTRY: NR 2 ENGINE FIRE B-LOOP INOPERABLE. OK TO CONTINUE PER MEL 26-1-1. MPCW ON OVERNIGHT REPLACE D NR 2 ENGINE B-LOOP PYLON ELEMENT CONNECTOR. OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 2000020500005 20000205 00005 WP 2000 2 5 HALA0000002 1 19991231 A 2170 WATER SEPARATOR DOUG DC10 DC1010 3022110 WP NR 1 PACK CONTAMINATED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 160AA 46710 HNL - FLT 01 - FUEL FUMES AND SMELL INTERMITTENT COCKPIT. REMOVED AND REPLACED NR 1 PACK WATER SEPARATOR, GROUND RUN OK . LEAK CHECK, SMELL CHECK OK. (X) 2 L 7 3 4F A22WE 2000020500006 20000205 00006 WP 2000 2 5 HALA0000001 1 19991230 A 3232 ACTUATOR DOUG DC9 DC951 3022051 WP MLG DOOR FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 649HA 47715 HNL - FLT 103 - (AIR TURN BACK) NOSE GEAR DOOR FAILS TO CLOSE PROPERLY AFTER TAKEOFF. ALL GEAR LIGHTS OUT. RECYCLED 2 TIMES WITH SAME EFFECT. REPLACED RT FORWARD GEAR DOOR ACTUATOR LINK. GEAR SWING OPS CHECK GOOD PER MM 32-22-1. (X) 2 L 7 2 4F RT A6WE 2000020500008 20000205 00008 WP 2000 2 5 HALA9900253 1 19991129 A 2842 PROBE DOUG DC9 DC951 3022051 WP FUEL SYSTEM MALFUNCTIONED A HALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 13 679HA 47662 HNL - FLT 105 - AIRCRAFT REQUIRES 4 UNITS OF LEFT AILERON TRIM WITH 50 DEGREES FLAPS TO STAY LEVEL. CHECKED FLAP MOVEME NT, FOUND SYMMETRY ALL THE WAY DOWN. FOUND FUEL IMBALANCE. REPLACED FUEL QUANTITY PROBES 1, 3, 4, AND 6, AND 7. GROUN D OPS CHECKED OKAY. (X) 2 L 7 2 4F RT A6WE 2000020500009 20000205 00009 NM 2000 2 5 2000ZZZX248 1 19991229 A 7500 652244143 DUCT BOEING 727 727230 1384080 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE CRACKED A C8GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 15 357KP 47632 2311 20675 687407 KXAS/KAUS - FLT 311 - DURING TAKEOFF AND JUST AFTER ROTATION, NR 1 ENGINE FIRE WARNING CAME ON. NR 1 ENGINE THRUST LEVE R WAS RETARDED TO FLIGHT IDLE. FIRE WARNING LIGHT WENT OUT. RETURNED TO KLAX WITHOUT FURTHER INCIDENT. FOUND 13TH STA GE DUCT WITH CRACK ALONG WELD AROUND FLANGE OF DUCT. REMOVED AND REPLACED 13TH STAGE DUCT IAW B727 MM 75-31-00. LEAK C HECKED ENGINE TO PART POWER, SYSTEM OPS CHECKED NORMAL. RETURNED TO SERVICE. (X) 2 L 7 3 4F 4 F A3WE E2EA 2000020500011 20000205 00011 NM 2000 2 5 2000ZZZX249 1 19991208 A 3350 AVAI0141 LIGHT BOEING 727 7272B7 138407L NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 762AT 22162 DURING PRE-FLIGHT, FOUND EGRESS LIGHT ABOVE R1 DOOR INOPERABLE WHEN EMERGENCY EGRESS IS TURNED ON. REMOVED AND REPLACED LIGHT ASSY, OPS CHECKED NORMAL. (X) 2 L 7 3 4F A3WE 2000020500012 20000205 00012 NM 2000 2 5 2000ZZZX250 1 19991101 A 2730 65178235 MODULE BOEING 727 727214 138407R NM ELEVATOR LEAKING A AMTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 785AT 21691 CLE/LAS - FLT 8053 - AFTER GEAR AND FLAP RETRACTION, A-HYDRAULIC SYSTEM PRESSURE QUANTITY DROPPED TO ZERO. ALL APPROACH CHECKLISTS WERE ACCOMPLISHED, MANUAL GEAR, ALTERNATE FLAP, AND FUEL DUMP. AFTER TAXI OFF RUNWAY, B-SYSTEM PRESSURE AND QUANTITY WENT TO ZERO. REMOVED AND REPLACED ELEVATOR HYDRAULIC MODULAR UNIT IAW MM 27-30-91, NO LEAKS NOTED. (X) 2 L 7 3 4F A3WE 2000020500013 20000205 00013 NM 2000 2 5 2000ZZZX251 1 19991114 A 7997 WIRE BOEING 727 727227 1384078 NM INDICATOR BROKEN A AMTA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 768AT 21996 PHX - FLT 751 - DURING TAXI FOR TAKEOFF, THE NR 2 ENGINE OIL PRESSURE FROZE AT 45 PSI, RETURNED TO GATE. REPAIRED BROKE N GROUND WIRE FOR NR 2 ENGINE OIL PRESSURE TRANSMITTER, OPS CHECKED NORMAL. (X) 2 L 7 3 4F A3WE 2000020500014 20000205 00014 NM 2000 2 5 ASAA9940166 1 19991129 A 3350 FUSE BOEING 737 7374Q8 NM BATTERY PACK FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 754AS 25095 LAX - DURING MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FORWAR D FIRST CLASS CABIN AREA. REPLACED FUSE IN THE LEFT FORWARD BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 2000020500015 20000205 00015 NM 2000 2 5 ASAA9940165 1 19991127 A 3350 8100022601 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT TRACK LIGHTS AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER WERE FOU ND INOPERATIVE. REPLACED THE AFT TRACK LIGHT ASSEMBLY AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER AND LIGHTS OPERATED NOR MALLY. REF: OPER CNTRL NR 2000ZZZX252. (X) 2 L 7 2 4F RT A16WE 2000020500016 20000205 00016 NM 2000 2 5 2000ZZZX252 1 19991127 A 3350 7024091007 SIGN BFGOODRICH BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT TRACK LIGHTS AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER WERE FOU ND INOPERATIVE. REPLACED THE AFT TRACK LIGHT ASSEMBLY AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER AND LIGHTS OPERATED NOR MALLY. REF: OPER CNTRL NR ASAA9940165. 2 L 7 2 4F RT A16WE 2000020500017 20000205 00017 NM 2000 2 5 ASAA9940164 1 19991122 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 GEG - PRIOR TO FLT 570, 3 EACH EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED LOOSE WIRING/CONNECTI ON AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 2000020500018 20000205 00018 NM 2000 2 5 ASAA9910264 1 19991209 A 3350 86210144 BATTERY INTVLV BOEING 737 7372Q8C 138448S NM ROW 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 16. REPLACED BATTER Y AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 2000020500019 20000205 00019 NM 2000 2 5 ASAA9910263 1 19991203 A 3350 883200312 RECEIVER INTVLV BOEING 737 737290C 138448V NM ROW 12 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - AFTER RECONFIGURATION AND PRIOR TO FLT 65, THE EMERGENCY EXIT LIGHTS AT ROW 12 WERE FOUND INOPERATIVE AND THE MID TRANSMITTER WAS NOT BEING RECEIVED. REPLACED RECEIVER AT ROW 12 AND THE BATTERY FOR THE MID CABIN TRANSMITTER, ALL OPE RATED NORMALLY. REF: OPER CNTRL NR 2000ZZZX253. (X) 2 L 7 2 4F A16WE 2000020500020 20000205 00020 NM 2000 2 5 2000ZZZX253 1 19991203 A 3350 86210144 BATTERY INTVLV BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - AFTER RECONFIGURATION AND PRIOR TO FLT 65, THE EMERGENCY EXIT LIGHTS AT ROW 12 WERE FOUND INOPERATIVE AND THE MID TRANSMITTER WAS NOT BEING RECEIVED. REPLACED RECEIVER AT ROW 12 AND THE BATTERY FOR THE MID CABIN TRANSMITTER, ALL OPE RATED NORMALLY. REF: OPER CNTRL NR ASAA9910263. 2 L 7 2 4F A16WE 2000020500021 20000205 00021 NM 2000 2 5 ASAA9910262 1 19991130 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 737210C 1384459 NM ROW 11 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - PRIOR TO FLT 145 THE EMERGENCY EXIT TRACK LIGHTS AT ROW 11 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGH TS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 2000020500022 20000205 00022 NM 2000 2 5 ASAA9910261 1 19991122 A 3350 8821004 BATTERY PACK INTVLV BOEING 737 737298C 1384490 NM ROW 3 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 3 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 2000020500023 20000205 00023 NM 2000 2 5 ASAA9910260 1 19991121 A 3350 86210144 BATTERY INTVLV BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR LOWER EMERGENCY EXIT IDENTIFIER LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE BATTERY AND THE LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 2000020500024 20000205 00024 NM 2000 2 5 ASAA9910259 1 19991116 A 3350 86210144 BATTERY INTVLV BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - PRIOR TO FLT 65, THE SMOKE BARRIER EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 2000020500025 20000205 00025 WP 2000 2 5 AALA9980290 1 19991212 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 PDX - DURING MAINTENANCE CHECK, THE FORWARD TWO EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND RELAMPED AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500026 20000205 00026 WP 2000 2 5 ASAA9980289 1 19991211 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - AFTER ARRIVAL OF FLT 395, CREW REPORTED THE FORWARD TWO EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTE D WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500027 20000205 00027 WP 2000 2 5 ASAA9980288 1 19991210 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTOR A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 33 WERE FOUND INOPERATIVE. SECURED LOOSE CONNEC TOR IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500028 20000205 00028 WP 2000 2 5 ASAA9980286 1 19991207 A 3350 014597101 BATTERY MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 53471 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500029 20000205 00029 WP 2000 2 5 ASAA9980281 1 19991202 A 3350 014597101 BATTERY MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 PDX - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500030 20000205 00030 WP 2000 2 5 ASAA9980280 1 19991129 A 3350 60030431 POWER SUPPLY MIDLANDROSS DOUG DC9 DC982 3022082 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SEA - PRIOR TO DEPARTURE OF FLT 650, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOP ERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 2000020500031 20000205 00031 WP 2000 2 5 ASAA9980278 1 19991124 A 3350 014597101 BATTERY MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 SEA - AFTER ARRIVAL OF FLT 631, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FLICKERED ON LANDING. ACCOMPLISHED OPERA TIONAL CHECK OF THE EMERGENCY LIGHTS SYSTEM. ALL LIGHTS OPERATED NORMALLY WITH THE EXCEPTION OF THE OVERHEAD EMERGENCY LIGHTS AT ROW 15. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 2000020500032 20000205 00032 WP 2000 2 5 ASAA9980269 1 19991122 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SAN - PRIOR TO DEPARTURE OF FLT 231, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500033 20000205 00033 WP 2000 2 5 ASAA9980268 1 19991122 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - PRIOR TO DEPARTURE OF FLT 230, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500034 20000205 00034 WP 2000 2 5 ASAA9980267 1 19991121 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - PRIOR TO DEPARTURE OF FLT 92, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE . RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500035 20000205 00035 2000 2 5 ASAA9980266 4 19991119 A 2565 D29982107 SLIDE AIRCRUISERS DOUG DC9 DC983 3022083 WP PASSENGER DOOR WILL NOT TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 0099 53451 OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (X) 2 L 7 2 4F RT A6WE 2000020500036 20000205 00036 WP 2000 2 5 ASAA9980265 1 19991118 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 977AS 53453 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. SECURED C ONNECTORS TO LIGHT SOCKETS IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500037 20000205 00037 WP 2000 2 5 ASAA9980264 1 19991114 A 3350 014597101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING MAINTENANCE CHECK THE FORWARD AFT INTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER PACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500038 20000205 00038 WP 2000 2 5 ASAA9980263 1 19991114 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING MAINTENANCE CHECK, THE FORWARD FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED CONNECTOR TO LIGHT ASSEMBLY IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500039 20000205 00039 WP 2000 2 5 ASAA9980262 1 19991113 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROWS 13-16 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 THROUGH 16 WERE FOUND INOPERATIVE. RECO NNECTED CONNECTOR TO LIGHT ASSEMBLY IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500040 20000205 00040 WP 2000 2 5 ASAA9980245 1 19991109 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED CONNECTOR TO LIGHT ASSEMBLY IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500041 20000205 00041 WP 2000 2 5 ASAA9980224 1 19991029 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECE D WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500042 20000205 00042 WP 2000 2 5 ASAA9980223 1 19991028 A 3350 014597101 BATTERY MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMEGENCY LIGHTS FROM ROWS 19 TO 21 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER USPPLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000020500043 20000205 00043 SO 2000 2 5 ASOA99171 1 19991227 A 5411 12003851003 FRAME EMB 120 EMB120RT SO LT & RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 265AS 120170 DURING INSPECTION, FOUND BOTH LT AND RT NR 1 FRAMES CRACKED. MAINTENANCE C/W EO 120-54-0034, WHICH OUTLINED FRAME REPLA CEMENT PROCEDURES. AIRCRAFT IS CURRENTLY IN C-CHECK. (X) 2 L 7 2 4T RT A31SO 2000020500044 20000205 00044 SO 2000 2 5 ASOA99170 1 19991227 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 266AS 17573 51 120188 DURING INSPECTION, FOUND EMERGENCY FORWARD TRACK LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK. OPERATIONAL CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 2000020500045 20000205 00045 SO 2000 2 5 ASOA99169 1 19991223 A 2120 UNKNOWN EMB 120 EMB120RT 3260202 SO CABIN SMOKE A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 246AS 120100 FLT 4063 - CREW NOTICED SMOKE IN AIRCRAFT DURING TAXI. THERE WERE NO ASSOCIATED PACK, DUCT, OR BLEED INDICATION WARNING LIGHTS ILLUMINATED. MAINTENANCE RAN BOTH NR 1 AND NR 2 ENGINES FOR 15 MINUTES, CYCLED BOTH PACKS, AND SHUT BLEEDS ON A ND OFF. MAINTENANCE ALSO INSPECTED ELECTRIC BAY, ACM HOSE AND ENGINE BLEEDS FOR OIL THEN RAN ENGINES NR 1 AND NR 2 FOR 15 MINUTES AGAIN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 2000020500047 20000205 00047 WP 2000 2 5 AALA006009 1 19991227 A 2170 21D101 COALESCER DOUG DC9 DC983 3022083 WP AC BAY CONTAMINATED A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 879RA 53185 APPROXIMATELY ONE MINUTE AFTER TAKEOFF, F/A'S REPORTED SMELLING STRONG SMOLDERING LIKE SMELL IN CABIN. ALSO, SMELLED IN COCKPIT. EMERGENCY DECLARED. AIRCRAFT LANDED AT 132,000 POUNDS. INSPECTED AIRCRAFT AND FOUND OIL SMELL COMING FROM B OTH AIR CONNDITIONING PACKS. REPLACED BOTH COALESCER BAGS. NO OIL WAS FOUND IN BAGS. PERFORMED BURN-OUT PROCEDURE DUE TO STRONG SMELL REPORTS. RAN AIR CONDITION PACK FULL HOT AND COLD AT POWER. NO SMELL OR FUMES NOTED. INSPECTED RECIR CULATING FANS AND ACM. BOTH ARE NORMAL. LANDING WEIGHT IS WITHIN LIMITS. (X0 2 L 7 2 4F RT A6WE 2000020500052 20000205 00052 NE 2000 2 5 AALA996058 2 19991228 A 7250 6A5583C01 BLADE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE LT ENGINE FAILED A AALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 904RA 54323 5432 53570 V20040 SFO - LEFT ENGINE EXPERIENCED OFF IDLE COMPRESSOR STALLS DESCENDING THROUGH 30,000 FEET. NO ABNORMAL INDICATING NOTED E XCEPT ENGINE WOULD NOT ACCELERATE AT LOWER ALTITUDE. ENGINE RESPONDED NORMALLY IN ALL RESPECTS. REMOVED AND REPLACED N R 1 ENGINE PER CARDS UN-014UN-020 AND CARD UN-016. PERFORMED ENGINE RUN-UP PER MM. NO LEAKS NOTED. OPS CHECK GOOD. ( X) 2 L 7 2 4F 4 F RT A6WE E40NE 2000020500057 20000205 00057 EU 2000 2 5 2000ZZZX254 1 19991231 A 3240 C20216332292C BSCU AIRBUS 320 A320231 3930325 EU E/E BAY MALFUNCTIONED A P9RA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 09 447TM 842 447 HOT BRAKE INDICATION AFTER TAKEOFF ABOUT 15 MINUTES INTO FLIGHT, TEMPERATURE REACHED ABOUT 320 DEGREES. RETURNED TO MIA MI FOR CHECK NR 1 BRAKE. PER MAINTENANCE CONTROL, PLACED BRAKE TEMPERATURE INDICATOR ON DMI PER MEL 32-47-01 CAT C CON TROL NR 1340. BRAKE TEMP OK. (X) 2 L 7 2 4F RT A28NM 2000020500058 20000205 00058 NM 2000 2 5 EISA99240 1 19991110 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 990-1130 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON MAIN CABIN SEAT TRACK AT LBL 24 AT BS 990 TO BS 1130. REMOVED CORROSION AND MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED TRACK SECTION AND FABRICATED NE W SECTION PER SAMPLE. INSTALLED NEW TRACK FROM BS 990 TO BS 1130 PER SRM'S 51-10-1 AND 51-30-2. TT: 65,345:17 HOURS. T C: 43,816. (X) 2 L 7 3 4F A3WE 2000020500059 20000205 00059 NM 2000 2 5 EISA99239 1 19991013 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 848-990 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 353PA 20622 DURING THE ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON MAIN CABIN SEAT TRACK AT BS 848 TO BS 990 R BL 20. CORROSION REMOVED PER SRM 51-10-6 AND MATERIAL LOSS OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK PER SAMPLE. REPLACED TRACK SECTION FROM BS 848 TO BS 990 PER SRM'S 51-10-1 AND 51-30-2. TT: 65,345:17 HOURS. TC: 43,816. (X) 2 L 7 3 4F A3WE 2000020500089 20000205 00089 WP 2000 2 5 MWEA99966 1 19991212 A 5210 9915565161 ANGLE DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 AFT ENTRANCE DOOR, RIGHT EDGE OF NR 7 RIB IS CRACKED. MAINTENANCE DRILLED AND INSTALLED NEW ANGLE. 2 L 7 2 4F A6WE 2000020500090 20000205 00090 WP 2000 2 5 MWEA99967 1 19991222 A 5321 9910078 FLOOR PANEL DOUG DC9 DC932 3022066 WP COCKPIT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 COCKPIT FLOOR HAS A HOLE IN IT, 6 AFT. OF F/O'S LOWER INBOARD SEAT RAIL. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000020500091 20000205 00091 WP 2000 2 5 MWEA99969 1 19991221 A 5330 5911412 SKIN DOUG DC9 DC932 3022066 WP BS 332 - 351 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 THREE DENTS BETWEEN FUSELAGE STATION 332 TO 351 FROM LONGERON 23 RIGHT TO 25 RIGHT. MAINTENANCE FABRICATED AND INSTALLE D DOUBLER. 2 L 7 2 4F A6WE 2000020500092 20000205 00092 WP 2000 2 5 MWEA99970 1 19991228 A 5320 99234847 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 180 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 INTERCOSTAL IS CRACKED AT FUSELAGE STATION 180, 20 LEFT OF CENTER BELOW SUBFLOOR. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000020500095 20000205 00095 WP 2000 2 5 MWEA99968 1 19991221 A 5230 59101575N DOOR PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 AFT CARGO DOOR INNER LINER PAN FORWARD END HAS A CRACK IN THE RADIUS UNDER THE UPPER DOOR STOP. MAINTENANCE DRILLED AND INSTALLED NEW INNER DOOR PAN. 2 L 7 2 4F A6WE 2000020500098 20000205 00098 WP 2000 2 5 ABXA000021 1 19991208 A 5753 5910042504 VANE DOUG DC9 DC932F 3022067 WP TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND THE RIGHT FLAP CENTER FIXED VANE DELAMINATED ON UPPER SURFACE. REPLACED FIXED VANE IAW DC9 MM 27- 51-3. 2 L 7 2 4F A6WE 2000020500099 20000205 00099 WP 2000 2 5 ABXA000022 1 19991208 A 5753 5910042503 VANE DOUG DC9 DC932F 3022067 WP TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND THE LEFT FLAP CENTER FIXED VANE DELAMINATED AT OUTBOARD END. REPLACED FIXED VANE IAW DC9 MM 27-51 -3. 2 L 7 2 4F A6WE 2000020500100 20000205 00100 WP 2000 2 5 ABXA000023 1 19991208 A 5320 39130751 ANGLE DOUG DC9 DC932F 3022067 WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT WHEEL WELL LATERAL CONTROL MIXER TOP ATTACH ANGLE CORRODED AT OUTBOARD TOP END. REPLACED ANG LE IAW DC9 SRM 51-20-0 AND 51-30-5. 2 L 7 2 4F A6WE 2000020500101 20000205 00101 WP 2000 2 5 ABXA000024 1 19991208 A 5730 59134383 PANEL DOUG DC9 DC932F 3022067 WP LEFT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND BONDED PANEL AT INBOARD LOWER TRAILING EDGE OF LEFT WING CORRODED. REPLACED PANEL IAW DC9 SRM 51- 30-2. 2 L 7 2 4F A6WE 2000020500102 20000205 00102 WP 2000 2 5 ABXA000025 1 19991116 A 5320 99155101 FITTING DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LOWER WING ATTACH FITTING CRACKED. REPLACED FITTING IAW SRM 51-30-2 AND 51-30-5 2 L 7 2 4F A6WE 2000020500105 20000205 00105 WP 2000 2 5 ABXA000026 1 19991213 A 5320 9915558231 STIFFENER DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND APB HORIZONTAL STIFFENER LOWER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-10-5. 2 L 7 2 4F A6WE 2000020500106 20000205 00106 WP 2000 2 5 ABXA000027 1 19991213 A 5320 39164181 ANGLE DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND LOWER LEFT SLANT PANEL ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2000020500107 20000205 00107 WP 2000 2 5 ABXA000028 1 19991213 A 5320 D0489819 WEB DOUG DC9 DC931 3022065 WP BS 598 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 598. REPLACED CUSP WEB IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2000020500108 20000205 00108 WP 2000 2 5 ABXA000029 1 19991213 A 5320 9915558509 STIFFENER DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL WEBS CRACKED AT OUTBOARD END. REPAIRED RADIALS IAW DC9 SRM DWG K0515 9. 2 L 7 2 4F A6WE 2000020500109 20000205 00109 WP 2000 2 5 ABXA000030 1 19991116 A 5320 99101555 PANEL DOUG DC9 DC932F 3022067 WP BS 744 - 754 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT WHEEL WELL UPPER PRESSURE PANEL HEAVILY CORRODED BETWEEN STATION 744 TO 754 AND LBL 38-45. R EPLACED UPPER PRESSURE PANEL IAW DC9 SRM 51-30-2, 51-30-1, 51-30-5, AND DACO DRAWING 9910155. 2 L 7 2 4F A6WE 2000020500110 20000205 00110 WP 2000 2 5 ABXA000031 1 19991123 A 5320 49164092 FITTING DOUG DC9 DC931 3022065 WP RT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND RIGHT OUTBOARD SLANT PANEL SUPPORT CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2000020500111 20000205 00111 WP 2000 2 5 ABXA000032 1 19991129 A 5320 39558921 PANEL DOUG DC9 DC931 3022065 WP CARGO BAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND CORROSION ON LEFT SLANT PANEL. INSTALLED NEW SLANT IAW DOUGLAS DWG NR 5956065 AND DC9 SRM 51-30-1 . 2 L 7 2 4F A6WE 2000020500112 20000205 00112 WP 2000 2 5 ABXA000033 1 19991129 A 5320 39558922 PANEL DOUG DC9 DC931 3022065 WP CARGO BAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK INSPECTION, FOUND HEAVY CORROSION ON RIGHT SLANT PANEL. REPLACED SLANT PANEL IAW DOUGLAS DWG NR 5956065 AND DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 2000020500113 20000205 00113 WP 2000 2 5 ABXA000034 1 19991129 A 5320 3916209501 ANGLE DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK INSPECTION, FOUND CENTER TANK TO FLOOR ANGLE BEAM CRACKED AT STA 680 LBL 44.0. REPLACED CENTER TANK TO F LOOR ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2000020500114 20000205 00114 WP 2000 2 5 ABXA000035 1 19991203 A 5320 99101553 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 737 - 756 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND CORROSION ON REPAIR AT PRESSURE PANEL STATION 737 - 756 LBL 8. REPLACED REPAIR DOUBLER IAW DC9 SR M 51-30-2. 2 L 7 2 4F A6WE 2000020500115 20000205 00115 WP 2000 2 5 ABXA000036 1 19991203 A 5312 5910130391 BULKHEAD DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD NR 6 TEE CAP CRACKED. REPLACED NR 6 TEE CAP IAW EA 53120037. 2 L 7 2 4F A6WE 2000020500116 20000205 00116 WP 2000 2 5 ABXA000037 1 19991203 A 5312 5910130392 BULKHEAD DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD NR 2 TEE CAP CRACKED. REPLACED TEE CAP IAW EA 53120033. 2 L 7 2 4F A6WE 2000020500117 20000205 00117 WP 2000 2 5 ABXA000038 1 19991203 A 5280 5913433504 HINGE DOUG DC9 DC931 3022065 WP MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND RIGHT MLG OUTBOARD DOOR HINGE CRACKED. REPLACED HINGE IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2000020500118 20000205 00118 WP 2000 2 5 ABXA000039 1 19991213 A 5320 D0489821 WEB DOUG DC9 DC931 3022065 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 617. REPLACED CUSP WEB IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2000020500119 20000205 00119 WP 2000 2 5 ABXA000040 1 19991213 A 5320 J06011940 SHEAR TIE DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND SHEAR TIE SPLICE ANGLE CRACKED AT STATION 980 LONGERON 14 RIGHT. REPLACED SHEAR TIE IAW DC9 SRM 5 1-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 2000020500124 20000205 00124 WP 2000 2 5 ABXA000041 1 19991129 A 5320 49567712 FITTING DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND FITTING AT FORWARD RIGHT CORNER OF KEEL WEB CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2000020500125 20000205 00125 WP 2000 2 5 ABXA000042 1 19991129 A 5320 9910555 WEB DOUG DC9 DC932F 3022067 WP BS 737 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND THE UPPER PRESSURE PANEL IN THE LEFT WHEEL WELL STATION 737 BULGED AND CORRODED AROUND FASTENERS. REPLACED WEB IAW DC9 SRM 51-30-2, 51-30-1, 51-30-5. 2 L 7 2 4F A6WE 2000020500126 20000205 00126 WP 2000 2 5 ABXA000044 1 19991129 A 5755 591005512 PANEL DOUG DC9 DC932F 3022067 WP SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND THE RIGHT OUTBOARD SPOILER PANEL DELAMINATED ON UPPER SURFACE. REPLACED SPOILER PANEL IAW DC9 SMM 27-61-01.. 2 L 7 2 4F A6WE 2000020500127 20000205 00127 WP 2000 2 5 ABXA000045 1 19991129 A 5730 59134383 SKIN DOUG DC9 DC932F 3022067 WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND CORROSION ON THE LEFT WING TRAILING EDGE INBOARD LOWER BONDED DOUBLER. REPLACED BONDED DOUBLER. 2 L 7 2 4F A6WE 2000020500133 20000205 00133 WP 2000 2 5 ABXA000043 1 19991129 A 5755 5910055515 PANEL DOUG DC9 DC932F 3022067 WP SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING D-CHECK, FOUND LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL IAW DC9 SMM 27-60-01. 2 L 7 2 4F A6WE 2000020500139 20000205 00139 EU 2000 2 5 QXEA0000140 1 19991206 A 5210 DOOR FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 GEG - MAIN CABIN DOOR WILL NOT OPEN. RESET CIRCUIT BREAKERS IN FORWARD CARGO COMPARTMENT. OPERATIONAL CHECKS GOOD AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 2000020500153 20000205 00153 WP 2000 2 5 ABXA000055 1 19991217 A 5730 56429402 PANEL DOUG DC8 DC861 3021952 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 DURING C-CHECK, CRACKS FOUND IN RIGHT WING UPPER AFT SKIN PANELS. REPAIRED RIGHT WING UPPER AFT SKIN PANEL IAW ABX REA D85733696 MR. 2 L 7 4 4F 4A25 2000020500154 20000205 00154 WP 2000 2 5 ABXA000056 1 19991230 A 5320 3917624513 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED AT INBOARD END OF THIRD HORIZONTAL STIFFENER R IGHT SIDE. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2000020500155 20000205 00155 WP 2000 2 5 ABXA000057 1 19991230 A 5320 3917624517 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED AT INBOARD END OF FIRST HORIZONTAL STIFFENER LEFT SIDE. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2000020500156 20000205 00156 WP 2000 2 5 ABXA000058 1 19991227 A 5320 4916270501 FITTING DOUG DC9 DC932 3022066 WP BS 636 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 WHILE COMPLYING WITH A C-CHECK INSPECTION FOUND LONGERON FITTING CRACKED AT STATION 636 AND LONGERON 29 RIGHT. REPLACED BRACKET IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2000020500157 20000205 00157 WP 2000 2 5 ABXA000059 1 19991230 A 5230 59101577 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR OUTER PAN CRACKED IN THREE PLACES. REPAIRED DOOR PAN IAW ABX REA D95234667. 2 L 7 2 4F A6WE 2000020500158 20000205 00158 WP 2000 2 5 ABXA000060 1 19991230 A 5311 995821519 FRAME DOUG DC9 DC932 3022066 WP BS 917 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND THE FUSELAGE FRAME AT STATION 917 AND LONGERON 23 LEFT CORRODED. REPLACED FRAME IAW DC9 SRM 51-30 -2 AND 51-30-5. 2 L 7 2 4F A6WE 2000020500159 20000205 00159 WP 2000 2 5 ABXA000051 1 19991230 A 5320 995558234 CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER, 4TH UP FROM FRP RIGHT SIDE, CLIP CRACKED. REPLACE D CLIP IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2000020500160 20000205 00160 WP 2000 2 5 ABXA000052 1 19991230 A 5320 9915558229N STIFFENER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD STIFFENER LEFT SIDE, 4TH UP FROM FRP AT OUTBOARD END CRACKED. REPAIRED STIFFENER IAW DC9 SRM DWG K05159. 2 L 7 2 4F A6WE 2000020500167 20000205 00167 WP 2000 2 5 ABXA000066 1 19991123 A 5230 3926046505N FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK INSPECTION, FOUND FORWARD LOWER CARGO DOOR END FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2000020500170 20000205 00170 WP 2000 2 5 MWEA99973 1 19991220 A 5330 99155872 SKIN DOUG DC9 DC932 3022066 WP WINDOW BELT LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 WINDOW 20 RIGHT HAND SIDE HAS TWO APPARENT LIGHTENING STRIKES ON THE AFT SIDE OF THE WINDOW. -- MTC FABRICATED, DRILLE D, AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000020500171 20000205 00171 WP 2000 2 5 MWEA99974 1 19991222 A 5320 5912285509 PAN DOUG DC9 DC932 3022066 WP BS 700 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 CABIN WINDOW PAN CRACKED AT STATION 700 NEAR LONGERON 12 LEFT. MAINTENANCE FABRICATED AND INSTALLED NEW WINDOW PAN. 2 L 7 2 4F A6WE 2000020500172 20000205 00172 WP 2000 2 5 MWEA99975 1 19991228 A 5312 5910130279 BULKHEAD DOUG DC9 DC932 3022066 WP PRESS BULKHEAD DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 AFT PRESSURE BULKHEAD HAS DRILLED START MARK ON AFT SLIDE AT THE LEFT THRUST REVERSER SECTOR BEARING AREA. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2000020500173 20000205 00173 WP 2000 2 5 MWEA99976 1 19991228 A 5320 9910078 CHANNEL DOUG DC9 DC932 3022066 WP BS 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FLOORBOARD J CHANNEL HAD MODERATE CORROSION AT STATION 160. MAINTENANCE FABRICATED AND INSTALLED NEW J CHANNEL. 2 L 7 2 4F A6WE 2000020500174 20000205 00174 WP 2000 2 5 MWEA99977 1 19991222 A 5321 995791917 FLOOR BOARD DOUG DC9 DC932 3022066 WP BS 267 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FLOORBOARD E2 AT STATION 267, THE FORWARD EDGE IS MODERATELY CORRODED. MAINTENANCE FABRICATED AND INSTALLED NEW FLOORBO ARD. 2 L 7 2 4F A6WE 2000020500175 20000205 00175 WP 2000 2 5 MWEA99978 1 19991222 A 5321 995791820 FLOOR BOARD DOUG DC9 DC932 3022066 WP BS 267 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FORWARD EDGE ON FLOORBOARD F2 IS MODERATELY CORRODED AT STATION 267. MAINTENANCE FABRICATED AND INSTALLED NEW FLOORBOAR D. 2 L 7 2 4F A6WE 2000020500181 20000205 00181 WP 2000 2 5 MWEA99971 1 19991221 A 3310 59568901 CONTROL PANEL DOUG DC9 DC914 3022034 WP COCKPIT INOPERATIVE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 400ME 45727 DURING MAINTENANCE INSPECTION NOTICED SMOKE IN COCKPIT. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S INSTRUMENT CONTROL P ANEL. 2 L 7 2 4F A6WE 2000020500182 20000205 00182 WP 2000 2 5 MWEA99972 1 19991222 A 5610 59529653 RETAINER DOUG DC9 DC932 3022066 WP COCKPIT WINDOW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 BOTH LEFT AND RIGHT COCKPIT UPPER WINDOW RETAINERS HAVE A CRACK. MAINTENANCE FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 2000020500183 20000205 00183 EU 2000 2 5 QXEA0000041 1 19991229 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT CARGO DOOR INNER SKIN FORWARD AND AFT DOUBLER BRACKETS ARE BROKEN JUST BELOW HINGE. REPAIRED IAW FOKKER SRM 5 2-30-00, PAGE 12, FIGURE 4, AND SRM 51-31-05. 2 L 7 2 4F RT A20EU 2000020500184 20000205 00184 EU 2000 2 5 QXEA0000042 1 19991227 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CENTER CARGO DOOR INNER SKIN HAS THREE DENTS IN CENTER OF SKIN PANEL MEASUREING APPROXIMATELY .040, .060 AND .090 DEEP. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, SRM 51-31-01, 51-30-02 AND 51-31-05. 2 L 7 2 4F RT A20EU 2000020500186 20000205 00186 EU 2000 2 5 QXEA0000043 1 19991227 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CENTER CARGO DOOR FORWARD LOWER CORNER HAS TWO DENTS THAT MEASURE APPROXIMATELY .065 AND .024 DEEP. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2000020500187 20000205 00187 EU 2000 2 5 QXEA0000044 1 19991220 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CENTER CARGO DOOR LOWER AFT CORNER HAS TWO DENTS THAT MEASURE APPROXIMATELY .065 AND .023 DEEP. REPAIRED IAW FOKK ER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2000020500189 20000205 00189 EU 2000 2 5 QXEA0000046 1 19991222 A 3250 PLATE FOKKER F28 F28MK4000 4990810 EU NLG STEERING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - TWO CRACKS IN REINFORCE PLATE FOR NOSE WHEEL STEERING CABLE FEED THROUGH ON UNSIDE ON NOSE LANDING GEAR BAY TOP CO VER.. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2000020500190 20000205 00190 EU 2000 2 5 QXEA0000047 1 19991223 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACK IN FRAME LOWER FORWARD FLANGE ADJACENT TO NUT PLATE FOR RIGHT NOSE LANDING GEAR WHEEL BRAKE, FORWARD LEFT AN D RIGHT ATTACH BOLT. REPAIRED IAW HORIZON AIR EA 4-53-942. 2 L 7 2 4F RT A20EU 2000020500191 20000205 00191 EU 2000 2 5 QXEA0000048 1 19991223 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUSELAGE SKIN CORROSION UNDER LOWER VHF COMM ANTENNA BASE. REPAIRED IAW FOKKER MM PAGE 9, PARAGRAPH A(1) AND B(2) , AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000020500192 20000205 00192 EU 2000 2 5 QXEA0000049 1 19991220 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUSELAGE SKIN CORROSION UNDER LOWER ATC ANTENNA. REPAIRED IAW FOKKER SRM 53-01-4, PAGE 9, PARAGRAPH 4, STEPS A TH ROUGH B2. 2 L 7 2 4F RT A20EU 2000020500193 20000205 00193 EU 2000 2 5 QXEA0000050 1 19991219 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUSELAGE SKIN UNDER NR 1 DME ANTENNA SHOWS CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4, A, B. 2 L 7 2 4F RT A20EU 2000020500194 20000205 00194 EU 2000 2 5 QXEA0000051 1 19991222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 12875 - 13345 GORGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT OUTBOARD SEAT TRACK GOUGED .010 DEEP BETWEEN FRAME 12875 AND 13345. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 206, PARAGRAPH 4B, STEP 5. 2 L 7 2 4F RT A20EU 2000020500195 20000205 00195 EU 2000 2 5 QXEA0000052 1 19991225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 12405 - 12875 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT INBOARD SEAT TRACK GOUGED ON SEVERAL TRACK LOBES BETWEEN FUSELAGE FRAMES 12405 AND 12875. REPAIRED IAW HORI ZON AIR EA 4-53-948. 2 L 7 2 4F RT A20EU 2000020500197 20000205 00197 EU 2000 2 5 QXEA0000054 1 19991220 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUSELAGE SKIN CORROSION UNDER UPPER ATC ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 AND SRM 53- 01-01, PAGE 6, PARAGRAPH B, STEP 2A. 2 L 7 2 4F RT A20EU 2000020500198 20000205 00198 EU 2000 2 5 QXEA0000055 1 19991223 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUSELAGE SKIN CORROSION UNDER UPPER NAV/COM ANTENNA BASE. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH 4C AND SRM 51-10-4, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 2000020500199 20000205 00199 EU 2000 2 5 QXEA0000056 1 19991219 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT PRESSURE BULKHEAD SKIN, FORWARD SIDE HAS A .015 DEEP MARK FROM SCREW LOCATED 7 BELOW STRINGER 35. REPAIRED IA W FOKKER SRM 53-02-01, PAGE 3 (1,3). 2 L 7 2 4F RT A20EU 2000020500201 20000205 00201 EU 2000 2 5 QXEA0000058 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13345 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - GOUGE IN CENTER OF LEFT INBOARD SEAT TRACK, 8 FORWARD OF FRAME 13345. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201, 202 AND 206, FIGURE 205, AND SRM 53-40-01, PAGE 205. 2 L 7 2 4F RT A20EU 2000020500202 20000205 00202 EU 2000 2 5 QXEA0000059 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13815-13815A GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - GOUGE IN LEFT OUTBOARD SEAT TRACK BETWEEN FRAME 13815 AND 13815A. REPAIRED IAW FOKKER SRM 53-40-01, PAGE 201 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000020500203 20000205 00203 EU 2000 2 5 QXEA0000060 1 19991226 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - VERTICAL STABILIZER RIGHT SIDE PAINT/SKIN HAS TOOLING SCRATCH AT LOWER CORNER OF PANEL 56G CUT OUT. REPAIRED IAW FOKKER SRM 51-10-4 AND SRM 55-01-01, PAGE 3, PARAGRAPH D. 2 L 7 2 4F RT A20EU 2000020500204 20000205 00204 EU 2000 2 5 QXEA0000061 1 19991221 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT VERTICAL STABILIZER SKIN CUTOUT FOR PANEL 56D HAS FRETTING/PITTING AROUND ALL FASTENER HOLES. REPAIRED IAW F OKKER SRM 51-10-4, PARAGRAPH 4 B AND C. 2 L 7 2 4F RT A20EU 2000020500205 20000205 00205 EU 2000 2 5 QXEA0000062 1 19991220 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT VERTICAL STABILIZER SKIN CUTOUT FOR PANEL 56C HAS FRETTING/PITTING AR0UND SEVERAL FASTENER HOLES. REPAIRED I AW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500206 20000205 00206 EU 2000 2 5 QXEA0000063 1 19991230 A 2730 BOOSTER UNIT FOKKER F28 F28MK4000 4990810 EU ELEVATOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - ELEVATOR BOOSTER UNIT LOOSE IN MOUNTS. REPAIRED IAW FOKKER SRM 27-32-01. 2 L 7 2 4F RT A20EU 2000020500207 20000205 00207 EU 2000 2 5 QXEA0000064 1 19991230 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - DAMAGED LIGHTNING HOLE IN FORWARD PRESSURE BULKHEAD, HORIZONTAL BEAM VI AT CENTERLINE. METAL IS TORN APPROXIMATEL Y .070. REPAIRED IAW FOKKER SRM 53-02-01. 2 L 7 2 4F RT A20EU 2000020500253 20000205 00253 WP 2000 2 5 RRXA991256 1 19990321 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 580 - 879 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 580 AND STA 879 AT BL 13 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 51-1-8 PGS 16-20 AND 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500254 20000205 00254 WP 2000 2 5 RRXA991257 1 19990318 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN INT UNDER FLOOR PLANK TOP W/W AT STA 980, BL 24 LEFT. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IA W DC8 SRM 51-1-8 PG 20 AND 53-01-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500255 20000205 00255 WP 2000 2 5 RRXA991258 1 19990315 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP BS 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOORBEAM AT STA 580, BL 45 RIGHT, DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER ANGLE IAW FAA APPROVED JOSSAIR, CO. DER ENGINEERING SKETCH NR 18R5371101. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500256 20000205 00256 WP 2000 2 5 RRXA991259 1 19990314 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 360 - 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 360 AND STA 520 AT BL 20 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER I AW DC8 SRM 51-1-8 PG 17 AND 53-2-3 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500257 20000205 00257 WP 2000 2 5 RRXA991260 1 19990314 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 360 - 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 360 AND STA 520 AT BL 54 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-0 PG 1 AND 51-1-21 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500258 20000205 00258 WP 2000 2 5 RRXA991262 1 19990314 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 1500 - 1520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 1500 AND STA 1520 AT BL 42 RIGHT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500259 20000205 00259 WP 2000 2 5 RRXA991263 1 19990314 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 330 - 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 330 AND STA 520 AT BL 12 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLERS IAW DC8 SRM 51-1-8 PG 16 AND 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500260 20000205 00260 WP 2000 2 5 RRXA991264 1 19990312 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 260 - 380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 260 AND STA 380, BL 20 RIGHT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500261 20000205 00261 WP 2000 2 5 RRXA991265 1 19990312 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 600 - 640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 600 AND STA 640 AT BL 35 LEFT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500262 20000205 00262 WP 2000 2 5 RRXA991266 1 19990312 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 380 - 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 380 AND STA 580 AT BL 20 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3 FIG 10 PGS. 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500263 20000205 00263 WP 2000 2 5 RRXA991267 1 19990311 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 260 - 320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 260 AND STA 320 AT BL 54 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500264 20000205 00264 WP 2000 2 5 RRXA991268 1 19990311 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 670 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 670, BL 49 RIGHT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC 8 SRM 53-2-3 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500265 20000205 00265 WP 2000 2 5 RRXA991269 1 19990311 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK AT STA 700, BL 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND NEW SECT ION OF FLOOR PANEL IAW DC8 SRM 53-1-0 PG 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500266 20000205 00266 WP 2000 2 5 RRXA991270 1 19990311 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 300 - 360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN SEAT TRACK BETWEEN STA 300 AND STA 360 AT BL 24 LEFT. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTIO N OF SEAT TRACK AND SPLICE IAW DC8 SRM 53-2-3 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500267 20000205 00267 WP 2000 2 5 RRXA991271 1 19990311 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 260 - 280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 260 AND STA 280, BL 36 RIGHT AND WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500268 20000205 00268 WP 2000 2 5 RRXA991272 1 19990310 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 538 - 548 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 538 AND STA 548 AT BL 36 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500269 20000205 00269 WP 2000 2 5 RRXA991273 1 19990310 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 640 - 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 640 AND STA 660 AT BL 20 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 PGS 39/40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500270 20000205 00270 WP 2000 2 5 RRXA991274 1 19990310 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 690 - 710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BETWEEN STA 690 AND STA 710 AT BL 20 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500271 20000205 00271 WP 2000 2 5 RRXA991275 1 19990310 A 5315 FLOOR BOARD DOUG DC8 DC862F 3021972 WP BS 1520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBOARD, 1-1/2 AT STA 1520, BL 22 RIGHT. DAMAGE EXCEEDED LIMIT S IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 FIG 10 PGS 39/40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500272 20000205 00272 WP 2000 2 5 RRXA991276 1 19990801 A 7722 65003003 EGT INDICATOR DOUG DC8 DC873F 302199F WP NR 4 ENGINE MALFUNCTIONED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 870TV 46086 ON TAKEOFF, NR 4 ENGINE EGT WENT TO 929 DEGREES C AT 91 PERCENT N, OAT ON ATIS 35 DEGREES C, 29 DEGREES C FROM TOWER 120 KIAS, TARGET N1 91.8. REMOVED AND REPLACED NR 4 ENG EGT INDICATOR, CHECKED PMC, CHECKED INLETS AND EXHAUST FOR DAMAGE, CHECKED VSV'S AND VBV FOR DAMAGE, NONE NOTE. CHECKED EGT THERM/COUPLE HARNESS, CHECKED N2 ALTERNATOR FOR OPERATION, PER FORMED PMC TEST AND CLEANED ALL CONNECTIONS. OPS CHECKED TURBINE CLEARANCE CONTROL VALVE. CHECKED PNEUMATIC SYSTEM FOR LEAKS. NO DEFECTS NOTED. COULD NOT DUPLICATE. 2 L 7 4 4F RT 4A25 2000020500273 20000205 00273 WP 2000 2 5 RRXA991277 1 19990315 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 55 - 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LAVATORY FLOOR AND SHROUD CONNECTED AT LOCATION BETWEEN STA 55 AND STA 70 AND BETWEEN BL 60 RIGHT AND BL 40 RIGHT AT WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SECTION AND SHROUD IAW DC8 SRM 53-2-3 AND M/M 25-40-0. (CORR OSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500274 20000205 00274 WP 2000 2 5 RRXA991278 1 19990304 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 240 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 30 RIGHT AT STA 240. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM . REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED LONGERON SECTION IAW DC8 SRM 51-1-20D AN D 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500275 20000205 00275 WP 2000 2 5 RRXA991279 1 19990303 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1110 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1110, LONGERON 29 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING AND WEB IAW DC8 SRM 51-3 -0, 51-1-20D, AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500276 20000205 00276 WP 2000 2 5 RRXA991280 1 19990303 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1380 - 1400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERCOSTAL BETWEEN STA 1380 AND STA 1400 AT LONGERON 34 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCO STAL IAW DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500277 20000205 00277 WP 2000 2 5 RRXA991281 1 19990303 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP BS 1206 - 1380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CTR FLOOR ATTACH CHANNEL BETWEEN STA 1260 AND STA 1380 AT LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 2E/2F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500278 20000205 00278 WP 2000 2 5 RRXA991282 1 19990303 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1340 BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME S ECTION AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIG 2 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500279 20000205 00279 WP 2000 2 5 RRXA991283 1 19990305 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 863 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MAIN CARGO COMPT NR 9 FLOOR PANEL AT STA 863, BL 46 LEFT, WL 0. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR PANEL IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500280 20000205 00280 WP 2000 2 5 RRXA991284 1 19990318 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 460 - 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR PANEL, CARGO COMPARTMENT NR 5 BETWEEN STA 460 AND STA 540 AT BL 20 RIGHT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D AND INSTALLED PANEL IAW DC8 SRM 53-2-3, 51-3-0, 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500281 20000205 00281 WP 2000 2 5 RRXA991285 1 19990324 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 860 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT OUTBOARD PRESSURE BOX RT W/W LOWER L ANGLE AND WEB AT STA 860, LONGERON 24 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED L ANGLE AND WEB IAW DC8 SRM 51-1-4 AND 51-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500282 20000205 00282 WP 2000 2 5 RRXA991286 1 19990111 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 676 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, SKIN, AT SCREEN HOLE RT WING O/B L/E I/B SEGMENT AT STA XFS 676.756 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED DOUBLER AND FILLER IAW DC8 SRM 57-2-0 FIG 38 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) . 2 L 7 4 4F RT 4A25 2000020500283 20000205 00283 WP 2000 2 5 RRXA991287 1 19990112 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 13.75 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, L/E UPPER SURFACE AT STA XFS 13.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 57-2- 1 FIG 37. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500284 20000205 00284 WP 2000 2 5 RRXA991288 1 19990112 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 7.50 - 32.5 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, L/E UPPER SURFACE FROM STA XFS 7.50 TO STA XFS 32.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPRO VED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-004 AND 8110-3 DATED 01/19/99. (CORROSION DAMAGE RECOR DED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500285 20000205 00285 WP 2000 2 5 RRXA991289 1 19990211 A 5320 FINGER DOUBLER DOUG DC8 DC871F 302199D WP BS 32 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER AT LT CUSP LINE STA -32. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500286 20000205 00286 WP 2000 2 5 RRXA991292 1 19990113 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD AT STRAP, FRAME, AT STA 160, BETWEEN LONGERONS 36 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED STRAP AND REPAIR FASTENERS IAW DC8 SRM 51-1-4 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500287 20000205 00287 WP 2000 2 5 RRXA991293 1 19990113 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE UNDER NR 3 O-BOTTLE CRADDLE ABOVE FRAME AT STA 100, LONGERON 28 RIG HT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500288 20000205 00288 WP 2000 2 5 RRXA991294 1 19990113 A 5320 STIFFNER DOUG DC8 DC871F 302199D WP BS 100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT AT STA 100, BETWEEN BL 21 RIGHT AND BL 33 RIGHT, HORIZONTA L STIFFENER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED STIFFENER IAW DCI SRM 51-1-4 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500289 20000205 00289 WP 2000 2 5 RRXA991295 1 19990113 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME AT STA 120, BETWEEN LONGERONS 30 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED ANGLE DOUBLER IAW DC8 SRM 53-2-0 FIG 1B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500290 20000205 00290 WP 2000 2 5 RRXA991296 1 19990113 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME ATTACH ANGLE AT STA 140, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACH ANGLE IAW DC8 SRM 51-1-4 AND 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500291 20000205 00291 WP 2000 2 5 RRXA991297 1 19990113 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME ATTACH ANGLE AT STA 160, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC 8 SRM 51-2-0 FIG 50 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500292 20000205 00292 WP 2000 2 5 RRXA991298 1 19990113 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD ACCESSORY COMPT FRAME AT STA 70, BETWEEN LONGERONS 31 LEFT AND LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 51-1-21 AND 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500293 20000205 00293 WP 2000 2 5 RRXA991299 1 19990115 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 280 - 287 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, BETWEEN STA 280 AND STA 287, AND BETWEEN LONGERONS 28 LEFT AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED REPAIR PARTS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-016 AND DC 8 SRM 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500294 20000205 00294 WP 2000 2 5 RRXA991300 1 19990130 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME AT STA 480, BETWEEN LONGERONS 35 LEFT AND LONGERON 3 3 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED DOUBLERS IAW DC8 SRM 51-3-0 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500295 20000205 00295 WP 2000 2 5 RRXA991301 1 19990130 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD PIT FRAME AT STA 420, BETWEEN LONGERONS 36 AND LONGERON 27 RIG HT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500296 20000205 00296 WP 2000 2 5 RRXA991302 1 19990108 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP BS 1420 - 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE GILL LINER ATTACHMENT SUPPORT FROM STA 1420R TO STA 1440R AT LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D AND INSTALLED SUPPORT IAW DC8 SRM 51-1-4 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500297 20000205 00297 WP 2000 2 5 RRXA991303 1 19990113 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP BS 120 - 140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SUPPORT STRAP, FWD PIT BETWEEN STA 120 AND STA 140 AND BETWEEN LON GERONS 36 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 . FABRICATED AND INSTALLED SUPPORT STRAP IAW DC8 SRM 51-1-4 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION P ROGRAM). 2 L 7 4 4F RT 4A25 2000020500298 20000205 00298 WP 2000 2 5 RRXA991304 1 19990110 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ACCESSORY, FWD, FRAME AT STA 680, BETWEEN LONGERONS 34 LEFT AND LO NGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A ND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-003 AND 8110-3 DATED 01/18/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500299 20000205 00299 WP 2000 2 5 RRXA991306 1 19990109 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1306 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE UPPER CAP UNDER NUT PLATE AND WEB AT STA 1306, BETWEEN LONGE RONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51 -1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-0 AND 53-02-0. (CORROSION DAMAGE RECORDED IN EWA CORROS ION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500300 20000205 00300 WP 2000 2 5 RRXA991307 1 19990109 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE, OUTPLATES TOP CAP AND AFT FACE OF WEB FRAME, AT STA 1260 BE TWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS, REPAIR STRAP, REPAIR ANGLE IAW FAA APPROVED TENESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-002. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500301 20000205 00301 WP 2000 2 5 RRXA991308 1 19990110 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE FRAME AT NUTPLATES, AT STA 1040, BETWEEN LONGERONS 28 LEFT A ND LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 53-2-0 FIG F. AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA COR ROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500302 20000205 00302 WP 2000 2 5 RRXA991309 1 19990110 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE AT STA 1100, LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLES IAW DC8 SRM 51-1-9 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500303 20000205 00303 WP 2000 2 5 RRXA991310 1 19990112 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB AREA AT STA 540, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2 -0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500304 20000205 00304 WP 2000 2 5 RRXA991311 1 19990112 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 1380 - 1400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MEMBRANE, LT UPPER CUSP BETWEEN STA 1400 AND STA 1380 AT LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500305 20000205 00305 WP 2000 2 5 RRXA991312 1 19990111 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP DOOR FRAME FITTING AT STA 1620, LONGERON 21 LEFT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOOR F RAME FITTING IAW DC8 SRM 51-1-3 FIG 55 AND 51-1-3 PARAGRAPH 5. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500306 20000205 00306 WP 2000 2 5 RRXA991313 1 19990111 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, R-2 DOOR FWD FRAME INSIDE WEB AT STA 1620, LONGERON 21 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED 2 EACH FITTINGS IAW DC8 SRM 51-2-0, 51-3-0, AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500307 20000205 00307 WP 2000 2 5 RRXA991314 1 19990107 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 487 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ANGLE, RT UPPER CUSP LONGITUDINAL AT STA 487, FLOOR LEVEL, LONGERO N 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IN STALLED ANGLE IAW DC8 SRM 51-1-4 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500308 20000205 00308 WP 2000 2 5 RRXA991315 1 19990121 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 8 - 80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ENTRANCE AND LAV FLOOR, BETWEEN STA -8.0 AND STA 80. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL SKINS ON 9 EA PANELS IAW DC8 SRM 53-2-3 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500309 20000205 00309 WP 2000 2 5 RRXA991316 1 19990107 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT UPPER CUSP MEMBRANE WEB AT STA 560, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IA W FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR 99-010 WITH 8110-3 DATED 01/25/99. (CORROSION DAM AGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500310 20000205 00310 WP 2000 2 5 RRXA991317 1 19990110 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 640 - 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MARKER BEACON MOUNTING SKIN BETWEEN STA 640 AND STA 660 AND BETWEE N LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. FAA APPROVED TENNESSEE TECHNICAL SERV ICES DER ENGINEERING SKETCH NR EO 99-008 AND 8110-3 DATED 01-20-99 ALLOWS LIMITS TO EXCEED DC8 SRM 51-1-8, REMOVED CORR OSION AND BLEND AREA FLAP PEEN, REWORKED AREA PROTECT AREA PER DC8 SRM 51-1-8 AND FILL TO ENSURE SMOOTH CONTOUR PER NR E O 99-008 AND 8110-3 DATED 01-20-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500311 20000205 00311 WP 2000 2 5 RRXA991318 1 19990113 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1793 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1793, BETWEEN LONGERONS 35 LEFT AND LONGERON 35 RIGH T IN CHANNEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 53-5-1 INDEX E. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500312 20000205 00312 WP 2000 2 5 RRXA991319 1 19990107 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1843 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT FRAME AT STA 1843, LONGERON 6 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENN ESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-011 AND 8110-3 DATED 01/27/99. (CORROSION DAMAGE RECORDED IN EW A CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500313 20000205 00313 WP 2000 2 5 RRXA991321 1 19990403 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 55 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON FITTING AT STA 55, LONGERON 32 RIGHT AT FWD PRODUCTION SP LICE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D NEW FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500314 20000205 00314 WP 2000 2 5 RRXA991322 1 19990403 A 5711 SPAR DOUG DC8 DC871F 302199D WP WS 485 & 710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, O/B L/E O/B SECTION UPPER SURFACE 17 FWD OF FRONT SPAR BETWEEN ST A XFS 710 AND STA XW 485. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. LIM ITATIONS EXCEEDED SRM LIMITATIONS, FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR 99-57-03251 APPRO VES ADDITIONAL LIMITATIONS THAT EXCEEDED SRM LIMITS. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500315 20000205 00315 WP 2000 2 5 RRXA991323 1 19990307 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 178 - 230.5 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, AROUND SCREW HOLES RIGHT WING OUTBOARD FLAP INBOARD SEGMENT UPPER SURF ACE BETWEEN STA XRS 230.500 AND STA XRS 178.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IA W DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-21 AND 57-2-1 FIG 2Q. (CORROSION DAMAG E RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500316 20000205 00316 WP 2000 2 5 RRXA991324 1 19990811 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 HOLE AND DENT IN BELLY BY A/C ACCESS DOOR. REMOVED DAMAGED AREA, TREATED STRUCTURE IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED FUSELAGE PLATE REPAIR IAW DC-8 SRM 53-2-1. 2 L 7 4 4F RT 4A25 2000020500317 20000205 00317 WP 2000 2 5 RRXA991325 1 19990413 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 878.75 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, O/B L/E O/B SEGMENT LWR SURFACE AT STA XFS 878.750. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER A ND FILLER IAW DC8 SRM 57-2-1 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500318 20000205 00318 WP 2000 2 5 RRXA991326 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 878.75 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B L/E O/B SEGMENT O/B END LWR SURFACE 22 FWD OF FRONT SPAR AT STA XFS 878.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A ND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 51-1-21 AND 57-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2000020500319 20000205 00319 WP 2000 2 5 RRXA991327 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, IN SCREW HOLES O/B LEADING EDGE OUTBOARD SEGMENT INBOARD EDGE AT STA XFS 710. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 57-2-1 AND 57-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRA M). 2 L 7 4 4F RT 4A25 2000020500320 20000205 00320 WP 2000 2 5 RRXA991328 1 19990430 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, SKIN EDGE AND SCREW HOLES AT WING O/B LEADING EDGE I/B SECTION O F STA XS 540 BETWEEN + 38 AND +45 FORWARD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATE D AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 57-2-1 AND 51-1-21. (CORROS ION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500321 20000205 00321 WP 2000 2 5 RRXA991329 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B LEADING EDGE I/B SEGMENT O/B EDGE AT STA XFS 710. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 57-2-1 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500322 20000205 00322 WP 2000 2 5 RRXA991330 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 566 & 603 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, IN SCREW HOLES O/B LEADING EDGE, I/B SEGMENT UPPER SURFACE AT FR ONT SPAR BETWEEN STA XFS 566.250 AND STA XFS 603.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AR EA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 57-2-1, 51-1-21, AND 51-1-21A. (CORROS ION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500323 20000205 00323 WP 2000 2 5 RRXA991331 1 19990423 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 304 - 397 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, AROUND SCREW HOLES, L/E CENTER SECTION UPPER SURFACE BETWEEN STA XFS 304 AND STA XFS 397.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED AND INSTALLED DOUBLER AND FILLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99 085. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500324 20000205 00324 WP 2000 2 5 RRXA991332 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B SLOT UPPER I/B PANEL AT L/E, STA XFS. 2 L 7 4 4F RT 4A25 2000020500325 20000205 00325 WP 2000 2 5 RRXA991333 1 19990420 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 286 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, IN SCREW HOLES, LEADING EDGE CENTER SECTION LOWER SURFACE, 46 FOR WARD OF FRONT SPAR AT STA XFS 286.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 57-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500326 20000205 00326 WP 2000 2 5 RRXA991334 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 191.625 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACEO/B END AT STA XFS 191.625. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-21 AND 51-1-20A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500327 20000205 00327 WP 2000 2 5 RRXA991335 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 151.25 - 157 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E TANK UPPER SURFACE AROUND SCREW HOLES BETWEEN STA XFS 15 1.250 AND XFS 157.500. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-08 5 AND DC8 SRM 51-1-12. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500328 20000205 00328 WP 2000 2 5 RRXA991336 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 7.5 - 26.25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 7.50 AND STA XFS 26.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED REPAIR DOUBLERS AND FILLERS IAW FAA APROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-085 AN D DC8 SRM 57-2-1 FIG 37. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500329 20000205 00329 WP 2000 2 5 RRXA991337 1 19990422 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 95 - 101.25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, L/E TANK UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 95.000 AND STA XFS 101.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-085. (CORROSION DAM AGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500330 20000205 00330 WP 2000 2 5 RRXA991338 1 19990417 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 7.5 - 26.25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN STA XFS 7.50 AND XF S 26.25. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED DOUBLER IAW DC8 SRM 52-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500331 20000205 00331 WP 2000 2 5 RRXA991339 1 19990417 A 5522 SKIN DOUG DC8 DC873F 302199F WP WS 259 - 269 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LT ELEVATOR, 3 SPOTS BETWEEN STA XE259 AND STA XE 269. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLERS TO TRAILI NG EDGE IAW DC8 SRM 51-1-1 TABLE B AND 51-1-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500332 20000205 00332 WP 2000 2 5 RRXA991340 1 19990417 A 5522 SKIN DOUG DC8 DC873F 302199F WP WS 32 - 50 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, LT ELEVATOR, AREA UNDER PANEL 69 BETWEEN STA XE 32.937 AND STA XE 50.00. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-085 AND DC8 SRM 55-2-0. (CORROSIO N DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500333 20000205 00333 WP 2000 2 5 RRXA991341 1 19990426 A 5522 WEB DOUG DC8 DC873F 302199F WP WS 32 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT ELEVATOR INBOARD LIGHTNING HOLES AT STA XE 32.9. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 55-2- 1. REPAIR INDEX 2E AND 51-2-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500334 20000205 00334 WP 2000 2 5 RRXA991342 1 19990421 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 8 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 33 RIGHT END TIE FITTING AT STA 8.00. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW FAA APPROVE D TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR 99 085. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500335 20000205 00335 WP 2000 2 5 RRXA991343 1 19990414 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 100 - 120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LAV SERVICE DOOR PANEL BETWEEN STA 100 AND STA 120 RIGHT AND BETWE EN LONGERONS 24 RIGHT AND LONGERON 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC -8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-085/6256 AND 8110-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500336 20000205 00336 WP 2000 2 5 RRXA991344 1 19990413 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 717 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM SKIN AT STA 717 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENN ESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-085. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500337 20000205 00337 WP 2000 2 5 RRXA991345 1 19990413 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 702 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM SKIN AT STA 702 BETWEEN LONGERONS 34 LEFT AND LONGERON 34 R IGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR II-085 AND DC8 SRM 53-2-0. (CORROSIO N DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500338 20000205 00338 WP 2000 2 5 RRXA991346 1 19990430 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1746 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN FORWARD OF TAIL SKID AT STA 1746, LONGERON 36. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SR M 51-1-21 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500339 20000205 00339 WP 2000 2 5 RRXA991347 1 19990420 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 660 - 702 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM OF FUSELAGE MARKER BEACON ANTENNA FROM BASE AROUND SKIN BET WEEN STA 680 AND STA 702 AT LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 S RM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DC8 SRM 53-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PRO GRAM). 2 L 7 4 4F RT 4A25 2000020500340 20000205 00340 WP 2000 2 5 RRXA991348 1 19990413 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE AT NUT PLATES STA 640 BETWEEN LONGERONS 27 LEFT AND L ONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500341 20000205 00341 WP 2000 2 5 RRXA991349 1 19990515 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 460 - 480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER, B-PIT, LEFT FWD BETWEEN STA 460 AND STA 480 AT LON GERON 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-085. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500342 20000205 00342 WP 2000 2 5 RRXA991350 1 19990413 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE, FRAME AT STA 360, AFT SIDE ABOVE BETWEEN LONGERONS 3 1 RIGHT AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED TENNESSEE TECHNIDAL SERVICES DER ENGINEERING SKETCH NR 99-085. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500343 20000205 00343 WP 2000 2 5 RRXA991351 1 19990417 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE, LOWER AFT CARGO COMPARTMENT AT STA 1320, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED DOUBLER AND SUPPORT ANGLE IAW DC8 SRM 53-2-0 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500344 20000205 00344 WP 2000 2 5 RRXA991352 1 19990415 A 5320 CHANNEL DOUG DC8 DC873F 302199F WP BS 980 - 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR ATTACH CHANNEL BETWEEN STA 980 AND STA 1140 AT LONGERON 33 L EFT.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D FLOOR CHANNEL IAW DC8 SRM 51-1-4 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500345 20000205 00345 WP 2000 2 5 RRXA991353 1 19990415 A 5320 CHANNEL DOUG DC8 DC873F 302199F WP BS 980 - 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR ATTACH CHANNEL BETWEEN STA 980 AND STA 1140 AT LONGERON 33 R IGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D FLOOR CHANNEL IAW DC8 SRM 51-1-21 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500346 20000205 00346 WP 2000 2 5 RRXA991354 1 19990413 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM UNDER SEAT TRACK 3 ABOVE LONGERON 32 LEFT AT STA 1700. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO 99-085. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500347 20000205 00347 WP 2000 2 5 RRXA991355 1 19990419 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1726 - 1745 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SPLICE, LONGERON 36, BETWEEN STA 1726 AND STA 1745. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE AND LONGERON SECTION IAW DC8 SRM 53-2-9, 51-1-2 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500348 20000205 00348 WP 2000 2 5 RRXA991356 1 19990419 A 5320 SHIM DOUG DC8 DC873F 302199F WP BS 400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP AT STA 400 FRAME ATTACH ANGLE SHIM FROM UNDER SHIM M ARKED 12 NR 83. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AN D INSTALLED SHIM IAW DC8 SRM 51-1-21 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500349 20000205 00349 WP 2000 2 5 RRXA991357 1 19990424 A 5320 SHIM DOUG DC8 DC873F 302199F WP BS 380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP AT STA 380 FROM FRAME ATTACH ANGLE SHIM, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED SHIM IAW DC8 SRM 51-1-4 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500350 20000205 00350 WP 2000 2 5 RRXA991358 1 19990419 A 5320 SHIM DOUG DC8 DC873F 302199F WP BS 360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP FRAME AT STA 360 FROM SHIM AT ATTACH ANGLE, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED SHIM AND FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500351 20000205 00351 WP 2000 2 5 RRXA991359 1 19990420 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT UPPER CUSP FRAME AT STA 560 ATTACH ANGLE, LONGERON 21 LEFT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DA C DWG 5753488 AND DC8 SRM 51-1-21 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500352 20000205 00352 WP 2000 2 5 RRXA991360 1 19990413 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH FITTING AT STA 460, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT ATTACH FITTI NG IAW DC8 SRM 51-3-0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500353 20000205 00353 WP 2000 2 5 RRXA991361 1 19990423 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1746 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT UNDER CLIP NUTS, AT STA 1746, BETWEEN BL 1.5 LEFT AN D BL 20.5 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AN D INSTALLED FLOORBEAM SUPPORT IAW DC8 SRM 51-1-21 AND 51-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500354 20000205 00354 WP 2000 2 5 RRXA991362 1 19990510 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR TRACK NR 4 SUPPORT FITTING AT STA 1700, BL 35 LEFT, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED FITTING IAW DAC DWG NR 2652479 AND DC8 SRM 51-1-2, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500355 20000205 00355 WP 2000 2 5 RRXA991363 1 19990423 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1746 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT UNDER CLIP NUTS AT STA 1746, BETWEEN BL 7-1/2 RIGHT AND BL 23 1/2 RIGHT AT LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUPPORT IAW DC8 SRM 51-2-0, 53-4-1, AND 51-1-21. (CORROSION DAMAGE RECORDED IN EW A CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500356 20000205 00356 WP 2000 2 5 RRXA991364 1 19990503 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 606AL 46044 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MID AC COMPARTMENT ACCESS DOOR FRAME, FWD SIDE AROUND CAM LOCK HOL ES, AT STA 640, BETWEEN BL 12 RIGHT AND BL 24 RIGHT, AT WL 45 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAM AGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-21 AND 51-1-0, 52- 2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500357 20000205 00357 WP 2000 2 5 RRXA991365 1 19990703 A 5720 INTERCOSTAL DOUG DC8 DC871F 302199D WP WS 129 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, INTERCOSTAL TOP CUP BETWEEN LEFT WING NR 2 AND NR 3 SPOILERS AT S TA XW 129. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED DOUBLERS IAW DC8 SRM 57-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500358 20000205 00358 WP 2000 2 5 RRXA991366 1 19990308 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 11.25 - 194 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B LEADING EDGE BETWEEN STA XFS 11.25 AND XFS 194. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21, 51-1-20D, 57-2-4 FIG 37 AND 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500359 20000205 00359 WP 2000 2 5 RRXA991367 1 19990111 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 660 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, ACCY COMPT AT LONGERON 34 LEFT, STA 660 ATTACHMENT POINT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILL ER AND DOUBLER IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500360 20000205 00360 WP 2000 2 5 RRXA991368 1 19990203 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 500 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 500, LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 AND 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500361 20000205 00361 WP 2000 2 5 RRXA991369 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 1080 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN SEAT TRACK AT STA 1080, BL 45 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SECTION EXTRUSION AND SPLIC ES IAW DC8 SRM 53-2-3 PGS 49-50. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500362 20000205 00362 WP 2000 2 5 RRXA991370 1 19990304 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN SEAT TRACK AT STA 1420, BL 24 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SECTION AND SPLICE REPAIR IA W DC8 SRM 53-2-3 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500363 20000205 00363 WP 2000 2 5 RRXA991371 1 19990303 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PANEL AT STA 1480, BL 38 RIGHT. DAMAGE EXCEEDED LIMIT S IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 PGS 2P FIG 1F AND 53-2-3 PGS 39-40 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500364 20000205 00364 WP 2000 2 5 RRXA991372 1 19990302 A 5730 SKIN DOUG DC8 DC862F 3021972 WP WS 178 - 217 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, SKIN, LT O/B FLAP I/B BETWEEN STA XRS 178 AND XRS 217. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN IAW DC8 SR M 57-7-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500365 20000205 00365 WP 2000 2 5 RRXA991373 1 19990301 A 5312 BULKHEAD DOUG DC8 DC862F 3021972 WP BS 960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BULKHEAD, LMLG W/W TOP PRESSURE DECK AT OUTBOARD EDGE, STA 960, BL 60 LEFT, PRIMARY STRUCTURE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG NR SRO 8530026. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) . 2 L 7 4 4F 4A25 2000020500366 20000205 00366 WP 2000 2 5 RRXA991374 1 19990301 A 5312 BULKHEAD DOUG DC8 DC862F 3021972 WP BS 870 & 874 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BULKHEAD, RT MLG W/W PRESSURE DECK, BL 48 RIGHT, STA 874, 4 AFT OF FWD BULKHEAD STA 870. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED DOUBLER AND ANGLE IAW FAA APPROVED COMMODORE AVIATION DER ENGINEERING SKETCH NR 99-0016RR. (CORROSIO N DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500367 20000205 00367 WP 2000 2 5 RRXA991375 1 19990301 A 5312 BULKHEAD DOUG DC8 DC862F 3021972 WP BS 870 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BULKHEAD, ON FWD BULKHEAD, IN R/MLG W/W AT STA 870, BL 30 RIGHT, W L 10 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IN STALLED REAR SPAR TO FUSELAGE ANGLE REPAIR IAW DC8 SRM 53-2-5 PG 16. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRA M). 2 L 7 4 4F 4A25 2000020500368 20000205 00368 WP 2000 2 5 RRXA991376 1 19990305 A 5530 ANGLE DOUG DC8 DC862F 3021972 WP ` VERTICAL STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, VERTICAL STABILIZER, RT SIDE ATTACH ANGLE BRACKET STRIP AT STA 1542, LONGERO N 2 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED NEW ANGLE SECTION AND SPLICE IAW DC8 SRM 53-2-5, FIG 16A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500369 20000205 00369 WP 2000 2 5 RRXA991379 1 19990610 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, AFT LOWER CARGO COMPARTMENT AT STA 1220, BL 45 RIGHT FLOOR STRUT DOUBLER NEX T TO FLOORBEAM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND R EPLACED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO- 99-094 WITH APPROVED 8110-3, DATED JUNE 12, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500370 20000205 00370 WP 2000 2 5 RRXA991380 1 19990616 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 75 - 105 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN, BOTTOM OF FWD LAV SERVICE PANEL BETWEEN STA 75R AND STA 105R , AND BETWEEN LONGERONS 25 RIGHT AND LONGERON 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 11, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500371 20000205 00371 WP 2000 2 5 RRXA991381 1 19990702 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT AT STA 1320, BL 55 RIGHT, FLOOR PANEL AND SUPPORT BEAM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 AND DC8 SRM 51-1-20D, WITH APPROVED 8110-3 DATED JUNE 12, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500372 20000205 00372 WP 2000 2 5 RRXA991382 1 19990609 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 54 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT WING I/B L/E UPPER SURFACE AT STA XFS 54.000. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IA W FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500373 20000205 00373 WP 2000 2 5 RRXA991383 1 19990601 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 38.75 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, SCREW HOLE LEFT WING I/B L/E UPPER SURFACE AT XFS 38.750 AT FRONT SPAR . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FI LLERS AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110- 3 DATED JUNE 12, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500374 20000205 00374 WP 2000 2 5 RRXA991384 1 19990618 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 8 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, POPPED RIVET AND BULGE IN EXTERNAL SKIN, LONGERON FITTING END CORR ODED INSIDE FWD ACCESSORY COMPARTMENT AT STA 8, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE D, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 25, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500375 20000205 00375 WP 2000 2 5 RRXA991385 1 19990723 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1020 - 1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 1020 AND STA 1060, AND BET WEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT, ON SKIN. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED A REA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED, REPLACED SKIN FROM STA 1120 TO STA 1020, BETWEEN LONGERONS 34 LEFT A ND LONGERON 34 RIGHT IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 811 0-3 DATED JULY 06, 1999.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500376 20000205 00376 WP 2000 2 5 RRXA991386 1 19990608 A 5320 FINGER DOUGLER DOUG DC8 DC873F 302199F WP BS 67 - 82 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BULGE AND RIVETS POPPED ON FINGER DOUBLER AT STA -82 TO STA -67 RI GHT HAND SIDE BL 60 RIGHT, 10 BELOW COCKPIT FLOOR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENG INEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2000020500377 20000205 00377 WP 2000 2 5 RRXA991387 1 19990625 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 291 - 297 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, LEADING EDGE CENTER SECTION I/B EDGE BETWEEN STA 291.5 TO 297.50 0, 15 TO 21 INCHES FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500378 20000205 00378 WP 2000 2 5 RRXA991388 1 19990617 A 5320 FINGER DOUGLER DOUG DC8 DC873F 302199F WP BS 616 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BLISTER AT FINGER DOUBLER AT STA 616 BETWEEN LONGERONS 32 RIGHT AN D LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED AND INSTALLED NEW FINGER DOUBLER AND SKIN SPLICE STRAP IAW DC8 SRM 53-2-1 AND INSTALLED IAW DC8 SRM 51-1-20D.. (CORR OSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500379 20000205 00379 WP 2000 2 5 RRXA991389 1 19990610 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1020 - 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 1020 AND STA 1140, FLOOR T RACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D NEW TRACK IAW DC8 SRM 51-1-22 AND INSTALLED PER DC8 SRM 51-1-20. TRACK MATERIAL 7178-T6511 SUBSTITUTED FOR 7075T6 PER FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500380 20000205 00380 WP 2000 2 5 RRXA991390 1 19990610 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 980 - 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 980 AND STA 1100 TRACK. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TR ACK IAW DC8 SRM 51-1-22 AND INSTALLED IAW DC8 SRM 51-1-20. TRACK MATERIAL 7075-T6 REPLACED WITH 7178-T6511 IAW FAA APPR OVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUEN 12, 1999. (CORROS ION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500381 20000205 00381 WP 2000 2 5 RRXA991391 1 19990604 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN UNDER A PIT DOOR CORRODED AND MISSING LAYER AT STA 320, LONG ERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS AND FILLERS FROM 7075-T6 .050 LOT NR 341343 IAE FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINE ERING SKETCH NR EO-99-094. INSTALLED DOUBLER AND FILLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING S KETCH NR EO 99-094 AND DC8 SRM 51-1-20D AND 51-1-21 WITH APPROVED 8110-3 DATED JUNE 11, 1999. (CORROSION DAMAGE RECORDE D IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500382 20000205 00382 WP 2000 2 5 RRXA991392 1 19990728 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1420 - 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LOWER EXTERIOR SKIN BETWEEN STA 1420 AND STA 1440, AT LONGERON 36 PREVIOUS REPAIR DOUBLER SHEARED FASTENER AND CORROSION EMANATING FROM UNDER DOUBLER. DAMAGE EXCEEDED LIMITS IAW DC-8 SR M. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TEN NESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 25, 1999. (CORROSION DAMA GE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500383 20000205 00383 WP 2000 2 5 RRXA991393 1 19990604 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LOWER SKIN AT STA 1420, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW D C-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPRO VED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APROVED 8110-3 DATED JUNE 25, 1999. (CORROSIO N DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500384 20000205 00384 WP 2000 2 5 RRXA991394 1 19990625 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP BS 1745 - 1766 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT CABIN BETWEEN STA 1745 AND STA 1766 FLOOR SUPPORT CHANNEL CROS S OVER STIFFENER HAS CORROSION EXFOLIATION EMANATING FROM FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMA GED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNELS AND CROSS OVER STIFFENERS FROM 7 076-T6 EXTRUSIED IAW DC8 SRM 51-1-4. INSTALLED HAT CHANNELS AND STIFFENERS IAW DC8 SRM 51-1-20D IAW FAA APPROVED TENNES SEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500385 20000205 00385 WP 2000 2 5 RRXA991395 1 19990616 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 31 LEFT AT STA 1220. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM . REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLATE DOUBLER IAW DC8 SRM 51-1-21 AND IA W FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JULY 01, 1999 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500386 20000205 00386 WP 2000 2 5 RRXA991396 1 19990628 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 260 - 280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD LAV SVC PANEL WELL AREA, ALSO RUSTED DOME NUTS BETWEEN STA 260 AND STA 280, AND BETWEEN LONGERONS 24 RIGHT AND LONGERON 26 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAG ED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS AND FILLER IAW DC8 SRM 51-1-21 AND IAW FAA APPR OVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 10, 1999. (CORROS ION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500387 20000205 00387 WP 2000 2 5 RRXA991397 1 19990725 A 3213 STRUT PIN DOUG DC8 DC873F 302199F WP LT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT MLG RETRACT CYL A-PIN REPAIR/INSP IAW MA-A1 3210-01-03, S/B 32-102. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED EYE BOLT, RETRACT PIN, REMOVED CORROSION FROM BOSS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPRO VED 8110-3 DATED JUNE 20, 1999 AND C/W MA-A1 3210-01-03 AND S/B 32-102. (CORROSION DAMAGE RECORDED IN EWA CORROSION PRO GRAM). 2 L 7 4 4F RT 4A25 2000020500388 20000205 00388 WP 2000 2 5 RRXA991398 1 19990725 A 3213 STRUT PIN DOUG DC8 DC873F 302199F WP RT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG RETRACT CYL A-PIN REPAIR/INSP IAW MA-A1 3210-01-03, S/B 32-102. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED EYE BOLT, RETRACT PIN AND REMOVED CORROSION FROM BOSS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPR OVED 8110-3 DATED JUNE 20, 1999 AND C/W MA-A1 3210-01-03 AND S/B 32-102. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F RT 4A25 2000020500389 20000205 00389 WP 2000 2 5 RRXA991399 1 19990702 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME CAP AT STA 1100 BETWEEN LONGERONS 35 LEFT AND LONGERON 35 RI GHT.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D FILLERS AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8 110-3 DATED JUNE 24, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500390 20000205 00390 WP 2000 2 5 RRXA991400 1 19990702 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BLISTER ON FRAME 70, BETWEEN LONGERONS 33 RIGHT AND LONGERON 32 RI GHT.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).. 2 L 7 4 4F RT 4A25 2000020500393 20000205 00393 WP 2000 2 5 AT0000040 1 19991209 A 5720 FITTING DOUG DC9 DC932 3022066 WP WS 111 - 500 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND GOUGE IN WING LEADING EDGE FITTING XRS 111-500. BLENDED G OUGE AND NDT TESTED IAW EO 99-1406. 2 L 7 2 4F A6WE 2000020500394 20000205 00394 WP 2000 2 5 AT0000041 1 19991207 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 897 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND HOLES AND CRACKS IN RIGHT FUSELAGE FRAME AT BS 897. REPAI RED HOLES AND CRACKS IN RIGHT FUSELAGE FRAME BS 897 IAW EO 99-1404. 2 L 7 2 4F A6WE 2000020500395 20000205 00395 WP 2000 2 5 RRXA991623 1 19990521 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WHEEL WELL ANGLE FITTING TOP OF W/W AT STA 980, BL 46 LEFT AND WL 10 RIGHT, BELOW SEAT TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED AND INSTALLED NEW FITTING AND REPAIR ANGLES IAW DC8 SRM 51-1-4 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500396 20000205 00396 WP 2000 2 5 RRXA991624 1 19990523 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1890 - 1916 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, AFT FUSELAGE, TAIL CONE AROUND ACCESS PANEL 62 INTERIOR FRAME BETWEEN STA 18 90 AND STA 1916, AND BETWEEN LONGERONS 34 RIGHT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAM AGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME DOUBLERS IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500397 20000205 00397 WP 2000 2 5 RRXA991625 1 19990828 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 341.5 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, LE, UPPER SKIN BETWEEN XFS 341.50 AND XOLDI 6.225. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW FAA SKE TCH NR 087-252. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500398 20000205 00398 WP 2000 2 5 RRXA991626 1 19990825 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 6.225 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, OB, SLOT VANE, INNER DOUBLER AT XOLDI 6.225. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAC DWG 576 9933-21 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500399 20000205 00399 WP 2000 2 5 RRXA991627 1 19990822 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 250 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, AND BULGED SKIN AT FRONT SPAR, STA XS 250.089. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57 -2-0 FIG 2A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500400 20000205 00400 WP 2000 2 5 RRXA991628 1 19990820 A 5711 FRAME DOUG DC8 DC871F 302199D WP WS 7.20 - 20 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, LE, AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND X FS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED THE CHORD IAW DC8 SRM 51-1-20D, 51-1-21A, AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500401 20000205 00401 WP 2000 2 5 RRXA991629 1 19990831 A 5720 FITTING DOUG DC8 DC871F 302199D WP WS 410 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, RIGHT, RT OB FLAP AT STA X=410 FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED REPAIR IAW SKETCH NR 087-305. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500402 20000205 00402 WP 2000 2 5 RRXA991630 1 19990921 A 5510 PLANK DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, HORIZONTAL STABILIZER, CENTER SECTION UPPER CENTER PLANK UPPER SURFACE AT RB L X30. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED PLANK IAW SB 55-15. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500403 20000205 00403 WP 2000 2 5 RRXA991631 1 19990817 A 5320 FINGER DOUBLER DOUG DC8 DC871F 302199D WP BS 100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER AT LONGERON 31 RIGHT, AT STA 100. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DA C DWG 5779917 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500404 20000205 00404 WP 2000 2 5 RRXA991632 1 19990817 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 350 - 370 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SUFRACE OF OUTER SKIN BETWEEN LONGERONS 31 LEFT AND LONGERON 31 RIGHT AND BETWEEN STA 350 AND STA 370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SKETCH NR SK087-990 8110-3 APPROVED. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500405 20000205 00405 WP 2000 2 5 RRXA991633 1 19990819 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT AT STA 600, BETWEEN LONGERON 33 RIGHT AND LONGERON 3 6. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED F LOOR SUPPORT IAW DAC DWG 5707967 AND DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500406 20000205 00406 WP 2000 2 5 RRXA991634 1 19990824 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1120, BETWEEN LONGERONS 36 AND LONGERON 34 RIGHT. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ED FRAME IAW DC8 SRM 53-2-0, FIG 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500407 20000205 00407 WP 2000 2 5 RRXA991635 1 19990901 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1727 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM AT STA 1727 AT FRAME R/S. DAMAGE EXCEEDED LIMITS IAW DC -8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM IAW FAA DER ENGINEERING SKETCH NR SK-087-316.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500408 20000205 00408 WP 2000 2 5 RRXA991636 1 19990901 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1727 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE FRAME AT FLOORBEAM AT STA 1727, LONGERON 21 RIGHT. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500409 20000205 00409 WP 2000 2 5 RRXA991637 1 19990819 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 920 - 940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB, BETWEEN STA 920 AND STA 940, AT LONGERON 22 RIGHT AND RIGHT B L 60. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D REPAIR WEB IAW FAA SKETCH NR SK0870089, APPROVED 8110-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500410 20000205 00410 WP 2000 2 5 RRXA991638 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 5162 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, WING, LEFT, UPPER T/E SKIN, UPPER SEVERAL FASTENER HOLES BETWEEN 1 AND 4 AFT OF REAR SPAR AT XR 5162.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED AND REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2000020500411 20000205 00411 WP 2000 2 5 RRXA991639 1 19990815 A 5280 SKIN DOUG DC8 DC871F 302199D WP MLG DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, RT MLG DOOR ON INNER SKIN AT O/B CORNER OF AFT END CENTER WING TO WING . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPA IRED IAW DC8 SRM 52-6-1 FIG 1. 2 L 7 4 4F RT 4A25 2000020500412 20000205 00412 WP 2000 2 5 RRXA991640 1 19990816 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 208 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT, L/E, LWR SKIN AT STA XS 208, 31 FWD OF THE SPAR. THE CRACK IS APPR OX 2 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLE D CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 2000020500413 20000205 00413 WP 2000 2 5 RRXA991641 1 19990816 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 163.75 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LOWER END. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500414 20000205 00414 WP 2000 2 5 RRXA991642 1 19990816 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 301.25 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN AT STA XFS 301.25, 14 FWD OF THE SPAR IS CRACKED AT A RIVE T HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AN D REPAIRED IAW DC8 SRM 57-2-0 FIG 1A. 2 L 7 4 4F RT 4A25 2000020500415 20000205 00415 WP 2000 2 5 RRXA991643 1 19990816 A 5720 INTERCOSTAL DOUG DC8 DC871F 302199D WP WS 335.25 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT, L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL G USSET AFT FASTENERS IS CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 . STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500416 20000205 00416 WP 2000 2 5 RRXA991644 1 19990816 A 5720 RIB DOUG DC8 DC871F 302199D WP WS 354 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 354, CRACKED AT THE AFT UPPER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57 -2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500417 20000205 00417 WP 2000 2 5 RRXA991645 1 19990829 A 3230 RETRACT PIN DOUG DC8 DC871F 302199D WP LT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG, RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAM AGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED LT LMG RETRACT PIN BOSS BORE IAW AAR FAA 99-417 AND EWA MA AI-3210-01: 03. 2 L 7 4 4F RT 4A25 2000020500418 20000205 00418 WP 2000 2 5 RRXA991646 1 19990829 A 3230 RETRACT PIN DOUG DC8 DC871F 302199D WP RT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG, RETACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMA GED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED RT MLG CYL RETRACT PIN BOSS BORE IAW AAR FAA-99-417 AND EWA MA AI-3210- 01:03. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500419 20000205 00419 WP 2000 2 5 RRXA991647 1 19990816 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 385 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FI G 2. 2 L 7 4 4F RT 4A25 2000020500420 20000205 00420 WP 2000 2 5 RRXA991648 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 572 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN, INTERNAL DOUBLER AT STA XFS 572.5, CRACKED AT THE DRAIN HO LE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW MFG DWG NR 676900 AND DC8 SRM 51-1-20 AND SRM 51-1-21D. 2 L 7 4 4F RT 4A25 2000020500421 20000205 00421 WP 2000 2 5 RRXA991649 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 772 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 772.5, CRACKED AT THE AFT LOWER END. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500422 20000205 00422 WP 2000 2 5 RRXA991650 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 735 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 735.00, CRACKED AT THE AFT LOWER END. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500423 20000205 00423 WP 2000 2 5 RRXA991651 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN INTERNAL DOUBLER AT STA XFS 597.5, CRACKED AT THE DRAIN HOLE, CRACK RUNS AFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED DOUBLER IAW MFG DWG 6769600-3 AND DC8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2000020500424 20000205 00424 WP 2000 2 5 RRXA991652 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 616 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 616.25, CRACKED AT THE LWR FASTENER. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 S RM 57-2-0 FIB 2. 2 L 7 4 4F RT 4A25 2000020500425 20000205 00425 WP 2000 2 5 RRXA991653 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 653 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, WING, LEFT, LOWER L/E RIB, CRACKED AT FASTENER END AT STA XFS 653.75 FWD OF ACC ESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500426 20000205 00426 WP 2000 2 5 RRXA991654 1 19990817 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 580 - 600 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA 580 AND STA 600 AT LONGERON 33 LEFT, 2 CRACKS FWD OF STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D INTERCOSTAL IAW MFG DWG 5750785 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500427 20000205 00427 WP 2000 2 5 RRXA991655 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 585 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LT O/B L/E UPPER RIB CRACKED AT FASTNER END OF STA XFS 585. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500428 20000205 00428 WP 2000 2 5 RRXA991656 1 19990816 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 430 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN INTERNAL TRIPLER AT STA XFS 430 AT THE SPAR, CRACKED IN TWO. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F8 REPAIR IAW MFG DWG 5 769891 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500429 20000205 00429 WP 2000 2 5 RRXA991657 1 19990816 A 5720 ANGLE DOUG DC8 DC871F 302199D WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW MF G DWG 5613646 AND DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000020500430 20000205 00430 WP 2000 2 5 RRXA991658 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 521 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING L/E UPPER RIB AT STA XFS 521.168, CRACKED 6 FWD OF THE SPAR. THE CRA CK IS APPROX 2.5 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIB AND REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2000020500431 20000205 00431 WP 2000 2 5 RRXA991659 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 622 - 628 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LT L/E LOWER RIB CRACKED AT FASTENER END AT STA XFS 622.5 AND STA XFS 628.750 FW D OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 . STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500432 20000205 00432 WP 2000 2 5 RRXA991660 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 630 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN AT STA XFS 630, 3 FWD OF THE SPAR, CRACKED AT A RIVET H EAD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND R EPAIRED IAW DC8 SRM 57-2-0 FIG 6. 2 L 7 4 4F RT 4A25 2000020500433 20000205 00433 WP 2000 2 5 RRXA991661 1 19990820 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 423 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E UPPER SKIN AT STA XFS 423.25, CRACKED AT 2 RIVET HOLES, ALSO HAS 12 RIVET HEAT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED REPAIR IAW FAA APPROVED ENGINEERING SKETCH NR 087-125. 2 L 7 4 4F RT 4A25 2000020500434 20000205 00434 WP 2000 2 5 RRXA991662 1 19990821 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 347,354 & 372 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, WING, LT CENTER L/E UPPER RIB CRACKED AT FASTENER END AT STA XFS 347.75, 354, AN D 372.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED REPAIR IAW DC8 SRM 57-2-0 FIG. 2. 2 L 7 4 4F RT 4A25 2000020500435 20000205 00435 WP 2000 2 5 RRXA991663 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 316 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LEFT WING, CENTER L/E UPPER SKIN CRACKED AT STA XFS 316.5 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2000020500436 20000205 00436 WP 2000 2 5 RRXA991664 1 19990816 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 163 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LWR END. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IA W DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500437 20000205 00437 WP 2000 2 5 RRXA991665 1 19990817 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1260 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, AT STA 1260. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW MF G DWG 4753059 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500438 20000205 00438 WP 2000 2 5 RRXA991666 1 19990817 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, FLOORBEAM SUPPORT STRUT LOWER FITTING CRACKED AT AFT SIDE OF TEE AT STA 1160, TO P OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500439 20000205 00439 WP 2000 2 5 RRXA991667 1 19990815 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1755 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, EXTERIOR FUSELAGE SKIN CRACKED AND CORROSION AT STA 1755, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED SKIN AREA IAW DC8 SRM 53-2-1 FIG 7. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500440 20000205 00440 WP 2000 2 5 RRXA991668 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 250 - 250.89 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, LEADING EDGE SKIN BETWEEN XFS 250 AND XFS 250.89. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0 FIG 2A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500441 20000205 00441 WP 2000 2 5 RRXA991669 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 7.5 - 20 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, LEADING EDGE, EXTERNAL SKIN BETWEEN XFS 7.5 AND XFS 20. DAMAGE E XCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLE R IAW DC8 SRM 57-2-1 FIG 37. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500442 20000205 00442 WP 2000 2 5 RRXA991670 1 19991102 A 5711 FRAME DOUG DC8 DC871 302199A WP WS 454 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, NR 4 PYLON STUB WING FRAME AT STA XW 454. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND INST REPAIR IAW DC 8 SRM 51-1-20 AND DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F 4A25 2000020500443 20000205 00443 WP 2000 2 5 RRXA991671 1 19991102 A 5711 FRAME DOUG DC8 DC871 302199A WP WS 454 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E OB UPPER T-CHORD AT STA XS 454. DAMAGE EXCEEDED LIMIT S IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F 4A25 2000020500444 20000205 00444 WP 2000 2 5 RRXA991672 1 19991102 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 454 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E INNER DOUBLER AT STA XW 454. DAMAGE EXCEEDED LIMITS IAW DC-8 SR M. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RI DOUBLER IAW MFG DWG 5769769 AND DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 2000020500445 20000205 00445 WP 2000 2 5 RRXA991673 1 19991102 A 5712 RIB DOUG DC8 DC871 302199A WP WS 304 - 484 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E UPER RIBS AT FWD AT STA XS 484.895, XS 467.323, XFS 36 6.5, XFS 304, XF 322.75 AND XFS 379. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC8 SRM 57-2-0 FIG. 2. 2 L 7 4 4F 4A25 2000020500446 20000205 00446 WP 2000 2 5 RRXA991674 1 19991102 A 5712 RIB DOUG DC8 DC871 302199A WP WS 442 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E UPPER RIB AT END AT STA XS 442.185. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57 -2-0 FIG 2. 2 L 7 4 4F 4A25 2000020500447 20000205 00447 WP 2000 2 5 RRXA991675 1 19991102 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 6.225 & 20 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E INNER TRIPPLER CRACKED AT STA XOLI 6.225, 20 FWD OF LWR T/E.. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TRIPP ER IAW DC8 SRM 57-3-1, FIG 4. 2 L 7 4 4F 4A25 2000020500448 20000205 00448 WP 2000 2 5 RRXA991676 1 19991102 A 5712 RIB DOUG DC8 DC871 302199A WP WS 347 & 360 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, CENTER L/E RIBS AT STA XFS 347.75 AND XFS 360.25. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS AND INST IAW DC8 SRM 53-2-0 FIG 1B.. 2 L 7 4 4F 4A25 2000020500449 20000205 00449 WP 2000 2 5 RRXA991677 1 19991102 A 5712 RIB DOUG DC8 DC871 302199A WP WS 566 - 703 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIBS AT STA XFS 703.75, XFS 672.5, XFS 566.25, XFS 585, XFS 591. 25, XF 603.75, XFS 622.5, XFS 635. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51- 1-8. FABRICATED AND INSTALLED DOUBLERS AND INST IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F 4A25 2000020500450 20000205 00450 WP 2000 2 5 RRXA991678 1 19991102 A 5712 SKIN DOUG DC8 DC871 302199A WP WS 710 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E OB OF NR 4 PYLON AT STA XFS 710, CRACKED SKIN IN 2 PLACES. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 57-2-1 FIG 24. 2 L 7 4 4F 4A25 2000020500451 20000205 00451 WP 2000 2 5 RRXA991679 1 19991102 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 710 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 811AL 46099 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RIGHT O/B L/E O/B SECTION FROM NR 4 PYLON SKIN AT STA XFS 710. CRAC K TERMINATES AT FASTENER HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INST DOUBLER IAW DC8 SRM 57-2-1 FIG 2H. 2 L 7 4 4F 4A25 2000020500452 20000205 00452 WP 2000 2 5 RRXA991401 1 19990622 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 506 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BLISTER AND CRACK IN FINGER DOUBLER B PIT AT STA 506.000, LONGERON 30 RIGHT LOWER LEG, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED C ORROSION, CUT OUT DAMAGED FINGER DOUBLER. TREATED, PRIMED AND REPAIRED IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DE R ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 11, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500453 20000205 00453 WP 2000 2 5 RRXA991402 1 19990604 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND A-PIT DOOR CUT-OUT BOTTOM SKIN CRACK AND CHIPPED OFF, ALSO GOUGES. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IA W FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3, DATED JUNE 11, 199 9. 2 L 7 4 4F RT 4A25 2000020500454 20000205 00454 WP 2000 2 5 RRXA991403 1 19990616 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 55 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CRACK IN SKIN AT STA 55, LONGERON 34 RIGHT EXTERNAL. DAMAGE EXCEEDED LIMITS IAW DC-8 S RM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TE NNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED AUGUST 14, 1999. 2 L 7 4 4F RT 4A25 2000020500455 20000205 00455 WP 2000 2 5 RRXA991404 1 19990723 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 107 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING UPPER SKIN AT STA 107.000 STR 9. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM . REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLUG AND DOUBLER IAW DC8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2000020500456 20000205 00456 WP 2000 2 5 RRXA991405 1 19990604 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1400 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE SKIN AT STA 1400, AT DOOR LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA AP PROED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 25, 1999. 2 L 7 4 4F RT 4A25 2000020500457 20000205 00457 WP 2000 2 5 RRXA991406 1 19990604 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1445 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE SKIN BY AFT CARGO DOOR STA 1445, LONGERON 32 RIGHT. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 25, 1999. 2 L 7 4 4F RT 4A25 2000020500458 20000205 00458 WP 2000 2 5 RRXA991407 1 19990719 A 2810 SUMP HEATER DOUG DC8 DC873F 302199F WP FUEL DRAIN FAILED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND BURN, LEFT CENTER FUEL DRAIN HEATER BURNED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMO VED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED SUMP HEATER BLANKET IAW DC8 M/M 28-10-3. OPS CHECK S GOOD IAW DC8 M/M 28-10-3. 2 L 7 4 4F RT 4A25 2000020500459 20000205 00459 WP 2000 2 5 RRXA991408 1 19990602 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 285 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN LEFT WING CENTER L/E I/B EDGE 45 FWD FRONT SPAR AT STA XFS 2 85.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED REPAIR DOUBLER IAW DC8 SRM 57-2-1. INSTALLED CONICAL FILLER AND DOUBLER IAW DC8 SRM 51-1-21 AND 57-2-1. 2 L 7 4 4F RT 4A25 2000020500460 20000205 00460 WP 2000 2 5 RRXA991409 1 19990604 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND SMALL GOUGE IN SKIN FWD OF EXTERNAL POWER RECEPTACLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED GOUGE. FABRICATED AND INSTALLED ANGLE IAW FAA APPROVE D TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 11, 1999. 2 L 7 4 4F RT 4A25 2000020500461 20000205 00461 WP 2000 2 5 RRXA991410 1 19990621 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 520 CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN RIGHT WING CENTER L/E STA 520.168, 30 TO 36 INCHES FWD OF FR ONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED REPLACEMENT DOUBLER AND EXTERIOR DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR E O-99-094 WITH APPROVED 8110-3 DATED JUNE 25, 1999. 2 L 7 4 4F RT 4A25 2000020500462 20000205 00462 WP 2000 2 5 RRXA991411 1 19990610 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 304 CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND CRACK EMANATING FROM RIVET LT WING CENTER L/E STA XFS 304, 15 FWD OF FRONT SPAR ON LWR SURFACE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DAT ED JUNE 12, 1999. 2 L 7 4 4F RT 4A25 2000020500463 20000205 00463 WP 2000 2 5 RRXA991412 1 19990610 A 5730 PLATE DOUG DC8 DC873F 302199F WP WS 304 CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN LEFT WING CENTER L/E LWR SURFACE STA XFS 304, 2 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999. 2 L 7 4 4F RT 4A25 2000020500464 20000205 00464 WP 2000 2 5 RRXA991413 1 19990607 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 250 CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND LEFT WING CENTER L/E HAS SCREWS AND WASHERS WEARING INTO SKIN BY I/B SLOT DOOR AT STA 250.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED NEW DOUBLER FROM .063 301 1/4H HEAT NR 879865 AND FABRICATED AND INSTALLED EXTERIOR DOUBLER FROM .063 301 1/4H HEAT NR 879865 IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 09,1999. 2 L 7 4 4F RT 4A25 2000020500465 20000205 00465 WP 2000 2 5 RRXA991414 1 19990718 A 5320 ACCESS PANEL DOUG DC8 DC873F 302199F WP WS 191 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CRACK IN ACCESS PLATE LAND RIGHT WING, FUEL TANK PLATE 505E AT STA 191.000. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS FROM 7 075-T6 .160 LOT NR 341392, 7075-T6 .500 LOT NR 295751 AND 7075-T6 .063 IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 24, 1999 AND DC8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2000020500466 20000205 00466 WP 2000 2 5 RRXA991415 1 19990702 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP MISREPAIRED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND LEFT WING LEFT HAND NR 2 FLAP WEDGE PREVIOUS REPAIR IMPROPER BETWEEN STA XW 101 AND XW 115. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D NEW SKIN IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 24, 1999. 2 L 7 4 4F RT 4A25 2000020500467 20000205 00467 WP 2000 2 5 RRXA991416 1 19990702 A 5350 FAIRING DOUG DC8 DC873F 302199F WP BS 1688 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CABIN AT STA 1688 LT FAIRING (SHROUD) CRACKED, CARGO CONFIGURATION. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FAIRING IAW FAA APP ROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 24, 1999. 2 L 7 4 4F RT 4A25 2000020500468 20000205 00468 WP 2000 2 5 RRXA991417 1 19990702 A 5350 FAIRING DOUG DC8 DC873F 302199F WP BS 1688 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND CABIN AT STA 1688 RT FAIRING (SHROUD) CRACKED AND BROKEN, CARGO CONFIGURATION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FAIRIN G IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 24, 1999. 2 L 7 4 4F RT 4A25 2000020500469 20000205 00469 WP 2000 2 5 RRXA991418 1 19990624 A 2150 PLENUM DOUG DC8 DC873F 302199F WP AIR DIST CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND RT FWD PLENUM ASSY PRIMARY HEAT EXCHANGER HAS SEVERAL CRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOPPED DRILLED CRACKS, WELDED IAW FAA APPROVED TENNE SSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 24, 1999. 2 L 7 4 4F RT 4A25 2000020500470 20000205 00470 WP 2000 2 5 RRXA991419 1 19990622 A 5244 DOOR PANEL DOUG DC8 DC873F 302199F WP BS 1540 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND AFT LOWER CARGO COMPT STA 1540 AFT BULKHEAD DOOR BENT AND CRACKED. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOOR IAW FAA APPROV ED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JULY 01, 1999. 2 L 7 4 4F RT 4A25 2000020500471 20000205 00471 WP 2000 2 5 RRXA991420 1 19990702 A 5244 PANEL DOUG DC8 DC873F 302199F WP BS 1340 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND AFT LOWER CARGO COMPT BULKHEAD BETWEEN PIT CENTER PANEL NEEDS REPAIR CRACKED AT STA 13 40. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PARTITION IAW DAC DWG NR 99-085-1 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99- 094 WITH APPROVED 8110-3 DATED JUNE 11, 1999. 2 L 7 4 4F RT 4A25 2000020500472 20000205 00472 WP 2000 2 5 RRXA991421 1 19990810 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1875 & 1908 BUCKLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND TAIL SECTION BETWEEN STA 1875 AND STA 1908 SKIN BUCKLED. DAMAGE EXCEEDED LIMITS IAW D C-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED TAIL CONE AND REPAIRED DAMAGE SECTIONS IAW FAA AP PROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED AUGUST 10, 1999. 2 L 7 4 4F RT 4A25 2000020500473 20000205 00473 WP 2000 2 5 RRXA991422 1 19990816 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 849 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND RT W/W FWD PRESS WEB CRACKED IN RECESS OF REMOVABLE PRESS PANEL O/B OF PANEL BETWEEN S TA 849 - XCW 64. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A ND INSTALLED NEW WEB IAW IAW DC8 SRM 51-1-4 AND 51-1-20. 2 L 7 4 4F RT 4A25 2000020500474 20000205 00474 WP 2000 2 5 RRXA991423 1 19990625 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 597 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND LEFT WING O/B L/E I/B SECTION HAS CRACK AT DRIPLESS DRAIN AT STA 597.500. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REINSTALLED RIVET ACCEPTABLE TO RETURN TO SERVICE IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JU NE 12, 1999. 2 L 7 4 4F RT 4A25 2000020500475 20000205 00475 WP 2000 2 5 RRXA991424 1 19990614 A 5311 FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND MAIN CARGO DOOR UPPER JAM 2 AREAS CRACKED OUT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESS EE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 12, 1999. 2 L 7 4 4F RT 4A25 2000020500476 20000205 00476 WP 2000 2 5 RRXA991425 1 19990714 A 2752 SUPPORT DOUG DC8 DC873F 302199F WP TE FLAP ACTUATOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY AT STA 219.498 LEFT AND RIGHT POSITIONS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINKS SUPP ORT ASSYS IAW DC8 M/M 27-51-12 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WIT H APPROVED 8110-3 DATED JULY 14, 1999. 2 L 7 4 4F RT 4A25 2000020500477 20000205 00477 WP 2000 2 5 RRXA991426 1 19990721 A 2752 SUPPORT DOUG DC8 DC873F 302199F WP TE FLAP ACTUATOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY AT STA 339.723 LEFT AND RIGHT POSITIONS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPO RT ASSY IAW DC8 M/M 27-51-12 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JULY 14, 1999. 2 L 7 4 4F RT 4A25 2000020500478 20000205 00478 WP 2000 2 5 RRXA991427 1 19990718 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 191 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND CRACK IN ACCESS PLATE LAND RIGHT WING FUEL TANK PLATE 505E AT STA 191.000. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW DC8 SRM 57-2-1 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH APPROVED 8110-3 DATED JUNE 24, 1999. 2 L 7 4 4F RT 4A25 2000020500479 20000205 00479 WP 2000 2 5 RRXA991428 1 19990702 A 5754 SUPPORT DOUG DC8 DC873F 302199F WP LE FLAP BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT, FOUND LEFT WING O/B SLOT DOOR SUPPORT PREVIOUS REPAIR SUPPOT BROKEN AND CORRODED. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC 8 SRM 57-23-1, 51-1-8, 57-2-1, AND FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094 WITH AP PROVED 8110-3 DATED JULY 15, 1999. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500480 20000205 00480 WP 2000 2 5 RRXA991429 1 19990810 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 250 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT, FOUND EXTERIOR RT LIGHTNING STRIKE AT STA 250 RT BETWEEN LONGERONS 21 RIGHT AND LONGERON 22 RIGHT (EO). 2 L 7 4 4F RT 4A25 2000020500481 20000205 00481 WP 2000 2 5 RRXA991430 1 19990815 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1755 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT, FOUND CORROSION AND CRACK, FUSELAGE, AT FSY 1755, LONGERON 31 RIGHT EXTERNAL FUSELAGE. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IA W DC8 SRM 53-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500482 20000205 00482 WP 2000 2 5 RRXA991431 1 19990819 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP BS 600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FLOOR SUPPORT, AT LOCATION Y600, BETWEEN LONGERONS 33 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED FLOOR SUPPORT IAW DAC DWG 5707967 AND DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500483 20000205 00483 WP 2000 2 5 RRXA991432 1 19990824 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME AT FSY 1120, BETWEEN LONGERONS 36 AND LONGERON 34 RIGHT. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED FRAME IAW DC8 SRM 53-2- 0 FIG 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500484 20000205 00484 WP 2000 2 5 RRXA991433 1 19990817 A 5320 FINGER DOUBLER DOUG DC8 DC871F 302199D WP BS 100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER, AT STA Y100, LONGERON 31 RIGHT. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG NR 5779917 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500485 20000205 00485 WP 2000 2 5 RRXA991434 1 19990817 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 350 - 370 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SURFACE OF OUTER SKIN, BETWEEN LONGERON S 31 LEFT AND LONGERON 31 RIGHT, AND BETWEEN STATIONS Y350 AND STA Y370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED ENGINEERING SKETCH NR SK 087-990, 8110-3 APPROVED. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500486 20000205 00486 WP 2000 2 5 RRXA991435 1 19990901 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1727 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR BEAM AT STA Y1727 AT FRAME. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM SECTION IAW FAA APPROVED E NGINEERING SKETCH NR DH SK087-316, APPROVED 8110-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500487 20000205 00487 WP 2000 2 5 RRXA991436 1 19990820 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 12 - 32 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, NLG UPPER PRESSURE PANEL JUST AFT OF AIR CONDITIONING UNIT BETWEEN STA -32 AND STA -12, AND BETWEEN BL 5 RIGHT AND BL 10 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TRE ATED AREA IAW DC-8 SRM 51-1-8. REPAIRED PRESSURE PANEL IAW FAA APPROVED DER ENGINEERING SKETCH NR DH- SK087-388 APPROVE D 8110-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500488 20000205 00488 WP 2000 2 5 RRXA991437 1 19990825 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 660 - 680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 31 LEFT BETWEEN STA Y660 AND STA Y680, UPPER FLANGE.. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED LONGERON SECTION IAW FA A APPROVED DER ENGINEERING SKETCH NR DK- SK087-352 APPROVED 8110-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM ). 2 L 7 4 4F RT 4A25 2000020500489 20000205 00489 WP 2000 2 5 RRXA991438 1 19990819 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 920 - 940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, WEB, BETWEEN STA Y920 AND SAT Y940, AT LONGERON 22 RIGHT, BL 60 RIGHT. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED WEB IAW F AA APPROVED DER ENGINEERING SKETCH NR DH SK-087-089 APPROVED 8110-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRA M). 2 L 7 4 4F RT 4A25 2000020500490 20000205 00490 WP 2000 2 5 RRXA991439 1 19990820 A 5711 FRAME DOUG DC8 DC871F 302199D WP WS 7.5 - 20 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D THE CHORD IAW DC8 SRM 51-1-20, 51-21A, AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500491 20000205 00491 WP 2000 2 5 RRXA991440 1 19990824 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, RT INBD FLAP UPPER SKIN BETWEEN STA XW0 TO STA XW5, AT 5 TO 6 INCHES F WD OF THE T/E. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW DAC DWG 564960 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500492 20000205 00492 WP 2000 2 5 RRXA991441 1 19990813 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1755 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION AND CRACK AT LONGERON 31 RIGHT, STA 1755. DAMAGE EXCEEDED LIMITS IAW DC-8 SR M. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-1. (CO RROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500493 20000205 00493 WP 2000 2 5 RRXA991442 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 5162 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LEFT WING, UPPER T/E SKIN, SEVERAL FASTENER HOLES BETWEEN 1 AND 4 AFT OF REAR SP AR AT STA XR5162.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DR ILLED, FABRICATED AND INSTALLED REPAIR DOUBLER PER DC8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2000020500494 20000205 00494 WP 2000 2 5 RRXA991443 1 19990815 A 5280 SKIN DOUG DC8 DC871F 302199D WP MLG DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT MAIN LANDING GEAR DOOR ON INNER SKIN AT O/B CORNER OF AFT END, CENTER WING TO WING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FA BRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 52-6-1, FIG 1. 2 L 7 4 4F RT 4A25 2000020500495 20000205 00495 WP 2000 2 5 RRXA991444 1 19990816 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 208 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN AT STA XS 208, 31 FWD OF THE SPAR. THE CRACK IS APPROXIMAT ELY 2 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILL ED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER DC8 SRM 57-2-0, FIG 2A. 2 L 7 4 4F RT 4A25 2000020500496 20000205 00496 WP 2000 2 5 RRXA991445 1 19990816 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 301 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACKED RT WING L/E LWR SKIN AT STA XFS 301.25, 14 FWD OF THE SPAR AT A RIVET HOLE. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED A ND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0, FIG 1A. 2 L 7 4 4F RT 4A25 2000020500497 20000205 00497 WP 2000 2 5 RRXA991446 1 19990816 A 5720 INTERCOSTAL DOUG DC8 DC871F 302199D WP WS 335 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL GUSSET AFT FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500498 20000205 00498 WP 2000 2 5 RRXA991447 1 19990816 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 354 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING LE RIB AT STA XFS 354 AT THE AFT UPPER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBL ER PER DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500499 20000205 00499 WP 2000 2 5 RRXA991448 1 19990816 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 385 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500500 20000205 00500 WP 2000 2 5 RRXA991449 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 572 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN, INTERNAL DOUBLER, AT STA XFS 572.5 AT THE DRAIN HOLE. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAC DWG NR 676900, AND DC8 SRM 51-1-20 AND 51-1-21D. 2 L 7 4 4F RT 4A25 2000020500501 20000205 00501 WP 2000 2 5 RRXA991450 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 772 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 772.5 AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500502 20000205 00502 WP 2000 2 5 RRXA991451 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 735 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 735.0 AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOU BLER IAW DC8 SRM 57-20-0 FIG 2. 2 L 7 4 4F RT 4A25 2000020500503 20000205 00503 WP 2000 2 5 RRXA991452 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN, INTERNAL DOUBLER AT STA XFS 597.5 AT THE DRAIN HOLE, CRACK RUNS AFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED DOUBLER IAW DAC DWG NR 6769600-3 AND DC8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2000020500504 20000205 00504 WP 2000 2 5 RRXA991453 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 616 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 616.25 AT THE LWR FASTENER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500505 20000205 00505 WP 2000 2 5 RRXA991454 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 653 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LT WING LOWER L/E RIB AT FASTENER END AT STA XFS 653.75, FWD OF ACCESS PANEL 519 C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK , FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500506 20000205 00506 WP 2000 2 5 RRXA991455 1 19990817 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 580 - 600 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA FS 580 AND FS 600 AT LONGERON 33 LEFT, FWD OF STA FS 600 . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IN TERCOSTAL PER DAC DWG NR 5750785 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500507 20000205 00507 WP 2000 2 5 RRXA991456 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 585 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LT OBD L/E UPPER RIB AT FASTENER END AT STA XFS 585. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUB LER IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500508 20000205 00508 WP 2000 2 5 RRXA991457 1 19990816 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 430 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN INTERNAL TRIPLER AT STA XFS 430 AT THE SPAR, CRACKED IN TW O. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED R EPAIR IAW DAC DWG NR 5769891 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500509 20000205 00509 WP 2000 2 5 RRXA991458 1 19990816 A 5720 ANGLE DOUG DC8 DC871F 302199D WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DAC DWG NR 5613646 AND DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000020500510 20000205 00510 WP 2000 2 5 RRXA991459 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 521 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E UPPER RIB AT STA XFS 521.168, 6 FWD OF THE SPAR. THE CRACK APPROXIM ATELY 25 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DR ILLED RIB AND REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F RT 4A25 2000020500511 20000205 00511 WP 2000 2 5 RRXA991460 1 19990815 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 622 & 628 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LT L/E LOWER RIB AT FASTENER END, BETWEEN STA XFS 622.5 AND XFS 628.75 FWD OF AC CESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500512 20000205 00512 WP 2000 2 5 RRXA991461 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 630 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN AT STA XFS 630. 3 FORWARD OF THE SPAR, AT A RIVET HEAD. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER DC8 SRM 57-2-0 FIG 6. 2 L 7 4 4F RT 4A25 2000020500513 20000205 00513 WP 2000 2 5 RRXA991462 1 19990820 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 423 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E UPPER SKIN AT STA XFS 423.25 AT 2 RIVET HOLES, ALSO HAS 12 RIVET HEA T CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED REPAIR IAW FAA APPROVED DER ENGINEERING SKETCH NR SK-087-125. 2 L 7 4 4F RT 4A25 2000020500514 20000205 00514 WP 2000 2 5 RRXA991463 1 19990821 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 347, 354 &372 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LT CENTER L/E UPPER RIB AT FASTENER END, AT STA XFS 347.75, XFS 354, AND XFS 372 .750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D REPAIR LT, L/E RIB IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500515 20000205 00515 WP 2000 2 5 RRXA991464 1 19990815 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 316 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LEFT WING CENTER, L/E UPPER SKIN AT STA XFS 316.5 AT FRONT SPAR. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1. 2 L 7 4 4F RT 4A25 2000020500516 20000205 00516 WP 2000 2 5 RRXA991465 1 19990828 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 341 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, L/E UPPER SKIN BETWEEN STA XFS 341.50 VOID AND STA XFS 6.225. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN I AW FAA APPROVED DER ENGINEERING SKETCH NR SK-087-252, 8110-3 APPROVED. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2000020500517 20000205 00517 WP 2000 2 5 RRXA991466 1 19990816 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 163 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB, AT STA XFS 163.75, AT THE AFT LOWER END. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57- 2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500518 20000205 00518 WP 2000 2 5 RRXA991467 1 19990822 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 250 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LT WING L/E HAS BULGED SKIN AT FRONT SPAR AT STA XS 250.089. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-0, FIG 2A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500519 20000205 00519 WP 2000 2 5 RRXA991468 1 19990815 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1755 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION AND CRACK AT LONGERON 31 RIGHT, STATION 1755, EXTERIOR FUSELAGE. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 S RM 53-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500520 20000205 00520 WP 2000 2 5 RRXA991469 1 19990916 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING LINE INSPECTION FOUND 6 EACH POPPED FASTENERS ON EXTERNAL SKIN AT STA 270 AND LONGERON 21 RIGHT. INSPECTED ENTER NAL AREA AND FOUND DOUBLER WITH CORROSION DAMAGE BEYOND LIMITS. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABR ICATED AND INSTALLED INTERNAL DOUBLER IAW FAA APPROVED COTNEY DER ENGINEERING SKETCH J23-R01. (CORROSION DAMAGE RECORDE D IN EWA CORRSION PROGRAM). 2 L 7 4 4F 4A25 2000020500521 20000205 00521 WP 2000 2 5 RRXA991470 1 19990816 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 163 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E EDGE RIB AT STA XFS 163.75 AT THE AFT LOWER END. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKED, FABRICATED AND INSTALLED R EPAIR DOUBLER IAW DC8 SRM 57-2-0, FIG 2. 2 L 7 4 4F RT 4A25 2000020500522 20000205 00522 WP 2000 2 5 RRXA991471 1 19990901 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1727 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE FRAME, AT STA 1727, AT THE FLOORBEAM (LON L/R). DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53- 2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500523 20000205 00523 WP 2000 2 5 RRXA991472 1 19990829 A 3230 RETRACT PIN DOUG DC8 DC871F 302199D WP MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, MAIN LANDING GEAR, RIGHT MLG, RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED RIGHT MLG CYL RETRACT PIN BOSS BORE IAW ARR FAA APPROVED DER ENGINEERING SKETCH NR 99-417 AND EMERY WORLWIDE MA NR AI-3210-01:03. (CORROSION DAMAGE RECORDED IN EWA CO RROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500524 20000205 00524 WP 2000 2 5 RRXA991473 1 19990829 A 3230 RETRACT PIN DOUG DC8 DC871F 302199D WP MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMA GED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED LT MLG RETRACT PIN BOSS BORE IAW AAR FAA APPROVED DER ENGINEERING SKETC H NR 99-417 AND EMERY WORLDWIDE MA NR AI-3210-01:03. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500525 20000205 00525 WP 2000 2 5 RRXA991474 1 19990307 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, SKIN, FWD CARGO COMPARTMENT AT STA 440, BETWEEN LONGERONS 35 LEFT AND 33 RIG HT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW DAC DRAWING NR 18R5331084. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500526 20000205 00526 WP 2000 2 5 RRXA991475 1 19990306 A 5321 FLOOR PANEL DOUG DC8 DC862 3021970 WP BS 640 & 720 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BL 36 LEFT BETWEEN STA 640 AND STA 720. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER REPA IR IAW DC8 SRM 51-1-8 PG 17-20 AND DC8 SRM 53-2-3 FIG 10 PG 39-40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) . 2 L 7 4 4F 4A25 2000020500527 20000205 00527 WP 2000 2 5 RRXA991476 1 19990306 A 5321 FLOOR PANEL DOUG DC8 DC862F 3021972 WP BS 640 & 700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 997CF 46154 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MAIN CARGO DOOR PLANK BETWEEN STA 640 AND STA 700, AT BL 20 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BI REPAIR DOUBLER IAW DC8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500528 20000205 00528 WP 2000 2 5 RRXA991477 1 19991001 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 225 - 255 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 998CF 46139 DURING POST-FLIGHT INSPECTION FOUND THREE (3) POPPED RIVETS TO EXTERNAL SKIN BETWEEN STA 225 TO STA 255 AND LONGERON 21 RIGHT. REMOVED RIVETS FROM SKIN PANEL FROM STA 225 TO STA 255 AND LONGERON 21 RIGHT TO GAIN ACCESS TO REMOVE CORROSION. TREATED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WAS NEGLIGIBLE, NO OTHER DAMAGE FOUND. INSTALLED RIVETS IAW DC-8 SRM CHAPTER 51. DURING REPAIRS FOUND MORE CORROSION DAMAGE NOT FOUND DURING THE INTIAL INSPECTION. CORROSION DAMAGE HA D SEPARATE TO LONGERON 31 RIGHT. RECEIVED SPECIAL FLIGHT PERMIT, FORM ME007 FROM KDAY TO KBHM FOR REPAIRS. 2 L 7 4 4F 4A25 2000020500529 20000205 00529 WP 2000 2 5 RRXA991478 1 19990930 A 5753 FITTING DOUG DC8 DC873F 302199F WP AILERON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A POST-FLIGHT, FOUND RIGHT WING INBOARD AILERON HINGE FITTING CRACKED BEYOND LIMITS. REMOVED CRACKED FITTING, RE CEIVED NEW FITTING AND INSTALLED IAW DC-8 MM CHAPTER 57. OPERATIONS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2000020500530 20000205 00530 WP 2000 2 5 RRXA991479 1 19990927 A 5230 DEPRESSOR DOUG DC8 DC873 302199C WP CARGO DOOR BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 DURING A MAINTENANCE VISIT, FOUND AFT LOWER MAIN CARGO DOOR SEAL DEPRESSOR BENT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO ORIGINAL CONTOUR AND WELDED IAW COTNEY DRAWING NR J40-R01 WITH APPROVED 8110-3 DATED 09-26-99. REPAIR TO BE REPLACED WITH PERMANENT REPAIR WITHIN 30 CYCLES. 2 L 7 4 4F RT 4A25 2000020500531 20000205 00531 WP 2000 2 5 RRXA991480 1 19990703 A 5311 FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND MAIN CARGO DOOR UPPER JAM SKIN SECTION DAMAGED BETWEEN STA 151 AND STA 177 LT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 0 8-05-99. 2 L 7 4 4F RT 4A25 2000020500532 20000205 00532 WP 2000 2 5 RRXA991481 1 19990722 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, I/B AREA BETWEEN LONGERONS 10 RIGHT AND LONGE RON 11 RIGHT, A 2.75 CRACK BETWEEN BL 24.750T LEFT AND BL 27.250 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DA MAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED CRACK IAW DC8 SRM 53-2-5 AND IAW FAA APPROVED TENNESSEE TECHNICAL SER VICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500533 20000205 00533 WP 2000 2 5 RRXA991482 1 19990617 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 RIGHT AND LONGERON 11 RIG HT, APPROX 3.75 INCH CRACK BETWEEN BL 33.50 LEFT AND BL 37.00 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAG ED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED CRACK IAW DC8 SRM 53-2-5 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVIC ES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500534 20000205 00534 WP 2000 2 5 RRXA991483 1 19990722 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEFT , APPROX 2-1/2, BETWEEN BL 25.0 RIGHT AND BL 27.250 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREAT ED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER, TRIPLER IAW DC8 SRM 53-2-5 AND 51-1-21. 2 L 7 4 4F RT 4A25 2000020500535 20000205 00535 WP 2000 2 5 RRXA991484 1 19990617 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEF T, APPROX 3-1/2 CRACK BETWEEN BL 35.0 RIGHT AND BL 35.750 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER, TRIPLER IAW DC8 SRM 53-2-5 AND 51-1-21. 2 L 7 4 4F RT 4A25 2000020500536 20000205 00536 WP 2000 2 5 RRXA991485 1 19990630 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 591 CRACK A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CRACKS, SKIN, LEFT WING O/B LEADING EDGE I/B SECTIONS LOWER SURFACE AT STA XFS 591.250, 1 TO 4 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FA BRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH #EO-99-109 WITH APPR OVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500537 20000205 00537 WP 2000 2 5 RRXA991486 1 19990628 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 478 - 484 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, FOUND TWO SMALL GOUGES, LEFT WING CENTER LEADING EDGE LOWER SURFACE AT STA XS 478.897 AND ST A XS 484.895 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500538 20000205 00538 WP 2000 2 5 RRXA991487 1 19990630 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND LEFT WING OUTBOARD SLOT LEADING EDGE I/B EDGE HAS SCREWS PULLING THROUGH SKIN AND MISSI NG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500539 20000205 00539 WP 2000 2 5 RRXA991488 1 19990905 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 491 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, FOUND FASTENERS LOOSE RIGHT WING O/B SLOT L/E O/B END AT STA XS 491.193. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAA AP PROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109-2 WITH APPROVED 8110-3 DATED 08-04-99. 2 L 7 4 4F RT 4A25 2000020500540 20000205 00540 WP 2000 2 5 RRXA991489 1 19990811 A 2120 DUCT DOUG DC8 DC873F 302199F WP BS 70 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND UPPER CARGO COMPT AIR DUCT AT STA 70, LT SIDE DUCT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED AND WELDED IAW FAA APPROVED TENNESSEE TECHN ICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500541 20000205 00541 WP 2000 2 5 RRXA991490 1 19990721 A 7160 SKIN DOUG DC8 DC873F 302199F WP NR1 NACELLE DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND DENT, NR 1 ENGINE RING COWL AT 5 O'CLOCK POSITION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM . REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. CUT ACCESS HOLE, STRAIGHTENED DENT WITHIN LIMITS DC8 SRM 71-5-2. FABRICATED AND INSTALLED PLATE IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH A PPROVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500542 20000205 00542 WP 2000 2 5 RRXA991491 1 19990825 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 515 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, FOUND NR 4 STUB WING MOUNTING HOLE BROKEN OUT AT DOUBLER AT STA XS 515.720, 26 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D NEW DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DAT ED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500543 20000205 00543 WP 2000 2 5 RRXA991492 1 19990818 A 5230 DOOR TRACK DOUG DC8 DC873F 302199F WP BS 360 BENT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND A PIT RT TRACK WORN AND BENT AT STA 360. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED TRACK IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERIN G SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. 2 L 7 4 4F RT 4A25 2000020500544 20000205 00544 WP 2000 2 5 RRXA991493 1 19990817 A 5414 PANEL DOUG DC8 DC873F 302199F WP NR 3 PYLON MISSING A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND ROBBED PYLON PANEL ASSY FOR A/C N8085U NR 3 PYLON (EO). DAMAGE EXCEEDED LIMITS IAW DC- 8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW FAA APPROVED TENNESSE E TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-02-99. 2 L 7 4 4F RT 4A25 2000020500545 20000205 00545 WP 2000 2 5 RRXA991494 1 19990818 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 849 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND RT W/W FWD PRESS WEB CRACKED IN RECESS OF REMOVEABLE PANEL O/B OF PANEL AT STA 849 XCW 64. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PRESSURE WEB IAW DC8 SRM 51-1-4, AND 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500546 20000205 00546 WP 2000 2 5 RRXA991495 1 19990903 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 69.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND 4 CRACK EXTENDING FROM RIVET RT WING UPPER SURFACE AT STA 69.5 AT REAR SPAR. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 57-2-1 AND FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-26-99. 2 L 7 4 4F RT 4A25 2000020500547 20000205 00547 WP 2000 2 5 RRXA991496 1 19990828 A 2120 DUCT DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND DUCT THAT GOES UNDER CONSTANT SECTION HAS HOLE (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 S RM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLIT SLEEVE AND WELDED OVER CUT OUT. NDT WELD. NO DEFECTS FOUND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 DATED 08- 24-99. 2 L 7 4 4F RT 4A25 2000020500548 20000205 00548 WP 2000 2 5 RRXA991498 1 19990819 A 2752 SUPPORT DOUG DC8 DC873F 302199F WP TE FLAP ACTUATOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 A ND FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 07-15-99. 2 L 7 4 4F RT 4A25 2000020500549 20000205 00549 WP 2000 2 5 RRXA991499 1 19990812 A 2752 SUPPORT DOUG DC8 DC873F 302199F WP TE FLAP ACTUATOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY LT O/B AT STA 340. DAMAGE EXCEEDED LIMITS IAW D C-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-1 2 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 07-15- 99. 2 L 7 4 4F RT 4A25 2000020500550 20000205 00550 WP 2000 2 5 RRXA991500 1 19990831 A 2752 SUPPORT DOUG DC8 DC873F 302199F WP TE FLAP ACTUATOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT REMOVE AND REPLACE FLAP LINK SUPPORT ASSY RT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SR M. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 07-15-99. 2 L 7 4 4F RT 4A25 2000020500551 20000205 00551 WP 2000 2 5 RRXA991501 1 19990831 A 2752 SUPPORT DOUG DC8 DC873F 302199F WP TE FLAP ACTUATOR DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY RT O/B STA 340. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 57-51-12 AN D IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 07-15-99. 2 L 7 4 4F RT 4A25 2000020500552 20000205 00552 WP 2000 2 5 RRXA991502 1 19990902 A 5347 INSERT DOUG DC8 DC873F 302199F WP CARGO BEAM STRIPPED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, FOUND NUMEROUS TRAY TIE DOWN INSERTS STRIPPED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE D DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED DYNA SYSTEM THREAD INSERTS P/N: 021-1-8200 IN PLACE OF P/N: 3755 486-1 IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 09-02 -99. 2 L 7 4 4F RT 4A25 2000020500553 20000205 00553 WP 2000 2 5 RRXA991503 1 19990629 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 12 - 52 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, SEVERAL RIVET HEADS POPPED ON DOUBLER BETWEEN STA -52 TO STA -12, 20 RIGHT C ENTER COCKPIT PRESSURE DECK AFT OF F/E TABLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW D C-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING S KETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500554 20000205 00554 WP 2000 2 5 RRXA991504 1 19990825 A 3230 RETRACT PIN DOUG DC8 DC873F 302199F WP MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, MAIN LANDING GEAR STRUT, LT AND RT MLG RETRACT PIN ASSY (EO). DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. COMPLIED WITH MA-A1-3210 AND S/B 32-102 REP LACED PINS AND REWORKED BOSS AREA IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 07-07-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500555 20000205 00555 WP 2000 2 5 RRXA991505 1 19990717 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 718 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT STA 718, LONGERON 35 RIGHT ON EXTERNAL SKIN UNDER FWD FILLET PA NEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08 -05-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500556 20000205 00556 WP 2000 2 5 RRXA991506 1 19990626 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, RT WING, OUTBOARD LEADING EDGE O/B SECTION LWR. SURFACE I/B END, CORROSION C RACK AT STA XFS 710.000 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99 -109 WITH APPROVED 8110-3 DATED 08-05-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500557 20000205 00557 WP 2000 2 5 RRXA991507 1 19990905 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 20 & 38 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, SCREWS PULLING THROUGH SKIN LEFT WING INBOARD LEADING EDGE UPPER BETWE EN STA XFS 20 AND STA XFS 38.750 AT FRONT SPAR. CORROSION FOUND IN SCREW HOLES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESS EE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. (CORROSION DAMAGE RECORD ED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500558 20000205 00558 WP 2000 2 5 RRXA991508 1 19990820 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRE S SKIN REPLACEMENT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FILLED GA P WITH HYSOLEA934NA. FABRICATED AND INSTALLED SKIN DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERIN G SKETCH NR EO-99-109-1 WITH APPROVED 8110-3 DATED 08-03-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500559 20000205 00559 WP 2000 2 5 RRXA991509 1 19990717 A 5510 WEB DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION BLISTER AT STA 1766, LONGERON 10 RIGHT, 24 LEFT OF RBL ON STAB FRONT SPAR ANG LED WEB DIRECTLY BEHIND AFT BULKHEAD INSIDE ACCESS HOLE 60. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREA TED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINE ERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 08-05-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500560 20000205 00560 WP 2000 2 5 RRXA991510 1 19990820 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, UPPER CARGO COMPARTMENT FLOOR PANEL CORRODED (EXFOLIATION) REQUIRE S REPAIR DOUBLERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED F LOOR PANELS IAW DC8 SRM 51-1-8 AND 53-2-3 AND IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO -99-109-2 WITH APPROVED 8110-3 DATED 08-03-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500561 20000205 00561 WP 2000 2 5 RRXA991511 1 19990905 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 440 & 460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, FINGER DOUBLER AT LONGERON 31 LEFT BETWEEN STA 440 AND STA 460 LT. DAMAGE E XCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FA A APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-109 WITH APPROVED 8110-3 DATED 07-12-99. (CORRO SION DAMAGE RECORDED IN EWA CORROSION PROGRAM).. 2 L 7 4 4F RT 4A25 2000020500562 20000205 00562 WP 2000 2 5 RRXA991513 1 19990828 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 940 - 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT FINGER DOUBLERS ABOVE M/W/W BETWEEN STA 940 AND STA 980, 8 CEN TER OF FLOOR PRESS PANEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FAB RICATED AND INSTALLED FILLERS AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99 -109 WITH APPROVED 8110-3 DATED 08-25-99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500563 20000205 00563 WP 2000 2 5 RRXA991515 1 19991001 A 3231 LOCK DOUG DC8 DC871F 302199D WP NLG DOOR OUT OF ADJUST A RRXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 801GP 46039 AFTER GEAR RETRACTION, LOUD NOISE IN NOSE GEAR AREA, CYCLED GEAR NO HELP. ADJ NLG DOOR LOCKS, LUBED, INSPECTED SWUNG GE AR 3 TIMES. OPS CHECK GOOD AT THIS TIME. 2 L 7 4 4F RT 4A25 2000020500564 20000205 00564 WP 2000 2 5 RRXA991516 1 19990822 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 250 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E HAS BULGED SKIN AT FRONT SPAR AT STA XS 250.089. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SR M 57-2-0, FIG 2A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500565 20000205 00565 WP 2000 2 5 RRXA991517 1 19990817 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1260 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC D WG NR 470359 AND DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500566 20000205 00566 WP 2000 2 5 RRXA991518 1 19990831 A 5720 FITTING DOUG DC8 DC871F 302199D WP WS 410 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND SPOTS OF CORROSION ON RT O/B FLAP AT STA X-410, FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED REPAIR IAW FAA APPROVED. AIRCRAFT MAINTENANCE DER ENGINEERING SKETCH NR SK-087-305 .. (CORROSION DAMAGE RECORD ED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500567 20000205 00567 WP 2000 2 5 RRXA991519 1 19990817 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CRACK, FLOOR BEAM SUPPORT STRUT LOWER FITTING, CRACKED AT AFT SIDE OF TEE, AT STA 1160, TOP OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FA BRICATED AND INSTALLED FITTING IAW DC8 SEM 51-1-20D. 2 L 7 4 4F RT 4A25 2000020500568 20000205 00568 WP 2000 2 5 RRXA991520 1 19990825 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 6.225 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, LT O/B SLOT VANE INNER DOUBLER HAS HEAVY CORROSION AT STA XOLDI 6.225. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER I AW DAC DWG NR 5769933 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500569 20000205 00569 WP 2000 2 5 RRXA991521 1 19990921 A 5512 PANEL DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 DURING A MAINTENANCE VISIT FOUND CORROSION, HORIZONTAL STAB, CENTER SECTION, UPPER CENTER PLANK, UPPER SURFACE AT BL -30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED PLANK IAW DC8 SB 55-15. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500570 20000205 00570 WP 2000 2 5 RRXA991523 1 19991106 A 3230 56165545503 BOGIE TRIM CYL DOUG DC8 DC873F 302199F WP MLG FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 831AL 46146 AFTER TAKEOFF, ON GEAR RETRACTION, GEAR NOT LATCHED LIGHT AND DOOR NOT LATCHED LIGHT CAME ON WITH GEAR RETRACTED. FOUND RIGHT BOGIE TRIM CYLINDER AFT BOLT BROKEN CAUSING GEAR NOT TO BE ALL THE WAY IN THE WELL. REMOVED AND REPLACED BOGIE T RIM CYLINDER OPS AND LEAK CK GOOD. JACKED ACFT AND CYCLED GEAR THROUGH SEVERAL CYCLES. ALL OPS CK GOOD, NO OTHER DEFEC T NOTED. 2 L 7 4 4F RT 4A25 2000020500571 20000205 00571 WP 2000 2 5 RRXA991524 1 19991108 A 2910 AE211600060301 LINE DOUG DC8 DC873F 302199F WP HYD SYSTEM LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 870TV 46086 AFTER GEAR UP ON TAKEOFF OUT OF MMMX, HYD QTY DROPPED TO STAND-PIPE. REMOVED AND REPLACED RT BOGIE TRIM CYLINDER HYD LI NE, OPS CHECK GOOD ON ENGINE RUN. SERVICED HYD RES QTY TO FULL AFTER ENG RUN. 2 L 7 4 4F RT 4A25 2000020500572 20000205 00572 WP 2000 2 5 RRXA991525 1 19991108 A 7722 3716072501 RECTIFIER DOUG DC8 DC873F 302199F WP EGT INDICATOR FAILED A RRXA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 15 791FT 46045 LOST POWER TO EGT INDICATORS ANS SAI WHILE IN FLIGHT AT FL330. FOUND DC BUS BLOCKER RECTIFIER R7-5 WDM 24-4-1 P44 BAD. REMOVED AND REPLACED SAME, OPS CKS NORMAL AT THIS TIME. 2 L 7 4 4F RT 4A25 2000020500573 20000205 00573 WP 2000 2 5 RRXA991526 1 19990526 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 421 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, UPPER SKIN SURFACE AT STA XRS=421 AND STRINGER 9. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DAC FAX NR EAF-MIA-99-0037RR. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500574 20000205 00574 WP 2000 2 5 RRXA991527 1 19990526 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 22 & 107 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING UPPER SKIN BETWEEN FRONT SPAR AND CENTER SPAR, BETWEEN STA XW=22. 750 AND STA XW=107. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D AND INSTALLED REPAIR DOUBLER DAC FAX NR EAF-MIA-99-0037RR. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500575 20000205 00575 WP 2000 2 5 RRXA991528 1 19990722 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 69.5 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING SKIN AT STA XCW=69.5 AND STRINGER 9 RIGHT. DAMAGE EXCEEDED LIMIT S IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DAC DW G EAF-MIA-99-0032RR. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500576 20000205 00576 WP 2000 2 5 RRXA991529 1 19990607 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 460 - 600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION TO LONGERON 32 RIGHT, BETWEEN STA 460 TO STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED LONGERON 32 RIGHT BY CLAD PLATING AND INSTALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500577 20000205 00577 WP 2000 2 5 RRXA991530 1 19990619 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 480 & 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INNER SKIN BETWEEN STA 480 AND STA 580, AND BETWEEN LONGERONS 34 LE FT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FAB RICATED AND INSTALLED NEW SKIN SECTION IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500578 20000205 00578 WP 2000 2 5 RRXA991531 1 19990607 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 500, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755 827. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500579 20000205 00579 WP 2000 2 5 RRXA991532 1 19990607 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 540, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500580 20000205 00580 WP 2000 2 5 RRXA991534 1 19990607 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 34 RIGHT AT STA 580. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM . REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC8 SRM 53-1-20 FIGURE 1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500581 20000205 00581 WP 2000 2 5 RRXA991535 1 19990531 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 600 & 620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 30 RIGHT, SPLICE DOUBLER BETWEEN STA 600 AND STA 620. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLICE DOUBLER IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500582 20000205 00582 WP 2000 2 5 RRXA991536 1 19990606 A 5320 ANGLE DOUG DC8 DC862 3021970 WP BS 500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO ATTACHMENT ANGLE AT STA 500, LONGERON 33 RIGHT. DAMAGE EXCEEDE D LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT ANGL E IAW DC8 SRM 5-1-20D.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500583 20000205 00583 WP 2000 2 5 RRXA991537 1 19990607 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500584 20000205 00584 WP 2000 2 5 RRXA991538 1 19990607 A 5320 ANGLE DOUG DC8 DC862 3021970 WP BS 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME ATTACHMENT ANGLE AT STA 580, BETWEEN LONGERONS 33 LEFT AN D LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D AND INSTALLED NEW FRAME ATTACHMENT ANGLE IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500585 20000205 00585 WP 2000 2 5 RRXA991539 1 19990527 A 5320 FINGER DOUBLER DOUG DC8 DC862 3021970 WP BS 310 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FINGER DOUBLER AT STA 310 AND LONGERON 21 RIGHT. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500586 20000205 00586 WP 2000 2 5 RRXA991540 1 19990526 A 5320 BRACKET DOUG DC8 DC862 3021970 WP BS 1165 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO BRACKET AT STA 1165, BETWEEN LONGERONS 29 RIGHT AND LONGERON 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED NEW BRACKET IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500587 20000205 00587 WP 2000 2 5 RRXA991541 1 19990723 A 5320 STRAP DOUG DC8 DC862 3021970 WP BS 1180 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO CIRCUMFERENCIAL STRAP AT STA 1180, LONGERON 34 RIGHT. DAMAGE E XCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CIRCUMFER ENCIAL STRAP IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500588 20000205 00588 WP 2000 2 5 RRXA991542 1 19990612 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 35 RI GHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC8 SRM 53-2-0 FIGURE 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500589 20000205 00589 WP 2000 2 5 RRXA991543 1 19990607 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 1220 & 1240 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE BETWEEN STA 1220 AND STA 1240, AND BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FAB RICATED AND INSTALLED NEW SHEAR TIE IAW DC8 SRM 53-2-0 FIGURE 2B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500590 20000205 00590 WP 2000 2 5 RRXA991544 1 19990607 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 1235 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1235, BETWEEN LONGERONS 33 RIGHT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED ENW SHEAR TIE IAW DC8 SRM 53-2-0 FIGURE 2B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500591 20000205 00591 WP 2000 2 5 RRXA991545 1 19990702 A 5320 INTERCOSTAL DOUG DC8 DC862 3021970 WP BS 1240 & 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO INTERCOSTAL BETWEEN STA 1240 AND STA 1280, AT WL 4 RIGHT, AND L ONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A ND INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500592 20000205 00592 WP 2000 2 5 RRXA991546 1 19990702 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 36 AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 364835 9. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500593 20000205 00593 WP 2000 2 5 RRXA991547 1 19990607 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 35 RIGHT AT STA 1280. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3646937. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500594 20000205 00594 WP 2000 2 5 RRXA991548 1 19990527 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME AT STA 1420, BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RE PAIR DOUBLER IAW DC8 SRM 53-2-0 FIGURE 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500595 20000205 00595 WP 2000 2 5 RRXA991549 1 19990530 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1180 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME STRAP AT STA 1180, BETWEEN LONGERONS 33 RIGHT AND LONGERO N 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IN STALLED REPAIR ANGLE IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).. 2 L 7 4 4F 4A25 2000020500596 20000205 00596 WP 2000 2 5 RRXA991550 1 19990607 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 3 6. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED N EW SHEAR TIE IAW DC8 SRM 53-2-0 FIGURE 2B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500597 20000205 00597 WP 2000 2 5 RRXA991551 1 19990607 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8 SRM 53-2-0 FIGURE 2B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).. 2 L 7 4 4F 4A25 2000020500598 20000205 00598 WP 2000 2 5 RRXA991552 1 19990607 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 LEFT AND LONGERON 3 6. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED N EW SHEAR TIE IAW DC8 SRM 53-2-0, FIGURE 2B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500599 20000205 00599 WP 2000 2 5 RRXA991553 1 19990607 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 33 LEFT AND 34 LEFT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLE D IAW DC8 SRM 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500600 20000205 00600 WP 2000 2 5 RRXA991554 1 19990607 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8 SRM 53-2-0 FIGURE 2B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500601 20000205 00601 WP 2000 2 5 RRXA991555 1 19990607 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 1240 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1240 AND LONGERON 35 RIGHT. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8 SRM 53-2-0, FIGURE 2B.. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500602 20000205 00602 WP 2000 2 5 RRXA991556 1 19990526 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1240 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1240, BETWEEN LONGERONS 34 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR DOUBLER IAW DC8 SRM 51-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500603 20000205 00603 WP 2000 2 5 RRXA991557 1 19990607 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1240 & 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 LEFT, BETWEEN STA 1240 AND STA 1260. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTI ON IAW DAC DRAWING 3645897. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500604 20000205 00604 WP 2000 2 5 RRXA991558 1 19990607 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1250 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1250 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME IAW DC8 SRM 53-4-1, FI GURE 52. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500605 20000205 00605 WP 2000 2 5 RRXA991559 1 19990607 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 RIGHT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC- 8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWIN G 5754184. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500606 20000205 00606 WP 2000 2 5 RRXA991560 1 19990531 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 461 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO NUMBER 2 LOWER CARGO DOOR JAMB FRAME WEB AT STA 461, BETWEEN LO NGERONS 33 RIGHT AND 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW WEB IAW DAC NR 18R5321111. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500607 20000205 00607 WP 2000 2 5 RRXA991561 1 19990708 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 490 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT DOOR JAMB TORQUE BOX FITTING AT STA 490, BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. R ECEIVED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500608 20000205 00608 WP 2000 2 5 RRXA991562 1 19990707 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB TORQUE BOW FITTING AT STA 500, BETWEEN LONGERONS 32 R IGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED AND INSTALLED NEW FITTING IAW DAC DRAWING 3755825. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500609 20000205 00609 WP 2000 2 5 RRXA991563 1 19990709 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1240 - 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB PAN SKIN BETWEEN STA 1240 AND STA 1280, AND BETWEEN L ONGERONS 31 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 S RM 51-1-8. FABRICATED AND INSTALLED NEW SKIN SECTION IAW DC8 SRM 53-2-0, FIGURE 23. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500610 20000205 00610 WP 2000 2 5 RRXA991564 1 19990601 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 260 AND BL 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 53-1-0. (CORROSION DA MAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500611 20000205 00611 WP 2000 2 5 RRXA991565 1 19990524 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 270 - 340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 270 AND STA 340, AT BL 56 LEFT , DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500612 20000205 00612 WP 2000 2 5 RRXA991566 1 19990517 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 310 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK AT STA 310 AND BL 24 RIGHT. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500613 20000205 00613 WP 2000 2 5 RRXA991567 1 19990525 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 400 - 500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 400 AND STA 500 AT BL 22 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500614 20000205 00614 WP 2000 2 5 RRXA991568 1 19990517 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 480 - 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 480 AND STA 540 AT BL 24 RIGHT . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NE W SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500615 20000205 00615 WP 2000 2 5 RRXA991569 1 19990525 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 500 - 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 500 AND STA 560 AT BL 22 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500616 20000205 00616 WP 2000 2 5 RRXA991570 1 19990525 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 560 - 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 560 AND STA 660 AT BL 56 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500617 20000205 00617 WP 2000 2 5 RRXA991571 1 19990525 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 580 - 620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 580 AND STA 620 AT BL 0. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500618 20000205 00618 WP 2000 2 5 RRXA991572 1 19990524 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 640 - 690 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 690 AND STA 640 AT BL 56 RIGHT . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NE W SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500619 20000205 00619 WP 2000 2 5 RRXA991573 1 19990523 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 1015 - 1090 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 1015 AND STA 1090 AT BL 0.. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW S EAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500620 20000205 00620 WP 2000 2 5 RRXA991574 1 19990523 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 1020 - 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 1020 AND STA 1040 AT BL 58 LEF T. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED N EW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500621 20000205 00621 WP 2000 2 5 RRXA991575 1 19990524 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 1060 - 1080 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 1060 AND STA 1080 AT BL 56 LEF T. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED N EW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500622 20000205 00622 WP 2000 2 5 RRXA991576 1 19990524 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 1320 - 1340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 1320 AND STA 1340 AT BL 0.. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW S EAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500623 20000205 00623 WP 2000 2 5 RRXA991577 1 19990523 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 1360 - 1380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 1360 AND STA 1380 AT BL 22 LEF T. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED N EW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500624 20000205 00624 WP 2000 2 5 RRXA991578 1 19990524 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 1420 - 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 1420 AND STA 1440 AT BL 0.. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW S EAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500625 20000205 00625 WP 2000 2 5 RRXA991579 1 19990525 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 270 - 340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 270 AND STA 340 AT BL 0. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500626 20000205 00626 WP 2000 2 5 RRXA991581 1 19990525 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 500 - 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 500 AND STA 560 AT BL 56 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500627 20000205 00627 WP 2000 2 5 RRXA991582 1 19990525 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP BS 560 - 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO MAIN DECK SEAT TRACK BETWEEN STA 560 AND STA 660 AT BL 45 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500628 20000205 00628 WP 2000 2 5 RRXA991583 1 19990525 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 64 RIGHT, AND WL 3 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500629 20000205 00629 WP 2000 2 5 RRXA991584 1 19990525 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 24 RIGHT AT STA 920, BL 24 RIGHT. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SR M 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500630 20000205 00630 WP 2000 2 5 RRXA991585 1 19991119 A 2130 CONTROLLER DOUG DC8 DC862 3021970 WP CABIN PRESSURE MALFUNCTIONED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 993CF 46028 AT FL 260, AIRCRAFT EXPERIENCED A RAPID CLIMB IN CABIN PRESSURE CREW DESCENDED TO FL 120 AND LANDED IN (MKE). PRESSURIZ ED A/C TO 1.5 DPSI NO MAJOR LEAKS NOTED. INSPECTED ALL DOOR SEALS, AIRCRAFT EXTERIOR AND OUT FLOW VALVE. NO DEFECTS NO TE. A/C IS SAFE FOR PRESSURIZED FLIGHT. 2 L 7 4 4F 4A25 2000020500631 20000205 00631 WP 2000 2 5 RRXA991586 1 19991124 A 2130 1031549092 VALVE DOUG DC8 DC862 3021970 WP CABIN PRESSURE INOPERATIVE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 993CF 46028 DURING FLIGHT AT FL 26.0 MADE AN EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURIZATION. REPLACED LEFT AND RIGHT PRESSUR IZATION VALVES. PERFORMED PRESSURIZATION CHECK PER MM 21-31-00 WITH ENGINES 2 AND 3 RUNNING. PRESSURIZED TO 8.0 PSID, NO LEAK OR DEFECTS NOTED. 2 L 7 4 4F 4A25 2000020500632 20000205 00632 WP 2000 2 5 RRXA991591 1 19991207 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1440 - 1453 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 873SJ 46091 AIRCRAFT HAS 18-24 GASH IN OUTER SKIN APPROX 4 FT AFT OF D PIT DOOR. REPLACED LONGERON 28R AT FUSELAGE SATION (FS) 1440 -1453 AND FS 1470-1510 AND SKIN REPAIR AT FS 1470-1510 I/A/W SRM 53-2-1 FIG 7. NO OTHER DEFECTS NOTED I/A/W SRM 51 AND 53. 2 L 7 4 4F RT 4A25 2000020500633 20000205 00633 NE 2000 2 5 RRXA991593 2 19991220 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 4 FAILED A RRXA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 15 831AL 46146 NR 4 ENG FLAMED OUT AT FL 39.0 TIME 19:14-Z , OIL PRESS AND TEMP NORMAL, FUEL PRESS 38 PSI PRIOR TO FLAME OUT TANK BOOST PUMP ON. UNABLE RELIGHT AS PER QRH. AFTER INFLT SHUT DOWN CHECK, WINDMILL PARAMETERS WERE OIL PRESS 7 PSI FUEL PRESS 5 PSI, NO RELIGHT ON 2ND TRY AT 19000. SUMPED NR 4 FUEL TANK. REMOVED AND REPLACED NR 4 ENG MAIN FUEL FILTER, PERFORME D PWR ASSURANCE RUN IAW DC-8 RUN UP HANDBOOK. ALL PARAMETERS NORMAL, FILTER LK CK OK IAW 73-22-0. 2 L 7 4 4F 4 F RT 4A25 E2GL 2000020500634 20000205 00634 WP 2000 2 5 RRXA991594 1 19990514 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 49.5 - 64 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL SKIN SECTION, BETWEEN STA 49.5 AND STA 64, AND BETWEEN LO NGERONS 33 RIGHT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SR M 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO-99-094. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500635 20000205 00635 WP 2000 2 5 RRXA991595 1 19990606 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 50 - 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BETWEEN STA 50 AND STA 70, AND AT LONGERON 21 RIGHT. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IA W DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500636 20000205 00636 WP 2000 2 5 RRXA991596 1 19990511 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 25 - 55 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO EXTERNAL SKIN SECTION BETWEEN STA 25 AND STA 55 BETWEEN LONGERO NS 23 RIGHT AND LONGERON 25 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51- 1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR EO -99- 094. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500637 20000205 00637 WP 2000 2 5 RRXA991597 1 19990523 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 960 - 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ON FINGER DOUBLER ANGLE BETWEEN STA 960 AND STA 980 -43 LBL, AT WL 10 RIGHT, BELOW NR 2 SEAT TRACK, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1- 8. REMOVED AND REPLACED FINGER DOUBLER ANGLE IAW DC8 SRM 51-1-20D AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORRO SION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500638 20000205 00638 WP 2000 2 5 RRXA991598 1 19990601 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP BS 857 - 878 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TOP OF WHEEL WELL (MAIN CABIN) AND POPPED RIVET HEADS BETWEEN STA 857 AND STA 878, BETWEEN LEFT BL 64 AND LEFT BL 68 AT WL 9 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE D, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DC8 SRM 53-2-0. (CORROSION DAMAGE REC ORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500639 20000205 00639 WP 2000 2 5 RRXA991599 1 19990516 A 5320 PANEL DOUG DC8 DC873F 302199F WP BS 960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LWR FUSELAGE KEEL PANEL NR 161CC, HAD CORROSION BLISTERS, BARE MET AL LIGHT CORROSION, AT STA 960 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROS ION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500640 20000205 00640 WP 2000 2 5 RRXA991600 1 19990521 A 5320 TIE DOUG DC8 DC873F 302199F WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBOARD TIE ENDS, 5 EACH, AT STA 980, BETWEEN LONGERONS 21 LEFT AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRI CATED AND INSTALLED FLOORBOARD TIE END IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500641 20000205 00641 WP 2000 2 5 RRXA991601 1 19990603 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1688 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN, AT STA 1688, FLOOR PANEL A CORRODED AND CRACKED AT LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED NEW FLOORBOARD IAW DC8 SRM 53-2-0 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500642 20000205 00642 WP 2000 2 5 RRXA991602 1 19990524 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1766 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT PRESSURE BULKHEAD AT STA 1766, LONGERON 21 LEFT, HORIZONTAL ST IFFENER FLOOR SUPPORT TEES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED AND INSTALLED SUPPORT TEE'S IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500643 20000205 00643 WP 2000 2 5 RRXA991603 1 19990523 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1766 - 1745 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT CABIN RIGHT FLOOR PANEL SUPPORT BETWEEN STA 1766 AND STA 1745 RIGHT AT NUT PLATES BOTTOM SIDE BL 20 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC -8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500644 20000205 00644 WP 2000 2 5 RRXA991604 1 19990515 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1240 - 1320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT BETWEEN STA 1240 AND STA 1320, AT LONGERON 36 FLOOR TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED NEW SECTION IAW DC8 SRM 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500645 20000205 00645 WP 2000 2 5 RRXA991605 1 19990515 A 5320 DOOR FRAME DOUG DC8 DC873F 302199F WP BS 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT AFT DOOR FRAME FOR THRESHHOLD AND CRACKED AT S TA 1440 AND LONGERON 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 . FABRICATED AND INSTALLED NEW DOOR FRAME IAW DC8 SRM 51-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500646 20000205 00646 WP 2000 2 5 RRXA991606 1 19990514 A 5320 BRACKET DOUG DC8 DC873F 302199F WP BS 1395 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT AT STA 1395 AND LONGERON 33 RIGHT INSIDE LIGHT HOLE PIECE OF METAL MISSING AND LIGHT CORROSION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA I AW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW BRACKET IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSI ON PROGRAM). 2 L 7 4 4F RT 4A25 2000020500647 20000205 00647 WP 2000 2 5 RRXA991607 1 19990514 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT BETWEEN STA 1500 AND STA 1504 AT LONGERON 26 R IGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SECTION O F LONGERON AND SPLICED IAW DC8 SRM 53-2-2 AND 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500648 20000205 00648 WP 2000 2 5 RRXA991608 1 19990518 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT AT STA 1540 AND LONGERON 33 RIGHT, CRACKED AND CORRODED 2 FTY AFT OF BULKHEAD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1- 8. FABRICATED AND INSTALLED NEW SECTION IAW DC8 SRM 51-1-21 AND 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F RT 4A25 2000020500649 20000205 00649 WP 2000 2 5 RRXA991609 1 19990521 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 585 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, WING, RIGHT, O/B L/E SECTION UPPER SURFACE (SKIN) AT XFS 585.000 AT FRONT SP AR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 57-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500650 20000205 00650 WP 2000 2 5 RRXA991610 1 19990520 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT PIT FRAME AT STA 1500 AND LONGERON 26 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME REPAIR IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500651 20000205 00651 WP 2000 2 5 RRXA991611 1 19990520 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1766 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CENTER FLOORBEAM AT AFT PRESSURE BULKHEAD FRAME ATTACHED FASTENERS LOOSE BOTH SIDES ATTACH ANGLE AND CORROSION EMANATING FROM FASTENERS AT STA 1766 AND LONGERON 36. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR SUPPORTS IAW DC 8 SRM 51-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500652 20000205 00652 WP 2000 2 5 RRXA991612 1 19990521 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, CENTER L/E UPPER SURFACE (SKIN) AT SCREW HOLE AT XFS 400.00 AT FR ONT SPAR ATTACHMENT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 57-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500653 20000205 00653 WP 2000 2 5 RRXA991613 1 19990522 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1690 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERIOR AT STA 1690, AFT OF PRODUCTION SPLICE AT LONGERON 31 RIGH T FITTING CRACKED AND CORROSION EXFOLIATION INSIDE FITTING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREA TED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EW A CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500654 20000205 00654 WP 2000 2 5 RRXA991614 1 19990526 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTH INTER-COSTALS AT STA 1540 DOOR FRAME RIGHT SIDE, BETWEEN BL 1 6 RIGHT AND BL 32 RIGHT, AND BETWEEN WL 20 RIGHT AND WL 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED , TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTALS IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RE CORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500655 20000205 00655 WP 2000 2 5 RRXA991615 1 19990526 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 35 - 80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN BETWEEN STA 35 AND STA 80 AND LONGERON 32 RIGHT, CORROSION BU LGE WITH PULLING FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. R EMOVED CORROSION IAW DC8 SRM 51-1-8. FUSELAGE SKIN WITHIN LIMITS IAW SRM 53-2-0. FABRICATED AND INSTALLED NEW SECTION LONGERON AND SPLICE IAW DC8 SRM 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500656 20000205 00656 WP 2000 2 5 RRXA991616 1 19990602 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CUSP FRAME SUPPORT AND WEB AT STA 25 AND LONGERON 25 RIGHT FLOOR LEVEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500657 20000205 00657 WP 2000 2 5 RRXA991617 1 19990710 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, C PIT FLOORBEAM SUPPORT STRUT AT STA 1160, BL 48 RIGHT, BETWEEN WL 10 RIGHT AND WL 40 RIGHT AND LONGERON 28 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW STRUT IAW DC8 SRM 51-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION P ROGRAM). 2 L 7 4 4F RT 4A25 2000020500658 20000205 00658 WP 2000 2 5 RRXA991619 1 19990716 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 280 - 320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, A PIT DOOR HINGED SILL GUARD RAMP FWD SUPPORT ANGLE LWR END BOLT H OLE AND CRACKED BETWEEN STA 280 AND STA 320. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC -8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2000020500659 20000205 00659 WP 2000 2 5 RRXA991620 1 19990619 A 5330 PANEL DOUG DC8 DC873F 302199F WP BS 659 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LEFT O/B AILERON I/B LWR ACCESS PANEL TOP PLATE AT XA 659. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL I AW DC8 SRM 51-3-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500660 20000205 00660 WP 2000 2 5 RRXA991621 1 19990609 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 616 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LWR FWD CARGO COMPT AT STA 616 AND LONGERON 31 RIGHT, SPLICE CRACK ED AND HAS CORROSION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICA TED AND INSTALLED SPLICE, FILLER AND SPLICE DOUBLERS IAW DC8 SRM 51-1-24 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN E WA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500661 20000205 00661 WP 2000 2 5 RRXA991622 1 19990519 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 450 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 604AL 46047 DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, UPPER SURFACE (SKIN) CENTER L/E AT STA XFS 450.000 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FIL LER AND DOUBLER IAW DC8 SRM 57-2-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000020500669 20000205 00669 NM 2000 2 5 UPS00231393 1 19990118 A 5311 FRAME BOEING 727 72722C 138400F NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 BS 930 FRAME INBOARD AND OUTBOARD FLANGE CRACKED, FROM STRINGER 18A TO MAIN LANDING GEAR PRESSURE DECK. REPLACED BS930 FITTING, RIGHT SIDE IN ACCORDANCE WITH BOEING DRAWING 65-16336. 2 L 7 3 4F A3WE 2000020500722 20000205 00722 NM 2000 2 5 UPS00231405 1 19991121 A 5311 FRAME BOEING 727 72725C 138400H NM BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI WHILE ACCESSING MCD FOR NDT, FOUND CORROSION UNDER SEAL DEPRESSOR BS 620 LT ABOVE SPLICE WL 268 ON FR AME. REPAIRED CORRODED FRAME IAW ER-6435A. 2 L 7 3 4F A3WE 2000020500745 20000205 00745 NM 2000 2 5 9905682289 1 19991201 A 5314 KEELBEAM BOEING 727 727251 138408H NM BS 950A CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 289US 21377 DURING H CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF KEEL BEAM. REPAIRED PER EA 22-170745. 2 L 7 3 4F A3WE 2000020500746 20000205 00746 NM 2000 2 5 9905696626 1 19991208 A 5320 DOUBLER BOEING 747 747251B 1384892 NM BS 999 - 1019 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 626US 21708 DURING M CHECK, FOUND CRACK ON DOUBLER LOCATED ON THE LOWER FLOOR STRUCTURE KEEL BEAM BOX INTERIOR. REPAIRED PER EA 66- 171527. 2 L 7 4 4F A20WE 2000020500747 20000205 00747 NM 2000 2 5 9905706626 1 19991215 A 5711 SPAR BOEING 747 747251B 1384892 NM WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 626US 21708 DURING M CHECK, FOUND CORROSION ON FRONT SPAR LOWER SURFACE OF THE LOWER CHORD. REPAIRED PER EA 66-171325. 2 L 7 4 4F A20WE 2000020500748 20000205 00748 NM 2000 2 5 9905716626 1 19991130 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 600 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 626US 21708 DURING M CHECK, FOUND CORROSION BETWEEN T CHORD AND WEB AT FLOOR LEVEL. REPAIRED PER EA 66-171436. 2 L 7 4 4F A20WE 2000020500808 20000205 00808 EU 2000 2 5 QXEA0000065 1 19991226 A 5320 POST FOKKER F28 F28MK4000 4990810 EU WINDOW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT-HAND NR 3 WINDOW POST IS CRACKED AT THE UPPER END. REPLACED IAW HORIZON AIR EO 4-53-56B. 2 L 7 2 4F RT A20EU 2000020500810 20000205 00810 EU 2000 2 5 QXEA0000067 1 19991223 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU BS 4150 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - NOSE LANDING GEAR DOG HOUSE BOX STRUCTURE IS DENTED ON TOP SKIN AND RIGHT-HAND CORNER AT FRAME 4150, VIEWED THROUG H FORWARD CARGO BAY. REPAIRED IAW HORIZON AIR EA 4-53-947. 2 L 7 2 4F RT A20EU 2000020500811 20000205 00811 EU 2000 2 5 QXEA0000068 1 19991231 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU BS 3450 - 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUSELAGE STRINGER 68 HAS CORROSION ON TOP SIDE ALONG RIVET LINE FROM FRAME 3450 TO 4900. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4 B AND C. 2 L 7 2 4F RT A20EU 2000020500812 20000205 00812 EU 2000 2 5 QXEA0000069 1 19991226 A 5320 SPLICE FOKKER F28 F28MK4000 4990810 EU BS 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT SIDE OF FRAME 4900, INTERIOR SKIN SPLICE DOUBLER HAD APPROXIMATELY FIVE SQUARE INCH OF WHITE POWDER CORROSION BETWEEN STRINGER 7 AND 8. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500813 20000205 00813 EU 2000 2 5 QXEA0000070 1 19991228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 9305A CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FUSELAGE FRAME 9305A HAS CORROSION UNDER TWO NUT PLATES LOCATED BETWEEN STRINGER 1 AND 74, TOP FLANGE OF FRAME UND ERSIDE. REPAIRED IAW HORIZON AIR EA 4-53-944. 2 L 7 2 4F RT A20EU 2000020500814 20000205 00814 EU 2000 2 5 QXEA0000071 1 19991220 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU BS 15635 BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT CARGO PIT GILLINER SUPPORT AT FRAME 15635 ABOVE STRINGER 74 IS BROKEN. REPAIRED IAW FOKKER SRM 53-22-11, PAGE 10-11 AND 52, 51-31-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 2000020500815 20000205 00815 EU 2000 2 5 QXEA0000072 1 19991230 A 5230 HINGE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT CARGO DOOR HINGE UNDER DOOR SEAL HAS LIGHT PITTING CORROSION. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGR APH 4B. 2 L 7 2 4F RT A20EU 2000020500816 20000205 00816 EU 2000 2 5 QXEA0000073 1 19991227 A 5320 COVER FOKKER F28 F28MK4000 4990810 EU BS 2475 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - NOSE LANDING GEAR BAY TOP COVER CRACKED IN TWO PLACES ALONG FORWARD SIDE OF RIVET ROW AT STATION 2475. REPAIRED I AW HORIZON AIR EA 4-53-913. 2 L 7 2 4F RT A20EU 2000020500817 20000205 00817 EU 2000 2 5 QXEA0000074 1 19991227 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 9305A CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FORWARD FUSELAGE CUTOUT JUST AFT OF FRAME 9305A HAS CORROSION FORWARD AND AFT UNDER BLANKING PLATE MOUNT DOUBLER A ND AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-53-951. 2 L 7 2 4F RT A20EU 2000020500818 20000205 00818 EU 2000 2 5 QXEA0000075 1 19991227 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 9305A CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT FUSELAGE CUTOUT JUST AFT OF FRAME 9305B HAS CORROSION FORWARD AND AFT UNDER BLANKING PLATE MOUNT DOUBLER AND A ROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-53-951. 2 L 7 2 4F RT A20EU 2000020500819 20000205 00819 EU 2000 2 5 QXEA0000076 1 19991221 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 476US 11224 PDX - CENTER CARGO DOOR LOWER FRAME UNDER HINGE HAS TWO AREAS OF TOOLING MARKS. REPAIRED IAW FOKKER SRM 52-30-00, PAGE 3, ITEM 160 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000020500820 20000205 00820 EU 2000 2 5 QXEA0000077 1 19991231 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU BS 3450 - 4150 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - STRINGER 68 BETWEEN FRAME 3450 AND 4150 HAS CRACK IN RIVET HOLE, FOUR RIVETS FORWARD OF FRAME 4150. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 2000020500842 20000205 00842 EU 2000 2 5 QXEA0000078 1 19991230 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT CARGO PIT AFT DOOR APERTURE HAS IMPACT DAMAGE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2000020500843 20000205 00843 EU 2000 2 5 QXEA0000079 1 19991230 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AFT CARGO PIT FORWARD DOOR APERTURE HAS IMPACT DAMAGE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2000020500844 20000205 00844 EU 2000 2 5 QXEA0000080 1 19991231 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU BS 4150 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RE-WORK REQUIRED FOR VERTICAL STIFFNER ANGLE FOR RIGHT-HAND INBOARD SEAT TRACK THAT TIES TO FRAME 4150. REPAIRED I AW FOKKER SRM 51-31-01, 53-11-05, PAGE 14, FIGURE 4. 2 L 7 2 4F RT A20EU 2000020500845 20000205 00845 EU 2000 2 5 QXEA0000081 1 19991229 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU BULKHEAD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - STIFFENER ON AFT PRESSURE BULKHEAD HAD THREE CRACKS AT RIVETS AT BL1300L BETWEEN WL300 AND WL500. REPAIRED IAW FO KKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 2000020500846 20000205 00846 EU 2000 2 5 QXEA0000082 1 19991230 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME CASTELLATION HAS A CRACK AT RIVET, FRAME 16060 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, F IGURE 2. 2 L 7 2 4F RT A20EU 2000020500847 20000205 00847 EU 2000 2 5 QXEA0000083 1 19991230 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME CASTELLATION HAS A CRACK AT RIVET, FRAME 16060 AND STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, F IGURE 2. 2 L 7 2 4F RT A20EU 2000020500849 20000205 00849 EU 2000 2 5 QXEA0000085 1 19991221 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - AREA OF EXPOSED METAL EXHIBITING LIGHT CORROSION APPROXIMATELY 1 X 1 LOCATED JUST FORWARD OF FRAME 13815 ON RIGHT- HAND INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500850 20000205 00850 EU 2000 2 5 QXEA0000086 1 19991221 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4610 - 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT-HAND SEAT TRACK HAS SEVERAL AREAS OF EXPOSED METAL EXHIBITING LIGHT CORROSION BETWEEN FRAMES 4610 AND 7305. REPAIRED IAW FOKKER SRM 51-10-04 AND SRM 53-40-01, PAGE 201. 2 L 7 2 4F RT A20EU 2000020500851 20000205 00851 EU 2000 2 5 QXEA0000087 1 19991221 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4610 - 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS SEVERAL AREAS OF EXPOSED METAL EXHIBITING LIGHT CORROSION BETWEEN FRAMES 4610 A ND 7305. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500852 20000205 00852 EU 2000 2 5 QXEA0000088 1 19991227 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 6805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACK IN RIGHT-HAND INBOARD SEAT TRACK APPROXIMATELY .200 LONG, LOCATED AT FRAME 6805. REPAIRED IAW HORIZON AIR E A 4-53-952. 2 L 7 2 4F RT A20EU 2000020500853 20000205 00853 EU 2000 2 5 QXEA0000089 1 19991231 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 5805 - 6305 DAMAGED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 476US 11224 PDX - TOOL DAMAGE ON RIGHT-HAND INBOARD SEAT TRACK. DAMAGE IS AT LOBE FOR FLOORBOARD FASTENER RECEPTICLE AND IS .145 WI DE X .182 LONG, LOCATED BETWEEN 5805 AND 6305. REPAIRED IAW HORIZON AIR EA 4-53-955. 2 L 7 2 4F RT A20EU 2000020500854 20000205 00854 EU 2000 2 5 QXEA0000090 1 19991221 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 9305C DAMAGED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT-HAND OUTBOARD SEAT TRACK HAS TOOL DAMAGE .300 LONG X .050 WIDE, LOCATED 10.5 AFT OF FRAME 9305C. REPAIRED I AW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500855 20000205 00855 EU 2000 2 5 QXEA0000091 1 19991221 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 10346 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT-HAND INBOARD SEAT TRACK HAD TWO GOUGES APPROXIMATELY .020 DEEP, LOCATED JUST FORWARD OF FRAME 10346. REPAIR ED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500856 20000205 00856 EU 2000 2 5 QXEA0000092 1 19991230 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU BS 3450 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON UNDERSIDE OF UPPER FLANGE OF NR 1 GALLEY FLOOR SUPPORT BEAM, 7 FORWARD OF FRAME 3450. REPAIRED IAW F OKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4 B AND C. 2 L 7 2 4F RT A20EU 2000020500857 20000205 00857 EU 2000 2 5 QXEA0000093 1 19991229 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU BS 3870 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - NR 1 GALLEY FLOOR SUPPORT BEAM AFT END IS CORRODED ON TOP, JUST AFT OF FRAME 3870. REPAIRED IAW FOKKER SRM 51-10- 04, PAGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500858 20000205 00858 EU 2000 2 5 QXEA0000094 1 19991231 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - TWO CRACKS IN VERTICLE SUPPORT UPPER NUT PLATE SUPPORT FOR AFT END OF NR 1 GALLEY SUPPORT BEAM. REPAIRED IAW FOKK ER SRM 51-31-01, 53-11-05, PAGE 10, FIGURE 03 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000020500859 20000205 00859 EU 2000 2 5 QXEA0000095 1 19991222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRETTING CORROSION ON LEFT-HAND OUTBOARD SEAT TRACK AT STATION 4900. REPAIRED IAW FOKKER SRM 51-10-4, PARAGRAPH 4 . 2 L 7 2 4F RT A20EU 2000020500860 20000205 00860 EU 2000 2 5 QXEA0000096 1 19991220 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU BS 6805 - 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON LEFT-HAND OUTBOARD FLOOR BOARD CHANNEL BETWEEN FRAMES 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-0 4. 2 L 7 2 4F RT A20EU 2000020500861 20000205 00861 EU 2000 2 5 QXEA0000097 1 19991222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 6805 - 7305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - NUMEROUS GOUGES IN LEFT-HAND OUTBOARD SEAT TRACK BETWEEN FRAME 6805 AND 7305. REPAIRED IAW FOKKER SRM 51-10-4, PA RAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500862 20000205 00862 EU 2000 2 5 QXEA0000098 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13815A GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - GOUGES IN LEFT-HAND OUTBOARD SEAT TRACK AT FRAME 13815A. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500863 20000205 00863 EU 2000 2 5 QXEA0000099 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13815A GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - GOUGES IN LEFT-HAND OUTBOARD SEAT TRACK, 5 AFT OF FRAME 13815A. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500864 20000205 00864 EU 2000 2 5 QXEA0000100 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 13815A-13815B CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRETTING CORROSION ON OUTBOARD FLANGE OF THE LEFT-HAND INBOARD SEAT TRACK BETWEEN FRAMES 13815A AND 13815B. REPAI RED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500865 20000205 00865 EU 2000 2 5 QXEA0000101 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 14755 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - GOUGES IN CENTER OF LEFT-HAND OUTBOARD SEAT TRACK, 4 AFT OF FRAME 14755. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 2000020500866 20000205 00866 EU 2000 2 5 QXEA0000102 1 19991219 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU BS 4175 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACK IN SUPPORT BRACKET AT FRAME 4175, BL620L. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7A (1-5). 2 L 7 2 4F RT A20EU 2000020500867 20000205 00867 EU 2000 2 5 QXEA0000103 1 19991223 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION AT RIGHT-HAND INBOARD SEAT TRACK WHERE IT ABUTS FLOORBEAM. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 3, PA RAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500868 20000205 00868 EU 2000 2 5 QXEA0000104 1 19991228 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4850 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON LEFT-HAND INBOARD SEAT TRACK AT FRAME 4850. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 2000020500869 20000205 00869 EU 2000 2 5 QXEA0000105 1 19991222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 6305 - 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON OUTBOARD FLANGE OF LEFT-HAND INBOARD SEAT TRACK BETWEEN FRAME 6305 AND 6805. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500870 20000205 00870 EU 2000 2 5 QXEA0000106 1 19991225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 6805 - 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON FLANGES OF LEFT-HAND INBOARD SEAT TRACK BETWEEN FRAMES 6805 AND 7305. REPAIRED IAW HORIZON AIR EA 4- 55-946. 2 L 7 2 4F RT A20EU 2000020500871 20000205 00871 EU 2000 2 5 QXEA0000107 1 19991222 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 7305 - 7805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - NICKS AND GOUGES IN INBOARD FLANGE OF LEFT-HAND INBOARD SEAT TRACK BETWEEN FRAMES 7305 AND 7805. REPAIRED IAW FOKK ER SRM 51-10-04, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500872 20000205 00872 EU 2000 2 5 QXEA0000108 1 19991220 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 7805 - 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION ON INBOARD FLANGE OF LEFT-HAND SEAT TRACK BETWEEN FRAMES 7805 AND 8305. REPAIRED IAW FOKKER SRM 51-10-4 . 2 L 7 2 4F RT A20EU 2000020500873 20000205 00873 EU 2000 2 5 QXEA0000109 1 19991229 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CORROSION APPROXIMATELY 1 X 3 ON OUTBOARD FLOOR SUPPORT ANGLE FOR PANEL 258C. REPAIRED IAW FOKKER SRM 51-10-04, P AGE 9, PARAGRAPH 4. 2 L 7 2 4F RT A20EU 2000020500874 20000205 00874 EU 2000 2 5 QXEA0000110 1 19991231 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 461D CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - OUTBOARD FLANGE OF RIGHT-HAND INBOARD SEAT TRACK CORRODED IN AND UNDER NUTPLATE RECEPTICAL, 2 FORWARD OF FRAME 461 D. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-957. 2 L 7 2 4F RT A20EU 2000020500875 20000205 00875 EU 2000 2 5 QXEA0000111 1 19991231 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 22293 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 22293 IS CRACKED BETWEEN STRINGER 21 AND 21A. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON AIR EA 4-53-945. 2 L 7 2 4F RT A20EU 2000020500876 20000205 00876 EU 2000 2 5 QXEA0000112 1 19991229 A 5320 HINGE FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT-HAND SPEED BRAKE LOWER HINGE ATTACH POINT BEARING BORE IS CORRODED ON LOWER MATING FLANGE AND SPLINE CHIP GR OOVE. REPAIRED IAW HORIZON AIR EA 4-53-949. 2 L 7 2 4F RT A20EU 2000020500877 20000205 00877 EU 2000 2 5 QXEA0000113 1 19991228 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISDRILLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - WEB TIE INSIDE OF SKIN FORWARD OF APU EXHAUST JUST AFT OF REAR PRESSURE BULKHEAD HAD FIVE DRILL STARTS ON WEB TIE AND ONE ON VERTICAL STIFFENER OF SAME WEB UNDER LAST RIVET. REPAIRED IAW HORIZON AIR EA 4-53-954. 2 L 7 2 4F RT A20EU 2000020500878 20000205 00878 EU 2000 2 5 QXEA0000114 1 19991228 A 5532 PANEL FOKKER F28 F28MK4000 4990810 EU VERTICAL STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - TOP ATTACH ANGLE FOR VERTICAL STABILIZER PANEL 57NB IS CRACKED FIVE INCHES. REPAIRED IAW HORIZON AIR EA 4-55-177. 2 L 7 2 4F RT A20EU 2000020500886 20000205 00886 EU 2000 2 5 QXEA0000116 1 19991221 A 5720 PLATE FOKKER F28 F28MK4000 4990810 EU BS 1700 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT-HAND FORWARD CENTER WING TO OUTER WING LOWER TIE PLATE HAD A GOUGE FROM A FAIRING FASTENER STATION 1700 NEAR LEADING EDGE. REPAIRED IAW HORIZON AIR EA 4-57-339. 2 L 7 2 4F RT A20EU 2000020500887 20000205 00887 EU 2000 2 5 QXEA0000117 1 19991223 A 5720 APERTURE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - 74A APERATURE HAD MINOR CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4C (2B). 2 L 7 2 4F RT A20EU 2000020500888 20000205 00888 EU 2000 2 5 QXEA0000118 1 19991223 A 5720 APERTURE FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - 74B APERATURE HAD MINOR CORROSION AT SCREW HOLES. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 4B (2B). 2 L 7 2 4F RT A20EU 2000020500889 20000205 00889 EU 2000 2 5 QXEA0000119 1 19991231 A 3210 BRACKET FOKKER F28 F28MK4000 4990810 EU MLG CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT-HAND WING MAIN LANDING GEAR BACK UP UPPER BRACKET WAS CRACKED AT LOWER BOLT, WITHIN PANEL 81X. REPAIRED IAW FOKKER SRM 57-07-09. 2 L 7 2 4F RT A20EU 2000020500891 20000205 00891 EU 2000 2 5 QXEA0000121 1 19991222 A 5711 SPAR FOKKER F28 F28MK4000 4990810 EU CENTER WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LIGHT CHAFING BELOW PANEL 92G AT AFT SPAR AND OUTER/CENTER WING ATTACHMENT. REPAIRED IAW SRM 51-10-4, PAGE 9, PAR AGRAPH 4 A, B, C. 2 L 7 2 4F RT A20EU 2000020500892 20000205 00892 EU 2000 2 5 QXEA0000122 1 19991223 A 5711 SPAR FOKKER F28 F28MK4000 4990810 EU CENTER WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - GOUGE BELOW PANEL 92G AT AFT SPAR AND OUTER/CENTER WING ATTACHMENT. REPAIRED IAW HORIZON AIR EA 9-57-340 AND FOKK ER SRM 51-10-4, PARAGRAPH 4 A, B, C. 2 L 7 2 4F RT A20EU 2000020500894 20000205 00894 EU 2000 2 5 QXEA0000128 1 19991227 A 5320 NUT PLATE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - REMOVED 3 HI-LOKS FROM RIGHT-HAND WINDOW POST UPPER FORWARD FLANGE OF POST TO GAIN ACCESS FOR NUT PLATE REMOVAL AN D REINSTALLATION. REPLACED THE BAD NUT PLATE IAW HORIZON AIR EO 4-53-56B, FIGURE 5. 2 L 7 2 4F RT A20EU 2000020500895 20000205 00895 EU 2000 2 5 QXEA0000129 1 19991230 A 5320 STRINGER CLIP FOKKER F28 F28MK4000 4990810 EU BS 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACK AT FRAME 5305 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 2000020500927 20000205 00927 EA 2000 2 5 2000ZZZX262 2 19991213 A 8520 CAMSHAFT CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA ENGINE FAILED A ZTUA K NONE O OTHER IN INSP/MAINT 1 EA 11 9934Q 17265878 METAL FOUND IN OIL FILTER DURING ROUTINE INSPECTION. ENGINE CAM LOB FAILURE. POSSIBLE INCORRECT HARDENEING PROCEDURES ON CAM. 1 H 7 1 3O 3 O NT 3A12 E274 2000020500933 20000205 00933 EA 2000 2 5 WVBA019/99 2 19991229 A 7414 10382681 CAPACITOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MAGNETO FAILED A WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 42WP 86 WAV004 318252038 LEFT ENGINE WOULD NOT START. MAGNETO WAS EXAMINED AND BOTH CAPACITORS WERE FOUND SHORTED OPEN. PART TTIS: 86.1 HOURS. REF: OPER CNTRL NR: 2000ZZZX268. (X) 1 L 7 2 3O 3 O A20SO E14EA 2000020500934 20000205 00934 EA 2000 2 5 2000ZZZX268 2 19991229 A 7414 10382681 CAPACITOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MAGNETO FAILED A WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 42WP 86 WAV007 318252038 LEFT ENGINE WOULD NOT START. MAGNETO WAS EXAMINED AND BOTH CAPACITORS WERE FOUND SHORTED OPEN. PART TTIS: 86.1 HOURS. REF: OPER CNTRL NR: WVBA019/99. 1 L 7 2 3O 3 O A20SO E14EA 2000020500935 20000205 00935 EA 2000 2 5 WVBA018/99 2 19991229 A 7414 10382681 CAPACITOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MAGNETO FAILED A WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 42WP 15 318252038 ENGINE WOULD NOT START. BOTH CAPACITORS WERE FOUND SHORTED OPEN. PART TTIS: 14.5 HOURS. (X) 1 L 7 2 3O 3 O A20SO E14EA 2000020500936 20000205 00936 EA 2000 2 5 WVBA017/99 2 19991229 A 7414 10382681 CAPACITOR PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MAGNETO FAILED A WVBA O OTHER O OTHER NR NOT REPORTED 1 AL 01 42WP 138 WAV008 318252038 RIGHT ENGINE WOULD NOT START. MAGNETO WAS REPLACED. DURING TIMING PROCESS, RIGHT CAPACITOR WAS FOUND OPEN. PART TTIS: 138.4 HOURS. (X) 1 L 7 2 3O 3 O A20SO E14EA 2000020500940 20000205 00940 WP 2000 2 5 2000ZZZX272 1 19991215 A 6220 369D21210501 STRAP 369D21200503 HUGHES 369 369D 4470706 WP MAIN ROTOR CRACKED A A IZWA K NONE O OTHER IN INSP/MAINT 1 NM 09 214PC 6034 566 461 1100851D MAIN ROTOR HUB STRAP PACK ASSY WAS FOUND WITH ONE CRACKED LEG AT 226.2 HOURS TSO, SECOND CRACK FOUND AT 542.1 HOURS. BO TH CRACKS WERE IN THE LAG (TRAILING EDGE) LEG OF THE SAME PACK. THIRD AND FAILING CRACK WAS FOUND AT 578.8 HOURS TSO. R EPLACED WITH ZERO HRS TSO ITEM. THIS AIRCRAFT HAS BEEN USED FOR THE SAME ACTIVITIES (POWERLINE CONSTRUCTION AND MAINTEN ANCE) FOR THE PRECEDING 6,000 HRS AND THIS IS THE FIRST STRAP PACK FAILURE (ON LAST 3 HUB ASSY'S). ALSO, OPERATE 4 OTHE R HUGHES 369 SERIES ACFT AND NO STRAP PACK FAILURES ON ANY OF THOSE EITHER. SB DN-154 COVERS THE INSPECTION OF THIS COM PONENT. STRAP S/N'S F707 THROUGH F7111. 1 G 7 1 3U H3WE 2000020500941 20000205 00941 SW 2000 2 5 NXTA457U 1 19991227 A 6510 407340339101 BEARING BELL 407 407 SW COOLER BLOWER FAILED A P A NXTA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 19 148CF 475 53326 IN-FLIGHT 2 OR 3 MINUTES PRIOR TO LANDING, A SEVERE VIBRATION AND LOUD NOISE WAS FELT AND HEARD. THE AIRCRAFT LANDED. I T WAS DISCOVEREDTHE AFT OIL COOLER BLOWER SHAFT AFT BEARING HAD FAILED AND COME APART. THE INNER RACE AND BALL BEARINGS DAMAGED THE IMPELLER. THE OUTER RACE AND HANGAR DAMAGED THE BLOWER SHAFT. POSSIBLE CAUSE WAS OVERHEATING. BEARING WAS LUBRICATED APPROXIMATELY 80 HRS PRIOR TO OCCURRENCE. REPORTED TO BELL HELICOPTER PRODUCT SUPPORT FOR INVESTIGATION. BE ARING WAS NEW STYLE TYPE (BLUESEAL).(X) 1 G 7 1 3U O H2SW 2000020500946 20000205 00946 CE 2000 2 5 CA000118002 1 19991231 A 3260 444EN496 SQUAT SWITCH 101810000606 BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE HARTZL HCD4N3 HCD4N3A GL RT MLG OUT OF ADJUST W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 5037 PCE93618 FY1335 (CAN) AFTER TAKEOFF, THE GEAR FAILED TO RETRACT WHEN SELECTED UP. RETRACTION CHECKED CARRIED OUT IN HANGAR. FAILURE FO UND TO BE RIGHT SQUAT SWITCH OUT OF ADJUSTMENT. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 2000020500950 20000205 00950 EU 2000 2 5 CA000118013 1 19991221 A 5610 NF20216402 WINDOW HEAT BRAERO BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 12211 L223505 LF05683A (CAN) WINDSHIELD HEAT UNSERVICEABLE. WINDSHIELD REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 2000020500958 20000205 00958 NE 2000 2 5 CA000118031 2 19991215 A 7230 4002T20P02 CARBON SEAL GE CF7002D2 AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE NR 1 ENGINE LEAKING W B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 3183 304435B 304435B (CAN) OIL SMOKE ENTERING VIA BLEED AIR SYSTEM. 2 L 7 2 4F 4 F RT A7EU E7EA 2000020500959 20000205 00959 NM 2000 2 5 CA000118034 1 19991222 A 2910 82970010415 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W E D ENGINE SHUTDOWN RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 25395 120329 870304 (CAN) DURING THE ENGINE START, HYDRAULIC FLUID QUANTITY DROPPED TO .5 QUARTS. MAINTENANCE FOUND THE PRESSURE LINE TO TH E QUANTITY LIMITING VALVE TO BE CHAFED AND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000020500960 20000205 00960 NM 2000 2 5 CA000118035 1 19991221 A 2910 82950010273 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 25404 TM120796 900948 (CAN) HYDRAULIC LINE TO THE LEFT INBOARD SPOILER ACTUATOR WAS FOUND CRACKED AND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000020500961 20000205 00961 NM 2000 2 5 CA000118036 1 19991221 A 2761 A509521 HOUSING DOWTY A44700009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE SPOILER ACTUATOR CRACKED W O OTHER K FLUID LOSS LD LANDING 1 CA 22668 0799 120549 LH10087 (CAN) THE FLIGHT CREW REPORTED THAT THE LEFT OUTBOARD ROLL SPOILER DID NOT DEPLOY DURING LANDING. MAINTENANCE FOUND THA T THE SPOILER ACTUATOR WAS LEAKING FROM A CRACK IN THE HOUSING AT THE PRESSURE INLET FITTING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000020500962 20000205 00962 EA 2000 2 5 CA000118037 1 19991229 A 2611 302313 SMOKE DETECTOR KIDDE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE CARGO BAY MALFUNCTIONED W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA 19264 31439 123144 LH750 (CAN) DURING TAXI, THE BAGGAGE COMPARTMENT SMOKE DETECTOR WARNING CAME ON. THE FLIGHT CREW SHUT DOWN AND EVACUATED THE A IRCRAFT. MAINTENANCE FOUND MOISTURE ON THE SMOKE DETECTOR AND CANNON PLUG. THEY DETERMINED THE MOISTURE CAME FROM SNOW WHICH HAD BLOWN INTO THE BAGGAGE COMPARTMENT DURING LOADING OPERATIONS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000020500966 20000205 00966 CE 2000 2 5 CA000118053 1 19991216 A 3260 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL MLG LOOSE W B EMER. DESCENT J WARNING INDICATION LD LANDING 1 CA 24773 PCE32185 FWA2435 (CAN) FIRST INCIDENT, THE AIRCRAFT LANDING GEAR SYSTEM FUNCTION TESTED OK IN THE HANGAR SO PERSONNEL WERE UNABLE TO DUPL ICATE PROBLEM. AFTER SECOND OCCURRENCE MAINTENANCE PERSONNEL COULD DUPLICATE THE PROBLEM ON THE GROUND AND ATTRIBUTED I T TO A BENT PIN AT THE CONNECTION J107 ON THE RIGHT GEAR LEG. AT THE THIRD RECURRENCE, THE LANDING GEAR RELAY WAS CHANG ED. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 2000020500969 20000205 00969 CE 2000 2 5 CA000118056 1 19991207 A 3297 602EN16 WIRE AIRIGHT 11238002223 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE NLG BROKEN W O OTHER J WARNING INDICATION AP APPROACH 1 CA 5500 576 PCEPS0103 HJ733 (CAN) ON APPROACH TO GOOSE BAY, THE CREW NOTED THERE WAS NO DOWN AND LOCKED INDICATION (GREEN) FOR THE NOSE GEAR. MAINT ENANCE DISCOVERED A BROKEN WIRE AT THE ENTRY INTO THE MICROSWITCH ON THE NOSE GEAR ACTUATOR. ACTUATOR REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2000020500970 20000205 00970 CE 2000 2 5 CA000118058 1 19991221 A 3397 L33J20 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE COCKPIT FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 5590 PCEPS0103 HJ733 (CAN) LOSS OF INSTRUMENT LIGHTING ON CPT AND COPILOT INSTRUMENT PANEL. LIGHTS CONTROLLED BY 2 SEPARATE POTENTIOMETERS ON OVERHEAD PANEL. PROBLEM ACTUATED C/B 21 LOCATED UNDER FLOOR WHICH FEEDS BOTH INSTRUMENT PANEL LIGHTS. MAINT FOUND T HAT BEHIND AUDIO SELECTOR PANEL, WIRE L33J20 WAS CHAFED ON CENTER FORMER STA 94. NOTED THAT L33J20 WAS NOT SECURED TO A NYTHING. WIRE L33J20 FEEDS POST LIGHTS ON INSTRUMENT PANEL AND IS FED FROM TB118 TERMINAL 7 WHICH IS CONTROLLED BY C/B 21. SHORT ALSO CAUSED TRANSISTOR Q5 WHICH CONTROLS PILOT FLIGHT LIGHTS TO SHORT OUT. THE CHAFED WIRE WAS SECURED, TR ANSISTOR REPLACED, C/B 21 RESET. SUBMITTER SAYS FEED TO 2 PILOTS SHOULD BE SEPARATED AND OFF 2 C/B'S. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2000020500971 20000205 00971 CE 2000 2 5 CA000118059 1 19991222 A 2140 RH502 RESISTOR ELECTROMECH EM6302 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HEATER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3856 2068 PCEPS0276 (CAN) CREW REPORTED REDUCED AIRFLOW THROUGH CABIN VENTS. MAINTENANCE DISCOVERED FORWARD HEATER NOT WORKING. BLOWER ASS Y REMOVED (P/N EM630-2/114-380028-5) AND UPON INSPECTION, FOUND TO BE VERY STIFF TO ROTATE. RESISTOR COVER REMOVED AND IT WAS DISCOVERED THE 2 RESISTORS HAD MOVED OUT FROM THEIR HEAT SINK (ONE BY 11.0 MM THE OTHER 5.4 MM). ONE RESISTOR SH OWED SIGNS OF HEAT DAMAGE AS WELL AS BEING CRACKED AROUND ITS CIRCUMFERENCE. FWD BLOWER REPLACED. SUBMITTER SUGGESTS S ETTING AN OVERHAUL TIME LIMIT ON BLOWER. 2 L 7 2 4T 4 T RT A24CE E26NE 2000020501005 20000205 01005 NM 2000 2 5 UPS00231450 1 19990128 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, MAIN ENTRY BY COCKPIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY, CHECKS OK. 2 L 7 3 4F A3WE 2000020501007 20000205 01007 NM 2000 2 5 UPS00231453 1 19990128 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE:N/A, RT FWD OVERWING DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 2000021200307 20000212 00307 NE 2000 2 12 USAAD99154 2 19991031 A 7310 320115 VALVE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE RT ENGINE FAILED OPEN A USAA A E UNSCHED LANDING ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 19 920VJ 39814 36166 48140 PIT/SBN - FLT 664 - DURING CRUISE, THE RIGHT ENGINE OIL TEMPERATURE GAUGE CLIMBED INTO THE YELLOW RANGE AND STABILIZED A T 130 DEGREES CELSIUS AFTER TOPPING AT 140 DGREES CELSIUS. AFTER 15 MINUTES WITH THE OIL TEMPERATURE IN THE YELLOW RANG E, THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO FWA AND LANDED WITHOUT INCIDENT. THERE 15 MINUTES SINGLE ENGIN E TIME. MAINTENANCE REPLACED THE RIGHT ENGINE AIR/FUEL HEATER VALVE. THE RIGHT ENGINE OIL AND OIL FILTER WERE ALSO REP LACED. (X) 2 L 7 2 4F 4 F A6WE E2EA 2000021200308 20000212 00308 NE 2000 2 12 A6WA9900122 2 19991030 A 7321 77390010 FUEL CONROL BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE FAILED A A6WA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 31 608AW 16255 F6601 E2049 COS/DEN - FLT 5568 - UNCOMMANDED ROLL BACK ON NR 2 ENGINE, ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 FUEL CONTROL UNIT . FUEL CONTROL UNIT TSR 3166 CSR 3553. PART TOTAL CYCLES, 19,244. (X) 2 H 7 4 4F 4 F RT A49EU E6NE 2000021200309 20000212 00309 NM 2000 2 12 AALA991872 1 19991205 A 2170 COALESCER BAG BOEING 737 737823 13844BZ NM CABIN AIR ODOR A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 905AN 29507 SAN - FLT 1626 - AFTER TAKEOFF, RUBBER ODOR IN CABIN. RETURNED AND LANDED SAN WITHOUT FURTHER INCIDENT. MAINTENANCE AC COMPLISHED OPERATIONS CHECK OF ELECTRICAL EQUIPMENT. UNABLE TO DUPLICATE RUBBER ODOR. AS A PRECUATIONARY, CHANGED COAL ESER BAGS. OPERATED PACKS WITH ENGINES AND APU WITH NO RUBBER ODOR NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X ) 2 L 7 2 4F RT A16WE 2000021200311 20000212 00311 WP 2000 2 12 2000ZZZX332 1 19990902 A 5330 57503293 SKIN DOUG DC8 DC861 3021952 WP BS 742 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION DAMAGE AT STA 742, LONGERON L1. REPAIRED COR ROSION DAMAGE IAW FINE AIRLINES EA NR G5313-11:00, SEMAN EO NR 990085 AND BOEING MESSAGE M-7200-99-08106. 2 L 7 4 4F 4A25 2000021200312 20000212 00312 WP 2000 2 12 2000ZZZX333 1 19990902 A 5330 57503293 SKIN DOUG DC8 DC861 3021952 WP BS 680-702 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK, INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION DAMAGE AT STA FS 680 TO STA FS 702 BETWEEN LONGERONS L4 LT TO L6 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-02:00, SEMAN EO NR 990080 AND BOEING MESSAGE M7200-99-07382. 2 L 7 4 4F 4A25 2000021200313 20000212 00313 WP 2000 2 12 2000ZZZX334 1 19990902 A 5313 57501981 LONGERON DOUG DC8 DC861 3021952 WP BS 960-980 CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LEFT LONGERON 24 WITH TWO CRACKS BETWEEN STA 960 AND STA 980. REPAIRED CRACKS IAW FINE AIRLINES EA NR G5313-03:00, SEMAN EO NR 990088 AND BOEING MESSAGE M7200-99-06994. 2 L 7 4 4F 4A25 2000021200314 20000212 00314 WP 2000 2 12 2000ZZZX335 1 19990902 A 5330 57503293 SKIN DOUG DC8 DC861 3021952 WP BS 857 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK, INSPECTION, FOUND THE FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 857 BETWEEN LONGERONS L1 AND L2 RIGHT . REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-08:00, SEMAN EO NR 990098 AND BOEING MESSAGE SEU-LIM-99-00016 H. 2 L 7 4 4F 4A25 2000021200315 20000212 00315 WP 2000 2 12 2000ZZZX336 1 19990902 A 5730 3758032 PANEL DOUG DC8 DC861 3021952 WP WS 408 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON RT WING AT INNER AFT PLATING PANEL AT STA XW 408 BETWEEN S TRINGERS 5 AND 7. REPAIRED CORROSION DAMAGE IAW FINE AIR EA NR G5730-08:00, SEMAN EO 990103 AND BOEING MESSAGE M7200-99 -08364. 2 L 7 4 4F 4A25 2000021200316 20000212 00316 WP 2000 2 12 2000ZZZX337 1 19990902 A 5330 57555214 SKIN DOUG DC8 DC861 3021952 WP BS 1260 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 1260, BETWEEN LONGERSONS L1 AND L2 RIG HT. REPAIRED CORROSION DAMAGE IAW FINE ARLINES EA NR G5313-06:00, SEMAN EO NR 990097 AND BOEING MESSAE M-7200-99-07702. 2 L 7 4 4F 4A25 2000021200317 20000212 00317 WP 2000 2 12 2000ZZZX338 1 19990902 A 3211 5750092504 FITTING DOUG DC8 DC861 3021952 WP RT MLG CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RIGHT MAIN LANDING GEAR TRAPEZOIDAL SUPPORT FITTING WITH FOUR CRACKS AT STA 868 IN RT WHEELWELL. REPAIRED CRACKS IAW SEMAN EO NR 9900990 AND BOEING MESSAGE M-72-00-99-06884. FINE AIRLINES EA NR G3211-01:00. 2 L 7 4 4F 4A25 2000021200318 20000212 00318 WP 2000 2 12 2000ZZZX339 1 19990902 A 5330 57503294 SKIN DOUG DC8 DC861 3021952 WP BS 898-911 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 898 TO STA 911 BETWEEN LONGERONS L2 LT AND L4 RT. REPAIRED FUSELAGE CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-05:00, SEMAN EO 990099 AND BOEING MESSAGE SEU-LIM-99-00019H. 2 L 7 4 4F 4A25 2000021200319 20000212 00319 WP 2000 2 12 2000ZZZX340 1 19990902 A 5320 36471171 FITTING DOUG DC8 DC861 3021952 WP BS 960 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 960 IN LT WHEELWELL. REPAIRED CORORSION DAMAGE IAW SRM 53-2-0. 2 L 7 4 4F 4A25 2000021200320 20000212 00320 WP 2000 2 12 2000ZZZX341 1 19990902 A 5320 3641004501 FITTING DOUG DC8 DC861 3021952 WP BS 879.3 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 879.375 IN LT WHEELW ELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0. 2 L 7 4 4F 4A25 2000021200321 20000212 00321 WP 2000 2 12 2000ZZZX342 1 19990902 A 5320 36471172 FITTING DOUG DC8 DC861 3021952 WP BS 960 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON RT LONGERON 24 CORROSION DAMAGED AT STA 960 IN RT WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-20-0. 2 L 7 4 4F 4A25 2000021200322 20000212 00322 WP 2000 2 12 2000ZZZX343 1 19990902 A 5330 57503294 SKIN DOUG DC8 DC861 3021952 WP BS 980 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND FOLLOWING: CORROSION ON FUSELAGE TOP AT STA 980, BETWEEN LONGERONS L2 LT AND L2 RT. R EPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-07: 00, SEMAN EO NR 990093 AND BOEING MESSAGE M-7200-99-07595. 2 L 7 4 4F 4A25 2000021200323 20000212 00323 WP 2000 2 12 2000ZZZX344 1 19990902 A 5330 56138593 SKIN DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT PASSENGER DOOR, LOWER AFT JAMB CORNER CRACKED. REPAIRED CRACK DOOR IAW FINE AIRLINES EA NR G5320-01:00; SEMAN EO NR 990082 AND BOEING MESSAGE M-7200-99-07463 2 L 7 4 4F 4A25 2000021200324 20000212 00324 WP 2000 2 12 2000ZZZX345 1 19990902 A 5330 57503293 SKIN DOUG DC8 DC861 3021952 WP BS 717 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION DAMAGE AT STA 717 BETWEEN LONGERONS L1 TO L2 , LT. REPAIRED CORROSION DAMAGE IAW WITH FINE AIRLINES EA NR G5313-10:00, SEMAN EO NR 990084 AND BOEING MESSAGE M-7200- 99-08106. 2 L 7 4 4F 4A25 2000021200325 20000212 00325 WP 2000 2 12 2000ZZZX346 1 19990902 A 5330 57503294 SKIN DOUG DC8 DC861 3021952 WP BS 940 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE TOP HAS CORROSION AT STA 940.000 AND BETWEEN LONGERONS L1 AND L2 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-09:00, SEMAN EO NR 990091 AND BOEING MESSAGE M-7200-99- 07538. 2 L 7 4 4F 4A25 2000021200326 20000212 00326 WP 2000 2 12 2000ZZZX347 1 19990902 A 5531 56114081 SPAR DOUG DC8 DC861 3021952 WP RT AND LT WING CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION ON VERTICAL FIN ON LT AND RT REAR SPAR AT STA ZR 45. REPAIRE D CORROSION DAMAGE IAW FINE LINES EA NR G5531-01:00, SEMAN EO NR 990092 AND BOEING MESSAGE M-7200-99-08438. 2 L 7 4 4F 4A25 2000021200327 20000212 00327 WP 2000 2 12 2000ZZZX348 1 19990902 A 5313 57501981 LONGERON DOUG DC8 DC861 3021952 WP BS 960-980 CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT LONGERON 24 CRACKED BETWEEN STA 960 AND STA 980 IN LT WHEELWELL. RE PAIRED CRACK IAW FINE LINES EA NR G5313-12:00, SEMAN EO NR 990089 AND BOEING MESSAGE M-7200-99-06994. 2 L 7 4 4F 4A25 2000021200328 20000212 00328 WP 2000 2 12 2000ZZZX349 1 19990902 A 5320 36469561 FITTING DOUG DC8 DC861 3021952 WP BS 940 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FITTING ON LT LONGERON 24 CORROSION DAMAGED AT STA 940 IN LR WHEELWELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0. 2 L 7 4 4F 4A25 2000021200329 20000212 00329 WP 2000 2 12 2000ZZZX350 1 19990902 A 5730 561135025 PANEL DOUG DC8 DC861 3021952 WP LT WING CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CRACK AND CORROSION ON LT WING INNER AFT PLATING PANEL AT STA XRS 69 AF T OF REAR SPAR. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-07:00, SEMAN EO NR 990101 AND BOEING MESSAGE M- 7200-99-08151. 2 L 7 4 4F 4A25 2000021200330 20000212 00330 WP 2000 2 12 2000ZZZX351 1 19990902 A 5315 5750092504 FLOORBEAM DOUG DC8 DC861 3021952 WP BS 1680 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE FLOORBEAM AT STA FS 1680. REPAIRED CORROSION DAMAGE I AW WITH FINE AIRLINES EA NR G5310-05:00, SEMAN EO 9908241. 2 L 7 4 4F 4A25 2000021200331 20000212 00331 WP 2000 2 12 2000ZZZX352 1 19990902 A 5730 57695893 SKIN DOUG DC8 DC861 3021952 WP LT WING CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION AND CRACK ON LT WING INNER EXTENDED LEADING EDGE AT LOWER SKI N BETWEEN STA FS 304 TO XFS 341. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-03:00, SEMAN EO NR 990102 AND BOEING MESSAGE SEU-LIM-99-0025H. 2 L 7 4 4F 4A25 2000021200332 20000212 00332 WP 2000 2 12 2000ZZZX353 1 19990902 A 5730 561135025 PANEL DOUG DC8 DC861 3021952 WP LT WING CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: LT WING INNER AFT TOP PANEL PLATING CRACKED AND CORRODED AT STA XW 408 BETWEEN STRINGERS 2 AND 3. REPAIRED CRACK IN WING IAW FINE AIRLINES EA NR G5730-04:00, SEMAN EO NR 990095 AND BOEING ME SSAGE M-7200-99-07795. 2 L 7 4 4F 4A25 2000021200333 20000212 00333 WP 2000 2 12 2000ZZZX354 1 19990902 A 5730 57696006 PANEL DOUG DC8 DC861 3021952 WP RT WING CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT WING CORRODED AT OUTER WING OUTBOARD OF EXTENDED LEADING EDGE AT STA XFS 710. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5754-01:00, SEMAN EO NR 990096 AND BOEING MESSAGE M-7200-9 9-08383 AND M-7200-99-08600. 2 L 7 4 4F 4A25 2000021200334 20000212 00334 WP 2000 2 12 USAA991388 1 19991212 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 658 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 72088 47508 PIT - DURING C-3 CHECK, FOUND CRACK .50 INCH LONG. CRACK IN LONGERON AT STA 658 LONGERON 2 LT. INSTALLED LONGERON SECT ION PER 53-04 FIG 38. (X) 2 L 7 2 4F A6WE 2000021200335 20000212 00335 WP 2000 2 12 2000ZZZX355 1 19991229 A 5311 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 982VJ 43564 48158 PIT - DURING A CHECK, FOUND 3 INCH CRACK IN TAIL CONE ATTACH FRAME RT SIDE AT RUDDER ACTUATOR ATTACH POINT. CUT OUT DAM AGE. SPLICED IN SECTION PER DOUGLAS DRAWING 9911843. (X) 2 L 7 2 4F A6WE 2000021200336 20000212 00336 NM 2000 2 12 USAA990795 1 19990812 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 809 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35396 23552 CLT - ON PARKED, OUT OF TIME AIRCRAFT, FOUND 1.5 INCH CRACK AT STR 22R, STA 809. INSTALLED DOUBLER PER SRM 53-00-01. ( X) 2 L 7 2 4F RT A16WE 2000021200337 20000212 00337 NM 2000 2 12 USAA990798 1 19990803 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 39475 23316 TPA - DURING CX-1 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK BELLY SKIN AFT EQUIPMENT COOLING EXHAUST STA 380 FUSELAGE S KIN. INSTALLED REPAIRED DOUBLER PER TR 53-30-07. (X) 2 L 7 2 4F RT A16WE 2000021200341 20000212 00341 NM 2000 2 12 USAA991465 1 19991229 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AU 46390 22795 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN EXTERIOR SKIN STA 727A PLUS 8 INCHES AND STR 18 RT SK IN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (X) 2 L 7 2 4F A16WE 2000021200343 20000212 00343 NM 2000 2 12 USAA990859 1 19990807 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 40331 22957 PIT - DURING CX3 CHECK, FOUND .3750 INCH CRACK IN SKIN AT AFT ENTRY DOOR UPPER HINGE CUTOUT. DOUBLER INSTALLED PER SRM 53-60-01 FIG 205. 2 L 7 2 4F RT A16WE 2000021200345 20000212 00345 NM 2000 2 12 USAABB99060 1 19991215 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 27198 LAX - FOUND L4 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER BATTERY. (X) 2 L 7 2 4F RT A2NM 2000021200346 20000212 00346 NM 2000 2 12 USAABB99061 1 19991231 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 9 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 SFO - FOUND FLOOR EMERGENCY LIGHT AT ROW INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F RT A2NM 2000021200347 20000212 00347 NM 2000 2 12 ISAABB0050 1 19991215 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROWS 18 AND 33 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 LAX - FOUND FLOOR EMERGENCY ESCAPE PATH LIGHTS AT ROWS 18 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (X) 2 L 7 2 4F RT A2NM 2000021200348 20000212 00348 NM 2000 2 12 USAABB99057 1 19991220 A 3350 233T321028 LIGHT PANEL BOEING 767 767201 1385125 NM COCKPIT MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 649US 23901 PHL - CREW DISCOVERED A PROBLEM WITH THE EMERGENCY LIGHT PANEL. MAINTENANCE REPLACED THE PANEL. (X) 2 L 7 2 4F RT A1NM 2000021200351 20000212 00351 NM 2000 2 12 TWRA9985 1 19991229 A 3350 6012111 BATTERY PACK BOEING 747 747131 1384881 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 608FF 1166 19672 DURING DAILY CHECK, FOUND EXTERIOR EXIT LIGHT RIGHT SIDE REAR INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERA TIONAL CHECK OK PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 2000021200360 20000212 00360 WP 2000 2 12 2000ZZZX360 1 19990902 A 5315 FLOORBEAM DOUG DC8 DC861 3021952 WP BS 920 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE FLOORBEAM AT STA BS 920 APPROXIMATELY LBL 45. REPAIRE D CORROSION DAMAGE IAW FINE AIRLINES EA NR G5310-06:00, SEMAN EO NR 9908202. 2 L 7 4 4F 4A25 2000021200373 20000212 00373 WP 2000 2 12 AT0000067 1 19991203 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 197 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND FLOOR SUPPORT AT BS 197 BL 0 TO LBL 44 HAD EXFOLIATION CORROSION. REMOVED FLOOR SUPPORT, FABRICATED, TRIMMED, DRI LLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW SUPPORT IAW DC9 SRM 51-10-4, 53-11-1 FIG 13, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 2000021200374 20000212 00374 WP 2000 2 12 AT0000068 1 19991220 A 5720 TEE CAP DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 FOUND TEE CAP IN LT WING BETWEEN STRINGER 12 AND 17 CORRODED. FABRICATED AND INSTALLED REPAIR CLIPS IAW SB 57-98R8. 2 L 7 2 4F A6WE 2000021200513 20000212 00513 NM 2000 2 12 MZZA99231 1 19991121 A 5400 65207623 FLANGE BOEING 727 727264 138408M NM BS 1342 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON NR 2 ENGNE S-DUCT MOUNTIN G FLANGE AT BS 1342. THE CRACKED FLANGE WAS REMOVED AND REPLACED WITH A NEW ONE PER B727SB 727-54-15R2 AND CMI ECRA 541 0-01525. (M) 2 L 7 3 4F A3WE 2000021200514 20000212 00514 NM 2000 2 12 MZZA99230 1 19991121 A 5320 ANGLE BOEING 727 727264 138408M NM BS 1253 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .5 INCH LONG CRACK WAS FOUND ON RIGHT LOWER TORQUE BOX H ORIZONTAL WEB SUPPORT L ANGLE AT BS 1253. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M) 2 L 7 3 4F A3WE 2000021200515 20000212 00515 EU 2000 2 12 2000ZZZM89 1 19991210 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 429AT 429 RIGHT AFT INBOARD SEAT TRACK HAS CORROSION AROUND HI-LOK HOLES AT FLOORBEAM NR 36. BLENDED CORROSION IAW ATR-72 SRM 51- 21-42. COMPLIED WITH EO NR E9-5300-013 R4, PART 'B' WAS SATISFACTORILY ACCOMPLISHED. (M) 2 H 7 2 4T RT A53EU 2000021200516 20000212 00516 EU 2000 2 12 SIMA3491 1 19991215 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 309AE A3895 340B309 JFK - FLT 5121 - AVIONICS SMOKE DETECTOR GAVE SMOKE INDICATION IN FIGHT. AIRCRAFT TURNED BACK TO FIELD. REMOVED AND RE PLACED AVIONICS SMOKE DETECTOR DUE TO FALSE INDICATION. (M) 2 L 7 2 4T RT A52EU 2000021200517 20000212 00517 EU 2000 2 12 SIMA3558 1 19991219 A 2611 72111211000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 21 202KD A3461 340B202 DFW - FLT 3252 - AVIONIC SMOKE LIGHT CAME ON FOR ABOUT 10 SECONDS THEN WENT OUT. NO OTHER SIGNS OF SMOKE. REMOVED AND REPLACED AVIONIC SMOKE DETECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2000021200518 20000212 00518 SO 2000 2 12 SIMA993451 1 19991211 A 3350 7287103507 MODULE EMB 145 EMB145LR SO CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AE SM00455R 145079 DFW - FLT 3664 - FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH DOES NOT FUNCTION. REMOVED AND REPLACED CONTROL MODULE ASSEMBL Y. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2000021200519 20000212 00519 EU 2000 2 12 SIMA993442 1 19991210 A 3350 7239410803 LIGHT SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346SB 340B346 DFW - FLT 3356 - EMERGENCY LIGH TAT SEAT 3C DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMLBY. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000021200520 20000212 00520 SO 2000 2 12 SIMA993441 1 19991210 A 3350 RPS1B BATTERY EMB 145 EMB145LR SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 620AE 12550 145102 ABI - FLT 3502 - EMERGENCY LIGHT AFT OF GALLEY DOES NOT ILLUMINATE. REMOVED AND REPLACED ASSOCIATED EMERGENCY BATTERY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2000021200521 20000212 00521 EU 2000 2 12 SIMA993432 1 19991209 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 350CF A5302 340B350 ISP - FLT 5153 - AVIONIC SMOKE MASTER WARNING ACTIVATED. COULD NOT DUPLICATE DISCREPANCY. REMOVED AND REPLACED AVIONIC S RACK SMOKE DETECTOR FOR SUSPECTED INTERMITTENT FALSE WARNING. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000021200522 20000212 00522 EU 2000 2 12 SIMA993431 1 19991209 A 3350 702632 SIGN SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AE 340B319 DFW - FLT 3410 - EMERGENCY EXIT SIGN ABOVE SEAT 8A IS LOOSE. RESECURED EXIT SIGN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000021200523 20000212 00523 SO 2000 2 12 SIMA993421 1 19991208 A 2520 12108301 SET SCREWS EMB 145 EMB145 SO SEAT 18 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AE 145073 XNA - PASSENGER SEAT 18BC FORWARD LOCK DOWN SET SCREWS DAMAGED. REMOVED AND REPLACED SET SCREWS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000021200524 20000212 00524 EU 2000 2 12 SIMA993411 1 19991207 A 3350 2LA00511500 SOCKET SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 268AE 340B268 JFK - FLT 5140 - EMERGENCY LIGHT ABOVE SEAT 7A DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT SOCKET. OPERA TIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000021200525 20000212 00525 SO 2000 2 12 SIMA993393 1 19991205 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 630AE 05916 145132 DFW - FLT 3603 - AFTER TAKEOFF, BAGGAGE SMOKE INDICATION CAME ON. CREW DISCHARGED BOTH FIRE EXTINGUISHERS. DECLARED AN EMERGENCY AND RETURNED TO DFW. VERIFIED EVENT AS FALSE WARNING AND DEFERRED BAGGAGE SMOKE DETECTION SYSTEM AND FIRE EX TINGUISHER SYSTE. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED FORWARD BAGGAGE SMOKE DETECTOR. MEL WAS RESTORED AND THE AIRCRAFT WAS AGAIN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2000021200526 20000212 00526 EU 2000 2 12 SIMA35510 1 19991218 A 3350 GE85 LAMP SAAB SF340 340B 7860101 EU COCKPIT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 202KD 340B202 DFW - FLT 3252 - EMERGENCY ARMED LIGHT ON F/A PANEL INOPERATIVE. REMOVED AND REPLACED LAMP ON F/A PANEL. OPS CHECK GOO D. (M) 2 L 7 2 4T RT A52EU 2000021200527 20000212 00527 EU 2000 2 12 SIMA3559 1 19991219 A 3350 GE85 LAMP SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 204NE 340B204 DFW - FLT 3752 - EMERGENCY ARMED LIGHT ON F/A PANEL INOPERATIVE. REMOVED AND REPLACED LAMP ON F/A PANEL. OPS CHECK GOO D.. (M) 2 L 7 2 4T RT A52EU 2000021200528 20000212 00528 SO 2000 2 12 SIMA3557 1 19991217 A 2611 SMOKE DETECTOR EMB 145 EMB145LR SO LAVATORY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 630AE 145132 GRR - FLT 4152 - LAVATORY SMOKE INDICATION CAME ON AFTER TAKEOFF AND WENT OUT 1 MINUTE LATER. CREW DECLARED AN EMERGENC Y AND RETURNED TO GRR. NO EVIDENCE OF SMOKE OR BURNING. PERFORMED OPS CHECK OF SYSTEM, SYSTEM FOUND GOOD. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2000021200529 20000212 00529 NM 2000 2 12 F3LA99141 1 19991026 A 5330 SKIN BOEING 737 7372P6 NM BS 344/360 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 1PC 21613 DEN - DURING C-7 CHECK, INSPECTION REPORTED CORROSION IN LOWER LOBE OF E/E COMPARTMENT, BETWEEN BS 344 AND 360, STRINGER 28L TO 28R. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED DAMAGED AREA PER EA NR 53-737-049, SRM 51-40-3, SRM 51-10-6, SRM 53-10-2, SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 2000021200530 20000212 00530 EU 2000 2 12 SIMA3556 1 19991219 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 5 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 241AE 340B241 JFK - FLT 5030 - ROW R EMERGENCY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED BULB AT 5BC FLOOR LIGHT. OPS CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 2000021200531 20000212 00531 EU 2000 2 12 SIMA3553 1 19991220 A 2460 A2043C PDU SAAB SF340 340B 7860101 EU RIGHT FAILED A SIMA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 21 201AE CJ95644 340B201 JFK - FLT 5106 - RIGHT MAIN BUS FAILED IN FLIGHT. AUTO PILOT DISCONNECTED AND F/O EFIS FAILED. RESET ITSELF. 3 TO 5 M INUTES LATER FAILED AGAIN. DECLARED EMERGENCY, LANDED UNEVENTFUL. REMOVED AND REPLACED RIGHT PDU. OPS CHECK GOOD. (M ) 2 L 7 2 4T RT A52EU 2000021200532 20000212 00532 EU 2000 2 12 SIMA3552 1 19991220 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 268AE 17702 340B268 DCA - FLT 5157 - EMERGENCY LIGHTS OVER AFT WINDOW EXITS AND LIGHTS OVER SEATS 6AB TO 9B AND FLOOR LIGHTS INOPERATIVE. R EMOVED AND REPLACED POWER SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2000021200533 20000212 00533 EU 2000 2 12 SIMA35511 1 19991221 A 3320 6500111 CONNECTORS SAAB SF340 340B 7860101 EU ROWS 5/6 FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 382AE 340B382 AMA - FLT 3652 - ELECTRICAL SMOKE COMING OUT OF OVERHEAD AREA AT ROWS 5 AND ROWS 6 ON RIGHT SIDE AFT CABIN. FOUND BURNE D LIGHT SOCKET ON ROW 5 FLOURESCENT LIGHT. REMOVED AND REPLACED CONNECTOR AND LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2000021200534 20000212 00534 CE 2000 2 12 2000ZZZM90 1 19991123 A 5260 5044003713 ANCHOR BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 846CA 229 UE49 AIRSTAIR DOOR, FORWARD TOP CABLE ANCHOR BROKEN. REPLACED ANCHOR WITH NEW PART MANUFACTURED FROM WRONG MATERIAL. (M) 2 L 7 2 4T RT A24CE 2000021200535 20000212 00535 CE 2000 2 12 2000ZZZM91 1 19991122 A 3251 11438801817 ACTUATOR BEECH 1900 1900D 1154162 CE NLG STEERING LEAKING A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 836CA DD0313 UE32 NOSE WHEEL STEERING ACTUATOR LEAKS FLUID. REPLACED STEERING ACTUATOR. (M) 2 L 7 2 4T RT A24CE 2000021200536 20000212 00536 CE 2000 2 12 2000ZZZM92 1 19991123 A 3251 11438801817 ACTUATOR BEECH 1900 1900D 1154162 CE NLG STEERING BINDING A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 833CA DD0333 UE24 NOSE WHEEL STEERING FAILS TO TURN FREE IN POWER OR CASTOR MODES. STEERING ACTUATOR REPLACED. (M) 2 L 7 2 4T RT A24CE 2000021200537 20000212 00537 NE 2000 2 12 2000ZZZM93 3 19991122 A 6111 BLADE BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3I NE LT ENGINE LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 855CA UE61 HJ59A LEFT PROPELLER BLADE MOVEMENT OUTSIDE ALOOWABLE LIMITS IN HARTZELL SERVICE INSTRUCTIONS. PROPELLER REMOVED AND REPLACED . (M) 2 L 7 2 4T RT A24CE 5 C P10NE 2000021200538 20000212 00538 CE 2000 2 12 2000ZZZM94 1 19991129 A 2822 1143890425 PUMP BEECH 1900 1900D 1154162 CE LT ENGINE LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 842CA B823 UE41 LEFT ENGINE LOW PRESSURE FUEL PUMP LEAKING. UNIT REPLACED. (M) 2 L 7 2 4T RT A24CE 2000021200539 20000212 00539 CE 2000 2 12 2000ZZZM95 1 19991129 A 2822 1143890425 PUMP BEECH 1900 1900D 1154162 CE RT ENGINE LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 842CA B1156 UE41 RIGHT ENGINE LOWER PRESSURE FUEL PUMP LEAKING. UNIT REPLACED. (M) 2 L 7 2 4T RT A24CE 2000021200540 20000212 00540 SO 2000 2 12 ASOA99159 1 19991126 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 258AS 18410 120131 DURING INSPECTION, EMERGENCY BATTERY PACK FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTE RY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000021200541 20000212 00541 SO 2000 2 12 ASOA99158 1 19991124 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 229AS 19008 120042 DURING INSPECTION, FOUND EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PAC K. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000021200542 20000212 00542 SO 2000 2 12 ASOA99156 1 19991120 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 233AS 23978 120031 DURING INSPECTION, FOUND NR 2 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY B ATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000021200543 20000212 00543 NE 2000 2 12 A6WA9900127 2 19991203 A 7260 3037223 CARBON SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RT ENGINE FAILED A A6WA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 336PH 3014 FLT 7092 - COD-DEN - RIGHT ENGINE OIL PRESSURE DROPPED TO 40 PSI EN ROUTE, PERFORMED ENGINE SHUTDOWN. REMOVED AND REPLA CED ACCESSORY GEARBOX BREATHER CARBON SEAL. (M) 2 H 7 2 4T 4 T RT A45NM E20NE 2000021200544 20000212 00544 NE 2000 2 12 A6WA9900126 2 19991203 A 7260 3037223 CARBON SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE NR 2 ENGINE FAILED A A6WA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 335PH 3013 FLT 7081 - DEN-GUC - CREW REPORTED FLUCTUATING OIL PRESSURE ON NR 2 ENGINE, SHUTDOWN ENGINE AT 40 PSI, RETURNED DEN. RE MOVED AND REPLACED ACCESSORY GEARBOX BREATHER CARBON. (M) 2 H 7 2 4T 4 T RT A45NM E20NE 2000021200545 20000212 00545 EU 2000 2 12 A6WA9900133 1 19991116 A 5320 STIFFENER BAG BAE146 BAE146200A 1500266 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 183US E2043 HYDRAULICS BAY FRAME 29 HAS 4 VERTICAL STIFFENERS CRACKED. NUMBERS 4/5 ON LEFT SIDE AND 4/5 ON RIGHT SIDE. REPAIRED ST IFFENERS ON FRAME 29 AT LEFT AND RIGHT STATIONS 25.94 AND 31.13 IAW AIR WISCONSIN EO E95/003/653 ORIGINAL ISSUE. (M) 2 H 7 4 4F RT A49EU 2000021200546 20000212 00546 EU 2000 2 12 A6WA9900132 1 19991115 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FRAME 14-15 OIL CAN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 183US E2043 BELLY SKIN IS QUILTED AND CANNING AT FRAME 14-15 JUST TO THE RIGHT SIDE OF THE CENTER LINE. REPAIRED IAW FAX REF NR BAR A/AVR/4610/99 AND BARA/AVR/3409/99. (M) 2 H 7 4 4F RT A49EU 2000021200547 20000212 00547 EU 2000 2 12 A6WA9900130 1 19991102 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 183US E2043 RIGHT WING 10 INCHES INBOARD OF RIB 9, TOP WING SKIN STIFFENER IS CRACKED AT FORWARD END. REMOVED, REPAIRED AND INSTALL ED TOP WIN STIFFENER. REPAIR ACCOMPLISHED IAW BAE FAX-REF DJR/RJ0630-98. (M) 2 H 7 4 4F RT A49EU 2000021200548 20000212 00548 EU 2000 2 12 A6WA9900131 1 19991104 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 183US E2043 LEFT WING 10 INCHES INBOARD OF RIB 8, TOP WING SKIN STIFFENER IS CRACKED AT FORWARD END. REMOVED, REPAIRED AND INSTALLE D SAID STIFFENER. REPAIRED STIFFENER IAW BAE FAX DJR/RJ0630-98 AND FOUND SERVICEABLE. (M) 2 H 7 4 4F RT A49EU 2000021200549 20000212 00549 EU 2000 2 12 A6WA9900129 1 19991118 A 5320 DIAPHRAM BAG BAE146 BAE146200A 1500266 EU FUSELAGE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 183US CRACKED E2043 NLG LEFT SIDEWALL DIAPHRAM HAS SEVERAL CRACKS IN BORE FOR RETRACTION RAM ATTACH PIN, PER BAE FAX NLJ/RJ/1603-99. THIS S IDEWALL MAY CONTINUE IN SERVICE FOR 120 CYCLES WITH A DV INSPECTION AT 60 CYCLES FROM NOW, DUE REPLACEMENT AT THE END OF 120 CYCLES. DV AT 23920. REPLACED AT 23,980. (M) 2 H 7 4 4F RT A49EU 2000021200550 20000212 00550 EU 2000 2 12 A6WA9900128 1 19991201 A 3240 BRAKE BAG BAE146 BAE146200A 1500266 EU MLG FAILED A A A6WA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 606AW E2033 FLT 5545 - ORD-MLI - AFTER CHOCKS WERE PULLED. AIRCRAFT STARTED ROLLING FORWARD, BRAKING DID NOT STOP AIRCRAFT. AIRCRA FT HIT TERMINAL BLDG. AIRCRAFT REMOVED FROM SERVICE FOR REPAIR. (M) 2 H 7 4 4F RT A49EU 2000021200551 20000212 00551 NM 2000 2 12 AALA991743 1 19991118 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 644AA 24602 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2000021200552 20000212 00552 NM 2000 2 12 USAA991435 1 19991209 A 5330 SKIN BOEING 737 737301 1384611 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 41883 23228 PIT - DURING RON VISIT, FOUND 1.0625 INCH LONG CRACK ON FUSELAGE SKIN AT RT SIDE, STATION 767 STRINGER 22 TO 23 RT. REM OVED CRACK WITH CUTOUT. INSTALLING EXTERNAL DOUBLER PER SRM 53-00-00-01, FIG 201, EA 53528. (M) 2 L 7 2 4F RT A16WE 2000021200553 20000212 00553 NM 2000 2 12 USAA991425 1 19991218 A 5210 SKIN BOEING 737 7374B7 1384702 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 429US 30082 24551 TPA - DURING AC-5 CHECK VISUAL INSPECTION, FOUND THE DOOR SKIN BENT AND CRACKED JUST ABOVE LOWER HINGE CUTOUT. REPAIRED PER EA 66130. (M) 2 L 7 2 4F RT A16WE 2000021200554 20000212 00554 NM 2000 2 12 USAA991412 1 19991215 A 5511 SPAR BOEING 737 737401 1384701 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK RIGHT HORIZONTAL STAB 1.25 INCH FORWARD OF AFT SPAR BET WEEN STAB STATION 96 AND 97.5. INSTALLED DOUBLER PER SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 2000021200555 20000212 00555 NM 2000 2 12 USAA991411 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK BETWEEN STRINGER 8R AND 9R FRAME 380 FRAME. INSTALLE D DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200556 20000212 00556 NM 2000 2 12 USAA991392 1 19991215 A 5720 FITTING BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 44382 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LEFT WING INBOARD TOP SIDE OF SUPPORT FRAME. REMOVED F ASTENERS, NDT, REINSTALL PER TR 57-40-13 AND MM 28-22-15. (M) 2 L 7 2 4F RT A16WE 2000021200557 20000212 00557 NM 2000 2 12 USAA991382 1 19991215 A 5720 FITTING BOEING 737 737401 1384701 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 44382 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK RIGHT WING INBOARD TOP SIDE OF SUPPORT FRAME. REMOVED FASTENERS, NDT, REINSTALL PER TR 57-40-13 AND MM 28-22-15. (M) 2 L 7 2 4F RT A16WE 2000021200558 20000212 00558 NM 2000 2 12 USAA991379 1 19991215 A 5414 SKIN BOEING 737 737401 1384701 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 44382 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK TOP FORWARD CORNER OF ACCESS DOOR 5724L CUTOUT SKIN. IN STALLED DOUBLER PER TR 54-50-040. (M) 2 L 7 2 4F RT A16WE 2000021200559 20000212 00559 NM 2000 2 12 USAA991368 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK BETWEEN STRINGER 8R AND 9R FRAME 400 INBOARD RIVET.. INSTALLED DOUBLE PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200560 20000212 00560 NM 2000 2 12 USAA991367 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS BETWEEN STRINGER 8R AND 9R FRAME 747 INBOARD RIVET. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200561 20000212 00561 NM 2000 2 12 USAA991366 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKS BETWEEN STRINGER 8R AND 9R FRAME 787 INBOARD RIVET . INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200562 20000212 00562 NM 2000 2 12 USAA991365 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .375 INCH CRACKS BETWEEN STRINGER 8R AND 9R FRAME 907 INBOARD RIVET. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200563 20000212 00563 NM 2000 2 12 USAA991364 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 747 INBOARD RIVET. INS TALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200564 20000212 00564 NM 2000 2 12 USAA991363 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 400 INBOARD RIVET. INS TALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2000021200565 20000212 00565 NM 2000 2 12 USAA991362 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 400 OUTBOARD RIVET. I NSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2000021200566 20000212 00566 NM 2000 2 12 USAA991361 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 440 INBOARD RIVET. INS TALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200567 20000212 00567 NM 2000 2 12 USAA991348 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKS BETWEEN STRINGER 8R AND 9R FRAME 867 INBOARD RIVET . INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200568 20000212 00568 NM 2000 2 12 USAA991357 1 19991215 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 328-344.17 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION TWO 10 INCH AREAS AT FORWARD STATION 328 TO FORWARD STATION 34 4.17, CHORD ANGLE. CORROSION LEVEL 1. BLENDED WITHIN SRM 53-10-51 LIMITS. (M) 2 L 7 2 4F RT A16WE 2000021200569 20000212 00569 NM 2000 2 12 USAA991356 1 19991215 A 5320 ANGLE BOEING 737 737401 1384701 NM BS 294.5/328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION TWO 15 INCH AREAS AT RT CREASEBEAM INNER CHORD STATION 294.5 T O 328 CHORD ANGLE. CORROSION LEVEL 1. REMOVED CORROSION PER 53-10-51 AND 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000021200570 20000212 00570 NM 2000 2 12 USAA991355 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 787 INBOARD RIVET. IN STALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200571 20000212 00571 NM 2000 2 12 USAA991354 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 827 INBOARD RIVET.. INSTALLED DOUBLER PER TR 52-00-01. (M) 2 L 7 2 4F RT A16WE 2000021200572 20000212 00572 NM 2000 2 12 USAA991353 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 867 INBOARD RIVET.. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200573 20000212 00573 NM 2000 2 12 USAA991352 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK BETWEEN STRINGER 8R AND 9R FRAME 440 INBOARD RIVET.. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200574 20000212 00574 NM 2000 2 12 USAA991351 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND FOUR .375 INCH CRACKS BETWEEN STRINGER 8R AND 9R FRAME 480 INBOARD RIVET . INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200575 20000212 00575 NM 2000 2 12 USAA991350 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 480 INBOARD RIVET.. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200576 20000212 00576 NM 2000 2 12 USAA991349 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 907 INBOARD RIVET. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021200577 20000212 00577 NM 2000 2 12 USAASB99304 1 19991227 A 2751 2061141 INDICATOR BOEING 737 7374B7 1384702 NM COCKPIT FAILED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 438US 32750 24560 PHL - FLT 1424 - FLIGHT WAS ON APPROACH TO PHL AND AS THE CAPTAIN EXTENDED THE FLAPS/SLATS, THE SLATS OPERATED NORMALLY BUT THE FLAPS WOULD NOT EXTEND. CAPTAIN PUT THE FIGHT IN A HOLD PATTERN AND WENT THROUGH PROCEDURES. FLAPS STILL WOULD NOT EXTEND. CAPTAIN DECLARED AN EMERGENCY AND ADVISED PASSENGERS THE LANDING WOULD BE A LITTLE FASTER THAN NORMAL. FL IGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2000021200578 20000212 00578 NM 2000 2 12 USAASB99302 1 19991225 A 3230 BOEING 737 7374B7 1384702 NM UNKNOWN A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 435US 24557 PIT - FLT 744 - UPON LOWERING GEAR HANDLE, THE NOSE GEAR RED LIGHT ILLUMINATED WITH NO OTHER RED OR GREEN GEAR LIGHT IND ICATIONS. CREW COULD NOT ARM AUTO-BRAKES AND GEAR HORN SOUNDED CONSTANT WITH FLAPS ABOVE 15 DEGREES. CREW ACCOMP A MAN UAL GEAR EXTENSION AND VISUAL CHECK OF THE GEAR PER QUICK REFERENCE HANDBOOK MANUAL. TWO FLYBYS WERE ALSO PERFORMED TO CONFIRM GEAR WAS DOWN. PACKED TRIPPED UPON LANDING AT PIT, FLIGHT LANDED WITHOUT INCIDENT. MX MET THE FLT ON THE RUNWA Y, PINNED THE GEAR AND TOWED THE AIRCRAFT TO THE GATE. AN EMERGENCY WAS DECLARED. MX FOUND THE LANDING GEAR AIR/GROUND RELAY AND LIGHTS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND CYCLED GEAR SEVERAL TIMES. LANDING GEAR AND GEAR L 2 L 7 2 4F RT A16WE 2000021200579 20000212 00579 NM 2000 2 12 USAASB99301 1 19991223 A 2120 UNKNOWN BOEING 737 737301 1384611 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 355US 23558 MCO - FLT 2152 - 20 MINUTES AFTER T/O FROM RSW, UNIDENTIFIED FUMES WERE RECOGNIZED IN THE AFT GALLEY. CREW TURNED OFF G ALLEY POWER SWITCH AND PULLED ALL CIRCUIT BREAKERS IN THE GALLEY. NO SMOKE WAS PRESENT BUT FUMES BECAME STRONGER. CREW DECLARED EMERGENCY AND THE FLIGHT DIVERTED TO MCO. FLT LANDED WITHOUT INCIDENT. MX FOUND THE FOUL ODOR IN THE FORWARD CARGO COMPT TO BE COMING FROM A CARDBOARD BOX CONTAINING CHINCHILLAS. CONTENTS WERE REMOVED AND THE ODOR DISSIPATED. I NSPECTED OTHER AIRCRAFT COMPARTMENTS. RAN APU, ENGINES AND AIR CONDITIONING PACKS AT VARIOUS POWER SETTINGS. RESET CIR CUIT BREAKERS AND OPERATIONALLY CHECKED ALL COFFEE MAKERS. NO FUMES OR ODORS DETECTED. (M) 2 L 7 2 4F RT A16WE 2000021200580 20000212 00580 NM 2000 2 12 USAASB99299 1 19991220 A 5230 SEAL BOEING 737 7373B7 1384580 NM CARGO DOOR LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 376US 22955 CLT - FLT 703 - ON CLIMB-OUT FROM CLT, AT APPROXIMATELY FL240, FLIGHT LOST PRESSURIZATION. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED CABIN PRESSURE LEAKAGE TEST. FOUND EXCESSIVE LEAKAGE AT FORWARD CARGO DOOR FORWARD LOWER CORNER. FOUND PRESSURE SEAL (APPROX A 12 INCH SECTION) NO T SECURED IN RETAINER. REINSTALLED SEAL AND SECURED. PERFORMED LEAKAGE TEST AGAIN AND FOUND TO BE WITHIN LIMITS. (M) 2 L 7 2 4F RT A16WE 2000021200581 20000212 00581 NM 2000 2 12 USAASB99298 1 19991220 A 2751 2061141 INDICATOR BOEING 737 737401 1384701 NM COCKPIT FAILED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 421US 14864 23988 BDL - FLT 2232 - ON APPROACH TO BDL, UPON SELECTING FLAPS 5, THE FLAPS STOPPED WITH RIGHT INDICATING 1 AND LEFT INDICATI NG 2. FLAPS WOULD NOT RETRACT. CREW EXECUTED A MISSED APPROACH. ON THE GO-AROUND, THE FLAPS WERE CYCLED AND THE CREW DEPLOYED FLAPS 1 FOR THE LANDING. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT BDL. NO EMERGENCY WAS DECLARED. MAINTENAN CE INSPECTED FLAPS AND FOUND BOTH FLAPS AT 1 UNIT. RAN FLAPS UP ELECTRICALLY. REMOVED AND REPLACED FLAP POSITION INDIC ATOR. OPERATIONAL CHECK GOOD. INSPECTED TIRES AND BRAKES PER MM 05-51-07 AND FOUND NORMAL. (M) 2 L 7 2 4F RT A16WE 2000021200582 20000212 00582 WP 2000 2 12 USAAD99182 1 19991223 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DISCHARGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 816US 48096 CLT - FLT 2280 - THE NOSE GEAR WOULD NOT RETRACT. UPON RECYCLING THE GEAR A SECOND TIME, WITHOUT SUCCESS, THE FLIGHT RE TURNED TO THE FIELD. MAINTENANCE SERVICED THE NOSE STRUT. SWUNG GEAR SEVERAL TIMES, OPS CHECKED OK. (M) 2 L 7 2 4F A6WE 2000021200583 20000212 00583 2000 2 12 USAAD99183 4 19991226 A 2565 11331780 SLIDE DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 39343 47508 ATL - FOUND FORWARD ENTRY DOOR ESCAPE SLIDE PRESSURE BELOW MINIMUMS. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. ( M) 2 L 7 2 4F A6WE 2000021200584 20000212 00584 WP 2000 2 12 USAA991456 1 19991219 A 5320 3924809503 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913VJ 74376 45846 PIT - DURING SHEET METAL REPAIR OPEN UP, FOUND 4 INCH CRACK AND 1.5 INCH BY 2 INCH CORRODED AREA (INTERGRANUAR) AT LONGE RON 30 AFT END FORWARD CARGO AT T-CAP. REPLACED WITH IDENTICAL PART NUMBER. (M) 2 L 7 2 4F A6WE 2000021200585 20000212 00585 WP 2000 2 12 USAA991457 1 19991219 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 579-604 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913VJ 74376 45846 PIT - DURING VISUAL (RON CHECK) FOUND CORROSION ON, UNDER AND AROUND PREVIOUS REPAIR (5 INCH BY 7 INCH) ON SKIN ON DOUBL ER AT STATION 579-604 LONGERON 28L TO 28R. CORROSION LEVEL 2. REPLACED REPAIR DOUBLERS WITH NEW, REMOVED CORROSION PER SRM 53-04 FIG 43 SHEET 6. (M) 2 L 7 2 4F A6WE 2000021200586 20000212 00586 WP 2000 2 12 USAA991458 1 19991219 A 5330 5911412 SKIN DOUG DC9 DC931 3022065 WP BS 230-579 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913VJ 74376 45846 PIT - DURING RON, FOUND NUMEROUS AREAS AFFECTED OVER LISTED SKIN AREA CORROSION ALONG FRAMES, LONGERONS AND AT ANTENNA D OUBLERS AT STATION 230 TO STATION 579, LONGERON 26L TO LONGERON 26R. CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH I DENTICAL PART NR. (M) 2 L 7 2 4F A6WE 2000021200587 20000212 00587 2000 2 12 USAASB99294 4 19991215 A 2210 4030952902 COUPLER BOEING 737 737201 1384454 NM E/E BAY FAILED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 245US 32596 22751 BWI - FLT 2674 - EN ROUTE FROM TPA TO BOS, AT FL230, A/C ENCOUNTERED SOME LIGHT CHOP AND STARTED TO OSCILLATE. YAW DAMP ER APPEARED NORMAL WITH NO LIGHT INDICATIONS. AIRCRAFT CONTINUED TO OSCILLATE. CAPT LEVELED FLT AT FL310 AND TURNED YA W DAMPER OFF. NO CHANGE. TURNED BACK ON AND STILL NO CHANGE. FLEW WITH YAW DAMPER SWITCH OFF.. ENCOUNTERED LIGHT CHO P AGAIN. BASED ON FORECAST FOR TURBULENCE AND WEATHER, CAPT DECIDED TO DIVERT TO BWI. FLT LANDED WITHOUT FURTHER INCID ENT. NO EMERGENCY WAS DECLARED. MX FOUND THE YAW DAMP COUPER HARD FAILED. REMOVED AND REPLACED YAW DAMP COUPLER. FUN CTIONAL CHECK FOUND SATISFACTORY. (M) 2 L 7 2 4F A16WE 2000021200588 20000212 00588 NM 2000 2 12 USAA991332 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 807 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021200589 20000212 00589 NM 2000 2 12 USAA991331 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 9L STATION 787 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021200590 20000212 00590 NM 2000 2 12 USAA991330 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 6R STATION 767 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021200738 20000212 00738 WP 2000 2 12 RRAX991706 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=880 TO Y=900. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FA A APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200741 20000212 00741 WP 2000 2 12 RRXA991683 1 19990905 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, UPPER SURFACE SKIN BETWEEN XFS=20 TO XFS=3 8.750. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INS TALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200742 20000212 00742 WP 2000 2 12 RRXA991684 1 19990719 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 857 - 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL SKIN BETWEEN Y=857 TO Y=980 AND LONGERON 36. REMOVED DAMA GE SKIN, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED NEW SKIN PANEL IAW DC-8 SRM 53-3-0. 2 L 7 4 4F RT 4A25 2000021200743 20000212 00743 WP 2000 2 12 RRXA991685 1 19990906 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FORWARD PRESSURE PANEL BETWEEN Y=-52 TO Y=-12 AND Z=-8. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER IAW FAA APPROVED DER ENGINEERING SKETCH EO=99-109. 2 L 7 4 4F RT 4A25 2000021200744 20000212 00744 WP 2000 2 12 RRXA991686 1 19990617 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BULKHEAD MOUNT AT Y=1360 BETWEEN LONGERONS 34 LEFT TO 34 RIGHT. DA MAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED MOUNT, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED NEW MOUNT IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2000021200745 20000212 00745 WP 2000 2 12 RRXA991687 1 19990712 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME AT Y=1320 AND LONGERON 27 LEFT. DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED FRAME, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOO R SUPPORT FRAME IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2000021200746 20000212 00746 WP 2000 2 12 RRXA991688 1 19990615 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM UPPER SURFACE AT Y=1700 BETWEEN LONGERONS 21 LEFT TO 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2000021200747 20000212 00747 WP 2000 2 12 RRXA991689 1 19990615 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1745 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL AT Y=1745 AND X=-10. DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNE L IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000021200748 20000212 00748 WP 2000 2 12 RRXA991690 1 19990615 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1766 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL AT Y=1766 AND X=-10. DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNE L IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000021200749 20000212 00749 WP 2000 2 12 RRXA991691 1 19990615 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1745 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL BETWEEN Y=1745 TO Y=1766 AND LONGER ON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AN D INSTALLED NEW HAT CHANNEL IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000021200750 20000212 00750 WP 2000 2 12 RRXA991692 1 19990615 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1766 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT BEAM HAT CHANNEL BETWEEN AT Y=1766 AND LONGERON 35 RI GHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED NEW HAT CHANNEL IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2000021200751 20000212 00751 WP 2000 2 12 RRXA991693 1 19990614 A 5210 DOUBLER DOUG DC8 DC873F 302199F WP PAX DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING FOUND CORROSION DAMAGE TO L-1 DOOR WINDOW EXTERNAL DOUBLER AT Y=160 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGED DOUBLER, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW DC-8 SRM 51-1-20 . 2 L 7 4 4F RT 4A25 2000021200752 20000212 00752 WP 2000 2 12 RRXA991694 1 19990624 A 5230 ANGLE DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO DOOR, SEAL ATTACHMENT ANGLE BETWEEN SPOOLS 2 AND 3 AND BET WEEN Y=160 TO Y=180. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8 . RECEIVED NEW ATTACHMENT ANGLE AND INSTALLED IAW DC-8 SRM 53-1-0. 2 L 7 4 4F RT 4A25 2000021200753 20000212 00753 WP 2000 2 12 RRXA991695 1 19990624 A 5230 ANGLE DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO DOOR, SEAL ATTACHMENT ANGLE BETWEEN Y=213 TO Y=240. DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ATTACHMENT ANGLE AND INSTALLED IAW DC-8 SRM 53-1-0. 2 L 7 4 4F RT 4A25 2000021200754 20000212 00754 WP 2000 2 12 RRXA991696 1 19990824 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP BS 940 - 960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN Y=940 TO Y=960 AND BETWEEN X=0 TO X=-6 AND Z =-8. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED REPAIR FINGER DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200755 20000212 00755 WP 2000 2 12 RRXA991697 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 95 - 110 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E BETWEEN Y=95 TO Y=110 AND BETWEEN X=-27 TO X=30 . DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200756 20000212 00756 WP 2000 2 12 RRXA991698 1 19990727 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 280 - 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E BETWEEN Y=280 TO Y=580 AND X=45. DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLE R IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200757 20000212 00757 WP 2000 2 12 RRXA991699 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 329 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E AT Y=329 AND X=-50. DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APP ROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200758 20000212 00758 WP 2000 2 12 RRXA991700 1 19990624 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 AT Y=360 BETWEEN X=16 TO X=24. DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLE R IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200759 20000212 00759 WP 2000 2 12 RRXA991701 1 19990612 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 409 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=409 TO Y=417 AND LONGERON 21 LEFT. DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPA IR DOUBLER IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000021200760 20000212 00760 WP 2000 2 12 RRXA991702 1 19990629 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 435 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL AT Y=435 BETWEEN X=16 TO X=24. DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200761 20000212 00761 WP 2000 2 12 RRXA991703 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-2 BETWEEN Y=580 TO Y=435 AND X=24. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200762 20000212 00762 WP 2000 2 12 RRXA991704 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 584 - 600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=584 TO Y=600. DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA AP PROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200763 20000212 00763 WP 2000 2 12 RRXA991705 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 760 - 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=760 TO Y=1000 AND X=15. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200764 20000212 00764 WP 2000 2 12 RRXA991706 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 813 - 990 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=813 TO Y=990. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FA A APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200765 20000212 00765 WP 2000 2 12 RRXA991708 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 900 - 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-1 BETWEEN Y=900 TO Y=920. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW F AA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200766 20000212 00766 WP 2000 2 12 RRXA991709 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 907 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D AT Y=907 AND X=-15. DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPR OVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200767 20000212 00767 WP 2000 2 12 RRXA991710 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 960 - 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=960 TO Y=1000. DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200768 20000212 00768 WP 2000 2 12 RRXA991711 1 19990716 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 940 - 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-3 BETWEEN Y=940 TO Y=980 AND X=50. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200769 20000212 00769 WP 2000 2 12 RRXA991712 1 19990720 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 949 - 952 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=949 TO Y=952 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200770 20000212 00770 WP 2000 2 12 RRXA991713 1 19990720 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 968 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=968 TO Y=973 AND BETWEEN X=45 TO X=59. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200771 20000212 00771 WP 2000 2 12 RRXA991714 1 19990629 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 AND X=15. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200772 20000212 00772 WP 2000 2 12 RRXA991715 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1020 - 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-1 BETWEEN Y=1020 TO Y=1040. DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200773 20000212 00773 WP 2000 2 12 RRXA991716 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1300 - 1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=1300 TO Y=1580. DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200774 20000212 00774 WP 2000 2 12 RRXA991717 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1330 - 1500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-2 BETWEEN Y=1330 TO Y=1500 AND X=30. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200775 20000212 00775 WP 2000 2 12 RRXA991718 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1357 - 1360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1357 TO Y=1360 AND BETWEEN X=0 TO X =-8. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200776 20000212 00776 WP 2000 2 12 RRXA991719 1 19990828 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1500 - 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1500 TO Y=1540. DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200777 20000212 00777 WP 2000 2 12 RRXA991720 1 19990827 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-2 AT Y=1560. DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DE R ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200778 20000212 00778 WP 2000 2 12 RRXA991722 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1580 - 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-1 BETWEEN Y=1580 TO Y=1680 AND X=-5. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200779 20000212 00779 WP 2000 2 12 RRXA991723 1 19990727 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 280 - 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-1 BETWEEN Y=280 TO Y=580 AND X=30. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200780 20000212 00780 WP 2000 2 12 RRXA991724 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 280 - 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-1 BETWEEN Y=280 TO Y=580 AND X=-15. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200781 20000212 00781 WP 2000 2 12 RRXA991725 1 19990727 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 280 - 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=280 TO Y=580 AND X=40. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200782 20000212 00782 WP 2000 2 12 RRXA991726 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 280 - 580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=280 TO Y=580 AND X=50. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200783 20000212 00783 WP 2000 2 12 RRXA991727 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 580 - 880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-1 BETWEEN Y=580 TO Y=880. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW F AA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200784 20000212 00784 WP 2000 2 12 RRXA991728 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 580 - 880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 BETWEEN Y=580 TO Y=880 AND X=-15. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM.REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200785 20000212 00785 WP 2000 2 12 RRXA991729 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 580 - 880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=580 TO Y=880. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FA A APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200786 20000212 00786 WP 2000 2 12 RRXA991730 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 880 - 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-1 BETWEEN Y=880 TO Y=1000 AND X=-15. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200787 20000212 00787 WP 2000 2 12 RRXA991731 1 19990629 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 AND X=-10. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200788 20000212 00788 WP 2000 2 12 RRXA991732 1 19990629 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 AND X=-15. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200789 20000212 00789 WP 2000 2 12 RRXA991733 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-2 BETWEEN Y=1000 TO Y=1300 AND X=40. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200790 20000212 00790 WP 2000 2 12 RRXA991734 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=1000 TO Y=1300 AND X=40. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200791 20000212 00791 WP 2000 2 12 RRXA991735 1 19990712 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-1 BETWEEN Y=1000 TO Y=1300 AND X=15. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200792 20000212 00792 WP 2000 2 12 RRXA991736 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL F BETWEEN Y=1000 TO Y=1300 AND X=-50. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200793 20000212 00793 WP 2000 2 12 RRXA991737 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=1000 TO Y=1300 AND X=-30. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200794 20000212 00794 WP 2000 2 12 RRXA991738 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=1000 TO Y=1300 AND X=30. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200795 20000212 00795 WP 2000 2 12 RRXA991739 1 19990615 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=1000 TO Y=1300 AND X=50. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200796 20000212 00796 WP 2000 2 12 RRXA991740 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1000 - 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=1000 TO Y=1300 AND X=20. DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200797 20000212 00797 WP 2000 2 12 RRXA991741 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1300 - 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 BETWEEN Y=1300 TO Y=1680 AND X=-10. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200798 20000212 00798 WP 2000 2 12 RRXA991742 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1300 - 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-3 BETWEEN Y=1300 TO Y=1680 AND X=-20. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200799 20000212 00799 WP 2000 2 12 RRXA991744 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1300 - 1620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1620 AND X=50. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200800 20000212 00800 WP 2000 2 12 RRXA991745 1 19990614 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1300 - 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1680 AND X=-10. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200801 20000212 00801 WP 2000 2 12 RRXA991746 1 19990615 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1300 - 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1680 AND X=56. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200802 20000212 00802 WP 2000 2 12 RRXA991747 1 19990827 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1500 - 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-2 BETWEEN Y=1500 TO Y=1540 AND X=-10. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200803 20000212 00803 WP 2000 2 12 RRXA991748 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1580 - 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=1580 TO Y=1680 AND X=-24. DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200804 20000212 00804 WP 2000 2 12 RRXA991749 1 19990827 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 1580 - 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1580 TO Y=1680. DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021200805 20000212 00805 WP 2000 2 12 RRXA991750 1 19990621 A 5321 ANGLE DOUG DC8 DC873F 302199F WP BS 1766 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO VERTICAL STABILIZER FRONT SPAR ATTACHMENT ANGLE AT Y=1766 AND X=24. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2000021800001 20000218 00001 NM 2000 2 18 TSAA9933501 1 19991211 A 3350 8731002511 LIGHT BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2000021800002 20000218 00002 NM 2000 2 18 TSAA9933502 1 19991211 A 3350 87310025111 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED FORWARD ENTRY DOOR IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800003 20000218 00003 NM 2000 2 18 TSAA9933503 1 19991213 A 3350 963100211 LIGHT BOEING 737 7372S5C 1384499 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 2 POSITION FLOOR LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2000021800004 20000218 00004 2000 2 18 2000ZZZM87 4 19991120 A 2565 5917689 ANGLE 9915565521 DOUG DC9 DC932 3022066 WP PAX DOOR OUT OF ADJUST A A4JA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 35 12532 45791 AFTER ARRIVING AT SFB AIRPORT AND PRIOR TO THE DISEMBARKATION OF PASSENGERS AN INADVERTENT DEPLOYMENT OF THE L-1 DOOR SL IDE OCCURRED. THE FLT ATTENDANT HAD OPENED THE L1 DOOR AND SECURED THE DOOR IN THE OPEN POSITION WHEN THE SLIDE PACK CO VER FELL OFF. THIS CAUSED THE SLIDE DEPLOYMENT HANDLE TO CATCH ON THE DOOR AND DEPLOY. AN ADJUSTMENT WAS MADE TO THE S LIDE PACK COVER BRACKET AND A CONTINUED TIME SLIDE AND THE SLIDE PACK COVER WAS INSTALLED IAW 26-62-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2000021800005 20000218 00005 EU 2000 2 18 COEA9901702 1 19991209 A 5330 SKIN FOKKER F27 F27MK600 4990706 EU BS 19180 DENTED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 702FE 10350 LAS VEGAS - A/C WAS HIT BY A UPS CARGO CONTAINER WHILE THE AIRCRAFT WAS PARKED ON THE AIRPORT RAMP. THE CONTAINER WAS B LOWN ACROSS THE RAMP BY A HIGH WIND. STRUCTURAL DAMAGE OCCURRED TO THE REAR SECTION OF THE AIRCRAFT FUSELAGE. REMOVED AND REPLACED FRAME STATION 19180. REPAIRED SKIN DAMAGE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 2000021800006 20000218 00006 NM 2000 2 18 USAA991345 1 19991209 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 23938 27122 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND SEAT TRACK CORROSION AT STATION 377 AND LBL 47. CORROSION LEVEL 1. INS TALLED NEW SEAT TRACK PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2000021800007 20000218 00007 NM 2000 2 18 USAA991346 1 19991209 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 23938 27122 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND SEAT TRACK CORROSION AT STATION 377.0 AND LBL 24. CORROSION LEVEL 1. I NSTALLED NEW SEAT TRACK PER SRM 53-00-52. (M) 2 L 7 2 4F RT A2NM 2000021800008 20000218 00008 NM 2000 2 18 USAA991347 1 19991209 A 5320 BEAM BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 23938 27122 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION ON BEAM AT STATION 377.7, LBL 24 AND LBL 47 T-CAP. CORROSION LEVEL 2. INSTALLED NEW T-CAP PER TR 53-15-01 AND EA 66210. (M) 2 L 7 2 4F RT A2NM 2000021800009 20000218 00009 NM 2000 2 18 USAA991375 1 19991209 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 610AU 23938 27122 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY .5 INCH STATION 377, LBL 61 FLOORBEAM. CORROSION L EVEL 2. INSTALLED T-CAP PER TR 53-10-01 AND EA 66210. (M) 2 L 7 2 4F RT A2NM 2000021800010 20000218 00010 WP 2000 2 18 HALA9900274 1 19991219 A 3260 SENSOR DOUG DC9 DC951 3022051 WP MLG FAILED A HALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 13 709HA 47764 NOSE GEAR UNSAFE LIGHT ON FLYBY TOWER CONFIRMED. RECYCLED GEAR ALL GREEN. ELECT CHECK, REPLACED LOCK SENSOR. REPLACED NOSE GEAR BUNGEE CYL GEAR SWING. LEAK CHECK GOOD PER MM 32-32-7. (M) 2 L 7 2 4F RT A6WE 2000021800011 20000218 00011 NM 2000 2 18 MASA99177 1 19991115 A 5246 85321086059 DOOR DHAV DHC8 DHC8202 2809007 NM LAV SERVICE OPEN A MASA A UNSCHED LANDING W INADEQUATE Q C NR NOT REPORTED 1 SW 07 448YV 448 FLT 6542 - PHX-CLD - DURING FLIGHT THE CREW NOTICED A LOUD NOISE AS THE AIRCRAFT REDUCED SPEED THROUGH 230KN. THE CREW DECLARED AN EMERGENCY AND DID A FLYBY THE TOWER WHICH NOTED NOTHING WRONG. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT . DURING THE POST FLIGHT, THE CREW FOUND THE LAV SERVICE DOOR OPEN. MAINTENANCE INSPECTED AND FOUND NO DEFECTS AND SEC URED THE DOOR. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2000021800012 20000218 00012 NM 2000 2 18 P2EA99334 1 19991130 A 5240 INTERCOSTAL BOEING 737 737222 1384473 NM SERVICE DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - FORWARD SERVICE DOOR INTERCOSTAL CRACKED AT BEAM 3. ANGLE REPLACED PER SRM 51-10-1 PAGE 5, 51-30-2 PAGE 8. (M) 2 L 7 2 4F A16WE 2000021800013 20000218 00013 NM 2000 2 18 P2EA99343 1 19991210 A 2613 CONNECTOR BOEING 737 737244 138448U NM NR 1 ENGINE CONTAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 MSP - FLT 705 - DURING FLIGHT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED, THE SAME LIGHT REMAINED EXTINGUISHED AT REDUC ED THROTTLE SETTINGS. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO INCIDENT. CLEANED CANNON PLUG ON FIRE TEST UN IT AND FIRE PROTECTION BOX. ENGINE RUN PERFORMED AT 75 PERCENT N2, ALL INDICATIONS NORMAL PER MM CHAPTER 71. (M) 2 L 7 2 4F A16WE 2000021800014 20000218 00014 NM 2000 2 18 P2EA99340 1 19991209 A 5330 SKIN BOEING 737 737247 138448D NM BS 727A DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 ATL - DURING TRANSIT CHECK, FOUND MARK ON LEFT SIDE OF FUSELAGE, 5 WINDOWS AFT OF EMERGENCY EXIT, BS 727A, STRINGER 16L, WL 216. EDDY CURRENT PERFORMED TO VERIFY CRACK. REPAIRED IAW SRM 53-30-3. (M) 2 L 7 2 4F A16WE 2000021800015 20000218 00015 NM 2000 2 18 P2EA99342 1 19991203 A 5245 6548685115 SKIN BOEING 737 737281 138448P NM AC BAY DOOR DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, LEFT AC BAY DOOR DELAMINATED. REPAIRED LEFT AC BAY DOOR PER EO COO-CMP-3-53-704-99 DATED DECEMBER 4, 199 9. (M) 2 L 7 2 4F A16WE 2000021800016 20000218 00016 NM 2000 2 18 P2EA99339 1 19991129 A 5242 SKIN BOEING 737 737222 1384473 NM E/E DOOR SCRATCHED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - C-CHECK, E/E DOOR WITH DEEP SCRATCHES AND MISSING MATERIAL. DEFECT SIZE, LENGTH 1.125 INCH, WIDTH .250 INCH, DEPT H .040 INCH. REPLACED DOOR SKIN PER SRM 51-10-1 PAGE 5 AND PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000021800017 20000218 00017 NM 2000 2 18 P2EA99341 1 19991129 A 5330 SKIN BOEING 737 737222 1384473 NM BS 764-767 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - C-CHECK, FUSELAGE SKIN CRACK FROM BS 764 TO BS 767 BETWEEN STRINGER 18 AND 19 LEFT. DEFECT SIZE, LENGTH 3 INCH, W IDTH .032 INCH, DEPTH .028 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 759.5 TO BS 771, BETWEEN STRINGER 18 LT AND 20 LT PER COOPESA EO COO-3-53-702-99 DATED DECEMBER 2, 1999 AND BOEING FAX COO-SJO-99-00596H DATED DECEMBER 2, 1999. (M) 2 L 7 2 4F A16WE 2000021800018 20000218 00018 NM 2000 2 18 P2EA99337 1 19991201 A 5347 SEAT TRACK BOEING 737 737222 1384473 NM BS 360-380 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - C-CHECK, SEAT TRACK CORRODED FROM BS 360 TO BS 380, LBL 35 INCHES. DEFECT SIZE, LENGTH 8 INCHES, WIDTH 2.25 INCHE S, DEPTH .200 INCHES. REPAIRED SEAT TRACK SECTION FROM BS 344 TO BS 380, LBL 25 INCHES PER SRM 53-10-5, FIG 2. (M) 2 L 7 2 4F A16WE 2000021800019 20000218 00019 NM 2000 2 18 P2EA99336 1 19991130 A 5330 SKIN BOEING 737 737281 138448P NM BS 268-277 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 268 TO BS 277, BETWEEN STRINGER 15 RT AND 16 RT. DEFECT SIZE 1 INCH. REPA IRED FUSELAGE SKIN SECTION FROM BS 263.5 TO BS 280, BETWEEN STRINGER 14 RT AND STRINGER 17 RT PER SRM 53-30-3, FIG 17. ( M) 2 L 7 2 4F A16WE 2000021800020 20000218 00020 NM 2000 2 18 P2EA99335 1 19991202 A 5312 BULKHEAD BOEING 737 737281 138448P NM BS 178 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - C-CHECK, WEB CRACKED AT BS 178, LBL 10 INCHES, WL 235. DEFECT SIZE, LENGTH .375 INCH. REPAIRED BULKHEAD WEB AT B S 178 FROM LBL 7 TO LBL 17.5, BETWEEN WL 240 AND WL 230.5 PER SRM 53-10-11 FIG 1. (M) 2 L 7 2 4F A16WE 2000021800021 20000218 00021 NM 2000 2 18 P2EA99338 1 19991130 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 344 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - C-CHECK, FLOORBEAM UPPER CHORD CORRODED AT BS 344, WL 208, BETWEEN LBL 32 AND BL 0. DEFECT SIZE, LENGTH 15 INCHES , WIDTH 1.5 INCH, DEPTH .050 INCH. REPAIRED FLOORBEAM AT BS 344, BETWEEN RBL 9 INCHES AND LBL 40 INCHES PER SRM 53-10-2 , FIG 7. (M) 2 L 7 2 4F A16WE 2000021800024 20000218 00024 NE 2000 2 18 GTIA9901225 2 19991204 A 7250 TURBINE WHEEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE RT ENGINE DAMAGED A GTIA E C ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 23 133NK 48111 700766 MYR - FLT 309 - RIGHT ENGINE REVERSE UNLOCK LIGHT ILLUMINATED ACCOMPANIED BY YAW AND VIBRATION, RIGHT ENGINE WAS IMMEDIA TELY SHUT DOWN. NR 2 ENGINE INSPECTION FOUND TURBINE BLADE DAMAGE. REMOVED AND REPLACED NR 2 ENGINE IAW DC9 MM 71-00. ADJUSTMENT TEST SATISFACTORY. LEAKED CHECKED GOOD. (M) 2 L 7 2 4F 4 F A6WE E2EA 2000021800025 20000218 00025 WP 2000 2 18 GTIA9901228 1 19991212 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 ACY - FLT 262 - PATH LIGHTING STRIP IS COMING UP. REATTACH PATHWAY LIGHTING STRIP. OPS GOOD AS PER 33-50-00. (M) 2 L 7 2 4F A6WE 2000021800026 20000218 00026 WP 2000 2 18 GTIA9901232 1 19991221 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 DTW - FLT 712 - EMERGENCY FLOOR LIGHTING TRACK, 1ST THREE ROWS, WILL NOT STAY ATTACHED TO FLOOR. RESECURED FLOOR LIGHTI NG TRIM COVER IAW MD-80 MM 33-50-00. (M) 2 L 7 2 4F RT A6WE 2000021800027 20000218 00027 WP 2000 2 18 GTIA9901233 1 19991219 A 3350 LIGHT DOUG DC9 DC987 3022087 WP ROW 25 INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 750RA 49777 DTW - EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 25 NEEDS TO BE REPLACED. REMOVED AND REPLACED FLOOR TRACK LIGHT SOCKE T. SYSTEM OPS CHECKS GOOD IAW MM 33-50-00. (M) 2 L 7 2 4F RT A6WE 2000021800028 20000218 00028 WP 2000 2 18 GTIA9901234 1 19991225 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 MCO - FLT 92 - AFT ENTRY EMERGENCY 'EXIT' SIGN ON LEFT SIDE WALL INOPERATIVE. REPAIRED GROUND WIRE AT AFT ENTRY OVERHEA D. PANEL AND OPS CHECKED GOOD PER MM CHECK 33-50-00. (M) 2 L 7 2 4F A6WE 2000021800029 20000218 00029 2000 2 18 GTIA9901236 4 19991222 A 2565 SLIDE DOUG DC9 DC982 3022082 WP CABIN LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 801NK 48048 LGA - FLT 403 - GALLEY PACK SLIDE FELL OFF. RETURNED TO GATE ON LEG 2. REINSTALLED SLIDE PACK AND COVER IAW 25-62-00. (M) 2 L 7 2 4F A6WE 2000021800030 20000218 00030 WP 2000 2 18 GTIA9901237 1 19991226 A 3350 LIGHT DOUG DC9 DC987 3022087 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 750RA 49777 DTW - FLT 378 - EMERGENCY FLOOR LIGHTING LOOSE NEAR FORWARD GALLEY. REPLACED AND RESECURED FLOOR TRACK LIGHTING NEAR FO RWARD GALLEY AS REQUIRED. FUNCTIONAL CHECK GOOD. REF MD 80 MM 33-53-01.. (M) 2 L 7 2 4F RT A6WE 2000021800031 20000218 00031 WP 2000 2 18 GTIA9901240 1 19991224 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 802NK 53168 FLL - FLT 47 - COVER ON AISLE TRACK LIGHTING LOOSE, CARPET STICKING UP. RESECURED TRACK LIGHTING AND CARPET AS REQUIRED . (M) 2 L 7 2 4F RT A6WE 2000021800032 20000218 00032 WP 2000 2 18 GTIA9901241 1 19991223 A 3350 LIGHT DOUG DC9 DC941 302207N WP EXTERIOR INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 CLE - FLT 541 - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. PLACED EMERGENCY LIGHT ON DMI 539. REF MEL 33-20 CAT 'B'. ( M) 2 L 7 2 4F A6WE 2000021800033 20000218 00033 WP 2000 2 18 GTIA9901242 1 19991223 A 3350 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 DTW - FLT 570 - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT EXTERIOR EMERGENCY LIGHT POWER SUPPLY IAW 24-2 1-00. OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 2000021800035 20000218 00035 WP 2000 2 18 GTIA0000002 1 19991113 A 3350 LENS DOUG DC9 DC932 3022066 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12505 45788 DTW - RIGHT FORWARD OVERWING EXIT EMERGENCY LIGHT LENS COVER BROKEN. REPLACED RIGHT FORWARD OVERWING EXIT EMERGENCY LIG HT COVER. CHECKS NORMAL IAW DC-9 MM 33-00-00. (M) 2 L 7 2 4F A6WE 2000021800036 20000218 00036 WP 2000 2 18 GTIA0000003 1 19991227 A 3397 WIRE DOUG DC9 DC941 302207N WP BATTERY PACK LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 ISP - FLT 438 - EMERGENCY EXIT LIGHTS GOING OFF AND ON DURING FLIGHT. FOUND LOOSE WIRE AT OVERWING BATTERY PACK. RESEC URED WIRE. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2000021800037 20000218 00037 WP 2000 2 18 GTIA0000007 1 19991228 A 3350 4TL1110B SWITCH DOUG DC9 DC932 3022066 WP COCKPIT INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941ML 47131 CLE - FLOOR TRACK LIGHTS DO NOT ILLUMINATE WHEN SELECTED TO 'ON' POSITION IN COCKPIT. REPLACED EMERGENCY LIGHT SWITCH I N COCKPIT. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2000021800039 20000218 00039 WP 2000 2 18 AALA996052 1 19991217 A 3350 CONNECTED DOUG DC9 DC987 3022087 WP SEAT 11 DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 752RA 49780 SJC - FLT 11D EMERGENCY LIGHT OUT. RECONNECTED CANNON PLUG AT BULKHEAD. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2000021800040 20000218 00040 WP 2000 2 18 AALA996054 1 19991218 A 3397 WIRE DOUG DC9 DC982 3022082 WP SEAT 3 DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 823RA 49889 SJC - ON SEAT 3 DEF EMERGENCY LIGHT IN OPERATIVE. RECONNECTED WIRES ON EMERGENCY LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 2000021800041 20000218 00041 WP 2000 2 18 AALA996053 1 19991218 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 23-26 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 754RA 49641 EMERGENCY LIGHTS ROW 23 THROUGH 26 ILLUMINATED DURING FLIGHT, COULD NOT TURN THEM OFF WITH ANY SWITCH POSITION. REMOVED AND REPLACED EMERGENCY POWER PACK FOR ROWS 23 THROUGH 26 AS REQUIRED, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 2000021800042 20000218 00042 WP 2000 2 18 AALA996048 1 19991209 A 3350 5100303 BATTERY DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 833RA 53045 CHECKED EMERGENCY EVAC LIGHTS AFTER LANDING. COCKPIT LIGHTS OUT. CABIN FLOOR LIGHTS OK. CHANGED BATTERIES IN POWER SU PPLY FOR COCKPIT AND ENTRY E LIGHTS. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 2000021800043 20000218 00043 WP 2000 2 18 AALA996049 1 19991210 A 5270 H2028B SWITCH DOUG DC9 DC983 3022083 WP TAIL CONE MALFUNCTIONED A AALA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 833RA 53045 AT GATE IN SJC, TAIL CONE UNSAFE ILLUMINATED. REINSTALLED JETTISON CABLE TO SWITCH ASSEMBLY. GROUND CHECKS NORMAL IAW MM 52-70-11. (M) 2 L 7 2 4F RT A6WE 2000021800044 20000218 00044 WP 2000 2 18 AALA996055 1 19991228 A 3350 BR9661105 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 832RA 53044 RNO-CCI - AFT SECTION OF AISLE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 2000021800045 20000218 00045 WP 2000 2 18 AALA996050 1 19991209 A 5220 DC26F106PW CONNECTOR DOUG DC9 DC983 3022083 WP TAILCONE SWITCH FAILED A AALA O OTHER O OTHER LD LANDING 1 SW 07 833RA 53045 UPON LANDING, TAILCONE UNSAFE LIGHT APPEARED. TAXIED CLEAR AT RUNWAY. F/A REPORTED TAILCONE WAS ATTACHED. INSPECTED AL L LOCKS AND CABLES. ALL SECURED, NO DEFECTS NOTED. CLEANED CANNON PLUG TO UNLATCH SWITCH. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 2000021800046 20000218 00046 NM 2000 2 18 USAASB99288 1 19991205 A 2612 6678 FIRE DETECTOR BOEING 737 7374B7 1384702 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 438US 24560 MIA - FLT 1040 - DURING CLIMB-OUT FROM MIA, AT FL200, THE NR 2 ENGNE OVERHEAT LIGHT ILLUMINATED. SINCE THE 'A' LOOP OVE RHEAT SYSTEM WAS ALREADY ON MEL, CREW DECIDED TO RETURN TO FIELD AT MIA AND DECLARE AN EMERGENCY. LIGHT EVENTUALLY WENT OUT ON APPROACH TO MIA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIRE DETECTOR CORE LOOP AND THE FIRE/OVERHEAT CONTROL MODULE (P/N 6594-01). FIRE DETECTION SYSTEM OPERATIONAL TEST NORMAL P ER MM 26-11-00. CLEARED MEL 26-2A. (M) 2 L 7 2 4F RT A16WE 2000021800047 20000218 00047 NM 2000 2 18 USAASB99279 1 19991126 A 2131 7102048 CONTROLLER BOEING 737 737301 1384611 NM E/E BAY FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 563AU 40413 23551 PHL - FLT 435 - EN ROUTE FROM BTV TO PHL, AT FL260, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW VERIFIED CABIN ALTITU DE READING AT 10,000 FT. CREW COMPLIED WITH ABNORMAL PROCEDURES AND ACCOMPLISHED A STEEP DESCENT TO FL120. NO OXYGEN M ASKS WERE DEPLOYED. A/C DID NOT REGAIN NORMAL PRESSURIZATION WHEN LEVEL AT FL120 UNTIL CAPTAIN SWITCH TO STANDBY PRESSU RIZATION MODE. CAPTAIN ELECTED TO CONTINUE ONTO PHL AND ELECTED TO FLY AT THE LOWER ALTITUDE. FLIGHT LANDED WITHOUT FU RTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER PER MM 21-31 -00. OPS TEST GOOD. (M) 2 L 7 2 4F RT A16WE 2000021800048 20000218 00048 NM 2000 2 18 USAASB99278 1 19991125 A 2751 2061141 INDICATOR BOEING 737 737301 1384611 NM TE FLAP FAILED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 560AU 30027 23514 CLT - FLT 2202 - DURING CLIMB-OUT FROM CLT, THE FLAPS FAILED TO RETRACT AS FLAP INDICATOR FAILED AT 5 DEGREES FLAPS. FL IGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 2000021800049 20000218 00049 NM 2000 2 18 USAASB99277 1 19991125 A 2170 V1211 COALESCER BAG BOEING 737 737301 1384611 NM PACK BAY CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 341US 23510 LGA - FLT 6461 - EN ROUTE FROM BOS TO IAD, THE F/A REPORTED THAT COCKPIT CREW SMELLED BURNING ELECT ODOR IN CABIN. CAPT DECIDED TO DIVERT TO LGA. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX ACCOMP GROUND ENG RUN W ITH PACKS ISOLATED AND WITH APU AIR SOURCE. INSPECTED PACK BAYS. NO DEFECTS NOTED. FOUND RT PACK BAY COALESCER BAG CO NTAMINATED. REPLACED SAME ALONG WITH LEFT PACK COALESCER BAG. ALSO, INSPECTED FWD AND AFT GALLEYS AND LAVATORIES. INS PECTED ENTIRE CABIN, COCKPIT AND E/E COMPARTMENTS. NO EVIDENCE OF ELECTRICAL SMOKE OR BURNING SMELL. REMOVED AND REPLA CED FWD GALLEY OVEN (P/N2510-0007-03) AS PRECAUTIONARY DUE TO STRONG FOOD ODOR AFTER PROLONGED HEATING. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2000021800050 20000218 00050 NM 2000 2 18 USAA991343 1 19991209 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 41738 23312 TPA - DURING CX-3 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .5 INCH CRACK IN SKIN AT STATION 380, BL 3LT. INSTA LLED DOUBLER PER TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 2000021800051 20000218 00051 NM 2000 2 18 USAASB99283 1 19991128 A 5210 DOOR BOEING 737 737301 1384611 NM AFT OPEN A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 573US 23560 MCO - FLT 1232 - A/C FAILED TO PRESSURIZE IMMEDIATELY AFTER T/O FROM FLL. CAPT ASKED F/A TO CHECK THE DOORS AND FOUND T HE AFT RIGHT SERVICE DOOR CLOSED WITH HANDLE DOWN BUT THE DOOR DID NOT APPEAR TO BE SEALING PROPERLY. NO DOOR WARNING L IGHTS WERE ILLUMINATED IN COCKPIT. FLT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTE NANCE FOUND THE AFT RIGHT SERVICE DOOR FALSELY LOCKE. THIS WAS VISIBLE FROM THE OUTSIDE OF THE AIRCRAFT, BUT ON THE INS IDE OF THE AIRCRAFT, THE DOOR APPEARED CLOSED. OPERATED DOOR SEVERAL TIMES. DOOR AND DOOR WARNING OPERATIONALLY CHECKE D GOOD. (M) 2 L 7 2 4F RT A16WE 2000021800052 20000218 00052 CE 2000 2 18 C2XA99CL128 1 19991217 A 6121 5038912129 SWITCH BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 81553 0037 UE222 CLE - FLT 3134 - AFTER TAKEOFF FROM CLE, LEFT AUTOFEATHER ADVISORY (GREEN) LIGHT AND REPEATER (AFX) FAILED TO ILLUMINATE . AIRCRAFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE LOW PRESSURE AUTOFEA THER SWITCH IAW BEECH 1900 MM 61-21-01. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2000021800054 20000218 00054 NM 2000 2 18 TSAA9933500 1 19991211 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 4 FLOOR LIGHT EMERGENCY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2000021800055 20000218 00055 WP 2000 2 18 GTIA0000005 1 19991231 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 34 EXPOSED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 805NK 48087 EMERGENCY FLOOR TRACK LIGHTING WIRES EXPOSED AT ROW 34. COVERED FLOOR TRACK LIGHTING WIRES IAW MD80 MM 33-51-00. (M) 2 L 7 2 4F A6WE 2000021800059 20000218 00059 NM 2000 2 18 TSAA0057022 1 19991030 A 5730 6545455 SKIN BOEING 737 737297 1384480 NM WS 15 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 LEFT WING HAS EXFOLIATION IN GAP BETWEEN WING SKINS UPPER SURFACE 16 INCH OUTBOARD FROM FS 15 WBL 92.5. REPAIRED IAW SR M 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800060 20000218 00060 NM 2000 2 18 TSAA0057023 1 19991030 A 5753 6018642 SPAR BOEING 737 737297 1384480 NM TE FLAP CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 LEFT OUTBOARD MIDFLAP CORRODED ON SPAR UPPER CHORD ANGLE. REPAIRED ANGLE IAW SRM 51-40-4 FIG 1. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F A16WE 2000021800061 20000218 00061 NM 2000 2 18 TSAA0053024 1 19991030 A 5315 BAC1518399 FLOORBEAM BOEING 737 737297 1384480 NM BS 986 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 FLOORBEAM CAP CORRODED AT STATION 986. REPAIRED FLOORBEAM CAP IAW 53-10-9. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800062 20000218 00062 NM 2000 2 18 TSAA0057021 1 19991030 A 5711 69466097 SPAR BOEING 737 737297 1384480 NM WS 113 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 LEFT WING FRONT SPAR FORWARD SIDE CORRODED AT WBL 90 FSS 113. REPAIRED IAW 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800063 20000218 00063 NM 2000 2 18 TSAA0053019 1 19991030 A 5347 BAC1320792 SEAT TRACK BOEING 737 737297 1384480 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 SEAT TRACK AT AFT RIGHT OF CABIN AFT SERVICE DOOR WAY TO 1016 CORRODED. REPLACED SEAT TRACK IAW SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800064 20000218 00064 NM 2000 2 18 TSAA0057020 1 19991030 A 5711 BAC15061745 SPAR BOEING 737 737297 1384480 NM WS 286.9 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 LEFT WING HAS CORROSION ON FRONT SPAR WEB AT FSS 286.9. REPAIRED WEB IAW ECO 3021 AND SRM 51-10-6. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 2000021800065 20000218 00065 NM 2000 2 18 TSAA0057018 1 19991030 A 5711 69914432 SPAR BOEING 737 737297 1384480 NM LT WING CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 FOUND CRACK IN PAINT BETWEEN RIVETS ON LEFT UPPER INBOARD WING SKIN 6 INCH FORWARD FROM REAR SPAR AT WBL 114. REPAIRED LEFT INBOARD WING SKIN IAW SB 737-57-1144. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800066 20000218 00066 NM 2000 2 18 TSAA0057016 1 19991030 A 5711 6545320285 SPAR BOEING 737 737297 1384480 NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 LEFT WING FRONT SPAR FORWARD SIDE WEB AND LOWER CHORD CORRODED AT WBL 367. REPAIRED LEFT WING FRONT SPAR IAW ECO3019 AN D SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800067 20000218 00067 NM 2000 2 18 TSAA0053017 1 19991030 A 5314 QQA20011E KEEL BEAM BOEING 737 737297 1384480 NM FUSELAGE CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 LEFT AIR CONDITIONING BAY OUTER KEEL BEAM CORRODED. REPLACED CHORD IAW SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800068 20000218 00068 NM 2000 2 18 TSAA0053015 1 19991030 A 5311 BAC15061745 FRAME BOEING 737 737297 1384480 NM BS 570 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 RIGHT A/C BAY AT BBL 40.875 RT LOWER CHORD CORRODED AT S570 IAW SRM 51-30-2. REPAIRED RIGHT A/C BAY IAW SRM 51-30-2.. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800070 20000218 00070 NM 2000 2 18 TSAA0057006 1 19991109 A 5730 69372201 SKIN BOEING 737 7372T4 1384492 NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPAIRED LEFT LOWER WING SKIN AT TANK PANEL NR 7212 IAW ECO 3061. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800071 20000218 00071 NM 2000 2 18 TSAA0057007 1 19991109 A 5753 65464234140 SKIN BOEING 737 7372T4 1384492 NM TE FLAP CORROSION A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPLACEMENT OF LEADING EDGE SKIN RIGHT INBOARD AFT FLAP IAW ECO 3069. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800072 20000218 00072 NM 2000 2 18 TSAA0057009 1 19991109 A 5730 65515892 SKIN BOEING 737 7372T4 1384492 NM WS 531-583 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPAIRED RIGHT WING LOWER SKIN ALONG TRAILING EDGE IN NUMEROUS LOCATIONS BETWEEN WS 531 TO WS 583 IAW ECO 3059. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800073 20000218 00073 NM 2000 2 18 TSAA0057010 1 19991109 A 5730 65515892 SKIN BOEING 737 7372T4 1384492 NM WS 383-418 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPAIRED RIGHT UPPER/LOWER TRAILING EDGE LOWER WING SKIN AT WS 383-418 IAW ECO 3051. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800074 20000218 00074 NM 2000 2 18 TSAA0053011 1 19991109 A 5330 652072 BEAR STRAP BOEING 737 7372T4 1384492 NM BS 491 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPAIRED FORWARD CARGO DOOR BEARSTRAP BS 491 IAW ECO 3062. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800075 20000218 00075 NM 2000 2 18 TSAA0057012 1 19991109 A 5754 6546423278 SKIN BOEING 737 7372T4 1384492 NM NR 4 SLAT CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPAIRED NR 4 SLAT TRAILING EDGE EXTRUSION IAW ECO 3057. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800076 20000218 00076 NM 2000 2 18 TSAA0057013 1 19991109 A 5753 6546846114 SKIN BOEING 737 7372T4 1384492 NM TE FLAP DELAMINATION A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPAIRED RIGHT INBOARD MID-FLAP TRAILING ASSEMBLY IAW ECO 3068. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800077 20000218 00077 NM 2000 2 18 P2EA00002 1 19990102 A 7500 655812310 DUCT BOEING 737 737222 1384473 NM NR 1 ENGINE CRACKED A P2EA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 209US 19548 BUF - FLT 374 - NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT, AFTER THRUST LEVER IS RETARDED TO FLIGHT IDLE THE OVER HEAT LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO GROUND UNEVENTFUL. DUPLICATED PROBLEM ON GROUND, FOUND 13TH STAGE BLEED AIR DUCT CRACKED. REMOVED AND REPLACED DUCT PER MM 75-10-00. ENGINE RUN PERFORMED WITH NO DEFECTS NOTED. (M) 2 L 7 2 4F A16WE 2000021800082 20000218 00082 2000 2 18 2000ZZZM88 4 19991230 A 2210 6225798022 YAW DAMPER BEECH 1900 1900D 1154162 CE RUDDER MALFUNCTIONED A GLBA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 01 260GL 3132 UE260 YAW DAMPER ENGAGED ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FLIGHT CONTROL PAN EL. SYSTEM TESTS SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 2000021800085 20000218 00085 NM 2000 2 18 MZZA99237 1 19991125 A 3230 ROLLER BOEING 727 727264 138408M NM RT MLG SEIZED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FROZEN ROLLER WAS FOUND ON RIGHT MLG MANUAL EXTENSION CR ANK. THE FROZEN ROLLER WAS REMOVED AND REPLACED WITH A NEW ONE AND OPERATIONAL CHECK FOUND SATISFACTORY PER B727 MM CHA PTER 32-32-0. (M) 2 L 7 3 4F A3WE 2000021800086 20000218 00086 NM 2000 2 18 MZZA99236 1 19991129 A 3230 BEARING BOEING 727 727264 138408M NM NLG DAMAGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO STIFFENED BEARINGS WAS FOUND ON NOSE LANDING GEAR MANU AL EXTENSION CABLE DRUM. THE STIFFENED BEARINGS WAS REMOVED AND REPLACED WITH A NEW ONE AND OPERATIONAL CHECK FOUND SAT ISFACTORY PER B727 CHAPTER 32-33-0. (M) 2 L 7 3 4F A3WE 2000021800087 20000218 00087 NM 2000 2 18 MZZA99235 1 19991201 A 2710 CONTROL CABLE BOEING 727 727264 138408M NM AILERON FRAYED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FRAYED RIGHT WING INBOARD AILERON TAB CABLE WAS FOUND ON RT TE CAVITY BELOW NR 2 AND NR 3 ENGINE FUEL FEED LINE SHROUD. THE FRAYED CABLE WAS REMOVED AND REPLACED WITH A NEW ON E AND OPERATIONAL CHECK FOUND SATISFACTORY PER B727 MM CHAPTER 27-10-71. (M) 2 L 7 3 4F A3WE 2000021800088 20000218 00088 NM 2000 2 18 MZZA99234 1 19991201 A 5713 STRINGER BOEING 727 727264 138408M NM WS 656.5 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT OUTER WING IN SPAR UPPER STRING ER S-9 AT WS 656.5. THE CRACKED STRINGER WAS REPAIRED PER B727 SB 727-57A159R5. (M) 2 L 7 3 4F A3WE 2000021800089 20000218 00089 NM 2000 2 18 MZZA99233 1 19991126 A 5730 SKIN BOEING 727 727264 138408M NM LT WING CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INBH BY 2 INCH BY .084 INCH DEEP IG CORROSION WAS FOUN D ON LEFT WING CENTER SECTION LOWER SKIN BETWEEN S-4C AND S-53 AT LBBL 29.5. THE CORROSION WAS BLENDED OUT AND REPAIRED PER B727 SRM CHAPTER 57-30-03 FIG 10. (M) 2 L 7 3 4F A3WE 2000021800090 20000218 00090 NM 2000 2 18 MZZA99232 1 19991124 A 5713 STRINGER BOEING 727 727264 138408M NM WS 629 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT OUTER WING IN SPAR UPPER VENT S TRINGER S-13 AT WS 629. THE CRACK WAS REPAIRED PER B727 SB 727-57A 159R5. (M) 2 L 7 3 4F A3WE 2000021800091 20000218 00091 NM 2000 2 18 USAA991329 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 767 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800092 20000218 00092 NM 2000 2 18 USAA991328 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 747 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800093 20000218 00093 NM 2000 2 18 USAA991327 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 7R STATION 727B TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-01 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000021800094 20000218 00094 NM 2000 2 18 USAA991326 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 6L STATION 727B TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800095 20000218 00095 NM 2000 2 18 USAA991325 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 3L STATION 727B TIE CLIP. INSTALLED TIE C LIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800096 20000218 00096 NM 2000 2 18 USAA991324 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 7L STATION 727A TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800097 20000218 00097 NM 2000 2 18 USAA991323 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 727A TIE CLIP. INSTALLED TIE C LIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800098 20000218 00098 NM 2000 2 18 USAA991322 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 8R STATION 706 TIE CLIP. INSTALLED TIE CLI P PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000021800099 20000218 00099 NM 2000 2 18 USAA991321 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO 1.125 INCH CRACKS AT STRINGER 4L STATION 685 TIE CLIP. INSTALLED TI E CLIP PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2000021800100 20000218 00100 NM 2000 2 18 USAA991320 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 3R STATION 685 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2000021800101 20000218 00101 NM 2000 2 18 USAA991319 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 10R STATION 663 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800102 20000218 00102 NM 2000 2 18 USAA991318 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 4R STATIN 639 TIE CLIP. INSTALLED TIE CLI P PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000021800103 20000218 00103 NM 2000 2 18 USAA991317 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 3R STATION 639 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000021800104 20000218 00104 NM 2000 2 18 USAA991316 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK AT STRINGER 3L STATION 597 TIE CLIP. REPAIRED PER SR M 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800105 20000218 00105 NM 2000 2 18 USAA991315 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 578 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STRINGER 8L STATION 578 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-30-02. (M) 2 L 7 2 4F A16WE 2000021800106 20000218 00106 NM 2000 2 18 USAA991314 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 500B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT FASTENER BS 500B STRINGER 3R TIE CLIP. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800107 20000218 00107 NM 2000 2 18 USAA991313 1 19991225 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH AREA OF CORROSION AROUND NUT PLATE HOLES STATION 312, LBL 7 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 2000021800108 20000218 00108 NM 2000 2 18 USAA991408 1 19991225 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION STATION 294.5 LBL 13 TO RBL 1 FLOOR BEAM. CORROSION LEVEL 2. REPLACED T-CAP PER TR 53-10-04 B. (M) 2 L 7 2 4F A16WE 2000021800109 20000218 00109 NM 2000 2 18 USAA991381 1 19991225 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 313-324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION STRINGER 28R, STATION 313 TO 324.. CORROSION LEVEL 2. INSTALLED STRINGER SPLICE REPAIR AND CLIP PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 2000021800110 20000218 00110 NM 2000 2 18 USAA991380 1 19991225 A 5320 DOOR FRAME BOEING 737 7372B7 1384560 NM BS 847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION ON SURFACE STATION 847, RBL 24, AFT CARGO DOOR CUTOUT AFT FRAME. CORROSION LEVEL 1. REPAIRED PER EA 66271. (M) 2 L 7 2 4F A16WE 2000021800111 20000218 00111 NM 2000 2 18 USAA991378 1 19991225 A 5320 69620141 STIFFENER BOEING 737 7372B7 1384560 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AFT SIDE 663 BULKHEAD, LBL 7, 16 FT UP FROM KEEL BEAM S TIFFENER. REMOVED AND REPLACED STIFFENER PER EA 66242. (M) 2 L 7 2 4F A16WE 2000021800116 20000218 00116 NM 2000 2 18 USAABB99058 1 19991223 A 3260 MS25237387 BULB BOEING 767 7672B7 1385107 NM COCKPIT FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 651US 24764 PHL - FLT 893 - ON APPROACH TO PHL, BOTH NOSE LANDING GEAR GREEN LIGHTS FAILED TO ILLUMINATED WITH GEAR EXTENDED. CREW ACCOMPLISHED A FLYBY FOR PHL TOWER WHO OBSERVED GEAR TO BE DOWN. AFTER CONSULATION WITH PHL MAINTENANCE AND PIT MAINTEN ANCE CONTROL, FLIGHT CREW REPLACED BOTH NOSE GEAR BULBS AND INDICATIONS BECAME NORMAL. FLIGHT LANDED AT PHL WITHOUT INC IDENT. NO EMERGENCY WAS DECLARED. INCIDENT NOTED BY PHL MAINTENANCE. NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4F RT A1NM 2000021800119 20000218 00119 NM 2000 2 18 USAA991442 1 19991221 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 23939 27124 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 6 INCH AREA OF CORROSION AT STATION 377.7, LBL 24 SEAT TRACK . CORROSION LEVEL 1. REMOVED DAMAGED SEAT TRACK AND REPLACED PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 2000021800120 20000218 00120 NM 2000 2 18 USAA991441 1 19991221 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 23939 27124 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 6 INCH AREA OF CORROSION AT STA 377.7, LBL 45 SEAT TRACK, CO RROSION LEVEL 1. REMOVED DAMAGED SEAT TRACK AND REPLACED PER SRM 51-20-=01 A01 AND SRM 51-10-00. (X) 2 L 7 2 4F RT A2NM 2000021800121 20000218 00121 NM 2000 2 18 USAA991427 1 19991221 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 345 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 23939 27124 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION TOP SURFACE OF FLOORBEAM STA 345, LBL 9 - LBL 18. CORROSION LEVEL 1. INSTALLED DOUBLERS PER EA 66281. (X) 2 L 7 2 4F RT A2NM 2000021800122 20000218 00122 NM 2000 2 18 USAA991426 1 19991221 A 5320 ANGLE BOEING 757 7572B7 1384964 NM BS 345-324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 23939 27124 CLT - DURING C-1 CHECK VISUAL INSPECTION FOUND A 4 INCH BY 6 INCH AREA OF CORROSION LBL 30 TO LBL 32 AT FS 345 TO FS 324 TRANSITIONAL ANGLE, CORROSION LEVEL 1. 2 L 7 2 4F RT A2NM 2000021800123 20000218 00123 NM 2000 2 18 USAA991466 1 19991221 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 23939 27124 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH AREAS OF CORROSION AT FUSELAGE STA 377.7, FROM ZERO BUTTL INE TO LBL 54 BEAM CAP. CORROSION LEVEL 1. (X) 2 L 7 2 4F RT A2NM 2000021800124 20000218 00124 EA 2000 2 18 MASA99191 1 19991229 A 3350 GE1317 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77260 7260 FLT 6336 - BFL-PHX - IN PHX, THE CREW NOTED THEY HAD AN AFT EMEGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE WAS CALLED OUT AND REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 2000021800126 20000218 00126 NM 2000 2 18 MASA99190 1 19991217 A 3350 OL6839BPE LIGHT BRUCE 6512003001 DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 6103 - PSP-PHX - DURING STANDARD PRE-FLIGHT CHECK, THE CREW NOTED THEY HAD AN EMERGENCY EXIT LIGHT INOPERATIVE. MAI NTENANCE WAS CALLED OUT AND REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A13NM 2000021800136 20000218 00136 WP 2000 2 18 AALA996057 1 19991230 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP SEAT 3-7 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 823RA 49889 SJC-CCI - EMERGENCY LIGHTS ON SEAT 3, 4, 5, 6 AND 7 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 2000021800146 20000218 00146 NM 2000 2 18 GAIA99220 1 19991201 A 5330 BEAR STRAP BOEING 727 727232 1384082 NM FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CE RTIFICATE. FORWARD GALLEY DOOR CUTOUT AT LOWER AFT CORNER BEAR STRAP HAS CRACK. STOP DRILLED CRACK AT GALLEY DOOR CUTO UT BEAR STRAP IAW B727 SRM 51-10-1. PERFORMED HFEC TO VERIFY NO ADDITIONAL CRACKS. INSTALLED REPAIR IAW BOEING SB 727- 53-188 REV 2. (M) 2 L 7 3 4F A3WE 2000021800147 20000218 00147 NM 2000 2 18 GAIA99221 1 19991201 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1050 MISMANUFACTURED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA C ERTIFICATE. SEAT TRACK AT LBL 24.75 TOO SHORT AT SPLICES FOR CARGO MOD BODY STATION 1050 TO 1070. REMOVED AND REPLACED SEAT TRACK AT LBL 24.75 FROM BS 1050 TO BS 1070, PER B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 2000021800148 20000218 00148 NM 2000 2 18 GAIA99222 1 19991201 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1148 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY (MIAMI) PRIOR TO THIS AIRCRAFT BEING ON TH E KHA CERTIFICATE. CORROSION AT STRINGER 7R UPPER FLANGE, JUST FORWARD OF BS 1148. REMOVED CORRODED AREA AT STRINGER 7 R UPPER FLANGE FORWARD OF BS 1148. CUT OUT DAMAGED AREAS AND REPAIRED AREA AND STRINGER UPPER FLANGE FORWARD OF BS 1148 . CUT OUT DAMAGED AREAS AND REPAIRED AREA AND STRINGER UPPER FLANGE PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2000021800149 20000218 00149 NM 2000 2 18 GAIA99223 1 19991201 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 850 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA C ERTIFICATE. MAIN CABIN STRINGER 17L BODY STATION 850, ANGLE IS CRACKED, INBOARD SIDE OF FRAME. ACCOMPLISHED REPAIR ON MAIN CABIN STRINGER 17L STATION 850, ANGLE IS CRACKED, INBOARD SIDE OF FRAME, IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM 067. RO-1 REV 1, DATED 10/5/99. (M) 2 L 7 3 4F A3WE 2000021800150 20000218 00150 NM 2000 2 18 GAIA99224 1 19991201 A 2810 VENT LINES BOEING 727 727232 1384082 NM FUEL SYSTEM CHAFED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA C ERTIFICATE. FUEL VENT TUBING WAS FOUND TO BE CHAFING AT THE FOLLOWING WING STATIONS, LWS 656.5, LWS 546.5, LWS 519.0, R WS 601.5 AND RWS 546.5. REPAIRED ALL ABOVE NOTED FUEL VENT LINES IAW AVITAS ENGINEERING REPAIR ORDER. WORK ORDER NR 99 AVHM.063RO-1. (M) 2 L 7 3 4F A3WE 2000021800151 20000218 00151 NM 2000 2 18 GAIA99225 1 19991201 A 5311 FRAME BOEING 727 727232 1384082 NM BS 303 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CE RTIFICATE. NOSE SECTION INTERNAL CIRCUMFERENTIAL FRAME HAS CORROSION ON LEFT SIDE OF DOG HOUSE BELOW HORIZONTAL WALKWAY BEAM BS 303 AND STRINGER 26L AND LOWER END. CUT OUT DAMAGED AREA ON FRAME IAW 53-10-4. INSTALLED REPAIR AT CIRCUMFERE NTIAL FRAME AT BODY STATION 303 STRINGER 26L IAW B727 SRM 53-10-4. (M) 2 L 7 3 4F A3WE 2000021800152 20000218 00152 NM 2000 2 18 GAIA99226 1 19991201 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1183 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEABY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA C ERTIFICATE, BS 1183 BULKHEAD LEFT VERTICAL BEAM HAS CRACK AT LOWER END, LBL 8. PERFORMED NDT INSPECTION TO DETERMINE EN D OF CRACK, PER B727 NDT PART 6 OF 51-00-00. CUTOUT DAMAGED AREA PER B727 S/B 53-0175. ACCOMPLISHED VERTICAL BEAM REPA IR IAW B727, S/B 53-175. (M) 2 L 7 3 4F A3WE 2000021800153 20000218 00153 NM 2000 2 18 GAIA99227 1 19991201 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 1183 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CE RTIFICATE. TAIL SKID CAVITY BULKHEAD WEB AT STATION 1183 HAS CRACK ON LEFT SIDE 5 INCHES BELOW FLOOR. REMOVED EXISTING REPAIR AND INSPECTED IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4. ROUTED OUT CRACK IAW B727 S/B 53-175. ACCOMPLISHED RE PAIR IAW B727 S/B 53-175. (M) 2 L 7 3 4F A3WE 2000021800154 20000218 00154 NM 2000 2 18 GAIA99237 1 19991216 A 3243 26011826 BRAKE BOEING 727 727223 1384074 NM MLG LOCKED A GAIA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 6838 20191 FLT 1728 - MEM-DEN, NR 1 BRAKE DEBOOSTER WILL NOT RESET. NR 1 BRAKE ASSEMBLY LOCKED UP. REPLACED NR 1 BRAKE ASSEMBLY P ER B727 MM 32-41-32. ALSO, REPLACED NR 1 BRAKE LOCK OUT DEBOOST VALVE PER B 727 MM 32-41-21. ALL SYSTEMS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2000021800155 20000218 00155 NM 2000 2 18 GAIA99270 1 19991221 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT FAILED A GAIA O OTHER O OTHER CR CRUISE 1 SW 07 6833 20186 FLT 2508, FROM GEG TO PDX, COCKPIT EMERGENCY EXIT LIGHT DOES NOT TURN ON. AIRCRAFT CONTINUED ON TO PDX WITH NO ADDITION AL PROBLEMS NOTED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN PDX. FOUND EMERGENCY LIGHT FIXTURE CONNECTOR LOOSE. RE-SECU RED CONNECTOR AND TESTED EMERGENCY LIGHTING SYSTEM. SYSTEM TEST GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2000021800156 20000218 00156 NM 2000 2 18 GAIA99238A 1 19991220 A 2750 MOT6111 MOTOR BOEING 727 727223 1384074 NM TE FLAP LEAKING A GAIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 6812 19487 DURING INITIAL CLIMB-OUT FROM MHR TO LAX. FLT NR 2008, AFTER FLAP RETRACTION 'A' SYS LOW LVL LIGHT ILLUMINATED. QTY CON TINUED TO DECREASE WITH ALL 'A' SYS SWITCHES TURNED OFF. PERFORMED ABNORMAL CHECKLIST. GEAR CRANKED DOWN AND ALTERNATE EXTENSION OF FLAPS WERE ACCOMPLISHED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MHR. MAINTENANCE REMOVED AND REPLACED RI GHT INBOARD FLAP DRIVE MOTOR IAW AA BOEING 727 MM 27-51-62. TROUBLE SHOOTING PROCEDURES COMPLIED WITH IAW AA BOEING 727 MM 29-00. REPLACED BOTH 'A' SYS ENG DRIVEN PUMPS, CASE DRAIN FILTERS. INSPECTED SYSTEM 'A' MAIN FILTERS. NO KNOWN PR OBLEMS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2000021800157 20000218 00157 NM 2000 2 18 GAIA99229 1 19991203 A 3350 307 LAMP BOEING 727 727251 138408H NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 255US 19974 DURNIG ROUTINE MAINTENANCE IN DEN, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHTS AT THE MAIN ENTRANCE DOOR WERE INOPE RATIVE. RELAMPED THE EMERGENCY EXIT LIGHTS AT THE MAIN ENTRANCE DOOR. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2000021800158 20000218 00158 SO 2000 2 18 C2XA99BT118 1 19991229 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16963 145116 EWR - FLT 4202 - DURING ROUTINE INSPECTION, FOUND BOTH LEFT AND RIGHT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 3 BATTERY PACK AND OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 2000021800159 20000218 00159 GL 2000 2 18 C2XA99TY003 2 19991231 A 7200 2307002 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT MAKING METAL A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14939 145030 CAE311008 TYS - DURING A SCHEDULED INSPECTION THE RIGHT ENGINE WAS FOUND TO BE MAKING METAL BEYOND MANUFACTURES LIMITS. MAINTENAN CE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2000021800160 20000218 00160 NE 2000 2 18 C2XA99IA639 2 19991227 A 7200 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE LEFT FAILED A C2XA A UNSCHED LANDING X ENGINE FLAMEOUT NR NOT REPORTED 1 SW 09 99838 18463 259 120880 SHV - DURING FLIGHT 3490 FROM IAH TO SHV, THE CREW REPORTED THAT THE NR 1 ENGINE FAILED IN FLIGHT. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE (M) 2 H 7 2 4T 4 T RT A53EU E20NE 2000021800161 20000218 00161 NM 2000 2 18 USAA991371 1 19991225 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATES HOLES IN FLOORBEAM 6 EACH 1 INCH BY 1 INCH ST ATION 328, BL 0 TO RBL 35. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. REPLACED T-CAP SECTION PER TR 53-10-13. ( M) 2 L 7 2 4F A16WE 2000021800162 20000218 00162 NM 2000 2 18 USAA991370 1 19991225 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 5 INCH BY 15 INCHES AT BS 344, WL 208, BL 0 - LBL 1 5 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-01. INSTALLED REPAIR STRAPS PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 2000021800163 20000218 00163 NM 2000 2 18 USAA991369 1 19991225 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 725-727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK LEFT STRINGER 18A SHELF, STATION 725 TO 727, 4 INCHES OF SKIN. INSTALLED NEW AFT SHELF SECTION PER SRM 51-10-1 AND 51-30-3. (M) 2 L 7 2 4F A16WE 2000021800164 20000218 00164 NM 2000 2 18 USAA991360 1 19991225 A 5320 SPLICE BOEING 737 7372B7 1384560 NM BS 908 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN STRINGER PRODUCTION SPLICE BS 908 STRINGER 4R. INSTA LLED NEW STRINGER SPLICE PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2000021800165 20000218 00165 NM 2000 2 18 USAA991359 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 4R STATION 767 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2000021800166 20000218 00166 NM 2000 2 18 USAA991358 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK AT STRINGER 2L STATION 727A TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2000021800167 20000218 00167 NM 2000 2 18 USAA991338 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .1875 INCH CRACK AT STRINGER 4L STATION 907 TIE CLIP. INSTALLED TIE C LIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800168 20000218 00168 NM 2000 2 18 USAA991337 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3125 INCH CRACK AT STRINGER 2L STATION 867 TIE CLIP. INSTALLED TIE C LIP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800169 20000218 00169 NM 2000 2 18 USAA991336 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 847 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STRINGER 5L STATION 847 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000021800170 20000218 00170 NM 2000 2 18 USAA991335 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 2L STATION 827 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800171 20000218 00171 NM 2000 2 18 USAA991334 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 10L STATION 807 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 2000021800172 20000218 00172 NM 2000 2 18 USAA991333 1 19991225 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 6R STATION 807 TIE CLIP. INSTALLED TIE CL IP PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 2000021800173 20000218 00173 NM 2000 2 18 USAA991446 1 19991225 A 5320 BEAM BOEING 737 7372B7 1384560 NM BS 312-328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES 12 EACH 1 INCH BY 1 INCH STATION 312 TO 328, RBL 11 T-SUPPORT BEAM. CORROSION LEVEL 2. REPAIRED T-CAP PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 2000021800174 20000218 00174 NM 2000 2 18 USAA991445 1 19991225 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 5 INCH CRACK AT BS 294.5, STRINGER 17R SUPPORT ANGLE. REPLACED PART P ER SRM 51-40-01. (M) 2 L 7 2 4F A16WE 2000021800175 20000218 00175 NM 2000 2 18 USAA991444 1 19991225 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LOWER AFT CORNER OF FORWARD ENTRY DOOR CUTOUT SKIN. IN STALLED DOUBLER AND TRIPLER PER EO 65C27257. (M) 2 L 7 2 4F A16WE 2000021800176 20000218 00176 NM 2000 2 18 USAA991429 1 19991225 A 5320 CCN6320022 FITTING BOEING 737 7372B7 1384560 NM BS 695 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 695 STRINGER 18A OUTBOARD VERTICAL FLANGE FORWARD FITT ING. REPLACED FITTINGS PER EO NR 5391G625. (M) 2 L 7 2 4F A16WE 2000021800177 20000218 00177 NM 2000 2 18 USAA991428 1 19991225 A 5230 SKIN BOEING 737 7372B7 1384560 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK FORWARD CARGO DOOR ASSIST CABLE CUTOUT INTERIOR SKIN. R ESKINNED DOOR PER BOEING DWG 65-46921 AND EA 66250. (M) 2 L 7 2 4F A16WE 2000021800178 20000218 00178 NM 2000 2 18 USAA991416 1 19991225 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 941-947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 2 INCH AREA OF CORROSION STRINGER AFT CARGO STRINGER 27L STA TION 941-947, CORROSION LEVEL 2. REMOVED AND REPLACED STRINGER SECTION PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 2000021800179 20000218 00179 NM 2000 2 18 USAA991415 1 19991225 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 950-991 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND STRINGER REPAIR SKIN CUTOUT 18.25 INCH LENGTH BY 3 INCHES WIDE BY 23.75 INCHES IN LENGTH BY 8 INCHES WIDE CENTER LINE OF STRINGER 27L, BS 950 TO BS 991 SKIN. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 6 AND FIG 17. (M) 2 L 7 2 4F A16WE 2000021800180 20000218 00180 NM 2000 2 18 USAA991414 1 19991216 A 5230 6546921528M SKIN BOEING 737 7372B7 1384560 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 44573 23114 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK UPPER AFT CORNER OF HANDLE CUTOUT, FORWARD CARGO DOOR SKIN. INSTALLED REPAIR DOUBLER PER SRM 52-30-2 FIG 3. (M) 2 L 7 2 4F A16WE 2000021800181 20000218 00181 NM 2000 2 18 USAA991413 1 19991215 A 5313 BAC1498158 STRINGER BOEING 737 737201 1384454 NM BS 987-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 45386 22798 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND CORROSION BETWEEN STATION 987 AND 1016, STRINGER 27L. CORROSION LEVEL 1. REPLACED DEFECTIVE STRINGER SECTION PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 2000021800182 20000218 00182 NM 2000 2 18 USAA991410 1 19991225 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK HFEC INSPECTION, FOUND A CRACK AT BS 727 STRINGER 18A LEFT CHORD. REPAIRED PER EA 66261 AND EO 5 394G068. (M) 2 L 7 2 4F A16WE 2000021800183 20000218 00183 NM 2000 2 18 USAA991409 1 19991225 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 46288 22885 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT SKIN. INSTA LLED TRIPLERS PER SRM 53-30-3 FIG 26. (M) 2 L 7 2 4F A16WE 2000021800184 20000218 00184 NM 2000 2 18 USAA991310 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8R AND 9R STATION 440 FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021800185 20000218 00185 NM 2000 2 18 USAA991311 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUDN TWO .25 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 380 OUTBOARD RIVET. FABRICATED DOUBLER PER SRM 53-00-07 FIG 201. (M) 2 L 7 2 4F RT A16WE 2000021800186 20000218 00186 NM 2000 2 18 USAA991312 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS BETWEEN STRINGER 8L AND 9L FRAME 380 INBOARD RIVET. FABRICATED DOUBLER PER SRM 53-00-07 FIG 201. (M) 2 L 7 2 4F RT A16WE 2000021800187 20000218 00187 NM 2000 2 18 USAA991309 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8L AND 9L STATION 440 FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021800188 20000218 00188 NM 2000 2 18 USAA991308 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8L AND 9L STATION 867 FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021800189 20000218 00189 NM 2000 2 18 USAA991307 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUDN A .25 INCH CRACK BETWEEN STRINGER 8R AND 9R STATION 867 FRAME. INSTALLE D DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021800190 20000218 00190 NM 2000 2 18 USAA991306 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 8L AND 9L STATION 400 INBOARD RIVET FR AME. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2000021800191 20000218 00191 NM 2000 2 18 USAA991305 1 19991215 A 5311 FRAME BOEING 737 737401 1384701 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK BETWEEN STRINGER 8L AND 9L FRAME 907. I NSTALLED DOUBLER PER TR 53-10-14. (M) 2 L 7 2 4F RT A16WE 2000021800192 20000218 00192 NM 2000 2 18 USAA991304 1 19991215 A 5320 SILL BOEING 737 737401 1384701 NM BS 947-1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AT BS 947-1006, WL 208, RBL 55 LOWE R SILL ASSEMBLY. CORROSION LEVEL 1. REPAIRED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000021800193 20000218 00193 NM 2000 2 18 USAA991303 1 19991215 A 5320 CREASE BEAM BOEING 737 737401 1384701 NM BS 294.5-338 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION RIGHT CREASE BEAM INNER CHORD UPPER SURFACE FROM BS 294.5 TO 338. CORROSION LEVEL 1. REMOVED CORROSION PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000021800194 20000218 00194 NM 2000 2 18 USAA991302 1 19991215 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 30932 23990 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY 20 INCH AREA OF CORROSION AFT ENTRY DOOR CREASE BEAM INNER CHORD Z-ANGLE. CORROSION LEVEL 1. CORROSION TASK C 53-107-02. INSTALLED NEW CREASE BEAM INNER CHORD PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000021800195 20000218 00195 NM 2000 2 18 TSAA9933517 1 19991230 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 1 FLOOR EMERGENCY POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000021800196 20000218 00196 NM 2000 2 18 TSAA9933516 1 19991231 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.. ( M) 2 L 7 2 4F A16WE 2000021800197 20000218 00197 NM 2000 2 18 TSAA9933518 1 19991229 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED BATTERY PACK FOR NR 2 EMERGENCY FLOOR PROX LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 2000021800198 20000218 00198 NM 2000 2 18 TSAA9933514 1 19991224 A 3350 9221009 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED FORWARD SERVICE EXIT IDENTIFIER BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 2000021800199 20000218 00199 NM 2000 2 18 TSAA9933513 1 19991226 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2000021800200 20000218 00200 NM 2000 2 18 2000ZZZM84 1 19991208 A 2720 4030952901 COUPLER BOEING 727 727231 1384079 NM E/E BAY DAMAGED A MYWA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 SO 19 808MA 21988 MIA - ON CLIMB-OUT, WITH AUTO PILOT ENGAGED AT 10000 PLUS 250-260 KTS RUDDER SPLIT AND AUTO PILOT COULD NOT CONTROL AIRC RAFT. DISCONNECTED AUTO PILOT AND FOUND IT TOOK 4 DEGREES RIGHT TRIM TO KEEP AIRCRAFT FROM YAWING. RETURNED TO MIA. T ROUBLE SHOT SYSTEM, FOUND UPPER YAW DAMPER COUPLER AT FAULT. REMOVED AND REPLACED UPPER YAW DAMPER COUPLER. OPS CHECKE D OK IAW 22-11-131. ADJUSTED LOWER RUDDER POSITION SENSOR. OPS CHECKED OK IAW 22-11-51. (M) 2 L 7 3 4F A3WE 2000021800201 20000218 00201 NM 2000 2 18 2000ZZZM85 1 19991031 A 2910 69191222 FITTING BOEING 727 727225 1384077 NM NLG CRACKED A MYWA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 804MA 43761 22435 JFK - ON FINAL APPROACH, AIRCRAFT LOST 'A' SYSTEM HYDRAULICS. MADE UNEVENTFUL LANDING, UNABLE TO TAXI A/C DUE LOSS OF F LUID IN NOSE STEERING SYSTEM. ON INSPECTION FOUND NLG DOWNLOCK ACTUATOR HYDRAULIC LINES DAMAGED AND DOWNLOCK SUPPORT CH ANNEL FLANGE ON AFT BULKHEAD CRACKED AND SEPARATED FROM CHANNEL. PURGED 'A' SYSTEM HYDRAULICS, REPLACED CASE FILTER, PI NNED AND SECURED NOSE LANDING GEAR, FERRIED A/C TO MIAMI. REPLACED DOWNLOCK ACTUATOR SUPPORT CHANNEL PER SRM 51-30-2. I N ADDITION, REPLACED NOSE LANDING GEAR LOCK ACTUATOR P/N 65-40467-6, OPS AND LEAK CHECKED PER MM 32-33-22. PERFORMED RE TRACTION AND EXTENSION CHECK PER 32-33-0. OPS CHECK OK. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2000021800202 20000218 00202 NM 2000 2 18 GAIA99271 1 19991227 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6816 19491 NO FLIGHT FOUND DURING GROUND MX AT DFW, MAIN ENTRY DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED MAIN ENTRY EMERGENCY EXIT LIGHT. SYSTEM TEST GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 2000021800203 20000218 00203 NM 2000 2 18 GAIA0001 1 19990103 A 3350 GE307 BULB BOEING 727 727243 138408D NM COCKPIT FAILED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 579PE 21662 DURING POST FLIGHT, MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHT OVER THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE RE-LAMPED THE LIGHT ASSEMBLY AND PERFORMED AN SATISFACTORY OPS CHECK IAW BOEING 727 MM 33-50-4. THE AIRCRAFT WAS THEN R ELEASED BACK TO SERVICE. (M) 2 L 7 3 4F RT A3WE 2000021800204 20000218 00204 NM 2000 2 18 2000ZZZM86 1 19990815 A 2781 106180379 LIGHT BOEING 727 727259 138408J NM COCKPIT MALFUNCTIONED A FX7A O OTHER N FALSE WARNING CL CLIMB 1 SO 19 203AV 22474 ON FAE FLIGHT NR 484 - TTPP-KMIA - DURING CLIMB-OUT, R-5 L/E FLAP LIGHT WOULD NOT EXTINGUISH DURING FLAP RETRACTION. AI RCRAFT RETURNED TO TTPP. ON GROUND MAINTENANCE INSPECTED L/E DEVICES FOR DAMAGE AND FOUND NONE. MAINTENANCE ALSO PERFO RMED GROUND OPS CHECK AND SYSTEM CHECK PER MM 27-82-0 AND MM 27-81-0 AND FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 3 4F A3WE 2000021900090 20000219 00090 WP 2000 2 19 2000ZZZX372 1 19991229 A 6320 71668 SHAFT ROBSIN R44 R44 7640120 WP IDLER GEAR SHEARED A A RP8A K NONE O OTHER IN INSP/MAINT 1 WP 13 7056H 1500 0497 DURING ROUTINE MAINTENANCE, METAL WAS FOUND IN SCREEN AND FILTER AND SENT TO LYCOMING. ENGINE TAKEN OUT RIGHT AWAY, AND SHAFT P/N 21668 THAT HOLDS GEAR P/N 71652 HAD FLANGE SHEARED OFF AT BOLT AND STUD AND SPACER. CAUSED MAJOR DAMAGE TO AL L GEARS, CRANKCASE, AND ACCESSORY HOUSING. THE GEAR WAS ONLY HELD IN PLACE BY THE THREE SURROUNDING GEARS SINCE THE SHA FT WAS NOT SUPPORTING IT ANYMORE. TEETH WERE BROKEN OFF. ENGINE WAS MOMENTS FROM FAILING. 1 G 7 1 3O H11NM 2000021900139 20000219 00139 CE 2000 2 19 2000ZZZX421 1 19991124 A 2620 1015700216 SWITCH BEECH 1900 1900C 1154161 CE FIRE EXTING DISCONNECTED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 01 1563C UC20 WHILE PERFORMING OTHER MAINTENANCE, FOUND LT ENGINE SQUIB POWER SWITCH DISLOCATED FROM ENGINE FIRE EXTINGUISHER ANNUNCIA TOR/ACTUATOR ASSEMBLY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FOUND ON HALF OF INSPECTED AIRCRAFT. SUGGEST A CHANGE IN DESIGN OF THE ASSEMBLY FOR POSITIVE ATTACHMENT OF SQUIB POWER SWITCH. NOTE: THE CONDITION FOUND ON THIS ASSY WOULD PREVENT THE FLIGHT CREW FROM BEING ABLE TO DISCHARGE THE AF FECTED ENGINE FIRE BOTTLE AT ANYTIME. ALSO, THERE IS NO WAY FOR THE CREW TO PRE-FLIGHT THIS SYSTEM TO VERIIFY THAT THE FIRE BOTTLE SQUIB COULD BE BLOWN IF NEEDED. 2 L 7 2 4T RT A24CE 2000021900140 20000219 00140 CE 2000 2 19 2000ZZZX422 1 19991119 A 2620 1015700216 SWITCH BEECH 1900 1900C 1154161 CE FIRE EXT DISCONNECTED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 01 41UE UC41 WHILE PERFORMING 'NEW INSP REQUIREMENT, FOUND SQUIB POWER SWITCH DISLOCATED FROM MAIN ENG FIRE EXTINGUISHER ANNUNCIATOR/ ACTUATOR ASSY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION WAS FOUND O N 2 ASSYS OUT OF 6 CHECKED. NEW REPLACEMENT ASSY FOUND ONLY MARGINALLY BETTER FOR RETENTION OF SQUIB SWITCH MODULE ON A FT END OF ANNUNCIATOR/ACTUATOR ASSY. SUGGEST A CHANGE IN DESIGN OF THE ASSY FOR POSITIVE ATTACHMENT OF SQUIB POWER SWIT CH. NOTE: CONDITION FOUND ON THE TWO ASSYS WOULD PREVENT FLT CREW FROM BEING ABLE TO DISCHARGE AFFECTED ENG FIRE BOTTL ES AT ANYTIME. ALSO, THERE IS NO WAY FOR CREW TO PRE-FLIGHT SYS TO VERIFY FIRE BOTTLE SQUIBS WOULD BE BLOWN IF NEEDED. 2 L 7 2 4T RT A24CE 2000021900141 20000219 00141 CE 2000 2 19 2000ZZZX423 1 19991123 A 2620 101570216 SWITCH BEECH 1900 1900C 1154161 CE FIRE EXT DISCONNECTED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 01 45GL UC45 WHILE PERFORMING 'NEW' INSP REQUIREMENT, FND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENG FIRE EXTING ANNUNCIATOR/ ACTUATOR ASSY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FN D ON HALF OF INSPECTED ACFT. SUGGEST A CHANGE IN DESIGN OF ASSY FOR POSITIVE ATTACHMENT OF SQUIB POWER SWITCH. NOTE: C ONDITION FOUND ON 2 ASSYS WOULD PREVENT FLIGHT CREW FROM BEING ABLE TO DISCHARGE AFFECTED ENG FIRE BOTTLES AT ANY TIME. THERE IS NO WAY FOR CREW TO PRE-FLIGHT SYS TO VERIFY THE FIRE BOTTLE SQUIBS COULD BE BLOWN IF NEEDED. 2 L 7 2 4T RT A24CE 2000021900316 20000404 00316 NM 2000 4 4 9905726302 1 19991223 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM BS 940 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING M-CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD, TOP FLANGE. REPAIRED PER EA63-173152. 2 L 7 4 4F RT A20WE 2000021900317 20000404 00317 NM 2000 4 4 9905736302 1 19991214 A 5320 FLOOR SUPPORT BOEING 747 747451 1384940 NM BS 480 - 520 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED PER EA 63-173153. 2 L 7 4 4F RT A20WE 2000021900318 20000404 00318 NM 2000 4 4 9905746302 1 19991223 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM BS 860 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING M-CHECK, FOUND CORROSION ON FLOORBEAM, UPPER CHORD. REPAIRED PER EA63-171416. 2 L 7 4 4F RT A20WE 2000021900364 20000219 00364 EU 2000 2 19 2000ZZZM155 1 19991208 A 5320 S5367800821602 ZEE AEROSP ATR72 ATR72212 EU FRAME 39-41 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 AFT CARGO BAY, RIGHT 'Z' MEMBER IS CORRODED. BLENDED OUT CORROSION IAW ATR 72 SRM. REMOVED AND REPLACED RIGHT 'Z' MEMB ER IN AFT CARGO BAY IAW ATR 72 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2000021900365 20000219 00365 EU 2000 2 19 2000ZZZM156 1 19991208 A 5320 S53671217334 SILL PLATE AEROSP ATR72 ATR72212 EU FRAME 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 PAX DOOR SILL CORRODED TOP AND BOTTOM. BLENDED OUT CORROSION ON SILL PLATE, (NOMINAL .071, REMAINING .061) IAW ATR 72 S RM 51-21-42. INSTALLED NEW DOOR SILL (WEB) IAW ATR 72 SRM 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000021900366 20000219 00366 EU 2000 2 19 2000ZZZM157 1 19991208 A 5320 S53671217336 DRAIN TRACK AEROSP ATR72 ATR72212 EU FRAME 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 PAX DOOR SILL DRAIN TRACK CORRODED. BLENDED OUT CORROSION ON SILL DRAIN TRACK, AND FOUND TO BE OUT OF LIMITS IAW ATR 72 SRM 51-21-42. INSTALLED PAX DOOR SILL DRAIN TRACK IAW ATR 72 SRM 51-25-01 AND 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000021900367 20000219 00367 EU 2000 2 19 2000ZZZM158 1 19991208 A 5315 S53672408254 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 FLOORBEAM NR 39, CORROSION AROUND NUTPLATES. BLENDED OUT CORROSION IAW ATR 72 SRM 51-21-58. INSTALLED NEW FLOORBEAM NR 39 IAW ATR 72 SRM 51-25-02. (M) 2 H 7 2 4T RT A53EU 2000021900368 20000219 00368 EU 2000 2 19 2000ZZZM159 1 19991208 A 5315 S53572407252 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 38 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 FLOORBEAM NR 38, CORROSION AROUND NUTPLATES. REMOVED AND BLENDED OUT CORROSION IAW ATR-72 SRM 51-21-58. REMOVED AND RE PLACED FLOORBEAM NR 38 IAW ATR-72 SRM 51-25-01, 51-25-03 AND 51-25-04. (M) 2 H 7 2 4T RT A53EU 2000021900369 20000219 00369 EU 2000 2 19 2000ZZZM160 1 19991208 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FRAME 36 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 FLOORBEAM NR 36, CORROSION AROUND NUTPLATES. REMOVED AND BLENDED OUT CORROSION IAW ATR-72 SRM 51-21-58. REMOVED AND RE PLACED FLOORBEAM NR 36 IAW ATR-72 SRM 51-25-05. (M) 2 H 7 2 4T RT A53EU 2000021900370 20000219 00370 EU 2000 2 19 2000ZZZM161 1 19991108 A 5320 S53671290422 SUPPORT AEROSP ATR42 ATR42300 8680920 EU 38/39 FRAME A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 AFT FLOOR SUPPORT CHANNEL ON PAX DOOR SILL PLATE IS CORRODED, IAW SRM 51-211-58. REMOVED AND INSTALLED NEW AFT FLOOR SU PPORT BETWEEN FRAME 38 AND 39 LEFT IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 2000021900371 20000219 00371 EU 2000 2 19 2000ZZZM162 1 19991026 A 5347 F95300013023 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FRAME 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 351AT 354 RIGHT FLIGHT ATTENDANT SEAT TRACK HAS CORROSION. BLENDED AFFECTED AREA IAW ATR 42 SRM 51-21-58 AND FOUND TO BE OUT OF L IMITS IAW ATR SRM 53-00-00 PAGE 314A. REPLACED RIGHT FLIGHT ATTENDANT SEAT TRACK IAW EO E9-5300-013R4. (M) 2 H 7 2 4T RT A53EU 2000021900372 20000219 00372 EU 2000 2 19 2000ZZZM163 1 19991026 A 5347 E95300013023 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FRAME 17-18 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 351AT 354 LEFT OUTBOARD FORWARD SEAT TRACK HAS CORROSION BETWEEN FLOORBEAMS, 17 AND 18. BLENDED AFFFECTED AREA IAW ATR 42 SRM 51- 21-58 AND FOUND TO BE OUT OF LIMITS IAW ATR SRM 53-00-00 PAGE 314A. REPLACED SEAT TRACK IAW EO NR E9-5300-013. (M) 2 H 7 2 4T RT A53EU 2000021900373 20000219 00373 EU 2000 2 19 2000ZZZM164 1 19991108 A 5311 S2397140226051 FRAME AEROSP ATR42 ATR42300 8680920 EU FRAME 27A CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 972NA 023 MLG FAIRING FRAME 27A HAS CORROSION (AS VIEWED FROM WHEEL WELL) BLENDED OUT AND FOUND TO BE BEYOND LIMITS IAW SRM 51-00- 00 TABLE 2. SPLICED FRAME 27A IAW SRM 53-91-43. MFG PART NUMBERS, LT S539702261, RT S53971402261 AND SEE BOX K. (M) 2 H 7 2 4T RT A53EU 2000021900374 20000219 00374 NM 2000 2 19 2000ZZZM165 1 19991119 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF ADJUST A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 429EX 19100 FLT 711 - EWR-IND - NR 3 ENGINE DETECTION GROUND LOOP LIGHT ILLUMINATES ON DESCENT THROUGH 10,000, THEN GOES BACK OUT. A DJUSTED NR 3 ENGINE FIRE PROTECTION DETECTION GROUND LOOP. (M) 2 L 7 3 4F A3WE 2000021900375 20000219 00375 NM 2000 2 19 2000ZZZM166 1 19991123 A 2612 1825280037525 FIRE LOOP BOEING 727 727172C 1384058 NM NR 3 ENGINE OUT OF ADJUST A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 527PC 19665 FLT 713 - CLT-IND - NR 3 DETECTION CIRCUIT GROUND LIGHT ON INTERMITTENTLY. ADJUSTED NR 3 ENGINE GROUND FAULT LIGHT CIRC UIT LOOP. (M) 2 L 7 3 4F A3WE 2000021900376 20000219 00376 NM 2000 2 19 2000ZZZM167 1 19991123 A 2612 182580037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF ADJUST A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 429EX 19100 FLT 9002 - SEA-IND - FIRE DETECTION CIRCUIT GROUND LIGHT NR 3 CAME ON DURING DESCENT THROUGH FL290. WENT OUT BELOW FL18 0. REPOSTIONED FIRE LOOP. (M) 2 L 7 3 4F A3WE 2000021900377 20000219 00377 NM 2000 2 19 2000ZZZM168 1 19991124 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 429EX 19100 FLT 710 - SEA-MSP - NR 3 DETECTOR CIRCUIT GROUND LIGHT ON IN FLIGHT. REPOSITIONED FIRE LOOP ON NR 3 ENGINE. DEFERRED I N MSP, CLEARED IN IND. (M) 2 L 7 3 4F A3WE 2000021900378 20000219 00378 NM 2000 2 19 2000ZZZM169 1 19991125 A 3110 308 BULB BOEING 727 727151C 138404V NM COCKPIT FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 432EX 19867 FLT 613 - GSO - SERVICE CHECK, SMOKE DETECTOR BULB INOPERATIVE. RELAMPED SMOKE DETECTOR LIGHTS. (M) 2 L 7 3 4F A3WE 2000021900379 20000219 00379 NM 2000 2 19 2000ZZZM170 1 19991125 A 2612 1825280037525 FIRE LOOP BOEING 727 727172C 1384058 NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 527PC 19665 FLT 719 - PHX-IND - NR 3 ENGINE FIRE PROTECTION AMBER WARNING LIGHT INTERMITTENT ILLUMINATES. REPOSITIONED NR 3 ENGINE GROUND FAULT LOOP. (M) 2 L 7 3 4F A3WE 2000021900380 20000219 00380 NM 2000 2 19 2000ZZZM171 1 19991128 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING DE DESCENT 1 CE 07 429EX 19100 FLT 9002 - TPA-IND - NR 3 FIRE DETECTION LIGHT CAME ON DURING DESCENT WHEN POWER IS PULLED BACK, GOES OUT WHEN POWER IS APPLIED. REPOSITIONED NR 3 ENGINE GROUND FAULT LOOP. (M) 2 L 7 3 4F A3WE 2000021900381 20000219 00381 NM 2000 2 19 2000ZZZM172 1 19991130 A 2613 356644400 ELEMENT BOEING 727 72777C 1380420 NM NR 3 ENG STRUT OUT OF ADJUST A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 526PC 20370 FLT 714 - CLE-IND - ON CLIMB-OUT, WITH ENGINE AND WING ANTI-ICE ON, NR 3 STRUT OVERHEAT LIGHT COMES ON. FOUND ENGINE 3 STRUT FIRE DETECTION LOOP ROUTED TO CLOSE TO DUCT, REPOSITIONED AND OPERATION CHECK GOOD ON GROUND. (M) 2 L 7 3 4F A3WE 2000021900382 20000219 00382 NM 2000 2 19 2000ZZZM173 1 19991130 A 2612 1825280037525 FIRE LOOP BOEING 727 72721 1384003 NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 329QS 19038 FLT 735 - DSM-IND - NR 3 ENGINE FIRE DETECTION GROUND FAULT LIGHT IS ILLUMINATED. REPOSITIONED NR 3 ENGINE FIRE LOOP, L IGHT EXTINGUISHED. (M) 2 L 7 3 4F A3WE 2000021900383 20000219 00383 NM 2000 2 19 2000ZZZM174 1 19991130 A 2612 1825280037525 FIRE LOOP BOEING 727 727172C 1384058 NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CL CLIMB 1 CE 07 527PC 19665 FLT 644 - DFW-IAH - NR 3 FIRE DETECTOR LIGHT IS ON. REPOSITIONED NR 3 ENIGNE SENSOR LOOP. (M) 2 L 7 3 4F A3WE 2000021900384 20000219 00384 NM 2000 2 19 2000ZZZM175 1 19991130 A 2612 1825280037525 FIRE LOOP BOEING 727 727172C 1384058 NM NR 3 ENGINE MISROUTED A RYNA O OTHER W N INADEQUATE Q C FALSE WARNING CL CLIMB 1 CE 07 527PC 19665 FLT 619 - IND-PHX - ENGINE NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ON. REROUTED FIRE DETECTOR LOOP (NR 3) FROM OIL LINE AND COWLING CONTACT. (M) 2 L 7 3 4F A3WE 2000021900385 20000219 00385 NM 2000 2 19 2000ZZZM176 1 19991202 A 2612 1825270037525 FIRE LOOP BOEING 727 727172C 1384058 NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 527PC 19665 FLT 610 - MSP-SEA - NR 3 GROUND FAULT DETECTOR LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 3 ENGINE SENSOR LOOP. (M) 2 L 7 3 4F A3WE 2000021900386 20000219 00386 NM 2000 2 19 2000ZZZM177 1 19991203 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING DE DESCENT 1 CE 07 429EX 19100 FLT 663 - IND-ORD - ENGINE NR 3 FIRE GROUND FAULT LIGHT ILLUMINATED DURING DESCENT. REPOSITIONED FIRE LOOP. (M) 2 L 7 3 4F A3WE 2000021900387 20000219 00387 NM 2000 2 19 2000ZZZM178 1 19991207 A 2612 1825280037525 FIRE LOOP BOEING 727 727134C 138404H NM NR 1 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING NR NOT REPORTED 1 CE 07 424EX 20042 FLT 731 - PHX-IND - NR 1 ENGINE DETECTOR CIRCUIT GROUND LIGHT ON CONTINUOUSLY. REPOSITIONED NR 1 ENGINE FIRE LOOP. (M) 2 L 7 3 4F A3WE 2000021900388 20000219 00388 NE 2000 2 19 2000ZZZM179 2 19991208 A 7200 ENGINE BOEING 727 727151C 138404V NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A RYNA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 07 432EX 19867 654806 FLT 608 - IND-IND - AFTER TAKEOFF, TOWER SAID OTHER AIRCRAFT REPORTED SPARKS AND DEBRIS FROM NR 1 ENIGNE. REPLACED NR 1 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000021900389 20000219 00389 EU 2000 2 19 2000ZZZM180 1 19991209 A 3350 D335916000087 SIGN AIRBUS 320 A320231 3930325 EU CABIN MALFUNCTIONED A RYNA O OTHER O OTHER CR CRUISE 1 CE 07 GSUEE 363 FLT 8810 - SJD-DEN - TRANSFER FROM CABIN DEFECTS LOG EXIT LIGHTS ABOVE AFT DOORS FLICKER AND TURN OFF INTERMITTENTLY. C OULD NOT DUPLICATE ON GROUND, PERFORMED BITE CHECK, CHECK OK. (M) 2 L 7 2 4F RT A28NM 2000021900390 20000219 00390 NM 2000 2 19 2000ZZZM181 1 19991211 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE OUT OF POSITION A RYNA K NONE N FALSE WARNING DE DESCENT 1 CE 07 429EX 19100 FLT 614 - CLE-BUF - NR 3 ENGINE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON DESCENT. COULD NOT DUPLICATE ON GROUND. R EPOSITIONED NR 3 ENGINE FIRE LOOP AND TESTED, OPERATION CHECK GOOD. (M) 2 L 7 3 4F A3WE 2000021900391 20000219 00391 NM 2000 2 19 2000ZZZM182 1 19991211 A 2612 1825280037525 FIRE LOOP BOEING 727 72751C 1384015 NM NR 3 ENGINE OUT OF ADJUST A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 436EX 19289 FLT 733 - ORD-IND - NR 3 FIRE PROTECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATES INTERMITTENTLY. ADJUSTED NR 3 FIRE L OOP. (M) 2 L 7 3 4F A3WE 2000021900392 20000219 00392 NM 2000 2 19 2000ZZZM183 1 19991214 A 2612 1825280037525 FIRE LOOP BOEING 727 72751C 1384015 NM NR 3 ENGINE OUT OF ADJUST A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 436EX 19289 FLT 720 - DTW-IND - NR 3 GROUND FAULT LIGHT CAME ON IN FLIGHT. FOUND LOOP CLOSE TO OTHER LINES, RE-ROUTED LOOP. (M) 2 L 7 3 4F A3WE 2000021900393 20000219 00393 NM 2000 2 19 2000ZZZM184 1 19991218 A 2612 1825280037525 FIRE LOOP BOEING 727 72782C 1384026 NM NR 3 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 528PC 19597 FLT 607 - IND-DEN - ENGINE NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATES SPORADICALLY IN FLIGHT. REPOSITIONED FIR E LOOP NR 3 ENGINE. (M) 2 L 7 3 4F A3WE 2000021900394 20000219 00394 NM 2000 2 19 2000ZZZM185 1 19991219 A 2612 1825280037525 FIRE LOOP BOEING 727 72751C 1384015 NM NR 2 ENGINE OUT OF POSITION A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 436EX 19289 FLT 607 - IND-DEN - NR 2 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATES INTERMITTENTLY. RE-SECURED AND RE-POSITIONED FI RE LOOP ON NR 2 ENGINE, GROUND CHECK GOOD. (M) 2 L 7 3 4F A3WE 2000021900395 20000219 00395 NM 2000 2 19 2000ZZZM186 1 19991225 A 3110 308 BULB BOEING 727 72722C 138400F NM COCKPIT FAILED A RYNA O OTHER O OTHER CR CRUISE 1 CE 07 428EX 19097 FLT 726 - MSP-IND - LIGHT INOPERATIVE ON LOWER SMOKE DETECTOR ON FLIGHT ENGINEERS PANEL. RELAMPED LOWER SMOKE DETECTOR ON FLIGHT ENGINEERS PANEL. (M) 2 L 7 3 4F A3WE 2000021900396 20000219 00396 NM 2000 2 19 2000ZZZM187 1 19991228 A 3110 308 BULB BOEING 727 727151C 138404V NM COCKPIT FAILED A RYNA O OTHER O OTHER CR CRUISE 1 CE 07 432EX 19867 FLT 715 - PIT-IND - LIGHT OUT ON TOP LEFT SIDE OF SMOKE DETECTOR. RELAMPED LIGHT ON LEFT SIDE OF SMOKE DETECTOR. (M) 2 L 7 3 4F A3WE 2000021900401 20000219 00401 WP 2000 2 19 ASAA9980271 1 19991123 A 5320 99305388N WEB DOUG DC9 DC983 3022083 WP BS 712-815 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSIN ON CUSP WEB FROM FS 712 TO 815, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTA LLED NEW PIECES IAW DC9 SRM 51-10-03. (M) 2 L 7 2 4F RT A6WE 2000021900402 20000219 00402 WP 2000 2 19 ASAA9980270 1 19991123 A 5320 993053823 WEB DOUG DC9 DC983 3022083 WP BS 598-712 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURNG 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 598 TO 712, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTA LLED NEW PIECES IAW DC0 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2000021900403 20000219 00403 WP 2000 2 19 ASAA9980285 1 19991129 A 5320 DOOR FRAME DOUG DC9 DC983 3022083 WP BS 370-427 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON FORWARD CARGO COMPARTMENT LOWER DOOR JAMB FROM FS 370 TO 427. REMOVED DAMAGE D MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05, FIG 44. (M) 2 L 7 2 4F RT A6WE 2000021900404 20000219 00404 WP 2000 2 19 ASAA9980283 1 19991129 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 1320 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON FLOORBEAM UNDER RIGHT AFT LAVATORY AT FS 1320. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 53-05 FIG 20A. (M) 2 L 7 2 4F RT A6WE 2000021900405 20000219 00405 WP 2000 2 19 ASAA9980284 1 19991129 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1193-1212 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1193 TO 1212, LONGERON 18R. REMOVED DAMAGED MATERIAL AND IN STALLED NEW PIECES IAW DC9 SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000021900406 20000219 00406 WP 2000 2 19 ASAA9980282 1 19991129 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 1079 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1079, BETWEEN LONGERONS 29L AND 29R. REMOVED DAMAGED MATERIAL AN D INSTALLED NEW PIECES IAW AMS EA 10-5310-0215. (M) 2 L 7 2 4F RT A6WE 2000021900412 20000219 00412 WP 2000 2 19 ASAA9980276 1 19991124 A 5320 5936068505 ANGLE DOUG DC9 DC983 3022083 WP BS 1250 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME ATTACH ANGLE AT FS 1250, LONGERON 28R. REMO VED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02 AND DRAWING 5936068. (M) 2 L 7 2 4F RT A6WE 2000021900413 20000219 00413 WP 2000 2 19 ASAA9980275 1 19991124 A 5347 6022044 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1041-1102 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1041 TO 1102. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2000021900414 20000219 00414 WP 2000 2 19 ASAA9980274 1 19991123 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 966 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 966, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIE CES IAW DC9 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2000021900415 20000219 00415 WP 2000 2 19 ASAA9980273 1 19991123 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 1211 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURIGN 30K CHECK, FOUND CORROSION ON FRAME AT FS 1211, BETWEEN LONGERONS 29L AND 30. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES IAW DC9 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2000021900416 20000219 00416 WP 2000 2 19 ASAA9980272 1 19991123 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1104-1136 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1104 TO 1136, LONGERON 18R. REMOVED DAMAGED MATERIAL AND IN STALLED NEW PIECES IAW DC9 SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000021900417 20000219 00417 WP 2000 2 19 ASAA9980277 1 19991116 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 503 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND GOUGE IN CABIN SEAT TRACK AT FS 503, LBL 44. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-04. (M) 2 L 7 2 4F RT A6WE 2000021900418 20000219 00418 WP 2000 2 19 ASAA9980279 1 19991128 A 5610 PIN DOUG DC9 DC983 3022083 WP COCKPIT DISLODGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 SEA - AFTR ARRIVAL OF FLT 160, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. REPOSITIONED H INGE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000021900419 20000219 00419 WP 2000 2 19 ASAA9980199 1 19991001 A 5610 PIN DOUG DC9 DC982 3022082 WP COCKPIT DISLODGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 955AS 48080 LAX - AFTER ARRIVAL OF FLT 414, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. RESEATED FORWA RD UPPER LATCH PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2000021900420 20000219 00420 WP 2000 2 19 ASAA9980197 1 19990930 A 5248 SPRING DOUG DC9 DC983 3022083 WP TAILCONE MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 PHX - DURING C-CHECK, THE TAILCONE DID NTO RELEASE DURING PERFORMANCE OF TAILCONE RELEASE TEST. FOUND AFT CABIN ENTRY D OOR PUSH-PULL CABLE INTERNAL RELEASE SPRING MISSING. INSTALLED SPRING AND ADJUSTED TAILCONE RELEASE MECHANISM, TAILCONE RELEASE OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000021900421 20000219 00421 WP 2000 2 19 ASAA9980252 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 984-1003 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 984 TO 1003, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000021900422 20000219 00422 WP 2000 2 19 ASAA9980251 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 965-984 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 965 TO 984, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 2000021900423 20000219 00423 NM 2000 2 19 ASAA9910273 1 19991218 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM BS 727B DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING SCHEDULED C-CHECK, THE FLOORBEAM AT STATION 727B BL 0 LOWER FLANGE WAS FOUND TO BE DAMAGED. REPAIRED PER E A 5310-01778 AND BOEING TELEX ASA-SEA-99-0412H. (M) 2 L 7 2 4F A16WE 2000021900424 20000219 00424 NM 2000 2 19 ASAA9940169 1 19991222 A 5210 DOOR BOEING 737 7374Q8 NM FUSELAGE LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 780AS 25112 PDX - PRIOR TO FLIGHT 419, THE L1 DOOR WAS FOUND TO BE HARD TO CLOSE. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2000021900425 20000219 00425 NM 2000 2 19 ASAA9940170 1 19991222 A 5210 SNUBBER BOEING 737 737490 1384715 NM PAX DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 768AS 27082 SEA - PRIOR TO FLT 457, THE L1 DOOR WAS DIFFICULT TO CLOSE. REPLACED THE L1 DOOR SNUBBER AND THE DOOR OPERATED NORMALLY . (M) 2 L 7 2 4F RT A16WE 2000021900426 20000219 00426 WP 2000 2 19 ASAA9980313 1 19991215 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1022 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, AFT SIDE OF MAIN FRAME WAS FOUND CORRODED AT THE ATTACH ANGLE TO LONG ERONS, STATION 1022, LONGERON 30. REPAIRED PER SRM 53-14-3. (M) 2 L 7 2 4F RT A6WE 2000021900427 20000219 00427 WP 2000 2 19 ASAA9980312 1 19991215 A 5320 TIE CLIP DOUG DC9 DC983 3022083 WP BS 1231 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, TOP OF MAIN FRAME TIE CLIP WAS FOUND CORRODED AT STATION 1231, LONGER ON 27R-28R. REPAIRED PER SRM 51-31-00. (M) 2 L 7 2 4F RT A6WE 2000021900428 20000219 00428 WP 2000 2 19 ASAA9980311 1 19991215 A 5320 SHEAR TIE DOUG DC9 DC983 3022083 WP BS 1041 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, FORWARD SIDE SHEAR TIE CLIP WAS FOUND CORRODED AT STATION 1041, LONGE RON 29L-30. REPAIRED AND REPLACED DAMAGED SHEAR TIE PER SRM 53-03, FIG 3. (M) 2 L 7 2 4F RT A6WE 2000021900429 20000219 00429 WP 2000 2 19 ASAA9980310 1 19991215 A 5320 J0602283 DOOR SILL DOUG DC9 DC983 3022083 WP BS 370-427 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS J0602283 53018 PHX - DURING 30K CHECK, THE FORWARD CARGO COMPARTMENT DOOR CUTOUT, LOWER SILL WAS FOUND CORRODED AROUND RIVET HOLES FROM STATION 370-427 ABOVE LONGERON 28R. REPAIRED PER SRM 53-05, FIG 44. (M) 2 L 7 2 4F RT A6WE 2000021900430 20000219 00430 WP 2000 2 19 ASAA9980309 1 19991215 A 5320 FITTING DOUG DC9 DC983 3022083 WP BS 712 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE FRAME SUPPORT FITTING, RIGHT STATION 712, L18 IS EXFOLIATED. REPAIRED PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2000021900431 20000219 00431 WP 2000 2 19 ASAA9980308 1 19991215 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 1231 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE FRAME AT STATION 1231, LONGERON 25L ON INTERCOSTAL AT ATTACH FLANGE OF IN TERCOSTAL. REPAIRED PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000021900432 20000219 00432 WP 2000 2 19 2000ZZZM192 1 19991206 A 5711 SPAR DOUG DC9 DC931 3022065 WP WS 164 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 967VJ 77354 47375 PIT - DURING C-3 CHECK, FOUND 1.3125 INCH LONG CRACK IN LOWER SPAR CAP, LEFT SIDE STATION 164. DETECTED BY EDDY CURRENT . INSTALLED DOUBLER PER JO60271-503 DRAWING/EO 577D348. (M) 2 L 7 2 4F A6WE 2000021900433 20000219 00433 WP 2000 2 19 USAA991387 1 19991212 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 658 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 72088 47508 PIT - DURING C-3 CHECK, FOUND CRACK .125 INCH LONGERON SKIN CRACK .15625 INCH AT STATION 658 LONGERON 2L. SPLICED LONGE RONS PER SRM 53-02 FIG 18 AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 2000021900434 20000219 00434 WP 2000 2 19 ASAA9980246 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 522 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON CUSP WEB AT FS 522, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INS TALLED DOUBLER IAW DC9 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000021900435 20000219 00435 WP 2000 2 19 ASAA9980247 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 569 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 569, LBL 58. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER I AW DC9 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000021900436 20000219 00436 WP 2000 2 19 ASAA9980248 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 572-579 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 572 TO 579, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INST ALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000021900437 20000219 00437 WP 2000 2 19 ASAA9980249 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 945 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB AT FS 945, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED DOU BLER IAW DC9 SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000021900438 20000219 00438 WP 2000 2 19 ASAA9980250 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 946-965 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 946 TO 965, LONGERON 18L. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-02. (M) 2 L 7 2 4F RT A6WE 2000021900439 20000219 00439 WP 2000 2 19 ASAA9980287 1 19991209 A 5610 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 963AS 53077 PDX - AFTER ARRIVAL OF FLIGHT 470, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. REPOSITION ED FORWARD UPPER BAYONET MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000021900440 20000219 00440 WP 2000 2 19 ASAA9980328 1 19991217 A 5610 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 963AS 53077 SEA - AFTER ARRIVAL OF FLIGHT 470, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. REPOSITION ED FORWARD UPPER GUIDE ARM INTO GUIDE SLOT AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000021900443 20000219 00443 NM 2000 2 19 USAABB99063 1 19991229 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROWS 1/9 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 CLT - FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE AT ROWS 1 AND 9. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 2000021900461 20000219 00461 SO 2000 2 19 AU990416020 1 19990319 A 3213 TORQUE LINK PIPER PA28 PA28140 7102802 SO LYC O320 O320E3D 41508 EA LT MLG SHEARED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 4110 L4657627A (AU) AIRCRAFT HAD LANDED AND PARKED. THE LEFT WING WAS MUCH HIGHER THAN THE RIGHT .UPON FURTHER INSPECTION THE TORQUE LINK HAD SHEARED FROM THE TRUNNION. UPPER PORTION WAS REPLACED BY A USED PART. LOWER OLEO, TORQUE LINK, AND LINKAGE WAS REUSED. PART GIVEN TO TRANSPORT FOR METAL ANALYSIS. PIPER SERVICE LETTER 760 NOVEMBER 12, 1975 REFERS TO THIS PROBLEM WHICH OCCURRED. 1 L 7 1 3O 3 O 2A13 E274 2000021900464 20000219 00464 CE 2000 2 19 AU990416026 1 19990405 A 3234 MS25125E3 SWITCH BEECH 95 D95A 1153408 CE LYC O360 IO360B1B 41514 EA COCKPIT FAILED W O OTHER O OTHER AP APPROACH 1 CA 1338 L285951A (AU) ON APPROACH, THE LANDING GEAR FAILED TO EXTEND ELECTRICALLY. THE LANDING GEAR MOTOR WAS REPLACED. SEVERAL FLIGHT S LATER THE SAME FAULT OCCURRED AGAIN. ON A SUBSEQUENT TEST, THE SELECTOR SWITCH WAS FOUND TO BE THE CAUSE. 1 L 7 2 3O 3 O 3A16 1E10 2000021900475 20000219 00475 NE 2000 2 19 AU990420019 2 19990408 A 7322 FCU PWA JT9D7R4D BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE MALFUNCTIONED W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA P709673 P709673 (AU) ON TAKEOFF, NR 2 ENGINE NEVER SPOOLED UP, BUT REMAINED AT IDLE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE NR 2 ENGINE FUEL CONTROL UNIT WAS REPLACED, LEAK CHECK AND CONTROL TRIM CHECKS WERE CARRIED OUT SERVIC EABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 2000021900476 20000219 00476 NE 2000 2 19 AU990420021 2 19990405 A 7230 712360 SPACER PWA JT9D7AH BOEING 747 747* NM PWA JT9 JT9D7AH 52054 NE COMPRESSOR UNAPPROVED PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 662936 662936 (AU) DURING INSPECTION A SPACER SUSPECTED OF BEING AN UNAPPROVED PART, WAS FOUND ON A JT9D ENGINE BELLCRANK. THE ENGINE HAD BEEN INDUCTED INTO THE SHOP FOR REFURBISHMENT. THIS PART IS CRITICAL TO ENGINE OPERATION BECAUSE IT IS HOLDING A R OD ATTACHED TO THE INLET GUIDE VANES. FAILURE OF THIS PART COULD CAUSE A SURGE WHICH COULD RESULT IN AN ENGINE IN-FLIGH T SHUTDOWN. THE SUSPECTED PART HAD FAILED A HARDNESS PER THE MAINTENANCE MANUAL. 2 L 7 4 4F 4 F RT A20WE E20EA 2000021900477 20000219 00477 NE 2000 2 19 AU990420022 2 19990403 A 7200 ENGINE PWA JT8D7A DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE NR 2 MALFUNCTIONED W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA P653454D P653454D (AU) NR 2 ENGINE HAD A PARTIAL POWER LOSS ON TAKEOFF. THE NR 1 ENGINE EPR WAS 1.95, THE NR 2 WAS 1.60, AND THE EXHAUST GAS TEMPERATURE WAS 100 DEGREES GREATER THAN THE NR 1 ENGINE. THE NR 2 ENGINE WAS REPLACED AND GROUND RUN SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 2000021900498 20000219 00498 EA 2000 2 19 AU991028042 1 19991002 A 3020 300013000002 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED W O OTHER O OTHER AP APPROACH 1 CA 807217 (AU) LEFT COWL ANT-I ICE FAILED. COWL ANTI-ICE VALVE REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2000021900499 20000219 00499 NM 2000 2 19 AU991103079 1 19991012 A 2780 92CV CONTROLLER CFMINT CFM565A5 AIRBUS A319 A319114 NM LE FLAP FAILED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 731973 (AU) FLIGHT CONTROLS SLATS LOCKED IN-FLIGHT WITH WING TIP BRAKE MESSAGE ON ECAM. REPLACED RELAYS 92CV AND 96CV. 2 L 7 2 4F RT A28NM 2000021900500 20000219 00500 NM 2000 2 19 AU991103080 1 19991013 A 3412 MPN102EH2EB TAT SENSOR AIRBUS A319 A319114 NM COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (AU) AUTOPILOT FLIGHT DIRECTOR ETC FAILED IN-FLIGHT. NR 1 TAT SENSOR REPLACED. 2 L 7 2 4F RT A28NM 2000021900501 20000219 00501 EU 2000 2 19 AU991103085 1 19991021 A 2742 MPN47045131 HSTA AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE VERTICAL STAB FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA 21726 731786 (AU) POST TAKEOFF ECAM MESSAGE, FLIGHT CONTROL ELEVAT0OR AILERION COMPUTER FAULTS 1 AND 2. AIRCRAFT DIVERTED AND LANDED . REPLACED HORIZONTAL STABILIZER PITCH TRIM ACTUATOR (HSTA). 2 L 7 2 4F 4 F RT A28NM E29NE 2000021900502 20000219 00502 EU 2000 2 19 AU991103086 1 19991023 A 5270 ABS012110 PROX SENSOR AIRBUS AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE RT MLG DOOR FAILED W K NONE O OTHER LD LANDING 1 CA 731670 (AU) RIGHT GEAR DOOR REMAINED OPEN ON LANDING. PROXIMITY SENSOR REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2000021900505 20000219 00505 EU 2000 2 19 AU000120034 1 19990917 A 2913 704A33690004 BELT SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A3 41560 NE HYD PUMP DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 293 LE43177CE (AU) HYDRAULIC PUMP BELT WAS NOTED TO BE COMING APART AT THE SEAM. THERE HAVE BEEN A NUMBER OF PROBLEMS WITH THESE BELTS FAILING PREMATURELY. 1 G 7 1 3U 3 U H9EU E5NE 2000021900514 20000219 00514 WP 2000 2 19 AU000128021 2 19991118 A 7200 NAS5094 NUT 3219012127 FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE LT ENGINE NOT SAFETIED W D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 258 P70269 981662 (AU) THE LEFT ENGINE DID NOT RESPOND WHEN THE SPEED LEVER WAS ADVANCED FOR TAKEOFF. THE SPEED LEVER CONTROL CABLE WAS FO UND DISCONNECTED FROM THE BALL JOINT. THE RIGHT ENGINE SPEED LEVER CABLE WAS FOUND TO BE MISSING THE JAM NUT AND THE RE MAINING NUT WAS NOT SAFETY WIRED. ACFT TOTAL TIME: 257 HOURS . 2 L 7 2 4T 4 T RT A18SW E4WE 6 C 3PNE 2000021900522 20000219 00522 SO 2000 2 19 AU000128042 2 19991214 A 8530 653446A1 CYLINDER CESSNA 206 U206D 2073342 CE CONT O520 IO520F 17032 SO MCAULY 2A34C D2A34C58 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 562 FC05132 552992 770088 (AU) CYLINDER FOUND CRACKED AT UPPER SPARK PLUG HOLE MOVING FORWARD PAST THE INBOARD SIDE OF THE INJECTOR HOLE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P3EA 2000021900532 20000219 00532 CE 2000 2 19 AU000128062 1 19991215 A 2750 1013800006 FLEX DRIVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TE FLAP BROKEN W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 8300 GGMPS0054 (AU) AFTER LANDING , THE PILOT SELECTED THE FLAP UP AND THEY JAMMED AT 17 DEGREES. INVESTIGATION FOUND THE R/T OUTBOARD FLAP FLEX DRIVE WAS BROKEN APPROXIMATELY 24INCHES FROM THE END. DAMAGED PARTS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 2000021900537 20000219 00537 CE 2000 2 19 AU000201009 1 19991217 A 2823 1013890253 VALVE BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1083 PCE25272 (AU) FUNCTIONAL CHECK OF FIREWALL SHUT-OFF VALVE DURING MAINTENANCE CHECK (D.I.)REVEALED THAT AFTER 2 SECONDS, FUEL PRES SURE LIGHT WENT OUT INDICATING FUEL BYPASSING THE VALVE. VALVE REPLACED. 1 L 7 2 3T 4 T RT 3A20 E4EA 2000021900538 20000219 00538 CE 2000 2 19 AU000201010 1 19991222 A 2823 1013890253 VALVE ELECTROMECH BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA FUEL SYSTEM FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 4 2549 PCE25272 (AU) FUNCTION CHECKED OK IN HANGAR. FAILED 4.0 HRS AIR TIME. VALVE REPLACED. 1 L 7 2 3T 4 T RT 3A20 E4EA 2000021900546 20000219 00546 CE 2000 2 19 AU000203005 1 19991228 A 3250 50820035 ROD BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA NLG STEERING CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 18727 PCE41762 (AU) ROD CORRODED AT CLOSED END. CORROSION PERFORATED THE TUBE WALL A HALF INCH FROM THE END. 1 L 7 2 3T 4 T A14CE E4EA 2000021900571 20000219 00571 EU 2000 2 19 SIMA3623 1 19991223 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 377AT 1012 377 MIA - FLT 5356 - EMERGENCY EXIT LIGHT ON DURING FLIGHT. REMOVED AND REPLACED BATTERY IN SUPPLY UNIT. OPS CHECK GOOD. ( M) 2 H 7 2 4T RT A53EU 2000021900572 20000219 00572 2000 2 19 USAAD99187 4 19991225 A 2565 D29985103 SLIDE DOUG DC9 DC981 3022081 WP SERVICE DOOR MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 PIT - THE AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE FAILED TO INFLATE IN ALLOCATED TIME DUE TO DELAYED START OF INFLAT ION AFTER DOOR OPENING. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 2000021900573 20000219 00573 2000 2 19 USAAD99188 4 19991228 A 2565 D29984213 SLIDE DOUG DC9 DC982 3022082 WP TAIL WON'T TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 824US 49143 PIT - THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED TO AUTO DEPLOY, MANUAL DEPLOYMENT NORMAL. MAINTENANCE REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 2000021900577 20000219 00577 NM 2000 2 19 USAASB99308 1 19991231 A 5610 5893543110 WINDSHIELD BOEING 737 7373B7 1384580 NM COCKPIT CRACKED A USAA A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 EA 19 387US 20655 22959 DCA - FLT 6443 - EN ROUTE FROM BOS-IAD, AT CRUISE ALTITUDE, THE FIRST OFFICERS NR 1 WINDSHIELD CRACKED AND ARCED AT THE TOP SIDE OF THE WINDOW. CRACKS BEGAN TO TRAVEL THROUGHOUT THE WINDSHIELD. FLIGHT DIVERTED TO DCA AND LANDED WITHOUT FU RTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS NR 1 WINDSHIELD PER JOB CARD J356-11-01 AND MM 56-11-11. ALSO, REMOVED AND REPLACED THE FIRST OFFICERS WINDOW HEAT CONTROLLER (P/N 83000-05602 ) AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2000021900578 20000219 00578 NM 2000 2 19 USAASB99309 1 19991231 A 3234 SELECTOR BOEING 737 737301 1384611 NM COCKPIT LACK OF LUBE A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 336US 23233 PIT - FLT705 - ON APPROACH INTO PIT, AS LANDING GEAR WAS SELECTED DOWN, ALL THREE GEAR SHOWED SIMULTANEOUS RED AND GREEN INDICATIONS. CREW BROKE OFF APPROACH AND ACCOMPLISHED CHECKLIST PROCEDURES. GEAR WAS VISUALLY OBSERVED DOWN THROUGH V IEWPORTS AND BY TOWER. FLIGHT LANDED AT PIT WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND TH E LANDING GEAR SELECTOR HANDLE NOT ALL THE WAY IN DETENT. LUBRICATED GEAR SELECTOR HANDLE. OPERATIONAL CHECK GOOD. (M ) 2 L 7 2 4F RT A16WE 2000021900579 20000219 00579 NM 2000 2 19 USAASB99305 1 19991227 A 2612 355604310 FIRE LOOP BOEING 737 737301 1384611 NM RT ENGINE FAILED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 354US 23557 MCI - FLT 328 - AFTER TAKEOFF FROM MCI, THE RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THREE MINUTES LATER, THE LEF T WING TO BODY OVERHEAT LIGHT ILLUMINATED AND A STRONG BURNING SMELL WAS PRESENT IN THE COCKPIT. FLIGHT RETURNED TO FIE LD AT MCI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED OVERHEAT LO OP M1204 IN THE RIGHT ENGINE PYLON FOR THE RIGHT WING TO BODY OVERHEAT. OPERATIONAL CHECK GOOD. COULD NOT DUPLICATE LE FT WING TO BODY OVERHEAT. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2000021900580 20000219 00580 EU 2000 2 19 USAAF99059 1 19991231 A 2820 SWITCH FOKKER F28 F28MK0100 4990807 EU COCKPIT OUT OF POSITION A USAA A UNSCHED LANDING W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 887US 11349 CLT-IAH - FLT 463 - DURNG CLIMB-OUT FROM CLT, CAPTAIN RECEIVED AUTO FUEL CROSSFEED FAIL ALERT. ALSO, CLT TOWER ADVISED THAT THERE WAS SUBSTANTIAL FUEL ESCAPING FROM WINGS. SEVERAL TURNS WERE MADE TO BURN FUEL TO REACH LESS THAN MAXIMUM LA NDING WEIGHT. FLIGHT RETURNED TO FIELD FOR A NORMAL LANDING. MAINTENANCE FOUND THE FORWARD REFUELING PANEL SWITCH IN T HE ON POSITION. RETURNED SWITCH TO THE OFF POSITION. FUELING PANEL FOUND OK. (M) 2 L 7 2 4F RT 2000021900583 20000219 00583 NM 2000 2 19 USAA991383 1 19991124 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 53483 21817 TPA - DURING CX-3 CHECK, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727A PLUS 8 AT STRINGER 18R. INSTALLED REPAIR D OUBLER PER SRM, DOUBLE MADE FROM 2024-T3 .071 PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 2000021900584 20000219 00584 WP 2000 2 19 ASAA9980307 1 19991215 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP BS 1287 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON SUPPORT IN AFT CARGO PIT AT STATION 1287, 28R. REPAIRED AND REPLACED DAMAGED BRACKET PER SRM 51-30-00. (M) 2 L 7 2 4F RT A6WE 2000021900585 20000219 00585 WP 2000 2 19 ASAA9980306 1 19991215 A 5320 BRACKET DOUG DC9 DC983 3022083 WP BS 1220 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION AT STATION 1220 BETWEEN LONGERON 28R AND 27R, ON AND AROUND FASTENER COMMON TO C ARGO TRACK BRACKET. REPAIRED AND REPLACED DAMAGED BRACKET PER SRM 53-01.. (M) 2 L 7 2 4F RT A6WE 2000021900586 20000219 00586 WP 2000 2 19 ASAA9980305 1 19991215 A 5320 SHEAR TIE DOUG DC9 DC983 3022083 WP BS 1174 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION IN THE AFT CARGO COMPARTMENT AT THE MAIN FRAME SHEAR TIE CLIP, FORWARD AND AFT, STATION 1174, LONGERON 29L-29R. REPAIRED AND REPLACED DAMAGED SHEAR CLIP PER SRM 57-10, 53-14-3 AND 53-30. (M) 2 L 7 2 4F RT A6WE 2000021900587 20000219 00587 WP 2000 2 19 ASAA9980304 1 19991215 A 5320 SHEAR TIE DOUG DC9 DC983 3022083 WP BS 1193 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION IN THE AFT CARGO COMPARTMENT AT THE MAIN FRAME SHEAR TIE CLIP, FORWARD AND AFT, STATION 1193, LONGERON 28L-29R. REPAIRED AND REPLACED DAMAGED SHEAR TIE AD CLIP PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2000021900588 20000219 00588 WP 2000 2 19 ASAA9980303 1 19991215 A 5320 TIE CLIP DOUG DC9 DC983 3022083 WP BS 1117 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FUOND CORROSION IN THE AFT CARGO COMPARTMENT ON TOP OF THE INTERCOSTAL TIE CLIP, STATION 1117, L ONGERON 28R. REPLACED DAMAGED TIE CLIP PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2000021900589 20000219 00589 WP 2000 2 19 ASAA9980302 1 19991215 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 1309-1322 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION IN THE AFT CARGO PIT ON THE INTERCOSTAL, STATION 1309 - 1322, LONGERON 28L. REP AIRED PER SRM 53-24-0, FIG 11. (M) 2 L 7 2 4F RT A6WE 2000021900590 20000219 00590 WP 2000 2 19 ASAA9980301 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1150 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1150, LONGERON 18R. REPAIRED AND INSTALLED DOUBLER REP AIR PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000021900591 20000219 00591 WP 2000 2 19 ASAA9980300 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1098-1117 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1098 TO 1117 RIGHT, LONGERON 18. INSTALLED DOUBLER REP AIR PER SRM 51-01 AND 51-30. (M) 2 L 7 2 4F RT A6WE 2000021900592 20000219 00592 WP 2000 2 19 ASAA9980299 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1060-1079 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1060 TO 1079 RIGHT, LONGERON 18. INSTALLED DOUBLER REP AIR PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000021900593 20000219 00593 WP 2000 2 19 ASAA9980298 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 712-731 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 712 TO 731 RIGHT, LONGERON 18. INSTALLED DOUBLER REPAI R PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000021900594 20000219 00594 WP 2000 2 19 ASAA9980297 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 665 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 665 TO 674 RIGHT, LONGERON 18. REPAIRED PER SRM 53-01. . (M) 2 L 7 2 4F RT A6WE 2000021900595 20000219 00595 WP 2000 2 19 ASAA9980296 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1183 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 1183, LEFT LONGERON 18. REPAIRED CORRODED SECTION OF W EB AND SPLICE PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000021900596 20000219 00596 WP 2000 2 19 ASAA9980295 1 19991215 A 5310 WEB DOUG DC9 DC983 3022083 WP BS 545-560 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 545-560, LEFT LONGERON 18. REPAIRED AND INSTALLED DOUB LER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000021900597 20000219 00597 WP 2000 2 19 ASAA9980294 1 19991215 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 478 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION ON THE CUSP WEB, STATION 478, LEFT LONGERON 18. REPAIRED AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000021900598 20000219 00598 NM 2000 2 19 ASAA9910269 1 19991218 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 DURING SCHEDULED C-CHECK, THE FLOORBEAM AT STATION 540-727B LBL 45.75 WAS FOUND CORRODED. REPAIRED PER EA 5310-01754, B OEING TELEX ASA-SEA-99-00371H, AND BOEING TELEX ASA-SEA-99-00372H. (M) 2 L 7 2 4F A16WE 2000021900599 20000219 00599 NM 2000 2 19 ASAA9910268 1 19991218 A 5320 BEAM BOEING 737 737290C 138448V NM BS 663 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING SCHEDULED C-CHECK, THE STUB BEAM AT STATION 663 RBL 45-60 WAS FOUND TO BE CORRODED. REPAIRED PER E 5310-01 747 AND BOEING TELEX ASA-SEA-99-00346H. (M) 2 L 7 2 4F A16WE 2000021900600 20000219 00600 NM 2000 2 19 ASAA9910267 1 19991218 A 5260 HINGE BOEING 737 737290C 138448V NM AIRSTAIR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING SCHEDULED C-CHECK, THE AFT AIRSTAIR AFT HINGE ARM LOWER FLANGE WAS FOUND CORRODED. REPAIRED PER EA 5260-01 078 AND BOEING TELEX ASA-SEA-99-00326H. (M) 2 L 7 2 4F A16WE 2000021900601 20000219 00601 NM 2000 2 19 ASAA991268 1 19991218 A 5320 BEAM BOEING 737 737290C 138448V NM BS 663 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING SCHEDULED C-CHECK, THE STUB BEAM AT STATINO 663 RBL 45-60 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-0 1747 AND BOEING TELEX ASA-SEA-99-00346H. (M) 2 L 7 2 4F A16WE 2000021900602 20000219 00602 WP 2000 2 19 ASAA9980293 1 19991215 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 598-658 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION AROUND FASTENER AT THE MID CARGO BAY, LONGERON 30, FROM STATION 598 TO 658. REP LACED DAMAGED LONGERON SECTION FROM STATION 588 TO 665 AND A SPLICE AT STATION 664.5 PER EA 5310-01764. (M) 2 L 7 2 4F RT A6WE 2000021900603 20000219 00603 WP 2000 2 19 ASAA9980292 1 19991215 A 5320 SPLICE DOUG DC9 DC983 3022083 WP BS 579-598 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURNG 30K CHECK, FOUND CORROSION ON LONG SPLICE AT THE MID CARGO BAY, LONGERON 30, FROM STATION 579 TO 598. REPLA CED LONG SPLICE PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2000021900604 20000219 00604 WP 2000 2 19 ASAA9980291 1 19991215 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 1338 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON TOP SURFACE OF FLOOR STRUCTURE, STATION 1338 RIGHT AT RBL 41 AND RB L 49. REPAIRED FLOORBEAM PER AMS EA 10-5310-0227, ASA EA 5310-01762. (M) 2 L 7 2 4F RT A6WE 2000021900605 20000219 00605 2000 2 19 ASAA9980331 4 19991220 A 2565 BOTTLE DOUG DC9 DC983 3022083 WP ESCAPE SLIDE DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 PDX - DURING MAINTENANCE CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. R EPLACED THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2000021900606 20000219 00606 WP 2000 2 19 ASAA9980225 1 19991101 A 5610 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 955AS 48080 OAK - PRIOR TO DEPARTURE OF FLIGHT 325, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. REINST ALLED FORWARD UPPER GUIDE PIN IN TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2000021900607 20000219 00607 WP 2000 2 19 ASAA9980227 1 19991102 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 712 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PHX - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT FS 712 BETWEEN LONGERONS 28L AND 28R. REMOVED DAMAGED MATERIAL AN D INSTALLED NEW PIECES IAW ASA EA 5310-01722. (M) 2 L 7 2 4F A6WE 2000021900608 20000219 00608 WP 2000 2 19 ASAA9980228 1 19991102 A 5720 FITTING DOUG DC9 DC982 3022082 WP WS 195 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PHX - DURING C-CHECK, FOUND CRACK ON RIGHT WING LEADING EDGE RIB FITTING AT XFS 195. REPAIRED IAW ASA EA 5740-01182. ( M) 2 L 7 2 4F A6WE 2000021900677 20000219 00677 WP 2000 2 19 RRXA991751 1 19990612 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 718 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERIOR SKIN PANEL AT Y=718 AND LONGERON 35 RIGHT. DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900678 20000219 00678 WP 2000 2 19 RRXA991752 1 19990719 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERIOR SKIN PANEL BETWEEN Y=857 TO Y=980 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900818 20000219 00818 WP 2000 2 19 RRXA991775 1 19990921 A 5754 SKIN DOUG DC8 DC871F 302199D WP LE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, TOP SKIN AT XFS=793. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED ENGINEERING SKETCH EO 99-174. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900819 20000219 00819 WP 2000 2 19 RRXA991776 1 19990918 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT SKIN CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, SKIN SECTION AT XW=693 AND BETWEEN STRINGERS 2 TO 4. CO RROSION DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO 99-174. 2 L 7 4 4F RT 4A25 2000021900820 20000219 00820 WP 2000 2 19 RRXA991777 1 19990916 A 5754 SKIN DOUG DC8 DC871F 302199D WP LE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, INBOARD FLAP, TOP SKIN AT XW=5. DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-7-0. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900821 20000219 00821 WP 2000 2 19 RRXA991779 1 19991102 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 69 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA=-69 BETWEEN BL=0 TO BL=45L AND WL-9.5. DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE I AW FAA APPROVED DER ENGINEERING SKETCH EO 99-174. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900822 20000219 00822 WP 2000 2 19 RRXA991780 1 19991022 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 980 - 995 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 980 TO STA 995 AND LONGERON 35 LEFT. DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW IN TERCOSTAL IAW DC-8 SRM 53-2-1. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900823 20000219 00823 WP 2000 2 19 RRXA991781 1 19991006 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1280 AND LONGERON 35 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 5 1-1-21. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900824 20000219 00824 WP 2000 2 19 RRXA991782 1 19990924 A 5320 FINGER DOUBLER DOUG DC8 DC871F 302199D WP BS 25 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA -25 AND BL 36L AND WL -9. DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DC-8 SRM 53-3-1. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900825 20000219 00825 WP 2000 2 19 RRXA991783 1 19991003 A 5230 BOLT DOUG DC8 DC871F 302199D WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CARGO DOOR T-BOLT BETWEEN STA 280 TO STA 340 AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW T-BOLT AND INSTALLED DC-8 SRM 52-34-1. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900826 20000219 00826 WP 2000 2 19 RRXA991784 1 19991001 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1420 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 53-2- 0. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900827 20000219 00827 WP 2000 2 19 RRXA991785 1 19991008 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 520 - 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 520 TO STA 540 AND LONGERON 32 RIGHT. DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW I NTERCOSTAL IAW DC-8 SRM 51-1-4. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900828 20000219 00828 WP 2000 2 19 RRXA991786 1 19991103 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 340 TO STA 346. DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SR M 53-2-3. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900829 20000219 00829 WP 2000 2 19 RRXA991787 1 19991103 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 1240 - 1348 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 1240 TO STA 1348 AND BETWEEN BL 48L TO BL 6 2L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900830 20000219 00830 WP 2000 2 19 RRXA991788 1 19991103 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 40 - 80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 40 TO STA 80 AND BETWEEN BL 56L TO BL 68L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900831 20000219 00831 WP 2000 2 19 RRXA991789 1 19991103 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 750 - 860 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 750 TO STA 860. DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SR M 53-2-3. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900832 20000219 00832 WP 2000 2 19 RRXA991790 1 19991103 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP BS 660 - 750 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 660 TO STA 750. DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SR M 53-2-3. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000021900833 20000219 00833 WP 2000 2 19 RRXA991791 1 19990916 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 70 AND BL 18R. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2 -3. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM. 2 L 7 4 4F RT 4A25 2000022300001 20000223 00001 NM 2000 2 23 SWAA992135 1 19991226 A 5311 6546546 FRAME BOEING 737 7373K2 13844BA NM BS 767,787 & 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 340LV 23738 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAMES CRACKED, BS 907, BS 787, AND BS 767 ABOVE STRINGER 9L. REPAIRE D FRAMES PER ER NR 99-6410, AND SRM. 2 L 7 2 4F RT A16WE 2000022300007 20000223 00007 NM 2000 2 23 QXEA9902692 1 19991217 A 5330 ICE SHIELD DHAV DHC8 DHC8102 2809003 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - TWO DEEP SCRATCHES FOUND ABOVE RIGHT ICE SHIELD. REPAIRED IAW HORIZON AIR EA 9-53-530. 2 H 7 2 4T RT A13NM 2000022300008 20000223 00008 NM 2000 2 23 QXEA9902695 1 19991220 A 5400 WEB DHAV DHC8 DHC8102 2809003 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 285PH 213 PDX - TOP EXHAUST DECK HAS CHAFE HOLE CENTER OF DECK AT RIVET LINE. REPAIRED IAW RD8-54-866. 2 H 7 2 4T RT A13NM 2000022300009 20000223 00009 EU 2000 2 23 QXEA9902723 1 19991229 A 5300 FRAME FOKKER F28 F28MK4000 4990810 EU BS 16660 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CHAFE DAMAGE ON UPPER FLANGE OF FRAME 16660 AT STRINGER 47. REPAIRED IAW HORIZON AIR EA 4-53-953. 2 L 7 2 4F RT A20EU 2000022300012 20000223 00012 NM 2000 2 23 AT9900923 1 19991223 A 3350 LIGHT BOEING 717 717200 1383700 NM SEAT 11 INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 947AT 55010 FOUND ROW 11 EMERGENCY PATH LIGHT INOPERATIVE, PINCHED BETWEEN SEAT AND SEAT TRACK. SPLICED NEW WIRE IAW B717 MPS 1465 AND STANDARD WIRING MANUAL 20-10-03. 2 L 7 2 4F TR A6WE 2000022300017 20000223 00017 CE 2000 2 23 CA991208073 1 19991108 A 2752 100384040 ACTUATOR ELECTROMECH 1005240731 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCB3T HCB3TN3 GL TE FLAP BURNT W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 2527 2241 PCE80016 BU7545 (CAN) AIRCRAFT FLAPS WERE LOWERED FOR PRE-FLIGHT WALK AROUND INSPECTION. DURING THE COCKPIT PRE-FLIGHT INSPECTION, THE FLAP MOTOR CIRCUIT BREAKER POPPED OUT. THE C/B WAS RESET AND APPEARED OK. THE STDB ENGINE WAS STARTED AND THEN THE POR T ENGINE. SMOKE WAS SMELLED IN THE COCKPIT AND THEN VISUALLY OBSERVED. THE AIRCRAFT WAS SHUT DOWN AND MAINTENANCE CALL ED. MAINTENANCE CHECKS WERE COMPLETED AND THE MOTOR FOUND BURNT. FLAP MOTOR AND GEARBOX ASSY. REPLACED AND FLAP SYS TEM FUNCTION CHECKED SERVICEABLE. 1 L 7 2 4T 4 T A24CE E4EA 6 C P15EA 2000022600001 20000226 00001 NM 2000 2 26 GAIA99209 1 19991123 A 5310 STRUCTURE BOEING 727 727287 1384020 NM FUSELAGE DAMAGED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 916PG 21690 AIRCRAFT FELL FROM JACKS. INSPECTED AND REPAIRS ACCOMPLISHED PER AVITAS REPAIR ORDER 99AVHM.059R0-1, REV A 8110-3 DTD 1 1/21/99 N/R 2998. (X) 2 L 7 3 4F RT A3WE 2000022600002 20000226 00002 NM 2000 2 26 GAIA99176 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 219.80 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 SKIN DENTS AT BS 211.8 AND BS 219.80 JUST LWR OF LWR RT PITOT TUBE. INSTALLED DOUBLER REPAIR AT BS 219.8 EXTERIOR FUSEL AGE SKIN JUST LWR OF THE LWR RT PITOT TUBE. MATERIAL USED 2024-T3, 0-.050 INCH, 9 INCH BY 9 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. REF: N/R 3580 FOR DETAILS. NO DENT FOUND ON STA 211.8. (X). 2 L 7 3 4F RT A3WE 2000022600003 20000226 00003 NM 2000 2 26 GAIA99177 1 19991123 A 5753 CARRIAGE BOEING 727 727287 1384020 NM TE FLAP CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 LEFT WING INBOARD FLAP. MID-FLAP NR 11 RIB LOCATED BY NR 4 FLAP. CARRIAGE COMPARTMENT HAS A CRACK. INSTALLED CARRIAGE DOUBLER REPAIR AT LT WING INBOARD FLAP, MID-FLAP NR 11 RIB LOCATED BY THE NR 4 FLAP CARRIAGE. REPAIR ACCOMPLISHED IAW SRM 57-50-4 FIG 2. REF: NON-ROUTINE 1845 FOR DETAILS. (X) 2 L 7 3 4F RT A3WE 2000022600004 20000226 00004 NM 2000 2 26 GAIA99178 1 19991123 A 5330 SKIN BOEING 727 727287 1384020 NM BS 400 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 CHECK INTEGRITY OF FLUSH MP PATCH REPAIR PREVIOUSLY MADE AT BS 400 BETWEEN STR 21R AND STR 22R. REPLACED FLUSH REPAIR A T BS 400 BETWEEN STR 21R AND STR 22R. REPAIR ACCOMPLISHED IAW SRM 53-30-2 FIG 2. REF: N/R 3585 FOR DETAILS. (X) 2 L 7 3 4F RT A3WE 2000022600005 20000226 00005 NM 2000 2 26 GAIA99179 1 19991123 A 5320 SHEAR PLATE BOEING 727 727287 1384020 NM BS 1110-1130 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 916PG 21690 LEFT AFT LAVATORY FLOOR - MANY AREAS OF CORROSION AND CORROSION ON ALL WALL SUPPORT ANGLES. REPLACED SECTION OF SHEAR P LATE FROM BS 1130 TO BS 1176, FROM LBL 15 TO LBL 68.5. REPAIR ACCOMPLISHED IAW SRM 51-10-1 PARA 4 AND SRM 51-30-2. REP LACED SECTION OF SEAT TRACK FROM BS 1110 TO BS 1130 FROM BL L24 TO BL L48. REPAIR ACCOMPLISHED IAW SRM 53-10. (X) 2 L 7 3 4F RT A3WE 2000022600006 20000226 00006 2000 2 26 2000ZZZX424 4 19991223 A 3422 6226136002 GYRO COLLINS BEECH 1900 1900D 1154162 CE COCKPIT STUCK A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 843CA 2576 3170 UE43 CAPTAIN'S HEADING INDICATOR STUCK. REPLACED DGS-65. SYSTEM CHECKS SATISFACTORY. 2 L 7 2 4T RT A24CE 2000022600007 20000226 00007 2000 2 26 2000ZZZX425 4 19991221 A 6122 1223890373 GOVERNOR WOODWARD BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A JJBA K NONE L NO TEST IN INSP/MAINT 1 EA 01 855CA 1665 2490357 UE61 RIGHT ENGINE OVERSPEED GOVERNOR WILL NOT TEST. REPLACED GOVERNOR WITH OVERHAULED UNIT. OPERATIONAL AND LEAK CHECK SATI SFACTORY. 2 L 7 2 4T RT A24CE 2000022600008 20000226 00008 NE 2000 2 26 2000ZZZX426 2 19991223 A 7314 1143890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 842CA 160 B1558 UE41 FUEL LEAK RIGHT ENGINE NACELLE. FOUND LOW PRESSURE FUEL PUMP LEAKING. REMOVED AND REPLACED UNIT, SYSTEM LEAK AND OPS C HECK SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2000022600010 20000226 00010 NM 2000 2 26 K4HA99096 1 19990802 A 5753 65B12736126 SKIN BOEING 747 747146 NM RT WING CRACKED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 IAB - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND RIGHT WING LEADING EDGE SKIN AT WS 1 310 AT THE UPPER EDGE INSIDE OF THE 65B12736-126, ON SKIN PANEL THERE IS A 1 INCH BY 2 INCH AREA OF SEVERE EXFOLIATED CO RROSION. THREE CRACKS FOUND. WORKED REPAIR PER ENG DISPOSITION AND SRM 5720-03. (X) 2 L 7 4 4F A20WE 2000022600011 20000226 00011 NM 2000 2 26 K4HA99094 1 19990802 A 5730 SKIN BOEING 747 747146 NM WING CORROSION A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 IAB - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP CARDS, FOUND THE FLANGE OF THE ACCESS HOLES HAS MODERA TE TO SEVERE CORROSION AND DETERIORATION AROUND THE PERIMETER OF THE DOOR MATING SURFACE. AREA OF CORROSION REMOVAL IS BEYOND LIMITS OF SRM 57-30-03. ACCOMPLISHED A 10X VISUAL INSPECTION TO ENSURE THAT ALL CORROSION HAD BEEN REMOVED IAW SRM 57-30-03. (X) 2 L 7 4 4F A20WE 2000022600012 20000226 00012 NE 2000 2 26 2000ZZZX427 2 19990503 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MA 590 7107 LE45126EA SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000022600013 20000226 00013 NE 2000 2 26 2000ZZZX428 2 19990503 A 7250 410106802 SPRING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE RING EXPANDER WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MA 590 7107 LE45126EA SPRING WORN BEYOND SERVICEBLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000022600014 20000226 00014 EU 2000 2 26 2000ZZZX429 1 19991030 A 6410 704A33633116 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5771C 434 1369 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM KIT 355A09-1036-01, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000022600015 20000226 00015 EU 2000 2 26 2000ZZZX430 1 19990728 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 449 2728 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000022600016 20000226 00016 EU 2000 2 26 2000ZZZX431 1 19991118 A 7720 L772M10C1005 INDICATOR UROCOP EC135 EC135P1 8680990 EU TOT STICKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 570 0020 EC1350054 BOTH NEEDLES STICK INTERMITTENTLY. REPLACED W ITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2000022600017 20000226 00017 EU 2000 2 26 2000ZZZX432 1 19991118 A 7714 L771M40C1005 INDICATOR UROCOP EC135 EC135P1 8680990 EU TRIPLE TACH STICKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 840 0045 EC1350054 NR NEEDLE STICKS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2000022600018 20000226 00018 EU 2000 2 26 2000ZZZX433 1 19991123 A 6240 614764021 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 139 305 2728 NEEDLE DROPS INTERMITTENTLY BELOW 20 PERCENT THEN COMES BACK TO NORMAL. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000022600019 20000226 00019 SW 2000 2 26 2000ZZZX434 1 19991225 A 6510 407340340101 DISC PACK 407012101111 BELL 407 407 SW T/R DRIVE CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 437AL RNFS2982 53141 DURING 25-HOUR AD INSPECTION, NR 7 DISC PACK CRACKED IN ONE LOCATION ON AFT DISC. 1 G 7 1 3U O H2SW 2000022600039 20000226 00039 WP 2000 2 26 USAAD99177 1 19991216 A 2450 RELAY DOUG DC9 DC981 3022081 WP GENERATOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 800US 48034 PIT/MSY - FLT 1635 - AFTER LIFT OFF THE ELECTRICAL SYSTEM AC CROSS-TIE LOCKOUT LIGHT ILLUMINATED. SINCE THE LEFT GENERA TOR WAS ON MEL, THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR CONTROL RELAY AND REMOVED THE MEL ON THE LEFT GENERATOR. THE CROSS-TIE SYSTEM WAS PLACED ON MEL AND THE AIRCRAFT DISPA TCHED. DURING THE OVERNIGHT MAINTENANCE THE CROSS-TIE SYSTEM WAS CHECKED AND NO DISCREPANCIES FOUND. THE CROSS-TIE MEL WAS REMOVED. (X) 2 L 7 2 4F A6WE 2000022600073 20000226 00073 EU 2000 2 26 2000ZZZX439 1 19991216 A 2150 JBS8803 MIXING VALVE UROCOP EC135 EC135P1 8680990 EU HEATER INOPERATIVE A R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 11 135SJ 599 055 EC1350054 MIXING VALVE INOPERATIVE. WHEN BLEED AIR HEAT IS 'OFF', CDS DISPLAY CONTAINS BLEED AIR 'ON'. THIS OCCURS WHILE SELECTI NG BLEED AIR HEAT SYSTEM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2000022600077 20000226 00077 SO 2000 2 26 SWIA971637 1 19991226 A 2912 FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYD SYSTEM REPLACED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 LEFT HYDRAULIC FILTER LIGHT CAME ON AFTER TAKEOFF, RETURNED TO LAX. REMOVED AND REPLACED LEFT HYDRAULIC RETURN FILTERS, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600078 20000226 00078 SO 2000 2 26 SWIA971638 1 19991229 A 2432 BATTERY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EMERGENCY BUSS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 293SW 120320 EMERGENCY BUSS OFF LIGHT ILLUMINATED IN FLIGHT. RETURNED TO PDX. REPLACED BACK UP BATTERY IAW MM CHP 24. OPS CHECK GO OD. SN ON 10023, SN OFF 8772. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600079 20000226 00079 SO 2000 2 26 SWIA971639 1 19991229 A 3230 UPLOCK HARNESS EMB 120 EMB120RT SO PWA 118 PW118 NE MLG MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 1110J 120110 AFTER TAKEOFF, SELECTED LANDING GEAR UP, ALL LIGHTS ON GEAR CONTROL PANEL ILLUMINATED. NO GEAR DOOR NOISE OR GEAR RETRA CTION HEARD CYCLED LANDING GEAR HANDLE WITH THE SAME RESULTS. RETURNED TO LAX. REPLACED RIGHT GEAR UPLOCK A HARNESS. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600084 20000226 00084 SO 2000 2 26 SWIA971627 1 19991214 A 3010 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 583SW 120351 DURING CLIMB-OUT, MIDDLE RIGHT WING LIGHT ON THE LEADING EDGE OVERHEAD ICE PANEL ILLUMINATED. RETURNED TO SEA. REMOVED AND REPLACED RIGHT WING MIDDLE DE-ICE PRESSURE SWITCH IAW MM 301005. OPS CK GOOD, SN ON: 0115 SN OFF: 0497. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600085 20000226 00085 SO 2000 2 26 SWIA971628 1 19991215 A 2432 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MAIN BATTERY FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 297SW 120327 BATTERY OFF BUS ILLUMINATED IN FLIGHT, RETURNED TO SFO. REPLACED K0022 RELAY AND MAIN BATTERY, RAN SYSTEM. OPS CK GOOD , PN ON: 40769, SN 49107, SN OFF: 44722. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600086 20000226 00086 SO 2000 2 26 SWIA971630 1 19991219 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAP FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 296SW 120325 FLAP CONTROL FAULT ILLUMINATED IN FLIGHT AND WOULD NOT RESET. RETURNED TO LAX. REPLACED FLAP CONTROL UNIT. OPS CHECKS GOOD, SN ON 0057, SN OFF 0031. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600087 20000226 00087 SO 2000 2 26 SWIA971631 1 19991220 A 5280 BEARING EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG DOOR LOOSE A SWIA O OTHER J WARNING INDICATION LD LANDING 1 NM 07 284YV 120284 LEFT MAIN LANDING GEAR WOULD NOT RETRACT, BOTH RED A AND B LIGHTS STAYED ON. INSPECTED LEFT FOWARD GEAR DOOR AND FOUND OUTBOARD DOOR FOWARD BEARING LOOSE, ALLOWING DOOR TO BE LOOSE AT DOOR SEQUENCE VALVE. REMOVED AND REPLACED LOOSE BEARIN G AS NEEDED AND ADJUSTED SEQUENCE VALVE TARGET IAW MM 528100. GEAR SWUNG AS NEEDED, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600088 20000226 00088 SO 2000 2 26 SWIA971632 1 19991220 A 3610 LINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE DEICE VALVE SPLIT A SWIA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 NM 07 250YV 120250 DUCT LEAKAGE RIGHT ENGINE AFTER TAKEOFF LAX. RETURNED TO LAX. LIGHT WENT OUT ON FINAL APPROACH, DUCT LEAK LIGHT CAME O N AGAIN. SHUT RIGHT ENGINE DOWN AFTER LANDING AND TAXIED TO GATE. INSTALLED SERVICEABLE DE-ICE VALVE. FOUND SPLIT ON FLEXIBLE LINE AT DE-CE VALVE. PERFORMED TEMPORARY REPAIR ON EXISTING LINE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600089 20000226 00089 SO 2000 2 26 SWIA971633 1 19991220 A 2932 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HYD SYSTEM DAMAGED A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 207SW 120266 GREEN SYSTEM MAIN PUMP LOW PRESSURE LIGHT AND LOW LEVEL LIGHT ILLUMINATED WITHIN A FEW SECONDS OF EACH OTHER. QUANTITY INDICATOR FOR GREEN SYSTEM INDICATED EMPTY. RETURNED TO SALT LAKE, LEFT HYDRAULIC PRESSURE SWITCH FOUND BLOWN APART. R EMOVED AND REPLACED PRESSURE SWITCH IAW SMB120 MM 293006. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600090 20000226 00090 SO 2000 2 26 SWIA971634 1 19991222 A 2750 FLAP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WING MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 197SW 120186 FLAP ASYMMETRY LEFT OUTBOARD AFTER TAKEOFF. RETURNED TO PIH. RESET FLAP SYSTEM. CYCLED UP AND DOWN 5 FAULT FREE CYCLE S. CHECKED FLAP TRACKS AND ROLLERS, CHECKED GOOD. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600091 20000226 00091 SO 2000 2 26 SWIA971635 1 19991225 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 220SW 120288 RIGHT MLG WILL NOT RETRACT AFTER TAKEOFF. RETURNED TO FAT. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR, PERFORMED GE AR SWING. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600092 20000226 00092 SO 2000 2 26 SWIA971636 1 19991226 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 220SW 120288 RIGH MAIN LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. RETURNED TO FAT. REPLACED AND ADJUSTED RIGHT MAIN LANDING GEAR S EQUENCE VALVES. OPS CHECKS GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 2000022600588 20000226 00588 EU 2000 2 26 2000ZZZX440 1 19991224 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU BS 33 -36 RT CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.02 HOURS. TLDG: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9860. RIGHT AFT INBOARD SEAT TRACK CORRODED . BLENDED, FOUND OUT OF LIMITS. ATR-42 IAW SRM 53-00-00 FIG 304. REMOVED AND REPLACED RT AFT INBOARD SEAT TRACK IAW E O NR E9-5300-013 R4. 2 H 7 2 4T RT A53EU 2000022600589 20000226 00589 EU 2000 2 26 2000ZZZX441 1 19991224 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU BS 33 -36 LT CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.02 HOURS. TLDG: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,859. LEFT AFT INBOARD SEAT TRACK CORRODED . BLENDED, FOUND OUT OF LIMITS. ATR-42 IAW SRM 53-00-00 FIG 304. REMOVED AND REPLACED LEFT AFT INBOARD SEAT TRACK IAW EO NR E9-5300-013 R4. 2 H 7 2 4T RT A53EU 2000022600590 20000226 00590 EU 2000 2 26 2000ZZZX442 1 19991223 A 5320 S5367800821602 ZEE AEROSP ATR42 ATR42300 8680920 EU BS 39-41 RT CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.0 HOURS. TAC: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,877. RIGHT AFT CARGO Z-MEMBER CORRODED. BL ENDED AND REMOVED CORROSION IAW ATR SRM 51-21-42 AND FOUND OUT OF LIMITS. INSTALLED NEW Z-MEMBER IAW ATR 42 SRM 51-25-0 3. 2 H 7 2 4T RT A53EU 2000022600591 20000226 00591 EU 2000 2 26 2000ZZZX443 1 19991223 A 5320 S537129034801 BRACKET AEROSP ATR42 ATR42300 8680920 EU BS 38 - 39 LT CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.0 HOURS. TAC: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,872. PASSENGER DOOR SILL FOLDING STEP SUPPOR T BRACKET CORRODED. BLENDED OUT CORROSION AND FOUND OUT OF LIMITS IAW ATR 42 SRM 51-00-00. REMOVED AND INSTALLED SUPPO RT BRACKET IAW ATR 42 SRM 51-25-02 AND SRM 51-25-03. 2 H 7 2 4T RT A53EU 2000022600592 20000226 00592 EU 2000 2 26 2000ZZZX444 1 19991223 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU BS 36 - 39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.0 HOURS. TAC: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,865. LEFT F/A'S SEAT TRACK CORRODED. BLENDED OUT CORROSION AND FOUND OUT OF LIMITS IAW ATR 42 SRM 53-00-00 FIG 304. INSTALLED NEW SEAT TRACK AT LEFT F/A POSITION I AW ATR 42 SRM 51-25-04 AND EO NR E9-5300-013R4. 2 H 7 2 4T RT A53EU 2000022600593 20000226 00593 EU 2000 2 26 2000ZZZX445 1 19991223 A 5320 S5367121729801 DRAIN TRACK AEROSP ATR42 ATR42300 8680920 EU BS 37 - 39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.0 HOURS. TAC: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,422. SERVICE DOOR DRAIN TRACK CORRODED. RE MOVED AND BLENDED CORROSION IAW ATR SRM 53-61-00, FIG 301. REMOVED AND REPLACED DRAIN TRACK WITH NEW PART IAW ATR SRM 5 1-25-02. 2 H 7 2 4T RT A53EU 2000022600594 20000226 00594 EU 2000 2 26 2000ZZZX446 1 19991223 A 5315 S5367240820201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU BS 39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.0 HOURS. TAC: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,874. FLOORBEAM NR 39 CORRODED. REMOVED AND BLENDED CORROSION IAW ATR SRM 51-21-42. REMOVED AND REPLACED FLOORBEAM WITH NEW IAW SRM 51-21-42. 2 H 7 2 4T RT A53EU 2000022600597 20000226 00597 EU 2000 2 26 2000ZZZX448 1 19991223 A 5315 S53672407201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU BS 38 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.02. TLDG: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,870. FLOORBEAM NR 38 CORRODED. BLENDED, FLOORB EAM 38 NOMINAL '0.063 INCH REMOVAL', 0.045 INCH FOUND TO BE OUT OF MANUAL LIMITS IAW ATR-42 SRM 53-00-00 FIG 318 51-21-4 2. INSTALLED NEW FLOORBEAM NR 38 IAW SRM 51-25-02. 2 H 7 2 4T RT A53EU 2000022600598 20000226 00598 EU 2000 2 26 2000ZZZX449 1 19991224 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU BS 33 - 36 RT CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 242AT 242 TAT: 17,939.02 HOURS. TLDG: 20,490. LGPG: 1,121,465. STA: SAW CRIC: 9,861. RIGHT AFT OUTBOARD SEAT TRACK CORRODED. B LENDED, FOUND OUT OF LIMITS. ATR-42 IAW SRM 53-00-00 FIG 304. INSTALLED NEW SEAT TRACK IAW EO NR E9-5300-013 R4. 2 H 7 2 4T RT A53EU 2000022600602 20000226 00602 NM 2000 2 26 USAA991422 1 19991221 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377.7 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 23939 27124 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 6 INCH AREA OF CORROSION AT STA 377.4, LB7 24 SEAT TRACK, CO RROSION LEVEL 1. REMOVED DEAMAGED SEAT TRACK AND REPLACED PER SRM 51-10-00. (X) 2 L 7 2 4F RT A2NM 2000022600612 20000226 00612 2000 2 26 2000ZZZX451 4 19991222 A 3422 GYRO DGS656226136 BEECH 1900 1900D 1154162 CE COCKPIT INTERMITTENT A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 169GL 1725 UE169 NR 1 DIRECTIONAL GYRO PRECESSES INTERMITTENTLY IN THE SLAVED MODE. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. COMPONE NT P/N DGS-65/622-6136-002. 2 L 7 2 4T RT A24CE 2000022600613 20000226 00613 EU 2000 2 26 AALA991997 1 19991216 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU BS 4862 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - NUMEROUS SPOTS OF CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 76 AND 82 ON FLOOR TRACK E LEFT. INSTALLED NEW FLOOR TRAK E LEFT, CPN 4035847 PER SRM 51-72-10-0. TST: 32,291.11 HOURS. CYCLES: 12,979. (X) 2 L 7 2 4F RT A35EU 2000022600614 20000226 00614 EU 2000 2 26 AALA991996 1 19991227 A 5347 LAVATORY TRACK AIRBUS 300 A300B4605R 3930308 EU BS 30-31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - CORROSION ON LAVATORY SUPPORT IKNBOARD FLANGE BRACKET TRACK B ANC C LEFT SIDE BETWEEN FRAMES 30 AND 31. INSTALLED NEW LAVATORY SUPPORT TRACK PER SRM 51-72-10-0. TST: 32,241.11 HOURS. CYCLES: 12,979. (X) 2 L 7 2 4F RT A35EU 2000022600615 20000226 00615 EU 2000 2 26 AALA991995 1 19991216 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU BS 75-80 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - NUMEROUS SPOTS OF CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 75 AND 80 ON FLOOR TRACK E, RIGHT. INSTALLED NEW FLOO R TRACK E RIGHT, PER SRM 51-72-10-0. TST: 32,241.11 HOURS. CYCLES: 12,979. P/N A53278453200. (X) 2 L 7 2 4F RT A35EU 2000022600619 20000226 00619 SO 2000 2 26 C2XA00CL002 1 19991229 A 2611 SMOKE DETECTOR EMB 120 EMB120RT SO CABIN MALFUNCTIONED A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 09 57734 120199 CLE - FLT 3147 - ON TAKEOFF ROLL, CREW RECEIVED A SMOKE ALARM INDICATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETU RNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IAW MEL 21-51-2. (X) 2 L 7 2 4T RT A31SO 2000022600621 20000226 00621 EU 2000 2 26 C2XA99IA644 1 19991223 A 5315 S53672409218 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU BS 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 DURING C-CHECK, FOUND CORROSION ON FLOORBEAM AT FRAME 40, RBL 13. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ST RAPS IAW SRM 51-21-42 AND EC5310-01037. AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACTT: 20,664.9 HOURS. ACTC: 23,807 . (X) 2 H 7 2 4T RT A53EU 2000022600622 20000226 00622 EU 2000 2 26 C2XA99IA643 1 19991223 A 5320 S5367800920001 ANGLE AEROSP ATR42 ATR42320 8680930 EU BS 38-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 DURING C-CHECK, FOUND CORROSION ON PASSENGER DOOR THRESHOLD SUPPORT ANGLE BETWEEN FRAMES 36 AND 38. REMOVED AND REPLACE D ANGLE IAW SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACTT: 20,664.9 HOURS. ACTC: 23,807. (X) 2 H 7 2 4T RT A53EU 2000022600623 20000226 00623 EU 2000 2 26 C2XA99IA642 1 19991223 A 5320 S5367800826801 CHANNEL AEROSP ATR42 ATR42320 8680930 EU BS 38-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 DURING C-CHECK, FOUND CORROSION ON PASSENGER DOOR THRESHOLD SUPPORT CHANNEL BETWEEN FRAMES 38 AND 39. REMOVED AND REPLA CED SUPPORT CHANNEL IAW SRM 51-24-01 AND SRM 51-25-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACTT: 20,664.9 HOURS. ACTC: 23,807. (X) 2 H 7 2 4T RT A53EU 2000022600629 20000226 00629 WP 2000 2 26 2000ZZZX452 1 19991124 A 2150 1588578119 DUCT LKHEED 1011 10113851 5265010 WP NR 3 PACK CRACKED A AMTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 191AT 193C1084 DURING CLIMB, UNABLE TO CONTROL CABIN ALTITUDE BELOW 10,000 FEET WITH PACK NR 1 AND NR 3 ON. DIVERTED TO JFK, LANDED WI THOUT INCIDENT. REPLACED BLOWN DUCT TO NR 3 AIR CONDITIONING PACK. LEAK CHECKED GOOD. PACK OPS CHECKED PER MM CHAPTER 21. (X) 2 L 7 3 4F A23WE 2000022600632 20000226 00632 NM 2000 2 26 USAA991443 1 19991221 A 5753 ANGLE BOEING 757 7572B7 1384964 NM TE FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 612AU 23939 27124 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK INBOARD MAIN FLAP, OUTBOARD T/E AT NR 3 FLAP TRACK JUNCTI ON LEFT WING ANGLE SUPPORT BRACKET. REMOVED AND REPLACED DAMAGE PER SRM 51-10-00. (X) 2 L 7 2 4F RT A2NM 2000022600652 20000226 00652 NM 2000 2 26 MZZA99239 1 19991224 A 3230 1U1085 HOUSING BOEING 727 727232 1384082 NM RT MLG CRACKED A MZZA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 15781 20636 GUM - FLT 988 - EN ROUTE TO SPN, STARTED NOTICING A LOSS OF A-SYSTEM HYDRAULIC QUANTITY. REMOVED AND REPLACED MLG SEQU ENCE VALVE PER MM 32-32-31. (X) 2 L 7 3 4F A3WE 2000022600653 20000226 00653 NE 2000 2 26 PLGA991210A 2 19991210 A 7597 7292533501 WIRE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT NACELLE BROKEN A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 743BA 340A093 BOS- FLT 4719 - AFTER DEPARTURE OF FLIGHT 4719 BOS TO ROC, THE RIGHT AIR VALVE FAIL LIGHT CAME ON. THE AIRCRAFT RETURNE D TO BOS. AFTER TROUBLESHOOTING AND A TEST FLIGHT, MAINTENANCE FOUND A BROKEN WIRE IN THE WHITE HARNESS OF THE RIGHT NA CELLE, WIRE HL519-22 AT CONNECTOR 25HL. AIRCRAFT RELEASED FOR A TEST FLIGHT AND FLEW SATISFACTORILY. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 2000022600654 20000226 00654 EU 2000 2 26 AALA991978 1 19991227 A 3350 P2010031303 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80084 675 JFK - DURING OVERNIGHT MAINTENANCE, 3L DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED 3L DOOR EMERGENCY EXIT SIGN. SYS TEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600656 20000226 00656 NE 2000 2 26 PLGA991210 2 19991210 A 7510 VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 743BA 340A093 BOS - FLT 4793 - DURING FLIGHT 4793 BOS TO BTV, THE RIGHT AIR VALVE LIGHT STAYED ON WHENEVER POWER LEVERS WERE OVER 90 P ERCENT N1. DUE TO WEATHER, THE AIRCRAFT DIVERTED BACK TO BOS. MAINTENANCE REPLACED THE ANTI-ICE AIR SHUTOFF VALVE AND PERFORMED ALL REQUIRED CHECKS, GOOD. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 2000022600657 20000226 00657 NE 2000 2 26 PLGA991216 2 19991216 A 7532 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE BLEED VALVE LOOSE A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 358BE 340B279 BOS - FLT 4855 - DURING FLIGHT, THE RIGHT LOW PRESSURE BLEED VALVE WAS NOT FUNCTIONING AND STUCK OPEN. AIRCRAFT RETURNE D TO BOS. AFTER TROUBLESHOOTING MAINTENANCE, FOUND THE CONNECTOR AT THE RIGHT BLEED VALVE LOOSE. THE CONNECTOR WAS RE SECURED, REQUIRED OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 2000022600658 20000226 00658 EU 2000 2 26 PLGA991228 1 19991228 A 2420 51634002 GCU SAAB SF340 SF340A 7850100 EU LEFT GENERATOR FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 346BE 670 340A150 BOS/SYR - FLT 4705 - AFTER TAKEOFF, CREW NOTED THE LEFT AC GENERATOR HAD FAILED AND WOULD NOT RESET. THE AIRCRAFT DIVER TED BACK TO BOS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AC GENERATOR AND GENERATOR CONT ROL UNIT AND PERFORMED ALL OPERATIONAL CHECKS, AIRCRAFT WAS THEN RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 2000022600660 20000226 00660 EU 2000 2 26 USAAF00001 1 19990102 A 3234 715441 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU MLG FAILED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 881US 20909 11333 RDU/CLT - FLT 2327 - DURING CLIMB-OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. RECYCLED GEAR AFTER 2-3 MINUTES, GEAR R ETRACTED. ON APPROACH, GEAR SELECTED DOWN, BUT MAINS DID NOT EXTEND. FOUR MINUTES LATER, RECEIVED THREE GREEN INDICATI ONS. MADE SAFE LANDING AT CLT. MAINTENANCE REPLACED THE MLG SELECTOR VALVE. LEAKS AND OPS CHECKED GOOD. (X) 2 L 7 2 4F RT 2000022600661 20000226 00661 EU 2000 2 26 USAAF99060 1 19991231 A 3234 715381 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU NLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 881US 21182 11333 CLT/ROA - FLT 2122 - DURING CLIMB OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED CHECKLIST PROCEDURES. RET URNED TO FIELD FOR A NORMAL LANDING. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. LEAKS AND OPS CHECKED GOOD. ALL GEAR RETRACT. (X) 2 L 7 2 4F RT 2000022600662 20000226 00662 EU 2000 2 26 USAASA99009 1 19991122 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 710UW 1019 RDU - FOUND EMERGENCY LIGHT SYSTEM FAILED OPERATIONAL TEST. MAINTENANCE REPLACED THE AFT EPSU. OPS CHECKED OKAY. (X) 2 L 7 2 4F RT A28NM 2000022600663 20000226 00663 WP 2000 2 26 USAAD99174 1 19991208 A 2612 89280904001 CONTROL UNIT DOUG DC9 DC931 3022065 WP E/E BAY FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 959VJ 73719 47352 LGA/ORF - FLT 1703 - AFTER TAKEOFF, THE MASTER CAUTION LIGHT AND THE RIGHT ENGINE 'B' FIRE LOOP LIGHT ILLUMINATED WITH A N INTERMITTENT RIGHT ENGINE FIRE LIGHT. THERE WAS NO ENGINE FIRE BELL. THE RIGHT ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. SEVEN MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE RIGHT E NGINE FIRE DETECTOR CONTROL UNIT. (X) 2 L 7 2 4F A6WE 2000022600664 20000226 00664 WP 2000 2 26 USAAD99176 1 19991211 A 2133 20219741 ACTUATOR DOUG DC9 DC981 3022081 WP OUTFLOW VALVE FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 827US 48049 PIT/TPA - FLT 1845 - WHILE CRUISING AT 35,000 FEET, THE CABIN ALTITUDE SLOWLY CLIMBED TO 10,000. AFTER CREW WAS UNABLE TO CONTROL THE CABIN ALTITUDE MANUALLY, AN EMERGENCY DESCENT WAS INITIATED AND THE AIRCRAFT DIVERTED TO CLT AND LANDED W ITHOUT INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE OUTFLOW VALVE ACTUATOR. (X) 2 L 7 2 4F A6WE 2000022600665 20000226 00665 NE 2000 2 26 USAASB99292 2 19991209 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE LEFT LEAKING A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 248US 39840 6379 22755 709100 IAD - FLT 2721 - ON CLIMB-OUT AT FL 200, CAPTAIN NOTICED THE NR 1 ENGINE OIL QUANTITY DROPPED FROM 3 GALLONS AT DEPARTUR E TIME TO ZERO GALLONS. PRESSURE WAS OK, STARTED TO DECREASE, THEN WENT TO YELLOW BAND. CAPTAIN FOLLOWED QUICK REFEREN CE HANDBOOK PROCEDURES AND SHUT DOWN THE NR 1 ENGINE. AN EMERGENCY WAS DECLARED AS THE FLIGHT RETURNED TO FIELD AND LAN DED WITHOUT FURTHER INCIDENT AT IAD. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. FIRE RESCUE STATED THEY DID NOT SEE INDICATION OF FIRE BUT OIL ON THE OUTSIDE OF ENGINE. TOTAL SINGLE ENGINE TIME WAS 20 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F A16WE E2EA 2000022600666 20000226 00666 NM 2000 2 26 USAASB99287 1 19991205 A 5210 6990299 HINGE BOEING 737 7373B7 1384580 NM PASSENGER DOOR FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 523AU 23858 TPA - FLT 1610 - AFTER TAKEOFF, A VERY LOUD NOISE WAS HEARD COMING FROM THE FORWARD ENTRY DOOR DURING CLIMB-OUT. THE AI RCRAFT DID NOT LOSE PRESSURIZATION, BUT THE CAPTAIN DECIDED TO RETURN TO FIELD AT TPA. FLIGHT LANDED WITHOUT FURTHER IN CIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR LOWER HINGE FLAP ASSEMBLY. PRESSURIZATION CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 2000022600667 20000226 00667 NM 2000 2 26 USAASB99300 1 19991221 A 3411 856AE18 PROBE BOEING 737 7374B7 1384702 NM PITOT SYSTEM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 782AU 14987 25021 CLT/GSP - FLT 248 - EN ROUTE, THE CAPTAIN'S NR 1 AUXILIARY PITOT STATIC LIGHT ILLUMINATED. CREW FOUND CIRCUIT BREAKER T RIPPED. RESETTING CIRCUIT BREAKER WAS NO HELP. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGEN CY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S LOWER RIGHT NR 1 AUXILIARY PITOT PROBE PER MM 34-11-11. OPERATIONAL CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 2000022600676 20000226 00676 NM 2000 2 26 2000ZZZX453 1 19991118 A 2611 302842 SMOKE DETECTOR BOEING 727 727222 1384073 NM CARGO BAY FAILED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 7643U 20037 MDT - FLT 111 - CENTER UPPER ZONE WILL NOT TEST ON THE CARGO SMOKE DETECTION SYSTEM. FOUND BAD CONNECTION AT CONNECTOR OF NR 2 CARGO SMOKE DETECTOR, MADE SERVICEABLE REPAIR AND RELAMPED TEST LIGHT, OPERATION CHECKED GOOD. (X) 2 L 7 3 4F A3WE 2000022600677 20000226 00677 NE 2000 2 26 2000ZZZX454 2 19991114 A 7200 ENGINE BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 2 FOD A RYNA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 CE 07 427EX 19090 655144 SFO - FLT 9008 - ON TAKEOFF ROLL, NR 2 ENGINE HEAVY COMPRESSOR STALL. ANOTHER AIRCRAFT REPORTED SEEING A LARGE BIRD GO INTO NR 2 INLET. FLAME OUT REAR. REPLACED NR 2 ENGINE. (X) 2 L 7 3 4F 4 F A3WE E2EA 2000022600678 20000226 00678 NM 2000 2 26 2000ZZZX455 1 19991124 A 2610 308 BULB BOEING 727 72722C 138400F NM SMOKE DETECTOR FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 421EX 19099 RIC/IND - FLT 712 - RIGHT BULB IN SMOKE DETECTOR INDICATOR IS OUT. RELAMPED BULB. (X) 2 L 7 3 4F A3WE 2000022600679 20000226 00679 EU 2000 2 26 UF6A991104 1 19991105 A 2560 GE12 FLASHLIGHT GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE AFT VESTIBULE EMERGENCY FLASHLIGHT IS INOPERABLE. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT. (X) 2 L 7 2 4T RT A27NM 2000022600680 20000226 00680 EU 2000 2 26 UF6A991106 1 19991109 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - THE AFT LEFT EXTERIOR EMERGENCY LIGHT IN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 2000022600681 20000226 00681 EU 2000 2 26 UF6A991105 1 19991105 A 3350 1317 BULB BAG ATP ATP EU BS 289 FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE AFT RIGHT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 2000022600682 20000226 00682 EU 2000 2 26 UF6A991020 1 19991024 A 7600 3085003001 SWITCH KORRY BAG ATP ATP EU COCKPIT FAILED A UF6A O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 859AW 2036 YNG - FLT 5709 - UNABLE TO SELECT ANY OF THE POWER RATINGS PRIOR TO TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE MAXIM UM CONTINGENCY SWITCH. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 2000022600683 20000226 00683 EU 2000 2 26 UF6A991019 1 19991023 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 SBN - AFT EMERGENCY LIGHT BULB IS INOPERATIVE ON THE RIGHT AND LEFT SIDES. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 2000022600689 20000226 00689 EU 2000 2 26 AALA991953 1 19991221 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 12 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7083A 645 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH FLOOR LIGHTS BETWEEN SEAT 12H AND 14H INOPERATIVE. REPLACED EME RGENCY EXIT PATH FLOOR LIGHT STRIP AT SEAT 12H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600690 20000226 00690 EU 2000 2 26 AALA991318 1 19990825 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN UNSECURED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7082A 643 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT 4L DOOR INOPERATIVE. RESECURED CONNECTOR TO EM ERGENCY EXIT FLOOR PATH LIGHTING AT 4L DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600691 20000226 00691 EU 2000 2 26 AALA991979 1 19991227 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU SEAT 33 DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80084 675 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 33G INOPERATIVE. REPAIRED EMERGENCY EXIT PATH LIG HT CONNECTOR AT SEAT 33G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600692 20000226 00692 EU 2000 2 26 AALA991836 1 19991130 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA O OTHER O OTHER CR CRUISE 1 SW 07 25071 514 LHR - FLT 0155 - DURING FLIGHT WITH EMERGENCY EXIT LIGHT SIWTCH IN ARM POSITION, EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMI NATE INTERMITTENTLY. RE-SEATED R3 EMERGENCY EXIT LIGHT PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600693 20000226 00693 EU 2000 2 26 AALA991840 1 19991202 A 3350 SIGN AIRBUS 300 A300B4605R 3930308 EU CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 25071 514 JFK - DURING OVERNIGHT MAINTENANCE, LHR PREVIOUSLY REPORTED INTERMITTENT EMERGENCY EXIT LIGHT OPERATION AFFECTED BY MOVE MENT OF R3 OVERHEAD EXIT SIGN. INSPECTED AND CLEANED. NO FAULT FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600694 20000226 00694 WP 2000 2 26 AALA991874 1 19991208 A 3320 LIGHT DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 233AA 49180 ORD - FLT 1631 - AFTER TAKEOFF ODOR OF OVERHEATED ELECTRICAL EQUIPMENT REPORTED BY FLIGHT ATTENDANTS. RETURNED AND LAND ED ORD WITHOUT FURTHER INCIDENT. CABIN RECIRCULATION FAN CHECKED, ALL CABIN LIGHTS CHECKED WITH TWO OVERHEAD LIGHTS RIG HT SIDE AFT WERE INOPERATIVE. HAD BROKEN TABS. REPLACED LIGHT RECEPTACLES. SYSTEM GROUND CHECKED, NORMAL OPERATION. F UNCTIONAL CHECK FLIGHT CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000022600695 20000226 00695 WP 2000 2 26 AALA991903 1 19991214 A 2120 UNKNOWN DOUG DC9 DC982 3022082 WP COCKPIT SMOKE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 499AA 49737 DFW - FLT 0847 - EN ROUTE, RIGHT PACK PRODUCED LIGHT SMOKE AND SMELL. SHUT DOWN PACK. SMOKE WENT AWAY. RAN ENGINES FR OM IDLE TO TAKEOFF POWER WITH PACKS ON. COULD NOT DUPLICATE SMOKE. SYSTEM GROUND CHECKED, NORMAL OPERATION. NEXT FLIG HT, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 2000022600696 20000226 00696 EU 2000 2 26 AALA991985 1 19991229 A 3350 P2010031303 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 20 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14065 508 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 20G INOPERATIVE. REPLACED EMERGENCY EXIT SEA T PATH LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600697 20000226 00697 EU 2000 2 26 AALA991959 1 19991223 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 11060 470 MIA - DURING OVERNIGHT MAINTENANCE, L2 EMERGENCY EXIT SIGN INOPERATIVE. RECONNECTED L2 EMERGENCY EXIT SIGN CONNECTOR. S YSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600698 20000226 00698 EU 2000 2 26 AALA991323 1 19990904 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7055A 462 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT CENTER SECTION NEAR L3 DOOR INOPERATIVE. REPLAC ED CONNECTORS TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT CENTER SECTION NEAR L3 DOOR. SYSTEM GROUND CHECKED, NORMAL OP ERATION. (X) 2 L 7 2 4F RT A35EU 2000022600699 20000226 00699 EU 2000 2 26 AALA991991 1 19991229 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 25 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80058 466 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 25H INOPERATIVE. REPLACED EMERGENCY EXIT F LOOR PATH LIGHT STRIP AT SEAT 25H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 2000022600702 20000226 00702 WP 2000 2 26 2000ZZZX459 1 19991102 A 3310 BA170 BALLAST DOUG DC8 DC8F54 3021926 WP COCKPIT FAILED A FXLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 19 44UA 45800 AFTER TAKEOFF FROM MIA, EXPERIENCED SMOKE AND ELECTRICAL ODOR IN THE COCKPIT; RETURNED TO MIA AND LANDED WITHOUT INCIDEN T. INSPECTION REVEALED THE BALLAST FOR THE FIRST OFFICER LIGHT WAS OVERHEATED. REPLACED BALLAST AND RETURNED AIRCRAFT TO SERVICE. (X) 2 L 7 4 4F 4A25 2000022600703 20000226 00703 WP 2000 2 26 2000ZZZX460 1 19990827 A 5315 FLOORBEAM DOUG DC8 DC8F54 3021926 WP BS 1480 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 427FB 45684 DURING B-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE STA FS 1480. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5310-01:00. (X) 2 L 7 4 4F 4A25 2000022600704 20000226 00704 WP 2000 2 26 2000ZZZX461 1 19990827 A 5315 FLOORBEAM DOUG DC8 DC8F54 3021926 WP BS 1480 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 427FB 45684 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE STA FS 1480. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA G5310-03:00. (X) 2 L 7 4 4F 4A25 2000022600707 20000226 00707 WP 2000 2 26 2000ZZZX464 1 19990827 A 5315 FLOORBEAM DOUG DC8 DC8F54 3021926 WP BS 1380 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 427FB 45684 DURING B-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORROSION DAMAGE UPPER FLANGE AT STA FS 1380 RBL 38. REPAIRE D CORROSION DAMAGE IAW FINE AIRLINES EA G5310-02:00. (X) 2 L 7 4 4F 4A25 2000022600708 20000226 00708 WP 2000 2 26 2000ZZZX465 1 19991111 A 5730 SKIN DOUG DC8 DC8F54 3021926 WP WS 210 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 57FB 45669 DURING B-CHECK INSPECTION, FOUND THE FOLLOWING: 4.5 INCH CRACK IN RIGHT INBOARD FORWARD LOWER WING SKIN AT STA XRS 210 BETWEEN 66 AND 67. REPAIRED CRACK IAW BOEING SERVICE ENGINEERING ROD SKETCH 99-08-13 AND SRM 57-2-1 FIGURE 35, FINE AIR LINES EA G5730-02:00. (X) 2 L 7 4 4F 4A25 2000022600711 20000226 00711 WP 2000 2 26 2000ZZZX468 1 19991005 A 3510 4714037517 LINE DOUG DC8 DC861 3021952 WP OXYGEN SYSTEM FAILED A FXKA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 AL 01 30UA 45888 DURING LANDING ROLL-OUT AT SDQ, BELOW 100 KNOTS, CREW OBSERVED AN ELECTRICAL SPARK AND SMALL FIRE AND A HIGH AIR PRESSUR E 'HISSING' SOUND COMING FROM THE FORWARD OBSERVER OXYGEN PANEL. INSPECTION FOUND THE MAIN OXYGEN LINE BLOWN OFF AT THE CONNECTOR AND FOUND TWO SHORTED WIRES IN THE FIRST OBSERVER BOX. IT APPEARS THE RUBBER HOSE THAT SUPPLIES OXYGEN TO T HE REGULATOR RUPTURED AND DAMAGED THE LIGHT PANEL WIRES, A FLEET CAMPAIGN IS BEING CONDUCTED TO INSPECT THE HOSES FOR PO SSIBLE DETERIORATION. (X) 2 L 7 4 4F 4A25 2000022600712 20000226 00712 WP 2000 2 26 2000ZZZX469 1 19991208 A 5330 SKIN DOUG DC8 DC861 3021952 WP BS 52 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 30UA 45888 DURING B-CHECK INSPECTION, FOUND THE FOLLLOWING: CORROSION DAMAGE LEFT FUSELAGE ABOVE NLG DOOR AT STA 52.00. REPAIRED CORROSION DAMAGE IAW SRM 53-2-1. (X) 2 L 7 4 4F 4A25 2000022600713 20000226 00713 WP 2000 2 26 ASAA9980229 1 19991102 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PHX - DURING C-CHECK, FOUND CORROSION ON FRAME AT FS 1322 BETWEEN LONGERONS 24L AND 24R. REMOVED AND DAMAGED MATERIAL A ND INSTALLED NEW PIECES IAW DC9 SRM 53-03, FIG 2A. (M) 2 L 7 2 4F A6WE 2000022600714 20000226 00714 WP 2000 2 26 ASAA9980240 1 19991105 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 206 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOOR PANEL AT FS 206. REMOVED CORROSION AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000022600715 20000226 00715 WP 2000 2 26 ASAA9980241 1 19991105 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP BS 1254-1265 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TIE-DOWN TRACK IN AFT CARGO COMPARTMENT FROM FS 1254 TO 1265, LBL 17. R EMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW ASA EA 5310-01721. (M) 2 L 7 2 4F RT A6WE 2000022600716 20000226 00716 WP 2000 2 26 ASAA9980242 1 19991105 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 503 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, A DENT WAS FOUND IN FUSELAGE SKIN AT FS 503 BETWEEN LONGERON 20R AND 21E. INSTALLED REPAIR DOUB LER IAW DC9 SRM 53-04, FIG 12B. (M) 2 L 7 2 4F RT A6WE 2000022600717 20000226 00717 WP 2000 2 26 ASAA9980243 1 19991105 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, A GOUGE WAS FOUND IN THE LEFT ELEVATOR SKIN NEAR THE INBOARD HOIST POINT. REMOVED DAMAGED MATER IAL AND SPLICED IN NEW SECTION IAW ASA 5520-01074. (M) 2 L 7 2 4F RT A6WE 2000022600718 20000226 00718 WP 2000 2 26 ASAA9980239 1 19991105 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 180-188 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOOR PANEL FROM FS 180 TO 188. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-03, FIG 1. (M) 2 L 7 2 4F RT A6WE 2000022600719 20000226 00719 WP 2000 2 26 ASAA9980238 1 19991105 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP BS 148-210 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN FLOOR PANEL FROM FS 148 TO 210. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PANEL IAW DC9 SRM 51-30-02 AND 51-30-05. (M) 2 L 7 2 4F RT A6WE 2000022600720 20000226 00720 WP 2000 2 26 ASAA9980237 1 19991105 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 256 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 356, RBL 44. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2000022600721 20000226 00721 WP 2000 2 26 ASAA9980236 1 19991105 A 5347 6019943 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1099-1102 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1099 TO 1102, LBL 44. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2000022600722 20000226 00722 WP 2000 2 26 ASAA9980235 1 19991105 A 5347 6022044 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 265 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 265, RBL 22. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2000022600723 20000226 00723 WP 2000 2 26 ASAA9980234 1 19991105 A 5347 S00200 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1099-1103 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1099 TO 1103, 1202, TO 1205 AND 1224 TO 1230, LBL 22 . REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTIONS IAW DC9 SRM 53-05, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000022600724 20000226 00724 WP 2000 2 26 2000ZZZM193 1 19991105 A 5347 S00200 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1202-1205 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK FROM FS 1099 TO 1103, 1202, TO 1205 AND 1224 TO 1230, LBL 22 . REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTIONS IAW DC9 SRM 53-05, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000022600725 20000226 00725 WP 2000 2 26 ASAA9980233 1 19991105 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 741-744 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND ON CABIN SEAT TRACK FROM FS 741 TO 744, LBL 22. REMOVED DAMAGED MATERIAL AND SPLICED IN N EW SECTION IAW DC9 SRM 53-05, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000022600726 20000226 00726 WP 2000 2 26 ASAA9980232 1 19991105 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND CORROSION ON R1 DOOR CUTOUT FLOOR CLOSEOUT WEB ON FORWARD INTERIOR SURFACE. REMOVED DAMAG ED MATERIAL AND INSTALLED NEW PIECES IAW DC0 SRM AND DWG 9957828. (M) 2 L 7 2 4F RT A6WE 2000022600727 20000226 00727 WP 2000 2 26 ASAA9980231 1 19991105 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1265 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 PHX - DURING 30K CHECK, FOUND IN CUSP WEB AT FS 1265, LONGERON 18L. REMOVED DAMAGED MATERIAL AND INSTALLED NEW PIECES I AW DC9 SRM 53-05, FIG 97. (M) 2 L 7 2 4F RT A6WE 2000022600728 20000226 00728 WP 2000 2 26 ASAA9980216 1 19991027 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 1006-1022 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING 30K CHECK, FOUND EXFOLIATION ON LONGERON 30 FROM FS 1006 TO 1022. REMOVED DAMAGED SECTION AND SPLICED IN N EW SECTION IAW ASA EA 5310-01717. (M) 2 L 7 2 4F RT A6WE 2000022600729 20000226 00729 WP 2000 2 26 ASAA9980217 1 19991027 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 1126 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING 30K CHECK, FOUND CORROSION ON FUSELAGE SKIN AT ANTENNA MOUNT HOLE AT FS 1126 BETWEEN LONGERON 30 AND LONGER ON 29L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW ASA EA 5330-01406. (M) 2 L 7 2 4F RT A6WE 2000022600730 20000226 00730 WP 2000 2 26 ASAA9980219 1 19991027 A 5753 MOUNT DOUG DC9 DC983 3022083 WP TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING 30K CHECK, FOUND CORROSION ON RIGHT OUTBOARD FLAP MID HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES. RE PAIRED IAW ASA EA 2750-01080. (M) 2 L 7 2 4F RT A6WE 2000022600731 20000226 00731 WP 2000 2 26 ASAA9980220 1 19991027 A 5753 591921812 MOUNT DOUG DC9 DC983 3022083 WP TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING 30K CHECK, FOUND CORROSION ON RIGHT OUTBOARD FLAP INBOARD HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES. . REPAIRED IAW ASA EA 2750-01080. (M) 2 L 7 2 4F RT A6WE 2000022600732 20000226 00732 WP 2000 2 26 ASAA9980221 1 19991027 A 5753 MOUNT DOUG DC9 DC983 3022083 WP TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING 30K CHECK, FOUND CORROSION ON LEFT OUTBOARD FLAP MID HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES. REP AIRED IAW ASA EA 2750-01080. (M) 2 L 7 2 4F RT A6WE 2000022600733 20000226 00733 WP 2000 2 26 ASAA9980222 1 19991027 A 5753 MOUNT DOUG DC9 DC983 3022083 WP TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 OAK - DURING 30K CHECK, FOUND CORROSION ON LEFT OUTBOARD FLAP INBOARD HINGE CASTING BEARING RETAINER PLATE MOUNT HOLES. REPAIRED IAW ASA EA 2750-01080. (M) 2 L 7 2 4F RT A6WE 2000022600734 20000226 00734 WP 2000 2 26 ASAA9980205 1 19991010 A 5610 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 PDX - AFTER ARRIVAL OF FLT 102, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. REINSTALLED U PPER GUIDE BEARING INTO TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000022600735 20000226 00735 2000 2 26 ASAA9980201 4 19991006 A 2565 SLIDE DOUG DC9 DC983 3022083 WP CABIN WON'T TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 PHX - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2000022600736 20000226 00736 WP 2000 2 26 ASAA9980261 1 19991110 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 237 CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CHAFING WAS FOUND ON CABIN SEAT TRACK AT FS 237, RBL 45. REMOVED DAMAGED MATERIAL AND SPL ICED IN NEW SECTION IAW DC9 SRM 53-05 FIG 4F. (M) 2 L 7 2 4F RT A6WE 2000022600737 20000226 00737 WP 2000 2 26 ASAA9980260 1 19991110 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1155 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT FS 1155, LBL 40. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 2000022600738 20000226 00738 WP 2000 2 26 ASAA9980259 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1142 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON WEB AT FS 1142, LBL 52. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW D C9 SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000022600739 20000226 00739 WP 2000 2 26 ASAA9980258 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 200 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, A TEAR WAS FOUND IN WEB AT FS 200, RBL 54. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-02 AND 53 -14-01. (M) 2 L 7 2 4F RT A6WE 2000022600740 20000226 00740 WP 2000 2 26 ASAA9980257 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 190 PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, A PUNCTURE WAS FOUND IN WEB AT FS 190, LBL 35. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER I AW DC9 SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000022600741 20000226 00741 WP 2000 2 26 ASAA9980256 1 19991110 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 180 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT FS 180, FROM RBL 6 TO RBL 38. REMOVED DAMAGED MATERIA L AND INSTALLED NEW PIECES IAW DC9 SRM 53-01 AND 53-14-01. (M) 2 L 7 2 4F RT A6WE 2000022600742 20000226 00742 WP 2000 2 26 ASAA9980255 1 19991110 A 5311 39364451 FRAME DOUG DC9 DC983 3022083 WP BS 1117 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON FRAME AT FS 1117, BETWEEN LONGERONS 29L AND 30. REMOVED AND REPLAC ED FRAME FROM LONGERON 26L TO LONGERON 26R IAW DC9 SRM 53-01, FIG 1. (M) 2 L 7 2 4F RT A6WE 2000022600743 20000226 00743 WP 2000 2 26 ASAA9980254 1 19991110 A 5310 39364451 FRAME DOUG DC9 DC983 3022083 WP BS 1098 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON FRAME AT FS 1098, BETWEEN LONGERONS 28L AND 30. REMOVED AND REPLACED FRAME F ROM LONGERON 26L TO LONGERON 26R IAW DC9 SRM 53-01, FIG 1. (M) 2 L 7 2 4F RT A6WE 2000022600744 20000226 00744 WP 2000 2 26 ASAA9980253 1 19991110 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1142-1146 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 PHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB FROM FS 1142 TO 1146 AND 1153, LONGERON 18R. REMOVED DAMAGED MATERI AL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000022600745 20000226 00745 NM 2000 2 26 P2EA99356 1 19991130 A 5751 SKIN BOEING 737 737222 1384473 NM AILERON DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK, RIGHT AILERON INBOARD TRAILING EDGE DISBONDED AT REAR SPAR AREA. REPAIRED RIGHT AILERON PER SRM 5 1-40-6, PAR 5. (M) 2 L 7 2 4F A16WE 2000022600746 20000226 00746 NM 2000 2 26 2000ZZZM194 1 19991111 A 2612 1825280037525 FIRE LOOP BOEING 727 72722C 138400F NM NR 3 ENGINE MALFUNCTIONED A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 429EX 19100 FLT 611 - IND-EWR - NR 3 ENGINE FIRE DETECTOR GROUND LIGHT ILLUMINATED. TROUBLESHOOTING, AIRCRAFT HAS BRIEF HISTORY OF REPEAT WRITE UPS. VISUALLY CHECKED FIRE LOOP, NO ABNORMAL CONDITION NOTICED. LIGHT HAS NOT BEEN ON SINCE AIRCRAFT WAS PARKED. UNABLE TO DUPLICATE OR CREATE INDICATION. (M) 2 L 7 3 4F A3WE 2000022600747 20000226 00747 NM 2000 2 26 2000ZZZM195 1 19991112 A 2120 UNKNOWN BOEING 727 72722C 138400F NM CABIN ODOR A RYNA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 428EX 19097 FLT 710 - MSP-IND - A STRONG BURNING RUBBER SMELL ON TAKEOFF OUT OF MSP, WHICH STOPPED AFTER 3000 FT AGL AFTER TAKEOFF. PERFORMED OPERATIONAL CHECK ON AIRCRAFT AIR CONDITIONING SYSTEM, OPERATION CHECK GOOD, NO DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 2000022600754 20000226 00754 NM 2000 2 26 2000ZZZM202 1 19991117 A 3040 2311M694 MOTOR BOEING 727 72722C 138400F NM WINDSHIELD WIPER FAILED A RYNA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 428EX 19097 FLT 620 - DTW-GRR - A STRONG ELECTRICAL SMOKE SMELL ON RIGHT SIDE OF COCKPIT. AFTER SMELL WENT AWAY DISCOVERED RIGHT WI PER CIRCUIT BREAKER POPPED, DID NOT RESET. DEFERRED IN GRR CLEARED IN IND. REPLACED FIRST OFFICERS WINDSHIELD WIPER MO TOR. (M) 2 L 7 3 4F A3WE 2000022600761 20000721 00761 NM 2000 7 21 USAABB99062 1 19991231 A 2910 271T00703 SEAL BOEING 767 767201 1385125 NM HYD SYSTEM RUPTURED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 647US 23899 CDG - FLT 23 - AFTER TAKEOFF FROM CDG, CREW NOTED THE LEFT HYDRAULIC QUANTITY DECREASING TO ZERO, AND THE LEFT SYSTEM QU ANTITY AND PRESSURE LIGHTS ILLUMINATING. CRWE ALSO RECEIVED THE EICAS MESSAGES L HYD QTY AND L HYD SYS PRESS. FLIGHT R ETURNED TO CGD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A SEAL RUPTURED IN THE LEFT EDP PRESSURE AND CASE DRAIN FILTER MODULE ASSEMBLY. MODULE WAS REPLACED. THE VENDOR REPORTED THAT A PRESSURE SURGE OCCURED WHICH DESTROYED THE FILTER AND COCKED THE FILTER HOUSING, DAMAGING BOTH THE FILTER HOUSING AND CASE THREADS, RESULTING IN THE LEAK. (M) 2 L 7 2 4F RT A1NM 2000022600797 20000226 00797 WP 2000 2 26 USAAD99179 1 19991216 A 3260 MS25237387 LAMP DOUG DC9 DC982 3022082 WP INSTRUMENT PANEL FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 816US 48096 DFW-CLT - FLT 1977 - ON APPROACH, AFTER GEAR EXTENSION, THE RIGHT MLG GREEN LIGHT WAS INOPERATIVE. THE FLIGHT CREW CHEC KED THE GEAR POSITION THROUGH THE PERISCOPE AND FLEW BY THE TOWER TO CONFIRM THE GEAR WAS DOWN. THE A/C LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MLG INDICATION LAMP. (M) 2 L 7 2 4F A6WE 2000022600798 20000226 00798 NE 2000 2 26 USAAD99178 2 19991216 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE RIGHT BIRDSTRIKE A USAA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 EA 19 926VJ 48146 649325 IND-DCA - FLT 769 - AFTER TAKEOFF THE RIGHT ENGINE HAD A COMPRESSOR STALL THAT LASTED FOR ABOUT 3 SECONDS.. THIS WAS AC COMPLISHED BY AN UNUSUAL ODOR IN THE CABIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANC E FOUND EVIDENCE OF A BIRD STRIKE. THE ENGINE WAS INSPECTED AND NO DAMAGE WAS FOUND. (M) 2 L 7 2 4F 4 F A6WE E2EA 2000022600799 20000226 00799 NE 2000 2 26 2000ZZZM204 2 19990816 A 7321 487094 B-NUT BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FCU LOOSE A FX7A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 79750 22452 ON FAE - FLT 945 - KMEM TO NBJ, DURING CLIMB, THROUGH FL260 NR 3 ENGINE STARTED FLUCTUATING INTERMITTENT AT FIRST THEN S TEADY. AFTER LEVEL OFF AT FL290, NR 3 ENGINE CONTINUED TO FLUCTUATE. AIRCRAFT RETURNED TO KMEM. ON GROUND MAINTENANCE INSPECTED NR 3 ENGINE AND FOUND LOOSE 'B' NUT ON THE FUEL CONTROL UNIT. 'B' NUT WAS TIGHTENED AND LEAK CHECKED PER MM 73-20-00. ENGINE WAS RAN IAW MM 71-00-00 AND OPS CHECKED NROMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000022600800 20000226 00800 NM 2000 2 26 UIEA9998 1 19991216 A 3150 EICAS BOEING 747 74747UF 1384949 NM GE CF6 CF650E2 30018 NE COCKPIT MALFUNCTIONED A UIEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 408MC 29261 FLT AZ9162 - MXP-ORD - ON TAKEOFF ROLL AT 20 KNOTS, THE FLT CREW SAW A MOMENTARY RED FLASH ON THE EICAS. BELIEVED TO BE A FIRE WARNING MESSAGE, BUT IT WAS TOO QUICK TO READ. TAKEOFF WAS ABORTED WITHOUT EXCEEDING TAXI SPEED AND A/C RETURNE D TO BLOCKS. WHEN A/C ARRIVED AT THE BLOCKS, THERE WAS NOT EICAS MESSAGE. ALSO, THERE WERE NO PRESENT LEG FAULT(PFL) M ESSAGES. PERFORMED FIRE WARNING/OVERHEAT TEST AND FOUND TO BE NORMAL. AIRCRAFT VISUALLY CHECKED FOR ABNORMALITIES AND NONE FOUND. NO HISTORY MESSAGES IN THE CMC. UNABLE TO DUPLICATE THE REPORTED DISCREPANCY. (M) 2 L 7 4 4F 4 F RT 1384945 E23EA 2000022600801 20000226 00801 WP 2000 2 26 2000ZZZM205 1 19990620 A 5315 FLOORBEAM DOUG DC8 DC8F55 3021928 WP BS 1480 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION, FOUND CORROSION DAMAGE FLOORBEAM AT STATION FS 1480 RBL 41. REPAIRED CORROSION DAMAGE IAW FI NE AIR EO NR 9906212. (M) 2 L 7 4 4F 4A25 2000022600802 20000226 00802 WP 2000 2 26 2000ZZZM206 1 19990620 A 5315 FLOORBEAM DOUG DC8 DC8F55 3021928 WP BS 1320 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION FOUND CORROSION DAMAGE FLOORBEAM AT STATION FS 1320 LBL 25 TO 35. REPAIRED CORROSION DAMAGE I AW FINE AIR EO NR 9906201. (M) 2 L 7 4 4F 4A25 2000022600803 20000226 00803 WP 2000 2 26 2000ZZZM207 1 19990620 A 5315 FLOORBEAM DOUG DC8 DC8F55 3021928 WP BS 1400 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION, FOUND CORROSION DAMAGE FLOORBEAM AT STATION FS 1400 LBL. REPAIRED CORROSION DAMAGE IAW FINE AIR EO NR 9906204. (M) 2 L 7 4 4F 4A25 2000022600806 20000226 00806 NM 2000 2 26 USAA020001 1 19990717 A 7603 MS250081 SWITCH BOEING 727 727225 1384077 NM NR 2 ENGINE OUT OF ADJUST A USAA O OTHER N FALSE WARNING TO TAKEOFF 1 EA 19 918TS 20445 FLT 6161 - BOS-LGA - UPON GEAR RETRACTION, AURAL WARNING STEADY HORN SOUNDED. GEAR RETRACTED AND EXTENDED NORMALLY. AU RAL WARNING WENT OUT AFTER AT 3 MINUTES AFTER 2ND GEAR RETRACTION. ALL RED LIGHTS REMAINED ILLUMINATED ON GEAR RETRACTI ON. TROUBLESHOT PROBLEM TO ADJUSTMENT OF THE NR 2 ENGINE POWER LEVER/LANDING GEAR SWITCH. ADJUSTED SAME PER MM 31-26-0 AND TESTED OK PER MM 31-26-0 (SEVERAL TIMES). (M) 2 L 7 3 4F A3WE 2000022600813 20000226 00813 WP 2000 2 26 2000ZZZM210 1 19990916 A 5313 LONGERON DOUG DC8 DC8F55 3021928 WP BS 1490-1600 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 LONGERON 6R STATION 1490 TO 1600 HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED AND REPAIR PER DC-8 SRM 53-2-2 PAGE 59/60 PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8/11/99. (M) 2 L 7 4 4F 4A25 2000022600814 20000226 00814 WP 2000 2 26 2000ZZZM211 1 19990915 A 7830 RING DOUG DC8 DC8F55 3021928 WP THRUST REVERSER CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 INBOARD TOP SIDE OF TRANSLATING RING HAS CRACK NR 4 ENGINE. STOP DRILLED CRACK, NDT TO ASSURE CRACK STOPPED. FABRICATE D DOUBLER AND INSTALLED PER EO NR 99-136 WITH APPROVED 8110-3 DATED 9/2/99. (M) 2 L 7 4 4F 4A25 2000022600815 20000226 00815 WP 2000 2 26 2000ZZZM212 1 19990823 A 5552 FITTING DOUG DC8 DC8F55 3021928 WP ELEVATOR GOUGED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 NR 4 RIGHT ELEVATOR 'A' FRAME AFT MOUNT GOUGED. GOUGE IS A MAXIMUM OF .019 INCHES DEEP. BLENDED GOUGE SMOOTH. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8/20/99. (M) 2 L 7 4 4F 4A25 2000022600816 20000226 00816 WP 2000 2 26 2000ZZZM213 1 19991108 A 5711 SPAR DOUG DC8 DC8F55 3021928 WP WS 680 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 LOWER FRONT SPAR HORIZ LEG 10 INCHES CRACK FS 680 - 26.5 TO 36.5 INCH RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS AND INSTALLED IAW DC-8 S/B 57-30R5. (M) 2 L 7 4 4F 4A25 2000022600817 20000226 00817 WP 2000 2 26 2000ZZZM214 1 19991029 A 5711 SPAR DOUG DC8 DC8F55 3021928 WP WS 31.04 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 FOUND DURING C-CHECK, A 4.75 INCH CORROSION CRACK APPROX STATION XCW 31 LEFT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. RO UTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK. REMOVED, TREATED AND PRIMED. FILLED SEALER CONTINUED THE INSTALLATION OF LOWER FRONG SPAR CAP. REPAIR PER NR 57-2-6- PER EO NR 99-136 WITH APPROVED 8110-3 DATED 10/18/99. (M) 2 L 7 4 4F 4A25 2000022600818 20000226 00818 WP 2000 2 26 2000ZZZM215 1 19991102 A 5753 WEB DOUG DC8 DC8F55 3021928 WP TE FLAP CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 FOUND DURING C-CHECK, RIGHT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT CRACKED SECTION. FABRICATED NEW WEB AND INSTALLED PER EO NR 99-136 WITH APPROVED 8110-3, DATED 10/29/99. (M) 2 L 7 4 4F 4A25 2000022600819 20000226 00819 WP 2000 2 26 2000ZZZM216 1 19990818 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 1320 GOUGED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 DEEP GOUGE FORWARD OF R-2 DOOR FUSELAGE STATION 1320 RIGHT. BLEND SMOOTH AND REMOVED CRACK BY DRILLING .5 INCH DIAMETER HOLE. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8/11/99. (M) 2 L 7 4 4F 4A25 2000022600822 20000226 00822 NM 2000 2 26 USAA020003 1 19991106 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS 20447 FOUND ON L/S - R-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKS OK. (M) 2 L 7 3 4F A3WE 2000022600880 20000226 00880 EU 2000 2 26 RAIA9912039 1 19991229 A 2731 48635028010 INDICATOR AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 423TE 4593 119 FLT 7402 - STL - PITCH TRIM CIRCUIT BREAKER POPPED WOULD NOT RESET. MAINTENANCE REPLACED PITCH TRIM INDICATOR. (M) 2 H 7 2 4T RT A53EU 2000022600881 20000226 00881 WP 2000 2 26 HALA9900290 1 19991219 A 3231 SENSOR DOUG DC9 DC951 3022051 WP LT MLG MALFUNCTIONED A HALA O OTHER O OTHER AP APPROACH 1 WP 13 699HA A49792 47763 FLT 151 - APP TO HNL, LT LANDING GEAR WOULD NOT LOCK DOWN, SELECTED. (NO GREEN LIGHT, RED LIGHT GEAR UNSAFE ON) RECYCLE D TWICE, LOCKED DOWN OK. LEFT GEAR DOWN LOCK SENSOR WIRE OPEN. REPLACED SENSOR ASSY ELECT CHECK OK. (M) 2 L 7 2 4F RT A6WE 2000022600882 20000226 00882 WP 2000 2 26 HALA9900282 1 19991222 A 3231 CONTROL BOX DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A HALA O OTHER O OTHER AP APPROACH 1 WP 13 709HA 47764 HNL - FLT 170 - NOSE GEAR DID NOT EXTEND. PERFORMED ALTERNATE GEAR EXTENTION PROCEDURE. GEAR CAME DOWN. NOSE SAFE LIG HT DID NOT ILLUMINATE, NOR DID NOSE LIGHT ILLUMINATE, GEAR UNSAFE. FOUND SKIN DAMAGED RT OF DRAIN HOLE, JUST AFT OF NLG . REPLACED PROXIMITY CONTROL BOX. BITE CHECK GOOD. FOUND SPRING TOOL WEDGED INTO AREA AROUND SEIVEL GLANDS, REMOVED T OOL ACCOMPLISHED GEAR SWING GEAR PER MM. NO DEFECTS NOTED. REPAIRED PER HAL M105 NR 10195 INTERIM REPAIR. PERMANENT A T NEXT C-CHECK. (M) 2 L 7 2 4F RT A6WE 2000022600883 20000226 00883 WP 2000 2 26 HALA9900286 1 19991224 A 2820 SEPARATOR DOUG DC9 DC951 3022051 WP FUEL SYSTEM CONTAMINATED A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 603DC 47784 FLT 388 - HNL - STRONG FUEL SMELL IN CABIN, STRONGEST ABOUT EMERGENCY EXIT. REPLACED LEFT AND RIGHT SEPARATORS, LEAK CH ECK AND SMELL CHECK OK. INSPECTED APU SECTION FOR FUEL LEAKS. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A6WE 2000022600885 20000226 00885 WP 2000 2 26 USAAD99189 1 19991215 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802US 48036 CLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED 8 AISLE LIGHT BATTERIES, 1 CONTROL MODULE B ATTERY, AND 1 AFT SERVICE DOOR LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2000022600886 20000226 00886 WP 2000 2 26 2000ZZZM223 1 19991215 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802US 48036 CLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED 8 AISLE LIGHT BATTERIES, 1 CONTROL MODULE B ATTERY, AND 1 AFT SERVICE DOOR LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2000022600887 20000226 00887 WP 2000 2 26 2000ZZZM224 1 19991215 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802US 48036 CLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED 8 AISLE LIGHT BATTERIES, 1 CONTROL MODULE B ATTERY, AND 1 AFT SERVICE DOOR LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 2000022600888 20000226 00888 WP 2000 2 26 USAAD99180 1 19991221 A 3350 14597101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48042 PHL - THE GALLEY SERVICE DOOR AND RIGHT AFT EMERGENCY WINDOW EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE GALLEY SER VICE DOOR AND EMERGENCY WINDOW EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2000022600889 20000226 00889 WP 2000 2 26 2000ZZZM225 1 19991221 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48042 THE AFT AIRSTAIR EXIT IDENTIFIER LIGHT WAS INOPERATIVE. REPLACED THE AFT AIRSTAIR EXIT IDENTIFIER BATTERY. (M) 2 L 7 2 4F A6WE 2000022600890 20000226 00890 WP 2000 2 26 2000ZZZM226 1 19991221 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 48042 THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED 7 LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 2000022600891 20000226 00891 WP 2000 2 26 USAAD99181 1 19991223 A 3350 14597101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 814US 48094 BOS - THE TAILCONE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 2000022600892 20000226 00892 WP 2000 2 26 USAAD99184 1 19991227 A 3350 AD4002P BATTERY DOUG DC9 DC931 3022065 WP CABIN DIRTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920VJ 48140 LGA - FOUND CABIN EMERGENCY FLOOR LIGHTING INOPERATIVE FORWARD OF ROW FIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE BA TTERY PACK. (M) 2 L 7 2 4F A6WE 2000022600893 20000226 00893 NM 2000 2 26 USAASB99297 1 19991218 A 8000 1G309 PRESSURE SWITCH BOEING 737 7372B7 1384560 NM NR 1 ENGINE FAILED A USAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 EA 19 286AU 23133 BWI - FLT 2740 - ON DESCENT INTO BWI, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW SHUTDOWN THE NR 1 ENGINE AT 6,000 FT PER HANDBOOK PROCEDURES. FLIGHT LANDED AT BWI WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 7 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE START VALVE OPEN LIGHT PRESSURE SWI TCH. ORIGINAL SWITCH WAS FOUND SHORTED. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 2000022600894 20000226 00894 NE 2000 2 26 USAAD99185 2 19991229 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE RIGHT FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M Y OVER TEMP ENGINE STOPPAGE CL CLIMB 1 EA 19 929VJ 32643 48118 657064 MKE - FLT 359 - AT FLT LEVEL 2000 FT, SHUTDOWN RIGHT ENGINE DUE TO EXCESSIVE EGT. CAPTAIN DECLARED AN EMERGENCY AND RET URNED TO THE FIELD, MAKING A SAFE, UNEVENTFUL LANDING. FOUR MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE RIGHT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 2000022600895 20000226 00895 NE 2000 2 26 USAAF00002 2 19990103 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAY65015 54557 NE NR 1 VIBRATION A USAA A UNSCHED LANDING E VIBRATION/BUFFET DE DESCENT 1 EA 19 851US 11278 IND-PIT - FLT 430 - ON DESCENT, ENGINE 1 HIGH VIBRATION CAUTION WAS INDICATED ON THE MFDU. VIBRATION FELL WITHIN LIMITS ONCE THRUST LEVER WAS RETARDED TO THE IDLE POSITION. AN EMERGENCY WAS DECLARED FOLLOWED BY AN UNEVENTFUL LANDING. THE ENGINE WAS NOT SHUT DOWN. MAINTENANCE INSPECTED ENGINE INLET AND EXHAUST, BOTH MAG PLUGS, TURBINE (HP AND LP) SCREENS, THRUST BEARING AND INTERNAL AND HS GEARBOX SCREENS. ALL FOUND OK. FINALLY, RAN ENGINES AND FOUND ALL PARAMETERS WERE WITHIN LIMITS. (M) 2 L 7 2 4F 4 F RT E25NE 2000022600896 20000226 00896 NE 2000 2 26 USAASB99296 2 19991217 A 7320 8063207 MEC BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 337US 22962 23235 CLT - FLT 299 - ON CLIMB-OUT FROM CLT, AT FL210, THE NR 1 ENGINE N1 INDICATOR BEGAN FLUCTUATING IN ALL PARAMETERS OF FLI GHT. THE N1 WOULD SURGE PLUS OR MINUS 7 PERCENT EVERY 7 TO 10 SECONDS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITH OUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE MAIN ENGINE CONTROL. PERFORMED ENGINE RUN. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2000022600897 20000226 00897 EU 2000 2 26 USAAF99058 1 19991221 A 3232 1252525 ACTUATOR FOKKER F28 F28MK0100 4990807 EU MLG DOOR FAILED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 885US 11345 PIT-CLT - FLT 1948 - DURING LANDING GEAR RETRACTION ON CLIMB-OUT THE NR 1 HYDRAULIC SYSTEM INDICATED LOW PRESSURE AND LO W QUANTITY. THE AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT INCIDENT, AND WAS TOWED TO THE GATE DUE TO NO NOSEWHEEL STEERING. MAINTENANCE REPLACED THE RIGHT INBOARD MAIN LANDING GEAR DOOR FORWARD ACTUATOR. (M) 2 L 7 2 4F RT 2000022600898 20000226 00898 EU 2000 2 26 SIMA0047 1 19991227 A 3350 601321 POWER SUPPLY SAAB SF340 340B 7860101 EU FAILED UNKNOWN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 247AE 17492 340B247 DFW - FLT 3414 - EMERGENCY LIGHT OVER 3B/C, 5B/C AND 4A INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT 20LN. OPS CH ECKS GOOD. (M) 2 L 7 2 4T RT A52EU 2000022600899 20000226 00899 2000 2 26 SIMA0048 4 19991225 A 3460 6227491210 FCC SAAB SF340 340B 7860101 EU E/E BAY FAILED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 253AE 2040 340B253 JFK - FLT 5051 - AFTER TAKEOFF, AIRCRAFT ROLLED 15 TO 20 DEGREES TO LEFT. ON CLIMB, AIRCRAFT YAW RIGHT AND LEFT THEN PI TCHED DOWN 5 DEGREES TO APPROX LEVEL. AIRCRAFT RETURNED WITH NO INCIDENT. REMOVED AND REPLACED FLIGHT CONTROL COMPUTER , OPS CHECK AND FCF OF AIRCRAFT GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000022600900 20000226 00900 EU 2000 2 26 SIMA0049 1 19991224 A 3350 6500111 LAMP HOLDER SAAB SF340 340B 7860101 EU ROW 10C FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 392AE 340B392 DFW - FLT 3609 - AIRCRAFT WAS AIR INTERRUPT FOR SMOKE IN CABIN DUE TO LIGHT BALLAST AT SEAT 10C. REMOVED AND REPLACED L AMP HOLDER AT 10C. OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 2000022600901 20000226 00901 EU 2000 2 26 SIMA3647 1 19991218 A 3350 LIGHT SAAB SF340 340B 7860101 EU ROW 6-11 INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 304AE 340B304 MIA - FLT 5226 - ROWS 6 THROUGH 11 OVERHEAD AND FLOOR EMERGENCY LIGHTING INOPERATIVE. EMERGENCY EXIT LIGHTS ROW 8 INOPE RATIVE. TROUBLESHOT SYSTEM. ALL LIGHTS AND EMERGENCY LIGHTS ILLUMINATED. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000022600903 20000226 00903 NE 2000 2 26 SIMA3551 2 19991218 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MALFUNCTIONED A SIMA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 313AE 15451 340B313 GE785347 SRQ - FLT 5365 - LOSS OF OIL PRESSURE ON RIGHT ENGINE. SHUT DOWN ENGINE IN FLIGHT WITH WARNING LIGHT AND 0.0 PRESSURE. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL AND LEAK CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 2000022600904 20000226 00904 EU 2000 2 26 SIMA3624 1 19991220 A 7120 S5421020000400 Z-MOUNT AEROSP ATR42 ATR42300 8680920 EU RT ENGINE WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 47AE A6TG0068 047 SAW - DURING INSPECTION/MAINTENANCE, FOUND RIGHT ENGINE INBOARD AFT ZEE-MOUNT AND THE FORWARD W-MOUNT CHAFED BEYOND LIMI TS. REMOVED AND REPLACED FORWARD AND AFT MOUNT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000022600905 20000226 00905 EU 2000 2 26 2000ZZZM227 1 19991220 A 7120 S5411020000400 W-MOUNT AEROSP ATR42 ATR42300 8680920 EU RT ENGINE WORN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 47AE 644 047 SAW - DURING INSPECTION/MAINTENANCE, FOUND RIGHT ENGINE INBOARD AFT ZEE-MOUNT AND THE FORWARD W-MOUNT CHAFED BEYOND LIMI TS. REMOVED AND REPLACED FORWARD AND AFT MOUNT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000022900001 20000229 00001 CE 2000 2 29 2000ZZZX470 1 19991230 A 7920 AS3209017 SEAL BEECH 1900 1900D 1154162 CE ENGINE OIL LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 835CA 491 114063 UE30 POST-FLIGHT INSPECTION FOUND OIL LEAKING FROM RT ENGINE LOWER FORWARD COWL. INSPECTION REVEALED THE SOURCE OF LEAK TO B E THE POWER SECTION OIL TRANSFER TUBE ELBOW. REPLACED 3 EACH PACKINGS. LEAK CHECK SATISFACTORY ON GROUND RUN. 2 L 7 2 4T RT A24CE 2000022900002 20000229 00002 WP 2000 2 29 2000ZZZX471 1 19990817 A 2910 AE2460001J0165 LINE DOUG DC8 DC861 3021952 WP HYDRAULIC SYSTEM CHAFED A FXLA A UNSCHED LANDING K S FLUID LOSS AFFECT SYSTEMS CL CLIMB 1 SO 19 30UA 45888 AFTER TAKEOFF FROM MIA, EXPERIENCED HYDRAULIC QUANTITY LOSS AND PRESSURE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED HYDRAULIC PRESSURE LINE CHAFED AT NR 3 ENGINE HYDRAULIC PUMP. REPLACED LINE AND CHECKED FILTERS. S ERVICED SYSTEM AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 2000022900003 20000229 00003 NE 2000 2 29 2000ZZZX472 2 19991021 A 7321 71128719 FCU DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE INOPERATIVE A FXLA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 19 7046H 46011 645498 DURING SHORT FINAL, NR 3 ENGINE FLAMEOUT; FUEL ON NR 3 TANK WAS 5800; SUSPECT FCU MALFUNCTION. CHANGED AND TESTED FCU U NIT IAW PW MM 72-0. (X) 2 L 7 4 4F 4 F 4A25 1E8 2000022900004 20000229 00004 WP 2000 2 29 2000ZZZX473 1 19990923 A 2910 37775901 LINE DOUG DC8 DC8F54 3021926 WP HYDRAULIC SYSTEM LEAKING A FXLA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 7046H 46011 FLT 790 - ON DESCENT INTO MIA FROM POS, REPORTED LOSS OF HYDRAULIC FLUID DOWN TO STANDPIPE. PERFORMED EMERGENCY CHECKLI ST. DECLARED EMERGENCY AND LANDED FULL FLAPS AT MIA WITHOUT INCIDENT. FOUND NR 2 ENGINE DRIVE HYDRAULIC PUMP LINE LEAK ING, RE-TORQUED LINE PER MM 13-6-1 AND LEAK CHECKED OK. CAPTAIN'S IRREGULARITY REPORT SENT TO FAA ON 9-23-99. (X) 2 L 7 4 4F 4A25 2000022900005 20000229 00005 NM 2000 2 29 USAASB99303 1 19991226 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AU 22757 CLE - WHILE ACCOMPLISHING OVERNIGHT CHECK AND PERFORMING EMERGENCY LIGHT TEST, MAINTENANCE FOUND THE AFT RIGHT EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOO D. (X) 2 L 7 2 4F A16WE 2000022900006 20000229 00006 NM 2000 2 29 2000ZZZX474 1 19991205 A 5300 BUFFET BOEING 727 727231 1384079 NM STRUCTURE DETECTED A MYWA J A DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 808MA 21988 ON TAKEOFF FROM ACA WHILE CLIMBING THROUGH 18,000 FEET, FELT AIRCRAFT JOLT. RETURNED TO ACA FOR GROUND INSPECTION. RET URNED TO ACA AFTER DUMPING FUEL TO OBTAIN PROPER WEIGHT FOR LANDING. INSPECTED AIRCRAFT PER INSTRUCTIONS FROM MIAMI AIR MAINTENANCE CONTROL, FOUND NO DEFECTS OR MALFUNCTIONING SYSTEMS. PERFORMED LOCAL FLIGHT OF AIRCRAFT, NO ABNORMAL FLIGH T PROFILES, NO ABNORMALTIES EXPERIENCED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F A3WE 2000022900011 20000229 00011 2000 2 29 WRLA99023 4 19991204 A 2211 4059001907 COMPUTER HONEYWELL DOUG MD11 MD11 3023602 NM E/E BAY FAILED A WRLA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 277WA 48743 AUTOPILOT NR 1 AND NR 2 FAILED ON DEPARTURE FROM PGUM. AIRCRAFT RETURNED TO PCUM FOR CORRECTIVE ACTION. REMOVED AND RE PALCED NR 2 FCC. RETURN TO SERVICE TEST SATISFIED. DEFERRED NR 1 AUTOPILOT PER MEL 22-10-1. AIRCRAFT DOWNGRADED TO CA T II SINGLE LAND. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (X) 2 L 7 3 4F RT A22WE 2000022900012 20000229 00012 NM 2000 2 29 USAASB00005 1 19990107 A 2131 7110025 SELECTOR BOEING 737 7374B7 1384702 NM CABIN PRESSURE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 427US 44932 35394 24549 TPA - FLT 984 - ON CLIMB-OUT FROM TPA, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO FIELD AT TPA AND LAND ED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE CABIN PRESSURE SELECTOR PANEL AT FAULT P ER JOB CARD J321-30-10. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL. ALSO, AS PRECAUTIONARY, REMOVED AND REPLAC ED THE CABIN PRESSURE CONTROLLER (P/N 763810-1). RAN ENGINES AND OPERATED PRESSURE CONTROL VALVE PER JOB CARD. NO AIRF RAME AIR LEAKAGE NOTED. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4F RT A16WE 2000022900013 20000229 00013 NM 2000 2 29 USAABB99056 1 19991017 A 2497 300672 WIRE BOEING 767 767201 1385125 NM GALLEY ARCED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 649US 23901 PIT - FLT 781 - CREW NOTED ELECTRICAL SMELL IN AFT GALLEY. (CIRCUIT BREAKER HAD TRIPPED.) MAINTENANCE FOUND THE CABLE ASSEMBLY FOR HEATED MEAL CART A201 ARCING AND REPLACED IT. (X) 2 L 7 2 4F RT A1NM 2000022900014 20000229 00014 NM 2000 2 29 TSAA9933499 1 19991207 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 6 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 2000022900015 20000229 00015 NM 2000 2 29 TSAA9933497 1 19991209 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED BATTERY PACK FOR NR 2 POSITION FLOOR LIGHT DUE TO NO TEST. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 2000022900016 20000229 00016 NM 2000 2 29 TSAA9933496 1 19991208 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED BATTERY PACK FOR NR 2 POSITION FLOOR LIGHT DUE TO NO TEST. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 2000022900017 20000229 00017 NM 2000 2 29 AALA991375 1 19990911 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 8 AB LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 393AN 29430 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 8 A/B INOPERATIVE. RESECURED CONNECTOR TO EMERGENC Y EXIT SEAT LIGHT AT ROW 8 A/B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000022900018 20000229 00018 NM 2000 2 29 AALA991964 1 19991224 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 678AN 29428 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT IN MID-GALLEY AREA INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000022900019 20000229 00019 NM 2000 2 29 AALA991945 1 19991219 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AN 29590 MIA - DURING OVERNIGHT MAINTENANCE, EEMRGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000022900020 20000229 00020 EA 2000 2 29 ASOA99164 1 19991213 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 828AS 7213 DURING INSPECTION, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING ON FLOOR LIGHTS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4F RT A21EA 2000022900021 20000229 00021 SO 2000 2 29 C2XA99BT107 1 19991118 A 3350 3025101 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12967 145133 EWR - FLT CO4228 - CREW REPORTED RIGHT EMERGENCY LIGHT LENSE CRACKED. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMER GENCY. OPS CHECK SYSTEM GOOD. (X) 2 L 7 2 4F RT T00011AT 2000022900022 20000229 00022 GL 2000 2 29 C2XA99TY002 2 19991026 A 7200 23070402 ENGINE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16501 381 145145 CAE311159 TYS - DURING A SCHEUDLED INSPECTION, THE LEFT ENGINE WAS FOUND TO BE PRODUCING METAL THAT WAS BEYOND MANUFACTURER'S LIMI TS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB-135 MM 71-00-00, OPERATIONAL AND LEAK CHECKS WERE SATISFAC TORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4F 4 F RT T00011AT TE6CH 2000022900023 20000229 00023 2000 2 29 2000ZZZX479 4 19991013 A 3417 HG280D80 ADC DOUG DC10 DC1040 3023508 WP COCKPIT MALFUNCTIONED A CLCA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 142WE 46966 KMIA/MPTO - FLT 055 - AT 2:20 Z, ABORTED TAKEOFF, ON TAKEOFF ROLL FIRST OFFICER'S AIRPSPEED INDICATOR READS 20 KNOTS LO WER THAN THE CAPTAIN'S, AND STANDBY INDICATORS (THEY READ 100 KNOTS). FIRST OFFICER'S READS 75 KNOTS. NOTE: NO HIGH E NERGY STOP. PERFORMED PITOT STATIC LEAK CHECK ON FIRST OFFICER'S PITOT STATIC SYSTEM, NO LEAKS NOTED. REMOVED AND REPL ACED FIRST OFFICER'S DIGITAL AIR DATA COMPUTER. FIRST OFFICER'S AIRSPEED WITHIN TOLERANCE. OPERATIONAL CHECK GOOD IAW MM 34-11-00. RELEASED AIRCRAFT FOR REVENUE SERVICE. (X) 2 L 7 3 4F A22WE 2000022900024 20000229 00024 WP 2000 2 29 AALA20000062 1 19991230 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1521 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - SUPPORT ANGLE UNDER NR 6 ROLLER TRAY CORRODED AT STA 1521. REMOVED AND REPLACED CORRODED SECTION WITH NEW SERVICE ABLE SECTION PER ECO 73491 DATED 1-3-2000. TST: 96,475.29 HOURS. CYCLES: 19,001. (X) 2 L 7 3 4F A22WE 2000022900035 20000229 00035 NM 2000 2 29 F3LA99130 1 19991028 A 5330 SKIN BOEING 737 737228 13844AG NM R1 DOORWAY CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 237TR 32975 279 23007 DEN - DURING SERVICE CHECK, INSPECTION REPORTED A 2.5 INCH CRACK AT THE LOWER AFT CORNER OF THE R-1 DOOR CUTOUT. MAINTE NANCE REPAIRED PER SRM 53-30-3, FIG 26, PAGE 90 THROUGH PAGE 92B. CYCLES: 187. (X) 2 L 7 2 4F RT A16WE 2000022900036 20000229 00036 NM 2000 2 29 F3LA99145 1 19991128 A 3233 65488105 ACTUATOR BOEING 737 7373S1 138447S NM RT MLG FAILED A F3LA O OTHER J WARNING INDICATION AP APPROACH 1 NM 03 311FL 1356 5209 24856 SFO - FLT 653 - DURING APPROACH INTO SFO, FLIGHT CREW REPORTED THE RT MAIN LANDING GEAR WOULD NOT EXTEND. USED ALTERNAT E METHOD TO EXTEND GEAR AND GREEN LIGHT ILLUMINATED. FERRIED AIRCRAFT TO DEN. MAINTENANCE REPLACED RT MAIN LANDING GEA R DOWNLOCK ACTUATOR. PERFORMED OPERATIONAL CHECK, LEAK CHECK AND GEAR SWING, AND SYSTEM CHECKED OKAY. CYCLES: 617. ( X) 2 L 7 2 4F RT A16WE 2000022900037 20000229 00037 WP 2000 2 29 GTIA99001202 1 19991111 A 2751 SWITCH DOUG DC9 DC983 3022083 WP FLAP WARNING CONTAMINATED A GTIA O OTHER O OTHER NR NOT REPORTED 1 GL 23 808NK 49504 TPA - FLT 632 - DURING POWER APPLICATION, TAKEOFF WARNING HORN SOUNDED (FLAPS). ALL FLIGHT CONTROLS WERE IN THEIR PROPE R POSITION. FOUND FLAP HANDLE WARNING SWITCH S1-492 COVERED WITH DUST/FUZZ. CLEANED SWITCH. SYSTEM OPS GOOD PER MM 31 -51-02. (X) 2 L 7 2 4F RT A6WE 2000022900038 20000229 00038 NM 2000 2 29 2000ZZZX480 1 19990925 A 3230 2732513 CONTROL CABLE 657376112 BOEING 737 737222 1384473 NM RT MLG JAMMED C KNNB A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 25 135TA PDS7099 19940 UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. LATER INVESTIGATION REVEALED THE AIR/GROUND TELEFLEX CABLE ON THE RIGHT L ANDING GEAR JAMMED. THE CABLE WAS REPLACED IAW BOEING MM AND LANDING GEAR RETRACT CHECK WAS PERFORMED. CHECKED OK. 2 L 7 2 4F A16WE 2000022900039 20000229 00039 2000 2 29 2000ZZZX481 4 19990925 A 2297 WIRE 6552812 BOEING 737 737222 1384473 NM E/E GAY BROKEN C A KNNB O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 25 135TA M176 19940 UNCOMMANDED RT AND LT YAW AFTER TAKEOFF. SWITCHED YAW DAMPER TO THE 'OFF' POSITION AND YAWING STOPPED. MAINTENANCE FOU ND A BROKEN WIRE IN THE D4117J ELECTRICAL CONNECTOR AT THE FORWARD END OF THE E1 EQUIPMENT RACK FOR THE AUTOPILOT ACCESS ORY UNIT. THE WIRE WAS REPAIRED IAW B737-22-120. SYSTEM CHECKED OK. 2 L 7 2 4F A16WE 2000022900040 20000229 00040 NE 2000 2 29 NOCA11099 2 19990923 A 7250 HPC BLADES BOEING 737 7378Q8 13844BX NM GE CFM56 CFM567B24 NE ENGINE DAMAGED A NOCA K NONE O OTHER UK UNKNOWN 1 EA 15 800NA 3152 28215 875284 DURING C-SERVICE BORESCOPE, FOUND DAMAGED BLADES IN HIGH PRESSURE COMPRESSOR IN STAGES 2, 3, 4, 6, 7, AND 8. THE BLADES HAD NICKS, TEARS, IMPACT DAMAGE. ENGINE REMOVED FOR SHOP REPAIR. (X) 2 L 7 2 4F 4 F RT A16WE E00055EN 2000022900041 20000229 00041 NM 2000 2 29 F3LA99128 1 19991011 A 2780 DETENT ARM BOEING 737 737228 13844AG NM LE FLAPS OUT OF ADJUST A F3LA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 03 237TR 57 23007 DEN - FLT 416 - FLIGHT CREW REPORTED AIRCRAFT ROLLED TO RIGHT WITH FLAPS EXTENDED AND REQUIRED 10 DEGREES AILERON TO COM PENSATE. MAINTENANCE ADJUSTED NR 1 AND NR 6 LEADING EDGE SLAT DETENT ARM TENSION PER MM 27-81-21. FOUND LT WING OUTBOA RD TRAILING EDGE FLAP OUT OF RIG IN 'UP' POSITION. RIGGED FLAPS PER 27-51-01. PERFORMED TEST FLIGHT AND CHECKED OKAY. CYCLES: 37. (X) 2 L 7 2 4F RT A16WE 2000022900042 20000229 00042 SO 2000 2 29 SIMA993201 1 19991116 A 3234 7455501 CONTROL LEVER EMB 145 EMB145LR SO COCKPIT FAILED A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 624AE 0084 145111 DFW - FLT 3619 - AFTER TAKEOFF, THE LANDING GEAR CONTROL LEVER COULD NOT BE MOVED TO THE UP POSITION. REMOVED AND REPLA CED LANDING GEAR CONTROL LEVER. FUNCTIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 2000022900043 20000229 00043 SO 2000 2 29 SIMA993274 1 19991123 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 629AE 145130 ORD - FLT 4162 - STRONG FUEL ODOR IN CABIN NEAR PASSENGER SEAT ROWS 14 AND 15. INSPECTED AIRCRAFT EXTERNAL DRAINS AND P ANELS. OPENED CABIN FLOOR PANELS AND PERFORMED ENGINE GROUND RUNS, BUT NO EVIDENCE OF LEAKS OR VAPORS WAS DETECTED OF A NY KIND. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 2000022900049 20000229 00049 EA 2000 2 29 UHLA991420 1 19991228 A 5210 85210368001 CABLE DHAV DHC8 DHC8311 1386006 EA PAX DOOR BROKEN A UHLA O OTHER O OTHER IN INSP/MAINT 1 NE 03 804SA 288 375 ILG/BUF - FLT 207 - WHILE PREPARING TO DEPLANE PASSENGERS, MAIN CABIN DOOR WOULD NOT FULLY EXTEND. MAINTENANCE WAS CALL ED AND CABLE WAS DISCONNECTED FOR PASSENGER DEBOARDING. REMOVED AND REPLACED MAIN CABIN DOOR ASSIST CABLE IAW DMM62 10- 00 REF WO 2181. DOOR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENT. (X) 2 H 7 2 4T RT A13NM 2000022900050 20000229 00050 EA 2000 2 29 UHLA991261 1 19991122 A 5210 CABLE DHAV DHC8 DHC8311 1386006 EA PAX DOOR DAMAGED A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 804SA 375 BUF/BED - FLT 222 - WHILE PREPARING AIRCRAFT FOR DEPLANING, MAIN CABIN DOOR WOULD NOT OPEN FULLY. MAINTENANCE WAS CALLE D AND DOOR CABLE WAS DISCONNECTED FOR PASSENGER DEBOARDING. REMOVED AND REPLACED MAIN CABIN DOOR ASSIST CABLE IAW DMM 5 2-10-00 REF WO 1939. OPS CHECK OF DOOR WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER INCIDENT. (X) 2 H 7 2 4T RT A13NM 2000022900051 20000229 00051 EA 2000 2 29 UHLA991312 1 19991207 A 5210 85210181008 CABLE DHAV DHC8 DHC8311 1386006 EA PAX DOOR BROKEN A UHLA O OTHER O OTHER IN INSP/MAINT 1 NE 03 803SA 16576 221 ALB/BUF - FLT 193 - WHILE PREPARING TO DEPLANE PASSENGERS, MAIN CABIN DOOR WAS LOWERED AND CABLE BROKE. REMOVED AND REP LACED MAIN CABIN DOOR ASSIST CABLE IAW DMM 52-10-00. INSPECTION REVEALED SPRING STRUT CABLE FRAYED. REMOVED AND REPLAC ED SPRING STRUT CABLE P/N 85210180001 IAW DMM 52-10-00. REF: WO 1312. OPS CHECK OF DOOR WAS SATISFACTORY. AIRCRAFT R ETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (X) 2 H 7 2 4T RT A13NM 2000030100004 20000301 00004 EU 2000 3 1 2000ZZZX491 1 19991221 A 6720 AC67032 SERVO SNIAS 350 AS350B2 8680813 EU TAIL ROTOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 851HW 2829 FR128 2622 SERVO LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000030100008 20000301 00008 NM 2000 3 1 USAA990564 1 19990621 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 178 BULKHEAD RBL 314 WL 187. INSTALLED DOUBL ER PER SRM 53-10-08 FIG 203. (M) 2 L 7 2 4F RT A16WE 2000030100009 20000301 00009 NM 2000 3 1 USAA991051 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 312, BL 0 UPPER CHORD BEAM. CORRO SION LEVEL 2, CORROSION TASK C53-107-02. INSTALLED NEW SECTION OF T-CAP WITH REPAIR SPLICES PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030100010 20000301 00010 NM 2000 3 1 USAA991078 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH AND 1 INCH UPPER CHORD STATION 328, LBL 28 BEAM. CORRO SION LEVEL 1. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030100011 20000301 00011 WP 2000 3 1 K4HA99099 1 19991218 A 3110 BALLAST DOUG DC8 DC855 3021927 WP INSTRUMENT PANEL FAILED A K4HA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 807CK 45767 SJS - FLT 14949 - SMOKE COMING FROM F/O RAIN REMOVAL HANDLE AREA. INSPECTED AND FOUND BURNED BALLAST FOR MAIN INSTRUMEN T LIGHTS. REMOVED CANNON PLUG AND STOWED PLUG, PLACED ON DMI. INSTALLED PLACARDS. (M) 2 L 7 4 4F 4A25 2000030100015 20000301 00015 SO 2000 3 1 SIMA3622 1 19991225 A 2611 SMOKE DETECTOR EMB 145 EMB145LR SO LAVATORY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 633AE 145148 ORD - FLT 4226 - LAVATORY SMOKE INDICATION IN FLIGHT. TROUBLESHOT SYSTEM AND PERFORMED OPERATIONAL CHECK, COULD NOT DUP LICATE PROBLEM. (M) 2 L 7 2 4T RT T00011AT 2000030200003 20000302 00003 EU 2000 3 2 2000ZZZX496 1 19991220 A 6520 350A33020006 SEAL SNIAS AS350 AS350B3 8680954 EU T/R GEARBOX LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 52285 16 MA1159 3251 LEAKING AT INPUT SEAL BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U NC H9EU 2000030200004 20000302 00004 EU 2000 3 2 2000ZZZX497 1 19991110 A 5511 355A1305200301 SPAR SNIAS 350 AS350B2 8680813 EU HORIZONTAL STAB CRCKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 162EH 5498 2147 HORIZONTAL STABILIZER SKIN ALONGLOWER RIGHT SIDE OF SPAR IS CRACKED. 1 G 7 1 3U H9EU 2000030200039 20000302 00039 NM 2000 3 2 USAA991047 1 19991013 A 5314 KEEL BEAM BOEING 737 737301 1384611 NM BS 532 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION .75 INCH BY 5 INCH AT STATIN 532, RLB 6.5 STRINGER 28R KEEL BE AM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. INSTALLED REPAIR STRAP AND ANGLE PER EA 65811. (M) 2 L 7 2 4F RT A16WE 2000030200040 20000302 00040 WP 2000 3 2 2000ZZZM228 1 19991022 A 2612 893244 FIRE LOOP PWA DOUG DC8 DC861 3021952 WP NR 4 LOOSE A FXLA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 29UA 645748 46159 NR 4 ENGINE FIRE WARNINGS CAME ON AFTER REACHING 3,000 FT FOLLOWED EMERGENCY CHECKLIST IAW FINE AIR POLICY. TROUBLESHOO T SYSTEM AND FOUD LOWER ENGINE FIRE LOOP LOOSE. RE-SECURED LOOP IAW MM 26-10-1. (M) 2 L 7 4 4F 4A25 2000030200041 20000302 00041 WP 2000 3 2 2000ZZZM229 1 19990902 A 5720 5614372503 FITTING DOUG DC8 DC8F55 3021928 WP WS 98 CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING B-CHECK INSPECTION, FOUND 20 INCH CRACK AT LEFT INBOARD CANOE FITTING AT STATION 98. REPLACED FITTING AT LEFT CA NOE IAW MM 27-27-7. (M) 2 L 7 4 4F 4A25 2000030200044 20000302 00044 WP 2000 3 2 2000ZZZM231 1 19990831 A 5711 5597826504 SPAR DOUG DC8 DC8F54 3021926 WP WS 69.5 CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 426FB 45667 DURING D-CHECK INSPECTION, FOUND 4 INCH CRACK IN RIGHT LOWER SPAR CAP AT XCW 69.5. REPAIRED ACCOMPLISH IAW BOEING SERVI CE ENGINEERING FAX FAS-MIA-99-0010RR AND SRO8570012 PER FINE AIR EA G5710-02, 00. (M) 2 L 7 4 4F 4A25 2000030200045 20000302 00045 WP 2000 3 2 2000ZZZM232 1 19990902 A 5330 57503294 SKIN DOUG DC8 DC861 3021952 WP BS 822-834 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING; CORROSION DAMAGE FUSELAGE TOP AT STATION 822-834, BETWEEN LONGERON L1 AN D L2 RIGHT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5313-01;00, SEMAN EO NR 990094 AND BOEING MESSAGE M-7200 -99-07589. (M) 2 L 7 4 4F 4A25 2000030200046 20000302 00046 EU 2000 3 2 SIMA0045 1 19991229 A 3350 1317 BULB SAAB SF340 340B 7860101 EU ROW 8/9 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AE 340B245 DFW - FLT 3608 - EMERGENCY LIGHT ABOVE 8C AND EMERGENCY LIGHT BELOW 9B INOPERATIVE. REMOVED AND REPLACED LIGHT BULB ABO VE 8C AND BELOW 9B. OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 2000030200048 20000302 00048 NE 2000 3 2 2000ZZZM233 2 19991103 A 7230 3044800 NR 1 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A JJBA E A ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 EA 01 862CA UE180 114172 DURING CLIMB-OUT AT 3000 FT, LEFT ENGINE EMITTED FLAMES FROM EXHAUST STACK, PRECEDED BY 'POP' NOISE. ENGINE WAS SECURED , EMERGENCY DECLARED AND THE AIRCRAFT RETURN TO FIELD WITHOUT INCIDENT. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 2000030200050 20000302 00050 NE 2000 3 2 GTIA9901221 2 19991210 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 FAILED A GTIA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 800NK 49144 PBI - FLT 648A - LOUD BANG CLIMBING OUT OF 1400 FEET. NR 2 ENGINE FAILURE. ACCOMPLISHED ENGINE FAILURE CHECKLIST AND S HUTDOWN LIST. RETURNED TO PBI. OVERWEIGHT LANDING (140,00 LBS). (M) 2 L 7 2 4F 4 F A6WE E9NE 2000030300001 20000303 00001 NM 2000 3 3 USAASB99307 1 19991230 A 3350 3114981 REFLECTOR BOEING 737 7373B7 1384580 NM CABIN DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 TPA - MAINTENANCE FOUND THE LEFT AFT EGRESS EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE REFLEC TOR ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2000030300002 20000303 00002 NM 2000 3 3 USAASB99306 1 19991228 A 3397 WIRE BOEING 737 737201 1384454 NM ROW 12 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 232US 22018 SYR - PILOT REPORTED THAT SEVERAL ROWS OF SEAT MOUNTED EMERGENCY LIGHTS, IN THE FORWARD CABIN, ILLUMINATED WITH SWITCH I N THE ARMED POSITION AND NORMAL POWER ON AIRCRAFT. MAINTENANCE REPAIRED WIRE AT EMERGENCY LIGHT CONNECTOR LOCATED AT SE AT ROW 12ABC. OPERATIONAL CHECK GOOD. MAINTENANCE THEN FOUND THE SINGLE AISLE LIGHT AT SEAT ROW 2ABC INOPERATIVE. REP AIRED CONNECTOR AT SEAT 2A. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2000030300004 20000303 00004 2000 3 3 USAAD99186 4 19991224 A 2565 7A127516 ESCAPE SLIDE DOUG DC9 DC981 3022081 WP SERVICE DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 30020 48036 PIT - DURING ANNUAL OPERATIONAL CHECK OF THE AFT SERVICE DOOR ESCAPE SLIDE, THE ESCAPE SLIDE DID NOT INITIALLY INFLATE A S THE ESCAPE SLIDE HUNG ON GIRT BAR SEVERAL MINUTES UNTIL BEING JIGGLED, THEN INFLATED. ALSO, THE ESCAPE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT SERVICE DOOR ESCAPE SLIDE. (M) 2 L 7 2 4F A6WE 2000030300006 20000303 00006 NE 2000 3 3 2000ZZZM250 2 19991019 A 7261 LK47660 OIL PUMP LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENGINE FAILED A WRNA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 05 311EA 3937 193A1012 10513 NR 2 ENGINE RAPID LOSS OF OIL QTY ENGIEN RAN APPROXIMATELY 2 MINUTES PRIOR TO SHUTDOWN WINDMILLED WITH NO OIL QTY 23 MIN UTES OIL PRESSURE NR 2 LIGHT ON. RETURNED TO BQN, LANDING NORMAL. REMOVED AND REPLACED PRIMARY OIL PUMP ASSEMBLY IAW M M 72-63-03. RUN AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A23WE E12EU 2000030300008 20000303 00008 NM 2000 3 3 USAA991341 1 19991206 A 5314 KEEL BEAM BOEING 737 737201 1384454 NM BS 727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 47148 22752 TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND MINOR CORROSION 4 INCH BY 6 INCH BOTTOM KEEL BEAM STAT ION 727 STRINGER 26L. CORROSION LEVEL 1. INSTALLED DOUBLER PER SRM 53-30-3 FIG 28. (M) 2 L 7 2 4F A16WE 2000030300011 20000303 00011 NE 2000 3 3 MALA976681 2 19991228 A 7260 CHIP DETECTOR SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE CONTAMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 112XJ 340A112 MSP - FLT 3324 - LEFT CHIP DETECTOR LIGHT CAME ON DURING CLIMB-OUT. RETURNED TO MSP. MAINTENANCE PERFORMED CHIP LIGHT TASK CARD 7910-303 AND SCAVENGE SCREEN TASK CARD 791107. FOUND SMALL SPIRAL MACHINE TYPE DEBRIS PIECE IN CHIP DETECTOR, CLEANED DETECTOR, CHECKED SCAVENGE SCREENS. NO FURTHER DEBRIS NOTED, RAN ENGINE, NO LIGHT, GOOD FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 2000030400002 20000304 00002 NE 2000 3 4 TSAA9972515 2 19991228 A 7200 ENGINE BOEING 737 7372T4 1384492 NM PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 808AL 23445 FLT 504 - CXI-HNL - DURING THRUST REDUCTION AT TOP OF CLIMB, LOUD COMPRESSOR STALL NR 1 ENGINE, 2 MORE AT CRUISE POWER. RETURNED TO XMAS ISLAND. REMOVED FOD ON NR 1 INTAKE (ENGINE). PERFORMED/INSPECTED NR 1 ENGINE, FRONT AND BACK. GROUN D RUN ENGINE AT MAX POWER SETTING AND PART POWER. NO COMPRESSOR STALL NOTED AT THE TIME. ENGINE IS WITHIN LIMIT AT DIF FERENT POWER SETTINGS, FINAL INSPECTION ON NR 1 ENGINE. OK FOR RELEASE BACK TO SERVICE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 2000030400003 20000304 00003 EU 2000 3 4 USAASB99275 2 19991120 A 7260 3353107060 GARLOCK SEAL BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 559AU 23513 DEN - FLT 624 - EN ROUTE FROM LAS TO PIT, AT APPROXIMATELY FL330, THE RIGHT ENGINE OIL QTY DROPPED TO .25 GALLON. OIL P RESSURE REMAINED NORMAL. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO ENGINE SHUTDOWN OCCURRED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE STARTER GARLOCK SEAL AND STARTER FLANGE SEA L. GROUND RAN ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 2000030400004 20000304 00004 EU 2000 3 4 SIMA0042 1 19991231 A 3350 LIGHT SAAB SF340 340B 7860101 EU ROW 4/5 LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 238AE 340B238 DFW - FLT 3924 - EMERGENCY FLOOR LIGHT INOPERATIVE AT ROWS 4 AND 5. FOUND LOOSE LIGHT SOCKET ON FLOOR LIGHT, TIGHTEN SA ME. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2000030400007 20000304 00007 NE 2000 3 4 2000ZZZM234 2 19991206 A 7314 378200 PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A MYWA J DUMP FUEL X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 19 806MA 22437 700575 UPON DEPARTURE FROM MCO, NR 1 ENGINE EPR DROPPED TO 1.4 AND N1 TO 80 PERCENT WITH A THROTTLE EVEN WITH NR 2 AND NR 3 AS WE CONTINUED CLIMBING THE ENGINE CONTINUED DECREASING.. BROUGHT ENGINE THROTTLE TO IDLE AND LOST CONTROL OF THE ENGINE WITH THE THROTTLE OIL TEMP STARTED RISING. ENGINE FLAMED OUT. DUMPED FUEL. COMPLIED WITH ALL APPR EMERGENCY PROCEDURE S AND RETURNED TO MCO. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL, P/N 743602-5 S/N 82934, AND ENGINE DRIVEN FUEL PU MP PER MM 73-21-1 AND 73-11-1. INSPECTED ENGINE FOR EXTERNAL DAMAGE, NONE NOTED. ACCOMPLISHED TRIM AND LEAK CHECK, OPS CHECK OK PER MM 71-00. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000030400008 20000304 00008 WP 2000 3 4 2000ZZZM235 1 19991018 A 5280 DRAIN DOUG DC8 DC8F55 3021928 WP MLG DOOR CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 45764 FOUND DURING C-CHECK, LEFT MAIN GEAR WELL FORWARD DRAIN SPOUT CRACKED. NDT TO DETERMINE END OF CRACK, STOP DRILLED AND WELDED PER MIL-STD-2219. NDT NO FLAWS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 10/01/99. (M) 2 L 7 4 4F 4A25 2000030400009 20000304 00009 WP 2000 3 4 2000ZZZM236 1 19990808 A 2910 7614031504 PIPE DOUG DC8 DC8F55 3021928 WP HYD SYSTEM LEAKING A FXLA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS TO TAKEOFF 1 SO 19 55FB 45678 ON TAKEOFF, AT TNT EXPERIENCE HYDRAULIC QUANTITY LOSS DOWN TO STAND PIPE EXECUTED ABNORMAL PROCEDURES, LANDED AT MIA WIT HOUT INCIDENT. INSPECTION, REVEALED HYDRAULIC PIPE LEAKING AT LEFT MAIN GEAR DOOR MECHANISM, REPLACED PIPE AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 2000030400010 20000304 00010 EU 2000 3 4 SIMA3644 1 19991229 A 3350 60207 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AE 340B374 DFW - FLT 3668 - EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2000030400013 20000304 00013 NM 2000 3 4 USAA990585 1 19990621 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK ON FRAME AT STATION 727D AT LBL 2 INCH AT VERTICAL ANGLES FOR ANTENNA MOUNT. CUTOUT CRACK AND INSTALLED FILLER AND DOUBLER PER EA 64800. (M) 2 L 7 2 4F RT A16WE 2000030400014 20000304 00014 NM 2000 3 4 USAA991057 1 19991013 A 5314 65621257 KEEL BEAM BOEING 737 737301 1384611 NM BS 500C CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CORRODED AREA KEEL BEAM AT BS 500C PLUS 9.5 INCH LBL 5. CORROS ION LEVEL 2. INSTALLED REPAIR DOUBLER PER EA 65730. (M) 2 L 7 2 4F RT A16WE 2000030400015 20000304 00015 NM 2000 3 4 USAA991103 1 19991016 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 3 INCH BY 5 FT AT FORWARD FRAME OF AFT CARGO DOOR OUTBOARD OF SILL FRAME. CORROSION LEVEL 1, CORROSION TASK NR C53-202-01. REPAIRED PER BOEING 737-300 SRM 53-60-15. (M) 2 L 7 2 4F RT A16WE 2000030400016 20000304 00016 NM 2000 3 4 USAA991099 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CEHCK VISUAL INSPECTION, FOUND 4 CORRODED AREAS .75 INCH BY .5 INCH EACH AT BS 312, WL 208.1, LBL 14, L BL 20, LBL 26 AND LBL 33 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP, REPAIR ANGL ES AND STRAPS PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030400017 20000304 00017 NM 2000 3 4 USAA991098 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 5 CORRODED AREAS .75 INCH BY .5 INCH EACH AT BS 312, WL 208.1, LBL 11 TO RBL 8 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPAIRED T-CAP AND SPLICES PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030400018 20000304 00018 NM 2000 3 4 USAA991097 1 19991016 A 5320 CREASEBEAM BOEING 737 7373B7 1384580 NM BS 290-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS AT BS 290 TO BS 344, RBL 57, WL 208.1 CREASEBEAM INNER CHORD ANGLE. CORROSIN LEVEL 2, CORROSION TASK NR C53-107-02. REPAIRED Z-ANGLE PER SRM 51-30-01. (M) 2 L 7 2 4F RT A16WE 2000030400019 20000304 00019 NM 2000 3 4 USAA991096 1 19991014 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 40116 23560 CLT - DURING A DROP IN VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT FLOORBEAM STATIN 967, LBL 5, L BL 17 AND RBL 18. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. FABRICATED NEW T-CAP AND ANGLES PER SRM 53-00-51 F IG 202. (M) 2 L 7 2 4F RT A16WE 2000030400020 20000304 00020 NM 2000 3 4 USAA991095 1 19991014 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 573US 40116 23560 CLT - DURING A DROP-IN VISUAL INSPECTINO, FOUND A 1 INCH AREA OF CORROSION AT NUTPLATE HOLES ON UPPER CHORD FLOORBEAM T- CAP STATION 986.5 BETWEEN LBL 45 AND RBL 45. CORROSION LEVEL 1. INSTALLED NEW SECTION OF T-CAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2000030400021 20000304 00021 NM 2000 3 4 USAA991061 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORROSION AREAS AT BS 344, WL 208.1, RBL 8 FLOO RBEAM. CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-15-01A. (M) 2 L 7 2 4F RT A16WE 2000030400022 20000304 00022 NM 2000 3 4 USAA991060 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL .5 INCH BY .5 INCH CORROSION AREAS AT SCREW HOLES FLOORBEAM STAT ION 344, RBL 8 - RBL 56 UPPER CHORD. CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-15-01A. (M) 2 L 7 2 4F RT A16WE 2000030400023 20000304 00023 NM 2000 3 4 USAA991040 1 19991016 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND NUMEROUS SPOTS OF CORROSION .5 INCH BY .5 INCH AT STATION 312, LBL 33 TO RBL 8 FLOORBEAM. CORROSION LEVEL 1. REPLACED T-CAP OF FLOORBEAM PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030400024 20000304 00024 NM 2000 3 4 USAA991039 1 19991016 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM BS 328-340 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 12 INCH BY .5 INCH AT BS 328 TO 340, WL 208.1, RBL 45 SEAT TRA CK. CORROSION LEVEL 1, CORROSION TASK NR C53-107-02. REPLACED SEAT TRACK PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 2000030400025 20000304 00025 NM 2000 3 4 USAA991030 1 19991016 A 5320 SILL BOEING 737 7373B7 1384580 NM CARGO BAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 38811 23383 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION WIDE SPREAD AFT CARGO DOOR SILL WEB. CORROSION LEVEL 2. CORR OSION TASK NR C55-202-01. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000030400026 20000304 00026 NM 2000 3 4 USAA991130 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 867 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AT STATION 867, RBL 13.80 FRAME. CORRO SION LEVEL 1. CORROSION TASK NR C53-208-01. REMOVED CORROSION PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2000030400027 20000304 00027 NM 2000 3 4 USAA991129 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 2 INCH AT STATION 847 BETWEEN STRINGER 24R AND 25R FRAME. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. INSTALLED DOUBLER AND FILLER PER SRM 53-00-07 FIG 201 AN D EA 65717. (M) 2 L 7 2 4F RT A16WE 2000030400028 20000304 00028 NM 2000 3 4 USAA991128 1 19991018 A 5320 PAN BOEING 737 737301 1384611 NM BS 807/847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AND A 2 INCH BY 2 INCH AT FORWARD AND A FT ENDS STATION 807 AND 847, RBBL 20 AFT CARGO DOOR THRESHOLD PAN. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. R EMOVED AND REPLACED WEB PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000030400029 20000304 00029 NM 2000 3 4 USAA991127 1 19991019 A 5315 DEC51057901 FLOORBEAM BOEING 737 7373B7 1384580 NM CARGO BAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 37350 23705 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND TWO CORRODED AREAS AFT CARGO COMP FIRST FLOORBEAM INSIDE DOOR. CORROSI ON LEVEL 1. REPLACED WITH IDENTICAL PART. (M) 2 L 7 2 4F RT A16WE 2000030400030 20000304 00030 NM 2000 3 4 USAA991080 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 1016, RBL 6, RBL 27, RBL 29 LWR SURFACE OF T-CAP BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. REMOVED AND REPLACED BEAM PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 2000030400031 20000304 00031 NM 2000 3 4 USAA991079 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 1006, LBL 38 T-CAP BEAM. CORROSION LEV EL 2. CORROSION TASK NR C53-202-01. REMOVED AND REPLACED BEAM PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 2000030400032 20000304 00032 NM 2000 3 4 USAA991050 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 294, LBL 12 BEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. INSTALLED NEW SECTION OF T-CAP WITH REPAIR ANGLES PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030400033 20000304 00033 NM 2000 3 4 USAA991049 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 294, RBL 12 BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED NEW SECTION OF T-CAP WITH REPAIR SPLICES PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030400034 20000304 00034 NM 2000 3 4 USAA991033 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 108 INCH SPAN OF CORROSION ALL NUTPLATE HOLES STATION 967 FLOORBEAM CA P LBL 54 TO RBL 54. CORROSION LEVEL 2. REPLACED DAMAGED CAP SECTION PER TR 53-10-05 AND SRM 51-30-01. (M) 2 L 7 2 4F RT A16WE 2000030400035 20000304 00035 NM 2000 3 4 USAA991014 1 19991018 A 5320 65C80735116 CREASE BEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION LEFT SERVICE DOOR Z-ANGLE INNER CHORD OF CREASE BEAM . CORROSION LEVEL 2, CORROSION TASK NR C53-202-01. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000030400036 20000304 00036 NM 2000 3 4 USAA991005 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 28 INCH AREA OF CORROSION AT BS 986 FLOORBEAM UPPER SURFACE RBL 13 - L BL 15. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. SPLICED IN NEW T-CAP SECTION PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 2000030400037 20000304 00037 NM 2000 3 4 USAA990995 1 19991018 A 5510 LUG BOEING 737 737301 1384611 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION LEFT LOWER FRONT HORIZ STAB TO LTR SECTION ATTACH LUG. CORROS ION LEVEL 1. REPAIRED SPOTFACE AND SHOTPEEN SURFACES PER EA 65596. (M) 2 L 7 2 4F RT A16WE 2000030400038 20000304 00038 NM 2000 3 4 USAA990994 1 19991018 A 5320 CREASE BEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AT RIGHT SERV DOOR Z-ANGLE INNER CHORD OF CREASE BEAM. CORROS ION LEVEL 2. REPLACED DOOR SILL PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000030400039 20000304 00039 NM 2000 3 4 USAA990978 1 19991018 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL AREAS OF CORROSION 1 INCH BY 1 INCH AT BS 328, RBL 25-35. CORRO SION LEVEL 2, CORROSON TASK NR C53-107-02. INSTALLED NEW SECTION OF T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000030400040 20000304 00040 NM 2000 3 4 USAA990952 1 19991018 A 5311 FRAME BOEING 737 737301 1384611 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 38332 23237 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON FRAME AT BS 1006 BETWEEN STRINGER 18L AND 19L. CORROSION L EVEL 2, CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 2000030400041 20000304 00041 NE 2000 3 4 USAASB99293 2 19991214 A 7200 ENGINE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE NR 1 VIBRATION A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 355US 23558 CLT - FLT 8052 - ON CLIMB-OUT FROM CLT, THE NR1 ENGINE VIBRATION MONITOR INDICATED 2 UNITS ACCELERATING THROUGH 210 KNOT S. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCYWAS DECLARED. MAINTENACNE ACCOMP LISHED TROUBLESHOOTING PROCEDURE PER MM 71-00-00 PAGE 24Y AND PERFORMED JOB CARD J377-30-1 AVM SIGNAL CONDITIONER CHECK . ALL P ARAMETERS ARE WITHIN THE NO ACTION REQUIRED RANGE. AIRCRAFT OK FOR SERVICE. CL T - FLT 1531, LATER THAT DAY, FLT RETURNED TO FIELD A SECOND TIME AT CLT FOR SAM E ENGINE VIBRATION. AIRCRAFT WAS AT FL260 WHEN THE CAPTAIN DECIDED T O RETURN TOFIELD. FLIGHT LANDED WITHOUT INCIDENT. NO EMEREGNCY WAS DECLARED. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2000030400042 20000304 00042 NE 2000 3 4 USAASB99164 2 19990706 A 7200 ENGINE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE LT/RT FATIGUED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 339US 23236 BOS - FLT 221 - JUST AFTER TAKEOFF, CREW ENCOUNTERED A WINDSHEAR ON DEPARTURE AND APPLIED FIREWALL POWER FOR A PERIOD AP PROXIMATELY 10 SECONDS. CAPTAIN FELT HE OVERBOOSTED THE ENGINES AND ELECTED TO RETURN TO FIELD AT BOS. FLIGHT LANDED W ITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE INTAKE AND EXHAUST OF BOTH ENGINES PER MM 72-00-00. ENGINES DID NOT EXCEED N1 RPM. AIRCRAFT OK FOR SERVICE (M) 2 L 7 2 4F 4 F RT A16WE E2GL 2000030400043 20000304 00043 NM 2000 3 4 USAA990617 1 19990621 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND .75 INCH CRACK ON SKIN AT PILOTS NR 1 WINDOW CUTOUT UPPER OUTBOARD CORNER. FABRICATED DOU BLER PER EA 64783A. (M) 2 L 7 2 4F RT A16WE 2000030400044 20000304 00044 NM 2000 3 4 USAA990563 1 19990610 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 708.5-709.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN LONGITUDINAL FLOORBEAM AT BS 708.5 AND BS 709.5. INSTALLED DOUBLER AND FI LLER PER SRM 511-70-13. (M) 2 L 7 2 4F RT A16WE 2000030400045 20000304 00045 NM 2000 3 4 USAA990606 1 19990621 A 5230 6547952524M SKIN BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A SMALL SKIN CRACK AT CARGO DOOR HANDLE CUTOUT AFT CARGO DOOR, AFT RADIU S OF HANDLE ACCESS CUTOUT EXTERIOR SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 52-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 2000030400046 20000304 00046 NM 2000 3 4 USAA990586 1 19990621 A 5311 FRAME BOEING 737 737301 1384611 NM BS 727D CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT STATION 727D AT LBL 02 AND RBL 02 FRAME. INSTALLED DOU BLER AND FILLERS PER SRM 53-60-07 AND EA 64800. (M) 2 L 7 2 4F RT A16WE 2000030400047 20000304 00047 NM 2000 3 4 2000ZZZM237 1 19991226 A 2731 10600171 CONTROL CABLE BOEING 727 727221 1384071 NM ELEVATOR SHEARED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 363PA 22535 SFB - AFTER ARRIVAL OF FLT, NR 1 TO SFB CREW NOTICED TRIM TAB INDICATOR STUCK AT 7.5 UNITS NOSE UP BOTH SIDES, CAPTAINS AND FIRST OFFICERS. MAINTENANCE REMOVED AND REPLACED CABLE WITH NEW. ALL WORK AND ADJUSTMENTS DONE IAW BOEING MM 27-40 -0. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 3 4F A3WE 2000030400048 20000304 00048 WP 2000 3 4 2000ZZZM238 1 19990902 A 5315 7075T6 FLOORBEAM DOUG DC8 DC861 3021952 WP BS 1640 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, MAIN CARGO COMPARTMENT RIGHT FLOORBEAM WEB CORRODED AT RBL 35 TO RBL 50, STATION 1640. REPAIRED CORROSION DAMAGE IAW FINE AIR EA NR G5310-04:00, SEMAN EO 9908201. (M) 2 L 7 4 4F 4A25 2000030400049 20000304 00049 WP 2000 3 4 2000ZZZM239 1 19990902 A 5320 36469562 FITTING DOUG DC8 DC861 3021952 WP BS 940 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, FITTING ON RIGHT LONGERON 24 CORROSION DAMAGE AT STATION 940 IN RIGHT WH EEL WELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0. (M) 2 L 7 4 4F 4A25 2000030400050 20000304 00050 WP 2000 3 4 2000ZZZM240 1 19990902 A 5320 364100502 FITTING DOUG DC8 DC861 3021952 WP BS 879.375 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, FITTING ON RIGHT LONGERON CORROSION DAMAGE AT STATION 879-375 IN RIGHT W HEEL WELL. REPAIRED CORROSION DAMAGE IAW SRM 53-2-0. (M) 2 L 7 4 4F 4A25 2000030400051 20000304 00051 WP 2000 3 4 2000ZZZM241 1 19990902 A 5730 561135025 PANEL DOUG DC8 DC861 3021952 WP WS 408 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION ON LEFT WING AT INNER AFT TOP PANEL PLATING AT STATION XW 408 STRINGER 5. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EA NR G5730-06:00, SEMAN EO NR 990104 AND BOEING MESSAGE M-7200 -99-07795. (M) 2 L 7 4 4F 4A25 2000030400052 20000304 00052 WP 2000 3 4 2000ZZZM242 1 19990902 A 5711 55978412 SPAR DOUG DC8 DC861 3021952 WP WS 763 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 29UA 46159 DURNG C-CHECK INSPECTION, FOUND THE FOLLOWING, RIGHT WING HAS CORROSION DAMAGE ON REAR SPAR AT STATINO XRS 763. REPAIRE D CORROSION DAMAGE AT RIGHT WING XRS 763 IAW FINE AIRLINES EA NR G5711-01:00. SEMAN EO NR 990083 AND BOEING MESSAGE SEU -LIM-99-00023H. (M) 2 L 7 4 4F 4A25 2000030400053 20000304 00053 WP 2000 3 4 2000ZZZM243 1 19990620 A 5315 FLOORBEAM DOUG DC8 DC8F55 3021928 WP BS 1460 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE FLOORBEAM AT STATION FS 1460 RBL 35 TO 41. REPAIRED CO RROSION DAMAGE IAW FINE AIR EO NR 9906211. (M) 2 L 7 4 4F 4A25 2000030400054 20000304 00054 WP 2000 3 4 2000ZZZM244 1 19990618 A 5315 FLOORBEAM DOUG DC8 DC8F55 3021928 WP BS 1380 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE FLOORBEAM AT STATION FS 1380, LBL 20. REPAIRED CORROSI ON DAMAGE IAW FINE AIR EO NR 9906181. (M) 2 L 7 4 4F 4A25 2000030400055 20000304 00055 WP 2000 3 4 2000ZZZM245 1 19990831 A 5542 SKIN DOUG DC8 DC8F55 3021928 WP RUDDER CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE AT LEFT AND RIGHT RUDDER SKIN. REPAIRED CORROSION DAMA GE IAW FINE AIR EO NR 9808131, SRM 51-1-21. (M) 2 L 7 4 4F 4A25 2000030400057 20000304 00057 WP 2000 3 4 2000ZZZM247 1 19990618 A 5315 FLOORBEAM DOUG DC8 DC8F55 3021928 WP BS 1480 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE FLOORBEAM AT STATION FS 1480 RBL 1. REPAIRED CORROSION DAMAGE IAW FINE AIR EO NR 9906182. (M) 2 L 7 4 4F 4A25 2000030400058 20000304 00058 WP 2000 3 4 2000ZZZM248 1 19990421 A 5754 5597825 SKIN DOUG DC8 DC8F54 3021926 WP LE FLAP CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 426FB 45667 DURING D-CHECK INSPECTION, FOUND LEADING UPPER CAP CRACKED. REPAIRED CRACK ON WING RIGHT IAW FINE AIRLINES EA NR G5711- 02:00. (M) 2 L 7 4 4F 4A25 2000030400059 20000304 00059 WP 2000 3 4 2000ZZZM249 1 19991024 A 3310 BA170 BALLAST DOUG DC8 DC851 3021920 WP COCKPIT FAILED A FXLA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 508DC 45935 DURING TAXI NOTICED THAT SMOKE STARTED COMING OUT FROM THE FLIGHT ENGINEER QUADRANT. COMPLETE PHASE ONE SMOKE SOURCE ID ENTIFICATION AND REMOVED AND REPLACED BALLAST TRANSFORMER. OPERATION CHECK NORMAL. (M) 2 L 7 4 4F 4A25 2000030400060 20000304 00060 EU 2000 3 4 SIMA0046 1 19991229 A 3350 1317 BULB SAAB SF340 340B 7860101 EU ROW 4 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 222NE 340B222 DFW - FLT 3516 - EMERGENCY LIGHT OVER 4A INOPERATIVE. REMOVED AND REPLACED LIGHT BULB OVER 4A. OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 2000030400061 20000304 00061 EU 2000 3 4 USAAF00003 1 19990107 A 3241 ANTI-SKID SYSTEM FOKKER F28 F28MK0100 4990807 EU MLG MALFUNCTIONED A USAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 19 897US 11392 CLT-BHM - FLT 1252 - ON TAXI OUT FOR TAKEOFF, WHEN BRAKES WERE APPLIED (20 KNOTS), ANTI-SKID WOULD RELEASED BRAKES, MAKI NG IT HARD TO SLOW DOWN. MAINTENANCE ACTION PENDING. AIRCRAFT WAS RELEASED ON MEL. (M) 2 L 7 2 4F RT 2000030400063 20000304 00063 NM 2000 3 4 USAASB00002 1 19990102 A 3350 500000043 CHARGER BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 SYR - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN IN THE FORWARD CABIN CEILING INOPERTIVE. MAINTENANCE REMOVED AND REPLAC ED THE CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 2000030400085 20000304 00085 WP 2000 3 4 99T64R444EWA 1 19991104 A 5312 BULKHEAD DOUG DC8 DC871 302199A WP BS 440 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. 'A' PIT AFT BULKHEAD BOTTOM NEEDS TO BE TRIMMED STA 440. (EO). FABRICATED NEW DOOR USING DRAWIN G NR 99-174-1. TREATED AND PRIMED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-20-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400086 20000304 00086 WP 2000 3 4 99T64R445EWA 1 19991007 A 5320 BUSHING MOUNT DOUG DC8 DC871 302199A WP BS 1600 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. AFT PASSENGER DOOR (L2) HAS CRACK AT UPPER HINGE BUSHING AREA STA 1600. REMOVED CRACK SECTION BY CUT OUT. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED, AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-01-99 . REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400087 20000304 00087 WP 2000 3 4 99T64R451EWA 1 19991026 A 5753 57546643 ACTUATOR CRANK DOUG DC8 DC871 302199A WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. LT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRANK ON FLAP ACTUATOR ASSY IAW DC-8 OHM 27-28-7. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400088 20000304 00088 WP 2000 3 4 99T64R532EWA 1 19991027 A 5753 VANE DOUG DC8 DC871 302199A WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 5 VANE INBOARD UPPER END HAS ELONGATED HOLE. DRILLED AND REAMED HOLE TO . 75 INCH DIAMETER. TREATED AND PRIMED. FABRICATED PLUG AND INSTALLED, DRILLED PLUG TO CORRECT HOLE SIZE PER EO 99-174 W ITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400089 20000304 00089 WP 2000 3 4 99T64R533EWA 1 19991113 A 5720 FASTENER DOUG DC8 DC871 302199A WP RT WING MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RT WING L/E ABOVE NR PYLON. ONE LOOSE FASTENER WITH SKIN WASHER, ONE FASTENER MISSING. (EO). T IGHTENED THE LOOSE FASTENER. INSTALLED NAS1670L4 JO-BOLT IN OPEN HOLE. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99 -174 WITH APPROVED 8110-3 DATED 11-12-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400090 20000304 00090 WP 2000 3 4 99T64R534EWA 1 19991109 A 3230 PIN BOSS DOUG DC8 DC871 302199A WP RT MLG CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RT MAIN LANDING GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-15-99. INSTALLED BUSHING AND PIN IAW DC-8 SB 32-102. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400091 20000304 00091 WP 2000 3 4 99T64R535EWA 1 19991111 A 3211 FASTENER DOUG DC8 DC871 302199A WP RT MLG MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RT MAIN LANDING GEAR FITTING MISSING FASTENER AFT SIDE. (EO). LEFT THE SHEARED SHANK IN THE HOL E, FILLED HOLE WITH PR1422B 1/2 SEAL. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8110-3 DATED 11 -11-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400092 20000304 00092 WP 2000 3 4 99T64R536EWA 1 19991022 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 7.500-190.250 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 RIGHT INBOARD LEADING EDGE TOP MOUNT HOLES DAMAGED OR ELONGATED, 7 EACH. DRILLED, PRIMED AND INSTALLED IAW EO NR 99-174 WITH APPROVED 8110-3 DATED 9-14-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400093 20000304 00093 WP 2000 3 4 99T64R537EWA 1 19991103 A 5320 PANEL DOUG DC8 DC871 302199A WP BS 1600 BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. STA 1660 SIDE RAIL PANEL BROKEN STA 1650 - STA 1700. (EO). FABRICATED NEW SIDE RAIL PANEL PER E O 99-174 WITH APPROVED 8110-3 DATED 10-20-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400094 20000304 00094 WP 2000 3 4 99T64R538EWA 1 19991018 A 5320 KICK PLATE DOUG DC8 DC871 302199A WP CARGO BAY CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. AFT LOWER CARGO RACKS AND DENTS. (EO). STRAIGHTEN DENTS. NDT VERIFIED NO CRACKS, STOP DRILLED CRACKS AND WELDED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-11-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400095 20000304 00095 WP 2000 3 4 99T64R539EWA 1 19991110 A 5250 DOOR DOUG DC8 DC871 302199A WP CARGO BAY MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 DURING D-CHECK. FABRICATED AND INSTALLED DIVIDER WALL BETWEEN C AND D PITS. (EO). FABRICATED A NEW DOOR USING DRAWING 99-174-2. TREATED AND PRIMED PER EO 999-174 WITH APPROVED 8110-3 DATED 11-8-99. REF: EMERY WORLDWIDE A/L. RRXA. ( X) 2 L 7 4 4F 4A25 2000030400096 20000304 00096 WP 2000 3 4 99T64R545EWA 1 19991119 A 3230 PIN BOSS DOUG DC8 DC871 302199A WP LT MLG CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 DURING D-CHECK. LT MAIN GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-15-99. INSTALLED BUSHING AND PIN IAW DC-8 SB 32-102 . REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400097 20000304 00097 WP 2000 3 4 2000T74R547EW 1 19991112 A 5400 METAL STRIP DOUG DC8 DC871 302199A WP LT NACELLE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 DURING C-CHECK. NR 2 ENGINE LT SIDE METAL STRIP ABOVE REVERSER COWL HAS .75 INCH CRACK. NDT TO DETERMINE LENGTH OF CRA CK. STOP DRILLED AND NDT TO CONFIRM CRACK. STOP DRILLED - BROKEN SHARP EDGES. TREATED, PRIMED AND FILLED STOP DRILL H OLES WITH SEALER PER EO 99-174 WITH APROVED 8110-3 DATED 11-12-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400098 20000304 00098 WP 2000 3 4 99T64R426EWA 1 19991001 A 5347 SEAT TRACKS DOUG DC8 DC871 302199A WP CABIN WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 F/E SEAT AFT TRACK LOCK HOLES WORN TO LIMITS. REMOVED AND REPLACED F/E'S SEAT TRACK IAW DC-8 SRM 51-1-21. REF: EMER Y WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400099 20000304 00099 WP 2000 3 4 99664R428EWA 1 19991007 A 5330 SKIN DOUG DC8 DC871 302199A WP BS 250 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 EXTERIOR RT LIGHTING STRIKE STA 250 RT BETWEEN L21R - L22R. (EO). BLENDED ROUGH AREAS SMOOTH, REAMED HOLES AND INSTALL ED MS20470AD8 RIVET. TREATED AND PRIMED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-16-99. REF: EMERY WORLDWIDE A/L . RRXA. (X) 2 L 7 4 4F 4A25 2000030400100 20000304 00100 WP 2000 3 4 99T64R429EWA 1 19990925 A 5754 SHIM DOUG DC8 DC871 302199A WP TE FLAP BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 NR 3 STUB WING L/E INBOARD LOWER SPAR CAP SHIM BROKEN OFF XILD .7095. (EO). SMOOTHED REMAINING EDGE OF SHIM. NDT TO A SSURE THAT NO CRACKS EXIST. (NONE FOUND). TREATED AND PRIMED, INSTALLED INBOARD PIECE AS A SHIM USE FACTORY FASTENERS PER EO 99-174 WITH APPROVED 8110-3, DATED 9-21-99. REF: EMERY WORLDWIDE A/L. RRXA. (X) 2 L 7 4 4F 4A25 2000030400101 20000304 00101 WP 2000 3 4 99T64R430EWA 1 19990918 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 93 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 LEFT WING STATION XW 693 BETWEEN STR 4 AND STR 2, SKIN BULGED. REMOVED CORROSION. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-14-99. REF: EMERY WORLD WIDE A/L: RRKA. 2 L 7 4 4F 4A25 2000030400102 20000304 00102 WP 2000 3 4 99T64R431EWA 1 19990912 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 793.0 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 LEFT WING UPPER L/E T/E FASTENER HAS CORROSION EMANATING FROM FASTENER HOLE STA 793.00. CUT OUT CORROSION AREA APPROXIM ATELY 16.5 TO 22.5 INCHES. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED PER EO NR 99-174, WITH APPROVED 8110-3 DA TED 9-16-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400103 20000304 00103 WP 2000 3 4 99T64R432EWA 1 19991018 A 5320 STIFFENER DOUG DC8 DC871 302199A WP RT MLG WW BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 RIGHT WHEELWELL FORWARD WEBBING STIFFENER BROKEN. (EO). WELDED NEW SECTION OF TUBING IAW MIL-STD-2219. NDT WELD NO FL AWS FOUND PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400104 20000304 00104 WP 2000 3 4 99T64R433EWA 1 19990923 A 5320 WEB DOUG DC8 DC871 302199A WP BS 960-980 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 CORROSION ON MAIN LANDING GEAR PRESSURE DECK FS 960 - FL 980.. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400105 20000304 00105 WP 2000 3 4 99T64R434EWA 1 19991018 A 5320 STIFFENER DOUG DC8 DC871 302199A WP LT MLG WW BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 45947 LEFT WHEELWELL FORWARD WEBBING FRAME BROKEN. (EO). WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS F OUND. ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-24-99. REF: EMERY WORLD WIDE A /L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400106 20000304 00106 WP 2000 3 4 99T64R440EWA 1 19991002 A 5712 RIB DOUG DC8 DC871 302199A WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 LEFT WING T/E STA 261 FLAP WELL RIB CRACKED BELOW NR 4 SPOILER. CUT OUT CRACK. TREATED AND PRIMED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400107 20000304 00107 WP 2000 3 4 99T64R452EWA 1 19991026 A 5753 57546643 ACTUATOR CRANK DOUG DC8 DC871 302199A WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RIGHT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRACK ON FL AP ACTUATOR ASSEMBLY IAW DC-8 OHM 27-28-7. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400108 20000304 00108 WP 2000 3 4 99T64R453EWA 1 19991008 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 520.168 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK, LT MID-WIND LEADING EDGE OUTBOARD END SLOT VANE STA 520.168, HOLES WORN AND ELONGATED. (EO). FAB RICATED REPAIR STRAP 12 INCHES BY 2.25 INCHES. TREATED AND PRIMED. INSTALLED CONICAL WASHERS AND INSTALLED REPAIR STRA P PER EO 99-174 WITH APPROVED 8110-3 DATED 10-4-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400109 20000304 00109 WP 2000 3 4 99T64R454EWA 1 19991012 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 416.500 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RT MID LEADING EDGE TWO DOUBLER LOWER EXTERIOR TO EVALUATE DAMAGE STA XFS 416.500 - XS 435.289. ( EO). REMOVED AND REPLACED THE OUTBOARD EXTERNAL SKIN WITH NEW SKIN SAME SIZE. SHAPE AND MATERIAL AS THE ORIGINAL PER E O 99-174 WITH APROVED 8110-3 DATED 10-05-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400110 20000304 00110 WP 2000 3 4 99T64R455EWA 1 19991004 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 300 LIGHTNING STRIKE B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. LIGHTNING STRIKE STA 300 RT BETWEEN L18R - L19R (EO). OPENED LIGHTNING STRIKE HOLE TO .375 INCH. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-4-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400111 20000304 00111 WP 2000 3 4 99T64R467WEA 1 19990923 A 5712 RIB DOUG DC8 DC871 302199A WP WS 250.089 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. NR 2 STUB WING LEADING EDGE, 7 INCH CRACK TOP RIB STA 250.089. STOP DRILLED CRACK IAW DC-8 SRM 5 7-2-0. FABRICATED TWO DOUBLERS IAW DC-8 SRM 57-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC -8 SRM 51-1-20D AND SRM 51-3-0. (X) 2 L 7 4 4F 4A25 2000030400112 20000304 00112 WP 2000 3 4 99T64R475EWA 1 19990928 A 5730 SKIN DOUG DC8 DC871 302199A WP WS 520/186 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK, MID-WING LEADING EDGE SLOT VANE HOLE OVERSIZED AND WORN AT STA XS 520.186. (EO). CLEANED EXISTNG COUNTERSINKS, ALODINED, TREATED AND PRIMED. FABRICATED CONICAL WASHERS AND FILLED THE COUNTERSINKS. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400113 20000304 00113 WP 2000 3 4 99T64R500EWA 1 19991006 A 5320 COVER DOUG DC8 DC871 302199A WP WS 1420 GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. 'D' PIT DOOR THRESHOLD PLATE GOUGED/SCRATCHED STA 1420. (EO). REMOVED THE EXISTING D-PIT THRESH OLD PLATE. FABRICATED NEW THRESHOLD, WELDED CURVED PORTIONS AND NDT WELDS. NO FLAWS FOUND AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-05-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400114 20000304 00114 WP 2000 3 4 99T64R503EWA 1 19991025 A 5753 SKIN DOUG DC8 DC871 302199A WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 6 VANE INBOARD END TOP SIDE HAS HOLE ELONGATED. DRILLED AND REAMED HOLE T O .375 INCH. FABRICATED PLUG AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/ L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400115 20000304 00115 WP 2000 3 4 99T64R504EWA 1 19991108 A 5230 DRAIN PLUG DOUG DC8 DC871 302199A WP CARGO DOOR MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. C-PIT DOOR MISSING DRAIN PLUG. FABRICATED FILLER. TREATED AND PRIMED. INSTALLED FILLERS AND D RAIN PLUG PER EO 99-174 WITH APPROVED 8110-3 DATED 11-02-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400116 20000304 00116 WP 2000 3 4 99T64R506EWA 1 19991005 A 5311 FRAME DOUG DC8 DC871 302199A WP BS -67 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUDN DURING D-CHECK. CORROSION AT STA -67 APPROXIMATELY 45 INCHES LEFT OF CENTER ON SUB-FLOOR FRAME IN COCKPIT. (EO). REMOVED CORROSION. TREATED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. FABRICATED REPAIR ANGLE AND INSTALLED PE R EO 99-174 WITH APPROVED 8110-3 DATED 10-01-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400117 20000304 00117 WP 2000 3 4 99T64R507EWA 1 19991012 A 5320 KICK PLATE DOUG DC8 DC871 302199A WP CARGO BAY GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. B-PIT DOOR KICK PLATE GOUGED/SCRATCHED. (EO). FABRICATED NEW KICK PLATE. WELDED ACCORDING TO M IL-STD-2219, NDT WELD TO ASSURE NO FLAWS IN WELD. NONE NOTED, AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9 -20-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400118 20000304 00118 WP 2000 3 4 99T64R508W 1 19991018 A 5320 KICK PLATE DOUG DC8 DC871 302199A WP CABIN DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. TYPE ONE EMERGENCY EXIT DOOR LEFT SIDE. KICK PLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO A SSURE CRACKS HAD BEEN STOPPED. WELDED KICK PLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH AP PROVED 8110-3 DATED 10-14-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400119 20000304 00119 WP 2000 3 4 99T64R509EWA 1 19991014 A 5320 KICK PLATE DOUG DC8 DC871 302199A WP CABIN DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. TYPE ONE EMERGENCY DOOR AFT RIGHT SIDE KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASS URE CRACKS HAD BEEN STOPPED. WELDED KICKPLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPRO VED 8110-3 DATED 10-15-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400120 20000304 00120 WP 2000 3 4 99T64R510EWA 1 19991014 A 5320 KICK PLATE DOUG DC8 DC871 302199A WP CABIN DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING C-CHECK. TYPE ONE EMERGENCY DOOR RIGHT FORWARD KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSUR E CRACKS HAVE BEEN STOPPED, WELDED KICKPLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPROVE D 8110-3 DATED 10-14-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400121 20000304 00121 WP 2000 3 4 99T64R511EWA 1 19990917 A 5311 FRAME DOUG DC8 DC871 302199A WP BS 1764 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. MAIN CABIN STA 1764 LT BETWEEN L10L - L11L LBL 45 INCH - 46.5 Z AXIS 61 INCHES TO 64 INCHES FRAME PLATE CORROSION. (EO). REMOVED CORROSION, SMOOTH FINISH 63VRHR ALODINE, PRIMED AND FINISHED TO FACTORY SPECS, IT IS A CCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8110-3 DATED 9-16-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400122 20000304 00122 WP 2000 3 4 99T64R512EWA 1 19991018 A 7110 COWL DOUG DC8 DC871 302199A WP NR 1 ENGINE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. HOLE ON INSIDE OF LT FORWARD OF LT FORWARD COWL NR 1 ENGINE. CUT OUT DAMAGED AREA, FILLED WITH L Y5052 02 RESIN AND HY5052 02 RESIN CATALYST AND MIRCO BALLONS. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPR OVED 8110-3 DATED 10-07-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400123 20000304 00123 WP 2000 3 4 99T64R513EWA 1 19991018 A 7830 THRUST REVERSER DOUG DC8 DC871 302199A WP NR 3 ENGINE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. RT FAN REV DAMAGED ON LOWER VERTICAL SURFACE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYST MIXED WITH MICRO BALLOONS. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 81 10-3 DATED 10-01-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400124 20000304 00124 WP 2000 3 4 99T64R514EWA 1 19991015 A 2620 3756845515 LINE DOUG DC8 DC871 302199A WP EXTINGUISHER CHAFED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. FIRE RETARDANT LINE CHAFED FORWARD OF TOMBSTONE NR 3 PYLON. BLENDED CHAFE SMOOTH FILLED CHAFE WI TH WELD, NDT WELD NO FLAWS FOUND PER EO 99-174 WITH APPROVED 8110-3 DATED 10-7-99. REF: EMERY WORLD WIDE A/L, RRXA. ( X) 2 L 7 4 4F 4A25 2000030400125 20000304 00125 WP 2000 3 4 99T64R515EWA 1 19991008 A 7830 THRUST REVERSER DOUG DC8 DC871 302199A WP NR 4 ENGINE LIGHTNING STRIKE B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. THREE LIGHTNING STRIKES, RIGHT FAN REV. TRAILING EDGE OUTER SECTION MIDDLE AND BOTTOM NR 4 ENGINE . (EO). BLENDED THE EDGE OF THE LIGHTNING STRIKES, SMOOTH, ALODINED AND FINISHED PER FACTORY SPECS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8110-3 DATED 10-6-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400126 20000304 00126 WP 2000 3 4 99T64R518EWA 1 19991027 A 5753 SKIN DOUG DC8 DC871 302199A WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 8079U 84047 45947 FOUND DURING D-CHECK. LEFT WING OUTBOARD FLAP VANE INBOARD END UPPER SURFACE HAS IMPROPER REPAIR OF ELONGATED HOLE. DR ILLED AND REAMED HOLE TO .375 INCH DIAMETER. FABRICATED PLUG AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-2 1-99. REF: EMERY WORLD WIDE A/L, RRXA. (X) 2 L 7 4 4F 4A25 2000030400145 20000304 00145 NE 2000 3 4 USAASB99267 2 19991107 A 7261 MS29513030 O-RING BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 EA 19 245US 22751 MCO - FLT 2763 - ON TAKEOFF ROLL, OIL QTY ON THE NR 2 ENGINE WENT FROM 3.6 GALLONS TO 1 GALLONS. THE TOWER ALSO REPORTE D SMOKEON TAKEOFF ROLL FROM THE SAME ENGINE. CAPTAIN ELECTED TO RETURN TO FIELD AT MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENA NCE FOUND THE NR 2 ENGINE MAIN OIL FILTER LEAKING. REPLACED OIL FILTER (P/N ACC 336F1665) AND O-RINGS (P/N RD3018). RAN ENGINE. NO LEAKS NOTED. (M) 2 L 7 2 4F 4 F A16WE E2EA 2000030400159 20000304 00159 EU 2000 3 4 USAAF99056 2 19991205 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING R B J PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 860US 11295 17229 MCO - FLT 7001 - ON CLIMB-OUT, EXPERIENCED ENGINE THRUST FLUCTUATION IN NR 1 ENGINE. ENGINE FAIL LIGHT CAME ON AND WENT OFF RIGHT AWAY. CAPTAIN THEN DECLARED AN EMERGENCY. ON SHORT FINAL, ENGINE FAILED AND WAS SHUT DOWN AFTER LANDING. S OME FUMES WERE EXPERIENCED IN THE CABIN, HOWEVER, PASSENGERS WERE DEPLANED WITHOUT INCIDENT. (M) 2 L 7 2 4F 4 F RT 2000030400160 20000304 00160 SO 2000 3 4 SIMA3643 1 19991218 A 2612 PU90431R1 FIRE DETECTOR EMB 145 EMB145 SO CARGO BAY INOPERATIVE A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 611AE 05769 145074 ORD - FLT 4266 - BAGGAGE SMOKE WARNING INDICATOR ILLUMINATED AFTER LANDING. VISUALLY CONFIRMED NO SMOKE. BAGGAGE EXTIN GUISHER BOTTLES WERE DISPENSED. NO FURTHER INCIDENTS. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH EXTINGUISHERS. PER FORMED OPS CHECK OF SYSTEM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2000030400161 20000304 00161 SO 2000 3 4 2000ZZZM251 1 19991218 A 2621 4600931 FIRE BOTTLE EMB 145 EMB145 SO CARGO BAY DISCHARGED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 611AE 16641F 145074 ORD - FLT 4266 - BAGGAGE SMOKE WARNING INDICATOR ILLUMINATED AFTER LANDING. VISUALLY CONFIRMED NO SMOKE. BAGGAGE EXTIN GUISHER BOTTLES WERE DISPENSED. NO FURTHER INCIDENTS. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH EXTINGUISHERS. PER FORMED OPS CHECK OF SYSTEM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2000030400162 20000304 00162 SO 2000 3 4 2000ZZZM252 1 19991218 A 2621 737000271 FIRE BOTTLE EMB 145 EMB145 SO CARGO BAY DISCHARGED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 611AE 3444301 145074 ORD - FLT 4266 - BAGGAGE SMOKE WARNING INDICATOR ILLUMINATED AFTER LANDING. VISUALLY CONFIRMED NO SMOKE. BAGGAGE EXTIN GUISHER BOTTLES WERE DISPENSED. NO FURTHER INCIDENTS. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH EXTINGUISHERS. PER FORMED OPS CHECK OF SYSTEM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2000030400163 20000304 00163 SO 2000 3 4 SIMA3648 1 19991204 A 2612 PU90431R1 FIRE DETECTOR EMB 145 EMB145LR SO CARGO BAY INOPERATIVE A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 601GH 05986 145046 DFW - FLT 3636 - BAGGAGE COMPARTMENT FIRE WARNING LIGHT ILLUMINATED. NO INDICATION OF SMOKE DISCHARGED BOTTLES. NO FUR THER INCIDENT. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH FIRE BOTTLES. PERFORMED OPS CHECK OF SYSTEM. OPS CHECK GO OD. (M) 2 L 7 2 4T RT T00011AT 2000030400164 20000304 00164 SO 2000 3 4 2000ZZZM253 1 19991204 A 2621 34600931 FIRE BOTTLE EMB 145 EMB145LR SO CARGO BAY DISCHARGED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 601GH 3210201 145046 DFW - FLT 3636 - BAGGAGE COMPARTMENT FIRE WARNING LIGHT ILLUMINATED. NO INDICATION OF SMOKE DISCHARGED BOTTLES. NO FUR THER INCIDENT. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH FIRE BOTTLES. PERFORMED OPS CHECK OF SYSTEM. OPS CHECK GO OD. (M) 2 L 7 2 4T RT T00011AT 2000030400165 20000304 00165 SO 2000 3 4 2000ZZZM254 1 19991204 A 2621 737000271 FIRE DETECTOR EMB 145 EMB145LR SO CARGO BAY DISCHARGED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 601GH 1579179 145046 DFW - FLT 3636 - BAGGAGE COMPARTMENT FIRE WARNING LIGHT ILLUMINATED. NO INDICATION OF SMOKE DISCHARGED BOTTLES. NO FUR THER INCIDENT. REMOVED AND REPLACED SMOKE DETECTOR AND BOTH FIRE BOTTLES. PERFORMED OPS CHECK OF SYSTEM. OPS CHECK GO OD. (M) 2 L 7 2 4T RT T00011AT 2000030400166 20000304 00166 EU 2000 3 4 SIMA0044 1 19991230 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 844 017 CMI - FLT 4364 - CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE BY ROWS 2, 3 AND 5. REMOVED AND REPLACED POWER SUPP LY AT 29WL AND 10WL.OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2000030400167 20000304 00167 EU 2000 3 4 2000ZZZM255 1 19991230 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 11834 017 CMI - FLT 4364 - CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE BY ROWS 2, 3 AND 5. REMOVED AND REPLACED POWER SUPP LY AT 29WL AND 10WL. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2000030400249 20000304 00249 WP 2000 3 4 TWAA0003023 1 19991209 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 598 - 617 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 110HM 49787 DURING CHECK-C MAINT, FOUND MEMBRANE CORRODED BETWEEN STA 598 AND 617 ON LT SIDE. REMOVED CORROSION PER SPM 6-80-01. T REATED AND PRIMED PER SRM 51-10-03 PAGE 15 AND 16. REPAIRED PER SRM 53-01 FIG 4. 2 L 7 2 4F RT A6WE 2000030700001 20000307 00001 CE 2000 3 7 RU3A99014 1 19991210 A 3234 1013841377 SWITCH BEECH 300 300BEECH 1152930 CE MLG STICKING A RU3A A UNSCHED LANDING O OTHER LD LANDING 1 SW 21 71 FF6 LANDING GEAR FAILED TO EXTEND WHEN 'GEAR DOWN' SELECTED.. RESULTED IN EMERGENCY EXTENSION OF LANDING GEAR. THE MICRO-S WITCH IN THE LANDING GEAR CONTROL SWITCH ASSEMBLY WAS FOUND TO BE STICKING. THE LANDING GEAR CONTROL SWITCH WAS REPLACE D AND SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4T A24CE 2000030700002 20000307 00002 EU 2000 3 7 REXA99036 1 19991203 A 3230 HP848430621 VALVE SAAB SF340 SF340A 7850100 EU MLG INOPERATIVE A REXA O OTHER J WARNING INDICATION LD LANDING 1 SO 25 402BH 340A058 DURING LANDING PHASE OF FLT, CREW SELECTED L/G GEAR DOWN AND L/G FAILED TO EXTEND. TRANSIT LIGHT WAS ILLUMINATED AND HY D PUMP CONTINUED TO RUN WITH NORMAL ACCUMULATOR PRESSURE AND HYD FLUID QTY. CREW ATTEMPTED TO HAND PUMP THE GEAR DOWN W ITH NEGATIVE RESULTS. EMERGENCY GEAR EXTENSION HANDLE WAS PULLED AND LANDING GEAR EXTENDED WITH GEAR INDICATING DOWN AN D LOCKED. AFTER A NORMAL LANDING, IT WAS DISCOVERED THAT THE NOSE WHEEL STEERING WAS INOPERATIVE. DIFFERENTIAL POWER W AS UTILIZED FOR TAXI TO THE GATE. LANDING CONTROL VALVE DETERMINED TO BE INOPERATIVE. REMOVED AND REPLACED LANDING GEA R CONTROL VALVE AND LEFT/RIGHT SEPARATION BOLTS. PERFORMED FUNCTIONAL/OPERATIONAL TEST OF LANDING GEAR SYSTEM WITH NO F 2 L 7 2 4T RT A52EU 2000030700003 20000307 00003 EU 2000 3 7 REXA99037 1 19991209 A 3230 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU MLG LEAKING A REXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 407BH 340A078 AFTER TAKEOFF PILOT REPORTED LOSS OF HYDRAULIC PRESSURE AND QUANTITY AFTER GEAR CAME UP. AN EMERGENCY EXTENSION OF THE LANDING GEAR WAS PERFORMED. MAIN LANDING GEAR HYDRAULIC SWIVEL LEAKING. REMOVED AND REPLACED HYDRAULIC SWIVEL. PERFOR MED OPERATIONAL AND FUNCTIONAL CHECK OF THE LANDING GEAR SYSTEM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000030700004 20000307 00004 EU 2000 3 7 UF6A991202 1 19991212 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU ROW 7/8 FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 855AW 13316 2029 SBN - EMERGENCY LIGHT STRIP INOPERATIVE AT ROW 7 AND 8. MAINTENANCE REMOVED AND REPLACED THE NR 7 POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 2000030700005 20000307 00005 EU 2000 3 7 UF6A991203 1 19991212 A 2150 LS6066 SENSOR BAG ATP ATP EU COOLING FAN FAILED A UF6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 858AW 2035 ORD - FLT 5712 - THE NR 1 AVIONICS COOLING FAN FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED FLOW SENSOR HM23. SY STEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 2000030700006 20000307 00006 EU 2000 3 7 2000ZZZM74 1 19991208 A 5320 S53678008220 CHANNEL AEROSP ATR72 ATR72212 EU FRAME 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 PAX DOOR SILL SUPPORT IS CORRODED (AFT). BLENDED OUT TO BEYOND MANUAL LIMITS (IAW ATR-72 SRM 51-21-42). INSTALLED NEW FLOOR SUPPORT BETWEEN FRAME 36 AND 39 IAW ATR 72-SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 2000030700007 20000307 00007 EU 2000 3 7 2000ZZZM75 1 19991208 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 24-29 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 RIGHT MID INBOARD SEAT TRACK HAS CORROSION FROM FRAME 24 TO 29, (.27 INCH ON T-5 AREA). BLENDED OUT CORROSION FOUND TO BE BEYOND LIMIT OF .033 INCH. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000030700008 20000307 00008 EU 2000 3 7 2000ZZZM76 1 19991208 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 24-29 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 LEFT MID INBOARD SEAT TRACK HAS CORROSION FROM FRAME 24 TO 29 BLENDED OUT CORROSION FOUND TO BE BEYOND LIMIT .028 INCH. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000030700009 20000307 00009 EU 2000 3 7 2000ZZZM77 1 19991208 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 24-29 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 LEFT MID OUTBOARD SEAT TRACK HAS CORROSION AT FRAME 28D BLENDED OUT CORROSION FOUND TO BE BEYOND LIMITS AT ATTACHMENT PO INT. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000030700010 20000307 00010 EU 2000 3 7 2000ZZZM78 1 19991208 A 5347 S53578001244 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 LEFT AFT OUTBOARD SEAT TRACK HAS CORROSION IN TRACK (.025 INCH) TO T-5 AREA. BLENDED OUT CORROSION FOUND TO BE BEYOND L IMITS. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000030700011 20000307 00011 EU 2000 3 7 2000ZZZM79 1 19991208 A 5315 S536780022251 FLOORBEAM AEROSP ATR72 ATR72212 EU BS 39-40 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 FLOOR SUPPORT BETWEEN FLOORBEAMS 30 TO 40 CORRODED.. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 5125-25-58 . REMOVED AND REPLACED SUPPORT IAW SRM 51-25-02 AND 51-25-03. (M) 2 H 7 2 4T RT A53EU 2000030700012 20000307 00012 EU 2000 3 7 2000ZZZM80 1 19991208 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 36-39 CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 417AT 417 RIGHT AFT FLIGHT ATTENDANT SEAT TRACK IS CORRODED AROUND THE NUTPLATES. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS . REMOVED AND REPLACED SUPPORT IAW EO NR E9-5300-013 R4. (M) 2 H 7 2 4T RT A53EU 2000030700013 20000307 00013 NM 2000 3 7 TSAA9933512 1 19991201 A 3350 86210066 BATTERY BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 6 FLOOR PROXIMITY LIGHT FAILED BATTERY TEST. REPLACED NR 6 FLOOR PROXIMITY LIGHT. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 2000030700014 20000307 00014 EU 2000 3 7 SIMA993262 1 19991122 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 1605 540 HRL - FLT 3724 - EMERGENCY LIGHTS WON'T ARM. THE LIGHTS COME ON IN THE ARM POSITION AND WILL NOT EXTINGUISH. FERRIED A IRCRAFT TO DFW AND THE EMERGENCY LIGHT BATTERY PACKS WERE REPLACED AT LOCATIONS 43WL, 61WL, 73WL AND 82WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700015 20000307 00015 EU 2000 3 7 2000ZZZM81 1 19991122 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 1658 540 HRL - FLT 3724 - EMERGENCY LIGHTS WON'T ARM. THE LIGHTS COME ON IN THE ARM POSITION AND WILL NOT EXTINGUISH. FERRIED A IRCRAFT TO DFW AND THE EMERGENCY LIGHT BATTERY PACKS WERE REPLACED AT LOCATIONS 43WL, 61WL, 73WL AND 82WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700016 20000307 00016 EU 2000 3 7 2000ZZZM82 1 19991122 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 1535 540 HRL - FLT 3724 - EMERGENCY LIGHTS WON'T ARM. THE LIGHTS COME ON IN THE ARM POSITION AND WILL NOT EXTINGUISH. FERRIED A IRCRAFT TO DFW AND THE EMERGENCY LIGHT BATTERY PACKS WERE REPLACED AT LOCATIONS 43WL, 61WL, 73WL AND 82WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700017 20000307 00017 EU 2000 3 7 2000ZZZM83 1 19991122 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 1601 540 HRL - FLT 3724 - EMERGENCY LIGHTS WON'T ARM. THE LIGHTS COME ON IN THE ARM POSITION AND WILL NOT EXTINGUISH. FERRIED A IRCRAFT TO DFW AND THE EMERGENCY LIGHT BATTERY PACKS WERE REPLACED AT LOCATIONS 43WL, 61WL, 73WL AND 82WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700018 20000307 00018 EU 2000 3 7 SIMA993341 1 19991130 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AT 804 274 DFW - FLT 3701 - ALTERNATING EMERGENCY FLOOR PROXIMITY LIGHTS, TWO EXIT LIGHTS AND EXIT SIGN ABOVE COCKPIT DOOR DO NOT I LLUMINATE. REMOVED AND REPLACED BATTERY PACK IN ONE EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700019 20000307 00019 EU 2000 3 7 SIMA993371 1 19991203 A 3350 GE44 LAMB AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AT 355 MIA - FLT 5276 - MAIN CABIN DOOR STAIRS EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CH ECK GOOD. (M) 2 H 7 2 4T RT A53EU 2000030700020 20000307 00020 EU 2000 3 7 SIMA993555 1 19991219 A 3350 3071BPEGPL LIGHT SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AE 340B348 DFW - FLT 3577 - FLOOR PROX EMERGENCY LIGHT INOPERATIVE SEAT 4A. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. ( M) 2 L 7 2 4T RT A52EU 2000030700021 20000307 00021 EU 2000 3 7 SIMA993554 1 19991220 A 3350 5211309111 LIGHT AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AT 434 MIA - FLT 5339 - FLOOR PROX EMERGENCY LIGHT IN FRONT OF GALLEY CART INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY L IGHT. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2000030700022 20000307 00022 EU 2000 3 7 SIMA993232 1 19991119 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU SEAT 9 BROKEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 310DK 310 ORD - FLT 4350 - EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 9B DOES NOT ILLUMINATE. REPAIRED BROKEN WIRE AT CANNON PLUG 37 WLA PIN C. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2000030700023 20000307 00023 EU 2000 3 7 SIMA993273 1 19991123 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 581 135 ORD - FLT 4205 - LOWER EMERGENCY LIGHTS AT THE RIGHT FORWARD EMERGENCY EXIT DO NOT ILLUMINATE. REMOVED AND REPLACED RIG HT EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700024 20000307 00024 EU 2000 3 7 SIMA993321 1 19991128 A 2530 16707 SOCKETS AEROSP ATR42 ATR42300 8680920 EU GALLEY DAMAGED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 327AT 327 MIA - FLT 5401 - FLIGHT ATTENDANT REPORTS ODOR COMING FROM AN UNKNOWN SOURCE IN THE AFT CABIN. INSPECTED AND FOUND BOTH HOT CONTAINER SOCKETS TO BE DAMAGED. REMOVED AND REPLACED BOTH HOT CONTAINER SOCKETS AND BOTH HOT CONTAINERS. OPERATI ONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700025 20000307 00025 EU 2000 3 7 SIMA993352 1 19991201 A 3350 AD3127 TERMINAL AEROSP ATR42 ATR42300 8680920 EU BATTERY PACK BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ 16631 135 SAW - DURING PS-2 INSPECTIN, FOUND THE FORWARD EMERGENCY FLOOR PROXIMITY LIGHTS BETWEEN SEAT 1AB AND 5AB DID NOT ILLUMIN ATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 3WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700026 20000307 00026 EU 2000 3 7 SIMA993404 1 19991206 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 424MQ 6486 045 ORD - FLT 4276 - SEVERAL EMERGENCY FLOOR PROXIMITY LIGHTS REMAIN ILLUMINATED WITH BATTERY SWITCH OFF. REMOVED AND REPLA CED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT LOCATION 29WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700027 20000307 00027 NM 2000 3 7 TSAA9949510 1 19991221 A 4920 38042814 APU BOEING 737 73725A 1384481 NM APU BAY LEAKING A TSAA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 819AL 11713 23791 FLT 29 - HNL-KOA - APU SHUTDOWN IN FLIGHT. INSPECTED APU AND FOUND LOW OIL QTY. APU LEAKING OIL. REMOVED AND REPLACED APU PER FORM M-133. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2000030700028 20000307 00028 NM 2000 3 7 TSAA9933508 1 19991220 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 5 FLOOR LIGHT EMERGENCY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2000030700029 20000307 00029 NM 2000 3 7 TSAA9933507 1 19991217 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 4 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 2000030700030 20000307 00030 NM 2000 3 7 TSAA9933505 1 19991218 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 1 POSITION PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F A16WE 2000030700031 20000307 00031 NM 2000 3 7 TSAA9933506 1 19991217 A 3350 9221009 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT ASSY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 2000030700032 20000307 00032 EU 2000 3 7 C2XA99IA641 1 19991230 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14451 512 IAH - DURING MAINTENANCE INSPECTION, THE NR 2 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE LOW. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW ATR42-500 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 2000030700033 20000307 00033 EU 2000 3 7 C2XA99IA640 1 19991229 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING MAINTENANCE INSPECTION, THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-320 JIC 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700034 20000307 00034 SO 2000 3 7 C2XA99IA637 1 19991221 A 5550 14531597602 ANGLE EMB 145 EMB145ER SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15948 145056 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHOR IZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000030700035 20000307 00035 SO 2000 3 7 C2XA99IA636 1 19991221 A 5550 14531597601 ANGLE EMB 145 EMB145ER SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15948 145056 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORI ZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000030700036 20000307 00036 SO 2000 3 7 C2XA99IA635 1 19991221 A 5320 SUPPORT EMB 145 EMB145ER SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15948 145056 IAH - DURING C-CHECK INSPECTION, THE LEFT SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED NEAR FRAME 20. MAINTENANCE REMOVE D THE CORROSION AND INSTALLED A REPAIR DOUBLER ON THE AFFECTED SUPPORT IAW EMBRAER FAX SST 1274-99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000030700037 20000307 00037 SO 2000 3 7 C2XA99IA632 1 19991210 A 5320 14531597602 ANGLE EMB 145 EMB145ER SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12946 145052 IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER RIGHT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC-5 330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000030700038 20000307 00038 SO 2000 3 7 C2XA99IA631 1 19991210 A 5320 14531597601 ANGLE EMB 145 EMB145ER SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12946 145052 IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER LEFT DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC-53 30-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000030700039 20000307 00039 SO 2000 3 7 C2XA99IA630 1 19991210 A 5320 14522460007 BEAM EMB 145 EMB145ER SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12946 145052 IAH - DURING C-CHECK INSPECTION, THE OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20 LEFT. MAINTENANCE REMOVED THE CORR OSION AND INSTALLED A REPAIR DOUBLER IAW EMBRAER SCHEME STS1274/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000030700040 20000307 00040 SO 2000 3 7 C2XA99CL129 1 19991218 A 3230 12038594001 CONTROL PANEL EMB 120 EMB120RT SO MLG FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 15730 120187 CLE - FLT 3061 - AFTER TAKEOFF FROM CLE, THE LEFT MAN GEAR GREEN LIGHT REMAINED ILLUMINATED (A-SYSTEM). THE CREW CYCLED THE GEAR AGAIN AND GREEN LIGHT STAYED ILLUMINATED. AIRCRAFT RETUREND TO CLE WITH NO FURTHER INCIDENT. MAINTENANCE REM OVED AND REPLACED THE LANDING GEAR CONTROL PANEL AND PERFORMED OPERATIONAL CHECKS IAW EMB 120MM 32-30-00. THE AIRCRAFT WAS RELEASES TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000030700041 20000307 00041 EU 2000 3 7 C2XA99IA634 1 19991217 A 3350 3013000 POWER SUPPLY AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 2000030700042 20000307 00042 SO 2000 3 7 C2XA99IA633 1 19991216 A 5330 12301695011 SKIN EMB 145 EMB145ER SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12946 145052 IAH - DURING MAINTENANCE INSPECTION, THE LEFT SKIN UNDER THE CAPTAINS SIDE WINDOW WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED THE SKIN IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01112, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000030700043 20000307 00043 SO 2000 3 7 C2XA99CL130 1 19991229 A 3260 85271 SWITCH EMB 145 EMB145LR SO RT MLG FAILED A C2XA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 14950 1898 A10949 145061 CLE - FLT 3875 - THE CREW REPORTED, RECEIVED LANDING GEAR AIR/GROUND FAIL MESSAGE DURING LANDING APPROACH. THE LANDING WAS ABORTED AND THE CREW PERFORMED THE PROCEDURES IN THE QRH MANUAL. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER I NCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 WEIGHT ON WHEELS SWITCH ON THE RIGHT MAIN LANDING GEAR. OPERATIONAL CHECKS WERE GOOD IAW EMBRAER 145 MM 32-63-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT T00011AT 2000030700044 20000307 00044 SO 2000 3 7 C2XA99BT114 1 19991219 A 3350 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14959 145091 BTV - FLT 4218 - DURING SERVICE CHECK, FOUND RIGHT EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE ADJUSTED AND CLEANED RIG HT EMERGENCY LIGHT AND OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 2000030700045 20000307 00045 EU 2000 3 7 C2XA99BT115 1 19991226 A 3234 F96GA0102 CONTROL LEVER AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 15816 365 105 EWR - FLT 3136 - CREW REPORTED LANDING GEAR WOULD NOT RETRACT. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPS CHECK SYSTEM GOOD, AND RETURNED THE AIRCRAFT FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 2000030700046 20000307 00046 WP 2000 3 7 GAIA99169 1 19991117 A 5230 1414813 TEE DOUG DC9 DC915F 3022037 WP CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND A CRACK AT THE FORWARD END OF THE NR 5 TOP BEAM TEE ON THE AFT LOWER CARGO DOOR. THE B EAM TEE WAS REPAIRED IAW DC-9 SRM THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2000030700047 20000307 00047 WP 2000 3 7 GAIA99170 1 19991117 A 5330 99155872 WINDOW DOUG DC9 DC915F 3022037 WP BS 465-484 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND A CRACK ABOVE THE RIGHT WINDOW BELT JUST FORWARD OF THE OVERWING EXIT. THE SKIN WAS RE PAIRED IAW MCDONNEL DOUGLAS DRAWING J060109 THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2000030700048 20000307 00048 WP 2000 3 7 GAIA99171 1 19991117 A 5313 2777922 LONGERON DOUG DC9 DC915F 3022037 WP BS 313 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND A CRACK ON LONGERON 28 LEFT AT FUSELAGE STATION 313. THE LONGERON WAS REPAIRED IAW THE DC-9 SRM THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2000030700049 20000307 00049 WP 2000 3 7 GAIA99172 1 19991117 A 5240 5910084 CLIP DOUG DC9 DC915F 3022037 WP SERVICE DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND A CRACKED CLIP AT THE FORWARD END OF THE NR 1 BEAM ON THE FORWARD GALLEY SERVICE DOOR. THE CLIP WAS REPLACED IAW THE DC-9 SRM THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2000030700050 20000307 00050 WP 2000 3 7 GAIA99173 1 19991117 A 5330 591142459 SKIN DOUG DC9 DC915F 3022037 WP BS 758-780 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND TEMPORARY REPAIR ON THE SKIN BY THE AFT BAG BIN. THE SKIN WAS REPAIRED IAW KITTY HAWK EA D9-53-079 THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 2000030700051 20000307 00051 NE 2000 3 7 GAIA99212 2 19991124 A 7320 SENSE LINE BOEING 727 727224 1384076 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE DISCONNECTED A GAIA E C ENGINE SHUTDOWN ABORTED TAKEOFF J X WARNING INDICATION ENGINE FLAMEOUT TO TAKEOFF 1 SW 07 69735 20664 666960 FLT 2027 - DEN-MHR - DURING TAKEOFF, THE NR 2 ENGINE FAILED AFTER TAKEOFF. THE CREW PERFORMED ABNORMAL CHECKLIST AND RE TURNED TO DEN DECLARING AN EMERGENCY LANDING. THE AIRCRAFT LANDED SAFELY WITHOUT ANY INCIDENT. MAINTENANCE FOUND THE S ENSE LINE TO THE FUEL CONTROL DISCONNECTED. RECONNECTED SENSE LINE. RAN ENGINE ALL PARAMETERS NORMAL AT THIS TIME. TH E AIRCRAFT WAS RELEASE TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000030700052 20000307 00052 NM 2000 3 7 GAIA99214 1 19991201 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1090 MISMANUFACTURED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CE RTIFICATE, SEAT TRACK AT RBL 24.75 TOO SHORT FOR CARGO MOD BODY STATION 1090 TO 1110. REMOVED AND REPLACED SEAT TRACK A T RBL 24.75 FROM BS 970 TO BS 1136 PER B727 SRM 53-10-5. (M) 2 L 7 3 4F A3WE 2000030700053 20000307 00053 NM 2000 3 7 GAIA99215 1 19991201 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 680 MISMANUFACTURED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KGA CE RTIFICATE, SEAT TRACK AT RBL 45.5, BS 680 TO BS 720A HAS WRONG SPLICE FOR 9G BULKHEAD. REMOVED AND REPLACED SEAT TRACK AT RBL 45.5 FROM STATION 560 TO 720A, IAW AEISTC SA 1797SO AND SA1798SO. (M) 2 L 7 3 4F A3WE 2000030700054 20000307 00054 NM 2000 3 7 GAIA99216 1 19991201 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 400 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CER TIFICATE, CABIN FLOORBEAM AT BODY STATION 400, RBL 12 CORRODED. REMOVED CORROSION AT FLOORBEAM. CUTOUT AND REMOVED DAM AGED AREAS PER SRM 53-10-8 PAGE 18. FABRICATED REPAIR PARTS AND INSTALLED IAW 53-10-8. (M) 2 L 7 3 4F A3WE 2000030700055 20000307 00055 NM 2000 3 7 GAIA99217 1 19991201 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1110 MISMANUFACTURED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERT IFICATE, SEAT TRACK AT LBL 45.5 TOO SHORT FOR CARGO MOD BODY STATION 1110 TO 1130. REMOVED AND REPLACED SEAT TRACK AT L BL 45.5 FROM BS 1030 TO BS 1136, PER B727 SRM 53-10-5, FIG 7. (M) 2 L 7 3 4F A3WE 2000030700056 20000307 00056 NM 2000 3 7 GAIA99218 1 19991201 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 970 MISMANUFACTURED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERT IFICATE, SEAT TRACK AT RBL 45.5 IS TOO SHORT FOR CARGO MOD AT SPLICE, BODY STATION 1090 TO 1110. REMOVED AND REPLACED S EAT TRACK AT RBL 45.5 FROM STATION 970 TO 1136 IAW B727 SRM 53-10-5. (M) 2 L 7 3 4F A3WE 2000030700057 20000307 00057 NM 2000 3 7 GAIA99219 1 19991201 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 380 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 77780 20635 FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CER TIFICATE, CABIN FORWARD GALLEY FLOORBEAM AT BODY STATION 380, RBL 14 TO RBL 64 IS CORRODED. REMOVED CORROSION AT FLOORB EAM. CUTOUT AND REMOVED DAMAGED AREAS AT BS 380 FROM RBL 14 TO RBL 58 PER SRM 53-10-8. FABRICATED REPAIR PARTS AND INS TALLED IAW 53-10-8 FIG 3. (M) 2 L 7 3 4F A3WE 2000030800001 20000308 00001 NM 2000 3 8 AALA991735 1 19991116 A 2597 WIRE BOEING 767 767323 1385205 NM SIGN SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 351AA 24032 BOS - FLT 68 - EN ROUTE MIA-MAD - BURNING ELECTRICAL SMELL OCCURRED IN THE FIRST CLASS CABIN NEAR SEATS 3A AND 3B. DISS IPATED AFTER A FEW MINUTES. AFTER SMELL RETURNED, CREW TURNED OFF UTILITY BUSSES AND RECIRCULATING FAN. DIVERTED TO BO S AND LANDED WITHOUT INCIDENT. REPAIRED WIRE AT FIRST CLASS LAV F2 RETURN TO SEAT SIGN. SYSTEM GROUND CHECK NORMAL O PERATION. (M) 2 L 7 2 4F RT A1NM 2000030800002 20000308 00002 NM 2000 3 8 USAA991340 1 19991206 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 47148 22752 TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK AT LOWER HINGE CUTOUT ON DOOR STRINGE R 17L, BS 312 SKIN. INSTALLED DOUBLER PER TR 52-10-05. (M) 2 L 7 2 4F A16WE 2000030800004 20000308 00004 NE 2000 3 8 MZZA99229 2 19991115 A 7260 07726090002 GEARBOX BOEING 727 727264 138408M NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE DAMAGED A MZZA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 625DH 9207 20780 MNL - FLT 892 - PRECAUTIONARY ENGINE NR 3 SHUTDOWN, DUE TO OIL QTY LOSS DURING CLIMB-OUT. NO ENGINE PARAMETERS EXCEEDED . MAINTENANCE REMOVED AND REPLACED GEARBOX PER TASK CARD 99-7260-1-4005. OPS AND LEAKCHECK GOOD ENGINE COWL SECURED. A IRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000030800007 20000308 00007 NM 2000 3 8 WRLA99018 1 19990912 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 277WA 48743 DURING PERFORMANCE OF 1C CHECK, MAINTENANCE PERSONNEL FOUND CORROSION UNDER MOON MAT AND STRUCTURE AT GALLEY'S G3, G4, G 5, AND G8. REPAIRED SEAT TRACKS AND STRUCTURE IAW MD11 SRM 53. CORROSION WAS DETERMINED TO BE LEVEL1. (M) 2 L 7 3 4F RT A22WE 2000030900025 20000309 00025 NM 2000 3 9 WRLA99016 1 19990912 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 277WA 48743 DURING PERFORMANCE OF "1C" CHECK, MAINTENANCE PERSONNEL FOUND CORROSION IN SEAT TRACKS AT LAVATORIES A, B, C, D, E, F, M . REPAIRED SEAT TRACKS AND STRUCTURE IAW MD 11 SRM 53. CORROSION WAS DETERMINED TO BE LEVEL 1. (M) 2 L 7 3 4F RT A22WE 2000030900027 20000309 00027 2000 3 9 AALA991971 4 19991226 A 2397 WIRE AIRBUS 300 A300B4605R 3930308 EU VIDEO RECORDER CHAFED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 91050 423 PTY - FLT 917 - DURING FLIGHT ELECTRICAL BURING SMELL AROUND BUSINESS CLASS VIDEO RECORDER. DIVERTED AND LANDED PTY WIT HOUT INCIDENT. REPAIRED CHAFED WIRING. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED VIDEO RECORDER AS PRECAUTION. ( M) 2 L 7 2 4F RT A35EU 2000030900029 20000309 00029 NE 2000 3 9 WRLA99022 2 19991109 A 7230 54A831 BLADE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE BENT A WRLA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CR CRUISE 1 EA 27 272WA 48437 DURING FLT, NR 3 ENGINE SHUTDOWN DUE TO VIBRATION, VIBRATION MONITOR AT 5 FOR COMPRESSOR DURING T/O. VIBRATION MONITOR REDUCED TO 2.5 AT LOWER RPM IAW FCOM VOL I PROCEDURES FUEL WAS DUMPED TO MAXIMUM LANDING WEIGHT (85,000 LBS) AND A/C RET URNED TO SSN WITHOUT FURTHER INCIDENT. AFTER LANDING AT SNN, AN INSPECTION OF THE ENGINE SHOWED EVIDENCE OF A BIRD STRI KE/INGESTION. ENGINE NR 3 FAN BLADES NR 29, 30, 31 AND 33 FOUND BENT AND OUT OF LIMITS PER MM 72-31-00. FURTHER INSPEC TION PER MX TASK CARD 0268 FOR BIRD STRIKES, THE ENGINE BORESCOPE AT THE 5TH, 8TH, 9TH, 13TH AND 14TH STAGES. NO DAMAGE OR DEFECTS WERE FOUND. REPLACED FAN BLADES PER MATCHED SETS. GROUND RUN ENGINE OK. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 2000030900030 20000309 00030 EU 2000 3 9 SIMA3645 1 19991228 A 3350 3013000 POWER PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 538AT 0479 538 CRP - FLT 3750 - FOUND SERVICE DOOR AND PASSENGER DOOR EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED POWER PACK. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 2000030900031 20000309 00031 NE 2000 3 9 AALA991770 2 19991123 A 7200 AC9806F65 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RIGHT MALFUNCTIONED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 424AA 49336 PHX - FLT 1267 - EN ROUTE DFW-LAX, RIGHT ENGINE LOW OIL PRESSURE ILLUMINATED. OIL QTY READ ZERO. SHUT ENGINE DOWN. CR EW DECLARED EMERGENCY AND LANDED PHX WITHOUT FURTHER INCIDENT. REPLACED NUMBER 6 PUMP CARBON SEAL ASSEMBLY AND BEARING ASSEMBLY AS A PRECAUTION AND REPLACED MAIN ENGINE OIL FILTER. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 2000030900033 20000309 00033 2000 3 9 AALA991981 4 19991227 A 2220 285N001140 CONTROLLER BOEING 757 757223 1384957 NM E/E BAY FAILED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 626AA DO2766 24584 ORD - FLT 84 - ON APPROACH, LEADING EDGE SLAT DISAGREE 20 DEGREES. EMERGENCY DECLARED LANDED ORD WITHOUT INCIDENT. REP LACED FLAP/SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. FLAPS WERE NEVER OVER SPED. (M) 2 L 7 2 4F RT A2NM 2000030900045 20000309 00045 WP 2000 3 9 AALA2000119 1 19991230 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 474 49649 TUL - TWO CRACKS IN FUSELAGE SKIN AT STATION 380 ANTENNA ATTACHMENT AT 6 O'CLOCK POSITION, STRINGER 30, STATION 380. CU T OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F A6WE 2000030900056 20000309 00056 NE 2000 3 9 TSAA9905519 2 19991230 A 7200 ENGINE BOEING 737 737230C 1384472 NM PWA JT8 JT8D15 52051 NE NR 1 BIRD STRIKE A TSAA O OTHER C F.O.D. NR NOT REPORTED 1 WP 13 820AL 22138 FLT 63 - HNL-LIH - BIRD STRIKE NR 1 ENGINE. ENGINE ROLLED BACK INITIALLY AND RETURNED TO NORMAL PARAMETERS. RETURNED T O HNL. UNEVENTFUL LANDING. PERFORMED BIRD STRIKE CONDITION INSPECTION IAW FORM M-106. NO DEFECTS NOTED. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 2000030900059 20000309 00059 NM 2000 3 9 AALA991955 1 19991222 A 3350 MS25308302 SWITCH BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 649AA 24607 ORD - FLT 1470 - BEFORE FLIGHT AT GATE, R3 AND L3 AFT SLIDE EMERGENCY LIGHTS FAILS TEST FROM EXTERIOR EMERGENCY LIGHT TE ST SWITCH. LEFT MIDWING EMERGENCY LIGHT AND RIGHT MIDWING AFT EMERGENCY LIGHT FAIL TEST FROM EXTERIOR EMERGENCY TEST SW ITCH. ALL TEST GOOD FROM INTERIOR EMERGENCY LIGHT TEST SWITCH. REPLACED EXTERIOR EMERGENCY LIGHT SWITCH. SYSTEM GROUN D CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 2000030900061 20000309 00061 WP 2000 3 9 2000ZZZM260 1 19991105 A 5730 SKIN DOUG DC8 DC8F55 3021928 WP WS 454 DAMAGED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 55626 45764 SCREWS PULLING THROUGH SKIN L/E CENTER SECTION LOWER SURFACE XW454 LEFT WING. REPLACED SCREWS AND INSTALLED DIMPLE WASH ERS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 11/05/99. (M) 2 L 7 4 4F 4A25 2000030900068 20000309 00068 WP 2000 3 9 AALA991755 1 19991116 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 235-237 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 465A 49595 TUL - DEEP CORROSION ON L-30 STA 325 - STA 237. INSTALLED LONGERON SPLICE AT STA 235 ON LONGERON 30 PER ESO 80559 DATED 11-16-99. (X) 2 L 7 2 4F RT A6WE 2000031100059 20000311 00059 WP 2000 3 11 T64R387AR 1 19990705 A 5512 COVER DOUG DC8 DC862 3021970 WP HORIZ STAB PUNCTURED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 ARROW AIR - NR 2073, LEFT HORIZ STABILIZER T/E OUTBOARD DAMPER WELL HOLE PUNCHED THROUGH. REMOVED DAMPER WELL COVER IAW DC-8 SRM 51-1-21, WELDED HOLE PER EO 99-061 AND REINSTALLED IAW DC-8 SRM 51-1-21. (M) 2 L 7 4 4F 4A25 2000031100060 20000311 00060 WP 2000 3 11 99T64R386AR 1 19990707 A 5753 5614376513 FITTING DOUG DC8 DC862 3021970 WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2579 - REMOVE FLAP CANOE FITTING AT STATION XF340, HOLE ELONGATED. REMOVED FLAP CANOE FITTING AT STATINO XF340 IAW D C-8 MM 27-51-12. REPLACED FLAP CANOE FITTING IAW DC-8 MM 27-51-12, SB27-260 R2 AND BOEING MESSAGE M-72-99-04220. (M) 2 L 7 4 4F 4A25 2000031100061 20000311 00061 WP 2000 3 11 99T64R385AR 1 19990515 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1120-1160 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2395, C-PIT UNDER KICK PLATE CORRODED. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PE EO 99- 047 AND EO 99-061. (M) 2 L 7 4 4F 4A25 2000031500001 20000315 00001 NE 2000 3 15 2000ZZZM63 2 19991130 A 7230 NR 3 DISK BOEING 727 7272J7 138400E NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 15 128NA 49423 20879 655968 FLT 312 - KCLT-KMIA - AFTER TAKEOFF EPR DECREASED AND EGT INCREASED. RETARDED THROTTLE TO CONTROL EGT WHEN VIBRATION WA S NOTICED AND EXPERIENCED COMPRESSOR STALL. WHEN THROTTLE RETURNED TO IDLE, EGT CONTINUED TO CLIMB. PERFORMED ENGINE I NFLIGHT SHUTDOWN PROCEDURES AND RETURNED TO KCLT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. FOUND NR 3 COMPRESSOR DISK HAD DROPPED. REMOVED AND REPLACED NR 1 ENGNIE. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000031500002 20000315 00002 NM 2000 3 15 AALA991855 1 19991204 A 2121 215201 FAN BOEING 727 727223 1384074 NM ACM BAY FAILED A AALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 860AA AA12986 21087 MIA - FLT 1403 - DESCENDING THROUGH 8000 FEET AT MIA, A STRONG ELECTRICAL AND PLASTIC ODOR OCCURRED THROUGH OUT CABIN. D ECLARED EMERGENCY AND LANDED MIA WITHOUT INCIDENT. REPLACED GASPER FAN. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000031500003 20000315 00003 EU 2000 3 15 AALA991333 1 19990907 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1401G 11352 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000031500004 20000315 00004 EU 2000 3 15 AALA991445 1 19990924 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU ROW 4 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1434A 11419 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 4 INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT SEGMENT AT ROW 4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000031500005 20000315 00005 EU 2000 3 15 AALA991501 1 19991003 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1468A 11501 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH MARKER AT AFT OVERWING DOOR INOPERATIVE. REPLACED EMERGEN CY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A20EU 2000031500006 20000315 00006 EU 2000 3 15 AALA991548 1 19991015 A 3350 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN MISINSTALLED A AALA K NONE L W NO TEST INADEQUATE Q C IN INSP/MAINT 1 SW 07 1411G 11369 TUL - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTING FORWARD AND AFT HALVES FLASHED ON AND OFF OPPOSITE EACH OTHER. REVERSED POLARITY ON NR 2 AND THREE BATTERY MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000031500007 20000315 00007 EU 2000 3 15 AALA991552 1 19991016 A 3350 1501051 LIGHT GRIMES FOKKER F28 F28MK0100 4990807 EU LT FAIRING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1442E 11437 DFW - DURING OVERNIGHT MAINTENANCE, LEFT FAIRING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT FAIRING EMERGNCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000031500008 20000315 00008 EU 2000 3 15 AALA991527 1 19991010 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1407D 11360 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000031500009 20000315 00009 EU 2000 3 15 AALA991526 1 19991010 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1440A 11435 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN OVER FORWARD SERVICE DOOR INOPERATIVE. REPAIRED WIRE ON EMERGEN CY EXIT SIGN OVER FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.. (M) 2 L 7 2 4F RT 2000031500010 20000315 00010 EU 2000 3 15 AALA991273 1 19990824 A 7732 ENGINE FOKKER F28 F28MK4000 4990810 EU NR 1 MALFUNCTIONED A AALA O OTHER E VIBRATION/BUFFET AP APPROACH 1 SW 07 1468A 11501 DFW - FLT 1794 - ON APPROACH TO DFW FROM MTY, NR 1 ENGINE VIBRATION INDICATOR INDICATED VIBRATION IN RED ZONE USING BOTH PRIMARY AND ALTERNATE SELECTIONS. POWER TO NR 1 ENGINE REDUCED TO IDLE AND VIBRATION INDICATION RETURNED TO GREEN ZONE . EMERGENCY WAS DECLARED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. INVESTIGATION FOUND NO DISCREPANCIES. BOTH ENGINES RUN TO FULL POWER SEVERAL TIMES WITH NO VIBRATIONS NOTED ON PRIMARY AND ALTERNATE SELECTIONS. SYSTEM GROUND CHECKED NO RMAL OPERATION. (M) 2 L 7 2 4F RT A20EU 2000031500011 20000315 00011 NM 2000 3 15 AALA991654 1 19991103 A 3350 1001141 LIGHT GRIMES BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 717AA 20610 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMEGNCY EXIT LIGH T ASSEMBLY. SYSTEM GROUND CHCKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000031500012 20000315 00012 NM 2000 3 15 AALA991691 1 19991113 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720AA 20613 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS CLOSE TO AFT ENTRY DOOR INOPERATIVE. REPLACED EMER GENCY EXIT FLOOR PATH LIGHT STRIP AT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000031500013 20000315 00013 NM 2000 3 15 AALA991793 1 19991125 A 3350 1001191 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 727AA 20734 DFW - DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000031500014 20000315 00014 NM 2000 3 15 AALA991745 1 19991118 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 726AA 20733 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED FORWARD FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000031500015 20000315 00015 WP 2000 3 15 USAA990084 1 19990212 A 5210 995576311 WEB DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 829US 35668 49429 PIT - DURING C2 CHECK, FOUND 1 INCH CRACK ON VERTICAL WEB AT CENTER OF DOOR ADJACENT TO DOOR OPERATING MECHANISM BETWEEN BEAM 4 AND 5 INNER DOOR HINGE, BOX AFT INTERCOSTAL. INSTALLED DOUBLER P/N SR09520001-3 PER SRM 52-05 FIG 4-5. (M) 2 L 7 2 4F A6WE 2000031500016 20000315 00016 NM 2000 3 15 USAA990083 1 19990207 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 767-787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 44562 22883 PIT - DURING A CHECK, FOUND 3 INCH CRACK IN SKIN ALSO INTERNAL ANTENNA CHANNEL CRACKED 8 INCH - 10 INCH LONG BETWEEN STA TION 767 AND 787 BL0. INSTALLED EXTERNAL DOUBLER AND REPLACED INNER ANTENNA CHANNEL PER SRM 53-30-3 FIG 1, FOR REPAIR D OUBLER. (M) 2 L 7 2 4F A16WE 2000031500017 20000315 00017 NM 2000 3 15 USAA990927 1 19990904 A 5720 STIFFENER BOEING 737 737201 1384454 NM BS 540 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 44852 22797 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION, LOWER END OF STIFFENER, STATION 5 40, RBL 14.90. CORROSION LEVEL 1. INSTALLED REPAIR DOUBLER PER SRM 51-40-4 FIG 1.. (M) 2 L 7 2 4F A16WE 2000031500018 20000315 00018 NM 2000 3 15 USAA990304 1 19990401 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AU 22795 TPA - DURING EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK AT AFT ENTRY DOOR, UPPER HINGE CUTOUT FUSELAGE SKIN. REPA IRED PER SRM 53-30-03 FIG 21A. (M) 2 L 7 2 4F A16WE 2000031500019 20000315 00019 NM 2000 3 15 USAA119920 1 19991127 A 5320 BEAM BOEING 727 727227 1384078 NM BS 1183 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FOUND DURING C-CHECK, AFT PRESSURE BULKHEAD, FORWARD FLANGE CRACK, BLR 17.8, WL 278 IN FLAGE RADIUS. ACCOMPLISHED REPAI R AT AFT PRESSURE BULKHEAD RBL 17.8 WL 278 IAW B727 SB NR 727-53-55. (M) 2 L 7 3 4F A3WE 2000031500020 20000315 00020 WP 2000 3 15 USAAD99171 1 19991202 A 2100 20495054 ACM DOUG DC9 DC981 3022081 WP AC BAY SEIZED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 814US 41917 48094 PIT-DFW - FLT 546 - AFTER TAKEOFF THE CABIN PRESSURIZATION FLOW LIGHT ILLUMINATED AND THE FLIGHT CREW WAS NTO ABLE TO ST ABILIZE THE CABIN PRESSURE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE LANDING WEIGHT WAS 133 ,700 LBS. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING PACK COOLING TURBINE AND THE RIGHT AIR CONDITIONING PACK WATER SEPARATOR TEMP CONTROL VALVE. AN OVERWEIGHT LANDING INSPECTINO WAS PERFORMED. (M) 2 L 7 2 4F A6WE 2000031500021 20000315 00021 WP 2000 3 15 2000ZZZM64 1 19991202 A 2100 97968011 VALVE DOUG DC9 DC981 3022081 WP AC BAY STUCK A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 814US 3903 48094 PIT-DFW - FLT 546 - AFTER TAKEOFF THE CABIN PRESSURIZATION FLOW LIGHT ILLUMINATED AND THE FLIGHT CREW WAS NTO ABLE TO ST ABILIZE THE CABIN PRESSURE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE LANDING WEIGHT WAS 133 ,700 LBS. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING PACK COOLING TURBINE AND THE RIGHT AIR CONDITIONING PACK WATER SEPARATOR TEMP CONTROL VALVE. AN OVERWEIGHT LANDING INSPECTINO WAS PERFORMED. (M) 2 L 7 2 4F A6WE 2000031500022 20000315 00022 NE 2000 3 15 USAAD99172 2 19991203 A 7250 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT FAILED A USAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 19 823US 49142 PIT - BUF - FLT 1648 - AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE AND VIBRATION. THE CREW SUSPECTED A NOSE GEAR DOOR NO T FULLY CLOSED AS THER WERE NO ABNORMAL ENGINE INDICATIONS. HALF WAY THROUGH THE FLIGHT THE LEFT ENGINE REVERSE THRUST LIGHT ILLUMINATED. THE LEFT EGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. SINGLE ENGINE IS UNKNOWN. M AINTENANCE REPLACED THE LEFT ENGINE DUE TO TURBINE FAILURE. (M) 2 L 7 2 4F 4 F A6WE E9NE 2000031500023 20000315 00023 WP 2000 3 15 USAAD99173 1 19991207 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918VJ 48138 IAD - FOUND THE PIN PULLED ON THE MAIN ENTRANCE DOOR EMERGENCY CHUTE LIGHT. MAINTENANCE REPLACED BATTERY. LIGHT CHECKS GOOD. (M) 2 L 7 2 4F A6WE 2000031500024 20000315 00024 NE 2000 3 15 2000ZZZM65 3 19991118 A 6110 57253 THRUST WASHER DOUG DC6 DC6A 3021706 WP HAMSTD 43E 43E60 NE NR 1 PROPELLER BROKEN A NACA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 AL 03 1027N 43580 SHUTDOWN NR 1 DUE TO VIBRATION OF UNKNOWN ORIGIN, AIRCRAFT RETURNED TO PABE. MAINTENANCE REMOVED PROP FOR FERRY TO PANC . PROP DISASSEMBLED AND FOUND NR 1 BLADE THRUST WASHER BROKEN. (M) 2 L 7 4 4R 6A3 6 C P871 2000031500025 20000315 00025 NE 2000 3 15 HALA9900255 2 19991202 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 FAILED A HALA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 WP 13 699HA 47763 688739 FLT 104 - HNL - NR 2 ENGINE FAILURE ON TAKEOFF. TAKEOFF CANCELLED, RAMP RETURN, NO FURTHER INCIDENTS. NOT AIRBORNE. ( M) 2 L 7 2 4F 4 F RT A6WE E2EA 2000031500026 20000315 00026 2000 3 15 AALA996039 4 19991105 A 2565 D29982107 SLIDE DOUG DC9 DC983 3022083 WP PAX DOOR LOOSE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833RA 53045 SJC - MAIN ENTRY DOOR SLIDE STARTED TO COME OUT OF CASE. REINSTALLED LATCH. (M) 2 L 7 2 4F RT A6WE 2000031500027 20000315 00027 NM 2000 3 15 ASAA9910248 1 19991018 A 3350 LIGHT BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER WAS FOUND INOPERATIVE. REPLACED BATTERY P ACK AND LIGHT ASSEMBLY, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000031500028 20000315 00028 NM 2000 3 15 2000ZZZM66 1 19991018 A 3350 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER WAS FOUND INOPERATIVE. REPLACED BATTERY P ACK AND LIGHT ASSEMBLY, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000031500029 20000315 00029 WP 2000 3 15 AALA996038 1 19991105 A 3350 BR966115 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 823RA 49889 RNO - FIRST THREE ROWS IN FIRST CALSS CABIN OF EMERGENCY PATH LIGHTING INOPERATIVE. REMOVED AND REPLACED FORWARD BATTER Y PACK, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 2000031500030 20000315 00030 NM 2000 3 15 AALA991847 1 19991202 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 21387 TUL - EMERGENCY EXIT LIGHT INOPERATIVE OVERAFT END OF AFT AIRSTAIRS. REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 2000031500031 20000315 00031 NM 2000 3 15 AALA991831 1 19991201 A 3350 LIGHT BOEING 727 727223 1384074 NM BS 804 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 887AA 21526 TUL - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT HAS ONE LAMP INOPERATIVE. REPLACED BOTH LAMPS AND OPS CHECKED EMERGEN CY LIGHTING PER MM 33-50-011-2 PAGE 201. (M) 2 L 7 3 4F A3WE 2000031500032 20000315 00032 NM 2000 3 15 AALA991845 1 19991129 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 21387 TUL - AFT CARGO DOOR EMERGENCY EXIT LIGHT ASSEMBLY HAD WIRE THAT WAS INTERMITTENT RT AFT EXT EMERGENCY LT ON AFT CARGO D OOR HAS 1 LAMP OUT. REPLACED LIGHT ASSEMBLY CPN LIE 5844 MPN 30-0593-1 OPS CHECKED OK, (E583093460. (M) 2 L 7 3 4F A3WE 2000031500033 20000315 00033 NM 2000 3 15 AALA991631 1 19991028 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 876AA 21388 TUL - LEFT AND RIGHT OVERWING EXIT EMERGENCY LIGHT, SHORTED TO GROUND INOP. RESPLICED IN NEW LIGHT ASSY. (M) 2 L 7 3 4F A3WE 2000031500034 20000315 00034 NM 2000 3 15 AALA991615 1 19991020 A 3350 LIGHT BOEING 727 727227 1384078 NM BS 294.5-351-2 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721AA 20729 TUL - LIGHT ASSEMBLY BROKEN. INSTALLED NEW LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 2000031500035 20000315 00035 NM 2000 3 15 AALA991684 1 19991111 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 879AA 21391 TUL - EMERGENCY EXIT AREA LIGHT OVER VENTRAL STAIR INOPERATIVE. INSTALLED SERVICEABLE LIGHT, LIG5714, PER MM 33-50-061- 4, OPS CHECKED OK. (M) 2 L 7 3 4F A3WE 2000031500036 20000315 00036 WP 2000 3 15 AALA991859 1 19991201 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 712-731 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 412AA 49323 TUL - FOUND CORROSION ON FUSELAGE SKIN IN MID CARGO BELLY AREA STATION 712 THROUGH 731 LONGERON L30 THROUGH L29RT. SRM 53-04 FIG 12B AND ESO 80559, DATED 12-2-99 RFS GENERATED RFS 225844. (M) 2 L 7 2 4F A6WE 2000031500037 20000315 00037 NM 2000 3 15 AALA991860 1 19991206 A 5330 SKIN BOEING 727 727223 1384074 NM BS 330 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FOUND DENT IN SKIN. DOUBLER WITH STRINGER SPLICE PER SRM 53-10-3 FIG 3 SHEET 4 AND SRM 53-10-3 FIG 1 SHEET 4 DETA IL II. (M) 2 L 7 3 4F A3WE 2000031500038 20000315 00038 NM 2000 3 15 AALA991861 1 19991201 A 5522 SKIN BOEING 727 727223 1384074 NM ELEVATOR DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FOUND LARGE 3 INCH DENT ON RIGHT ELEVATOR UPPER SURFACE. DYE-CHECKED, NO CRACK FOUND. INSTALLED DOUBLER OVER DEN T PER SRM 55-20-3 PAGE 1-9. (M) 2 L 7 3 4F A3WE 2000031500039 20000315 00039 NM 2000 3 15 AALA991862 1 19991203 A 5312 BULKHEAD BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FOUND CRACK IN BULKHEAD 1183 RBL 25 WL 169. REPAIRED PER CARD 5478 SB 727-53-0215. FASTENERS IN REPAIR ARE INSTA LLED WITH HEADS AFT SB CALLS FOR HEADS FORWARD. (M) 2 L 7 3 4F A3WE 2000031500040 20000315 00040 NM 2000 3 15 AALA991863 1 19991201 A 5532 SKIN BOEING 727 727223 1384074 NM VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - VERTICAL STABILIZER RIGHT SIDE SKIN IS CRACKED .5 INCH AT STABILIZER TO FUSELAGE MATE POINT. STOP DRILLED CRACK V ISUAL AND NDT VERIFIED STOP DRILL OF CRACK. INSTALLED DOUBLER PER BOEING SERVICE BULLETIN 727-55-82. (M) 2 L 7 3 4F A3WE 2000031500041 20000315 00041 NM 2000 3 15 AALA991846 1 19991201 A 5720 ANGLE BOEING 727 727223 1384074 NM WS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 875AA 21387 TUL - RIGHT 760 CHORD ANGLE HFEC INDICATES CRACK BELOW RPR DOUBLER. INSTALLED REPAIR DOUBLER AT STATION 760 RIB CHORD A NGLE IAW SERVICE BULLETIN 727-57-0112, REV 5 AFTER CRACK STOP DRILLED. (M) 2 L 7 3 4F A3WE 2000031500042 20000315 00042 NM 2000 3 15 AALA991864 1 19991206 A 5311 FRAME BOEING 727 727223 1384074 NM BS 783.95 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - STATION 783.95 RIGHT FRAME CRACKED LT BOTTOM INBOARD AFT SIDE RADIUS APPROX RBL 65 AT 6 INCHES BELOW FLOOR CRACK 1 .5 INCH LONG. REPAIRED CRACKED FRAME PER SB 727-53-0197. (M) 2 L 7 3 4F A3WE 2000031500043 20000315 00043 NM 2000 3 15 AALA991865 1 19991206 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 480-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - STRINGER 27L CORRODED FROM 480-500. REPLACED STRINGER SECTION AND INSTALLED REPAIR PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2000031500044 20000315 00044 NM 2000 3 15 AALA991866 1 19991206 A 5330 SKIN BOEING 727 727223 1384074 NM BS 480-510 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - FOUND SKIN CORRODED FROM STATION 480 TO 510 AT STRINGER 27L, FUSE SKIN CRACKED 1 BULGED STATION 500, STRINGER 27L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A. (M) 2 L 7 3 4F A3WE 2000031500045 20000315 00045 NM 2000 3 15 AALA991867 1 19991206 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - FOUND STRINGER 27L CORRODED ON OUTBOARD SIDE FS 580. REMOVED AND REPLACED SECTION OF STRINGER 27L AND INSTALLED S TRINGER SPLICE REPAIR PER 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2000031500046 20000315 00046 NM 2000 3 15 AALA991868 1 19991206 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - FOUND STRINGER 27L HAS CORROSIN ON THE OUTBOARD SIDE FORWARD FS 560 NEAR STRINGER CLIP ATTACH RIVETS. REMOVED AND REPLACED STRINGER 27L SECTION AND INSTALLED REPAIR PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 2000031500047 20000315 00047 NM 2000 3 15 AALA991869 1 19991204 A 5330 SKIN BOEING 727 727223 1384074 NM BS 570-580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - SEVERAL AREAS OF SKIN CORROSION STATION 570-580 AT STRINGER 27L. INSTALLED DOUBLER IAW SRM 53-30-3. (M) 2 L 7 3 4F A3WE 2000031500048 20000315 00048 NM 2000 3 15 AALA991835 1 19991130 A 3350 CONNECTOR BOEING 727 727227 1384078 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 716AA 20608 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS NEAR AFT DOOR INOPERATIVE. RE-SEATED EMERGENCY EXIT PATH LIGHTS CONNECTOR NEAR AFT DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000031700130 20000317 00130 CE 2000 3 17 2000ZZZX655 1 19991223 A 2731 3352402351 SERVO BEECH 90 65A90 1152908 CE ELEVATOR TRIM DAMAGED A IB7A O OTHER E VIBRATION/BUFFET DE DESCENT 1 CE 09 10127 1452 910B91 LJ222 AIRCRAFT REPORTED VIBRATION ON DESCENT. INVESTIGATION FOUND BOLT AND BUSHING MISSING ON RIGHT ELEVATOR TRIM TAB HORN. F URTHER INSPECTION FOUND ELEVATOR ELECTRIC TRIM SERVO BOTTOM BEARING DROPPED DOWN OUT OF THE HOUSING ALLOWING DRUM AND SH AFT TO WOBBLE. THE CABLE WAS TANGLED AROUND THE DRUM. SUBMITTER STATED DO NOT KNOW WHAT OCCURRED FIRST, I.E., SERVO CA USING FLUTTER DESTROYING TAB BOLT AND BUSHINGS OR VICE VERSA. (X) 1 L 7 2 3T 3A20 2000031700137 20000317 00137 NE 2000 3 17 2000ZZZX662 2 19990803 A 7321 FCU UROCOP EC120 EC120B 8680987 EU TMECA ARRIUS ARRIU2F NE ENGINE CONTAMINATED A L HXSA A UNSCHED LANDING K X J FLUID LOSS ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 AL 05 121TH 1003 ENGINE FAILURE RESULTING IN EMERGENCY LANDING. INVESTIGATION REVEALED A PIECE OF BLACK RUBBER APPROXIMATELY 18 BY 8 MI LLIMETERS IN SIZE LODGED IN THE EJECTOR PUMP ORIFICE OF THE FUEL SYSTEM LOW PRESSURE UNIT. THIS CAUSED THE HIGH PRESSUR E FUEL PUMP, INSIDE THE FUEL CONTROL UNIT TO SHUT DOWN, RESULTING IN COMPLETE POWER LOSS. TEMSCO HELICOPTERS BELIEVES T HE RUBBER PARTICLE WAS A RESULT OF MANUFACTURE ASSEMBLY. TEMSCO RECOMMENDS THE MANUFACTURER INSTALL AN AIRFRAME MOUNTED FUEL FILTER UPSTREAM OF THE LOW PRESSURE UNIT. CURRENTLY, THE LOW PRESSURE UNIT/EJECTOR PUMP IS NOT PROTECTED BY THE E XISTING FUEL FILTER. (X) 1 G 7 2 3U 3 U NC R0001RD E34NE 2000031700138 20000317 00138 NE 2000 3 17 2000ZZZX663 2 19990106 A 7322 0292928150 FUM SNIAS AS350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B NE ENGINE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 104LN 449 253B 3134 22057 UNIT INOPERATIVE. RED GOVERNOR LIGHT CAME ON AFTER FLIGHT. DISPLAY SYSTEM DID NOT SHOW DEFECT WITH BATTERY POWER OR GR OUND RUN (ONLY OCCURS AFTER FLIGHT). FADAC DATA: FAIL 1 0000, FAIL 2 0200, FAULT DIAG. NR 17. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X) 1 G 7 1 3U 3 U NC H9EU E00054EN 2000032100001 20000413 00001 NM 2000 4 13 AALA991717 1 19991115 A 3397 WIRE BOEING 767 767323 1385205 NM SEAT 23 FAILED A K NONE L NO TEST IN INSP/MAINT 1 SW 07 397AN 29604 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 23HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY E XIT SEAT LIGHT AT SEAT 23HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 2000032100002 20000321 00002 NM 2000 3 21 AALA991736 1 19991116 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 677AN 29427 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH FLOOR LIGHT JUMPER WIRE BETEEN COFFEE BAR AND MAIN CABIN INOPERA TIVE. REPLACED EMERGENCY EXIT PATH FLOOR LIGHT JUMPER WIRE. SYSTEM GROUND CHECK, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 2000032100003 20000321 00003 EA 2000 3 21 A6W9900125 1 19991129 A 2421 GENERATOR CNDAIR CL600 CL6002B19 EA NR 1 FAILED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 403AW 7288 NR 1 GENERATOR FAILS IN-FLIGHT. DURING TROUBLESHOOTING OF NR 1 GENERATOR, MAINTENANCE FOUND EVIDENCE THAT TERMINAL BLOC K GB209 (ENGINE TO AIRFRAME) AND WIRE NR 2XA73A4ORN WERE BURNT. NR 1 GENERATOR PLACED ON MEL AND ISOLATED THE DAMAGED T ERMINAL BLOCK AND WIRE. (ATW). (X) 2 L 7 2 4F RT A21EA 2000032100004 20000321 00004 EA 2000 3 21 ASOA99157 1 19991122 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 834AS 2980 7254 DURING INSPECTION, FOUND NR 2 AND NR 4 EMERGENCY BATTERY PACKS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 AND N R 4 EMERGENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 2000032100005 20000321 00005 SO 2000 3 21 C2XA99CL126 1 19991212 A 2740 3621001007 CONTROLLER EMB 135 EMB135ER 3260203 SO HORIZ STABILIZER FAILED A C2XA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 09 19503 477 1233 145176 MDW - FLT 3908 - AFTER TAKEOFF WITH PITCH TRIM SET AT 6 DEGREES NOSE-UP HAD NO CONTROL OF PITCH TRIM FROM CAPTAINS OR BA CK-UP STATIONS. AIRCRAFT RETURNED TO MDW WITH NO FURTHER INCIDENT ON CMC HORIZONTAL STABILIZER CONTROL UNIT FAIL AND CO NTROL WHEEL TRIM SWITCH FAULT WERE DISPLAYED. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW E MB 135 MM 27-40-01. OPERATIONAL CHECKS WERE GOOD IAW EMB 135 MM 27-40-00. MAINTENANCE ALSO REMOVED AND REPLACED CAPTAI N'S TRIM WHEEL SWITCH FOR PRECAUTIONARY REASONS. OPERATIONAL CHECKS WERE GOOD IAW EMB 135 MM 27-40-00. AIRCRAFT WAS TE ST FLOWN WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 2000032100006 20000321 00006 WP 2000 3 21 GTIA99001223 1 19991211 A 2150 DUCT DOUG DC9 DC981 3022081 WP LT PACK LOOSE A GTIA G O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 GL 23 806NK 48051 PBI - FLT 350 - P556 - JUST PRIOR TO STARTING TO DESCEND OUT OF FL 350, CABIN ALTITUDE STARTED CLIMBING. COULD NOT CONT ROL PRESSURIZATION. STARTED RAPID DESCENT, MASKS DEPLOYED AT 14,000 FEET CABIN ALTITUDE. P 557 - LT A/C VALVE INOPERAB LE IN AUTO AND MANUAL. REF ITEM P557 - SECURED DUCT LT PACK. NO OTHER DEFECTS NOTED. REF MM 21-00-00-501 CABIN PRESSU RIZATION CHECKED GOOD. P557 - FOUND DUCT BLOWN OFF LT PACK WATER SEPARATE SECURED DUCT. LEAK CHECK DUCT. OPS CHECKED LT PACK REF MM 21-20-00 A501. (X) 2 L 7 2 4F A6WE 2000032100007 20000321 00007 WP 2000 3 21 GTIA99001245 1 19991229 A 3350 LENS DOUG DC9 DC981 3022081 WP CABIN MISSING A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 806NK 48051 DTW - FLT 372 - M 460 - OVERWING EXIT FLOOR TRACK LIGHT LENS MISSING (FAA). M 461 - MISING LIFE VEST PLACARDS IN FRONT OF SEATS 1D, E, F. (FAA). M 460 - REPLACED MISSING FLOOR TRACK LIGHT LENS. IAW MD-80 MM CHAP 33-53-01. M 461 - REPLA CED MISSING LIFE VEST PLACARDS IN FRONT SEATS 1, D, E, F. IAW MD-80 MM CHAP 11-41-00. (X) 2 L 7 2 4F A6WE 2000032100009 20000321 00009 WP 2000 3 21 GTIA0000004 1 19991231 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 808NK 49504 EWR - FLT 447 - EMERGENCY TRACK FLOOR LIGHTING IS OUT IN BACK. RECONNECTED EMERGENCY TRACK RED LIGHT. OPS CHECK OK. ( X) 2 L 7 2 4F RT A6WE 2000032100010 20000321 00010 WP 2000 3 21 GTIA99001217 1 19991207 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 808NK 49504 DTW - AISLE PATH LIGHTING IN REAR OF AIRCRAFT IS COMING OFF THE FLOOR. REMOVED AND REPLACED CRACKED SECTIONS OF AISLE E MERGENCY LIGHT PATH AND TRIM IAW MD-80 MM 25-20-00. EMERGENCY LIGHTING FUNCTION NORMAL. (X) 2 L 7 2 4F RT A6WE 2000032100011 20000321 00011 2000 3 21 GTIA99001244 4 19991223 A 2561 ROLLER DOUG DC9 DC983 3022083 WP CABINET LACK OF LUBE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 809NK 49503 ISP - FLT 755 - LIFE JACKET STORAGE CONTAINER WILL NOT OPEN. LUBED ROLLER ON CABINET. OPERATES NORMALLY. (X) 2 L 7 2 4F RT A6WE 2000032100012 20000321 00012 SO 2000 3 21 2000ZZZX665 1 19991216 A 3241 426871 ECC EMB 120 EMB120RT SO BRAKE INOPERATIVE A GLBA O OTHER O OTHER LD LANDING 1 CE 01 108UX 120108 DURING LANDING, THE POWER LEVERS WOULD NOT GO INTO REVERSE PITCH. WHEN THE BRAKES WERE APPLIED, THEY LOCKED UP. THE AN TI-SKID ELECTRONIC CONTROL UNIT AND BOTH MAIN LANDING GEAR AIR/GROUND PROXIMITY SWITCHES, PN 20505, WERE REPLACED. (X) 2 L 7 2 4T RT A31SO 2000032100014 20000321 00014 EA 2000 3 21 MASA99160 1 19991003 A 7830 CF343A1 WARNING LIGHT GE CF34 CNDAIR CL600 CL6002B19 EA RIGHT ENGINE ILLUMINATED A MASA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 27318 87252 7318 MDW/CHM - FLT 5080 - DURING CRUISE ALTITUDE, THE RIGHT THRUST REVERSER UNLOCK MESSAGE ILLUMINATED AT AN ALTITUDE OF 23,0 00 FEET OVER FWA. THE CREW DECLARED AN EMERGENCY AND C/W THE DFM CHECK LIST AND DIVERTED TO DAY. THE AIRCRAFT LANDED I N DAY WITH NO INCIDENT AND THERE WAS NO EVIDENCE OF THE THRUST REVERSER DEPLOYING IN-FLIGHT. (X) 2 L 7 2 4F RT A21EA 2000032100015 20000321 00015 EA 2000 3 21 MASA99178 1 19991123 A 5210 H341425 LATCH 601R319003 CNDAIR CL600 CL6002B19 EA PASSENGER DOR MALFUNCTIONED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 17275 7275 SBA/LAS - FLT 5160 - AFTER TAKEOFF, THE CREW NOTED THE MAIN CABIN DOOR HANDLE POPPED OUT. THE CREW RETURNED TO THE FIEL D. MAINTENANCE GROUND CHECKED THE DOOR CLOSING MECHANISM AND PRESSURIZED THE AIRCRAFT AND CHECKED THE DOOR LOCKS. NO D ISCREPANCIES WERE NOTED, OPS CHECKED GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 2000032100016 20000321 00016 CE 2000 3 21 2000ZZZX666 1 19991014 A 5610 WINDSHIELD BEECH 200 B200 1152922 CE COCKPIT CRACKED A OCXA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 55PC BB1170 BTV/RDU - FLT 260 - EN ROUTE, THE INSIDE GLASS LAYER OF THE PILOT'S WINDSHIELD CRACKED. OUTSIDE LAYER REMAINED INTACT. NO CHANGE IN CABIN PRESSURE. IMMEDIATELY DESCENDED AND DIVERTED TO POU WHERE PILOT'S WINDSCREEN WAS REPLACED. 1 L 7 2 4T A24CE 2000032100017 20000321 00017 SO 2000 3 21 SIMA993231 1 19991119 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 621AE 05777 145105 STL - FLT 4123 - BAGGAGE SMOKE WARNING INDICATION ACTIVATED. FIRE EXTINGUISHER DISCHARGED. DIVERTED TO STL. INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE. MEL'D SYSTEM AND FLIGHT CONTINUED TO XNA. ON 11-20-99, REMOVED AND REPLACED N R 1 BAGGAGE SMOKE DETECTOR. MEL RESTORED AND AIRCRAFT WAS AGAIN RETURNED TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 2000032100019 20000321 00019 NM 2000 3 21 GAIA99241 1 19991220 A 5311 FRAME BOEING 727 727222 1384073 NM BS 780.9 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). DURING A BHEC INSPECTION, FOUND TWO EACH HOLES CRACKED ON BBL 70.5 AT BS 780.95, LEFT SIDE. REPAIRED RIP CORD IAW BOEING SB 57- 0112 AND REO W00003. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100020 20000321 00020 NM 2000 3 21 GAIA99242 1 19991220 A 5311 FRAME BOEING 727 727222 1384073 NM BS 760.9 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). DURING A BHEC INSPECTION, FOUND THREE EACH HOLES CRACKED ON BBL 70.5 AT BS 760.95 RIGHT SIDE. REPAIRED RIP CORD IAW BOEING SB 57-0112 AND REO W0002. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100021 20000321 00021 NM 2000 3 21 GAIA99243 1 19991220 A 5330 SKIN BOEING 727 727222 1384073 NM BS 660 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINDSTO/SALEM, NC). ONE EAC H SMALL GOUGE ON MCD CUT OUT, AFT DOUBLER BS 660, STR S12L. REPAIRED GOUGE IAW RFTS N180AX-13-20563 AND 8110-3, DATED 1 1-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100022 20000321 00022 NM 2000 3 21 GAIA99244 1 19991220 A 5330 SKIN BOEING 727 727222 1384073 NM BS 650 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). SIX INC H GOUGE ON MCD CUT OUT, AFT DOUBLER BS 650, STR S13L TO STR S15L. REPAIRED GOUGE IAW RFTS N180AX-18-20564 AND 8110-3, D ATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100023 20000321 00023 NM 2000 3 21 GAIA99245 1 19991220 A 5330 SKIN BOEING 727 727222 1384073 NM BS 650 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). GOUGE O N AFT EDGE OF SKIN, AFT SIDE OF MCD CUT OUT BETWEEN STR S7L AND STR S8L. REPAIRED GOUGE IAW RFTS N180AX-14-20563 AND 81 10-3, DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100024 20000321 00024 NM 2000 3 21 GAIA99246 1 19991220 A 5320 STRAP BOEING 727 727222 1384073 NM BS 650 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND 1 3 DRILL MARKS ON MCD CUT OUT INTERNAL DOUBLER EXTENDING THROUGH GILLINER STRAP HOLES FROM BS 660 TO BS 670, STR S4L TO S TR S7L. REPAIRED DRILL START MARKS ON MCD INTERNAL DOUBLER STRAP IAW RFTS N180AX-11-20568 AND N180AX-38-21961 AND 8110- 3, DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100025 20000321 00025 NM 2000 3 21 GAIA99247 1 19991220 A 5320 STRAP BOEING 727 727222 1384073 NM BS 470 TO 500 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND 2 0 DRILL MARKS ON MCD CUT OUT FORWARD END OF INTERNAL DOUBLER PROTRUDING THROUGH GILLINER STRAP BS 470 TO BS 500, STR S4 L TO STR S12L. REPAIRED DRILL START MARKS ON MCD INTERNAL DOUBLER STRAP IAW RFTS N180AX-10-20569 AND 8110 3, DATED 11-1 -99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100026 20000321 00026 NM 2000 3 21 GAIA99248 1 19991220 A 5751 SKIN BOEING 727 727222 1384073 NM AILERON GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND R IGHT WING, INBOARD AILERON, UPPER FIXED LEADING EDGE GOUGED AND CHAFED. REPAIRED IAW BOEING SRM 51-40-5. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100027 20000321 00027 NM 2000 3 21 GAIA99249 1 19991220 A 5311 FRAME BOEING 727 727222 1384073 NM BS 930 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND F RAME AT STA 930, STR S14L CRACKED. REPAIRED IAW BOEING SRM CHAPTERS 51 AND 53. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100028 20000321 00028 NM 2000 3 21 GAIA99250 1 19991220 A 5320 STRAP BOEING 727 727222 1384073 NM BS 380 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND M AIN CARGO 9G BARRIER SAFETY STRAP AT STA 380 AND STR S6R HAS THREE EACH DOUBLE DRILLED HOLES. REPAIRED IAW BOEING SRM C HAPTERS 51 AND 53. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100029 20000321 00029 NM 2000 3 21 GAIA99251 1 19991220 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 440 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND A T STA 440, FLOOR FRAME AT RBL 12 HAS CORROSION. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW RFTS N180AX-19-20760. AI RCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100030 20000321 00030 NM 2000 3 21 GAIA99252 1 19991220 A 5210 TORQUE BOX BOEING 727 727222 1384073 NM PASSENGER DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND A T L-1 DOOR, FORWARD TORQUE BOX UPPER DOOR HINGE CUT OUT CRACKED. REMOVED AND REPLACED TORQUE BOX IAW BOEING SRM CHAPTER 51. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100031 20000321 00031 NM 2000 3 21 GAIA99253 1 19991220 A 5330 SKIN BOEING 727 727222 1384073 NM BS 1263 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND G OUGE ON FUSELAGE SKIN AT BS 1263, 35 INCHES ABOVE NR 3 PYLON. INSTALLED REPAIR DOUBLER IAW BOEING SRM CHAPTERS 51 AND 5 3. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100032 20000321 00032 NM 2000 3 21 GAIA99254 1 19991220 A 5713 STRINGER BOEING 727 727222 1384073 NM WS 656.5 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND C RACK EXTENDING OUT FROM PREVIOUS REPAIR AT WS 656, UPPER STR 9, RIGHT WING. RIGHT WING UPPER STR 9 RIGHT REPAIR AT WS 5 65.5 WAS REPAIRED IAW REO W00005 AND BOEING SB 727-57A159. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100033 20000321 00033 NM 2000 3 21 GAIA99255 1 19991220 A 5320 WEB BOEING 727 727222 1384073 NM BS 653 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND M CD LOWER AFT CORNER WEB AND INTERNAL WEB GOUGED. REPAIRED MCD LOWER AFT CORNER WEB AND INTERNAL WEB AT STA 656 LBL 66 I AW RFTS N180AX-38-21961 AND 8110-3, DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100034 20000321 00034 NM 2000 3 21 GAIA99256 1 19991220 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 500 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND O NE EACH DOUBLE DRILLED HOLE ON FLOORBEAM CAP AT STA 500, LBL 60, WL 208. C/W REPAIR IAW RFTS 180AX-36-22018, AND 8110-3 , DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100035 20000321 00035 NM 2000 3 21 GAIA99257 1 19991220 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 480 LBL 64 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND O NE EACH DOUBLE DRILLED HOLE ON FLOORBEAM CAP AT STA 480, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22032, AND 8110-3, DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100036 20000321 00036 NM 2000 3 21 GAIA99258 1 19991220 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 460 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND O NE EACH DOUBLE DRILLED HOLE ON FLOOR BEAM CAP AT STA 460, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22033, AND 8110-3, DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100037 20000321 00037 NM 2000 3 21 GAIA99259 1 19991220 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 440 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND O NE EACH DOUBLE DRILLED HOLE ON FLOORBEAM CAP AT STA 440, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22034, AND 8110-3, DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100038 20000321 00038 NM 2000 3 21 GAIA99260 1 19991220 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 380 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND O NE EACH DOUBLE DRILLED HOLE ON FLOORBEAM CAP AT STA 380, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22035, AND 8110-3, DATED 11-1-99. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100039 20000321 00039 NM 2000 3 21 GAIA99261 1 19991220 A 5320 FITTING BOEING 727 727222 1384073 NM BS 940 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND STA 940 FITTING MISDRILLED. REPLACED STA 940 FITTING IAW BOEING SB 727-53-0018 AND BOEING DRAWING 65C15732. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100040 20000321 00040 NM 2000 3 21 GAIA99262 1 19991220 A 5320 FITTING BOEING 727 727222 1384073 NM BS 870 GOUGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). UPON REMO VAL OF LT WING AFT BOTTLE BOLT BUSHING, FOUND INNER RACE GOUGED. REPAIRED GOUGE IAW REO W00008 AND 8110-3, DATED 12-2-9 9. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100041 20000321 00041 NM 2000 3 21 GAIA99263 1 19991220 A 5313 STRINGER BOEING 727 727222 1384073 NM BS 990 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND COR ROSION ON STR S20R, STA 990. REMOVED AND REPLACED STR S20R, STA 990 IAW BOEING SRM. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100042 20000321 00042 NM 2000 3 21 GAIA99264 1 19991220 A 5315 FLOORBEAM BOEING 727 727222 1384073 NM BS 400 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND FLO ORBEAM AT STA 400, BL 44 HAS DOUBLE DRILLED HOLES. REPAIRED IAW ATA EDR 99-008 AND BOEING SRM. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100043 20000321 00043 NM 2000 3 21 GAIA99266 1 19991220 A 5320 STRAP BOEING 727 727222 1384073 NM CARGO BAY DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND 9G BUYLKHEAD SAFETY STRAP DRILLED INTO STR 2-3L. REAPIRED IAW ATS EDR 99-002 AND BOEING SRM. AIRCRAFT WAS RETURNED TO SER VICE. (X) 2 L 7 3 4F A3WE 2000032100044 20000321 00044 NE 2000 3 21 GAIA99267 2 19991220 A 7220 CASE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND FIB ERGLASS PATCH DETERIORATED AND PEELING AT THE 12 O'CLOCK POSITION BETWEEN IGV HEAT VALVES AND SIX INCHES AFT ON OUTER CA SE OF NR 3 ENGINE. REPAIRED IAW AIA EA B2-72-031 AND 8110-3, DATED 12-17-99. AIRCRAFT WAS RETURNED TO SERIVCE. (X) 2 L 7 3 4F 4 F A3WE E2EA 2000032100045 20000321 00045 NM 2000 3 21 GAIA99240 1 19991220 A 5313 STRINGER BOEING 727 727222 1384073 NM BS 945 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). STRINGER S18L IS CRACKED AT STA 945. REPAIRED IAW BOEING SB 52-0118 AND BAC DRAWING 65C29069. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100046 20000321 00046 NM 2000 3 21 GAIA99239 1 19991220 A 5320 BEAM BOEING 727 727222 1384073 NM BS 1183 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 180AX 20041 'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). 1183 BULK HEAD CRACKED AT 182, LBL 8 EXTENDING FROM LOWER FASTENER OF VERTICAL BEAM. INSTALLED REPAIR IAW 727 SB 53-0175. AIRCRAF T WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 2000032100047 20000321 00047 WP 2000 3 21 2000ZZZX667 1 19990824 A 5320 PLATE DOUG DC8 DC8F55 3021928 WP BS 510 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 MAIN CARGO DOOR AFT JAM BOX FRAME FORWARD EDGECRACK, BENT AND GOUGED, STA 510L, L7L - L21L. STOP DRILLED CRACK, NDT TO ASSURE CRACK HAD STOPPED. IT IS ACCEPTABLE TO RETURN TO SERVICE. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100048 20000321 00048 WP 2000 3 21 2000ZZZX668 1 19990820 A 2710 ARM DOUG DC8 DC8F55 3021928 WP AILERON CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 PERFORMED POST-REMOVAL INSPECTION OF AILERON REVERSION MECHANISM AND SUPPORT LT SIDE DAMAGE DURING REMOVAL. REMOVED AND REPLACED AILERON REVERSION CONTROL SUPPORTS (LT FOUND CRACKED) IAW DC-8 SRM 51-3-4 AND EO NR 99-136 WITH APPROVED 8110- 3 DATED 11-1-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100049 20000321 00049 WP 2000 3 21 2000ZZZX669 1 19991021 A 7830 RING DOUG DC8 DC8F55 3021928 WP WIND SOCK MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 FOUND DURING C-CHECK. DOUBLER AROUND CIRCUMFERENCE OF FORWARD SIDE OF WIND SOCK HAS SECTION MISSING. NR 4 ENGINE. FAB RICATED NEW SECTION, WELDED IN PLACE NDT WELD (NO FLAWS) PER EO NR 99-136 WITH APPROVED 8110-3 DATED 10-19-99. REF: Z ANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100050 20000321 00050 WP 2000 3 21 2000ZZZX670 1 19991104 A 5720 56455382 TEE DOUG DC8 DC8F55 3021928 WP WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 THROUGH ACCESS HOLE 506C AND THROUGH INBOARD RIB CUT-OUT, INBOARD LOWER WING STR 63-72 AT STA XW.000 IN NR 3 MAIN TANK H AS CORROSION BETWEEN STRINGER. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND T-CHORD OUT OF LIMITS IAW DC-8 SRM 57-2-0. REPLACED T-CHORD IAW DC-8 SRM'S 51-1-21 AND 51-1-20, AND 51-3-0. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. ( X) 2 L 7 4 4F 4A25 2000032100051 20000321 00051 WP 2000 3 21 2000ZZZX671 1 19991108 A 5711 SPAR DOUG DC8 DC8F55 3021928 WP WS 39 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LOWER FRONT SPAR 1.50 INCH CRACK FS 680 LBL 34 INCHES Z AXIS -47 AND .50 INCH CRACK BS 680 LBL XCW 39 INCHES AND XCW 43 INCHES Z AXIS -47 INCH. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30-R5. REF: ZAN TOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100052 20000321 00052 WP 2000 3 21 2000ZZZX672 1 19990923 A 5552 FITTING DOUG DC8 DC8F55 3021928 WP ELEVATOR CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 RIGHT ELEVATOR NR 2 A-FRAME CRACKED. REMOVED AND REPLACED NR 2 POSITION A-FRAME RT ELEVATOR IAW DC-8 OHM 27-30-1. (X) 2 L 7 4 4F 4A25 2000032100053 20000321 00053 WP 2000 3 21 2000ZZZX673 1 19990914 A 5313 LONGERON DOUG DC8 DC8F55 3021928 WP BS 320 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LONGERON 30, 31 RIGHT AT STA 320 HAD CORROSION. REMOVED CORROSION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99 -136 WITH APPROVED 8110-3 DATED 9-1-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100054 20000321 00054 WP 2000 3 21 2000ZZZX674 1 19990826 A 5730 SKIN DOUG DC8 DC8F55 3021928 WP WS 291.5 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LEFT WING CENTER L/E OTBD EDGE XFS 291.500 FWD VERTICAL PLATE CRACKED APPROXIMATELY 3 INCHES. REMOVED OUTBOARD END WEB. FABRICATED NEW SECTION AND SPLICE PLATE AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-20-99. REF: ZANTO P INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100055 20000321 00055 WP 2000 3 21 2000ZZZX675 1 19991111 A 5730 SKIN DOUG DC8 DC8F55 3021928 WP WS 214.25 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 FOUND DURING C-CHECK. CRACK LOCATED AT INBOARD SLOT LOWER L/E, 1.50 INCHES LONG ON RT WING XFS 214.25. NDT CRACK TO AS SURE THAT CRACK HAD BEEN STOPPED. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11 -11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100056 20000321 00056 WP 2000 3 21 2000ZZZX676 1 19991111 A 5730 SKIN DOUG DC8 DC8F55 3021928 WP WS 213.5 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 DURING C-CHECK, FOUND .50 INCH LOWER L/E SURFACE AT INBOARD SLOT APPROXIMATELY XFS 213.5 LT WING. NDT TO ASSURE CRACK H AD BEEN STOPPED. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-11-99. REF: Z ANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100057 20000321 00057 WP 2000 3 21 2000ZZZX677 1 19991102 A 5751 SKIN DOUG DC8 DC8F55 3021928 WP AILERON CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 INBOARD AILERON L/E PLATING AT STA XA 503.5 HAS A 2.5 INCH CRACK (EO). ROUTED OUT CRACK. FABRICATED DOUBLER AND INSTAL LED PER EO 99-136 WITH APPROVED 8110-3 DATED 10-28-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100058 20000321 00058 WP 2000 3 21 2000ZZZX678 1 19990927 A 5753 SKIN DOUG DC8 DC8F55 3021928 WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LEFT WING OUTBOARD FLAP SKIN JUST BELOW HINGE FITTING IS CRACKED STA XR 219. STOP DRILLED CRACKS, NDT TO ASSURE CRACKS HAD BEEN STOPPED. FABRICATED DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 9-15-99. REF: ZANTOP IN TERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100059 20000321 00059 WP 2000 3 21 2000ZZZX679 1 19991105 A 5280 SKIN DOUG DC8 DC8F55 3021928 WP RT MLG DOOR DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 RT MLG DOOR CENTER STRUT/SEVERAL SCREWS STARTING TO PULL THROUGH SKIN. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100060 20000321 00060 WP 2000 3 21 2000ZZZX680 1 19991105 A 5350 FAIRING DOUG DC8 DC8F55 3021928 WP FUSELAGE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 PANEL 161V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100061 20000321 00061 WP 2000 3 21 2000ZZZX681 1 19991105 A 5350 FAIRING DOUG DC8 DC8F55 3021928 WP FUSELAGE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 PANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 81 10-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100062 20000321 00062 WP 2000 3 21 2000ZZZX682 1 19991102 A 5751 FITTING DOUG DC8 DC8F55 3021928 WP AILERON CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 PANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 81 10-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100063 20000321 00063 WP 2000 3 21 2000ZZZX683 1 19990915 A 5243 LEG DOUG DC8 DC8F55 3021928 WP LT MLG WW BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LEFT MAIN W/W SAFETY NET LEG BROKEN OFF. WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 9-10-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100064 20000321 00064 WP 2000 3 21 2000ZZZX684 1 19991117 A 5250 DOOR DOUG DC8 DC8F55 3021928 WP COCKPIT DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 REPLACED COCKPIT DOOR. FABRICATED NEW COCKPIT DOOR PER EO 99-136 WITH APPROVED 8110-3 DATED 8-3-99. REF: ZANTOP INTER NATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100065 20000321 00065 WP 2000 3 21 2000ZZZX685 1 19990830 A 5754 PANEL DOUG DC8 DC8F55 3021928 WP LE FLAP CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 OUTBOARD SLOT LEFT WING L/E HAS AREA OF EXFOLIATION XW 454. CUT OUT AREA OF EXFOLIATION. FABRICATED FILLER, DOUBLER, AN D INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-13-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100066 20000321 00066 WP 2000 3 21 2000ZZZX686 1 19990910 A 5754 PANEL DOUG DC8 DC8F55 3021928 WP LE FLAP CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LEFT OUTBOARD MOST UPPER SLOT DOOR BOTTOM INBOARD OF INBOARD ADJ SCREW HAS CORROSION XS 503.789. BLENDED OUT CORROSION, TREATED AND PRIMED. MAXIMUM UNDER CUT IN RIB IS DOWN .078 INCHES. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 8-27-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032100067 20000321 00067 2000 3 21 2000ZZZX687 2 19991005 A 7520 577246423 PIPE DOUG DC8 DC8F55 3021928 WP NR 3 CHAFED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 FOUND DURING C-CHECK. NR 3 PYLON VENTILATION PIPE CHAFED. FABRICATED DOUBLERS AND WELDED IN PLACE IAW BOEING MESSAGE M -7200-99-07969 WITH APPROVED 8110-3 DATED 10-22-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200001 20000322 00001 WP 2000 3 22 2000ZZZX688 1 19991102 A 2550 GILLINER DOUG DC8 DC8F55 3021928 WP CABIN DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 REPLACED MAIN CABIN GILLINER AND STRAPS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 7-24-99. REF: ZANTOP INTERNAL AIRL INES, INC. ZIAA. 2 L 7 4 4F 4A25 2000032200002 20000322 00002 WP 2000 3 22 2000ZZZX689 1 19991014 A 5311 FRAME DOUG DC8 DC8F55 3021928 WP BS 460 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 FUSELAGE STATION 460 LONGERON 21R FRAME BENT AND FRAME CAP CRACKED. REMOVED DAMAGED SECTION OF FRAME. FABRICATED FRAME SPLICES IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW DC-8 SRM 51-1-20D. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200003 20000322 00003 WP 2000 3 22 2000ZZZX690 1 19991118 A 2752 56422051 FITTING DOUG DC8 DC8F55 3021928 WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LEFT HAND STA 98 FLAP ACTUATOR ATTACH FITTING (INSIDE PANEL 562L) HAS APPROXIMATELY 1 INCH CRACK IN IT. REMOVED AND REP LACED FITTING IAW DC-8 SRM'S 57-3-0, 51-3-2, AND 51-1-20D. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200004 20000322 00004 WP 2000 3 22 2000ZZZX691 1 19990916 A 5313 LONGERON DOUG DC8 DC8F55 3021928 WP BS 1490-1600 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AN D REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60 PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200005 20000322 00005 WP 2000 3 22 2000ZZZX692 1 19990915 A 7830 RING DOUG DC8 DC8F55 3021928 WP NR 4 ENGINE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AN D REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60 PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200006 20000322 00006 WP 2000 3 22 2000ZZZX693 1 19990823 A 5552 FITTING DOUG DC8 DC8F55 3021928 WP ELEVATOR GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 NR 4 RIGHT ELEVATOR A-FRAME AFT MOUNT GOUGED. GOUGE IS A MAXIMUM OF .091 INCH DEEP. BLENDED GOUGE SMOOTH. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8-20-99. REF: ZANTOP INTER NATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200007 20000322 00007 WP 2000 3 22 2000ZZZX694 1 19991108 A 5711 SPAR DOUG DC8 DC8F55 3021928 WP BS 680 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LOWER FRONT SPAR HORIZONTAL LEG 10 INCH CRACK BS 680 - 26.5 INCHES TO 36.50 INCHES RBL CENTER WING TANK. CUT OUT DAMAGE . FABRICATED FILLER, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30R5. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X ) 2 L 7 4 4F 4A25 2000032200008 20000322 00008 WP 2000 3 22 2000ZZZX695 1 19991029 A 5711 SPAR DOUG DC8 DC8F55 3021928 WP WS 31.04 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 FOUND DURING C-CHECK. A 4.75 INCH CORROSION CRACK APPROXIMATE STA XCW 31.0 LT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. R OUTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK, REMOVED. TREATED AND PRIMED. FILLED SEALER, CONTINUED THE INSTALLATION OF LOWER FRONT SPAR CAP. REPAIRED PER 57-2-6 PER EO 99-136 WITH APROVED 8110-3 DATED 10-18-99. REF: ZANTOP INTERNATIO NAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200009 20000322 00009 WP 2000 3 22 2000ZZZX696 1 19991014 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 1400 MISREPAIRED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LEFT HAND AFT ENTRY DOOR FUSELAGE SKIN CUT-OUT, PREVIOUS REPAIR IMPROPER STA 1400 - L21L. REMOVED EXISTING DOUBLER. FA BRICATED NEW DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-4-99. REF: ZANTOP INTERNATIONAL AIRLINES , INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200010 20000322 00010 WP 2000 3 22 2000ZZZX697 1 19991116 A 5321 FLOOR PANEL DOUG DC8 DC8F55 3021928 WP BS 280-1490 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 812TC 55626 45764 CORROSION EXISTS ON THE SURFACE OF ALL FLOOR PLANKS FROM STA 280 TO STA 1490 L21L TO L21R. REMOVED CORROSION BY CHEMICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. R EF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200011 20000322 00011 WP 2000 3 22 2000ZZZX698 1 19990823 A 5552 FITTING DOUG DC8 DC8F55 3021928 WP ELEVATOR GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 NR 1 RT ELEVATOR A-FRAME TRAILING EDGE BOLT HOLE BOSS GOUGED. BLENDED GOUGE SMOOTH. TREATED AND PRIMED. ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATD 8-19-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. ( X) 2 L 7 4 4F 4A25 2000032200012 20000322 00012 WP 2000 3 22 2000ZZZX699 1 19991006 A 7130 HEAT SHIELD DOUG DC8 DC8F55 3021928 WP NR 1 ENGINE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 NR 1 ENGINE HEAT SHIELD FOR MAIN FUEL LINE CRACKED. STOP DRILLED CRACK, NDT TO ASSURE CRACK HAD BEEN STOPPED. WELDED ACCORDING TO MIL-STD-2219. NDT WELD NO FLAWS PER EO 99-136 WITH APPROVED 8110-3 DATED 8-25-99. REF: ZANTOP INTERNATI ONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200013 20000322 00013 NE 2000 3 22 2000ZZZX700 2 19990915 A 7220 SPINNER DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D1 52039 NE NR 4 ENGINE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 NOSE COWL CRACKED AT 6:00 O'CLOCK POSITION NR 4 ENGINE. CUT OUT PREVIOUS WELD, NDT TO ASSURE ALL CRACKS STOPPED. FABR ICATED PLUG AND WELDED IN PLACE. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 8-31-99. REF: ZANTO P INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4 F 4A25 1E8 2000032200014 20000322 00014 WP 2000 3 22 2000ZZZX701 1 19990909 A 7160 RIVET DOUG DC8 DC8F55 3021928 WP INTAKE SHEARED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 NR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR OIL COOLER. IT IS ACCEPTABLE TO USE AS IS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200015 20000322 00015 WP 2000 3 22 2000ZZZX702 1 19991009 A 7160 RIVET DOUG DC8 DC8F55 3021928 WP INTAKE SHEARED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 NR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR PNEUMATIC HEAT EXCHANGER. IT IS ACCEPTABLE TO USE AS IS, IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200016 20000322 00016 WP 2000 3 22 2000ZZZX703 1 19991028 A 5414 SKIN DOUG DC8 DC8F55 3021928 WP NR 3 NACELLE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 AFT LEFT COWL DOOR HAS 3 INCH CRACK OUTSIDE SKIN AT INLET SCOOP NR 3 ENGINE. STOP DRILLED, NDT CONFIRMED CRACK HAS BEEN STOPPED. WELDED CRACK AND NDT NO FLAWS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATE D 9-8-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200017 20000322 00017 WP 2000 3 22 2000ZZZX704 1 19991019 A 2612 DUCT DOUG DC8 DC8F55 3021928 WP NR 2 ENGINE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 NR 2 ENGINE INBOARD SIDE 1 O'CLOCK POSITION. FIRE EXTINGUISHER DUCT CRACKED AT ATTACH ANGLE. REMOVED DUCT, REPAIRED PE R BOEING MEMO 99-00006 H AND EO 99-136 WITH APPROVED 8110-3 DATED 8-23-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., Z IAA. (X) 2 L 7 4 4F 4A25 2000032200018 20000322 00018 WP 2000 3 22 2000ZZZX705 1 19990819 A 5320 ANGLE DOUG DC8 DC8F55 3021928 WP BS 683 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 FUSELAGE STATION 684R L31R FILLET SUPPORT ANGLE CRACKED. REMOVED AND FABRICATED ANGLE IAW DC-8 SRM 51-1-4. INSTALLED P ER EO 99-136 WITH APPROVED 8110-3 DATED 8-24-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200019 20000322 00019 WP 2000 3 22 2000ZZZX706 1 19990908 A 2133 OUTFLOW VALVE DOUG DC8 DC8F55 3021928 WP BS 1323 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 SUGAR SCOOP CORRODED (OUTFLOW VALVE) STA 1323. REMOVED CORROSION IAW DC-8 SRM 51-1-8. WELDED AREA, NDT TO ASSURE NO FL AWS (NONE FOUND) BLEND SMOOTH AND FINISHED PER FACTORY SPECS PER EO 99-136 WITH APPROVED 8110-3 DATED 8-14-99. REF: ZA NTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200020 20000322 00020 WP 2000 3 22 2000ZZZX707 1 19990816 A 5512 SKIN DOUG DC8 DC8F55 3021928 WP HORIZ STABILIZER DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 LEFT HORIZONTAL LEADING EDGE SCREW HOLES DEFORMED, STA XFS 123 AND XFS 160. REAMED HOLES TO .500 INCH. FABRICATED PLUG AND INSTALLED. FABRICATED STRAP AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-3-99. REF: ZANTOP INTERNATI ONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200021 20000322 00021 WP 2000 3 22 2000ZZZX708 1 19991111 A 5711 FILLER DOUG DC8 DC8F55 3021928 WP WS 69.5 MISSING B T64R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 03 812TC 55626 45764 DUE TO EXISTING REPAIR, DOUBLER ON LT FRONT SPAR (XRS 69.5) LOWER WING PLANK, TAPER FILLERS NEED TO BE FABRICATED TO COM PLETE SB 57-2OR5. FABRICATED FILLERS AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-22-99. REF: ZANTOP INT ERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200022 20000322 00022 WP 2000 3 22 2000ZZZX709 1 19991025 A 5523 57025792 GEAR TAB DOUG DC8 DC8F55 3021928 WP ELEVATOR DENTED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 RT ELEVATOR GEAR TAB DAMAGED DENT/CREASE. REPAIRED RT ELEVATOR GEAR TAB PER EO 99-136 WITH APPROVED 8110-3 DATED 10-15- 99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200023 20000322 00023 WP 2000 3 22 2000ZZZX710 1 19990818 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 1320 GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 DEEP GOUGE FORWARD OF R-2 DOOR BS 1320 RT. BLEND SMOOTH AND REMOVED CRACK BY DRILLING .5 INCH DIAMETER HOLE. FABRICATE D DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZI AA. (X) 2 L 7 4 4F 4A25 2000032200024 20000322 00024 WP 2000 3 22 2000ZZZX711 1 19991102 A 5753 WEB DOUG DC8 DC8F55 3021928 WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 812TC 55626 45764 FOUND DURING C-CHECK. RT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT INSTALLED PER EO 99-136 WITH APPROVED 8110 -3 DATED 10-29-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X) 2 L 7 4 4F 4A25 2000032200025 20000322 00025 WP 2000 3 22 99T64R384AR 1 19990309 A 5531 SPAR DOUG DC8 DC862 3021970 WP VERTICAL STAB CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2569 - VERTICAL STABILIZER REAR SPAR LT TIP FAIRING ATTACH POINT ABOVE STA ZV299 HAS CORROSION. REMOVED CORROSION IA W DC-8 SRM 51-1-8. DYE PENETRANT BLENDED AREA NO CRACKS EXIST, FLAP PEENED AND TREATED AREA PER EO 99-044 AND 99-061 WI TH APPROVED FAA FORM 8110-3 DATED JUNE 14, 1999. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032200026 20000322 00026 WP 2000 3 22 99T64R383AR 1 19990609 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1240-1280 GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 46105 NR 0907 D-PIT DOOR CUTOUT - SKIN FORWARD LOWER EDGE GOUGED. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED PER EO 99-048 AND 99-061 WITH APPROVED FAA FORM 8110-3 DATED JUNE 14, 1999. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032200027 20000322 00027 WP 2000 3 22 99T64R382AR 1 19990226 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 291.500 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 46105 NR 0324 - TOP INBOARD STUB WING CORROSION AROUND SCREWS LT WING. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-027 AND 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032200028 20000322 00028 WP 2000 3 22 99T64R381AR 1 19990226 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 710 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0281 - LT OUTBOARD LEADING EDGE CORROSION ON SKIN AROUND SCREWS. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-029 AND 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032200029 20000322 00029 WP 2000 3 22 99T64R380AR 1 19990311 A 5414 FASTENER DOUG DC8 DC862 3021970 WP NR 2 PYLON MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0557 - NR 2 PYLON LOWER SURFACE 2 EACH FASTENERS MISSING OUTBOARD SIDE ABOVE TAILPIPE. YN 219 AND YN 300. REAMED HO LES TO -197/-199 DIAMETER. INSTALLED MS21141 - V06 FASTENER PER EO 99-036 WITH APPROVED FAA FORM 8110-3 DATED 2-24-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032200030 20000322 00030 WP 2000 3 22 99T64R379AR 1 19990313 A 5532 SKIN DOUG DC8 DC862 3021970 WP VERTICAL STAB CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 066 - CORROSION ON VERTICAL STABILIZER UPPER AND LOWER ATTACH RUSTY SCREWS STA 185. REMOVED CORROSION, FABRICATED FI LLERS AND DOUBLERS AND INSTALLED PER EO 99-046 WITH APPROVED FAA FORM 8110-3 DATED 3-3-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300408 20000404 00408 WP 2000 4 4 9905751233 1 19991223 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1903 - 2000 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING H-CHECK, FOUND CORROSION ON FLOOR SUPPORT FROM BS 1903 TO 2000 AT LBL 57. REPAIRED PER EA12-171341. 2 L 7 3 4F A22WE 2000032300409 20000404 00409 WP 2000 4 4 9905761233 1 19991206 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1509 - 1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING H-CHECK, FOUND CORROSION ON FUSELAGE SKIN AREA BS 1509 - 1531 AT L48L TO L48R. REPAIRED PER EA12-172779. 2 L 7 3 4F A22WE 2000032300410 20000404 00410 WP 2000 4 4 9905771233 1 19991229 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING H-CHECK, FOUND CORROSION ON T-CHORD AT BS 2007 RBL 22. REPAIRED PER EA12-170348. 2 L 7 3 4F A22WE 2000032300411 20000404 00411 WP 2000 4 4 9905781233 1 19991206 A 5320 CAP DOUG DC10 DC1030 3023501 WP BS 1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING H-CHECK, FOUND CORROSION ON PRESSURE BULKHEAD CAP AT BS 1521 BETWEEN LBL 31 AND RBL 31. REPAIRED PER EA12-172780 . 2 L 7 3 4F A22WE 2000032300412 20000404 00412 WP 2000 4 4 9905791233 1 19991223 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING H-CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT BS 1887 RBL 38 TO RBL 57. REPAIRED PER EA12-171342. 2 L 7 3 4F A22WE 2000032300468 20000323 00468 NM 2000 3 23 USAASB99261 1 19991029 A 2530 5000387D4 COFFEEMAKER BOEING 737 737301 1384611 NM GALLEY MALFUNCTIONED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 355US 12752 23558 IAD - FLT 488 - EN ROUTE FROM PIT-BWI, F/A REPORTED SMELL OF BURNING WIRES AND FUMES IN THE AFT CABIN. NO VISIBLE SMOKE WAS NOTED. AN EMERGENCY WAS DECLARED AND FLT DIVERTED TO NEAREST AIRPORT AT IAD. FLT LANDED W/O FURTHER INCIDENT. MX RAN BOTH ENGINES TO 70 PERCENT N1 FOR 20 MINUTES WITH BOTH AIR CONDITIONING PACKS ON. TURNED ALL COFFEE MAKERS ON. LO WERERED CEILING PANELS AND CHECKED ALL LIGHTS. CHECKED BOTH AFT LAVATORIES, INCLUDING WATER HEATERS, TRASH CANS FOR SIG NS OF FIRE AN FLUSHED TOILETS. CHECKED FIRE EXTINGUISHERS. ALSO, RAN APU.. NO SMELL OR FUMES NOTED. REMOVED AND REPL ACED UPPER AFT GALLEY COFFEEMAKER AS PRECAUTIONARY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 2000032300469 20000323 00469 NM 2000 3 23 USAASB99262 1 19991030 A 2130 7110025 SELECTOR PANEL BOEING 737 737301 1384611 NM COCKPIT FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 591US 35606 23936 BWI - FLT 401 - CRUISING AT FL350, LGA-TPA, CABIN ALT WARNING HORN SOUNDED. THE CABIN ALTITUDE INDICATED 10,500 FT AND THE CABIN WAS CLIMBING AT APPROX 1,000 FT PER MINUTE. A DESCENT WAS INITIATED TO A FLT ALTITUDE OF 10,000 FT. DURING D ESCENT, THE STANDBY MODE WAS SELECTED ON THE PRESSURIZATION SELECTOR PANEL AND THE CABIN RATE OF CLIMB WENT TO 4,000 FT PER MINUTE INSTANTLY. MANUAL DC WAS THEN SELECTED AND OPERATED NORMALLY THROUGHOUT REMAINDER OF FLT. FLT DIVERTED TO B WI AND LANDED W/O FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED THE CABIN PRESSURIZATION SELECT OR PANEL. ALSO, REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER (P/N 763810-2) AND THE AFT OUTFLOW VALVE (P/N 711003 2 L 7 2 4F RT A16WE 2000032300470 20000323 00470 NM 2000 3 23 USAASB99290 1 19991208 A 2130 CABIN PRESSURE BOEING 737 737301 1384611 NM FUSELAGE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 PIT - FLT 2380 - DURING CLIMB-OUT FROM PIT, THE AUTO PRESSURIZATION SYSTEM FAILED TO STANDBY. CREW WAS UNABLE TO CONTRO L CABIN IN STANDBY OR MANUAL MODE. CABIN CONTINUED TO CLIMB WITH OUTFLOW VALVE CLOSED. DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RAN AIRCRAFT IN AUTO AND MANUAL MODE AND INSPECTED ALL DOORS AND WINDOWS FOR LEAKS. NO DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4 PSI ON GROUND. ALL SY STEMS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 2000032300477 20000323 00477 WP 2000 3 23 AALA200098 1 19991230 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1174/1193 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 460AA 49565 TUL - FOUND CORROSION ON BEAM AT DOOR STOP BRACKETS. INSTALLED DOUBLERS AT FORWARD AND AFT STOP LOCATIONS PER AARD 53-1 0-00-3 AND 53-10-00-16. (M) 2 L 7 2 4F A6WE 2000032300478 20000323 00478 NM 2000 3 23 AALA984202 1 19991214 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 386AA 27060 AFW - FLOORBEAM AT STATION 347 HAD AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301.5 SS .050. ALODINE ALL BARE ALUM SURFACES FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS 10-11 PRIMER. FILL BLENDS WITH B MS 5-92, INSTALL STRAP WET W/BMS 5-95 SEALANT, PROSEAL 870 REPAIR PER MRB 767-1980. (M) 2 L 7 2 4F RT A1NM 2000032300479 20000323 00479 NM 2000 3 23 AALA994203 1 19991215 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 792-827 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 386AA 27060 AFW - FOUND CORROSION IN THE UPPER CHORD OF THE LBL 33 AND RBL 33 LONGITUDINAL FLOORBEAMS, AT BODY STATIONS 827 AND 792. VERIFY CORROSION COMPLETELY REMOVED AND BLENDED AREA IS CRACK FREE. ROTO PEEN BLENDED AREA. APPLY ALODINE AND 2 COAT S PRIMER, FILL BLENDS WITH BMS5-95 SEALANT MRB 767-1981. (M) 2 L 7 2 4F RT A1NM 2000032300480 20000323 00480 NM 2000 3 23 AALA994204 1 19991215 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 386AA 27060 AFW - FLOORBEAM AT STATION 347 HAD CORROSION ON TOP SURFACE BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OF 301..5 H SS, .050 INCH THICK, ALODINE ALL BARE ALUM FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS 10-11 PRIMER. FILL BLENDS W/BMS 5-92. INSTALL REPAIR STRAP WET W/BMS 5-95 SEALANT, PROSEAL 970 MRB REPAIR 767-1982. (M) 2 L 7 2 4F RT A1NM 2000032300481 20000323 00481 NM 2000 3 23 AALA994205 1 19991215 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 386AA 27060 AFW - FLOORBEAM AT STATION 1480 HAD CORROSION ON TOP SURFACE BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OF 301.5 H SS .050 INCH CHICK. ALODINE ALL BARE ALUM SURFACES, FINISH BLENDS AND REPAIR PARTS W/2 COATS BMS 10-11 PRIMER FILL BL ENDS WITH BMS 5-92. INSTALL STRAP WET W/BMS 5-95. PROSEAL 870 MRB767-1983. (M) 2 L 7 2 4F RT A1NM 2000032300635 20000323 00635 WP 2000 3 23 99T64R378AR 1 19990329 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 680 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0735 - MID ACC. COMPT CORROSION - SKIN L34R - L35L STA 680. REMOVED CORROSION, FABRICATED FILLERS AND DOUBLERS AND I NSTALLED PER EO 99-040 WITH APROVED FAA FORM 8110-3 DATED 3-4-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300636 20000323 00636 WP 2000 3 23 99T64R253AR 1 19990528 A 5320 WEB DOUG DC8 DC862 3021970 WP BS 188-208 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2483 - CORROSION FROM FRAME 188 TO FRAME 208 RT SUB FLOOR WEB AND CORROSION ON FLANGE DOUBLER L22R. REMOVED CORROSIO N IAW DC-8 SRM 51-1-8. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS PER EO 99-061 WITH APPROVED FAA FORM 8110- 3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300637 20000323 00637 WP 2000 3 23 99T64R252AR 1 19990609 A 5753 SKIN DOUG DC8 DC862 3021970 WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2392 - LEFT INBOARD FLAP WEDGE, DAMAGED SKIN LOWER STA XW 47. FABRICATED NEW LOWER SKIN LEFT INBOARD FLAP WEDGE PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300638 20000323 00638 WP 2000 3 23 99T64R251AR 1 19990603 A 5220 WINDOW FRAME DOUG DC8 DC862 3021970 WP BS 717-742 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2286 - FORWARD LT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 717-742. REMOVED CORROSION IAW DC-8 SRM 51-1- 8. INSTALLED HYSOL EA 9309NA TO FRAME, FAIRED TO ORIGINAL THICKNESS OF FRAME. TREATED AND PRIMED PER EO 99-061 WITH AP PROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300639 20000323 00639 WP 2000 3 23 99T64R249AR 1 19990504 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1620 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1928 - EXTERIOR CORROSION AROUND ACCESS DOOR CUT OUT AT STA 1620. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300640 20000323 00640 WP 2000 3 23 99T64R247AR 1 19990420 A 5753 SKIN DOUG DC8 DC862 3021970 WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1554 - REMOVED AND REPLACED RT INBOARD FLAP WEDGE LOWER SKIN DUE TO EXCESSIVE DAMAGE. FABRICATED NEW RT INBOARD FLAP WEDGE LOWER SKIN PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARR OW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300641 20000323 00641 WP 2000 3 23 99T64R246AR 1 19990331 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORIZONTAL STAB MISINSTALLED B T64R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1780, RT HORIZONTAL STABILIZER OUTBOARD L/E TOP OUTBOARD DOUBLER REMOVE/REPLACE AND INSTALL WITH CONICAL WASHERS. FA BRICATED DOUBLERS IAW DC-8 SRM 51-1-4 ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, AND INSTALLED IAW DC-8 SRM'S 55-2-1, 51-1 -21, AND 51-1-4. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300642 20000323 00642 WP 2000 3 23 99T64R245AR 1 19990413 A 5753 CHAFE STRIP DOUG DC8 DC862 3021970 WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1248 - RT INBOARD CHAFE STRIP DAMAGED AND CRACKED XW 138. REMOVED DAMAGED CHAFE STRIP, FABRICATED NEW STRIP AND INST ALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300643 20000323 00643 WP 2000 3 23 99T64R243AR 1 19990617 A 5244 ACCESS DOOR DOUG DC8 DC862 3021970 WP BS 1380 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1066 - ACCESS DOOR STA 1380 BENT AND CRACKED (PLEXIGLASS CRACKED). FABRICATED NEW ACCESS DOOR PER EO 99-061 WITH APP ROVED FAA FORM 8110-3 DATED 6-10-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300644 20000323 00644 WP 2000 3 23 99T64R242AR 1 19990407 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 520 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0888 - NR 2 PIT DOOR OPENING LOWER EDGE SKIN CRACKED AT EDGE STA 520. CUT OUT DAMAGED AREA AND REPAIRED PER EO 99-04 9 WITH APPROVED FAA FORM 8110-3 DATED 3-8-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300645 20000323 00645 WP 2000 3 23 99T64R240AR 1 19990519 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1800-1811 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0572 - TAILE CONE, HOLE CORRODED THROUGH TAIL CONE JUST FORWARD BOTTOM TAIL LIGHT BS 1800 - BS 1811. REMOVED PREVIOU S DOUBLER REPAIR, REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED NEW DOUBLERS AND INSTALLED IAW DC-8 SRM'S 53-2-0 AN D 51-1-21. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300646 20000323 00646 WP 2000 3 23 99T64R238AR 1 19990330 A 5314 KEEL BEAM DOUG DC8 DC862 3021970 WP BS 920-980 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0310 - CORROSION SIDE KEEL BEAM INSPECTION PLATES RT WW FROM GEAR DOOR ACTUATOR CYLINDER AFT STA 920 - STA 980. REMO VED CORROSION IAW DC-8 SRM 51-1-8. FLAP PEENED TREATED AND PRIMED, FILLED WITH PRC 1422 PER EO 99-035 ADN EO 99-061 WIT H APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300647 20000323 00647 WP 2000 3 23 99T64R237AR 1 19990427 A 5753 FITTING DOUG DC8 DC862 3021970 WP TE FLAP CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0076 - LT INBOARD FLAP WEDGE CORROSION AROUND ATTACH FITTINGS. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED AN D INSTALLED DOUBLERS PER EO 99-061 WITH APPROVEDF FAA FORM 8110-3 DATED 6-8-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300648 20000323 00648 WP 2000 3 23 99T64R248AR 1 19990511 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1060 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1584 - CORROSION FRAME 1060 TO CHORD, ALSO SEVERAL NUTPLATES BROKEN FROM L33R-L33L. REMOVED CORROSION IAW DC-8 SRM 5 1-1-8. CUT OUT DAMAGED AREA, FABRICATED REPAIR STRAP PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTAL LED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300649 20000323 00649 WP 2000 3 23 99T64R236AR 1 19990529 A 5411 9753263519 FRAME DOUG DC8 DC862 3021970 WP NR 1 PYLON CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0164 - 5 INCH CRACK IN PYLON CAP FORMER 2ND SECTION NR 1 PYLON STA YN 190. FABRICATED REPLACEMENT PART PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300650 20000323 00650 WP 2000 3 23 99T64R115AR 1 19990426 A 5414 ANCHOR NUT DOUG DC8 DC862 3021970 WP NR 1 PYLON MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0525 - ONE EACH ANCHOR NUTPLATE MISSING, NR 1 PYLON REMOVABLE PLANK. INSTALLED JO-BOLT IAW EO 99-026 WITH APPROVED F AA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300651 20000323 00651 WP 2000 3 23 99T64R114AR 1 19990426 A 5414 ANCHOR NUT DOUG DC8 DC862 3021970 WP NR 2 PYLON MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0524 - 2 EACH, ANCHOR NUTPLATES MISSING NR 2 PYLON REMOVABLE PLANK. INSTALLED JO-BOLTS IAW EO 99-026 WITH APPROVED F AA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300652 20000323 00652 WP 2000 3 23 99T64R113AR 1 19990426 A 5414 ANCHOR NUT DOUG DC8 DC862 3021970 WP NR 3 PYLON MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0523 - ONE EACH, ANCHOR NUTPLATES MISSING NR 3 PYLON REMOVABLE PLANK. INSTALLED JO-BOLT IAW EO 99-026 WITH APPROVED FAA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300653 20000323 00653 WP 2000 3 23 99T64R112AR 1 19990426 A 5320 SPLICE DOUG DC8 DC862 3021970 WP BS 400-420 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0416 - CORROSION L24R SPLICE BETWEEN FRAMES 400-420 RT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED 2 EACH, S PLICE FITTINGS. REPLACED LONGERON AND INSTALLED PER DC-8 SRM'S 53-2-2 AND 51-3-2. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300654 20000323 00654 WP 2000 3 23 99T64R273AR 1 19990422 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 188 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2654 - FRAME STA 188 CORROSION AT L6R. REMOVED CORROSION IAW 51-1-8. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-0. FAB RICATED DOUBLER IAW DC-8 SRM 53-2-0 AND INSTALLED IAW DC-8 SRM 53-2-0 REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300655 20000323 00655 WP 2000 3 23 99T64R271AR 1 19990304 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 297.500 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0507 - TWO EACH, CORROSION BULGES AROUND FASTENERS LT WING LEADING EDGE LOWER SKIN INBOARD T/E XFS 297.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLER/DOUBLER AND INSTALLED PER EO 99-037 WITH APPROVED FAA FORM 8110-3 DATE D 2-25-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300656 20000323 00656 WP 2000 3 23 99T64R270AR 1 19990407 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 710 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0328 - RT WING UPPER LEADING EDGE, TRAILING EDGE LIGHT SURFACE CORROSION EMANATING FROM SCREW HOLE XW 693,XFS 766.250 . REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLERS AND DOUBLERS, INSTALLED PER EO 99-051 AND 99-061 WITH APRO VED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300657 20000323 00657 WP 2000 3 23 99T64R269AR 1 19990602 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 1120 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2958 - CORROSION BLISTER AFT SIDE CABIN FLOORBEAM STA 1120 RBL 34 INCHES. REMOVE CORROSION IAW DC-8 SRM 51-1-8. FAB RICATED DOUBLER AND INSTALLED PER EO 99-016 WITH APPROVED FAA FORM 8110-3 DATED 6-7-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300658 20000323 00658 WP 2000 3 23 99T64R268AR 1 19990528 A 5711 SPAR DOUG DC8 DC862 3021970 WP BS 505 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2886 - LT WING FRONT SPAR STA 505 CORROSION SPOT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SPECIAL WASHERS AND DOUBLER, INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300659 20000323 00659 WP 2000 3 23 99T64R267AR 1 19990602 A 5720 NUTPLATE DOUG DC8 DC862 3021970 WP WS 14-64 MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 288 - TWO EACH, CHANNEL NUTPLATES AND SCREWS MISSING LT INBOARD L/E FUEL TANK XRS 64-XFS 14. INSTALLED NAS-1670-4 BL IND FASTENERS PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300660 20000323 00660 WP 2000 3 23 99T64R265AR 1 19990607 A 5711 SPAR DOUG DC8 DC862 3021970 WP WS 139-172 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2841 - LT WING REAR SPAR HAS 4 EACH AREAS OF CORROSION BETWEEN XRS 139-172. REMOVED CORROSION IAW DC-8 SRM 51-1-8. F ABRICATED SPECIAL WASHERS AND DOUBLER, INSTALLED PER EO 99-061 WITH APPROVEDF FAA FORM 8110-3 DATED 6-14-99. REF: ARRO W AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300661 20000323 00661 WP 2000 3 23 99T64R264AR 1 19990529 A 5711 SPAR DOUG DC8 DC862 3021970 WP WS187-195 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2840 - LT WING CENTER SPAR HAS 2 EACH AREAS OF CORROSION BETWEEN XRS 187 AND XRS 195. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SPECIAL WASHERS AND DOUBLER, INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. R EF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300662 20000323 00662 WP 2000 3 23 99T64R263AR 1 19990420 A 5720 SHIM DOUG DC8 DC862 3021970 WP WS 510.222 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2681 - RT WING BOTTOM FRONT SPAR CAP SHIM PLATE CRACKED APPROXIMATELY 1 FOOT INBOARD NR 4 PYLON XS 510.222. REMOVED SHIM, BLENDED SMOOTH THE CRACKED SURFACE, ALODINED AND PRIMED. RE-INSTALLED SHIM AND SEALED WITH PR 1422 B 1/2 PER EO 9 9-061 WITH APPROVED FAA FORM 8110-3 DATED 66-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300663 20000323 00663 WP 2000 3 23 99T64R262AR 1 19990421 A 5720 SHIM DOUG DC8 DC862 3021970 WP WS 510.222 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2680 - LT WING BOTTOM FRONT SPAR CAP SHIM PLATE CRACKED XS 510.222. REMOVED SHIM, BLENDED SMOOTH THE CRACKED SURFACE , ALODINED AND PRIMED. RE-INSTALLED SHIM AND SEALED WITH PR 1422 B 1/2 PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATE D 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300664 20000323 00664 WP 2000 3 23 99T64R261AR 1 19990420 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 485.000 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2651 - LT WING, OUTBOARD STUB WING UPPER TRAILING EDGE CORRODED XW 485.000. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS, INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300665 20000323 00665 WP 2000 3 23 99T64R260AR 1 19990603 A 5220 WINDOW FRAME DOUG DC8 DC862 3021970 WP BS 798-822.500 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2633 - AFT LT OVER WING DOOR, WINDOW FRAME CORRODED STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. I NSTALLED HYSOL 9309NA, FAIR TO ORIGINAL THICKNESS, TREATED AND PRIMED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300666 20000323 00666 WP 2000 3 23 99T64R259AR 1 19990422 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1080-1100 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2602 - CORROSION BETWEEN STA 1080 - STA 1100 LT AFT DOUBLER ABOVE L28L. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABR ICATED DOUBLER AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300667 20000323 00667 WP 2000 3 23 99T64R258AR 1 19990625 A 7921 57542041 DUCT DOUG DC8 DC862 3021970 WP OIL COOLER CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0161 - CSD OIL COOLER DUCT CRACKED AT FORWARD MOUNTING FLANGE ENG S/N 670982 NR 4 POSITION. WELDED CRACK IAW BOEING ENGINEERING MESSAGE M-7200-99-05081 WITH APPROVED FAA FORM 8110-3 DATED 6-21-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300668 20000323 00668 WP 2000 3 23 99T64R257AR 1 19990420 A 5753 SKIN DOUG DC8 DC862 3021970 WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2520 - RT INBOARD FLAP WEDGE, SKIN WORN THROUGH AT CORNER ATTACH HOLE XW 122. FABRICATED REPAIR DOUBLERS AND INSTALL ED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300669 20000323 00669 WP 2000 3 23 99T64R256AR 1 19990406 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 257.5-223.5 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0901 - RT WING UPPER SURFACE NR 3 INBOARD STUB WING CORROSION EXFOLIATION TRAILING EDGE AND CORROSION EMANATING FROM SCREW HOLES XW 257.500 TO XW 223.500. CUT OUT 2 EACH DAMAGED AREAS, FABRICATED DOUBLER REPAIRS AND INSTALLED PER EO 99- 023 AND 99-061, TASK NR 0901 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300670 20000323 00670 WP 2000 3 23 99T64R255AR 1 19990413 A 5720 WEB DOUG DC8 DC862 3021970 WP WS 69.5 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2484 - LT FLAP WELL WEB DAMAGED XCW 69.5 BS 980 - BS 1020. REMOVED WEB, FABRICATED NEW WEB AND INSTALLED PER EO 99-0 61 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300671 20000323 00671 WP 2000 3 23 99T64R254AR 1 19990406 A 5720 WEB DOUG DC8 DC862 3021970 WP WS 69.5 DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1253 - RT INBOARD FLAP WELL WEB, FASTENERS PULLED THROUGH XCW 69.5 BS 980 - BS 1020. REMOVED WEB, FABRICATED NEW WEB AND INSTALLED PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300672 20000323 00672 WP 2000 3 23 99T64R294AR 1 19990329 A 5730 561235516 SKIN DOUG DC8 DC862 3021970 WP WS 408 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0382 - PREVIOUS CORROSION BLEND OUT STRINGER 11 RT WING STA XW 408. REMOVED PAINT, FASTENERS AND CORROSION IAW DC-8 SRM'S 51-1-8 AND 51-1-20D. REMAINING SKIN THICKNESS IS ACCEPTABLE IAW DACO DOCUMENT M-7200-99-02208 ITEM 4. TREATED AN D PRIMED IAW SRM 51-1-8. INSTALLED FASTENERS IAW DC-8 SRM 51-1-20D AND APPROVED FAA FORM 8110-3 DATED 4-19-99. REF: A RROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300673 20000323 00673 WP 2000 3 23 99T64R279AR 1 19990420 A 5400 CONDUIT DOUG DC8 DC862 3021970 WP NR 2 PYLON CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2869 - GENERATOR LEADS CONDUIT DENTED NR 2 PYLON JUST FORWARD OF WING LEADING EDGE, YN 260. CUT OUT DAMAGED AREA IAW EO AS11047. INSPECTED WIRING INSULATION, NO DAMAGE. FABRICATED DOUBLER AND INSTALLED PER EO AS11047 WITH APROVED FAA FORM 8110-3, DATED 5-12-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300674 20000323 00674 WP 2000 3 23 99T64R244AR 1 19990401 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1320-1340 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1153 - CORROSION AND CRACKED LONGERON 36 BETWEEN FRAMES 1320 - 1340. REMOVED DAMAGED SECTION OF L36, FABRICATED REPA IR PARTS AND INSTALLED PER EO 99-055 WITH APPROVED FAA FORM 8110-3 DATED 3-11-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300675 20000323 00675 WP 2000 3 23 99T64R293AR 1 19990513 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 225 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0890 - EVALUATED REPAIR ON FUSELAGE SKIN FORWARD CABIN DOOR OPENING TOP FORWARD CORNER STA 225. REMOVED DOUBLER, FOU ND SKIN CRACKED, CUT OUT CRACK IAW DC-8 SRM 53-2-2 FIG 15. FABRICATED FILLER AND DOUBLER IAW DC-8 SRM 52-2-0. INSTALLE D FILLER AND DOUBLER IAW 51-1-20D. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300676 20000323 00676 WP 2000 3 23 99T64R291AR 1 19990428 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 44 MISREPAIRED B T64R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2824 - NOSE FUSELAGE SECTION STA 44 2 O'CLOCK POSITION JUST AFT PRESSURE BULKHEAD FRAME 44 ILLEGAL SKIN AND FRAME REP AIR. REMOVED SKIN/FRAME REPAIR, FABRICATED NEW FILLER AND DOUBLER IAW DC-8 SRM 53-2-1. INSTALLED IAW DC-8 SRM'S 53-2-0 AND 53-2-1. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300677 20000323 00677 WP 2000 3 23 99T64R290AR 1 19990413 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1260-1280 DENTED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2786 - REPAIR DENT IN FUSELAGE EXTERNAL SKIN BETWEEN STA 1260 AND STA 1280 BETWEEN L34L AND L33L. REMOVED DENT BY CU T-OUT IAW DC-8 SRM 53-2-1. FABRICATED DOUBLER IAW DC-8 SRM 53-2-1. INSTALLED DOUBLER IAW DC-8 SRM'S 51-1-21 AND 51-1-2 0. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300678 20000323 00678 WP 2000 3 23 99T64R289AR 1 19990421 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1520 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0997 - CORROSION FRAME 1520 LOWER CHORD BETWEEN L24R - L26R. REMOVED DAMAGED SECTION IAW DC-8 SRM 53-2-0. FABRICATE D NEW SECTION OF FRAME IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 53-2-0. RE F: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300679 20000323 00679 WP 2000 3 23 99T64R288AR 1 19990407 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1200-1240 DENTED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2565 - DENT EXTERIOR RT FUSELAGE FORWARD OF D-PIT DOOR BETWEEN L24R AND L27R STA 1200 - STA 1240. REMOVED DAMAGED AR EA IAW DC-8 SRM 53-2-1. FABRICATED DOUBLERS AND INSTALLED IAW EC-8 SRM IAW DC-8 SRM'S 53-2-1 AMND 51-1-20D. REF: ARRO W AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300680 20000323 00680 WP 2000 3 23 99T64R287AR 1 19990401 A 5312 BULKHEAD DOUG DC8 DC862 3021970 WP BS 1606 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2348 - POSSIBLE CRACK IN WEB OF AFT PRESSURE BULKHEAD APPROXIMATELY 15 INCHES INBOARD OF L10R. CRACK CONFIRMED BY ND T. ROUTED OUT CRACK IAW DC-8 SRM 53-2-5. FABRICATED FILLERS AND DOUBLERS IAW DC-8 SRM 53-2-5. INSTALLED IAW DC-8 SRM' S 51-1-21 AND 51-1-20D. (X) 2 L 7 4 4F 4A25 2000032300681 20000323 00681 WP 2000 3 23 99T64R239AR 1 19990322 A 5510 FITTING DOUG DC8 DC862 3021970 WP HORIZ STABILIZER CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 0542 - RT HORIZONTAL STABILIZER, BATH TUB FITTING CORRODED STA XE77. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICA TED STRAP REPAIR AND INSTALLED PER EO 99-045 APPROVED FAA FORM 8110-3 DATED 3-2-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000032300682 20000323 00682 WP 2000 3 23 99T64R250AR 1 19990603 A 5220 WINDOW FRAME DOUG DC8 DC862 3021970 WP BS 798-822 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2285 - AFT RIGHT O/W EXIT DOOR, CORROSION WINDOW FRAME INTERNAL. STA 798 - STA 822.500. REMOVED CORROSION IAW DC-8 SRM 51-1-8. INSTALLED HYSOL EA 9309NA TO FRAME, FAIRED TO ORIGINAL THICNESS OF FRAME. TREATED AND PRIMES PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X) 2 L 7 4 4F 4A25 2000040300013 20000403 00013 NE 2000 4 3 20000329SH049 2 19991215 A 7200 ENGINE LEAR 25 25D 5170514 CE GE CJ610 CJ6106 30006 NE RIGHT FLAMED OUT E EFAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 21 251DS 6708 1701 218 251753A AIRCRAFT AT 43,000 CRUISE M.780, RT ENGINE ROLL BACK RE-LIGHT AT 35,000. PERFORMED INSPECTION OF BLEED AIR SYSTEM, COMP RESSOR FOR FOD. NONE NOTED. PERFORMED MAXIMUM ALTITUDE ACCEL CHECK. ALL WORK PERFORMED IAW MFG MM SEI 186. (X) 2 L 7 2 4J 4 J A10CE 1E16 2000040400433 20000404 00433 WP 2000 4 4 000451233 1 19991206 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1509 - 1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING H-CHECK, FOUND CORROSION ON FUSELAGE SKIN AREA BS 1509-1531 AT L48L TO L48R. REPAIRED PER EA12-172779. 2 L 7 3 4F A22WE 2000040400434 20000404 00434 WP 2000 4 4 0000471233 1 19991206 A 5320 CAP DOUG DC10 DC1040 3023508 WP BS 1521 CORRODED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 223NW 46580 DURING ''''H'''' CHECK, FOUND CORROSION ON PRESSURE BULKHEAD CAP AT BS 1521 BETWEEN LBL 31 AND RBL 31. REPAIRED PER EA1 2-172780. 2 L 7 3 4F A22WE 2000040400435 20000404 00435 WP 2000 4 4 0000481233 1 19991223 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING ''H'' CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT BS 1887 RBL 38 TO RBL 57. REPAIRED PER EA12-171342. 2 L 7 3 4F A22WE 2000040400436 20000404 00436 WP 2000 4 4 0000461233 1 19991229 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 DURING H-CHECK, FOUND CORROSION ON T-CHORD AT BS 2007 RBL 22. REPAIRED PER EA12-170348. 2 L 7 3 4F A22WE 2000040400534 20000404 00534 NM 2000 4 4 EISA99215 1 19991122 A 2611 302842 SMOKE DETECTOR BOEING 727 72725 1384006 NM NR 4 WILL NOT TEST A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 290NE 13635 18972 NUMBER FOUR SMOKE DETECTOR WOULD NOT TEST. REMOVED AND REPLACED NUMBER 4 SMOKE DETECTOR. OPERATIONS CHECK GOOD. (M) 2 L 7 3 4F A3WE 2000040400556 20000404 00556 WP 2000 4 4 G60A045 1 19990307 A 5310 STRUCTURE DOUG DC10 DC1030F 3023504 WP FUSELAGE DAMAGED A G6OA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 EA 27 607GC 46978 DURING GROUND OPERATIONS LOADING AT SAN DIEGO, CA, THE AIRCRAFT WAS STRUCK BY A FORK LIFT. THE DAMAGE TO THE AIRCRAFT ST RUCTURE CONSISTS OF A 48 INCH BY 6 INCH HOLE FORWARD OF THE FORWARD EQUIPMENT BAY. (M) 2 L 7 3 4F RT A22WE 2000040400639 20000404 00639 NM 2000 4 4 ABXA000175 1 19991229 A 5720 112TT1001 BOLT BOEING 767 767281 1385109 NM LT WING BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785AX 23018 LEFT WING LOAD FITTING BOLT BROKEN. (REF: S/B 767-57A064 AND AD 99-19-29). REPLACEDBOLT AND REPAIRED FITTING IAW ABX R EA B653-34274MR AND BOEING FAX ABX-ILN-99-00410H. 2 L 7 2 4F RT A1NM 2000040500004 20000405 00004 NM 2000 4 5 ABXA000181 1 19991201 A 5320 96F5667698101 STRINGER BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 785AX 23018 CRACK ON UPPER SIDE OF STRINGER 18A RIGHT, BETWEEN STATION 412R AND 434R. REPAIREDIAW B767 SRM 53-00-03 AND ABX REA B65 3-32119MR. 2 L 7 2 4F RT A1NM 2000040500010 20000405 00010 NE 2000 4 5 EIA990294 2 19991211 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 2 LEAKING A EIAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 EIAA 20712 662321 KJFK - AT LOWER POWER SETTING, AIR COND SMOKE WAS NOTICEABLE IN UPPER DECK/COCKPIT AREA. FOUND OIL OUT OF NR 2 ENGINE, NR 3 BEARING VENT. (M) 2 L 7 4 4F 4 F A20WE E20EA 2000040500011 20000405 00011 NE 2000 4 5 EIA990293 2 19991211 A 7200 ENGINE BOEING 747 747273C 1384896 NM PWA JT8 JT8D* NE NR 4 BIRD STRIKE A EIAA C ABORTED TAKEOFF C X J F.O.D. ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 NM 09 470EV 20653 662229 KTOL - DURING TAKEOFF ROLL, JUST PRIOR TO ROTATION, NR 4 ENGINE INGESTED A BIRD AND FAILED. DUMPED FUEL TO BELOW STRUCT URAL LIMITS AND RETURNED FOR LANDING. GROUND CHECK CONFIRMED NR 4 ENGINE AND NOSE COWL DAMAGE DUE TO BIRD STRIKE. (M) 2 L 7 4 4F 4 F A20WE E2EA 2000040500012 20000405 00012 NE 2000 4 5 EIA990292 2 19991211 A 7200 ENGINE BOEING 747 747128 1384894 NM PWA JT9 JT9D7A 52054 NE NR 1 STALLED A EIAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 NM 09 3203Y 19751 685679 KCLT - NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT NORMAL CLIBM POWER THROUGH FL260. EGT OVER 1,000 FOR FIVE SECONDS. PRIOR TO STALL, ALL PARAMETERS NORMAL. ATTEMPTED ONE RESTART AND FOUND ENGINE DID NOT NORMALIZE, BUT WAS STABLE WITH HI GH EGT WITHIN LIMITS, AND OIL AND FUEL CONDITIONS NORMAL. SHUT DOWN ENGINE. WINDMILLING OIL PRESSURE 21 PSI. NO VIBRA TION NOTED AT ANYTIME. FOUND HEAVY METAL DEPOSITS IN TAILPIPE UPON INSPECTION AT KCLT. (M) 2 L 7 4 4F 4 F A20WE E20EA 2000040500013 20000405 00013 NM 2000 4 5 EIA990291 1 19991206 A 2432 401764 BATTERY BOEING 747 747131 1384881 NM E/E BAY FAILED A EIAA O OTHER N B FALSE WARNING SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 472EV 20320 PGUA - IN FLIGHT MAIN BATTERY VOLTS DROPPED 20 VOLTS, HAD ELECTRICAL SMELL AND ADVISED FE TABLE, TURNED OFF BATTERY AND PULLED C/B FOR BATTERY CHARGER. FOUND 1 BATTERY CELL LEAKING. SWAPPED MAIN BATTERY WITH APU BATTERY, MAIN BATTERY REMOV ED. (M) 2 L 7 4 4F A20WE 2000040500014 20000405 00014 WP 2000 4 5 EIA990290 1 19991103 A 3350 BATTERY PACK DOUG DC9 DC933F 302207A WP CABIN INOPERATIVE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 SEA - CABIN EMERGENCY LT WILL NOT DISARM WITH AC POWER ON AIRPLANE. CABIN EMERGENCY LT IN COCKPIT AND CENTER FORWARD CA BIN WILL NOT TEST. REMOVED AND REPLACED RIGHT EMERGENCY BATTERY POWER SUPPLY ASSY PER 33-53-0, OPS CHECK GOOD. REMOVED AND REPLACED B5-23 EMERGENCY BATTERY PACK AND BATTERY, CORRECTED WIRING TO SAME WD 33-51-01. (M) 2 L 7 2 4F A6WE 2000040500025 20000405 00025 CE 2000 4 5 20000404SH007 1 19991117 A 2730 115610010325 TORQUE TUBE BEECH 99 99 1154002 CE ELEVATOR CRACKED A TIMA K NONE O OTHER IN INSP/MAINT 1 NM 11 199GL U15 CRACK IN LEFT ELEVATOR TORQUE TUBE FOUND DURING 100-HOUR INSPECTION. (X) 1 L 7 2 3T A14CE 2000040500034 20000405 00034 2000 4 5 20000404SH021 4 19991217 A 3416 KEA346 ENCODER BEECH 1900 1900C 1154161 CE COCKPIT FAILED C YADA O OTHER O OTHER NR NOT REPORTED 1 AL 05 5632C 1487 UC81 ALTIMETER QUIT AT 950 FEET. ENCODING FUNCTION ALSO QUIT. FLAG DROPPED AND STAYED IN VIEW. UNIT BENCH CHECKED AS INOPE RABLE. SUBMITTER STATED THIS IS THE SECOND UNIT, OF THIS PART NUMBER, IN A WEEK TO FAIL. (X) 2 L 7 2 4T RT A24CE 2000040500036 20000405 00036 EU 2000 4 5 20000404SH024 1 19991216 A 6220 552200 BEARING UROCOP EC135 EC135P1 8680990 EU MAIN ROTOR ROUGH A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 893 EC1350054 BEARING ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X) 1 G 7 2 3U O H88EU 2000041100101 20000411 00101 NM 2000 4 11 20000410AP001 1 19991230 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 GL 11 768AT 21996 DURING PREFLIGHT, FOUND FIRST 15 FEET OF EMERGENCY FLOOR LIGHTING IS INOPERATIVE. FOUND THE FIRST FEW FEET OF FLOOR TRA CK PULLED LOOSE AND SEVERAL WIRES BROKEN. REPAIRED AS REQUIRED, OPS CHECK GOOD PER MM. (M) 2 L 7 3 4F A3WE 2000041100145 20000411 00145 SO 2000 4 11 20000407SH013 1 19990930 A 2731 CONTROL CABLE PIPER PA32 PA32R300 7103213 SO STABALATOR TRIM BROKEN E K NONE O OTHER IN INSP/MAINT 1 AL 05 2930Q 32R7780269 STABALATOR TRIM CABLE BROKEN, P/N 62701-041. (X) 1 L 7 1 3O A3SO 2000041100163 20000411 00163 SO 2000 4 11 20000407SH022 1 19991007 A 2730 CONTROL CABLE PIPER PA32 PA32300 7103212 SO STABALATOR DAMAGED E K NONE O OTHER IN INSP/MAINT 1 AL 05 3957X 4373 327640003 STABALATOR TRIM CABLE HAD BROKEN STRANDS AT AFT DRUM. 510.89 TK TIME. (X) 1 L 7 1 3O A3SO 2000041100175 20000411 00175 EU 2000 4 11 20000411AP001 1 19991229 A 5347 S53570205202 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP INSPECTION, FOUND LEFT MIDDLE OUTBOARD AND LEFT MIDDLE INBOARD SEAT TRACKS CORRODED BEYOND LIMITS. RE MOVED AND REPLACED LEFT MIDDLE OUTBOARD AND INBOARD SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000041100182 20000411 00182 NM 2000 4 11 ASAA9910253 1 19991030 A 3350 883200312 LIGHT BOEING 737 737290C 138448V NM ROW 14 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 14. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100183 20000411 00183 NM 2000 4 11 ASAA9910254 1 19991103 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM ROW 18 DISCHARGED A ASAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 NM 01 730AS 22577 ANC - PRIOR TO FLIGHT 21, THE EMERGENCY EXIT FLOOR TRACK LIGHTS NEAR ROW 18 ILLUMINATED. REPLACED BATTERY PACK AND LIGH TS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100184 20000411 00184 NM 2000 4 11 ASAA9910255 1 19991104 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM ROW 18 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE BULKHEAD EMERGENCY EXIT TO REAR LIGHT AND THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 18 WERE FOUND TO BE INOPERATIVE. REPLACED BULKHEAD AND ROW 18 RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100185 20000411 00185 NM 2000 4 11 ASAA9910257 1 19991111 A 3397 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING RECON, PRIOR TO F41, AN AFT CABIN EMERGENCY EXIT FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED LIGHT/W IRING AND THE LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100186 20000411 00186 NM 2000 4 11 ASAA9910258 1 19991111 A 3397 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 742AS 23136 ANC - PRIOR TO F55, ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATAIVE. REPAIRED WIRING AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100187 20000411 00187 NM 2000 4 11 ASAA9910265 1 19991213 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, BOTH INTERIOR OVERWING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. REPLACED BATT ERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100188 20000411 00188 NM 2000 4 11 ASAA9910266 1 19991214 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 4 WOULD NOT EXTINGUISH. REPLACED BATTERY P ACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2000041100189 20000411 00189 NM 2000 4 11 ASAA9910274 1 19991219 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 11, 14, AND 18 WOULD NOT TEST PROPERLY. R EPLACED MID AND AFT BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100190 20000411 00190 NM 2000 4 11 ASAA9910275 1 19991220 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM ROW 8 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 8 WERE FOUND INOPERATIVE. REPLACED RECEIVE R AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100191 20000411 00191 NM 2000 4 11 ASAA9910276 1 19991220 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM ROW 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 16 PALLET. REPLACED BATTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041100192 20000411 00192 NM 2000 4 11 20000411AP003 1 19991220 A 3350 883200312 BATTERY BOEING 737 737210C 1384459 NM ROW 16 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 16 PALLET. REPLACED BATTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000041200035 20000412 00035 NM 2000 4 12 20000412AP001 1 19991206 A 3230 CABLE BOEING 727 727214 138407R NM MLG LOOSE G O OTHER O OTHER DE DESCENT 1 GL 11 786AT 21692 LAS-IND - FLT 402 - LOUD POPPING UNDER FLOOR IN EMERGENCY WINDOW EXIT ROW, REPORTED BY FLIGHT ATTENDANTS AND PASSENGERS DURING DESCENT AND APPROACH. THE FLOOR IN CABIN AT ROW 19 MOVES AN INCH AND POPS DURING FLIGHT. FOUND LOW CABLE TENSIO N TO LEFT AND RIGHT MLG ALTERNATE EXTENSION AND TO STABILIZER TRIM CABLES, PERFORMED ADJUSTMENTS/TESTS TO ALL THE CABLES AND TESTED AND FOUND OK FOR RETURN TO SERVICE PER MM 32-34-0 AND 27-40-0. FLOOR REPLACED. (M) 2 L 7 3 4F A3WE 2000041200036 20000412 00036 NM 2000 4 12 20000412AP003 1 19991217 A 2612 PIN BOEING 727 727227 1384078 NM NR 1 ENGINE LOOSE G AMTA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 766AT 21999 FLL - FLT 572, AFTER ENGINE SHUTDOWN FIRE BELL SOUNDED WITH NO FIRE LIGHT INDICATION. BELL COULD NOT BE SILENCED AS PER ABNORMAL CHECK LIST WITH EITHER OVERHEAD OR GLARESHIELD CUT OUTS. CLEANED AND RESEATED NR 1 ENGINE LOWER LOOP. CLEANE D AND RESEATED STUB WING CONNECTOR. FOUND PIN PUSHED BACK AT NR 1 ENGINE STUB WING CONNECTOR, RESEATED PIN. RAN ENGINE S, OPS CHECKED FIRE WARNING SYSTEM AND FOUND OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 2000041200037 20000412 00037 NM 2000 4 12 20000412AP004 1 19991203 A 5210 SEAL BOEING 727 727227 1384078 NM PAX DOOR WORN G AMTA O OTHER O OTHER CR CRUISE 1 GL 11 766AT 21999 DURING CRUISE, L-1 DOOR IS VERY NOISY. REPLACED L1 DOOR SEAL PER MM 52-11-711. (M) 2 L 7 3 4F A3WE 2000041200094 20000412 00094 SO 2000 4 12 C2XA99IA592 1 19991115 A 3350 3025101 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19966 145131 IAH - DURING MAINTENANCE INSPECTION, THE LEFT WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 2000041200097 20000412 00097 GL 2000 4 12 WVBAD1499 3 19991205 A 6111 982929 SEAL MCAULY PIPER PA31 PA31350 7103110 SO MCAULY 3DF36C B3DF36C526 GL LT PROPELLER LEAKING I WVBA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3527U 317952141 982929 DURING INSPECTION OF PROPELLER, RED HUB OIL WAS FOUND LEAKING FROM THE BASES OF ALL 3 BLADES. THE INSIDE OF THE SPINNER AND SPINNER BULKHEAD ALSO HAD A NOTICEABLE AMOUNT OF RED OIL ON THEM. THE PROP WAS WASHED DOWN AND THE ENGINE RAN FOR 5 MINUTES AND SHUT DOWN. RED HUB OIL WAS STILL TO BE SEEN LEAKING FROM THE BLADE BASES. AMBIENT TEMPERATURES WERE IN TH E ZERO TO MINUS 20 DEGREE FAHRENHEIT RANGE. SUBMITTER SUSPECTED THE SEAL MATERIAL IS FAILING WITH TIME IN SERVICE, AND EXPOSURE TO SUB-ZERO TEMPERATURES. PROPELLER WAS REPLACED. (X) 1 L 7 2 3O A20SO 5 C 2000041200098 20000412 00098 GL 2000 4 12 WVBAO1399 3 19991205 A 6111 SEAL MCAULY PIPER PA31 PA31350 7103110 SO MCAULY 3DF36C B3DF36C526 GL RIGHT PROPELLER LEAKING I K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 3527U 1146 317952141 981105 DURING INSPECTION OF PROPELLER, RED HUB OIL WAS FOUND LEAKING FROM THE BASES OF ALL 3 BLADES. THE INSIDE OF THE SPINNER AND SPINNER BULKHEAD ALSO HAD A NOTICEABLE AMOUNT OF RED OIL ON THEM. THE PROP WAS WASHED DOWN AND THE ENGINE RAN FOR 5 MINUTES AND SHUT DOWN. RED HUB OIL WAS STILL TO BE SEEN LEAKING FROM THE BLADE BASES. AMBIENT TEMPERATURES WERE IN TH E ZERO TO MINUS 20 DEGREE FAHRENHEIT RANGE. SUBMITTER SUSPECTED THE SEAL MATERIAL IS FAILING WITH TIME IN SERVICE, AND EXPOSURE TO SUB-ZERO TEMPERATURES. PROPELLER WAS REPLACED. (X) 1 L 7 2 3O A20SO 5 C 2000041300016 20000413 00016 WP 2000 4 13 99T64R303AR 1 19990409 A 5730 561235516 SKIN DOUG DC8 DC862 3021970 WP WS 100 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2798, STRINGER 13 AT XRS 100 CORROSION AT FASTENERS RIGHT WING. REMOVED CORROSION IAW 51-1-8. BLENDED AREA IAW BOEI NG MESSAGE M-7200-99-02208 RED D ITEM 6. ARROW AIR (M) 2 L 7 4 4F 4A25 2000041300017 20000413 00017 WP 2000 4 13 99T64R302AR 1 19990509 A 5730 561134029 SKIN DOUG DC8 DC862 3021970 WP WS 172-255 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2175 - LEFT WING, UPPER PLATING SEVERAL AREAS CORRODED BEYOND LIMITS XRS 172-255 STRINGERS 9-11. REMOVED CORROSION I AW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TEMP DOUBLER IAW BOEING MESSAGE M-7200-99-02532, ITEMS 4, 6 AND 10 AND TTS -MQY 99-04-30-012. ACCEPTABLE FOR STRENGTH AS A TEMP REPAIR IAW M-7200-99-0377 REF A. PERM REPAIR TO BE MADE WITHIN 1 YEAR (JUN 2000). VISUAL INSPECTION TO BE MADE AT 3 MONTH INTERVALS FOR FURTHER DAMAGE. NOTIFY COGNIZANT PMI OF THIS RE QUIREMENT. RECORD THIS REQUIREMENT IN THE SHIP RECORDS. ARROW AIR (M) 2 L 7 4 4F 4A25 2000041300018 20000413 00018 WP 2000 4 13 99T64R301AR 1 19990426 A 5730 561135033 SKIN DOUG DC8 DC862 3021970 WP WS 340-358 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2178 - LEFT WING UPPER PLATING AREAS CORRODED BEYOND LIMITS XRS 340-358 AT STRINGER 7. REMOVED CORROSION IAW DC-8 SR M 51-1-8. BLENDED AREA IAW BOEING MESSAGE M-7200-99-02532 PAGE 4 OF 4, ITEMS 2/3 DATED 4-22-99. ARROW AIR (M) 2 L 7 4 4F 4A25 2000041300019 20000413 00019 WP 2000 4 13 99T64R300AR 1 19990408 A 5730 561134030 SKIN DOUG DC8 DC862 3021970 WP WS 341 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2795, CORROSION STRINGER 11XRS 3411 FASTENER HOLE. REMOVED CORROSION IAW DC-8 SRM 51-1-8. BLENDED AREA IAW BOEING M ESSAGE M-7200-99-02208 REF D ITEMS 11-15. ARROW AIR (M) 2 L 7 4 4F 4A25 2000041300020 20000413 00020 WP 2000 4 13 99T64R299AR 1 19990414 A 5730 561235515 SKIN DOUG DC8 DC862 3021970 WP WS 375-454 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2176 - LEFT WING UPPER PLATING SEVERAL AREAS CORRODED BEYOND LIMITS XRS 375-454 STRINGERS 10 AND 11. REMOVED CORROSI ON IAW DC-8 SRM 51-1-8. BLENDED AREAS IAW BOEING MESSAGE M-7200-99-02532 ITEM 16, 17, 19, 28. ARROW AIR (M) 2 L 7 4 4F 4A25 2000041300021 20000413 00021 WP 2000 4 13 99T64R297AR 1 19990814 A 5730 561134030 SKIN DOUG DC8 DC862 3021970 WP WS 50 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 46105 NR 0928 - PREVIOUS REPAIR SKIN CORRODED AND CORROSION EMANATING FROM UNDER REPAIR DOUBLER RIGHT WING UPPER SKIN STATION XW 50 STRINGER 11. REMOVED DOUBLERS. REMOVED CORROSION AND REINSTALLED DOUBLERS IAW BOEING MESSAGE M-7200-99-0228. AR ROW AIR (M) 2 L 7 4 4F 4A25 2000041300042 20000413 00042 NM 2000 4 13 USAA991461 1 19990117 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 500A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 28666 24552 PIT - DURING Q-1 CHECK, FOUND .125 - .25 INCH CRACK IN FRAME STATION 500A BETWEEN STRINGER 8, 9 LEFT. DOUBLER INSTALLE D PER EA NR 53440. (M) 2 L 7 2 4F RT A16WE 2000041300043 20000413 00043 NM 2000 4 13 USAA991460 1 19990117 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 601 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 28666 24552 PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACK IN STATION 601 FRAME STRINGER 17. CUT OUT DAMAGE, INSTALLED FILLERS AND REPA IR DOUBLERS PER EA 53506. (M) 2 L 7 2 4F RT A16WE 2000041300044 20000413 00044 NM 2000 4 13 USAA991459 1 19990117 A 5347 SEAT TRACK BOEING 737 7374B7 1384702 NM BS 355, 363, 365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 28666 24552 PIT - DURING Q-1 CHECK, FOUND 36 INCHES TOTAL SEAT TRACK HAS CORROSION BEYOND LIMITS, FROM BS 355, BS 363 AND BS 365, 12 FT SECTION REMOVED AND REPLACED. CORROSION LEVEL 1. REMOVED AND REPLACED PASSENGER SEAT TRACK, MAJOR REPAIR PER SRM 5 3-00-52 FIG 101. (M) 2 L 7 2 4F RT A16WE 2000041300051 20000413 00051 NM 2000 4 13 USAA990584 1 19990621 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, BL 0 LBL 7 AND RBL 8 FLOORBEAM, CORR OSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 2000041300052 20000413 00052 NM 2000 4 13 USAA990583 1 19990621 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL1 AND LBL 11 FLOORBEAM. CORROSIO N LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 2000041300053 20000413 00053 NM 2000 4 13 USAA990582 1 19990621 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL 12 T-CAP. CORROSION LEVEL 2, CO RROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205.. (M) 2 L 7 2 4F RT A16WE 2000041300054 20000413 00054 NM 2000 4 13 USAA990581 1 19990621 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 60 INCH AREA OF CORROSION AT STATION 986.5 FLOORBEAM. INSTALLED UPPER T -CAP PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2000041300055 20000413 00055 NM 2000 4 13 USAA990580 1 19990621 A 5320 WEB BOEING 737 737301 1384611 NM LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AFT RIGHT LAV FILL CONN ON FLOOR WEB, CORROSI ON LEVEL 2. NEW WEB INSTALLED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000041300056 20000413 00056 NM 2000 4 13 USAA990579 1 19990621 A 5311 FRAME BOEING 737 737301 1384611 NM BS 993.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION ON INBOARD J CHANNEL BS 993.5 FRAME AT WL 208 .1, CORROSION LEVEL 2. INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 2000041300057 20000413 00057 NM 2000 4 13 USAA990578 1 19990621 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT STATION 986.5 LBL 24 FLOORBEAM, CORROSION LEVEL 2. FABRICATED NEW PART PER SRM 51-40-02 AND DWG 6561381. (M) 2 L 7 2 4F RT A16WE 2000041300058 20000413 00058 NM 2000 4 13 USAA990576 1 19990621 A 5320 CHANNEL BOEING 737 737301 1384611 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 986.5 RBL 24 HOT CHANNEL. CORROSION LE VEL 2. INSTALLED FABRICATED PART PER SRM 51-40-04 AND DWG 65-61381. (M) 2 L 7 2 4F RT A16WE 2000041300059 20000413 00059 NM 2000 4 13 USAA990575 1 19990621 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION ON T-CAP AND AROUND NUT PLATE HOLES AT BS 294.5 FROM LBL 12 TO RBL 7. CORROSION TASK NR C53-107-102-02. REMOVED ALL CORROSION ON T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000041300060 20000413 00060 NM 2000 4 13 USAA990574 1 19990621 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 270 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 20 INCH AREA OF CORROSION BS 270, LBL 10 - RBL 10 FLOOR SUPPORT. INST ALLED NEW Z-ANGLE PER TR 53-20-04 AND EA 64680. (M) 2 L 7 2 4F RT A16WE 2000041300061 20000413 00061 NM 2000 4 13 USAA990573 1 19990621 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727D CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 12 INCH AREA OF FUSELAGE OF CORROSION BETWEEN NR 3 VHF ANTENNA MOUNT S TATION 727D PLUS 3 TO 727D PLUS 15 AND INTERIOR SKIN FUSELAGE BL 0. REMOVED EXISTING DOUBLER AND REPLACED WITH LARGER S IZE DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 2000041300062 20000413 00062 NM 2000 4 13 USAA990565 1 19990621 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH, 1 INCH AND .75 INCH CRACK AT STATION 178 RIGHT SIDE PLUS 6 IN CHES WL 200 AT 4.75 AND 6.75 BULKHEAD. INSTALLED DOUBLER PER SRM 53-10-07. (M) 2 L 7 2 4F RT A16WE 2000041300063 20000413 00063 NM 2000 4 13 USAA990484 1 19990621 A 5320 6546877143 WEB BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 38169 23235 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .300 INCH CRACK AT STATION 727 STRINGER 18A LEFT MAIN WHEEL WELL SHEAR WEB. INSTALLED DEFECTIVE PART WITH IDENTICAL PART PER BOEING 6546877 BLUEPRINT. (M) 2 L 7 2 4F RT A16WE 2000041300064 20000413 00064 WP 2000 4 13 99T64R286AR 1 19990409 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1500 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1738 - CRACK L2 DOOR CUT OUT UPPER REAR CORNER STATION 1500. CUT OUT DAMAGED AREA IAW DC-8 SRM 53-2-0. FABRICATED F ILLER AND DOUBLERS IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW DC-8 SRM 53-2-0. ARRO W AIR (M) 2 L 7 4 4F 4A25 2000041300065 20000413 00065 WP 2000 4 13 99T64R285AR 1 19990331 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1140 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1498, CORROSION FRAME 1140 UPPER CHORD, WEB SHEER TIE FROM L33R - L31L. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABR ICATED FRAME SPLICES IAW DC-8 SRM 53-2-9. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED IAW DC-8 SRM 53-2-0. ARROW AIR (M) 2 L 7 4 4F 4A25 2000041300066 20000413 00066 WP 2000 4 13 99T64R284AR 1 19990320 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 878 CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1966, LEFT WING OUTBOARD LEADING EDGE OUTBOARD SECTION, CORROSION STATION 878. REMOVED CORROSION IAW DC-8 SRM 51-1-8 . CUT OUT DAMAGED AREA IAW DC-8 SRM 57-2-0. FABRICATED DOUBLER IAW DC-8 SRM 57-2-1. TREATED AND PRIMED IAW DC-8 51-1- 8. INSTALLED DOUBLER IAW DC-8 SRM 57-2-1. ARROW AIR (M) 2 L 7 4 4F 4A25 2000041300067 20000413 00067 WP 2000 4 13 99T64R283AR 1 19990625 A 7921 7760680 DUCT DOUG DC8 DC862 3021970 WP OIL COOLER CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 3050 - NR 3 TURBO COMPRESSOR OIL COOLING DUCT CRACKED. WELDED CRACK IAW BOEING MESSAGE M-7200-99-05081. ARROW AIR ( M) 2 L 7 4 4F 4A25 2000041300068 20000413 00068 NM 2000 4 13 USAASB99265 1 19991106 A 2910 LINE BOEING 737 737301 1384611 NM RT MLG LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 356US 23559 PHL - FLT 2204 - AFTER TAKEOFF AND GEAR RETRACTION FROM PHL, FLIGHT LOST A SYSTEM HYDRAULICS. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. CAPTAIN TAXIED AIRCRAFT TO WITHIN 30 FEET OF GATE AND WAS THEN TOWED IN FRO M THERE. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK ACTUATOR INBOARD HYDRAULIC L INE. SERVICED RESERVOIR. OPERATIONAL CHECK AND LEAK CHECK GOOD PER MM 32-32-41. ALSO, REMVOED AND REPLACED A HYDRAULI C SYSTEM MAIN FILTER AND CASE DRAIN FILTERS FOR ENGINE DRIVEN PUMPS, ELECTRIC PUMPS AND STANDBY PUMP. NO METAL FOUND. (M) 2 L 7 2 4F RT A16WE 2000041300069 20000413 00069 NM 2000 4 13 USAA991002 1 19991013 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH AREA OF CORROSION FLOORBEAM 967 UPPER CHORD AT LBL 27.5, CORROS ION LEVEL 1. REPAIRED DOUBLER PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 2000041300070 20000413 00070 NM 2000 4 13 USAA991023 1 19991013 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986.5-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION FLOORBEAM BETWEEN STATION 986.5 BY 1016 DIAGO NALLY FROM RBL 19 TO RBL 5. CORROSION LEVEL 1. REPAIRED WITH IDENTICAL PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000041300071 20000413 00071 NM 2000 4 13 USAA991022 1 19991013 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM STATION 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM UPPER CHORD STATION 986 FROM BL 3.5 TO RBL 9.5, CORROSION LEVEL 1. INSTALLED DOUBLER PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 2000041300072 20000413 00072 NM 2000 4 13 USAA991032 1 19991013 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER T-CAP AT NUTPLATE HOLES 10 INCH AT BS 294.5, LBL 22 TO RBL 22, BEAM CAP. CORROSION LEVEL 2. INSTALLED T-CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 2000041300073 20000413 00073 NM 2000 4 13 USAA991031 1 19991013 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 285-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 349US 35403 23552 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 59 INCH AREA OF CORROSION AT STATION 285-344, WL 208.1 Z-ANGLE. CORRO SION LEVEL 2. REMOVED AND REPLACED Z-ANGLE EPR SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 2000041300074 20000413 00074 WP 2000 4 13 99T64R389AR 1 19990518 A 5230 AE2420 FASTENER DOUG DC8 DC862 3021970 WP CARGO DOOR MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 46105 NR 2342 AND 2370, FOUND DURING C-CHECK, MISSING, BROKEN AND/OR LOOSE FASTENER AND MISSING SHIMS (JOGGLE). INSTALLED FAS TENERS IAW DWG AS11041. (M) 2 L 7 4 4F 4A25 2000041300075 20000413 00075 WP 2000 4 13 99T64R388AR 1 19990305 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1340-1360 MISREPAIRED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 1071 - EVALUATE SKIN REPAIR AND CORRECT IF REQUIRED BETWEEN L29L - L28L BETWEEN FRAMES 1340-1360 LT. REMOVED DAMAGED SKIN, FABRICATED FILLER AND DOUBLER AND INSTLLED PER EO 99-028. (M) 2 L 7 4 4F 4A25 2000041300077 20000413 00077 WP 2000 4 13 ASAA9980338 1 19991226 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300078 20000413 00078 WP 2000 4 13 ASAA9980337 1 19991224 A 3397 WIRE DOUG DC9 DC983 3022083 WP DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 SEA - AFTER ARRIVAL OF FLIGHT 557, CRWE REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. . RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300079 20000413 00079 WP 2000 4 13 ASAA9980336 1 19991224 A 3350 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300080 20000413 00080 WP 2000 4 13 ASAA9980335 1 19991223 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 53453 PHX - PRIOR TO DEPARTURE OF FLIGHT 721, CREW REPORTED THE FORWARD 2 EMERGENCY FLOOR TRACK RED LIGHTS WERE INOPERATIVE. SECURED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300081 20000413 00081 WP 2000 4 13 ASAA9980334 1 19991222 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - PRIOR TO DEPARTURE OF FLIGHT 100, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED WIRING I NFLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300082 20000413 00082 WP 2000 4 13 ASAA9980333 1 19991222 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 13-15 FAILED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 13 TO 15 WERE FOUND INOPERATIVE. REPLACED WI RING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300083 20000413 00083 WP 2000 4 13 ASAA9980332 1 19991222 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300084 20000413 00084 WP 2000 4 13 ASAA9980330 1 19991219 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - PRIOR TO DEPARTURE OF FLIGHT 386, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300085 20000413 00085 WP 2000 4 13 ASAA9980244 1 19991107 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 PDX - DURING MAINTENANCE CHECK, ONE OVERHEAD EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2000041300086 20000413 00086 WP 2000 4 13 ASAA9980230 1 19991105 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 PDX - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000041300087 20000413 00087 WP 2000 4 13 ASAA9980226 1 19991102 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP ROW 9-26 INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PHX - DURING C-CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 9 TO 26 WERE FOUND INOPERATIVE. REPLACED THE POWER SUP PLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2000041300205 20000413 00205 NE 2000 4 13 AALA19991751 2 19991118 A 7200 ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 2 STALLED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1756 48491 MIA - FLT 1769 - ON CLIMB-OUT FROM MIA, NR 2 ENGINE COMPRESSOR STALLS PASSING 12,000 FOOT CLIMB POWER. AIRCRAFT RETURNE D AND LANDED MIA WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL WITH ENGINE AT IDLE FOR THREE MINUTES PRIOR TO ENGINE SHUTDOWN. AIRCRAFT FERRIED TO DFW FOR ENGINE CHANGE. ARRIVED AND LANDED DFW WITHOUT INCIDENT. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. ENGIEN FAILURE WAS DUE TO LIBERATION OF A FITH STAGE HIGH COMPRESSOR BLADE PART NR K65P08 IN THE DOVETAIL. (M) 2 L 7 3 4F 4 F RT A22WE E31N3 2000041300226 20000413 00226 WP 2000 4 13 G60A044 1 19990209 A 7120 BOLT DOUG DC10 DC1030 3023501 WP NR 3 PYLON LOOSE A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 605GC 97399 47925 NR 3 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON LOWER FORWARD SIDE ATTACH BOLTS LOOSE. INSPECTED FORWARD MOUNT TRUSS F ITTINGS AS PER DRAWING AVB 7011 '2' AND PER BOEING JAC GC 116-02 AND S/B A54-99. REFER TO SINGLE ITEM SQUAWK NUMBERS 23 7887 AND 228931. COMPLIED WITH GEMINI EO NR 00-5411-009. (M) 2 L 7 3 4F A22WE 2000041300227 20000413 00227 WP 2000 4 13 G6OA043 1 19990209 A 7120 BOLT DOUG DC10 DC1030 3023501 WP NR 1 PYLON LOOSE A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 605GC 97399 47925 NR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON, HAS SIX LOOSE PYLON BOX BOLTS ON LOWER FORWARD SIDE, AND THREE HI-LOCK S ON LOWER FORWARD SHOWS EVIDENCE OF SPINNING. INSPECTED FWD MOUNT TRUSS FITTINGS AS PER DRAWING AVB 7000-503 AND 504 P ER BOEING JAC GC 116-01 AND S/B A54-00, REVISION 4 DATED FEB 15, 1995. (M) 2 L 7 3 4F A22WE 2000041300228 20000413 00228 WP 2000 4 13 G6OA041 1 19990204 A 7120 BOLT DOUG DC10 DC1030F 3023504 WP NR 1 PYLON LOOSE A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 602GC 98919 47923 NR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON MOUNT BOLTS SHOWS SLIPPAGE ON TORQUE STRIPE INDEX. PERFORMED RE-WORK A S REQUIRED BY REF DC-10-SB A54-00, REVISION 4 DATED FEB 15, 1995. (M) 2 L 7 3 4F RT A22WE 2000041300229 20000413 00229 WP 2000 4 13 G6OA042 1 19990204 A 7120 BOLT DOUG DC10 DC1030F 3023504 WP NR 3 PYLON LOOSE A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 602GC 98919 47923 NR 1 ENGINE FORWARD MOUNT TRUSS FITTING TO PYLON MOUNT BOLTS SHOWS SLIPPAGE ON TORQUE STRIPE INDEX. PERFORMED RE-WORK A S REQUIRED BY REF; DC-10 SB A54-99, REVISION 4 DATED FEB 15, 1995. (M) 2 L 7 3 4F RT A22WE 2000041300234 20000413 00234 NE 2000 4 13 2000ZZZX729 2 19990728 A 7240 408126201 HOUSING HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 7104 LE45134EA HOUSING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300235 20000413 00235 NE 2000 4 13 2000ZZZX730 2 19990728 A 7240 408126301 COVER HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 7104 LE45134EA COVER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300236 20000413 00236 NE 2000 4 13 2000ZZZX731 2 19990728 A 7230 410101003 VANE HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 TRMC9476 7104 LE45134EA VANE CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300237 20000413 00237 NE 2000 4 13 2000ZZZX733 2 19990728 A 7240 410106802 SPRING HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 7104 LE45134EA SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300238 20000413 00238 NE 2000 4 13 2000ZZZX734 2 19990708 A 7250 411100720 SHROUD HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 7104 LE45134EA EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300239 20000413 00239 NE 2000 4 13 2000ZZZX736 2 19990728 A 7240 430124203 BEARING HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 1688 7104 LE45134EA BREARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300240 20000413 00240 NE 2000 4 13 2000ZZZX737 2 19990728 A 7240 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 836 8F950036 7104 LE45134EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300241 20000413 00241 NE 2000 4 13 2000ZZZX738 2 19990728 A 7240 4301250601 SEAL HONEYWELL 1783 BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 836 1783 7104 LE45134EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300242 20000413 00242 NE 2000 4 13 2000ZZZX739 2 19990728 A 7230 430404701 SEAL HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 936 4J955 7104 LE45134EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300243 20000413 00243 NE 2000 4 13 2000ZZZX740 2 19990826 A 7420 430111201 IGNITION LEAD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 534 4399 7111 IGNITION LEAD HAD INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300244 20000413 00244 EU 2000 4 13 2000ZZZX743 1 19991225 A 7714 430106202 PICKUP HONEYWELL BOLKMS 117 BK117B1 5626012 EU NR 1 ENGINE INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 161 991402600292 7229 PICK-UP UNIT OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300247 20000413 00247 EU 2000 4 13 2000ZZZX749 1 19991217 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 102LN 537 3065 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000041300249 20000413 00249 NE 2000 4 13 2000ZZZX751 2 19991119 A 7240 430150601 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 371 1930 7063 LE45144EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300250 20000413 00250 NE 2000 4 13 2000ZZZX752 2 19991018 A 7210 230001303 BEARING BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE GEARBOX CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 404EM 299 47514 LE47003EA BEARING HAD EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H9SW E5NE 2000041300251 20000413 00251 SW 2000 4 13 2000ZZZX753 1 19991018 A 6322 408204002 GEAR HONEYWELL BELL 222 222U 1182140 SW COOLER BLOWER SPALLED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 404EM 299 47514 GEAR MAKING METAL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H9SW 2000041300252 20000413 00252 NE 2000 4 13 2000ZZZX755 2 19990519 A 7240 430150601 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 783 1641 7127 LE45382EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300253 20000413 00253 NE 2000 4 13 2000ZZZX756 2 19990519 A 7250 411100720 SHROUD HONEYWELL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 783 7127 LE45382EA SHROUD HAD EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300258 20000413 00258 NE 2000 4 13 2000ZZZX763 2 19991214 A 7420 430111202 IGNITION LEAD HONEYWELL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 654 2569 7231 INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 2000041300263 20000413 00263 GL 2000 4 13 2000ZZZX768 2 19990924 A 7230 E23034784 GEAR AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL COMPRESSOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 53LH 407 CI15055 5093 GEAR TEETH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H11EU E4CE 2000041300264 20000413 00264 NE 2000 4 13 2000ZZZX769 2 19990519 A 7310 430167601 MANIFOLD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE FUEL SYSTEM MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 185 1ZM02554 7127 LE45382EA IMPROPER NOZZLE SPRAY PATTERN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300265 20000413 00265 NE 2000 4 13 2000ZZZX771 2 19990806 A 7240 410106802 SPRING HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SECTION WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 424MB 582 7082 LE45115EA SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300266 20000413 00266 EU 2000 4 13 2000ZZZX773 1 19990806 A 7920 416176003 TUBE HONEYWELL BOLKMS 117 BK117A3 5626015 EU OIL SYSTEM LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 424MB 582 7082 TUBE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300267 20000413 00267 NE 2000 4 13 2000ZZZX774 2 19990806 A 7310 416183001 TUBE HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE FUEL SYSTEM LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 424MB 582 7082 LE45115EA TUBE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300268 20000413 00268 NE 2000 4 13 2000ZZZX775 2 19990806 A 7240 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 424MB 582 8F950023 7082 LE45115EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300269 20000413 00269 NE 2000 4 13 2000ZZZX776 2 19990612 A 7240 430124203 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURBINE SECTION FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 71703 1412 7227 LE45755EFA BEARING HAD EXCESSIVE PITTING (FAILED ON TEST CELL). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 2000041300270 20000413 00270 NE 2000 4 13 2000ZZZX778 2 19991119 A 7310 417187001 TUBE HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE FUEL SYSTEM LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 163BK 371 7063 LE45144EA TUBE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300271 20000413 00271 EU 2000 4 13 2000ZZZX779 1 19991221 A 6700 L672M20905207 CONTROL ROD UROCOP EC135 EC135P1 8680990 EU YAW ACTUATOR BROKEN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 907 EC1350054 CONTROL ROD WORN BEYOND SERVICEABLE LIMITS. CONTROL ROD BROKE WHILE REMOVING FROM YAW ACTUATOR. REPLACED WITH NEW UNIT , CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2000041300272 20000413 00272 NE 2000 4 13 2000ZZZX781 2 19990930 A 7240 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 420MB 397 8F950279 7077 LE45242EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300273 20000413 00273 NE 2000 4 13 2000ZZZX782 2 19990930 A 7240 430150601 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 420MB 397 2108 7077 LE45242EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041300277 20000413 00277 EU 2000 4 13 2000ZZZX787 1 19991115 A 6340 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU ROTOR OIL SYSTEM INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 293 W52235 2014 SWITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 2000041300278 20000413 00278 EU 2000 4 13 2000ZZZX788 1 19991105 A 6340 6607A2114 SWITCH W65470 BOLKMS 105 BO105LSA3 5626020 EU ROTOR OIL SYSTEM INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 248 2014 SWITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 2000041300279 20000413 00279 EU 2000 4 13 2000ZZZX789 1 19990921 A 6340 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117B1 5626012 EU MAIN ROTOR MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 188 61033A101 7231 TRANSMITTER CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300280 20000413 00280 EU 2000 4 13 2000ZZZX790 1 19991214 A 5210 11724274101 GUIDE BOLKMS 117 BK117B1 5626012 EU DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 62LF 575 7163 GUIDE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300281 20000413 00281 EU 2000 4 13 2000ZZZX791 1 19991214 A 5210 1172427302 GUIDE BOLKMS 117 BK117B1 5626012 EU DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 62LF 556 7163 GUIDE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300282 20000413 00282 EU 2000 4 13 2000ZZZX792 1 19991127 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU TORQUE INDICATOR INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 49 1070 7169 TRANSUDCER UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300283 20000413 00283 EU 2000 4 13 2000ZZZX793 1 19990804 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU TORQUE INDICATOR INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 62LF 173 7163 TRANSDUCER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300284 20000413 00284 EU 2000 4 13 2000ZZZX794 1 19991103 A 7931 IPT70RT11000250G TRANSDUCER BOLKMS 117 BK117B1 5626012 EU ENGINE OIL ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 164 60145B72 7229 TRANSDUCER ERRATIC. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300285 20000413 00285 EU 2000 4 13 2000ZZZX795 1 19990815 A 7931 IPT70RT11000250G TRANSDUCER BOLKMS 117 BK117B1 5626012 EU ENGINE OIL INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 215 58996A136 7229 TRANSDUCER UNIT OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300286 20000413 00286 EU 2000 4 13 2000ZZZX796 1 19990821 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU TORQUE INDICATOR LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 821 7229 TRANSDUCER LEAKING AND HAS INACCURATE READINGS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300287 20000413 00287 EU 2000 4 13 2000ZZZX797 1 19990830 A 6400 1053170018 BOLT BOLKMS 117 BK117B1 5626012 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 417BK 936 7143 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300288 20000413 00288 EU 2000 4 13 2000ZZZX799 1 19990904 A 6400 10531717 BOLT BOLKMS 117 BK117A3 5626015 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MV 407 7089 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300290 20000413 00290 EU 2000 4 13 2000ZZZX801 1 19990726 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 94 13260 S754 TRANSMMITTER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 2000041300307 20000413 00307 SO 2000 4 13 C2XA99IA638 1 19991225 A 3350 3025101 LIGHT EMB 145 EMB145 SO FUSELAGE INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22971 145149 IAH - DURING MAINTENANCE INSPECTION, THE RIGHT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM-33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 2000041300309 20000413 00309 EU 2000 4 13 2000ZZZX822 1 19991029 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU TORQUE INDICATOR ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 61LF 38 984 7230 TRANSDUCER ERRATIC. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041300358 20000413 00358 NE 2000 4 13 2000ZZZX772 2 19990806 A 7250 411100720 BLADE HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 424MB 582 7082 KE45115EA EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041700014 20000417 00014 EU 2000 4 17 20000417AP001 1 19991223 A 5347 PLAL7075T6511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 ABI - SEAT TRACK CORRODED BEYOND LIMITS AT FS 594.8 TO FS 686.8 TRACK 18L. REMOVED AND REPLACED SEAT TRACK AT 18.3L, 92 INCH SECTION. (M) 2 L 7 2 4T RT A52EU 2000041700015 20000417 00015 EU 2000 4 17 20000417AP002 1 19991115 A 5347 7253799383 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 219AE 340B219 FOUND SEAT TRACK AT BL 18.3L AND BL 0.0 CORRODED BEYOND SRM LIMITS. REMOVED FASTENERS EXISTING SEAT TRACKS. DRILLED FA STENERS HOLES ON NEW SEAT TRACK EXTRUSIONS AND TREATED. INSTALLED NEW SEAT TRACKS AND SECURED. APPLIED DINOTROL TO SEA T TRACK ANS SUPPORTS. WORK DONE IAW SAAB 340 AMM 20-10-00, SRM 72LKS 3079 51-40-21, 51-40-22, 51-40-23, 51-40-25, 51-20 -42, 51-20-43, 51-20-45 AND STANDARD SRM REPAIR PRINCIPLES. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 2000041700026 20000417 00026 EU 2000 4 17 20000417AP007 1 19991227 A 5347 PLAL7075T6511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 SEAT TRACK CORRODED BEYOND LIMITS AT BL 0.0. REMOVED AND REPLACED 12 INCH OF SEAT TRACK AT BL 0.0. (M) 2 L 7 2 4T RT A52EU 2000041700039 20000417 00039 EU 2000 4 17 20000417AP006 1 19991227 A 5347 PLAL7075T6511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 ABI - FOUND CORROSION BEYOND SRM LIMITS ON SEAT TRACK 18.3L AT FS 300. REMOVED AND REPLACED 12 INCH SECTION OF SEAT TRA CK. (M) 2 L 7 2 4T RT A52EU 2000041700053 20000417 00053 NM 2000 4 17 TSAA200033058 1 19991123 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN INOPERATIVE A TSAA O OTHER O OTHER NR NOT REPORTED 1 WP 13 726AL 22426 REPLACED BATTERY FOR THE NR 3 POSITION FOR THE EMERGENCY FLOOR PROX LIGHT. OPS CHECK OK. (M) 2 L 7 2 4F A16WE 2000041700054 20000417 00054 NE 2000 4 17 2000ZZZX732 2 19990728 A 7240 410106701 SEAL HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 7104 LE45134EA SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041700055 20000417 00055 NE 2000 4 17 2000ZZZX735 2 19990728 A 7250 411104061 SEAL HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 836 7104 LE45134EA LABYRINTH SEAL EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041700059 20000417 00059 EU 2000 4 17 2000ZZZX742 1 19990915 A 7714 430106202 PICKUP BOLKMS 117 BK117B1 5626012 EU NR 1 ENGINE ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 480 97A0130 7169 PICK-UP ERRATIC. REPLACED IWTH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041700060 20000417 00060 2000 4 17 2000ZZZX745 4 19990108 A 3422 066304607 PLATE HONEYWELL SNIAS 350 AS350B2 8680813 EU INDICTOR LOOSE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 102LN 543 86725 3065 FACE PLATE WORKED LOOSE FROM MAIN HOUSING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000041700062 20000417 00062 EU 2000 4 17 2000ZZZX757 1 19991224 A 7810 L713M2054101 EXHAUST PIPE UROCOP EC135 EC135P1 8680990 EU ENGINE CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 922 EC1350054 EXHAUST STACK CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 2000041700063 20000417 00063 EU 2000 4 17 2000ZZZX759 1 19991120 A 6520 350A33200405 SPIDER GEAR SNIAS 350 AS350B3 8680954 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 104LN 317 M0949 3134 EXCESSIVE PLAY BETWEEN SLIDER AND CONTROL TUBE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000041700065 20000417 00065 NE 2000 4 17 2000ZZZX777 2 19991119 A 7240 413102002 COMBUSTION CHAMB HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 371 7063 LE45144EA EXCESSIVE BURN IN SOME AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041700066 20000417 00066 2000 4 17 2000ZZZX780 4 19991216 A 3454 071010520000 TRANSMITTER SNIAS 350 AS350B3 8680954 EU VOR SYSTEM INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 104LN 394 55464 3134 TRANSMITTER UNIT INOPERATIVE. REGRESSES 20 DEGREES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 2000041700069 20000417 00069 EU 2000 4 17 2000ZZZX798 1 19990809 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A3 5626015 EU TORQUE INDICATOR INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 625MB 264 976 7108 TRANSDUCER INOPER ATIVE. CAUSES NR 2 TORQUE NEEDLE TO READ 20 PERCENT HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041700077 20000417 00077 NM 2000 4 17 CA000110016 1 19991220 A 5320 B737200 WINDOW POST BOEING BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 57388 702707 (CAN) INSP REVEALED CRACKS OF C-D WINDOW POST UPPER OTBD CORNERS OF LT AND RT WINDOWS. ROUTED OUT TO REVEAL UNDER SKIN ALSO CRACKED FROM SITE MARKS. REPAIRED PER BOEING TELEX. 2 L 7 2 4F 4 F RT A16WE E2EA 2000041700078 20000417 00078 NM 2000 4 17 CA000110017 1 19991220 A 5740 69598861 FITTING BOEING BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE WING DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 702707 (CAN) REMOVED FITTING FOR BEARING REWORK AND FOUND HIDDEN DAMAGE. THREE OF FOUR BOLTS FROZEN IN BORES, TWO BOLTS SHEARE D, EVIDENCE OF EXTENSIVE CORROSION TO SHEAR FACE. FWD INBD BOLT CUT FOR REMOVAL. FITTING REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 2000041700080 20000417 00080 EU 2000 4 17 2000ZZZX821 1 19991029 A 7797 430121302 WIRE HONEYWELL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 ENGINE SHORTED A K NONE O OTHER IN INSP/MAINT 1 NM 11 61LF 567 961048400017 7230 LE45988EF INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 2000041700081 20000417 00081 EU 2000 4 17 2000ZZZX823 1 19991022 A 8000 151PS01A6A SWITCH BOLKMS BK117 BK117C1 5626025 EU STARTER STUCK A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117SU 7527 SWITCH STICKS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H13EU 2000041700082 20000417 00082 NM 2000 4 17 CA000110018 1 19991222 A 2917 72909 REGULATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE HYD TANK FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 42962 542 709396 HYDRAULIC PRESSURE REGULATOR FAILED ON DESCENT. (ADP) 2 L 7 2 4F 4 F A16WE E2EA 2000041700083 20000417 00083 NM 2000 4 17 CA000110020 1 19991223 A 3500 106017425 LINE BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE OXYGEN SYSTEM RUPTURED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 655389 (CAN) FLIGHT CREW HEARD A BANG, ISOLATED TO 02 PRESSURE DROPPING. FLEX LINE TO THE FOS 02 REGULATOR FAILED, REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2000041700084 20000417 00084 NM 2000 4 17 CA000110021 1 19991223 A 2612 65249203 CONTROLLER BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE FIRE DETECTOR FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA 666237 (CAN) ON FINAL APPROACH, WHEELWELL FIRE WARNING OCCURRED, W/W FIRE DRILL CARRIED OUT. LIGHT WENT OUT IMMEDIATELY AFTER GEAR EXTENDED AND STAYED OUT. AFTER INSPECTION, NO EVIDENCE FOUND. WHEELWELL FIRE CONTROL UNIT REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 2000041700085 20000417 00085 EU 2000 4 17 CA000110030 1 19991220 A 2430 914F5696 GCU WESTINGHOUSE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU GENERATOR FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA OT3231A 9288 (CAN) PILOTS REPORTED DURING BOARDING PROCESS A HEAVY SMOKE SMELL FROM THE MAIN CB PANEL EMANATING THROUGHOUT THE COCKPI T. CREW UNABLE TO PINPOINT SOURCE. A/C SHUT DOWN AND PASSENGERS DEPLANED. REPLACED COCKPIT GCU AND AC BUS CONTACTOR. 2 L 7 2 4F 4 F RT A20EU E2EU 2000041700086 20000417 00086 EU 2000 4 17 CA000110031 1 19991231 A 3230 A7872200 SPRING 200642005 FOKKER F28 F28MK1000 4990808 EU UPLOCK BROKEN W O OTHER J WARNING INDICATION AP APPROACH 1 CA DRG299270 (CAN) ON APPROACH ON DOWN SELECTION 5 GREEN LIGHT BUT THE LT MLG RED LIGHT REMAINED ON. GEAR CYCLED, SAME. MAINT REQUEST ED CREW CYCLE GEAR WITH UTILITY PUMPS OFFLOADED, THIS CONFIRMED FAULT AS IND. LT GEAR DOOR UPLOCK SPRING BROKEN, REPLAC ED. 2 L 7 2 4F RT A20EU 2000041700087 20000417 00087 NM 2000 4 17 CA000110076 1 19991122 A 2400 FRF6327PW08 CONNECTOR BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE NLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 30680 (CAN) DURING INSPECTION ON THE ELECTRICAL HARNESS IN THE NOSE GEAR WHEELWELL, THE ELECTRICAL HARNESS BRACKET ALD393 AND THE CONNECTOR D40488P FOUND CONTAMINATED WITH WATER ON 25 PERCENT OF CONNECTOR AREA. CAUSES WIRES TO BECOME BRITTLE AT CRIMPED AREA. THE BACKSHELL OF THE CONNECTOR WAS SEIZED DUE TO CORROSION. CONNECTOR, BACKSHELL AND PLUG REPLACED. SI 3-24-007 APPLIES. 2 L 7 2 4F 4 F RT A2NM E12EU 2000041700088 20000417 00088 WP 2000 4 17 CA000110088 1 19991227 A 3244 TIRE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE MLG FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA P657374D (CAN) RT FLAPS DAMAGED DUE TO NR 3 TIRE TREAD SEPARATION, WHEEL REPLACED AND FLAPS REPAIRED. 2 L 7 2 4F 4 F A6WE E2EA 2000041700119 20000417 00119 2000 4 17 2000ZZZX784 4 19991223 A 3457 071015530200 ANTENNA HONEYWELL BOLKMS 117 BK117B1 5626012 EU GPS INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911VU 670 25376 7141 ANTENNA INOPERATIVE. WILL NOT LOCK-ON SATELLITE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041700120 20000417 00120 2000 4 17 2000ZZZX825 4 19991016 A 3120 E19558 INDICATOR BOLKMS BK117 BK117C1 5626025 EU CYCLE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117SU 99 7527 COUNTER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H13EU 2000041700152 20000417 00152 EA 2000 4 17 20000407SH035 2 19991006 A 7414 6351 MAGNETO PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA ENGINE MALFUNCTIONED E LABA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION IN INSP/MAINT 1 AL 05 6117J 213 327640095 L1972548A AIRCRAFT VERY HARD TO START. MAGNETO AND ENGINE HAD TOTAL OF 213.0 HOURS SINCE NEW. (X) 1 L 7 1 3O 3 O A3SO 1E4 2000041700240 20000417 00240 EU 2000 4 17 2000ZZZX744 1 19991021 A 7714 430106202 PICKUP BOLKMS 117 BK117B1 5626012 EU NR 1 ENGINE ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 747 981402500014 7229 PICK-UP ERRATIC. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 2000041700244 20000417 00244 NE 2000 4 17 2000ZZZX770 2 19990806 A 7240 410106701 SEAL HONEYWELL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 424MB 582 7082 LE45115EA SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTIVE PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2000041800155 20000418 00155 NM 2000 4 18 QXEA9902652 1 19991221 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 825PH 213 PDX - CORROSION ON UNDER SIDE OF HORIZONTAL STIFFENING RIB ON AFT FLANGE OF FRAME 253.400, BETWEEN STRINGERS 24 LT AND 2 5 LT. REPAIRED IAW HORIZON AIR EA 9-53-534. 2 H 7 2 4T RT A13NM 2000041900222 20000419 00222 EU 2000 4 19 SIMA3642 1 19991229 A 5347 D53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 355AT 355 SAW - DURING CPCP INSPECTION, FOUND LEFT MIDDLE OUTBOARD AND LEFT MIDDLE INBOARD SEAT TRACKS CORRODED BEYOND LIMITS. RE MOVED AND REPLACED LEFT MIDDLE OUTBOARD AND INBOARD SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 2000041900323 20000419 00323 NE 2000 4 19 CA000301008 1 19991030 A 6320 S613723054001 BEVEL GEAR SKRSKY S61352060004 SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE M/R GEARBOX BROKEN W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA 437 A1H2666211 295089 (CAN) MAIN GEAR BOX BEVEL GEAR HAS A BROKEN TOOTH. BEVEL GEAR SENT TO ENGINEERING FIRM FOR ANALYSIS AS TO DETERMINE THE CAUSE OF FAILURE. FRACTURE OCCURRED AT HEEL OF THE TOOTH AND FAILURE OCCURRED AS A RESULT OF A FATIGUE MODE OF PROGRESSI VE FAILURE. 2 G 7 2 4U 4 U 1H15 1E3 2000042000162 20000420 00162 EA 2000 4 20 CA990513002 2 19990503 A 7322 30764 FLOAT PRECISION MA45 ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA CARBURETOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1007 75058206 L2499940A (CAN) THE CARBURETOR FLOAT PIVOT POINT WAS WORN AND THE FLOAT BRACKET (P/N 136-62) WAS BENT. THESE TWO PROBLEMS CAUSED THE FLOAT PONTOON TO RUB AGAINST THE CARBURETOR BOWL ASSEBLY. THERE WAS MINIMAL EVIDENCE OF THIS ON THE FLOAT PONTOON. T HIS MAY HAVE CAUSED THE FLOAT TO HANG UP. ALL PARTS WERE REPAIRED OR REPLACED AND THE CARBURETOR WAS RETURNED TO SERVIC E. 1 G 7 1 3O 3 O H11NM E295 2000042000163 20000420 00163 NE 2000 4 20 CA990513005 3 19990505 A 6111 AG10045 BLADE PWA R1340AN1 AYRES S2 S2R 7630202 CE PWA R1340 R1340AN1 52016 NE HAMSTD 12D 12D40 NE PROPELLER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 1388 ZP103455 ZP103455 778098 (CAN) INSPECTION FOUND THE PROPELLER BLADE FILLETS CORRODED ON BOTH BLADES AND THE COUNTERWEIGHTS (CWT) BUSHINGS CRACKED , TWO LONG BEARING RACES DENTED, ONE CAP RACE CORRODED AND ONE BROKEN. THE BLADES WERE MACHINED TO REMOVE THE CORROSION AND ALL OUTER PARTS WERE REPLACED. 1 L 7 1 3R 3 R NC A4SW 5E2 5 C P257 2000042000165 20000420 00165 NM 2000 4 20 20000420AP002 1 19990413 A 7830 1225P11 SWITCH BOEING 737 737200 1384453 NM PWA JT8 JT8D17A 52049 NE THRUST REVERSER DAMAGED A SOKF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 23 261LR 22402 P702675B DURNG FLIGHT LR-628, AIRCRAFT RETURN TO SJO STATION, BECAUSE IT WAS REPORTED THAT ISOLATION VALVE LIGHT ILLUMINATED AND TAKEOFF CONFIGURATION WARNING LIGHT CAME ON. AT SJO STATION, SWITCHERS WERE REPLACED AND TESTED SYSTEM IAW MM 32-33-11, IT WAS WORKING SATISFACTORY. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A16WE E2EA 2000042000166 20000420 00166 NM 2000 4 20 20000420AP003 1 19990319 A 2612 894093 FIRE LOOP BOEING 737 737296 1384486 NM NR 2 ENGINE DAMAGED A RJEF O OTHER N FALSE WARNING CR CRUISE 1 SO 23 232TA 22277 DURING FLIGHT TA410 (SAL-IAH) ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WE RE ACCOMPLISHED BY THE CREW, DUE TO THIS SITUATION THE A/C LANDED AT CANCUN AIRPORT. AT CANCUN, MAINTENANCE TECHS PERFO RMED A COMPLETE VISUAL INSPECTION AT ENGINE NR 2, NO FIRE EVIDENCE WAS FOUND. ALSO LOWER FIRE LOOP SENSING ELEMENT WAS REMOVED AND REPLACED AND ONE FIRE EXTINGUISHER BOTTLE P/N 33600011, AS PER AMM 26-10-00 AND 26-21-10. OPERATIONAL TEST WAS PERFORMED WITH SATISFACTORY RESULTS. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A16WE 2000042000167 20000420 00167 NM 2000 4 20 20000420AP004 1 19990721 A 3246 26066712 WHEEL BOEING 737 7372K5 138448X NM RT MLG FAILED A RJEF O OTHER O OTHER NR NOT REPORTED 1 SO 23 233TA 312 312 22601 GUA - FLT 910 - DURING TRANSIT CHECK, FOUND MLG NR 4 TIRE DISBANDED. VISUAL INSPECTION WAS PERFORMED IAW MM 5-51-251 AN D IT WAS FOUND TO HAVE DAMAGE ONLY IN THE INBOARD TRAILING EDGE AFT FLAP HAS DAMAGE OF 24 INCHES AND INBOARD LANDING GEA R DOOR WITH LITTLE DAMGE UPPER CORNER. MAIN WHEEL ASSY WAS REMOVED AND INSTALLED, AND ALSO INBOARD AFT FLAP AND MAIN LA NDING GEAR INNER DOOR. THE AIRPLANE RETURNED TO NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A16WE 2000042000168 20000420 00168 EU 2000 4 20 20000420AP005 1 19991216 A 7110 INTAKE DUCT AIRBUS 320 A320233 EU IAE V2527 V2527A5 NE NR 1 ENGINE DAMAGED A RJEF C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 23 460TA 1007 10542 SAL - FLT 390 - DURING TAKEOFF (SAL-TGU-SAP-MIA) A LARGE BIRD IMPACTED THE ENGINE NR 1, HOWEVER THE ENGINE PARAMETERS RE MAINED NORMAL, DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO EL SALVADOR STATION FOR MAINTENANCE. AT EL SALVADOR, MAIN TENANCE TECHNICANS PERFORMED VISUAL INSPECTION OF ENGINE NR 1, IT WAS FOUND THAT THE AIR INTAKE COWL NR 1 WITH A LARGE D ENT AT 6 O''''CLOCK POSITION, ACOUSTIC LINING PANELS CRACKED, ACOUSTIC LININGS BETWEEN 12 TO 3 O''''CLOCK PRESENTED SEVE RAL DENTS, MISSING MATERIAL AT ONE IGV PANEL, SEVERAL IGV AND RUBBER PANELS WITH MISALIGNMENT BETWEEN THE 12 TO 3 O''''C LOCK. THE FAN BLADES WERE INSPECTED BY NDT DID NOT FOUND CRACKS. BORESCOPE INSPECTION WAS PERFORMED REVEALED NO INTERN 2 L 7 2 4F 4 F RT A28NM E40NE 2000042100007 20000421 00007 2000 4 21 CA000110089 4 19991218 A 3460 MPN6224591512 COMPUTER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA P709632 (CAN) ON CLIMB OUT, FIRST OFFICER LOST FLIGHT DIRECTOR INDICATIONS, CAPTAIN''S FD ALREADY ON DEVIATION, SELECTED CENTER SOURCE, FD RETURNED BUT THEN AUTOPILOT DISCONNECTED. A/C DIVERTED. LEFT FLIGHT CONTROL COMPUTER REPLACED, SEVICEABLSE. 2 L 7 2 4F 4 F RT A1NM E3NE 2000042100008 20000421 00008 NM 2000 4 21 CA000110090 1 19991219 A 2530 OVEN BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE GALLEY SMOKE W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA P707529 (CAN) DURING TAKEOFF, OVEN IN REAR GALLEY BEGAN TO SMOKE, OVEN DEACTIVATED, OVEN REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 2000042100009 20000421 00009 NM 2000 4 21 CA000110093 1 19991226 A 7931 41824044TX TRANSMITTER PWA JT9D7R4D BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA P709670 P709670 (CAN) AFTER TAKEOFF, RT ENGINE OIL PRESSURE INDICATION IN AMBER AND DECREASING WITH THROTTLE MOVEMENT. A/C RETURNED, AF TER LANDING IDLE 57,58 PSI 13,14 OIL QTY, TEMP NORMAL. OIL PRESS TRANSMITTER REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 2000042100010 20000421 00010 NM 2000 4 21 CA000110095 1 19991220 A 2420 BMS1358T1C1G10 WIRE BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE RT GENERATOR OVERHEATED W K NONE M OVER TEMP IN INSP/MAINT 1 CA P709673 (CAN) AIRCRAFT HAD A HISTORY OF RT HYD INDICATION FLUCTUATIONS. TWO RT GEN FEEDER CABLES BADLY OVERHEATED CAUSING SOME O F ITS INSULATION TO MELT AND ALSO INSULATION ON ADJACENT WIRE BUNDLES. ALL DAMAGED CABLES REPAIRED. 2 L 7 2 4F 4 F RT A1NM E3NE 2000042100011 20000421 00011 NM 2000 4 21 CA000110098 1 19991229 A 5711 SPAR BOEING BOEING 737 7372A9C 1384495 NM PWA JT8 JT8D9A 52048 NE RT WING CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 674318 (CAN) RIGHT WING FROM SPAR LOWER CHORD CORRODED BEYOND SRM LIMITS AT STA 122. REPAIRED PER BOEING INSTRUCTION - FAX. 2 L 7 2 4F 4 F A16WE E2EA 2000042500001 20000425 00001 EU 2000 4 25 20000424AP005 1 19991029 A 2780 CONNECTOR AIRBUS 300 A300B4203 3930306 EU KRUEGER FLAP CONTAMINATED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 59140 140 MIA - FLT TA811 - AFTER TAKEOFF, KRUEGER FLAP DID NOT RETRACT, DUE TO THIS PROBLEM THE AIRCRAFT RETURNED TO MIA AIRPORT. AT MIAMI, MAINTENANCE TECHS PERFORMED VISUAL INSPECTION OF THE KRUEGER FLAPS AND FOUND CANNON PLUG AT THE LEFT SIDE KR UEGER FLAP CONTAMINATED WITH HYDRAULIC FLUID. IT WAS CLEANED AND RESET CENTRAL WARNING BOX. OPERATIONAL TEST WITH NORM AL RESULTS AS PER AMM 27-54-00 WAS PERFORMED. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 2000042500002 20000425 00002 NE 2000 4 25 20000424AP006 2 19991218 A 7520 COOLER AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE ENGINE CRACKED A RJEF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 59107 107 455828 MIA - FLT TA807 - DURING CRUISE, THE NR 2 ENGINE HIGH TEMPERATURE LIGHT CAME ON AND PACK NR 2 AUTOMATICALLY CLOSE. WHEN CROSS BLEED VALVE WAS OPENED NR 1 BLEED AIR TEMPERATURE STARTED TO RISE. BOTH ENGINES BLEED WERE CLOSED AND THE AIRCRA FT RETURNED TO MIAMI FOR MAINTENANCE. AT MIAMI, TECHS PERFORMED INSPECTION ON BOTH ENGINES. FOUND BOTH PRECOOLERS WITH CRACKS OUT OF LIMITS. THE AIRCRAFT REMAINS ON GROUND AWAITING THESE PRECOOLERS. AS PART OF THE TROUBLESHOOTING, REMOV ED AND REPLACED THE PNEUMATIC CONTROLLERS AS PER AMM 36-11-19. (M) 2 L 7 2 4F 4 F RT A35EU E23EA 2000042500003 20000425 00003 2000 4 25 20000424AP007 4 19991028 A 3442 20704100101 TRANSMITTER AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE WEATHER RADAR INOPERATIVE A RJEF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 59107 107 455828 SAL - FLT TA821 - DURING CRUISE, THE WEATHER RADAR SYSTEM FAULT, DUE TO THIS SITUATION THE AIRCRAFT DIVERTED TO EL SALVA DOR STATION FOR MAINTENANCE. AT SAL, MAINTENANCE TECHS PERFORMED TROUBLE SHOOTING OF THE WEATHER RADAR SYSTEM AND WAS F OUND RADAR TRANSCEIVER/RECEIVER AND ANTENNA INOPERATIVE. REMOVED AND REPLACED RADAR TRANSCEIVER, RECEIVER AND ANTENNA A S PER AMM 34-41-00. OPERATIONAL TEST WITH NORMAL RESULTS WAS PERFORMED. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M ) 2 L 7 2 4F 4 F RT A35EU E23EA 2000042500004 20000425 00004 2000 4 25 20000424AP008 4 19991028 A 3442 20704090101 ANTENNA AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE WEATHER RADAR INOPERATIVE A RJEF A UNSCHED LANDING O OTHER CR CRUISE 1 SO 23 59107 107 455828 SAL - FLT TA821 - DURING CRUISE, THE WEATHER RADAR SYSTEM FAULT, DUE TO THIS SITUATION THE AIRCRAFT DIVERTED TO EL SALVA DOR FOR MX. AT SAL, MX TECHS PERFORMED TROUBLESHOOTING OF THE WEATHER RADAR SYSTEM AND FOUND RADAR TRANSCEIVER/RECEIVER AND ANTENNA INOPERATIVE. REMOVED AND REPLACED RADAR TRANSCEIVER, RECEIVER AND ANTENNA AS PER AMM 34-41-00. OPERATIONA L TEST WITH NORMAL RESULTS WAS PERFORMED. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A35EU E23EA 2000042500005 20000425 00005 NM 2000 4 25 20000424AP009 1 19990413 A 7830 1225P11 PRESSURE SWITCH BOEING 737 737200 1384453 NM PWA JT8 JT8D17 52049 NE COCKPIT DAMAGED A SOKF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 261LR 22402 P702675B DURING FLIGHT, AIRCRAFT RETURNED TO SJO, BECAUSE IT WAS REPORTED THAT ISOLATION VALVE LIGHT ILLUMINATED AND TAKEOFF CONF IGURATION WARNING LIGHT CAME ON. AT SJO, SWITCHERS WERE REPLACED AND TESTED SYSTEM IAW MM 32-33-11, IT WAS WORKING SATI SFACTORY. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A16WE E2EA 2000042500006 20000425 00006 NM 2000 4 25 20000424AP010 1 19990721 A 3246 26066712 WHEEL BOEING 737 7372K5 138448X NM RT MLG FAILED A RJEF K NONE O OTHER IN INSP/MAINT 1 SO 23 233TA 312 22601 GUA - FLT 910 - DURING TRANSIT CHECK, FOUND MAIN LANDING GEAR NR 4 TIRE DISBANDED. VISUAL INSPECTION WAS PERFORMED IAW MM 5-51-251 AND IT WAS FOUND DAMAGED ONLY IN: INBOARD TRAILING EDGE AFT FLAP HAS A DAMAGE OF 24 INCHES AND INBOARD LANDI NG GEAR DOOR WITH LITTLE DAMAGE UPPER CORNER. MAIN WHEEL ASSY WAS REMOVED AND INSTALLED, AND ALSO INBOARD AFT FLAP AND MAIN LANDING GEAR INNER DOOR. THE AIRPLANE RETURNED TO NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A16WE 2000042500007 20000425 00007 NM 2000 4 25 20000424AP011 1 19990319 A 2612 33600011 FIRE DETECTOR BOEING 737 737296 1384486 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE MALFUNCTIONED A RJEF A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 23 232TA 22277 P688401 CUN - FLT TA410 - ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLIS HED BY THE CREW, DUE THIS SITUATION THE AIRCRAFT LANDED AT CANCUN. CANCUN MX TECHS PERFORMED A COMPLETE VISUAL INSPECTI ON AT ENGINE NR 2, NO FIRE EVIDENCE WAS FOUND. ALSO LOWER FIRE LOOP SENSING ELEMENT WAS REMOVED AND REPLACED AND ONE FI RE EXTINGUISHERS BOTTLE P/N 33600011, AS PER AMM 26-10-00 AND 26-10-00 AND 25-21-10. OPS TEST WS PERFORMED WITH SATISFA CTORY RESULTS. THE AIRCRAFT RETURNED TO NORMAL OPS. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 2000042500008 20000425 00008 EU 2000 4 25 20000424AP012 1 19990410 A 2822 P99C38601 PUMP AIRBUS 320 A320233 EU IAE V2527 V2527A5 NE FUEL BOOST INOPERATIVE A RJEF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 458TA 912 V10445 CUN - FLT TA581 - DURING CRUISE OF THE FLIGHT, THE LEFT AND RIGHT NR 1 WING FUEL BOOST PUMPS FAULT LIGHTS CAME ON. THE FLIGHT WAS DIVERTED TO CANCUN FOR MAINTENANCE. AT CANCUN, MAINTENANCE TECHS REMOVED AND REPLACED THE LEFT AND RIGHT NR 1 WING FUEL BOOSTS PUMPS, THEN TEST WAS PERFORMED AS PER MM 28-21-51 WITH NORMAL RESULTS. THE AIRCRAFT RETURNED TO NORM AL OPERATION. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2000042500009 20000425 00009 EU 2000 4 25 20000424AP013 1 19990410 A 2822 P99C38601 PUMP AIRBUS 320 A320233 EU IAE V2527 V2527A5 NE FUEL BOOST INOPERATIVE A RJEF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 458TA 912 V10445 CUN - FLT TA581 - DURING CRUISE OF THE FLIGHT, THE LEFT AND RIGHT NR 1 WING FUEL BOOST PUMPS FAULT LIGHTS CAME ON. THE FLIGHT WAS DIVERTED TO CANCUN FOR MAINTENANCE. AT CANCUN, MAINTENANCE TECHNICIANS REMOVED AND REPLACED THE LEFT AND RIG HT NR 1 WING FUEL BOOST PUMPS, THEN WAS PERFORMED AS PER MM 28-21-51 WITH NORMAL RESULTS. THE AIRCRAFT RETURNED TO NORM AL OPERATION. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2000042500010 20000425 00010 EU 2000 4 25 20000424AP014 1 19991107 A 3411 C16195AA PITOT LINE AIRBUS 320 A320233 EU IAE V2527 V2527A5 NE FUSELAGE OBSTRUCTED A RJEF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 451TA 733 V10265 SAL - AFTER TAKEOFF, PILOTS NOTED A 50 KNOT DISCREPANCY BETWEEN THE CAPTAIN AND FIRST OFFICER AIRSPEED INDICATIONS, THEN AT FLIGHT LEVEL 3,000 FEET THE CAPTAIN SIDE SHOWED 240 KTS AND F/O''S 165 KTS, DUE THIS SITUATION THE FLIGHT RETURNED T O SAL AIRPORT. AFTER UNEVENTFUL LANDING AT EL SALVADOR, MAINTENANCE TECHS PERFORMED FLUSHING OF THE TOTAL PRESSURE LINE OF THE AIR DATA MODULE ON THE CAPTAIN AND F/O''S SIDES AS PER AMM 34-13-00, AND FOUND FOREIGN MATERIAL ON THE FIRST OFF ICER PITOT PROBE. PERFORMED CHECK FLIGHT WITH NORMAL RESULTS. THE AIRPLANE RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2000042500011 20000425 00011 EU 2000 4 25 20000424AP015 1 19990725 A 3230 37GA SENSOR AIRBUS 320 A320233 EU IAE V2527 V2527A5 NE NLG DOOR DAMAGED A RJEF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 23 453TA 747 V10276 MIA - FLT 391 - DURING TAKEOFF, THE LGCIU NR 1 FAULT AND AFT CARGO DOOR MSG CAME ON THE UPPER ECAM DISPLAY, DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO MIAMI AIRPORT. AFTER UNEVENTFUL LANDING AT MIAMI AIRPORT, THE CREW REPORTED OVERWEIG HT LANDING. MAINTENANCE TECHS PERFORMED CFDS TEST OF THE LGCIU NR 1, THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2 L 7 2 4F 4 F RT A28NM E40NE 2000042500012 20000425 00012 EU 2000 4 25 20000424AP016 1 19991223 A 5347 PLAL7075T6511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 349SB 340B349 ABI - SEAT TRACK CORRODED BEYOND LIMITS AT FS 294. REMOVED AND REPLACED SEAT TRACK AT FS 294, 11 INCH SECTION FROM FS 2 94 TO 305. (M) 2 L 7 2 4T RT A52EU 2000042500013 20000425 00013 NM 2000 4 25 20000424AP043 1 19991119 A 2822 320552 TERMINAL BOEING 727 727222 1384073 NM BOOST PUMP FAILED A RYNA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 CE 07 7644U 20038 FLT 216 - CVG - ON CLIMB-OUT FROM DAY, SMELLED ELECTRICAL SMOKE IN COCKPIT, AND SAW SLIGHT WHISP OF SMOKE FORM BEHIND LE FT OF FLIGHT ENGINEER PANEL. LANDED IN CVG. SMOKE SEEMED TO DISSIPATE PRIOR TO LANDING. FOUND SHORTED RING TERMINAL A T NR 2 FORWARD RIGHT BOOST PUMP ON/OFF SWITCH. REPAIRED WIRE. INSTALLED NEW TERMINAL. (M) 2 L 7 3 4F A3WE 2000042500014 20000425 00014 2000 4 25 20000424AP044 4 19991224 A 2565 A31517109 SLIDE AIRBUS 320 A320214 EU PAX DOOR DEPLOYED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 GBXKC 730 FLT 2312 - ORD - INADVERTENT DEPLOYMENT OF L-2 ESCAPE SLIDE. REPLACED L-2 ESCAPE SLIDE. (M) 2 L 7 2 4F RT A28NM 2000042500019 20000425 00019 WP 2000 4 25 99T64R544EWA 1 19991203 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LT TRAPEZOIDAL FITTING HAS ELONGATED HOLE. REAMED HOLE. FABRICATED BUSHING AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/12/99. (M) 2 L 7 4 4F RT 4A25 2000042500020 20000425 00020 2000 4 25 20000424AP018 4 19990130 A 2565 SLIDE BOEING 757 75723N 1384973 NM PAX DOOR DEPLOYED A AMTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 11 523AT 30232 DURING GROUND HANDLING, A CLEANER UNINTENTIONALLY ACTIVATED THE R1 DOOR WITH THE ESCAPE SLIDE HANDLE IN ARMED POSITION. SLIDE FULLY DEPLOYED AND DOOR ASSIST BOTTLE BLOWN. REPLACED SLIDE -AFT ASSY AT R1 DOOR PER MM 25-66-01 AND REPLACED TH E DOOR ASSIST BOTTLE PER MM 52-11-30. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2000042500021 20000425 00021 WP 2000 4 25 20000424AP019 1 19991123 A 5320 46143971N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, A PIT FORWARD STATION 70 L31L END FITTING CORRODED. REMOVED FITTING. REPLACED FITTING IAW IAW DC -8 SRM 51-1-21, 51-1-24. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-21D, 53-4-1. (M) 2 L 7 4 4F RT 4A25 2000042500022 20000425 00022 WP 2000 4 25 20000424AP021 1 19991017 A 5720 ANGLE DOUG DC8 DC873F 302199F WP RT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, NR 3 RT STUB WING HAS CRACK INSIDE L/E DOUBLER. REMOVED CRACKED ANGLE. FABRICTED NEW ANGLE, TREA TED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AND 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000042500023 20000425 00023 WP 2000 4 25 20000424AP022 1 19991014 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT FLOORBEAM EXFOLIATED STATION 1500 XCW 50 LEFT. REMOVED CORROSION IAW DC-8 SRM 5 1-18-8. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-2-0 AND 51-1-8 AND 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000042500024 20000425 00024 WP 2000 4 25 20000424AP023 1 19991115 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT STATION 25 JUST AFT CREW ENTRY DOOR SEAT EXFOLIATED. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW DC-8 SRM 51-3 -3 AND 53-2-3 AND 53-2-0. (M) 2 L 7 4 4F RT 4A25 2000042500025 20000425 00025 WP 2000 4 25 20000424AP024 1 19991019 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT FLOOR PANEL 760-1100, 5-6 INCH CRACK ON FLOOR PANEL. CUT OUT DAMAGED AREA IAW D C-8 SRM 53-2-0. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND 53-2-3 AND 51-1-21. (M ) 2 L 7 4 4F RT 4A25 2000042500026 20000425 00026 WP 2000 4 25 20000424AP025 1 19991014 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT FLOOR PANEL 580-840 AREA OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 53-2-0 AND 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000042500027 20000425 00027 WP 2000 4 25 20000424AP026 1 19991008 A 5220 SKIN DOUG DC8 DC873F 302199F WP EMERGENCY EXIT CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, LEFT AFT OVERWING EXIT DOOR FOUND CRACK IN DOOR UNDER BOTTOM PLATE THAT WAS REMOVED FOR CORROSION. STOP DRILLED CRACK IAW DC-8 SRM 52-20-0. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1 -21D. (M) 2 L 7 4 4F RT 4A25 2000042500028 20000425 00028 WP 2000 4 25 20000424AP027 1 19991014 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT LONGERON 9 STATION 1300-1340 LT SURFACE CORROSION. REMOVED CORROSION IAW DC-8 S RM 51-1-8. CUTOUT DAMAGED AREA. FABRICATED DOUBLER PARTS IAW DC-8 SRM 53-2-2. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-2. (M) 2 L 7 4 4F RT 4A25 2000042500029 20000425 00029 WP 2000 4 25 20000424AP028 1 19991007 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT LIGHT SURFACE CORROSION STATION 1200 LONGERON 9-10 LEFT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21, 53-2-0 AND 51-1-4. (M) 2 L 7 4 4F RT 4A25 2000042500030 20000425 00030 WP 2000 4 25 20000424AP030 1 19991011 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FINGER DOUBLER CORRODED AND RIVET CORRODED STATION 857 TO 902 CENTER OF AIRCRAFT 10 INCHES BELOW C ABIN FLOOR. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FINGER DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AND 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000042500031 20000425 00031 WP 2000 4 25 20000424AP031 1 19991119 A 5313 RIB DOUG DC8 DC873F 302199F WP TAILCONE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, THROUGH ACCESS PANEL 602 IN TAILCONE ON RIGHT SIDE STATION 1923 1ST RIB PASSED PANEL AFT WORN AREA IN RIB. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AND 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000042500032 20000425 00032 WP 2000 4 25 20000424AP032 1 19991116 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FUSELAGE STATION 1890 L10 INTERCOSTAL CRACKED. FABRICATED NEW INTERCOSTAL. TREATED, PRIMED AND I NSTALLED IAW DC-8 SRM 51-1-4, 51-1-8 AND 51-1-20. (M) 2 L 7 4 4F RT 4A25 2000042500035 20000425 00035 2000 4 25 ASAA9980339 4 19991228 A 2565 SLIDE DOUG DC9 DC983 3022083 WP PAX DOOR WILL NOT TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 PHX - DURING 30K CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOO R EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 2000042500041 20000425 00041 WP 2000 4 25 ASAA9980329 1 19991217 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 20 UNSECURE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 WERE FOUND INOPERATIVE. SECURED LOOSE CONNEC TOR IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000042500042 20000425 00042 WP 2000 4 25 20000424AP033 1 19991001 A 5511 SPAR DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LEFT INBOARD HORIZ STAB L/E CRACK AT FRAME XFS 53.75 UNDER SKIN EXTENDED PAST STOP DRILL. STOP DR ILLED CRACK IAW DC-8 SRM 55-2-0. FABRICATED ANGLE REPAIR. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AN D 51-1-20D.(M) 2 L 7 4 4F RT 4A25 2000042500080 20000425 00080 NM 2000 4 25 CA000215041 1 19990507 A 7110 COWLING CFMINT CFM565A5 AIRBUS A319 A319114 NM GE CFM56 CFM565A 13802 NE RT ENGINE SEPARATED W A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 CA 731943 731943 (CAN) ON CLIMB AFTER TAKEOFF THROUGH 14,000 FEET, LOUD BANG HEARD ACCOMPANIED WITH A LOSS OF NR 2 HYD PRESSURE. UPON LAN DING, INVESTIGATION REVEALED SUBSTANTIAL DAMAGE TO RIGHT ENGINE COWLING, HORIZONTAL STABILIZER, AND ENGINE REVERSER. TS B AND THE MANUFACTURER ARE INVESTIGATING. , 2 L 7 2 4F 4 F RT A28NM E29NE 2000042500085 20000425 00085 CE 2000 4 25 20000424AP035 1 19990525 A 5320 521304012 CHANNEL CESSNA 404 404CESSNA 2075901 CE NLG WW CRACKED A BQTA K NONE O OTHER IN INSP/MAINT 1 NE 05 5409G 12000 4040028 FOUND BOTH LEFT AND RIGHT T CHANNELS CRACKED APPROX 8 INCHES. THESE CHANNELS ARE LOCATED ON THE FORWARD CORNERS OF THE NOSE WHEEL WELL BOX ASSY AND ACCESSED FROM THE NOSE BAGGAGE AREA. POSSIBLE CAUSE FOR CRACKING DUE TO EXCESSIVE SIDE LOA DING WHILE TAXIING. (M) 1 L 7 2 3O A25CE 2000042500086 20000425 00086 WP 2000 4 25 20000424AP036 1 19991101 A 5520 SKIN LKHEED 1011 1011385114 WP ELEVATOR PUNCTURED A FXLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 19 260FA 193A1158 DURING TAKEOFF FROM BOGOTA, BLEW TWO REAR TIRES ON THE LEFT SIDE OF A/C, CAUSING DAMAGE TO LEADING EDGE AND RIB OF ELEVA TOR STATION ES 248-272 LEFT. REPAIRED DAMAGE IAW FINE AIR EA L5520-01. (M) 2 L 7 3 4F A23WE 2000042500087 20000425 00087 WP 2000 4 25 20000424AP037 1 19991104 A 2435 31008011 GENERATOR DOUG DC8 DC8* WP STARTER/GEN FAILED A FXLA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 19 505FB 45410 GENERATOR 1, 2, AND 3 FREQUENCY WAS 406 AND NR 4 GENERATOR FREQUENCY WAS 398. GENERATOR NR 4 WOULD NOT PARALLEL CAUSING CIRCUIT BREAKER TO POP. CREATING SMOKE IN THE COCKPIT FROM THE MAIN CIRCUIT BREAKER. REMOVED AND REPLACED NR 4 AC CON TROL PANEL IAW MM 24-5-3. OPS CHECK ON GROUND OK IAW MM 25-5-0 ENTERED ON DMI 12403 PER MEL 24-1. (M) 2 L 7 4 4J F 4A25 2000042500088 20000425 00088 2000 4 25 20000424AP038 4 19991012 A 2210 HARNESS EMB 120 EMB120RT SO RADAR ANTENNA FAILED A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 01 108UX 120108 UNCOMMANDED RUDDER ACTIVATION TO THE LEFT AT CRUISE ALTITUDE. PROBLEM ISOLATED TO YAW DAMPER SYSTEM WHICH WAS DEACTIVAT ED. PROBLEM WAS CORRECTED BY REPAIRING FAULTY WIRING AT THE RADAR ANTENNA CONNECTOR. (M) 2 L 7 2 4T RT A31SO 2000042500089 20000425 00089 2000 4 25 20000424AP039 4 19991222 A 3422 GYRO COLLINS BEECH 1900 1900D 1154162 CE COCKPIT INTERMITTENT A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 150UX UE150 NR 1 DIRECTIONAL GYRO INTERMITTENTLY FREEZED IN TURNS. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. (M) 2 L 7 2 4T RT A24CE 2000042500090 20000425 00090 2000 4 25 20000424AP040 4 19991223 A 3422 GYRO BEECH 1900 1900D 1154162 CE COCKPIT INTERMITTENT A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 150UX UE150 NR 1 DIRECTIONAL GYRO INTERMITTENTLY FREEZES IN TURNS. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. (M) 2 L 7 2 4T RT A24CE 2000042500093 20000425 00093 SO 2000 4 25 20000424AP042 1 19990303 A 3246 40193 WHEEL EMB 110 EMB110P1 3260122 SO NLG CRACKED A BQTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NE 05 51BA 110404 WHILE REPORTING FROM UPS RAMP TO FBO RAMP IN BUF A GRINDING NOISE WAS HEARD WHEN TURNING AIRCRAFT WHILE TAXIING. THE NO SE WHEEL HALF BROKE LEAVING THE AXLE BOLT AND TWO WHEEL BEARINGS ON THE AXLE. BEARINGS WERE FOUND TO BE CORRODED. PROB ABLE CAUSE, FREQUENT DE-ICINGS WITH GLYCOL WASHED OUT NOSEWHEEL BEARINGS. WHEELBEARINGS ARE NOW INSPECTED EVERY 150 HOU RS. (M) 1 L 7 2 4T A21SO 2000042500108 20000425 00108 WP 2000 4 25 20000424AP034 1 19991101 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CORROSION ON FRAME 1793 IN CHANNEL L32L TO L32R. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICAT ED DOUBLERS, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000042500112 20000425 00112 WP 2000 4 25 20000424AP020 1 19991123 A 5320 4614392N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, A PIT FORWARD STATION 70 L31L END FITTING CORRODED. REMOVED FITTING. REPLACED FITTING IAW DC-8 S RM 51-1-21, 51-1-24. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-21D, 53-4-1. (M) 2 L 7 4 4F RT 4A25 2000042500113 20000425 00113 WP 2000 4 25 20000424AP029 1 19991016 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, WHEEL WELL PRESS PANEL HAS CORROSION AROUND RIVETS AND PANEL STATION 902 TO 920 RBL 20 INCH. REMO VED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FINGER DOUBLER REPAIR. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-4 AND 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000042500312 20000425 00312 WP 2000 4 25 AALA006029 1 19991224 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 872RA 49793 BOTH EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MD80 MM 33-53-00. OPS CHECK GOO D IAW MD80 MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2000042500320 20000425 00320 NE 2000 4 25 AALA19991936 2 19991214 A 7200 9324M60G01 ENGINE BOEING 737 737823 13844BZ NM CFMINT CFM567 CFM567B22 13802 NE NR 1 STALLED A AALA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 SW 21 905AN 29507 MSP - FLT 188 - DURING FLIGHT, NR 1 ENGINE COMPRESSOR STALL AT FL370. NR 1 ENGINE ROLLED BACK BUT RECOVERED. FLIGHT AT TENDANT OBSERVED FLAMES FROM EXHAUST. LANDED MSP WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. ENGINE SHUTDOWN DUE TO FAILURE OF NR 4 ROLLER BEARING, PART NUMBER 340-167-901-0, SERIAL NUMBER DA355 521. (M) 2 L 7 2 4F 4 F RT A16WE E00055EN 2000042700002 20000427 00002 EU 2000 4 27 USAASA99010 1 19991125 A 3350 Z010H0005119 LIGHT AIRBUS A319 A319112 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 719US 582 1084 PIT - FOUND EMERGENCY EXIT LIGHTS IN CABIN WILL NOT EXTINGUISH WITH PED SWITCH OFF. MAINTENANCE REPLACED CIDS DIRECTOR. GROUND TESTS OK. (M) 2 L 7 2 4F RT A28NM 2000042700018 20000427 00018 2000 4 27 CA990513010 4 19990416 A 2562 AK450 ELT AMERIKING CASA C212 C212CC 2410204 EU GARRTT TPE331 TPE33110 01514 WP CABIN MALFUNCTIONED W K NONE L NO TEST IN INSP/MAINT 1 CA 4504129 (CAN) DURING ROUTINE TESTING OF THE EMERGENCY LOCATION TRANSMITTER (ELT) IT WAS FOUND TO BE NOT OPERATING. DIRECT AND R EMOTE METHODS WERE USED WITHOUT SUCCESS. UNIT WAS LAST CHECKED AT THE OVERHAUL FACILITY.N.B. A SIMILAR EXPERIENCE HAS OCCURRED ONCE BEFORE. DEFECT WAS CONFIRMED BY AN OUTSIDE REPAIR AGENCY, BUT WHEN SENT TO THE MANUFACTURER IT WAS REPORT ED IN A SERVICEABLE CONDITION. 2 H 7 2 4T 4 T A43EU E4WE 2000042700019 20000427 00019 GL 2000 4 27 CA990513017 2 19990504 A 7230 6877410 CASE ALLSN 6890550 BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL COMPRESSOR SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 1833 CAC36908 CAE831812 (CAN) DURING MID-POINT INSPECTION, THE COMPRESSOR CASE ASSEMBLY''S PLASTIC LINING WAS FOUND SEPARATED WITH PIECES MISSIN G. 1 G 7 1 3U 3 U H2SW E4CE 2000042700020 20000427 00020 EA 2000 4 27 CA990513018 2 19990506 A 7322 10367832 CARBURETOR LYC O320E2A PIPER PA28 PA28140 7102802 SO LYC O320 O320E2A 41508 EA LEAKING LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 99 L2459127A L2459127A (CAN) DURING INSPECTION, THE CARBURETOR WAS FOUND TO BE LEAKING FUEL AT THE SEAMS OF THE TWO HALVES. THE CARBURETOR WAS REPLACED. 1 L 7 1 3O 3 O 2A13 E274 2000042700021 20000427 00021 SO 2000 4 27 CA990513019 1 19990506 A 2421 4111810 ALTERNATOR PIPER PA28 PA28140 7102802 SO LYC O320 O320E3D 41508 EA ELECTRICAL FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 CA 92 L3704327A (CAN) DURING FLIGHT, THE AMPERE GAUGE WAS SLOWLY GOING TO ZERO. THE AIRCRAFT RETURNED TO BASE. THE ALTERNATOR WAS REPL ACED. 1 L 7 1 3O 3 O 2A13 E274 2000042700022 20000427 00022 GL 2000 4 27 CA990514003 3 19990507 A 6110 31505 ROLL PIN MCAULY D3A34C402C CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO MCAULY D3A34 D3A34C402 GL PROPELLER MISSING W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 983879 517742 799852 (CAN) AFTER PROPELLER INSTALLATION, WHILE CARRYING OUT AN ENGINE RUNUP AT 2,700 RPM, THERE WAS A VIBRATION SIMILAR TO MI SS ON A CYLINDER. THE ENGINE WAS SHUT DOWN. P OST RUNUP INVESTIGATION FOUND THAT ONE OF THE PROP BLADES COULD BE MOVED B Y HAND. T HE PROPELLER WAS SENT TO OVERHAUL WHERE IT WAS FOUND THE PROPELLER WAS IMPROPERLY ASSEMBLED AFTER INSPECTION. IT WAS FOUND THAT THE LINK PISTON PIN FROM NR 1 BLADE HAD NOT BEEN RETAINED WITH A P/N 31505 ROLL PIN AND SUBSEQUENTLY DISLODGED FROM THE PISTON ASSEMBLY ALLOWING THE BLADE LINK AND PISTON TO FALL INTO THE HUB CAVITY. 1 H 7 1 3O 3 O 3A21 E8CE 5 C P47GL 2000042700023 20000427 00023 NE 2000 4 27 CA990514006 2 19990426 A 7261 HOUSING PWA JT8D7 DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE OIL FILTER LEAKING W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA P649139D P649139D (CAN) NR 2 ENGINE LOST OIL PRESSURE, WITH OIL QUANTITY AT ZERO. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED. POST-FLIGHT INSPECTION FOUND AN OIL LEAK AT THE OIL FILTER HOUSING. THE LEAK WAS REPAIRED AND CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 2000042700024 20000427 00024 SO 2000 4 27 CA990514015 1 19990506 A 3710 212CW PUMP LYC IO360C1E6 PIPER PA34 PA34200 7103405 SO LYC O360 IO360C1E6 41514 EA VACUUM SYSTEM FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 1463 L27667A L27667A (CAN) PILOT REPORTED THE RIGHT RED BALL WAS VISIBLE IN THE VACUUM GAUGE. THE VACUUM PUMP WAS REMOVED AND INSPECTION FOUN D THE DRIVE SHAFT WAS SHEARED. THE PUMP WAS REPLACED. 1 L 7 2 3O 3 O A7SO 1E10 2000042700025 20000427 00025 GL 2000 4 27 CA990521003 2 19990503 A 7210 6874525 BEARING ALLSN 250C20B HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL GEARBOX MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 10382 6788 CAE832839 CAE832839 (CAN) METAL FLAKES WERE FOUND IN THE CHIP DETECTOR. THE CHIP DETECTOR WAS CLEANED AND THE ENGINE GROUND RUN. THE CHIP L IGHT ILLUMINATED AT GROUND IDLE. THE ENGINE WAS REMOVED DUE TO EXCESSIVE METAL IN THE CHIP DETECTOR. DISASSEMBLY FOUND THE NR 3 AND NR 4 BALL BEARINGS HAD FAILED. A NEW ROLLER BEARING WAS INSTALLED. 1 G 7 1 3U 3 U H3WE E4CE 2000042700026 20000427 00026 NE 2000 4 27 CA990521015 2 19990507 A 7210 SEAL LYC ALF502R5 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 3 ENGINE LEAKING W O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 CA LF05558A LF05558A (CAN) ODOR IN CABIN ON FINAL APPROACH. INSPECTION FOUND THE NR 9 SEAL LEAKING. T HE SEAL WAS REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 2000081800008 20000818 00008 NM 2000 8 18 CA990521016 1 19990427 A 7931 1163P181 PRESSURE SWITCH PWA JT8D17A BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE OIL SYSTEM MALFUNCTIONED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 9715 709397 709397 (CAN) NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON IN CRUISE. THROTTLE BACK, LIGHT REMAINED ON. ALL ENGINE PARAMETERS WE RE NORMAL. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED. MEL 79-02 WAS COMPLIED WITH. THE OIL FILTER WAS INS PECTED AND FOUND CLEAN. THE NR 1 ENGINE OIL FILTER DIFFERENTIAL SWITCH WAS REPLACED. (X) 2 L 7 2 4F 4 F A16WE E2EA 2001030700596 20010307 00596 NM 2001 3 7 CA991229023 1 19991214 A 2433 COOLING FAN DHAV DHC8 DHC8202 2809007 NM TRU INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TRU COOLING FAN FOUND INOPERATIVE AT C CHECK 2 H 7 2 4T RT A13NM 2001030700593 20010307 00593 NM 2001 3 7 CA991229024 1 19991214 A 2433 COOLING FAN DHAV DHC8 DHC8202 2809007 NM TRU INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TRU COOLING FAN FOUND INOPERATIVE AT C CHECK 2 H 7 2 4T RT A13NM 2001030700610 20010307 00610 NM 2001 3 7 CA991229025 1 19991214 A 2433 COOLING FAN DHAV DHC8 DHC8202 2809007 NM TRU INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TRU COOLING FAN FOUND INOPERATIVE AT C CHECK 2 H 7 2 4T RT A13NM 2000042700060 20000427 00060 WP 2000 4 27 AALA996056 1 19990610 A 3350 6011779 POWER SUPPLY DOUG DC9 DC987 3022087 WP OVERWING FAILED A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 754RA 49641 OKC - THE FOLLOWING EMERGENCY LIGHTS ARE INOPERATIVE, ROWS 10-18, LT FORWARD OVERWING, RT FORWARD OVERWING, LT OVERHEAD VERTICAL STAIRS. REMOVED AND REPLACED OVERWING POWER SUPPLY IAW MD-80 MM 33-53-00. OPS CHECK GOOD IAW MD80 MM 33-53-00 . (M) 2 L 7 2 4F RT A6WE 2000042700084 20000427 00084 WP 2000 4 27 99T64R351AR 1 19990415 A 5730 561135034 PLATE DOUG DC8 DC862 3021970 WP TRUNNION FITTING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 ARROW AIR - RIGHT WING UPPER SURFACE CORROSION AT TRUNNION FITTING FASTENERS. REMOVED CORROSION AND BLENDED AREA IAW BO EING MESSAGE M-7200-99-02208 ITEM 18 WITH APPROVED FAA FORM 8110.3 DATED 4-19-99. INSTALLED FASTENERS IAW DC-8 SRM 51-1 -20D. (M0 2 L 7 4 4F 4A25 2000042700093 20000427 00093 WP 2000 4 27 T64R543EWA 1 19991118 A 5320 THRESHOLD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, L1 DOOR THRESHOLD CRACKED. STOP DRILLED CRACK AND WELDED PER EO NR 99-186 WITH APPROVED 8110-3 DA TED 11/17/99. (M) 2 L 7 4 4F RT 4A25 2000042700107 20000427 00107 NE 2000 4 27 UIEA9997 2 19991214 A 7530 32065254 VALVE BOEING 747 7472F6B 1384807 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE STUCK A UIEA A J UNSCHED LANDING DUMP FUEL M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 15 535MC 21833 FLT GT57 - NR 2 ENGINE FIRE WARNING ILLUMINATED AFTER TAKEOFF. IT OCCURRED DURING CLIMB WITH CLIMB POWER SET. BOTH NAC ELLE TEMPS WERE 8.5. ENGINE SECURE DIAW FHB. DECLARE EMERGENCY AND JETTISONED 14 KGS OF FUEL. LANDING WAS UNEVENTFUL. FOUND NR 2 ENGINE PRESSURE RELIEF VALVE STUCK OPEN. REPLACED VALVE. ENGINE RUN UP NORMAL. (M) 2 L 7 4 4F 4 F A20WE E23EA 2000042700108 20000427 00108 WP 2000 4 27 99T64R447EWA 1 19991102 A 5320 3773973IN FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CRACK IN UPPER CUSP CARGO DOOR FRAME ATTACH FITTING FRAME STATION 120 FORWARD ATTACH FITTING. REM OVED AND REPLACED FITTING IAW DC-8 SRM 51-1-8, 51-3-0 AND 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000042700109 20000427 00109 WP 2000 4 27 T64R442EWA 1 19991123 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 REAR PRESSURE BULKHEAD CIRCUMFERENTIAL FRAME TOP RIGHT SIDE HAS CRACK STATION 1766-L3R. NDT CONFIMRED END OF CRACK. CU T OUT CRACK SECTION. FABRICATED REPAIR ANGLES. TREATED AND PRIMED. INSTALLED REPAIR PER EO NR 99-186 WITH APPROVED 81 10-3 DATED 9/24/99. (M) 2 L 7 4 4F RT 4A25 2000042700110 20000427 00110 WP 2000 4 27 99T64R673EWA 1 19991210 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LEFT MID WING LEADING EDGE OUTBOARD END MOUNT HOLES, OVERSIZED, ELONGATED AND GOUGED STATION XS 52 0.168. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21. FABRICATED NEW DOUBLER. TREATED PRIMED AND INSTALLED IAW DC-8 SRM 51-1-4 AND 51-1-8. INSTALLED DIMPLE WASHER PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/08/99. (M) 2 L 7 4 4F RT 4A25 2000042700111 20000427 00111 WP 2000 4 27 99T64R469EWA 1 19991215 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT, FLOORBEAM EXFOLIATED STATION 1540 XCW 69 LEFT. REMOVED CORROSION IAW DC- 8 SRM 51-1-8. FABRICATED REPAIR ANGLE IAW DC-8 SRM 53-2-0. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21 AND 53-2-0. (M) 2 L 7 4 4F RT 4A25 2000042700112 20000427 00112 WP 2000 4 27 99T64R459EWA 1 19991109 A 5313 3640887N STRINGER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT STATION 960-980 10 INCHES BELOW FLOOR XCW 20 LEFT FLOOR STRINGER SIGNS OF EXFOLIATION. REMOVED AND REPLACED STRINGER FITTING IAW DC-8 SRM 51-1-21, 51-1-20 AND 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000042700113 20000427 00113 WP 2000 4 27 99T64R460EWA 1 19991210 A 3610 234064401 DUCT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, GROUND PNEUMATIC CONNECTION HAS LEAK IN DUCT UPSTREAM OF COUPLING. STOP DRILLED CRACK. NDT CONFI RMED CRACK HAD BEEN STOPPED. WELDED CRACK IAW MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110 -3 DATED 10/06/99. (M) 2 L 7 4 4F RT 4A25 2000042700114 20000427 00114 WP 2000 4 27 99T64R466EWA 1 19991120 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURNIG D-CHECK, FORWARD ACCESSORY COMPT LONGERON 35 RIGHT HAS CORROSION AT PREVIOUS REPAIR DOUBLER STATION 55 TO 7 0. REMOVED CORROSION AND PREVIOUS REPAIR IAW DC-8 SRM 51-1-8 AND 51-1-2. FABRICATED NEW SECTION OF LONGERON. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED REPAIR IAW DC-8 SRM 51-1-21 AND 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000042700115 20000427 00115 WP 2000 4 27 99T64R458EWA 1 19991109 A 5313 3640887N STRINGER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT STATION 960-980 10 INCHES BELOW FLOOR XCW 10 LEFT FLOOR STRINGER SIGNS OF EXFOLI ATION. REMOVED AND REPLACED STRINGER FITTING IAW DC-8 SRM 51-1-21, 51-1-20 AND 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000042700116 20000427 00116 WP 2000 4 27 99T64R450EWA 1 19991122 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CRACK IN RIB AT STATION XRS 178 MIDDLE AFT EDGE IN FLAP WELL LEFT WING. ROUTED OUT CRACK. FABRIC ATED REPAIR ANGLE AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 1/27/99. (M) 2 L 7 4 4F RT 4A25 2000042700117 20000427 00117 WP 2000 4 27 99T64R457EWA 1 19991109 A 5320 3640887N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, W/W PRESSURE PANEL ATTACH ANGLE CORRODED STATION 960 TO 980 RBL 8 INCH. REMOVED AND REPLACED ATTA CH ANGLE AND STRINGER FITTING IAW DC-8 SRM 51-1-20, 51-1-21 AND 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000042700118 20000427 00118 WP 2000 4 27 20000427AP003 1 19990929 A 5350 FAIRING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, D PIT FORWARD DOOR FRAME, FAIRING CRACKED. REMOVED FAIRING. FABRICATED FAIRING IAW DC-8 SRM 51-1 -4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000042700119 20000427 00119 WP 2000 4 27 20000427AP005 1 19991110 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 1 XCW 69 LEFT STATION 757-781 WORN. REMOVED DAMAGED SEAT TRACK IAW DC-8 SRM 51 -1-21. INSTALLED SEAT TRACK IAW DC-8 SRM 53-2-3. TREATED, PRIMED, AND INSTALLED 53-2-3, 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000042700120 20000427 00120 WP 2000 4 27 20000427AP006 1 19991130 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 1 XCW 69 LEFT STATION 120-240 WORN. REMOVED SEAT TRACK IAW DC-8 SRM 51-1-21. INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-1-21, 51-3-0, 51-1-8, 53-2-3. (M) 2 L 7 4 4F RT 4A25 2000042700121 20000427 00121 WP 2000 4 27 20000427AP007 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 5 XCW 0 STATION 1040 WORN. REMOVED DAMAGED AREA OF SEAT TRACK IAW DC-8 SRM 53 -2-3. INSTALLED SEAT TRACK REPAIR IAW DC-8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. EWA (M) 2 L 7 4 4F RT 4A25 2000042700122 20000427 00122 WP 2000 4 27 20000427AP004 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK WORN NR 5 TRACK AT STATION 680. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-3. INSTA LLED REPAIR PLUG IAW DC-8 SRM 52-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. EWA (M) 2 L 7 4 4F RT 4A25 2000042700123 20000427 00123 EU 2000 4 27 USAASA99011 1 19991129 A 3350 CIRCUIT BREAKER AIRBUS A319 A319112 EU COCKPIT TRIPPED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 707UW 949 DCA - FOUND THE EMERGENCY LIGHTS NOT TESTING. MAINTENANCE CYCLED THE CIDS CIRCUIT BREAKER, PERFORMED THE EMERGENCY LIGH TS TEST AGAIN. OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A28NM 2000042800022 20000428 00022 NM 2000 4 28 20000428AP004 1 19991221 A 2150 COALESCER BAG BOEING 757 75723N 1384973 NM ACM BAY CONTAMINATED A AMTA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 519AT 27975 MDW - FLT 866 - DURING TAXI, THE PACKS WERE STARTED AFTER DE-ICING, SMOKE OR FUME WAS GENERATED INTO THE CABIN AND COCKP IT FOR ABOUT 5 MINUTES. RETURNED TO GATE. PERFORMED INSPECTION AND REMOVAL OF COALESCER BAGS SHOWED DE-ICE FLUID CONTA MINATION. REPLACED COALESCER BAGS IN AIR CONDITIONING SYSTEM PER MM 21-00-01, OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 2000042800032 20000428 00032 WP 2000 4 28 20000428AP015 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 5 XCW 0 STATION 240 WORN. REMOVED DAMAGED SEAT TRACK IAW DC-8 SRM 53-2-3, 51- 1-21. INSTALL TRACK REPAIR IAW DC 8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000042800033 20000428 00033 WP 2000 4 28 20000428AP016 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 8 XCW RIGHT STATION 600 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-3. INST ALLED TRACK REPAIR IAW DC-8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000042800034 20000428 00034 WP 2000 4 28 20000428AP017 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 8 XCW 60 RIGHT STATION 680 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-3. I NSTALLED TRACK REPAIR IAW DC-8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000050100024 20000501 00024 WP 2000 5 1 RRXA000199 1 19991203 A 5753 FITTING DOUG DC8 DC873F 302199F WP TE FLAP CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO NR 3 FLAP CANOE TRAILING EDGE TRACK BOLTS HOLES. DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REAMED HOLES TO REMOVE CORROSION, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED TWO NAS4653151-7- 27 BOLTS AND ASSOCIATED HARDWARE IAW FAA APPROVED DER ENGINEERING SKETCH EO 99-186 WITH APPROVED 8110-3 DATED 11/12/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000050100025 20000501 00025 WP 2000 5 1 RRXA000200 1 19991119 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FUSELAGE SKIN UNDER TAIL SKID FAIRING. DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2000050100026 20000501 00026 WP 2000 5 1 RRXA000201 1 19991202 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACH ANGLE IN FRONT OF RT WING LIGHT LENS COMMON TO FILLET PANEL 26 2 RIGHTHAND. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A ND INSTALLED DOUBLERS IAW FAA APPROVED DER ENGINEERING SKETCH EO 99-186 WITH APPROVED 8110-3 DATED 11/19/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000050100061 20000501 00061 WP 2000 5 1 99T64R527EWA 1 19991122 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1220 L36 TO L35R STATION FRAME HAS CORROSION TOP FORWARD SIDE. BLEN DED OUT CORROSION USING MECHANICAL METHOD. FABRICATED REPAIR ANGLES. TREATED AND PRIMED. INSTALLED REPAIR PER EO NR 9 9-186 WITH APPROVED 8110-3 DATED 11/18/99. (M) 2 L 7 4 4F RT 4A25 2000050100062 20000501 00062 WP 2000 5 1 99T64R526EWA 1 19991108 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER BILGE STATION 1160-1200 L32R RIGHT SIDE OF LONGERON HAS CORROSION. BLENDED OUT CORROSIO N USING MECHANICAL METHOD. APPLIED TWO COATES OF PRIMER AND FINISH PER DC-8 SRM 51-1-8. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000050100063 20000501 00063 WP 2000 5 1 99T64R524EWA 1 19991122 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1150-1160 L35R CORROSION ON TOP OF LONGERON. BLENDED OUT CORROSION USING MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110 -3 DATED 11/18/99. (M) 2 L 7 4 4F RT 4A25 2000050100064 20000501 00064 WP 2000 5 1 99T64R520EWA 1 19991119 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT WING NR 3 STUB WING TRAILING EDGE UPPER SCREW HOLES CORRODED AND ELONGATED, XFS 233-245. RE AMED HOLES TO .375 COUNTER SINK TO .65. FABRICATED PLUGS AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/1 5/99. (M) 2 L 7 4 4F RT 4A25 2000050100065 20000501 00065 WP 2000 5 1 99T64R502EWA 1 19991109 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT STATION 960-980 XCW 69 LEFT PRESS PANEL EXFOLIATED UNDER FINGER DOUBLER. REMOVED CORROSION. TREATED AND PRIMED. FABRICATED NEW LARGER FINGER DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROV ED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000050100066 20000501 00066 WP 2000 5 1 99T64R501EWA 1 19991122 A 5753 3751693501 FITTING DOUG DC8 DC873F 302199F WP TE FLAP CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT WING FLAP STATION 410 STOP FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-3- 0. (M) 2 L 7 4 4F RT 4A25 2000050100067 20000501 00067 WP 2000 5 1 99T64R499EWA 1 19991119 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FOUND CORROSION ON FUSELAGE FROM AROUND TAIL SKID FAIRING AND AROUND DOOR 60. REMOVED CORROSION. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/18/99. (M) 2 L 7 4 4F RT 4A25 2000050100068 20000501 00068 WP 2000 5 1 99T64R498EWA 1 19991120 A 5320 3755827501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, A PIT AT STATION 280 AT L33R CORROSION INSIDE LIGHTING HOLE FORWARD DOOR FRAME. REMOVED AND REPLA CED FITTING IAW DC-8 SRM 51-1-8 AND 51-1-20. (M) 2 L 7 4 4F RT 4A25 2000050100069 20000501 00069 WP 2000 5 1 99T64R495EWA 1 19991117 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, B PIT BETWEEN STATION 200-220 AT L31L CRACK IN DOUBLER IN FACTORY SPLICE. REMOVED FITTING. FABRI CATED NEW SPLICE FITTING AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-20. (M) 2 L 7 4 4F RT 4A25 2000050100070 20000501 00070 WP 2000 5 1 99T64R494EWA 1 19991119 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD ACCY COMPARTMENT FRAME 70 HAS CORROSION AROUND FASTENERS FROM L30L TO L31L. REMOVED CORRO SION. FABRICATED STRAP AND EXTERNAL DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/05/99. (M) 2 L 7 4 4F RT 4A25 2000050200253 20000502 00253 EU 2000 5 2 SIMA36411 1 19991223 A 5347 7075T76511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 352SB 340B352 SEAT TRACK CORRODED BEYOND LIMITS AT FS 594.8 TO FS 686.8 TRACK 18.3L. REMOVED AND REPLACED SEAT TRACK AT 18.3L, 92 INC H SECTION. (M) 2 L 7 2 4T RT A52EU 2000050200255 20000502 00255 EU 2000 5 2 SIMA993191 1 19991115 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 219AE 340B219 ABI - FOUND SEAT TRACK AT BL 18.3L AND BL 0.0 CORRODED BEYOND SRM LIMITS. REMOVED FASTENERS EXISTING SEAT TRACKS. DRILL ED FASTENERS HOLES ON NEW SEAT TRACK EXTRUSIONS AND TREATED. INSTALLED NEW SEAT TRACKS AND SECURED. APPLIED DINOTROL T O SEAT TRACK AND SUPPORTS. WORK DONE IAW SAAB 340 AMM 20-10-00, SRM 72LKS 3079 51-40-21, 51-40-22, 51-40-23, 51-40-25, 51-20-42, 51-20-43, 51-20-45 AND STANDARD SRM REPAIR PRINCIPLES. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000050200256 20000502 00256 EU 2000 5 2 SIMA993003 1 19991027 A 2910 AE7064588 HOSE SAAB SF340 340B 7860101 EU NLG WW FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 280AE 340B280 LBB - FLT 3492 - LARGE HYDRAULIC LEAK IN NOSE WHEEL WELL. HAPPENED AFTER TAKEOFF. LANDED WITH NO INCIDENT. REMOVED AN D REPLACED FAILED NOSE LANDING GEAR DOWN-LINE, RESERVICED SYSTEM, LEAK AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000050200262 20000502 00262 EU 2000 5 2 SIMA993392 1 19991205 A 3240 50125893 BRAKE SAAB SF340 340B 7860101 EU RT MLG FAILED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 222NE 340B222 DFW - FLT 3366 - OUTBOARD BRAKE HYDRAULIC SYSTEM FAILED. REMOVED AND REPLACED RIGHT OUTBOARD BRAKE ASSEMBLY. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 2000050200263 20000502 00263 EU 2000 5 2 SIMA993402 1 19991206 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AE 340B319 ABI - DAMAGE TO LT LWR AFT OF FUSELAGE SKIN AT APPROX FS 725.5 TO 760 AND SL 1520 TO 1524. CLEANED AREA AND PERFORMED C UT OUT THREE AREAS OF DAMAGE BETWEEN FS 725.5 AND 760 AND SL 1520 AND 1524. DEBURRED, CLEANED, ALODINED AND APPLIED EPO XY PRIMER TO FUSELAGE AND EDGES OF CUT OUTS. FABRICATED 15.5 BY 32.5 INCH, 13.5 BY 15 INCH, 14.5 BY 14 INCH. REPAIR DO UBLERS AND TAPERED SHIM .050 THICK. DEBURRED ALL HOLES IN FUSELAGE, CLEANED, DEBURRED, COUNTERSUNK ALL HOLES, CHAMFERE EDGES, ALODINED AND APPLIED EPOXY PRIMER TO REPAIR PARTS. APPLIED EPOXY PRIMER TO REPAIR AREAS OF FUSELAGE. APPLIED FA Y SEALANT, POSITIONED REPAIR DOUBLER AND INSTALLED ALL FASTENERS WET WITH SEALANT. FAIRED IN EDGES OF REPAIR DOUBLERS. 2 L 7 2 4T RT A52EU 2000050200264 20000502 00264 EU 2000 5 2 SIMA3641 1 19991228 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU MLG DISCONNECTED A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 301AE 340B301 DFW - FLT 3296 - UNSAFE RIGHT GEAR INDICATION. PERFORMED EMERGENCY PROCEDURES. PULLED EMERGENCY HANDLE FOR GEAR DOORS. AIRCRAFT LANDED WITHOUT EVENT. INSPECTED RIGHT GEAR ASSY AND FOUND MLG DRAG BRACKE CANNON PLUG DISCONNECTED. RECONNE CTED CANNON PLUG, REPLACED EMERGENCY SEPARATION BOLTS FOR LEFT RIGHT GEAR DOORS. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2000050200265 20000502 00265 EU 2000 5 2 SIMA3649 1 19991227 A 5347 7075T76511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 ABI - FOUND CORROSION SRM LIMITS ON SEAT TRACK 18.3L AT FS 300.00. REMOVED AND REPLACED 12 INCH SECTION OF TRACK. (M) 2 L 7 2 4T RT A52EU 2000050200266 20000502 00266 EU 2000 5 2 SIMA36410 1 19991227 A 5347 7075T76511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 373AE 340B373 SEAT TRACK CORRODED BEYOND LIMITS AT BL 0.0. REMOVED AND REPLACED 12 INCH OF SEAT TRACK AT BL 0.0. (M) 2 L 7 2 4T RT A52EU 2000050200268 20000502 00268 EU 2000 5 2 SIMA992992 1 19991026 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 350CF 340B350 ABI - DEN IN RIGHT SIDE OF FUSELAGE SKIN BETWEEN FRAMES AT STATION 363 AND 376 AND BETWEEN SL 1617 AND SL 1618. PERFORM ED A 1 INCH CUTOUT OF DAMAGED SKIN. PERFORMED DYE PENETRANT INSPECTION OF CUTOUT WITH NO DEFECTS NOTED. FABRICATED EXT ERNAL DOUBLER .050 THICK, MEASURING 10.5 INCH BY 7.25 INCH. APPLIED PROTECTIVE COATING OF ALODINE AND EPOXY PRIMERS. F AY SEALED ALL REPAIRS PARTS AND WET INSTALLED ALL FASTENERS (AF138AD4/5). EDGE SEALED REPAIR. RESTORED FINISH. WORK D ONE IAW DATA CONTAINED IN SAAB SRM PART NR 72LKS 3079 REF NR SAAB 340 SRM 53-70-10 PARA 4 REVISION 34 AUG 01/99. AIRCRA FT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 2000050200269 20000502 00269 EU 2000 5 2 SIMA36412 1 19991223 A 5347 7075T76511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 349SB 340B349 ABI - SEAT TRACK CORRODED BEYOND LIMITS AT FS 294.0. REMOVED AND REPLACED SEAT TRACK AT FS 294.0 11 INCH SECTION FROM F S 294 TO 305. (M) 2 L 7 2 4T RT A52EU 2000050200270 20000502 00270 EU 2000 5 2 SIMA36413 1 19991227 A 5347 7075T76511 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 283AE 340B283 ABI - SEAT TRACK CORRODED BEYOND LIMITS AT FS 619 TO 686.88 18.3L. REMOVED AND REPLACED SEAT TRACK 18.3L FROM FS 619 TO FS 686.88. (M) 2 L 7 2 4T RT A52EU 2000050200271 20000502 00271 EU 2000 5 2 SIMA36414 1 19991221 A 5347 7253725193 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 283AE 340B283 ABI - FOUND CORROSION ON SEAT TRACK BEYOND LIMITS AT BL 0. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT BL 0. (M) 2 L 7 2 4T RT A52EU 2000050200284 20000502 00284 NE 2000 5 2 K4HA99101 2 19991207 A 7314 PUMP BOEING 747 747132 1384882 NM PWA JT9 JT9D* NE FUEL SYSTEM FAILED A K4HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 709CK 20247 SEA - FLT 14235 - NR 1 ENGINE COMPRESSOR STALLED AT 26K, ATTEMPTED 2 RESTARTS, OIL PRESSURE 16 PSI. FOUND NR 1 ENGINE F UEL PUMP FAILED. REPLACED NR 1 FCU AND EDF PUMP. ADJUSTED AND TESTED GOOD IAW 747 MM 32-53-04. (M) 2 L 7 4 4F 4 F A20WE E20EA 2000050200285 20000502 00285 WP 2000 5 2 K4HA00104 1 19991214 A 3230 ARM DOUG DC8 DC861 3021952 WP MLG BROKEN A K4HA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 24UA 45963 PHL - FLT 14324 - GEAR WARNING LIGHTS, ON GO AROUND WHEN GEAR HANDLE PLACED UP, GEAR RETRACTED BUT DOORS NOT LATCHES AND GEAR NOT LATCHED, LIGHTS DID NOT GO OUT. FOUND BOGIE UNLOCKED PIVOT ARM BROKEN. REPLACED AND REPAIRED PIVOT ARM IAW 3 2-53. ALSO, FOUND HYD LINE ON MLC DOOR DAMAGED, REPLACED AND REPAIRED. (M) 2 L 7 4 4F 4A25 2000050200292 20000502 00292 NM 2000 5 2 K4HA99095 1 19990802 A 5730 65B00112 SKIN BOEING 747 747269B NM RT WING CORRODED A K4HA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 IAB - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND EXTERIOR OF THE RIGHT WING FROM WING TO BODY FAIRINGS TO TIP, INCLUDING UPPER AND LOWER INSPAR SKINS AND FASTENERS, LEADING AND TRAILING EDGE STRUCTURE BEYO ND SRM LIMITS. REMOVED CORROSION PER SRM 51-10-01. UNABLE TO ACCOMPLISH BLEND OUT PER SRM 57-30-01. (M) 2 L 7 4 4F RT A20WE 2000050200297 20000502 00297 EU 2000 5 2 MALA976678 1 19991228 A 7810 NF24668057 NOZZLE SAAB SF340 340B 7860101 EU ENGINE EXHAUST FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 427XJ 427 MSP - FLT 2757 - RIGHT INTAKE LIGHT CYCLED ON AND OFF DURING FLIGHT WITH ENGINE ANTI-ICE ON, DID NOT CYCLE ON AND OFF ON THE GROUND. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT EXHAUST NOZZLE. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 2000050200298 20000502 00298 EU 2000 5 2 MALA976677 1 19991225 A 3230 HP848430721 VALVE SAAB SF340 340B 7860101 EU MLG FAILED A MALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 15 437XJ 340B437 CVG - FLT 3345 - ON APPROACH TO CVG, GEAR WAS SELECTED DOWN TRANSIT LIGHT CAME ON AND NEVER WENT OUT. NO WHEEL SHOWED D OWN AND LOCKED, HYDRAULIC PUMP RAN CONTINUOUSLY. RETRACTED GEAR AND IT LOCKED IN UP POSITION, PUMP STOPPED. PUT GEAR H ANDLE DOWN SAME RESULT AS BEFORE, ALL HYDRAULIC PRESSURES AND QUANTITIES WERE NORMAL. MX SAID TO PULL AND RESET LANDING CONTROL CB, THIS GAVE NORMAL 3 GREEN INDICATION. MAINTENANCE REPLACED LANDING GEAR CONTROL VALVE. ALL CHECKS GOOD. ( M) 2 L 7 2 4T RT A52EU 2000050200304 20000502 00304 EU 2000 5 2 MALA976683 1 19991230 A 3610 5701C000002 THERMOSTAT BAC 146 AVRO146RJ85A 1500097 EU NR 3 ENGINE INOPERATIVE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 517XJ E2335 DTW - FLT 3601 - JUST AFTER LIFT OFF, THE FOLLOWING LIGHTS CAME ON; NR 3 ENGINE AIR FAULT AND AIR VALVE, THEN INTAKE 3 L OW PRESS AND AIR SUPPLY LIGHTS ON MWP. RETURNED TO DTW. MAINTENANCE REPLACED NR 3 THERMOSTAT. OPS CHECK GOOD. (M) 2 H 7 4 4F RT A49EU 2000050200305 20000502 00305 EU 2000 5 2 MALA976679 1 19991228 A 3020 HTE2500761 VALVE BAC 146 AVRO146RJ85A 1500097 EU NR 2 ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 521XJ E2346 DTW - FLT 3631 - LEFT INNER WING DE-ICE ILLUMINATED WITH SWITCH TURNED ON. CYCLED SWITCH SEVERAL TIMES VALVE WILL NOT O PEN, RETURNED TO DTW. MAINTENANCE REPLACED NR 2 ENGINE DE-ICE VALVE FOR LEFT INNER WING. OPS CHECK GOOD. ALL IAW 30-1 1-17. (M) 2 H 7 4 4F RT A49EU 2000050200308 20000502 00308 EU 2000 5 2 MALA976674 1 19991211 A 5330 SKIN SAAB SF340 SF340A 7850100 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 68XJ 068 CWA - DURING HEAVY CHECK INSPECTION, TWO DENTS IN RIGHT FUSELAGE AT STATION 368.5 AND 384.4. MAINTENANCE REPAIRED IAW E O NR S53035. (M) 2 L 7 2 4T RT A52EU 2000050200310 20000502 00310 NM 2000 5 2 N8TA00010701 1 19991230 A 5210 140N27004 HANDLE BOEING 757 75728A 1384976 NM PAX DOOR CORRODED A N8TA K NONE O OTHER IN INSP/MAINT 1 WP 19 517NA 24260 R4 DOOR EXTERIOR HANDLE PAN ASSY DEEPLY GOUGED AND HOLE NEAR HANDLE. CORROSION FOUND BETWEEN INNER AND OUTER SHAFTS. ( M) 2 L 7 2 4F RT A2NM 2000050200313 20000502 00313 EU 2000 5 2 SIMA0043 1 19991230 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 540 SGF - FLT 3617 - FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. (M) 2 H 7 2 4T RT A53EU 2000050200315 20000502 00315 WP 2000 5 2 AALA996059 1 19990610 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 754RA 49641 OKC - EMERGENCY LIGHTS INOPERATIVE AT ROW 27-29. REMOVED AND REPLACED BATTERY PACK FOR AFT CABIN DOOR EXIT ID. OPS CHE CK GOOD IAW MD-80 MM 33-53-00. (M) 2 L 7 2 4F RT A6WE 2000050200321 20000502 00321 NM 2000 5 2 USAA020004 1 19991128 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 3 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925TS 21244 FLT 6330 - LGA-BOS - FOUND ON L/S, EMERGENCY EXIT LIGHT AT ROW 3 INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKS GOOD. (M) 2 L 7 3 4F A3WE 2000050200326 20000502 00326 WP 2000 5 2 GTIA99001218 1 19991202 A 3210 UNKNOWN DOUG DC9 DC981 3022081 WP RT MLG SMOKE A GTIA O OTHER O OTHER LD LANDING 1 GL 23 806NK 48051 ON LANDING IN MCO, TOWER AND OTHER AIRCRAFT REPORTED SMOKE COMING FROM RIGHT MAIN TIRE AREA. TRANSFERRED TO DMI NR 310 PER MEL 32-10 CAT C PLACARD INSTALLED, DISPATCH NOTIFIED. (M) 2 L 7 2 4F A6WE 2000050200354 20000502 00354 NM 2000 5 2 USAASB99145 1 19990614 A 3233 ACTUATOR BOEING 737 7373B7 1384580 NM NLG MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 504AU 23379 CLT - FLT 821 - AFTER TAKEOFF AND GEAR RETRACTION, CREW RECEIVED A NOSE GEAR UNSAFE LIGHT AND A WIND NOISE FROM THE NOSE GEAR AREA ONCE THE GEAR LEVER WAS PLACED TO THE OFF POSITION FROM THE UP POSITION. CREW PLACED GEAR LEVER BACK TO THE UP POSITION AND WIND NOISE STOPPED BUT UNSAFE LIGHT REMAINED ILLUMINATED. CREW RECYCLED GEAR WITH SAME RESULTS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. ON GEAR EXTENSION, CREW RECEIVED THE NORMAL THREE GEAR G REEN LIGHTS. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPPER DRAG STRUT AND RE TRACT ACTUATOR PER MM 32-21-21 AND 32-33-11. PERFORMED NOSE LANDING GEAR EXTENSION AND RETRACTION CHECK AND ALTERNATE G 2 L 7 2 4F RT A16WE 2000050200357 20000502 00357 NM 2000 5 2 USAA020002 1 19991113 A 3340 32TS13 SWITCH BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A USAA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 EA 19 919TS 20447 FLT6311 - BOS-LGA - HEAVY SMOKE SEEN FROM RUNWAY TURNOFF LIGHT SWITCHES WHEN PLACED TO O. SMOKE STOPPED WHEN SWITCH PLA CED TO OFF. CI NR M849917 ASSIGNED FOR LEFT RUNWAY TURNOFF LIGHT SWITCH PER MEL SEQ 33-12. CI NR M849918 ASSIGNED FOR RT RUNWAY TURNOFF LIGHT SWITCH AS PER LGA TECH CONTROL. WIRING CHECKED TO RUNWAY TURNOFF SWITCHES. WIRING FOUND TO BE GOOD. REPLACED LEFT AND RIGHT RUNWAY TURNOFF LIGHT SWITCHES. OPS CHECKS OK PER MM 33-10-0 ON 11/13/99. (M) 2 L 7 3 4F A3WE 2000050200364 20000502 00364 NM 2000 5 2 ASAA9910277 1 19991222 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 742AS 23136 ANC - PRIOR TO FLT 23, THE AFT GALLEY EMERGENCY EXIT LIGHT WAS FOUND TO BE FLICKERING. REPLACED THE BATTERY ASSEMBLY AN D THE LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000050200365 20000502 00365 NM 2000 5 2 ASAA9910278 1 19991230 A 3397 WIRE BOEING 737 737210C 1384459 NM CABIN DISCONNECTED A D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 NM 01 744AS 21822 SEA - PRIOR TO FLIGHT 65, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WOULD NOT EXTINGUISH. REPAIRED GROUND WIRE ON MID TRANS MITTER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 2000050200392 20000502 00392 2000 5 2 EISA2000001 4 19991229 A 3420 5224280109 RECEIVER COLLINS BOEING 727 727243 138408D NM E/E BAY SHORTED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 17410 B4192 21663 NR 1 NAV RECEIVER INOPERATIVE. INSTALLED SERVICEABLE NAV RECEIVER. (M) 2 L 7 3 4F RT A3WE 2000050200405 20000502 00405 WP 2000 5 2 99T64R492EWA 1 19991027 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT STATION 822 LEFT XCW 51 FLOORBEAM HAS AREA OF EXFOLIATION. (M) 2 L 7 4 4F RT 4A25 2000050200406 20000502 00406 WP 2000 5 2 99T64R490EWA 1 19991105 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING LOOSE B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, NR 2 ENGINE STUB WING TEMP REPAIR FR XS 246 - XS 233 PULLING LOOSE BOTTOM SIDE. REMOVED TEMPORARY REPAIR. TREATED AND PRIMED. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/27/99. ( M) 2 L 7 4 4F RT 4A25 2000050200407 20000502 00407 NE 2000 5 2 99T64R489EWA 2 19991027 A 7310 7751562590 PIPE DOUG DC8 DC873F 302199F WP PWA JT8 JT8* 52044 NE FUEL SYSTEM GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FUEL PIPE ASSY P/N 7751562590 HAS 3 DEEP GOUGES AND COUPLING THREADS HAVE DAMAGE. DRILLED NR 30 H OLE IN CENTER OF 3 GOUGES. FABRICATED PATCH AND WELDED IN PLACE. NDT WELD, NO FLAWS FOUND. PRESSURE TESTED TO 90 PSI, NO LEAKS FOUND. DRESSED THREADS PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/20/99. (M) 2 L 7 4 4F 4 F RT 4A25 E2EA 2000050200408 20000502 00408 WP 2000 5 2 99T64R487EWA 1 19991122 A 2120 DUCT DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, HOT AIR DUCTS DAMAGED THROUGH OUT MAIN CABIN. REPAIRED HOT AIR DUCTS PER EO NR 99-186 WITH APPROV ED 8110-3 DATED 11/14/99. (M) 2 L 7 4 4F RT 4A25 2000050200409 20000502 00409 WP 2000 5 2 99T64R486EWA 1 19991029 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD LT TYPE 1 DOOR BELOW ON FLOORWEB UNDERNEATH DOOR MOUNTING BRACKET HAS CORROSION. REMOVED CORROSION BY MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROV ED 8110-3 DATED 10/20/99. (M) 2 L 7 4 4F RT 4A25 2000050200410 20000502 00410 WP 2000 5 2 99T64R485EWA 1 19991029 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD RIGHT TYPE 1 DOOR BELOW ON FLOOR WEB UNDERNEATH DOOR MOUNTING BRACKET HAS CORROSION. REMO VED CORROSION BY MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH AP PROVED 8110-3 DATED 10/20/99. (M) 2 L 7 4 4F RT 4A25 2000050200411 20000502 00411 WP 2000 5 2 99T64R484EWA 1 19991110 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, SEVERAL AREAS OF CORROSION ALONG ENTIRE LENGTH OF FORWARD WING ATTACH FITTING (BATH TUBE FITTING) L24L. REPLACED LONGERON 24 LEFTO N NON-ROUTINE 1C055 W/O NR 1455. (M) 2 L 7 4 4F RT 4A25 2000050200412 20000502 00412 WP 2000 5 2 99T64R483EWA 1 19991203 A 5720 FITTING DOUG DC8 DC873F 302199F WP RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, NR 3 FLAP CANOE T/E CHAFFED TRACK BOLT HOLES HAVE CORROSION EMANATING FROM THEM. REAMED HOLES TO REMOVE CORROSION. TREATED AND PRIMED. INSTALLED TWO NAS4653151-7-27 BOLTS AND ASSOCIATED HARDWARE PER EO NR 99-186 WIT H APPROVED 8110-3 DATED 11/12/99. (M) 2 L 7 4 4F RT 4A25 2000050200413 20000502 00413 WP 2000 5 2 99T64R482EWA 1 19991105 A 5720 FITTING DOUG DC8 DC873F 302199F WP LT WING CHAFED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, NR 2 FLAP CANOE XW 98 T/E CHAFFED. REMOVED GOUGES BY BLENDING. TREATED AND PRIMED. IT IS ACCEPT ABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000050200414 20000502 00414 WP 2000 5 2 99T64R481EWA 1 19991105 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, NR 2 ENGINE STUB WING SCREWS PULLING THROUGH COUNTER SINKS FR XS 250. REMOVED TEMPORARY REPAIR, T REATED, PRIMED. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/27/99. (M) 2 L 7 4 4F RT 4A25 2000050200415 20000502 00415 WP 2000 5 2 99T64R478EWA 1 19991103 A 5720 FITTING DOUG DC8 DC873F 302199F WP LT WING GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, NR 3 CANOE FITTING INBOARD AFT SIDE IS GOUGED. REMOVED GOUGES BY BLENDING SMOOTH. TREATED AND PR IMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/02/99. (M) 2 L 7 4 4F RT 4A25 2000050200416 20000502 00416 WP 2000 5 2 99T64R479EWA 1 19991026 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LEFT INBOARD WING LE 9 TOP MOUNT HOLE COUNTER SINKS ELONGATED. (M) 2 L 7 4 4F RT 4A25 2000050200417 20000502 00417 WP 2000 5 2 99T64R473EWA 1 19991019 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO CARGO COMPT SEAT TRACK XCW.0 STATION 1540 EXFOLIATED. 2 L 7 4 4F RT 4A25 2000050200418 20000502 00418 WP 2000 5 2 99T64R472EWA 1 19991116 A 5714 WEB DOUG DC8 DC873F 302199F WP WING MISDRILLED B T64R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, HOLE MISDRILLED INSIDE LEFT CENTER TANK AT XCW 69.5 UPPER SURFACE, FUSELAGE STATION 761. BLENDED OUT DRILL START, SPOT FACED. TREATED AND PRIMED. INSTALLED FACTORY FASTENER. IT IS ACCEPTABLE TO RETURN TO SERVICE PE R EO NR 99-186 WITH APPROVED 8110-3 DATED 11/12/99. (M) 2 L 7 4 4F RT 4A25 2000050200419 20000502 00419 WP 2000 5 2 99T64R468EWA 1 19991025 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT STATION 1580 UPPER CUSP LINE FRAME CRACKED AND BENT LONGERON 21 LEFT. CUTOUT DA MAGED SECTION IAW DC-8 SRM 53-2-0. FABRICATED REPAIR FILLER AND DOUBLER IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC -8 SRM 51-1-8. INSTALLED REPAIR IAW DC-8 SRM 53-2-0. (M) 2 L 7 4 4F RT 4A25 2000050200420 20000502 00420 WP 2000 5 2 99T64R470EWA 1 19991018 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT CORROSION ON FLOORBEAM SEAT TRACK ATTACH POINT XCW 40 RIGHT STATION 1440. (M) 2 L 7 4 4F RT 4A25 2000050200421 20000502 00421 WP 2000 5 2 99T64R465EWA 1 19991015 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPE CARGO COMPT STATION 1120 XCW 50 LEFT FLOORBEAM SEAT TRACK MOUNT POINT, AREA OF CORROSION. (M ) 2 L 7 4 4F RT 4A25 2000050200422 20000502 00422 WP 2000 5 2 99T64R464EWA 1 19991105 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIHT WING L/E NR 3 STUB WING UPPER INBOARD EDGE HAS 6 INCH CRACK STATION EX 257.50. COMBINED REPA IR, ALSO TASK 1B178. CUT OUT DAMAGED AREA. FABRICATED REPLACEMENT SECTION FOR SECTION REMOVED. FABRICATED SPLICE PLAT ES. TREATED, PRIMED AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/01/99. (M) 2 L 7 4 4F RT 4A25 2000050200423 20000502 00423 WP 2000 5 2 99T64R463EWA 1 19991108 A 5720 SHIM DOUG DC8 DC873F 302199F WP LT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LEFT WING FRONT LOWER SPAR CAP STATION XFS 520 SHIM PLATE HAS CRACK APPROX .75 INCH. CUT OUT DOUB LER AT CRACK. FINISHED ENDS OF SHIM SMOOTH. TREATED AND PRIMED. BONDED PIECE OF SHIM IN PLACE. IT IS ACCEPTABLE TO R ETURNE TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/08/99. (M) 2 L 7 4 4F RT 4A25 2000050200424 20000502 00424 WP 2000 5 2 99T64R448EWA 1 19990903 A 5720 FLANGE DOUG DC8 DC873F 302199F WP WING GOUGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, FLANGE ON AFT SIDE OF OUTBOARD W/W AT WING AT WING STATION XRS 90.0 GOUGE APPROX .25 INCH IN DIAME TER. (M) 2 L 7 4 4F RT 4A25 2000050200425 20000502 00425 WP 2000 5 2 T64R675EWA 1 19991028 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, NR 3 RIGHT STUB WING UPPER FASTENER HOLES L/E ATTACH POINT HAVE CORROSION. BLEND OUT CORROSION US ING MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/26/99. (M) 2 L 7 4 4F RT 4A25 2000050200426 20000502 00426 WP 2000 5 2 T64R548EWA 1 19991206 A 5320 PLATE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, MAIN CARGO COMPARTMENT STATION 1680 TO 1700 LEFT SCUFF PLATE PANEL GUIDE CRACKED. STOP DRILLED CR ACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRACK IAW MIL-STD-2219 AND NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/24/99. (M) 2 L 7 4 4F RT 4A25 2000050200427 20000502 00427 WP 2000 5 2 99T64R540EWA 1 19991126 A 5320 PLATE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT AFT PASSENGER DOOR SCUFF PLATE CRACKED IN CORNER AND BROKEN ON ENDS. STOP DRILLED CRACK. N DT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRACK PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPR OVED 8110-3 DATED 11/17/99. (M) 2 L 7 4 4F RT 4A25 2000050200428 20000502 00428 WP 2000 5 2 99T64R547EWA 1 19991202 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT WING LEADING EDGE HAS 4 NUT PLATES MISSING TOP OF L/E STATION XFS 22.75 - 24 AND 103-104.25. INSTALLED NAS 1670-4L FASTENERS WET WITH PR 1422B.5 PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/24/99. (M) 2 L 7 4 4F RT 4A25 2000050200429 20000502 00429 WP 2000 5 2 99T64R542EWA 1 19991118 A 5320 THRESHOLD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, R2 DOOR THRESHOLD CRACKED. STOP DRILLED CRACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRA CK PER MIL-STD-2219, NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/17/99. (M) 2 L 7 4 4F RT 4A25 2000050200430 20000502 00430 WP 2000 5 2 99T64R541EWA 1 19991118 A 5320 THRESHOLD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, R1 DOOR THRESHOLD CRACKED. STOP DRILLED CRACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRAC K PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/17/99. (M) 2 L 7 4 4F RT 4A25 2000050200431 20000502 00431 WP 2000 5 2 99T64R530EWA 1 19991119 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, SHEAR TIE CRACKED AT FRAME STATION 660 L21-22R. STOP DRILLED CRACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRACK PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/15/99. (M) 2 L 7 4 4F RT 4A25 2000050200432 20000502 00432 WP 2000 5 2 99T64RR531EWA 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT SEAT TRACK NR 2 WORN STATION 240 XCW 60 LEFT. (M) 2 L 7 4 4F RT 4A25 2000050200455 20000502 00455 NM 2000 5 2 20000502AP001 1 19991027 A 5712 652163229 RIB BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND 1 INCH CRACK IN RIB ADJACENT TO CENTER FOREFLAP TRACK GUIDE, LEFT INBOARD MIDFLAP. REMOVED AND REPLACED FLAP ASSY WITH SERVICEABLE UNIT. (M) 2 L 7 3 4F A3WE 2000050200456 20000502 00456 NM 2000 5 2 20000502AP002 1 19991027 A 5522 SKIN BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND NR 2 S DUCT ANTI-ICE INNER SKIN CRACKED AT LOWER CORNER. LOCATED IN FORTH COMPARTMENT DOWN FROM V STABILIZER ACCE SS PLATE. STOP DRILLED DRILLED CRACK AND INSTALLED REPAIR PER SRM 51-40-2 PAGE 6. (M) 2 L 7 3 4F A3WE 2000050200457 20000502 00457 NM 2000 5 2 20000502AP003 1 19991027 A 5531 STRINGER BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND STRINGER CRACKED IN COMPARTMENT ABOVE FIN STATION 133.8, STRINGER IS FIFTH UP FROM BOTTOM OF COMPARTMENT. INSTALL ED REPAIR PER SRM 55-30-1 FIG 1. (M) 2 L 7 3 4F A3WE 2000050200458 20000502 00458 NM 2000 5 2 20000502AP004 1 19991027 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990, LBL 24. REPLACED SEAT TRACK PER SRM 53-10 -5 FIG 2. (M) 2 L 7 3 4F A3WE 2000050200459 20000502 00459 NM 2000 5 2 20000502AP005 1 19991027 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990 RBL 24. REPLACED SEAT TRACK PER SRM 53-10- 5 FIG 1 SHEET 4. (M) 2 L 7 3 4F A3WE 2000050200460 20000502 00460 NM 2000 5 2 20000502AP006 1 19991027 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990, RBL 45. REPLACED SEAT TRACK PER SRM 53-10 -5 FIG 1. (M) 2 L 7 3 4F A3WE 2000050200461 20000502 00461 NM 2000 5 2 20000502AP007 1 19991027 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990, RBL 45. REPLACED SEAT TRACK PER SRM 53-10 -5 FIG 1. (M) 2 L 7 3 4F A3WE 2000050200462 20000502 00462 NM 2000 5 2 20000502AP008 1 19991027 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 680 TO STATION 740 LBL 24. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. (M) 2 L 7 3 4F A3WE 2000050200463 20000502 00463 NM 2000 5 2 20000502AP009 1 19991027 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 480 TO STATION 690 LBL 45. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. (M) 2 L 7 3 4F A3WE 2000050200464 20000502 00464 NM 2000 5 2 20000502AP010 1 19991027 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 480 TO STATION 690 LBL 24. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. (M) 2 L 7 3 4F A3WE 2000050200465 20000502 00465 NM 2000 5 2 20000502AP011 1 19991027 A 5320 SUPPORT BRACKET BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN R1 DOOR SILL 4 EACH SUPPORT BRACKETS CORRODED. FABRICATED NEW BRACKETS AND REPLACED PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 2000050200466 20000502 00466 NM 2000 5 2 20000502AP012 1 19991027 A 5720 BRACKET BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND BRACKET CRACKED AT RIGHT WING LOWER TRAILING EDGE SUPPORT, OUTBOARD OF NR 6 FLAP TRACK. REMOVED DOUBLER FABRICATE D NEW DOUBLER PER SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2000050200475 20000502 00475 NM 2000 5 2 ASAA9940168 1 19991218 A 3397 WIRE BOEING 737 7374S3 1384711 NM ROWS 18 - 19 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 18-19 WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING/CONNECTOR AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 2000050200491 20000502 00491 CE 2000 5 2 20000502AP014 1 19990712 A 5312 1144400221 BULKHEAD BEECH 1900 1900C 1154161 CE FLANGE CRACKED A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 01 45GL 26738 UC45 DURING A ROUTINE ACE CAMP INSPECTION NR 6, HEAVY AFT FUSELAGE AND EMPENNAGE, FOUND MULTIPLE CRACKS IN CANTED BULKHEAD, S TATION 588.10, IN EXCESS OF CRACK LIMITS PROVIDED IN BEECHCRAFT SERVICE BULLETIN 2564, REV 1 INCORPORATION OF SB 2564 KI T NR 129-4005-1S BEING PERFORMED AS A RESULT OF THE FINDINGS. (M) 2 L 7 2 4T RT A24CE 2000050200492 20000502 00492 CE 2000 5 2 20000502AP015 1 19990418 A 5330 SKIN BEECH 1900 1900C 1154161 CE FUSELAGE CRACKED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 01 41UE 25889 UC41 ON ROUTINE INSPECTION, FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT FUSELAGE STATION 544.25, WATER LINE 113.00. THIS LOCAT ION HAS A BULKHEAD AND STRINGER JOINT LOCATED BEHIND IT. THE BULKHEAD FLANGE WAS ALSO CRACKED AT THIS LOCATION. NO CAU SE FOR THE CRACK COULD BE DETERMINED FROM A VISUAL INSPECTION. ALL DAMAGE WAS REPAIRED IAW THE BEECH STRUCTURAL REPAIR MANUAL. (M) 2 L 7 2 4T RT A24CE 2000050200493 20000502 00493 EA 2000 5 2 20000502AP016 2 19990406 A 7261 310732401 HOUSING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA SCAV PUMP ERODED A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 01 41UE UC41 PCE32006 ON PREFLIGHT INSPECTION, NOTICED OIL LEAKING FROM NR 2 ENGINE. FOUND PIN HOLE IN ENGINE SCAVENGE PUMP HOUSING. TEAR DO WN INSPECTION REVEALED DEEP CAVITATION WEAR THAT HAD PERFORMED THE PUMP BODY WALL. THIS PUMP HOUSING WAS IN COMPLIANCE WITH PWA S/B 13088 CONCERNING REWORK OF THE HOUSING TO ALLEVIATE THIS PROBLEM. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2000050200494 20000502 00494 CE 2000 5 2 20000502AP017 1 19990403 A 7921 10656C COOLER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE OIL CRACKED A YADA O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 01 5632C UC81 PCE97086 MECHANICS NOTICED OIL LEAKING FROM NR 1 ENGINE LOWER CHIN COWLING. REMOVED COWLING AND FOUND OIL COOLER LEAKING AT EDGE WELD. REPLACED OIL COOLER WITH 0 TSN UNIT. SERVICED OIL RESERVOIR WITH 2 QUARTS. THIS IS THE SECOND OIL COOLER TO FA IL ON THIS AIRCRAFTS NR 1 POSITION WITHIN ONE WEEK. BOTH UNITS WERE 0 TIME SINCE OVERHAUL FROM SOUTHWEST COOLER SERVICE , INC AT TIME OF INSTALLATION. BOTH UNITS CRACKED OUT AN EDGE WELD IN THE SAME PLACE. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2000050300020 20000503 00020 WP 2000 5 3 RRXA000216 1 19991011 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM AT STA. 1220 XCW 51 R/H. DAMAGE EXCEEDED LIMITATIONS IAW D C-8 SRM.///// CORRECTIVE ACTION ///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AN D INSTALLED IAW DC-8 SRM 51-1-4, 51-1-8 AND 51-1- 21. (COROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) 2 L 7 4 4F RT 4A25 2000050500037 20000505 00037 NM 2000 5 5 20000505AP008 1 19991027 A 5300 SKIN BOEING 727 727225 1384077 NM JACK PAD PUNCTURED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND SKIN PUNCTURED NEAR FORWARD JACK PAD. REPAIRED SKIN PER BOEING INSTRUCTION MIA-99-00029H. (M) 2 L 7 3 4F A3WE 2000050500038 20000505 00038 NM 2000 5 5 20000505AP009 1 19991027 A 5315 BAC1518347 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND CABIN FLOORBEAM AT STATION 1130, RBL 36, CORROSION AROUND SCREW HOLES. REPAIRED FLOORBEAM PER JOSSAIR DWG NR 72R5 371137 FROM LBL 65 TO RBL 65. (M) 2 L 7 3 4F A3WE 2000050500039 20000505 00039 NM 2000 5 5 20000505AP011 1 19991027 A 5710 BAC5602 FRAME BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 WING TRAILING EDGE CHORD ANGLE CRACKED BELOW NR 8 SPOILER (WBL 125.0). REPAIRED CRACK PER BOEING SERVICE BULLETIN 727-5 7-158 R1. (M) 2 L 7 3 4F A3WE 2000050500040 20000505 00040 NM 2000 5 5 20000505AP012 1 19991027 A 3397 58791 WIRE BOEING 727 727225 1384077 NM CABIN SHORTED A K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FORWARD E-PATH LIGHT STRIP INOPERATIVE ON TEST. REPLACED SHORTED WIRING CABLE LEAD ASSY. (M) 2 L 7 3 4F A3WE 2000050500041 20000505 00041 NM 2000 5 5 20000505AP014 1 19991027 A 5730 SKIN BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND .3125 INCH CRACK AT LEFT WING, UPPER SURFACE AT NR 4 OUTBOARD HOOK CUTOUT, AT AFT OUTBOARD CORNER. STOP DRILLED C RACK, PERFORMED HIGH FREQUENCY EDDY CURRENT TO ENSURE CRACK CONTAINMENT. REPAIR INSTALLED PER SRM 57-30-4. (M) 2 L 7 3 4F A3WE 2000050500042 20000505 00042 NM 2000 5 5 20000505AP016 1 19991027 A 5712 RIB BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND .5 INCH CRACK AT LEFT WING TRAILING EDGE RIB, FROM AFT END TO RIVET HOLE, JUST FORWARD OF OUTBOARD AILERON OUTBOAR D HINGE AREA. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE, TREATED, PRIMED AND PAINTED. INSTALLED IAW 51-40-3. (M) 2 L 7 3 4F A3WE 2000050500043 20000505 00043 NM 2000 5 5 20000505AP017 1 19991027 A 5712 RIB BOEING 727 727225 1384077 NM NR 6 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND NR 1 INCH CRACK AT BOTTOM OF RIB NR 6 SLAT ADJACENT TO INBOARD SIDE OF ACTUATOR ROD END ATTACHMENT. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 2000050500044 20000505 00044 NM 2000 5 5 20000505AP018 1 19991027 A 5754 SKIN BOEING 727 727225 1384077 NM LE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND .5 INCH CRACK AT LEADING EDGE OF RIGHT OUTBOARD FORE FLAP ADJACENT TO NR 7 FLAP TRACK. STOP DRILLED CRACK, FABRIC ATED DOUBLER AND INSTALLED PER SRM 57-50-4 FIG 7. (M) 2 L 7 3 4F A3WE 2000050500045 20000505 00045 NM 2000 5 5 20000505AP019 1 19991027 A 5754 6614734 SKIN BOEING 727 727225 1384077 NM LE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND .375 INCH CRACK IN LOWER SURFACE OF RIGHT OUTBOARD FORE FLAP AT THE OUTBOARD ATTACHMENT AREA. INSTALLED REPAIR PE R SRM 57-50-4 FIGURE 7. (M) 2 L 7 3 4F A3WE 2000050500046 20000505 00046 NM 2000 5 5 20000505AP020 1 19991027 A 5720 65281248 BRACKET BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND 3 INCH CRACK IN NR 8 JACKSCREW FARING AT AFT MOUNT. REMOVED DAMAGED BRACKET AND FABRICATED REPLACEMENT PART. (M) 2 L 7 3 4F A3WE 2000050500047 20000505 00047 NM 2000 5 5 20000505AP021 1 19991027 A 5320 FLANGE BOEING 727 727225 1384077 NM MLG WW CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 APU AIR INLET SCREEN MOUNTING FLANGE CORRODED ALONG BOTTOM FLANGE. FABRICATED REPLACEMENT FLANGE (ANGLE) PER SRM 51-10- 1. (M) 2 L 7 3 4F A3WE 2000050500048 20000505 00048 NM 2000 5 5 20000505AP022 1 19991027 A 5350 FAIRING BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 NR 5 FLAP TRACK MOVEABLE FAIRING, FORWARD RIB CRACKED AT LOCK BOLT SAFETY WIRE HOLE. INSTALLED REPAIR PER SRM 51-40-3 P AGE 3. (M) 2 L 7 3 4F A3WE 2000050500049 20000505 00049 NM 2000 5 5 20000505AP024 1 19991027 A 5754 651622296 SKIN BOEING 727 727225 1384077 NM NR 6 LE SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 NR 6 SLAT INNER SKIN CRACKED AT FASTENER. INSTALLED REPAIR PER SRM 57-50-3 FIG 1. (M) 2 L 7 3 4F A3WE 2000050500050 20000505 00050 NM 2000 5 5 20000505AP025 1 19991027 A 5753 RIB BOEING BOEING 727 727225 1384077 NM TE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND .625 INCH CRACK IN INBOARD MOST RIB OF THE LEFT OUTBOARD MIDFLAP. STOP DRILLED CRACK, HFEC TO VERIFY CRACK CONTAI NMENT. INSTALLED REPAIR PER SRM 51-40-2 FIG 1 SHEET 4. (M) 2 L 7 3 4F A3WE 2000050500051 20000505 00051 NM 2000 5 5 20000505AP026 1 19991027 A 3210 BRACKET BOEING BOEING 727 727225 1384077 NM RT MLG CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 RT MLG DEBOOSTER VALVE BRACKET CRACKED AT TOP CENTER EDGE. STOP DRILLED CRACK, HFEC TO VERIFY CRACK CONTAINMENT. INSTA LLED REPAIR PER SRM 51-40-2 FIG 1 SHEET 4. (M) 2 L 7 3 4F A3WE 2000050500052 20000505 00052 CE 2000 5 5 20000505AP027 1 19990329 A 7921 10656C COOLER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 1 ENGINE OIL CRACKED A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 01 5632C UC81 PCE97086 TWENTY MINUTES SOUTH OF BARROW, AK, LOST OIL PRESSURE ON NR 1 ENGINE AND LOW OIL PRESSURE LIGHT CAME ON. ENGINE SECURED AND AN UNEVENTFUL LANDING WAS EXECUTED. VERIFIED LOW OIL LEVEL. VERIFIED CRACKED OIL COOLER. REPLACED OIL COOLER AND COMPLIED WITH OIL FILTER INSPECTION. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 2000050500053 20000505 00053 CE 2000 5 5 20000505AP028 1 19990821 A 7810 MS937116 SEAL BEECH 1900 1900C 1154161 CE FLOW DIVIDER LEAKING A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 01 1566C 44 UC36 PILOT REPORTED HEAVY EXHAUST FUMES ENTERING CABIN THROUGH BLEED AIR SYSTEM. THIS WAS THE THIRD REPORT IN A ROW. PREVIO US REPAIRS INCLUDED REPLACING A CRACKED EXHAUST STACK. COULD NOT DUPLICATE ON GROUND. THE FINAL DISCREPANCY REPAIRED W AS TO REPLACE NR 1 ENGINE FUEL NOZZLE SEALS. THE FINAL DISCREPANCY WAS VERIFIED ON GROUND RUNS AS WAS THE CORRECTION. (M) 2 L 7 2 4T RT A24CE 2000050500120 20000505 00120 NM 2000 5 5 20000505AP010 1 19991027 A 5730 SKIN BOEING 727 727225 1384077 NM LT WING CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 LEFT WING LOWER SKIN HAS CORROSION IN SEVEN LOCATIONS BETWEEN WING STATION 165 AND WING STATION 270 BELOW FRONT SPAR. R EMOVED CORROSION FROM SEVEN LOCATIONS BLENDED DAMAGE, COLD WORKED HOLES, FLAP PEENED SURFACE AND REPLACED FASTENERS PER BOEING INSTRUCTION MIB-MIA-99-00018H. (M) 2 L 7 3 4F A3WE 2000050500121 20000505 00121 NM 2000 5 5 20000505AP015 1 19991027 A 5720 ANGLE BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 FOUND 1.25 INCH CRACK AT ANGLE INSIDE LEFT WING TRAILING EDGE AT OUTBOARD END OF AFT FALSE SPAR ACCESS THROUGH PANEL 840 7. REMOVED ANGLE AND FABRICATED REPLACEMENT ANGLE AND INSTALLED IAW 51-10-1. (M) 2 L 7 3 4F A3WE 2000050500122 20000505 00122 NM 2000 5 5 20000505AP023 1 19991027 A 5754 SKIN BOEING 727 727225 1384077 NM NR 6 LE SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 887MA 21857 NR 6 SLAT OUTBOARD, HOOK CUTOUT CRACKED. INSTALLED REPAIR PER SRM 57-30-4 FIG 9. (M) 2 L 7 3 4F A3WE 2000050800075 20000508 00075 EU 2000 5 8 20000426SH035 1 19991112 A 3251 618212 ROD BAG JETSTM JETSTM3201 1500217 EU NLG STEERING CRACKED A PAIR K NONE K FLUID LOSS IN INSP/MAINT 1 SO 05 431AM 22368 SJA370 881 NOSE LANDING GEAR STEERING JACK, PN 6182/3, SN SJA-370, WAS RETURNED WITH A REPORT OF ''LEAKING''. TESTING REVEALED FLU ID LEAKAGE FROM INSIDE THE PISTON ROD, PN 618212, SN DHL-8F. UNIT DISASSEMBLED, AND MAGNETIC PARTICLE INSPECTION REVEAL ED AN INDICATION AROUND THE OUTSIDE DIAMETER OF THE PISTON ROD, IN THE TRANSITION RADIUS TO THE CENTER PISTON SECTION. PISTON ROD HAS BEEN RETURNED TO APPH FOR INVESTIGATION. (X) 2 L 7 2 4T RT A56EU 2000050800093 20000508 00093 EU 2000 5 8 20000427SH018 1 19991112 A 3250 618212 ROD BAG JETSTM JETSTM3201 1500217 EU NLG STEERING FAILED B PAIR O OTHER O OTHER NR NOT REPORTED 1 SO 05 958AE JRL2471 958 NOSE LANDING GEAR STEERING JACK, PN 6182/3, S/N JRL-2471, WAS RETURNED FOR OVERHAUL. INSPECTION REVEALED THE PISTON ROD , P/N 618212, S/N 4A HAD MAGNETIC PARTICLE INDICATIONS AROUND THE OUTSIDE DIAMETER OF THE ROD IN THE TRANSITION RADIUS T O THE CENTER PISTON SECTION. PISTON ROD HAS BEEN RETURNED TO APPH FOR INVESTIGATION. (X) 2 L 7 2 4T RT A56EU 2000050800095 20000508 00095 EU 2000 5 8 20000427SH020 1 19991207 A 3250 618212 ROD BAG JETSTM JETSTM3201 1500217 EU NLG STEERING BROKEN B PAIR O OTHER O OTHER NR NOT REPORTED 1 SO 05 916AE SJA437 916 NOSE LANDING GEAR STEERING JACK, P/N 6182/3, S/N SJA-437, WAS RETURNED FOR REPAIR WITH THE COMMENT ''BROKEN''. INSPECTI ON REVEALED THE PISTON ROD, P/N 618212, S/N 93283, HAD BROKEN OFF, AND A PORTION OF THE PISTON ROD WAS STILL THREADED ON THE END WHERE THE END FITING IS ATTACHED. THIS PISTON ROD HAD FAILED AT THE TRANSITION RADIUS AT THE TERMINATION OF TH E INSIDE DIAMETER THREADS ON THE END WHERE THE END FITTING IS ATTACHED. THE FAILED PISTON ROD HAS BEEN RETURNED TO APPH FOR INVESTIGATION. (X) 2 L 7 2 4T RT A56EU 2000051000179 20000510 00179 WP 2000 5 10 99T64R377AR 1 19990324 A 5330 PLATE DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 CUSTOMER REQUEST EVALUATE REPAIR ON FUSELAGE SKIN STATION 445-L22R. REMOVED DAMAGED/CORROSION AREA. FABRICATED FILLERS AND DOUBLERS AND INSTALLED PER EO 99-042 WITH APPROVED FAA FORM 8110-3 DATED 3-2-99. (M) 2 L 7 4 4F 4A25 2000051000180 20000510 00180 WP 2000 5 10 99T64R337AR 1 19990607 A 5320 STCSA106450 BEAM DOUG DC8 DC862 3021970 WP CARGO DOOR JAM MISMANUFACTURED B T64R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 03 1808E 65019 46105 MAIN CARGO DOOR JAM AFT JAM AFT BEAM INBOARD LEAG TO SHORT. FABRICATED DOUBLER SHIM/SPACER IAW EO DWG AS 11042. TREATE D AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW EO AS11042 AND DC-8 SRM 51-1-21 WITH APPROVED FAA FORM 8110-3 DATED MAY 12, 1999. (M) 2 L 7 4 4F 4A25 2000051000181 20000510 00181 WP 2000 5 10 99T64R338AR 1 19990503 A 5320 STCSA106350 CLIP DOUG DC8 DC862 3021970 WP CARGO DOOR JAM MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 MAIN CARGO DOOR, UPPER JAM INSTALLATION CLIPS MISSING 2 EACH. FABRICATED CLIPS AND INSTALLED IAW DWG AS11035 AND DC-8 S RM 51-1-8. (M) 2 L 7 4 4F 4A25 2000051000182 20000510 00182 WP 2000 5 10 99T64R339AR 1 19990525 A 5320 AE244712 FLANGE DOUG DC8 DC862 3021970 WP CARGO DOOR SEAL DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 MAIN CARGO DOOR AFT LOWER CORNER DAMAGED. FABRICATED NEW SEAL DEPRESSOR IAW DC-8 SRM 51-0, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-3-0 AND AS 11038. (M) 2 L 7 4 4F 4A25 2000051000183 20000510 00183 WP 2000 5 10 99T64R340AR 1 19990503 A 5320 AE246315 CLIP DOUG DC8 DC862 3021970 WP CARGO DOOR JAM MISSING A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 MAIN CARGO DOOR UPPER JAM INSTALLATION STATION 500 CLIPS MISSING 2 EACH. FABRICATED CLIPS AND INSTALLED IAW DWG AS11035 AND DC-8 SRM 51-1-8. (M) 2 L 7 4 4F 4A25 2000051000188 20000510 00188 CE 2000 5 10 20000503SH008 1 19990824 A 3246 9561042 WHEEL RKWELL NA265 NA26580 7630108 CE RT MLG FAILED H QH5R A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 15 7148J 98 38033 THE AIRCRAFT RETURNED TO THE USMS RAMP WITH A DISCREPANCY ON THE NR 3 TIRE BEING FLAT. THE NR 3 WHEEL ASSY WAS REMOVED AND THE RIM HAD A 6-10 INCH SECTION OF THE INBOARD RIM LIP BROKEN OFF. (X) 2 L 7 2 4F A2WE 2000051000243 20000510 00243 WP 2000 5 10 99T64R370AR 1 19990707 A 8012 575507913 DUCT DOUG DC8 DC862 3021970 WP NR 2 STARTER WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 NR 2 ENGINE STARTER SUPPLY DUCT BADLY WORN. WELDED DUCT IAW BOEING MESSAGE M7200-99-05-0359. (M) 2 L 7 4 4F 4A25 2000051000244 20000510 00244 WP 2000 5 10 99T64R371AR 1 19990530 A 5411 9753263527 FRAME DOUG DC8 DC862 3021970 WP NR 1 PYLON CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND 5 INCH CRACK IN NR 1 PYLON CAP NUT PLATE FORMER (HORSE COLLAR) YN 161. FABRICATED AND INSTALLED NEW FORMER IAW EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000245 20000510 00245 WP 2000 5 10 99T64R372AR 1 19990305 A 5330 PLATE DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION SKIN BETWEEN STATION 1480-1500 RT L28R. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND D OUBLERS AND INSTALLED PER EO 99-039. (M) 2 L 7 4 4F 4A25 2000051000246 20000510 00246 WP 2000 5 10 99T64R369AR 1 19990311 A 5730 PLATE DOUG DC8 DC862 3021970 WP LT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 TOP LEFT WING CORROSION ON SKIN AND SCREW RUSTY INBOARD END WING L/E BETWEEN 1 AND 2 PYLONS, XFS 291.500. REMOVED CORRO SION, FABRICATED DOUBLER AND FILLER AND INSTALLED PER EO 99-061 AND 99-031. (M) 2 L 7 4 4F 4A25 2000051000247 20000510 00247 WP 2000 5 10 99T64R373AR 1 19990324 A 5542 PLATE DOUG DC8 DC862 3021970 WP RUDDER LIGHTNING STRIKE B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LIGHTNING STRIKE HOLE TOP TRAILING EDGE RUDDER. CUT OUT DAMAGE, FABRICATED FILLERS AND DOUBLERS PER EO 99-030 AND INSTA LLED PER EO 99-030 AND DC-8 SRM 51-1-21. (M) 2 L 7 4 4F 4A25 2000051000248 20000510 00248 WP 2000 5 10 99T64R344AR 1 19990715 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING DENTED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT WING BOTTOM OUTBOARD OF RIGHT MLG PANEL DENTED IN TWO PLACES STATION XW90. NDT AREA, NO CRACKS NOTED, FILLED DENT S WIT HYSOL EA 934 NA, FABRICATED DOUBLER AND INSTALLED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000249 20000510 00249 WP 2000 5 10 99T64R345AR 1 19990604 A 5711 SPAR DOUG DC8 DC862 3021970 WP LT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LT WING AFT SPAR HAS 7 EACH AREAS OF CORROSION AT XRS 190. REMOVED CORROSION, FABRICATED SPECIAL WASHERS AND DOUBLERS A ND INSTALLED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000250 20000510 00250 WP 2000 5 10 99T64R346AR 1 19990607 A 5320 ANGLE DOUG DC8 DC862 3021970 WP LT & RT SIDERAIL DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 CLEAN INSPECT REPAIR AS NECESSARY ALL SIDE RAIL SYSTEM. CUT OUT DAMAGED AREAS FABRICATED ANGLE TIERNAY AND INSTALLED PE R AS 11040. (M) 2 L 7 4 4F 4A25 2000051000251 20000510 00251 WP 2000 5 10 99T64R347AR 1 19990401 A 5730 PLATE DOUG DC8 DC862 3021970 WP WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION ON RIGHT OUTBOARD WING LEADING EDGE INBOARD SEGMENT ALONG TRAILING EDGE FASTENERS. REMOVED CORROSION, F ABRICATED DOUBLERS AND INSTALLED PER EO 99-033. (M) 2 L 7 4 4F 4A25 2000051000252 20000510 00252 WP 2000 5 10 99T64R348AR 1 19990715 A 2120 7760418 DUCT DOUG DC8 DC862 3021970 WP NOSE CHAFED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LEFT UPPER NOSE SECTION AC DUCT (HORSE SHOE) DUCT HAS HOLE CHAFFED IN IT. FABRICATED DOUBLER STRAP AND WELDED TO DUCT I AW BOEING MESSAGE M-7200-99-03383. (M) 2 L 7 4 4F 4A25 2000051000253 20000510 00253 WP 2000 5 10 99T64R349AR 1 19990607 A 8012 5755079501 DUCT DOUG DC8 DC862 3021970 WP NR 3 ENGINE CHAFED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 HEAVY CHAF MARK NR 3 ENGINE STARTER DUCT 10 OCL POS. FABRICATED DOUBLERS AND WELDED ON DUCT IAW BOEING MESSAGE M-7200-9 9-04226. (M) 2 L 7 4 4F 4A25 2000051000254 20000510 00254 WP 2000 5 10 99T64R350AR 1 19990707 A 5711 5597838502 SPAR DOUG DC8 DC862 3021970 WP RT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT WING LOWER FORWARD TANG OF FRONT SPAR OUTBOARD OF STATION XFS 515, 3 HOLES CRACKED. REMOVED NUT CHANNEL IAW DC-8 SRM 51-1-21. REAMED HOLES, EDDY CURRENT HOLES, NO DEFECTS. INSTALLED BUSHING IAW BOEING MESSAGE XXX-MEM-99-0007RR. (M ) 2 L 7 4 4F 4A25 2000051000255 20000510 00255 WP 2000 5 10 99T64R352AR 1 19990429 A 5711 5615058506N SPAR DOUG DC8 DC862 3021970 WP RT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 INBOARD LOWER AUX SPAR CAP CRACKED AT OUTBOARD END WHERE IT ATTACHES TO GEAR TRUNNION RIGHT GEAR LARGE PIN LUG. REMOVED AND INSTALLED NEW AUX SPAR CAP IAW DC-8 S/B 57-85R1. (M) 2 L 7 4 4F 4A25 2000051000256 20000510 00256 WP 2000 5 10 99T64R353AR 1 19990515 A 5330 PLATE DOUG DC8 DC862 3021970 WP CARGO BAY CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 46105 AFT PIT STATION 1090 PRODUCTION BREAK, FINGER DOUBLER BETWEEN L36 AND L35R CRACKED AND BROKEN. REMOVED CRACKED AND BROK EN FINGERS, BLENDED AREA, TREATED AND PRIMED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000257 20000510 00257 WP 2000 5 10 99T64R354AR 1 19990329 A 5210 PLATE DOUG DC8 DC862 3021970 WP PAX DOOR DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 REMOVED L-2 DOOR SCUFF PLATE AND INSPECT EXPOSED AREA. REMOVED SCUFF PLATE, INSPECTED AREA. NO CORROSION NOTED. PLUGG ED EXISTING HOLES TREATED AND RPIMED PER EO 99-053. (M) 2 L 7 4 4F 4A25 2000051000258 20000510 00258 WP 2000 5 10 99T64R355AR 1 19990407 A 5730 PLATE DOUG DC8 DC862 3021970 WP LT WING DENTED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LEFT WING LEADING EDGE DENT AT BOTTOM FORWARD STATION 32. VERIFIED NO CRACKS BY NDT METHOD. FABRICATED DOUBLER AND INS TALLED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000259 20000510 00259 WP 2000 5 10 99T64R356AR 1 19990414 A 5753 PANEL DOUG DC8 DC862 3021970 WP RT TE FLAP CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT FLAP NR 1 REMOVED LEADING EDGE PANEL LIGHT SURFACE CORROSION. REMOVED CORROSION, FABRICATED DOUBLER AND FILLER AN D INSTALLED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000260 20000510 00260 WP 2000 5 10 99T64R390AR 1 19990426 A 5230 AE2420 SHIM DOUG DC8 DC862 3021970 WP CARGO DOOR MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND DURING C-CHECK, MISSING, BROKEN AND/OR LOOSE FASTENER AND MISSING SHIMS (JOGGLE). REPLACED SHIMS IAW DWG AS11041. (M) 2 L 7 4 4F 4A25 2000051000261 20000510 00261 WP 2000 5 10 99T64R391AR 1 19990430 A 5230 AE2420 FASTENER DOUG DC8 DC862 3021970 WP CARGO DOOR LOOSE B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND DURING C-CHECK, MISSING, BROKEN AND/OR LOOSE FASTENER AND MISSING SHIMS (JOGGLE). REPLACED RIVETS, BROKEN/LOOSE F ASTENERS AND MISSING SHIMS IAW DWG AS11041. (M) 2 L 7 4 4F 4A25 2000051000262 20000510 00262 WP 2000 5 10 99T64R392AR 1 19990517 A 5230 AE2420 FASTENER DOUG DC8 DC862 3021970 WP CARGO DOOR MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND DURING C-CHECK, MISSING, BROKEN AND/OR LOOSE FASTENER AND MISSING SHIMS (JOGGLE). INSTALLED FASTENERS, SHIMS IAW DWG AS11041. (M) 2 L 7 4 4F 4A25 2000051000263 20000510 00263 WP 2000 5 10 99T64R368AR 1 19990603 A 5220 DOOR DOUG DC8 DC862 3021970 WP EMERGENCY DOOR CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FORWARD RIGHT O/W EXIT DOOR CORROSION WINDOW FRAME INTERNAL STATION 730. REMOVED CORROSION FILLED WITH HYSOL EA 9309NA. FAIRED TO ORIGINAL THICKNESS. TREATED AND FINISHED IAW DC-8 SRM 51-1-8 PER EO NR 99-061. (M) 2 L 7 4 4F 4A25 2000051000264 20000510 00264 WP 2000 5 10 99T64R393AR 1 19990526 A 5230 AE2420 FASTENER DOUG DC8 DC862 3021970 WP CARGO DOOR MISSING B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND DURING C-CHECK, MISSING, BROKEN AND/OR LOOSE FASTENER AND MISSING SHIMS (JOGGLE). INSTALLED FASTENERS, SHIMS IAW DWG AS11041. (M) 2 L 7 4 4F 4A25 2000051000265 20000510 00265 WP 2000 5 10 99T64R109AR 1 19990426 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LEFT WING TOP OUTBOARD TIP LEADING EDGE. CORROSION AROUND SCREWS STATION 695 XW 761. CORROSION REMOVED IAW DC-8 SRM 51 -1-8. FABRICATED FILLER AND DOUBLER IAW DC-8 SRM 57-2-1 AND INSTALLED IAW DC-8 SRM 51-1-21. (M) 2 L 7 4 4F 4A25 2000051000266 20000510 00266 WP 2000 5 10 99T64R110AR 1 19990426 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LEFT OUTBOARD L/E SECTION CORROSION IN SCREW HOLES, T/E XFS 810 - XFS 960. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABR ICATED FILLER AND DOUBLER IAW DC-8 SRM 57-2-1 AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-22 AND 57-2-1. (M) 2 L 7 4 4F 4A25 2000051000267 20000510 00267 WP 2000 5 10 99T64R111AR 1 19990426 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED B K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND PIT SKIN CORROSION BETWEEN FRAME 580-600 L26R AND L27R. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLE RS AND INSTALLED PER EO 99-019. (M) 2 L 7 4 4F 4A25 2000051000268 20000510 00268 WP 2000 5 10 99T64R357AR 1 19990709 A 3010 TUBE DOUG DC8 DC862 3021970 WP NOSE CHAFED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT NOSE CHIN SCOOP ANTI-ICE TUBE T PULLED LOOSE AND CHAFFED HALF THROUGH O/B OF VALVE. WELDED CHAFFED AREA, REINSTAL LED T TUBE AND WELDED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000269 20000510 00269 WP 2000 5 10 99T64R358AR 1 19990709 A 3010 TUBE DOUG DC8 DC862 3021970 WP NOSE LOOSE B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LEFT NOSE SCOOP ANTI-ICE TUBE T PULLED LOOSE FROM DUCT OUTBOARD OF VALVE. REINSTALLED T AND WELDED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000270 20000510 00270 WP 2000 5 10 99T64R359AR 1 19990510 A 5313 LONGERON DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION L36 BETWEEN STATION 1080-1100. REMOVED CORROSION IAW DC-8 SRM 51-1-8. NEGLIGIBLE AMOUNT MATERIAL REMOV ED. FABRICATED AND INSTALLED STRAP PER EO 99-061 (DUE TO ELONGATED HOLES). (M) 2 L 7 4 4F 4A25 2000051000271 20000510 00271 WP 2000 5 10 99T64R360AR 1 19990506 A 5313 LONGERON DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION L36 BETWEEN 1220-1240. REMOVED CORROSION, FABRICATED STRAP AND INSTALLED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000272 20000510 00272 WP 2000 5 10 99T64R361AR 1 19990506 A 5313 LONGERON DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION L35R BETWEEN 1220-1240. REMOVED CORROSION, FABRICATED STRAPS AND INSTALLED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000273 20000510 00273 WP 2000 5 10 99T64R362AR 1 19990506 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION L35R BETWEEN STATION 1260-1240. REMOVED CORROSION, FABRICATED STRAPS AND INSTALLED PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000274 20000510 00274 WP 2000 5 10 99T64R363AR 1 19990517 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION FRAME UPPER AND LOWER CHORDS AND WEB AREA FRAME 1280, L34R-L31L. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER IAW DC-8 SRM 51-1-21 SIZE 3 INCH BY 12 INCH AND INSTALLED IAW DC-8 SRM 51-1-21. WELDED FRAME FLOOR SUPPORT PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000275 20000510 00275 WP 2000 5 10 99T64R364AR 1 19990303 A 5512 PLATE DOUG DC8 DC862 3021970 WP HORIZONTAL STAB CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LEFT HORIZ STAB LEADING EDGE CORROSION ALONG SCREW ROW TOP STATION XFS 166 TO 328. REMOVED CORROSION, FABRICATED FILLER S AND DOUBLERS AND INSTALLED PER EO 99-061 AND 99-025. (M) 2 L 7 4 4F 4A25 2000051000276 20000510 00276 WP 2000 5 10 99T64R365AR 1 19990511 A 5754 PANEL DOUG DC8 DC862 3021970 WP RT LE FLAP CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT WING OUTBOARD SLOT PANEL HAS CORROSION EMANATING FROM SCREW HOLES XS 497.491. REMOVED CORROSION AND BLENDED AREA PER EO99-061. (M) 2 L 7 4 4F 4A25 2000051000277 20000510 00277 WP 2000 5 10 99T64R366AR 1 19990225 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT WING OUTBOARD STUB WING UPPER TRAILING EDGE CORRODED BEYOND LIMITS XFS 566.250. REMOVED CORROSION, FABRICATED DOU BLER AND FILLER AND INSTALLED PER EO 99-032 AND 99-061. (M) 2 L 7 4 4F 4A25 2000051000278 20000510 00278 WP 2000 5 10 99T64R367AR 1 19990624 A 5754 PANEL DOUG DC8 DC862 3021970 WP RT LE FLAP CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT OUTBOARD INBOARD SLOT PANEL HAS CORROSION XS 442.185. REMOVED CORROSION AND BLENDED AREA IAW EO 99-061. (M) 2 L 7 4 4F 4A25 2000051000327 20000510 00327 2000 5 10 20000510AP002 4 19990130 A 2565 SLIDE BOEING 757 75723N 1384973 NM PAX DOOR DEPLOYED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 523AT 30232 DURING GROUND HANDLING, A CLEANER UNINTENTIONALLY ACTIVATED THE R1 DOOR WITH THE ESCAPE SLIDE HANDLE IN ARMED POSITION. SLIDE FULLY DEPLOYED AND DOOR ASSIST BOTTLE BLOWN. REPLACED SLIDE, RAFT ASSY AT R1 DOOR PER MM 25-66-01 AND REPLACED T HE DOOR ASSIST BOTTLE PER MM 52-11-30. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 2000051000329 20000510 00329 NM 2000 5 10 20000510AP004 1 19991208 A 5700 WEB BOEING 727 727225 1384077 NM TE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND 1.75 INCH CRACK AT LEFT WING OUTBOARD MID FLAP INBOARD MOST RIB AT LOWER AFT END. STOP DRILLED CRACK IAW SRM 51-1 0-1. FABRICATED WEB REPAIR IAW 51-40-2 PAGE 5. HFEC INSPECTION CONFIRMED CRACK WAS CONTAINED. FABRICATED WEB REPAIR I AW 51-40-2 PAGE 5. TREATED/PRIMED IAW 51-10-2 PAGE 1. INSTALLED IAW SRM 51-30-2, PAGE 4. (M) 2 L 7 3 4F A3WE 2000051000330 20000510 00330 NM 2000 5 10 20000510AP005 1 19991208 A 5754 SKIN BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND .5 INCH CRACK AT FASTENER HOLE AND TWO RIVETS CRACKED LOWER LEADING EDGE SKIN OF LEFT WING NR 3 SLAT BELOW UPSTOP PAD AREA. ACCOMPLISHED HFEC INSPECTION AND MARKED END OF CRACK IAW 51-00-00 PART 6. STOPPED DRILLED END OF CRACK IAW 5 1-10-1 PAGE 3. HFEC CONFIRMED CRACK IS CONTAINED IAW 51-00-00 PART 6, FABRICATED DOUBLER IAW 57-50-3 FIG 1. INSTALLED D OUBLER AND FILLER IAW 51-30-5 FIG 1 TREATED, PRIMED AND INSTALLED IAW 57-30-3. (M) 2 L 7 3 4F A3WE 2000051000331 20000510 00331 NM 2000 5 10 20000510AP007 1 19991208 A 5754 SKIN BOEING 727 727225 1384077 NM LE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND .4374 INCH CRACK THROUGH FASTENER HOLE AT RIGHT OUTBOARD FOREFLAP LEADING EDGE ABOVE NR 7 FLAP TRACK AREA. STOP D RILLED CRACK IAW SRM 51-10-1 PAGE 1. FABRICATED COUPLER REPAIR IAW 57-50-4 PAGE 17. HFEC INSPECTION OF CUTOUT CONFIRME D NO CRACKS. FABRICATED NEW LEADING AREA IAW 57-50-4 PAGE 9. INSTALLED REPAIR PARTS IAW 51-10-2 AND 51-30-00. (M) 2 L 7 3 4F A3WE 2000051100067 20000511 00067 WP 2000 5 11 CA990614032 2 19990520 A 7230 31081822 IMPELLER SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP COMPRESSOR SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 17 960350102065 P54093 (CAN) DAMAGE TO NR 1 IMPELLER , REPORT TO FOLLOW. 2 L 7 2 4T 4 T RT A8SW E4WE 2000051100068 20000511 00068 NE 2000 5 11 CA990915033 2 19990908 A 7230 7720090001 COMPRESSOR WHEEL PWA JT8D9A BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE 3RD STAGE DAMAGED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 46060 6722 P687793B P687793B (CAN) COMPRESSOR DAMAGE FROM 3RD STAGE AND BEYOND FOUND, CAUSE UNKNOWN. 2 L 7 2 4F 4 F A16WE E2EA 2000051100120 20000511 00120 EA 2000 5 11 CA000307013 1 19991210 A 5531 C2TP57ND SPAR DHAV C2TP1A DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE VERTICAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11938 201063 (CAN) DURING INSPECTION, STABILIZER CENTER SECTION OF FRONT SPAR FOUND CRACKED. SECTION REPLACED COMPLETE WITH NEW SPLI CE PLATE AND DOUBLERS. 1 H 7 1 3R 3 R A806 5E1 2000051100128 20000511 00128 SO 2000 5 11 CA990521040 1 19990511 A 7120 MOUNT LYC O360E1A6D PIPER PA44 PA44180 7104402 SO LYC O360 O360E1A6 41514 EA ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 6050 RL22577T RL22577T (CAN) FOLLOWING REMOVAL OF RIGHT ENGINE, A CRACK WAS NOTED IN THE EDGE OF THE WELD SECURING THE LEFT UPPER LORD MOUNT RI NG TO THE REST OF THE MOUNT. THE SUBMITTER NOTED THAT THE LT ENGINE MOUNT HAD BEEN REPAIRED IN THE SAME AREA A FEW YEARS AGO. 1 L 7 2 3O 3 O A19S0 E286 2000051100129 20000511 00129 SW 2000 5 11 CA990521049 1 19990506 A 7714 MILG26611B ROLL PIN SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE TACH GENERATOR SHEARED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 040214 P44663 881750 (CAN) ON APPROACH, THE RT ENGINE TACHOMETER BECAME ERRATIC THEN DROPPED TO ZERO RPM. MAINTENANCE FOUND THE TACH GENERA TOR DRIVE SHAFT ROLL PIN SHEARED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2000051100130 20000511 00130 2000 5 11 CA990531018 4 19990518 A 6122 57A3107 COIL LYC F631 BBAVIA 8 8KCAB 2110612 CE LYC O320 AEIO320E1B 41508 EA SNSNCH 74D 74DM EA RELIEF VALVE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA B4469T L546455A (CAN) GOVERNOR OUTPUT PRESSURE LOW. REMOVED OLD SPRING AND FOUND IT TO BE BROKEN INTO THREE PIECES. 1 H 7 1 3O 3 O A21CE 1E12 5 N P88614 2000051100131 20000511 00131 SO 2000 5 11 CA990614030 1 19990326 A 5740 1177303 LIFT STRUT PIPER PIPER PA20 PA20 7102002 SO LYC O290 O290D 41506 EA FORK END CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 3172 57221 (CAN) DURING ROUTINE ANNUAL INSPECTION TO ACCOMPLISH AWD 99-01-05, FRONT STRUT WAS FOUND CORRODED THROUGH NEW N2 FILLED STRUTS AND FORK ENDS ORDERED FROM UNIVAIR. 1 H 7 1 3O 3 O 1A4 E229 2000051100132 20000511 00132 EU 2000 5 11 CA990614045 1 19990310 A 2530 3510001607 COFFEEMAKER AIRBUS 320 A320212 EU GALLEY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 0445 (CAN) NR 1 COFFEE MAKER CIRCUIT BREAKER FOUND OPEN. COFFEE POT REPLACED. 2 L 7 2 4F RT A28NM 2000051100133 20000511 00133 EA 2000 5 11 CA991104001 1 19991011 A 2750 ACTUATOR 601R140001 CNDAIR CL600 CL6002B19 EA TE FLAP LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) FLAPS FAIL ON SELECTION FROM 30-45, STOPPED AT 45 DEGREES. CIRCUIT BREAKER RESET SYSTEM SERVICEABLE. 2 L 7 2 4F RT A21EA 2000051100162 20000511 00162 EA 2000 5 11 CA990531010 2 19990520 A 7414 10382585 POINTS BENDIX 10513659 ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA MAGNETO BROKEN W O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 529 786468 L2515940A (CAN) DURING GROUND RUN, MAGNETO CHECK WAS PERFORMED A PER ENGINE RUN-UP LIST. WHEN THE RIGHT MAG WAS SELECTED, THE RIG HT ENGINED DIED. INVESTIGATION REVEALED THAT THE MAIN POINT CAM FOLLOWER WAS BROKEN OFF AND MISSING. MAGNETO WAS REPLA CED. 1 G 7 1 3O 3 O H11NM E295 2000051100163 20000511 00163 2000 5 11 CA990603032 4 19990514 A 2200 AFCS AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE COCKPIT FAILED W O OTHER O OTHER DE DESCENT 1 CA 731335 (CAN) DURING DESCENT, LOUD SNAP HEARD/FELT THROUGH PEDESTAL. AIRCRAFT FLEW NORMALLY WITH AP SELECTED OFF. CAPTAIN''S S IDESTICK ASSY FAILED. UNIT REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2000051100164 20000511 00164 EU 2000 5 11 CA990614079 1 19990606 A 3230 CONTROLLER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE MLG FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 731555 (CAN) LANDING GEAR DID NOT RETRACT ON INITIAL ATTEMPT, GEAR UNLOCK LIGHT ON. LANDING GEAR CONTROL AND INTERFACE UNIT RE PLACED, SYSTEM CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E29NE 2000051100165 20000511 00165 EU 2000 5 11 CA990614084 1 19990529 A 4900 APU AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE APU BAY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 731661 (CAN) FLIGHT CREW REPORTED ODOR COMING FROM AIR CONDITIONING SYSTEM. APU REPLACED, NO FURTHER REPORTS. 2 L 7 2 4F 4 F RT A28NM E29NE 2000051100166 20000511 00166 EU 2000 5 11 CA990614088 1 19990526 A 3242 BRAKE AIRBUS A340 A340313 EU NR 5 FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CA (CAN) WHEEL NR 5 BRAKE TEMPERATURE AT SHUT DOWN 635 DEGREES CELSIUS. REPLACED NR 5 MAIN WHEEL ASSY AND INSPECTED BRAKE UNIT. NO FAULT FOUND WITH BRAKE UNIT. 2 L 7 4 4F RT A197 2000051100167 20000511 00167 EU 2000 5 11 CA990614094 1 19990520 A 3260 SENSOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE GEAR DOOR FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 CA 731880 (CAN) LGCIU FAULT NR 1 ON ECAM. GEAR DOOR NOT LATCHED UP. RIGHT GEAR DOOR PROXIMITY SENSOR REPLACED. SYSTEM SERVICEAB LE. 2 L 7 2 4F 4 F RT A28NM E29NE 2000051100168 20000511 00168 EA 2000 5 11 CA991007084 1 19991005 A 5753 SKIN DHAV DHAV DHC3 DHC3 2800202 EA PWA R1340 S3H1G 52016 NE LE FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION, FOUND THE RT AILERON FOREFLAP TOP SKIN WAS CRACKED AT CENTER HINGE. THE CRACK WAS REPAIRED. 1 H 7 1 3R 3 R A815 E142 2000051100227 20000511 00227 EU 2000 5 11 CA000324006 1 19991002 A 6320 4638303001 BEVEL GEAR ZENITH 4638001001 BOLKMS 105 BO105S 5626006 EU TRANSMISSION FAILED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 2996 618 (CAN) UPON RECEIPT OF TRANSMISSION FROM OVERHAUL, THE LT INPUT PINION BEVEL GEAR TEETH WERE FOUND DAMAGED. SUBMITTER ST ATED CAUSE OF DAMAGE IS NOT YET KNOWN, BUT COULD BE SPALLING AS A RESULT OF OVERLOADING, CORROSION, OR METAL DEFECT. 1 G 7 2 3U H3EU 2000051100229 20000511 00229 NM 2000 5 11 CA000327003 1 19991203 A 3240 BRACKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 121158 910442 (CAN) DURING FLEET CAMPAIGN TO INSPECT ALL ANTI-SKID VALVE MOUNTING BRACKETS, THE LT BRACKET WAS FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000051100230 20000511 00230 EA 2000 5 11 CA000327004 1 19991203 A 3240 BRACKET DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 123116 (CAN) DURING FLEET CAMPAIGN TO INSPECT ALL ANTI-SKID VALVE MOUNTING BRACKETS, THE LT BRACKET WAS FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 2000051100231 20000511 00231 NM 2000 5 11 CA000327005 1 19991203 A 3240 BRACKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 120152 890915 (CAN) DURING FLEET CAMPAIGN TO INSPECT ALL ANTI-SKID VALVE MOUNTING BRACKETS, THE RT BRACKET WAS FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000051100232 20000511 00232 NM 2000 5 11 CA000327006 1 19991203 A 3240 BRACKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 120322 880521 (CAN) DURING FLEET CAMPAIGN TO INSPECT ALL ANTI- SKID VALVE MOUNTING BRACKETS, THE LT AND RT BRACKETS WERE FOUND CRACKED . 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2000051100233 20000511 00233 EA 2000 5 11 CA000327007 1 19991203 A 3240 BRACKET DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 123126 (CAN) DURING FLEET CAMPAIGN TO INSPECT ALL ANTI-SKID VALVE MOUNTING BRACKETS, THE RT BRACKET WAS FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 2000051100237 20000511 00237 EU 2000 5 11 SIMA993071 1 19991103 A 5347 PLAL7075T7351 CARGO TRACK SAAB SF340 340B 7860101 EU CARGO BAY CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 210AE 340210 ABI - FOUND SEAT TRACK BL 18.3R WAS FOUND CRACKED IN THE CARGO AREA. CUTOUT EXISTING SEAT TRACK FROM STATION 640.138 TO STATION 686.888. DEBURRED, ALODINED, PRIMERED AND PAINTED EDGES. FABRICATED AN EXTRUSION OF 4650000-43 EXTRUDED MATER IAL, DEBURRED, ALODINED AND PAINTED. FABRICATED A 15INCH LONG U-BEAM MATERIAL, DEBURRED, ALODINE AND PAINTED SURFACES. POSITIONED REPAIR U-BEAM INSIDE EXISTING SEAT TRACK AND DRILLED HOLES. FIXED REPAIR EXTRUSION, DRILLED, AND COUNTERSUN K HOLES. MOUNTED NAS 1580-A3T6 BOLTS AND MS 21042L3 NUTS THROUGH TOP OF SEAT TRACK AND NAS 1670-08L-3 FASTENERS THROUGH FLANGES. PRIMED AND PAINTED FASTENERS. WORK DONE IAW SAAB 340 SRM 72LKS 3079 REVISION 34 CHAPTER 53-70-60 AND STANDAR 2 L 7 2 4T RT A52EU 2000051100238 20000511 00238 EU 2000 5 11 SIMA993351 1 19991201 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 214DA 340B214 ABI - SEAT TRACK AT BL 0 CORRODED. REMOVED FASTENERS AND THE EXISTING SEAT TRACK. DRILLED FASTENER HOLES ON THE NEW SE AT TRACK EXTRUSION AND TREATED. INSTALLED THE NEW SEAT TRACK AND SECURED TO SUPPORTS. APPLIED DINOTROL TO SEAT TRACK S UPPORTS. WORK DONE IAW SAAB 340 SRM 72LKS 3079 REV 34, 51-40-00, 51-40-21, 51-40-22, 51-40-23, 51-40-25 AND AMM 72LKS 3 076 REVE 34, AND ATA 20-10-00. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 2000051100248 20000511 00248 NM 2000 5 11 20000510AP006 1 19991208 A 5753 RIB BOEING 727 727225 1384077 NM TE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND .75 INCH CRACK AT RIGHT WING OUTBOARD MIDFLAP INBOARD MOST RIB AT LOWER AFT END. REMOVED JACKSCREW FAIRING. FABR ICATED SINGLE REPAIR IAW 57-50-2 PAGE 5. HFEC CONFIRMED CRACK IS CONTAINED BY STOP HOLE IAW 51-00-00 PAGE 6. INSTALLED ANGLE REPAIR IAW 57-50-2 PAGE 5. REINSTALLED REMOVED FAIRING. (M) 2 L 7 3 4F A3WE 2000051100249 20000511 00249 NM 2000 5 11 20000511AP001 1 19991208 A 5720 ANGLE BOEING 727 727225 1384077 NM AILERON CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 ANGLE HAS .25 INCH CRACK AT BOTTOM OF LEFT WING UPPER TRAILING EDGE PANEL, 5 FT FORWARD OF LEFT INBOARD AILERON INBOARD LEADING EDGE. REMOVED ANGLE AND FABICATED NEW ANGLE IAW 51-10-1 PAGE 2. INSTALLED ANGLE IAW 51-10-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051100250 20000511 00250 NM 2000 5 11 20000511AP002 1 19991208 A 5720 ANGLE BOEING 727 727225 1384077 NM NR 3 FLAP TRACK CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FLAP FAIRING SUPPORT ANGLE HAS 1.125 INCH CRACK AT INBOARD SIDE OF LEFT WING NR 3 FLAP TRACK BELOW AFT FALSE SPAR AREA. REMOVED FAIRING, ACCOMPLISHED HFEC INSPECTION CONFIRMED ENDS OF CRACK IAW 51-00-00 PAGE 6. STOP DRILLED CRACK IAW 51-1 0-1 PAGE 6B. HFEC INSPECTED CONFIRMED CRACK CONTAINED IAW 51-00-00 PAR 6. FABRICATED DOUBLER IAW 51-40-3 FIG 1. TREAT ED, PRIMED AND INSTALLED REPAIR IAW 51-30-2 FIG 1. (M) 2 L 7 3 4F A3WE 2000051100251 20000511 00251 NM 2000 5 11 20000511AP003 1 19991208 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 CABIN SEAT TRACK STATION 344-400 LBL 24 HAS CORROSION. REMOVED CORROSION AND FOUND SEAT TRACK OUT OF LIMITS IAW 51-10-6 PAGE 12. FABRICATED NEW SEAT TRACK STATION 344-400 LBL 24 IAW 53-10-5 PAGE 4. TREATED AND PRIMED IAW 51-10-2 PAGE 2-4 . INSTALLED SEAT TRACK STATION 344-400 LBL 24 IAW 51-30-2 PAGE 6. (M) 2 L 7 3 4F A3WE 2000051100252 20000511 00252 NM 2000 5 11 20000511AP004 1 19991208 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 CABIN SEAT TRACK STATION 344 TO 400 LBL 44 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 53-10-1 FIG 3. FAB RICATED SEAT TRACK IAW 51-30-5 PAGE 1. TREATED INSTALLED IAW 51-10-2 PAGE 1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 2000051100253 20000511 00253 NM 2000 5 11 20000511AP005 1 19991208 A 5755 HINGE BOEING 727 727225 1384077 NM NR 4 SPOILER CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND .3125 INCH CRACK AT CUT OUT ON TOP OF LEFT WING FOR NR 4 SPOILER 2ND FROM OUTBOARD HINGE. STOP DRILLED CRACK IAW 51-10-1 PAGE 6B. HFEC INSPECTION CONFIRMED CRACK CONFINED IAW 51-30-2 PAGE 1. FABRICATED DOUBLER REPAIR IAW 57-30-4 FI G 10.8 PAGE 3. TREATED, PRIMED AND INSTALLED DOUBLER REPAIR IAW 57-30-04 FIG 10 PAGE 3. (M) 2 L 7 3 4F A3WE 2000051100254 20000511 00254 NM 2000 5 11 20000511AP006 1 19991208 A 5720 STRAP BOEING 727 727225 1384077 NM NR 5 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND .03125 INCH CRACK AT RIGHT WING FIXED LEADING EDGE AT AFT INBOARD END OF CUTOUT WHERE NR 5 SLAT INBOARD HOOK GOES INTO. REMOVED FASTENERS IAW 51-30-2 PAGE 1-2. STOP DRILLED CRACK IAW 51-10-1 PAGE 6. HFEC INSPECTION CONFIRMED CRACK CONTAINED IAW 51-00-00. CUT OUT STRAP, HFEC INSPECTION OF STRAP, NO CRACKS NOTED. FABRICATED STRAP IAW 57-30-4 PAGE 26 . TREATED AND PRIMED AND INSTALLED STRAP. (M) 2 L 7 3 4F A3WE 2000051100255 20000511 00255 NM 2000 5 11 20000511AP008 1 19991208 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND CABIN SEAT TRACK LBL 44 STATION 1110 TO 1070 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-10-6 PAG E 6. REMVOED SEAT TRACK IAW 51-30-2 PAGE 5. FABRICATED SEAT TRACK IAW 53-10-5 PAGE 4. TREATED AND PRIMED IAW 51-10-2 PAGE 6. INSTALLED TRACK IAW 51-30-2 PAGE 4. (M) 2 L 7 3 4F A3WE 2000051100256 20000511 00256 NM 2000 5 11 20000511AP009 1 19991208 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 CABIN FLOORBEAM STATION 320 LBL 46 HAS CORROSION AT ANCHOR NOT. REMOVED CORROSION IAW 51-10-6 PAGE 12. ACCOMPLISHED UT THICKNESS CHECK FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA IAW 53-10-8 PAGE 49. FABRICATED ANGLES AND SPLICE, INSTALLE D, TREATED IAW 53-10-2 FIG 9. (M) 2 L 7 3 4F A3WE 2000051100257 20000511 00257 NM 2000 5 11 20000511AP011 1 19991208 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND CABIN SEAT TRACK STATION 360 TO 440 RBL 48 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 12 FOUND OUT OF LIMI TS IAW 51-10-1 PAGE 15. FABRICATED NEW SEAT TRACK IAW 53-10-5 PAGE 21. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW 53 -10-5 PAGE 21. (M) 2 L 7 3 4F A3WE 2000051100258 20000511 00258 NM 2000 5 11 20000511AP012 1 19991208 A 5754 BRACKET BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 MYWA 21854 OUTBOARD BRACKET CRACKED .375 INCH AT INBOARD TRACK OF LET WING NR 3 SLAT WHERE SKIN ATTACHES. REMOVED DAMAGED BRACKET AND FASTENERS IAW 51-30-2 PAGE 6. FABRICATED BRACKET IAW 51-20-1 PAGE 8. TREATED, PRIMED AND INSTALLED IAW 51-30-2 PAG E, 51-20-1 PAGE 18, AND 51-10-2 PAGE 4. (M) 2 L 7 3 4F A3WE 2000051100259 20000511 00259 NM 2000 5 11 20000511AP013 1 19991208 A 5720 6521795335 FAIRING BOEING 727 727225 1384077 NM LEFT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND 1.5 INCH CRACK AT AFT MOUNT HOLE OF LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. (M) 2 L 7 3 4F A3WE 2000051100260 20000511 00260 NM 2000 5 11 20000511AP014 1 19991208 A 5720 6521795336 FAIRING BOEING 727 727225 1384077 NM WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND .75 INCH CRACK AT TOP OF RIGHT INBOARD FLAP AFT TEARDROP FAIRING. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT TEA RDROP FAIRING. (M) 2 L 7 3 4F A3WE 2000051100261 20000511 00261 NM 2000 5 11 20000511AP015 1 19991208 A 5320 ANGLE BOEING 727 727225 1384077 NM CABIN DAMAGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 CABIN FLOOR PANEL SUPPORT RIB BETWEEN STATION 720F AND 740 BL 0 TORN. REMOVED ANGLE SUPPORT BETWEEN STATION 720F TO 740 AT BL 0 IAW 51-30-2 PAGE 1. FABRICATED ANGLE SUPPORT IAW 53-10-4 PAGE 2. TREATED, PRIMED AND INSTALLED IAW 51-10-2 AN D 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051100262 20000511 00262 NM 2000 5 11 20000511AP016 1 19991208 A 5532 SKIN BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 VERTICAL STABILIZER LOWER LEADING EDGE FAIRING NR 9501 HAS .5 INCH CRACK IN SKIN AND CHAFED AROUND END. CUT OUT DAMAGED AREA IAW 51-40-2 FIG 1. FABRICATED DOUBLER IAW 51-40-2 FIG 1. INSTALLED REPAIR IAW 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051100263 20000511 00263 NM 2000 5 11 20000511AP017 1 19991208 A 5720 RETAINER BOEING 727 727225 1384077 NM TE FLAP CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND SEAL RETAINER CHANNEL CORRODED, LOCATED AT TRAILING EDGE OF RIGHT OUTBOARD MID FLAP. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED NEW RETAINER CHANNEL IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNEL IAW 51-30-3 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051100264 20000511 00264 NM 2000 5 11 20000511AP018 1 19991208 A 5320 ANGLE BOEING 727 727225 1384077 NM CABIN CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 CABIN FLOOR SUPPORT INTERCOSTAL TOP ANGLE CRACKED AT SCREWHEAD BL 0 BETWEEN BS 950A AND 950B. REMOVED ANGLE IAW 51-30-2 PAGE 2. FABRICATED NEW ANGLE IAW 51-40-2 PAGE 3. TREATED AND PRIMED IAW 51-10-2. INSTALLED ANGLE IAW 51-30-2 PAGE 12 . (M) 2 L 7 3 4F A3WE 2000051100265 20000511 00265 NM 2000 5 11 20000511AP019 1 19991208 A 5320 SUPPORT BRACKET BOEING 727 727225 1384077 NM CABIN BENT A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 SUPPORT FOR CONDUIT CRACKED AND BENT BS 1110 TO 1130 LBL 33. REMOVED DAMAGED U CHANNEL SUPPORT AND ANGLE BRACKET IAW 51 -30-2 PAGE 1/2. FABRICATED NEW U CHANNEL IAW 51-40-3 PAGE 3. TREATED, PRIMED AND PAINTED IAW 51-10-2 PAGE 2. INSTALLE D U CHANNEL SUPPORT IAW 51-30-2 PAGE 1/2. (M) 2 L 7 3 4F A3WE 2000051100266 20000511 00266 NM 2000 5 11 20000511AP020 1 19991208 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM CABIN GROOVED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND FLOORBEAM BS 1110 LBL 45 HAS 2.5 INCH GROOVE CENTER OF TOP FLANGE. REMOVED WEB, SIDE WALLS AND SEAT TRACK. CUT O UT DAMAGED AREA IAW 53-10-2 FIG 3. ACCOMPLISHED HFEC INSPECTION AROUND EDGES OF CUTOUT IAW 51-00-00. NO CRACKS NOTED. FABRICATED FLOORBEAM AND SPLICES IAW 53-10-2 FIG 3. INSTALLED FLOORBEAM AND SPLICE IAW 51-30-1 PAGE 10. (M) 2 L 7 3 4F A3WE 2000051100267 20000511 00267 NM 2000 5 11 20000511AP021 1 19991208 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND FLOOR SUPPORT BS 1110 TO 1130 LBL 12 CORRODED. REMOVED FLOOR SUPPORT IAW 51-30-2 PAGE 1. FABRICATED SUPPORT IAW 51-10-1 PAGE 2. TREATED AND PRIMED IAW 51-10-2. INSTALLED FLOOR SUPPORT IAW 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051100268 20000511 00268 NM 2000 5 11 20000511AP022 1 19991208 A 5720 FLAP TRACK BOEING 727 727225 1384077 NM WING CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 RIGHT OUTBOARD MID FLAP INBOARD TRAILING EDGE FLAP TRACK CORRODED. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRIC ATED RETAINER IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNEL IAW 51-30-3 PA GE 2. (M) 2 L 7 3 4F A3WE 2000051100269 20000511 00269 NM 2000 5 11 20000511AP023 1 19991208 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 TOP OF FLOORBEAM BS 1110 BL 0 - LBL 12 AND BL 0 - RBL 12. REMOVED CORROSION IAW 51-10-6 PAGE 2. AREA OUT OF LIMITS. C UT OUT DAMAGED AREA IAW 53-10-8 FIG 8. FABRICATED ANGLE AND FILLER REPAIR IAW 53-10-8 FIG 8 SHEET 4-5. ACCOMPLISHED HF EC AROUND EDGES OF CUTOUT IAW PART 6 51-00-00. NO CRACKS NOTED, TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED REPAI R PARTS ON FLOORBEAM STATION 1110 BETWEEN LBL 12 TO RBL 12 IAW 53-10-8 FIG 8. (M) 2 L 7 3 4F A3WE 2000051100270 20000511 00270 NM 2000 5 11 20000511AP024 1 19991208 A 5755 69396331 BRACKET BOEING 727 727225 1384077 NM NR 7 SPOILER CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND NR 7 SPOILER OUTBOARD HINGE SUPPORT CRACKED. REMOVED CRACKED HINGE SUPPORT BRACKET. DRILLED NEW SUPPORT BRACKET IAW 51-10-1 PAGE 14. INSTALLED NEW HINGE SUPPORT BRACKET IAW 51-10-1 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051100271 20000511 00271 NM 2000 5 11 20000511AP025 1 19991208 A 5530 WEB BOEING 727 727225 1384077 NM VERTICAL STAB TORN A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 VERTICAL LEADING EDGE CENTER SECTION INTERIOR WEB IS DAMGED AT THREE CORNERS. CUT OUT DAMAGED AREAS IAWS 51-40-2 PAGES 2/3. HFEC SHOWS NO CRACKS IAW 51-00-00 PAR 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED REPAIR IAW 51-40-2. ( M) 2 L 7 3 4F A3WE 2000051100272 20000511 00272 NM 2000 5 11 20000511AP026 1 19991208 A 5530 WEB BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 VERTICAL FIN LEADING EDGE PANEL 9602 INNER CURVED WEB HAS 1 INCH CRACK AT CORNER. STOP DRILLED CRACK IAW 51-10-1 PAGE 6 13. FABRICATED DOUBLER IAW 51-40-2 PAGE 2, 3, 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED DOUBLER AND WEB IAW 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051100273 20000511 00273 NM 2000 5 11 20000511AP027 1 19991208 A 5320 RETAINER BOEING 727 727225 1384077 NM WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 SEAL RETAINER CRACKED ABOVE RIGHT ELEPHANT EAR FAIRING ON AFT SEGMENT. REMOVED SEAL RETAINER, DRILLED HOLES IN NEW RETA INER IAW 51-30-2 PAGE 5. INSTALLED RETAINER IAW 51-30-2 PAGE 5. (M) 2 L 7 3 4F A3WE 2000051100274 20000511 00274 NM 2000 5 11 20000511AP028 1 19991208 A 5755 BEAM BOEING 727 727225 1384077 NM NR 8 SPOILER CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND J BEAM HAS .375 INCH CRACK AT RIGHT WING ABOVE NR 8 SPOILER ACTUATOR AREA. REMOVED RIGHT WING TOP SKIN AND WALKIN G BEAM PANEL IAW 51-30-2 PAGE 2. REMOVED J BEAM AT RIGHT WING ABOVE NR 8 SPOILER. INSTALLED NEW J BEAM IAW 51-30-2 PAG E 1. INSTALLED REMOVED PANELS. (M) 2 L 7 3 4F A3WE 2000051100275 20000511 00275 NM 2000 5 11 20000511AP029 1 19991208 A 5755 BEAM BOEING 727 727225 1384077 NM NR 7 SPOILER CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND J BEAM HAS TWO .375 INCH CRACKS AT LEFT WING TRAILING EDGE AREA ABOVE NR 7 SPOILER ACTUATOR AREAS. REMOVED WALKIN G BEAM PANEL AND SMALL SKIN PANEL IAW 51-30-2 PAGE 2. REMOVED J BEAM IAW 51-30-2 PAGE 1. INSTALLED J BEAM IAW 51-30-2 PAGE 4. INSTALLED REMOVED PANELS IAW 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051200025 20000512 00025 WP 2000 5 12 RRXA000202 1 19991029 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE ON FLOOR WEB BELOW R1 ENTRY DOOR. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW FAA APPROVED DER ENGINEERING SKETCH EO NR 99-186 WITH APPROVED 8110-3 DATED 10/20/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200026 20000512 00026 WP 2000 5 12 RRXA000203 1 19991028 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE ON NR 3 RIGHT HAND STUB-WING UPPER FASTENER ATTACH HOLES. DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW FAA APPROVED DE R ENGINEERING SKETCH EO NR 99-186 WITH APPROVED 8110-3 DATED 10/26/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2000051200027 20000512 00027 WP 2000 5 12 RRXA000204 1 19991119 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE ON NR 3 RIGHT HAND STUB-WING TRAILING EDGE UPPER SCREWS HOLES XFS 233 TO XFS 245. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REAMED HOLES AN D FABRICATED PLUGS AND INSTALLED IAW FAA APPROVED DER ENGINEERING SKETCH EO NR 99-186 WITH APPROVED 8110-3 DATED 11/15/9 9. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200028 20000512 00028 WP 2000 5 12 RRXA000205 1 19991011 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP CABIN FLOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE FROM FS 857 TO FS 902 AT BL 0.0 BELOW CABIN FLOOR. DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW D C-8 SRM 51-1-8, 51-1-4 & 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200029 20000512 00029 WP 2000 5 12 RRXA000206 1 19991016 A 5320 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO WHEEL WELL PRESSURE PANEL AROUND RIVETS FROM STA 902 TO STA 920 RBL 2 0.0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED FINGER DOUBLERS IAW DC-8 SRM 51-1-8, 51-1-4 & 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200030 20000512 00030 WP 2000 5 12 RRXA000207 1 19991007 A 5320 3640887N ANGLE DOUG DC8 DC873F 302199F WP RT MLG WW CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO WING PRESSURE PANEL ATTACH ANGLE FROM STA 960 TO STA 980 AT RIGHT BUT T LINE8.0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND RE PLACED ATTACH ANGLE AND STRINGER FITTING IAW DC-8 SRM 51-1-20, 51-1-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CO RROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200031 20000512 00031 WP 2000 5 12 RRXA000208 1 19991007 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER CARGO COMPARTMENT LIGHT AT STA 1200 BETWEEN LONGERON NR 9 & 10 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE,TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS AN D INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21 & 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200032 20000512 00032 WP 2000 5 12 RRXA000209 1 19991110 A 5320 3640887N FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR STRINGER BETWEEN STA 960 TO STA 980 AT XCW 10 LT. DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED STRINGER FITTING IAW DC-8 SRM 51-1-21, 51-1-20 & 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200033 20000512 00033 WP 2000 5 12 RRXA000210 1 19991014 A 5313 LONGERON DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON NR 9 BETWEEN STA 1300 TO STA 1340 LT. DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 5 3-2-2 & 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200034 20000512 00034 WP 2000 5 12 RRXA000211 1 19991109 A 5320 3640887N FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO FLOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR STRINGER BETWEEN STA 960 AND STA 980 AT XCW 20 LT. DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED STRINGER FITTING IAW DC-8 SRM 51-1-8, 51-1-21 AND 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200035 20000512 00035 WP 2000 5 12 RRXA000212 1 19991014 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP CARGO FLOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER CARGO COMPARTMENT FLOOR PANEL BETWEEN STA 580 TO STA 840. DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAI R DOUBLER IAW DC-8 SRM 51-1-8, 51-2-0 & 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200036 20000512 00036 WP 2000 5 12 RRXA000213 1 19991115 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 70.0 AFT OF L1 DOOR. DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 51 -3-3, 53-2-3 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200037 20000512 00037 WP 2000 5 12 RRXA000214 1 19991215 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1540 XCW 69 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 51-1-8, 51 -1-21 AND 53-2-0 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200038 20000512 00038 WP 2000 5 12 RRXA000215 1 19991014 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1500 XCW 50 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED IAW DC-8 SRM 51-2-0, 51-1-8 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200039 20000512 00039 WP 2000 5 12 RRXA000217 1 19991025 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1140 XCW 60 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200040 20000512 00040 WP 2000 5 12 RRXA000219 1 19991119 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1540 XCW 53 RT. DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED OUT CORROSION BY MECHANICAL METHOD. ORIGINAL THICKNE SS .132 FINAL THICKNESS .102. RETURNED TO SERVICE IAW FAA APPROVED DER ENGINEERING SKETCH EO NR 99- 186 WITH APPROVED 8 110-3 DATED 11/15/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200041 20000512 00041 WP 2000 5 12 RRXA000220 1 19991112 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP STA. 760 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 760 BETWEEN SEAT TRACKS NR 6 & NR 7. DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CORROSION BY MECHANICAL METHOD. RETURNED TO SERVICE PER FAA APPROVED DER ENGINEERING SKETCH EO NR 99-186 WITH APPROVED 8110-3 DATED 11/11/99. (CORROSI ON DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200042 20000512 00042 WP 2000 5 12 RRXA000221 1 19991109 A 5320 PRESSURE PANEL DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO PRESSURE PANEL FROM STA 857 TO STA 980 AT XCWO-XCW 69 LT. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUB LER REPAIR IAW FAA APPROVED DER ENGINEERING SKETCH EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200043 20000512 00043 WP 2000 5 12 RRXA000222 1 19991101 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1320 BETWEEN SEAT TRACK NR 5 AND 6. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILL ER IAW DC-8 SRM 51-1-21, 51-1-8 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200046 20000512 00046 WP 2000 5 12 RRXA000223 1 19991109 A 5320 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO PRESSURE PANEL FROM STA 960 TO STA 980 AT XCW 69 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER I AW FAA APPROVED DER ENGINEERING SKETCH EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200048 20000512 00048 WP 2000 5 12 RRXA000224 1 19991209 A 5313 LONGERON DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WEB BETWEEN STA 1145 TO STA 1135 UNDER THE SHEAR FOOT AT CUSP L21 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED NEW CUSP T IAW FAA APPROVED DER ENGINEERING SKETCH EO NR 99-186 WITH APPROVED 8110-3 DATED 11/19/99. (CORROSION DA MAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200050 20000512 00050 WP 2000 5 12 RRXA000226 1 19991128 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1680 BETWEEN SEAT TRACK NR 6 & 7. DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM EXTRUSIO N IAW DC-8 SRM 51-1-8, 51-1-21 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051200047 20000512 00047 WP 2000 5 12 AT0000142 1 19991203 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 FOUND AFT CARGO DOOR PIN HAS PREVIOUS REPAIRS SPACING LESS THAN 5.0 INCHES NOT AS REQUIRED PER SRM 52-30. REMOVED 2 PRE VIOUS REPAIRS, FABRICATED DOUBLER ON TRAVLER, HEAT TREATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-03 FIGURE 8, 51-1 0-4 AND 51-10-3. 2 L 7 2 4F A6WE 2000051200049 20000512 00049 WP 2000 5 12 AT0000120 1 19990831 A 5320 ANGLE DOUG DC9 DC932 3022066 WP AIRSTAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND AFT AIRSTAIR NR 8 SUPPORT ANGLE CORRODED BEYOND LIMITS. F ABRICATED NEW ANGLE IAW DC9 SRM 52-60 FIG 3 AND 51-10-03. 2 L 7 2 4F A6WE 2000051200052 20000512 00052 WP 2000 5 12 AT0000121 1 19990831 A 5320 ANGLE DOUG DC9 DC932 3022066 WP AIRSTAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND AFT AIRSTAIR NR 7 SUPPORT ANGLE CORRODED BEYOND LIMITS. F ABRICATED NEW ANGLE IAW DC9 SRM 52-60 FIG 3 AND 51-10-03. 2 L 7 2 4F A6WE 2000051200053 20000512 00053 WP 2000 5 12 AT0000124 1 19991118 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BOWED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 833AT 47489 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND EXISTING FLOORBEAM REPAIR BOWING AT BS 389. INSTALLED NEW DOUBLER IAW DC9 SRM 53-05 FIG 86. 2 L 7 2 4F A6WE 2000051200054 20000512 00054 WP 2000 5 12 AT0000129 1 19991111 A 3230 5919289501 TRUNNION DOUG DC9 DC932 3022066 WP RT MLG CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 846AT 47226 FOUND RIGHT MAIN LANDING GEAR TRUNNION MOUNT HOLE FOR FIXED SIDE BRACE HAS SURFACE CORROSION. REMOVED CORROSION, FABRI CATED REPLACEMENT SHIM AND REINSTALLED FIXED SIDE BRACE IAW DC9 MM 51-10-3 AND EO 99-1370. 2 L 7 2 4F A6WE 2000051200058 20000512 00058 WP 2000 5 12 TWAA0005808 1 19991129 A 5400 ANGLE DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, NUMBER 2 PYLON INTERIOR, O/B VERTICAL ANGLE WAS CRACKED AT BOTTOM, JUST AFT OF 13TH STAGE PNEU MATIC DUCT. DIRECTLY BELOW FIRE SPRAY TUBE. REPAIRED FLANGE USING 2 FABRICATED DOUBLERS OF 0.012 ALUMINUM PER SRM 53-0 1, PAGE 10 FIG 2, SHEET 4. 2 L 7 2 4F A6WE 2000051200059 20000512 00059 WP 2000 5 12 TWAA0005809 1 19991213 A 5400 ANGLE DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, NUMBER 2 PYLON FWD END OF CANNON PLUG CONNECTOR HOOK UP, IN PYLON FWD I/B ANGLE WAS CRACKED OU T BEYOND STOP DRILL. ADDITIONAL DAMAGE FOUND ON ANGLE. REMOVED AND REPLACED PER DRAWING 9958193. CANCELLED ARA 16323 WITH 16323A. REPLACEMENT OF PART PER SPM 6-70-01, 4A PAGE 2 AND 3. 2 L 7 2 4F A6WE 2000051200061 20000512 00061 WP 2000 5 12 TWAA0005807 1 19991119 A 5754 SKIN DOUG DC9 DC932 3022066 WP LE FLAP PUNCTURED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 925L 47357 DURING OP 16 MAINT CHECK, THE RT WING L/E HAD SMALL PUNCTURE HOLE AT L/E ON O/B END, AFT OF O/B END OF NUMBER 5 L/E SLAT . REMOVED WING TIP SUPPORT EXTENSION L/E PER SRM 51-30 AND 51-10-4. SENT PART TO WELDING SHOP TO BE WELDED PER DRAWING 5923349. CLEANED UP OR GROUND WELD PER DRAWING 5923349. PAINTED AND TREATED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30. 2 L 7 2 4F A6WE 2000051600001 20000516 00001 NM 2000 5 16 20000515AP042 1 19990823 A 5320 FRAME BOEING 727 727225 1384077 NM EMERGENCY EXIT CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 LEFT AFT EXIT HATCH FRAME HAS SIGNS OF CORROSION AT LOWER AFT CORNER. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBL ER REPAIR IAW SRM 53-30-1 PAGE 11, 53-303 PAGE 93, 51-30-2 PAGE 18. (M) 2 L 7 3 4F A3WE 2000051600002 20000516 00002 NM 2000 5 16 20000515AP043 1 19990814 A 5754 2040T3 SKIN BOEING 727 727225 1384077 NM NR 4 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND .3125 INCH CRACK AT LT WING FIXED LE CUTOUT ABOVE NR 4 SLAT INBOARD TRACK AREA. STOP DRILLED CRACK. FABRICATED A ND INSTALLED REPAIR IAW SRM 57-30-4 PAGE 7. (M) 2 L 7 3 4F A3WE 2000051600003 20000516 00003 NM 2000 5 16 20000515AP044 1 19990820 A 5754 BAC15141559 ANGLE BOEING 727 727225 1384077 NM NR 1 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 APPROX TWO 2.25 INCH CRACKS AT NR 1 LEADING EDGE SLAT CHORD WHERE OUTBOARD AND INBOARD UPSTOP PAD MOUNTS. REMOVED AND F ABRICATED NEW SLAT CHORD AND INSTALLED IAW SRM 51-10-2 PAGE 4, 51-20-1 FIG 7, 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051600004 20000516 00004 NM 2000 5 16 20000515AP045 1 19990820 A 5754 7075T6 BRACKET BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 BOTH SUPPORT BRACKETS CRACKED .25 INCH AT BOTTOM OF NR 3 SLAT OUTBOARD TRACK WHERE IT ATTACHES TO THE LOWER SKIN EXTENSI ON. REMOVED FABRIATED AND INSTALLED 2 SUPPORT BRACKETS IAW SRMS 51-20-1 FIG 7, 51-20-2 PAGE 7, 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051600005 20000516 00005 NM 2000 5 16 20000515AP046 1 19990817 A 5754 BAC15031420 RIB BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND 1.75 INCH CRACK AT OUTBOARD SIDE LEFT WING FIXED LEADING EDGE RIB AT UPER AFT END THROUGH TWO BOLT HOLES WS 330. REMOVED RIB. FABRICATED AND INSTALLED RIB REPAIR IAW SRM 51-20-1 PAGE 18. (M) 2 L 7 3 4F A3WE 2000051600006 20000516 00006 NM 2000 5 16 20000515AP047 1 19990823 A 5753 652165827 CHANNEL BOEING 727 727225 1384077 NM TE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FUOND 1.5 INCH CRACK AT LEFT WING LOWER TRAILING EDGE OUTBOARD SUPPORT RIB WHERE IT ATTACHES TO DIAGONAL BRACE APPROX 12 INCHES OUTBOARD OF NR 3 SPOILER ACTUATOR. REMOVED AND REPLACED SUPPORT RIB IAW SRM 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051600007 20000516 00007 NM 2000 5 16 20000515AP048 1 19990823 A 5754 STRUCTURE BOEING 727 727225 1384077 NM LE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 APPROX .625 INCH CRACK AT LEFT OUTBOARD FOREFLAP LOWER LEADING ABOVE NR 1 FLAP TRACK. FABRICATED AND INSTALLED DOUBLER REPAIR IW SRM 57-50-4 FIG 1. (M) 2 L 7 3 4F A3WE 2000051600008 20000516 00008 NM 2000 5 16 20000515AP050 1 19990819 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN SEAT TRACK STATION 380-480 RBL 45 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SEAT TRACK STATION 380-480 RBL 45 IAW SRM 53-10-5 PAGE 3, 53-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051600009 20000516 00009 NM 2000 5 16 20000515AP051 1 19990815 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN SEAT TRACK STATION 440 RBL 24 HAS DAMAGE. REMOVED AND REPLACED SEAT TRACK 440 RBL 24 IAW SRM 53-10-5 PAGE 2 , 51-10-2 PAGE 14. (M) 2 L 7 3 4F A3WE 2000051600010 20000516 00010 NM 2000 5 16 20000515AP052 1 19990820 A 5754 2024T3 BRACKET BOEING 727 727225 1384077 NM NR 6 KRUEGER CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 OUTBOARD BRACKET HAS .015625 INCH VISIBLE CRACK AT OUTBOARD END BETWEEN BEND RADIUS AND BOLT HOLE WHERE NR 6 LEADING EDG E FLAP ACTUATOR MOUNTS. REMOVED FABRICATED AND INSTALLED BRACKET IAW SRM''S 51-30-1 PAGE 1, 51-20-1 FIG 7, 51-30-2 PAGE 6. (M) 2 L 7 3 4F A3WE 2000051600011 20000516 00011 NM 2000 5 16 20000515AP053 1 19990820 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT STATION 400 TO 420 RBL 4 HAS CORROSION. REMOVED FLOOR SUPPORT ANGLE, CRACKED. FABRICATED AND INSTALLED ANGLE SUPPORT IAW SRM 51-20-1 FIG 7, 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051600012 20000516 00012 NM 2000 5 16 20000515AP054 1 19990825 A 5347 BAC1518338 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOORBEAM STATION 400 LBL 12 TO RBL 12 HAS CORROSION AND DAMAGED HOLE. REMOVED DAMAGED AREA STATION 400 RBL 24 TO LBL 30. FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-10-8 PAGE 21. (M) 2 L 7 3 4F A3WE 2000051600013 20000516 00013 NM 2000 5 16 20000515AP055 1 19990817 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN SEAT TRACK STATION 680-740 LBL 45 HAS CORROSION, GOUGES AND GROOVES. REMOVED AND REPLACED SEAT TRACK FROM S TATION 720C-720E LBL 45 IAW SRM 53-10-5 PAGE 3, 51-10-2 PAGE 14. (M) 2 L 7 3 4F A3WE 2000051600014 20000516 00014 NM 2000 5 16 20000515AP002 1 19990819 A 5311 BAC15171147 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND RIGHT FUSELAGE INTERIOR AT STATION STRINGER 13 CIRCUMFERENTIAL MOUNTING HAS CRACK. REMOVED FASTENERS, CUT OUT DAM AGED ANGLE AREA. FABRICATE AND INSTALL REPAIR ANGLE IAW SRM 51-40-1 FIG 1, 51-10-2 PAGE 4, 51-40-4 PAGE 3. (M) 2 L 7 3 4F A3WE 2000051600015 20000516 00015 NM 2000 5 16 20000515AP003 1 19990901 A 5311 BAC1517706 FRAME BOEING 727 727225 1384077 NM FUSELAGE CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CRACK IN FORMER AT STATION 930 AND STRINGER 14L. REPAIRED FRAME IAW SB 727-53-0162, REVISION 1. (M) 2 L 7 3 4F A3WE 2000051600016 20000516 00016 NM 2000 5 16 20000515AP004 1 19990820 A 5311 BAC1493577 WEB BOEING 727 727225 1384077 NM FUSELAGE CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT INTERCOSTAL WEB HAS APPROX .25 INCH CRACK AT FORWARD END JUST AFT OF BS 400 BL 0. REMOVED INT ERCOSTAL WEB. FABRICATED AND INSTALLED NEW WEB IAW SRM 51-30-2 PAGE 2, 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 2000051600017 20000516 00017 NM 2000 5 16 20000515AP005 1 19990822 A 5720 2024T30040 WEB BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND LEFT WING LEADING EDGE WBL 92 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER. STOP DRILLED CRACK. F ABRICATED AND INSTALLED DOUBELR REPAIR IAW SRM 53-10-9 PAGE 19. (M) 2 L 7 3 4F A3WE 2000051600018 20000516 00018 NM 2000 5 16 20000515AP006 1 19990822 A 5720 69201141 STIFFENER BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND LEFT WING LEADING EDGE WBL 92 TOP OF CENTER STIFFENER CRACKED AT JOGGLE BELOW HI-LOCK THROUGH ACCESS 6302. REMOVE D AND REPLACED CRACKED STIFFENER IAW SRM 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051600019 20000516 00019 NM 2000 5 16 20000515AP007 1 19990831 A 5530 2024T3 BRACKET BOEING 727 727225 1384077 NM VERTICAL STAB DAMAGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND VERTICAL STABILIZER LEADING EDGE THROUGH PANEL 9502 UPPER RIGHT CORNER BRACKET AND WEB DAMAGED. REMOVED INNER PAN EL, CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-1 PAGE 4, 51-40-2 PAGE 2, 51-30-1 PAGE 1, 55-10 -1 PAGE 6. (M) 2 L 7 3 4F A3WE 2000051600020 20000516 00020 NM 2000 5 16 20000515AP008 1 19990902 A 5753 651920612 FLAP TRACK BOEING 727 727225 1384077 NM LT WING CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND NR 3 FLAP TRACK AFT ATTACH AREA TOP SURFACE CORRODED. ACCOMPLISHED REPAIR AND INSTALLED FLAP TRACK IAW SB 727-57- 0178. (M) 2 L 7 3 4F A3WE 2000051600021 20000516 00021 NM 2000 5 16 20000515AP009 1 19990905 A 5754 SKIN BOEING 727 727225 1384077 NM LT WING LE FLAP CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND LEFT INBOARD FORE FLAP LEADING EDGE HAS CUT AT CENTER SECTION. STOP DRILLED IAW SRM 57-50-4 HFEC, CRACK CONTAINED AT STOP DRILL PART 6 51-00-00, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-4 AND 51-30-2 PAGE 4. (M) 2 L 7 3 4F A3WE 2000051600022 20000516 00022 NM 2000 5 16 20000515AP010 1 19990910 A 5754 SKIN BOEING 727 727225 1384077 NM LT WING KRUGER TORN A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND LEFT WING NR 3 LEADING EDGE FLAP TORN AT TRAILING EDGE. BLENDED OUT DAMAGED AREA PER SRM 57-50-3. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-3 PAGE 10 AND 51-10-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051600032 20000516 00032 NM 2000 5 16 20000515AP001 1 19990825 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SEAT TRACK HAS CORROSION AT STATION 950 THROUGH 990 LBL 45. REMOVED CORROSION OUT OF LIMITS STATION 9 70-1010. REMOVED AND REPLACED SEAT TRACK STATION 970-1010 LBL 45 IAW SRM 53-10-5 FIG 7, 51-10-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051600033 20000516 00033 NM 2000 5 16 20000515AP027 1 19990828 A 5530 AND101341204 ANGLE BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND VERTICAL STAB INNER COMPARTMENT RIB NR 9 RIGHT STRINGER NR 9 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT A REA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M) 2 L 7 3 4F A3WE 2000051600034 20000516 00034 NM 2000 5 16 20000515AP031 1 19990819 A 5320 BAC150643 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT LBL 30 STATION 340 TO COCKPIT WALL HAS CORROSION. REMOVED FLOOR SUPPORT. FABRICATED AND INST ALLED SUPPORT IAW SRM 51-10-2 PAGE 2/4, 51-20-1 FIG 7. (M) 2 L 7 3 4F A3WE 2000051600048 20000516 00048 EU 2000 5 16 CA000404010 1 19990824 A 6520 350A33020005 GEARBOX SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 4481 1469 M1735 345 (CAN) MAKING METAL. FERROUS FLAKES SET OFF THE CHIP LIGHT. DRAINING OF THE OIL REVEALED NON-FERROUS METAL AS WELL. OI L HAD APPEARANCE OF MILKY PAINT. 1 G 7 1 3U 3 U H9EU E19EU 2000051600054 20000516 00054 WP 2000 5 16 CA000404011 1 19990922 A 6210 369A10045 PIN HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R BLADE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 40711 0098848104 CAE832056 (CAN) M/R BLADE FOLDING PIN FOUND BROKEN DURING REMOVAL FOR 300 HOUR INSPECTION. ALL THE PINS WERE SUBSEQUENTLY REMOVED FOR INSPECTION. 1 G 7 1 3U 3 U H3WE E4CE 2000051600055 20000516 00055 SW 2000 5 16 CA000404012 1 19991103 A 2435 23046020 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA STARTER/GEN FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 893 34619 CPPS60468 (CAN) DURING FIRST START OF THE DAY, THE STARTER/GENERATOR WAS MAKING A RUMBLING/GROWLING NOISE. STARTER/GENERATOR REPL ACED AND ON FURTHER INSPECTION, SOME BEARING PLAY WAS NOTED AT THE FAN END. SUSPECT DAMAGED BEARINGS. 1 G 7 1 4U 4 U H4SW E22EA 2000051600139 20000516 00139 NM 2000 5 16 20000515AP040 1 19990831 A 5510 65245712 BEAM BOEING 727 727225 1384077 NM HORZONTAL STAB CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE SKIN FROM NR 1 TO NR 3 ELEVATOR ATTACH HINGE AREA HAS SPOTS OF CORROSION . REMOVED TRAILING EDGE BEAM IAW SRM 51-30-2 PAGE 1. INSTALLED TRAILING EDGE BEAM IAW SRM 55-10-6 FIG 1, 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051600140 20000516 00140 NM 2000 5 16 20000515AP049 1 19990819 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN SEAT TRACK STATION 480-680 LBL 24 HAS CORROSION, GOUGES AND GROOVES. REMOVED AND REPLACED SEAT TRACK FROM S TATION 460-520 RBL 45 IAW SRM 53-10-5 PAGE 2, 51-10-2 PAGE 14. (M) 2 L 7 3 4F A3WE 2000051600156 20000516 00156 NM 2000 5 16 20000515AP032 1 19990819 A 5754 BAC15141559 ANGLE BOEING 727 727225 1384077 NM NR 6 SLAT CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND APPROX 2.5 INCH CRACK AT RIGHT WING NR 6 SLAT LOWER CHORD WHERE INBOARD UPSTOP MOUNTS. REMOVED DAMAGE AREA IAW SR M 51-40-3 PAGE 3. FABRICATED PARTS AND SPLICE IAW SRM 51-40-2 AND INSTALLED REPAIR IAW SRM 51-40-3 PAGE 3. (M) 2 L 7 3 4F A3WE 2000051600157 20000516 00157 NM 2000 5 16 20000515AP021 1 19990824 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN SEAT TRACK STATION 870-970 LBL 45 HAS CORROSION, GOUGES AND GROOVES. REMOVED AND REPLACED SEAT TRACK FROM S TATION 870-950D LBL 45 IAW SRM 53-10-5 PAGE 3, 51-10-2 PAGE 14. (M) 2 L 7 3 4F A3WE 2000051600158 20000516 00158 NM 2000 5 16 20000515AP022 1 19990824 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE GOUGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN SEAT TRACK STATION 870-960 LBL 24 HAS CORROSION, GOUGES AND GROOVES. REMOVED AND REPLACED SEAT TRACK FROM S TATION 870-950 PLUS 10 LBL 24 IAW SRM 53-10-5 PAGE 3, 51-10-2 PAGE 14. (M) 2 L 7 3 4F A3WE 2000051600159 20000516 00159 NM 2000 5 16 20000515AP023 1 19990824 A 5210 PANEL BOEING 727 727225 1384077 NM PAX DOOR CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 L1 DOOR LINNER SUPPORT PANEL AT LOWER CENTER AREA CRACKED AT HOLE. REMOVED FABRICATED AND INSTALLED NEW PANEL L1 DOOR L INER SUPPORT IAW SRM 52-10-1 PAGE 1, 51-30-2 PAGE 4, 52-10-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000051600160 20000516 00160 NM 2000 5 16 20000515AP024 1 19990819 A 5210 PANEL BOEING 727 727225 1384077 NM PAX DOOR CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 L2 DOOR FORWARD LINNER SUPPORT PANEL CRACKED AT UPPER CORNER AREA. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLE R REPAIR IAW SRM 51-10-0 PAGE 6, 51-40-2 PAGE 1, 51-40-2 PAGE 5. (M) 2 L 7 3 4F A3WE 2000051600161 20000516 00161 NM 2000 5 16 20000515AP025 1 19990828 A 5530 AND101341204 ANGLE BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND VERTICAL STAB INNER COMPARTMENT NR 6 RIGHT SUPPORT WEB BETWEEN STRINGER NR 8 AND NR 9 CRACKED AT LOWER CORNER. RE MOVED CRACKED ANGLE. FABRICATED AND INSTALLED ANGLE IAW SRM 51-40-3 PAGE 7. (M) 2 L 7 3 4F A3WE 2000051600162 20000516 00162 NM 2000 5 16 20000515AP026 1 19990828 A 5530 AND101341204 ANGLE BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND VERTICAL STABILIZER INNER COMPARTMENT NR 8 RIGHT STRINGER NR 8 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT AREA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M) 2 L 7 3 4F A3WE 2000051600163 20000516 00163 NM 2000 5 16 20000515AP028 1 19990829 A 5511 2040T3 FRAME BOEING 727 727225 1384077 NM HORIZONTAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 LEFT HORIZONTAL STABILIZER INNER COMPARTMENT NR 5 INBOARD RIB HAS SUPPORT CHORD CRACKED. CUT OUT SKIN TO GAIN ACCESS TO SUPPORT CHORD 3 INCH BY 6 INCH. REMOVED SUPPORT CHORD. FABRICATED AND INSTALLED SUPPORT CHORD. INSTALLED DOUBLER REP AIR TO SKIN CUT OUT IAW SRM 55-10-3 PAGE 7, 55-10-4 PAGE 4. (M) 2 L 7 3 4F A3WE 2000051600164 20000516 00164 NM 2000 5 16 20000515AP011 1 19990825 A 5320 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT ANGLE AT STATION 1045 LBL 25 HAS CORROSION. REMOVED FABRICATE AND INSTALLED SUPPORT ANGLE IAW SRM 51-20-01 FIG 7, 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051600165 20000516 00165 NM 2000 5 16 20000515AP012 1 19990829 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SEAT TRACK SUPPORT BASE HAS CORROSION AT STATION 1020 THROUGH 1130 LBL 25. REMOVED CORROSION, OUT OF LIMITS STATION 990-1130. REMOVED AND REPLACED SEAT TRACK STATION 990-1130 IAW SRM 53-10-30 PATE 20, 51-10-2 PAGE 1. (M ) 2 L 7 3 4F A3WE 2000051600166 20000516 00166 NM 2000 5 16 20000515AP013 1 19990826 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SEAT TRACK STATION 1060 RBL 24 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STATION 1060 RBL 24 IAW SRM 53-10-5 PAGE 3, 51-10-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051600167 20000516 00167 NM 2000 5 16 20000515AP014 1 19990826 A 5320 BAC1503100068 INTERCOSTAL BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR INTERCOSTAL AT STATION 1110 THROUGH 1130 AT BL 0 HAS CORROSION AT UPPER AND LOWER SURFACE. REMOVED IN TERCOSTAL. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2 PAGE 6, 51-20-1 PAGE 4. (M) 2 L 7 3 4F A3WE 2000051600168 20000516 00168 NM 2000 5 16 20000515AP015 1 19990902 A 5315 BAC1518338 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOORBEAM AT STATION 1110 RBL 18 THROUGH LBL 18 HAS CORROSION AT UPPER AND LOWER SURFACE. REMOVED CORROSION AT FLOORBEAM BETWEEN LBL 18 THROUGH RBL 16. REPAIRED FLOORBEAM AT RBL 17 IAW SRM 53-10-8 FIG 3. (M) 2 L 7 3 4F A3WE 2000051600169 20000516 00169 NM 2000 5 16 20000515AP019 1 19990820 A 5320 BAC1510335 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN AFT LEFT LAV FLOOR SUPPORT ANGLE HAS CORROSION STATION 1140 LBL 54. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 51-20-1 PAGE 18, 51-30-2 PAGE 6. (M) 2 L 7 3 4F A3WE 2000051600172 20000516 00172 SW 2000 5 16 CA000404014 1 19991208 A 6730 41103750 SERVO BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL PILOT VALVE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 708 3480 CAE801518BA (CAN) EXCESSIVE VERTICAL PLAY AT PILOT INPUT TRUNNION AND PILOT VALVE AREA OF THE SERVO. FEEDBACK IS EXCESSIVE, ALSO CH ATTERING AN VIBRATING AND NOISY DURING GROUND RUN AND TEST FLIGHTS. 1 G 7 1 3U 3 U H2SW E4CE 2000051600177 20000516 00177 NM 2000 5 16 20000515AP041 1 19990908 A 3350 1102833 LIGHT BOEING 727 727225 1384077 NM LT WING INOPERATIVE A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 AFT AIRSTAIR UPPER EMERGENCY LIGHT DOES''NT WORK. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW MM 33-50-61 PAGE 40 3. (M) 2 L 7 3 4F A3WE 2000051600214 20000516 00214 SO 2000 5 16 C2XA00IA070 1 19990311 A 2150 22051201 ACM EMB 120 EMB120RT SO FUSELAGE INOPERATIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 12709 120101 IAH - FLT 3686 - DURING CLIMB, THE CREW REPORTED SMOKE IN THE CAIN. THE AIRCRAFT RETURNED IAH WITHOUT INCIDENT, WHERE M AINTENANCE UNSTUCK THE RIGHT ACM AND OPERATIONLLY CHECKED. THE PROBLEM REPEATED ON FINAL FOR FLIGHT 3686 WHERE THE AIRC RAFT LANDED AT MLU WITHOUT INCIDENT. MAINTENANCE PLACED THE RIGHT ACM ON MEL NR 21-50-2 CONTROL NR 173565, AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 2000051600347 20000516 00347 NE 2000 5 16 EISA2000033 2 19991229 A 7532 658385B1 BLEED VALVE BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE WORN A EISA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SW 07 74318 20051 DURING ENGINE RUN ACCELERATION PRIOR TO TAKEOFF ROLL ENGINES WERE STABILIZED ABOUT 1.4 EPR AND WE HEARD A LOUD BANG. AT ABOUT 1.7 EPR AFTER CHECKING ALL THREE ENGINES WE HEAR THE SAME BANG AND COMPRESSOR STALL ON NR 2 ENGINE WHICH WHICH WE SHUT DOWN AND RETURNED TO THE RAMP. VISUALLY CHECK INLET, EXHAUST AND PULLED END CAPS. NO DEFECTS FOUND. REMOVED AND REPLACED PRESSURE BLEED CONTROL VALVE, OPS CHECK GOOD. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000051600391 20000516 00391 NM 2000 5 16 USAA040002 1 19990804 A 3350 90052 CHARGER BOEING 727 727227 1384078 NM CABIN INOPERATIVE A K NONE O OTHER IN INSP/MAINT 1 EA 19 924TS 21041 FOUND ON L/S CHECK, RIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK. (M ) 2 L 7 3 4F A3WE 2000051600405 20000516 00405 EU 2000 5 16 A6WA0000005 1 19991213 A 5712 RIB BAG BAE146 BAE146200A 1500266 EU RIGHT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 292UE E2087 RIGHT WING TIP FALSE RIB HAS A CRACK. REPAIRED ASSY PER ABOVE IAW AW-57-02-9412-06. (M) 2 H 7 4 4F RT A49EU 2000051600406 20000516 00406 2000 5 16 A6WA9900124 4 19991125 A 3418 STICK SHAKER DORNER DO32 DO328100 2996000 NM STALL WARNING FAILED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 330PH 3008 FLT 7127 - DEN-BIS - AOA FAIL/STICK PUSHER FAIL ON TAKEOFF ROLL. MESSAGES WENT AWAY AFTER 30 SECONDS. RESET STICK PUSH ER SYSTEM. OPS CHECKS GOOD. (M) 2 H 7 2 4T RT A45NM 2000051800006 20000518 00006 WP 2000 5 18 RRXA000218 1 19991029 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1500 XCW 40 AND XCW 53 RT. DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 S RM 51-1-8, 51-1-20 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000051800054 20000518 00054 WP 2000 5 18 99T64R343AR 1 19990707 A 2780 GUIDE DOUG DC8 DC862 3021970 WP RT WING BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 RIGHT WING INBOARD LEADING EDGE OUTBOARD END HAS CABLE GUIDE (PHENOLIC BLOCK) BROKEN. APPLIED EPOXO 88 TWO PART EPOXY W ITH AN ADDITIONAL 4 FASTENERS PER EO 99-061. (M) 2 L 7 4 4F 4A25 2000051800058 20000518 00058 EU 2000 5 18 20000504SH023 1 19990104 A 3231 DOOR AMD FALC20 FALCON 2720302 EU MLG MALFUNCTIONED A CEDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 207CA 153 AIRCRAFT TOOK OFF FROM MCI. GEAR DOORS WOULD NOT CLOSE. AIRCRAFT LANDED. GEAR DOORS CLOSED. CYCLED GEAR 50 TIMES. C OULD NOT DUPLICATE PROBLEM. SUSPECT ICE, SNOW FROZEN ON GEAR CAUSED PROBLEM. (X) 2 L 7 2 4F A7EU 2000051800059 20000518 00059 CE 2000 5 18 20000504SH024 1 19990611 A 2612 875135 FIRE LOOP LEAR 25 25B 5170511 CE LT ENGINE CHAFED A CEDA O OTHER N FALSE WARNING DE DESCENT 1 SW 05 233CA 133 AT FL 430, THE LT FIRE DETECTON LIGHT CAME ON. THE THROTTLE WAS PULLED BACK AND LIGHT SENT OUT. ON DESCENT, THE LIGHT CAME BACK ON. AIRCRAFT LANDED AT STL WITH NO FURTHER INCIDENTS. (X) 2 L 7 2 4J A10CE 2000051800063 20000518 00063 CE 2000 5 18 20000504SH028 1 19991227 A 3230 141EN24 SWITCH RKWELL NA265 NA26580 7630108 CE RT MAIN GEAR FAILED B K NONE O OTHER IN INSP/MAINT 1 SW 15 71460 3805 THE AIRCRAFT RETURNED TO THE USMS RAMP WITH A LOG ENTRY STATING THE GEAR WILL NOT LOCK NORMAL, FREE FELL GEAR ALL GREEN. THE AIRCRAFT WAS PLACED ON JACKS AND THE GEAR SYSTEM WAS INSPECTED. (X) 2 L 7 2 4F A2WE 2000051800068 20000518 00068 NM 2000 5 18 20000515AP029 1 19990822 A 5320 BAC150643 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT ANGLE HAS CORROSION AT STATION 1030 THROUGH 1050 LBL 18. REMOVED FLOOR SUPPORT ANGLE. FABRIC ATED AND INSTALLED FLOOR SUPPORT IAW SRM 51-30-2 PAGE 2, 51-20-1 FIG 7. (M) 2 L 7 3 4F A3WE 2000051800069 20000518 00069 NM 2000 5 18 20000515AP030 1 19990822 A 5315 BAC1518338 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOORBEAM STATION 1030 LBL 25 THROUGH RBL 25 HAS CORROSION. REMOVED CORROSION, OUT OF LIMITS. FABRICATE AN GLE REPAIR AND STRAP IAW SRM 51-40-2 PAGE 6, 51-10-6 PAGE 12. (M) 2 L 7 3 4F A3WE 2000051800070 20000518 00070 NM 2000 5 18 20000515AP016 1 19990819 A 5320 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT ANGLE STATION 1050 THROUGH 1110 LBL 18 HAS CORROSION. REMOVED CORROSION STATION 1070 AND 1110 . REPLACED ANGLE AT STATION 1090 SRM 51-20-1 PAGE 18, 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051800071 20000518 00071 NM 2000 5 18 20000515AP017 1 19990825 A 5320 BAC1518334 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT ANGLE HAS CORROSION STATION 1069 LBL 34. REMOVED CORROSION. FABRICATED AND INSTALLED ANGLE S UPPORT IAW SRM 51-20-1 PAGE 18, 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000051800072 20000518 00072 NM 2000 5 18 20000515AP018 1 19990825 A 5320 CHANNEL BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN AFT LEFT LAVATORY FLOOR SUPPORT ANGLE HAS CORROSION STATION 1140 LBL 36. REMOVED CORROSION, FOUND HAT CHANN EL OUT OF LIMITS. FABRICATED AND INSTALLED HAT CHANNEL IAW SRM 51-20-1 PAGE 18, 51-30-2 PAGE 6. (M) 2 L 7 3 4F A3WE 2000051800073 20000518 00073 NM 2000 5 18 20000515AP020 1 19990819 A 5320 BAC150643 ANGLE BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 803MA 22434 FOUND CABIN FLOOR SUPPORT ANGLE HAS CORROSION STATION 1069 LBL 54 TO 64. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRI CATED AND INSTALLED SUPPORT ANGLE LBL 54 IAW SRM 51-20-1 PAGE 18, 51-30-2 PAGE 6. (M) 2 L 7 3 4F A3WE 2000052200026 20000522 00026 WP 2000 5 22 RRXA000227 1 19991201 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1580 BETWEEN NR 1 AND NR 2 SEAT TRACK. DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW D C-8 SRM 53-2-0, 51-1-8 & 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000052200027 20000522 00027 WP 2000 5 22 RRXA000228 1 19991207 A 5320 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM SUPPORT BETWEEN STA 1320 TO STA 1340 AT LONGERON 22. DAMAG E EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FLOORBEAM SUPPORT AN D INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000052200028 20000522 00028 WP 2000 5 22 RRXA000229 1 19991110 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD WING ATTACH FITTING L24 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED LONGERON 24 LT ON NON-ROUTINE NR 1C-055. 2 L 7 4 4F RT 4A25 2000052200029 20000522 00029 WP 2000 5 22 RRXA000230 1 19991115 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AND SHEAR FOOT AT STA 660 FROM LONGERON 34L TO LONGERON 34R. D AMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FR AME IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 2000052200030 20000522 00030 WP 2000 5 22 RRXA000231 1 19991020 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD ACCESSORY COMPARTMENT SKIN ABOVE LONGERON 31 RT AT FUSELAGE STA 4 2.0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED REPAIR DOUBLER IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROG RAM). 2 L 7 4 4F RT 4A25 2000052200046 20000522 00046 WP 2000 5 22 20000522AP023 1 19991010 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, D PIT STATION1540 BULKHEAD FRAME UPPER ANGLE CORRODED. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FA BRICATED ANGLE IAW DC-8 SRM 51-1-5. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200047 20000522 00047 WP 2000 5 22 20000522AP025 1 19991016 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT SEAT TRACK NR 6 XCW 25 RIGHT STATION 500-510. CUT OUT WORN SECTION OF TRA CK. INSTALLED NEW TRACK AND SPLICES IAW DC-8 SRM 53-2-3, 51-1-8 AND 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000052200048 20000522 00048 WP 2000 5 22 20000522AP026 1 19990930 A 5350 FAIRING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, D PIT AFT DOOR FRAME FAIRING CRACKED. REMOVED FAIRING. FABRICATED FAIRING IAW DC-8 SRM 51-1-4. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000052200049 20000522 00049 WP 2000 5 22 20000522AP027 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 3 STATION 1580-1610 XCW 55 LEFT WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 51-1- 21. INSTALLED TRACK REPAIR IAW DC-8 SRM 51-1-21. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052200050 20000522 00050 WP 2000 5 22 20000522AP028 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 9 XCW 69 RT STATIN 1560 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 51-1-21. INS TALLED TRACK REPAIR IAW DC-8 SRM 51-1-21. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052200051 20000522 00051 WP 2000 5 22 20000522AP029 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 9 XCW 69 RT STATION 1300 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-3. INS TALLED TRACK REPAIR IAW DC-8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052200052 20000522 00052 WP 2000 5 22 20000522AP030 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURNIG D-CHECK, CABIN SEAT TRACK NR 9 XCW 69 RT STATION 82-95 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 53-2-3. IN STALLED TRACK REPAIR IAW DC-8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052200053 20000522 00053 WP 2000 5 22 20000522AP013 1 19991114 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FOUND CABIN STATION 45 XCW 53 LEFT - XCW 53 RT FLOOR MEMBRANE NUMEROUS CRACKS. FABRICATED DOUBLER IAW DC-8 SRM 53-2-0, 51-1-4. TREATED, PRIMED, AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-21, 53-2-0. (M) 2 L 7 4 4F RT 4A25 2000052200054 20000522 00054 WP 2000 5 22 20000522AP014 1 19991024 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FOUND CABIN STATION 1380 FLOOR MEMBRANE CRACKED AT FLOORBEAM. REMOVED MEMBRANE IAW DC-8 SRM 51-1- 21. FABRICATED MEMBRANE, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-4, 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200055 20000522 00055 WP 2000 5 22 20000522AP015 1 19991119 A 5320 3641126501N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN RT SIDE STATION 781.500 XCW 47.5 CRACK ON VERTICAL FITTING ABOVE CENTER FUEL TANK. REMOVED FITTING IAW DC-8 SRM 51-1-21. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052200056 20000522 00056 WP 2000 5 22 20000522AP016 1 19991207 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN STATION 798 XCW 47.5 RIGHT CRACK ON HORIZONTAL FITTING. REMOVED FITTING IAW DC-8 SRM 51-1-2 0D. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052200057 20000522 00057 WP 2000 5 22 20000522AP017 1 19991104 A 5320 36411211 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN CRACKED HORIZONTAL FITTING STATION 798 XCW 47.5 LEFT. REMOVED FITTING IAW DC-8 SRM 51-1-21. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000052200058 20000522 00058 WP 2000 5 22 20000522AP018 1 19991025 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN STATION 1140 XCW 60 LEFT FLOORBEAM AREA EXFOLIATED. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER IAW DC-8 SRM 53-2-0. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000052200059 20000522 00059 WP 2000 5 22 20000522AP020 1 19991119 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN STATION 1630-1660 WEB HAS SEVERAL BROKEN OUT HOLES. REMOVED CRACKED AREA IAW DC-8 SRM 53-2- 0. FABRICATED DOUBLER. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200060 20000522 00060 WP 2000 5 22 20000522AP021 1 19991118 A 5320 BRACE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SCREW HOLE HAS CORROSION AT FLOOR BRACE AT STATION 1680. REMOVED CORROSION IAW DC-8 SRM 51- 1-8. REMOVED FLOOR BRACE. FABRICATED FLOOR BRACE TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200061 20000522 00061 WP 2000 5 22 20000522AP022 1 19991118 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FUSELAGE SEAT TRACK BROKEN AND WORN FROM STATION 1550-1585 TRACK 2-3. REMOVED SEAT TRACK IAW DC-8 SRM 53-2-3. FABRICATED TRACK SPLICE. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-3, 51-1-8 AND 53-1-0. (M) 2 L 7 4 4F RT 4A25 2000052200062 20000522 00062 WP 2000 5 22 20000522AP006 1 19991121 A 5320 46143972N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD ACCESSORY COMPT LONGERON 31R BOTH END FITTINGS CORRODED STATION 70. REMOVED FITTINGS. RE MOVED CORROSION IAW DC-8 SRM 51-1-8, 51-1-21. TREATED, PRIMED AND INSTALLED FITTINGS IAW DC-8 SRM 51-1-8, 53-2-0, 51-1- 21D. (M) 2 L 7 4 4F RT 4A25 2000052200063 20000522 00063 WP 2000 5 22 20000522AP007 1 19991004 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER FUSELAGE CABIN, CORROSION AT L30R STATION 25. REMOVED CORROSION, REMOVED LONGERON IAW DC-8 SRM 51-1-8, 53-2-0. FABRICATED LONGERON. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200064 20000522 00064 WP 2000 5 22 20000522AP009 1 19991207 A 5320 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, BETWEEN STATION 1340-1320 AT LONGERON 22 FLOORBEAM SUPPORT CRACKED AND EXFOLIATION. REMOVED FLOOR BEAM SUPPORT IAW DC-8 SRM 51-1-20. FABRICATED FLOORBEAM SUPPORT. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51 -1-20D, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200065 20000522 00065 WP 2000 5 22 20000522AP010 1 19991207 A 5320 SUPPORT BRACKET DOUG DC8 DC873F 302199F WP BS 1340-1320 CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FOUND BETWEEN STATION 1340-1320 AT LONGERON 22 FLOORBEAM SUPPORT CRACKED AND EXFOLIATED. REMOVED FLOORBEAM SUPPORT IAW DC-8 SRM 51-1-20. FABRICATED FLOORBEAM SUPPORT. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1- 8, 51-1-20D, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200066 20000522 00066 WP 2000 5 22 20000522AP011 1 19991201 A 5320 BRACE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CRACK IN FLOOR BRACE AT STATIN 1740 AT XCW 40 LEFT CABIN. REMOVED FLOOR BRACE IAW DC-8 SRM 51-1-4 . FABRICATED L ANGLE BRACE. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-20, 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052200067 20000522 00067 WP 2000 5 22 99T64R456EWA 1 19991014 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FUSELAGE CORRODED AROUND NUT PLATE HOLES FOR WING FILLET ATTACH UPPER STATION 980 TO 1120. REMOVE D CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER IAW DC-8 53-2-1. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-8 SR M 51-1-8, 51-1-21 AND 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000052200068 20000522 00068 WP 2000 5 22 20000522AP012 1 19991012 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT LONGERON AND FUSELAGE WEB ATTACHMENT CORROSION EXIST FROM STATION 879 TO 960. BLENDED OUT C ORROSION. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/11/ 99. (M) 2 L 7 4 4F RT 4A25 2000052200072 20000522 00072 WP 2000 5 22 99T64R488EWA 1 19991122 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO COMPARTMENT STATION 1440-1460, L31R FINGER DOUBLER HAS CORROSION. REMOVED CORROSI ON, CUT FINGER DOUBLER OFF. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8 110-3 DATED 10/27/99. (M) 2 L 7 4 4F RT 4A25 2000052200073 20000522 00073 WP 2000 5 22 99T64R529EWA 1 19991220 A 3213 BOSS DOUG DC8 DC873F 302199F WP RT MLG CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 DURING D-CHECK, C/W MAIN LANDING GEAR SHOCK STRUT ASSEMBLY RETRACT PIN BOSS AND RETRACT PIN INSPECTION PER S/B 32-102 AN D MA AI-3210-01:03. COMPLIED WITH MA AI-3210-01:03, AFTER BLENDING REBORE EXCEEDED LIMITS OF MIA. REPAIRED PER EO NR 9 9-186 WITH APPROVED 8110-3 DATED 11/11/99. C/W S/B 32-102 AND GEAR SWING IAW DC-8 MM 32-30-0. (M) 2 L 7 4 4F RT 4A25 2000052200075 20000522 00075 WP 2000 5 22 RRXA000234 1 19991214 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT LONGERON 24 FROM STA 879 TO STA 960. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 2000052200076 20000522 00076 WP 2000 5 22 AT0000177 1 19990624 A 5320 5956034538N ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND INTERCOSTAL ATTACH ANGLE AT BS 996 LONGERON 27 RIGHT CORRO DED BEYOND LIMITS. REMOVED ATTACH ANGLE AT BS 996 LONGERON 27 RIGHT IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 2000052200077 20000522 00077 WP 2000 5 22 AT0000180 1 19990623 A 5320 CAP DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND END CAP AT BS 598 CORRODED. AFTER CORROSION REMOVAL FOUND OUT OF LIMITS. REMOVED AND REPLACED WITH NEW END CAP IAW DC9 SRM 51-10-04, 51-10-03, 51-30-02, AND 51-30-01. 2 L 7 2 4F A6WE 2000052200078 20000522 00078 WP 2000 5 22 AT0000181 1 19990623 A 5320 STRUCTURE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR BEAM STRUT ATTACHMENT STRINGER CORRODED AT BS 927. AFTER CORROSION REMOVAL FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR STRAP IAW DC9 SRM 53-11-03, 51-10-03, AND 51-30- 02. 2 L 7 2 4F A6WE 2000052200079 20000522 00079 WP 2000 5 22 AT0000182 1 19990623 A 5347 5295597812000 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FOUND FORWARD PIT CARGO TRACK CORRODED. REMOVED AND REPLACED WITH NEW TRACK IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 2000052200080 20000522 00080 WP 2000 5 22 AT0000183 1 19990620 A 5347 5295597812000 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FOUND CARGO PIT TRACK, FORWARD, RIGHT HAND SIDE AT BS 560 - 588 WAS CORRODED. REMOVED AND REPLACED WITH NEW TRACK IAW D C9 SRM 51-10-4. 2 L 7 2 4F A6WE 2000052200081 20000522 00081 WP 2000 5 22 AT0000184 1 19990620 A 5347 5295597812000 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FOUND CARGO TRACK FORWARD PIT AT BS 405 - 484 CORRODED. REMOVED AND REPLACED WITH NEW TRACK IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 2000052200082 20000522 00082 WP 2000 5 22 AT0000186 1 19990623 A 5347 5295597812000 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FOUND FORWARD CARGO TRACK FORWARD PIT CORRODED. MECHANICALLY REMOVED CORROSION, FOUND OUT OF LIMITS. DRILLED, COUNTER SUNK, ALODINED AND PRIMED NEW TRACK IAW DC9 SRM 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 2000052200083 20000522 00083 WP 2000 5 22 AT0000187 1 19990623 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FOUND FORWARD CARGO DOOR CUT OUT LOWER SKIN CORRODED BETWEEN LAYERS AT BS 427 - 370. REMOVED CORROSION, OUT OF LIMITS. CUT, TRIMMED, DRILLED, COUNTERSUNK, PRIMED, TREATED AND REPAIR DOUBLER AND TRIPLER IAW EO 99-1187, 53-10-3, 53-01. 2 L 7 2 4F A6WE 2000052200084 20000522 00084 WP 2000 5 22 AT0000188 1 19990928 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 802AT 47177 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FLOOR PANEL RIGHT INBOARD HAT SECTION AT BS 579 - 617 CORR ODED. FOUND OUT OF LIMITS AFTER CORROSION REMOVAL. INSTALLED NEW HAT SECTIONS IAW DC9 SRM 53-01, 51-10-04, AND 53-21. 2 L 7 2 4F A6WE 2000052200090 20000522 00090 WP 2000 5 22 99T64R550EWA 1 19991215 A 2120 DUCT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LOWER RIGHT AIR CONDITIONING DUCT AND BULKHEAD FEED THROUGH WORN AND CRACKED STATION 8 L32R. STOP DRILLED CRACK AND WELDED. WELDED WORN AREA'S PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/02/99. (M) 2 L 7 4 4F RT 4A25 2000052200091 20000522 00091 WP 2000 5 22 99T64R668EWA 1 19991207 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1480 L31L AT FRAME FINGER DOUBLER AND SKIN HAS CORROSION. REMOVED C ORROSION IAW DC-8 SRM 51-1-8. CUT OFF DAMAGED FINGERS PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/07/99. (M) 2 L 7 4 4F RT 4A25 2000052200092 20000522 00092 WP 2000 5 22 99T64R737EWA 1 19991230 A 5753 BUSHING DOUG DC8 DC873F 302199F WP TE FLAP MISALIGNED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT INBOARD FLAP OUTBOARD FITTING FORWARD BUSHING NOT. ALIGNED WITH INBOARD BUSHING. REAMED IN BOARD FITTING. FABRICATED BUSHING AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/29/99. (M) 2 L 7 4 4F RT 4A25 2000052200093 20000522 00093 WP 2000 5 22 99T64R738EWA 1 19991202 A 5720 ANGLE DOUG DC8 DC873F 302199F WP RT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, ATTACH ANGLE IN FRONT OF WING LIGHT LENS CORRODED ON WING FILLET PANEL 262A RIGHT. BLENDED OUT CO RROSION. FABRICATED DOUBLERS AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/19/99. (M) 2 L 7 4 4F RT 4A25 2000052200098 20000522 00098 NM 2000 5 22 20000522AP002 1 19991118 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND CABIN FLOORBEAM STATION 360 BL 24 TO 24 CORROSION AT ANCHOR NUT HOLES. NOTED 1 INCH CRACK AT RBL 5 UNDER FORWARD FLANGE. REMOVED CORROSION TO AFFECTED AREA IN ANCHOR NUT HOLES, WITHIN LIMITS IAW SRM 51-10-6. AT 1 IN CH CRACK REMOVED CORROSION, WITHIN LIMITS IAW SRM 53-10-1, CUT OUT DAMAGED AREA PER SRM 53-10-8. PERFORMED HFEC OF CUTO UT AREA. NO CRACKS NOTED PER SRM 51-00-00 PART 6. FABRICATED ANGLES, UPPER CHORD AND STRAPS, TREATED, PRIMED AND INSTA LLED PARTS IAW SRM 53-10-8. (M) 2 L 7 3 4F A3WE 2000052200099 20000522 00099 NM 2000 5 22 20000522AP003 1 19991118 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND CABIN FLOORBEAM STATION 344 WALL TO WALL HAS SPOTS OF CORROSION. REMOVED AND FABRICATED NEW FLOOR BEAM PER SRM 51-10-1 PAGE 14. TREATED AND PRIMED PER SRM 51-10-6 PAGE 2. INSTALLED FLOORBEAM PER SRM 53-10-1 PAGE 14. (M) 2 L 7 3 4F A3WE 2000052200100 20000522 00100 NM 2000 5 22 20000522AP004 1 19991118 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND CABIN FLOORBEAM STATION 314 BL 0 HAS CORROSION. REMOVED CORROSION PER SRM 51-10-6, FOUND OUT OF L IMITS PER SRM 53-10-8, CUT OUT DAMGED FLOORBEAM IAW SRM 53-10-8, PERFORMED HFEC INSPECTION. NO CRACKS NOTED PER SRM 51- 10-00. FABRICATED NEW UPPER CHORD, ANGLES SUPPORT IAW SRM 53-10-8. TREATED AND PRIMED PER SRM 51-10-6 PAGE 2. INSTALL ED FLOORBEAM PER SRM 53-10-1 PAGE 14. (M) 2 L 7 3 4F A3WE 2000052200107 20000522 00107 WP 2000 5 22 99T64R674EWA 1 19991210 A 5320 DRAIN LINE DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, EXTERIOR STATION 1382, L36 OVERBOARD DRAIN BROKEN. FABRICATED EXTERNAL DOUBLER AND INSTALLED DRAI N FITTING PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/09/99. (M) 2 L 7 4 4F RT 4A25 2000052200108 20000522 00108 WP 2000 5 22 20000522AP008 1 19991115 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CORROSION ON FRAME AND SHEAR FOOT STATION 660L 34L - 34R MID ACCY COMPT. REMOVED CORROSION IAW DC -8 SRM 51-1-8. FABRICATED FRAME IAW DC-8 SRM 53-1-5. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200109 20000522 00109 WP 2000 5 22 20000522AP019 1 19991101 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN CORROSION ON FLOORBEAM AT STATION 1320 BETWEEN 5-6 TRACK. REMOVED CORROSION IAW DC-8 SRM 51 -1-8. FABRICATED DOUBLER AND FILLER IAW DC-8 SRM 51-1-21, 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 5 1-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200110 20000522 00110 WP 2000 5 22 20000522AP024 1 19991024 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO COMPARTMENT STATION 1160-1180 L26R END OF LONGERON HAS CORROSION. REMOVED CORROSI ON IAW DC-8 SRM 51-1-8. FABRICATED FITTING IAW DC-8 SRM 51-1-4, 51-1-21. TREATED AND PRIMED, AND INSTALLED IAW DC-8 SR M 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000052200111 20000522 00111 WP 2000 5 22 20000522AP031 1 19991115 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN SEAT TRACK NR 9 XCW 69 RT STATION 1690 WORN. REMOVED DAMAGED AREA IAW DC-8 SRM 51-1-21, 51- 3-0. INSTALLED TRACK REPAIR IAW DC-8 SRM 53-2-3. TREATED, PRIMED IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000052300007 20000523 00007 WP 2000 5 23 AT0000179 1 19990812 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 839AT 47089 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FORWARD CABIN FLOORBEAM AT BS 160 - 237 BL 0 TO HAVE CORRO SION. REMOVED AND INSTALLED NEW FLOOR SUPPORT AT BS 160 - 237 BL 0 IAW DC9 SRM 51-10-02, 51-30-02, 51-10-04, 51-10-03. 2 L 7 2 4F A6WE 2000052300008 20000523 00008 WP 2000 5 23 AT0000185 1 19990623 A 5347 5295597812000 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 832AT 47451 FOUND CARGO TRACK FORWARD PIT AT BS 484 - 590 CORRODED. MECHANICALLY REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED A ND REPLACED WITH NEW TRACK IAW DC9 SRM 53-01 FIGURE 1, 51-10-04, 51-10-3. 2 L 7 2 4F A6WE 2000052300090 20000523 00090 NM 2000 5 23 UPS00232374 1 19991228 A 5311 FRAME BOEING 727 72725C 138400H NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:SI ACCESSED HOLES COMMON TO REMOVED CROWN SKIN, DISCOVERED CRACK IN BS 480 FRAME LBL 60 STR 10L AFT ROW. REPAIRED BS 480 FRAME PER ER 99-6617, UNDER UPS FILE NUMBER 727-53-2248. 2 L 7 3 4F A3WE 2000060500028 20000605 00028 NE 2000 6 5 CA990423013 2 19990415 A 7220 215T50191010 DUCT PWA CNDAIR CL215 CL2156B11415 EA PWA PW120 PW123 NE INLET DUCT CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 109086 (CAN) INSPECTION FOUND THE COOLING INLET DUCT (PN 215T50191010) WILL MAKE CONTACT AND CHAFE THE OIL PRESSURE FUEL HEATE R LINE IF A BAD WELD LED TO SEPARATION. THE DUCT WAS REPLACED. (X) 2 H 7 2 4T 4 T RT A14EA E20NE 2000060500032 20000605 00032 EA 2000 6 5 CA990423015 1 19990415 A 7603 87620105001 GUARD PWA CNDAIR CL215 CL2156B11215 EA PWA PW120 PW123 NE ENGINE CABLE CRACKED W O OTHER O OTHER NR NOT REPORTED 1 CA 1979 109004 (CAN) INSPECTION FOUND THE ENGINE CONTROL CABLE FAIRLEADS WERE CRACKED AROUND THE WELDS. (X) 2 H 7 2 4T 4 T RT A14EA E20NE 2000060500033 20000605 00033 SW 2000 6 5 CA991208069 1 19991014 A 6220 D2B11002 BEARING KAMOV KA32 KA32A1 SW ROTOR MAST WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 3200044 (CAN) UPON CHECKING OIL IN FLAPPING HINGE, STEEL FLAKES WERE DISCOVEREDL. ROTOR MAST WAS THEN REPLACED. (X) 1 G 7 2 4U NC 2000060500034 20000605 00034 NM 2000 6 5 CA991103047 1 19991023 A 3320 BV033001248 SOCKET DHAV DHC8 DHC8106 NM ROW 2 FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA (CAN) F/A NOTICED SMOKE SMELL IN CABIN AREA. MAINTENANCE FOUND 2 BURNT OVERHEAD LAMP HOLDERS. PARTS REPLACED. AIRCRA FT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 2000060800010 20000608 00010 NM 2000 6 8 ASAA9940167 1 19991217 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 12 - 13 DISCONNECTED A K NONE L NO TEST IN INSP/MAINT 1 NM 01 713AS 30161 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 12-13 WERE FOUND TO BE INOPERATIVE. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 2000060800012 20000608 00012 WP 2000 6 8 99T64R341AR 1 19990615 A 5320 STCSA106350 ANGLE DOUG DC8 DC862 3021970 WP FUSELAGE MISINSTALLED B T64R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 03 1808E 46105 MAIN CARGO DOOR UPPER JAM INSTALLATION Z ANGLE INCORRECTLY INSTALLED STATION 450. DOES NOT EFFECT THE INTEGRITY OF THE DOOR. NO CORRECTIVE MEASUREMENTS NECESSARY IAW DWG AS11048. (M) 2 L 7 4 4F 4A25 2000060800042 20000608 00042 NM 2000 6 8 20000511AP007 1 19991208 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND CABIN SEAT TRACK STATION 1070 LBL 50 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-30-2 PAGE 2. RE MOVED HAT CHANNEL STATION 1070 LBL 50 IAW 51-30-2 PAGE 2. FABRICATED HAT CHANNEL IAW 51-10-1 PAGE 2. TREATED INSTALLED HAT CHANNEL IAW 51-10-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000060800043 20000608 00043 NM 2000 6 8 20000511AP010 1 19991208 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 889MA 21854 FOUND CABIN TRACK STATION 360 TO 420 RBL 24 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 2 FOUND OUT OF LIMITS. F ABRICATES SEAT TRACK IAW 51-10-1. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED TRACK IAW 51-30-2. (M) 2 L 7 3 4F A3WE 2000060900526 20000609 00526 EU 2000 6 9 USAASA99012 1 19991215 A 3350 D31516113 LIGHT AIRBUS A319 A319112 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 720US 1089 LGA - FOUND AIRCRAFT EMERGENCY LIGHTS SYSTEM FAILS LEFT FWD EXIT POS. MAINTENANCE REPLACED THE FORWARD LEFT SLIDE ASSEM BLY. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A28NM 2000060900528 20000609 00528 WP 2000 6 9 20000609AP003 1 19991209 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD LOWER CARGO BILGE STATION 620 L36 UNDER FRAME HAS CORROSION (SKIN) FRAME DOUBLER. REMOVED EXISTING DOUBLER IAW DC-8 SRM 51-120. CUTOUT DAMAGED AREA, REMOVED ALL CORROSION. FABRICATED DOUBLER AND FILLER IAW D C-8 SRM 51-1-8 AND 51-1-20D AND EO NR 99-186 WITH APPROVED 8110-3 DATED 12/08/99. (M) 2 L 7 4 4F RT 4A25 2000060900529 20000609 00529 WP 2000 6 9 20000609AP004 1 19991209 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, B CARGO PIT STATION 560 L34R FRAME CRACKED. ROUTED OUT DAMAGED AREA ON FRAME. FABRICATED ANGLE. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51-1-20D AND EO NR 99-186 WITH APROVED 8110-3 DATED 12/09/99. ( M) 2 L 7 4 4F RT 4A25 2000060900530 20000609 00530 WP 2000 6 9 20000609AP005 1 19991027 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1240 L35R TOP OF LONGERON METAL STRIP CRACKED. REMOVED BRACKET IAW DC-8 SRM 51-3-20. FABRICATED METAL STRIP IAW DC-8 SRM 53-2-0. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3- 0. (M) 2 L 7 4 4F RT 4A25 2000060900531 20000609 00531 WP 2000 6 9 20000609AP006 1 19991112 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD LOWER CARGO BILGE STATION 450 L26R LIGHT CORROSION. REMOVED CORROSION, FABRICATED SPLICE IAW DC-8 SRM 51-1-8, 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000060900532 20000609 00532 WP 2000 6 9 20000609AP007 1 19991218 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T54R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD LOWER CARGO BILGE STATION 520 L31R INSIDE DOOR JAM ANGLE CRACKED AND BENT UP. REMOVED ANG LE, FABRICATED DOUBLER IAW DC-8 SRM 51-1-21, 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000060900533 20000609 00533 WP 2000 6 9 20000609AP008 1 19991007 A 5320 DOOR FRAME DOUG DC8 DC873F 302199F WP BULKHEAD CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, STATION 1540 BULKHEAD DOOR FRAME HAS CORROSION BLISTER 30 INCHES ABOVE L33R. REMOVED CORROSION IA W DC-8 SRM 51-1-8. FABRICATED DOUBLER IAW DC-8 SRM 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000060900534 20000609 00534 WP 2000 6 9 99T64R739EWA 1 19991202 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, LEFT FILLET SKIN CORROSION AT L35L BETWEEN STATION 781-742. REMOVED CORROSION IAW DC-8 SRM 51-1-8 . FABRICATED SPLICE PLATE AND REPLACEMENT SKIN AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/01/99. (M) 2 L 7 4 4F RT 4A25 2000060900535 20000609 00535 WP 2000 6 9 99T64R740EWA 1 19991202 A 5314 KEELBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, KEEL BEAM STATION 720 TO 781 HAS EXFOLIATED CORROSION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FA BRICATED FILLER AND DOUBLER AND INSTALLED PER BOEING M-7200-99-10647 AND M7200-99-10680 WITH APPROVED 8110-3 DATED 12/10 /99. (M) 2 L 7 4 4F RT 4A25 2000060900536 20000609 00536 WP 2000 6 9 99T64R676EWA 1 19991108 A 5711 SPAR DOUG DC8 DC873F 302199F WP RT WING MISDRILLED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT WING OUTBOARD LEADING EDGE UPPER SPAR CAP HAS SEVERAL MISDRILLED HOLES AT NUT CHANNEL. DRIL LED THE DISCREPANT HOLES ROUND TO ELIMINATE THE DOUBLE DRILLED CONDITION. TREATED AND PRIMED. LEFT OVERSIZED HOLES OPE N. INSTALLED REMAINDER OF GANG CHANNEL PER FACTORY SPECS, PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/08/99. (M) 2 L 7 4 4F RT 4A25 2000060900537 20000609 00537 WP 2000 6 9 99T64R703EWA 1 19991213 A 2550 110660600003 PANEL DOUG DC8 DC873F 302199F WP CARGO WALL DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, REPLACED GIL-LINER FROM STATION 8 TO REAR PRESSURE BULKHEAD. INSTALLED NEW GIL-LINER AND SPLICE S TRIPS PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/30/99. (M) 2 L 7 4 4F RT 4A25 2000060900538 20000609 00538 WP 2000 6 9 99T64R686EWA 1 19991122 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE WORN B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, EXTERIOR DRAIN FITTING WORN STATION 1270 L36. FABRICATED EXTERNAL DOUBLER AND INSTALLED DOUBLER A ND DRAIN FITTING PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/19/99. (M) 2 L 7 4 4F RT 4A25 2000060900539 20000609 00539 WP 2000 6 9 99T64R685EWA 1 19991207 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, C-PIT DOOR FUSELAGE CUT OUT AFT LOWE CORNER LOOSE RIVETS AND CRACKED LIP ON FRAME. CUT OFF DAMAGE D SEAL DEPRESSOR. FABRICATED TWO REPAIR STRAPS AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/23/99. (M) 2 L 7 4 4F RT 4A25 2000060900540 20000609 00540 WP 2000 6 9 99T64R682EWA 1 19991119 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, DENT IN FUSELAGE AT STATION 25 L32-33L. BLENDED OUT DENT. FINISHED THE TITANIUM PER FACTORY SPEC S IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/16/99. (M) 2 L 7 4 4F RT 4A25 2000060900541 20000609 00541 WP 2000 6 9 99T64R681EWA 1 19991118 A 2120 DUCT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN AIR DISTRIBUTION DUCT HAS TWO CRACKS ON TOP AT APPROX STATION 1345/1348. STOP DRILLED CRACK S. NDT CONFIRMED CRACKS HAD BEEN STOPPED. WELDED CRACKS. NDT WELDS NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110- 3 DATED 11/14/99. (M) 2 L 7 4 4F RT 4A25 2000060900542 20000609 00542 WP 2000 6 9 99T64R680EWA 1 19991109 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT STATION 857 TO 980 LIGHT SURFACE CORROSION ON PRESSURE PANEL XCWO-XCW 69 L EFT. BLENDED OUT CORROSION. FABRICATED FINGER DOUBLER REPAIR. TREATED AND PRIMED. INSTALLED REPAIR PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000060900543 20000609 00543 WP 2000 6 9 99T64R679EWA 1 19991112 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, TWO NUT PLATES BROKEN OFF AND CORROSION AROUND HOLES ON UNDER SIDE OF FLOORBEAM STATION 760 BETWEE N SEAT TRACKS NR 6 AND NR 7. REMOVED CORROSION BY MECHANICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN T O SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/11/1999. (M) 2 L 7 4 4F RT 4A25 2000060900544 20000609 00544 WP 2000 6 9 99T64R677EWA 1 19991203 A 2120 RETAINER DOUG DC8 DC873F 302199F WP A/C DUCT CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RETAINER RING CRACKED GROUND AIR CONDITIONER CONNECTOR DUCT TO FUSELAGE ATTACHMENT FORWARD ACCESSO RY COMPARTMENT. STOPPED DRILLED CRACKS. NDT CONFIRMED CRACKS HAD BEEN STOPPED. WELDED CRACKS PER MIL-STD-2219 AND NDT WELD. NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/14/99. (M) 2 L 7 4 4F RT 4A25 2000060900545 20000609 00545 WP 2000 6 9 20000609AP009 1 19991209 A 5330 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, PANEL 262K AFT RIGHT IS DELAMINATED AND HAS CORROSION. FABRICATED NEW SKIN AND ANGLES. TREATED, PRIMED AND ASSEMBLIED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 12/08/99. (M) 2 L 7 4 4F RT 4A25 2000060900546 20000609 00546 WP 2000 6 9 99T64R446EWA 1 19991214 A 5313 5750198502 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RIGHT LONGERON 24 AND FUSELAGE STATION 879 TO STATION 940, CORROSION ON UPPER SURFACE ON FITTING A ND 2 PREVIOUS REPAIR DOUBLERS ALSO RUNNING UNDER REPAIR DOUBLERS. REPLACED RIGHT L24 FITTING IAW DOUGLAS L24 REPLACEMEN T GUIDE SRM 51-1-20D, 51-3-0, 53-2-2 AND EO NR 99-186 WITH APPROVED 8110-3 DATED 11/16/99. (M) 2 L 7 4 4F RT 4A25 2000060900547 20000609 00547 WP 2000 6 9 99T64R449EWA 1 19991217 A 5753 VANE DOUG DC8 DC873F 302199F WP TE FLAP DAMAGED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LEFT INBOARD FLAP NR 2 VANE INBOARD END SLIDING HINGE COVER TRACK MOUNT HOLES ELONGATED. FABRICAT ED REPAIR DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000060900548 20000609 00548 NM 2000 6 9 20000609AP010 1 19991130 A 5400 ANGLE BOEING 727 727225 1384077 NM NR 1 ENG PYLON CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND NR 1 ENGINE PYLON T/E RIB ATTACH ANGLE CRACKED AND RIB HOLES ELONGATED. REMOVED CRACKED ANGLE, FA BRICATED NEW REPAIR PARTS PER SRM 51-40-2. INSTALLED NEW REPAIR PARTS AND SEALED AREA PER SRM 51-10-1 AND SRM 51-40-2. (M) 2 L 7 3 4F A3WE 2000060900549 20000609 00549 WP 2000 6 9 99T64R374AR 1 19990318 A 5320 ANGLE DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 19 1808E 65019 46105 FOUND CORROSION ON CUSP LINE RIGHT LINE L21R FROM STATION 208-270. REMOVED CORROSION, CUT OUT DAMAGED AREA FABRICATED F ILLER AND PLUG AND INSTALLED PER EO 99-061, WITH APPROVED FAA FORM 8110-3 DATED 6/14/99. (M) 2 L 7 4 4F 4A25 2000060900550 20000609 00550 WP 2000 6 9 99T64R375AR 1 19990309 A 5730 PLATE DOUG DC8 DC862 3021970 WP STUB WING CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 LT OUTBOARD STUB WING CORROSION. REMOVED CORROSION, FABRICATED FILLERS, DOUBLERS AND INSTALLED PER EO 99-034 WITH APPRO VED FAA FORM 8110-3 DATED 3-3-99. (M) 2 L 7 4 4F 4A25 2000060900551 20000609 00551 WP 2000 6 9 99T64R342AR 1 19990528 A 5230 STCSA106350 HINGE DOUG DC8 DC862 3021970 WP CARGO DOOR CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 MAIN CARGO DOOR AFT HINGE ASSY AFT LUG CRACKED ALSO JAM NUT ON FORWARD SIDE NOT SECURED. REMOVED AND REPLACED HINGE PER DRAWING AE2411, AS 11034 AND DC-8 SRM 51-3-0 WITH APPROVED FORM 8110-3 DATED MAY 12, 1999. (M) 2 L 7 4 4F 4A25 2000060900552 20000609 00552 WP 2000 6 9 99T64R376AR 1 19990305 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 1808E 65019 46105 FOUND CORROSION ON SKIN BETWEEN STATION 1480-1500 LT AT L32L. REMOVED CORROSION, FABRICATED FILLERS, DOUBLERS AND INSTA LLED PER EO 99-043, WITH APPROVED FAA FORM 8110-3 DATED 3-1-99. (M) 2 L 7 4 4F 4A25 2000060900553 20000609 00553 WP 2000 6 9 99T64R493EWA 1 19991020 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FORWARD ACCY COMPT CORROSION UNDER DOME NUT AIR CONDITION FRAME JUST ABOVE LONGERON 31 RT STATION 42. BLENDED CORROSION USING MECHANICAL METHOD NOT TO EXCEED .128 REMAINING THICKNESS. TREAT AND PRIME PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/26/99. (M) 2 L 7 4 4F RT 4A25 2000060900554 20000609 00554 WP 2000 6 9 20000609AP011 1 19991201 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, FLOORBEAM AT STATION 1580 BETWEEN NR 1 - NR 2 SEAT TRACKS HAS BLOWOUT OF CORROSION AT NUT PLATE. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 5 1-1-20D. (M) 2 L 7 4 4F RT 4A25 2000060900555 20000609 00555 WP 2000 6 9 20000609AP012 1 19991207 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, STATION 55 AT XW 32 INCH FLOOR WEB SUPPORT FITTING CRACKED IN CABIN. REMOVED FLOOR WEB SUPPORT FI TTING IAW DC-8 SRM 51-1-20D. REPLACED FLOOR WEB SUPPORT FITTING IAW DC-8 SRM 51-30-0. TREATED, PRIMED, AND INSTALLED I AW DC-8 SRM 51-1-21, 51-1-8. (M) 2 L 7 4 4F RT 4A25 2000060900556 20000609 00556 WP 2000 6 9 20000609AP013 1 19991128 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN STATION 1680 FLOORBEAM BETWEEN SEAT TRACK 6-7 HAS EXFOLIATED CORROSION. REMOVED CORROSION I AW DC-8 SRM 51-1-8. FABRICATED FLOORBEAM EXTRUSION. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21, 51-1- 4. (M) 2 L 7 4 4F RT 4A25 2000060900557 20000609 00557 WP 2000 6 9 20000609AP014 1 19991119 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, CABIN WEB UNDER SEAT TRACK NR 1 BETWEEN STATION 140-160 CRACKED AROUND 1 INCH IN DIAMETER. REMOVE D CRACKED AREA IAW DC-8 SRM 53-2-0. FABRICATED DOUBLER IAW DC-8 SRM 51-1-4. TREATED, PRIMED, AND INSTALLED IAW DC-8 SR M 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000060900558 20000609 00558 WP 2000 6 9 20000609AP015 1 19991203 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT FLOOR WEB CRACKED STATION 1580 AND 1600 APPROX 10 INCH FROM LEFT CUSP LINE . REMOVED WEB. FABRICATED NEW WEB OUT OF 2024T3. TREATED AND PRIMED AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-2 1, 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000060900559 20000609 00559 WP 2000 6 9 20000609AP016 1 19991208 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, UPPER CARGO COMPARTMENT FRAME 1060 AT L36 L ANGLE CORRODED FORWARD SIDE. REMOVED CORROSION IAW DC -8 SRM 51-1-81. REMOVED ANGLE IAW DC-8 SRM 51-1-20, FABRICATED ANGLE. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1- 4, 51-1-8, 51-1-20. (M) 2 L 7 4 4F RT 4A25 2000061300353 20000613 00353 2000 6 13 20000505SH020 4 19990607 A 2562 AK450 ELT BEECH 23 B19 1151215 CE CABIN MALFUNCTIONED H K NONE L NO TEST IN INSP/MAINT 1 NM 02 2048A MB904 DURING TEST (ANNUAL), THIS UNIT COULD NOT BE RE-ARMED WITHOUT ACTIVATION. (X) 1 L 7 1 3O A1CE 2000061300368 20000613 00368 NE 2000 6 13 20000508SH034 2 19990715 A 7250 BLADE BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER WORN A R7MA O OTHER O OTHER NR NOT REPORTED 1 NM 07 911BY 625 7127 LE45022EA EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X) 1 G 7 2 3U 3 U H13EU E5NE 2000061300377 20000613 00377 WP 2000 6 13 99T64R702EWA 1 19991209 A 2830 DUMP VALVE DOUG DC8 DC873F 302199F WP LT WING CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LEFT FUEL DUMP CHUTE HAS CORROSION IN O-RING CUTOUT. REMOVED CORROSION BY MECHANICAL METHOD. FIL LED UNDER CUT AREAS WITH WELD, NDT WELD TO ASSURE NO FLAWS, NONE FOUND. BLEND SMOOTH PER EO NR 99-186 WITH APPROVED 811 0-3 DATED 12/08/99. (M) 2 L 7 4 4F RT 4A25 2000061300378 20000613 00378 WP 2000 6 13 20000613AP001 1 19991203 A 5320 3755843501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO COMPARTMENT STATION 1220 LONGERON L34R-L35R BATH TUB FITTING CRACKED. REMOVED FIT TING IAW DC-8 SRM 51-1-20D. FABRICATED ANGLES AND FITTING IAW DC-8 SRM 53-2-0 SHEET 2 F17, 18. TREATED, PRIMED AND INST ALLED ANGLES AND FITTING IAW DC-8 SRM 51-1-8, 51-1-24, 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000061300379 20000613 00379 WP 2000 6 13 20000613AP002 1 19991123 A 5320 37558411 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO COMPT STATION 1220 L33R-L34R END FITTING CORRODED. REMOVED FITTING IAW DC-8 SRM 5 1-1-20D, CUT NEW FITTING IAW DC-8 SRM 53-3-0, 53-20 F2C SHEET 1. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 , 51-1-20D. (M) 2 L 7 4 4F RT 4A25 2000061300380 20000613 00380 WP 2000 6 13 20000613AP003 1 19991127 A 5320 37558401 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO COMPARTMENT STATION 1220 L32R END FITTING CORRODED. REMOVED FITTING IAW DC-8 SRM 51-1-20D. CUT NEW FITTING IAW DC8 SRM 53-2-0 F2 SHEET 2. TREATED, PRIMED AND INSTALLED FITTING IAW DC-8 SRM 51-1-8, 53 -2-0. (M) 2 L 7 4 4F RT 4A25 2000061300381 20000613 00381 WP 2000 6 13 20000613AP004 1 19991119 A 5320 3754946502N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, C PIT DOOR UPPER AFT CUTOUT CORNER STATION 1220 L23R CRACKED FITTING. REMOVED FITTING IAW DC-8 SR M 51-1-20D. LOCATED AND DRILLED REPLACEMENT FITTING IAW DC-8 SRM 51-1-20D. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-120D, 51-1-21, 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000061300382 20000613 00382 WP 2000 6 13 20000613AP005 1 19991126 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, C PIT STATION 1060 L36 CORROSION ON CIRCUMFERENTIAL FRAME. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED NEW FRAME AND DOUBLERS FOR SPLICE IAW DC-8 SRM 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 5 1-1-20D AND EO NR 99-186 WITH APPROVED 8110-3 DATED 12/09/99. (M) 2 L 7 4 4F RT 4A25 2000061300383 20000613 00383 WP 2000 6 13 20000613AP006 1 19991123 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 46106 FOUND DURING D-CHECK, UPPER CARGO COMPT STATION 1380-1400 INTERCOSTAL EXFOLIATED XCW 48 RT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SECTION OF INTERCOSTAL IAW DC-8 SRM 53-2-0. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M) 2 L 7 4 4F RT 4A25 2000061300384 20000613 00384 NM 2000 6 13 20000613AP007 1 19991118 A 5720 BEAM BOEING 727 727225 1384077 NM RT WING DAMAGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH PREVIOUS REPAIR ABOVE RIGHT WING NR 8 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M) 2 L 7 3 4F A3WE 2000061300385 20000613 00385 NM 2000 6 13 20000613AP008 1 19991111 A 5720 BEAM BOEING 727 727225 1384077 NM LT WING DAMAGED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH IMPROPER PREVIOUS REPAIR ABOVE LEFT WING NR 7 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M) 2 L 7 3 4F A3WE 2000061300386 20000613 00386 NM 2000 6 13 20000613AP009 1 19991109 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM CABIN CORRODED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND CABIN SEAT TRACK STATION 680 TO 740 LBL 24 HAS CORROSION OUT OF LIMITS PER SRM 53-10-1, PAGE 16. REMOVED AND FABRICATED SEAT TRACK, INSTALLED PER SRM 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000061300387 20000613 00387 NM 2000 6 13 20000613AP010 1 19991113 A 5400 RIB BOEING 727 727225 1384077 NM NR 3 PYLON CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND NR 3 ENGINE PYLON T/E INNER COMPARTMENT, AFT OF AFT ENGINE MOUNT SUPPORT RIB CRACKED. FABRICATED NEW MOUNT SUPPORT RIB PER SRM 51-10-2 PAGE 1 AND INSTALLED PER SRM 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000061300388 20000613 00388 WP 2000 6 13 99T64R491EWA 1 19991215 A 2752 37741531 BELLCRANK DOUG DC8 DC873F 302199F WP FLAP ACTUATOR CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, MID WING FLAP CRANK HAS CRACK APPROX .1875 INCH IN LENGTH AT STATION 219 LEFT. REPLACED MIDWING F LAP CRANK IAW DC-8 O/H/M 27-28-8. (M) 2 L 7 4 4F RT 4A25 2000061400209 20000614 00209 WP 2000 6 14 99T64R477EWA 1 19991210 A 5711 5615057510N SPAR DOUG DC8 DC873F 302199F WP RT WING CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, RT AUX SPAR UPPER SPAR CAP CRACKED .625 INCH AT OUTBOARD AFT ATTACH BOLT. REMOVED AND REPLACED RI GHT AUX SPAR UPPER SPAR CAP IAW DC-8 SRM 51-1-24, 51-1-20D AND 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000061400210 20000614 00210 WP 2000 6 14 99T64R476EWA 1 19991214 A 2752 37741721 BELLCRANK DOUG DC8 DC873F 302199F WP FLAP ACTUATOR CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, INBOARD FLAP ACTUATOR ASSY CRANK HAS TWO CRACKS, ONE IS .5 INCH IN LENGTH AND THE OTHER IS .375 IN CH LENGTH. REPLACED CRANK IAW DC-8 O/H/M 27-28-9. (M) 2 L 7 4 4F RT 4A25 2000061400211 20000614 00211 WP 2000 6 14 99T64R496EWA 1 19991203 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, A PIT AT STATION 340 AT L27R CRACK IN AFT DOOR FRAME. FABRICATED FITTING. TREATED, PRIMED AND IN STALLED IAW DC-8 SRM 51-1-8, 51-1-20D AND 51-3-0. (M) 2 L 7 4 4F RT 4A25 2000061400212 20000614 00212 WP 2000 6 14 99T64R521EWA 1 19991209 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, STATION 1145 TO STATION 1135 CORROSION IN WEB AND CRACK APPROX 6 INCHES LONG UNDER SHEAR FOOT AT C USP L21L. BLENDED OUT CORROSION, CUT OUT DAMGED AREA. FABRICATED NEW CUSP T, SPLICE AND INSTALLED PER EO NR 99-186 WIT H APPROVED 8110-3 DATED 11/19/99. (M) 2 L 7 4 4F RT 4A25 2000061400213 20000614 00213 WP 2000 6 14 99T64R516EWA 1 19991214 A 5313 5750198501 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, LEFT W/W LONGERON 24 STATION 857 HAS CRACK 1.5 INCHES LONG. REMOVED AND REPLACED LEFT L24 IAW DC- 8 REPLACEMENT GUIDE AND SRM 51-1-21, 51-1-20D AND 53-2-2. (M) 2 L 7 4 4F RT 4A25 2000061400214 20000614 00214 WP 2000 6 14 99T64R497EWA 1 19991205 A 5320 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, A PIT AT STATION 280 BETWEEN L26 AND 27 RT SIDE CRACK IN FORWARD DOOR FRAME. REPLACED FITTING IAW DC-8 SRM 53-2-0, 51-1-20D AND EO NR 99-186 WITH APPROVED 8110-3 DATED 12/03/99. (M) 2 L 7 4 4F RT 4A25 2000061400215 20000614 00215 WP 2000 6 14 99T64R523EWA 1 19991208 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1160-1220 L34R RIGHT SIDE CORROSION ON LONGERON ON LONGERON NEXT TO SKIN. REMOVED CORROSION. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000061400216 20000614 00216 WP 2000 6 14 99T64R525EWA 1 19991208 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1180-1200 L34R TOP WEB HAS CORROSION. REMOVED CORROSION. FABRICATE D REPAIR DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000061400217 20000614 00217 WP 2000 6 14 99T64R522EWA 1 19991208 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 FOUND DURING D-CHECK, AFT LOWER CARGO BILGE STATION 1200 L35R TOP OF WEB HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/03/99. (M) 2 L 7 4 4F RT 4A25 2000061400218 20000614 00218 WP 2000 6 14 99T64R528EWA 1 19991220 A 3230 BOSS DOUG DC8 DC873F 302199F WP LT MLG CORRODED B T64R K NONE O OTHER IN INSP/MAINT 1 SO 03 605AL 88287 46106 DURING D-CHECK, C/W MAIN LANDING GEAR SHOCK STRUT ASSEMBLY RETRACT PIN BOSS AND RETRACT IN INSPECTION PER S/B 32-102 AND MA AI-3210-01:03. C/W MA-A1-3210-01:03, AFTER BLENDING REBORE EXCEEDED LIMITS OF MA. REPAIRED PER EO NR 99-186 WITH A PPROVED 8110-3 DATED 11/11/99. C/W S/B 32-102 AND GEAR SWING IAW DC-8 MM 32-30-0. (M) 2 L 7 4 4F RT 4A25 2000061400227 20000614 00227 WP 2000 6 14 EIA990296 1 19991027 A 5320 9915560501 FRAME DOUG DC9 DC933F 302207A WP CABIN WINDOW MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 941F 47193 MZJ - CABIN WINDOW L1 REPAIR NOT PER SRM 53-04. REMOVED EXTERNAL TEMPORARY REPAIR DOUBLER. SPOT FACED THE HOLES. TRIM MED THE FORWARD ADJACENT SKIN PANEL. FABRICATED FILLERS. REINSTALLED REMOVED DOUBLER PER ECRA 941-53-070-2. (M) 2 L 7 2 4F A6WE 2000061400228 20000614 00228 WP 2000 6 14 EIA990297 1 19991101 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 941F 47193 MZJ - FUSELAGE SKIN REPAIR ON RIGHT SIDE OF FUSELAGE AT FS 168.750 OVERLAPPING SKIN PANEL BUTT JOINT ON LONGERON 26 NEED S TO BE CHANGED FROM A CLASS TWO REPAIR TO A CLASS ONE REPAIR. CURRENTLY NO FINGER DOUBLER INSTALLED. REPAIRED DOUBLER S PER ECRA 941-53-081-2. FABRICATED EXTERIOR DOUBLER, FINGER DOUBLERS, FILLERS AND INSTALLED PER ECRA. PART NR 941-53- 081-1, -2, -3, -4, -5.(M) 2 L 7 2 4F A6WE 2000061400229 20000614 00229 WP 2000 6 14 EIA990298 1 19991101 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - FOUND RIGHT SKIN AT STATION 229-588 HAS A LOT OF DAMAGE. REMOVED AND REPLACED SKINS FROM FS 229-588 BETWEEN L18 A ND L26 AND FWD CARGO DOOR DOUBLER FROM FS 362-434 RIGHT PER ECRA 941-53-003-2 REV A, AND FLIGHT VEHICLES INC DRAWING 53- 99165-1 SHEET 1-3. (M) 2 L 7 2 4F A6WE 2000061400230 20000614 00230 WP 2000 6 14 EIA990299 1 19991102 A 5311 99234362 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - FRAME 718 RIGHT CRACKED ON FORWARD SIDE OF INTERMEDIATE POCKET, LOWER AFT RADIUS, FROM FASTENER HOLE TO FASTENER H OLE UNDER CABIN FLOOR. REMOVED CORROSION, FABRICATED DOUBLER/FILLERS, AND INSTALLED PER ECRA 941-53-067-2. (M) 2 L 7 2 4F A6WE 2000061400231 20000614 00231 WP 2000 6 14 EIA990300 1 19991103 A 5320 WEB DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - INSIDE FORWARD LOWER CARGO BAY, JUST AFT OF DOOR THRESHOLD, STATION 427 BETWEEN 24 AND 24R LONGERONS, WEB AT LIGHT ENING HOLE IS CRACKED AND HAS PIECE MISSING. INSTALLED NEW SECTION OF WEB WITH TWO RING DOUBLERS PER ECRA 941-53-080-2. (M) 2 L 7 2 4F A6WE 2000061400232 20000614 00232 WP 2000 6 14 EIA990301 1 19991106 A 5711 SPAR DOUG DC9 DC933F 302207A WP RT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - RIGHT WING TRAILING EDGE REAR SPAR AT APPROX STATION XW251.680 HAS CORROSION BY UPPER INBOARD BOLT HOLE. REPLACED SECTION OF RT WING REAR SPAR UPPER CAP BETWEEN XRS 180.1 AND XRS 319.5 PER ECRA 941-57-015-2. (M) 2 L 7 2 4F A6WE 2000061400233 20000614 00233 WP 2000 6 14 EIA990302 1 19991116 A 5230 SKIN DOUG DC9 DC933F 302207A WP CARGO DOOR DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - SKIN REPAIR ON LOWER AFT CORNER OF MAIN CABIN CARGO DOOR NEEDS TO BE CHANGED FROM A CLASS TWO TO A CLASS ONE REPAI R. REMOVED DOUBLER PER SRM 51-30-1. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER ECRA 941-52-046-2. (M) 2 L 7 2 4F A6WE 2000061400234 20000614 00234 WP 2000 6 14 EIA990303 1 19991118 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - FUSELAGE SKIN REPAIR BELOW MAIN CABIN CARGO DOOR THRESHOLD BETWEEN FS 351 AND FS 408 NEEDS TO BE CHANGED FROM A CL ASS TWO REPAIR TO A CLASS ONE REPAIR. CURRENTLY NO FINGER DOUBLER INSTALLED. FABRICATED AND INSTALLED DOUBLERS/FILLERS PER SRM 51-10-3, 51-30-5 AND ECRA 941-53-010-2. (M) 2 L 7 2 4F A6WE 2000061400235 20000614 00235 WP 2000 6 14 EIA990304 1 19991118 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 941F 47193 MZJ - FS 936 BETWEEN LONGERON 14 AND 15R, REPAIR NOT PER SRM. REPLACED NON-DOCUMENTED DOUBLERS AND CLEANED UP TRIMOUT A REA PE ECRA 941-53-082-2 REV B. (M) 2 L 7 2 4F A6WE 2000061400236 20000614 00236 WP 2000 6 14 EIA990305 1 19991119 A 5311 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE MISREPAIRED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - 941-45 ENGR REQUEST THAT FUSELAGE STATION 996 BETWEEN LONGERON 28R AND 29R, EXISTING REPAIR NOT PER SRM. CHANGE F ROM CLASS TWO TO A CLASS ONE REPAIR. FABRICATED AND INSTALLED DOUBLERS/FILLERS PER ECRA 941-53-051-2. (M) 2 L 7 2 4F A6WE 2000061400237 20000614 00237 WP 2000 6 14 EIA990306 1 19991120 A 5312 SPLICE DOUG DC9 DC933F 302207A WP PRESS BULKHEAD CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - AFT PRESS BULKHEAD, FORWARD SIDE AT THE 9:30 AND 11:00 O''CLOCK POSITIONS THE -15 SPLICES ARE CRACKED. REPAIRED E LONGATED FASTENER HOLES, GOUGE, AND CRACK DAMAGE ASSOCIATED WITH AFT PRESS BULKHEAD TEE-CHORD SPLICE AT L6L-L8L. REPAIR ED SEAL PLATE AT TEE CHORD SPLICE AT L17L-L18L PER ECRA 941-53-077-2 REV A. (M) 2 L 7 2 4F A6WE 2000061400238 20000614 00238 NM 2000 6 14 EIA990307 1 19991203 A 5311 FRAME BOEING 747 747SR46 NM BATTERY BAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 DURING B-CHECK, APU BATTERY COMPT STATION 2598 LEFT BULKHEAD CHORD FOUND CRACKED AT LATERAL FLANGE FASTENERS HOLE AREA A DJACENT TO S-12L. REPAIRED AS PER SRM 51-40-04 FIG 3 STRINGER 11L, 2 EACH FITTING REPLACED AS PER SRM 51-10-01 AND SB 7 47-53A-2410. (M) 2 L 7 4 4F A20WE 2000061400239 20000614 00239 WP 2000 6 14 EIA990308 1 19991211 A 5315 FLOORBEAM DOUG DC9 DC933F 302207A WP CARGO BAY CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - AFT CARGO PIT STATION 917 BL 0 FLOORBEAM CHAFED. FABRICATED REPAIR PARTS AND INSTALLED PER ECRA 941-53-094-2 AND DWG SR09530190. (M) 2 L 7 2 4F A6WE 2000061400240 20000614 00240 WP 2000 6 14 EIA990309 1 19991211 A 5320 99578383 INTERCOSTAL DOUG DC9 DC933F 302207A WP PAX DOOR SILL CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 941F 47193 MZJ - MULTIPLE FASTENERS SEVERELY CORRODED BELOW FORWARD ENTRY DOOR LOWER SILL AND ABOVE AIRSTAIR DOOR FRAME. REPLACED 9957838-3 INTERCOSTAL, SPLICED NEW SECTION OF UPPER CUSP ANGLE, AND INSTALLED REPAIR ANGLE ON LOWER CUSP ANGLE PER ECRA 941-53-075-2 REV A. (M) 2 L 7 2 4F A6WE 2000061400241 20000614 00241 WP 2000 6 14 EIA990310 1 19991118 A 5522 FASTENER DOUG DC9 DC932F 3022067 WP ELEVATOR DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 MZJ - FASTENER HEAD COMING OFF/BENDING BACK, LOWER SIDE OF RIGHT ELEVATOR 23.5 INCH INBOARD OF OUTBOARD TIP. REPAIRED P ER ECRA 935-55-047-2. (M) 2 L 7 2 4F A6WE 2000061400242 20000614 00242 WP 2000 6 14 EIA990311 1 19991119 A 5330 SKIN DOUG DC9 DC932F 3022067 WP FUSELAGE MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 935F 47220 MZJ - PREVIOUS FUSE SKIN PANEL REPAIR AT FS 133.425 NOT PER SRM 53-04, FIG 12B, SHEET 2. ALSO HAS NUMEROUS GOUGES IN RE PAIR. REPAIRED PER ECRA 935-53-048-2 REV A AND SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 2000061400271 20000614 00271 EU 2000 6 14 UR6A991104 1 19991105 A 2560 GE12 FLASHLIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - THE AFT VESTIBULE EMERGENCY FLASHLIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT. (M) 2 L 7 2 4T RT A27NM 2000061600303 20000616 00303 WP 2000 6 16 RRXA000482 1 19991203 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FORWARD AFT LOWER CARGO DOOR JAMB FRAME FITTING AT STA 340 AND LONGERON 27 RIGHT. DAMA GE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW F ITTING IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000061600304 20000616 00304 WP 2000 6 16 RRXA000483 1 19991205 A 5230 FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FORWARD AFT LOWER CARGO DOOR JAMB FRAME CRACKED AT STA 280 BETWEEN LONGERONS 26 RIGHT T O 27 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AN D INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600305 20000616 00305 WP 2000 6 16 RRXA000485 1 19991209 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FRAME CRACKED AT STA 560 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600306 20000616 00306 WP 2000 6 16 RRXA000486 1 19991218 A 5230 ATTACH FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LOWER CARGO DOOR JAMB ATTACHMENT FITTING CRACKED AT STA 520 AND LONGERON 31 RIGHT. DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPA IR IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2000061600307 20000616 00307 WP 2000 6 16 RRXA000488 1 19991207 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND EXTERNAL SKIN CRACKED AT STA 1220 AND LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED EN GINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600308 20000616 00308 WP 2000 6 16 RRXA000489 1 19991119 A 5230 3754946502N FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LOWER CARGO DOOR JAMB FITTING CRACKED AT STA 1220 AND LONGERON 23 RIGHT. DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-3 -0. 2 L 7 4 4F RT 4A25 2000061600309 20000616 00309 WP 2000 6 16 RRXA000490 1 19991203 A 5230 3755843501 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LOWER CARGO DOOR JAMB FITTING CRACKED AT STA 1220 BETWEEN LONGERONS 34 RIGHT TO 35 RIGH T. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED REPAIR IAW DC-8 SRM 53-2-0 SHEET 2 FIGURE 17 & 18. 2 L 7 4 4F RT 4A25 2000061600310 20000616 00310 WP 2000 6 16 RRXA000491 1 19991118 A 5210 FRAME DOUG DC8 DC873F 302199F WP PAX DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND R1 PASSENGER DOOR FRAME CRACKED. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DA MAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-1 86. 2 L 7 4 4F RT 4A25 2000061600311 20000616 00311 WP 2000 6 16 RRXA000492 1 19991118 A 5210 FRAME DOUG DC8 DC873F 302199F WP PAX DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND R2 PASSENGER DOOR FRAME CRACKED. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DA MAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-1 86. 2 L 7 4 4F RT 4A25 2000061600312 20000616 00312 WP 2000 6 16 RRXA000493 1 19991118 A 5210 FRAME DOUG DC8 DC873F 302199F WP PAX DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND L1 DOOR FRAME CRACKED. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREA TED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-168. 2 L 7 4 4F RT 4A25 2000061600313 20000616 00313 WP 2000 6 16 RRXA000494 1 19991203 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FLOOR PANEL CRACKED BETWEEN STA 1580 TO STA 1600. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000061600339 20000616 00339 WP 2000 6 16 RRXA000317 1 19991125 A 5340 37540432 ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FITTING CRACKED AT STA 1200 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000061600340 20000616 00340 WP 2000 6 16 RRXA000318 1 19991104 A 5510 3641121 ATTACH FITTING DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND HORIZONTAL STABILIZER LEFT SIDE ATTACHMENT FITTING CRACKED AT XCW 47.5. DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW ATTACHMENT FITTING IAW DC- 8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000061600341 20000616 00341 WP 2000 6 16 RRXA000319 1 19991207 A 5510 FITTING DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND HORIZONAL STABILIZER FITTING RIGHT SIDE AT STA 1798 AND XCW 47.5. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000061600342 20000616 00342 WP 2000 6 16 RRXA000321 1 19991024 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FLOOR PANEL MEMBRANE AT STA 1380 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED MEMBRANE IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2000061600343 20000616 00343 WP 2000 6 16 RRXA000322 1 19991114 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FLOOR PANEL MEMBRANE CRACKED AT STA 45 AND BL 53 RIGHT. DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2000061600344 20000616 00344 WP 2000 6 16 RRXA000324 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK DAMAGE BETWEEN STA 82 TO STA 95 AND BL 69 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 53- 2-3. 2 L 7 4 4F RT 4A25 2000061600345 20000616 00345 WP 2000 6 16 RRXA000325 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK AT STA 1300 AND BL 69 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600346 20000616 00346 WP 2000 6 16 RRXA000326 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK DAMAGE AT 1560 AND BL 69 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2000061600347 20000616 00347 WP 2000 6 16 RRXA000327 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK BETWEEN STA 1580 TO STA 1610 AND BL 55 LEFT. DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2000061600348 20000616 00348 WP 2000 6 16 RRXA000328 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND SEAT TRACK DAMAGED AT STA 680 AND BL 60 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600349 20000616 00349 WP 2000 6 16 RRXA000330 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND SEAT TRACK DAMAGED AT STA 240 AND BL 0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600377 20000616 00377 NM 2000 6 16 20000615AP003 1 19991114 A 5532 PANEL BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL NR 9502, INNER AFT EDGE CRACKED. REMOVED INNER SKIN PER SRM 51-30-2 PAGE 1, FABRICATED NEW INNER SKIN PER SRM 55-10-2. INSTALLED PER SRM 55-10-2. (M) 2 L 7 3 4F A3WE 2000061600378 20000616 00378 NM 2000 6 16 20000615AP004 1 19991114 A 5530 BRACKET BOEING 727 727225 1384077 NM VERTICAL STAB CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURNIG C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL 9503 LEFT AND RIGHT LOWER SECTION BRACKETS CRACKED. REMOVED BRACKET S, FABRICATED, TREATED AND INSTALLED PER SRM 51-30-3 APGE 14A. (M) 2 L 7 3 4F A3WE 2000061600379 20000616 00379 NM 2000 6 16 20000615AP005 1 19991111 A 5720 ANGLE BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND RIGHT WING RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANG LE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000061600380 20000616 00380 NM 2000 6 16 20000615AP006 1 19991111 A 5712 RIB BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND RIGHT WING L/E RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANGLE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M) 2 L 7 3 4F A3WE 2000061600381 20000616 00381 NM 2000 6 16 20000615AP007 1 19991111 A 5754 SLAT TRACK BOEING 727 727225 1384077 NM LT WING LE CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND .375 INCH CRACK AT LT WING FIXED L/E CUTOUT ABOVE NR 4 SLAT OUTBOARD TRACK. TRIMMED OUT DAMAGED SK IN AND FABRICATED DOUBLER AND FILLER, INSTALLED REPAIR PER SRM 57-30-4, PAGE 6. (M) 2 L 7 3 4F A3WE 2000061600382 20000616 00382 NM 2000 6 16 20000615AP008 1 19991112 A 5720 ANGLE BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND .375 INCH CRACK AT ANGLE ON BOTTOM OF RIGHT WING UPPER T/E PANEL AT WEB 5 INCHES FORWARD OF INBOAR D AILERON L/B LEADING EDGE. FABRICATED NEW ANGLE PER SRM 51-10-1 PAGE 4. INSTALLED ANGLE PER SRM 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000061600383 20000616 00383 NM 2000 6 16 20000615AP009 1 19991112 A 5720 652165827 CHANNEL BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND RIGHT WING LOWER TRAILING EDGE SUPPORT INBOARD CHANNEL CRACKED APPROX 1 INCH. REPLACED CHANNEL IA W SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 2000061600384 20000616 00384 NM 2000 6 16 20000615AP011 1 19991112 A 5712 RIB BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND RIGHT WING FIXED L/E RIB AFT END HAS TWO .75 INCH CRACKS THROUGH BOLT HOLES WHERE IT MOUNTS TO FRO NT SPAR. CUT OUT CRACK AREAS AT R/W L/E INTERIOR WEB STATION 130-599 IAW SRM 51-40-2 FIG 1. FABRICATED FILLER AND REPA IR DOUBLER AND INSTALLED IAW SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 2000061600385 20000616 00385 NM 2000 6 16 20000615AP012 1 19991112 A 5712 RIB BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND TWO EACH 1 INCH CRACKS INSIDE LEFT WING FIXED L/E AT TOP AFT END OF NOSE RIB-SLAT STATION 0, SEEN FROM OUTBOARD SIDE. FABRICATED NEW RIB AND INSTALLED IAW 51-10-1, PAGE 4. (M) 2 L 7 3 4F A3WE 2000061600386 20000616 00386 NM 2000 6 16 20000615AP013 1 19991113 A 5720 652165826 CHANNEL BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND 1.5 INCH CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT CHANNEL. INSTALLED NEW CHANNEL IAW SR M 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000061600387 20000616 00387 NM 2000 6 16 20000615AP014 1 19991113 A 5720 ANGLE BOEING 727 727225 1384077 NM LT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND TWO RIVETS PULLING, AND .375 INCH CRACK AT DOUBLER AT LT WING LOWER FAIRING SUPPORT ANGLE AFT FALS E SPAR AREA, OUTBOARD OF NR 3 FLAP TRACK. REMOVED DOUBLER FOR CRACK AND TWO RIVETS PULLING AS PER SRM 51-30-2 PAGE 1. FABRICATED NEW DOUBLER REPAIR AS PER SRM 51-10-1 PAGE 4. INSTALLED DOUBLER PER SRM 51-30-2 PAGE 1. (M) 2 L 7 3 4F A3WE 2000061600434 20000616 00434 WP 2000 6 16 RRXA000475 1 19991130 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK BETWEEN STA 120 TO STA 240 AND BL 69 LEFT. DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-3. 2 L 7 4 4F RT 4A25 2000061600435 20000616 00435 WP 2000 6 16 RRXA000477 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND SEAT TRACK DAMAGED AT STA 680 AND BL 0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600436 20000616 00436 WP 2000 6 16 RRXA000478 1 19991118 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND SEAT TRACK BETWEEN STA 1550 TO STA 1585 AND BL 0. DAMAGE EXCEEDED LIMITATIONS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600437 20000616 00437 WP 2000 6 16 RRXA000479 1 19991207 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN FLOOR PANEL SUPPORT FITTING AT STA 55 AND BL 32 LEFT. DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SUPPORT FITTING IAW DC-8 SRM 51-1 -21. 2 L 7 4 4F RT 4A25 2000061600438 20000616 00438 WP 2000 6 16 RRXA000480 1 19991214 A 5313 5750198501 LONGERON DOUG DC8 DC873F 302199F WP LT WHEEL WELL CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LONGERON 24 LEFT CRACKED AT STA 857. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVE D DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW LONGERON 24 LEFT IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000061600441 20000616 00441 NM 2000 6 16 20000615AP010 1 19991112 A 5720 BRACKET BOEING 727 727225 1384077 NM RT WING CRACKED A MYWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802EA 22433 DURING C-CHECK, FOUND BRACKET HAS 1 INCH CRACK WHERE RT WING NR 8 SLAT LOWER SKIN EXTENSION ATTACHES TO BOTTOM OF INBOAR D TRACK. REPLACED BRACKET IAW SRM 51-10-1 AND 51-30-2 PAGE 1 AND PAGE 4. (M) 2 L 7 3 4F A3WE 2000061600462 20000616 00462 WP 2000 6 16 RRXA000297 1 19991217 A 5753 VANE DOUG DC8 DC873F 302199F WP LT TE FLAP DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LEFT WING INBOARD FLAP NR 2 VANE HAS MOUNT HOLE ENLONGATED. DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600463 20000616 00463 WP 2000 6 16 RRXA000298 1 19991122 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LEFT WING, FLAP WELL, RIB CRACKED AT XRS 178. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA DER APPROVED ENGINEE RING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600464 20000616 00464 WP 2000 6 16 RRXA000299 1 19991210 A 5754 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LEFT WING, LEADING EDGE, MOUNT HOLES ENLONGATED AT XFS 520.168. DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600465 20000616 00465 WP 2000 6 16 RRXA000300 1 19991108 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LEFT WING, FORWARD LOWERS PAR CAP CRACKED AT XFS 520. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER ENGINEERING SK ETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600466 20000616 00466 WP 2000 6 16 RRXA000303 1 19991001 A 5511 FRAME DOUG DC8 DC873F 302199F WP HORZONTAL STAB CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE FRAME CRACKED AT XFS 53.75. DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2000061600467 20000616 00467 WP 2000 6 16 RRXA000304 1 19991116 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND INTERCOASTAL CRACKED AT STA 1890 AND LONGERON 10 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SRM 51- 1-20. 2 L 7 4 4F RT 4A25 2000061600468 20000616 00468 WP 2000 6 16 RRXA000305 1 19991119 A 5311 FRAME DOUG DC8 DC873F 302199F WP TAIL SECTION CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND TAIL CONE FRAME CRACKED RIGHT SIDE AT STA 1923. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2000061600469 20000616 00469 WP 2000 6 16 RRXA000306 1 19991017 A 5754 ANGLE DOUG DC8 DC873F 302199F WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND RIGHT WING LEADING EDGE INTERNAL ANGLE CRACKED AT XW 230. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-4 . 2 L 7 4 4F RT 4A25 2000061600470 20000616 00470 WP 2000 6 16 RRXA000307 1 19991105 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND RIGHT WING LEADING EDGE WITH 6 INCH CRACK AT XW 257.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGI NEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600471 20000616 00471 WP 2000 6 16 RRXA000309 1 19991122 A 5720 3751693501 FITTING DOUG DC8 DC873F 302199F WP RT WING FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND RIGHT WING FLAP STOP FITTING CRACKED AT XFS 410. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FLAP STOP FITTING IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000061600472 20000616 00472 WP 2000 6 16 RRXA000310 1 19991102 A 5340 37739731N ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND UPPER CARGO DOOR JAMB FRAME ATTACHMENT FITTING CRACKED AT STA 120 AND LONGERON 21 RIGHT . DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FRAME ATT ACHMENT FITTING IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2000061600473 20000616 00473 WP 2000 6 16 RRXA000311 1 19991126 A 5320 PLATE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND AFT LOWER CARGO DOOR EXTERNAL SKIN SCUFF PLATE CRACKED RIGHT SIDE STA 1240. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600474 20000616 00474 WP 2000 6 16 RRXA000312 1 19991123 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND AFT PRESSURE BULKHEAD CRACKED AT STA 1766 AND LONGERON 3 RIGHT. DAMAGE EXCEEDED LIMITA TIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPR OVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600475 20000616 00475 WP 2000 6 16 RRXA000313 1 19991019 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FLOOR PANEL CRACKED BETWEEN STA 760 TO 1100. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600476 20000616 00476 WP 2000 6 16 RRXA000315 1 19991025 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND FRAME CRACKED AT STA 1580 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2000061600477 20000616 00477 WP 2000 6 16 RRXA000316 1 19991028 A 5340 4750419502N ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CUSP ATTACHMENT FITTING CRACKED AT STA 1160 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW CUSP ATTACHMENT FITTING IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000061600478 20000616 00478 WP 2000 6 16 RRXA000314 1 19991016 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND UPPER CARGO SEAT TRACK DAMAGED BETWEEN STA 500 TO STA 510 AND BL 25 RIGHT. DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLI CE IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600479 20000616 00479 WP 2000 6 16 RRXA000301 1 19991105 A 5730 SKIN DOUG DC8 DC873F 302199F WP LH WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT REMOVED TEMPORARY REPAIR FROM LEFT WING LEADING EDGE AT XFS 250. REMOVED TEMPORARY REPAIR, T REATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW REPAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600480 20000616 00480 WP 2000 6 16 RRXA000476 1 19991110 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND SEAT TRACK BETWEEN STA 757 TO STA 781 AND BL 69 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600481 20000616 00481 WP 2000 6 16 RRXA000323 1 19991115 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK DAMAGE AT STA 1690 AND BL 69 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600482 20000616 00482 WP 2000 6 16 RRXA000329 1 19991117 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND SEAT TRACK DAMAGED AT STA 600 AND BL 60 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600483 20000616 00483 WP 2000 6 16 RRXA000331 1 19991116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK DAMAGED AT STA 1040 AND BL 0. DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2000061600484 20000616 00484 WP 2000 6 16 RRXA000302 1 19991119 A 5311 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND SHEAR TIE CRACKED AT STA 660 BETWEEN LONGERONS 21 RIGHT TO 22 RIGHT. DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061600485 20000616 00485 WP 2000 6 16 RRXA000320 1 19991119 A 5500 3641126501N ATTACH FITTING DOUG DC8 DC873F 302199F WP EMPENNAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND VERTICAL STABILIZER ATTACHMENT FITTING CRACKED AT STA 1781 AND XCW 47.5. DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW ATTACHMENT FITTING IAW DC -8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2000061600486 20000616 00486 WP 2000 6 16 RRXA000481 1 19991203 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND LONGERON 31 LEFT SPLICE FITTING CRACKED BETWEEN STA 200 TO STA 220. DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLICE FITTING IAW DC-8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2000061600487 20000616 00487 WP 2000 6 16 RRXA000484 1 19991206 A 5320 PLATE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND EXTERNAL SKIN SCUFF PLATE CRACKED BETWEEN STA 1680 TO STA 1700 AND LONGERON 21 LEFT. D AMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RE PAIR IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2000061900174 20000619 00174 CE 2000 6 19 S2YA99030 1 19991220 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A S2YA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 92SK UE92 DURING APPROACH OF FLIGHT 1024, MKE-ATW, LT MAIN GEAR SAFE LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR SEVERAL TIMES AND THEN MADE AN UNEVENTFUL LANDING. OUTSTATION MX INSPECTED AND PINNED THE GEAR. THE AIRCRAFT WAS FERRIED TO M KE AND INSPECTED BY MAINTENANCE. MAINTENANCE REPLACED LT MAIN ACTUATOR AND ADJUSTED THE DOWNLOCK SWITCH. AFTER OPS AND LEAK CHECK THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 2000061900176 20000619 00176 CE 2000 6 19 S2YA99031 1 19991227 A 3260 1143610441 HARNESS BEECH 1900 1900D 1154162 CE SQUAT SWITCH SHORTED A S2YA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 145SK UE145 FLT 1826 - MKE-CMH - THE STALL WARNING (HEAT) LIGHT ILLUMINATED. THE CREW CYCLED THE SWITCH SEVERAL TIMES AND THEN MADE AN AIRTURN BACK TO MKE. MAINTENANCE INSPECTED THE SYSTEM AND FOUND HIGH RESISTANCE FOR THE GROUND WIRE ON THE LEFT SQU AT SWITCH. MAINTENANCE REPLACED THE SQUAT SWITCH WIRE HARNESS AND OPS CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4T RT A24CE 2000062900181 20000629 00181 WP 2000 6 29 RRXA000798 1 19991230 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN UPPER CARGO COMPT STA 1180 BETWEEN LONGERONS 21R TO 21L, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FAB RICATED STRAP DOUBLER AND GUSSETTS FROM 7075-T6 AND INSTALLED PER EO NR 99-236 WITH APPROVED 8110-3 DATED 12-3-99. 2 L 7 4 4F 4A25 2000062900182 20000629 00182 WP 2000 6 29 RRXA000799 1 19991230 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT STA 1160 AND LONGERONS 21R TO 21L, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES , FABRICATED STRAP DOUBLER & GUSSETTS FROM 7075-T6 AND INSTALLED IAW EO 399-236 WITH APPROVED 8110-3 DATED 12-3-99. 2 L 7 4 4F 4A25 2000062900184 20000629 00184 WP 2000 6 29 RRXA000801 1 19991229 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT STA 1040 AND LONGERONS 21R TO 21L, DAMAGE EX CEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED ALL DISCREPANT H OLES, FABRICATED STRAP DOUBLERS & GUSSETTS FROM 7075-T6 AND INSTALLED PER EO NR 99-236 WITH APPROVED 8110-3 DATED 12-3-9 9. 2 L 7 4 4F 4A25 2000071100011 20000711 00011 NE 2000 7 11 20000517SH026 2 19991228 A 7421 3038221 IGNITER DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE CABLE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 202 90000012 PCE206018 IGNITER HAD EXCESSIVE BURN IN SOME AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X) 1 G 7 2 3U 3 U NC H19NM E42NE 2000071100012 20000711 00012 NE 2000 7 11 20000517SH027 2 19991208 A 7421 3038221 IGNITER DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE CABLE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 202 90000012 PCE206018 IGNITER HAD EXCESSIVE BURN IN SOME AREAS. (X) 1 G 7 2 3U 3 U NC H19NM E42NE 2000071100013 20000711 00013 NM 2000 7 11 20000517SH028 1 19990806 A 7720 312299201 CONTROL BOX DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE MGT INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 271 90000012 PCE206018 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X) 1 G 7 2 3U 3 U NC H19NM E42NE 2000071100014 20000711 00014 NM 2000 7 11 20000517SH029 1 19991208 A 7720 312299201 CONTROL BOX DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE MGT FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 90000012 REJECTED NEW OUT-OF-BOX. BOX WAS TRIMMED TO 111 C, BUT LATER FOUND OUT THAT PWC HAD ALREADY TRIMMED THE OVERHAULED ENGI NE IN THE TEST CELL FOR ADDITIONAL 9 C THAT IS OPERATED WITH SB 28171. REPLACED W ITH NEW UNIT, CORRECTED PROBLEM. (X) 1 G 7 2 3U 3 U NC H19NM E42NE 2000071800011 20000718 00011 WP 2000 7 18 ASAA9980317 1 19991215 A 5347 6022044 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE LEFT INBOARD TRACK WAS FOUND CORRODED ON THE EDGE AND INSIDE WEB OF THE TRACK AT APPROXIMATE LY STATION 1041. REPAIRED AND REPLACED TRACK FROM STATION 1032 TO 1241 WITH SPLICES PER SRM 53-05, FIG 4F. (M) 2 L 7 2 4F RT A6WE 2000071800013 20000718 00013 WP 2000 7 18 ASAA9980322 1 19991215 A 5320 5936660167 CHANNEL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE MID CARGO BAY Z CHANNEL FLOOR SUPPORT FROM STATION 693 TO 731 ABOVE LONGERON 28R WAS FOUND C ORRODED. REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F RT A6WE 2000071800014 20000718 00014 WP 2000 7 18 ASAA9980327 1 19991215 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE LEFT SIDE OF FUSELAGE SKIN WAS FOUND CRACKED APPROX .20 INCH AT STATION 1401, 4.5 INCH BELOW LONGERON 13L. REPAIRED AND INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 18. (M) 2 L 7 2 4F RT A6WE 2000071800110 20000718 00110 EA 2000 7 18 20000714SH023 2 19990521 A 8520 75191 CAMSHAFT GULSTM 500 500B 0141106 SW LYC O540 IO540E1A5 41532 EA BROKEN E A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 99 888CA 1730 1318127 RL30348 FORWARD END OF CAMSHAFT BROKE WHERE PROPELLER GOVERNOR DRIVING GEAR ATTACHES. THIS RESULTED IN LOSS OF PROPELLER GOVERN OR AND LOSS OF RPM. ENGINE WAS FEATHERED AND LANDED SAFELY. (X) 1 H 7 2 3O 3 O 6A1 1E4 2000071800206 20000718 00206 WP 2000 7 18 RRXA001651 1 19991228 A 5310 DOUBLER DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE DOUBLER TO LONGERON IN THE AFT LOWER CARGO BILGE AT STA 1140 T O 1160 AND L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 7075-T6 AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORR OSION PROGRAM). 2 L 7 4 4F 4A25 2000071800241 20000718 00241 WP 2000 7 18 RRXA000864 1 19991228 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES TO THE UPPER CARGO COMPT AT STA 1060 AND L21R TO L21L, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES, FABRICATED DOU BLER AND GUSSET PLATES FROM 7075-T6 AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 99-236 WITH APPROVED 8110-3 DATED 12-3- 99. 2 L 7 4 4F 4A25 2000071800242 20000718 00242 WP 2000 7 18 RRXA000967 1 19991222 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT AT STA 500 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT AND MISDRIL LED HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800256 20000718 00256 WP 2000 7 18 RRXA000964 1 19991228 A 5320 STIFFENER DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE FWD LOWER CARGO COMPARTMENT RIGHT STIFFENER AT STA 550 TO 560 AND L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRI CATED AND INSTALLED NEW STIFFENER IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000071800259 20000718 00259 WP 2000 7 18 RRXA000966 1 19991228 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT STA 520 AND L21R TO L21L, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES, FABRICATED DOUBLER AND GUSSETS FROM 7075-T6 AND INSTALLED IAW EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800260 20000718 00260 WP 2000 7 18 RRXA000968 1 19991223 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 460 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES, FABRICAT ED DOUBLER FROM 7075-T6 AND INSTALLED IAW EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800261 20000718 00261 WP 2000 7 18 RRXA000969 1 19991221 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 440 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE,TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES PER EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800262 20000718 00262 WP 2000 7 18 RRXA000970 1 19991221 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 420 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT AND MISDRILLED HOLES PER E O NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800264 20000718 00264 WP 2000 7 18 RRXA000865 1 19991228 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT AT STA 1100 AND L21R TO L21L, DAMAGE EXCEEDE D LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES, FABRICATED DOU BLER AND SHIMS FROM 7075-T6 AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 99-236 WITH APPROVED 8110-3 DATED 12-03-99. 2 L 7 4 4F 4A25 2000071800265 20000718 00265 WP 2000 7 18 RRXA000866 1 19991222 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND NUMEROUS MISDRILLED HOLES TO THE FRAME AT STA 270 AND L21R TO L21L, DAMAGE EXCEEDED LI MITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 7075-T6 A ND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800266 20000718 00266 WP 2000 7 18 RRXA000971 1 19991223 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 400 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED PER EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800267 20000718 00267 WP 2000 7 18 RRXA000972 1 19991223 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 380 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800268 20000718 00268 WP 2000 7 18 RRXA000973 1 19991223 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND NUMEROUS MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 360 AND L21R TO L21L, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DI SCREPANT HOLES, FABRICATED DOUBLER FROM 7075-T6 AND INSTALLED PER EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800269 20000718 00269 WP 2000 7 18 RRXA000975 1 19991229 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 280 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED PER EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800310 20000718 00310 WP 2000 7 18 ASAA9980314 1 19991215 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT, MAIN FRAME SPLICE WAS FOUND CORRODED AT STATION 1271, LONGERON 29L-30 . REPAIRED PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2000071800311 20000718 00311 WP 2000 7 18 ASAA9980315 1 19991215 A 5347 3936595524 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, FORWARD END HAS THREE CORRODED FASTENERS AND NUTPLATES, STATION 1011, BL 6. REPAIRED PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2000071800312 20000718 00312 WP 2000 7 18 ASAA9980316 1 19991215 A 5347 6019943 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE LEFT OUTBOARD TRACK WAS FOUND CORRODED AT STATION 1155. REPAIRED AND REPLACED SEAT TRACK, S TATION 1030 TO 1220, LEFT OUTBOARD, PER SRM 53-05, FIG 4. (M) 2 L 7 2 4F RT A6WE 2000071800313 20000718 00313 WP 2000 7 18 SAA9980318 1 19991215 A 5347 5936663503 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM, WAS FOUND CORRODED AT STATION 1222-1322 , BL 16. REPAIRED PER SRM 53-05, FIG 4C AND SRM 53-20-0, FIG 11. (M) 2 L 7 2 4F RT A6WE 2000071800314 20000718 00314 WP 2000 7 18 ASAA9980319 1 19991215 A 5347 5936663505N CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM, WAS FOUND CORRODED AT STATION 1212-1322 , BL 16R. REPLACED TRACK PER SRM 51-31-0. (M) 2 L 7 2 4F RT A6WE 2000071800315 20000718 00315 WP 2000 7 18 ASAA9980320 1 19991215 A 5347 S00062 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM, WAS FOUND CORRODED AT STATION 1007-1222 , BL 16L. REPLACED TRACK PER SRM 53-01 AND 53-05, FIG 4G. (M) 2 L 7 2 4F RT A6WE 2000071800316 20000718 00316 WP 2000 7 18 ASAA9980321 1 19991215 A 5347 5936663501 CARGO TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT TIEDOWN TRACK, TOP AND BOTTOM WAS FOUND CORRODED AT STATION 1007-1155 ABOVE LONGERON 27R. REPAIRED PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000071800317 20000718 00317 WP 2000 7 18 ASAA9980323 1 19991215 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE PASSENGER CABIN SUBFLOOR WAS FOUND CORRODED AT STATION 180, LBL 5. REPAIRED PER SRM 53-01, FIG 4 SHEET 3. (M) 2 L 7 2 4F RT A6WE 2000071800318 20000718 00318 WP 2000 7 18 ASAA9980324 1 19991215 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE PASSENGER CABIN SUBFLOOR WAS FOUND PUNCTURED AT LBL 7.50, STATION 200. INSTALLED DOUBLER RE PAIR PER SRM 53-01. (M) 2 L 7 2 4F RT A6WE 2000071800319 20000718 00319 WP 2000 7 18 ASAA9980325 1 19991215 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE INTERNAL DOUBLER IN THE CENTER CARGO COMPARTMENT WAS FOUND CORRODED AT STATION 560 BETWEEN L ONGERON 29R AND 30. INSTALLED DOUBLER REPAIR PER SRM 51-30. (M) 2 L 7 2 4F RT A6WE 2000071800320 20000718 00320 WP 2000 7 18 ASAA9980326 1 19991215 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 943AS 53018 PHX - DURING 30K CHECK, THE RIGHT SIDE OF FUSELAGE SKIN WAS FOUND CRACKED APPROX .25 INCH AT STATION 1401, 4.5 INCH BELO W LONGERON 13R. REPAIRED AND INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 18. (M) 2 L 7 2 4F RT A6WE 2000071800508 20000718 00508 WP 2000 7 18 RRXA001504 1 19991228 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 340 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES, FABRICATED ATTACH S TRAP FROM 7075-T6 AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 99-236 WITH APPROVED 8110-3 DATD 12-01-99. 2 L 7 4 4F 4A25 2000071800509 20000718 00509 WP 2000 7 18 RRXA001505 1 19991228 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT FS 392 AND L21R TO L21L, DAMAGE EXCEEDED LIM ITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES, FABRICATED DO UBLER FROM 7075-T6 AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071800553 20000718 00553 WP 2000 7 18 RRXA001514 1 19991221 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT FLOORBEAM UPPER LOWER CARGO COMPT FS 235 AND XCW 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLES FROM 2024-T3 AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-20C AND EO NR 99-236 WITH APPROVED 8110-3 DATED 12-16-99. 2 L 7 4 4F 4A25 2000071800561 20000718 00561 WP 2000 7 18 RRXA001626 1 19991230 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT AT FS 1020 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABR ICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EO NR 99-236 WITH APPROVED 8110-3 DATED 12-03-99. 2 L 7 4 4F 4A25 2000071800562 20000718 00562 WP 2000 7 18 RRXA001627 1 19991229 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT AT FS 1000 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED ALL DISCREPANT HOLES, FABRICATED DOUBLER FROM 7075-T6 AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 99-236 WITH APPROVED 8110-3 DATED 12-03-99. 2 L 7 4 4F 4A25 2000071800563 20000718 00563 WP 2000 7 18 RRXA001629 1 19991223 A 5311 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT AT FS 480 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES, FABRI CATED DOUBLERS FROM 7075-T6 AND INSTALLED PER EO 99-236 WITH APPROVED 8110-3 DATED 12-01-99. 2 L 7 4 4F 4A25 2000071900253 20000719 00253 WP 2000 7 19 ASAA9980340 1 19991229 A 5240 PIN DOUG DC9 DC983 3022083 WP SERVICE DOOR CONTAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING MAINTENANCE CHECK, THE R1 DOOR WOLD NOT LATCH OPEN. FOUND GUST LOCK CATCH PIN COVERED WITH SEALANT, REMOVE D SEALANT AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2000072500256 20000725 00256 CE 2000 7 25 20000725AP004 1 19990701 A 7120 11490455 TRUSS BEECH 1900 1900 1154160 CE RT ENGINE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 189GA UB9 C-2 INSPECTION, RIGHT ENGINE TRUSS HAS A CRACK AT INBOARD COWLING ATTACH BRACKET. REMOVED AND REPLACED RIGHT ENGINE TRU SS. (M) 2 L 7 2 4T RT A24CE 2000072500261 20000725 00261 NM 2000 7 25 AALA991942 1 19991217 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT STAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 871AA 21383 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY E XIT LIGHT ASSEMLBY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000072500262 20000725 00262 NM 2000 7 25 AALA991972 1 19991226 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 887AA 21526 DFW - DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT FLOOR PATH LIGHTS IN COACH CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRING AT AFT LAVATORY. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000072500263 20000725 00263 NM 2000 7 25 AALA991999 1 19991230 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 873AA 21385 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 29 AND 30 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEATS 29 AND 30. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000072500309 20000725 00309 NM 2000 7 25 USAA991932 1 19991214 A 3350 LIGHT BOEING 727 727223 1384074 NM EMERGENCY EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 877AA 21389 TUL - FOUND FORWARD GALLEY LEFT DOOR FRAME EMERGENCY EXIT LIGHT MARKER DAMAGED E-58 3095015. INSTALLED SERVICEABLE P2-0 1-0031-302 WORK ACCOMPLISHED PER MM 33-50-001-0 AND 33-60-098-0. (M) 2 L 7 3 4F A3WE 2000072500310 20000725 00310 NM 2000 7 25 AALA990933 1 19990623 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 710AA 22467 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN COACH INOPERATIVE. SECURED EMERGENCY EXIT FLO OR PATH LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000072500311 20000725 00311 NM 2000 7 25 AALA991933 1 19991214 A 3350 SIGN BOEING 727 727223 1384074 NM COCKPIT MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 877AA 21389 TUL - FOUND EMERGENCY EXIT LIGHT SIGN ABOVE COCKPIT DOOR IS DIM, E-583095020. INSTALLED SERVICEABLE LTG 5192 WORK ACCOM PLISHED PER MM 33-50-101-2. (M) 2 L 7 3 4F A3WE 2000072500312 20000725 00312 NM 2000 7 25 AALA991958 1 19991221 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 878AA 21390 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 3E HAS ONE BULB INOPERATIVE. REPLACED EMERG ENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 3E. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000072600145 20000726 00145 NM 2000 7 26 AALA991962 1 19991223 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 38C INOPERATIVE. REPLACED EMERGENCY EXIT F LOOR PATH LIGHT STRIP AT SEAT 38C. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600146 20000726 00146 NM 2000 7 26 AALA991965 1 19991223 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 29C INOPERATIVE. REPLACED EMERGENCY EXIT F LOOR PATH LIGHT STRIP AT SEAT 29C. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600147 20000726 00147 NM 2000 7 26 AALA991875 1 19991208 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1758B 48527 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 20G INOPERATIVE. REPLACED EMERGENCY EXIT F LOOR PATH LIGHT STRIP AT SEAT 20G. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600148 20000726 00148 2000 7 26 AALA991451 4 19990925 A 2330 6047660001 VIDEO UNIT DOUG MD11 MD11 3023602 NM PAX SEAT FAILED A AALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 1760A 48550 LHR - FLT 91 - DURING PUSH BACK SEAT 3A IN SEAT VIDEO EMITTED A STRONG ELECTRICAL SMOKE, CABIN BUS WAS SWITCHED OFF AND SMOKE STOPPED. REPLCED IN SEAT VIDEO PLAYER AT SEAT 3A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600149 20000726 00149 NM 2000 7 26 AALA991788 1 19991124 A 3350 1001191 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD DOOR JAM 4L INOPERATIVE. REPLACED EMERGENCY EXIT LI GHT AT FORWARD DOOR JAM 4L. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600150 20000726 00150 NM 2000 7 26 AALA991789 1 19991124 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 20C INOPERATIVE. REPLACED EMERGENCY EXIT F LOOR PATH LIGHT STRIP AT SEAT 20C. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600151 20000726 00151 NM 2000 7 26 AALA991742 1 19991117 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 20C-21C WERE INOPERATIVE. REPLACED EME RGENCY FLOOR PATH LIGHT STRIP AT SEAT ROW 20C-21C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600152 20000726 00152 NM 2000 7 26 AALA991741 1 19991117 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 34G-20G WERE INOPERATIVE. REPLACED EME RGENCY FLOOR PATH LIGHT STRIP AT SEAT ROW 34G-20G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600153 20000726 00153 NM 2000 7 26 AALA991700 1 19991111 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1765B 48596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 38G INOPERATIVE. REPLACED EMERGENCY EX IT FLOOR PATH LIGHT FLAT CONDUCTOR AT SEAT ROW 38G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072600154 20000726 00154 NM 2000 7 26 AALA991663 1 19991105 A 3350 SIGN DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 1755 48490 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT IDENTIFIER SIGN ON CABIN DOOR 2R ATTACHMENT PIN BROKEN. REPLACED EME RGENCY EXIT IDENTIFIER SIGN ON CABIN DOOR 2R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 2000072700190 20000727 00190 EU 2000 7 27 AALA991993 1 19991231 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A K NONE L NO TEST IN INSP/MAINT 1 SW 21 1413A 11376 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT RIGHT AFT AND FORWARD OVERWING LIGHTS INOPERATIVE. REPAIRED WIRING A T CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT SIGN. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F RT 2000081000090 20000810 00090 WP 2000 8 10 AT0000372 1 19991203 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND FORWARD SIDE OF STRINGER 23 TO HAVE EXFOLIATED CORROSION. REMOVED CORRODED AREA IAW EO 99-1426 REV 1R. 2 L 7 2 4F A6WE 2000081000091 20000810 00091 WP 2000 8 10 AT0000373 1 19991201 A 5320 WEB DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 824AT 47278 DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CRACK IN AFT CARGO BIN DOOR IN NR 5 WEB BEAM. STOP DRILLE D CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 52-01. 2 L 7 2 4F A6WE 2000081600105 20000816 00105 EA 2000 8 16 USAASA00022 1 19990610 A 5270 PSEU CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE PASSENGER DOOR FAILED W B I G A EMER. DESCENT CABIN DEPRESSURIZATION O2 MASK DEPLOYED UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) DOOR WARNING UNSAFE INDICATION. SUSPECT IMPROPER DOOR CLOSURE AT DEPARTURE. CONFIRMED WITH FEEDBACK FROM BOMBARD IER. 2 L 7 2 4F 4 F RT A21EA E15NE 2000081600184 20000816 00184 NM 2000 8 16 AALA990905 1 19990619 A 3350 1001141 LIGHT BOEING 727 727227 1384078 NM AIRSTAIRS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 726AA 20733 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON CEILING AT BOTTOM OF AFT STAIRS INOPERATIVE. REPLACED EMERG ENCY EXIT CEILING LIGHT AT BOTTOM OF AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000081600185 20000816 00185 NM 2000 8 16 AALA990906 1 19990619 A 3350 EL104 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 726AA 20733 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY DOOR MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALL EY DOOR MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000081600186 20000816 00186 NM 2000 8 16 AALA990904 1 19990513 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 727AA 20734 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 6D AND 28D INOPERATIVE. REPLACED EME RGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000081600187 20000816 00187 NM 2000 8 16 AALA991977 1 19991227 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 718AA 20611 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT SECTION OF COACH INOPERATIVE. REPLACED EMER GENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000081600188 20000816 00188 NM 2000 8 16 AALA991954 1 19991221 A 3350 3005441 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 722AA 20730 DFW - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY EXIT L1 DOOR LIGHT INOPERATIVE. REPLACED EXTERIOR EMERGENCY EXIT L1 DOOR LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 2000082400210 20000824 00210 NM 2000 8 24 RIVA9900001 1 19991226 A 2741 10600171 CONTROL CABLE BOEING 727 727221 1384071 NM TRIM TABS SHEARED A RIVA K NONE O OTHER IN INSP/MAINT 1 NE 05 363PA 22535 AFTER ARRIVAL OF FLIGHT NR 1 IN SFB, CREW NOTICED TRIM TAB INDICATOR STUCK AT 7.5 UNITS NOSE UP BOTH SIDES (CAPT''S & F/ O''S). MAINTENANCE REMOVED AND REPLACED CABLE WITH NEW. ALL WORK AND ADJUSTMENTS DONE IN ACCORDANCE WITH THE BOEING MA INTENANCE MANUAL CHAPTER 27-40-0. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2000090500127 20000905 00127 WP 2000 9 5 RRXA002953 1 19991229 A 5321 SPLICE DOUG DC8 DC873F 302199F WP FLOOR SUPPORT CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR SPLICE BETWEEN STA 280 - 340 AT X-48 AND Z-50, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000092500001 20000925 00001 NM 2000 9 25 20000707SH011 1 19991116 A 7540 232A92211 LINE BOEING 737 7377CG 13844FA NM BLEED AIR CHAFED B P7UR K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 17 888GW 30751 INSPECTION REVEALED WIRE BUNDLE RUN W2705 (HGS) MAKES HARD CONTACT WITH TAT PROBE BLEED AIR LINE AT BS 312 LBL 47.0 WL 2 02.6. THIS HAS BEEN FOUND ON THE LAST 4 AIRCRAFT. CAUSE - BUNDLE NOT ROUTED PROPERLY. SUBMITTER RECOMMENDED RELOCATING WIRE BUNDLE DURING MANUFACTURING. (X) 2 L 7 2 4F RT A16WE 2000100300002 20001003 00002 WP 2000 10 3 L1GA200000307 1 19991228 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A L1GA K NONE O OTHER IN INSP/MAINT 1 SW 07 14534 47110 FWD CARGO COMPARTMENT FLOOR RAIL CORRODED. 2 L 7 2 4F A6WE 2000100300004 20001003 00004 WP 2000 10 3 L1GA200000309 1 19991226 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A L1GA K NONE O OTHER IN INSP/MAINT 1 SW 07 14534 47110 AFT CARGO COMPARTMENT SHORT RAIL CORRODED 1 X 12 INCHES. 2 L 7 2 4F A6WE 2000100300150 20001003 00150 WP 2000 10 3 L1GA200000305 1 19991226 A 5347 CARGO TRACK DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A L1GA K NONE O OTHER IN INSP/MAINT 1 SW 07 14534 47110 AFT CARGO COMPARTMENT RT FLOOR TRACK CORRODED 1 X 24 INCHES. 2 L 7 2 4F A6WE 2000100300258 20001003 00258 WP 2000 10 3 L1GA200000303 1 19991226 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP CARGO BAY CORRODED A L1GA K NONE O OTHER IN INSP/MAINT 1 SW 07 14534 47110 AFT CARGO COMPARTMENT LT FLOOR RAIL CORRODED 1 X 12 INCHES. 2 L 7 2 4F A6WE 2000101000458 20001010 00458 NE 2000 10 10 99UAL900446 2 19990824 A 7230 CARBON SEAL AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE NR 1 ENGINE LEAKING A UALA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 807UA 798 V10092 AFTER SHUTDOWN NOTICED FIRE IN TAILPIPE OF NR 1 ENGINE. DRY MOTORED ENG 3 TIMES TO EXTINGUISH FIRE. FIRE LASTED APPROX 15 MINS INTERMITTENLY DURING MOTORING. *S/D* FOUND OIL LEAKING PAST NR 5 BEARING CARBON SEAL INTO EXHAUST CASE GASPAT H. REPLACED CARBON SEAL ASSEMBLY. SHOP MANUAL LIMITS FOR CARBON SEAL BEING REVISED BY MANUFACTURER. 2 L 7 2 4F 4 F RT A28NM E40NE 2000101000459 20001010 00459 NM 2000 10 10 99UAL900547 1 19991022 A 3411 4107311 HOSE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE PITOT SYSTEM SPLIT A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 614UA 21875 CHRONIC PITOT-STATIC SYSTEM FAULTS. ALTIMETERS SPLIT. SPLIT IN INDICATIONS BECOME MORE APPARENT WITH INCREASING AIRSPE ED AND ALTITUDE. *S/D* LEAKAGE ON THE PILOT STATIC SYSTEM. REPLACED SEVERAL COMPONENTS DURING PROCESS OF TROUBLESHOOT ING, INCLUDING: PITOT PROBE, ALTIMETER, AOA SENSOR , LT UPR PITOT PROBE FLEX HOSE. PRESSURIZED THE ACFT WITH 6.0 DP AN D TESTED PITOT/STATIC SYSTEM TO 40K FT. SYSTEM LEAKAGE WITHIN LIMITS PER MM. TEST FLIGHT AT 37K FT FOR ALTIMETER VERIF ICATION, OBTAINED READINGS: CAPT 37000 FT, FIRST OFFICER 37050 FT, WITHIN LIMITS. 2 L 7 2 4F 4 F RT A1NM E3NE 2000101100456 20001011 00456 NE 2000 10 11 99UAL900602 2 19991114 A 7250 STATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 589UA 15725 15725 28707 726524 THE NUMBER ONE ENGINE WAS SHUT DOWN SHORTLY AFTER TAKEOFF DUE TO A COMPRESSOR STALL. THE AIRCRAFT RETURNED TO DEN. *S/ D* AFTER LANDING AT DEN METAL WAS FOUND IN THE TAILPIPE AND THE ENGINE WAS REMOVED AND SENT TO THE SHOP FOR INVESTIGATI ON AND REPAIR. THE SHOP DISASSEMBLY FINDINGS WERE A FAILED 10TH STAGE HPC STATOR. THIS IS AN INDUSTRY PROBLEM AND IS U NDER INVESTIGATION BY PWA. 2 L 7 2 4F 4 F RT A2NM E17NE 2000101600426 20001016 00426 NM 2000 10 16 99UAL900604 1 19991116 A 4920 523587F96159 BEARING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU FAILED A UALA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7277U 204 21424 663785 WHILE USING APU TO POWER AIRCRAFT, AIRCRAFT STARTED TO FILL WITH SMOKE. APU MADE SEVERAL LOUD BANGS, APU WAS SHUT DOWN. SMOKE CONTINUED FROM EXHAUST. *S/D* FRONT COMPRESSOR BEARING FAILED. COMPRESSOR IMPELLER RUBBED HOUSING, FRONT SEAL DESTROYED CAUSING CONDITION. METAL WAS FOUND IN GEARBOX FILTER SCREEN. 2 L 7 3 4F 4 F A3WE E2EA 1999123100147 20001016 00147 NM 2000 10 16 99UAL900650 1 19991215 A 2421 CONNECTOR BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 1 PYLON DAMAGED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 163UA 1006 21353 689531 STRONG SMELL OF SMOKE AT CLIMB AT 23000, MOMENTARY FLAGS ON EPR AND FUEL FLOW GAUGE. NR 1 GEN FIELD LIGHT ON-SAI TOPPED . AFTER RESET APPEARED NORMAL. *S/D* SMOKE SMELL WAS CAUSED BY EXCESSIVE VOLTAGE (~100 VDC) APPLIED TO THE BRIDGE CIR CUIT OF THE NR 1 CSD TEMP INDICATOR. HIGH VOLTAGE WAS CAUSED BY AN INTERNAL SHORT IN THE D11J FIREWALL DISCONNECT ELECT RICAL CONNECTOR. THE CONNECTOR INSULATION WAS DETERIORATED, PROBABLY BY ENGINE OIL. THE INSULATION DAMAGE CAUSED PINS 20, 21 AND 8 TO SHORT TOGETHER. SIGNAL FROM THE CSD TO THE OIL TEMP INDICATOR. SHORTING CAUSED EXCITER POWER TO BE APP LIED TO THE TEMP INDICATOR COIL, WHICH BURNED. SHORT ALSO CAUSED THE GENERATOR TO TRIP OFF-LINE. REPLACED THE D11J CON 2 L 7 4 4F 4 F A20WE E20EA 2000101600427 20001016 00427 2000 10 16 99UAL900667 4 19991225 A 2200 AFCS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 766UA 26917 REJECTED TAKEOFF AT 135 KIAS. RETURNED TO GATE. *S/D* ENGINEERING AND OPERATIONS ANALYSIS HAS CONCLUDED THAT THE AIRC RAFT SYSTEMS WERE OPERATING WITHIN NORMAL PARAMETERS AS THE AIRCRAFT WAS CONFIGURED DURING THE TAKEOFF ROLL. CONTROL FO RCES WITH THE AUTO-PILOT ENGAGED WILL BE SIGNIFICANTLY GREATER THAN FORCES NORMALLY ENCOUNTERED BY THE CREW WITH THE AUT O-PILOT DISENGAGED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2000101600428 20001016 00428 NM 2000 10 16 99UAL900668 1 19991218 A 2760 65B08099 SUPPORT BRACKET BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE SPOILER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 163UA 82898 21353 DURING TROUBLESHOOTING OF THE GROUND SPOILER CABLES, MAINTENANCE FOUND THE RIGHT GROUND (INBOARD) SPOILER SUPPORT FITTIN G ASSEMBLY, (P/N 65B08099-6), DAMAGE AT THE MOST INBOARD CLEVIS LUG. APPROXIMATELY 60 PERCENT OF THE LUG WAS FOUND MISS ING. *S/D* REPLACED RIGHT GROUND SPOILER SUPPORT ASSEMBLY, (P/N 65B08099-6). 2 L 7 4 4F 4 F A20WE E20EA 2000101600429 20001016 00429 NM 2000 10 16 99UAL900669 1 19991226 A 3840 42HY3314483 SWITCH BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE POTABLE WATER FAILED A UALA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 794UA 26953 AFTER TAKEOFF FROM CDG UNABLE TO GET WATER PRESSURE TO GALLEYS OR LAVS. DUMPED FUEL AND DIVERTED TO LHR. *S/D* CAUSE WAS DETERMINED TO BE THE QUANTITY/PRESELECT SWITCH (P/N: 42HY331448-3) NOT BEING IN THE OFF/RESET POSITION. THIS CAUSED THE PRESELECT OVERFLOW FILL VALVE TO REMAIN OPEN CAUSING PRESSURE TO BE VENTED OVERBOARD. THE CONDITION WAS CORRECTED BY RESETTING THE QUANTITY PRESELECT SWITCH. 2 L 7 2 4F 4 F RT T0001SE E46NE 2000101600430 20001016 00430 NM 2000 10 16 99UAL900672 1 19991222 A 2760 B435413 PCU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AILERONS FAILED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 774UA 16267 26936 RIGHT OUTBORAD SPOILER (NR 14) IN THE DEPLOYED POSITION. AILERONS REQUIRE ONE UNIT OF TRIM. *S/D* MAINTENANCE MESSAGE 27-11513 SPOILER PCU NR 14 POSTION TRANSDUCER HAS FEEDBACK FAULT WAS ACTIVE. SPOILER PCU NR 14 (P/N: B43541-3) WAS RE PLACED AND TESTED PER AMM 27-61-08. SUSPECT A FAILURE OF THE POSITION TRANSDUCER LVDT AND POTTING COMPOUND. THIS IS A SUBJECT OF A VENDER SERVICE BULLETIN AND THE MODFICATION WILL BE ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2000101600431 20001016 00431 WP 2000 10 16 99UAL900674 1 19991218 A 5330 SKIN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1829U 46628 DURING MAINTENANCE, THE FWD RT SIDE OF THE PRESSURE BULKHEAD AND FUSELAGE SKIN AT STA 275 WAS DAMAGED DUE TO AN IMPACT W ITH AN A320 WHICH WAS BEING TOWED INTO THE HANGAR. *S/D* DAMAGED AREA WAS REPAIRED PER APPLICABLE SRM. 2 L 7 3 4F 4 F A22WE E23EA 2000101600432 20001016 00432 2000 10 16 99UAL900675 4 19991008 A 2330 285W01293 CONTROL PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN FAILED A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 789UA 26935 FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN VICINITY OF DOOR 2 LEFT. FOUND CACP (CABIN AREA CONTROL PANEL) SCREEN BL ANKED OUT. PULLED CIRCUIT BREAKER D9 ON P210 PANEL TO REMOVE ELECTRICAL POWER SUPPLY TO PANEL. *S/D* INSTALLED NEW CA CP (P/N: 285W0129-3) TOUCHSCREEN SCREEN. NO EVIDENCE OF AIRCRAFT ELECTRICAL SYSTEM PROBLEMS. AIRCRAFT RETURNED TO SER VICE WITH NO FURTHER DIFFICULTIES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2000101600433 20001016 00433 2000 10 16 99UAL900676 4 19990918 A 2330 285W00123 CONTROL PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 793UA 26946 REPORT OF ODOR IN AREA OF DOOR 4 RIGHT. FOUND CACP (CABIN AREA CONTROL PANEL) AT DOOR 4 RIGHT BURNED OUT. PULLED CIRCU IT BREAKER TO REMOVE POWER SUPPLY TO PANEL. *S/D* INSTALLED NEW CACP SCREEN (P/N: 285W0012-3). NO EVIDENCE OF AIRCRAF T ELECTRICAL SYSTEM PROBLEMS. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER DIFFICULTIES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2000101600434 20001016 00434 NM 2000 10 16 99UAL900677 1 19991225 A 2750 PUSHROD BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE TE FLAPS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 158UA 83415 21054 HNL MAINTENANCE FOUND THE LEFT I/B MIDFLAP TRAVELED OUTBOARD AND STRUCK THE I/B AILERON. INSPECTION FOUND THESE PARTS B ROKEN: 65B15635-1 CRANK, 65B15651-7 PUSH ROD, 65B15651-4 PUSH ROD, AND 65B39351-3 FTG ITEMS (1) & (2) WERE NEAR THE NR 4 FLAP TRACK; WHILE ITEMS (3) & (4) WERE NEAR THE NR 3 FLAP TRACK. THE RESPECTIVE FLAP TRACK CANOE FAIRINGS WERE SEVERE LY DAMAGE. *S/D* FAILURE OF ITEM (1), 65B15635-1 CRANK, MAY HAVE CAUSE THE OTHER COMPONENT''S FAILURE. REPAIRS WERE A CCOMPLISHED ON THE INBOARD AILERON, THE INBOARD MID AND AFT FLAPS, AND THE FLAP TRACK CANOE FAIRINGS. THE BROKEN PARTS, ITEMS WERE ALL REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 2000101900057 20001019 00057 NE 2000 10 19 EISA99252 2 19991207 A 7261 657566 ENGINE BOEING 727 7272A7 138407K NM PWA JT8 JT8D* NE NR 3 LACK OF LUBE A EISA E ENGINE SHUTDOWN W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 310NE 20241 NR 3 ENGINE SHUT DOWN DUE TO LOW OIL QUANTITY, AND LOW OIL PRESSURE. ENGINE WINDMILLED BELOW TEN PSI OIL PRESSURE FOR O NE HOUR AND TEN MINUTES. (M) 2 L 7 3 4F 4 F A3WE E2EA 2000121200070 20001212 00070 EA 2000 12 12 20001212AP012 1 19990816 A 5310 6003303025 WINDSHIELD CNDAIR CL600 CL6001A11 1900302 EA COCKPIT CRACKED A EXOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 17 63HJ 1021 TAKEOFF FROM PUEBLO, COLORADO WAS NORMAL. AFTER 1:45 OF FLIGHT, A CRACK APPEARED ON THE LEFT WINDSHIELD. THE LEFT WIND SHIELD HEAT C/B WAS MANUALLY SWITCHED OFF; WEATHER WAS CAVU TO FXE. (M) 2 L 7 2 4F RT A21EA 2000122900010 20001229 00010 SO 2000 12 29 SIMA3646 1 19991218 A 3230 7455501 CONTROLLER EMB 145 EMB145LR SO COCKPIT FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 614AE 145086 ORD - FLT 4017 - AFTER TAKEOFF, CREW GOT A LANDING GEAR LEVER DISAGREE MESSAGE ON THE EICAS. GEAR WAS RECYCLED AND GOT THREE GREENS. AIRCRAFT RETURNED TO ORD WITHOUT FURTHER INCIDENTS. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. OP S CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 2000122900011 20001229 00011 SO 2000 12 29 SIMA3621 1 19991224 A 3200 CONNECTOR EMB 145 EMB145 SO MLG CONTAMINATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 611AE 145074 MSN - FLT 9120 - DURING TAKEOFF, RIGHT LANDING GEAR DID NOT SHOW UP AND LOCKED. CREW FOLLOW QRC PROCEDURES, PROBLEM STI LL PERSIST. CREW RETURNED TO MSN SAFELY. FOUND DE-ICER FLUID HAD BEEN SPRAYED ON LANDING GEAR AREA. CLEANED CANNON PL UG AND CONTACTS ON PROXIMITY SWITCHES. SWUNG GEAR, OPS CHECK GOOD. (M) 2 L 7 2 4F RT T00011AT 2001011104010 20010111 04010 NM 2001 1 11 CA000118046 1 19991221 A 2910 506848474 TUBE BOEING 720 720023B 1383841 NM PWA JT3D JT3D3B 52039 NE HYD SYSTEM WORN W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 668461 (CAN) DURING FLIGHT CREW ACTIVATED GEARDOWN AND FLAPS DOWN FOR TEST, NOTHING MOVED, FE NOTICED HYD RESEVOIR WAS EMPTY, E MER DECLARED, LG MANUALLY LOWERED AND AUX PUMP USED FOR LANDING. HYD RETURN LINE ON NO 2 ENG UNDER LH WING SAIL BOAT FAR ING HAD A HOLE IN THE TUBE CAUSED BY BROKEN P CLAMP AND THE LINE CHAFFED AGAINST BULKHEAD HOLDING P CLAMP. REPAIRED. 2 L 7 4 4F 4 F 4A28 1E8 2001011104059 20010111 04059 NM 2001 1 11 CA000209038 1 19991229 A 2530 3412131 CHILLER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE LT & RT FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA P709673 (CAN) ON PREFLIGHT SMOKE COMING FROM REAR GALLEY AND BEGAN TO FILL CABIN PASS DEPLANED. DEACTIVATED BOTH CHILLERS AND RE PLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001011105687 20010111 05687 WP 2001 1 11 ASAA9980068 1 19990323 A 5610 HINGE PIN DOUG DC9 DC983 3022083 WP COCKPIT WINDOW LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 LAX - AFTER ARRIVAL OF FLT 290, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED AND SECURED HINGE PIN ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011105667 20010111 05667 WP 2001 1 11 ASAA9980050 1 19990223 A 5610 HINGE PIN DOUG DC9 DC983 3022083 WP COCKPIT WINDOW DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 964AS 53078 SEA - AFTER ARRIVAL OF FLIGHT 472, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDO W AFT HINGE PIN MIGRATING OUT, REINSTALLED HINGE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011105669 20010111 05669 WP 2001 1 11 ASAA9980053 1 19990226 A 5610 HINGE PIN DOUG DC9 DC983 3022083 WP COCKPIT WINDOW LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 PDX - AFTER ARRIVAL OF FLT 317, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW OPERATING MECHANISM DETACHED. FOUND WINDOW LOWER AFT HINGE PIN MIGRATING OUT. REINSTALLED HINGE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011105671 20010111 05671 WP 2001 1 11 ASAA9980055 1 19990228 A 5610 HINGE PIN DOUG DC9 DC983 3022083 WP COCKPIT WINDOW LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 963AS 53077 PDX - PRIOR TO DEPARTURE OF FLT 95, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW OPERATING MECHANISM DETACH ED. FOUND WINDOW LOWER AFT HINGE PIN MIGRATING OUT. REINSTALLED HINGE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011105684 20010111 05684 WP 2001 1 11 ASAA9980060 1 19990309 A 5610 BOLT DOUG DC9 DC983 3022083 WP COCKPIT WINDOW LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 53022 SJD - PRIOR TO DEPARTURE OF FLT 231 - CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. SECURED LOOSE BOLT ON WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011105686 20010111 05686 WP 2001 1 11 ASAA9980067 1 19990322 A 5210 LATCH DOUG DC9 DC982 3022082 WP PAX DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 SEA - AFTER ARRIVAL OF FLT 361, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. LUBRICATED DOOR OPERATING MECHANISM AN D OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 2001011105666 20010111 05666 WP 2001 1 11 ASAA9980041 1 19990212 A 5610 LATCH DOUG DC9 DC983 3022083 WP COCKPIT WINDOW BINDING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 ANC - AFTER ARRIVAL OF FLT 90, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOLD NOT OPEN. LUBRICATED UPPE R WINDOW LATCH MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011105665 20010111 05665 WP 2001 1 11 ASAA9980038 1 19990209 A 5210 BEARING DOUG DC9 DC983 3022083 WP PAX DOOR BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 981AS 53472 ANC - DURING GROUND SERVICING, THE L2 DOOR WOULD NOT OPEN. FOUND DOOR LOWER SNUBBER BEARING AT FUSELAGE ATTACHMENT BROK EN. REPLACED BEARING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011105664 20010111 05664 WP 2001 1 11 ASAA9980037 1 19990209 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 LCQ - DURING 15K CHECK, DENT WAS FOUND IN FUSELAGE SKIN AT FS 229. REPAIRED IAW ASA EA 5330-01363. (M) 2 L 7 2 4F A6WE 2001011105670 20010111 05670 WP 2001 1 11 ASAA9980054 1 19990228 A 5610 29190701 SPRING DOUG DC9 DC983 3022083 WP COCPIT WINDOW DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 PDX - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW LOWER AFT LOCKING SPRING WAS FOUND DAMAGED. REPLACED THE SPRING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 2001011601234 20010116 01234 EU 2001 1 16 20000714SH002 1 19990224 A 2740 SWITCH FOKKER F28 F28MK4000 4990810 EU HYD SYSTEM STUCK G QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 05 479AU 11228 PILOT REPORTED STABILIZER HYDRAULIC LIGHT ILLUMINATED. TROUBLESHOOTING REVEALED THE STABILIZER ''STICKING SWITCH'' WAS FAULTY. (X) 2 L 7 2 4F RT A20EU 2001011601351 20010116 01351 EU 2001 1 16 20001113SH023 1 19990703 A 2913 887673 PUMP AIRBUS 310 A310324 3930206 EU HYDRAULIC SYSTEM OVERHEATED A AJLF O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 23 841AB 13949 13736 686 DURING CRUISE, YELLOW HYD PUMP LOW PRESS LIGHT ILLUMINATED WITH ECAM WARNING. 10 MINUTES LATER, YELLOW HYD RESERVOIR LO W LIGHT ILLUMINATED. REPORT FOR HYD PUMP REVEALED PUMP OVERHEATED, INTERNAL PARTS DAMAGED. SKYDROL BURNED INSIDE PUMP SCRAPPED. 2 L 7 2 4F RT A35EU 2001011601360 20010116 01360 EU 2001 1 16 20001114SH001 1 19990320 A 2913 887673 PUMP AIRBUS 310 A310325 EU HYDRAULIC SYSTEM OVERHEATED A AJLF O OTHER M OVER TEMP NR NOT REPORTED 1 SO 23 835AB 18459 18234 650 EN ROUTE, PILOT HAD A YELLOW HYD SYS LOW PRESSURE. SYS TURNED OFF REMAINDER OF FLIGHT. INVEST FOR HYD PUMP, FOUND PUMP OVERHEATED, INTERNAL PARTS DAMAGED. SKYDROL BURNED INSIDE PUMP, CREATING DEPOSITS. CLEANING IMPOSSIBLE. PUMP SWAPPED . ENG ANALYSIS OF FLUID REVEALED NO CHEMICAL CONTAMINATION. 2 L 7 2 4F RT A35EU 2001011601361 20010116 01361 EU 2001 1 16 20001114SH003 1 19990826 A 3150 WARNING SYSTEM AIRBUS 320 A320214 EU NR 1 & 2 ECAM MALFUNCTIONED A AJLF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 23 630AJ 5552 5399 630 FLT JM 090 - DURING CLIMB, ECAM SHOWED ''FLIGHT CONTROL ALTERNATE LAW''. ECAM PROCEDURE PERFORMED, AIRCRAFT LANDED. AF TER LANDING, SEC NR 1 AND NR 3 AND ADIRU NR 1 AND NR 3 WERE INTERCHANGED, BUT NIL FIX. THE AIRCRAFT WAS DE-POWERED AND THE WARNING DISAPPEARED AFTER POWER-UP. AIRCRAFT WAS THEN DISPATCHED. (X) 2 L 7 2 4F RT A28NM 2001011601362 20010116 01362 EU 2001 1 16 20001114SH004 1 19990829 A 2913 887673 PUMP AIRBUS 310 A310324 3930206 EU HYDRAULIC SYSTEM OVERHEATED A AJLF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 23 841AB 14332 14091 686 JFK/KIN - FLT JM 016 - NR 2 ENGINE YELLOW HYD PUMPS OVERHEAT WARNING CAME ON 2.50 HRS INTO FLIGHT. REPORT FROM O/H AGEN CY REVEALED THE PUMP WAS BURNT. QUANTITY TRANSMITTERS INSTALLED ON THIS ACFT WERE FOUND TO BE MODIFIED PER TFU 29.31.00 .002. REGARDING CHAFING WIRES TO SHUTOFF VALVE, ONCE ONLY INSP A310/052 ISSUED. WIRES TO ALL VALVES ON THIS ACFT CHECK ED, FOUND MINOR NICKS ON OUTERMOST INSULATIONS. ALL NICKS RECTIFIED. REF: TFU 24.92-00-018. (X) 2 L 7 2 4F RT A35EU 2001011601363 20010116 01363 EU 2001 1 16 20001114SH023 1 19991117 A 7500 THERMOSTAT AIRBUS 320 A320214 EU CFMINT CFM56 CFM565B4P NE BLEED AIR SYSTEM MALFUNCTIONED A AJLF A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 23 624AJ 7676 7320 624 MBJ/LAX - FLT JM 055 - DURING CLIMB-OUT, NR 1 BLEED TRIPPED DUE TO HIGH TEMPERATURE. MAINT DISCOVERED BOTH TEMP CONTROL THERMOSTATS (TCT) HAD BEEN THE CAUSE OF ERRONEOUS INDICATIONS AND LOSS OF BLEED SYSTEMS. TCT HAD BEEN SUBJECT OF A TFU REF 36.11.43.005. PROBLEMS ARE STILL BEING EXPERIENCED WITH MODIFIED UNITS ISSUED BY VENDOR. AIR JAMAICA HAS FITTED M ODIFIED UNITS TO RECTIFY THIS DEFECT AND WILL BE FITTING IMPROVED UNITS TO ALL AIRCRAFT WHEN THEY BECOME AVAILABLE FROM THE VENDOR. (X) 2 L 7 2 4F 4 F RT A28NM E38NE 2001011601365 20010116 01365 EU 2001 1 16 20001114SH005 1 19990919 A 2913 887673 PUMP AIRBUS 310 A310324 3930206 EU HYDRAULIC SYSTEM FAILED A AJLF O OTHER J WARNING INDICATION DE DESCENT 1 SO 23 840AB 15052 14822 682 ON DESCENT, CREW REPORTED A YELLOW SYS LOW PRESSURE, ECAM CHECKLIST CARRIED OUT. DURING GROUND RUN OF NR 2 ENG, FOUND A LL FILTERS WITH INDICATION OF BEING CLOGGED. CASE DRAIN FILTER HAD METAL PARTICLES. PUMP, FILTERS REPLACED, SYS SERVIC ED. STRIP REPORT FROM REPAIR AGENCY INDICATED THE FAILIURE WAS CAUSED BY NORMAL WEAR AND WAS NOT INFLUENCED BY ANY EXTE RNAL FAILURE. (X) 2 L 7 2 4F RT A35EU 2001011601366 20010116 01366 WP 2001 1 16 20001114SH006 1 19991017 A 2913 A56641115666 PUMP DOUG DC9 DC983 3022083 WP HYD SYSTEM FAILED A AJLF O OTHER J WARNING INDICATION CL CLIMB 1 SO 23 191AJ 7558 7446 53191 ATL/MBJ - FLT JM 056 - AFTER TAKEOFF, RIGHT HYDRAULIC PRESSURE LOW INDICATION CAME ON WITH RUDDER CONTROL MANUAL LIGHT O N. FLIGHT CREW ACCOMPLISHED PROCEDURE PER CHECKLIST. RIGHT PRESSURE INDICATION ZERO. MAINT FOUND RIGHT ENGINE DRIVEN PUMP UNSERVICEABLE. PUMP WAS REPLACED AND A LEAK CHECK CARRIED OUT. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A6WE 2001011601379 20010116 01379 WP 2001 1 16 20001114SH014 1 19991007 A 3500 980871194P005005 SWITCH DOUG DC9 DC983 3022083 WP PAX OXYGEN MASKS FAILED A AJLF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 23 192AJ 6691 6456 53192 MBJ/ORD - FLT JM 051 - OXYGEN MASKS DEPLOYED PRIOR TO TAXI FROM GATE. ANEROID SWITCH FOUND AT FAULT, IT WAS REPLACED AN D OPERATIONAL CHECKED OKAY. AIRCRAFT WAS THEN RETURNED TO SERVICE. LANDINGS: 3,661. (X) 2 L 7 2 4F RT A6WE 2001011601380 20010116 01380 WP 2001 1 16 20001114SH015 1 19990929 A 3500 OXYGEN MASK DOUG DC9 DC983 3022083 WP CABIN DEPLOYED A AJLF O OTHER O OTHER CL CLIMB 1 SO 23 192AJ 6627 6456 53192 ORD/MBJ - FLT JM 050 - FLIGHT CREW REPORTED THAT AFTER INITIAL CLIMB-OUT IN ICING AND MODERATE TURBULENCE, AIRCRAFT WAS IN CRUISE AT 11,000 FEET FOR AN EXTENDED PERIOD. AFTER BEING CLEARED TO FL 230, ON PASSING THROUGH 15,000 FEET, THE PUR SER REPORTED TO THE CAPTAIN THAT ALL CABIN OXYGEN MASKS HAD DEPLOYED. RAPID DECOMPRESSION CHECKLIST ACCOMPLISHED, PRESS URIZATION RETURNED TO NORMAL. AIRCRAFT OPERATED OK IN MANUAL MODE. AT A LOWER ALTITUDE, AIRCRAFT RETURNED TO AUTO MODE AND FLIGHT CONTINUED. ON LANDING, MAINT CARRIED OUT RELEVANT GROUND CHECKS IN AUTO AND MANUAL MODES, THESE CHECKED SER VICEABLE. A NUMBER OF OXYGEN GENERATORS WERE USED. AIRCRAFT RETURNED TO SERVICE UNDER THE APPROPRIATE MEL. (X) 2 L 7 2 4F RT A6WE 2001011601381 20010116 01381 WP 2001 1 16 20001114SH016 1 19991020 A 2410 696233 CSD DOUG DC9 DC983 3022083 WP NR 1 ENGINE OVERHEATED A AJLF A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SO 23 192AJ 6785 6547 53192 MBJ/ATL - FLT JM 053 - DURING FLIGHT, NR 1 ENGINE CSD OIL TEMPERATURE WENT HIGH. THE CSD WAS DISCONNECTED AND THE AIRC RAFT DIVERTED TO MIAMI. THE CSD WAS THEN INSPECTED, BUT NO DEFECT FOUND. AIRCRAFT DISPATCHED PER MEL. AFTER ARRIVAL I N ATLANTA, THE CSD WAS SERVICED AND CHECKED, BUT THE FAULT DID NOT RECUR. (X) 2 L 7 2 4F RT A6WE 2001011601386 20010116 01386 EU 2001 1 16 20001114SH022 1 19991111 A 3260 ABS012110 SENSOR AIRBUS 320 A320214 EU MLG DIRTY A AJLF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 624AJ 7640 7320 624 MIA/KIN - FLT JM 020 - AIRCRAFT RETURNED TO MIAMI AFTER TAKEOFF DUE LANDING GEAR WOULD NOT RETRACT. ECAM REPORT SHOWED NLG PROXIMITY SENSORS 24GA, 25GA, AND LGCIU 1 AT FAULT. THE PROXIMITY SENSORS WERE FOUND COVERED WITH GREASE DURING INS PECTION; BOTH SENSORS WERE SUBSEQUENTLY CLEANED. AIRCRAFT WAS DEPOWERED AND LGCIU FAULT DISAPPEARED WHEN POWER RESTORED . BITE TEST OF LGCIU AND PROXIMITY DETECTORS 24GA AND 25GA TESTED OKAY. AIRCRAFT WAS THEN DISPATCHED. (X) 2 L 7 2 4F RT A28NM 2001011601387 20010116 01387 EU 2001 1 16 20001114SH025 1 19991014 A 3030 45150320 SENSOR AIRBUS 320 A320214 EU AOA HEAT FAILED A AJLF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 23 630AJ 5934 3986 630 UVP/JFK - FLT JM 093 - AFTER ENGINE START AND PUSH BACK, AOA SENSOR HEAT FAULT ON ECAM. AIRCRAFT RETURNED TO GATE AND S ENSOR CONFIRMED AT FAULT. AIRCRAFT DISPATCHED PER MEL. (X) 2 L 7 2 4F RT A28NM 2001011601388 20010116 01388 EU 2001 1 16 20001114SH026 1 19991015 A 2720 LIMIT SWITCH AIRBUS 320 A320214 EU RUDDER MALFUNCTIONED A AJLF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 23 628AJ 6472 6124 628 MIA/KIN - FLT JM 020 - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED A RUDDER TRAVEL LIMIT 2 LIGHT ON ECAM. DURING MAINTENAN CE INVESTIGATION, NR 2 RUDDER TRAVEL LIMITATION UNIT 4CC WAS FOUND TO BE AT FAULT. THE UNIT WAS CHANGED, THE SYSTEM WAS OPERATIONALLY CHECKED IAW MM 27-23-41-400-001 AND FOUND SERVICEABLE. (X) 2 L 7 2 4F RT A28NM 2001011601438 20010116 01438 EU 2001 1 16 20001115SH001 1 19991214 A 5210 SKIN AIRBUS 310 A310324 3930206 EU PAX DOOR PUNCTURED A AJLF K NONE O OTHER IN INSP/MAINT 1 SO 23 839AD 16563 16332 678 EWR/MBJ - FLT JM 018 - DURING WALK-AROUND INSPECTION OF AIRCRAFT, MAINTENANCE CREW DISCOVERED A SMALL PUNCTURE OF APPROX IMATELY ONE INCH IN DIAMETER ON THE OUTSIDE OF DOOR 3L. THE PUNCTURE WAS BETWEEN RIBS 6 AND 7. THE AIRCRAFT WAS FERRIE D TO EFFECT THE NECESSARY REPAIRS WHICH WERE CARRIED OUT IAW SRM 52-10-00. AIRCRAFT SUBSEQUENTLY RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A35EU 2001011601439 20010116 01439 EU 2001 1 16 20001115SH002 1 19991212 A 2913 887673 PUMP AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE HYDRAULIC SYSTEM LEAKING A AJLF O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 23 841AB 3582 686 KIN/MBJ - FLT JM 019 - AIRCRAFT LOST GREEN SYSTEM HYDRAULIC FLUID RESULTING IN MANUAL EXTENSION OF GEARS FOR LANDING. A FAILED PACKING WAS IDENTIFIED AS THE CAUSE. AFTER REPLACEMENT AND RE-SERVICING, AIRCRAFT WAS RETURNED TO SERVICE. NEX T FLIGHT, GREEN SYSTEM LOW LEVEL OCCURRED AFTER GEAR RETRACTION, RESULTED IN AIRCRAFT RETURNING. A LEAK CONFIRMED FROM THE NR 2 ENGINE GREEN SYSTEM ENGINE DRIVEN PUMP. THE AIRCRAFT HAS BEEN REMOVED PENDING PUMP REPLACEMENT. ALL GREEN SYS TEM HYDRAULIC PUMP CASE DRAIN FILTERS CHECKED FOR CONTAMINATION DUE SUSPECTED CAVITATION AND FOUND OK. PRESENTLY AWAITI NG STRIP REPORT AFTER REPAIR OF DAMAGED PUMP TO ESTABLISH REASON FOR FAILURE. (X) 2 L 7 2 4F RT A35EU E24NE 2001011601448 20010116 01448 EU 2001 1 16 20001115SH006 1 19991216 A 2913 6506606 PUMP AIRBUS 310 A310324 3930206 EU HYDRAULIC FAILED A AJLF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 23 841AB 14854 686 JFK/KIN - FLT JM 010 - GREEN PUMP LOW PRESSURE LIGHT CAME ON IN-FLIGHT, AND COULD NOT BE RECOVERED. GREEN PUMP, PN 6506 6-06, SN 273874, IS AN ABEX UNIT WHICH WAS INSTALLED ON 12-13-99. THIS WAS A LOANER UNIT AND INSTALLED UNDER THE AUTHOR ITY OF A ''NO TECHNICAL OBJECTION'', REF: 997.0554/99. THE APPROVED EDP FOR THIS AIRCRAFT IS MFG BY VICKERS WITH P/N 8 87673. AFTER RE-INSTALLATION OF CORRECT TYPE PUMP ON 12-17-99, THERE HAS SINCE BEEN NO REPORTED DISCREPANCY ON THIS SYS TEM. (X) 2 L 7 2 4F RT A35EU 2001011601452 20010116 01452 NE 2001 1 16 20001115SH007 2 19990921 A 7230 FAN BLADE AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE NR 2 ENGINE FOD A AJLF C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SO 23 840AB 14822 682 MBJ/EWR - FLT JM 2019 - ACFT EXPERIENCED HIGH VIBRATION ON THE N1 OF NR 2 ENG DURING INITIAL TAKEOFF ROLL. TAKEOFF DIS CONTINUED, ACFT RETURNED TO RAMP. NR 2 ENG SUFFERED FOD DAMAGES TO 2 FAN BLADES ON 9-16-99. AFTER ASSESSMENT AND APPLI CATION OF A310 MM 72-21-00, ACFT RELEASED FOR 50 FLT HRS DURING WHICH BLADES WOULD BE REPLACED. PRIOR TO DEPARTURE, DAM AGED FAN BLADES REPLACED. A310 MM 72-21-02-4 FOLLOWED, 2 BLADES REPLACED IN MATCHED PAIRS. PG 3 ALLOWS A 1.0 OUNCE IN CH MOMENT WEIGHT DIFFERENCE BETWEEN MATCHED PAIR OF BLADES, 1 PAIR HAD 1.0 OUNCE INCH DIFFERENCE, THE OTHER, 0.3 OUNCE INCH DIFFERENCE. WITH REQUIREMENTS OF MM MET, SUSPECT HEAVIER OF BOTH PRS OF BLADES INSTALLED ADJ CREATED IMBALANCE. 2 L 7 2 4F RT A35EU E24NE 2001011601454 20010116 01454 EU 2001 1 16 20001115SH009 1 19991109 A 2750 531B000007 PCU AIRBUS 310 A310324 3930206 EU TE FLAPS DEFECTIVE A AJLF O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 23 840AB 15360 15205 682 PHL/JFK - FLT JM 2016 - EN ROUTE, CREW REPORTED FLAP SYSTEM FAULT OCCURRED ON FLAP EXTENSION FROM 15 DEGREES AND INDICAT ION OF FLAP MOVEMENT STUCK. FLAP SYSTEM INSPECTION CARRIED OUT, NO FAULT FOUND. NR 1 SFCC REPLACED AND SYSTEM OPERATED SATISFACTORY. EN ROUTE, WHEN 20 DEGREES FLAP SELECTED, FLAP SYSTEMS 1 AND 2 FAULTED, BUT SYSTEM WAS UNABLE TO RESET. AIRCRAFT DIVERTED TO JFK. THE FLAP CONTROL UNIT VALVE BLOCKS WERE FOUND AT FAULT. THE COMPLETE FLAP CONTROL UNIT WAS R EPLACED AND THE SYSTEM CHECKED SATISFACTORY. A NON-REVENUE FLIGHT PERFORMED, NO DEFECT FOUND. (X) 2 L 7 2 4F RT A35EU 2001011601488 20010116 01488 EU 2001 1 16 20001115SH010 1 19991004 A 2913 88763 PUMP AIRBUS 310 A310324 3930206 EU HYDRAULIC OVERHEATED A AJLF O OTHER M J OVER TEMP WARNING INDICATION LD LANDING 1 SO 23 838AB 15579 15379 676 MBJ/JFK - FLT JM 011 - DURING LANDING GEAR RETRACTION AFTER TAKEOFF, FLIGHT CREW REPORTED FAULT LIGHT ON NR 2 ENGINE GRE EN HYDRAULIC PUMP. RESERVOIR QUANTITY INCREASED AFTER TAKEOFF AND REQUIRED CREW ACTION. INVESTIGATION REVEALED HYDRAUL IC PUMP FAILURE AND HYDRAULIC FIRE SHUT-OFF VALVE PARTIAL CLOSURE DUE TO WIRING DAMAGE. HYDRAULIC PUMP REPLACED. WIRIN G REPAIRED AND AIRCRAFT DISPATCHED. (X) 2 L 7 2 4F RT A35EU 2001013000009 20010130 00009 CE 2001 1 30 20000523SH018 1 19991207 A 3234 CONTROL HANDLE RAYTHN DH125 HAWKER800XP CE CABIN OBSTRUCTED H O OTHER O OTHER AP APPROACH 1 SW 11 833QS 258433 DURING APPROACH, ATTEMPTED TO MOVE LANDING GEAR SELECTOR HANDLE TO DOWN POSITION, BUT COULD ONLY GET APPROXIMATELY 2/3 TRAVEL DOWN. CYCLED HANDLE AGAIN WITH SAME RESULT. APPROACH ABANDONED. CHECK LIST PROCEDURES WERE FOLLOWED FOR MANUA L EXTENSION. FOLLOWING EMERGENCY DECLARATION, REQUESTED A FLY-BY, A REVIEW OF ALL NORMAL AND EMERG LANDING PROCEDURES W AS CONDUCTED, A FLAT APPROACH WITH FULL FLAPS AND VREF SPEED WAS MADE. UPON TOUCH-DOWN, ROLLED TO STOP, SHUT DOWN LT EN GINE. MAINTENANCE FOUND SCREW (PN A116-2B) LODGED UNDER A LEVER ARM (PN 25-CX-1355) RESTRICTING TRAVEL OF THE ARM. AF TER REMOVING SCREW, WERE ABLE TO LOWER HANDLE ALL THE WAY DOWN. (X) 2 L 7 2 4F RT A3EU 2001020500021 20010205 00021 NM 2001 2 5 20000712SH039 1 19990728 A 2120 B193334 ELEMENT BOEING 747 747400 NM OZONE CONVERTER SEPARATED H K NONE O OTHER NR NOT REPORTED 1 SO 09 OZONE CONVERTER, SN 5039, RETURNED FOR REPAIR. CATALYST ELEMENT (THERMAL SPRAYED FOIL) FOR CLASS III COMPONENT SEPARATE D FROM WELDED INTERNAL SUB-ASSY AND WAS DRAWN INTO ACFT A/C SYS CAUSING DAMAGE TO 2 ACFT PNEUMATIC DUCTS AND DISCONNECTS . THIS CONVERTER WAS 1 OF 70 MFG BETWEEN 5-11, 1995. (X) 2 L 7 4 4F RT A20WE 2001020500031 20010205 00031 NE 2001 2 5 20000713SH004 2 19990726 A 7200 ENGINE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAYMK6118 NE RT ENGINE VIBRATION B BTVR O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 1SL 1167 16442 DURING CLIMB-OUT FROM KUGN AT 10,000 MSL, THE CREW NOTICED SUDDEN, HIGH VIBRATIONS FROM THE RIGHT ENGINE. REDUCING POWE R PUT VIBRATIONS AT AN ACCEPTABLE LEVEL. ALL TROUBLESHOOTING PER THE TAY MM PROVED NEGATIVE AS TO A DEFINITIVE CAUSE OF THE VIBRATIONS. THE ENGINE WAS REJECTED BASED ON THE VIBRATION LEVELS AND SENT TO A REPAIR FACILITY FOR EVALUATION. ( X) 2 L 7 2 4F 4 F RT A12EA A25NE 2001020500097 20010205 00097 2001 2 5 20000623SH008 4 19991222 A 3452 75100700901 TRANSPONDER AMD FALC20 FALCON200 2730150 EU COCKPIT UNSECURE B K NONE O OTHER IN INSP/MAINT 1 SW 99 999TH 512 DURING ACCOMPLISHMENT OF FAR 91.413 AND AD 99-23-22R1, FOUND THAT MODES S WOULD NOT TRANSMIT TAIL NUMBER DURING TEST. F URTHER INVESTIGATION REVEALED THAT BOTH CONFIGURATION MODULES WERE NOT STRAPPED PROPERLY W9-W32 WERE ALL BINARY ZEROS. (X) 2 L 7 2 4F RT A7EU 2001020600066 20010206 00066 CE 2001 2 6 20000713SH013 1 19990113 A 7830 62184165 DIODE CESSNA 650 650 2076802 CE CIRCUIT BOARD OPEN C K NONE O OTHER NR NOT REPORTED 1 EA 21 2606 3630 6500194 RIGHT THRUST REVERSER WOULD NOT STOW IN NORMAL OR EMERGENCY RE-STOW. FOUND NO POWER TO ISOLATION VALVE WHEN STOW WAS CO MMANDED IN NORMAL OR EMERGENCY STOW. FOUND DIODE D91 OPEN ON PC BOARD 62184165. SUBMITTER RECOMMENDED MAKING THE EMERG ENCY STOW A FULLY REDUNDANT CIRCUIT. (X) 2 L 7 2 4F A9NM 2001020600069 20010206 00069 NM 2001 2 6 20000713SH027 1 19990630 A 2120 D193334 DUCT BOEING 747 74745E 1384947 NM A/C BAY DAMAGED H A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 03 409EV 28097 AFTER TAKEOFF, CAPTAIN REPORTED BLEED DUCT LEAK C. BLEED DUCT LEAK L AND PACK 1 MESSAGE SHOWN. AIRCRAFT AIR TURN-BACK. GROUND MAINTENANCE FOUND PACK 1 CATALYTER OZONE CONVERTER AND TUBE DAMAGED. (X) 2 L 7 4 4F RT A20WE 2001020600070 20010206 00070 GL 2001 2 6 20000713SH028 2 19990312 A 7200 ENGINE BOEING 747 74745E 1384947 NM GE CF6 CF680C2* GL NR 1 ENGINE VIBRATION H A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 03 405EV 21974 27142 702891 PILOT FELT THE AIRCRAFT VIBRATION DURING CLIMB UP TO AROUND 30,000 FEET. FOUND HIGH VIBRATION ON THE NR 1 ENGINE, CAUSE D AIR RETURN AT TPE ON 3-11-99. MAINTENANCE PERFORMED CONDITION CHECK OF ONE ENGINE FAN INLET. EXHAUST OUTLET AND MCD, BSI FOR HPC. HPT AND LPT AS REQUIRED. RESULTS OF INSPECTION ARE NORMAL. (X) 2 L 7 4 4F 4 F RT A20WE E23EA 2001020600075 20010206 00075 CE 2001 2 6 20000714SH003 1 19990428 A 2910 2407003466 HYDRAULIC LINE LEAR 25 25D 5170514 CE HYDRALIC SYSTEM CHAFED B FEHR O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 19 531CW 231 THE LEFT ENGINE HYDRAULIC LINE RUPTURED DUE TO WEAR AGAINST ANOTHER HYDRAULIC LINE''S FITTINGS. THE LINE IS LOCATED AT THE AFT PRESSURE BULKHEAD. SUBMITTER STATED IT IS IMPORTANT TO KNOW THAT THE POINT OF ''RUBBING'' IS DIFFICULT TO INSPE CT. THE RUPTURE OF THE LINE ALLOWED SYSTEM FLUID TO DEPLETE RESULTING IN LOSS OF SYSTEM PRESSURE. (X) 2 L 7 2 4J A10CE 2001020600076 20010206 00076 NM 2001 2 6 20000714SH010 1 19990510 A 2932 211C223297 PRESSURE SWITCH BOEING 767 7673T7 1385201 NM NR 1 PYLON FAILED H A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 03 601EV 25076 DURING CRUISE, ''RUDDER RATIO, L-HYD SYS PRESS'' MESSAGE SHOWN ON EICAS AND L-DEMAND PUMP LOW PRESSURE LIGHT ON. AIRCRA FT AIR TURN-BACK AT CKS APIRPORT. GROUND CHECK FOUND L-HYD SYSTEM PRESSURE SWITCH FAILED. REPLACED L-HYD SYSTEM PRESSU RE SWITCH AND GROUND OPER CHK CONDITION IS NORMAL. (X) 2 L 7 2 4F RT A1NM 2001020800967 20010208 00967 EU 2001 2 8 20000731SH023 1 19990831 A 5330 SKIN AMD FALC50 FALCON900 2700160 EU FUSELAGE CORRODED A QU2R K NONE O OTHER IN INSP/MAINT 1 EA 17 612BH 122 ILG - AIRCRAFT ARRIVED WITH AERODYNAMIC CORE FILL SMOOTHER FOR RIGHT SATCOM ANTENNA, PN 1333-200-200, MISSING. REMAININ G FILLER REMOVED, FOUND EXTENSIVE CORROSION ON FUSELAGE SKIN, RIGHT SIDE BETWEEN FUSELAGE FRAMES 7 AND 8. AFTER REMOVIN G ANTENNA, SAME P/N, FROM LEFT SIDE AND REMOVING FILLER, FOUND SAME CONDITION. (X) 2 L 7 3 4F RT A46EU 2001021600002 20010216 00002 NM 2001 2 16 20000717SH019 1 19990107 A 7930 CHIP DETECTOR AMD FALC50 FALCON2000 2730170 NM GARRTT TFE731 TFE73131C 01518 NE NR 1 ENGINE CONTAMINATED C A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 25 96LT 4762 72 P76658 TWENTY MINUTES AFTER TAKEOFF, CREW WAS ALERTED BY A NR 1 ENGINE ''OIL'' LIGHT ON MASTER CAUTION PANEL. OIL PRESSURE WAS NORMAL. AIRCRAFT RETURNED TO HOME BASE (MMU). ENGINE CHIP DETECTOR INSPECTION REVEALED A CHIP ABOUT .1250 INCH LONG. DRAINED OIL FROM GEARBOX AND FOUND CHIPS IN OIL. SOAP SAMPLE TAKEN, FOUND NORMAL. CHIPS ANALYSED AND FOUND COMING FROM AIRFOIL SEPARATOR. SEPARATOR REPLACED. (X) 2 K 7 3 4F 4 F RT A50NM E6WE 2001021600004 20010216 00004 EU 2001 2 16 20000731SH022 1 19990721 A 3246 L305649 BEARING ISRAEL 1124 1124 4500102 EU GARRTT TFE731 TFE73131G 29003 NE RT MLG FAILED B XZAR K NONE O OTHER LD LANDING 1 EA 17 666K 130 OCT8242 321 RIGHT OUTBOARD MAIN WHEEL BEARING HAD CATASTROPHIC FAILURE ON LANDING ROLL-OUT JUST AS AIRCRAFT LEFT MAIN RUNWAY. INSPE CTION OF WHEEL REVEALED THE OUTBOARD BEARING (INBOARD TO ACFT) FAILED FOR UNKNOWN REASONS. DETAILS ARE ON FILE UNDER EL CORTA, INC., W/O 99223. (X) 2 M 7 2 4F 4 F A2SW E6WE 2001021600007 20010216 00007 WP 2001 2 16 20000808SH021 1 19991001 A 2740 BOLT CVAC 440 C131E 2422904 WP ELEVATOR TAB FAILED B VGSR K NONE O OTHER IN INSP/MAINT 1 CE 05 4753B 20660 554753 RIGHT ELEVATOR TAB PUSH/PULL ROD ATTACH BOLT FAILED CAUSING A VIBRATION THAT DAMAGED ELEVATOR AND TAB. THE PILOT MADE A SAFE EMERGENCY LANDING. (X) 2 L 7 2 4R 6A6 2001022000188 20010220 00188 SO 2001 2 20 20000830SH022 1 19991028 A 3242 1331096 STATOR BFGOODRICH EMB 120 EMB120 3260201 SO BRAKE ASSY CRACKED B XC4R K NONE O OTHER IN INSP/MAINT 1 SO 19 1491A BRAKE ASSY, P/N 2-1585, FAILED PREMATURELY. NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS. HEAT STAC K WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY A ND THE MOST BRAKE CONFIGURATION, P/N 2-1585. (X) 2 L 7 2 4T RT A31SO 2001022000189 20010220 00189 SO 2001 2 20 20000830SH023 1 19991026 A 3242 1331096 STATOR BFGOODRICH EMB 120 EMB120 3260201 SO BRAKE ASSY CRACKED B XC4R K NONE O OTHER IN INSP/MAINT 1 SO 19 0011 BRAKE ASSY, P/N 2-1585, FAILED PREMATURELY. NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATI ON, P/N 2-1585. (X) 2 L 7 2 4T RT A31SO 2001022000190 20010220 00190 SO 2001 2 20 20000830SH024 1 19991102 A 3242 1331096 STATOR BFGOODRICH EMB 120 EMB120 3260201 SO BRAKE ASSY BROKEN B XC4R K NONE O OTHER IN INSP/MAINT 1 SO 19 0639A BAKE ASSY, PN 2-1585, FAILED PREMATURELY. NR 1 STATOR BROKEN AND BINDING IN TORQUE TUBE KEY SLOTS. SUBMITTER STATED TH IS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2 -1585. (X) 2 L 7 2 4T RT A31SO 2001030100030 20010301 00030 WP 2001 3 1 20001101SH021 1 19991112 A 2422 INVERTER CVAC 340 34032 2422706 WP FWD FUSELAGE FAILED B A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 3427 90 AIRCRAFT WAS IN LEVEL CRUISE FLIGHT VFR PART 91. CREW NOTICED SMOKE IN CABIN/COCKPIT. EMERGENCY PROCEDURE INITIATED. AIRCRAFT LANDED WITHOU INCIDENT. OVERHAULED INVERTER INSTALLED. OPERATIONAL CHECK PERFORMED. AIRCRAFT RETURNED OT SER VICE. (X) 2 L 7 2 4R 6A6 2001030800088 20010308 00088 EA 2001 3 8 CA991209060 1 19991026 A 2910 AV16B2003D VALVE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL HYDRAULIC SYS FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA L26226 (CAN) WHILE TAXING FOR TAKE OFF NR1 HYD PUMP CAUTION LITE ILLUMINATED. THERE WAS NO LOSS OF FLUID SO A SHEARED PUMP WAS SUSPECTED.THE PUMP WAS EXAMINED AND FOUND SERVICEABLE.FURTHER INVESTIGATION REVEALED THE HYD SHUT-OFF VALVE IN THE CLOS ED POSITION, OPPOSITE OF WHAT SHOULD BE THE NORMAL CONFIGURATION. THE FIRE T HANDLE WAS PULLED AND THE VALVE DID NOT FUN CTION AS IT SHOULD HAVE. THE NR1 ENGINE HYD AND FUEL SHUT-OFF VALVE CIRCUIT BREAKER WAS FOUND POPPED.THE C/B WAS RESET AND THE VALVE CYCLED AGAIN BUT DID NOT FUNCTION PROPERLY. VALVE WAS REPLACED. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 2001030800089 20010308 00089 2001 3 8 CA991209070 4 19991118 A 3457 631135 SWITCH STACOSWITCH FRCHLD SA227 SA227CC SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE INSTRUMENT PANEL SHORTED W D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, THE CREW DETECTED A BURNING PLASTIC SMELL. THE CREW NOTICED THE ANNUNCIATOR PANEL GO ON AND OFF AS WE LL AS LOSING SOME INDICATORS. THE AIRCRAFT RETURNED TO BASE FOR MAINTENANCE. THE MAINTENANCE CREW DETERMINED THAT THE GP S/NAV SWITCH HAD SHORTED AND OVERHEATED. 2 L 7 2 4T 4 T RT A18SW E4WE 6 C 3PNE 2001030800090 20010308 00090 EA 2001 3 8 CA991209071 1 19991118 A 2731 C3CF4187 ROD DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE ELEVATOR TRIM WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION, IT WAS FOUND THAT THE PUSH PULL ROD FOR THE ELEVATOR TRIM TAB WAS SEVERELY WORN. THE WEAR SPOT OCCURRED WHERE THE PUSH PULL ROD RUNS THROUGH THE BULKHEAD AND CONTACTS THE ROLLERS WHICH IT RIDES ON. THE ROD WAS REMO VED AND INSPECTED-THE ROLLERS HAD WORN THROUGH THE ROD. THE ROD WAS INSPECTED. 1 H 7 1 3R 4 T A815 E4EA 2001030800091 20010308 00091 EA 2001 3 8 CA991209072 1 19991115 A 2730 MS20470AD516 RIVET C6CFM10963 DHAV DHC6 DHC6200 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL ELEV CONTROL ROD LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION OF THE ELEVATOR CONTROL SYSTEM, IT WAS NOTICED THAT THE PUSH PULL RIVETS WERE BLACK AND STAINED. THE PUSH PULL ROD WAS REMOVED FROM THE AIRCRAFT AND INSPECTED.AT THAT POINT WE DISCOVERED THAT THE RIVETS WERE LOOSE. T HE RIVETS WERE REMOVED, THE ROD DISASSEMBLED, RIVETED WITH NEW RIVETS AND REINSTALLED ON THE AIRCRAFT.IT SHOULD BE NOTED THAT IT IS A VERY DIFFICULT AREA TO INSPECT. FAILURE OF THE RIVETS COULD CAUSE SEPERATION OF THE ROD WHICH WOULD RESULT IN LOSS OF CONTROL OF THE ELEVATORS. 1 H 7 2 3T 4 T A9EA E4EA 6 C P15EA 2001030800092 20010308 00092 EA 2001 3 8 CA991209073 1 19991126 A 2720 VALC3CF1995R CONTROL CABLE DHAV DHC3 DHC3 2800202 EA PWA R1340 S3H1G 52016 NE RUDDER FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION OF THE RUDDER CABLES, WE FOUND A FLAT SPOT WITH A COUPLE OF BROKEN STRANDS. THE CABLE WAS REMOVE D FOR INSPECTION AND WAS FOUND SEVERLY FRAYED. CABLE WAS REPLACED. IT SHOULD BE NOTED THAT THIS PARTICULAR CABLE IS ONE OF THE NEW STAINLESS STEEL CABLES, AS OPPOSED TO THE ORIGINAL GALVINIZED TYPE CABLES WHICH WERE PREVIOUSLY USED. WE HAVE FOUND BECAUSE OF THEIR BRITTLENESS, DO NOT LAST NEAR AS LONG AND SUSPECT THIS CABLE WAS ONLY INSTALLED FOR 400-500 HOUR S. UNLIKE THE GALVINIZED CABLES, WHICH YOU FIND ONE OR TWO STRANDS BROKEN AND LITTLE DAMAGE UPON REMOVAL. THE SS CABLES SEEM TO HAVE 1-2 STRANDS BROKEN ON THE OUTSIDE BUT ARE SEVERELY DAMAGED INTERNALLY ONCE REMOVED AND INSPECTED. 1 H 7 1 3R 3 R A815 E142 2001030800093 20010308 00093 EA 2001 3 8 CA991209075 1 19991126 A 2750 FITTING C3CF1057 DHAV DHC3 DHC3 2800202 EA PWA R1340 S3H1G 52016 NE ROD END LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE CARRING OUT AN INDEPENDENT INSPECTION ON THE AILERON CONTROL SYSTEM, THE ENGINEER INVOLVED NOTICED THAT THER E WAS BLACK STAINING AROUND THE FLAP PUSH PULL ROD END FITTING. THE END FITTING WAS CHECKED AND FOUND TO BE LOOSE IN THE PUSH PULL ROD. THE ROD WAS REMOVED FROM THE AIRCRAFT, DISASSEMBLED, INSPECTED, RIVETS REPLACED AND RETURNED TO SERVICE. IT SHOULD BE NOTED THAT FAILURE OF THIS END FITTING COULD RESULT IN AN ASYMETRIC FLAP CONDITION 1 H 7 1 3R 3 R A815 E142 2001030800094 20010308 00094 CE 2001 3 8 CA991210006 1 19991102 A 3213 AN3105 NUT CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL TORQUE LINK MISSING W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, THE LEFT MAIN GEAR TORQUE LINKS SEPARATED CAUSING THE AIRCRAFT TO BE UNABLE TO TAXI. MAINTENANCE FOUN D THE NUT AT THE TORQUE LINK KNEE JOINT MISSING,WITH PART OF THE COTTER PIN STILL IN THE BOLT. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2001030800096 20010308 00096 SW 2001 3 8 CA991210010 1 19991104 A 2910 278103262 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE LT NACELLE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 22522 (CAN) DURING INSPECTION, THE LEFT ENGINE HYDRAULIC FLUID RETURN LINE WAS FOUND CHAFING ON ELECTRICAL WIRING INSIDE THE L EFT ENGINE NACELLE. THE LINE WAS REPLACED AND THE WIRING SECURED. 2 L 7 2 4T RT A8SW 6 C 3PNE 2001030800097 20010308 00097 EU 2001 3 8 CA991210011 1 19991110 A 5730 A5796505500000 FAIRING AIRBUS AIRBUS 310 A310304 EU LT WING MISSING W K NONE D INFLIGHT SEPARATION CR CRUISE 1 CA (CAN) L/H WING NR3 FAIRING, FWD NOSE ASSY FOUND MISSING AFTER FLIGHT. 2 L 7 2 4F RT A35EU 2001030800098 20010308 00098 EU 2001 3 8 CA991210012 1 19991113 A 2750 CONNECTOR AIRBUS 310 A310304 EU TE FLAPS DIRTY W K NONE F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) TRAILING EDGE FLAPS FAILED DURING APPROACH. INSPECTION REVEALED NO FAULT FOUND. CONNECTOR 39 AND 40 CLEANED. FLAP SYSTEM RESET. 2 L 7 2 4F RT A35EU 2001030800099 20010308 00099 EU 2001 3 8 CA991210013 1 19991115 A 2910 A2918107700000 HYDRAULIC LINE AIRBUS 310 A310304 EU HYD SYSTEM RUPTURED W O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA (CAN) LOSS OF GREEN SYSTEM HYD FLUID. INVESTIGATION REVEALED A RUPTUTRED LINE NEAR THE REAR SPAR. LINES REPLACED. 2 L 7 2 4F RT A35EU 2001030800100 20010308 00100 EA 2001 3 8 CA991210019 2 19991124 A 8500 ENGINE LYC O320D2A AVIONS R2160 R2160 0960101 EU LYC O320 O320D2A 41508 EA ENGINE FAILED W A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CA 1070 L1854039A (CAN) ENGINE STOPPED AT ALT, ENG WOULD NOT RESTART. NO FAULTS WERE FOUND WITH ENG AT BENCH TEST AFTER INCIDENT. 1 L 7 1 3O 3 O RT A48EU E274 2001030800101 20010308 00101 EA 2001 3 8 CA991210021 2 19991125 A 8530 LW15014 ROCKER LYC O360E1A6D PIPER PA44 PA44180 7104402 SO LYC O360 O360E1A6 41514 EA CYLINDER BROKEN W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 723 L24477T (CAN) ROCKER WAS FOUND BROKEN, ALL WERE REPLACED DUE TO EXCESSIVE WARE OR PRECAUTION. 1 L 7 2 3O 3 O A19S0 E286 2001030800102 20010308 00102 EU 2001 3 8 CA991210030 1 19991223 A 2742 DH004509 TRIM MOTOR AIRBUS A340 A340313 EU STABILIZER LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) GREEN SYSTEM HYD QUANTITY AND PRESSURE LOSS DURING FLIGHT. INVESTIGATION REVEALED A LEAKING PITCH TRIMMER LEAKING. UNIT REPLACED ALONG WITH BOTH ENGINE DRIVEN PUMPS AND CASE DRAIN FILTERS. 2 L 7 4 4F RT A197 2001030800103 20010308 00103 2001 3 8 CA991210031 4 19991026 A 2565 7A1508109 SLIDE RAFT AIRBUS A340 A340313 EU R1 DOOR FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) R1 DOOR SLIDE/RAFT FAILED TO DEPLOY ON TEST. PACKBOARD SPEED LACING DID NOT RELEASE. UNIT REPLACED. 2 L 7 4 4F RT A197 2001030800104 20010308 00104 NE 2001 3 8 CA991210032 2 19991027 A 7200 MSN740381 ENGINE CFMINT CFM565C4 AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE WING FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 741670 (CAN) REPORT TO FOLLOW. VSV ACTUATOR POSITION DEMAND DISAGREE FAULT VSVACT/HMU/J6 ANNUNCIATION. OPERATOR HAS FORBIDDEN D ISPATCH WITH SIMILAR FAULT MESSAGES. INITIAL TESTING HAS SO FAR NOT REVEALED ANY FAULT. CFMI IS INVESTIGATING. 2 L 7 4 4F 4 F RT A197 E37NE 2001030800105 20010308 00105 NE 2001 3 8 CA991210035 2 19991030 A 7320 657717D LINE PWA JT8D7 DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE LT ENGINE LEAKING W A UNSCHED LANDING R K J PARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION CR CRUISE 1 CA P657446D (CAN) EPR DECREASE DUE TO P2 LINE FITTING LEAKING. 2 L 7 2 4F 4 F A6WE E2EA 2001030800106 20010308 00106 EU 2001 3 8 CA991210039 1 19991102 A 2150 757A000008 ACM AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE AC BAY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) BURNT SMELL IN CABIN, NR2 ACU PACK TURNED OFF, SMELL DISSIPATED. NR2 ACM REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001030800107 20010308 00107 NM 2001 3 8 CA991210040 1 19991102 A 5330 RIVET AIRBUS AIRBUS A319 A319114 NM FUSELAGE CRACKED W K NONE O OTHER CR CRUISE 1 CA (CAN) LOUD HIGH PITCH NOISE IN CABIN IN SEAT ROW 14-17 AREA. INVESTIGATION REVEALED 4 CRACKED DOUBLER RIVETS AROUND UPPE R ANTI COLLISION LIGHT ASSY. RIVETS REPLACED. 2 L 7 2 4F RT A28NM 2001030800108 20010308 00108 EU 2001 3 8 CA991210054 1 19991108 A 3231 DOOR AIRBUS A340 A340313 EU LANDING GEAR OUT OF ADJ W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AMBER IN TRANSIT LIGHT ON FOR CENTER GEAR DOOR AFTER RETRACTION. AIRCRAFT LANDED. ADJUSTED CENTER LINE GEAR FIXED DOOR. SYSTEM OK. 2 L 7 4 4F RT A197 2001030800109 20010308 00109 EU 2001 3 8 CA991210055 1 19991120 A 4920 49900011 SEAL AIRBUS A340 A340313 EU APU LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) SMOKE IN CABIN WITH APU ON AND ACU PACKS ON. INVESTIGATION REVEALED APU LOAD COMPRESSOR OIL SEAL LEAK. APU REPLACE D. 2 L 7 4 4F RT A197 2001030800110 20010308 00110 EU 2001 3 8 CA991210056 1 19991111 A 2750 FLAP AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE WING FAILED W K NONE J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 CA (CAN) FLAPS FAILED AT O DEGREES ON APPROACH. AIRCRAFT LANDED FLAP BRAKES RESET. 2 L 7 2 4F 4 F RT A28NM E29NE 2001030800111 20010308 00111 NM 2001 3 8 CA991210058 1 19991121 A 3150 DISPLAY AIRBUS A319 A319114 NM COCPIT MALFUNCTIONED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA (CAN) ECAM MESSAGE SKIN AIR VALVE FAIL. NO FAULT FOUND. 2 L 7 2 4F RT A28NM 2001030800112 20010308 00112 NM 2001 3 8 CA991210059 1 19991122 A 2130 87292325V04 COMPUTER AIRBUS A319 A319114 NM EE BAY FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) UNABLE TO PRESSURIZE AFTER TAKEOFF. AVIONIC VENT COMPUTOR AND SKIN OUTLET AIR VALVE REPLACED. 2 L 7 2 4F RT A28NM 2001030800113 20010308 00113 EU 2001 3 8 CA991210060 1 19991123 A 5240 BOTTLE AIRBUS AIRBUS A340 A340313 EU R3 DOOR DISCHARGED W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) DOOR R3 SHOWING NOT ARMED ON FLIGHT ATTENDANDANTS PANEL AND ON ECAM. R3 DOOR ASSIST BOTTLE RECHARGED. 2 L 7 4 4F RT A197 2001030800114 20010308 00114 NE 2001 3 8 CA991210064 2 19991105 A 7261 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT ACTIVATED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 59577532 (CAN) EICAS MESSAGE RECEIVED ALONG WITH ENG OIL AURAL MESSAGE. ENG WAS SHUT DOWN. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030800115 20010308 00115 EA 2001 3 8 CA991210065 1 19991105 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT WING FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA 1002A (CAN) ON APPROACH FLAPS FAILED WHEN SELECTED TO 8 DEG. BPSU REPLACED 2 L 7 2 4F RT A21EA 2001030800116 20010308 00116 EA 2001 3 8 CA991210067 1 19991105 A 7603 M640631 THROTTLE 2100140003 CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED W E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA 618 (CAN) CREW REPORTED THE LEFT ENGINE POWER LEVER WAS UNABLE TO RETARD TO IDLE CUTOFF. ENG SHUT DOWN BY FIRE PUSH BUTTON. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030800117 20010308 00117 EA 2001 3 8 CA991210068 1 19991113 A 2750 860D10018ABC CONTROL UNIT CNDAIR CL600 CL6002B19 EA FLAP FAILED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 526 (CAN) FLAPS FAILED ON DECENT. FLAPLESS LANDING CARRIED OUT. FECU FOUND FAULTY. 2 L 7 2 4F RT A21EA 2001030800118 20010308 00118 EA 2001 3 8 CA991210069 1 19991113 A 2752 854D10012 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE RT WING JAMMED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 830 (CAN) FLAPS SELECTED TO 45 DEG AND FAILED AT 23 DEG. NR4 ACTUATOR FOUND HARD JAMMED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030900080 20010309 00080 EU 2001 3 9 CA991209065 1 19991116 A 2612 D237060 FIRE LOOP BRAERO 748 HS7482A 4231001 EU NR 2 ENGINE CHAFED W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CA (CAN) DURING CRUISE NR2 ENG FIRE WARN ILLUMINATED. ENGINE SECURED AND FIRE DRILL COMPLETED. INVESTIGATION REVEALED FIREW IRE CHAFFED AND SHORTING TO GROUND.COMPONENT REPLACED. 2 L 7 2 3T A24EU 2001030900083 20010309 00083 EA 2001 3 9 CA991210075 1 19991128 A 2750 855D100 CONNECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT BPSU CORRODED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH FLAP FAIL MESSAGE AFTER 20 DEG. R/H BPSU CANNON PLUG FOUND CORRODED ALONG WITH PINS AT BPSU. L/H CANNO N PLUG REPLACED AS PRECAUTION 2 L 7 2 4F 4 F RT A21EA E15NE 2001030900084 20010309 00084 EA 2001 3 9 CA991210076 1 19991128 A 2752 854D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE FLAPS FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH FLAPS FAIL WHEN SELECTED FROM 30 TO 45. FLAPS WOULDN''T RETRACT AFTER LANDING. MAINT COLD SOAKED FLAP ACTUATORS NR4 LH AND 2&3 RH. A/C TEST FLEW U/S. PDU REPLACED SERV. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030900085 20010309 00085 EA 2001 3 9 CA991210077 1 19991127 A 2750 FLAP CNDAIR CL600 CL6002B19 EA WING FAILED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) FLAPS FAILED WHEN SELECTED TO 8 DEG. SYSTEM RESET 2 L 7 2 4F RT A21EA 2001030900086 20010309 00086 EA 2001 3 9 CA991210078 1 19991120 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE FLAP MALFUNCTIONED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 CA (CAN) ON DECENT FLAPS FAILED WHEN SELECTED TO 8 DEG. EXCESSIVE TORQUE IN NR 3 ACTUATOR. ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030900087 20010309 00087 EA 2001 3 9 CA991210079 1 19991127 A 3244 299K631 TIRE CNDAIR CL600 CL6002B19 EA MLG SEPARATED W K NONE E VIBRATION/BUFFET TO TAKEOFF 1 CA (CAN) SHORTLY AFTER TAKE OFF, CREW REPORTED A LOUD BANG AND VIBRATION.AFTER UNEVENTFUL LANDING MAINT. REPORTED NR2 MAINW HEEL TIRE TREAD HAD SEPERATED FROM TIRE. L/H FLAP ALSO FOUND DAMAGED @ I/B TRAILING EDGE AND FUSELAGE FAIRING. FLAP AND WHEEL ASSY REPLACED. 2 L 7 2 4F RT A21EA 2001030900093 20010309 00093 EA 2001 3 9 CA991210085 1 19991120 A 2752 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA RT FLAP MALFUNCTIONED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA 998 (CAN) ON APPROACH FLAPS SELECTED TO 8 DEG WITH FLAP FAIL MESSAGE. A/C LANDED WITH O FLAPS. R/H I/B FLAP, I/B ACTUATOR EX CESSIVE TORQUE. 2 L 7 2 4F RT A21EA 2001030900095 20010309 00095 NE 2001 3 9 CA991210087 2 19991120 A 7261 4027T69P06 VALVE GE CF343B1 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE RT ENGINE FAILED W K NONE O OTHER CR CRUISE 1 CA (CAN) OIL PX FLUX AT ALT. AFTER DESCENT TO 18000'' OIL PX STABILIZED. OIL TANK PX VALVE REPLACED AND SENT TO GE FOR INV ESTIGATION. 2 L 7 2 4F 4 F RT A21EA E15NE 2001030900096 20010309 00096 EA 2001 3 9 CA991210088 1 19991120 A 2916 NAS122164 O-RING CNDAIR CL600 CL6002B19 EA HYD RESERVOIR BROKEN W D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING ENGINE START PILOT NOTED A LOUD VIBRATION COMING FROM R/H EMGINE. PRIOR TO TAKE-OFF HYD PUMP 2B CAUTION MES SAGE ILLUMINATED. AIRCRAFT RETURNED TO GATE AND HYD LOW PRESS ILLUMINATED. MAINT. FOUND THE ORING ON THE RESERVOIR END F ITTING BROKEN. 2 L 7 2 4F RT A21EA 2001030900098 20010309 00098 EA 2001 3 9 CA991210093 2 19991115 A 8520 CRANKSHAFT LYC TIO540A2B PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 433 L207261 (CAN) A SECTION OF THE CRANKSHAFT COUNTER WEIGHT LUG FAILED. 1 L 7 2 3O 3 O A20SO E14EA 2001030900100 20010309 00100 GL 2001 3 9 CA991210096 2 19991123 A 7261 6853301 SUMP ALLSN 23038160 BELL 206 206L 1181522 SW ALLSN 25OC 250C20R GL ENGINE DEFORMED W K NONE O OTHER IN INSP/MAINT 1 CA 6 CAT15311 (CAN) SUMP SEAT DEFORMED NOT ALLOWING CRUSH WASHER TO FOR A SEAL. 1 G 7 1 3U 3 U H2SW E4CE 2001030900102 20010309 00102 NM 2001 3 9 CA991229001 1 19991122 A 5743 SUPPORT BRACKET DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE LT NACELLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 21842 (CAN) THE BRACKET WHICH SUPPORTS THE DUAL SKID CONTROL VALVE, IN THE LEFT ENGINE NACELLE WAS FOUND CRACKED. THE RIGHT SI DE BRACKET WAS CHECKED AND ALSO FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030900103 20010309 00103 NE 2001 3 9 CA991229002 3 19991122 A 6111 SFA13M10A BLADE HAMSTD 14SF7 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15163 5446 86354137 (CAN) NICKEL LEADING EDGE SHEATH CRACK PROPAGATED BEYOND ALLOWABLE LIMITS. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030900104 20010309 00104 NM 2001 3 9 CA991229003 1 19991202 A 3020 8SC0041001 BOOT 87140011007 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 INTAKE DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 6587 S2WAE0441 (CAN) # 1 ENGINE INTAKE DEICE BOOT FOUND DELAMINATING FROM ENGINE INTAKE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030900105 20010309 00105 EU 2001 3 9 CA991229004 1 19991203 A 2750 676101238 CONTROL UNIT BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FLAP FAILED W K NONE F J FLT CONT AFFECTED WARNING INDICATION IN INSP/MAINT 1 CA 1086D1112 (CAN) INVESTIGATION INTO A RECURRENT FLAP CAUTION LIGHT LED TO THE REPLACEMENT OF THE GREEN SYSTEM RESOLVER ON THE FLAP POWER UNIT. 2 H 7 4 4F 4 F A49EU E6NE 2001030900106 20010309 00106 EU 2001 3 9 CA991229005 1 19991207 A 2810 HTE7300F1218 O-RING BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION A FUEL LEAK WAS DISCOVERED AT NR4 PYLON. THE SOURCE OF THE LEAK WAS DETERMINED TO BE THE SEAL AT THE FUEL TANK TO PYLON ELBOW. SEAL REPLACED 2 H 7 4 4F 4 F A49EU E6NE 2001030900107 20010309 00107 EU 2001 3 9 CA991229006 1 19991208 A 2760 3799H1 SERVO VALVE BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE AIRBRAKE FAILED W K NONE F FLT CONT AFFECTED AP APPROACH 1 CA 18106 7889 FYH158773 (CAN) FLIGHT CREW REPORTED AN UNCOMMANDED DEPLOYMENT OF THE AIRBRAKE DURING APPROACH. AIRBRAKE SERVO VALVE REPLACED. 2 H 7 4 4F 4 F A49EU E6NE 2001030900108 20010309 00108 NM 2001 3 9 CA991229007 1 19991203 A 5743 SUPPORT BRACKET DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE LT NACELLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE BRACKET WHICH SUPPORTS THE DUAL SKID CONTROL VALVE, IN THE LEFT ENGINE NACELLEWAS FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030900109 20010309 00109 EU 2001 3 9 CA991229008 1 19991212 A 3411 QP122A PITOT HEAD BAC 146 146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE PITOT/STATIC SYS FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 12475 40186 (CAN) Q FEEL HEATER FAIL CAUTION LIGHT ILLUMINATED DURING CLIMB. AIRCRAFT RETURNED AND Q FEEL PITOT HEAD REPLACED. 2 H 7 4 4F 4 F A49EU E6NE 2001030900110 20010309 00110 NM 2001 3 9 CA991229009 1 19991212 A 2910 8Z6069179 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) WHILE INVESTIGATING A REPORTED HYDRAULIC LEAK IN THE NR2 ENGINE NACELLE, THE NR2 SYSTEM RUDDER RETURN LINE WAS FOU ND CHAFED AND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030900111 20010309 00111 NM 2001 3 9 CA991229010 1 19991213 A 7603 87620134007 ROD END PWA PW120A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FUEL CONTROL LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 120854 (CAN) DURING SCHEDULED INSPECTION, THE NR 2 ENGINE CONDITION CONTROL ROD FROM THE TERMINAL QUADRANT TO THE HYDROMECHANIC AL FUEL CONTROL UNIT WAS FOUND TO HAVE A LOOSE ROD END AND WAS MISSING A RETAINING RIVIT. THE ROD WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030900112 20010309 00112 NM 2001 3 9 CA991229011 1 19991211 A 2530 1095BL COFFEEMAKER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE GALLEY OVERHEATED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) FLIGHT ATTENDANT REPORTED A BURNING/ELECTRICAL SMELL IN THE GALLEY AREA. LIGHTING AND GALLEY EQUIPMENT WAS SWITCHE D OFF AND THE SMELL DISSIPATED. MAINTENANCE INVESTIGATION REVEALED THAT THE SMELL WAS COMING FROM THE COFFEE WARMER AND REPLACED IT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001030900113 20010309 00113 EA 2001 3 9 CA991229012 1 19991127 A 5743 SUPPORT BRACKET DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT NACELLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE BRACKET WHICH SUPPORTS THE DUAL SKID CONTROL VALVE, IN THE LEFT ENGINE NACELLEWAS FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001030900114 20010309 00114 NM 2001 3 9 CA991229013 1 19991206 A 2510 034143 FAN SMITHSIND 1633930401 BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE COCKPIT JAMMED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 21093 0000431 (CAN) ELECTRICAL SMOKE FOUND IN COCKPIT DURING B CHECK. SMOKE COMING OUT OF PEDESTAL. FOUND PDC CONTROL UNIT PANEL FAN J AMMED AND SMOKING. CONTROL DISPLAY UNIT AND AREA VENTILATED, FLIGHT DECK CLEANED AND SEAT COVERS REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2001030900115 20010309 00115 NM 2001 3 9 CA991229014 1 19991208 A 2520 EEP77848 SEAT BOEING 767 767375 NM CABIN MALFUNCTIONED W H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 48927 260 178 (CAN) SHORTLY AFTER TAKEOFF SEAT 3G RECLINED ON ITS OWN AND NO FURTHER CONTROL AVAILABLE. HOT PLASTIC SMELL THEN PERSIST ED IN FORWARD CABIN. POWER TO ALL SEATS TURNED OFF, RECIRC FAN OFF ON FIX. A/C RETURNED FOR REPAIRS. 2 L 7 2 4F RT A1NM 2001030900116 20010309 00116 NM 2001 3 9 CA991229015 1 19991203 A 5260 65566562 HOUSING BOEING 65529971 BOEING 737 737275C NM PWA JT8 JT8D9A 52048 NE AFT STAIRS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 0752 (CAN) FOUND AFT STAIR NOT FULLY EXTENDED. AFT STAIR FORWARD TRANSMISSION HOUSING CRACKED AND TOP STEP AFT HINGE SEGMENT CRACKED. PARTS REPLACED OR REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 2001030900119 20010309 00119 SW 2001 3 9 CA991229018 1 19991125 A 2435 23046020 STARTER GEN BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA ENGINE MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE IN INSP/MAINT 1 CA 8769 189 11966 (CAN) STARTER OVERHEAT DURING COMPRESSOR WASH CYCLES CAUSING SMOKE AND FLAMES IN STARTER. 1 G 7 1 4U 4 U H4SW E22EA 2001030900120 20010309 00120 WP 2001 3 9 CA991229019 1 19991209 A 2752 NAS5623 BOLT 5328468 DOUG DC6 DC6B 3021712 WP HAMSTD 43E 43E60 NE FLAP ACTUATOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 27509 (CAN) DURING INSP FLAPS AND AILERONS REMOVED FOR INSP. PORT INBD FLAP ACTUATOR-TO-FLAP ATTACH BOLT FOUND BROKEN, NO DAMA GE TO SURROUNDING AREA. BOLT REPLACED. 2 L 7 4 4R 6A4 6 C P871 2001030900121 20010309 00121 GL 2001 3 9 CA991229020 2 19991214 A 7313 6890917 NOZZLE ALLSN BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL SYSTEM CONTAMINATED W E ENGINE SHUTDOWN E VIBRATION/BUFFET IN INSP/MAINT 1 CA 986 AG43534 (CAN) N2 BLEED OFF EXPERIENCED WHEN POWER REQUESTED. FUEL NOZZEL REMOVED AND FOUND TO HAVE CARBON BUILD-UP. NOZZEL SENT FOR O/H. 1 G 7 1 3U 3 U H2SW E4CE 2001030900123 20010309 00123 NE 2001 3 9 CA991229022 2 19991208 A 7321 7257256 FUEL CONTROL SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE NR 2 ENGINE FAILED W O OTHER E VIBRATION/BUFFET AP APPROACH 1 CA 12 410707BR (CAN) NR2 ENGINE WOULD NOT RESPOND PROPERLY TO INCREASED POWER SETTING. FCU REPLACED BUT SUBSEQUENT FAILURE 50 HRS LATER . FCU''S AND FUEL SAMPLES WERE SENT FOR INVESTIGATION. AWAITING FOLLOW UP REPORT. CALL RECEIVED FROM OPERATOR SPECIFYING MATERIAL BREAKDOWN FROM FILTER. FAA ALERT 43-16A AND CORRECTIVE ACTION ADVISORY TO BE ISSUED TO OPERATORS. 2 G 7 2 4U 4 U 1H15 1E3 2001030900125 20010309 00125 CE 2001 3 9 CA991229033 1 19991206 A 3260 90422912 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE INSTRUMENT PNL INOPERATIVE W O OTHER N FALSE WARNING AP APPROACH 1 CA 478 734 (CAN) DURING APPROACH THE NOSE GEAR LIGHT DID NOT ILLUMINATE WHEN GEAR SELECTED DOWN. GEAR MANUALLY EXTENDED.THE ANNUNC IATOR WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 2001030900126 20010309 00126 CE 2001 3 9 CA991229034 1 19991206 A 3233 11238002219 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 5199 713 (CAN) DURING APPROACH IN WAS DISCOVERED THAT THE NOSE LANDING GEAR LIGHT FAILED TO ILLUMINATE.UPON INSPECTION MAINTENANC E NOTED THE NOSE LANDING GEAR INTERNAL DOWNLOCK SWITCH HAD HIGH RESISTANCE. THE ACTUATOR (BY FRISBY) WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 2001030900127 20010309 00127 CE 2001 3 9 CA991229035 1 19991218 A 7714 1303800445 INDICATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT MALFUNCTIONED W K NONE N FALSE WARNING CL CLIMB 1 CA 5280 610 (CAN) PILOT REPORTED R/H N1 GAUGE READING 115% IN SPITE OF NORMAL ENGINE PERFORMANCE. N1 INDICATOR WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 2001030900129 20010309 00129 WP 2001 3 9 CA991229037 2 19991217 A 7200 TPE33111U611G ENGINE GARRTT TPE3311U SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE3311U 01514 WP NR1 ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 19352 P44661C (CAN) LOSS OF OIL PX PRECLUDED ENGINE IFSD.SUSPECTED CAUSE TO BE INTERNAL OIL SE AL FAILURE ALLOWING OIL TO EXIT TAILPIP E. REPORT TO FOLLOW. IT WAS DETERMINED THAT A BIRD STRIKE HAD OCCURED ON THIS ENGINE AND REPAIRS WERE MADE ATUSA O/H FAC ILITY AFTER WHICH THIS ENG WAS PUT ON WING BY THIS OPERATOR.WAR ENTY ISSUE ONLY. 2 L 7 2 4T 3 T RT A8SW E3WE 2001030900131 20010309 00131 GL 2001 3 9 CA991229039 3 19991210 A 6110 PROPELLER MCAULY D2AF34C308 REIMS 337 FT337GP 7535726 EU CONT O360 TSIO360CB 17025 SO MCAULY 2AF34C D2AF34C308 GL ENGINE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 14 791951 (CAN) PROPELLER SEIZED DUE CORROSION. 1 H 7 2 3O 3 O A23EU E9CE 5 C P5EA 2001032000004 20010320 00004 SW 2001 3 20 CA991229030 1 19991207 A 6310 205040242001 BEARING BELL 205540010101 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE FREEWHEEL UNIT NOISY W K NONE O OTHER IN INSP/MAINT 1 CA 1017 ABT01048 (CAN) DURING ROUTINE INSPECTION, THE AME ROTATED THE MAIN INPUT SHAFT TO ENSURE PROPER FUNCTION ON FREEWHEEL UNIT AND HE ARD UNUSUAL NOISES. FREEWHEEL UNIT WAS REMOVED AND THE INNER RACE OF THE BEARING WAS FOUND DAMAGED. NO OIL LEAK, DISCOLO RATION OR METAL WAS FOUND IN THE GEARBOX. 1 G 7 1 4U 4 U H1SW E17EA 2001032000005 20010320 00005 WP 2001 3 20 CA991229031 1 19991130 A 6310 369D25351 SPRAG CLUTCH HUGHES 369A535041 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL CLUTCH ASSY BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 446 6039 (CAN) DURING 300 HOUR INSPECTION OF THE O/R CLUTCH ASSY, THE SPRAG ASSY (S/N 5433) WAS FOUND TO HAVE A PIECE OF ONE OF T HE SPAGS BROKEN OFF. THE PIECE WAS APPRX 1/4 X 1/4 INCH AND CAME FROM THE INSIDE DIAMETER OF THE SPRAG CLUTCH. 1 G 7 1 3U 3 U H3WE E4CE 2001032000006 20010320 00006 CE 2001 3 20 CA991229032 1 19991204 A 3297 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG SELECTOR CHAFED W O OTHER O OTHER CR CRUISE 1 CA 4932 (CAN) DURING CRUISE THE 2 AMP MLG CONTROL CIRCUIT BREAKER TRIPPED AND WASN''T ABLE TO RESET. EXTENSIVE TESTING COULD NO T DUPLICATE FAULT. THE LANDING GEAR RELAY WAS REPLACED AND FAULT REAPPEARED ON TEST FLIGHT. EXTENSIVE INSPECTION OF WI RING FROM THE C/B TO THE LANDING GEAR SERVICE VALVE WAS CRRIED OUT.MAINTENANCE DISCOVERED THE WIRE WAS CHAFFED UNDERNEAT H THE CABIN ENTRANCE FLOOR AT THE JUNCTION OFTHE FLOOR AND WALL. 2 L 7 2 4T 4 T RT A24CE E26NE 2001032000007 20010320 00007 CE 2001 3 20 CA991229041 1 19991208 A 2842 100380006119 PROBE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE LT AUX TANK WORN W K NONE L NO TEST IN INSP/MAINT 1 CA 4334 (CAN) MAINTENANCE LOCATED FUEL QUANTITY ERRATIC READINGS TO BE FROM THE LT CENTRE AUX TANK PROBE.UPON EXAMINATION IT WAS DISCOVERED THAT THE FUEL PROBE SOUTER SHEATH OF THE CAPACITOR WAS LOOSE AT THE UPPER ATTACH RIVETS. THIS MOVEMENT WOULD HAVE VARIED THE ELECTRICAL SIGNAL. 1 L 7 2 4T 4 T A24CE E4EA 2001032000008 20010320 00008 CE 2001 3 20 CA991229042 1 19991210 A 5610 10138402515 WINDSHIELD BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE COCKPIT CRACKED W B EMER. DESCENT O OTHER CR CRUISE 1 CA 1711 (CAN) WINDSHIELD CRACKED IN FLIGHT BELIEVED TO HAVE BEEN CAUSED BY HAILSTONE STRIKING WINDSCREEN AND PREVIOUS DELAMINATI ON. UPON REMOVAL OF WINDSCREEN IT WAS DISCOVERED THAT THE MINIMUM ALLOWABLE CLEARANCE BETWEEN THE WINDSCREEN FLANGEAND T HE AIRFRAME WAS BELOW LIMITS. THE PRELOAD ON THE WINDSCREEN PLUS THE HAILSTONE IMPACT MAY HAVE CONTRIBUTED TO THE CRAC KING. 1 L 7 2 4T 4 T A24CE E4EA 2001032000009 20010320 00009 CE 2001 3 20 CA991229043 1 19991221 A 7603 509440763 LEVER BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE CAM BOX SLIPPED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 4341 (CAN) CAMBOX INPUT LEVER SLIPPING ON SHAFT, DUE TO INTERFERENCE FROM IMPROPERLY RIGGED FUEL SHUTOFF LINKAGE. OPERATOR RE QUESTS TORQUE VALUE FOR IMPUT LEVERFROM MANUFACTURER, NOTE SHAFT IS SERRATED STANDARD MAINTENANCE PRACTICES CAN BE IMPLO YED. 1 L 7 2 4T 4 T A24CE E4EA 2001032000010 20010320 00010 CE 2001 3 20 CA991229044 1 19991217 A 5740 351150595 ATTACH FITTING BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE FUSELAGE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 4332 (CAN) DAMAGE FOUND ON COUNTERBORE FITTINGS FACE OF UPPER AND LOWER AFT WING ATTACH POINTS.FOUND INCORRECT PART NUMBER WA SHER, USED ON BOLT STACK-UP FOR AFT FITTINGS. 1 L 7 2 4T 4 T A24CE E4EA 2001032000012 20010320 00012 GL 2001 3 20 CA991229046 1 19991204 A 7810 2078000107 MANIFOLD DIAMON DA20 DA20A1 GL ROTAX 912 ROTAX912 55555 EU ENGINE EXHAUST SEPARATED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 2396 (CAN) AS THE AIRCRAFT DEVELOPED TAKE-OFF POWER, THE PILOT NOTICED ABNORMAL ENGINE NOISE AND ABORTED THE TAKE-OFF. AN IN SPECTION OF THE ENGINE REVEALED THAT THE LEFT REAR EXHAUST MANIFOLD HAD SEPARATED FROM ITS MOUNTING FLANGE. EXHAUST MANI FOLD REPLACED WITH PART NO. 20-7800-01-07. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 2001032000013 20010320 00013 SW 2001 3 20 CA991229047 1 19990814 A 7714 83900155 SENSOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 138 (CAN) LOW ROTOR WARNING LITE AND HORN ACTIVATED WITH THE RPM AT 100%. UNIT REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2001032000014 20010320 00014 SW 2001 3 20 CA991229048 1 19990808 A 6710 206010342002 PITCH LINK BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) INSPECTION OF M/R PITCH LINKS REVEALED DAMAGE IN AREA OF THE LOCKWIRE TAB LOCK. PITCH LINKS REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 2001032000015 20010320 00015 WP 2001 3 20 CA991229049 1 19990910 A 7720 6100034 INDICATOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL COCKPIT INACCURATE W O OTHER O OTHER CR CRUISE 1 CA 265 (CAN) TOT GUAGE READS INACCURATELY. UNIT REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 2001032000016 20010320 00016 GL 2001 3 20 CA991229050 2 19990909 A 7323 23057870 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W O OTHER O OTHER DE DESCENT 1 CA 1135 (CAN) ENGINE OVERSPEEDS AND RECOVERS VERY SLOWLY. 1 G 7 1 3U 3 U H2SW E4CE 2001032000017 20010320 00017 WP 2001 3 20 CA991229051 1 19991021 A 6510 369D255031 BOLT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL T/R DRIVESHAFT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) BOLT FOR THE FWD T/R DRIVESHAFT COUPLING WAS FOUND LOOSE. BOLT REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 2001032000018 20010320 00018 EU 2001 3 20 CA991229053 1 19991220 A 2420 914F5696 GCU FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU GENERATOR FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) PILOT REPORTED THAT DURING THE BOARDING PROCESS. A HEAVY SMOKE SMELL FROM THE MAIN CABIN CB PANEL WAS EMANATING T HROUGH THE COCKPIT. THE CREW WRE UNABLE TO PINPOINT THE SOURCE. THE AIRCARAFT WAS SHUTDOWN AND THE PASSENGERS WERE DEPLA NED WITHOUT INCIDENT. MAINTENANCE REPLACED THE COCKPIT GENERATOR CONTROL UNIT, SYSTEM CHECKED SERVICEABLE AND REPLACED T HE AC BUS CONTACTOR. 2 L 7 2 4F 4 F RT A20EU E2EU 2001032000024 20010320 00024 NM 2001 3 20 CA991229060 1 19991201 A 5210 STRUCTURE BOEING 737 737284 138448R NM PWA JT8 JT8D9A 52048 NE PAX DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSP OF FWD ENTRY DOOR A CRACK WAS FOUND IN THE LOWER 1/3 OF DOOR NEAR DOOR CENTERLINE BETWEEN RIVETS. A/C FERRIED FOR REPAIR. 2 L 7 2 4F 4 F A16WE E2EA 2001032000025 20010320 00025 EU 2001 3 20 CA991229061 1 19991130 A 3242 9595801511 BRAKE ASSY PILATS PC12 PC1245 EU MLG SEIZED W O OTHER O OTHER LD LANDING 1 CA 897 (CAN) ON LANDING THE AIRCRAFT PULLED TO THE LEFT. MAINTENANCE DETERMINED THAT THE LEFT BRAKE ASSEMBLY WAS SEIZED/FROZEN. DUE TO THE RUNWAY BEING SNOW COVERED, DIRECTIONAL CONTROL WAS MAINTAINED IN SPITE OF THE SEIZED BRAKE. 1 L 7 1 3T RT A78EU 2001032000026 20010320 00026 EU 2001 3 20 CA991229062 1 19991203 A 2752 951D10011 ACTUATOR PILATS PC12 PC1245 EU TE FLAPS MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA 1528 65 234A (CAN) LT OUTBOARD FLAP ACTUATOR REPLACED DUE TO EXCESSIVE BACKLASH MEASURED AT 65 CYCLE INSPECTION. 1 L 7 1 3T RT A78EU 2001032000027 20010320 00027 EU 2001 3 20 CA991229063 2 19991205 A 7250 BLADE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 2 ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) NR 2 LP TURBINE BLADE FAILURE. R/R 2 L 7 2 4F 4 F RT A20EU E2EU 2001032000028 20010320 00028 SW 2001 3 20 CA991229066 1 19991217 A 7120 LB9130121 BUSHING BELL 206 206B 1181511 SW ALLSN 250C 250C20J 03013 GL ENGINE MOUNT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 6932 (CAN) DURING 100 HOUR INSPECTION, RT ENGINE MOUNT WAS FOUND LOOSE. UPON DISASSEMBLY, THE BUSHING WAS FOUND TO BE SEPARAT ED (RUBBER BONDS WERE SEPARATED). BUSHING ID & OD WERE WORN BEYOND LIMITS. RT ENGINE MOUNT LEGS WERE ALSO FOUND TO HAVE THE BUSHING MOUNTING BORES WORN BEYOND LIMITS. 1 G 7 1 3U 3 U H2SW E4CE 2001032000029 20010320 00029 NM 2001 3 20 CA991229068 1 19991226 A 2131 7612608 CONTROLLER BOEING 737 737204 1384458 NM PWA JT8 JT8D15 52051 NE CABIN PRESSURE FAILED W B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) CREW REPORTED THAT DURING CLIMB AT ABOUT 14,000 FT AN AURAL WARNING WAS HEARD FOLLOWED BY DEPLOYMENT OF PASS O2 MA SKS. EMEG DESCENT AND RETURN TO BASE. MAINT INSP CARRIED OUT AND NO DISCREPANCIES FPUND, ONGOING INVESTIGATION. PRESSURE CONTROLLER REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2001032000031 20010320 00031 SO 2001 3 20 CA991229072 1 19991203 A 5510 4653815 SPAR PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8071 (CAN) ROUTINE INSPECTION REVEALED SPAR WEB CRACKING AT STATION 110 OF L/H HORIZONTAL STABILIZER.CRACK JUST VISISBLE FRON AFT VIEW.STABILIZER SKINS LIFTED TO GAIN ACCESS TO INTERNAL AREA.CRACKED DETERMINED TO BE APPROX. 0.750 IN LENGTH AND O RIGINATING FROM RIVET HOLE (SPAR CAP TO SPAR WEB). OUTBOARD SPAR WEB REMOVED AND REPLACED. 1 L 7 2 3T 4 T A8EA E4EA 2001032000032 20010320 00032 EU 2001 3 20 CA991229073 1 19991203 A 7110 LATCH BNORM BN2 BN2A27 1520227 EU LYC O540 O540E4C5 41532 EA LT ENGINE COWL WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) COWL LATCH FOUND WEARING A HOLE IN THE LT ENGINE NR 1 CYLINDER VALVE COVER. 1 H 7 2 3O 3 O A17EU E295 2001032000033 20010320 00033 CE 2001 3 20 CA991229074 1 19991210 A 5330 55111324 SKIN CESSNA 500 500CESSNA 2076602 CE BUTT JOINT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14536 (CAN) EDDY CURRENT INSPECTION OF SKIN BUTT JOINTS AT SCHEDULED MAINTENANCE INTERVAL, REVEALED AN ANOMALY WHICH RESULTED IN FINDING A CRACK OF 3 INCH LENGTH IN THE SUBJECT DOUBLER. THE LOCATION OF THE CRACK WAS AT F.S 262.02, WL 153.0 1 L 7 2 4F A22CE 2001032000034 20010320 00034 CE 2001 3 20 CA991230001 1 19991129 A 3243 3507218160511 SPRING PARAMOUNT 9038000111 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MASTER CYLINDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 06644 (CAN) RT BRAKE CITED AS ''SOFT''. AME REMOVED RT SHUTTLE VALVE AND DISSASSEMBLED IT. CUT O-RING REPLACED. FAULT STILL APPEARED. AME REMOVED RT MASTER CYLINDER (P/N90-380001-11(VI-15-1000)) AND DISASSEMBLED.SPRING WASHER FOUND TO BE SPLIT IN HALF.SPRING REPLACED.CHECKED OK. 1 L 7 2 4T 4 T A24CE E4EA 2001032000035 20010320 00035 2001 3 20 CA991230002 4 19991202 A 6122 1310511 VALVE WOODWARD 8210003 PIPER PA31T PA31T2 7103127 SO PWA PT6 PT6A135 52043 NE PROP GOVERNER CONTAMINATED W C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CA 1500 (CAN) ON THE TAKE-OFF ROLL THE LT ENGINES PROP WOULDN''T EXCEED 1300 RPM. THE PROBLEM WAS FOUND TO BE A DIRTY HYDRAULIC TOPPING GOVERNOR VALVE. THE UNIT WAS CLEANED AND RETURNED TO SERVICE. 1 L 7 2 3T 4 T RT A8EA E4EA 2001032000036 20010320 00036 EU 2001 3 20 CA991230003 1 19991118 A 3246 A32266 BOLT C20211160 AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE WHEEL BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 10975 (CAN) WHEN ASSEMBLING WHEEL BOLTS STRETCHED BEFORE REACHING SPECIFIED TORQUE.WHEEL TIE BOLTS STRETCHED AT 180 FT/LBS TOR QUE. 2 L 7 2 4F 4 F RT A35EU E23EA 2001032000037 20010320 00037 GL 2001 3 20 CA991230008 3 19991210 A 6111 B4460 PIN MCAULY D3A32C90 CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO MCAULY 3A32C D3A32C90 GL PROP BLADE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 975 756820 (CAN) DEEP CORROSION PITS, ACTUATING PINS REPLACED. 1 H 7 1 3O 3 O A4CE E5CE 5 C P21EA 2001032000038 20010320 00038 GL 2001 3 20 CA991230009 3 19991210 A 6114 HUB CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO MCAULY 3A32C D3A32C90 GL PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 975 (CAN) FOUND CRACK IN DICATION USING EDDY CURRENT ON HUB SOCKET. NR 1 AND NR 2 HUB REPLACED. 1 H 7 1 3O 3 O A4CE E5CE 5 C P21EA 2001032000039 20010320 00039 GL 2001 3 20 CA991230012 3 19991210 A 6114 A4140 PLUG MCAULY D3A32C90 CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO MCAULY 3A32C D3A32C90 GL HUB SOCKETS MISSING W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 975 756820 (CAN) TWO LOCKING EXPANSION PLUGS FOR EACH BLADE ALL WERE FOUND NOT INSTALLED. LOCKING EXPANSION PLUGS ARE USED TO LOCK THE BLADES TO THE HUB . THIS IS AN O/H OVERSIGHT AND A MAINTENANCE ISSUE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P21EA 2001032000041 20010320 00041 CE 2001 3 20 CA991230016 1 19991130 A 2913 10138800519 POWERPACK AIRIGHT BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE HYD SYSTEM INTERMITTENT W K NONE L NO TEST IN INSP/MAINT 1 CA 161 (CAN) HYDRAULIC POWER PACK OPERATED NORMALLY ON GEAR RETRACTIONS WHILE ON JACKS, BUT WOULD INTERMITTANTLY POP 60 AMP CON TROL BREAKER IN THE AIR.REPLACED UNIT. 2 L 7 2 4T 4 T A24CE E4EA 2001032000043 20010320 00043 SO 2001 3 20 CA991230018 1 19991107 A 7603 6763908 CABLE LYC O320E3D PIPER PA28 PA28140 7102802 SO LYC O320 O320E3D 41508 EA POWER LEVER BROKEN W E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 CA L3120927A (CAN) UPON POWER REDUCTION, THE THROTTLE CONTROL CABLE BROKE AND ENGINE WENT INTOHIGH POWER.CONTROL CABLE REPLACED WITH NEW PART. UPON DISSASEMBLY, TELEFLEX CABLE WAS FOUND BROKEN APPROX. 1 INCH BELOW SWAGEDARM AT THROTTLE CONTROL LEVER QU ADRANT IN COCKPIT. THERE APPARENTLY WAS NO THROTTLE BINDING PRIOR TO GIVEING ANY WARNING. AS TELEFLEX IS COMPLETELY ENC LOSED IN OUTER HOUSING, VISUAL INSPECTION / DETECTION OF FRAYING IS NOT POSSIBLE. 1 L 7 1 3O 3 O 2A13 E274 2001032000044 20010320 00044 EA 2001 3 20 CA991230019 1 19991208 A 2824 2780473105 CHECK VALVE CNDAIR CL601 CL6012A12 1900303 EA FUEL SYSTEM FAILED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) IT WAS DISCOVERED THAT OVER THE NIGHT, FUEL HAD MIGRATED FROM THE RT WING TO THE AUX TANK. THIS WAS VARIFIED AT AP PROX. 100 LBS / HR. A/C DEFUELED AND MAINT DISCOVERED AUX TRANSFER EJECTOR CHECK VALVE TO BE OUT OF ALIGNMENT DUE TO THE HINGE PIN COMING OUT OF THE SIDE OF ITS HOLDER. NEW EJECTOR INSTALLED. UNABLE TO VERIFY TTSN BUT SURE ITS 8177.0 2 L 7 2 4F RT A21AE 2001032000045 20010320 00045 EA 2001 3 20 CA991230020 1 19991209 A 2133 LINE CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE OUTFLOW VALVE MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) DURING CLIMB AT APPROX. 5000 FT AUTO PRESSURE WAS NOTICED NOT TO BE WORKING AS CABIN ALT WAS CLIMBING AT 7500 FT. MANUAL PRESSURIZATION WAS SELECTED AND THE RATE OF CLIMB IN THE CABIN WAS VERY HIGH AND THE SPEED BARBER POLE ON THE CA PTAINS ASI DROPPED 30 KNOTS CAUSING A SPEED ADVANCE. FLIGHT CONTINUED UNPRESSURIZED AND A/C LANDED AT HOME BASE. STATIC AND PRESS LINES ON WERE FOUND CROSSED ON OUTFLOW VALVE. 2 L 7 2 4F 4 F RT A21AE E15NE 2001032000046 20010320 00046 EA 2001 3 20 CA991230021 1 19991210 A 2432 HA9A048 CONTACTOR CNDAIR CL601 CL6012A12 1900303 EA MAIN BATTERY FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) ON SELECTION OF MAIN BATTERY SWITCH, BATTERY POWER FAILED TO POWER UP MAIN BATTERY BUSS. MAIN BATTERY CONTACTOR FA ILED 2 L 7 2 4F RT A21AE 2001032000047 20010320 00047 CE 2001 3 20 CA991230022 1 19991213 A 5740 651102523 ATTACH FITTING CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT & RT NICKED W K NONE O OTHER IN INSP/MAINT 1 CA 3613 (CAN) DURING A PHASE 5 INSPECTION, A NICK WAS FOUND ON THE AFT LUG OF THE UPPER FWD WING ATTACH FITTING. FOLLOWING A REP AIR WHICH INCLUDED BLENDING OF THE AFFECTED AREA OF THE FITTING, AN EDDY CURRENT CHECKOF THE FITTING REVEALED FERROUS ME TAL INCLUSIONS AT SEVERAL LOCATIONS AROUND THE RADIUS OF THE LUG. 1 L 7 2 4F 4 F A22CE E1NE 2001032000048 20010320 00048 CE 2001 3 20 CA991230023 1 19991213 A 5730 65210008 SKIN PANEL CESSNA CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT STUB WING CANNING W K NONE O OTHER IN INSP/MAINT 1 CA 3613 (CAN) 2 STIFFENERS WERE FOUND FWD OF THE REAR SPAR ON THE RIGHT WING, RIVETED TO SUBJECT SKIN PANEL. BOTH STIFFENERS WER E FOUND CRACKED. NO IPC REFERENCE TO THE STIFFENERS EXISTED AND THE SUBMITTER QUESTIONED CESSNA ABOUT THEM. CESSNA STATE D THEY HAD BEEN INSTALLED AT THE FACTORY TO PREVENT SKIN OIL CANNING BUT THERE WAS NO DATA TO APPPROVE THEIR INSTALLATIO N. CESSNA REQUESTED THAT THE STIFFENERS BE REMOVED AND THE SKIN PANEL BE MONITORED FOR CRACKING. 1 L 7 2 4F 4 F A22CE E1NE 2001032000050 20010320 00050 SO 2001 3 20 CA991230027 1 19991208 A 3246 16108000 WHEEL PIPER PA31T PA31T2 7103127 SO PWA PT6 PT6A135 52043 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING TIRE & TUBE REPLACEMENT, THE WHEEL ASSEMBLY WAS INSPECTED AND ONE WHEEL HALF WAS FOUND CRACKED. 1 L 7 2 3T 4 T RT A8EA E4EA 2001032000051 20010320 00051 EA 2001 3 20 CA991230028 1 19991220 A 2742 6009230165 ACTUATOR CNDAIR CL600 CL6001A11 1900302 EA STABILIZER FAILED W O OTHER L NO TEST IN INSP/MAINT 1 CA 3162 (CAN) DURING POST INSTALLATION TESTING,CHANNEL 2 FOUND HARD FAILED. UNIT WAS RECEIVED IN THIS CONDITION FROM SUPPLIER. 0 .0 HOURS 2 L 7 2 4F RT A21EA 2001032100001 20010321 00001 EA 2001 3 21 CA991230029 1 19991220 A 2742 6009230165 ACTUATOR CNDAIR CL600 CL6001A11 1900302 EA STABILIZER INTERMITTENT W K NONE L NO TEST IN INSP/MAINT 1 CA 6600 152E (CAN) DURING POST INSTALLATION TEST, CHANNEL 2 FOUND OPERATING INTERMITTENTLY. DURING TRIM COMMAND MOTOR WOULD OPERATE B UT SCREW JACK WOULD NOT ALWAYS TURN. COMPONENT RECIEVED IN THIS CONDITION FROM SUPPLIER. 2 L 7 2 4F RT A21EA 2001032100002 20010321 00002 EU 2001 3 21 CA991230030 1 19991207 A 7120 837691474 BOLT IAE V2527A5 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ENGINE MOUNT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1108 V10582 (CAN) AFTER ENGINE REMOVAL BOLT SENT FOR NDI AS PER AIRBUS NTM PART 8-51-80-00 AND FOUND CRACK.THIS FAIL SAFE BOLT CAME FROM A QUICK CHANGE KIT RECEIVED FR OM BF GOODRICH WITH LOANER ENG. UPON ENG REMOVAL 333 CYCLES LATER,THE BOLT ARE REQUI RED TO PASS NDI INSP. PRIOR TO REUSE. THE OPERATOR SUSPECTS THE BOLT WAS LIKE THIS FROM FACTORY AND HAS NOT EXPERIENCED A CRACK ON HIS FLEET PRIOR TO THIS OCCURRENCE.QUERY AS TO LAE NDI PROCEDURE PRIOR TO DELIVERY OF QEC ENGINES REQUESTED F ROM SUBMITTER.IAE TO ANNALYSE THE BOLT FOR METALERGICAL PROPERTIES. FURTHER TO FOLLOW.// REPORT RECEIVED CRACK WAS EVIDE NTLYA MANUFACTURED THREAD LAP WHICH CAUSED NDI INDICATION, BOLT MET ALL SPECS. 2 L 7 2 4F 4 F RT A28NM E40NE 2001032100003 20010321 00003 EU 2001 3 21 CA991230031 1 19991209 A 2720 DV84567015 LIMIT SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) ECAM WARNING RUDDER TRAVEL LIMIT NR 1 & 2 ILLUMINATED ON CLIMB. AIRCRAFT LANDED, RUDDER TRAVEL LIMITER REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 2001032100004 20010321 00004 SO 2001 3 21 CA991230032 1 19991211 A 5511 465303 RIB PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA HORIZONTAL STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8331 (CAN) FOUND LEFT HORIZONTAL STABILIZER TIP CRACKED UPPER AND LOWER SKINS AT AFT CORNER. 1 L 7 2 3T 4 T A8EA E4EA 2001032100005 20010321 00005 NM 2001 3 21 CA991230033 1 19991102 A 2133 1036721 OUTFLOW VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE CABIN PRESSURE FAILED W B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA 28445 (CAN) WHILE IN CRUISE FLIGHT, THE AIRCRAFT DEPRESSURIZED. MAINTENANCE REPLACED THE OUTFLOW VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032100006 20010321 00006 2001 3 21 CA991230034 4 19991203 A 3425 7003110901 DISPLAY DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE COCKPIT FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 24430 (CAN) THE CAPTAINS EADI SCREEN HAD NO DISPLAY AND SMELLED BURNED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032100007 20010321 00007 NE 2001 3 21 CA991230035 2 19991208 A 7323 8210176C STUD 8210176C DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE GOVERNOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 5815 (CAN) AFTER SHUTDOWN, OIL WAS FOUND LEAKING FROM THE NR 2 ENGINE. MAINTENANCE FOUND THE OVERSPEED GOVERNOR LEAKING AT A STRIPPED STUD. THE STUD WAS LOOSE IN THE PUMP BODY. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032100008 20010321 00008 NM 2001 3 21 CA991230036 1 19991204 A 2910 82970010609 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT NACELLE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING A PREFLIGHT INSPECTION, HYDRAULIC FLUID WAS NOTICED DRIPPING FROM THE RT ENGINE NACELLE. A PINHOLE WAS FOUN D IN THE PRESSURE LINE FOR THE FORWARD GEAR DOOR ACTUATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032100009 20010321 00009 EU 2001 3 21 CA991230037 1 19991129 A 3234 9746101102 SOLENOID 532311210 PILATS PC12 PC1245 EU MLG SELECTOR STUCK W O OTHER O OTHER CL CLIMB 1 CA 1069 (CAN) AFTER TAKEOFF THE PILOT COULD NOT SELECT THE GEAR UP BECAUSE THE GEAR SELECTOR HANDLE WOULD NOT MOVE. AFTER LANDIN G, MAINTENANCE DISCOVERED THE HANDLE LOCK OUT SOLENOID WAS STIFF TO OPERATE BECAUSE OF HEAVY GREASE ON THE SOLENOID SHAF T. THE SOLENOID WAS CLEANED AND LUBRICATED FOR PROPER OPERATION TO BE RESTORED. 1 L 7 1 3T RT A78EU 2001032100010 20010321 00010 CE 2001 3 21 CA991230038 1 19991213 A 2497 WIRE BEECH 5036430821 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA (CAN) WHEN PILOT SELECTED GEAR DOWN AIRCRAFT EXPERIENCED MULTIPLE FAILURES OF MLG & FLT INSTRUMENTS, ALSO THERE WAS SM OKE IN COCKPIT. PILOT EXTENDED THE MLG MANUALLY & LANDED W/O INCIDENT. MAINT DISCOVERED 2 PROBLEMS: THE WIRE GOING TO BUS FEEDER DIODE WAS NOT PROPERLY CRIMPED & BECAME LOOSE. SOME ARCING OCCURED WHEN WIRE BECAME LOOSE & CAUSED SMOKE. THE CONNECTOR AT ENGINE INSTRUMENT C/B PANEL HAD BECOME CORROADED BECAUSE OF WATER COMING IN SIDE PANEL & NOT ALLOWED CU RRENT GO THROUGH IT, THIS CAUSED MLG & FLIGHT INSTRUMENTS TO FAIL. 1 L 7 2 3T 4 T A14CE E4EA 2001032100012 20010321 00012 CE 2001 3 21 CA991230040 1 19991213 A 7603 5038015221 CABLE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA POWER LEVER STUCK W E ENGINE SHUTDOWN E VIBRATION/BUFFET DE DESCENT 1 CA (CAN) AFTER COMPLETING THE DECENT CHECKS, THE CREW ATTEMPTED TO REDUCE POWER ON BOTH ENGINES. THE POWER LEVER FOR THE RT ENGINE WOULD NOT MOVE. ALL ATTEMPTS TO MOVE THE POWER LEVER WERE UNSUCESSFUL SO THECREW ELECTED TO SHUT THE RT ENGINE DOWN. ON THE GROUND, MAINTENANCE LUBRICATED THE CABLE AND IT APPEARED TO FUNCTION NORMALLY. HOWEVER, UPON RETURN TO BAS E THE CREW DISCOVERED THE SAME FAULT. INVESTIGATION REVEALED THE CASE ON THE CABLE WAS SPLIT IN NUMEROUS PLACES AND THE MOISTURE HAD ENTERED INTO THE STRANDS CAUSING CORROSION. 1 L 7 2 3T 4 T A14CE E4EA 2001032100014 20010321 00014 CE 2001 3 21 CA991230043 1 19991215 A 7500 311351101 DRAIN VALVE PWA 312021201 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE P3 FILTER ASSY STUCK W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 3066 (CAN) THE A/C EXPERIENCED INTERMITENT HUNG STARTS DUE TO THE POPPET DRAIN VALVE WITHIN THE P3 FILTER ASSY REMAINING OPE N. FILTER IS POST SB 1495. 1 H 7 1 3T 3 T A37CE E4EA 2001032100015 20010321 00015 EU 2001 3 21 CA991230044 1 19991215 A 5753 FLAP PILATS PC12 PC1245 EU WINGS FROZEN W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 702 (CAN) THE AIRCRAFT TOOK OFF IN RAIN AT +1 DEGREES CELSIUS. ON APPROACH THE CREW SELECTED FLAPS, NO FLAP MOVEMENT WAS NOT ED AND THE FLAP CAUTION LIGHT ILLUMINATED. THE CREW CARRIED OUT A FLAPLESS LANDING. MAINTENANCE DISCOVERED THE FLAPS WER E FROZEN TO THE LOWER WING SKIN. 1 L 7 1 3T RT A78EU 2001032100016 20010321 00016 EU 2001 3 21 CA991230045 1 19991101 A 2120 MY20721108101 DUCT AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE HEAT EXCHANGER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 188 (CAN) DURING SCHEDULED MAINTENANCE THE HEAT EXCHANGER DUCT WAS FOUND CRACKED. IT HAD BEEN REPLACED 188 HOURS PREVIOUSLY. 2 L 7 2 4F 4 F RT A7EU E7EA 2001032100017 20010321 00017 SO 2001 3 21 CA991230046 1 19991114 A 7603 LINE LYC IO320B1A PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA PRESSURE SENSE CRACKED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA L582855A (CAN) PILOT DISCOVERED LT MANIFOLD PRESSURE GAUGE NOT RESPONDING APPROPRIATELY TO THROTTLE SETTINGS. MAINTENANCE DISCOV ERED A CRACK IN THE LT ENGINE SENSE LINE ABOUT 2 INCH FORWARD OF THE FIREWALL. 1 L 7 2 3O 3 O A1EA 1E12 2001032100018 20010321 00018 2001 3 21 CA991230048 4 19991216 A 3130 HARNESS CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE FLIGHT RECORDER CUT W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 3612 (CAN) FLIGHT DATA RECORDER FAIL LIGHT CAME ON. MAINTENANCE FOUND ONE CORNER OF THE AIR CYCLE MACHINE FLANGING HAD CUT TH ROUGH THE CHAFING PROTECTION AROUND THE WIRE HARNESS AND HAD PENETRATED THE INSULATIONOF ONE WIRE. THE WIRE WAS R12A22 (THE ANNUNCIATOR CIRCUIT). 1 L 7 2 4F 4 F A22CE E1NE 2001032100019 20010321 00019 EU 2001 3 21 CA991230049 1 19991214 A 3213 5321012175 STRUT PILATS PC12 PC1245 EU MLG LEAKING W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 1399 (CAN) WHILE TAXIING, THE AIR GROUND SWITCH ACTIVATED DUE TO A LEAK IN THE LANDING GEAR SHOCK STRUT THAT ALLOWED THE HIGH PRESSURE SIDE TO LEAK INTO THE LOW PRESSURE SIDE. 1 L 7 1 3T RT A78EU 2001032100021 20010321 00021 NE 2001 3 21 CA991231002 2 19991115 A 7310 4024T95P03 CLAMP CNDAIR CL604 CL604 EA GE CF34 CF343B1 NE LT ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 1321 (CAN) V-BAND CLAMP HOLDING THE FCU AND FUEL PUMP FOUND PARTIALLY BROKEN.SB73-003 8 NOT COMPLIED WITH. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032100022 20010321 00022 EA 2001 3 21 CA991231003 2 19991130 A 8500 ENGINE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA RIGHT MAKING METAL W E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CA 2094 (CAN) NON METALIC CHIPS FOUND IN SCREEN BUT NOT IN DISPOSABLE FILTER. ENG REMOVED. 1 L 7 2 3O 3 O A20SO E14EA 2001032100024 20010321 00024 SO 2001 3 21 CA991231007 1 19991205 A 5210 4475004 LATCH PIPER PA31 PA31 7103102 SO LYC O540 LTIO540J2BD 41533 EA PAX DOOR BINDING W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) DURING FLIGHT, ABOUT 22:45 HRS. THE FRONT LEFT DOOR OPENED BY ABOUT 1.THE PILOTS CHECKED THE DOOR AFTER RETURNING TO SEPT-ILES. NO DEFECT FOUND, BUT NOTED THAT THE DOOR HANDLE HAD TO BE PUSHED ALL THE WAY TO REALLY LOCK THE DOOR. T HERE IS NO SYSTEM TO CONFIRM THE LOCKING OTHER THAN FOR THE PILOT. MAINTENANCE ADVISED THE PILOTS. 1 L 7 2 3O 3 O A20SO E14EA 2001032100025 20010321 00025 CE 2001 3 21 CA991231008 1 19991206 A 2140 BLOWER CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO HEATER OVERHEATED W K NONE M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) WHILE TAXIING AND AFTER STARTING THE COMBUSTION HEATER, SMOKE ENTERED THE CABIN. THE CREW SHUT DOWN THE AIRCRAFT A ND DEPLANED THE PASSENGERS AND THEMSELVES. MAINTENANCE DETERMINED THAT THE COMBUSTION HEATER GROUND BLOWER HAD OVERHEATE D. 1 L 7 2 3O 3 O A7CE E8CE 2001032100026 20010321 00026 EA 2001 3 21 CA991231010 1 19991216 A 2913 COUPLING CNDAIR CL215 CL2151A10 EA HYD PUMP WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FOLLOWING A SPECIAL INSPECTION TO CHECK THE HYD PUMP INTERNAL GEARS AS WARRANTED BY EARLIER PROBLEMS, WE FOUND THI S PART TO BE EXCESSIVELY WORN, TO THE POINT OF NOT INSTALLING ON THE A/C. PUMP WAS RECENTLY OVERHAULED AND CERTIFIED BY THE SUPPLIER. 2 H 7 2 4R A14EA 2001032100027 20010321 00027 SO 2001 3 21 CA991231011 1 19991203 A 7111 5142001 MOTOR DUKES PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA COWL FLAP INTERMITTENT W O OTHER O OTHER CL CLIMB 1 CA 260 0379 (CAN) PILOT REPORTED LT COWL FLAP REFUSED TO OPEN IN FLIGHT. MAINTENANCE DISCOVERED ACTUATOR MOTOR OPERATING INTERMITTA NTLY. MOTOR (DUKESP/N:5142-00-1; PIPER P/N475-194) REPLACED.SUBMITTER NOTED THAT ASSEMBLY DATE FOR UNSERVICEABLE PART WA S MARCH 10,1999. 1 L 7 2 3O 3 O A20SO E14EA 2001032100028 20010321 00028 SO 2001 3 21 CA991231013 1 19991215 A 3232 484701 O-RING 31901 PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA DOOR ACTUATOR CUT W K NONE K FLUID LOSS IN INSP/MAINT 1 CA WTC2112 (CAN) PILOT OBSERVED POOL OF HYDRAULIC FLUID RUNNING FROM LT ENGINE NACELLE. MAINTENANCE DISCOVERED LEAKS COMING FROM R OD END OF DOOR ACTUATOR. REPLACED CUT O-RINGS (P/N 484-701)(AN6227-7) (MS28775-012)). 1 L 7 2 3O 3 O 1A10 1E4 2001032100029 20010321 00029 SO 2001 3 21 CA991231014 1 19991203 A 3234 BRACKET PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA MLG SELECTOR BROKEN W L ABORTED APPROACH O OTHER AP APPROACH 1 CA 10002 (CAN) WHEN THE PILOT TRIED TO LOWER THE WHEELS FOR LANDING, THE WHEELS DID NOT EXTEND. AFTER MANY ATTEMPTS AND TRYING W ITH THE EMERGENCY PUMP, THE PILOT MOVED THE LEVER FROM BELOW THE INSTRUMENT PANEL.THE SUPPORT BRACKET OF THE SHAFT WAS F OUND UNSCREWED AND LOOSE. SO WHEN THE LEVER WAS MOVED, THE SHAFT MOVED BUT IT DID NOT ACT UPON THE POWER PACK. 1 L 7 2 3O 3 O A20SO E14EA 2001032100030 20010321 00030 SO 2001 3 21 CA991231015 1 19991217 A 3710 DRIVE SHAFT ARO 212401 PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA LT ENGINE VACUUM SHEARED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 274 15260 (CAN) WHILE IN FLIGHT PILOT NOTICED THE RED NOT SUCTION LIGHT ILLUMINATE. VACUUM PUMP ((P/N:(ARO21240-1) (PIPER32171-000 )). 1 L 7 2 3O 3 O 1A10 1E4 2001032100031 20010321 00031 NM 2001 3 21 CA991231016 1 19991124 A 3231 MPNS4340131004 VALVE AIRBUS A319 A319114 NM MLG FAILED W A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA (CAN) LOUD INTERMITTANT RUMBLE EVIDENT IN FLIGHT ALONG WITH ECAM MESSAGE GEAR DOORS AMBER. LANDING GEAR SAFTEY VALVE RE PLACED. 2 L 7 2 4F RT A28NM 2001032100032 20010321 00032 NE 2001 3 21 CA991231017 2 19991128 A 7320 C2514900 CONTROL UNIT AIRBUS A319 A319114 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED W A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 CA (CAN) NR 2 ENGINE ELECTRONIC POWER PLANT CONTROL UNIT FAILED P/N 182M27P09, AND NR 1 LOW PX TURBINE CLEARANCE ACTUATING CONTROL VALVE FAILED, P/N C2514900. 2 L 7 2 4F 4 F RT A28NM E2GL 2001032100033 20010321 00033 NM 2001 3 21 CA991231018 1 19991207 A 2530 CIRCUIT BREAKER AIRBUS A319 A319114 NM COFFEE MAKER TRIPPED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) IN CRUISE MILD ELECTRICAL SMELL IN GALLEY FOLLOWED BY COFFEE MAKER CB POPPING. REPLACED COFFEE MAKER. 2 L 7 2 4F RT A28NM 2001032100034 20010321 00034 EU 2001 3 21 CA991231019 1 19991126 A 5753 SEAL AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE LE FLAPS MISSING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LEADING EDGE CUSHON SEAL FOUND MISSING ON INBOARD TRAILING FLAP. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100035 20010321 00035 EU 2001 3 21 CA991231020 1 19991127 A 2420 MNP740120C GCU AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA (CAN) AIRCRAFT OPERATING ON MEL WITH FAILED RT IDG. APU SHUTDOWN INFLIGHT CAUSING A LOSS OF ELECTRICAL POWER. AIRARAFT L ANDED AND NR 2 ENGINE GCU AND IDG REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100036 20010321 00036 EU 2001 3 21 CA991231021 1 19991130 A 3610 MPN6713D040000 VALVE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 ENGINE FAILED W O OTHER O OTHER CR CRUISE 1 CA (CAN) UNABLE TO MAINTAIN CABIN PRESSURISATION IN AUTO OR MANUAL MODE. NR 1 HIGH PRESSURE VALVE REEPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100037 20010321 00037 EU 2001 3 21 CA991231022 1 19991130 A 2760 COMPUTER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE SLAT CONTROL FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) ECAM MESSAGE SLAT WARN ILLUMUINATED. AIRCRAFT LANDED SLAT COMPUTER RESET. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100038 20010321 00038 EU 2001 3 21 CA991231024 1 19991208 A 5610 66642024 CONTROLLER AIRBUS AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE HEATER SMOKE W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA (CAN) BOTH WINDSCREENS ARCING AND STRONG SMELL OF SMOKE IN COCKPIT ON APPROACH. AIRCRAFT LANDED BOTH WINDSCREENS AND WIN DSHIELD HEAT CONTROLLER REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100039 20010321 00039 EU 2001 3 21 CA991231025 1 19991210 A 4920 MPN49200011 APU AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE APU BAY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) OILY SMELL IN AIRCRAFT DURING FLIGHT. INVESTIGATION REVEALED APU INTERNAL FAIL 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100040 20010321 00040 EU 2001 3 21 CA991231026 1 19991213 A 4920 49200011 APU AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE APU BAY ODOR W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) PUNGENT SMELL EVIDENT WITH AIR CONDITIONING PACKS ON AND SOURCE SELECTED TOAPU AIR.OIL CONTAMINATION FOUND IN APU COMPARTMENT, APU REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100041 20010321 00041 EU 2001 3 21 CA991231027 1 19991203 A 7600 1960M56P01 ECU AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 3 ENGINE FAILED W A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA (CAN) ENGINE FAILED, RELITE AND SUSEQENT COMPRESSOR STALL EXPERIENCED. ENGINE BORESCOPED WITH NO FAULTS FOUND, BOTH VARI ABLE STATOR ACTS AND ECU REPLACED. 2 L 7 4 4F 4 F RT A197 E37NE 2001032100042 20010321 00042 NE 2001 3 21 CA991231028 2 19991231 A 7250 71007741850 BEARING AIRBUS A340 A340313 EU CFMINT CFM56 CFM565C4 13802 NE NR 3 ENGINE FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) NR 4 BEARING FAILURE ON NR 3 ENGINE, 2 L 7 4 4F 4 F RT A197 E37NE 2001032100043 20010321 00043 NM 2001 3 21 CA991231029 1 19991125 A 2750 285T004950 FSEU BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER DEPARTURE TRAILING FLAPS FAIL MESSAGE. UNABLE TO GET FLAPS TO RETRACT, A/C RETURNED. FLAPS OPERATED AND FLAP S FAILED TO RETRACT. A/C RTU. FLAPS OPERATED AND FLAPS FAILED ON RETRACTION FROM FULL DOWN WITH MESSAGE TRAILING EDGE FL APS SHUT DOWN. FLAP SLAT ELECTRONIC CONTROL UNIT CHANGED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001032100044 20010321 00044 NM 2001 3 21 CA991231030 1 19991203 A 5610 141T480150 WINDSHIELD BOEING BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT FAILED W O OTHER O OTHER AP APPROACH 1 CA (CAN) FIRST OFFICERS WINDSHIELD SHATTERED ON APPROACH, WINDSHIELD REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001032100045 20010321 00045 NM 2001 3 21 CA991231031 1 19991204 A 2910 LINE BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) RT HYD QTY DROPPED STEADILY ABOUT 30-40 PERCENT PER MINUTE. STOPPED AT .43 WHEN PUMPS TURNED OFF. FOUND RT ENG HYD PUMP FLEX LINE WORN THROUGH. REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 2001032100046 20010321 00046 WP 2001 3 21 CA991231032 1 19991121 A 5610 WINDSHIELD DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE COCKPIT ARCED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) DURING RAMP CHECK OBSERVED ARCING AND SMOKE AT TOP OF CENTER OF FIRST OFFICERS WINDSCREEN. RT WINDOW AND HEAT CON TROLLER REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 2001032100047 20010321 00047 WP 2001 3 21 CA991231033 1 19991124 A 2530 RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE OVEN OUTLET LOOSE W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) FLIGHT ATTENDANT RECEIVED SHOCK FROM OVEN WHEN INSERTING OVEN IN TROLLY. OVEN OUTLET HANGING LOOSE AND MISSING PRO NGS FROM PLUG. REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 2001032100048 20010321 00048 WP 2001 3 21 CA991231034 1 19991130 A 2510 SEAT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE COCKPIT DAMAGED W O OTHER O OTHER CR CRUISE 1 CA (CAN) CAPTAINS CHAIR FAILED TO LOCK FORE AND AFT. CHAIR REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 2001032100050 20010321 00050 EA 2001 3 21 CA991231038 1 19991123 A 3222 MPN1612001 STRUT CNDAIR CL600 CL6002B19 EA NLG FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) ON ARRIVAL TO GATE, NOSE OLEO COLLAPSED. CORROSION FOUND ON NOSE GEAR PISTON LOWER END AT AXLE FITTING BOLT HOLE A REA. CORROSION ON PISTON, AXLE FITTING, BOLT BUSHING AND AXLE FITTING. 2 L 7 2 4F RT A21EA 2001032100051 20010321 00051 EA 2001 3 21 CA991231039 1 19991203 A 5600 NP1393226 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE COCKPIT CRACKED W B I EMER. DESCENT CABIN DEPRESSURIZATION O OTHER NR NOT REPORTED 1 CA (CAN) RT WINDSHIELD CRACKED AT 37,000FT. A/C DECENTED AND MANUALLY DEPRESSURIZED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032100052 20010321 00052 EA 2001 3 21 CA991231040 1 19991205 A 2840 7981146 CONTROL PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE FUEL INDICATOR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) FUEL IMBALANCE ON TAKE OFF, LOST FUEL INDICATION IN CLIMB, AUTONATIC TRANFLOW INHIBIT IN CLIMB. FUEL QUANTITY INDI CATORS FLUCTUATING. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032100053 20010321 00053 EA 2001 3 21 CA991231041 1 19991208 A 5210 LATCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR OUT OF RIG W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) PASSENGER DOOR LATCH MESSAGE ON CLIMB FROM WASHINGTON, THEN RED PASS DOOR AND AURAL WARNING. DOOR RE-RIGGED AND A/ C PRESSURIZED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032100054 20010321 00054 EA 2001 3 21 CA991231042 1 19991128 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) FLAP FAIL ON APPROACH. ZERO DEG FLAP LANDING. COULD NOT DUPLICATE ON GROUND AFTER FECU C/B RESET. 2 L 7 2 4F RT A21EA 2001032100055 20010321 00055 EA 2001 3 21 CA991231043 1 19991208 A 4920 APU CNDAIR CL600 CL6002B19 EA APU BAY FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA (CAN) APU OIL PRESSURE EICAS MESSAGE DURING DESCENT. UPON LANDING ROLL APU AUTO SHUTDOWN. 2 L 7 2 4F RT A21EA 2001032100056 20010321 00056 EA 2001 3 21 CA991231044 1 19991208 A 2752 852D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA TE FLAPS DAMAGED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH DURING FLAP SELECTION FROM 30-45 DEG, THE FLAPS STOPPED AT 40 DEG. LT NR 1 ACTUATOR REPLACED. 2 L 7 2 4F RT A21EA 2001032100057 20010321 00057 EA 2001 3 21 CA991231045 1 19991212 A 3234 750006000 VALVE CNDAIR CL600 CL6002B19 EA NLG SELECTOR FAILED W O OTHER J WARNING INDICATION LD LANDING 1 CA (CAN) AIR LITTORAL REPORTED NLG DID NOT EXTEND.RED ALARM GEAR DISAGREE. EMERG. GEAR EXTENSION CARRIED OUT. NOSE DOORS WO ULD NOT MOVE ON THE GROUND. NLG SELECTOR VALVE WAS REPLACED. 2 L 7 2 4F RT A21EA 2001032100058 20010321 00058 EA 2001 3 21 CA991231046 1 19991212 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAPS FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 643 (CAN) FLAP FAIL MESSAGE WHILE CRUISING AT FL280. LANDING UNEVENTALLY WITH ZERO DEG FLAP. BPSU REPLACED. 2 L 7 2 4F RT A21EA 2001032100059 20010321 00059 EA 2001 3 21 CA991231048 1 19991217 A 3220 16144101 TORQUE LINK CNDAIR CL600 CL6002B19 EA NLG BROKEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER T/O WHEN GEAR RETRACTED, RECEIVED GEAR DISAGREE, STEERING INOP, WOW INPUT CAUTION AND WARNING MESSAGES WITH WOW OUTPUTSTATUS MESSAGE. RTB. AT APPROX. 80 KTS, SEVERE VIBRATION AND NO NOSE WHEEL STEERING. TORQUE LINKS FOUND DISSCO NNECTED AND PART OF IT WAS FOUND BROKEN. 2 L 7 2 4F RT A21EA 2001032100061 20010321 00061 EA 2001 3 21 CA991231050 1 19991217 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) FLAPS FAILED AT ZERO DEG. C/B RESET 2 L 7 2 4F RT A21EA 2001032100062 20010321 00062 EA 2001 3 21 CA991231051 1 19991217 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) FLAPS FAILED AT 42 DEG ON APPROACH. C/B RESET 2 L 7 2 4F RT A21EA 2001032100063 20010321 00063 EA 2001 3 21 CA991231052 1 19991217 A 7931 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE NACELLE MALFUNCTIONED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA (CAN) OIL PX OUT OF LIMITS, IFSD COMPLETED. PROBLEM NOT SPECIFICALLY IDENTIFIED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032100064 20010321 00064 EA 2001 3 21 CA991231053 1 19991217 A 7931 OIL FILTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE RT ENGINE CLOGGED W O OTHER J WARNING INDICATION CL CLIMB 1 CA (CAN) HIGH OIL PX ADDRESSED BY REPLACING CLOGGED OIL FILTER, B SUMP REG VALVE AND CLEANED OIL PUMP SCAVENGE SCREENS. NO REASON GIVEN AS TO MATERIAL CLOGGING THESE ITEMS? 2 L 7 2 4F 4 F RT A21EA E15NE 2001032100065 20010321 00065 NE 2001 3 21 CA991231054 2 19991116 A 7314 GP200MK11 PUMP BOEING 757 757236 NM RROYCE RB211 RB211535E437 54555 NE RT ENGINE FAILED W D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA 3946 (CAN) PRECAUTIONARY REPLACEMENT MEASURE TAKEN OF HP FUEL PUMP AS PER MM 2 L 7 2 4F 4 F RT A2NM E12EU 2001032600124 20010326 00124 NE 2001 3 26 CA000203004 2 19991210 A 7300 5002T83P02 PUMP SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE FUEL SYSTEM SEIZED W K NONE E J VIBRATION/BUFFET WARNING INDICATION TX TAXI/GRND HDL 1 CA 1226 (CAN) NO CONTAMINATION WAS FOUND WITHIN THE FCU AND THE FUEL CENTRIFUGAL PURIFI ER. THE EDP MATCHED BEARINGS WERE FOUND SEIZED IN PUMP BODY. FAA AC 43 -16A ISSUED MAY 1999 WAS REFRENCED TO THE OPERATOR AND THEY HAVE REVIEWED THEIR SYSTEMS AND VERIFIED THE USE OF FAUCETT FILTERS AND NOT THE SUSPECT VELC ON FILTERS AS STATED WITHIN THE AC.OPERATOR IS SUSPECTI NG JET B AND THE LACK OF LUBRICATING PROPERTIES AS A POSSIBLE CAUSE. 2 G 7 2 4U 4 U 1H15 1E3 2001032600125 20010326 00125 CE 2001 3 26 CA000203005 1 19991228 A 3250 50820035 ROD BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 18727 (CAN) ROD CORRODED AT CLOSED END. CORROSION PERFORATED THE TUBE WALL A HALF INCH FROM THE END. 1 L 7 2 3T 4 T A14CE E4EA 2001032600288 20010326 00288 EU 2001 3 26 CA000209020 1 19991220 A 3246 TIRE PILATS PC12 PC1245 EU MLG LEAKING W O OTHER O OTHER LD LANDING 1 CA 335 0265 (CAN) DURING THE LANDING ROLL OUT, THE AIRCRAFT SLOWLY PULLED TO THE RIGHT DUE TO A FLAT TIRE. WHILE TRYING TO REINFLATE THE TIRE, IT WAS NOTICED THAT THE WHEEL HAD A LOOSE VALVE CORE. MAINTENANCE REPLACED THE ENTIRE WHEEL ASSEMBLY. 1 L 7 1 3T RT A78EU 2001032600290 20010326 00290 EU 2001 3 26 CA000209028 1 19991221 A 2780 4911710 COMPUTER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE SLAT/FLAPS SYS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) SLAT LOCKED ON APPROACH ACCOMPANIED WITH NR 1 SLAT/FLAP COMPUTER FAIL (SFCC) ECAM WARN ILLUMINATED. SFCC REPLACED . 2 L 7 2 4F 4 F RT A28NM E29NE 2001032600428 20010326 00428 EU 2001 3 26 CA000209036 1 19991224 A 5414 PANEL AIRBUS A340 A340313 EU NR 4 PYLON DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PANEL NEAR LEADING EDGE OF NR 4 PYLON FOUND DELAMINATED. PANEL REPLACED. 2 L 7 4 4F RT A197 2001032600450 20010326 00450 EA 2001 3 26 CA000209048 1 19991229 A 5270 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR DIRTY W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) CREW REPORTED PASSENGER DOOR WARNING MESSAGE SHORTLY AFTER TAKE OFF, A/C RETURNED TO CHIGAGO. CLEANED SENSORS AND BITE CHECK CARRIED OUT OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032600463 20010326 00463 EA 2001 3 26 CA000209061 1 19991204 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT CRACKED W O OTHER L NO TEST AP APPROACH 1 CA 1 (CAN) DURING TEST FLIGHT ON APPROACH FOR AUTO PILOT MOD, RT WINDSHIELD CRACKED. REPLACED 2 L 7 2 4F 4 F RT A21EA E15NE 2001032700181 20010327 00181 NM 2001 3 27 CA991103041 1 19991016 A 2910 8Z6069155 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 2988 (CAN) DURING MAINTENANCE, A HYDRAULIC LEAK WAS NOTED AT THE RIGHT WING ROOT. FOUND HYDRAULIC LINE LEAKING AT FITTING. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032700182 20010327 00182 NM 2001 3 27 CA991103079 1 19991012 A 2780 92CV COMPUTER AIRBUS A319 A319114 NM SLAT CONTROL MALFUNCTIONED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA (CAN) FLIGHT CONTROLS SLATS LOCKED IN FLIGHT WITH WING TIP BRAKE MESSAGE ON ECAM.REPLACED RELAYS 92CV AND 96CV. 2 L 7 2 4F RT A28NM 2001032700183 20010327 00183 2001 3 27 CA991103080 4 19991013 A 2210 MPN102EH2EB SENSOR AIRBUS A319 A319114 NM NR 1 TAT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AUTOPILOT FLIGHT DIRECTOR ETC FAILED IN FLIGHT. NR 1 TAT SENSOR REPLACED. 2 L 7 2 4F RT A28NM 2001032700184 20010327 00184 NM 2001 3 27 CA991103081 1 19991025 A 3010 ANTI-ICE SYSTEM AIRBUS A319 A319114 NM ENGINE LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) ON CLIMBOUT WITH ANTI ICE SELECTED ON A STRONG ODOR AND SLIGHT HAZE WAS NOTICED IN CABIN AND COCPIT. SUSPECTED CAU SE WAS INJESTATION OF DEICE FLUID INTO ACU INTAKE. 2 L 7 2 4F RT A28NM 2001032700185 20010327 00185 EU 2001 3 27 CA991103084 1 19991018 A 5210 STOP AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE PAX DOOR HANDLE OUT OF ADJ W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA (CAN) L1 CABIN DOOR VERY HARD TO OPEN. INNER HANDLE STOP ADJUSTED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032700186 20010327 00186 EU 2001 3 27 CA991103085 1 19991021 A 2742 MPN47045131 ACTUATOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE STAB TRIM FAILED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA 21726 (CAN) POST TAKE OFF ECAM MESSAGE, FLIGHT CONTROL ELEVAT0OR AILERION COMPUTER FAULTS 1 AND 2. AIRCRAFT DIVERTED AND LANDE D. REPLACED HORIZONTAL STAB PITCH TRIM ACTUATOR (HSTA) 2 L 7 2 4F 4 F RT A28NM E29NE 2001032700187 20010327 00187 EU 2001 3 27 CA991103086 1 19991023 A 5270 ABS012110 SENSOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE MLG DOOR FAILED W O OTHER O OTHER LD LANDING 1 CA (CAN) RT GEAR DOOR REMAINED OPEN ON LANDING. PROX SENSOR REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032700188 20010327 00188 NM 2001 3 27 CA991103097 1 19991102 A 3246 431276B BOLT BOEING 757 757236 NM RROYCE RB211 RB211535E437 54555 NE MLG WHEEL BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSP FOUND MW WITH WITH PORTION OF LUG BOLT MISSING. BOLTS REPLACED . 2 L 7 2 4F 4 F RT A2NM E12EU 2001032700189 20010327 00189 EA 2001 3 27 CA991116028 2 19991104 A 8530 STUD PIPER PA34 PA34200 7103405 SO LYC O360 LIO360C1E6 41515 EA NR 3 CYLINDER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ITEM SENT FOR TRANSLATION./ STUDS FOUND BROKEN ON NR 3 CYLINDER, WITH CYLINDER BACKED OFF. 1 L 7 2 3O 3 O A7SO 1E10 2001032700190 20010327 00190 EA 2001 3 27 CA991208077 2 19991026 A 7200 ENGINE BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA RIGHT FAILED W O OTHER O OTHER IN INSP/MAINT 1 CA (CAN) NEW O/H ENGINE INSTALLED, OIL PX LOW AND NOT DUE TO POWER SECTION OR PX RELIEF VALVE. OIL PX PUMP HOUSING DAMAGED. 1 L 7 2 3T 4 T A14CE E4EA 2001032700191 20010327 00191 EA 2001 3 27 CA991209002 1 19991111 A 2435 230481470 LINER DHAV DHC6 DHC6200 EA BEARING WRONG PART W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UNIT SENT FOR OVERHAUL. DURING INSPECTION IT WAS NOTED THAT THE DRIVE END BALL BEARING LINER HAD BEEN REPAIRED WIT H A COPPER LIKE PLATING, IN ORDER TO RESTORE THE LINERS ORIGINAL DEMENSIONS. ALTHOUGH A PLATING REPAIR IS AVAILABLE IN O RDER TO ACCOMPLISH THIS, THE REPAIRS MADE WERE NOT UP TO THE LUCAS STANDARD. THE END BELL WAS REPAIRED USING THE LUCAS S TANDARD. 1 H 7 2 3T A9EA 2001032700192 20010327 00192 EU 2001 3 27 CA991209011 1 19991113 A 3233 200498005 ACTUATOR FOKKER F28 F28MK1000 4990808 EU DOWNLOCK INTERMITTENT W O OTHER J WARNING INDICATION DE DESCENT 1 CA 7979 (CAN) ON GEAR DOWN SELECTION RT MLG WOULD NOT INDICATE DOWN AND LOCKED. SEVERAL ATTEMPTS TO EXTEND UNCESSFOU ALTERNATE E XTENSION UNCESSFUL. A/C LANDED SUCCESSFUL. A/C FERRIED FOR MAINT. DOWNLOCF ACTUATOR INTERMITTENT, REPLACED. 2 L 7 2 4F RT A20EU 2001032800041 20010328 00041 EA 2001 3 28 CA991209023 1 19990923 A 5711 89WM13453 SPAR CAP DHAV DHC2 DHC2* 2800108 EA WRIGHT R1820 982C9HE2 67020 EA WING CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 6256 (CAN) DURING A ROUTINE ULTRASONIC INSPECTION AS PER CF83-23, SPAR CAP INSPECTION, A DEFECT WAS DETECTED BEHIND AN INTACT HINGE TANG IN THE UPPER SPAR CAP AREA. UPON FURTHER INVESTIGATION OF THE DEFECTIVE SECTION IT WAS NOTED THE CORROSION HAD ORIGINATED FROM THE END OF A MILLED SECTION OF THE SPAR CAP EXTRUSION (UPPER OUTBOARD END). IT IS QUESTIONABLE IF T HIS DEFECT COULD HAVE BEEN DETECTED USING THE APPROVED ALTERNATIVE DYE PENTRANT INSPECTION. REPAIRED AS PER DRAWING NO. CON 1542A57108, SPAR CAP SPLICE - REAR BEAM UPPER CAP. APPROVAL NO. P-RDA94-2481D. 1 H 7 1 3R 4 R A806 E259 2001032800053 20010328 00053 GL 2001 3 28 CA991209040 3 19991111 A 6111 F8052 BLADE PIPER PA46 PA46310P 7104605 SO HARTZL HCC2Y BHCC2YF1 GL PROPELLER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 1350 (CAN) CORROSION FOUND UNDERDEICE BOOTS. 1 L 7 1 3O RT A25SO 5 C P920 2001032800104 20010328 00104 NM 2001 3 28 CA000110046 1 19991215 A 2910 82950010269 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 22620 (CAN) WHEN TOPPING UP THE HYDRAULIC SYSTEM, A LEAK WAS NOTICED ON THE RIGHT WING. INVESTIGATION REVEALED THAT IT WAS COM ING FROM A PINHOLE LEAK IN THE RIGHT HAND LIFT DUMP PRESSURE LINE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032800107 20010328 00107 EU 2001 3 28 CA000110052 1 19991221 A 5610 9598110121 WINDOW PILATS PC12 PC1245 EU COCKPIT DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 1459 (CAN) COCKPIT DV WINDOW FOUND TO BE DELAMINATING AROUND SCREW HOLES. 1 L 7 1 3T RT A78EU 2001032800108 20010328 00108 EU 2001 3 28 CA000110053 1 19991223 A 3242 959560151 BRAKE ASSY PILATS PC12 PC1245 EU LEFT & RIGHT FROZEN W O OTHER O OTHER LD LANDING 1 CA (CAN) BOTH LEFT AND RIGHT BRAKES FROZE AND ON LANDING BOTH WHEELS SKIDDED, CAUSING THE TIRES TO FAIL. 1 L 7 1 3T RT A78EU 2001032800109 20010328 00109 CE 2001 3 28 CA000110056 1 19991130 A 2140 1025 HEATER BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA CABIN FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) AIRCRAFT LEFT SIOUX LOOKOUT AND HAD TO RETURN DUE TO SMOKE. THE COMBUSTION HEATER WAS FOUND TO BE THE PROBLEM. 1 L 7 2 3T 4 T A14CE E4EA 2001032800110 20010328 00110 CE 2001 3 28 CA000110057 1 19991223 A 3411 PITOT TUBE BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA AIRSPEED FROZEN W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA (CAN) TAKE-OFF ABORTED DUE TO NO AIRSPEED INDICATION. FROZEN PITOT TUBE. MOISTURE DRAINED AND RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 2001032800111 20010328 00111 EA 2001 3 28 CA000110059 2 19991231 A 7250 3032651 VANE BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA PCE50392 (CAN) OPERATOR EXPRESSES THAT OEM INSERT REPAIR TO T/EDGES OF VANESDOES NOT LAST AND CAUSES SIGNIFICANT DAMAGE TO ENGINE . 1 L 7 2 3T 4 T A14CE E4EA 2001032800126 20010328 00126 EA 2001 3 28 CA000110079 1 19991217 A 3310 RHEOSTAT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE FLOOD LIGHT BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA (CAN) ON INITIAL FLOOD LIGHT SELECTION AN ELECTRICAL ARC AND SMOKE EMERGED FROM THE FIRST OFFICER SIDE PANEL. CB POPPED AND SMOKE STOPPED. FOUND RHEOSTAT BEHIND PANEL BURNED, HEAT DAMAGE FOUND ON WIRES. ALL EFFECTED PARTS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032800127 20010328 00127 EA 2001 3 28 CA000110080 1 19991222 A 5210 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR FOULED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) PASSENGER DOOR HANDLE MESSAGE DURING CLIMB THROUGH FL220. WHILE PERFORMING QUICK REFERENCE HANDBOOK PROCEDURE, PAS SENGER DOOR WARNING MESSAGE CAME ON.REMOVED GRAVEL FROM DOOR SEAL, DEPRESSOR AND SILL AREA, DOOR CLOSED AND CONFIRMED ST OWED AND LOCKED. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032800128 20010328 00128 NM 2001 3 28 CA000110081 1 19991209 A 4920 MPN49200011 APU AIRBUS A319 A319114 NM APU BAY CONTAMINATED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) OILY SMELL IN AIRCRAFT DURING FLIGHT. INVESTIGATION REVEALED APU INTERNAL FAILURE 2 L 7 2 4F RT A28NM 2001032800129 20010328 00129 NM 2001 3 28 CA000110082 1 19991223 A 2510 TAA1233PE0101 SEAT AIRBUS A319 A319114 NM COCKPIT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PILOTS SEAT WOULD NOT STAY IN UPRIGHT POSITION. SEAT REPLACED. 2 L 7 2 4F RT A28NM 2001032800130 20010328 00130 NE 2001 3 28 CA000110084 2 19991221 A 7530 MOTOR GE CFM565A1 AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA 731335 (CAN) COMPRESSOR FAULT MESSAGE DISPLAYED.VARIABLE BLEED VANE GEAR MOTOR ASSY REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032800131 20010328 00131 EU 2001 3 28 CA000110085 1 19991222 A 2530 MPN4110001145 COFFEEMAKER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE GALLEY SHORTED W H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 CA (CAN) FLIGHT ATTENDANT REPORTED RECIEVING AN ELECTRICAL SHOCK FROM COFFEEMAKER. COFFEEMAKER REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032800132 20010328 00132 NE 2001 3 28 CA000110086 2 19991224 A 7200 71200011 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 SURGES W E ENGINE SHUTDOWN R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 CA (CAN) ENGINE SURGES EXPERIENCED, N1 FLUCTUATIONS THEN ENGINE STALLED ON APPROACH. EGT HIT 700C, FIRE SURPRESSION INITIAT ED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032800133 20010328 00133 EU 2001 3 28 CA000110087 1 19991218 A 2761 MPNS43000460 ACTUATOR AIRBUS A340 A340313 EU NR 5 SPOILER LEAKING W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA (CAN) GREEN HYD SYS QUANTITY DROPPED TO ZERO, 1 & 4 PUMPS SHUT OFF AND ALTERNATE GEAR SELECTION CARRIED OUT. INVESTIGATI ON REVEALED NR 5 RT SPOILER SERVO ACTUATOR LEAKING. 2 L 7 4 4F RT A197 2001032800145 20010328 00145 EA 2001 3 28 CA000110096 1 19991217 A 3600 89034607 COMPRESSOR FRCHLD F27 F27F 3373008 EA RROYCE DART DART5297E 54507 EU PNEUMATIC SYS SEPARATED W E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CA 986 (CAN) STAGE 2 CYLINDER FOUND SEPARATED FROM PNEUMATIC COMPRESSOR CAUSING CASING CAUSING GEAR BOX OIL LOSS. 2 H 7 2 4T 4 T 7A1 E297 2001032800146 20010328 00146 SO 2001 3 28 CA000110097 1 19991223 A 5541 4004400 RIB 4004626 PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12015 (CAN) RUDDER TIP RIB AND FORWARD BRACING CHANNEL WERE FOUND TO BE CRACKED DURING A 1000 HR INSPECTION. CRACKS WERE FOUN D AROUND THE NUTPLATES HOLDING THE BALANCE WEIGHT ON TOP OF THE RUDDER. HARDWARE SECURING THE WEIGHT BECAME LOOSE AND W AS UNDETECTED UNTIL NOW.SUBMITTER SUGGESTS THIS TO BE AN AREA OF CONCERN, PARTICULARLY ON OLDER AIRCRAFT. 1 L 7 2 3O 3 O A20SO E14EA 2001032800147 20010328 00147 SW 2001 3 28 CA000110099 1 19991230 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW ROTOL R321 R321482F8 GL MLG FAILED W L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 CA (CAN) LANDING GEAR IN TRANSIT LIGHT NOT OPERATING. MAINTENANCE REPLACED SWITCH ON NOSE GEAR 2 L 7 2 4T RT A8SW 6 C P61GL 2001032800148 20010328 00148 CE 2001 3 28 CA000118001 1 19990923 A 7120 BRACE BEECH 95910005 BEECH 95 D95A 1153408 CE LYC O360 IO360B1B 41514 EA ENGINE MOUNT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 6229 (CAN) THE AIRCRAFT WAS IN FOR A 100 HR. INSPECTION. WHEN THE COWLS WERE REMOVED FROM THE RT ENGINE IT WAS NOTICED THAT A N O/B DIAGONAL BRACE WAS BROKEN. THE MOUNT WAS REMOVED AND SHIPPED TO AN APPROVED AMO FOR WELDING REPAIRS AND TUBE REPLA CEMENT. 1 L 7 2 3O 3 O 3A16 1E10 2001032800150 20010328 00150 EA 2001 3 28 CA000118004 1 19991227 A 5210 NP15790214 WINDOW DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE PAX DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13171 (CAN) DURING SCHEDULED MAINTENANCE, A 4 INCH CRACK WAS FOUND IN THE RIGHT SIDE COCKPIT DV WINDOW 2 H 7 2 4T 4 T RT A13NM E20NE 2001032800158 20010328 00158 NE 2001 3 28 CA000118029 2 19991229 A 7321 4503034 FUEL CONTROL STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE ENGINE FAILED W E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 CA 925 (CAN) TACH VALVE GUIDE PIN BACKED OUT WHICH DAMAGED THE BALLHEAD RETAINER AND THE BEARING SEIZED. THE FCU COUPLING WAS A LSO DAMAGED AS A RESULT. PIN HAS PRELOAD AND IS BRAISED IN DURRING ASSY. THIS IS THE FIRST INSTANCE NOTED AND WOODWARD I S INVESTIGATING. 2 H 7 2 4T 4 T A41EU E4EA 2001032800189 20010328 00189 EU 2001 3 28 CA000118032 1 19991215 A 2150 AR360000150B ACTUATOR 14640113A AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE CONDITION VALVE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 8 8302 (CAN) THE CONDITIONING VALVE(23D) FAILED TO OPEN AFTER TAKEOFF. THE CABIN FAILED TO PRESSURIZE AS A RESULT. MAINTENANCE FOUND THE CONDITIONING VALVE ACTUATOR MOTOR JAMMED DUE TO A FAILURE OF ONE OF THE LIMIT SWITCHES. THE MOTOR HAD BEEN REP LACED 3 DAYS PREVIOUSLY. 2 L 7 2 4F 4 F RT A7EU E7EA 2001032800205 20010328 00205 EU 2001 3 28 CA991231056 1 19991214 A 6710 BUSHING SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) T/R PITCH LINK WAS REMOVED FOR I INSPECTION. SILENT BLOCK (ELASTOMERIC BUSHING)INNER RACE OF BEARING WAS FOUND CRA CKED (9MM). 1 G 7 1 3U 3 U NC H9EU E19EU 2001032800206 20010328 00206 WP 2001 3 28 CA991231057 1 19991119 A 5270 SENSOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE AFT CARGO DOOR OUT OF ADJ W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA (CAN) AFT CARGO DOOR UNSAFE WARN ILLUMINATED ON TAXI. DOOR WARN SWITCH TARGET ADJUSTED. 2 L 7 3 4F 4 F A23WE E12EU 2001032800207 20010328 00207 EA 2001 3 28 CA000118052 2 19991206 A 8530 38135015 STUD PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA CYLINDER BROKEN W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 1871 (CAN) CYLINDER STUDS FAILED. STUDS WERE REINSTALLED AFTER PREVIOUS CYLINDER REPLACEMENT. AT INSTALLATION NO DEFECTS WERE NOTED ON REUSED STUDS. 1 L 7 2 3O 3 O A20SO E14EA 2001032800209 20010328 00209 WP 2001 3 28 CA991231058 1 19991209 A 2400 9811P571 CONNECTOR LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE COCKPIT ARCED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING C CHECK MAINT FOUND ONE WIRE FROM HARNESS OF CONNECTOR 9811-P571 ENGINE START CONTROLPANEL ARCING ON THE BA CKSHELL OF THE CVR CONNECTOR 23-71-P1. INSULATION IN AREA FOUND BURNT AND MELTED. FLEET CAMPAIGN INITIATED. INVESTIGATIO N REVEALED POSITIONING OF THE BACKSHELL TO HAVE CAUSED PROBLEM. 2 L 7 3 4F 4 F A23WE E12EU 2001032800210 20010328 00210 2001 3 28 CA991231060 4 19991116 A 3197 WIRE CNDAIR CL601 CL6012A12 1900303 EA NR3 JUNCTION BOX BURNED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) DURING CRUISE C/B B247 (HYD FAN CONTROL)POPPED. AT THAT TIME THERE WERE NO FAULTS OR MASTER CAUTION LIGHTS. C/B WA S RESET AND POPPED AGAIN. THEN THE LT ENGINE 10TH STAGE AIR LIGHT ILLUMINATED. CREW TRIEDTO OPERATE 10TH STAGE VALVE, BU T THE LIGHT STAYED ON. TEN MINUTES LATER CREW NOTICED NR 3 HYD QUANTITY SLOWLY GOING DOWN. MAINTENANCE CHECKED WITH NO L OSS OF FLUID FROM NR 3 SYSTEM. FURTHER INVESTIGATION FOUND WIRE BUNDLES FROM CONNECTORS P76 & P80 BURNT TO THE EXTENT SE VERAL WIRES WERE BARE AND BURNT THROUGH. NO SIGH OF CHAFING WAS FOUND. WIRE SHIELDING FROM ONE OF THE WIRES IN THE BUNDL E SHORTED. 2 L 7 2 4F RT A21AE 2001032800211 20010328 00211 SO 2001 3 28 CA991231062 2 19990222 A 8520 SAHS24665227 COTTER PIN PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360E 17025 SO NR 2 CONNECT ROD BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 100 (CAN) COTTER PIN FOUND IN OIL SCREEN AT 100HR INSP. 1 L 7 2 3O 3 O A7SO E9CE 2001032800212 20010328 00212 SO 2001 3 28 CA991231063 2 19990222 A 8520 643633 CRANKSHAFT PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360E 17025 SO ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1245 (CAN) TWO CRACKS FOUND BY NDI SHOP, CRANK REJECTED. 1 L 7 2 3O 3 O A7SO E9CE 2001032800213 20010328 00213 CE 2001 3 28 CA991231064 1 19991208 A 5610 50420006933 WINDSHIELD BEECH 100 B100 1152919 CE GARRTT TPE331 TPE3316252B 01514 WP COCKPIT CRACKED W I CABIN DEPRESSURIZATION O OTHER CR CRUISE 1 CA 1847 (CAN) IN CRUISE, THE PILOT NOTICED A 2 INCH CRACK AT THE TOP RIGHT OF THE LEFT WINDSCREEN.THEY DEPRESSURIZED AND CONTINU ED TOWARDS THE MAINTENANCE BASE.THE WINDSCREEN HAD ONLY 2 1/2 YEARS SINCE INSTALLATION. WE COMMUNICATED WITH THE AIRCRA FT BUILDER AND WERE TOLD THAT THAT WAS NEAR NORMAL. 1 L 7 2 4T 4 T A14CE E2WE 2001032800216 20010328 00216 CE 2001 3 28 CA000120001 1 19991228 A 2730 12952408525 CONTROL CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ELEVATOR FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 5539 (CAN) DURING INSPECTION OF CONTROL CABLES BENEATH FLOORBOARDS, IT WAS DISCOVERED THAT THE ELEVATOR DOWN CABLE WAS FRAYED AT STATION 522.5, LOCATED UNDER THE AFT CARGO FLOOR. THE CABLE HAD RUBBED THROUGH ITS PHENOLIC BUMPER ALLOWING IT TO R UB AGAINST THE EDGE OF THE LIGHTENING HOLE. CABLE & BUMPER REPLACED. ADJUSTMENTS MADE TO ALLOW MAXIMUM CLEARANCE THROU GHOUT ITS RUN. 2 L 7 2 4T 4 T RT A24CE E26NE 2001032800221 20010328 00221 EU 2001 3 28 CA000110001 1 19991101 A 6520 369D25418 BEARING HUGHES 369 369FF EU ALLSN 250C 250C30 03013 GL GEARBOX MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 1372 (CAN) INPUT ALIGNMENT BEARING MAKING METAL. GEARBOX STRIPPED TO DETERMINE CAUSE OF PROBLEM.(CHIP LLTE IN FLIGHT) 1 G 7 1 3U 3 U H3WE E1GL 2001032800222 20010328 00222 WP 2001 3 28 CA000110002 1 19991004 A 6520 369D25418 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL GEARBOX MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 1267 (CAN) INPUT ALIGNMENT BEARING MAKING METAL (CHIP LITE IN FLIGHT). GEARBOX STRIPPED TO DETERMINE CAUSE OF METAL GENERATIO N. 1 G 7 1 3U 3 U H3WE E4CE 2001032800224 20010328 00224 WP 2001 3 28 CA000110004 1 19991014 A 6420 369D25418 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL GEARBOX MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 517 (CAN) INPUT ALIGNMENT BEARING MAKING METAL. (CHIP LITE IN CRUISE). GEARBOX STRIPPED TO DETERMINE CAUSE OF FAILURE. 1 G 7 1 3U 3 U H3WE E4CE 2001032800225 20010328 00225 NE 2001 3 28 CA000110005 2 19990924 A 7210 218001602 SPUR GEAR BELL 214 214B1 1182105 SW LYC T55 T5508D 41555 NE GEARBOX BROKEN W O OTHER E J VIBRATION/BUFFET WARNING INDICATION HO HOVERING 1 CA 3444 (CAN) SPUR GEAR THAT DRIVES FCU FAILED. THIS WAS SPECIFIED TO BE A GEAR ALLIENMENT PROBLEM ORIGINATING AT MANUFACTURE. TSB NOTIFIED BY OPERATOR. BULLETIN EXPECTED TO FOLLOW FROM ALLIED TO HAVE RGB BORE ALIGNMENT CHECKED AT O/H. 2 G 7 1 4U 4 U H6SW E4NE 2001032800256 20010328 00256 SW 2001 3 28 CA000120012 1 19991231 A 2460 AN32302 SWITCH FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C652 NE RT BUS TIE DAMAGED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 323 (CAN) DURING FLIGHT, THE CREW SMELLED A BURNING / ELECTRICAL SMELL, FOLLOWED SHORTLY BY THE LOSS OF A ''FEW'' ELECTRICAL SYSTEMS. MAINTENANCE PERSONNEL FOUND THE RIGHT BUS TIE SWITCH BURNED AND MELTED. THE CAUSE OF THE SWITCH OVERHEAT COND ITION WAS LOOSE TERMINAL NUTS ON THE SWITCH. THE AIRCRAFT HAD 323 HOURS SINCE NEW. 2 L 7 2 4T 4 T RT A18SW E4WE 6 C 3PNE 2001032800268 20010328 00268 EU 2001 3 28 CA000120033 1 19990622 A 2810 350A77121321 PLUG SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL TANK WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION OF FUEL TANK AREA, THE AME PLACED FINGER PRESSURE ON CENTRE PORTION OF PLUG WHICH CAUSED THE RUB BER TO STRETCH AND A FATIGUE LINE APPEARED ON THE BOND LINE OF THE CAP END TO CYLINDRICAL SECTION OF PLUG. A SECOND PLUG WAS FOUND IN A SIMILAR CONDITION & A FLEET WIDE INSPECTION WAS INSTITUTED. 1 G 7 1 3U 3 U NC H9EU E19EU 2001032800269 20010328 00269 EU 2001 3 28 CA000120034 1 19990917 A 2913 704A33690004 BELT SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A3 41560 NE HYD PUMP DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 293 (CAN) HYDRAULIC PUMP BELT WAS NOTED TO BE COMING APART AT THE SEAM. THERE HAVE BEEN A NUMBER OF PROBLEMS WITH THESE BELT S FAILING PREMATURELY. 1 G 7 1 3U 3 U H9EU E5NE 2001032800271 20010328 00271 EA 2001 3 28 CA000120036 2 19991125 A 8530 SL75089 PISTON LYC IO320B1A PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 668 L68555 (CAN) NO INDICATION AT COMPRESSION TEST OR IN OIL FILTER BUT OIL WOULD NOT DRAINFROM THE SUCTION SCREEN. PIECES OF PISTO N SKIRT FOUND WHEN SUMP REMOVED. 1 L 7 2 3O 3 O A1EA 1E12 2001032800297 20010328 00297 EU 2001 3 28 CA000128041 1 19991230 A 3222 SEAL PILATS PC12 PC1245 EU NLG STRUT LEAKING W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 721 (CAN) AFTER TAKEOFF THE CREW NOTICED THAT THE NOSE GEAR IN TRANSIT LIGHT WAS SLOW TO GO OUT. AFTER THE AIRCRAFT LANDED, MAINTENANCE PERSONELL NOTICED SCRATCHES/GOUGES IN BOTH SIDES OF THE NOSE GEAR FORK. THE NOSE GEAR STRUT HAD FAILED TO FU LLY EXTEND AFTER LIFTOFF CAUSING THE NOSE GEAR FORK TO INTERFERE WITH THE GEAR DOOR RETRACTION MECHANISM DURING RETRACTI ON.THIS WAS CAUSED BY A FAILURE OF THE SEAL BETWEEN THE LOW AND HIGH PRESSURE SIDES OF THE STRUT SHOCK ABSORBER. 1 L 7 1 3T RT A78EU 2001032800298 20010328 00298 SO 2001 3 28 CA000128042 2 19991214 A 8530 653446A1 CYLINDER CESSNA 206 U206D 2073342 CE CONT O520 IO520F 17032 SO MCAULY 2A34C D2A34C58 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 562 (CAN) CYLINDER FOUND CRACKED AT UPPER SPARK PLUG HOLE MOVING FWD PAST THE INBRD SIDE OF THE INJECTOR HOLE. 1 H 7 1 3O 3 O A4CE E5CE 5 C P3EA 2001032800307 20010328 00307 SW 2001 3 28 CA000128052 1 19991227 A 3250 3505051 SERVO VALVE SWRNGN SA226 SA226AT 8780405 SW GARRTT TPE331 TPE33110 01514 WP NLG STEERING INTERMITTENT W A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CA (CAN) DURING TAKEOFF THE AIRCRAFT PULLED SLIGHTLY TO THE LEFT WHEN THE PILOT RELEASED THE NOSE GEAR STEERING BUTTON. AFT ER TAKE OFF, THE CREW SELECTED GEAR UP AND THE NOSE GEAR IN TRANSIT LIGHT STAYED LIT. AN ATTEMPT TO LOWER THE GEAR NORMA LLY AND USING THE EMERGENCY EXTENSION FAILED TO EXTINGUISH THE IN TRANSIT LIGHT AND THE NOSE GEAR STAYED IN THE WHEEL WE LL. THE AIRCRAFT LANDED WITH THE NOSE GEAR RETRACTED. MAINTENANCE TRACED THE PROBLEM TO THE NOSE GEAR STEERING SERVO VAL VE. 2 L 7 2 4T 4 T RT A5SW E4WE 2001032800315 20010328 00315 CE 2001 3 28 CA000128062 1 19991215 A 2752 1013800006 DRIVE SHAFT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TE FLAP ACTUATOR BROKEN W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 8300 (CAN) AFTER LANDING THE PILOT SELECTED THE FLAP UP AND THEY JAMMED AT 17 DEGREES. INVESTIGATION FOUND THE RT OUTBOARD F LAP FLEX DRIVE WAS BROKEN APPROXIMATELY 24 INCHES FROM THE END.DAMAGED PARTS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 2001032800316 20010328 00316 CE 2001 3 28 CA000128063 1 19991228 A 2110 206SZZC BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COMPRESSOR WORN W O OTHER O OTHER LD LANDING 1 CA (CAN) DURING REMOVAL OF THE COMPRESSOR SUPPORT ASSY FOUND PULLEY ) WAS CHAFFING AGAINST THE COMPRESSOR DRIVE SUPPORT ). BOTH PARTS WERE WORN DUE TO FRICTION.ALSO FOUND THEQUILL SHAFT TEETH BADLY DAMAGED AND THE BEARING EDGE WORN.SUSPECT TH E BEARING LOCATED IN THE CAP SLID AND CAUSED PLAY IN THE PULLEY DRIVE. ALL DAMAGED PARTS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 2001032800317 20010328 00317 CE 2001 3 28 CA000128064 1 19991107 A 3020 MS16555622 PIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CONTROL LINKAGE WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING MAINTENANCE INSPECTION, FOUND PARTS OF THE INERTIAL ICE VANE CONTROL LINKAGE LYING ON THE BOTTOM OF THE COW LING JUST BELOW INLET SCREEN. HARDWARE REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 2001032800318 20010328 00318 SW 2001 3 28 CA000110006 1 19991220 A 2913 357950120053 SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL DRIVE END STRIPPED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) HYDRAULIC SYSTEM FAILURE WHICH WAS LATER ATTRIBUTED TO COUPLING FAILURE INSIDE HYD PUMP. 1 G 7 1 3U 3 U H2SW E4CE 2001032800319 20010328 00319 NE 2001 3 28 CA000110008 2 19991215 A 7230 210193006 BEARING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 MAKING METAL W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 17585 (CAN) REPORT TO FOLLOW. RETAINING PIN ON NR 2 BEARING PACK FAILED. 2 H 7 4 4F 4 F RT A49EU E6NE 2001032800320 20010328 00320 EU 2001 3 28 CA000110009 1 19991214 A 3350 6035501 POWER SUPPLY BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN INTERMITTENT W K NONE L NO TEST IN INSP/MAINT 1 CA 3952 1087 (CAN) FLIGHT CREW REPORTED EMERGENCY LIGHTS IN FORWARD CABIN INTERMITTENT OPERATION. POWER SUPPLY FOUND AT FAULT, REPLAC ED. 2 H 7 4 4F 4 F RT A49EU E6NE 2001032800321 20010328 00321 NM 2001 3 28 CA000110010 1 19991228 A 2424 31343551608003 GCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 GENERATOR FAILED W C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 CA 22727 2724 559 (CAN) DURING THE TAKEOFF ROLL,THE NR 1 AC GENERATOR CAUTION LIGHT CAME ON. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETU RNED TO MAINTENANCE. MAINTENANCE REPLACED THE AC GCU AND RETURNED THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032800322 20010328 00322 NM 2001 3 28 CA000110011 1 19991228 A 3240 82940010101 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PARKING BRAKE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) THE PARKING BRAKE WAS FOUND TO BE LOOSING PRESSURE WHILE UNDERGOING MAINTENANCE. INVESTIGATION REVEALED THE PARKIN G BRAKE PRESSURIZING LINE WAS CRACKED AND LEAKING FLUID. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032800326 20010328 00326 NE 2001 3 28 CA000110012 2 19991220 A 7320 324485318 FUEL CONTROL PWA PW123 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE ENGINE FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA 6112 895 123116 (CAN) ENGINE TORQUE WOULD NOT GO BELOW 27 PERCENT AT FLIGHT IDLE. MFC CHANGED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032800327 20010328 00327 EA 2001 3 28 CA000110013 1 19991230 A 3320 BV0330012150 RECEPTACLE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE CABIN SHORTED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) THE FLIGHT CREW REPORTED A BURNING/ELECTRICAL SMELL COMING FROM THE CABIN OVERHEAD LIGHTS. MAINTENANCE FOUND THE L IGHT SOCKET ON THE FLOURECENT CABIN LIGHT ASSEMBLY AT ROW 6 (LT) BURNED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032800328 20010328 00328 EA 2001 3 28 CA000110014 1 19991227 A 3610 7821004 SWITCH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE BLEED AIR FROZEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) THE FLIGHT CREW EXPERIENCED POWER SURGES ON BOTH ENGINES ON TAKEOFF AND CLIMB. BLEED AIR WAS SELECTED OFF AND THE AIRCRAFT RETURNED FOR LANDING. MAINTENANCE INVESTIGATION REVEALED THAT THE AIR CONDITIONING BLEED AIR SWITCHESAND LINES HAD BEENCONTAMINATED WITH WATER CAUSING THE SWITCHES TO FREEZE. THE SWITCHES WERE REMOVED, CLEANED AND REINSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032800332 20010328 00332 NE 2001 3 28 CA000110023 2 19991020 A 7321 6003T91P13 FUEL CONTROL SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE ENGINE FAILED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION TX TAXI/GRND HDL 1 CA 3204 (CAN) FUEL CONTAMINATION WAS FOUND WITHIN THE FCU AND THE FUEL CENTRIFUGAL PURIFIER. THE PURIFIER HAS BEEN SENT FOR TEAR DOWN. 2 G 7 2 4U 4 U 1H15 1E3 2001032800336 20010328 00336 SO 2001 3 28 CA000110026 1 19991216 A 7713 4708869002 CONTROLLER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA MANIFOLD GAUGE SURGES W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 869 (CAN) MANIFOLD GUAGE OBSERVED TO BE SURGING, DIFF. CONTROLLER REPLACED 1 L 7 2 3O 3 O A20SO E14EA 2001032800337 20010328 00337 EA 2001 3 28 CA000110027 2 19991221 A 7414 1068291018 MAGNETO PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 230 (CAN) MAGNETO FAILED TO PRODUCE SPARK AT START UP. 1 L 7 2 3O 3 O A20SO E14EA 2001032800339 20010328 00339 EU 2001 3 28 CA000110029 2 19991215 A 7250 EU33245 TURBINE WHEEL FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU LP TURBINE FAILED W C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 CA 17930 6526 (CAN) NR 2 LP TURBINE BLADE FAILURE. SEE PROJECT-CORRECTIVE ACTION 1999. CAA AWARE OF PROBLEMS AND R.R ESTABLISHED DIMEN SIONAL MEASUREMENTS AS INDICATOR FORSUSPECT BLADE IRREGULARITIES THE EFFECTIVENESS OF THE TOOL IS UNDER 2 L 7 2 4F 4 F RT A20EU E2EU 2001032800341 20010328 00341 SW 2001 3 28 CA000110034 1 19990530 A 2435 STARTER GEN BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 133 (CAN) DURING PRE-FLIGHT, THE PILOT FOUND PIECES OF BRUSHES & CLIPS IN ENGINE PAN. STARTER-GENERATOR WAS REPLACED AND SEN T BACK. 1 G 7 1 3U 3 U H2SW E4CE 2001032800342 20010328 00342 NE 2001 3 28 CA000110035 2 19991124 A 7321 180315 BEARING STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE FUEL CONTROL FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 2425 (CAN) PRE SB 60034-73-1 BEARING FOUND TO BE FAILING DURING ROUTINE BENCH CHECK. POST SB BEARING AVAILABLE WHICH HAS LARG ER RETAINER TYPE BALL BEARINGS. 2 H 7 2 4T 4 T A41EU E4EA 2001032800343 20010328 00343 EA 2001 3 28 CA000110037 1 19991216 A 5312 C2FS533 BULKHEAD DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14174 (CAN) THE BULKHEAD AT STN 228 WAS INSPECTED AS PER CF-98-38 AND SB 2/52. THE BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCA TIONS AND REPLACED 1 H 7 1 3R 3 R A806 5E1 2001032800344 20010328 00344 CE 2001 3 28 CA000110038 1 19991223 A 3231 08411065 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL MLG DOOR BROKEN W O OTHER J WARNING INDICATION AP APPROACH 1 CA 14521 (CAN) LEFT GEAR DOOR RETRACTION BELLCRANK FOUND BROKEN AFTER LANDING. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 2001032800346 20010328 00346 GL 2001 3 28 CA000110042 3 19991230 A 6114 830 STOP HARTZL HCB3TN5G SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL PROPELLER HUB FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1803 BV13150 (CAN) STOP LOCK FAILED TO RELEASE. THIS CAUSED CASTING AND GUIDE ROD TO BE DAMAGED FOR ONE BLADE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 2001032800372 20010328 00372 NE 2001 3 28 CA991209014 2 19991104 A 7322 324485318 FUEL CONTROL DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 17085 (CAN) AFTER TAKEOFF THE NR 2 ENGINE PARAMETERS BEGAN TO FLUCTUATE WITH SEVERE ASSOCIATED YAW. THE AIRCRAFT RETURNED FO R LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL UNIT. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032900006 20010329 00006 CE 2001 3 29 CA000201009 1 19991217 A 2823 1013890253 SHUTOFF VALVE BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA FUEL SYSTEM LEAKING W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) FUNCTIONAL CHECK OF FIREWALL SHUT-OFF VALVE DURING MAINTENANCE CHECK REVEALED THAT AFTER 2 SECONDS, FUEL PRESSURE LIGHT WENT OUT INDICATING FUEL BYPASSING THE VALVE. VALVE REPLACED. 1 L 7 2 3T 4 T RT 3A20 E4EA 2001032900007 20010329 00007 CE 2001 3 29 CA000201010 1 19991222 A 2823 1013890253 SHUTOFF VALVE BEECH 90 C90A 1152911 CE PWA PT6 PT6A21 52043 EA FUEL SYSTEM FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 4 (CAN) FUNCTION CHECKED OK IN HANGAR. FAILED 4.0 HRS. AIR TIME. VALVE REPLACED. 1 L 7 2 3T 4 T RT 3A20 E4EA 2001040200205 20010402 00205 WP 2001 4 2 CA000110041 2 19991228 A 7321 8070425 FUEL CONTROL SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313U 01514 WP ENGINE FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 4595 (CAN) HIGH WF AND HIGH ITT DURING START. FCU REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 2001050300205 20010503 00205 CE 2001 5 3 20010501CW018 1 19990312 A 7312 10585FSB08 FUEL HEATER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE CRACKED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 5632C 40 UC81 LOWER BOTTOM PLADE CRACKED AT EDGE WELD. LARGE QUANTITY OF OIL LOST. THIS IS THE SECOND FAILURE, CRACK, ON THIS FUEL HEATER IN 40.8 HOURS. SUSPECT IMPROPER/POOR REPAIR AND TEST PROCEDURES AT OVERHAUL BY VENDOR. 2 L 7 2 4T 4 T RT A24CE E4EA 2001071600003 20010716 00003 CE 2001 7 16 20010607CW007 1 19991123 A 2620 1015700216 SWITCH BEECH 1900 1900C 1154161 CE EXTINGUISH SYS DISCONNECTED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 45GL UC45 WHILE PERFORMING A NEW INSPECTION REQUIREMENT, FOUND BOTH SQUIB POWER SWITCHES DISLOCATED FROM MAIN ENGINE FIRE EXTINGUI SHER ANNUNCIATOR/ACTUATOR ASSEMBLY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION HAS BEEN FOUND ON HALF OF INSPECTED AIRCRAFT. SUGGEST CHANGE IN DESIGN OF THE ASSEMBLY FOR POSITIVE ATTACHMEN T OF SQUIB POWER SWITCH. NOTE: THE CONDITION FOUND ON THE TWO ASSEMBLIES WOULD PREVENT THE FLIGHT CREW FROM BEING ABLE TO DISCHARGE THE AFFECTED ENGINE FIRE BOTTLES AT ANY TIME. ALSO, THERE IS NO WAY FOR THE CREW TO PREFLIGHT THIS SYSTEM TO VERIFY THAT THE FIRE BOTTLE SQUIBS COULD BE BLOWN IF NEEDED. 2 L 7 2 4T RT A24CE 2001071600004 20010716 00004 CE 2001 7 16 20010607CW008 1 19991124 A 2620 1015700216 SWITCH BEECH 1900 1900C 1154161 CE LT ENGINE DISCONNECTED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 1563C UC20 WHILE PERFORMING OTHER MAINTENANCE, FOUND LEFT ENGINE SQUIB POWER SWITCH DISLOCATED FROM ENGINE FIRE EXTINGUISHER ANNUNC IATOR/ACTUATOR ASSEMBLY. FOUND SQUIB SWITCH MODULE NOT PROPERLY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION H AS BEEN FOUND ON HALF OF INSPECTED AIRCRAFT. SUGGEST A CHANGE IN DESIGN OF THE ASSEMBLY FOR POSITIVE ATTACHMENT OF SQUI B POWER SWITCH. NOTE: THE CONDITION FOUND ON THIS ASSEMBLY WOULD PREVENT THE FLIGHT CREW FROM BEING ABLE TO DISCHARGE THE AFFECTED ENGINE FIRE BOTTLE AT ANYTIME. ALSO, THERE IS NO WAY FOR THE CREW TO PREFLIGHT THIS SYSTEM TO VERIFY THAT THE FIRE BOTTLE SQUIB COULD IN FACT BE BLOWN IF NEEDED. 2 L 7 2 4T RT A24CE 2001072300088 20010723 00088 WP 2001 7 23 RRXA000308 1 19991210 A 5711 5615057510N SPAR CAP DOUG DC8 DC873F 302199F WP CENTER WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND RIGHT UPPER SPAR CAP CRACKED AT OUTBOARD AFT ATTACHMENT, DAMAGE EXCEEDED LIMITATIONS IA W DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SPAR CAP IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001080200126 20010802 00126 CE 2001 8 2 YAD2001F00000 1 19991119 A 2620 1015700216 SWITCH BEECH 1900 1900C 1154161 CE EXTINGUISHER DISCONNECTED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 41UE UC41 FOUND SQUIB POWER SWITCH DISLOCATED FROM MAIN ENG FIRE EXTING ANNUNCIATOR/ACTUATOR ASSY. SQUIB SWITCH MODULE NOT PROPER LY RETAINED BY TABS ON ANNUNCIATOR BODY. THIS CONDITION WAS FOUND ON TWO ASSEMBLIES OUT OF SIX CHECKED. NEW REPLACEMEN T ASSY FOUND TO BE MARGINALLY BETTER FOR RETENTION OF SQUIB SWITCH MODULE ON AFT END OF ANNUNCIATOR/ ACTUATOR ASSY. SUG GEST A CHANGE IN DESIGN OF ASSY FOR POSITIVE ATTACHMENT OF SQUIB POWER SWITCH. NOTE: THE CONDITION FOUND ON THE TWO AS SY WOULD PREVENT THE FLT CREW FROM BEING ABLE TO DISCHARGE THE AFFECTED ENGINE FIRE BOTTLES AT ANYTIME. ALSO, THERE IS NO WAY FOR THE CREW TO PREFLIGHT THIS SYSTEM TO VERIFY THAT THE FIRE BOTTLE SQUIBS COULD BE BLOWN IF NEEDED. 2 L 7 2 4T RT A24CE 2001081000082 20010810 00082 WP 2001 8 10 RRAX000001 1 19990701 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=880 TO Y=900. DAMAGE EXCEEDED LIMI TATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH EO-99-109. 2 L 7 4 4F RT 4A25 2001081300019 20010813 00019 WP 2001 8 13 RRXA000193 1 19991014 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANACE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN AT BETWEEN STA 980 TO 1120. DAMAGE EXCEEDED LIMITAT IONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-1. 2 L 7 4 4F RT 4A25 2001081300020 20010813 00020 WP 2001 8 13 RRXA000194 1 19991202 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN BETWEEN STA. 781 TO STA. 742 AND LONGERON 35 LEFT. D AMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR DOUBLER IAW FAA APPROVED DER ENGINEERING SCRTCH EO 99-186. 2 L 7 4 4F RT 4A25 2001081300032 20010813 00032 WP 2001 8 13 RRXA000233 1 19991119 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR JAM TORQUE BOX FROM STA. 280 TO STA. 360.DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED AIRCRAFT TO SERVICE IAW FAA APPROVED DER ENGINEERING SKETCH EO 99-186 WITH APPROVED 8110-3 DATED 11/16/99.(CORROSION DAMAGE REPORTED IN EWA CORROSION PROGRA M) 2 L 7 4 4F RT 4A25 2001081300034 20010813 00034 WP 2001 8 13 RRXA000236 1 19991202 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 36 BETWEEN STA 720 TO STA 781, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER & DOUBLER IAW BOEING M-72 00-99-10647 & M7200-99-10680. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2001081300035 20010813 00035 WP 2001 8 13 RRXA000237 1 19991209 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN AT LONGERON 36 AND STA 620, DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER & DOUBLER IAW FAA APPR OVED DER ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300037 20010813 00037 WP 2001 8 13 RRXA000238 1 19991122 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN STA 1440 TO STA 1460 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FI NGER DOUBLER IAW FAA DER APPROVED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300039 20010813 00039 WP 2001 8 13 RRXA000239 1 19991208 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 35 RIGHT AT STA 1200, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM . REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FILLER & DOUBLER IAW FAA DER APPRO VED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300041 20010813 00041 WP 2001 8 13 RRXA000240 1 19991208 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 34 RIGHT BETWEEN STA 1160 TO STA 1220, DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FILLER & DOUBLER IAW FAA DER APPROVED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300042 20010813 00042 WP 2001 8 13 RRXA000241 1 19991122 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 35 RIGHT BETWEEN STA 1150 TO STA 1160, DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLEND-OUT CORROSION DAMAGE TO A ACCEPTABLE LIMIT IAW FAA DER APPROVED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300043 20010813 00043 WP 2001 8 13 RRXA000242 1 19991126 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1060 AND LONGERON 36, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FILLER & DOUBLER IAW FAA DER AP PROVED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300044 20010813 00044 WP 2001 8 13 RRXA000243 1 19991108 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 32 RIGHT BETWEEN STA 1160 TO STA 1200, DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLEND-OUT DAMAGE TO A ACCEPTABLE LIMIT IAW FAA D ER APPROVED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300045 20010813 00045 WP 2001 8 13 RRXA000244 1 19991122 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1220 BETWEEN LONGERON 36 TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLEND-OUT DAMAGE TO A ACCEPTABLE LIMIT IAW FA A DER APPROVED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300046 20010813 00046 WP 2001 8 13 RRXA000245 1 19991207 A 5330 FINGER DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 1480 AND LONGERON 31 LEFT, DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. CUT AND REMOVED DAMAGED FINGERS IAW FAA DER APPR OVED ENGINEERING SKETCH 99-186. 2 L 7 4 4F RT 4A25 2001081300047 20010813 00047 WP 2001 8 13 RRXA000246 1 19991208 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 1060 AND LONGERON 36, DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT ANGLE IAW DC-8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2001081300049 20010813 00049 WP 2001 8 13 RRXA000247 1 19991123 A 5320 37558411 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 1220 BETWEEN LONGERONS 33 RIGHT TO 34 RIGHT, DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FIT TING IAW DC-8 SRM 53-2-0 FIGURE SHEET 1. 2 L 7 4 4F RT 4A25 2001081300050 20010813 00050 WP 2001 8 13 RRXA000248 1 19991127 A 5320 37558401 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 1220 AND LONGERON 32 RIGHT, DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE SHEET 1. 2 L 7 4 4F RT 4A25 2001081300051 20010813 00051 WP 2001 8 13 RRXA000249 1 19991123 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOASTAL BETWEEN STA 1380 TO STA 1400 AND XCW 48 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTION O F INTERCOASTAL IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001081300080 20010813 00080 WP 2001 8 13 RRXA000250 1 19991007 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER AFT CARGO DOOR JAMB (FRAME) AT STA 1540 AND LONGERON 33 RIGH T, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RE PAIR SPLICE IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001081300082 20010813 00082 WP 2001 8 13 RRXA000251 1 19991010 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 1540 BL-R 40 AND WL-15, DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT ANGLE I AW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001081300084 20010813 00084 WP 2001 8 13 RRXA000252 1 19991024 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING BETWEEN STA 1160 TO STA 1180 AND LONGERON 26 RIGHT, D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FI TTING IAW DC-8 SRM 53-2-0 FIGURE SHEET 1. 2 L 7 4 4F RT 4A25 2001081300085 20010813 00085 WP 2001 8 13 RRXA000253 1 19991112 A 5320 SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SPLICE FITTING TO LONGERON 26 RIGHT AT STA 450, DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 S RM 51-1-21. 2 L 7 4 4F RT 4A25 2001081300086 20010813 00086 WP 2001 8 13 RRXA000254 1 19991123 A 5320 46143971N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 70 AND LONGERON 31 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 5 3-4-1. 2 L 7 4 4F RT 4A25 2001081300087 20010813 00087 WP 2001 8 13 RRXA000255 1 19991120 A 5320 3755827501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER FORWARD CARGO DOOR JAMB FITTING AT STA 280 AND LONGERON 33 R IGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D NEW FITTING IAW DC-8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 2001081300089 20010813 00089 WP 2001 8 13 RRXA000256 1 19991121 A 5320 46143972N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 70 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMIT S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53 -4-1. 2 L 7 4 4F RT 4A25 2001081300090 20010813 00090 WP 2001 8 13 RRXA000257 1 19991120 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 35 RIGHT BETWEEN STA 55 TO STA 70, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2001081300092 20010813 00092 WP 2001 8 13 RRXA000258 1 19991118 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT AT STA 1680, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE MOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2001081300094 20010813 00094 WP 2001 8 13 RRXA000259 1 19991004 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT AT STA 25, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001081300098 20010813 00098 WP 2001 8 13 RRXA000264 1 19991006 A 5330 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO PRESSURE PANEL BETWEEN STA 880 TO STA 900 AND BL 69L, DAMAGE EXCEE DED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC -8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001081300100 20010813 00100 WP 2001 8 13 RRXA000265 1 19991013 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 880 TO STA 1100 AND BL 45R, DAMAGE EXCEED ED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC- 8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2001081300101 20010813 00101 WP 2001 8 13 RRXA000266 1 19991025 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 80 TO STA 100 AND LONGERON 13 RIGHT, DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-24. 2 L 7 4 4F RT 4A25 2001081300102 20010813 00102 WP 2001 8 13 RRXA000267 1 19990924 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 900 AND LONGERON 24 RIGHT, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 2001081300103 20010813 00103 WP 2001 8 13 RRXA000268 1 19990924 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 879 AND LONGERON 24 RIGHT, DAMAGE EXCEEDED LIMITATI ONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 2001081300108 20010813 00108 WP 2001 8 13 RRXA000269 1 19991119 A 5714 ANGLE DOUG DC8 DC873F 302199F WP CENTER WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL CENTER TANK ATTACHMENT ANGLE BETWEEN STA 710 TO STA 720 AN D BL 47R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001081300109 20010813 00109 WP 2001 8 13 RRXA000270 1 19990927 A 5340 BRACKET DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO 2 EACH BRACKETS AT STA -131 AND LONGERON 23 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 S RM 53-2-0. 2 L 7 4 4F RT 4A25 2001081300112 20010813 00112 WP 2001 8 13 RRXA000271 1 19990929 A 5322 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 60 AND LONGERON 6 LEFT, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME TIE IAW DC-8 SR M 53-2-2. 2 L 7 4 4F RT 4A25 2001081300117 20010813 00117 WP 2001 8 13 RRXA000272 1 19991008 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 55 TO STA 62 AND BL 48L, DAMAGE EXCEEDED L IMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL AND INSTALLED IA W DC-8 SRM 51-1-9. 2 L 7 4 4F RT 4A25 2001081300123 20010813 00123 WP 2001 8 13 RRXA000273 1 19991012 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN PANEL 262 BETWEEN STA 960 TO STA 1000 AND LEFT SIDE, DAMAGE E XCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2001081300125 20010813 00125 WP 2001 8 13 RRXA000274 1 19991002 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME STA 781 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001081300126 20010813 00126 WP 2001 8 13 RRXA000275 1 19991005 A 5340 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 680 AND BETWEEN LONGERONS 22 RIGHT TO 23 RI GHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED NEW ATTACHMENT ANGLE IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001081300127 20010813 00127 WP 2001 8 13 RRXA000276 1 19991007 A 5320 CHANNEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO U-CHANNEL AT STA 98 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW U-CHANNEL AND INSTALLED IAW DC-8 SRM 51- 1-4. 2 L 7 4 4F RT 4A25 2001081300131 20010813 00131 WP 2001 8 13 RRXA000277 1 19991008 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 260 TO STA 280 AND BETWEEN LONGERONS 32 LEF T TO 32 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL AND INSTALLED IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2001081300132 20010813 00132 WP 2001 8 13 RRXA000278 1 19991008 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 260 TO STA 280 AND BETWEEN LONGERONS 32 LEF T TO 32 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL AND INSTALLED IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 2001081300134 20010813 00134 WP 2001 8 13 RRXA000279 1 19991112 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 70 AND LONGERON 31 LEFT, DAMAGE EXCEEDED LIMITATION S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 53-4 -1. 2 L 7 4 4F RT 4A25 2001081300136 20010813 00136 WP 2001 8 13 RRXA000280 1 19991008 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 340 TO STA 360 AND BETWEEN LONGERONS 32 LEF T TO 32 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL. 2 L 7 4 4F RT 4A25 2001081300137 20010813 00137 WP 2001 8 13 RRXA000281 1 19991126 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOASTAL BETWEEN STA 520 TO STA 560 AND LONGERON 33 RIGHT, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW INTERCOASTAL A ND INSTALLED IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001081300138 20010813 00138 WP 2001 8 13 RRXA000282 1 19991116 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 27 RIGHT SPLICE FITTING AT STA 450, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FITTING AND INSTALLED IAW DC-8 S RM 51-1-4. 2 L 7 4 4F RT 4A25 2001081300139 20010813 00139 WP 2001 8 13 RRXA000283 1 19991129 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 1050 AND LONGERON 21 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4. 2 L 7 4 4F RT 4A25 2001081300141 20010813 00141 WP 2001 8 13 RRXA000284 1 19990930 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 400 BETWEEN LONGERON 22 LEFT TO 23 LEFT, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURN TO SERVICE, LIMITS ACCEPTABLE IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-186. 2 L 7 4 4F RT 4A25 2001081300146 20010813 00146 WP 2001 8 13 RRXA000287 1 19991230 A 5347 3657041 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 832AL 46063 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FE'S FORWARD SEAT TRACK. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 2001082700011 20010827 00011 WP 2001 8 27 RRXA003418 1 19991108 A 5320 BRACKET DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE "D" PIT GILL LINER SUPPORT AT STA 1380 TO 1400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, 51-1-4 AND 51-1-21. 2 L 7 4 4F RT 4A25 2001082700012 20010827 00012 WP 2001 8 27 RRXA003419 1 19991002 A 5320 STRAP DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR BEAMS METAL STRIP FOR GILL LINER AT STA 1390, DAMAGE EXCE EDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW D C-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001082700013 20010827 00013 WP 2001 8 27 RRXA003420 1 19991006 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT INBOARD FLAP FAIRING PLATE AT XRS 172, DAMAGE EXCEEDED LIMIT ATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57 -2-0, 51-1-4, 51-3-0 AND 51-1-21. 2 L 7 4 4F RT 4A25 2001082700014 20010827 00014 WP 2001 8 27 RRXA003421 1 19991005 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON END FITTINGS AT STA 70 L31R, DAMAGE EXCEEDED LIMITATIO NS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 2001082700015 20010827 00015 WP 2001 8 27 RRXA003422 1 19991008 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND SCREW HOLES INSIDE AND OUTSIDE OF THE RT WING FILLET PANEL 262B , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 AND 51-1-21. 2 L 7 4 4F RT 4A25 2001082700016 20010827 00016 WP 2001 8 27 RRXA003423 1 19991008 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH ANGLE IN FRONT OF WING LENS ON WING FILLET PANEL 261A AT STA 640-660 AND XCW 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. R ECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 AND 51-1-4. 2 L 7 4 4F RT 4A25 2001082700017 20010827 00017 WP 2001 8 27 RRXA003424 1 19991009 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WING FILLET PANEL 261E RUB STRIP AT STA 960-980 AND XCW 69, DAM AGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPA IR IAW DC-8 SRM 53-2-0, 51-1-4 AND 51-1-21. 2 L 7 4 4F RT 4A25 2001082700018 20010827 00018 WP 2001 8 27 RRXA003425 1 19991009 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON BACK SIDE OF WING FILLET PANEL 161F AT STA 880-920, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-24. 2 L 7 4 4F RT 4A25 2001082700019 20010827 00019 WP 2001 8 27 RRXA003426 1 19991009 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 605AL 46106 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WING FILLET PANEL 261C LT TOP FWD CORNER ATTACH ANGLE AT STA 96 0-990, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 5-1-8. FABRICATED AND INSTA LLED REPAIR IAW DC-8 SRM 51-1-21 AND 51-1-4. 2 L 7 4 4F RT 4A25 2001101500182 20011015 00182 WP 2001 10 15 9900431233 1 19991223 A 5315 SUPPORT FITTING DOUG DC10 DC1030 3023501 WP CORRODED A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 233NW 46640 During "H" check found corrosion on floor support from BS1903 to 2000, at LBL57. Repaired per EA12-171341. 2 L 7 3 4F A22WE 1999110500560 19991105 00560 EA 1999 11 5 CA990614078 1 19990610 A 5270 PSEU CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE PASSENGER DOOR FAILED W B I G A EMER. DESCENT CABIN DEPRESSURIZATION O2 MASK DEPLOYED UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) DOOR WARNING UNSAFE INDICATION. SUSPECT IMPROPER DOOR CLOSURE AT DEPARTURE. CONFIRMED WITH FEEDBACK FROM BOMBARD IER. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200501 19990212 00501 NM 1999 2 12 AT9900094 1 19990208 A 3397 WIRE BOEING 737 7372T4 1384492 NM CABIN LOOSE A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 467AT 22055 AFT PORTION OF AISLE WAY EMERGENCY EXIT LIGHTING WAS SNAGGED BY PASSENGER, WIRING IS LOOSE. REPAIRED LOOSE WIRING AS PE R MM 2050, OPERATIONAL CHECKED GOOD PER 33-53. 2 L 7 2 4F A16WE 1999022600538 19990226 00538 SO 1999 2 26 C2XA99IA063 1 19990118 A 3397 W182000924 WIRE EMB 120 EMB120RT SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING PREFLIGHT INSPECTION, TWO AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED T HE AFFECTED WIRES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999040200681 19990402 00681 WP 1999 4 2 AALA990178 1 19990214 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT AIR STAIRS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 234AA 49181 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRING TO THE AFT AIR STA IRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999040900237 19990409 00237 SO 1999 4 9 COMA9910052 1 19990404 A 3397 WIRE EMB 120 EMB120RT SO CABIN SHORTED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 179CA 120179 EMERGENCY LIGHTS CIRCUIT BREAKER TRIPS WHEN SYSTEM TESTED. REPAIRED SHORTED WIRING AT F/A LIGHT PANEL. 2 L 7 2 4T RT A31SO 1999070900140 19990709 00140 NM 1999 7 9 TWAA9909101 1 19990629 A 3397 WIRE BOEING 727 727231 1384079 NM EMERGENCY EXIT BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54335 20462 THE RIGHT WING AFT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. FOUND BROKEN WIRES IN A FLEXIBLE CONDUIT. REPLACED 2 WIRES FROM SPLICE POINT SP5 TO CONNECTOR D5024P, PINS 5 AND 6. CHECK-C 7-31-98. 2 L 7 3 4F A3WE 1999081200467 19990812 00467 NM 1999 8 12 CA990310062 1 19990220 A 5297 W125610922 WIRE BOEING 767 767375 1385217 NM OVERWING EXIT FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 39031 (CAN) DURING INSPECTION, FOUND WIRES SHORTED AND BROKEN AT RT OVERWING EXIT FORWARD HEATER BLANKET CONNECTOR, DUE TO PHY SICAL DOOR TO CONNECTOR INTERFERENCE. WIRES SEPARATED, BURNT AND MELTED, SURROUNDING AREA BLACKENED WITH SMOKE. REPAIR ED AS REQUIRED. 2 L 7 2 4F RT A1NM 1999102900119 19991029 00119 NM 1999 10 29 SWAA991731 1 19991018 A 2597 W268005 WIRE BOEING 737 7372H4 138448C NM GALLEY FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 082SW 22731 AIR TURNBACK, SMOKE SMELL IN AFT GALLEY. FOUND SHORT BETWEEN COFFEE MAKER POWER WIRE AND WORK LIGHT WIRE BEHIND AFT GAL LEY. REPAIRED WIRING PER MM. 2 L 7 2 4F A16WE 1999121000042 19991210 00042 SO 1999 12 10 COMA9910176 1 19991118 A 3231 WIRE EMB 120 EMB120RT 3260202 SO PROX SENSOR FAILED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 179CA 120179 TRIM FAIL WARNING DURING TAKEOFF. REPAIRED PROX SENSOR WIRE SPLICE AT ELEVATOR TRIM. 2 L 7 2 4T RT A31SO 1999121800365 19991218 00365 NM 1999 12 18 DL72W992684 1 19991208 A 3397 WIRE BACC63CC123 BOEING 727 727247 138408F NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 22108 AFT AISLE EXIT LIGHT INOP. FOUND BROKEN WIRE AT CANNON PLUG. REMOVED AND REPLACED CANNON PLUG. 2 L 7 3 4F A3WE 1999123100413 19991231 00413 WP 1999 12 31 AALA991767 1 19991122 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 575AM 53152 DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRING IN TAIL COMPARTM ENT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999112500233 19991125 00233 WP 1999 11 25 TWAA9915801 1 19991119 A 2420 WIRE DOUG DC9 DC982 3022082 WP RT GENERATOR DAMAGED A TWAA A UNSCHED LANDING B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CL CLIMB 1 CE 05 915TW 49186 DURING CLIMB, THE RT GENERATOR FAILED WITH AC CROSSTIE LOCKOUT LIGHT ON. CREW NOTICED ELECTRICAL ODOR IN COCKPIT. FLT RETURNED TO SEA. THE RT GENERATOR FEEDER CABLE WAS FOUND DAMAGED AT STA 237. ISOLATED DAMAGED WIRING AND MAINTENANCE F ERRIED THE AIRCRAFT TO LAX FOR CORRECTIONS. CHECK-C 7-23-99 MCI. 2 L 7 2 4F A6WE 1999090300575 19990903 00575 EU 1999 9 3 UF6A990563 1 19990531 A 2750 3F12844 CONTROL CABLE BAG ATP ATP EU LT TE FLAP OUT OF ADJ A UF6A O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 851AW 2020 ORD - FLT 5731 - FLAP CWP ILLUMINATED WITH FLAPS SET AT 7 DEGREES AFTER TAKEOFF. MAINTENANCE ADJUSTED FLAP CABLE ASSEMB LY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1999012200131 19990122 00131 SO 1999 1 22 LR7A9901 1 19990108 A 5230 LS5974H271200 CABLE LKHEED 382 382G 526414U SO CARGO DOOR OUT OF ADJ A LR7A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 AL 03 401LC 4606 REJECTED T/O, DOOR WARNING LIGHT CAME ON DURING ROLL, ADJUSTED CARGO DOOR DOWN LOCK CABLES IAW SMP 58152-30 PAGE 206. 2 H 7 4 4T A1SO 1999121800217 19991218 00217 EU 1999 12 18 99ZZZX4554 1 19991130 A 7603 285003 CONTROL CABLE STBROS SD3 SD330 8100602 EU POWER LEVER SEIZED A DATA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 GL 13 334AC SH3029 UPON REACHING CRUISING ALTITUDE FROM PLB, THE THROTTLES ON THE RIGHT SIDE WOULD NOT ADVANCE OR RETARD IN-FLIGHT. THE CA PTAIN SHUT DOWN THE NR 2 ENGINE AND LANDED UNEVENTFULLY IN PLB. 2 H 7 2 4T A41EU 1999031901115 19990319 01115 CE 1999 3 19 99ZZZX932 1 19990118 A 2730 5052443931 CONTROL CABLE BEECH 90 E90 1152914 CE ELEVATOR BROKEN A L A GNLA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 01 16NM 10536 LW62 DURING CRUISE, A LOUD POP WAS HEARD, THE CONTROL COLUMN FELL AGAINST THE FWD STOP AND ACFT PITCHED UP. PILOT FOUND HE H AD UP ELEV CONTROL ONLY. EMERG DECLARED AND ACFT SAFELY LANDED USING ENG POWER AND TRIM. INVEST FOUND THE DOWN ELEVATO R CABLE HAD CHAFED THROUGH AN ELEC WIRE BENEATH THE PILOT'S SEAT AND CABLE WAS BURNED THROUGH. 1 L 7 2 3T 3A20 1999022600361 19990226 00361 NM 1999 2 26 ASAA9940007 1 19990118 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 PDX - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING AND LI GHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999042300824 19990423 00824 NM 1999 4 23 ASAA9940064 1 19990311 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 PDX - DURING MAINTENANCE CHECK, THE FORWARD TWO TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPER ATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999061800564 19990618 00564 NM 1999 6 18 ASAA9940103 1 19990503 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 756AS 25097 SNA - FLT 389 - BOTH FORWARD RED EMERGENCY EXI TFLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHT S OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999090300720 19990903 00720 NM 1999 9 3 ASAA9940138 1 19990722 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 778AS 25110 PDX - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED L IGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999100100240 19991001 00240 EA 1999 10 1 COMA9960542 1 19990922 A 5270 WIRE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 PAX DOOR OUTER HANDLE CAUTION MESSAGE, NEXT TURNED TO PAX DOOR WARNING, THEN BACK TO CAUTION. REPAIRED BROKEN WIRING ON PAX DOOR. 2 L 7 2 4F RT A21EA 2002070800063 20020708 00063 GL 2002 7 8 ALG2002F00045 2 19990720 A 7250 6898782 TURBINE WHEEL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DAMAGED E ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 107AL 1027 S772 CAE835216 UPON DISASSEMBLY OF TURBINE FOR EVALUATION DUE TO ENGINE QUITTING DURING OPERATION. UPON INSPECTION OF ALL PARTS NR 2 W HEEL HAD ONE BLADE MISSING. PERFORM INSPECTION OF WHEELS UPON ASSEMBLY AT MANUFACTURER FOR POSSIBLE IMPERFECTIONS. 1 G 7 2 3U 3 U H3EU E4CE 2003010300014 20030103 00014 SW 2003 1 3 CZMA082748 1 19990628 A 6520 212040004009 GEARBOX BELL 412 412 1182202 SW TAIL ROTOR MAKING METAL E CZMA K NONE O OTHER IN INSP/MAINT 1 SO 03 911BE 4857 36018 EXCEESIVE METAL DEPOSITS ON CHIP DETECTOR REPLACED GEARBOX WITH NEW PART FROM MANUFACTURER 1 G 7 2 4U H4SW 2003010300016 20030103 00016 SW 2003 1 3 CZMA082750 1 19990713 A 6220 412010427101 BEARING BELL 412 412 1182202 SW ROTOR HEAD DEFECTIVE E CZMA K NONE O OTHER IN INSP/MAINT 1 SO 03 911BE 26 A360 36018 MAIN ROTOR HEAD BEARINGS BECAME UNSTAKED FROM DRIVE LINK REPLACED BEARINGS AS PER BHT CR & O V1 1 G 7 2 4U H4SW 2004042600046 20040426 00046 SO 2004 4 26 SWIA971108 1 19990905 A 3010 BOOT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT WING DE ICE INOPERATIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 RIGHT INBOARD WING DE-ICE BOOT INOP. RETURNED TO SLC. FOUND SPLIT IN LEFT INBOARD DE-ICE BOOT. REMOVED BOOT, INSTALLE D NEW DE-ICER ON LEFT INBOARD LEADING EDGE. 2 L 7 2 4T 4 T RT A31SO E20NE 1999121800223 19991218 00223 1999 12 18 99ZZZX4560 4 19991202 A 6122 430202403 GOVERNOR BENDIX PROPELLER MISMANUFACTURED A NXTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 19 37636 AT INSTALLATION, GOVERNOR WOULD NOT PRODUCE PARTIAL POWER TOPPING. REMOVED AND HAND CARRIED TO ALLIED SIGNAL BENDIX FOR INVESTIGATION. UPON TESTING AND DISASSEMBLY, VERIFIED INCORRECT SIZED PG ORIFACE. UNIT DID NOT MEET SPECS ON BENCH. A LLIED SIGNAL INVESTIGATION TO CORRECT ISSUE. 1999102900325 19991029 00325 EA 1999 10 29 CA990927022 2 19990803 A 8510 89P102569 SUPPORT WRIGHT 982C9HE2 WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 834 BL516162 BL516162 516162 (CAN) CRACK AT BASE OF THE INTAKE MANIFOLD ATTACH SUPPORT BRACKET. 4 R E259 6 C P8879 1999090300313 19990903 00313 1999 9 3 CA990804003 1 19990721 A 7600 202255053 TMS ACTUATOR LYC ALF502 ALF502R5 41580 NE ENGINE STUCK W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA LF05465A (CAN) ENGINE WOULD NOT SHUT DOWN WITH POWER LEVER. ENGINE REQUIRED TO BE SHUT DOWN WITH OVERSPEED PROCEDURE. TMS ACTUA TOR FOUND IN FULLY EXTENDED POSITION. TMS ACTUATOR REPLACED. 4 F E6NE 1999070200076 19990702 00076 WP 1999 7 2 99ZZZX2461 2 19990411 A 7320 1390136 DIAPHRAGM WOODWARD 89356111 GARRTT TPE331 TPE331* 01514 WP ENGINE WORN B K NONE O OTHER IN INSP/MAINT 1 CE 05 1294294 FUEL CONTROL INSTALLED ON AGRICULTURAL AIRCRAFT INVOLVED IN INCIDENT. 3 T E2WE 1999041700538 19990417 00538 1999 4 17 TWRA9906 4 19990224 A 2564 23829109 LIFE RAFT AIRCRUISERS CABIN MALFUNCTIONED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 7583375 DURING WET DITCHING TRAINING CLASS 9901, THE LIFE RAFT USED DID NOT INFLATE PROPERLY, WHEN THE MANUAL HAND WAS PULLED TH E UPPER CANNISTER DISCHARGED INTO THE AIR DUE TO RUPTURED PRESSURE HOSE. THE SECOND CANNISTER INFLATION CABLE WAS TWIST ED AND PREVENTED INFLATION. INFLATION WAS ACCOMPLISHED BY PULLING ON THE CABLE DRILL WAS ACCOMPLISHED WITH ONE BUOYANCY TUBE. LIFE RAFT WAS SENT TO THE VENDOR. (M) 1999052800096 19990528 00096 NE 1999 5 28 CA990420025 2 19990329 A 7230 724723 COMPRESSOR PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED W A UNSCHED LANDING O OTHER TO TAKEOFF 1 CA P724723 (CAN) ON CLIMB-OUT, AFTER TAKEOFF, NR 1 ENGINE FAILED. LOUD BANG WAS HEARD WITH VIBRATIONS, ALL ENGINE PARAMETERS DROPP ED TO ZERO WITH EXHAUST GAS TEMPERATURE IN THE RED EXCEEDING 740 DEGREES CELSIUS. 4 F E24NE 1999111900637 19991119 00637 1999 11 19 VTZA9909428 1 19990618 A 3234 750006000 VALVE NLG FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 FLT 7797 - IAD-RDU - DURING CLIMB AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOUD NOISE COMING FROM GEAR WELL. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NLG SELECTOR VALVE. MAINTE NANCE PERFORMED GEAR SWINGS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 1999070200075 19990702 00075 WP 1999 7 2 99ZZZX2460 2 19990611 A 7320 180188 BEARING GARRTT TPE331 TPE331* 01514 WP FCU WORN B K NONE O OTHER IN INSP/MAINT 1 CE 05 3000 BEARING WORN ON FCU. 3 T E2WE 1999090300274 19990903 00274 1999 9 3 CA990707017 1 19990617 A 3211 65841061 NUT 65841061 MLG SUPPORT CHIPPED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN) REAR MLG SUPPORT NUT NOT AS PER MANUFACTURER'S SPECIFICATIONS. HARDNESS, FINISH AND THREAD CHIPPING. 1999052800094 19990528 00094 NE 1999 5 28 CA990412031 2 19990328 A 7250 TURBINE LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE SEIZED W E C ENGINE SHUTDOWN ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA 21392 3056 LF05485A (CAN) ON TAKEOFF, THE CREW NOTICED LOSS OF N2 INDICATION ON NR 2 ENGINE AND ABORTED TAKEOFF. THE ENGINE WAS REMOVED AND PRELIMINARY INSPECTION REVEALED N2 LOCKUP, INDICATIVE OF HP TURBINE FAILURE. HOT METALLIC FRAGMENTS MIGRATED AFT AND E MBEDDED IN THE LP STAGE, WHEN AFTER COOLING FUSED BETWEEN THE TURBINE BLADE TIP SHROUDS PREVENTING N1 ROTATION. THE ENG INE WILL BE TORN DOWN FOR CAUSE AND A FURTHER REPORT WILL FOLLOW. 4 F E6NE 1999070200077 19990702 00077 WP 1999 7 2 99ZZZX2462 2 19990615 A 7321 1410126 BEARING WOODWARD 86919924 GARRTT TPE331 TPE331* 01514 WP FCU WORN B K NONE O OTHER IN INSP/MAINT 1 CE 05 294 851636 BEARING SUPPORTING THE OVERSPEED FUEL VALVE HAD WORN CREATING METAL CONTAMINATION. 3 T E2WE 1999081200363 19990812 00363 1999 8 12 CA990301009 1 19990223 A 2731 03102971 BEARING 03102971 ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ONE BEARING IN BATCH FOUND CRACKED. THIS BEARING IS USED IN THE ELEVATOR SYSTEM AND WAS A REPLACEMENT PART. 1999090300305 19990903 00305 1999 9 3 CA990728018 1 19990707 A 7920 LINE GE CF6 CF680C2B6 NE OIL SYSTEM LOOSE W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 702384 702384 (CAN) NR 2 ENGINE OIL QUANTITY INDICATED ZERO AT CRUISE. OIL PRESSURE REDUCED TO 46 PSI. ENGINE THRUST REDUCED TO IDLE , FLIGHT DIVERTED. OIL LEAK ISOLATED TO LINE AT OIL PRESSURE TRANSMITTER. LINE TIGHTENED, LEAK CHECK CARRIED OUT. SYS TEM SERVICEABLE. 4 F E13NE 1999100100639 19991001 00639 1999 10 1 99ZZZX3736 1 19990819 A 3246 WHEEL PARKERHANFIN MLG CRACKED A LABA K NONE O OTHER IN INSP/MAINT 1 AL 05 TOTAL TIME NOT KNOWN. THIS IS A TYPICAL FAILURE POINT/AREA ON A CLEVELAND WHEEL HALF. 1999100100640 19991001 00640 EA 1999 10 1 99ZZZX3737 2 19990819 A 7414 M3333 IMPULSE COUPLING SLICK LYC O540 IO540* 41532 EA MAGNETO WORN A LABA K NONE O OTHER IN INSP/MAINT 1 AL 05 800 PIVOT PINS AND FLYWEIGHTS MADE OUT OF MATERIAL THAT IS TOO SOFT AND/OR ENGINE DOES NOT PROVIDE LUBRICATION TO IMPULSE. 3 O 1E4 1999052800108 19990528 00108 NE 1999 5 28 CA990514012 2 19990426 A 7200 ENGINE PWA JT9 JT9D7R4D 52054 NE NR 2 FAILED W C ABORTED TAKEOFF Z SIGNIFICANT FAILURE REPORT TO TAKEOFF 1 CA P707553 (CAN) DURING ENGINE SPOOL UP ON TAKEOFF, TWO LOUD BANGS WERE HEARD WITH A NOTICEABLE PULL TO THE RIGHT. TAKEOFF WAS ABO RTED. INVESTIGATION FOUND THE NR 2 ENGINE HAD FAILED. PRELIMINARY REPORT. 4 F E3NE 1999051400549 19990514 00549 1999 5 14 99ZZZM281 1 19990331 A 3244 922C86T1 TIRE NLG OUT OF BALANCE A OIZA K NONE O OTHER NR NOT REPORTED 1 WP 19 A/C NOSE TIRES MANUFACTURED GOODYEAR TIRES WITH THE FOLLOWING SERIAL NUMBERS HAVE HAD THE INTERNAL BALANCE PATCHES COME LOOSE WHILE THE TIRES WERE IN SERVICE, 7302T402, 7302T403, 7203T406, 7203T415 AND 7302T421. SERIAL NR 7203T423, 7203T42 4 AND 7302T28 AND BEING REMOVED FROM SERVICE AS QUICKLY AS SPARE NOSE WHEELS CAN BE BUILT UP. ACCORDING TO GOODYEAR TIR ES, THE TIRES WERE PRODUCED IN THAILAND. TIRES HAVE BEEN IN SERVICE ANYWHERE FROM 3 CYCLES TO OVER 128 CYCLES BEFORE LO OSING THE INTERNAL BALANCE PATCHES. DISCREPANCIES HAVE RANGED FROM VIBRATION NOTICED ON TAKEOFF, TO SEVERE VIBRATION AT V1 FROM NOSE GEAR. (M) 1999090300334 19990903 00334 NE 1999 9 3 CA990812038 2 19990723 A 7200 ENGINE PWA JT9 JT9D7R4D 52054 NE LEFT FAILED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA P709673 (CAN) ENGINE FAILED TO ACCELERATE ON LEVEL OFF AFTER DESCENT. FUEL CONTROL AND HP PUMP REPLACED. NOTE: LT ENGINE MSG ON IECAS, LT ENG SURGE DETECT. 4 F E3NE 1999081200664 19990812 00664 NE 1999 8 12 CA990330006 2 19990309 A 7230 SEAL LYC ALF502 ALF502R5 41580 NE NR 1 ENGINE LEAKING W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 20339 1014 LF05543A (CAN) FLIGHT CREW REPORTED FUMES IN THE CABIN DURING FLIGHT. (AIRCRAFT OPERATING ON NR 1 PACK - NR 2 PACK INOPERATIVE O N MEL.) AIRCRAFT RETURNED WITH PACKS OFF. POST-FLIGHT INSPECTION FOUND NR 4 ENGINE NR 1 SEAL LEAKING, CONTAMINATING TH E CABIN AIR SUPPLY. NR 4 ENGINE WAS REPLACED. 4 F E6NE 1999091700551 19990917 00551 EA 1999 9 17 99ZZZX3450 2 19990816 A 7414 1052947 MAGNET BENDIX LYC O540 IO540V4A5 41532 EA MAGNETO CRACKED D S K NONE O OTHER IN INSP/MAINT 1 WP 25 A259111ER ROTATING MAGNET PN 10-52947 HAS CRACKS, 2 EACH, BETWEEN DRIVE END OF CASTING AND MAGNETIC LAMINENTS ON BOTH POLES ONE OF WHICH IS APPROXIMATELY 75 PERCENT THROUGH MATERIAL. COMPONENT P/N S6LN-20410-163050-9. 3 O 1E4 1999102900374 19991029 00374 GL 1999 10 29 CA991007040 2 19990916 A 7313 6890917 NOZZLE ALLSN ALLSN 250C 250C20B 03013 GL FUEL SYSTEM CRACKED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA AG19561 (CAN) FUEL NOZZEL OUTER AIR SHROUD CRACKED WHEN RECEIVED FROM VENDOR. 3 U E4CE 1999043000666 19990430 00666 NE 1999 4 30 99ZZZX1829 2 19990412 A 7250 404029001 BLADE LYC LTS101 LTS101650B1 41560 NE PT ROTOR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 1660 SC14130 LE45143 FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TC: 4,795.7 . 3 U E5NE 1999082000232 19990820 00232 NE 1999 8 20 CA990719002 2 19990616 A 7200 ENGINE GE 37C300353G01 GE CT58 CT581401 30011 NE ENGINE BAY FAILED W A UNSCHED LANDING X ENGINE FLAMEOUT HO HOVERING 1 CA 2783 2829 280225A (CAN) ENGINE FLAMED OUT WHILE HOVERING. ROTORCRAFT RETURNED TO MAINTENANCE BASE USING REMAINING ENGINE. ENGINE CHANGED . 4 U 1E3